20081028 NM 2008 10 28 DHL2008F00033 120040918A2612 FIRE LOOP BOEING727 7272B7 138407LNM MLG WW MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 GL05770AT 21953 IN CRUISE FLIGHT, HAD 3 INSTANCES OF MOMENTARY FIRE WARNING BELL WITH A FLICKER OF WHEEL WELL FIRE WARNING LIGHT. PERFORMED CONTINUITY TEST OF ENGINE AND WHEEL WELL FIRE LOOPS, TEST OK. INSPECTED WHEEL WELL WIRING AND FIRELOOPS, NO DEFECTS FOUND. COULD NOT DUPLICATE PROBLEM. REPLACED FIRE AND OVERHEAT ASSY UNIT AS PRECAUTIONARY IAW B727 MM 26-12-0, OPS CHECK OK. ACFT WAS GROUNDED. (K) 2L73 4F A3WE 20081028 NM 2008 10 28 KNN2008F00003 120040918A5340 STRINGER CLIP BOEING737 737291 138448WNM FUSELAGE DAMAGED A KNNAO OTHER O OTHER NRNOT REPORTED 1 WP25977UA 21508 WHILE COMPLYING WITH AD 93-08-04 AND SB 737-53-1268. DURING THE CURRENT C-CHECK. WE FOUND STRINGER CLIP THAT FAILED NDT INSPECTION. THE STRINGER CLIP WAS REPLACED IAW SB-737-53-1268. ALL SUPPLEMENTAL INSPECTIONS WERE ALSO COMPLIED WITH IAW THE SB. (K) 2L72 4F A16WE 20081028 EU 2008 10 28 VY12008F00000 120041109A6520350A33020004 GEARBOX SNIAS 350 AS350B 8680801EU TAIL ROTOR DESTROYED L VY1RK NONE O OTHER ININSP/MAINT 1 SW19655TV 1590 PERFORMED A PRELIMINARY REVIEW OF THE SERVICE HISTORY OF THE GEARBOX THAT WAS RECEIVED FOR OVERHAUL. IT WAS DETERMINED THAT THE GEARBOX WAS INVOLVED IN AN ACCIDENT. BASED ON THE ACCIDENT THAT OCCURRED ON 9 NOV 2004, MFG HAS DETERMINED THAT ALL DYNAMIC COMPONENTS INSTALLED ON THIS ACFT AT THE TIME OF THE CRASH ARE NOT TO BE RETURNED TO SERVICE FOR ANY REASON. THE LOG CARD RECEIVED WITH THE GEARBOX DID NOT INDICATE THAT IT WAS INVOLVED IN AN ACCIDENT. RECOMMENDS THAT THIS COMPONENT AND ALL INTERNAL SUBCOMPONENTS BE MULATED IN A MANNER TO PREVENT THEM FROM BEING INTRODUCED INTO SERVICE FOR INSTALLATION ON A TYPE CERTIFICATED PRODUCT. AE HAS PERMANENTLY IDENTIFIED THE GEARBOX AS SCRAP. 1G71 3U H9EU 20040809000752004080900075EA 2004 8 9 COMA0470059 120040726A32406007300 SENSOR CNDAIRCL600 CL6002C10 1390015EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01354CA 10064 FLT 5524 BRAKE OVERHEAT WARNING. REPLACED THE RT OUTBOARD BRAKE TEMP SENSOR. 2L72 4F RTA21EA 20040809000552004080900055EU 2004 8 9 ASOA04316 120040413A5320S5367800821602 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE ZEE FLOOR SUPPORT ON THE RIGHT SIDE FROM FRAME 39 TO FRAME 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ZEE FLOOR SUPPORT ON THE RT SIDE FROM FRAME 39 TO FRAME 41 IAW SRM 51-25-01. (M) 2H72 4T RT 20010111041292001011104129WP 2001 1 11 SPAA0000035 120040106A2700369A7304 BRACKET HUGHES369 369D 4470706WP ALLSN 250C 250C* GL FLIGHT CONTROLS DAMAGED B EOORK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03511SB11913 1090592D FOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SORT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (K) (ALO3200411231) 1G71 3U3 U H3WE E4CE 20041109000172004110900017WP 2004 11 9 ABXA040358 120041018A55305912101501 BRACKET DOUG DC9 DC931 3022065WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 RUDDER UPPER HINGE BRACKET CRACKED AT RIGHT MOUNT HOLE. REMOVED AND REPLACED UPPER HINGE BRACKET IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20040219000012004021900001EA 2004 2 19 COMA0460132 120040206A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01938CA 7046 FLIGHT 5806 WING ANTI ICE CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040219000022004021900002EA 2004 2 19 COMA0460131 120040206A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01938CA 7046 FLIGHT 5898 RIGHT WING ANTI ICE CAUTION. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040219000142004021900014NM 2004 2 19 UPS04441860 120040121A5313BAC14981477075 STRINGER BOEING747 747123 1384873NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040219000152004021900015NM 2004 2 19 UPS04441861 120040123A5320BAC1509100312 CHANNEL BOEING747 747123 1384873NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D- BS 2320 TO 2350 LBL 40 HAT SECTION FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED PER SRM 51-10-01 PG 8 & P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM 53-10-17. 2L74 4F A20WE 20040219000172004021900017NM 2004 2 19 UPS04441863 120040127A5315HXC108662 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- RT STA 2240 FLOORBEAM LOWER SECTION FOUND CORRODED IN BETWEEN RBL 6 AND RBL 40. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 LIMITS. STA 2240 RBL 30 FLOORBEAM LOWER SECTION REPAIRED AS PER SRM 51-40-04 FIG 2. CIC APPLIED IAW CPM53-10-17. 2L74 4F A20WE 20040219000192004021900019WP 2004 2 19 UPS04841854 120040201A53403758570U2 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LONGERON 35R INTERCOSTAL TO FRAME ATTACH FITTING AT STA 1230 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570 AND SRM 51-1-20D. 2L74 4F RT4A25 20040219000272004021900027NM 2004 2 19 04036405 120040205A5311 FRAME DORNERDO32 DO328300 NM FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING HEAVY INSPECTION FRAME 35 WAS FOUND WITH LEVEL 2 CORROSION. THE FRAME WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF MAINTENANCE CHECK. 2H72 4T RTA55NM 20040219000292004021900029SO 2004 2 19 C2XA04SH067 120040216A531514522461011 DOUBLER EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000302004021900030SO 2004 2 19 C2XA04SH068 120040216A531514522461011 DOUBLER EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE RT FLOORBEAM DOUBLER CAP AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER CAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000372004021900037SO 2004 2 19 C2XA04SH070 120040216A531514522226003 BUTTSTRAP EMB 135 EMB135ER 3260203SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE LAVATORY BETWEEN FRAMES 55 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000382004021900038SO 2004 2 19 C2XA04SH069 120040216A532014522460015 BUTTSTRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000422004021900042EU 2004 2 19 MALA040186 120040205A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, LT FUSELAGE AFT OF NR 2 ICE SHIELD HAS NUMEROUS DENTS. FABRICATED AND INSTALLED 2 EACH EXTERNAL DOUBLERS IAW MESABA EO NR S53009. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2L72 4T RTA52EU 20040219000442004021900044EU 2004 2 19 MALA040180 120040207A2130 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU CABIN PRESS CONTMALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15106XJ 340A106 AFTER TAKEOFF, TURNED BLEED VALVES TO OPEN, AND HAD A RAPID RATE OFF DECELERATION IN CABIN RATE AND CABIN ALTITUDE. AIR RETURN TO CWA. MAINTENANCE RESET CABIN PRESSURE CONTROL CIRCUIT BREAKER. PRESSURIZATION SYSTEM OPS CHECK GOOD. VISUALLY INSPECTED WIRING BEHIND LT C/B PANEL. NO DEFECTS NOTED. 2L72 4T RTA52EU 20040219000462004021900046EU 2004 2 19 MALA040179 120040207A2612 CONNECTOR SAAB SF340 340B 7860101EU LT NACELLE CONTAMINATED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15441XJ 340B441 IN CRUISE FLT THE LT FIRE DETECT FAIL CWP CAUTION LIGHT REPEATEDLY CYCLED ON & OFF. LIGHT WOULD GO OUT FOR 3 SECONDS AND COME BACK ON, QRH COMPLETE. AIR RETURN TO MQT. MAINTENANCE FOUND CONTAMINATED CONNECTOR AT ENGINE NACELLE, CLEANED & SAFTETIED. OPS CHECK GOOD. SEE CONTINUATION CARDS NR 062320 & NR 062319 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20040219000502004021900050WP 2004 2 19 04FDEA00405 120040213A5753 SKIN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD FLAP VANE, NR 3 FLAP VANE ATTACH HORN HAS TWO CORRODED/PITTED HOLES. REPLACED PER M/M 27-50-03-2 AND TORQUED PER M/M 20-50-20. 2L73 4F A22WE 20040219000512004021900051WP 2004 2 19 04FDEA00404 120040213A5753 SKIN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD FLAP VANE NR 2 FLAP VANE ATTACH HORN HAS 2 CORRODED/PITTED HOLES. REPAIRED PER EA 8-5750-68462. 2L73 4F A22WE 20040219000522004021900052WP 2004 2 19 04FDEA00403 120040213A5753 HORN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD FLAP VANE NR 1 FLAP VANE ATTACH HORN HAS PITTED AFT HOLE. 2L73 4F A22WE 20040219000552004021900055NM 2004 2 19 SWAA040406 120040208A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 2 TO RBL 2. REPAIRED WEB PER ACO. 2L72 4F RTA16WE 20040219000602004021900060 2004 2 19 SWAA040236 420040123A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000632004021900063NM 2004 2 19 SWAA040238 120040126A5315BAC1505 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED 5Y CHECK, FOUND CORROSION ON FLOORBEAMS AT BS 772, LBL 17.5 TO LBL 3 AND BS 727, RBL 3 TO LBL 3. REPAIRED FLOORBEAMS PER EA. 2L72 4F RTA16WE 20040219000712004021900071NM 2004 2 19 2004UALA00096 120040202A3350 BATTERY PACK BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29788UA 26942 EMERGENCY EXIT CEILING LIGHTS INOP FIRST ROW COACH TO DOOR 3L. REPLACED BATTERY PACK. 2L72 4F4 FRTT0001SE E46NE 20040219000812004021900081NM 2004 2 19 SWAA040356 120040204A53126546568 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, RBL 1. REPAIRED WEB PER AD. 2L72 4F A16WE 20040219000822004021900082NE 2004 2 19 DXTA200400242 220040212A7200 ENGINE BRAERO1000 HAWKER1000 7450005EU PWA 306 PW306B NE NR 1 SHUTDOWN E DXTAF ACTIVATE FIRE EXT. J WARNING INDICATION LDLANDING 1 GL07548QS 259048 PCE305072 ON LANDING WHILE PULLING BACK ON THE THRUST REVERSER LEVERS, NR 1 ENGINE WENT TO SHUTDOWN AND NR 1 ENGINE FIRE LIGHT ILLUMINATED. PULLED NR 1 ENGINE FIRE BOTTLE, AIRCRAFT ARRIVED AT GATE WITHOUT FURTHER INCIDENTS. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA3EU E35NE 20040219000882004021900088NM 2004 2 19 PCAA0402163 120040203A3150V319 SWITCH DHAV DHC8 DHC8102 2809003NM LT CONTROL LEVERSTICKING A PCAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA13839EX 226 FLIGHT 3755 FROM SYRACUSE HAD TO RETURN TO GATE DUE TO RECEIVING THE TAKEOFF WARNING HORN WITH THE AIRCRAFT PROPERLY CONFIGURED FOR TAKEOFF. MAINTENANCE FOUND THE LT CONDITION LEVER SWITCH 3151-S3 TO BE STICKING. MAINTENANCE REPLACED SWITCH AND OPERATIONAL CHECKED SYSTEM, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040219000922004021900092NM 2004 2 19 SWAA040358 120040204A555265C25798 FITTING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE FITTING PER SRM. 2L72 4F RTA16WE 20040219000962004021900096NM 2004 2 19 SWAA040362 120040204A53106546581 DOOR FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FRAME CUTOUT CRACKED AT DOOR STOP. REPAIRED R1 DOOR FRAME CUTOUT PER SRM. 2L72 4F RTA16WE 20040219000972004021900097EU 2004 2 19 F3LA200400005 120040204A5610NP1653116 WINDSHIELD AIRBUSA318 A318111 3940019EU COCKPIT CRACKED A F3LAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03801FR 1939 AIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S WINDSHIELD PER 56-11-11-000-001 AND 56-11-11-400-001. PERFORMED TEST OF WINDOW HEAT AND DEFOGGING PER 30-42-00-710-001 AND CHECKED OKAY. 2L72 4F RT 20040219000992004021900099NM 2004 2 19 SWAA040340 120040203A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 980, STRINGER 23 L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001012004021900101NM 2004 2 19 SWAA040342 120040203A53116546546 FRAME BOEING737 7372T4 1384492NM WINDOW BELT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED SPV, FOUND RT SIDE OF FUSELAGE WINDOW BELT FRAMES CRACKED AT BS 842, BS 822, BS 365, BS 385. REPAIRED WINDOW BELT FRAMES PER EA. 2L72 4F A16WE 20040219001022004021900102NM 2004 2 19 SWAA040343 120040203A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SPV, FOUND 2 EACH CRACKS ON WEB AT BS 178, WL 217, LBL 11 AND AT BS 178, WL 207, LBL 24. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040219001042004021900104 2004 2 19 SWAA040345 420040203A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219001052004021900105NM 2004 2 19 SWAA040346 120040203A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040219001072004021900107NM 2004 2 19 SWAA040348 120040203A53116546533 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040219001092004021900109NM 2004 2 19 SWAA040350 120040203A3350D717011000 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29716SW 27850 DURING SCHEDULED SPV, FOUND L1 DOOR AND RT BULLNOSE AT ROW 1 TO ROW 4, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM. 2L72 4F RTA16WE 20040219001122004021900112NM 2004 2 19 SWAA040211 120040121A53106546546 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 767, LBL 2. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040219001132004021900113NM 2004 2 19 SWAA040212 120040121A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17 L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040219001152004021900115NM 2004 2 19 SWAA040214 120040121A53116546650 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CORRODED AT BS 787, STRINGER 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040219001222004021900122NM 2004 2 19 SWAA040221 120040122A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 518, STRINGER 10R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040219001232004021900123NM 2004 2 19 SWAA040222 120040122A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO. 2L72 4F RTA16WE 20040219001252004021900125 2004 2 19 SWAA040224 420040122A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20040219001272004021900127NM 2004 2 19 SWAA040226 120040122A53106545857 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER FRAME HINGE CUTOUT RADIUS CRACKED. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20040219001322004021900132NM 2004 2 19 SWAA040231 120040122A575465C26603 WEDGE BOEING737 7373A4 1384585NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM. 2L72 4F RTA16WE 20040219001342004021900134NM 2004 2 19 SWAA040233 120040122A5312 CAP BOEING737 7373A4 1384585NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD AT BS 1016, CRACKED AT CENTER CAP. REPAIRED PER EA. 2L72 4F RTA16WE 20040219001362004021900136EA 2004 2 19 COMA0460105 120040203A5551600210617 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 BUSHING IN VERTICAL STABILIZER LEFT HAND LUG FOR HORIZONTAL STAB PIVOT POINT MIGRATED .029 INCHES. REMOVED AND REPLACED BUSHING. 2L72 4F RTA21EA 20040219001392004021900139EA 2004 2 19 COMA0460116 120040103A5320601R35031241 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01812CA 7381 CARGO FLOOR ANGLE AT FS 621.00 BULKHEAD, LEFT AND RIGH SUPPORT, CRACKED. COMPLIED WTIH BOMBARDIER REO 601R-53-61-004. PAINTED REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-00. 2L72 4F RTA21EA 20040219001412004021900141NM 2004 2 19 C1HA200483001 120040202A3297 CONNECTOR BOEING727 7272S7 138407ZNM MLG DIRTY A C1HAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL15683CA 22490 WHEN GEAR HANDLE PLACED TO DOWN POSTION, GEAR DID NOT CYCLE NORMALLY. NOSE GEAR STAYED INTO UP & LOCKED POSITION. AFTER GO-AROUND GEAR OPS NORMAL. VISUAL CHECK, CLEAN PLUG PER MC 32-61-01. 2L73 4F A3WE 20040219001662004021900166 2004 2 19 SWIA200412843 420040201A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07567SW8727 8727 120342 CREW REPORTS NR 1 AUTOPILOT WON'T CAPTURE HDG. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040219001812004021900181NM 2004 2 19 CALA0400075 120040205A5320 ANGLE BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2739726 28796 INSPECTION FOUND RT SIDE ZEE ANGLE CORRODED AT STA 727-797. A NEW ZEE ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040219001852004021900185NM 2004 2 19 CALA0400079 120040122A5320 FLANGE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND THE UPPER SURFACE OF THE FORWARD FLANGE OF THE ZEE FRAME CORRODED AT STA 270, BL 0.0. THE FRAME WAS REPAIRED IAW ECRA 5321-01169. 2L72 4F RTA16WE 20040219001872004021900187CE 2004 2 19 DXTA200400235 120040130A3234 CONTROL HANDLE CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07953QS 7500153 AFTER TAKEOFF GEAR HANDLE STUCK IN THE DOWN POSITION, COULD NOT RETRACT GEARS, ACCOMPLISHED AIR TURNBACK. TROUBLESHOT NOSE GEAR SQUAT SWITCH, ALL WIRING CHECKED GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE, AIRCRAFT REQUIRES OCF FOR LANDING GEAR CONTROL SYSTEM. ALL WORK DONE IAW CESSNA 750 MM CHAPTER 32-30-00. 2L72 4J RTT00007WI 20040219001882004021900188CE 2004 2 19 DXTA200400233 120040128A3240 RELAY CESSNA500 560CESSNA 2076750CE BRAKE SYSTEM MALFUNCTIONED E DXTAO OTHER JS WARNING INDICATION AFFECT SYSTEMS LDLANDING 1 GL07392QS 5600429 ON FINAL APPROACH THE POWER BRAKE LOW PRESSURE AND ANTISKID INOP ANNUNCIATOR ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES CHECKLIST AND PLACED THE ANTISKID SWITCH IN THE OFF POSITION. BRAKES FAILED NEAR THE END OF LANDING ROLLOUT, BRAKE PEDALS WENT TO THE FLOOR DURING EMERGENCY BRAKE APPLICATION. GAINED ACCESS TO BRAKE ACCUMULATOR, POWER BRAKE VALVE & ANTISKID SERVO, HYDRAULIC BRAKE RESERVOIR, INSPECTED AREA AND NO HYDRAULIC FLUID LEAKING NOTED. TROUBLESHOT BRAKE SYSTEM AND CHECKED CONNECTORS, ALL SECURED, CHECKED ANTISKID BITE INDICATOR, NO BITE SHOWING, REMOVED GROUND WIRES FROM GROUNDING STUBS, INSPECTED AND REINSTALLED. REPLACED BRAKE RELAY, BLED SYSTEM IAW CESSNA 560 MM CHAPTER 32-40-00. 2L72 4F RTA22CE 20040219001892004021900189CE 2004 2 19 DXTA200400236 120040202A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07395QS 5600496 UPON TOUCH DOWN AND INITIAL APPLICATION OF BRAKES, CAPTAIN’S SIDE HAD POSITIVE BRAKE PRESSURE BUT AIRCRAFT WOULD NOT SLOW DOWN. AFTER APPLICATION OF EXCESSIVE BRAKE PRESSURE A/C BRAKES GRABBED AND AIRCRAFT SLOWED RAPIDLY. BLED BRAKE SYSTEM, OPS CHECK OF BRAKES GOOD AT THIS TIME IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20040219001902004021900190CE 2004 2 19 DXTA200400238 120040205A21202724128714 CONTROL VALVE CESSNA560 560XL 2076702CE AIR DISTRIBUTIONFAILED E DXTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL07688QS2443 5605188 AIR DUCT OVERHEAT COCKPIT LIGHT ILLUMINATED 30 SECONDS AFTER TAKEOFF, PASSENGERS SAW SMOKE IN THE CABIN. SELECTED MANUAL TEMPERATURE CONTROL TO COLD FOR 30 SECONDS WITHOUT A CHANGE, THE SOURCE TEMP REACHED 325 DEGREES, EMERGENCY DECLARED, AIRCRAFT DIVERTED TO CHS AND LANDED SAFELY. COMPLIED WITH GROUND RUN CHECKS OF THE TEMP CONTROL SYSTEM, NO DISCREPANCIES NOTED, CHECKED ELECTRICAL CONNECTORS ON CONTROLLER & COCKPIT TEMP CONTROL VALVE. REMOVED & REPLACED VALVE DUE TO CESSNA RECOMMENDATION. SYSTEM OPS CHECK & LEAK CHECK GOOD ON GROUND RUN. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 21-61-00. 2L72 4F RTA22CE 20040219001922004021900192NM 2004 2 19 04FDEA00317 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040219001942004021900194NM 2004 2 19 04FDEA00319 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP. INBD. HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040219001952004021900195NM 2004 2 19 04FDEA00320 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNTING HOLE (7) INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD. FLAP INBD HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040219002042004021900204NM 2004 2 19 04FDEA00329 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT I/B FLAP O/B HINGE FWD UPPER ATTACH FITTING FOUND CRACKED. RT I/B FLAP O/B AFT HINGE ASSY REMOVED & REPLACED AS PER DRAWING NR NRC6060. 2L73 4F RTA22WE 20040219002162004021900216NM 2004 2 19 QXEA200400107 120040127A5730 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - LEFT WING PANEL 522AT COUNTER SINKS HAVE FRETTING FROM SCREWS AT INBOARD AND OUTBOARD ENDS. REPAIRED IAW DHC-8-200 SRM 51-20-16. 2H72 4T RTA13NM 20040219002182004021900218NM 2004 2 19 QXEA200400109 120040128A5520 FITTING DHAV DHC8 DHC8202 2809007NM ZONE 300 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - LEFT HAND FORWARD HORIZONTAL STAB SPAR FITTING SCRATCHED. REPAIRED IAW RD 8-55-847. 2H72 4T RTA13NM 20040219002192004021900219NM 2004 2 19 QXEA200400113 120040203A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - UPPER FORWARD OUTBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2H72 4T RTA13NM 20040219002222004021900222NM 2004 2 19 QXEA200400102 120040129A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - RIGHT OUTBOARD SEAT TRACK NR 11 CORROSION TOP AND BOTTOM SEAT ATTACH AREA APPROXIMATELY X438.00. REPAIRED IAW DASH 8-200 SRM 51-40-11, SRM 51-40-00. 2H72 4T RTA13NM 20040219002262004021900226EA 2004 2 19 QXEA200400117 120040206A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 FORWARD CARGO COMPARTMENT CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPEATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040219002322004021900232SO 2004 2 19 C2XA04TY034 120040207A531514522460013 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002342004021900234SO 2004 2 19 C2XA04CL009 120040206A3397 WIRE EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPAIRED WIRE SPLICE SP3676, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040219002412004021900241SO 2004 2 19 C2XA04BT019 120040206A2120P1097 FILTER EMB 145 EMB145LR 3260212SO FAN FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2716561 145610 CREW REPORTED, MELTING PLASTIC ODOR FOLLOWED BY BLEED NR 2 OVERHEAT WHILE IN ICING CONDITIONS. MAINTENANCE PERFORMED FIM TASK 36-11-00-810-803A, REMOVED AND REPLACED FAN AIR VALVE FILTER IAW EMB145 MM 36-11-03. PERFORMED OPS CHECK IAW EC3610-01062 STEPS 2.4 THROUGH 2.12. NO BURNING SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040219002442004021900244NM 2004 2 19 CALA0400081 120040206A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 2 INCH CRACK IN AFT CABIN L-ANGLE AT TOP OF INTERCOSTAL WEB AT FASTENER HOLES (4 EACH), STA 927-947, BL 0, WL 209. A SHEAR WEB ANGLE WAS INSTALLED IAW SRM 51-40-02 AND BOEING DRAWING 69-36656. 2L72 4F RTA16WE 20040219002482004021900248NM 2004 2 19 CALA0400085 120040207A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 6 INCH CRACK IN INTERCOSTAL BETWEEN STA 344 AND 360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040219002522004021900252NM 2004 2 19 CALA0400089 120040208A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND R-1 DOOR CUTOUT ZEE ANGLE CORRODED FROM STA 290-360. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000012004022000001EU 2004 2 20 118161 120040206A7720 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 406 ON 02-06-04, APPROX 16450 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON. 2L72 4T4 TRTA52EU E8NE6 20040220000132004022000013EA 2004 2 20 COMA0460119 120040103A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01812CA 7381 CARGO ENTRY WAY FORWARD FRAME AT FS 574.00 APPROXIMATELY STRINGER 15L HAS DAMAGE. COMPLIED WITH REO 601R-53-61-690 TO FACILITATE CARGO ENTRY WAY FORWARD FRAME FS 574.00 REPAIR. PARTIALLY REMOVED FRAME AT FS 574.00 IN ACCORDANCE WITH CRJ SRM 51-40-06. LOCATED FRAME, SPLICE DOUBLER AND FRAME ANGLE AND COMPLETED INSTALLATION OF FRAME REPAIR AT FS 574.00 IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-901. APPLIED TOPCOAT TO FS 574.00 REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-16. 2L72 4F RTA21EA 20040220000142004022000014EA 2004 2 20 COMA0460120 120040205A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01967CA 7134 FLIGHT 5242 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040220000162004022000016EA 2004 2 20 COMA0460122 120040203A3230555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01964CA 7129 FLIGHT 5351 NOSE DOOR OPEN WARNING DURING GEAR RETRACTION. REPLACED THE NLG DOOR SELECTOR VALVE. 2L72 4F RTA21EA 20040220000212004022000021NM 2004 2 20 UPS04441841 120040126A5310 SHEAR TIE BOEING747 747123 1384873NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT CARGO BILGE AREA - FX 1820, STR 44R - 46R SHEAR TIES CORRODED. BS 1820 TO 1820, STR R44-R46 CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 0.5 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. FLANGE REPAIRED REFER SRM 53-10-04 FIG 3 AND CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040220000232004022000023WP 2004 2 20 UPS04841819 120040114A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1540 RBL 30 INTERCOSTAL ON AFT BULKHEAD CRACKED AT NUT PLATE. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040220000282004022000028WP 2004 2 20 UPS04841824 120040106A53205888479 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, SHEARED RIVET HEAD, BULGE & CORRODED SHEAR WEB ABOVE & BELOW L21R CUSP MAIN CABIN COURIER AREA FS 25. REMOVED FRAME FITTING AND FLOOR SUPPORTS TO FOM, REMOVED CUSP ANGLES AND FABRICATED NEW ANGLE IAW DC8 SRM 53-3-3 AND DAC DWG 5888479. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP ANGLES, FRAME FITTING AND FLOOR SUPPORTS IAW DC8 SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040220000302004022000030WP 2004 2 20 UPS04841826 120040107A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, UPPER CARGO BETWEEN STA 1000-1020 AT LONG 13L SHEAR TIE IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. FABRICATED NEW SHEAR TIE IAW DC8 SRM 53-4-1 FIG 51 AND 51-1-24. HEAT TREAT TO 7075-T6 .080 IAW TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20040220000352004022000035WP 2004 2 20 UPS04841831 120040110A5340 SUPPORT FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1140 L35L SUPPORT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED NEW FITTING AND DRILLED EXISTING FASTENER HOLES IAW DC8 SRM 51-3-2 AND 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040220000472004022000047WP 2004 2 20 UPS04841851 120040205A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01750UP UPS2964 45950 EMERGENCY LIGHTS INOP DUE TO POWER ON AC AND LIGHT SWITCH LEFT IN ARMED POSITION. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. 2L74 4F RT4A25 20040220000482004022000048NM 2004 2 20 UPS04M41837 120040120A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-919 X=8.5. CORROSION REMOVED ON SEAT TRACK PER SRM 51-21-01 VOL II REV 34, MAT REMOVED 0.036 INCH, ORIGINAL THICK 0.112 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 800-929 X =8.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000512004022000051NM 2004 2 20 UPS04M41840 120040119A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 775-899 X=-75.0. CORROSION REMOVED ON SEAT TRACK AT STA 775-815 MAT REMOVED 0.007 INCH, ORIGINAL THK 0.112 INCH FOUND WITHIN LIMIT PER SRM 53-70-00 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 815-909 X=-75.0 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000532004022000053NM 2004 2 20 AWXA200400157 120040207A2120 ODOR AIRBUSA319 A319132 3930340NM COCKPIT/CABIN DETECTED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP28820AW11483 1397 AN ELECTRICAL BURNING ODOR OBSERVED IN THE COCKPIT & CABIN NEAR SEAT ROW 4, DECLARED EMERGENCY, LANDED WITHOUT FURTHER DIFFICULTIES. MX REMOVED AFT WALL OF FWD BAG PIT & INSPECTED RECIRCULATION FANS & DUCTING FOR EVIDENCE OF OVERHEATING & ODOR, NO DEFECTS NOTED. DUE TO FAILURE HISTORY: REPLACED AVIONICS COOLING FAN (18HQ) IAW AMM 21-26-51-401, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF AVIONICS COOLING FAN CONFIRMED FAILURE, BEARING NOISE COULD BE HEARD DURING TEST. R & R WORN BEARINGS & BALANCED ROTOR & MOTOR IMPELLER IAW CMM. RE-TEST OF UNIT GOOD. 2L72 4F RTA28NM 20040220000542004022000054EU 2004 2 20 AWXA200400158 120040207A2120 ODOR AIRBUS320 A320231 3930325EU GALLEY DETECTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28625AW 064 MSP - DIVERSION - FLT 0232 - APPROXIMATELY 45 MINUTES AFTER TAKEOFF FROM DTW, EN ROUTE FOR LAS, THE FLIGHT ATTENDANTS REPORTED A STRONG ODOR OF GAS OR SULFUR IN THE AFT GALLEY, DIVERTED TO MSP. WHEN MAINTENANCE ARRIVED, FOUND NO ODOR IN AFT GALLEY. THE MSP FIRE DEPARTMENT GAS ANALYZER WAS USED TO DETECT ANY EVIDENCE OF GAS, ANALYZER READ -0-. AFT GALLEY OVENS AND COFFEEMAKERS WERE OPERATED, NO SULFUR ODOR WAS NOTED, RAN BOTH ENGINES AND OPERATED AIR CONDITIONING PACKS, NO ODOR WAS NOTED. 2L72 4F RTA28NM 20040220000602004022000060NM 2004 2 20 AALA20040202 120040205A3350 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21688AA 25730 DFW EMERGENCY LIGHT AT SEAT 22 INOPERATIVE. FOUND LOOSE WIRE. REINSTALLED WIRE CONNECTION FOR EMERGENCY LIGHT AT SEAT 22. SYSTEM GROUND CHECKED NORMAL OPERTION. 2L72 4F RTA2NM 20040220000612004022000061NM 2004 2 20 AALA20040195 120040206A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 DFW SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220000622004022000062NM 2004 2 20 AALA20040201 120040206A3350 LIGHT BOEING767 767323 1385205NM 4L DOOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21354AA 24035 MIA EMERGENCY EXIT INDICATOR LENS AT LOWER AFT DOOR 4L IS DAMAGED. REPLACED EMERGENCY EXIT INDICATOR AT LOWER AFT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040220000652004022000065WP 2004 2 20 AALA20040194 120040207A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21269AA 49292 STL CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000682004022000068WP 2004 2 20 AALA20040199 120040206A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21588AA 53251 DFW CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040220000692004022000069WP 2004 2 20 AALA20040192 120040208A33506011770 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 ORD LEFT HAND AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACKS FOR LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000732004022000073NE 2004 2 20 AALA20040204 220040207A7320 FUEL CONTROL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ZONE 600 INOPERATIVE A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW219624T 53594 717857 DFW AT 10,000 FT AS POWER CAME UP THE RIGHT ENG INITIALLY CAME UP THEN DROPPED QUICKLY TO .92 EPR THEN SURGED UP TO ABOUT 1.8 EPR AND THEN IMMEDIATELY DROPPED TO .09 EPR. ENGINE WINDMILLED. RETURNED TO DFW. AIRCRAFT WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE FUEL PUMP AND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20040220000772004022000077SO 2004 2 20 SWIA200412849 120040114A5411 FRAME EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 LEFT NACELLE INBOARD HALF FRAME UNDER TAILPIPE AFT MOUNT FRAME CRACK. DISCOVERED DURING C-CHECK INSPECTION. REPLACED NACELLE HALF FRAME IAW 120 SRM 51-10-02. 2L72 4T RTA31SO 20040220000822004022000082EA 2004 2 20 SWIA200412854 120040201A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07918SW 7645 FLAPS FAIL CAUTION MESSAGE ON WHEN FLAPS SELECTED AT APPROXIMATELY 13,000 FT. REMOVED AND REPLACED RIGHT NR 1 AND LEFT NR 1 ACTUATOR (FLAP), IAW 27-53-01, 27-53-05, AND RII 27-412. OPS CHECKS GOOD. S/N OFF RIGHT: 3392. 2L72 4F RTA21EA 20040220000842004022000084EA 2004 2 20 SWIA200412856 120040203A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07929SW9284 5793 7703 BOTH STAB AND MACH TRIM CAUTION LIGHTS CAME ON DURING FINAL APPROACH. UNABLE TO RESET TRIM FOR MORE THAN 10 TO 15 SEC BETWEEN DISCONNECTS. REPLACED HORIZONTAL TRIM ACTUATOR AND HORIZONTAL TRIM MOTOR CONTROL UNIT AND THE HSTCU, OPS CHECKS GOOD IAW 27-41-00-740-801. MOTOR CONTROL UNIT P/N: 9062-3, S/N ON: 961, S/N OFF: 757. HSTCU P/N: 7060-9, S/N OFF: 1364. 2L72 4F RTA21EA 20040220000882004022000088SO 2004 2 20 LR7A04004 120040124A5312 CAP LKHEED382 382G 526414USO BLKHD BEAM CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FS 479 WL 200 LT INTERCOSTAL BEAM BROKEN/CRACKED THROUGH. BEAM CAP (TEE) REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 LBL 62. 2H74 4T A1SO 20040220000902004022000090SO 2004 2 20 LR7A04006 120040124A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FWD FUSELAGE SKIN CRACKED THROUGH RIVET HEAD AT LT JACK PAD AREA FS 191 WL 180L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 191 WL 180 LBL 61. 2H74 4T A1SO 20040220000922004022000092SO 2004 2 20 LR7A04008 120040124A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RAMP DOOR BOTTOM SKIN DENT & PITTING CORROSION AT FS 820 BL 18R. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 820 RBL 18. 2H74 4T A1SO 20040220000982004022000098SO 2004 2 20 LR7A04014 120040124A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5315 FOUND LT FS 844 WL 180 RBL 62 FOUND BRACKET CRACKED. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-10, FS 844 WL 180 RBL 62. 2H74 4T A1SO 20040220001092004022000109SO 2004 2 20 LR7A04025 120040205A5310 WINDOW POST LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 768 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND RT AFT DV WINDOW POST CRACKED. REPAIR CARRIED OUT IAW SMP583 CH 53-30-25, FS 116 WL 255 RBL 40. 2H74 4T A1SO 20040220001122004022000112WP 2004 2 20 04FDEA00366 120040208A78309152M45P004A RIB DOUG DC10 DC1010 3022110WP THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-73868 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM. 2L73 4F A22WE 20040220001162004022000116NM 2004 2 20 04FDEA00355 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORRODED. LT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001192004022000119NM 2004 2 20 04FDEA00352 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001202004022000120NM 2004 2 20 04FDEA00351 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001212004022000121NM 2004 2 20 04FDEA00350 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. WINGS - RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001222004022000122NM 2004 2 20 04FDEA00349 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75249. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040220001252004022000125NM 2004 2 20 04FDEA00346 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FACE REMAINING IS WITHIN THE LIMITS OF DWG ARC 0502 SHEET 4. 2L73 4F RTA22WE 20040220001262004022000126NM 2004 2 20 04FDEA00344 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040220001312004022000131NM 2004 2 20 F3LA200400009 120040209A5347 MOUNT BOEING737 7373S1 138447SNM LAVATORY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 24856 DURING C-7 CHECK, INSPECTION REPORTED FWD LAVATORY MOUNT BLOCK AT STA 303, LBL 12, CORRODED. REPLACED LAVATORY MOUNT PER SRM 53-10-15, SRM 53-10-51 AND DRAWING 65C33970. 2L72 4F RTA16WE 20040220001322004022000132NM 2004 2 20 2004UALA00007 120040104A21337207375 RELIEF VALVE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP29377UA 24642 AT FLIGHT LEVEL 33.0 LOST PRESSURIZATION, OXYGEN MASKS DEPLOYED INADVERTENTLY. CABIN SAFETY PRESSURE RELIEF VALVES FAILED. REPLACED INBOARD & OUTBOARD RELIEF VALVES. 2L72 4F4 FRTA16WE E2GL 20040220001342004022000134NE 2004 2 20 2004UALA00086 220040130A7320 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUEL CONTROL ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29827UA 1022 RETURN TO FIELD DUE TO ECAM NR 2 FUEL CONTROL FAULT. DEBRIS FLOWING THROUGH FMU CAUSED TORQUEMOTOR FAULT. THE DEBRIS WAS SUBSEQUENTLY FLUSHED OUT. THIS IS AN ISOLATED INCIDENT AND ENGINEEING WILL CONTINUE TO MONITOR THE FMU. 2L72 4F4 FRTA28NM E40NE 20040220001352004022000135NM 2004 2 20 2004UALA00087 120040130A2910 VALVE AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE HYDRAULIC SYSTEMFAILED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29822UA 948 FLIGHT EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE. REPLACED THE HYDRAULIC SAFETY VALVE. 2L72 4F4 FRTA28NM E40NE 20040220001372004022000137EU 2004 2 20 04019314A 120040119A5320 INTERCOSTAL JETAIRJETSTMJETSTM4101 1500501EU FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27314UE 41027 DURING HEAVY INSPECTION THE INTERCOSTAL AT STATION 4 WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF THE INSPECTION. 2L72 4T RTA41NM 20040220001412004022000141EA 2004 2 20 04016633 120040116A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE RIGHT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001422004022000142NM 2004 2 20 P5CA0401034 120040209A80123978921 START VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650* 30018NE NR 4 ENGINE MALFUNCTIONED A P5CAK NONE J WARNING INDICATION ININSP/MAINT 1 WP23505MC 21251 517529 NR 4 ENG STARTER VALVE WOULD NOT CLOSE 50 PERCENT. REPLACED START VALVE, OPS CHECK OK PER MM 80-11-04. 2L74 4F4 FRTA20WE E23EA 20040220001462004022000146NM 2004 2 20 QXEA200400121 120040209A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09379PH 530 BOI - FLIGHT 2206 - ON CLIMBOUT THE LAVATORY SMOKE DETECTOR SOUNDED. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040220001472004022000147EA 2004 2 20 04022670 120040122A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27670BR 7561 DURING INSPECTION THE EMERGENCY LIGHT ON THE GALLEY WALL WAS FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001482004022000148EA 2004 2 20 04024620 120040124A7830 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF RIG A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27620BR 7179 DURING CRUISE OF FLIGHT 9950 THE CREW REPORTED THE THRUST REVERSER UNLOCKED DURING FLIGHT. THE THRUST REVERSER WAS RIGGED AND ADJUSTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001492004022000149EA 2004 2 20 04025676 120040125A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27676BR 7644 DURING INSPECTION THE LEFT HAND MID WING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001542004022000154EA 2004 2 20 COMA0460128 120040206A7830864808 PSEU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01488CA3165 7730 FLIGHT 5928 RIGHT THRUST REVERSER UNSAFE CAUTION. REPLACED THE PSEU. 2L72 4F RTA21EA 20040220001582004022000158NM 2004 2 20 04FDEA00375 120040209A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CORROSION, AFT CARGO BAY, CORROSION ON 1183 BULKHEAD BS 1183 LBL 2 WL 153. *S/D* REMOVED BS 1183 BL 0 (I) BEAM. FABRICATED AND INSTALLED NEW (I) BEAM IAW FED EX EA 7-5310-70618 & SRM 51-30-2. 2L73 4F RTA3WE 20040220001592004022000159NM 2004 2 20 04FDEA00376 120040209A3231 CABLE BOEING727 727200 138407ENM MLG DOOR DAMAGED A FDEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO25480FE 21462 RED DOORS WARNING LIGHT ILLUMINATED ON GEAR RETRACTION S/O'S PANEL. NOSE GEAR DOOR LIGHT ALSO ILLUMINATED AFTER FOLLOWING QRH PROCEDURES. THE LIGHTS REMAINED ILLUMINATED. RETURN TO MEM. REMOVED AND REPLACED BOTH DOOR CABLE, ADJ AND RIGGED NOSE GEAR FWD DOORS. ALSO C/W GEAR SWING. NOSE DOOR LIGHT CHECK AND MANUAL EXTENSION ON NOSE GEAR C/W. ALL WORK ACCOMPLISHED PER AMM 727-200-32-22-001-5. 2L73 4F RTA3WE 20040220001602004022000160NM 2004 2 20 04FDEA00380 120040209A5753 FAIRING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT WING O/B FLAP I/B HINGE FAIRING FOUND O/B BRACKET CRACKED. LT WING O/B FLAP I/B HINGE FAIRING FWD OUTER CRACKED BRACKET REMOVED, FABRICATED, AS PER DRWG ARC7717 & COMPLIED AS PER EA 1-5750-74228. TE FLAP O/B TE FLAP AFT HINGE BRACKET AERODYNAMIC FAIRINGS FWD SUPPORT BRACKET. FABRICATION, AND INSTALLED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20040220001662004022000166EU 2004 2 20 04FDEA00389 120040210A2170 COALESCER BAG AIRBUS310 A310 EU CABIN AIR DIRTY A FDEAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO25412FE 360 ON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BAGS VERY DIRTY. REMOVED AND REPLACED WATER SEPARATOR BAGS IAW MM 21-51-16-4, OPS CHECK NORMAL. NO SIGN OF SMOKE OR OTHER SIGN OF ABNORMAL ODORS, OK FOR SERVICE. 2L72 4F RTA35EU 20040220001672004022000167EA 2004 2 20 COMA0460127 120040207A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01981CA 7163 FLIGHT 5131 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040220001712004022000171EA 2004 2 20 04030675 120040130A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 DURING INSPECTION A CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040220001762004022000176NM 2004 2 20 04031420 120040131A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27420FJ 3178 DURING INSPECTION AN OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040220001822004022000182NM 2004 2 20 CALA0400097 120040209A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 2 INCH CRACK IN SHEAR WEB PANEL FORWARD OF STA 578, S17L. THE WEB WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-70-13. THE WEB WAS REINSTALLED IAW SRM 51-41-02. 2L72 4F RTA16WE 20040220001832004022000183NM 2004 2 20 CALA0400098 120040209A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND SHEAR WEB IN RT AFT LAV AREA CORRODED AT FS 1019, RBL 28. THE SHEAR WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220001852004022000185NM 2004 2 20 0400186740 120040102A5312 BULKHEAD BOEING747 747251F 1384898NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01640US 23888 DURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093. 2L74 4F A20WE 20040220001952004022000195WP 2004 2 20 AALA20040206 120040209A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21975TW 53625 SEA OVERHEAD EMERGENCY EXIT LIGHT AT LIFE RAFT STORAGE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B5-101 FOR EMERGENCY EXIT LIGHT AT LIFE RAFT STORAGE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040220001992004022000199NM 2004 2 20 QXEA200400124 120040204A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - DENT IN FUSELAGE SKIN - LEFT HAND SIDE UNDER ICE SHIELD 10.5 INCHES ABOVE NR 2 WINDOW. REPAIRED IAW HORIZON AIR EA 2-53-541 AND RD 8-53-7768. 2H72 4T RTA13NM 20040219000052004021900005WP 2004 2 19 04FDEA00335 120040206A78309059M42P019A BUMPER BLOCK DOUG DC10 DC1010 3022110WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 NR 1 ENGINE OUTBOARD THRUST REVERSER MOST FWD UPPER BUMPER ASSY CRACKED. REMOVED AND REPLACED BUMPER ASSY IAW SRM 51-31-01 AT MAE ON N/R N01145. 2L73 4F A22WE 20040219000132004021900013NM 2004 2 19 UPS04441859 120040123A5313BAC14981427075 STRINGER BOEING747 747123 1384873NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT- LT STA 720 - STA 740 STRINGER 47 FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040219000162004021900016NM 2004 2 19 UPS04441862 120040123A5320BAC1509100312 CHANNEL BOEING747 747123 1384873NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D- BS 2315 LBL 11 TO LBL 38 HAT SECTION FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 8. P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM53-10-17. 2L74 4F A20WE 20040219000332004021900033SO 2004 2 19 C2XA04SH066 120040215A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000342004021900034NM 2004 2 19 SWAA040443 120040211A53126546568 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C1 CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 3R AND STRINGER 5R. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040219000352004021900035CE 2004 2 19 57827 120040111A6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162CE LT ENGINE MALFUNCTIONED A AMWAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE07244YV UE244 ON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULDN'T TEST. CREW RETURNED TO THE GATE WITH NO FURTHER INCIDENT. RAN BOTH ENGINES, ALL SYS OPS CK NORMAL. 2L72 4T RTA24CE 20040219000432004021900043EU 2004 2 19 MALA040187 120040126A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, LT ICE SHIELD IS DENTED. REMOVED DENTED ICE SHIELD, CUT OUT DAMAGED AREA, FABRICATED DOUBLER, INSTALLED DOUBLER AFTER TREATING. FABRICATED ICE SHIELD, TREATED, INSTALLED ICE SHIELD IAW EO NR S53005. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2L72 4T RTA52EU 20040219000612004021900061NM 2004 2 19 SWAA040410 120040208A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040219000662004021900066NM 2004 2 19 2004UALA00091 120040131A3397 TERMINAL BLOCK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT MISSING A UALAK NONE L NO TEST ININSP/MAINT 1 WP29197UA 26901 EMERGENCY LIGHT ON DOOR NR 2 LEFT, STAYS ON ALL THE TIME. FOUND GROUND MISSING AT TERMINAL BLOCK. SECURED GROUND TERMINAL. LIGHT ASSY OPS CHECKS OK FOR ALL FUNCTIONS. 2L74 4F4 FRTA20WE E24NE 20040219000782004021900078NM 2004 2 19 SWAA040353 120040204A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 FUSELAGE SKIN CRACKED UNDER R1 DOOR BS 319, STRINGER 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219000802004021900080NM 2004 2 19 SWAA040355 120040204A57536549508 FLAP TRACK BOEING737 7373Q8 1384670NM LT WING WORN A SWAAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW29689SW 23387 AIRFRAME VIBRATION WHEN FLAPS SELECTED TO 5 DEGREES. REPAIRED LT WING T/E INBOARD MIDFLAP TRACK PER EA. 2L72 4F RTA16WE 20040219000832004021900083NM 2004 2 19 UPS04441738 120040104A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, U/D - BS 530 - 590 LBL 66, TIE DOWN TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 0.5 X 2.5 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20040219000872004021900087SO 2004 2 19 C2XA04SH57 120040204A532014528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040219000892004021900089CE 2004 2 19 58604 120040205A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE PAX DOOR FALSE INDICATIONA AMWAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07182YV UE182 WHILE ON FLIGHT, PASSENGER DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CAPTAIN FOLLOWED PROCEDURES TO LAND AT AN ALTERNATE FIELD TRI. CREW INSPECTED DOOR AND FOUND ANNUNCIATOR GAVE FALSE ILLUMINATION. THIS ITEM WAS DEFERRED. THEN PROCEEDED TO FINAL DESTINATION. STILL AWAITING MORE INFORMATION TO COME AT A LATER DATE. 2L72 4T RTA24CE 20040219000942004021900094NM 2004 2 19 SWAA040360 120040204A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001062004021900106NM 2004 2 19 SWAA040347 120040203A5315BAC1509 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 986, RBL 55 TO LBL 14, WL 208. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20040219001212004021900121 2004 2 19 SWAA040220 420040122A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040219001422004021900142NM 2004 2 19 SWAA040239 120040123A2560PH22300L STRIP BOEING737 7373L9 1384470NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED SPV, FOUND EEPLS PHOTO LUMINESCENT STRIP CRACKED AT RT, BS 833.45 TO BS 847.45. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20040219001552004021900155NM 2004 2 19 SWAA040252 120040124A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 617, LBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040219001572004021900157NM 2004 2 19 SWAA040254 120040126A335007912 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 EEPLS FLOOR TRACK LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS FLOOR STRIP PER MM. 2L72 4F RTA16WE 20040219001582004021900158NM 2004 2 19 SWAA040255 120040126A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STRINGER 5L. REMOVED AND REPLACED CRACKED CLIP PER SRM. 2L72 4F RTA16WE 20040219001672004021900167SO 2004 2 19 SWIA200412844 120040107A5720 BRACKET EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07232SW 120306 LEFT INBOARD WING, BRACKET CRACKED AT RIB STATION 8 AFT LOWER OUTBOARD ACCESS PANEL, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRACKET AT RIB STATION NR 8 AFT OF OUTBOARD FUEL ACCESS PANEL PER SRM 51-40-02. NO LEAKS AT THIS TIME. 2L72 4T RTA31SO 20040219001732004021900173WP 2004 2 19 DHL2004807004 120040206A2120 ODOR DOUG DC8 DC873F 302199FWP CABIN DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01807DH 45990 TOP OF DESCENT STRONG ODOR, INCREASE IN CABIN FLOW ODOR GOES AWAY. OPERATED LT AND RT PACKS AT VARIOUS SETTINGS IAW 21-50-0. NO ODORS NOTED. OPS GOOD. 2L74 4F RT4A25 20040219001752004021900175EU 2004 2 19 AWXA200400156 120040205A33501013081 LIGHT AIRBUS320 A320232 3930326EU SEAT ROW 11 RT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW 543 EWR - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH SIDEWALL LIGHT AT SEAT ROW 11 RT INOPERATIVE, BULB REPLACEMENT DID NOT HELP. MAINTENANCE REPLACED THE EMERGENCY ESCAPE PATH SIDEWALL LIGHT ASSEMBLY AT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040219001862004021900186NM 2004 2 19 CALA0400080 120040128A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 IN PREPARATION FOR INSTALLING A PERMANENT REPAIR, A TEMPORARY REPAIR DOUBLER ON THE INNER SKIN OF THE AFT CARGO DOOR ABOVE THE DOOR HANDLE CUTOUT WAS REMOVED AND A SMALL AREA OF DAMAGE TO THE INNER SKIN WAS DISCOVERED. A REPAIR DOUBLER WAS INSTALLED AS A PERMANENT REPAIR IAW ECRA 5232-01044. 2L72 4F RTA16WE 20040219002052004021900205WP 2004 2 19 04FDEA00333 120040206A3000 PRESSURE SWITCH DOUG DC10 DC1010 3022110WP ANTI ICE SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25388FE 46622 DURING CLIMBOUT WITH WING & ENGINE ANTI ICE ON GOT A NR 1 MANFOLD FAIL ALERT. COMPLIED WITH QRH AND RTB. TROUBLESHOT PER FIM CH 36-23 FOUND MANIFOLD FAULT INDICATOR SET (LEFT WING PRESSURE SW SHOWN) SWITCH WOULD NOT RESET. REMOVED AND REPLACED PRESS SWITCH IAW MM CH 36-23-03-4. OPS CHECK NORMAL. 2L73 4F A22WE 20040219002082004021900208WP 2004 2 19 AALA20040184 120040205A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21441AA 49460 DEN - OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS DIVIDER INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040219002122004021900212NM 2004 2 19 AALA20040188 120040129A5753 SUPPORT FITTING BOEING777 777223 1385213NM FLAPERON GROOVED A AALAK NONE O OTHER ININSP/MAINT 1 SW21790AN 30251 AFW - RT WING FIXED TRAILING EDGE FLAPERON OUTBOARD SUPPORT FITTING HAS 0.7 X 2.0 AND 0.092 DEPTH GROOVE WORN ON UPPER SURFACE. BLENDED OUT DAMAGE AND PERFORMED HFEC FOR CRACKS. ROTO PEENED BLENDED AREA. ALODINE AND APPLIED TWO COATS OF PRIMER TO REWORKED AREA. 2L72 4F RTT00001SE 20040219002152004021900215NM 2004 2 19 QXEA200400106 120040127A5740 ATTACH FITTING DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - RIGHT INBOARD WING FORWARD SPAR AT STATION YW138.0 BOTH UPPER AND LOWER LEADING EDGE ATTACH FITTINGS CRACKED. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20040219002212004021900221NM 2004 2 19 QXEA200400115 120040203A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACHMENT CLIP CRACKED AT LEFT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2H72 4T RTA13NM 20040219002302004021900230SO 2004 2 19 C2XA04TY032 120040206A532014524131009 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER DOOR SILL PLATE ATTACH BRACKET. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKET IAW EMB SRM 51-40-02 AND CPM 51-21-05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002332004021900233SO 2004 2 19 C2XA04TY035 120040207A531514522460013 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOP CAP AT FRAME 15. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002352004021900235NM 2004 2 19 F3LA200400006 120040205A5313 STRINGER BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AT STA 727B, STR 2L. REPLACED FLOOR BEAM STRINGER PER SRM 53-00-53 FIG 201. 2L72 4F RTA16WE 20040219002382004021900238SO 2004 2 19 C2XA04BT017 120040206A3210 LANDING GEAR EMB 145 EMB145LR 3260212SO MAINS MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2729906 145472 CREW REPORTED, AIR RETURNED, GEAR WOULD NOT RETRACT. MAINTENANCE OPERATIONALLY CHECKED LANDING GEAR EXTENSION AND RETRACTION, FOUND NORMAL OPERATION IAW EMB145 AMM 32-30-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040219002422004021900242SO 2004 2 19 C2XA04CL010 120040202A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714907 145468 IAH FLIGHT 2636, THE CREW REPORTED THE EMERGENCY LIGHT OVER 12A WAS INOPERATIVE. MAINTENANCE RELAMPED THE EMERGENCY LIGHT OVER 12A. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040219002542004021900254NM 2004 2 19 CALA0400091 120040208A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND STRAP UNDER BEAM AT C-2 DOOR CUTOUT I/B SILL STRUCTURE CORRODED AT STA 800. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000062004022000006EU 2004 2 20 MALA040175 120040123A5330 SKIN SAAB SF340 SF340A 7850100EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 LEFT UPPER FUSELAGE HAS NUMEROUS DENTS AT FS 339-345 STRINGER 1505-1206. MAINTENANCE FABRICATED DOUBLER FOR FUSELAGE SKIN AT FS 339-345, STRINGER 1505-1506, TREATED AND PRIMED, INSTALLED DOUBLER, TOP COATED IAW SAAB 340 SRM 53-70-10-2. A/C RELEASE DATE 2/5/04. 2L72 4T RTA52EU 20040220000172004022000017EA 2004 2 20 COMA0460123 120040205A3000355523255 ELEMENT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FAILED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01719CA 7253 FLIGHT 5803 ANTI ICE DUCT WARNING. REPLACED BLEED LEAK SENSING ELEMENT. 2L72 4F RTA21EA 20040220000182004022000018EA 2004 2 20 COMA0460124 120040203A55516002100617 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 BUSHING IN VERTICAL STABILIZER LEFT HAND LUG FOR HORIZONTAL STAB PIVOT POINT MIGRATED .029 INCHES. THE BUSHING IN THE RIGHT VERTICAL STABILIZER IS IMPROPERLY REAMED CAUSING MISALIGNMENT AND BINDING. REMOVED THE LT AND RT VERTICAL STABILIZER LUG BUSHINGS. MACHINED AND CADMIUM PLATED OVERSIZED BUSHINGS IAW WVAC EO 601R-55-4669. INSTALLED BUSHINGS IAW CRJ AMM 20-26-00-910-803. LINE REAMED BUSHING IAW DRAWING 600-21029. 2L72 4F RTA21EA 20040220000222004022000022NM 2004 2 20 UPS04441842 120040123A5310 FORGING BOEING747 747123 1384873NM WINDOW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- BS 1560-1580 LT WINDOW FORGING AFT EDGE ATT SKIN FOUND CORROSION REVEALED. BS 1560-1580, STR L19-L22 CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM 53-30-01 FIG 1 LIMIT. WINDOW FORGING REPAIRED PER RS R-53-61-35104 & UPS ENGINEERING FILE 747-53-20164, CIC APPLIED IAW CPM 53-10-47. 2L74 4F A20WE 20040220000252004022000025WP 2004 2 20 UPS04841821 120040104A534336410042 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, RIGHT MLG WW L24R AT STA 879 VERT BATHTUB FITTING HAS CORROSION ON FWD SIDE. REMOVED CORROSION & FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53 -2-0 FIG 1F. REMOVED FITTING, FABRICATED REPAIR SPLICES AND INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0 FIG 8. 2L74 4F RT4A25 20040220000452004022000045WP 2004 2 20 UPS04841848 120040203A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING CENTER L/E LOWER RIB HAS A HOLE WORN THRU AT XFS 416. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040220000502004022000050NM 2004 2 20 UPS04M41839 120040120A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-899 X=-27.5. CORROSION REMOVED ON SEAT TRACK PER SRM 51-21-01 VOL II REV 34, MAT REMOVED 0.030 INCH, ORIGINAL THK 0.112 INCH EXCEED LIMIT OF SRM 53-70-00 FIG 3 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 800-909 X=-27.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000582004022000058WP 2004 2 20 AALA20040190 120040208A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21269AA 49292 STL OVERHEAD EMERGENCY LIGHTS AT L1 AND R1 COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT L1 AND R1 COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000712004022000071NM 2004 2 20 AALA20040200 120040206A3350 LIGHT BOEING767 767323 1385205NM SEAT 2G BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21354AA 24035 MIA EMERGENCY LIGHT DIRECTIONAL ARROW IN FRONT OF SEAT 2G IS BROKEN. REPLACED DIRECTION ARROW EMERGENCY LIGHT IN FRONT OF SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040220000932004022000093SO 2004 2 20 LR7A04009 120040124A5230339119 FAIRING LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RAMP DOOR BOTTOM PEDESTAL FWD FAIRING AND LT & RT FAIRINGS WARPED. FAIRINGS REPLACED IAW SMP583 CHP51-60 & 51-70, FS 845 BL 18R. 2H74 4T A1SO 20040220000992004022000099SO 2004 2 20 LR7A04015 120040124A5522 SKIN LKHEED382 382G 526414USO RT ELEVATOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND RT ELEVATOR (QTY 4 EA) SKIN CRACKED & DENTED AT HSS196. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, HSS196. 2H74 4T A1SO 20040220001042004022000104SO 2004 2 20 LR7A04020 120040124A5320 CAP LKHEED382 382G 526414USO WW INTERCOSTAL CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND AFTER REMOVAL OF RT MLG INTERCOSTAL BRACKET FS 557 WL 198, O/B CAP BROKEN AT TIP END. REPAIR CARRIED OUT IAW SMP583 FIG 53-40-14, FS 557 WL 198 RBL 62. 2H74 4T A1SO 20040220001102004022000110SO 2004 2 20 LR7A04026 120040205A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 768 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND FS 617 BULKHEAD AT WL 210 EXISTING REPAIR CRACKED AT LBL 60. REPAIRED IAW SMP583 FIG 53-40-10, FS 617 WL 200 - 210 LBL 63-73. 2H74 4T A1SO 20040220001242004022000124NM 2004 2 20 04FDEA00347 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE, INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FACE REMAINING THICKNESS (0.472 INCH) IS WITHIN THE LIMITS OF DWG ARC0502 SHT 4. 2L73 4F RTA22WE 20040220001292004022000129SO 2004 2 20 C2XA04SH059 120040210A533014520553005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 19 AND 20 AT STRINGER 7L, JUST AFT OF THE MAIN DOOR. MAINTENANCE REMOVED THE AFFECTED SECTION OF STRINGER 7L, RE-CONTOURED THE DENTED AREA OF SKIN, AND INSTALLED A NEW 7L STRINGER SECTION IAW CONTINENTAL EXPRESS EC 5330-01242. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040220001442004022000144EA 2004 2 20 04019626 120040119A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAULTY A VTZAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27626BR 7225 DURING FLIGHT THE CREW REPORTED A LAVATORY SMOKE INDICATION. FLIGHT LANDED WITHOUT INCIDENT. UPON MAINTENANCE THE SMOKE DETECTOR WAS FOUND TO GIVE FALSE INDICATIONS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001502004022000150EA 2004 2 20 04027308 120040127A33506040751 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27308UE 41023 DURING INSPECTION THE EMERGENCY TRACK LIGHTING FROM ROW 8 TO REAR OF THE AIRCRAFT. THE POWER SUPPLY WAS FOUND DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040220001622004022000162NM 2004 2 20 04FDEA00383 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CABIN LEFT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13. CABIN LT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001652004022000165NM 2004 2 20 04FDEA00386 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 FWD CABIN RT FRAME SCRATCHED AT STA 695 BETWEEN STR 12 & 13. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001752004022000175NM 2004 2 20 HNAA0400010 120040208A7931 CONNECTOR DHAV DHC8 DHC8102 2809003NM TRANSMITTER LOOSE A HNAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA07911HA4738547385 034 NR 1 OIL PRESSURE INDICATES 45 PSI WITH NO WARNING LIGHT. FEATHERED ENGINE OIL PRESSURE BECAME ERRATIC. INFLIGHT EMERGENCY DECLARED AND DIVERTED TO CHO. INDICATION PROBLEM, FERRIED AIRCRAFT TO ROA. FOUND LOOSE CONNECTOR ON ENGINE. TIGHTENED AND RAN ENGINE BUT PROBLEM RETURNED. REPLACED OIL PRESSURE TRANSDUCER, GROUND RUN OPERATIONAL AND LEAK CHECK GOOD. 2H72 4T RTA13NM 20040220001772004022000177SO 2004 2 20 C2XA04SH047 120040205A532014521725013 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040220001782004022000178NM 2004 2 20 CALA0400093 120040209A5312 STIFFENER BOEING737 7373T0 1384582NM PRESS BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FORWARD SIDE LOWER AFT PRESSURE BULKHEAD CENTER CHANNEL STIFFENER CORRODED AT BS 1016-1025, BL 0. STIFFENERS AND SPLICES WERE INSTALLED IAW BOEING DRAWING 65C28106. 2L72 4F RTA16WE 20040220001912004022000191 2004 2 20 AWXA200400164 420040117A256565659723 PLATE BOEING737 737277 1384570NM GIRT BAR ADAPTERCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - EES - DURING C-15 CHECK CORROSION WAS FOUND IN R-2 DOOR GIRT BAR FITTING ADAPTER PLATE BS 328, RBL 74. MAINTENANCE REMOVED AND REPLACED L-2 DOOR GIRT BAR FITTING ADAPTER PLATE IAW T/C C1D25006. 2L72 4F RTA16WE 20040220001942004022000194WP 2004 2 20 AALA20040207 120040209A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGNEYC DISLODGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21478AA 49653 DFW AISLE EMERGENCY PATH LIGHT ASSEMBLY BETWEEN AFT LAVATORIES INOPERATIVE. FOUND BATTERY DISLODGED ON FORWARD BATTERY PACK. REINSTALLED BATTERY PACK FOR AISLE EMERGENCY PATH LIGHT ASSEMBLY BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220002012004022000201NM 2004 2 20 04035411 120040204A3010001D553A1800002 BOOT DORNERDO32 DO328300 NM EMPENNAGE DEICE FAULTY A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27411FJ 3166 DURING AIRCRAFT OPERATION THE CREW REPORTED A TAIL DEICE SYSTEM FAILURE. THE EMPENNAGE CROSS BOOT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040223000112004022300011EU 2004 2 23 00124 120040105A2612 FIRE LOOP AMD FALC20FALCON 2720302EU NR 1 ENGINE GROUNDED E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05977TW 13 PILOT REPORTED AFTER DEPARTURE, AN EMERGENCY HORN SOUNDED, ALL SYSTEMS CHECKED OK. PILOT REQUESTED RETURN FOR MAINTENANCE, NO EMERGENCY DECLARED. MAINTENANCE FOUND A FIRE LOOP ON NR 1 ENGINE GROUNDING OUT. REPOSTIONED FIRE LOOP, OPS CHECKED NORMAL AT THIS TIME. 2L72 4F A7EU 20040223000402004022300040SO 2004 2 23 RAIA00401002 120040105A3610SU2226 SEAL EMB 145 EMB145LR 3260212SO BLEED LINE BLOWN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 5673-STL- BLEED 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE SEAL UNDER AFT CARGO FLOOR. 2L72 4T RTT00011AT 20040223000412004022300041EU 2004 2 23 00125 120040105A2612 FIRE LOOP AMD FALC20FALCON 2720302EU NR 2 ENGINE GROUNDED E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05977TW 13 PILOT REPORTED AFTER DEPARTURE FROM ADS FIRE HORN SOUNDED WITH NO FIRE INDICATION LIGHTS, RETURN TO ADS FOR MAINTENANCE. MAINTENANCE FOUND FIRE LOOP GROUNDING OUT ON ENGINE DRAIN MAST ON THE NR 2 ENGINE REPOSITIONED AND OPS CHECKED NORMAL AT THIS TIME. 2L72 4F A7EU 20040223000422004022300042EU 2004 2 23 00126 120040106A7931 TRANSMITTER AMD FALC20FALCON 2720302EU NR 1 OIL PRESS MALFUNCTIONED E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05977TW 13 PILOT REPORTED AFTER DEPARTURE FROM ADS NR 1 ENGINE OIL TEMP AMD PRESSURE LIGHT ILLUMINATED, RETURN TO ADS FOR MAINTENANCE. R & R LT ENGINE OIL PRESSURE TRANSMITTER OPS AND LEAK CK NORMAL. 2L72 4F A7EU 20040223000432004022300043NE 2004 2 23 NACA20040002 220040105A8530356993 CYLINDER PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 6 MAKING METAL A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL0399330317 317 43576 P33192 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING, NR 6 CYLINDER LT AND RT LOW RESISTANCE SECONDARY. REPLACED NR 4 ENGINE DUE TO MAKING METAL. 2L74 4R4 R 6A3 5E8 20040223000592004022300059EA 2004 2 23 COMA0460016 120040104A3010 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01914CA 7012 FLIGHT 5898 LT FUSELAGE 14TH STAGE DUCT WARNING. COULD NOT DUPLICATE. SYSTEM OPERATON NORMAL. 2L72 4F RTA21EA 20040223000602004022300060EA 2004 2 23 COMA0460015 120040105A301011513361 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ANTI-ICE MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01938CA5736 7046 FLIGHT 5125 WING ANTI ICE CAUTION MESSAGE. REPLACED THE TEMP CONTROLLER. 2L72 4F RTA21EA 20040223000612004022300061EA 2004 2 23 COMA0460014 120040104A3010 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA FALSE INDICATIONA COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01473CA 7668 FLIGHT 5821 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040223000692004022300069SO 2004 2 23 C2XA04BT002 120040105A2120 ODOR EMB 145 EMB145ER 3260211SO COCKPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2715948 145056 CREW REPORTED (STRONG FUEL ODOR UPON APU START.) MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE APU GOOD. NO DEFECTS NOTED (SUSPECT POSSIBLE TAILWIND DURING START PROCESS) AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040223000732004022300073 2004 2 23 SWIA200412746 420040102A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07237SW8671 8671 120314 CAPTAIN'S AP FAILS IN FLIGHT. REMOVED AND REPLACED AUTOPILOT NR 1 COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040223000812004022300081NM 2004 2 23 750WL0001 120040103A3350BP573 CHARGER BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY LIGHTS AT ROW 2 AND L1 DOOR INOPERATIVE. REPLACED BATTERY CHARGER IAW MM 33-51-10. OPS CHECKS NORMAL. 2L72 4F RTA2NM 20040223000902004022300090NM 2004 2 23 200400288 120040108A262130903889 SQUIB BOEING757 757200 1384950NM FIRE BOTTLE DISCHARGED B AAIAK NONE O OTHER ININSP/MAINT 1 WP07TFARD 22211 WHEN FORWARD CARGO PIT ARM SWITCH WAS SELECTED TO ARM BOTH BOTTLE 1 AND BOTTLE 2, DISCHARGE LIGHTS CAME ON AND BOTTLES FIRED. TROUBLESHOT, FOUND SWITCH WAS BAD, REPLACED SWITCH AND REPLACED SQUIB. IAW MM 26-00-00. 2L72 4F RTA2NM 20040223000952004022300095EA 2004 2 23 UIA9301 120040108A324221517 BRAKE ASSY DHAV DHC8 DHC8311 1386006EA NR 1 & 4 JAMMED Z D RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 TW0015239 571 RT MLG BRAKE JAM DURING TAXI, CHK FOUND NR 1 AND NR 4 BRAKE STUCK. REPLACED NR 1 AND NR 4 BRAKE AND PERFORM BRAKE SYSTEM BLEED AND ANTI-SKID FUNCTIONAL TEST NML. 2H72 4T RTA13NM 20040223000962004022300096NM 2004 2 23 PCAA0401152 120040108A3260 BULB DHAV DHC8 DHC8102 2809003NM MLG INDICATOR BLOWN A PCAAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA13805EX 228 FLIGHT NR 3882 FROM BWI TO LGA HAD TO CYCLE GEAR DUE TO THE LACK OF RT MAIN GEAR FAILING TO INDICATE DOWN. ONCE GEAR WAS CYCLED THE RT MAIN GEAR STILL DID NOT INDICATE DOWN. ALTERNATE INDICATION WAS USED TO DETERMINE GEAR WAS DOWN AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE WAS NOTIFIED AND INSPECTED GEAR IDICATION SYSTEM AND FOUND THE RT MAIN GEAR INDICATION LAMPS INOPERATIVE LAMPS WERE REMOVED AND REPLACED AND SYSTEM TEST O.K., AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040223001052004022300105 2004 2 23 372PA0039 420040106A2230 SYNCRONIZER BOEING737 737306 13844BGNM AUTOTHROTTLES OUT OF ADJUST A PIDAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO05372PA 23546 AUTO THROTTLES DISENGAGED ON TAKE OFF ROLL. ADJUSTED PLA SYNCHRO. OPS NORMAL IAW MM 22-31-00. 2L72 4F RTA16NE 20040223001092004022300109NE 2004 2 23 0400076632 220040106A731470680137 PUMP BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE FUEL SYSTEM MALFUNCTIONED A NWAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL01632NW 23113 715053 AT FL380, THE CREW OBSERVED DECREASING PARAMETERS ON THE NR 4 ENGINE. THE COM PROCEDURES WERE FOLLOWED BUT THE ENGINE REMAINED AT IDLE. ALL INDICATIONS REMAINED IN THE NORMAL RANGE, SO THE ENGINE WAS LEFT AT IDLE POWER. WHEN DESCENDING THROUGH 8000 FEET ON APPROACH, THE ENGINE ROLLED BACK BELOW IDLE AND THE CREW SECURED THE ENGINE. THE FLIGHT CONTINUED TO ITS DESTINATION LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN FUEL PUMP, FUEL CONTROL, AND FUEL HEAT VALVE. AN ENGINE RUN AND LEAK CHECK WERE COMPLETED WITH NORMAL INDICATIONS. 2L74 4F4 F A20WE E3NE 20040223001102004022300110 2004 2 23 GLBA2003523 420040101A3454 DISPLAY BEECH 1900 1900D 1154162CE VOR SYSTEM DEFECTIVE A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03208GL UE208 BOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, PENDING CORRECTIVE ACTION. 2L72 4T RTA24CE 20040223001122004022300112CE 2004 2 23 GLBA2003525 120040105A5610 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03100UX UE100 FO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD. 2L72 4T RTA24CE 20040223001152004022300115CE 2004 2 23 GLBA2003528 120040108A7712 CONNECTOR BEECH 1900 1900D 1154162CE TORQUE XDUCER INOPERATIVE A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03255GL UE255 104 PERCENT N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE. 2L72 4T RTA24CE 20040223001192004022300119NM 2004 2 23 UPS04441702 120040109A2133 CHECK VALVE BOEING747 747200 1384847NM CABIN PRESSURE STUCK A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01520UP 1 DECOMP LIGHT AND ALT WARNING HORN 10000 ALT CAME ON AT ALT 22000. ACCOMPLISHED RAPID DECOMP AND EMERGENCY DESCENT. CHECK LIST BUMP PUEL ATB FOUND PNEU GROUND CONNECT CHECK VALVE INTERMITTENT, STUCK OPEN POS. REMOVED AND REPLACED PNEU GND CONNECT CHECK LEFT VALVE AND CHECKED O.K. IAW MM 36-11-14ALL DOOR SEALS AND PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CONDITION INSP COMPLETE IAW AMM 05-51-08 P201. AND PRESS CONT SYS TEST O.K IAW AMM 21-31-00P 501 2L74 4F RTA20WE 20040223001222004022300122SO 2004 2 23 ACE010704 220040107A8530TISN712ACA CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED E YADAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 AL039874M998 20700745 291045R PILOT REPORTED POWER LOSS AND VIBRATION - RE-ROUTED AND MADE A SAFE LANDING. MAINTENANCE DISCOVERED THE NR 2 CYLINDER HAD 100 PERCENT HEAD SEPARATION AT THE HEAD TO BARREL INTERFACE IN LINE WITH THE TOP OF THE STEEL BARREL. 1H71 3O3 O A16CE E5CE 20040223001232004022300123EA 2004 2 23 COMA0460029 120040107A5210601R31881273 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR PANEL CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01455CA5525 7592 PAX DOOR PRESSURE PANEL CABLE (ICE BREAK) IS BROKEN AT THE END OF THE CLEAVIS DUE TO RUBBING ON THE FLAP. PAX DOOR PRESSURE PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE. THE FLAP (DECOMPRESSION PANEL) NEEDS TO HAVE A RECESSION CUT INTO THE INTERIOR LIP TO ALLOW THE CABLE MORE ROOM AND TO PREVENT IT FROM BEING BROKEN FROM NORMAL USE. 2L72 4F RTA21EA 20040223001352004022300135WP 2004 2 23 IXXA0400002O 120040110A3231 RELEASE SYSTEM DOUG DC8 DC862 3021970WP NLG STICKING A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW1131CX 777731799 45911318 DURING TAKE OFF, WHEN GEAR RETRACTED HAD EVIDENCE OF NOISE AND VIBRATRION COMING FROM NOSE GEAR AREA. GEAR WAS RECYCLED AND ALL INDICATIONS WERE NORMAL. MAINTENANCE FOUND LT FORWARD NOSE GEAR DOOR MANUAL RELEASE MECHANISM STICKING INTERMITTENTLY. MAINTENANCE LUBED MANUAL RELEASE MECHANISM AND MANUALLY CYCLED DOOR SEVERAL TIMES IAW ALL APPLICABLE MANUALS. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001362004022300136WP 2004 2 23 IXXA0400003O 120040110A3231510361 LINK ASSY DOUG DC8 DC862 3021970WP NLG BROKEN A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW1131CX 777741800 45911318 DURING CLIMB, 1550Z WHILE TRANSITIONING THROUGH FL 330 CREW SUSPECTED NOSE GEAR OPENED IN FLIGHT. SLOWED AIRCRAFT BELOW 230 DESCENDED AND RETURNED AIRPORT. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED NOSE GEAR DOOR ADJUSTMENT/TEST. FOUND LT FWD NOSE GEAR DOOR, FORWARD LINK ASSY WILL NOT LATCH - UNABLE TO ADJUST LINKAGE. MAINTENANCE REMOVED AND REPLACED LT FORWARD LINK ASSEMBLY, OPERATIONAL CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001372004022300137NE 2004 2 23 IXXA0400004O 220040111A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 1 MALFUNCTIONED A IXXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW1131CX 777841811 45911318 DURING CLIMB, THE NR 1 ENGINE WOULD NOT GO ABOVE 1.60 EPR WHEN SETTING CLIMB POWER. CREW RETURNED AIRCRAFT TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED NR 1 ENGINE FCU MOISTURE TRAP AND INSPECTED PRBC. NO DEFECTS WERE NOTED. PERFORMED ALL OPERATIONAL CHECKS IAW ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20040219001632004021900163EA 2004 2 19 SWIA200412840 120040202A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07927SW 7693 FLOOR LEVEL ESCAPE PATH LIGHTING ROWS 1-5 IS ENTIRELY INOPERATIVE. REMOVED NR 1 EMERGENCY LIGHT BATTRY PACK AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040219001642004021900164 2004 2 19 SWIA200412841 420040202A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07251YV8840 8840 120251 CAPTAIN SIDE AUTOPILOT FAILS WHEN ENGAGED EN ROUTE. FD OPERATES NORMALLY BUT AP DSC FLAG AND AP ERROR LIGHT APPEAR ON FCP AND AP CONTROL PANEL INDICATES AP DIS AND RED AP LIGHT AND AMBER FLAG ERRORS. REMOVED AND REPLACED AP CONTROL PANEL WITH NEW CONTROL PANEL IAW 24-10-04. OPS CHECK GOOD. 2L72 4T RTA31SO 20040219001652004021900165EA 2004 2 19 SWIA200412842 120040125A2730 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA RT ELEVATOR OUT OF ADJUST A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07963SW 7865 ELEVATOR INDICATION ON RT SIDE INDICATES HIGHER ON THE RIGHT SIDE IN ALL POSITIONS. ADJUSTED RT ELEVATOR POSITION TRANSMITTER IAW CRJ MM 27-34-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20040219001762004021900176NM 2004 2 19 UPS04241816 120040122A5320 BRACKET BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 NDF. REPAIR CARRIED OUT IAW SRM 51-40-04. 2L73 4F A3WE 20040219001912004021900191NM 2004 2 19 04FDEA00316 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. INBD. HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040219002132004021900213NM 2004 2 19 QXEA200400103 120040129A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PITTING CORROSION IN CUT OUT AND CHANNEL APPROXIMATELY STATION X266.0, RIGHT HAND OUTBOARD NR 10 SEAT TRACK. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20040219002202004021900220NM 2004 2 19 QXEA200400114 120040203A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2H72 4T RTA13NM 20040219002232004021900223NM 2004 2 19 QXEA200400105 120040130A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - RIGHT HAND INBOARD SEAT TRACK HAS PITTING CORROSION ON TOP END FROM FS 220.00 TO FS 246.00. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040219002312004021900231SO 2004 2 19 C2XA04TY033 120040206A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FRAME 20 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER RAMP ANGLE AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002472004021900247NM 2004 2 19 CALA0400084 120040206A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND SHEAR WEB PANEL CRACKED IN TWO PLACES AT LT FUSELAGE FORWARD OF STA 639 AT S17L. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000322004022000032WP 2004 2 20 UPS04841828 120040110A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:C1 RIGHT WHEEL WELL AFT OTBD SIDE CANTED FRAME HAS SEVERAL AREAS OF CORROSION. REMOVED -3 FRAME WHICH WAS CORRODED BEYOND LIMITS IAW DC8 SRM 53-2-0. FABBED NEW CANTED FRAME CLIP, SPLICE AND DOUBLER IAW REO G09664 AND DAC DWG 5646444. ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED -3 FRAME, CLIP, SPLICE AND DOUBLER AND -36 PNL IAW REO G09664 AND DAC DWG 5646 444. 2L74 4F RT4A25 20040220000372004022000037WP 2004 2 20 UPS04841833 120040114A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, CABIN STA 680 LONGERON 11 RIGHT SIDE FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-3-5. LOCATED NEW FITTING, DRILLED EXISTING FASTENER HOLES, DEBURRED IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040220000442004022000044WP 2004 2 20 UPS04841847 120040131A534037739061 SUPPORT FITTING DOUG DC8 DC871F 302199DWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STATION 742 RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040220000462004022000046WP 2004 2 20 UPS04841849 120040130A57515764617U51 PANEL DOUG DC8 DC871F 302199DWP LT OB.AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LT WING OUTBOARD AILERON WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN XA 614 TO XA 638. REMOVED, FABRICATED AND REPLACED WEIGHTED PANEL IAW DWG 5764617 AND DOUBLER IAW DWG 5763133 AND SRM 51-1-21, 51-3-0. 2L74 4F RT4A25 20040220000552004022000055NM 2004 2 20 AWXA200400159 120040208A3150 WARNING LIGHT AIRBUSA319 A319132 3930340NM COCKPIT ILLUMINATED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28822AW 1410 LAS - ABORTED TAKEOFF - FLT 0108 - DURING TAKEOFF AT LAS EN ROUTE FOR LAX RECEIVED ECAM MESSAGES FOR VENT SKIN VALVE FAULT AND VENT AVIONICS SYSTEM FAULT, REJECTED TAKEOFF AT 70 KTS. MAINTENANCE RESET THE AEVC SYSTEM, OPERATIONAL CHECK WAS GOOD IAW AMM TASK 21-26-00-810-830. 2L72 4F RTA28NM 20040220000632004022000063NM 2004 2 20 AALA20040189 120040208A3350 LIGHT BOEING757 757223 1384957NM R1 DOOR BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21174AA 31308 ORD EMERGENCY EXIT LIGHT AT R1 DOOR HAS BROKEN BASE PLATE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220000662004022000066NM 2004 2 20 AALA20040196 120040206A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 DFW SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220000752004022000075CE 2004 2 20 58598 120040205A5210MS166241075 HANDLE BEECH 1900 1900D 1154162CE PAX DOOR SEPARATED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07142YV UE142 WHEN PREPARING TO BOARD, DOOR HANDLE CAME OFF IN THE PILOTS HAND. MX VERIFIED INDOOR HANDLE. PLANE WAS FERRIED TO LIT FOR REPAIR. REMOVED OUTSIDE DOOR HANDLE RETAINER. REINSTALLED HANDLE AND NEW SNAP RING. ALSO, REINSTALLED HANDLE ASSY, OPS CHECK NORMAL. 2L72 4T RTA24CE 20040220000762004022000076SO 2004 2 20 SWIA200412848 120040114A5210 CHANNEL EMB 120 EMB120ER 3260203SO PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 PAX DOOR MID SECTION OF DOOR AFT CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION AFT AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20040220000802004022000080EA 2004 2 20 SWIA200412852 120040203A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS OUTBOARD ATTACH ANGLE CRACKED AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM. 2L72 4F RTA21EA 20040220000872004022000087SO 2004 2 20 LR7A04003 120040124A5330 SKIN LKHEED382 382G 526414USO FS CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND DENT AND SCRATCHES ON BELLY SKIN AT FS 718 BL 58R. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 718 RBL 58. 2H74 4T A1SO 20040220000912004022000091SO 2004 2 20 LR7A04007 120040124A5312 CAP LKHEED382 382G 526414USO RT MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND HAIRLINE CRACK RT MWW INTERCOSTAL BEAM O/B CAP AT FS 479 WL 200. BEAM CAP REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 RBL 62. 2H74 4T A1SO 20040220000972004022000097SO 2004 2 20 LR7A04013 120040124A5330 SKIN LKHEED382 382G 526414USO FUSLEAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT FUSELAGE LT SKIN CRACKED AT FS 860 WL 200 BL 82L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-10, FS 860 WL 200 LBL 82. 2H74 4T A1SO 20040220001052004022000105SO 2004 2 20 LR7A04021 120040124A5320 BRACKET LKHEED382 382G 526414USO MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND LT MLG WHEEL WELL FS 491 WL 200 BL 61 BRACKET CRACKED AT TOP CORNER. BRACKET REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 491 WL 200 LBL 61. 2H74 4T A1SO 20040220001082004022000108SO 2004 2 20 LR7A04024 120040124A5523 RIB LKHEED382 382G 526414USO LT ELEVATOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND LT ELEVATOR TRIM TAB WELL RIB CRACK AT HSS 87 & 97 DURING STRAP REMOVAL FOR REPLACEMENT. RIB AT HS87 & 97 REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS 87/HSS 97 LT. 2H74 4T A1SO 20040220001132004022000113WP 2004 2 20 04FDEA00365 120040208A78309152M45P004A RIB DOUG DC10 DC1010 3022110WP THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-73868 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM. 2L73 4F A22WE 20040220001142004022000114NM 2004 2 20 04FDEA00357 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001152004022000115NM 2004 2 20 04FDEA00356 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001272004022000127WP 2004 2 20 04FDEA00341 120040206A5753NRC6068509 VANE DOUG DC10 DC1010 3022110WP ZONE 500 BROKEN A FDEAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25363FE3277 48263 JUST PRIOR TO PUSHBACK FORT WORTH POLICE DEPT. REPORTED AN A/C PART HAD COME OFF A FEDEX A/C. LOWERED FLAPS AND FOUND LEFT O/B FLAP VANE HAD APPROX 5 FOOT MISSING. HONEYCOMB HAD BROKEN OFF INBOARD END. A/C NOT SAFE FOR FLIGHT. VANE IS IN WORK. INSTALLED LT OUTBOARD FLAP VANE IAW MM 27-50-03-2, AND FLAP VANE OPS CHECKS NORMAL. AS PRECAUTIONARY CHECKED LT OUTBOARD FLAP FOR DAMAGE, NONE FOUND, AND FLAP VANE SPRING FOR SECURITY AND DAMAGE, NONE FOUND. ALSO CHECKED VANE TRACKS AND ROLLERS FOR SECURITY AND OPERATION, NO DEFECTS NOTED. OKAY FOR SERVICE. 2L73 4F A22WE 20040220001302004022000130SO 2004 2 20 C2XA04CL011 120040209A335066903 LIGHT EMB 135 EMB135ER 3260203SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716501 145145 CLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040220001332004022000133 2004 2 20 2004UALA00026 420040109A2210MR22176 COUPLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE YAW DAMPER MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29331UA 24192 YAW DAMPER TRIPPED OFF. *S/D* REPLACED YAW DAMPER COUPLER. 2L72 4F4 FRTA16WE E2GL 20040220001382004022000138EU 2004 2 20 04019303 120040129A5320 ANGLE JETAIRJETSTMJETSTM4101 1500501EU FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 DURING HEAVY CHECK THE ANGLE BRACKET AT STATION 4, 7 O`CLOCK POSITION WAS FOUND CRACKED. A NEW BRACKET WAS INSTALLED. AIRCRAFT WAS RELEASED FOR SERVICE UPON INSPECTION COMPLETION. 2L72 4T RTA41NM 20040220001432004022000143NM 2004 2 20 QXEA200400120 120040209A2133 SEAL BOMBDRDHC8 DHC8401 1390041NM OUTFLOW VALVE FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09415QX 4081 SMF - FLIGHT 2438 - AIRCRAFT FAILED TO PRESSURIZE ON CLIMBOUT AND THE CREW RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SYSTEM ON MEL. MAINTENANCE REPLACED THE SEAL ON THE AFT PASSENGER DOOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040220001452004022000145EA 2004 2 20 04021684 120040121A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27684BR 7708 DURING INSPECTION THE LEFT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001552004022000155NM 2004 2 20 04FDEA00368 120040206A5311ADA0049 FRAME DOUG MD11 MD11 3023602NM ZONE 200 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25604FE 48460 CABIN - PREVIOUS FRAME REPAIR AT RIGHT STA 1541 STR 12 - 13 WAS FOUND SECURED WITH RIVETS, INSTEAD OF HI-LOKS. CABIN - PREVIOUS FRAME REPAIR AT RT STA 1541 STR 12 - 13 DOUBLER REMOVED AND REPLACED IAW SRM 53-30-00 FIG 1 VOL I WITH REF TO EA 1-5310-74305, FUSELAGE - MAIN FRAME - TRACKING OF CATEGORY-B REPAIRS ON FRAME. 2L73 4F RTA22WE 20040220001642004022000164NM 2004 2 20 04FDEA00385 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13. CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001702004022000170EU 2004 2 20 04029314 120040129A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27314UE 41027 DURING INSPECTION THE RIGHT HAND FORWARD EXTERIOR BULB WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040220001742004022000174NM 2004 2 20 HNAA0400009 120040209A2751 WARNING HORN DHAV DHC8 DHC8102 2809003NM TE FLAPS ACTIVATED A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07937HA 148 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. RE-SELECTED FLAPS TO 5 DEGREES. 2H72 4T RTA13NM 20040220001802004022000180NM 2004 2 20 CALA0400095 120040209A5730 SKIN BOEING757 757224 1384958NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717126 27566 INSPECTION FOUND MULTIPLE CRACKS IN LT WING L/E SKIN AT O/B END OF NR 4 SLAT, OSS 430. THE LONGEST CRACK WAS SIX INCHES. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, SEQ 399. 2L72 4F RTA2NM 20040220001902004022000190 2004 2 20 AWXA200400163 420040117A256565659723 PLATE BOEING737 737277 1384570NM GIRT BAR ADAPTERCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - EES - DURING C-15 CHECK CORROSION WAS FOUND IN L-2 DOOR GIRT BAR FITTING ADAPTER PLATE BS 328, LBL 74. MAINTENANCE REMOVED AND REPLACED L-2 DOOR GIRT BAR FITTING ADAPTER PLATE IAW T/C C1D25006. 2L72 4F RTA16WE 20040220001962004022000196WP 2004 2 20 AALA20040210 120040207A2170 COALESCER BAG DOUG DC9 DC982 3022082WP CABIN AIR DIRTY A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21286AA 49298 MIA INFLIGHT T1968/07, FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN IMMEDIATELY AFTER TAKEOFF. THE PACKS WERE TURNED OFF BUT SMOKE WAS NOT CLEARING. RETURNED TO STATION. LANDED WITHOUT INCIDENT. SMOKE CLEARED UPON LANDING. VISUAL CHECK DETECTED NO SIGN OF FIRE OR SMOKE. PERFORMED PACK BURN. REPLACED AIR CONDITIONING PILOT PRESSURE, REPLACED THERMAL SWITCH CONTROL, REPLACED COALESCER AND WATER SEPARATOR ASSEMBLY, COALESCER BAGS, ALTITUDE BAGS, AND BIAS SOLENOID VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040223000202004022300020EU 2004 2 23 06041 120040105A26131734362 DETECTOR SAAB SF340 340B 7860101EU TAILPIPE INOPERATIVE A NSVAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA27252CJ 340B252 TAIL PIPE HOT ANNUNCIATION FOR LT ENGINE DURING CLIMBOUT. REDUCED POWER IAW CHECKLIST, LIGHT REMAINED ILLUMINATED, EXECUTED PRECAUTIONARY IN-FLIGHT ENGINE SHUTDOWN. REMOVED AND REPLACED THREE ENGINE DETECTORS IAW MM. ENGINE RUN, NO DISCREPANCIES NOTED. 2L72 4T RTA52EU 20040223000712004022300071SO 2004 2 23 SWIA200412744 120040102A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO RT NACELLE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07251YV8796 8796 120251 FLAP DISAGREEMENT DURING RETRACTION. RT NACELLE FLAP ACTUATOR FOUND TO BE BYPASSING. REPLACED RT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW 27-50-08. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040223000802004022300080EA 2004 2 23 COMA0460026 120040107A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01815CA9312 7397 THE UNDER FLOOR SUPPORT ANGLE P/N 601R35031-239 IS CRACKED AT FS 621.9 WL 73, LBL 41.5 AND RBL 41.5. REMOVED THE CRACKED AREAS AND INSTALLED REPAIR PARTS IAW REO 601R-53-61.117 REV.B. 2L72 4F4 FRTA21EA E15NE 20040223001042004022300104NM 2004 2 23 DHL2004745002 120040109A3260 SWITCH BOEING727 727224 1384076NM MLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 REF. LOG PAGE NR 370129; AFTER GEAR RETRACTION WITH GEAR HANDLE SET TO OFF BOTH FORWARD RED DOOR ANNUNCIATOR LIGHT AND RED GEAR DOOR S/O'S ANNUNCIATOR PANEL AMBER LIGHT ILLUMINATED. PERFORMED ABNORMAL AND SET GEAR HANDLE UP, BOTH LIGHTS OUT. ADJUSTED RT GEAR DOOR ACTUATOR SWITCH IAW BMM CHAPTER 32-12-01, OPS CHECKED GOOD ON GROUND. 2L73 4F A3WE 20040223001112004022300111 2004 2 23 GLBA2003524 420040105A3414 INDICATOR BEECH 1900 1900D 1154162CE AIRSPEED INTERMITTENT A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03170GL UE170 CAPT HAS NO AIRSPEED IND, ASI STARTED WORKING ABOUT HALF WAY TO DEN ON FERRY FLIGHT. DID PITOT STATIC TEST, OPS CK GOOD 2L72 4T RTA24CE 20040223001342004022300134WP 2004 2 23 IXXA0400001O 120040109A3231 DOOR DOUG DC8 DC862 3021970WP NLG UNLATCHED A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW1131CX 777661793 45911318 AFTER TAKE OFF AND GEAR RETRACTION, CREW NOTICED A VIBRATION AND NOISE. CREW RECYCLED LANDING GEAR, DID NOT CORRECT PROBLEM. SUSPECT NOSE GEAR DOOR NOT CLOSE PROPERLY. CREW CONTINUED FLIGHT TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENACE PERFORMED FUNCTIONAL CHECK OF LOCKING MECHANISM OF LT AND RT NOSE LANDING GEAR. OPERATIONAL CHECK GOOD ON GROUND IAW ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001422004022300142NM 2004 2 23 2004UALA00011 120040106A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSLEAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 CABIN SHEAR TIES CRACKED AT STA BS706 S11R BS440 S16R. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040223001442004022300144NM 2004 2 23 2004UALA00015 120040107A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29385UA 24660 STR SPLICE IS CRACKED BETWEEN 2 RIVETS AT BS 907 S4L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SHEAR CLIP AND STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040223001452004022300145NM 2004 2 23 2004UALA00021 120040109A5320 DOUBLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE WEB GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 WEB DOUBLER GOUGED AT BS 187 WL 207 RBL 28. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040223001462004022300146WP 2004 2 23 0400109906 120040105A5312 CHANNEL DOUG DC9 DC931 3022065WP PRESS BULKHEAD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01956N 47252 DURING L-CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD CHANNEL. REPAIRED IAW EA 99-197419. 2L72 4F A6WE 20040223001632004022300163WP 2004 2 23 0400119867 120040112A2120 DUCT DOUG DC9 DC951 3022051WP RT ACM LOOSE A NWAAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 GL01776NC 47786 AT REACHING FL330, THE CABIN CONTINUED TO CLIMB. CREW WAS NOT ABLE TO CONTROL CABIN CLIMB SO AN EMERGENCY DESCENT WAS PERFORMED. ACCOMPLISHED COM PROCEDURES. CABIN ALTITUDE DID NOT EXCEED 11,500 FEET AND MASKS WERE NOT DEPLOYED. FLIGHT CONTINUED AT 10,000 FEET AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE DUCT TO THE RIGHT ACM COMPRESSOR INLET OFF. RE-ATTACHED THE DUCT. SYSTEM LEAK CHECK OK. 2L72 4F RTA6WE 20040223001692004022300169SW 2004 2 23 2004F00037 120040113A243651509002B GCU SWRNGNSA227 SA227AC 8780603SW LT GENERATOR FAILED E C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL27371PH AC576 WHILE ON THE TAKEOFF ROLL, THE LT GENERATOR FAIL WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND MAINTENANCE WAS NOTIFIED. UPON INVESTIGATION, IT WAS DETERMINED THAT THE GENERATOR CONTROL UNIT FAILED. 2L72 4T RTA8SW 20040223001802004022300180EU 2004 2 23 CX7A194J0402 120040113A26131734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE FALSE ACTIVATIONA CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03307CE 340B204 RT TAILPIPE HOT LIGHT ILLUMINATED DURING TEST. 2L72 4T RTA52EU 20040223001822004022300182NM 2004 2 23 SCNA04001 120040113A3350 LAMP BOEING737 737 UTILSYSNM EMERGENCY LIGHT BURNED OUT A SCNAO OTHER O OTHER LDLANDING 1 GL15PHHZC 28379 LT AFT OVERWING WARNING LIGHT ON OVERHEAD PANEL BURNED OUT. RELAMPED OVERWING WARNING LIGHT AS REQUIRED. 2L72 4F RTA16WE 20040223001952004022300195EU 2004 2 23 AALA20040064 120040113A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211443A 11446 ORD CEILING EMERGENCY LIGHTS AT LT AND RT HATCH EXIT ABOVE 17D AND 12D AND UPPER RT FUSELAGE INOPERATIVE. REPLACED BATTERY PACK FOR LT AND RT HATCH EXIT ABOVE 17D AND 12D AND UPPER RIGHT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RT 20040223001972004022300197SO 2004 2 23 RAIA00401003 120040104A3610S242226 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR SYS BLOWN A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 BLEED NR 2 LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED RT BLEED DUCT O-RING IN AFT CARGO BAY. 2L72 4T RTT00011AT 20040223002002004022300200EA 2004 2 23 MASA200400007 120040104A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0717231 7231 DURING CLIMB OUT, A FLAP FAIL CAUTION MSG OCCURED. AIRCRAFT RETURNED TO FIELD WHERE MECHANIC COMPLIED WITH PART "A" OF FLAP FAIL PROCEDURES AND AN OVER WEIGHT LANDING INSPECTION. NO DEFECTS WERE NOTED. A/C WAS RETURNED TO SERVICE. NO PARTS USED 2L72 4F RTA21EA 20040223002022004022300202NM 2004 2 23 COOSDR030032 120040101A5514 ATTACH FITTING BOEING737 737300 1384610NM HORIZONTAL STAB CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23318FL 26293 LT HORIZONTAL STABILIZER FRONT SPAR, LOWER ATTACH LUG SURFACE CORRODED. 2L72 4F RTA16WE 20040223002032004022300203NM 2004 2 23 COOSDR030033 120040101A57556517347 SKIN BOEING727 72731 1384010NM NR 2 SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 LT WING, SPOILER NR 2, UPPER SURFACE IB AND OB, SKIN DELAMINATED. 2L73 4F A3WE 20040223002052004022300205NM 2004 2 23 COOSDR030035 120040101A5755 SKIN BOEING727 72731 1384010NM LT WING SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 LT WING, SPOILER NR 4, UPPER SURFACE IB END FORWARD SECTION DELAMINATED. 2L73 4F A3WE 20040223002062004022300206NM 2004 2 23 COOSDR030036 120040101A5755 SKIN BOEING727 72731 1384010NM RT WING SPOILER DELAMINATED A EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE TO85 18905 RT WING, TE SECTION SPOILER NR 9, UPPER SURFACE, DELAMINATED. 2L73 4F A3WE 20040223002102004022300210NM 2004 2 23 COOSDR030039 120040101A5511 RIB BOEING727 72731 1384010NM HORIZONTAL STAB CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 LT HORIZONTAL STABILIZER, ELEV. STA 17.20 ELEVATOR HINGE, OB AFT END, SUPPORT RIB, CRACKED. 2L73 4F A3WE 20040223002122004022300212NM 2004 2 23 COOSDR030041 120040101A5753 SKIN BOEING727 72731 1384010NM TE FLAP DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 LT WING IB MID FLAP DELAMINATED. 2L73 4F A3WE 20040223002132004022300213NM 2004 2 23 COOSDR030043 120040101A572065508191014 ANGLE BOEING737 737200 1384453NM RT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, TRAILING EDGE - RSS486, ANGLE CORRODED. 2L72 4F A16WE 20040223002142004022300214NM 2004 2 23 COOSDR030044 120040101A571265479342 RIB BOEING737 737200 1384453NM RT WING CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, FSS 263 LEADING EDGE RIB CRACKED. 2L72 4F A16WE 20040223002152004022300215NM 2004 2 23 COOSDR030045 120040101A571265479352 RIB BOEING737 737200 1384453NM RT WING CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, FSS 266 LEADING EDGE RIB CRACKED. 2L72 4F A16WE 20040223002172004022300217NM 2004 2 23 COOSDR030047 120040101A5320 CHANNEL BOEING737 737200 1384453NM MLG CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT MAIN LANDING GEAR CHANNEL. 2L72 4F A16WE 20040224000032004022400003NM 2004 2 24 COOSDR030050 120040101A57306550820 PANEL BOEING737 737200 1384453NM RT WING DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, FIXED PANEL PN 65-50820-142, TMC-284 DELAMINATED. 2L72 4F A16WE 20040224000042004022400004NM 2004 2 24 COOSDR030051 120040101A5753656715616 FLAP TRACK BOEING737 737200 1384453NM LT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 LT WING, FLAP TRACK NR 2 CORRODED. 2L72 4F A16WE 20040224000072004022400007NM 2004 2 24 N770AN 120040116A5753113W93391 HINGE BOEING777 777223 1385213NM TE FLAP MISSING D AALAO OTHER O OTHER NRNOT REPORTED 1 GL13770AN 29578 HINGE BROKEN, SEAL AND BRACKET ASSY DEPARTS THE AIRCRAFT. 2L72 4F RTT00001SE 20040224000082004022400008 2004 2 24 GLBA20030532 420040115A34006226137201 RECEIVER BEECH 1900 1900D 1154162CE NR1 NAV FAILED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03208GL2379 UE208 NR 1 NAV FAILED, REMOVED AND REPLACED NR 1 NAV RECEIVER PN 622-6137-201. 2L72 4T RTA24CE 20040224000092004022400009EA 2004 2 24 ASOA04009 120040105A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11846AS10982 7328 DURING TAKEOFF, THE CREW RECEIVED A FLAPS FAIL MESSAGE WHEN SELECTING THE FLAPS TO ZERO DEGREES. QRH PROCEDURES WERE COMPLIED WITH AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ICT AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAPS AND RESET THE FLAPS ELECTRONIC CONTROL UNIT USING THE BREAKERS IAW ASA EO 600-27-0004A. (M) 2L72 4F RTA21EA 20040224000102004022400010EU 2004 2 24 ASOA04029 120040110A3050E420361 RESISTOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE ELE ANTI HORN MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO11530AS 453 DURING CLIMB-OUT, THE CREW RECEIVED A RUDDER AND LT ELEVATOR HEAT FAULT. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AC LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT ELEVATOR ANTI-HORN RESISTOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20040224000112004022400011EA 2004 2 24 ASOA04017 120040106A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE RT INTERCOSTAL CLIP AT APPROXIMATELY FS 484 IB AND OB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT INTERCOSTAL CLIP AT APPROXIMATELY FS 484 IB AND OB IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20040224000122004022400012EA 2004 2 24 ASOA04016 120040106A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE LT INTERCOSTAL AT FS 484, BL 27-36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT INTERCOSTAL AT FS 484, BL 27-36 IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20040224000132004022400013EA 2004 2 24 ASOA04015 120040106A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR FRAME CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040224000142004022400014EA 2004 2 24 ASOA04014 120040106A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000152004022400015EA 2004 2 24 ASOA04013 120040106A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA SILL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK, THE CARGO SILL PLATE UNDER THE FORWARD ATTACH BRACKET AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO SILL PLATE UNDER THE FORWARD ATTACH BRACKET AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040224000172004022400017EU 2004 2 24 ASOA04019 120040107A7712311649902 PROBE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE ENG TORQUE INOPERATIVE A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO11535AS 464 DURING CRUISE, THE CREW EXPERIENCED A SIGNIFICANT POWER FLUCTUATION ON RT ENGINE AND SHORTLY AFTER LEVELING OFF AT 11,000 FEET AIRCRAFT YAWED TO RT. THE CREW NOTED THE RT ENGINE TORQUE GAUGE NEEDLE INCREASED TO 120 PERCENT, WHILE THE DIGITAL GAUGE SIMULTANEOUSLY DECREASED TO 25-30 PERCENT. THE FLUCTUATION AND YAW TO THE RT OCCURRED TWICE. AFTER ADVANCING THE CONDITION LEVERS TO 100 PERCENT NP, THE RT ENGINE STABILIZED. BOTH ENGINES OPERATED WITHIN NORMAL LIMITS DURING THE REMAINDER OF THE FLIGHT. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT TORQUE PICK-UP PROBE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20040224000202004022400020EA 2004 2 24 A6WA200440005 120040110A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL31443AW 7781 SMOKE TOILET CAS MESSAGE ON TAXI, COMPLIED WITH QRH. FIRE DEPARTMENT INSPECTED LAV, NO EVIDENCE OF SMOKE OR FIRE. INSTALLED SMOKE DETECTOR AFT LAV, TESTED OK. REMOVED FROM MEL. (M) 2L72 4F RTA21EA 20040224000232004022400023EA 2004 2 24 ASOA04028 120040109A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11909EV 7658 DURING HANGAR MAINTENANCE, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040224000242004022400024EA 2004 2 24 ASOA04030 120040111A5346 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ENG SUPPORT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11880AS 7606 DURING AN A-CHECK, THE LT FORWARD IB CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT FORWARD IB CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F4 FRTA21EA E15NE 20040224000252004022400025EA 2004 2 24 ASOA04021 120040107A33974871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING HANGAR MAINTENANCE, THE EMERGENCY FLOOR LIGHTING FROM ROW 6 C/D AFT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS AT ROW 6 C/D AFT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000262004022400026EA 2004 2 24 ASOA04020 120040107A5260601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 FLT 4858 - DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000282004022400028EU 2004 2 24 A6WA200460001 120040105A492038000864 APU BAC 146 146200A 1500266EU APU BAY INOPERATIVE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31607AW E2052 SMOKE IN CABIN WHEN APU IS SUPPLYING AIR TO PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND REMOVED AND REPLACED APU. (M) 2H74 4F A49EU 20040224000292004022400029EA 2004 2 24 A6WA200440004 120040109A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR INOPERATIVE A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401AW 7280 DURING CLIMB-OUT, AMBER DOOR LATCH CAS MESSAGE, FOLLOWED QRH. AT APPROXIMATELY FL20.0 RED PASSENGER DOOR MESSAGE ILLUMINATED FOLLOWED QRH DIVERTED. INSPECTED DOOR ALIGNMENT PINS AND INTERROGATED PSEU. FOUND 3 FAULTS ON PSEU. DOOR CLOSES AND LOCKS NORMALLY. PRESSURIZED CABIN TO 5 PSID. ADJUSTED PASSENGER DOOR OUTER HANDLE IAW 52-11-03. OPS CHECK GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20040224000302004022400030EU 2004 2 24 USAASA04005 120040115A492020499004 FILTER AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE OZONE CONTAMINATED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19107US 1052 EN ROUTE, CREW RECEIVED AN ECAM WARNING FOR SMOKE IN AN AFT LAV. NO FIRE OR SMOKE WAS FOUND. A SECOND ECAM ALERT WAS RECEIVED FOR THE OTHER AFT LAV. AGAIN, NO EVIDENCE OF A FIRE WAS FOUND. SHORTLY THEREAFTER, A WARNING WAS RECEIVED FOR THE FORWARD LAV. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LT OZONE FILTER CONTAMINATED WITH AN OIL FILM FROM PREVIOUS APU OIL LEAK. REPLACED BOTH LT AND RT OZONE FILTERS, RECIRCULATION FILTERS, AND LAVATORIES A, D, AND E SMOKE DETECTORS. ALSO, PERFORMED A (RESIDUAL BURNING) CLEANING OF THE ENGINES, APU, AND CROSSBLEED DUCTS. OPS CHECKED OK. (M) 2L72 4F4 FRTA28NM E2GL 20040224000312004022400031NM 2004 2 24 USAABB04015 120040129A3150 WARNING LIGHT BOEING767 7672B7 1385107NM GE CF6 CF680 30025NE COCKPIT FALSE ACTIVATIONA USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19651US 24764 EN ROUTE, THE CREW RECEIVED THE E/M'S (AILERON LOCKOUT) AND (FLAP/SLAT ELEC). FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURES FOR BOTH SYSTEMS. NO FAULTS FOUND. AIRCRAFT RELEASED FOR VERIFICATION FLIGHT. (M) 2L72 4F4 FRTA1NM E13NE 20040224000322004022400032EA 2004 2 24 ASOA04059 120040122A5210600380745 FITTING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11703EV 10038 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE REMOVED AND REPLACED THE ANCHOR FITTING ON THE PASSENGER DOOR COUNTERBALANCE SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040224000332004022400033EA 2004 2 24 ASOA04058 120040123A5210 STEP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11703EV 10038 DURING A C-CHECK IN MCN, THE TOP AND BOTTOM STEPS WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP P/N 601R3167017, AND BOTTOM STEP P/N 601R3198067. (M) 2L72 4F4 FRTA21EA E15NE 20040224000352004022400035EU 2004 2 24 USAASA04007 120040125A3397 WIRE AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19762US 1358 THE SEAT MOUNTED EMERGENCY LIGHT ON SEAT 3L WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (M) 2L72 4F4 FRTA28NM E2GL 20040224000362004022400036EU 2004 2 24 USAABA04001 120040202A3350321431 BATTERY PACK AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19676UW 0375 EPSU 11 WL FAULTED DURING TEST. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F RTA46NM 20040224000402004022400040EU 2004 2 24 USAASA04006 120040117A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW 1112 DCA - FOUND INTERNAL FAULT ON LEFT EPSU. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA28NM 20040224000412004022400041EU 2004 2 24 USAASA04009 120040128A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19714US 1046 DCA - THE EMERGENCY LIGHTS WOULD NOT PASS THE SELF TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MID CABIN, RIGHT HAND POSITION. OPS CHECKED OK. (M) 2L72 4F RTA28NM 20040224000432004022400043EA 2004 2 24 A6WA200440014 120040131A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 FOUND SKIN DAMAGED, LEFT SIDE OF AIRCRAFT AT FS 682 TO FS 718 BETWEEN STRINGERS 16L AND 18L. (M) 2L72 4F RTA21EA 20040224000462004022400046EA 2004 2 24 ASOA04054 120040120A3231750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG DOOR INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11884AS 7513 DURING CRUISE FROM ATL-MTY, THE NOSE GEAR DOOR OPENED UNCOMMANDED AND THE CREW RECEIVED A GEAR DISAGREE WARNING ACCOMPANIED BY AN AIR DISTURBANCE AND A VIBRATION IN THE AIRCRAFT. THE CREW REDUCED AIR SPEED TO 250 KIAS AND THE WARNINGS WENT AWAY WITH EVERYTHING RETURNING TO NORMAL. THE AIRCRAFT DIVERTED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SELECTOR VALVE AND THE NLG SELECTOR VALVE. OPS CAND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000472004022400047 2004 2 24 USAASA04010 420040129A2565 SLIDE AIRBUSA319 A319112 3930323EU PAX DOOR DEPLOYED A K NONE W INADEQUATE Q C ININSP/MAINT 1 EA19740UW 1265 PRIOR TO DEPARTURE, THE MAIN ENTRY DOOR WAS OPENED WHILE THE SLIDE WAS ARMED. THE SLIDE DID NOT INFLATE. MAINTENANCE REMOVED THE SLIDE AND DEPLETED THE AIR PRESSURE FROM THE CYLINDER. AIRCRAFT FERRIED FOR MAINTENANCE TO PIT. THE SLIDE WAS REPLACED. IN THE SHOP, THE SLIDE TIME CONTINUATION TASK WAS PERFORMED. OK FOR SERVICE. 2L72 4F RTA28NM 20040223000392004022300039SO 2004 2 23 RAIA00401001 120040104A3230 CONNECTOR EMB 145 EMB145LR 3260212SO MLGEU DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03827HK 145021 5621-STL- LANDING GEAR AIR GROUND FAIL MESSAGE. MAINTENANCE CLEANED ELECTRICAL CONNECTOR ON LANDING GEAR ELECTRONIC UNIT. 2L72 4T RTT00011AT 20040223000722004022300072SO 2004 2 23 SWIA200412745 120040103A272155298 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07564SW 120339 UNABLE TO USE RUDDER TRIM AT HIGH ALTITUDES AND COLD TEMP. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW EMB 120 MM 27-23-02. OPS CK GOOD. 2L72 4T RTA31SO 20040223000872004022300087EU 2004 2 23 AWXA200400020 120040106A3510MXP801 STOWAGE BOX AIRBUS320 A320232 3930326EU ZONE 212 STICKING A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28650AW 856 MCI - DIVERSION - FLT 0688 - EN ROUTE, 2 HOURS AND 20 MINUTES INTO FLIGHT, CREW OXYGEN PRESSURE INDICATED 20 PSI, DIVERTED. MAINTENANCE FOUND FIRST OFFICERS MASK TEST BUTTON STUCK KEEPING VALVE PARTIALLY OPEN, AFTER TAPPING ON BUTTON THE VALVE RESET, OPERATIONAL TEST WAS PERFORMED SEVERAL TIMES WITH NO DISCREPANCIES NOTED. REMOVED AND REPLACED CREW OXYGEN BOTTLE, LEAK CHECK WAS GOOD. WHEN AIRCRAFT ARRIVED, MAINTENANCE REPLACED THE FIRST OFFICERS OXYGEN MASK STOWAGE BOX IAW AMM 35-12-41-401, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20040223001132004022300113SO 2004 2 23 GLBA2003526 120040105A3210 LANDING GEAR EMB 120 EMB120ER 3260203SO RIGHT INOPERATIVE A GLBAO OTHER J WARNING INDICATION CLCLIMB 1 NM03299UX 120299 RT MAIN LANDING GEAR WILL NOT RETRACT, PENDING CORRECTIVE ACTION 2L72 4T RTA31SO 20040223001142004022300114CE 2004 2 23 GLBA2003527 120040107A2750 FLAP BEECH 1900 1900D 1154162CE WING STUCK A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03154GL UE154 FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION 2L72 4T RTA24CE 20040223001172004022300117 2004 2 23 GLBA20030524 420040105A3414 INDICATOR BEECH 1900 1900D 1154162CE AIRSPEED INTERMITTENT A GLBAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NM03170GL UE170 CAPT HAS NO AIRSPEED INDICATION, ASI STARTED WORKING ABOUT HALF WAY ON FERRY FLIGHT. DID PITOT STATIC TEST OPS CK GOOD. 2L72 4T RTA24CE 20040223001202004022300120NM 2004 2 23 UPS04541697 120040108A2612 FIRE WARNING BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE CARGO BAY FALSE INDICATIONA IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01411UP 23851 AT 3000 FEET ON APP INTO SAT WE RECEIVED A MASTER WARNING AND CARGO FIRE BELL WITH ICAS MESSAGE. IT WENT OUT ABOUT A SECOND LATER, T/S IAW FIM 26-16-00 SHEETS 1-9 SYS. OPS CKS OK, OK FOR SERVICE. 2L72 4F4 FRTA2NM E17NE 20040223001812004022300181NM 2004 2 23 N136FE0401 120040113A555065982962 HINGE BOEING727 72725C 138400HNM GROUND SPOILER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 136 61773 19855 DURING SERVICE CHECK, FOUR CRACKS WERE FOUND ON THE NR 7 GROUND SPOILER SUPPORT HINGE. HINGE REPLACED WITH NEW PART. ALL HINGES INSPECTED FOR CRACKS, NO FAULTS FOUND. 2L73 4F A3WE 20040223001942004022300194WP 2004 2 23 AALA20040063 120040112A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21298AA 49310 DEN EMERGENCY LIGHT AT OVERHEAD AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040223002012004022300201NM 2004 2 23 COOSDR030029 120040101A531165163008687 FRAME BOEING737 737300 1384610NM BULKHEAD CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23318FL 26293 BS 178, RBL 28 AND LBL 28, SIDE CHORDS CRACKED. 2L72 4F RTA16WE 20040223002072004022300207NM 2004 2 23 COOSDR030037 120040101A5755651734748 SKIN BOEING727 72731 1384010NM RT WING SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 RT WING, SPOILER NR 14, LOWER SURFACE DELAMINATED. 2L73 4F A3WE 20040223002082004022300208NM 2004 2 23 COOSDR030038 120040101A5755 SKIN BOEING727 72731 1384010NM SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SW23220NE 502 18905 RT WING, SPOILER NR 11, LOWER SURFACE DELAMINATED. 2L73 4F A3WE 20040223002162004022300216NM 2004 2 23 COOSDR030046 120040101A5755 SKIN BOEING737 737200 1384453NM SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW BN073 20258 RT WING, FLIGHT SPOILER NR 7 UPPER SURFACE DELAMINATED. 2L72 4F A16WE 20040224000022004022400002NM 2004 2 24 COOSDR030049 120040101A572069464978 CHANNEL BOEING737 737200 1384453NM RT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING TRAILING EDGE CAVITY UPPER FIXED PANEL CHANNEL CORRODED. 2L72 4F A16WE 20040224000182004022400018EA 2004 2 24 ASOA04012 120040106A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK, THE CARGO COMPARTMENT AFT FLOOR SUPPORT ANGLES ON THE LT AND RT SIDES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT FLOOR SUPPORT ANGLES ON THE LT AND RT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040224000342004022400034EU 2004 2 24 USAASA04008 120040126A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19751UW5599 1317 MAINTENANCE FOUND THE MID RIGHT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REPLACED MID RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F4 FRTA28NM E2GL 20040224000372004022400037EA 2004 2 24 ASOA04057 120040121A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11867AS 7463 DURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW TEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040224000382004022400038EA 2004 2 24 ASOA04056 120040121A33974871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000582004022400058EA 2004 2 24 ASOA04027 120040109A27419960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM JAMMED A ASOAO OTHER G MULTIPLE FAILURE CLCLIMB 1 SO11904EV 7628 DURING CLIMB-OUT FROM MEM-DFW, AT APPROXIMATELY 9,000 FEET THE STAB TRIM AND MACH TRIM DISENGAGED. THE TRIM WOULD NOT RESET AND WAS LAST POSITIONED AT THREE DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000632004022400063CE 2004 2 24 DXTA200400239 120040209A2821 FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL SYSTEM BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07960QS 7500160 CAE330339 ON TAKEOFF ROLL THE FUEL FILTER BYPASS L AMBER MESSAGE ILLUMINATED, REJECTED TAKEOFF. REMOVED AND REPLACED FUEL FILTER AND O-RING, RAN ENGINE FOR OPS CHECK AND LEAK CHECK. ALL WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 73-30-00. 2L72 4J4 FRTT00007WITE6CH 20040224000642004022400064EA 2004 2 24 040038662 120040207A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27662BR 7526 DURING INSPECTION THE RIGHT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000662004022400066EU 2004 2 24 04038333 120040207A33503022471 LIGHT JETAIRJETSTMJETSTM4101 1500501EU LT OVERWING INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27333UE 41101 DURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY WAS FOUND INOPERATIVE. THE ASSEMBLY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040224000672004022400067NM 2004 2 24 04040405 120040209A33508GA004003306 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING INSPECTION THE RIGHT HAND OUTER EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2H72 4T RTA55NM 20040224000762004022400076EA 2004 2 24 COMA0460133 120040211A53116003603032 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01982CA16547 7168 RIGHT FS 718 BETWEEN STRINGERS 10R AND 12R P/N 600-36030-32 IS CRACKED. PERFORMED A MAJOR REPAIR TO FS 718 BETWEEN STRINGERS 10R AND 12R BY REMOVING AND REPLACING DOUBLER P/N 600-36030-32 IAW CRJ 200 SRM 51-42-00 AND 51-42-21. 2L72 4F RTA21EA 20040224000792004022400079NM 2004 2 24 QXEA200400126 120040208A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - ON FLIGHT 2243 FLOOR EMERGENCY LIGHT SEGMENT IS INOPERATIVE AT FORWARD RIGHT SIDE. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT SEGMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040224000802004022400080EA 2004 2 24 COMA0460135 120040211A5330601R53211801 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BENT A COMAK NONE O OTHER ININSP/MAINT 1 SO01982CA 7168 PREVIOUS REPAIR TO LEFT SIDE FUSELAGE SKIN HAS SUBSTAINED FURTHER DAMAGE ON FUSELAGE SKIN EXTERNAL DOUBLER. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 310 BETWEEN STRINGER 15R AND 16R BY REMOVING DAMAGED TOP REPAIR DOUBLER. NO DAMAGE FOUND ON BOTTOM DOUBLER AND FILLER. FABRICATING NEW REPAIR DOUBLER FROM 2024T3.063 (WVAC PO 32572/1) AND INSTALLING IAW BOMBARDIER INC REO 601R-53-21-180 REV NC. 2L72 4F RTA21EA 20040224000812004022400081EA 2004 2 24 COMA0460136 120040207A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO01912CA 7011 FLIGHT 5589 RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040224000852004022400085EA 2004 2 24 COMA0470016 120040209A3610GG670950103 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA BLEED AIR MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01379CA2158 10102 FLIGHT 5073 LEFT COWL ANTI ICE AND LEFT BLEED CAUTION MESSAGE. REPLACED THE TEMP CONTROL VALVE. 2L72 4F RTA21EA 20040224000872004022400087EA 2004 2 24 COMA0460141 120040210A2760278003 PCU CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILER BROKEN A COMAL ABORTED APPROACH JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO01941CA22443 7050 FLIGHT 5110 GROUND SPOILER DEPLOY MESSAGE DURING APPROACH. LEFT OUTBOARD SPOILER PCU BROKEN. REPLACED PCU. 2L72 4F RTA21EA 20040224000892004022400089EA 2004 2 24 COMA0460140 120040210A33506464 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR UNRELIABLE A COMAL ABORTED APPROACH O OTHER ININSP/MAINT 1 SO01487CA 7729 FLIGHT 5786 ONE SECTION OF EMERGENCY FLOOR LIGHTS IS INOP. REPLACED LIGHT STRIP. 2L72 4F RTA21EA 20040224000942004022400094WP 2004 2 24 UPS04841857 120040208A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RT WING O/B LEADING EDGE LOWER RIB IS CRACKED AT XFS 825. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224000982004022400098WP 2004 2 24 GKZR200482302 120040203A5343 SUPPORT DOUG DC8 DC871F 302199DWP MLG CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 LEFT MLG SUPPORT MITTING CRACKED (TRAP) TOP FLANGE. REMOVED LT TRAP FITTING IAW DC-8 MM 20-16-0. FITTED AND DRILLED NEW L/H TRAP IAW ATI DRAWING 5750127 SPOT FACED HOLES AS REQUIRRED. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. TORQUED LT TRAP FITTING IAW SB DC-8 53-061. 2L74 4F RT4A25 20040224001012004022400101NM 2004 2 24 04FDEA00378 120040207A3244 TIRE BOEING727 727200 138407ENM MLG FAILED A FDEAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO25481FE 21463 SHORTLY AFTER TAXI OUT FROM OAK RAMP, HEARD A VERY LOUD BANG AND AIRCRAFT SHUDDERED SLIGHTLY. BROUGHT THE AIRCRAFT TO A SLOW STOP. ENGINE INDICATIONS NORMAL. REQUESTED FEDEX MX INSPECTION. BLOWN NR 3 TIRE NOTED BY MX. TOWED BACK TO RAMP. 2L73 4F RTA3WE 20040224001022004022400102NM 2004 2 24 04FDEA00393 120040211A2420 GENERATOR BOEING727 727200 138407ENM MALFUNCTIONED A FDEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO25287FE 21849 DURING CLIMBOUT LIGHTS FLICKERED ON & OFF, A/P CYCLED. ALL GEN LOADS VARIED FROM 18 KW TO 30 KW, SIMULTANEOUSLY APPROX 1/2 SEC IN DURATION. GEN VOLT STEADY; FREQUENCY SPIKED WITH GEN SPIKES. INITIALLY OCCURRED AT HIGH POWER SETTINGS. STABILIZED ON POWER REDUCTION DURING DESCENT AND THEN REOCCURRED, WITH SPEED BRAKE DEPLOYED LIGHT CYCLED FROM ARMED TO DO NOT ARM. 2L73 4F RTA3WE 20040224001032004022400103WP 2004 2 24 04FDEA00394 120040211A5753ARC03291 SUPPORT DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-5750-73880 WINGS - INBOARD FLAP ACTUATOR SUPPORT ASSY BARREL NUT HOLE GOUGED. REPAIR P/N ARC0329-1. COMPLIED WITH EA 8-5750-73880. 2L73 4F A22WE 20040224001062004022400106NM 2004 2 24 AWXA200400169 120040210A2560P4010021 BATTERY BOEING737 73733A 1384673NM ZONE 900 - LAVATDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040224001072004022400107NM 2004 2 24 AALA20040211 120040209A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21654A 24612 MIA EMERGENCY LIGHT ON FUSELAGE AT L4 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040224001092004022400109NM 2004 2 24 AALA20040213 120040210A3350 REFLECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 ORD RT EMERGENCY LIGHTS IMMEDIATELY AFT OF FLAPS INOPERATIVE. REPLACED SOCKET REFLECTOR ASSEMBLY FOR RT EMERGENCY LIGHTS AFT OF FLAPS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040224001102004022400110WP 2004 2 24 AALA20040214 120040210A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21964TW 53614 MIA EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. FOUND LOOSE WIRING. SECURED WIRING FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040224001132004022400113WP 2004 2 24 AALA20040216 120040202A2497 TERMINAL DOUG DC9 DC983 3022083WP OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21562AA 49344 TUL THREE EACH WIRE RING TERMINAL INSULATION FOR UPPER AFT SIDE SHOW SIGNS OF OVERHEATING AT RESISTER R4-9. REPLACED THREE EACH WIRE RING TERMINALS AT RESISTER R4-9 PER SWPM 20-20-01. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040224001142004022400114NM 2004 2 24 QXEA200400130 120040209A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - PERMANENT REPAIR TO CHAFED LEFT HAND FUSELAGE SIDE SKIN PANEL 85310477-119/-123. REPAIRED IAW RD8-53-7706 AND HORIZON AIR EA 2-53-513B. 2H72 4T RTA13NM 20040224001172004022400117NM 2004 2 24 QXEA200400128 120040209A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09405QX 4047 SEA - ON FLT NR 9850, WHEN SELECTING APPROACH FLAPS, FLAP POWER CAUTION LIGHT ILLUMINATED. PER CHECKLIST, THE FLAP CONTROL CIRCUIT BREAKER WAS CYCLED. CYCLED SHIPS POWER. OPERATED FLAPS. FLAP POWER CAUTION REMAINS EXTINGUSHED. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040224001182004022400118SO 2004 2 24 C2XA04TY036 120040210A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717513 145292 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 19. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040224001192004022400119NM 2004 2 24 0400206302 120040208A3350 LIGHT BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK, FOUND LEFT AND RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040224001232004022400123WP 2004 2 24 0400199933 120040207A3320 BALLAST DOUG DC9 DC931 3022065WP ZONE 200 OVERHEATED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL018986E 47402 AT ABOUT 800 FOOT ALTITUDE DURING APPROACH INTO IND, THE FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN THE CABIN. OTHER PASSENGERS REPORTED SEEING WHAT LOOKED LIKE SMOKE AND SMELLING AN ELECTRICAL OZONE SCENT. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT, AND TAXIED TO GATE UNDER ITS OWN POWER. CFR ENTERED THE AIRCRAFT AT THE GATE WITH THE PASSENGERS STILL ON BOARD BUT DID NOT FIND ANY EVIDENCE OF FIRE. AIRCRAFT DEPLANED NORMALLY THROUGH THE JETWAY. MAINTENANCE COULD NOT REPRODUCE THE SMOKE VIA ENGINE OR APU RUNS. A CABIN LIGHT BALLAST WAS FOUND TO BE DISCOLORED AS IF OVERHEATED AND WAS REPLACED ALONG WITH THE NR 3 GALLEY POWER RELAY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040224001262004022400126EA 2004 2 24 COMA0460143 120040211A3020300013000003 VALVE CNDAIRCL600 CL6002B19 1900309EA LEFT ANTI ICE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01451CA6415 7562 FLIGHT 5612 LEFT COWL ANTI-ICE MESSAGE. REPLACED THE ANTI-ICE VALVE. 2L72 4F RTA21EA 20040224001272004022400127EA 2004 2 24 COMA0470019 120040205A2750766389G CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01331CA3 10061 FLIGHT 5476 FLAPS HALF SPEED MESSAGE. REPLACED THE SFECU. 2L72 4F RTA21EA 20040224001332004022400133SO 2004 2 24 C2XA04SH061 120040212A531014522226003 BUTTSTRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001352004022400135SO 2004 2 24 C2XA04SH063 120040212A531514521713005 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001372004022400137WP 2004 2 24 04FDEA00399 120040212A2750 CONTROL VALVE DOUG DC10 DC1010 3022110WP TE FLAPS MALFUNCTIONED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25560FE 46938 DURING FLAP RETRACTION AFTER TAKEOFF GOT FLAP DISAGREE ALERT. INBOARD FLAPS DID NOT RETRACT, STAYED AT 11; OUTBOARD LEFT INDICATED 5 AND OUTBOARD RIGHT INDICATED 6. QRH PROCEDURE ACCOMPLISHED. NOTE: TAKEOFF FLAP SETTING WAS 10.9. REMOVED AND REPLACED INBOARD FLAP CONTROL VALVE AS PER MM 27-52-02-2. CYCLED FLAPS SEVERAL TIMES AND OPERATIONAL CHECK IS NORMAL. LEAK CHECK IS SATISFACTORY. SERVICED HYDRAULIC FLUID AS PER MM 12-13-02-3. 2L73 4F A22WE 20040224001392004022400139WP 2004 2 24 0400259918 120040108A5330 SKIN DOUG DC9 DC932 3022066WP FUSLEAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01940N 47572 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 76.55 RBL 16. REPAIRED PER EA 99-197447. 2L72 4F A6WE 20040224001422004022400142NM 2004 2 24 CALA0400102 120040102A5315654681025 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND CORROSION ALONG THE UPPER SURFACE OF THE UPPER SECTION OF THE STA 967 FLOORBEAM. THE CORRODED UPPER SECTION WAS TRIMMED OUT AND A NEW REPAIR SECTION WAS INSTALLED IAW ECRA 5311-01142. 2L72 4F RTA16WE 20040224001432004022400143NM 2004 2 24 CALA0400103 120040211A575465C26270 PANEL BOEING737 737524 1384721NM NR 4 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714655 28916 INSPECTION FOUND TWO 1.5 INCH CRACKS IN RT WING FIXED UPPER LEADING EDGE PANEL AT NR 4 SLAT ACTUATOR, SLAT STA 65.92. THE LEADING EDGE PANEL WAS REPAIRED IAW ECRA 5721-01116. 2L72 4F RTA16WE 20040224001442004022400144NM 2004 2 24 CALA0400104 120040211A5311146N1014 FRAME BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717126 27566 INSPECTION FOUND FRAME DENTED AT BS 1460, S27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 201. 2L72 4F RTA2NM 20040224001462004022400146NM 2004 2 24 CALA0400106 120040212A532065524572 WEB BOEING737 7373T0 1384582NM FUSLAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND AFT WEB RT SIDE ADJACENT TO RUBBER MEMBRANE AT APB, STA 1016, RBL 0 TO RBL 48, CORRODED. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040224001472004022400147NM 2004 2 24 CALA0400107 120040212A532069353593 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 4 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL UNDER TRANSITION PANEL AT STA 928, RBL 26. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040224001492004022400149NM 2004 2 24 CALA0400109 120040212A335020131A BATTERY PACK BOEING737 7373T0 1384582NM L-2 DOOR INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714307 23358 INSPECTION FOUND L-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20040224001502004022400150NM 2004 2 24 CALA0400110 120040212A5510185A18021 STRAP BOEING737 737824 13844BZNM HORIZONTAL STAB LIGHTNING STRIKEA CALAK NONE O OTHER ININSP/MAINT 1 SW2724212 28772 INSPECTION FOUND RIGHT O/B HORIZONTAL STABILIZER TRAILING EDGE STRAP WITH EVIDENCE OF A LIGHTNING STRIKE. THE AFT O/B UPPER TRAILING EDGE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. THE FIBERGLASS UNDERNEATH WAS REPAIRED IAW SRM 51-70-08 AND 51-21-101-701. 2L72 4F RTA16WE 20040224001522004022400152SO 2004 2 24 C2XA04BT021 120040211A3350 WIRE EMB 145 EMB145ER 3260211SO EMERGNECY LIGHT BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714947 145054 DURING PREFLIGHT CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND AND REPAIRED BROKEN WIRE ON EMERGENCY AISLE PATH LIGHT STRIP, OPS CHECKED GOOD IAW EMB145 MM 33-50-00. 2L72 4F RTT00011AT 20040224001532004022400153NM 2004 2 24 UPS04241872 120040130A5350 BRACKET BOEING727 72722C 138400FNM WING-BDY FAIRINGDAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01. 2L73 4F A3WE 20040224001552004022400155NM 2004 2 24 UPS04241874 120040121A2621 SOLENOID VALVE BOEING727 72722C 138400FNM NR 1 ENG EXTING STICKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, ENGINE NR 1 FIRE EXTINGUISHING SOLENOID STICKS DURING OPERATION. ENGINE NR 1 FIRE SOLENOID VALVE REPLACED IAW MM 26-21-21. TEST AND FOUND SATISFACTORY IAW MM 21-21-00. 2L73 4F A3WE 20040224001562004022400156NM 2004 2 24 UPS04241875 120040202A2571 BRACKET BOEING727 72722C 138400FNM BATTERY CHARGER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, BATTERY CHARGER FWD MOUNTING BRACKET CRACKED ON E3 RACK LOWER RT SIDE. REMOVED CRACKED BRACKET IAW SRM 51-30-02. FABRICATED NEW BRACKET IAW SRM 51-20-01. NEW BRACKET REPROTECTED IAW SRM 51-10-02, AND RE-INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20040224001572004022400157NM 2004 2 24 UPS04241876 120040125A5320 BRACKET BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, SUSPECT CORROSION WHERE 259.5 RT STIFFENER AND TOP LEFT HAND CORNER OF NWW TORQUE BOX MEET BRACKET. REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. FASTENERS INSTALLED IAW SRM 51-30-2 & APPLIED SEALANT IAW SRM 51-20-04. BRACKET REPROTECTED IAW SRM 51-10-02. 2L73 4F A3WE 20040224001592004022400159NM 2004 2 24 UPS04441871 120040127A532065B0434527 STIFFENER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- LT STA 2160 STRINGER 40 STIFFENER ANGLE FOUND CRACKED. AFT OF BULK CARGO LT STA 2160 FRAME AT STRINGER 40 STIFFENER ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20040224001612004022400161NM 2004 2 24 UPS04441893 120040127A5311 FRAME BOEING747 747123 1384873NM SECTION 41 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, SECTION 41, FS 250 BETWEEN STR 40L - 41L, FRAME WEB CRACKED BS 260 CANTED BULKHEAD WEB SEGMENT BETWEEN STR 38L AND STR 41L. REPLACED AS PER HX RS R-53-13-35101 AND UPS ENGINEERING FILE NUMBER 747-53-20167. 2L74 4F A20WE 20040224001642004022400164WP 2004 2 24 UPS04841868 120040204A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, FUSELAGE SKIN IS CRACKED AT FASTENER HOLE AT STATION 1342 LONG 31R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040224001652004022400165WP 2004 2 24 UPS04841869 120040128A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 1690-1700 LONG 35L-35R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040224001662004022400166WP 2004 2 24 UPS04841877 120040129A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1735 LONGERON 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STATION 1716-1742, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040224001692004022400169WP 2004 2 24 UPS04841880 120040130A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 372.75, XFS 379. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001702004022400170WP 2004 2 24 UPS04841881 120040130A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 766.250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001722004022400172WP 2004 2 24 UPS04841883 120040130A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 778.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001732004022400173WP 2004 2 24 UPS04841884 120040130A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001782004022400178WP 2004 2 24 UPS04841889 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XS 478.897. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001792004022400179WP 2004 2 24 UPS04841890 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 410.25, XFS 347.75, XFS 354. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001812004022400181WP 2004 2 24 ABXA040063 120040214A5320 PLATE DOUG DC8 DC861 3021952WP FUSELAGE MISREPAIRED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 FOUND MAIN ENTRY DOOR SCUFF PLATE DID NOT MEET REQUIREMENTS OF SERVICE REWORK DRAWING SRO8530021. TEMPORARY REPAIRED MAIN ENTRY DOOR SCUFF PLATE IAW REA D853-49056MR. PLACED ON CARRY OVER NR COI 46070. PROPER FASTENERS TO BE INSTALLED ON OR BEFORE 9-6-2005. 2L74 4F 4A25 20040224001822004022400182WP 2004 2 24 ABXA040062 120040210A5210 DOOR DOUG DC9 DC931 3022065WP MAIN PAX OBSTRUCTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 PASSENGER ENTRY DOOR WOULD NOT OPEN FROM INSIDE, WORKED OKAY FROM OUTSIDE. FOUND DOUBLER PLATE INTERFERING WITH MOVEMENT OF OUTER DOOR HANDLE. FAIRED DOUBLER IAW DC-9 SRM 52-01. OPERATED DOOR SEVERAL TIMES. OPS CHECKED GOOD. 2L72 4F A6WE 20040224001852004022400185NM 2004 2 24 CALA0400112 120040213A53106552863507 HINGE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 1 INCH CRACK IN R-2 DOOR HINGE HOUSING AT LOWER SURFACE, STA 954, RBL 55, WL 230. THE HOUSING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040224001862004022400186NM 2004 2 24 CALA0400113 120040213A5230654795278 STIFFENER BOEING737 737524 1384721NM C-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714655 28916 INSPECTION FOUND A 1 INCH CRACK IN TEE STIFFENER AT C-2 DOOR AFT LOWER CORNER. THE TEE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040224001872004022400187NM 2004 2 24 CALA0400114 120040213A533065C33756 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 324 JUST BENEATH S20R. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2L72 4F RTA16WE 20040224001882004022400188NM 2004 2 24 CALA0400115 120040214A5320654580148 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND ANGLE ATTACHED TO FORWARD WALL OF NOSE WHEEL WELL CORRODED AT STA 227, RBL 14. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040224001902004022400190NM 2004 2 24 CALA0400117 120040214A5320BMS569 WEB BOEING737 737724 13844BYNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A 4 INCH CRACK IN RT MAIN WHEEL WELL AFT WEB. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-40-71 AND 51-10-2. 2L72 4F RTA16WE 20040224001952004022400195NM 2004 2 24 CALA0400123 120040215A5347655384426 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND AFT BAGGAGE BIN TIE DOWN RAIL CORRODED AT FASTENER HOLES FROM STA 787-847. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-00-53. 2L72 4F RTA16WE 20040224001972004022400197NM 2004 2 24 UPS04241898 120040123A5320 WEB BOEING727 72722C 138400FNM RT TORQUE BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CARRIED OUT IAW EO B727-5310-1239-E & MM 20-10-05. 2L73 4F A3WE 20040224001992004022400199NM 2004 2 24 UPS04441899 120040125A5340 FITTING BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C BS 1241 RT CANTED PRESSURE DECK FITTING AFT HOLE FOUND CRACK APPROX 0.030 INCH RUNNING DOWN. BS 1241 RT CANTED P/D FITTING AFT BOLT HOLE REPAIRED PER RS R53-41-35107 & ENG'R FILE 747-53-20170, REPAIR IS CONSIDERED A TIME-LIMITED REPAIR 2 YEARS/1500 FLT CYCLES WHICHEVER COMES FIRST, AT WHICH TIME CANTED FITTING SHOULD BE REPLACED. SPLICE STRAP SHOULD BE REPLACED WITHIN 2 YEARS OF CRACK DISCOVERY, DUE TO CRACK WAS DISCOVERY DURING PRESENT MAINTENANCE. 2L74 4F A20WE 20040224002002004022400200NM 2004 2 24 UPS04441900 120040126A53302024T30090IN STRAP BOEING747 747123 1384873NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FX SKIN BUTT JOINT SPLICE STRAP OVAL HOLES FOUND AFTER REPAIR PATCH REMOVED AT FS 2180- 2181 ON BOTH SIDE OF STR 50R. FX SKIN BUTT JOINT SPLICE STRAP REPAIRED AT BS 2180-2181 ON BOTH SIDE OF STR 50R AREA AS PER RS R-53-61-35105 AND UPS ENGINEERING FILE 747-53-20169 ISSUED. 2L74 4F A20WE 20040224002012004022400201NM 2004 2 24 UPS04441901 120040202A5330 DOUBLER BOEING747 747123 1384873NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, RAP ITEM N672UP 42-11 AT BS 680-703 STR 40R-41R AREA, REPAIR DOUBLER HAS LESS THAN 3 ROW FASTENERS FOR REPAIR AFTER NDT DEFINED CUTOUT RE-DO THE REPAIR REQ'D. BS 680-703 STR 40R-41R AREA DOUBLER REMOVED & DISCARDED AS PER SRM 51-30-02 BS 678-689 & BS 692-704 STR 40R-41R EXTENDED DOUBLER INSTALLED REPAIR AS PER SRM 53-30-03 FIG 1 & ZERO-TIME FASTENERS INSTALLED AS PER SRM 51-10-01 PG 11 AT STR 40R-41R AREA CLASSIFIED A CATEGORY-A REPAIR. 2L74 4F A20WE 20040225000012004022500001WP 2004 2 25 COOSDR030064 120040101A53203936595513 SUPPORT BRACKET DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23135NJ 49440 AFT CARGO COMPARTMENT, SUPPORT BRACKETS CORRODED AT Y:STA 1250 AND Y:STA 1271 BETWEEN LONG 27L AND 28L. 2L72 4F A6WE 20040225000022004022500002WP 2004 2 25 COOSDR030065 120040101A5320 FLOOR SUPPORT DOUG DC9 DC914 3022034WP FUSELAGE CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23600ME 45725 AFT AND FORWARD CARGO COMPARTMENT, FLOOR SUPPORT LATERAL ANGLES AT B/S Y:STA 351, 427, 465, AND 737 BETWEEN LONG 28L AND 28R, WITH CRACKS. 2L72 4F A6WE 20040225000032004022500003NM 2004 2 25 COOSDR030066 120040101A5315 FLOORBEAM BOEING727 727224 1384076NM FUSELAGE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 PAX CABIN BODY STATION 380.0 INCHES, FLOORBEAM UPPER CHORD AFT FLANGE CORRODED AT RBL 62.0 INCHES. 2L73 4F A3WE 20040225000042004022500004NM 2004 2 25 COOSDR030067 120040101A5320656097130 FLOOR SUPPORT BOEING727 727224 1384076NM PAX CABIN CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 PAX CABIN, BS 1034 FLOOR SUPPORT PN 65-60971-30 CORRODED. 2L73 4F A3WE 20040225000052004022500005NM 2004 2 25 COOSDR030068 120040101A5510 BEAM BOEING727 727224 1384076NM HORIZONTAL STAB CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 LT HORIZONTAL STABILIZER, TRAILING EDGE, UPPER BEAM CORRODED. 2L73 4F A3WE 20040225000112004022500011NM 2004 2 25 COOSDR030074 120040101A57306519281158 PANEL BOEING727 727224 1384076NM RT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 RT WING, LOWER SURFACE FIXED PANEL PN 65-19281-158, OUTER SKIN, CORRODED. 2L73 4F A3WE 20040225000122004022500012NM 2004 2 25 COOSDR030076 120040101A5753652163261 SKIN BOEING727 727224 1384076NM LT WING TE FLAP CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 LT WING, IB MID FLAP TRAINING EDGE PN 65-21632-61 SN BN281, UPPER AND LOWER SKIN CORRODED. 2L73 4F A3WE 20040225000162004022500016NM 2004 2 25 COOSDR030080 120040101A532065561852 SPLICE BOEING727 727224 1384076NM FUSLEAGE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 AFT CARGO COMPARTMENT, BS 1050 STRINGER 27R SPLICE CORRODED. 2L73 4F A3WE 20040225000232004022500023EA 2004 2 25 UIA9304 120040116A8010AJA4N176 RELAY DHAV DHC8 DHC8311 1386006EA STARTER FAULTY Z O OTHER S AFFECT SYSTEMS CRCRUISE 1 TW0015229 407 IN FLT RUD PRESS B, NR 1 RUD HYD, BRUD FULL PRESS B TOUCHED RUNWAY CAUTION LT'S ON. EMERGENCY LANDING INSPECTION FOUND 2431-K2 RELAY FAULT. REPLACED NEW RELAY AND ENGINE RUNUP FUNCTION CHECK CONDITION, BACK NORMAL. 2H72 4T RTA13NM 20040225000262004022500026EU 2004 2 25 2004F00044 120040104A769730709341 WIRE HARNESS BRAERODH125 HS125700A 4230170EU RT ENGINE DETERIORATED E A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CE03120JC6970 NA0247 WHILE ENROUTE, NOTED RT ENGINE AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED INDICATED LOSS OF POWER RT ENGINE. CONSULTED OPERATORS MANUAL AND COMPLIED WITH EMERGENCY PROCEDURES WHICH INCLUDED TO SWITCH TO MANUAL CONTROL AND MONITOR ALL ENGINE PARAMETERS. IMMEDIATE NOTIFICATION TO ATC AND REQUESTED TO DIVERT FOR INSPECTION. INSPECTION WAS PERFORMED AND FOLLOWING TROUBLESHOOTING AND INSPECTION THAT THE SOURCE OF THE DEFECTS WAS THE RT ENGINE PT2 HARNESS. PARTS WERE REPLACED AND PN 3070934-1 HARNESS. SYSTEM WAS OPERATIONALLY TESTED WITH NO FURTHER DEFECTS NOTED. 2L72 4F A3EU 20040225000312004022500031GL 2004 2 25 JIKA200400001 320040116A61147503503AF PACKING SWRNGNSA227 SA227AT 8780610SW ROTOL R321 R321482F8 GL LEFT PROPELLER CUT E JIKAEA ENGINE SHUTDOWN UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP01246DH AT625B DGIDRG160280 AFTER TAKE-OFF AT APPROXIMATELY 6000 FT AGL, PILOT NOTED LT ENGINE R.P.M. DROPPED FROM 100 PERCENT TO 97 PERCENT WITH SPEED LEVER FULL FORWARD. SHORTLY AFTER, COCKPIT FILLED UP WITH BLUE SMOKE AND LT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PILOT SHUT DOWN THE LT ENGINE, DECLARED AN EMERGENCY, RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE AND FOUND OIL LEVEL ABOUT 6 QUARTS LOW. OIL WAS LEAKING FROM PROPELLER HUB. INSPECTION OF THE PROPELLER HUB REVEALED PROPELLER PISTON O-RING P/N 7503503AF CUT IN HALF CAUSING THE OIL LEAK. THIS MASSIVE OIL LEAK FROM THE PROPELLER HUB INTO THE ENGINE INLET WAS THE CAUSE OF THE SMOKE IN THE COCKPIT. 2L72 4T RTA5SW 6 CP61GL 20040225000422004022500042 2004 2 25 MEX2004007 420040105A3416 INDICATOR DOUG MD80 MD83 3023681NM ALTIMETER MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23491SH 49150 AIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTING THE PO ALTIMETER FLAG CAME ON. CADC NR 2 WAS RESEATED AND TESTED IAW MM, ALL TESTED CORRECT. THE FLAG DISAPPEARED BUT IT HAD 130 FEET INDICATION BETWEEN ALTIMETERS. PNEUMATIC CONNECTIONS OF CADC NR 2 AND ALTIMETER WERE DRAINED AND CLEANED, ALL CORRECT. 2L72 4F RT 20040225000452004022500045NM 2004 2 25 MEX2004012 120040108A3213920629515 PISTON DOUG MD88 MD88 3023688NM NLG STRUT DAMAGED W ASMFC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SW23169PL 53175 AIRCRAFT RETURN OF FLIGHT, DURING TAKEOFF ROLL, THE NLG HIT A BIG BUMP ON THE RUNWAY AND IT DID NOT RETRACT. DURING REVISION WAS DETECTED THE NLG SHOCK STRUT LOW. AIRCRAFT WAS SENT TO HANGAR, WHERE THE PISTON AXLE ASSEMBLY CYLINDER ASSY AND SHOCK STRUT SEALS WERE REPLACED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM, ALL CORRECT. 2L72 4F RTA6WE 20040225000522004022500052CE 2004 2 25 DWH2004F00000 120040102A3297 WIRE HARNESS BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA MLG INDICATOR BROKEN E DWHAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP014QL 7891 BB942 PILOT REPORTED LT MLG DOWN AND LOCKED INDICATOR WAS NOT ILLUMINATED AFTER LANDING GEAR EXTENSION AND DECLARED AN EMERGENCY. THE AIRCRAFT WAS LANDED ANT VNY WITHOUT INCIDENT. UPON INVESTIGATION, A TY-WRAP WAS MISSING FROM THE LT MLG DRAG ACTUATING ROLLER HAD CAUGHT THE WIRE BUNDLE AND BROKEN THE DOWN AND LOCKED CIRCUIT WIRE UPON GEAR RETRACTION. THE WIRE WAS REPAIRED, THE WIRE BUNDLE WAS RESECURED, AND THE LANDING GEAR WAS OPERATIONALLY TESTED WITH NO FURTHER DISCREPANCIES NOTED. 1L72 4T3 T A24CE E2NE 20040225000532004022500053EA 2004 2 25 JRP2004F00000 120040112A5711C6WM10271 FITTING DHAV DHC6 DHC6 2802606EA PWA PT6 PT6* 52043EA SPAR CAP CRACKED A JRPRO OTHER O OTHER NRNOT REPORTED 1 WP21885EA22197 454 LATERAL CRACK BETWEEN RIVETS IN VERTICAL LEG OF FITTING AT WS 40 AND AT WS 47.5 FITTING IS PART OF FORWARD WING ATTACHMENT ASSEMBLY. NOTE: PART NAME IS FRONT SPAR CAP ADAPTOR FITTING. 1H72 3T3 TRTA9EA E2NE 20040223000572004022300057EA 2004 2 23 COMA0460017 120040104A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 GENERATOR LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01729CA 7265 FLIGHT 5157 GENERATOR 1 CAUTION MESSAGE. SERVICED THE LT ENGINE IDG OIL SYSTEM. OPERATION NORMAL. 2L72 4F RTA21EA 20040223000642004022300064CE 2004 2 23 DXTA200400212 120040105A3260G2387 BULB CESSNA560 560XL 2076702CE MLG INDICATOR INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07639QS 5605139 AFTER EXTENDING LANDING GEAR, LT MAIN GEAR GREEN LIGHT DOES NOT ILLUMINATE, BLOW-DOWN OF GEAR. FOUND BOTH LT GEAR INDICATOR BULBS TO BE INOPERATIVE. REMOVED BULBS AND REPLACED WITH 2 NEW BULBS, OPS CHECK GOOD IAW CESSNA 560XL MM CHAPTER 33-10-06. 2L72 4F RTA22CE 20040223000882004022300088EU 2004 2 23 AWXA200400022 120040104A335032145410 EPSU AIRBUS320 A320231 3930325EU ZONE 221 DEFECTIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28645AW111099031 238 MCN - EEL - DURING C-02 CHECK FOUND EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, & 4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE THE L-1 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2L72 4F RTA28NM 20040223000892004022300089NM 2004 2 23 AWXA200400023 120040104A575165C2591118A SPAR BOEING737 73733A 1384673NM AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL ATTACHMENT WS 430. MAINTENANCE TRIMMED OUT DAMAGE ON RT AILERON FORWARD SPAR, LOWER FLANGE; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAIR IAW AWA E.R. 03-5751-00159-SS2. 2L72 4F RTA16WE 20040223001022004022300102WP 2004 2 23 DHL2004801001 120040108A5210 DOOR DOUG DC8 DC873F 302199FWP MAIN CABIN LACK OF LUBE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR IAW DC-8 M/M 52-11-1. OPERATES NORMAL AT THIS TIME. 2L74 4F RT4A25 20040223001272004022300127NE 2004 2 23 2004F00041 220040111A7310UL11207 LINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE FUEL DISTRIB CHAFED D O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 GL13671AA 25336 31138 ENGINE HYDRAULIC LINES WERE RUBBING ON FUEL LINE. HYDRAULIC PRESSURE LINE WORE A HOLE IN THE LOW PRESSURE FUEL LINE. SHOULD HAVE STANDOFF FOR HYDRAULIC LINES AND OR MORE FREQUENT INSPECTION. 2L72 4F4 FRTA2NM E12EU 20040223001292004022300129EA 2004 2 23 UIA9302 120040110A2910DSC252B40124 LINE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HYD SYSTEM LEAKING Z B EMER. DESCENT KS FLUID LOSS AFFECT SYSTEMS DEDESCENT 1 TW0015237 467 AE0001 IN FLT NR 2 HYD SYSTEM QTY LOW. A/C MANUAL DOWN LANDING GEAR. PFM INSP FOUND HYD FLUID LEAK FORM NOSE GEAR UPLOCK HYD TUBE(PIN-HOLE). IAW AMM29-10-00 REPLACED NR 2 EDPAND CASE DRAIN FILTER AND HYD TUBE . LDG SWING CHK COND NML . ENG RUNUP CHK NR 2 EDP FUNCTION NML. 2H72 4T4 TRTA13NM E20NE 20040223001432004022300143NM 2004 2 23 2004UALA00013 120040106A5310 DOOR FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO BAY DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29952UA 26699 AFT PIT AFT DOOR FRAME DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040223001512004022300151WP 2004 2 23 IXXA0400005O 120040112A5320 CURTAIN DOUG DC8 DC871 302199AWP NLG WW UNSECURE A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW11829BX87071210 45994 DURING TAKEOFF AND UPON GEAR RETRACTION, A NOISE WAS HEARD FROM NOSE GEAR AREA. CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR BRACKETS AND HINGES FOR DEFECTS AND NONE WERE NOTED. CHECKED DOOR LINKAGES, SEALS AND MECHIANISM AND NO DEFECTS WERE NOTED. LT NOSE WHEEL WELL INSPECTION FOUND CURTAIN WAS UNSNAPPED. RESECURED NOSE WHEEL WELL CURTAIN, THEN INSPECTED GEAR DOOR. PERFORMED GENERAL INSPECTION OF NOSE GEAR, NOSE WHEELS, WHEEL WELL AND RETRACTION SYSTEM IAW ALL APPLICABLE MANUALS. NO DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001522004022300152WP 2004 2 23 IXXA0400006O 120040109A3241 WARNING LIGHT DOUG DC8 DC873F 302199FWP ANTI SKID SYSTEMILLUMINATED A IXXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW11606AL903722124 46044 WHEN LANDING GEAR WAS EXTENDED THE ANTI-SKID INOP LIGHT AND LAO AND LAI LIGHTS ILLUMINATED. LAO AND LAI LIGHT REMAINED ILLUMINATED IN MANUAL ON THE SKID MONITOR PANEL. RECYCLED MAIN LANDING GEAR, ANTI-SKID CONTROL SWITCH AND RESET CIRCUIT BREAKER, NO HELP. CREW HAD TO OVER FLY KEWR FOR ANTI-SKID INOP, AND LANDED AIRCRAFT AT KBDL WITHOUT INCIDENT. MAINTENANCE AT KBDL DEFERRED ANTI-SKID AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040223001712004022300171WP 2004 2 23 ZW0A0400101 120040112A33507732 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 20 TO 26. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED 2L72 4F RTA6WE 20040223001722004022300172WP 2004 2 23 ZW0A0400102 120040112A33507732 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED 2L72 4F RTA6WE 20040223001792004022300179EU 2004 2 23 03009305 120040109A3220 LANDING GEAR JETAIRJETSTMJETSTM4101 1500501EU NOSE INOPERATIVE A VTZAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 EA27305UE 41019 DURING LANDING OF FLIGHT 7768 TO IAD NOSE GEAR NOT LOCKED INDICATION. CREW PERFORMED MISSED APPROACH, DECLARED EMERGENCY, AND VERFIED WITH TOWER THAT GEAR WAS NOT DOWN. CREW PERFORMED AN EMERGENCY NO NOSE GEAR LANDING AND PASSENGERS DEPLANED THROUGH EMERGENCY EXIT DOOR ON RUNWAY WITH NO INJURIES. 2L72 4T RTA41NM 20040223002042004022300204NM 2004 2 23 COOSDR030034 120040101A5751 SKIN BOEING727 72731 1384010NM AILERON DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE AA019 18905 LT WING, OB AILERON TRAILING EDGE LOWER SURFACE DELAMINATED. 2L73 4F A3WE 20040223002112004022300211NM 2004 2 23 COOSDR030040 120040101A5755 SKIN BOEING727 72731 1384010NM SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 313 18905 LT WING GROUND SPOILER (NR 6) UPPER SURFACE TRAILING EDGE DELAMINATED. 2L73 4F A3WE 20040224000442004022400044EA 2004 2 24 A6WA200440012 120040130A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401AW 7280 ON CLIMB-OUT, PASSENGER DOOR LATCH CAUTION MESSAGE FOLLOWED BY PASSENGER DOOR WARNING. FLIGHT ATTENDANT STATED THE TWO TOP ALIGNMENT MARKS WERE OFF. REMOVED AND REPLACED AFT UPPER PASSENGER DOOR BEARING ROD. ADJUSTED DOOR LATCH MECHANISM. PERFORMED OPS AND FUNCTINAL TEST OF PASSENGER DOOR, OPS CHECK GOOD AT THIS TIME. (M) 2L72 4F RTA21EA 20040224000602004022400060EA 2004 2 24 ASOA04025 120040108A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11906EV 7642 FLT 4561 - DURING TAKEOFF AND CLIMB-OUT FROM ATL-MOB, THE CREW NOTICED A STRONG OIL ODOR WHICH WAS MOST NOTICEABLE AFTER TRANSFER OF BLEED AIR TO THE ENGINES. THE ODOR WENT AWAY AFTER FOUR TO FIVE MINUTES. THE AIRCRAFT LANDED SAFELY IN MOB. MAINTENANCE INSPECTED THE PACKS AND GROUND RAN THE ENGINES WHILE CYCLING THE PACKS. NO OIL ODOR OR DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000612004022400061EA 2004 2 24 ASOA04024 120040108A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN AIR CONTAMINATED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11906EV 7642 FLT 4156 - DURING CLIMB-OUT FROM EVV-ATL, THE CREW NOTICED A STRONG OIL ODOR IN THE CABIN AND COCKPIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE COALESCER BAGS TO THE AIR CYCLE MACHINE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000652004022400065 2004 2 24 04038638 420040207A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAULTY A VTZAO OTHER S AFFECT SYSTEMS APAPPROACH 1 EA27638BR 7311 DURING APPROACH CREW REPORTED A STALL SYSTEM FAILURE WHEN FLAPS WERE SELECTED TO 8 DEGREES. THE STALL COMPUTER WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000692004022400069EA 2004 2 24 04040651 120040209A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27651BR 7426 DURING INSPECTION THE LEFT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000772004022400077EA 2004 2 24 COMA0460134 120040211A53306003301039 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01982CA16547 7168 RIGHT AND LEFT SIDE LOWER FUSELAGE SKINS ARE CRACKED AT NOSE LANDING GEAR CUTOUT AT FS 235 STRINGERS 26R AND 26L. CRACKS ARE 1.0 INCH LONG. PERFORMED A MAJOR REPAIR FUSELAGE SKIN AT FS 235 STRINGER 26R AND 26L BY CUTTING OUT DAMAGED AREAS, FABRICATING REPAIR FILLERS AND DOUBLERS FROM 2024T3.050 (WVAC PO 33196/1) AND 2024T3.063 (WVAC PO 32572/1). PERFORMING LP1 TO ENSURE CUTOUT AREAS ARE CRACK FREE AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-11-010 REV C AND REO 601R-53-11-014 REV NC. 2L72 4F RTA21EA 20040224000822004022400082EA 2004 2 24 COMA0460137 120040206A325016745101 PRESSURE SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG STEERING MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01983CA 7169 FLIGHT 5262 NWS FAILED MESSAGE DURING GEAR EXTENSION. COULD NOT DUPLICATE. REPLACED THE STEERING PRESSURE SWITCHES. 2L72 4F RTA21EA 20040224001042004022400104GL 2004 2 24 04FDEA00395 220040211A7210 HOUSING DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 ENG GEARBOXGOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7260-75573. ENGINE DRAIN - TRANSFER GEARBOX HOUSING DAMAGE INTERIM REPAIR. COMPLIED WITH EA 8-7260-75573. 2L73 4F4 F A22WE E23EA 20040224001082004022400108WP 2004 2 24 AALA20040212 120040211A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21453AA 49558 PHX AFT ACCESSORY CEILING EMERGENCY LIGHTS AND EMERGENCY LIGHTS FOR EMERGENCY SLIDES INOPERATIVE. REPLACED BATTERY PACK AT STATION 1338R FOR AFT ACCESSORY CEILING EMERGENCY LIGHTS AND EMERGENCY LIGHTS FOR SLIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040224001212004022400121NM 2004 2 24 0400216637 120040205A3097CWC011210 TERMINAL BOEING747 747251B 1384892NM 1L WINDOW BURNED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01637US 23548 DURING CLIMB, A STRONG BURNING ODOR EMITTED FROM THE CAPTAIN'S L1 LOWER LEFT WINDOW HEAT ELECTRICAL CONNECTIONS. PLACED L1 IN OVERRIDE AND ODOR DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT LOWER AND UPPER WINDOW HEAT TERMINALS ON L1 WINDOW AND REPLACED THE WINDOW HEAT CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040224001222004022400122NM 2004 2 24 0400236309 120040207A3350 LIGHT BOEING747 747451 1384940NM ROWS 21-31 INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21 TO 31. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040224001282004022400128NM 2004 2 24 AALA20040218 120040210A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21765AN 32879 DFW EMERGENCY LIGHTS AT ROWS 20 THROUGH 26 CENTER INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ROWS 20 THROUGH 26 CENTER AT 3R FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040224001302004022400130NM 2004 2 24 AALA20040219 120040211A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21932AN 29530 DTW SEAT MOUNTED EMERGENCY EXIT LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY EXIT LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040224001382004022400138CE 2004 2 24 DXTA200400241 120040212A2120 ODOR CESSNA500 560CESSNA 2076750CE GALLEY DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07341QS 5600341 HOT ELECTRICAL ODOR COMING FROM THE CABIN. ODOR STARTED AT FL100 AND CONTINUED TO GET WORSE. CREW TURNED DOWN THE HEATER CLOSED FOOT WARMERS, PULLED COFFEE POT OUT OF SLOT. ODOR DID NOT STOP. AT FL180 TO FL200 CREW MADE DECISION TO RETURN TO CLT ON DESCENT BEGAN TO QUIT AT FL100. ODOR WAS GONE ON THE GROUND. 2L72 4F RTA22CE 20040224001402004022400140NM 2004 2 24 CALA0400100 120040211A5753 SKIN BOEING737 7373T0 1384582NM LT TE FLAP DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW271433539947 BN839 23573 INSPECTION FOUND THE NR 1 T/E FOREFLAP DELAMINATED BELOW NR 2 SPOILER PANEL, LT WING. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37. 2L72 4F RTA16WE 20040224001412004022400141NM 2004 2 24 CALA0400101 120040211A5320143A7510 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717719 28938 INSPECTION FOUND LIGHT SURFACE CORROSION IN FORWARD CARGO BIN ON ZEE CHANNEL JUST AFT OF CARGO DOOR CUTOUT AT STA 500-500A. THE Z-CHANNEL WAS REMOVED AND A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-30-15, 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20040224001452004022400145NM 2004 2 24 CALA0400105 120040211A5414311A1400 SKIN BOEING737 7373T0 1384582NM NR2 PYLON STRUT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20040224001542004022400154NM 2004 2 24 UPS04241873 120040123A5280 HINGE BOEING727 72722C 138400FNM MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02. 2L73 4F A3WE 20040224001602004022400160NM 2004 2 24 UPS04441892 120040121A5320 WEB BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D - BS 270 LT STR 26L VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040224001622004022400162WP 2004 2 24 UPS04841866 120040201A534037592221N FITTING DOUG DC8 DC871F 302199DWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STA 1270 LONG 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D. 2L74 4F RT4A25 20040224001742004022400174WP 2004 2 24 UPS04841885 120040131A5320 FLOOR SUPPORT DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOOR SUPPORT CHANNEL IS CRACKED AT STA 863 AT LBL 23. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL IAW DWG 5758265 AND SRM 51-1-20D. 2L74 4F RT4A25 20040224001752004022400175WP 2004 2 24 UPS04841886 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 641.25. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001802004022400180WP 2004 2 24 UPS04841891 120040212A3510 REGULATOR DOUG DC8 DC873F 302199FWP OXYGEN SYSTEM LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 F/O OXYGEN REGULATOR LEAKING. REMOVED AND REPLACED 02 BOTTLE IAW MM 12-70-01-3, NO LEAKS NOTED. 2L74 4F RT4A25 20040224001912004022400191NM 2004 2 24 CALA0400118 120040215A5330 SKIN BOEING737 737524 1384721NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714655 28916 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1064, S16L. A DOUBLER WAS INSTALLED IAW SRM 53-80-01. 2L72 4F RTA16WE 20040224001922004022400192NM 2004 2 24 CALA0400119 120040215A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714655 28916 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 344-360, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040224001962004022400196NM 2004 2 24 CALA0400124 120040216A532065479571 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A .25 INCH CRACK IN C-2 DOOR OPENING LOWER FORWARD SILL WEB AT STA 787. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040224002022004022400202NM 2004 2 24 UPS04441902 120040125A532065B05002186 REVEAL BOEING747 747123 1384873NM R4 DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- R4 DOOR CUTOUT FWD REVEAL CRACK, BETWEEN STRINGER 17 & 18 (BS 1662-1664, STR R17, R18). REPLACED DOOR CUTOUT FWD REVEAL PER SRM 51-10-01 PG 8. DOOR RIGGING & ADJUSTMENT DONE RESULT: SATISFACTORY PER MM 52-10-00. 2L74 4F A20WE 20040225000062004022500006NM 2004 2 25 COOSDR030069 120040101A5210655714634 SEAL DEPRESSOR BOEING727 727224 1384076NM DOOR NR 1 WORN W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 FORWARD CARGO COMPARTMENT, DOOR NR 1, FORWARD (65-57146-4) AND AFT (65-57146-3) LOWER CORNER SEAL DEPRESSOR WITH WEAR. 2L73 4F A3WE 20040225000082004022500008NM 2004 2 25 COOSDR030071 120040101A5743 BEAM BOEING727 727224 1384076NM LT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 LT WING, MAIN LANDING GEAR SUPPORT BEAM FROM WBL 70.597 TO WBL 126 LOWER FLANGE WITH CORROSION. 2L73 4F A3WE 20040225000172004022500017NM 2004 2 25 COOSDR030081 120040101A5313655612910 STRINGER BOEING727 727224 1384076NM FUSELAGE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 AFT CARGO COMPARTMENT, BS 950E STRINGER 27 RT CORRODED. 2L73 4F A3WE 20040225000342004022500034 2004 2 25 SPAA0400068 420040115A2565 PIN BFGOODRICH BOEING737 7372Y5 1384554NM ESCAPE SLIDE INSTALLED A SPAAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 WP28712S 0444 23038 L-2 DOOR ESCAPE SLIDE DID NOT DEPLOY DURING CABIN CREW TRAINING EXERCISE. FOUND DISCHARGE BOTTLE SAFETY PIN INSTALLED. MAINTENANCE REMOVED SAFETY PIN, CREW TRAINING RESUMED, SLIDE DEPLOYED. 2L72 4U RTA16WE 20040225000462004022500046NM 2004 2 25 MEX2004013 120040108A3213 STRUT DOUG MD88 MD88 3023688NM NLG FAILED W ASMFD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW23169PL 53175 AIRCRAFT RETURNED, DURING LANDING, NLG DID NOT RETRACT. AT PLATFORM WAS DETECTED THE SHOCK STRUT WET WITH HYDRAULIC FLUID AND THE PISTON AND CYLINDER ASSY COMPRESSED. AIRCRAFT WAS SENT TO THE HANGAR WHERE THE NLG STRUT SEALS WERE REPLACED IAW MM AND EXTENSION AND RETRACTION TESTS WERE PERFORMED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM, ALL CORRECT. FLIGHT DATA RECORDER WAS REPLACED. 2L72 4F RTA6WE 20040225000472004022500047CE 2004 2 25 2004F00045 120040113A2612 FIRE LOOP LEAR 25 25B 5170511CE GE CJ610 CJ6108 30006NE NACELLE DIRTY E O OTHER N FALSE WARNING CRCRUISE 1 GL257810W 117 249044A FALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGINE INSPECTED, NO INDICATION OF FIRE/OVERHEAT. DETECTION LOOP INTACT/NO DAMAGE. WIRING CONNECTIONS AT FIREWALL DISCONNECTED, APPEARED TO BE MORE THAN NORMAL BUILD UP OF GRIME/CARBON. CLEANED TERMINALS/CONTACTS, RECONNECTED. GROUND RUN, UNABLE TO DUPLICATE FIRE INDICATION. 2L72 4J4 J A10CE 1E16 20040225000582004022500058WP 2004 2 25 MEX2004014 120040109A213339613011 REGULATOR VALVE DOUG DC9 DC9* WP PWA JT8 JT8D* NE CABIN PRESSURE FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23501AM 49188 AC PERFORMED UNSCHEDULED LANDING DUE TO A PRESSURIZATION FAILURE. CAPT REPORTED, DURING CRUISE AT FL35 WHEN ANTI-ICE WAS TURNED ON CABIN CLIMB INDICATION MOVES ALTERNATIVELY +/- 1000 FT. PRESSURIZATION CONTROL VALVE WENT TO OPEN W/O CONTROL, HAVING UNCONTROLLABLE RATE OF CABIN CLIMB MORE THAT 25,000 FT AND OXYGEN MASK WERE DEPLOYED, AT PLATFORM DURING SYS TEST, PRESSURE REGULATORY VALVE WAS FOUND IN OPEN POSITION. AC CAME BACK AS FERRY FLIGHT AND DURING VERIFICATION OF ANTI-ICE PERFORMANCE, IT WAS OBSERVED NEWLY A PRESSURIZATION FAILURE. FLOW CONTROL VALVES, AC REGULATORY VALVE AND WING ICE PROTECTION SHUTOFF VALVE WERE REPLACED AND SYS WAS TESTED IN MODE 1 AND 2, ALL CORRECT. 2L72 4F4 F A6WE E2EA 20040225000892004022500089CE 2004 2 25 GLBA20030533 120040115A2100 ANNUNCIATOR BEECH 1900 1900D 1154162CE ENVIR SYS ACTIVATED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03170GL UE170 RT ENVIRO FAIL ANNC ILLUM ON TAKEOFF, PERFORMED GROUND PERFORMANCE RUN. OPS CK GOOD. 2L72 4T RTA24CE 20040225000902004022500090CE 2004 2 25 GLBA20030534 120040116A61201293640919 CIRCUIT BOARD BEECH 1900 1900D 1154162CE NR 2 PROP FAILED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03179GL UE179 AFX DISABLE ILLUMINATED WHEN SETTING TAKE OFF POWER, NR 2 AFX LIGHT DID NOT ILLUMINATE, AFX DISABLE STAYED ILLUMINATED, REMOVED AND REPLACED A123 PCB PN 129-364091-9. OPS CK GOOD. 2L72 4T RTA24CE 20040225000932004022500093 2004 2 25 BAQA092100 420040116A3416066305401 ALTIMETER AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL RADAR STICKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03652PM 5179 RADAR ALTIMETER UNIT INOPERATIVE, STICKING. FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 01/20/2004 1G72 3U3 U H11EU E4CE 20040225000982004022500098EU 2004 2 25 CX7A194J0405 120040125A3260 BULB SAAB SF340 340B 7860101EU MLG INDICATOR BURNED OUT A CX7AO OTHER P NO WARNING INDICATION APAPPROACH 1 GL03300CE 340B184 ON APPROACH WHEN GEAR IS SELECTED DOWN, LT GEAR LIGHT (MAIN) DID NOT ILLUMINATE, HOWEVER INTRANSIT LIGHT WAS OUT. GEAR CONFIRMED DOWN. 2L72 4T RTA52EU 20040225001002004022500100EU 2004 2 25 MALA040131 120040109A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING 4K INSPECTION IN LCQ, RT IB SEAT TRACK HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK IAW MESABA EO NR S53060 DATED 3 NOV 2003. 2L72 4T RTA52EU 20040225001012004022500101EU 2004 2 25 MALA040129 120040109A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING 4K INSPECTION IN LCQ, EXTERIOR FUSELAGE HAS DENTS AT FS 350. MAINTENANCE FABRICATED AND INSTALLED 2 EACH EXTERNAL DOUBLER REPAIRS IAW MESABA EO NR S53009 DATED 21 SEPT 2001. 2L72 4T RTA52EU 20040225001052004022500105EU 2004 2 25 MALA040132 120040119A21507769106 ACM SAAB SF340 340B 7860101EU LEFT SEIZED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15365PX 340B265 POST FLIGHT OF NR 3084, LT ACM BURNING ODOR. SECONDARY INDICATION OF INMINENT LT ACM FAILURE, BURNING ODOR GRINGING NOSIES LT SIDE MIDSECTION. MAINTENANCE FOUND BURNING ODOR FROM RT ACM, FOUND RT ACM SEIZED. REPLACED RT ACM PN 776910-6 SEE 409 NR 071530 FOR DETAILS. OPS CHECKS OF BOTH ACMS GOOD. RT AUTO TEMP CONTROL INOPERATIVE REPLACED AIR CONDITIONING PANEL PN 7739019-505 OPS CHECK GOOD. 2L72 4T RTA52EU 20040225001082004022500108EA 2004 2 25 AKG2004F00000 220040116A732132447452 FUEL CONTROL BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA LT ENGINE MALFUNCTIONED B AKGRA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CE05475JA 2193 LJ1147 PCE25421 AFTER TAKEOFF AND SHORTLY INTO FLIGHT THE LT ENGINE ROLLED BACK TO IDLE WITH THE POWER LEVER NOT BEING MOVED. MAKING A GROUND RUNUP, FOUND THAT THE FCU WAS VERY UNSTABLE AND NOT RESPONSIVE TO POWER LEVER CONTROL INPUTS. 1L72 3T4 TRT3A20 E4EA 20040225001122004022500112CE 2004 2 25 GVR2004F00000 120040115A2520551900912 SEAT BACK CESSNA501 501 2076603CE PWA JT15 JT15D1 52060NE CABIN CRACKED B GVRRO OTHER O OTHER NRNOT REPORTED 1 CE0513ST 5010285 UPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. ALSO, CHAIR BASE HAS HAD PREVIOUS INAPPROPRIATE REPAIR MADE. CHAIR WAS REPAIRED. 1L72 4F4 F A27CE E1NE 20040225001142004022500114WP 2004 2 25 MEX2004017 120040114A27601474253 SELECTOR VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE SPOILER LEAKING W ASMZO OTHER K FLUID LOSS NRNOT REPORTED 1 SW23838AM1242612426 49397 DURING TRANSIT CHECK IT WAS DETECTED A HYDRAULIC LEAKAGE IN THE RT MAIN LANDING GEAR COMPARTMENT. THE SPOILER SELECTOR VALVE WAS FOUND DAMAGED. IT WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM. AT OVERNIGHT SERVICE, THE SYSTEM WAS TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001152004022500115NM 2004 2 25 MEX2004018 120040115A2913 PUMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE HYD SYSTEM FAILED W ASMZO OTHER O OTHER NRNOT REPORTED 1 SW23158PL8120 3019 49761 DURING TRANSIT SERVICE THE ELECTRICAL HYDRAULIC PUMP DOES NOT WORK. THE PUMP WAS CHECKED AND A PUMP BREAKER WAS DAMAGED. THE PUMP WAS REPLACED AND TEST WAS CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001162004022500116NM 2004 2 25 MEX2004019 120040115A7830 THRUST REVERSER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LEFT FAILED W ASMZO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23805AM 26272 DURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND ICE AND SNOW WAS DETECTED INTO THE REVERSE. THE REVERSER WAS NOT CLOSED COMPLETELY BECAUSE A GAP OF 2 INCHES IS BETWEEN COVERS. THE CABLE BETWEEN ACTUATORS WAS REMOVED AND REVERSER WAS RETRACTED. THE AIRCRAFT WAS DISPATCHED BY MEL. DURING OVERNIGHT SERVICE THE REVERSER ACTUATOR WAS TRIMMED IAW MM, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20040225001172004022500117WP 2004 2 25 MEX2004020 120040116A30007914644501 DUCT DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE TAIL CONE BROKEN W ASMZA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23214AM 49585 AIRCRAFT RETURNED DUE TO LIGHT OF TAIL CONE HIGH TEMPERATURE CAME ON, AFTER 3 MINUTES THAT THE ANTI-ICE PROTECTION WAS USED. AIRCRAFT WAS CARRIED TO THE HANGAR TO ATTEND REPORT. AT OVERNIGHT SERVICE, THE ANTI-ICE DUCT ASSY WAS REPLACED AND SYSTEM WAS TESTED IAW MM. HARD LANDING INSPECTION WAS PERFORMED IAW MM, DETECTING A FUEL LEAKAGE IN THE CENTRAL LOWER SECTION OF THE FUEL TANK FRONT SPAR. THE FUEL TANK WAS SEALED IAW SRM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001182004022500118NE 2004 2 25 MEX2004021 220040117A7412103538754 IGNITER BOX DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMZD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23753RA519 49587 725439 AIRCRAFT RETURNED TO PLATFORM, THE RT ENGINE DID NOT START WHEN THE FUEL CONTROL WAS PUT ON, SHUTTING DOWN THE IGNITION AND THE START VALVE. THE IGNITION BOX WAS REPLACED AND SYSTEM TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040225001192004022500119NM 2004 2 25 MEX2004026 120040118A5754 SKIN BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE NR 5 DAMAGED W ASMZK NONE O OTHER ININSP/MAINT 1 SW23802AM AL0644 26270 DURING OVERNIGHT SERVICE, IT WAS DETECTED THAT THE SLAT NR 5 HAD DAMAGES AND MATERIAL LOST IN A 20 X 10 INCH AREA, AND THE WING LEADING EDGE HAD DAMAGES TOO. SLAT NR 5 WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW MM, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20040225001242004022500124EA 2004 2 25 X6PA200400002 220040127A7414SS1001 BOOSTER PIPER PA32 PA32260 7103206SO LYC O540 IO540* 41532EA MAGNETO INOPERATIVE E X6PAO OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SO334817 15 321277 L2001540A DURING RUNUP THE PILOT FOUND LT MAGNETO WAS INOPERATIVE. A MECHANIC INSPECTED THE AIRCRAFT AND FOUND THE SLICK START MAGNETO START BOOST BOX STC NR SA593CH MALFUNCTIONED AND GROUNDED THE LEFT MAGNETO OUT. THE MECHANIC REPLACED THE SLICK START BOX; THIS FIXED THE PROBLEM. 1L71 3O3 O A3SO 1E4 20040225001262004022500126NM 2004 2 25 DHL2004781001 120040127A7714 TACH GENERATOR BOEING727 727227 1384078NM ENGINE INOPERATIVE A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01781DH 21996 AT TAKEOFF, THRUST WITH ENGINE ANTI-ICE ON NR 3 EPR AT 2.18, NR 3 N1 INDICATED 80 PERCENT WITH TARGET N1 96 PERCENT. AIRCRAFT WEIGHT 151.5, IAS AT RTO - 85KTS, OAT - -1C, PRESSURE ALTITUDE 680 FT, BAROMETER 29.61, AND BRAKE ENERGY ZONE - NORMAL. INSPECTED ENGINE NR 3 C-1, C-2, INLET, EXH, LPT, SADDLE DUCTING, PT7, PT2, AND TIT PROBE. RUN ENGINES NR 1 AND NR 3 TO EPR 2.20, N1, N2, EGT, AND FUEL FLOW PARAMETERS NORMAL. SUBJECTED ENGINES TO VARIOUS BLEED LOADS (ANTI-ICE, PACKS) ALL OPS NORMAL IAW JRH 7.0. REMOVED AND REPLACED N1 TACH GENERATOR IAW BMM 77-21-1. COMPLIED WITH RTO SPCC CHECKS IAW BMM 05-51-121, ALL OPS NORMAL. 2L73 4F A3WE 20040225001272004022500127NM 2004 2 25 DHL2004750003 120040128A33501000677 LIGHT BOEING727 7272M7 138407SNM EMERGENCY EXIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01750DH 21951 ON P/F MAIN EXIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/N ON: 10-0067-7, S/N ON: 23781) 2L73 4F A3WE 20040225001322004022500132NM 2004 2 25 UPS04441903 120040202A5330 SKIN BOEING747 747123 1384873NM FUSELAGE MISREPAIRED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, DURING WORK ACCOMPLISH FOR RAP, ITEM N672-46-28 AT BS 1960-1975 STR 45R-47R EXISTING PATCH FOUND NOT MATCH WITH SRM 53-30-03 FIG 19 AS PROVIDED BY CUSTOMER RE-DO THE REPAIR REQUIRE. EXPANDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 48 AT FX STA 1960 TO STA 1980 BETWEEN STR 45R AND STR 47R AREA SUBSEQUENT INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 48 SHT 9 TABLE II & SHT 13 TABLE III. THIS REINSPECTION WILL BE CONTROLLED BY EO B747-5330-13494-H. 2L74 4F A20WE 20040225001332004022500133NM 2004 2 25 UPS04441904 120040122A53302024T30071IN SKIN BOEING747 747123 1384873NM EMPENNAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C EMP- LT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 STR 2L TO STR 3L VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2L-4L AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2290-2310 STR 2L-3L & BS 2330-2360 STR 2L-4L. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1 (UPS MPI ASSIGNED FOR REPEAT INSPECTION). 2L74 4F A20WE 20040225001342004022500134NM 2004 2 25 UPS04441905 120040127A5330 SKIN BOEING747 747123 1384873NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C DURING REPAIR ASSESSMENT PROGRAM ACCOMPLISH, ITEM N672-41-08 AT BS 447-463 STR 42R-44R 2 LAYERS REPAIR DOUBLER FOUND SINCE THE OUTER DOUBLER IS ONLY 0.040 INCH THK WHICH WILL CREATE KNIFE-EDGE CONDITION, RE-DO THE REPAIR REQUIRE. EXISTING DOUBLER REMOVED & DISCARDED AS PER SRM 53-30-03 FIG 1. HFEC INSPECTED AT THE REPAIR AREA FASTENER HOLES, NO CRACK REVEALED. NEW EXTENDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 1. SUBSEQUENCE INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 1 TABLE IV (REPEAT INSPECTION PER EO B747-5330-13494H). 2L74 4F A20WE 20040225001362004022500136NM 2004 2 25 UPS04441907 120040122A53302024T3007IN SKIN BOEING747 747123 1384873NM EMPENNAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C EMP- RT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 , STR 2R TO 3R VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2R-3R AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2329-2360 STR 2R-4R. BS 2280-2310 STR 2R-3R SKIN REPAIRED AS PER SRM 53-30-03 FIG 1. (UPS MPI ASSIGNED FOR REPEAT INSPECTION). 2L74 4F A20WE 20040225001372004022500137NM 2004 2 25 UPS04441908 120040125A5415AISI3010012IN FITTING BOEING747 747123 1384873NM NR 3 PYLON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, NR 3 PYLON DIAGONAL BRACE FWD ATTACH FITTING BASE AREA PITTING CORROSION FOUND. NR 3 PYLON DIAGONAL BRACE ATTACH FITTING LOWER SURFACE CORROSION REPAIR CARRIED OUT AS PER HX RS R-54-54-35098. (FAA 8110-3 DATED FEB 5, 2004 & EO B747-5440-19929-A APPROVED). 2L74 4F A20WE 20040225001402004022500140NM 2004 2 25 UPS04441911 120040121A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- BS 380 RT STR 25R FRAME FOUND CRACKED. REPAIRED FRAME PER RS 53-12-35103 AT BS 380 STR 25R AREA AND EO B747-5310-19928-A. 2L74 4F A20WE 20040225001412004022500141NM 2004 2 25 UPS04441912 120040127A5310 SHEAR TIE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2220 IN BETWEEN STR 40 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.071 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. ANGLE REPAIRED PER SRM 51-40-03 FIG 2. CIC APPLIED IAW EO M-5100-2780-1. 2L74 4F A20WE 20040225001422004022500142NM 2004 2 25 UPS04441913 120040121A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT- RT STA 790- STA 810 STRINGER 46 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED PER HX RS R53-21-35100 & UPS ENGINEERING FILE 747-53-20168. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040225001432004022500143NM 2004 2 25 UPS04441914 120040124A532065B065691 FLOOR SUPPORT BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- BS 2240 TP 2270 LBL 80 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8. CIC APPLIED IAW CPM53-10-17. 2L74 4F A20WE 20040225001452004022500145NM 2004 2 25 UPS04541896 120040206A5320 WEB BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01405UP 23727 INSPECTION TYPE:C-CHECK, CORROSION ON FLOOR SHEAR WEB IN SEVERAL AREAS BETWEEN BS 365 TO 395 LBL 46 TO LBL 62 WL 208. BS 368 LBL 46 OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS ALL WORK DONE IAW SRM 53-00-51 FIG 101, 51-70-13, 51-40-08, 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA2NM 20040225001462004022500146NM 2004 2 25 04FDEA00412 120040216A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232. 2L73 4F RTA3WE 20040225001502004022500150NM 2004 2 25 2004UALA00117 120040210A5315 FLOORBEAM BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 UPPER DECK FLOORBEAM WEB IS DENTED AND CRACKED STA 380 RBL 14. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED WEB, TAPER SHIM & STIFFENER REPAIRS. 2L74 4F4 FRTA20WE E24NE 20040225001512004022500151NM 2004 2 25 2004UALA00118 120040210A2150 JACKSCREW BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT PACK FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29643UA 25093 FLIGHT DIVERTED DUE TO LEFT PACK TEMPERATURE CONTROL MESSAGE AND LIGHT. THE LEFT PACK INLET ACTUATOR WAS FOUND MECHANICALLY FROZEN. THE JACK SCREW ASSEMBLY FAILED. THE ACTUATOR WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED. 2L72 4F4 FRTA1NM E24NE 20040223001532004022300153NM 2004 2 23 QXEA200400007 120040110A2710LA11A2118 ACTUATOR DHAV DHC8 DHC8202 2809007NM ZONE 600 FAILED A QXEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM09358PH13835 506 AFTER TAKEOFF FROM SEA, THE A/C HAD A SLIGHT ROLLING MOTION TO THE RT. THE CONTROLS FELT HARD TURNING TO THE LT. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT AILERON TRIM TAB SPRINGS AND THE AILERON TRIM ACTUATOR. OPERATIONAL CHECKS AND A CHECK FLIGHT WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040223001582004022300158SO 2004 2 23 ENHA2004P3101 120040108A5280 HINGE PIPER PA31 PA31350 7103110SO RT MLG DOOR BROKEN E ENHAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL034105D 318252027 AT TAKEOFF INITIAL CLIMB GEAR UP SELECTED (IN TRANSIT) LIGHT WOULD NOT EXTINGUISH. SELECT GEAR DOWN ALL GEAR GREEN. LANDED WITH OUT INCIDENT. FOUND RT MLG IB DOOR FWD HINGE BROKEN. LANDING GEAR LAST INSPECTED IAW AD 2000-25-01 AT 10754.9. REPLACED FWD HINGE WITH NEW P/N 47529-32. C/W SB 682. REINSPECTED AFT HINGE IAW AD 00-25-01 NO DEFECTS. 1L72 3O A20SO 20040223001932004022300193WP 2004 2 23 AALA20040065 120040113A80109794104 START VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED A AALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW219628W 53598 728182 DURING CLIMBOUT LT ENGINE FIRE WARNING CAME ON 5-10 SECONDS THEN WENT OUT. STAYED OUT 5-10 SECONDS THEN BACK ON FOR 2-3 SECONDS AND STAYED OFF FOR REMAINDER OF FLIGHT. ENGINE WAS SHUT DOWN USING FIRE HANDLE. ENGINE WINDMILLED 3 OR 4 MINUTES WITH NORMAL OIL PRESSURE. NO OTHER WARNING LIGHTS OR INDICATIONS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND LT ENGINE STARTER DISINTEGRATED AND FOUND 2 BY 3 INCH HOLE IN OUTSIDE SURFACE OF FAN BYPASS DUCT WITH ONE INCH HOLE PENETRATING THROUGH INTO FAN DUCT. REPLACED STARTER AND START VALVE. MADE INTERIM REPAIR TO ENGINE CASE. AIRCRAFT WILL BE FERRIED OR ENGINE CHANGE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F4 FRTA6WE E9NE 20040223001982004022300198EU 2004 2 23 RAIA00401004 120040104A3350 LAMP AEROSPATR72 ATR72202 8680940EU EMERGENCY LIGHT BLOWN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03723TE 283 ENTRY DOOR STEP EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2H72 4T RTA53EU 20040224000012004022400001NM 2004 2 24 COOSDR030048 120040101A5343 CHANNEL BOEING737 737200 1384453NM LT MLG CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 LT MAIN LANDING GEAR CHANNEL, CRACKED. 2L72 4F A16WE 20040224000052004022400005NM 2004 2 24 COOSDR030054 120040101A575165464542 SKIN BOEING737 737200 1384453NM RT WING AILERON DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, AILERON (PN-65-46454-2) SN 305, SKIN DELAMINATED. 2L72 4F A16WE 20040224000062004022400006NM 2004 2 24 COOSDR030055 120040101A55106553746127 SEAL BOEING737 737200 1384453NM HORIZONTAL STAB CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 LT HORIZONTAL STABILIZER BLADE SEAL CRACKED. 2L72 4F A16WE 20040224000192004022400019EA 2004 2 24 ASOA04018 120040107A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, FRAME FS 718, STRINGERS 10-11 ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED FRAME FS 718, STRINGERS 10-11 ON THE RT SIDE IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20040224000212004022400021EA 2004 2 24 ASOA04010 120040105A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A GROUND INSPECTION, THE AFT OVERHEAD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OVERHEAD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040224000222004022400022EA 2004 2 24 ASOA04053 120040120A5260601R317731 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11886AS 7531 DURING A HANGAR INSPECTION, THE TOP STEP PANEL ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040224000392004022400039EU 2004 2 24 ASOA04055 120040121A3350OL3042BPE LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11532AS 458 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY EXIT LIGHT AT THE SERVICED DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040224000422004022400042EU 2004 2 24 USAASA04002 120040111A4990 OIL COOLER AIRBUS320 A320214 3930316EU APU LEAKING A USAAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19107US13654 1052 PHL - FLT 160, CREW NOTED OIL ODOR IN CABIN AFTER TAKEOFF FROM PHX. MAINTENANCE FOUND LEAK IN THE APU OIL COOLER. THE APU WAS PLACED ON MEL AND WAS REPLACED SUBSEQUENT TO THIS REPORT. (M) 2L72 4F RTA28NM 20040224000452004022400045EA 2004 2 24 A6WA200440015 120040130A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS STUCK A A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31429AW 7711 ON TAKEOFF, FLAPS STUCK AT 20 DEGREES. FECU INTERROGEAED NIL FAULTS FOUND. AIRCRAFT HANGARED 4.5 HOURS. FECU SYSTEM TESTED AS PER 27-51-05-946-009 JOB TASK. FLAPS CYCLED ALL POSITIONS, CHECKED SERVICEABLE. (M) 2L72 4F RTA21EA 20040224000482004022400048EU 2004 2 24 USAASA04003 120040113A49904500001B APU AIRBUS320 A320214 3930316EU APU BAY LEAKING A USAAFA ACTIVATE FIRE EXT. UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19107US 1052 ALB - FLT 1471 - EN ROUTE PHL-MHT, CREW RECEIVED THE AFT CARGO FIRE WARNING. CREW ALSO NOTED AN OIL ODOR IN THE CABIN/COCKPIT. CREW DISCHARGED THE CARGO FIRE BOTTLES AND FLIGHT DIVERTED TO ALB. FLIGHT LANDED WITHOUT FURTHER INCIDENT. THIS INCIDENT IS BELIEVED TO BE RELATED TO THE OIL LEAK FROM THE APU. MAINTENANCE REPLACED THE APU, THE CARGO COMPARTMENT FIRE BOTTLE, AND FIRE BOTTLE SQUIBS. ALSO, PERFORMED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040224000512004022400051EA 2004 2 24 ASOA04022 120040107A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 FLT 4725 - DURING A GROUND INSPECTION IN DFW, THE THIRD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE THIRD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000542004022400054NM 2004 2 24 GAIA04003OP 120040120A2420 GENERATOR BOEING727 727214 138407RNM NR 1 & 2 MALFUNCTIONED A GAIAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW07751US 21513 FLT 734 - FWA-DFW - DURING CLIMB, THE FLIGHT CREW NOTICED ELECTRICAL SPIKING ON THE NR 1 AND NR 2 GENERATORS AND THAT THE LIGHTS AND THE RADAR WERE FLICKERING. THE AIRCRAFT RETURNED TO FWA AND MADE AN OVERWEIGHT LANDING WITHOUT INCIDENT. (M) 2L73 4F A3WE 20040224000592004022400059EA 2004 2 24 ASOA04026 120040108A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, A CLIP UNDER THE CARGO COMPARTMENT SILL PLATE AT FS 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED A CLIP UNDER THE CARGO COMPARTMENT SEAL PLATE AT FS 589, IAW SRM 51-42-21. (M) 2L72 4F RTA21EA 20040224000842004022400084EA 2004 2 24 COMA0470015 120040208A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA LANDING GEAR UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01653CA187 10129 FLIGHT 5661 GEAR DISAGREE WARNING AFTER T/O. REPLACED THE L/G SELECTOR VALVE. 2L72 4F RTA21EA 20040224000972004022400097WP 2004 2 24 GKZR200482301 120040203A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 RIGHT SIDE STA 35 L30 SKIN HAS CORROSION. REMOVED FASTENERS IAW DC-8 SRM 51-1-20, DRILLED NEW DOUBLER PART NUMBER 5649028U AND INSTALLED IAW DC-8 SRM 51-1-21, DRILL AND INSTALLED NEW LONGERON PART NUMBER 3648667 IAW DC-8 SRM 51-1-21. (CLOSED) 2L74 4F RT4A25 20040224000992004022400099WP 2004 2 24 GKZR200482303 120040203A53215007C5042B FLOOR PANEL DOUG DC8 DC871F 302199DWP FUSELAGE DELAMINATED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 MAIN CARGO FLOOR FORM PALLET POSITION 4 AFT HAS MULTIPULE AREAS OF DISBONDING. REMOVED ALL HARDWARE FROM MAIN CARGO COMPARTMENT FLOOR P4 AFT IAW DC-8 SRM 51-03-00. FABRICATED REPLACEMENT FLOOR BOARDS FROM GIL FAB BOARD 16 EA. FROM 5042B ATI PO 16802. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 51-3-0 THE REMAING FLOORBOARDS CONFORM TO ATI REQ. REF PART INFORMATION LETTER 47 DATED FEB. 17, 2004.(CLOSED) 2L74 4F RT4A25 20040224001162004022400116NM 2004 2 24 QXEA200400129 120040207A2121AE1716B00 FAN DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH12884 520 PDX - ON FLIGHT NUMBER 2006, AFTER GROUND FAN WAS SHUT OFF, THERE WAS A POTENT ACRID BURNING ODOR. ODOR DISSIPATED BUT FAN WILL NOT WORK. REMOVED AND REPLACED GROUND AIR FAN. INSTALLED NEW FUSE IN DC CONTACTOR BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040224001322004022400132SO 2004 2 24 C2XA04SH060 120040212A532014521725001 SILL EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV-DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001342004022400134SO 2004 2 24 C2XA04SH062 120040212A531014522460013 BUTTSTRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001362004022400136SO 2004 2 24 C2XA04SH064 120040212A531314528737001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01106 AND EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001482004022400148NM 2004 2 24 CALA0400108 120040212A335020131A BATTERY PACK BOEING737 7373T0 1384582NM R-2 DOOR INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2714307 23358 INSPECTION FOUND R-2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20040224001512004022400151NM 2004 2 24 CALA0400111 120040213A5315BAC150910046 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND AFT CARGO FLOORBEAMS UNDER CROSS STRAP CORRODED AT STA 767 + 6, RBL 8, RBL 3, AND LBL 3. REPAIRS WERE INSTALLED IAW ECRA 5320-01603. 2L72 4F RTA16WE 20040224001632004022400163WP 2004 2 24 UPS04841867 120040131A5320975400284 FLOOR SUPPORT DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, FLOOR SUPPORT FITTING IS CRACKED AT STATION 340 LONG 36-33L. REMOVED AND REPLACED FITTING IAW DWG 9754002 AND SRM 51-1-20D. 2L74 4F RT4A25 20040224001762004022400176WP 2004 2 24 UPS04841887 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001842004022400184NM 2004 2 24 04FDEA00397 120040211A5311AKC76023 FRAME DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 AFT TAIL CONE LT FWD FRAME FOUND WITH CHAFED MARK. AFT TAIL CONE LT FWD FRAME REMOVED & REPLACED AS PER SRM 513101 V2. 2L73 4F RTA22WE 20040224001892004022400189NM 2004 2 24 CALA0400116 120040214A5320149761411 STRUCTURE BOEING737 737724 13844BYNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A 1 INCH CRACK IN RT MAIN WHEEL WELL AFT CHORD. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040224001942004022400194NM 2004 2 24 CALA0400122 120040215A5315146A9401 FLOORBEAM BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714731 28799 INSPECTION FOUND AFT CARGO FLOORBEAM STRAP CORRODED AT STA 727D + 6. THE FLOORBEAM STRAP WAS REMOVED AND REPLACED IAW SRM 53-60-53. 2L72 4F RTA16WE 20040225000072004022500007NM 2004 2 25 COOSDR030070 120040101A5711 SPAR BOEING727 727224 1384076NM LT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 LT WING, FRONT SPAR LOWER CHORD PLATE, LOWER SURFACE CORRODED, BETWEEN SS 130.250 AND SS 143.750. 2L73 4F A3WE 20040225000092004022500009NM 2004 2 25 COOSDR030072 120040101A5313 STRINGER BOEING727 727224 1384076NM FUSELAGE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 AFT CARGO COMPARTMENT, STRINGER 28R CORRODED, BETWEEN BS 950D+18 AND BS 950E+12. 2L73 4F A3WE 20040225000102004022500010NM 2004 2 25 COOSDR030073 120040101A57306521656601 PANEL BOEING727 727224 1384076NM LT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 LT WING, LOWER SURFACE FIXED PANEL PN:65-21656601, OUTER SKIN, CORRODED. 2L73 4F A3WE 20040225000152004022500015NM 2004 2 25 COOSDR030079 120040101A552365727993 SKIN BOEING727 727224 1384076NM LT ELEVATOR TAB DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 LT ELEVATOR TAB PN 65-72799-3 SN BN1687 UPPER AND LOWER SKIN DELAMINATED. 2L73 4F A3WE 20040225000202004022500020NM 2004 2 25 COOSDR030085 120040101A5755 SKIN BOEING727 727224 1384076NM RT WING SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 1236 22448 RT FLIGHT SPOILER NR 8 DELAMINATED. 2L73 4F A3WE 20040225000212004022500021NM 2004 2 25 COOSDR030088 120040101A5751 SKIN BOEING727 727224 1384076NM LT WING AILERON DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 BN319 22448 LT WING, OB AILERON PN65-21766-19, SN BN319 TRAILING EDGE DELAMINATED. 2L73 4F A3WE 20040225000282004022500028EU 2004 2 25 2004F00043 120040119A769730709341 WIRE HARNESS BRAERODH125 HS125700A 4230170EU RT ENGINE DETERIORATED E A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CE03120JC6970 NA0247 WHILE EN ROUTE TO MMSD, NOTED RT ENGINE AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED INDICATED LOSS OF POWER RT ENGINE. CONSULTED OPERATORS MANUAL AND COMPLIED WITH EMERGENCY PROCEDURES WHICH INCLUDED TO SWITCH TO MANUAL CONTROL AND MONITOR ALL ENGINE PARAMETERS. IMMEDIATELY NOTIFICATION TO ATC AND REQUESTED TO DIVERT TO DAL FOR INSPECTION AND REPAIR. FOLLOWING INSPECTION AND TROUBLESHOOTING, IT WAS NOTED THAT THE PT2 HARNESS HAD INTERMITTENT CONTACT AND WAS DEFECTIVE. THE PN 3070934-1 WAS REPLACED AND SYSTEM FUNCTION TEST WAS WITHOUT DEFECTS. 2L72 4F A3EU 20040225000332004022500033SO 2004 2 25 X6PA200040001 120040117A79218529245 OIL COOLER PIPER PA32 PA32R300 7103213SO RT ENGINE BROKEN E X6PAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO334498F 32R7680453 THE PILOT CONDUCTED A NORMAL PREFLIGHT. APPROXIMATELY 35 MINUTES AFTER TAKE OFF, THE PILOT NOTICED AN OIL PRESSURE DROP, AND DECLARED AN EMERGENCY. THE PILOT LANDED SAFELY. THE AIRCRAFT'S BELLY WAS FOUND COVERED IN OIL. FURTHER INSPECTION SHOWED THE OIL LEAK COMING FROM THE REAR RIGHT OIL COOLER COOLING FINS. 1L71 3O A3SO 20040225000572004022500057 2004 2 25 MEX200410 420040107A3417HG280D80 COMPUTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE AIR DATA FAILED W ASMFA UNSCHED LANDING O OTHER CLCLIMB 1 SW23168PL 53174 AC RETURNED TO PLATFORM DURING TAKEOFF, LT SPEED INDICATOR HAD 80 KNTS AND RT SPEED INDICATOR AT 65 KNTS. DURING REVISION WERE DETECTED CADC NR 2 WITH FAILURE IN CDUS, RT SPEED INDICATOR FLAG AND FAST/ SLOW FUNCTION IN RT PFD WITH FAILURE. CADC NR 2 WAS TESTED IAW MM, CONNECTION LINES AND PITOT TUBE AND STATIC PORT WERE CLEANED, ALL TEST CORRECT. BOTH CADC WERE REPLACED, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001032004022500103EU 2004 2 25 MALA040134 120040121A5310 PLATE SAAB SF340 340B 7860101EU PAX DOORWAY DIRTY A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15430XJ 340B430 DURING FLIGHT NR 3027, MAIN DOOR HANDLE LIGHT ON INDEX MARK DO NOT MATCH. AIR RETURN TO MSP. MAINTENANCE FOUND DOOR TO BE CLOSED AND HANDLE AFT END JUST SLIGHTLY FROM FULLY DOWN. DOOR INDEXES ARE VISABLE INSPECTED DOOR SWITCH. NO FAULTS FOUND. CLEANED AND LUBED DOOR FRAME CONTACT PLATES TO ALLOW SMOOTHER DOOR OPERATION DO AND INDICATION OPS CHECK GOOD. 2L72 4T RTA52EU 20040225001062004022500106EU 2004 2 25 MALA040135 120040118A52607256200503 AIRSTAIR SAAB SF340 340B 7860101EU PAX DOOR BROKEN A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15415XJ 340B415 STATION AGENT REPORTS THAT THE STAIRS ARE BROKEN AND WILL NOT STOW. AIRSTAIRS RAILING LINKS BROKE WHEN LOWERING IN GFK. MAINTENANCE REPLACED AIRSTAIR ASSEMBLY PN 7256200-503 IAW AMM 52-60-03. OPS CHECK GOOD. 2L72 4T RTA52EU 20040225001112004022500111 2004 2 25 V9M2004F00000 420040106A6122F635 GOVERNOR PIPER PA60 PA60600 7106001NM LYC O540 IO540J4A5 41532EA HARTZLHCC3Y HCC3YR2 NE LT ENG PROP FAILED B V9MRA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO098234J 1591 600638796120L2422248A CK2016E PROPELLER GOVERNOR WENT TO HIGH PITCH CONDITION DURING CRUISE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. 1M72 3O3 ORTA17WE 1E4 5 CP25EA 20040225001132004022500113GL 2004 2 25 ALG2004F00000 220040108A7200223005290 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 2 MAKING METAL E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03519AL 760058 CAE890416S IN FLIGHT, NR 2 ENGINE CHIP LIGHT CAME ON. MAINTENANCE FOUND METAL ON FWD PLUG ON NR 2 ENGINE. SMALL RING OF TINY FLAKES ON OUTSIDE PERIMETER OF CHIP PLUG. AIRCRAFT AOG FOR ENGINE. 1G72 3U3 U H1NE E1GL 20040225001282004022500128NM 2004 2 25 2004UALA00088 120040201A5753 HINGE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE TE FLAPS CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 RIGHT INBOARD FLAP CENTER HINGE, OUTBOARD FLANGE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE FITTING. 2L72 4F4 FRTA1NM E24NE 20040225001352004022500135NM 2004 2 25 UPS04441906 120040128A5230 SKIN BOEING747 747123 1384873NM AFT CARGO DR. DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, EO 747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING RAP INSPECTION, ITEM N672-46-24, BS 1840-1860 STR 42R AFT CARGO DOOR LWR EDGE REPAIR DOUBLER HAS LESS THAN 2 ROWS OF FASTENER BEYOND THE DAMAGE AREA. THIS REPAIR IS CLASSIFIED AS PER -D- REPAIRED. EXPANDED DOUBLER REPAIRED AS PER SRM 52-30-06 FIG 1 AT AFT CARGO DOOR. MID LOWER EDGE AT BS 1840-1860 STR 42R AREA REPEAT INSPECTION REQ'D SRM 52-30-06 FIG 1 SHT 12 TABLE II. (REPEAT INSPECTION PER EO B747-5330-13494-H). 2L74 4F A20WE 20040225001832004022500183NM 2004 2 25 DL76S040001 120040101A2560P2070003001 FLASHLIGHT BOEING767 767332 1382001NM CABIN UNSERVICEABLE A DALAO OTHER O OTHER CRCRUISE 1 SO27133DN 24982 DURING MEDICAL EMERGENCY, EEMK, WALKAROUND 02 BOTTLE, FLASHLIGHT, AND BIOHAZARD KIT WERE USED. REPLACED EEMK O2 BOTTLE FLASHLIGHT BIOHAZARD KIT AND EMK. OK CONTINUED SERVICE. 2L72 4F RTA1NM 20040225001842004022500184NM 2004 2 25 DL738040002 120040103A25302281 CHILLER BOEING737 737832 13844CFNM FWD GALLEY OVERHEATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27395DN 30773 FUMES IN CABIN AT FL 350 INCREASING IN INTENSITY. SECURED GALLEY POWER AND ENTERTAINMENT SYSTEM. DIVERTING TO CLT. ISOLATED SMELL TO FWD GALLEY CHILLER DUE TO OVERHEAT FROM CLOGGED FILTER AND CLOGGED DUCT TO CHILLER. REPLACED CHILLER AND CLEANED DUCT. 2L72 4F RTA16WE 20040225001862004022500186NM 2004 2 25 DL764040004 120040102A3350D71702001 POWER SUPPLY BOEING767 767432ER 1385134NM EMERGENCY LIGHT FAILED A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27825MH 29696 EMERGENCY LIGHTS ON SEATS 17AB THRU 25AB INOP. SEATS ONLY LEFT SIDE. FOUND PWR SUPPLY M 6759 AT FAULT. REPLACED SAME, CHECKS GOOD. 2L72 4F RTA1NM 20040225001872004022500187NM 2004 2 25 DLM88040005 120040103A2432249701544 BATTERY DOUG MD88 MD88 3023688NM FWD E/E OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27977DL 53258 FOUND BATTERIES OVERHEATING AT GATE WITH WHITE SMOKE. REPLACED BATTERIES AND CHARGER. 2L72 4F RTA6WE 20040225001882004022500188NM 2004 2 25 DLM88040006 120040103A3260387 BULB DOUG MD88 MD88 3023688NM MLG INDICATOR BURNED OUT A DALAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO27902DE 53379 RIGHT MAIN LANDING GEAR LIGHT BURNED OUT. GEAR INSPECTION VIEWING PORT DIRTY AND DIFFICULT TO SEE THROUGH. RELAMPED RT MLG INDICATOR CAPSULE AND CLEANED VIEWING PRISM. 2L72 4F RTA6WE 20040225001892004022500189NM 2004 2 25 DL733040007 120040104A3244 TIRE BOEING737 737347 1384647NM NR 2 CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO27302WA 23182 ON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM. 2L72 4F RTA16WE 20040225001922004022500192NM 2004 2 25 DLM88040010 120040106A53305920323211 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27907DL 49538 A CRACK WAS FOUND IN THE UPPER, FWD CORNER OF THE C-1 DOOR JAMB IN BOTH THE SKIN AND ALUM DOUBLER. A TYPICAL SRM REPAIR ALSO EXISTS IN THE NEARBY AREA. NEW DAMAGE AND OLD DAMAGE INCORPORATED INTO ONE REPAIR PER ERA 386012-14. 2L72 4F RTA6WE 20040225001962004022500196NM 2004 2 25 DLM88040015 120040108A2120 ODOR DOUG MD88 MD88 3023688NM COCKPIT DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27928DL 49715 ON SHORT FINAL WITH ENG AND AIRFOIL A/I ON, THERE WAS A BURNING ODOR IN AFT CABIN AND F/O SIDE AFT LAV SMOKE DETECTOR WAS SOUNDING. ODOR CLEARED WHEN AIRFOIL A/I WAS TURNED OFF. CHECKED A/C FOR ENGINE AND HYDRAULIC LEAKS. NONE NOTED. PERFORMED OPN 5089 PNEU SYSTEM DUCT BURNOUT. CHECKS GOOD. ALSO PERFORMED OPN 5088 PNEU DIST CABIN SMOKE/ODOR TROUBLESHOOTING. 2L72 4F RTA6WE 20040225001972004022500197NM 2004 2 25 DL75K040016 120040108A2750 CONNECTOR BOEING757 757232 1384965NM TE FLAPS DIRTY A DALAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 SO276706Q 30422 TRAILING EDGE FLAP DISAGREE ON FINAL WHEN GOING FROM 20 DEGREES TO 25 DEGREES SETTING. RESET TO 20 DEGREES AND ACCOMPLISHED ABNORMAL CHECKLIST. UNEVENTFUL LANDING. SPEED WAS 180 KTS WHEN REQUESTED TO 25 DEGREES. PERFORMED BITE ON FLAP/SLAT UNITS NO EXISTING FAULTS. NR 1 FSEU ON LEG O FAULTING FLA FAIL CODE 217. FLAP LOAD RELIEF - INTERMITTENT. T/S PER FIM CLEANED CONNECTOR ON FLAP LOAD RELIEF SOLENOID. NO FAULTS ON ADC PER FIM. CYCLED AND FLAP/SLATS SEVERAL TIMES WITH NO LOCKOUT MESSAGES. 2L72 4F RTA2NM 20040225001982004022500198NM 2004 2 25 DL757040017 120040108A5754570467178A SKIN BOEING757 757232 1384965NM NR 9 SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27665DN 25013 NR 9 SLAT WORN ON LOWER SURFACE. REPAIRED PER SRM 51-70-10 PERMANENT REPAIR. 2L72 4F RTA2NM 20040226000282004022600028NM 2004 2 26 ASAA0410036 120040119A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040226000312004022600031NM 2004 2 26 ASAA0410041 120040125A33508821004 BATTERY PACK BOEING737 737290C 138448VNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - DURING INSPECTION, FOUND TRACK LIGHTING INOPERATIVE AT ROW 17. REPLACED BATTERY ON SEAT PALLET 8-13. OPS CHECK GOOD. (M) 2L72 4F A16WE 20040226000352004022600035NM 2004 2 26 ASAA0410037 120040120A335086210144 BATTERY BOEING737 7372X6C 1384552NM EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 SEA - DURING INSPECTION, FOUND MID CABIN OVERHEAD EXIT SIGN INOPERATIVE AND FLOOR TRACK LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. REPLACED MID CABIN OVERHEAD SIGN BATTERY PACK AND TRACK LIGHTING CONTROL MODULE (P/N 873203041) THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040226000372004022600037NM 2004 2 26 ASAA0410043 120040126A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC - DURING INSPECTION, FOUND TRACK LIGHTING INOPERATIVE AT PALLET 9-10. REPLACED BATTERY ON SEAT PALLET 9-10. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040226000382004022600038NM 2004 2 26 ASAA0410039 120040124A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040226000412004022600041NM 2004 2 26 QXEA200400125 120040210A272182410608007 TRIM PANEL BOMBDRDHC8 DHC8401 1390041NM RUDDER MALFUNCTIONED A QXEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM09407QX5846 4049 GEG - FLIGHT 2356 IN CRUISE PHASE OF FLIGHT, RUD TRIM WENT FULL RIGHT UNCOMMANDED. CREW NEUTRALIZED SITUATION AND RAN CHECK LIST, AND PULLED CIRCUIT BREAKERS. REPLACED AILERON/RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040226000422004022600042NM 2004 2 26 QXEA200400133 120040206A3210 LANDING GEAR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - NR 1 MAIN LANDING GEAR FOUND TO BE CHAFED BEHIND AFT CENTER FAIRING ASSEMBLY. REPAIRED IAW HORIZON AIR EA 6-32-296. 2H72 4T RTA13NM 20040226000442004022600044NM 2004 2 26 AALA20040222 120040212A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21962AN 30858 RDU - SEAT MOUNTED EMERGENCY LIGHTS IN FIRST FIVE ROWS OF COACH INOPERATIVE. REPLACED BATTERY PACK M1676 FOR SEAT MOUNTED EMERGENCY LIGHTS IN FIRST FIVE ROWS OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040226000452004022600045NM 2004 2 26 AALA20040223 120040212A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 SFW - INTERIOR EMERGENCY EXIT LIGHT AT SEATS 31 THROUGH 40HJ INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT SEATS 31 THROUGH 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040226000472004022600047NM 2004 2 26 QXEA200400145 120040213A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09354PH5950 5950 498 MFR - ON FLIGHT 2083 IMMEDIATELY AFTER TAKEOFF, NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST AND CYCLED NR 2 AC GENERATOR SWITCH OFF, THEN ON. NO CHANGES NOTED. NR 2 AC GENERATOR CAUTION LIGHT IS STILL ILLUMINATED. REMOVED AND REPLACED NR 2 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040226000482004022600048NM 2004 2 26 QXEA200400146 120040212A24324011769 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH7936 13 480 SEA - ON FLIGHT 2045 STANDBY BATTERY TEMPERATURE INDICATED CAUTION AREA. RUBBER ODOR IN COCKPIT. REMOVED AND REPLACED MAIN AND AUXILLARY BATTERIES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040226000502004022600050EA 2004 2 26 QXEA200400148 120040213A2460830CE02Y01 CIRCUIT BOARD CNDAIRCL600 CL6002C10 1390015EA ZONE 200 INOPERATIVE A QXEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NM09617QX259 259 10130 DEN - ON FLIGHT 4093 DURING TAKEOFF ROLL CAPTAIN'S PFD, MFD, NR 2 EDU & NR 1 RTU WENT BLANK, THEN CAME BACK ON. REMOVED AND REPLACED PCB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040226000542004022600054NM 2004 2 26 QXEA200400140 120040213A7120 STRUT DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX - LITE CHAFING DAMAGE ON NR 1 ENGINE LOWER INBOARD SUPPORT STRUT AT APPROXIMATELY STATION XN85.00. REPAIRED IAW HORIZON AIR EA 2-54-201. 2H72 4T RTA13NM 20040226000562004022600056NM 2004 2 26 DL738040019 120040109A7710 ACQUISITION UNIT BOEING737 737832 13844CFNM ENGINE UNSERVICEABLE A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO273747D 29665 AFTER PUSHING TOGA BUTTONS FOR INITIAL T/O POWER ADVANCED TO NEAR T/O POWER. IMMEDIATELY RECEIVED A MASTER CAUTION LIGHT. MASTER CAUTION LIGHT WENT OUT 2 TO 3 SECS AFTER THROTTLE TO IDLE. AMBER REVERSER LIGHTS FOR BOTH ENGINES WERE ON AND REMAINED ON FOR A FEW MORES SECS THEN WENT OUT. ENGINE ANTI ICE WAS ON. T/S PER FIM. REPLACED ENGINE ACQUISITION UNIT PER MM AS PRECAUTION. 2L72 4F RTA16WE 20040226000582004022600058NM 2004 2 26 DL73S040021 120040109A53306545800602 SKIN BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 THE FUSELAGE SKIN WAS FOUND DENTED FROM BS 328 TO BS 344, BETWEEN S20R AND S21R. DENT WAS REPAIRED PER ERA 386008-14. 2L72 4F A16WE 20040226000602004022600060 2004 2 26 DL757040023 420040108A2565 SPRING BOEING757 757232 1384965NM R4 DOOR GIRT BARWORN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27686DA 27589 ON ARRIVAL F/A REPORTED R4 DOOR SLIDE DIFFICULT TO DISARM. FOUND GIRT BAR RETAINING SPRINGS WORN. REPLACED GIRT BAR PER MM, RII COMPLIED WITH. 2L72 4F RTA2NM 20040226000612004022600061NM 2004 2 26 DLM88040024 120040110A3350339101295 BATTERY PACK DOUG MD88 MD88 3023688NM EMERGENCY LIGHT OVERHEATED A DALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SO27965DL 49984 ON FINAL APPROACH TO ATL CREW REPORTING BURNING ODOR, AFT LEFT LAV SMOKE DETECTOR SOUNDING. FLIGHT CREW DONNED O2 MASKS. FOUND FORWARD EMERGENCY LIGHT BATTERY PACK OVERHEATING. REPLACED SAME. 2L72 4F RTA6WE 20040226000632004022600063NM 2004 2 26 DL76S040026 120040110A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27138DL 25409 DURING SVC CHECK FOUND LT FWD CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2L72 4F RTA1NM 20040226000652004022600065NM 2004 2 26 DL73S040029 120040112A3234324202845 SOLENOID BOEING737 737247 138448DNM COCKPIT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27380DL 23607 DURING TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE AS PER THE CHECKLIST FLAP WERE RETRACTED TO 0 AND NO T/O WARNING HORN WAS NOTICED. REPLACED GEAR HANDLE INTERLOCK SOLENOID. 2L72 4F A16WE 20040226000662004022600066NM 2004 2 26 DL76P040030 120040110A5753113T22525 FITTING BOEING767 767332 1382001NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO271402A 25989 INSPECTION OF THE COLLAR BOLTS ON THE INBOARD MAIN FLAP COLLAR FITTING (LT & RT) AT THE INBOARD END OF THE FLAP REVEALED CORROSION IN THE HOLE BORES OF THE FITTINGS. THE DAMAGED COLLAR FITTINGS WERE REMOVED AND REPLACED PER BAC S/B 57A0066 AND ER/A 088153-14AD. 2L72 4F RTA1NM 20040226000672004022600067NM 2004 2 26 DL764040031 120040112A5330146T35313 SKIN BOEING767 767432ER 1385134NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27831MH 29702 THE FUSELAGE SKIN WAS DENTED BY GROUND EQUIPMENT NEAR FS 1367 AND STRINGER 29R. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 088020-14, REV B. 2L72 4F RTA1NM 20040226000712004022600071NM 2004 2 26 DL738040035 120040114A2120 ODOR BOEING737 737832 13844CFNM COCKPIT DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27383DN926 30346 STRONG ELECTRICAL ODOR OBSERVED SHORTLY AFTER FLIGHT. FLIGHT WAS AN AIR TURNBACK. RAN ENGS TO ALL POWER SETTINGS, INSPECTED ALL GALLEY OVENS AND COFFEEMAKERS AND E&E COMPARTMENT, NOTHING FOUND. 2L72 4F RTA16WE 20040226000732004022600073NM 2004 2 26 DLM88040037 120040115A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27902DL 49533 DENTS IN FUSELAGE STA 223 BETWEEN STR 17L & 18L. ALSO DENTS AT FS 218-227 BETWEEN STR 18L & 19L. ALL DENTS REPAIRED PER DRD 53-04D FIG 12B SHT 34 - 36 & 95 PG 60F. THE A/C RECEIVED THE FWD 2 REPAIRS AND THE UPPER AFT REPAIR AS ILLUSTRATED IN THE FIGURE. 2L72 4F RTA6WE 20040226000762004022600076NM 2004 2 26 DL73S040040 120040115A5330654577319 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 DENTING NOTED IN THE FUSELAGE SKIN AT APPROXIMATELY BS 862, BETWEEN S13L AND S14L. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385998-14. 2L72 4F A16WE 20040226000782004022600078NM 2004 2 26 DL764040042 120040115A5754 FLAP BOEING767 767432ER 1385134NM LEFT WING OUTBD BIRD STRIKE A DALAO OTHER O OTHER NRNOT REPORTED 1 SO27844MH 29717 LEFT OUTBOARD FLAP BIRD STRIKE CAUSING DELAMINATION. PER SRM WILL REQUIRE MAJOR REPAIR. REMOVED DAMAGE AND LAYERED UP REPAIR PER SRM 57-53-01 AND 51-70. OK TO INSTALL REPAIR QC1446. INSTALLED REPAIR PER SRM 51-70-1. OK TO REFINISH REPAIR QC1446. RESTORED FINISH PER AMM QC14. 2L72 4F RTA1NM 20040226000792004022600079NM 2004 2 26 DL73S040043 120040115A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 DURING ACCOMPLISHMENT OF INSPECTIONS PER AD 2003-08-15, 3 CRACKS WERE FOUND IN LOWER ROW FASTENER LOCATIONS OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 559 & 579. THE CRACKED AREA OF SKIN WAS CUTOUT. THE CUTOUT WAS REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3, FIG 42 AND ER/A 087880-14AD. 2L72 4F A16WE 20040226000822004022600082NM 2004 2 26 DL73S040046 120040116A53156545410223 FLOORBEAM BOEING737 737247 138448DNM BL 0.07, BS667 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 DURING ACCOMPLISHMENT OF 03-062982-03AD THE UPPER CHORD OF THE BL 0.07 FLOORBEAM WAS FOUND SEVERED AT A TYPICAL LOCATION (BS 661) AND A CRACK INDICATION AT BS 665, BS 669 AND BS 673. DAMAGE WAS REPAIRED AS PER ERA 385959-14AD. 2L72 4F A16WE 20040226000842004022600084NM 2004 2 26 DLM88040048 120040116A3260 SWITCH DOUG MD88 MD88 3023688NM NLG INTERMITTENT A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27967DL 53116 ON TAKEOFF CREW NOTICED EXCESSIVE NOSE GEAR VIBRATION. AFTER GEAR RETRACTION, HAD RED NOSE GEAR UNSAFE LIGHT. COMPLIED WITH POM GOT THREE GREEN LIGHTS. FOUND SWITCH S1-412 OPERATING INTERMITTENTLY. REPLACED SAME. 2L72 4F RTA6WE 20040226000862004022600086NM 2004 2 26 DL76L040051 120040116A5753113T220137C SKIN BOEING767 767332 1382001NM LT WING TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO271201P 28458 DENT OCCURRED TO INBOARD T/E MAIN FLAP LOWER SKIN DUE TO MLG TREAD SEPARATION. DENT FOUND DURING MTC AND INSPECTION OF AIRCRAFT AFTER FLIGHT. DENT WAS CUT OUT AND REPAIRED WITH METAL BOND REPAIR. REPAIRED PER ERA 426883-14. 2L72 4F RTA1NM 20040226000892004022600089NM 2004 2 26 DL73S040054 120040116A5330654577320 LAP JOINT BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 INSPECTION OF THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT BETWEEN FS 727 & 908 REVEALED A SCRIBE LINE ALONG THE LENGTH OF THE PANEL. THE ENTIRE LAP JOINT ALONG THE PANEL LENGTH WAS CUT AND REMOVED AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER BAC S/B 737-53A1177 AND ER/A 087849-14. 2L72 4F A16WE 20040226000912004022600091NM 2004 2 26 DL76L040056 120040119A2560P4010021SM BATTERY BOEING767 767332 1382001NM FLASHLIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27179DN 25144 L2 FLASHLIGHT INOP. REPLACED BATTERY AND BULB OPS CHECK OK PER MM. MCO AND PLACARD REMOVED. 2L72 4F RTA1NM 20040226000922004022600092NE 2004 2 26 DL757040057 220040117A7200 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27631DL48332 23612 716479 RT ENGINE IFSD FOR LOW OIL PSI. AFTER SHUTDOWN RT ENGINE OIL PSI FLUCTUATED 0-3 PSI. FOUND METAL ON CHIP DETECTORS. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20040226000942004022600094 2004 2 26 DLM88040059 420040120A22971C610X20RD WIRE DOUG MD88 MD88 3023688NM YAW DAMPER SHORTED A DALAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO27946DL 49819 CLIMBING THRU 11,500 ACCELERATING THRU 280 KTS THE DFG SW A C/B POPPED. A/P AND A/T DISSENGAGED. A/T ALERT WINDOW BLANK, YAW DAMP OFF MSG, MACH TRIM INOP MSG AND NOTICEABLE YAW. FOUND WIRE 1C610X20RD SHORTED TO GROUND AT TOP OF VERTICAL STAB. REPAIRED WIRING RAN NR 1 AND NR 2 A/P RTS ALL CHECKS GOOD. CB DFGS SWITCH A DOES NOT POP. 2L72 4F RTA6WE 20040226000952004022600095NM 2004 2 26 DL733040060 120040117A5330654577572 SKIN BOEING737 737347 1384647NM S-23R, FS 727D CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27302WA 23182 THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEEN FS 727D & 727E. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386104-14, REV A. 2L72 4F RTA16WE 20040226000982004022600098NM 2004 2 26 DL73S040063 120040120A53306545771653 LAP JOINT BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN OF THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE PANEL LENGTH FROM FS 540 - FS 727. THE LAP JOINT WAS DISASSEMBLED, INSPECTED, ALL DAMAGE MACHINED AWAY, RE-INSPECTED AND RE-ASSEMBLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 087868-14. 2L72 4F A16WE 20040226000992004022600099NM 2004 2 26 DLM88040064 120040120A3350RPS1 BALLAST DOUG MD88 MD88 3023688NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27916DL 49591 EMERGENCY PATH LIGHTS ROW 1-12 INOP. REPLACED BALLAST B5-211, OPS CHECK OK. 2L72 4F RTA6WE 20040226001002004022600100NM 2004 2 26 DL73S040065 120040121A5330654580022 SKIN BOEING737 737247 138448DNM FUSLEAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN PANEL AT THE STRINGER 10L SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 345 TO FS 360. THE LOWER SKIN WAS CUT BELOW THE SCRIBE AND THE DAMAGED SECTION REMOVED. THE CUT AND LAP JOINT WERE REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386029-14, REV A. 2L72 4F A16WE 20040226001012004022600101NM 2004 2 26 DLM88040066 120040121A3610777795 DUCT DOUG MD88 MD88 3023688NM NR 2 ENGINE RUPTURED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27917DL 49573 248089 TEN MINUTES AFTER TAKEOFF GOT RIGHT ENGINE FIRE WARNING WITH BELLS, AURAL WARNING, AND LIGHT IN HANDLE. PER PROCEDURE REDUCED THROTTLE TO IDLE ALL INDICATION CEASED AT 1.30 EPR. OTHER INSTRUMENTS NORMAL, NO VIBRATIONS. REPLACED 13TH STAGE ANTI-ICE DUCT ON RIGHT ENGINE. 2L72 4F RTA6WE 20040226001022004022600102NM 2004 2 26 DL73S040067 120040122A5330655298873 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 SCRIBE MARKS FOUND IN THE LOWER SKIN OF THE LAP SPLICE AT S10L BETWEEN BS 908 AND 1016. THE SKIN PANEL WAS BEING REPLACED. THE NEW PANEL WAS NOTED AS HAVING SEVERAL DISCREPANCIES FROM THE MANUFACTURER. DISCREPANCIES WERE NOTED ALONG THE S20L LAP AND WERE REWORKED IAW ERA 386019-14. 2L72 4F A16WE 20040224000622004022400062EA 2004 2 24 ASOA04023 120040107A52102R5206B ACTUATOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11915EV 7754 FLT 4399 - DURING A GROUND INSPECTION IN JAX, THE PASSENGER DOOR WOULD NOT CLOSE OR OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000682004022400068EA 2004 2 24 04040649 120040209A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE INDICATIONA VTZAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27649BR 7414 DURING AIRCRAFT OPERATION THE CREW REPORTED A LAVATORY SMOKE INDICATION. THE LAVATORY SMOKE DETECTOR WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000702004022400070EA 2004 2 24 04041647 120040210A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27647BR 7399 DURING INSPECTION THE RIGHT HAND OUTSIDE FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000902004022400090EA 2004 2 24 COMA0470017 120040208A2780 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01398CA 10112 FLIGHT 5362 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER, SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040224000912004022400091EA 2004 2 24 COMA0470018 120040208A3260895304 PSEU CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01653CA191 10129 FLIGHT 5084 GEAR DISAGREE WARNING, L/G FAILED TO EXTEND. REPLACED THE PSEU. 2L72 4F RTA21EA 20040224000922004022400092EA 2004 2 24 COMA0460139 120040210A26136243843 SENSOR CNDAIRCL600 CL6002B19 1900309EA RT WING OVERHEATUNRELIABLE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01988CA13031 7204 FLIGHT 5429 WING OVERHEAT WARNING IFSD. REPLACED THE RIGHT WING OVERHEAT SENSOR. 2L72 4F RTA21EA 20040224000932004022400093SO 2004 2 24 C2XA04BT020 120040210A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716954 145072 CREW REPORTED, AISLE PATH EMERGENCY EXIT LOCATOR STRIP LIGHT INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE TO FORWARD AISLE PATH EMERGENCY LIGHT STRIP. REPAIRED BROKEN WIRE AS REQUIRED IAW EMB145 MM 70-60-00. OPS CHECKED EMERGENCY LIGHTS GOOD. 2L72 4T RTT00011AT 20040224000952004022400095WP 2004 2 24 UPS04841858 120040129A5320575352211 FLOOR SUPPORT DOUG DC8 DC871F 302199DWP AFT CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, AFT PRESSURE BULKHEAD FWD SIDE FLOOR SUPPORT CHANNEL AND ANGLE IS CORRODED BEYOND LIMITS STATION 1766 LBL 5 - LBL 15. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL AND ANGLE IAW DWG 5753522, 5755032 AND SRM 51-1-20D, 51-1-21, 51-3-0. 2L74 4F RT4A25 20040224000962004022400096NM 2004 2 24 UPS04M41865 120040210A2560 SMOKE GOGGLES DOUG MD11 MD11F 3023600NM COCKPIT CRACKED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01271UP RT SUPERNUMERARY SEAT HAS CRACKED SMOKE GOGGLES. REMOVED AND REPLACED SMOKE GOGGLES FOR RIGHT HAND SUPERNUMERARY SEAT. 2L73 4F RTA22WE 20040224001052004022400105NM 2004 2 24 AWXA200400165 120040209A3242214747 BRAKE BOEING737 7373Q8 1384670NM LT MLG BINDING A AWXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP28327AW277401128 23507 DURING TAKEOFF, BOTH ENGINES AT 60 PERCENT, TOGA SWITCH WAS ACTIVATED & ENGS ACCELERATED NORMALLY, WITHIN SECONDS F/O STATED HE COULD NOT CONTROL A/C & NEEDED FULL RT RUDDER TO KEEP THE A/C STRAIGHT, NWS TILLER WAS CENTERED, REJECTED TAKEOFF AT 90 KTS. ON RETURN TO GATE BRAKES APPEARED NORMAL, NO DRAGGING OR PULLING NOTED, ALL OTHER SYSTEMS APPEARED NORMAL (RTO, HYDS, YAW DAMPER, & ELECTRICAL) & NO WARNING INDICATIONS OF ANY KIND. UPON ARRIVAL AT GATE MX FOUND NR 1 BRAKE EXTREMELY HOT COMPARED TO OTHER BRAKES. R & R NR 1 BRAKE ASSEMBLY, OPS & LEAK CHECKS GOOD. AS PRECAUTION PERFORMED RUDDER POWER CONTROL UNIT TEST & TAXI CHECK, BRAKING & STEERING SYS NORMAL. COULD NOT DUPLICATE PROBLEM ON BRAKE ASSY . 2L72 4F RTA16WE 20040224001112004022400111WP 2004 2 24 AALA20040215 120040210A3397 TERMINAL DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW219625W 53595 STL EMERGENCY EXIT LIGHTS AT BOTH FORWARD OVERWING EXIT DOORS INOPERATIVE. FOUND LOOSE TERMINAL ON POWER SUPPLY. SECURED LOOSE TERMINAL ON POWER SUPPLY FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040224001122004022400112WP 2004 2 24 AALA20040217 120040202A2497 WIRE DOUG DC9 DC983 3022083WP OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21562AA 49344 TUL FEEDER CABLE WIRE NUMBERS 3X1C2A, 3X2C2B, 3X1D2A, 3X2D2B TO R2-41 LEFT AUXILLARY POWER RELAY AT LOWER FORWARD EPC PANEL SHOWS SIGNS OF OVERHEATING. ADEL CLAMP FOR CABLE 3X1C2A SHOWS SIGNS OF BEING OVERHEATED. REPLACED WIRE FEEDER CABLES 3X1C2A, 3X2C2B, 3X1D2A, 3X2D2B TO R2-41 LEFT AUXILLARY POWER RELAY AT LOWER FORWARD EPC PANEL AND REPLACED ONE ADEL CLAMP FOR CABLE 3X1C2A PER MM 24-20-06-2. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040224001152004022400115NM 2004 2 24 QXEA200400127 120040202A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09405QX 4047 PDX - ON FLT NR 2309, FLAP POWER CAUTION LIGHT ILLUMINATED WHEN FLAPS SELECT FROM 15 DEGREES TO 35 DEGREES. ON 1 MILE FINAL, DID NOT HAVE TIME TO CYCLE FLAP CONTROL CIRCUIT BREAKER IAW CHECKLIST. LANDED WITHOUT INCIDENT. CYCLED SHIP POWER. OPERATED FLAPS THROUGH SEVERAL CYCLES. CAUTION LIGHTS REMAIN EXTINGUSHED. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040224001202004022400120NM 2004 2 24 0400226315 120040207A3397 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHT LOOSE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01675NW 33001 DURING LINE CHECK, FOUND B-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. SECURED LOOSE CONNECTION ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040224001242004022400124WP 2004 2 24 ABXA040061 120040212A3260 CONNECTOR DOUG DC9 DC932 3022066WP MLG DOWNLOCK DAMAGED A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23900AX 47380 ABORTED APPROACH AND CYCLED THE GEAR ON A GO-AROUND. WHEN GEAR WAS EXTENDED, RIGHT MAIN GEAR UNSAFE LIGHT DID NOT COME ON. RIGHT LANDING GEAR GREEN LIGHT DID NOT COME ON. PROX INDICATION WAS NORMAL. PROBLEM VERIFIED. FOUND NR 5 PIN ON RIGHT MAIN LANDING GEAR DOWNLOCK CONNECTOR PUSHED BACK INTO RECEPTICAL. PROPERLY LOCKED NR 5 PIN INTO POSITION. ALL RIGHT MAIN LANDING GEAR INDICATION LIGHTS OPERATED NORMALLY. PERFORMED ADJUSTMENT CHECK OF LANDING GEAR POSITION AND WARNING IAW DC-9 MM 32-60-00-2. OPS CHECKED GOOD. 2L72 4F A6WE 20040224001252004022400125EA 2004 2 24 COMA0460142 120040211A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01484CA 7702 FLIGHT 5733 ONE EMERGENCY LIGHT BY MAIN DOOR IS INOP. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040224001312004022400131NE 2004 2 24 AALA20040220 220040210A7200 ENGINE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 CONTAMINATED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2190070 513 690251 MIA INFLIGHT T/1901/10 ON CLIMBOUT NR 2 OIL QUANTITY BEGINS TO DECREASE. AT 20000 FEET OIL QUANTITY WAS AT ZERO AND OIL TEMPERATURE WENT UP TO 154. OIL PRESSURE FLUCTUATED BETWEEN 30 PSI AND 50 PSI. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. AFTER LANDING ALL INDICATIONS RETURNED TO NORMAL. FOUND OIL SYSTEM CONTAMINATION. REPLACED NR 2 ENGINE IN ACCORDANCE WITH MCM 71-93-07. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20040224001582004022400158NM 2004 2 24 UPS04441870 120040128A5320BAC15048183 STIFFENER BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2200 STR 44 FRAME AFT ATT STIFFENER FOUND CORROSION. AFT OF BULK CARGO COMPT RT STA 2200 STR 44 FRAME AFT ATT STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. DUE TO CORROSION BLEND OUT DEPTH 0.020 , WIDTH 1 & LENGTH 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F A20WE 20040224001672004022400167WP 2004 2 24 UPS04841878 120040130A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 828.75, XFS 816.25, XFS 810, XFS 803.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001682004022400168WP 2004 2 24 UPS04841879 120040130A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LT WING L/E LOWER RIB IS CRACKED AT XFS 822.5. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001712004022400171WP 2004 2 24 UPS04841882 120040130A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 791.250. STOPODRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001772004022400177WP 2004 2 24 UPS04841888 120040201A5712 RIB DOUG DC8 DC871 302199AWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E LOWER RIBS ARE CRACKED AT XFS 847.5, XFS 791.25. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F 4A25 20040224001832004022400183WP 2004 2 24 04FDEA00411 120040215A7160AHL7050662 PIPE DOUG DC10 DC1010 3022110WP NR 2 ENG DRAIN DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7160-73881. POWERPLANT - ENGINE DRAINS MINOR DEVIATION TO FEDEX EO 8-7160-7-5000. POWERPLANT - ENGINE DRAINS - MINOR DEVIATION TO FEDEX EO 8-7160-7-5000 COMPLIED WITH AT BFM/MAE. 2L73 4F A22WE 20040224001932004022400193NM 2004 2 24 CALA0400120 120040215A5320149A761415 STRUCTURE BOEING737 737724 13844BYNM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A .75 INCH CRACK IN LT MLG WHEEL WELL CHORD. THE CHORD WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040224001982004022400198NM 2004 2 24 UPS04441897 120040127A5313BAC14935157075 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2180 - 2200 STRINGER L51 FOUND CRACKED. DEFECTIVE AREA STRINGER REPAIRED AS PER SRM 53-10-03 FIG 14. 2L74 4F A20WE 20040225000132004022500013NM 2004 2 25 COOSDR030077 120040101A57536521630174 SKIN BOEING727 727224 1384076NM RT WING TE FLAP DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 RT WING, INBOARD FORE FLAP PN 65-21630-174 SN BN395, LOWER SKIN DELAMINATED. 2L73 4F A3WE 20040225000142004022500014NM 2004 2 25 COOSDR030078 120040101A5753652163262 SKIN BOEING727 727224 1384076NM RT WING TE FLAP CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 RT WING, IB MID FLAP TRAILING EDGE PN 65-21632-62, SN BN281, UPPER AND LOWER SKIN CORRODED. 2L73 4F A3WE 20040225000182004022500018NM 2004 2 25 COOSDR030082 120040101A52306559947501 SEAL DEPRESSOR BOEING727 727224 1384076NM NR 2 CARGO DOOR CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 NR 2 CARGO DOOR, FORWARD LOWER CORNER SEAL DEPRESSOR CRACKED. 2L73 4F A3WE 20040225000192004022500019NM 2004 2 25 COOSDR030084 120040101A5755 SKIN BOEING727 727224 1384076NM RT WING SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 315 22448 RT FLIGHT SPOILER NR 4 DELAMINATED AND FITTING DAMAGED. 2L73 4F A3WE 20040225000432004022500043NM 2004 2 25 MEX2004008 120040105A3150 WARNING LIGHT BOEING757 757200 1384950NM COCKPIT ILLUMINATED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23703AM 27203 AIRCRAFT RETURNED TO PLATFORM DURING TAXING (ELEV FEEL AND RUDDER RATIO) EICAS MESSAGES APPEARS. THERE WAS BITE TEST PERFORMED IAW 27-31-00 AND BOTH CHANNELS WORKED CORRECT. 2L72 4F RTA2NM 20040225000442004022500044 2004 2 25 MEX2004010 420040107A3417HG280D80 COMPUTER DOUG MD88 MD88 3023688NM POS 1,POS 2 FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23168PL3221 53174 AIRCRAFT RETURNED TO PLATFORM DURING TAKE OFF LT SPEED INDICATOR HAD 80 KNTS AND RT SPEED INDICATOR HAD 65 KNTS. DURING REVISION WERE DETECTED CADC NR 2 WITH FAILURE IN CDUS, RT SPEED INDICATOR FLAG AND FAST/SLOW FUNCTION IN RT PFD WITH FAILURE. CADC NR 2 WAS TESTED IAW MM 34-11, CONNECTION LINES AND PITOT TUBE AND STATIC PORT WERE CLEANED, ALL TEST CORRECT. BOTH CADC WERE REPLACED, ALL CORRECT. 2L72 4F RTA6WE 20040225000652004022500065EA 2004 2 25 GZQ2004F00001 220040101A8500 CASE HALF PIPER PA28 PA28180 7102808SO LYC O360 O360A4A 41514EA SNSNCH76E 76EM8S5 EA ENGINE CRACKED E GZQAO OTHER O OTHER NRNOT REPORTED 1 SW13828MC4688 1805 284615 L1201136A 31882K A CRACK WAS FOUND ON THE LT CASE HALF FORWARD OF TOP THROUGH BOLT. 1L71 3O3 O 2A13 E286 5 NP4EA 20040225000672004022500067EA 2004 2 25 GZQ2004F00002 220040101A8500 CASE HALF PIPER PA28 PA28R200 7102811SO LYC O360 IO360C1C 41514EA MCAULYC3D36CC3D36C41582 NE ENGINE CRACKED E GZQAO OTHER O OTHER NRNOT REPORTED 1 SW13415856036 3028 28R7435203 L1204851A 962384 A CRACK WAS FOUND ON THE LT CASE HALF TOP FORWARD SECTION. 1L71 3O3 O 2A13 1E10 5 NSA645NE 20040225000942004022500094EU 2004 2 25 BAQA091942 120040106A6420L642A2005102 TORSION BAR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE TAIL ROTOR DISTORTED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME825 132 TAIL ROTOR TORSION BAR DISTORTED. REPLACED WITH SERVICABLE UNITS. 01/23/2004 1G72 3U3 U H88EU E34NE 20040225001022004022500102 2004 2 25 MALA040133 420040119A2565D31050105 SLIDE BAC 146 AVRO146RJ85A1500097EU CABIN DISCHARGED A MALAK NONE O OTHER TXTAXI/GRND HDL 1 GL15525XJ E2350 DURING THE PREFLIGHT INSPECTION OF FLIGHT NR 3688, EVAC SLIDE PSI LOW IN NO GO RANGE NOTED BY FA. MAINTENANCE REPLACED EVAC SLIDE FOR DOOR 1R PN D31050-105 SN/OFF 0585 SN/ON 1184 IAW AMM 25-60. 2H74 4F RTA49EU 20040225001392004022500139NM 2004 2 25 UPS04441910 120040125A5330 PANEL BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D- BS 1238 - 1265 LBL 75.92 - 95.58 CLOSEOUT PANEL CRACKED. REPAIRED CLOSEOUT PANEL PER EO 747-5310-2758 APP-C. ALL RELATED STEPS RESTORED TO NORMAL CONFIGURATION. 2L74 4F A20WE 20040225001482004022500148NM 2004 2 25 2004UALA00115 120040210A5310 DOOR FRAME BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 RIGHT NR 5 MED, FWD FRAME INBOARD WEB CRACKED AT LOWER DOOR HINGE AREA. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20040225001912004022500191NM 2004 2 25 DL767040009 120040105A5744113T12551 BEAM BOEING767 767232 1385132NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27104DA 22216 CORROSION WAS FOUND IN THE HOLE BORES OF THE '9-10' BEAM WHICH PROVIDES THE OUTBOARD SUPPORT FOR THE INBOARD FLAP ON THE LT WING. THE CORRODED HOLES WERE OVERSIZED TO REMOVE CORROSION AND BUSHED TO ALLOW INSTALLATION OF PROPER SIZE BOLTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 088082-14. 2L72 4F RTA1NM 20040226000362004022600036NM 2004 2 26 ASAA0410042 120040126A3397N140L90220MA WIRE BOEING737 7372X6C 1384552NM EMERGENCY LIGHT DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC - DURING INSPECTION FOUND EMERGENCY EXIT LIGHTING CONTROL CIRCUIT BREAKER WILL NOT TEST. REPAIRED WIRING. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040226000432004022600043NM 2004 2 26 AALA20040224 120040204A5315141T5114 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW217375A 25202 AFW - FLOORBEAM AT STATION 347, ON THE BOTTOM SURFACE OF THE UPPER FLOORBEAM AT APPROXIMATELY RBL 73, HAD CORROSION IN AN AREA OF 0.8 INCHES BY 0.5 INCHES AND A DEPTH OF 0.026 AND WAS BEYOND SRM LIMITS. BLENDED OUT CORROSION IN AN AREA OF 0.80 BY 0.50 INCHES MAXIMUM DEPTH OF 0.026 INCHES. PARENT MATERIAL THICKNESS IS 0.090 INCHES. TOTAL THICKNESS LOSS IS 28.9 PERCENT. AREA ALODINED AND FINISHED WITH TWO COATS OF BMS10-11 PRIMER. BLENDED AND FILLED WITH BMS5-95. 2L72 4F RTA1NM 20040226000462004022600046NM 2004 2 26 QXEA200400144 120040210A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09365PH 526 PDX - CABIN FLOOR PROXIMITY LIGHTING HAS TWO FORWARD SECTION UNSERVICABLE. REMOVED AND REPLACED FLOOR PROXIMITY EMERGENCY ESCAPE LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040226000512004022600051NE 2004 2 26 QXEA200400134 220040212A7200 ENGINE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 500 MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09347PH11767987 480 PCEAG0098 SEA FLIGHT 2045 RETURN TO FIELD FOR TORQUE SPLIT AND/OR FUEL FLOW SPLIT EN ROUTE TO PDT. ON RETURN TO SEA ON APPROACH AT 5,000 FEET CABIN AND COCKPIT FILLED WITH SMOKE. CAPTAIN DECLARED EMERGENCY BUT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040226000572004022600057NM 2004 2 26 DL73S040020 120040108A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 THE FUSELAGE SKIN IN THE KEEL AREA BETWEEN FS 661 & 727 WAS FOUND WITH CRACKS AT SEVERAL OF THE ACCESS CUTOUTS IN THE PANEL. THE CRACKING IS TYPICAL OF BAC S/B 737-53-1104. THE SKIN PANEL WAS REMOVED AND A MODIFIED PANEL MANUFACTURED AND INSTALLED. THE REPAIR WAS ACCOMPLISHED PER THE S/B AND PER ER/A 386067-14. 2L72 4F A16WE 20040226000592004022600059NM 2004 2 26 DL73S040022 120040109A53116546541504 FRAME BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 CRACKS WERE NOTED IN THE BS 663 FRAME AT S3L, S2L, S1 AND S2R WHICH REQUIRED THE FUSELAGE SKIN TO BE TRIMMED AWAY. CRACKS INDICATIONS WERE REMOVED AND REPAIR INSTALLED PER ERA 385971-14. 2L72 4F A16WE 20040226000622004022600062NM 2004 2 26 DL73S040025 120040110A2910000AE908T0662 HOSE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENG HYD SYSLEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27301DL 23073 709213 LOSS OF A-SYSTEM HYDRAULICS IN FLIGHT. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE LEAKING. REPLACED NR 2 ENG HYDRAULIC PRESSURE HOSE. HOSE LEAK CHECKS GOOD. SERVICED A-SYSTEM HYDRAULICS TO FULL. SPUN & RAN ENGINE PRESSURE AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E2EA 20040226000682004022600068 2004 2 26 DLM88040032 420040114A3440 IRU DOUG MD88 MD88 3023688NM E/E BAY OUT OF ADJUST A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO27907DL 49538 FLIGHT DIVERSION, MAP FAIL CAPT AND F/O`S FLIGHT DIRECTOR FAIL COURSE INFO NOT RELIABLE. FMA PANELS INTERMITTENT, STALL INDICATION FAIL AUTO SLAT FAIL. REALIGNED IRUS. PERFORMED RTS, CHECKS GOOD. 2L72 4F RTA6WE 20040226000802004022600080NM 2004 2 26 DLM88040044 120040115A2121 FAN DOUG MD88 MD88 3023688NM COCKPIT MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27911DL 49542 AFTER TURNING OFF RUNWAY A HOT ODOR AND HAZE OF SMOKE WAS NOTICED WITH A GRINDING NOISE FROM FEET AREA ON F/O SIDE ODOR AND HAZE DISSIPATED DURING TAXI IN. FOUND INSTRUMENT COOLING FAN SOURCE OF NOISE AND ODOR DEACTIVATED COOLING FAN PER MEL. NO DAMAGE NOTICED IN AREA. 2L72 4F RTA6WE 20040226000882004022600088NM 2004 2 26 DL75K040053 120040116A5330143N33206 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO276704Z 30396 THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS. ONE DENT WAS LOCATED JUST ABOVE THE S-17L CREASE AT STRINGER 16L & FS 600. THE OTHER DENT WAS BELOW THE S-17L CREASE AT FS 620. THE DENTS WERE REMOVED WITH 4 INCH CUTOUTS AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS. THE REPAIRS WERE ACCOMPLISHED PER ER/A 088228-14, REV B AND ER/A 088229-14, REV B. 2L72 4F RTA2NM 20040226001032004022600103NM 2004 2 26 DL73S040068 120040122A5330655298873 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 SCRIBE MARKS FOUND ON THE LOWER SKIN OF THE LAP SPLICE AT S10L, BETWEEN BS 908 TO 1016. A NEW SKIN PANEL IS TO BE INSTALLED. HOWEVER, THE NEW PANEL WAS NOTED TO HAVE DISCREPANCIES. THE SUBJECT SKIN PANEL WAS REWORKED AT BS 908, S-14L PER ERA 386020-14, IN ORDER TO INSTALL THE SUBJECT PANEL. 2L72 4F A16WE 20040226001042004022600104NM 2004 2 26 DL73S040069 120040122A533065458001181 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 SCRIBE MARKS WERE FOUND AT THE LAP JOINT LOCATED AT S10R, BETWEEN BS 259 TO BS 290. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386028-14. 2L72 4F A16WE 20040226001052004022600105NM 2004 2 26 DL73S040070 120040122A53126546568524 BULKHEAD BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 CORROSION WAS NOTED ON THE BS 1016 PRESSURE BULKHEAD, AT BL 0 AND AFFECTED BOTH THE WEB AND CHANNEL STIFFENERS. CORROSION WAS REMOVED AND DAMAGE REPAIRED PER ERA 385929-14. 2L72 4F A16WE 20040226001072004022600107NM 2004 2 26 DL73S040072 120040121A5330654577518 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN OF THE STRINGER 14R SKIN LAP JOINT WAS FOUND WITH A SCRIBE ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE WERE CUT OUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087866-14. 2L72 4F A16WE 20040226001102004022600110NM 2004 2 26 DL73S040075 120040122A53306545767575 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN OF THE STRINGER 14L LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360-540. THE LAP JOINT AND SCRIBE WERE COMPLETELY CUT OUT TO REMOVE ALL DAMAGE. THE AREA WAS RESTORED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087863-14. 2L72 4F A16WE 20040226001122004022600112NM 2004 2 26 DL757040077 120040121A5330143N34204 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27688DL 27587 THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 630 BETWEEN STRINGERS 23R & 24R. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 386118-14, REV A. 2L72 4F RTA2NM 20040226001172004022600117NM 2004 2 26 DLM88040082 120040125A5610SCOTCHCAL639 TAPE DOUG MD88 MD88 3023688NM F/O 3R WINDOW LOOSE A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27906DL 49537 PRESSURE SENSITIVE TAPE COVERING CURING WINDOW SEALANT ON FIRST OFFICER'S AFT WINDOW 3R CAME OFF INFLIGHT. ALL ENGINE INDICATIONS NORMAL/NO ENGINES SHUTDOWN IN FLIGHT. A/C ATB. PERFORMED GEN VISUAL INSP OF RT ENGINE, NO DEFECTS FOUND. REMOVED REMAINING TAPE DUE SEALANT CURED. 2L72 4F RTA6WE 20040226001202004022600120NM 2004 2 26 DL73S040085 120040126A533065458001141 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 SCRIBE MARKS WERE NOTED IN THE LWR SKIN AT LAP SPLICE LOCATED AT S14L BETWEEN BS 345 TO BS 360. SCRIBE MARKS REMOVED AND AREA REPAIRED PER ERA 088065-14. 2L72 4F A16WE 20040226001232004022600123NM 2004 2 26 DL764040088 120040126A3241 WARNING LIGHT BOEING767 767432ER 1385134NM ANTI SKID SYS ILLUMINATED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27845MH 29719 RECEIVED INTERMITTENT NORMAL ANTI SKID STATUS MSG. BITE ANTI SKID/ AUTOBRAKE CONTROLLER, NO CURRENT FAULTS AND NO FAULT ON INBD FLT LEG. DIVERTED TO HNL DUE TO SHORT RUNWAY IN OGG. DUE TO HISTORY OF NORMAL ANTI SKID STATUS MSG AND CAUSING RECENT DIVERSION. PERFORM ANTISKID/AUTOBRAKE CONTROLLER BITE PER FIM 32-42-00 FIG 103 AND RECALL INFLIGHT FAULTS IF ANY FOUND T/S PER TABLE -A- IF NTF CONTINUE TO T/S PER FIG 103. C/W BITE TO BOX 3, NO FAULTS DISPLAYED. 2L72 4F RTA1NM 20040226001252004022600125NM 2004 2 26 DL733040090 120040127A2622 EXTINGUISHER BOEING737 737347 1384647NM AFT CABIN DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305WA 23346 PORTABLE FIRE EXTINGUISHER PRESSURE LOW. REPLACED SAME. 2L72 4F RTA16WE 20040226001262004022600126NM 2004 2 26 DLM90040091 120040127A2560 DIODE DOUG MD90 MD9030 3023690NM FLASHLIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27911DA 53391 AFT EMERGENCY FLASHLIGHT LED INOP. REPLACED FLASHLIGHT AND BATTERY. 2L72 4F RTA6WE 20040226001272004022600127NM 2004 2 26 DL73G040093 120040127A256061020 BATTERY BOEING737 737330 13844BJNM FLASHLIGHT DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27241DL 23833 EMERGENCY FLASHLIGHT BATTERY DEAD. REPLACED BATTERY PACK. 2L72 4F RTA16WE 20040226001282004022600128NM 2004 2 26 DL73S040095 120040128A53306545770576 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 DURING CROWN INSPECTION FOUR FASTENERS HOLES WERE NOTED WITH CRACK INDICATIONS. DISCREPANCIES WERE REPAIRED PER ERA 386057-14AD. 2L72 4F A16WE 20040226001302004022600130NM 2004 2 26 DL73S040097 120040128A5310656777514 BEAM BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 DAMAGE INCURRED TO THE VERTICAL FLANGE OF THE LOWER CHORD AT RBL 63, IN THE BS 639 STUB BEAM. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386099-14. 2L72 4F A16WE 20040226001312004022600131NM 2004 2 26 DL73S040098 120040128A53146562125502 KEELBEAM BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 CORROSION WAS NOTED AT BS 606 ON THE LWR SURFACE OF THE RIGHT KEELBEAM INBOARD FLANGE. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386066-14. 2L72 4F A16WE 20040226001322004022600132NM 2004 2 26 DL73S040099 120040128A531165528742 FRAME BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 BS 951 FRAME SUSTAINED DAMAGE IN THE RADIUS AT WL 203. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386060-14. 2L72 4F A16WE 20040226001332004022600133NM 2004 2 26 DL73S040100 120040128A533065458001172 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S10L LAP SPLICE BETWEEN BS 259 AND 291. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386027-14. 2L72 4F A16WE 20040226001342004022600134NM 2004 2 26 DL73S040101 120040128A5510 FITTING BOEING737 737247 138448DNM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 DURING INSPECTION AND REWORK OF THE HORIZONTAL STABILIZER LUGS, SEVERAL LUGS WERE REWORKED BEYOND PUBLISHED LIMITS. CORROSION REMOVED AND LUGS REWORKED IAW ERA 386090-14AD. 2L72 4F A16WE 20040226001352004022600135NM 2004 2 26 DL73S040102 120040128A53156546800508 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 DURING INSPECTION THE BS 520 FLOORBEAM WAS NOTED WITH CRACKS IN THE RADIUS, ALONG THE UPPER CHORD TO WEB RADIUS AT LBL 24.75, LBL 45.5 AND RBL 24.75. UPPER CAP WAS REMOVED AND A NEW SECTION SPLICED IN PER ERA 386080-14. 2L72 4F RTA16WE 20040226001362004022600136NM 2004 2 26 DL73S040103 120040128A555065505087 FITTING BOEING737 737247 138448DNM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 DURING ACCOMPLISHMENT OF 03-085220-03 CORROSION WAS NOTED ON THE TWO VERT STAB FIN LUGS. ADDITIONALLY, TWO FUSELAGE CLEVIS LUGS WERE NOTED AS HAVING LUG THICKNESSES BELOW THAT ALLOWED BY 03-085220-03. CORROSION REMOVED AND LUGS/CLEVISES REWORKED PER ERA 386006-14. 2L72 4F A16WE 20040226001372004022600137NM 2004 2 26 DL73S040104 120040128A5550 ATTACH FITTING BOEING737 737232 1384475NM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 NUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMOVED AND LUGS REWORKED IAW ERA 386108-14AD. 2L72 4F RTA16WE 20040226001382004022600138NM 2004 2 26 DL73S040105 120040127A5330654577463 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 THE FUSELAGE SKIN WAS FOUND WITH A 2.75 INCH CRACK RUNNING ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 19L BETWEEN FS 776 & 787. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC S/B 737-53-1065 AND ER/A 088294-14. 2L72 4F RTA16WE 20040226001412004022600141NM 2004 2 26 DLM90040108 120040129A3230 O-RING DOUG MD90 MD9030 3023690NM SCHRADER VALVE DAMAGED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27905DA 53385 AFTER TAKEOFF NOSE GEAR FAILED TO RETRACT. DURING POM PROCEDURE GEAR HANDLE WOULD NOT RAISE. CONTINOUS T/O AURAL WARNINGS OF FLAPS, STABILIZER, SLATS IN AIR. NO PRESSURIZATION AUTO FAIL INOP 1 AND 2. AUTO SPOILERS INOP OAP MESSAGE. ALSO HAD LEFT AND RIGHT STRAKE FAULT MESSAGE ON STATUS MSG. TAIL TEMP FAULT AND STRAKE ICE MSG ON OAP. FOUND O-RING ON NOSE GEAR STRUT SERVICING SCHRADER VALVE IN POOR CONDITION. REPLACED SAME. SERVICED NOSE STRUT PISTON PER MM. INSP NLG STRUT PISTON IN FULL EXT. CHECKED GOOD CYCLED ALL 3 GEARS SEVERAL TIMES, OPS AND INDICATION NORMAL. 2L72 4F RTA6WE 20040226001452004022600145NM 2004 2 26 DLM88040112 120040129A3350 LENS DOUG MD88 MD88 3023688NM AFT LIFE RAFT DISLODGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27956DL 49887 DURING LETTER CHECK M-2, FOUND EMERGENCY LIGHT AT AFT RAFT AREA INOP, REF NRC 76. FOUND EMERGENCY LIGHT AND STANDBY LIGHT ON AFT RAFT INSTALLED IN OPPOSITE POSITION. INSTALLED PER MM. OPS CHECK GOOD PER MM. 2L72 4F RTA6WE 20040226001462004022600146NM 2004 2 26 DLM88040113 120040130A28223980001 PUMP DOUG MD88 MD88 3023688NM FUEL BOOST MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27901DL 49532 CENTER FUEL WAS UNUSEABLE BOOST PUMPS POPPING C/B`S. RESET C/B`S, TRANSFERRED FUEL OUT OF CENTER TANK. UNABLE TO DUPLICATE. 2L72 4F RTA6WE 20040226001472004022600147NM 2004 2 26 DL76S040114 120040129A5410313T1100107 CAP BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 2 ENG PYLON MISSING A DALAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO27128DL 24078 580364 DURING FLIGHT, NR ENGINE PYLON DEPARTED AIRCRAFT. UNDER INVESTIGATION. 2L72 4F4 FRTA1NM E13NE 20040226001502004022600150NM 2004 2 26 DLM88040119 120040131A2740279001351 TRIM MOTOR DOUG MD88 MD88 3023688NM STAB TRIM FAILED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO27960DL 49979 ALTERNATE TRIM INOP WITH AUTOPILOT ON OR WITH CHICLET SWITCHES. BOTH DFGC ATTEMPTED. REPLACED ALTERNATE STAB TRIM MOTOR. 2L72 4F RTA6WE 20040226001532004022600153NM 2004 2 26 DLM88040122 120040130A54105930645509 NOSE COWL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27972DL 001884 53215 726047 NUMBER 2 ENGINE COWLING LOOSE. PORTION MISSING. FOUND ON POST FLIGHT WALKAROUND. REMOVED AND REPLACED RIGHT NOSE COWL ASSY PER MM. ASSOC PARTS REPLACED AS FOLLOWS, THERMOSTATIC REGUALTOR VLV 759702239 S/N 5969C. NOSE COWL A/I SHUTOFF VLV 754001305 S/N 23227. DUCT 759102267 S/N N/A. 2L72 4F4 FRTA6WE E9NE 20040226001542004022600154NM 2004 2 26 DL767040123 120040131A2121211002939 FAN BOEING767 767232 1385132NM RIGHT FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27108DL 22220 IN FLIGHT THE CREW REPORTED, GOT A RT RECIRC FAN INOP LIGHT ACCOMPANIED BY A STRONG PUNGENT ODOR. THE ODOR WENT AWAY WHEN BOTH RECIRC FANS WERE TURNED OFF. ALSO PULLED THE CIRCUIT BREAKER FOR THE RT RECIRC FAN. THE LT RECIRC FAN OPERATED NORMALLY ON THE GROUND AND THE RT RECIRC FAN WAS PUT ON MCO PER MEL 21-25-01A. RT RECIRC FAN WAS REPLACED IN BDL ON 020104 REF LOG E638468 ITEM 003. 2L72 4F RTA1NM 20040226001552004022600155NM 2004 2 26 DL73S040124 120040201A213039606411 CONTROL VALVE BOEING737 737247 138448DNM LEFT PACK INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27378DL 23605 ACFT WOULD NOT PRESSURIZE, AT FL190 CABIN ALT WARNING HORN SOUNDED. FOUND LEFT A/C PACK CONTROL VALVE FLUCTUATING. REPLACED SAME. ACFT PRESSURIZES NORMALLY. 2L72 4F A16WE 20040226001562004022600156NM 2004 2 26 DL76L040125 120040201A3810288237 COMPRESSOR BOEING767 767332 1382001NM POTABLE WATER OVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27185DN 27961 ELECTRICAL FUMES STRONG IN AFT GALLEY AREA DURING PREFLIGHT. FOUND POTABLE WATER COMPRESSOR SMOKING. REPLACED COMPRESSOR MM, OPS CHECK AND LEAK CHECK GOOD. VERIFIED PRESSURE SWITCH OPS NORMAL. 2L72 4F RTA1NM 20040226001572004022600157NM 2004 2 26 DL738040126 120040201A2120 ODOR BOEING737 737832 13844CFNM COCKPIT DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO273747D 29665 ON TAKEOFF FUMES DETECTED IN CABIN AND COCKPIT. RECIRC FANS TURNED OFF AND ODOR DISSIPATED. RAN PACKS WITH ENGINES AND INSPECTED AIRCRAFT. UNABLE TO DUPLICATE. 2L72 4F RTA16WE 20040226001582004022600158NM 2004 2 26 DL73S040127 120040120A5330655298863 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309DL 23081 THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT WAS FOUND WITH 2 SMALL CRACKS IN THE BONDED SKIN AND UNDERLYING BEAR STRAP. THE CRACKS WERE REMOVED WITH 1 INCH CUTOUTS. THE CUTOUTS WERE REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3 AND ER/A 088350-14, REV A. 2L72 4F RTA16WE 20040226001592004022600159NM 2004 2 26 DL767040128 120040130A5753 FITTING BOEING767 767232 1385132NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27108DL 22220 WHILE ACCOMPLISHING BOLT REPLACEMENTS FOR THE INBOARD FLAP SUPPORT FITTINGS ON THE LT & RT WINGS PER AD 2002-22-07, SEVERAL FITTING HOLE BORES WERE FOUND WITH CORROSION. THE HOLE BORES WERE OVERSIZED TO REMOVE ALL CORROSION, HFEC INSPECTED, AND BUSHED. NEW BOLT HOLES WERE THEN REAMED AND THE NEW BOLTS INSTALLED. THE REPAIRS WERE PER ER/A'S 088285, 088313, 088286, 088287 & 088289-14. 2L72 4F RTA1NM 20040226001602004022600160NM 2004 2 26 DL764040129 120040202A30409004089 MOTOR BOEING767 767432ER 1385134NM WINDSHIELD WIPERLIGHTNING STRIKEA DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27828MH 29699 LIGHTNING STRIKE ON DEPARTURE. PHOSPHORUS ODOR IN COCKPIT. STRUCK NOSE OF A/C. REPLACED CAPTS WINDSHIELD WIPER MOTOR PER MM. CHECKS OK. 2L72 4F RTA1NM 20040226001612004022600161NM 2004 2 26 DL757040130 120040203A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27623DL 22913 F/A'S REPORTED BURNING ELEC ODOR AROUND TV MONITORS NEAR EXIT ROWS AT CRUISE. UTILITY BUSSES TURNED OFF, ODOR NO LONGER REPORTED. NO VISIBLE SIGNS OF SMOKE. POWERED ALL SYSTEMS, DROPPED CEILING PANELS IN AREA, NO ODORS OR ABNORMALATIES FOUND. ALL LIGHTS, COFFEEMAKERS, MONITORS OPN NORMAL. 2L72 4F RTA2NM 20040226001622004022600162NM 2004 2 26 DL73S040131 120040131A5312654656841 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CANNING A DALAK NONE O OTHER ININSP/MAINT 1 SO27309DL 23081 THE WEB OF THE FS 1016 AFT P-DOME WAS FOUND WITH AN OIL-CAN CONDITION BETWEEN S-3L & S-5L. THE DAMAGED AREA OF WEB WAS CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 088351-14AD. 2L72 4F RTA16WE 20040226001632004022600163NM 2004 2 26 DLM88040132 120040203A7603 THROTTLE CABLE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE BINDING A DALAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO27908DE 53417 725945 ABORTED TAKEOFF AT 65 KIAS ENGAGED AUTOTHROTTLES FOR FLEX 50 TAKEOFF AT 75 PERCENT N1 THROTTLES IMMEDIATELY CLAMPED AND DID NOT ADVANCE AT ALL TOWARDS TAKEOFF THRUST. ABORTED T/O FOR THIS REASON. FOUND THRUST CABLE AT ENGINE BINDING. REPLACED SAME. 2L72 4F4 FRTA6WE E9NE 20040226001642004022600164NM 2004 2 26 DLM88040133 120040204A3230 CONTROL CABLE DOUG MD88 MD88 3023688NM MLG LOOSE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27918DL 49583 ON TAKEOFF GEAR WOULD NOT RETRACT. FOUND RETRACT CABLES 118A AND 118B LOOSE. RIGGED SYSTEM, CHECKS GOOD. 2L72 4F RTA6WE 20040226001652004022600165NM 2004 2 26 DLM88040134 120040202A3250329001542 VALVE DOUG MD88 MD88 3023688NM NLG STEERING STICKING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27996DL 53363 AFTER TAKEOFF UNABLE TO RAISE GEAR HANDLE TO UP DETENT. REPLACED NOSE GEAR STEERING VALVE. 2L72 4F RTA6WE 20040226001662004022600166NM 2004 2 26 DL757040135 120040204A3244 TIRE BOEING757 757232 1384965NM MLG PUNCTURED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27655DL 24395 NR 5 TIRE ARRIVED PHL WITH A SCREW IN THE NR 5 TIRE. TIRE LEAKED AFTER SCREW REMOVAL. REPLACED NR 5 WHEEL ASSY PER M/M. 2L72 4F RTA2NM 20040226001682004022600168NE 2004 2 26 DL757040137 220040207A7230 BLADE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO27660DL48078 716487 24422 716487 FAILURE OF LEFT ENGINE ON CLIMBOUT AT FL230. EGT, N2 & FF WERE NORMAL. EPR AND N1 ROLLED BACK TO IDLE. A/C YAW INDICATED COMPLETE LOSS OF THRUST. WINDMILLED FOR 15 MIN, POSITIVE OIL PRESSURE. DURING BOROSCOPE FOUND DAMAGE TO 6TH AND 7TH STAGE COMPRESSOR BLADES. ENGINE CHANGE IN PROGESS. 2L72 4F4 FRTA2NM E17NE 20040226001692004022600169NM 2004 2 26 DL757040138 120040207A3244B757M TIRE BOEING757 757232 1384965NM MLG PUNCTURED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO27683DA 27103 FOUND BOLT IN NR 7 MLG TIRE. REMOVED AND REPLACED NR 7 MLG WHEEL ASSY PER MM. 2L72 4F RTA2NM 20040226001702004022600170NM 2004 2 26 DL757040139 120040208A3397 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27689DL 27172 FOUND DURING MAINTENANCE CHECK EMERGENCY LIGHTS IN ALL FIRST CLASS SEATS INOP. TROUBLESHOOTING FOUND SHORTED WIRING AT SEAT 4C. REPAIRED WIRING, OPERATIONAL CHECKS OK. 2L72 4F RTA2NM 20040226001742004022600174NM 2004 2 26 DL73S040143 120040209A7603 CONTROL CABLE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE STIFF A DALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO27334DL43373 709225 23105 709225 DURING CLIMB TO 370 FROM 330 NR 1 THROTTLE POPPED BACK AND FORTH. A/T DISCONNECTED AND THROTTLE STIFF. AFTER DESCENT BELOW 330 THROTTLE WORKED NORMAL AND NOT AS STIFF. REPLACED NR 1 ENGINE THROTTLE PUSH-PULL CABLE. RAN ENGINE PER PFHB. OPS GOOD. 2L72 4F4 FRTA16WE E2EA 20040226001752004022600175NM 2004 2 26 DL73S040144 120040209A5753654640917 FLAP TRACK BOEING737 737232 1384475NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 THE REAR ENGINE MOUNT ATTACH HOLES, LOCATED AT THE NR 2 AND NR 3 T/E FLAPS, OUTBOARD TRACKS WERE NOTED WITH CORROSION IN THE BORES. CORROSION WAS REMOVED AND TRACKS WERE REWORKED PER ERA 386130-14. 2L72 4F RTA16WE 20040226001762004022600176NM 2004 2 26 DL777040145 120040210A2121218040025 FAN BOEING777 777232 1385232NM FWD CARGO FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27862DA 29734 EQUIPMENT VENT FAN FAIL ELECTRICAL SMOKE ODOR IN CARGO BIN. REPLACED SAME AND TEST PER FIM, TEST OK. 2L72 4F RTT00001SE 20040226001772004022600177NM 2004 2 26 DL73S040146 120040210A276165445616 ACTUATOR BOEING737 737232 1384475NM LT WING SPOILERSLEAKING A DALAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO27306DL 23078 NR 2 FLT SPOILER LEAKING. LOSS OF A-SYSTEM HYD. REMOVED NUMBER 1 SPOILER ACTUATOR. 2L72 4F RTA16WE 20040226001782004022600178NM 2004 2 26 DLM88040147 120040210A3350RPS1B POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27913DE 49956 FOUND EMERGENCY LIGHTS FROM ROW 31 AFT INOP. REPLACED POWER SUPPLY. CHECKS GOOD. 2L72 4F RTA6WE 20040226001792004022600179NM 2004 2 26 DL75K040148 120040210A3397 WIRE HARNESS BOEING757 757232 1384965NM EMERGENCY LIGHT DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO276708D 30480 SEAT MOUNTED EMERGENCY LIGHT INOP AT 31D DURING TEST. FOUND PIN PUSHED BACK IN CONNECTOR FOR SEAT HARNESS. SECURED SAME LIGHT, CHECKS GOOD. 2L72 4F RTA2NM 20040226001812004022600181NM 2004 2 26 DLM88040150 120040211A2420249001269 METER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A DALAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27989DL 53341 725977 AC CROSSTIE LOCKOUT LIGHT ON. LT GEN LOAD FLUC FROM .4 TO.6, RT GEN VOLTS FREQ OK BUT LOAD AT ZERO. WHEN RT GEN RESET LOST ALL ELEC PWR MOMENTARILY. RT GEN BACK TO OFF AND THEN LT GEN PICKED UP LOAD OK. REPLACED LOAD METER. 2L72 4F4 FRTA6WE E9NE 20040226001832004022600183NM 2004 2 26 DL73S040152 120040212A53126546568524 BULKHEAD BOEING737 737232 1384475NM CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 CORROSION WAS NOTED AT BS 1016 PRESSURE BLKHD, AT BL 0 AND AFFECTED THE WEB/GORE AND CHANNEL STIFFENERS. REPAIRED PER ERA 386069-14AD. 2L72 4F RTA16WE 20040226001872004022600187NM 2004 2 26 DL757040156 120040213A2120 ODOR BOEING757 757232 1384965NM GALLEY DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27682DA 26958 APPROX 1 HR INTO FLIGHT, THE FLIGHT ATTENDANTS IN THE AFT GALLEY COMPLAINED OF AN ODOR, MAYBE OF A CHEMICAL NATURE COMING FROM AFT GALLEY AND ABOUT 4 ROWS OF SEATS FWD OF GALLEY. ODOR WAS OFF AND ON FOR REMAINDER OF FLIGHT. TURNED ON ALL LIGHTS, OVENS AND COFFEEMAKERS THRU-OUT A/C RAN BOTH PACKS WITH APU, NO FAULTS OR ODORS NOTED. RAN BOTH ENGS AND ISOLATED BOTH AIR SOURCES TO RUN PACKS. NO CHEMICAL OR ANY OTHER UNUSUAL ODORS NOTED. ALL CHECKS NORMAL. 2L72 4F RTA2NM 20040226001892004022600189NM 2004 2 26 DL767040158 120040215A3350 FUSE BOEING767 767232 1385132NM EMERGENCY LIGHT BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27108DL 22220 ON MAINTENANCE PREFLIGHT INSPECTION FOUND FIRST CLASS EMERGENCY LIGHTS INOP IN THE SEAT PANELS. TROUBLESHOOTING FOUND BLOWN FUSE IN POWER SUPPLY M9008. REPLACED FUSE, LIGHTS NOW OPERATIONAL CHECK OK. 2L72 4F RTA1NM 20040226001922004022600192NM 2004 2 26 DL76G040161 120040215A3897 WIRE BOEING767 7673P6 1385105NM FWD LAV OVERHEADCHAFED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO271501P 24983 WORKING MCO LAV 1 LIGHTING INOP. FOUND PLUG D808 IN LAV OVERHEAD SHORTED PIN 12 AFTER FURTHER TROUBLESHOOTING FOUND MANY WIRES IN WIRE BUNDLE BEING CHAFED BY THE L1 DOOR HANDLE EVERY TIME HANDLE IS ACTUATED. REPAIRED ALL. 2L72 4F RTA1NM 20040226001932004022600193WP 2004 2 26 ABXA040064 120040214A25105641031501ABX1 SEAT DOUG DC8 DC863F 302198FWP COCKPIT LACK OF LUBE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23819AX 380 45927 FIRST OFFICER'S SEAT INTERMITTENTLY SLIPPED OUT OF SELECTED FLOOR LATCHED POSITION. CLEANED AND LUBED FIRST OFFICER'S SEAT TRACKS. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 28-11-01-2-0001. 2L74 4F 4A25 20040226001952004022600195NM 2004 2 26 DXTA200400245 120040216A2613 WARNING LIGHT AMD FALC50FALCON2000 2730170NM COCKPIT ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07251QS 202 FIFTEEN MINUTES INTO FLIGHT AT FL290, LT WHEEL WELL OVERHEAT LIGHT ILLUMINATED WITH AUDIO FOR 1 SECOND. TWO MINUTES LATER IT OCCURRED AGAIN, 3 MINUTES LATER LIGHT CAME ON WITH AUDIO FOR APPROXIMATELY 15 SECONDS. ALL THREE TIMES LIGHT EXTINGUISHED BY ITSELF, PERFORMED EMERGENCY PROCEDURE AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2K73 4F RTA50NM 20040226001982004022600198EA 2004 2 26 COMA0470022 120040215A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01331CA2894 10061 FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20040226002012004022600201EA 2004 2 26 COMA0460151 120040214A27507805013 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01915CA11535 7013 FLIGHT 5257 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP CONTROL LEVER. 2L72 4F RTA21EA 20040226002032004022600203WP 2004 2 26 GKZR200482306 120040217A5720 CLIP DOUG DC8 DC871F 302199DWP LT WING CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 LEFT WING UPPER CLIP INSIDE NR 1M ACCESS HOLE 505C AT STA 252-351 BETWEEN REAR SPAR NR 1 STRINGER CLIP CRACKED. REMOVED LT UPPER WING CLIP INSIDE NR 1 MAIN TANK ACCESS HOLE 505C AT STA 252-351 ON STRINGER NR 1. FABRICATED AND INSTALLED REPLACEMENT PART IAW DC-8 SRM 51-1-20 MATERIAL 60-18391/7075T6511. (CLOSED) 2L74 4F RT4A25 20040227000042004022700004NM 2004 2 27 QXEA200400073 120040125A2131 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM CABIN PRESSURE MALADJUSTMENT A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09415QX 4081 AFTER TAKE-OFF, CLIMBING THROUGH 3600 FEET, THE CREW FELT A PRESSURIZATION BUMP AND LOST ALL PRESSURIZATION. FLIGHT ATTENDANT (B) HEARD A BANGING NOISE FROM AFT CARGO AREA. MAINTENANCE INSPECTED THE ACM AND RE-CIRC FAN DUCTING AND CLAMPS. NO DISCREPANCIES WERE NOTED BY SIGHT OR FEEL WITH APU BLEED AIR TURNED ON. NO FAULTS WERE NOTED IN CDS AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040227000052004022700005WP 2004 2 27 DHL2004873002 120040128A7602 BOLT DOUG DC8 DC873F 302199FWP START LEVER LOOSE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 NR 2 START LEVER WILL NOT SHUT OFF, STUCK IN ON POSITION. REINSTALLED BOLT AND NUT ASSEMBLY ON NR2 ENGINE POWER CONTROL MECHANISM IAW M/M 76-11-1. RAN NR 2 ENGINE IAW JET RUN UP 13.1. CHECKED OPERATION OK. NR 2 FIRE HANDLE WILL NOT SHUT DOWN NR 2 ENGINE. AFTER C/A IN ITEM 1P PERFORMED TEST OPERATION IAW M/M 76-11-1 ON NR 2 FIRE HANDLE, ENGINE SHUT DOWN OK. 2L74 4F RT4A25 20040225000852004022500085SO 2004 2 25 GLBA20030538 120040121A323312025276501 ACTUATOR EMB 120 EMB120ER 3260203SO MLG INOPERATIVE A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0396ZK 2476 120096 LT MAIN WILL NOT RETRACT, REMOVED AND REPLACED ACTUATOR. 2L72 4T RTA31SO 20040225000952004022500095EA 2004 2 25 HNAA0400005 120040124A3320BV0330012150 SOCKET DHAV DHC8 DHC8311 1386006EA CABIN LIGHTS BURNED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07330EN2373623736 274 ELECTRICAL OVERHEAT ODOR AT CABIN ROWS 11, 12, 13. FOUND LAMP HOLDER 1AC BURNED. REMOVED BULB IAW EO AND MEL LIGHT. 2H72 4T RTA13NM 20040225001042004022500104EU 2004 2 25 MALA040128 120040110A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING 4K INSPECTION IN LCQ, NUMEROUS DENTS ON LT FWD NR 3 ICE SHIELD. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PLATE IAW MESABA EO NR S53005 DATED 24 FEB 1999. 2L72 4T RTA52EU 20040225001222004022500122CE 2004 2 25 DRU2004F00000 120040113A2612 FIRE DETECTOR LEAR 25 25B 5170511CE GE CJ610 CJ6108 30006NE RT ENGINE FALSE INDICATIONE DRUAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL257810W 117 249044A FALSE FIRE WARNING DURING FLIGHT. AFTER THE AIRCRAFT LANDED, THE PILOT REPORTED THAT THE INDICATION WAS INTERMITTENT. THE RT ENGINE COWLING WAS REMOVED, AND THE ENGINE WAS INSPECTED. THERE WAS NO INDICATION OF FIRE IN THE ENGINE AREA. THE FIRE LOOP LOOKED OK, NO DAMAGE NOTED. NOT HOT SPOTS ON THE ENGINE WERE NOTED, FROM BLEED AIR LINES OR OTHERWISE. THE WIRING CONNECTIONS AT THE NACELLE FIREWALL WERE DISCONNECTED, AND THERE APPEARED MORE THAN NORMAL BUILD UP OF GRIME AND CARBON. CLEANED THE TERMINALS AND CONTACTS. RECONNECTED THE WIRES. RAN THE AIRCRAFT WITHOUT AND WITH THE COWLINGS ON, COULD NOT DUPLICATE THE FALSE FIRE INDICATION. 2L72 4J4 J A10CE 1E16 20040311000642004031100064NM 2004 3 11 QXEA200400071 120040123A2131 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM CABIN PRESSURE OUT OF ADJUST A QXEAK NONE J WARNING INDICATION DEDESCENT 1 NM09400QX 4030 SEA - FLIGHT 2272 - DESCENDING THROUGH 9000 FEET, CABIN LOST PRESSURE AND RATE PEGGED AT MAX. NO NOISES OR LEAKS NOTED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LDC ALT ON THE CABIN PRESS CONTROLLER SET 48 FEET. CONTROLLER WAS SET TO 400 FEET. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PART REPLACED. 2H72 4T RTA13NM 20040225001312004022500131NM 2004 2 25 AALA20040225 120040204A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21387AM 27184 AFW - EMERGENCY EXIT LIGHT ON RIGHT SIDE OF BUSINESS CLASS SEATS AND OVERHEAD INOPERATIVE. REPLACED BATTERY AND BATTERY CHARGER FOR EMERGENCY EXIT LIGHTS ON RIGHT SIDE OF BUSINESS CLASS SEATS AND OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040225001382004022500138NM 2004 2 25 UPS04441909 120040121A5313BAC14981477075 STRINGER BOEING747 747123 1384873NM FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT- LT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER TRIMMED OUT AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040225001442004022500144NM 2004 2 25 UPS04541895 120040206A5310 WEB BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01405UP 23727 INSPECTION TYPE: C, CORROSION ON FLOOR SHEAR WEB IN SEVERAL AREAS BETWEEN BS 334 TO BS 365 LBL 46 TO LBL 62 WL 208 (CP53-221-02.05-1I). BS 351 LBL 46, BS 339 LBL 46 OUT OF LIMITS PER SRM 53-00-51 FIG 101. FABRICATED DOUBLERS, FILLERS AND INSTALLED REPAIR PARTS. ALL WORK DONE IAW SRM 51-70-13, 51-40-08, 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA2NM 20040225001472004022500147NM 2004 2 25 04FDEA00413 120040216A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 FUSELAGE EXTERNAL SKIN IS GOUGED AT BS 1143 JUST 3 INCHES ABOVE STRINGER 12 LT. 2L73 4F RTA3WE 20040225001522004022500152NM 2004 2 25 2004UALA00119 120040210A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29319UA 23951 FWD GALLEY DOOR CUTOUT HAS CRACKED AT AFT LWR CORNER APPROX 1 INCH LONG. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040225001932004022500193NM 2004 2 25 DL764040011 120040106A253072077500 OVEN BOEING767 767432ER 1385134NM FWD GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27826MH 29697 NR 1 OVEN SHORTED OUT WHEN TURNED ON. WOULD NOT SHUTOFF WITH CONTROL PANEL. SPARKS AND ELECTRICAL FIRE ODOR CONTINUED C/B DID NOT POP. F/A PULLED C/B AND SPARKS AND SMELL DISSIPATED. REPLACED OVEN ASSY, OPS CHECKS OK. 2L72 4F RTA1NM 20040225001992004022500199NM 2004 2 25 DL73S040018 120040109A335020131A BATTERY PACK BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27303DL 23075 ON PREFLIGHT FOUND FWD ESCAPE PATH LIGHTING INOP. REPLACED BATTERY PACK AND RACK. 2L72 4F RTA16WE 20040226000342004022600034NM 2004 2 26 ASAA0410038 120040123A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 SEA - DURING INSPECTION, FOUND THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040226000522004022600052EA 2004 2 26 QXEA200400149 120040212A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 PDX - FORWARD CARGO COMPARTMENT CENTER CHIMNEY AND FORWARD CENTER CHIMNEY METAL MESH IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20040226000532004022600053NM 2004 2 26 QXEA200400136 120040213A2750C14867420003 FCU BOMBDRDHC8 DHC8401 1390041NM TE FLAPS MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX191 4061 YYC FLIGHT 2329 AFTER DEPARTURE AIRCRAFT HAD FLAP POWER CAUTION MESSAGE. RAN CHECKLIST, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FCU. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040226000692004022600069NM 2004 2 26 DL73S040033 120040113A5521 SPAR BOEING737 737247 138448DNM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27382DL 3698 23609 RIGHT ELEVATOR REAR SPAR FOUND DAMAGED AT OUTBOARD END. REPAIR ACCOMPLISHED FROM ELEV STA 88 TO OUTBOARD END PER ER/A 426886-14. 2L72 4F A16WE 20040226000722004022600072NM 2004 2 26 DL75K040036 120040114A5754 WEDGE BOEING757 757232 1384965NM NR 2 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO276704Z 30396 FOUND ON PSV - 3 DENT ON NUMBER 2 SLAT WEDGE 48 INCHES FROM INBOARD EDGE. REPAIRED PER SRM 57-43-02D AND OPERATION 1000. 2L72 4F RTA2NM 20040226000752004022600075NM 2004 2 26 DL73S040039 120040115A5311652072270 FRAME BOEING737 737247 138448DNM BS440, S26R DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 A DAMAGED HOLE WAS CREATED IN THE BS 440 FRAME NEAR S26R. HOLE WAS OVERSIZED TO 0.3670 TO REMOVE DAMAGE. FRAME WAS REPAIRED PER ERA 386004-14. 2L72 4F A16WE 20040226000972004022600097NM 2004 2 26 DL73S040062 120040120A53306545771654 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A LIGHT SCRIBE MARK ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE LAP JOINT WAS UNFASTENED, SEPARATED, ALL DAMAGE REMOVED THROUGH MACHINING, AND THOROUGHLY INSPECTED TO ENSURE NO CRACKS OR FURTHER DAMAGE. THE JOINT WAS THEN REASSEMBLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 087869-14. 2L72 4F A16WE 20040226001222004022600122NE 2004 2 26 DL73S040087 220040124A7250JT8D15AHK BLADE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE BROKEN A DALAO OTHER E VIBRATION/BUFFET DEDESCENT 1 SO27327DL47406 23099 709129 AT TOP OF DESCENT UPON THROTTLE RETARD NR 2 ENGINE VIBRATION. ALL ENGINE PARAMETERS NORMAL. AT 75 PERCENT VIBRATION DISCONTINUED. LEFT ENGINE AT 75 PERCENT. FOUND TURBINE BLADE DAMAGE. REPLACED ENGINE. 2L72 4F4 FRTA16WE E2EA 20040226001292004022600129NM 2004 2 26 DL73S040096 120040128A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 A GOUGE WAS NOTED ON THE UPPER SKIN LAP SPLICE AT S26R AT BS 440. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386070-14. 2L72 4F A16WE 20040226001392004022600139NM 2004 2 26 DLM88040106 120040128A2497 WIRE DOUG MD88 MD88 3023688NM RELAY BROKEN A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27997DL 53364 WHILE T/S FOR RT GEN INOP, APU GOT TRIPPED OFF WITH CROSS-TIE LOCKOUT, FOUND BROKEN TERMINAL ON RELAY R2-40. TERMINAL HAD ARCED AND WORN ON A WIRE BUNDLE CAUSING DAMAGED WIRING. ARCING WAS FOUND WHILE AC ON GROUND DURING MTC. REPLACED RELAY AND REPAIRED DAMAGED WIRING. 2L72 4F RTA6WE 20040226001442004022600144NE 2004 2 26 DL757040111 220040129A7320 EEC BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 SO27620DL46026 22910 716526 UPON LANDING WITH T/R DEPLOYED, COCKPIT LEFT OIL PRESS LIGHT ILLUMINATED AND SMOKE WAS SEEN TRAILING LEFT SIDE BY TOWER. ENGINE WAS SHUT DOWN DURING ROLLOUT. REMOVED AND CLEANED EEC CANNON PLUGS. INSP WIRING RUN THRU PEDESTAL FROM LT FUEL CONTROL SWITCH. WHILE MOVING T/R LEVER, NO CHAFING OR BINDING FOUND. CHECK CUTOFF CIRCUIT FOR 28VDC AT PIN 1 D41948P, 0 VOLTS FOUND NORMAL. REMOVED AND REPLACED ENG FIR CONTROL PANEL, RAN ENG, CHECK GOOD. REMOVED AND REPLACED FUEL CONTROL PER MM, OPS CHECK NORMAL. MEGGED CUTOFF WIRING CHECK NORMAL. VERIFIED 28VDC FOR 5 SEC TO FCU, RAN ENG AND T/R NO FAULTS FOUND. REMOVED AND REPLACED EEC. 2L72 4F4 FRTA2NM E17NE 20040226001672004022600167NM 2004 2 26 DLM90040136 120040206A575559545921 HINGE DOUG MD90 MD9030 3023690NM LT WING SPOILER BROKEN A DALAO OTHER O OTHER LDLANDING 1 SO27915DN 53395 FOUND WHILE WORKING MCO FOR SPOILER DEPLOY MSG. FOUND LEFT INBOARD FLT SPOILER I/B HINGE BROKEN. CAUSED DAMAGE TO THE POSITION SENSOR AND PUNCTURED HOLE INTO O/B FORE FLAP. REPLACING NEXT HIGHER ASSY THE SPOILER AND THE LEFT O/B FORE FLAP. 2L72 4F RTA6WE 20040226001732004022600173NM 2004 2 26 DLM88040142 120040209A2130 CONTROL PANEL DOUG MD88 MD88 3023688NM CABIN PRESSURE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27941DL 49814 ON TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. LOUD NOISE COMING FROM F/O'S SLIDING WINDOW. EVEN IN MANUAL PRESSURE MODE A/C WOULD NOT PRESSURIZE WELL. PERFORMED PAPER TEST ON WINDOW. NO RESISTANCE ON THE UPPER AFT PART OF WINDOW. BIT BOTH PRESSURE CONTROLLERS. BOTH FAULT AC MOTOR WITH NO ASSOCIATED ALERTS IN FLIGHT DECK RIGGED F/O'S WINDOW. REPLACED OVERHEAD PRESS CONTROL PANEL. PRESSURIZED A/C F/O'S WINDOW LEAK CHECKS GOOD. PRESS CONTROLLER RESET. PRESSURIZATION NOW CHECKS GOOD. A/C OK FOR SERVICE. 2L72 4F RTA6WE 20040226001822004022600182NM 2004 2 26 DL76L040151 120040118A5200 LATCH BOEING767 767332 1382001NM SLIDE COMPART CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27173DN 24800 DURING OFFWING SLIDE COMPARTMENT DOOR LATCH INSPECTION OPN 5894AD, MISC HARDWARE FOUND TO BE CORRODED. REPLACED DELTA PART NUMBERS: 251211768, 011216100, 251210507, 251210349, 011214656, MFG 416T2824-3, 416T2075-1, 416T2836-9, NAS43HT4-10, BACT32G64-1072, 251210196. 2L72 4F RTA1NM 20040226001842004022600184NM 2004 2 26 DL75K040153 120040206A2150 ODOR BOEING757 757232 1384965NM A/C PACKS DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO276707A 30395 FLT ATTENDANTS REPORTED VISIBLE SMOKE AND DE-ICE FLUID ODOR WHEN PACKS TURNED ON WITH APU AFTER PARKING IN FLL. TURNED PACKS OFF AND APU BLEED BLEED VALVE OFF SMOKE DISSIPATED. OPERATED BOTH PACKS, NO ODOR NOTED SYSTEM CHECKS GOOD AT THIS TIME. 2L72 4F RTA2NM 20040226001852004022600185NM 2004 2 26 DL767040154 120040210A5744113T1212 FITTING BOEING767 767232 1385132NM LT WING TE FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27107DL 22219 THE INBOARD SUPPORT BEAM FOR THE INBOARD FLAP ON THE LT WING WAS FOUND WITH CORROSION IN THE FLAP ATTACH HOLES. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLES. ALUMINUM REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IN THE HOLE BORES. THE REPAIR WAS ACCOMPLISHED PER ER/A 088453-14. 2L72 4F RTA1NM 20040226001862004022600186NM 2004 2 26 DL73S040155 120040212A53306545767153 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312DL 23084 THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH TYPICAL CRACK IMMEDIATELY ABOVE STRINGER 16L. THE CRACK RAN ALONG THE EDGE OF THE BONDED INTERNAL DOUBLER AT THE STRINGER. THE CRACK WAS REMOVED WITH A CUTOUT THROUGH THE SKIN AND BONDED DOUBLER AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 088513-14, REV A. 2L72 4F RTA16WE 20040226001882004022600188NM 2004 2 26 DLM88040157 120040214A2420 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE #1 ENGINE INOPERATIVE A DALAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO27976DL38257 53257 718238 ON TAKEOFF ROLL AFTER AUTO THROTTLES ENGAGED LEFT GENERATOR CAUSED ELECTRICS TO FLUCUATE AND DISENGAGE AUTO THROTTLES ABORT AT 20-30 KNOTS ACCOMPLISHED. WORKING MCO LEFT CSD LOW PRESSURE LIGHT. RAN ENGINE AND FOUND LEFT CSD BAD. CHANGED MEL TO 24-00-01A. CSD DISC LOW LIGHT GOOD AND NO VOLTS OR FREQS. RECONNECTED CANNON PLUG. 2L72 4F4 FRTA6WE E9NE 20040226001902004022600190 2004 2 26 DL76L040159 420040215A23301302045101 MONITOR BOEING767 767332 1382001NM SEAT 4B ODOR A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27196DN 28453 DURING PDC, NOTICED ELEC ODOR IN AREA OF 4A AND B FOUND SEAT 4-B INSEAT MONITOR TO BE SOURCE OF ODOR. REPLACED MONITOR. MONITOR CHECKS OK. 2L72 4F RTA1NM 20040226001962004022600196CE 2004 2 26 DXTA200400244 120040216A3210 LANDING GEAR CESSNA500 560CESSNA 2076750CE MAINS INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07395QS 5600496 AFTER TAKEOFF COULD NOT RETRACT LANDING GEAR, DIVERTED AIRCRAFT TO SUA. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040227000062004022700006NM 2004 2 27 QXEA200400069 120040127A5210 GUIDE DHAV DHC8 DHC8202 2809007NM CABIN DOOR LACK OF LUBE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH14607 500 SEA - FLIGHT 2062 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND LUBED THE DOOR GUIDES. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040227000072004022700007NM 2004 2 27 QXEA200400070 120040127A5210 HAND RAIL DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR LACK OF LUBE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09355PH14607 500 SEA - FLIGHT 2054 - THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE RESEATED THE AFT HANDRAIL SUPPORT NUT; LUBED ALL MOVING POINTS; PRESSURIZED THE AIRCRAFT TO ENSURE THE DOOR SEAL WAS DEFLATING. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040227000082004022700008NM 2004 2 27 C1HA200482002 120040127A57536521630187 SKIN BOEING727 7272S7 138407ZNM TE FLAP DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15682CA 22019 LEFT IB FORE FLAP DELAMINATED AT IB AFT EDGE. PIN 65-21630-249A REQ NR 125615 REMOVED AND REPLACED. LT IB FORE FLAP, OPS CHECKED OK IAW MM 27-51-01 RII ACCOMPLISHED FOR INSTALLATION AND OPS CHECKS. 2L73 4F A3WE 20040227000102004022700010NM 2004 2 27 SCNA04002 120040128A2913849589 PUMP BOEING737 737800* NM NR 1 ENG HYD SYSFAILED A SCNAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15PHHZC 28375 ENGINE 1 HYD A LOW PRESSURE LT ILLUMINATED IN CRUISE. ACCOMPLISHED NNC IAW QRH. 11 MIN LATER ENG 2 HYD B LOW PRESS LIGHT ILLUMINATED. HYD B LOW PRESSURE LT EXTINGUISHED ON DECENT. EMERGENCY DECLARED AFTER ILLUMINATION OF ENG 2 HYD B LOW PRESSURE LT ILLUMINATION. REMOVED AND REPLACED NR 1 ENG HYD PUMP AND ENGINE CASE DRAIN FILTER. GROUND RUN OPS CHECKED GOOD. NO LEAKS DETECTED. RAN NR 2 ENG, NO TROUBLE FOUND. 2L72 4F RTA16WE 20040227000112004022700011EA 2004 2 27 COMA0460088 120040126A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01915CA 7013 FLIGHT 5923 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F RTA21EA 20040227000132004022700013EA 2004 2 27 COMA0460089 120040126A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01967CA 7134 FLIGHT 5034 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F RTA21EA 20040227000152004022700015EA 2004 2 27 COMA0460091 120040126A2130 VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE STUCK A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01819CA 7415 FLIGHT 5322 OVERBOARD COOL CAUTION MESSAGE, AIRCRAFT WOULD NOT PRESSURIZE. OVERBOARD COOL VALVE STUCK OPEN, REPOSITIONED VALVE. SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040227000162004022700016NM 2004 2 27 F3LA200400004 120040128A5330 SKIN BOEING737 7373S1 138447SNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1938 24856 DURING C-7 CHECK, INSPECTION REPORTED RT AFT FUSELAGE SKIN CRACKED JUST BELOW EMERGENCY LIGHT AT STA. 727, STR. 25R. CUT OUT DAMAGED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, PAGE 204-206. 2L72 4F RTA16WE 20040227000182004022700018CE 2004 2 27 VAZ2004F00000 120040114A3220 LINKAGE CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO NLG CRACKED B VAZVO OTHER O OTHER NRNOT REPORTED 1 NE01660W 402B0828 PARTS WERE FOUND CRACKED AT THE RT PIVOT POINT OF THE NOSE GEAR RETRACTION LINKAGE OF AIRCRAFT. 1L72 3O3 O A7CE E8CE 20040227000202004022700020WP 2004 2 27 GTIA040025 120040107A5315 FLOORBEAM DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CABIN STATION 218 LBL 30 TO LBL 36 FLOORBEAM CORRODED. REMOVED CORRODED FLOOR SUPPORT. FABRICATED NEW FLOORBEAM. INSTALLED NEW FLOORBEAM. (M) 2L72 4F A6WE 20040227000242004022700024 2004 2 27 GTIA040032 420040126A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FLL - FLT 679 - L1 DOOR SLIDE NOT ATTACHED AT BOTTOM SIDE. REINSTALLED L1 DOOR SLIDE. (M) 2L72 4F A6WE 20040227000252004022700025WP 2004 2 27 GTIA040033 120040126A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP NLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23812NK 48021 FLL - FLT 1123 - NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH UPON RETRACTION. RECYCLED PER QRH, WHICH DID NOT REMEDY SITUATION. LIGHT FINALLY WENT OUT APPROXIMATELY 2 MINUTES AFTER LAST RETRACTION. REMOVED AND REPLACED NOSE GEAR UPLOCK PROXIMITY SENSOR (D1-31). BITE CHECK, OPS CHECK NORMAL ON PROXIMITY DETECTOR UNIT. (M) 2L72 4F A6WE 20040227000272004022700027WP 2004 2 27 GTIA040041 120040128A4930 PACKING DOUG DC9 DC983 3022083WP APU FUEL HEATER DAMAGED A GTIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23826NK 49391 DTW - FOUND FUEL ODOR IN AIRCRAFT CABIN. REPLACED A PACKING AT APU FUEL HEATER. (M) 2L72 4F RTA6WE 20040227000302004022700030WP 2004 2 27 GTIA040022 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE PEELING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD ENTRY WAY STATION 160-200 EXPOSED HONEYCOMB ON UPPER FACE, PEELING FIBERGLASS. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040227000332004022700033WP 2004 2 27 GTIA040028 120040119A3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP MLG LOOSE A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23808NK 49504 MCO - FLT 1912 - NOSE GEAR RED LIGHT REMAINS ON WITH GEAR HANDLE UP, FOLLOWED QRH PROCEDURE. T/S FOUND NOSE GEAR UP/DOWN AND LOCKED SENSOR LOOSE. SECURED SAME. PERFORMED NOSE GEAR RETRACTION TEST SEVERAL TIMES, OPS CHECK GOOD AT THIS TIME. (M) 2L72 4F RTA6WE 20040227000342004022700034WP 2004 2 27 GTIA040029 120040120A2560 GLOWSTRIP DOUG DC9 DC982 3022082WP L2 DOOR MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 MCO - FLT 1863 - FLOOR GLOW PATH STRIP MISSING BY L2 DOOR. REPLACED MISSING SAFTGLO SUPPORT FLOOR PATH STRIP. (M) 2L72 4F A6WE 20040227000352004022700035WP 2004 2 27 GTIA040020 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE PEELING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD LEFT OUTBOARD STATION 160-200 MISSING EDGE FILLER, PEELING FIBERGLASS. FABRICATED NEW CENTER CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040227000362004022700036WP 2004 2 27 GTIA040023 120040107A5315 FLOORBEAM DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CABIN STATION 218 LBL 13 INCHES RBL 13 INCHES FLOORBEAM CORRODED TWO FROZEN SCREWS. REMOVED FLOORBEAM. DRILLED AND LOCATED HOLES. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20040227000422004022700042WP 2004 2 27 GTIA040039 120040107A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW = FOND MID PIT CRACKED INTERCOSTAL IN OVERHEAD AT PAX CABIN FLOORBOARD NUT CLIP HOLES, FS 769-788 0 BL. REMOVED INTERCOSTAL. CUT OFF DAMAGED LIP. FABRICATED REPAIR DOUBLER. INSTALLED INTERCOSTAL AT STATION 769-788 0 BL. (M) 2L72 4F RTA6WE 20040227000572004022700057WP 2004 2 27 AALA20040149 120040128A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21223AA 49173 SEAT EMERGENCY EXIT LIGHTS FROM AFT OVERWING EXIT DOOR TO AFT OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK AT AFT GALLEY FOR SEAT EMERGENCY EXIT LIGHTS FROM AFT OVERWING EXIT DOOR TO AFT OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. -CLOSED-- 2L72 4F A6WE 20040227000582004022700058WP 2004 2 27 AALA20040146 120040128A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21416AA 49327 EMERGENCY LIGHTS AT TAIL CONE AND AT COCKPIT ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS AT TAILCONE AND AT COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F A6WE 20040227000592004022700059NM 2004 2 27 AALA20040147 120040128A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21961AN 30092 EMERGENCY LIGHTING AT ROWS 1 TO 11 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 7 SIDE WALL FOR EMERGENCY LIGHTING AT ROWS 1 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040227000602004022700060CE 2004 2 27 RJ19002 120040122A3230 UPLOCK BEECH MU300 400BEECH CE MLG OUT OF RIG E ERYAO OTHER J WARNING INDICATION DEDESCENT 1 CE07598JL RJ19 NOSE GEAR EXTENDED DURING DESCENT ON ITS OWN. EXTENDED GEAR, VERIFIED GEAR DOWN AND LOCKED, CONTINUED DESCENT TO ORIGINAL DESTINATION, LANDED WITHOUT EVENT. FOUND NLG UPLOCK MECHANISM OUT OF RIG. RE-RIG, LUBRICATE AND OP TEST SATISFACTORY. 2H72 4F RTA16SW 20040227000612004022700061CE 2004 2 27 A075SA2 120040125A3231 UPLOCK ROLLER MTSBSIMU300 MU300 5780602CE PWA JT15 JT15D4 52112NE RT MLG OUT OF RIG E ERYAO OTHER J WARNING INDICATION APAPPROACH 1 CE07824DW A075SA RT MAIN LANDING GEAR INBOARD DOOR DID NOT LOCK IN UP POSITION DURING GEAR EXTENSION. VERIFIED GEAR DOWN AND LOCKED, CONTINUED APPROACH, LANDED WITHOUT EVENT. INSPECTION FOUND GEAR DOOR UPLOCK MECHANISM OUT OF RIG. RE-RIGGED, AND FUNCTIONAL TEST PERFORMED SATISFACTORY. 2H72 4F4 FRTA14SW E1NE 20040227000632004022700063GL 2004 2 27 O05R200412704 320040127A6114 FLANGE FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE331* 01514WP ROTOL R321 R321482F8 GL PROP HUB CRACKED B K NONE O OTHER ININSP/MAINT 1 GL05698FA DRIDRG1360 RELEVANT INDICATION FOUND IN HUB MOUNTING FLANGE USING ULTRASOUND IN COMPLIANCE WITH MFG S.B. 61-1125R1. 2L72 4T3 TRTA18SW E2WE 6 CP61GL 20040227000652004022700065GL 2004 2 27 O05R200423591 320040127A611166070924017 BLADE FRCHLD22 22C7A 3370104EA GARRTTTPE331TPE331* 01514WP ROTOL R321 R321482F8 GL PROPELLER UNSERVICEABLE B K NONE O OTHER ININSP/MAINT 1 GL05698FA14223 DRG136084 BLADE REJECTED IAW MFG CONCESSION 102566/C/P. 1H71 3I3 T ATC438 E2WE 6 CP61GL 20040227000682004022700068NM 2004 2 27 SCNA04004 120040129A3350 LIGHT BOEING737 737800* NM ROWS 11&12 LOOSE A SCNAK NONE O OTHER LDLANDING 1 GL15PHHZG 28379 CREW REPORTED EMERGENCY FLOOR LIGHTING LOOSE AT ROWS 11 AND 12 ABC. MAINTENANCE SECURED EMERGENCY FLOOR TRACK LIGHTING AT ROWS 11 AND 12 ABC. SECURITY AND OPS CHECKED GOOD. 2L72 4F RTA16WE 20040227000692004022700069NM 2004 2 27 SCNA04005 120040127A3350 FACEPLATE BOEING737 737800* NM EXIT SIGN MISSING A SCNAK NONE O OTHER ININSP/MAINT 1 GL15PHHZV 30650 EXIT SIGN FACE PLATE MISSING BY 2L. RECOVERED AND REPLACED FACEPLATE AT 2L. OK FOR SERVICE. 2L72 4F RTA16WE 20040227000702004022700070WP 2004 2 27 0400149915 120040128A2910 RELIEF VALVE DOUG DC9 DC931 3022065WP RT HYD SYSTEM FAILED A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01965N 47417 AT ABOUT 100 MILES OUT FROM LANDING THE AIRCRAFT, PRODUCED SMOKE IN THE COCKPIT. ALSO NOTICED THE LOSS OF THE RT HYDRAULIC SYSTEM AS QUANTITY WENT TO ZERO ACCOMPANIED BY 'R HYD PRES LOW' LIGHT. FLIGHT CREW DECLARED AN EMERGENCY, REQUESTED CFR, AND LANDED UNEVENTFULLY AT MCO. CREW SUSPECTED THAT THE APU WAS INGESTING THE LEAKING HYDRAULIC FLUID CAUSING SMOKE. MAINTENANCE REPLACED A FAILED VACUUM BREAKER RELIEF VALVE, RT ENGINE HYDRAULIC PUMP AND FILTERS, AND BOTH WATER COALESCER BAGS. SERVICED AND LEAK CHECK OK. AIRCRAFT RETURNED TO REVENUE FLIGHT. 2L72 4F A6WE 20040227000712004022700071EU 2004 2 27 BAQA092392 120040121A80000174078030 START VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03365KY1255 6529 START DRAIN VALVE, LEAKING. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1G72 3U3 U H10EU E19EU 20040227000722004022700072EU 2004 2 27 BAQA092410 120040121A80129550147560 SOLENOID VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE STARTER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY1255 6529 UNIT INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1G72 3U3 U H10EU E19EU 20040227000732004022700073EU 2004 2 27 BAQA091933 120040112A71700174078010 DRAIN VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENG START LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM1000 6396 DRAIN VALVE LEAKING. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1G72 3U3 U H10EU E19EU 20040227000802004022700080EU 2004 2 27 BAQA090556 120040113A672041800876800 ACTUATOR UROCOPEC135 EC135T1 5620026EU TAIL ROTOR MALFUNCTIONED B BAQAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA03511ME235 0143 AMBER 4 AND ACTUATION ON CPDS AND FLI. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/02/2004 1G72 3U H88EU 20040227000842004022700084NM 2004 2 27 DHL2004743002 120040130A5220 STOP BOEING727 727225 1384077NM DOOR FRAME LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 LT FORWARD OVER WING EXIT HAS UPPER AFT STOP PAD LOOSE IN DOOR FRAME. REPAIRED STOP PAD AFT UPPER LT FORWARD OVER WING EXIT DOOR IAW B-727 M/M 52-21-00. 2L73 4F A3WE 20040227000852004022700085NM 2004 2 27 373PA0039 120040202A5320 ATTACH ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 ATTACH ANGLE CRACKED, AFT SIDE OF FRAME STA 727A UNDER TRANSITION ANGLE. REPLACED ANGLE IAW SRM 51-10-2. 2L72 4F RTA16WE 20040227000892004022700089NM 2004 2 27 373PA0043 120040202A5320 THRESHOLD BOEING737 7373Y0 1384671NM FWD CARGO CORNERCRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 FWD CARGO FWD THRESHOLD CORNER IS CRACKED. REPAIRED IAW SPM 20-3 AND MFG PROCESS SPEC. BAC5975. 2L72 4F RTA16WE 20040227000912004022700091WP 2004 2 27 MWEA040014 120040130A2910NAS16128 O-RING DOUG DC9 DC981 3022081WP LANDING GEAR LEAKING A MWEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31806ME 48032 RT HYDRAULIC QUANTITY GAUGE INDICATED IN RED ARC FOLLOWED BY RT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS ILLUMINATING. ACCOMPLISHED QRH PROCEDURES. -- REMOVED AND REPLACED O-RING AT TOP REDUCER. 2L72 4F A6WE 20040227000962004022700096SO 2004 2 27 C2XA04IA010 120040128A335020131A BATTERY EMB 145 EMB145 3260210SO ALLSN AE3007AE3007C GL EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713964 145123 DURING SCHEDULED MAINTENANCE THE FORWARD EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE EMERGENCY LIGHTS AND CLEARED THE DISCREPANCY. 2L72 4F4 FRTT00011ATTE6CH 20040227000982004022700098CE 2004 2 27 TCH2004F00000 120040126A2823 SHUTOFF VALVE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE FUEL SYSTEM FAILED E TCHAO OTHER O OTHER NRNOT REPORTED 1 GL03234DK1 RK182 NEW PART INSTALLED ON AIRCRAFT, FAILED AFTER ONLY 1.0 HOUR IN SERVICE. THIS VALVE FUNCTIONS AS THE LT FIREWALL SHUTOFF. 2H72 4F4 FRTA16SW E25EA 20040227001022004022700102CE 2004 2 27 ACS2004F00000 120040120A323057271109 ACTUATOR CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RT MAIN UPLOCK INOPERATIVE E ACSAO OTHER O OTHER NRNOT REPORTED 1 AL01402ET13949 402C0054 PILOT SELECTED GEAR DOWN AND DID NOT GET AN INDICATION OF THE RT GEAR DOWN AND LOCKED. AFTER CYCLING THE GEAR SEVERAL TIMES WITHOUT SUCCESS OF A DOWN AND LOCKED LIGHT, PILOT THEN PERFORMED EMERGENCY LANDING GEAR EXTENSION WITH THE BLOW DOWN BOTTLE. GEAR ON RT STILL DID NOT GIVE A DOWN LIGHT. AC WAS FORCED TO LAND WITH RT MAIN STILL IN THE WHEEL WELL. GEAR SWINGS WERE PERFORMED TO FIND THAT ALL SYSTEMS WORKED AS NEEDED WATER WAS PRESENT IN THE HYDR SYS, UPLOCK ACTUATOR. FLUID WAS TESTED AND FOUND THAT IT WOULD FREEZE. DETERMINED THAT FLUID IN UPLOCK ACTUATOR HAD FROZEN NOT ALLOWING THE UPLOCK TO RELEASE. THIS UPLOCK ACTUATOR ON THIS SYS IS A ONE-WAY CYLINDER AND FLUID DOES NOT CIRCULATE. 1L72 3O3 O A7CE E8CE 20040227001042004022700104EU 2004 2 27 ILD2004F00000 120040110A2913704A33690004 BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE HYDRAULIC PUMP BROKEN E ILDAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 WP13451H 435 3231 AIRCRAFT LOST HYDRAULIC POWER DURING SEES SIGHT TOUR. PILOT MADE PRECAUTION LANDING. AIRCRAFT WAS INSPECTED AND FOUND HYDRAULIC BELT BROKEN. HYDRAULIC BELT WAS REPLACED. RUNUP AND FUNCTIONAL TESTED HYDRAULIC SYSTEM WORKS NORMAL. AIRCRAFT RETURNED TO SERVICE AFTER AN OPERATIVE FLIGHT CHECK. 1G71 3U3 U H9EU E19EU 20040227001052004022700105CE 2004 2 27 GLBA20030550 120040130A273011452403725 CONTROL CABLE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR INOPERATIVE A GLBAO OTHER O OTHER APAPPROACH 1 NM0394GL UE94 MANUAL TRIM INOPERATIVE, REMOVED AND REPLACED FWD ELEVATOR TRIM CABLE PN 114-524037-25. OPS CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040227001062004022700106SO 2004 2 27 R6U2004F00000 120040129A5313 STRINGER GULSTMG1159 G1159 3953505SO FUSELAGE CRACKED B R6URO OTHER O OTHER NRNOT REPORTED 1 GL03251JS13287 251 STRINGER 24R WAS FOUND TO HAVE A 1.5 INCH CRACK IN THE FLANGE RADIUS AT FS596.00. PROBABLE CAUSE: FATIGUE. 2L72 4F RTA12EA 20040301000012004030100001CE 2004 3 1 VAZ2004F00001 120040114A534352130404 WEB CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO RT NOSEWHEEL WELCRACKED B VAZVO OTHER O OTHER NRNOT REPORTED 1 NE01119PA6000 402B0610 NLG WW WEB FOUND CRACKED AT THE RT PIVOT POINT OF THE NOSE GEAR RETRACTION LINKAGE. 1L72 3O3 O A7CE E8CE 20040301000042004030100004NE 2004 3 1 JYD2004F00003 220040122A7230670802 COMPRESSOR WHEEL SKRSKYS64 CH54B 8142610NE PWA JFTD12JFTD12A4A 52047NE ENGINE CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09223AC4902 1087 677782 64086 A CRACK WAS FOUND IN THE BLADE RETENTION HOLE OF THE 2ND STAGE COMPRESSOR DISK. COMPRESSOR, SN 677782, WAS REMOVED FOR HSI/OVERHAUL. DURING THE INSPECTION PROCESS, NDT DETECTED A CRACK IN THE BLADE RETENTION HOLE, CENTER LAND USING EDDY CURRENT. THE CRACK WAS VERIFIED BY FPI. LOOKING AT THE REAR FACE OF THE DISK WITH THE WORD (REAR) AT THE 12 OCLOCK POSITION, THE CRACK BEGINS AT APPROXIMATELY THE 9 OCLOCK POSITION EXTENDING AT A 45 DEGREE ANGLE COUNTER CLOCKWISE. THE LENGTH OF THE CRACK EXTENDS FROM THE HOLE TO THE OUTER EDGE OF LAND APPROXIMATELY .3000 INCH LONG. PROBABLE CAUSE IS UNKNOWN. NO RECOMMENDATION FOR PREVENTION. (MDR04-043) 2G72 4U4 U H6EA E15EA 20040301000242004030100024SW 2004 3 1 QML2004F00000 120040109A6220MS2125006010 BOLT BELL 222 222U 1182140SW LYC LTS101LTS101* NE M/R HUB ASSY DAMAGED E QMLAO OTHER O OTHER NRNOT REPORTED 1 NM03911NM1945 47569 THE BOLTS HOLDING THE WEIGHT SUPPORT SHEARED AND DEPARTED THE AIRCRAFT. THIS CAUSED DAMAGE TO THE M/R GRIP, DAMAGE FOUND TO BE WITHIN LIMITS AFTER REPAIR. THE BOLTS ON THE OPPOSITE SIDE DEPARTED SUPPORT SHOWED 5 LOOSE BOLTS AND ONE BOLT SHEARED.(K) 1G72 3U3 U H9SW E5NE 20040301000252004030100025EU 2004 3 1 PG92004F00002 120040107A2913S40 COUPLING SLEEVE SNIAS 350 AS350B2 8680813EU FAILED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19170PA5575 2637 COUPLING SLEEVE FAILED WITH ONLY 354 HOURS, SHAFT SEIZED TO COUPLING SLEEVE. (RMA NR R046420) (K) 1G71 3U H9EU 20040301000272004030100027EU 2004 3 1 PG92004F00005 120040123A2910704A34412038 LINE SNIAS 350 AS350B2 8680813EU HYD SYSTEM LEAKING E PG9AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP19453NW 2475 HOSE LOST PRESSURE AND LEAKED HYDRAULIC OIL OUT, CAUSING LOSS OF FLIGHT CONTROL BOOST AND SUBSEQUENT PRECAUTIONARY LANDING. REMOVED AND REPLACED HOSE WITH NEW. (K) 1G71 3U H9EU 20040301000522004030100052SW 2004 3 1 QS72004F00000 120040211A6520206040439001 SHAFT BELL BELL 206 206B 1181511SW ALLSN 250C 250C* GL T/R GEARBOX WORN B QS7RK NONE O OTHER ININSP/MAINT 1 NM09921RB6702 846 ALO11974 2624 DURING ANNUAL INSPECTION FOUND KNURLED NUT WORN BEYOND LIMITS. UPON REMOVAL OF THE KNURLED NUT AND TAIL ROTOR BALANCE WHEEL FOUND THREADS ON TAIL ROTOR GEARBOX OUTPUT SHAFT, UNDER BALANCE WHEEL, EXCESSIVELY WORN AND GALLED. CUSTOMERS PILOT REPORTED THAT THEY HAD EXPERIENCED DIFFICULTY IN MAINTAINING TORQUE ON THE KNURLED NUT. 1G71 3U3 U H2SW E4CE 20040301000622004030100062CE 2004 3 1 GLBA20030551 120040202A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA CABIN DOOR FALSE ACTIVATIONA GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM0396UX UE96 CABIN DOOR ANNUNCIATOR CAME ON IN FLIGHT, CABIN DOOR ANNUNCIATOR OPS CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040302000022004030200002WP 2004 3 2 AALA20040241 120040215A3350 SIGN DOUG DC9 DC983 3022083WP CABIN UNSERVICEABLE A AALAK NONE O OTHER ININSP/MAINT 1 SW21436AA 49454 DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT UNREADABLE. REPLACED EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040302000052004030200005NM 2004 3 2 SWAA040448 120040212A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040302000062004030200006NM 2004 3 2 SWAA040449 120040212A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 867, BETWEEN STRINGERS 8L AND 9L, AND BS 907, BS 887, BS 867, BETWEEN STRINGERS 8R AND 9R. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20040302000112004030200011NM 2004 3 2 SWAA040425 120040210A3350610478 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040302000132004030200013NM 2004 3 2 SWAA040427 120040210A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 277, RBL 55, WL 250 AND BS 277, RBL 55, WL 254. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040302000142004030200014NM 2004 3 2 SWAA040428 120040210A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C4 CHECK, FOUND STRINGER 18L CRACKED AT BS 750. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040302000172004030200017NM 2004 3 2 SWAA040431 120040210A3350013071BPEGPL LIGHT BOEING737 7373A4 1384585NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040302000272004030200027NM 2004 3 2 SWAA040417 120040209A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND SHEAR TIES CORRODED AT AFT CARGO COMPT BS 767, BL 0, BS 807, LBL 17. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040302000442004030200044NM 2004 3 2 SWAA040373 120040205A5530183A4211 FITTING BOEING737 7373Y0 1384671NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB RT AND LT FITTING AFT SPAR LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER. 2L72 4F RTA16WE 20040302000562004030200056WP 2004 3 2 AALA20040267 120040223A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21577AA 53154 DEN - CEILING EMERGENCY LIGHTS AT STATION 1209L INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-107 FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000692004030200069WP 2004 3 2 AALA20040254 120040219A213121171803 CONTROLLER DOUG DC9 DC983 3022083WP CABIN PRESSURE INOPERATIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21562AA 49344 ORD - INFLIGHT T2373/19 UPON TAKEOFF FROM MDW THE AIRCRAFT WOULD NOT PRESSURIZE AND THE STANDBY LIGHT ILLUMINATED. LANDED AT ORD WITHOUT INCIDENT. REPLACED NR 1 CONTROLLER. BITE CHECKED BOTH NR 1 AND NR 2 CONTROLLERS AND NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040302000702004030200070NM 2004 3 2 AALA20040250 120040219A3350 LIGHT BOEING767 767323 1385205NM EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139365 24046 SFO - RIGHT HAND EMERGENCY LIGHT ABOVE AFT WING AND EXTENDING TO BODY FAIRINGS INOPERATIVE. CLEANED CONTACTS AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040302000742004030200074WP 2004 3 2 AALA20050256 120040220A3260833703 SENSOR DOUG DC9 DC982 3022082WP NLG FAULTY A AALAK NONE N FALSE WARNING CLCLIMB 1 SW21412AA 49323 ON GEAR RETRACTION AFTER TAKEOFF NOSE LANDING GEAR POSITION INDICATOR REMAINED RED. RECYCLED GEAR. NOSE LANDING GEAR POSITION LIGHT STILL REMAINED RED. NOSE LANDING GEAR INDICATOR PIN ON CENTER CONSOLE. COMPLETELY RETRACTED. ON GEAR EXTENSION, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. NOSE LANDING GEAR VISUAL INDICATOR PIN ON THE CENTER CONTROL PEDESTAL WAS FULLY EXTENDED INDICATING NOSE GEAR DOWN AND LOCKED. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SENSOR D1-32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000812004030200081NM 2004 3 2 CALA0400145 120040220A575365C263102 SKIN BOEING737 7373T0 1384582NM NR 3 MID FLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND NR 3 MID FLAP OUTBOARD L/E SKIN GOUGED JUST FORWARD OF EXHAUST GATE. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5752-01144. 2L72 4F RTA16WE 20040302000822004030200082NM 2004 3 2 CALA0400146 120040221A5320BAC1496377X7075TCHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716732 28948 INSPECTION FOUND RT FLOOR PANEL Z-CHANNEL SUPPORT RAIL CORRODED AT STA 727-767. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040302000922004030200092NM 2004 3 2 CALA0400141 120040220A5415313A1380114 SUPPORT FITTING BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND NR 2 ENGINE PYLON O/B MID SPAR FITTING PANEL AFT RETAINER (SUPPORT FITTING) CRACKED AT UPPER AREA, PYLON STA 279.5. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040302000992004030200099NM 2004 3 2 CALA0400157 120040223A5510180A16122 PIN BOEING737 737824 13844BZNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND THE RT HORIZONTAL STABILIZER LOWER AFT PIN AND LT HORIZONTAL STABILIZER AFT MIDDLE PIN CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040302001312004030200131NM 2004 3 2 SWAA040267 120040127A53206545829 FITTING BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER END TIE CORRODED AT BS 365, STRINGER 28L. REPAIRED END TIE PER SRM. 2L72 4F RTA16WE 20040302001322004030200132NM 2004 3 2 SWAA040268 120040127A53116545805 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 277, STRINGER 16 L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040302001362004030200136NM 2004 3 2 SWAA040273 120040128A3350101114 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. INSTALLED LENS AT RT OVERWING DOOR PER MM. 2L72 4F RTA16WE 20040302001442004030200144NM 2004 3 2 SWAA040281 120040128A53116546551 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 827, STRINGER 9L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040302001452004030200145NM 2004 3 2 SWAA040282 120040128A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CRACKED AT BS 663.5, BL 0. REPAIRED BEAM PER SB. 2L72 4F RTA16WE 20040302001512004030200151NM 2004 3 2 SWAA040301 120040130A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STRINGER 21R. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040302001632004030200163NM 2004 3 2 SWAA040313 120040130A53116546526 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 400, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040302001692004030200169NM 2004 3 2 SWAA040319 120040130A53116546558 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 907, STRINGER 9R AND AT BS 907, STRINGER 9L. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20040302001712004030200171 2004 3 2 SWAA040374 420040207A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 R2 DOOR EVAC SLIDE PRESSURE LOW INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000032004021900003NM 2004 2 19 04FDEA00338 120040206A5711ARB74054 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 538 TO XORS 582. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 538 TO XORS 562 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II. 2L73 4F RTA22WE 20040219000042004021900004NM 2004 2 19 04FDEA00337 120040206A5711ARB74054 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING- UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 562 TO XORS 623. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 562 TO XORS 623 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II. 2L73 4F RTA22WE 20040219000062004021900006NM 2004 2 19 SWAA040436 120040211A2823W38801020 WIRE BOEING737 7373A4 1384585NM JUNCTION BOX SHORTED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29675AA 23253 AIRTURN BACK, SHORTLY AFTER TAKEOFF FELT A LIGHT VIBRATION AND THEN SMOKE AND FUMES IN COCKPIT. SMOKE SMELLED ELECTRICAL AND DISIPATED ALMOST IMMEDIATELY. VIBRATION ALSO CEASED. FOUND DISCONNECT D970 SHORTED TO GROUND AND WIRES W388-010-20 AND W388-027-20 BURNED IN JUNTION BOX AT BS 720R. SPLICED NEW WIRES AND REPLACED D970 CONNECTOR PER MM. ALSO, REMOVED AND REPLACED P5-2 FUEL SYSTEM MODULE PER MM. 2L72 4F RTA16WE 20040219000072004021900007 2004 2 19 SWAA040437 420040211A25651061323 SLIDE BOEING737 7375H4 138449DNM L1 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 L1 DOOR EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000082004021900008NM 2004 2 19 SWAA040438 120040211A53136546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 727C, RBL 6, WL148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040219000092004021900009 2004 2 19 SWAA040439 420040211A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000102004021900010NM 2004 2 19 SWAA040440 120040211A552365C26384 TAB BOEING737 7373Q8 1384670NM ELEVATOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD ATTACHMENT FITTING. REMOVED AND REPLACED TAB PER MM. 2L72 4F RTA16WE 20040219000112004021900011NM 2004 2 19 SWAA040441 120040211A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STRINGER 24L. REPAIRED FUSELAGE SKIN PER SRM. 2L72 4F RTA16WE 20040219000122004021900012NM 2004 2 19 SWAA040442 120040211A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACK AT BS 870, STRINGER 25R. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040219000182004021900018NM 2004 2 19 UPS04441864 120040121A53207075T6007IN WEB BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D- BS 270 RT STR 26R VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040219000202004021900020WP 2004 2 19 UPS04841855 120040131A534037739061 FITTING DOUG DC8 DC871F 302199DWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 798, RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D. 2L74 4F RT4A25 20040219000212004021900021WP 2004 2 19 UPS04841856 120040203A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 1260-1350 LONGERON 31R. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17A, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040219000222004021900022WP 2004 2 19 ZW0A0400301 120040213A3350408822101 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE L NO TEST ININSP/MAINT 1 CE13950U 49230 AFTER BOARDING THE FLIGHT CREW ARMED THE EMERGENCY LIGHTS AND THE AISLE EGRESS LIGHTS BETWEEN ROW 22 AND 28 WERE BLINKING. REPLACED THE BATTERY PACK. CHECK-C STL 12-18-03. 2L72 4F A6WE 20040219000232004021900023SO 2004 2 19 C2XA04SH058 120040210A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RT APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040219000242004021900024EA 2004 2 19 04035628 120040204A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27628BR 7240 DURING APPROACH THE CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS AT 0 DEGREE POSITION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040219000252004021900025NM 2004 2 19 04036428 120040205A3397 WIRE DORNERDO32 DO328300 NM EMERGENCY LIGHT KINKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27428FJ 3193 DURING INSPECTION THE FORWARD EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE WIRES WERE FOUND TO BE PINCHED AND WERE REPAIRED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040219000262004021900026EA 2004 2 19 04036710 120040205A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040219000282004021900028EA 2004 2 19 04039632 120040209A3350OL3071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27632BR 7268 DURING INSPECTION THE AFT INTERIOR CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE FILAMENT IN THE LIGHT ASSEMBLY WAS FOUND BURNED OUT AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040219000312004021900031SO 2004 2 19 C2XA04SH065 120040215A532014525480003 SILL EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000322004021900032NM 2004 2 19 2004UALA00089 120040201A5240 ACCESS DOOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29674UA 29242 FUSELAGE EXTERIOR AT MAIN EQUIPMENT CENTER, ACCESS DOOR 119AL HAS LIGHTNING STRIKE DISCHARGE ON EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHED. DOOR REPAIRED WITH NEW DOUBLER. 2L72 4F4 FRTA1NM E24NE 20040219000362004021900036NE 2004 2 19 58279 220040126A7532311701101 BLEED VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 2 ENGINE COMPMALFUNCTIONED A AMWAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 CE0723YV UE23 ON APPROACH FOR LANDING NR 2 ENGINE BEGAN COMPRESSOR STALL CAUSING ERRATIC TORQUE READINGS AND FLAMES TO BE EMITTED FROM EXHAUST STACKS. CREW DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENG BLEED VALVE, OPS CHECK NORMAL. 2L72 4T4 TRTA24CE E26NE 20040219000392004021900039EU 2004 2 19 MALA040182 120040202A3150005WS00 WEU SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15426XJ 340B426 CREW REPORTED RT ESS BUSS LIGHT ON AND THE RT AC GENERATOR CAUTION LIGHT ON. AIR RETURN TO MSP. REMOVED ESS BUSS CAUTION LIGHT ON (EQUIP OFF THIS BUSS SEEMS TO BE WORKING.) REPLACED WEU. 2L72 4T RTA52EU 20040219000402004021900040EU 2004 2 19 MALA040188 120040127A5330 DOUBLER SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, LOWER FUSELAGE TCAS ANTENNA DOUBLER HAS EVIDENCE OF CORROSION. REMOVED CORROSION, HFEC SKIN (CRACK FREE) FABRICATED TCAS DOUBLER, TREATED INSTALLED DOUBLER TOP COATED IAW MESABA EO S53203. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2L72 4T RTA52EU 20040219000412004021900041EU 2004 2 19 MALA040183 120040131A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, RT FUSELAGE STA 329 HAS DENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW SAAB 340 SRM 53-70-10-2. A/C RELEASE DATE 2/16/04. REFER TO NR 1258951 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20040219000452004021900045EU 2004 2 19 MALA040184 120040126A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, RT ICE SHIELD FUSELAGE STA 329 HAS DENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED 2 EACH EXTERNAL DOUBLER REPAIRS. REMOVED AND REPLACED NR 6 & 7 ICE GUARDS IAW SAAB 340 SRM 53-70-10 SAAB 340 SRM 53-70-102. 2L72 4T RTA52EU 20040219000472004021900047EU 2004 2 19 MALA040181 120040206A3260 SWITCH SAAB SF340 340B 7860101EU MLG CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15367PX 340B271 AFTER GEAR RETRACTION ON TAKEOFF THE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED ICE FROM SWITCHES ON MLG & CLEANED SWITCHES, OPS CHECK GEAR IAW 32-30-00-5 ALL CHECKS GOOD. 2L72 4T RTA52EU 20040219000482004021900048WP 2004 2 19 04FDEA00408 120040213A5753 SKIN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD, D-FLAP, NR 5 FLAP VANE ATTACH HORN HAS TWO CORRODED / PITTED HOLES. REPLACED NR 5 FLAP VANE HORN PER M/M 27/50/03/2 AND TORQUED PER 20/50/02. 2L73 4F A22WE 20040219000492004021900049WP 2004 2 19 04FDEA00406 120040213A5753 SKIN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RT WING OUTBOARD FLAP, NR 4 FLAP VANE ATTACH HORN HAS 2 CORRODED AREAS AROUND HOLES. REPLACED NR 4 FLAP VANE ATTACH HORN PER M/M 27/50/03/2 AND TORQUED BOLTS PER M/M 20/50/20. 2L73 4F A22WE 20040219000532004021900053NM 2004 2 19 SWAA040405 120040208A5312BAC1514 STIFFENER BOEING737 7373H4 1384600NM BULKHEAD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD CHANNEL STIFFNERS AT BS 1016, BL 0. REPAIRED PER ACO. 2L72 4F RTA16WE 20040219000542004021900054WP 2004 2 19 DHL2004801002 120040205A5270 WARNING LIGHT DOUG DC8 DC873F 302199FWP CARGO DOOR FALSE INDICATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01801DH 46033 MAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED AT FL240. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE. PRESSURIZATION NORMAL. CONTINUED FLIGHT. INSPECTED MAIN CARGO DOOR VENT SYSTEM. PERFORMED OPS CHECK OF DOOR SYSTEM AND FOUND NO DEFECT. OK FOR SERVICE PER DC-8 MMS 52-70-00. 2L74 4F RT4A25 20040219000562004021900056NM 2004 2 19 SWAA040407 120040208A53146545866 KEELBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND CORROSION ON KEEL BEAM LT OUTBOARD FLANGE AT BS 727. REMOVED AND REPLACED OUTBOARD FLANGE PER ER. 2L72 4F RTA16WE 20040219000572004021900057NM 2004 2 19 SWAA040408 120040208A5531 SPAR BOEING737 7373Y0 1384671NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND CORROSION ON VERTICAL STAB FRONT SPAR RT LUG FORWARD AND AFT FACES. REPAIRED STAB PER EO. 2L72 4F RTA16WE 20040219000582004021900058NM 2004 2 19 SWAA040409 120040208A53306545700 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKS AT THE FOLLOWING, BS 585, BS 692, BS 700, BS 703, ALL AT STRINGER 4L. REPAIRED SKIN PER EO. 2L72 4F RTA16WE 20040219000592004021900059NM 2004 2 19 SWAA040235 120040123A3350 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17 ABC. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040219000622004021900062NM 2004 2 19 SWAA040237 120040124A2612896767 FIRE DETECTOR BOEING737 7373H4 1384600NM APU FALSE ACTIVATIONA SWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW29331SW 23695 DIVERSION, DURING CRUISE FLIGHT APU WARNING/BELL CAME ON WITH APU OFF. CW CHECKLIST, FIRED THE EXTINGUISHER, RED LIGHT WENT OUT. INSPECTED APU, HOUSING, AND TAILPIPE, FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED THE FIRE DETECTOR PER MM. 2L72 4F RTA16WE 20040219000642004021900064NM 2004 2 19 SWAA040411 120040208A3350100031 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040219000652004021900065EU 2004 2 19 2004UALA00090 120040130A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29408UA 457 AFT PIT STRINGER 43L IS CORRODED FROM FRAME 54 TO FRAME 56. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SECTION AND SPLICE REPAIRS. 2L72 4F4 FRTA28NM E40NE 20040219000672004021900067NM 2004 2 19 2004UALA00092 120040203A3350 LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29597UA 28750 DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECK OK. 2L72 4F4 FRTA2NM E17NE 20040219000682004021900068NM 2004 2 19 2004UALA00093 120040202A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29382UA 24657 STA 199 HORIZONTAL WEB AT STR 17L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20040219000692004021900069NM 2004 2 19 2004UALA00094 120040202A2597 CIRCUIT BREAKER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE GALLEY FAILED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29790UA 26943 BURNING ODOR FROM FORWARD GALLEY WITH SMOKE DRIFTING INTO FIRST CLASS CABIN AND DISBURSED IN BUSINESS. REPLACED CIRCUIT BREAKER C002. 2L72 4F4 FRTT0001SE E46NE 20040219000702004021900070NM 2004 2 19 2004UALA00095 120040203A3350 LAMP BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29784UA 26951 AFT EEL LIGHT AT 1E BROKEN IN TWO. REPLACED EEL LAMP ASSY. 2L72 4F4 FRTT0001SE E46NE 20040219000722004021900072NM 2004 2 19 2004UALA00097 120040202A2720 MODULE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RUDDER HYD SYS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29664UA 29236 RETURNED TO FIELD DUE TO RUDDER RATIO/AILERON TRIM MESSAGE. REPLACED BOTH STABILIZER TRIM/AILERON LOCKOUT MODULES. 2L72 4F4 FRTA1NM E24NE 20040219000732004021900073 2004 2 19 2004UALA00098 420040204A2565131W18131202 SUPPORT FITTING BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE GIRT BAR BROKEN A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29788UA 26942 DOOR 2L WILL NOT DISARM. ONE OF THE CASTINGS THAT LIFT THE SLIDE GIRT BAR WHEN ACTUATED BY THE DOOR ARM/DISARM LEVER, WAS FOUND BROKEN, PREVENTING THE SLIDE GIRT BAR FROM BEING LIFTED FREE OF THE FLOOR GIRT FITTING. THE FITTING WAS REPLACED AND THE GIRT BAR OPERATION WAS CHECKED. UAL HAS AN AMM MAINTENANCE TIP TO ADVISE TO CHECK FOR THIS CONDITION SHOULD THE DOOR BE HARD TO DISARM. 2L72 4F4 FRTT0001SE E46NE 20040219000742004021900074 2004 2 19 2004UALA00099 420040203A2565 SLIDE BOEING777 777222 1385219NM PWA PW4077PW4077 NE PAX DOOR DEPLOYED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29211UA 30217 THE 2R EMERGENCY EVACUATION SLIDE PARTIALLY DEPLOYED. DOOR 2R SLIDE/RAFT PARTIAL DEPLOYMENT OCCURRED DURING SLIDE INSTALLATION. DURING INSTALLATION SEQUENCE THE DOOR WAS ARMED, THEN WAS INADVERTENTLY OPENED SUFFICIENT TO RELEASE THE SLIDE PACK. AMM PROVIDES A WARNING STATEMENT TO REMIND PERSONNEL TO NOT ALLOW THE DOOR TO MOVE FROM THE CUTOUT, OTHERWISE THE SLIDE PACK CAN RELEASE WHILE THE DOOR IS ARMED. HOWEVER, THIS WARNING WAS APPARENTLY NOT OBSERVED DURING THE SLIDE/RAFT INSTALLATION AND THE SLIDE PERFORMED AS DESIGNED. 2L72 4F4 FRTT0001SE E46NE 20040219000752004021900075NM 2004 2 19 2004UALA00100 120040205A2120 ODOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29820UA 898 RETURN TO FIELD DUE TO AN ELECTICAL ODOR IN THE CABIN. AVIONICS COOLING BLOWER FAN BEARINGS FAILED. REPLACED UNIT WITH NO FURTHER PROBLEMS REPORTED. 2L72 4F4 FRTA28NM E40NE 20040219000762004021900076NM 2004 2 19 2004UALA00101 120040203A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29594UA 28145 LIGHTNING STRIKE ON EXTERIOR FUSE SKIN APPROX 2.5 INCH FWD OF BS 560 STR 2R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040219000772004021900077 2004 2 19 SWAA040352 420040204A2565D31354 SLIDE BOEING737 7372T4 1384492NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE IN CONTAINER PER MM. 2L72 4F A16WE 20040219000792004021900079NM 2004 2 19 SWAA040354 120040204A32601899 SENSOR BOEING737 7373G7 1384595NM NOSE GEAR OUT OF ADJUST A SWAAO OTHER N FALSE WARNING CRCRUISE 1 SW29683SW 24008 DURING CRUISE AT FL 22O, 250 KIAS, NOSE GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT SLOWED TO 220 KIAS, GEAR CYCLED, LIGHT WENT OUT. ADJUSTED NLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20040219000842004021900084SO 2004 2 19 C2XA04SH054 120040204A7160 STRUCTURE EMB EMB 145 EMB145LR 3260212SO LT ENG INTAKE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 NC1095 145563 SHV - DURING C-CHECK THE LEFT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040219000852004021900085SO 2004 2 19 C2XA04SH055 120040204A7160 STRUCTURE EMB EMB 145 EMB145LR 3260212SO NR 2 ENG INTAKE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 NC1126 145563 SHV - DURING C-CHECK THE RIGHT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040219000862004021900086SO 2004 2 19 C2XA04SH056 120040204A532014528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040219000902004021900090CE 2004 2 19 58596 120040205A6120 PROPELLER BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RIGHT OUT OF ADJUST A AMWAK NONE O OTHER TXTAXI/GRND HDL 1 CE07165YV UE165 WHILE TAXIING IN ON FLIGHT 5433, THE RIGHT PROP STUCK IN LOW PITCH. THE AIRCRAFT ARRIVED AT THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE LOW PITCH. NO PARTS WERE USED. 2L72 4T RTA24CE 5 CP10NE 20040219000912004021900091NM 2004 2 19 SWAA040357 120040204A53206551698 SPLICE BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F A16WE 20040219000932004021900093NM 2004 2 19 SWAA040359 120040204A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219000952004021900095NM 2004 2 19 SWAA040361 120040204A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STRINGER 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219000982004021900098 2004 2 19 SWAA040339 420040203A25656557463 FITTING BOEING737 7373A4 1384585NM GIRT BAR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 L2 DOOR EVAC SLIDE GIRT BAR BRACKET SPRING INOP. REMOVED AND REPLACED L2 DOOR EVAC SLIDE BRACKET PER MM. 2L72 4F RTA16WE 20040219001002004021900100 2004 2 19 SWAA040341 420040203A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040219001032004021900103NM 2004 2 19 SWAA040344 120040203A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM. 2L72 4F RTA16WE 20040219001082004021900108NM 2004 2 19 SWAA040349 120040203A531565C26402 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707 TO BS 713, LBL 25, WL 203. REPAIRED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040219001102004021900110NM 2004 2 19 SWAA040209 120040121A53206553698 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, STRINGER 4R AND STRINGER 4L. REPAIRED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20040219001112004021900111NM 2004 2 19 SWAA040210 120040121A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 4L, AND BS 344, STRINGER 9R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040219001142004021900114NM 2004 2 19 SWAA040213 120040121A5310BAC1517 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, ABOVE L2 DOOR. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040219001162004021900116NM 2004 2 19 SWAA040215 120040121A5313BAC1503 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 663, STRINGER 2R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040219001172004021900117NM 2004 2 19 SWAA040216 120040121A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND SKIN CORRODED AT FAIRING ATTACHMENT POINT BS 727B + 10 TO BS 727D, BETWEEN STRINGER 21R AND STRINGER 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001182004021900118NM 2004 2 19 SWAA040217 120040121A53206545410 STRAP BOEING737 7373Y0 1384671NM CARGO FLOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND MID CABIN FLOOR SUPPORT STRAP CRACKED AT BS 540, RBL 1, WL 208. REPAIRED FLOOR STRAP PER SRM. 2L72 4F RTA16WE 20040219001192004021900119NM 2004 2 19 SWAA040218 120040121A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 637, RBL 65, WL 208. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20040219001202004021900120NM 2004 2 19 SWAA040219 120040121A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED A1 CHECK, FOUND STRINGER 24L, AT BS 807 CRACKED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040219001242004021900124NM 2004 2 19 SWAA040223 120040122A2560P2070001 FLASHLIGHT BOEING737 7372T4 1384492NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED RON, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040219001262004021900126 2004 2 19 SWAA040225 420040122A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219001282004021900128NM 2004 2 19 SWAA040227 120040122A53306545768 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 312, STRINGER 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001292004021900129NM 2004 2 19 SWAA040228 120040122A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17R. REMOVED AND REPLACED FRAME PER SRM. 2L72 4F RTA16WE 20040219001302004021900130NM 2004 2 19 SWAA040229 120040122A53106546529 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500, LBL 1 TO LBL 3, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040219001312004021900131NM 2004 2 19 SWAA040230 120040122A57436582770 BEAM BOEING737 7373Y0 1384671NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND CORROSION ON RT MLG BEAM ON AFT STABILIZER BEAM FITTING. REMOVED AND REPLACED BEAM FITTING PER MM. 2L72 4F RTA16WE 20040219001332004021900133NM 2004 2 19 SWAA040232 120040122A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED MS, FOUND EMERGENCY EXIT LIGHT AT ROW 13 DEF INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040219001352004021900135NM 2004 2 19 SWAA040234 120040122A5312BAC1514 STIFFENER BOEING737 7373A4 1384585NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD ZEE STIFFENERS CRACKED AT 12 AND 7 O'CLOCK POSITIONS. REPAIRED STIFFENERS PER SRM. 2L72 4F RTA16WE 20040219001372004021900137EA 2004 2 19 COMA0460114 120040103A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO FLOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01812CA 7381 CARGO FLOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-433. 2L72 4F RTA21EA 20040219001382004021900138EA 2004 2 19 COMA0460115 120040103A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO FLOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01812CA 7381 CARGO FOOR LANDING PLATE AT FS 589 CRACKED FROM RIVET HOLE TO EDGE OF PLATE. COMPLIED WITH BOMBARDIER REO 601R-53-61-433. 2L72 4F RTA21EA 20040219001402004021900140EA 2004 2 19 COMA0460117 120040204A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 GENERATOR LACK OF LUBE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01938CA 7046 FLIGHT 5111 NR 2 IDG AND GENERATOR CAUTION. SERVICED THE RT IDG WITH OIL TO PROPER LEVEL. OPERATION CHECK NORMAL. 2L72 4F RTA21EA 20040219001432004021900143NM 2004 2 19 SWAA040240 120040123A5315BAC1505 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY LONGITUDINAL FLOORBEAM CORRODED AT BS 857, LBL 3, AND AT BS 945, LBL 3. REMOVED AND REPLACED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040219001442004021900144NM 2004 2 19 SWAA040241 120040123A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY SHEAR TIES CORRODED AT BS 767, STRINGER 27R, AND AT BS 747, STRINGER 27R. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040219001452004021900145NM 2004 2 19 SWAA040242 120040123A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20040219001462004021900146NM 2004 2 19 SWAA040243 120040123A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C2 CHECK, FOUND 2 CRACKS ON FUSELAGE SKIN AT BS 390, STRINGER 17R. REPAIRED SKIN CRACKS PER SRM. 2L72 4F RTA16WE 20040219001472004021900147 2004 2 19 SWAA040244 420040123A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 L1 DOOR EVAC SLIDE INADVERTENTLY FELL OUT OF HOUSING. REINSTALLED L1 DOOR EVAC SLIDE INTO HOUSING PER MM. 2L72 4F RTA16WE 20040219001482004021900148NM 2004 2 19 SWAA040245 120040124A7720162BL804A INDICATOR BOEING737 7373H4 1384600NM NR 1 ENG TEMP FAULTY A SWAAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SW29645SW 28330 INFLIGHT SHUTDOWN/DECLARED EMERGENCY, DURING FLIGHT NR 1 ENGINE OIL TEMP GAUGE READ 180-190C. ENGINE WAS SHUT DOWN IAW QRH. REMOVED AND REPLACED TEMP GAUGE PER MM. 2L72 4F RTA16WE 20040219001492004021900149NM 2004 2 19 SWAA040246 120040124A21216454051 FAN BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW29322SW 23343 RECIRCULATING FAN CAUSING ODOR IN COCKPIT. REMOVED AND REPLACED RECIRCULATING FAN PER MM. 2L72 4F RTA16WE 20040219001502004021900150NM 2004 2 19 SWAA040247 120040125A3350BR9442 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 EMERGENCY EXIT LIGHT AT FWD F/A JUMPSEAT BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040219001512004021900151NM 2004 2 19 SWAA040248 120040125A25606956819 PANEL BOEING737 7373H4 1384600NM ESCAPE ROPE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND FIRST OFFICERS EMERGENCY ESCAPE ROPE PANEL NOT OPENING. FOUND ROPE CAUGHT IN DOOR, REMOVED AND REPLACED ROPE PER MM. 2L72 4F RTA16WE 20040219001522004021900152NM 2004 2 19 SWAA040249 120040125A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND CRACK IN EXTERNAL SKIN L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001532004021900153NM 2004 2 19 SWAA040250 120040125A57536546430 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040219001542004021900154NM 2004 2 19 SWAA040251 120040125A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP LOWER INBOARD CORNER DELAMINATED. REMOVED AND REPLACED OUTBOARD FLAP PER MM. 2L72 4F RTA16WE 20040219001562004021900156NM 2004 2 19 SWAA040253 120040124A3350101114 COVER BOEING737 7373H4 1384600NM RT EMER EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 RT OVERWING EMERGENCY EXIT LIGHT AT DOOR HAS LOOSE COVER. REINSTALLED EXIT LIGHT COVER PER MM. 2L72 4F RTA16WE 20040219001592004021900159NM 2004 2 19 SWAA040256 120040126A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED AT BS 380. REMOVED AND REPLACED CRACKED STRINGER PER SRM. 2L72 4F RTA16WE 20040219001602004021900160WP 2004 2 19 DHL2004801003 120040205A5270BAN70241 SWITCH DOUG DC8 DC873F 302199FWP VENT DOOR MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01801DH 46033 MAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE. PRESSURIZATION NORMAL. CONTINUED FLIGHT REPEAT WRITE-UP. ITEM TRANSFERRED TO DMI LOG PER MEL 52-2-1 DMI 15651 PLACARD INSTALLED. REF DMI 15651 MAIN CARGO DOOR SYSTEM-A LIGHT ILLUMINATED IN FLIGHT. ACCOMPLISHED MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT EMERGENCY PROCEDURE PRESSURIZATION NORMAL. CONTINUED FLIGHT. REPEAT WRITE-UP. REPLACE VENT DOOR SWITCH IAW DC-8 M/M 52-36-1. OPS CHECKED GOOD. THIS CLEARS DMI 15651. STICKER REMOVED P/N: BAN7024-1. 2L74 4F RT4A25 20040219001612004021900161 2004 2 19 SWIA200412838 420040126A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07292SW173 173 120319 CAPTAIN SIDE FCP HAS A RED TRIM WARNING ACCOMPANIED WITH COMPUTER FLAG ON ADI. REPLACED LEFT APC65 WITH SERVICEABLE UNIT. ALL FUNCTIONAL CHECKS FOUND GOOD. P/N: 622-8315-402, S/N ON: 2470, S/N OFF: 1641. 2L72 4T RTA31SO 20040219001622004021900162 2004 2 19 SWIA200412839 420040131A34206226190204 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE ATTITUDE MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07582SW1 1 120350 IN FLIGHT, AUTOPILOT FAILED ON CAPTAIN'S SIDE. AHRS FLAGS ATT, HDG, AND FD. CYCLED ON AND OFF. F/O'S AUTOPILOT OPERATES NORMAL. INSTALLED NEW SERVICEABLE AHRS COMPUTER ON CAPTAIN'S SIDE. SYSTEM OPS CHECKS GOOD AND AUTOPILOT OPS CHECKS GOOD IAW MM 34-21-00. 2L72 4T4 TRTA31SO E20NE 20040219001682004021900168SO 2004 2 19 SWIA200412845 120040107A5320 BRACKET EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07232SW 120306 FRAME 12 BRACKET BEHIND PILOT'S DV WINDOW IS CRACKED AT FLANGE HOLE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL AT FRAME NR 12 BEHIND PILOT'S DV WINDOW PER EMB120 SRM 51-40-02. 2L72 4T RTA31SO 20040219001692004021900169SO 2004 2 19 SWIA200412846 120040114A5712 RIB EMB 120 EMB120ER 3260203SO RT WING LE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 RT INBOARD LEADING EDGE I/B RIB IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AFFECTED CRACKED RIB AND INSTALLED NEW-LIKE UNIT IAW EMB120 SRM 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20040219001702004021900170SO 2004 2 19 SWIA200412847 120040114A5210 CHANNEL EMB 120 EMB120ER 3260203SO PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 PAX DOOR MID SECTION OF DOOR FWD CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION FORWARD AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20040219001712004021900171WP 2004 2 19 DHL2004807002 120040206A2751 WARNING LIGHT DOUG DC8 DC873F 302199FWP TE FLAPS FALSE INDICATIONA DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01807DH 45990 REJECTED T/O AT 110 KNOTS DUE TO SLOT LIGHT ILLUMINATION, 264 MTOW, 24 DEGREES TEMP, NORMAL ZONE. CHECK BRAKE TEMPERATURES DO TO REJECTED T/O. CHECKED BRAKE TEMPERATURES PER AOM 4.1 PAGE 18. CHECKED OK. PERFORMED UNSCHEDULED MX INSPECTION DUE REJECTED T/O. PERFORMED UNSCHEDULED MX INSPECTION TYPE-A IAW M/M 05-51-0. NO DEFECTS NOTED. REFER DMI 15652 REJECTED T/O AT 110 KNOTS DUE TO SLOT LIGHT ILLUMINATED. (264 TOWEIGHT, 24 DEGREES TEMP NORMAL ZONE). FOUND NO VOLTAGE ON 22-233. ALSO VOLTAGE MISSING FROM FLAP LIMIT SWITCH S1-460. NO VOLTAGE INBOARD R/H SLOT SWITCH NEEDS TO CHECK R/H OUTBOARD SLOT SWITCH. FOUND WIRE (W250F24) DAMAGED. REPAIRED BOTH SYSTEM OPS CHECKED OK. IAW M/M 27-80-2. 2L74 4F RT4A25 20040219001722004021900172WP 2004 2 19 DHL2004807003 120040206A2760H141008 SWITCH DOUG DC8 DC873F 302199FWP SPOILER WARNING MALFUNCTIONED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01807DH 45990 REJECTED T/O AFTER T/O WARNING HORN SOUNDED AFTER ADVANCING THRUST LEVERS, WT 264.0, OAT 26 DEGREES CELSIUS, SPEED 5 KTS. (P/N: H14-1008) REMOVED AND REPLACED SPOILER T/O WARNING SWITCH PER M/M 27-63-1. OPS CHECKED OK IAW 27-63-0. PERFORM UNSCHEDULED MAINTENANCE INSPECTION DUE TO REJECTED T/O. PERFORMED UNSCHEDULED MAINTENANCE INSPECTION TYPE-A IAW M/M 05-51-0. NO DEFECTS NOTED. 2L74 4F RT4A25 20040219001742004021900174WP 2004 2 19 ABXA040059 120040128A53129915558143 STIFFENER DOUG DC9 DC941 302207NWP PRESS BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23962AX 47768 AFT PRESSURE BULKHEAD FORWARD RIGHT STIFFENER, 4TH FROM TOP, WAS CRACKED AT TEE. REPAIRED AREA IAW DC-9 SSRM K05159. 2L72 4F A6WE 20040219001772004021900177WP 2004 2 19 UPS04841836 120040206A2150 DUCT DOUG DC8 DC871F 302199DWP A/C COMPT OVERTEMP A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01752UP 45952 VERY STRONG ODOR OF FUEL IN COCKPIT THROUGH ENTIRE FLIGHT. RAN PACKS ON GROUND FOR 30 MINS, COULD NOT DETECT ANY KIND OF ODOR IN COCKPIT. SUSPECT ODOR DUE TO OVERTEMP OF DUCT, NO DEFECTS NOTED ON GROUND. 2L74 4F RT4A25 20040219001782004021900178 2004 2 19 YENA200407 420040203A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ENTERTAIN SYS FAULTY A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15563JB2524 2006 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR AROUND ROWS 12 & 13. INSPECTED ROWS 9 THRU 15 PER INFO NOTICE 2003-T050TRA, FOUND 12D VDU INOP, LIVE TV PLACED ON MEL PER 25-22-03, C/B'S ZN 1-3, ZN 1-4 OPENED. UPON ARRIVAL AT JFK PERFORMED INFORMATION NOTICE 2003-T050TRA LV TV SYS INTEGRITY CHECK CONCERNING ELEC ODOR. FOUND EVIDENCE OF ELECTRIC ODOR AND SPILL AT SEB 13R. REMOVED AND REPLACED SEB IAW LV TV AMM 23-39-00. SYSTEM CHECK OK. 2L72 4F RTA28NM 20040219001792004021900179NM 2004 2 19 CALA0400073 120040203A5320 SUPPORT BOEING737 7373T0 1384582NM THRESHOLD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND R-1 DOOR THRESHOLD SUPPORTS CORRODED AT STA 300-326. THE SUPPORTS WERE REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040219001802004021900180NM 2004 2 19 CALA0400074 120040205A5330 SKIN BOEING757 757324 1384930NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2774856 32815 THE FUSELAGE SKIN WAS PUNCTURED BETWEEN BS 1380 AND BS 1400 AT S28R-29R. THE SKIN WAS REPAIRED IAW ECRA 5331-01137. 2L72 4F RTA2NM 20040219001822004021900182NM 2004 2 19 CALA0400076 120040205A5347 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FORWARD ENTRY SEAT TRACK CORRODED FROM STA 270-294.5, RBL 40. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040219001832004021900183NM 2004 2 19 CALA0400077 120040205A5320 SUPPORT BOEING737 7373T0 1384582NM THRESHOLD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND L-1 DOOR THRESHOLD SUPPORTS CORRODED. INNER AND OUTER THRESHOLD SUPPORTS WERE INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040219001842004021900184NM 2004 2 19 CALA0400078 120040206A5330 SKIN BOEING737 737524 1384721NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714655 28916 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887-907, S26R. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2L72 4F RTA16WE 20040219001932004021900193NM 2004 2 19 04FDEA00318 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75242. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS 2L73 4F RTA22WE 20040219001962004021900196NM 2004 2 19 04FDEA00321 120040205A5711ARB74054 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - UPPER SURFACE IN SPAR AREA BETWEEN XORS 264 TO XORS 298 FOUND WITH CORROSION. CORROSION ON RH WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 264 TO XORS 298, STR 12 TO STR 13 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN LIMITS AS PER SRM 57-10-00, FIG. 32, VOL. I. 2L73 4F RTA22WE 20040219001972004021900197NM 2004 2 19 04FDEA00322 120040205A5313AFA7786503 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CENTER CARGO COMPARTMENT. LT TUNNEL LONGERON NR 34 AFT OF FRAME AT STA 1621 FOUND WITH CHAFE MARKS. COMPLIED WITH FEDEX EA 1-5310-75254. BS 1622 LONGERON 34 LT REPAIR. 2L73 4F RTA22WE 20040219001982004021900198NM 2004 2 19 04FDEA00323 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75242. WINGS, TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS 2L73 4F RTA22WE 20040219001992004021900199NM 2004 2 19 04FDEA00324 120040205A3220 CYLINDER BOEING727 727200 138407ENM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25201FE 22924 NOSE GEAR OUTER CYLINDER IS CRACKED INBOARD OF LEFT TRUNNION. C/W WITH W/C 32T2501 NOSE LANDING GEAR AND DRAG BRACE REMOVAL/INSTALL. COMPLIED WITH W/C 32T2501 REMOVED AND REPLACED NOSE LANDING GEAR ASSY AND DRAG BRACE. 2L73 4F RTA3WE 20040219002002004021900200NM 2004 2 19 04FDEA00325 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) I/B STRAP PIVOT HOLE CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREA (STRAP PIVOT HOLE) EXCEED CMM 57-52-03 LIMITATION. R & R WITH NEW HINGE ASSY AS PER DRAWING NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2L73 4F RTA22WE 20040219002012004021900201NM 2004 2 19 04FDEA00326 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2L73 4F RTA22WE 20040219002022004021900202NM 2004 2 19 04FDEA00327 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (O/B PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2L73 4F RTA22WE 20040219002032004021900203NM 2004 2 19 04FDEA00328 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT I/B FLAP O/B HINGE (FLAP SIDE) O/B STRAP PIVOT HOLE & LUG CORRODED. RT I/B FLAP O/B HINGE (FLAP SIDE) REWORKED AREAS (O/B STRAP PIVOT HOLE & LUG SURFACE) EXCEED CMM 57-52-03 LIMITATION. REMOVED & REPLACED WITH NEW HINGE ASSY AS PER DWG NRC6060. REF SNRM N0763 FOR JOB DETAILS. 2L73 4F RTA22WE 20040219002062004021900206NM 2004 2 19 04FDEA00334 120040206A3350 POWER SUPPLY BOEING727 727200 138407ENM EMERGENCY LIGHT INOPERATIVE A FDEAK NONE L NO TEST ININSP/MAINT 1 SO25469FE 21581 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY IN EMERGENCY EXIT LIGHT PER 727-200 MM 33-50-121-2. OPS CHECK GOOD, AIRCRAFT OK TO CONTINUE. 2L73 4F RTA3WE 20040219002072004021900207WP 2004 2 19 AALA20040183 120040205A335060030451 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21428AA 49340 CEILING EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040219002092004021900209WP 2004 2 19 AALA20040185 120040205A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21441AA 49460 DEN - OVERHEAD EMERGENCY LIGHT AT SEAT 4 AND 5B INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT 4 AND 5B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040219002102004021900210WP 2004 2 19 AALA20040186 120040205A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21466AA 49596 DEN - EMERGENCY LIGHTS AT FORWARD OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK AT B5-103 FOR EMERGENCY LIGHTS AT FORWARD OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040219002112004021900211NM 2004 2 19 AALA20040187 120040204A2121 FAN BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21394AN 29431 MIA INFLIGHT, THREE AND ONE HALF HOURS INTO FLIGHT SMELLED BURNING SMELL AND NOTICED SMOKE COMING FROM UNDER THE GLARESHIELD. TURNED OFF UTILITY BUSSES AND RECIRCULATING FANS AND SMOKE DISSIPATED. NO EICAS OR OTHER INDICATIONS. REMAINDER OF FLIGHT WAS NORMAL. FOUND FORWARD EXHAUST FAN FAULTING BREAKER. REPLACED FORWARD EXHAUST FAN. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2L72 4F RTA1NM 20040219002142004021900214NM 2004 2 19 QXEA200400104 120040131A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - NR 5 SEAT TRACK INBOARD FLANGE HAS A CHAFE AT X434. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-26. 2H72 4T RTA13NM 20040219002172004021900217NM 2004 2 19 QXEA200400108 120040128A5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - CRACK AT CLIP STRINGER 4 AND FRAME 4 AT REAR FUSELAGE CEILING. REPAIRED IAW RD 8-55199. 2H72 4T RTA13NM 20040219002242004021900224NM 2004 2 19 QXEA200400110 120040201A5310 STRUCTURE DHAV DHC8 DHC8202 2809007NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - AREA OF NICKS, SMALL DENTS AFT OF RIGHT NOSE GEAR, 6 INCHES TO 40 INCHES AFT OF NOSE WHEEL WELL. REPAIRED IAW DHC-8-200 SRM 51-80-26. 2H72 4T RTA13NM 20040219002252004021900225NM 2004 2 19 QXEA200400116 120040204A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - FRONT PART OF FLOOR TRACK LIGHTING AT ROW 1 IS BROKEN. REMOVED AND REPLACED STRIP TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040219002272004021900227EU 2004 2 19 189301 120040206A7720 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE COCKPIT ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL17140CQ 140 463 ON 02-06-04, APPROX 1500 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON. 2L72 4T4 TRTA52EU E8NE6 20040219002292004021900229SO 2004 2 19 C2XA04TY031 120040206A531514521721005 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY FLOOR SUPCORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717513 145292 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE DIGITAL IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040219002362004021900236NM 2004 2 19 F3LA200400007 120040205A5320 PANEL BOEING737 7373S1 138447SNM CARGO BAY CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED TRANSITION PANEL IN FWD CARGO COMPARTMENT CRACKED AT NUT PLATE HOLE, STA 430 + 11, BL 24R. FABRICATED AND INSTALLED NEW TRANSITION STRIP PER SRM 51-40-02. 2L72 4F RTA16WE 20040219002372004021900237 2004 2 19 304AW0003 420040208A2210R1053M182 RELAY BOEING737 7373G7 1384595NM LIMITER CLUTCH STICKING A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05304AW 24011 CREW REPORTED THAT THE AUTOPILOT COMMAND-A WILL NOT ENGAGE UNLESS COMMAND-B IS ENGAGED FIRST. REPLACED AILERON FORCE LIMITER CLUTCH RELAY DUE TO STICKING. CHECKS OK PER MM 22-11-13. 2L72 4F RTA16WE 20040219002392004021900239SO 2004 2 19 C2XA04BT018 120040205A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714542 145547 DURING ROUTINE INSPECTION, MAINTENANCE FOUND LEFTHAND WING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED LEFTHAND WING EMERGENCY LIGHT IAW EMB145 MM 33-50-10, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040219002402004021900240NM 2004 2 19 F3LA200400008 120040205A5313 STRINGER BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AFT OF STA 727A, RT MID STRINGER. REPAIRED AFT CARGO COMPARTMENT FLOORBEAM PER SRM 53-00-53 FIG 201. 2L72 4F RTA16WE 20040219002432004021900243NM 2004 2 19 QXEA200400118 120040206A2760 SPOILER BOMBDRDHC8 DHC8401 1390041NM MALFUNCTIONED A QXEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM09409QX 4051 CREW NOTED A PARTIAL RIGHT INBOARD SPOILER DEPLOYMENT DURING CRUISE FLIGHT. THERE WAS FULL RIGHT INBOARD SPOILER DEPLOYMENT ON FINAL APPROACH. ON GROUND, THE SPOILERS WERE NORMAL. THERE WERE NO INDICATIONS OR CAUTION LIGHTS DURING CRUISE OR APPROACH. THE LANDING WAS UNEVENTFUL. THE AIRCRAFT IS CURRENTLY DOWN FOR MAINTENANCE AND THE SDR WILL REMAIN OPEN PENDING FINAL CORRECTIVE ACTION. 2H72 4T RTA13NM 20040219002452004021900245NM 2004 2 19 CALA0400082 120040206A5420 ATTACH ANGLE BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND A .5 INCH CRACK IN ATTACH ANGLE I/B OF NR 2 PYLON JUST AFT OF MIDSPAR ATTACH BOLT. REPAIRED ANGLE IAW SRM 51-70-12. 2L72 4F RTA16WE 20040219002462004021900246NM 2004 2 19 CALA0400083 120040206A5320 ATTACH ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 4 INCH CRACK IN ANGLE ON TOP OF INTERCOSTAL BETWEEN STA 380 AND 400, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-30-51. 2L72 4F RTA16WE 20040219002492004021900249WP 2004 2 19 CALA0400086 120040207A5720 BRACKET DOUG DC9 DC981 3022081WP LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716883 48073 INSPECTION FOUND LT WING X-SUPPORT BRACKET AT T/E BETWEEN UPPER AND LOWER PANELS O/B OF GROUND SPOILER ACTUATOR CRACKED AT STA XW 99.016. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-05. 2L72 4F A6WE 20040219002502004021900250NM 2004 2 19 CALA0400087 120040207A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006-1016. REPAIRED IAW BOEING DRAWING 65-45776. 2L72 4F RTA16WE 20040219002512004021900251NM 2004 2 19 CALA0400088 120040208A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND STRINGER 8R CRACKED AT FIVE ADJACENT FASTENERS AT FRAME BS 380. THE CRACKS WERE .75 INCH LONG. A STRINGER PLATE WAS INSTALLED WITH LOCK FASTENERS IAW SRM 51-40-02. 2L72 4F RTA16WE 20040219002532004021900253NM 2004 2 19 CALA0400090 120040208A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND STRAP I/B OF C-2 DOOR THRESHOLD CORRODED FROM STA 787 TO 847 IN AFT BAG BIN. REPLACED STRAP IAW SRM 51-40-02. 2L72 4F RTA16WE 20040219002552004021900255NM 2004 2 19 CALA0400092 120040209A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND STRINGER 25L CORRODED BETWEEN STRINGER END FITTING FORWARD OF STA 1016. A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, PAGE 206. 2L72 4F RTA16WE 20040220000022004022000002NM 2004 2 20 QXEA200400119 120040206A2131 CONTROLLER BOMBDRDHC8 DHC8401 1390041NM CABIN PRESSURE MALFUNCTIONED A QXEAO OTHER O OTHER DEDESCENT 1 NM09413QX 4060 AIRCRAFT LOST PRESSURIZATION WHILE INBOUND FOR BOI WHILE AT 8000 MSL. CABIN CLIMBED AT 3000+ FT PER MINUTE UNTIL DIFFERENTIAL WAS CLOSE TO ZERO. MAINTENANCE C/W PRESSURIZATION CHECK IAW THE Q00 AMM AND THE SYSTEM OPERATED NORMALLY. NO DOOR LEAKS OR LEAKS OF ANY KIND WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040220000032004022000003EA 2004 2 20 COMA0460118 120040203A5330601R53211801 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BENT A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 PREVIOUS REPAIR TO LEFT SIDE FUSELAGE SKIN HAS SUBSTAINED FURTHER DAMAGE. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED REPAIR DOUBLER AND FILLER, FABBING NEW REPAIR DOUBLER AND FILLERS FROM 2024T3-050 PO 29672 AND 2024T3.063 PO 16956 AND INSTALLED REPAIR PARTS. ALL WORK DONE IAW BOMBARDIER INC REO 601R-53-21-180 REV NC DATED 25 AUG 98. 2L72 4F RTA21EA 20040220000042004022000004EU 2004 2 20 MALA040167 120040204A5270 WARNING LIGHT SAAB SF340 340B 7860101EU PAX DOOR ILLUMINATED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15443XJ 340B443 DURING FLIGHT 3021/3022/3092 MAIN DOOR HANDLE CAUTION LIGHT W/DOOR INDEX THAT DID NOT LINE UP. AIR RETURN TO MSP. MAINTENANCE PRESSURIZED AIRCRAFT & COULD NOT DUPLICATE PROBLEM. CLEANED & LUBRICATED INTERNAL HANDLE GEAR SEGMENT & PINION. PERFORMED OPS TEST OF PAX DOOR IAW AMM 52-10-00. OPS TEST GOOD. PERFORMED MAIN DOOR WARNING OPS TEST IAW AMM 52-70-00. OPS TEST GOOD. VERIFIED CORRECT POSITIONING OF ALIGNMENT MARKS WITH HANDLE IN CLOSED POSITION. 2L72 4T RTA52EU 20040220000052004022000005EU 2004 2 20 MALA040170 120040205A3010 BOOT SAAB SF340 340B 7860101EU DE ICE SYSTEM DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15410XJ 340B410 DURING FLIGHT 3161, DEICE TIMER LIGHT ILLUMINATED, STABILIZER INOP IN MANUAL MODE. AIR RETURN TO MEM. MAINTENANCE REPLACED DEICE BOOT ON RT HORIZONTAL LEADING EDGE IAW SF340 AMM 30-10-35-4. ALSO RE-INSTALLED LEADING EDGE IAW 55-10-05-04. PERFORMED OPS CHECK. ALL CHECKS GOOD. SEE 409 180780 FOR DETAIL. 2L72 4T RTA52EU 20040220000072004022000007NE 2004 2 20 MALA040169 220040205A7530216118218 BLEED BAND BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15505XJ E2313 DURING FLIGHT 3674/3411, NR 4 ENGINE TEMP 613 DEGREES, NG, 7 PERCENT BELOW OTHERS ENGINE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 4 ENGINE BLEED BAND REF EO A72023 FOR DETAILS (P/N 2-161-182-18) (S/N ON 03246371277) (P/N OFF 2-161-182-01) (S/N OFF UNK). OPS CHECK GOOD . 2H74 4F4 FRTA49EU E6NE 20040220000082004022000008EU 2004 2 20 MALA040172 120040205A35201018090 SWITCH BAC 146 AVRO146RJ85A1500097EU OXYGEN SYSTEM FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15522XJ E2347 DURING FLIGHT 3667/3409 WHILE DESCENDING FROM 11,000 FT TO 10,000 FT ALL 02 MASKS DROPPED OUT, PRESSURIZATION WAS WORKING NORMAL INDICATING A LANDING OF ABOUT 1,400 FT. OVERRIDE SWITCHES WERE NOT ACTIVATED, NO CABIN HI ALT ANNUNCIATOR WAS INDICATED. MAINTENANCE REMOVED AND REPLACED O2 GENERATOR AND SWITCH, REMOVED AND REPLACED ANEROID SWITCH P/N 101809-02 9824176A, S/N OFF 09218, IAW 35-20-35 AND 02 GENERATOR P/N 9903976, S/N OFF 00616, S/N ON 117028-03, IAW JC 0501, REMOVED FROM DMR MXC NOTIFIED. 2H74 4F RTA49EU 20040220000092004022000009EU 2004 2 20 MALA040173 120040205A3040 RELAY BAC 146 AVRO146RJ85A1500097EU SCREEN HEAT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15534XJ E2370 DURING FLIGHT 3500/3556/3542/3477, RT SCREEN HIGH TEMP LIGHT ON AND THE NR 2 ADC FAILED. AIR RETURN TO DTW. MAINTENANCE VERIFIED WIRES INSTALLED CORRECT. CHECKED RES AT ELEMENTS & THERM. CHECKED OUTPUT VOLT FROM NET FILTERS. CHECKED SYS WIRING. ALL CHECKS GOOD. REPLACED RELAYS 2HL14 & 2HL15, BOARD CAPACITOR 2HL23, & PCB 2HL18. PERFORMED SCREEN HEAT OPS TEST IN BOTH GROUND & AIR MODE. CHECKS GOOD. REF MM409 066888. 2H74 4F RTA49EU 20040220000102004022000010EU 2004 2 20 MALA040176 120040129A5330 SKIN SAAB SF340 SF340A 7850100EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 DURING INSPECTION IN LCQ, TCAS ANTENNA SKIN MATING SURFACE HAS EXFOLIATION CORROSION AND DOUBLER IS DISBONDING. MAINTENANCE REMOVED CORROSION FROM SKIN MATING SURFACE, REMOVED AND REPLACED TCAS ANTENNA DOUBLER AND INSTALLED REPAIR DOUBLER IAW MESABA, EO S53198. A/C RELEASE DATE 2/5/2004. 2L72 4T RTA52EU 20040220000112004022000011EU 2004 2 20 MALA040178 120040129A5347 SEAT TRACK SAAB SF340 SF340A 7850100EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 DURING INSPECTION IN LCQ, LT O/B SEAT TRACK STA 686 HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 2/5/04. 2L72 4T RTA52EU 20040220000122004022000012EU 2004 2 20 MALA040177 120040129A5321 FLOOR PANEL SAAB SF340 SF340A 7850100EU COCKPIT CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 DURING INSPECTION IN LCQ, RT STA 176.1 CO-PILOT COCKPIT FLOOR CORRODED HEAVILY. MAINTENANCE REMOVED CORRODED AREA AND INSTALLED DOUBLER REPAIR IAW MESABA EO S53197. A/C RELEASE DATE 2/5/2004. 2L72 4T RTA52EU 20040220000152004022000015EA 2004 2 20 COMA0460121 120040202A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR DIRTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01467CA 7637 FLIGHT 5008 GEAR DISAGREE WARNING, NLG DID NOT INDICATE DOWN. CLEANED DIRT FROM NLG PROXIMITY SENSORS. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040220000192004022000019 2004 2 20 UPS04141852 420040206A2565 GIRT BAR AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE DETACHED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01134UP 0818 MAIN ENTRY DOOR SLIDE EMERGENCY ESCAPE SLIDE RELEASE MECHANISM SLIDER & GIRT BAR DETACHED FROM DOOR. GRIT BAR HANGING FROM SLIDE ASSY. RE-ATTACHED GRIT BAR & SLIDER TO ESCAPE SLIDE PER MM 52-10-30-4 (6), OK FOR CONTINUED SERVICE. 2L72 4F RTA35EU 20040220000202004022000020EU 2004 2 20 UPS04141853 120040206A2611 SMOKE DETECTOR AIRBUSA300 A300F4622R 3930360EU E/E BAY INTERMITTENT A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01138UP 0821 INSPECTION TYPE:N/A AVIONICS SMOKE INTERMITTENTLY. REMOVED AND REPLACED MAIN BAY SMOKE DETECTOR 11 IAW 26-15-124, OPS CHECK GOOD. 2L72 4F RTA35EU 20040220000242004022000024WP 2004 2 20 UPS04841820 120040104A523037551721N FITTING DOUG DC8 DC873F 302199FWP C1 DOOR GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, FWD PIT CROSS-SLIDE DOOR T-BOLT FITTINGS GOUGED 6 EACH. BLENDED OUT LATCH FITTING IAW DC8 SRM 51-1-8 OUT OF LIMITS IAW DAC DWG 3754051. RECEIVED, LOCATED, & DRILLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-24 AND 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED 6 EACH LATCH FITTINGS IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-0. 2L74 4F RT4A25 20040220000262004022000026WP 2004 2 20 UPS04841822 120040105A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING NICKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, LEFT WING L/E HAS NICKS AT XFS114. REMOVED DAMAGED AREA IAW REO G09663, FABBED NEW DOUBLER FILLER IAW REO G09663, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-27. 2L74 4F RT4A25 20040220000272004022000027WP 2004 2 20 UPS04841823 120040106A5330 DOUBLER DOUG DC8 DC873F 302199FWP L1 DOOR MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, L1 DOOR UPPER FWD CORNER REPAIR IS NOT PER SRM. REMOVED EXISTING DOUBLERS ABOVE L1 DOOR UPPER FWD CORNER IAW DC8 SRM 51-1-21. FABBED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED -15 & -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 15, TR 53-182 AND DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040220000292004022000029WP 2004 2 20 UPS04841825 120040106A531037735121 DOOR FRAME DOUG DC8 DC873F 302199FWP R2 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, R2 DOOR UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER AND L1 1R, FOUND BY RADIOGRAPHY. FAB DOUBLERS & FILLERS -19, -21, -23, & -25 IAW DC8 SRM 53-2-0. TRIMMED EXTERIOR SKIN AND INTERNAL DOUBLER IAW DC8 SRM 53-2-0 TR 130. REMOVED DAMAGED L 11RT STA 1570-1700. RECEIVED, LOCATED, & DRILLED NEW LONGERON P/N 377351 2-1, INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21. ALODINED, PRIMED & INSTALLED IAW DC8 SRM 53-2-0 TR130, TR183 AND REO G09643. 2L74 4F RT4A25 20040220000312004022000031WP 2004 2 20 UPS04841827 120040108A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, SEAT TRACK CRACKED AT STA 145. BLENDED CRACKED SEAT TRACK IAW DC8 SRM 53-2-3, OUT OF LIMITS IAW DC8 SRM 53-2-3 AND 53-2-0. REMOVED DAMAGED SEAT TRACK IAW DC8 SRM 51-3-0 & 51- 3-1. LOCATED, DRILLED NEW SEAT TRACK AND SPLICE IAW DC8 SRM 53-2-3. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK SPLICE IAW DC8 SRM 51-3-0 & 51-3-1. 2L74 4F RT4A25 20040220000332004022000033WP 2004 2 20 UPS04841829 120040110A53205645332109 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, STA 900 RT CUSP AREA WEB HAS SIGNS OF CORROSION. FOUND FINGER DOUBLER & WEB OUT OF LIMITS; CORROSION ON FLOORBEAM FS 879 FOUND DURING CORROSION REMOVAL. CUTOUT -3 WEB; REMOVED CORROSION ON FLOORBEAM (IN LIMITS); DYE PEN PANEL (NO CRACKS); FABBED 2EA FINGER DOUBLERS, 2EA INTERNAL SPLICES, 1EA F ILLER, 1EA EXT DOUBLER FOR WEB REPAIR. ALODINED & PRIMED; INSTALLED REPAIR; ALL IAW REO G09650, SRM 53-2-0, 51-1-8, 51-1-20D, 51-1-21, DWG 5645332, ASTM 1417. 2L74 4F RT4A25 20040220000342004022000034WP 2004 2 20 UPS04841830 120040110A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1540 L27L CORROSION ON UNDERSIDE OF FLANGE. REMOVED FITTING IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED NEW FITTING AND DRILLED EXISTING HOLES IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20040220000362004022000036WP 2004 2 20 UPS04841832 120040110A532037592221N SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1260-1280 LONG 36 SPLICE CORROSION CENTER OF SPLICE PLATE. REMOVED SPLICE PLATE IAW DC8 SRM 51-3-0 AND 51-1-20D. RECEIVED NEW FITTING SPLICE P/N 3759222-1N PO 0, LOCATED AND DRILLED IAW DC8 SRM 51-3-0 AND 51-1-20D. INSTALLED FITTING SPLICE IAW DC8 SRM 51-3-0 AND 51-1-20D. 2L74 4F RT4A25 20040220000382004022000038WP 2004 2 20 UPS04841834 120040115A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, REMOVED BATHTUB FITTING AT STA 879 AND FOUND THE SKIN UNDER FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 AND 53-4-1. MATERIAL ID FOR FILLER IAW REO G09662, FABBED FILLER IAW REO G09 662. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER IAW REO G09662. 2L74 4F RT4A25 20040220000392004022000039WP 2004 2 20 UPS04841835 120040124A5310 BEAM DOUG DC8 DC873F 302199FWP C1 DOORWAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, FWD PIT C1 DOOR JAMB CORNER TORQUE BOX BEAM IS CORRODED BEHIND T-BOLT LATCHES. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION FOUND WITHIN LIMITS IAW DAC DWG 9754007, REO G09673. MAT ID FOR SHIM 4340 STEEL BAR PO 371199.1 IAW REO G0967 3, FABRICATED SHIM IAW REO G09673, PRIMED SHIM IAW DC8 SRM 51-1-8, INSTALLED SHIIM IAW REO G09673. 2L74 4F RT4A25 20040220000402004022000040WP 2004 2 20 UPS04841843 120040201A5730 DOUBLER DOUG DC8 DC871F 302199DWP RT WING LE. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5760545 AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20040220000412004022000041WP 2004 2 20 UPS04841844 120040203A57513653812 BRACKET DOUG DC8 DC871F 302199DWP RT OB AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT O/B AILERON HINGE BRACKET IS CRACKED AT STATION 610.882. REMOVED AND REPLACED BRACKET IAW DWG 3653812 AND SRM 51-1-21. 2L74 4F RT4A25 20040220000422004022000042WP 2004 2 20 UPS04841845 120040130A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB IS CRACKED AT XS 491. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040220000432004022000043WP 2004 2 20 UPS04841846 120040131A534037739061 SUPPORT FITTING DOUG DC8 DC871F 302199DWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 822 RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D. 2L74 4F RT4A25 20040220000492004022000049NM 2004 2 20 UPS04M41838 120040124A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-919 X=-8.5. CORROSION REMOVED AT SEAT TRACK AT STA 805-909 FOUND EXCEED LIMIT PER SRM 53-70-00 VOL I FIG 3 REV 34. NEW SEAT TRACK & SPLICE INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I REV 34 AT STA 800-909 X=-8.5. CORROSION REMOVED AT SEAT TRACK AT STA 909-919 X=-8.5 MAT REMOVED 0.00 6, ORIGINAL THK 0.112 WITHIN LIMIT OF SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000522004022000052WP 2004 2 20 ABXA040060 120040129A5340AND0101332001 ATTACH ANGLE DOUG DC9 DC932 3022066WP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23901AX 47381 AFT SIDE OF UPPER HORIZONTAL ATTACH ANGLE AT FS 996 EXFOLIATED AT LEFT BUTT LINE 6, RIGHT BUTT LINE 6, AND RIGHT BUTT LINE 10. REPAIRED ATTACH ANGLE IAW DC-9 SSRM, WITHIN LIMITS IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040220000562004022000056NM 2004 2 20 AWXA200400160 120040207A2560P20700012015 FLASHLIGHT AIRBUSA319 A319132 3930340NM ZONE 900 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28820AW 1397 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040220000572004022000057NM 2004 2 20 AWXA200400161 120040121A53306552988 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK A .5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT L-2 DOOR LOWER HINGE CUTOUT BS 954, STR 14 LT. MAINTENANCE TRIMMED OUT CRACK AT L-2 DOOR LOWER HINGE CUTOUT, BS 954, STR 14 LT; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-04033-SS1. 2L72 4F RTA16WE 20040220000592004022000059WP 2004 2 20 AALA20040203 120040206A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT PINCHED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21588AA 53251 DFW EMERGENCY EXIT DOUBLE ARROW LIGHT ASSEMBLY ON FORWARD GALLEY AISLE WALL NEAR FLOOR INOPERATIVE. FOUND WIRE PINCHED BEHIND ONE OF CONNECTORS. CUT OFF PINCHED WIRE AND REINSTALLED CONNECTOR FOR EMERGENCY EXIT LIGHT AT FORWARD GALLEY WALL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040220000642004022000064NM 2004 2 20 AALA20040193 120040207A3350 BATTERY PACK BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21321AA 22322 DFW RIGHT HAND OVERWING EMERGENCY LIGHTS AND RIGHT HAND FORWARD SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND OVERWING EMERGENCY LIGHTS AND RIGHT HAND FORWARD SLIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040220000672004022000067NM 2004 2 20 AALA20040197 120040206A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21949AN 29537 RNO RIGHT HAND UPPER EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND UPPER EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040220000702004022000070NM 2004 2 20 AALA20040198 120040206A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21619AA 24577 MIA SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR SEAT MOUNTED EMERGENCY LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220000722004022000072WP 2004 2 20 AALA20040191 120040208A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 SAT OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000742004022000074NM 2004 2 20 AALA20040205 120040208A2822 PUMP BOEING737 737823 13844BZNM ZONE 700 INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21964AN 30093 MIA BOTH CENTER FUEL BOOST PUMPS LOW PRESSURE LIGHTS ILLUMINATED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PRIMED BOTH PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040220000782004022000078EA 2004 2 20 SWIA200412850 120040203A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT LBL 9.0 HAS A CRACKED INBOARD ATTACH ANGLE AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM. 2L72 4F RTA21EA 20040220000792004022000079EA 2004 2 20 SWIA200412851 120040203A5315601R3111358 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07919SW 7657 DURING C-CHECK INSPECTION, MAIN FUSELAGE FLOORBEAM AT RBL 9.0 HAS INBOARD AND OUTBOARD ATTACH ANGLES CRACKED AT FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM. 2L72 4F RTA21EA 20040220000812004022000081SO 2004 2 20 SWIA200412853 120040127A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07187SW6477 6477 120037 FLAP CONTROL FAULT, DISAGREE, AND ASYM MESSAGE OVERHEAD FLAP AND ADVANCED SWS ON MAP STAY ON. INSTALLED A SERVICEABLE FLAP ANNUNCIATOR IAW 27-50-05. OPS CHECK GOOD. REMOVED AND REPLACED FLAP CONTROL UNIT. P/N OFF: 347200-1001, SN OFF: 0194. 2L72 4T RTA31SO 20040220000852004022000085SO 2004 2 20 SWIA200412857 120040203A771230005000053 SIGNAL COND UNIT EMB 120 EMB120ER 3260203SO ENG TORQUE MALFUNCTIONED A SWIAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 NM07221SW7010 5573 120290 ON APPROACH, LEFT ENGINE HAD UNCOMMANDED AUTOFEATHER. TORQUE REACHED 115 PERCENT. REPLACED TORQUE SENSOR, SIGNAL CONDITIONER AND EEC HARNESS WITH SERVICEABLE UNIT IAW EMB-120 MM 73-22-00. OPS CHECKS GOOD. TORQUE SENSOR P/N OFF: 3105076-01. 2L72 4T RTA31SO 20040220000862004022000086SO 2004 2 20 LR7A04002 120040124A5330 SKIN LKHEED382 382G 526414USO FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RT FUSELAGE SKIN WARPED & BUCKLED FROM FS 777E TO 817E WL 142-170 AND 3 PATCH REPAIR EXISTING AT FS 807E-817E; WL 200-250. SKIN REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 777E - FS 817E WL 142 - WL 170 RBL 62. 2H74 4T A1SO 20040220000892004022000089SO 2004 2 20 LR7A04005 120040124A5330 SKIN LKHEED382 382G 526414USO FUSELAGE PUNCTURED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND FUSELAGE SKIN CRACKED/PUNCTURED AT FS 812 WL 160 LT FUSELAGE EXTERIOR SURFACE. REPAIR CARRIED OUT IAW SMP583 CHP 51-140-12, FS 812 WL 160 LBL 82. 2H74 4T A1SO 20040220000942004022000094SO 2004 2 20 LR7A04010 120040124A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND CRACK AROUND 10 O'CLOCK POSITION OF PRESSURIZATION VALVE AT CARGO DOOR LOWER SURFACE. SKIN DOUBLER FABRICATED AND INSTALLED IAW SMP583 CHP 51-60 & 51-70, FS 1004 LBL 56. 2H74 4T A1SO 20040220000952004022000095SO 2004 2 20 LR7A04011 120040124A5343 WEB LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND NWW AT FS 196 WL 140 BL 28L HAIRLINE CRACK AT AFT DOOR ARM FITTING ATTACHMENT. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-17, FS 196 WL 140 LBL 28. 2H74 4T A1SO 20040220000962004022000096SO 2004 2 20 LR7A04012 120040124A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND FWD FUSELAGE LOWER SKIN INDENT EXCEED LIMIT AT FS 235 BL 20L/R AT NLG AFT DOOR LOWER DOOR BUMPER PAD. DRESSED UP DENTS IAW SMP583 CHP 51-140 PG 22 & DOUBLERS QTY 2 EA REPLACED IAW CHP 51-60 & 51-70, FS 235 RBL 20 LBL 20. 2H74 4T A1SO 20040220001002004022000100SO 2004 2 20 LR7A04016 120040124A5230 GUSSET LKHEED382 382G 526414USO MCD BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5211 FOUND CARGO DOOR INTERIOR BULKHEAD GUSSET (DOUBLER) CRACK AT FS 994 BL 60L. GUSSET REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 994 LBL 60. 2H74 4T A1SO 20040220001012004022000101SO 2004 2 20 LR7A04017 120040124A5311 FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5317 FOUND CABIN FRAME FLANGE CRACK AT FS 477-497 BL 16.5R WL 285. FRAME REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 477-FS 497 WL 285 RBL 16.5. 2H74 4T A1SO 20040220001022004022000102SO 2004 2 20 LR7A04018 120040124A5312 TEE FITTING LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND FS 477 CABIN OVERHEAD BULKHEAD TEE CRACK AT BL 0-8R. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-22, FS 477 WL 285 LBL 8 - LBL 10. 2H74 4T A1SO 20040220001032004022000103SO 2004 2 20 LR7A04019 120040124A55223539381L SKIN LKHEED382 382G 526414USO LT ELEVATOR NICKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND LT ELEVATOR T/E SKIN FOUND WARPED, NICKS WITH QTY 2 EA PATCHES EXISTING AT I/B SIDE. T/E SKIN REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT. 2H74 4T A1SO 20040220001062004022000106SO 2004 2 20 LR7A04022 120040124A5522 STRAP LKHEED382 382G 526414USO LT ELEVATOR BROKEN A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND AFTER T/E SKIN REMOVAL INNER STRAP BROKEN AT HSS77 LT ELEVATOR. STRAP REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT. 2H74 4T A1SO 20040220001072004022000107SO 2004 2 20 LR7A04023 120040124A5521 RIB LKHEED382 382G 526414USO ELEVATOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND AFTER T/E SKIN REMOVAL, RIB FORMER CRACKED AT HSS77 LT ELEVATOR. RIB FORMER REPLACED IAW SMP583 CHP 51-60 & 51-70, HSS77 LT. 2H74 4T A1SO 20040220001112004022000111WP 2004 2 20 04FDEA00377 120040209A54103110M24P001A BRACKET DOUG DC10 DC1010 3022110WP NR 3 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 NR 3 ENGINE I/B TRAILING EDGE LOWER BALL SCREW G/B SUPPORT BRACKET IS CRACKED. REMOVED DAMAGED BRACKET IAW SRM 51-35-01. RECEVIED NEW BRACKET P/N 311OM24POO1A. LOCATED AND DRILLED IAW SRM 51-31-01. INSTALLED BRACKET ACTUATOR IAW SRM 51-31-01 AND 51-31-01. 2L73 4F A22WE 20040220001172004022000117NM 2004 2 20 04FDEA00354 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE O/B STRAP PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE O/B STRAP PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001182004022000118NM 2004 2 20 04FDEA00353 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001232004022000123NM 2004 2 20 04FDEA00348 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75249. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040220001282004022000128NM 2004 2 20 04FDEA00339 120040206A5711ARB74054 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 455 TO XORS 506. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 455 TO XORS 506 CORROSION REMOVED AND REPAIR CARRIED OUT AS PER SRM 51-21-01 VOL. II. 2L73 4F RTA22WE 20040220001362004022000136EU 2004 2 20 04019314 120040119A2897 WIRE JETAIRJETSTMJETSTM4101 1500501EU LT FUEL PROBE CHAFED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27314UE 41027 DURING INSPECTION THE LEFT HAND WING FUEL PROBE WIRING AT RIB 16 WAS FOUND TO BE CHAFING. THE INSULATION AND WIRE WERE RESECURED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4T RTA41NM 20040220001392004022000139EU 2004 2 20 04029303A 120040129A5320 ANGLE JETAIRJETSTMJETSTM4101 1500501EU FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 DURING HEAVY INSPECTION THE ANGLE BRACKET A STATION 4, 4 O`CLOCK POSITION WAS FOUND CRACKED. A NEW BRACKET WAS INSTALLED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4T RTA41NM 20040220001402004022000140EU 2004 2 20 04029303B 120040129A5320 INTERCOSTAL JETAIRJETSTMJETSTM4101 1500501EU FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27303UE 41015 DURING INSPECTION THE INTERCOSTAL AT STATION 4, 11O`CLOCK POSITION WAS FOUND CRACKED. A NEW INTERCOSTAL WAS INSTALLED AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4T RTA41NM 20040220001512004022000151EA 2004 2 20 04028622 120040128A339764641 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27622BR 7187 DURING INSPECTION THE FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE CABLE ASSEMBLY WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040220001522004022000152EA 2004 2 20 COMA0460130 120040206A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01937CA 7044 FLIGHT 5685 LEFT THRUST REVERSER UNLOCK MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040220001532004022000153EA 2004 2 20 COMA0460129 120040206A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01991CA 7216 FLIGHT 5530 FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE NR 2 INVERTER. 2L72 4F RTA21EA 20040220001562004022000156NM 2004 2 20 04FDEA00373 120040209A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON STR 24L BS 306. REMOVED DAMAGE ON STR 24L BS 306. DAMAGE FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-3. 2L73 4F RTA3WE 20040220001572004022000157NM 2004 2 20 04FDEA00374 120040209A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION, STA 760 BL 0 WL 148, DELTA BEAM LWR L-ANGLE HAS CORROSION. ACCESSED DELTA BEAM WEB. REMOVED L-ANGLE AND FOUND L-ANGLE OUT OF LIMITS. FABRICATED NEW L-ANGLE, INSTALLED ANGLE AND REINSTALLED ACCESSED DELTA BEAM WEB FASTENERS AND DME NR 2 ANTENNA CLIPS. ALL WORK DONE IAW SRM 51-30-2, 51-10-2, 51-20-1. 2L73 4F RTA3WE 20040220001612004022000161NM 2004 2 20 04FDEA00382 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 FUSELAGE FRAME DENTED AT STA 5-93 BETWEEN STR 12 & 13. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENTS PER SRM - DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001632004022000163NM 2004 2 20 04FDEA00384 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CABIN LT SIDEWALL FRAME DENTED AT STA 1681 BETWEEN STR 12 & 13. CABIN LT SIDEWALL FRAME DENTED AT STA 1681 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM. DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001682004022000168EA 2004 2 20 COMA0460126 120040206A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01981CA 7163 FLIGHT 5027 FLAPS FAIL MESSAGE AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040220001692004022000169EA 2004 2 20 COMA0460125 120040205A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01814CA9886 7387 FLIGHT 5864 LT SIDE WINDOW SHATTERED. REPLACED SIDE WINDOW. 2L72 4F RTA21EA 20040220001722004022000172NM 2004 2 20 0467400018 120040102A5312 BULKHEAD BOEING747 747251F 1384898NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01640US 23888 DURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093. 2L74 4F A20WE 20040220001732004022000173EA 2004 2 20 04030675A 120040130A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 DURING INSPECTION THE RIGHT HAND EMERGENCY EXTERIOR LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001792004022000179NM 2004 2 20 CALA0400094 120040209A5312 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD LEFT AND RIGHT OF CENTER STIFFENER (APB DOME WEB) CORRODED AT STA 1016, BL 0. A REPAIR DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106. 2L72 4F RTA16WE 20040220001812004022000181NM 2004 2 20 CALA0400096 120040209A5330 SKIN BOEING757 757224 1384958NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717126 27566 INSPECTION FOUND THREE CREASES IN FUSELAGE SKIN FROM S24R - S26R, STA 1787, WL 138.5. REPAIRED IAW ECRA 5330-03323. 2L72 4F RTA2NM 20040220001842004022000184NM 2004 2 20 CALA0400099 120040210A5755 SKIN BOEING737 7373T0 1384582NM SPOILER PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND RT WING NR 6 FLIGHT SPOILER PANEL PUNCTURED IN CENTER SECTION. REPAIRED SPOILER PANEL IAW SRM 57-70-1. 2L72 4F RTA16WE 20040220001862004022000186NM 2004 2 20 AWXA200400162 120040118A5310654797332 CREASE BEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND IN CREASE BEAM AT BS 662, RBL 74. MAINTENANCE REMOVED CRACKED CREASE BEAM AT BS 662, RBL 74; FABRICATED A NEW REPLACEMENT CREASE BEAM; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02, PARA 4. 2L72 4F RTA16WE 20040220001872004022000187NM 2004 2 20 AWXA200400166 120040116A53136948948501 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT AT BS 344, AFT EDGE OF E&E BAY DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED STRINGER 28 RT FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT STRINGER CHANNEL PER DWG 69-48948; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12 PG 1 & 38. 2L72 4F RTA16WE 20040220001882004022000188EU 2004 2 20 AWXA200400167 120040130A33971703302 TERMINAL AIRBUS320 A320231 3930325EU SEAT ROW 17 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW 091 MCN - EEL - DURING C-03 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT TERMINAL BROKEN AT SEAT ROW 17 LT. MAINTENANCE REPLACED BROKEN TERMINAL FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040220001892004022000189NM 2004 2 20 AWXA200400168 120040104A55116050578 SPAR CAP BOEING737 737301 1384611NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER AFT SPAR UPPER CAP BETWEEN STAB STA 159 - 164.5. MAINTENANCE BLENDED OUT CORROSION ON LT HORIZONTAL STABILIZER AFT SPAR UPPER CAP FROM STAB STA 159 TO STAB STA 164.5; PERFORMED HFEC INSPECTION TO ENSURE DAMAGE REMOVED; FABRICATED AN EXTERNAL DOUBLER, REPAIR ANGLE, AND RADIUS FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5500-04027-SS3. 2L72 4F RTA16WE 20040220001922004022000192WP 2004 2 20 AALA20040209 120040209A4990 O-RING DOUG DC9 DC983 3022083WP APU OIL SYS LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21434AA 49452 EWR INFLIGHT T1877/09, SMOKE IN CABIN AFTER TAKEOFF. SLIGHT ODOR IN COCKPIT. FLIGHT ATTENDANT REPORTED SMOKE WAS NOT GOING AWAY. RAN CABIN FIRE SMOKE PROCEDURE AND DEPRESSURIZED CABIN TO REMOVE SMOKE. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. FOUND APU OIL LEAK INTO AIR INLET. REPLACED APU CHIP DETECTOR O-RING AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040220001932004022000193NM 2004 2 20 AALA20040208 120040209A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21677AN 29427 ORD - SEAT SIDE EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. FOUND WIRES DISCONNECTED. RECONNECTED WIRES FOR SEAT SIDE EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220001972004022000197NM 2004 2 20 QXEA200400122 120040202A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - FUSELAGE SKIN SURFACE UNDER LOWER TCAS ANTENNA HAS CORROSION. REPAIRED IAW HORIZON AIR EA 2-53-540. 2H72 4T RTA13NM 20040220001982004022000198NM 2004 2 20 QXEA200400123 120040204A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - DENT IN FUSELAGE SKIN - LEFT HAND SIDE UNDER ICE SHIELD 4 INCHES ABOVE NR 2 WINDOW. REPAIRED IAW RD 8-53-7763 AND HORIZON AIR EA 2-53-541. 2H72 4T RTA13NM 20040220002002004022000200EU 2004 2 20 04035311 120040204A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27311UE 41029 DURING INSPECTION THE AFT EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE EMERGENCY BATTERY WAS FOUND DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040220002022004022000202CE 2004 2 20 DXTA200400240 120040208A2120 ODOR RAYTHNDH125 HAWKER800XP 7150012CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07863QS 258463 DURING CLIMBOUT NOTICED ODOR OF SMOKE FROM CABIN BLEED AIR, ACCOMPLISHED AIR TURNBACK TO DEN. PERFORMED ENGINE RUNS AND APU RUNS, APPLIED BLEED AIR IN AUTO AND MANUAL, ALL INDICATIONS NORMAL. DID NOT OBSERVE THE ODOR OF SMOKE FROM CABIN BLEED AIR DUCT OR IN CABIN, ALL WORK DONE IAW HAWKER 800XP MM CHAPTER 20-00-00 STANDARD PRACTICES. 2L72 4F RTA3EU 20040319001672004031900167 2004 3 19 SWAA040718 420040307A2565D31354 SLIDE BOEING737 7373L9 1384470NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040319001692004031900169NM 2004 3 19 SWAA040720 120040306A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, WL 208 LT SIDE. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040319001882004031900188NM 2004 3 19 VNAA0403006 120040302A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ROW 4 FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07425JS 3037 THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTING AT ROW 4 WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AMBER LIGHT STRIP IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001892004031900189NM 2004 3 19 VNAA0403005 120040302A3300 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ROW 8 FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07434JS 3051 THE CREW REPORTED THAT THE ROW 8 EMERGENCY FLOOR LIGHTING WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AMBER LIGHT STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001912004031900191CE 2004 3 19 072041 120040309A1430 SCREW BEECH 1900 1900C 1154161CE ELEVATOR LOOSE A NSVAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 EA27119CJ UC19 DURING FLIGHT CONTROL CHECK, CONTROL COLUMN WOULD NOT RETURN TO FULL FORWARD POSITION. INSPECTED AND FOUND ONE SCREW MIGRATED FROM LEFT ELEVATOR, RESET SCREW AND SECURED WITH SPEED TAPE, FERRIED AIRCRAFT TO HEF, FOUND BALANCE WEIGHT ASSY AT O/B ELEVATOR L/E WITH INCORRECT SIZE SCREW. REPOSITIONED SCREWS AND SECURED PER MM 55-20-00, OP CHECKED GOOD. 2L72 4T RTA24CE 20040319001932004031900193NM 2004 3 19 VNAA0403001 120040301A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAV FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07442JS 3060 THE CREW REPORTED RECEIVING A SMOKE LAV CAS MESSAGE. MAINTENANCE THEN DEFERRED THE LAVATORY SMOKE DETECTOR PER MEL 26-3 CODE C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001972004031900197NM 2004 3 19 VNAA0402013 120040229A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07432JS 3045 THE CREW REPORTED THAT THE FIRST STRIP OF EMERGENCY FLOOR LIGHTING WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND RESECURED THE EMERGENCY FLOOR LIGHT STRIP CONNECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040322000032004032200003NM 2004 3 22 AWXA200400236 120040223A5320652981818 BRACKET BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND 2 CRACKS IN L-1 DOOR SILL ATTACH ANGLE BRACKET AT BS 302, LBL 66, WL 207.5. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL BRACKET AT BS 302, LBL 66, WL 207.5; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2L72 4F RTA16WE 20040322000072004032200007NM 2004 3 22 AWXA200400240 120040221A531565528941 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .3125 INCH CRACK WAS FOUND IN LT CENTER CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, BL -0-, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM BL -0- TO LBL 25, WL 208; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SOPM 20-50-01 FIG 1 PG 1-8. 2L72 4F RTA16WE 20040322000082004032200008NM 2004 3 22 AWXA200400241 120040303A5754 SKIN BOEING737 7373B7 1384580NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A 2 INCH CRACK WAS FOUND AT RIVET HOLE ALONG LOWER AFT EDGE OF NR 6 SLAT, SPAR STA 597. MAINTENANCE CUT OUT DAMAGE ON NR 6 SLAT AT SPAR STA 597; FABRICATED A FILLER & REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219. 2L72 4F RTA16WE 20040322000102004032200010NM 2004 3 22 AWXA200400242 120040305A3397BMS13311122 WIRE BOEING737 7373Y0 1384671NM SEAT ROW 17 LT LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE SPLICE AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040322000172004032200017NM 2004 3 22 AWXA200400247 120040222A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM ZONE 221 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28831AW8809 1576 MCN - EEL - DURING B-02 CHECK THE EMERGENCY ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE AT SEAT ROWS 1, 4 AND 20 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE L-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040322000262004032200026NM 2004 3 22 AWXA200400256 120040228A5311651630086 FRAME BOEING737 7373B7 1384580NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .75 INCH CRACK WAS FOUND IN RADIUS OF BS 178 BULKHEAD LT SIDE CHORD AT LBL 55, WL 207. MAINTENANCE REMOVED DAMAGED SECTION OF LT SIDE CHORD AT LBL 55, WL 207; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4. 2L72 4F RTA16WE 20040322000282004032200028NM 2004 3 22 AWXA200400258 120040225A53156546560 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 1016, RBL 33, WL 208. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 1016, RBL 33, WL 208; FABRICATED A REPAIR STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 203 PG 212-215. 2L72 4F RTA16WE 20040322000502004032200050NM 2004 3 22 CALA0400241 120040311A53206545834300 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND MAIN CABIN FLOOR INTERCOSTAL UPPER FLANGE CORRODED AT STA 297, RBL 32. REPAIRED IAW BOEING DRAWING 65-45834 AND SRM 51-40-02. 2L72 4F RTA16WE 20040322000672004032200067EU 2004 3 22 04066330 120040306A2612 SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT FIRE WARNING INTERMITTENT A VTZAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27330UE 41098 CREW RECEIVED A FIRE WARNING INDICATION FOR THE LT ENGINE. THERE WERE NO INDICATIONS OF AN ENGINE FIRE. THE FLIGHT RETURNED TO THE GATE NORMALLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT HAND FIRE TEST SWITCH TO BE STICKING AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICES. 2L72 4T RTA41NM 20040322000812004032200081SO 2004 3 22 C2XA04SH157 120040313A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 245 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322000822004032200082SO 2004 3 22 C2XA04SH158 120040313A531014525381003 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE LEFT BUTTSTRAP AT FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322000882004032200088NM 2004 3 22 SWAA040766 120040310A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001042004032200104NM 2004 3 22 SWAA040783 120040312A5312BAC1514 STIFFENER BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED SPV, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER ACO. 2L72 4F RTA16WE 20040322001132004032200113SO 2004 3 22 C2XA04TY051 120040313A532014525397607 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT LOWER SILL IAW EMB-135 SRM 51-40-02. 2L72 4F RTT00011AT 20040322001162004032200116NE 2004 3 22 MALA040249 220040307A7261200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 LEAKING A MALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15525XJ E2350 P07868 NR 4 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL QUANTITY AND PRESSURE. AT FL 2900 NR 4 OIL LOW PRESS LIGHT ILLUMINATED. INSPECTED NR 4 ENG FOR OIL LOSS, FOUND 12 QTS LOST. CHIP DETECTORS WERE NOT CONTAMINATED. INSTALLED 3 ENG FERRY KIT AS PER TASK CARD THREE ENGINE FERRY ON NR 4 ENG. A/C INSPECTED AND FOUND SAFE FOR 3 ENG FERRY IN METEROLOGICAL CONDITIONS ACCEPTABLE TO CREW FROM EWR TO MSP. REMOVED AND REPLACED NR 4 ENG. P/N 2-003-040-15, S/N OFF P07868, S/N ON LF07629. OPS AND LEAK GOOD. 2H74 4F4 FRTA49EU E6NE 20040322001262004032200126NM 2004 3 22 CALA0400245 120040315A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727015 28678 INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED FORWARD OF R-4 DOOR AT STA 1983, S29R-30R. REPAIRED IAW SRM 53-00-01, REPAIR 7. 2L72 4F RTT00001SE 20040322001392004032200139NM 2004 3 22 AWXA200400274 120040312A3397BR963180 WIRE HARNESS BOEING737 7373S3 1384711NM SEAT ROW 2 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 PHX - EEL - DURING INSPECTION A BROKEN SPLICE WAS FOUND ON WIRE FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 2 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040322001492004032200149NM 2004 3 22 AWXA200400284 120040301A5751 PANEL BOEING737 7373G7 1384595NM AILERON SEPARATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND THE LT AILERON LEADING EDGE PANEL LAND SEPARATING AT SECOND HINGE FROM OUTBOARD END WS 574.698. MAINTENANCE PERFORMED A BOND REPAIR ON LT AILERON LEADING EDGE PANEL LAND IAW B737-300 SRM 51-70-17 FIG 20 PG 26 & 57. 2L72 4F RTA16WE 20040322001612004032200161NM 2004 3 22 SWAA040796 120040314A53116546563 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 970, STR 7L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040322001652004032200165NM 2004 3 22 SWAA040749 120040310A212165771 BLOWER BOEING737 7373G7 1384595NM E/E BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29671SW 23785 F/A REPORTED ELECTRICAL ODOR IN CABIN. TURNING OFF RECIRC FAN ODOR ELIMINATED. REMOVED AND REPLACED RECIRC FAN BLOWER PER MM. 2L72 4F RTA16WE 20040322001712004032200171NM 2004 3 22 SWAA040755 120040309A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STRINGER 21L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001822004032200182EA 2004 3 22 COMA0460196 120040312A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01716CA 7250 FLGIHT 5710 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040322001882004032200188SO 2004 3 22 C2XA04SH161 120040316A531514522459003 FLOORBEAM EMB 145 EMB145 3260210SO FUSLEAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO BE CRACKED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE CRACKED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001912004032200191SO 2004 3 22 C2XA04SH164 120040316A531114525681007 FRAME EMB 135 EMB135LR 3260305SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE ATTACH ANGLE ON THE LOWER END OF THE T-SECTION AT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACKED ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001982004032200198NM 2004 3 22 SWAA040805 120040315A53306552988 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 911, BETWEEN STR 27L & STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322002002004032200200NM 2004 3 22 DHL2004750006 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 520. CUT OUT DAMAGE AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1, FABRICATED DOUBLER REPAIR FROM MAT 7075-T6 .063 PO 900166 DIM 9 X 3.75 INCH IAW B727 SRM 51-40-3 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR UPPER CABIN RT STA 520 BETWEEN STRINGER 16R AND 17R IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040322002022004032200202WP 2004 3 22 DHL2004809003 120040315A5740 FITTING DOUG DC8 DC873F 302199FWP RT MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 RIGHT-HAND WHEEL WELL STA 931 FALSE SPAR STA 1.50 FITTING IS CRACKED 1.50 INCH LONG FORWARD TO AFT. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTERED AS DMI 16041E. ONLY 2 REVENUE FLIGHTS WITH NOTED DAMAGE. REF. DMI NR 16041E RT WHEEL WELL STA. 931 FALSE SPAR STA. 1.50 FITTING IS CRACKED. REPLACED FITTING AND FABRICATED PER ASTAR EA 5730-012 DATED 03-17-04. INSTALLED IAW SRM 51-10-1 P/N: 4652201-2SP MINOR REPAIR THIS CLEARS DMI 16041E. 2L74 4F RT4A25 20040323000152004032300015EU 2004 3 23 BAQA092395 120040120A6240AWEURO4 SIGNAL COND UNIT UROCOPEC135 EC135T1 5620026EU MAST MOMENT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH401 0273 MMI INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 02/04/2004 1G72 3U H88EU 20040323000252004032300025EU 2004 3 23 BAQA092593 120040208A249745043006 MASTER SWITCH UROCOPEC135 EC135T1 5620026EU NR 2 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME2254 0143 NR 2 ENGINE WILL NOT START, BOX WILL NOT PASS SELF TEST. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/17/2004 1G72 3U H88EU 20040323000272004032300027 2004 3 23 BAQA092611 420040206A221041600297006 MODULE UROCOPEC135 EC135P2 5620027EU TRIM ACTUATOR FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03868ME137 0288 TRIM ACTUATOR MODULE WILL NOT TURN ON, OR TEST. 3 SLASHES ON PFD INDICATING MASSIVE FAILURE OF APM. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/10/2004 1G72 3U H88EU 20040323000542004032300054EU 2004 3 23 USAASA04016 120040216A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19122US10640 1298 PHL - THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT WAS FAULTING DURING TEST. MAINTENANCE REPLACED THE MID CABIN, LEFT EMERGENCY POWER SUPPLY UNIT. (M) 2L72 4F RTA28NM 20040323000592004032300059EA 2004 3 23 ASOA04083 120040201A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE CABLE INTERCOSTAL BRACKETS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CABLE INTERCOSTAL BRACKETS AT FS 484, LBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040323000632004032300063EA 2004 3 23 ASOA04069 120040127A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11901EV 7616 FLT 4713 - DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000652004032300065NM 2004 3 23 DHL2004755006 120040316A4900 APU BOEING727 727225 1384077NM APU BAY ODOR A DHLAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01755DH 21857 ON TAXI OUT NOTED SMOKE IN COCKPIT. EXECUTED SMOKE SOURCE IDENTIFICATION CHECKLIST AND SMOKE APPEARED TO CEASE. RETURNED TO BLOCKS. FOUND APU PNEUMATIC SYSTEM TO BE THE CAUSE OF THE FOUL ODOR IN THE COCKPIT. DEFERRED APU PER MEL 49-1. ASSIGNED DMI 16049 PLACARD INSTALLED. REF. DMI NR 16049 ON TAXI OUT NOTED SMOKE IN COCKPIT, EXECUTED SMOKE SOURCE IDENTIFICATION CHECKLIST AND SMOKE APPEARED TO CEASE. RETURNED TO BLOCKS. CLEANED WATER SEPARATOR COALESCER BAGS IAW M/M 21-55-51. AIR CONDITIONING SYSTEM OPS CHECKED NORMAL. DMI NR 16049 CLEARED. PLACARD REMOVED. 2L73 4F A3WE 20040323000832004032300083NM 2004 3 23 UPS04442021 120040228A5310 SHEAR TIE BOEING747 747SR46 1384816NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, AFT CARGO COMPT - STA 1840 IN BETWEEN STR 51L AND STR 51R SHEAR TIE FOUND CRACKED. DEFECTIVE AREA SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3. 2L74 4F RTA20WE 20040323000872004032300087CE 2004 3 23 DXTA200400267 120040316A5297 WIRE CESSNA560 560XL 2076702CE POSITION SWITCH SHORTED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07612QS 5605312 ABORTED TAKEOFF DUE TO ACCESSORY DOOR UNLOCKED TAIL ANNUNCIATOR AND MASTER CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 70 KNOTS, ABORTED TAKEOFF. TROUBLESHOT TO SHORTED WIRES OUT BACK SIDE OF BATTERY DOOR LOCK SENSOR. REMOVED AND REPLACED SWITCH. OPS CHECK GOOD, ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 52-70-00. 2L72 4F RTA22CE 20040323000932004032300093WP 2004 3 23 UPS04842033 120040302A53113614944505 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, STATION 1300 FRAME IS CORRODED BEYOND LIMITS ON LOWER FLANGE AT LONG 36. CUT OUT DAMAGED FRAME SECTION, FABRICATED, INSTALLED 2 SPLICES, ANGLES AND REPLACEMENT FRAME SECTION IAW SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20040323000942004032300094WP 2004 3 23 UPS04842034 120040303A5330 SKIN DOUG DC8 DC871F 302199DWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, REMOVE EXTERNAL DOUBLER AT STATION 1722 LONGERON 17R-18R IAW EO DC8-5330-17288-A APPROX C AND REPAIR IAW SRM 53-2-1 FIG 7. REMOVED EXISTING DOUBLER, CUT OUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040323000952004032300095WP 2004 3 23 UPS04842035 120040303A5320575503225 FLOOR SUPPORT DOUG DC8 DC871F 302199DWP AFT CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, FLOOR SUPPORT IS CORRODED BEYOND LIMITS BETWEEN STATION 1702 -1723 AT LBL 19. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755032 AND SRM 51-1-20D, 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20040323000972004032300097SO 2004 3 23 C2XA04BT036 120040314A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 DURING SERVICE AND ROUTINE INSPECTION OF AIRCRAFT, MAINTENANCE FOUND ROW NR 3 EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040323001012004032300101NM 2004 3 23 CALA0400247 120040313A5230UNK SKIN BOEING737 737824 13844BZNM CARGO DOOR SCRATCHED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714237 28802 INSPECTION FOUND A 20 INCH SCRATCH IN AFT CARGO DOOR SKIN. REPAIRED IAW ECRA 5231-01049. 2L72 4F RTA16WE 20040324000262004032400026NM 2004 3 24 MEX2004058 120040214A3150 SENSOR DOUG MD88 MD88 3023688NM SPOILERS DIRTY A ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23161PL 49764 FLT 174 - MZT-MEX - AIRCRAFT RETURNED TO PLATFORM DUE TO SPOILER DEPLOYED LIGHT TURNED ON. DURING REVISION THE SENSORS WERE CLEANED AND AIRCRAFT WAS DISPATCHED UNDER MEL 27-32. (M) 2L72 4F RTA6WE 20040324000342004032400034WP 2004 3 24 UPS04842014 120040303A5330 DOUBLER DOUG DC8 DC871F 302199DWP ACCESSORY BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, AFT SIDE STATION 1540 LONGERON 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17D, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040324000362004032400036NM 2004 3 24 SWAA040806 120040316A2560P2070001 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 FWD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED FWD FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040324000372004032400037NM 2004 3 24 SWAA040807 120040316A2560P2070001 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040324000392004032400039NM 2004 3 24 SWAA040809 120040316A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29768SW 30587 EEPLS COVER MISSING IN FWD CABIN. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040324000412004032400041NM 2004 3 24 SWAA040811 120040316A335065C34691 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 14 ABC. SECURED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040324000422004032400042 2004 3 24 SWAA040812 420040316A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR MOUNT FITTING CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE MOUNT FITTING PER SRM. 2L72 4F RTA16WE 20040324000442004032400044NM 2004 3 24 SWAA040814 120040316A53106546569 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 967, LBL 1. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040324000452004032400045NM 2004 3 24 SWAA040815 120040316A531069353656 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360 BETWEEN STRINGERS 14R AND 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040324000482004032400048EA 2004 3 24 SWIA200413020 120040313A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07448SW 7678 AFT OVERHEAD EMERGENCY EXIT LIGHT BURNED OUT. REMOVED AND REPLACED AFT MOST OUTBOARD EMERGENCY EXIT LIGHT LAMP. OPS CHECK GOOD. P/N: 1317. 2L72 4F RTA21EA 20040324000492004032400049EA 2004 3 24 SWIA200413021 120040314A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07934SW2950 2950 7722 STAB CHANNEL NR 2 CIRCUIT BREAKER 3A5 KEEPS TRIPPING. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPS CHECK GOOD FOR CRJ MM 27-42-01 AND 27-42-05. MOTOR CONTROL UNIT P/N 7062-3, S/N OFF 1009. 2L72 4F RTA21EA 20040324000502004032400050EA 2004 3 24 SWIA200413022 120040315A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY FAILED A SWIAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 NM07587SW4826 4826 7062 APU SHUTDOWN AUTOMATICALLY ON GROUND, HAD BEEN CYCLING BETWEEN 690 DEGREES - 725 DEGREES, FLAMES OUT THE EXHAUST AND CONTINUED FUMES LED TO PRECAUTIONARY DEPLANING. REMOVED AND REPLACED APU ASSY IAW RII49-401. 2L72 4F RTA21EA 20040324000512004032400051EA 2004 3 24 SWIA200413023 120040314A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07909SW6068 6068 7558 ON PUSHBACK FLIGHT SPOILER FAULT. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01 AND RIGHT SECU IAW MM 27-61-05. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20040324000522004032400052 2004 3 24 AALA20040328 420040303A2565 CONNECTOR BOEING767 767323 1385205NM SLIDE DIRTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21351AA 24032 SFO - MAINTENANCE ENTRY SQUIB NR 1 RIGHT OVERWING ESCAPE WILL NOT TEST. FOUND D1128 CONNECTOR IN NEED OF CLEANING. CLEANED D1128 CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040324000532004032400053SO 2004 3 24 SWIA200413024 120040315A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07291SW8805 8805 120318 WHEN RETRACTING FLAPS AFTER LANDING, NACELLE FLAPS REMAINED DOWN WITH FLAP DISAGREEMENT. REPLACED RIGHT NACELLE ACTUATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324000552004032400055SO 2004 3 24 SWIA200413026 120040212A5414 SKIN EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07233SW 120307 RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP CRACKED AT RIVET. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2L72 4T RTA31SO 20040324000562004032400056EA 2004 3 24 SWIA200413027 120040309A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, FS 193 LEFT SIDE ELECTRICAL BAY FLOOR CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLOOR IAW CRJ REO 601R-53-11-081 REV. NC AND RII 53-401 2L72 4F RTA21EA 20040324000572004032400057CE 2004 3 24 DXTA200400264 120040315A3241 WARNING LIGHT CESSNA560 560XL 2076702CE ANTI SKID SYSTEMILLUMINATED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07679QS 5605279 AFTER LANDING, DURING TAXI ANTISKID INOP AND LO BRAKE PRESS ANNUNCIATOR ILLUMINATED. BRAKES FELT HARD AND INEFFECTIVE BUT DID NOT GO TO THE FLOOR, USED EMERGENCY BRAKE TO STOP AIRCRAFT ON TAXIWAY. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040324000582004032400058CE 2004 3 24 DXTA200400263 120040315A3241NAS1611012 O-RING CESSNA500 560CESSNA 2076750CE ANTI SKID SYSTEMFAILED E DXTAO OTHER JS WARNING INDICATION AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07318QS 5600418 BRAKES FAILED WHILE TAXIING, POWER BRAKE AND ANTI-SKID INOP, ANNUNCIATOR ILLUMINATED. FOUND BRAKE SYSTEM LEAKING FROM THE ANTI-SKID SYSTEM PUMP. REPLACED O-RING, BLED BRAKES & PERFORMED OPS AND LEAK CHECK, NO FURTHER DEFECTS NOTED. ALL WORK WAS DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20040324000592004032400059CE 2004 3 24 DXTA200400259 120040311A5220 DOOR CESSNA500 560CESSNA 2076750CE EMERGENCY EXIT STUCK E DXTAK NONE O OTHER ININSP/MAINT 1 GL07335QS 5600335 DURING EMERGENCY EGRESS TRAINING, FOUND EMERGENCY EXIT DOOR WOULD NOT OPEN. FOUND SEALANT BONDED TO EXIT STRUCTURE. REMOVED EXIT AND CLEANED SEAL, REMOVED AND REINSTALLED EMERGENCY EXIT SEVERAL TIMES, OPS CHECK GOOD IAW CESSNA 560 MM CHAPTER 52-20-01. 2L72 4F RTA22CE 20040324000602004032400060CE 2004 3 24 DXTA200400260 120040311A3260H111499 POSITION SWITCH CESSNA650 650 2076802CE NLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS CLCLIMB 1 GL07791QS 6507091 AFTER TAKEOFF, TOOK SEVERAL ATTEMPS TO MOVE GEAR HANDLE TO RAISE LANDING GEAR. JACKED AIRCRAFT AND CYCLED LANDING GEAR, COULD NOT DUPLICATE DISCREPANCY. GAINED ACCESS TO NOSE GEAR CENTERING SWITCH, OHMED OUT AND FOUND SWITCH TO BE INTERMITTENT. REMOVED AND REPLACED NOSE GEAR CENTERING SWITCH, OPS CHECK AT INSTALLATION AND ADJUSTMENT CHECKED GOOD. ALL WORK DONE IAW 650 MM 32-60-00. 2L72 4F A9NM 20040324000622004032400062CE 2004 3 24 DXTA200400262 120040315A3150 WARNING LIGHT CESSNA750 750 2076810CE COCKPIT ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07986QS 7500086 DURING TAKEOFF ROLL MASTER WARNING AND NO TAKEOFF CAS MESSAGE CAME ON AT APPROX 90 KNOTS, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20040324000642004032400064WP 2004 3 24 AALA20040330 120040308A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217533A 49987 DFW - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324000662004032400066WP 2004 3 24 AALA20040331 120040308A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21251AA 49270 STL - EMERGENCY EGRESS LIGHT AT OVERHEAD AFT STAIRWELL INOPERATIVE. FOUND LOOSE WIRING. SECURED WIRING CONNECTION FOR EMERGENCY EGRESS LIGHT AT OVERHEAD AFT STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324000682004032400068NM 2004 3 24 SWAA040824 120040317A57406546460 ATTACH ANGLE BOEING737 7373Q8 1384670NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPV, FOUND LT WING LOWER ATTACH ANGLE AT WBL 135.5, S2, CRACKED. REMOVED AND REPLACED LT WING ATTACH ANGLE PER SRM. 2L72 4F RTA16WE 20040324000692004032400069NM 2004 3 24 SWAA040825 120040317A531069353656 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPV, FOUND SHEAR TIES AT BS 360, STRINGERS 14R AND 14L, CRACKED. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040324000712004032400071 2004 3 24 SWAA040827 420040317A256565C19901 CABLE BOEING737 7375H4 138449DNM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040324000732004032400073 2004 3 24 SWAA040819 420040317A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 L1 DOOR EVAC SLIDE INADVERTENTLY PULLED FROM CASE. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040324000762004032400076NM 2004 3 24 SWAA040822 120040317A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING IN BULLNOSE AT ROW 3 ABC. REINSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040324000802004032400080EA 2004 3 24 SWIA200413003 120040306A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07946SW 7776 APPROXIMATELY 9 FEET OF EMERGENCY LIGHTS FAIL TO ILLUMINATE THE CABIN. CLEANED MOISTURE FROM MIDDLE FLOOR EMERGENCY LIGHT STRIP. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040324000812004032400081SO 2004 3 24 SWIA200413004 120040307A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAP LEVER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07586SW4783 4783 120354 CAPT REPORTS MULTIPLE CONTROL FAULTS (ON TAXI OUT AND APPROACH). REPLACED FLAP CONTROL HANDLE PER MM 27-50-01. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324000822004032400082 2004 3 24 SWIA200413005 420040306A3418 VANE CNDAIRCL600 CL6002B19 1900309EA AOA FAILED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07962SW 7859 AFTER TAKEOFF, STALL FAIL MSG CAME ON. STAYED ON FOR DURATION OF FLIGHT. BOTH AIRSPEED INDICATORS ARE THE SAME. LEFT LOWER RED FLAP INDICATES HIGHER THAN RIGHT SIDE. REMOVED AND REPLACED LEFT AOA VANE WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. COMPLETED IAW AMM 27-35-05. 2L72 4F RTA21EA 20040324000832004032400083SO 2004 3 24 SWIA200413006 120040308A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN FLOOR INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07292SW 120319 FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REPLACED FORWARD CABIN EMERGENCY EXIT LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324000842004032400084EA 2004 3 24 SWIA200413007 120040308A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERONS FAILED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW 7279 LEFT SPOILERON FAULT MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECK GOOD. P/N 49-164-06, S/N OFF 0929. 2L72 4F RTA21EA 20040324000852004032400085EA 2004 3 24 SWIA200413008 120040308A76032100140007 GEARBOX CNDAIRCL600 CL6002B19 1900309EA NR 1 THRUST MALFUNCTIONED A SWIAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 NM07443SW5145 5145 7638 NR 1 THRUST LEVER STUCK AT CRUISE POWER SETTINGS. PERFORMED QRH AND SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED LT POWER LEVER CONTROL GEAR BOX IAW CRJ MM 76-11-17. OPS CHECK GOOD. 2L72 4F RTA21EA 20040324000872004032400087WP 2004 3 24 ABXA040096 120040313A27603644322507 CRANK ASSY DOUG DC8 DC863F 302198FWP SPOILERS BROKEN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23814AX 46041 SPOILER EXTEND LIGHT STAYED ON AFTER RETRACTION. NORMAL SPOILER HYDRAULIC PRESSURE INDICATION. MAINTENANCE FOUND RIGHT WING INBOARD TWO SPOILER DRIVE ARMS THAT ATTACH TO SPOILER CABLES BROKEN. REPLACED REAR SPAR ACTUATOR CRANK ASSEMBLIES ON INBOARD SPOILER PANEL FOR THE RIGHT WING IAW DC-8 MM 27-61-01-2. AFTER REPLACEMENT OF RIGHT HAND INBOARD SPOILER CRANKS, SPOILER DEPLOYED SWITCH INSTALLED IN CORRECT POSITION. OPS CHECKED GOOD IAW DC-8 MM CHAPTER 27-63-01-02-0001, PARA 3A. 2L74 4F 4A25 20040324000882004032400088WP 2004 3 24 DHL2004809004 120040315A5711 SPAR DOUG DC8 DC873F 302199FWP LT MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 LT MLG WHEEL WELL FUSELAGE STA 931 FALSE SPAR STA 1.50 THE UPPER END OF CHANNEL HAS A .375 INCH CRACK IN RADIUS OF VERT LONG. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 16042E. ONLY 2 REVENUE FLIGHTS WITH NOTED DAMAGE. COMPLY WITH ASTAR J/C MSI57300035-001-D REF. DMI 16042E LT MLG WHEEL WELL STA. 931 FALSE SPAR STA. 1.50 3.75 CRACK IN RADIUS OF VERT LONG. P/N: 5643117-30. COMPLIED WITH J/C MSI57300035-001-D REPLACED CHANNEL P/N: 5643117-30. THIS CLEARS DMI 16042E. 2L74 4F RT4A25 20040324000892004032400089EU 2004 3 24 UPS04141993 120040226A5311 FRAME AIRBUSA300 A300F4622R 3930360EU FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01145UP 0828 INSPECTION TYPE: C1, FOUR BLIND RIVETS INSTALLED BETWEEN STA 794 AND 815 AT 600 POS D268358 XFRD TO NRC 725518. REMOVED FITTING AT STA 2771 STR 43L. REMOVED BLIND FASTENERS & INSTALLED SOLID FASTENERS IAW A300-600 SRM 51-41-10. OK TO REINSTALL FITTING. REMOVED FLOORBOARDS & INSULATION FR STA 1499 TO 2559 TO FOM. OK TO REINSTALL INSULATION. INSTALLED INSULATION IAW A300-600 53-10-29, OK TO INSTALL FLOORBOARDS. INSTALLED FITTING IAW A300-600 SRM 51-40-21. REMOVED & INSTALLED FASTENERS IAW A300-600 SRM 51-40-21. REMOVED & REINSTALLED FITTING IAW A300-600SRM. 2L72 4F RTA35EU 20040324000902004032400090EU 2004 3 24 UPS04142018 120040304A5330A53986202200 SKIN AIRBUSA300 A300F4622R 3930360EU TAIL JACK PAD DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01144UP 0827 INSPECTION TYPE: C1, AFT LOWER FUSELAGE, DENT IN FUSELAGE SKIN, FWD OF TAIL JACK PAD. FOUND DENT OUT OF LIMITS; MAT ID DOUBLER 2024-T3.071 PO 424146.8; FABBED DOUBLER; ALODINED & PRIMED; INSTALLED DOUBLER; ALL IAW A300-600 SRM 53-10-12, 51-21-10. 2L72 4F RTA35EU 20040324000912004032400091WP 2004 3 24 UPS04842017 120040302A55425644210505 SKIN DOUG DC8 DC871F 302199DWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, RUDDER EXTERIOR SKIN IS CRACKED AT RT UPPER SIDE. REMOVED AND REPLACED RUDDER IAW MM 27-21-01. 2L74 4F RT4A25 20040324000922004032400092WP 2004 3 24 UPS04842022 120040312A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01807UP 46007 INSPECTION TYPE:P/S FOUND EMERGENCY BATTERY INOPERATIVE DURING PERIODIC SERVICE CHECK PARA 9C. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY UNIT IAW AMM 33-50-01-2. 2L74 4F RT4A25 20040324000932004032400093EA 2004 3 24 SWIA200413028 120040309A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, FS RIGHT SIDE ELECTRICAL BAY FLOOR CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLOOR DAMAGE IAW CRJ REO 601R-53-11-345 REV. NC AND RII53-401. 2L72 4F RTA21EA 20040324000942004032400094EA 2004 3 24 SWIA200413029 120040309A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA COCKPIT FLOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, COCKPIT FLOOR HATCH; AFT CAMLOCK ANGLE IS CRACKED AT FS 280.00; RBL-8.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-21-11, 51-23-00, AND 51-25-16, AND RII53-401. 2L72 4F RTA21EA 20040324001012004032400101NM 2004 3 24 AALA20040340 120040311A3397 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21328AA 22328 SFO - EMERGENCY LIGHT AT SEAT 28AB INOPERATIVE. REPAIRED BROKEN WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040324001022004032400102WP 2004 3 24 AALA20040341 120040311A3350 LIGHT DOUG DC9 DC982 3022082WP GALLEY INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21580AA 53157 MIA - EMERGENCY LIGHT AT GALLEY WALL ACROSS FROM FORWARD LAV WILL NOT TEST. REPLACED LIGHT ASSEMBLY AT FORWARD LIGHT AT GALLEY WALL ACROSS FROM FORWARD LAV AND REPAIRED BROKEN WIRE PER M/M. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001032004032400103EU 2004 3 24 MALA040271 120040314A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING INSPECTION IN LCQ, FS 297 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/17/04. 2L72 4T RTA52EU 20040324001042004032400104EU 2004 3 24 MALA040268 120040310A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438XJ 340B438 DURING INSPECTION IN LCQ, FWD FUSELAGE AT STA 319 TO 307 HAS NUMEROUS DENTS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER AND TRIPLER REPAIR, FABRICATED AND INSTALLED ICE SHIELDS NR 5, 6, 7 & 8 IAW MESABA EO S53208. A/C RELEASE DATE 3/14/2004. 2L72 4T RTA52EU 20040324001052004032400105EU 2004 3 24 MALA040272 120040315A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 DURING INSPECTION IN LCQ, LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/19/2004. 2L72 4T RTA52EU 20040324001062004032400106EU 2004 3 24 MALA040274 120040315A5320 SILL SAAB SF340 340B 7860101EU COCKPIT CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 DURING INSPECTION IN LCQ, LEFT LOWER SILL COCKPIT ENTRY WAY CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW MESABA EO S53209. A/C RELEASE DATE 3/19/2004. 2L72 4T RTA52EU 20040324001072004032400107EA 2004 3 24 SWIA200413014 120040311A2721 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER INTERMITTENT A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07969SW 7876 RUDDER TRIM SWITCH INOP INTERMITTENTLY TO THE LEFT. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL. SYSTEM OPS CHECK GOOD. 2L72 4F RTA21EA 20040324001092004032400109 2004 3 24 SWIA200413017 420040313A3418 VANE CNDAIRCL600 CL6002B19 1900309EA AOA OBSTRUCTED A SWIAA UNSCHED LANDING WN INADEQUATE Q C FALSE WARNING CLCLIMB 1 NM07426SW 7468 LOUD BUZZING/WHISTLING SOUND FROM NOSE AND STALL FAIL MESSAGE. RETURNED TO BASE AND EMERGENCY EQUIPMENT RESPONDED. SUSPECT O2 SERVICE DOOR PARTIALLY OPEN CAUSING AIRFLOW INTERFERENCE OVER RIGHT AOA VANE. PROPERLY SECURED DOOR. PERFORMED STALL PROTECTION SYSTEM TEST PER MM 27-35-01. NO DEFECTS NOTED. 2L72 4F RTA21EA 20040324001102004032400110EA 2004 3 24 SWIA200413018 120040307A2613 SENSOR CNDAIRCL600 CL6002B19 1900309EA LT ENG TAILPIPE MALFUNCTIONED A SWIAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING DEDESCENT 1 NM07919SW 7657 WHILE ON APPROACH TO DEN LEFT JETPIPE OVERHEAT WARNING CAME ON. SHUTDOWN LEFT ENGINE AS PER THE QRH. REMOVED AND REPLACED LEFT ENGINE JETPIPE OVERHEAT SENSING ELEMENTS ON BOTH A AND B SYSTEMS IAW CRJ MM ATA CHPT 26-11-00 AND 26-11-01. P/N: 26212000. 2L72 4F RTA21EA 20040324001112004032400111 2004 3 24 SWIA200413019 420040312A341845150340 SENSOR CNDAIRCL600 CL6002B19 1900309EA AOA MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07417SW1053510535 7400 DURING TAXI OUT STALL FAIL MESSAGE INTERMITTENLY CYCLES ON AND OFF. REMOVED AND REPLACED RIGHT AOA VANE IAW MM 27-35-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040324001132004032400113NM 2004 3 24 CALA0400252 120040317A5320BAC1496377X7075TCHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718243 28806 INSPECTION FOUND AFT CARGO Z-CHANNEL CORRODED AT STA 727-847. THE CORRODED SECTION WAS REMOVED AND A NEW CHANNEL WAS SPLICED IN IAW SRM 53-00-53, REPAIR 5. 2L72 4F RTA16WE 20040324001142004032400114NM 2004 3 24 CALA0400253 120040317A2560 BATTERY BARFIELD BOEING737 737824 13844BZNM MEGAPHONE WEAK A CALAK NONE O OTHER ININSP/MAINT 1 SW2733262 32402 INSPECTION FOUND AFT PASSENGER CABIN MEGAPHONE WEAK. THE MEGAPHONE WAS REPLACED. 2L72 4F RTA16WE 20040324001152004032400115NM 2004 3 24 CALA0400254 120040318A5320149A7611 WEB BOEING737 737724 13844BYNM LT MGL WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727733 28800 INSPECTION FOUND A 2 INCH CRACK AROUND NUT PLATE OF FORWARD O/B WEB OF WHEEL WELL WEB SKI JUMP AT LBL 50.0. THE LEFT WHEEL WELL O/B WEB ON SKI JUMP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040324001162004032400116NM 2004 3 24 CALA0400255 120040318A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND THE FUSELAGE SKIN DENTED AT STA 1080, WL 192, RBL 8. THE AREA WAS REPAIRED IAW SRM 53-00-01 AND 51-21-41. 2L72 4F RTA16WE 20040324001172004032400117WP 2004 3 24 UPS04842016 120040309A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01798UP 45898 EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OP'S CHECKS NORMAL PER MM 33-50-01-2 ITEM 4. 2L74 4F RT4A25 20040324001182004032400118NM 2004 3 24 UPS04M42006 120040307A2750 CONTROL VALVE DOUG MD11 MD11F 3023600NM TE FLAPS INOPERATIVE A IPXAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01253UP T/E FLAPS LOCKED OUT AT 15 DEGREES DURING INITIAL CLIMB. FLAP DISAGREE MESG DISPLAYED. FUEL WAS DUMPED TO ACHEIVE LANDING BACK TO BOM, ATB. REMOVED AND REPLACED INBOARD WING FLAP CONTROL VALVE IAW 27-52-03, LEAK CHECK GOOD. FLAP OPERATION RANGE MOTION TEST NORMAL PER MM 27-50-00. 2L73 4F RTA22WE 20040324001222004032400122NM 2004 3 24 AALA20040317 120040303A5415 FITTING BOEING757 757223 1384957NM BULKHEAD OVERSIZED A AALAK NONE O OTHER ININSP/MAINT 1 SW21656AA 24614 TUL - OUTBOARD LOWER FORWARD HOLE OVERSIZED WHEN CRACK REMOVED AT NR 1 MID BULKHEAD FITTING. AREA IS 0.640 BY 0.640 WITH A DEPTH OF 0.250. FABRICATED BUSHING AND INSTALLED PER ESO 90309. 757 SRM 54-50-02, 51-20-07, 757 AARD 54-50-003, SERVICE BULLETIN 757-54-A0039, FCD FF0377G, AND BOEING COMMUNICATION AAL-TUL-04-00172F FOR OUTBOARD LOWER FORWARD HOLE AT NR 1 MID BULKHEAD FITTING. 2L72 4F RTA2NM 20040324001252004032400125NM 2004 3 24 AALA20040320 120040305A335060030451 BATTERY DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219413T 53188 EMERGENCY LIGHT IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHT IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040324001262004032400126NM 2004 3 24 AALA20040321 120040305A3397 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW219413T 53188 DFW - EMERGENCY LIGHT AT SEAT ROW 19 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040324001282004032400128EA 2004 3 24 SWIA200413030 120040220A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 DISCOVERED DURING C-CHECK INSPECTION, BRACKET CRACKED ON LEFT LOWER SIDE OF COCKPIT ENTRANCE. REPLACED BRACKET IAW CRJ SRM 51-40-11, PARA. 4, 51-42-16. 2L72 4F RTA21EA 20040324001292004032400129EA 2004 3 24 SWIA200413031 120040220A1430 NUT CNDAIRCL600 CL6002B19 1900309EA RUDDER BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 DISCOVERED DURING C-CHECK INSPECTION, RUDDER LEFT SIDE ANCHOR NUT BROKEN AT CENTER HINGE PANEL ATTACH POINT. REPLACED ANCHOR NUT IAW CRJ SRM 51-45-00. REPLACED SEALANT IAW SRM 51-23-00. 2L72 4F RTA21EA 20040324001302004032400130EA 2004 3 24 SWIA200413032 120040220A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 DISCOVERED DURING C-CHECK INSPECTION, CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 42.00. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV. ''A'' AND RII53-401. 2L72 4F RTA21EA 20040324001312004032400131EA 2004 3 24 SWIA200413033 120040220A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE RBL 9.0 HAS INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED AT FS 280.00. ANGLES REPLACED AT FS 280.0, RBL 9.0 IAW CRJ SRM. 2L72 4F RTA21EA 20040324001332004032400133EA 2004 3 24 SWIA200413035 120040220A5340 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, PAX DOOR SUPPORT ANGLE CRACKED ADJACENT TO DOOR ASSIST CABLE BRACKET. REPAIRED DAMAGE IAW CRJ REO 601R-52-11-448 REV ''NC''. 2L72 4F RTA21EA 20040324001362004032400136EA 2004 3 24 SWIA200413038 120040220A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT FLOORBEAM ANGLE CRACKED AT FS 621.00 RBL 42.0. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401. 2L72 4F RTA21EA 20040324001402004032400140EA 2004 3 24 SWIA200413042 120040227A5220 SHAFT CNDAIRCL600 CL6002B19 1900309EA DOOR HANDLE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, CREW ESCAPE HATCH OUTER HANDLE SHAFT IS CORRODED. REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW HARTWELL CORPORATION CMM 52-22-03. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040324001412004032400141EA 2004 3 24 SWIA200413043 120040227A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ANGLE AT STR 14R, FS 625 REPLACED IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F RTA21EA 20040324001422004032400142EA 2004 3 24 SWIA200413044 120040227A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' AND RII 53-401. 2L72 4F RTA21EA 20040324001432004032400143EA 2004 3 24 SWIA200413046 120040309A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07412SW 7101 MAIN FUSELAGE; FS 280.00, RBL 9.0, LOWER FLANGE CRACKED ON TRANSVERSE BEAM. REPAIRED IAW CRJ REO 601R-53-11-171 REV. NC AND RII53-401. 2L72 4F RTA21EA 20040324001452004032400145EA 2004 3 24 SWIA200413048 120040309A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 CARGO PIT; FS 589.00 AND 605.00; TRANSVERSE BEAM ATTACH ANGLES FOR LANDING PLATE STOP FITTINGS CRACKED. REPLACED ANGLES (2 OF) IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-21-11, 51-25-16, 51-41-04. 2L72 4F RTA21EA 20040324001492004032400149WP 2004 3 24 AALA20040346 120040314A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21411AA 49322 SFO - OVERHEAD EMERGENCY LIGHT ABOVE TAIL CONE SLIDE INOPERATIVE. RESET BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ABOVE TAIL CONE SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001502004032400150WP 2004 3 24 AALA20040348 120040314A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21499AA 49737 DFW - EMERGENCY AFT OVERHEAD LIGHT BATTERY PACK MOUNT BROKEN. REPLACED BATTERY PACK FOR EMERGENCY AFT OVERHEAD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001522004032400152EA 2004 3 24 SWIA200413049 120040309A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 CARGO PIT; STEP PLATE SUPPORT IS BROKEN OUT ALONG INBOARD SIDE. CARGO PIT STEP PLATE SUPPORT REPLACED IAW CRJ SRM 51-41-02 AND SRM 51-23-00. 2L72 4F RTA21EA 20040324001532004032400153SO 2004 3 24 SWIA200412975 120040125A5420 BRACKET EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 INTERIOR BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW SRM 54-10-03 FIG 201. P/N 120-41419-001. 2L72 4T RTA31SO 20040324001542004032400154SO 2004 3 24 SWIA200412976 120040125A5415 ATTACH BRACKET EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 ATTACH BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL AT 3RD RIVET FROM BOTTOM (INTERIOR OF WALL). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BRACKET LOCATED AT LEFT NACELLE OUTBOARD OF WHEEL WELL IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1. 2L72 4T RTA31SO 20040324001582004032400158SO 2004 3 24 SWIA200412981 120040212A5420 CLIP EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07233SW 120307 RIGHT WING OUTBOARD OF NACELLE 1ST FUEL PANEL OUTBOARD MIDDLE LOWER CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SHEAR TIE RIGHT WING (MIDDLE LOWER). NO LEAKS NOTED. 2L72 4T RTA31SO 20040324001592004032400159 2004 3 24 SWIA200412983 420040225A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07217SW9493 9493 120286 DURING FLIGHT, CAPTAIN'S ADI AND FLIGHT DIRECTOR WERE ERRATIC CAUSING A COMPUTER FAILURE AND THE A/P TO DISENGAGE. INSTALLED SERVICEABLE APC-65B ON THE CAPTAIN'S SIDE IAW EMB 120 MM CHAPTER 22-10-02. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324001632004032400163EU 2004 3 24 MALA040273 120040315A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 DURING INSPECTION IN LCQ, RT SEAT TRACK CORRODED, CUT OUT DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/19/2004. 2L72 4T RTA52EU 20040324001642004032400164SO 2004 3 24 CHQA000469 120040316A5610163500112 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT CRACKED A CHQAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11370 5711 145515 FLIGHT 3144 LGA - CHS SHORTLY AFTER CLIMBING THROUGH 20,000 FT WITH WINDSHIELD HEAT ON, THERE WAS A BANG AND THE FIRST OFFICERS FRONT WINDSCREEN WAS CRACKED (SPIDER WEBBED). IMMEDIATELY REDUCED SPEED, DECLARED EMERGENCY, AND DIVERTED TO JFK DUE TO LGA BELOW LANDING MINIMUMS. RAN ALL NECESSARY CHECKLISTS AND LANDED AT JFK WITHOUT INCIDENT. MX REMOVED AND REPLACED F/O'S WINDSHIELD IAW EMB-145 MM CH 56-10-01. PRESSURIZED ACFT FOR LEAK CHECKS, NO LEAKS FOUND. WINDSHIELD HEAT CHECKED OK. 2L72 4T RTT00011AT 20040324001662004032400166NM 2004 3 24 AALA20040311 120040304A33500201991003 LIGHT BOEING757 757223 1384957NM SEAT 17D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21611AM 24487 AFT EMERGENCY PATH LIGHT ON SEAT 17D INOPERATIVE. REPLACED AFT EMERGENCY PATH LIGHT ASSEMBLY ON SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040322001072004032200107NM 2004 3 22 SWAA040786 120040312A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY SIGN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LOWER SIGN LENS BROKEN. REMOVED AND REPLACED SIGN LENS PER MM. 2L72 4F RTA16WE 20040322001122004032200112SO 2004 3 22 C2XA04TY050 120040313A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714558 145598 TYS, DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE FORWARD CENTER DIGITAL PLATE AT THE FORWARD NUT PLATE HOLE. MAINTENANCE REPAIRED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-145 SRM 51-21-01 AND CMP-51-21 04/05/06. 2L72 4T RTT00011AT 20040322001152004032200115EU 2004 3 22 MALA040247 120040305A2560 PBE BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15525XJ E2350 MID CABIN PBE LOST VACUUM SEAL. MX REPLACED PBE. 2H74 4F RTA49EU 20040322001332004032200133NM 2004 3 22 AALA20040351 120040303A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21788AN 30011 DFW EMERGENCY LIGHTS AT PARTITION BETWEEN L4/R4 DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT PARTITION BETWEEN L4/R4 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040322001372004032200137WP 2004 3 22 AALA20040342 120040312A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21516AM 49893 DFW CEILING EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040322001422004032200142NE 2004 3 22 AWXA200400277 220040311A7230 BLADE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE CRACKED A AWXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28620AW4231014747 052 V0014 AFTER TAKEOFF, EN ROUTE. NR 2 ENG STALLED WITH EGT OVERTEMP OF 843 DEGREE, FOLLOWED ECAM & DECLARED EMERGENCY. MX R / R NR 2 ENG IAW T/C. BORESCOPE OF HPC REVEALED 1, 7TH STAGE BLADE FRACTURED ROOT, & A SECTION OF 7TH STAGE REAR DAMPER WIRE MISSING OVER A SPAN OF FRACTURED BLADE & 2 ADJACENT BLADES. EXAMINATION OF BLADE SURFACE FOUND FRACTURE INDICATIVE OF HIGH CYCLE FATIGUE WITH ORIGIN CLOSE TO LE CONCAVE CORNER AT TOP EDGE OF BEDDING. A SHARP CORNER FOUND AT LOCATION & BELIEVED TO BE PRESENT WHEN BLADE WAS NEW. STRESS ANALYSIS ON 7TH STAGE BLADE WITH REAR DAMPER WIRE LEFT OUT, FOUND LACK OF DAMPER WIRE CAUSED BENDING THAT INCREASES STRESS ON LEADING EDGE OF BLADE WHERE ORIGIN OF FRACTURE WAS FOUND. 2L72 4F4 FRTA28NM E311NE 20040322001482004032200148NM 2004 3 22 AWXA200400283 120040303A575465C267996 SKIN BOEING737 7373G7 1384595NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 CRACKS WERE FOUND ON NR 6 SLAT LOWER SKIN BELOW ACTUATOR WBL 440.98 RT. MAINTENANCE CUT OUT DAMAGE ON NR 6 SLAT LOWER SKIN WBL 440.98 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 201 PG 216-219. 2L72 4F RTA16WE 20040322001552004032200155NM 2004 3 22 SWAA040790 120040314A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 33 TO RBL 39. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040322001562004032200156NM 2004 3 22 SWAA040791 120040314A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20040322001622004032200162NM 2004 3 22 SWAA040797 120040314A53126546568 BULKHEAD BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AT FUSELAGE BULKHEAD, BS 1016, STR 7R, AND OUTBOARD OF DOME CAP. REPAIRED BULKHEAD WEB PER ER. 2L72 4F RTA16WE 20040322001632004032200163NM 2004 3 22 SWAA040747 120040310A3260655825029 CIRCUIT CARD BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW29334SW 23938 DIVERSION, RED AND GREEN NOSE GEAR LIGHTS STAY ON WITH HANDLE IN THE UP AND OFF POSITION. REMOVED AND REPLACED M983 CARD AND ADJUSTED NOSE GEAR LOCK SENSOR PER MM. 2L72 4F RTA16WE 20040322001692004032200169NM 2004 3 22 SWAA040753 120040310A53306546881 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1050, STRINGER 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001732004032200173NM 2004 3 22 SWAA040758 120040309A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STRINGER 21L AND BS 938, STRINGER 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001812004032200181EA 2004 3 22 COMA0460195 120040311A2910601R5239455 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA LT MLG WW LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01984CA 7171 FLIGHT 5588 HYDRAULIC SYSTEM 2 LOW PRESSURE CAUTION. REPLACED DEFECTIVE HYDRAULIC LINE IN LEFT WHEEL WELL. 2L72 4F RTA21EA 20040322001852004032200185NM 2004 3 22 AWXA200400286 120040315A3397BMS13311122 WIRE BOEING737 73733A 1384673NM SEAT ROW 14 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRING AT FLOOR CONNECTOR SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040322001942004032200194 2004 3 22 SWAA040798 420040315A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 R2 DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040322001962004032200196NM 2004 3 22 SWAA040802 120040315A2560P2070004 HOLDER BOEING737 7373Q8 1384670NM FWD CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY FLASHLIGHT HOLDER CRACKED AT FWD F/A'S SEAT. REMOVED AND REPLACED FLASHLIGHT HOLDER PER MM. 2L72 4F RTA16WE 20040323000112004032300011 2004 3 23 BAQA091935 420040202A34214021541791 AHRS BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME400 7243 AUTO PILOT WOULD DECOUPLE. REPLACED WITH SERVICABLE UNIT. 02/03/2004 1G72 3U3 U H13EU E5NE 20040323000302004032300030EU 2004 3 23 BAQA092644 120040123A5610L521M00X1022 WINDOW UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF286 0281 WINDOW CRACKED NEAR BOTTEM LT CORNER. REPLACED WITH SERVICABLE UNIT. 02/11/2004 1G72 3U3 U H88EU E34NE 20040323000312004032300031EU 2004 3 23 BAQA091139 120040212A28101176416901 DRAIN VALVE BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE FUEL TANK LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03955ME6462 7243 WARRANTY. UNIT LEAKING. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1G72 3U3 U H13EU E5NE 20040323000372004032300037NE 2004 3 23 I05R092763 220040105A7261350A54113800 CLAMP SNIAS 350 AS350* EU TMECA ARRIELARRIEL2B NE OIL/AIR VENT CRACKED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP0529LB 1000 3560 CRACKED CLAMP, REPLACED PART. 1G71 3U3 U H9EU E00054EN 20040323000392004032300039EU 2004 3 23 I05R092765 120040115A6330L633M2001105B010MOUNT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE M/R GEARBOX FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP07552BA1521 190 MAIN ROTOR GEARBOX MOUNT FAILED. REPLACED MOUNT. 1G72 3U3 UO H88EU E42NE 20040323000412004032300041EA 2004 3 23 ASOA04072 120040129A5610NP13932110 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A ASOAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11885AS 7521 FLT 4596 - DURING CRUISE FROM YOW-ATL, AT APPROXIMATELY 35,000 FT THE RIGHT WINDSHIELD SHATTERED. PRESSURIZATION REMAINED NORMAL, THE QRH WAS COMPLIED WITH AND THE AIRCRAFT DESCENDED TO 10,000 FEET. AN EMERGENCY WAS DECLARED AND THE ARICRAFT DIVERTED TO TRI, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000512004032300051EA 2004 3 23 ASOA04074 120040130A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT AFT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040323000532004032300053SO 2004 3 23 SIMA200404601 120040204A551014524978001 BUSHING EMB 145 EMB145LR 3260212SO HORIZONTAL STAB WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21619AE 145101 DURING SCHEDULED MAINTENANCE, FOUND HORIZONTAL STAB HAS PLAY AT RIGHT AFT HINGE MOUNT PIN. REPAIRED HORIZONTAL STAB REAR MOUNT BUSHING IAW EMB 145 SRM 55-10-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040323000562004032300056EA 2004 3 23 ASOA04067 120040126A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING HANGAR MAINTENANCE IN BTR, THE SECOND EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND EXTERIOR EMERGENCY LIGHT LAMP ON THE RIGHT SIDE. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000602004032300060EU 2004 3 23 ASOA04082 120040201A5343 SUPPORT BEAM AEROSPATR72 ATR72212 8680945EU MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11636AS 375 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT FORWARD NOSE LANDING GEAR DOOR AFT SUPPORT FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE WEB ON THE RIGHT FORWARD NOSE LANDING GEAR DOOR AFT SUPPORT FRAME BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER IAW SRM 51-24-05 AND 51-25-00. (M) 2H72 4T RTA53EU 20040323000612004032300061EA 2004 3 23 ASOA04076 120040131A33508GH00247308 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11702EV 10035 DURING A C-CHECK IN MCN, THE OVERWING EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE WERE FUOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE OVERWING EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000622004032300062EA 2004 3 23 ASOA04073 120040130A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER CENTER UNDER THE FIRE LOOP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER CENTER UNDER THE FIRE LOOP BRACKET IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040323000662004032300066NM 2004 3 23 UPS04442038 120040224A5320BAC1505100081 ANGLE BOEING747 747SR46 1384816NM FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, FX- AIRCON BAY FAIRING SUPPORT UPPER SURFACE CORROSION AT STA 1040 FROM RBL 15 - 57. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-50-01 FIG 5 LIMITS, FAIRING SUPPORT REPLACED PER SRM 51-10-01 PG 8 & CIC APPLIED IAW EO M5100-2780-E. 2L74 4F RTA20WE 20040323000762004032300076WP 2004 3 23 ABXA040101 120040302A532029223681 BRACKET DOUG DC9 DC941 302207NWP CARGO TRACK CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD CARGO AT FS 484 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040323000852004032300085NM 2004 3 23 UPS04M42027 120040313A3350 LIGHT DOUG MD11 MD11F 3023600NM COCKPIT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01251UP FLIGHT DECK EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN CONDUCTING TC 403 STEP 10 PARA G STEP 3. OPERATIONAL CHECK OF FLT DECK EMERGENCY LIGHTS NORMAL IAW MM 33-50-00. PER NRC 735354 2L73 4F RTA22WE 20040323001132004032300113SO 2004 3 23 C2XA04SH168 120040317A5310 SUPPORT BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE AFT GALLEY SUPPORT BEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040323001152004032300115NM 2004 3 23 AALA20040318 120040226A5330 SKIN BOEING777 777223 1385213NM FUSELAGE DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21792AN 30253 AFW - FUSELAGE SKIN AT STATION 390 BETWEEN STRINGER 44 RIGHT AND STRINGER 45 RIGHT HAS A DENT THAT HAS BEEN REWORKED IN AN AREA OF 4.5 INCH BY 4.5 INCH WITH A DEPTH OF 0.110 INCH. SKIN THICKNESS IS 0.071. DENT IS ADJACENT TO SKIN SPLICE. 2L72 4F RTT00001SE 20040323001202004032300120 2004 3 23 MALA040264 420040307A3420HG2001BC02 IRU BAC 146 AVRO146RJ85A1500097EU NR 1 FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15515XJ E2333 PASSING THRU 10,000 FT LOSS IRU ON CAPT SIDE (LEFT), RETURNED TO DTW. REMOVED AND REPLACED NR 1 IRU, ALL CHECKS GOOD IAW RJ-85 MM CH 34. P/N ON&OFF HG2001BC02, S/N OFF 97120734, S/N ON 97110762. 2H74 4F RTA49EU 20040323001232004032300123WP 2004 3 23 IXXA0400015O 120040317A323056165545503 CYLINDER DOUG DC8 DC871F 302199DWP LT MLG LEAKING A IXXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW11821BX847891892 45811 AFTER DEPARTURE FROM VTBU TO RJTY NOTED HYD FLUID AND PRESSURE LOSS. CREW FOLLOWED ABNORMAL CHECKLIST, PROCEEDED TO RJTY FOR AN UNEVENTFUL LANDING. MX DISCOVERED LEFT MLG BOGIE TRIM CYLINDER LEAKING AND REPLACED THIS COMPONENT. SYSTEM LEAKS AND OPS CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20040323001252004032300125NM 2004 3 23 AALA20040333 120040309A33971721651 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHTSBROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21386AA 27060 ORD - EMERGENCY LIGHTS AT SEAT 22B INOPERATIVE. REPLACED BROKEN CONNECTOR AT SIDEWALL PANEL FOR EMERGENCY LIGHTS AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040323001272004032300127NM 2004 3 23 AALA20040334 120040310A3350 SOCKET DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219413T 53188 STL - EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. REPLACED SOCKET FOR EMERGENCY EXIT LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040324000062004032400006WP 2004 3 24 MEX2004066 120040217A2913AS66411LS666 PUMP DOUG DC9 DC982 3022082WP HYDRAULIC SYS FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23505MD 49149 FLT 351 - MEX-ZIH - AIRCRAFT RETURNED TO PLATFORM, DUE TO LOSS OF HYDRAULIC PRESSURE. CAPTAIN REPORTED THAT THE LEFT HYDRAULIC SYSTEM WITH 1100 PSI ON HIGH, LOW AND SHUTOFF POSITION. THE LEFT HYDRAULIC PUMP WAS REPLACED IAW MM 29-00-00, TEST CORRECT. (M) 2L72 4F A6WE 20040324000072004032400007WP 2004 3 24 MEX2004053 120040211A3260DC61E10SL3PN RECEPTACLE DOUG DC9 DC982 3022082WP DOWNLOCK SENSOR DAMAGED A ASMFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW231003Y 48068 FLT 278 - MEX-CJS - AIRCRAFT RETURNED DUE TO NOSE LANDING GEAR RED LIGHT TURNED ON. DURING CHECK IT WAS DETECTED A WIRE BROKEN IN THE NOSE LANDING GEAR DOWN SENSOR RECEPTACLE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE RECEPTACLE R5-1157 AND WIRE WAS ROUTED IAW SDM 32-61-0, TESTS CORRECT. (M) 2L72 4F A6WE 20040324000332004032400033EA 2004 3 24 04078710 120040318A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040324000382004032400038NM 2004 3 24 SWAA040808 120040316A3350D71702001 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29737JW 27869 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHTS AT L1 DOOR AND R1 DOOR, EEPLS AT ROW 2ABC TO 5ABC INOP. REMOVED AND REPLACED FWD RT BATTERY PACK PER MM. 2L72 4F RTA16WE 20040324000402004032400040 2004 3 24 SWAA040810 420040316A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040324000612004032400061CE 2004 3 24 DXTA200400261 120040312A3241 WARNING LIGHT CESSNA500 560CESSNA 2076750CE ANTI SKID SYS ILLUMINATED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07302QS 5600402 ON APPROACH POWER BRAKE LOW PRESS AND ANTI-SKID INOP, ANNUNCIATORS ILLUMINATED. EMERGENCY CHECKLIST PROCEDURE WAS COMPLIED WITH AND ANNUNCIATOR REMAINED ILLUMINATED. LANDING WAS MADE AND BRAKING ACCOMPLISHED USING BACK UP PNEUMATIC SYSTEM. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040324000632004032400063NM 2004 3 24 AALA20040329 120040308A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21771AN 29579 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 AND 24 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS AT SEAT ROWS 20 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040324000702004032400070NM 2004 3 24 SWAA040826 120040317A3350311500 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED C2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED FWD LIGHT LENS PER MM. 2L72 4F RTA16WE 20040324000742004032400074NM 2004 3 24 SWAA040820 120040317A53156525966 FLOORBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SPV, FOUND FLOORBEAM AT BS 312, LBL 11 CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F A16WE 20040324000752004032400075NM 2004 3 24 SWAA040821 120040317A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD AT WS 135.5, BETWEEN S-2 AND S-3, CRACKED. REPAIRED LT WING RIB CHORD PER ACO. 2L72 4F RTA16WE 20040324000792004032400079 2004 3 24 SWIA200413002 420040306A22106225798013 CONTROL PANEL EMB 120 EMB120ER 3260203SO FLT CONTROL MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07251YV8127 8127 120251 FD FLAG CAPTAIN SIDE. REPLACED CONTROL PANEL (FCP65) IAW 22-10-03. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040324000962004032400096SO 2004 3 24 SWIA200413011 120040309A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07284YV8210 8210 120284 ONE STRIP OF FLOOR EMERGENCY LIGHTING INOP. REMOVED MIDDLE ELBP AND INSTALLED SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324001082004032400108EA 2004 3 24 SWIA200413016 120040312A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07938SW 7741 EMERGENCY LIGHTS STRIP INSIDE CABIN HAS APPROX 12 FEET OF LIGHTS NOT WORKING BETWEEN ROW 2 AND ROW 5. INSTALLED SERVICEABLE CONNECTOR P38LZ AT ROW 5. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040324001232004032400123WP 2004 3 24 AALA20040323 120040306A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21219AA 49171 ORD - EMERGENCY CEILING LIGHTS BETWEEN ROWS 28 AND 30 INOPERATIVE. REPLACED BATTERY PACK AT B5-107 FOR EMERGENCY CEILING LIGHTS BETWEEN ROWS 28 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001352004032400135 2004 3 24 AALA20040350 420040314A2565D29982125 SLIDE DOUG DC9 DC982 3022082WP GALLEY DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21578AA 53155 DFW - MAINTENANCE ARRIVED AT AIRCRAFT AND FOUND FORWARD GALLEY SERVICE DOOR SLIDE PACK HANGING OUTSIDE THE AIRCRAFT WITH THE GIRT BAR STILL HOOKED. THE SLIDE CAME OUT OF THE SLIDE PACK BUT DID NOT DEPLOY. REPLACED SLIDE FOR THE FORWARD GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001382004032400138EA 2004 3 24 SWIA200413040 120040220A5246 DOOR CNDAIRCL600 CL6002B19 1900309EA WATER SERVICE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 RIGHT EXTERIOR AFT FUSELAGE, AFT POTABLE WATER SERVICE DOOR, DOOR PANEL REBATE IS CRACKED IN AFT LOWER CORNER. DISCOVERED DURIING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ SRM 53-00-31 FIG 103 SHEETS 1 & 3. 2L72 4F RTA21EA 20040324001472004032400147NE 2004 3 24 AALA20040352 220040312A7261 O-RING DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FILTER HOUSING CUT A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21435AA 49453 725760 STL - INFLIGHT T1986/12 RIGHT ENGINE OIL QUANTITY DECREASED TO ZERO. RIGHT ENGINE LOW PRESSURE LIGHT ILLUMINATED AND PRESSURE DECREASED TOWARDS ZERO. SHUTDOWN RIGHT ENGINE PER QRH PROCEDURE. ENGINE WINDMILLED NORMALLY FOR 15 MINUTES. LANDED STL WITHOUT INCIDENT. FOUND RIGHT OIL FILTER HOUSING O-RING CUT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20040324001482004032400148WP 2004 3 24 AALA20040345 120040314A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21411AA 49322 SFO - OVERHEAD EMERGENCY LIGHT ABOVE AIRSTAIR WALKWAY INOPERATIVE. RESET BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT ABOVE AIRSTAIR WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001512004032400151EU 2004 3 24 AALA20040349 120040314A3397 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW2140064 507 MIA - EMERGENCY LIGHT AT SEAT 14G INOPERATIVE. FOUND LOOSE CONNECTION. RESET LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 14G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040324001552004032400155SO 2004 3 24 SWIA200412977 120040125A5712 RIB EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RIGHT FORWARD MOST OUTBOARD SMALL FUEL PANEL, RIB INSIDE WING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT MOST OUTBOARD NOSE RIB WEB IAW SRM 120 57-20-07 PG 210 FIG 203. 2L72 4T RTA31SO 20040324001562004032400156SO 2004 3 24 SWIA200412979 120040125A5415 CRADLE EMB 120 EMB120ER 3260203SO NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RIGHT OUTBOARD EXHAUST CRADLE OUTBOARD CORNER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOUBLER IAW EMB SRM 51-10-02. 2L72 4T RTA31SO 20040324001572004032400157SO 2004 3 24 SWIA200412980 120040212A5310 WINDOW FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07233SW 120307 COCKPIT LEFT SIDE FRAME 12 SUPPORT AFT/MIDDLE OF DV WINDOW FRAME. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED COCKPIT LEFT SIDE FRAME 12 SUPPORT AFT/MIDDLE OF DV WINDOW FRAME WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2L72 4T RTA31SO 20040324001602004032400160NM 2004 3 24 04069402 120040309A291342152 PUMP DORNERDO32 DO328300 NM HYD SYSTEM INOPERATIVE A VTZAB EMER. DESCENT S AFFECT SYSTEMS APAPPROACH 1 EA27402FJ 3147 DURING APPROACH OF FLIGHT 6127 TO BOS CREW REPORTED A HYDRAULIC SYSTEM A FAILURE. THE CREW MANUALLY DEPLOYED THE LANDING GEAR AND FLIGHT LANDED WITHOUT INCIDENT. THE MAIN SYSTEM A PUMP WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040324001612004032400161EA 2004 3 24 04081691 120040321A261324403615 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA MLG WW INOPERATIVE A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27691BR 7740 DURING APPROACH OF FLIGHT 7256 CREW RECEIVED A MLG BAY OVERHEAT INDICATION AND DECLARED AN EMERGENCY FLIGHT LANDED UNEVENTFULLY. THE LEFT HAND MAIN LANDING GEAR LOOP DETECTOR WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001622004032400162EU 2004 3 24 MALA040269 120040312A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438XJ 340B438 DURING INSPECTION IN LCQ, RIGHT ICE SHIELDS AND THREE EXISTING SKIN REPAIRS WERE REMOVED IN ORDER TO EVALUATE ALL DENTS, AND CUTOUTS. SIXTEEN NEW DENTS WERE FOUND, AND TWO OF THOSE WERE CUT OUT. TEN OF THE DENTS WERE TO CLOSE TO MEET SRM SPACING REQUIREMENTS. DOUBLER & TRIPLER REPAIR WAS INSTALLED TO STA 339 TO 351 IAW SAAB 340 SRM 53-70-10-2 & EO S53208. A/C RELEASE DATE 3/14/2004. 2L72 4T RTA52EU 20040324001672004032400167EU 2004 3 24 AALA20040313 120040305A3320D77311001 BALLAST AIRBUS300 A300B4605R 3930308EU CABIN LIGHTS OVERHEATED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2125071 514 INFLIGHT T882/5 FLIGHT ATTENDANT REPORTED SMOKE AND ELECTRICAL ODOR NEAR SEAT 15G. SHUT OFF OVERHEAD LIGHT SYSTEM AND SMOKE AND ELECTRICAL ODOR WENT AWAY. FOUND BALLAST AT 15 CENTER HOT AND SIGNS OF OVERHEAT. REPLACED BALLAST AND INSPECTED ALL BALLAST LIGHT ASSEMBLIES FROM ROW 10 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040324001682004032400168EU 2004 3 24 AALA20040314 120040304A5311 FRAME AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 TUL - FRAME 18 IS CORRODED IN A 16 INCH AREA BETWEEN STRINGER 54 RIGHT AND 53 LEFT. REMOVED CORRODED SECTION OF FRAME 18 BETWEEN STRINGER 54 RIGHT AND 53 LEFT AND REPAIRED PER ESO 30595. 2L72 4F RTA35EU 20040324001702004032400170WP 2004 3 24 AALA20040309 120040304A3397 TERMINAL DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21245AA 49257 SFO - EMERGENCY LIGHT AT SEATS 23D AND 26D INOPERATIVE. FOUND LOOSE TERMINAL LUG AT BATTERY PACK. TIGHTENED TERMINAL LUG AT BATTERY PACK FOR EMERGENCY LIGHTS AT 23D AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001722004032400172SO 2004 3 24 SWIA200412984 120040226A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07583SW 120351 EMERGENCY LIGHT OUT ON FLOOR STRIP. REMOVED AND REPLACED LIGHT BULB ON EMERGENCY LIGHT FLOOR STRIP. 2L72 4T RTA31SO 20040324001732004032400173SO 2004 3 24 SWIA200412985 120040301A3350 LIGHT EMB 120 EMB120ER 3260203SO ROW 6A BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07582SW 120350 EMERGENCY SIDEWALL LIGHT AT 6A BROKEN. REPLACED LIGHT FIXTURE. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324001742004032400174 2004 3 24 SWIA200412986 420040302A22156225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07234SW5874 5874 120308 WHEN AUTOPILOT ENGAGED ON FIRST OFFICER'S SIDE, THE AIRCRAFT ABRUPTLY LEVELS OFF 300 FEET PRIOR TO SELECTED ALTITUDE. REPLACED ELEVATOR SERVO AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-10-00. 2L72 4T RTA31SO 20040324001762004032400176EA 2004 3 24 04075643 120040315A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27643BR 7363 DURING INSPECTION THE RIGHT HAND FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001782004032400178EA 2004 3 24 04075710 120040315A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE RIGHT HAND FORWARD EMERGENCY EXIT LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001802004032400180NM 2004 3 24 04077426 120040317A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27426FJ 3190 DURING INSPECTION THE FORWARD OVERHEAD CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040324001812004032400181NM 2004 3 24 04078416 120040318A3397 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27416FJ 3171 DURING INSPECTION THE FORWARD AND CENTER EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE CONNECTOR WAS FOUND LOOSE AND RECONNECTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040324001822004032400182EA 2004 3 24 04078657 120040318A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27657BR 7491 DURING INSPECTION THE NR 2 EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001842004032400184EA 2004 3 24 04082633 120040322A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE RIGHT HAND AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001862004032400186EU 2004 3 24 MALA040276 120040318A54107271110271 DOOR SAAB SF340 340B 7860101EU RT NACELLE OPEN A MALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL15366PX 340B267 RIGHT COWLING POPPED OPEN INFLIGHT. AIR RETURN TO MEM. REPLACED LEFT AND RIGHT FWD COWLINGS ON RIGHT ENGINE WITH SERVICEABLE UNITS. RIGHT P/N 7271110-271, LEFT P/N 7271110-269. GOOD FOR SERVICE. 2L72 4T RTA52EU 20040324001892004032400189EA 2004 3 24 04080685 120040320A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27685BR 7712 DURING INSPECTION THE EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. THE LIGHT STRIP WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001922004032400192NM 2004 3 24 04FDEA00370 120040209A5340A5A7114511 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CTR CARGO - LOWER BILGE AREA LONGERON NR 49 RIGHT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKS. CRACKED SPLICE AT CENTER CARGO LOWER BILGE AREA LONGERON 49 RT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED SPLICE AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040324001932004032400193NM 2004 3 24 04FDEA00369 120040209A5340A5A7114511 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CTR CARGO - LOWER BILGE AREA LONGERON 49 LT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKS AT TWO PLACES. CRACK SPLICE AT CENTER CARGO LOWER BILGE AREA LONGERON 49 LT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED SPLICE AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040325000012004032500001EU 2004 3 25 ASOA04104 120040209A2530L1750103 COFFEEMAKER AEROSPATR72 ATR72 EU GALLEY BURNED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11640AS 405 FLT 4313 - DURING APPROACH INTO ATL FROM MGM, THE FLIGHT ATTENDANT NOTICED AN ELECTRICAL ODOR IN THE CABIN. THE CREW REQUESTED EMERGENCY VEHICLES AS A PRECAUTION AND THE TOWER DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE FOUND THE LEFT SIDE COFFEE POT PLUG BURNED AND WET. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE COFFEE POT, CLEANED AND DRIED THE COFFEE POT RECEPTACLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040325000022004032500002EA 2004 3 25 ASOA04123 120040214A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621 ON THE RIGHT SIDE IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040325000042004032500004EA 2004 3 25 ASOA04115 120040211A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CLIP AT FS 484, RBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040325000072004032500007EA 2004 3 25 ASOA04125 120040214A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE ON THE LEFT SIDE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLE ON THE LEFT SIDE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040325000092004032500009EA 2004 3 25 ASOA04120 120040213A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000122004032500012EA 2004 3 25 ASOA04127 120040215A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 ON THE LEFT SIDE IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040325000132004032500013EA 2004 3 25 ASOA04116 120040211A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040325000152004032500015EA 2004 3 25 ASOA04132 120040215A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSLAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKET AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD BRACKET AT FS 280, LBL 9 IAW SRM 51-42-21 AND 51-41-02. (M) 2L72 4F RTA21EA 20040325000172004032500017EA 2004 3 25 ASOA04128 120040215A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040325000182004032500018EA 2004 3 25 ASOA04131 120040215A3260895303 PSEU CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11712EV 10074 FLT 4580 - DURING CLIMB-OUT FROM ATL-TOL, AFTER GEAR RETRACTION THE CREW RECEIVED PROXIMITY SYSTEM CAUTION AND PROXIMITY SYSTEM TWO FAULT STATUS MESSAGES. QRH PROCEDURES WERE COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000192004032500019EA 2004 3 25 ASOA04106 120040209A5210601R9455011 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 FLT 4628 - DURNIG A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WOULD NOT CLOSE ALL THE WAY. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SERVO MOTOR ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000202004032500020EA 2004 3 25 ASOA04129 120040215A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKET AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD BRACKET AT FS 280, RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040325000242004032500024NM 2004 3 25 USA2004F00019 120040302A3233654610912 ARM BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE LT MLG ACTUATOR CRACKED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19355US59000 23558 UPON GEAR RETRACTION, CREW HEARD A LOUD THRUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. LT MAIN LANDING GEAR ACTUATOR BEAM ARM FOUND CRACKED. REAR MAIN LANDING GEAR SUPPORT BEAM DAMAGED. BEAM ARM HAD 59,000 LANDINGS. LAST ULTRASONIC INSPECTION WAS DEC, 2003. PARTS TO BE ANALLYZED. 2L72 4F4 FRTA16WE E2GL 20040325000512004032500051NE 2004 3 25 HEEA093480 220040206A73200164348810 FUEL CONTROL SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE NR 2 ENGINE FAILED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03223421877 760096 3041 NR 2 ENGINE HIGH SIDE FAILURE. MAINTENANCE REPLACED FUEL CONTROL. 1G72 3U3 U H1NE E19EU 20040325000522004032500052NE 2004 3 25 HEEA093481 120040129A67302376 PRESSURE SWITCH SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE ROTOR SERVO INOPERATIVE B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03278X 760440 IB TO GRAND ISLE THE NR 1 SERVO CAUTION LIGHT ILLUMINATED. LANDED WITHOUT INCIDENT. 1G72 3U3 U H1NE E19EU 20040325000662004032500066 2004 3 25 BAQA093002 420040220A3416D120P2T ENCODER AEROSPAS355 AS355F 8680806EU ALLSN 250C 250C20 03013GL ALTIMETER OUT OF TOLERANCEB BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03912KY 5500 ENCODER UNIT IS OUT OF TOLERANCE. REPLACED WITH SERVICABLE UNIT (S/N 33768) 03/02/2004 1G72 3U3 U H11EU E4CE 20040325000672004032500067EU 2004 3 25 BAQA093508 120040216A7160430110217 ACTUATOR BOLKMS117 BK117B1 5626012EU ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601EH 7181 MECHANIC WAS UNABLE TO ADJUST FLOW OF ACTUATOR. REPLACED WITH SERVICABLE UNIT FROM ITS 03/05/2004 1G72 3U H13EU 20040325000732004032500073NE 2004 3 25 AC2A093322 120040120A67307665009805110 SERVO SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL ROTOR BROKEN E AC2AK NONE O OTHER ININSP/MAINT 1 SO077266K611 760283 PILOT VALVE INPUT ROD TURN BARREL HAD BROKEN RETAINING BOLT. THIS ENABLED THE BARREL TO TURN WHICH COULD ALTER THE SERVO TIMING. REPLACED MAIN ROTOR ASSEMBLY. 1G72 3U3 U H1NE E1GL 20040325000762004032500076SW 2004 3 25 AC2A093325 120040203A6410430310101107 RESTRAINT BELL 430 430 1182150SW ALLSN 250C 250C* GL BLUE BLADE DEBONDED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH3141 49037 RESTRAINT DISBONDED. PIN DISBONDED FROM RESTRAINT. RETAINING PLATES WERE DAMAGED. REPLACED PART 1G72 3U3 URTH9SW E4CE 20040325000792004032500079SW 2004 3 25 AC2A093329 120040217A6220430310101107 RESTRAINT BELL 430 430 1182150SW MAIN ROTOR DEBONDED E AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CT 49089 RESTRAINT DISBONDED. SHEAR RESTRAINT DISBONDED AT PIN. REPLACED RESTRAINT. 1G72 3U RTH9SW 20040325000812004032500081NE 2004 3 25 BAQA093257 220040212A73130319307840 INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE NR 1 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME502 0143 30166 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/24/2004 1G72 3U3 U H88EU E19EU 20040323000242004032300024EU 2004 3 23 BAQA092592 120040208A249745023502 MASTER SWITCH UROCOPEC135 EC135T1 5620026EU NR 2 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME2001 0143 NR 2 ENGINE WILL NOT START, BOX WILL NOT PASS SELF-TEST. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1G72 3U H88EU 20040323000292004032300029EU 2004 3 23 BAQA092483 120040130A65204639003007 GEARBOX BOLKMS117 BK117A1 5626010EU TAIL ROTOR MAKING METAL B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP2997 7249 TAIL ROTOR GEARBOX REMOVED DUE TO METAL GENERATION, AND CASE HAS PITTING ON IT. HARDCARDS ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 02/10/2004 1G72 3U H13EU 20040323000482004032300048EU 2004 3 23 ASOA04075 120040130A7712311649902 PROBE AEROSPATR72 ATR72212 8680945EU ENGINE INOPERATIVE A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO11535AS 464 FLT 4862 - DURING DESCENT INTO ATL FROM TYS, A TORQUE FLUCTUATION WAS NOTICED ON THE RIGHT ENGINE. THE CREW REDUCED THE TORQUE TO APPROXIMATELY FIFTY PERCENT AND THE RIGHT ENGINE CONTINUED TO FLUCTUATE BETWEEN 0 TO 102 PERCENT. THE CREW THEN REDUCED THE TORQUE TO FLIGHT IDLE AND IT REMAINED CONSTANT. THE TOWER DECLARED AN EMERGENCY AND ROLLED THE EMERGENCY VEHICLES AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT TORQUE PICK-UP PROBE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040323000502004032300050EA 2004 3 23 ASOA04084 120040202A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 FLT 4228 - DURNIG A GROUND INSPECTION IN DFW, THE BOTTOM STAIR CONTROL ROD ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000572004032300057GL 2004 3 23 UIEA200400022 120040219A2120 ODOR BOEING747 747300 GL CABIN DETECTED A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA1524837 24837 ONCE AIRCRAFT LANDED, NOTICEABLE FUEL FUMES IN AIRCRAFT AND ONCE L1 DOOR WAS OPENED THE GROUND HANDLER NOTICED FUMES TOO. CHECKED ENGINES FOR ANY EVIDENCE OF BIRD STRIKE OR FOD DAMAGE IAW MM 05-51-14, NIL DAMAGE FOUND. CARRIED OTU GENERAL VISUAL INSPECTION OF APU AREA AND FUEL TANK, NIL EVIDENCE OF LEAKAGE FOUND. (M) 2L74 4F RTA20WE 20040323000712004032300071NM 2004 3 23 AALA20040362 120040310A2780 CONTROL UNIT BOEING757 757223 1384957NM LE FLAPS INOPERATIVE A AALAO OTHER J WARNING INDICATION APAPPROACH 1 SW21661AA 25295 POS INFLIGHT T1819/10 ON APPROACH LEADING EDGE FLAP ASYMMETRY EICAS MESSAGE. FLAPS JAMMED AT ONE DEGREE. USED ALTERNATE METHOD TO GET FLAPS DOWN TO 20. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK FSEU WITH NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040323000782004032300078WP 2004 3 23 ABXA040098 120040301A534049133251 FITTING DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 AFT ACCESSORY LONGERON 11 RIGHT END FITTING EXFOLIATED JUST FORWARD OF CANTED FRAME. REPLACED LONGERON 11 RIGHT END FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040323000812004032300081WP 2004 3 23 ABXA040100 120040302A532029223681 BRACKET DOUG DC9 DC941 302207NWP CARGO TRACK CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 541 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040323000842004032300084NM 2004 3 23 UPS04442026 120040313A3350 BATTERY PACK BOEING747 747200 1384847NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01528UP 1 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BATTERY DEAD. REMOVED AND REPLACED 2 EMERGENCY LIGHT POWER PACKS, OPS CHECK GOOD PER AMM 33-51-04. 2L74 4F RTA20WE 20040323000882004032300088WP 2004 3 23 ABXA040102 120040302A532029223681 BRACKET DOUG DC9 DC941 302207NWP CARGO TRACK CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 446 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040323001002004032300100NM 2004 3 23 CALA0400246 120040313A5230 SKIN BOEING737 737824 13844BZNM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714237 28802 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED IN CENTER FORWARD SECTION. REPAIRED IAW ECRA 5231-01050. 2L72 4F RTA16WE 20040323001022004032300102NM 2004 3 23 CALA0400248 120040315A5330 SKIN BOEING777 777224 1385225NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727015 28678 INSPECTION FOUND 2 DENTS IN FUSELAGE SKIN AT BS 676, STRINGER 22L-28L. REPAIRED IAW SRM 53-00-01, REPAIR 7 AND ECRA 5330-01394. 2L72 4F RTT00001SE 20040323001192004032300119EU 2004 3 23 MALA040265 120040308A3231 DOOR BAC 146 AVRO146RJ85A1500097EU LT MLG OBSTRUCTED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15509XJ E2321 LT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR UP SELECTION, NO ABNORMAL HANDLING OR VIBRATION NOTED. FOUND GAP AT AFT EDGE OF LEFT MLG DOOR TO BE LESS THAN MIN CLEARANCES, TRIMMED LEFT AFT FUSE TO GEAR DOOR FAIRING. FOUND GAP BETWEEN AFT PART OF GEAR DOOR & FUSELAGE FAIRING TO BE LESS THAN MINIMUM PER AMM 32-16-21 CAUSING DOOR TO OVERLAP FAIRING WHEN UNDER AIR LOAD TRIMMED FAIRING AS REQ'D TO GET MINIMUM CLEARANCE BETWEEN GEAR DOOR & FUSELAGE AS STATED IN 32-10-21. 2H74 4F RTA49EU 20040323001222004032300122SO 2004 3 23 C2XA04IA033 120040313A335014532843401 PANEL EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716541 145542 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT MESSAGE ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. THE POWER WAS RESET AND THE MESSAGE INITIALLY CLEARED BUT ILLUMINATED AGAIN AFTER A SHORT PERIOD OF TIME. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040323001242004032300124SO 2004 3 23 C2XA04TY053 120040319A361014531675409 TUBE EMB 145 EMB145LR 3260212SO NR 1 ENGINE LOOSE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714558 145598 TYS DURING CLIMBOUT THE CREW GOT A INDICATION THAT THE NR 1 ENG HAD A BLEED LEAK AND RETURNED TO THE BLOCK. MAINT FOUND A LOOSE BURST DETECT LINE ON THE LT LEADING EDGE. TIGHTENED IAW EMB135/145 MM 20-10-03. PERFORMED AIRBLEED OPS CHECK IAW 145 AMM 36-00-00-700-803A, PERFORMED ANTI-ICE TEST IAW EMB 145 AMM 30-00-00-700-802A, PERFORMED COOLING PACK TEST IAW EMB 145 MM 21-51-00-700-802A. ALL WORK WAS ACCOMPLISHED AND ALL CHECKS WERE POSITIVE AND WAS RELEASED FOR TEST FLIGHT AND TEST FLIGHT WAS GOOD. ALL RECORDED ON LOG PG 919465 AND 602 NR 743788 FOR CORRECTIVE ACTION. A/C WAS RELEASED FOR REVENUE SERVICE. 2L72 4T RTT00011AT 20040323001292004032300129SO 2004 3 23 C2XA04SH166 120040317A531514525523003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK, THE T-SECTION IN THE LOWER CARGO DOOR CUTOUT AT FRAME 67 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED T-SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040323001312004032300131EU 2004 3 23 MALA040260 120040223A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU CRACKED CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15532XJ E2366 DURING INSPECTION IN LCQ, FRAME 18 FLOORBEAM CRACKED AT RCL 42 STA 216.65. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND ANGLES IAW MESABA EO A53155. A/C RELEASE DATE 3/10/04. 2H74 4F RTA49EU 20040323001332004032300133EU 2004 3 23 MALA040263 120040223A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15532XJ E2366 DURING INSPECTION IN LCQ, SEAT TRACK NR 4 CORRODED FRAME 18-20. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 3/10/04. 2H74 4F RTA49EU 20040323001362004032300136NM 2004 3 23 HNAA0400023 120040315A3320336710 BALLAST DHAV DHC8 DHC8102 2809003NM CABIN LIGHTS BURNED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07942HA 163 BURNING SMELL IN CABIN. MX FOUND SIDEWALL LIGHT BALLAST AT 4DF SMOKING. DISCONNECTED AND SECURED POWER WIRE TO BALLAST IAW EO 8-33-04-0156. INSPECTED FOR HIDDEN DAMAGE, NO DEFECTS NOTED. 2H72 4T RTA13NM 20040324000202004032400020NE 2004 3 24 MEX2004067 220040218A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LEFT FOD A ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23216AM 49586 P718411 FLT 106 - GDL-MEX - DURING TRANSIT CHECK TWO BLADES ON LEFT ENGINE AND NOISE SUPPRESSOR WERE DETECTED WITH DAMAGE BY FOD. THE DAMAGES WERE WITHIN LIMITS IAW MM 72-33-22. THE BLADES WERE REPAIRED IAW MM 72-33-22. THE NON ROUTINE CARD NR A0055136 WAS ISSUED TO OPERATE THE ENGINE FOR UP TO 24 FLIGHT HOURS BEFORE THE VIBRATION CHECK IS ACCOMPLISHED IAW MM 72-00-00. DURING OVERNIGHT SERVICE A BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 12-60-03, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20040324000222004032400022WP 2004 3 24 MEX2004055 120040212A79971163P0041 SWITCH DOUG DC9 DC987 3022087WP OIL FILTER FAILED A ASMFA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW23205AM 49405 FLT 944 - MEX-CUN - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT VER AS A CONSEQUENCE DURING FLIGHT, THE RIGHT OIL STRAINER CLOGGING LIGHT TURNED ON. NO METALLIC BURRS WERE DETECTED DURING MAIN FILTER. LP5 AND LP6 OIL RESTRICTORS WERE CLEANED WITH AIR BUT FAILURE CONTINUED DURING ENGINES RUNNING TEST. ELECTRICAL CONNECTOR ON THE OIL FILTER TRANSMITTER WAS DISCONNECTED AND FAIL WAS DEFERRED IAW MEL 79-5 CAT B. AT CUN, THE SWITCH WAS REPLACED AND OIL FILTER WAS CHECKED AND BLOW WITH AIR IAW MM 79-30-00. DURING OVERNIGHT SERVICE, OIL MAIN FILTER WAS REPLACED AN ALL THE SYSTEM WAS CHECKED AND CLEANED, ALL CORRECT. (M) 2L72 4F RTA6WE 20040324000302004032400030WP 2004 3 24 MEX2004057 120040214A3260 SENSOR DOUG DC9 DC982 3022082WP MLG FAILED A ASMFL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW23505MD 49149 FLT 256 - MEX-HMO - DURNIG APPROACH THE RED MAIN LANDING GEAR LIGHT TURNED ON. DURING REVISION IN HANGAR THE MLG SENSOR WAS CALIBRATED IAW MM 32-60-05 AND CHAFING BETWEEN HYDRAULIC LINE AND BRAKE CONNECTOR WAS CORRECTED IAW MM 32-11-02. (M) 2L72 4F A6WE 20040324000352004032400035WP 2004 3 24 IXXA0400014O 120040316A2731 CONTROL CABLE DOUG DC8 DC871F 302199DWP ELEVATOR TRIM LOOSE A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW11825BX849241874 45978 DURING CLIMB FROM KLAX TO KTOL, AT LOW SPEEDS, CREW HAD ELEVATOR VIBRATION. VIBRATION WENT AWAY WHEN AIRCRAFT REACHED 280 KTS SPEED. CREW CONTINUED FLIGHT TO KTOL. AN INVESTIGATION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. LEFT HAND ELEVATOR CONTROL TAB HAD TRAILING EDGE PLAY. MAINTENANCE FOUND LEFT ELEVATOR TRIM CABLE TENSION LOW. ADJUSTED AND INSPECTED ELEVATOR PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK WAS GOOD AND TEST FLIGHT WAS NOT REQUIRED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040324000432004032400043NM 2004 3 24 SWAA040813 120040316A53106546540 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616, RBL 71, WL 208. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040324000472004032400047NM 2004 3 24 DHL2004750007 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 620. CUT OUT DAMAGED AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1, FABRICATED DOUBLER MAT 7075-T6 .063 PO 900489, DIM 3.75 X 7.625 INCH IAW B727 SRM 51-40-3 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER ON UPPER CABIN RT SIDE BETWEEN STR 16R AND 17R FRAME IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040324000652004032400065WP 2004 3 24 AALA20040332 120040308A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21461AA 49566 DFW AFT CEILING PANEL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK CHARGER FOR AFT CEILING PANEL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324000862004032400086SO 2004 3 24 SWIA200413009 120040308A2750 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07186SW 120034 DURING TAKEOFF RUN JUST AFTER POWER UP, A SINGLE CHIME WITH FLAP, CONTROL FAULT, ADVANCED SWS. PERFORMED THE ABORT AND RETURNED TO THE GATE. RERACKED FLAP CONTROL UNIT PER MAINT MM 22-50-06. CYCLED POWER, PERFORMED HIGH SPEED TAXI WITH CREW. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324000952004032400095 2004 3 24 SWIA200413010 420040309A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07188SW 120039 STALL WARNING LIGHT ON MAP ILLUMINATED IN FLIGHT. TURNED OFF SYSTEM 2 WARNING SWITCH, STILL WON`T RESET, NO LIGHT ON LOWER PANEL BUT MAP LIGHT STAYS ILLUMINATED. REMOVED AND REPLACED STALL WARNING CONTROL PANEL. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324000982004032400098 2004 3 24 SWIA200413013 420040310A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07237SW7391 7391 120314 AUTO PILOT, EITHER SIDE, WILL NOT HOLD ALTITUDE. REPLACED APP-65 WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040324000992004032400099EU 2004 3 24 MALA040270 120040313A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING INSPECTION IN LCQ, LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/17/2004. 2L72 4T RTA52EU 20040324001192004032400119WP 2004 3 24 AALA20040326 120040307A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW217547A 53029 DFW - EMERGENCY SIDE WALL LIGHTS AT AFT STAIRWAY INOPERATIVE. REPAIRED BROKEN WIRE IN TAIL CONE AREA FOR STAIRWAY SIDE WALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001202004032400120NM 2004 3 24 AALA20040327 120040306A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21784AN 29588 DFW - EMERGENCY ESCAPE PATH LIGHTS AT L-1 CLOSET INOPERATIVE. REPLACED LIGHT FOR EMERGENCY ESCAPE PATH AT L1 CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040324001272004032400127WP 2004 3 24 AALA20040319 120040305A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217520A 49897 DFW - EMERGENCY LIGHTS IN TAIL CONE AREA INOPERATIVE. REPLACED BATTERY PACK AT B5-28 FOR EMERGENCY LIGHTS IN TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001372004032400137EA 2004 3 24 SWIA200413039 120040220A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA DOOR FRAME CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT TRANSVERSE BEAM ATTACH ANGLE FOR CARGO DOOR STOPS IS CRACKED AT FS 605.00 LBL 43.00. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 AND MM 20-21-00 & RII 53-401. 2L72 4F RTA21EA 20040324001392004032400139EA 2004 3 24 SWIA200413041 120040227A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07446SW 7666 DISCOVERED DURING C-CHECK INSPECTION, FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00 & RII 53-401. 2L72 4F RTA21EA 20040324001652004032400165WP 2004 3 24 AALA20040310 120040305A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 MIA - EMERGENCY EXIT LIGHTS ABOVE LEFT AND RIGHT HAND OVERWING EXIT INOPERATIVE. RESET BATTERY PACKS FOR EMERGENCY EXIT LIGHTS ABOVE LEFT AND RIGHT HAND OVEWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001712004032400171WP 2004 3 24 AALA20040312 120040304A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2173444 49470 DEN - EMERGENCY LIGHTS AT MID CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-105 FOR EMERGENCY LIGHTS AT MID CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001752004032400175NM 2004 3 24 04075426 120040315A3350321430 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27426FJ 3190 DURING INSPECTION OF THE AIRCRAFT SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERIES WERE FOUND DISCHARGED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040324001882004032400188EU 2004 3 24 MALA040275 120040317A3260MS2740017 RELAY BAC 146 AVRO146RJ85A1500097EU MLG FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15530XJ E2364 RIGHT GEAR RED ILLUMINATED WITH GEAR UP AFTER TAKEOFF. GEAR EXTENDED NORMALLY FOR LANDING. MX REMOVED AND REPLACED RELAY GF7 AND PCB GH21. RELAY P/N MS27400-17, PCB P/N 8-060-02, S/N OFF A187117, S/N ON A187898. SWUNG GEARS SEVERAL TIMES IAW AMM 32-30-00. NO DEFECTS NOTED. 2H74 4F RTA49EU 20040324001902004032400190 2004 3 24 P5CA0401060 420040317A34207057V9 INDICATOR BOEING747 747341 13848AMNM ATTITUDE FAILED A P5CAO OTHER O OTHER CRCRUISE 1 WP23354MC 23394 STANDBY ATTITUDE INDICATOR ROLLS 10 DEG RIGHT AND LEFT IN LEVEL FLIGHT. REMOVED AND REPLACED STBY AI, PERFORMED CHECK PER 34-24-00. SYSTEM OPS CHECKS NORMAL. 2L74 4F RTA20WE 20040325000052004032500005EA 2004 3 25 ASOA04117 120040212A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11826AS 7210 DURNG HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000082004032500008EA 2004 3 25 ASOA04121 120040212A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE TWO AFT EMERGENCY CEILING LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE TWO AFT EMERGENCY CEILING LIGHTS. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20040325000102004032500010EA 2004 3 25 ASOA04119 120040213A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11914EV 7752 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE ATTACHMENT LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325001002004032500100EU 2004 3 25 BAQA093307 120040225A6330L633M2010103 MOUNT UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE GEARBOX OUT OF LIMITS B BAQAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA03911NH142 0273 EXCESSIVE AIRFRAME VIBRATION, OUT OF LIMITS, REMOVED FROM RT AFT POSITION. REPLACED WITH SERVICABLE UNIT. 02/27/2004 1G72 3U3 U H88EU E19EU 20040325001072004032500107SW 2004 3 25 Y3AR093654 120040222A5510206021103106 CASTING CLARK 1000 1000CLARK 2230102SW HORIZONTAL STAB CRACKED B Y3ARO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO2092 BP364 HORZ STAB WAS REMOVED FOR DAMAGE TO BOOM ASSY. WHEN FIN ASSY WAS REMOVED TOP AFT 5. 1Q71 3R 2A6 20040325001092004032500109SW 2004 3 25 HEEA093478 120040125A7931 WARNING LIGHT BELL 214 214ST 1182106SW OIL SYSTEM ILLUMINATED B HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW035748M 28102 45 MINUTES AFTER TAKEOFF, PILOT REPORTED LOW PRESSURE READING ON NR 2 OIL PRESSURE GAUGE. RETURNED TO MCY. 2G72 4U H10SW 20040325001152004032500115EU 2004 3 25 BAQA093318 120040219A6330L633M2010105 MOUNT UROCOPEC135 EC135P2 5620027EU M/R GEARBOX CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135WJ37 0287 MAIN ROTOR GEARBOX MOUNT HAS A CRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1G72 3U H88EU 20040325001192004032500119EU 2004 3 25 BAQA093299 120040224A6240L771M40C1005 INDICATOR UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206A NE TRIPLE TACH FAILED B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03603ME179 0284 SELF-TEST ON POWER UP FAILED MULTIPLE TIMES. REPLACED WITH SERVICABLE UNIT. 03/01/2004 1G72 3U3 U H88EU E42NE 20040325001282004032500128EU 2004 3 25 BAQA093489 120040229A243245043006 MASTER BOX UROCOPEC135 EC135P2 5620027EU WILL NOT TEST B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03135WJ59 0287 MASTERBOX WILL NOT SELF TEST. REPLACED WITH SERVICEABLE UNIT. 03/05/2004 1G72 3U H88EU 20040325001292004032500129EU 2004 3 25 BAQA093005 120040222A6330L633M2010105A001MOUNT UROCOPEC135 EC135P1 8680990EU M/R GEARBOX COLLAPSED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF47 0140 MAIN ROTOR GEARBOX MOUNT COLLAPSED, AND FLAT. PART ONLY LASTED 46.5 HOURS. REPLACED WITH SERVICEABLE UNIT. 03/01/2004 1G72 3U O H88EU 20040325001332004032500133EU 2004 3 25 BAQA093635 120040304A6310117151321 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG4955 7506 WARRANTY REPAIR/EXCHANGE : SINCE JULY 2, 1996 BLADE HAS FLOWN ONLY 346.1 HOURS. BLADE HAS ZERO HOURS AFTER BEING REMOVED FOR SUSPECTED COWLING STRIKE ON JULY 9, 1998 (A/C 7109). BLADE REPAIRED THREE TIMES SINCE 1998 AND BLADE IS STILL UNABLE TO FLY. LAST REPAIR TOOK PLACE SEPTEMBER 16, 2002 UNDER OUR PO 8-080096-09. 1G72 3U NCH13EU 20040325001352004032500135EU 2004 3 25 BAQA093336 120040214A672041800876800 ACTUATOR UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206A NE TAIL ROTOR UNSERVICEABLE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03584AE1445 0288 ACTUATION LIGHT AMBER LETTER Y ILLUMINATE ON DFD. UNIT WAS CANNED FROM A/C S/N 0132. HARDCARD ENCLOSED REPLACED WITH SERVICABLE UNIT. 02/27/2004 1G72 3U3 U H88EU E42NE 20040325001452004032500145EU 2004 3 25 BAQA093648 120040217A6210117151321 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR OUT OF TRACK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG2771 7506 BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTAL OF 2.4 HOURS. BLADE WAS RECEIVED AS AN EXCHANGE, UNDER OUR PO 8-080114-36. 1G72 3U NCH13EU 20040325001482004032500148EU 2004 3 25 BAQA093650 120040202A6210117151321 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG733 7506 EXCESSIVE BLADE LAG, BLADE WAS INSTALLED BUT NEVER FLOWN DUE TO EXCESSIVE LAG. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080103-07, BLADE IS UNSERVICABLE WITH ZERO HOURS ON IT. BLADE HAS ACCUMULATED ONLY 733.4 HOURS ON IT SINCE 09/15/1997 BUT HAS BEEN IN FOR REPAIR EIGHT TIMES WITH THIS BEING THE NINTH. 1G72 3U NCH13EU 20040325001492004032500149EU 2004 3 25 BAQA093652 120040218A6210 BUSHING UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE M/R BLADE UNSERVICEABLE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME2153 862 0157 INSPECTION REVEALED DAMAGED GRIP AT BUSHINGS. TEFLON LINERS WERE REPLACED BY REP. BLADE DIMENSION TO THICK AT GRIP FOR INSTALLATION AFTER LINERS WERE INSTALLED. SUSPECT GRIP TO THICK TO BEGIN WITH, PREVIOUS LINERS WERE DAMAGED AT BLADE REMOVAL (HARD TO PULL BLADE) BLADE WAS REPLACED WITH S/N 852 OUT OF OUR ASSET STOCK. 1G72 3U3 U H88EU E34NE 20040326000012004032600001EU 2004 3 26 BAQA093490 120040229A2432 MASTER BOX UROCOPEC135 EC135P2 5620027EU WILL NOT TEST B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135WJ59 0287 BOX WILL NOT TEST AND IS CAUSING LT GENERATOR TO FAIL. REPLACED WITH SERVICABLE MASTER BOX, 03/05/2004 1G72 3U H88EU 20040326000032004032600003WP 2004 3 26 0400459750 120040318A2780 CONTROL CABLE DOUG DC9 DC941 302207NWP NR 5 SLAT STRETCHED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01750NW 47114 DURING APPROACH FOR LANDING, THE AIRCRAFT ROLLED WHEN SLATS WERE SELECTED TO EXTEND. BOTH BLUE SLAT EXTEND AND SLAT DISAGREEMENT LIGHTS WERE FLICKERING. DISAGREE LIGHT WENT OUT AND EXTEND LIGHT CAME ON STEADY AT 135 KTS. CREW STATES THAT WHEN THE LIGHTS WERE FLICKERING THE AIRCRAFT WAS BEING CONTROLLED MANUALLY (NOT AUTOPILOT) AND DID NOT FEEL ANY ROLLING TENDENCIES. LANDING AT DTW WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT EXTEND SWITCH AND THEN FOUND BOTH WINGS SLAT EXTEND CABLES WERE OUT OF LIMITS. CABLES WERE REPLACED AND RIGGED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040326000052004032600005NM 2004 3 26 0400476307 120040319A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01667US 24222 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51AB-62AB. RECONNECTED WIRE AT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040326000092004032600009EA 2004 3 26 COMA0460206 120040312A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01915CA 7013 FRAME CRACKED AT LEFT SIDE FS 640.00 AT STRINGER 9. REPAIRED IN ACCORDANCE WITH REO 601R-53-61.487. 2L72 4F RTA21EA 20040326000102004032600010EA 2004 3 26 COMA0460201 120040317A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT WING FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01729CA6494 7265 FLIGHT 5157 RECEIVED A FLAP FAIL MESSAGE DURING CLIMBOUT OF CMH. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE BRAKE AND POSITION SENSOR. 2L72 4F RTA21EA 20040326000122004032600012EA 2004 3 26 COMA0460200 120040316A301060180332 DUCT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE LEAKING A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA 7017 FLIGHT 5889 DURING CLIMBOUT OF CVG RECEIVED A WING ANTI-ICE DUCT MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE RIGHT WING LEADING EDGE BLEED AIR DUCT. 2L72 4F RTA21EA 20040326000132004032600013EU 2004 3 26 CX7A194J0412 120040301A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03308CE 340B210 ABORTED T/O FOR LEFT TAILPIPE HOT AT 85 KNOTS. 2L72 4T RTA52EU 20040326000142004032600014EA 2004 3 26 COMA0460214 120040321A27507805013 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01818CA3780 7408 FLIGHT 5800 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR CONTROL. 2L72 4F RTA21EA 20040326000152004032600015EA 2004 3 26 COMA0460215 120040319A5330 SEAL CNDAIRCL600 CL6002B19 1900309EA SKIN LEAKING A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01721CA 7259 FLIGHT 5892 WATER LEAKING FROM CABIN CEILING. RESEALED AROUND ADF ANTENNA. 2L72 4F RTA21EA 20040326000162004032600016NE 2004 3 26 MWEA040024 220040312A7200JT8D7B ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE LEFT VIBRATION A MWEAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 GL31501ME 47132 649644 LEFT ENGINE VIBRATION. COMPLIED WITH VIBRATON TEST, INLET HAS A VIBRATION OF 1.0 MILS, TEST 1 VIBRATION CHECKED OK FOR SERVICE. 2L72 4F4 F A6WE E2EA 20040326000172004032600017WP 2004 3 26 0400449988 120040109A5320 CLIP DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING H-CHECK, FOUND CRACK IN FRAME SHEAR CLIP AT BS 1038 L14R. REPAIRED PER EA 99-197375. 2L72 4F A6WE 20040326000182004032600018 2004 3 26 371PA0039 420040315A221065528179 ACCESSORY UNIT BOEING737 737306 13844BGNM AFCS MALFUNCTIONED A PIDAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SO05371PA 23543 AIRCRAFT PITCHES UP AT OR ABOVE .75 MACH WITH AUTOPILOT ENGAGED. REPLACED AFC ACCESSORY UNIT PER MM 22-11-36. OPS CHECKS GOOD. 2L72 4F RTA16NE 20040326000202004032600020EA 2004 3 26 COMA0460217 120040320A3520 OXYGEN MASK CNDAIRCL600 CL6002B19 1900309EA ROW 9 ACTIVATED A COMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01960CA 7117 FLIGHT 5118 02 MASK AT ROW 9 DROPPED DURING T/O. RESTOWED 02 MASKS AT ROW 9. 2L72 4F RTA21EA 20040326000212004032600021NM 2004 3 26 219PA0014 120040314A5270 PROXIMITY SWITCH BOEING737 737222 1384473NM CARGO DOOR OUT OF ADJUST A PIDAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO05219PA 19956 AFT CARGO DOOR LIGHT CAME ON AT 75 KTS. RTO, NO BRAKES APPLIED, REVERSERS ONLY. ADJUSTED PROXIMITY SWITCH AND OPS CHECKED PER MM 52-10-00. 2L72 4F A16WE 20040326000232004032600023NM 2004 3 26 2004UALA00235 120040313A3350 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29173UA 24380 EMERGENCY LIGHTS AT SEATS 32, 33, 34 A, B & C COME ON AND OFF INTERMITTENTLY WHILE AT THE GATE. REPLACED POWER SUPPLY UNIT ABOVE 3L. 2L74 4F4 FRTA20WE E24NE 20040326000242004032600024NM 2004 3 26 2004UALA00236 120040315A5320 FLOOR SUPPORT AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29825UA 980 CABIN FLOOR SUPPORT CORRODED AT FRAME 66 AT RBL 42. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA28NM E40NE 20040326000272004032600027NM 2004 3 26 2004UALA00239 120040313A2121 IMPELLER BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIR DISTRIBUTIONOUT OF BALANCE A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29540UA 25252 SMOKE IN THE FLT DECK AND CABIN ON TAXI. THE ROTOR-IMPELLER WAS FOUND TO BE OUT OF BALANCE, ALLOWING IT TO RUB AGAINST THE FAN HOUSING. BURNED RESIDUE WAS DISCOVERED WITHIN THE ASSEMBLY. RIGHT RECIRCULATION FAN REPLACED. 2L72 4F4 FRTA2NM E17NE 20040326000282004032600028EU 2004 3 26 2004UALA00240 120040316A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29411UA 464 STRINGER 42L CORRODED FROM FRAME 53 TO FRAME 59. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER, INSTALLED ATTACHING HARDWARE AND RESTORED FINISH. 2L72 4F4 FRTA28NM E40NE 20040326000302004032600030EU 2004 3 26 2004UALA00242 120040316A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29411UA 464 STRINGER 43L CORRODED FROM FRAME 54 TO 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR. 2L72 4F4 FRTA28NM E40NE 20040326000342004032600034EA 2004 3 26 COMA0460202 120040316A2752853D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LEFT WING FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01729CA4218 7265 FLIGHT 5157 RECEIVED A FLAP FAIL MESSAGE DURING CLIMBOUT OF CMH. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE INBOARD ACTUATOR OF THE OUTER LEFT FLAP. 2L72 4F RTA21EA 20040326000352004032600035EU 2004 3 26 CX7A194J0406 120040220A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE MALFUNCTIONED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03311CE 340B214 DURING TAILPIPE HOT LIGHT ON T/O. ABORT T/O, RAN CHECKLIST AND RETURNED TO GATE. LEFT TAILPIPE HOT LIGHT ON FOR 30 SECONDS. 2L72 4T RTA52EU 20040329000012004032900001EA 2004 3 29 ASOA04111 120040210A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040329000022004032900002EA 2004 3 29 ASOA04102 120040208A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYS LEAKING A ASOAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO11924EV 7830 FLT 4777 - DURING APPROACH INTO DFW FROM ORD, THE CREW RECEIVED A HYDRAULIC THREE LOW PRESSUER CAUTION LIGHT WHEN THE GEAR HANDLE WAS LOWERED, FOLLOWED BY A GEAR DISAGREE WARNING. THE NOSE GEAR INDICATED DOWN AND LOCKED WITH THE MAINS UNSAFE. THE AIRCRAFT PERFORMED A GO-AROUND AND THE QRH WAS COMPLIED WITH. THE NR 3 HYDRAULIC SYSTEM FLUID LEVEL WAS AT FIVE PERCENT AND THE PRESSURE INDICATED 100 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ORD. DURING SERVICING OF THE NR 3 HYDRAULIC SYSTEM, MAINTENANCE OBSERVED A LEAK FROM THE NR 3 HYDRAULIC RESERVOIR, REMOVED AND REPLACED IT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040329000082004032900008EU 2004 3 29 ASOA04107 120040210A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11632AS 338 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040329000112004032900011EA 2004 3 29 ASOA04114 120040210A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE CLIP AT FS 280, RBL 9 INBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 280, RBL 9 INBOARD IAW SRM 51-42-21. (M) 2L72 4F RTA21EA 20040329000122004032900012EA 2004 3 29 ASOA04113 120040210A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 INBOARD AND OUTBOARD IAW SRM 51-42-21. (M) 2L72 4F RTA21EA 20040329000132004032900013EA 2004 3 29 ASOA04112 120040210A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040324000462004032400046NM 2004 3 24 SWAA040816 120040316A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 616, STRINGER 4 R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040324000542004032400054EA 2004 3 24 SWIA200413025 120040316A2750860D10018 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07915SW2152 2152 7615 PLACED FLAP HANDLE TO 20 FLAP POSITION INDICATED 8, RECEIVED FLAPS FAIL MESSAGE. REMOVED AND REPLACED FECU IAW MM 27-51-04. OPS CHECK GOOD. 2L72 4F RTA21EA 20040324000672004032400067NM 2004 3 24 SWAA040823 120040317A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 2 TO BS 500D + 6, STRINGER 12L. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040324000772004032400077 2004 3 24 SWIA200413000 420040227A22166225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07196SW9621 9621 120151 ELECTRIC TRIM INOP. REMOVED AND REPLACED ELEVATOR TRIM SERVO. OPS CHECKS GOOD IAW MM 22-10-09. 2L72 4T RTA31SO 20040324000972004032400097 2004 3 24 SWIA200413012 420040310A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07157323 3 120195 DURING STALL TEST ON GROUND, F/O'S SHAKER WAS NOT ACTIVATING DURING THE TEST. CLACKER AND PUSHER ONLY. R/R FIRST OFFICER'S STICK SHAKER IAW 27-34-00. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040324001002004032400100EU 2004 3 24 MALA040267 120040301A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438XJ 340B438 DURING INSPECTION IN LCQ, LEFT FUSELAGE AT STA 351 WL 135 HAS A DENT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53005. A/C RELEASE DATE 3/14/2004. 2L72 4T RTA52EU 20040324001122004032400112NM 2004 3 24 CALA0400251 120040317A7120310A10325 LINK BOEING737 7373T0 1384582NM ENG MOUNT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND NR 2 ENGINE AFT MOUNT HANGAR LINK CRACKED. THE LINK WAS REPLACED IAW MM 71-21-03. 2L72 4F RTA16WE 20040324001212004032400121EU 2004 3 24 AALA20040316 120040304A5311 FRAME AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 FRAME CORROSION ALONG AFT NOSE LANDING GEAR BULKHEAD LOWER FLANGE FROM STRINGER 6 LEFT HAND TO STRINGER 6 RIGHT HAND IN A AREA OF 3 INCHES BY 50 INCHES. REMOVED CORROSION AND REPAIRED PER ESO 30595. 2L72 4F RTA35EU 20040324001242004032400124WP 2004 3 24 AALA20040322 120040306A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21291AA 49303 BOTH AFT ACCESSORY WALL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ABOVE MID GALLEY FOR AFT ACCESSORY WALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001322004032400132EA 2004 3 24 SWIA200413034 120040220A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE LBL 9.0 HAS INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED AT FS 280.00. REPLACED IAW CRJ SRM. 2L72 4F RTA21EA 20040324001342004032400134EA 2004 3 24 SWIA200413037 120040220A5420 FRAME CNDAIRCL600 CL6002B19 1900309EA ACCESS PANEL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON UPPER ACCESS PANEL 422AB STIFFENER FRAME CRACKED. REPLACED STIFFENER IAW SHORTS CMM 20-40-11, 20-42-06, 20-27-11 & 20-27-11. 2L72 4F RTA21EA 20040324001442004032400144EA 2004 3 24 SWIA200413047 120040309A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 MAIN FUSELAGE; FS 280.00; LBL-9; UPPER FLANGE CRACKED ON TRANSVERSE BEAM. REPAIRED IAW CRJ REO 601R-53-11-138 REV. NC AND RII53-401. 2L72 4F RTA21EA 20040324001462004032400146WP 2004 3 24 AALA20040363 120040318A2910AS115060172 HOSE DOUG DC9 DC982 3022082WP DOOR CYLINDER LEAKING A AALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21464AA 49594 EN ROUTE DFW TOTAL LOSS OF HYDRAULIC QUANTITY ON LEFT HAND SYSTEM. RETURNED MCO AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE LINE TO RETRACT SIDE OF NOSE GEAR DOOR CYLINDER WITH 3000 PSI FLEX LINE DUE TO RUPTURE. SERVICED HYDRAULIC QUANTITY TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040324001832004032400183EA 2004 3 24 04078663 120040318A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27663BR 7527 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001852004032400185WP 2004 3 24 ABXA040109 120040318A2611302842 SMOKE DETECTOR DOUG DC8 DC861 3021952WP CARGO BAY DEFECTIVE A ABXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23847AX 312 46031 UPPER CARGO FIRE SMOKE SOUNDED IN FLIGHT. ISOLATED TO NR 3 DETECTOR. TESTED NORMAL AFTER LANDING. REPLACED NR 3 SMOKE DETECTOR IAW DC-8 MM 26-10-05-2-0001. OPS CHECKED GOOD. 2L74 4F 4A25 20040324001872004032400187 2004 3 24 MALA040277 420040318A22104068300904 COMPUTER BAC 146 AVRO146RJ85A1500097EU FLIGHT GUIDANCE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15510XJ E2323 AP DISCONNECTED IN CRUISE. FLIGHT WITH THE FOLLOWING SYSTEM FAILURES NOTED: FTC, EL TRIM, YD, AP, MCP/F/D TRP/AUTOTHROTTLES, WITH FGS ADVISORY LIGHTS , FGC1 AND YAW DAMPER. MX REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER IAW RH AMM 22-10-11-201. REMOVED AND REPLACED FLIGHT GUIDANCE COMPUTER IAW RH AMM 22-10-11-201. RTS TEST GOOD. REF 22-10-2 PG 5001. MX SCREEN DIAGNOSTICS RECORDED FGC FAILURES DURING LAST LEG OF FLIGHT. AC GOOD FOR SERVICE. 2H74 4F RTA49EU 20040324001912004032400191NM 2004 3 24 P5CA0401058 120040311A7711ED7472012 TRANSMITTER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE EPR FAILED A P5CAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP23921FT 21575 689169 NR 1 ENG WOULD NOT PRODUCE TAKEOFF THRUST OF 1.53 EPR. DROPPED TO 1.45 EPR AT FWD THROTTLE STOP. ABORTED T/O. REPLACED EPR TRANSMITTER PER MM 77-11-02. ENGINE GROUND OPS CHECK OK PER MM 71-00-11 TEST NR 9. 2L74 4F4 F A20WE E3NE 20040325000142004032500014EA 2004 3 25 ASOA04130 120040215A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040325000212004032500021EA 2004 3 25 ASOA04124 120040214A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11859AS 7421 DURING HANGAR MAINTENANCE IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000252004032500025NE 2004 3 25 BAQA091781 220040108A73200164448760 FUEL CONTROL BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE NR 1 ENGINE UNSERVICEABLE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY506 7544 NR 1 ENGINE WAS DIFFICULT TO START. UNIT WAS CANNED FROM ORIGINAL ENG. S/N 18167 FOR ENG S/N 18024, THEN PUT BACK ON ENG S/N 18167. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/16/2004 1G72 3U3 UNCH13EU E19EU 20040325000652004032500065NE 2004 3 25 HEEA093483 220040125A72000292005250 ENGINE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE NR 1 FAILED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW03761PH 760224 WHILE IN CRUISE FLIGHT HEARD A BUMP, THE AIRCRAFT YAWED, NR 1 ENGINE OUT LIGHT CAME ON, MAST CAUTION LIGHT CAME ON, ENGINE CHIP LIGHT CAME ON, AND ALL GAUGES WENT TO ZERO ON THE NR 1 ENGINE. CONTINUED FLIGHT AND LANDED AT AIRPORT. 1G72 3U3 U H1NE E19EU 20040325000742004032500074 2004 3 25 AC2A093330 420040217A34161003511424 ALTIMETER BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE COCKPIT MALFUNCTIONED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CT 49089 ALTIMETER MALFUNCTIONED. 60 FT LOW ON CERTIFICATION CHECK. REPLACED 1G72 3U3 URTH9SW E1GL 20040325000842004032500084EU 2004 3 25 BAQA093335 120040221A2150510286C OUTPUT SEAL UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE A/C PACK GEARBOXLEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH444 0273 A/C PACK GEARBOX OUTPUT SEAL LEAKS. REPLACED WITH SERVICABLE UNIT. 02/27/2004 1G72 3U3 U H88EU E19EU 20040325001082004032500108SW 2004 3 25 HEEA093477 120040215A2910MS21924W4 COUPLING BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE HYD PUMP CRACKED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW038045T 28101 OIL COOLER CAUTION LIGHT ILLUMINATED IN FLIGHT. REPLACED CRACKED UNION ON THE UTILITY HYDRAULIC PUMP. 2G72 4U4 U H10SW E8NE 20040325001142004032500114EU 2004 3 25 BAQA093317 120040219A6330L633M2010105 MOUNT UROCOPEC135 EC135P2 5620027EU M/R GEARBOX CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135WJ37 0287 MAIN ROTOR GEARBOX MOUNT HAS A CRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1G72 3U H88EU 20040326000072004032600007EU 2004 3 26 CX7A194J0420 120040317A3260 CONNECTOR SAAB SF340 340B 7860101EU MLG INDICATOR DISCONNECTED A CX7AO OTHER P NO WARNING INDICATION APAPPROACH 1 GL03315CE 340B343 LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION, RECYCLED GEAR AND CONDITION REMAINED. T/O INHIBIT AND GROUND OPS INOP. 2L72 4T RTA52EU 20040326000192004032600019EA 2004 3 26 COMA0460216 120040317A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM UNRELIABLE A COMAL ABORTED APPROACH JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01917CA8912 7017 FLIGHT 5607 GEAR DISAGREE WARINING, NLG INDICATED UNSAFE. REPLACED THE SYSTEM 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20040326000292004032600029EU 2004 3 26 2004UALA00241 120040316A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29411UA 464 STRINGER 43L CORRODED FROM FRAME 58 TO 59. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED ANGLE REPAIR. 2L72 4F4 FRTA28NM E40NE 20040326000312004032600031NM 2004 3 26 2004UALA00243 120040315A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE LAV DOOR AREA INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29507UA 24743 EEL IS INOPERATIVE AT AFT FWD LAV DOOR OPENING. REPLACED EEL STRIP, OPS NORMAL. 2L72 4F4 FRTA2NM E17NE 20040326000322004032600032NM 2004 3 26 2004UALA00244 120040315A2421 GENERATOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29829UA 1211 FLIGHT DIVERTED DUE TO A LOST GENERATOR. NR 2 GENERATOR BUSS LOSS. NUMBER 2 GENERATOR FAULT LIGHT ILLUMINATED SUPPLEMENTAL DATA UPDATE PIN AND SOCKET ON PYLON FIREWALL CONNECTOR 400VC CORRODED AND BURNED. REPLACED HARNESS ASSEMBLIES. 2L72 4F4 FRTA28NM E40NE 20040329001092004032900109NE 2004 3 29 CX7A194J0407 220040111A7313 BOSS SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUEL INJECTOR BROKEN A CX7AK NONE O OTHER ININSP/MAINT 1 GL03317CE 3322 340B352 785572 LEFT ENGINE 1 O'CLOCK FUEL INJECTOR BOSS IS BROKEN. 2L72 4T4 TRTA52EU E8NE 20040329001122004032900112EA 2004 3 29 COMA0460207 120040312A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01915CA 7013 RIGHT HAND LOWER WING PLANK AT WS 148.019 IS CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-67-21-130. 2L72 4F RTA21EA 20040329001132004032900113EA 2004 3 29 COMA0460208 120040317A2150 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT SMOKE A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO01518CA 7816 FLIGHT 5852 SMOKE ODOR IN COCKPIT. DEFERRED LEFT ACM PER MEL. 2L72 4F RTA21EA 20040329001172004032900117EA 2004 3 29 COMA0470029 120040317A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ICED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01369CA 10079 FLIGHT 5661 RIGHT THRUST REVERSER CAUTION DURING T/O. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040329001182004032900118EA 2004 3 29 COMA0460211 120040317A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01805CA 7354 FLIGHT 5749 TAKEOFF CONFIG SPOILERS WARNING DURING T/O. RESET SECU, SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040329001202004032900120EA 2004 3 29 COMA0460203 120040316A32204622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01966CA21538 7132 FLIGHT 5205 RECEIVED A GEAR DISAGREE AND NOSE DOOR WARNING AFTER TAKEOFF FROM DTW. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040329001222004032900122WP 2004 3 29 MWEA040027 120040319A573059305036 SKIN DOUG DC9 DC981 3022081WP RT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT WING EXTERIOR BOTTOM AFT SKIN HAS A SPOT OF CORROSION AT STATION XRS410 AFT SPAR TEE AREA. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20040329001242004032900124NE 2004 3 29 CX7A194J0410 220040128A7313 BOSS SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUEL INJECTOR BROKEN A CX7AK NONE O OTHER ININSP/MAINT 1 GL03311CE 2954 340B214 785573 RIGHT ENGINE REQUIRES REMOVAL DUE TO 9 O'CLOCK FUEL INJECTOR BOSS BROKEN. 2L72 4T4 TRTA52EU E8NE 20040329001262004032900126NM 2004 3 29 304AW0004 120040318A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05304AW 24011 MID CABIN EMERGENCY ESCAPE LIGHTS ALONG SEAT BOTTOMS INOP. ALSO AFT EMERGENCY FLASHLIGHT INOP. REPLACED 1 FUSE ON BATTERY PACK LOCATED ON RIGHT AFT DOOR. CABIN LIGHTS OP NORMAL. REPLACED BATTERY IN FLASHLIGHT, OPS NORMAL. 2L72 4F RTA16WE 20040329001282004032900128NM 2004 3 29 0400426314 120040314A3350 LIGHT BOEING747 747451 1384940NM E ZONE INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01674US 30269 DURING LINE CHECK, FOUND E-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED LEFT AND RIGHT FLOOR PATH EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040329001292004032900129EU 2004 3 29 CX7A194J0416 120040307A261251533172 FIRE LOOP SAAB SF340 340B 7860101EU RT ENGINE CHAFED A CX7AE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL03303CE 340B194 RIGHT BLEED AIR LEAK IN FLIGHT ILLUMINATED. FOLLOWED PROCEDURE, SHUTDOWN ENGINE. RETURNED TO LEX. 2L72 4T RTA52EU 20040329001342004032900134 2004 3 29 CX7A194J0419 420040318A2340 HANDSET SAAB SF340 340B 7860101EU INTERPHONE DISCONNECTED A CX7AO OTHER O OTHER NRNOT REPORTED 1 GL03316CE 340B348 INTERPHONE SYSTEM INOPERATIVE. CREW ALSO REPORTED A BURNING SMELL COMING FROM HANDSET ASSEMBLY. 2L72 4T RTA52EU 20040329001372004032900137NM 2004 3 29 2004UALA00198 120040305A5311 FRAME BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 BULK CARGO PIT FRAME STA 1920 UPPER CHORD AFT FLANGE IS EXFOLIATED UNDER NUT PLATES AT LBL 20, RBL 3, 6 & 12, LBL 20, RBL 3, RBL 6, RBL 12. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW CHORD SECTION. 2L74 4F4 FRTA20WE E24NE 20040329001382004032900138NM 2004 3 29 2004UALA00199 120040305A5312 BULKHEAD BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 AFT PRESSURE BULKHEAD (STA 2360) HAS 2 EACH DENTS JUST BELOW WL 274.87 AT RBL 45 AND RBL 55. MAJOR REPAIR ACCOMPLISHED. INSTALLED 2 EACH REPAIR DOUBLERS. 2L74 4F4 FRTA20WE E24NE 20040329001392004032900139NM 2004 3 29 2004UALA00200 120040305A5311 FRAME BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 AFT PIT FRAME 1920 T-CHORD EXFOLIATED AT RBL 57. MAJOR REPAIR ACCOMPLISHED. REPLACED CORRODED T-CHORD SECTION. 2L74 4F4 FRTA20WE E24NE 20040329001422004032900142NM 2004 3 29 2004UALA00203 120040307A5330 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 STRINGER CRACKED AT BS 380 STR 21L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND SPLICE. 2L72 4F4 FRTA16WE E2GL 20040329001432004032900143NM 2004 3 29 2004UALA00204 120040307A2420 IDG BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU FAILED A UALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29566UA 26670 LEFT GENERATOR CONTROL OFF LIGHT AND EICAS MESSAGE CAME ON. THREE ATTEMPTS TO START THE APU WERE UNSUCCESSFUL. REPLACED THE LEFT IDG.ONE PISTON IN THE HYDRAULIC UNIT FAILED CONTAMINATING THE IDG WITH METAL SHAVINGS. 2L72 4F4 FRTA2NM E17NE 20040329001442004032900144NM 2004 3 29 2004UALA00205 120040307A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 STRINGER CRACKED AT BS 380 STR 23L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040329001452004032900145NM 2004 3 29 2004UALA00206 120040307A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 STRINGER CRACKED AT BS 380 STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED STRINGER AND SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040329001472004032900147NM 2004 3 29 2004UALA00208 120040305A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP2989UA 24664 STRINGER CLIP CRACKED BS 727D S4R. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20040329001492004032900149NM 2004 3 29 MWEA040022 120040224A27604074750301 CONTROL UNIT BOEING717 717200 1383700NM SPOILERS FALSE INDICATIONA MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31913ME 55176 SPOILER FAULT ALERT CAME ON. DURING FAULT REVIEW OF SPOILER ELECTRONIC CONTROL UNIT SECU, DISCOVERED FAULT 276051, PERFORMED FIM TASK SPOILER ELECTRONIC CONTROL UNIT SYSTEM, OPERATIONS CHECKED GOOD. 2L72 4F TRA6WE 20040329001512004032900151NM 2004 3 29 2004UALA00210 120040305A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP2989UA 24664 BS 706 S4R HAS A CRACKED BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW BRACKET. 2L72 4F4 FRTA16WE E2GL 20040329001532004032900153NM 2004 3 29 2004UALA00212 120040309A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29122UA 29168 SLIDE LIGHT INOP AT DOOR 3L. REPLACED & TESTED DOOR SLIDE LIGHT LAMP, TESTS GOOD. 2L74 4F4 FRTA20WE E24NE 20040329001552004032900155 2004 3 29 MWEA040028 420040320A22204083700903 COMPUTER BOEING717 717200 1383700NM FLT CONTROL INTERMITTENT A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31910ME 55174 LOW SPEED HIGH PROTECTION CAME ON TOGETHER AND STICK SHAKER. PERFORMED ADJUSTMENT TEST OF NUMBER 1 FLIGHT CONTROL COMPUTER AND NR 2 FLIGHT CONTROL COMPUTER STALL WARNING SYSTEM BOTH PASSED STALL WARNING CHECK. 2L72 4F TRA6WE 20040329001582004032900158EU 2004 3 29 CX7A194J0414 120040304A26131734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE FALSE ACTIVATIONA CX7AE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL03309CE 340B201 RIGHT TAILPIPE HOT LIGHT CAME ON, SHUT ENGINE DOWN AND RETURNED TO MDW. LIGHT REMAINED ON. 2L72 4T RTA52EU 20040329001592004032900159NM 2004 3 29 2004UALA00188 120040304A5311 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 DENT LOCATED 3 INCHES AFT OF THE AFT FRAME OF THE FWD CARGO DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIRS. 2L72 4F4 FRTA16WE E2GL 20040329001632004032900163NM 2004 3 29 2004UALA00217 120040213A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 INTERCOSTAL CRACKED AT BS 312 - 328 LBL 45. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2GL 20040329001652004032900165NM 2004 3 29 2004UALA00219 120040309A5512 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29389UA 24664 RIGHT HORIZONTAL L/E HAS A TEMPORARY REPAIR 82 INCHES FROM I/B END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040329001672004032900167EU 2004 3 29 CX7A194J0413 120040304A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE FALSE ACTIVATIONA CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03318CE 340B358 ABORTED T/O DUE TO LEFT TAILPIPE HOT LIGHT ILLUMINATED. 2L72 4T RTA52EU 20040329001692004032900169EU 2004 3 29 2004UALA00222 120040309A5315 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29452UA 955 FLOORBEAM BETWEEN FR 19-20 IS CORRODED LBL 6. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM. 2L72 4F4 FRTA28NM E40NE 20040329001702004032900170EU 2004 3 29 2004UALA00223 120040309A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29452UA 955 AFT CABIN FLOOR SUPPORT RBL 34 FROM FRAME 64 TO 66 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME FLOOR SUPPORT. 2L72 4F4 FRTA28NM E40NE 20040329001742004032900174NM 2004 3 29 2004UALA00227 120040310A5313 STRINGER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29603UA 21864 AFT PIT AT STA 1088, STR 33L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER WITH -U- AND -J- CHANNEL SPLICE ANGLES. 2L72 4F4 FRTA1NM E3NE 20040329001752004032900175NM 2004 3 29 2004UALA00228 120040310A5414 SKIN BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 2 PYLON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29603UA 21864 NR 2 PYLON ACCESS 446BR, UPPER FWD CORNER OF ACCESS CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA1NM E3NE 20040329001762004032900176NM 2004 3 29 2004UALA00229 120040310A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29521UA 24891 FOUND PUNCTURE ON FUSELAGE FWD OF THE APU, APPROX STA 1860 NEAR STRINGER 22. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040329001822004032900182NM 2004 3 29 P5CA0401059 120040317A2910 HOSE BOEING747 74747UF 1384949NM HYD SYSTEM LOOSE A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23496MC 29257 LOSS OF HYD FLUID, SYSTEM NR 1 ENG PUMP SELECTED OFF. SYSTEM NR 1 PRESS NORMAL TO COMPLETION OF FLIGHT. FOUND PRESS HOSE AT EDP LOOSE. TIGHTENED HOSE/LINE PER MM 29-11-08. NO LEAKS NOTED PER MM 71-00-00. 2L74 4F RT1384945 20040329001832004032900183 2004 3 29 MWEA040019 420040222A256539522731 GIRT BAR DOUG DC9 DC981 3022081WP SERVICE DOOR BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 THE GIRT BAR AT THE FORWARD SERVICE DOOR WILL NOT STAY IN IT'S HOLDER. FOUND HOLDER BENT, ADJUSTED HOLDER. 2L72 4F A6WE 20040329001842004032900184 2004 3 29 MWEA040020 420040222A2565 BOTTLE DOUG DC9 DC981 3022081WP LOW A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME PO174 48032 AFT ACCESS EVACUATION SLIDE PRESSURE BELOW 2000 PSI. REMOVED AND REPLACED AFT EVACUATION SLIDE. 2L72 4F A6WE 20040329001942004032900194NM 2004 3 29 AALA20040339 120040303A3350 LIGHT BOEING767 767323 1385205NM LAVATORY BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 DFW - EMERGENCY LIGHT ON WALL AT AFT LEFT LAVATORY BROKEN. REPLACED EMERGENCY LIGHT ON WALL AT AFT LEFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040329001952004032900195NM 2004 3 29 2004UALA00246 120040313A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 CORROSION ON TOP OF FLOORBEAM CAP AT STA 986.5 RBL 45.5. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FLOORBEAM REPAIR. 2L72 4F4 FRTA16WE E2GL 20040329001962004032900196NM 2004 3 29 2004UALA00232 120040311A7921 OIL COOLER BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29541UA 25253 NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO AND OIL PRESSURE LIGHT FLICKERING. SUPPLEMENTAL DATA UPDATE AIRCRAFT INDICATED OIL CONSUMPTION FOR SEVERAL DAYS BEFORE THE EVENT. THE SHOP FOUND FUEL/OIL COOLER THE SOURCE OF OIL CONSUMPTION (OIL ENTERED FUEL). THE REPAIR PROCESS OF COOLER HAS BEEN REVIEWED AS A PRECAUTION. COOLERS HAVE BEEN ADDED TO SAM PROGRAM. 2L72 4F4 FRTA2NM E17NE 20040329001972004032900197NM 2004 3 29 2004UALA00233 120040302A5751113W72122 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE AILERON ACTUATORCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29779UA 26941 I/B ACTUATOR FITTING CRACKED. REPLACED ACTUATOR FITTING. 2L72 4F4 FRTT0001SE E46NE 20040329002012004032900201NM 2004 3 29 0400436638 120040314A2530813640407 OVEN BOEING747 747251B 1384892NM 2B GALLEY BURNED A NWAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NRNOT REPORTED 1 GL01638US 23549 DURING FLIGHT, FIRE FLASHED FROM THE GALLEY 2B POSITION 2-17 OVEN. PULLED OVEN CIRCUIT BREAKERS AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED OVEN AND REMOVED DEBRIS FROM BEHIND THE OVEN. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040330000012004033000001NM 2004 3 30 04FDEA00621 120040310A5753ARC2512503 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75300 - WINGS - INBOARD TRAILING EDGE FLAP, LEFT HAND OUTBOARD BRACKET (FLAP SIDE), PIVOT BORE CORROSION - REPAIR. 2L73 4F RTA22WE 20040330000082004033000008NM 2004 3 30 DL73S040229 120040311A2915 RELIEF VALVE BOEING737 737232 1384475NM HYD RESERVOIR FAILED A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27329DL 23101 DURING APPROACH PHASE AFTER PLACING THE FLAP LEVER TO 5 SYSTEM A PRESSURE WENT TO ZERO WITH ASSOCIATED SYSTEM A LOW PRESSURE LIGHTS ILLUMINATED. REPLACED SEVERAL LINES AND RESERVOIR PRESSURE RELIEF VALVE. 2L72 4F RTA16WE 20040330000092004033000009NM 2004 3 30 DL757040230 120040310A5330141N33111 SKIN BOEING757 757232 1384965NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27602DL 22809 THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 2 INCH CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CUTOUT THROUGH ALL LAYERS OF THE SKIN ASSEMBLY. THE AREA WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 088886-14. 2L72 4F RTA2NM 20040330000112004033000011NM 2004 3 30 DL73S040233 120040309A53306545770565 SKIN BOEING737 737232 1384475NM LAP JOINT SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27315DL 23087 THE LOWER SKIN OF THE STRINGER 4L SKIN LAP SPLICE WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 540-727. THE ENTIRE LAP JOINT WAS CUT AWAY TO REMOVE THE DAMAGE. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ER/A 088477-14. 2L72 4F RTA16WE 20040330000122004033000012NM 2004 3 30 DL73S040234 120040309A5330654577320 SKIN BOEING737 737232 1384475NM LAP JOINT SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27315DL 23087 THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH SCRIBE DAMAGE. THE LAP JOINT WAS CUTOUT FROM FS 727 TO FS 908 TO REMOVE THE JOINT AND THE DAMAGE. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ER/A 088561-14. 2L72 4F RTA16WE 20040330000152004033000015NM 2004 3 30 DL733040216 120040305A2530 WIRE BOEING737 737347 1384647NM GALLEY OVEN SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27309WA 85010005 23442 AFT OVEN RIGHT SIDE DOUBLE HAD SMOKE COMING FROM BEHIND OVEN CONTROL. REMOVED OVEN, FOUND BURNED WIRES. REPAIRED SAME. 2L72 4F RTA16WE 20040330000162004033000016NM 2004 3 30 DL777040217 120040305A381010586 VALVE BOEING777 777232 1385232NM WATER PRESSURE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27877DA UNK 29739 CREW REPORTS LOSS OF WATER PRESSURE IN CABIN, DIVERTING TO JFK FOR REPAIRS. INSPECTED ALL WATER AND AIR PRESSURE LINES AT WATER TANKS AND VERIFIED ALL VALVES CLOSED. NO LEAKS. CKD AIR COMP AND VERIFIED GOOD AIR PRESS. FOUND AIR COMP CHECK VALVE STUCK OPEN AND VERY LOW AIR PRESS AFTER PRESS REGULATOR WITH APU AIR ON. RECOMMEND REPLACE CHECK VLV/IN-LINE FILTER AND PRESSURE REG FWD POTABLE WATER SYS TO MCO AND PLACARD PER MEL 38-10-01B WATER SYSTEM DRAINED. MTC REMOVED AND REPLACED CHECK VLV SYSTEM, CHECKS OK. 2L72 4F RTT00001SE 20040112001782004011200178SO 2004 1 12 GLBA20030526 120040105A3210 LANDING GEAR EMB 120 EMB120ER 3260203SO RIGHT INOPERATIVE A GLBAO OTHER J WARNING INDICATION CLCLIMB 1 NM03299UX 120299 RT MAIN LANDING GEAR WILL NOT RETRACT, OPS CK GEAR SWING OPS CK GOOD. 2L72 4T RTA31SO 20040112001972004011200197WP 2004 1 12 UPS04841701 120040109A2612 WARNING LIGHT DOUG DC8 DC873F 302199FWP FIRE DETECTOR ILLUMINATED A IPXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01804UP 46004 FIRE WARNING ILLUMINATED ON PIT 34. ON DESCENT APPROX 5 MINS AFTER SELECTING TAIL DEICE THE LOWER CARGO FIRE LIGHT ILLUMINATED SECURED TAIL DEICE AND ACCOMPLISHED EMERGENCY CHECKLIST. RAN TAIL DEICE SYS AFTER SEVERAL MINS HAD LOWER CARGO IRE LIGHT ON F/O PANEL & MSG AFT D FIRE WITH VISIBLE SMOKE AN R & R AFT 2 SMOKE DETECTORS IN AFT PIT NEEDS OPS CK OPS CHECK GOOD PER 26 18 01 4 5. ***CLOSED*** 2L74 4F RT4A25 20040112002732004011200273NM 2004 1 12 AALA20040022 120040105A3397 WIRE HARNESS BOEING777 777223 1385213NM CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21776AN 29582 EMERGENCY PROXIMITY LIGHTS AT AFT FLOOR ARE INOPERATIVE. REPLACED EMERGENCY PROXIMITY LIGHT CABLE BETWEEN SEATS 41 AND 42. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040113000312004011300031NM 2004 1 13 AWXA200400027 120040111A30201726257 ANTI-ICE VALVE BOEING737 7373G7 1384595NM RT ENGINE BINDING A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28303AW162174050 24010 PHX - AIR TURNBACK - FLT 0071 - ON CLIMBOUT, EN ROUTE. THE RT ENG ANTI-ICE COWL VALVE OPEN LIGHT REMAINED INTRANSIT, VALVE NEVER OPENED OR INDICATED A DECREASE IN DUCT PRESSURE. TURNED BACK & LANDED WITHOUT FURTHER EVENT. MAINT R & R RT ENG INLET COWL THERMAL ANTI-ICE VALVE IAW BMM 30-21-11, OPERATIONAL CHECK GOOD. INDUCTION TEST OF ENG INLET COWL THERMAL ANTI-ICE VALVE CONFIRMED FAILURE OF UNIT FOR EXCESSIVE PORT & CASE LEAKAGE, & LOW REGULATION. DISASSY OF UNIT FOUND BOTH FLOW BODIES, SEALS, DIAPHRAGM, POPPET ASSY, & RING WORN BEYOND LIMITS. REPLACED FLOW BODIES, SEALS, DIAPHRAGM RING. BUSHINGS , BEARINGS, POPPET ASSY, & MINOR HARDWARE. UNIT FUNCT TESTED & RETURNED TO SERVICE. 2L72 4F RTA16WE 20040112002322004011200232WP 2004 1 12 AALA20040026 120040106A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 EMERGENCY LIGHTS ABOVE ROWS 7, 8, 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7, 8, AND 9. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F A6WE 20040112002332004011200233NM 2004 1 12 AALA20040016 120040102A3350020172003 LIGHT BOEING737 737823 13844BZNM CABIN MALFUNCTIONED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21925AN 29526 ORD EMERGENCY LIGHT ASSEMBLY SMOKING AT SEAT 10D. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. -CLOSED-- 2L72 4F RTA16WE 20040112002562004011200256WP 2004 1 12 AALA20040007 120040103A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21458AA 49563 OVERHEAD EMERGENCY LIGHTS AT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTER PACK FOR ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002582004011200258WP 2004 1 12 AALA20040009 120040103A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW2173444 49470 EMERGENCY LIGHT ON SEAT 27D INOPERATIVE. REPLACED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002602004011200260NM 2004 1 12 AALA20040018 120040102A3350 CONNECTOR BOEING737 737823 13844BZNM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21966AN 30094 EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RESEAT CONNECTOR AT 20D EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040113000672004011300067NE 2004 1 13 BAQA091938 220040104A73100319928770X PUMP AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE FUEL SYSTEM MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109DU224 11503 PUMP MAKING AIRCRAFT SLOW TO START WITH EXCESSIVE FLAME AND SMOKE OUT OF EXHAUST DURING START SEQUENCE. PART REPLACED WITH SERVICABLE UNIT 01/12/2004 1G72 3U3 URTH7EU E42NE 20040112002432004011200243WP 2004 1 12 AALA20040004 120040101A3350 BATTERY PACK DOUG DC9 DC982 3022082WP TAIL CONE DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21491AA 49684 EMERGENCY LIGHTS ABOVE AFT TAIL CONE ENTRANCE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE AFT TAIL CONE ENTRANCE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002552004011200255NM 2004 1 12 AALA20040006 120040103A3350 CONNECTOR BOEING737 737823 13844BZNM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21928AN 29528 EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED CONNECTOR ON SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040112002572004011200257WP 2004 1 12 AALA20040008 120040103A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2173444 49470 EMERGENCY EXIT LIGHT AT AFT RT OVERWING INOPERATIVE. RESEATED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040112002592004011200259NM 2004 1 12 AALA20040017 120040102A3350 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21395AN 29432 SFO EMERGENCY LIGHT ON CEILING NEAR SEAT 13H INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA1NM 20040113000302004011300030GL 2004 1 13 BAQA091886 220040105A732323065123 GOVERNOR AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20B 03013GL TURBINE INOPERATIVE B BAQAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 EA035797X1783 5182 GOVERNOR HAS SLUGGISH RESPONSE IN FLIGHT. 8130 ENCLOSED PART REPLACED WITH SERVICABLE UNIT 01/09/2004. 1G72 3U3 U H11EU E4CE 20040113002032004011300203SO 2004 1 13 C2XA04IA002 120040105A21214611028900 FAN EMB 145 EMB145LR 3260212SO CABIN FAILED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW271697610335 145171 CREW REPORTED A STRONG BURNING SMELL WHEN THE ANTI-ICE SYSTEM WAS ACTIVATED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 RECIRCULATION FAN TO BE INOPERATIVE. THE AFFECTED FAN WAS REMOVED AND REPLACED AND THE RECIRCULATION SYSTEM OPERATIONALLY TESTED. 2L72 4T RTT00011AT 20040113002152004011300215SO 2004 1 13 C2XA04SH014 120040111A532014528737001 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711548 145565 DURING C CHECK STRINGER REINFORCEMENT 19L AT FRAME 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002162004011300216SO 2004 1 13 C2XA04SH013 120040109A531214547494403 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RT MOUNT. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW EA 5340-01016. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002182004011300218SO 2004 1 13 CX2A04SH012 120040109A711014576518004 ANGLE EMB 145 EMB145LR 3260212SO NR 2 COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT OB EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040113002212004011300221SO 2004 1 13 C2XA04SH015 120040111A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711548 145565 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM AND FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040112002722004011200272NM 2004 1 12 AALA20040021 120040105A3350 CONNECTOR BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21629AA 24587 MIA EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY LIGHT WIRE BUNDLE CONNECTOR AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040113002132004011300213SO 2004 1 13 C2XA04IA004 120040108A326023092111003 BRACKET EMB 135 EMB135LR 3260305SO LT MLG DISTORTED A C2XAK NONE N FALSE WARNING CLCLIMB 1 SW2714514 145303 FLIGHT 3250 - PILOT REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MAIN LANDING GEAR PROXIMITY SWITCH MOUNT BRACKET TO BE DISTORTED. THE AFFECTED BRACKET WAS REMOVED AND REPLACED. THE LANDING GEAR SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040113002232004011300223SO 2004 1 13 C2XA04TY007 120040110A532014521725613 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL YAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040113002252004011300225SO 2004 1 13 C2XA04TY006 120040110A5553KSC270720V ATTACH FITTING EMB 135 EMB135ER 3260203SO VERTICAL STAB GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716501 145145 DURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTACH POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040113002222004011300222SO 2004 1 13 C2XA04TY009 120040110A531514526437001 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE RT OMEGA BEAM TOP CAP AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE RT OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040113002242004011300224SO 2004 1 13 C2XA04TY005 120040110A532014522459003 ANGLE EMB 120 EMB120ER 3260203SO ALLSN AE3007AE3007C GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716501 145145 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T4 FRTA31SO TE6CH 20040114001942004011400194SO 2004 1 14 MASA200400014 120040107A5240 ROLLER EMB 145 EMB145LR 3260212SO SERVICE DOOR LACK OF LUBE A MASAK NONE O OTHER ININSP/MAINT 1 SW07840MJ 145429 ASH NR 2721 HAD THE GALLEY SERVICE DOOR DIFFICULT TO CLOSE. MECHANIC LUBED THE DOOR ROLLERS AND DOOR OPERATED NORMALLY. NO PARTS USED 2L72 4T RTT00011AT 20040115000592004011500059 2004 1 15 04005316 420040105A22104006719904 SERVO JETAIRJETSTMJETSTM4101 1500501EU FAULTY A VTZAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 EA27316UE 41055 DURING OPERATION OF AIRCRAFT CREW REPORTED OSCILLATIONS IN VERTICAL MODE OF FLIGHT DIRECTOR WITH AUTOPILOT DISCONNECTING. THE AUTOPILOT SERVO WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040115000622004011500062EU 2004 1 15 AALA20040028 120040103A3244 TIRE FOKKERF28 F28MK0100 4990807EU LT MLG SEPARATED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW211411G 11369 ATL T744/3 RECEIVED LEFT HAND MAIN LANDING GEAR NO UPLOCK INDICATION. RIGHT HAND MAIN LANDING GEAR DID NOT EXTEND WHEN RECYCLED. USED ALTERNATE EXTENSION TO GET GEAR DOWN. LANDED WITHOUT INCIDENT. FOUND LEFT MAIN GEAR TIRE SEPARATION THAT DAMAGED GEAR SENSORS AND FUEL LINE IN LEFT WHEEL WELL AREA. AIRCRAFT OUT OF SERVICE FOR REPAIRS. 2L72 4F RT 20040115000842004011500084NM 2004 1 15 04FDEA00112 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD ACTUATOR LUG BORE. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000862004011500086NM 2004 1 15 04FDEA00023 120040104A5753ARC41251 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING O/B FLAP (FLAP SIDE) FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-74168 - WINGS - OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR 2L73 4F RTA22WE 20040115000872004011500087NM 2004 1 15 04003428 120040103A2611SD942201 SMOKE DETECTOR DORNERDO32 DO328300 NM FAULTY A VTZAD RETURN TO BLOCK BN SMOKE/FUMES/ODORS/SPARKS FALSE WARNING TXTAXI/GRND HDL 1 EA27428FJ 3193 DURING GROUND HANDLING OF FLIGHT 6128 TO BOS CREW RECEIVED LAVATORY SMOKE CAUTION MESSAGE WITH NO EVIDENCE OF SMOKE. THE SMOKE DETECTOR WAS DETERMINED TO BE FAULTY AND WAS REPLACED IN BOS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20040115000882004011500088NM 2004 1 15 04FDEA00056 120040106A5753ARC199114 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING FOUND LOOSE. LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75221, TITLE : WINGS - TE & TE DEVICES - RT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040115000942004011500094EA 2004 1 15 04003691 120040103A2910NAS16126 O-RING CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR LEAKING A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27691BR 7740 DURING PASSENGER BOARDING THE CREW REPORTED A STONG SMELL OF FUMES AND NOTICED A LARGE POOL OF HYDRUALIC FLUID BELOW THE MAIN LANDING GEAR DOORS. THE PASSENGERS WERE DEPLANED NORMALLY. THE LEAK WAS FOUND TO BE AN O-RING ON THE MAIN LANDING GEAR RETRACT ACTUATOR WHICH WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040113002102004011300210SO 2004 1 13 C2XA04IA003 120040106A323023092900001 UPLOCK EMB 145 EMB145ER 3260211SO LT MLG MALFUNCTIONED A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW271792814063 145007 FLIGHT 2072 - PILOT REPORTED THAT THE MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED AND LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX. THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM WAS OPERATIONALLY TESTED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040113002142004011300214SO 2004 1 13 C2XA04CL003 120040107A3040163500112 TERMINAL BLOCK EMB 145 EMB145XR SO COCKPIT MELTED A C2XAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2712135 145718 THE CREW REPORTED EXTREME ELECTRICAL SMOKE SMELL DURING THE LAST 20 MINUTES OF FLIGHT. NO VISUAL SMOKE WAS NOTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE FIRST OFFICER'S WINDSHIELD TERMINAL BLOCK WAS MELTED. THE WINDSHIELD WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040114001492004011400149NM 2004 1 14 AALA20040010 120040104A335050004003 BATTERY BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21634AA 24592 SFO EMERGENCY EXIT LIGHTS FROM AISLE SEAT 24D TO 34D INOPERATIVE. REPLACED BATTERY ABOVE RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040114001502004011400150WP 2004 1 14 AALA20040019 120040103A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2159523 49915 MIA LEFT AND RIGHT FORWARD EMERGENCY LIGHTS. REPLACED BATTERY PACK FOR LEFT AND RIGHT FORWARD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040114001512004011400151NM 2004 1 14 AALA20040048 120040110A335002031461201 LIGHT BOEING737 737823 13844BZNM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21970AN 30096 MIA RIGHT HAND AFT EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED RIGHT HAND EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040114001532004011400153WP 2004 1 14 AALA20040057 120040113A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21408AA 49319 PHX CEILING EMERGENCY LIGHTS AT STATION 902 RIGHT INOPERATIVE. REPLACED BATTERY PACK B5-104 FOR CEILING EMERGENCY LIGHTS AT STATION 902 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040114001552004011400155WP 2004 1 14 AALA20040058 120040112A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW OVERHEAD EMERGENCY LIGHT AT ROWS 18 THROUGH 21 AND AFT GALLEY ENTRY DOOR AND TAIL CONE EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR ROWS 18 THROUGH 21 OVERHEAD EMERGENCY LIGHTS, REPLACED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY ENTRY DOOR AND REPLACED BATTERY FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040114001562004011400156WP 2004 1 14 AALA20040059 120040113A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21484AA 49677 DFW EMERGENCY LIGHTS BETWEEN ROWS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK BETWEEN ROWS 17 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040115000612004011500061EU 2004 1 15 AALA20040027 120040105A3233 SCHRADER VALVE AIRBUS300 A300B4605R 3930308EU RT MLG ACTUATOR LEAKING A AALAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW2170072 515 BOS T2087/5 UNABLE TO RETRACT MAIN LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND MAIN LANDING GEAR TILT ACTUATOR SHRADER VALVE AND SERVICED ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040115000642004011500064NM 2004 1 15 04FDEA00110 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000662004011500066NM 2004 1 15 04FDEA00130 120040112A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP VANE TEE FITTING NR 5 (COUNTING FROM INBOARD) FOUND CORROSION ON FWD HOLE BORE AREA. LT OTBD FLAP VANE TEE FITTING NR 5 REPAIRED AS PER EA 1-5750-74291, WINGS - LT AND RT OUTBOARD FLAP - NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040115000672004011500067NM 2004 1 15 04FDEA00022 120040104A5340ACA73511 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CABIN LEFT 9-G NET YOKE ATTACHMENT FRAME DENTED. NET YOKE ATTACHMENT FRAME DENTED REPAIR CARRIED OUT AS PER DWG SRZ-53-503. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. 2L73 4F RTA22WE 20040115000692004011500069NM 2004 1 15 04FDEA00057 120040106A5753ARC198414 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG I/B SIDE BUSHING FOUND LOOSE. COMPLIED WITH FEDEX EA 1-5750-75219 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040115000722004011500072WP 2004 1 15 04FDEA00093 120040110A291063602 VALVE DOUG DC10 DC1010 3022110WP RT MLG LEAKING A FDEAK NONE KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO2568059 46907 RECEIVED MASTER CAUTION LIGHT & THEN HYD SYSTEM 3 PRESS LO LIGHTS. LOST 2 GAL HYD FLUID ON SYSTEM 3, STOPPED AT 6 GAL WHEN S/O TURNED PUMPS (SYST 3) OFF. RAN PHASE 1 RED TABS, DECLARED EMERGENCY. GEAR AND FLAPS WERE ALREADY SET AT THE TIME. LANDED UNEVENTFULLY. CRASH CREW REPORTED MASSIVE LEAK AT RIGHT MAIN GEAR TRUCK INSTALLED NEW VALVE PER MM 32-31-06. 2L73 4F A22WE 20040115000742004011500074NM 2004 1 15 04FDEA00097 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED ON SPOT FACES AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000832004011500083NM 2004 1 15 04FDEA00111 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE SPOT FACES. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000852004011500085NM 2004 1 15 04FDEA00113 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HINGE FOUND CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HINGE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000892004011500089NM 2004 1 15 04FDEA00101 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000902004011500090NM 2004 1 15 04FDEA00119 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD ACTUATOR LUG CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000922004011500092NM 2004 1 15 04FDEA00121 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE), OUTBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040122000362004012200036NM 2004 1 22 DHL2004745008 120040117A5730 PANEL BOEING727 727224 1384076NM LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 LT WING LOWER SURFACE OF PLANK BETWEEN PANELS 7213 AND 7212 WING STA 546 (APPROX) EXFOLIATED. CORROSION APPROX 1 X .75 INCH AT PLANK SEAM FWD PANEL. 2L73 4F A3WE 20040115001802004011500180WP 2004 1 15 AALA20040020 120040107A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21483A 49676 PHX EMERGENCY LIGHTS IN AFT CABIN DROP CEILING PANELS AND NR 1 EMERGENCY LIGHT FOR TAIL SLIDE INOPERATIVE. REPLACED B5-27 BATTERY PACK/CHARGER ASSEMBLY AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040115001862004011500186NM 2004 1 15 04FDEA00043 120040106A5753ARC198413 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING OB FLAP IB HINGE (FLAP SIDE) ACTUATOR LUG IB SIDE BUSHING FOUND LOOSE. REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TITLE : WINGS - TE & TE DEVICES - LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040122000382004012200038SW 2004 1 22 MV5R0551 120040109A5521 RIB MOONEYM20 M20C 5870208SW LYC O360 O360* 41514EA ELEVATOR CRACKED B MV5RO OTHER O OTHER NRNOT REPORTED 1 GL116034Q5288 3237 CRACKED OB RIB PN 430004 AND DAMAGED SKIN. 1L71 3O3 O 2A3 E286 20040115001872004011500187NM 2004 1 15 04FDEA00040 120040105A5753NRC6055509 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE SURFACE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WINGS - TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2L73 4F RTA22WE 20040115001912004011500191NM 2004 1 15 04FDEA00102 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115001932004011500193NM 2004 1 15 04FDEA00122 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115001982004011500198NM 2004 1 15 04FDEA00054 120040106A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 MAIN CABIN SEAT TRACK GOUGED & DAMAGED AT FS 910 RBL 62. GOUGE IN TRACK OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED BAD SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW TRACK SECTION ON TRAVELER T2/394338. INSTALLED NEW TRACK SECTION RBL 62 STA 870 TO 960 IAW SRM 51-30-2. 2L73 4F RTA3WE 20040115002012004011500201NM 2004 1 15 04FDEA00051 120040106A5712 RIB BOEING727 727200 138407ENM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 RIGHT WING, L/E OPENING UPPER INTERIOR, CORROSION ON L/E RIBS WHERE WIRE BUNDLE CLIP NUTS ATTACH WS 290 & 300. WS 301 BLENDED CORROSION IAW SRM 57-20-1, OUT OF LIMITS. REMOVED CORRODED T-CAP IAW SRM 51-30-2 AT WS 301, FABRICATED NEW T-CAP IAW SRM 51-20-1, 7075-T6 BATCH 677023, INSTALLED NEW T-CAP WS 301 IAW SRM 51-30-2, WS 290 BLENDED CORROSION IAW SRM 57-20-1, TREATED & PRIMED IAW SRM 51-10-2, RECONNECTED WIRING HARNESS CLAMP IAW SRM 51-30-2. 2L73 4F RTA3WE 20040115002022004011500202NM 2004 1 15 04FDEA00050 120040106A5720 ANGLE BOEING727 727200 138407ENM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 RIGHT WING L/E AT NR 6 K-FLAP OPENING, L/E LOWER SURFACE, PANEL TO SEAL RETAINER ANGLE IS EXFOLIATED (BELOW & FWD OF NR 6 K-FLAP ACTUATOR). REMOVED SEAL RETAINER ANGLE IAW 727 SRM 51-30-2. FABRICATED NEW SEAL RETAINER ANGLE IAW 727 SRM 51-20-1 FROM BAC 1506-1523, BATCH 687730. INSTALLED SEAL RETAINER ANGLE IAW 727 SRM 51-30-2. 2L73 4F RTA3WE 20040115002042004011500204NM 2004 1 15 04FDEA00003 120040101A2611774001 SMOKE DETECTOR BOEING727 727200 138407ENM CARGO BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25217FE1400914009 22938 ON CLIMBOUT, MAIN CARGO SMOKE WARNING ACTIVATED. SHORTLY THERE AFTER LIGHT EXTINGUISHED. APPROXIMATELY 1.5 TO 2 MINS LATER MAIN CARGO SMOKE WARNING RE-ACTIVATED. ALSO MIGRATED FROM ONE ZONE ILLUMINATED TO 2 ZONES (BULBS) ILLUMINATED. REPLACED ZONE 1 AND 2 DETECTION UNITS. ALL TESTS OK MM 26-16-001-0. 2L73 4F RTA3WE 20040115002052004011500205NM 2004 1 15 04FDEA00004 120040102A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 WHILE WORKING CARD NR N00298, FOUND DENTED AND CRACKED FRAME AT BS 640 RBL 13 WL 152. FOUND CRACK IN 640 FRAME OUT OF LIMITS. REPAIRED PER FED EX EA 7-5330-70609, SRM 53-10-1. 2L73 4F RTA3WE 20040115002062004011500206WP 2004 1 15 04FDEA00005 120040102A78309036M28G04 SUPPORT FITTING DOUG DC10 DC1010 3022110WP THRUST REVERSER WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-7832-73857. EXHAUST - THRUST REVERSER - REWORK OF WORN AREA ON T-R SUPPORT FITTING. CLOSING ACTION ON N/R S00022 ON 12/29/03. COMPLIED WITH EA 8-7832-73857. 2L73 4F A22WE 20040115002082004011500208WP 2004 1 15 04FDEA0006 120040102A5753ARB0005 CAP DOUG DC10 DC1010 3022110WP T/E FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-5710-73861. WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861. 2L73 4F A22WE 20040115002092004011500209NM 2004 1 15 04FDEA00025 120040105A5753NRC6055510 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WINGS - TRILAING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2L73 4F RTA22WE 20040127002512004012700251SW 2004 1 27 AC2A092336 120040108A6520 STUD BELL 430 430 1182150SW T/R GEARBOX BROKEN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CV3410 A720 49072 GEARBOX HAD TWO BROKEN MOUNTING STUDS. REMOVED GEARBOX FROM AIRCRAFT AND REPLACED STUDS, CHECKED GEARBOX PER MANUFACTURERS LETTER AND RE-INSTALLED GEARBOX. 1G72 3U RTH9SW 20040129000162004012900016SO 2004 1 29 MASA200400004 120040103A335014534984403 SOCKET EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ5617 145481 ASH 2701 CLT, MID CABIN EMERGENCY EXIT LIGHT INOP. MX TROUBLESHOT TO FAULTY LIGHT ASSY. MX REPLACED THE LIGHT ASSY, OP CHECKS GOOD. 2L72 4T RTT00011AT 20040129000172004012900017SO 2004 1 29 MASA200400008 120040102A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07825MJ 145179 ASH 2807 CLT-SDF, CEILING EMERGENCY EXIT LIGHT INOP AT ROW 12. WHEN MX ARRIVED THE LIGHT WAS OPERATING NORMALLY. NO PARTS USED. 2L72 4T RTT00011AT 20040129000962004012900096NE 2004 1 29 0400039905 220040104A7230 COMPRESSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 1 ENGINE STALLED A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01955N 47160 656996 DURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. TAKEOFF ABORTED AT 110 KNOTS. FLIGHT CREW INDICATED SNOW AND SLUSH ON RUNWAY. MAINTENANCE INSPECTED THE INLET AND EXHAUST, PS3 FILTER, AND SADDLE DUCTS; NO TROUBLE FOUND. ENGINE GROUND RUN TO TAKEOFF POWER AND ACCELERATION CHECKS WERE PERFORMED. EVERYTHING WITHIN LIMITS. 2L72 4F4 F A6WE E2EA 20040129000982004012900098NM 2004 1 29 0400056302 120040104A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 DURING L-CHECK, FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21ABC - 31ABC. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040129001262004012900126NM 2004 1 29 QXEA200400001 120040103A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09352PH 494 PDX- LAVATORY SMOKE ALARM SOUNDED DURING CLIMBOUT. FLIGHT ATTENDANT INVESTIGATED AND FOUND NO SMOKE IN LAVATORY OR CABIN. ALARM RESET BY FLIGHT ATTENDANT FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040129001272004012900127NM 2004 1 29 QXEA200400002 120040104A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09352PH 494 LMT- ON FLIGHT 2093 LAVATORY SMOKE ALARM CONTINOUSLY SOUNDS IN FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (CLOSED) 2H72 4T RTA13NM 20040129001322004012900132EA 2004 1 29 COMA0460011 120040102A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01949CA 7080 FLIGHT 5682 RIGHT THRUST REVERSER UNLOCK INFLIGHT. SECURED AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040129001332004012900133EA 2004 1 29 COMA0460012 120040102A2613355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT ENGINE UNRELIABLE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01952CA 7092 FLIGHT 5874 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED THE LEFT PYLON BLEED LEAK SENSING ELEMENT. 2L72 4F RTA21EA 20040129001342004012900134EA 2004 1 29 COMA0460013 120040104A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01962CA 7123 FLIGHT 5791 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040129001362004012900136 2004 1 29 MWEA040001 420040102A34224034241972 COMPUTER DOUG MD88 MD88 3023688NM E & E BAY INOPERATIVE A MWEAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL31601ME 49762 CAPTAINS FLIGHT MODE ANNUNCIATOR WENT BLANK AND THE CAPTAINS FLIGHT SYSTEM AND FLIGHT DIRECTOR FAIL INDICATIONS APPEARED ON THE CAPTAIN'S PRIMARY FLIGHT DISPLAY. REMOVED AND REPLACED LEFT DIGITAL FLIGHT GUIDANCE COMPUTER. 2L72 4F RTA6WE 20040129001382004012900138WP 2004 1 29 ABXA040001 120040106A3260 UPLOCK DOUG DC9 DC931 3022065WP LT MLG OUT OF ADJUST A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23944AX 47550 AFTER TAKEOFF, LT GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. PERFORMED THE UPLATCH CHECK ABNORMAL AND GEAR UNSAFE ABNORMAL. THIS DID NOT SOLVE THE PROBLEM. FOUND UPLATCH OUT OF ADJUSTMENT. ADJUSTED UPLATCH IAW DC-9 MM 32-31-04-2-0103. OPS CHECKED GOOD. POSITION AND WARNING SYSTEM TESTED GOOD IAW DC-9 MM 32-60-00-2-0101. 2L72 4F A6WE 20040129001452004012900145WP 2004 1 29 AALA20040023 120040106A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170529 49921 STL OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 18 THROUGH 21 INOPERATIVE. RESEATED BATTERY FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040129001472004012900147WP 2004 1 29 AALA20040025 120040105A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21448AA 49474 DFW LEFT HAND AND RIGHT HAND EXTERIOR OVERWING EMERGENCY ESCAPE LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK B45 49 LEFT HAND AND RIGHT HAND OVERWING EMERGENCY LIGHTS L2 663 AND L2 633. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040129001492004012900149NE 2004 1 29 0400029860 220040102A7230 ENGINE DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE FAILED A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01769NC451347669 47757 707924 DURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND LOSS OF POWER AT 105 KNOTS. FLIGHT CREW ABORTED TAKEOFF. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 1 ENGINE. 2L72 4F4 FRTA6WE E2EA 20040129001502004012900150NM 2004 1 29 DHL2004755001 120040105A3350 LIGHT BOEING727 727225 1384077NM L1 DOOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01755DH 21857 L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED L-1 DOOR EMERGENCY EXIT LIGHT IAW M/M 33-50-71. OPS CHECKED GOOD. 2L73 4F A3WE 20040129001512004012900151NM 2004 1 29 DHL2004763001 120040107A2612 FIRE LOOP BOEING727 727264 138408MNM NR 1 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01763AT 22983 NR 1 FIRE PROTECTION GROUND FAULT CIRCUIT LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 1 ENGINE FIRE LOOP FOR GROUND FAULT LIGHT. OK PER M/M 26-11-01. 2L73 4F A3WE 20040129001532004012900153NM 2004 1 29 HNAA0400002 120040105A5270 PROXIMITY SENSOR DHAV DHC8 DHC8301 1386003NM PAX DOOR OUT OF ADJUST A HNAAO OTHER N FALSE WARNING CRCRUISE 1 EA07331EN 331EN FORWARD EXIT DOOR WARNING LIGHT ILLUMINATED IN-FLT. ADJUSTED PROX SENSOR GAP, OPS CHECK GOOD. 2H72 4T RTA13NM 20040129001572004012900157EA 2004 1 29 COMA0460021 120040105A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01927CA 7031 FLIGHT 5504 SEVERAL EMERGENCY LIGHTS ARE INOP. REPLACED THE FLOOR LIGHT STRIP. 2L72 4F RTA21EA 20040129001582004012900158EA 2004 1 29 COMA0460020 120040105A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM STICKING A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO01472CA 7667 FLIGHT 5948 STAB TRIM AND MACH TRIM CAUTION MESSAGE. CLEANED STICKING DISCONNECT SWITCH. 2L72 4F RTA21EA 20040129001612004012900161WP 2004 1 29 0400069950 120040106A27805919526807 SLAT DOUG DC9 DC932 3022066WP LT WING MALFUNCTIONED A NWAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL019346 47376 DURING APPROACH INTO DCA, AIRCRAFT EXPERIENCED AN UNCOMMANDED LEFT ROLL WHEN SLATS WERE EXTENDED. THE SLAT DISAGREE LIGHT ILLUMINATED AND SLAT EXTEND DID NOT. COMPLIED WITH COM PROCEDURE AND SLATS WERE RETRACTED. A LONGER RUNWAY WAS NEEDED WITH SLATS RETRACTED SO THE FLIGHT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE DID NOT FIND ANY DEFECTS WITH THE SLAT SYSTEM. SLATS ON BOTH WINGS WERE CLEANED AND LUBRICATED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040129001662004012900166SO 2004 1 29 SWIA200412751 120040104A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07217SW9186 9186 120286 CREW REPORTED FLAP DISAGREE ALARM WHEN RETRACTING FLAPS. LEFT NACELLE FLAP SLOW TO ACTUATE IN OVERRIDE UP. REPLACED LEFT FLAP ACTUATOR WITH SERVICEABLE UNIT IAW EMB MM 27-50-08. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040129001672004012900167SO 2004 1 29 SWIA200412752 120040105A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07237SW 120314 ON APPROACH AT 130 KIAS SELECTED FLAP 45, GOT FLAP LIGHT ON MAP WITH ASSOCIATED CONTROL FAULT FLAP WARNING INDICATION. FLAPS OPERATED NORMALLY ON GROUND. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OP CHECK GOOD. S/N OFF: 0074. 2L72 4T RTA31SO 20040129001682004012900168 2004 1 29 04FDEA00064 420040107A3416 ALTIMETER AIRBUS300 A300B4622R 3930312EU COCKPIT MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25722FD 479 AT AROUND 60 - 70 KTS ON FIRST TAKEOFF, GOT A NAV ADC FAILURE ON ECAM. AFTER CLEARING RUNWAY FAILURE WENT AWAY. A SECOND TAKEOFF INITIATED AND UNABLE TO TOGA AND GOT A RUNWAY POSITION ERROR. CHECKED MTP AT BLOCK-IN, NO FAULTS OR LIGHTS SET. PERFORMED BITE TESTS OF BOTH ADC'S IAW M/M 34-10-00-5. CREW RE-INITIALIZED FMS, ALL SYS'S NORMAL. 2L72 4F RTA35EU 20040129001692004012900169NM 2004 1 29 04FDEA00059 120040106A5270 WARNING LIGHT BOEING727 727100 1384036NM CARGO DOOR ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25198FE 19154 MAIN CARGO DOOR LIGHT ILLUMINATED CLIMBING THRU FL270, .79 COMPLETED RED TABS AND LIGHT REMAINED ILLUMINATED. VISUALLY INSPECTED MCD, LATCHES AND ACTUATORS. OPERATED MCD FULL TRAVEL SEVERAL TIMES. MCD OPERATION IS NORMAL PER 727-100 AMM 52-34-009-0. CLEANED AND INSPECTED LATCH SWITCHES AND MCD WARNING LIGHT SOCKET IN AFT AIRSTAIR. PRESSURIZED AIRCRAFT TO 3.0 PSI PER JRH 7-23. MAIN CARGO DOOR LIGHT, CHECKS NORMAL. 2L73 4F RTA3WE 20040129001702004012900170 2004 1 29 027412 420040107A3431 RECEIVER SAAB SF340 SF340A 7850100EU VOR SYSTEM INOPERATIVE A UHLAO OTHER J WARNING INDICATION DEDESCENT 1 GL17360SZ 340A006 ON THIS DATE 1/7/04 AT APPROXIMATELY 1745Z, FLIGHT 4649 FROM BGM-PIT DECLARED AN EMERGENCY FOR VOR SYSTEM SHOWING RED LETTERS ON EFIS SYSTEM. BOTH VOR SYSTEMS INOP. 2L72 4T RTA52EU 20040129001722004012900172EA 2004 1 29 COMA0460022 120040106A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01506CA 7793 FLIGHT 5837 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040129001732004012900173EA 2004 1 29 COMA0460023 120040106A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01409CA 7441 FLIGHT 5222 CABIN DOOR WARNING DURING FLIGHT. COULD NOT DUPLICATE. INSPECTED DOOR AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20040129001832004012900183NM 2004 1 29 AALA20040033 120040107A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21691AA 25697 DFW SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPLACED SEAT 10D MOUNTED EMERGENCY LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040129001842004012900184NM 2004 1 29 AALA20040032 120040107A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21678AN 29428 MIA EMERGENCY LIGHT INOPERATIVE AT SEAT 20D. CLEANED DIRTY CONNECTOR CONTACT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040129001852004012900185WP 2004 1 29 AALA20040031 120040105A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21216AA 49167 TUL FOUND ONE INCH BY ONE INCH CORROSION ON LONGERON 22L AT STATION 1290. INSTALLED DOUBLER REPAIR PER SRM 53-02-00. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040129001922004012900192NM 2004 1 29 04FDEA00078 120040108A5754 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT WING - NR 16 SLAT TRACK LEADING EDGE INBOARD BRACKET CRACKED. RT WING NR 16 SLAT TRACK LEADING EDGE INBD BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II 2L73 4F RTA22WE 20040129001932004012900193NM 2004 1 29 04FDEA00077 120040108A5754ARC26531 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) FOUND 01 EA BRACKET CRACKED AT OUTBOARD SIDE APPROX 12 INCHES FROM FLAP LOWER SURFACE, 24 INCHES FROM FWD EDGE OF HINGE. LT INBD FLAP OTBD HINGE (FLAP SIDE) OTBD SIDE LOWER AREA 01 BRACKET EDGE CRACK TRIMMED OUT FOUND WITHIN LIMIT AS PER SRM 57-00-01 V1. 2L73 4F RTA22WE 20040129001942004012900194NM 2004 1 29 04FDEA00076 120040108A5754ARC25943 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. RT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 V2. 2L73 4F RTA22WE 20040129001952004012900195NM 2004 1 29 04FDEA00075 120040108A5754ARC25943 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET FOUND CRACKED. LT INBD FLAP OUTBD HINGE (FLAP SIDE) MOST AFT UPPER BRACKET REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040129001962004012900196NM 2004 1 29 04FDEA00074 120040108A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS, STA XOS 510 UNDER REFUEL ACCESS PANEL. LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I. 2L73 4F RTA22WE 20040129001972004012900197NM 2004 1 29 04FDEA00073 120040108A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 635 LEFT X=47.5. CABIN, CRACKED FLOOR TRACKS AT STA 635 LT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I 2L73 4F RTA22WE 20040129001982004012900198NM 2004 1 29 04FDEA00072 120040108A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=47.5. FLOOR TRACKS CRACKED AT STA 635 RT X=47.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG. 1 VOL. I. 2L73 4F RTA22WE 20040129002012004012900201NM 2004 1 29 04FDEA00069 120040108A5754 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING LEADING EDGE - NR 16 SLAT TRACK INTERNAL STRUCTURE CRACKED AT INBOARD TRACK BRACKET. LT WING LEADING EDGE NR 16 SLAT TRACK INTERNAL STRUCTURE I/B RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND EA 1-5750-74279, WINGS - LEFT HAND SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK. 2L73 4F RTA22WE 20040129002042004012900204NM 2004 1 29 QXEA200400003 120040106A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09366PH 241 510 PDX- EMERGENCY LIGHTS WOULD NOT SHUT OFF. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040129002062004012900206NE 2004 1 29 NACA20040003 220040107A8530356993 CYLINDER DOUG DC6 DC6B 3021712WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL037919C1604 1604 43554 NK510061 NR 1 ENGINE BMEP DROP FOLLOWED BY NR 1 CYLINDER TEMP. OIL ON COWLING. REPLACED NR 1 ENGINE, NR 2 CYLINDER DUE TO BEING CRACKED. 2L74 4R4 R 6A4 5E8 20040129002092004012900209NM 2004 1 29 SWAA040036 120040105A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED A1 CHECK, FOUND SKIN CRACK AT BS 790, STRINGER 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040129002102004012900210 2004 1 29 SWAA040037 420040105A2565D31354 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 DURING SCHEDULED C2 CHECK, FOUND R1, L1 AND L2 DOORS EVACUATION SLIDE GIRT BAR ASSEMBLIES OUT OF ADJUST. ADJUSTED R1, L1 AND L2 DOORS EVACUATION SLIDE PER MM. 2L72 4F RTA16WE 20040129002112004012900211NM 2004 1 29 SWAA040038 120040105A335010114 LIGHT BOEING737 7377H4 1384404NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 DURING MS CHECK, FOUND EMERGENCY EXIT FLOOR LIGHT INOP AT L1 DOOR. RELAMPED PER MM. 2L72 4F RTA16WE 20040129002122004012900212NM 2004 1 29 SWAA040039 120040105A55516551524 MOUNT BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND CORROSION AT HORIZONTAL STABILIZER RIGHT CENTER SECTION HINGE HOUSING UPPER MOUNT LUG. REPAIRED MOUNT LUG PER ER. 2L72 4F RTA16WE 20040129002132004012900213NM 2004 1 29 SWAA040001 120040101A3350207377 LENS BOEING737 7372T4 1384492NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 FOUND EEPLS TRACK LENS MISSING AT ROW 18. REPLACED TRACK LENS PER MM. 2L72 4F A16WE 20040129002152004012900215NM 2004 1 29 SWAA040003 120040101A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 933, STRINGER 24 R. REPAIRED PER SRM. 2L72 4F A16WE 20040129002162004012900216NM 2004 1 29 SWAA040004 120040101A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED CHECK, FOUND SKIN CRACKED AT BS 852, STRINGER 20 L. REPAIRED PER SRM. 2L72 4F RTA16WE 20040129002172004012900217NM 2004 1 29 SWAA040005 120040101A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED SP CHECK, FOUND STRINGER 16 L CRACKED AT BS 500. REPAIRED PER SB. 2L72 4F RTA16WE 20040130000022004013000002NM 2004 1 30 SWAA040007 120040101A52306547952 SKIN BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT UPPER AFT CORNER OF HANDLE CUTOUT. REPAIRED PER SRM. 2L72 4F RTA16WE 20040203000952004020300095SO 2004 2 3 C2XA04BT008 120040119A335020131A BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 DURING SERVICE CHECK MAINTENANCE FOUND NR 3 EMERGENCY LIGHT BATTERY WILL NOT CHARGE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB135 33-50-04. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040203001052004020300105NM 2004 2 3 UPS04441763 120040102A5320 REVEAL BOEING747 747123F NM L5 DOOR FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - L5 DOOR FWD CUTOUT REVEAL FOUND CRACK BETWEEN STRINGER S17L TO S18L. CUTOUT REVEAL PANEL, REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040203001062004020300106NM 2004 2 3 UPS04441764 120040103A532065B05002269 REVEAL BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - BS 805 BETWEEN LT STR -24 & STR -25 CUTOUT REVEAL FOUND CRACKED AS MARKED. CUTOUT REVEAL PANEL, REPLACED AS PER SRM 51-10-01. 2L74 4F A20WE 20040203001102004020300110NM 2004 2 3 UPS04441768 120040102A5320 REVEAL BOEING747 747123F NM R5 DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT REVEAL FOUND CRACK BETWEEN STRINGER S17R - S18R. M/D - R5 DOOR FWD EDGE BS 2231 STR 16R TO STR 19R FRAME STRAP AND REVEAL REPAIR CARRIED OUT IAW HX RS R-53-61-35096. (UPS EO NO B747-5310-19827-A). 2L74 4F A20WE 20040203001112004020300111NM 2004 2 3 UPS04441772 120040105A5310 SHEAR TIE BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, FWD CARGO COMPT BILGE SKIN SHEAR T/E FOUND CORRODED AT THE AREA BETWEEN STR 46 - 47 APPROX RBL 7 FRAME BS 540. SHEAR TIE REPLACED AS PER SRM 51-10-01. THE CORRODED AREA OF THE SHEAR TIE WAS DEPTH 0.050 INCH X LENGTH 3 INCH X WIDTH 2 INCH OUT OF LIMIT PER SRM 53-10-01 FIG 1. 2L74 4F A20WE 20040203001172004020300117NM 2004 2 3 QXEA20040051 120040120A33501014011 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09353PH 496 PDX- RIGHT HAND AFT EMERGENCY EXIT LIGHT BRIGHTNESS LEVEL IS LOWER THAN 100 MICRO LAMBERTS. REMOVED AND REPLACED BETA LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203001182004020300118NM 2004 2 3 QXEA20040052 120040120A33501014011 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09353PH 496 PDX- RIGHT HAND FORWARD EMERGENCY EXIT LIGHT BRIGHTNESS LEVEL IS LOWER THAN 100 MICRO LAMBERTS. REMOVED AND REPLACED BETA LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203001312004020300131EA 2004 2 3 MASA200400016 120040108A2730 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT ILLUMINATED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07510MJ 10101 ASH 7115 STL-DEN, CAPTAIN REPORTED A STAB TRIM/MACH TRIM CAUTION IN FLIGHT. A/C LANDED WITHOUT INCIDENT. MX RESET SYSTEM IAW FIM, OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040203001502004020300150EA 2004 2 3 COMA0460070 120040120A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01934CA 7042 FLIGHT 5596 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040203001522004020300152NM 2004 2 3 MWEA040008 120040122A53305910158111 DOUBLER BOEING717 717200 1383700NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31908ME 55172 FUSELAGE SKIN AT STATION 994 LONGERON 24 RIGHT IS DENTED AND CRACKED. INSTALLED EXTERNAL DOUBLER. 2L72 4F TRA6WE 20040203001532004020300153NM 2004 2 3 MWEA040009 120040122A53305910158113 SKIN BOEING717 717200 1383700NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31908ME 55172 FUSELAGE SKIN AT AFT CARGO DOOR OPENING AT STATION 982 IS DENTED AND CRACKED. INSTALLED EXTERNAL DOUBLER. 2L72 4F TRA6WE 20040203001572004020300157NM 2004 2 3 DHL2004755002 120040121A2612 FIRE LOOP BOEING727 727225 1384077NM NR 2 ENGINE MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01755DH 21857 NR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 FLASHES CONTINUOUSLY. DEFERRED PER MEL 26-9-1, DMI 15458, PLACARDS INSTALLED. REF DMI 15458 NR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 FLASHES CONTINUOUSLY. REPOSITIONED DETECTOR LOOP, AND CLEANED CONNECTORS IAW B-727 M/M 26-11-012. OPS CHECKED GOOD. THIS CLEARS DMI 15458. PLACARDS REMOVED. 2L73 4F A3WE 20040203001612004020300161NM 2004 2 3 CALA0400050 120040121A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 540, RBL 2 AND AT LBL 2. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040203001652004020300165EA 2004 2 3 COMA0460074 120040121A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01931CA 7037 FLIGHT 5004 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040203001822004020300182NM 2004 2 3 SWAA040186 120040120A3350OL3071BPEGPL LAMP BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED PM CHECK, FOUND AFT SECTION OF EEPLS TRACK INOP. RELAMPED PER MM. 2L72 4F A16WE 20040203001862004020300186NM 2004 2 3 SWAA040190 120040120A3350300432 LIGHT BOEING737 7373H4 1384600NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT PER MM. 2L72 4F RTA16WE 20040203001882004020300188NM 2004 2 3 SWAA040192 120040120A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 663.75, BL 0. REPAIRED FLOORBEAM WEB PER ER. 2L72 4F RTA16WE 20040203001952004020300195NM 2004 2 3 SWAA040199 120040120A2560P4010021 BATTERY BOEING737 7377H4 1384404NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED C1 CHECK, FOUND 2 EACH AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES FAILED. REMOVED AND REPLACED BOTH BATTERIES PER MM. 2L72 4F RTA16WE 20040203002062004020300206NM 2004 2 3 SWAA040093 120040109A5753 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E, AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM. 2L72 4F RTA16WE 20040203002092004020300209NM 2004 2 3 SWAA040096 120040109A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY LIGHT LENS COVER CRACKED. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT LENS PER MM. 2L72 4F RTA16WE 20040203002112004020300211 2004 2 3 SWAA040098 420040110A2565D31354 SLIDE BOEING737 737301 1384611NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040203002222004020300222 2004 2 3 SWAA040080 420040108A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PMC, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040203002282004020300228NM 2004 2 3 SWAA040061 120040107A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM FWD CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 FWD UPPER EMERGENCY FLASHLIGHT RED LED DOES NOT BLINK. REMOVED AND REPLACED UPPER FLASHLIGHT AND BATTERY PACK ASSEMBLY. 2L72 4F RTA16WE 20040203002312004020300231NM 2004 2 3 SWAA040064 120040107A53206551698 SPLICE BOEING737 7373H4 1384600NM STRINGER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 10L. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040203002422004020300242NM 2004 2 3 SWAA040129 120040112A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED PMC, FOUND SKIN CRACKED AT BS 757, STRINGER 18R. REPAIRED SKIN CRACK PER SRM. 2L72 4F A16WE 20040203002482004020300248NM 2004 2 3 SWAA040135 120040113A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STRIGER 4L. REPAIRED STRINGER SPILCE PER SRM. 2L72 4F RTA16WE 20040203002542004020300254NM 2004 2 3 SWAA040105 120040110A53106546550 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, RBL 15. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040203002642004020300264NM 2004 2 3 SWAA040115 120040111A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SC, FOUND SKIN CRACK AT BS 487, STRINGER 17R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002672004020300267NM 2004 2 3 SWAA040118 120040112A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACK AT BS 761, STRINGER 19R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002732004020300273NM 2004 2 3 SWAA040124 120040112A57536546481 BEARING BOEING737 7373H4 1384600NM TE FLAP LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C2 CHECK, FOUND PLAY AT RT WING OUTBOARD MIDFLAP INBOARD SPINDLE BEARING. REMOVED AND REPLACED RT WING OUTBOARD MIDFLAP SPINDLE BEARING PER MM. 2L72 4F RTA16WE 20040203002742004020300274 2004 2 3 SWAA040125 420040112A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002772004020300277NM 2004 2 3 SWAA040128 120040112A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED SC, FOUND SKIN CRACKED AT BS 515 TO BS 517 AT STRINGER 12L. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002922004020300292NM 2004 2 3 SWAA040154 120040115A52106547952 SKIN BOEING737 7373H4 1384600NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT L2 DOOR TOP HINGE. REPAIRED DOOR SKIN PER EA. 2L72 4F RTA16WE 20040203002942004020300294NM 2004 2 3 SWAA040156 120040115A53206584100 ANGLE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL LEG ANGLE CRACKED AT BS 700 STRINGER 18A, LBL 63. REPAIRED PER SRM. 2L72 4F RTA16WE 20040203003002004020300300NM 2004 2 3 SWAA040162 120040116A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040203003042004020300304 2004 2 3 SWAA040166 420040116A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29700GS 27835 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203003052004020300305NM 2004 2 3 SWAA040167 120040116A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED MS CHECK, FOUND OVERHEAD RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040203003142004020300314NM 2004 2 3 SWAA040176 120040118A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 380 BETWEEN STRINGERS 27L AND 27R. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040203003592004020300359NM 2004 2 3 P9RA20040004 120040121A2780251N509114 DRIVE ASSY BOEING757 757236 1384971NM RROYCERB211 RB211535E43754555NE SLATS BINDING A P9RAO OTHER J WARNING INDICATION APAPPROACH 1 SO11522NA29366 25133 ON APPROACH IN TO POS; AS FLAPS WERE SELECTED DOWN, EICAS MESSAGE L/E SLAT ASSY APPEARED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SLAT PDU IAW BMM 27-81-00. 2L72 4F4 FRTA2NM E12EU 20040203003732004020300373EA 2004 2 3 SWIA200412797 120040121A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07906SW 7510 SECOND ROW OF CABIN EMERGENCY LIGHTS (CEILING) INOP. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040203003782004020300378EU 2004 2 3 AALA20040103 120040122A3350 LIGHT FOKKERF28 F28MK0100 4990807EU CABIN LOOSE A AALAO OTHER O OTHER CRCRUISE 1 SW211403M 11354 SAT INFLIGHT T1983/22 EMERGENCY FLOOR LIGHT STRIP NEAR FORWARD GALLEY IS LOOSE. SECURED EMERGENCY FLOOR LIGHT NEAR FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040203003792004020300379NM 2004 2 3 AALA20040104 120040122A3350 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21646AA 24604 MIA SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. FOUND BROKEN WIRE ON EMERGENCY LIGHT AT SEAT 16D. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040203003882004020300388NM 2004 2 3 HNAA0400003 120040122A712087110016009 STRUT DHAV DHC8 DHC8201 2809001NM LT ENGINE CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07998HA1202112021 509 DURING MAINTENANCE INSPECTION, THE LT AFT ENGINE MOUNT VERTICAL STRUT WAS FOUND TO BE CRACKED. THE STRUT WAS REPLACED. 2H72 4T RTA13NM 20040203003962004020300396WP 2004 2 3 DHL2007806543 120040113A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 EXTERNAL FUSELAGE FWD SVC DOOR JAMB FWD UPPER CORNER CRACKED 1.000 AT STA 160.000 L-11R - L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181, DWG SRO8530021, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT CRACKED AREA IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181. FABRICATED FILLER (7075-T6AL 0.063), 2 EA DOUBLERS (7075-T6AL 0.063) (7075-T6AL 0.080) IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLERS AND FILLER IAW SRM 53-2-0 FIG 14 SHEET 3, TR 53-181, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040203003992004020300399WP 2004 2 3 DHL2004806526 120040106A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RT OUTER WING OUTBOARD L/E FORMER 0.250 INCH CRACK, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040204000082004020400008NM 2004 2 4 0400126303 120040117A3350 LIGHT BOEING747 747451 1384940NM ROW 21ABC-31ABC DISCONNECTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21ABC-31ABC. RECONNECTED FLOOR PATH LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040211000312004021100031NM 2004 2 11 AMTA200400029 120040110A2560 TRACK BOEING737 73783N 13844HINM GLOW STRIP MISSING A AMTAK NONE O OTHER ININSP/MAINT 1 GL11305TZ 30706 FOUND SECTION OF PHOTOLUMINESCENT EGRESS TRACK MISSING IN FARTHEST AFT CABIN ON LEFT. REPLACED SECTION OF PHOTOLUMNINESCENT TRACK LIGHTING AS REQ'D. (M) 2L72 4F RTA16WE 20040211000492004021100049EA 2004 2 11 COMA0460097 120040129A5230 SEAL CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR PINCHED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01976CA 7151 FLIGHT 5167 CABIN WOULD NOT PRESSURIZE AFTER T/O. CARGO HARNESS WAS PINCHED BETWEEN DOOR SEAL AND FUSELAGE. REPOSITIONED HARNESS. 2L72 4F RTA21EA 20040211000652004021100065NM 2004 2 11 04FDEA00291 120040203A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000792004021100079EA 2004 2 11 SWIA200412818 120040127A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07408SW5008 5008 7055 SPOILERONS FAULT STATUS MESSAGE ON TAXI OUT. RIGHT SPOILERON PANEL DEPICTION WAS WHITE ON FLIGHT CONTROL PAGE. REMOVED AND REPLACED RIGHT INBOARD PCU ON SPOILERON. OPS AND LEAK CHECKS GOOD IAW MM 27-61-01. 2L72 4F RTA21EA 20040211000812004021100081SO 2004 2 11 SWIA200412820 120040129A5720 SUPPORT EMB 120 EMB120ER 3260203SO RT WING LE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 A 7 INCH CRACK IN RIGHT WING INBOARD LEADING EDGE SUPPORT. DISCOVERED DURING LINE INSPECTION. REPLACED RIGHT WING INBOARD LEADING EDGE INBOARD SUPPORT IAW SRM 51-40-02. 2L72 4T RTA31SO 20040211000842004021100084EA 2004 2 11 SWIA200412824 120040127A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07407SW 7034 ON APPROACH, FLAP FAIL CAUTION MESSAGE AFTER SELECT FLAPS 30. PERFORMED QRH PROCEDURE AND LANDED OK. PERFORMED OPS CHECK OF FLAPS SYTSEM (FECU) IAW 27-51-10. ALL SYSTEM CHECKS GOOD, NO FAULTS, OPERATED FLAP IN ALL POSITIONS. 2L72 4F RTA21EA 20040211000932004021100093EU 2004 2 11 MALA040142 120040131A5300 STRUCTURE BAC 146 AVRO146RJ85A1500097EU AIRFRAME VIBRATION A MALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL15510XJ E2323 DURING FLT, VIBRATION FELT IN CONTROL COLUMN. HIGH FREQUENCY VIBRATION STILL FELT AT 250 KTS-270 KTS. VIBRATION MOST PRONOUNCED WHEN BANKING LEFT; ESPECIALLY WHEN RIGHT BANK ESTABLISHED, THEN LEFT CONTROL (ROLL) INPUT ENTERED. AIR RETURN TO MEM. WHILE REDUCED HIGH FREQUENCY VIBRATION STILL FELT AT 250 KTS-270 KTS. VIBRATION MOST PRONOUNCED WHEN BANKING LEFT; ESPECIALLY WHEN RIGHT BANK ESTABLISHED, THEN LEFT CONTROL (ROLL) INPUT ENTERED. MAINTENANCE INSPECTED LT TRAILING EDGE SEAL, FOUND IT NEEDED SOME ADJUSTMENTS TO 3 OF 5 SECTIONS. INSPECTED ROLL SPOILER ACTUATORS & ROD ENDS ALONG WITH CABLES TO BOTH LT & RT SIDES, ALL CHECKS GOOD. A/C NEEDS TEST FLIGHT FOR SLIGHT VIBRATION CHECK. 2H74 4F RTA49EU 20040211000952004021100095EU 2004 2 11 MALA040145 120040125A2710 CONTROL CABLE SAAB SF340 340B 7860101EU AILERON LOOSE A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING POST FLIGHT 3351, CONTROL COLUMN REQUIRES EXCESSIVE FORCE TO BANK AIRCRAFT TO THE LEFT. DOES NOT SPRINGLOAD BACK TO POSITION ON GROUND. MAINTENANCE FOUND LT AILERON CABLE TENSION LOW. ADJUSTED CABLE TENSION WITHIN LIMITS IAW AMM 27-11-00-2. LUBED LT AILERON SYS IAW MM REF AMM 27-11: ON GROUND-SPRING BACK MAY NOT OCCUR. MAY REQUIRE NEGLIGIBLE CTRL WHEEL MOVEMENT TO RETURN FROM FULL DEFLECTION. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040211000992004021100099NM 2004 2 11 AALA20040167 120040203A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21928AN 29528 MIA EMERGENCY LIGHTS ON SEATS 7D TO 11D INOPERATIVE. REPLACED BATTERY PACK AND CENTRAL MODULE FOR EMERGENCY LIGHTS ON SEATS 7D TO 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040211001012004021100101NM 2004 2 11 AALA20040169 120040202A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21690AN 29590 ORD AISLE EMERGENCY LIGHTS AT SEAT 9D INOPERATIVE. FOUND LOOSE CONNECTOR. RE-SECURED LOOSE CONNECTOR FOR AISLE EMERGENCY LIGHTS AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040211001112004021100111EU 2004 2 11 AWXA200400134 120040201A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 26 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20040211001152004021100115NM 2004 2 11 AWXA200400138 120040120A5315BAC1505100246 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 328, BETWEEN RBL 24 AND RBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER TEE CAP AT BS 328, BETWEEN RBL 24 AND RBL 45; FABRICATED A NEW REPLACEMENT UPPER TEE CAP AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 FIG 005. 2L72 4F RTA16WE 20040211001242004021100124SO 2004 2 11 RAIA00401036 120040126A2120 SMOKE EMB 145 EMB145 3260210SO COCKPIT DETECTED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03804HK 145082 5271-PIT, SMOKE IN COCKPIT AND CABIN. POSSIBLE GLYCOL NOT ELECTRIC. MAINTENANCE GROUND RAN BOTH ENGINES AND OPS CHECKED BLEED AND PACK SYSTEMS. NOTED FAINT GLYCOL ODOR WHICH DISSIPATED, NO SMOKE AT THIS TIME. 2L72 4F RTT00011AT 20040211001312004021100131SO 2004 2 11 C2XA04SH045 120040204A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040211001432004021100143EA 2004 2 11 VNAA0401013 120040124A2131 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE MALFUNCTIONED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07209PS 7874 DURING CLIMB, CREW COULD NOT PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO YOW. MAINTENANCE DEFERRED BOTH AUTO CABIN PRESSURE CONTROLLERS 21-31-1 CODE C. 2L72 4F4 FRTA21EA E15NE 20040211001472004021100147WP 2004 2 11 ABXA040052 120040129A3297 WIRE DOUG DC9 DC941 302207NWP LT MLG DOWNLOCK SHORTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 LEFT GEAR DOWNLOCK WIRE 16230E20 WAS SHORTED BETWEEN 53-65 AND P3-9100. ALSO FOUND WIRING CONDUIT CUT THROUGH IN OUTBOARD LEFT WHEEL WELL. REPAIRED ALL DAMAGED WIRES AND CONDUIT IN THE LEFT WHEEL WELL. 2L72 4F A6WE 20040211001482004021100148EA 2004 2 11 QXEA200400100 120040202A4930 FILTER CNDAIRCL600 CL6002C10 1390015EA APU FUEL ODOR A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09616QX 10128 DEN FLIGHT NR 4015 DURING STARTUP, INITIALLY HAD AN APU FAULT. THAT MESSAGE WENT AWAY. STARTED APU UP AND AIRCRAFT WAS FILLED WITH A STRONG ODOR OF JET FUEL. REPLACED FUEL FILTER. PERFORMED OPERATIONAL TEST AND LEAK TEST OF APU IAW CRJ700 MM TASK 49-31-01-400-801-A01 STEP 2E. OPERATIONAL AND LEAK TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040211001882004021100188NM 2004 2 11 UPS04441806 120040126A5310 SHEAR TIE BOEING747 747123 1384873NM AFT CARGO BILGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT CARGO BILGE AREA - FS 1680, STR S47L - 48L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 47L AND STR 48L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2L74 4F A20WE 20040211001902004021100190NM 2004 2 11 UPS04441808 120040127A5310 SHEAR TIE BOEING747 747123 1384873NM AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT CARGO COMPT - LT STA 1680 IN BETWEEN STR 45 AND STR 46 SHEAR TIE FOUND CRACKED. AFT CARGO COMPT BS 1680 BETWEEN STR 45L AND STR 46L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2L74 4F A20WE 20040211002022004021100202EA 2004 2 11 COMA0460108 120040202A26136243843 SENSOR CNDAIRCL600 CL6002B19 1900309EA RT WING MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01435CA7844 7473 FLIGHT 5167 WING OVERHEAT WARNING MESSAGE. REPLACED THE RT WING OVERHEAT SENSOR. 2L72 4F RTA21EA 20040324001692004032400169EU 2004 3 24 AALA20040315 120040303A5311 FRAME AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - FOUND CORROSION ON 1.0 BY 1.0 SECTION OF FRAME 56 AT STRINGERS 45 LEFT AND 46 LEFT (AFT CARGO) WITH A DEPTH OF 0.032. INSTALLED NEW FRAME SUPPORT FOR FRAME 56 AT STRINGERS 45 LEFT AND 46 LEFT PER SRM 53-10-13. 2L72 4F RTA35EU 20040324001772004032400177EA 2004 3 24 04078648 120040318A2170P1096 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN AIR DIRTY A VTZABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27648BR 7406 DURING CLIMB OF FLIGHT 7332 CREW RECEIVED A LAVATORY SMOKE MESSAGE AND CONFIRMED SMOKE WAS PRESENT IN THE CABIN. CREW RETURNED TO FIELD AND PASSENGERS DEPLANED THROUGH NORMAL DOOR ON TAXIWAY. THE SMOKE WAS FOUND TO BE CAUSED BY APU OIL OVER SERVICING CAUSING THE COALESCER BAGS TO BECOME OIL SOAKED THUS CREATING THE SMOKE IN THE CABIN. THE OIL LEVEL WAS CORRECTED AND COALESCER BAGS WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040324001792004032400179NM 2004 3 24 04077409 120040317A273043274 DISCONNECT UNIT DORNERDO32 DO328300 NM ELEVATOR INOPERATIVE A VTZABA EMER. DESCENT UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27409FJ 3161 DURING CLIMB OF FLIGHT 9844 CREW RECEIVED AN ELEVATOR DISCONNECT INDICATION AND RETURNED TO FIELD. THE ELEVATOR DISCONNECT UNIT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T RTA55NM 20040325000032004032500003EA 2004 3 25 ASOA04122 120040212A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040325000062004032500006EA 2004 3 25 ASOA04126 120040215A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL 28 AND LBL 28 OUTBOARD WING BOX FLOOR AREA WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL 28 AND LBL 28 OUTBOARD WING BOX FLOOR AREA IAW ASA EO 600-53-0111. (M) 2L72 4F RTA21EA 20040325000112004032500011EA 2004 3 25 ASOA04103 120040207A5270864808 PSEU CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11838AS 7246 FLT 4736 - DURING CLIMB-OUT FROM ICT-ATL, THE CREW RECEIVED A PASSENGER DOOR LATCH CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH. THE FLIGHT ATTENDANT VERIFIED SECURITY OF THE DOOR AND DETERMINED IT WAS CORRECTLY CLOSE. PRESSURIZATION BEING NORMAL, THE AIRCRAFT CONTINUED TO CLIMB. WHEN PASSING THROUGH 15,000 FEET A PASSENGER DOOR WARNING WAS RECEIVED AND IMMEDIATE DESCENT INITIATED. THE AIRCRAFT RETURNED TO ICT AND CREW REQUESTED EMERGENCY EQUIPMENT DUE TO HIGH GROSS WEIGHT AND ICY RUNWAY CONDITIONS. THE AIRCRAFT LANDED SAFELY IN ICT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000162004032500016EA 2004 3 25 ASOA04105 120040209A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11867AS 7463 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040325000222004032500022EU 2004 3 25 ASOA04118 120040212A5343S53973202216 SUPPORT BRACKET AEROSPATR72 ATR72212 8680945EU LT MLG CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURING AN A-CHECK IN MCN, THE LEFT MAIN LANDING GEAR UPSTOP SUPPORT BRACKET ON THE TOP SIDE AT 'C' WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPSTOP SUPPORT BRACKET. (M) 2H72 4T RTA53EU 20040325000772004032500077SW 2004 3 25 AC2A093326 120040205A6510430044100101 DRIVE SHAFT BELL 430 430 1182150SW ALLSN 250C 250C* GL NR 2 BLISTERED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 PAINT IS BLISTERED AND PEELING FROM OVERHEATING. REPLACED DRIVE SHAFT 1G72 3U3 URTH9SW E4CE 20040325000802004032500080NE 2004 3 25 BAQA093253 220040212A73130319307840 INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE NR 1 ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME502 0143 30166 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/24/2004 1G72 3U3 U H88EU E19EU 20040325000822004032500082GL 2004 3 25 BAQA092464 220040223A7532 SHAFT AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL BLEED VALVE WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03912KY5278 FF13293 5500 CAE841019 BLEED VALVE SHAFT WORN. BLEED VAVLE IS ORIGINAL EQUIPMENT OFF OF ENGINE. REPLACED WITH SERVICABLE UNIT. 02/25/2004 1G72 3U3 U H11EU E4CE 20040325000832004032500083GL 2004 3 25 BAQA092608 220040209A720023057142 CASE HALF AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL ENGINE CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03912KY 5500 CAE841019 PLASTIC MISSING/CRACKED BEYOND LIMITS. UNIT ORIGINAL EQUIPMENT OFF OF ENG.. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1G72 3U3 U H11EU E4CE 20040325001102004032500110SW 2004 3 25 HEEA093479 120040217A2910 PACKING BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE HYD PUMP LEAKING B HEEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW038045T 28101 THE OIL COOLER WARNING LIGHT ILLUMINATED. RETURNED. FOUND A CUT PACKING ON FITTING ON UTILITY HYDRAULIC PUMP ALLOWING ALL FLUID TO LEAK OUT. REPLACED PACKING. 2G72 4U4 U H10SW E8NE 20040325001112004032500111EU 2004 3 25 BAQA091778 120040219A28221176415103 PUMP BOLKMS117 BK117B1 5626012EU FUEL BOOST INTERMITTENT B BAQAL ABORTED APPROACH J WARNING INDICATION NRNOT REPORTED 1 EA03945ME 7235 PUMP HAS A INTERMITTENT FAIL LIGHT. REPLACED WITH SERVICABLE UNIT FROM AEC. 1G72 3U H13EU 20040325001132004032500113EU 2004 3 25 BAQA093316 120040221A6330L633M2010104 MOUNT UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE M/R GEARBOX OUT OF LIMITS B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH448 0273 A/C VIBRATION, MOUNT OUT OF LIMITS, REMOVED FROM RT FWD POSITION. THIS UNIT WAS ONE OF THE 4 SENT TO A/C S/N 0287. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1G72 3U3 U H88EU E19EU 20040325001162004032500116EU 2004 3 25 BAQA093319 120040219A6330L633M2010105 MOUNT UROCOPEC135 EC135P2 5620027EU M/R GEARBOX CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135WJ37 0287 MAIN ROTOR GEARBOX MOUNT HAS ACRACKED INNER BELLOWS. REPLACED WITH SERVICABLE UNIT. 02/26/2004 1G72 3U H88EU 20040325001172004032500117 2004 3 25 BAQA092533 420040205A221041800562312 ACTUATOR AEROSPAS365 AS365N2 8680815EU PITCH INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME659 6417 PITCH ACTUATOR INTERMITTENT KICK OFF. OFF PITCH LANES. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004 1G72 3U RTH10EU 20040325001302004032500130EU 2004 3 25 BAQA091960 120040222A6330L633M2010103 MOUNT UROCOPEC135 EC135P1 8680990EU M/R GEARBOX COLLAPSED B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03577LF119 0140 COLLAPSED AND FLAT, LEAKING FLUIDS, PLUNGER SUCKED UP INSIDE. REPLACED WITH SERVICABLE UNIT. 03/02/2004 1G72 3U O H88EU 20040325001432004032500143EU 2004 3 25 BAQA093638 120040217A6210117151321 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG3048 7506 BLADE DIVES IN FORWARD FLIGHT. BLADE WAS INSTALLED .2 HOURS SINCE WE HAD RECEIVED AS AN EXCHANGE UNDER OUR PO 8-080114-10. BLADE HAS ACCUMULATED 106.1 HOURS SINCE 10/23/2001 AND HAS BEEN REPAIRED THREE TIMES IN THAT TIME SPAN WITH THIS BEING THE FOURTH. AIR METHODS HAD BLADE INSTALLED ON A/C 7111 ON 02/26/2003 FOR A TOTAL OF .3 HOURS BEFORE RECEIVED. 1G72 3U NCH13EU 20040325001442004032500144EU 2004 3 25 BAQA093639 120040217A6210117151321 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR OUT OF TRACK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG6941 7506 BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. BLADE WAS INSTALLED ON A/C N911TG/7506 FOR A TOTAL OF 2.4 HOURS. LAST REPAIR WAS A INSURANCE CLAIM, REF. PO 1-010199-41. 1G72 3U NCH13EU 20040325001472004032500147EU 2004 3 25 BAQA093315 120040224A6710L673M40A1001 BEARING UROCOPEC135 EC135T1 5620026EU ACTUATOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME1572 0157 BEARING HAS PLAY BEYOND LIMITS. INSTALLED UNIT WAS CANNED FROM A SHIP. REPLACED WITH SERVICABLE UNIT. 03/04/2004 1G72 3U H88EU 20040325001502004032500150EU 2004 3 25 BAQA093669 120040224A7714L21176209 CASE BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE ENGINE WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G4604 7179 CASE IS WORN AND BENT. AEC SCRAP SHEET AND MMIR BEING FAXED. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1G72 3U3 U H13EU E5NE 20040326000042004032600004 2004 3 26 0400469960 420040321A2213258668911 CONTROL PANEL DOUG DC9 DC931 3022065WP CENTER CONSOLE SHORTED A NWAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL01920RW 47163 COCKPIT CREW REPORTED HEAVY SMOKE AND SPARKS COMING FROM THE CENTER CONSOLE WHILE AT CRUISE. FLIGHT DIVERTED TO AN UNEVENTFUL SAFE LANDING AT GRR. NO FIRE EXTINGUISHER WAS USED AND SOURCE OF THE SMOKE STAYED RESTRICTED TO THE AUTOPILOT CONTROL PANEL LIGHTING. MAINTENANCE AT GRR FOUND THE CONTROL PANEL LIGHT PLATE HAD SHORTED OUT AND REPLACED IT. ALL CHECKS WERE GOOD AND SYSTEM WAS QUALIFIED FOR LLM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040326000222004032600022 2004 3 26 2004UALA00234 420040314A2565 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE GIRT BAR OUT OF ADJUST A UALAK NONE O OTHER ININSP/MAINT 1 WP29773UA 26929 DOOR 4L AFT GIRT BAR PICK UP FITTING CRACKED. CAUSE LATER WAS DETERMINED TO BE THE THRESHOLD GIRT BAR FITTING OUT OF ADJUSTMENT, RESULTING IN A PRELOAD ON THE GIRT BAR AND THE GIRT BAR FITTING WHEN THE DOOR WAS CYCLED THROUGH ARM/DISARM. THE GIRT BAR FITTING WAS REPLACED, BUT THE THRESHOLD GIRT FLOOR FITTING WAS NOT ADJUSTED, RESULTING IN THE SAME FITTING CRACKING 6 DAYS LATER (SEE MRR 2004UALA00268) 2L72 4F4 FRTT0001SE E46NE 20040329000092004032900009EA 2004 3 29 ASOA04110 120040210A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040329000102004032900010EA 2004 3 29 ASOA04109 120040210A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621, AFT PRESSURE BULKHEAD IN THE CARGO AREA ON THE LEFT AND RIGHT SIDES WERE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621, AFT PRESSURE BULKHEAD IN THE CARGO AREA ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040329001142004032900114EA 2004 3 29 COMA0460209 120040317A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01988CA 7204 FLIGHT 5711 FLAPS FAIL WARNING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040329001192004032900119EA 2004 3 29 COMA0460212 120040315A2752854D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01977CA3385 7157 FLIGHT 5851 FLAPS FAILED AT 3 DEGREES. COULD NOT DUPLICATE. REPLACED NR 4 FLAP ACTUATOR. 2L72 4F RTA21EA 20040329001272004032900127 2004 3 29 0400413217 420040315A2565D30664105 SLIDE AIRBUS320 A320211 3930320EU CABIN WILL NOT TEST A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01317US3177713 197 DURING EMERGENCY SYSTEM TEST, RECEIVED EXT LOAD FWD L MESSAGE. REPLACED THE RIGHT SLIDE GIRT BAR AND SLIDE ASSEMBLY, TESTED OK. REINSTALLED SLIDE COVER AND RE-ARMED DOOR ASSIST BOTTLE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040329001302004032900130WP 2004 3 29 0400409617 120040314A5313 LONGERON DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617NW 47235 DURING H-CHECK FOUND CRACK IN LONGERON AT FORWARD BULKHEAD BS 756. REPAIRED PER EA 96-197855. 2L72 4F A6WE 20040329001352004032900135EU 2004 3 29 2004UALA00196 120040306A5610 SEAL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE WINDSHEILD FAILED A UALAO OTHER O OTHER APAPPROACH 1 WP29449UA 851 DURING APPROACH WINDSHIELD CRACKED AND BEGAN TO ARC. WEATHER SEAL DETERIORATION LED TO DELAMINATION OF WINDOW ALLOWING WATER INGRESION CAUSING ARCING AT THE BUS BAR AND HEAT FILM RESULTING IN CRACKING OF THE WINDSHIELD. THE WINDSHIELD WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040329001402004032900140NM 2004 3 29 2004UALA00201 120040305A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 LIGHTNING STRIKE BLENDED OUT OF LIMIT AT STA 190 AND STRINGER 28AL (LEFT). MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED EXTERNAL SKIN DOUBLER. 2L74 4F4 FRTA20WE E24NE 20040329001482004032900148WP 2004 3 29 MWEA040021 120040224A801138334221 STARTER DOUG DC9 DC981 3022081WP ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31807ME 48033 ENGINE STOPPED ROTATING AT APPROXIMATELY 12 PERCENT HIGH PRESSURE COMPRESSOR SHAFT SPEED RPM DURING START ATTEMPT AND RETURNED TO ZERO. REMOVED AND REPLACED STARTER ASSEMBLY. 2L72 4F A6WE 20040329001502004032900150NM 2004 3 29 2004UALA00209 120040305A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP2989UA 24664 STRINGER CLIP CRACKED AT BS 727C S4R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED BRACKET. 2L72 4F4 FRTA16WE E2GL 20040329001562004032900156NM 2004 3 29 MWEA040029 120040322A2420762888B GENERATOR BOEING717 717200 1383700NM APU FALSE INDICATIONA MWEAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 GL31905ME 55169 GENERATOR FAILED APU STARTED AND POWER BUSSES NORMAL, STATUS PAGE SHOWS LEVEL TWO ALERTS THAT ARE PRESENT. PERFORMED FIM 24-20-801, NO FAULTS FOUND. 2L72 4F TRA6WE 20040329001602004032900160EU 2004 3 29 CX7A194J0415 120040304A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE FALSE ACTIVATIONA CX7AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03308CE 340B210 LEFT TAILPIPE HOT IN FLIGHT. AIR RETURN TO SBN. 2L72 4T RTA52EU 20040329001622004032900162NM 2004 3 29 2004UALA00216 120040213A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 AFT PIT SHEAR TIE CRACKED AT BS 907 STR 19L. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED SHEAR TIE AND FILLER MATERIAL. 2L72 4F4 FRTA16WE E2GL 20040329001642004032900164NM 2004 3 29 2004UALA00218 120040309A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 SKIN AT BS 380 STR 22L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND SPLICE. 2L72 4F4 FRTA16WE E2GL 20040329001682004032900168EU 2004 3 29 2004UALA00221 120040309A5315 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29452UA 955 CABIN FLOOR FRAME SUPPORT AT FR 12.24 CORRODED AT RIGHT O/B AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME. 2L72 4F4 FRTA28NM E40NE 20040329001712004032900171EU 2004 3 29 2004UALA00224 120040309A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29452UA 955 FLOOR SUPPORT CORRODED BETWEEN FR 19-20 RBL 6. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM. 2L72 4F4 FRTA28NM E40NE 20040329001772004032900177NM 2004 3 29 2004UALA00230 120040310A5753 FITTING BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LT WING TE FLAP WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29603UA 21864 LEFT WING INBOARD FLAP COLLAR FITTING WORN. MAJOR REPAIR ACCOMPLISHED. REPLACED LEFT WING INBOARD FLAP COLLAR FITTING. 2L72 4F4 FRTA1NM E3NE 20040329001872004032900187NE 2004 3 29 2004UALA00175 220040228A7200 ENGINE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RIGHT OVERHEATED A UALAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION DEDESCENT 1 WP29799UA 26926 RIGHT ENGINE OIL TEMP TO 145C AND OIL PRESSURE DROPPED TO 40-45 PSI TOP OF DESCENT INTO KIX. SHUT DOWN ENGINE. NR 1 BEARING FAILURE. THIS IS THE MAIN THRUST BALL BEARING SUPPORTING THE N1 ROTOR. OUTER RACE HEAVILY SPALLED THROUGH 100¡ ARC. ONE BALL HEAVILY SPALLED; ALL OTHERS, LIGHT-MODERATE SPALLING. CAGE FRACTURED AXIALLY THROUGH ONE BALL POCKET. NO SPALLING ON INNER RACES. BEARING IS PRE PRATT & WHITNEY SERVICE BULLETIN PW4G-112-72-212 PART NUMBER. BEARING WILL BE REPLACED WITH POST SB-212 PN WHICH HAS INCREASED DURABILITY. NOTE: ENGINE THRUST BALANCE SYSTEM WAS CONFIRMED TO BE FUNCTIONING NORMALLY. 2L72 4F4 FRTT0001SE E46NE 20040329001922004032900192WP 2004 3 29 AALA20040338 120040310A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21437AA 49455 TPA - FORWARD CABIN AND COCKPIT EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-34 FOR FORWARD CABIN AND COCKPIT EMERGENCY OVERHEAD LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040330000022004033000002NM 2004 3 30 04FDEA00623 120040310A5744ARC050214 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75298 - WINGS - OUTBOARD TRAILING EDGE FLAPS, INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, - REPAIR. 2L73 4F RTA22WE 20040330000052004033000005NM 2004 3 30 DLM88040226 120040310A2420696233B CSD DOUG MD88 MD88 3023688NM LT ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING M OVER TEMP CRCRUISE 1 SO27903DL 49534 TEN MINUTES INTO FLT GOT LT GEN OFF MSG. LEFT CSD TEMP WAS RISING THRU YELLOW AND RED ARC. REPLACED LT ENGINE CSD AND GENERATOR. 2L72 4F RTA6WE 20040330000102004033000010NM 2004 3 30 DL757040231 120040312A7500PW2037RTC ACTUATOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENG BLEED FAILED A DALAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 SO27616DL 22823 727297 FLAMEOUT DURING LANDING ROLLOUT. REPLACED 2.5 BLEED ACTUATOR. 2L72 4F4 FRTA2NM E17NE 20040330000132004033000013NM 2004 3 30 DL757040214 120040303A2820125334D VALVE BOEING757 757232 1384965NM RT WING MALFUNCTIONED A DALAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO27661DN 24972 FUEL LEAKING AT GOOD RATE OUT OF RIGHT WING TIP. SECURED ALL FUEL PUMPS. NOTICED FUEL HAD TRANSFERRED FROM LEFT MAIN TO RIGHT MAIN TANK. FOUND RT ENGINE SPAR VALVE BODY CRACKED. REPLACED VALVE, CHECKS OK. 2L72 4F RTA2NM 20040330000142004033000014NM 2004 3 30 DLM88040215 120040303A3240 MANIFOLD DOUG MD88 MD88 3023688NM BRAKES FAILED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27942DL 49815 AFTER TOUCHDOWN THE CREW APPLIED MAX BRAKES WITH NO A BRAKE PRESSURE AVAILABLE. REPLACED BRAKE MANIFOLD AND VALVE. 2L72 4F RTA6WE 20040330000172004033000017NM 2004 3 30 DLM88040218 120040307A2432021904000 BATTERY DOUG MD88 MD88 3023688NM E/E COMPARTMENT OVERHEATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27913DL 49544 SMOKE OBSERVED COMING FROM BATTERY VENTS JUST AFT OF NOSEWHEEL AT GATE. REPLACED ACFT BATTERIES AND CHARGER AND BATTERY THERMAL SENSORS PER M/M. 2L72 4F RTA6WE 20040330000182004033000018NM 2004 3 30 DL73G040219 120040307A3397 WIRE BOEING737 73735B 13844BMNM EMERGENCY LIGHTSDAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27225DL 25069 SEVERAL EMERGENCY LIGHTS INOP. REPAIRED WIRING, CHECKS NORMAL. 2L72 4F RTA16WE 20040330000202004033000020NM 2004 3 30 DLM88040221 120040308A3350 LENS DOUG MD88 MD88 3023688NM EMERGENCY LIGHT MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27935DL 49722 AFT STAIRWAY CENTER EMERGENCY LIGHT MISSING LENS AND INOP. REPLACED LENS AND BATTERY PACK. 2L72 4F RTA6WE 20040330000232004033000023NM 2004 3 30 DL76S040225 120040303A5532175T20011 PANEL BOEING767 767332 1382001NM VERTICAL STAB DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27129DL 24079 VERTICAL STABILIZER LEFT LOWER PANEL ASSY, FWD TORQUE BOX FSS 12 - FSS 271 DELAMINATION. REPAIRED PER ER/A 088833-14. 2L72 4F RTA1NM 20040330000242004033000024NM 2004 3 30 DL75K040236 120040312A2910271N61191 LINE BOEING757 757232 1384965NM HYD SYSTEM RUPTURED A DALAO OTHER K FLUID LOSS LDLANDING 1 SO27645DL 24216 ON TOUCHDOWN GOT LEFT HYDRAULIC SYSTEM FAILURE, QUANTITY IS AT .07RF. THE AIRCRAFT WAS TOWED BACK TO THE GATE, INSPECTED THE LEFT LANDING GEAR AND FOUND THE DOWNLOCK ACTUATOR FWD HYDRAULIC LINE LEAKING. THE LINE WAS REPLACED AND THE HYDRAULIC SYSTEM WAS REFILLED AND PRESSURIZED WITHOUT INCIDENT. 2L72 4F RTA2NM 20040330000252004033000025NM 2004 3 30 DLM90040237 120040314A273008BHG36ABJF733 TRANSMITTER DOUG MD90 MD9030 3023690NM ELEVATOR MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27915DN 53395 PYLON FLAP FAULT AND ELEVATOR SPLIT MESSAGE CAME ON AT FL310. REMOVED AND REPLACED RT AND LT ELEVATOR POSITION SENSORS PER M/M. ADJUSTED BOTH PER M/M. BOTH LEFT AND RIGHT TRANSMITTERS WITHIN M/M LIMITS. PYLON FLAP TEST CHECK GOOD. 2L72 4F RTA6WE 20040330000272004033000027NM 2004 3 30 DLM88040239 120040315A3220329001106 CYLINDER DOUG MD88 MD88 3023688NM NLG FAILED A DALAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 SO27946DL 49819 NOSE GEAR DID NOT EXTEND DURING NORMAL EXTENSION. REPLACED NOSE GEAR BUNGEE CYLINDER. 2L72 4F RTA6WE 20040330000282004033000028NM 2004 3 30 DL76S040240 120040314A3270849704 PSEU BOEING767 767332 1382001NM DOOR WARNING FAILED A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27134DL 25123 ENTRY DOORS, EMERGENCY DOOR, CARGO DOORS, ACCESS DOOR ALL ILLUMINATED AT ONCE. PLUS THE SLIDE LIGHTS BLINKING IN CABIN WITH ASSOCIATED EICAS MSGS. SEAT BELT FAIL TO EXTINGUISH IN AUTO. REPLACED PSEU, CKS OK PER M/M. DOOR SLIDE SEAT BELT SIGNS WARNING INDICATIONS CHECK OK. 2L72 4F RTA1NM 20040330000292004033000029NM 2004 3 30 DL73S040241 120040316A2420244702780 CSD BOEING737 737232 1384475NM RT GENERATOR FAILED A DALAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SO27324DL 23096 ON TAKEOFF RT GEN LOW OIL PRESS LIGHT ON WITH GEN DROPPING OFF LINE WITH APU POWERING LEFT BUS DUE TO MCO ON LEFT GEN. AFTER FIVE MINUTES LOW OIL PRESSURE LIGHT OUT AND RIGHT GEN BACK ON RIGHT BUS, FREQS LOW AT 390, RIGHT GEN FELL OFF BUS AGAIN FOR REMAINDER OF FLIGHT. REPLACED CSD AND COOLER. 2L72 4F RTA16WE 20040330000322004033000032NM 2004 3 30 DL757040245 120040317A3350487191 SPLICE BOEING757 757232 1384965NM EMERGENCY LIGHT SEPARATED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27606DL 22813 EMERGENCY TRACK LIGHTS INOP ROWS 19-27. REPLACED SPLICE AT SEAT ROW 27. 2L72 4F RTA2NM 20040330000332004033000033NM 2004 3 30 DL73S040246 120040318A2781 PROXIMITY SENSOR BOEING737 737247 138448DNM NR 6 SLAT FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27242WA 23516 DISCONTINUED T/O AT 30 KTS FOR NR 6 SLAT IND. REPLACED NR 6 SLAT PROX SENSOR. 2L72 4F A16WE 20040330000342004033000034NM 2004 3 30 DL738040247 120040318A2750S256A40450 TRANSMITTER BOEING737 737832 13844CFNM LT WING INTERMITTENT A DALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO27381DA 30350 SELECTING FLAPS ON APPROACH TRAILING EDGE FLAPS STOPPED BETWEEN UP AND 1 DEG AND LEADING EDGE TRANSIT AMBER LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL CK LIST AND LANDED WITH TOUCH DOWN SPEED OF 178 KTS. AUTO BRAKES SET TO 2, WT 139.5 T/S PER FIM 27-51-00-810-836. SYSTEM CHECKS GOOD. NO CURRENT FAULTS ON FSEU. DUE TO FAULT 27-52259. T/E FLAP SENSOR L ON FSEU HIST LEG 12. REPLACED LT FLAP POS IND SENSOR PER MM. ALL CKS GOOD. NOT AN RII ITEM PER TOPPS 40-30-05. 2L72 4F RTA16WE 20040330000372004033000037 2004 3 30 DLM88040251 420040321A3417349001222 COMPUTER DOUG MD88 MD88 3023688NM AIR DATA FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27983DL 53247 ON T/O ROLL, CP AIRSPEED IND FAIL AFTER 80 KTS. ABORTED AT 90 KTS. REPLACED NR 2 ADC. 2L72 4F RTA6WE 20040330000402004033000040NM 2004 3 30 DL73S040254 120040321A335020131A BATTERY BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27334DL 23105 FOUND AFT UPPER LT EMERGENCY LIGHTS 3 EACH INOP. REPLACED BATTERY ASSY, OPS NORMAL. 2L72 4F RTA16WE 20040330000422004033000042NM 2004 3 30 DL73S040258 120040320A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27302DL 23047 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 14R SKIN LAP JOINT. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE DAMAGED AREA AND AN ALUMINUM REPAIR DOUBLER INSTALLED PER B737 SRM AND DOCUMENTED PER ER/A 089003-14AD. 2L72 4F RTA16WE 20040330000442004033000044NM 2004 3 30 DL76K040260 120040323A33501317 BULB BOEING767 767332 1382001NM RIGHT WING BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27177DZ 29698 EXTERNAL EMERGENCY LIGHTS, FWD OF C2 DOOR AND AFT TWO OVER RIGHT WING, INOP. CLEANED SOCKET ON EMERGENCY LIGHT FWD OF C2 DOOR. RELAMPED THE TWO RIGHT OVERWING. CHECKS GOOD. 2L72 4F RTA1NM 20040330000462004033000046NM 2004 3 30 2004UALA00177 120040229A3230272W61613 LINK ASSY BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT MLG CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29790UA29578 26943 HYDRAULIC LINE SUPPORT BRACKET BROKEN AT TRUCK OF LEFT MAIN LANDING GEAR. LEFT MLG HYD TUBE SUPPORT LINK ASSY (P/N 272W6161-3) WAS FOUND CRACKED AT THE INBOARD LOWER ATTACH LEG. SUPPORT LINK ASSEMBLY WAS REPLACED. BOEING NOTIFIED THIS IS A REOCCURRING PROBLEM FOR THE FLEET. 2L72 4F4 FRTT0001SE E46NE 20040330000472004033000047NM 2004 3 30 2004UALA00250 120040315A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 DENT IN FUSELAGE 4:00 O'CLOCK POSITION FWD OF FWD CARGO DOOR (APPROX 12 INCHES BELOW AND 10 INCHES FWD OF OXYGEN THERMAL DISCHARGE DISC). MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040330000502004033000050NM 2004 3 30 2004UALA00253 120040316A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29107UA 26900 EMERGENCY EXIT LIGHTS AT DOOR 4R INOP AT TWO LOCATIONS. REPLACE BATTERY PACK BASE AND PACK. 2L74 4F4 FRTA20WE E24NE 20040330000512004033000051NM 2004 3 30 2004UALA00254 120040316A5270 TARGET BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR OUT OF ADJUST A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29305UA 23666 RETURNED TO THE FIELD DUE TO A CARGO DOOR INDICATION. ADJUSTED TARGET. THE TARGET CAN BE DAMAGED/MISALIGNED DURING THE BAG LOADING PROCESS. THIS IS THE TYPICAL CAUSE OF NOTED CONDITION. 2L72 4F4 FRTA16WE E2GL 20040330000532004033000053NM 2004 3 30 2004UALA00256 120040317A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ROW 21 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29831UA 1291 FOUND WHITE EEL LIGHT IS INOP AT ROW 21 ABC. REPLACED EEL LIGHT. OPS CHECKED NORMAL. 2L72 4F4 FRTA28NM E40NE 20040330000542004033000054EU 2004 3 30 2004UALA00257 120040310A5753 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE TE FLAP BIRD STRIKE A UALAK NONE O OTHER ININSP/MAINT 1 WP29457UA 1146 BIRD STRIKE DAMAGE. LEFT O/B FLAP REPAIRED LOWER SKIN AND SPAR. 2L72 4F4 FRTA28NM E40NE 20040330000552004033000055NM 2004 3 30 2004UALA00258 120040318A5753 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 LEFT WING INBOARD FLAP MAIN TO AFT FLAP HINGE IS CRACKED ON BOTH SIDES. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIRS. 2L72 4F4 FRTA1NM E24NE 20040330000582004033000058NE 2004 3 30 2004UALA00260 220040318A7250 BEARING CAGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 3 FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29530UA 25043 RT ENGINE OIL TEMP IN YELLOW AND OIL FILTER BYPASS EICAS MESSAGE. SHOP TEARDOWN CONFIRMED THAT THE NR 3 BEARING CAGE HAD FAILED. THIS IS THE FIRST FAILURE OF THIS TYPE. 2L72 4F4 FRTA2NM E17NE 20040330000602004033000060NM 2004 3 30 2004UALA00182 120040302A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29397UA 24672 LEFT FUSELAGE STA 1084 EXTERNAL SKIN DAMAGED, ALSO STRINGER DENTED STR 14L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040330000622004033000062NM 2004 3 30 2004UALA00183 120040302A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29397UA 24672 BS 1084 S-14L IS DENTED ON SKIN ATTACHMENT FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND TIE CLIP. 2L72 4F4 FRTA16WE E2GL 20040330000642004033000064NM 2004 3 30 2004UALA00187 120040303A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN SHORTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29302UA 23643 AFT GALLEY EEL LIGHT IS SHORTING OUT THE AFT SECTION OF THE EEL SYSTEM. REPLACED LIGHT STRIP. 2L72 4F4 FRTA16WE E2GL 20040330000652004033000065NM 2004 3 30 2004UALA00189 120040304A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 MAIN CABIN UPPER LOBE STA 867 BETWEEN STR 8L AND 9L FRAME CRACKED AROUND RIVET BUCK TAIL. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME. FABRICATED REPAIR ANGLES AND CLIPS. STOP DRILLED CRACK ENDS. 2L72 4F4 FRTA16WE E2GL 20040330000662004033000066NM 2004 3 30 2004UALA00190 120040303A2130 SEAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29307UA 23668 UNPLANNED DSM STOP DUE TO LOSS OF CABIN PRESSURE. FOUND APU DUCT FLEXIBLE PRESSURE SEAL AT STA 1016 DAMAGED. REPLACED APU DUCT PRESSURE SEAL AND PRESSURIZED AIRCRAFT USING APU IN AUTO, STANDBY AND MANUAL TO ENSURE CORRECT OPERATION. NO DEFECT NOTED. 2L72 4F4 FRTA16WE E2GL 20040330000682004033000068NM 2004 3 30 2004UALA00195 120040304A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29309UA 23670 DENT LOCATED 32 INCHES AFT OF THE FWD CARGO DOOR FROM ABOUT 10 INCHES BELOW THRESHOLD, DENT MEASURING 20 INCHES L X 1.8875 INCH W X 0.065 INCH D. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040330000712004033000071NM 2004 3 30 04FDEA00703 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 LEFT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE, ACTUATOR ROD END NR 8 CORRODED. COMPLIED WITH FEDEX EA 1-5740-75913, WINGS - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20040330000732004033000073NM 2004 3 30 04FDEA00706 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE BARREL NUT HOLE NR 7 MATING SURFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-09 AND DWG ARC0503 SHEET 2 ZONE 22 2L73 4F RTA22WE 20040330000752004033000075NM 2004 3 30 04FDEA00708 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE ACTUATOR ROD END HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75979, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FALP OUTBOARD HINGE BRACKET REAPAIRS. 2L73 4F RTA22WE 20040330000762004033000076NM 2004 3 30 04FDEA00709 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000792004033000079NM 2004 3 30 04FDEA00711 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000802004033000080NM 2004 3 30 04FDEA00712 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000812004033000081NM 2004 3 30 04FDEA00713 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000822004033000082NM 2004 3 30 04FDEA00714 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000832004033000083NM 2004 3 30 04FDEA00715 120040323A5713ARB75111 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING STRINGER 11 CRACKED. LEFT WING STRINGER 11 REPAIRED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040330000852004033000085NM 2004 3 30 04FDEA00717 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000862004033000086NM 2004 3 30 04FDEA00718 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000872004033000087NM 2004 3 30 04FDEA00719 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE, BARREL NUT HOLE NR 2B MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75980, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040330000882004033000088NM 2004 3 30 04FDEA00720 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75980, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040330000892004033000089NM 2004 3 30 04FDEA00615 120040310A5311AFA7819 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK LEFT FRAME INNER EDGE FOUND DENTED AT STA 1581 STRINGER 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL I AND FEDEX EA 1-5330-75320. FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAME BETWEEN STATIONS 5- 113 AND 1721 LEFT AND RIGHT AS DETAILED IN THE WORKSTEPS. 2L73 4F RTA22WE 20040330000902004033000090NM 2004 3 30 04FDEA00616 120040310A5311AFA78181 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1581 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TITLE : FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILED IN THE WORK STEPS. 2L73 4F RTA22WE 20040330000952004033000095NM 2004 3 30 04FDEA00624 120040310A5720ARC050213 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-75296 TITLE: WINGS - O/B TRAILING EDGE FLAPS - I/B HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040330000972004033000097NM 2004 3 30 04FDEA00725 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001012004033000101NM 2004 3 30 04FDEA00729 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001022004033000102NM 2004 3 30 04FDEA00730 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP INBOARD AFT HINGE OUTBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001062004033000106NM 2004 3 30 04FDEA00721 120040323A5753 HINGE DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR ROD END HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75980, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040330001112004033000111NM 2004 3 30 04FDEA00628 120040310A5340ALC81061 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 TAIL TANK - NR 14L BARREL NUT BORE FOUND CORRODED AT BEARING SURFACE. NEW NR 14L BARREL NUT BORE FITTING FABRICATED AS PER EA 1-5510-74321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. DAMAGED NR 14L BARREL NUT BORE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040330001122004033000112NM 2004 3 30 04FDEA00629 120040310A5340ALC81071 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 TAIL TANK - NR 26L BARREL NUT BORE FOUND CORRODED AT BEARING SURFACE. NEW NR 26L BARREL NUT BORE FITTING FABRICATED AS PER EA 1-5510-74321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. DAMAGED 26L BARREL NUT BORE FITTING REMOVED AND REPLACED AS PER SRM 51-33-00 VOL II. 2L73 4F RTA22WE 20040330001132004033000113NM 2004 3 30 04FDEA00630 120040309A5320AEA709469 BRACKET DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT MLG - W/W HYD SERVICING CONTAINER SUPPORT INBOARD ANGLE BRACKET CRACKED. REPAIRED AS PER EA 1-5310-75313, TITLE: FUSELAGE - LEFT WHEEL WELL - HYDRAULIC RESERVOIR SUPPORTING STRUCTURE - BRACKET REPAIR. 2L73 4F RTA22WE 20040330001142004033000114NM 2004 3 30 04FDEA00631 120040309A5712ARC25943 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING I/B FLAP O/B HINGE BRACKET (FLAP SIDE) MOST UPPER AFT FAIRING SUPPORT BRACKET FOUND CRACKED. REPAIRED AS PER EA 1-5750-75304, TITLE: WINGS - T/E FLAPS - LEFT I/B FLAP - O/B HINGE BRACKET FAIRING - CRACK REPAIR. 2L73 4F RTA22WE 20040330001152004033000115NM 2004 3 30 04FDEA00614 120040310A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK FLOOR SUPPORT BEAM AT STA 635/ X = 8.5 FOUND CRACK AT THE EXISTING REPAIR SECTION. MAIN DECK FLOOR SUPPORT BEAM AT STA 635/ X = 8.5 FOUND CRACK AT THE EXISTING REPAIR SECTION REMOVED & REPAIR CARRIED OUT SECTIONAL REPLACED SEAT TRACK FROM STA 525 - STA 545 -X=8.5 AS PER MD11 SRM 53-70-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON EXISTING TRIMMED AREA AT STA 525 & STA 545 CRACK FREE CONDITION. 2L73 4F RTA22WE 20040330001162004033000116EU 2004 3 30 04FDEA00673 120040317A5270 CONNECTOR AIRBUS310 A310 EU DOOR WARNING DAMAGED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25454FE 278 ON CLIMBOUT (APPROX 10,000 FT) ECAM WARNING OF FWD CARGO DOOR NOT CLOSED, RT ECAM DOOR PAGE ALL GREEN, PRESSURIZATION NORMAL. MEL 17MAR04 02:33 RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 27MAR04. MEL 52-71-01: (IDENTIFY) LWR FWD CARGO DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE INOP, LOWER FWD CARGO DOOR VISUALLY CHECKED CLOSED & LOCKED. FOUND LOT OF WATER IN C/P 14WS AND 16WS. FOUND PIN-A CRACKED JONC/P 14WS. REMOVED AND REPLACED 14WS PER MM 52-71-11. FWD CARGO INDICATION CHECKED NORMAL. 2L72 4F RTA35EU 20040331000022004033100002WP 2004 3 31 ABXA040065 120040214A3230 UPLOCK DOUG DC8 DC863F 302198FWP MLG DAMAGED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23811AX 46113 GEAR UPLATCH CHECK FAILED. RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED WITH LANDING GEAR RED UNSAFE LIGHT. IAS DID NOT EXCEED 230 KTS. DEFERRED MAIN LANDING GEAR DOOR UPLATCH SYSTEM IAW DC-8 MEL 32-14, CAT A, CODE 1. PLACARD INSTALLED. MUST BE REPAIRED WITHIN 2 FLIGHT DAYS. REPLACED UPLATCH MECHANISM ON RIGHT MAIN LANDING GEAR IAW DC-8 AMM 32-31-04. PERFORMED ADJUSTMENT/TEST OF RIGHT MAIN LANDING GEAR DOOR UPLATCH MECHANISM IAW DC-8 MM 32-31-04-5, PARA. 3A THROUGH COMPLETION AND PERFORMED LANDING GEAR SWING IAW DC-8 MM 32-11-01. OPS CHECKED GOOD. NO UNSAFE LIGHT. 2L74 4F 4A25 20040331000282004033100028NM 2004 3 31 04FDEA00490 120040220A53116516339 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 970, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55243 2L73 4F RTA3WE 20040331000332004033100033WP 2004 3 31 UPS04841962 120040227A5280 RETAINER DOUG DC8 DC873F 302199FWP RT MLG DOOR INOPERATIVE A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01814UP 46090 RT MLG DOOR OPEN IN FLIGHT. POSSIBLE PROBLEM WITH DOOR RETRACT SYSTEM. FERRY TO SDF FOR REPAIR. RMVD RT MLG IB DOOR. RMVD ACCESS COVER FOR ALT INDICATOR SINKER PLATE. INSTALLED MLG DOOR ALT IND STRIKER PLATE. OK TO REINSTALL ACCESS COV ER. OK TO INSTALL SERVICEABLE RT INBOARD GEAR DR. INSTALLED HINGE PINS. OK TO INSTALL HINGE PIN RETAINERS. INSTALLED HINGE PINS RETAINERS. INS TALLED & ADJUSTED RH MAIND GEAR DOOR IAW DC8 MM 32-12-01. 2L74 4F RT4A25 20040331000452004033100045NM 2004 3 31 04FDEA00343 120040207A5340A5A71141 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CENTER CARGO - LT TUNNEL AREA LONGERON NR 40 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACK. CENTER CARGO STA 5-113 AND STA 1541 LONGERON 40L CRACK SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040331000552004033100055 2004 3 31 SWAA040850 420040321A25656557463 GIRT BAR BOEING737 7372H4 138448CNM L1 DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SPV, FOUND L1 DOOR EVAC SLIDE FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED GIRT BAR FITTINGS PER SRM. 2L72 4F A16WE 20040331000572004033100057NM 2004 3 31 SWAA040852 120040321A3350BR2013 LIGHT BOEING737 737301 1384611NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C1 CHECK, FOUND RT FWD EEPLS TRACK LOOSE. RESECURED EEPLS TRACK PER MM. 2L72 4F RTA16WE 20040331000662004033100066NM 2004 3 31 SWAA040841 120040319A53126546568 BULKHEAD BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 1016, STRINGER 23L, CRACKED. REPAIRED BULKHEAD PER ER. 2L72 4F RTA16WE 20040331000862004033100086 2004 3 31 SWAA040856 420040322A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040331000882004033100088NM 2004 3 31 SWAA040858 120040322A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRAP AT BS 487 TO BS 490, RBL 22, WL 156, CORRODED. REMOVED AND REPLACED STRAP PER SRM. 2L72 4F RTA16WE 20040331001062004033100106NM 2004 3 31 SWAA040884 120040324A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29439WN 29834 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040331001082004033100108NM 2004 3 31 04FDEA00739 120040324A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FWD CARGO BILGE AREA, LONGERON NR 52 AT STA 919 TO 939 CORRODED. FWD CARGO BILGE AREA, LONGERON 52 AT STA 919 TO 939 REPAIRED AS PER SRM 53-10-00 VOL I FIGURE 1 AND FIGURE 2. 2L73 4F RTA22WE 20040331001142004033100114WP 2004 3 31 04FDEA00641 120040312A5753ARC1457508 FITTING DOUG DC10 DC1010 3022110WP TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25680532065 2053 47807 RIGHT WING OUTBOARD FLAP, SUPPORT FITTING HOUSING FOR NR 3 VANE TRACK SUPPORT FITTING HAS CORRODED FASTENERS ON SIDES. 2L73 4F A22WE 20040331001182004033100118NM 2004 3 31 04FDEA00645 120040314A5753 BEARING BOEING727 727200 138407ENM ZONE 500 LOOSE A FDEAO OTHER O OTHER LDLANDING 1 SO25201FE 22924 INBOARD FLAPS INDICATE ASYMMETRIC BETWEEN 2 DEG & 5 DEG ON RETRACTION AFTER LANDING. REMOVED AND REPLACED NR 4 FLAP TRANSMISSION IAW MM 7-51-041-4, LEAK AND OPS CHECKS GOOD IAW MM 27-51-00 0-5. 2L73 4F RTA3WE 20040331001192004033100119NM 2004 3 31 04FDEA00646 120040314A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 MAIN DECK - SEAT TRACK AT STA Y = 6-10 TO 6-90 (X= -8.50), FOUND WITH CORROSION. MAIN DECK - STA Y = 6-10 TO 6-90 (X= -8.50), NEW SEAT TRACK FABRICATED AS PER DWG AGA7082. CORRODED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20040401000492004040100049NM 2004 4 1 UIEA200400011 120040206A5754 STIFFENER BOEING747 747243B 1384830NM KRUEGER FLAP CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, FOUND NR 16 KRUEGER FLAP INBOARD STIFFENER CRACKED. TRIMMED OUT CRACKED SEGMENT OF STRINGER FLANGE TO REMOVE DAMAGE. NDT INSPECT STRINGER TO INSURE CRACK AND DEFECT FREE CONDITION. INSTALLED ALUMINUM REPAIR ANGLE AND ALUMINUM FILLER TO COMPENSATE FOR MATERIAL REMOVED. REFINISHED TRACK TO DESIGN CONDITION. (M) 2L74 4F A20WE 20040401000502004040100050EA 2004 4 1 A6WA200440019 120040202A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 FOUND STRINGER 17L DAMAGED BETWEEN FS 687 AND FS 710. REMOVED DAMAGED SECTION OF STRINGER 17L FROM FS 686 TO FS 707. INSTALLED SECTION OF STRINGER P/N 601R35004-51 WITH SPLICE PIECES FROM 7075-T6 .050 INCH IAW WVAC EO 601R-53-4653A. (M) 2L72 4F RTA21EA 20040401000512004040100051EA 2004 4 1 A6WA200440018 120040204A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A A6WAO OTHER E VIBRATION/BUFFET LDLANDING 1 GL31456ZW 7849 FLAP FAIL MESSAGE, PERFORMED ZERO FLAP LANDING, LANDED 165 KNOTS OW 45, 350 VSI 150 FPM FLAPS FAILED AS SOON AS HANDLE MOVED. REMOVED AND REPLACED LEFT BPSU AND FECU. (M) 2L72 4F RTA21EA 20040401000672004040100067NM 2004 4 1 UIEA200400012 120040209A5753 SPAR BOEING747 747243B 1384830NM TE FLAP CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING DC-CHECK AT SIN, FOUND CORROSION ON THE LOWER SECTION OF THE UPPER T-CHORD OF SPAR NR 1 AND NR 2 OF RIGHT INOARD MID FLAP. FOUND ON ROUTINE CARD 12FM40010. CORROSION LEVEL 1. LOCALLY BLEND OUT CORROSION DAMAGE FROM THE EFFECTED CHORD FLANGE LOWER SURFACE. BOTH NR 1 AND NR 2 SPARS. NDT INSPECT TO ENSURE CRACK AND DEFECT FREE CONDITION. REFINISH CHORDS TO DESIGN STANDARD. REASSEMBLED MID-FLAP WITH OVERSIZE FASTENERS AT LOCATIONS COMMON TO CORROSION REWORK. (M) 2L74 4F A20WE 20040401000872004040100087NM 2004 4 1 SWAA040918 120040328A5320BAC1518 STIFFENER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 727, RT AND LT KEEL BEAM VERTICAL STIFFENERS CRACKED. REMOVED AND REPLACED VERTICAL STIFFENERS PER SRM. 2L72 4F RTA16WE 20040401000892004040100089NM 2004 4 1 04FDEA00632 120040310A5753ARC1984502 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B FWD BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000902004040100090NM 2004 4 1 04FDEA00633 120040310A5753ARC1984502 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B CTR BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000962004040100096NM 2004 4 1 04FDEA00639 120040310A5753ARC199114 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT AFT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401001072004040100107NM 2004 4 1 04FDEA00745 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 5-113 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3380. 2L73 4F RTA22WE 20040401001132004040100113NM 2004 4 1 04FDEA00750 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1721 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2L73 4F RTA22WE 20040401001142004040100114NM 2004 4 1 04FDEA00751 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1741 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2L73 4F RTA22WE 20040401001392004040100139CE 2004 4 1 DBC2004F00001 120040217A323311238002211 ACTUATOR BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE MLG FAILED E DBCAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL131250 7892 FA88 ON DEPARTURE, NLG WOULD NOT RETRACT. MLG RETRACTED AND LOCKED. CREW EXTENDED LANDING GEAR. ALL THREE GEAR SHOWED DOWN AND LOCKED. AIRCRAFT LANDED UNEVENTFULLY. PLACED AIRCRAFT ON JACKS AND CONFIRMED DISCREPANCY. TROUBLESHOT AND DETERMINED NLG ACTUATOR INTERNAL DOWN LOCK FAILED AND WOULD NOT RELEASE. REPLACED NLG ACTUATOR WITH OVERHAULED UNIT. OPS CHECKED GOOD. (DBCA122D) 2L72 4T4 T A24CE E4EA 20040401001502004040100150CE 2004 4 1 WK42004F00000 120040210A3244265K682 TIRE RKWELLNA265 NA26565 7630107CE MLG DAMAGED B WK4RO OTHER O OTHER NRNOT REPORTED 1 SO1765SR 32 46554 CENTER TREAD CHUNKED AFTER 19 LANDINGS ON LEFT LAND TIRE. 2L72 4J A2WE 20040401001522004040100152CE 2004 4 1 CNQ2004F00000 120040122A326065430087 UPLOCK SWITCH CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE NLG PINCHED B CNQRO OTHER O OTHER NRNOT REPORTED 1 CE07647CE226 5600647 THE NOSE LANDING GEAR FAILED TO LOCK IN THE UP POSITION. THE NOSE GEAR WOULD RETRACT AND EXTINGUISH THE HYDRAULIC PRESSURE LIGHT, BUT WOULD THEN FALL BACK OUT OF THE WHEEL WELL. FOUND SHIMMY DAMPENER INTERFERING WITH THE NOSE GEAR UPLOCK SWITCH WIRE BUNDLE. THE WIRES WERE NOT SECURED TIGHT ENOUGH TO THE ANCHORS. REPAIRED THE WIRE BUNDLE AND ENSURED THAT THE WIRES WERE SECURED TO THE ANCHORS. 2L72 4F4 FRTA22CE E00053EN 20040401001552004040100155NM 2004 4 1 OWF2004F00000 120040216A7120DSC2362 BEARING DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE ENGINE MOUNT WORN B OWFRO OTHER O OTHER NRNOT REPORTED 1 CE05813SN DEH1732 032 THE BEARING INCORPORATED AS PART OF THE ENGINE REAR MOUNT STRUT ASSEMBLY HAS BECOME WORN TO THE POINT OF FALLING OUT OF THE STRUT. THE OUTER SURFACE OF THE BEARING IS DEEPLY GROOVED. THIS DISCREPANCY OCCURRED UNDER NORMAL WEAR AND UTILIZATION. 2H72 4T4 TRTA13NM E20NE 20040401001612004040100161CE 2004 4 1 AKG2004F00004 120040220A76031317651F ROD END BEECH 58 58 1152740CE CONT O550 IO550* SO CONTROL CABLE FAILED B AKGRK NONE O OTHER ININSP/MAINT 1 CE0536VF 412 TH2039 WHILE REPLACING THE ENGINE POWER CONTROL CABLE. THE ROD END AT THE THROTTLE BODY WAS FOUND WITH THE BRASS INSERT AND THE STEEL PIVOT BALL FALLING OUT OF THE ROD END HOUSING. THERE IS NOT A LARGE AREA SAFETY WASHER INSTALLED. IT WAS JUST A MATER OF TIME AND THE CONTROL WOULD HAVE FALLEN AWAY FROM THE THROTTLE ARM AND LOSS OF ENGINE CONTROL. 1L72 3O3 O 3A16 E3SO 20040406000072004040600007NM 2004 4 6 04FDEA00794 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2L73 4F RTA22WE 20040406000112004040600011NM 2004 4 6 04FDEA00776 120040330A5753ARC4102502F SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25619FE 48770 RT O/B TRAILING EDGE FLAP STOP BOLT SUPPORT ISLAND IS CRACKED (2 PLACES) REFER FIGURE 1 (SHEET 10 OF 11 ) FIGURE AV OF 1-5750-7-5002 B. REMOVED & REPLACED SUPPORT FITTINGS PER SRM51-31-01 & DAC DWG. ARC4100. COMPLIED BY AMT 357288. 2L73 4F RTA22WE 20040406000122004040600012NM 2004 4 6 04FDEA00777 120040330A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25619FE 48770 LT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE UPPER RADIUS. CRACK VERIFIED BY NDT. ORDERED NEW FITTING. INSTALLED NEW BEARINGS PER W/C E-1-5750-7-5003BL, SEQ 459 STEPS 33-34. INSTALLED NEW FITTING, TORQUED BOLTS PER SMP M/M 20-50-02-2. 2L73 4F RTA22WE 20040406000242004040600024NM 2004 4 6 04FDEA00788 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000302004040600030NM 2004 4 6 04FDEA00690 120040322A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 CORROSION ON LEFT KEELBEAM STA 980 O/B FLANGE. REMOVED CORROSION FROM LEFT KEEL BEAM AT BS 980 O/B FLANGE. MATERIAL LOSS WAS .045 DEEP X .75 X .75 INCH FROM AN ORIGINAL THICKNESS OF .150 AND IS OUT OF LIMITS IAW FED EX SR 27-53-023A. REPAIRED KEEL BEAM IAW FED EX SR 27-53-023A. 2L73 4F RTA3WE 20040406000332004040600033NM 2004 4 6 04FDEA00595 120040305A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LEFT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040406000442004040600044NM 2004 4 6 04FDEA00811 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000462004040600046NM 2004 4 6 04FDEA00814 120040401A5730 SKIN BOEING727 727200 138407ENM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 CORROSION LT WING UPPER SKIN T/E SPAR AREA 8 INCHES FROM WING TO BODY FAIRING UPPER SURFACE OF SKIN. BLENDED CORROSION LT WING UPPER SKIN T/E SPARE 8 INCHES FROM WING TO BODY FAIRING. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA 1.25 X 1 INCH AND REPAIRED IAW FED-EX EA 7-5710-72363. LEAK CHECKED GOOD IAW FED-EX MM 28-11-000-8 STEP 7. 2L73 4F RTA3WE 20040406000472004040600047NM 2004 4 6 04FDEA00815 120040401A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 FUSELAGE SKIN IS GOUGED AT BS 1005 BETWEEN STR 25R AND 26R. GOUGE IN SKIN AT BS 1005, STR 25R & 26R WAS FOUND TO BE OUT OF LIMITS. REPAIRED SKIN PER FED EX EA 7-5330-76233. 2L73 4F RTA3WE 20040406000482004040600048NM 2004 4 6 04FDEA00754 120040325A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25285FE 22622 FOUND CORROSION AT BS 1142-1148 WL 152 BL 0 ON INNER SKIN. *S/D* REMOVED CORROSION ON INNER SKIN AT BS 1139-1164 LBL 1 TO LBL 2 AT WL 152. FOUND TO BE IN LIMITS. DEEPEST BLEND WAS .012 ORIGINAL THICKNESS IS .140. ALODINED, PRIMED AND PAINTED PER 727 SRM 51-10-6, 53-30-1, 53-30-2 FIG 2, 51-10-2 AND 727 M/M 51-21-151. 2L73 4F RTA3WE 20040406000502004040600050NM 2004 4 6 04FDEA00756 120040325A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5740-75923, LEFT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY. 2L73 4F RTA22WE 20040406000572004040600057WP 2004 4 6 04FDEA00765 120040327A5753ARC0503 BRACKET DOUG DC10 DC1010 3022110WP RT TE FLAP CORRODED A FDEAK NONE O OOTHER OTHER ININSP/MAINT 1 SO25389FE 46623 WINGS RIGHT OUTBOARD FLAP - OUTBOARD HINGE REWORK OF SIDE BRACE ATTACH HOLE. COMPLIED WITH EA 8-5740-75127 REWORKED SIDE BRACE ATTACHED HOLES, RIGHT OUTBOARD FLAP, OUTBOARD HINGE IAW EA 8-5740-75127 AT MAE. 2L73 4F A22WE 20040406000612004040600061NM 2004 4 6 04FDEA00805 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 . LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000632004040600063NM 2004 4 6 04FDEA00807 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000662004040600066WP 2004 4 6 04FDEA00677 120040314A143077711622 BOLT DOUG DC10 DC1010 3022110WP TE FLAP UNDERTORQUED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25375FE 46613 MX FOUND BOLT INSTALLED IN INBOARD FLAP VANE INSTALLED, UNDER TORQUED. MX INSTALLED BOLT IN LEFT I/B FLAP VANE ATTACH POINTS. 2L73 4F A22WE 20040406000682004040600068WP 2004 4 6 04FDEA00679 120040318A1430 BOLT DOUG DC10 DC1010 3022110WP ZONE 500 UNDERTORQUED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25550FE 46521 BOLT FAILED TORQUE CHECK ON POS 556JT LT OUTBOARD FLAP VANE. MX TORQUED PER FCD REQUIREMENTS. 2L73 4F A22WE 20040406000702004040600070NM 2004 4 6 04FDEA00809 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000722004040600072WP 2004 4 6 04FDEA00767 120040329A5712ARB109825 RIB DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 EA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098-25. COMPLIED WITH EA 8-5710-73891 WINGS - REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1098.25. 2L73 4F A22WE 20040406000732004040600073WP 2004 4 6 04FDEA00768 120040330A5753ARC255750 DOUBLER DOUG DC10 DC1010 3022110WP RT TE FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 RIGHT INBOARD FLAP VANE OUTBOARD LEADING EDGE RUB STRIP IS GOUGED/ WORN ALL THE WAY THRU LOWER SURFACE. REMOVED AND REPLACED DOUBLER/RUB STRIP IAW SRM 51-31-01 & SRM 57-10-00. 2L73 4F A22WE 20040406000742004040600074WP 2004 4 6 04FDEA00769 120040330A5321WSP07851 FLOOR PANEL DOUG DC10 DC1010 3022110WP MAIN CARGO DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 UPPER MAIN CARGO DECK STA 475 FLOOR PANEL AT NR 5 RCB FITTING EXFOLIATED. REMOVED AND REPLACED PANEL IAW SRM 51-31-01. 2L73 4F A22WE 20040406000772004040600077NM 2004 4 6 04FDEA00770 120040330A5280ANB7093U2 HINGE DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT MAIN LANDING GEAR, DOOR HINGE FOUND CRACKED. RT MAIN LANDING GEAR - CRACKED DOOR HINGE REMOVED AND REPLACED AS PER DWG ANB7093 AND SRM 51-35-01 VOL II 2L73 4F RTA22WE 20040406000792004040600079NM 2004 4 6 04FDEA00772 120040330A5320 INTERCOSTAL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25285FE 22622 CORROSION WHILE WORKING N00402 FOUND INTERCOSTAL CORRODED AT BL 0 BS 1130-1148. *S/D* CORROSION ON INTERCOSTAL FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-20-1, 51-10-2, 51-30-2. 2L73 4F RTA3WE 20040406000802004040600080NM 2004 4 6 04FDEA00773 120040330A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25285FE 22622 CORROSION ON SHEAR TIE, IN AFT CARGO BAY, BS 1148, WL 149, LBL 9. *S/D* COMPLIED WITH FED EX EA 7-5310-55267 ON SHEAR TIE THAT WAS CORRODED AT BS 1148 WL 149 LBL 9. 2L73 4F RTA3WE 20040406000812004040600081NM 2004 4 6 04FDEA00774 120040330A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25285FE 22622 CORROSION WHILE WORKING N00607 FOUND CORROSION AT BS 1142-1148 WL 152 ON STR 30. *S/D* COMPLIED WITH FED EX EA 7-5330-70652 ON CORRODED STRINGER AT BS 1142-1148 WL 152 ON STR 30. 2L73 4F RTA3WE 20040406000822004040600082NM 2004 4 6 04FDEA00775 120040330A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25285FE 22622 CORROSION WHILE WORKING N00607 FOUND CORROSION AT BS 1148 WL 153 ON SHEAR TIE. COMPLIED WITH FED EX EA 7-5310-55267 ON SHEAR TIE THAT WAS CORRODED AT BS 1148 WL 153. 2L73 4F RTA3WE 20040406000832004040600083WP 2004 4 6 04FDEA00742 120040324A5753ARC0502 HINGE DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 COMPLY WITH EA 8-5750-75126 WINGS - REWORK OF LEFT OUTBOARD FLAP, INBOARD FWD HINGE ASSY P/N ARC0502. COMPLIED WITH EA 8-5750-75126. 2L73 4F A22WE 20040406000842004040600084NM 2004 4 6 04FDEA00694 120040323A5730ARB71131 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 CORROSION OBSERVED ON UPPER SKIN SURFACE FROM XORS 197 TO 264 AND BETWEEN STRINGERS S11 TO S21. LEFT WING XORS 197 TO 264 AND BETWEEN STRINGERS S11 TO S21 UPPER SKIN SURFACE CORROSION REMOVED AS PER SRM 57-10-00 VOL I FIG 32. 2L73 4F RTA22WE 20040406000852004040600085NM 2004 4 6 04FDEA00697 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING INBOARD FLAP, OUTBOARD HINGE PIVOT HOLE SPOTFACE FOUND WITH CORROSION. COMPLIED WITH FEDEX WITH EA 1-5750-75978, TRAILING EDGE DEVICES RT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040406000912004040600091NM 2004 4 6 04FDEA00661 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000932004040600093NM 2004 4 6 04FDEA00663 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000942004040600094NM 2004 4 6 04FDEA00664 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000962004040600096NM 2004 4 6 04FDEA00666 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING - OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000982004040600098NM 2004 4 6 04FDEA00668 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2L73 4F RTA22WE 20040406001002004040600100NM 2004 4 6 04FDEA00670 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE, OUTBOARD PIVOT SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406001022004040600102NM 2004 4 6 04FDEA00672 120040316A5270 LIGHT BOEING727 727200 138407ENM WARNING SYS MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25479FE 21461 AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT CLIMBING THROUGH 18,000 AT 310 KTS. LIGHT REMAINED ON 30 MINUTES, EXTINGUISHED ONCE DESCENDED AND SLOWED TO LAND. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 26MAR04, MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2L73 4F RTA3WE 20040406001032004040600103EA 2004 4 6 SWIA200413095 120040328A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA STAB TRIM SWITCHDAMAGED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07407SW 7034 FIRST OFFICER'S STAB TRIM SWITCH WILL NOT TRIM NOSE UP. TAXI BACK TO GATE. REPAIRED WIRE IAW WM 20-00-00. OPS CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20040406001042004040600104SO 2004 4 6 SWIA200413096 120040329A2121AE1209AA0 FAN EMB 120 EMB120ER 3260203SO CABIN FAILED A SWIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07284YV20 20 120284 DURING DESCENT, EXPERIENCED A BURST OF SMOKE COMING FROM THE PACKS AND INTO THE COCKPIT AND CABIN. THE SMOKE SUBSIDED AFTER TURNING OFF THE RECIRC AND GASPER FANS. AFTER DEPLANING THE PASSENGERS, TRIED TURNING ON THE FANS AND THE SMOKE STARTED AGAIN. REPLACED LEFT RECIRC FAN. OPS CHECK GOOD. NO SMOKE NOTED. 2L72 4T RTA31SO 20040406001052004040600105 2004 4 6 SWIA200413097 420040327A3420 COMPUTER EMB 120 EMB120ER 3260203SO NR 2 AHRS OUT OF ADJUST A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07197SW 120186 COPILOT'S COMPUTER FLAG CAME ON AUTOPILOT, WOULD NOT ENGAGE. REORIENTED NR 2 AHRS COMPUTER. AUTO PILOT OPS CHECKS GOOD. 2L72 4T RTA31SO 20040406001072004040600107NM 2004 4 6 CALA0400315 120040403A5312149A761116 WEB BOEING737 737824 13844BZNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND A 3 INCH CRACK IN O/B WEB OF RT SIDE O/B AFT WHEEL WELL RING. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001092004040600109NM 2004 4 6 CALA0400317 120040403A5321 FLOOR PANEL BOEING737 737824 13844BZNM CARGO BAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND FLOOR PANEL 140BF CORRODED AND WITH SEVERAL HOLES IN AFT PIT. A NEW FLOOR PANEL WAS INSTALLED IAW BAC DRAWING 453A2610 AND GMM 10-900-01. 2L72 4F RTA16WE 20040406001112004040600111NM 2004 4 6 CALA0400285 120040326A5512 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND TWO 3 INCH CRACKS IN LEFT HORIZONTAL STABILIZER LOWER SKIN, SPAR STA 131 AND 140. REPAIRED IAW ECRA 5510-01616. 2L72 4F RTA16WE 20040406001132004040600113NM 2004 4 6 CALA0400287 120040326A5315141N511213 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND FLOORBEAM CORRODED AT BS 365, RBL 18. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20040406001142004040600114NM 2004 4 6 CALA0400288 120040326A5315141N5113 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLE, BS 377.7, LBL 58, WBL 208.10. REPAIRED IAW SRM 53-00-51. 2L72 4F RTA2NM 20040406001162004040600116WP 2004 4 6 CALA0400319 120040404A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772822 49482 INSPECTION FOUND FLOOR SUPPORT CORRODED IN MID BAG BIN AT STA 788, LBL 24. REPAIRED FLOOR SUPPORT IAW SRM 51-70-5. 2L72 4F A6WE 20040406001182004040600118NM 2004 4 6 CALA0400321 120040404A5510180A16121 PIN BOEING737 737824 13844BZNM HORIZONTAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718220 28929 INSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, REV C. 2L72 4F RTA16WE 20040406001202004040600120NM 2004 4 6 CALA0400268 120040322A53306545774575 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT FUSELAGE SKIN AT STA 727C. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20040406001252004040600125NM 2004 4 6 CALA0400301 120040331A53206545783502 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 INSPECTION FOUND FORWARD CARGO COMPARTMENT BILGE ANTENNA SUPPORT CHANNEL CORRODED AT STA 500-500A, BL 0. THE SUPPORT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001262004040600126NE 2004 4 6 SWIA200413015 320040311A61148147211 HUB EMB 120 EMB120ER 3260203SO HAMSTD14RF 14RF9 NE PROPELLER CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07224SW 120294 RIGHT PROP HUB ASSEMBLY HAS CORROSION DAMAGE. DISCOVERED DURING E001 INSPECTION. REPLACED RIGHT PROP HUB ASSEMBLY WITH SERVICEABLE UNIT IAW MM 61-10-00. S/N OFF 1823. 2L72 4T RTA31SO 6 CP11NE 20040406001292004040600129NM 2004 4 6 CALA0400309 120040401A5315146N508919 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS 1640, BL 0 TO LBL 24.5. REPAIRED IAW ECRA 5320-01749. 2L72 4F RTA2NM 20040406001302004040600130NM 2004 4 6 CALA0400310 120040401A5315143N550317 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND FLOORBEAM UPPER SURFACE CORRODED AT BS 700, LBL 58.2. REPAIRED IAW ECRA 5320-01746. 2L72 4F RTA2NM 20040406001312004040600131NM 2004 4 6 CALA0400311 120040401A5315141N516152 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND FLOORBEAM CORRODED AT BS 378, RBL 10. REPAIRED IAW ECRA 5320-01747. 2L72 4F RTA2NM 20040406001322004040600132WP 2004 4 6 CALA0400312 120040402A533059102285 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716883 48073 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 1437 BETWEEN LONGERON 4L AND 5L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 27. 2L72 4F A6WE 20040406001342004040600134SO 2004 4 6 SWIA200412978 120040125A5712 RIB EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 CRACKED RIB AT RIVET OUTBOARD OF SMALL FUEL ACCESS PANEL NR 3 OF LEFT WING. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED LEFT NOSE RIB WEB NR 19 IAW EMBRAER REF 1C2004-120/0414 AND SRM 57-20-07 AND CARD RII 28-301. 2L72 4T4 TRTA31SO E20NE 20040406001352004040600135EA 2004 4 6 SWIA200412982 120040224A2751 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAP IND DAMAGED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07903SW 7425 FLAPS EICAS PAGE (FLT CTRL) SHOWS FLAP DISCREP F20 INDICATES = 20 LT, 16 RT, F8 = 8 LT, 4 RT, F45 = 45 LT, 41 RT, F30 = 30 LT, 26 RT. NO ABNORMAL MSGS. A/C FLIES STRAIGHT. NO HANDLING PROBLEMS. FOUND CONNECTOR PIN HOLE 40 ON PLUG 211 WORN AND WILL NOT RETAIN PIN PROPERLY, CAUSING ERRATIC FLAP INDICATION (POSITION). REPLACED PLUG CONNECTOR P211 IAW WM 27-17-10. ACCOMPLISHED OPS, CHECK OF FLAP POSITION TRANSMITTER IAW MM 27-55-01 AFTER REPLACEMENT OF CANNON PLUG P11 ON JB9. 2L72 4F4 FRTA21EA E15NE 20040406001362004040600136EA 2004 4 6 SWIA200413060 120040318A274070609 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07919SW 7657 STAB CHANNEL NR 2 WILL NOT ENGAGE. REPLACED STAB DISCONNECT SWITCH ON F/O'S YOKE. REPLACED HSTCU. OPS CHECKS GOOD IAW MM 27-41-00. S/N OFF: 1384. 2L72 4F RTA21EA 20040406001372004040600137EA 2004 4 6 SWIA200413061 120040318A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA SERVICE LACK OF LUBE A SWIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM07957SW 7829 CABIN SERVICE DOOR DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. LUBRICATED SERVICE DOOR SEAL. OPS CHECKED GOOD. 2L72 4F RTA21EA 20040406001382004040600138EA 2004 4 6 SWIA200413062 120040318A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07442SW 7609 CAPTAIN'S TRIM SWITCH NOSE DOWN INOP. REMOVED AND REPLACED CAPTAIN'S TRIM SWITCH PER CRJ MM 27-41-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20040406001432004040600143SO 2004 4 6 SWIA200413068 120040319A5753 PANEL EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT NACELLE FLAP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07560SW 120334 LEFT NACELLE FLAP HAS A CRACK ON THE OUTBOARD SIDE PANEL. DISCOVERED DURING ROUTINE MAINTENANCE INSPECTION. REMOVED AND REPLACED LEFT NACELLE FLAP WITH A SERVICEABLE UNIT IAW MM 27-50-02. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040406001442004040600144EA 2004 4 6 SWIA200413069 120040318A5210 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 PAX DOOR AFT ANCHOR FITTING IS CRACKED THROUGH 2 FACES. DISCOVERED DURING B004 INSPECTION. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING PER CRJ MM 52-11-17. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040406001452004040600145NM 2004 4 6 CALA0400302 120040331A5320146A750220 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND RIGHT Z-CHANNEL AFT OF CARGO DOOR CUTOUT CORRODED. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001462004040600146NM 2004 4 6 CALA0400303 120040331A5320146A940116 FLOOR SUPPORT BOEING737 737724 13844BYNM CARGO BAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND AFT PIT MIDDLE FLOOR PANEL SUPPORT RAIL CORRODED. THE SUPPORT RAIL WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001472004040600147NM 2004 4 6 CALA0400304 120040331A5210411A2129321 BRACKET BOEING737 737724 13844BYNM L-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND A 1 INCH CRACK IN L-2 DOOR LOWER LINER SUPPORT PAN BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001482004040600148NM 2004 4 6 CALA0400305 120040331A5320143A848535 ANGLE BOEING737 737824 13844BZNM FWD CARGO BAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND BULKHEAD PAD CAMLOCK RECEPTACLE L-ANGLE CORRODED AT STA 500I, RBL 21 TO LBL 21. THE L-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001512004040600151 2004 4 6 SWIA200412988 420040305A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07962SW 7859 STALL FAIL MESSAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-34. OPS CHECKS GOOD. STALL FAIL LIGHT ILLUMINATED LATER IN THE DAY AND STAYED ON FOR DURATION OF THE FLIGHT. CHECKED ASSOCIATED WIRING BEHIND STALL PROTECTION COMPUTER. NO DEFECTS FOUND. RERACKED AND RESET COMPUTER. OPS CHECK GOOD IAW MM 27-53-00. 2L72 4F4 FRTA21EA E15NE 20040406001532004040600153SO 2004 4 6 SWIA200412990 120040304A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY EXIT BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07579SW 120347 EMERGENCY EXIT LIGHTED PLACARD RIGHT FORWARD DOOR IS BROKEN. REMOVED AND REPLACED EXIT SIGN AT FORWARD DOOR. OPS CHECK GOOD. 2L72 4T RTA31SO 20040406001542004040600154EA 2004 4 6 SWIA200412991 120040305A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A SWIAO OTHER LFJNO TEST FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07912SW 7595 STAB CHANNEL 1 INOP. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT AS REQUIRED PER CRJ MM 27-40-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040406001552004040600155EA 2004 4 6 SWIA200412992 120040306A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA TE FLAP DENTED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07947SW2087 2087 7786 ON POST-FLIGHT WALKAROUND, FOUND THE RIGHT SIDE INBOARD FLAP HAS A DENT. REMOVED AND REPLACED THE RIGHT INBOARD FLAP IAW 27-54-01 AND 27-54-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040407000012004040700001EA 2004 4 7 ASOA04179 120040228A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-74-00. (M) 2L72 4F RTA21EA 20040407000022004040700002EA 2004 4 7 ASOA04178 120040305A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL AT FS 484, LBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040407000062004040700006EA 2004 4 7 ASOA04171 120040303A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR DETACHED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11901EV 7616 DURING A GROUND INSPECTION IN DFW, AN EMERGENCY FLOOR LIGHTING STRIP WAS FOUND DETACHED. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000072004040700007EA 2004 4 7 ASOA04160 120040228A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 LEFT AND RIGHT CORNERS WERE FOUND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040407000082004040700008EA 2004 4 7 ASOA04157 120040227A4990 O-RING CNDAIRCL600 CL6002B19 1900309EA APU OIL CAP LEAKING A ASOAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO11925EV 7831 FLT 4768 - DURING DESCENT AND APPROACH INTO ATL FROM GTR, THE CREW SMELLED FUMES AFTER SELECTING THE BLEEDS TO THE APU. SMOKE FILLED THE COCKPIT AND CABIN ACCOMPANIED BY A SMOKE LAVATORY MESSAGE. THE CREW SWITCHED THE BLEEDS BACK TO THE ENGINES AND THE SMOKE DISSIPATED SHORTLY AFTERWARDS FOLLOWED BY THE SMOKE LAVATORY MESSAGE EXTINGUISHING. THE TOWER ROLLED EMERGENCY VEHICLES AS A PRECAUTION WITH THE AIRCRAFT LANDING SAFELY IN ATL. MAINTENANCE REMOVED EXCESS OIL FROM THE AUXILIARY POWER UNIT AND REPLACED THE CAP O-RING. OPS CHECKS GOOD. NO SMOKE WAS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000092004040700009EA 2004 4 7 ASOA04175 120040303A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE CARGO FLOOR THRESHOLD SILL AT THE AFT INTERCOSTAL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO FLOOR THRESHOLD SILL AT THE AFT INTERCOSTAL IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20040407000112004040700011EA 2004 4 7 ASOA04173 120040303A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 AND RBL 9. (M) 2L72 4F RTA21EA 20040407000132004040700013EA 2004 4 7 ASOA04185 120040308A33506100928 LAMP CNDAIRCL600 CL6002C10 1390015EA EXIT SIGN BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11706EV 10054 FLT 9951 - DURING A GROUND INSPECTION IN DFW, THE RIGHT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT SIGN LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000152004040700015EA 2004 4 7 ASOA04172 120040303A5210601R317011 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX LACK OF LUBE A ASOAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11920EV 7810 FLT 4748 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000162004040700016EA 2004 4 7 ASOA04156 120040224A5320601R3117115 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD INTERCOSTAL AT FS 484, BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT OUTBOARD INTERCOSTAL AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040407000172004040700017EA 2004 4 7 ASOA04180 120040306A5210601R3167013 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11701EV 10020 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP AT THE ATTACH LINKS WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040407000222004040700022EA 2004 4 7 ASOA04168 120040301A5330 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUT OUT ON BOTH AFT CORNERS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR CUT OUT ON BOTH AFT CORNERS AT FS 235 IAW ASA EO 600-53-0122. (M) 2L72 4F RTA21EA 20040407000232004040700023EA 2004 4 7 ASOA04167 120040301A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS COVER ON THE LOWER SIDE VENT PANEL WAS FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY ON THE LOWER SIDE VENT PANEL. (M) 2L72 4F RTA21EA 20040407000242004040700024EA 2004 4 7 ASOA04166 120040301A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL 27 AND LBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL 27 AND LBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040407000252004040700025EU 2004 4 7 ASOA04165 120040229A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11632AS 338 DURING AN A-CHECK IN MCN, THE PASSEGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040407000282004040700028EA 2004 4 7 ASOA04170 120040302A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT STRINGERS 13 AND 14 JUST FORWARD OF FS 625.30 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL AT STRINGERS 13/14 JUST FORWARD OF FS 625.30 ON THE LEFT SIDE IAW REO 601R-53-61-105. (M) 2L72 4F RTA21EA 20040407000302004040700030EA 2004 4 7 ASOA04161 120040228A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040407000322004040700032EA 2004 4 7 ASOA04182 120040307A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 FLT 4884 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040414000962004041400096NM 2004 4 14 CALA0400334 120040407A5510180A16121 PIN BOEING737 737724 13844BYNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733714 28785 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696. 2L72 4F RTA16WE 20040414000982004041400098NM 2004 4 14 CALA0400336 120040407A5320654580515 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 1 INCH CRACK IN FORWARD ANGLE THAT ATTACHES TO FRAME AND SKIN AT STA 277 BETWEEN S14L AND S15L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02, 51-40-02, AND BOEING DRAWING 65-45805. 2L72 4F RTA16WE 20040414001062004041400106NM 2004 4 14 04FDEA00877 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414001082004041400108WP 2004 4 14 04FDEA00884 120040408A5714 SKIN DOUG DC10 DC1030 3023501WP CENTER WING CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25310FE 48299 EXFOLIATING CORROSION ON TOP OF CENTER WING AT STA 1331, LBL 97.0 ON AN AREA OF APPROXIMATELY 6 X 8 INCH. REMOVED ALL EVIDENCE OF CORROSION. INSTALLED FILLERS AND DOUBLERS AS PER EA 8-5730-74212-WING UPPER AFT SKIN PANEL, CENTER BOX-CORROSION. 2L73 4F A22WE 20040414001112004041400111 2004 4 14 SWAA040921 420040329A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2/R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED C1 CHECK, FOUND BOTH R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20040414001292004041400129NM 2004 4 14 SWAA040950 120040331A5320BAC1514 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, 6 O'CLOCK POS, CORRODED. REPAIRED STIFFENER PER EA. 2L72 4F RTA16WE 20040414001372004041400137NM 2004 4 14 SWAA040930 120040329A531165C25228 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727E, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040414001732004041400173WP 2004 4 14 UPS04842110 120040401A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RIGHT WING O/B LEADING EDGE RIB IS CRACKED AT XFS 603.75. CRACK TERMINATES AT FASTENER HOLE, NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040414001752004041400175WP 2004 4 14 UPS04842112 120040331A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, LEFT WING LEADING EDGE UPPER RIBS ARE CRACKED AT XFS 747.5 AND XFS 753.75. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040415000312004041500031EA 2004 4 15 QXEA200400187 120040302A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY ACTIVATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09603QX 10011 PDX - FLIGHT 2555 - AIRCRAFT RETURNED TO FIELD AFTER THE LAVATORY SMOKE DETECTOR SOUNDED AND A SLIGHT ODOR WAS NOTICED. MAINTENANCE GROUND RAN THE AIRCRAFT WITH BOTH PACS RUNNING. COULD NOT DUPLICATE WRITE-UP. NOTED BY MAINTENANCE, THAT THE ENGINES HAD BEEN PRESSURE WASHED THE DAY/EVENING PRIOR TO THE EVENT. OPERATIONAL CHECKS WERE ALL GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2L72 4F RTA21EA 20040415000402004041500040NM 2004 4 15 QXEA200400199 120040307A26122600J24 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM FIRE DETECTOR DEFECTIVE A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09416QX 4083 GEG - FLIGHT 2353 - CREW REPORTS THAT WHEN CHECKING THE ADVISORY LIGHTS, THE FIRE DETECTION BELL SOUNDS. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEMS AND AFTER TROUBLESHOOTING FOUND THE NR 1 ENGINE FIRE DETECTOR LOOP -A- CONNECTOR BAD. THE CONNECTOR WAS REPLACED, OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000502004041500050NM 2004 4 15 2004UALA00276 120040324A3240VF6137A25461104 SELECTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE AUTOMATIC BRAKE LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29807UA 798 AIRCRAFT LOST YELLOW SYSTEM HYDRAULIC SYSTEM. RETURN TO FIELD. FOUND HYD FLUID (AFT RT WHEEL WELL) LEAKING FROM AUTOMATIC SELECTOR BRAKE VALVE. REMOVED VALVE FOUND O RING DAMAGED. REPLACED AUTOMATIC SELECTOR BRAKE VALVE. 2L72 4F4 FRTA28NM E40NE 20040415000692004041500069WP 2004 4 15 ASAA0480170 120040307A523059101573 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND AFT CARGO BAY DOOR SKIN IS DENTED AT FS 1199. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 52-05. (M) 2L72 4F RTA6WE 20040415000802004041500080WP 2004 4 15 ASAA0480090 120040222A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRUSHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL CORNER IS CRUSHED AT FS 905-977. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001082004041500108WP 2004 4 15 ASAA0480100 120040224A52105910018135 SKIN DOUG DC9 DC983 3022083WP L1 DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND FORWARD PAX L1 DOOR INNER SKIN IS CRACKED AT LOWER FORWARD CORNER. REMOVED PRIOR REPAIR AND INSTALLED REPLACEMENT DOUBLER PER SRM 52-05. (M) 2L72 4F RTA6WE 20040415001182004041500118EA 2004 4 15 QXEA200400176 120040224A2612473971 FIRE LOOP CNDAIRCL600 CL6002C10 1390015EA RT ENGINE FAULTY A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09603QX5473 10011 LAX - FLIGHT 2543 - CREW REPORTS A FIRE SYSTEM FAULT MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT ENGINE LOWER FIRE LOOP RAIL ASSY. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415001222004041500122EA 2004 4 15 QXEA200400186 120040228A26119847101505 SCREEN CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 PDX - FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20040415001242004041500124EA 2004 4 15 QXEA200400189 120040303A27605120011 PCU CNDAIRCL600 CL6002C10 1390015EA LT WING FAILED A QXEAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM09607QX5674 10024 ELP - FLIGHT 4011 - DURING DESCENT THE CREW ATTEMPTED TO EXTEND THE FLIGHT SPOILERS. FELT A ROCKING MOTION AS IF THE SPOILERS MAY HAVE INITIALLY EXTENDED ASYMMETRICALLY. THE O/B SPOILERONS AND THE O/B FLT SPOILERS CAUTION MESSAGES APPEARED. THE INBOARD SPOILERS WORKED OK AND UPON LANDING, THE GROUND SPOILERS WORKED NORMALLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT OUTBOARD MULTI FUNCTION SPOILER PCU. THE OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415001282004041500128NM 2004 4 15 QXEA200400207 120040313A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG FAULTY A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX5702 1832 4047 SEA - FLIGHT 2445 - AFTER DEPARTURE FROM YVR, THE LANDING GEAR DID NOT RETRACT, HAD 3 GREEN LIGHTS AND 3 RED LIGHTS WITH THE GEAR HANDLE UP. AFTER CONCURRENCE WITH MAINTENANCE CONTROL AND DISPATCH, THE FLIGHT CONTINUED ON TO SEA. MAINTENANCE INSPECTED THE AIRCRAFT AND INTERROGATED THE PSEU AND THE SCU AND FOUND FAULTS: P-SW, PRESS SWITCH FAULT IN THE SCU AND NWCENT FAULT, PROX SENSE OPEN IN THE PSEU. MAINTENANCE REPLACED THE WOW 2 NOSE WHEEL CENTERING WIRING HARNESS. THE RIG AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001502004041500150NM 2004 4 15 SWAA040974 120040402A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 917, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001542004041500154NM 2004 4 15 SWAA040978 120040403A53116546569 BELTFRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND BELT FRAME AT BS 947.5, STRINGER 18L, CRACKED. REMOVED AND REPLACED BELT FRAME PER SRM. 2L72 4F RTA16WE 20040415001602004041500160NM 2004 4 15 SWAA040985 120040403A3350100885 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EEPLS INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2L72 4F RTA16WE 20040415001712004041500171EA 2004 4 15 QXEA200400260 220040410A7320 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NR 1 FADEC DIRTY A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09416QX 4083 PCEFA0110 BOI - FLIGHT 2444 ON FLIGHT FROM SEA TO IDA DIVERTED TO BOI FOR POWERPLANT MESSAGE. CLEANED CONNECTOR TO NR 1 FADEC AND PEC. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040415001862004041500186NM 2004 4 15 QXEA200400227 120040318A5720 ATTACH BRACKET BOMBDRDHC8 DHC8401 1390041NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - RIGHT HAND INBOARD WING TRAILING EDGE SUPPORT U-CHANNEL ATTACH ANGLE CRACKED AT WS YX98-75. REPAIRED IAW RD 8/4-57-177. 2H72 4T RTA13NM 20040415001912004041500191NM 2004 4 15 QXEA200400255 120040331A3234574205A SELECTOR VALVE DHAV DHC8 DHC8202 2809007NM LANDING GEAR FAILED A QXEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 NM09364PH12645 524 YVR - FLIGHT 2124 - THE CREW PERFORMED A MISSED APPROACH WHEN AFTER SELECTING THE GEAR DOWN, THE GEAR FAILED TO RETRACT. THE GEAR WAS LOWERED WITH THE ALTERNATE EXTENSION. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040416000142004041600014 2004 4 16 GAIA04027OP 420040206A2210 AUTOPILOT SYS BOEING727 727251 138408HNM COCKPIT MALFUNCTIONED A GAIAO OTHER J WARNING INDICATION CRCRUISE 1 SW07278US 21157 FLT 278 - SFO-FWA - DUIRNG CRUISE HAD TO KEEP AUTO PILOT TURN KNOB ALL THE WAY TO THE LEFT TO HAVE AIRPLANE FLY STRAIGHT AND LEVEL. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED AUTOPILOT SYSTEM OPS CHECKS ON GROUND. COULD NOT DUPLICATE ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000272004041600027NM 2004 4 16 GAIA04028OP 120040209A2611100089901 SMOKE DETECTOR BOEING727 727224 1384076NM CARGO BAY INOPERATIVE A GAIAK NONE N FALSE WARNING ININSP/MAINT 1 SW0769740 20668 DURING MAINTENANCE, THE LOWER AFT SMOKE DETECTOR WAS FOUND INOPERATIVE GIVING A FALSE ALARM. REMOVED AND REPLACED THE SMOKE DETECTOR OPERATIONAL CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000012004041900001WP 2004 4 19 ASAA0480025 120040120A532199366481 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL JOINING STRIP HAS DISBONDED AT FS 1155-1250. REBONDED JOINING STRIP PER SRM 51-70-1. (M) 2L72 4F RTA6WE 20040419000032004041900003WP 2004 4 19 ASAA0480026 120040120A53219936651557 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AT FS 1003-1041. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000042004041900004WP 2004 4 19 ASAA0480027 120040120A532199366461 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 1079-1155. FILLED PUNCTURE WITH FIBER RESIN AND GLASS OVERLAY PER SRM 51-70-1. (M) 2L72 4F RTA6WE 20040419000082004041900008WP 2004 4 19 ASAA0480063 120040131A2611PU90431R3 SMOKE DETECTOR DOUG DC9 DC983 3022083WP LAVATORY MALFUNCTIONED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01975AS 53451 DURING FILGHT, FOUND LEFT AFT LAVATORY SMOKE DETECTOR CAUSED FALSE CHIME ALARM. REPLACED DETECTOR. CHECKED OK. (M) 2L72 4F RTA6WE 20040419000312004041900031WP 2004 4 19 ASAA0480018 120040120A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 826-864. REPLACED CHANNEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000322004041900032WP 2004 4 19 ASAA0480006 120040120A53475930566509 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND SEAT TRACK GOUGED AT FS 1145-1222. REPLACED DAMAGED SECTION PER SRM 53-05 AND 51-30-2. (M) 2L72 4F RTA6WE 20040419000342004041900034NM 2004 4 19 GAIA04041OP 120040227A2611302842 SMOKE DETECTOR BOEING727 727223 1384074NM CARGO COMP INOPERATIVE A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07854AA 20995 FLT 734 - FWA-DFW - DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVED AND REPLACED BAD NR 1 SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L73 4F A3WE 20040419000362004041900036 2004 4 19 GTIA040150 420040226A2565 CABLE DOUG DC9 DC982 3022082WP R1 DOOR SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 ORD - FLT 1103 - FOUND CABLE ON SLIDE PACK NOT ATTACHED, R1 DOOR SLIDE PACK FELL OFF. REINSTALLED SLIDE PACK FOR R1 DOOR. INSTALLED SLIDE PACK CABLE. (M) 2L72 4F A6WE 20040419000372004041900037WP 2004 4 19 GTIA040147 120040207A3231 SEQUENCE VALVE DOUG DC9 DC983 3022083WP MLG DOOR OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND LEFT GEAR UNSAFE RED LIGHT GOES OUT DURING RETRACTION AFTER DOOR LIGHT GOES OUT. ADJUSTED DOOR SEQUENCE OF MLG CONTROL VALVE. (M) 2L72 4F RTA6WE 20040419000392004041900039EU 2004 4 19 USAASA04011 120040206A2121EVT3454H FAN AIRBUSA319 A319112 3930323EU AVIONICS BAY BURNED OUT A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19768US128701513 1389 PHL - FLT 514 - DCA-PHL - EN ROUTE, THE CREW DETECTED AN ODD ODOR THROUGHOUT THE CABIN, AND FAINTLY IN THE COCKPIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT IN PHL. MAINTENANCE REPLACED THE AVIONICS BLOWER FAN. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040419000402004041900040 2004 4 19 GTIA040153 420040219A2565 LANYARD DOUG DC9 DC981 3022081WP R1 DOOR SLIDE MISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23818NK 48018 FLL - R1 DOOR ESCAPE SLIDE LANYARD INSTALLED INCORRECTLY. ROUTED LANYARD CORRECTLY. (M) 2L72 4F A6WE 20040419000492004041900049EU 2004 4 19 USAABA04005 120040306A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19672UW 0333 PHL - EPSU 15WL FAILED CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA46NM 20040419000532004041900053NM 2004 4 19 GAIA04036OP 120040226A2612 FIRE LOOP BOEING727 727225 1384077NM NR 1 ENGINE OUT OF ADJUST A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07936PG 22441 FLT 213 - ATL-FWA - DURING CRUISE, THE NR 1 ENGINE FIRE DETECTION LIGHT ILLUMINATED ON THE FLIGHT ENGINEERS PANEL. REPOSITIONED NR 1 ENGINE FIRE LOOP OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000632004041900063EU 2004 4 19 ASOA04096 120040207A3397M2275941249 WIRE AEROSPATR72 ATR72 EU EMERGENCY SIGN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE AFT EMERGENCY EXIT SIGN AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES ON THE BACK OF THE AFT EMERGENCY EXIT SIGN ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040419000732004041900073EA 2004 4 19 ASOA04098 120040207A5210601R317011 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11881AS 7496 FLT 4719 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO CLOSE ACCOMPANIED BY A PRESSURE SQUEAL AT ALTITUDE. MAINTENANCE REPLACED THE EPOXY AT THE CENTER SPADE FITTINGS ON THE PASSENGER DOOR AND PRESSURIZED THE AIRCRAFT WITH NO SQUEAL NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040419000762004041900076NM 2004 4 19 GAIA04034OP 120040221A2740 JACKSCREW BOEING727 727223 1384074NM STABILIZER LACK OF LUBE A GAIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW076809 19484 FLT 1736 - BNA-ATL - AIRCRAFT APPEARS OVERLY SENSITIVE IN PITCH WITH CHANGES IN STABILIZER TRIM. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND OPS CHECKED STAB TRIM, TRIM WHEEL COAST GOOD, MANUAL, ELECTRONIC CONTROLS TEST GOOD, SECURITY OF JACK SCREW AND GEAR BOX GOOD, UPPER LOWER STAB PANELS, ELEVATORS CHECK GOOD. JACK SCREW NUT IN NEED OF LUBE. LUBE JACK SCREW NUT. TRIM MOTORS AND BRAKES CHECK GOOD. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000842004041900084EA 2004 4 19 ASOA04086 120040203A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 DURING HANGAR MAINTENANCE IN BTR, THE BOTTOM STOP FOLD DOWN BRACKET ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040419000872004041900087WP 2004 4 19 ASAA0480105 120040224A53219936651519 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE SEAL MISSING FS 1009-1041. RESEALED PER DPS 1.901 AND DWG 9936584. (M) 2L72 4F RTA6WE 20040419000882004041900088WP 2004 4 19 ASAA0480104 120040224A5347593054787 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND SEAT TRACK IS CORRODED AT FS 236-266. REPLACED DAMAGED SECTION PER SRM 51-30-1 AND 51-30-5. (M) 2L72 4F RTA6WE 20040419000972004041900097EA 2004 4 19 ASOA04088 120040204A5320601R3117115 SUPPORT BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD INTERCOSTAL SUPPORT BRACKET AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT OUTBOARD INTERCOSTAL SUPPORT BRACKET AT FS 484, RBL 36 IAW ASA EO 600-53-0137. (M) 2L72 4F RTA21EA 20040419001032004041900103WP 2004 4 19 ASAA0480085 120040221A53219936688503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AT EDGE AT FS 808-826. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001062004041900106WP 2004 4 19 ASAA0480169 120040307A532199365471 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS MISSING AND CORRODED INSERTS AT FS 148-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001152004041900115NM 2004 4 19 DHL2004760001 120040413A57536521634131 SKIN BOEING727 7272B7 138407LNM TE FLAP DELAMINATED A DHLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01760AT 21954 WHILE CLIMBING THROUGH FL 290 A SEVERE VIBRATION COULD BE FELT IN THE AIR FRAME, AND CONTROL YOKE ACCOMPANIED BY A DEEP RUMBLE SOUND. DEPLOYMENT OF SPEED BRAKE WAS NO HELP. FLAP DAMAGE AT LEFT INBOARD AFT FLAP. INSPECTED NR 1 ENG INLET FOR (BMM) FOD DAMAGE AND NONE FOUND (71-00-0). ON POST-FLIGHT FOUND LEFT INBOARD FLAP DE-LAMINATED WITH PIECES MISSING. REPLACED LEFT AFT INBOARD FLAP IAW BMM 27-51-2. OPS NORMAL. INSPECTED AIRCRAFT NO DAMAGE NOTED. 2L73 4F A3WE 20040419001162004041900116NM 2004 4 19 AWXA200400365 120040413A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT DID NOT TEST. REMOVED AND REPLACED BATTERIES IN FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040419001172004041900117NM 2004 4 19 DHL2004750033 120040229A5330 SKIN BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, RT FUSELAGE HAS A DENT BS 1130 BELOW STR 21R. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1061. CUT OUT DAMAGED AREA 2.5 X 1.5 INCH AND FABBED REPAIR DOUBLER FROM 2024 T3 .071 PO 900484 DIM 12 X 7 INCH IAW 727 SRM 53-30-3 FIG 1 & 53-30-2 FIG 2. DOUBLER TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 53-30-3 FIG 1. 2L73 4F A3WE 20040419001202004041900120NM 2004 4 19 DHL2004750036 120040229A5512 SKIN BOEING727 7272M7 138407SNM HORIZONTAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, RIGHT HORIZ STAB, I/B LEADING EDGE AT STAB STA 13.7 HAS A DENTED GOUGE. DENTED GOUGE OUT OF LIMITS IAW B727 SRM 55-10-1 FIG 2. CUT OUT DAMAGE AREA IAW B727 SRM 55-10-3 FIG 2. FABRICATED DOUBLERS FROM 2024 T3 .071 & FILLER FROM 2024 T3 .050 PO 900484 DIM 7.5 X 3.5 INCH & 7.5 INCH X 3 FT & FILLER PO 900641 DIM 3.5 X 2.5 INCH. TREATED & PRIMED ALL PARTS & AREAS IAW B727 SRM 55-10-3 & 51-10-2. INSTALLED PARTS IAW B727 SRM 55-10-3. 2L73 4F A3WE 20040419001272004041900127NM 2004 4 19 DHL2004750010 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND STR 17R FRAME IS DENTED AT BS 600. CUT OUT DAMAGED AREA DIM 1 INCH X .75 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .053 PO 900489 DIM 8 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 1 & 51-40-3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 51-40-3 FIG 1. 2L73 4F A3WE 20040419001312004041900131EA 2004 4 19 COMA0460219 120040328A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01811CA7033 7380 FLIGHT 5791 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040419001322004041900132EA 2004 4 19 COMA0460220 120040328A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01818CA 7408 FLIGHT 5851 LEFT T/R UNLOCKED MESSAGE DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM WAS SATISFACTORY. 2L72 4F RTA21EA 20040419001332004041900133NM 2004 4 19 QXEA200400242 120040323A3350B07B932BZ18006 RELAY DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09374PH 528 SEA - ON FLIGHT 2176 EMERGENCY LIGHTS CIRCUIT BREAKERS C3 AND L1 ARE TRIPPED. REMOVED AND REPLACED EMERGENCY LIGHTS POWER RELAYS K3 AND K4. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040419001352004041900135EA 2004 4 19 COMA0460222 120040328A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01719CA23404 7253 FLIGHT 5921 HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION AND GEAR DISAGREE WARNING. REPLACED SYSTEM 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20040419001432004041900143EA 2004 4 19 COMA0460229 120040328A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01924CA 7026 FLIGHT 5396 AIRCRAFT DID NOT PRESSURIZE. DEFERRED THE OVERBOARD EXHAUST SOV PER MEL 21-24-06 (B). 2L72 4F RTA21EA 20040419001442004041900144NM 2004 4 19 SWAA041050 120040412A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040419001562004041900156NM 2004 4 19 SWAA041036 120040410A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES AT BS 907, AND BS 867, BETWEEN STRINGERS 8L AND 9L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040419001592004041900159NM 2004 4 19 QXEA200400252 120040327A561080260006 WINDSHIELD BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CRACKED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09407QX5247 32 4049 BOI - FLIGHT 2343 - WHILE EN ROUTE TO SUN, THE FIRST OFFICERS WINDSHIELD CRACKED. THE FLIGHT WAS DIVERTED TO BOI. THE REST OF THE FLIGHT AND THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FIRST OFFICERS WINDSHIELD. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040419001622004041900162NM 2004 4 19 DHL2004750014 120040223A5330 SKIN BOEING727 7272M7 138407SNM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, RIGHT FWD OVERWING EMERGENCY EXIT HATCH TOP EXTERIOR SKIN EDGE IS BENT OUT WITH RIVET HEADS PULLING THROUGH SKIN. REMOVED FASTENERS AS REQUIRED FOR ACCES IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA, DIMENSION: 9.75 X 1.375 INCH IAW B727 SRM 52-00-3, FABRICATED FILLER, MAT USED 2024T3 .050 PO 900641 DIMENSION: 9.75 X 1.375 INCH AND DOUBLER 2024T3 .063 PO 900355, DIMENSION 15.75 X 5.625 INCH IAW B727 SRM 52-00-3, ALODINED AND PRIMED IAW B727 SRM 51-10-2, FAB & INSTALLED COUNTERSINK WASHER SRM 51-30-8, INSTALLED REPAIR PORTS IAW SRM 51-30-2 & 52-00-3 FIG 3. 2L73 4F A3WE 20040419001642004041900164NM 2004 4 19 SWAA041042 120040411A3350BR9442 LIGHT BOEING737 7373K2 13844BANM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 EMERGENCY EXIT LIGHT NEXT TO FORWARD F/A'S SEAT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040419001682004041900168NM 2004 4 19 SWAA041047 120040412A5344907822 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER HINGE STRAP FWD UPPER RADIUS CRACKED. REPAIRED L1 DOOR LOWER HINGE STRAP PER EA. 2L72 4F RTA16WE 20040419001712004041900171NE 2004 4 19 SWAA041009 220040408A7200JT8D9AHK ENGINE BOEING737 7372H4 138448CNM PWA JT8 JT8D9 52048NE LEFT FAILED A SWAAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 SW29073SW 22673 687758 ABORTED TAKEOFF, NR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2L72 4F4 F A16WE E2EA 20040419001742004041900174 2004 4 19 SWAA041012 420040408A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040419001772004041900177NM 2004 4 19 SWAA041013 120040408A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 980, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419001782004041900178NM 2004 4 19 QXEA200400257 120040331A5330 ICE SHIELD BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - MAINTENANCE FOUND A DENT ON A PATCH LOCATED ON THE LEFT SIDE BEHIND THE ICE SHIELD. MAINTENANCE REMOVED THE PREVIOUS REPAIR. A NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW RD8/4-53-440. 2H72 4T RTA13NM 20040419001792004041900179EU 2004 4 19 2004UALA00306 120040403A3610 BLEED VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29479UA 1538 RETURNED TO FIELD DUE TO FAILED BLEED VALVE. FAN AIR VALVE CONTROL THERMOSTAT FAILED. REPLACED FAN AIR VALVE CONTROL THERMOSTAT. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040419001822004041900182EU 2004 4 19 MALA040322 120040405A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 4Y/2Y INSPECTION, CORROSION ON LEFT I/B SEAT TRACK AT STA 294-295. REMOVED AND REPLACED LEFT I/B SEAT TRACK AT STA 288-324, IAW MESABA EO S53060. A/C RELEASE DATE 4/9/04. 2L72 4T RTA52EU 20040419001872004041900187NM 2004 4 19 SWAA041018 120040408A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 20L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040419001892004041900189NM 2004 4 19 SWAA041020 120040408A3260655825029 CIRCUIT CARD BOEING737 7373Q8 1384670NM MLG FAULTY A SWAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW29672SW 23406 DECLARED EMERGENCY, UNSAFE NOSE GEAR INDICATION, CYCLED GEAR SEVERAL TIMES, WITH SAME RESULT. OBTAINED SAFE INDICATION AFTER LANDING. REMOVED AND REPLACED LOGIC CARD, ADJUSTED SENSOR AND PERFORMED INTEGRITY CHECK OF WIRING PER MM. 2L72 4F RTA16WE 20040419001902004041900190NM 2004 4 19 SWAA041021 120040408A335007912 COVER BOEING737 7377H4 1384404NM ROW 2 ABC CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 2 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040419001952004041900195NM 2004 4 19 SWAA041026 120040409A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040419002012004041900201NM 2004 4 19 SWAA041004 120040407A5320CLAD2024 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FLOOR WEB AT BS 270 TO BS 277, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040419002022004041900202NM 2004 4 19 SWAA041005 120040407A57536546434369 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM. 2L72 4F RTA16WE 20040419002032004041900203NM 2004 4 19 SWAA041006 120040407A3350MS155721 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040419002042004041900204 2004 4 19 SWAA041007 420040407A25656556685 BRACKET BOEING737 737301 1384611NM R2 DOOR SLIDE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE BRACKET PER MM. 2L72 4F RTA16WE 20040419002172004041900217EA 2004 4 19 COMA0460241 120040401A2751855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LT TE FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01811CA16233 7380 FLIGHT 5778 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20040419002212004041900221NM 2004 4 19 04FDEA00913 120040412A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FORWARD CABIN FLOOR SUPPORT FOUND CORRODED STA 465 LBL 27.5. SEAT TRACK CORROSION REMOVED AND FOUND CRACKED THROUGH EXCEED LIMIT IAW SRM 53-70-00 FIG 3 VOL 1. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL1. 2L73 4F RTA22WE 20040419002222004041900222NM 2004 4 19 04FDEA00914 120040407A26128550 SMOKE DETECTOR DOUG MD11 MD11 3023602NM CARGO BAY MALFUNCTIONED A FDEAF ACTIVATE FIRE EXT. BN SMOKE/FUMES/ODORS/SPARKS FALSE WARNING APAPPROACH 1 SO25587FE 48489 AT 200 FT AGL ON LANDING GOT CABIN SMOKE LEVEL 3 ALERT, WENT OUT SHORTLY. ALERT ON DURING LANDING ROLL THEN WENT OUT. EMERGENCY DECLARED. ON TAXI, CABIN SMOKE LEVEL 3 ALERT, STEADY. APU RUNNING, ENGINE SHUTDOWN. F/O WENT BACK TO OPEN DOOR, SMELLED SMOKE. EMERGENCY EVACUATION DECLARED. APU FIRE HANDLE PULLED. AGENT WAS DISCHARGED. EXITED BY L-1 ENTRY DOOR SLIDE. R&R CARGO COMPT AFT CARGO DET 5 PER MM 26-14-01-4, DUE FAIL ON TEST & SENT MESSAGE ALERT. R&R NR 2 FIREX ENG/APU CONTAINER PER MM 26-21-01-4. R&R MSC PER MD-11 MM 31-42-01-4 & OPS TEST PER MD-11 MM 31-42-01-5 FOR PRECAUTIONARY PURPOSE. R&R NR 1, 2 & 3 WATER SEPARATOR COALESCER PER MD-11 AMM 21-54-05-2. 2L73 4F RTA22WE 20040419002232004041900223EU 2004 4 19 04FDEA00915 120040412A5311 FRAME AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO LEFT SIDE FRAME 39 BETWEEN L3 AND L4, TWO HOLES CORRODED BOTTOM SIDE. REMOVED DISCREPANT CROSS BEAM AND INSTALLED NEW CROSS BEAM IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040420000052004042000005EU 2004 4 20 04FDEA00919 120040412A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN CABIN SMALL SIDE TRACK BETWEEN R4 AND R3 AT FRAME 61 HAS DEEP GOUGE. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-40-21. 2L72 4F RTA35EU 20040420000102004042000010EU 2004 4 20 04FDEA00923 120040412A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN CARGO COMP 1ST SEAT TRACK LT SIDE FROM CENTER AT FRAME 70 JUST AFT HAS MILD CORROSION UPPER SURFACE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-16. FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 53-10-16 AND 51-40-21. 2L72 4F RTA35EU 20040420000132004042000013EA 2004 4 20 COMA0460232 120040323A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01920CA 7022 ONE MISDRILLED HOLE IN 574 FRAME ANGLE FORWARD SWITCH STOP. REPAIRED IN ACCORDANCE WITH REPAIR ENGINEERING ORDER 601R-53-61-964. 2L72 4F RTA21EA 20040420000212004042000021NM 2004 4 20 2004UALA00313 120040406A5313 SPLICE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 4 STRINGER CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 AFT CABIN NR 4L STR SPLICE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040420000302004042000030NM 2004 4 20 2004UALA00323 120040408A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29174UA 24381 FWD PIT STA 760 RBL 56 FLOORBEAM CRACKED AND DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. FABRICATED AND REPLACED SECTION. 2L74 4F4 FRTA20WE E24NE 20040420000352004042000035NM 2004 4 20 04FDEA00898 120040411A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000382004042000038NM 2004 4 20 04FDEA00911 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP, O/B HINGE PIVOT BORE AREA FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76012. WING TRAILING EDGE & TRAILING EDGE DEVICES. LT INBOARD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040420000422004042000042NM 2004 4 20 DHL2004750024 120040315A5740 BRACKET BOEING727 7272M7 138407SNM FLAP ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, NR 1 LEADING EDGE FLAP ACTUATOR BRACKETS TRUNNION SUPPORT CRACKS BOTH SIDES I/B & O/B. REMOVED AND REINSTALLED NR 1 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED BRACKETS FROM NR 1 L/E FLAP ACTUATOR IAW B727 SRM 51-30-2, 2EA LEFT & RIGHT FABRICATED BRACKETS FROM 7075-T6 .063, 6 X 3.5 INCH, 2EA, PO 900489 IAW B727 SRM 51-20-2 FIG 1. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2, INSTALLED REPAIR ANGLES IAW B727 SRM 51-40-3 FIG 1. PERFORMED L/E FLAP OP'S LEAK CHECK FOUND OK IAW B727 MM 27-81-00. 2L73 4F A3WE 20040420000442004042000044EA 2004 4 20 COMA0460235 120040318A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01920CA 7022 LEFT WING FUEL ACCESS HOLE WS 188.040 HAVE INDICATIONS AT POSITION -A- FLAT HORIZONTAL SURFACE CHAMBER. REPAIRED AND ROTO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030. 2L72 4F RTA21EA 20040420000482004042000048EA 2004 4 20 QXEA200400254 120040330A3244 TIRE CNDAIRCL600 CL6002C10 1390015EA NR 4 FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09604QX 10019 AIRCRAFT RETURNED TO FIELD WHEN DURING THE TAKEOFF ROLL THE NUMBER 4 MAIN TIRE CAME APART. THE NUMBER 4 MAIN WHEEL ASSEMBLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NOTE - THE TIRE WAS AT RE-CAP LEVEL 1. RE-CAPPED TIRES NO LONGER BEING USED. 2L72 4F RTA21EA 20040420000502004042000050NM 2004 4 20 QXEA200400209 120040314A5270 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR ILLUMINATED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09413QX 4060 LAX - FLIGHT 2343 - THE AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE FUSELAGE DOORS WARNING ILLUMINATED DURING CLIMBOUT. THE AFT BAGGAGE DOOR WAS CHECKED WITH NO DISCREPANCIES NOTED. MAINTENANCE THEN LUBED THE BAGGAGE DOOR HANDLE. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040420000512004042000051NM 2004 4 20 QXEA200400231 120040322A3297471513 HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG WOW FLUCTUATES A QXEAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM09415QX500 4081 PDX - FLIGHT 2354 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE GEAR FAILED TO RETRACT. THE GREEN AND RED LIGHTS ILLUMINATED, BUT THE CREW RECEIVED NO YELLOW LIGHTS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR PROXIMITY SENSOR FLUCTUATING. THE NOSE LANDING GEAR WOW/NWCENT PROX SENSOR HARNESS WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040420000522004042000052WP 2004 4 20 DHL2004801004 120040318A5250 LATCH DOUG DC8 DC873F 302199FWP COCKPIT DOOR OUT OF ADJUST A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01801DH 46033 COCKPIT DOOR WILL NOT LATCH. ADJUSTED DOOR LATCH AS PER M/M 52-10-00, DOOR LATCHES NORMAL. 2L74 4F RT4A25 20040420000532004042000053WP 2004 4 20 UPS04842113 120040331A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 810. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040420000552004042000055EU 2004 4 20 AWXA200400363 120040412A3222C54001181 SEAL AIRBUS320 A320232 3930326EU NOSE STRUT TORN A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28652AW 953 AFTER TAKEOFF FROM MSP EN ROUTE FOR LAS RECEIVED ECAM MESSAGE NOSE LANDING GEAR (NLG) SHOCK ABSORBER FAULT, TURNED BACK TO MSP AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE MET AIRCRAFT BACK AT GATE AND FOUND THE NLG SHOCK ABSORBER FLAT. SERVICE NLG SHOCK STRUT AND CHECKED FOR LEAKS NONE WERE FOUND. OBSERVED STRUT FOR HALF AN HOUR WITH NO FLUID LOSS OR DEFLATION NOTED. ENGINEERING WROTE A FOLLOW UP AND WHEN THE AIRCRAFT ARRIVED IN PHX IT WAS TOWED TO THE HANGAR FOR A NLG STRUT REPACK. UPON DISASSEMBLY FOUND SCRAPER SEAL ON UPPER CAM TORN. REPACKED NOSE STRUT IAW T/C R4N32305, SERVICED AND CHECKED FOR LEAKS. 2L72 4F RTA28NM 20040420000582004042000058WP 2004 4 20 UPS04842115 120040331A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RT WING LE LOWER RIB IS CRACKED AT XFS 335.25. CUT OUT DAMAGE, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040420000602004042000060WP 2004 4 20 UPS04842117 120040401A572097532958 ANGLE DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RT WING L/E STUBWING HAS VERTICLE ANGLE CRACKED AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753295 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040420000642004042000064NM 2004 4 20 UPS04442042 120040228A5740 FITTING BOEING747 747SR46 1384816NM NR 1 DIA BRACE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, CRACK FOUND AT NR 1 DIA BRACE UNDERWING ATTACHED FITTING'S MOST AFT HOLE OF THE O/B ROW, CRACK LENGTH .125 INCH LONG APPROX AT THE UPPER SURFACE. CRACKED HOLE REPAIRED PER RS R57-04-35118 AND EO B747-5740-20132-A. 2L74 4F RTA20WE 20040420000682004042000068NM 2004 4 20 UPS04442046 120040302A5320 STRAP BOEING747 747SR46 1384816NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, REF EO B747-5310-1093M LEFT BS 1241 FWD HOLE FOUND A BUSHING IN BULKHEAD FORGING. LEFT BS 1241 FWD HOLE FORGING OLD BUSHING REMOVED. HFEC INSPECTED, RESULT NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACB30US12K46 INSTALLED PER RS R53-43-35119 AND EO B747-5310-20150-A, REF SB 747-53-2283 REV 4, UPS-HKG-04-00059H. 2L74 4F RTA20WE 20040420000752004042000075NM 2004 4 20 04FDEA00927 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP VANE, NR 1 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75927. LEFT AND RIGHT OUTBOARD FLAP NR 1 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000782004042000078NM 2004 4 20 DHL2004750029 120040225A5720 STIFFENER BOEING727 7272M7 138407SNM LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 1ST FWD OF SPAR HAS LOWER END CRACKED THRU FASTENER. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 7075-T6 .040 PO 900226 DIM 5 X 2 X 2 INCH AND DOUBLER FROM 7075-T6 .050 PO 900489 DIM 7 X 2 X 2 INCH IAW 727 SRM 57-20-2 FIG 1 & 51-40-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040420000852004042000085NM 2004 4 20 04FDEA00949 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP O/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000872004042000087NM 2004 4 20 04FDEA00951 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP O/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000902004042000090NM 2004 4 20 04FDEA00931 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP VANE, NR 5 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75931. LEFT AND RIGHT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000922004042000092NM 2004 4 20 04FDEA00933 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP VANE, NR 2 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75928. LEFT AND RIGHT OUTBOARD FLAP NR 2 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000932004042000093NM 2004 4 20 04FDEA00934 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP VANE, NR 3 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75929. LEFT AND RIGHT OUTBOARD FLAP NR 3 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000972004042000097NM 2004 4 20 04FDEA00938 120040413A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP I/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08 AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHT 4. 2L73 4F RTA22WE 20040420001002004042000100EU 2004 4 20 04FDEA00952 120040413A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN CABIN FR 40 TO 42 NR 3 RIGHT SEAT TRACK SPOT OF CORROSION ON TWO AREAS AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040420001022004042000102NM 2004 4 20 DHL2004740003 120040331A5711 SPAR BOEING727 7272Q9 138448MNM LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 SMALL AREA OF EXFOLIATION CORROSION AT FORWARD SPAR WING WELL STA 198 TO 210 LEFT-HAND WING. REMOVED CORROSION AT LEFT WING FORWARD LOWER CHORD. TREATED AND PRIMED PER B-727 SRM 51-10-6 & 51-10-2, MATERIAL REMOVED LESS THAN .080 CROSS SECTIONAL AREA REDUCED BY .010 WHICH IS WITHIN LIMITS PER B727 SRM 57-10-1 FIG 2. 2L73 4F RTA3WE 20040420001032004042000103NM 2004 4 20 DHL2004740004 120040331A5720 CHANNEL BOEING727 7272Q9 138448MNM RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 CORROSION ON CHANNEL LOCATED IN RIGHT-HAND LEADING EDGE WING WELL STA 220 THRU STA 224. REMOVED DAMAGE, INSTALLED MINOR EXTRUDED REPAIR IAW B-727 SRM 51-40-4. 2L73 4F RTA3WE 20040420001052004042000105NM 2004 4 20 04FDEA00940 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP I/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420001112004042000111NM 2004 4 20 DHL2004750032 120040229A5330 SKIN BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, RIGHT FUSELAGE HAS 3 DENTS BS 1090 BELOW STR 19R. ACTION AS FOLLOWS; DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-80-1 FIG 1. CUT OUT DAMAGED AREA DIM 2.75 X 2 INCH AND FABBED DOUBLER FROM 2024 T3 .071 PO 900484 DIM 13 X 7.75 INCH IAW 727 SRM 53-30-3 FIG 1. PART INSTALLED IAW 727 SRM 53-30-3 FIG 1. AFTER BEING TREATED & PRIMED IAW 727 SRM 51-10-2. 2L73 4F A3WE 20040420001122004042000112NM 2004 4 20 UPS04442128 120040326A53307075T60071IN DOUBLER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, M/D - BS 270 LEFT VERTICAL WEB FOUND CRACKED AT I/B CHORD AREA AT STR 26. VERTICAL WEB DOUBLER REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040420001172004042000117NM 2004 4 20 UPS04242056 120040304A5330 SKIN BOEING727 72730C 1384009NM FUSELAGE BULGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOSS OF 15-20 PERCENT. DUE TO EXCESS MATERIAL LOSS IND ON SKIN PNL ABOVE & GOUGE IN SAME SKIN PNL BEYOND LIMITS REPLACED SKIN PNL BETWEEN BS 259.5 & BS 360, 19L - 24L IAW SRM 51-30-02. 2L73 4F A3WE 20040420001232004042000123NE 2004 4 20 BAQA094031 220040324A73100319739400 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE RT INJECTION CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 32056 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U3 U H88EU E34NE 20040420001302004042000130WP 2004 4 20 UPS04842067 120040228A533057552713 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:C2 LOWER FUSELAGE SKIN IS BULGED AT STA 275 LONG 34R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, TRIPLER, INTERNAL DOUBLER FILLER AND SKIN FILLER IAW SAA SK 706-550 AND DC8-5330-20148-A. 2L74 4F RT4A25 20040420001312004042000131NM 2004 4 20 UPS04M42064 120040305A5347S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 996 RBL 76 FLOOR PANEL ATTACHMENT HOLE FOUND ELONGATED. DAMAGED SEAT TRACK PORTION REMOVED AS PER SRM 51-31-01 V2 REV 34. HFEC REWORK CARRIED OUT & NEW SEAT TRACK FABRICATED AS PER SRM 53-70-00 FIG 1 VOL 1 REV 34. NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 FIG 1, VOL 1 REV 34, STA 969 - STA 1009 RBL 76. 2L73 4F RTA22WE 20040420001322004042000132NM 2004 4 20 UPS04M42065 120040305A5347S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 996 RBL 28 FLOOR PNL ATTACHMENT ELONGATED. REMOVED DAMAGED PORTION OF SEAT TRACK AS PER SRM 51-31-01, V2, R34. NEW SEAT TRACK REWORKED & SPLICE AS SRM 53-70-00 FIG 1, V1 REV 34. NEW SEAT TRACK & SPLICE INSTALLED 2/EA AS PER SRM 53-70-00 FIG 1 V1, REV 34. 2L73 4F RTA22WE 20040420001332004042000133NM 2004 4 20 UPS04M42066 120040226A5347S49291477075T65 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 INSPECTION TYPE:C CABIN SEAT TRACK STA 899 TO 919, X=8.50 LEFT FOUND CORROSION. CORRODED SEAT TRACK FROM STA 899-919 X=8.5 LEFT FOUND EXCEED LIMIT AS PER SRM 53-70-00, V1, R34. DAMAGED AREA TRIMMED FROM STA 860-939. NEW SEAT TRACK & SPLICE FAB 2/EA AS PER 53-70-00, V1, FIG 1, R.34. PROTECTED AS SRM 51-21-01 V1, R34. PAINTING AS PER SRM 51-21-02, V2, R34. NEW SEAT TRACK INSTALLED AS PER 51-21-02, V2, R34 AT REWORKED AREA. 2L73 4F RTA22WE 20040505001462004050500146EA 2004 5 5 SWIA200413156 120040306A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, FORWARD EQUIPMENT COMP FS 193.0 LT SIDE FLOOR WEB CRACKED BY FRAME. REPAIRED IAW CRJ REO 601R-53-11-081 REV. NC, RII 53-401. 2L72 4F RTA21EA 20040505001492004050500149EA 2004 5 5 SWIA200413207 120040416A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT; FUSELAGE FRAME AT FS 589.00 HAS 1 CRACKED FLANGE THAT ATTACHES TO STR 18L LOWER SIDE. REPAIRED IAW CRJ REO 601R-53-61-999 REV. A. REPAIRED IAW CRJ REO 601R-53-61-999 REV. A. 2L72 4F RTA21EA 20040505001692004050500169EA 2004 5 5 SWIA200413212 120040416A5312 STIFFENER CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS621 BULKHEAD RIGHT VERTICAL STIFFENER RBL 9.0 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401. 2L72 4F RTA21EA 20040505001832004050500183NM 2004 5 5 ASAA0410082 120040216A5310 STRUCTURE BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND CORROSION ON NOSE WHEEL WELL TUNNEL AREA AT FS 277. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040505001952004050500195NM 2004 5 5 ASAA0410075 120040215A53116546595194 FRAME BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND AFT CARGO COMPARTMENT AT STATION 727A HAS CORROSION ON AFT SIDE OF FRAME. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040505001982004050500198NM 2004 5 5 ASAA0410072 120040215A533065458001 SKIN PANEL BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 263-271, STRINGER 24L DENTED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002012004050500201NM 2004 5 5 SWAA041246 120040503A5751654645624 AILERON BOEING737 7372H4 138448CNM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING RON CHECK, FOUND RT WING AILERON DELAMINATED. REMOVED AND REPLACED RT AILERON PER MM. 2L72 4F A16WE 20040505002042004050500204NM 2004 5 5 SWAA041248 120040503A575465C266032 WEDGE BOEING737 737317 138447PNM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20040505002142004050500214NM 2004 5 5 ASAA0410066 120040213A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC- DURING INSPECTION, FOUND THE EMERGENCY FLOOR TRACK LIGHTS ON SEAT PALLET 8-6 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040505002172004050500217NM 2004 5 5 ASAA0410063 120040210A53106547960570 SHEAR TIE BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SHEAR TIE AT BS 907, STRINGER 27L-27R CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002862004050500286NM 2004 5 5 SWAA041202 120040428A53106546529 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040505002882004050500288 2004 5 5 SWAA041204 420040428A256565C19901 CABLE BOEING737 7375H4 138449DNM EVAC SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040505002972004050500297 2004 5 5 SWAA041188 420040427A2565D31591475 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040505002992004050500299NM 2004 5 5 SWAA041206 120040429A2530112251 COFFEEMAKER BOEING737 7377H4 1384404NM AFT GALLEY FAULTY A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29769SW 30588 STRONG ELECTRICAL SMELL FROM AFT COFFEEMAKER IN FLIGHT. WHEN CB PULLED SMELL WENT AWAY. REMOVED AND REPLACED BOTH AFT COFFEEMAKERS PER MM. 2L72 4F RTA16WE 20040505003012004050500301 2004 5 5 SWAA041208 420040429A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040505003042004050500304NM 2004 5 5 SWAA041211 120040429A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 21R, BS 941, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040506000022004050600002EU 2004 5 6 BAQA094293 120040428A6720 BEARING BOLKMS117 BK117B1 5626012EU BELLCRANK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 509 7235 BEARING WORN AND TEFLON MISSING IN BEARING. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1G72 3U H13EU 20040506000042004050600004EU 2004 5 6 BAQA094295 120040419A642010513241 BEARING BOLKMS117 BK117B1 5626012EU FORK LINK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME286 7235 BEARINGS WORN IN FORK LINK. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1G72 3U H13EU 20040506000052004050600005EU 2004 5 6 BAQA094296 120040419A6510 BEARING BOLKMS117 BK117B1 5626012EU DRIVE LINK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME286 3626 7235 TAIL ROTOR DRIVE LINK BEARINGS WORN AND HAVE PLAY. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1G72 3U H13EU 20040506000112004050600011 2004 5 6 ASMF200404019 420040426A3422 SYMBOL GENERATOR DOUG DC9 DC987 3022087WP MALFUNCTIONED W ASMFO OTHER HGJELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SW23204AM 49404 CAPTAIN REPORTED THAT DURING CRUISE BOTH PFD AND FIRST OFFICER ND WITHOUT INFORMATION AND ON BOTH SIDES FMA´S, ILS, HEADING, AND MONITOR LIGHTS FLASHED ALL THE TIME. CIRCUIT BREAKER B10-377 WAS RESET IAW MM 20-50-06 AND FAIL CONTINUE. THE SYMBOL GENERATORS WERE INTERCHANGED AND FAIL WAS DETECTED ON LT SIDE. THE SYMBOL GENERATORS WERE RETURNED TO THE ORIGINAL POSITION AND RT SYMBOL GENERATOR WAS COOLED WITH THE AIR CONDITIONING SYSTEM. DURING OVERNIGHT SERVICE EFIS SYSTEM WAS TESTED IAW MM 34-22-00, 34-22-06, 34-23-06 AND 34-22-10, ALL CORRECT. 2L72 4F RTA6WE 20040506000652004050600065SW 2004 5 6 ALG2004F00019 120040328A5302206031004117S SKIN BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TAIL BOOM CRACKED B ALGAK NONE O OTHER ININSP/MAINT 1 SW03198H 14236 3647 CAE832754 WHILE PERFORMING AN INSPECTION, CRACK IN LOWER SKIN AT T/B STA 153. STARTING AT EDGE OF SKIN, MEASURING 2.5 INCHES LONG, RUNNING THE CIRCUMFERENCE DIRECTION , POSSIBLY CAUSED BY ROUGH EDGE IN SKIN OR MAYBE A VIBRATION. 1G71 3U3 U H2SW E4CE 20040506000842004050600084NM 2004 5 6 UPS04242260 120040406A5320 ANGLE BOEING727 72731C 1384011NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C LT 950 FITTING LWR SPLICE ANGLE HAS SUSPECT CORROSION UNDER THE ANGLE. ANGLE WAS ALSO FOUND CORRODED AFTER REMOVAL. ANGLE REPLACED AND BS 950 REPAIR CARRIED OUT IAW SRM 51-20-1 AND SMRO EO 2004-027-002. UPS ENGINEERING FILE NR B727-5310-20302-A 2L73 4F A3WE 20040506000902004050600090EU 2004 5 6 MALA040345 120040416A2930MS2740017 RELAY SAAB SF340 SF340A 7850100EU HYD SYSTEM FAILED A MALAO OTHER J WARNING INDICATION DEDESCENT 1 GL15106XJ 340A106 AFTER SELECTING GEAR DOWN HYDRAULIC CAUTION LIGHT CAME ON, MAIN ACCUMULATOR LOW, EMERGENCY ACCUMULATOR NORMAL, HYDRAULIC QUANTITY NORMAL NOSE GEAR DOWN, MAIN GEAR NOT DOWN, QRH CHECK LIST ALL NORMAL. SELECTED OVERRIDE MAIN GEAR DOWN AND MAIN ACCUMULATOR NORMAL. MAINTENANCE REMOVED AND REPLACED RELAY 7ML, P/N MS27400-17, HYDRAULIC PUMP FUNCTIONAL TEST GOOD IAW AMM 29-10-00, GEAR EXTENSION AND RETRACTION FUNCTIONAL TEST GOOD IAW 32-30-00. 2L72 4T RTA52EU 20040506000942004050600094 2004 5 6 MALA040332 420040403A3440 MOUNT SAAB SF340 340B 7860101EU ANTENNA CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION, CORROSION ON LOWER TCAS ANTENNA MOUNT. MAINTENANCE REPAIRED LOWER TCAS ANTENNA MOUNT IAW MESABA EO S53216. AIRCRAFT RELEASE DATE 4/16/2004. 2L72 4T RTA52EU 20040506001012004050600101NM 2004 5 6 CALA0400448 120040502A5320BAC1496444 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND THE LEFT Z-CHANNEL IN FORWARD CARGO AREA CORRODED AT ZONE 110. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040506001142004050600114NM 2004 5 6 CALA0400461 120040504A573065C26714 SKIN BOEING737 7373T0 1384582NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND A .5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-40-01, FIGURE 201, PROCEDURE 2. 2L72 4F RTA16WE 20040506001182004050600118NM 2004 5 6 CALA0400465 120040505A3350110049 CHARGER BOEING737 7373T0 1384582NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714335 23573 THE EMERGENCY LIGHTS IN FIRST CLASS CABIN AND AT FORWARD SERVICE ENTRY DOOR WERE FOUND INOPERATIVE. THE BATTERY CHARGER AT STA 338 WAS REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20040506001272004050600127WP 2004 5 6 ASAA0480160 120040312A53219936545501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND INSERTS PULLING OFF, CORRODED AND PANEL CRACKED AT LOWER SURFACE, FORWARD CABIN STATION 148-200. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040506001292004050600129WP 2004 5 6 ASAA0480153 120040313A53219936537503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND FORWARD CABIN FLOOR PANEL STATION 148 TO STATION 168 HAS DELAMINATION AROUND FASTENER HOLES. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040506001442004050600144NM 2004 5 6 ASAA0410093 120040229A5310654655134 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND HOLES OVERSIZED AT SHEAR TIE STATION 807. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040506001462004050600146WP 2004 5 6 ASAA0480188 120040314A5320593655203 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR CUTOUT INTERNAL WEB IS CORRODED AROUND ATTACH HARDWARE AT FS 1155-1211. REPLACED DAMAGED AREA OF WEB AND INSTALLED DOUBLER PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040506001492004050600149WP 2004 5 6 ASAA0480156 120040313A532199365521 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 200-256 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040506001512004050600151NM 2004 5 6 ASAA0410068 120040213A33508821004 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY FLOOR TRACK LIGHTS ON PALLET 10-3 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHT TESTED NORMAL. (M) 2L72 4F A16WE 20040506001542004050600154NM 2004 5 6 ASAA0410089 120040220A33508821004 BATTERY PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 8-2 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040507000142004050700014NE 2004 5 7 HEEA094282 120040421A77000177987070 TORQUE BOX SKRSKYS76 S76C 8143008NE NR 2 ENGINE FAULTY E HEEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03274X 760440 AFTER TAKEOFF, THE DECU DISPLAYED A MINOR FAULT ON THE NR 2 ENGINE. RETURNED. MAINTENANCE REPLACED THE NR 2 ENGINE TORQUE CONFIRMATION BOX. 1G72 3U NCH1NE 20040507000432004050700043NM 2004 5 7 S04852010 120040215A5210 WARNING LIGHT BOEING737 737800* NM CFMINTCFM56 CFM567B26US NE L3 DOOR ILLUMINATED W SAJFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP03 29106 738 B18611 RTO AT TPE DUE TO L3 CABIN DR WARNING LIGHT ON. IAW AMM 05-51-07 FIGURE 201 BRAKE COOLING SCHEDULE SHOW NO SPECIAL PROCEDURES REQUIRED. PSEU FAULT HISTORY NO FAULT LEG WAS FOUND. PFM L3 DOOR WARNING SWITCH FUNCTION CHECK NORMAL. IAW FIM D633A103-CHI THE SUBJECT ITEM SHOULD BE AN INTERMITTENT FAULT. ITEM CLOSE. 2L72 4F4 FRTA16WE E00055EN 20040507000602004050700060SW 2004 5 7 ALG2004F00013 120040310A6220 SPRING BELL 407 407 1182206SW ALLSN 250C 250C47B GL FRAHM DAMPER MISALIGNED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03577AL 53247 SLIGHT VIBRATION ON LANDING, CHECKED ROTOR SYSTEM ON POST FLIGHT AND FOUND FRAHM DAMPER SPRING MISALIGNED. MAINTENANCE FOUND BROKEN SPRING IN FRAHM DAMPER. REMOVED AND REPLACED FRAHM DAMPER. 1G71 3U3 UO H2SW E1GL 20040507000612004050700061NE 2004 5 7 MDR04043 220040122A7230670802 COMPRESSOR WHEEL SKRSKYS64 CH54B 8142610NE PWA JFTD12JFTD12A4A 52047NE 2ND STG COMP DISCRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09223AC4902 64086 A CRACK WAS FOUND IN THE BLADE RETENTION HOLE OF THE 2ND STAGE COMPRESSOR DISK. COMPRESSOR SN 677782, WAS REMOVED FOR HSI/OVERHAUL. DURING THE INSPECTION PROCESS, NDT DETECTED A CRACK IN THE BLADE RETENTION HOLE, CENTER LAND USING EDDY CURRENT. THE CRACK WAS VERIFIED BY FPI. LOOKING AT THE REAR FACE OF THE DISK WITH THE WORD (REAR) AT THE 12 OCLOCK POSITION, THE CRACK BEGINS AT APPROXIMATELY THE 9 OCLOCK POSITION EXTENDING AT A 45 DEGREE ANGLE COUNTER CLOCKWISE. THE LENGTH OF THE CRACK EXTENDS FROM THE HOLE TO THE OUTER EDGE OF LAND APPROXIMATELY .300 INCHES LONG. PROBABLE CAUSE UNKNOWN. 2G72 4U4 U H6EA E15EA 20040507000622004050700062NM 2004 5 7 S04425003 120040119A253072070501 OVEN BOEING747 747400 NM PWA 4056 PW4056 NE GALLEY FAILED W SAJFO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP03 28711 744 B18203, SMOKE FOUND ON STEAM OVEN (508) OF GALLEY UINT 7 WHEN OPERATION OF OVEN. C/A: STEAM OVEN REPLACED AND FUCTIONAL TEST FOUND NORMAL. REMOVED STEAM OVEN WAS FOUND WITH THE SENSOR BOARD BURN OUT CAUSED BY MOISTURE BASED ON THE SHOP REPORT AND NOTIFIED FOR FURTHER IMPROVEMENT. 2L74 4F4 FRTA20WE E24NE 20040507000632004050700063SW 2004 5 7 ALG2004F00018 120040403A2810 FUEL CAP BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUEL CELL MISSING E ALGAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW03116AL 2389 CAE836031 AFTER APPROX 5 MINUTES OF FLIGHT AFTER TAKE OFF FROM EC-160, PILOT NOTICED A STRONG ODOR OF FUEL AND GAUGE WAS FUNCTIONING PROPERLY. RETURNED TO EC-106, SHUT DOWNED AND INSPECTION OF AIRCRAFT SHOWED MISING FUEL CAP. FUEL CAP HAD BEEN REPLACED AFTER REFUELING AND WAS PRESENT ON PREFLIGHT WALK AROUND. MAINTENANCE INSTALLED NEW FUEL CAP AND AIRCRAFT WAS INSPECTED FOR DAMAGE, NONE FOUND, RETURNED AIRCRAFT TO SERVICE. 1G71 3U3 U H2SW E4CE 20040507000652004050700065SW 2004 5 7 ALGA094362 120040504A6230412040104103 NUT BELL 412 412EP 1182205SW MAST CORRODED D ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XATTF2489 A723 36273 FOUND MAST NUT CORRODED ON THREADED AREA AND ON LOWER SURFACE OF NUT. MAST PIPE PN:412-040-101-129 ALSO CORRODED. 1G72 4U H4SW 20040507000702004050700070SO 2004 5 7 SWIA200413262 120040414A5720 CLIP EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07580SW 120348 MIDDLE LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. DISCOVERED DURING C-CHECK INSPECTION. REPLACED MIDDLE LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07. 2L72 4T RTA31SO 20040507000712004050700071EA 2004 5 7 SWIA200413213 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM CHAFED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 CHAFE IN NR 1 HYDRAULIC MANIFOLD ATTACH INTERCOSTAL AT FS 712.00 BEYOND LIMITS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040507000732004050700073EA 2004 5 7 SWIA200413215 120040418A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 RIGHT SIDE 625 OBLIQUE ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED & REPLACED OBLIQUE ANGLE P/N 601-35012-52 IAW SRM 51-42-06. 2L72 4F RTA21EA 20040507000752004050700075EA 2004 5 7 SWIA200413245 120040423A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 CARGO PIT STEP PLATE ASSY SUPPORT IS CRACKED OUT ALONG INBOARD EDGE. DISCOVERED DURING C-CHECK INSPECTION. SUPPORT REPLACED IAW CRJ SRM 51-41-02. 2L72 4F RTA21EA 20040507000772004050700077EA 2004 5 7 SWIA200413247 120040416A57206001020427 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 LEFT WING SECTION 48.30 PART NUMBER IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20040507000792004050700079EA 2004 5 7 SWIA200413249 120040416A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 LEFT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20040507000812004050700081EA 2004 5 7 SWIA200413217 120040418A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 LEFT ENGINE SUPPORT BEAM UPPER ATTACHMENT ANGLE P/N 601-35006-61 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ATTACHMENT ANGLE LEFT TOP ENGINE SUPPORT BEAM AS REQUIRED IAW CRJ SRM 51-42-21. 2L72 4F RTA21EA 20040507000832004050700083EA 2004 5 7 SWIA200413219 120040418A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FS 484 RBL 27 OUTBOARD INTERCOSTAL ANGLE CRACKED .25 INCH IN THE ANGLE RADIUS AT WL 73. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED ANGLE WITH NEW ANGLE PN 601R31171-9 AT FS 484 RBL 27 INBD SIDE IAW CRJ 200 SRM 51-42-21, 51-42-06, 51-40-11, AND 51-21-11 AND EO #601R-53-4865 AND SKYWEST EA RJ240-53. 2L72 4F RTA21EA 20040507000852004050700085EA 2004 5 7 SWIA200413221 120040418A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FS 484 WL 73 LBL 27 OUTBOARD INTERCOSTAL ATTACHMENT ANGLE IS CRACKED .25 INCH. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED ANGLE PN 601R31171-17 AT FS 484 LBL 27 OUTBOARD SIDE IAW CRJ 200 SRM 51-42-21, 51-42-06, 51-40-11, 51-21-11 AND EO # 601R-53-4865 AND SKYWEST EA NO. RJ240-53. 2L72 4F RTA21EA 20040507000872004050700087EA 2004 5 7 SWIA200413163 120040306A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FUSELAGE SEAT TRACKS HAVE CORROSION FS 399 TO 599 + 96 RBL 9. DISCOVERED DURING C-CHECK INSPECTION. SEAT RAIL FS 409+126 TO FS 559+04 REPLACED. SEAT RAIL FS 559+04 TO FS 559+85 REPLACED. 2L72 4F RTA21EA 20040507000892004050700089EA 2004 5 7 SWIA200413165 120040306A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FS 364 STR 8L IS CRACKED FROM FASTENER HOLE ON UPPER FRAME FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME FLANGE IAW REO 601R-53-21-492 AND RII53-401. 2L72 4F RTA21EA 20040507000912004050700091EA 2004 5 7 SWIA200413167 120040306A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FOUND WIRES BURNED AND CHAFED UNDER RIGHT PASSENGER COMPARTMENT CEILING PANEL 274BLC-274CRC. DISCOVERED DURING C-CHECK INSPECTION. WIRES SPLICED IAW CRJ AWM CHAPTER 20-16-00 AND CHAPTER 33-21-00. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040507000922004050700092EA 2004 5 7 SWIA200413168 120040413A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 FS 484 INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. A AND RII 53-401. 2L72 4F RTA21EA 20040507000942004050700094EA 2004 5 7 SWIA200413170 120040413A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A. 2L72 4F RTA21EA 20040507000962004050700096EA 2004 5 7 SWIA200413172 120040413A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 LEFT ELECTRICAL BAY FLOOR AT FS 193, LBL 30 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-081 NC. 2L72 4F4 FRTA21EA E15NE 20040507000982004050700098EA 2004 5 7 SWIA200413160 120040306A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 INTERIOR FUSELAGE TRANSVERSE BEAM UPPER FLANGE CRACKED IN 2 PLACES, FS 280.00 LBL 9.0 AND RBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-136 REV NC AND 601R-53-11-13 REV NC. 2L72 4F RTA21EA 20040507000992004050700099EA 2004 5 7 SWIA200413161 120040306A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FUSELAGE IS CRACKED AT RIGHT AILERON AFT BELLCRANK MOUNTING POINTS AT FS 559.00559.00, RBL 9.00 AND RBL 18.00. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-197 REV NC AND RII53-401. 2L72 4F RTA21EA 20040507001002004050700100EA 2004 5 7 SWIA200413162 120040306A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FUSELAGE SEAT TRACKS HAVE CORROSION FS 399 TO 599 + 96 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. SEAT RAIL FS 409+126 TO 559+04 REPLACED. SEAT RAIL FS 559+04 TO 559+85 REPLACED. 2L72 4F4 FRTA21EA E15NE 20040507001012004050700101EA 2004 5 7 SWIA200413174 120040413A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 NOSE HYDRAULIC COMPARTMENT AT FS 202.75 STR 21 CLIP IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CLIP (CLEAT) IAW CRJ SRM 53-11-19 FIG 1, SHEET 1. 2L72 4F4 FRTA21EA E15NE 20040507001022004050700102EA 2004 5 7 SWIA200413175 120040413A5320 RECEPTACLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 SEVERAL CRACKS FOUND RADIATING FROM 115 VAC RECEPTACLE CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F4 FRTA21EA E15NE 20040507001032004050700103NM 2004 5 7 CALA0400439 120040501A3350D71702030 POWER SUPPLY BOEING767 767424ER 1385270NM CABIN FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2767058 29453 THE M732 EMERGENCY LIGHT POWER SUPPLY FAILED FUNCTIONAL TEST PER WORK CARD 64-3350-1-7100. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07. 2L72 4F RTA1NM 20040507001042004050700104EA 2004 5 7 SWIA200413176 120040413A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 MAIN FUSELAGE; LOWER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-171 REV NC AND RII 53-401. 2L72 4F4 FRTA21EA E15NE 20040507001052004050700105NM 2004 5 7 CALA0400440 120040501A5420311A17301 BRACE BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE AFT LOWER PYLON AREA DIAGONAL BRACE. THE DIAGONAL BRACE WAS REMOVED AND REPLACED IAW MM 54-10-01. 2L72 4F RTA16WE 20040507001062004050700106EA 2004 5 7 SWIA200413177 120040413A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 MAIN FUSELAGE; UPPER TRANSVERSE BEAM CRACKED AT FS 280.00 LBL 11.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-138 REV NC AND RII53-401. 2L72 4F4 FRTA21EA E15NE 20040507001072004050700107NM 2004 5 7 CALA0400441 120040501A5320143A751025 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND A 2 INCH CRACK IN RIGHT INTERCOSTAL AT STA 500G-500H. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-20-01, 51-40-02, AND DRAWING 143A7510. 2L72 4F RTA16WE 20040507001092004050700109EA 2004 5 7 SWIA200413179 120040413A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 MAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 LBL 27.0 AND LBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A REF RII 53-401. 2L72 4F4 FRTA21EA E15NE 20040507001112004050700111NM 2004 5 7 CALA0400443 120040501A5320143A948534 SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND PANEL 121EW LOWER SUPPORT FRAME CORRODED AT AFT BULKHEAD OF FORWARD CARGO AREA. A NEW SUPPORT FRAME WAS INSTALLED IAW SRM 51-40-02 AND 51-10-02. 2L72 4F RTA16WE 20040507001122004050700112NM 2004 5 7 CALA0400431 120040427A534265538343 FITTING BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 VERTICAL STABILIZER AFT ATTACH LUG, FWD FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03. 2L72 4F RTA16WE 20040507001152004050700115NM 2004 5 7 CALA0400434 120040427A322165C25636517 BEARING BOEING737 7373T0 1384582NM NLG TRUNNION DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 NOSE GEAR, RIGHT TRUNNION BEARING IN BULKHEAD FITTING PITTED. REPAIRED PER ECRA 5343-01013. 2L72 4F RTA16WE 20040507001162004050700116NM 2004 5 7 CALA0400435 120040428A322165C25636518 BEARING BOEING737 7373T0 1384582NM NLG TRUNNION DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 NOSE GEAR, LEFT TRUNNION BEARING IN BULKHEAD PITTED. REPAIRED PER ECRA 53543-01013. 2L72 4F RTA16WE 20040507001172004050700117NM 2004 5 7 CALA0400436 120040428A3397 WIRE BOEING737 7373T0 1384582NM CABIN SHORTED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2710323 23374 EMERGENCY LIGHTS INOP AT SEAT ROWS 5-12. REPAIRED SHORTED WIRE UNDER SEAT ROW 5 PER STANDARD PRACTICES MANUAL. 2L72 4F RTA16WE 20040507001182004050700118NM 2004 5 7 CALA0400444 120040501A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 THE RIGHT O/B SEAT TRACK UPPER LOBE BROKE DURING SEAT REMOVAL AT STA 887, RBL 34. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204. 2L72 4F RTA16WE 20040507001192004050700119NM 2004 5 7 CALA0400445 120040501A5320143A7510 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND INTERCOSTAL CORRODED UNDER Z-CHANNEL IN FORWARD CARGO AREA AT RIGHT SIDE, STA 500E-500F. THE INTERCOSTAL WAS REPLACED IAW DRAWING 143A7510 AND SRM 51-40-02. 2L72 4F RTA16WE 20040507001232004050700123NM 2004 5 7 CALA0400411 120040423A5420313A1355203 HEAT SHIELD BOEING737 7373T0 1384582NM LT ENGINE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 LEFT ENGINE HEAT SHIELD CRACKED 2 INCHES. INSTALLED DOUBLER PER ECRA 5450-01073. 2L72 4F RTA16WE 20040507001242004050700124NM 2004 5 7 CALA0400412 120040423A532065C25230 CLIP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 AFT BAG BIN STA 727E SKIN CLIP CORRODED AT S-26R &S-27R. REPLACED SECTION PER SRM 53-0007, FIG 204. 2L72 4F RTA16WE 20040507001262004050700126NM 2004 5 7 CALA0400414 120040424A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 RIGHT AFT PIT CHANNEL CORRODED AT STA 727+4, AND 767 APPROX 22 FT. REPLACED Z-CHANNEL PER SRM 51-40-02. 2L72 4F RTA16WE 20040507001272004050700127NM 2004 5 7 CALA0400415 120040424A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 AFT PIT LEFT Z-CHANNEL CORRODED BETWEEN STA 727+4 AND 787. REPLACED Z-CHANNEL PER SRM 53-00-53. 2L72 4F RTA16WE 20040507001282004050700128NM 2004 5 7 CALA0400416 120040424A53472A0590171 SEAT TRACK BOEING737 7373T0 1384582NM COCKPIT WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 FIRST OFFICERS SEAT TRACK WORN, 6 HOLES. REPLACED SEAT TRACK PER 25-11-11. 2L72 4F RTA16WE 20040507001292004050700129NM 2004 5 7 CALA0400417 120040424A53472A0590171 SEAT TRACK BOEING737 7373T0 1384582NM COCKPIT WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 CAPTAINS SEAT TRACK WORN, 6 HOLES. REPLACED TRACK PER AMM 25-11-11. 2L72 4F RTA16WE 20040507001302004050700130NM 2004 5 7 CALA0400418 120040424A53116546533 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 UPPER FLANGE CRACKED AT STA 500 1 X 1 INCH. INSTALLED DOUBLER PER SRM 51-70-11, FIG 1. 2L72 4F RTA16WE 20040507001312004050700131WP 2004 5 7 CALA0400419 120040425A335060030431 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2771828 49488 COCKPIT, GALLEY AND FWD ENTRY EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. REPLACED BATTERY CHARGER AND PACK PER AMM 33-53-00. 2L72 4F A6WE 20040507001322004050700132NM 2004 5 7 CALA0400420 120040425A53306552988 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 FUSELAGE SKIN DENTED BETWEEN STA 986.5 AND 1006, 3 PLACES, .1562 INCH DIA. REPAIRED PER SRM 53-00-01. 2L72 4F RTA16WE 20040507001342004050700134NM 2004 5 7 CALA0400422 120040425A53306552988 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 FUSELAGE DENT AFT OF BS 986.5+4, 12 INCHES ABOVE DRAIN MAST. REPAIRED PER SRM 53-00-01. 2L72 4F RTA16WE 20040507001352004050700135NM 2004 5 7 CALA0400423 120040425A5320BAC1496444 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 FWD CARGO PIT LT Z-CHANNEL FROM STA 490 CORRODED 207 X 3 INCHES. REPLACED Z-CHANNEL PER SRM 53-00-53. 2L72 4F RTA16WE 20040507001362004050700136NM 2004 5 7 CALA0400424 120040425A5320BAC1496444 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 FWD CARGO PIT RT Z-CHANNEL CORRODED FROM STA 490, 177 X 3 INCHES. REPLACED Z-CHANNEL PER SRM 53-00-53. 2L72 4F RTA16WE 20040507001372004050700137NM 2004 5 7 CALA0400425 120040426A55122024T3 PANEL BOEING737 7373T0 1384582NM HORIZ STAB CRACKED A CALAO OTHER O OTHER ININSP/MAINT 1 SW2718350 23588 GAP PANEL BETWEEN LT HORIZONTAL STAB AND TAIL CONE CRACKED. REPLACED PART PER SRM 51-10-02. 2L72 4F RTA16WE 20040507001382004050700138NM 2004 5 7 CALA0400468 120040505A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344. THE FLOORBEAM WAS REPAIRED IAW SRM 51-70-12. 2L72 4F RTA16WE 20040507001392004050700139WP 2004 5 7 CALA0400426 120040426A3397 WIRE HARNESS DOUG DC9 DC982 3022082WP EXTERIOR LIGHT DEFECTIVE A CALAO OTHER O OTHER CRCRUISE 1 SW2718833 49493 POSITION LIGHTS CIRCUIT BREAKER POPPED AND WILL NOT RESET. REPLACED R5-1051 WIRE BUNDLE PER STD WIRE PRACTICE MANUAL 20-31-15. 2L72 4F A6WE 20040507001412004050700141NM 2004 5 7 CALA0400428 120040426A5320146A75018 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 CARGO FLOOR TRACK STA 790 & 847 RBL 16 CORRODED. INSTALLED REPAIR STRAPS PER ECRA 5321-01185. 2L72 4F RTA16WE 20040507001432004050700143NM 2004 5 7 CALA0400430 120040427A532069374606 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INTERCOSTAL CHANNEL BELOW APU BLEED AIR DUCT AT STA 639 WORN. REPLACED INTERCOSTAL PER SRM 51-10-2. 2L72 4F RTA16WE 20040507001462004050700146EA 2004 5 7 COMA0470038 120040504A2760 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT FALSE ACTIVATIONA COMAO OTHER N FALSE WARNING DEDESCENT 1 SO01371CA 10082 FLIGHT 5291 FLIGHT SPOILER AND SPOILERON CAUTION MESSAGE. COULD NOT DUPLICATE RESET CONTROL UNITS. SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040507001482004050700148EA 2004 5 7 COMA0460294 120040504A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01786CA 7333 FLIGHT 5438 CABIN DOOR OUTER HANDLE STOW CAUTION MESSAGE. ADJUSTED THE DOOR HANDLE PROXIMITY SENSOR. 2L72 4F RTA21EA 20040507001492004050700149EA 2004 5 7 COMA0460295 120040504A33976464 CABLE CNDAIRCL600 CL6002B19 1900309EA CABIN UNRELIABLE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01934CA 7042 FLIGHT 5554 EMERGENCY FLOOR LIGHTS ROWS 5 TO 8 ARE INOP. REPLACED THE FLOOR LIGHTS CABLE ASSY. 2L72 4F RTA21EA 20040507001502004050700150EA 2004 5 7 COMA0460269 120040413A3260 PSEU CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01933CA 7040 FLIGHT 5479 NWS INOP, WOW INPUT CAUTION AND CIRCUIT BREAKER TRIPPED. RESET PSEU AND OPERATIONAL CHECK OF NWS WAS SATISFACTORY. 2L72 4F RTA21EA 20040507001512004050700151EA 2004 5 7 COMA0460282 120040426A301032144424 ANTI-ICE VALVE CNDAIRCL600 CL6002B19 1900309EA LEFT FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01984CA23064 7171 FLIGHT 5351 WING OVERHEAT MESSAGE. REPLACED THE LEFT WING MODULATING VALVE. 2L72 4F RTA21EA 20040507001522004050700152EA 2004 5 7 COMA0460280 120040426A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01969CA30481 7141 FLIGHT 5187 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20040507001562004050700156EA 2004 5 7 COMA0460285 120040424A5245 SERVICE DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SYS OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01781CA 7312 FLIGHT 5609 STALL FAIL WARNING AND LOUD WHINING NOISE. THE 02 SERVICE DOOR WAS OPEN, REPAIRED DOOR AND SECURED CLOSED. 2L72 4F RTA21EA 20040507001572004050700157EA 2004 5 7 COMA0460281 120040423A2612 FIRE WARNING CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01977CA 7157 FLIGHT 5400 DURING CRUISE FLIGHT AT FLIGHT LEVEL 270 RECEIVED A CARGO BOTTLE LOW PRESSURE MESSAGE, EXTINGUISHED AT FLIGHT LEVEL 180. CREW DECLARED AN EMERGENCY, DIVERTED TO JAX AND LANDED SAFELY. PERFORMED INSPECTION OF CARGO BAY, NO EVIDENCE OF FIRE. DEFERRED THE CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01. 2L72 4F RTA21EA 20040507001592004050700159EA 2004 5 7 COMA0460277 120040425A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01917CA 7017 FLIGHT 5927 FLAP FAIL CAUTION WHILE PARKED AT THE GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20040507001612004050700161EA 2004 5 7 COMA0460279 120040424A3231 DOOR CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF RIG A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01926CA 7027 FLIGHT 9464 AFTER GEAR RETRACT, LOUD BANGING OF THE NLG DOORS. ADJUSTED THE RIGGING OF THE NLG DOORS PER AIRCRAFT M/M. 2L72 4F RTA21EA 20040507001632004050700163EA 2004 5 7 COMA0460292 120040502A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA23248 7043 FLIGHT 5803 GEAR DISAGREE WARNING. REPLACED THE 3B ACMP. 2L72 4F RTA21EA 20040507001642004050700164EA 2004 5 7 COMA0470034 120040420A5755CC670170835 FITTING CNDAIRCL600 CL6002C10 1390015EA SPOILER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA3963 10064 DMI 34502 RIGHT OUTBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4857. 2L72 4F RTA21EA 20040507001652004050700165EA 2004 5 7 COMA0470035 120040502A5755CC670170835 HINGE FITTING CNDAIRCL600 CL6002C10 1390015EA SPOILER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01367CA3932 10069 RIGHT INBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4910. 2L72 4F RTA21EA 20040507001662004050700166EA 2004 5 7 COMA0470036 120040502A32349752671 FLOW VALVE CNDAIRCL600 CL6002C10 1390015EA LANDING GEAR MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01391CA2246 10108 FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3B FLOW LIMITING VALVE. 2L72 4F RTA21EA 20040507001692004050700169EA 2004 5 7 COMA0460276 120040422A3260 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE ACTIVATIONA COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01957CA 7109 FLIGHT 5417 DURING APPROACH INTO BNA RECEIVED A NR 3 HYDRAULIC LOW PRESSURE CAUTION FOLLOWED BY NOSE GEAR DISAGREE. CREW DECLARED AN EMERGENCY, CAUTION MESSAGES CLEARED, AIRCRAFT LANDED SAFELY. REFERENCE CRJ FSM NORMAL PROCEDURES 3-98, A NUISANCE GEAR DISAGREE MESSAGE MAY ANNUNCIATE IF THE LANDING GEAR IS SELECTED DOWN, PRIOR TO SELECTING FLAPS GREATER THAN 0 DEGREES. IF THE MESSAGE IS NOT DISPLAYED AFTER THE GEAR IS DOWN AND LOCKED, THERE ARE NO RESTRICTIONS AND THE ANOMALY SHOULD BE DISREGARDED. 2L72 4F RTA21EA 20040507001702004050700170EA 2004 5 7 COMA0470033 120040420A5755CC670170835 FITTING CNDAIRCL600 CL6002C10 1390015EA SPOILER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01354CA3963 10064 DMI 34502 RIGHT OUTBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4857. 2L72 4F RTA21EA 20040507001732004050700173EA 2004 5 7 COMA0460270 120040413A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01917CA9349 7017 FLIGHT 5034 GEAR DISAGREE WARNING NLG INDICATED UNSAFE. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040507001742004050700174EA 2004 5 7 COMA0460267 120040415A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01936CA 7043 FLIGHT 5146 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD98-20-01. 2L72 4F RTA21EA 20040510000012004051000001EA 2004 5 10 SWIA200413180 120040413A5340 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 MAIN FUSELAGE FITTING CRACKED AT FS 460.00 RBL 9.0 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND RII 53 401. 2L72 4F4 FRTA21EA E15NE 20040510000032004051000003EA 2004 5 10 SWIA200413182 120040413A5320 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 FUSELAGE LEFT VERTICAL BEAM LWR OUTBOARD FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV NC AND IAW RII53-401. 2L72 4F4 FRTA21EA E15NE 20040510000072004051000007SO 2004 5 10 SWIA200413227 120040422A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07583SW7879 7879 120351 EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-50-01. OPS CHECK GOOD. 2L72 4T RTA31SO 20040510000092004051000009SO 2004 5 10 SWIA200413229 120040423A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO FLAP LEVER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07189SW756 756 120048 IN CRUISE FLIGHT FLAP, ADV SWS AND CONTROL FAULT LIGHTS ILLUMINATED AND CLEARED THEMSELVES MULTIPLE TIMES. REMOVED AND REPLACED FLAP SELECTOR LEVER. OPS CHECKS GOOD IAW EMB MM 27-50-01. 2L72 4T RTA31SO 20040510000112004051000011EA 2004 5 10 SWIA200413231 120040422A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS ILLUMINATED A SWIAC ABORTED TAKEOFF JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07446SW 7666 DURING TAKEOFF ATTEMPT RECEIVED CONFIG SPOILER MESSAGE, THEN INBOARD AND FLIGHT SPOILER FAULT MESSAGE. COMPLIED WITH SPOILERON SYSTEM RESET PROCEDURE AS PER AMM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040510000122004051000012EA 2004 5 10 SWIA200413232 120040426A26218978892 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY WILL NOT TEST A SWIAO OTHER LJ NO TEST WARNING INDICATION NRNOT REPORTED 1 NM07925SW3888 3888 7682 CARGO BOTTLE LOW CAUTION MESSAGE ON EICAS FOR APPROXIMATELY 5 MINUTES THEN WENT AWAY. RAN QRH. BOTTLES DID NOT PASS TEST IN FLIGHT. INSTALLED NEW CARGO BOTTLE. OPS CHECK GOOD. 2L72 4F RTA21EA 20040510000132004051000013SO 2004 5 10 SWIA200413233 120040422A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07188SW1540 1540 120039 OUTBOARD FLAP PAIR CAUSES DISAGREEMENT ON FLAP RETRACTION AFTER TAKEOFF. FIXES ITSELF AND RETRACTS FLAPS AFTER ABOUT 2 SECS, HAPPENED ON 3 FLIGHTS. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD IAW EMB MM 27-50-06. 2L72 4T RTA31SO 20040510000172004051000017EA 2004 5 10 SWIA200413254 120040426A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA FWD CABIN MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07952SW 7805 SMOKE CARGO WARNING / FAN FAIL MESSAGE INFLIGHT. REPLACED FORWARD CARGO SMOKE DETECTOR. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040506000232004050600023EU 2004 5 6 BAQA094254 120040426A3050C19267VG11 DISPLAY UROCOPEC135 EC135T1 5620026EU COCKPIT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME1048 132 EFIS TUBE FAILED IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 04/27/2004 1G72 3U H88EU 20040506000532004050600053EU 2004 5 6 MALA040369 120040411A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, SEAT TRACK NR 1 CORRODED OUT OF LIMITS. CUT OUT CORRODED SECTION OF NR 1 SEAT TRACK, LOCATED AND DRILLED NEW SECTION OF SEAT AND INSTALLED IAW MESABA EO A53026. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040506000862004050600086EU 2004 5 6 MALA040349 120040424A7697 LEAD BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE PICKUP SHORTED A MALAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15530XJ E2364 IN CLIMB AT APPROX 7000 FT HEARD LOUD POPPING NOISE THEN APPROX 1 MIN LATER ANOTHER POPPING NOISE FOLLOWED BY POWER LOSS ON NR 3 ENGINE AS INDICATED BY N1 AND N2 AS WELL AS AIRCRAFT YAW. COMPLETED SHUTDOWN OF NR 3 ENGINE. FLIGHT ATTENDANT REPORTED, PASSENGER SAW FIRE FROM ABOVE. ENG 3 FIRE EXTINGUISHER 1 WAS ACTIVATED AS A PRECAUTION. MAINTENANCE REMOVED AND REPLACED OVERSPEED PICKUPS AND ELECTRICAL LEADS DUE TO SHORTING CONDITION, CAUSING OVERSPEED SYSTEM TO SHUT THE ENGINE DOWN. ALL WORK PERFORMED IAW LF-507 MANUAL AND JOBCARD, ALL CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20040506000892004050600089EU 2004 5 6 MALA040348 120040424A2611CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101EU CARGO BAY FAILED A MALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15457XJ 340B457 CARGO SMOKE ILLUMINATED ON CWP DURING PREFLIGHT. MAINTENANCE REMOVED & REPLACED CARGO AFT SMOKE DETECTOR P/N CGAB1201-01, S/N ON 1128, S/N OFF 750, OPS CHECK GOOD. 2L72 4T RTA52EU 20040506001162004050600116NM 2004 5 6 CALA0400463 120040504A5320143A750114 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN FORWARD CARGO BIN BETWEEN STA 500 AND 500A. THE CORRODED SECTION OF Z-CHANNEL WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040506001422004050600142WP 2004 5 6 ASAA0480128 120040229A5230591014167 DOOR FRAME DOUG DC9 DC983 3022083WP CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO DOOR CRACKED AT OUTBOARD FRAME ON TRAILING EDGE OF DOOR JUST ABOVE AND OUTBOARD OF DOOR LATCH TORQUE TUBE. STOP DRILLED CRACK, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 52-03 AND NDTM PT6. (M) 2L72 4F RTA6WE 20040506001502004050600150NM 2004 5 6 ASAA0410045 120040202A335086210144 BATTERY BOEING737 737290C 138448VNM SMOKER BARRIER DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY EXIT SIGN ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN LIGHT TESTED NORMAL. (M) 2L72 4F A16WE 20040506001532004050600153NM 2004 5 6 ASAA0410065 120040213A335086210144 BATTERY BOEING737 737298C 1384490NM SMOKE BARRIER DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING ROUTINE INSPECTION, FOUND THE EXIT IDENTIFIER ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN EXIT IDENTIFIER TESTED NORMAL. (M) 2L72 4F RTA16WE 20040506001562004050600156WP 2004 5 6 ASAA0480134 120040229A5311993607317 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO PIT CORROSION ON AFT AND FRONT SIDE OF FORMER AT STATION 1211 BETWEEN LONGERON 30 AND 22R. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW MD80 SRM 51-30-3. (M) 2L72 4F RTA6WE 20040506001572004050600157WP 2004 5 6 ASAA0480149 120040302A5320993033886 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CORROSION AT WEB LONGERON 18 BETWEEN STATION 275 AND 294. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-01. (M) 2L72 4F RTA6WE 20040507000072004050700007NM 2004 5 7 ANCF200400005 120040323A2841 INDICATOR BOEING767 767259 1385136NM FUEL QTY MALFUNCTIONED W ANCFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO23986AN 24835 TOTAL FUEL DIFFERS FROM CAPT AND F/0 FMC(S) CALCULATED FUEL QTY. FUEL QTY ERROR PROG 2/2 ALERT MSG DISPLAYED ON CDU AND EICAS MSG FMC MESSAGE DISPLAYED FUEL FLOW WAS NORMAL TOTAL FUEL 94.100 LBS FMC CALCULATED 101.300 LBS. TRANSFER TO DMI 436 MEL 28-41-1-2 CAT C. PERFORMED MEL PROCEDURE C/B PULL OUT IAW FIM 34-INDEX FUEL QTY ERROR DISAGREE PROGRESS 2/2, THE FIM 34-61-00 FG 106 SHEET 1 BLOCKS 1-10-20-2-21 WERE PERFORMED, IN ADDITION WAS PERFORMED FIM 28-41-00 SHEET 1 BLOCKS 1-2 SHEET 2 BLOCKS 2-25 THE SYSTEM IS OK , DOES NOT DUPLICATE FAILURE. 2L72 4F RTA1NM 20040507000292004050700029EU 2004 5 7 ULX2004F00006 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP23232LA502 3356 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U3 U H9EU E19EU 20040507000672004050700067EA 2004 5 7 SWIA200413259 120040504A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07445SW4964 4964 7651 NR 2 STAB TRIM WOULD NOT ENGAGE. REMOVED AND REPLACED HSTA IAW MM 27-42-05, 27-42-01 & 27-40-00. REPLACED MCU P/N: 7062-3, S/N OFF: 904. REPLACED STAB ENGAGE PANEL. P/N: 601R51706-3. OPS CHECK GOOD. 2L72 4F RTA21EA 20040507000722004050700072EA 2004 5 7 SWIA200413214 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA HYD MANIFOLD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 CRACK IN NR 1 HYDRAULIC MANIFOLD ATTACH INTERCOSTAL AT FS 718.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040507000742004050700074EA 2004 5 7 SWIA200413216 120040418A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FUSELAGE SKIN AT FS 235.0 LBL 6.0 AND RBL 6.0 (TRAILING EDGE OF NLG CUTOUT) POSSIBLE CRACKS. DISCOVERED DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REPAIR PANELS IAW REO 601R-53-11-010 REV. C. 2L72 4F RTA21EA 20040507000762004050700076EA 2004 5 7 SWIA200413246 120040416A5720 ANGLE CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 RIGHT WING SECTION 48.30 ANGLE PART NUMBER 600-10204-28 IS CRACKED 1 INCH IN RADIUS. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20040507000782004050700078EA 2004 5 7 SWIA200413248 120040416A5320601R3114863 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 LEFT FLOOR SILL P/N 601R3114863 FS 364 AND FS 379 IS SEVERELY CORRODED. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20040507000802004050700080EA 2004 5 7 SWIA200413159 120040306A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 INTERCOSTAL ATTACH ANGLE CRACKED FS 484 LBL 36. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-20, AND REO 601R-53-41-059 REV A NOTES 5 TO 14. 2L72 4F RTA21EA 20040507000822004050700082EA 2004 5 7 SWIA200413218 120040418A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FS 484 INTERCOSTAL ANGLE AT RBL 9 OUTBOARD IS CRACKED .5 INCH IN RADIUS OF ANGLE AT WL 73. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PN 601R31171-9 PER BRAS EO STEP 1 AND SRM 51-42-21 AND SKYWEST EA NO. RJ240-53. 2L72 4F RTA21EA 20040507000842004050700084EA 2004 5 7 SWIA200413220 120040418A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FS 484 WL 73 LBL 9 OUTBOARD INTERCOSTAL ATTACHMENT ANGLE IS CRACKED .25 INCH. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW ANGLE PN 601R31171-27 PER BRAS EO STEPS 1 AND SRM 51-42-21, AND SKYWEST EA NO. RJ240-53. 2L72 4F RTA21EA 20040507000862004050700086EA 2004 5 7 SWIA200413222 120040418A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 CRACK FOUND AT FS 202.75 BULKHEAD LBL 2A AT PARKING BRAKE CONTROL ROD CUTOUT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED BULKHEAD AT FS 202.75 LBL 2A BETWEEN STRINGERS 20L AND 21L IAW REO 601R-53-11-767. 2L72 4F RTA21EA 20040507000882004050700088EA 2004 5 7 SWIA200413164 120040306A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 FS 364 STR 8R IS CRACKED FROM FASTENER HOLE ON UPPER FRAME FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME FLANGE IAW REO 601R-53-21-492 AND RII53-401. 2L72 4F RTA21EA 20040507000902004050700090EA 2004 5 7 SWIA200413166 120040306A5411 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 LEFT PYLON LEADING EDGE RIB CRACKED ON LOWER FLANGE AT FS 605.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, AND RII53-401. 2L72 4F RTA21EA 20040507000932004050700093EA 2004 5 7 SWIA200413169 120040413A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 INTERCOSTAL CLIP ANGLE CRACKED IN RADIUS, FS 625.3 STR 14 RT. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-23-00. 2L72 4F RTA21EA 20040507000952004050700095EA 2004 5 7 SWIA200413171 120040413A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07448SW 7678 FS 621 LEFT FLOOR SUPPORT ANGLE LBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII53-401. 2L72 4F RTA21EA 20040507000972004050700097EA 2004 5 7 SWIA200413173 120040413A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 RIGHT ELECTRICAL BAY FLOOR AT FS 193, RBL 30 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-245 NC. 2L72 4F4 FRTA21EA E15NE 20040507001102004050700110NM 2004 5 7 CALA0400442 120040501A5320143A948535 SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND PANEL 121HW LOWER SUPPORT FRAME CORRODED AT AFT BULKHEAD OF FORWARD CARGO AREA. THE SUPPORT FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040507001202004050700120NM 2004 5 7 CALA0400446 120040501A5347BAC1509100688 CARGO TRACK BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND A 2 INCH CRACK IN AFT PIT FLOOR RAIL AT STA 727I, RBL 13-84. THE FLOOR RAIL WAS REPAIRED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040507001332004050700133NM 2004 5 7 CALA0400421 120040425A53306552988 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 FUSELAGE DENTED AT BS 1006 MINUS 4 INCHES, 12 INCHES ABOVE DRAIN MAST. REPAIRED PER SRM 53-00-01. 2L72 4F RTA16WE 20040507001402004050700140NM 2004 5 7 CALA0400427 120040424A2910 B-NUT BOEING767 767424ER 1385270NM HYD SYSTEM LOOSE A CALAA UNSCHED LANDING K FLUID LOSS LDLANDING 1 SW2776054 29449 HYDRAULIC LEAK AT LOOSE B-NUT ON LANDING GEAR UP POSITION LINE. TIGHTENED B-NUT, SERVICED SYSTEM, LEAKED CHECKED. 2L72 4F RTA1NM 20040507001542004050700154EA 2004 5 7 COMA0460288 120040423A3411 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA PITOT/STATIC SYSCONTAMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01528CA 7841 FLIGHT 5208 ABORTED TAKEOFF AT 75 KTS DUE TO INOPERATIVE STANDBY AIRSPEED INDICATION. PURGED WATER FROM THE STANDBY PITOT SYSTEM LINE. 2L72 4F RTA21EA 20040507001552004050700155EA 2004 5 7 COMA0460287 120040424A2121AE0804AA2 COOLING FAN CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01496CA13352 7791 FLIGHT 5527 DISPLAY COOL CAUTION MESSAGE. REPLACED THE COCKPIT DISPLAY COOLING FAN. 2L72 4F RTA21EA 20040507001602004050700160EA 2004 5 7 COMA0460278 120040423A3234555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01926CA22562 7027 FLIGHT 5243 AFTER TAKEOFF, GEAR RETRACTION WAS ABNORMALLY NOISY. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20040507001672004050700167EA 2004 5 7 COMA0460283 120040424A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A COMAK NONE O OTHER APAPPROACH 1 SO01729CA16754 7265 FLIGHT 5818 DURING APPROACH INTO MEM THE NOSE GEAR AND DOOR TOOK TWO MINUTES TO EXTEND UPON SELECTING GEAR DOWN. REPLACED THE HYDRAULIC PUMP 31. 2L72 4F RTA21EA 20040510000152004051000015SO 2004 5 10 SWIA200413252 120040428A2611 ANNUNCIATOR EMB 120 EMB120ER 3260203SO SMOKE DETECTOR MALFUNCTIONED A SWIAO OTHER N FALSE WARNING DEDESCENT 1 NM07292UX 120292 SMOKE TRIPLE CHIME IN FLIGHT ON FINAL DESCENT. LAV SMOKE DETECTOR LIGHTS FLASHING. NO SMOKE IN CABIN AT ALL, OR LAV. REMOVED AND REPLACED SMOKE DETECTOR ANNUNICATOR PANEL WITH SERVICEABLE PANEL. OPS CHECK GOOD. 2L72 4T RTA31SO 20040510000162004051000016SO 2004 5 10 SWIA200413253 120040426A3150 WARNING SYSTEM EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07236SW 120312 DURING TAXI-IN, RECEIVED SPORADIC TRIPLE CHIME TAKEOFF TRIM WITH TRIM IN GREEN BAND. PERFORMED TEST AFTER SHUT DOWN AND DID NOT PASS. RERACKED AURAL WARNING UNIT AND RESET AURAL WARNING CB. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040510000202004051000020EA 2004 5 10 SWIA200413257 120040430A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER FL FLT CONT AFFECTED NO TEST TXTAXI/GRND HDL 1 NM07948SW 7789 STAB TRIM CHANNEL 2 INOP. CLEANED STAB 2 ENGAGE SWITCH AND REPLACED HSTCU. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040510000222004051000022EA 2004 5 10 SWIA200413045 120040309A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 MAIN FUSELAGE; FS 280.00; RBL 9; UPPER FLANGE CRACKED. REPAIRED IAW CRJ REO 601R-53-11-137 REV NC AND RII53-401. 2L72 4F4 FRTA21EA E15NE 20040510000242004051000024 2004 5 10 SWIA200413145 420040419A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07929SW6832 6825 7703 UPON TAXI OUT YD2 DISENGAGED, ALSO NUMEROUS TIME INFLIGHT ASSOCIATED WITH AP DISCONNECT. REMOVED AND REPLACED FCC NR 2. 2L72 4F RTA21EA 20040510000262004051000026EA 2004 5 10 SWIA200413147 120040419A26218978892 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA APU BAY LOW A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07912SW6331 6331 7595 APU BOTTLE LOW CAUTION MESSAGE ON. REPLACED LEFT FIREX CONTAINER IAW MM 26-22-01. OPS TEST GOOD. 2L72 4F RTA21EA 20040510000272004051000027SO 2004 5 10 SWIA200413148 120040417A1420 CONNECTOR EMB 120 EMB120ER 3260203SO FLAP CONTROL CONTAMINATED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07290SW 120317 ON TAXI CHECK, GOT OUTBOARD FLAP CONTROL FAULT UPON APPLICATION TO FLAPS 15; RESET SUCCESSFULLY AS PER QRH, THEN HAPPENED 2 MORE TIMES UPON SETTING FLAPS 15 DURING TAXI BACK TO GATE. REMOVED WATER FROM CONNECTOR. OPS CHECKED NORMAL. 2L72 4T RTA31SO 20040510000282004051000028SO 2004 5 10 SWIA200413149 120040401A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07235SW 120310 LEFT FORWARD FLOOR SEAT TRACK HAS CORROSION ON FORWARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT FORWARD FLOOR SEAT TRACK END. 2L72 4T RTA31SO 20040510000292004051000029SO 2004 5 10 SWIA200413150 120040401A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07235SW 120310 LEFT AFT FLOOR SEAT TRACK HAS CORROSION ON SEVERAL SPOTS. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK AS REQUIRED. NO DEFECTS NOTED. 2L72 4T4 TRTA31SO E20NE 20040510000302004051000030SO 2004 5 10 SWIA200413151 120040417A3240 CONTROL PANEL EMB 120 EMB120ER 3260203SO EMERGENCY BRAKE MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07297SW 120327 ELECTRIC ODOR & SMOKE COMING FROM CENTER CONSOLE. REMOVED AND REPLACED PRESS SYSTEM/EMERGENCY PARK BRAKE PANEL AND LIGHTING ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 120-40220-001. 2L72 4T RTA31SO 20040510000312004051000031EA 2004 5 10 SWIA200413152 120040419A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER DEDESCENT 1 NM07952SW 7805 ON DESCENT, PASSING THRU 10,000 FT, CAPTAIN'S SIDE WINDOW CRACKED/SHATTERED. REMOVED AND REPLACED CAPTAIN'S WINDOW WITH SERVICEABLE UNIT IAW MM 56-12-01 AND RII CARD 56-402. P/N: 601R33033-11, S/N OFF: 04050H6013. 2L72 4F RTA21EA 20040510000322004051000032SO 2004 5 10 SWIA200413153 120040418A32331959500007 ACTUATOR EMB 120 EMB120ER 3260203SO MLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07235SW7011 7011 120310 ON TAKEOFF DURING GEAR RETRACTION LEFT MAIN WOULD NOT RETRACT. REPLACED LEFT GEAR MAIN ACTUATOR IAW RII 32-302. OPS AND LEAK CHECK GOOD. 2L72 4T RTA31SO 20040510000352004051000035SO 2004 5 10 2004F00103 120040408A3260487862 DOWNLOCK SWITCH PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA HARTZLHCE2Y HCE2YR2 GL LT MLG INOPERATIVE E UQMAO OTHER O OTHER NRNOT REPORTED 1 CE019085Y 31119 RL96061 CJ762 ON A PART 91 FLIGHT THE GEAR DID NOT GET A LT DOWN LIGHT AND THE GEAR SELECTOR DID NOT COME BACK TO CENTER. AFTER A SAFE LANDING FOUND THE SWITCH NOT OPENING ALL THE WAY. CLEANED SWITCH AND BELIEVE THAT THE INTERNAL SPRING IS BROKEN AND ONLY ALLOWING HALF TRAVEL OUT AND NOT DISENGAGING SWITCH. 1L72 3O3 O A20SO E14EA 5 CP9EA 20040510000362004051000036NM 2004 5 10 USA2004F00014 120040214A2130 CABIN PRESSURE BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE FAILED A USAABGA EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19518AU 23704 ENROUTE, WHILE LEVEL AT FL330, THE AIRCRAFT LOST PRESSURIZATION. CREW ACCOMPLISHED A RAPID DESCENT TO 10,000 FT. OXYGEN MASKS DID DEPLOY DURING DESCENT. STANDBY AND MANUAL PRESSURIZATION MODES WERE USED BUT WERE NOT EFFECTIVE. OUTFLOW VALVE WAS REPORTED TO BE FULLY CLOSED. A RUMBLING SOUND WAS HEARD BENEATH THE FLOORBOARDS BY THE FORWARD AND AFT CABIN CREW MEMBERS. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA16WE E2GL 20040510000382004051000038EU 2004 5 10 EKL2004F00000 120040308A2910704A34412038 HOSE SNIAS 350 AS350B2 8680813EU HYDRAULIC SYS LEAKING B EKLRO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP07955TV 3246 AFTER START, WHILE AT FLIGHT IDLE, PRIOR TO TAKE OFF, THE PILOT RECEIVED THE HYD LIGHT ON THE WARNING PANEL. PILOT SHUT DOWN AC WITHOUT INCIDENT. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT A SMALL PIN HOLE SIZE LEAK HAD DEVELOPED IN THE PRESSURE LINE FROM THE HYD PUMP TO THE REGULATING UNIT, ALLOWING ALL THE FLUID OF HYD SYSTEM TO BE DISCHARGED THROUGH THIS LEAK AND GIVING THE PILOT HYD SYSTEM FAILURE AND LIGHT. 1G71 3U H9EU 20040510000452004051000045WP 2004 5 10 AALA20040526 120040504A33506030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21474 49649 DEN AFT EMERGENCY LIGHTS IN TAIL INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000482004051000048NM 2004 5 10 AALA20040530 120040505A33971703643 PIN BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21386AA 27060 JFK EMERGENCY LIGHT ON THE SIDE OF ROW 39H INOPERATIVE. REPAIRED BROKEN CONTACT PIN FOR EMERGENCY LIGHTS AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20040510000502004051000050EA 2004 5 10 COMA0470037 120040430A5245 DOOR CNDAIRCL600 CL6002C10 1390015EA O2 SERVICE DOOR OPEN A COMAB EMER. DESCENT O OTHER CRCRUISE 1 SO01653CA 10129 FLIGHT 5640 CREW 02 PRESSURE GAUGE READS----. COULD NOT DUPLICATE. FOUND 02 SERVICE DOOR OPEN, CLOSED DOOR, SYSTEM FUNCTION NORMAL. 2L72 4F RTA21EA 20040510000512004051000051EA 2004 5 10 COMA0460265 120040416A2751855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAULTY A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01518CA2315 7816 FLIGHT 5849 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING TAXI-IN WHEN FLAPS WERE RETRACTED. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20040510000522004051000052 2004 5 10 COMA0460266 420040416A3418 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01483CA 7689 FLIGHT 5713: DURING CRUISE FLIGHT RECEIVED A MACH TRIM/STAB TRIM CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT DESTINATION CITY, BGR. PERFORMED SYSTEM RESET, CAUTION MESSAGE CLEARED. 2L72 4F RTA21EA 20040510000532004051000053EA 2004 5 10 COMA0460289 120040422A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01408CA 7440 CRACK INDICATION NOTED AT RIGHT HAND LOWER WING PLANK ACCESS PANEL CUTOUT 650 AB. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-030. 2L72 4F RTA21EA 20040510000572004051000057NE 2004 5 10 DLM90040391 220040503A7200V2528D5 ENGINE DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 2 MALFUNCTIONED A DALAK NONE A FLAME/FIRE TXTAXI/GRND HDL 1 SO27907DA22709 53387 020046 ACS REPORTED TAIL PIPE FIRE NR 2 ENGINE AFTER ENGINE SHUTDOWN. REPLACED ENGINE. 2L72 4F4 FRTA6WE E40NE 20040510000582004051000058EU 2004 5 10 MALA040329 120040401A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION, CORROSION ON FWD LEFT I/B SEAT TRACK AT STA 288-322. MAINTENANCE REPAIRED SEAT TRACK IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 4/16/04. 2L72 4T RTA52EU 20040510000592004051000059EU 2004 5 10 MALA040356 120040421A3350 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15406XJ 340B406 DURING CAPACITY CHECK BATTERY PACK P/N 3301-51, S/N 2072 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/5/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED BATTERY PACK 3301-31 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/16/04. 2L72 4T RTA52EU 20040510000602004051000060EU 2004 5 10 MALA040354 120040407A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15529XJ E2363 DURING CAPACITY CHECK BATTERY PACK P/N 61-2275-1, S/N 9801234 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/7/04 & 4/10/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK 61-2274-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/16/04. 2H74 4F RTA49EU 20040510000622004051000062EU 2004 5 10 MALA040358 120040428A3350 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE L NO TEST NRNOT REPORTED 1 GL15448XJ 340B448 LEFT EXTERIOR LIGHT FOUND INOPERATIVE. INSPECTED LIGHT AND FOUND EXTERIOR LIGHT ASSEMBLY SHORTED INTERNALLY AND POWER SUPPLY 74LN NOT SUPPLYING POWER TO LIGHT. REPLACED LIGHT ASSEMBLY AND POWER SUPPLY WITH SERVICEABLE UNITS. EMERGENCY LIGHTING OPS CHECKED GOOD. 2L72 4T RTA52EU 20040510000632004051000063EU 2004 5 10 MALA040355 120040407A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15506XJ E2314 DURING CAPACITY CHECK BATTERY PACK P/N 61-2275-1, S/N 0001243 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/5/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK 61-2274-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/16/04. 2H74 4F RTA49EU 20040510000642004051000064EU 2004 5 10 MALA040353 120040407A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15529XJ E2363 DURING CAPACITY CHECK BATTERY PACK P/N 61-2275-1, S/N 97080024 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/7/04. UNIT FAILED. UNIT CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/14/04. 2H74 4F RTA49EU 20040510000662004051000066WP 2004 5 10 AALA20040531 120040505A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21974TW 53624 OVERWING EMERGENCY LIGHTS AT ROWS 10 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK AT B5-101 FOR OVERWING EMERGENCY LIGHTS AT ROWS 10 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20040510000672004051000067EU 2004 5 10 MALA040330 120040401A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION CORROSION ON FWD RIGHT I/B SEAT TRACK. MAINTENANCE REMOVED CORRODED SEAT TRACK AT STA 288-322 AND REPAIRED IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 4/16/04. 2L72 4T RTA52EU 20040510000682004051000068EU 2004 5 10 MALA040335 120040413A2612523402 PRINTED CKT BOAR BAC 146 AVRO146RJ85A1500097EU FIRE WARNING SYSCONTAMINATED A MALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL15520XJ E2345 FIRE WARNING FLASHED ON TAKEOFF ROLL. LOOP FAULT ON ALL 4 ENGINES ON LOOP A, WENT AWAY WHEN SWITCH TO LOOP B. MAINTENANCE FOUND PCB WAS CONTAMINATED. REPLACED PCB, ALL CHECKS GOOD IAW 26-11-00 501, P/N 5234-02, S/N OFF 911, S/N ON 875. 2H74 4F RTA49EU 20040510000712004051000071EU 2004 5 10 MALA040336 120040414A2460 SUPPRESSOR SAAB SF340 340B 7860101EU ELECTRICAL SYS FAULTY A MALAK NONE J WARNING INDICATION CRCRUISE 1 GL15451XJ 340B451 ON APPROACH LEFT MAIN/ESS BUS BREAKER POPPING. MAINTENANCE REMOVED AND REPLACED TRANSIENT SUPPRESSOR 55PC PER MAINT ENGINEERING, ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20040510000722004051000072NM 2004 5 10 AALA20040534 120040504A3350 CIRCUIT BREAKER BOEING767 767323 1385205NM EMERGENCY LIGHT POPPED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21393AN 29430 MIA EMERGENCY LIGHTS IN CABIN INOPERATIVE. RESET CIRCUIT BREAKER FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20040510000732004051000073NM 2004 5 10 AALA20040535 120040504A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21967AN 29545 BDL EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040510000742004051000074WP 2004 5 10 AALA20040518 120040503A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217541A 49995 DTW COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000802004051000080SO 2004 5 10 C2XA04CL043 120040429A2730 CONTROL CABLE EMB 145 EMB145LR 3260212SO ELEVATOR OUT OF ADJUST A C2XAK NONE F FLT CONT AFFECTED CRCRUISE 1 SW2713550 145575 CLE FLIGHT NR 2300 THE CREW REPORTED THE AIRCRAFT ELEVATORS WERE MUSHY AND THAT THEY RAN OUT OF ELEVATOR AUTHORITY IN THE FLARE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND ADJUSTED THE ELEVATOR CONTROL CABLES. TEST FLIGHT RESULTS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTT00011AT 20040510000812004051000081SO 2004 5 10 C2XA04SH275 120040509A532014524131005 BRACKET EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE MAIN DOOR SILL FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510000822004051000082SO 2004 5 10 C2XA04SH277 120040509A532014522459003 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE RAMP ANGLE ON THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510000832004051000083GL 2004 5 10 C2XA04CL042 220040426A720023074862 ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 2 FAILED A C2XAA UNSCHED LANDING MJBOVER TEMP WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2741104 145646 CAE312263 CMH FLIGHT NR 2699 THE CREW REPORTED THE NR 2 ENGINE EXCEEDED 950 DEGREES ON CLIMBOUT. THE AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. THE CREW ALSO REPORTED A SMOKE SMELL. MAINTENANCE REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRT TE6CH 20040510000842004051000084SO 2004 5 10 C2XA04TY076 120040505A531514521699003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM TOP CAP AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040510000852004051000085WP 2004 5 10 AALA20040520 120040503A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21587AA 53250 DEN OVERHEAD EMERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-23 FOR EMERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000862004051000086WP 2004 5 10 AALA20040521 120040503A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21587AA 53250 DEN OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-100 FOR OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000882004051000088NM 2004 5 10 AALA20040517 120040502A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHTSLOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21384AA 26996 MIA EMERGENCY LIGHT AT A6 LAVATORY HAS WIRE HANDING DOWN FROM BUMPER RUB STRIP. REINSTALLED WIRING IN CHANNEL FOR EMERGENCY LIGHT AT A6 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20040510000922004051000092EU 2004 5 10 AALA20040523 120040504A3350 LIGHT AIRBUS300 A300B4605R 3930308EU SEAT 9G BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW2118066 509 MIA EMERGENCY LIGHT AT SEAT 9G BROKEN. INSTALLED NEW EMERGENCY LIGHT ASSEMBLY AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA35EU 20040510000952004051000095SO 2004 5 10 C2XA04CL046 120040501A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715985 145248 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS OVER THE SERVICE DOOR AND THE FIRST TWO AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040510000972004051000097NM 2004 5 10 AALA20040498 120040428A3350 SIGN BOEING767 767323 1385205NM EMERGENCY LIGHTSLOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21350AN 33089 ORD EMERGENCY EXIT SIGN AT SEAT ROW 20AB IS HANGING DOWN INTO THE AISLE. RE-SECURED EMERGENCY EXIT SIGN AT SEAT ROW 20AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20040510000982004051000098WP 2004 5 10 AALA20040499 120040428A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21406A 49317 DFW SEAT MOUNTED EMERGENCY LIGHT BETWEEN ROWS 27 AND 30 INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR SEAT MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 27 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001032004051000103SO 2004 5 10 C2XA04SH260 120040503A531514521700007 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001042004051000104NM 2004 5 10 AALA20040501 120040426A5347FBE12041 SEAT TRACK BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21699AN 27051 TUL CORROSION FOUND ON NUMBER FOUR SEAT TRACK AT ANCHORS FOR COFFEE BAR AT STATIONS 676 AND 686. CORROSION AREA WAS FOUR INCHES BY 10 INCHES AND LOCATED ON CABIN FLOOR. REPLACED NUMBER FOUR SEAT TRACK AT STATION 640 THROUGH 780. (CLOSED) 2L72 4F RTA2NM 20040510001052004051000105EU 2004 5 10 AALA20040503 120040428A5730 SKIN AIRBUS300 A300B4605R 3930308EU LT WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2180057 465 TUL LEFT HAND UPPER WING SKIN PANEL NUMBER 2 HAS A CRACK FROM FASTNER AT RIB 4, INBOARD FASTNER THIRD ROW AFT OF JOINT. CRACK LENGTH IS 0.821 AND 0.255 AT A DEPTH OF 0.167. INSTALLED DOUBLER PER AIR BUS DRAWING R57340132. CRACK REPAIRED PER ESO 30595 DATED 04/27/2004. (CLOSED) 2L72 4F RTA35EU 20040510001062004051000106NM 2004 5 10 AALA20040500 120040426A5347 SEAT TRACK BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21699AN 27051 TUL CORROSION FOUND ON NUMBER 3 SEAT TRACK AT STATION 676 AND 686 - ANCHORS FOR COFFEE BAR. CORRODED AREA IS FOUR INCHES BY 10 INCHES ON CABIN FLOOR. REPLACED NUMBER THREE SEAT TRACK FROM STATION 640 TO STATION 780. (CLOSED) 2L72 4F RTA2NM 20040510001072004051000107EU 2004 5 10 AALA20040536 120040506A3246 WHEEL AIRBUS300 A300B4605R 3930308EU MLG SEPARATED A AALAO OTHER O OTHER LDLANDING 1 SW2114065 508 JFK T896/06 UPON LANDING AT JFK NR 1 MAIN LANDING GEAR WHEEL SEPARATED FROM AXLE AND DEPARTED AIRCRAFT. TAXIED UNEVENTFULLY TO GATE. AIRCRAFT OUT OF SERVICE FOR DAMAGE ASSESSMENT.--OPEN-- 2L72 4F RTA35EU 20040510001092004051000109SO 2004 5 10 C2XA04SH261 120040503A52701SE1 SWITCH EMB 145 EMB145 3260210SO EMERGENCY EXIT DIRTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE LEFT EMERGENCY EXIT FAILED THE WARNING MESSAGE OPERATIONAL CHECK. MAINTENANCE CLEANED DIRT AND DEBRIS FROM THE EMERGENCY EXIT MICRO SWITCH. MAINTENANCE PERFORMED THE OPERATIONAL CHECK IAW EMB 145 AMM 52-21-00-700-801-A AGAIN. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001102004051000110NM 2004 5 10 AALA20040509 120040430A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21607AM 27058 SFO FIRST CLASS EMERGENCY LIGHTS ON SEATS INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 4EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20040510001112004051000111SO 2004 5 10 C2XA04SH256 120040430A532014521725015 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001122004051000112SO 2004 5 10 C2XA04SH257 120040430A711014576631622 STRUCTURE EMB 145 EMB145LR 3260212SO NR 2 COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712564 145618 SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040510001132004051000113WP 2004 5 10 AALA20040504 120040428A3213 STRUT DOUG DC9 DC982 3022082WP MLG LEAKING A AALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW21432AA 49350 MFE INFLIGHT T1534 AFTER TAKE OFF LANDING GEAR FAILED TO RETRACT. SERVICED NOSE GEAR STRUT PER MAINTENANCE MANUAL 32-21-02. CHECKED FUEL LEVEL AND SERVICED WITH NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001182004051000118NM 2004 5 10 AALA20040511 120040501A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21933AN 30080 BDL EMERGENCY LIGHTS AT SEAT ROWS 12, 13, AND 14 INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHTS AT SEAT ROWS 12, 13, AND 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040510001202004051000120WP 2004 5 10 AALA20040510 120040430A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217528A 49920 DFW RIGHT AND LEFT HAND EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR RIGHT AND LEFT HAND EMERGENCY OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001232004051000123WP 2004 5 10 AALA20040514 120040501A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21582AA 53159 DFW EMERGENCY ESCAPE PATH LIGHTING AT 11D INOPERATIVE. REPLACED SOCKET ASSEMBLY AT SEAT 11D FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001242004051000124WP 2004 5 10 AALA20040516 120040503A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21501AA 49738 PHX AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGER AT STATION 1190R FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001252004051000125NM 2004 5 10 AALA20040512 120040501A3350 SOCKET BOEING777 777223 1385213NM EMERGENCY LIGHTSSHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21766AN 32880 DFW AFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED SHORTED LIGHT SOCKET AT SEAT ROW 4 FOR AFT CABIN EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTT00001SE 20040510001272004051000127SO 2004 5 10 C2XA04SH267 120040506A532014525480003 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001282004051000128NM 2004 5 10 AWXA200400436 120040427A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHTSFAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28802AW107763400 924 PHX - EEL - DURING 8-DAY CHECK WHILE PERFORMING PUSH BUTTON TEST OF EMERGENCY LIGHT SYSTEM RECEIVED MESSAGE "EPSU UNIT FWD L". MAINTENANCE REMOVED AND REPLACED L/H FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040510001292004051000129SO 2004 5 10 C2XA04TY080 120040506A5320 PLATE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-01 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040510001332004051000133SO 2004 5 10 C2XA04SH276 120040509A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001342004051000134NM 2004 5 10 AWXA200400439 120040413A5312651758349 VERTICAL BEAM BOEING737 7373S3 1384711NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT LBL 5.7, WL 176. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH TAPERED SHIMS, A REPAIR WEB & FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 212. 2L72 4F RTA16WE 20040510001352004051000135NM 2004 5 10 AWXA200400440 120040402A53106545409602 PRESSURE PANEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN MAIN DECK PRESSURE WEB AT BS 665, LBL 31. MAINTENANCE CUTOUT DAMAGED SECTION OF PRESSURE WEB AT BS 665, LBL 31; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-51, FIG. 203, DETAIL II. 2L72 4F RTA16WE 20040510001372004051000137NM 2004 5 10 AWXA200400477 120040505A3397BMS13311122 WIRE BOEING757 7572G7 1384963NM EMER LIGHT CONN BURNED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 PHX - EEL - DURING 8-DAY CHECK A BURNED WIRE WAS FOUND AT EMERGENCY LIGHT POWER SUPPLY CONNECTOR D9006 PIN 18, BS 1650. MAINTENANCE SPLICED DAMAGED WIRE AT EMERGENCY LIGHT POWER SUPPLY CONNECTOR D9006 PIN 18, BS 1650, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040510001382004051000138NM 2004 5 10 AWXA200400478 120040505A3397M227591118 WIRE BOEING757 7572S7 1384962NM EMERGENCY LIGHT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - EEL - DURING THRU-FLIGHT INSPECTION FOUND DAMAGED WIRE SPLICED INTO THREE OTHER WIRES THAT TERMINATE IN PINS 1, 7, AND 18 OF AFT GALLEY CENTER OVERHEAD EMERGENCY POWER SUPPLY. MAINTENANCE REPAIRED DAMAGED WIRE AT AFT GALLEY CENTER OVERHEAD EMERGENCY POWER SUPPLY BS 1678; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040510001442004051000144NM 2004 5 10 AWXA200400481 120040405A5755654645262BE PANEL BOEING737 7373S3 1384711NM RT WING SPOILER CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW18163 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON NO. 5 SPOILER PANEL ALONG LEADING EDGE OF LOWER SEAL BETWEEN WBL 71.24 AND WBL 191 R/H. MAINTENANCE REMOVED AND REPLACED NO. 5 SPOILER PANEL IAW AMM 27-62-12, FIG. 401, PG. 1-5. 2L72 4F RTA16WE 20040510001492004051000149NM 2004 5 10 AWXA200400395 120040331A533065529888 SKIN PANEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT BS 958, STR 17 LT. MAINTENANCE PERFORMED HFEC INSPECTION OF CRACKED SKIN AND FOUND CRACK EXTENDED THROUGH DOUBLER AND STRAP. MAINTENANCE CUTOUT DAMAGE IN SKIN, DOUBLER, & STRAP AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT; FABRICATED INNER, MIDDLE, & OUTER PATCHES AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG. 203. 2L72 4F RTA16WE 20040510001502004051000150NM 2004 5 10 AWXA200400396 120040331A575365C3570330 SKIN BOEING737 7373G7 1384595NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK FOUND PREVIOUS REPAIR ON UPPER SURFACE OF RT OUTBOARD FORE FLAP DELAMINATING, 9.5 INCHES FROM INBOARD END WS 290. MAINTENANCE REMOVED DELAMINATED DOUBLER ON UPPER SURFACE OF RT OUTBOARD FORE FLAP; FABRICATED A NEW REPLACEMENT DOUBLER; CLEANED & PREPARED SURFACE; PERFORMED HOT BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 31. 2L72 4F RTA16WE 20040510001512004051000151NM 2004 5 10 AWXA200400397 120040406A53156546881 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM BS 1016, STR 17 RT, RBL 5. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM UPPER CHORD AT BS 1016, FROM LBL 65 TO RBL 65; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW 737-300 SRM 53-00-51, FIG. 202. 2L72 4F RTA16WE 20040510001522004051000152GL 2004 5 10 C2XA04CL048 220040505A720023074862 ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XABA EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SW27111273194 1868 145697 CAE312274 CLE FLIGHT NR 2843 THE CREW REPORTED THE NR 1 ENGINE SHUT DOWN IN FLIGHT. THE SHUT DOWN WAS UNCOMMANDED. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRT TE6CH 20040510001562004051000156SO 2004 5 10 C2XA04SH263 120040504A532014522459003 ANGLE EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE RIGHT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001572004051000157NM 2004 5 10 AWXA200400400 120040410A5311651630087 FRAME BOEING737 7373Y0 1384671NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 3/4 INCH CRACK WAS FOUND IN SIDE FRAME ON AFT SIDE OF BS 178 BULKHEAD AT RBL 63, WL 195. MAINTENANCE REMOVED AND REPLACED CRACKED SIDE FRAME ON AFT SIDE OF BS 178 BULKHEAD AT RBL 63, WL 195 IAW B737-300 SRM 51-40-02, FIG. 8. 2L72 4F RTA16WE 20040510001582004051000158SO 2004 5 10 C2XA04SH264 120040504A532014522460015 STRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE AFT DIGITAL STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001602004051000160SO 2004 5 10 C2XA04SH265 120040504A532013500079001 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AFT OF FRAME 23 AND FORWARD OF FRAME 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001612004051000161EU 2004 5 10 AWXA200400402 120040328A5320D53471124200 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR PLATE, FORWARD SIDE OF FR 70, STR 23 LT. MAINTENANCE REMOVED CORRODED SHEAR PLATE AT FR 70, STR 23 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 53-41-17, FIG. 1. 2L72 4F RTA28NM 20040510001622004051000162NM 2004 5 10 AWXA200400465 120040416A53206517688126 WEB BOEING737 7373S3 1384711NM DOOR SILL CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND IN L-1 DOOR SILL WEB, BS 328, LBL 60. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL WEB AT BS 328, LBL 60; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12. 2L72 4F RTA16WE 20040510001642004051000164SO 2004 5 10 C2XA04SH266 120040506A532014521725613 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE RIGHT HAND FORWARD SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040510001652004051000165SO 2004 5 10 C2XA04TY077 120040505A531514521699003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714516 145323 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE MOUNTING SURFACE FOR PASSENGER SEAT TRACK NR LF1. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02, CPM 51-14-00. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040510001662004051000166SO 2004 5 10 C2XA04CL045 120040503A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO NLG FAULTY A C2XAK NONE O OTHER CLCLIMB 1 SW2715572 145636 CLE FLIGHT NR 2351 THE CREW REPORTED AFTER TAKEOFF THEY HEARD A LOUD RUMBLE FROM THE NOSE AREA. THE GEAR INDICATION SHOWED UP. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS DID NOT RETRACT. THEY REPLACED THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040510001672004051000167NM 2004 5 10 AWXA200400466 120040425A5320654795711 STRAP BOEING737 7373S3 1384711NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (STRAP) BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL STRAP AT BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4B. 2L72 4F RTA16WE 20040510001682004051000168NM 2004 5 10 AWXA200400467 120040420A532065479573 WEB BOEING737 7373S3 1384711NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND UNDER FORWARD INBOARD CORNER OF AFT CARGO COMPARTMENT DOOR SILL WEB BS 794, RBL 30. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT BS 794, RBL 30; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-47688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 9. 2L72 4F RTA16WE 20040510001702004051000170SO 2004 5 10 C2XA04CL049 120040505A527014528237001 SWITCH EMB 145 EMB145XR 3260214SO EMERGENCY EXIT STICKING A C2XAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SW2717146 145746 DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT DOOR SWITCH ACTUATOR WAS STICKING. THE DOOR DID NOT INDICATE OPEN INDICATION ON THE ECIAS WHEN THE DOOR WAS OPENED. MAINTENANCE CLEANED AND LUBED THE RIGHT EMERGENCY EXIT SWITCH ACTUATOR. OPERATIONAL CHECKS WERE GOOD I/A/W 52-75-00. 2L72 4F RT 20040510001722004051000172NM 2004 5 10 AWXA200400404 120040423A2730 SERVO AIRBUSA319 A319132 3930340NM ELEVATOR FAILED A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28809AW17074 1111 EN ROUTE AT FL 220, 340 KTS, FELT A VERY STRONG VIBRATION THROUGHOUT ENTIRE AIRFRAME, VIBRATION STRONGER IN REAR, SLOWED TO 240 KTS & VIBRATION WENT AWAY. REMAINDER OF FLT NORMAL, DID NOT EXCEED 290 KTS. MX PERFORMED ELEVATOR FREE PLAY CHECK IAW T/C 16C55304, YELLOW ELEV SERVO CONTROL FAILED STEP 12, R & R YELLOW ELEV SERVO CONTROL IAW AMM, OPS CHK GOOD. CONFIRMED FAILURE OF ELEV SERVO CONTROL FINDING BEARING IN EYE FLATTENED, INSULATION OF SERVO VALVE AND WIRING OUT OF LIMITS, AND ACCUMULATOR COVER DAMAGED. REPAIRED WIRING AND REPLACED BEARING, SERVO VALVE, AND ACCUMULATOR COVER. REPAIR AND FUNCTIONAL TEST ACCOMPLISHED IAW CMM. 2L72 4F RTA28NM 20040510001732004051000173NM 2004 5 10 AWXA200400405 120040423A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 19 LT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT LENS COVER WILL NOT STAY ATTACHED TO LIGHT ASSEMBLY AT SEAT ROW 19 L/H. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 19 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040510001742004051000174NM 2004 5 10 AWXA200400406 120040424A2560P2070001101 FLASHLIGHT BOEING757 757225 1384959NM ZONE 900 - LAV INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 DURING 4-DAY CHECK FOUND THE MID CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED MID CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040510001752004051000175WP 2004 5 10 04FDEA01007 120040419A5744ARC0502502 HINGE DOUG MD10 MD1010F 3022112WP RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-77340 WINGS RT OUTBD FLAP FLAP INBD HINGE. CORROSION REPAIR (P/N ARC0502-502), COMPLIED WITH EA 8-5740-77340 WINGS RT OUT'BD FLAP FLAP INBD HINGE CORROSION REPAIR P/N ARC 0502-502. 2L73 4F RTA22WE 20040115000652004011500065NM 2004 1 15 04FDEA00118 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040122000372004012200037WP 2004 1 22 JRAA001 120040120A5330 PANEL DOUG DC3 DC3 3021401WP FUSELAGE CORRODED E JRAAO OTHER O OTHER ININSP/MAINT 1 GL11376A 18996 DURING INSPECTION FOUND CORROSION AROUND THE LT TOP NOSE FUSELAGE SKIN PANELS FROM FUSELAGE STATION 49.125 TO 76.5 (COCKPIT ROOF AREA). BOTH LT UPPER SKIN PANELS WERE REMOVED FOR REPLACEMENT. ALSO CENTER WINDOW FRAME WAS REMOVED FOR REPLACEMENT. 2L72 4R A669 20040115000682004011500068NM 2004 1 15 04FDEA00030 120040105A5754 FILLET DOUG MD11 MD11 3023602NM L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 LEFT WING HIGH PERFORMANCE FILLET O/B RIB FOUND CRACKED APPROX 1.5 INCH LENGTH AT UPPER STUD AREA. 2L73 4F RTA22WE 20040115000792004011500079NM 2004 1 15 04FDEA00063 120040107A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 FWD CARGO COMPARTMENT LONGERON 46 RT CORRODED AT STA 6-37. FWD CARGO STA 6-37 LONGERON 46 RT CORROSION LONGERON REMOVED AND REPLACED AS PER DWG NGA6713, SRM 51-33-01 VOL. II, SRM 51-35-01 VOL.II AND SRM 51- 38-01 VOL. II. 2L73 4F RTA22WE 20040115000812004011500081NM 2004 1 15 04FDEA00041 120040105A57537254501 FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING I/B FLAP I/B SIDE LOAD FITTING FOUND CRACKED. LT WING I/B FLAP I/B SIDE LOAD FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. 2L73 4F RTA22WE 20040115000912004011500091NM 2004 1 15 04FDEA00120 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115001012004011500101NM 2004 1 15 04FDEA00061 120040106A5270211FW104 SWITCH BOEING727 727200 138407ENM CARGO DOOR MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25223FE 20935 MAIN CARGO DOOR LIGHT ILLUMINATED WHILE LEVELING AT FL 290. CABIN PRESSURE WAS VERIFIED AT 8.0 PSID & NO OTHER INDICATION OF AN OPENED DOORS NOTED. FOLLOWED ORH PROCEDURES AND RETURNED TO MIA. REMOVED AND REPLACED S9033, ADJUSTED AND TESTED IAW MM 52-70-009-5. MCD OK FOR SERVICE. 2L73 4F RTA3WE 20040115001032004011500103NM 2004 1 15 04FDEA00024 120040104A5753ARC41252 STOP FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING O/B FLAP (FLAP SIDE) STOP FITTING FOUND CRACKED. COMPLIED WITH FEDEX EA 1-5750-74168 - WINGS - OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20040115002002004011500200NM 2004 1 15 04FDEA00052 120040106A5320 CHANNEL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 FLOOR STRUCTURE, HAT SECTION UNDER LAV DOOR IS EXFOLIATED. REMOVED HAT SECTION IAW SRM 51-30-2. FABRICATED NEW HAT SECTION PER SRM 57-10-1 FROM 60-8088/18, B/N 0000519140 & MST0010249. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW HAT SECTION IAW SRM 51-30-2. 2L73 4F RTA3WE 20040120000252004012000025NM 2004 1 20 04FDEA00090 120040109A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 CORROSION (C53-113-01(1) FWD CARGO BAY BS 720 SHEAR TIE CORRODED, BETWEEN STR 27R - 28R WL 149 AFT SIDE OF FRAME. REMOVED CORROSION FROM SHEAR TIE AT BS 720 BETWEEN STR 27R AND 28R WL 149 MATERIAL LOSS WAS .010 DEEP X 1 X 1.25 FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IAW SRM 53-10-1. CUT OFF DAMAGED SHEAR TIE AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 13. 2L73 4F RTA3WE 20040120000292004012000029SO 2004 1 20 C2XA04IA006 120040109A335074441 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 CREW REPORTED THAT THE CABIN EMERGENCY EXIT SIGN WAS INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN AND OPERATIONALLY TESTED THE LIGHTING SYSTEM. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT. 2L72 4F RTT00011AT 20040120000402004012000040NM 2004 1 20 04FDEA00132 120040112A2612AUL7202519 FIRE DETECTOR DOUG MD11 MD11 3023602NM NR 3 ENGINE CHAFED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25579FE 48470 NR 3 ENGINE FIRE WARNING AT T/O 5 MINUTES. WARNING WAS INTERMITTENT. TESTED FIRE WARNING SYSTEM, TEST GOOD. INSPECTED NR 3 ENGINE FIRE LOOPS WIRE HARNESSES, FOUND A LOOP WIRE HARNESS CHAFED AND SHORTING OUT. REMOVED A LOOP WIRE HARNESS. REMOVED A AND B LOOP PYLON DETECTORS PER MM 26-11-03-4. INSTALLED NR 3 ENGINE FIRE DETECTORS "A" AND "B" PYLON LOOPS IAW MM 26-11-03-4. OPS CHECKS AND R-T-S-PASS FOR FDCU 3. NR 3 ENGINE COWLS CLOSED IAW MM 71-10-00. 2L73 4F RTA22WE 20040120000412004012000041NM 2004 1 20 04FDEA00134 120040112A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 CORROSION 1) NR 1 CARGO DOOR CUTOUT FWD FRAME BETWEEN WEB AND I/B CHORD STA 560 RBL 26 WL 166. CORROSION NR 1 CARGO DOOR CUT OUT FWD FRAME BETWEEN WEB AND I/B CHORD STA 560, RBL 26, WL 166, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AREA PER EA 7-5310- 70612. 2L73 4F RTA3WE 20040120000482004012000048NE 2004 1 20 DXTA200400215 220040109A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT SMOKE E DXTAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07353QS 5600530 AFTER LANDING AT ALB, DURING TAXIING TOWER INSTRUCTED FLIGHT CREW TO SHUTDOWN AIRCRAFT AND EVACUATE DUE TO SMOKE COMING OUT FROM LT ENGINE. DISCHARGED BOTH BOTTLES BUT PRELIMINARY INSPECTION SHOWS NO ENGINE FIRE. PERFORMED ENGINE RUNS AND CHECKED FOR OIL LEAKS, NO DEFECTS NOTED, SERVICED ENGINE OIL IAW CESSNA560 MM CHAPTER 12-11-02. PERFORMED GROUND RUNS AT 72 PERCENT N1 FOR 1 HOUR, NO OIL CONSUMPTION NOTED, ENGINE PRODUCED N1 IAW CESSNA 560 AFM. 2L72 4F4 FRTA22CE E25EA 20040120000622004012000062CE 2004 1 20 GLBA20030525 120040105A5610 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03100UX UE100 FO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD. 2L72 4T RTA24CE 20040120000662004012000066NM 2004 1 20 04FDEA00001 120040101A5754ARH0518501 STRUT DOUG MD11 MD11 3023602NM ZONE 100 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 INBOARD SLAT MECHANICAL RT STRUT ASSY BEARING FOUND MIGRATED. I/B SLAT MECHANICAL RT STRUT ASSY REMOVED & REPLACED AS PER CMM 27- 03-20. 2L73 4F RTA22WE 20040120000672004012000067NM 2004 1 20 04FDEA00032 120040105A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 SKIN PILLOWING STA 1110 - 1130 STR 28L. REMOVED CORROSION FROM SKIN BS 1115 UNDER STR 28L AREA 1X2X.025 FROM ORIGINAL .052 FOUND OUT OF LIMITS PER SRM 53-30-1. REMOVED CORROSION FROM STR 28L AREA 1X1 X 100 PERCENT MATERIAL LOSS AT BS 1115 FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED SKIN PER SRM 53-30-03 FIG 3. REPAIRED STRINGER 28L PER SRM 53-10-3 FIG 1 2L73 4F RTA3WE 20040115000442004011500044NM 2004 1 15 P9RA20040001 120040112A33501000677 LIGHT BOEING727 7272J4 1384006NM PWA JT8 JT8D* NE COCKPIT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11288SC 20765 EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. IN FLIGHT COMPARTMENT IAW BMM 33-50-01. 2L73 4F4 FRTA3WE E2EA 20040115000732004011500073NM 2004 1 15 04FDEA00096 120040112A5753 SUPPORT DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE. RT OTBD FLAP, UP STOP RIB SUPPORT ISLAND REPAIRED AS PER EA 1-5750-74278, OUTBOARD TRAILING EDGE FLAPS - SECONDARY UP STOP - REPAIR. 2L73 4F RTA22WE 20040115000752004011500075NM 2004 1 15 04FDEA00098 120040112A5744 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. RT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115000762004011500076NM 2004 1 15 04FDEA00131 120040112A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP VANE TEE FITTING NR 5 (COUNTING FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OTBD FLAP VANE TEE FITTING NR 5 REPAIRED AS PER EA 1-5750-74291, WINGS - LT AND RT OUTBOARD FLAP - NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040115000802004011500080NM 2004 1 15 04FDEA00042 120040106A5320AFA7237501 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CTR CARGO - BETWEEN BS 1801-1821, RT 40 LONGERON SPLICE CRACKED. COMPLIED WITH FEDEX EA 1-5310-74180 - FUSELAGE- LONGERON SPLICE AT F.S. 1810, LONGERON 40 RT - CORROSION REPAIR 2L73 4F RTA22WE 20040115001882004011500188NM 2004 1 15 04FDEA00035 120040105A5230FX69506772 BRACKET BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 FWD COUNTER BALANCE ASSY, THE AFT MOUNT BRACKET IS CRACKED (FOR THE DOOR). REMOVED AND REPLACED MOUNT BRACKET IAW SRM 51-30-2. FABRICATED NEW MOUNT BRACKET ON TRAVELER T2/353468 PER DWG 69-50677, P/N FX 69-50677-2. 2L73 4F RTA3WE 20040115001922004011500192NM 2004 1 15 04FDEA00114 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES. LT OTBD FLAP INBD HINGE (FLAP SIDE), INBD ACTUATOR LUG SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115001942004011500194NM 2004 1 15 04FDEA00099 120040112A5730 SKIN DOUG MD11 MD11 3023602NM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235, RIGHT X = 30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RH X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION 2L73 4F RTA22WE 20040115001972004011500197NM 2004 1 15 04FDEA00055 120040106A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 MAIN CABIN SEAT TRACK GOUGED & DAMAGED AT FS 910 RBL 62. GOUGE IN TRACK OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED BAD SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW TRACK SECTION ON TRAVELER T2/394338. INSTALLED NEW TRACK SECTION RBL 62 STA 870 TO 960 IAW SRM 51-30-2. 2L73 4F RTA3WE 20040115001992004011500199NM 2004 1 15 04FDEA00053 120040106A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 MAIN CABIN SEAT TRACK GOUGED & DAMAGED AT FS 910 RBL 62. GOUGE IN TRACK OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED BAD SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW TRACK SECTION ON TRAVELER T2/394338. INSTALLED NEW TRACK SECTION RBL 62 STA 870 TO 960 IAW SRM 51-30-2. 2L73 4F RTA3WE 20040115002102004011500210NM 2004 1 15 04FDEA00033 120040105A552165174447 RIB BOEING727 727100 1384036NM ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25193FE 19142 STABILIZER- ELEVATOR HINGE SUPPORT RIB INSPECTION S/B 727-55A0091, COMPLY WITH EO 7-5510-7-5001 REV B1 POS PT2. 2L73 4F RTA3WE 20040115002122004011500212NM 2004 1 15 04FDEA00060 120040106A5270 SWITCH BOEING727 727100 1384036NM CARGO DOOR DEFECTIVE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25198FE 19154 MAIN CARGO DOOR WARNING LIGHT ILLUMINATED PASSING FL 250, 315 KIAS, CABIN ALTITUDE SHOWED 2000 FEET COMPLETED RED TABS AND LIGHT REMAINED ON. FOUND DOOR WARNING SWITCH SH009 OUT OF ADJUSTMENT, ADJUSTED SWITCH PER M/M 52-70-009-5. ALSO FOUND FWD DOOR WARNING SWITCH SH010 BOTTOMING OUT BEFORE MAKING CONTACT, REQUIRES NEW SWITCH REMOVED AND REPLACED LATCH SWITCH PER M/M 52-70-009-5. PRESSURIZED A/C TO 4 PSID PER M/M 05-51-101-6 WITH NO DEFECTS NOTED. 2L73 4F RTA3WE 20040115002132004011500213NM 2004 1 15 04FDEA00085 120040108A5320 WEB BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 WEB CRACKED BETWEEN STA 1070 & 1090, STR 25L. REMOVED WEB IAW SRM 51-30-2, FABRICATED NEW WEB ANGLE IAW SRM 51-20-1. LOCATED AND DRILLED IAW SRM 51-30-2. INSTALLED WEB ANGLE IAW SRM 51-30-2. 2L73 4F RTA3WE 20040115002142004011500214NM 2004 1 15 04FDEA00086 120040109A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT CENTER CARGO NR 45 LONGERON SPLICE FOUND CRACKED BETWEEN STA 1661 TO 1681. CRACKED NR 45 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 1661 TO 1681 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING AFA7113 AND INSTALLED AS PER SRM 51-33-01, VOL.II. 2L73 4F RTA22WE 20040115002152004011500215WP 2004 1 15 04FDEA00049 120040106A5242115AZ FRAME DOUG DC10 DC1010 3022110WP E/E BAY DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 THE LOWER INNER FRAME OF THE AFT AVIONICS COMPARTMENT DOOR 115AZ HAS SEVER CORROSION. REMOVED DOOR IAW M/M 52-41-01-2, REMOVED CORRODED PARTS IAW SRM 51-31-01, NEW CAP ANGLES FABBED ON MAE TRAVLER T4/392156 AND T2/392154. SPLICE FABBED ON T2/392153, INTERCOSTALS FABBED ON T2/392148 AND T2/392152. INSTALLED NEW PARTS IAW SRM 51-31-01. INSTALLED DOOR IAW M/M 52-41-01-2. 2L73 4F A22WE 20040120000272004012000027SO 2004 1 20 C2XA04SD001 120040107A243232845001 BATTERY EMB 145 EMB145XR SO MASTER ARCED A C2XAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2712135817 718 SMOKE ODOR IN COCKPIT. A/C ENGINES WERE RAN WITH PACKS OPERATING. COULD NOT DUPLICATE THE SMOKE ODOR. UPON FURTHER INVESTIGATION, BATTERY TERMINAL SHOWED SIGNS OF ARCING. BATTERY REPLACED AND OPERATIONALLY CHECKED GOOD WITH NO REPEAT OF THE SMOKE ODOR IN THE COCKPIT. A/C FERRIED TO CLE WHERE FURTHER INSPECTION REVEALED THE NR 1 WINDSHIELD TERMINAL STRIP WAS BURNED. WINDSHIELD WAS REPLACED, TEST FLIGHT CHECKED GOOD. 2L72 4F RT 20040120000382004012000038CE 2004 1 20 DXTA200400211 120040101A32307093011 CONTROL MODULE CESSNA650 650 2076802CE MLG FAILED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07785QS3521 6507085 AFTER TAKE-OFF GEAR COULD NOT RETRACT GEAR WHEN GEAR LEVER WAS PUT IN THE (UP) POSITION, ACCOMPLISHED AIR TURN BACK. TROUBLESHOT AND FOUND LANDING GEAR CONTROL FAULTY, REMOVED AND REPLACED LANDING GEAR CONTROL ASSEMBLY IAW 650 MM CHAPTER 32-30-01. SYSTEM OPS CHECKED GOOD. 2L72 4F A9NM 20040120000392004012000039NM 2004 1 20 04FDEA00148 120040114A5730 SKIN BOEING727 727200 138407ENM LT WING DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 DENT ON LT WING FIXED L/E SKIN AT NR 3 SLAT TAI DUCT. DENT ON L/W FIXED L/E SKIN AT NR 3 SLAT TAI DUCT, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-1. REPAIRED DENT IAW SRM 57-30-4 PG 2 2L73 4F RTA3WE 20040120000462004012000046EU 2004 1 20 04FDEA00062 120040107A78303205225 PILOT VALVE AIRBUS300 A300F4605R 3930327EU NR 1 ENGINE FAILED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25681FE 799 ON TAKEOF ROLL WHEN PWR ADVANCED ABOVE 60 PERCENT N1 RECEIVED NR 1 ENG REVERSE PRESSURIZED ECAM. ABORTED T/O ROLL RETURNED TO GATE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A MEL 78-30-01-A: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND REPLACED NBR 1 ENG DIRECTIONAL PILOT VALVE. R & R NR 1 ENGINE. RAN ENGINE TO 60 PERCENT TO VERIFY NO "ECAM" ALERT ON T/R. PER A300-600 JRH. OPS. CHECK GOOD. 2L72 4F RTA35EU 20040120000612004012000061CE 2004 1 20 GLBA20030528 120040108A7714 CONNECTOR BEECH 1900 1900D 1154162CE TRANSDUSER DIRTY A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03255GL UE255 104 PERCENT, N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE. 2L72 4T RTA24CE 20040121000542004012100054EA 2004 1 21 A6WA200440003 120040106A2721272613 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA RUDDER FAILED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL31433AW8920 7289 RUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M) 2L72 4F RTA21EA 20040121001122004012100112NM 2004 1 21 04FDEA00008 120040103A5753ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR O/B BORE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, TITLE : TE DEVICES. LT O/B FLAP. O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040121001142004012100114NM 2004 1 21 04FDEA00010 120040103A5710ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING O/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, WINGS - TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040115001812004011500181NM 2004 1 15 AALA20040060 120040110A324059130032 COUPLING BOEING777 777223 1385213NM NR 10 BRAKE LEAKING A AALAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SW21791AN 30254 LHR T101/10 WHILE TAXIING NUMBER 10 BRAKE LOCKED UP. AIRCRAFT WAS TOWED TO GATE AFTER MAINTENANCE RELEASED LOCK. REPLACED NUMBER 10 MAIN WHEEL AND BRAKE ASSEMBLIES. ACCOMPLISHED AXLE INSPECTION, NO DAMAGE. FOUND BRAKE QUICK RELEASE COUPLING LEAKING. REPLACED BRAKE QUICK RELEASE COUPLING, SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040115002162004011500216NM 2004 1 15 04FDEA00047 120040106A5753ARC199114 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75221, TITLE : WINGS - TE & TE DEVICES - RT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040115002172004011500217NM 2004 1 15 04FDEA00046 120040106A5753ARC199114 BUSHING DOUG MD11 MD11 3023602NM T/E FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR LUG I/B SIDE BUSHING FOUND LOOSE. 2L73 4F RTA22WE 20040115002182004011500218NM 2004 1 15 04FDEA00115 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. LT OTBD FLAP INBD HINGE (FLAP SIDE), OUTBD ACTUATOR LUG BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040115002192004011500219NM 2004 1 15 04FDEA00123 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040120000472004012000047NE 2004 1 20 UPS04841703 220040109A7532 BLEED VALVE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 2 ENGINE INOPERATIVE A IPXAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO01813UP 46059 NR 2 AND NR 3 ENGINES AT IDLE DUE TO COMPRESSOR STALLS ENG NR3 FOUND CRACKS GURNS & MISSING MATERIAL ON STATOR OF LPT ACCESS THRU 517. BOROSCOPE 72-00-00 P 620, 72-31-00 72-54. ENGINE NR 2 COMPLIED WITH VISUAL & BOROSCOPE INSPECTION OF NR 2 ENG POST STALL, NR 2 ENG MASTER BLEED VALVE FEED BACK ROD BENT & BLEED VALVE ACTUATOR ARM BROKEN R & R MASTER BLEED VALVE PER MM C/W CHECK SYS ACTUATOR SYS TEST PER MM. NORMAL. LEAK CK GROUND IDLE & FLIGHT IDLE TEST & P WR ASSURANCE TEST PERFORMED IAW MM. TESTED GOOD. (CLOSED) 2L74 4F4 FRT4A25 E2GL 20040120000602004012000060CE 2004 1 20 GLBA20030527 120040107A2750 FLAP BEECH 1900 1900D 1154162CE STUCK A GLBAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM03154GL UE154 FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION 2L72 4T RTA24CE 20040122000162004012200016NM 2004 1 22 04FDEA00045 120040106A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING FOUND LOOSE. LT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT LUG I/B SIDE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES. LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040122000172004012200017NM 2004 1 22 04FDEA00044 120040106A5753ARC198413 HINGE DOUG MD11 MD11 3023602NM ZONE 500 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. LT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE LOOSE BUSHING REMOVED & REPLACED WITH NEW BUSHING AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES. LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040122000182004012200018NM 2004 1 22 04FDEA00039 120040105A5753NRC6055509 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178, TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2L73 4F RTA22WE 20040122000212004012200021NM 2004 1 22 DXTA200400214 120040106A3260803682 PROXIMITY SWITCH AMD FALC50FALCON2000 2730170NM MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07245QS 145 DURING APPROACH, PLACED GEAR HANDLE IN THE DOWN POSITION AND GOT GEAR UNSAFE LIGHTS. RECYCLED GEAR HANDLE AND GOT ONE GREEN LIGHT AND 3 RED. FOLLOWED EMERGENCY GEAR EXTENSION AND LANDED SAFELY. FOUND LANDING GEAR DOOR PROX SWITCHES INOPERATIVE, REMOVED AND REPLACED BOTH L/H AND R/H LANDING GEAR DOOR PROX SWITCHES. JACKED AIRCRAFT AND PERFORMED NUMEROUS LANDING GEAR FUNCTIONAL TEST ALL CHECKED SATISFACTORY IAW FALCON 2000 MM MAINTENANCE PROCEDURE 32-300. 2K73 4F RTA50NM 20040122000232004012200023NM 2004 1 22 UPS04641690 120040106A7930 WARNING SYSTEM BOEING767 76734AF 1385212NM GE CF6 CF680C2B7 NE LT ENGINE OIL MALFUNCTIONED A IPXAJA DUMP FUEL UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 SO01303UP 27241 INSPECTION TYPE: ETOP ATB, ABOUT 30 MIN OUT OF ANC, LT ENG OIL QTY DROPPING. A/C RETURNED TO ANC. NO EMERGENCY DECLARED. INSPECTED ENGINE OIL SYSTEM, DRAINED OIL TANK & RESERVICED WITH 23 QTS PER FIM 79-11-00 FIG 107. RAN ENG, NO DEFECTS NOTED. OK FOR SERVICE. 2L72 4F4 FRTA1NM E13NE 20040122000242004012200024NM 2004 1 22 UPS04641691 120040107A7920 OIL SYSTEM BOEING767 76734AF 1385212NM LT ENGINE LOW A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01303UP 27241 LT ENGINE OIL QTY DROPPED THRU 38 (WENT AS LOW AS 17). OIL TEMP WAS CLIMBING THROUGH 130. R/R MAIN LUBE FILTER AND TANK PRESS VALVE. NO HELP. REPLACED LT ENGINE PER TC 6002 LEAK AND OPS CHECK NORMAL. 2L72 4F RTA1NM 20040122000272004012200027EU 2004 1 22 AALA20040029 120040106A27202VA3925G1 ACTUATOR AIRBUS300 A300B4605R 3930308EU RUDDER MALFUNCTIONED A AALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW2141063 506 JFK DURING CLIMB AIRCRAFT STARTED TO YAW BACK AND FORTH. ECAM SHOWED SMALL RUDDER DEFLECTION. TRIED SWITCHING AUTOPILOTS; NO CHANGE. ACCOMPLISHED FDR DOWNLOAD, BILL OF WORK TO REPLACE NR1 YAW DAMP ACTUATOR, 2VA3925G1 AND NR 1 AUTOPILOT ACTUATOR, OPERATIONAL TEST AND LAMP TEST COMPLETE ON NR 1 AUTOPILOT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA35EU 20040122000282004012200028 2004 1 22 249TR0002AA 420040104A2210 COMPUTER BOEING737 7372K5 138448XNM AUTOPILOT MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05249TR 22598 HEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED PER MM 22-11-01. REPLACED BATTERY PER MM 24-31-11. TEST OK. 2L72 4F RTA16WE 20040122000292004012200029NM 2004 1 22 04FDEA00066 120040107A5350AKC75393 FRAME DOUG MD11 MD11 3023602NM ZONE 200 SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 FWD TAILCONE, LAST FRAME FOUND WITH SCRATCHES. COMPLIED WITH FEDEX EA 1-5300-74174 - FUSELAGE, EXTENDED TAILCONE, FORWARD SECTION, FRAME REPAIR. 2L73 4F RTA22WE 20040122000302004012200030NM 2004 1 22 04FDEA00089 120040109A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 CORROSION IN FWD CARGO BAY BS 640 SHEAR TIE CORRODED BETWEEN STR 27R - 26R WL 149 AFT SIDE OF FRAME. REMOVED CORROSION FROM SHEAR TIE AT BS 640 BETWEEN STR 27R AND 26R. MATERIAL LOSS WAS .017 DEEP X 1 X 4 INCHES FROM AN ORIGINAL THICKNESS OF .058 AND IS OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-30-2. 2L73 4F RTA3WE 20040122000322004012200032CE 2004 1 22 K5LA620JS 120040102A561010138402523 WINDSHIELD BEECH 200 A200 1152921CE PWA PT6 PT6A41 52043EA COCKPIT CRACKED E K5LAA UNSCHED LANDING O OTHER CLCLIMB 1 EA05636B 590 BC61 CLIMBING THROUGH 14000 FT IN THE CLOUDS WITH W/S HEAT ON, OAT-5C PILOTS WINDSHIELD OUTER PLY CRACKED ACROSS ENTIRE WINDSHIELD. RETURNED TO AIRPORT AND LANDED. REPLACED WINDSHIELD, NO OTHER DAMAGE NOTED. 1L72 4T4 T A24CE E4EA 20040122001402004012200140NM 2004 1 22 COOSDR030057 120040101A57116550821142 SPAR BOEING737 737200 1384453NM RT WING CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, REAR SPAR LOWER CHORD SECTION, FROM WBL 113 INCHES TO WBL 130 INCH OB SPLICE PN 65-50821-142. 2L72 4F A16WE 20040123000262004012300026NM 2004 1 23 COOSDR030056 120040101A551065475284 WEB BOEING737 737200 1384453NM HORIZONTAL STAB WORN W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT HORIZONTAL STABILIZER TRAILING EDGE, HINGE RIB, WEB WITH WEAR. 2L72 4F A16WE 20040123000302004012300030NM 2004 1 23 COOSDR030052 120040101A5414 SKIN BOEING737 737200 1384453NM NR 2 NACELLE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 NR 2 ENGINE OB COWLING EXTERNAL SKIN CORRODED. 2L72 4F A16WE 20040121000532004012100053NE 2004 1 21 A6WA200440002 220040105A7230 BLADE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT ENGINE NICKED A A6WAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL31459AW 7863 873916 AFTER TAKEOFF RT ENGINE VIBRATION WENT TO 3.9, FLET AIRFRAME VIBRATION, WITH THRUST REDUCED VIBRATION INDICATION REDUCED TO GREEN RANGE. AIR RETURN, INSPECTED FAN IAW 72-20-00. BLENDED NICKS FROM SEVERAL BLADES IAW AMM TASK 72-20-00-300-801, ALL MINOR BLENDING. GROUND RAN CHECKED GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20040122000192004012200019NM 2004 1 22 04FDEA00038 120040105A5753NRC6055509 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT I/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178, TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2L73 4F RTA22WE 20040122000222004012200022CE 2004 1 22 DXTA200400213 120040105A7830 THRUST REVERSER CESSNA560 560XL 2076702CE LT & RT ENGINE LACK OF LUBE E DXTAO OTHER WEJINADEQUATE Q C VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL07675QS 5605275 DURING FLIGHT, THE LT THRUST REVERSER LIGHT CAME ON AND A SLIGHT VIBRATION FELT FROM THE LT SIDE OF AIRPLANE. COMPLIED WITH NORMAL CHECKLIST AND EMERGENCY STOW PROCEDURE, LIGHT WENT OUT ALONG WITH VIBRATION. REMOVED LT & RT ENGINE INBOARD & OUTBOARD STANGS, PERFORMED VISUAL INSPECTION TO THE THRUST REVERSER SYSTEM, NOTICED SYSTEM IS DRY. LUBED BOTH TR’S AND ADJUSTED LT STOW SWITCH IAW CESSNA 560XL MM CHAPTER 78-31-00. SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20040123000572004012300057NM 2004 1 23 COOSDR030053 120040101A5755 SKIN BOEING737 737200 1384453NM RT WING SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW MA358 20258 RT WING, IB GROUND SPOILER (PN 65-79952-6) SN MA358, DELAMINATED. 2L72 4F A16WE 20040123000762004012300076NM 2004 1 23 COOSDR030061 120040101A5753 CARRIAGE BOEING737 737200 1384453NM TE FLAPS DAMAGED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 LT AND RT INBOARD MIDFLAP (PN 6571902-11/12) CARRIAGE ASSY PN 65-52246-9/10 AND 11/12 DAMAGED. 2L72 4F A16WE 20040126000042004012600004 2004 1 26 BAQA091862 420040108A3425656767 COMPENSATOR BOLKMS117 BK117A3 5626015EU COCKPIT HSI CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03952CJ 7052 BASE OF HSI COMPENSATOR IS CRACKED REPLACED WITH SERVICEABLE UNIT (S/N 17507). 1G72 3U H13EU 20040126000052004012600005SW 2004 1 26 ALGA091973 120040113A6520206033426001 MOUNT BELL 206 206L1 1182107SW TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 AL033192P19325 45780 TAIL ROTOR 90 DEGREE GEARBOX MOUNT. FITTING AFT LT ATTACH POINT HOLE HAS CRACK EMITTING FROM IT FORWARD & AFT. CRACK RUNS FORWARD APPROXIMATELY 1.5 INCHES. 1G71 3U H2SW 20040126000092004012600009CE 2004 1 26 BAQA092068 120040114A3000606534802 TIMER LEAR 55 55LEAR 5170702CE DE ICE SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11508 092 DE ICE TIMER WILL NOT HEAT RT PARTING ELEMENT. REPLACED WITH SERVICEABLE UNIT. 01/16/2004 2L72 4F A10CE 20040126000112004012600011EU 2004 1 26 BAQA091750 120040108A2822P94C16602 PUMP AEROSPAS355 AS355F1 8680810EU FUEL BOOST FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03652PM 5179 FUEL BOOST PUMP PRODUCING INSUFFICIENT PRESSURE. UNIT FAILED OUT OF BOX, REPLACED WITH SERVICEABLE UNIT. 01/19/2004 1G72 3U H11EU 20040126000142004012600014EU 2004 1 26 BAQA091965 120040113A6330L633M2010104A001MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135MF268 0281 Z-ARIS MOUNT LEAKING AFTER 267.8 HOURS REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040126000192004012600019EU 2004 1 26 BAQA091988 120040109A6330L633M2010104 MOUNT UROCOPEC135 EC135P2 EU M/R GEARBOX LEAKING B BAQAO OTHER KE FLUID LOSS VIBRATION/BUFFET NRNOT REPORTED 1 EA03584AE69 0288 MAIN ROTOR GEARBOX MOUNT LEAKING AND HAS VIBRATION. REPLACED WITH SERVICEABLE UNIT. 01/14/2004 1G72 3U H88EU 20040126000202004012600020EU 2004 1 26 BAQA091989 120040109A6330L633M2010101A003MOUNT UROCOPEC135 EC135P2 EU M/R GEARBOX LEAKING B BAQAO OTHER KE FLUID LOSS VIBRATION/BUFFET NRNOT REPORTED 1 EA03584AE69 0288 MAIN ROTOR GEARBOX MOUNT IS LEAKING AND HAS VIBRATION. REPLACED WITH SERVICEABLE UNITS. 1G72 3U H88EU 20040126000212004012600021EU 2004 1 26 BAQA091994 120040114A3150L316M30C1003 CDU UROCOPEC135 EC135P1 8680990EU COCKPIT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF356 0140 CENTRAL DISPLAY UNIT HAS LED LIGHTS BAD LINES THREW DISPLAY. REMOVED AND REPLACED WITH A SERVICEABLE UNIT. 1G72 3U O H88EU 20040126000222004012600022EU 2004 1 26 BAQA091996 120040104A6330L633M2010102A004MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH2671 0131 Z-ARIS FAILED. REPLACED WITH SERVICEABLE UNIT. 01/15/2004 1G72 3U H88EU 20040126000242004012600024 2004 1 26 BAQA091999 420040112A342455508340N5L INDICATOR UROCOPEC135 EC135T1 5620026EU TURN AND SLIP MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH384 0273 TURN AND SLIP INDICATOR BACKLIGHTING INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040121001132004012100113NM 2004 1 21 04FDEA00009 120040103A5753ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE) ACTUATOR I/B BORE HOLE FOUND CORROSION. CORROSION ON LT WING O/B FLAP OB HINGE (FLAP SIDE) ACTUATOR I/B BORE HOLE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75220, : TE & TE DEVICES - LT O/B FLAP / O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040122000132004012200013NM 2004 1 22 04FDEA00029 120040105A5512ALC81031 PANEL DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 HORIZONTAL STABILIZER LT UPPER AFT PLANK 35 BARREL NUT BORE CORROSIONS FOUND EXCEED EO 1-5510-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-7522, HORIZONTAL STAB - BARREL NUT BORE REWORK / REPAIR / A.D. 2003-22-08. 2L73 4F RTA22WE 20040122000312004012200031EA 2004 1 22 COMA0470005 120040107A3310 LIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT FIRE A COMAO OTHER AH FLAME/FIRE ELECT. POWER LOSS-50 PC APAPPROACH 1 SO01398CA 10112 COPILOTS FWD FLOOD LIGHT CAUGHT ON FIRE. DEACTIVATED BY PULLING CIRCUIT BREAKER AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040122000332004012200033NM 2004 1 22 AWXA200400035 120040111A3097E0488HL WIRE AIRBUSA319 A319132 3930340NM ZONE 210 ARCED A AWXAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 WP28802AW 924 ON CLIMBOUT, ECAM INDICATED RT WINDOW HEAT ACCOMPANIED BY ARCING COMING FROM THE FIRST OFFICERS RT SLIDING WINDOW AREA, TURNED BACK TO RDU AND LANDED WITHOUT FURTHER INCIDENT. MAINT FOUND RT SLIDING WINDOW ELECTRICAL CORD SHORTED TO GROUND WHERE CORD COMES OUT FROM LOWER SIDE OF CONDUIT AT SHELF NEAR FIRST OFFICERS ARM REST. ISSUED MEL, C-1, RT SLIDING WINDOW HEAT INOP. DISCONNECTED CONNECTOR (9GD2) FOR RT SLIDING WINDOW AND PERFORMED OPS TEST OF WINDOW HEAT FOR RT WINDSHIELD AND FIXED WINDOWS, TEST WAS GOOD. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS SLIDING WINDOW, WINDOW HEAT WIRE HARNESS, OPERATIONAL TEST WAS GOOD IAW AMM 30-42-00. 2L72 4F RTA28NM 20040122000342004012200034NE 2004 1 22 RAIA00401005 220040104A732010200010 PROBE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE TT2 MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03571HK 41090 0001 RT IEC CAPTION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED TT2 PROBE. 2L72 4T4 TRTA41NM E18NE 20040123000682004012300068WP 2004 1 23 COOSDR030063 120040101A53205946034101 SUPPORT BRACKET DOUG DC9 DC982 3022082WP AFT CARGO BAY CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23135NJ 49440 AFT CARGO COMPARTMENT SUPPORT BRACKET WITH CRACK AT Y: STA 1211 BETWEEN LONG 24L AND 25L. 2L72 4F A6WE 20040126000062004012600006NE 2004 1 26 BAQA091980 220040113A74129550177760 EXCITER AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE ENGINE INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109DU1090 11503 EXCITER INTERMITTENT DURING STARTS CAUSING TORCHING DURING STARTS. REPLACED WITH SERVICEABLE UNIT 01/14/2004 1G72 3U3 URTH7EU E42NE 20040126000072004012600007EU 2004 1 26 BAQA091931 120040109A243523032022 STARTER GEN BOLKMS117 BK117A3 5626015EU DC SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LG384 7032 STARTER GENERATOR WILL NOT COME ONLINE. REPLACED WITH SERVICEABLE UNIT. 01/15/2004 1G72 3U H13EU 20040126000102004012600010EU 2004 1 26 BAQA092080 120040110A2422SPS1307A INVERTER AEROSPAS365 AS365N2 8680815EU ELECTRICAL FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 INVERTER INOPERATIVE. FAILED OUT OF THE BOX. REPLACED WITH SERVICEABLE UNIT. 01/19/2004 1G72 3U RTH10EU 20040126000152004012600015EU 2004 1 26 BAQA091966 120040116A6330L633M2010101A004MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135MF268 0281 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 01/16/2004 1G72 3U H88EU 20040126000162004012600016EU 2004 1 26 BAQA091967 120040116A6330L633M2010101A004MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF268 0281 MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 01/16/2004 1G72 3U H88EU 20040122000102004012200010NM 2004 1 22 04FDEA00017 120040103A5720ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE FOUND CORROSION. CORROSION ON LT WING O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT BORE I/B SIDE SURFACE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, TE & TE DEVICES - LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040122000112004012200011NM 2004 1 22 04FDEA00018 120040103A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. CORROSION ON LH WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE REMOVED & FOUND WITHIN LIMITS AS PER FEDEX EA 1-5750-75218, LT O/B FLAP / I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040122000122004012200012NM 2004 1 22 04FDEA00026 120040105A5753NRC6055510 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING I/B FLAP O/B HINGE (FLAP SIDE) PIVOT O/B BORE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-74178 - WINGS - TRAILING EDGE FLAPS - PIVOT BORE CORROSION - REPAIR 2L73 4F RTA22WE 20040122000152004012200015 2004 1 22 04FDEA00048 420040106A2565D31073101 SLIDE BOEING727 727200 138407ENM CABIN MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25236FE 21330 UPON INCOMING INSPECTION FOUND ESCAPE SLIDE STILL HAD SAFETY STRAP FOR SHIPPING INSTALLED. REMOVED SAFETY STRAP PER FED EX M.M. 25-60-015-2 2L73 4F RTA3WE 20040122000252004012200025NM 2004 1 22 UPS04M41692 120040106A2420 BUSS DOUG MD11 MD11F 3023600NM NR 1 FAILED A IPXABA EMER. DESCENT UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO01270UP DURING FLT AT FL360 A/C BUS 1 FAILED & NUMEROUS C/B BEGAN TO POP. THE FOLLOWING ITEMS ALSO FAILED: NR 2 DU, CAPTS NAV GUIDANCE, NR 3 DU DISPLAYED INOPERATIVE FAIL, GROSS WEIGHT, FUEL QTY, CG X'D OUT, EPR NR 1; 2 INDICATORS OUT, UNABLE TO GET NR 1 TO OP STBY, F/F NR 1 OUT, OIL PRES NR 1 OUT, OIL QTY NR 3 OUT, NR 1 COMM FAILED, ACARS FAILED, TAIL R PUMP LO, TANK NR 1 FWD PUMP OFF, ATC 1 TRANSPONDER INOP, FUEL CONFIG, AUTO SLAT FAIL, NO AUTOL AND, AUX IRU FAILED, IRU AUX ON BATT, IRU BATT LO LT ON, AVIONIC FLOW LT ILLUMINATED, FUEL QTY ALERTS ON. REPLACED RCCB B1-174 PER MM 24-50-01. OPS NORMAL. THIS CLEARS ALL FAULTS 2L73 4F RTA22WE 20040122000262004012200026NM 2004 1 22 04FDEA00058 120040106A5753ARC198414 HINGE DOUG MD11 MD11 3023602NM ZONE 600 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE) ACTUATOR LUG O/B SIDE BUSHING FOUND LOOSE. TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2L73 4F RTA22WE 20040122000352004012200035NM 2004 1 22 DHL2004747001 120040116A7711JG298A4 INDICATOR BOEING727 727224 1384076NM NR 3 EPR INOPERATIVE A DHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO01747DH 22253 NR 3 EPR INDICATOR INOPERATIVE. WEIGHT: 156000, AIRSPEED: 40 KNOTS, AND OAT -22 C. DEFERRED NR 3 EPR PER MEL 77-1-1 CAT-A DMI 15408. 2L73 4F A3WE 20040123000622004012300062SO 2004 1 23 AIHR109C 220040109A8530711 CYLINDER CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO ENGINE CRACKED B AIHRO OTHER O OTHER NRNOT REPORTED 1 GL11468TW 923 414A0071 813607R PILOT REPORTED VIBRATION AFTER 2 HRS INTO FLIGHT, COULD NOT DETERMINE ORIGIN OF VIBRATION. ANOTHER PILOT PERFORMED GROUND RUN-UP AND COULD NOT DETECT VIBRATION. PILOT FLEW AIRCRAFT AND AFTER 15 MINUTES A VIBRATION OCCURRED, PILOT NARROWED VIBRATION ORIGIN TO LT ENGINE AND PERCEIVED A RT MAGNETO PROBLEM. AFTER LANDING, A MECHANIC RAN UP AIRCRAFT AND FOUND THE RT MAG ON THE LT ENGINE ROUGH. AFTER UNCOILING THE LT ENGINE FOUND NR 2 CYLINDER HAD SEPARATED FROM BARREL. ALSO FOUND ENG WOULD NOT IDLE BELOW 1400 RPM. (PTRS NR GL11200406248) 1L72 3O3 O A7CE E8CE 20040123000672004012300067NM 2004 1 23 COOSDR030060 120040101A5753ASBT33101 THRUST BEARING BOEING737 737200 1384453NM RT AND LT WING DAMAGED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT AND LT WING, OB MIDFLAP THRUST BEARING DAMAGED. 2L72 4F A16WE 20040126000132004012600013EU 2004 1 26 BAQA091964 120040113A6330L633M2010104A004MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135MF268 0281 Z-ARIS MOUNT IS LEAKING AFTER 267.8 HOURS. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H88EU 20040123000522004012300052NM 2004 1 23 COOSDR030059 120040101A57206550821144 SPLICE BOEING737 737200 1384453NM RT WING CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, REAR SPAR LOWER CHORD SECTION, OUTBOARD SPLICE PN 6550821144 CORRODED AND CRACKED. 2L72 4F A16WE 20040126000082004012600008NE 2004 1 26 BAQA092047 220040111A7200 ENGINE UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME1928 0009 ENGINE FAILED AFTER 27.4 HOURS. COMPRESSOR STALLS AT STARTUP AND TAKEOFF. REPLACED WITH ANOTHER SERVICEABLE RENTAL 1G72 3U3 UO H88EU E42NE 20040127002462004012700246NE 2004 1 27 AC2A092345 120040121A5610076204002 WINDSHIELD SKRSKYS76 S76A 8143006NE COCKPIT CRACKED B AC2AK NONE O OTHER ININSP/MAINT 1 SO077266K 760283 WINDSHIELD IS CRACKED ON RIGHT HAND SIDE OF WINDSHIELD. CRACK RUNS INBOARD TOWARD CENTER OF WINDSHIELD FROM RIGHT HAND SIDE. WE HAVE EXPERIENCED SIMILAR CRACKING IN THESE WINDSHIELDS BEFORE. THE MECHANICS INVOLVED THINK THIS CRACKING IS DUE TO THE STRESSES CREATED BY POOR FITTING WINDSHIELDS. THE WINDSHIELDS DO NOT MATCH AIRCRAFT CONTOURS VERY WELL. REPLACED WINDSHIELD. 1G72 3U H1NE 20040127002502004012700250SW 2004 1 27 AC2A092335 120040108A6220430010122101 STUD BELL 430 430 1182150SW M/R HEAD CRACKED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CV3410 49072 STUD IS CRACKED WHERE THREADED PORTION TRANSITIONS INTO FLANGE. REPLACED WITH NEW STUDS. 1G72 3U RTH9SW 20040127002532004012700253SW 2004 1 27 AC2A092338 120040108A63214000434 DISK BELL 430 430 1182150SW ROTOR BRAKE WORN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CV3410 49072 BRAKE DISC IS WORN. REPLACED WITH SERVICEABLE PART. 1G72 3U RTH9SW 20040127002582004012700258CE 2004 1 27 BAQA092327 120040119A323399810057652 ACTUATOR BEECH 100 100BEECH 1152916CE MLG MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 SO03999G 1798 B144 MLG ACTUATOR TURNS HARD. REPLACED WITH SERVICABLE UNIT. 01/22/2004 1L72 3T A14CE 20040128000032004012800003 2004 1 28 BAQA092348 420040120A3422066040211111 SYMBOL GENERATOR BOLKMS117 BK117A1 5626010EU ADI INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03300CP168 7249 ADI READS 8 DEGREES HIGHER THAN IT SHOULD. REPLACED SYMBOL GENERATOR WITH SERVICABLE UNIT. 1G72 3U H13EU 20040128000042004012800004 2004 1 28 BAQA092357 420040123A22114033089901 COMPUTER AGUSTAA109 A109E 0260119EU AUTOFLIGHT MALFUNCTIONED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0312UW 1703 11074 DH LIGHT ON PILOT AND CO-PILOTS ADI DOESN"T EXTINGUISH. REPLACED WITH SERVICABLE UNIT. 01/26/2004 1G72 3U RTH7EU 20040128000122004012800012 2004 1 28 BAQA091780 420040109A34225050031904 GYRO BOLKMS117 BK117B1 5626012EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6605 7235 FLAG SHOWING ON DIRECTIONAL GYRO. INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 1G72 3U H13EU 20040127002562004012700256SW 2004 1 27 AC2A092342 120040118A6220430010122101 STUD BELL 430 430 1182150SW M/R HEAD CRACKED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CM 49090 4 DOWN STOP STUDS CRACKED 1G72 3U RTH9SW 20040127002572004012700257SW 2004 1 27 AC2A092346 120040122A6220430010122101 STUD BELL 430 430 1182150SW M/R HEAD CRACKED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CM427 49090 CRACKED WHERE THREADED PORTION TRANSITIONS TO FLANGED PART. REPLACED PART. 1G72 3U RTH9SW 20040128000012004012800001CE 2004 1 28 BAQA092328 120040119A32331153800025 MOTOR BEECH 100 100BEECH 1152916CE MLG WEAK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 1798 B144 MLG MOTOR WEAK. REPLACED WITH SERVICABLE UNIT. 01/22/2004 1L72 3T A14CE 20040128000092004012800009NE 2004 1 28 HEEA092091 220040109A73217046M95G03 ECU BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE ENGINE MALFUNCTIONED B HEEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0359806 28140 GEE343231 AFTER TAKEOFF TORQUE GUAGES FLUCTUATED. RETURNED TO BASE. 2G72 4U4 U H10SW E8NE 20040128000132004012800013EU 2004 1 28 BAQA092103 120040121A6330L633M2001106A004MOUNT UROCOPEC135 EC135P1 8680990EU M/R GEARBOX DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME1200 0009 MAIN ROTOR GEARBOX MOUNT PLUNGER RETRACTED. REPLACED WITH SERVICABLE UNIT. 1G72 3U O H88EU 20040128001642004012800164EU 2004 1 28 004851 120040102A3020 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R390 R3904123F27 NE DE ICE SYS ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17340SZ 340A004 401 DRG4098 ON 01/02/2004 APPROX 1230 (UTC), FLT 4587 TTN-BED, CREW REPORTED THAT THE RT ENGINE INTAKE DE-ICE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO TTN. 2L72 4T4 TRTA52EU E8NE6 6 CP31NE 20040128001802004012800180SO 2004 1 28 C2XA04TY001 120040102A532014524321011 CLIP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS, DURING A SCHEDULED INSPECTION THE SHEAR CLIP AT FR61 BETWEEN ST20L AND 21L WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CLIP IAW EMB-135/145 SRM 51-40-02. 2L72 4F RTT00011AT 20040128001812004012800181SO 2004 1 28 C2XA04TY002 120040102A532014525363015 BRACKET EMB 145 EMB145 3260210SO STAB PULLEY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT SUPPORT PULLY CMD STAB BRACKET BETWEEN FR60 AND 61, STR 21L AND 20L. MAINTENANCE REMOVED AND REPLACED THE PULLY SUPPORT BRACKET IAW EMB 135/145 SRM 51-40-02. 2L72 4F RTT00011AT 20040128001822004012800182SO 2004 1 28 C2XA04TY003 120040102A532014526855010 CLIP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SHEAR CLIP AT FR59 BETWEEN STR 20L AND 21L. MAINTENANCE REMOVED AND REPLACED THE SHEAR CLIP IAW EMB 135/145 SRM 51-40-02. 2L72 4F RTT00011AT 20040128001832004012800183SO 2004 1 28 C2XA04TY004 120040102A532014526436 SUPPORT EMB 145 EMB145 3260210SO LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713964 145123 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT FLOOR SUPPORT BETWEEN FR60 AND 61, STR 161 AND 181. MAINTENANCE CUT OUT THE CORRODED AREA, FABRICATED A NEW FLOOR SUPPORT, ALODINED, PRIMED, PAINTED AND INSTALLED IAW EMB 135/145 SRM 51-40-02, 51-20-03, 51-40-06, CMP-51-40-02/03/06. 2L72 4F RTT00011AT 20040128001842004012800184SO 2004 1 28 C2XA04SH001 120040104A531314528737001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE GOUGED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040128001852004012800185SO 2004 1 28 C2XA04SH002 120040104A531314528737001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728529 145512 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040128001862004012800186SO 2004 1 28 C2XA04SH003 120040104A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040128001882004012800188SO 2004 1 28 C2XA04SH005 120040104A531014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040128002132004012800213WP 2004 1 28 0400019763 120040102A2910 LINE DOUG DC9 DC951 3022051WP HYD SYSTEM FAILED A NWAAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS DEDESCENT 1 GL01763NW 47396 AT TOP OF DESCENT, RIGHT HYDRAULIC QUANTITY INDICATED ZERO. A SHORT TIME LATER, THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND LANDING GEAR EXTENDED NORMALLY WITHOUT THE USE OF ALTERNATE EXTENSION PROCEDURES. FLIGHT LANDED WITHOUT INCIDENT AT RDU, STOPPED ON THE RUNWAY, AND WAS TOWED TO THE GATE. MAINTENANCE FOUND A HOLE IN THE RIGHT HYDRAULIC PRESSURE RETURN LINE. LINE WAS REPLACED, FILTERS AND PUMP WERE CHECKED, AND SYSTEM WAS RESERVICED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20040128002142004012800214NM 2004 1 28 DHL2004743001 120040101A33501000673 LIGHT BOEING727 727225 1384077NM MAIN ENTRY INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 MAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN ENTRY EMERGENCY LIGHT IAW B-727 M/M 33-50-00. OPS CHECKED NORMAL. 2L73 4F A3WE 20040129000202004012900020SO 2004 1 29 C2XA04CL001 120040104A3350 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 CLE FLIGHT 2598 THE CREW REPORTED THE AFT AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE AFT AISLE PATH EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040129000582004012900058NM 2004 1 29 04FDEA00019 120040104A2910MS9391130ZE MOTOR BOEING727 727200 138407ENM FLAP DRIVE LEAKING A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25286FE 22623 DURING CLIMBOUT OF MEMPHIS, HYDRAULIC PUMP 1 LOW PRESSURE LIGHT FLASHED, FOLLOWED BY AND IMMEDIATE LOSS OF PRESSURE AND QUANTITY. PRESSURE, QUANTITY WAS AT ZERO PRIOR TO PUMPS BEING TURNED OFF. SUSPECT PROBLEM IS IN RIGHT WHEEL DUE TO SKYDROL MIST IN THE AREA. REPLACED RIGHT O/B FLAP DRIVE MOTOR REF 727-200 M/M 27-51-062-4. 2L73 4F RTA3WE 20040129000592004012900059NE 2004 1 29 04FDEA00020 220040104A7200JT8D17AQM ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE NR 3 FAILED A FDEACD ABORTED TAKEOFF RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO25285FE1987919879 22622 709261 APPROACHING MAX POWER SETTING (215) FOR TAKEOFF ROLL NR 3 ENGINE FAIL LIGHT ILLUMINATED WITH A LOUD BANG. SUSPECT FAILURE OF NR 3 ENGINE. ENGINE EXPERIENCED TURBINE FAILURE AND IS SITTING IN THE POWERPLANT SHOP AWAITING SHIPMENT TO OVERHAUL FACILITY 2L73 4F4 FRTA3WE E2EA 20040129000602004012900060WP 2004 1 29 04FDEA00034 120040105A5210 DRIVE CHAIN DOUG DC10 DC1010 3022110WP ZONE 800 OUT OF RIG A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-5211-73858. DOORS- ENTRY DEVIATION TO FWD PAX DOOR DRIVE CHAIN RIGGING. CLOSING ACTION ON 01/03/04 ON N/R S00024. COMPLIED WITH EA 8-5211-73858. 2L73 4F A22WE 20040129000692004012900069SO 2004 1 29 SWIA200412741 120040102A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07234SW7110 4088 120308 IN CRUISE AT 22K FT, A/C STARTED TO PITCH UP SLOWLY AND AIR SPEED WAS BLEEDING OFF AT 160 KTS. REPLACED BOTH ELEVATOR TRIM ACTUATORS IAW EMB 120 MM 27-32-02. ALSO REPLACED VERTICAL STAB LEADING EDGE DEICE BOOT. OPS CHECK GOOD. ACTUATOR S/N OFF LEFT SIDE: 623. 2L72 4T RTA31SO 20040129000712004012900071NM 2004 1 29 AALA20040011 120040104A3350P4010049 BATTERY BOEING757 757223 1384957NM EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21634AA 24592 SFO EMERGENCY EXIT LIGHTS INOPERATIVE AT L4 AND R4. REPLACED BATTERY ABOVE RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040129000742004012900074WP 2004 1 29 AALA20040014 120040104A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21412AA 49323 DFW EMERGENCY AUXILLARY LIGHTS AT L2 245 AND L2 246 LEFT AND RIGHT AT STATION 916 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK B5 105 L2 245 L2 246 LEFT AND RIGHT AT STATION 916. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040129000762004012900076SO 2004 1 29 C2XA04SH008 120040106A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 SHV- DURING C-CHECK STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040129000772004012900077SO 2004 1 29 C2XA04SH009 120040106A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 SHV- DURING C-CHECK STRINGER T-REINFORCEMENT 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040129000782004012900078SO 2004 1 29 C2XA04SH010 120040106A716014575001409 STRUCTURE EMB 145 EMB145LR 3260212SO NR 1 ENG INTAKE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040129000792004012900079SO 2004 1 29 C2XA04SH011 120040106A716014575001409 STRUCTURE EMB 145 EMB145LR 3260212SO NR 2 ENG INTAKE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040127002522004012700252SW 2004 1 27 AC2A092337 120040108A6510430044100101 DRIVE SHAFT BELL 430 430 1182150SW TAIL ROTOR CORRODED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CV 49072 TAIL DRIVESHAFT IS DISCOLORED AND PAINT IS BLISTERED FROM HEAT, CORROSION PIT FORMING AT BLISTERS. REPLACED WITH SERVICEABLE DRIVESHAFT. 1G72 3U RTH9SW 20040127002542004012700254SW 2004 1 27 AC2A092339 120040108A5210NAS5623R7A CAM FOLLOWER BELL 430 430 1182150SW PAX DOOR BROKEN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CV3410 49072 ROLLER WAS BROKEN. REPLACED WITH NEW ROLLER. 1G72 3U RTH9SW 20040128000072004012800007NE 2004 1 28 HEEA092089 220040110A73217046M95G03 ECU BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 1 ENGINE MALFUNCTIONED B HEEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0359806 28140 SHORTLY AFTER TAKE OFF NR 1 ENGINE TORQUE FLUCTUATED. MAINTENANCE FOUND ECU DEFECTIVE. 2G72 4U4 U H10SW E8NE 20040128000102004012800010SW 2004 1 28 HEEA092092 120040108A2913MS21924W4 COUPLING BELL 214 214ST 1182106SW HYD SYSTEM SHEARED B HEEAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW03598062 28140 OIL COOLER BLOWER LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE FOUND UNION ON UTILITY HYDRAULIC PUMP SHEARED CAUSING THE LOSS OF HYDRAULIC FLUID. 2G72 4U H10SW 20040128000142004012800014EU 2004 1 28 BAQA092104 120040121A6330L633M2010104 MOUNT UROCOPEC135 EC135P1 8680990EU M/R GEARBOX DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME1170 0009 MAIN ROTOR GEARBOX MOUNT PLUNGER RETRACTED. REPLACED WITH SERVICABLE UNIT. 01/23/2004 1G72 3U O H88EU 20040128001672004012800167 2004 1 28 AWXA200400002 420040101A2213C12850AB02 CONTROL UNIT AIRBUS320 A320232 3930326EU COCKPIT MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28668AW103214478 1764 AFTER TAKEOFF AT DTW EN ROUTE FOR PHX RECEIVED ECAM MESSAGE AUTO FLIGHT FCU 1 & 2 FAULT. ALTIMETER FLIGHT CONTROL UNIT (FCU) WINDOWS WENT BLACK, AND HAD LOSS OF AUTO THRUST & HEADING SELECT, TURNED BACK TO DTW AND LANDED WITHOUT EVENT. MAINTENANCE REMOVED AND REPLACED FLIGHT CONTROL UNIT IAW 22-81-12, OPERATIONAL CHECK WAS GOOD. BENCH TEST OF FLIGHT CONTROL UNIT S/N C12850003088 COULD NOT DUPLICATE REASON FOR REMOVAL. POWER TRANSIENT PERFORMED ON SIDE, THEN SIDE 2 WITH NFF, PREFORMED TEMPERATURE TEST AT 0ºC TO POWER, NFF. RAN ENDURANCE TEST FOR 70 HOURS, NFF. UNIT MODIFIED WITH SB C12850A-22-006. 2L72 4F RTA28NM 20040128001872004012800187SO 2004 1 28 C2XA04SH004 120040104A542014576631622 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040128001892004012800189SO 2004 1 28 C2XA04SH006 120040104A531014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSLEAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712996 145296 SHV- DURING C-CHECK THE FWD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040128001912004012800191SO 2004 1 28 C2XA04SH007 120040104A533014520554003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711544 145557 SHV-DURING C-CHECK THE LEFT SIDE OF THE AIRCRAFT SKIN WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040129000142004012900014EA 2004 1 29 MASA200400001 120040101A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER L NO TEST ININSP/MAINT 1 SW0775999 7471 ASH 2848 PHL-BNA, CAPTAIN REPORTED AN AFT INTERIOR CEILING EMERGENCY LIGHT HAD A BULB INOP DURING A TEST. MX RESEATED THE BULB AND THE LIGHT CHECKED GOOD. AIRCRAFT CONTINUED REVENUE FLIGHT. NO PARTS USED. 2L72 4F RTA21EA 20040129000572004012900057WP 2004 1 29 04FDEA00006 120040102A5710ARB0005 BULKHEAD DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2540061 46973 COMPLY WITH EA 8-5710-73861 WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861. 2L73 4F A22WE 20040129000722004012900072NM 2004 1 29 AALA20040012 120040103A3350 HOUSING BOEING777 777223 1385213NM EMERGENCY LIGHT MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21798AN 30797 DFW EMERGENCY LIGHT AT RIGHT SIDE FORWARD GALLEY MISSING LIGHT AND ASSEMBLY. REPLACED EMERGENCY LIGHT HOUSING AT RIGHT SIDE FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040129000752004012900075EU 2004 1 29 AALA20040015 120040104A2560 BATTERY FOKKERF28 F28MK0100 4990807EU FLASHLIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211410E 11368 DTW EMERGENCY FLASHLIGHT AT AFT RIGHT HAND NOT BLINKING. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT AFT RIGHT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040129000862004012900086NM 2004 1 29 CALA0400001 120040105A523065C36321 SKIN BOEING737 7373T0 1384582NM C2 DOOR CANNING A CALAK NONE O OTHER ININSP/MAINT 1 SW0912322 23373 C2 DOOR LOWER SKIN OIL CANNED LOWER AFT. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-00-01. 2L72 4F RTA16WE 20040129001292004012900129EA 2004 1 29 COMA0460008 120040104A2913601R753051 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYS 3 UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01518CA 7816 FLIGHT 5384 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE 3B HYDRAULIC PUMP. 2L72 4F RTA21EA 20040129001462004012900146WP 2004 1 29 AALA20040024 120040105A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21448AA 49474 DFW AFT CABIN EMERGENCY LIGHTS L2 615 AND L2 671 AND TAIL COMPARTMENT EMERGENCY LIGHT L2 694 COME ON WITH FLIGHT ATTENDANT EMERGENCY LIGHTS SWITCH IS PLACED ON. REPLACED BATTERY PACK B5 27 FOR AFT CABIN EMERGENCY LIGHTS L2 615 AND L2 671 AND TAIL COMPARTMENT EMERGENCY LIGHT L2 694. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040129001522004012900152NM 2004 1 29 HNAA0400001 120040105A3234 SELECTOR PANEL DHAV DHC8 DHC8102 2809003NM MLG INOPERATIVE A HNAAO OTHER J WARNING INDICATION LDLANDING 1 EA07911HA 034 WHEN SELECTED LANDING GEAR DOWN, 3 UNSAFE LIGHTS, GEAR DID NOT OPERATE, RECYCLED GEAR HANDLE, GEAR OPERATED NORMALLY. REMOVED AND REPLACED LANDING GEAR SELECTOR PANEL, OPS CHECK GOOD. (OPEN) 2H72 4T RTA13NM 20040129001592004012900159EA 2004 1 29 COMA0460019 120040104A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY CONTAMINATED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01436CA 7482 FLIGHT 5762 SMOKE IN CABIN AND COCKPIT. DETERMINED SMOKE TO BE FROM GYCOC IN APU. DEFERRED APU PER MEL. 2L72 4F RTA21EA 20040129001782004012900178NE 2004 1 29 MWEA040006 220040107A7321114E6112G120 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE LT & RT ENGINE FAILED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31907ME 55171 13370 RIGHT AND LEFT ENGINE FAIL ALERT CAME ON. REMOVED AND REPLACED ENGINE ELECTRONIC CONTROLLER. 2L72 4F4 FTRA6WE E00057EN 20040129001912004012900191NM 2004 1 29 04FDEA00079 120040108A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT WING - OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK CRACKED. OUTBOARD FLAP INBOARD HINGE BRACKET (WING SIDE) SIDE LINK TENSION STRAP SUPPORT REMOVED AND REPLACED AS PER DAC SB57-10. 2L73 4F RTA22WE 20040129002072004012900207NM 2004 1 29 SWAA040034 120040105A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, BETWEEN STRINGERS 15L AND 14L. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040129002082004012900208NM 2004 1 29 SWAA040035 120040105A531065C26402 CREASE BEAM BOEING737 7373H4 1384600NM AFT PAX CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 776, LBL 68, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040130000532004013000053NM 2004 1 30 04FDEA00084 120040108A5311 FRAME BOEING727 727200 138407ENM DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 SCREW DAMAGE IN FRAME AT BS 1110 STR 26. *S/D* FOUND SCREW DAMAGE ON FRAME TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGE AREA AND FABRICATED REPAIR DOUBLER FROM 7075-70 .071 LOT 491543, APPLIED PROTECTIVE TREATMENT AND INSTALLED REPAIR DOUBLER. ALL WORK DONE IAW SRM 51-40-3, 51-10-2, 51-30-2 AND DOUBLER WAS HEAT TREATED TO T6 CONDITION AND REPAIRED PER FED EX EA 7-5310-55192. 2L73 4F RTA3WE 20040130000562004013000056NM 2004 1 30 DHL2004763002 120040108A261269689553 BRACKET BOEING727 727264 138408MNM FIRE LOOP MISSING A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01763AT 22983 NR 1 FAULT DETECTOR LIGHT INTERMITTENT DURING FLIGHT. DEFERRED PER MEL 26-9 CAT-C DMI 15327. REF DMI 15327 (NR 1 FAULT DETECTOR LIGHT INTERMITTENT DURING FLIGHT. FOUND LOOP CHAFING WHERE BRACKET WAS MISSING. INSTALLED SERVICEABLE BRACKET P/N: 69-68955-3, IAW B-727 OHM 71-02-01. OPS CHECKED GOOD IAW MM 26-11-0. THIS CLEARS DMI 15327. 2L73 4F A3WE 20040130000592004013000059EA 2004 1 30 COMA0460027 120040108A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01815CA9312 7397 THE LEFT WING LOWER PLANK ACCESS HOLE CUTOUTS HAVE CORROSION AT 540CB AND 550 AB. REMOVED THE CORROSION AND RESTORED SURFACE FINISH IAW REO 601R-57-21-030 REV C. 2L72 4F RTA21EA 20040130000612004013000061EA 2004 1 30 COMA0470004 120040105A3260895304 PSEU CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01641CA 10122 FLIGHT 5290 GEAR DISAGREE WARNING, LANDING GEAR FAILED TO RETRACT. REPLACED THE PSEU. 2L72 4F RTA21EA 20040130000652004013000065WP 2004 1 30 UPS04841699 120040106A5310 SHEAR TIE DOUG DC8 DC871F 302199DWP TAIL COMP'T CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, SHEAR TIE CRACKED AT STA 1766 BETWEEN LONGERONS 9R AND 10R. STOP DRILLED CRACK AND INSPECTED PER NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR PER DAC DWG 5772706, AND DC8 SRM 53-2-0 FIG 1B. 2L74 4F RT4A25 20040130000662004013000066 2004 1 30 0401413 420040101A22104006719910 SERVO DORNERDO32 DO328300 NM AUTOPILOT FAULTY A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27413FJ 3168 DURING OPERATION OF AIRCRAFT CREW REPORTED OSCILLATIONS WITH THE AUTOPILOT ENGAGED. THE AILERON SERVO MOTOR WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040130000672004013000067 2004 1 30 AWXA200400024 420040104A2297 WIRE BOEING737 737277 1384570NM AUTOPILOT DAMAGED A AWXAH DEACTIVATE SYST/CIRCUITS FS FLT CONT AFFECTED AFFECT SYSTEMS CLCLIMB 1 WP28184AW 22651 ON CLIMBOUT, WHEN AUTOPILOT-B ENGAGED A/C BANKED HARD RT PAST 30 DEGREES. REATTEMPTED TO ENGAGE AUTOPILOT-B SAME RESULTS. AS SOON AS AUTOPILOT-B ENGAGED CONTROL WHEEL STEERING INDICATED ROLL RT, AUTOPILOT-A NORMAL. MAINT TROUBLESHOT AUTOPILOT SYS, B-SYS GOES HARD RT REGARDLESS OF MODE INPUTS, BITE TEST DID NOT REVEAL A FAILED COMPONENT. RANG OUT WIRING BETWEEN TRANSFER VALVE AND AUTOPILOT AILERON CONTROL ACTUATORS, ACTUATOR-B PINS INDICATE OPEN BETWEEN PINS 7 & 8, ALL OTHER ACTUATORS CHECKED GOOD. PARTS ORDERED. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT AILERON CONTROL ACTUATOR IAW BMM 22-011-012-4, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040130000712004013000071EU 2004 1 30 04003301 120040103A33506047051 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27301UE 41012 DURING INSPECTION THE FOWARD SECTION OF EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLY WAS FOUND TO BE DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040130000722004013000072EA 2004 1 30 04004683 120040104A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27683BR 7692 DURING INSPECTION THE FOWARD EXTERNAL FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040130000742004013000074EA 2004 1 30 COMA0460030 120040107A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01916CA 7014 REPAIR FUSELAGE DAMAGE FROM FS 280.0 TO FS 379.0 DAMAGED STRINGERS 25R, 24R AND 23R; FRAME DAMAGE AT FS 349.00 BETWEEN STRINGER 23R AND 24R AND AT FS 319.70 BETWEEN STRINGER 25R AND 26R. REMOVED DAMAGED SKIN AND STRINGERS AND FRAMES IN AREA OF DAMAGE. INSTALLED REPAIR SKINS AND DOUBLERS, STRINGERS, SPLICES, AND FRAMES IAW REO 601R-53-21-471. FILLET SEALED SKIN AND DOUBLERS IAW REO 601R-53-21-471 AND CRJ SRM 51-14-16. PRINTED REPAIR, PAINTED INSIDE, AND APPLIED DINOTROL. PAINTED EXTERIOR AND INSTALLED REMOVED PARTS. 2L72 4F RTA21EA 20040130000902004013000090NM 2004 1 30 AALA20040037 120040107A3350 BATTERY BOEING777 777223 1385213NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21772AN 29580 DFW WALL MOUNTED EMERGENCY LIGHTS IN BUSINESS CLASS GALLEY INOPERATIVE. REPLACED BATTERY FOR WALL MOUNTED EMERGENCY LIGHTS IN BUSINESS CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040130000922004013000092NM 2004 1 30 AALA20040036 120040108A3350 LIGHT BOEING757 757223 1384957NM EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21695AN 26975 MIA SEAT MOUNTED EMERGENCY EXIT LIGHTS AFT OF ROW 24 INOPERATIVE. REPLACED MODULE AND BATTERY. SYSTEM GROUNG CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040130000942004013000094WP 2004 1 30 AALA20040038 120040108A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213507A 49801 SAT OVERHEAD EMERGENCY LIGHT OVER SEATS 8 AND 9 INOPERATIVE. REPLACED BATTERY PACK B5-100 AND 101 FOR OVERHEAD EMERGENCY LIGHT OVER SEATS 8 AND 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130000962004013000096NM 2004 1 30 QXEA200400004 120040106A5210 SEAL BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LEAKING A QXEAO OTHER O OTHER CLCLIMB 1 NM09406QX 4048 SEA- ON FLIGHT 2292 DURING CLIMBOUT AT 12000, CABIN LOST PRESSURE. AFTER 2-3 MINUTES CABIN SLOWLY REPRESSURIZED. AFT FLIGHT ATTENDANT REPORTS LOUD HISS AT AFT PASSENGER DOOR. REMOVED AND REPLACED AFT PASSENGER DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040130001012004013000101SO 2004 1 30 C2XA04TY008 120040110A532014524131009 SILL EMB 145 EMB145 3260210SO PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE MAIN ENTRANCE DOOR SILL UNDER THE THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRANCE DOOR SILL IAW EMB SRM 51-40-02. 2L72 4F RTT00011AT 20040128001662004012800166 2004 1 28 AWXA200400001 420040101A344146502003030312 ADIRU AIRBUS320 A320232 3930326EU ZONE 127, POS 3 FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28670AW1915 2029 IMMEDIATELY AFTER TAKEOFF FROM JFK EN ROUTE FOR LAS RECEIVED NR 1 & 3 IR FAULTS, TURNED BACK AND LANDED WITHOUT EVENT. MAINT RESET & RERACKED NR 1 & 3 AIR DATA INERTIAL REFERENCE UNITS IAW AMM. PERFORMED BITE TEST IAW T/C A1B34309, & AUTOMATIC FLIGHT SYSTEM TEST IAW AMM. NO FAULTS NOTED. ON RETURN FLT IR NR 3 FAULTED AGAIN. MAINT R & R NR 3 ADIRU IAW T/C R2A34304, OPS CHECK GOOD. CONFIRMED FAILURE OF ADIRU S/N 4289. DOWN LOAD VERIFIED FAULT FID 396, Z QUANTIZER SATURATION THAT IS CAUSED BY EXCESSIVE INPUT IN THE VERTICAL AXIS, BELIEVED TO BE THE RESULT OF UNIT IMPACTING THE SHELF ABOVE (KNOWN AIRBUS PROBLEM). COMPLIED WITH SERVICE BULLETIN 101-34-57 AND PERFORMED THERMAL CALIBRATION TEST IAW AT261847. 2L72 4F RTA28NM 20040129000012004012900001WP 2004 1 29 DHL2004873001 120040102A2742 TRIM MOTOR DOUG DC8 DC873F 302199FWP MALFUNCTIONED A DHLAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01873SJ 46091 AFTER ROTATION AIRCRAFT RAPIDLY PITCHED UP TO 20 DEG ACTUATING THE STICK SHAKER. CREW PUSHED FULL UP ON CONTROL WHEEL TO FORWARD STOP. F/O ACTIVATED TRIM FROM 5.3 TO ZERO. RETURNED TO NORMAL CLIMB ATTITUDE. TRIM WAS 10 TO 2 DEG FOR CRUISE, 4.0 FOR APPROACH, 6.0 FOR LANDING. INSPECTED AND CHECKED ELEVATOR, ELEVATOR GEAR TAB AND ELEVATOR CONTROL TAB. OPS CHECKS OF ELEVATOR AND CONTROL SURFACES GOOD. PERFORM A PITOT LEAK TEST / CHECK ON CAPT, ALT AND F/O'S SYSTEM. OPS CHECKED SERVICEABLE. AIRCRAFT HAS BEEN INSPECTED AND FOUND TO BE IN SAFE OPERATING CONDITION FOR THE REQUIRED ACCEPTANCE FLIGHT. TEST FLIGHT SATISFACTORY AS REQUIRED BY MX22 SPECIAL ACCEPTANCE FLIGHT. NOTED BY MAINTENANCE. 2L74 4F RT4A25 20040129000552004012900055SO 2004 1 29 C2XA04CL002 120040104A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2716976 145171 CLE FLIGHT 2468 THE CREW REPORTED A STRONG BURNING ODOR ON DESCENT WHEN THE ANTI-ICING SYSTEM IS ACTIVATED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. 2L72 4T RTT00011AT 20040129000732004012900073WP 2004 1 29 AALA20040013 120040104A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 TPA EMERGENCY CEILING LIGHT BETWEEN AFT LAVATORY AND EMERGENCY LIGHT AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK B5 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040129000972004012900097NM 2004 1 29 0400046301 120040105A3350 BATTERY PACK BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040129001372004012900137NE 2004 1 29 MWEA040002 220040104A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE LEFT MALFUNCTIONED A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31806ME 48032 LEFT ENGINE WOULD NOT GO ABOVE 1.8 ENGINE PRESSURE RATIO. COMPLIED WITH POWER ASSSURANCE CHECK. ALL SYSTEMS NORMAL. 2L72 4F4 F A6WE E9NE 20040129001632004012900163SO 2004 1 29 C2XA04BT001 120040105A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2714952 145067 CREW REPORTED, BURNING ODOR AROUND ROW 3 AND 4 IN CABIN AFTER POWERED UP. MAINTENANCE REMOVED ROW 3 AND 4 OVERHEAD PANELS, INSPECTED CEILING LIGHTS AND SIDE WALL LIGHTS, NO ODOR NOTED NOR DEFECTS FOUND IAW EMB145 AMM 05-25-05. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040129001642004012900164EA 2004 1 29 SWIA200412749 120040105A2751 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07948SW 7789 INFLT FL270 SPEED TAPE WENT TO 230 KTS. THE 1B HYD PUMP AND 3B HYD PUMP ON EDI. TURNED SWITCH TO ON MSG WENT AWAY. TURNED SWITCH BACK TO AUTO AND MESSAGE RETURNED, ALSO 2B PUMP SHOWED INOP, BUT NO MESSAGE. REMOVED AND REPLACED RIGHT FLAP POSITION TRANSMITTER IAW MM 27-55-01. OPS CK GOOD. 2L72 4F RTA21EA 20040129001652004012900165EA 2004 1 29 SWIA200412750 120040104A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07916SW4283 4283 7634 ON DESCENT INTO DEN, RECEIVED A FLAPS FAIL MESSAGE WHEN MOVING FLAPS FROM 0 DEGREES TO 8 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-50-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040129001892004012900189NM 2004 1 29 04FDEA00081 120040108A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP VANE NR 2, 3, 4 AND 5 T-FITTING (COUNTING FROM INBOARD) FOUND FWD HOLE CORRODED AT BORES. LT OUTBOARD FLAP VANE NR 2 TEE FITTING REPAIRED AS PER EA 1-5750-74288, LT & RT OUTBD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040129002022004012900202NM 2004 1 29 04FDEA00068 120040107A5311AFA7001501 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 MINOR DENT ON FRAME IN CABIN AT STA 1541 BETWEEN STR 12-13 LEFT. 2L73 4F RTA22WE 20040129002052004012900205CE 2004 1 29 57548 120040101A2910W901J24CE COUPLING BEECH 1900 1900D 1154162CE LT WING WORN A AMWAO OTHER O OTHER APAPPROACH 1 CE07174YV UE174 UPON APPROACH TO MCI LANDING GEAR WOULD NOT EXTEND. CREW AND MX CONTROL DECIDED TO HAVE AIRCRAFT RETURN TO LIT, AS IT WAS A REPOSITION FLIGHT. UPON ARRIVAL AT LIT, THE GEAR WAS PUMPED DOWN AND HAD 3 GREENS. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACING ENTIRE POWER PACK, SAFETY SWITCH, IT'S WIRING, ALL MELTED TIE WRAPS, THE DRAIN TUBE, AND ALL EVA TUBING IN THE AREA. THE COUPLING, A CONNECTING TUBE, AND IT'S ASSOCIATED PACKINGS WERE REPLACED. 2L72 4T RTA24CE 20040130000602004013000060EA 2004 1 30 COMA0460028 120040106A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01467CA4991 7637 FLIGHT 5055 FLAPS FAIL MESSAGE. REPLACED THE FLP PDU. 2L72 4F RTA21EA 20040130000912004013000091NM 2004 1 30 AALA20040039 120040101A3350 LIGHT BOEING767 767323 1385205NM EMERGENCY EXIT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 ORD EMERGENCY EXIT LIGHT AT AFT LEFT SERVICE DOOR L-3 INOPERATIVE. REPAIRED AND RELAMPED AFT EMERGENCY EXIT LIGHT AT L-3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040130000932004013000093NM 2004 1 30 AALA20040035 120040108A3350 LIGHT BOEING757 757223 1384957NM EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21695AN 26975 MIA EMERGENCY EXIT LIGHTS AT 4 LT AND 4 RT DOOR AREA INOPERATIVE. REPLACED MODULE AND BATTERY FOR 4 LT AND 4 RT DOOR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040130001022004013000102SO 2004 1 30 C2XA04TY010 120040110A532014526436401 MOUNT EMB 145 EMB145 3260210SO LAV SINK DRAIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LAVATORY SINK DRAIN CABLE/HOSE MOUNT PLATE. MAINTENANCE REMOVED AND REPLACED THE DRAIN CABLE/HOSE MOUNT PLATE IAW EMB SRM 51-40-02, 51-30-01 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040130001112004013000111WP 2004 1 30 MWEA040007 120040110A1430 RIVET DOUG DC9 DC981 3022081WP AILERON SKIN LOOSE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 LEFT AILERON SKIN HAS LOOSE RIVET IN TOP SKIN AT STATION XRS 475, HOLE IS ENLARGED. INSTALLED DOUBLER TO REPAIR HOLE IN AILERON SKIN. 2L72 4F A6WE 20040130001132004013000113SO 2004 1 30 MASA200400017 120040108A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 ASH 2820, CLT-STL. DURING PREFLIGHT, EMERGENCY EXIT LIGHT INOP AT ROW 12. MX RELAMPED, OP CHECKS GOOD. 2L72 4T RTT00011AT 20040130001142004013000114EA 2004 1 30 MASA200400018 120040109A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727318 7318 ASH 6231 PHX, FORWARD CABIN EMERGENCY EXIT LIGHT WAS INOP DURING TEST. MX REPLACED BULB, OP CHECKS GOOD. 2L72 4F RTA21EA 20040130001152004013000115 2004 1 30 P5CA0401026 420040108A3418285U0084210 CIRCUIT CARD BOEING747 74746NF 13848BTNM STALL WARNING FAILED A P5CAO OTHER N FALSE WARNING CRCRUISE 1 WP23454PA 30812 IN CRUISE STICK SHAKER CAME ON STEADY A/S & ATTITUDE NORMAL. PULLED R STICK SHAKER C/B. DEFERRED TO DMI 32052 AS MEL 27-32-01. INSTALLED PLACARDS. REMOVED AND REPLACED A10 STALL WARNING CARD. 2L74 4F RTA20WE 20040130001172004013000117NM 2004 1 30 UPS04441705 120040104A5320707500063IN WEB BOEING747 747123F NM MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, LT BLG W/W O/B SIDE LOWER FAIRING SUPPORT WEB CRACKED AT STA 1438. WEB REPLACED PER SRM 51-40-03 FIG 1. 2L74 4F A20WE 20040130001182004013000118NM 2004 1 30 UPS04441706 120040103A532065B119535 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, COCKPIT BS 340-360 BL 0, FLOOR SUPPORT UPPER CHORD FOUND CRACKED. BS 340-360 BL 0 FLR SUPPORT UPPER CHORD REPLACED PER SRM 51-10-01. 2L74 4F A20WE 20040130001202004013000120NM 2004 1 30 UPS04441708 120040103A5411155PH0100IN SPAR BOEING747 747123F NM NR 3 PYLON I/B CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, NR 3 PYLON I/B AFT LOWER SPAR WEB FASTENER FOUND CRACKS JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 3 PYLON I/B AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 22 AT NAC STA 221.9. 2L74 4F A20WE 20040130001212004013000121NM 2004 1 30 UPS04441709 120040103A5411177PH0125IN SPAR BOEING747 747123F NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, NR 1 PYLON I/B AFT LOWER SPAR WEB FOUND CRACKED JUST AFT OF REAR ENGINE MOUNT BULKHEAD. NR 1 PYLON LOWER SPAR WEB I/B EDGE AREA REPAIRED AS PER SRM 54-10-03 FIG 23. 2L74 4F A20WE 20040130001222004013000122 2004 1 30 UPS04841700 420040108A2565 SLIDE DOUG DC8 DC873F 302199FWP PAX DOOR DISLODGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 EVACUATION SLIDE ON MAIN ENTRY DOOR FELL OUT OF THE CASE O/B CLIP. OK TO CONTINUE IN SERVICE IAW MEL 57-7-4. 2L74 4F RT4A25 20040130001242004013000124WP 2004 1 30 0400099152 120040111A2910 LINE DOUG DC9 DC914 3022034WP HYD SYSTEM LEAKING A NWAACH ABORTED TAKEOFF DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL018911E 45825 THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED SAFELY AT 100 KTS AT IND. MAINTENANCE FOUND THE PRESSURE LINE ON THE RIGHT HYDRAULIC SYSTEM ELECTRIC PUMP LEAKING. PRESSURE LINE, SYSTEM FILTER, AND ENGINE DRIVEN PUMP WERE ALL REPLACED. THE NR 4 LINE ON LT MLG SWIVEL FITTING WAS REPLACED WITH A TEMPORARY LINE DUE TO LEAKING. ALL SYSTEM LINES AND PUMPS WERE CHECKED AND A MONITOR WAS OPEN AGAINST THE TEMP LINE. 2L72 4F A6WE 20040130001252004013000125NM 2004 1 30 DHL2004782001 120040109A2130 VALVE BOEING727 727227 1384078NM LT PACK FAILED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01782DH 21998 AFTER T/O THE A/C CABIN PRESSURIZATION WAS CLIMBING AT A HIGH ABNORMAL RATE. THE LT PACK MIX VALVE WOULD NOT MOVE. THE APPROPRIATE ABNORMAL PROCEDURES WAS USED. AT 17000 FT THE CABIN ALTITUDE CLIMBED ABOVE 10000 FT WITH THE CARGO HEAT OUTFLOW VALVE AND PRESS VALVES FULLY CLOSED. RIGHT PACK - OPS NORMAL. FOUND LEFT FORWARD PACK VALVE INOPERATIVE. REMOVED AND REPLACED SAME. OPS NORMAL IAW M/M 21-30-0. OK FOR SERVICE. 2L73 4F A3WE 20040130001272004013000127NM 2004 1 30 DHL2004745003 120040110A3260 UPLOCK BOEING727 727224 1384076NM MLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION BOTH FORWARD RED DOOR ANNUNCIATOR AND R GEAR DOOR LIGHT (S/O'S PANEL) ILLUMINATED. PERFORMED ABNORMAL PROCEDURE AND BOTH LIGHTS EXTINGUISHED. DISCONNECTED RT MLG ACTUATOR. ADJUSTED MANUAL UNLOCK CRANK TO .055 INCH, RECONNECTED ACTUATOR AND PERFORMED OPS CHECK PER B-727 M/M 32-62-11. GROUND CHECK GOOD (LG DOOR WARNING SWITCH). 2L73 4F A3WE 20040130001282004013000128NM 2004 1 30 DHL2004749001 120040110A3150 WARNING LIGHT BOEING727 727200 138407ENM COCKPIT ILLUMINATED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01749DH 22013 REJECTED T/O DUE TO ENGINE FAIL LIGHTS ILLUMINATED, PACKS TRIPPED OFF. NO ENGINE FAILURE NOTED. AIRCRAFT WT: 169860, 10 KTS, -11C, AND 450 PRESSURE ALTITUDE. REJECTED T/O DUE TO ENGINE FAIL LIGHTS ILLUMINATED, PACKS TRIPPED OFF. NO ENGINE FAILURE NOTED. RESET AUTO-PACK TRIP NORMAL. DEFERRED PER MEL 21-30 DMI CONTROL NUMBER 15360. REF DMI 15360 REJECTED T/O DUE TO ENGINE FAIL LIGHTS ILLUMINATED, PACKS TRIPPED OFF. NO ENGINE FAILURE NOTED. RESET AUTO-PACK TRIP NORMAL, ABNORMAL CHECK LIST COMPLETED. RESET CIRCUIT BREAKER AUTO-PACK TRIP; CHECKED PNEUMATIC SENSORS, RAN ENGINES, CHECKED OPS OF AUTO PACK TRIP AND WORKED GOOD PER M/M 21-10-00. PLACARD REMOVED. THIS CLEAR DMI 15360. 2L73 4F RTA3WE 20040130001292004013000129NM 2004 1 30 DHL2004782002 120040110A3260656021132 ACCESSORY UNIT BOEING727 727227 1384078NM MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01782DH 21998 DURING GEAR RETRACTION, RED LT MAIN GEAR DISAGREEMENT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT, IAW BMM CHAPTER 32-09-121. 2L73 4F A3WE 20040130001332004013000133EU 2004 1 30 AWXA200400026 120040109A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 263 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 PHX - EEL - DURING INSPECTION HAD A BATTERY TEST FAULT AT AFT LT EMERGENCY POWER SUPPLY UNIT (13WL). MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT AFT LT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040130001362004013000136WP 2004 1 30 AALA20040041 120040111A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21412AA 49323 DFW FWD EMERGENCY OVERWING LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY OVERWING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130001372004013000137WP 2004 1 30 AALA20040042 120040111A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219619V 53566 COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5 23 FOR COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040130001382004013000138WP 2004 1 30 AALA20040043 120040111A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW213507A 49801 DTW OVERHEAD EMERGENCY LIGHTS AT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR ROW 6. SYSTEM GOUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130001402004013000140WP 2004 1 30 AALA20040045 120040111A33501001191 LIGHT DOUG DC9 DC982 3022082WP PAX DOOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21278AA 49294 AUS FORWARD ENTRY EMERGENCY LIGHT WILL NOT GO OFF. REPLACED FORWARD ENTRY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130001422004013000142EU 2004 1 30 AALA20040047 120040110A3350 LIGHT AIRBUS300 A300B4605R 3930308EU SEAT 11G INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 MIA EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040130001442004013000144WP 2004 1 30 AALA20040050 120040109A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2170425 49337 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS B5-28 FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130001452004013000145NM 2004 1 30 AALA20040051 120040109A3350 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21348AN 33087 SFO RIGHT AFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. CLEANED LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040130001482004013000148EU 2004 1 30 AALA20040054 120040111A2730861CAE1 SENSOR AIRBUS300 A300B4605R 3930308EU ZONE 200 BIRD STRIKE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2114077 612 JFK INFLIGHT/T1193/11 AFTER LIFTOFF STICK SHAKER STARTED AND CONTINUED UNTIL LANDING. INSPECTION FOUND ANGLE OF ATTACK DAMAGED DUE TO A BIRD STRIKE. REPLACED CAPTAINS ANGLE OF ATTACH SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040130001502004013000150EU 2004 1 30 04FDEA00095 120040111A3260BDM3003 PROXIMITY SENSOR AIRBUS300 A300F4605R 3930327EU MLG MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25658FE 752 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT PAST INTERLOCK; SWITCHED TO SYSTEM NR 2, SAME PROBLEM. ENT BY: 502223 RPT BY: 123564 FACT 11JAN04 PERFORMED LANDING GEAR SAFETY RELAY CONTROL SIMULATOR TEST SET ON LANDING GEAR SWITCH UNIT (2GA) PER M/M 32-00-00-5, ALL INDICATIONS NORMAL. REMOVED AND REPLACED PROX DET UNIT (54GB) PER M/M 32-31-71-4 BITE CHECK C/O ALL INDICATIONS NORMAL. SERVICED RT PITCH DAMPER TO CORRECT PRESS PER M/M 12-12-32-0. REMOVED RT MAIN GEAR BOGIE BEAM PROXIMITY DETECTOR BOLT FOUND IT TO BE PACKED WITH ICE, CLEANED AND DRIED AREA RECHECKED TARGET GAPS INSTALLED PER M/M 32-00-00-4, ALL CHECKS NORMAL. 2L72 4F RTA35EU 20040130001522004013000152NM 2004 1 30 04FDEA00104 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001542004013000154NM 2004 1 30 04FDEA00106 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001562004013000156NM 2004 1 30 04FDEA00108 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001572004013000157NM 2004 1 30 04FDEA00109 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. LT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001592004013000159NM 2004 1 30 04FDEA00117 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. LT OTBD FLAP INBD HINGE (FLAP SIDE), OTBD ACTUATOR LUG SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001602004013000160NM 2004 1 30 04FDEA00124 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74277, WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20040130001612004013000161NM 2004 1 30 04FDEA00125 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001662004013000166NM 2004 1 30 PCAA0401153 120040110A5260 SENSOR DHAV DHC8 DHC8102 2809003NM ZONE 800 MISRIGGED A PCAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 EA13808EX 299 FLIGHT 3904, LGA TO ROC HAD TO LOWER ALTITUDE AND DEPRESSURIZE DUE TO PASSENGER AIRSTAIR DOOR WARNING LIGHT ILLUMINATING DURING CRUISE. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND THE OVERCENTER PROXIMITY SWITCH OUT OF ADJUSTMENT. SENSOR WAS ADJUSTED PER MAINTENANCE MANUAL AND DOOR WAS OPERATIONAL CHECKED. ALL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040130001672004013000167NM 2004 1 30 PCAA0401154 120040110A323282970018013 ACTUATOR DHAV DHC8 DHC8102 2809003NM MLG DOOR BYPASSING A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13811EX2687 201 FLIGHT 3777 HAD TO RETURN TO FIELD DUE TO ABNORMAL GEAR DOOR INDICATION AFTER CYCLING DURING CLIMBOUT. MAINTENANCE FOUND THE FORWARD MAIN GEAR DOOR ACTUATOR BYPASSING. THE ACTUATOR WAS REPLACED AND THE SYSTEM RIGGING CHECKED AND ADJUSTED AS NEEDED. SYSTEM WAS OPERATIONAL CHECKED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040130001692004013000169CE 2004 1 30 013041 120040112A5210 HANDLE BEECH 1900 1900C 1154161CE PAX DOOR LACK OF LUBE A NSVAK NONE O OTHER ININSP/MAINT 1 EA27210CJ UC110 PAX DOOR HANDLE HARD TO TURN. LUBED DOOR HANDLE, OPS CHECKED GOOD. 2L72 4T RTA24CE 20040130001732004013000173WP 2004 1 30 CALA0400019 120040112A5320 BEAM DOUG DC9 DC982 3022082WP CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND FASTENER HOLE ELONGATED IN MID CARGO DOOR THRESHOLD ZEE BEAM. THE FASTENER HOLE WAS REPAIRED IAW ECRA 5311-01182. 2L72 4F A6WE 20040130001742004013000174WP 2004 1 30 CALA0400020 120040112A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND A 3 INCH CRACK IN WEB CUTOUT AT STA 1155, LONGERON 27R IN AFT BAGGAGE BIN. THE WEB CUTOUT WAS REPAIRED IAW ECRA 5310-04393. 2L72 4F A6WE 20040130001772004013000177NM 2004 1 30 DHL2004752501 120040105A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, REPAIR AT BS 1130 BETWEEN STR 21R TO 24R DENTED AND ENDS ON STRINGER. REMOVED PREVIOUS REPAIR AND FOUND SKIN DENTED OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. REMOVED RT AFT SIDEWALL IN AFT PIT FOR ACCESS IAW B-727 MM 25-52-02. CUT OUT DAMAGED AREA DIM 1.625 INCH X 1.625 INCH AND FABBED FILLER FROM 2024 T3 .063 PO 900355 DIM .5 INCH X .5 INCH AND DOUBLER FROM 2024 T3 .071 PO 900408 DIM 11.5 INCH X 11 INCH IAW B-727 SRM 53-30-3 FIG 3. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 3. REINSTALLED LINER IAW B-727 MM 25-52-02. 2L73 4F A3WE 20040130001812004013000181NM 2004 1 30 2004UALA00005 120040102A5330 SKIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE SCRATCHED A UALAK NONE O OTHER ININSP/MAINT 1 WP29845UA 1585 APPROX 2 FT LONG SCRAP ALONG FUSELAGE BELLY AT FWD CARGO DOOR LEADING TO LOWER TCAS ANTENNA. MAJOR REPAIR. DOUBLER TRIPLER REPAIR TO SKIN AT STRINGER 42R AND FRAME 27. 2L72 4F4 FRTA28NM E40NE 20040130001832004013000183NE 2004 1 30 2004UALA00008 220040106A7200 ENGINE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 1 FLAMED OUT A UALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP29767UA 26918 NR 1 ENGINE FLAMEOUT IN FLIGHT. CREW UNABLE TO RESTART ON 2 ATTEMPTS. FUEL PUMP MAIN STAGE FAILURE. IMPLEMENTING SOFT TIME THRESHOLD FOR OVERHAUL OF PUMPS AT SHOP VISIT. REMOVING HIGH-TIME PUMPS IN-SERVICE. TEARDOWN FINDINGS WILL BE ANALYZED TO DETERMINE IF HARD TIME LIMIT, IN ADDITION TO SOFT TIME THRESHOLD, IS ALSO REQUIRED. 2L72 4F4 FRTT0001SE E46NE 20040130001852004013000185NM 2004 1 30 2004UALA00016 120040107A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29385UA 24660 FWD CARGO DOOR CUTOUT UPPER FWD CORNER SKIN IS BENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040130001872004013000187NM 2004 1 30 2004UALA00018 120040107A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 STRINGER SPLICE CRACKED AT BS 907 S4L & S4R. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040130001882004013000188NM 2004 1 30 2004UALA00019 120040107A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 BS 194 WL 207 RT SHEAR WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20040130001892004013000189NM 2004 1 30 DHL2004752505 120040106A5720 STIFFENER BOEING727 727223 1384074NM RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, RT WING HAS L/E OF FRONT SPAR VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER IAW B-727 SRM 51-30-2. FABBED NEW FROM BAC 1517-1406 PO 3448268 DIM 32 INCHES AND FILLER (SHIM) FROM 7075-T6 .190 PO 314676 DIM 27.5 X 1.5 INCH IAW B-727 SRM 57-10-2 FIG 3 AND 51-20-1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040130001902004013000190NM 2004 1 30 DHL2004752506 120040105A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE EXT SKIN BS 1090 STR 2312 IS CREASED. DAMAGE BELOW STRINGER OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .063 PO 900355 DIM 9.3125 INCH X 3 INCH, 2 EACH SHIMS SAME MAT DIM 3.5 INCH X .75 INCH AND DOUBLER FROM 2024-T3 .071 PO 900408 DIM 19 INCH X 9.25 INCH IAW B-727 SRM 53-30-3 FIG 4. 2L73 4F A3WE 20040130001912004013000191EU 2004 1 30 DHL2004364001 120040113A3240 TRANSMITTER AIRBUS300 A300B4203 3930306EU MLG BRAKE MALFUNCTIONED A DHLAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01364DH 141 AIRCRAFT SHUTTERED AND STOPPED ABRUPTLY WITH SMOOTH APPLICATION OF BRAKES WITH A SLOW TAXI SPEED. AFT OUTER BRAKE TRANSMITTER CIRCUIT BREAKER 804 B-2 POPPED. CLEANED AND RE-SEATED AFT OUTER PEDAL POSITION TRANSMITTER, AND BLED GREEN BRAKE SYSTEM. OPS CHECKED GOOD IAW M/M 32-42-00. 2L72 4F RTA35EU 20040130001922004013000192NM 2004 1 30 04FDEA00091 120040109A2841 INDICATOR DOUG MD11 MD11 3023602NM FUEL QTY MALFUNCTIONED A FDEAJ DUMP FUEL J WARNING INDICATION CRCRUISE 1 SO25616FE 48747 NR 3 FUEL QTY INDICATOR FAILED INFLIGHT. RETURN TO HKG. DUMPED 50000 LBS OF FUEL, INDICATOR RETURN TO NORMAL. MEL 28-01-01-02: TANK NR 3 FUEL TANK SYNOPTIC QTY DISPLAY INOP. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 3 QTY WITH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPERATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LAT. TAIL FUEL MGMT, INOP. 2L73 4F RTA22WE 20040130001942004013000194EU 2004 1 30 04FDEA00094 120040110A5270ABSO3O901 SWITCH AIRBUS300 A300F4605R 3930327EU CARGO DOOR DAMAGED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25655FE 742 AIR TURNBACK AFT CARGO DOOR ILLUMINATED AT 1000 ON TAKEOFF. RETURNED TO MEM AND LANDED, NO PRESSURIZATION. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 20JAN04. REMOVED AND REPLACED AFT CARGO DOOR WARNING SWITCH 34WS IAW M/M 52-71-11-4-02. OPS CHECKED GOOD. DEFERRAL CLEARED. PLACARD REMOVED RII:097606. 2L72 4F RTA35EU 20040130001952004013000195NM 2004 1 30 04FDEA00135 120040112A5753 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP, UP STOP RIB SUPPORT ISLAND FOUND 01 CRACK APPROX 0.25 INCH LONG AT OUTBOARD SIDE. 2L73 4F RTA22WE 20040130002072004013000207WP 2004 1 30 ABXA040003 120040111A2120 ODOR DOUG DC9 DC932 3022066WP CABIN DETECTED A ABXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23900AX 47380 APPROXIMATELY 5 MINUTES AFTER TAKEOFF, NOTICED PRESSURIZATION BUMPS ON CLIMBOUT FOLLOWED BY LIGHT SMOKE AND ODOR IN COCKPIT. RETURNED TO ILN. INSPECTED AFT ACCESSORY COMPARTMENT DUCT WORK AND FLUID LINES. FOUND NO VISIBLE DAMAGE OR FLUID LEAKS AND FOUND NO EVIDENCE OF FLUID RESIDUE IN DUCT WORK AROUND EITHER HEAT EXCHANGER. RAN ENGINES FOR APPROXIMATELY 2 HOURS AT VARIOUS THROTTLE SETTINGS BETWEEN 1.65 AND 1.9 EPR. 2L72 4F A6WE 20040129001312004012900131EA 2004 1 29 COMA0460010 120040102A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01805CA 7354 FLIGHT 5040 FLIGHT SPOILER AND GROUND SPOILERS MESSAGE. CYCLED C/B'S AND SYSTEM TEST NORMAL. COULD NOT DUPLICATE. 2L72 4F RTA21EA 20040129001392004012900139NM 2004 1 29 04FDEA00037 120040105A5320FXFAB773 CLIP BOEING727 727200 138407ENM FRAME CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 STRINGER 27L, FS 1130 STRINGER TO FRAME CLIP CORRODED. REMOVED AND REPLACED CORRODED CLIP IAW SRM 51-30-2. 2L73 4F RTA3WE 20040129001402004012900140NM 2004 1 29 04FDEA00036 120040105A5230FX69506771 BRACKET BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 FWD PIT - AFT COUNTER BALANCE ASSY FOR THE DOOR, THE FWD BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2. FABRICATED NEW BRACKET ON TRAVELER T2/393469 PER DWG 65-50677, P/N 65-50677-1. 2L73 4F RTA3WE 20040129001602004012900160EA 2004 1 29 COMA0460018 120040104A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01941CA 7050 FLIGHT 5833 ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040129001742004012900174EA 2004 1 29 COMA0460025 120040106A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY FLAMED OUT A COMAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO01506CA 7793 FLIGHT 5837 APU FLAMED OUT DURING T/O. RESET TRIPPED CIRCUIT BREAKER. 2L72 4F RTA21EA 20040129001902004012900190NM 2004 1 29 04FDEA00080 120040108A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5-113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT RT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A 7114 AND INSTALLED AS PER SRM 51-33-01, VOL. II. 2L73 4F RTA22WE 20040129001992004012900199NM 2004 1 29 04FDEA00071 120040108A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 635 RIGHT X=8.5. CRACKED FLOOR TRACKS AT STA 635 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL. I 2L73 4F RTA22WE 20040129002002004012900200NM 2004 1 29 04FDEA00070 120040108A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CABIN - FLOOR TRACKS CRACKED AT STA 5-78 RIGHT X=8.5. FLOOR TRACKS CRACKED AT STA 5-78 RT X=8.5 CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 V1. 2L73 4F RTA22WE 20040129002142004012900214 2004 1 29 SWAA040002 420040101A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29782SA 29808 FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVACUATION SLIDE PER MM. 2L72 4F RTA16WE 20040130000012004013000001NM 2004 1 30 SWAA040006 120040101A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR LOWER HINGE CUTOUT HAS A CRACK PROGRESSING FROM SKIN LAP FWD LOWER RADIUS. REPAIRED PER EA. 2L72 4F RTA16WE 20040130000522004013000052NM 2004 1 30 04FDEA00083 120040108A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 SCREW DAMAGE ON FRAME AT BS 1070 STR 26L WL 148. *S/D* DAMAGE ON FRAME AT BS 1070 STR 26L WL 148 OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED PER FED EX EA 7-5310-55191 AND SRM 51-40-3, 51-10-2. 2L73 4F RTA3WE 20040130000542004013000054NM 2004 1 30 04FDEA00087 120040109A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT CENTER CARGO NR 47 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED LONGERON SPLICE AT RT CTR CARGO NR 447, STA 5-113 TO STA 1541, REMOVED AND REPALCED WITH NEW SPLICE AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040130000572004013000057NM 2004 1 30 DHL2004745001 120040108A3260 WARNING LIGHT BOEING727 727224 1384076NM MLG FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 RIGHT MAIN GEAR DOOR LIGHT (S/O'S PANEL) AND RED FORWARD DOOR LIGHT REMAINED ILLUMINATED AFTER RETRACTION WITH GEAR HANDLE OFF. RAISED GEAR HANDLE TO UP AS PER ABNORMAL AND BOTH LIGHTS OUT. VERIFIED RIGHT MAIN GEAR DOOR IS GOING UP AND LOCKED. GEAR WARNING SYSTEM DEFERRED IAW MEL 32-1 CAT-C DMI 15338. REF DMI 15338 RIGHT MAIN GEAR DOOR (S/O'S PANEL) AND RED FORWARD DOOR LIGHT REMAINED ILLUMINATED AFTER RETRACTION WITH GEAR HANDLE OFF. RAISED GEAR HANDLE TO UP AS PER ABNORMAL AND BOTH LIGHTS OUT CAT-C. CANNOT DUPLICATE. OPS CHECKED GOOD PER M/M 32-00. THIS CLEARS DMI 15338. 2L73 4F A3WE 20040130000582004013000058WP 2004 1 30 0400089872 120040108A2133 OUTFLOW VALVE DOUG DC9 DC951 3022051WP CABIN PRESSURE BINDING A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01781NC 48121 WHEN AIRCRAFT LEVELED OFF AT FL330, THE CABIN STARTED TO UNCONTROLLABLE LOSE PRESSURIZATION AT 1000 FPM. OUTFLOW VALVE SHOWED FULL CLOSED SO CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. THE MAXIMUM ALTITUDE THE CABIN EVER REACHED WAS 13,500 FT AND NO MASKS DROPPED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT AT DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY, COULD NOT FIND ANY LEAKS, AND ALL DUCTING WAS SECURE. THE OUTFLOW VALVE WAS FOUND TO BE NOISY, RUNNING SLOW, AND STICKING AT TIMES. THE ACTUATOR WAS REPLACED. OPERATIONAL CHECK GOOD. 2L72 4F RTA6WE 20040130000692004013000069NM 2004 1 30 04003401 120040103A3350321431 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27401FJ 3145 DURING INSPECTION THE CENTER SECTION OF EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE BATTERY WAS FOUND DISCHARGED AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040130000752004013000075EA 2004 1 30 COMA0460031 120040108A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01467CA 7637 FLIGHT 5838 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20040130000972004013000097NM 2004 1 30 QXEA200400005 120040108A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX- DENT IN FUSELAGE SKIN PANEL BETWEEN STATION X312.35 AND X333.3 AND STRINGERS 11P AND 12P. REPAIRED IAW HORIZON AIR EA 2-53-186A. 2H72 4T RTA13NM 20040130001162004013000116 2004 1 30 QXEA200400006 420040109A3418C16258AA VANE CNDAIRCL600 CL6002C10 1390015EA AOA DAMAGED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09607QX5632 10024 PDX - FLIGHT 2422 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A STALL FAIL CAUTION MESSAGE. THE STICK SHAKER ACTIVATED WELL ABOVE APPROXIMATE STALL SPEED RANGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE DAMAGED RIGHT ANGLE OF ATTACK VANE. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040130001192004013000119NM 2004 1 30 UPS04441707 120040102A53157075T60040IN FLOORBEAM BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, BS 1220 LBL 110 FLOORBEAM WEB FOUND CRACKED AS MARKED. FLOORBEAM WEB REPLACED PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040130001302004013000130WP 2004 1 30 NACA20040004 120040108A32301330046 PIN DOUG DOUG DC6 DC6 3021702WP NLG SHEARED A NACAA UNSCHED LANDING O OTHER CLCLIMB 1 AL0343872 LS227 533294 NOSE LANDING GEAR DID NOT COME UP PROPERLY AFTER DEPARTURE. FOUND UNLATCH ROLLER PIN SHEARED, INSPECTED UPLATCH AND FOUND NO OTHER DEFECTS. REPLACED ROLLER PIN. TESTED RETRACT 5 CONSECUTIVE TIMES WITH NO PROBLEMS. CHECKED GOOD. 2L74 4R A781 20040130001342004013000134NM 2004 1 30 DHL2004782004 120040110A3260189929 UPLOCK SENSOR BOEING727 727227 1384078NM MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01782DH 21998 LEFT GEAR RED UNSAFE LIGHT ON WITH GEAR UP. RAN ABNORMAL PROCEDURE. REMOVED AND REPLACED LEFT GEAR UP LOCK SENSOR IAW B-MM 32-61-81. OPS CHECKED GOOD IAW B-MM 32-61-81. INSTALLED 1 EA SENSOR P/N: 1-899-29. 2L73 4F A3WE 20040130001392004013000139WP 2004 1 30 AALA20040044 120040110A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2176201 53291 MIA CEILING EMERGENCY LIGHTS FROM ROW 13 TO 17 INOPERATIVE. REPLACED BATTERY PACK R5-102 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040130001472004013000147EU 2004 1 30 AALA20040053 120040109A2913PV32402F PUMP AIRBUS300 A300B4605R 3930308EU HYD SYSTEM INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2114056 463 EWR INFLIGHT/T881/09 YELLOW HYDRAULIC SYSTEM LOW PRESSURE ECAM WARNING. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040130001512004013000151NM 2004 1 30 04FDEA00103 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001712004013000171NM 2004 1 30 CALA0400017 120040109A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712322 23373 INSPECTION FOUND STRINGER 25L CORRODED AFT OF STA 967. A REPAIR WAS INSTALLED IAW SRM 53-60-03 AND 53-00-03. 2L72 4F RTA16WE 20040130001752004013000175NM 2004 1 30 DHL2003752502 120040104A5230 SKIN BOEING727 727223 1384074NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR NR 1 CARGO DOOR SKIN IS DENTED LOWER AFT SIDE. DAMAGE FOUND TO BE OUT OF LIMITS IAW B-727 SRM 52-00-02. CUT OUT DAMAGED AREA DIM 1.75 INCH X 1 INCH AND FABRICATED DOUBLER REPAIR FROM MAT 2024-T3 .050 PO 900471 DIM 7.25 INCH X 6.75 INCH IAW B-727 SRM 52-00-3 FIG 3. TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR FROM NR 1 CARGO DOOR SKIN IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040130001842004013000184NM 2004 1 30 2004UALA00010 120040105A335058781 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHTSDAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29304UA 23665 EEL LIGHT INOP FROM ROW 15A BACK. REPLACED FEEDER STRIP FROM SIDE WALL TO ROW 20. ALSO REPLACED EEL AT AFT GALLEY AND COVER FROM ROW 15 TO 21. 2L72 4F4 FRTA16WE E2GL 20040130001972004013000197NM 2004 1 30 04FDEA00137 120040113A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CABIN - SURFACE CORROSION FOUND ON FLOOR SUPPORT AT STA 5-0 (APPROXIMATELY STA 1531) RT X = 8.5. SURFACE CORROSION AT CABIN FLOOR TRACKS STA 5-0 (APPROXIMATELY STA 1531) RT X=8.5 REMOVED AS PER SRM 51-21-01 VOL 2, MATERIAL THICKNESS, 0.080 INCH, THICKNESS REMAINED 0.075" & FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL 1. 2L73 4F RTA22WE 20040130001992004013000199NM 2004 1 30 04FDEA00139 120040113A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. LT OTBD FLAP OTBD HINGE (WING MOUNTED), OTBD ACTUATOR LUG HOLE BORE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5740-74286, WINGS - LT & RT OTBD FLAP, OTBD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040130002012004013000201NM 2004 1 30 04FDEA00141 120040113A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040130002172004013000217EU 2004 1 30 AWXA200400028 120040112A3350ABS0374B HOUSING AIRBUS320 A320231 3930325EU SEAT ROW 13 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 PHX - EEL - DURING E-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT HOUSING AT SEAT ROW 13 LT BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HOUSING AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040130002182004013000218EU 2004 1 30 AWXA200400029 120040112A3397ABS0374A24 CABLE AIRBUS320 A320231 3930325EU SEAT ROW 5 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 PHX - EEL - DURING E-01 CHECK FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 5 LT. MAINTENANCE REPAIRED THE BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040130002232004013000223EU 2004 1 30 AWXA200400034 120040111A3231D23071001 ROD END AIRBUS320 A320231 3930325EU NLG DETACHED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28628AW314751197 67 AFTER TAKEOFF, NLG FAILED TO RETRACT, CYCLED MLG TO DOWN POSITION & GEAR INDICATED DOWN & LOCKED. TURNED BACK & LANDED WITHOUT EVENT. MAINT FOUND NLG RETRACT ACTUATOR PISTON ROD END HAD SEPARATED FROM BEARING. R & R NLG RETRACT ACTUATOR IAW AMM 32-31-22, CYCLED GEAR SEVERAL TIMES WITH NO FAULTS NOTED. INVESTIGATION OF NLG RETRACT ACTUATOR FOUND PISTON ROD END BORE ELONGATED WHICH IS BELIEVED TO HAVE BEEN CAUSED BY FORCES APPLIED DURING RETRACTION & EXTENSION. CONTINUED OPERATION IN THIS CONDITION CAUSED BEARING THAT ALSO HAD INDICATIONS OF EQUAL DISTORTION TO MIGRATE OUT OF ROD END BORE. OTHER FINDINGS INDICATED THAT THE SWAGING OF THE BEARING WAS INADEQUATE & BEARING HOUSING MATERIAL MAY NOT BE ABLE TO WIT2L72 4F RTA28NM 20040130002352004013000235EU 2004 1 30 MALA040107 120040104A3150 WARNING LIGHT SAAB SF340 340B 7860101EU COCKPIT FALSE ACTIVATIONA MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15448XJ 340B448 DURING FLIGHT 2735, OAT INDIATIONS ON CAP AND F/O'S SIDE INOP. FLIGHT DIRECTOR AND A/P INOP. AIR RETURN TO DTW. MAINTENANCE UNABLE TO DUPLICATE PROBLEM CHECKED PROBE RESISTANCE AND HEATING. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040130002422004013000242 2004 1 30 SWIA200412756 420040105A2210 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07429SW 7518 YAW DAMPER 2 WOULD NOT ENGAGE. REMOVED AND REPLACED YAW DAMPER PANEL. OPS CHECK GOOD AT THIS TIME. P/N OFF: 601R51594-1. 2L72 4F RTA21EA 20040130002482004013000248EA 2004 1 30 SWIA200412762 120040105A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07430SW4266 4266 7523 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 2 ELBP IAW 33-51-04. OPS CHECK GOOD. 2L72 4F RTA21EA 20040202000012004020200001NM 2004 2 2 04FDEA00147 120040113A2740 POWERPACK BOEING727 727200 138407ENM RT ELEVATOR CONTAMINATED A FDEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO25283FE 22350 WITH AUTOPILOT DISENGAGED AT CRUISE FLT, UNCOMMANDED FWD/AFT MOVEMENT OF CONTROL WHEEL HAD TO BE COUNTER-ACTED WITH FIRM PRESSURE. UNCOMMANED MOVEMENT OF CONTROL WHEEL SEEMED TO LESSEN WITH SLOWER AIRSPEED (310-200 KIAS). THIS PROBLEM WAS DISCOVERED AFTER DISENGAGING A/P BECAUSE OF ACCOMPANYING WRITE UP. WITH -A- AND B-HYD SYSTEMS PRESSURIZED, A/P OFF AND C/B'S PULLED, FOUND RT ELEVATOR TRIM TAB WOULD DEFLECT INTERMITTENTLY. REMOVED LARGE COMPACTED BIRD NEST FROM RT ELEVATOR POWER PACKAGE BAY AND BLED B-SYSTEM WITH BLEED NEXT TO B-MODULAR PACKAGE IN AFT STAIR WELL. RT TRIM TAB NOW IS STEADY. CHECKED ELEVATOR TRIM TABS AND ELEVATORS FOR BINDING. OPS CHECKS GOOD PER MM 27-30-000-5. 2L73 4F RTA3WE 20040202000022004020200002NE 2004 2 2 NACA20040005 220040111A853076271 CAM DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 1 ENGINE FAILED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 AL032907F1040 1040 533265 510065 NR 1 ENGINE SHUTDOWN DUE TO DOUBLE SHORTED SECONDARY ON NR 5 & 13 CYLINDERS. REPLACED NR 1 ENGINE DUE TO REAR CAM FAILURE. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040202000032004020200003NM 2004 2 2 DHL2004753503 120040108A5330 SKIN BOEING727 727223 1384074NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, FWD ENTRY DOOR (L1) LWR HINGE CUTOUT CRACKED NDT VERIFIED BS 310. REMOVED FASTENERS PER ACCESS AT FWD ENTRY DOOR LOWER HINGE IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA DIM APPROX 1 INCH X BY .375 INCH IAW S/B 727-53-0198. PART MADE FROM P/N 301 .5 INCH HD, .063 INCH DIM APPROX 17 INCH BY 6.5 INCH IAW S/B 727-53-0198. TREATED BARE METAL AROUND CUTOUT LOWER HINGE FWD ENTRY DOOR AND PRIMED PART REPAIR IAW B-727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT FWD ENTRY DOOR LOWER CUT OUT IAW S/B 727-53-0198. 2L73 4F A3WE 20040202000042004020200004NM 2004 2 2 DHL2004F00000 120040106A5330 SKIN BOEING727 727223 1384074NM FUSELAGE MISREPAIRED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, VERIFY CONFORMITY OF EXTERNAL REPAIR BS 259-264 STR 11L-12L 5 X 6 INCH DIM. REMOVED FASTENERS AND EXTERNAL REPAIR BS 259, 264, STR 11L-12L IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER, MATERIAL USED 2024 T-3 .050, PO 900414. DIMENSION 7.75 X 4 INCH SKIN IDENTIFICATION 53-30-2 FIG 2 IAW B-727 SRM 53-30-3 FIG 3A. ALODINED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040202000072004020200007NM 2004 2 2 QXEA200400010 120040111A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - NR 1 NACELLE THE LEFT HAND FORWARD SPINE COWL CLIP IS CRACKED ON FORWARD LEG OF CLIP BY BOLT HEAD. REPAIRED IAW HORIZON AIR EA 6-54-282 AND SRM 51-42-65. 2H72 4T RTA13NM 20040202000102004020200010EA 2004 2 2 COMA0460032 120040103A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01924CA 7026 REPAIR WING PLANK CRACK AT WS 148.019 RIGHT HAND SIDE. REPAIRED RT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WITH AEROSPACE REPAIR ENGINEERING ORDER 601R-57-21-130. 2L72 4F RTA21EA 20040202000112004020200011EA 2004 2 2 COMA0460034 120040109A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01443CA 7539 FLIGHT 5603 BURNING ODOR IN COCKPIT. COULD NOT DUPLICATE. RAN ENGINES AND APU AND NO BURNING ODOR FOUND. 2L72 4F RTA21EA 20040202000122004020200012EA 2004 2 2 COMA0460035 120040109A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01442CA8147 7483 FLIGHT 5553 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTS BATTERIES. 2L72 4F RTA21EA 20040202000132004020200013EA 2004 2 2 COMA0460036 120040110A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01999CA 7230 FLIGHT 5708 - CABIN DOOR OUTER HANDLE CAUTION. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040202000142004020200014EA 2004 2 2 COMA0460037 120040110A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 LACK OF LUBE A COMAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO01457CA 7612 FLIGHT 5123 NR 2 GENERTOR OFFLINE DURING RESET ADG DEPLOYED. SERVICED THE NR 2 IDG OIL SYSTEM, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040202000162004020200016GL 2004 2 2 MASA200400019 220040110A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 SHUTDOWN A MASAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SW07860MJ 145773 312513 ASH 2607 ROC-DCA. NR 1 ENGINE SHUTDOWN AFTER PERFORMING FADEC RESET AS A PART OF DE-ICE PROCEDURES. RETURNED TO GATE, MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USED. 2L72 4T4 FRTT00011ATTE6CH 20040202000192004020200019WP 2004 2 2 UPS04841712 120040106A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STATION 1726 AND 1746 AND LONG 15L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040202000212004020200021EA 2004 2 2 QXEA200400013 120040108A5230 DEFLECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DETERIORATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX4867 10031 PDX - MAINTENANCE FOUND THAT THE FORWARD CARGO DOOR DEFLECTOR SEAL IS DETERIORATED. THE SEAL WAS REPLACED IAW THE CRJ-700 SRM 51-42-06 AND 51-41-02. 2L72 4F RTA21EA 20040202000222004020200022NM 2004 2 2 DHL2004752507 120040104A5330 SKIN BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR BS 300 TO 294.5 ABOVE STR 25R AREAS OF SKIN BULGING AND DENTS. REMOVED RT WALKWAY HORIZ WEB FOR ACCESS, AREAS FOUND TO BE OUT OF LIMITS. CUT OUT 2 EA AREAS 5 INCH X 1.625 INCH + 2.75 INCH X 1.75 INCH. FABBED 2 FILLERS FROM 2024-T3.050 PO 900505 DIM 5.125 INCH X 2.75 INCH X 1 INCH STRUCTURAL FILLER DIM 19.125 INCH X 2.75 INCH AND DOUBLER FROM 2024-T3.063 PO 900355 DIM 19.875 INCH X 10.125 INCH IAW B-727 SRM 53-30-3 FIG 4. TREATED AND PRIMED PARTS AND AREA IAW B-727-SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727-SRM 53-30-3 FIG 4. REINSTALLED RT WALKWAY HORIZ WEB IAW B-727-SRM 51-30-2. 2L73 4F A3WE 20040202000232004020200023EA 2004 2 2 QXEA200400014 120040106A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA PAX DOOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX5257 10005 PDX - THE MAIN CABIN DOOR FORWARD LOWER SKIN REQUIRES PERMANENT REPAIR. MAINTENANCE FABRICATED REPAIR STRAP AND FILLERS FROM 2024T3 AND INSTALLED SAME IAW EA R-52-132A AND REO 670-52-11-040. 2L72 4F RTA21EA 20040202000242004020200024NM 2004 2 2 DHL2004752508 120040106A5754 ANGLE BOEING727 727223 1384074NM LE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, RT WING WBL 130.7 HAS CRACK IN L-ANGLE OF L/E FLAP AREA. STOP DRILLED CRACK IAW 727 SRM 51-10-1 & FABBED REPAIR ANGLE FROM 2024T3050 DIM 6 INCH X 2 INCH PO 900471 IAW 727 SRM 51-40-3 FIG 1. REPAIR TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040202000252004020200025NM 2004 2 2 QXEA200400015 120040105A5753 FITTING BOMBDRDHC8 DHC8401 1390041NM FLAP CARRIAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX4954 4051 PDX - THE OUTBOARD FLAP AT THE NR 4 TRACK CARRIAGE FRONT SPAR ATTACHMENT INBOARD BRACKET, OUTBOARD LUG, HAS SOME CHAFE DAMAGE. REPAIRED DAMAGED AREA IAW RD 8/4-57-228. THE GAP CHECK IS WITHIN LIMITS. 2H72 4T RTA13NM 20040202000262004020200026NM 2004 2 2 DHL2004752504 120040106A5754 SKIN BOEING727 727223 1384074NM FOREFLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, LT INBOARD FOREFLAP UPPER INBOARD SURFACE PREVIOUS REPAIR DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIR. FABRICATED FILLER APPROX 13 INCH X 13 INCH AND DOUBLER APPROX 13 INCH X 5 INCH FROM 2024 T3 .016 PO 900291. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER AND ADHESIVE TO ALL REPAIR PARTS. BONDED, CLEANED, TREATED, PRIMED AND SEALED REPAIR IAW B-727 SRM 57-50-1 FIG 3, 51-40-6 FIG 2, 57-50-2 FIG 3, 51-40-20 FIG 30. BONDED RUBSTRIP IAW B-727 MM 51-51-11. 2L73 4F A3WE 20040202000272004020200027NM 2004 2 2 AWXA200400042 120040107A5753693720910 SUPPORT BOEING737 73733A 1384673NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REPLACED RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057. 2L72 4F RTA16WE 20040202000282004020200028NM 2004 2 2 AWXA200400043 120040107A575369406579 SUPPORT BOEING737 73733A 1384673NM TE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REPLACED LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT PER AWA T/C I3R57057. 2L72 4F RTA16WE 20040202000292004020200029NM 2004 2 2 AWXA200400044 120040113A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28156AW 23778 DEN - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE EMERGENCY FLASHLIGHT AT THE AFT JUMP SEAT INOPERATIVE. REMOVED AND REPLACED THE AFT JUMP SEAT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040202000332004020200033EU 2004 2 2 RAIA00401007 120040106A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03550HK 41039 MX-STL- EMERGENCY PATH LIGHTS INOP. MAINTENANCE RESECURED CONNECTOR TO EMERGENCY PATH LIGHTS. 2L72 4T RTA41NM 20040202000352004020200035CE 2004 2 2 DXTA200400216 120040113A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07337QS 5600437 DURING TAXI, CO-PILOT LEFT BRAKE PEDAL GOES TO THE FLOOR DURING BRAKE APPLICATION, PILOT BRAKES OPERATE NORMALLY. INSPECTED CO-PILOT'S MASTER CYLINDER, NO DEFECTS FOUND. APPLIED HYDRAULIC POWER AND CHECKED LEFT BRAKE PEDAL AND NOTICED IT WAS SPONGY. BLED BRAKE SYSTEM IAW CESSNA MM CHAPTER 32-42-00, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20040202000372004020200037NM 2004 2 2 EIA2004001 120040105A3350 LIGHT BOEING747 747121 1384871NM ESCAPE SLIDE INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 CEILING EMERGENCY LIGHT IN AISLE TO ESCAPE SLIDE INOP. DMI ACCOMPLISHED. ITEM TO REMAIN OPEN TILL FIXED. 2L74 4F A20WE 20040202000422004020200042NE 2004 2 2 EIA2004005 220040112A7270 GUIDE VANE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 4 ENGINE MISSING A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 663076 ON POST FLIGHT WALKAROUND FOUND FAN EXIT GUIDE VANE MISSING AT 6:30 POSITION ON NR 4 ENGINE. VANE STRUCK T/E OF T/R SLEEVE CAUSING TEAR AT 6:30 POSITION AND PUT A HOLE IN THE LT INBOARD COWL. TRANSFERRED TO COI NR 053 MAX 50 HRS FLY BACK ENGINE SCHEDULED AT MZJ DUE AT 98908 PER MM 72-31-05 PAGE 604. REPAIRS MADE TO COWL AND SLEEVE. 2L74 4F4 F A20WE E20EA 20040202000432004020200043EA 2004 2 2 QXEA200400016 120040114A308054011484 VALVE CNDAIRCL600 CL6002C10 1390015EA ANTI ICE SYS INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09600QX1504 256 10005 SMF FLIGHT 2527 RETURNED TO FIELD. RIGHT COWL ANTI ICE FAULT CAUTION MESSAGE WHEN SELECTED ON. REPLACED VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040202000442004020200044NM 2004 2 2 P5CA0401028 120040114A7932J221P124 O-RING BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 1 ENGINE DISPLACED A P5CAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP23452PA 30810 706222 NR 1 ENG HAD LOSS OF OIL QUANTITY. ENG SHUT DOWN & RETURN TO MIA. FOUND GEARBOX CRANKPAD COVER O-RING CUT, 50 PERCENT OF RING DISPLACED. REPLACED SAME, RESERVICED ENG OP'S & LEAK CHECK OK. 2L74 4F4 FRTA20WE E23EA 20040202000502004020200050WP 2004 2 2 AALA20040067 120040114A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21965TW 53615 DFW EMERGENCY PATH LIGHT AT ROW 12 INOPERATIVE. FOUND CONNECTOR LOOSE AT ROW 12 LIGHT ASSEMBLY. RESECURED CONNECTOR FOR EMERGENCY PATH LIGHT ASSEMBLY AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040202000512004020200051WP 2004 2 2 AALA20040068 120040114A253046700017 COFFEEMAKER DOUG DC9 DC982 3022082WP GALLEY SHORTED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2190511 49805 MIA INFLIGHT FUMES WERE SMELLED IN COCKPIT AND FORWARD GALLEY. LIGHT SMOKE DETECTED IN FORWARD GALLEY. EMERGENCY DECLARED AND LANDED AT MSY. NO PASSENGER OR CREW ILLNESS. FOUND COFFEEMAKER WIRE SHORTED AND BURNED ON WATER SENSOR ON NUMBER 1 COFFEEMAKER. REPLACED NUMBER 1 COFFEEMAKER IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040202000522004020200052WP 2004 2 2 AALA20040066 120040114A259783700249 HARNESS DOUG DC9 DC982 3022082WP ESCAPE SLIDE DAMAGED A AALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW21577AA 53154 DFW SECURITY ISSUE. AIRCRAFT RETURNED TO STATION. UPON LANDING TAIL CONE WAS DROPPED BUT EMERGENCY EVACUATION SLIDE DID NOT DEPLOY. FOUND SLIDE PROPERLY CONNECTED TO COVER. TAB SNAP BUTTON ON TAIL CONE LANYARD DAMAGED. WOULD NOT SNAP TO COVER. LANYARD ATTACHED TO COVER BY VELCRO ONLY. REPLACED SLIDE, TAIL CONE AND LANYARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040202000542004020200054EA 2004 2 2 04003651 120040103A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM CONTAMINATED A VTZAA UNSCHED LANDING CF F.O.D. FLT CONT AFFECTED CLCLIMB 1 EA27651BR 7426 DURING CLIMB OF FLIGHT 7267 CREW REPORTED STABILIZER TRIM SYSTEM 1 AND 2 FAILURE MESSAGES. CREW DECLARED EMERGENCY AND RETURNED TO ORD. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. THE DISCONNECT SWITCHES WERE FOUND ENGAGED DUE TO FOD AND WERE CLEANED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040202000552004020200055 2004 2 2 016041 420040114A2210 COMPUTER BEECH 1900 1900C 1154161CE YAW DAMPER MALFUNCTIONED A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27210CJ UC110 RT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C. 2L72 4T RTA24CE 20040202000602004020200060EA 2004 2 2 04010676 120040110A5610NP1393226 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27676BR 7644 DURING CRUISE OF FLIGHT 7832 CREW REPORTED FIRST OFFICERS SIDE WINDOW CRACKED. CREW RETURNED TO IAD AND FLIGHT LANDED UNEVENTFULLY. PASSENGERS WERE DEPLANED NORMALLY. THE WINDOW WAS REPLACED AND A SATISFACTORY PRESSURIZATION CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040202000612004020200061EA 2004 2 2 04014645 120040114A33508GS00542405 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27645BR 7383 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LAMP WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040202000622004020200062 2004 2 2 372PA0040 420040110A2230106201730 COMPUTER BOEING737 737306 13844BGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION CLCLIMB 1 SO05372PA 23546 AUTOTHROTTLE DISCONNECTED ON TAKEOFF AND INITIAL CLIMB THROUGH 16,000. PLACED ON MEL 22-4. REPLACED AUTOTHROTTLE COMPUTER PER MM 22-31-10. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20040202000632004020200063EA 2004 2 2 04014662 120040114A27501104SD100501 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DAMAGED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27662BR 7526 DURING CLIMB OF FLIGHT 7643 CREWED RECEIVED A FLAP SYSTEM FAILURE MESSAGE AT 8 DEGREES. CREW RETURNED TO YUL, FLIGHT LANDED UNEVENTFULLY, AND PASSENGERS DEPLANED NORMALLY. THE NR 5 FLEX DRIVE SHAFT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040202000642004020200064EA 2004 2 2 04014671 120040114A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT WORN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING INSPECTION THE AFT PORTION OF THE EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE CONNECTOR WAS FOUND WORN AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040202000662004020200066EA 2004 2 2 SWIA200412764 120040112A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 F/O STAB TRIM INOPERATIVE. REMOVED AND REPLACED F/O'S STAB TRIM SWITCH IAW AMM 27-41-05. OPS CHECK GOOD. P/N: 309-4334. 2L72 4F RTA21EA 20040202000682004020200068EA 2004 2 2 SWIA200412766 120040111A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07587SW5887 5887 7062 HORIZONTAL STAB TRIM WILL NOT ENGAGE, EITHER CHANNEL. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL IAW MM 27-42-01. OPS CHECKS GOOD. P/N: 7062-3, S/N OFF: 135. 2L72 4F RTA21EA 20040202000702004020200070EA 2004 2 2 SWIA200412768 120040112A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07946SW1816 1816 7776 STAB TRIM CHANNEL 1 WILL NOT ENGAGE ON THE GROUND. REMOVED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT AND INSTALLED SERVICEABLE UNITS IAW MM 27-40-00. STAB TRIM OPS CHECKS GOOD. P/N: 7062-3, S/N ON: 606, S/N OFF: 851. 2L72 4F RTA21EA 20040202000712004020200071SO 2004 2 2 SWIA200412769 120040112A2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO RT ELEVATOR MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07301YV 120301 ON TAKEOFF, RECEIVED TAKEOFF TRIM AURAL WARNING WITH TRIM SET AT 25 PERCENT. ABORTED TAKEOFF. REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW 120 MM 27-32-05. OPS CHECK GOOD. 2L72 4T RTA31SO 20040202000722004020200072EA 2004 2 2 SWIA200412770 120040113A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07908SW 7540 RIGHT WINDSHIELD CRACKED (OUTER PLY) ON CLIMBOUT. RETURNED TO AIRPORT. REPLACED RIGHT WINDSHIELD IAW MM 56-00-00 AND RII CARD RII 56-402. P/N: NP-13, S/N OFF: 01094H4926. 2L72 4F RTA21EA 20040202000732004020200073SO 2004 2 2 SWIA200412771 120040107A1230 HYDRAULIC SYSTEM EMB 120 EMB120ER 3260203SO LT (GREEN) LOW A SWIAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM07298SW 120328 LEFT (GREEN) HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED. QUANTITY GAUGE READ ZERO. (MADE EMERGENCY LANDING DEN) SERVICED HYDRAULIC SYSTEMS. RAN ENGINES, SWUNG GEAR AND OPERATED ALL GREEN HYDRAULIC SYSTEM COMPONENTS. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040202000802004020200080NM 2004 2 2 04FDEA00149 120040115A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT BORE AREA. LT INBD FLAP OTBD HINGE (FLAP SIDE) INBD PIVOT HOLE BORE CORROSION. REMOVED AND REPAIRED AS PER EA 1-5750-74282, WINGS - LEFT INBD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20040202000832004020200083NM 2004 2 2 04FDEA00152 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), PIVOT HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040202000842004020200084EA 2004 2 2 COMA0460039 120040114A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FS 310 FUSELAGE SKIN PREVIOUS BETYWEEN STRINGERS 16 AND 17 HAS SUSTAINED FURTHER DAMAGE. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER FROM 2024-T3.063 (WVAC PO 32512) AND 2024-T3.050 (WVAC PO 29669/1), INSTALLED IAW BOMBARDIER, INC REO 601R-53-21-180. 2L72 4F RTA21EA 20040202000872004020200087NM 2004 2 2 04FDEA00155 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040202000882004020200088NM 2004 2 2 04FDEA00156 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. RT OTBD FLAP OTBD HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, WINGS - LT AND RT OTBD FLAP - OTBD HINGE BRACLET ASSEMBLY CORROSION. AND DWG ARC0503 AND CMM 57-44-08 AND FOUND WITHIN LIMITS. 2L73 4F RTA22WE 20040202000912004020200091NM 2004 2 2 04FDEA00159 120040115A5320 STIFFENER DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 STIFFENER CRACKED. MAIN CARGO DECK RT 1169 BETWEEN SEAT TRACK REF X = 47.5 AND X = 75.25 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED STIFFENER AS PER DWG NR NPB6272. FABRICATED STIFFENER PROTECTED AND PAIN TOUCH UP AS PER SRM 51-21-01 VOL II. PART MARK AS PER GMM 7-0-1001. FABRICATED STIFFENER INSTALLED AS PER SRM 51-33- 01 VOL II. 2L73 4F RTA22WE 20040202000922004020200092NM 2004 2 2 04FDEA00160 120040115A5320 STIFFENER DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RIGHT STA 1169 BETWEEN SEAT TRACK REF X = 27.5 AND X = 47.5 STIFFENER CRACKED. MAIN CARGO DECK RT STA 1169 BETWEEN SEAT TRACK REF. X = 27.5 AND X = 47.5 CRACKED STIFFENER REMOVED AS PER SRM 51-31-01, VOL.II. STIFFENER FABRICATED IAW DRAWING NR NPB 6272. FABRICATED STIFFENER PROTECTED AND PAINT TOUCHED UP AS PER SRM 51- 21-01, VOL. II. PART MARKED AS PER GMM 7-0-1001. FABRICATED STIFFENER INSTALLED I.A.W SRM 51-33- 01, VOL.II. 2L73 4F RTA22WE 20040202000952004020200095NM 2004 2 2 04FDEA00165 120040115A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. GUIDE RAIL UPPER FLANGE BETWEEN STA 1541 TO STA 5-113 CORROSION REMOVED. ORIGINAL THK 0.090 MATERIAL REMAINING 0.078 MIN. WITHIN LIMITS PER SRM 53-00-01 FIG 3 VOL 1 2L73 4F RTA22WE 20040202000962004020200096NM 2004 2 2 04FDEA00166 120040115A3260 CONNECTOR BOEING727 727100 1384036NM MLG CONTAMINATED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25151FE 19147 ON APPROACH, UPON LOWERING LANDING GEAR, NOSE GEAR INDICATED UNSAFE (RED GEAR LIGHT ON, GREEN LIGHT OUT). RAN EMERGENCY PROCEDURES, CYCLED GEAR AND GOT 3 DOWN INDICATIONS. CLEANED SNOW AND ICE FROM LOCK AND POSITION SWITCHES CLEANED CONNECTOR. NOSE GEAR STILL SHOWS GREEN DOWN AND LOCKED INDICATION. OK FOR SERVICE. 2L73 4F RTA3WE 20040202000972004020200097EA 2004 2 2 COMA0460040 120040114A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 LEFT WING LOWER WING PLANK SKIN AT WS 148.00 IS CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLERS FROM 2024-T3.125 (WVAC PO 21137) AND FILLER FROM 2024-T3.100 (WVAC PO 27013), INSTALLED IAW BOMBARDIER, INC REO 601R-57-21-120 REV D. 2L72 4F RTA21EA 20040202000982004020200098EA 2004 2 2 COMA0460041 120040114A5320601R311711 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FS 484 LBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC. REO601R-53-41-059. 2L72 4F RTA21EA 20040202000992004020200099EA 2004 2 2 COMA0460042 120040114A5320601R311712 ANGLE CNDAIRCL600 CL6002B19 1900309EA FS 484 CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FS 484 RBL 36 INBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-41-059. 2L72 4F RTA21EA 20040202001002004020200100EA 2004 2 2 COMA0460043 120040114A5320601R3117117 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FS 484 LBL 27 OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE, FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-41-059. 2L72 4F RTA21EA 20040202001012004020200101GL 2004 2 2 04FDEA00167 220040113A7200 ENGINE DOUG DC10 DC1010F 3022111WP GE CF6 CF6* 30020GL NR 3 FAILED A FDEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO25383FE 46616 AT CRUISE THRUST, NR 3 ENGINE STARTED COMPRESSOR STALLING FL 310. ALL PARAMETERS SHOWING MAJOR FLUCUATIONS, ALONG WITH AIRCRAFT YAW. NR 3 THROTTLE PULLED TO IDLE AND ALL INDICATIONS STABILIZED. AFTER A FEW MINUTES N1 STARTED FLUCUATIONS OF 10-12 PERCENT AND EGT 60 DEG CELSIUS. ENGINE SHUTDOWN AND DIVERTED TO MEM. THERE IS TIP CLANG ON SEVERAL STAGES OF THE HIGH PRESSURE COMPRESSOR. REMOVED AND REPLACED NR 3 ENGINE AS PER FED EX WORK CARDS 71T0701-3, LEAK AND OPS CHECK GOOD. A/C RETURNED TO SERVICE. 2L73 4F4 F A22WE E23EA 20040202001032004020200103EA 2004 2 2 COMA0460045 120040114A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FLOORBEAM CAP AT FS 559+12 TO 620 AT LBL 27 CORRODED. REMOVED AND REPLACED CAP IAW WVAC EO 601R-53-4581. 2L72 4F RTA21EA 20040202001052004020200105EA 2004 2 2 COMA0460047 120040114A5320601R3220823 STIFFENER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 VERTICAL BEAM CRACKED AT BL 0 BULKHEAD WEB AT FS 409+128 TOP RIVET LOCATION ON REINFORCING PLATE. PERFORMED A MAJOR REPAIR TO CRACKED VERTICAL BEAM, FS 409+128 BL 0 (TOP RIVET ON REINFORCING PLATE) BY TRIMMING OUT CRACKED PORTION OF STIFFENER, FABBING FILLER AND REPAIR ANGLE, AND INSTALLING PER WVAC EO 601R-53-4572 AS APPROVED BY FAA FORM 8110-3 DATED 1-12-2004. 2L72 4F RTA21EA 20040202001072004020200107NM 2004 2 2 C1HA200474001 120040112A3520 OXYGEN MASK BOEING727 727225 1384077NM CABIN WILL NOT TEST A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15674MG 21450 TRANSFERRED FROM NR M12 ALL CABIN O2 MASKS FAILED DROP TEST (FAA CONE), DEPLOYED ALL PAX & F/A O2 MASKS. CLEANED ALL MASK ASSY IAW MM 35-21-49, RESTOWED ALL O2 MASKS IAW MM 35-21-51. PERFORMED INSPECTION CHECK IAW MM 35-21-44. PERFORMED TEST IAW MM 35-21-00. RETURN SYSTEM IAW MM 35-21-00 PG 201. 2L73 4F A3WE 20040202001082004020200108NM 2004 2 2 C1HA200482001 120040114A3231 SWITCH BOEING727 7272S7 138407ZNM RT MLG DOOR OUT OF ADJUST A C1HAO OTHER J WARNING INDICATION CLCLIMB 1 GL15682CA 22019 AFTER TAKEOFF ON GEAR RETRACTION, RIGHT GEAR DOOR LIGHT STAYED ILLUMINATED. RAN COM PROCEDURE 2.32.29. ADJUSTED RIGHT MLG DOOR SWITCH PER CHAMPION AIR MM 32-62-11, OPS CHECK NORMAL. 2L73 4F A3WE 20040202001092004020200109NM 2004 2 2 PCAA0401155 120040115A3060 DEICE SYSTEM DHAV DHC8 DHC8102 2809003NM NR 2 PROPELLER ARCED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA13831EX251815717 160 FLIGHT 3841 ON CLIMBOUT FROM SYRACUSE HAD TO RETURN TO FIELD DUE TO SPARKS BEING OBSERVED COMING FROM THE NR 2 PROP. NO EMERGENCY DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 PROP BLADE ON THE RIGHT HAND SIDE TO BE AT FAULT. BLADE WAS REMOVED AND REPLACED, OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202001112004020200111NM 2004 2 2 DHL2004752510 120040114A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR AT BS 420, BETWEEN STR 23R AND STR 24R DENT IN SKIN. DAMAGE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 1 INCH DIA AND FABBED FILLER FROM 2024-T3 .050 PO 900471 DIM 1 INCH AND DOUBLER FROM 2024-T3 .063 PO 900355 DIM 3.9375 INCH DIA IAW B-727 SRM 53-30-2 FIG 13 AND 53-30-2 FIG 2. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 13. 2L73 4F A3WE 20040202001142004020200114EA 2004 2 2 COMA0460050 120040112A7700 MONITOR CNDAIRCL600 CL6002B19 1900309EA RT ENG VIBRATIONMALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01962CA 7123 FLIGHT 5701 RIGHT ENGINE VIBRATION INDICATION DURING T/O. COULD NOT DUPLICATE. RESET VIBRATION MONITOR, RUN CHECKS WERE NORMAL. 2L72 4F RTA21EA 20040202001152004020200115EA 2004 2 2 COMA0470007 120040112A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01398CA 10112 FLIGHT 5079 RIGHT THRUST REVERSER UNSAFE MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040202001162004020200116EA 2004 2 2 COMA0460051 120040115A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 WHILE PERFORMING TASK 002-57-900-60/601 FOUND CORROSION ON THE LOWER RT WING PLANK ACCESS HOLE CUTOUT (FOR PANEL 640BB) ON THE FORWAD AND AFT CHAMFERS. REMOVED THE CORROSION AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV C. 2L72 4F RTA21EA 20040202001172004020200117SO 2004 2 2 C2XA04IA007 120040113A3350RPS1B CHARGER EMB 145 EMB145LR 3260212SO EMERGENCYLIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714543 145553 FLIGHT 3462 - PILOT REPORTED THAT THE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED A EMERGENCY LIGHT BATTERY CHARGER AND OPERATIONALLY TESTED THE LIGHTING SYSTEM. 2L72 4T RTT00011AT 20040202001192004020200119EA 2004 2 2 COMA0460053 120040114A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 GENERATOR LACK OF LUBE A COMAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 SO01991CA 7216 FLIGHT 5251 IDG NR 1 FAULT MESSAGE DURING T/O. SERVICED THE IDG OIL SYSTEM. 2L72 4F RTA21EA 20040202001202004020200120EA 2004 2 2 COMA0460054 120040114A2150 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT SMOKE A COMAF ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 SO01804CA 7352 FLIGHT 5176 CARGO SMOKE WARNING, DISCHARGED FIRE BOTTLES. DEFERRED MAINT ON RIGHT ACM. 2L72 4F RTA21EA 20040202001212004020200121EA 2004 2 2 COMA0460055 120040114A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01484CA 7702 FLIGHT 5016 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040202001222004020200122NE 2004 2 2 COMA0460056 220040112A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT VIBRATION A COMAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01810CA9591 7370 807608 FLIGHT 5402 RIGHT ENGINE VIBRATION AND LOSS OF OIL PRESSURE IFSD. REPLACED THE RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040202001232004020200123NE 2004 2 2 COMA0470008 220040114A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RIGHT VIBRATION A COMAD RETURN TO BLOCK EJ VIBRATION/BUFFET WARNING INDICATION TXTAXI/GRND HDL 1 SO01376CA 10092 FLIGHT 5874 RIGHT ENGINE VIBRATION CAUTION MESSAGE. COULD NOT DUPLICATE. RUN CHECKS WERE NORMAL. 2L72 4F4 FRTA21EA EOOO63EN 20040202001242004020200124NM 2004 2 2 AALA20040069 120040116A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM SEAT 20-24 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21771AN 29579 EMERGENCY ESCAPE PATH LIGHT AT SEATS 20-24 INOPERATIVE. REPLACED BATTERY PACK AT 3R OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040202001272004020200127CE 2004 2 2 018041 120040114A32338210310 ACTUATOR BEECH 1900 1900C 1154161CE NLG MALADJUSTMENT A NSVAO OTHER J WARNING INDICATION APAPPROACH 1 EA2732017 UC37 NOSE GEAR UNSAFE, NOSE GEAR WOULD NOT EXTEND AND LOCK, NO GREEN LIGHT, AND RED LIGHT IN THE HANDLE REMAINED ILLUMINATED. RESET CIRCUIT BREAKER, NOSE GEAR CAME DOWN. REPLACED ALL THREE RETRACT ACTUATORS, HYD SERVICE VALVE, AND FLUSHED SYSTEM. 2L72 4T RTA24CE 20040202001292004020200129NE 2004 2 2 QXEA200400017 320040115A6110 PROPELLER DHAV DHC8 DHC8202 2809007NM HAMSTD14SF 14SF23 NE OUT OF BALANCE A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 NM09348PH 484 SEA FLIGHT 2026 RETURNED TO FIELD. PROP VIBRATION AT 1050 NP. BALANCED PROP. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20040130000512004013000051NM 2004 1 30 04FDEA00082 120040108A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25277FE 22042 SCREW DAMAGE ON FRAME BS 1090 STR 26L WL 148. *S/D* FOUND SCREW DAMAGE ON FRAME TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 7075-0 .071, HEAT TREATED TO T6 AND INSTALLED PER SRM 51-40-3, 51-10-2, 51-30-2. 2L73 4F RTA3WE 20040130000552004013000055NM 2004 1 30 04FDEA00088 120040109A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT CENTER CARGO NR 49 LONGERON SPLICE FOUND CRACKED BETWEEN STA 5- 113 TO STA 1541. CRACKED NR 49 LONGERON SPLICE AT LT CENTER CARGO BETWEEN STA 5-113 TO STA 1541 REMOVED AND REPLACED WITH NEW FABRICATED PART AS PER DRAWING A5A7114 AND INSTALLED AS PER SRM 51-33-01, VOL. II. 2L73 4F RTA22WE 20040130000702004013000070EA 2004 1 30 04003654 120040103A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27654BR 7454 DURING OPERATION OF AIRCRAFT THE CREW REPORTED A FLAP CONTROL SYSTEM FAILURE AT ZERO DEGREES. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT BRAKE PRESSURE SENSING UNIT AND THE FLAP ELECTRONIC CONTROL UNIT WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040130001352004013000135WP 2004 1 30 AALA20040040 120040111A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217512A 49806 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130001432004013000143NM 2004 1 30 AALA20040049 120040110A3397 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21324AA 22325 JFK LT MID GALLEY CROSS AISLE EMERGENCY LIGHT INOPERATIVE. FOUND HIGH RESISTANCE AT L9072 GROUND SPLICE. RESPLICED AT L9072 GROUND SPLICE FOR LEFT HAND MID GALLEY CROSS AISLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040130001462004013000146WP 2004 1 30 AALA20040052 120040110A2910 LINE DOUG DC9 DC982 3022082WP HYD SYSTEM FAILED A AALAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW21465A 49595 RT HYDRAULIC SYSTEM FAILED AFTER LANDING. EMERGENCY DECLARED. REPLACED NR 4 MAIN LANDING GEAR BRAKE LINE AND SERVICED LEFT HAND AND RIGHT HAND HYDRAULIC SYSTEM. PERFORMED ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040130001532004013000153NM 2004 1 30 04FDEA00105 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74275, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001552004013000155NM 2004 1 30 04FDEA00107 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); INBOARD PIVOT HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001582004013000158NM 2004 1 30 04FDEA00116 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND CORRODED AT SPOT FACES. RT OUTBD FLAP INBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001652004013000165NM 2004 1 30 04FDEA00129 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP VANE TEE FITTING NR 4 (COUNTING FROM INBOARD); FOUND CORROSION ON FWD HOLE BORE AREA. LT OTBD FLAP VANE TEE FITTING NR 4 REPAIRED AS PER EA 1-5750-74290, WINGS - LEFT AND RIGHT OUTBOARD FLAP - NR 4 FITTING SUPPORT VANE TO TRACK CORROSION 2L73 4F RTA22WE 20040130001682004013000168SO 2004 1 30 C2XA04IA005 120040108A3350 LIGHT EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711121 145683 CREW REPORTED THAT THE EMERGENCY LIGHTS DID NOT WORK. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT. THE EMERGENCY LIGHT SYSTEM WAS OPERATIONALLY TESTED AND THE DISCREPANCY COULD NOT BE CONFIRMED. 2L72 4F RT 20040130001762004013000176NM 2004 1 30 DHL2004752503 120040104A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR BS 380.0 BETWEEN STR 22 AND 23R SKIN IS DENTED (PREVIOUSLY MAPPED). DENT FOUND TO BE OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024-.T3 .040 PO 90489 DIM 2.6875 INCH X 1.1875 INCH AND DOUBLER FROM 2024T3.050 PO 900226 DIM 12.25 INCH X 8.625 INCH IAW 727 SRM 53-30-3 FIG 3. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20040130001822004013000182NM 2004 1 30 2004UALA00006 120040101A2612 FIRE LOOP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 ENGINE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29907UA 25007 RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEAT INDICATION LIGHT. MAINTENANCE PERFORMED TROUBLESHOOTING OF THE NR 2 OVERHEAT DETECTION SYSTEM AND REPLACED M1121 LOWER FAN "A & B" LOOP OVERHEAT DETECTORS. AFTER REPLACEMENT, NR 2 ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20040130001862004013000186NM 2004 1 30 2004UALA00017 120040108A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29385UA 24660 STA 616 LT FRAME IS CRACKED AT FASTENER BELOW FLOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040130001962004013000196NM 2004 1 30 04FDEA00136 120040113A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CABIN - FLOORBEAM CORRODED AT STA 5/73 RIGHT X = 47.5 TO 75.25. CORRODED FLOOR SUPPORT AT CABIN STA 5/73 RT X = 47.5 TO 75.25 REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT AS PER DWG AEA736 AND AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040130001982004013000198NM 2004 1 30 04FDEA00138 120040113A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE. LT OUTBD FLAP OUTBD HINGE (WING MOUNTED), INBD ACTUATOR LUG HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040130002002004013000200NM 2004 1 30 04FDEA00140 120040113A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), UPPER INBOARD ATTACH HOLE (SPAR MOUNTED) CORRODED AT BORE. LT OTBD FLAP OTBD HINGE (WING MOUNTED) UPPER INBD ATTACH HOLE (SPAR MOUNTED) BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040130002192004013000219EU 2004 1 30 AWXA200400030 120040112A3397ABS0374A24 CABLE AIRBUS320 A320232 3930326EU SEAT ROW 9 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28663AW 1419 PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040130002212004013000221NM 2004 1 30 AWXA200400032 120040104A2560P4010021 BATTERY BOEING737 737301 1384611NM ZONE 900 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE FORWARD LAVATORY WALL MOUNTED EMERGENCY FLASHLIGHT WILL NOT BLINK WITHIN 10 SECONDS. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040202000052004020200005NM 2004 2 2 QXEA200400008 120040105A3150 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09353PH 496 ON FLIGHT 2036 LT TRU AND LT STALL WARNING MASTER CAUTION LIGHTS CAME ON DURING FLIGHT. RAN CHECKLIST. FOUND LEFT TRU CIRCUIT BREAKER AND HGS COOLING CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKERS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202000092004020200009NM 2004 2 2 QXEA200400012 120040112A2730 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM COCKPIT FALSE INDICATIONA QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09400QX 4030 SEA - FLIGHT 2309 - CREW ABORTED THE TAKEOFF, RECEIVED AN A/C TRIM MISALIGNED MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND C/W SERVICE LETTER DH8-400-SL-27-006-R1. NO TAKEOFF WARNING WAS RECEIVED WHEN THE PITCH TRIM WAS IN THE TAKEOFF RANGE. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040202000152004020200015EA 2004 2 2 COMA0470006 120040108A3230533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01391CA1297 10108 FLIGHT 5520 NR 3 HYDRAULIC SYSTEM LOW PRESSURE AND GEAR DISAGREE WARNING. REPLACED THE L/G SELECTOR VALVE. 2L72 4F RTA21EA 20040202000402004020200040NM 2004 2 2 EIA2004003 120040111A2150 A/C PACK BOEING747 747212B 1384886NM NR 1 ODOR A EIAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM09486EV 20888 WHILE AIRCRAFT WAS IN CLEAN CONFIGURATION AND LEVEL AT 6000 FEET HAD AN ELECTRICAL TYPE ODOR THAT APPEARS TO BE COMING FROM NR 1 A/C PACK, INTERMITTENT ODOR DURING APPROACH AND LANDING. DEFERRED NR 1 A/C PACK DMI 470. 2L74 4F A20WE 20040202000472004020200047NM 2004 2 2 DHL2004782005 120040114A5755 STRUCTURE BOEING727 727227 1384078NM NR 1 SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 UPPER WING PANEL OUTBOARD NR 1 SPOILER SEAL SUPPRESSOR CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR IAW B-727 SRM 51-10-1 & 51-40-6. 2L73 4F A3WE 20040202000482004020200048NM 2004 2 2 DHL2004750001 120040115A3350 LIGHT BOEING727 7272M7 138407SNM CABIN DISLODGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01750DH 21951 FORWARD ENTRY EMERGENCY EXIT LIGHT FELL OUT OF ITS MOUNT. REPLACED AND SECURED EMERGENCY EXIT LIGHT IAW B-M/M 33-50-101. OPS CHECKED GOOD. 2L73 4F A3WE 20040202000492004020200049CE 2004 2 2 015041 120040114A3230 CONNECTOR BEECH 1900 1900D 1154162CE MLG DOWNLOCK CONTAMINATED A NSVAO OTHER N FALSE WARNING APAPPROACH 1 EA27191CJ UE19 NOSE GEAR DOWN AND LOCK INDICATOR FAILED TO ILLUMINATE WITH GEAR SELECTED DOWN (GEAR WAS DOWN). INSPECTED ALL 3 LANDING GEARS, INSPECTED CONNECTOR GOING FROM DOWNLOCK SWITCHES TO AIRCRAFT. CHECKED FOR HYDRAULIC LEAKS, AND FLUID LEVEL FOR POWER PACK. VISUALLY INSPECTED CONNECTOR RECEPTICAL, FOUND NOSE LANDING GEAR RECEPTICAL CONTAMINATED WITH DIRT. CYCLED GEAR SEVERAL TIMES IAW MANUAL, PROBLEM COULD NOT BE DUPLICATED. 2L72 4T RTA24CE 20040202000582004020200058CE 2004 2 2 017041 120040113A291011438800013 POWERPACK BEECH 1900 1900D 1154162CE HYD SYSTEM FAILED A NSVAO OTHER J WARNING INDICATION LDLANDING 1 EA27172MJ UE72 LANDING GEAR WOULD NOT EXTEND, MANUAL EXTENSION PERFORMED. REPLACED HYD POWER PACK IAW MM, OP AND LEAK CHECKED GOOD. 2L72 4T RTA24CE 20040202000652004020200065 2004 2 2 SWIA200412763 420040106A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07431SW4622 4622 7536 EN ROUTE TO SLC AUTOPILOT FAILED FOLLOWED BY YD1, FD1, TERRAIN FAIL STATUS MSGS. LEFT SIDE WITNESS LIGHT ON FCP DO NOT ILLUMINATE. REPLACED NR 1 FCC CARD. AUTOPILOT OPS CHECK GOOD IAW 22-10-00. 2L72 4F RTA21EA 20040202000672004020200067EA 2004 2 2 SWIA200412765 120040109A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07463SW1393 1393 7820 FIRST CABIN CEILING EMERGENCY LIGHT IS INOP. REPLACED NR 1 ELBP IAW 33-51-04, OPS CHECK GOOD. 2L72 4F RTA21EA 20040202000692004020200069 2004 2 2 SWIA200412767 420040111A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07221SW4005 2073 120290 AUTOPILOT FAILS INTERMITTENTLY ON CAPTAIN'S SIDE. WHEN THE AUTOPILOT ENGAGES, THE AIRCRAFT IS OUT OF PITCH TRIM. ADJUSTED ELEVATOR SERVO MOUNT BREAK AWAY TORQUE AND REPLACED ELEVATOR SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040202000742004020200074 2004 2 2 SWIA200412772 420040111A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07429SW6808 6801 7518 YAW DAMP NR 2 DISENGAGED ON THE GROUND AT SLC AND WOULD NOT RE-ENGAGE. REMOVED AND REPLACED NR 2 FCC CARD PER CRJ MM 22-12-14. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040202000902004020200090NM 2004 2 2 04FDEA00158 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. RT OUTBD FLAP OUTBD HINGE (WING MOUNTED), OUTBD ACTUATOR LUG HOLE BORE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5740-74286, WINGS - LT & RT OUTBD FLAP OUTBD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040202000932004020200093NM 2004 2 2 04FDEA00161 120040115A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5. FLOOR SUPPORT CORRODED AT STA 1887 CENTER SECTION X = -8.5 TO 8.5 P/NO AGA7559-3N REMOVED AND REPLACED IAW MM 20-50-02. AGA7080 SUPPORT FABRICATEF AS PER DWG AGA7080 AND INSTALLED AS PER MM 20-50-02. 2L73 4F RTA22WE 20040202001042004020200104EA 2004 2 2 COMA0460046 120040109A5320601R31171 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01815CA9312 7397 THE INTERCOSTAL FLANGES AT BL 36 LT AND RT AND ATTACH ANGLE AT LBL 27 AT FS 484.0, WL 70 TO WL 73 ARE CRACKED. REMOVED THE CRACKED ANGLE AND CUT OFF THE CRACKED FLANGED, FABRICATED AND INSTALLED REPAIR ANGLES IAW WVAC EO 601R-53-4532. 2L72 4F RTA21EA 20040202001062004020200106SO 2004 2 2 LR7A04001 120040114A5512 SKIN LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 335 4763 DURING SCHEDULED A1 INSPECTION, FOUND FS 1070 HORIZONTAL STAB LOWER SKIN CRACKED AT RBL 50, WL 265. REPAIRED IAW SRM SMP 583 55-20-06. LP 19339, M2. 2H74 4T A1SO 20040202001182004020200118EA 2004 2 2 COMA0460052 120040104A5210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01810CA 7370 FLIGHT 5602 CABIN DOOR WARNING MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK OF DOOR AND WARNING SYSTEM WAS NORMAL. 2L72 4F RTA21EA 20040202001422004020200142 2004 2 2 UPS04841716 420040114A2565 SLIDE DOUG DC8 DC871F 302199DWP CABIN DOOR DISLODGED A IPXAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SO01700UP 45900 ESCAPE SLIDE FELL OUT OF PACK UPON CLOSING DOOR. STOWED FED SLIDE. 2L74 4F RT4A25 20040202001462004020200146WP 2004 2 2 UPS04841721 120040107A57205804007507 CLIP DOUG DC8 DC871F 302199DWP NR 1 FUEL TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 61 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED AT NR 1 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED SLIP IAW DWG 5804007 AND SRM 51-1-20D. 2L74 4F RT4A25 20040202001472004020200147WP 2004 2 2 UPS04841722 120040107A57205804007514 CLIP DOUG DC8 DC871F 302199DWP NR 4 FUEL TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE AT NR 4 PYLON IS CRACKED IN NR 4 ALT TANK AT APPROX XW 485. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 5804007 AND SRM 51-1-20D. 2L74 4F RT4A25 20040202001492004020200149WP 2004 2 2 UPS04841724 120040102A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, LONGERON 36 IS CORRODED BEYOND LIMITS BETWEEN STATION 120 - 160. CUT OUT LONGERON SECTION BETWEEN STATION 120 - 205, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040202001522004020200152WP 2004 2 2 UPS04841746 120040107A57205804007513 CLIP DOUG DC8 DC871F 302199DWP NR 1 FUEL TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, 1 EACH CLIP FWD OF STRINGER 63 OUTBOARD SIDE OF OUTBOARD SKATE ANGLE NR 1 PYLON IS CRACKED, APPROX STATION XW 485. REMOVED, FABRICATED AND INSTALLED CLIP IAW DWG 5804007 AND SRM 51-1-20D. 2L74 4F RT4A25 20040202001572004020200157NM 2004 2 2 04FDEA00169 120040116A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING - LEADING EDGE PANEL INTERIOR HAS SEVERAL CRACKS AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK. LT WING LEADING EDGE PANEL INTERIOR AT XOS 550 BETWEEN REFUEL PANEL AND OUTBOARD SLAT TRACK , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I. 2L73 4F RTA22WE 20040202001592004020200159NM 2004 2 2 04FDEA00171 120040116A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING LEADING EDGE 2 CRACKS AT RIVETS STA XOS 630 LEADING EDGE PANEL INTERIOR. LT WING LEADING EDGE : STA XOS 630 LEADING EDGE PANEL INTERIOR, 02 EACH CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I. 2L73 4F RTA22WE 20040202001612004020200161NM 2004 2 2 04FDEA00173 120040116A5714 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION AT STA 1235 RT X =30. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK AT STA 1235 RT X = 30 CORRODED AREA CARRIED OUT REPAIR IAW EA 1 5710-74294, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION 2L73 4F RTA22WE 20040202001632004020200163EU 2004 2 2 MALA040113 120040110A5347 GALLEY TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15407XJ 340B407 DURING INSPECTION IN LCQ, GALLEY TIE DOWN TRACK AT BS 231-272 HAS CORROSION AT SEVERAL LOCATIONS. MAINTENANCE REMOVED AND REPLACED GALLEY TIE DOWN TRACK AT BS 231-272, IAW SAAB 340 SRM 51-40-40-0 PAR 4. 2L72 4T RTA52EU 20040202001682004020200168EU 2004 2 2 MALA040110 120040109A2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU E/E BAY MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1579XJ 340A079 DURING FLT 3136, AVIONICS SMOKE DETECTOR LIGHT ILLUMINATED DURING DEPARTURE, RAN QRH, AIR RETURN TO MSP. MAINTENANCE REMOVED AVIONICS DOOR 220AZ, NO EVIDENCE OF SMOKE NOTED. SUSPECT FAULTY SYSTEM DETECTION SYSTEM. MAINTENANCE CLEANED OPTIC LENS. 2L72 4T RTA52EU 20040202001692004020200169EU 2004 2 2 MALA040109 120040101A25604566M37B042NM PBE BAC 146 AVRO146RJ85A1500097EU CABIN WILL NOT TEST A MALAK NONE L NO TEST ININSP/MAINT 1 GL15504XJ E2311 FWD PBE LOST VACUUM SEAL. REMOVED AND REPLACED FWD PBE P/N ON AND OFF 4566M37B-042NM, S/N OFF E964037, S/N ON E9900515 AS REQ. 2H74 4F RTA49EU 20040202001702004020200170NM 2004 2 2 04FDEA00174 120040116A5730APB74471 SKIN DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION FROM STA 1235 LT X =13 TO RT X =5. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK STA 1235 LH X = 13 TO RT X = 5. CORRODED AREA CARRIED OUT REPAIR IAW EA 1-5710-74294, WINGS - CENTER WING UPPER PANEL SKIN CORROSION. 2L73 4F RTA22WE 20040202001712004020200171NM 2004 2 2 04FDEA00175 120040116A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT CENTER CARGO CHANNEL GUIDE RAIL FOUND WITH CORROSION BETWEEN STA 1541 TO STA 5-113. CORROSION BETWEEN STA 1541 TO STA 5-113 GUIDE RAIL UPPER FLANGE, CORROSION REMOVED. ORIGINAL THICKNESS 0.090. MATERIAL REMAINING 0.082. WITHIN LIMIT PER SRM 53-00-01, FIG.3, VOL.I. 2L73 4F RTA22WE 20040202001742004020200174NM 2004 2 2 04FDEA00178 120040116A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RIGHT STA 1896 TO STA 2007 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. RT STA 1896 TO STA 2007 FLOOR SUPPORT (01 EACH) REMOVED AND REPLACED IAW SRM 51-31-01 VOL II 2L73 4F RTA22WE 20040202001752004020200175NM 2004 2 2 04FDEA00179 120040116A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RT STA 1912 FLOORBEAM CORRODED BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5. CORRODED FLOORBEAM SUPPORT BETWEEN FLOOR SUPPORT AT 53.5 FROM CENTER LINE AND SEAT TRACK 89.5 AT MAIN CARGO DECK RT STA 1912 REMOVED AND REPLACED WITH NEW SUPPORT AND INSTALLED AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20040202001772004020200177EU 2004 2 2 AWXA200400046 120040113A2822 SEAL AIRBUS320 A320231 3930325EU BOOST PUMP LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP28636AW4330732269 0762 098 LAS - FUEL SPILL - WHILE REPLACING O-RING SEAL FOR FUEL LEAK AT RT AFT WING PUMP A LARGE QUANTITY OF FUEL SPILLED WHEN PUMP WAS REMOVED FROM CANISTER, CHECK VALVE LOCKING DEVICE WAS IN CLOSED POSITION. MAINTENANCE FOUND THE TAB ON CHECK VALVE LOCKING DEVICE THAT CLOSES THE CHECK VALVE HAD BROKEN OFF ALLOWING VALVE TO REMAIN OPEN. REMOVED AND REPLACED RT WING FUEL PUMP IAW AMM 28-21-51-401, AND CHECK VALVE LOCKING DEVICE, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040202001782004020200178NM 2004 2 2 AWXA200400050 120040115A3350S283T00857 LIGHT BOEING757 757225 1384959NM EXTERIOR INOPERATIVE A AWXAO OTHER L NO TEST NRNOT REPORTED 1 WP28915AW 22209 PHX - EEL - DURING 4-DAY CHECK FOUND L-3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED L-3 DOOR EXTERIOR EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040202001822004020200182EA 2004 2 2 COMA0460061 120040115A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01467CA 7637 FLIGHT 5347 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040202001852004020200185EA 2004 2 2 COMA0460058 120040114A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SO01528CA954 7841 FLIGHT 5710 STAB TRIM AND MACH TRIM DISENGAGED DURING T/O. REPLACED THE HSTCU. 2L72 4F RTA21EA 20040202001862004020200186EA 2004 2 2 COMA0460057 120040114A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A COMAO OTHER O OTHER CRCRUISE 1 SO01812CA9825 7381 FLIGHT 5219 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20040202001962004020200196WP 2004 2 2 CALA0400031 120040115A2560S168MA MEGAPHONE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2712811 49265 INSPECTION FOUND THE FORWARD CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED. 2L72 4F A6WE 20040202001972004020200197NM 2004 2 2 CALA0400032 120040109A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE FLOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2739343 23581 INSPECTION FOUND DAMAGE TO THE PRESSURE DECK WEB AT STA 665 TO 675, RBL 35 TO 45. THE PRESSURE WEB DECK WAS REPAIRED IAW ECRA 5312-01023. 2L72 4F RTA16WE 20040202001982004020200198SO 2004 2 2 C2XA04SH016 120040117A531014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714998 145302 SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 59 TO 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202001992004020200199SO 2004 2 2 C2XA04SH017 120040117A531014526437001 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714998 145302 SHV- DURING C-CHECK THE RIGHT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTANANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202002012004020200201NM 2004 2 2 DHL2004753506 120040108A5311 FRAME BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, C-2 DOOR AFT FRAME BS 990 STR 26R TRANSITION PANEL PREVIOUS DOUBLER REPAIR DAMAGED AND CORROSION. REMOVED FASTENERS AND CUT OUT DAMAGE AREA ON WEB OF FRAME IAW B-727 SRM 51-30-2 AND 51-40-2 FIG 1. FABRICATED WEB SECTION MATERIAL USED 2024 T-3 .040 PO 900471 DIMENSION 8 X 4 INCHES SPLICE DIMENSION 4.5 X 4 INCHES IAW B-727 SRM B-727, SRM 51-40-2 FIG 1. ALODINED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED WEB PIECES AND SPLICE AT AFT FRAME IAW B-727 SRM 51-30-2. MATERIAL ID 53-10-2 FIG 5. 2L73 4F A3WE 20040202002022004020200202NM 2004 2 2 DHL2004753507 120040103A5310 BEAM BOEING727 727223 1384074NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, BS 1183 VERTICAL BEAM RBL 36.9 WL 249 CRACK INDICATION. VERIFIED NDT AT VERTICAL BEAM 1183 MARQUED END OF CRACK IAW NDT MAN PART 6, 51-00-00 FIG 4. STOPDRILL AT END OF CRACK .250 INCH IAW B-727 S/B 53-0192. DRILL NEW PARTS PO 342172 P/N 65C34406-13 AND INSTALLED AT BS 1183 RBL 36.9 WL 249. TREATED WITH ALODINED AND PRIMER IAW S/B 53-0129 AND SRM 51-10-2. 2L73 4F A3WE 20040202002032004020200203SO 2004 2 2 C2XA04TY011 120040115A532014521725615 SILL EMB 145 EMB145 3260210SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FRAME AFT SILL. MAINTENANCE REMOVED AND REPLACED THE FRAME SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002062004020200206SO 2004 2 2 C2XA04TY013 120040115A532014520609001 FLANGE EMB 145 EMB145 3260210SO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE WALL MOUNT FLANGE THAT SUPPORTS THE GALLEY FLOORBOARD NR 231HF AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE WALL MOUNT FLANGE IAW EMB 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002072004020200207SO 2004 2 2 C2XA04TY014 120040116A531514522459003 FLOORBEAM EMB 145 EMB145 3260210SO GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE CENTER FLOORBEAM OF FRAME 18. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAE EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002082004020200208SO 2004 2 2 C2XA04TY015 120040116A531514521713003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE CENTER FLOORBEAM IAW EMB SRM 51-40-02 AND CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002112004020200211SO 2004 2 2 C2XA04TY018 120040117A531514530643401 FLOORBEAM EMB 145 EMB145 3260210SO GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT THE CARBON FIBER GALLEY FLOOR SUPPORT. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB MM 53-21-10 AND CPM 51-21-04/05/06, SRM 53-21-10, 51-40-02. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002152004020200215EU 2004 2 2 RAIA00401010 120040109A7797 WIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE TT2 PROBE DAMAGED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03561HK 41077 76109 5544 - MEM, RIGHT IEC WARNING LIGHT CAME ON. MAINTENANCE REPAIRED WIRE TO TT2 PROBE. 2L72 4T4 TRTA41NM E18NE 20040202002162004020200216EU 2004 2 2 RAIA00401011 120040109A3350 CONNECTOR AEROSPATR42 ATR42300 8680920EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE 228 FORWARD FLOOR EMERGENCY LIGHTING INOP. MAINTENANCE RECONNECTED POWER SUPPLY CONNECTOR. 2H72 4T RTA53EU 20040202002172004020200217EU 2004 2 2 RAIA00401012 120040111A2460A2104F PDU JETAIRJETSTMJETSTM4101 1500501EU NR 1 GENERATOR MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03555HK125425016 41072 NR 1 GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED LEFT PDU. 2L72 4T RTA41NM 20040202002182004020200218EU 2004 2 2 RAIA00401013 120040113A3234877701 SELECTOR JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03562HK11584486 41078 LANDING GEAR INTRANSIT LIGHT REMAINED ON. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR HANDLE. 2L72 4T RTA41NM 20040202002192004020200219EU 2004 2 2 RAIA00401014 120040115A2422PC125123B INVERTER JETAIRJETSTMJETSTM4101 1500501EU EFIS DISPLAY FAILED A RAIAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 CE03555HK1944 41072 5341 - CVG, CAPTAIN'S EFIS SCREEN WENT BLANK AND ALL CABIN LIGHTS WENT OUT WITH MULTIPLE CAPTION PANEL LIGHTS ILLUMINATED. MAINTENANCE REMOVED AND REPLACE LEFT INVERTER. 2L72 4T RTA41NM 20040202002222004020200222NM 2004 2 2 237TR0001 120040114A33501000679 BATTERY PACK BOEING737 737228 13844AGNM FUSELAGE INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05237TR 23007 R2 DOOR EMERGENCY LIGHT INOP AND MID-CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT THE R2 DOOR AND THE BATTERY PACK AND CHARGER IN THE MID-CABIN. SYSTEM CHECKS GOOD PER MM 33-50-0. 2L72 4F RTA16WE 20040202002242004020200224NM 2004 2 2 DHL2004752512 120040106A5730 PANEL BOEING727 727223 1384074NM LT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, LT WING UPPER T/E PANEL WBL 124 HAS ONE SMOOTH DENT OUTBOARD AND ONE SHARP DENT INBOARD. CUT OUT 2 DENTED AREAS ON LT WING UPPER T/E PANEL, 1 APPROX 1.75 INCH DIA & 2 APPROX 2.25 INCH DIA. FABRICATED FILLERS 1 APPROX 1.75 INCH & 2 APPROX 2.25 INCH DIA AND DOUBLERS 1 APPROX 5 INCH DIA AND 2 APPROX 6 INCH FROM 2024T3.020 PO 900242. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES IAW B727 SRM 57-30-1 FIG 1, 57-30-2 FIG 4 AND 51-40-20 FIG 3. 2L73 4F A3WE 20040202002252004020200225NM 2004 2 2 QXEA200400035 120040116A3320 WIRE BOMBDRDHC8 DHC8401 1390041NM PAX DOOR CHAFED A QXEAF ACTIVATE FIRE EXT. AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09410QX4927 4053 SEA - FLIGHT 2431 - FLIGHT ATTENDANT NOTICED SMOKE AND A ONE INCH FLAME COMING FROM THE THE MAIN CABIN DOOR HINGE BRUSH GUARD. TWO FIRE EXTINGUISHERS WERE USED TO PUT FLAME OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND MAIN CABIN DOOR. A CHAFED WIRE TO THE MAIN CABIN DOOR LIGHTING WAS FOUND AND REPAIRED. OPERATIONAL CHECKS WERE PERFORMED, THE FIRE EXTINGUISHERS WERE REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRSTAIR LIGHTING WAS PLACED ON MEL. 2H72 4T RTA13NM 20040202002272004020200227NM 2004 2 2 DHL2004752513 120040108A571265172769 RIB BOEING727 727223 1384074NM NR 5 SLAT DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, NR 5 SLAT AT ACTUATOR ATTACH HAS INBOARD ATTACH FRAME CRACKED. REMOVED AND REPLACED DAMAGED RIBS P/N 65-17276-9 PO 342198 AND 65-17276, PO 343446 IAW B-727 SRM 51-20-12 AND 51-30-2. 2L73 4F A3WE 20040202002332004020200233NM 2004 2 2 04FDEA00185 120040117A5230 ACCESS PANEL BOEING727 727100 1384036NM CARGO DOOR BENT A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25188FE 19081 MAIN CARGO DOOR LIGHT CAME ON PASSING 15,000 FT AT 310 KNOTS. REPEAT WRITE-UP, APPROX CABIN PRESSURE 4.5 PSI. CHECKLIST ACCOMPLISHED, RETURNED TO AUS. OPENED MAIN CARGO DOOR, INSPECTED ALL SWITCHES ON MAIN CARGO DOOR, LATCH SWITCHES, LOCK TUBE SWITCHES, FOUND ACCESS PANEL ON LOWER AFT MAIN CARGO DOOR BENT IN AND MAKING CONTACT WITH THE TARGETS ON THE AFT TWO LATCH SWITCHES. STRAIGHTENED ACCESS PANEL AND FOUND BOTH TARGETS ON AFT TWO SWITCHES BENT AND OUT OF ADJUSTMENT. ADJUSTED BOTH TARGETS AND SWITCHES PER 727-100 MM CHAPTER 52-34-009-5. CLOSED CARGO DOOR, DOOR WARNING SYSTEM OPS CHECK'S NORMAL. OK FOR SERVICE. 2L73 4F RTA3WE 20040202002342004020200234NM 2004 2 2 04FDEA00186 120040117A5270 WARNING LIGHT BOEING727 727100 1384036NM CARGO DOOR FALSE INDICATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25188FE 19081 MAIN CARGO DOOR LIGHT CAME ON DURING CLIMBOUT PASSING 15,000 FT MSL AT 310 KAUS, CHECKLIST ACCOMPLISHED, RETURNED TO AUS. AFTER AIRCRAFT BLOCK IN, OPENED MAIN CARGO DOOR. FOUND AFT THRESHOLD LOCK DOWN, WITH RED LIGHT ON. LOCKED THRESHOLD LOCK. CHECKED DOOR SWITCHES; CHECKED GOOD. CLOSED MAIN CARGO DOOR, WARNING LIGHT WENT OUT. PRECAUTIONARY PRESSURIZED AIRCRAFT TO 3.5 PSI ON GROUND. WARNING LIGHT DID NOT COME ON. NO LEAKS NOTED ON OUTSIDE OF MCD. MAIN CARGO DOOR WARNING SYSTEM OPS CHECKS NORMAL. AIRCRAFT PRESSURIZED PER 727 JRH CH 7. OKAY FOR SERVICE. 2L73 4F RTA3WE 20040202002362004020200236WP 2004 2 2 IXXA0400007O 120040119A3260 INDICATOR DOUG DC8 DC871F 302199DWP MLG MALFUNCTIONED A IXXAO OTHER P NO WARNING INDICATION LDLANDING 1 SW11820BX844211733 46065 ON LANDING GEAR EXTENSION INTO FJDG GEAR CAME DOWN WITH NORMAL INDICATIONS, AT APPROXIMATELY 200 FT BOTH LEFT AND RIGHT MAIN GEAR INDICATIONS WENT OUT. CREW EXECUTED A GO-AROUND, CYCLED GEAR AND LANDED WITH A NORMAL GEAR DOWN INDICATION. MAINTENANCE CYCLED GEAR HANDLE, DIMMING SWITCH BRIGHT TO DIM SEVERAL TIMES. CHECKED GEAR SWITCHES PER APPLICABLE MANUALS AND OPERATES NORMAL ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040202002372004020200237NE 2004 2 2 NACA20040006 220040117A7421RHB32E SPARK PLUG PWA DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENG CYLINDER CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL03779TA263 263 A651WMHO 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING, NR 13 CYLINDER DOUBLE SHORTED SECONDARY. ADJUSTED VALVES AND REPLACED BOTH FRONT & REAR PLUGS ON NR 13 CYLINDER DUE TO CRACKED CERAMICS. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040202002422004020200242NM 2004 2 2 QXEA200400034 120040113A2611 LAMP DHAV DHC8 DHC8202 2809007NM SMOKE DETECTOR INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09352PH14861 494 PSC - MAINTENANCE FOUND THAT THE NR 1 SMOKE DETECTOR WILL NOT TEST. THE SMOKE DETECTOR WAS RELAMPED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202002472004020200247NM 2004 2 2 QXEA200400039 120040114A5753 CARRIAGE BOMBDRDHC8 DHC8401 1390041NM RT TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - RIGHT FLAP, FLAP TRACK CARRIAGES NR 4, 5 AND THE NR 4 FLAP TRACK FRONT FITTINGS REQUIRE REWORK. REPAIRED TRACKS AND FITTINGS IAW EO 6-27-147, RD 8/4-57-226, AND RD8/4-57-228. 2H72 4T RTA13NM 20040202002512004020200251NM 2004 2 2 DHL2004745006 120040117A5753 SKIN BOEING727 727224 1384076NM TE FLAP CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 RIGHT OUTBOARD MID FLAP T/E UPPER SURFACE CORROSION NUMEROUS AREAS. REMOVED CORROSION AND PRIMED IAW B727 SRM 51-10-2. 2L73 4F A3WE 20040202002532004020200253SO 2004 2 2 CHQA000432 120040115A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO LAV SMOKE FALSE INDICATIONA CHQAO OTHER N FALSE WARNING CLCLIMB 1 GL11276 145348 CAE312123 ON CLIMBOUT OF DFW AT 500 FT AGL, GOT LAV SMOKE WARNING ON EICAS. FLIGHT ATTENDANT VERIFIED NO SMOKE OR ODOR. EICAS MSG CLEARED AFTER 2 MINUTES. CLEANED LAV SMOKE DETECTOR. THE SAME PROBLEM OCCURRED THREE TIMES AGAIN OF IND ON 1/15, CMH ON 1/16, AND CMH ON 1/17. THE LAV SMOKE DETECTOR AND PANEL WAS REPLACED. THE FINAL FIX WAS REPLACEMENT OF NR 2 ENGINE DUE TO SUSPECTED CAUSE OF FALSE SMOKE WARNING. NO FURTHER PROBLEMS REPORTED. 2L72 4T RTT00011AT 20040202002542004020200254EU 2004 2 2 AALA20040079 120040117A2913M8372395K1203NLCPUMP AIRBUS300 A300B4605R 3930308EU HYD SYSTEM INOPERATIVE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2170079 619 SJU INFLIGHT/T0661/17 AIRCRAFT RETURNED TO STATION DUE TO LOSS OF GREEN SYSTEM HYDRAULIC FLUID. FOUND NR 1 ENGINE GREEN SYSTEM HYDRAULIC PUMP SOLENOID DETACHED FROM THE PUMP CAUSING THE FLUID LOSS. REPLACED NR 1 GREEN ENGINE DRIVEN PUMP AND SOLENOID CONNECTOR PARTS. ALSO REPLACED NR 2 ENGINE DRIVEN PUMP DUE TO RUNNING IT DRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040202002562004020200256WP 2004 2 2 AALA20040073 120040117A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21289AA 49301 DFW EMERGENCY LIGHT BATTERY PACK B5-28 INOPERATIVE. EMERGENCY ARROW MARKER LIGHT SIGN ASSEMBLY IN FORWARD ENTRY AISLE ON GALLEY WALL NEAR FLOOR IS BROKEN. REPLACED BATTERY PACK ASSEMBLY B5-28 FOR EMERGENCY LIGHTS AND REPLACED THE EMERGENCY ARROW MARKER LIGHT SIGN ASSEMBLY IN FORWARD ENTRY AISLE ON GALLEY WALL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040202002582004020200258WP 2004 2 2 AALA20040078 120040118A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21259AA 49289 SAT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED OVERWING EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040202002662004020200266NM 2004 2 2 CALA0400037 120040117A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 927 BETWEEN S27L AND S27R. INSTALLED REPAIR IAW SRM 53-00-01, FIGURE 202. 2L72 4F RTA16WE 20040202002682004020200268NM 2004 2 2 CALA0400039 120040117A5730 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 INSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 441.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20040202002702004020200270NM 2004 2 2 CALA0400041 120040117A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND MAIN CABIN FLOOR Z-ANGLE CORRODED FROM STA 956-997, RBL 50. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040202002762004020200276NM 2004 2 2 04FDEA00188 120040119A53206518636378 ANGLE BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 BULKHEAD 870 SUPPORT ANGLE IN RT WHEEL WELL IS CRACKED WL 180 RBL 8 BS 870 FOUND ON FED EX QA WALK. REMOVED AND REPLACED 870 BULKHEAD SUPPORT ANGLE RT WHEEL WELL, LEAK CHECK GOOD ON DUCTS. REINSTALLED ALL ITEMS REMOVED FOR ACCESS IAW FED EX MM 36-00-000-5 AND SRM 51-30-2, 51-10-1, 51-30-5. 2L73 4F RTA3WE 20040202002772004020200277NM 2004 2 2 F3LA200300192 120040113A5315 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP FROM L2 DOOR MOP SILL TO 20 INCHES INBOARD, STA 986.5. REPAIRED FLOORBEAM CAP PER EA B3-53R-10275. 2L72 4F RTA16WE 20040202002782004020200278WP 2004 2 2 04014308 220040114A7200310349015 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33143 01514WP LEFT MALFUNCTIONED A VTZAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 EA27308UE19746 41023 P75041 DURING CRUISE OF FLT 7711 CREW REPORTED LOW ENGINE OIL PRESSURE AND SHUTDOWN THE LEFT ENGINE. FLIGHT SAFELY RETURNED TO FIELD AND PASSENGERS DEPLANED NORMALLY. THE ENGINE AND ENGINE HYDRAULIC PUMP WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T4 TRTA41NM E2WE 20040202002792004020200279NM 2004 2 2 F3LA200300193 120040113A5315 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATE HOLES ON FLOORBEAM UPPER CAP AT STA 947.5. REPAIRED DAMAGED SECTION OF FLOORBEAM UPPER CAP AT STA 947.5 PER EA B3-53R-10270. 2L72 4F RTA16WE 20040202002812004020200281NM 2004 2 2 QXEA200400042 120040116A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09353PH 496 PSC- EMERGENCY LIGHT STRIP AT ROW 1, THIRD AND FOURTH RED MARKER LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202002822004020200282NM 2004 2 2 QXEA200400043 120040115A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09366PH2689 261 510 PDX- ON FLIGHT 2223 NR 1 AC GENERATOR LIGHT ILLUMINATED IN FLIGHT. RAN CHECKLIST AND LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 1 AC GENERATOR AND NR 1 GENERATOR CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202002832004020200283CE 2004 2 2 DXTA200400217 120040116A3240 RESERVOIR CESSNA500 560CESSNA 2076750CE MLG BRAKES LOW E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07323QS 5600323 ON LANDING, PILOT HAD NO BRAKE PRESSURE ON THE RT SIDE, BRAKE PRESSURE CAME UP SUDDENLY AFTER 3 SECONDS. FOUND BRAKE RESERVOIR LEVEL HALF WAY ON UPPER SIGHT GAGE, SERVICED BRAKE RESERVOIR IAW CESSNA 560 MM CHAPTER 12-10-02. BLED BRAKE SYSTEM AND PERFORMED ANTI-SKID FUNCTIONAL TEST IAW CESSNA 560 MM CHAPTER 32-42-00, NO DEFECTS OR LEAKS NOTED. 2L72 4F RTA22CE 20040202002882004020200288EA 2004 2 2 COMA0460064 120040115A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01484CA 7702 FLIGHT 5005 FLAPS FAIL CAUTION MESSAGE. C/W RIGGING OF THE RIGHT BPSU. 2L72 4F RTA21EA 20040202002902004020200290EA 2004 2 2 COMA0460066 120040116A275285210019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01484CA3428 7702 FLIGHT 5713 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT INBOARD FLAP ACTUATOR. 2L72 4F RTA21EA 20040202002932004020200293NM 2004 2 2 234TR0014 120040103A7330 O-RING BOEING737 737228 13844AGNM FF TRANSMITTER LEAKING A PIDAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SO05234TR 23004 WHEN SERVICING NR 2 ENGINE OIL, SMELLED FUEL. FOUND FUEL FLOW TRANSMITTER LEAKING. REPLACED 3 O-RINGS. LEAK CHECKED OK PER MM 73-31-12. 2L72 4F RTA16WE 20040202002942004020200294SO 2004 2 2 ACE010904 220040109A8530TISN712ACA CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED E YADAO OTHER REJPARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 AL039874M1000 20700745 291045R PILOT REPORTED LOSS OF POWER AND VIBRATION ON LANDING. MAINTENANCE DISCOVERED THE NR 3 CYLINDER HEAD CRACKED. 1H71 3O3 O A16CE E5CE 20040202002962004020200296SO 2004 2 2 C2XA04BT006 120040118A335020131A BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 DURING RON CHECK MAINTENANCE FOUND THE FORWARD RIGHTHAND OVERWING EMERGENCY LIGHT DOES NOT WORK AND FLOOR PROXIMITY LIGHTS ARE NOT WORKING. MAINTENANCE REMOVED AND REPLACED BATTERY PACK NR 1 IAW EMB135 AMM 33-50-04. EMERGENCY LIGHTS OPS. CHECKED GOOD IAW EMB135 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040202002982004020200298SO 2004 2 2 MASA200400023 120040111A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07831MJ 145273 ASH 2603 CLT, FORWARD CABIN FLOOR PROX LIGHTING INOP. SERVICE DOOR EXIT SIGN ALSO INOP. MX RESECURED THE BATTERY, OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040202002992004020200299EA 2004 2 2 MASA200400027 120040112A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LOIGHTBURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717358 7358 ASH 6102 PHX-SBP, THE CREW REPORTED FLOOR STRIP LIGHTING INOP IN ROW 3. ALSO A CEILING EMERGENCY LIGHT AT ROW 5 INOP. THE FLOOR LIGHTING WAS REPAIRED AND THE LAMP WAS REPLACED. OP CHECKS GOOD. 2L72 4F RTA21EA 20040202003002004020200300EA 2004 2 2 MASA200400028 120040112A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777286 7286 ASH 6152 PHX-SBA, LEFT OVERWING FWD EXTERIOR EMERGENCY LIGHT INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040202003012004020200301SO 2004 2 2 MASA200400029 120040112A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07829MJ 145228 ASH 2723 SDF, CABIN EMERGENCY FLOOD ROW 6 INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4T RTT00011AT 20040202003022004020200302SO 2004 2 2 MASA200400030 120040114A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07856MJ 145626 ASH 2674 PIT, RIGHT WING EMERGENCY EXIT LIGHT INOP. MX REPLACED BULB, OP CHECKS GOOD. 2L72 4T RTT00011AT 20040202003032004020200303EA 2004 2 2 MASA200400032 120040114A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737228 7228 ASH 6338 PHX, PAX DOOR FLOOR EMERGENCY FLOOD LIGHT INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4F RTA21EA 20040202003042004020200304NM 2004 2 2 MASA200400037 120040118A3350 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07445YV 445 ASH 6282 PHX-ASE, DURING PREFLIGHT CREW REPORTED THE EMERGENCY FLOOR PATH LIGHTING INOP. MX TIGHTENED THE NR 1 AND 2 BATTERY PACKS AND CHARGED THE BATTERIES. OP CHECKS GOOD. NO PARTS USED. 2H72 4T RTA13NM 20040202003052004020200305SO 2004 2 2 C2XA04BT007 120040119A33501317 BULB EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 DURING 2A INSPECTION MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT AT AFT OF THE CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB AT THE LAST OVERHEAD EMERGENCY LIGHT IAW EMB145 33-50-00 (STANDARD PRACTICES), OPS CHECKED EMERGENCY LIGHTS GOOD. 2L72 4F RTT00011AT 20040202003072004020200307NE 2004 2 2 002072 220040120A7320 FUEL CONTROL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE NR 1 ENGINE MALFUNCTIONED A UHLAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL17340SZ 340A004 504 DRG550089 ON 01-20-2004, APPROX 1400 (UTC), FLT 4568, PIT-LYH, NR 1 ENGINE HAS NO FUEL FLOW, ENGINE WILL NOT START. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040202003082004020200308NM 2004 2 2 AWXA200400053 120040118A3397ABS0374A24 WIRE AIRBUSA319 A319132 3930340NM SEAT ROW 12 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040130001312004013000131NM 2004 1 30 DHL2004782003 120040110A3260 UPLOCK SENSOR BOEING727 727227 1384078NM LT MLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01782DH 21998 LT MAIN GEAR RED DISAGREEMENT LIGHT ILLUMINATED WITH GEAR HANDLE OFF. PERFORMED ABNORMAL PROCEDURE, LIGHT REMAINED ILLUMINATED. CLEANED UPLOCK SENSOR, PERFORMED ADJUSTMENT TEST PER M/M 32-61-81. OPS CHECKED GOOD. 2L73 4F A3WE 20040130001322004013000132EU 2004 1 30 AWXA200400025 120040109A3350BR8164005 LIGHT AIRBUS320 A320231 3930325EU ZONE 220 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 PHX - EEL - FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH FIXTURE AT FORWARD BULKHEAD WAS BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT FORWARD BULKHEAD, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040130001412004013000141WP 2004 1 30 AALA20040046 120040110A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219681B 53631 DFW LEFT HAND AND RIGHT HAND EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-125 FOR LEFT HAND AND RIGHT HAND OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040130001492004013000149NE 2004 1 30 AALA20040055 220040111A7310UL11207 LINE BOEING757 757223 1384957NM RROYCERB211 RB211* 54555NE ZONE 600 LEAKING A AALAK NONE O OTHER CRCRUISE 1 SW21671AA 25336 ORD T2095/11 CARGO REPORTED EVIDENCE OF FLUID LEAK FROM THE RIGHT HAND ENGINE UPON ARRIVAL AT GATE. INVESTIGATION REVEALED LP FUEL PUMP LINE HAD CHAFED AGAINST THE HYDRAULIC LINE CAUSING A HOLE IN THE FUEL PUMP LINE. REPLACED FUEL LINE ON NR 2 ENGINE. LEAK CHECK GOOD ON ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM A12EU 20040130001622004013000162NM 2004 1 30 04FDEA00126 120040112A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE); OUTBOARD ACTUATOR LUG FOUND CORRODED AT SPOT FACES AREA. COMPLIED WITH FEDEX EA 1-5750-74281, WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040130001642004013000164NM 2004 1 30 04FDEA00128 120040112A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP VANE TEE FITTING NR 4 (COUNTING FROM INBOARD) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OTBD FLAP VANE NR 4 TEE FITTING REPAIRED AS PER EA 1-5750-74290, LT AND RT OUTBOARD FLAP - NR 4 FITTING SUPPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040130001792004013000179NM 2004 1 30 DHL2004753502 120040106A5312 PRESSURE PANEL BOEING727 727223 1384074NM NLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, NOSE SECTION LWR LOBE INTERIOR PRESS WEB AT BS 294S PREVIOUS CRACK REPAIR DO NOT MEET SRM. REMOVED PREVIOUS REPAIR AT NOSE SECTION LWR LOBE INT PRESS WEB BS 294 IAW B-727 SRM 51-30-2. CUT OUT DAMAGED IAW B-727 SRM 51-40-2 FIG 3. REPAIR DOUBLER AND FILLER MAT USED 7075-T6, .071, PO 9012380, DIMENIONS AREA DOUBLER 5 INCH X 4.75 INCH AND FILLER 3 INCH X 2 INCH IAW B-727 SRM 51-40-2. ACCOMPLISHED MAT HFEC AROUND CUTOUT HICA PER PART 6, 51-00-00 FIG 6. NO CRACKS TREATED, ALODINED, AND PRIMED IAW B-727 SRM 51-10-2, INSTALLED DOUBLER AND FILLER REPAIR IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040130001802004013000180NM 2004 1 30 2004UALA00004 120040102A3350 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29182UA 25279 EMERGENCY EXIT LIGHTS FLOOR LIGHT DAMAGED AT ZONE-E AREA OF SEATS 57C - 58C. REPLACED EEL BATTERY IN FRONT OF 5L. 2L74 4F4 FRTA20WE E24NE 20040130001932004013000193NM 2004 1 30 04FDEA00092 120040110A5520 RIB BOEING727 727200 138407ENM LT ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25242FE 21178 LT ELEVATOR STA 136.5 SUPPORT RIB IS CRACKED AT LWR, INBOARD BOLT HOLE. REPAIRED ELEV STA 136.5 SUPPORT RIB IAW SRM 55-10-4. 2L73 4F RTA3WE 20040130002202004013000220NM 2004 1 30 AWXA200400031 120040112A3397BMS13311122 WIRE BOEING737 7373B7 1384580NM SEAT ROW 10 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 PHX - EEL - DURING 8-DAY CHECK FOUND A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 10 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040130002222004013000222NM 2004 1 30 AWXA200400033 120040104A2560P2070001214 FLASHLIGHT BOEING737 737301 1384611NM LAVATORY INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - EMERGENCY EQUIPMENT - DURING C-18 CHECK FOUND THE AFT LAVATORY WALL MOUNTED EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY, NO HELP. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040130002312004013000231WP 2004 1 30 AALA20040062 120040108A5248 MECHANISM DOUG DC9 DC983 3022083WP TAILCONE RELEASELACK OF LUBE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21599AA 53289 LAX TAIL CONE FAILED TO DEPLOY WHILE ACCOMPLISHING SPECIAL ITEMS CARD 5918, TAIL CONE JETTISON SYSTEM INSPECTION AND OPERATIONS CHECK. LUBED RELEASE MECHANISM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040202000062004020200006NM 2004 2 2 QXEA200400009 120040113A33506138001 POWER SUPPLY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09539DS866 866 4016 GEG- NR 2 POWER SUPPLY FOR EMERGENCY LIGHTS IS INOPERATIVE. REMOVED AND REPLACED BATTERIES L2 AND R2 OF NR 2 POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202000322004020200032SO 2004 2 2 RAIA00401006 120040104A3260832701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03827HK 5663-STL- AIR GROUND SWITCH FAIL MESSAGE. GEAR HANDLE WOULD NOT GO UP. MAINTENANCE REMOVED AND REPLACED LEFT AIR GROUND PROX SWITCH. 2L72 4F RTT00011AT 20040202000342004020200034EU 2004 2 2 RAIA00401008 120040108A3260AIR136070 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03562HK 41078 5327-PIT- RED LIGHT IN GEAR HANDLE REMAINED ON. MAINTENANCE REMOVED AND REPLACED LEFT HAND UPLOCK SWITCH. 2L72 4T RTA41NM 20040202000362004020200036EA 2004 2 2 04014621 120040114A7830 PLUNGER CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER FROZEN A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27621BR 7186 DURING CLIMB OF FLIGHT 7621 CREW REPORTED A THRUST REVERSER UNLOCKED MESSAGE. CREW RETURNED TO BUF AND FLIGHT LANDED UNEVENTFULLY. PASSENGERS WERE DEPLANED NORMALLY. UPON INSPECTION OF THE THRUST REVERSER SYSTEM ICE BUILDUP WAS FOUND ON THE THRUST REVERSER PLUNGERS AND WAS REMOVED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040202000392004020200039NM 2004 2 2 EIA2004002 120040109A3310245904 RHEOSTAT BOEING747 747212B 1384886NM COCKPIT LIGHTS OVERHEATED A EIAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NM09486EV 20888 ON FINAL APPROACH NOTICED STRONG ELECTRIAL BURNING ODOR UPON SELECTING FLAPS DOWN. FOUND CENTER FWD BACKGROUND LIGHTING DIMMER/TRANSFORMER EXTREMELY HOT CB T137, PULLED AND COLLARED DMI PER 33-1 DMI 469. REMOVED AND REPLACED INSTRUMENT LIGHT DIMMER AND CTR INSTRUMENT LIGHT RHEOSTAT. 2L74 4F A20WE 20040202000412004020200041NM 2004 2 2 EIA2004004 120040114A3397 WIRE BOEING747 747212B 1384886NM COCKPIT BROKEN A EIAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09486EV 20888 STRONG SMOKE /FUME ODOR, PULLED CTR PNL CB ODOR SEEMED TO GO AWAY. FOUND BROKEN WIRE L77-20 AT DIMMER BROKEN WITH SIGNS OF ARCHING AT TERMINAL. REPAIRED WIRE PER SWPM 20-10-13, OPS CHECKED PER B747 MM 33-11-00. NO ODOR NOTED. 2L74 4F A20WE 20040202000452004020200045EU 2004 2 2 DHL2004367001 120040115A5230 DOOR AIRBUS300 A300B4203 3930306EU CARGO BAY UNSECURE A DHLAO OTHER WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO01367DH 265 DURING CRUISE AT 290, THE DOORS LIGHT AND CHIME (MWP) ILLUMINATED BRIEFLY 2 TIMES AND EXTINGUISHED. PRESSURIZATION NORMAL. COMPLETED EMERGENCY CHECK LIST. NO LIGHT ON S/O'S PANEL. PERFORMED DOOR WARNING TEST AND FOUND RIGHT FORWARD COMPARTMENT DOOR NOT FULLY CLOSED. SECURED DOOR AND FINISHED TEST IAW M/M 52-71-00. OPS CHECKED GOOD ON GROUND. 2L72 4F RTA35EU 20040202000462004020200046SO 2004 2 2 C2XA04BT004 120040112A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2714920 145380 CREW REPORTED, BURNING ODOR WHEN PACKS ARE ON. MAINTENANCE INSPECTED AIRCRAFT AND RAN PACKS, NO ODOR DETECTED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040202000532004020200053 2004 2 2 015043 420040114A2210 COMPUTER BEECH 1900 1900C 1154161CE YAW DAMPER MALFUNCTIONED A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27210CJ UC110 RIGHT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C. 2L72 4T RTA24CE 20040202000572004020200057 2004 2 2 04007680 420040107A34604916406 COMPUTER CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A VTZAAD UNSCHED LANDING RETURN TO BLOCK F FLT CONT AFFECTED CLCLIMB 1 EA27680BR 7679 DURING CLIMB OF FLIGHT 7250 CREW REPORTED GROUND AND FLIGHT SPOILER FAULTS. CREW RETURNED TO IAD AND FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE NR 1 SPOILER ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20040202000752004020200075NM 2004 2 2 DHL2004752509 120040107A5330 SKIN BOEING727 727223 1384074NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE SKIN CRACK AT FWD ENTRY DOOR LOWER HINGE CUT OUT, VERIFIED BY NDT INSP. CUT OUT DAMAGED AREA DIM 1.625 X 1 INCH AND FABBED FILLER FROM 2024-T3 .080 PO 900474 DIM 1.625 X 1 INCH AND DOUBLER FROM 301 1/2 HD .063 PO 900125 DIM 15.75 X 6 INCH PER S/B 727-53A-0198 REV 2 FIG 3 AND 4. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW S/B 727-53A0198 REV 2 FIG 4. 2L73 4F A3WE 20040202000772004020200077NM 2004 2 2 AWXA200400048 120040114A5330 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 PHX - MAJOR REPAIR - A 2.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN LEFT SIDE OF AIRCRAFT AT STR 24 LEFT BETWEEN BS 927 AND BS 947. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN AT STR 24 LEFT BETWEEN BS 927 AND BS 947; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA ER 15-5331-04014-KB1. 2L72 4F RTA16WE 20040202000892004020200089NM 2004 2 2 04FDEA00157 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OUTBOARD FLAP OUTBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE CORRODED AT BORE. RT OUTBD FLAP OUTBD HINGE (WING MOUNTED), INBD ACTUATOR LUG HOLE BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74286, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040202000942004020200094NM 2004 2 2 04FDEA00162 120040115A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RIGHT STA 1922 TO STA 2007 SEAT TRACK REF X = 20.0, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1922 TO STA 2007 SEAT TRACK REF. X = 20.0, FLOOR SUPPORT 01 EA REMOVED AND REPLACED AS PER MM 20-50-02 (AGA7088-2). SUPPORT AGA7087 FABRICATED AS PER DWG NR AGA7087 ANS INSTALLED AS PER MM 20-50-02. 2L73 4F RTA22WE 20040202001022004020200102EA 2004 2 2 COMA0460044 120040114A5320601R311719 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FS 484 RBL 27, OUTBOARD SUPPORT ANGLE/INTERCOSTAL CRACKED. REMOVED ANGLE FABRICATED REPAIR ANGLE FROM 2024-T3.063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059. 2L72 4F RTA21EA 20040202001252004020200125WP 2004 2 2 AALA20040070 120040115A3350P4010051111 BATTERY PACK DOUG DC9 DC982 3022082WP SEAT 3-20 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21555AN 53085 SAT EMERGENCY LIGHTS AT SEATS 3 THROUGH 20 INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK FOR ROWS 3 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040202001262004020200126GL 2004 2 2 C2XA04CL004 220040114A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW27139491293912939 145057 CAE310043 EWR FLT 2247, THE CREW REPORTED A LOUD BANG FROM NR 2 ENGINE, ITT WENT TO 900 CELSIUS. POWER WAS REDUCED, TEMP STAYED AT 900 CELSIUS FOR 5 SECONDS, THEN ENGINE NR 2 FLAMED OUT. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER DIFFICULTY. NR 2 ENGINE WAS REPLACED. 2L72 4T4 FRTT00011ATTE6CH 20040202001282004020200128NM 2004 2 2 DHL2004721001 120040115A5210 ROLLER BOEING727 727228 1384083NM PAX DOOR LACK OF LUBE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01721DH 19545 MAIN ENTRY DOOR DIFFICULT TO OPEN, CLOSE, AND LATCH. INSPECTED ENTRY DOOR LINKAGE AND MECHANISM, NO DEFECTS NOTED. LUBED ROLLERS, OPS CHECKED GOOD IAW B-727 M/M 52-11-01. 2L73 4F RTA3WE 20040202001322004020200132 2004 2 2 UPS04141717 420040114A2565 SWITCH AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE STICKS A IPXAK NONE O OTHER ININSP/MAINT 1 SO01139UP 0805 CREW ENTRY DOOR SLIDE BUZZER SWITCH STICKS OCCASIONALLY WHEN PRESSED TO TEST. CLEANED CREW ENTRY DOOR SIDE WARNING BUZZER SWITCH WITH CONTACT CLEANER, TESTED A DOZEN, NO DEFECTS NOTED. 2L72 4F RTA35EU 20040202001552004020200155EU 2004 2 2 146951 120040116A2770 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE GUST LOCK ILLUMINATED A UHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL17148SD 340A148 462 DRG276584 ON 01-16-2004, APPROX 1245 (UTC), FLT 4625 SCE-PIT, CREW RETURNED TO GATE WHEN THE GUST LOCK WARNING ILLUMINATED WITH THE GUST LOCK RELEASED. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040202001562004020200156NM 2004 2 2 04FDEA00168 120040116A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING - ON LEADING EDGE SKIN PANEL INTERIOR FOUND SEVERAL CRACKS STA XOS 510 UNDER REFUEL ACCESS PANEL. LT WING : LEADING EDGE SKIN PANEL STA XOS 510 UNDER REFUEL ACCESS PANEL INTERIOR , CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG. 25, VOL. I. 2L73 4F RTA22WE 20040202001672004020200167NE 2004 2 2 MALA040111 320040109A614010223NO1R00 INDICATOR SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE PROPELLER FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15414XJ 340B414 DURING FLIGHT 3006 LEFT PROP RPM GAUGE DROPPED TO ZERO INFLIGHT. FLUCTUATES BETWEEN 200 AND 1270 RPM. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED LEFT PROP INDICATOR, OPS CHECKS GOOD. OK FOR SERVICE. 2L72 4T RTA52EU 6 CP31NE 20040202001722004020200172NM 2004 2 2 04FDEA00176 120040116A5320 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 TAIL TANK - RIGHT NR 36 BARREL NUT HOLE, BEARING SURFACE AND BOTTOM SURFACE FOUND CORRODED. REQUIRE CUTTING OF WEB FOR REAMING. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF RT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REPAIR CARRIED OUT AS PER EA 1-5320-74276 (TITLE: FUSELAGE - AUXILLIARY STRUCTURE - ACCESS FROM PANEL FOR 36LR - BARREL NUT MOD) 2L73 4F RTA22WE 20040202001832004020200183 2004 2 2 COMA0460060 420040115A2340151011 INTERPHONE CNDAIRCL600 CL6002B19 1900309EA AVIONICS NOISY A COMAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO01918CA20048 7018 FLIGHT 5718 LOUD TICKING NOISE IN HEADSET DURING T/O. REPLACED THE APU BAY INTERPHONE UNIT. 2L72 4F RTA21EA 20040202001882004020200188WP 2004 2 2 CALA0400023 120040114A5310 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2783870 48056 INSPECTION FOUND A 1 INCH CRACK IN SHEAR TIE AT BS 560 BETWEEN L22L AND L23L. REPAIRED IAW SRM 53-03, FIGURE 7. 2L72 4F A6WE 20040202002052004020200205SO 2004 2 2 C2XA04SH018 120040117A532014521725013 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202002132004020200213NE 2004 2 2 002171 220040116A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE LEFT MALFUNCTIONED A UHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL17146SD 146 501 DRG675484 ON 01-16-2004, AT APPROX 1125 (UTC), FLT 4633, BGM-PIT, CREW HAD RETURNED TO GATE. THE LEFT ENGINE WOULD NOT LIGHT OFF. THERE WAS NO FUEL FLOW INDICATION ON THE LEFT ENGINE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040202002202004020200220SO 2004 2 2 C2XA04SH021 120040119A532014521725015 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCEMENT DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE 5320-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202002442004020200244NM 2004 2 2 QXEA200400038 120040116A2810 O-RING DHAV DHC8 DHC8202 2809007NM POPPET VALVE LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09374PH 528 PDX - FUEL WAS FOUND LEAKING FROM THE NR 2 ENGINE NACELLE. MAINTENANCE INSPECTED THE AREA AND RESEATED THE FUELING ADAPTER POPPET VALVE O-RING. NO OTHER DEFECTS WERE NOTED AND NO PARTS WERE REPLACED. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202002462004020200246NM 2004 2 2 DHL2004746001 120040116A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01746DH 22252 LOWER FUSELAGE AT APPROX STA 685 APPROX 6 INCHES BELOW LOWER LAP SEAM AND ABOUT 5 INCHES AFT OF BUTT SEAM IS AN AREA OF EXFOLIATED CORROSION OPEN UP ABOUT 1.5 INCH LONG. REMOVED CORROSION IAW B727 SRM 53-30-3 MADE DOUBLER FROM 2024T3 .071 IAW B-727 SRM 53-30-3. INSTALLED DOUBLER USING 20426 D6 RIVETS HLT19-8-4 IAW B727 SRM 53-30-3 FS 685 TO 697. THIS IS A MAJOR REPAIR. 2L73 4F A3WE 20040202002592004020200259WP 2004 2 2 AALA20040074 120040117A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219615W 53562 DFW CEILING EMERGENCY LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR ROW 25 CEILING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040202002872004020200287EA 2004 2 2 COMA0460063 120040117A5330601R31145 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 RIGHT SIDE CABIN FLOOR SIL ASSY HAS CORROSION ON TOP SURFACE FROM FS 516 THRU 544. CLEANED CORRODED AREA BY BLENDING OUT CORROSION. CUT OUT AREA THAT WAS OUT OF LIMITS AND FABRICATED AND INSTALLED REPAIR PARTS. TREATED AND PAINTED ENTIRE WORK AEA IAW REO 601R-53-41-183. 2L72 4F RTA21EA 20040202002892004020200289EA 2004 2 2 COMA0460065 120040118A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01964CA 7129 FLIGHT 5339 LEFT THRUST REVERSER UNLOCK CAUTION DURING T/O. SECURED THRUST REVERSER AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040202002952004020200295SO 2004 2 2 C2XA04BT005 120040116A3260 SWITCH EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW2713997 145298 CREW REPORTED, AFTER TAKEOFF RECEIVED LANDING GEAR AIR/GROUND FAILURE WARNING, UNABLE TO RETRACT LANDING GEAR. AIR RETURNED, AND LANDED UNEVENTFULLY. AIRCRAFT MAINTENANCE FERRIED TO RIC. MAINTENANCE TIGHTENED NR 2 (RIGHTHAND) MAIN LANDING GEAR WOW PROXIMITY SWITCH IAW EMB145 AMM 32-61-02. OPS CHECKED GOOD (SEE M-602 677475), AIRCRAFT RELEASED FOR TEST FLIGHT, AIRCRAFT TEST FLOWN SATISFACTORILY, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040202002972004020200297SO 2004 2 2 MASA200400012 120040106A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 ASH 2762 BNA-DCA, CREW REPORTED GALLEY EMERGENCY EXIT LIGHT SIGN INOP. MX PERFORMED AN OPS CHECK AND FOUND TO BE OPERATING NORMALLY. NO PARTS USED. 2L72 4T RTT00011AT 20040202003092004020200309EU 2004 2 2 AWXA200400054 120040117A2910S4340092002 SOLENOID VALVE AIRBUS320 A320231 3930325EU ZONE 140 LEAKING A AWXACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 WP28622AW 054 ORD - ABORTED TAKEOFF - FLT 0654 - ON TAKEOFF AT ORD EN ROUTE FOR PHX RECEIVED YELLOW HYDRAULIC RESERVOIR LOW LEVEL INDICATION WITH ASSOCIATED BRAKE, ANTI-SKID, AND NOSE WHEEL STEERING FAULTS ON UPPER ECAM, REJECTED TAKEOFF BELOW 80 KTS. MAINTENANCE FOUND FLUID LEAKING FROM A CRACK IN THE POWER TRANSFER UNIT SOLENOID VALVE (1012GL) (2 WAY VALVE). REPLACED CRACKED VALVE IAW AMM 29-23-51-401. SERVICED YELLOW HYDRAULIC SYSTEM AND PERFORMED ENGINE RUN, OPERATIONAL AND LEAK CHECKS WERE GOOD. FUNCTIONAL TEST OF POWER TRANSFER UNIT SOLENOID VALVE S/N 0141 CONFIRMED FAILURE OF UNIT FOR INTERMITTENT OPENING AND CLOSING. REPLACED SEAL'S, O-RINGS, AND BACK UP RINGS, UNIT REPAIRED IAW CMM 29-10-12. 2L72 4F RTA28NM 20040202003102004020200310NE 2004 2 2 AWXA200400055 220040119A7320 FUEL CONTROL AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE NR 1 ENGINE MALFUNCTIONED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK JR WARNING INDICATION PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP28814AW 1281 PHX - ABORTED TAKEOFF - FLT 0820 - ON TAKEOFF AT PHX EN ROUTE FOR BOS THE NR 1 ENGINE FAILED TO ACCELERATE, REJECTED TAKEOFF AT 60 KTS. TAXIED CLEAR OF RUNWAY AND RAN UP NR 1 ENGINE, ENGINE AGAIN FAILED TO ACCELERATE ABOVE 1.1 EPR, RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL IAW T/C R5M73302, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF ELECTRONIC ENGINE CONTROL CONFIRMED FAILURE OF UNIT FOR SENSOR FAILURE. REPLACED P2 SENSOR, P5 SENSOR, PAMB SENSOR, AND PB PORT SCREEN IAW CMM 73-28-02, REV. 0. UNIT TESTED AND RETURNED TO SERVICE IAW HS14743. 2L72 4F4 FRTA28NM E311NE 20040202003152004020200315NM 2004 2 2 AALA20040085 120040119A79317055M58G01 RELIEF VALVE BOEING767 767323 1385205NM NR 1 ENGINE INOPERATIVE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21354AA 24035 LAX INFLIGHT T/217/19 OIL QUANTITY DECREASED IN FLIGHT TO 11 QUARTS. RECOVERED UPON LANDING. REPLACED NUMBER 1 ENGINE PRESSURIZATION AND PRESSURE RELIEF VALVES ON NR 1 ENGINE OIL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040202003172004020200317NM 2004 2 2 AALA20040083 120040119A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21968AN 30095 SNA EMERGENCY EXIT LIGHT AT RIGHT FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT FORWARD GALLEY DOOR AND REPLACED LENS ASSEMBLY. 2L72 4F RTA16WE 20040202003192004020200319NM 2004 2 2 AALA20040084 120040119A5210 SEAL BOEING737 737823 13844BZNM ZONE 800 OBSTRUCTED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21971AN 29547 SFP INFLIGHT T/1608/19 FLIGHT RETURNED TO STATION. UNABLE TO PRESSURIZE CABIN. LANDED WITHOUT INCIDENT. FOUND FORWARD CABIN DOOR DID NOT SEAL. DOOR SILL AND DOOR CHECKED NORMAL. PRESSURIZED AIRCRAFT TO 5 PSI AND NO LEAKS NOTED ON ANY PART OF THE L1 DOOR. CLEANED SEAL AND SILL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040202003212004020200321WP 2004 2 2 AALA20040086 120040119A262192743642 RELAY DOUG DC9 DC983 3022083WP NR 1 FIRE BOTTLEMISWIRED A AALAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW219615W 53562 DFW INFLIGHT T1310/19 APPROACHING 14,000 FEET AFT CARGO FIRE INDICATION AND MASTER WARNING LIGHTS CAME ON. DISCHARGED NR 1 FIRE BOTTLE. NO INDICATION OF DISCHARGE. FOLLOWED QRH AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND ON R2-5 RELAY A GROUND CONTROL WIRE MIS-WIRED FROM CARGO SMOKE CONTROL PANEL. REPLACED R2-5 GROUND CONTROL RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040202003222004020200322NM 2004 2 2 QXEA200400019 120040104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - TOP FLANGE NICKED AND CHANNEL PITTED ON RIGHT HAND OUTBOARD SEAT TRACK NR 10. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20040202003242004020200324NM 2004 2 2 QXEA200400021 120040105A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - INBOARD FLANGE GOUGED AND PITTED AROUND CAMLOCK REPECTICAL HOLE OF RIGHT HAND INBOARD TRACK NR 7. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040202003262004020200326NM 2004 2 2 QXEA200400023 120040103A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - RIGHT HAND INBOARD TRACK NR 7 INBOARD FLANGE SCRATCHED 4.5 INCH LONG. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040202003282004020200328NM 2004 2 2 QXEA200400025 120040106A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - RIGHT HAND INBOARD TRACK NR 8 OUTBOARD FLANGE CAMLOCK RECEPTICLE CORRODED. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050414000742005041400074NM 2005 4 14 QXEA200400027 120041118A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT DIRTY A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09368PH 512 EMERGENCY FLOOR PATH LIGHTS STRIP HAS INTERMITTENT RED LIGHTS. MAINTENANCE CLEANED AND INSPECTED CONNECTOR PRIOR TO INSTALLATION OF FLOORBOARD. OPERATIONAL CHECKED EMERGENCY EXIT FLOOR PATHS LIGHTS. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202003292004020200329NM 2004 2 2 QXEA200400029 120040106A5320 SILL DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - CARGO DOOR SILL CORROSION AROUND NUT PLATES BOTTOM SIDE X571.00 AND YL40.00. REMOVED CORROSION IAW CPM CHAPTER 4D(3A). 2H72 4T RTA13NM 20040202003312004020200331NM 2004 2 2 QXEA200400031 120040107A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - SCRATCHES IN FUSELAGE SKIN UNDER AFT SIDE OF 262DT. REPAIRED IAW HORIZON AIR EA 2-53-530. 2H72 4T RTA13NM 20040202003322004020200332NM 2004 2 2 QXEA200400032 120040102A5531 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK IN IT WHERE FRAME MEETS UP WITH THE FOURTH STRINGER FROM THE TOP LEFT OF FUSELAGE. REPAIRED IAW RD8-55-199. 2H72 4T RTA13NM 20040202003362004020200336WP 2004 2 2 ABXA040033 120040115A2450 WARNING LIGHT DOUG DC9 DC932 3022066WP EMERGENCY POWER ILLUMINATED A ABXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23900AX 47380 DURING PREFLIGHT, EMERGENCY POWER CHECK, A/C EMERGENCY BUSS POWER OFF LIGHT ILLUMINATED. RESET EMERGENCY BUS BREAKER B1-185 IAW DC-9 WD MANUAL 24-23-00. SYSTEM OPS CHECKED GOOD. 2L72 4F A6WE 20040202003372004020200337NM 2004 2 2 PCAA0401156 120040118A3320BV033001248 SOCKET DHAV DHC8 DHC8102 2809003NM CABIN LIGHT ARCED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13804EX 227 AN ELECTRICAL ODOR AT CABIN ENTRANCE AREA. MAINTENANCE WAS NOTIFIED AND INSPECTED AREA TO FIND THAT THE LIGHT SOCKET AT ROW 3AC TO BE AT FAULT. WIRES WERE ISOLATED AND APPROPRIATE CIRCUIT BREAKERS PULLED. ONCE AIRCRAFT ARRIVED MAINTENANCE BASE AND PARTS WERE AVAILABLE, SOCKET WAS REPLACED AND SYSTEM CHECK GOOD. 2H72 4T RTA13NM 20040202003392004020200339EU 2004 2 2 2004UALA00024 120040109A2611RAI2800M0706 CONTROL UNIT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SMOKE DETECTOR MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29425UA 600 508 FLIGHT DIVERTED DUE TO FWD CARGO SMOKE WARNING. *S/D* THE SMOKE DETECTOR CONTROL UNIT (SDCU, FIN 10WQ) WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040202003412004020200341 2004 2 2 2004UALA00027 420040110A2565 BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29178UA 24385 UPPER DECK RIGHT DOOR SLIDE BATTERY LIGHT PRESS TO TEST FUNCTION INOP. CHANGED BATTERIES. 2L74 4F4 FRTA20WE E24NE 20040202003432004020200343NM 2004 2 2 2004UALA00030 120040112A5311 FRAME AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29815UA 867 FRAME 23 AT STR 36L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPLACED FRAME 23 LWR SECTION PER EVA -MOC 8468A. 2L72 4F4 FRTA28NM E40NE 20040202003442004020200344NM 2004 2 2 2004UALA00031 120040112A3020 SWITCH BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE COCKPIT MISUSED A UALAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 WP29620UA 21880 RETURNED TO BLOCKS DUE TO ANTI ICE VALVE WARNING. THIS INCIDENT OCCURRED MOST LIKELY WHEN THE LT ENGINE ANTI-VALVE WAS DEFERRED INOPERATIVE PER THE MEL, AND, THE LT ENGINE ANTI-ICE VALVE SWITCH WAS LEFT IN THE INCORRECT POSITION AFTER REVIEWING THE MEL PROCEDURE, IT HAS BEEN FOUND THAT THE MEL WAS UNCLEAR WHAT POSITION THE VALVE SWITCH SHOULD BE IN WHEN THE VALVE WAS DEFERRED INOP. THIS STEP IS BEING CLARIFIED IN A REVISION TO THE MEL PROCEDURE. 2L72 4F4 FRTA1NM E3NE 20040202003462004020200346NM 2004 2 2 2004UALA00036 120040114A3030 HEATER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE PITOT HEAD INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29334UA 24229 DIVERTED TO ORD WHEN PITOT HEAT FAILED. F/O PITOT STATIC 2 AUX P-S LIGHT CAME ON AND STAYED ON. P18-3 BREAKERS WERE CYCLED, BUT NO HELP. LT LOWER PITOT PROBE REPLACED. LOW RANGE LEAK TEST SUCCESSFUL. 2L72 4F4 FRTA16WE E2GL 20040202003472004020200347NM 2004 2 2 2004UALA00037 120040102A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 REMOVED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER AT LEFT SIDE FUSELAGE STA BS 593 IN ANTICIPATION OF SKIN SECTION REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. REINSTALLED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER. 2L72 4F4 FRTA2NM E17NE 20040202003482004020200348NM 2004 2 2 2004UALA00038 120040115A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ROW 1-9 BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29787UA 26939 EEL LIGHT BROKEN ON WALL BEHIND SEAT 9F. EEL LIGHTS INOP IN ROWS 1 THRU 9. EEL LIGHTS ARE INOP LEFT HAND WALL OF CENTER LAV 1. REPLACED LIGHT 2 & 3. SECURED CONNECTOR ON BATTERY PACK. 2L72 4F4 FRTT0001SE E46NE 20040202003492004020200349 2004 2 2 2004UALA00039 420040115A3416 INDICATOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ALTIMETER MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29953UA 26700 RETURNED TO DEN WHEN THE FLIGHT CREW REPORTED A PROBLEM WITH THE CAPTAINS AIRSPEED AND ALTIMETER. STATIC LINE WAS LEAKING. FLEX LINE WAS REPLACED. 2L72 4F4 FRTA16WE E2GL 20040202003512004020200351WP 2004 2 2 ABXA040034 120040106A33505708458503 BATTERY PACK DOUG DC8 DC861 3021952WP EMERGENCY LIGHT DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23842AX 917 46015 DURING MAINTENANCE INSPECTION, FOUND BATTERIES FOR THE EMERGENCY LIGHT EXPLODED W/O 600187843. REPLACED BATTERY PACK AND OPS CHECKED GOOD IAW DC-8 MM 33-50-02-2. 2L74 4F 4A25 20040202003542004020200354EU 2004 2 2 MALA040121 120040119A3060660713245 CONTROL UNIT SAAB SF340 340B 7860101EU PROP DEICE SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15404XJ 340B404 DURING FLIGHT 3196/3047, LEFT PROP DEICE LIGHT ILLUMINATED. LT PROP HEAT ANN ON IN FLIGHT IN BOTH NORM AND MAX RANGE. AIR RETURN TO MSP. MAINTENANCE TROUBLESHOT AND INSPECTED WIRING FOR BRUSH BLOCK LEADS AND PROP BOOTS, NO DEFECTS FOUND. REPLACED CONTROL UNIT (P/N 660713245) IAW AMM CH 30-61-10-4 S/N OFF 044-98, ON 052-98. OPS CHECK GOOD. 2L72 4T RTA52EU 20040203000022004020300002NE 2004 2 3 MALA040117 220040114A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FAILED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL15420XJ 340B420 GEE785284 LT ENG FAILED INFLIGHT. ONE STAGE 1 TURBINE BLADE SEPARATED FROM DISK BELOW BLADE PLATFORM, BLADE IMPALED IN STAGE 1 SHROUD. STAGE 1 ROTOR CONTINUED TO ROTATE, REMAINING 33 STAGE 1 TURBINE BLADES MACHINED OFF BY IMPALED BLADE. DEBRIS FROM 34 STAGE 1 TURBINE BLADES EXITED TAILPIPE. NO INTACT TURBINE BLADES STAGES 1, 2, 3 & 4 DISKS. DAMAGE STAGE 2, 3 & 4 TURBINE NOZZLES. TWO OF POWER TURBINE STRUTS SPLIT OPEN, L/E & METAL PEELED BACK. REMAINING 6 STRUTS DAMAGED. STAGE 3 TURBINE BRAIDED SEAL MATL PROTRUDING FROM HOLE STAGE 4 TURBINE NOZZLE. HEAT DAMAGE. OIL LVL FULL, COLOR NORM. STAGE 1 TURBINE BLADES NEW, ACCUMULATED 2520 HRS/2699 CYC. NO ENG PARAMETER ABNORM PRIOR TO EVENT. ENG SENT TO H&S. 2L72 4T4 TRTA52EU E8NE 20040203000042004020300004EU 2004 2 3 MALA040118 120040116A243023080031 GENERATOR SAAB SF340 340B 7860101EU RIGHT DC INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15417XJ 340B417 AFTER TAKEOFF ON FLIGHT 3085, EN ROUTE TO LSE LOST BOTH RIGHT EFIS SCREENS RIGHT DC GEN VOLTAGE SHOWED 20 VOLTS AND DROPPING. SHUT RIGHT GEN DOWN AS DIRECTED BY QRH. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RIGHT DC GEN IAW JOB CARD 243103, OPS CHECKS GOOD. P/N ON & OFF 23080-031, S/N OFF 99955, S/N ON 96444. 2L72 4T RTA52EU 20040130002302004013000230NM 2004 1 30 AALA20040061 120040108A7930 CHIP DETECTOR BOEING737 737823 13844BZNM GE CFM56 CFM56* 13802NE ZONE 600 MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21931AN 30079 ORD INFLIGHT/T1803/08 NUMBER 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. RETURNED TO STATION. LANDED WITHOUT INCIDENT. REPLACED OIL FILTER AND FOUND SMALL AMOUNT OF METAL. REPLACED STARTER AS PRECAUTIONARY. EVALUATED FLIGHT DATA RECORDER. SENT OIL SAMPLE TO ENGINEERING LAB FOR ANALYSIS, REF MM12-13-11-3. NO METAL FOUND IN OIL SAMPLE. REPLACED SEAVAGE OIL FILTER, SUPPLY OIL FILTER, START MOTOR, CHECKED FRONT AND REAR CHIP DETECTOR, DRAINED OIL TANK, LEAK CHECKED AT IDLE DRY MOTOR, RAN AT 80 - 85 PERCENT N2 FOR 15 MINUTES. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED CHIP DETECTOR INSPECTION IN 25 FLIGHT HOURS. NO FINDINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA16WE E2GL 20040130002342004013000234EU 2004 1 30 MALA040101 120040102A5347 MOUNT SAAB SF340 340B 7860101EU LAVATORY CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, FWD LAV AFT I/B MOUNT HAS CORROSION. CLEANED, PREPPED, AND REPAIRED LAV AFT TIE DOWN FITTING IAW MESABA EO S25064. A/C RELEASE DATE 01/06/04. REFER TO NR 1195871 FOR ADDITIONAL INFO. 2L72 4T RTA52EU 20040130002432004013000243EA 2004 1 30 SWIA200412757 120040104A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07592SW5844 5844 7279 FLAP FAIL MESSAGE WHEN SELECTING FLAPS AT 45 DEGREES. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040130002472004013000247SO 2004 1 30 SWIA200412761 120040110A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07292UX7536 6945 120292 FLAP DISAGREEMENT ON DEPARTURE WHEN RETRACTING FROM 15-0. RESELECTED 15 THEN 0 PER QRH TWICE AT DIFFERENT AIR SPEEDS WITH SAME RESULT. FLAP PANEL INDICATION: OUTBOARD SHOWED 2 DOTS, NAC AND INBOARD SHOWED 1 DOT EACH. REMOVED AND REPLACED FLAP COMPUTER WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040202000082004020200008NE 2004 2 2 QXEA200400011 220040113A7230 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 VIBRATION A QXEAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 NM09600QX 10005 GEE965221 PDR FLIGHT 2553 RETURN TO FIELD - NR 1 ENGINE N1 VIBRATION 1.7 TO 1.9. COMPLIED WITH PIN LUBES AND ENGINE RUNS. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040202000302004020200030NM 2004 2 2 AWXA200400045 120040113A2560P4010021 BATTERY BOEING757 7572G7 1384963NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - EMERGENCY EQUIPMENT - DURING C-12 CHECK FOUND THE EMERGENCY FLASHLIGHTS INOPERATIVE AT THE L-4 & R-3 DOORS. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES AT THE L-4 & R-3 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040202000562004020200056EA 2004 2 2 04007681 120040107A27501104SD100501 SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DIRTY A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27678BR 7653 DURING OPERATION OF AIRCRAFT CREW REPORTED A FLAP FAILURE MESSAGE WHEN FLAPS WERE AT ZERO DEGREES AND SELECTED TO 8 DEGREES. 2L72 4F RTA21EA 20040202000592004020200059EA 2004 2 2 04009678 120040109A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A VTZAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 EA27678BR 7653 DURING APPROACH TO BUF CREW RECEIVED A FLAP SYSTEM FAILURE MESSAGE WHEN FLAPS WERE A ZERO DEGREES AND SELECTED TO 8 DEGREES. CREW PERFORMED MISSED APPROACH TO BUF AND DETERMINED RUNWAY LENGTH WAS NOT ADEQUATE. FLIGHT 7802 THEN DIVERTED TO IAD AND PERFORMED A ZERO FLAP LANDING. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP POWER DRIVE UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040202000762004020200076NM 2004 2 2 AWXA200400047 120040114A3350BR964411 LIGHT BOEING737 737301 1384611NM SEAT ROW 8 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DFW - EEL - DURING THRU FLIGHT INSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT SEAT ROW 8 LT BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040202000792004020200079EA 2004 2 2 COMA0460038 120040114A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01952CA20590 7092 FS 235 RBL 6 NLG AFT DOOR CUT OUT HAS A .25 INCH CRACK ON FUSELAGE SKIN. REMOVED DAMAGE, FABRICATED REPAIR ANGLE FROM 2024-T42.063 (WVAC PO 169562), FILLER FROM 2024-T3.050 (WVAC PO 32674), FILLER AND DOUBLER FROM 2024-T3 .063 (WVAC PO 32572) AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-11-048 REV B. 2L72 4F RTA21EA 20040202000812004020200081NM 2004 2 2 04FDEA00150 120040115A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE CORRODED AT SPOT FACES. LT INBD FLAP OTBD HINGE (FLAP SIDE), INBD PIVOT HOLE SPOT FACES CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74282, WINGS - LT INBD TE FLAP HINGE BRACKET CORROSION. 2L73 4F RTA22WE 20040202000822004020200082NM 2004 2 2 04FDEA00151 120040115A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE CORRODED AT BORE AREA. LT INBD FLAP OTBD HINGE (FLAP SIDE), OUTBD PIVOT HOLE BORE CORROSION. REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74282, WINGS - LT INBD TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040202000852004020200085NM 2004 2 2 04FDEA00153 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), INBOARD ACTUATOR LUG HOLE FOUND CORRODED AT BORE AREA. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040202001122004020200112EA 2004 2 2 COMA0460048 120040109A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01467CA5007 7637 FLIGHT 5886 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040202001132004020200113NE 2004 2 2 COMA0460049 220040109A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAD RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 SO01914CA 7012 807143 FLIGHT 5774 DURING DEICING - FLAMES WERE REPORTED COMING FROM LEFT ENGINE. REPLACED THE LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040202001542004020200154WP 2004 2 2 UPS04841751 120040116A3250 RELIEF VALVE DOUG DC8 DC871F 302199DWP BOGIE UNLOCK STUCK A IPXAO OTHER O OTHER CRCRUISE 1 SO01706UP 46056 DURING CRUISE NOTICED HYDRAULICS DECREASING. FOLLOWED POM PROCEDURE AND DEPRESSURIZED AND ISOLATED THE SYSTEM. FOUND BOGIE UNLOCK CYLINDER RELIEF VALVE ON LEFT MAIN FEAR STUCK OPEN. REPLACED RELIEF VALVE POF 32-53-02. NO LEAKS DETECTED. HYD WAS SERVICED. 2L74 4F RT4A25 20040202001582004020200158NM 2004 2 2 04FDEA00170 120040116A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT WING LEADING EDGE PANEL INTERIOR MANY CRACKS FROM EOS 560 TO 620 BETWEEN SLAT TRACKS 10 AND 11. LT WING LEADING EDGE SKIN PANEL INTERIOR STA XOS 560 TO XOS 620 BETWEEN SLAT TRACK 10 AND 11, CRACKED AREA REPAIRED AS PER SRM 57-10-00, FIG.25, VOL.I. 2L73 4F RTA22WE 20040202001602004020200160NM 2004 2 2 04FDEA00172 120040116A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT WING LEADING EDGE PANEL INTERIOR SEVERAL CRACKS AT XOS 546 OUTBD OF REFUELING PANEL. RT WING LEADING EDGE XOS 546 INNER DOUBLER. REPAIRED AS PER SRM 57-10-00 FIG 25 V1. 2L73 4F RTA22WE 20040202001622004020200162EU 2004 2 2 MALA040108 120040101A3230HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15518XJ E2337 DURING FLIGHT 3600, LANDING GEAR WOULDN'T EXTEND UPON LANDING AND SHORTLY AFTER THE GREEN HI TEMP LIGHT ILLUMINATED AFTER COMPLETING THE QRH. EMERGENCY GEAR EXTENSION AND LANDED. FROM LOG SHEET 1259127 FOUND LANDING GEAR SELECTOR VALVE LEAKING AND FWD TO GEAR. REMOVED AND REPLACED SELECTOR VALVE IAW RJ MM P/N HTE9490-4, S/N ON FRTR008AY, ALL CHECKS ARE GOOD AT THIS TIME. 2H74 4F RTA49EU 20040202001662004020200166EU 2004 2 2 MALA040115 120040112A2910 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU YELLOW HYD SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15513XJ E2329 DURING FLIGHT 3654, YELLOW HYDRAULIC HIGH TEMPERATURE LIGHT ILLUMINATED IN FLIGHT. QRH FOLLOWED. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED YELLOW ISOLATION VALVE. ALL CHECKS GOOD. 2H74 4F RTA49EU 20040202001732004020200173NM 2004 2 2 04FDEA00177 120040116A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK LT STA 1341 TO STA 1361 SEAT TRACK REF X =75.25 SEAT TRACK HAS SURFACE CORROSION. MAIN CARGO DECK RH STA 1341TO STA 1365 SEAT TRACK REF. X =75.25 SEAT TRACK FLANGE CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 5 V1. 2L73 4F RTA22WE 20040202001802004020200180 2004 2 2 AWXA200400052 420040111A256581020401 SENSOR BOEING757 7572G7 1384963NM GIRT BAR FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 LCQ - EEL - DURING C-17 CHECK FOUND THE R-1 DOOR FORWARD & AFT GIRT BAR PROXIMITY SENSORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD & AFT R-1 DOOR GIRT BAR PROXIMITY SENSORS IAW BMM 25-66-11, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040202001812004020200181EA 2004 2 2 COMA0460062 120040114A301014463101 PICCOLO TUBE CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01934CA 7042 FLIGHT 5146 WING OVERHEAT WARNING. REPLACED THE LEFT WING OUTBOARD PICCOLO TUBE. 2L72 4F RTA21EA 20040202001842004020200184EA 2004 2 2 COMA0460059 120040115A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01958CA 7111 FLIGHT 5090 FORWARD FLOOR EMERGENCY LIGHT IS INOP. SECURED LOOSE WIRE CONNECTION. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040202001912004020200191NM 2004 2 2 CALA0400026 120040114A5512 SKIN BOEING737 737524 1384721NM HORIZONTAL STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759630 27534 THE RT HORIZONTAL STABILIZER LOWER SKIN SURFACE WAS FOUND DENTED APPROXIMATELY 1 INCH FROM FORWARD LOWER SPAR AND APPROXIMATELY 5 FT I/B OF TIP. REPAIRED IAW ECRA 5510-01704. 2L72 4F RTA16WE 20040202001922004020200192NM 2004 2 2 CALA0400027 120040115A5754 SKIN BOEING737 7373T0 1384582NM NR 4 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 4 SLAT SKIN LOWER SURFACE O/B OF ACTUATOR ATTACH. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20040202001932004020200193NM 2004 2 2 CALA0400028 120040115A5511 SPAR BOEING737 737524 1384721NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759630 27534 INSPECTION FOUND A GOUGE IN RT HORIZONTAL STABILIZER L/E SPAR CAP BETWEEN STA 239.9 AND 249.1 AT I/B SIDE. REPAIRED IAW ECRA 5510-01704. 2L72 4F RTA16WE 20040202001952004020200195NM 2004 2 2 CALA0400030 120040115A335020131A BATTERY BOEING737 737524 1384721NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714601 27314 THE EMERGENCY AISLE PATH LIGHTING IN FIRST CLASS CABIN FAILED AFTER 30 SECONDS OF TESTING. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. 2L72 4F RTA16WE 20040202002002004020200200NM 2004 2 2 DHL2004753505 120040105A5330 SKIN BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 DURING C-CHECK, C-2 DOOR CUTOUT AT FRAME INNER CHORD SHOW CORROSION AND CRACK FROM FASTENER BS 990 STR 990 STR 26R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. REMOVED CORROSION ON L-2 DOOR CUTOUT AFT FRAME IAW B-727 SRM 51-10-6 MAT LOSS .001 FOUND WITHIN LIMITS IAW B-727 SRM 53-10-1. FAB ANGLE REPAIR FROM 1503-100274 SIZE 1 X 2 X 7.5 INCH IAW B-727 SRM 51-40-4 FIG 1. TREATED AND PRIMED ANGLE REPAIR AND AREA IAW B-727 SRM 51-10-2. INSTALLED ANGLE RETAIL IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040202002042004020200204SO 2004 2 2 C2XA04TY012 120040115A532014529150009 PROFILE EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE Z PROFILE OF THE CENTER FLOORBEAM AT FRAME 24. MAINTENANCE REMOVED AND REPLACED THE Z PROFILE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002092004020200209SO 2004 2 2 C2XA04TY016 120040116A531514522226003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM TOP CAP AT FRAME 58. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002142004020200214SO 2004 2 2 RAIA00401009 120040109A301010006492 VALVE EMB 145 EMB145LR 3260212SO ANTI ICE SYS MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03822HK7534 145069 STAB ANTI-ICE FAIL MESSAGE. MAINTENANCE REPLACED STAB ANTI-ICE VALVE. 2L72 4T RTT00011AT 20040202002212004020200221SO 2004 2 2 C2XA04SH022 120040119A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711548 145565 SHV- DURING C-CHECK THE FORWARD CEILING EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE DURING AN OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE ELECTROLUMINESCENT LAMP. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202002232004020200223NM 2004 2 2 DHL2004752511 120040104A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, FUSELAGE EXTERIOR ABOVE STR 28R BS 500 DENTED (PREVIOUSLY MAPPED). CUT OUT DAMAGED AREA DIM .5 X 5 INCH AND FABBED REPAIR DOUBLER FROM 2024 T3 .050 DIM 10 X 9 INCH PO 900414 IAW B-727 SRM 53-30-3 FIG 1. DOUBLER TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 53-30-3 FIG 1. 2L73 4F A3WE 20040202002262004020200226EU 2004 2 2 CX7A194J0403 120040117A26121734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03307CE 340B204 LEFT TAILPIPE HOT LIGHT ILLUMINATED WHEN POWER SELECTED ON. MOISTURE PRESENT IN AREA. RAN ENGINE AND LIGHT EXTINGUISHED. 2L72 4T RTA52EU 20040202002352004020200235WP 2004 2 2 04FDEA00187 120040118A3260 WARNING LIGHT DOUG DC10 DC1010 3022110WP MLG ILLUMINATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25366FE 46602 AFTER GEAR RETRACTION HAD RIGHT MAIN GEAR UNSAFE RED LIGHT ILLUMINATED ON FORWARD AND S/O PANEL. COMPLIED WITH QRH, CYCLED GEAR AND LIGHT WENT OUT. INSPECTED GEAR AND DOOR PER TAFI PG 109 32-30-00 AF. A/C OK FOR SERVICE. 2L73 4F A22WE 20040202002392004020200239NM 2004 2 2 QXEA200400036 120040117A3620 SWITCH BOMBDRDHC8 DHC8401 1390041NM OVERTEMP INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09410QX 4053 PDX - FLT 2307 RETURNED TO FIELD, BLEED HOT CAUTION ON CLIMBOUT. REPLACED OVERTEMP SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202002412004020200241NM 2004 2 2 ABXA040031 120040105A32311497695511 BELLCRANK BOEING767 767281 1385109NM RT MLG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23773AX 22788 RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BEAM ASSEMBLY HAD THE LOWER FITTING CRACKED AT THE INBOARD SIDE AT FASTENER. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR CENTER HINGE BELLCRANK AND OPS CHECKED IAW B767 MM 32-12-01-4 AND 32-12-00-0. 2L72 4F RTA1NM 20040202002432004020200243NM 2004 2 2 QXEA200400037 120040114A2611824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY DEFECTIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09352PH14861 494 SEA - LAVATORY SMOKE DETECTOR ALARM ACTIVATED IMMEDIATELY AFTER TAKEOFF. THERE WAS NO SMOKE OR HAZE IN CABIN. THE FLIGHT ATTENDANT PRESSED THE TEST BUTTON AND THE ALARM RESET. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202002452004020200245 2004 2 2 219PA0011 420040102A22104084042911 COUPLER BOEING737 737222 1384473NM YAW DAMPER DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05219PA 19956 YAW DAMPER LIGHT STAYS OFF WHEN SWITCHED FROM ON TO OFF. REPLACED YAW DAMPER COUPLER, OPS CHECKS NORMAL PER MM 22-12-01. 2L72 4F A16WE 20040202002602004020200260WP 2004 2 2 AALA20040072 120040117A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21443AA 49469 ORD CEILING EMERGENCY LIGHTS AT SEAT 18 THROUGH 21 INOPERATIVE. CLEANED BATTERY CONNECTIONS ATB5-104. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040202002612004020200261EU 2004 2 2 AALA20040075 120040117A3350 LIGHT AIRBUS300 A300B4605R 3930308EU EXIT SIGN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW218067A 510 MIA OVERHEAD EXIT SIGN AT L3 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR OVERHEAD EXIT SIGN AT L3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040202002622004020200262NM 2004 2 2 CALA0400033 120040116A5312 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714336 23574 INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT PRESSURE DECK AT STA 664. REPAIRED PRESSURE WEB DECK IAW SRM 53-60-51, FIGURE 203 AND ECRA 5312-01024. 2L72 4F RTA16WE 20040202002632004020200263NM 2004 2 2 CALA0400034 120040116A5414 SKIN BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND A 1.25 INCH CRACK NR 2 PYLON PANEL NR 5842R. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20040202002642004020200264NM 2004 2 2 CALA0400035 120040116A5330 SKIN BOEING757 757324 1384930NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757852 32811 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 630, L16L. THE SKIN WAS REPAIRED IAW SRM 53-00-01. 2L72 4F RTA2NM 20040202002802004020200280 2004 2 2 QXEA200400041 420040116A342042000332501 COMPUTER BOMBDRDHC8 DHC8401 1390041NM ELEVATOR FEEL FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09539DS2813 2813 4016 GEG- ON FLIGHT 2323 SEA TO HLN AIRCRAFT DIVERTED TO GEG DUE TO NR 1 PFD ATTITUDE AND HEADING FAILURE AND ELEVATOR FEEL CAUTION LIGHT ILLUMINATED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 1 AHRU COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202003062004020200306NE 2004 2 2 002701 220040120A7320 FUEL CONTROL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE NR 1 ENGINE INOPERATIVE A UHLAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL17340SZ 340A004 504 DRG550089 ON 01-20-2004, APPROX 1130 (UTC), FLT 4633 BGM-PIT, NR 1 ENGINE HAD NO FUEL FLOW, ENGINE WOULD NOT START. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040202003112004020200311 2004 2 2 AWXA200400056 420040117A2211 COMPUTER AIRBUSA319 A319132 3930340NM FLT MANAGE MALFUNCTIONED A AWXAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 WP28660AW 1234 JFK - AIR TURNBACK - FLT 0011 - AFTER TAKEOFF FROM JFK EN ROUTE TO PHX RECEIVED A DUAL FLIGHT MANAGEMENT GUIDANCE COMPUTER FAIL AND IR 3 FAULT, TURNED BACK TO JFK. MAINTENANCE PERFORMED A COMPLETE SYSTEM RESET. PERFORMED AUTO FLIGHT SYSTEM TEST IAW AMM 22-46-00-501, PERFORMED FLIGHT MANAGEMENT SYSTEM TEST IAW AMM 22-70--00-501, AND PERFORMED AIR DATA TEST FOR IR 3 FAULT IAW AMM 34-13-00-501, NO FAULTS WERE NOTED. 2L72 4F RTA28NM 20040202003122004020200312NM 2004 2 2 AWXA200400057 120040119A3150 WARNING HORN BOEING737 73733A 1384673NM SPEED BRAKES ACTIVATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28164AW 23625 PHX - ABORTED TAKEOFF - FLT 0429 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR ELP TAKEOFF WARNING HORN SOUNDED, REJECTED TAKEOFF AT 60 KTS. FOUND SPEED BRAKES NOT STOWED, STOWED SPEED BRAKES AND TOOK OFF WITHOUT FURTHER EVENT. 2L72 4F RTA16WE 20040202003162004020200316WP 2004 2 2 AALA40020082 120040120A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21466AA 49596 PHX CEILING EMERGENCY LIGHT AT ROWS 24 THROUGH 27 INOPERATIVE. REPLACED B5-106 BATTERY PACK/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHT FOR ROWS 24 THROUGH 27 AT STATION 1057R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050414000782005041400078NM 2005 4 14 QXEA200400018 120041219A2820 LINE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 LT HAND WING FUEL BAY AT 522CT, HAS TWO FUEL LINES RUBBING IN TANK YW1545. REPAIRED IAW AMM 28-21-06 AND HORIZON AIR EA 6-28-20. 2H72 4T RTA13NM 20040202003232004020200323NM 2004 2 2 QXEA200400020 120040104A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - TOP FLANGE GOUGED AND SCRATCHED ON RIGHT HAND OUTBOARD TRACK NR 11. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20040202003252004020200325NM 2004 2 2 QXEA200400022 120040106A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - RIGHT HAND INBOARD TRACK NR 8 INBOARD FLANGES CHAFED. REPAIRED IAW DHC-8-200 51-20-16. 2H72 4T RTA13NM 20040202003272004020200327NM 2004 2 2 QXEA200400024 120040106A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - CARGO COMPARTMENT LEFT INBOARD TRACK NR 6 CORROSION AROUNT NUT PLATE AT APPROXIMATELY X582.00. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20050414000732005041400073NM 2005 4 14 QXEA200400026 120040106A3350 CONNECTOR DHAV DHC8 DHC8202 2809007NM BATTERY PACK LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09375PH 529 PDX-3RD AND 4TH EMERGENCY TRACK LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. MAINTENANCE RESEATED CONNECTOR ON BATTERY PACK NR 5. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050414000752005041400075NM 2005 4 14 QXEA200400028 120041125A33501014011 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PSC-FORWARD EMERGENCY EXIT DOOR BETA LIGHT FAILS BRIGHTNESS CHECK. MAINTENANCE REMOVED AND RELACED FORWARD EMERGENCY EXIT DOOR BETA LIGHT ASSY. BRIGHTNESS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040202003302004020200330NM 2004 2 2 QXEA200400030 120040107A5340 FITTING DHAV DHC8 DHC8202 2809007NM ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - AFT LEFTHAND BATH TUB FITTING CHAFED. REPAIRED IAW RD 8-53-2108. 2H72 4T RTA13NM 20040202003332004020200333NM 2004 2 2 QXEA200400033 120040102A5531 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - VERTICAL STABILIZER FRAME NR 4 HAS A CRACK APPROXIMATELY 3.4 INCH LONG WHERE FRAME MEETS UP WITH THE 4TH STRINGER FROM THE TOP RIGHT SIDE OF FUSELAGE. REPAIRED IAW RD 8-55-199. 2H72 4T RTA13NM 20040202003352004020200335SO 2004 2 2 C2XA04SH024 120040121A531514522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV-DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 58 AND 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202003502004020200350WP 2004 2 2 ABXA040035 120040115A33505708458503 BATTERY PACK DOUG DC8 DC861 3021952WP EMERGENCY LIGHT DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23842AX 17 46015 DURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. OPS CHECKED EVERY EXIT LIGHT IAW DC8-1, STEP 7. OPS CHECKED GOOD. OPS CHECKED AGAIN, NO GOOD. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 WDM 33-51-01. OPS CHECKED GOOD IAW DC8-1, STEP 7. 2L74 4F 4A25 20040202003522004020200352NM 2004 2 2 252TR0016 120040116A7330 O-RING BOEING737 737228 13844AGNM FF TRANSMITTER LEAKING A PIDAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO05252TR 23001 RIGHT ENGINE HAS FUEL LEAK AT FUEL FLOW TRANSMITTER. REPLACED O-RINGS ON FWD AND AFT OF TRANSMITTER. NO LEAKS NOTED ON ENGINE RUN PER MM 73-31-12. 2L72 4F RTA16WE 20040203000012004020300001EU 2004 2 3 MALA040119 120040117A3260 SWITCH SAAB SF340 340B 7860101EU MLG FROZEN A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15420XJ 340B420 DURING FLIGHT 3008/3130, OUT OF MKG, THIS A/C DID AN AIR TURNBACK INTO MKG BECAUSE THE INTRANSIT LIGHT REMAINED ON AFTER TAKEOFF. OUTSTATION MAINTENANCE FOUND THE GEAR AND SWITCH WERE COVERED IN ICE. MAINTENANCE CLEANED OFF ICE AND CONDUCTED TEST FLIGHT 3130 TO VERIFY REPAIR. NO FURTHER PROBLEMS. 2L72 4T RTA52EU 20040203000032004020300003EU 2004 2 3 MALA040120 120040118A3620 CONNECTOR BAC 146 AVRO146RJ85A1500097EU NR 3 ENGINE LOOSE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15501XJ E2208 DURING FLIGHT 3545/3483/3447, NR 2 ENGINE INTAKE LOW PRESSURE LIGHT ILLUMINATED AND ANTI-ICE WARNING C/B POPPED. RESET, POPPED AGAIN. DURING CLIMBOUT ENGINE NR 2 LOW PRESSURE LIGHT CAME ON AFTER SELECTING ENGINE ICE ON. COMPLETED QRH AND NO HELP. AIR RETURN TO MEM. MAINTENANCE FOUND CONNECTOR ON NR 3 ENGINE LOW PRESSURE SWITCH NOT TIGHT, RESECURED. 2H74 4F RTA49EU 20040203000052004020300005WP 2004 2 3 ABXA040037 120040119A2422ASH7341 INVERTER DOUG DC9 DC932 3022066WP EMERGENCY POWER DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX8004 47380 DURING PRE-FLIGHT, TURNED EMERGENCY POWER SWITCH ON AND AC EMERGENCY BUS OFF LIGHT CAME ON. REMOVED AND REPLACED EMERGENCY AC POWER INVERTER IAW DC-9 MM. OPS CHECKED GOOD. 2L72 4F A6WE 20040203000972004020300097NM 2004 2 3 CALA0400046 120040119A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 303, RBL 54. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040203000992004020300099 2004 2 3 C1HA200474002 420040117A2565 SLIDE BOEING727 727225 1384077NM R-2 LOW A C1HAK NONE O OTHER ININSP/MAINT 1 GL15674MG 21450 R-2 EVACUATION SLIDE READING BELOW LIMITS. REMOVED AND REPLACED R2 ESCAPE SLIDE PER CHAMPION AIR MM 25-60-15. 2L73 4F A3WE 20040203001002004020300100NM 2004 2 3 UPS04441752 120040105A5330 SKIN BOEING747 747123F NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2348 - 2355 STR 3 (RT). THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1. 2L74 4F A20WE 20040203001012004020300101NM 2004 2 3 UPS04441753 120040105A5330 SKIN BOEING747 747123F NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2365 - 2390 RT STR 3, THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20040203001042004020300104NM 2004 2 3 UPS04441762 120040106A5320 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C- BS 680 - 700 LBL 78 LONGITUDINAL FLOOR SUPPORT WEB FOUND CRACKED AS MARKED. DEFECTIVE AREA WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040203001082004020300108NM 2004 2 3 UPS04441766 120040102A5320 SUPPORT BOEING747 747123F NM RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, RIGHT BLG WHEEL WELL O/B SIDE UPPER SKIN SUPPORT WEB CRACKED AT STA 1416. RIGHT BLG WHEEL WELL O/B BS 1416 STR 29R TO STR 31R FRAME REPAIR CARRIED OUT IAW HX RS R-53-42-35097. (RA 747-53-20163). 2L74 4F A20WE 20040203001092004020300109NM 2004 2 3 UPS04441767 120040106A575365B078455 RIB BOEING747 747123F NM LT WING TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 LEFT WING L/E NR 2 VC FLAP O/B ROTARY ACTUATOR SUPPORT RIB MOUNTING HOLE NR 2, 3, 4 AND NR 1 BORE FOUND SURFACE CORRODED (LOOKING O/B). LEFT WING L/E NR 2 V/C FLAP O/B ROTARY ACTUATOR SUPPORT RIB REPLACED PER SRM 51-10-01 PG 8. NR 2 V/C FLAP REF MM 27-81-02 RIGGING AND OPERATION CHECK CARRIED OUT PER MM 27-81-00. CORROSION BLEND OUT FINAL SIZE 0.434 INCH DIA OUT HOLES NR 2 TO NR 4 OLES 1453 .25. 2L74 4F A20WE 20040203001132004020300113NM 2004 2 3 P9RA20040003 120040121A3350S41750911SMI LIGHT BOEING757 757236 1384971NM RROYCERB211 RB211535E43754555NE AFT LAV. AREA INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962PG 24119 TWO EMERGENCY LIGHTS OUT AT AFT LAVATORY LOCATION. REMOVED AND REPLACED FLOOR LIGHT ASSY'S AT AFT LAV LOCATION IAW MM 33-10-01. 2L72 4F4 FRTA2NM E12EU 20040203001142004020300114NM 2004 2 3 04FDEA00199 120040121A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT WING - UPPER SURFACE, FASTENER (1 EA) POPPED UP AT XORS 230, STA 1413. 2L73 4F RTA22WE 20040203001192004020300119WP 2004 2 3 AALA20040088 120040119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21297AA 49309 DEN CEILING EMERGENCY LIGHTS AT 28 THROUGH 29 DEF INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203001202004020300120WP 2004 2 3 AALA20040087 120040119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21297AA 49309 DEN EMERGENCY LIGHTS AT CEILING 24 THROUGH 26DEF INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203001232004020300123WP 2004 2 3 AALA20040091 120040120A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21555AN 53085 SAN FORWARD EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED CONTROL MODULE AND REPAIRED SEAT WIRING FOR FORWARD EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203001242004020300124EA 2004 2 3 SWIA200412773 120040114A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07445SW2859 2859 7651 CREW REPORTS GROUND SPOILER FAULTS. REMOVED & REPLACED NR 1 SECU, REF MM 27-61-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040203001252004020300125EA 2004 2 3 SWIA200412774 120040112A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07432SW 7548 SPOILERONS FAULT STATUS MESSAGE APPEARED. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECKS GOOD. 2L72 4F RTA21EA 20040203001262004020300126SO 2004 2 3 SWIA200412775 120040106A2797 WIRE EMB 120 EMB120ER 3260203SO NACELLE FLAPS DAMAGED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07188SW 120039 ON TAXI WITH FLAP SELECTOR SET TO 15 DEGREES AFTER 1-2 MINUTES, FLAP & ADV SWS ON MAP POSITION INDICATOR 0 DEGREES OUTBOARD LIGHT BAR 4 LIGHTS NACELLE, INBOARD AND COMD ONE LIGHT BAR. AFTER FIVE MINUTES SYSTEM CORRECTED ITSELF. INSTALLED NEW WIRES TO I/B, O/B & NACELLE FLAP ACTUATORS FROM FUSELAGE P0365. INSTALLED CONNECTORS (NEW) AT ACTUATORS AND AT FUSELAGE P0365. REFERENCE EMB WM 27-51-00. CONTINUITY CHECK SATISFACTORY. 2L72 4T RTA31SO 20040203001292004020300129EA 2004 2 3 MASA200400010 120040105A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG LEAKING A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07759874198 2869 7405 ASH 2683 AVP-PHL, CREW REPORTED NOSE GEAR UNSAFE AFTER T/O. CREW TOOK A/C TO PHL. MX REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD ON CHECK FLIGHT. 2L72 4F RTA21EA 20040203001302004020300130EA 2004 2 3 MASA200400011 120040105A3230 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG LEAKING A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW077598712009 7405 ASH 2750 PHL-CVG. REPORTED NOSE GEAR UNSAFE AFTER T/O WITH NWS INOP MSG. MX REPLACED MLG PRIORITY VALVE. CHECKS BAD ON CHECK FLIGHT. MX IS TROUBLESHOOTING. MX REPLACED THE NOSE LANDING GEAR. OP CHECKS GOOD. 2L72 4F RTA21EA 20040203001352004020300135 2004 2 3 015042 420040114A2210 COMPUTER BEECH 1900 1900C 1154161CE YAW DAMPER ODOR A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27210CJ UC110 R ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER, YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C. 2L72 4T RTA24CE 20040203001362004020300136EU 2004 2 3 MALA040123 120040120A27518565M1 TRANSDUCER SAAB SF340 340B 7860101EU TE FLAPS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15429XJ 340B429 DURING FLT, FLAP FAULT LIGHT ON AFTER TAKEOFF. SHORTLY AFTER LEVELING FOR CRUISE FLIGHT, THE FLAP FAULT CWP ILLUMINATED AND WENT OUT SEVERAL TIMES. THE RIGHT FLAP INDICATOR MOVE SLIGHTLY WHEN THE CWP ILLUMINATED, ALSO FELT A SLIGHT PITCH CHANGE. AIR RETURN TO MSP. DURING THE RETURN FLIGHT TO MSP ALL WORKED PROPERLY, HOWEVER WITH THE FLAPS 15 AND 20 SELECTED THE INDICATOR SHOWED 13 DEG AND 18 DEG RESPECTIVELY. MAINTENANCE REMOVED AND REPLACED RIGHT FLAP TRANSDUCER PER AMM 27-53-05-2, OPS CHECK GOOD. P/N ON & OFF 8565M1, S/N OFF 96070041, S/N ON 96100078. 2L72 4T RTA52EU 20040203001382004020300138NM 2004 2 3 P5CA0401030 120040121A5230D20702 ACTUATOR BOEING747 74747UF 1384949NM CARGO DOOR FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23496MC 29257 ON ARRIVAL UNABLE TO OPEN SIDE CARGO DOOR MANUALLY. DOOR LATCH SYS PREVIOUSLY DEFERRED. REPLACED DOOR LATCH ACTUATOR PER MM 52-00-00, OPS CHECK NORMAL. DEFERRAL CLEARED. 2L74 4F RT1384945 20040203001402004020300140NM 2004 2 3 QXEA200400046 120040114A5740 BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - S-BRACKET CRACKED BOTH FLANGES AT TOP END. LEFT HAND WING FORWARD SPAR AT STATION YW55.0. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040203001412004020300141NM 2004 2 3 QXEA200400047 120040114A5720 BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - FRONT SPAR BLEED AIR ATTACH BRACKET CRACKED AT TOP, 2 RIVETS AT WS YW45.00 RIGHT HAND WING. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040203001432004020300143NM 2004 2 3 QXEA200400049 120040117A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - NR 10 SEAT TRACK HAS CORROSION PITS IN BOTTOM OF CHANNEL, BELOW RIGHT HAND LUG. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040203001442004020300144NM 2004 2 3 QXEA200400055 120040119A1430 RIVET DHAV DHC8 DHC8202 2809007NM ZONE 200 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - LOOSE RIVET IN RIGHT HAND WING ROOT FAIRING, LOWER EDGE X426 BELOW WING REAR SPAR. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040203001452004020300145NM 2004 2 3 DHL2004750002 120040120A3350 LIGHT BOEING727 7272M7 138407SNM CABIN INOPERATIVE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01750DH 21951 FOUND EMERGENCY EXIT LIGHT ASSEMBLY (LOCATED OVER ENTRY DOOR) ON ENTRY WAY FLOOR. REINSTALLED LIGHT ASSEMBLY, OPS CHECKED GOOD IAW B-727 M/M 33-50-01. 2L73 4F A3WE 20040203001462004020300146NM 2004 2 3 DHL2004742001 120040121A2612 INSULATION BOEING727 727225 1384077NM FIRE LOOP DAMAGED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01742DH 21290 ENGINE NR 1 DETECTOR CIRCUIT GROUND FAULT LIGHT ILLUMINATED P6-3 PANEL. TRANSFERRED TO DMI LOG 15451 MEL REF 36-9-1 CAT-C. PLACARD INSTALLED. REF DMI 15451 ENGINE NR 1 DETECTOR CIRCUIT GROUND FAULT LIGHT ILLUMINATED P6-3 PANEL. FOUND CLAMP INSULATION BENT ON FIRE LOOP ENGINE NR 1. ADJUSTED CLAMP INSULATION. OPS CHECKED GOOD AS PER M/M 26-11-00. THIS CLEARS DMI 15451. PLACARD REMOVED. 2L73 4F A3WE 20040203001472004020300147SO 2004 2 3 C2XA04BT009 120040121A4920 BLEED VALVE EMB 145 EMB145LR 3260212SO APU UNSECURE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2726545 145558 CREW REPORTED FUEL SMELL WHEN APU STARTS & BLEED IS ON. MAINTENANCE INSPECTED AND PLACED THE APU ON MEL AND RELEASED THE AIRCRAFT IAW MEL NR 49-00-00 CATEGORY-C CONTROL 035629. AFTER ARRIVAL EWR MAINTENANCE RESECURED THE APU BLEED AIR VALVE IAW EMB145MM 36-12-01. OPS CHECK GOOD. REMOVED APU FROM THE MEL, AND RETURNED AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20040203001492004020300149EA 2004 2 3 COMA0460069 120040120A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS FAILED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01716CA 7250 FLIGHT 5211 FLAPS FAILED AT 26 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040203001512004020300151EA 2004 2 3 COMA0460071 120040119A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STABILIZER MALFUNCTIONED A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01709CA 7238 FLIGHT 5839 STAB TRIM AND MACH TRIM DISENGAGED DURING FLIGHT. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040203001552004020300155NM 2004 2 3 MWEA040011 120040122A53205910158107 SEAL DEPRESSOR BOEING717 717200 1383700NM CARGO DOORWAY BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31908ME 55172 AFT CARGO DOOR OPENING LOWER SEAL DEPRESSOR IS BENT AT STATION 982. REMOVED AND REPLACED DEPRESSOR. 2L72 4F TRA6WE 20040203001562004020300156EA 2004 2 3 COMA0460072 120040119A77126015091013 SIGNAL COND UNIT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01962CA19550 7123 FLIGHT 5499 RT ENGINE VIBRATION CAUTION DURING T/O. REPLACED THE SIGNAL CONDITIONER. 2L72 4F RTA21EA 20040203001592004020300159NM 2004 2 3 CALA0400048 120040121A5730 PANEL BOEING737 7373T0 1384582NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND A .75 INCH CRACK IN RT WING NR 6 SLAT AUX TRACK AT I/B AUX TRACK CUTOUT (FIXED L/E PANEL). THE CRACK WAS STOP DRILLED IAW SRM 57-41-01, FIGURE 101, SHEET 4, NOTE O AND P. THE CRACK WAS PLACED ON DIP TO REINSPECT EVERY 400 HOURS AND REPAIR WITHIN 24 MONTHS OR NEXT CHECK. 2L72 4F RTA16WE 20040203001602004020300160NM 2004 2 3 CALA0400049 120040121A5710 BEAM BOEING737 7373T0 1384582NM LT WING T/E CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND A 2 INCH CRACK IN LT WING T/E BEAM (IN FRONT OF AILERON CENTER HINGE). REMOVED AND REPLACED BEAM IAW SRM 51-10-02. 2L72 4F RTA16WE 20040203001622004020300162NM 2004 2 3 AWXA200400060 120040121A3350BR964411 LIGHT BOEING757 7572S7 1384962NM SEAT ROW 13 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28903AW 23323 PHX - EEL - DURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040203001632004020300163EU 2004 2 3 AWXA200400061 120040119A3397E0052R8B3APNE CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 11 LT LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 MCN - EEL - DURING C-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 11 LT WILL NOT LOCK ONTO THE RECEPTACLE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 11 LT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040203001642004020300164EA 2004 2 3 COMA0460073 120040121A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01937CA 7044 FLIGHT 5506 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040203001662004020300166EA 2004 2 3 COMA0470010 120040121A2121GG670950283 FAN CNDAIRCL600 CL6002C10 1390015EA GALLEY MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01390CA1507 10106 FLIGHT 5326 RT PACK FAULT STATUS MESSAGE AND RT PRSOV CLOSED IN FLIGHT. REPLACED THE GALLEY FAN. 2L72 4F RTA21EA 20040203001672004020300167NM 2004 2 3 AALA20040096 120040120A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21782AN 30003 DFW EMERGENCY LIGHTS IN TOURIST CLASS ROWS 30 THROUGH 43 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT ROWS 30 THROUGH 43. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040203001682004020300168NM 2004 2 3 AALA20040097 120040120A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21782AN 30003 DFW FIRST CLASS EMERGENCY LIGHTS ON BOTH SIDES FOR ROWS 2 THROUGH 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON BOTH SIDES FOR ROWS 2 THROUGH 4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040203001692004020300169WP 2004 2 3 AALA20040101 120040120A30406172 CONTROLLER DOUG DC9 DC982 3022082WP WINDSHIELD INOPERATIVE A AALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2170401 49312 TUL INFLIGHT ORD-ABQ T0607/20 CENTER WINDSHIELD ARCHED THEN CRACKED AT FL280. PULLED CIRCUIT BREAKER X25 AS PRECAUTION. LANDED WITHOUT INCIDENT AT TUL. REPLACED CENTER WINDOW AND CENTER ANTI-ICE CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203001702004020300170NM 2004 2 3 AALA20040100 120040119A275118173810 TRANSMITTER BOEING737 737823 13844BZNM TE FLAPS INOPERATIVE A AALAO OTHER N FALSE WARNING DEDESCENT 1 SW21972AN 90097 ORD INFLIGHT T576/19 LEADING EDGE FLAPS TRANSIT LIGHT REMAINED ON DURING FLAP EXTENSION. TRAILING EDGE FLAP INDICATOR STUCK BETWEEN 0 AND 1. RECYCLED WITHOUT CORRECTING. LOWERED TRAILING EDGE FLAPS USING ALTERNATE MEANS. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FLIGHT DATA RECORDER INDICATED THE RIGHT HAND FLAP POSITION TRANSMITTER WAS LAGGING DURING EXTENSION. REPLACED RIGHT HAND FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040203001712004020300171NM 2004 2 3 AALA20040098 120040120A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21782AN 30003 DFW BUSINESS CLASS EMERGENCY LIGHTS ON BOTH SIDES AT ROWS 9 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS ON BOTH SIDES AT ROWS 9 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040203001772004020300177NM 2004 2 3 PCAA0401157 120040121A2910DSC252B40124 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA13837EX 217 FLIGHT NR 3928 WHILE ON GROUND IN DCA NOTICED THE NR 2 HYDRAULIC QUANTITY INDICATED 1.2 QUARTS. PRIOR TO AIRCRAFT PARKING THE HYDRAULIC ISOLATION VALVE ACTIVATED. MAINTENANCE REPLACED THE RIGHT HAND NOSE LANDING GEAR DRAG STRUT ACTUATOR LINE, SERVICED SYSTEM AND GROUND OPERATIONAL CHECKED. SYSTEM CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203001802004020300180NM 2004 2 3 SWAA040184 120040120A3350101331 LENS BOEING737 7373H4 1384600NM EXIT SIGN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20040203001832004020300183 2004 2 3 SWAA040187 420040120A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203001842004020300184 2004 2 3 SWAA040188 420040120A2565D31354 SLIDE BOEING737 7373Y0 1384671NM L2/R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C1 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040203001872004020300187NM 2004 2 3 SWAA040191 120040120A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR CUTOUT FORWARD LOWER CORNER FUSELAGE SKIN CRACKED. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203001912004020300191NM 2004 2 3 SWAA040195 120040120A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND 2 EACH FORWARD CARGO COMPARTMENT STRINGER CLIPS CRACKED AT BS 500D, BETWEEN STRINGER 19R AND STRINGER 19L. REPAIRED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040203001922004020300192NM 2004 2 3 SWAA040196 120040120A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACK AT BS 807. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040202001452004020200145WP 2004 2 2 UPS04841720 120040106A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STATION 1766 LONG 17L IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 5649327 AND SRM 51-1-20D, 51-1-21, 53-5-1 FIG 7. 2L74 4F RT4A25 20040202001512004020200151WP 2004 2 2 UPS04841745 120040106A57135644793502 STRINGER DOUG DC8 DC871F 302199DWP NR 4 FUEL TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE: C3, STRINGER 59 IS CRACKED OUTBOARD OF XRS 428 INSIDE 505B NR 4 ALT TANK. REMOVED, FABRICATED AND REPLACED FITTING IAW UPS ENGINEERING FILE NUMBER DC8-57-20103. 2L74 4F RT4A25 20040202001652004020200165EU 2004 2 2 MALA040116 120040115A3150GJ21 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU MLG ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15516XJ E2334 DURING FLIGHT 3483, RT GEAR UNSAFE LIGHT WITH GEAR HANDLE INTRANSIT LIGHT ILLUMINATED, WHILE GEAR SELECTED UP. WHEN GEAR SELECTED DOWN ALL INDICATIONS NORMAL. CHEATED RIGHT GEAR DOOR AND UPLOCK SWITCHES ALL CONDITIONS NORMAL. MANUALLY MOVED UPLOCK LATCHES TRAVEL, OPS NORMAL NEAR FAR PAX SWITCH OPS OK. SWAPPED PCB GJ21 AND GJ17 RIGHT MAIN, LT MAIN GEAR FOR T/S SEE DISC NR 6 FOR TEST FLT. 2H74 4F RTA49EU 20040202001762004020200176NM 2004 2 2 P9RA20040002 120040115A3260 POSITION SWITCH BOEING727 727231 1384079NM PWA JT8 JT8D* NE RT MLG DOOR DIRTY A P9RAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO1154344 21631 RIGHT GEAR DOOR LIGHT ON FLIGHT ENGINEERS PANEL DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION. CLEANED RIGHT HAND GEAR DOOR POSITION SWITCH AND CHECKED SWITCH ADJUSTMENT. OPS CHECK OF DOOR INDICATION SYSTEM GOOD IAW MM 32-62-11. 2L73 4F4 F A3WE E2EA 20040202001892004020200189WP 2004 2 2 CALA0400024 120040114A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2783870 48056 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 560 BETWEEN L22L AND L23L. REPAIRED IAW SRM 53-03, FIGURE 5. 2L72 4F A6WE 20040202001902004020200190NM 2004 2 2 CALA0400025 120040114A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND INTERCOSTAL IN E&E COMPARTMENT CORRODED AT STA 227.8, BL 0 TO RBL 7. THE CORROSION WAS REMOVED AND THE INTERCOSTAL AND A STIFFENER WERE REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040202001942004020200194NM 2004 2 2 CALA0400029 120040115A5230 BEAM BOEING737 737824 13844BZNM CARGO DOOR TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2712225 28934 INSPECTION FOUND A TEAR IN BEAM AT LIGHTENING HOLE OF FORWARD CARGO DOOR BELOW PULLEY. REPAIRED IAW ECRA 5232-01041. 2L72 4F RTA16WE 20040202002102004020200210SO 2004 2 2 C2XA04TY017 120040116A532014529495003 FLANGE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND WALL FLOOR MOUNT FLANGE AT FRAME 60. MAINTENANCE REMOVED AND REPLACED THE FLOOR MOUNT FLANGE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040202002122004020200212SO 2004 2 2 C2XA04SH020 120040115A21508152403 ACM EMB 145 EMB145LR 3260212SO NR 1 SEIZED A C2XAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27229099878 3198 145459 SHV- PACK 1 SMOKE IN COCKPIT IN FLIGHT, PACK 1 SIEZED UP. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR CYCLE MACHINE IAW EMB 145 AMM 21-51-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202002282004020200228CE 2004 2 2 DXTA200400220 120040118A3260 WARNING LIGHT CESSNA560 560XL 2076702CE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07664QS 5605264 LANDING GEAR UNLOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR ONCE WITH THE SAME RESULT. JACK UP AIRCRAFT INSPECTED UPLOCK ACTUATORS, SWITCHES AND CONNECTOR, ALSO INSPECTED NOSE GEAR STRUT FOR PROPER INFLATION. PERFORMED GEAR RETRACTION IAW CESSNA 560XL MM CHAPTER 32-30-00 SEVERAL TIMES WITH NO DEFECTS, OPERATIONAL CHECKS SATISFACTORY. 2L72 4F RTA22CE 20040202002292004020200229NM 2004 2 2 04FDEA00181 120040116A5320FXSRM53105 FLOOR SUPPORT BOEING727 727100 1384036NM CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 AFT LOWER PIT BS 970 TO 990 BETWEEN STR 29 AND LT KEEL BEAM CRACKED FLOOR SUPPORT AND CORRODED NUT PLATES. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-5 AT MAE ON N/R NOO419. 2L73 4F RTA3WE 20040202002302004020200230NM 2004 2 2 04FDEA00182 120040116A5347FXB275305145 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 MAIN CABIN SEAT TRACK AT APPROX RBL 24 FS 1140 TO 1183 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2 AT MAE ON N/R N00448. 2L73 4F RTA3WE 20040202002312004020200231NM 2004 2 2 04FDEA00183 120040116A5310FX65425107 WEB BOEING727 727100 1384036NM MAIN CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 UPPER DECK, CARGO DOOR UPPER BOX WEB FINGERS ARE CRACKED AT STA 490 AND 500 STR 2L. REMOVED DAMAGED WEB AND INSTALLED NEW WEB IAW SRM 51-30-2. 2L73 4F RTA3WE 20040202002322004020200232NM 2004 2 2 04FDEA00184 120040116A5320FX65234084 SUPPORT ANGLE BOEING727 727100 1384036NM LWR NOSE BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 LOWER NOSE COMPT DOOR CUTOUT SUPPORT ANGLE IS CRACKED AT FS 203 RBL 11. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-30-2 AT MAE ON N/R N00687. 2L73 4F RTA3WE 20040202002382004020200238 2004 2 2 U30A200400001 420040117A2210C13042AA01 COMPUTER AIRBUS320 A320214 3930316EU ZONE 128 FAULTY A U30AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA17261AV 1615 PRIOR TO DEPARTURE OF FLT 308 IN BWI (BWI-CUN), THE NR 2 FMGC (FLIGHT MANAGEMENT GUIDANCE COMPUTER) WENT INOP (ECAM MESSAGE AP2 & CAT 3 DUAL INOP). THE NR 2 FMGC WAS DEFERRED PER MEL 22-83-01. THE NR 2 FMGC WAS REPLACED IAW AMM 22-83-34-401 AND OPS CK'D OK 2 LEGS LATER WHEN THE AIRCRAFT RETURNED TO BWI. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA28NM 20040202002402004020200240WP 2004 2 2 ABXA040030 120040115A24322634006106 CHARGER DOUG DC9 DC931 3022065WP MASTER DEFECTIVE A ABXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23942AX3579 47552 IN FLIGHT, BATTERY CHARGER WAS CHARGING BATTERY CONTINUALLY AT 20 AMPS, THE BATTERY WAS AT 38 TO 39 VOLTS. REMOVED AND REPLACED BOTH MAIN BATTERIES, BATTERY CHARGER, AND BATTERY SENSOR IAW DC-9 AMM 24-30-01-4-0001 AND 24-30-02-2-001. OPS CHECKED GOOD. 2L72 4F A6WE 20040202002482004020200248NM 2004 2 2 DHL2004745004 120040117A5753 SKIN BOEING727 727224 1384076NM TE FLAP CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 LT INBOARD MID FLAP UPPER T/E NUMEROUS AREAS OF SURFACE CORROSION. REMOVED CORROSION AND PRIMED IAW B727 SRM 51-10-2. 2L73 4F A3WE 20040202002492004020200249NM 2004 2 2 QXEA200400040 120040113A5753 FITTING BOMBDRDHC8 DHC8401 1390041NM LT TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - LEFT FLAP SPAR FITTING AND FLAP TRACK FRONT FITTING AT ATTACHMENT TO SPAR REQUIRES REWORK. MAINTENANCE REPAIRED FITTINGS IAW EO 6-27-147 AND RD 8/4-57-226. 2H72 4T RTA13NM 20040202002502004020200250NM 2004 2 2 DHL2004745005 120040117A5753 SKIN BOEING727 727224 1384076NM LT TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 LT OUTBOARD T/E FLAP LARGE DELAM APPROX MID SPAN. REMOVED AND REPLACED OUTBOARD T/E FLAP IAW M/M 27-51-11. OPS CHECKED GOOD AT THIS TIME. 2L73 4F A3WE 20040202002522004020200252NM 2004 2 2 DHL2004745007 120040117A5720 BRACKET BOEING727 727224 1384076NM WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 COVE PANEL BELOW BELOW NR 2 SPOILER BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040202002552004020200255NM 2004 2 2 AALA20040076 120040118A3350 LIGHT BOEING757 757231 1384950NM SEAT ROW 2 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21723TW 29378 DFW EMERGENCY FLOOR TRACK LIGHTING AT SEAT ROWS 2 AND 3 INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHTING SEGMENT BETWEEN ROW 2 AND 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040202002572004020200257NM 2004 2 2 AALA20040077 120040118A33500201922001 LIGHT BOEING767 767323 1385205NM SEAT 35HJ INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21384AA 26996 SFO EMERGENCY LIGHT AT SEAT 35HJ INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040202002652004020200265NM 2004 2 2 CALA0400036 120040116A5712 RIB BOEING737 737724 13844BYNM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2739726 28796 INSPECTION FOUND THE AFT CENTER SUPPORT RIB FOR THE UPPER WING T/E PANEL JUST O/B OF THE I/B GROUND SPOILER CRACKED ON THE RIGHT AND LEFT WING. THE CRACKS WERE .5 INCH LONG. THE RIBS WERE REMOVED AND NEW RIBS WERE INSTALLED IAW SRM 51-20-01, 51-40-02 AND DRAWING 115A2930. 2L72 4F RTA16WE 20040202002672004020200267NM 2004 2 2 CALA0400038 120040117A5310 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714334 23572 INSPECTION FOUND SHEAR TIE CORRODED AT STA 927 BETWEEN S27L AND S27R IN AFT CARGO AREA. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 53-00-07, FIGURE 210. 2L72 4F RTA16WE 20040202002692004020200269NM 2004 2 2 CALA0400040 120040117A5730 SKIN BOEING757 757224 1384958NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712125 28967 INSPECTION FOUND A 9 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 450.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20040202002712004020200271NM 2004 2 2 CALA0400042 120040118A5320 SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND UPPER AND LOWER SURFACES OF MAIN CABIN FLOOR LAV WALL SUPPORT CORRODED AT STA 993 FROM RBL 16 TO RBL 46. THE SUPPORT WAS REMOVED AND A NEW SUPPORT CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040202002722004020200272NM 2004 2 2 CALA0400043 120040118A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER AND LOWER SURFACES CORRODED AROUND SCREW HOLES AT STA 986.5, RBL 0 TO RBL 50. THE CORRODED SECTION OF FLOORBEAM UPPER CHORD WAS REMOVED AND A NEW REPAIR CHORD WAS INSTALLED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20040202002732004020200273NM 2004 2 2 CALA0400044 120040119A5347 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND MAIN CABIN FLOOR RIGHT I/B AND O/B SEAT TRACKS CORRODED AT STA 917-927. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204. 2L72 4F RTA16WE 20040202002742004020200274CE 2004 2 2 57947 120040115A3240 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07146ZV UE146 BRAKES MUSHY ON CAPT'S SIDE WHEN THE PARKING BRAKE WAS SET. BLEED THE BRAKES. 2L72 4T RTA24CE 20040202002752004020200275NM 2004 2 2 04FDEA00180 120040116A533065C139132 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 SKIN PILLOWING STA 1040 - 1060 STR 28L. REPAIRED SKIN AT BS 1010 TO 1100 STR 26R TO 26L PER FED EX EA 7-5330-55202 AND SRM 53-30-3 FIG 12. 2L73 4F RTA3WE 20040202002842004020200284 2004 2 2 DXTA200400219 420040118A3414 INDICATOR CESSNA560 560XL 2076702CE AIRSPEED MALFUNCTIONED E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07603QS 5605203 ON TAKEOFF ROLL AT 70 KNOTS, F/O'S AIRSPEED INDICATOR FAILED TO DISPLAY. VISUALLY INSPECTED PITOT TUBES AND STATIC PORTS FOR MOISTURE, DEBRIS, OR ANY BLOCKAGE, NONE FOUND. COMPLETED AIRSPEED CALIBRATION TESTS OF BOTH AIR DATA COMPUTERS AND THE SECONDARY FLIGHT DISPLAY, ALL RESULTS WITHIN SPECIFIED TOLERANCES. ALL WORK COMPLETED IAW CESSNA CITATION 560XL MAINTENANCE MANUAL CHAPTER 34-11-08. 2L72 4F RTA22CE 20040202002852004020200285NM 2004 2 2 AT0400002 120040115A2821M259881160 SEAL BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FUEL FILTER BOWLLEAKING A ZZDAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO15927AT 55077 TOWER ADVISED FLUID COMING OUT OF LT ENGINE DURING CLIMBOUT. TOP OF CLIMB, BALANCED FUEL TANKS, IN 15 MINUTES, LEFT TANK WAS 800 POUNDS LOW. OPENED NR 1 ENGINE COWL AND FOUND FUEL FILTER BOWL SEAL LEAKING. REMOVED AND REPLACED FUEL FILTER AND SEAL IAW B717 AMM 73-11-01. LEAK CHECK GOOD IAW B717 71-00-11. 2L72 4F4 FTRA6WE E00061EN 20040202002912004020200291EA 2004 2 2 COMA0460067 120040117A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01484CA5902 7702 FLIGHT 5235 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040202003342004020200334SO 2004 2 2 C2XA04SH023 120040121A531514524280002 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV- DURING C-CHECK THE ATTACHMENT ANGLE BETWEEN THE RIGHT SILL AND THE CROSS BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ATTACHMENT ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040202003382004020200338NM 2004 2 2 2004UALA00023 120040109A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29122UA 29168 EMERGENCY EXIT LIGHTING ON AT SEATS 22-26 GHJ ZONE B. REMOVED, CHARGED & REINSTALLED BATTERY PACK, OP CHECKS OK. 2L74 4F4 FRTA20WE E24NE 20040202003422004020200342NM 2004 2 2 2004UALA00029 120040112A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 DENT ON LEFT SIDE OF FUSELAGE, MEASURES .125 INCH DEEP BY 3 INCH WIDE, LOCATED AT BS 610 BETWEEN STR 15L-16L JUST BELOW WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040203001032004020300103NM 2004 2 3 UPS04441755 120040105A53307075T60080IN SKIN BOEING747 747123F NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C - AFT FUSELAGE SKIN AT BS 2365 - 2385 LT STR 3. THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20040203001332004020300133EA 2004 2 3 MASA200400025 120040111A3040165911 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDSHIELD INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07172751691 7275 ASH 6158 PHX, RETURNED TO FIELD FOR LEFT WINDOW HEAT CAUTION MSG IN FLT. WEATHER AT DESTINATION WAS CALLING FOR ICE. MX REPLACED THE WINDSHIELD TEMP CONTROLLER. OP CHECKS GOOD. 2L72 4F RTA21EA 20040203001422004020300142NM 2004 2 3 QXEA200400048 120040117A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - NR 7 SEAT TRACK LEFT HAND FLOOR SUPPORT FLANGE HOLE IS CORRODED, 4 INCHES AFT OF X222. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-30-26. 2H72 4T RTA13NM 20040203001542004020300154NM 2004 2 3 MWEA0400010 120040122A53205912528503 PAN BOEING717 717200 1383700NM AFT CARGO DOOR BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31908ME 55172 AFT CARGO DOOR JAMB PAN IS BENT ON LOWER PORTION OF JAMB, JUST AFT OF CONTROL DOOR STOP FITTING. SPLICE IN NEW SECTION OF PAN. 2L72 4F TRA6WE 20040203001722004020300172EU 2004 2 3 AALA20040102 120040121A2913 PUMP AIRBUS300 A300B4605R 3930308EU YELLOW HYD SYS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2114056 463 JFK INFLIGHT T0635/21, YELLOW SYSTEM HYDRAULIC WENT TO 50 PSI SHORTLY AFTER TAKEOFF WITH ECAM MESSAGE. SYSTEM WENT TO 3300 PSI AFTER PTU PRESSED ON. RETURNED TO JFK. LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE YELLOW SYSTEM PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040203001792004020300179NM 2004 2 3 SWAA040183 120040120A57556544851 ACTUATOR BOEING737 7375H4 138449DNM RT WING SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 OUTBOARD SPOILER ACTUATOR END BROKEN. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20040203001852004020300185NM 2004 2 3 SWAA040189 120040120A53206545805 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUT OUT LOWER FORWARD STOP FITTING WEB DOUBLER CRACKED. REMOVED AND REPLACED PER SRM. 2L72 4F RTA16WE 20040203001942004020300194NM 2004 2 3 SWAA040198 120040120A551265C25727 SKIN BOEING737 7375H4 138449DNM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT AFT SPAR ATTACHMENT POINT, STATION 90. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203001962004020300196NM 2004 2 3 SWAA040200 120040120A33507003667 BALLAST BOEING737 7377H4 1384404NM EMERGNECY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20040203001982004020300198NM 2004 2 3 SWAA040085 120040109A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040203001992004020300199NM 2004 2 3 SWAA040086 120040109A2560P2070001 FLASHLIGHT BOEING737 7373A4 1384585NM AFT CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 AFT CABIN EMERGENCY FLASLIGHT INOP. REMOVED AND REPLACED AFT CABIN FLASHLIGHT AND HOLDER PER MM. 2L72 4F RTA16WE 20040203002002004020300200NM 2004 2 3 SWAA040087 120040109A3350101114 SIGN BOEING737 7375H4 138449DNM LT OVERWING LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 LT OVERWING EXIT SIGN COVER LOOSE. SECURED OVERWING EXIT SIGN PER MM. 2L72 4F RTA16WE 20040203002022004020300202NM 2004 2 3 SWAA040089 120040109A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 440 + 6, STRINGER 16R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002032004020300203NM 2004 2 3 SWAA040090 120040109A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10R AT BS 500B, CRACKED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040203002082004020300208 2004 2 3 SWAA040095 420040109A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002122004020300212NM 2004 2 3 SWAA040099 120040109A3350 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 21 AND ROW 1. REMOVED AND REPLACED EEPLS TRACK COVER PER MM. 2L72 4F RTA16WE 20040203002172004020300217NM 2004 2 3 SWAA040075 120040108A3350300432 LIGHT BOEING737 7373L9 1384470NM R2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SPV, FOUND R2 DOOR EMERGENCY EXTERIOR EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040203002192004020300219NM 2004 2 3 SWAA040077 120040108A2560P4010021 BATTERY BOEING737 7372T4 1384492NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F A16WE 20040203002202004020300220NM 2004 2 3 SWAA040078 120040108A3350101114 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8. INSTALLED NEW LENS PER MM. 2L72 4F RTA16WE 20040203002212004020300221NM 2004 2 3 SWAA040079 120040108A33501619 LAMP BOEING737 7372H4 138448CNM R1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PMC, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED PER MM. 2L72 4F A16WE 20040203002232004020300223NM 2004 2 3 SWAA040081 120040108A3350OL3071BPL5GPL LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED PMC, FOUND SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED OVERHEAD LIGHTS PER MM. 2L72 4F A16WE 20040203002252004020300225NM 2004 2 3 SWAA040083 120040108A53306545700 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKS AT BS 520, STRINGER 10R AND BS 747, STRINGER 23R. REPAIRED SKIN CRACKS PER SRM. 2L72 4F RTA16WE 20040203002262004020300226NM 2004 2 3 SWAA040059 120040107A291095850V0 LINE BOEING737 7377H4 1384404NM HYD SYSTEM FAILED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW29790SW 30604 DIVERSION, DECLARED EMERGENCY, ON APPROACH UNABLE TO LOWER FLAPS IN NORMAL. LOWERED FLAPS IN ALT, UNABLE TO LAND IN MDW AT 15. DIVERTED TO IND, CAUSED BY LOSS OF B SYSTEM HYD. FOUND HYD PUMP PRESS LINE BLOWN. REMOVED AND REPLACED HYD LINE PER MM. 2L72 4F RTA16WE 20040203002292004020300229 2004 2 3 SWAA040062 420040107A2565 BOTTLE BOEING737 7373H4 1384600NM ESCAPE SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 L2 DOOR EVACUATION SLIDE PRESS GAUGE IN THE RED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002302004020300230NM 2004 2 3 SWAA040063 120040107A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040203002322004020300232NM 2004 2 3 SWAA040065 120040107A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM CHORD CORRODED AT BS 340 TO BS 357. REPAIRED CREASE BEAM CHORD PER SRM. 2L72 4F RTA16WE 20040203002342004020300234NM 2004 2 3 SWAA040067 120040107A53306545768 BUTTSTRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND BUTTSTRAPS CRACKED AT BS 360 STRINGER 14L, BS 908, BETWEEN STRINGERS 15L AND 16L. REPAIRED STRAPS PER SRM. 2L72 4F RTA16WE 20040203002352004020300235NM 2004 2 3 SWAA040068 120040107A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 1000, RBL 62.50. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040203002382004020300238NM 2004 2 3 SWAA040071 120040107A53306545700 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED SPV, FOUND SKIN CRACKED AT BS 432, STRINGER 16L, BS 777, STRINGER 18L, BS 933, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040203002412004020300241NM 2004 2 3 SWAA040074 120040107A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, FROM LT TO RT TRANS ANGLES. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040203002432004020300243NM 2004 2 3 SWAA040130 120040113A3260806007 CIRCUIT CARD BOEING737 7373H4 1384600NM ELECTRONICS BAY FAULTY A SWAAO OTHER N FALSE WARNING CLCLIMB 1 SW29366SW 26577 AFTER TAKEOFF WITH GEAR HANDLE IN THE UP POSITION LEFT MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED AFTER A MINUTE REMAINED EXTINGUISHED AFTER GEAR HANDLE PLACED TO OFF. REMOVED AND REPLACED M 987 PC CARD. 2L72 4F RTA16WE 20040203002442004020300244 2004 2 3 SWAA040131 420040113A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002462004020300246NM 2004 2 3 SWAA040133 120040113A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BUTT STRAP CRACKED AT BS 360, STRINGER 10L. REPAIRED BUTT STRAP PER SRM. 2L72 4F RTA16WE 20040203002492004020300249NM 2004 2 3 SWAA040136 120040113A575465C26602 WEDGE BOEING737 7373TO 138447GNM NR 2 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED SLAT WEDGE PER SA-M 604. 2L72 4F RTA16WE 20040203002502004020300250NM 2004 2 3 SWAA040137 120040113A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 823, STRINGER 23L. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002522004020300252NM 2004 2 3 SWAA040139 120040113A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040203002552004020300255NM 2004 2 3 SWAA040106 120040110A53106546550 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BL 0. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040203002562004020300256NM 2004 2 3 SWAA040107 120040110A57306950711 SKIN BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C1 CHECK, FOUND RT WING FIXED L/E SKIN CRACKED AT WING STATION 213. REPAIRED WING SKIN CRACK PER EA. 2L72 4F RTA16WE 20040203002572004020300257NM 2004 2 3 SWAA040108 120040110A335020131A LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 7 INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040203002592004020300259NM 2004 2 3 SWAA040110 120040110A53106547951 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR FRAME UPPER AND LOWER HINGE CUTOUT CRACKED. REPAIRED L2 DOOR CUTOUT PER EA. 2L72 4F RTA16WE 20040203002602004020300260NM 2004 2 3 SWAA040111 120040110A33506104789 BATTERY PACK BOEING737 7373G7 1384595NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED SC, FOUND L1 AND R1 DOOR EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EXIT LIGHTS BATTERY PACK PER MM. 2L72 4F RTA16WE 20040203002612004020300261NM 2004 2 3 SWAA040112 120040111A3350D717020001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 DURING SCHEDULED MC, FOUND EMRGENCY EXIT LIGHTS INOP FROM ROW 6 TO ROW 10. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY. 2L72 4F RTA16WE 20040203002662004020300266NM 2004 2 3 SWAA040117 120040111A326080602 CIRCUIT CARD BOEING737 7373H4 1384600NM ELECTRONICS BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29366SW 26577 AIR TURN BACK, DECLARED EMERGENCY, AFTER TAKEOFF AND AFTER RAISING THE GEAR HANDLE, THE HANDLE IN THE OFF POSITION, THE LT GEAR GREEN LIGHT AND THE LT GEAR RED LIGHT BOTH ILLUMINATED. REMOVED AND REPLACED THE LT GEAR UP AND LOCK SWITCH PC CARD PER MM. 2L72 4F RTA16WE 20040203002702004020300270NM 2004 2 3 SWAA040121 120040112A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 294, RBL 55 AND BS 303, WL 216. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20040203002712004020300271NM 2004 2 3 SWAA040122 120040112A3397300432 WIRE BOEING737 7373H4 1384600NM EMERGENCY SIGN CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT WIRES CHAFFING. REMOVED AND REPLACED WIRE PER WDM AND MM. 2L72 4F RTA16WE 20040203002722004020300272NM 2004 2 3 SWAA040123 120040112A53106546540 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 380 TO BS 400 LT, WL 208 AND BS 500 TO 500A LT, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040203002752004020300275NM 2004 2 3 SWAA040126 120040112A53306545774 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 737, STRINGER 19R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002762004020300276 2004 2 3 SWAA040127 420040112A2565D31354 SLIDE BOEING737 7373TO 138447GNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002812004020300281NM 2004 2 3 SWAA040143 120040114A53126582671 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE DECK CRACKED AT BS 663, LBL 30. REPAIRED PRESSURE DECK PER SRM. 2L72 4F RTA16WE 20040203002822004020300282NM 2004 2 3 SWAA040144 120040114A53126546560 SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT BULKHEAD CENTER LOWER SUPPORT CHORD CORRODED AT BS 948. REPAIRED PER SRM. 2L72 4F RTA16WE 20040203002852004020300285NM 2004 2 3 SWAA040147 120040115A57536546481 SPINDLE BOEING737 7373H4 1384600NM TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED PM CHECK, FOUND LT WING NR 1 T/E FLAP SPINDLE WITH A CRACK INDICATION. REMOVED AND REPLACED NR 1 FLAP SPINDLE PER MM. 2L72 4F RTA16WE 20040203002862004020300286NM 2004 2 3 SWAA040148 120040114A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED BETWEEN BS 500C TO BS 500D, ABOVE STRINGER 10L. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002892004020300289NM 2004 2 3 SWAA040151 120040115A57536571909 SKIN BOEING737 7373H4 1384600NM TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND LT WING OUTBOARD T/E MIDFLAP L/E SKIN CRACKED AT WBL 205. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040203002902004020300290NM 2004 2 3 SWAA040152 120040115A53106547951 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME WEB CRACKED AT BS 787 + 6. REPAIRED PER SRM. 2L72 4F RTA16WE 20040203002952004020300295NM 2004 2 3 SWAA040157 120040117A5320BAC1514 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND RADIAL STIFFENER CORRODED AT BS 1016, BL 0. REPAIRED RADIAL STIFFENER PER ACO. 2L72 4F RTA16WE 20040203002972004020300297NM 2004 2 3 SWAA040159 120040116A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 1 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29748SW 29800 EEPLS FLOOR TRACK LIGHTING LOOSE AT ROW 1. SECURED TRACK PER MM. 2L72 4F RTA16WE 20040203002982004020300298 2004 2 3 SWAA040160 420040116A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 R1 DOOR EVAC SLIDE PRESSURE IND LOW. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203003012004020300301 2004 2 3 SWAA040163 420040116A25656556685 BRACKET BOEING737 7373H4 1384600NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2L72 4F RTA16WE 20040203003072004020300307NM 2004 2 3 SWAA040169 120040117A33507003667 BALLAST BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20040203003082004020300308 2004 2 3 SWAA040170 420040117A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203003092004020300309NM 2004 2 3 SWAA040171 120040117A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY SIGN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040203003112004020300311NM 2004 2 3 SWAA040173 120040117A57536546430 SKIN BOEING737 7373Q8 1384670NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C4 CHECK, FOUND RT WING, RT INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040203003122004020300312 2004 2 3 SWAA040174 420040117A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203003152004020300315NM 2004 2 3 SWAA040177 120040118A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040203003172004020300317 2004 2 3 SWAA040179 420040119A2565 INDICATOR BOEING737 7373H4 1384600NM SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203003182004020300318 2004 2 3 SWAA040180 420040117A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203003192004020300319NM 2004 2 3 SWAA040181 120040119A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT BAGGAGE BIN FLOORBEAMS CORRODED AT BS 770, LBL 8, BS 857, RBL 8 TO RBL 3, BS 857, LBL 12. REPAIRED AFT BAGGAGE BIN FLOORBEAMS PER EA. 2L72 4F RTA16WE 20040203003202004020300320NM 2004 2 3 SWAA040182 120040119A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 5L, BS 360, STRINGER 3L AND BS 344, STRINGER 11R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040203003392004020300339NE 2004 2 3 MASA200400015 220040108A7320 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE OUT OF ADJUST A MASAE ENGINE SHUTDOWN P NO WARNING INDICATION DEDESCENT 1 SW0775992 7401 872722 ASH 2670 PHL-STL, NR 1 ENGINE SHUT DOWN ON DESCENT WHEN THROTTLES SELECTED TO IDLE. CREW FOLLOWED CHECK LIST AND RESTARTED ENGINE. ENGINE PERFORMED PROPERLY THE REST OF THE DESCENT. MX PERFORMED ENGINE RUN AND FUEL CONTROL ADJUSTMENTS PER FIM. A/C CONTINUED WITHOUT INCIDENT. NO PARTS USED. 2L72 4F4 FRTA21EA E15NE 20040203003412004020300341NM 2004 2 3 CALA0400052 120040123A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711656 28917 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED FROM STA 270-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040203003422004020300342NM 2004 2 3 QXEA200400056 120040122A2611824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY FALSE INDICATIONA QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09352PH14905 494 PDX - THE LAVATORY SMOKE DETECTOR SOUNDED SHORTLY AFTER TAKEOFF. THE LAVATORY AND LAVATORY WASTE WAS CHECKED FOR EVIDENCE OF SMOKE AND BURNING ODOR. NONE WAS NOTED. THE LAVATORY DETECTOR WAS RESET AND THE OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203003432004020300343NM 2004 2 3 QXEA200400057 120040122A2611824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY DEFECTIVE A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09352PH14905 494 SEA - FLIGHT 2208 - THE LAV SMOKE DETECTOR SOUNDED AGAIN AFTER TAKEOFF FROM PDX. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LAVATORY SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203003462004020300346 2004 2 3 SWAA040202 420040121A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29413WN 29819 R2 DOOR EVAC SLIDE INADVERTENT SLIDE DEPLOYMENT. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040202003182004020200318WP 2004 2 2 AALA20040080 120040119A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21980TW 53630 DFW FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040202003202004020200320WP 2004 2 2 AALA20040081 120040119A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21588AA 53251 STL RIGHT AND LEFT EMERGENCY LIGHT AT FORWARD OVERWING EXIT INOPERATIVE. SECURED LOOSE WIRE TERMINAL ON FORWARD OVERWING EMERGENCY LIGHT POWER SUPPLY AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040202003402004020200340NM 2004 2 2 2004UALA00025 120040111A5320 SILL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 CORROSION FOUND ALONG AFT PIT LOWER DOOR SILL, ADJACENT STRINGER 26R, BS 1380-1440. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW STRAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20040202003532004020200353WP 2004 2 2 ARWA20040104 120040113A5314 KEELBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 DURING A C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W STATION 920, KEELBEAM LT TEE EXTRUSION WITH 3 INCH CRACK. REPAIRED KEEL WEB STIFFENER AT STA 920 IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02 MARCH 04, DC8 SRM 51-2-1, TR 51-130. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. ALSO N/R 1437; REPAIRED FUSELAGE KEEL LOWER TEE CAPS IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02-MAR-04, DRWAING NUMBER 5754125 & ROD SKETCH 04-02-19-001. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. PERFORMED CLOSE VISUAL INSPECTION FOR CRACK PROPAGATION AT "C" CHECK INTERVALS. 2L74 4F 4A25 20040203000932004020300093NM 2004 2 3 EIA2004006 120040115A3310 TRANSFORMER BOEING747 747212B 1384886NM COCKPIT LIGHTS OVERHEATED A EIAAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09486EV 20888 STRONG ELECTRICAL ODOR IN COCKPIT PANEL LIGHT. C/B PULLED FUMES DISSIPATED. TRANSFERRED TO DMI 475. REPLACED RIGHT EIDS DISPLAY DUE IT WAS REPORTED FLASHING ON T/O. REPLACED AVIONICS ADAPTER RACK AND REPLACED DIMMEN TRANSFORMER DUE TO SIGNS OF OVERHEAT. OPERATED P9 AND P2 LIGHTING FOR MORE THAN TWO HOURS WITH NO SIGN OF SMOKE. P9 AND P2 LIGHTING OPS CHECK IAW MM 33-11-00. 2L74 4F A20WE 20040203000962004020300096NM 2004 2 3 CALA0400045 120040119A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED BETWEEN STA 277 AND 380 AT RBL 54. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040203001022004020300102NM 2004 2 3 UPS04441754 120040105A5330 SKIN BOEING747 747123F NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:C EMP - AFT FUSELAGE SKIN AT BS 2340 - 2355 LT STR 3. THE DEPTH OF WEAR IN FUSELAGE SKIN HAS EXCEEDED EO B747-5330-18431 LIMIT AFT BLEND OUT. DEFECTIVE AREA SKIN REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1. 2L74 4F A20WE 20040203001152004020300115EU 2004 2 3 MTNA20041 120040121A3010227D504413 BOOT FOKKERF27 F27MK500 4990629EU ZONE 300 DETACHED A MTNAA UNSCHED LANDING DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 SO33725FE 10658 AFTER TAKEOFF FROM MEM A VIBRATION WAS DETECTED AND THE AIRCRAFT RETURNED TO MEM. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT OUTBOARD HORIZONTAL STABILIZER DEICE BOOT HAD SEPARATED FROM THE LEADING EDGE ON TOP FOR ABOUT A 5 FOOT SECTION. 2H72 4T A817 20040203001162004020300116NM 2004 2 3 QXEA20040050 120040120A33501014011 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER L NO TEST NRNOT REPORTED 1 NM09353PH 496 PDX- LEFT HAND AFT EMERGENCY EXIT LIGHT BRIGHTNESS LEVEL IS LOWER THAN 100 MICRO LAMBERTS. REMOVED AND REPLACED BETA LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203001212004020300121WP 2004 2 3 AALA20040090 120040120A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21286AA 49298 DFW OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203001222004020300122WP 2004 2 3 AALA20040089 120040120A3350 LIGHT DOUG DC9 DC982 3022082WP ROWS 3-20 MISINSTALLED A AALAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 SW21492AA 49730 DFW SEAT MOUNTED EMERGENCY LIGHT AT ROWS 3 THROUGH 20 INOPERATIVE. FOUND CONNECTION AT ROW 20 MOUNTED BACKWARDS. REMOUNTED CONNECTION FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203001322004020300132EA 2004 2 3 MASA200400024 120040111A361020035008067 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA RT ENG BLEED SYSINOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07873532668 7353 ASH 6412 PHX. RETURNED TO FIELD. RT ENGINE 14TH STAGE BLEED DUCT WARNING MSG. A/C RETURNED TO FIELD. MX REPLACED THE BLEED LEAK CONTROL UNIT. OP CHECKS GOOD. 2L72 4F RTA21EA 20040203001342004020300134EA 2004 2 3 MASA200400026 120040111A361014403103 DUCT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE SEPARATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW078735311149 7353 ASH 6443 PHX, AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE DUE TO A 14TH STAGE BLEED WARNING AND TAKEOFF CONFIG WARNING. MX FOUND DUCT BLOWN OFF AND RIGHT PYLON LOOP BAD. MX REPLACED DUCTING AND LOOP. OP CHECKS GOOD. 2L72 4F RTA21EA 20040203001392004020300139NM 2004 2 3 QXEA200400045 120040119A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - FUSELAGE SKIN AT TCAS ANTENNA MOUNT HAS CORROSION/PITTING AT STATION X501 AND Z35. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040203001482004020300148EA 2004 2 3 COMA0460068 120040120A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01436CA 7482 FLIGHT 5360 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE. SECURED AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040203001582004020300158NM 2004 2 3 CALA0400047 120040120A5314 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 INSPECTION FOUND LEFT AND RIGHT LOWER KEEL BEAM WITH ELONGATED HOLES AT STA 741. REPLACED KEEL BEAM LOWER CHORDS IAW ECRA 5311-01183. 2L72 4F RTA16WE 20040203001732004020300173NM 2004 2 3 AALA20040092 120040121A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21649AA 24607 MIA OVERHEAD EMERGENCY LIGHT AT 18C INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040203001742004020300174NM 2004 2 3 AALA20040093 120040121A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21649AA 24607 MIA EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHT ON AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040203001752004020300175NM 2004 2 3 AALA20040094 120040120A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21782AN 30003 DFW EMERGENCY LIGHTS AT FORWARD FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FORWRD FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040203001762004020300176NM 2004 2 3 AALA20040095 120040120A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21782AN 30003 DFW EMERGENCY LIGHTS AT AFT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040203001782004020300178NM 2004 2 3 PCAA0401158 120040121A3230DSC1832 RELAY DHAV DHC8 DHC8102 2809003NM MLG FAULTY A PCAAK NONE E VIBRATION/BUFFET CRCRUISE 1 EA13840EX 327 FLIGHT 3962 TO SYRACUSE REPORTED A RYTHMIC THUMPING SOUND EVERY 3-5 SECONDS IN FLIGHT AT VARIOUS PROP RPM SETTINGS. NO THUMPING REPORTED WHEN GEAR AND FLAPS EXTENDED. AIRCRAFT WAS INSPECTED AND FROM SYRACUSE A FERRY PERMIT WAS ISSUED FOR AIRCRAFT TO LOCATE TO MIDDLETOWN MAINTENANCE. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE GEAR CYCLING WHILE IN THE UP POSITION. RELAYS 3261-K13 AND 3261-K11 WERE REPLACED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203001812004020300181NM 2004 2 3 SWAA040185 120040120A335065C27093 LIGHT BOEING737 7372T4 1384492NM L2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040203001892004020300189NM 2004 2 3 SWAA040193 120040120A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520L, STRINGER 12L. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203001902004020300190NM 2004 2 3 SWAA040194 120040120A532165C33970 FLOOR PANEL BOEING737 7373Y0 1384671NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FLOOR WEB CRACKED FROM BS 178 TO BS 188, LBL 27. REPAIRED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040203001932004020300193 2004 2 3 SWAA040197 420040120A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002012004020300201NM 2004 2 3 SWAA040088 120040109A3397 WIRE BOEING737 7372H4 138448CNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29102SW 23108 DURING SCHEDULED PMC, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RECONNECTED LOOSE WIRES ON OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040203002072004020300207NM 2004 2 3 SWAA040094 120040109A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 787, STRINGER 8R AND BS 400, STRINGER 8R. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20040203002132004020300213NM 2004 2 3 SWAA040100 120040110A3350100885 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 DURING SCHEDULED MC, FOUND EEPLS INOP ROW 6 TO ROW 10. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2L72 4F RTA16WE 20040203002142004020300214NM 2004 2 3 SWAA040101 120040110A335090083 BATTERY BOEING737 7372H4 138448CNM EMERGNECY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED PMC, FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040203002152004020300215NM 2004 2 3 SWAA040102 120040110A53306545700 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C1 CHECK, FOUND 4 EACH SKIN CRACKS AT BS 480, STRINGER 16R, BS 270, STRINGER 9C, BS 500D, STRINGER 15L AND BS 578, STRINGER 10R. REPAIRED SKIN CRACKS PER SRM. 2L72 4F RTA16WE 20040203002162004020300216NM 2004 2 3 SWAA040103 120040110A57536546481 SPINDLE BOEING737 7373G7 1384595NM RT WING TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED PMC, FOUND NR 8 T/E FLAP SPINDLE WITH CRACK INDICATION. REMOVED AND REPLACED NR 8 FLAP SPINDLE PER MM. 2L72 4F RTA16WE 20040203002182004020300218NM 2004 2 3 SWAA040076 120040108A3233654491030 ACTUATOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29366SW 26577 AIR TURN BACK, AFTER TAKEOFF AND GEAR RETRACTION, RIGHT MAIN RED AND GREEN LIGHTS REMAINED ILLUMINATED. ON EXTENSION, RED LIGHT WENT OUT. REMOVED AND REPLACED RT GEAR RETRACT ACTUATOR PER MM. 2L72 4F RTA16WE 20040203002272004020300227NM 2004 2 3 SWAA040060 120040107A3350BR2013 LIGHT BOEING737 7372T4 1384492NM ROW 14 BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 CABIN FLOOR EEPLS BROKEN AT ROW 14. REPAIRED EEPLS AT ROW 14 PER MM 2L72 4F A16WE 20040203002392004020300239NM 2004 2 3 SWAA040072 120040107A3350D71701 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29743SW 29279 DURING SCHEDULED 5Y CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040203002402004020300240NM 2004 2 3 SWAA040073 120040107A5210651647 GATE BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING OTS, FOUND UPPER GATE CRACKED ON L1 DOOR. REMOVED AND REPLACED L1 DOOR GATE PER MM. 2L72 4F RTA16WE 20040203002452004020300245NM 2004 2 3 SWAA040132 120040113A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND LT FWD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040203002532004020300253 2004 2 3 SWAA040104 420040110A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002582004020300258NM 2004 2 3 SWAA040109 120040110A3350100031 SIGN BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C1 CHECK, FOUND CEILING OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED OVERWING EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040203002652004020300265NM 2004 2 3 SWAA040116 120040111A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CORRODED AT BS 363, WL 208, LBL 65. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040203002692004020300269NM 2004 2 3 SWAA040120 120040112A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED RON, FOUND SKIN CRACKED AT BS 740, STRINGER 20R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002792004020300279 2004 2 3 SWAA040141 420040114A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040203002802004020300280 2004 2 3 SWAA040142 420040114A256565C19901 CABLE BOEING737 7372H4 138448CNM R2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F A16WE 20040203002832004020300283 2004 2 3 SWAA040145 420040114A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002872004020300287NM 2004 2 3 SWAA040149 120040114A33507024091007 SIGN BOEING737 7377H4 1384404NM AFT GALLEY MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING RON, FOUND AFT GALLEY EMERGENCY EXIT SIGN NEAR L2 DOOR MISSING. REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040203003022004020300302NM 2004 2 3 SWAA040164 120040117A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STRINGER 10R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203003062004020300306NM 2004 2 3 SWAA040168 120040117A5315BAC1505 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 727 + 6, RBL 3 TO RBL 14. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040203003162004020300316NM 2004 2 3 SWAA040178 120040118A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND 2EA STRINGER CLIPS CRACKED AT BS 616, STRINGER 5R AND BS 597, STRINGER 8R. 2L72 4F RTA16WE 20040203003402004020300340NM 2004 2 3 CALA0400051 120040122A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711656 28917 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB BETWEEN STA 348 AND 360, BL 0. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040203003442004020300344NM 2004 2 3 QXEA200400058 120040122A7160 SWITCH DHAV DHC8 DHC8202 2809007NM AIR INTAKE DAMAGED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09368PH 512 RDM FLIGHT 2128, DIVERTED TO PDX DUE TO WEATHER NR 2 BYPASS DOOR SWITCH WILL NOT LATCH IN THE OPEN POSITION. REPLACED BYPASS CONTROL SWITCH IAW HORIZON AIR EO 2-30-04B. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040203003482004020300348NM 2004 2 3 SWAA040204 120040121A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L SPLICE CRACKED AT BS 540. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040203003492004020300349NM 2004 2 3 SWAA040205 120040121A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 11R CRACKED AT BS 828. REPAIRED STRINGER PER ERO. 2L72 4F RTA16WE 20040203003502004020300350NM 2004 2 3 SWAA040206 120040121A531165C22910 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED TO FRAME FROM BS 500D, BELOW STRINGER 10R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040203003542004020300354WP 2004 2 3 DHL2004804001 120040122A2612 FIRE LOOP DOUG DC8 DC873F 302199FWP NR 4 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01804DH 46124 NR 4 SHORT CIRCUIT LIGHT ILLUMINATED. SWITCHED TO LOOP-B. DEFERRED PER MEL 26-2-3 DMI 15475. NR 4 SHORT CIRCUIT LIGHT ILLUMINATED. SWITCHED TO LOOP-B. CHECKED NR 4 ENGINE FIRE LOOP FOR SECURITY, FOUND OK. REPOSITION LOOP FOR BETTER CLEARANCE CHECKED AS PER M/M 26-10-00. OPS OK. THIS CLEARS DMI 15475. 2L74 4F RT4A25 20040203003562004020300356NM 2004 2 3 DHL2004745009 120040122A2612 WARNING LIGHT BOEING727 727224 1384076NM NR 3 DETECTORS FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 FIRE PROTECTION SYSTEM NR 3 DETECTOR CIRCUIT GROUND ON CIRCUIT BREAKER P6-3 PANEL LIGHT ILLUMINATED. PERFORMED FIRE DETECTION TEST IAW B-727 M/M CHAPTER 26-11-001, AND VISUALLY INSPECTED LOOP. NO FAULTS NOTED. OPS CHECKED NORMAL. LIGHT DID NOT ILLUMINATE. 2L73 4F A3WE 20040203003572004020300357NM 2004 2 3 DHL2004763003 120040122A2612 WARNING LIGHT BOEING727 727264 138408MNM CARGO FIRE FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01763AT 22983 DURING TAXI CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. LIGHT EXTINGUISHED. SYSTEM OPS NORMAL ON GROUND AT MSP IAW M/M 26-16. 2L73 4F A3WE 20040203003622004020300362WP 2004 2 3 UPS04841777 120040121A5542 SKIN DOUG DC8 DC871F 302199DWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:C3 RUDDER L/E SKIN IS CRACKED ON LT SIDE AT ZR 289.343. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK. FABRICATED AND INSTALLED DOUBLER AND SHIMS IAW SRM 55-2-1 FIG 5. 2L74 4F RT4A25 20040203003632004020300363EU 2004 2 3 AWXA200400062 120040122A2560P4010021 BATTERY AIRBUS320 A320232 3930326EU ZONE 900 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040203003642004020300364EA 2004 2 3 SWIA200412788 120040113A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER LF NO TEST FLT CONT AFFECTED NRNOT REPORTED 1 NM07925SW 7682 CAPT SIDE ELEVATOR TRIM DOES NOT WORK IN THE UP OR DOWN DIRECTION. REMOVED CAPTAIN'S PITCH TRIM SWITCH AND INSTALLED NEW PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20040203003672004020300367 2004 2 3 SWIA200412791 420040114A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07268UE8829 8829 120207 ON TWO OCCASIONS THE YAW DAMPNER CAPTAIN'S SIDE DISENGAGED, HOWEVER THE AUTO PILOT REMAINS ON EVEN AFTER LANDING THEN TURNING OFF THE AUTO PILOT, YAW DISENGAGED REMAINS ILLUMINATED. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKS GOOD PER MM 22-11-00. 2L72 4T RTA31SO 20040203003682004020300368EA 2004 2 3 SWIA200412792 120040119A2740 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07916SW 7634 STAB TRIM CH1 INOP STATUS MESSAGE ON TAXI WOULD NOT RE-ENGAGE. REPLACED STAB TRIM CONTROL PANEL WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 601R51706-3. 2L72 4F RTA21EA 20040203003692004020300369EA 2004 2 3 SWIA200412793 120040119A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07438SW 7574 DURING TAXI OUT SPOILERON FAULT STATUS MSG CONTACTED. RETURNED TO GATE. REMOVED AND REPLACED NR 1 SECU. OPS CHECK GOOD. 2L72 4F RTA21EA 20040203003752004020300375WP 2004 2 3 AALA20040105 120040122A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217528A 49920 DEN EMERGENCY CEILING LIGHTS BETWEEN STATION 1152 AND STATION 1209 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT B5-107 STATION 1190. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203003762004020300376EU 2004 2 3 AALA20040109 120040121A3220 FITTING AIRBUS300 A300B4605R 3930308EU NLG DAMAGED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2119059 469 BOS INFLIGHT T1367/21 ON TAKEOFF WHEN GEAR HANDLE WAS RAISED A LOUD THUMP WAS HEARD IN THE NOSE GEAR AREA. NOSE GEAR WOULD NOT RETRACT. NOSE GEAR AMBER UNLOCK LIGHT REMAINED ON AND ASSOCIATED ECAM MESSAGE LANDING GEAR RETRACTION INOPERATIVE. RETURNED TO BOSTON. LANDED WITHOUT INCIDENT. INSPECTED AND APPROVED FOR FERRY FLIGHT TO JFK. FOUND NOSE GEAR UPLOCK ATTACH FITTING DAMAGED. REPLACED UPLOCK ATTACH FITTING AND UPLOCK ASSEMBLY FOR NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040203003772004020300377NM 2004 2 3 AALA20040107 120040121A3350 LIGHT BOEING777 777223 1385213NM CABIN DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21757AN 32636 DFW EMERGENCY LIGHT PATH LENS AND ASSEMBLY DAMAGED AT SEAT 32C. REPLACED LENS AND SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT PATH AT SEAT 32C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040203003802004020300380NM 2004 2 3 F3LA200300194 120040122A5320 SILL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03304FL 3318 27633 DURING C-7 CHECK, INSPECTION REPORTED L-2 DOOR FRAME MOP SILL CORRODED BETWEEN STA 947.5 AND STA 1006, STR 17L. REPLACED MOP SILL PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20040203003812004020300381SO 2004 2 3 C2XA04025 120040124A532014529495003 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714998 145302 SHV- DURING C-CHECK, THE LT LAVATORY FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040203003822004020300382SO 2004 2 3 C2XA04SH026 120040124A532014522460015 STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV-DURING C-CHECK, THE AFT DIGITAL STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040203003842004020300384SO 2004 2 3 C2XA04SH028 120040125A532014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV- DURING C-CHECK, THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040203003852004020300385SO 2004 2 3 C2XA04TY020 120040123A532014525422005 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FRAME 71. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB SRM 51-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040203003902004020300390NM 2004 2 3 P9RA20040006 120040123A3350 LAMP BOEING727 7272J0 138407ENM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11910PG 22606 DURING LINE CHECK, FOUND CENTER AISLE EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT IAW BMM 33-50-11. 2L73 4F RTA3WE 20040203003912004020300391EU 2004 2 3 DHL2004365500 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH SEAT TRACK BETWEEN FR37 & 38 APPROX RBL 18 TOOL MARKING IN TWO PLACES. REWORKED DAMAGE AREAS AT SEAT TRACK BETWEEN FR 37 & 38 APPROX RBL 18. FOUND OUT OF LIMITS AS PER A300 SRM 53-10-00. CUT OUT DAMAGED SECTION OF SEAT TRACK ON FR37 TO 38 APPROX RBL 18 IAW A300 SRM 53-10-10 FIG 724, SIZE OF CUTOUT 42 INCHES. NEW SECTION OF SEAT TRACK P/N 60-22457, PO 23236312 SIZE 42 INCHES AND JOINTING ANGLE P/N 297018-1 IAW A300 SRM 53-10-10, 51-30-30. TREATED AND PAINTED NEW SECTION OF SEAT TRACK AN JOINTING ANGLE IAW A300 SRM 51-40-13 AND 51-40-11. INSTALLED NEW SEAT TRACK SECTION AND SPLICING ANGLES IAW A300 SRM 53-10-10 AND SRM 51-30-30. 2L72 4F RTA35EU 20040203003922004020300392WP 2004 2 3 DHL2004806533 120040106A5754 ANGLE DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RT WING STUB WING SUPPORT ANGLE CRACKED 2.000 AT STA XILD 42.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SUPPORT ANGLE AL7075-T6 0.063 IAW SRM 57-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA AND SUPPORT ANGLE IAW SRM 51-1-8B. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040203003932004020300393WP 2004 2 3 DHL2004806522 120040104A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT OUTER WING OUTBOARD L/E FORMER CRACK 0.250, STA XFS 785.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040203003942004020300394WP 2004 2 3 DHL2004806545 120040110A5330 SKIN DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 AFT SERVICE DOOR JAMB WITH 1.000 INCH CRACK IN UPPER FWD CORNER, STA 1620.000 L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 17 SHEET 3, DWG SRO8530021, DWG 5750776, TR 53-184. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN AREA IAW SRM 53-2-0 FIG 17 SHEET 3, TR 53-184. FABRICATED FILLER (7075-T6AL 0.080) AND 2 EA DOUBLERS (7075-T6AL 0.090) (7075-T6AL 0.125) IAW SRM 53-2-0 FIG 17 SHEET 3, TR 53-184. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLERS IAW SRM 53-2-0 FIG 17 SHEET3, TR 53-184, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040204000012004020400001WP 2004 2 4 DHL2004806527 120040106A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING OUTBOARD FLAP T/E DENTED AT STA XF 391.000. REMOVED DENTED T/E IAW SRM 51-1-21 PG 1. FABRICATED NEW T/E (6061T6AL 0.032) IAW SRM 57-1-0 PG 1, SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED INTERNAL AREA IAW SRM 51-1-8B. INSTALLED NEW T/E WITH NEW FASTENERS IAW SRM 57-7-1 PG 2, SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. 2L74 4F RT4A25 20040204000032004020400003 2004 2 4 2004UALA00020 420040108A2565 SLIDE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT OVERWING WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29474UA 1475 LT OVERWING EXIT SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN HATCH WAS REMOVED AND DID DEPLOY WHEN MANUAL OVERRIDE WAS ENGAGED. SLIDE BOTTLE ASSY INFLATION CABLE WAS FOUND KINKED INSIDE THE PULLEY OF THE WIRE CONTROL ASSY AND THE END OF CABLE WAS FOUND TWISTED. THIS IS CAUSED BY THE INFLATION CABLE BEING PUSHED DURING INSTLN OF SLIDE BOTTLE ASSY. THE INFLATION SYSTEM MANUAL OVERRIDE CREATED FORCES TO DEPLOY THE SLIDE ASSEMBLY. THE AMM INSTRUCTIONS AND SAFETY PRECAUTIONS OF THE OFFWING SLIDE BOTTLE ASSY CAUTION AGAINST PUSHING THE INFLATION CABLE DURING INSTALLATION. 2L72 4F4 FRTA28NM E40NE 20040204000042004020400004NE 2004 2 4 SVB2004F00000 220040112A7200 ENGINE BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL RIGHT MAKING METAL E SVBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2731SV 6108 2505 BB1514 PCE93003 PY1365 ON JAN 6, 2004 AIRCRAFT DEPARTED, ABOUT 10 MILES OUT THE PILOT NOTICED A RT ENGINE CHIP LIGHT. PILOT RETURNED TO DEPARTURE AND MADE AN UNEVENTFUL LANDING. AFTER INSPECTION OF THE CHIP DETECTOR BY MAINT IT WAS FOUND TO HAVE A PIECE OF GEAR TOOTH ON IT. FURTHER INSPECTION OF ENGINE OIL FILTER FOUND TO HAVE METAL AND BRASS. ENGINE BEING REMOVED AND TO BE SENT FOR REPAIRS. 1L72 4T4 T A24CE E4EA 5 CSTC 20040204000052004020400005NM 2004 2 4 ANCF200400002 120040127A275049387671 SPRING DOUG MD80 MD83 3023681NM TE FLAPS BROKEN W ANCFO OTHER O OTHER LDLANDING 1 SO23EICEQ 53123 DURING APROACH WHEN EXTENDING SLATS, THE LEVER CAN NOT BE MOVED FROM UP/ RET POSITION. LANDING WAS MADE WITH FLAPS / SLATS RETRACTED AND 1.25 VS SPEED. SPRING DETENT HELICAL EXT WAS FOUND BROKEN IN CRANK OF THE FLAP LEVER. IT WAS REPLACED IAW AMM 27-50-00 PAGE 102. TEST ON GROUND SATISFACTORY. P/N OFF AND ON 4938767-1. 2L72 4F RT 20040204000062004020400006CE 2004 2 4 GLBA20030536 120040117A77121303890023 TRANSMITTER BEECH 1900 1900D 1154162CE TORQUE INOPERATIVE A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM0394GL 3969 UE94 RT TORQUE GAUGE STUCK AT ZERO ON TAKE OFF, REMOVED AND REPLACED NR 2 TORQUE TRANSMITTER. 2L72 4T RTA24CE 20040203001972004020300197 2004 2 3 SWAA040084 420040109A2565 INDICATOR BOEING737 7372H4 138448CNM ESCAPE SLIDE OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 CREW REPORTS R2 DOOR EVAC SLIDE GAUGE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040203002042004020300204NM 2004 2 3 SWAA040091 120040109A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 344, STRINGER 11R. REPAIRED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040203002052004020300205NM 2004 2 3 SWAA040092 120040109A53306545776 BUTTSTRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT FASTENER HOLE ON BUTT SPLICE STRAP AT BS 908, BELOW STRINGER 4L. REPAIRED BUTT STRAP SPLICE PER SRM. 2L72 4F RTA16WE 20040203002102004020300210NM 2004 2 3 SWAA040097 120040109A552265C26384 TAB BOEING737 7373H4 1384600NM RT ELEVATOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C1 CHECK, RT AND LT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH TAB PUSH ROD BUSHINGS PER MM. 2L72 4F RTA16WE 20040203002242004020300224NM 2004 2 3 SWAA040082 120040108A53406527314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STRINGER 14L. REPAIRED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040203002332004020300233NM 2004 2 3 SWAA040066 120040107A53116546529 BELTFRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME INNER CHORD AND WEB CRACKED AT BS 344 BETWEEN STRINGERS 23L AND 24 L. REPAIRED BELTFRAME INNER CHORD PER SRM. 2L72 4F RTA16WE 20040203002362004020300236NM 2004 2 3 SWAA040069 120040107A3350PH22300L LIGHT BOEING737 7373H4 1384600NM ROW 6-8 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP AT ROW 6 TO ROW 8 CRACKED. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20040203002372004020300237 2004 2 3 SWAA040070 420040107A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040203002472004020300247NM 2004 2 3 SWAA040134 120040113A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAMS CORRODED AT BS 300 TO BS 328 RT AND BS 400 TO BS 420 LT. REPAIRED CREASE BEAMS PER SRM. 2L72 4F RTA16WE 20040203002512004020300251NM 2004 2 3 SWAA040138 120040113A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED MS CHECK, FOUND MID CABIN AISLE AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACK PER MM. 2L72 4F RTA16WE 20040203002622004020300262NM 2004 2 3 SWAA040113 120040111A53306545765 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING THRU FLIGHT CHECK, FOUND SKIN CRACKED AT BS 520, STRINGER 16L. REPAIRED SKIN CRACK PER EA. 2L72 4F A16WE 20040203002632004020300263NM 2004 2 3 SWAA040114 120040111A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED SC, FOUND SKIN CRACKED AT BS 960, WL 185 LT SIDE. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040203002682004020300268NM 2004 2 3 SWAA040119 120040112A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT AFT CARGO DOOR FRAME BS 794, RBL 9. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040203002782004020300278NM 2004 2 3 SWAA040140 120040114A53206545819 WEB BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED PM CHECK, FOUND CRACK UNDER NOSE WHEELWELL BELOW RT SIDE FWD ACCESS PANEL AT BS 243. REPAIRED PER EA. 2L72 4F A16WE 20040203002842004020300284NM 2004 2 3 SWAA040146 120040114A53306545854 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR CUTOUT SKIN CRACKED AT LOWER CORNER. REPAIRED SKIN CRACK PER EA. 2L72 4F RTA16WE 20040203002882004020300288NM 2004 2 3 SWAA040150 120040114A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED FROM BS 948 TO BS 990, LBL 55, WL 208. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040203002912004020300291NM 2004 2 3 SWAA040153 120040115A5315BAC1505 FLOORBEAM BOEING737 7373H4 1384600NM AFT CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 859, RBL 8 TO LBL 3. REPAIRED BEAM PER EA. 2L72 4F RTA16WE 20040203002932004020300293NM 2004 2 3 SWAA040155 120040115A3350BCREF4146 LIGHT BOEING737 7372H4 138448CNM COCKPIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20040203002962004020300296NM 2004 2 3 SWAA040158 120040115A53116546540 FRAME BOEING737 7372H4 138448CNM FUSELAGE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED C3 CHECK, FOUND BS 639 LT SIDE FRAME BROKEN 1 INCH ABOVE FLOOR LEVEL. REPAIRED FRAME PER EA. 2L72 4F A16WE 20040203002992004020300299 2004 2 3 SWAA040161 420040116A2565 CABLE BOEING737 7372H4 138448CNM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MIS-ROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F A16WE 20040203003032004020300303NM 2004 2 3 SWAA040165 120040116A575465C26602 WEDGE BOEING737 7373Q8 1384670NM NR 4 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE UPPER INBOARD SURFACE DELAMINATED. REPAIRED SLAT WEDGE PER EA. 2L72 4F RTA16WE 20040203003102004020300310NM 2004 2 3 SWAA040172 120040117A57536546486 WEDGE BOEING737 7373Q8 1384670NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD MIDFLAP T/E WEDGE PANEL DELAMINATED. REMOVED AND REPLACED T/E WEDGE PANEL PER MM. 2L72 4F RTA16WE 20040203003132004020300313NM 2004 2 3 SWAA040175 120040117A3350610478 BATTERY PACK BOEING737 7377Q8 1384418NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29799SW 28209 DURING SCHEDULED MC, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP AT CEILING AND LT OVERWING EXIT DOOR. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040203003382004020300338EA 2004 2 3 MASA200400005 120040103A7930APTE142100013D TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENG OIL PRESS FLUCTUATES A MASAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW07772861344 7286 872204 ASH 6317 MTY-PHX, IN CRUISE AT FL390 GOT TRIPLE CHIME & LEFT ENGINE OIL PRESS MASTER WARNING, OIL PRESS FLUCTUATING BETWEEN 18 & 28 PSI. SHUT DOWN LEFT ENGINE AND DIVERTED TO ELP. MX REPLACED PRESSURE TRANSDUCER, OP CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040203003452004020300345NM 2004 2 3 SWAA040201 120040121A57546937841 ARM BOEING737 7373H4 1384600NM KRUEGER FLAP BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 NR 4 KRUEGER FLAP ACTUATOR ARM BROKEN. REMOVED AND REPLACED KRUEGER FLAP ACTUATOR ARM PER MM. 2L72 4F RTA16WE 20040203003522004020300352NM 2004 2 3 SWAA040208 120040121A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED 1/4D CHECK, FOUND AFT BAGGAGE BIN FLOORBEAM CORRODED AT BS 945, RBL 3. FLOORBEAM REPAIRED PER EA. 2L72 4F RTA16WE 20040203003532004020300353NM 2004 2 3 DHL2004752514 120040119A5330 SKIN BOEING727 727223 1384074NM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING C-CHECK, RT AFT OVERWING EMERGENCY EXIT HATCH AT AFT TOP EXTERIOR SKIN EDGE IS BENT AND DENTED. CLEANED AREA AND FOUND SKIN TO BE CRACKED AND OUT OF LIMITS IAW B-727 SRM 52-00-02. CUT OUT DAMAGED AREA SIZE 1 X 1.5 INCH ON RIGHT AFT OVERWING EMERGENCY EXIT HATCH AFT TOP EXTERIOR SKIN IAW B-727 SRM 52-00-3 FIG 4. FABRICATED REPAIR FILLER FROM 2024-T3 .063 SIZE 1 X 1.5 INCH PO 900355 AND DOUBLER FROM 2024-T3 .063 INCH SIZE 4 X 8 INCH PO 900355 IAW B-727-SRM 52-00-3 FIG 4. TREATED AND PRIMED PARTS AND AREA IAW B-727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B-727 SRM 52-00-3 FIG 4. 2L73 4F A3WE 20040203003602004020300360NM 2004 2 3 UPS04241775 120040120A3510 REGULATOR BOEING727 72722C 138400FNM OXYGEN SYSTEM INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: PFLT, OXYGEN REGULATOR AT S/O POSITION HAS FLOW IN ALL POSITIONS. REMOVED AND REPLACED S/O OXYGEN REGULATOR, OPS CHECK NORMAL. 2L73 4F A3WE 20040203003712004020300371 2004 2 3 SWIA200412795 420040121A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07295UX7712 7712 120295 AUTOPILOT ON CAPT'S SIDE DOES NOT PASS FIRST FLIGHT OF DAY CHECKS. REPLACED NR 1 AUTOPILOT COMPUTER. OPS CHECKED GOOD. 2L72 4T RTA31SO 20040203003742004020300374WP 2004 2 3 AALA20040106 120040122A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217540A 49994 DEN EMERGENCY LIGHTS AT LEFT AND RIGHT AFT OVERIWNG EXITS INOPERATIVE. REPLACED BATTERY PACK AT FOR EMERGENCY LIGHTS AT LOCATION B5-105. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040203003832004020300383SO 2004 2 3 C2XA04SH027 120040124A532014525381003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV- DURING C-CHECK, THE LEFT HAND BUTTSTRAP FROM FRAME 65 TO FRAME 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040203003872004020300387SO 2004 2 3 C2XA04TY022 120040123A575114569009408 FAIRING EMB 145 EMB145 3260210SO RT AILERON GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND AILERON TO PCA INBOARD FITTING. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EC5750-01177 AND CPM 51-21-05AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040203003952004020300395WP 2004 2 3 DHL2004806550 120040120A5754 DOOR DOUG DC8 DC873F 302199FWP LE SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT INBOARD SLOT UPPER DOOR WITH 0.750 CRACK IN IT. REMOVED AND REPLACED LEFT INBOARD SLOT UPPER DOOR IAW MM 27-80-1 PG 201-204. REFER TO NR 2228 FOR OPS CHECK. 2L74 4F RT4A25 20040203003972004020300397WP 2004 2 3 DHL2004806524 120040107A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT STUB WING FORMER CRACK 0.250, STA XFS 548.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040203003982004020300398WP 2004 2 3 DHL2004806525 120040106A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT INNER WING CTR L/E FORMER 1.000 INCH CRACK, STA XFS 385.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (2024T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 51-1-20D PG 9, SRM 57-2-0 PG 9, 10. 2L74 4F RT4A25 20040204000022004020400002NM 2004 2 4 2004UALA00012 120040106A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 CABIN SHEAR TIES CRACKED AT STA BS460 S16L, BS480 S16L AND BS500A S15L. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040204000192004020400019NM 2004 2 4 371PA0033 120040110A3350 LIGHT BOEING737 737306 13844BGNM CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING SYSTEM INOPERATIVE. FOUND TO BE SATURATED WITH WATER. INSPECTED, CLEANED AND DRYED TRACK, CABLE AND LIGHTS. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20040204002272004020400227NM 2004 2 4 WRLA200406 120040119A3213ARG70765511 CYLINDER DOUG MD11 MD11 3023602NM RT MLG UNDERSERVICED A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11277WA 48743 GEAR HANDLE LOCKED IN FLIGHT. AIR RETURN TO LAX. RESET HANDLE FUSE PER MAINTENANCE MANUAL 32-37-01 AND REBLEED BOGEY TRIM CLYINDER PER THE SAME MAINTENANACE MANUAL REFERENCE, GEAR HANDLE OPERATION IS NORMAL. LEAK CHECK OK. 2L73 4F RTA22WE 20040204002302004020400230NM 2004 2 4 WRLA200405 120040119A21216054578 FAN DOUG MD11 MD11 3023602NM CABIN AIR FAILED A WRLAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11804DE 48318 CABIN SMOKE LEFT SIDE ROWS 38-46 ABOUT 4 HOURS INTO FLIGHT. ODOR COMING FROM AIR SYSTEM E=EYE BALL VENTS. FOUND 3 PHASE C/B OF PASS AIR OUTLETS FAN AT 2R DOOR PANEL POPPED. REMOVED AND REPLACED PAX AIR OUTLET FAN ASSY AT FS 769, SYSTEM OPS CHECK GOOD. 2L73 4F RTA22WE 20040205000592004020500059EA 2004 2 5 ASOA04004 120040104A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 FLT 4409 - DURING A GROUND INSPECTION IN DFW, THE FILGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE PERFORMED OPERATIONAL TEST ON THE PASSENGER DOOR WITHOUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000602004020500060EA 2004 2 5 ASOA04003 120040104A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT COULD NOT GET THE PASSENGER DOOR TO CLOSE. MAINTENANCE OPERATED THE PASSENGER DOOR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000612004020500061EA 2004 2 5 ASOA04002 120040104A5210601R38370143 CABLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11856AS 7404 FLT 4740 - DURING A GROUND INSPECTION IN ICT, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SUPPORT WHEEL RETRACT CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000622004020500062EA 2004 2 5 ASOA04001 120040102A493038834491 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LOOSE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11865AS 7507 FLT 4138 - DURING FLIGHT FROM LIT-ATL, THE CREW NOTICED A STRONG JET FUEL ODOR IN THE COCKPIT WHEN THE ACM WERE SELECTED ON. THE ODOR OCCURRED WITH BLEEDS ON THE AUXILIARY POWER UNIT AND THE ENGINE. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE TIGHTENED A LOOSE TUBE ASSEMBLY CONNECTOR TO THE FUEL SOLENOID ON THE AUXILIARY POWER UNIT AND ALSO REMVOED AND REPLACED THE COALESCER BAGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000712004020500071EA 2004 2 5 ASOA04008 120040104A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11856AS 7404 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040205000812004020500081NM 2004 2 5 AWXA200400078 120040107A531190526912 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON FRAME FOOT AT BS 616, RBL 62. MAINTENANCE CUT OUT CRACK ON INNER CHORD FLANGE AT BS 616, RBL 62; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20040205000822004020500082NM 2004 2 5 AWXA200400079 120040107A53136545765125 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 4 EACH CRACKS WERE FOUND ON STRINGER 8 LT AT BS 380. MAINTENANCE PERFORMED HFEC INSPECTION OF CRACKS TO VERIFY CRACK ENDS; STOP DRILLED 4 EA CRACKS ON STRINGER 8 LT AT BS 380; PERFORMED HFEC INSPECTION TO VERIFY CRACKS ARE CONTAINED; FABRICATED A REPAIR CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-03, FIG 204, PG 217-219. 2L72 4F RTA16WE 20040205000842004020500084EA 2004 2 5 COMA0460079 120040122A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA17110 7158 RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED DAMAGED 625 OBLIQUE ANGLE AND REPLACED ANGLE WITH P/N 601-35012-42 IAW BOMBARDIER CRJ 200 SRM 51-42-21. 2L72 4F RTA21EA 20040203003472004020300347 2004 2 3 SWAA040203 420040121A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040203003512004020300351NM 2004 2 3 SWAA040207 120040121A3350PH22300L LIGHT BOEING737 7373H4 1384600NM ROW 8-10 SEPARATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FLOOR TRACK SEPARATED FROM ROW 8 TO ROW 10 LT SIDE. REMOVED AND REPLACED FLOOR TRACK PER MM. 2L72 4F RTA16WE 20040203003552004020300355SO 2004 2 3 C2XA04BT010 120040123A361014549070405 LINE EMB 145 EMB145 3260210SO CABIN AREA BROKEN A C2XABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2734111 145659 CREW REPORTED, BLEED LEAK IN FLIGHT, LOUD DECOMPRESSION, AND ODOR OF SMOKE FROM NR 2 ENGINE. PERFORMED EMERGENCY LANDING IN NEWARK, AIRCRAFT LANDED UNEVENTFULLY. DURING TROUBLESHOOTING MAINTENANCE FOUND BLEED AIR TUBING ASSEMBLY WHICH CONTROLS NR 2 ENGINE THERMOSTAT (HT)&(LT) FORWARD AUTO LATCHING COUPLING TO BE BROKEN. REMOVED AND REPLACED NR 2 BLEED DUCT AT CARGO BAY POSITION UNDER FLOOR IAW EMB145 MM 36-11-09, OPS AND LEAK CHECKED GOOD OF BLEED SYSTEM IAW EMB145 MM 36-00-00. PRESSURIZATION CHECKED GOOD IAW EMB145 MM 21-31-00. INSTALLED FLOOR PANELS 272AF AND 272BF. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040203003582004020300358NM 2004 2 3 04FDEA00204 120040122A5280 SEAL BOEING727 727200 138407ENM MLG DOOR OUT OF POSITION A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25278FE 22345 NOSE GEAR DOOR WARNING LIGHT ILLUMINATED WITH GEAR DOWN. AFTER GO-AROUND DOOR LIGHT EXTINGUISHED. VISUALLY INSPECTED BOTH NOSE GEAR DOOR SWITCHES, NO DEFECTS NOTED. FOUND BOTH DOORS WERE DIFFICULT TO OPEN AND CLOSE. WHEN DOORS WERE LATCHED HAD TO BE PUSHED UP TO BE FLUSH. THE SEAL IN FRONT OF DOORS APPEARS TO BE TOO THICK. REQUIRES MORE T/S. UNABLE TO JACK AC DUE TO HIGH GUST WINDS. TROUBLESHOOTING GEAR DOOR WARNING PER 727 MM 32-62-000-1, NLG DOOR BULB SEAL AT STA 227.8 RESTRICTING DOOR OPERATION. CLEANED DOOR BULB SEAL. DOOR OPERATION NORMAL. 2L73 4F RTA3WE 20040203003652004020300365EA 2004 2 3 SWIA200412789 120040112A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07912SW5151 5151 7595 SPOILERONS FAULT STATUS MESSAGE. REPLACED LT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT IAW MM 27-62-01. OPS & LEAK CHECK GOOD. 2L72 4F RTA21EA 20040203003662004020300366EA 2004 2 3 SWIA200412790 120040115A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07926SW 7687 STAB CH2 WILL NOT ENGAGE. REMOVED & REPLACED HSTCA AND HSTCU IAW CRJ MM 27-40-00, OPS CHECKS GOOD. P/N 7062-3, S/N OFF 943. 2L72 4F RTA21EA 20040203003702004020300370 2004 2 3 SWIA200412794 420040119A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07216SW 120285 CO-PILOT SIDE SHAKER/PUSHER ACTIVATES ON GROUND. REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL IAW 27-34-08. OPS CHECK GOOD. P/N: 120-34428-505. 2L72 4T RTA31SO 20040203003722004020300372EA 2004 2 3 SWIA200412796 120040120A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07952SW 7813 SPOILERON FAULT STATUS MESSAGE - RIGHT SPOILERON. REMOVED AND REPLACED RT SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20040203003862004020300386SO 2004 2 3 C2XA04TY021 120040123A532014521725613 SILL EMB 145 EMB145 3260210SO DOOR FRAME CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FRAME FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE SILL IAW EMB SRM 57-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040203003892004020300389NM 2004 2 3 P9RA20040005 120040125A5270MS250111 PROXIMITY SWITCH BOEING727 727200 138407ENM MLG DOOR OUT OF ADJUST A P9RAO OTHER J WARNING INDICATION CRCRUISE 1 SO11919PG 22604 IN CRUISE FLIGHT PIE TO SYR, NOSE WHEEL GEAR DOOR EXTENDS IN LIGHT CHOP. FOUND LEFT NOSE WHEEL WELL DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SAME PER MM 32-62-11, OPS CHECKED NORMAL. 2L73 4F RTA3WE 20040204000092004020400009GL 2004 2 4 O05R200416973 320040127A611166070924017 BLADE FRCHLDSA227 SA227CC 3377522SW GARRTTTPE331TPE331* 01514WP ROTOL R321 R321482F8 GL PROPELLER DAMAGED B K NONE O OTHER ININSP/MAINT 1 GL05698FA14223 AC698 DRIDRG1360 BLADE REJECTED IAW MFG CONCESSION 102566/C/P. 2L72 4T3 TRTA18SW E2WE 6 CP61GL 20040204000162004020400016NM 2004 2 4 P5CA0401025 120040110A5230D20702 ACTUATOR BOEING747 747259B 1384804NM CARGO DOOR FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23924FT 21730 MAIN SIDE CARGO DOOR WILL NOT LOCK. MOTOR RUNS BUT ACTUATOR DOES NOT TURN. CORRECTIVE ACTION TAKEN: REMOVED AND REPLACED LATCH ACTUATOR IAW AMM 52-32-09 OPERATION, INDICATION CK OK. 2L74 4F RTA20WE 20040204000182004020400018NM 2004 2 4 AWXA200400017 120040102A2752657327121 SHAFT BOEING737 7373Q8 1384670NM ZONE 309 LT WW STRIPPED A AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28327AW 23507 FLIGHT CONTROL - FLT 0137 - ON FINAL APPROACH, EN ROUTE, SELECTED TRAILING EDGE FLAPS TO 40, LT FLAP STAYED AT 30 AND RT FLAP WENT TO 40, FLAPS LOCKED OUT AND DID NOT MOVE EITHER DIRECTION. MAINTENANCE TROUBLESHOT AND FOUND THE LT FLAP DRIVE SHAFT FROM FLAP DRIVE UNIT TO THE NR 4 TRANSMISSION STRIPPED. REMOVED AND REPLACED DRIVE SHAFT IAW BMM 27-51-64, CYCLED FLAPS SEVERAL TIMES WITH NO DEFECTS NOTED. 2L72 4F RTA16WE 20040204002262004020400226NM 2004 2 4 WRLA200407 120040124A261180380203 FIRE DETECTOR DOUG MD11 MD11 3023602NM NR 2 ENGINE FAILED A WRLAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO11278WA 48746 NR 2 ENGINE AURAL FIRE WARNING AT TOP OF DESCENT NO VISUAL ALERT TESTED FIRE WARNING RECEIVED. VISUAL WHEN TEST FINISHED. SHUTDOWN NR 2 ENGINE IAW PROCEDURES FIRED BOTH BOTTLES. DID NOT EXTINGUISH ALERT. FCDU REMOVED. FAULTY REMOVED AND REPLACED FCDU. 2L73 4F RTA22WE 20040205000852004020500085NM 2004 2 5 QXEA200400080 120040128A5210 MECHANISM BOMBDRDHC8 DHC8401 1390041NM PAX DOOR LACK OF LUBE A QXEAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 NM09415QX 4081 GEG - FLIGHT 2358 - AFT PASSENGER DOOR WILL NOT OPEN. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED THE DOOR MECHANISM. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040205000862004020500086NM 2004 2 5 04FDEA00287 120040201A5310 STRUCTURE DOUG MD11 MD11 3023602NM MAIN DECK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA HAS CORROSION IN TWO PLACES. MAIN CARGO DECK RT STA 1821 TO STA 1831 FLANGE AREA, CORRODED AREA CARRIED OUT REPAIR IAW SRM 53-70-00, FIG. 5, VOL.I. 2L73 4F RTA22WE 20040205000872004020500087NM 2004 2 5 04FDEA00288 120040201A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 TAIL TANK, TO ACCOMPLISH E1-5510-7-5000 PT 1. LT NR 36 BARREL NUT HOLE CORROSION REMOVAL, WEB CUTTING REQUIRE FOR ACCESS. HORIZONTAL STABILIZER, TAIL TANK, WEB CUT OUT FOR ACCESS OF LT NR 36 BARREL NUT HOLE. CORROSION REMOVAL AND REPAIR CARRIED OUT AS PER EA 1-5320-74276 (TITLE: FUSELAGE - AUXILLIARY STRUCTURE - ACCESS FROM PANEL FOR 36LR - BARREL NUT MOD). 2L73 4F RTA22WE 20040205000882004020500088SO 2004 2 5 C2XA04SH043 120040203A531514522226003 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040206000252004020600025NM 2004 2 6 USAABB04001 120040101A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 PHL - FOUND ONE FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040206000762004020600076WP 2004 2 6 DHL2004806546 120040114A534037584952N FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01806DH84257 46002 AFT CARGO COMPT FITTING CRACKED 2.000, L-34R L-35R, STA 1240.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040206000802004020600080WP 2004 2 6 DHL2004806515 120040105A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 7 FLOOR TRACK LUG WORN, STA 190.000. CUT OUT DAMAGED SECTION OF NR 7 FLOOR TRACK IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUGS IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000882004020600088WP 2004 2 6 DHL2004806523 120040107A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT STUB WING FORMER CRACK 0.250, STA XFS 535.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.040) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040206000892004020600089WP 2004 2 6 DHL2004806549 120040112A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FUSELAGE TAIL SECTION L-17R, STA 1770.000 CRACKED 3.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED DETERIORATED LONGERON SECTION IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON SECTION IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000902004020600090WP 2004 2 6 DHL2004806551 120040121A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FWD ACCY COMPT BEAM JOINT ANGLE WITH INTERCOSTAL CRACKED 2.000 STA 70.000 LBL 47. REMOVED CRACKED ANGLE IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-3-1 PG 1, 2. 2L74 4F RT4A25 20040206000912004020600091WP 2004 2 6 DHL2004806552 120040121A534752772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 6 FLOOR TRACK LUGS WORN (STA 1590.000-1640.000). REMOVED TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. 2L74 4F RT4A25 20040206000922004020600092WP 2004 2 6 DHL2004806535 120040107A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FUSELAGE NOSE SECTION EXTERIOR SKIN CRACKED 0.250 AT STA 53.000 L-30L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 13. REMOVED EXISTING REPAIR IAW SRM 51-1-20D PG 21. TRIMMED OUT CRACKED AREA IAW SRM 53-2-0 FIG 13. FABRICATED FILLER (2024T3AL 0.050) AND DOUBLER (2024T3AL 0.071) IAW SRM 53-2-0 FIG 13. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0 FIG 13, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040206000932004020600093WP 2004 2 6 DHL2004806548 120040112A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FUSELAGE TAIL SECTION L-17L, STA 1770.000 CRACKED 2.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED DETERIORATED SECTION IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LONGERON SECTION IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000942004020600094WP 2004 2 6 DHL200480654 120040116A534037540432 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT CUSP EXTRUSION FWD FITTING CRACKED 3.000 AT STA 1180.000, L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000952004020600095WP 2004 2 6 DHL2004806510 120040104A534736575031 SEAT TRACK DOUG DC8 DC873F 302199FWP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FLIGHT COMPT F/E AFT SEAT TRACK WITH ELONGATED HOLES. REMOVED F/E AFT SEAT TRACK WITH ELONGATED HOLES IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK ASSY IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000222004020600022NM 2004 2 6 USAABB04002 120040101A335020121 CHARGER BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 PHL - FOUND THE AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2L72 4F RTA1NM 20040206000852004020600085WP 2004 2 6 DHL2004806538 120040106A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 7 FLOOR TRACK LUG WORN, STA 210.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000872004020600087WP 2004 2 6 DHL2004806516 120040106A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 4 FLOOR TRACK LUG WORN STA 390.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED PLUG AND CHANNEL IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206000972004020600097WP 2004 2 6 DHL2004806519 120040103A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING STUB WING FORMER UPPER INTERNAL PART CRACKED 0.500 AT STA XRS 537.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (2024-T3AL 0.032) IAW SRM 53-2-0 PG 2E. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLERS IAW SRM 53-2-0 PG 2E, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040206000992004020600099WP 2004 2 6 DHL2004806542 120040107A534752772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1590.000-1610.000). TRIMMED NR 2 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075-T6AL 0.100) (7075T6AL 0.125) (7075-T6AL 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED SPLICES AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0. 2L74 4F RT4A25 20040206001032004020600103WP 2004 2 6 DHL2004806513 120040106A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT NR 1 FLOOR TRACK LUG WORN AT STA 270.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3 PG 17, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206001052004020600105WP 2004 2 6 DHL2004806529 120040107A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 5 FLOOR TRACK LUGS WORN (STA 1680.000 - 1702.000). CUT OUT NR 5 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075T6AL 0.100) (7075T6AL 0.125) (7075T6AL 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA, NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206001062004020600106WP 2004 2 6 DHL2004806517 120040104A5712 RIB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT OUTER WING OUTBOARD L/E FORMER CRACKED 0.250 AT STA XFS 791.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024T3 AL 0.032) IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040206001072004020600107WP 2004 2 6 DHL2004806540 120040114A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER FUSELAGE EXTERIOR SKIN WITH 1.000 INCH CRACK IN IT (STA 1742.000-1743.000, L-16L TO L-17L), MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-5-3 FIG 1, SRM 53-2-1 FIG 7. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT CRACKED SKIN AREA IAW SRM 53-2-1 FIG 7. FABRICATED FILLER (7075-T6AL 0.063), FINGER DOUBLER (7075-T6AL 0.040) AND DOUBLER (7075T6 AL 0.071) IAW SRM 53-5-3 FIG 1, SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLER AND DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040206001082004020600108WP 2004 2 6 DHL2004806521 120040105A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT OUTER WING L/E FORMER CRACK 0.500, STA XFS 660.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B PG 16, 17. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10. 2L74 4F RT4A25 20040206001092004020600109WP 2004 2 6 DHL2004806528 120040106A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 3 FLOOR TRACK LUGS WORN (STA 1680.000-1702.000). CUT OUT NR 3 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. FABRICATED 3 EA SPLICES (7075T6AL 0.100) (7075T6AL 0.125) (7075T6AL 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA, NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49, 50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206001102004020600110WP 2004 2 6 DHL2004806537 120040112A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 ACCESSORY COMPT FORMER ATTACHING FRAME TO FUSELAGE 1.000 CRACK, STA 640.000 L-26R TO L-27R. REMOVED FASTENER IAW SRM 51-1-21 PG 1-2. CUT OUT FORMER DAMAGED AREA AND FABRICATED FORMER REPAIR ANGLE (7075 0.0.071) IAW SRM 53-2-0 PG 11 FIG 2A. HEAT TREATED IAW SRM 51-1-1 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FORMER REPAIR ANGLE IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20040206001112004020600111WP 2004 2 6 DHL2004806531 120040107A5754 SKIN DOUG DC8 DC873F 302199FWP LE STRUCTURE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT INNER WING OUTBOARD EXTENDED L/E SLOT SKIN CRACKED 4.000 AT STA XILD 42.000. REMOVED CRACKED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6AL 0.071) IAW SRM 57-3-3 PG 11. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACE IAW SRM 51-1-8B. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040206001122004020600112WP 2004 2 6 DHL2004806539 120040109A534037540322N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT CUSP EXTRUSION AFT FITTING CRACKED 2.000, STA 1177.000, L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1 IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1, SRM 51-3-1 PG 1. 2L74 4F RT4A25 20040206001132004020600113WP 2004 2 6 DHL2004806534 120040106A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1550.000-1590.000). REMOVED DAMAGED SEGMENT OF FLOOR TRACK NR 2 (STA 1550.000-1590.000) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040206001182004020600118WP 2004 2 6 DHL2004806532 120040112A57405769859U164 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 NR 3 RIGHT STUB WING ZEE PAN FITTING WITH 8.000 CRACK, STA XILD 42.000. REMOVED ZEE PAN FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN FITTING IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040206001192004020600119EU 2004 2 6 DHL2004365501 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH SEAT TRACK AT FR38 CENTER TRACK GOUGED IN TWO PLACES. REWORK AREA GOUGED AT SEAT TRACK AT FR38 CENTER TRACK, FOUND OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK BETWEEN FR37 AND 38 TO FR40 IAW A300 SRM 51-40-12, 51-30-30 AND 53-10-10 FIG 724. NEW SEAT TRACK P/N 60-22457, PO 23236312 LENGTH 55 INCHES SPLICING ANGLES P/N 60-12336. 2L72 4F RTA35EU 20040206001212004020600121WP 2004 2 6 MWEA040012 120040125A2913AS66411LS666 PUMP DOUG DC9 DC981 3022081WP LT HYD SYSTEM INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31812ME 48006 LEFT SYSTEM HYDRAULIC PRESSURE DROPPED TO ZERO PSI WHEN TRANSFER PUMP WAS TURNED OFF. REMOVED AND REPLACED ENGINE HYDRAULIC PUMP. 2L72 4F A6WE 20040206001232004020600123WP 2004 2 6 ABXA040038 120040121A3350 LIGHT DOUG DC8 DC863F 302198FWP CABIN WILL NOT TEST A ABXAK NONE L NO TEST NRNOT REPORTED 1 GL23819AX 45927 EMERGENCY EXIT LIGHT, DISARM CHECK, WOULD NOT TEST. RELAMPED, OPS CHECKED NORMAL. 2L74 4F 4A25 20040206001242004020600124WP 2004 2 6 ABXA040039 120040123A32305715307 LINK DOUG DC8 DC863F 302198FWP MLG LOOSE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23811AX 2820 46113 UPLATCH CHECK FAILED ON INITIAL CHECK. GEAR WAS CYCLED THROUGH ONCE THEN UPLATCH CHECK WAS ACCOMPLISHED. UPLATCH CHECK WAS SATISFACTORY. FOUND LEFT MAIN LANDING GEAR LOWER SIDE BRACE LOWER LINK AND LOWER SIDE BRACE UPPER LINK WITH EXCESSIVE PLAY. REPLACE UPPER SIDE BRACE LOWER LINK AND LOWER BRACE LINK BOLT AND UNIVERSAL BLOCK BOLT IAW DC-8 MM 32-11-03-2-0001 AND DOUGLAS DRAWING 5753118. REPLACED UPPER SIDE BRACE UPPER LINK AND CENTER JOINT BOLT. ADJUSTED LINK IAW 32-11-03-2-0001 AND DOUGLAS DRAWING 5753118. LEFT MAIN LANDING GEAR SWING OPS CHECKED GOOD IAW DC-8 MM 32-11-03-2. 2L74 4F 4A25 20040206001252004020600125EU 2004 2 6 XNOA1174 120040124A7603 TRACK AIRBUS300 A300B4203 3930306EU NR 1 THROTTLE OBSTRUCTED A XN0AA UNSCHED LANDING C F.O.D. CLCLIMB 1 GL23373PC 218 NR 1 THROTTLE WILL NOT ADVANCE PAST 35. FOUND METAL DEBRIS ON NR 1 ENGINE THROTTLE TRACK. REMOVED (FOD) & ADVANCED THROTTLE SEVERAL TIMES WITH NO FURTHER DEFECTS. AIRCRAFT OKAY FOR SERVICE IAW A-300 AMM 76-11-00. 2L72 4F RTA35EU 20040206001322004020600132EU 2004 2 6 DHL2004365507 120040113A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH REPAIR AT RIGHT FUSE FR19 STR 23R GOUGED. REMOVED EXISTING DOUBLER AT RIGHT FUSE FR19 STR23R IAW A300 SRM 51-30-30. SMOOTHED OUT FUSELAGE SKIN SECTION NEXT TO DOUBLER AREA AS PER A300 SRM 51-40-11. MAXIMUN MATERIAL LOSS-.011 ORIGINAL THICKNESS 0.63 FOUND TO BE OUT OF LIMITS PER A300 SRM 53-10-00 DIAGRAM 601 PG 610. REMOVED PANEL AT END CARGO COMP AND E&E COMP RT FOR ACCESS TO FUSE REPAIR AS PER A300 SRM 51-30-30. HFEC INSPECTED AREA AT FR19 STR23R IAW A300 NTM 51-30-00 PART 1 NO DEFECTS NOTED. INSTALLED DOUBLER REPAIR AT RT FUSE FR19 STR23R AS PER A300 SRM. INSTALLED PANEL AT FWD CARGO COMP AND E&E COMP RT AS PER A300 SRM. 2L72 4F RTA35EU 20040206001382004020600138 2004 2 6 VNAA0401004 420040110A3418 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT AOA FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07430JS 3044 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATIONS AND ABORTED TAKEOFF. MAINTENANCE CONTROL HAD OUTSTATION MAINTENANCE PERFORM OPERATION CHECKS AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001392004020600139 2004 2 6 VNAA0401005 420040110A3418861EF1 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT AOA FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07430JS12640 3044 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATIONS AND ABORTED TAKEOFF. MAINTENANCE WAS THEN DISPATCHED FROM DAY. MAINTENANCE THEN REPLACED THE LEFT HAND AOA SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001402004020600140EA 2004 2 6 VNAA0401007 120040113A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LAVATORY FAILED A VNAAO OTHER L NO TEST NRNOT REPORTED 1 GL07207PS 7873 THE CREW REPORTED A LAV SMOKE FAIL INDICATION WHEN TESTED. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH 26-3 CODE C. 2L72 4F4 FRTA21EA E15NE 20040206001442004020600144NM 2004 2 6 CALA0400053 120040123A5312 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE CANNING A CALAK NONE O OTHER ININSP/MAINT 1 SW2712318 23369 INSPECTION FOUND AFT PRESSURE BULKHEAD WEB REPAIR LIFTING OFF AT EDGES AT STA 1016. INSTALLED INTERIM REPAIR PER PART 1 OF ECRA 5311-01174. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 12,000 CYCLES. 2L72 4F RTA16WE 20040206001452004020600145NM 2004 2 6 CALA0400054 120040123A5230 SKIN BOEING737 7373T0 1384582NM C-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714324 23375 INSPECTION FOUND A 1 INCH CRACK AROUND LIGHTENING HOLE IN C-2 DOOR INNER SKIN ABOVE AND FORWARD OF DOOR HANDLE. REPAIRED SKIN IAW ECRA 5232-01039. 2L72 4F RTA16WE 20040206001462004020600146NM 2004 2 6 CALA0400055 120040123A5754 SKIN BOEING737 7373T0 1384582NM NR 5 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND FIVE 1 INCH CRACKS IN NR 5 SLAT SKIN LOWER SURFACE I/B OF AUX TRACK. A DOUBLER WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20040206001472004020600147NM 2004 2 6 CALA0400056 120040124A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND RT LOWER SURFACE OF PRESSURE DECK ANGLE CORRODED IN WHEEL WELL AT STA 706, RBL 64. A DOUBLER WAS INSTALLED IAW SRM 51-40-11 AND 51-40-02 AND DRAWING PL65-50733. 2L72 4F RTA16WE 20040206001492004020600149WP 2004 2 6 CALA0400058 120040125A38200036631823 CONNECTOR DOUG DC9 DC982 3022082WP WATER HEATER SHORTED A CALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW27819NY 49479 THE FORWARD LAV WATER HEATER CIRCUIT BREAKER POPPED WHILE ON DESCENT INTO EWR. THE LAV SMOKE DETECTOR ACTIVATED AND THE FLIGHT ATTENDANTS NOTICED SMOKE IN THE FORWARD LAV SHORTLY AFTER THE C/B POPPED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD LAV WATER HEATER CONNECTOR SHORTED. THE CONNECTOR WAS REMOVED AND REPLACED. THE CONNECTOR WAS DISCONNECTED AND SECURED WHILE THE WATER HEATER WAS PLACARD INOPERATIVE DUE TO NOT BEING IN STOCK. THE C/B WAS PULLED AND COLLARED. 2L72 4F A6WE 20040206001512004020600151NM 2004 2 6 CALA0400060 120040125A5730 SKIN BOEING737 7373T0 1384582NM LT WING LE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714325 23455 INSPECTION FOUND LT WING LEADING EDGE SKIN GOUGED AT CENTER AUX TRACK ICE DOOR CUTOUT (UNDER NR 1 SLAT). REPAIRED IAW SRM 51-70-16. 2L72 4F RTA16WE 20040206001532004020600153EA 2004 2 6 COMA0460076 120040122A53116003603024 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA16390 7158 RIGHT SIDE FS 718.0 FRAME AND FRAME DOUBLER IS CRACKED. REMOVED CRACKED FRAME AND FRAME DOUBLER, INSTALLED NEW FRAME AND FRAME DOUBLER IAW BOMBARDIER, INC REO 601R-53-61-243. 2L72 4F RTA21EA 20040206001542004020600154EU 2004 2 6 MALA040127 120040124A3000 VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ANTI ICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15426XJ 340B426 DURING FLIGHT, RIGHT AIR VALVE LIGHT INFLIGHT, RAN QRH AND NO FIX. AIR RETURN TO MSP. MAINTENANCE REPLACED ANTI ICE VALVE PER 75-00-00, OPS CHECKS GOOD PER 72-00-00. 2L72 4T4 TRTA52EU E8NE 20040206001552004020600155EU 2004 2 6 MALA040126 120040123A3230HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15508XJ E2318 AFTER TAKEOFF, LT MAIN GEAR WOULD NOT RETRACT, CONFIRMED BY BUFFETING AND RUDDER. RECYCLED THE GEAR AT WHICH POINT THE LT MAIN CAME UP BUT THE RT MAIN DID NOT INDICATE UP AND THE RT MAIN DID NOT INDICATED UP UNTIL HALFWAY TO MSP, HYDRAULIC GAUGES READ NORMAL. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE P/N HTE9490-4 S/N OFF FR012BB S/N ON FRTR003AW IAW 32-30-17 LEAK CHECK GOOD. OPS CHECK, NO GOOD. SLAVE IN NEW HANDLES NO HELP. REINSTALLED ORIGINAL BLEED LT & RT OLEO LOCK JACKS IAW 29-00-00, OPS CHECK GOOD IAW 32-30-00. REF 409 NR 194686 FOR DETAILS. 2H74 4F RTA49EU 20040206001572004020600157 2004 2 6 AWXA200400064 420040123A23707430304001 VIDEO UNIT AIRBUS320 A320232 3930326EU ZONE 250 SHORTED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28661AW7265 3852 1284 EN ROUTE FROM JFK TO PHX, FLIGHT ATTENDANT REPORTED A BURNING ODOR AND SMOKE COMING FROM VIDEO TAPE RECORDER IN REAR CABIN. MAINTENANCE REMOVED AND REPLACED VIDEO TAPE RECORDER IN REAR CABIN, OPERATIONAL CHECK WAS GOOD. ANALYSIS OF VIDE0 TAPE RECORDER S/N 100115 WAS NO FAULT FOUND. UNIT WAS OPENED AND A VISUAL INSPECTION OF CIRCUIT BOARDS WAS ACCOMPLISHED FINDING NO EVIDENCE OF DAMAGED PARTS. UNIT WAS REASSEMBLED AND TESTED WITH ALL FUNCTIONS OPERATING NORMALLY. 2L72 4F RTA28NM 20040206001582004020600158NM 2004 2 6 AWXA200400065 120040124A2150655281050 ACCESSORY UNIT BOEING737 7373G7 1384595NM RT A/C UNIT MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28155AW1375511825 23777 AFTER T/OFF, RT PACK WOULD NOT COOL A/CRAFT. GROUND DUCT TEMP 28 C, OAT 12 C, CABIN 22 C WITH RAM AIR DOOR OPEN, AT FL 210 GROUND DUCT 38 C, OAT 5 C, CABIN 30 C WITH RAM AIR DOOR CLOSED 15 DEG, GROUND DUCT 33 C, OAT 1 C, AND CABIN 30 C WITH RAM AIR DOOR CLOSED. LT PACK ALREADY ON MEL: TURNED BACK. WHILE PREPARING TO LAND WITH RAM AIR DOOR OPEN & FLAPS EXTENDED, MIX VALVE SHOWED FULL COLD. MX REPLACED RT AIR CON ACCY UNIT & AIR MIX VALVE IAW AWA T/C R2C21003, OPS CHECK GOOD. FUNCT TEST OF AIR MIX VALVE, NO FAULT FOUND. VENDOR FUNCT TEST OF A/CON ACCY UNIT CONFIRMED FAILURE. FOUND K2 & K17 RELAYS INTERMITTENT & HIGH CONTACT RESISTANCE. CLEANED UNIT & REPLACED K2 & K17 RELAYS, FUNCTIONAL TEST GOOD IAW CMM. 2L72 4F RTA16WE 20040206001592004020600159NM 2004 2 6 AWXA200400066 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 400, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 400, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 4, 8, & 12. 2L72 4F RTA16WE 20040206001602004020600160NM 2004 2 6 AWXA200400067 120040104A5320654580842 STIFFENER BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STIFFENER JUST FORWARD OF BS 294 AT STR 26 LT. MAINTENANCE REMOVED CORRODED STIFFENER BS 294, STR 26 LT; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45808; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 45. 2L72 4F RTA16WE 20040206001612004020600161NM 2004 2 6 AWXA200400068 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 4, 8 & 12. 2L72 4F RTA16WE 20040206001632004020600163NM 2004 2 6 AWXA200400070 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727C, STR 7 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727C, STR 7 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2L72 4F RTA16WE 20040206001682004020600168NM 2004 2 6 AWXA200400075 120040107A53116546531510 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON FRAME BETWEEN STRINGERS 28 LT AND 28 RT, AT BS 500. MAINTENANCE REMOVED DAMAGED AREA OF FRAME BETWEEN STRINGERS 28 LT AND 28 RT, AT BS 500; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07, FIG 201 PG 202-203. 2L72 4F RTA16WE 20040206001702004020600170NM 2004 2 6 AWXA200400077 120040107A531190526912 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON FRAME FOOT AT BS 616, LBL 62. MAINTENANCE CUT OUT CRACK ON INNER CHORD FLANGE AT BS 616, LBL 62; PERFORMED HFEC INSPECTION TO VERIFY NO CRACK EXISTS; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20040206001712004020600171EA 2004 2 6 COMA0460077 120040122A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA17110 7158 LEFT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED DAMAGED 625 OBLIQUE ANGLE AND REPLACED WITH ANGLE P/N 601-35012-51 IAW BOMBARDIER CRJ 200 SRM 51-42-21. 2L72 4F RTA21EA 20040206001722004020600172EA 2004 2 6 COMA0460078 120040122A53116003603024 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA17110 7158 RIGHT SIDE FS 718.0 FRAME AND FRAME DOUBLER IS CRACKED. REMOVED CRACKED FRAME AND FRAME DOUBLER AND INSTALLED NEW FRAME P/N 600-36030-24-2 AND FRAME DOUBELR P/N 600-36030-32 IAW BOMBARDIER INC REO 601R-53-61-193 REV A. 2L72 4F RTA21EA 20040206001732004020600173NM 2004 2 6 QXEA200400059 120040122A2130 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM COCKPIT ILLUMINATED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09355PH 500 PDX - FLIGHT 2820 - CLIMBING OUT OF 10,00 FT, CABIN PRESS AND MASTER WARNING ILLUMINATED. THE APPROPRIATE CHECKS WERE RUN. MAINTENANCE INSPECTED THE AIRCRAFT AND THE PRESSURE CONTROL SYS. THE SYSTEM OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040206001742004020600174NM 2004 2 6 04FDEA00214 120040123A53306518385 SKIN BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 FUSELAGE SKIN BULGE AT STA 1163 STRINGER 18L & 19L. REMOVED CORROSION IAW SRM 51-10-6, FABRICATED & INSTALLED REPAIR DOUBLER IAW EA 7-5330-73867A. 2L73 4F RTA3WE 20040206001752004020600175NM 2004 2 6 04FDEA00216 120040124A532065163387 STIFFENER BOEING727 727100 1384036NM LT WHEEL WELL CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 LEFT WHEEL WELL BULKHEAD STA 950 LOWER -TEE CHORD IS CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 ON N/R N00126 WO 24581 AT MAE. 2L73 4F RTA3WE 20040206001782004020600178NM 2004 2 6 ABXA040042 120040124A3040 ELEMENT BOEING767 767231 1385131NM COCKPIT WINDOW DEFECTIVE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23702AX TX2260R 22566 CREW DETECTED A BURNING ELECTRICAL ODOR IN THE COCKPIT AFTER TAKEOFF. THE PROBABLE SOURCE WAS LOCATED BY OBSERVING A DISCOLORED/CHARRED AREA OF THE RT FORWARD WINDOW. LOWER RIGHT CORNER WHERE THE ELECTRICAL WIRING CONNECTS TO THE WINDOW HEAT ELEMENT. RIGHT FORWARD WINDOW HEAT SWITCH WAS SELECTED TO OFF AND ODOR DISSIPATED. REPLACED R1 WINDOW IAW B767 AMM 56-11-01-4. REPLACED TERMINAL LEAD TO THE WINDOW HEAT. OPS CHECKED GOOD IAW B767 MM 30-41-00-5. 2L72 4F RTA1NM 20040206001802004020600180NM 2004 2 6 2004UALA00041 120040118A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29540UA 25252 EXTERNAL FUSELAGE STA 600-620 HAS 3 DENTS OUT OF LIMITS BETWEEN STR 16L-17L. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING REPAIRED SKIN SPLICE. 2L72 4F4 FRTA2NM E17NE 20040206001822004020600182NM 2004 2 6 2004UALA00044 120040120A5230 DOOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO UNSECURE A UALAJA DUMP FUEL UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 WP29171UA 24322 AFTER TAKEOFF UNABLE TO PRESSURIZE A/C. EICAS CAUTION DOOR AFT CARGO ILLUMINATED. FOUND LATCH CAM MANUAL LOCK HITTING CAM ON AFT CARGO DOOR. RERIGGED LATCH CAM TO ALLOW FOR 0.06 INCH CLEARANCE. 2L74 4F4 FRTA20WE E24NE 20040206001862004020600186NM 2004 2 6 2004UALA00048 120040120A3260 PROXIMITY SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE MLG MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29545UA 25323 GEAR DISAGREE EICAS MESSAGE WITH THE GEAR HANDLE IN THE UP POSITION. AMBER CAUTION LIGHT ILLUMINATED. THE CAUSE WAS A GEAR POSITION PROXIMITY SENSOR. MAINTENANCE JACKED THE AIRCRAFT AND CLEANED MULTIPLE PROXIMITY SENSOR TARGETS. 2L72 4F4 FRTA2NM E17NE 20040206001892004020600189NM 2004 2 6 2004UALA00052 120040115A5740113W721224 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE RT AIL ACT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29778UA 26940 INBOARD AND OUTBOARD ACTUATOR FITTINGS CRACKED. REPLACED ACTUATOR FITTINGS. 2L72 4F4 FRTT0001SE E46NE 20040206001912004020600191NM 2004 2 6 2004UALA00054 120040106A5754114W426011 WEDGE BOEING BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29774UA 0002 26936 T/E WEDGE DELAMINATED AND DENTED. REMOVED, REPAIRED AND REINSTALLED. 2L72 4F4 FRTT0001SE E46NE 20040206001932004020600193NM 2004 2 6 2004UALA00056 120040122A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 FUSELAGE BS 600L, STRINGER 14L-19L SKIN DENTED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040206001952004020600195NM 2004 2 6 AALA20040130 120040126A3350 MODULE BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21756AM 30264 FORWARD ECONOMY CLASS ESCAPE PATH LIGHTING INOPERATIVE. REPLACED LIGHT ASSEMBLY AT 3R LAV AND MODULE 33404. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040206001972004020600197NM 2004 2 6 AALA20040132 120040125A3350 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHTSLOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 SFO EMERGENCLY LIGHTS AT SEATS 22A THROUGH 36A INOPERATIVE. REPAIRED LOOSE CONNECTION FOR EMERGENCY LIGHTS AT SEATS 22A THROUGH 36A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040206001992004020600199EA 2004 2 6 HNAA0400006 120040125A3220 LANDING GEAR DHAV DHC8 DHC8311 1386006EA NOSE FROZEN A HNAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA07335EN 375 LOUD NOISE HEARD COMING FROM NOSE AREA DURING TAKEOFF AND CLIMBOUT. SUSPECT LARGE ACCUMULATION OF SNOW AND ICE ON NOSE GEAR AND DOORS. DEICED GEAR AND INSPECTED FOR DAMAGE AND SECURITY, NO DEFECTS NOTED. AIRCRAFT FOUND SATISFACTORY DURING EVALUATION FLIGHT. 2H72 4T RTA13NM 20040206002002004020600200NE 2004 2 6 HNAA0400007 220040125A7200 ENGINE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 2 SURGES A HNAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA07343EN 340 AFTER AUTOFEATHER WAS SELECTED IT DID NOT INITIALLY ARM DURING TAKEOFF ROLL. WHEN IT DID ARM, IT CAUSED NR 2 ENGINE TO SURGE UNCOMMANDED. GROUND RAN AIRCRAFT AND PERFORMED AUTOFEATHER AND STATIC TEST WITH NO DEFECTS NOTED. PERFORMED POWER RUN AND CONFIRMED AUTO FEATHER ARMING AT APPROXIMATELY 70 PERCENT TORQUE NUMEROUS TIMES WITH NO SURGING NOTED. 2H72 4T4 TRTA13NM E20NE 20040206002022004020600202EA 2004 2 6 COMA0460081 120040125A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01719CA 7253 FLIGHT 5201 LEFT ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED SYSTEM AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20040206002042004020600204EA 2004 2 6 COMA0460083 120040123A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01934CA 7042 FLIGHT 5749 FLAPS FAIL CAUTION MESSAGE. C/W INSPECTION OF FLAP SYSTEM PER EO 27-046 AD. 2L72 4F RTA21EA 20040206002052004020600205EA 2004 2 6 COMA0460084 120040122A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS FALSE ACTIVATIONA COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01506CA 7793 FLIGHT 5305 SPOILER FAULT STATUS MESSAGE. COULD NOT DUPLICATE. RESET SYSTEM, OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040206002062004020600206NE 2004 2 6 F3LA200400001 220040125A7230 FAN BLADE AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE NR 2 ENGINE BENT A F3LAA UNSCHED LANDING C F.O.D. CLCLIMB 1 NM03910FR 1761 575447 DURING CLIMBOUT, FLIGHT CREW REPORTED ABNORMAL NR 2 ENGINE NOISE (NO ABNORMAL ENGINE VIBRATION). FOUND FAN BLADES BENT DUE TO ICE INGESTION. REPLACED NR 2 ENGINE FAN BLADES PER MM 72-21-00-300-028, PERFORMED NR 2 ENGINE TRIM BALANCE PER MM 77-32-34-750-001 AND CHECKED NORMAL. 2L72 4F4 FRTA28NM E2GL 20040204002292004020400229NE 2004 2 4 WRLA200408 220040123A723054A821 FAN BLADE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 1 ENGINE SHINGLED A WRLAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SO11278WL 48746 723956 ENGINE 1 VIBRATION HIGH ALERT DISPLAYED ON TAKEOFF, ABORTED TAKEOFF AT 15 KNOTS. INSPECTED NR 1 ENGINE IAW FIM 77-32-01 FOUND FAN BLADES SHINGLED, FREED BLADES, NO DAMAGE NOTED, LUBED FAN SHROUDS AND ROOTS. OPS CHECKED GOOD ON GROUND RUN. 2L73 4F4 FRTA22WE E24NE 20040205000722004020500072EA 2004 2 5 ASOA04006 120040104A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SEAL CRACKED A ASOAO OTHER O OTHER CRCRUISE 1 SO11856AS 7404 FLT 4308 - DURING FLIGHT FROM CLT-ATL, THE FILGHT ATTENDANT NOTICED AN AIR RUSH ON THE TOP LEFT CORNER OF THE PASSENGER DOOR. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REPAIRED THE PASSENGER DOOR SEAL STRIKER IAW ASA EO 600-52-0008C. (M) 2L72 4F RTA21EA 20040205000742004020500074EA 2004 2 5 ASOA04007 120040104A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11712EV 10074 FLT 4199 - DURING A GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY CEILING LIGHT AT ROW SEVENTEEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY CEILING LIGHT LAMP AT ROW SEVENTEEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040206001162004020600116WP 2004 2 6 DHL2004806541 120040112A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER FUSELAGE EXTERIOR SKIN WITH 1.000 CRACK IN IT (STA 1742.000-1743.000, L-16R TO L-17R), MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7, SRM 53-5-3 FIG 1. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN AREA AND FABRICATED FILLER (7075-T6AL 0.00.063), FINGER DOUBLER (7075-T6AL 0.040) AND DOUBLER (7075-T6AL 0.071) IAW SRM 53-2-1 FIG 7, SRM 53-5-3 FIG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 53-2-1 FIG 1, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040206001202004020600120NM 2004 2 6 HNAA0400004 120040113A533085330024 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07931HA4014540145 132 R/S UNDERFLOOR STR 27 BETWEEN REAR SPAR FRAME AND X467 WAFFLE DOUBLER IS DEPARTING SKIN PANEL. 2H72 4T RTA13NM 20040206001222004020600122NM 2004 2 6 ABXA040040 120040124A3350BPS73 BATTERY PACK BOEING767 767281 1385109NM EMERGENCY LIGHT WEAK A ABXAK NONE O OTHER ININSP/MAINT 1 GL23785AX 23018 SPARE BATTERY PACK WOULD NOT OPERATE THE COCKPIT EMERGENCY LIGHTS. REPLACED SPARE EMERGENCY LIGHT BATTERY AND POWER SUPPLY. SYSTEM OPS CHECKED GOOD IAW B767 MM 33-51-00 AND A CHECK (B767-3A) ITEM 3 AND 27. 2L72 4F RTA1NM 20040206001272004020600127NE 2004 2 6 NACA20040007 220040124A8530356996 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE FAILED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA541 541 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. REPLACED NR 4 ENGINE, NR 11 CYLINDER DUE TO NO COMPRESSION. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040206001292004020600129EU 2004 2 6 DHL2004365504 120040105A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH MAIN CABIN SEAT TRACK BETWEEN FR22 AND FR20 HAS CORROSION AREA RBL 36. REMOVED CORROSION AT MAIN CARGO SEAT TRACK FR20 APPROX 36 INCHES OF RBL, MATL LOST .030 INCH. FOUND OUT OF LIMITS AS PER A300 SRM 53-10-00 FIG 612 & 51-40-11. REMOVED CABIN SEAT TRACK FROM 18.5 FRAME TO 26.5 FRAME RBL 36 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK P/N 7075-T6-511, TMS 60-224457 FROM 18.5 FRAME TO 26.5 FRAME RBL 36 AS PER A300 SRM 53-10-00, 51-40-11, 51-10-40, 51-40-12, 51-30-30, PO 23488101. 2L72 4F RTA35EU 20040206001342004020600134NM 2004 2 6 VNAA0401006 120040110A7900 SHIM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE OIL PRESS REG FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07459PS 3070 DURING FLIGHT, THE CREW RECEIVED A LEFT HAND OIL PRESSURE HIGH INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REMOVED A SHIM FROM THE LEFT HAND OIL PRESSURE REGULATOR IN ACCORDANCE WITH DOENIER MAINTENANCE MANUAL 79-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001362004020600136NM 2004 2 6 VNAA0401001 120040102A3350501122803 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07432JS20095356 3045 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WILL NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001412004020600141NM 2004 2 6 VNAA0401008 120040119A3060 TERMINAL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE DIRTY LOOSE A VNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL07441JS 3059 DURING FLIGHT, THE CREW RECEIVED A LT PROPELLER HEAT FAIL BOTH MODES AND RETURNED TO PIT. MAINTENANCE CLEANED SLIP RING AND TIGHTENED TERMINAL ENDS ON BRUSH BLOCK IN ACCORDANCE WITH DORNER MAINTENANCE MANUAL 30-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001432004020600143EU 2004 2 6 DHL2004365509 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH SEAT TRACK BETWEEN FR20 & FR21 APPROX RBL 58 EVIDENCE OF CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS AT SEAT TRACK FLANGES FR20 & FR21 APPROX RBL 58 AS PER A300 SRM 53-10-00 MATL LOSS .030 INCH CORROSION REMOVAL REF A300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR18.5 TO 26.5 RBL 58 AT MAIN CARGO AS PER A300 SRM 53-10-00/51-10-40/51-40-12. MATERIAL USED TMS 60-224457 A 532-74005D 7075T6511, PO 23488101. 2L72 4F RTA35EU 20040206001672004020600167NM 2004 2 6 AWXA200400074 120040109A5320655287415 WEB BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON L-2 DOOR FRAME SURROUND WEB AT BS 948, LBL 62, WL 251. MAINTENANCE REMOVED CRACKED L-2 DOOR FRAME SURROUND WEB AT BS 948, LBL 62, WL 251; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-52874-15; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 14, SHT 1. 2L72 4F RTA16WE 20040206001852004020600185NM 2004 2 6 2004UALA00047 120040109A5754114T411419 WEDGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 4 SLAT DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29642UA 25092 T/E WEDGE DENTED ON UPPER SURFACE OF NR 4 SLAT. MAJOR REPAIR. REPLACED WITH NEW T/E WEDGE. 2L72 4F4 FRTA1NM E24NE 20040206001872004020600187NM 2004 2 6 2004UALA00049 120040122A335020131 BATTERY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29649UA 25286 EMERGENCY EXIT PATH LIGHTS ROW 15-17 BLINK ON AND OFF. REPLACED M737 BATTERY ASSEMBLY. 2L72 4F4 FRTA1NM E24NE 20040206002072004020600207EA 2004 2 6 COMA0460085 120040122A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA FAILED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01491CA 7756 FLIGHT 5341 FLAPS FAILED AT 0 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040206002092004020600209EA 2004 2 6 COMA0460087 120040122A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01914CA 7012 FLIGHT 5825 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040206002112004020600211NM 2004 2 6 F3LA200400002 120040124A3260 INDICATOR BOEING737 73736E 138443ANM MLG MALFUNCTIONED A F3LAO OTHER N FALSE WARNING APAPPROACH 1 NM03317FL 25263 ON APPROACH INTO DEN, FLIGHT CREW REPORTED GREEN INDICATION LIGHT DID NOT ILLUMINATE WITH LANDING GEAR DOWN. VISUALLY CONFIRMED LANDING GEAR DOWN AND LOCKED. LANDED WITHOUT INCIDENT. PERFORMED INSPECTION/TEST OF LANDING GEAR POSITION WARNING IND. NO DEFECTS NOTED PER MM 32-61-00. 2L72 4F RTA16WE 20040206002132004020600213SO 2004 2 6 C2XA04CL005 120040122A3320BR90002 BALLAST EMB 145 EMB145ER 3260211SO CABIN LIGHT FAULTY A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2716927 145006 YUL FLIGHT 2847 THE CREW REPORTED SMOKE IN CABIN FROM PSU 11/12A. MAINTENANCE INSPECTED AND REPLACED THE CABIN LIGHT BALLAST AT 12A. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040206002162004020600216EA 2004 2 6 MASA200400040 120040121A3350 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775991 7422 ASH 2757 PHL, CREW REPORTED THE FWD EMERGENCY LIGHT FLOOR STRIP WAS INOP. MX RESECURED AND RECONNECTED THE LIGHT STRIP. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040206002172004020600217EA 2004 2 6 MASA200400041 120040122A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 ASH 6110 PHX, CREW REPORTED THAT ROW 1 EMERGENCY LIGHTING STRIP SECTION INOP. MX RESECURED AND RECONNECTED THE EMERGENCY LIGHTING STRIP. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040206002182004020600218EA 2004 2 6 MASA200400046 120040126A3397 SPLICE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 ASH 6150 PHX-SBA, FLOOR EMERGENCY PATHWAY LIGHTING WAS INOP. MX REPAIRED A LOOSE SPLICE. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040206002192004020600219SO 2004 2 6 C2XA04BT011 120040126A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714902 145496 DURING 4A INSPECTION MAINTENANCE FOUND ROW 3 OVERHEAD CENTER AISLE EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LAMP IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040206002202004020600220EU 2004 2 6 AWXA200400081 120040111A5270DHE1141 PROXIMITY SWITCH AIRBUS320 A320231 3930325EU L-2 DOOR FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28627AW 66 MCN - EES - DURING C-03 CHECK THE L-2 DOOR SLIDE ARMED LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ARM LIGHT PROXIMITY SWITCH, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040206002212004020600221NE 2004 2 6 AWXA200400082 220040126A7532AC69572 BLEED VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28656AW1660711825 1079 ON CLIMBOUT, ECAM INDICATED NR 2 ENG STALL, A/C SHUDDERED, A LOUD THUMP HEARD, & LT WING DIPPED, NO ABNORMAL ENG READING INDICATIONS NOTED. TURNED BACK & LANDED WITHOUT EVENT. MAINT TROUBLESHOT IAW TSM. R & R 7TH STAGE BLEED VALVE IAW AMM, & 7TH STAGE BLEED SOLENOID VALVE IAW AMM. ALSO TIGHTENED UNIONS ON 10TH STAGE BLEED SOLENOID VALVE, OPERATIONAL CHECK WAS GOOD PER AWA T/C F5M71312. CHECK OF BLEED SOLENOID VALVE CONFIRMED FAILURE OF UNIT, VALVE WOULD NOT OPERATE. DISASSY REVEALED PISTON SEALS & PLUNGER WORN BEYOND LIMITS. REPLACED PISTON, PLUNGER, SEALS, RING, & SHIMS. UNIT OVERHAULED & TESTED IAW CMM 75-32-51. VENDOR ALSO CONFIRMED FAILURE OF 7TH STAGE BLEED VALVE FOR NOT OPERATING WITHIN MANUFACTURERS2L72 4F4 FRTA28NM E40NE 20040206002302004020600230NM 2004 2 6 AWXA200400091 120040108A531365516982 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER 4 RT AT BS 867. MAINTENANCE REMOVED DAMAGED SECTION OF STRINGER 4 RT AT BS 867; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 203 PG 214-216. 2L72 4F RTA16WE 20040206002322004020600232WP 2004 2 6 DHL2004802002 120040125A2821 FUEL FILTER DOUG DC8 DC873 302199CWP GE CFM56 CFM562C1 13802NE NR 1 ENGINE CONTAMINATED A DHLAO OTHER J WARNING INDICATION DEDESCENT 1 SO01802DH 46076 692548 FUEL BYPASS LIGHT ILLUMINATED ON NR 1 ENGINE. PERFORMED ABNORMAL PROCEDURE, LIGHT DID NOT EXTINGUISH. ENGINE PARAMETERS NORMAL. CLEARED DESCENDING THRU 15,000. INSPECTED NR 1 ENGINE FUEL FILTER. FOUND SMALL NON-METALLIC DEBRIS. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER IAW CFM M/M 73-11-10. PERFORMED ENGINE RUN IDLE/FLIGHT IDLE CHECK PER JRH 13.2. OPS AND LEAK CHECKED GOOD. BYPASS LIGHT OPS GOOD. 2L74 4F4 FRT4A25 E2GL 20040206002372004020600237NM 2004 2 6 DHL2004749002 120040124A3040 CONTROL UNIT BOEING727 727200 138407ENM WINDOW HEAT MALFUNCTIONED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01749DH 22013 R2 WINDOW CRACKED. COMPLETED ABNORMAL PROCEDURE. REMOVED AND REPLACED RIGHT NR 2 WINDOW HEAT CONTROL UNIT. OPS CHECKED GOOD IAW 30-41-12. REPLACED R2 WINDOW, HEATING ELEMENT SHORTED OUT REPAIRED R2 WINDOW OPS CHECKED GOOD IAW 56-12-11. 2L73 4F RTA3WE 20040209000012004020900001EU 2004 2 9 DHL2004363002 120040126A2750 GEARBOX AIRBUS300 A300B4203 3930306EU TE FLAPS MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01363DH 85 ON APPROACH, FLAPS DID NOT EXTEND WITH FL 8 SELECTED. PERFORMED ABNORMAL PROCEDURE LANDED SL16/FL 0. ON TOUCHDOWN, FLAPS EXTENDED TO 8 DEGREES. CHECKED SERVICING ON THE FLAP CONTROL UNIT, DUPLEX AND SIMPLEX BEVEL GEARBOXES, TORQUE LIMITERS, DOWN DRIVE GEARBOXES, AND FLAP TEE GEARBOXES AS PER M/M 12-13-27. ALL GEARBOXES SERVICED NORMALLY. OPERATED FLAPS PER M/M 27-50-00. FLAPS OPERATE NORMALLY. 2L72 4F RTA35EU 20040209000042004020900004SO 2004 2 9 RAIA00401016 120040116A2923MPEV30086 PUMP EMB 145 EMB145LR 3260212SO HYD SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03832HK160 145771 8000-STL- LEFT ELECTRIC HYDRAULIC PUMP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 ELECTRIC HYD PUMP. 2L72 4T RTT00011AT 20040209000062004020900006SO 2004 2 9 RAIA00401018 120040120A2131 LINE EMB 145 EMB145LR 3260212SO PRESS CONTROLLERLOOSE A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03832HK 145771 AUTO AND MANUAL PRESSURIZATION INOP. MAINTENANCE SECURED LOOSE LINE IN PRESSURIZATION CONTROLLER. 2L72 4T RTT00011AT 20040209000072004020900007SO 2004 2 9 RAIA00401019 120040115A5320 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK7614 145256 DURING BLOCK CHECK FOUND SERVICE DOOR SILL PLATE CORROSION BEYOND BENDABLE LIMIT. MAINTENANCE REPAIRED SILL PLATE IAW EMB GST-1927/02A. 2L72 4T RTT00011AT 20040209000082004020900008SO 2004 2 9 RAIA00401020 120040115A5315 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK7614 145256 MX-STL- LEFT FLOORBEAM AT FRAME 20 CORRODED BEYOND BLENDABLE LIMITS. REPAIRED LT FLOORBEAM AT FRAME 20 IAW EMB 145 SRM 53-21-10. 2L72 4T RTT00011AT 20040209000112004020900011SO 2004 2 9 RAIA00401023 120040124A4920 APU EMB 145 EMB145LR 3260212SO APU BAY CONTAMINATED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03812HK 145373 5255-PIT- SMOKE IN FLIGHT DECK AREA. MAINTENANCE DISCOVERED APU HAD INGESTED GLYCOL AND DEFERRED APU BLEED. 2L72 4T RTT00011AT 20040209000132004020900013 2004 2 9 RAIA00401025 420040125A34207012100811 RMU JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03566HK168833172 41084 5524-STL- LEFT RMU FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 RMU. 2L72 4T RTA41NM 20040209000172004020900017 2004 2 9 371PA0035 420040123A2230735SUE1012 COMPUTER BOEING737 737306 13844BGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER CLCLIMB 1 SO05371PA 23543 AUTOTHROTTLE DISENGAGES ON TAKEOFF AND CLIMB. PLACED AUTOTHROTTLE ON MEL 22-4. REPLACED AUTOTHROTTLE COMPUTER PER MM 22-30-10. TESTS SATISFACTORY. 2L72 4F RTA16NE 20040209000182004020900018NM 2004 2 9 374PA0006 120040124A2781 WARNING HORN BOEING737 73736M 138443BNM COCKPIT FALSE ACTIVATIONA PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05374PA 28333 WARNING HORN ON TAKEOFF ROLL. NO LEADING EDGE FLAP/SLAT INDICATION. RESET LEADING EDGE POSITION INDICATOR CIRCUIT BREAKER. SYSTEM OPS CHECKS GOOD PER MM 27-88-00. 2L72 4F RTA16WE 20040209000192004020900019EU 2004 2 9 04FDEA00231 120040127A3230D221270005 DAMPER AIRBUS310 A310 EU MLG MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25428FE 248 AFTER T/O LANDING GEAR WOULD NOT RETRACT- TRIED BOTH SYSTEMS, FOLLOWED ECAM (270 SPEED WAS NOT EXCEEDED), FOLLOWED QRM, RETURNED. REMOVED LT GEAR PITCH DAMPER PER MM 32-11-15-4-01. INSTALLED NEW DAMPER THROUGH STEP 4 (B) (4). 2L72 4F RTA35EU 20040209000202004020900020WP 2004 2 9 04FDEA00230 120040128A3241 CONTROL UNIT DOUG DC10 DC1010 3022110WP ANTI SKID SYSTEMFAILED A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25361FE 48260 ON LANDING INTO FLL, PUT THE LANDING GEAR DOWN AND RECEIVED A LEVEL 2 ALERT, (ANTI-SKID RT FAIL). PERFORMED GO-AROUND TO COMPLETE ANTI-SKID FAILED CHECKLIST. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT. OPS CHECK GOOD AS PER MM CHAPTER 32-45-01-2. A/C OK FOR SERVICE. 2L73 4F A22WE 20040209000212004020900021WP 2004 2 9 04FDEA00229 120040128A3210 LANDING GEAR DOUG DC10 DC1010 3022110WP MAINS MALFUNCTIONED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO2568059 46907 ON INITIAL GEAR EXTENSION GEAR WOULD NOT COME DOWN AND LOCK. RECYCLED GEAR, EXTENSION NORMAL, ALL 3 DOWN AND LOCKED. INSPECTED GEAR, COULD NOT FIND ANY DEFECTS. A/C OK FOR SERVICE PER M/M 32-31-01 AND TAFI 32-30. 2L73 4F A22WE 20040209000222004020900022EU 2004 2 9 MALA040139 120040122A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 DURING FLIGHT 3489, GREEN SYSTEM HI TEMP LIGHT ILLUMINATED. GREEN HI TEMP CAME ON AT CRUISE PER QRH TURNED OFF THE PUMP HI TEMP LIGHT TURNED OFF AFTER 3 TO 4 MINUTES. AIR RETURN TO MSP. MAINTENANCE REMOVED & REPLACED NR 3 EDP P/N 521449, S/N OFF F9840491, S/N ON F9727550 IAW AMM 29-10-17, OPS AND LEAK CHECKS GOOD REF 409 194685 FOR DETAILS. 2H74 4F RTA49EU 20040209000242004020900024EU 2004 2 9 MALA040138 120040124A30107230100631 WATER TRAP SAAB SF340 340B 7860101EU DEICE SYSTEM CRACKED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15411XJ 340B411 DURING FLIGHT 2726, AFTER TAKEOFF THE DEICE TIMER LIGHT ILLUMINATED AND THE STAB WOULD NOT INDICATE INFLATION IN AUTO OR MANUAL. AIR RETURN TO MEM. MAINTENANCE FOUND RT DEICE WATER TRAP CRACKED. REMOVED AND REPLACED RT DEICE WATER TRAP ALL SYTSTEM TESTS OK IAW 30-10-00-5. 2L72 4T RTA52EU 20040209000262004020900026NM 2004 2 9 QXEA200400063 120040123A243023088002A GCU DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09352PH13239904 494 NR 1 DC GENERATOR CAUTION LIGHT CYCLING ON AND OFF. RAN CHECKLIST, TURNED NR 1 DC GENERATOR OFF WITH NO CHANGE. REMOVED AND REPLACED NR 1 DC GENERATOR CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209000282004020900028NM 2004 2 9 QXEA200400064 120040123A243096951 GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09352PH140695687 494 MFR- ON FLIGHT 2146 NR 1 DC GENERATOR CAUTION LIGHT BLINKING, MASTER CAUTION LIGHT, ANNUNCIATOR PANEL, PRESSURIZATION FAULT, TRANSPONDER LIGHTS BLINKING (LOOSING POWER, AUDIBLE TONE). RAN DC GENERATOR CHECKLIST. AFTER DC GENERATOR RESET EVERYTHING WAS THE SAME. TURNED DC GENERATOR OFF AND EVERYTHING STABILIZED. REMOVED AND REPLACED DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209000292004020900029NM 2004 2 9 QXEA200400065 120040125A7620 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE ILLUMINATED A QXEAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 NM09350PH 488 BOI FLIGHT 2196, NR 1 ENGINE MANUAL CAUTION ILLUMINATED. CHECKED ENGINE CONDITION PANEL. RESET BETA LOCKOUT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209000302004020900030WP 2004 2 9 AALA20040135 120040127A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21253AA 49286 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209000312004020900031NM 2004 2 9 AALA20040139 120040128A3350 BATTERY BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21679AN 29589 MIA AFT EMERGENCY PATH LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY FOR AFT EMERGENCY PATH LIGHT FOR ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040209000332004020900033NM 2004 2 9 AALA20040144 120040125A3350 LIGHT BOEING757 757223 1384957NM CABIN WRONG PART A AALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW21624AA 24582 DFW WRONG EMERGENCY LIGHT ASSEMBLY INSTALLED AT RIGHT HAND FORWARD ENTRY GALLEY WALL NEAR FLOOR. REPLACED RIGHT HAND EMERGENCY LIGHT ASSEMBLY AT FORWARD ENTRY GALLEY WALL NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040209000342004020900034NM 2004 2 9 AALA20040141 120040126A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21788AN 30011 DFW EMERGENCY PATH LIGHTS AT AFT GALLEY DIVIDER INOPERATIVE. REPLACED BATTERY PACK FOR AFT GALLEY DIVIDER LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040209000352004020900035NM 2004 2 9 AALA20040143 120040126A3397 WIRE HARNESS BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 MIA EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED WIRE ON HARNESS FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040209000412004020900041NM 2004 2 9 AALA20040127 120040125A5610141T480149 WINDSHIELD BOEING757 757223 1384957NM COCKPIT ARCED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21682AA 25339 DFW INFLIGHT T1477/25 PLUME OF HIGH SPEED SMOKE, SPARKS, AND SMOKE BLEW FROM LOWER LEFTHAND CORNER, FL310, OF CAPTAINS WINDSHIELD. WINDSHIELD CRACKED. RETURNED TO DFW. LANDED WITHOUT INCIDENT. REPLACED CAPTAINS WINDSHIELD AND WINDSHIELD HEAT CONTROLLER AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040209000422004020900042WP 2004 2 9 AALA20040136 120040127A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21253AA 49286 DFW AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR AFT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209000432004020900043 2004 2 9 UPS04141787 420040126A2565 SLIDE AIRBUS300 A300B4622R 3930312EU COCKPIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 INSPECTION TYPE:N/A DOOR SLIDE DIFFICULT TO ARM ON LAST 2 LEGS. CHECKED ESCAPE SLIDE ARM IAW MM 25-61-20-5, FOUND SATISFACTORY. LUBRICATED TELESCOPIC UNIT IAW MM 12-22-52, CHECKED OK. 2L72 4F RTA35EU 20040209000442004020900044WP 2004 2 9 UPS04841780 120040127A33975708458503 RELAY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS CAME ON WITH SWITCH IN ARM POSITION. C/B RESET, LIGHTS WENT OUT. EN ROUTE EMERGENCY EXIT LIGHTS CAME ON AGAIN. WOULD NOT RESET, DISARM LIGHT TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2, OPS CHECK GOOD. 2L74 4F RT4A25 20040209000452004020900045 2004 2 9 UPS04M41786 420040106A2565 SLIDE DOUG MD11 MD11F 3023600NM R1 DOOR WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01254UP INSPECTION TYPE:N/A R1 DOOR EVACUATION SLIDE PRESS TO TEST INOP DEFERRED M 273762 PER MEL 25-61-2 PLACARD. RELAMPED R1 DOOR SLIDE WARNING LIGHT MM 25-61-04. THIS CLEARS M 273762. 2L73 4F RTA22WE 20040209000462004020900046NM 2004 2 9 QXEA200400074 120040120A5230 HOUSING BOMBDRDHC8 DHC8401 1390041NM AFT CARGO DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX6214 4031 PDX - AFT BAGGAGE DOOR GUIDE ROLLER MOUNT HOUSINGS HAVE ONE INCH CRACKS ON THE BOTTOM WEBS. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT ROLLER GUIDE HOUSINGS. THE BRACKETS WERE REPLACED WITH NEW HARDWARE, SHIMMED FOR CORRECT FIT, AND A FUNCTIONAL CHECK WAS DONE. CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209000482004020900048NM 2004 2 9 CALA0400062 120040126A5321 FLOOR PANEL BOEING737 737824 13844BZNM FUSLAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716234 28946 INSPECTION FOUND FLOOR PANEL SPLICE BETWEEN 2ND AND 3RD FLOORBOARD CORRODED AT STA 727I. A NEW FLOOR PANEL SPLICE WAS INSTALLED IAW SRM 53-42-11. 2L72 4F RTA16WE 20040209000512004020900051NM 2004 2 9 CALA0400065 120040127A2913106047013 PUMP BOEING737 737524 1384721NM NR 1 ENGINE LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW271665016643 28911 THE A-HYDRAULIC SYSTEM QUANTITY AND PRESSURE BEGAN TO DROP WHILE CLIMBING THROUGH 24,000 FEET EN ROUTE FROM MDW TO EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-HYDRAULIC SYSTEM WARNING LIGHT. A MANUAL GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED PER OP NR 1 OF EA 2910-01325, REV D. OPERATIONAL AND LEAK CHECKS WERE GOOD. 2L72 4F RTA16WE 20040209000532004020900053CE 2004 2 9 029041 120040126A3246 BEARING BEECH 1900 1900D 1154162CE ZONE 700 FROZEN A NSVAO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 EA27171CJ312 UE71 NR 3 MAIN WHEEL ASSY DEPARTED AIRCRAFT ON TAKEOFF, AIRCRAFT LANDED WITHOUT INCIDENT. WHEEL RECOVERED AT AIRPORT. PROBABLE CAUSE WAS BEARING FAILURE. 2L72 4T RTA24CE 20040209000542004020900054EU 2004 2 9 AWXA200400093 120040127A2560P20700012015 FLASHLIGHT AIRBUS320 A320231 3930325EU ZONE 900 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 SEA - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040209000562004020900056NM 2004 2 9 AWXA200400095 120040127A3150285T025919 CIRCUIT CARD BOEING757 7572S7 1384962NM E/E RACK FAULTY A AWXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP28901AW 23321 BWI - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF AT PHX EN ROUTE FOR BWI TAKEOFF WARNING HORN SOUNDED AND RED STABILIZER EICAS MESSAGE WAS DISPLAYED, REJECTED TAKEOFF BELOW 10 KTS, STAB TRIM WAS AT 4.5. MAINTENANCE COMPLIED WITH FAULT ISOLATION MANUAL 31-51-00, REMOVED AND REPLACED M620 TAKEOFF CONFIGURATION CIRCUIT CARD MODULE IAW BMM 31-51-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040209000582004020900058NM 2004 2 9 AWXA200400097 120040107A53156545834252 FLOORBEAM BOEING737 737301 138447RNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 296, LBL 11, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM BS 296, LBL 11, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8, PG 1 & 38. 2L72 4F RTA16WE 20040209000592004020900059NM 2004 2 9 AWXA200400098 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK .1875 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 10 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, PG 3 - 5, 10 & 38. 2L72 4F RTA16WE 20040209000642004020900064NM 2004 2 9 AWXA200400103 120040107A531065317875 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF UPPER LEG ON UPPER FRAME AT L-1 DOOR WAY BS 315-340, LBL 59, WL 209. MAINTENANCE REMOVED CORRODED UPPER FRAME AT L-1 DOOR WAY FROM BS 315 TO BS 350, LBL 59, WL 209; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2L72 4F RTA16WE 20040209000662004020900066NM 2004 2 9 AWXA200400105 120040107A5320655964423 SPLICE BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE AT BS 361, STR 26 RT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 361, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-59644; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 PG 26-28. 2L72 4F RTA16WE 20040209000672004020900067NM 2004 2 9 AWXA200400106 120040107A53206559644501 SPLICE BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 353 AND BS 366, STR 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE BETWEEN BS 353 AND BS 366, STR 27 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-59644; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 PG 1, 26 & 28. 2L72 4F RTA16WE 20040209000682004020900068NM 2004 2 9 AWXA200400107 120040108A532065C10592154 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF UPPER LEG ON FLOOR SUPPORT BETWEEN BS 951 AND BS 963, LBL 42. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BETWEEN BS 951 AND BS 963, LBL 42; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592-154; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2L72 4F RTA16WE 20040209000702004020900070NM 2004 2 9 QXEA200400075 120040125A6120 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM AUTOFX MALFUNCTIONED A QXEAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NM09412QX 4059 SEA-ON FLIGHT NUMBER 2340, ON TAKEOFF ROLL WITH POWER AT TAKEOFF TORQUE WITH AUTOFX IN "SELECT". DID NOT GET AN ARM LIGHT. ABORTED TAKEOFF AT 60 KTS. PERFORMED OPERATIONS TEST OF AUTOFX AND UPTRIM SYSTEM. AUTOFX TEST CHECKED GOOD. NO FAULT CODES. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209000732004020900073SO 2004 2 9 C2XA04SH031 120040128A531014525480003 BEAM EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV-DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040209000742004020900074NM 2004 2 9 DHL2004750005 120040129A3350 LIGHT BOEING727 7272M7 138407SNM CABIN ILLUMINATED A DHLAO OTHER O OTHER LDLANDING 1 SO01750DH 21951 EMERGENCY EXIT LIGHTS IN COCKPIT ILLUMINATES ON TOUCHDOWN, EVEN GENTLE ONES. RESECURED EMERGENCY EXIT LIGHT IN COCKPIT IAW B-727 M/M 33-50-101. OPS CHECKED GOOD. 2L73 4F A3WE 20040209000762004020900076NM 2004 2 9 DHL2004753508 120040102A575465173104 FRAME BOEING727 727223 1384074NM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 NR 2 SLAT OUTBOARD FRAME AT ACT ROD END ATTACH HAS THE FWD LOWER CORNER CRACKED. REMOVED NR 2 SLAT ASSY FOR S/M REPAIR IAW B727 M/M 27-81-11. REMOVED INT ACCESS PNL & 3 RIBS AT O/B FRAME AT ACT IAW B727 SRM 51-30-2. DRILLED NEW HOLES AT RIB'S P/N 65-17310-4 / 65-17310-3, PO 342177, 3421124, AND P/N 65311-3 PO 3421112 IAW B727 SRM 51-30.5. TREATED RIBS IAW B727 SRM 51-10-2. INSTALLED NEW RIBS AT NR 2 SLAT (3 PLACES) IAW B727 SRM 51-30-2. INSTALLED INNER SKIN PNLS AT +2 SLAT IAW B727 SRM 51-30-2. REINSTALLED INT ACCESS PNL AT 2 SLAT IAW B727 SRM 51-30-2. REINSTALLED NR 2 SLAT IAW B727 MM 27-81-11, OP CHECK GOOD IAW B727 MM 27-81-0. 2L73 4F A3WE 20040209000782004020900078NM 2004 2 9 AWXA200400109 120040128A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28830AW 1565 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040209000812004020900081NM 2004 2 9 AWXA200400112 120040107A53206545410 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON LONGITUDINAL FLOOR SUPPORT WEB BETWEEN BS 708 AND BS 709, RBL 24.75. MAINTENANCE TRIMMED OUT DAMAGE ON FLOOR SUPPORT WEB BETWEEN BS 708 AND BS 709, RBL 24.75; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5715-04023-ES4. 2L72 4F RTA16WE 20040209000822004020900082NM 2004 2 9 AWXA200400113 120040121A532069366569 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK 3 EACH CRACKS WERE FOUND IN UPPER LEG OF INTERCOSTAL BETWEEN BS 932 AND BS 940, BL 0, WL 208. MAINTENANCE REMOVED UPPER LEG OF INTERCOSTAL BETWEEN BS 932 AND BS 940, BL 0; FABRICATED A NEW REPLACEMENT UPPER LEG PER DWG 69-36656; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20040209000832004020900083NM 2004 2 9 AWXA200400114 120040119A531165C257237 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK A .75 INCH CRACK WAS FOUND IN FRAME AT BS 616, LBL 64, WL 202. MAINTENANCE CUT OUT DAMAGED AREA OF FRAME CHORD AT BS 616, LBL 64, WL 202; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENER ANGLE AND CHORD FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20040209000842004020900084NM 2004 2 9 AWXA200400115 120040121A532065C333672 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT (INTERCOSTAL) BETWEEN BS 950 AND BS 959, RBL 46, WL 208. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BETWEEN BS 950 AND BS 959, RBL 46, WL 208; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER 65C33367; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20040209000852004020900085NM 2004 2 9 AWXA200400116 120040120A53116546539 FRAME BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND IN FRAME AT LOWER END UNDER CREASE BEAM AT BS 616, STR 17 RT, RBL 65, WL 208.1. MAINTENANCE CUT OUT DAMAGE ON INBOARD FRAME LOWER LEG AT BS 616, STR 17 RT, RBL 65, WL 208.1; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENER ANGLE AND CHORD FILLER; INSTALLED REPAIR PARTS IAW AWA ER 15-5311-01143-DD2. 2L72 4F RTA16WE 20040209000862004020900086NM 2004 2 9 AWXA200400117 120040122A531265171583 BULKHEAD BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 228. MAINTENANCE STOP DRILLED CRACK IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 228; PERFORMED A HFEC INSPECTION TO VERIFY CRACKS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-1-0-11 FIG 11 PG 1. 2L72 4F RTA16WE 20040209000872004020900087NM 2004 2 9 AWXA200400118 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500D, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500D, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2L72 4F RTA16WE 20040209000902004020900090CE 2004 2 9 AMWA111 120040102A54121299100345 FIREWALL BEECH 1900 1900D 1154162CE RT ENG NACELLE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07138ZV UE138 DURING INSPECTION RT ENGINE FIRE WALL WAS FOUND CRACKED AROUND THE O/B SECTION OF WEB APPROX AT 5 INCHES LONG IN VERT POSITION. BEHIND ATTACH ANGLE FOR COWLING. THEN CRACK TURNS HORIZONTAL GOING I/B APPROX 2.5. REPAIRED DAMAGE AREA BY STOP DRILLING CRACK ENDS AND INSTALLING DOUBLER PER BEECH SRM 51-70-17. 2L72 4T RTA24CE 20040209000952004020900095SO 2004 2 9 SWIA200412798 120040121A612078249046 PCU EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 NM07221SW6419 1977 120290 ON FINAL APPROACH APPROX 1000 FT LEFT ENGINE AUTOFEATHERED. CONTINUED APPROACH LEFT ENGINE SEEMED TO CYCLE OUT OF FEATHER AND THEN BACK INTO FEATHER. UPON LANDING, ALL PARAMETERS APPEARED NORMAL. REPLACED LEFT ENGINE PCU AND RELAY K0162 PER MM 61-21-00. OPS CHECKED GOOD IAW 61-00-00 TABLE 202. 2L72 4T4 TRTA31SO E20NE 20040209000972004020900097SO 2004 2 9 SWIA200412800 120040112A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07292UX4391 4391 120292 AFTER TAKEOFF DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD FLAPS. CYCLED FLAPS PER THE QRH, DISAGREEMENT REMAINED. OVERHEAD PANEL INDICATED OUTBOARDS STUCK AT 2 SEGMENT BARS. REPLACED FLAP SELECTOR WITH SERVICEABLE UNIT. CLEANED AND LUBED FLAP TRACKS. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040209000982004020900098 2004 2 9 SWIA200412801 420040114A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTO PILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07233SW8194 8194 120307 AFTER LANDING, AUTOPILOT KEPT RE-ENGAGING ITSELF, WOULD RE-ENGAGE ON BOTH SIDES REPEATEDLY. REPLACED AUTOPILOT CONTROL PANEL. OPS CHECK GOOD ON BOTH SIDE AUTOPILOT. 2L72 4T RTA31SO 20040209001002004020900100EA 2004 2 9 SWIA200412803 120040104A2750855D1007 SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07406SW 7030 ON CLIMBOUT FROM GTF, FLAPS FAIL CAUTION MESSAGE ILLUMINATED AT FLAPS 0. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20040209001012004020900101SO 2004 2 9 SWIA200412804 120040107A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07233SW1925 1925 120307 CONTROL FAULT WHEN FLAPS SELECTED FROM 25 DEGREES TO 45 DEGREES WITH NO COMMAND BARS. REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040206001422004020600142NM 2004 2 6 VNAA0401010 120040121A27418409 ACTUATOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE PITCH TRIM FAILED A VNAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL07429JS6269 3043 DURING FLIGHT CREW RECEIVED A PITCH TRIM ASSYM CAS MESSAGE. AIRCRAFT RETURNED TO PHL. MAINTENANCE INSPECTED AND CHANGED THE LT AND RT ELEVATOR TRIM ACTUATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE DONE ACCORDING TO DORNIER MAINTENANCE MANUAL 27-00-00. AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040206001522004020600152EA 2004 2 6 COMA0460075 120040122A53206003603031 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA17110 7158 LT FS 718, STR 10-11 LT. REMOVED CRACKED DOUBLER AND INSTALLED NEW DOUBLER IAW BOMBARDIER REO 601R-53-61-243. 2L72 4F RTA21EA 20040206001622004020600162NM 2004 2 6 AWXA200400069 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500C, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500C, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2L72 4F RTA16WE 20040206001642004020600164NM 2004 2 6 AWXA200400071 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727B, STR 7 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 7 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2L72 4F RTA16WE 20040206001662004020600166NM 2004 2 6 AWXA200400073 120040107A5340653535214 STRINGER CLIP BOEING737 737301 1384611NM FUSLAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .4375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 380, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 380, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 65-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2L72 4F RTA16WE 20040206001692004020600169NM 2004 2 6 AWXA200400076 120040107A5313654988630 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER 16 RT, 5 INCHES FORWARD OF FRAME 500D. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 RT, BS 500D; FABRICATED A CHANNEL, RADIUS FILLER, AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2L72 4F RTA16WE 20040206001762004020600176NM 2004 2 6 04FDEA00217 120040125A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RT FLOORBEAM 53.5 INCHES FROM CENTER LINE HAS EVIDENCE OF CORROSION. RT DAMAGED FLOOR SUPPORT STA 1891TO STA 2007, 53.5 INCHES FROM CENTER LINE REMOVED AS PER PER MM 20-50-02. FABRICATED AS PER DWG NR AGA7551. FABRICATED SUPPORT INSTALLED AS PER MM 20-20-02 2L73 4F RTA22WE 20040206001772004020600177NM 2004 2 6 ABXA040041 120040124A2120 ODOR BOEING767 767231 1385131NM COCKPIT DETECTED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23702AX 22566 UNUSUAL ODOR IN COCKPIT. STRONGEST IN FOOT WELLS. NO NOTICABLE ODOR AFT OF COCKPIT DOOR. RAN APU AND PACKS, STILL NO ODOR. INSPECTED COCKPIT AND FOUND NOTHING OUT OF ORDINARY. 2L72 4F RTA1NM 20040206001792004020600179NM 2004 2 6 2004UALA00040 120040118A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29540UA 25252 BS 620 AT STR 18L-19L, SHEAR TIE CRACKED ON BOTH ENDS. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20040206001812004020600181NM 2004 2 6 2004UALA00043 120040119A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29382UA 24657 STRINGER CLIPS AT STA 616 STR 4R, AT STA 616 STR 1L AND STA 500 STR 15R ARE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIPS. 2L72 4F4 FRTA16WE E2GL 20040206001842004020600184EU 2004 2 6 2004UALA00046 120040121A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29409UA 462 STRINGER 43L CORRODED BETWEEN FRAMES 56 AND 57. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED STRINGER SECTION. FABRICATED & INSTALLED NESTED STRINGER SPLICE REPAIR PER SRM 53-0013 FIG 201. 2L72 4F4 FRTA28NM E40NE 20040206002012004020600201EA 2004 2 6 COMA0460080 120040125A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01954CA 7100 FLIGHT 5792 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040206002032004020600203EA 2004 2 6 COMA0460082 120040123A5210 BOLT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01409CA 7441 FLIGHT 5103 CABIN DOOR OUTER HANDLE CAUTION. ADJUSTED INNER HANDLE STOP BOLT. 2L72 4F RTA21EA 20040206002222004020600222NM 2004 2 6 AWXA200400083 120040107A532065516982 SPLICE BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON STRINGER SPLICE AT BS 906, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 906, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-51698; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2L72 4F RTA16WE 20040206002232004020600223NM 2004 2 6 AWXA200400084 120040103A5311654654463 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN FRAME AT BS 695, WL 195, LBL 65. MAINTENANCE REMOVED CRACKED SECTION OF FRAME AT BS 695, WL 195, LBL 65; FABRICATED A NEW REPLACEMENT SECTION OF FRAME PER DWG 65-46544; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 44-45. 2L72 4F RTA16WE 20040206002242004020600224NM 2004 2 6 AWXA200400085 120040101A575465C2660297SP WEDGE BOEING737 737301 1384611NM NR 2 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK NR 2 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED INBOARD OF ANTI-ICE TELESCOPING TUBE. MAINTENANCE CUT OUT DELAMINATED SKIN ON LOWER SURFACE OF NR 2 SLAT; FABRICATED A DOUBLER & FILLER; BONDED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 30 PG 88C-88E. 2L72 4F RTA16WE 20040206002262004020600226NM 2004 2 6 AWXA200400087 120040107A57536546481106 CARRIAGE BOEING737 737301 1384611NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON NR 7 FLAP CARRIAGE SPINDLE. MAINTENANCE REMOVED AND REPLACED NR 7 FLAP CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024. 2L72 4F RTA16WE 20040206002282004020600228NM 2004 2 6 AWXA200400089 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 867, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 867, STR 4 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2L72 4F RTA16WE 20040206002342004020600234NM 2004 2 6 DHL2004721002 120040124A5270 SWITCH BOEING727 727228 1384083NM MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01721DH 19545 FORWARD ENTRY DOOR LIGHT ILLUMINATED UPON LANDING. LUBED DOOR INDICATION SWITCH ON FORWARD ENTRY, AND CYCLED DOOR SEVERAL TIMES IAW M/M 52-11-01. NO ABNORMAL INDICATIONS NOTED. 2L73 4F RTA3WE 20040206002362004020600236NM 2004 2 6 DHL2004746002 120040124A3350 BATTERY BOEING727 727224 1384076NM EMERGENCY LIGHT INOPERATIVE A DHLAO OTHER L NO TEST ININSP/MAINT 1 SO01746DH 22252 EMERGENCY EXIT LIGHT ABOVE FORWARD ENTRY DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT FORWARD ENTRY DOOR BATTERY IAW B-727 M/M 33-50-01, OPS GOOD. 2L73 4F A3WE 20040209000142004020900014SO 2004 2 9 C2XA04SH030 120040128A491014526850601 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE VERTICAL STIFFENER AND THE RIGHT ENDS OF THE 2ND AND 3RD HORIZONTAL STIFFENERS AND THE RIGHT UPPER APU MOUNTING BRACKET. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW CONTINENTAL EXPRESS EA 5340-01016. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040209000272004020900027EA 2004 2 9 QXEA200400068 120040126A2840P93A25602 CARTRIDGE CNDAIRCL600 CL6002C10 1390015EA FUEL PUMP FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09601QX5275 5275 10009 CREW RETURNED TO GATE. RECEIVED A CROSS FLOW PUMP CAUTION MESSAGE WITH ASSOCIATED CROSS FLOW PUMP FAIL INDICATIONS ON THE OVERHEAD PANEL. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE CROSS FLOW PUMP. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040209000372004020900037WP 2004 2 9 AALA20040142 120040126A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217526A 49918 SAN CEILING EMERGENCY LIGHTS AT ROWS 4 AND 7 INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT ROWS 4 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209000382004020900038WP 2004 2 9 AALA20040137 120040127A33506011779 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21253AA 49286 DFW FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209000392004020900039WP 2004 2 9 AALA20040138 120040127A33506011779 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21253AA 49286 DFW FORWARD OVERWING LEFT HAND EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY FOR FORWARD LEFT HAND OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209000472004020900047NM 2004 2 9 CALA0400061 120040126A5320 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716234 28946 INSPECTION FOUND FORWARD PIT ZEE CHANNEL CORRODED FROM STA 500-500I, RT SIDE. THE CHANNEL WAS REMOVED AND A NEW ZEE CHANNEL WAS INSTALLED IAW SRM 53-00-53, 51-20-01, AND 51-40-02. 2L72 4F RTA16WE 20040209000522004020900052CE 2004 2 9 028041 120040126A3246 BEARING BEECH 1900 1900D 1154162CE NR 3 WHEEL FROZEN A NSVAO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 EA27171CJ312 UE71 NR 3 MAIN WHEEL ASSY DEPARTED AIRCRAFT ON TAKEOFF, AIRCRAFT LANDED WITHOUT INCIDENT. WHEEL RECOVERED AT AIRPORT, PROBABLE CAUSE WAS BEARING FAILURE. 2L72 4T RTA24CE 20040209000612004020900061NM 2004 2 9 AWXA200400100 120040109A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727A, STR 2 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727A, STR 2 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 14 PG 1, 38 & 55. 2L72 4F RTA16WE 20040209000622004020900062NM 2004 2 9 AWXA200400101 120040108A5320654585569 WEB BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB AT R-2 DOOR LOWER SILL BS 990, RBL 49, WL 208. MAINTENANCE REMOVED CORRODED WEB BS 990, RBL 49, WL 208; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-01. 2L72 4F RTA16WE 20040209000772004020900077NM 2004 2 9 AWXA200400108 120040128A3350BR964411 LIGHT BOEING757 757225 1384959NM SEAT ROW 18 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040209000932004020900093EU 2004 2 9 04FDEA00244 120040129A3260837101A PROXIMITY SENSOR AIRBUS310 A310 EU MLG MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25428FE 248 ON TAKEOFF FROM IAD GEAR WOULD NOT RETRACT, BOTH SYSTEMS TRIED. FOLLOWED ECAMS. RETURNED TO IAD. REMOVED AND REPLACED PROX BOX PER MM 32-31-71, OP'S GOOD. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-371-01A. SERVICED LT LANDING GEAR BOGIE BEAM DAMPER PER MM 12-12-32-0. 2L72 4F RTA35EU 20040209001042004020900104SO 2004 2 9 SWIA200412807 120040123A2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO LT ELEVATOR TRIMMALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07293SW 120320 RECEIVED AURAL WARNING, TRIM ON TAKEOFF ROLL. TRIM SETTING WAS IN THE GREEN BAND. ABORTED T/O RETURNED TO GATE. REMOVED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR IAW EMB 120 MM 27-32-05. OPS CHECK GOOD. P/N 922AAZY-AGP-Z722. 2L72 4T RTA31SO 20040209001082004020900108SO 2004 2 9 C2XA04SH032 120040130A531514523186001 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001092004020900109SO 2004 2 9 C2XA04SH033 120040130A531314528737001 STRINGER EMB 145 EMB145 3260210SO FUSELAE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAMES 52-53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001102004020900110NM 2004 2 9 PCAA0401160 120040128A7930 CONNECTOR DHAV DHC8 DHC8102 2809003NM TRANSMITTER DEFECTIVE A PCAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA13827EX 390 FLIGHT 3716 ON TAKEOFF OUT OF ITHACA, HAD TO ABORT TAKEOFF DUE TO NR 1 OIL PRESSURE INDICATOR SHOWING FULL DEFLECTION OF APPROXIMATELY 100 PSI. MAINTENANCE CLEANED CONNECTOR FOR THE OIL PRESSURE TRANSMITTER AND OPERATIONAL CHECKED SYSTEM, ALL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. THEN DURING FLIGHT, NR 1 OIL PRESSURE INDICATIONS WERE 85-95 PSI ON APPROACH TO SYRACUSE. MAINTENANCE CLEANED CONNECTOR 7700 P1 AND OPERATIONAL CHECKS WERE AGAIN GOOD. AIRCRAFT RETURNED TO SERVICE. THEN FLIGHT 3850 TO DCA, NR 1 OIL PRESSURE READ 100 PSI ONCE AGAIN. MAINTENANCE REMOVED AND REPLACED NR 1 OIL PRESSURE TRANSMITTER. ALL OPERATIONAL CHECKS GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209001122004020900112NM 2004 2 9 P5CA0401032 120040129A523065B073296 PUSHROD BOEING747 7472U3B 1384846NM CARGO DOOR SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23922FT 22768 MAIN DECK CARGO DOOR FWD HOOK SHAFT PUSH ROD SHEARED ON OPEN SEQUENCE. INSTALLED FWD HOOK SHAFT PUSH ROD, OPS NORMAL IAW 52-32-11. 2L74 4F RTA20WE 20040209001132004020900113EA 2004 2 9 COMA0460092 120040116A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 FRETTING DAMAGE NOTED AT LOWER INBOARD END OF LEFT HAND LOWER WING ACCESS PANEL HOLE 540 DB. BLENDED DAMAGE AND ROTO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030. 2L72 4F RTA21EA 20040209001142004020900114EA 2004 2 9 COMA0460093 120040116A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 RIGHT HAND WING LOWER PLANK CRACKED AT WS 148.019. REPAIRED RIGHT HAND LOWER WING, PLANK AT WS 148.019 IN ACCORDANCE WITH BOMBARDIER REO 601R-57-21-138. 2L72 4F RTA21EA 20040209001152004020900115EA 2004 2 9 COMA0460094 120040116A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 LEFT HAND WING LOWER PLANK CRACKED AT WS 148.019. REPAIRED LEFT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WITH BOMBARDIER REO 601R-57=21-138. 2L72 4F RTA21EA 20040209001172004020900117NM 2004 2 9 UPS04241785 120040107A5512 SKIN BOEING727 72725C 138400HNM HORZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 INSPECTION TYPE: C, LEFT HORIZONTAL STAB UPPER SKIN ABOVE NR 1 BALANCE PANEL HAS SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-06, PANEL REPAIRED IAW SRM 51-40-20. 2L73 4F A3WE 20040209001182004020900118NM 2004 2 9 UPS04241788 120040129A5512 SKIN PANEL BOEING727 72725C 138400HNM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 INSPECTION TYPE:C RIGHT HORIZONTAL STAB, UPPER SURFACE STA 17.2 TO 50.5 SKIN ABOVE NR 1 BALANCE PANEL BAY HAS SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-6. 2L73 4F A3WE 20040209001222004020900122NM 2004 2 9 AWXA200400121 120040129A3246 WHEEL BOEING737 7373G7 1384595NM MLG DAMAGED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP28157AW 23779 PHX - ABORTED TAKEOFF - FLT 0540 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR DFW, AS POWER WAS ADVANCED, THE AIRCRAFT WAS SLOW TO ACCELERATE AND REQUIRED FULL RIGHT RUDDER TO MAINTAIN RUNWAY CENTERLINE. REJECTED TAKEOFF AT 60 KTS; POSSIBLE LT DRAGGING BRAKE. MAINTENANCE PERFORMED AUTOBRAKE TEST IAW BMM 32-43-01 PG 501-506, NO FAULTS NOTED. VERIFIED BRAKES RELEASED PROPERLY AND CHECKED NOSE WHEEL STEERING CENTERING FUNCTION, BOTH SYSTEMS NORMAL. PERFORMED ENGINE ACCEL TEST NR 8 AND HIGH SPEED TAXI CHECK, NO ABNORMALITIES NOTED. AS A PRECAUTION REMOVED AND REPLACED NR 1 & 2 MAIN LANDING GEAR WHEEL ASSEMBLIES IAW T/C R4M32013. 2L72 4F RTA16WE 20040209001242004020900124NM 2004 2 9 AWXA200400123 120040102A5755654645262A PANEL BOEING737 737301 1384611NM RT SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW15476 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK NR 5 SPOILER SKIN WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED NR 5 SPOILER PANEL IAW AMM 27-62-12. 2L72 4F RTA16WE 20040209001252004020900125NM 2004 2 9 AWXA200400124 120040119A5315BAC1518399 FLOORBEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT CABIN FLOORBEAM AT BS 986, LBL 18 TO RBL 44. MAINTENANCE REMOVED FLOORBEAM UPPER TEE CAP AT BS 986, LBL 18 TO RBL 44; FABRICATED A NEW REPLACEMENT TEE CAP; INSTALLED REPAIR PART IAW B737-200 SRM 53-10-09 FIG 2 PG 1. 2L72 4F RTA16WE 20040209001272004020900127EU 2004 2 9 DHL2004365511 120040107A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH MAIN DECK SEAT TRACK BETWEEN FR19 TO 26 APPROX LBL 57 HAS SPOTS OF CORROSION. REMOVED CORROSION ON SEAT TRACK BETWEEN FRAMES 19 AND 26 APPROX LBL 57 AS PER A300 SRM 51-40-11. MATERIAL LOSS .038 INCH AT FRAME 21 AND .041 INCH AT FRAME 24, OUT OF LIMITS AS PER A300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK FROM FRAME 19.5 TO FRAME 26.5. MATERIAL 7075T6511 TMS 60-22457 PO 23488101 SIZE 14 FT 8 INCHES REF A300 SRM 51-40-11, 53-10-11, 51-10-40, 51-40-12, 51-30-30. 2L72 4F RTA35EU 20040209001282004020900128NM 2004 2 9 CALA0400066 120040128A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 277, BL 0. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5321-01169. 2L72 4F RTA16WE 20040209001292004020900129NM 2004 2 9 CALA0400067 120040129A5330 SKIN BOEING737 737524 1384721NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711656 28917 INSPECTION FOUND FUSELAGE SKIN DAMAGED ON FORWARD CURVED SIDE AT RIGHT AFT HORIZONTAL STABILIZER ATTACH POINT. THE SKIN WAS REPLACED IAW SRM 51-40-2. 2L72 4F RTA16WE 20040209001322004020900132 2004 2 9 YENA200405 420040123A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU SEAT SMOKE A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15531JB287 1650 ROW 10 & 11 AIRCRAFT RIGHT PLASTIC ODOR. INVESTIGATED ODOR AND FOLLOWED PROCEDURE AS PER INFO NOTICE 2003-T050TR A. FOUND SEAT ELECTRONIC BOX (SEB) AT POS 9E SUSPECT W/ELEC ODOR. REMOVED AND REPLACED SEAT ELECTRONIC BOX AT 9E IAW LTV MM 23-39-00. OPS CHECK OK. 2L72 4F RTA28NM 20040209001332004020900133NM 2004 2 9 QXEA200400081 120040128A2621 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM APU FIRE BOTTLE DIRTY A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09414QX 4061 GEG - FLIGHT 2392 - CREW RECEIVED AN APU BOTTLE LOW MESSAGE WITH INTERMITTENT WARNINGS. MAINTENANCE CLEANED THE CONNECTOR P813, LOCATED ON THE REAR PRESSURE BULKHEAD. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040209001372004020900137NM 2004 2 9 ABXA040050 120040129A29167321870019 MODULE BOEING767 767281 1385109NM HYD SYSTEM LEAKING A ABXAO OTHER K FLUID LOSS APAPPROACH 1 GL23796AX18566 23146 CENTER HYDRAULIC QUANTITY DECREASED TO .13, SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ON APPROACH, COMPLETE LOSS OF CENTER HYDRAULICS. FOUND FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY LEAKING AT FILTER HOUSING. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY IAW B767 AMM 27-51-48-2. LEAK AND OPS CHECKED GOOD. SERVICED CENTER HYDRAULIC SYSTEM TO 1.12. 2L72 4F RTA1NM 20040209001382004020900138WP 2004 2 9 ABXA040044 120040113A57535910134143 SKIN DOUG DC9 DC941 302207NWP LT T/E FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 LEFT FLAP INBOARD UPPER SKIN SURFACE CORRODED BEYOND LIMITS. REPLACED SKIN ON LEFT FLAP INBOARD UPPER SKIN SURFACE IAW DC-9 SRM. 2L72 4F A6WE 20040209001402004020900140WP 2004 2 9 ABXA040045 120040113A53129915569157 BULKHEAD DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 FITTING BELOW UPPER HINGE INSIDE AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED DOOR FITTING IAW DC-9 SRM. 2L72 4F A6WE 20040209001422004020900142WP 2004 2 9 ABXA040048 120040115A531159135953 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 FRAME 1076 CRACKED AT LONGERON 3 LT. REPAIRED IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040209001432004020900143WP 2004 2 9 ABXA040049 120040116A5320D0489833 WEB DOUG DC9 DC933F 302207AWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 CUSP WEB AT FS 887, LEFT BUTT LINE 46 WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040209001452004020900145 2004 2 9 SWIA200412808 420040121A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07416SW7348 7348 7089 ON DESCENT AND DURING APPROACH, THE CONTROL WHEEL WOULD INTERMITTENTLY JERK, BUT THE AUTOPILOT DID NOT DISCONNECT. REMOVED AND REPLACED FCC NR 2 CARD AND ELEVATOR SERVO IAW MM 27-12-14, MM 22-11-24. OPS CHECKS GOOD. SERVO P/N: 622-5027-001, S/N OFF: 2935. 2L72 4F RTA21EA 20040209001462004020900146SO 2004 2 9 SWIA200412809 120040124A2730 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT ELEVATOR MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM07189SW 120048 TAKEOFF AURAL WARNING TRIM ALERTS WHEN TRIM IS SET IN GREEN, HAS HAPPENED ON TAKEOFF ROLL ONLY AND NOT DURING GROUND TEST. CLEANED GLYCHOL OFF PROX SENSORS ON ELEVATOR TRIM TABS. REPLACED RIGHT PROX SWITCH ON ELEVATOR TRIM TAB IAW MM 27-32-05, OPS CHECK GOOD. P/N ATG120R. 2L72 4T4 TRTA31SO E20NE 20040209001472004020900147EA 2004 2 9 SWIA200412810 120040125A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07945SW 7770 FORWARD FLOOR EMERGENCY LIGHT (ORANGE) INOPERATIVE. REPAIRED WIRING AS NEEDED. OPS CHECK GOOD IAW MM 33-51-01. 2L72 4F RTA21EA 20040209001482004020900148SO 2004 2 9 SWIA200412811 120040126A2731 WARNING HORN EMB 120 EMB120ER 3260203SO TRIM SYSTEM FALSE ACTIVATIONA SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07578SW 120346 ABORTED TAKEOFF DUE TO AURAL WARNING TRIM. TRIM WAS SET AT 34 PERCENT. PERFORMED OPERATIONAL CHECK OF TRIM SYSTEM. OP CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY. 2L72 4T RTA31SO 20040209001522004020900152EA 2004 2 9 SWIA200412815 120040125A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07459SW 7782 ON TAXI OUT, RECEIVED FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECK GOOD. P/N 865D100-7, S/N ON 0831, S/N OFF 1036. 2L72 4F RTA21EA 20040209001552004020900155WP 2004 2 9 AALA20040150 120040128A49005940405503 APU DOUG DC9 DC982 3022082WP APU BAY SMOKE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21403A 26294 49314 DFW INFLIGHT T563/28 SMOKE IN CABIN AFTER TAKEOFF AND REMAINED UNTIL LANDING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AUXILLARY POWER UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209001582004020900158NM 2004 2 9 04FDEA00249 120040130A5753ARB2850506 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING LEADING EDGE LOCATION WITH NR 16 TRACK INBOARD MOST FITTING CRACKED. RT WING NR 16 TRACK INBD MOST CRACKED FITTING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-31-01 VOL. II AND SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040209001592004020900159NM 2004 2 9 04FDEA00248 120040130A5753ARB2850505 TRACK DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND LEADING EDGE LOCATION WITH NR 16 TRACK INBOARD MOST FITTING CRACKED. LT WING NR 16 TRACK INBD MOST CRACKED FITTING REMOVED AND REPLACED WITH NEW FITTING AS PER SRM 51-31-01 VOL. II AND SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040209001612004020900161EA 2004 2 9 QXEA200400086 120040125A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 DEN - FORWARD CARGO COMPARTMENT CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040209001622004020900162 2004 2 9 QXEA200400085 420040129A3421H321ALM1 INDICATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09375PH1037610376 529 PDX- ON FLIGHT 2201 AIRCRAFT RETURNED TO FIELD DUE TO STANDBY ATTITUDE INDICATOR FAILED ON DEPARTURE. REMOVED AND REPLACED INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209001652004020900165SO 2004 2 9 C2XA04SH036 120040131A531014529150007 CROSSBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 DURING C-CHECK THE CROSSBEAM BETWEEN FRAMES 23 AND 24 AT STRINGER 15R WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001662004020900166SO 2004 2 9 C2XA04SH037 120040131A532014521725001 SILL EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE MAIN DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001672004020900167SO 2004 2 9 C2XA04TY024 120040131A532014525422005 SILL EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT AT FRAME 68 WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW EMB-135/145-SRM-51-40-02 / CMP-51-21-04/06. 2L72 4F RTT00011AT 20040209001682004020900168SO 2004 2 9 C2XA04TY025 120040131A532014525422001 SILL EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS, DURING A SCHEDULED INSPECTION THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 61 AND 64 WAS FOUND DAMAGED. MAINTENANCE REMOVED THE FLOOR SUPPORT, FABRICATED NEW PARTS, ALODINED, PRIMED AND INSTALLED IAW EMB-135/145 SRM 51-40-02/03 AND CMP-51-21-04. 2L72 4F RTT00011AT 20040209001712004020900171SO 2004 2 9 C2XA04TY028 120040131A531514522460013 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS, DURING A SCHEDULED INSPECTION THE CENTER TOP CAP IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE CLEANED AND BLENDED THE CORRODED AREA, ALODINED, PRIMED AND PAINTED IAW EMB-IC2004-145/0302. 2L72 4F RTT00011AT 20040209001732004020900173NE 2004 2 9 187531 220040201A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT MALFUNCTIONED A UHLAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL17158SD 158SD 149 DURING CRUISE THE CREW SET THE RIGHT ENGINE POWER AT 80 PERCENT TQ. THE CREW HEARD A LOUD BANG, FELT A SLIGHT YAW AND NOTICED THAT THE RIGHT TQ HAD DROPPED TO APPROX 70 PERCENT. THE CREW ADJUSTED THE TQ AND THEN HEARD MULTIPLE BANGS ALONG WITH A DROP IN RIGHT TQ AND AN ASSOCIATED RIGHT IGNITION WARNING LIGHT. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. A/C TAKEN OUT OF SERVICE AT 1710 (LT) 02-01-04. 2L72 4T4 TRTA52EU E8NE6 20040209001742004020900174NE 2004 2 9 187532 220040201A7230 COMPRESSOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ENGINE STALLED A UHLAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL17158SD 158 FLIGHT 4593 PIT-TOL. AFTER THE A/C RETURNED TO PIT DUE TO MULTIPLE COMPRESSOR STALLS, THE A/C WAS PARKED WHEN A BAGGAGE CART CAME LOOSE FROM THE TUG THAT WAS PULLING IT AND SLAMMED INTO THE AFT PART OF THE A/C FUSELAGE BEHIND THE CARGO DOOR. 2L72 4T4 TRTA52EU E8NE6 20040209001752004020900175SO 2004 2 9 C2XA04SH038 120040201A491014526850401 FIREWALL EMB 145 EMB145 3260210SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND AND RIGHT HAND SUPPORT ROD BRACKETS. MAINTENANCE PERORMED A DOUBLER REPAIR TO THE AFFECTED AREAS IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001762004020900176SO 2004 2 9 C2XA04SH039 120040201A531514522226003 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP BETWEEN FRAMES 59-61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001792004020900179CE 2004 2 9 DXTA200400222 120040119A3230 PROXIMITY SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07950QS 7500050 ON GEAR RETRACTION THE THREE GREEN LIGHTS WENT OUT, UNLOCK LIGHT STAYED ON AT 195 KNOTS, VIBRATION IN YOKE AND AN INCREASE IN NOISE. CYCLED GEAR WITH SAME RESULT. RIGGED NLG UPLOCK SWITCH AND ADJUSTED ROUTING OF NLG STEERING HOSES. PERFORMED LANDING GEAR OPERATIONAL CHECKS AND FUNCTIONAL CHECK, NO DEFECTS NOTED AT THIS TIME. ALL WORK PERFORMED IAW CESSNA MM CHAPTER 32-00. 2L72 4J RTT00007WI 20040209001822004020900182CE 2004 2 9 DXTA200400229 120040125A3260327 WARNING LIGHT CESSNA560 560XL 2076702CE MLG ILLUMINATED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07665QS 5605165 AFTER TAKEOFF FROM PHL UNSAFE NOSE GEAR LIGHT CAME ON, PULLED EMERGENCY BOTTLE AS PER EMERGENCY CHECKLIST. REPLACED 2 DEFECTIVE BULBS AT NOSE GEAR DOWNLOCK INDICATOR WITH 2 NEW BULBS. RESET GEAR DOWNLOCK VALVE AND SAFETIED, COMPLIED WITH GEAR RETRACTION CHECKS / FUNCTION CHECKS IAW CESSNA 560XL MM CHAPTER 32-61-00. 2L72 4F RTA22CE 20040209001832004020900183CE 2004 2 9 DXTA200400228 120040124A793031J170001 OIL FILTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE RT ENGINE CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07640QS 5605240 PCEDB0494 DURING TAKEOFF ROLL FOR THE FIRST FLIGHT OF THE DAY, WHILE APPROACHING 40 KNOTS THE RIGHT ENGINE OIL PRESSURE BYPASS ANNUNCIATOR AND MASTER CAUTION ILLUMINATED, ABORTED TAKEOFF. INSPECTED RT ENGINE CHIP DETECTOR LIGHT AND VISUALLY CHECKED OIL FILTER ALL FOUND SATISFACTORY, INSTALLED A NEW ENGINE OIL FILTER AND SEALS. RAN ENGINE AT TAKEOFF AND CRUISE POWER FOR 5 MINUTES, FILTER LEAK CHECK SATISFACTORY. ALL WORK PERFORMED IAW PW 545A MM CHAPTER 79-20-01 AND CESSNA 560XL MM CHAPTER 12-11-02. 2L72 4F4 FRTA22CE E00059EN 20040209001842004020900184 2004 2 9 DXTA200400226 420040123A23507012100805 RMU CESSNA650 650 2076802CE RADIO MANAGE FAILED E DXTAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07785QS 183 6507085 DURING TAXI NR 2 COM NAV DISPLAY WENT BLANK, APPROXIMATELY 5 MIN LATER DISPLAY WENT FULL BRIGHT THEN BEGAN TO SMOKE AND WENT BLANK AGAIN. AIRCRAFT RETURNED TO BLOCK. REPLACED RADIO MANAGEMENT UNIT IAW CE-650 MM CHAPTER 23-11-10, SYSTEM OPS CHECKED GOOD. 2L72 4F A9NM 20040209001852004020900185CE 2004 2 9 DXTA200400225 120040119A215073838433 ACM CESSNA750 750 2076810CE CABIN COOLING ODOR E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07984QS447 7500084 COCKPIT TEMP SELECTOR CANNOT CONTROL TEMP IN EITHER MANUAL OR AUTO MODE, COCKPIT TEMP (SUPPLY) REMAINS AT APPROX 140 DEGREES DURING FLIGHT. TEN MINUTES AFTER LANDING SUPPLY TEMP ROSE TO APPROX 235 DEGREES ACCOMPANIED BY STRONG ODOR, SIMILAR TO AN OVERHEATED ODOR. REMOVED AND REPLACED AFT ACM IAW CESSNA 750 MM CHAPTER 21-51-00 AND HAMILTON SUNDSTRAND MM CHAPTER 21-50-03, OPS CHECK AND LEAK CHECK GOOD. 2L72 4J RTT00007WI 20040209001862004020900186CE 2004 2 9 DXTA200400224 120040123A2722 LINE CESSNA650 650 2076802CE RUDDER ACTUATOR CONTAMINATED E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07787QS 6507087 DURING TAKEOFF WITH MAX TAKEOFF POWER APPLIED, THE RIGHT RUDDER PEDAL WENT FULL FORWARD POSITION, TAKEOFF WAS ABORTED. TROUBLESHOT AND FOUND LINE GOING TO RUDDER BIAS ACTUATOR HAD FROZEN MOISTURE IN IT. REMOVED LINE AND PURGED MOISTURE, REINSTALLED LINE, OPS CHECK LEAK CHECK GOOD IAW CESSNA 650 M/M CHAPTER 27-20-01. 2L72 4F A9NM 20040209001882004020900188CE 2004 2 9 DXTA200400227 120040125A2740 WIRE HARNESS CESSNA750 750 2076810CE PROXIMITY SWITCHDISCONNECTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07996QS 7500196 DURING THE TAKEOFF ROLL, A NO TAKEOFF MESSAGE APPEARED. ABORTED TAKEOFF, A-PITCH ROLL DISCONNECT MESSAGE CAME ON, ONCE CLEAR OF THE RUNWAY ALL SYSTEMS CHECKED NORMAL. GAINED ACCESS TO PITCH/ROLL DISCONNECT, FOUND DATA LOADER HARNESS INTERFERING BY PITCH/ROLL DISCONNECT PROXIMITY SWITCH. REROUTED DATA LOADER HARNESS, ALSO CHECK PROXIMITY SWITCH CLEARANCE IAW CESSNA 750 MAINTENANCE MANUAL CHAPTER 27-10-00, OPERATIONAL CHECKS SATISFACTORY. 2L72 4J RTT00007WI 20040209001892004020900189CE 2004 2 9 DXTA200400221 120040119A3320 WIRE CESSNA500 560CESSNA 2076750CE CABIN LIGHT LOOSE E DXTAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07320QS 5600321 DURING TAXIING OUT FOR TAKEOFF, PASSENGER NOTICED BURNING ELECTRICAL ODOR IN CABIN. CREW MEMBER VERIFIED THE ELECTRICAL ODOR COMING FROM THE CEILING NEAR THE REAR SPEAKER, AIRCRAFT RETURNED TO BLOCK. TROUBLESHOT BY GAINING ACCESS THRU CABIN OVERHEAD PANEL, FOUND AFT CABIN INFORMATION LIGHT INOP DUE TO LOOSE CONNECTION. TIGHTENED CONNECTION, OPS CHECK GOOD. RAN AIRCRAFT APPROX 30 MIN, COULD NOT DUPLICATE ELECTRICAL BURNING ODOR. RESTORED ACCESS IAW CESSNA 560 MM CHAPTER 25-22-03 AND 31-21-03. 2L72 4F RTA22CE 20040209001902004020900190NM 2004 2 9 373PA0024 120040202A551469731201 PIN BOEING737 7373Y0 1384671NM HOR STAB HINGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 DURING ACCOMPLISHMENT OF BOEING SB 737-55A1077 PART 2, FOUND CORROSION AROUND THREADS AND THREAD RELIEF ON RIGHT HORIZONTAL STABILIZER OUTER HINGE PIN. REPLACED INNER AND OUTER PINS PER SB737-55A1077 AND MM 27-41-31. 2L72 4F RTA16WE 20040209001912004020900191NM 2004 2 9 373PA0025 120040202A38108921270G2 DRAIN MAST BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 DRAIN MAST HAS HOLE CORRODED THROUGH SIDE ON BOTH SIDES OF MAST. REPLACED DRAIN MAST PER MM 38-31-21. 2L72 4F RTA16WE 20040209001982004020900198NM 2004 2 9 373PA0032 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 INTERCOSTAL BETWEEN STA 312 AND STA 328 HAS CORROSION AT LBL 10. REPLACED INTERCOSTAL CAP (SHIM) PER SRM 51-20-01 AND SRM 51-10-02. 2L72 4F RTA16WE 20040209002002004020900200NM 2004 2 9 QXEA200400087 120040130A213121278041 CONTROLLER DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09358PH13951 506 SEA - FLIGHT 2124 - DURING DESCENT AT 8000 FT, AIRCRAFT DEPRESSURIZED RAPIDLY. DIFFERENTIAL PRESSURE DROPPED TO 0. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. LEAK TEST AND OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209002012004020900201NM 2004 2 9 DHL2004740001 120040131A5210 HANDLE BOEING727 7272Q9 138448MNM PAX DOOR LACK OF LUBE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01740DH 21930 MAIN ENTRY DOOR HANDLE DOESN'T WANT TO STAY FLUSH. LUBED HANDLE ASSEMBLY AND STOWED REF M/M 52-11-01. 2L73 4F RTA3WE 20040209002032004020900203NM 2004 2 9 DHL2004745012 120040131A3260 SWITCH BOEING727 727224 1384076NM MLG DOORS OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION DOORS RED LIGHT AND AMBER RIGHT GEAR DOOR LIGHTS ILLUMINATED, ACCOMPLISHED ABNORMAL PROCEDURE, LIGHTS WENT OUT. CLEANED AND ADJUSTED RIGHT LANDING GEAR WHEEL WELL SWITCH, OPS CHECKED SEVERAL TIMES, OPS CHECKED NORMAL IAW M/M 32-12-0 & 32-12-1. 2L73 4F A3WE 20040209002042004020900204NM 2004 2 9 373PA0037 120040202A5310 TORQUE BOX BOEING737 7373Y0 1384671NM APU BAY CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 LITE CORROSION AND CRACKS AROUND NUT PLATES ON LOWER SURFACE OF TORQUE BOX LEFT SIDE OF APU AT APPROX BS 1100. REPAIRED AREA PER SRM 51-70-13. 2L72 4F RTA16WE 20040209002062004020900206NM 2004 2 9 373PA0038 120040202A5320 FLOOR SUPPORT BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 SUPPORT/ATTACH ANGLE CRACKED AT STA 807 UNDER FLOOR STRUCTURE AT RBL 20. FABRICATED SUPPORT ANGLE PER DRAWING 65-47957 AND INSTALLED. 2L72 4F RTA16WE 20040209002072004020900207NM 2004 2 9 373PA0040 120040202A5321 FLOOR PANEL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 FLOOR PANEL SPLICE STRAP, AFT OF FRAME 727D, HAS SEVERAL AREAS OF LITE CORROSION. FABRICATED NEW SPLICE STRAP PER DRAWING 65-46592 AND INSTALLED PER SRM 51-10-2. 2L72 4F RTA16WE 20040209002132004020900213NM 2004 2 9 373PA0045 120040202A5347 SEAT TRACK BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION ON AFT END OF LEFT INBOARD SEAT TRACK OF AFT GALLEY. REPAIRED PER SRM 53-00-52. 2L72 4F RTA16WE 20040209002142004020900214NM 2004 2 9 373PA0046 120040202A5320 ATTACH ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION UNDER RAMP FOR LARGE CART G-2 GALLEY. REPAIRED PER SRM 51-70-12. 2L72 4F RTA16WE 20040209002162004020900216EA 2004 2 9 COMA0460095 120040128A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CONTAMINATED A COMAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SO01484CA 7702 FLIGHT 5710 EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 1 THRU 6. CLEANED MOISTURE FROM WIRE CONNECTIONS, SYSTEM OPERATION SATISFACTORY. 2L72 4F RTA21EA 20040209002172004020900217WP 2004 2 9 IXXA0400008O 120040131A56105887276501 WINDSHIELD DOUG DC8 DC862 3021970WP COCKPIT CRACKED A IXXAA UNSCHED LANDING O OTHER CRCRUISE 1 SW1141CX 759482482 46129523 ONE HOUR AND A HALF INTO CRUISE FROM KBWI THE CAPTAINS WINDSHIELD CRACKED. CREW RETURNED THE AIRCRAFT TO KBWI AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED WINDSHIELD AND HEAT CONTROLLER PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040209002182004020900218NM 2004 2 9 QXEA200400090 120040201A3350566DH8SA221 LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX- EMERGENCY LIGHTING STRIP ARE LOOSE AT ROW 1 AND 2 IN FRONT OF SEATS. REMOVED AND REPLACED LIGHT STRIP. 2H72 4T RTA13NM 20040209002192004020900219NM 2004 2 9 QXEA200400091 120040129A3350566DH8SA221 LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 SEA- ON FLIGHT 2321 EMERGENCY FLOOR TRACK LIGHTING STRIP IS COMING UP IN FRONT OF ROW 1. REMOVED AND REPLACED FLOOR TRACK LUMINESCENT STRIPS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209002222004020900222NM 2004 2 9 AALA20040153 120040201A3350BP573 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21647AM 24605 AISLE EMERGENCY LIGHTS AT STATIONS 635L AND 830L INOPERATIVE. REPLACED BATTERY PACK M10567 FOR AISLE EMERGENCY LIGHTS AT STATIONS 635L AND 830L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040209002232004020900223EU 2004 2 9 AALA20040154 120040201A3397 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW217076A 610 SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 12C, 31C, 32C, AND 25G INOPERATIVE. FOUND UNDERSEAT CONNECTOR DISCONNECTED. RECONNECTED UNDERSEAT CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 12C, 31C, 32C, AND 25G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040209002242004020900224WP 2004 2 9 AALA20040155 120040201A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21474 49649 SEA - INSEAT EMERGENCY LIGHTS AT OVERWING EXIT INOPERATIVE. REPAIRED WIRING IN AFT TAIL COMPARTMENT FOR INSEAT EMERGENCY LIGHTS AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002252004020900225WP 2004 2 9 AALA20040156 120040201A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DIRTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21451AA 49477 DFW - EMERGENCY LIGHTS AT AFT LAVATORY AREA INOPERATIVE. CLEANED BATTERY PACK B5-27 CONTACTS FOR EMERGENCY LIGHTS AT AFT LAVATORY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002262004020900226WP 2004 2 9 AALA20040157 120040201A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21451AA 49477 DFW - EMERGENCY LIGHT AT FORWARD GALLEY LOWER WALL INOPERATIVE. REPLACED LIGHT ASSEMBLY AND ADJACENT CONNECTORS FOR EMERGENCY LIGHT AT FORWARD GALLEY LOWER WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002272004020900227WP 2004 2 9 AALS20040158 120040130A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21468AA 49598 TPA - CEILING EMERGENCY EXIT LIGHTS AT ROW 19 AND 20 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHTS AT ROW 19 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002302004020900230WP 2004 2 9 AALA20040161 120040130A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21468AA 49598 TPA - EMERGENCY EXIT PATH LIGHTS AT ROWS 4 THROUGH 19 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT PATH LIGHT AT ROWS 4 THROUGH 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002352004020900235NM 2004 2 9 QXEA200400093 120040130A323054C546349 SEQUENCE VALVE DHAV DHC8 DHC8202 2809007NM ZONE 400 FAULTY A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09357PH14127 504 SEA - FLIGHT 2025 - AT APPROXIMATELY 11,00 FT, INDICATING 230 KTS, THE LEFT LANDING GEAR DOOR LIGHT ILLUMINATED WITH A LANDING GEAR INOP CAUTION LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 LANDING GEAR DOOR SEQUENCE VALVE AND THE PSEU (FOR CARD A & B FAULTS). OPERATIONAL CHECKS WERE DONE AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209002372004020900237SO 2004 2 9 RAIA00401026 120040115A531514522460013 GUSSET EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK 145256 DURING BLOCK CHECK FOUND CENTER FLOORBEAM GUSSET CORRODED BEYOND BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED CENTER FLOORBEAM GUSSET. 2L72 4T RTT00011AT 20040209002402004020900240SO 2004 2 9 RAIA00401029 120040115A531114522460015 GUSSET EMB 145 EMB145LR 3260212SO FRAME CORRODED A RAIAO OTHER O OTHER ININSP/MAINT 1 CE03811HK 145256 MX-STL- DURING BLOCK CHECK AFT STRAP AT FRAME 18 FOUND CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED GUSSET AFT STRAP AT FRAME 18. 2L72 4T RTT00011AT 20040209002422004020900242NM 2004 2 9 04FDEA00252 120040131A5754ARB293349 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND LT WING LEADING EDGE SLAT NR 9 TRACK LOCATION WITH ACCESS CUTOUT FWD MOST CRACKED (OUTBOARD MOST REFUELING PANEL). LT WING - LEADING EDGE SLAT NR 9 TRACK LOCATION CUT-OUT FWD CRACK AREA REPAIR CARRIED-OUT AS PER SRM 51-33-01 VOL. II AND SRM 51-35-01 VOL. II. 2L73 4F RTA22WE 20040209002432004020900243NM 2004 2 9 04FDEA00253 120040131A5730ARB74054 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 231 TO XORS 264 FOUND WITH CORROSION. CORROSION ON RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 231 TO XORS 264 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN TOLERANCES OF DWG ARB7113. 2L73 4F RTA22WE 20040209002462004020900246NM 2004 2 9 04FDEA00256 120040131A2782 ACTUATOR BOEING727 727200 138407ENM LE FLAP MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25223FE6726 2751 20935 DURING FLAP RETRACTION FLAPS FROM 5 TO 2 DEGREE AMBER LIGHT. REMAINED ON AND NR 1 LED SHOWED INTRANSIT. COMPLIED WITH QRH AND RETURNED TO MEM. IN WORK, AFTER BLOCKING BACK INTO GATE, NR 1 LEADING EDGE FLAP WOULD RETRACT BUT WOULD CREEP BACK OPEN, WITH HYD SYSTEM PRESSURIZED, SUSPECT BAD ACTUATOR TRYING TO ORDER PARTS. REPLACED NR 1 L/E FLAP ACTUATOR IAW AMM 27-81-022-4. CHECKS NORMAL PREMATURE REMOVAL/INSTALLATION OFF MFG 65-17818-20. 2L73 4F RTA3WE 20040209002472004020900247WP 2004 2 9 04FDEA00257 120040201A4910AHL72851 SCREEN DOUG DC10 DC1010 3022110WP APU INTAKE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25550FE 46521 COMPLY WITH EA 8-4917-75549. APU - INLET SCREEN FRAME STUD REPAIR. CLOSING ACTION ON 01-31-04. ON N/R S00016. COMPLIED WITH EA 8-4917-75549. 2L73 4F A22WE 20040209002492004020900249NM 2004 2 9 04FDEA00259 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002512004020900251NM 2004 2 9 04FDEA00261 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002522004020900252NM 2004 2 9 04FDEA00262 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) OUTBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002532004020900253NM 2004 2 9 04FDEA00263 120040201A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBD FLAP, OUTBD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002542004020900254NM 2004 2 9 04FDEA00264 120040201A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002552004020900255NM 2004 2 9 04FDEA00265 120040201A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002562004020900256NM 2004 2 9 04FDEA00266 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE (1) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002572004020900257NM 2004 2 9 04FDEA00267 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002582004020900258NM 2004 2 9 04FDEA00268 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) INBOARD FACE CORRODED. 2L73 4F RTA22WE 20040209002592004020900259NM 2004 2 9 04FDEA00269 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD LT WING FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002622004020900262NM 2004 2 9 04FDEA00272 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002632004020900263NM 2004 2 9 04FDEA00273 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002662004020900266NM 2004 2 9 04FDEA00276 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002682004020900268NM 2004 2 9 04FDEA00278 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002692004020900269NM 2004 2 9 04FDEA00279 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002702004020900270NM 2004 2 9 04FDEA00280 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002712004020900271NM 2004 2 9 04FDEA00281 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040206000982004020600098WP 2004 2 6 DHL2004806520 120040104A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT WING STUB WING FORMER CRACKED 2.000 AT STA XFS 272.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9, 10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 57-2-0 PG 9, 10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040206001002004020600100WP 2004 2 6 DHL2004806530 120040108A5320 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT MLG W/W CEILING ANGLE WITH 0.500 CRACK IN IT, STA 865.000 RBL 46. REMOVED DAMAGED CEILING ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW ANGLE (7075-T6AL 0.071) IAW SRM 53-2-0 PG 1-2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040206001172004020600117WP 2004 2 6 DHL2004806536 120040109A53404897274501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FWD CARGO COMPT FITTING PAD CRACKED 1.000, L-28L, STA 300.000. REMOVED CRACKED FITTING PAD IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20040206001262004020600126EU 2004 2 6 DHL2004365502 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH SEAT TRACK BETWEEN FR25 & FR27 APPROX LBL 18. SEVERAL PLACES EVIDENCE OF SURFACE CORROSION. REMOVED CORROSION AT SEAT TRACK BETWEEN FR25 AN FR27 APPROX LBL 18. CHECKED LIMITS FOUND OUT OF LIMITS IAW A300 SRM 51-10-00 & 53-10-00. REMOVED SEAT TRACK AT MAIN CARGO FROM FR18.5 TO 26.5 LBL 18 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK AT MAIN CARGO FROM FR18.5 TO FR26.5 LBL 18. MATL USED 7075T6511 TMS 60-224457 AS PER A300 SRM 53-10-00 AND 51-10-40, 51-40-12, 51-30-30. 2L72 4F RTA35EU 20040206001282004020600128EU 2004 2 6 DHL2004365503 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH MAIN CABIN AFT OF FR20 APPROX BS 1360 APPROX LBL33 SEAT TRACK EVIDENCE OF CORROSION. REMOVED CORROSION AND FOUND AREA CRACK/ MAIN CABIN FR19 LBL 36 REF A300 SRM 51-10-00 & A300 SRM 53-10-00. REMOVED SEAT TRACK AT MAIN CARGO FROM FR18.5 TO FR26.5 LBL 36 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK AT MAIN CARGO FROM FR18.5 TO FR26.5 LBL 36, MATL USED 7075T6511, TMS 60-224457 AS PER A300 SRM 53-10-00, 51-40-11, 51-10-40, 51-40-12, 51-30-30, PO 23488101. 2L72 4F RTA35EU 20040206001302004020600130EU 2004 2 6 DHL2004365505 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH SEAT TRACK BETWEEN FR22 & FR23 APPROX RBL 18 EVIDENCE OF TOOL MARKINGS. REMOVED CORROSION I/B & O/B FLANGES FOUND OUT OF LIMITS, AT SEAT TRACK FR22 TO FR23 APPROX RBL 18 AS PER A300 SRM 51-10-00, 53-10-00, MATL LOST .030. REMOVED CABIN SEAT TRACK FROM FR18.5 AS PER A300 SRM 53-10-00. INSTALLED NEW SEAT TRACK P/N 7075T6511 TMS 60-224457 FROM FR18.5 TO FR26.5 RBL 18 AS PER A300 SRM 53-10-00, 51-40-11, 51-40-12, 51-30-30. MATL USED 7075T6511 TMS 60-224457, PO 23488101. 2L72 4F RTA35EU 20040206001312004020600131EU 2004 2 6 DHL2004365506 120040107A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH MAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 BL 0 HAS SPOTS OF CORROSION. REMOVED CORROSION IAW A300 SRM 51-40-11 PG 710. MATERIAL LOSS FROM FR22-FR26 APPROX 0.005 WITHIN LIMITS IAW A300 SRM 53-10-00 PG 619. MATL LOSS FROM FR21-FR22 IS 0.40 OUT OF LIMITS IAW A300 SRM 53-10-00. TREATED AND PRIMED FROM FR22-FR26 IAW A300 SRM 51-4-12 PG 701. REMOVED AND REPLACED SEAT TRACK FROM FR21.5 TO FR19.6 MATERIAL USED 7075T6511 TMS 60-224457 PO 23488101 SIZE 56 INCHES. REF A300 SRM 51-40-11, 53-10-11, 51-10-40, 51-40-12, 51-30-30. 2L72 4F RTA35EU 20040206001332004020600133EU 2004 2 6 DHL2004365508 120040122A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH FUSELAGE SKIN DENTED AT FR26 BETWEEN STR29R & STR30R. REWORKED DENTED AREA AS REQUIRED IAW A300 SRM 51-41-10 AFTER REWORK FOUND DENT WITHIN LIMITS IAW A300 SRM 51-00-00 FIG 609. NOTE:08 DEPTH 1.5 LENGHT THICKNESS .063. HFEC INSPECTED AREA AT FR26 BETWEEN STR29R & STR30R IAW A300 NTM 51-30-00 PART 1 FOUND CRACK INDICATION. CUT OUT DAMAGED SKIN AREA DEBURR AND CLEAN EDGES IAW A300 SRM 53-10-10 FIG 705. HFEC INSPECTED CUTOUT AREA FOR CRACKS AS PER A300 NTM 51-00-00 PART 1, NO DISCREPANCIES FOUND. TREATED AND PRIMED AREA & DOUBLER PER A300 SRM 51-40-11. INSTALLED DOUBLER REPAIR AT FR26 BETWEEN STR29R & STR30R. MATL USED 2024T3 .071 SIZE 12 X 8 INCH PO 83113526 PER A300 SRM 53-10-10. 2L72 4F RTA35EU 20040206001352004020600135NM 2004 2 6 VNAA0401002 120040104A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07463PS184771179 3087 THE CREW REPORTED THAT THE FIRST 4 ROWS OF EMERGENCY LIGHTING WILL NOT WORK. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001372004020600137 2004 2 6 VNAA0401003 420040108A3418 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT AOA FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA FAIL INDICATION AND ABORTED TAKEOFF. FLIGHT 2463 THEN RETURNED TO THE GATE TO HAVE MAINTENANCE REST THE AOA VANE LEVEL. FLIGHT 2463 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040206001482004020600148NM 2004 2 6 CALA0400057 120040125A5320 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716234 28946 INSPECTION FOUND RT ZEE CHANNEL IN AFT PIT CORRODED AT STA 727+4 TO 767, RBL 21. A NEW ZEE CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040206001502004020600150WP 2004 2 6 CALA0400059 120040125A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772830 49490 INSPECTION FOUND RT FLOOR SUPPORT ZEE ANGLE CORRODED IN MID BAGGAGE BIN AT STA 620. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-00-00. 2L72 4F A6WE 20040206001562004020600156NM 2004 2 6 AWXA200400063 120040123A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 13 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 DURING A1 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040206001652004020600165NM 2004 2 6 AWXA200400072 120040107A532065516982 SPLICE BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON STRINGER SPLICE AT BS 906, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 906, STR 4 RT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE PER DWG 65-51698; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20040206001882004020600188NM 2004 2 6 2004UALA00051 120040120A3397 WIRE HARNESS BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 SEAT 1E EMERGENCY PROX LIGHTS OUT. SEAT 3E EMERGENCY PROX LIGHT OUT. SEATS 39G AND 34C EMERGENCY PROX LIGHTS OUT. REPLACED HARNESS. REPLACED LAMP ASSY. RELAMPED. 2L72 4F4 FRTT0001SE E46NE 20040206001902004020600190NM 2004 2 6 2004UALA00053 120040112A5740113W721223 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE LT AIL ACTUATOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 ACTUATOR FITTINGS CRACKED. REPLACED FITTINGS. 2L72 4F4 FRTT0001SE E46NE 20040206001922004020600192NM 2004 2 6 2004UALA00055 120040123A5512 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE HORIZONTAL STAB GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29664UA 29236 LEFT HORIZONTAL STAB LOWER SKIN IS GOUGED AT OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20040206001942004020600194NM 2004 2 6 04FDEA00215 120040124A5230AFA80821 FITTING DOUG MD11 MD11 3023602NM ZONE 100 SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CENTER CARGO DOOR INTERIOR, BETWEEN NR 1 AND NR 2 LATCH, FITTING WITH SCRATCH MARK. FITTING REMOVED AND REPLACED IN ACCORDANCE WITH FEDEX EA 1-5230- 71905 - DOORS - CENTER CARGO 104 INCHES DOOR - ALIGNMENT PIN - MODIFICATION. 2L73 4F RTA22WE 20040206001962004020600196WP 2004 2 6 AALA20040131 120040126A3230 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW21587AA 53250 ORD T/636 EN ROUTE ORD-BOS UNABLE TO RAISE NOSE GEAR ON TAKEOFF. RETURNED ORD AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT FLAT AND PERFORMED FULL SERVICE PER MM 32-21-02. REPLACED SCHRADER VALVE AND RING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040206001982004020600198NM 2004 2 6 AALA20040133 120040126A3350 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPAIRED BROKEN WIRE ON HARNESS FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040206002102004020600210EA 2004 2 6 COMA0470011 120040121A2760 CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01398CA 10112 FLIGHT 5585 GROUND LIFT DUMP NOT ARMED MESSAGE. COULD NOT DUPLICATE. NO FAULTS LOGGED IN COMPUTER. 2L72 4F RTA21EA 20040206002252004020600225NM 2004 2 6 AWXA200400086 120040109A5753654648198 CARRIAGE BOEING737 737301 1384611NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON NR 8 FLAP CARRIAGE SPINDLE. MAINTENANCE REMOVED AND REPLACED NR 8 FLAP CARRIAGE SPINDLE ASSEMBLY IAW AWA T/C C3R57024. 2L72 4F RTA16WE 20040206002272004020600227NM 2004 2 6 AWXA200400088 120040107A5320652072640 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL WEB AFT OF FORWARD CARGO DOOR AT STR 26 RT BETWEEN BS 480 AND BS 500. MAINTENANCE REMOVED CORRODED INTERCOSTAL WEB AT STR 26 RT BETWEEN BS 480 AND BS 500; FABRICATED A NEW REPLACEMENT INTERCOSTAL WEB PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 8 PG 1 & 38. 2L72 4F RTA16WE 20040206002332004020600233NM 2004 2 6 DHL2004741001 120040123A5270 SWITCH BOEING727 7272Q9 138448MNM MLG DOOR DIRTY A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01741DH 21931 WITH GEAR HANDLE IN NEUTRAL RED DOORS LIGHT ILLUMINATED AND RT GEAR DOOR LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, AND PLACED GEAR HANDLE IN UP POSITION. LIGHTS EXTINGUISHED. CLEANED RT GEAR DOOR SWITCH WITH CONTACT CLEANER. OPEN AND CLOSED DOOR SEVERAL TIMES. OPS CHECKED GOOD PER M/M 32-12-01. 2L73 4F RTA3WE 20040206002352004020600235EU 2004 2 6 002841 120040127A2420 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R390 R3904123F27 NE AC GENERATOR ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17340SZ 340A004 401 DGR409890 ON 01-27-04, APPROX 1230 (UTC), FLT 4597 TOL-PIT. THE CREW EXPERIENCED AN AC GENERATOR FAIL LIGHT FOR THE RIGHT AC GENERATOR. WEATHER NOT PERMITTING THE FLIGHT TO CONTINUE, THE AIRCRAFT RETURNED TO TOL. 2L72 4T4 TRTA52EU E8NE6 6 CP31NE 20040209000052004020900005EU 2004 2 9 RAIA00401017 120040118A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSLOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03559HK 41075 FRONT SECTION ESCAPE PATH LIGHTS INOP. RE-SECURED LOOSE CONNECTOR AT PATH LIGHTS. 2L72 4T RTA41NM 20040209000102004020900010SO 2004 2 9 RAIA00401022 120040115A532014522461011 DOUBLER EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK7614 145256 MX-STL- DURING BLK CK FOUND CORROSION ON FWD AND AFT DOUBLERS AT SERVICE DOOR WITH CORROSION BEYOND BLENDABLE LIMITS. REMOVED AND REPLACED BOTH DOUBLERS. 2L72 4T RTT00011AT 20040209000322004020900032 2004 2 9 AALA20040145 420040126A256529985103 SLIDE DOUG DC9 DC983 3022083WP L2 DOOR DISPLACED A AALAK NONE O OTHER ININSP/MAINT 1 SW21571AA 49353 AUS L2 AFT SERVICE DOOR SLIDE FOUND BELOW GREEN BAND ON A CHECK. REPLACED L2 AFT SERVICE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040209000402004020900040NM 2004 2 9 AALA20040140 120040128A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21679AN 29589 MIA EMERGENCY PATH LIGHT AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK OR FIRST CLASS EMERGENCY PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040209000552004020900055NM 2004 2 9 AWXA200400094 120040127A2560P4010021 BATTERY BOEING757 757225 1384959NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040209000602004020900060NM 2004 2 9 AWXA200400099 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 727E, STR 8 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727E, STR 8 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 PG 3 - 5, 10 & 38. 2L72 4F RTA16WE 20040209000632004020900063NM 2004 2 9 AWXA200400102 120040108A53206546812185 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER INBOARD LEG BS 996-1004, LBL 14, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT BS 996-1004, LBL 14; FABRICATED A NEW REPLACEMENT SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2L72 4F RTA16WE 20040209000652004020900065NM 2004 2 9 AWXA200400104 120040105A5320654681282 WEB BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF WEB BS 1006-1016, STR 17 RT. MAINTENANCE REMOVED CORRODED WEB BS 1006-1016, STR 17 RT; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. 2L72 4F RTA16WE 20040209000792004020900079NM 2004 2 9 AWXA200400110 120040107A5320654541041 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .625 INCH CRACK WAS FOUND ON LONGITUDINAL FLOOR SUPPORT WEB AT BS 708, LBL 24.75. MAINTENANCE TRIMMED OUT DAMAGE ON FLOOR SUPPORT WEB AT BS 708, LBL 24.75; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5715-04023-ES3. 2L72 4F RTA16WE 20040209000912004020900091CE 2004 2 9 AMWA112 120040102A713011891002219 SEAL BEECH 1900 1900D 1154162CE RT ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07138ZV UE138 DURING INSPECTION RT ENGINE FIRE SEAL WAS FOUND TO BE CRACKED ON THE O/B CENTER WEB, IN CENTER AREA OF WEB APPROX 3.5 INCHES LONG. REPAIRED BY REPLACING WEB ASSY ACCORDANCE WITH SRM. 2L72 4T RTA24CE 20040209000992004020900099EA 2004 2 9 SWIA200412802 120040107A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07906SW5140 5140 7510 STAB CH 1 INOP STATUS MESSAGE WILL NOT GO OUT. REMOVED AND REPLACED HSTA AND MCU SYSTEM. OPS CHECK GOOD PER CRJ MM 27-12-01. MCU P/N: 7062-3, S/N OFF 1126. 2L72 4F4 FRTA21EA E15NE 20040209001052004020900105NM 2004 2 9 QXEA200400078 120040128A5754 SPAR DHAV DHC8 DHC8202 2809007NM ZONE 500 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX- STEP WORN INTO LOWER FLANGE OF LEFT WING FORWARD SPAR AT INBOARD END OF LEADING EDGE 511AL STA YW58.5. REPAIRED IAW RD8-57-811 AND RD8-57-2054. 2H72 4T RTA13NM 20040209001072004020900107NM 2004 2 9 PCAA0401159 120040121A3040 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003NM WINSHIELD HEAT SPARKS A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 EA13804EX 227 DURING LANDING IN PITTSBURGH FLIGHT 3706, EXPERIENCED A LARGE SPARK FROM BEHIND THE CAUTION PANEL. PILOT SUSPECTED IT TO HAVE COME FROM THE RIGHT WINDSHIELD HEAT TERMINAL BOARD. MAINTENANCE WAS NOTIFIED AND FOUND THE FIRST OFFICERS TERMINAL TO BE AT FAULT. THE AFFECTED TERMINAL WAS ISOLATED WITH HEAT SHRINK AS AN INTERIM REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040209001162004020900116NM 2004 2 9 UPS04241783 120040106A323165C8067862 SUPPORT FITTING BOEING727 72725C 138400HNM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 INSPECTION TYPE: C, NLG DOOR LINKAGE ATTACH FITTING CORRODED. REPLACED FITTING AND RIG CHECKED RIGHT HAND DOOR. 2L73 4F A3WE 20040209001192004020900119NM 2004 2 9 UPS04241790 120040129A3350 LIGHT BOEING727 72730C 1384009NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 BOTH EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERIES, OPS CHECK'S NORMAL. 2L73 4F A3WE 20040209001202004020900120NM 2004 2 9 UPS04241791 120040129A57116516201 SPAR BOEING727 72725C 138400HNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 INSPECTION TYPE: C, RIGHT WING REAR SPAR UPPER CHORD HAS CRACK INDICATION BETWEEN WS 288L TO WS 285. SPAR REPAIRED IAW UPS ENGINEERING AUTHORIZATION 727-57-20108. 2L73 4F A3WE 20040209001212004020900121NM 2004 2 9 DHL2004742003 120040129A5250 DOOR KNOB BOEING727 727225 1384077NM COCKPIT DOOR OUT OF ADJUST A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01742DH 21290 COCKPIT ENTRY DOOR VERY DIFFICULT TO OPEN FROM OUTSIDE. COCKPIT ENTRY DOOR KNOB ADJUSTED PER SMP, CHECK GOOD FOR SERVICE. 2L73 4F A3WE 20040209001362004020900136WP 2004 2 9 ABXA040047 120040115A541199582203 RIB DOUG DC9 DC933F 302207AWP LT ENG PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 LEADING EDGE ASSEMBLY RIB WAS CRACKED. REPAIRED IAW DC-9 SRM K05159. 2L72 4F A6WE 20040209001392004020900139WP 2004 2 9 ABXA040051 120040120A2760 CONTROL CABLE DOUG DC9 DC915 3022036WP PEDESTAL LACK OF LUBE A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23927AX 45717 FLIGHT SPOILERS WERE BINDING IN FLIGHT. UNABLE TO DEPLOY. INSPECTED CABLES AND LINKAGE IN PEDESTAL. INSPECTED AND LUBRICATED CABLES AND MIXERS IN WHEEL WELLS AND CABLES IN FLAP WELLS. SYSTEM OPS CHECKED GOOD ON GROUND IAW DC-9 AMM 27-61-00-2-0102. 2L72 4F A6WE 20040209001442004020900144EA 2004 2 9 QXEA200400084 120040127A4930D98C07605 PRESSURE SWITCH CNDAIRCL600 CL6002C10 1390015EA ZONE 100 LEAKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09607QX5734 10024 MAINTENANCE FOUND A FUEL LEAK AT THE CENTER BAY, FORWARD WING TO FUSELAGE PANELS. MAINTENANCE FOUND THE APU FUEL PUMP PRESSURE SWITCH/SENSOR RELEASING A STEADY STREAM FROM THE WEEP HOLE WHEN THE PUMP WAS ON. THE PRESSURE SWITCH/SENSOR WAS REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040209001492004020900149 2004 2 9 SWIA200412812 420040124A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STALL WARNING INOPERATIVE A SWIAO OTHER PF NO WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07221SW8893 8893 120290 NR 1 STALL WARNING SYSTEM INOP. MEL 27-36-2. REPLACED STICK SHAKER ON CAPTAIN'S SIDE. OPS CHECKS GOOD IAW MM 27-34-04. 2L72 4T RTA31SO 20040209001512004020900151SO 2004 2 9 SWIA200412814 120040125A5415 ATTACH BRACKET EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07585SW 120353 RIGHT HYDRAULIC RESERVOIR OUTBOARD ATTACH BRACKET CRACKED. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED ATTACH BRACKET IAW EMB 51-10-06 AND 51-40-02. 2L72 4T RTA31SO 20040209001532004020900153 2004 2 9 SWIA200412816 420040123A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLIGHT CONTROL MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07587SW5408 5095 7062 RED FD ON BOTH PRIMARY FLIGHT DIRECTOR'S, FD1 FAIL STATUS MESSAGE AND YD1 INOP STATUS MESSSAGE IN FLIGHT. RETURNED TO SLC. REMOVED AND REPLACED NR 1 FCC 4000 CARD. OPS CHECKS GOOD IAW 22-11-00 AND 22-12-14. 2L72 4F4 FRTA21EA E15NE 20040209001562004020900156NM 2004 2 9 AALA20040151 120040129A3397 CONNECTOR BOEING757 757223 1384957NM CABIN DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21640A 24598 DFW EMERGENCY EXIT LIGHT MOUNTED ON SEAT 34D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT 34D SIDEWALL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040209001572004020900157WP 2004 2 9 04FDEA00250 120040130A2621AHL73691AHL7037 LINE DOUG DC10 DC1030 3023501WP ZONE 100 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25313FE 48311 NR 2 ENGINE FIRE-EX MANIFOLD CHECK VALVE FAILED FWD FLOW OPERATIONAL CHECK PER WORK CARD 26C2306. FOUND NR 2 ENGINE FIRE-EX WYE-FIREEX DISCHARGED LINE CRACKED, AND HOLE IN PIPE ASSY FOR OUTBOARD ENGINE FIRE-EX PIPE. REMOVED AND REPLACED P/N AHL7369-1 AND P/N AHL7037-1 WYE FIRE-EX Y-DUCT PER M/M 26-21-04-4, LEAK CHECK GOOD PER STEP 3. 2L73 4F A22WE 20040209001642004020900164SO 2004 2 9 C2XA04SH035 120040131A532014521725615 SILL EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001692004020900169SO 2004 2 9 C2XA04TY026 120040131A532014529991003 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS, DURING A SCHEDULED INSPECTION, THE FORWARD PARTITION ON LEFT SIDE UNDER THE CABIN FIBER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB-135/145 SRM 51-40-02/03 AND CMP51-21-04. 2L72 4F RTT00011AT 20040209001772004020900177SO 2004 2 9 C2XA04SH040 120040201A532014525480003 SILL EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE CARGO DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001812004020900181CE 2004 2 9 DXTA200400230 120040126A323315231007 ACTUATOR CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07308QS3839 5600277 AFTER TAKEOFF GEAR UNSAFE LIGHT AND HYDRAULIC PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED AIR TURNBACK AND LANDED SAFELY. REMOVED FAULTY LT MAIN GEAR ACTUATOR AND INSTALLED SERVICEABLE ACTUATOR, ADJUSTED CAMBER AND PERFORMED OPERATIONAL CHECK AND LEAK CHECK. ALL WORK DONE IAW CESSNA 560 MAINTENANCE MANUAL CHAPTER 32-31-04. 2L72 4F RTA22CE 20040209001942004020900194NM 2004 2 9 373PA0027 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 INTERCOSTAL 4 INCHES AFT OF STA 294 RBL 16 TO RBL 30 HAS CORROSION. FABRICATED INTERCOSTAL PER DRAWING 65-45834 AND INSTALLED. 2L72 4F RTA16WE 20040209001962004020900196NM 2004 2 9 373PA0030 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION ON INTERCOSTAL AT LEFT LAV DOOR IN AFT CABIN. REPLACED INTERCOSTAL PER SRM 51-40-02. 2L72 4F RTA16WE 20040209002092004020900209NM 2004 2 9 373PA0044 120040202A5320 WEB BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 WEB AT ENTRY TO AFT CARGO HAS NUT PLATE CORRODED OUT OF LIMITS. REPAIRED PER SRM 51-70-13. 2L72 4F RTA16WE 20040209002152004020900215NM 2004 2 9 373PA0047 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION ON INTERCOSTAL AT RIGHT LAVATORY DOOR. FABRICATED NEW INTERCOSTAL PER DRAWING 65-46812 AND INSTALLED PER SRM 51-10-2. 2L72 4F RTA16WE 20040209002482004020900248WP 2004 2 9 04FDEA00258 120040201A5753ARC2177 CARRIAGE DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25550FE 46521 COMPLY WITH EA 8-5750-73878. WINGS - OUTBD FLAP SPINDLE CARRIAGE FITTING CORROSION REPAIR P/N ARC2177. CLOSING ACTION ON 02-01-04. ON N/R S00014. COMPLIED WITH EA 8-5750-73875. 2L73 4F A22WE 20040209002602004020900260NM 2004 2 9 04FDEA00271 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002642004020900264NM 2004 2 9 04FDEA00274 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) INBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002722004020900272NM 2004 2 9 04FDEA00282 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002732004020900273NM 2004 2 9 04FDEA00283 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002752004020900275SO 2004 2 9 C2XA04SH042 120040203A531514525422003 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE RIGHT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOORBEAM BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209002762004020900276CE 2004 2 9 58501 120040202A7603 SOLENOID BEECH 1900 1900D 1154162CE LOW PITCH DIRTY A AMWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07231YV UE231 ON TAKEOFF ROLL IN TAMPA FLORIDA ON FLIGHT 5536, THE LT ENGINE POWER LEVER FULL FORWARD WOULD ONLY GO TO 2000 LBS OF TORQUE AND 1500 PROP RPM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE LOW PITCH SOLENOID. NO PARTS WERE USED. 2L72 4T RTA24CE 20040210000522004021000052NM 2004 2 10 2004UALA00001 120040103A2782755299 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 3 JAMMED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29574UA 26686 AFTER TAKEOFF WITH FLAP HANDLE SELECTED TO UP HAD A LE EDGE SLAT DISAGREE MESSAGE AND LIGHT. FOUND JAMMED NR 3 LEADING EDGE (LE) SLAT ROTARY ACTUATOR. JAMMING WAS ATTRIBUTED TO EXCESSIVE TORQUE LOADING IN THE LE SLAT DRIVE TORQUE TUBE SYSTEM. NR 3 ROTARY ACTUATOR WAS REPLACED, THE NR 5 ACTUATOR WAS ALSO REPLACED AS PRECAUTION BECAUSE OVERLOAD INDICATOR WAS FOUND TRIPPED. LUBRICATED THE LE SLAT SYSTEM. 2L72 4F4 FRTA2NM E17NE 20040210000532004021000053NM 2004 2 10 04FDEA00286 120040202A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM AT FASTENER HOLES BS 344 LBL 59 - RBL 17 WL 208. REMOVED CORROSION AREAS 77 X 2 X .040 INCHES FROM ORIGINAL .100. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPALCED UPPER CHORD OF FLOORBEAM BS 344 LBL 65 TO RBL 65 PER SRM 51-30-02 AND FED-EX SR 27-53-007 2L73 4F RTA3WE 20040206002082004020600208EA 2004 2 6 COMA0460086 120040122A5210601R383831 BELLCRANK CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01708CA 7235 FLIGHT 5681 CABIN DOOR WARNING MESSAGE. REPLACED THE DOOR UPPER BELLCRANK ASSY. 2L72 4F RTA21EA 20040206002122004020600212NM 2004 2 6 QXEA200400053 120040120A33506038443 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09364PH7372 524 SEA- FORWARD 2 LIGHTS ON FLOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY AND BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040206002142004020600214SO 2004 2 6 C2XA04CL006 120040122A3350110049 CHARGER EMB 145 EMB145XR 3260214SO EMERGENCY EXIT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718120 145681 CLE FLIGHT 2230 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040206002292004020600229NM 2004 2 6 AWXA200400090 120040107A5340693535214 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK AND CORROSION WAS FOUND ON STRINGER TIE CLIP AT BS 500C, STR 26 RT. MAINTENANCE REMOVED CRACKED & CORRODED STRINGER TIE CLIP AT BS 500C, STR 26 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2L72 4F RTA16WE 20040209000032004020900003SO 2004 2 9 RAIA00401015 120040111A801232153581 START VALVE EMB 145 EMB145 3260210SO LT ENGINE STUCK A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03820HK11638 145064 5700-PHL- LEFT ENGINE HANGS UP AT 31 PERCENT N2 AND WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR START VALVE. 2L72 4F RTT00011AT 20040209000092004020900009SO 2004 2 9 RAIA00401021 120040115A531514521699003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK7617 145256 MX-STL- DURING HEAVY CHECK FOUND LT FLOORBEAM WITH CORROSION BEYOND BENDABLE LIMITS. REMOVED AND REPLACED LT FLOORBEAM. 2L72 4T RTT00011AT 20040209000122004020900012SO 2004 2 9 RAIA00401024 120040124A32405256550 TRANSDUCER EMB 145 EMB145 3260210SO MLG BRAKE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03801HK13417 145053 BRAKE DISAGREE MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE PRESSURE TRANSDUCER. 2L72 4F RTT00011AT 20040209000162004020900016 2004 2 9 181161 420040128A3414 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE COCKPIT ERRATIC A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17118SD 118 151 DRG936587 ON 01-28-04, APPROX 1535 (UTC), FLT 4501 PIT-LEX, AIRCRAFT RETURN TO FIELD WHEN THE CAPTAIN'S AIRSPEED INDICATOR HAS ERRATIC READING ALONG WITH THE RUDDER LIMIT ILLUMINATED ON THE CWP. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040209000232004020900023EU 2004 2 9 MALA040136 120040123A3020 WARNING LIGHT SAAB SF340 340B 7860101EU INTAKE HEAT FALSE INDICATIONA MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15424XJ 424 DURING FLIGHT 2999/2798, RT INTAKE HEAT LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO DTW. MAINTENANCE PERFORMED VISUAL INSPECTION OF ALL DUCTING. NO DEFECTS NOTED. PERFORMED 1 HOUR GROUND RUN OF SYSTEM WITH NO FAULTS NOTED. COULD NOT DUPLICATE DISCREPANCY. ALL CHECKS GOOD. REF SAAB AMM CH 30/71. 2L72 4T RTA52EU 20040209000252004020900025EU 2004 2 9 MALA040140 120040124A3260 UPLOCK SENSOR BAC 146 AVRO146RJ85A1500097EU MLG SEPARATED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15516XJ E2334 DURING FLIGHT 3666, INFLIGHT AFTER TAKEOFF FROM MEM, RT GEAR INTRANSIT LIGHT AND RED HANDLE ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE FERRIED TO MSP FOR FURTHER T/S AND REPAIR. MX REINSPECTED RT UPLOCK SENSOR FOUND BACKSHELL AT UPLOCK SENSOR RT MAIN GEAR COMPLETELY OFF CONNCTOR. CLEANED BACKSHELL AND CONNECTOR, REINSTALLED BACKSHELL AND PERFORMED TEST OF SENSOR OPERATION REF 32-60-17 501. TEST PASSES; OK FOR SERVICE. 2H74 4F RTA49EU 20040209000362004020900036WP 2004 2 9 AALA20040134 120040127A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21434AA 49452 RDU EMERGENCY PATH LIGHT AT ROW 15D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FOR ROW 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040209000492004020900049NM 2004 2 9 CALA0400063 120040126A5320 FLOOR SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716234 28946 INSPECTION FOUND FORWARD PIT FLOOR SUPPORT ANGLE CORRODED AT STA 500I. A NEW FLOOR SUPPORT ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040209000502004020900050NM 2004 2 9 CALA0400064 120040126A5320 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716234 28946 INSPECTION FOUND AFT PIT LT ZEE CHANNEL CORRODED AT STA 727+4 TO 847. A NEW ZEE CHANNEL WAS INSTALLED IAW SRM 53-00-53, PAGE 201. 2L72 4F RTA16WE 20040209000572004020900057EU 2004 2 9 AWXA200400096 120040127A2932501310000 PRESSURE SWITCH AIRBUS320 A320231 3930325EU NR 1 ENGINE CRACKED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28631AW 077 LAS - EMERGENCY LANDING - FLT 0868 - ON DESCENT INTO LAS EN ROUTE FROM EWR RECEIVED CLASS 1 ECAM FAULT GREEN HYDRAULIC NR 1 ENGINE PUMP LOW PRESSURE, THIS WAS FOLLOWED BY ECAM FAULT FOR GREEN HYDRAULIC RESERVOIR LOW LEVEL, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND NR 1 ENGINE DRIVEN PUMP (EDP) PRESSURE SWITCH (1074GK) CRACKED AND LEAKING. REMOVED AND REPLACED NR 1 EDP PRESSURE SWITCH (1074GK) IAW AMM 29-11-17, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040209000692004020900069NE 2004 2 9 QXEA200400066 220040126A73204120T00P10 FADEC BOMBDRDHC8 DHC8401 1390041NM GE CF34 CF348C1 NE ZONE 400 INOPERATIVE A QXEAO OTHER X ENGINE FLAMEOUT LDLANDING 1 NM09612QX87 10042 GEE965300 SJC-ON FLIGHT NUMBER 2457, JUST AFTER TOUCHDOWN THE RIGHT FADEC CAUTION MESSAGE CAME ON FOLLOWED BY THE RIGHT ENGINE FLAME OUT CAUTION MESSAGE. AFTER STOWING THE REVERSER LEVERS THE RIGHT REVERSER UNLOCKED CAUTION MESSAGE APPEARED. AFTER ENGINE SHUTDOWN THE RIGHT IGNITION-B FAULT STATUS MESSAGE CAME ON. REMOVED AND REPLACED NR 2 FADEC. OPERATED ENGINE AT SEVERAL POWER SETTINGS, SEVERAL TIMES AND DEPLAYED THRUST REVERSERS SEVERAL TIMES. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 FRTA13NM EOOO63EN 20040209000712004020900071CE 2004 2 9 58090 120040120A3260727725 WARNING HORN BEECH 1900 1900D 1154162CE MLG INTERMITTENT A AMWAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE07161YV UE161 ON APPROACH TO FKL, THE CREW REPORTED MAIN LANDING GEAR INDICATOR INTERMITTENT AND REQUESTED TO RETURN TO PIT. CREW REPORTED GOOD INDICATION AND LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED GEAR WARNING HORN SILENCE SWITCH/CB P/N 7277-2-5, P/N 02006. 2L72 4T RTA24CE 20040209000752004020900075NM 2004 2 9 0400136642 120040127A3350 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01642NW 21942 DURING LINE CHECK, FOUND ZONE E-FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040209000802004020900080NM 2004 2 9 AWXA200400111 120040103A52106545871110 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.0625 INCH CRACK WAS FOUND ON R-1 DOOR FRAME AT 3RD STOP CUTOUT FROM BOTTOM ON AFT EDGE BS 328, STR 14 RT. MAINTENANCE STOP DRILLED CRACK ON R-1 DOOR FRAME AT 3RD STOP CUTOUT FROM BOTTOM BS 328, STR 14 RT; PERFORMED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11 FIG 1 PG 1-6. 2L72 4F RTA16WE 20040209000882004020900088NM 2004 2 9 AWXA200400119 120040109A5210655287415 FRAME BOEING737 737301 1384611NM PAX DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1.1875 INCH CRACK WAS FOUND ON R-2 DOOR FORWARD FRAME SURROUND WEB BELOW DOOR ASSIST HANDLE BRACKET, BS 948, RBL 62, WL 251. MAINTENANCE REMOVED CRACKED SECTION OF R-2 DOOR WEB BELOW DOOR ASSIST HANDLE BRACKET, BS 948, RBL 62, WL 251; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-52874; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 14. 2L72 4F RTA16WE 20040209000942004020900094NM 2004 2 9 04FDEA00242 120040128A21215007024620 FAN BOEING727 727100 1384036NM AIR DISTRIBUTIONMALFUNCTIONED A FDEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO25189FE4581 4581 19082 ACRID BURNING ODOR WHEN GASPER FAN IS TURNED ON. MAINTENANCE WAS NOTIFIED AND NOTICED AN UNUSUAL SOUND WHEN GASPER FAN WAS TURNED ON. REMOVED AND REPLACED GASPER FAN, OPS CHECK GOOD PER 727-100 MM 21-23-011-4. 2L73 4F RTA3WE 20040209001022004020900102 2004 2 9 SWIA200412805 420040116A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AUTO PILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07579SW5868 5868 120347 ON TAXI OUT, SELECTED AP TO F/O. RECEIVED AP FAIL LIGHT ON MAP AND ASSOCIATED AP DIS & AP ON FCP. REPLACED F/O'S AP COMPUTER. OP CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040209001062004020900106NM 2004 2 9 QXEA200400079 120040127A5740 MOUNT DHAV DHC8 DHC8202 2809007NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX- UPPER OUTBOARD FITTING FOR MOUNT SCREW OF LEADING EDGE 511 AL IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040209001232004020900123NM 2004 2 9 AWXA200400122 120040108A53206546812188 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT UPPER TEE BETWEEN BS 1006-1016, RBL 8, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 1006 TO BS 1016, RBL 8; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812-188; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12 PG 1, 38 & 45. CORROSION LEVEL DETERMINATION CHANGED FROM LEVEL II TO LEVEL 1 DUE TO AREA WAS PREVIOUSLY REWORKED. 2L72 4F RTA16WE 20040209001302004020900130NM 2004 2 9 CALA0400068 120040129A5230 CROSSBEAM BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND A 2 INCH RACK AT LOWER FORWARD END OF AFT CARGO DOOR NR 5 CROSS BEAM TEE EXTRUSION. THE AFT CARGO DOOR WAS REMOVED AND A NEW DOOR WAS INSTALLED AND ADJUSTED. OPERATIONAL CHECKS WERE GOOD IAW MM 52-30-00. 2L72 4F RTA16WE 20040209001352004020900135EA 2004 2 9 QXEA200400083 120040127A2710601R593221 POWER SUPPLY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 FAILED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09614QX5173 5173 10049 SEA - FLIGHT 2462 - THE AILERON AND RUDDER TRIM INDICATORS SHOW VERY SLOW UNCOMMANDED TRIM MOTION. MAINTENANCE REPLACED THE RUDDER/AILERON TRIM POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040209001542004020900154 2004 2 9 SWIA200412817 420040129A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07563SW 120338 AUTO PILOT AURAL WARNING AND TRIPLE CHIME WHEN SELECTED TO F/O SIDE. INSTALLED SERVICEABLE APC-65. OPS CHECK GOOD. S/N OFF: 2736. 2L72 4T RTA31SO 20040209001602004020900160NM 2004 2 9 04FDEA00247 120040129A3297 WIRE BOEING727 727200 138407ENM NLG INDICATOR BROKEN A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25223FE 20935 RED NOSE GEAR UNSAFE LIGHT ON FOLLOWING GEAR RETRACTION; FOLLOWED RED TABS & RETURNED TO VLN FOR LANDING. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH & POSITION SWITCH. PERFORMED ADJUSMENT/TEST, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSMENT/TEST AS PER MM 32-61-071-4 AND DIDN'T HELP. ALSO PERFORMED WIRING CHECK BETWEEN LOCK SWITCH AND NOSE GEAR WHEEL WEEL CANNON PLUG AND FOUND WIRE C-BROKEN. FIXED WIRE-C AS PER 727-200 SWPM. REINSTALLED ORIGINAL LANDING GEAR ACCESSORY UNIT. PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSMENT/TEST, AND NOSE GEAR RED LIGHT WORKED PROPERLY WITH LANDING GEAR IN UP POSITION. 2L73 4F RTA3WE 20040209001632004020900163SO 2004 2 9 C2XA04SH034 120040131A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040209001782004020900178SO 2004 2 9 C2XA04SH041 120040202A531514525381003 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE LEFT HAND MIDDLE FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE CARGO AREA FROM FRAME 65 TO FRAME 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040209001872004020900187CE 2004 2 9 DXTA200400223 120040123A3260 BULB CESSNA560 560XL 2076702CE MLG INDICATOR BURNED OUT E DXTAA UNSCHED LANDING P NO WARNING INDICATION DEDESCENT 1 GL07697QS 5605197 DURING EN ROUTE TO SMO, THE RIGHT MAIN LANDING GEAR INDICATION WOULD NOT SHOW DOWN AND LOCK. PERFORMED MANUAL LANDING GEAR EXTENSION AND DIVERTED TO LAX, AIRCRAFT LANDED SAFELY. JACKED AIRCRAFT, RESET EMERGENCY GEAR RELEASE HANDLE TO NORMAL, TROUBLESHOT MLG INDICATION SYSTEM AND FOUND LIGHT BULBS BURNED OUT. INSTALLED NEW BULBS 6 EACH, SERVICED BLOW DOWN BOTTLE IAW CESSNA MM CHAPTER 12-13-01. ACCOMPLISHED GEAR SWING, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20040209001932004020900193NM 2004 2 9 373PA0026 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 INTERCOSTAL CORRODED RBL 10 STA 312 TO STA 328. FABRICATED NEW INTERCOSTAL PER DRAWING 65-45834 AND INSTALLED. 2L72 4F RTA16WE 20040209001972004020900197NM 2004 2 9 373PA0031 120040202A5315 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION ON STA 986.5 FLOORBEAM FROM INTERCOSTAL TO INTERCOSTAL. REPAIRED FLOORBEAM PER PACE AIRLINES REPAIR PROCEDURE REPORT, EA 53-010. 2L72 4F RTA16WE 20040209002022004020900202NM 2004 2 9 373PA0035 120040202A5330 PANEL BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 FWD, CENTER, AND AFT PANELS OF THE AFT CARGO DOOR THRESHOLD ARE CRACKED. REPAIRED PER SPM 20-3 AND BOEING PROCESS SPEC BAC5975. 2L72 4F RTA16WE 20040209002052004020900205NM 2004 2 9 DHL2004752001 120040131A3350 LIGHT BOEING727 727223 1384074NM COCKPIT DISLODGED A DHLAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SO01752DH 22466 COCKPIT EMERGENCY EXIT LIGHT FELL DURING FLIGHT. RE-SECURED COCKPIT EMERGENCY EXIT LIGHT, CHECKED GOOD IAW B-727 M/M 33-50-101. 2L73 4F A3WE 20040209002122004020900212NM 2004 2 9 UPS04641796 120040202A5753 RIB BOEING767 767300 1385204NM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01326UP 27752 RIGHT INBOARD TRAILING EDGE FLAP OUTBOARD CLOSURE RIB CRACK. ACCOMPLISHED PERMANENT REPAIR PER EO B767-5750-19900B THIS CLEARS D275 213. REFERENCE LP604020. 2L72 4F RTA1NM 20040209002202004020900220EU 2004 2 9 DHL2004365513 120040107A5315 FLOORBEAM AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH EXFOLATING CORROSION AT BOTTOM OF FLOOR BEAM FRAME 27 BELOW AFT END OF CARGO LOADING ROLLER AT 40 FT RT OF CENTER LINE. REMOVED CORROSION. FOUND OUT OF LIMITS .050 MAT LOSS. ACCOMPLISHED UT THICKNESS CHECK AFTER CORROSION REMOVED MAX THICKNESS FOUND .090. CUT OUT DAMAGE AREA OF THE CAP BEAM IAW A300 SRM 53-10-10, FABRICATED REPAIR PARTS FROM EXTRUSION P/N 60-14597 7075T6, PO 23488255 24 INCHES FILLER AND 2 SPLICES 10 INCHES EA IAW A300 SRM 53-10-10, TREATED AND PRIMED REPAIR PARTS IAW A300 SRM 51-40-11. INSTALLED TOP CAP BEAM REPAIR IAW A300 SRM 53-10-10. CUT OUT SECTION DAMAGED SECTIONS OF TOP CAP (FLOOR SUPPORT) BETWEEN RBL 18 TO RBL 43, FR 27. 2L72 4F RTA35EU 20040209002312004020900231WP 2004 2 9 AALA20040162 120040131A5280 LATCH DOUG DC9 DC982 3022082WP MLG DOOR INOPERATIVE A AALAO OTHER O OTHER CLCLIMB 1 SW21232AA 49179 IAH - INFLIGHT T1428/31, GEAR DOWN WOULD NOT RETRACT AFTER TAKEOFF. CREW RETURNED GEAR HANDLE TO DOWN POSITION AND FLEW GEAR DOWN TO DFW. LANDED WITHOUT INCIDENT. REPLACED GEAR DOOR BYPASS HANDLE LATCH ASSEMBLY AND RIGHT MAIN LANDING GEAR DOOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002322004020900232NM 2004 2 9 AALA20040163 120040131A2822 PUMP BOEING767 767323 1385205NM FUEL BOOST INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21352AA 24033 LAX INFLIGHT T283/31, AT CRUISE ALTITUDE TURNED ON CENTER PUMPS. BOTH PUMPS FAILED TO OPERATE. RETURNED TO LAX. LANDED WITHOUT INCIDENT. REPLACED LEFT AUXILLARY TANK OVERRIDE BOOST PUMP PER MM 28-22-05. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040209002412004020900241SO 2004 2 9 RAIA00401030 120040115A531114521721005 STRAP EMB 145 EMB145LR 3260212SO FRAME CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK 145256 MX-STL- DURING BLOCK CHECK FOUND FORWARD STRAP AT FRAME 14 CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED FORWARD STRAP DIGITAL AT FRAME 14. 2L72 4T RTT00011AT 20040209002452004020900245WP 2004 2 9 04FDEA00255 120040131A5753ARC1984 HINGE DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-5750-73872. WINGS - LT OUTBD FLAP, INBD HINGE ASSY ARC1984, PIVOT BORE REWORK. CLOSING ACTION ON 01/30/04, ON N/R S00013. COMPLIED WITH EA 8-5750-73872. 2L73 4F A22WE 20040209002502004020900250NM 2004 2 9 04FDEA00260 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD (3) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75238 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040209002672004020900267NM 2004 2 9 04FDEA00277 120040202A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000102004021100010NM 2004 2 11 USAASB04008 120040116A3234A42006028305 SOLENOID BOEING737 7374B7 1384702NM LEVER LATCH FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19440US 24811 AFTER TAKEOFF FROM BOS, EN ROUTE TO CLT, CREW COULD NOT GET THE LANDING GEAR RETRACTED. THE LANDING GEAR LEVER WOULD NOT MOVE PAST THE NEUTRAL POSITION. CREW PLACED GEAR LEVER DOWN AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE OPERATED GEAR. GEAR CHECKS NORMAL. REMOVED AND REPLACED LANDING GEAR LEVER LATCH SOLENOID AND NOSE AIR/GROUND SENSING RELAY R276 (P/N BACR13CG2AB) AS PRECAUTIONARY. OPERATED GEAR SEVERAL MORE TIMES. ALL CHECKS NORMAL. (M) 2L72 4F RTA16WE 20040211000242004021100024NM 2004 2 11 USAASB04001 120040101A2752569670 MOTOR BOEING737 7373B7 1384580NM TE FLAP FAILED A USAALA ABORTED APPROACH UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 EA19391US32390 23313 DURING APPROACH, CREW REPORTED LE & TE FLAPS WOULD NOT EXTEND. CREW RECYCLED CIRCUIT BREAKERS PER MAINT CONTROL REQUEST, BUT CONDITION REMAINED. FLT DIVERTED AS CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PRECEDURES FOR ALTERNATE FLAP EXTENSION. FLT LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINT R & R FLAP POSITION INDICATOR, AS PRECAUTION, PER MM. OPS CHECK GOOD. UNFORTUNATELY, PROBLEM REOCCURED NEXT DAY. CREW ACCOMPLISHED PROCEDURES FOR ALTERNATE FLAP EXTENSION. FLT LANDED WITHOUT INCIDENT. MAINTENANCE R & R TE FLAP HYD MOTOR. OPERATIONAL CHECK OF FLAPS GOOD. ALSO, LUBRICATED TE FLAP BALLSCREWS IN ASSOCIATION WITH MM. (M) 2L72 4F RTA16WE 20040211000252004021100025NM 2004 2 11 USAABB04007 120040115A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROW 23 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19632AU 27810 FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040211000262004021100026NM 2004 2 11 USAABB04006 120040115A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19632AU 27810 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20040211000302004021100030NM 2004 2 11 AMTA200400030 120040109A335070036611 BALLAST BOEING737 73783N 13844HINM EMERGENCY LIGHT FAILED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11306TZ 32348 FOUND LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BALLAST AS REQUIRED CHECKS GOOD. (M) 2L72 4F RTA16WE 20040211000322004021100032NM 2004 2 11 AMTA200400047 120040119A5330 PANEL BOEING737 73783N 13844HINM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11302TZ 32576 FOUND C-2 CARGO PANELS HAVE SURFACE CORROSION STATION 792 TO FORWARD BULKHEAD. CORROSION OUT OF LIMITS ON PANEL FROM STATION 767 TO 887. FABRICATED NEW PANEL, COATED AND INSTALLED NEW CARGO FLOOR PANEL IAW 727 SRM 51-40-02-0 AND AMM 25-52-10-400-801. (M) 2L72 4F RTA16WE 20040211000332004021100033WP 2004 2 11 AMTA200400025 120040108A3350516574 CHARGER LKHEED1011 10113853 5265020WP EMERGENCY LIGHT FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 FOUND RIGHT EMERGENCY DOOR AND R3 DOOR EXT EGRESS LIGHTS OUT. REMOVED AND REPLACED POWER PACK AT R3 DOOR IAW MM 33-51-03. EGRESS LIGHTS AND POWER PACK, OPS CHECK GOOD. (M) 2L73 4F A23WE 20040211000342004021100034NM 2004 2 11 AMTA200400048 120040119A5230 SKIN BOEING737 73783N 13844HINM CARGO DOOR GOUGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11302TZ 32576 FOUND TWO GOUGES ON THE C1 CARGO DOOR, BOTH VERTICALLY 7 INCHES AND 4.1, 8 LONG IN ADJACENT BAYS. COMPLY WITH ERA 737-52R-5423 FOR REPAIR. COMPLIED WITH ERA 737-52R-5423. GOUGES CUT OUT AND DOUBLER INSTALLED IAW ERA. (M) 2L72 4F RTA16WE 20040211000362004021100036WP 2004 2 11 AMTA200400024 120040108A33505165741 CHARGER LKHEED1011 10113853 5265020WP EMERGENCY LIGHT FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 FOUND LEFT EMERGENCY DOOR AND L3 DOOR EXT EGRESS LIGHTS OUT. REMOVED AND REPLACED POWER PACK AT L3 DOOR IAW MM 33-51-03. EGRESS LIGHTS AND POWER PACK, OPS CHECK GOOD. (M) 2L73 4F A23WE 20040211000372004021100037SO 2004 2 11 SIMA200401803 120040116A3230355022002 ECU EMB 135 EMB135LR 3260305SO MLG INOPERATIVE A SIMAO OTHER J WARNING INDICATION CLCLIMB 1 SW21710TB 145224 CREW REPORTED THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE FOUND FIVE FAULTS LOADED IN THE CENTRAL MAINTENANCE COMPUTER. THE LANDING GEAR ELECTRONIC UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040211000402004021100040SO 2004 2 11 SIMA200400702 120040106A27503632001003 PDU EMB 145 EMB145LR 3260212SO TE FLAPS INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21644AE 145204 DURING CRUISE FLIGHT CREW REPORTED A FLAP FAIL MESSAGE ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP POWER DRIVE UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040211000462004021100046GL 2004 2 11 CHQA000433 220040131A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FAILED A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL11290 145474 CAE311464 DURING CLIMBOUT OF LGA AT 10,000 FT CREW HEARD A POP WITH IMMEDIATE LOSS OF THRUST ON NUMBER 2 ENG. EICAS INDICATED A SPOOL DOWN WITH RAPIDLY RISING ITT. BROUGHT THRUST LEVER TO IDLE AS ITT REACHED 1050 DEGREES. ITT REDUCED AND ENGINE WAS SHUT DOWN. NO OTHER ABNORMALITIES NOTED. RETURNED TO LGA WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. LEAK AND OPERATIONAL CHECKS GOOD. NO DEFECTS NOTED. TEARDOWN INSPECTION REVEALED THAT THE ENGINE HAD EXPERIENCED 1ST STAGE NGV BURN THROUGH WHICH WAS THE ROOT CAUSE OF THE EVENT. THE CONDITION LED TO FAILURE OF A HPT-1 TURBINE BLADE WHICH CAUSED DAMAGE TO THE HPT-2 VANES AND BLADES. 2L72 4T4 FRTT00011ATTE6CH 20040211000472004021100047NM 2004 2 11 DHL2004754001 120040203A3210656021132 ACCESSORY UNIT BOEING727 727223 1384074NM MLG FAILED A DHLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01754DH 22008 GEAR HANDLE WOULD NOT GO UP PAST OFF. PERFORMED ABNORMAL PROCEDURE. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B-727 M/M 32-09-121. OPS CHECKED GOOD. 2L73 4F A3WE 20040211000512004021100051EA 2004 2 11 COMA0460099 120040131A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01967CA 7134 FLIGHT 5868 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040211000522004021100052EA 2004 2 11 COMA0460100 120040131A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYS SYS MALFUNCTIONED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01991CA14499 7216 FLIGHT 5898 GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20040211000532004021100053EA 2004 2 11 COMA0460101 120040201A2410755469C IDG CNDAIRCL600 CL6002B19 1900309EA LT ENGINE INOPERATIVE A COMAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01983CA19184 7169 FLIGHT 5406 LT ENGINE IDG AND GENERATOR CAUTION MESSAGE. REPLACED THE IDG. 2L72 4F RTA21EA 20040211000542004021100054EA 2004 2 11 COMA0460102 120040201A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 9-11 INOPERATIVE A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01487CA 7729 FLIGHT 5158 EMERGENCY LIGHTS INOP ROWS 9 THRU 11. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040211000562004021100056NM 2004 2 11 QXEA200400095 120040202A3260 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM MLG ILLUMINATED A QXEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 NM09363PH 520 THE CREW PERFORMED A PRECAUTIONARY GO-AROUND WHEN ON APPROACH, DID NOT GET A GREEN AND AMBER NOSE GEAR INDICATIONS. MAINTENANCE INSPECTED THE AIRCRAFT AND NOSE GEAR INDICATION SYSTEM. RESET BOTH THE NOSE GEAR DOWN AND LOCKED INDICATION, AND NOSE GEAR CYCLE INDICATION LAMP ASSEMBLIES. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040211000602004021100060EU 2004 2 11 2004UALA00069 120040127A2910 YOKE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYD MOTOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29457UA 1146 FLIGHT DIVERTED TO DEN AND CANCELLED DUE TO BLUE HYDRAULIC SYSTEM OVERHEATING. REPLACED BLUE SYSTEM HYDRAULIC PUMP. THE GUIDE YOKE BEARING FAILED IN THE MOTOR. 2L72 4F4 FRTA28NM E40NE 20040211000662004021100066NM 2004 2 11 04FDEA00292 120040203A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000672004021100067NM 2004 2 11 04FDEA00293 120040203A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000692004021100069NM 2004 2 11 04FDEA00295 120040203A5753 ROD DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000702004021100070EU 2004 2 11 04FDEA00298 120040203A27601225P422 SWITCH AIRBUS300 A300F4605R 3930327EU SPOILER MALFUNCTIONED A FDEACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO25663FE 766 REJECTED TAKEOFF AT 50 KNOTS FOR SPOILER FAULTS 3 & 2, 5 ON ECAM. REMOVED AND REPLACED YELLOW SYS SERVO PRESSURE SWITCH PER A300 MM 27-14-18-4, OPS CHECK GOOD OK FOR SERVICE. 2L72 4F RTA35EU 20040211000712004021100071NM 2004 2 11 04FDEA00299 120040203A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP LEADING EDGE LOCATION STOP FITTING ISLAND CRACKED. LT WING OUTBOARD FLAP LEADING EDGE LOCATION CRACKED STOP FITTING REMOVED AND REPLACED WITH NEW STOP FITTING AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040211000722004021100072NM 2004 2 11 04FDEA00300 120040203A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP LEADING EDGE LOCATION STOP FITTING ISLAND CRACKED. RT WING OUTBOARD FLAP LEADING EDGE LOCATION CRACK STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II AND SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040211000732004021100073NM 2004 2 11 04FDEA00301 120040203A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75240. TRAILING EDGE & TRAILING EDGE DEVICES. LT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040211000742004021100074NM 2004 2 11 04FDEA00302 120040203A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75240, TRAILING EDGE & TRAILING EDGE DEVICES. LT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040211000762004021100076SO 2004 2 11 C2XA04CL008 120040130A33503017 LIGHT EMB 145 EMB145 3260210SO FUSELAGE INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040211000772004021100077NM 2004 2 11 XNOA1175 120040203A3260 PROXIMITY SWITCH BOEING727 727200 138407ENM MLG MALFUNCTIONED A XN0AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL2376753 21249 RIGHT GEAR LIGHT REMAINS ON AFTER GEAR-UP, FOLLOW AS PER FOM. REMOVED AND REPLACED RT MLG PROX SWITCH IAW B727 MM 32-61-21, NO HELP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW B727 MM 32-09-111. PERFORMED OPERATIONAL GEAR SWING IAW B727 MM 7-11-0 & 32-31-1, NO DEFECTS NOTED AT THIS TIME. 2L73 4F RTA3WE 20040211000782004021100078WP 2004 2 11 IXXA0400009O 120040203A5230 DOOR DOUG DC8 DC873F 302199FWP CARGO BAY UNSECURE A IXXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW11603AL918842885 46003 CREW HAD MASTER WARNING LIGHT/BELLY DOOR LIGHT AT 90 KNOTS. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINTENANCE COMPLIED WITH REJECTED TAKEOFF INSPECTION AND NO DEFECTS WERE NOTED. MAINTENANCE THEN INSPECTED BELLY DOORS AND FOUND THE -B- PIT DOOR AJAR. THE DOOR WAS CYCLED AND BELLY DOOR LIGHTS SYTEMS TESTED NORMAL PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040211000822004021100082EA 2004 2 11 SWIA200412821 120040129A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07918SW1778 1778 7645 FLAPS FAIL AT -0- WHEN SELECTED. REMOVED AND REPLACED RIGHT AND LEFT FLAP BPSU, LEFT FLAP ACTUATOR IN THE NUMBER 3 POSITION AND THE RIGHT NR 3 FLAP ACTUATOR. RIGHT BPSU S/N OFF: 0801, ACTUATOR P/N: 853D100-19, LEFT S/N OFF: 1945. RIGHT S/N OFF: 1941. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040211000832004021100083SO 2004 2 11 SWIA200412822 120040129A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07188SW1445 252 120039 IN FLIGHT, RECEIVED CONTROL FAULT-FLAP, ADVANCED SWS ON MAP, NO LIGHTS ON FLAP PANEL. TRIED TO RESET PER QRH WITHOUT SUCCESS. REPLACED FLAP ANNUNCIATOR. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040211000852004021100085 2004 2 11 SWIA200412825 420040127A34606229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07407SW6567 6567 7034 AUTOPILOT DISCONNECTED INFLIGHT, HAD FD2 INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED FCC 2 WITH A SERVICEALBLE UNIT IAW MM 22-12-14. OPS CHECK. 2L72 4F RTA21EA 20040211000862004021100086EA 2004 2 11 SWIA200412826 120040127A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA YOKE PITCH TRIM MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07915SW 7615 ON CLIMBOUT LOST STAB AND MACH TRIM, WOULD NOT RE-ENGAGE. RETURNED TO FIELD. ON APPROACH MOMENTARILY GOT TRIM BACK THEN LOST IT AGAIN. REMOVED AND REPLACED CAPTAIN'S YOKE PITCH TRIM DISCONNECT SWITCH IAW CRJ AMM 27-41-30. P/N ON: 996-0013. 2L72 4F RTA21EA 20040211000872004021100087EA 2004 2 11 SWIA200412827 120040127A27603G5209C CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07405SW 7029 IN FLIGHT, THE FLIGHT SPOILER FAULT MESSAGE CAME ON. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW AMM 27-61-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040211000922004021100092EU 2004 2 11 MALA040141 120040127A3020 VALVE BAC 146 AVRO146RJ85A1500097EU ANTI ICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15521XJ E2346 DURING FLIGHT 3453/3505 THE NR 4 ENGINE INTAKE LOW PRESSURE LIGHT ILLUMINATED. A/C RETURNED TO DTW. REMOVED AND REPLACED INTAKE ANTI-ICE VALVE, ALL CHECKS GOOD. REMOVED AND REPLACED INTAKE ANTI-ICE VALVE ALL CHECKS GOOD AT THIS TIME. 2H74 4F RTA49EU 20040211000942004021100094EU 2004 2 11 MALA040144 120040125A5280 DOOR SAAB SF340 340B 7860101EU NLG BENT A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING MAINTENANCE WALK AROUND, NOTED RT TRAILING EDGE NOSE GEAR DOOR BENT. MAINTENANCE REPAIRED, DAMAGE IS NEGLIGABLE. ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20040211000962004021100096EU 2004 2 11 MALA040143 120040127A7603 HOUSING SAAB SF340 340B 7860101EU CONTROL CABLE CONTAMINATED A MALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL15411XJ 340B411 DURING FLIGHT 3011 INFLIGHT RT POWER LEVER STUCK. WHILE ATTEMPTING TO MOVE RT POWER LEVER HAD LOTS OF RESISTANCE AND SPRUNG BACK TO ORIGINAL STUCK POSITION. PILOT MOVED RT BACK AND FORTH AND WAS ABLE TO REDUCE ENGINE TORQUE TO 20-25 PERCENT FOR LANDING. ONCE ON THE GROUND RT POWER LEVER MOVED FULL TRAVEL BUT WITH SOME RESISTANCE. MAINTENANCE FOUND WATER IN CONTROL CABLE HOUSING REMOVED WITH NITROGEN PRESSURE. CABLE APPEARS CLEAN RAN ENGINE THROTLLE AND MOVEMENT IS OK. GOOD FOR SERVICE. 2L72 4T RTA52EU 20040211000972004021100097NE 2004 2 11 AALA20040164 220040202A7314HTE690001 PRESSURE SWITCH AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE FUEL PUMP INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217082A 643 SJU INFLIGHT T1522/02, RIGHT INNER NR 2 PUMP FAILURE AND NR 1 PUMP WAS ON MEL. RETURNED TO SJU. LANDED WITHOUT INCIDENT. SUMPED RIGHT INNER NR 2 TANK AND ACCOMPLISHED RIGHT INNER NR 2 PUMP OPERATION. REPLACED THE FUEL PRESSURE SWITCH FOR NR 1 PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20040211001002004021100100NM 2004 2 11 AALA20040168 120040203A3397 CONNECTOR BOEING737 737823 13844BZNM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21928AN 29528 MIA EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. FOUND SEAT CONNECTOR AT SIDEWALL LOOSE. RE-SECURED CONNECTOR SYSTEM FOR EMERGENCY LIGHTS AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040211001022004021100102EU 2004 2 11 AALA20040170 120040203A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2114065 508 MIA EMERGENCY LIGHTS AT ROWS 19G TO 28G INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS AT ROWS 19G TO 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040211001032004021100103WP 2004 2 11 AALA20040171 120040202A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217538A 49992 SFO OVERHEAD EMERGENCY LIGHT AT 1L DOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040211001072004021100107NM 2004 2 11 AWXA200400130 120040120A5315AND101362401 FLOORBEAM BOEING737 737277 1384570NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM BELOW FORWARD LAVATORY AT BS 300, LBL 10. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM AT BS 300, LBL 10; FABRICATED 8 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-09 FIG 005. 2L72 4F RTA16WE 20040211001092004021100109NM 2004 2 11 AWXA200400132 120040120A53126545409213 PRESSURE PANEL BOEING737 7373G7 1384595NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK A .125 INCH CRACK WAS FOUND ON PRESSURE WEB AT BS 665, LBL 30, WL 203. MAINTENANCE CUT OUT CRACKED SECTION OF WEB AT BS 665, LBL 30, WL 203; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-51 FIG 203, SHT 1, 2, 3 & 5. 2L72 4F RTA16WE 20040211001102004021100110NM 2004 2 11 AWXA200400133 120040201A3350E0062B1A4AD0A SWITCH AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT DEFECTIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28830AW 1565 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS WERE ON WHEN THE SWITCH IS IN ARMED POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT SWITCH ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040211001132004021100113NM 2004 2 11 AWXA200400136 120040202A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040211001142004021100114NM 2004 2 11 AWXA200400137 120040130A53306545774575 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST AFT OF WING TO BODY FAIRING BETWEEN BS 727D AND 727 E, AT STR 23 LT. MAINTENANCE CUT OUT DAMAGED SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 202. 2L72 4F RTA16WE 20040211001162004021100116NM 2004 2 11 AWXA200400139 120040121A53126517158353 BEAM BOEING737 737277 1384570NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND AT TOOLING HOLE OF BS 178 BULKHEAD VERTICAL BEAM LBL 5.7, WL 178. MAINTENANCE ENLARGED TOOLING HOLE TO NEXT SIZE AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; INSTALLED SOLID RIVET IAW B737-200 SRM 53-10-01, FIG 010, SHEET 6. 2L72 4F RTA16WE 20040211001172004021100117NM 2004 2 11 QXEA200400089 120040201A335081152900510 SIGN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX- RIGHT HAND FORWARD EMERGENCY EXIT LIGHT ASSEMBLY IS BROKEN AND LOOSE ON LOWER SIDE BY EMERGENCY EXIT DOOR. REMOVED AND REPLACED SIGN ASSEMBLY. 2H72 4T RTA13NM 20040211001182004021100118NM 2004 2 11 QXEA200400097 120040129A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 BOI- ON FLIGHT 2209 FRONT PART OF FLOOR TRACK LIGHT AT ROW 1 IS BROKEN. REMOVED AND REPLACED FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040211001192004021100119NM 2004 2 11 QXEA200400098 120040202A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH* 338 514 PDX- EMERGENCY CEILING PANEL LIGHT AT ROW 1 AND ROW 7 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2H72 4T RTA13NM 20040211001222004021100122EU 2004 2 11 RAIA00401033 120040125A302039702022 VALVE JETAIRJETSTMJETSTM4101 1500501EU RT ENG ANTI-ICE INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03559HK140911557 41075 RIGHT ENGINE ANTI-ICE FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE. 2L72 4T RTA41NM 20040211001232004021100123SO 2004 2 11 RAIA00401034 120040126A3020102AU1AF VALVE EMB 145 EMB145LR 3260212SO RT ENG ANTI-ICE INOPERATIVE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03835HK177 145670 RIGHT ENGINE ANTI-ICE FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE VALVE. 2L72 4T RTT00011AT 20040209001032004020900103SO 2004 2 9 SWIA200412806 120040117A215032900541 VALVE EMB 120 EMB120ER 3260203SO RT A/C PACK MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07189SW8019 4289 120048 RIGHT PACK FAILED ON GROUND. PACK CONTINUED TO RUN AND FAIL WITH PACK SWITCH IN OFF POSITION, SMELLED BAD WITH SMOKE. REMOVED AND REPLACED INLET VALVE IAW 21-50-00. OPS, CHECK GOOD. 2L72 4T RTA31SO 20040209001112004020900111EU 2004 2 9 DHL2004365510 120040103A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH SEAT TRACK BETWEEN FR20 & FR21 APPROX LBL 78 PIECE OF TRACK MISSING & EVIDENCE OF CORROSION. CHECK OF SEAT TRACK BETWEEN FR20 & FR21 APPR LBL 78 FOUND OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK FROM FRAME 19.5 TO FRAME 26.5 LBL 77 MATERIAL USED 7075T6511/TMS 60-224457/ A532-74005D PO 23488101 SIZE 14 FT 8 INCHES. REF A300 SRM 51-10-40, 51-40-12, 51-30-30. 2L72 4F RTA35EU 20040209001262004020900126NM 2004 2 9 AWXA200400125 120040120A5313BAC1498164 STRINGER BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN STRINGER 5 RT AT BS 1014. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 5 RT AT BS 1014; FABRICATED A FILLER AND 2 EACH ZEE ANGLES; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-10-03 FIG 003, PG 15-19. 2L72 4F RTA16WE 20040209001312004020900131EU 2004 2 9 DHL2004365512 120040107A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH MAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 APPROX LBL 77 HAS SPOTS OF CORROSION. REMOVED SEAT TRACK FROM FRAME 19 TO 26.5 ACCCOMPLISH WITH N/R5169. AT MAIN DECK LBL 77 APPROX AS PER A300 SRM 53-10-00. WORK ACCOMPLISHED WITH N/R 5169. REMOVED AND REPLACED SEAT TRACK SECTION FROM FRAME 19.5 TO 26.5 LBL 77. MATERIAL USED TMS 60-22457 7075T6511. PO 23488101 LONG 14 FT 8 INCHES IAW A300 SRM 51-10-40, 51-40-12, 51-30-30. 2L72 4F RTA35EU 20040209001342004020900134NM 2004 2 9 QXEA200400082 120040127A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09368PH 512 SEA - FLIGHT 2120 - THE LAV SMOKE DETECTOR SOUNDED FOR 30 SECONDS DURING CLIMB. THE FLIGHT ATTENDANT CHECKED THE LAV AND THE CABIN. NO SMOKE OR HAZE WAS NOTED. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED AN OPERATIONAL CHECK OF THE DETECTOR. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040209001412004020900141WP 2004 2 9 ABXA040046 120040113A52009915565155 HINGE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 FITTING ABOVE UPPER HINGE ON AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040209001502004020900150EA 2004 2 9 SWIA200412813 120040125A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER LF NO TEST FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07932SW 7714 STAB TRIM CH1 OR CH2 WILL NOT ENGAGE. RERACKED HSTCU. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20040209001702004020900170SO 2004 2 9 C2XA04TY027 120040131A532014524131009 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS, DURING A SCHEDULED INSPECTION THE PAX DOOR LOWER ENTRANCE SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR SILL IAW EMB-135/145 SRM-51-40-02. 2L72 4F RTT00011AT 20040209001722004020900172SO 2004 2 9 C2XA04TY029 120040131A532014525480003 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716963 145116 TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB-135/145 SRM-51-20-03, 51-40-02 AND CMP-51-21-04/05/06. 2L72 4F RTT00011AT 20040209001922004020900192NM 2004 2 9 373PA0028 120040202A5347 SEAT TRACK BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION UNDER SEAT TRACK RBL 45 STA 328 TO STA 344. REPAIRED SEAT TRACK PER SRM 53-00-52, FIG 202. 2L72 4F RTA16WE 20040209001952004020900195NM 2004 2 9 373PA0029 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 INTERCOSTAL BETWEEN STA 328 AND STA 344 CORRODED AT LBL 10. REPLACED INTERCOSTAL CAP (SHIM) PER SRM 51-20-01 AND SRM 51-10-02. 2L72 4F RTA16WE 20040209001992004020900199NM 2004 2 9 373PA0033 120040202A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 INTERCOSTAL BETWEEN FLOORBEAM 986.5 AND 1006 RBL 14 HAS TWO NUT PLATES GROUND OUT OF LIMITS. REPLACED INTERCOSTAL PER SRM 51-10-2. 2L72 4F RTA16WE 20040209002082004020900208 2004 2 9 ACE013104 420040131A3416066306200 INDICATOR BEECH 1900 1900C 1154161CE ALTIMETER FAILED E YADAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 AL03114AX UC36 PILOT REPORTED CAPTAIN'S ALTIMETER FAILED (FLAGGED) AT 600 FT AFTER TAKEOFF. RETURNED TO AIRPORT. MAINTENANCE REPLACED THE FAILED ALTIMETER. 2L72 4T RTA24CE 20040209002102004020900210NM 2004 2 9 UPS04441793 120040124A5310 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 980 IN BETWEEN STR 41 AND STR 42 FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04 FIG 52 AT FWD CARGO COMPT RT STA 980 BETWEEN STR 41 AND STR 42. 2L74 4F A20WE 20040209002112004020900211NM 2004 2 9 UPS04441795 120040201A3350 BULB BOEING747 747123 1384873NM EMERGENCY LIGHT BURNED OUT A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01676UP 20101 EMERGENCY LIGHTS UNARMED LAMPS OUT PILOT OVERHEAD RELAMPED 2 NR 387 BULBS FOR UNARMED STATUS ON EMERGENCY LIGHT PANEL. 2L74 4F A20WE 20040209002212004020900221WP 2004 2 9 AALA2040152 120040201A3350 BATTERY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21966TW 53616 MIA - CEILING EMERGENCY LIGHTS AT COCKPIT TO ROW 7D INOPERATIVE. REPLACED BATTERY FOR CEILING EMERGENCY LIGHTS AT COCKPIT TO ROW 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040209002282004020900228WP 2004 2 9 AALA20040159 120040131A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21505AA 49799 DEN - EMERGENCY LIGHTS AT UPPER OVERHEAD IN FORWARD CABIN LOCATION B5-100 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT UPPER OVERHEAD IN FORWARD CABIN AT LOCATION B5-100. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040209002292004020900229EU 2004 2 9 AALA20040160 120040130A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211413A 11376 ORD - EMERGENCY FLOOR LIGHTING FROM ENTRANCE TO SEAT 11D INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR EMERGENCY FLOOR LIGHTING FROM ENTRANCE TO SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040209002332004020900233WP 2004 2 9 AALA20040165 120040201A2822 CIRCUIT BREAKER DOUG DC9 DC983 3022083WP FUEL BOOST UNSECURE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21564AA 49346 ORD INFLIGHT T227/01 CENTER FUEL TANK UNABLE TO TRANSFER FUEL. DIVERTED TO TUL. LANDED WITHOUT INCIDENT. FOUND AFT CENTER TANK BOOST PUMP CIRCUIT BREAKER IN BUT NOT LATCHED. RESET CIRCUIT BREAKER. ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040209002342004020900234NM 2004 2 9 QXEA200400092 120040201A5210 HANDLE BOMBDRDHC8 DHC8401 1390041NM PAX DOOR FOD A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09415QX 4081 GEG - FLIGHT 2301 - AFT PASSENGER DOOR WILL NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE DOOR AND CLEANED THE DEBRIS FROM DOOR HANDLE ACCESS FLAP. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20040209002362004020900236SO 2004 2 9 RAIA00401031 120040123A3010129502 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO ANTI ICE SYSTEM MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03826HK4950 WING NR 1 ANTI-ICE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED ANTI-ICE LOW PRESSURE SWITCH. 2L72 4T RTT00011AT 20040209002382004020900238SO 2004 2 9 RAIA00401027 120040115A532014522459003 SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAO OTHER O OTHER ININSP/MAINT 1 CE03811HK 145256 MX-STL- DURING BLOCK CHECK FOUND RAMP SUPPORT CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED RAMP SUPPORT. 2L72 4T RTT00011AT 20040209002392004020900239SO 2004 2 9 RAIA00401028 120040115A532014521725001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03811HK 145256 MX-STL- DURING BLOCK CHECK FOUND LEFTHAND SILL CORRODED BEYOND BLENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACE LEFTHAND SILL. 2L72 4T RTT00011AT 20040209002442004020900244NM 2004 2 9 04FDEA00254 120040131A5730ARB74064 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING UPPER SURFACE AREA BETWEEN XORS 317 TO XORS 346 FOUND WITH CORROSION. CORROSION ON RH WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 317 TO XORS 346 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN LIMITS AS PER SRM 57-10-00 FIG. 32 VOL. I. 2L73 4F RTA22WE 20040209002612004020900261NM 2004 2 9 04FDEA00270 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD (3) OUTBOARD FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75239. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND RPAIR. 2L73 4F RTA22WE 20040209002652004020900265NM 2004 2 9 04FDEA00275 120040201A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) INBOARD FACE CORRODED. 2L73 4F RTA22WE 20040209002742004020900274SO 2004 2 9 C2XA04TY030 120040131A532014521700001 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711551 145411 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE OMEGA BEAM RAMP ANGLE AT FRAME 20. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 57-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040210000792004021000079EA 2004 2 10 A6WA200340204 120040103A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 FLOOR ANGLE AT FS 621, LEFT SIDE, NEXT TO CARGO DOOR IS CRACKED. REPAIR IAW BOMBARDIER REO 601R-53-61-117. SEALED AND PAINTED IAW BOMBARDIER REO 601-53-61-117. PRESSURIZED AIRCRAFT IAW AMM 21-32-00-863-801. NO LEAKS NOTED. (M) 2L72 4F RTA21EA 20040211000292004021100029NM 2004 2 11 AMTA200400043 120040115A2613 OVERHEAT LOOP BOEING757 75733N 1384931NM LT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11556TZ 32590 EICAS STATUS MSG L STRUT OH DET 1 DISPLAYED. DEFERRED LEFT LOOP, AIRCRAFT FLEW 3 LEGS WITH NO ISSUES. LEFT ENGINE OVERHEAT SYSTEM CHECKS NORMAL PER AMM 26-12-00-5. () 2L72 4F RTA2NM 20040211000352004021100035NM 2004 2 11 AMTA200400046 120040115A5330 SKIN BOEING737 73783N 13844HINM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11301TZ 28239 FOUND C-2 PIT JUST FORWARD OF DOOR CUT OUT STATION 792-760 FLOOR PANEL HAS CORROSION. CORROSON OUT OF LIMITS PER SRM. REMOVED FLOORPANEL AND FABRICATED NEW PANEL. INSTALLED NEW PANEL PER SRM 51-40-02-0. TOP COATED PANEL WITH BMS 10-86 TY1 FOR PROTECTION. (M) 2L72 4F RTA16WE 20040211000482004021100048EA 2004 2 11 COMA0460096 120040128A2740 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STABILIZER ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01924CA 7026 FLIGHT 5869 STAB TRIM CAUTION MESSAGE. COULD NOT DUPLICTE. FUNCTION CHECK OF STAB TRIM WAS NORMAL. 2L72 4F RTA21EA 20040211000552004021100055EA 2004 2 11 COMA0470013 120040129A3020GG670800025 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA LT NACELLE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01379CA2066 10102 FLIGHT 5319 COWL ANTI ICE AND LEFT BLEED CAUTION MESSAGE. REPLACED THE LT PRSOV. 2L72 4F RTA21EA 20040211000592004021100059 2004 2 11 2004UALA00065 420040127A3460 COMPUTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FLIGHT MANAGE FAILED A UALAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 WP29452UA 955 RETURN TO FIELD DUE TO DUAL FMS FAILURE. FMGC1 WAS FAULTED ON THE POST FLIGHT REPORT. REPLACEMENT OF THE FMGC1 WAS ACCOMPLISHED AND SUBSEQUENT OPERATIONS TEST REVEALED NO FURTHER ANOMALY. 2L72 4F4 FRTA28NM E40NE 20040211000612004021100061NM 2004 2 11 2004UALA00082 120040126A2597 WIRE BOEING777 777222 1385219NM PWA PW4077PW4077 NE GALLEY OVEN OVERHEATED A UALAH DEACTIVATE SYST/CIRCUITS M OVER TEMP CRCRUISE 1 WP29771UA 26932 FIRST CLASS GALLEY OVENS AND HOT PLATES INOPERATIVE. WIRES BECAME OVERHEATED AT CONNECTION POINT OF C1 LUG ON 15 AMP CIRCUIT BREAKER C003 SUPPLYING POWER TO A FIRST CLASS OVEN. THIS CIRCUIT BREAKER IS ALSO IN A PARALLEL CIRCUIT THAT SUPPLIES POWER TO ADDITIONAL OVENS AND WARMING PLATES DOWNSTREAM. CIRCUIT BREAKER APPEARS TO HAVE BEEN WORKING CORRECTLY AND VISUAL ANALYSIS OF BURNED WIRES INDICATE INCORRECT CRIMPING ON BOTH WIRE LUGS ATTACHED TO THE CIRCUIT BREAKER. ADDITIONALLY, WIRE LUGS MAY NOT HAVE BEEN TIGHT ON THE C1 TERMINAL ON THE CIRCUIT BREAKER. CIRCUIT BREAKER AND WIRES WERE REPLACED. 2L72 4F4 FRTT0001SE E46NE 20040211000632004021100063NM 2004 2 11 04FDEA00289 120040203A5753 ROD DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RIGHT WING - FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75247, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD. FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000752004021100075SO 2004 2 11 C2XA04CL007 120040202A3350 CONNECTOR EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714505 145192 CLE FLIGHT 2028 THE CREW REPORTED THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RECONNECTED LOOSE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040211000802004021100080 2004 2 11 SWIA200412819 420040129A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07909SW5807 5807 7558 AFTER POWER UP DURING ORIGINATING CHECKS, THE YD2 INOP. MESSAGE AND FD2 FAIL MESSAGE ILLUMINATED AND COULD NOT BE REMOVED. REMOVED AND REPLACED NR 2 FCC CARD IAW AMM CHAPTER 22-12-14. OPS CHECK GOOD. 2L72 4F RTA21EA 20040211000892004021100089NM 2004 2 11 CALA0400070 120040131A5754 SKIN BOEING737 737524 1384721NM NR 2 SLAT DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2711656 28917 INSPECTION FOUND O/B CORNER OF NR 2 SLAT SKIN DELAMINATED. REPAIRED IAW SRM 51-70-10. 2L72 4F RTA16WE 20040211000982004021100098WP 2004 2 11 AALA20040166 120040203A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DIRTY A AALAK NONE O OTHER ININSP/MAINT 1 SW21969TW 53619 DFW EMERGENCY CEILING LIGHTS AT ROWS 4, 5 AND 7 ARE INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY CEILING LIGHTS BATTERY PACK B5-100 FOR ROWS 4, 5 AND 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040211001052004021100105NM 2004 2 11 AWXA200400128 120040117A53206560552501 STRAP BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0156 INCH CRACK WAS FOUND ON FUSELAGE SPLICE STRAP AT BS 358, STR 28 RT, E & E COMPARTMENT. MAINTENANCE CUT OUT CRACKED SECTION OF STRAP BETWEEN STR 27 RT AND STR 28 RT AT BS 358; FABRICATED A NEW SECTION OF REPLACEMENT STRAP; INSTALLED REPAIR PART IAW AWA ER 03-5331-04029-ES1. 2L72 4F RTA16WE 20040211001062004021100106NM 2004 2 11 AWXA200400129 120040117A53306573742 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON EXISTING REPAIR ON EXTERNAL FUSELAGE SKIN BS 908, STR 27 LT TO STR 28 LT. MAINTENANCE REMOVED EXISTING DOUBLERS AT BS 908, STR 27 LT TO STR 28 LT; PERFORMED A HFEC INSPECTION AND FOUND CRACK AT FASTENER HOLE; CUT OUT CRACK AREA OF SKIN; FABRICATED A DOUBLER, FILLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-03 FIG 48. 2L72 4F RTA16WE 20040211001202004021100120 2004 2 11 QXEA200400099 420040130A2210 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 300 ILLUMINATED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09612QX 10042 BIL- ON FLIGHT 2508 AFTER TAKEOFF AUTOPILOT TRIM IS SHOWING A CAUTION MESSAGE. DISCONNECTED AUTOPILOT, RETRIMMED, THEN RECONNECTED PER CHECKLIST. NO FURTHER INCIDENTS. COMPLIED WITH AUTOPILOT SYSTEM OPERATIONAL CHECK IAW CRJ AMM 22-11-00-710-802 AND 22-11-24-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040211001212004021100121EU 2004 2 11 RAIA00401032 120040125A3241 ANTI-SKID SYS JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03558HK 41071 5371-GSO, IDLE GATE STUCK; POWER LEVER WOULD NOT GO INTO REVERSE, ANTI-SKID LIGHT ON, BRAKES INEFFECTIVE, ACFT WENT OFF END OF RUNWAY. MAINTENANCE REMOVED AND REPLACED BOTH LT MLG WHEEL AND TIRES, OPS CHECK POWER LEVERS AND COULD NOT DUPLICATE POWER LEVER MALFUNCTION, PERFORMED TAXI CHECK OF BRAKE SYSTEM, NO DEFECTS NOTED. 2L72 4T RTA41NM 20040211001252004021100125EU 2004 2 11 RAIA00401037 120040126A771431055863 PICKUP JETAIRJETSTMJETSTM4101 1500501EU RPM MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03573HK3987 41092 RIGHT IEC LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 MONOPOLE. 2L72 4T RTA41NM 20040211001262004021100126SO 2004 2 11 RAIA00401038 120040127A3150 WARNING HORN EMB 145 EMB145LR 3260212SO CONFIGURATION ACTIVATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03826HK 5644-CLT, TAKEOFF CONFIG WARNING (BRAKE) SOUNDED. MAINTENANCE RESET BRAKE I/B AND BRAKE O/B CIRCUIT BREAKERS. 2L72 4T RTT00011AT 20040211001272004021100127EU 2004 2 11 RAIA00401039 120040127A261351228801 OVERHEAT LOOP JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FALSE INDICATIONA RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03565HK 41082 5539-STL, LT OVERHEAT WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED LT HAND OVERHEAT LOOP. 2L72 4T RTA41NM 20040211001302004021100130SO 2004 2 11 C2XA04SH044 120040204A531514522459003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV- DURING C-CHECK THE RIGHT RAMP SUPPORT ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040211001322004021100132EA 2004 2 11 MASA200400049 120040127A335059465 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 ASH 6087 MRY-PHX, FLOOR PROX LIGHTING INOP AT ROWS 6-9. A/C FERRIED TO PHX, MX REPLACED THE RIBBION CABLE. 2L72 4F RTA21EA 20040211001332004021100133SO 2004 2 11 MASA200400055 120040131A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 ASH 2859 YYZ, FWD FACING EMERGENCY EXIT LIGHT INOP. MX PERFORMED AN OP CHECK. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040211001342004021100134SO 2004 2 11 MASA200400056 120040201A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12-18 INTERMITTENT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07826MJ 145214 ASH 2946 BTV-DCA, EMERGENCY FLOOR PATH LIGHTING INOP FROM ROW 12 TO 18. AFTER SEVERAL MINUTES THE LIGHTS STARTED WORKING NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2L72 4T RTT00011AT 20040211001352004021100135EA 2004 2 11 MASA200400057 120040201A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727318 7318 ASH 6412 PHX-COS, CREW REPORTED NR 2 OVERHEAD EMERGENCY LIGHT INOP. MX REPLACED THE LAMP. 2L72 4F RTA21EA 20040211001382004021100138NM 2004 2 11 QXEA200400094 120040202A61208193007007 FADEC BOMBDRDHC8 DHC8401 1390041NM NR 2 DEFECTIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09413QX3272 979 4060 SEA FLIGHT 2346 RETURNED TO FIELD, NR 2 PROP DID NOT REDUCE FROM 1020 NP WHEN COMMANDED. REPLACED FADEC. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040211001402004021100140EA 2004 2 11 VNAA0401014 120040127A21331037708 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07209PS323 7874 DURING CLIMB, CREW COULD NOT PRESURIZE AIRCRAFT. AIRCRAFT RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE PRIMARY OUTFLOW VALVE IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040211001412004021100141NM 2004 2 11 VNAA0401011 120040122A5210 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE CABIN DOOR FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07438JS 3056 DURING CRUISE, THE CREW RECEIVED A MAIN CABIN DOOR OPEN INDICATION. MAINTEMANCE INSPECTED AND REPLACED THE DOOR LINK ROD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040211001422004021100142EA 2004 2 11 VNAA0401012 120040123A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO DOOR ILLUMINATED A VNAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07213PS 7879 DURING TAXI, CREW RECEIVED A CARGO DOOR LIGHT MESSAGE. AIRCRAFT THEN RETURNED TO BLOCK. MAINTENANCE THEN DEFERRED THE CARGO DOOR INDICATION IN ACCORDANCE WITH 52-70-4 CODE C. 2L72 4F4 FRTA21EA E15NE 20040211001442004021100144 2004 2 11 VNAA0401017 420040131A3140701730011006 COMPUTER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE NR 1 FAILED A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07424JS6286 3909 3033 DURING FLIGHT, THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 IAC IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040211001452004021100145NE 2004 2 11 VNAA0401016 220040130A7297 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07206PS 7860 DURING FLIGHT, THE RIGHT HAND ENGINE WAS SURGING AND FLIGHT 2216 RETURNED TO DAY. MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND ENGINE CONNECTOR IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040211001462004021100146EA 2004 2 11 VNAA0401015 120040128A3397 PIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE F/A PANEL FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07221PS 7889 THE CREW REPORTED THAT THE FLIGHT ATTENDANT PANEL'S EMERGENCY LIGHT SWITCH WAS NOT WORKING PROPERLY. MAINTENANCE INSPECTED AND REPLACED A PIN IN THE PANEL'S CONNECTOR IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040211001512004021100151WP 2004 2 11 0400179750 120040203A27805919526507 DUCT DOUG DC9 DC941 302207NWP LT WING LE BINDING A NWAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL01750NW 47114 THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO THE LEFT WHEN THE SLATS WERE EXTENDED FOR LANDING AT GRB. THE BLUE SLAT EXTEND DID NOT ILLUMINATE AND THE SLAT DISAGREEMENT ANNUNCIATOR DID LIGHT UP. CREW RECYCLED SLATS AND GOT THE SAME RESULTS. FLIGHT RETURNED TO MSP, FOLLOWED COM PROCEDURES FOR LANDING, AND ARRIVED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT SLAT T-DUCT DUE TO BINDING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040211001562004021100156SO 2004 2 11 C2XA04BT003 120040113A3244 TIRE EMB 145 EMB145LR 3260212SO NLG DAMAGED A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2716976 145171 CREW REPORTED, AIRCRAFT DEPARTED TAXIWAY. UNSURE OF DAMAGE TO AIRCRAFT. MAINTENANCE INSPECTED AIRCRAFT IAW EMB145 MM 05-50-03, NO DAMAGE NOTED TO LANDING GEAR OR FUSELAGE. BOTH NOSE LANDING GEAR TIRES REPLACED FOR PRECAUTIONARY MEASURES DUE TO NOSE GEAR DEPARTING THE TAXIWAY IAW EMB145 32-49-05. AIRCRAFT RETURNED TO SERVICE. INVESTIGATED AND FOUND AIRCRAFT SLID OFF OF TAXIWAY ON ICE. 2L72 4T RTT00011AT 20040211001592004021100159EU 2004 2 11 MALA040160 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 13A & 13B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 13A,13B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001622004021100162EU 2004 2 11 MALA040148 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 6D, 6E, & 6F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 6D, 6E, 6F IAW MESABA EO NR A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001632004021100163EU 2004 2 11 MALA040149 120040120A5320 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 7A & 7B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 7A & 7B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001662004021100166EU 2004 2 11 MALA040152 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 8D, 8E, & 8F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 8D, 8E, 8F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001672004021100167EU 2004 2 11 MALA040153 120040118A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 9A & 9B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 9A & 9B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001692004021100169EU 2004 2 11 MALA040157 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 11D, 11E, CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 11D, 11E, IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001742004021100174EU 2004 2 11 MALA040163 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 14D CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 14D IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001752004021100175EU 2004 2 11 MALA040164 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 15A & 15B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 15A & 15B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001772004021100177EU 2004 2 11 MALA040150 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 7D, 7E, & 7F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 7D, 7E, 7F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001812004021100181NM 2004 2 11 UPS04441798 120040125A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D - BS 960 TO 980 LT STR 2AL STRINGER FOUND CRACK. BS 960 - BS 980 STR 2AL STRINGER REPAIR CARRIED OUT IAW SRM 53-10- 03 FIG 4. 2L74 4F A20WE 20040211001832004021100183NM 2004 2 11 UPS04441800 120040125A5310 SHEAR TIE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C BS 960 LT BETWEEN STR 7L AND 6L SHEAR TIE FOUND CRACK. BS 960 LT FRAME BETWEEN S6L AND 7L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 4. 2L74 4F A20WE 20040211001842004021100184NM 2004 2 11 UPS04441802 120040126A5310 SHEAR TIE BOEING747 747123 1384873NM AFT CARGO BILGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1720, STR 49R - 51R SHEAR TIES CRACKED. AFT CARGO COMPT BS 1720 STR 49R - STR 51R SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2L74 4F A20WE 20040211001852004021100185NM 2004 2 11 UPS04441803 120040125A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C BS 1438 S-13 / S-14R FRAME CRACKED. BS 1438 BETWEEN S13R AND S14R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 1. 2L74 4F A20WE 20040211001872004021100187NM 2004 2 11 UPS04441805 120040125A5311 FRAME BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C STA 1700 FRAME FOUND CRACK BETWEEN S-10 / S-11L. BS 1700 BETWEEN STR 10L AND STR 11L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 1. 2L74 4F A20WE 20040211001892004021100189NM 2004 2 11 UPS04441807 120040124A5310 ATTACH ANGLE BOEING747 747123 1384873NM SHEAR TIE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT - LT STA 900 IN BETWEEN STR 43 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CRACKED. FWD CARGO COMPT BS 900 BETWEEN STR 43L AND STR 44L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2L74 4F A20WE 20040211001912004021100191NM 2004 2 11 UPS04441809 120040126A5310 SHEAR TIE BOEING747 747123 1384873NM AFT CARGO BILGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C AFT CARGO BILGE AREA - FS 1700, STR 49L - 50L SHEAR TIE CRACKED. AFT CARGO COMPT BS 1700 BETWEEN STR 49L AND STR 50L SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 3. 2L74 4F A20WE 20040211001942004021100194WP 2004 2 11 UPS04841797 120040202A33506012235 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT UNSERVICEABLE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01750UP 45950 EMERGENCY LIGHTS INOP. BATTERY FAILED REPLACED EMERGENCY LIGHT BATTERY. 2L74 4F RT4A25 20040211001952004021100195WP 2004 2 11 UPS04841812 120040204A3350 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01852UP 46052 EMERGENCY LIGHTS STAY ON CONTINOUSLY WHEN IN ARMED POSITION. LIGHT WILL NOT ILLUMINATE. WHEN SWITCH SELECTED TO DISARM CHECK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT & PERFORMED ADJ/ TEST IAW MM 33-50-01-2. OPS CHECK GOOD. 2L74 4F RT4A25 20040211001962004021100196NE 2004 2 11 UPS04841813 220040203A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 FLAMED OUT A IPXAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO01880UP 46080 UPON THROTTLE REDUCTION TO IDLE FOR DESCENT FROM FL 370 M .80, NR 1 ENGINE FLAMED OUT. ENG READINGS WERE NORMAL WITH WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL300 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GENERAL INSP, CK FLT IDLE, SPECIFIC GRAVITY SETTING, MAGNETIC CHIP DETECTORS AND FUEL FILTER. NO DEFECTS WERE NOTED. CLEANED PAINT & PAINT STRIPPER OFF OF CDP TUBE DRAIN HOLES. RAN ENGINE TO MAX POWER, OPS WAS NORMAL. 2L74 4F4 FRT4A25 E2GL 20040211001972004021100197 2004 2 11 XNOA1176 420040204A2200 DAMPER AIRBUS300 A300B4203 3930306EU YAW FAILED A XN0AD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 GL23473AS 203 BTB DUE BOTH YAW DAMPERS FAILED DURING TAXI OUT. PART INSTALLED FOR YAW DAMPER AUTO STAB CONT. REPLACED WITH ORIGINAL UNIT. TRANSFERRED TO DMI 4053, ORIGINAL DMI CONTINUES. NEW AUTO STAB FAILED, BAD FROM STOCK, IAW A-300 AMM 22-21-00. R&R RATE GYRO OPS CK GOOD IAW A300 AMM 22-21-45, THIS CLEARS DMI 4053. (STATUS: SUPP/CLOSED) 2L72 4F RTA35EU 20040211001982004021100198EA 2004 2 11 COMA0460103 120040203A5730601R1004511 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA17150 7157 LEFT WING LOWER SKIN PLANK HAS CORROSION AT FUEL TANK ACCESS DOOR 540DB, WS 95.950. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION, PERFORMED NDT TO ENSURE COMPLETE REMOVAL OF DAMAGE. ROTO-PEENED REWORKED AREAS, SANDED REWORKED AREAS TO 63 MICRO INCHES. APPLIED CONVERSION COSTING AND FUEL TANK COATING. ALL WORK DONE IAW BOMBARDIER INC REO 601R-57-21-030 REV B. 2L72 4F RTA21EA 20040211001992004021100199EA 2004 2 11 COMA0460104 120040203A53306003301039 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA17150 7157 RIGHT SIDE LOWER FUSELAGE SKIN IS CRACKED AT NOSE LANDING GEAR CUTOUT AT FS 235 STR 26R CRACK IS 1.0 INCH LONG. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED AREA, FABBING REPAIR FILLER AND DOUBLERS FROM 2024T3.050, PO 29672/1, 2024T3.063, PO 32532 AND 2024T42.063, PO 15622/17. PERFORMED LPI TO ENSURE CUTOUT WAS CRACK FREE, INSTALLED REPAIR PARTS. ALL WORK DONE IAW BOMBARDIER INC REO 601R-53-11-048 REV B. 2L72 4F RTA21EA 20040211002002004021100200NE 2004 2 11 COMA0460106 220040201A7261 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE ENGINE OIL LOOSE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01981CA 7163 FLIGHT 5400 RT ENGINE OIL PRESSURE WARNING IFSD. TIGHTENED OIL SUPPLY LINES ON ENGINE AND ADDED 6 QTS OIL. OPS CHECK AND LEAK CHECK SATISFACTORY. 2L72 4F4 FRTA21EA E15NE 20040211002032004021100203EA 2004 2 11 COMA0470014 120040202A2750 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLAT ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01379CA 10102 FLIGHT 5077 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, FOUND NO FAULT CODES IN COMPUTER. SYSTEM OPERATION NORMAL. 2L72 4F RTA21EA 20040211002042004021100204CE 2004 2 11 02 120040203A3250MS16555624 ROLL PIN CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL STEERING TILLER SHEARED E I5EAK NONE O OTHER TXTAXI/GRND HDL 1 WP07998CX4380 7500098 STEERING TILLER DOES NOT STEER NOSE WHEEL. 2L72 4J4 FRTT00007WITE6CH 20040211002062004021100206NM 2004 2 11 AALA20040174 120040203A33500201991001 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21631AA 24589 MIA SEAT MOUNTED EMERGENCY EXIT LIGHT BROKEN AT SEAT 17D. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040211000162004021100016NM 2004 2 11 AMTA200400063 120040121A335020131A BATTERY PACK BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 FOUND TWO EGRESS LIGHTS OUT AT R2 DOOR. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY AT R2 DOOR PER AMM 33-51-07-2, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040211000502004021100050EA 2004 2 11 COMA0460098 120040130A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA TE FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01491CA 7756 FLIGHT 5712 FLAPS FAILED ON FINAL. C/W INSPECTION OF FLAP SYSTEM PER EO 27-046 AND AD 98-20-01. 2L72 4F RTA21EA 20040211000582004021100058NE 2004 2 11 2004UALA00009 220040106A72309325M85G04 BLADE BOEING737 737522 138449FNM GE CFM56 CFM563US 13802NE HP COMPRESSOR DAMAGED A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29920UA33414 25387 726352 ABORTED TAKEOFF AT 110KTS AFTER CREW FELT A PULL TO THE LEFT. NO REPORTED ENGINE PARAMETER CHANGES OR EXCEEDANCES. FLIGHT DATA RECORDER DID NOT REVEAL ANY ENGINE OR REVERSER RELATED DISCREPANCIES. BOTH ENGINES PARAMETERS WERE SIMILAR WITH NO EVIDENCE OF POWER LOSS OR STALLING. POSITION 1 REVERSER WAS INSPECTED AND CHECKED, WITH NO DISCREPANCIES FOUND. A POWER ASSURANCE RUN AND INSPECTION FOR COMPRESSOR STALL WAS ACCOMPLISHED ON NUMBER 1 ENGINE. ENGINE DID NOT MAKE, RATED TAKEOFF POWER. INSPECTION FOUND 4TH STAGE HIGH PRESSURE COMPRESSOR (HPC) BLADES DAMAGE. ENGINE WAS REMOVED. MEC AND PMC REPLACED AS PRECAUTIONARY. ENGINE SENT FOR FULL ENGINE SHOP VISIT AND TEST CELL RUN. 2L72 4F4 FRTA16WE E2GL 20040211000622004021100062NM 2004 2 11 ZW0A0400201 120040129A4900S351T0209 APU BOEING757 757231 1384950NM SMOKE A ZW0AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 CE13719TW 28487 FOR A TEST FLIGHT AFTER CHECK-C, DURING TAKEOFF AND INITIAL CLIMB THE COCKPIT AND CABIN FILLED WITH SMOKE. SHUTDOWN THE APU AND LANDED. REPLACED THE APU. 2L72 4F RTA2NM 20040211000642004021100064NM 2004 2 11 04FDEA00290 120040203A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD (4) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000682004021100068NM 2004 2 11 04FDEA00294 120040203A5753 ROD DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD (2) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040211000882004021100088NM 2004 2 11 CALA0400069 120040130A5297 WIRE BOEING737 7373T0 1384582NM PROX SENSOR SHORTED A CALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2716339 23577 AFT SERVICE & AFT ENTRY DOOR LIGHTS ILLUMINATED AT ROTATION. FORWARD SERVICE LIGHTS CAME ON AFTER A COUPLE OF MIN. FLT ATTENDANT REPORTED STRONG TOXIC FUMES IN CABIN & FUMES WERE PRESENT ON FLT DECK. AIRCRAFT RETURNED TO IAH. MAINTENANCE FOUND WIRING BUNDLE (W298) IN AFT CARGO COMPARTMENT BURNED. ENGINEERING CONCLUDED THAT AFT TOILET HEATER AND AFT DRAIN MAST HEATER WIRES BURNT WHICH CAUSED THE L-2 DOOR PROXIMITY SENSOR WIRING TO SHORT. ALL RELATED BURNT WIRES WERE IN THE SAME WIRE BUNDLE (W298). THE SWITCHING UNIT DAMAGED. WIRING BUNDLE REPAIRED. SWITCHING UNIT REMOVED & REPLACED. BOTH AFT SERVICE DOOR, FORWARD SERVICE DOOR & FORWARD CARGO DOOR PROXIMITY SENSORS REPLACED. GROUND CHECKS GOOD. 2L72 4F RTA16WE 20040211000912004021100091NM 2004 2 11 CALA0400072 120040108A5330 SKIN BOEING737 737524 1384721NM FUSLEAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2762631 27535 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT BS 420 BELOW S17L. THE SKIN WAS REPAIRED IAW ECRA 5331-01133. 2L72 4F RTA16WE 20040211001042004021100104WP 2004 2 11 AALA20040172 120040202A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21279AA 49295 DFW CEILING EMERGENCY LIGHTS AT BINS FOR ROWS 18 THROUGH 21 INOPERATIVE. ALSO AFT CEILING AIRSTAIR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS AT BINS 18 THROUGH 21 AND CEILING EMERGENCY LIGHTS AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040211001082004021100108NM 2004 2 11 AWXA200400131 120040118A53306591879 SKIN BOEING737 737277 1384570NM FUSELAGE WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 DURING C-15 CHECK LOOSE AND WORKING RIVETS WERE FOUND ON MLG WHEEL WELL KEELBEAM SKIN FROM BS 663 TO BS 727, STR 27 LT TO STR 27 RT. MAINTENANCE REMOVED KEEL BEAM SKIN FROM BS 663 TO BS 727, STR 27 LT TO STR 27 RT; FABRICATED NEW SKIN AND 2 EACH REPAIR DOUBLERS PER SB 737-53-104; INSTALLED REPAIR PARTS IAW AWA ER 15-5331-04020-SS1. 2L72 4F RTA16WE 20040211001122004021100112NM 2004 2 11 AWXA200400135 120040202A33973416302 CONNECTOR BOEING757 7572S7 1384962NM SEAT ROW 12 LT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - EEL - DURING A-08 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. MAINTENANCE FOUND DAMAGED CONNECTOR UNDER SEAT 12 LT. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTOR AND SOCKET ASSEMBLIES AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD. PART NAME; SOCKET, CONN, 22-18, GOLD PLATE, MFG; AMP INC, P/N; 170366-3, LOC; SEAT ROW 12 LT. 2L72 4F RTA2NM 20040211001282004021100128NE 2004 2 11 PCAA0402161 220040130A7397311479203 WIRE HARNESS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENG ECC FAULTY A PCAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA13981HA 378 120889 DURING TAXI, EXPERIENCED NR 2 ENGINE MANUAL CAUTION LIGHT. REMOVED AND REPLACED NR 2 ELECTRONIC ENGINE CONTROL & RETURNED AIRCRAFT TO SERVICE. THEN EXPERIENCED THE SAME CONDITION ON TAKEOFF ROLL. MAINTENANCE FURTHER INVESTIGATED AND FOUND CORROSION ON THE ASSOCIATED CANNON PLUG IN THE RIGHT HAND WING ROOT AT P9811-J14. CORROSION WAS CLEANED AND AIRCRAFT RETURNED TO SERVICE ON 31JAN04. THEN FLIGHT 4006 HAD SAME CONDITION PRESENT DURING TAXI. AIRCAFT WAS SCHEDULED FOR FERRY TO MIDDLETOWN MAINTENANCE. AIRCRAFT THEN HAD TEST EQUIPMENT HOOKED UP & RAN ON SYSTEMS, MAINTENANCE REMOVED AND REPLACED ENGINE AIRFRAME SPIDER HARNESS. ALL SYSTEMS OPS CHECKED GOOD & AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040211001292004021100129NE 2004 2 11 PCAA0402162 220040202A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RIGHT ODOR A PCAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA13844EX365676100 339 120448 FLIGHT 3884, SYRACUSE TO PHILADELPHIA, HAD TO DIVERT TO AVOCA DUE TO ODOR IN THE CABIN AND COCKPIT. MAINTENANCE INVESTIGATED AND REMOVED AND REPLACED THE AIR CYCLE MACHINE AND THE NR 2 AIR SWITCHING VALVE. PROBLEM STILL EXISTED. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REMOVAL AND REPLACEMENT OF THE RIGHT HAND ENGINE. 2H72 4T4 TRTA13NM E20NE 20040211001362004021100136EA 2004 2 11 MASA200400060 120040201A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 ASH 6231 SAT-PHX, CREW REPORTED LEFT SIDE AFT EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4F RTA21EA 20040211001532004021100153 2004 2 11 MWEA040015 420040203A2565 INDICATOR DOUG DC9 DC932 3022066WP PAX DOOR SLIDE INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31209ME 47730 FORWARD ENTRANCE DOOR SLIDE PRESSURE GAUGE IS INOPERATIVE. REMOVED AND REPLACED FORWARD EVACUATION SLIDE. 2L72 4F A6WE 20040211001602004021100160EU 2004 2 11 MALA040161 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 13E, & 13F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 13E,13F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001652004021100165EU 2004 2 11 MALA040151 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 8B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 8B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001682004021100168EU 2004 2 11 MALA040154 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 9D & 9E CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 9D & 9E IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001702004021100170EU 2004 2 11 MALA040158 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 12B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 12B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001712004021100171EU 2004 2 11 MALA040159 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 12D, 12E,CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 12D,12E, IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001722004021100172EU 2004 2 11 MALA040155 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 10D & 10F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 10D,10F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001762004021100176EU 2004 2 11 MALA040165 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 15F CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 15F IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001932004021100193NM 2004 2 11 UPS04441811 120040121A5420 WEB BOEING747 747123 1384873NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, NR 2 PYLON - LWR WEB CRACKED THRU AFT RT LONGITUDINAL STIFFENER APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LATERALLY. LWR SPAR WEB 5 LOCATIONS CRACK END BY STOP HOLE PRILLED AS PER SRM 54-10-03 FIG 2. NDT INSP NIL CRACKS AND PERFORMED A PERMANENT REPAIR AS PER SRM 54-10-03 FIG 2 AT NAC STA 213 COMBINED REPAIRED AT SAME AREA REF TO NRC UE56196. 2L74 4F A20WE 20040211002012004021100201EA 2004 2 11 COMA0460107 120040128A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01995CA7363 7229 FLIGHT 5481 NR 3 HYDRUALIC SYSTEM LOW PRESSURE & LOW QUANTITY WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20040213000362004021300036NM 2004 2 13 AALA20040176 120040202A3397 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21757AN 32636 JFK, EMERGENCY PATH LIGHTING AT SEATS 37C AND 37G INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY PATH LIGHTING AT SEAT 37G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040213000382004021300038WP 2004 2 13 AALA20040179 120040105A2497 WIRE DOUG DC9 DC983 3022083WP OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21565AA 49347 WIRE RING TERMINALS AT RESISTOR R4-9 SHOWS SIGNS OF OVERHEATING. REPLACED WIRE RING TERMINALS AT R4-9 RESISTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040213000402004021300040WP 2004 2 13 AALA20040178 120040105A2497 WIRE DOUG DC9 DC983 3022083WP COCKPIT OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21565AA 49347 TUL POWER CABLE TERMINAL ENDS ON WIRES 3X1C2A, 3X2C2B, AND 3X3C2C AT LEFT AUXILLARY POWER RELAY T1, T2, AND T3, AND AT S3-23, 1, 2, 3 POSTS AND WIRE RING TERMINALS OF WIRES 3X2T20B AND 3X3T20C AT S3-23 POSTS 2 AND 3 SHOWS SIGNS OF OVERHEATING. REPLACED POWER CABLES 3X1C2A, 3X3C2C, AND 3X3C2C AND REPLACED RING TERMINALS ON WIRES 3X2T20B AND 3X3T20C AT S3-23. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040213000412004021300041NM 2004 2 13 04FDEA00306 120040204A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RIGHT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75241. TRAILING EDGE & TRAILING EDGE DEVICES. RT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040213000422004021300042NM 2004 2 13 04FDEA00307 120040204A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RIGHT WING - FOUND INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75241 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040213000442004021300044SO 2004 2 13 RAIA00401041 120040130A3097 CONNECTOR EMB 145 EMB145LR 3260212SO WING ANTI ICE DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 STL- WING ANTI-ICE FAIL INDICATION. MAINTENANCE DOWNLOADED CMC, NO FAULTS. CLEANED PRESSURE SWITCH CONNECTOR, OPS CHECK OK. 2L72 4T RTT00011AT 20040213000452004021300045EU 2004 2 13 RAIA00402001 120040202A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03559HK 41075 STL - ESCAPE PATH LIGHTS INOP BEYOND ROW 7. MAINTENANCE RE-SECURED CONNECTOR AT PATH LIGHTS. 2L72 4T RTA41NM 20040213000482004021300048NM 2004 2 13 SWAA040321 120040131A3350610478 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED PM CHECK, FOUND R2 AND L2 DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040213000512004021300051 2004 2 13 SWAA040324 420040131A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040213000522004021300052NM 2004 2 13 SWAA040325 120040131A5315BAC1509 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY FLOORBEAM CORRODED AT BS 770, STRINGER 26R, BS 770, STRINGER 27L AND BS 770 STRINGER 27R. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040213000532004021300053 2004 2 13 SWAA040326 420040131A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040213000542004021300054NM 2004 2 13 SWAA040327 120040201A24606937315 MODULE BOEING737 737301 1384611NM COCKPIT FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29659SW 23229 AIRTURN BACK, POWER STANDBY LIGHT ILLUMNINATED IN FLIGHT. QRH PROCEDURES FOLLOWED. LIGHT WOULD NOT RESET. REMOVED AND REPLACED STANDBY POWER MODULE PER MM. 2L72 4F RTA16WE 20040213000562004021300056NM 2004 2 13 SWAA040329 120040201A3350D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040213000602004021300060NM 2004 2 13 SWAA040333 120040202A33501000679 LIGHT BOEING737 7372H4 138448CNM R2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040213000652004021300065NM 2004 2 13 SWAA040338 120040202A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040213000662004021300066EU 2004 2 13 100712 120040203A3097 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU DE ICE SYS TRIPPED A UHLAO OTHER G MULTIPLE FAILURE CRCRUISE 1 GL17152CQ 152 FLIGHT 4598 FROM TTN TO PIT. AIRCREW DECLARED EMERGENCY AND DESCENDED TO 5000 FT, AIRCREW HAD MULTIPLE LT DE-ICE FAILURES. WHEN AIRCRAFT LANDED IN PIT. A/C TAKEN OUT OF SERVICE AT 0915 LOCAL AND RETURN TO SERVICE AT 1000 LOCAL. MAINTENANCE FOUND C/B IN LT WHEEL WELL POPPED. RESET C/B AND A/C RETURNED TO SERVICE. 2L72 4T RTA52EU 20040213000672004021300067EU 2004 2 13 189661 120040205A6120 PROPELLER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE LEFT MALFUNCTIONED A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL17150CN 150 434 DRG49983 ON 02/05/04, APPROX 1630 (UTC), FLT 4518 ERI-PIT. CREW BEGAN TAKEOFF ROLL AND ENGAGED CTOT. ONCE THE CTOT WAS ENGAGED, THE LT TORQUE BECAME ERRATIC AND FLUCTUATED. CREW PULLED POWER BACK, ABORTED TAKEOFF AND RETURNED TO GATE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040213000682004021300068NM 2004 2 13 QXEA200400111 120040204A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM BAGGAGE DOOR UNSECURE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09408QX5772 4050 SEA - FLIGHT 2335 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A REAR BAGGAGE DOOR WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BAG DOOR HANDLE UNSECURE. MAINTENANCE SECURED THE HANDLE AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040213000702004021300070NM 2004 2 13 QXEA200400112 120040204A2930 HYDRAULIC SYSTEM BOMBDRDHC8 DHC8401 1390041NM NR 3 LOW A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09409QX 4051 PDR - FLIGHT 2307 - THE AIRCRAFT RETURNED TO GATE WHEN THE NUMBER 3 HYDRAULIC QUANTITY DROPPED TO FORTY PERCENT AFTER COMPLYING WITH THE ISO VALVE CHECK. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NUMBER 3 HYDRAULIC SYSTEM. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040213000712004021300071NM 2004 2 13 DHL2004741002 120040204A5710 MOUNT BOEING727 7272Q9 138448MNM K FLAP SYS CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 NR 6 LEADING EDGE K-FLAP ACTUATOR MOUNT ON SPAR APPEARS TO BE CRACKED AT INBOARD SIDE AT BASE OF TRUNNION CAP. REMOVED NR 6 LEADING EDGE K-FLAP ACTUATOR ASSEMBLY TO FOM. REMOVED INBOARD VERTICAL WEB SECTION OF NR 6 K-FLAP ACTUATOR MOUNT BOX, FABRICATED REPLACEMENT WEB SECTION PER B-727 SRM 51-20-1, USING OLD WEB AS A TEMPLATE. MATERIAL ID 7075T6 X .063 AS PER B-727 SRM 57-20-2. TREATED AND PRIMED WEB, AND INSTALLED PER B-727 SRM 51-10-1, & 51-30-2, AND 51-30-1. 2L73 4F RTA3WE 20040213000722004021300072EA 2004 2 13 COMA0460109 120040126A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01818CA 7408 FS 621 AT LBL 27 AND RBL 27 IS CRACKED ON FLOORBEAM. REPAIRED FS 621 FLOORBEAM AT LBL 27 AND RBL 27 IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-898. APPLIED FILLET SEAL ON FS 621 FLOORBEAM AT LBL 27 AND RBL 27 IN ACCORDANCE WITH CRJ SRM 51-23-00 AND APPLIED TOPCOAT TO REPAIRED AREAS IN ACCORDANCE WITH CRJ SRM 51-25-16. 2L72 4F RTA21EA 20040213000732004021300073EA 2004 2 13 COMA0460110 120040126A5730 DRAIN VALVE CNDAIRCL600 CL6002B19 1900309EA RIGHT CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01818CA 7408 CRACK INDICATION AT RT COLLECTOR VALVE AFT ATTACH HOLE BORE. OPENED HOLE TO .3125 INCH AND FABRICATED FREEZE PLUG FROM 7075-T6 BAR MATERIAL, LIQUID PENETRANT INSPECTION ON AREA OF DAMAGE PRIOR TO INSTALLING FREEZE PLUG. INSTALLED FREEZE PLUG AFTER CLEANING AREA. WORK WAS DONE IN ACCORDANCE WITH BOMBARDIER REO 601R-57-21-404. 2L72 4F RTA21EA 20040213000742004021300074EA 2004 2 13 COMA0460112 120040203A2612356024310 ELEMENT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE DUCT MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01809CA 7366 FLIGHT 5359 ANTI ICE DUCT WARNING. REPLACED SENSING ELEMENT A46WK. 2L72 4F RTA21EA 20040213000772004021300077WP 2004 2 13 04FDEA00310 120040204A5743ARB0622502 SUPPORT DOUG DC10 DC1010 3022110WP MLG CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 MAIN LANDING GEAR ATTACHMENT SUPPORT OVERSIZE HOLE REPAIR. COMPLIED WITH EA 8-5740-73874 WINGS - MAIN FRAME - MAIN LANDING GEAR ATTACHMENT SUPPORT OVERSIZE HOLE REPAIR. 2L73 4F A22WE 20040213000802004021300080EU 2004 2 13 04FDEA00314 120040205A3260BDM3003 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25661FE 760 COULD NOT RAISE HANDLE GEAR LEVER. NO LANDING GEAR RETRACTION. PERFORM ECAM PROC 2ND ATTEMP NR 2 SYSTEM TO RAISE GEAR FAILED. AFTER FURTHER T/S REPLACED PROX DETECTION UNIT PER AMM 32-31-71-4. ALSO REPLACED LANDING GEAR MICRO SWITCH PER AMM 32-31-11-4. PERFORMED ADJ & TEST WITH TEST SET PER AMM 32-31-11-4 AND GEAR RETRACTION INHIBITION TEST ON SYSTEM 1 & 2 PER AMM 32-31-00-5, ALL INDICATIONS CHECK NORMAL. CHECKED SERVICE ON LT PITCH DAMPNER PER AMM 12-12-32-0, SERVICED WITH NITROGEN. CHECKED SECURITY OF SENSORS 9GA & 11GA CHECKS NORMAL. JACKED REAR OF LT BOGIE TO POSITION SENSORS TO READ NEAR ON PROX DETECTOR CHECKS NORMAL. SYSTEM OPS CHECKS NORMAL AT THIS TIME AND OK FOR SERVICE. 2L72 4F RTA35EU 20040213000812004021300081EU 2004 2 13 04FDEA00315 120040205A3231A5281012500051 SEQUENCE VALVE AIRBUS310 A310203 3930313EU ZONE 700 MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25413FE 397 ON DEPARTURE AFTER GEAR RETRACTION THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. AS PER THE QRH, DID NOT RECYCLE BUT PUT THE HANDLE TO OFF. AT THAT POINT, LOTS OF NOISE AND SOME VIBRATION. RETURNED TO KMEM AND THE SPEED NEVER EXCEEDED (270K/M.65). REF THE AIRBUS A310 07-11-00-0, JACKED AIRCRAFT ANY FAULTS NOTED, SIX TIMES IN BOTH SYSTEMS 1 AND 2. REF THE AIRBUS A310 M/M 32-00-00-5, INSTALLED TEST BOX NR 97A32602004201-1 TO AIDE IN THE CYCLING OF THE NOSE GEAR. FURTHER TROUBLESHOOTING REQUIRED. PER MAINTENANCE CONTROL REMOVED AND REPLACED NOSE GEAR DOOR LEFT AND RIGHT SEQUENCE VALVES IAW A310-200MM 32-31-18-4. NOSE GEAR DOOR, RIGG AND OPS CHECK. 2L72 4F RTA35EU 20040213000822004021300082WP 2004 2 13 ABXA040055 120040130A53135616374108 LONGERON DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 AFT ACCESSORY COMPARTMENT CORROSION AT FUSELAGE SKIN AND DOUBLER LONGERON 33 RIGHT, FS 1620 - 1628, ADJACENT TO OUTFLOW VALVE. REPAIRED AREA IAW REA D853-48508MR. 2L74 4F 4A25 20040213000842004021300084WP 2004 2 13 ABXA040056 120040130A533057552713 FINGER DOUBLER DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 FORWARD CARGO LOWER LEFT SKIN FINGER DOUBLER CORRODED UNDERNEATH FROM STA 200 TO 220, LONGERON 35 LEFT TO 33 LEFT, BUTTLINE 7 TO BUTTLINE 20. REPAIRED AREA IAW REA D853-48505MR. 2L74 4F 4A25 20040213000852004021300085WP 2004 2 13 ABXA040057 120040130A571156149332 SPAR DOUG DC8 DC863 302198AWP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 RIGHT WING REAR SPAR XRS 139 JACKPAD TO REAR SPAR FITTING CRACKED. REPAIRED AREA IAW REA D857-48845MR. 2L74 4F 4A25 20040213000882004021300088EU 2004 2 13 00129 120040202A3231 UPLOCK AMD FALC20FALCON 2720302EU MGL DOOR CONTAMINATED E HAEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW05158TW 158 PILOT REPORTED THAT EN ROUTE FROM ATL TO SRB GEAR DOOR LIGHTS REMAINED RED. AIRCRAFT MOVED FROM SRB TO SDF FOR MAINTENANCE ON A SPECIAL FLIGHT PERMIT. RT MAIN GEAR DOOR UPLOCK OUT OF SEQUNCE DUE TO MOISTURE. REPAIRED IAW DA20 M/M CHAP 32, RAN GEAR MULTIPLE TIMES, RETURN TO SERVICE. 2L72 4F A7EU 20040213000912004021300091 2004 2 13 SWIA200412830 420040128A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 NM07167316 6 120190 INFLIGHT AUTOPILOT WOULD NOT HOLD ALTITUDE EITHER SIDE. REPLACED CAPTAINS AUTOPILOT COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040213000922004021300092SO 2004 2 13 SWIA200412831 120040130A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07292UX1935 1935 120292 ON TOUCHDOWN, FLAPS 45 LANDING AND RECEIVED A CONTROL FAULT ALL LIGHT BARS FLASHING 0, QRH PROCEDURE DID NOT FIX. REPLACED FLAP SELECTOR LEVER ASSEMBLY WITH SERVICEABLE UNIT. FLAPS OPS CHECK GOOD. 2L72 4T RTA31SO 20040213000952004021300095EA 2004 2 13 SWIA200412834 120040108A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 MAIN CABIN I/B AND O/B ATTACH CLIPS ARE CRACKED ON LBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20040213000972004021300097EA 2004 2 13 SWIA200412836 120040108A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 CARGO PIT FS 621.00 RBL 42.0 FLOORBEAM ANGLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV-A. 2L72 4F RTA21EA 20040213000982004021300098SO 2004 2 13 SWIA200412837 120040126A5730 PANEL EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07186SW 120034 STRINGER ON LT WING FORWARD OF NR 2 FUEL PANEL CRACKED. DISCOVERED DURING LINE INSPECTION. REPAIRED LEFT WING FORWARD STRINGER AT NR 2 FUEL PANEL IAW SRM 120 57-20-03 PG 205 TO 211, FIG 202 & IAW RII CARD 28-301. 2L72 4T RTA31SO 20040213000992004021300099WP 2004 2 13 ROSS0401 120040203A32207000010101 SWITCH DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NLG INTERMITTENT A ROSAK NONE P NO WARNING INDICATION LDLANDING 1 SW01229DE 47152 UPON EXTENDING GEAR, NOSE GEAR DOWN LIGHTS DID NOT ILLUMINATE, OTHER SWITCHING STUCK IN AIR MODE. NOTE: NO NOSE UNSAFE LIGHT ILLUMINATED, AFTER LANDING TAPPED ON NOSE GEAR DOWNLOCK SWITCH LIGHTS CAME ON. REMOVED AND REPLACED SWITCH AS PER DC9 MM CH 32-60-00 PG 1 PARA 1 GENERAL C 1 THRU 5 ITEM PARA 2A AND B1 AND 2. P/N 700-001-01-01, S/N OFF 9676, S/N ON 10841. 2L72 4F4 F A6WE E2EA 20040213001002004021300100 2004 2 13 AWXA200400141 420040203A2565D31865109 SLIDE AIRBUS320 A320232 3930326EU ZONE 500 - LEFT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28663AW209922485 1419 DURING THRU FLIGHT INSPECTION FOUND THE LT OVERWING EMERGENCY EXIT SLIDE DELAMINATED. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY EXIT SLIDE IAW T/C R1A25301. 2L72 4F RTA28NM 20040213001022004021300102NM 2004 2 13 AWXA200400143 120040119A5754654642389 SKIN BOEING737 737277 1384570NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON LT WING NR 3 SLAT SKIN AT CUTOUT FOR ACTUATOR WS 152. MAINTENANCE BLENDED OUT CRACKED SKIN AT CUTOUT LT WING NR 3 SLAT WS 152; PERFORMED HFEC INSPECTION OF BLEND OUT TO VERIFY NO CRACKS EXIST; TREATED AREA, REPAIR ACCOMPLISHED IAW B737-200 SRM 57-20-01, FIG 001, PG 1-2. 2L72 4F RTA16WE 20040211001392004021100139SO 2004 2 11 C2XA04IA011 120040201A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAL ABORTED APPROACH K FLUID LOSS ININSP/MAINT 1 SW27115364912 2542 145520 FLIGHT 2541 - CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040211001612004021100161EU 2004 2 11 MALA040146 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, ROW 5 SEAT 5B SEAT FRAME CRACKED AT WELD. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 5B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/04. 2H74 4F RTA49EU 20040211001642004021100164EU 2004 2 11 MALA040147 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRME 6B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 6B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001732004021100173EU 2004 2 11 MALA040162 120040120A2520 FRAME BAC 146 AVRO146RJ85A1500097EU SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15510XJ E2323 DURING C-CHECK INSPECTION IN LCQ, SEAT FRAME 14B CRACKED. MAINTENANCE ACCOMPLISHED WELD REPAIR ON SEAT FRAME 14B IAW MESABA EO A25031. A/C RELEASE DATE WAS 01/31/2004. 2H74 4F RTA49EU 20040211001822004021100182NM 2004 2 11 UPS04441799 120040125A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C S-7L STRINGER FOUND CRACK AT STA 1349 STR 7L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5. 2L74 4F A20WE 20040211001862004021100186NM 2004 2 11 UPS04441804 120040123A5411 FRAME BOEING747 747123 1384873NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C NR 4 PYLON - LOWER CAVITY NEAR NAC STA 211 RT VERT SUPPORT RIB CRACKED. NR 4 PYLON - LOWER CAVITY NEAR NAC 221 RT VERTICAL SUPPORT FRAME REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F A20WE 20040211001922004021100192NM 2004 2 11 UPS04441810 120040121A5410 SPAR BOEING747 747123 1384873NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C NR 2 PYLON - LWR WEB CRACKED THRU FASTENERS AFT OF PNEU DUCT CUTOUT APPROX 15 INCHES FWD OF AFT MOUNT, CRACK RUNS LONGITUDINALLY. LWR SPAR 5 LOCATIONS CRACK END BY STOP DRILLED HOLES PER SRM 54-10-03 FIG 2 NDT CONFIRMED NIL CRACKS AND PERFORMED A PERMANENT REPAIRED AS PER SRM 54-10-03 FIG 2 AT NAS STA 213. 2L74 4F A20WE 20040211002052004021100205WP 2004 2 11 AALA20040173 120040203A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21978TW 53628 DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040213000432004021300043EU 2004 2 13 RAIA00401040 120040127A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03572HK 41091 BWI - EXIT LIGHT AT 6A AND ONE STRIP OF PATH WAY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2L72 4T RTA41NM 20040213000472004021300047CE 2004 2 13 58572 120040204A6120 PROPELLER BEECH 1900 1900D 1154162CE RIGHT STUCK A AMWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07165YV UE165 ON POWER UP FOR TAKEOFF THE CREW NOTED THAT THE RIGHT PROP STUCK IN LOW PITCH. RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED LOW PITCH SOLENOID. NO PARTS WERE USED. 2L72 4T RTA24CE 20040213000572004021300057 2004 2 13 SWAA040330 420040201A256565C168209 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRT BARSHEARED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOK FASTENER SHEARED. REMOVED AND REPLACED RETAINER HOOK PER MM. 2L72 4F RTA16WE 20040213000752004021300075EA 2004 2 13 COMA0460113 120040202A3210 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA NOSE SLOW A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01995CA 7229 GEAR DISAGREE WARNING, NLG TOOK SEVERAL MINUTES TO EXTEND. COULD NOT DUPLICATE. FOUND NO DEFECTS, OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040213000902004021300090 2004 2 13 SWIA200412829 420040124A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AHRS MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 NM07416SW9950 9488 7089 WITH THE AUTOPILOT ON, THE CONTROL YOKE JERKS FORWARD SHARPLY. THE JERK IS MILD DURING CRUISE INTERMITTENTLY. THE JERK IS MORE PRONOUNCED DURING THE DESCENT AND LEVEL OFF AT LOW ALTITUDE FOR THE APPROACH. REMOVED AND REPLACED NR 2 AHC COMPUTER. OPS CHECKS GOOD IAW 34-21-01. 2L72 4F4 FRTA21EA E15NE 20040213001032004021300103NM 2004 2 13 AWXA200400144 120040204A3397BMS13311122 WIRE BOEING737 73733A 1384673NM ZONE 900 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 PHX - EEL - FLIGHT CREW REPORTED ELECTRICAL WIRE FOR EMERGENCY LIGHTING BROKEN IN AFT GALLEY AT LT TRASH BIN COMPARTMENT. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT IN AFT GALLEY; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040213001042004021300104NM 2004 2 13 AWXA200400145 120040121A5320 WEB BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR WEB BETWEEN BS 986.5 & BS 1006, RBL 45 TO RBL 65. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 986.5 TO BS 1006, RBL 45 TO RBL 65; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02 FIG 007. 2L72 4F RTA16WE 20040213001062004021300106NM 2004 2 13 AWXA200400147 120040120A5347BAC1520792 SEAT TRACK BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON G-4 GALLEY SEAT TRACK BETWEEN BS 986.5 AND BS 1006, RBL 39. MAINTENANCE REMOVED CORRODED GALLEY SEAT TRACK BETWEEN BS 986.5 AND BS 1006, RBL 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW B737-200 SRM 53-10-05 FIG 002. 2L72 4F RTA16WE 20040213001072004021300107NM 2004 2 13 AWXA200400148 120040121A5753654642825 FLAP TRACK BOEING737 737277 1384570NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER MATING SURFACE OF LT WING OUTBOARD FLAP, INBOARD FLAP TRACK WBL 254 LT. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FLAP, INBOARD FLAP TRACK IAW AWA T/C M3M57006. 2L72 4F RTA16WE 20040213001082004021300108NM 2004 2 13 AWXA200400149 120040121A531565498854 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF TRANSVERSE FLOORBEAM TEE CAP AT BS 986, RBL 35 TO RBL 45, WL 208. MAINTENANCE REMOVED CORROSION ON TRANSVERSE FLOORBEAM TEE CAP AT BS 986, RBL 35 TO RBL 45 AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; FABRICATED A REPAIR STRAP; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 203, PG 212-215. 2L72 4F RTA16WE 20040213001092004021300109NM 2004 2 13 AWXA200400150 120040121A575465C26601282SP WEDGE BOEING737 7373G7 1384595NM NR 6 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND THE NR 6 SLAT WEDGE DELAMINATED AT THE INBOARD END, WS 254 RT. MAINTENANCE REMOVED DAMAGED NR 6 SLAT SKIN AT WS 254; FABRICATED A REPAIR DOUBLER; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-10 FIG 31, PG 88 F, G, H. 2L72 4F RTA16WE 20040213001122004021300112NM 2004 2 13 AWXA200400154 120040202A3350276005 FUSE BOEING737 7373G7 1384595NM R1 DOOR BLOWN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - EEL - DURING C-13 CHECK FOUND THE EMERGENCY EXIT LIGHT ABOVE THE R-1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BLOWN FUSE FOR EMERGENCY EXIT LIGHT ABOVE THE R-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040213001132004021300113NM 2004 2 13 AWXA200400155 120040120A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 2 RT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - EEL - DURING C-13 CHECK FOUND THE EMERGENCY ESCAPE PATH RT NR 2 BULL NOSE LIGHT WIRE BROKEN. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH RT NR 2 BULL NOSE LIGHT WIRE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040213001152004021300115EU 2004 2 13 AALA20040180 120040204A3350 RECEPTACLE AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170072 515 MIA - EMERGENCY LIGHT RECEPTACAL PULLED OUT FROM SEAT 19G AND IS INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 19G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040213001162004021300116WP 2004 2 13 AALA20040181 120040204A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217527A 49919 BOTH FORWARD OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY EXIT SIGNS AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040213001192004021300119SO 2004 2 13 C2XA04SH048 120040205A531514522460013 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV - DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040213001202004021300120SO 2004 2 13 C2XA04SH049 120040204A531514522461001 BUTTSTRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE RIGHT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040213001212004021300121SO 2004 2 13 C2XA04SH050 120040204A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040213001222004021300122SO 2004 2 13 C2XA04SH051 120040204A531514529150003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE FLOORBEAM ANGLE AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040213001242004021300124SO 2004 2 13 C2XA04SH053 120040204A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040217000012004021700001EA 2004 2 17 2004F00055 120040122A7830MS244236 CONTROL VALVE CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE THRUST REVERSER DEFECTIVE A FDKAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07904FJ1420 15004 GEE194205 ABORTED TAKEOFF DUE TO LT ENGINE T/R UNLOCK MSG. MAINTENANCE REPLACED THE ISOLATION CONTROL VALVE ON THE LT THRUST REVERSER. ALL LEAK AND OPERATIONAL CHECKS GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20040217000022004021700002EA 2004 2 17 2004F00056 120040118A5270 SWITCH CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT DIRTY A FDKAO OTHER N FALSE WARNING CRCRUISE 1 SW07903FJ 15003 LT AFT EMERGENCY EXIT DOOR CAUTION ILLUMINATED WITH DOOR SECURED. MAINTENANCE CLEANED DOOR SWITCH AND CYCLED DOOR. SYSTEM CHECKED GOOD. (M) 2L72 4F RTA21EA 20040217000052004021700005CE 2004 2 17 2004F00058 120040115A3233112380022 ACTUATOR BEECH 300 300BEECH 1152930CE NLG WW INOPERATIVE A F0AAO OTHER J WARNING INDICATION APAPPROACH 1 SW2175 FF10 NO NOSE WHEEL GEAR GREEN LIGHT INDICATION WAS OBSERVED WHEN LANDING GEAR WAS EXTENDED. GEAR WAS CYCLED WITH SAME RESULTS, BUT 'RED' GEAR HANDLE LIGHT ILLUMINATED. A/C RETURNED TO BASE. UPON ARRIVAL, GEAR WAS EXTENDED WITH ALL PROPER INDICATIONS, THREE GREEN, NO RED. CRASH/FIRE/RESCUE EQUIPMENT ON STANDBY, A/C LANDED SAFELY. REPLACED NOSE GEAR ACTUATOR. (M) 2L72 4T A24CE 20040217000072004021700007SO 2004 2 17 SIMA200402005 120040101A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE 145589 DURING AN MBV INSPECTION, THE CENTER FLOORBEAM BETWEEN FRAME 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGED SECTION OF THE CENTER FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB145/1142, REV 24, CHAPTER 53-22-10, FIG 201 SHEET 2. (M) 2L72 4F RTT00011AT 20040217000112004021700011NM 2004 2 17 2004F00061 120040112A27512061141 INDICATOR BOEING737 737400 138449ANM TE FLAPS DEFECTIVE A RYNAO OTHER N FALSE WARNING CLCLIMB 1 SW07254RY 24690 ON DEPARTURE FROM MSP, DURING FLAP RETRACTION, DETECTED A ASYMETRICAL TRAILING EDGE FLAP CONDITION. EMERGENCY DECLARED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FLAP POSITION INDICATOR. INSPECTED FLAPS, FLAP DRIVE SYSTEM AND FLAP TRACK SYSTEM. NO DEFECTS NOTED. OPERATIONAL CHECK OF THE SYSTEM NORMAL. (M) 2L72 4F RTA16WE 20040217000232004021700023EA 2004 2 17 ASOA04038 120040115A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE CARGO THRESHOLD FLOOR LANDING PLATE AT FS 589 AND FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO THRESHOLD FLOOR LANDING PLATE AT FS 589 AND FS 605 IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20040217000242004021700024EU 2004 2 17 ASOA04052 120040102A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK BETWEEN FRAME 36 TO FRAME 39 AND THE RIGHT SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 36 TO FRAME 39 AND THE RIGHT SEAT TRACK BETWEEN FRAME 39 TO FRAME 40 IAW SRM 51-25-04 AND 51-25-01. (M) 2H72 4T RT 20040217000252004021700025EA 2004 2 17 ASOA04037 120040115A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDE AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT SIDE AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040217000262004021700026EU 2004 2 17 ASOA04050 120040102A5320 CHANNEL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A C-CHECK IN BNA, THE RIGHT FLOOR SUPPORT ZEE CHANNEL BETWEEN FRAME 39 TO 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SUPPORT ZEE CHANNEL BETWEEN FRAME 39 TO 41 IAW SRM 51-25-01. (M) 2H72 4T RT 20040217000272004021700027EU 2004 2 17 ASOA04051 120040102A5320 DOUBLER AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A C-CHECK IN BNA, THE SERVICE DOOR THRESHOLD DOUBLER FORWARD OF FR 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR THRESHOLD DOUBLER FORWARD OF FRME 36 IAW SRM 51-25-02 AND 51-25-01. (M) 2H72 4T RT 20040217000282004021700028EA 2004 2 17 ASOA04039 120040116A5320601R3110115773 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT THE PILOTS BULKHEAD FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT THE PILOTS BULKHEAD FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040217000302004021700030EA 2004 2 17 ASOA04048 120040118A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11860AS 7433 DURING DESCENT INTO SHV FROM DFW, THE CREW NOTICED A BURNING ODOR COMING FROM THE LT PACK. THE AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE TESTED AND INSPECTED THE LEFT PACK SYSTEM OPERATING THE PACK THROUGH ALL TEMPERATURE RANGES FOR AN EXTENDED PERIOD OF TIME WITH NO ODOR NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000312004021700031EU 2004 2 17 ASOA04049 120040102A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 DURING A C-CHECK IN BNA, FLOOR SUPPORT TEE ANGLE AT THE SERVICE DOOR THRESHOLD BETWEEN FRAME 36 TO FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT TEE ANGLE AT THE SERVICE DOOR THRESHOLD BETWEEN FRAME 36 TO FRAME 38 IAW SRM 51-25-01. (M) 2H72 4T RT 20040217000322004021700032EA 2004 2 17 ASOA04036 120040115A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000342004021700034EA 2004 2 17 ASOA04034 120040114A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE FRAME FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20040217000492004021700049 2004 2 17 2004F00073 420040102A2200 SWITCH BOEING757 75723A 1384967NM EPR FAILED A RYNAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07310FV 25488 ON TAKEOFF ROLL, EPR BUTTON WOULD NOT ILLUMINATE AND EPR READING ON LEFT SIDE WAS LOW. TAKEOFF ABORTED. CLEANED AND REPOSITIONED EPR PUSHBUTTON SWITCH. TESTED THRUST MANAGEMENT COMPUTER. OPERATIONAL CHECKED NORMAL. (M) 2L72 4F RTA2NM 20040217000502004021700050SO 2004 2 17 SIMA200402006 120040101A531514525381003 FLOORBEAM EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21825AE 145589 ABI - DURING MBV INSPECTION, THE LEFT FLOORBEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM EMB-145/1142, REV 24, CHAPTERS 53-21-10, FIGURE 202. (M) 2L72 4F RTT00011AT 20040217000512004021700051SO 2004 2 17 SIMA200402301 120040120A4950 APU EMB 145 EMB145LR 3260212SO CONTAMINATED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21646AE 145213 PIT- FLT 4153 - CRWE REPORTED WITH APU RUNNING AND MAINTEANCE ON BOARD THE CABIN AND COCKPIT FILLED WITH SMOKE. CREW SAID IT SEEMED TO BE COMING FROM THE NR 2 PACK. MAINTENANCE RAN THE NR 2 PACK WITH THE APU AND FOUND NO ODOR. SUSPECT ANTI-ICE FLUID ENTERED THE APU BLEED SYSTEM. COULD NOT DUPLICATE DISCREPANCY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040217000542004021700054EA 2004 2 17 2004F00076 120040116A3260 SENSOR CNDAIRCL600 CL6002B16 1900305EA MLG FAILED A RU3AH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION APAPPROACH 1 SW2187 5190 ON FINAL APPROACH GEAR EXTENSION AND ANTI-SKID OUTBOARD FAIL MALFUNCTION OCCURRED. GEAR RECYCLED AND SOME TROUBLESHOOTING WAS UNSUCCESSFUL. IN FLIGHT EMERGENCY WAS DECLARED, EQUIPMENT CALLED OUT, ANTI-SKID TURNED OFF AND UNEVENTFUL LANDING CARRIED OUT. NO DAMAGE TO TIRES OR AIRCRAFT. REPLACED TWO WHEEL SPEED SENSORS AND REPAIRED BROKEN WIRE. (M) 2L72 4F RTA21EA 20040217000572004021700057EA 2004 2 17 ASOA04046 120040118A5311 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FRAME CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING AN A-CHECK IN BTR, THE DOUBLER ON THE RIGHT FRAME FS 640 AT BL 45 BELOW STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE RIGHT FRAME FS 640 AT BL 45 BELOW STRINGER 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040217000592004021700059NM 2004 2 17 GAIA04005OP 120040122A2611160117301 BATTERY BOEING727 727251 138408HNM SMOKE DETECTOR WEAK A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07278US 21157 FLT 874 - LAX-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT ONE AFT CARGO SMOKE DETECTOR LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERIES IN THE SMOKE DETECTOR AND THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040217000602004021700060NM 2004 2 17 GAIA04001OP 120040117A5712 RIB BOEING727 727243 138408DNM RT WING CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING ROUTINE MAINTENANCE, FOUND CORROSION ON THE RIGHT WING LEADING EDGE SUPPORT RIB AT WING STATION 240. REPAIRED WING RIB IAW BOEING SRM CH 51-40-4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040217000622004021700062NM 2004 2 17 USAABB04009 120040120A3350417T50856 LIGHT BOEING767 7672B7 1385107NM ROW 19F INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19651US 24764 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHT AT ROW 19F INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA1NM 20040217000632004021700063NM 2004 2 17 USAABB04008 120040118A3397 CONNECTOR BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 PHL - FOUND LOW LEVEL LIGHTING AT LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE SECURED A CONNECTOR AT ROW 12, LEFT OVERWING EXIT. (M) 2L72 4F RTA1NM 20040217000642004021700064EA 2004 2 17 ASOA04040 120040117A3350OL307BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURNG AN A-CHECK IN BTR, THE NR 2 EMERGENCY EXIT CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY EXIT CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000652004021700065EA 2004 2 17 ASOA04041 120040117A3350MS2275941229 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE EMERGENCY LIGHT WIRING AT FS 461, RBL 9 WAS FOUND DAMAGED. MAINTENANCE REPAIRED THE EMERGENCY LIGHT WIRING AT FS 461.00, RBL 9. (M) 2L72 4F RTA21EA 20040217000672004021700067EA 2004 2 17 ASOA04043 120040118A5320601R31171917 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040217000682004021700068EA 2004 2 17 ASOA04044 120040118A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUT OUT AT FS 235 IN BOTH CORNERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR CUT OUT AT FS 235 IN BOTH CORNERS IAW ASA EO 600-53-0104. (M) 2L72 4F RTA21EA 20040217000712004021700071EA 2004 2 17 ASOA04032 120040114A3397M2275935229 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11828AS 7213 DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT SIGN BY THE FLOOR AT THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY EXIT SIGN BY THE FLOOR AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000722004021700072EA 2004 2 17 ASOA04031 120040112A5260601R3167013 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11701EV 10020 DURING A GROUND INSPECTION IN ATL, THE LOWER PASSENGER DOOR STEP MOUNTING ARM WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LOWER PASSENGER DOOR STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000792004021700079NE 2004 2 17 JYD2004F00001 120040122A64206516100010041 ROTOR HEAD SKRSKYS64 S64E 8142604NE TAIL ROTOR CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09CGESG42069 64065 DURING NORMAL AC INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET HAS 3 CRACKS RUNNING SPANWISE APPROXIMATELY .398 INCH FROM THE TRAILING EDGE. THE FIRST CRACK IS 7.5 INCH FROM THE TIP END AND .835 INCH LONG. THE SECOND CRACK IS 9 INCHES FROM THE TIP END AND .705 INCHES LONG. THE THIRD CRACK IS 11.875 INCHES FROM THE TIP END AND .684 INCH LONG. PROBABLE CAUSE IS UNKNOWN. THE RECOMMENDATION TO PREVENT RECURRENCE IS NOT KNOWN. (MDR04-041) 2G72 4U H4EA 20040217000932004021700093CE 2004 2 17 JIKA200400002 120040116A282010138901157 CHECK VALVE BEECH 99 C99 1154006CE RT NACELLE STUCK E JIKAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP018227P20913 U194 RT ENG WOULD NOT SHUT-OFF WITH CONDITION LEVER IN CUT-OFF POSITION. ATTEMPTS WERE MADE TO SHUT ENG DOWN WITH CONDITION LEVER; ENG WOULD NOT SHUT-OFF. PILOT CLOSED FUEL SHUT-OFF VALVE, ENG WOULD NOT SHUT DOWN. SHUT ENG DOWN BY MANUALLY MOVING FUEL CUT-OFF VALVE ON FCU TO OFF POSITION. MAINT FOUND CONDITION LEVER CABLE BROKEN AT CABLE HSG IN ENG COMPART THUS NOT ALLOWING ENG TO BE SHUT DOWN WITH CONDITION LEVER. MAINT FOUND CHECK VALVE IN FUEL TRANSFER SYS, STUCK IN OPEN POSITION ALLOWING FUEL TO BE GRAVITY FED BACK TO ENG DRIVEN FUEL PUMP. WITH CHECK VALVE STUCK OPEN AND FUEL SHUT-OFF VALVE CLOSED ENG WOULD NOT ACCELERATE ABOVE 70 PERCENT AND FUEL FLOW WAS FLUCTUATING. 1L72 3T A14CE 20041119000412004111900041EU 2004 11 19 KBM2004F00003 120040907A6720350A21136324 SUPPORT BRACKET SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R BELLCRANK CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 FOUND BRACKET CRACKED UNDER FLOOR STRUCTURE THAT SUPPORTS T/R CONTROL AND BELLCRANK SYSTEM. REPLACED BACKET WITH SERVICEABLE PART. 1G71 3U3 U H9EU E19EU 20040217000942004021700094 2004 2 17 373PA0048 420040129A2230106201730 COMPUTER BOEING737 7373Y0 1384671NM AUTOTHROTTLE INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 AUTO THROTTLE INOPERATIVE. WOULD NOT TEST AFTER INSTALLATION. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-0. OPS CHECKS GOOD. 2L72 4F RTA16WE 20040217000952004021700095CE 2004 2 17 GLBA20030531 120040113A219710136457217 CIRCUIT BOARD BEECH 1900 1900D 1154162CE ENVIRO SYS FAILED A GLBAO OTHER J WARNING INDICATION CLCLIMB 1 NM03204GL2229 UE204 NR 1 AND NR 2 ENVIRO FAILS, REMOVED AND REPLACED A130 PCB. OPS CK GOOD. 2L72 4T RTA24CE 20040217000992004021700099EU 2004 2 17 000011 120040102A2611 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE SMOKE DETECTORS ILLUMINATED A UHLAFD ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL1740SZ 40 E367503 DRG153688 ON 01/02/04, APPROX. 1530 (UTC), FLT 4632 CAK-PIT. THE CARGO AND LAV SMOKE LIGHT CAME ILLUMINATED ON THE GROUND. CREW BLEW THE CARGO FIRE EXTINGUISHER BOTTLE AND EVACUATED PASSENGERS. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040217001002004021700100CE 2004 2 17 0022 120040131A3230MS252534 SWITCH BEECH 200 200BEECH 1152920CE MLG CRACKED E CIEAO OTHER S AFFECT SYSTEMS APAPPROACH 1 NM03520MC 1318 BB43 LANDING GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES. LANDING GEAR WAS EXTENDED MANUALLY AND LANDING WAS PERFORMED NORMALLY. AC HAD BEEN IN AND OUT OF COLD AND SNOW ON ITS PREVIOUS FLIGHTS. AC WAS JACKED IN HANGAR AND GEAR WORKED NORMAL. GEAR WAS CYCLED SEVERAL TIMES. SWITCH WHICH DISABLES ELECTRIC MOTOR DURING AN EMERGENCY GEAR EXTENSION WAS FOUND CRACKED AND COMING APART. SUSPECT IT MIGHT HAVE CREATED AN INTERMITTENT CONNECTION. SWITCH WAS REPLACED AS A PRECAUTION. OTHER ITEMS INSPECTED WAS GEAR RIGGING, LANDING GEAR CONTROL RELAYS, AND GENERAL WIRING. NO OTHER ABNORMAL CONDITIONS WERE FOUND. GEAR WAS CYCLED A MINIMUM OF 20 TIMES IN THE HANGAR AND WORKED NORMAL EVERY TIME. 1L72 4T A24CE 20040217001012004021700101NM 2004 2 17 0400163136 120040130A49901319A APU AIRBUSA319 A319114 3930350NM APU BAY ODOR A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01336NB5518 5518 1683 DURING CLIMB, FUMES WERE REPORTED IN THE CABIN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. MAINTENANCE INSPECTED THE ENGINES, APU, AND AC PNEUMATIC DUCTING SYSTEM AND COMPONENTS. APU WAS PLACED ON MEL AND AC PACK SYSTEM BURNOUT PROCEDURES WERE PERFORMED. 2L72 4F RTA28NM 20040217001032004021700103NM 2004 2 17 0400156302 120040201A3350 LIGHT BOEING747 747451 1384940NM ROW 21A INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 21A TO DOOR 4L. REPAIRED LIGHT ASSEMBLY AT DOOR. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040217001072004021700107NM 2004 2 17 04FDEA00296 120040203A2750 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OB FLAP, IB AFT HINGE ACTUATOR ROD END. HOLE IB (1) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040217001092004021700109WP 2004 2 17 04FDEA00224 120040126A2700ACH702315 FAIRLEAD DOUG DC10 DC1010 3022110WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-5310-73870. FUSELAGE-REPAIR OF CONTROL CABLE FAIRLEAD AT STA 575 AND LBL 41.5. CLOSING ACTION ON 01/25/04.ON N/R S00011.COMPLIED WITH EA 8-5312-73870. 2L73 4F A22WE 20040217001132004021700113EU 2004 2 17 PG92004F00001 120040107A2914A5026780 SHAFT SNIAS 350 AS350B2 8680813EU HYD PUMP SEIZED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19170PA5575 2637 HYDRAULIC PUMP FAILED WITH ONLY 354 HOURS. SHAFT SEIZED TO PUMP AND TO COUPLING. (RMA NR R046420) (K) 1G71 3U H9EU 20040217001142004021700114NM 2004 2 17 QXEA200400060 120040119A2823AV24B1319D2 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09368PH2297 2297 512 FUEL LEAK WAS NOTED COMING FROM THE RT NACELLE. MAINTENANCE INSPECTED THE REFUELING VALVE AND NACELLE. THE REFUEL DEFUEL SHUTOFF VALVE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040217001162004021700116NM 2004 2 17 QXEA200400076 120040126A7312304983401 ACTUATOR VALVE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 INOPERATIVE A QXEAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 NM09400QX6269 4030 NR 2 ENGINE FUEL PUMP IN RED, REDUCED POWER LEVER TILL OUT OF RED. TURNED ON AUXILIARY PUMP AS DIRECTED BY CHECKLIST AFTER TEMP RESTABILIZED. AUXILIARY PUMP OFF, FUEL TEMP BEGAN TO RISE AGAIN. AUXILIARY SELECTED ON FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED FUEL HEATER THERMAL ACTUATOR VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040217001232004021700123WP 2004 2 17 AALA20040113 120040123A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21552AA 53034 ORD) OVERHEAD EMERGENCY LIGHTS AT SEAT 15A INOPERATIVE. REPLACED BATTERY INSIDE BIN 14DEF FOR EMERGENCY LIGHTS ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040217001242004021700124WP 2004 2 17 AALA20040122 120040126A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP SEAT 20 INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217546A 53028 DEN) OVERHEAD EMERGENCY LIGHTS AT SEAT 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEAT 20. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040217001252004021700125NM 2004 2 17 AALA20040114 120040123A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM ROW 7-11 INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21948AN 30086 SNA) EMERGENCY LIGHT AT ROW 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F RTA16WE 20040213000392004021300039WP 2004 2 13 AALA20040175 120040203A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217542A 49996 SAN EMERGENCY EXIT LIGHT SWITCH AT THE FORWARD FLIGHT ATTENDANT PANEL LEFT ON. REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040213000462004021300046EU 2004 2 13 RAIA00402002 120040202A7797 WIRE JETAIRJETSTMJETSTM4101 1500501EU DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03573HK 41092 STL - RIGHT IEC CAPTION LIGHT WITH TORQUE AND FUEL FLUX. MAINTENANCE REPAIRED WIRING AT MONOPOLE CONNECTOR. 2L72 4T RTA41NM 20040213000552004021300055NM 2004 2 13 SWAA040328 120040201A3350 LENS BOEING737 737317 138447PNM EMERGNECY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 FORWARD F/A STATION EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040213000612004021300061NM 2004 2 13 SWAA040334 120040202A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 616, STRINGER 5R AND BS 907, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040213000622004021300062NM 2004 2 13 SWAA040335 120040202A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 227, LBL 11. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040213000632004021300063 2004 2 13 SWAA040336 420040202A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040213000762004021300076WP 2004 2 13 04FDEA00309 120040204A5743ARB0622501502 SUPPORT DOUG DC10 DC1010 3022110WP MLG CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 MAIN LANDING GEAR ATTACHMENT SUPPORT CORROSION REPAIR (P/N ARB0622). WINGS - MAIN FRAME- MAIN LANDING GEAR ATTACHMENT SUPPORT CORROSION REPAIR (P/N ARB0622). 2L73 4F A22WE 20040213000832004021300083WP 2004 2 13 ABXA040053 120040130A53135750198502 LONGERON DOUG DC8 DC863 302198AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 RIGHT WHEEL WELL LONGERON 24 FITTING WAS CRACKED JUST UNDER BOTTLE BOLT. REMOVED AND REPLACED LONGERON 24 RIGHT IAW ABX REA D853-48504MR. 2L74 4F 4A25 20040213000862004021300086WP 2004 2 13 ABXA040054 120040130A531356138627 LONGERON DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 FORWARD ACCESSORY AT STA 25, LONGERON 31 LEFT WAS CORRODED. REPAIRED AREA IAW REA D853-48515MR. 2L74 4F 4A25 20040213000892004021300089EA 2004 2 13 SWIA200412828 120040127A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07443SW 7638 AFTER TAKEOFF, SELECTED FLAP FROM 20 DEGREES TO 8 DEGREES AND GOT A FLAPS FAIL MESSAGE. RETURNED TO FAT. RE-RIGGED FECU IAW 27-51-10. OPS CHECK GOOD ON GROUND. 2L72 4F RTA21EA 20040213000932004021300093EA 2004 2 13 SWIA200412832 120040108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 CABLE FAIRLEAD INTERCOSTAL AT FS 484 RBL 36.0 IS CRACKED AT O/B FLANGE. DISCOVERED DURIING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-059 REV-A. 2L72 4F RTA21EA 20040213000942004021300094EA 2004 2 13 SWIA200412833 120040108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 CABLE FAIRLEAD INTERCOSTAL AT FS 484 LBL 36.0 IS CRACKED AT FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-059 REV-A. 2L72 4F RTA21EA 20040213001012004021300101NM 2004 2 13 AWXA200400142 120040119A531065C807351 CREASE BEAM BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT MAIN CABIN CREASE BEAM BETWEEN BS 947 AND BS 1006, RBL 65. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 920 TO BS 1006, RBL 65; FABRICATED A NEW REPLACEMENT CREASE BEAM; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-02. 2L72 4F RTA16WE 20040213001052004021300105NM 2004 2 13 AWXA200400146 120040120A53476546813109 SEAT TRACK BOEING737 737277 1384570NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON SEAT TRACK AT BS 532, LBL 45. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK FROM BS 520 TO BS 540, LBL 45; IAW B737-200 SRM 53-10-05 FIG 002. 2L72 4F RTA16WE 20040213001112004021300111 2004 2 13 AWXA200400153 420040127A2565D30664109 SLIDE AIRBUS320 A320231 3930325EU R1 DOOR LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW429325221 091 MCN - EES - DURING C-03 CHECK FOUND THE R-1 DOOR SLIDE CONTACTING THE FUSELAGE BEFORE THE DOOR WOULD FULLY OPEN. MAINTENANCE FOUND THE R-1 DOOR SLIDE LACING BECAME RELAXED. REMOVED AND REPLACED R-1 DOOR SLIDE IAW T/C C1C52309, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040213001232004021300123SO 2004 2 13 C2XA04SH052 120040204A532014521718003 ANGLE EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE LOWER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040217000552004021700055NM 2004 2 17 GAIA04002OP 120040117A2824 VALVE BOEING727 7272J0 138407ENM RT WING MALFUNCTIONED A GAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07281KH 21105 FLT 2872 - LAX-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE NR 2 FUEL CROSS FEED VALVE APPEARED TO BE CLOSED. THE CREW DECIDED TO MAKE A PRECAUTIONARY LANDING IN PHX. OPENED THE NR 2 TANK TO ENGINE VALVE AND SAFETIED OPEN PER THE BOEING DISPATCH DEVIATION PROCEDURE GUIDE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040217000582004021700058 2004 2 17 GAIA04004OP 420040121A220025858029 CONTROL PANEL BOEING727 727251 138408HNM AUTOPILOT SYS INTERMITTENT A GAIAO OTHER O OTHER CRCRUISE 1 SW07278US 21157 FLT 851 - SEA-FWA - DURING CRUISE, THE FILGHT CREW NOTICED THAT THE AUTOPILOT IN A MODE WITH THE HEADING SELECTOR ON OR OFF INTERMITTENTLY LOCKS UP. REMOVED AND REPLACED THE AUTOPILOT CONTROL PANEL. OPERATIONAL CHECKS ON THE GROUND FOUND NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040217000702004021700070EA 2004 2 17 ASOA04033 120040114A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE LOWER STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040217000812004021700081WP 2004 2 17 ABXA040032 120040107A3310 LIGHT DOUG DC9 DC931 3022065WP COCKPIT MISINSTALLED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23946AX 47003 BLUE ELECTRICAL ARCING BEHIND LT OVERHEAD MAP LIGHT. BREAKER TRIPPED (T-42). FOUND GROUND POST HAVING WRONG HARDWARE. INSTALLED CORRECT HARDWARE AND RESET CIRCUIT BREAKER. OPS CHECKED GOOD IAW MM. 2L72 4F A6WE 20040217000822004021700082NM 2004 2 17 AALA20040148 120040128A3350 BATTERY BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21756AM 30264 ORD EMERGENCY LIGHTS AT SEATS 20 TO 27D AND 20 TO 23G INOPERATIVE. REPLACED BATTERY FOR EMERGENCY LIGHTS AT SEATS 20 TO 27D AND 20 TO 23G. SYSTEM GROUND CHECKED NORMAL OPERATION. -CLOSED- 2L72 4F RTT00001SE 20040217000922004021700092 2004 2 17 P5CA0401029 420040118A3160 DISPLAY BOEING747 74747UF 1384949NM COCKPIT FAILED A P5CAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP23496MC 29257 EXTERNAL POWER FAILED TWICE. WHEN RESTORED, FO'S PFD REMAINED BLANK. SWAPPED LOWER EICAS DISPLAY WITH FO'S PFD AND DEFERRED IAW MEL 31-61-1. DMI AUTH. NR 32082. 2L74 4F RT1384945 20040217001102004021700110EU 2004 2 17 YENA200404 120040119A5220L32A319160001 RELEASE CABLE AIRBUS320 A320232 3930326EU EMERGENCY EXIT BINDING A YENAK NONE O OTHER ININSP/MAINT 1 EA15556JB4433 1904 LT EMERGENCY EXIT RELEASE CABLE STIFF, CABLE DOES NOT EXTEND AS SOON AS THE LATCH PIN DISENGAGES FROM THE RELEASE LEVER WITH SPRING-LOADED TEST TOOL CONNECTED TO CABLE IAW CARD 522100-01-1. REPLACED OVERWING EXIT CONTROL CABLE ASSEMBLY IAW AMM 25-62-43-000-001. 2L72 4F RTA28NM 20040217001192004021700119NM 2004 2 17 AALA20040112 120040123A3350 BALLAST BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21959AN 30828 ORD EMERGENCY EXIT LIGHT AT RT FORWARD SIDEWALL INOPERATIVE. REPLACED BALLAST FOR EMERGENCY EXIT LIGHT AT RT FORWARD SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040217001212004021700121WP 2004 2 17 AALA20040118 120040124A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21450AA 49476 SAT) EMERGENCY LIGHTS ABOVE BOTH WING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS ABOVE BOTH WING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040217001222004021700122NM 2004 2 17 AALA20040099 120040123A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERTGENCY LIGHTINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21959AN 30828 ORD) EMERGENCY LIGHT AT AFT RT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT RT OVERWING LOCATION. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040217001292004021700129SO 2004 2 17 C2XA04BT015 120040201A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711536 145520 EWR---CO2430, DURING EWR TURNAROUND MAINTENANCE FOUND EMERGENCY BATTERY PACK TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, IAW EMB145 AMM NR 33-50-00 OPS. CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20040217001312004021700131WP 2004 2 17 EOO2004F00000 120040106A2700369A7304 BRACKET HUGHES369 369D 4470706WP ALLSN 250C 250C* GL FLIGHT CONTROLS DAMAGED B EOORK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03511SB11913 1090592D FOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SORT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (K) (ALO3200411231) 1G71 3U3 U H3WE E4CE 20040217001332004021700133NM 2004 2 17 373PA0034 120040202A5314 KEELBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 CORROSION IN RT KEELBEAM BETWEEN AIR CONDITIONING DOORS. REPAIRED KEELBEAM IAW PACE EA NO. 53-021. 2L72 4F RTA16WE 20040217001342004021700134NM 2004 2 17 373PA0036 120040202A5320 PLATE BOEING737 7373Y0 1384671NM CARGO BAY CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 AFT CARGO SCUFF PLATE HAS FASTENER HOLE CRACKED OUT. REPAIRED IAW SPM 20-3 AND MFG PROCESS SPEC. BAC5975. 2L72 4F RTA16WE 20040217001352004021700135NM 2004 2 17 DHL2004765001 120040131A2612 WARNING LIGHT BOEING727 727264 138408MNM CARGO FIRE FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01765AT 23014 CARGO FIRE DETECTION SYSTEM FAULT LIGHT ILLUMINATED DURING FLIGHT. TESTED SYSTEM IAW MM, NO FAULT INDICATED. OK FOR FURTHER SERVICE. 2L73 4F A3WE 20040217001372004021700137SO 2004 2 17 C2XA04BT014 120040131A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2748901 145501 DURING SERVICE/ROUTINE CHECK, MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHT TO BE INOPERATIVE ON THE RT SIDE. REMOVED AND REPLACED RT FORWARD OVERWING EMERGENCY LIGHT IAW EMB145 AMM NR 33-50-07, OPS. CHECKED GOOD. 2L72 4T RTT00011AT 20040217001392004021700139SO 2004 2 17 C2XA04TY019 120040118A532014525480003 SILL EMB 135 EMB135ER 3260203SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714505 145192 DURING A SCHEDULED INSPECTION THE CARGO DOOR LOWER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL BEAM. IAW-EMB-SRM-51-40-02. 2L72 4F RTT00011AT 20040217001402004021700140WP 2004 2 17 04FDEA00226 120040126A3260 PROXIMITY SWITCH DOUG DC10 DC1010 3022110WP MLG FAULTY A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25374FE 46612 WHEN WE LOWERED THE GEAR FOR LANDING WE FELT THE GEAR COME DOWN BUT RED LIGHTS STAYED ON. WE MOVED THE HANDLE A FEW TIMES BUT NO HELP. RECYCLED GEAR AND THE RED LIGHTS STAYED ON. JIGGLED THE HANDLE AND THE LIGHTS FINALLY TURNED GREEN ALL AT THE SAME TIME. INDICATIONS SAME AT THE S/O PANEL . FACT IAW TAFI, 32-30-00-BB REMOVED AND REPLACED PROXIMITY SWITCH CONTROL UNIT IAW MM 32-61-00-2. OPS CHECKS GOOD. 2L73 4F A22WE 20040217001452004021700145EU 2004 2 17 YENA200403 120040119A5220L32A319160001 RELEASE CABLE AIRBUS320 A320232 3930326EU CABIN BINDING A YENAK NONE O OTHER ININSP/MAINT 1 EA15556JB4433 1904 RT EMERGENCY EXIT RELEASE CABLE STIFF, CABLE DOES NOT EXTEND AS SOON AS THE LATCH PIN DISENGAGES FROM THE RELEASE LEVER WITH SPRING-LOADED TEST TOOL CONNECTED TO CABLE IAW JOB CARD 522100-01-1. REPLACED OVERWING EXIT CONTROL CABLE ASSEMBLY IAW AMM 25-62-43-000-001. 2L72 4F RTA28NM 20040217001492004021700149NM 2004 2 17 DHL2004752502 120040104A5330 SKIN BOEING727 727223 1384074NM CARGO DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING "C" CHECK, FUSELAGE EXTERIOR NR 1 CARGO DOOR SKIN IS DENTED LOWER AFT SIDE. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 52-00-02. CUT OUT DAMAGED AREA DIM. 1.7500 INCHES X 1INCH AND FABRICATED DOUBLER REPAIR FROM MAT 2024-T3 .050 P.O.NR 900471 DIM. 7.2500 INCH X 6.7500 INCH IAW SRM 52-00-3 FIG. 3. TREATED AND PRIMED IAW SRM 51-10-2. 3) INSTALLED DOUBLER REPAIR FROM NR 1 CARGO DOOR SKIN IAW SRM 51-30-2. 2L73 4F A3WE 20040217001512004021700151NM 2004 2 17 AALA20040123 120040125A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21924AN 29525 DTW EMERGENCY LIGHTS AT SEATS 12D, 13D, AND 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 12D, 13D, AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040217001572004021700157NE 2004 2 17 NACA20040001 220040104A8530356993 CYLINDER HEAD DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 6 CRACKED A NACAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 AL03438722283 2283 533294 35358 NR 1 ENGINE SHUT DOWN DUE TO HIGH OIL LOSS. REPLACED NR 1 ENGINE, NR 6 CYLINDER DUE TO CRACKED HEAD. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040217001632004021700163WP 2004 2 17 AALA20040128 120040122A33501001191 LIGHT DOUG DC9 DC982 3022082WP L1 DOOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21207AA 49158 DFW PORTABLE EMERGENCY PATH LIGHT AT L1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY PATH LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040217001722004021700172WP 2004 2 17 AALA20040115 120040124A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 ORD EMERGENCY LIGHTS ON CEILING AT ROW 8 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 8 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040217001732004021700173WP 2004 2 17 AALA20040116 120040124A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 ORD OVERWING EMERGENCY LIGHTS AT OVERWING EXIT IN ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS AT 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040217001742004021700174NM 2004 2 17 AALA20040117 120040124A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21630AA 24588 SFO EMERGENCY ESCAPE PATH LIGHT AT 20D INOPERATIVE. REPAIRED BROKEN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA2NM 20040217001752004021700175NM 2004 2 17 QXEA200400061 120040116A2823AV24B1319D3 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH3963 3963 506 SEA - FLIGHT 2074 - FUEL LEAKING FROM FUELING PANEL AREA. MAINTENANCE REPLACED THE REFUEL/DEFUEL SHUTOFF VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040217001762004021700176CE 2004 2 17 ACE012504 120040125A2822RA5326 DIAPHRAGM BEECH 1900 1900C 1154161CE FUEL PUMP RUPTURED E YADAK NONE K FLUID LOSS ININSP/MAINT 1 AL03114AX1791 UC36 MAINTENANCE NOTICED FUEL DRAINING FROM ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP DUE RUPTURED DIAPHRAGM 2L72 4T RTA24CE 20040217001772004021700177EA 2004 2 17 COMA0460024 120040105A284073664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FUEL INDICATION MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01798CA6013 7348 FLIGHT 5816 FUEL IMBALANCE AND SEVERE FUEL LOSS INDICATION. REPLACED THE FUEL COMPUTER. 2L72 4F RTA21EA 20040218000122004021800012NM 2004 2 18 04FDEA00021 120040104A5753ANB7254502 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING I/B FLAP SIDE LOAD FITTING FOUND CRACKED. RT WING I/B FLAP SIDE LOAD FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. 2L73 4F RTA22WE 20040218000132004021800013NM 2004 2 18 04FDEA00027 120040105A5712 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 RIGHT WING LOWER WINGLET FOUND CRACKED. RT WING LOWER WINGLET SUPPORT RIB REMOVED AND NEW RIB INSTALLED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040218000162004021800016 2004 2 18 GLBA20030523 420040101A3454 ANTENNA BEECH 1900 1900D 1154162CE VOR SYSTEM MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03208GL UE208 BOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, R&R ANTENNA 2L72 4T RTA24CE 20040218000212004021800021NE 2004 2 18 2004UALA00003 220040105A723052A241 FAN BLADE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 1 ENGINE CONTAMINATED A UALAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 WP29220UA10333 30223 222149 HIGH ENGINE VIBRATION ON NR 1. ENGINE CONDITION MONITORING DETECTED HIGH N1 FREQUENCY VIBRATION ON ALL 3 ACCELEROMETERS, ACCOMPANIED BY DOWNWARD SHIFT IN EGT MARGIN. CONSEQUENTLY, IMPENDING ENGINE FAILURE WAS SUSPECTED. THE EGT LOSS WAS SUBSEQUENTLY DETERMINED TO BE THE 2.5 BLEED NOT CLOSING FIRMLY & CONSISTENTLY ON TAKEOFF. THE VIBRATION WAS DETERMINED TO BE THE RESULT OF AN UNEVEN DISTRIBUTION OF DEICING FLUID AROUND FAN BLADE ROOTS. THIS PATTERN OF SHARP VIBRATION INCREASE, AND SUBSEQUENT RECOVERY, HAS BEEN SEEN BEFORE AFTER TAKEOFFS IN ICING CONDITIONS, BUT NEVER BEFORE AT SUCH HIGH VALUES. 2L72 4F4 FRTT0001SE E46NE 20040218000222004021800022 2004 2 18 2004UALA00014 420040107A2200SC47003 DAMPER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 YAW LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29401UA 435 16909 AIRCRAFT LANDED UNDER AMBER ALERT DUE TO FAILURE OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. SUBSEQUENT REPLACEMENT WITH NEW YAW DAMPER AND OPS CHECK WERE ACCOMPLISHED WITH NO FURTHER ANOMALY. 2L72 4F4 FRTA28NM E40NE 20040218000252004021800025NM 2004 2 18 04FDEA00144 120040113A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OD FLAP IB HINGE (WING MOUNTED), SIDE LOAD STRAP MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040218000272004021800027NM 2004 2 18 04FDEA00146 120040113A5753ARC70541 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OB FLAP VANE TEE FITTING NR 2 (COUNTING FROM IB) FOUND CORROSION ON FORWARD HOLE BORE AREA. RT OUTBD FLAP VANE TEE FITTING NR 2 REPAIRED AS PER FEDEX EA 1575074288, WINGS, LT & RT OUTBD FLAP, NR 2 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040218000282004021800028 2004 2 18 AALA20040056 420040108A25655A33073 SLIDE BOEING737 737823 13844BZNM RIGHT FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21906AN 29508 TUL, DURING SCHEDULED HEAVY C-1 MAINTENANCE RT EMERGENCY ESCAPE SLIDE AT FORWARD GALLEY FAILED TEST TO DEPLOY AUTOMATICALLY WITHIN 10 SECONDS. MANUAL DEPLOY FUNCTION NORMAL. REMOVED RT FORWARD ESCAPE SLIDE FROM AIRCRAFT PER MM 25-66-01. SLIDE SENT TO SHOP FOR OVERHAUL.--SUPP CLOSED-- 2L72 4F RTA16WE 20040218000302004021800030NM 2004 2 18 04FDEA00164 120040115A5347AEA732515 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RIGHT STA 1250 TO 1361 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 TO 1361 SEAT TRACK REF. X = 75.25. CORROSION ON SEAT TRACK REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL. II. MATERIAL THK: 0.080, THK REMAINED: 0.074 WITHIN LIMIT AS PER SRM 53-70-00 VOL. I. 2L73 4F RTA22WE 20040218000322004021800032NM 2004 2 18 UPS04441730 120040102A5320 FLOOR SUPPORT BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, MAIN DECK - BS 1236, RBL 116. LONGITUDINAL FLOOR SUPPORT I/B FLANGE FOUND CRACKED AS MARKED. FLOOR SUPPORT REPAIRED PER SRM 51-40-02 FIG 02. 2L74 4F A20WE 20040218000332004021800033NM 2004 2 18 UPS04441731 120040105A5712 SHEAR TIE BOEING747 747123F NM RT WING RIB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, RT WING, NR 3 MAIN TANK INTERNAL RIB 469.82 FWD SHEAR TIE FOUND CRACKED. RIB REPAIRED AS PER SRM 57-10-05 AND CWS FOR WORK DETAIL. 2L74 4F A20WE 20040218000342004021800034NM 2004 2 18 UPS04441732 120040104A5315 FLOORBEAM BOEING747 747123F NM COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, COCKPIT BS 380, LBL 22-24, FLOORBEAM UPPER TEE AFT FLANGE FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. 2L74 4F A20WE 20040218000352004021800035NM 2004 2 18 UPS04441733 120040101A5230 SKIN BOEING747 747123F NM CARGO DOOR DEFORMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, BULK CARGO DOOR FWD LOWER EXT SKIN DEFORM. DEFECTIVE AREA DOOR SKIN REPAIRED IAW SRM 52-00-03 FIG 3. 2L74 4F A20WE 20040218000372004021800037NM 2004 2 18 UPS04441735 120040105A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, UPPER DECK, BS 400 RBL 30 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.050 X 2 X 2 INCH. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 4. 2L74 4F A20WE 20040218000382004021800038NM 2004 2 18 UPS04441736 120040104A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, UPPER DECK, BS 530 - 590, RBL 66. TIE DOWN TRACK FLANGE AND CROWN AREA FOUND CORROSION. CORROSION BLEND OUT 0.053 X 0.5 X 2.5 INCH. BS 500 TO BS 590 RBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20040218000392004021800039NM 2004 2 18 UPS04441737 120040104A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, UPPER DECK, BS 510 - 530, LBL 66 TIE DOWN TRACK CROWN AREA FOUND CORRODED. CORROSION BLEND OUT 0.045 X 0.5 X 2 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20040218000412004021800041NE 2004 2 18 XNOA1173 220040122A7421 IGNITER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 ENGINE MALFUNCTIONED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2313974 126 NR 1 ENG B-SYSTEM IGNITION FAIL WITH IGNITION B-CIRCUIT BREAKER POPPED & NR 1 ENG IGNITION EXCITER POWER TRANSFER FAILED. RETIGHTENED B-IGNITER BOX PER A-300 AMM 74-21-00, OPS CHECK GOOD. DUE TO POWER TRANSFER FAIL, A-SYS INOP, POWER TRANSFER NOT REQUIRED UTILIZING B-SYS PER AMM 74-00-01-1. TRANSFERRED TO DMI 4023, CAT-C, PLACARD INSTALLED. R&R A-SYSTEM IGNITER PLUG AS REQ IAW A-300 AMM 74-21-01, OPS CK GOOD. THIS CLEARS DMI 4023, PLACARDS REMOVED. (STATUS: SUPP/CLOSED) 2L72 4F4 FRTA35EU E23EA 20040218000432004021800043NM 2004 2 18 C8GA20040001 120040203A5753 TENSION SPRING BOEING727 727223 1384074NM TE FLAP WEAK A C8GAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO15899AA 22015 DURING CLIMBOUT, KIAS 225 A/C EXPERIENCE AIRFRAME VIB. ADVISED CCIA FLT FOLLOWING & ATC OF PROBLEM & AIR TURNBACK. NO EMERGENCY ACTION TAKEN & A/C LANDED W/O INCIDENT. A/C INSPECTED & FOUND INBRD FLAPS ECCENTRICS NUT MISSING. REPLACED & ADJUST ECCENTRICS PER B727 MM. INSPECTED ALL FLT SURFACES, NO DEFECTS NOTED. A/C RETURNED TO SERVICE. DURING CLIMB, KIAS 225 NOTED AIRFRAME VIB MORE THAN PREVIOUS FLT. INFORMED CCIA FLT FOLLOWING, NOTIFIED ATC & A/C DIVERTED & LANDED W/O INCIDENT. A/C INSPECTED PER B727 MM INFLT VIBRATION TROUBLESHOOTING & FOUND A WEAK TENSION SPRING ON RT INBRD AFT FLAP. REPLACED TENSION SPRING IAW MM. LAF ACCOMPLISHED SATISFACTORY, NO VIB NOTED. A/C RETURNED TO SERVICE. (K) 2L73 4F A3WE 20040218000442004021800044WP 2004 2 18 ARWA20040101 120040112A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 DURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND, FUSELAGE EXTERIOR STA 1690 BETWEEN L-35R AND L-36 SKIN BROKEN, NEAR BUTT JOINT. PERFORMED REPAIR OF THE SKIN NEAR BUTT JOINT AT STA 1690, BTW LONGERON 35R & 36R IAW DC8SRM 53-2-1, FIG8, SHEET 1,2, PAGES 123/124 AND 125/126, AND TR 53-173. THE DETAIL OF THE REPAIRS FOLLOWED INSTRUCTIONS OF SERVICE REWORK DWG SR08530010, INCLUDED IN THE ABOVE SRM REFERENCE. SKIN REPLACED BTW LONGERON 31L AND 31R. 2L74 4F 4A25 20040218000452004021800045WP 2004 2 18 ARWA20040102 120040113A5310 DOOR FRAME DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 DURING AN A-CHECK INSPECTION, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB TOP FORWARD CORNER WITH CRACK STA 1440.000. TRIMMED OUT CRACK & FABRICATED FILLER, DOUBLER AND TRIPLER IAW DC8SRM 53-2-0, TR 53-188 AND SRM 51-1-21, 51-1-20D & 51-1-11. 2L74 4F 4A25 20040218000462004021800046NE 2004 2 18 ARWA20040103 220040119A7220 LINER LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE NR 3 ENGINE DAMAGED A ARWAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO19307GB694961224 193U1131 14613 ENGINE NR 3 EXPERIENCED A SLOW INCREASE IN VIBRATION FROM 105 TO 218 UNITS IN 3 MINUTES WITH A OR B SELECTED. ALL OTHER PARAMETERS NORMAL. INSPECT MASTER AND INTERNAL GEARBOX CHIP DETECTORS AND OIL FILTERS, NO EVIDENCE OF ENGINE FAILURE NOTED. ACOMPLISHED BOROSCOPE INSPECTION , NO DEFECTS NOTED. REMOVED, CLEANED, LUBRICATED AND RE-INSTALLED FAN BLADES. FOUND DAMAGE FAN ATRITTION LINER, REPAIR LINER IAW RB211 MM 72-31-01. ACCOMPLISHED VIBRATION SURVEY IAW RR MM 71-00-00, FOUND NORMAL. AIRCRAFT RETURN TO SERVICE. 2L73 4F4 F A23WE E12EU 20040218000472004021800047NM 2004 2 18 SWAA040351 120040202A79206558234 SWITCH BOEING737 7372H4 138448CNM NR 1 ENGINE FAULTY A SWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW29103SW 23109 INFLIGHT SHUTDOWN, AIRTURN BACK, DECLARED EMERGENCY, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED OIL FILTER, NO DEFECTS NOTED. DEFERRED OIL BYPASS SYSTEM PER MEL. ON 02/06/04 AT DAL, REMOVED AND REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH PER MM. 2L72 4F A16WE 20040218000502004021800050WP 2004 2 18 DHL2004804002 120040123A2612 CONNECTOR DOUG DC8 DC873F 302199FWP NR 4 FIRE LOOP DAMAGED A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01804DH 46124 SHORTLY FOLLOWING ENGINE START, NR 4 ENG SHORT CIRCUIT FIRE CAUTION LIGHT BEGAN FLASHING. LOOP-A TESTED OK SWITCHED TO B-LOOP MEL 26-2-3 CONTROL 15484. DEFERRED NR 4 ENGINE A-LOOP IAW MEL 26-2-3 DMI 15484 PLACARD INSTALLED. SHORTLY FOLLOWING ENGINE START NR 4 ENG SHORT CIRCUIT FIRE CAUTION LIGHT BEGAN FLASHING (LOOP-A), TESTED OK SWITCHED TO LOOP-B. INSPECTED NR 4 ENG LOOP-A GROMMETS & CONNECTIONS. R & R NR 4 POWER CONTROL UNIT, NO HELP. DMI 15484 REMAINS OPEN FOR FURTHER TROUBLESHOOTING. REPLACED ORIGINAL CONTROL UNIT IAW 26-10-00. DMI 15484, NR 4 ENGINE SHORT CIRCUIT LIGHT BEGAN FLASHING, LOOP-A. R & R A-LOOP CONNECTOR P17051 IAW MM. OPS CHECKED OK. NO DEFECTS NOTED. THIS CLEARS DMI 15484. 2L74 4F RT4A25 20040218000522004021800052NM 2004 2 18 UPS04M41774 120040121A3350 BATTERY DOUG MD11 MD11F 3023600NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP INSPECTION TYPE: PFLT, EMERGENCY LIGHT BATTERY 1 LOW ALERT APPEARS WHEN EMERGENCY LIGHTS ARE TESTED. R&R RECHARGEABLE BATTERY FOR EMERGENCY LIGHTS POWER SUPPLY IAW MM 33-51-01 OPS CHECKED OK. THIS CLOSES DEF M274570. 2L73 4F RTA22WE 20040218000552004021800055NM 2004 2 18 04FDEA00193 120040120A5320AFA3159539 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y= 675.00 THRU Y= 695.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218000582004021800058NM 2004 2 18 DHL2004747002 120040123A7711BACC45FT14A7S CONNECTOR BOEING727 727224 1384076NM NR 3 EPR IND FAILED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01747DH 22253 NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLIED. (TOGW 144900, IAS 20 KTS, OAT -16 C, 500 FT PA, AND BRAKE ENERGY ZONE NORMAL). TRANSFERRED TO DMI LOG 15488 MEL REF 77-1-1. PLACARDS INSTALLED. REF. DMI 15488 - NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLIED. TROUBLESHOT NR 3 ENGINE PER B-727 M/M 77-11-0. LEAK CHECK OF PT2/7 LINES OK. EVACUATED PT 2/7 LINES WITH NITROGEN. EVACUATED NOSE DOME. RANG WIRES & GROUNDS INDICATOR TO TRANSMITTER, CHECKED GOOD. RECOMMEND REPLACE CONNECTOR AT TRANSMITTER. DMI 15488 REMAINS. REF. DMI 15488 - NR 3 EPR GAUGE FAILED TO COME UP WHEN POWER APPLIED. REMOVED AND REPLACED CONNECTOR D840 AT NR 3 EPR TRANSMITTER PER B-727 W/D 77-13-01. RAN ENGINE AND OPS CHECKED GOO2L73 4F A3WE 20040218000592004021800059NM 2004 2 18 04FDEA00213 120040123A53306518420 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 RT EXTERIOR FUSELAGE SKIN HAS A DENT AT BS 196 BELOW STR 19R 4 INCHES BELOW SKIN LAP. REMOVED DAMAGE AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. 2L73 4F RTA3WE 20040218000632004021800063NM 2004 2 18 04FDEA00208 120040123A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 AFT CARGO BAY, FRAME IS DENTED AT BS 1070 BETWEEN STRINGER 25 RT AND 27 RT. REPAIRED AFT CARGO BAY FRAME AT BS 1070 STR 25-27R IAW FED EX E.A. 7-5310-55218. 2L73 4F RTA3WE 20040218000642004021800064NM 2004 2 18 04FDEA00200 120040121A5712ARC29663 RIB DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 FOUND DEEP CHAFING MARK ON LEFT INBOARD FLAP OUTBOARD VANE TRACK OUTBOARD SUPPORT RIB AT LEADING EDGE AREA. DEEP CHAFING REWORKED AS PER SRM 51-21-01, VOL.II AND EA 1-5750- 74284. WINGS - LEFT INBOARD FLAP VANE SUPPORT - RIB CHAFED ) AT LT INBD FLAP, OUTBD VANE TRACK OUTBD SUPPORT RIB LEADING EDGE AREA. 2L73 4F RTA22WE 20040213000492004021300049NM 2004 2 13 SWAA040322 120040131A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 1, WL 186.5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040213000502004021300050NM 2004 2 13 SWAA040323 120040131A26203370002 CONNECTOR BOEING737 7377H4 1384404NM DISCHARGE HANDLESHORTED A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29416WN 32453 DIVERSION, APU BOTTLE DISCHARGED, LIGHT CAME ON IN FLIGHT WITH ASSOCIATED BURNING ODOR. PINS 7/8 ON REMOTE DISCHARGE HANDLE IN WHEELWELL SHORTED, REPAIRED SAME PER MM. 2L72 4F RTA16WE 20040213000582004021300058NM 2004 2 13 SWAA040331 120040201A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9R. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040213000592004021300059NM 2004 2 13 SWAA040332 120040202A3350 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29410WN 27897 EEPLS COVER CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040213000642004021300064NM 2004 2 13 SWAA040337 120040202A33501619 LAMP BOEING737 7377H4 1384404NM LT OVERWING EXITINOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040213000692004021300069CE 2004 2 13 58580 120040204A3242 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER LDLANDING 1 CE07146ZV UE146 WHILE AIRCRAFT ARRIVED IN FARMINGTON, NEW MEXICO ON FLIGHT 715 THE PARKING BRAKE WHEN APPLIED THE PEDALS WERE MUSHY. MAINTENANCE BLED THE BRAKES. THE AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE USED. 2L72 4T RTA24CE 20040213000782004021300078NM 2004 2 13 04FDEA00312 120040205A5230AFA80821 FITTING DOUG MD11 MD11 3023602NM ZONE 800 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CTR CARGO - DOOR BETWEEN NR 1 & 2 LATCH FROM FWD GUIDE FITTING CHAFING. FEDEX EA 1-5230-74188 HAS BEEN COMPLIED WITH & FOUND SATISFACTORY. 2L73 4F RTA22WE 20040213000792004021300079NM 2004 2 13 04FDEA00313 120040205A2750MS9391130ZE MOTOR BOEING727 727200 138407ENM TE FLAPS LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25245FE7357 2852 22016 DURING CLIMBOUT FROM EWR AT 25,000 FT CREW NOTICED A RAPID LOSS OF HYDRAULIC SYSTEM-A FLUID FOLLOWED PROPER CHECKLISTS AND RETURNED TO BASE. EVENTUALLY LOST ALL SYSTEM-A FLUID. FOUND HYDRAULIC FLUID POURING OUT OF CASE DRAIN OVERFLOW LINE FROM FLAP DRIVE MOTOR IN RT WHEEL WELL. REMOVED FLAP DRIVE MOTOR. REPLACED RT HYDRAULIC FLAP DRIVE MOTOR IAW M/M 27-51-062-4, OPS CHECKS GOOD. BECAUSE OF WRITE-UP, ALSO REPLACED BOTH NR 1 AND 2 ENGINE CASE DRAIN FILTERS IAW M/M 29-11-041-2. THERE WAS NO CONTAMINATION FOUND IN OLD FILTERS. 2L73 4F RTA3WE 20040213000872004021300087WP 2004 2 13 ABXA040058 120040130A575356559881 ANGLE DOUG DC8 DC863 302198AWP LT WING GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 LEFT WING OUTBOARD FLAP STA 219 FOLD HINGE COVER WELL OUTBOARD LOWER SIDE GOUGED. REPAIRED AREA IAW REA D827-48510MR. 2L74 4F 4A25 20040213000962004021300096EA 2004 2 13 SWIA200412835 120040108A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 MAIN CABIN INBOARD AND OUTBOARD ATTACH CLIPS ARE CRACKED ON RBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20040213001102004021300110NM 2004 2 13 AWXA200400151 120040119A57536546431280 SKIN BOEING737 7373G7 1384595NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28322AW 25400 MCN - MAJOR REPAIR - DURING C-13 CHECK FOUND DISBOND AREA OF UPPER RT OUTBOARD FORE FLAP SKIN 10 INCHES FROM INBOARD END BETWEEN WS 211.69 AND WS 213.69 RT. MAINTENANCE CUTOUT DELAMINATED AREA OF UPPER FORE FLAP SKIN BETWEEN WS 211.69 AND WS 213.69 RT; FABRICATED REPAIR DOUBLERS; PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-10, FIG 33, PG 88 C, D, E. 2L72 4F RTA16WE 20040213001142004021300114NM 2004 2 13 AWXA200400152 120040104A5753 THRUST BEARING BOEING BOEING737 7373G7 1384595NM FLAP CARRIAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW P5801 24712 PHX - FLIGHT CONTROL - INFO ONLY (SEATTLE ACO) - DURING AD DRIVEN GAP CHECK OF FLAP CARRIAGE SPINDLES EXCESSIVE AXIAL MOVEMENT WAS DISCOVERED ON THE LT OUTBOARD FLAP OUTBOARD CARRIAGE THRUST BEARING. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FLAP NR 1 (WBL 254) & NR 2 (WBL 355) FLAP CARRIAGES IAW BMM 27-51-44, AND T/C R3M27013. PART NAME; FLAP CARRIAGE, OUTBOARD, LT, MFG; BOEING, P/N; 65-46481-105, S/N; 4053, TT; 2797, TC; 1595, LOC; WBL 254. 2L72 4F RTA16WE 20040213001172004021300117WP 2004 2 13 AALA20040182 120040204A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219677W 53627 EMERGENCY LIGHTS AT CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040213001182004021300118SO 2004 2 13 C2XA04SH046 120040205A531514522461011 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV - DURING C-CHECK THE RT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040217000332004021700033EU 2004 2 17 ASOA04035 120040115A33503011210 LIGHT AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 372 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040217000482004021700048NM 2004 2 17 GAIA04007OP 120040123A33501000679 LIGHT BOEING727 727223 1384074NM COCKPIT INOPERATIVE A GAIAK NONE O OTHER ININSP/MAINT 1 SW076806 19481 DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT DOOR EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040217000562004021700056SO 2004 2 17 SIMA200402001 120040119A272012009421251 ROD EMB 135 EMB135LR 3260305SO RUDDER INOPERATIVE A SIMAB EMER. DESCENT FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SW21734EK 145371 BGR - FLT 4649 - ON TAKEOFF RIGHT RUDDER WENT FULL FORWARD. EICAS MESSAGE RUDDER SYSTEM 1-2 INOPERATIVE. COULD NOT MOVE RUDDER IN EITHER DIRECTION. FOLLOWED AOM CHECKLIST. LANDED UNEVENTFULLY. FOUND RUDDDER CONTROL ROD NR 2 ROD BROKEN. REPLACED NR 1 AND NR 2 CONTROL RODS AND RUDDER NR 1 AND NR 2 OPERATIONAL CHECK AND FCF PASSED. A/C RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040217000662004021700066EA 2004 2 17 ASOA04042 120040117A29146619002 PUMP CNDAIRCL600 CL6002C10 1390015EA HYD SYSTEM INOPERATIVE A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO11712EV 10074 FLT 4836 - DURING CRUISE FROM OAK-SLC, THE CREW RECEIVED A HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE, INBOARD FLIGHT SPOILER CAUTION MESSAGE AND AN INBOARD SPOILERS CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND A FLAPS TWENTY DEGREE LANDING WAS PERFORMED. AN EMERGENCY WAS NOT DECLARED, HOWEVER, THE TRUCKS WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN SLC. MAINTENANCE REMOVED AND REPLACED THE ENGINE DRIVEN PUMP ON THE RIGHT ENGINE AND ALSO THE CASE DRAIN MANIFOLD FILTERS AS A PRECAUTIONARY MEASURE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217001122004021700112EU 2004 2 17 CX7A194J0401 120040104A26131734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE ACTIVATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03307CE 340B204 ABORTED TAKEOFF, FOR RIGHT TAIL PIPE HOT. 2L72 4T RTA52EU 20040217001172004021700117NM 2004 2 17 QXEA200400077 120040126A3010 DEICE SYSTEM BOMBDRDHC8 DHC8401 1390041NM RT WING MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09400QX 4030 ON APPROACH, DEICE PRESSURE CAUTION ILLUMINATED. NO TIME TO RUN CHECKLIST. ON GROUND FOUND THAT SECTION OF RT WING HALFWAY BETWEEN ENGINE AND TIP APPEARED NOT TO BE REMOVING ICE. C/W OPERATIONAL CHECK OF DEICE BOOTS. ALL INDICATIONS AND OPERATIONAL CHECK NORMAL. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040217001182004021700118NM 2004 2 17 QXEA200400096 120040129A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09347PH 480 EMERGENCY FLOOR TRACK LIGHT IS PROTRUDING ON THE RIGHT FRONT SIDE. REMOVED AND REPLACED BROKEN EMERGENCY LIGHT TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040217001262004021700126WP 2004 2 17 AALA20040119 120040125A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21298AA 49310 SAN) TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-27 FOR TAILCONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F A6WE 20040217001272004021700127NM 2004 2 17 AALA20040110 120040123A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21959AN 30828 ORD) EMERGENCY LIGHT AT RT AFT FUSELAGE FORWARD OF CREW EXIT INOPERATIVE. REPLACED BATTERY PACK FOR RT EMERGENCY LIGHT AT AFT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F RTA16WE 20040217001302004021700130CE 2004 2 17 KC82004F00000 120040112A29102407003466 LINE LEAR 25 25D 5170514CE GE CJ610 CJ6101 30006NE TAILCONE FAILED E KC8AO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL2375CK 18136 256 COMPLETE HYDRAULIC FAILURE OF THE NORMAL SYSTEM AFTER GEAR EXTENSION. AUXILIARY SYSTEM WORKED NORMALLY. FOUND HYDRAULIC LINE FROM LT ENGINE DRIVEN HYDRAULIC PUMP IN TAILCONE CHAFED THRU AND LEAKING. REPLACED LINE, SERVICED HYDRAULIC SYSTEM, AND PERFORMED LEAK CHECK IAW MFG MM. 2L72 4J4 J A10CE 1E16 20040217001442004021700144NE 2004 2 17 NACA20040008 220040124A7510 DUCT BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE CRACKED A NACAO OTHER J WARNING INDICATION DEDESCENT 1 AL03992AJ17 17 19428 649003 NR 3 ENGINE FIRE WARNING LIGHT ON APPROACH. RETARDED THROTTLE AND LIGHT WENT OUT. FOUND 13TH STAGE BLEED DUCT CRACKED IN HALF AT COWL ANTI-ICE VALVE. REPLACED DUCT. FOUND 8TH STAGE CHECK VALVE LEAKING, AND 8TH STAGE DUCT IN STUB WING LEAKING. REPLACED DUCTS AND CHECK VALVE. CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040217001462004021700146NM 2004 2 17 UPS04241778 120040112A5315 FLOORBEAM BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 INSPECTION TYPE: C, LIGHT SURFACE CORROSION AROUND SOME ANCHOR NUT ATTACH POINTS AT CABIN FLOOR STRUCTURE FROM BS1130 - BS 1183. CORROSION REMOVED IAW SRM 51-10-6. HFEC AREA NDF. AREA FLAP PEENED I AW SOPM 20-10-30. REPAIR CARRIED OUT IAW MFG INSTRUCTIONS SRV-SNN -04-00014H. 2L73 4F A3WE 20040217001472004021700147NM 2004 2 17 DHL2003752501 120040105A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01752DH 22466 DURING "C" CHECK, REPAIR AT BS 1130 BETWEEN STR 21 RT TO 24 RT DENTED AND ENDS ON STRINGER. REMOVED PREVIOUS REPAIR AND FOUND SKIN DENTED OUT OF LIMITS IAW SRM 53-30-1 FIG. 1.REMOVED RT AFT. SIDEWALL IN AFT. PIT FOR ACCESS IAW M.M. 25-52-02. CUT OUT DAMAGED AREA DIM. 1.6250 INCH X 1.6250 INCH AND FABBED FILLER FROM 2024 T3 .063 P.O.NR 900355 DIM. .5 INCH X .5 INCH AND DOUBLER FROM 2024 T3 .071 P.O.NR 900408 DIM. 11.5 INCH X 11 INCH IAW SRM 53-30-3 FIG. 3. PARTS TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED IAW SRM 53-30-3 FIG. 3. REINSTALLED LINER IAW M.M. 25-52-02. 2L73 4F A3WE 20040217001502004021700150EA 2004 2 17 SWIA200412823 120040129A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA OUT OF RIG A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07917SW 7641 FLAPS FAIL AT 20 DEGREES AFTER TAKE-OFF. RIGGED FLAPS IAW 27-54-00. OPS. CHECK GOOD. 2L72 4F RTA21EA 20040217001542004021700154EU 2004 2 17 CX7A194J0404 120040117A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03311CE 340B214 LT TAILPIPE HOT LIGHT ILLUMINATED AFTER POWER SELECTED ON. MOISTURE WAS PRESENT. RAN UP ENGINE AND LIGHT EXTINGUISHED. 2L72 4T RTA52EU 20040217001592004021700159NM 2004 2 17 AALA20040121 120040126A3397 WIRE HARNESS BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21191AN 32385 MIA EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED EMERGENCY LIGHT WIRE HARNESS ASSEMBLY AT SIDEWALL TO SEAT 20D ASSEMBLY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA2NM 20040217001652004021700165WP 2004 2 17 AALA20040126 120040125A213039271411 VALVE DOUG DC9 DC982 3022082WP ZONE 600 INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21403A 49314 DFW INFLIGHT T2427/25 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN INCREASING IN INTENSITY AT MAX POWER, EPR 1.95 PACKS ON AND APU OFF. RETURNED TO DFW. LANDED WITHOUT INCIDENT. FOUND PRESSURE REGULATOR VALVE ON RT PACK INOPERATIVE. REPLACED PRESSURE REGULATOR VALVE ON RT PACK AND PERFORMED ENGINE RUNS AT 1.95 EPR WITH APU OFF AND BOTH PACKS ON. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040218000152004021800015NM 2004 2 18 04FDEA00067 120040107A5311AFA7117501 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CABIN LEFT FRAME STA 1761 BETWEEN STR 12-13 DENTED. CABIN LT FRAME, STA 1761 BETWEEN STR 12-13 LT, CARRIED-OUT REPAIR AS PER SRM 53-30-00 FIG. 1 VOL. I AND COMPLIED WITH FEDEX EA 1-5330-74177 - FUSELAGE- FRAME REPAIR - DTR TRACKING - STATION 1761 2L73 4F RTA22WE 20040218000182004021800018SO 2004 2 18 GLBA20030529 120040110A2497 BUSS EMB 120 EMB120ER 3260203SO EMERGECNY SYSTEMFAILED A GLBAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 NM0371GL 120071 LOST EMERGENCY DC BUSS IN FLIGHT, REPLACED THE CB0348 WITH SERVICABLE IAW EMB120MM CH24-34. OPS CK GOOD 2L72 4T RTA31SO 20040218000192004021800019SO 2004 2 18 GLBA20030530 120040111A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM0371GL 5056 120071 FLAP ASSYMETRY CONTROL FAULT, R & R RT OB ACTUATOR PN 3203000-1007 OPS CK GOOD 2L72 4T RTA31SO 20040218000422004021800042NM 2004 2 18 04FDEA00336 120040206A5711ARB74054 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING, UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 506 TO XORS 538. RT WING, UPPER SURFACE IN SPAR AREA BETWEEN XORS 506 TO XORS 538 CORROSION REPAIRED AS PER SRM 51-21-01 VOL.II 2L73 4F RTA22WE 20040218000532004021800053NM 2004 2 18 04FDEA00191 120040120A5320AFA3159539 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25584FE 48436 MAIN DECK - INTERCOSTAL AT BODY STATIONS Y=515.00 THRU Y= 535.00 LONGERON 7 (LEFT HAND) FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218000562004021800056NM 2004 2 18 04FDEA00195 120040120A5320ADA83921 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y=775.00 THRU Y=791.75, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218000572004021800057NM 2004 2 18 04FDEA00196 120040120A5320AFA3159599 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y=808.00 THRU Y=824.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218000652004021800065NM 2004 2 18 04FDEA00201 120040121A5753ARC2950 TRACK DOUG MD11 MD11 3023602NM ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT INBOARD FLAP CENTER VANE TRACK CUTOUT FOUND GOUGES AT 4 PLACES. COMPLIED WITH FEDEX EA 1-5750-74283, WINGS - LEFT INBOARD FLAP VANE SUPPORT RIB CHAFED. 2L73 4F RTA22WE 20040218000662004021800066NM 2004 2 18 04FDEA00202 120040122A5320FX65207324 INTERCOSTAL BOEING727 727100 1384036NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25107FE 19202 AFT PIT BS 1080 TO 1050 AT STR 26R INTERCOSTAL DAMAGED AND HOLES ELONGATED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2. NEW INTERCOSTAL FABRICATED ON TRAVELER NR T4/398010. 2L73 4F RTA3WE 20040218000672004021800067NM 2004 2 18 04FDEA00387 120040209A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 FWD CABIN SEAT TRACK CORRODED FROM STA 459 TO 495 -X27.5. FWD CABIN SEAT TRACK CORRODED FROM STA 459 TO 495 -X27.5 CARRIED OUT SECTIONAL REPLACED FROM STA 450 TO 525 -X27.5 AS PER MD11 SRM 53-70-00 FIG1 V1, PERFORMED NDT INSPECTION ON TRIMMED AREA CRACK FREE CONDITION. 2L73 4F RTA22WE 20040218000682004021800068NM 2004 2 18 04FDEA00388 120040209A5311ACA7118 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CABIN G-NET YOKE ASSY ATTACHMENT AT LT SIDE STA 535 DENTED AT UPPER & LOWER LOCATION. CABIN G-NET YOKE ASSY ATTACHMENT AT LT SIDE STA 535 DENTED AT BOTH UPPER & LOWER LOCATION REPAIR CARRIED OUT AS PER DWG NR SRZ-53-503 & PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION . 2L73 4F RTA22WE 20040218000702004021800070NE 2004 2 18 04FDEA00304 220040203A7200PW44623 ENGINE DOUG MD11 MD11 3023602NM PWA 4060 PW4060 52119NE NR 2 MALFUNCTIONED A FDEAEFJAENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING MEJOVER TEMP VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO25620FE1343613436 48791 DURING CLIMBOUT IN VMC NR 2 ENG (LOUD NOISE) FROM TAIL AREA. NEXT HIGH EGT (RED) AND VIBRATION. REF QRH SHUT NR 2 ENG DOWN. LANDED RPLL. CREW DEBRIEF AT CLIMBOUT 19,000 FT ENCOUNTERED LOUD NOISE FROM TAIL AREA AND VIBRATION, PERFORMED WALK-AROUND INSPECTION ON TAIL AREA NO DAMAGED FOUND EXTERNALLY. ON EAD NR 2 ENG AMBER 662 DEG CELSIUS. MX UPON INSPECTION OF THE EXHAUST FOUND METAL IN THE TAILPIPE. POWERPLANT ENGINEER TREVOR STEDKE HAS APPROVED THIS ENGINE FOR CHANGE.. 2L73 4F4 FRTA22WE E24NE 20040218000722004021800072WP 2004 2 18 UPS04841818 120040205A2170 COALESCER BAG DOUG DC8 DC873F 302199FWP AIR CONDITIONINGDIRTY A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01814UP 46090 ODOR OF SMOKE IN COCKPIT. DURING DEPARTURE UNKNOWN ORIGIN MAYBE COMING FROM PACKS LT READ 80 DEGREES, RT READ 200 DEGREES ALL OTHER GAUGES READ NORMAL, T/S FOUND WATER SEPERATOR VERY DIRTY INDICATION WAS A PACK OVERHEAT RAN PACKS ON GROUND WITH NO ODOR OF SMOKE OR ANYTHING ELSE O.K. FOR CONTINUED SERVICE. 2L74 4F RT4A25 20040218000742004021800074CE 2004 2 18 DXTA200400234 120040129A329766187046 CIRCUIT BOARD CESSNA560 560XL 2076702CE MLG FAILED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07664QS 5605264 AFTER TAKEOFF AND GEAR HANDLE SELECTED TO THE UP POSITION THE UNLOCK LIGHT REMAINED ON, TRIED TO RECYCLE GEAR HANDLE BUT PROBLEM REMAINED THE SAME. REMOVED AND REPLACED L/G PC BOARD AND NOSE GEAR UP-LOCK SWITCH. PERFORMED UP-LOCK CHECK, SEQUENCE ACTUATOR RIGGING ADJUSTMENT AND NOSE LANDING GEAR ACTUATOR TEST. ALL WORK DONE IAW CESSNA CITATION MODEL 560XL MM CHAPTER 32-30-03 & 32-30-05. 2L72 4F RTA22CE 20040218000752004021800075NE 2004 2 18 DXTA200400232 220040128A7200304196001 ENGINE CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE RIGHT FLAMED OUT E DXTAO OTHER RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL07804QS1165 5600610 PCEDC0147 WHILE DESCENDING THROUGH FL 310 WITH THE RIGHT POWER LEVER AT FLIGHT IDLE, THE BOOST PUMP CAME ON AND OIL PRESSURE DROPPED TO ZERO, GENERATOR WENT OFF-LINE. THE RIGHT ENGINE FLAMED OUT, IT THEN AUTO RELIT AT FL 290. REMOVED AND REPLACED THE RT ENGINE IAW CESSNA 560 MM CHAPTER 71-01-05. PERFORMED ENGINE 5 POINT GROUND RUN, OPS AND LEAK CHECK GOOD 2L72 4F4 FRTA22CE E00053EN 20040218000832004021800083 2004 2 18 252TR0015 420040118A2210 RECEIVER BOEING737 737228 13844AGNM VOR/LOC SYS MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05252TR 23001 CHANNEL-A AUTOPILOT WILL NOT CAPTURE VOR-LOC. PLACED A-CHANNEL AUTOPILOT ON MEL 22-1. REPLACED NAV. RECEIVER AND PERFORMED AUTO-PILOT LRU VERIFICATIN BITE TEST PER MM 22-00. AUTO-PILOT CHECKS NORMAL. 2L72 4F RTA16WE 20040218000862004021800086NM 2004 2 18 2004UALA00022 120040109A5311 FRAME AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29815UA 867 FRAME 24 BENT BTWEEN STR 36L AND 37L. MAJOR REPAIR ACCOMPLISHED. REPAIR OF FRAME 24 WAS ACP'D PER EVA MOC1-8467C. 2L72 4F4 FRTA28NM E40NE 20040218000872004021800087NM 2004 2 18 2004UALA00028 120040109A3150S231T3001234 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE PARK BRAKE IND BURNED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29545UA 25323 ON ENGINE SHUTDOWN, ELECTRICAL ODOR IN COCKPIT. FOUND PARKING BRAKE ANNUNCIATOR BASE AND LENS ASSEMBLY FAILED. REPLACED LIGHT ASSEMBLY AND BASE L413. 2L72 4F4 FRTA2NM E17NE 20040218000882004021800088EU 2004 2 18 2004UALA00034 120040113A3220GA65920 LINK ASSY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG BENT A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29475UA 1495 FLIGHT DIVERTED DUE TO PROBLEM WITH THE LANDING GEAR. FOUND LINK ON PROXIMITY SENSOR ASSEMBLY BENT. STRAIGHTENED LINK AND PERFORMED OPERATIONAL CHECK OF GEAR RETRACTION. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040218000892004021800089 2004 2 18 2004UALA00035 420040109A3417 CONNECTOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ADC LOOSE A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29909UA 25009 RETURNED TO FIELD DUE TO AIRSPEED INDICATOR PROBLEM AND INOP ALTIMETER. FOUND PITOT STATIC QUICK DISCONNECT, LOOSE ON ADC. RESECURED LINE. ACCOMPLISHED AIR DATA COMPUTER SELF TEST AND AIR DATA SYSTEM OPS TEST. ALL CHECKS NORMAL. 2L72 4F4 FRTA16WE E2GL 20040218000912004021800091NM 2004 2 18 04FDEA00198 120040120A5320ADA3972505 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK INTERCOSTAL AT BODY STATIONS Y=840.25 THRU Y=859.00 LONGERON 30 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218000932004021800093 2004 2 18 QXEA200400054 420040121A3420 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 ILLUMINATED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09354PH 498 HSI HEADING MISMATCH ILLUMINATED DURING FLIGHT. ACCOMPLISHED CHECKLIST. PRESSED HDG/DG BUTTON TWICE, MESSAGE CLEARED. C/W MTC 9340019 STEPS OF AHRS SYSTEM SELF TEST. SYSTEM CHECKS GOOD, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040218000962004021800096NM 2004 2 18 04FDEA00205 120040123A5315BAC1518338 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM BS 460 LBL 10 WL 208. REMOVED CORROSION ON FLOOR BEAM BY REMOVING .030 FROM AN AREA OF 1X1 INCH. AREA IS OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGE AREA OF TOP FLANGE AND FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8 2L73 4F RTA3WE 20040218000982004021800098SO 2004 2 18 C2XA04SH025 120040124A532014529495003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714998 145302 SHV-DURING C-CHECK, THE LT LAVATORY FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040218000992004021800099NM 2004 2 18 04FDEA00228 120040127A2611774001 SMOKE DETECTOR BOEING727 727200 138407ENM NR 4 FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25242FE 21178 FIRE BELL, LIGHT AND NR 4 MAIN SMOKE SENSOR SHORTLY AFTER TAKEOFF. NO ODORS OR FUMES DETECTED. SHORTLY AFTERWARD BOTH DUCT OVERHEAT LIGHTS CAME ON. S/O HAD AIR MIX VALVE AT 12 O'CLOCK, NR 1 PACK ONLY, 100 DEG F OUTPUT INDICATED. FIRE INDICATION WENT OUT WITHIN 1 MIN. 2L73 4F RTA3WE 20040218001002004021800100EU 2004 2 18 DHL2004363001 120040125A4990 TUBE AIRBUS300 A300B4203 3930306EU APU OIL SYS FAILED A DHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01363DH 85 AFTER T/O, CLIMBING THRU 4500 FT MASTER WARNING PANEL (MWP) SMOKE LIGHT, AND FORWARD LEFT SMOKE DETECTOR LIGHTS ILLUMINATED. BEGAN IMMEDIATE RETURN TO JFK. AT INITIATION OF EMERGENCY CHECK LIST, SMOKE LIGHTS WENT OUT (APPROX 30 SECONDS) COMPLETED NORMAL APPROACH/LANDING. FOUND APU LOW ON OIL. FOUND NO EXTERNAL, OR INTERNAL LEAKS. SUSPECT OIL LIGHTLY INTO CABIN. OK IN COCKPIT. TRANSFERRED TO DMI 15524 PER MEL 49-11-01. RENDERING APU INOPERATIVE. RAN APU, FOUND PIPE AT MANIFOLD CRACKED - P/N: 977594-3. ORDERED ASSOCIATED PACKING AND TUBE. DMI 15524 REMAINS OPEN. REF. DMI 15524 AFTER T/O CLIMBING THRU 4500' LT SMOKE DETECTION LIGHTS ILLUMINATED. REPLACED OIL LUBE TUBE. OPS CHECKED GOOD IAW M/M 49-00-00.2L72 4F RTA35EU 20040218001012004021800101 2004 2 18 371PA0034 420040123A22104051600913 COMPUTER BOEING737 737306 13844BGNM FLT CONTROL MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05371PA 23543 AUTOPILOT DRIFTED OFF ALTITUDE IN CRUISE +320 FT, THEN RECAPTURED ASSIGNED ALTITUDE. PLACED AUTOPILOT ALTITUDE HOLD ON MEL 22-1. REPLACED "A" FLIGHT CONTROL COMPUTER PER MM 34-60. PERFORMED FCC TEST AND LAND VERIFY. TEST NORMAL. 2L72 4F RTA16NE 20040218001042004021800104NM 2004 2 18 04FDEA00232 120040128A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208. REPAIR CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208 PER SRM 53-10-8 2L73 4F RTA3WE 20040218001052004021800105NM 2004 2 18 QXEA200400067 120040126A3260858601 PROXIMITY SENSOR DHAV DHC8 DHC8202 2809007NM ZONE 100 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09375PH1000410004 529 CREW REPORTED THE LT GEAR DOOR LIGHT AND LANDING GEAR INOP CAUTION CAME ON IN FLIGHT. THE FLIGHT ATTENDANT CONFIRMED THE LT SIDE GEAR DOORS WERE OPEN. THE CREW FOLLOWED THE CHECKLIST AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND CODE 53 ON THE PSEU. THE PSEU WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040218001062004021800106NM 2004 2 18 04FDEA00240 120040128A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM BS 1110, RBL 22, WL 208. CUT OUT CORRODED SECTION OF FLOORBEAM'S TOP CHORD BS 1110 WL 208 RBL 8-23 AND INSTALLED REPAIR ANGLES, TEE CHORD AND STRAPS PER SRM 53-10-8. 2L73 4F RTA3WE 20040218001082004021800108NM 2004 2 18 04FDEA00246 120040129A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM BS 380 LBL 8-55 WL 208. BLENDED CORROSION ON BS 380 FLOORBEAM PER SRM 51-10-1. FOUND LBL 8 OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED REPAIR PARTS PER SRM 53-10-8. APPLIED ALODINE AND PRIMER TO CUT OUT AND REPAIR PARTS PER FED EX MM 51-20-021-7 & 51-20-151-7. INSTALLED REPAIR PER SRM 53-10-8. INSTALLED STIFFENER AT LBL 14 PER SRM 51-30-2. APPLIED ALODINE & PRIMER. IN LIMITS. BLEND AREA PER FED EX MM 51-20-021-7 & 51-20-151-7. 2L73 4F RTA3WE 20040218001092004021800109NM 2004 2 18 04FDEA00245 120040129A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CORROSION FWD CARGO BAY BS 685 STR 26R WL 145 ON STRINGER. LOCATED CORROSION FWD CARGO BAY BS 685 STR 26R WL 145 BLENDED CORRODED AREA (STR 26 RT) 4 INCHES LONG, BLEND OUT WAS OUT OF LIMITS. REPAIRED DAMAGED AREA, ALODINED & PRIMED IAW SRM 51-30-2, 51-30-1, 51-10-1, 51-40-3, 51-10-3, 51-30-8, 51-10-2. 2L73 4F RTA3WE 20040218001102004021800110NM 2004 2 18 04FDEA00243 120040126A5347S49291477075T65 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RT STA 795 SEAT TRACK REF. X = 27.5 SEAT TRACK DAMAGED IN TWO PLACES. MAIN CARGO DECK RT STA 795 SEAT TRACK REF = X =27.5 DAMAGED SEAT TRACK CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1. 2L73 4F RTA22WE 20040218001142004021800114NM 2004 2 18 SPAA0400069 120040127A33501000679 LIGHT BOEING737 7372Y5 1384554NM COCKPIT INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 ON PREFLIGHT FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECK GOOD. 2L72 4U RTA16WE 20040218001152004021800115WP 2004 2 18 04FDEA00251 120040130A5744ARC105202 MOUNT DOUG DC10 DC1030 3023501WP AILERON HINGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25313FE40741 48311 DURING C-CHECK AT LAX, THE RT OUTBOARD AILERON HINGE 5 MOUNT ASSY P/N ARC1052-02 WAS FOUND WITH THE LUGS CORRODED USED TO ATTACH THE SIDE LOAD STRUT. AFTER CORROSION REMOVAL, THE LUG BORE SIZES WERE INCREASED TO 0.450 INCH. THE ORIGINAL BORE SIZES ARE 0.4057/0.4067. NO REPAIR LIMITS EXIST IN CMM 57-51-02. THIS EA PROVIDES A BOEING APPROVED BUSHING REPAIR EA NR 8-5710-72676, RELEASE DATE: 01/29/2004. REPAIRED 2EA. CORRODED SIDE LOAD STRUT MOUNT LUGS PER EA 8-5710-72676 ON RT OUTBOARD AILERON HINGE 5 MOUNT HOLE. REINSTALLED BRACKET AND TORQUED BOLTS PER M/M 20-50-02-2. 2L73 4F A22WE 20040218001162004021800116EU 2004 2 18 AWXA200400126 120040130A5610NP1653117 WINDSHIELD AIRBUS320 A320232 3930326EU COCKPIT FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28661AW12927 1284 DURING CRUSIE THE CAPTAINS WINDSHEILDS OUTERPANE SHATTERED AT FL260. CABIN PRESSURE WAS MAINTAINED AT 5.0 PSO OR LESS AND DESCENT TO FL 230 ACCOMPLISHED. THE RETURN TO LAS WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE CAPTIANS WINDSHEILD PER AMM 56-11-11-401. MAINTENANCE PRESSURIZED THE AIRCRAFT PER AWA TASKCARD F1B21307. NO LEAKAGE NOTED. OK FOR SERVICE. MAINTENANCE ALSO REMOVED AND REPLACED THE WINDOW HEAT CONTROLLER FOR PRECAUTIONARY REASONS PER AMM 30-42-34-401 & 30-42-00-710-001. 2L72 4F RTA28NM 20040218001182004021800118EU 2004 2 18 04FDEA00284 120040202A5270A5397802220051 TARGET AIRBUS300 A300F4605R 3930327EU ZONE 800 WORN A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25655FE 742 PASSING 1500 FT ON DEPARTURE. AFT CARGO DOOR WARNING PRESENTED ON ECAM. NO PRESSURIZATION ABNORMALITY NOTED. RAN ECAM/QRH PROCEDURE. RETURNED TO JFK. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 11FEB04 MEL 52-71-01: AFT CARGO DOOR CLOSED & LOCKED, FOUND DOOR SWITCH (SE32WS) STOP TARGET WORN AND GOUGED. P/N A5397802220051, NIS AT EWR. PART ON ORDER. OPERATED AFT CARGO DOOR I.A.W. A300 M.M. 52-71-00-5 AFT CARGO DOOR INDICATIONS CHECK NORMAL AT THIS TIME. 2L72 4F RTA35EU 20040218001212004021800121EA 2004 2 18 QXEA200400101 120040202A2910MM67075294005 TUBE CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CHAFED A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM09609QX5064 10031 ON APPROACH, THE AIRCRAFT EXPERIENCED A FAILURE OF THE NR 2 HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 ENGINE DRIVEN PUMP HYDRAULIC LINE CHAFED THROUGH. A NEW FLEX LINE HAS TEMPORARILY BEEN INSTALLED AT THE CHAFED AREA, AND LEAK CHECKS WERE PERFORMED. NO LEAKS WERE NOTED. PERMANENT REPAIR TO BE COMPLETED WITHIN 450 HOURS. AIRCRAFT RETURNED TO SERVICE. -CLOSED- 2L72 4F RTA21EA 20040218001222004021800122NM 2004 2 18 04FDEA00305 120040203A2612774001 FIRE DETECTOR BOEING727 727200 138407ENM NR 4 CARGO BAY FALSE ACTIVATIONA FDEABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25236FE 21330 DURING CLIMBOUT FROM ONT A/C HAD FIRE WARNING WITH CORRESPONDING NR 4 MAIN CARGO LIGHT ILLUMINATED. PERFORMED QRH & RETURNED TO ONT. SMOKE LIGHT REMAINED ON UNTIL PULLING INTO THE ONT RAMP. VISUAL INSPECTION AFTER LANDING REVEALED NO INDICATION OF FIRE OR SMOKE. 2L73 4F RTA3WE 20040218001242004021800124NM 2004 2 18 DHL2004783001 120040205A2121 COOLING FAN BOEING727 727227 1384078NM CABIN COOLING BURNED OUT A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01783DH 21999 WITH APU ON AIRCRAFT PACKS ON LIGHTS FLICKERED BURNING ODOR NOTED INSIDE AND OUTSIDE THE AIRCRAFT. APU TEMPERATURE FLUCTUATING BETWEEN 200 & 500 DEGREES. DEFERRED LEFT HAND PACK COOLING FAN PER B-727 MEL 21-5-4 CAT-C. PLACARD INSTALLED. COMPLIED WITH SPECIAL PROCEDURE 21-5 DMI 15640. LT PACK COOLING FAN INOPERATIVE. REPLACED LT HAND PACK COOLING FAN PER M/M 21-56-91, OPS CHECKED GOOD. THIS CLEARS DMI 15640. 2L73 4F A3WE 20040218001252004021800125NM 2004 2 18 04FDEA00311 120040204A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25204FE 22926 ON DEPARTURE, AMBER AFT AIRSTAIR LIGHT ON F/E'S DOOR ANNUNCIATOR PANEL ILLUMINATED. COMPLIED WITH QRH. RETURN TO GTF. 2L73 4F RTA3WE 20040218001272004021800127NM 2004 2 18 04FDEA00331 120040206A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM AT FLOOR PANEL FASTENER HOLES BS 400 LBL 10 - RBL 10. REMOVED CORROSION IN A 1.0 X2.0 X .038 AREA. ORIG THICKNESS IS .125, TOP CHORD IS OUT OF LIMITS PER SRM 53-10-1. CUT-OUT DAMAGED UPPER CHORD PER SRM 53-10-8. FABRICATED CHORD FROM BAC1505-100617 M536763, ANGLE FROM BAC1490-2785, M 526583 AND BAC1490-2831 M537615 AND STRAP FROM BAC1512-3396 M531513 AND BAC1512-3353 PER SRM 53-10-8. LOCATED, DRILLED, ALODINED, PRIMED, PAINTED, AND INSTALLED ALL PARTS PER SRM 53-10-8. 2L73 4F RTA3WE 20040218001302004021800130NM 2004 2 18 04FDEA00361 120040208A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT O/B FLAP I/B HINGE I/B PIVOT HOLE AND LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORRODED. LT O/B FLAP I/B HINGE I/B PIVOT HOLE & LUG CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LH O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040218001312004021800131NM 2004 2 18 04FDEA00360 120040208A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT O/B FLAP I/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP I/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75244 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP I/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040218001322004021800132NM 2004 2 18 04FDEA00359 120040208A5753 TRACK DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B FITTING AND SKIN. LT I/B FLAP CTR VANE TRACK CUTOUT HAS CHAFE MARK ON I/B & O/B - CHAFE MARK AT I/B & O/B SKIN EDGE TRIMMED 0.080 AS PER SRM 51-21-01 VOL 2 WITHIN LIMIT AS PER SRM 57-00-01 FIG 1A VOL 1 & CHAFE MARK AT FITTING EDGE REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-74313 WING - LH LE I/B FLAP VANE SUPPORT - RIB CHAFFED, HFEC CARRIED OUT AT REWORKED AREA & FOUND NO CRACK EVIDENT. 2L73 4F RTA22WE 20040218001412004021800141SO 2004 2 18 C2XA04IA008 120040119A3260 CONNECTOR EMB 145 EMB145LR 3260212SO UPLOCK BOX LOOSE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW271395512852 251 145075 PILOT REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ELECTRICAL CONNECTIONS TO BE LOOSE ON THE LT MAIN GEAR UPLOCK BOX. THE AFFECTED CONNECTORS WERE CLEANED AND RECONNECTED, THE LANDING GEAR SYSTEM OPERATIONALLY TESTED, AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040218001422004021800142NM 2004 2 18 DHL2004745010 120040129A2612 FIRE LOOP BOEING727 727224 1384076NM NR 3 SHORTED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. NR 3 DETECTOR CIRCUIT GROUND LIGHT DEFERRED IAW MEL 26-9-1. CONTROL NR 15570. CAT. (C). ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND ENGINE NR 3 FIRE LOOP IN CONTACT WITH NR 3 GENERATOR WIRES. INSPECTED WIRES FOR CHAFFING, NONE FOUND. RAN NR 3 ENGINE PER JRH, OPS CHECKED NORMAL. THIS CLEARS DMI 15570. 2L73 4F A3WE 20040218001432004021800143CE 2004 2 18 GLBA20030546 120040130A561010138402522 WINDSHIELD BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA COCKPIT CRACKED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03153GL2224 UE153 FO'S WINDSHIELD CRACKED, R & R WINDSHIELD RT PN 129-5025-2 2L72 4T3 TRTA24CE E2NE 20040218001442004021800144CE 2004 2 18 GLBA20030547 120040131A2731 CONTROL CABLE BEECH 1900 1900D 1154162CE ELEVATOR TRIM INOPERATIVE A GLBAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM03169GL UE169 EMERGENCY LANDING FOR LOSS OF ELEV TRIM CONTROL, R & R FWD ELEV TRIM TAB CABLE PN 114-524037-25. 2L72 4T RTA24CE 20040217000122004021700012CE 2004 2 17 2004F00062 120040120A76031013890355 CONTROL CABLE BEECH 300 300BEECH 1152930CE NR 1 ENGINE SEIZED A RU3AE ENGINE SHUTDOWN O OTHER DEDESCENT 1 SW2167 FF2 IN AN ATTEMPT TO REDUCE POWER FOR DESCENT, NR 1 ENGINE POWER LEVER LOCKED UP AT CRUISE POWER. DESCENDING THROUGH 8000 FEET, ENGINE WAS SECURED AND AIRCRAFT LANDED SAFELY. REPLACED POWER CONTROL CABLE ASSEMBLY. (M) 2L72 4T A24CE 20040217000292004021700029EA 2004 2 17 ASOA04047 120040118A213332156222 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11860AS 7433 FLT 4749 - DURING DESCENT FROM SRQ-ATL, A STRONG BURNING ODOR OCCURRED FOR APPROXIMATELY ONE MINUTE WHEN THE POWER WAS BROUGHT FROM IDLE TO CRUISE WITH THE ENGINE BLEEDS ON. THE ODOR DID NOT OCCUR WHEN THE BLEEDS WERE SELECTED TO THE AUXILIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING SHUTOFF VALVE ON THE TENTH STAGE BLEED AIR SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040217000472004021700047 2004 2 17 GAIA04006OP 420040122A2200 AUTOPILOT SYS BOEING727 727251 138408HNM COCKPIT INTERMITTENT A GAIAO OTHER O OTHER CRCRUISE 1 SW07278US 21157 FLT 874 - LAX-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE AUTOPILOT HEADING SELECT INTERMITTENT. (M) 2L73 4F A3WE 20040217000692004021700069EU 2004 2 17 ASOA04045 120040118A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING HANGAR MAINTENANCE IN MCN, THE RIGHT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY AT 73WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040217000832004021700083EU 2004 2 17 YENA200406 120040130A261110261640004 SMOKE DETECTOR AIRBUS320 A320232 3930326EU E/E BAY MALFUNCTIONED A YENAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA15564JB2778 2020 AT 370 FT HAD (AFT AVIONICS COMPARTMENT) SMOKE ALARM GO OFF. NO ODOR OR INDICATION OF SMOKE. FLIGHT ATTENDANT SAID TV'S SHUT OFF. PUSHED (RACK POWER) SWITCH TO OFF. LOOKED IN QRH AND FCOM. AIR INC PHONE PATCH DISPATCH/MAINT. ADVISED TO RETURN TO MCO. AT NO TIME SMELLED SMOKE OR ACRID ODOR. UPON T/S FOUND LARGE AMOUNT OF DUST UNDER MRM 1 AND 2. SUSPECT THIS TO BE CAUSE OF (SMOKE) WARNING AND SHUTDOWN OF LIVE TV RACK. CLEANED MRM AREA IN AFT RACK. REMOVED AND REPLACED SMOKE DETECTOR SENSOR IAW JB MCC REQUEST. OPS GOOD IAW LTV AMM 23-39-00. IAW JB MCC REQUEST REPLACED SMOKE CONTROL PANEL AND MRM NR 1 AS A PRECAUTION. 2L72 4F RTA28NM 20040217001042004021700104SO 2004 2 17 C2XA04BT016 120040131A335066364 LIGHT EMB 145 EMB145XR 3260214SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 EWR---CO2205, CREW REPORTED, (EMERGENCY LIGHTING STRIP BY MAIN CABIN DOOR MISSING AND GALLEY STRIP IS BROKEN). MAINTENANCE REPLACED MISSING EMERGENCY LIGHT FLOOR STRIP AND BROKEN EMERGENCY LIGHT FLOOR STRIP. IAW EMB145 MM NR 33-50-12, OPS. CHECKED EMERGENCY LIGHTING GOOD. 2L72 4F RT 20040217001152004021700115NM 2004 2 17 04FDEA00297 120040203A2752 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING, FOUND OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE INBOARD (1) CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP / INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040217001322004021700132WP 2004 2 17 MEX2004041 120040201A321349724761 BUNGEE CYLINDER DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE NLG DAMAGED W ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23214AM 49585 CAPTAIN REPORTED THAT THE NLG RED LIGHT TURNE ON AND OFF SEVERAL TIMES DURING CLIMB, CRUISE AND DESCENT. AT PLATFORM IT AWS PERFORMED A BITE TO THE PROXIMITY SWITCH UNIT IAW MM. TEST, OK, AFTER CAPTAIN REPORTED THAT DURING CLIMB, A LOUD NOISE WAS HEARD IN THE NLG DURNG ITS RETRACTION. THE AIRCRAFT WAS CARRIED TO HANGAR TO ATTEND THE REPORT. NLG PROXIMITY SENSORS AND BUNGEE SPRINGS WERE REPLACED AND SYSTEM TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040217001362004021700136EA 2004 2 17 COMA0460033 120040103A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01924CA 7026 REPAIR WING PLANK CRACK AT WS 148.019 LT SIDE. REPAIRED LT HAND LOWER WING PLANK AT WS148.019 IAW EO 601R-57-21-130. 2L72 4F RTA21EA 20040217001482004021700148NM 2004 2 17 P5CA0401027 120040113A2510811369 SEAT BOEING747 747249F 1384849NM COCKPIT FAILED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23920FT 22237 CAPTAIN`S CHAIR WILL NOT LOCK IN POSITION, FOUND ON PUSH BACK. INSPECTED SEAT, ATTEMPTED TO ADJUST SAME - NO HELP. REMOVED CAPTAINS SEAT. OPS CK SAT OK FOR SRVC IAW MM 25-11-01. 2L74 4F A20WE 20040217001532004021700153EU 2004 2 17 028741 120040116A6123 AUTOCOARSEN SYS SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE INOPERATIVE A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL17150CN 150 434 DRG49983 ON 01-16-2004, APPROX. 1125 (UTC), FLT 4520 CMH-PIT. CREW ABORTED TAKEOFF WHEN THE AUTOCOARSEN SYSTEM DID NOT ARM. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040217001582004021700158NM 2004 2 17 AALA20040111 120040123A3350 BALLAST BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21959AN 30828 ORD EMERGENCY EXIT LIGHT AT AFT LT SIDEWALL INOPERATIVE. REPLACED BALLAST FOR EMERGENCY EXIT LIGHT AT AFT LT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA16WE 20040217001612004021700161EU 2004 2 17 AALA20040108 120040122A21216451101 BEARING FOKKERF28 F28MK0100 4990807EU RECIRC FAN DAMAGED A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW211453D 11465 ORD INFLIGHT T557/22 LIGHT SMOKE AND FUMES IN AIRCRAFT AT FL280. IAW CHECKLIST RECIRCULATION FANS WERE TURNED OFF. SMOKE AND FUMES DISSIPATED. INSPECTED FANS AND FOUND NOISY BEARING IN FAN ALONG WITH ODOR. REPLACED RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RT 20040217001622004021700162NM 2004 2 17 AALA20040129 120040120A5315141T5114 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21393AN 29430 AFW FLOORBEAM AT STATION BS 347 RBL 43 HAD .90 INCH BY .90 INCH, .045 INCH DEPTH CORROSION BLENDED BEYOND SRM LIMITS. REMOVE CORROSION. APPLY CORROSION PREVENTATIVE COMPOUND TO BARE ALUMINUM SURFACE OF REPAIR AREA. FABRICATE REPAIR STRAP FROM .050 INCH THINK 301 1/2 HARD STAINLESS STEEL. APPLY TWO COATS BMS10-11 PRIMER TO REPAIR STRAP AND TO REPAIR AREA OF FLOORBEAM. FILL BLENDED AREAS ON UPPER SURFACE OF FLOORBEAM WITH BMS5-92 OR BMS5-95 COMPOUND. INSTALL REPAIR STRAP WET WITH BMS5-95 SEALENT. INSTALL REPAIR STRAP USING BACR3ONWG OR EQUIVALENT. 2L72 4F RTA1NM 20040217001642004021700164WP 2004 2 17 AALA20040125 120040125A3213 STRUT DOUG DC9 DC982 3022082WP NLG DEFLATED A AALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW21495AA 49733 MIA INFLIGHT T2070/25 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. RETURNED TO MIA. LANDED WITHOUT INCIDENT. INSPECTED NOSE GEAR FOR LEAKS AND DEFECTS. AIRCRAFT OUT OF SERVICE TO PERFORM NOSE GEAR CHECK. NOTED NOSE GEAR STRUT DEFLATED TO BOTTOM. ACCOMPLISHED NOSE GEAR STRUT SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F A6WE 20040218000172004021800017NM 2004 2 18 AWXA200400021 120040107A21216062691 BEARING BOEING737 737277 1384570NM CABIN FAN SEIZED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP28184AW 38314 22651 AFTER LANDING & TAXING TO HOLD BAY, SHORTLY AFTER NR 2 ENG SHUTDOWN COCKPIT BEGAN TO DEVELOP AN ACRID ELEC BURNING ODOR FOLLOWED BY LIGHT BLUE SMOKEY HAZE. TURNED OFF GASPER FAN & WINDOW HEAT, ODOR SUBSIDED. MAINT TROUBLESHOT, FOUND FLT DECK CABIN AIR COND FAN EMITTING ELEC BURNING ODOR WHEN 1 AIR COND PACK IS TURNED OFF, PLACED ON MEL 21-30, COND. 2 "CONTROL CABIN AUGMENTATION FAN INOP. WIND MILLING MAX OAT 46 DEG. C". FAN CB PULLED AND COLLARED. FAN SCHEDULED FOR REPLACEMENT 01/08/2004. MAINT REPLACED FLT DECK CABIN AIR COND FAN IAW BMM. OPS CHECK GOOD. INSPECT OF AIR COND FAN CONFIRMED FAILURE. TEARDOWN FOUND BEARING SEIZED & END BELL DAMAGED. R & R 2 BEARINGS & END BELL, UNIT FUNCTIONAL TESTED IAW CMM. 2L72 4F RTA16WE 20040218000242004021800024NM 2004 2 18 04FDEA00143 120040113A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), LOWER INBOARD ATTACH HOLE (SPAR MOUNTED) CORRODED AT SPOT FACES. RT OUTBD FLAP INBD HINGE (WING MOUNTED), LOWER INBD ATTACH HOLE SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20040218000482004021800048NM 2004 2 18 DHL2004763004 120040123A2612 FIRE DETECTOR BOEING727 727264 138408MNM CARGO BAY MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01763AT 22983 LOWER CARGO FIRE DETECTION FAULT INDICATOR LIGHT ILLUMINATED SHORTLY AFTER DEPARTURE. PERFORMED ASSOCIATED ABNORMAL PROCEDURES. REFERENCE PREVIOUS WRITE UP ON LOG PAGE 367250. TRANSFERRED TO DMI 15487 PER MEL 26-19-4. REF DMI 15487 LOWER CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED AFTER DEPARTURE. COMPLIED WITH S/P 26-19-4 IAW MEL/CDL M/M DMI 15487 REMAINS IN EFFECT. REF. DMI 15487 LOWER CARGO FIRE DETECTION FAULT LIGHT ILLUMINATED AFTER DEPARTURE. PERFORMED TEST AFTER CLEANING MODULE IN E&E. OPS NORMAL PER M/M 26-00. THIS CLEARS DMI 15487. PLACARD REMOVED. 2L73 4F A3WE 20040218000542004021800054NM 2004 2 18 04FDEA00192 120040120A5320AFA3159537 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25584FE 48436 MAIN DECK, INTERCOSTAL AT BODY STATIONS Y= 595.00 THRU Y= 615.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218000602004021800060NM 2004 2 18 04FDEA00212 120040123A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CORROSION (C53-113-01, 2) AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950F BETWEEN STR 29 LT AND 30 LT. CORROSION ON FRAME SHEAR TIE AT BS 950F BETWEEN STR 29 AND 30L IS OUT OF LIMITS PER SRM 51-10-1. FABRICATED A NEW SHEAR TIE AND REPLACED IT PER SRM 51-30-5, SRM 51-30-6, SRM 53-10-4 AND SRM 51-30-2. 2L73 4F RTA3WE 20040218000622004021800062NM 2004 2 18 04FDEA00209 120040123A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 AFT CARGO BAY, FRAME CRACKED AT FASTENER HOLE BS 1050 RBL 20 WL 149 (FLOOR TO SIDEWALL SUPPORT ATTACH FASTENER HOLE). REPAIRED AFT CARGO BAY FRAME AT BS 1050, RBL 20, WL 149 IAW FED EX E.A. 7-5310-55217. 2L73 4F RTA3WE 20040218000692004021800069EU 2004 2 18 04FDEA00390 120040210A7830 THRUST REVERSER AIRBUS310 A310 EU NR 2 ENGINE OUT OF RIG A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25418FE 343 ON TAKEOFF ROLL, JUST AFTER TOGA AND BEFORE STANDARD PWR WAS SET NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON LEFT ECAM SCREEN. ABORTED T/O COMPLIED WITH QRH, RETURNED TO GATE. MAINTENANCE PROCEDURE PERFORMED IAW MEL 78-30-01-C. MANUALLY CLOSED PRSV AND DISCONNECTED BOTH SIDES MASTER ACTUATORS. THRUST REVERSER RIGGED AND RE-ACTIVATED IAW MM 71-13-03 FEDEX W/O 25086 2L72 4F RTA35EU 20040218000712004021800071NE 2004 2 18 UPS04841817 220040204A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 FLAMED OUT A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO01880UP 46080 NR 1 ENGINE FLAMED OUT AT TOP OF DESCENT WHEN POWER REDUCED. ENGINE READINGS WERE NORMAL W/ WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL 200 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GEN. INSP CK FLT IDLE, SPECIFIC GRAVITY SETTING. MAGNETIC CHIP DETECTORS & FUEL FILTER. NO DEFECTS. CLEANED PAINT & PAINT STRIPPER OFF CDP TUBE DRAIN HOLES. RAN ENGINE TO MAX PWR . OPS WERE NORMAL 2L74 4F4 FRT4A25 E2GL 20040218000732004021800073SO 2004 2 18 C2XA04BT013 120040127A2560P2070011100 FLASHLIGHT EMB 145 EMB145XR 3260214SO COCKPIT OVERHEATED A C2XAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2718102 145643 CREW REPORTED, STRONG ODOR OF SMOKE ON TAKEOFF NOT LIKE DEICING FLUID. MAINTENANCE FOUND CAPTAINS COCKPIT FLASHLIGHT TO HAVE BURNING ODOR. REMOVED AND REPLACED THE CAPTAINS COCKPIT FLASHLIGHT ASSEMBLY IAW EMB145 33-50-16, OPS CHECKED GOOD. PERFORMED ENGINE RUNS AT VARIOUS POWER SETTINGS, NO SMOKE OR ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20040218000762004021800076CE 2004 2 18 DXTA200400237 120040204A3150 WARNING LIGHT CESSNA750 750 2076810CE NR 2 ENGINE ILLUMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07907QS 7500201 ON TAKEOFF ROLL MASTER WARNING LIGHT AND AUDIO INDICATIONS APPEARED WITH NO OTHER CAS INDICATIONS. WARNINGS WENT OFF AFTER 1 CYCLE THEN REAPPEARED WITH NR 2 ENGINE ITT EXCEEDANCE. ITT EXCEEDANCE INDICATION LASTED 2 SECONDS. DOWNLOADED ALLISON TRENDS AND EICAS MESSAGE FOR REVIEW, NO ITT EXCURSION NOTED. ACCOMPLISHED SPEED CONTROL SYSTEM ADJUSTMENT/ TEST PER CESSNA 750 MAINTENANCE MANUAL CHAP 27-60-00, NO DEFECTS NOTED. ACCOMPLISHED GROUND ENGINE RUN PER CESSNA 750 MAINTENANCE MANUAL CHAP 71-00-04, ALL SYSTEMS CHECKED GOOD. 2L72 4J RTT00007WI 20040218000772004021800077EU 2004 2 18 YENA200401 120040116A5220L32A319160001 CONTROL CABLE AIRBUS320 A320232 3930326EU EMERGENCY EXIT BINDING A YENAK NONE L NO TEST ININSP/MAINT 1 EA15552JB4634 1862 LEFT EMERGENCY EXIT HATCH CABLE WILL NOT RETRACT AFTER BEING PULLED DURING AN OPERATIONAL TEST. REPLACED CONTROL CABLE ASSY PER AMM 25-62-43-401. 2L72 4F RTA28NM 20040218000782004021800078NM 2004 2 18 04FDEA00207 120040123A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CORROSION IN AFT CARGO BAY, CORROSION ON FRAME SHEAR TIE BS 950D BETWEEN STRINGER 29 LT AND 28 LT. REMOVED CORROSION ON SHEAR TIE AT BS 900D BETWEEN STR 29L AND 28L. FABRICATED SHEAR TIE. ALODINE, PRIMED AND INSTALLED SHEAR TIE AT BS 350D BETWEEN STR 29L AND 28L IAW SRM 53-10-4. 2L73 4F RTA3WE 20040218000812004021800081NM 2004 2 18 UPS04441740 120040104A5313 STRINGER BOEING747 747123F NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, MAIN DECK - BS 555 RT STR 26 STR WEB I/B FLANGE FOUND CRACKED AS MARKED. MAIN DECK - BS 555 RIGHT STR 26 STR WEB I/B FLANGE REPAIRED AS PER SRM 51-40-03 FIG 3. 2L74 4F A20WE 20040218000902004021800090NM 2004 2 18 04FDEA00197 120040120A5320ADA8392501 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25584FE 48436 MAIN DECK INTERCOSTAL AT BODY STATIONS Y=840.25 THRU Y=859.00, LONGERON 7 LT FOUND NOT INSTALLED. COMPLIED WITH FEDEX EA 1-5310-75232 - FUSELAGE - MAINFRAME - INTERCOASTAL INSTL. / PASS. TO FREIGHTER CONV. CONFIG. (SP11530060) / DISCREPANCIES 2L73 4F RTA22WE 20040218001032004021800103NM 2004 2 18 04FDEA00233 120040128A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 RT EXTERIOR FUSELAGE SKIN HAS CREASE AT BS 1143 STR 18R TO 3 INCHES BELOW STR 19R. DAMAGE ON EXTERNAL SKIN BS 1143 STR 18R TO 3" BELOW STR 19R A/Y RATION=76 AREA FOUND TO BE WITHIN LIMITS PER SRM 53-30-1 FIG 1 EXCEPT AT STR 19R. FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 FIG 1. CUT OUT DAMAGE AT BS 1145 STR 19R IN A 1.1 X 1.3 AREA. FABRICATED REPAIR DOUBLER FROM 2024T3 X 0.063 INCH 523505 AND INSTALLED REPAIR AT BS 1143 STR 19R PER SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20040218001112004021800111WP 2004 2 18 ARWA20040105 120040130A5524 ATTACH FITTING DOUG DC8 DC862 3021970WP ELEVATOR LOOSE A ARWAK NONE O OTHER ININSP/MAINT 1 SO198974U 46110 DURING PREFLIGHT FOUND ELEVATOR STARBOARD SIDE UP SLIGHTLY AND PORT SIDE SLIGHTLY DOWN, SLIGHT DIFFERENCE IN TRAVEL BETWEEN PORT AND STARBOARD SIDE ELEVATORS. FOUND LOOSE ATTACHMENT AT PORT SIDE ELEVATOR ATTACHMENT TO TORQUE TUBE. PERFORMED ELEVATOR INSPECTION / CHECK IAW MM 27-30-1, FOUND NORMAL; ALSO PERFORMED INSPECTION / CHECK AT BOTH ELEVATOR CHAMBERS IAW MM 27-30-5, FOUND NORMAL; NO LEAKS NOTED. REPLACED BOLTS AT LT INBOARD ELEVATOR HINGE AND INSPECTED AREA; NO OTHER DEFECTS NOTED; TORQUED IAW MM 27-30-1 PAGE 405. OPERATIONAL CHECK FOUND NORMAL IAW MM 27-30-1. 2L74 4F 4A25 20040218001332004021800133NM 2004 2 18 04FDEA00379 120040207A2612 WARNING HORN BOEING727 727200 138407ENM CARGO SMOKE FALSE ACTIVATIONA FDEAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SO25270FE 22035 LOWER CARGO SMOKE WARNING BELL ACTIVATED TWICE AT ALTITUDE FOR 1-2 SECONDS. WARNING LIGHTS AND HORN WENT OUT IMMEDIATELY WITHOUT ACTIVATING THE DISCHARGE BUTTON. BEGAN IMMEDIATE DESCENT INTO YMX. WARNING CAME ON CONTINUOUS AT 500 FT, PUSH BOTTLE DISCHARGE BUTTON. WARNING CAME ON AGAIN ON ROLLOUT. PUSHED BOTTLE 2 DISCHARGE BUTTON 1 SYSTEM TEST INDICATES NORMAL TEST WITH THE FORWARD FAULT LIGHT ILLUMINATED ON THE CARGO SMOKE PANEL. LIGHT AND HORN CONTINUED TO COME ON INTERMITTENTLY UNTIL BLOCK IN. 2L73 4F RTA3WE 20040217001382004021700138NM 2004 2 17 DHL2004750004 120040128A3350 LIGHT BOEING727 7272M7 138407SNM COCKPIT DOOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01750DH 21951 EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/N ON: 10-0067-7, S/N ON: 25899) 2L73 4F A3WE 20040217001422004021700142NM 2004 2 17 QXEA200400062 120040121A3050 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM MASTER WARNING DIRTY A QXEAK NONE N FALSE WARNING ININSP/MAINT 1 NM09414QX4798 4061 APU BOTTLE LOW/CHECK FOR DEFECT/MASTER WARNING COMES ON INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED AND RESECURED THE CONNECTOR. THE MASTER WARNING CLEARED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040217001562004021700156WP 2004 2 17 AALA20040120 120040125A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW217509 49803 MIA EMERGENCY LIGHTS AT LT AND RT FORWARD OVERWING WINDOW INOPERATIVE. RESET BATTERY PACK OF LT AND RT FORWARD OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F A6WE 20040217001602004021700160WP 2004 2 17 AALA20040124 120040125A3040 CONTROLLER DOUG DC9 DC983 3022083WP COCKPIT WINDOW ARCED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21433AA 49451 DFW INFLIGHT T802/25 FIRST OFFICERS WINDOW HEAT STARTED ARCHING ACROSS WINDOW AND WINDOW SHATTERED. RETURNED TO STATION. LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS WINDOW AND CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA6WE 20040217001672004021700167SO 2004 2 17 C2XA04SH029 120040124A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER NRNOT REPORTED 1 SW2714939 145030 SHV-THE EMERGENCY EXIT SIGN WAS FOUND TO OPERATE INTERMITENTLY. MAINTENANCE REMOVED AND REPLACED THE NUMBER 3 EMERGENCY SIGN INVERTER IAW MFG AMM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040217001702004021700170SO 2004 2 17 C2XA04BT012 120040123A335066364 LIGHT EMB 145 EMB145 3260210SO CABIN DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713969 145141 CREW REPORTED DURING PREFLIGHT, AFT FLOOR EMERGENCY PROXIMITY STRIP LIGHTING INOPERATIVE. MAINTENANCE RESECURED THE AFT EMERGENCY FLOOR PATH LIGHT STRIP. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040218000142004021800014NM 2004 2 18 04FDEA00028 120040105A5313A5A7116509 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25621FE 48792 CTR CARGO BAY BETWEEN BS 1513 -1547, LONGERON 45, LONGERON SPLICE CRACKED. SPLICE LONGERON AT BS 5-113 - 1547, 45 RT, REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. NEW SPLICE FABRICATED AS PER DWG A5A7116. 2L73 4F RTA22WE 20040218000202004021800020NM 2004 2 18 2004UALA00002 120040103A2910VK0654114087005 BYPASS VALVE AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE GREEN HYD SYSTEMLEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29802UA 690 FLIGHT DIVERTED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. FOUND NOSE LANDING GEAR BYPASS VALVE LEAKING, REPLACED BYPASS DOOR . ACCOMPLISHED GEAR SWING ALL GEAR OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040218000232004021800023NM 2004 2 18 04FDEA00142 120040113A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OB FLAP IB HINGE (WING MOUNTED), OB ACTUATOR LUG HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LT AND RT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040218000292004021800029NM 2004 2 18 04FDEA00163 120040115A5347AEA732515 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 MAIN CARGO DECK RIGHT STA 1250 SEAT TRACK REF X = 75.25, SEAT TRACK HAS EVIDENCE OF CORROSION. MAIN CARGO DECK RH STA 1250 SEAT TRACK REF - X = 75.25 SEAT TRACK CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01, VOL.II. MATERIAL THICKNESS : 0.080 , THICKNESS REMAINED: 0.076, WITHIN LIMIT AS PER SRM 53-70-00, VOL.I. REWORKED AREA PAINT TOUCHED UP AS PER SRM 51-21-01, VOL. II. 2L73 4F RTA22WE 20040218000492004021800049WP 2004 2 18 ABXA040029 120040115A2611 AMPLIFIER DOUG DC9 DC931 3022065WP SMOKE DETECTION FAILED A ABXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23908AX 47008 CARGO SMOKE LIGHT ON IN FLT. COULD NOT DUPLICATE. INSPECTED WIRING, TAPPED ON DETECTORS & AMPLIFIER, LIGHT REMAINED OUT. FOR PRECAUTION, R & R BOTH SMOKE DETECTORS & SMOKE DETECTOR AMP. PERFORMED CHECK USING LIQUID SMOKE. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 26-10-07-2. THE SMOKE DETECTORS THAT WERE REMOVED AS PRECAUTION, WERE NOT CONFIRMED FAILURES. SMOKE DETECTOR AMPLIFIER THAT WAS REPLACED AS PRECAUTION, PASSED THE FUNCTIONAL PART OF TEST, BUT FAILED MEGGER PORTION OF TEST. INSULATION RESISTANCE OUT OF SPEC & VARIED. IT APPEARED TO BE A FAULT OF RELAY INSIDE AMP. NO WAY OF KNOWING HOW THAT PROBLEM WOULD AFFECT A/C, OR WHAT KIND OF CONDITION IT WOULD CAUSE. PART WAS QUARANTINED FOR FURTHER TESTING. 2L72 4F A6WE 20040218000512004021800051WP 2004 2 18 UPS04841773 120040120A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 INSPECTION TYPE: PFLT, BELLY SKIN BULGED/CRACKED AREA OF PIT 34 DOOR CUTOUT AT LONG 35R & LR 36. ACCCOMPLISH LFEC INSP OF AREA FOUND INDICATION OF 30 PERCENT DEFECT IN 3 AREAS (MARKED) PER ENGINEERING REQUEST ACCOMPLISHED ETLF 6-10-02 TO MAP AREA OF DEFECT INSTALLED A REPAIR DOUBLER AS PER EO DC8 5330-19859A THIS CLOSES D274572. 2L74 4F RT4A25 20040218000612004021800061NM 2004 2 18 04FDEA00210 120040123A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148. BLENDED CORROSION ON SHEAR TIE AT BS 500 STR 27 LT WL 148 PER SRM 51-10-1. BLEND AREA WAS 2X1INCHES, ORIGINAL THICKNESS WAS .063. 100 PERCENT MATERIAL WAS REMOVED. REMOVED DAMAGED SHEAR TIE, BS 500, STR 27, WL 148 AND FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, PAINTED, AND INSTALLED NEW SHEAR TIE PER SRM 51-30-5, 51-30-6, 51-10-2, 51-30-2 AND FED EX MM 51-20-151-7 2L73 4F RTA3WE 20040218000792004021800079NM 2004 2 18 04FDEA00206 120040123A5315BAC1518378 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM BS 480 LBL 2-10 WL 208. REMOVED CORROSION BY REMOVING .035 FROM AN AREA OF 2X2 INCHES. AREA IS OUT OF LIMITS. REMOVED DAMAGED AREA OF TOP CHORD. REPAIRED FLOORBEAM IAW SRM 53-10-8, 53-10-1 2L73 4F RTA3WE 20040218000822004021800082NM 2004 2 18 UPS04441741 120040105A5315 FLOORBEAM BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, UPPER DECK - BS 340 RBL 4 - 40 LATERAL FLOORBEAM FOUND SERVICE CORROSION. FLOORBEAM UPPER SECTION REPAIRED PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 1 X 1 INCH. 2L74 4F A20WE 20040218000942004021800094EU 2004 2 18 DHL2004366001 120040120A2170 COALESCER BAG AIRBUS300 A300B4203 3930306EU A/C SYSTEM MISINSTALLED A DHLAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01366DH 249 DURING DESCENT, COCKPIT FILLED WITH CONDENSATION FOG AND ACRID ODOR. CONDENSATION AND ODOR DISAPPEARED WHEN PACK NR 1 WAS TURNED OFF. FOG WAS BAD ENOUGH COCKPIT VISIBILITY WAS GREATLY REDUCED. DEFERRED NR 1 AIR CONDITIONING PACK AS PER MEL 21-51-01, DMI 15439 ASSIGNED CAT-C. PLACARD INSTALLED. CHECKED AND FOUND WATER SEPARATOR COALESCENT BAG INSTALLED INCORRECTLY. INSTALLED CORRECTLY PER M/M 21-51-16, OPS CHECKED NORMAL. THIS CLEARS DMI #15439. 2L72 4F RTA35EU 20040218001232004021800123NM 2004 2 18 04FDEA00308 120040201A5510ALC86292 HINGE DOUG MD11 MD11 3023602NM ZONE 300 MISALIGNED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25604FE 48460 RIGHT HORIZONTAL STABILZER SLOT DOOR 344AB FASTENER HOLES FOUND MISALIGNED. RT HORIZONTAL STAB SLOT DOOR 344AB FASTENER HOLES MISALIGN AREA CARRIED OUT REPAIR IAW EA 1-5510-74301, STABILIZERS - HORIZONTAL STABILIZER - RT NR 1 SLOT DOOR ASSEMBLY REPAIR. 2L73 4F RTA22WE 20040218001282004021800128NM 2004 2 18 04FDEA00332 120040206A5531 STRINGER BOEING727 727200 138407ENM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 VERTICAL STAB LT STRINGER CRACKED, FIN STA 157.2 STR NR 7 FROM TOP, AT BOLT HOLE. REPAIRED CRACKED STRINGER NR 7L FIN STA 157.2 PER SRM 55-30-4 FIG 1. 2L73 4F RTA3WE 20040218001292004021800129NM 2004 2 18 04FDEA00362 120040208A5753ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT O/B FLAP O/B HINGE O/B PIVOT HOLE CORRODED. LT O/B FLAP O/B HINGE O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-75245 TITLE - WINGS - TE & TE DEVICES - LT O/B FLAP O/B SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040218001342004021800134NM 2004 2 18 04FDEA00381 120040209A5347ACA7102519 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CORROSION ON CABIN SEAT TRACK AT X27.5 STA 459 TO 480. CORROSION ON CABIN SEAT TRACK AT X27.5 STA 459 TO 480 SECTIONAL REPLACED FROM STA 450 TO STA 525 AS PER MD11 SRM 53-70-00 FIG1 VOL1. 2L73 4F RTA22WE 20040218001352004021800135NM 2004 2 18 0400246716 120040204A3260 CIRCUIT CARD BOEING747 747251F 1384898NM MLG INDICATOR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL013260 21120 DURING APPROACH, THE RED LANDING GEAR LIGHT ILLUMINATED WHILE THE LANDING GEAR INDICATED DOWN AND LOCKED. RECYCLED THE LANDING GEAR AND THE RED LANDING GEAR LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. RESEATED THE GPWS AND THE PRIMARY AND ALTERNATE LOGIC CARDS. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040218001362004021800136NM 2004 2 18 04FDEA00219 120040125A5753ARC2518501 STRAP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT IB FLAP OB HINGE (FLAP SIDE), OB PIVOT HOLE FOUND CORRODED AT STRAP FACE. LT INBD FLAP OUTBD HINGE (FLAP SIDE) OUTBD PIVOT HOLE ATTACH O/B STRAP REMOVED AND REPALCED AS PER SRM 51-33-01 VOL II & AMM 20-50-02. FABRICATED NEW STRAP AS PER DWG ARC2518. 2L73 4F RTA22WE 20040218001382004021800138NM 2004 2 18 04FDEA00221 120040126A5753ARC74903 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 SNRM N1201 : RT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RT INBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA 1-5750-74292, WINGS -LT AND RT INBD FLAP VANE -NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040218001402004021800140NM 2004 2 18 04FDEA00223 120040126A5753ARC74903 FITTING DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT IB FLAP VANE NR 3 TEE FITTING BUSHING BORES DIAMETER FOUND WORN, OUT OF LIMIT. LT INBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA# 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040218000802004021800080NM 2004 2 18 UPS04441739 120040104A5315 FLOORBEAM BOEING747 747123F NM COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, COCKPIT - BS 340, LBL 8 - 44, FLOORBEAM UPPER SECTION FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 3 INCH. FLOORBEAM UPPER SECTION REPAIRED PER SRM 53-10-07 FIG 23. 2L74 4F A20WE 20040218000842004021800084CE 2004 2 18 DXTA200400218 120040116A3246 FUSIBLE PLUG CESSNA500 560CESSNA 2076750CE MLG WHEEL BLOWN E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07807QS620 5600617 AFTER LANDING DURING TAXI, THE FUSIBLE PLUGS BLEW ON THE RT MAIN TIRE. REMOVED AND REPLACED RT MAIN WHEEL AND BRAKE ASSEMBLIES IAW CESSNA 560 MM CHAPTER 32-41-01 AND 32-42-01. INSPECTED AIRCRAFT AND DID NOT FIND ANY DAMAGE, BLED BRAKES AND OPS CHECKED GOOD. 2L72 4F RTA22CE 20040218000852004021800085EU 2004 2 18 YENA200402 120040116A5220L32A319160001 CONTROL CABLE AIRBUS320 A320232 3930326EU EMERGENCY EXIT BINDING A YENAK NONE O OTHER ININSP/MAINT 1 EA15552JB4634 1862 RT EMERGENCY EXIT HATCH CABLE DOES NOT RETRACT LEVER FWD OR AFT DURING OPERATIONAL TEST. REPLACED CONTROL CABLE AS PER AMM 25-62-43-401. 2L72 4F RTA28NM 20040218000922004021800092NE 2004 2 18 QXEA200400044 220040119A7230 COMPRESSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENGINE DAMAGED A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 NM09611QX4432 10041 10041 GEE965288 DEN FLIGHT 4275, RETURNED TO FIELD, NR 2 ENGINE FAN VIBRATION. BLENDED DAMAGED BLADES. COMPLIED WITH NDT. REMOVED AND REPLACED ENGINE. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERICE. 2L72 4F4 FRTA21EA EOOO63EN 20040218000952004021800095NM 2004 2 18 DHL2004755003 120040122A2697 WIRE BOEING727 727225 1384077NM FIRE LOOP BROKEN A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01755DH 21857 NR 2 ENGINE FIRE DETECTOR CIRCUIT GROUND ANNUNCIATOR ON P-6 IS ILLUMINATED. TRANSFERRED TO DMI 15476 PER MEL 26-9-1, PLACARD INSTALLED. FOUND WIRE BROKEN OFF AFT PLUG ON FIRE LOOP NR 2 ENGINE. REPLACED AFT PLUG ON NR 2 ENGINE FIRE LOOP PER BSW PM 20-62-17. OPS CHECKED SATISFACTORY PER B-727 M/M 26-11-01. PLUG P/N: 1625-1. THIS CLEARS DMI 15476. 2L73 4F A3WE 20040218000972004021800097NM 2004 2 18 04FDEA00203 120040122A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CRACK AT NR 1 CARGO AFT FRAME BS 620, TWO INCHES INBOARD OF NR 1 DOOR STOP. REMOVED CRACK AT NR 1 CARGO AFT FRAME BS 620, TWO INCHES INBOARD OF NR 1 DOOR STOP AND REPAIRED PER 727 SRM 51-40-2. 2L73 4F RTA3WE 20040218001072004021800107NM 2004 2 18 04FDEA00241 120040128A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 LEFT A/C BAY, DELTA BEAM LWR PLATE HAS CORROSION AT STA 800 LBL 6 WL 140. REMOVED CORROSION ON DELTA BEAM LWR PLATE AT BS 800, LBL 6, WL 140 IN A 2.500X1.00X.029 DEEP. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA 2.00X.500X.090. FABRICATED FILLER AND PLATE FROM 7075-T6 .090 THICK. ALODINED, PRIMERED, INSTALLED AND PAINTED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-30-2, SRM 51-10-3 AND FED EX MM. 2L73 4F RTA3WE 20040218001122004021800112EU 2004 2 18 UPS04141792 120040128A3510MF20501 OXYGEN MASK AIRBUS300 A300B4622R 3930312EU COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01121UP 0806 CREW AND ALL JUMPSEAT OXYGEN MASKS WILL NOT TEST. FOUND NR 1 COURIER MASK NOT STOWED. RESTOWED ALL MASKS, CHECK OK. NR 1 COURIER 02 MASK INOP. ENTERED DEFERRAL M274961 MEL 35-31-01 PLACARD INSTALLED, SEAT MUST BE UNOCCUPIED. REPLACE 02 MASK PER MM TESTS OK CLEARED M274961. 2L72 4F RTA35EU 20040218001132004021800113NM 2004 2 18 DHL2004745011 120040130A5420 SEAL BOEING727 727224 1384076NM NR 3 NACELLE LOOSE A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT, THIS IS A REPEAT ITEM. DEFERRED NR 3 FIRE WARNING GROUND FAULT DETECTOR PER MEL 29-9-1, DMI 15580, PLACARDS INSTALLED. REF. DMI 15580 (NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT). OPENED NR 3 OUTBD COWLING FOUND RUBBER WEATHER STRIP LOOSE INSIDE, REMOVED STRIP. FOUND DETECTOR LOOP TOUCHING 3 BRACKETS. REPOSITIONED LOOP, RAN NR 3 IAW JRH CHAPTER 5, OPS GOOD IAW 26-11-01. THIS CLEARS DMI 15580. PLACARD REMOVED. 2L73 4F A3WE 20040218001172004021800117EU 2004 2 18 AWXA200400127 120040201A2923693335 PUMP AIRBUS320 A320231 3930325EU HYD SYSTEM FAILED A AWXAO OTHER J WARNING INDICATION CRCRUISE 1 WP28633AW15313578 082 EN ROUTE, RECEIVED PILOT NOTICED AN ELECTRIC BLUE HYD PUMP SYS OVERHEAT MESSAGE ON THE ECAM. AIRCRAFT ARRIVED UNEVENTFUL AND MAINTENANCE REMOVED AND REPLACED THE ELECTRIC BLUE HYDRAULIC SYSTEM PUMP PER AMM 29-12-51-04. OPERATIONAL CHECK PERFORMED WITH NO LEAKS BEING REPORTED. CONFIRMED FAILURE OF ELECTRIC HYD PUMP, ROTOR OUT OF BALANCE. FOUND WORN STATOR, SHAFT SEALS, BEARINGS, RINGS, GASKETS, AND PUMP CONNECTOR. ALL DEFECTIVE PARTS REPLACED IAW CMM 29-21-20, REV. 4. 2L72 4F RTA28NM 20040218001192004021800119NM 2004 2 18 04FDEA00285 120040202A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION IN FWD CARGO BAY, CORROSION ON INNER SURFACE OF SKIN STA 684 BETWEEN STR 27 LT AND 28 LT. FOUND CORROSION ON SKIN AT BS 684, STR 27L AND 28L TO BE .015 DEEP X 4 X 6 INCHES FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IAW SRM 53-30-3. CUT OUT DAMAGE AREA FO SKIN AND FABRICATED DOUBLER AND FILLER FROM 2024T-3 .063 LOT 519699 AND 2024T-3 .050. LOT 532706 AND INSTALLED IAW SRM 53-30-3 FIG 3A. 2L73 4F RTA3WE 20040218001202004021800120NM 2004 2 18 AWXA200400140 120040117A521065458491 SKIN BOEING737 737277 1384570NM R-2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 DURING C-15 CHECK A .25 INCH CRACK WAS FOUND AT R-2 DOOR UPPER HINGE CUTOUT RUNNING DOWNWARD AND AFT FROM LOWER CORNER BS 328, RBL 65, STR 10 RT, WL 260. MAINTENANCE BLENDED OUT CRACK AT R-2 DOOR UPPER HINGE CUTOUT BS 328, RBL 65, STR 10 RT, WL 260; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA ER 15-5210-04029-ES2. 2L72 4F RTA16WE 20040218001262004021800126NM 2004 2 18 04FDEA00330 120040206A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOORBEAM BS 360 LBL 17 - RBL 7 WL 208. FOUND CORROSION ON FLOORBEAM BS 360, LBL 17 TO RBL 17 WL 208 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 20040218001372004021800137NM 2004 2 18 04FDEA00220 120040126A5753ARC74903 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. RH INBD FLAP VANE NR 1 TEE FITTING REPAIRED AS PER EA# 1-5750-74292, WINGS- LEFT AND RIGHT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040218001392004021800139NM 2004 2 18 04FDEA00222 120040126A5753ARC74903 FITTING DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LT IB FLAP VANE NR 1 TEE FITTING BUSHING BORES DIAMETER FOUND WORN OUT OF LIMIT. LT INBD FLAP VANE NR 1 TEE FITTING REPAIRED AS PER EA 1-5750-74292, WINGS - LT AND RT INBD FLAP VANE - NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040218001452004021800145NM 2004 2 18 04FDEA00239 120040128A5320 ANGLE BOEING727 727200 138407ENM RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 ANGLE CRACKED IN RT WHEEL WELL, FORWARD LOWER CORNER, AFT OF APU LOAD CONTROL VALVE. REMOVED ANGLE IN RT WHEEL WELL FWD LWR CORNER AFT OF APU LOAD CONTROL VALVE HOUSING. FABRICATED NEW ANGLE FROM BAC 1503-100058, 7075T6 LOT 509311. APPLIED PROTECTIVE TREATMENT AND INSTALLED. ALL WORK DONE IAW SRM 51-30-2, 51-30-5. 2L73 4F RTA3WE 20040225001852004022500185NM 2004 2 25 DLM88040003 120040103A3030279101891 HEATER DOUG MD88 MD88 3023688NM PITOT HEAD FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27987DL 53338 RECEIVED THE PITOT/STALL HEAT OFF OAP MSG. CYCLED THROUGH METER SEL AND NOTED 0 AMPS AT RUDDER LIMITER POS. AIRBORNE RETURNED TO CVG. REPLACED RUDDER LIMITER PITOT PROBE PER M/M. NOW PROBE HEAT AND LEAK CHECK NORMAL PER TOPPS 20-50 NOT AN RII ITEM. 2L72 4F RTA6WE 20040225001902004022500190NM 2004 2 25 DLM90040008 120040105A242028B5278 GENERATOR DOUG MD90 MD9030 3023690NM RIGHT FAILED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO27912DN 53392 RT AC FEEDER FAULT RT ELEC SYSTEM FAIL AND RT GEN OFF MESSAGE ON EOAP. WOULD NOT RESET IN FLT. FOUND METAL IN GENERATOR OIL. REPLACED GENERATOR. 2L72 4F RTA6WE 20040225001942004022500194NE 2004 2 25 DL73S040012 220040107A7200JT8D15AHK ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 FAILED A DALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO27309DL42552 23081 717141 AT CRUISE FROM YYZ - ATL NR 02 ENGINE OIL PRESS DROPPED TO 28 PSI ALL OTHER INDICATIONS NORM. NR 02 OIL QTY ON MCO NO LOW OIL PRESS LIGHT. AFTER CONSULTING WITH ATL DIVERT TO CVG AND NR 02 ENGINE SHUTDOWN. ENGINE SHUTDOWN REPORT COMPLETED. CHECKED OIL QTY AND OIL CAP FOUND FULL AND CAP IN PLACE. REPLACED ENGINE OIL FILTER INSP OIL FILTER AND CHIP DETECTORS ALL CLEAN. OIL PRESS LIGHT NEVER CAME ON UNTIL AFTER LANDING. CLEAN O/P ORFICE AND REPLACED O/P XMTR. RAN ENGINE TO TAKEOFF PWR AND O/P STAYED 48 PSI. ENGINE OK FOR SERVICE. 2L72 4F4 FRTA16WE E2EA 20040225001952004022500195NM 2004 2 25 DL738040013 120040104A2560P20700030 FLASHLIGHT BOEING737 737832 13844CFNM AFT CABIN INOPERATIVE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27374DA 29622 AFT EMERGENCY FLASHLIGHT INOP. REPLACED AFT JUMPSEAT FLASHLIGHT ASSY AND BATTERY. 2L72 4F RTA16WE 20040226000332004022600033NM 2004 2 26 ASAA0410040 120040124A3397BACC18Z2R CIRCUIT BREAKER BOEING737 7372X6C 1384552NM EMERGENCY LIGHTSINOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC- DURING INSPECTION, FOUND THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET THE EMERGENCY FLOOR PATH LIGHTING CIRCUIT BREAKER THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040226000492004022600049 2004 2 26 QXEA200400147 420040213A34106229819104 PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 200 INOPERATIVE A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09616QX428 428 10128 PDX - RETURNED TO FIELD, FIRST OFFICER'S SPEED BUGS WILL NOT SET PROPERLY. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED AIR DATA REFERENCE PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040226000552004022600055NM 2004 2 26 QXEA200400141 120040211A5753 BRACKET DHAV DHC8 DHC8202 2809007NM TORQUE SENSOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - SECONDARY FLAP DRIVE TORQUE SENSOR BRACKET IS CRACKED AT TOP LEFT HAND END OF BRACKET WHERE RIVETED TO REAR SPAR. REPAIRED IAW HORIZON AIE EA 2-27-252. 2H72 4T RTA13NM 20040226000642004022600064NM 2004 2 26 DL76L040027 120040111A3244321002928 TIRE BOEING767 767332 1382001NM RT MLG FAILED A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27194DN 28451 MID CABIN FLIGHT ATTENDANTS NOTICED VIBRATION ON RIGHT SIDE OF AIRCRAFT JUST PRIOR TO TAKEOFF. ALSO MADRID TOWER REPORTED RUBBER ON RUNWAY. FOUND NR 3 TIRE TREAD SEPARATED FROM TIRE. AIR PRESSURE OK. REMOVED AND REPLACED NR 3 TIRE. PERFORMED TIRE TREAD LOSS CONDITIONAL INSPECTION PER 05-51-16-212-014. DURING INSPECTION FOUND 3 CLAMPS ON RT GEAR HARNESS BROKEN AND 1 PANEL SUPPORT BENT IN RT WHEEL WELL. AWAITING REPAIR INSTRUCTIONS OR ERA. 2L72 4F RTA1NM 20040226000702004022600070NM 2004 2 26 DLM88040034 120040114A3244 TIRE DOUG MD88 MD88 3023688NM NR 4 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27904DL 49535 NR 4 TIRE HAS CHUNK MISSING. REPLACED SAME. 2L72 4F RTA6WE 20040226000742004022600074NM 2004 2 26 DL73S040038 120040115A53156546800508 FLOORBEAM BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27236WA 23184 DURING INSPECTION OF THE BS 520 FLOORBEAM, CRACKS WERE NOTED IN THE RADIUS OF THE UPPER CHORD AT LBL 24.75, 45.5 AND RBL 45.5. EACH CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH. UPPER CHORD WAS CUT OFF AND A NEW SECTION SPLICED IN PER ERA 385945-14. 2L72 4F A16WE 20040226000772004022600077NM 2004 2 26 DL73S040041 120040115A5330655298878 SKIN BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27238WA 23186 DENTS WERE NOTED IN THE FUSELAGE SKIN AROUND L2 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 386075-14. 2L72 4F A16WE 20040226000812004022600081NM 2004 2 26 DL73S040045 120040115A3350BPS75 CHARGER BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27302DL 23047 MCO OVERHEAD EMERGENCY LIGHT BULLNOSE INOP 19D. FOUND BATTERY CHARGER RACK AT M1134 STA 629L INOP. REPLACED CHARGER RACK. 2L72 4F RTA16WE 20040226000832004022600083NM 2004 2 26 DLM88040047 120040115A3260D00106 SENSOR DOUG MD88 MD88 3023688NM NLG INTERMITTENT A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27967DL 53116 AT CRUISE ALTITUDE NOSE GEAR UNSAFE LIGHT ILLUMINATED. FLT CREW REPORTED NO ABNORMAL FLIGHT CHARACTERISTICS. REPLACED UP AND DOWN LOCK PROX SENSORS PER M/M, OPS CHECKS OKAY. 2L72 4F RTA6WE 20040226000852004022600085 2004 2 26 DLM88040050 420040118A2320 CONNECTOR DOUG MD88 MD88 3023688NM ACARS BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27989DL 53341 UPON ARRIVAL CREW INFORMED MAINTENANCE ACARS C/B POPPING AND WILL NOT RESET. FOUND ACARS AUX UNIT AND RACK CONNECTOR WITH BURNED PINS. REPLACED UNIT. 2L72 4F RTA6WE 20040226000872004022600087NM 2004 2 26 DLM88040052 120040119A2560 BATTERY DOUG MD88 MD88 3023688NM FLASHLIGHT INOPERATIVE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27996DL 53363 EMERGENCY FLASHLIGHT LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL. 2L72 4F RTA6WE 20040226000902004022600090NM 2004 2 26 DL738040055 120040119A33501317 BULB BOEING737 737832 13844CFNM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO273740C 30800 EMERGENCY LIGHT INOP ROW 6D OVERHEAD. RELAMPED, OPN CHECKS NORMAL. 2L72 4F RTA16WE 20040226000932004022600093NM 2004 2 26 DLM88040058 120040119A3242392492A BOWL DOUG MD88 MD88 3023688NM HYD VALVE FILTERFAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27937DL 49810 ON CLIMBOUT LOST RIGHT HYD SYSTEM QTY AND PRESSURE. AIR TURNBACK TO IAH. FOUND LEFT INBOARD ANTISKID VALVE FILTER BOWL BROKEN. REPLACED LEFT INBOARD ANTISKID VALVE, NO OTHER LEAKS NOTED. 2L72 4F RTA6WE 20040226000962004022600096NM 2004 2 26 DL738040061 120040120A361032895625 CONTROL VALVE BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO273745B 32373 888326 ON CLIMBOUT, OUT OF 800 FT RIGHT BLEED TRIP OFF LIGHT ILLUMINATED. WOULD NOT RESET. FOUND RIGHT ENGINE PRE-COOLER CONTROL VALVE FAILED. REPLACED VALVE. 2L72 4F4 FRTA16WE E00055EN 20040226001062004022600106NM 2004 2 26 DL73S040071 120040121A5330654576622 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN OF THE STRINGER 10R SKIN LAP JOINT WAS FOUND WITH A SCRIBE LINE ALONG THE PANEL LENGTH FROM FS 360 TO FS 540. THE SKIN LAP JOINT WAS CUT OUT TO REMOVE THE LAP AND THE SCRIBE MARK. THE AREA WAS THEN REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087862-14. 2L72 4F A16WE 20040226001092004022600109NM 2004 2 26 DLM88040074 120040122A213039271011 AUGMENT VALVE DOUG MD88 MD88 3023688NM TAIL AREA FAILED A DALAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 SO27955DL 49886 LOST PRESSURIZATION AT FL LVL 330 EMERGENCY DESCENT. REPLACED RT AUG VALVE. 2L72 4F RTA6WE 20040226001142004022600114NM 2004 2 26 DL777040079 120040124A381012D151 VALVE BOEING777 777232 1385232NM BULK BAG BIN UNSERVICEABLE A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO27861DA 29952 INFLIGHT PROGRESSIVE FAILURE OF ONBOARD POTABLE WATER SYSTEM TO INCLUDE LOSS OF PRESSURE AND WATER FLOW IN ALL GALLEYS AND LAVATORIES EXCEPT AFT GALLEY AND 4 L/R LAVS. RESERVICED WATER SYSTEM. MANUALLY PLACED PRESELECT OVERFLOW VALVE IN THE OPEN POSITION FOR SERVICING. SUSPECT VALVE INTERMITTENT IN INOP POSITION FWD VALVE TO MCO AND PLACARD PER MEL 38-10-01A. DISCONNECTED AND STOWED VALVE ELECTRICAL CONNECTOR. ALSO DURING T/S FOUND L-4 ISOLATION VALVE NOT IN THE FULL OPEN POSITION. REPOSITIONED VALVE WATER SUPPLY, NOW NORMAL. 2L72 4F RTT00001SE 20040226001182004022600118NM 2004 2 26 DL73S040083 120040126A5310654653955 BEAM BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 A CRACK INDICATION WAS NOTED IN THE BS 616 STUB BEAM WEB. CRACK INDICATION WAS REMOVED THE REWORKED/REPAIRED PER ERA 386098-14. 2L72 4F A16WE 20040226001402004022600140NM 2004 2 26 DL757040107 120040128A5754114N4002147A WEDGE BOEING757 757232 1384965NM NR 1 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27605DL 22812 NR 1 SLAT TRAILING EDGE WEDGE DENTED 50 INCHES FROM I/B END. REPAIRED PER SRM 51-70-10. 2L72 4F RTA2NM 20040226001422004022600142NM 2004 2 26 DL73S040109 120040128A5343654654319 FITTING BOEING737 737247 138448DNM MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 THE BS 685 MLG SIDE STRUT SUPPORT FITTINGS ON BOTH THE LT & RT WERE FOUND WITH CORROSION IN THE LUG BORES. REMOVAL OF THE CORROSION RESULTED IN DECREASING THE LUG STRENGTH TO AN UNACCEPTABLE LEVEL. THE FITTING ON BOTH SIDES OF THE AIRCRAFT WERE REMOVED AND NEW FITTINGS INSTALLED PER ER/A 088086-14. 2L72 4F A16WE 20040226001432004022600143NM 2004 2 26 DL76L040110 120040129A3397 TERMINAL BOEING767 767332 1382001NM EMERGENCY LIGHT LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27190DN 28447 CEILING EMERGENCY LIGHT ON RT SIDE 4TH ONE AFT INOP. T/S FOUND BAD GROUND. TIGHTENED DOWN GROUND TERMINAL, OP CHECK OK. 2L72 4F RTA1NM 20040226001492004022600149 2004 2 26 DL764040117 420040130A2330 WIRE BOEING767 767432ER 1385134NM SEAT 7C VDU SPARKS A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27836MH 29709 SEAT 7C VIDEO MONITOR SPARKED. DEACTIVATED IFE SYSTEM, FWD TO MCO. 2L72 4F RTA1NM 20040226001522004022600152 2004 2 26 DL76P040121 420040131A34404336731006612 SWITCH BOEING767 767332 1382001NM COCKPIT BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27140LL 25988 CREW REPORTED SMOKE FROM THE GEAR HANDLE AREA AND GPS FAIL. PULLED GPWS C/BS AND SMOKE WENT AWAY. FOUND GPWS TERRAIN OVERRIDE SWITCH BAD. REPLACED SAME. 2L72 4F RTA1NM 20040226001722004022600172NE 2004 2 26 DL76L040141 220040208A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 STALLED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27181DN42574 25986 723843 NR 2 ENG STALLED ON TAKEOFF ROLL 110 KNOTS, RT ENG SURGE DET ON EICAS ENG EXCT RECORD 660 FOR 12 SEC. REPLACED NR 2 ENG S/N 723843 PER TRANS 1T149. 2L72 4F4 FRTA1NM E24NE 20040226001992004022600199WP 2004 2 26 GKZR200482305 120040217A5713 STRINGER DOUG DC8 DC871F 302199DWP LT WING CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 LEFT UPPER WING THRU ACCESS HOLE 506A AT STA 408.343 NR 7 UPPER STRINGER FROM REAR SPAR CRACKED AT SPLICE. CRACKED BLENDED OUT IAW DC-8 SRM 57-2-0. (CLOSED) 2L74 4F RT4A25 20040226002002004022600200EA 2004 2 26 COMA0460150 120040213A2410 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA IDG ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01814CA 7387 FLIGHT 5927 IDG NR 2 CAUTION MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040226002022004022600202EA 2004 2 26 COMA0470023 120040213A3260895001 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01331CA 10061 FLIGHT 5366 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE RT MLG UPLOCK PROXIMITY SENSOR HARNESS PX 18. 2L72 4F RTA21EA 20040227000032004022700003NM 2004 2 27 DHL2004742002 120040128A4930 ODOR BOEING727 727225 1384077NM CABIN DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01742DH 21290 APU GENERATES RAW JET-A ODOR AFTER STARTING AND TURNING PACKS ON. OPERATED PACKS, NO JET-A ODOR NOTICED, OK IAW MM 49-00-00. 2L73 4F A3WE 20040227000142004022700014EA 2004 2 27 COMA0460090 120040126A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01420CA 7451 FLIGHT 5883 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F RTA21EA 20040227000392004022700039WP 2004 2 27 GTIA040038 120040106A5340 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND FORWARD PIT STATION 237 STRINGER 28L INTERCOSTAL ATTACH ANGLE CRACKED. REMOVED ANGLE. FORMED ANGLE. INSTALLED ANGLE. (M) 2L72 4F RTA6WE 20040227000492004022700049WP 2004 2 27 GTIA040021 120040107A5315 FLOORBEAM DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CABIN CORRODED AT FLOORBEAM STATION 200 LBL 44 INCHES TO LBL 55 INCHES. NO MATERIAL LOSS AT FLOORBEAM. MATERIAL ID TAB END. FABRICATED NEW TAB. INSTALLED NEW TAB END. (M) 2L72 4F A6WE 20040227000502004022700050WP 2004 2 27 GTIA040045 120040202A3350 LIGHT DOUG DC9 DC981 3022081WP CABIN INOPERATIVE A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23811NK 48017 MCO - EMERGENCY LIGHT BELOW WATER SEPARATOR BAGS INOPERATIVE. SECURED WIRES TO LIGHT ASSEMBLY OF EMERGENCY LIGHT BELOW WATER SEPARATOR BAGS. OPS CHECK OK. (M) 2L72 4F A6WE 20040227000562004022700056CE 2004 2 27 57841 120040112A32601143610441 DOWNLOCK BEECH 1900 1900D 1154162CE RT MLG INOPERATIVE A AMWAO OTHER J WARNING INDICATION NRNOT REPORTED 1 CE07155ZV UE155 AFTER NORMAL EXTENSION OF LANDING GEAR RT MAIN DID NOT SHOW DOWN AND LOCK AFTER TOWER FLY BY. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED RT MAIN GEAR DOWN LOCK SWITCH AND HARNESS ASSY, RIGGED SWITCHES AND PERFORMED GEAR SWINGS AS REQUIRED. OPS CK GOOD. IAW BMM 32-60-04 2L72 4T RTA24CE 20040227000642004022700064GL 2004 2 27 O05R200411256 320040127A61116607092417 BLADE FRCHLD22 22C7A 3370104EA GARRTTTPE331TPE331* 01514WP ROTOL R321 R321482F8 GL PROPELLER DAMAGED B K NONE O OTHER ININSP/MAINT 1 GL05698FA14223 DRIDRG1360 BLADE REJECTED IAW MFG CONCESSION 102566/C/P. 1H71 3I3 T ATC438 E2WE 6 CP61GL 20040227000662004022700066GL 2004 2 27 O05R200466978 320040127A611166070924017 BLADE FRCHLD22 22C7A 3370104EA GARRTTTPE331TPE331* 01514WP ROTOL R321 R321482F8 GL PROPELLER DAMAGED B K NONE O OTHER ININSP/MAINT 1 GL05698FA14223 DRG136084 BLADE REJECTED IAW MFG CONCESSION 102556/C/P. 1H71 3I3 T ATC438 E2WE 6 CP61GL 20040227000672004022700067WP 2004 2 27 2004F00053 220040126A726131037511 GASKET SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE LEAKING E E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL273108B AC509 P44141 WHILE ON APPROACH, THE RT (LOW OIL PRESSURE) LIGHT ILLUMINATED. THE PILOT OBSERVED THE OIL PRESSURE INDICATOR WAS READING 40 PSI AND FALLING. THE DECISION WAS MADE TO SHUT THE RT ENGINE DOWN AS A PRECAUTION. THE FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. UPON INVESTIGATION BY MAINTENANCE, IT WAS DETERMINED THAT THE GASKET AT THE NOSE CONE OF THE RT ENGINE HAD FAILED AND SEEPED OIL UNTIL THERE WAS AN INSUFFICIENT SUPPLY. 2L72 4T4 TRTA8SW E4WE 20040227000932004022700093NM 2004 2 27 QXEA200400088 120040127A3350566DH8SA221 LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09546DS 4017 PDX- ROW 9 RT SIDE, ROW 13 LT HAND AND RT SIDE EMERGENCY ESCAPE PATH LIGHTING COVER IS CRACKED. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHTING. 2H72 4T RTA13NM 20040227000952004022700095SO 2004 2 27 C2XA04IA009 120040128A33501317 LAMP EMB 145 EMB145 3260210SO ALLSN AE3007AE3007C GL EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713964 145123 DURING SCHEDULED MAINTENANCE THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED THE LIGHT AND CLEARED THE DISCREPANCY. 2L72 4F4 FRTT00011ATTE6CH 20040227001072004022700107CE 2004 2 27 LHO2004F00000 120040109A2140 COMBUST CHAMBER BEECH 58 58 1152740CE CONT O520 IO520* 17032SO HEATER CORRODED E LHOAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA0585FS 1150 TH486 COMBUSTION TUBE WAS FOUND TO HAVE A CORROSION HOLE IN IT. PART FAILED SOME 25 PERCENT SHORT OF TBO. PILOT NOTED SOOT ON WINDSHIELD AND ODOR IN COCKPIT. THIS HEATER HAS AN EXTENDED LIFE CERAMIC COATED TUBE AND DOES NOT REQUIRE THE FREQUENT INSPECTIONS AND DECAY TEST OF AD96-20-07. ONLY A VISUAL OR PRESSURE DECAY TEST AT 1000 HRS (PER SB 106). TBO IS 1500 HRS. THIS OPERATOR FEELS EVEN THE CERAMIC COATED COMBUSTION TUBES NEED TESTING AND INSPECTIONS AT MORE FREQUENT INTERVALS. 1L72 3O3 O 3A16 E5CE 20040301000222004030100022CE 2004 3 1 EAT2004F00001 120040119A5730582291010 SKIN CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP RT WING LE CORRODED E EATRO OTHER O OTHER NRNOT REPORTED 1 GL096851X8998 4410212 CORROSION WAS FOUND ON THE RT LEADING EDGE SKIN DURING A ROUTINE DE-ICE BOOT CHANGE. IT WAS FOUND ON THE OUTER PORTION LOWER SIDE OF THE SKIN. THE CORROSION WAS OF SUCH A DEPTH AFTER ITS REMOVAL THAT REPAIRS WERE REQUIRED. THE MOST LIKELY CAUSE IS POOR BOOT INSTALLATION LEAVING GAPS IN THE ADHERING SURFACES. THIS MAY HAVE ALLOWED THE AREAS TO FORM CONDENSATION BETWEEN THE BOOT AND SKIN AND OVER THE DE-ICE BOOTS 7+YEARS OF SERVICE.(K) 1L72 3T3 TRTA28CE E2WE 20040301000402004030100040 2004 3 1 0406 420040205A2312066105500 AUDIO PANEL BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ2Y BHCJ2YF2C GL COCKPIT FAILED E BSYAO OTHER O OTHER APAPPROACH 1 GL079189Q TH148 ON APPROACH, LOST OVERHEAD SPEAKER,AND PILOTS HEADSET WAS INOPERATIVE. USED LIGHTS TO SIGNAL TOWER LANDED NO PROBLEM. REMOVED AND REPLACED AUDIO PANEL, OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 5 CP37EA 20040301000682004030100068WP 2004 3 1 UO22004F00000 220040129A723030745554 STATOR LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP COMPRESSOR DAMAGED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL1935TJ 5169 137 P89482 4TH LPC STATOR LOST 1 EACH VANE, RELATED DAMAGE INCLUDES HIGH AND LOW PRESSURE COMPRESSORS, AND HIGH AND LOW PRESSURE TURBINES. 2L72 4F4 F A10CE E6WE 20040301000722004030100072NM 2004 3 1 UIEA200400007 120040126A212065B946272 DUCT BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE COOLING EXHAUST MISALIGNED A UIEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA15809MC 20887 AIR TURNBACK DUE TO NR 3 ENGINE FIRE WARNING. NOTICED EGT AT 850 DEGREES, ON TAKEOFF AT 100 DEGREE HIGHER THAN NR 2 AND NR 4 ENGINES. REMOVED AND REPLACED T/R DRIVE DUCT ASSEMBLY IAW MM, PERFORMED PNEUMATIC LEAK TEST IAW MM, NO LEAKS FOUND. DISCOVERED TURBINE CASE COOLING EXHAUST DUCT MISALIGNED, CORRECTED INSTALLATION IAW MM AND SECURED DUCT. ACCOMPLISHED ENGINE RUN UP IAW MM; ENGINE RUN UP CHECKS GOOD. NO FUEL DUMPED. 2L74 4F4 F A20WE E23EA 20040301000872004030100087NM 2004 3 1 SO19200405477 120040201A2710 AILERON BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE WINGS INOPERATIVE A FX7AO OTHER O OTHER NRNOT REPORTED 1 SO19371FA 23631 IAW L/P 23142 EXCESSIVE RT ROLL AFTER T/O RETURNED WITHOUT INCIDENT, PERFORMED TROUBLESHOOTING INSPECTED LUBRICATED AND CHECKED CABLE TENSION FOR THE AILERON SYS IAW MM. OPS CHECK GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT AND RETURNED AIRCRAFT TO SERVICE WITHOUT INCIDENT. 2L72 4F4 FRTA16WE E2GL 20040301000912004030100091NM 2004 3 1 UIEA200400008 120040127A5710DWG65B07895 BEAM BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE RT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING (D) CHECK AT SIN, RT WING LEADING EDGE NOSE BEAM WEB FOUND WITH 4.2500 CRACK AT ILES 1042. REPAIR, TRIM OUT SECTION OF CRACKED WEB TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICE IN REPLACEMENT WEB REPAIR SECTION WITH ALUMINUM SPLICE DOUBLERS. REFINISH BEAM TO DESIGN STANDARD. REPAIR ACCOMPLISHED AT (C) CHECK INTERVALS NOT TO EXCEED 18 MONTHS FOR SIGNS OF CRACKS OR LOOSE FASTENERS. 2L74 4F4 F A20WE E23EA 20040301000922004030100092NM 2004 3 1 GAIA04011OP 120040203A3260 PROXIMITY SENSOR BOEING727 727224 1384076NM PWA JT8 JT8D9 52048NE NLG DIRTY A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0769739 20667 AFTER TAKEOFF THE FLIGHT CREW NOTICED THAT THE NOSE GEAR RED AND GREEN LIGHTS STAYED ON AFTER GEAR RETRACTION. A NORMAL LANDING WAS MADE. CLEANED NOSE GEAR PROXIMITY SWITCHES AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPS CHECK NORMAL IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040301000962004030100096NM 2004 3 1 GAIA04010OP 120040203A3246 BEARING BOEING727 727223 1384074NM LT MLG WHEEL SEIZED A GAIAO OTHER D INFLIGHT SEPARATION APAPPROACH 1 SW07856AA 20997 ON POST FLIGHT INSPECTION, CREW FOUND NR 1 WHEEL AND TIRE ASSEMBLY MISSING FROM MAIN GEAR. THIS FOLLOWED A NORMAL LANDING WITH NO BRAKING PRIOR TO 70 KNOTS AS THE CREW HAD ANTICIPATED LESS THAN IDEAL BRAKING CONDITIONS. ACCOMPLISHED SPECIAL STRUCTURAL INSPECTION HIGH DRAG/ SIDE LOAD LANDING INSPECTION IAW WK CARD BH 059614. NO AIRCRAFT STRUCTURAL OR ENGINE DAMAGE NOTED ALL DAMAGE LIMITED TO NR 1 AND NR 2 MLG TIRES AND NR 1 BRAKE ASSEMBLY. NR 1 AXLE INSPECTED, NO DAMAGE FOUND. REMOVED AND REPLACED THE NR 1 BRAKE ASSEMBLY AND REPLACED THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES IAW MFG MM. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20040301000982004030100098NM 2004 3 1 GAIA04008OP 120040129A5755 SKIN BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE GROUND SPOILER DELAMINATED A GAIAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW076833 20186 DURING CLIMB THE FLIGHT CREW NOTICED AIRFRAME VIBRATION AT 300 KNTS. REMOVED AND REPLACED NR 8 GROUND SPOILER IAW MM. THE SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040301000992004030100099NM 2004 3 1 RYN2004F00000 120040113A2613356802255 ELEMENT BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE LT AIRSTAIR OVERHEATED A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07801EA 22432 AFTER DEPARTURE, AT GEAR RETRACTION, RECEIVED A LOWER AFT BODY OVERHEAT LIGHT. ACCOMPLISHED APPROPRIATE CHECKLIST. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LT AIRSTAIR AFT BODY OVERHEAT ELEMENT. RAN ENGINES AT TAKEOFF POWER. SYSTEM CHECKS NORMAL. 2L73 4F4 F A3WE E2EA 20040301001152004030100115NE 2004 3 1 I6G2004F00000 220040205A72503028601 TURBINE BLADES CESSNA500 550 2076604CE PWA JT15 JT15* 52060NE ENGINE FAILED B I6GRO OTHER O OTHER NRNOT REPORTED 1 SO1131GA 1414 5500221 PCE70679 BLADE FAILURE. (HIGH TURBINE) CALLED IN FOR VIBRATION BORESCOPE REVEALED HT BLADE FAILURE. 1L72 4F4 T A22CE E1NE 20040301001342004030100134WP 2004 3 1 DHL2004806565 120040128A5347 SUPPORT FITTING DOUG DC8 DC873F 302199FWP SEAT TRACK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 ITEM REF. NR. 0593: FWD CARGO COMPT. SEAT TRACK SUPPORT FITTING CRACKED 1.000 STA 120.000, BL0. CORR.: REMOVED CRACKED SEAT TRACK SUPPORT FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG.9 2L74 4F RT4A25 20040301001362004030100136WP 2004 3 1 DHL2004806563 120040123A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RUDDER RT SKIN INTERNAL PART CORRODED AT STA ZR 140.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW MFG MSG NR DHL-CVG04-0012H, DHL-CVG04-0014H, ED3584-1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG.12. REMOVED CORRODED SKIN AND FINGER DOUBLER IAW SRM 51-1-21 PG.1. FABRICATED NEW SKIN(2024-T3AL 0.032) IAW MFG MSG NR DHL-CVG04-0012H, DHL-CVG04-0014H, ED3584-1. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN IAW MFG MSGT NR DHL-CVG04-0012H, DHL-CVG04-0014H, ED3584-1, SRM 51-1-21 PG.1. FOR REBALANCE SEE NR 2140. 2L74 4F RT4A25 20040301001372004030100137WP 2004 3 1 DHL2004806566 120040128A5523 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR TAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RT ELEVATOR CONTROL TAB T/E WITH 1.500 X 0.500 DENT IN IT. CLEANED DAMAGED AREA IAW SRM 51-1-9 PG.1. FABRICATED DOUBLER (2024-T3AL 0.016) IAW SRM 55-2-2 PG.5, PAR.5 FIG. 3B. BONDED DOUBLER WITH HYSOL IAW SRM 51-1-9 PAR.4. REFER TO NR 2428 FOR REBALANCING. 2L74 4F RT4A25 20040301001382004030100138WP 2004 3 1 DHL2004806572 120040131A5754 SKIN DOUG DC8 DC873F 302199FWP LT WING LE VANE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 ITEM REF. NR. 0738: LT WING CENTER L/E OB. VANE SLOT CORRODED AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDU80-8, DWG U80-R08. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG. 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80-8, DWG U80-R08. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6AL 0.063), DOUBLER (7075-T6AL 0.071) IAW ED-EDU80-8, DWG U80-R08. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INNER SIDE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER IAW ED-EDU80-8, DWG U80-R08, SRM 512L74 4F RT4A25 20040301001402004030100140NE 2004 3 1 58290 320040126A6140 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA HARTZLHCE4A HCE4A3A NE LT PROP STUCK A AMWAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 CE07237YV UE237 ON TAKEOFF ROLL THE LT PROP INDICATOR BEGAN TO READ HIGH, IT THEN WENT TO 2000 AND STUCK. CREW ABORTED TAKEOFF AND RETURNED TO GATE, ON SHUT DOWN INDICATOR STUCK AT 600. THERE WAS NO FURTHER INCIDENT OCCUR. COULD NOT DUPLICATE THE PROBLEM. 2L72 4T3 TRTA24CE E2NE 5 CP10NE 20040301001442004030100144NM 2004 3 1 QXEA200400137 120040209A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - GOUGE IN FUSELAGE SKIN ONE INCH FORWARD OF FRAME X196.000 AND 1 INCH ABOVE STRINGER 13R. REPAIRED IAW HORIZON AIR EA 6-53-326. 2H72 4T4 TRTA13NM E00062EN 20040301001462004030100146WP 2004 3 1 04FDEA00409 120040213A3233ARG70255529 ACTUATOR DOUG DC10 DC1010 3022110WP RT MLG INTERMITTENT A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25394FE 46628 ON T/O, GEAR RETRACTION, RT GEAR LIGHTS REMAINED RED ON BOTH GEAR PANEL AND ON CONFIGURATION PAGE. RAN QRH PROCEDURE, DUMPED FUEL, RETURNED TO PDX, WHEN GEAR LOWERED, RECEIVED TWO IMMEDIATE GREEN LIGHTS FOR THE RT GEAR. 2L73 4F A22WE 20040301001502004030100150NM 2004 3 1 F3LA200400011 120040212A2120 SMOKE AIRBUSA319 A319111 3930336NM COCKPIT DETECTED A F3LAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03920FR 1997 AFTER LANDING, FLIGHT CREW REPORTED SMOKE FILLED COCKPIT AND CABIN. ECAM STATED AFT CARGO FIRE. FOLLOWED ECAM PROCEDURES AND FIRED AGENT BOTTLE. SMOKE STARTED TO DISSIPATE AFTER FIRING AGENT BOTTLE. REPLACED FIRE BOTTLE DUE TO DISCHARGE IAW AMM 26-23-41-400-005. REMOVED 4 SMOKE DETECTOR UNITS IN AFT CARGO COMPARTMENT IAW AMM 26-16-15-000-001. INSTALLED 4 SMOKE DETECTOR UNITS IN AFT CARGO COMPARTMENT IAW AMM 26-16-15-400-001. PERFORMED OPERATIONAL CHECK ON AFT CARGO SMOKE DETECTION SYSTEM IAW AMM 26-16-00-710-001 AND CHECKED OK. 2L72 4F RTA28NM 20040301001512004030100151CE 2004 3 1 0408 120040113A323008421043 BELLCRANK CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C505 GL NLG BROKEN E BSYAO OTHER O OTHER APAPPROACH 1 GL073597G 310R0875 HAD NO NOSE GEAR DOWN AND LOCK LIGHT, PUT AIRCRAFT INTO NEG G'S NOSE GEAR CAME DOWN AND LOCKED OVER CENTER, LANDED OK. REMOVED AND REPLACED NOSE GEAR ACTUATING BELL CRANK. OPS CHECK GOOD. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20040301001532004030100153SW 2004 3 1 SDR02060432 120040206A321354510291 SHAFT OZONE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL LT MLG FRACTURED E HKGAO OTHER E VIBRATION/BUFFET LDLANDING 1 SW173114G2967648 AC583 UPON LANDING, DURING ROLL OUT PILOT REPORTED A HEAVY VIBRATION FOLLOWED BY AN ABRUPT PULL TO THE LEFT. INSPECTION OF THE LT MAIN GEAR ASSEMBLY REVEALED A BROKEN LOWER SCISSOR ASSEMBLY SHAFT WHICH ALLOWED THE YOKE TO ROTATE. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20040301001552004030100155WP 2004 3 1 0400269605 120040116A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01605NW 47223 DURING (L) CHECK FOUND CRACK IN SKIN AS BS 996 BETWEEN L7L AND L8L. REPAIRED IAW EA 96-197817. 2L72 4F A6WE 20040301001592004030100159NM 2004 3 1 UIA9305 120040216A5711 SPAR CAP DOUG MD90 MD9030 3023690NM RT WING CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017911 53535 DURING S90M CHECK FOUND TWO CORROSION SITES ON AFT EDGE OF RT WING UPPER SKIN AND TWO CORROSION NR 1-NR 4 ON LOWER P/N5935822-506 AND REAR SPAR CAP P/N 5911301-1 UPPER SURFACE OF RT WING NEAR STA XRS=546. PFM THE REPAIR TO CORROSION BLEADOUTS AND TEMPOARY REPAIR UNTIL NEXT C-CHECK FOR DAMAGE TOLERANCE ANALYSIS. 2L72 4F RTA6WE 20040301001622004030100162NM 2004 3 1 QXEA200400139 120040214A6120697072003 GOVERNOR BOMBDRDHC8 DHC8401 1390041NM NR 1 OVERSPEED MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX5179 4060 SEA FLIGHT NR 2328 AFTER-START PROCEDURE, WHEN AUTOFEATHER WAS SELECTED, NR 1 PROP FEATHERED BUT THERE WERE NO INDICATIONS OF THAT EXCEPT PROP RPM 220. REPLACED THE OVERSPEED GOVERNOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040301001632004030100163EU 2004 3 1 2004UALA00103 120040208A7830 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE THRUST REVERSER MALFUNCTIONED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29424UA 506 RETURN TO FIELD UNDER AMBER ALERT DUE TO YELLOW HYDRAULIC SYSTEM PROBLEM. REPLACED THE NUMBER ONE THRUST REVERSER ACTUATOR. 2L72 4F4 FRTA28NM E40NE 20040301001642004030100164NM 2004 3 1 2004UALA00104 120040208A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 STRINGER 16L HAS DAMAGE AT STA 617. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040301001682004030100168NM 2004 3 1 2004UALA00108 120040208A5610 WINDSHIELD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29328UA 24148 DIVERTED WITH L4 CRACKED WINDSHIELD. PROBABLE CAUSE: MOISTURE INGRESSION.WINDOW REPLACED. ALL FLIGHT DECK WINDOWS ARE INSPECTED FOR CONDITION EACH C CHECK. THE 'PART TIME SINCE INSPECTION' INFORMATION IS TIME SINCE LAST C CHECK. 2L72 4F4 FRTA16WE E2GL 20040301001692004030100169NM 2004 3 1 2004UALA00109 120040207A2410 BEARING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 GENERATOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29311UA 23672 RETURNED, DUE TO LOSS OF NR 2 GENERATOR. FOLLOW UP FROM SHOP CONFIRMED CSD LOWER BEARING FAILURE. 2L72 4F4 FRTA16WE E2GL 20040301001742004030100174EA 2004 3 1 COMA0460144 120040214A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01975CA 7150 FLIGHT 5473 RT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT. IAW MEL. 2L72 4F RTA21EA 20040301001752004030100175EA 2004 3 1 COMA0460145 120040214A27507805013 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01915CA11535 7013 FLIGHT 5110 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR UNIT. 2L72 4F RTA21EA 20040301001762004030100176EA 2004 3 1 COMA0460146 120040215A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT CHAFED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01977CA 7157 FLIGHT 5422, EMERGENCY FLOOR LIGHTS INOPERATIVE ROWS 6,7, AND 8. REPAIRED CHAFED WIRING AT ROW 5. 2L72 4F4 FRTA21EA E15NE 20040301001852004030100185NM 2004 3 1 DHL2004745013 120040210A2612 FIRE LOOP BOEING727 727224 1384076NM NR 3 ENGINE SHORTED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. DEFERRED NR 3 GROUND FAULT DETECTOR PER MEL 26-9-1. DMI 15683 PLACARD INSTALLED. REF DMI 15683 NR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND LOWER COWL RIBS COMING IN CONTACT WITH LOWER FIRE LOOP. RE-POSITIONED LOOP, NO FAULTS NOTED. THIS CLEARS DMI 15683. 2L73 4F A3WE 20040301001862004030100186NM 2004 3 1 DHL2004784001 120040210A3220 SMOKE BOEING727 727227 1384078NM COCKPIT DETECTED A DHLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO01784DH 22001 WHILE EN ROUTE TO EWR FROM CVG INFORMED BY ATC THAT AN AIRCRAFT AT CVG NOTICED THE NOSE GEAR WAS CANTERED AT 45 DEGREES AND SMOKE APPEARED TO BE COMING FROM THE NOSE GEAR AREA. BASED ON THIS INFORMATION, THE DECISION WAS MADE TO RETURN TO CVG, MAKE A FLYBY AND THEN/AND, WHILE EN ROUTE THE AOM WAS REVIEWED FOR LANDING GEAR MALFUNCTION, AND EMERGENCY EGRESS, NOTHING UNUSUAL WAS OBSERVED WHILE LANDING GEAR WAS RETRACTED OR EXTENDED. LANDING ON RETURN TO CVG WAS NORMAL, AFTER MECHANICS INSPECTION, NORMAL TAXI WAS MADE TO PARKING. INSPECTED NOSE GEAR STEERING COMPONENTS TORSIONAL STOP IAW B-727 M/M 32-21-21. NO FAULTS FOUND. OKAY FOR CONTINUED SERVICE. 2L73 4F A3WE 20040301001882004030100188WP 2004 3 1 DHL2004806573 120040205A55415656225U11 RIB DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RUDDER STRUCTURAL RIB CRACKED 2.000 AT STA ZR 101.000 (REF CTR DAMPER). REMOVED CRACKED RIB IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040301001892004030100189WP 2004 3 1 DHL2004806567 120040205A53203646688U505 CLIP DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 AFT ACCY COMPT CLIP CRACKED 1.000 STA 660.000 L-22L. REMOVED CRACKED CLIP ON AFT ACCY COMPT STA 660.000, L-22L IAW SRM 51-1-20D PG 21, SRM 53-1-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040301001902004030100190WP 2004 3 1 DHL2004806568 120040128A5523 SKIN DOUG DC8 DC873F 302199FWP ELEVATOR TAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT ELEVATOR CONTROL TAB EXTERNAL UPPER SKIN DENTED 1.500. REMOVED DAMAGED AREA IAW SRM 55-2-2 PG 5, PAR 5B. FABRICATED DOUBLER (2024-T3AL 0.016) IAW SRM 52-2-2 PG 5. INSTALLED DOUBLER IAW SRM 51-1-9 PAR 2. 2L74 4F RT4A25 20040301001912004030100191WP 2004 3 1 DHL2004806569 120040129A5720 INTERCOSTAL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING T/E INTERCOSTAL LOWER SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED DAMAGED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL (7075-TO-0.090) IAW SRM 57-1-0 PG 1. HEAT TREATED NEW INTERCOSTAL IAW SRM 51-1-1 PG 11, 13-21. CLEANED, TREATED AND PRIMED AREA AND NEW INTERCOSTAL IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21. 2L74 4F RT4A25 20040301001942004030100194WP 2004 3 1 GKZR200482309 120040217A5314 KEELBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 RIGHT KEEL BEAM AREA, FORMER JUST I/B OF MLG DOOR ACT MOUNT CRACKED. CRACK WAS STOP DRILLED BUT WENT PAST, CRACK 3 INCHES ABOVE END OF 1ST CRACK GOES FWD AND AFT. REMOVED FORMED WEB IAW DC-8 SRM 51-1-21. FABRICATED WEB MATERIAL USED 7075 .071. INSTALLED WEB IAW DC-8 SRM 51-1-21 AND 51-1-20. (CLOSED) 2L74 4F RT4A25 20040301001952004030100195WP 2004 3 1 AALA20040227 120040216A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217541A 49995 TUL - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE WHEN TESTED. RESET EMERGENCY LIGHT ARM AND TESTED CIRCUIT BREAKER FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040301001982004030100198NM 2004 3 1 AALA20040237 120040215A3397 CABLE BOEING757 7572Q8 1384972NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21710TW 28169 DFW - EMERGENCY PATH LIGHT STRIP AT MID LAVATORY BY 2L DOOR INOPERATIVE. REPLACED RIBBON CABLE TO EMERGENCY PATH LIGHT STRIP IN FRONT OF MID LAVATORY BY 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPRATION. 2L72 4F RTA2NM 20040301002012004030100201NM 2004 3 1 AALA20040231 120040216A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21766AN 32880 MIA - EMERGENCY EGRESS SEAT MOUNTED LIGHTS AT ROWS 20 THROUGH 28 INOPERATIVE. FOUND CONNECTOR OFF UNDER ROW 22 FOR ROWS 20-22. REPLACED BATTERY PACK FOR EGRESS SEAT MOUNTED EMERGENCY LIGHTS FOR ROWS 20 THROUGH 28 AND REPLACED CANNON PLUG AT ROW 22 FOR SEAT MOUNTED EMERGENCY LIGHTS ROWS 20 THROUGH 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040301002032004030100203NM 2004 3 1 AALA20040235 120040215A3350 LIGHT BOEING757 757223 1384957NM CABIN DETERIORATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21617AM 24525 DFW - EMERGENCY LIGHT EXIT MARKER DECAL AT LEFT HAND FORWARD OVERWING EXIT IS DETERIORATED. REPLACED EMERGENCY LIGHT EXIT MARKER DECAL FOR LEFT HAND FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040301002042004030100204NM 2004 3 1 AALA20040236 120040215A3350 LIGHT BOEING757 757231 1384950NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21711ZX 28481 STL - EMERGENCY EGRESS LIGHTS AT AFT CABIN FLOOR INOPERATIVE. CLEANED MOISTURE FROM AFT CABIN EGRESS EMERGENCY LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040301002072004030100207NM 2004 3 1 AALA20040240 120040216A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21633AA 24591 MIA - SEAT MOUNTED EMERGENCY EXIT LIGHT AT 31DEF INOPERATIVE. FOUND SEAT TO SIDEWALL CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY EXIT LIGHT AT 31DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040301002082004030100208 2004 3 1 SWAA040454 420040213A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040301002132004030100213NM 2004 3 1 SWAA040459 120040213A57536546430 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040301002152004030100215NM 2004 3 1 SWAA040461 120040213A53106550568 DOOR FRAME BOEING737 7373Q8 1384670NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR FRAME CUTOUT LOWER FORWARD CORNER CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040301002182004030100218NM 2004 3 1 SWAA040464 120040214A57536571909 FLAP BOEING737 7372H4 138448CNM LT WING BROKEN A SWAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW29086SW 22827 AIRCRAFT ROLLS LEFT WITH FLAPS AT 30 OR 40 DEGREES, REQUIRES A LOT OF AILERON TO HOLD LEVEL. REMOVED AND REPLACED LEFT OUTBOARD MID FLAP ASSEMBLY PER MM. 2L72 4F A16WE 20040301002202004030100220NM 2004 3 1 SWAA040466 120040214A53206561777 CHANNEL BOEING737 7373A4 1384585NM DOOR FRAME CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR FRAME CUTOUT H-CHANNEL CRACKED AT UPPER HINGE. REPAIRED PER EA. 2L72 4F RTA16WE 20040301002212004030100221NM 2004 3 1 SWAA040467 120040214A5310573149 WINDOW POST BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND RT FLIGHT COMPARTMENT WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20040226001082004022600108NM 2004 2 26 DL73S040073 120040121A5330654577416 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER FUSELAGE SKIN OF THE STRINGER 14L SKIN LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 727 TO FS 908. THE LAP JOINT AND SCRIBE LINE WERE REMOVED WITH A CUTOUT. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53-1177 AND ER/A 087865-14. 2L72 4F A16WE 20040226001112004022600111NM 2004 2 26 DL73S040076 120040123A5330654580024 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 THE LOWER SKIN OF THE STRINGER 10R LAP JOINT WAS FOUND SCRIBED ALONG THE LENGTH OF THE PANEL FROM FS 330-360. THE SCRIBED SECTION OF SKIN WAS CUT AND REMOVED. THE AREA WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386026-14. 2L72 4F A16WE 20040226001132004022600113 2004 2 26 DL757040078 420040124A2565404002 SLIDE BOEING757 757232 1384965NM R1 DOOR DISLODGED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27606DL 22813 THE 1R DOOR OPENED WHILE STILL ARMED, R1 DOOR ASSIST BOTTLE DISCHARGED. R1 DOOR FULLY OPENED, BUT SLIDE PACK FELL ON TO CATERING TRUCK PLATFORM AND DID NOT DEPLOY. REPLACED SLIDE PACK. 2L72 4F RTA2NM 20040226001152004022600115NM 2004 2 26 DLM88040080 120040124A3350RPS1B POWER SUPPLY DOUG MD88 MD88 3023688NM SEAT 31/38 INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27904DL 49535 EMERGENCY LIGHTS AT SEAT ROW 31DE THROUGH 38DE INOP. REPLACED POWER SUPPLY. CHECKS NORMAL. 2L72 4F RTA6WE 20040226001162004022600116NE 2004 2 26 DL78K040081 220040125A7250CFM567 BEARING BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE NR 1 ENGINE FAILED A DALAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO273730B5872 30538 876583 NR 1 ENG INFLIGHT SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT. FOUND METAL IN TAILPIPE AND FAN WOULD NOT SPIN. REPLACED ENGINE. 2L72 4F4 FRTA16WE E00055EN 20040226001192004022600119NM 2004 2 26 DL73S040084 120040126A5330654577655 SKIN BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 CORROSION WAS NOTED IN THE FUSELAGE SKIN AT S27L BETWEEN BS 947.50 TO 967. CORROSION WAS REMOVED AND AREA REPAIRED PER ERA 386110-14. 2L72 4F A16WE 20040226001212004022600121 2004 2 26 DLM88040086 420040126A3417HG280D80 ADC DOUG MD88 MD88 3023688NM E/E BAY MALFUNCTIONED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27918DE 49959 CAPTS A/S INDICATOR WOULD NOT INCREASE PAST 60 KTS ON T/O ROLL. ABORTED T/O AT 90 KTS ON F/O`S INDICATOR. REPLACED NR 1 CADC PER MM CHAPT 34. PERFORMED FUNCTIONAL TEST. OPERATION NORMAL. 2L72 4F RTA6WE 20040226001242004022600124NM 2004 2 26 DL764040089 120040126A3230 PSEU BOEING767 767432ER 1385134NM MLG MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27840MH 29717 AFTER TAKEOFF GOT EICAS MSGS TAILSKID AND TCAS DURING CLIMB. TAILSKID MSG WENT OUT AND GOT GEAR DISAGREE EICAS MSG ACCOMPANIED BY GEAR SYNOPTIC NOSE UP AND MAIN GEAR INTRANSIT. RETURNED TO LAX. CHECKED OUT WIRING AND GEAR HANDLE SWITCHES THROUGH TO PSEU PROBLEMS FOUND. REPLACED R33 DIODE, PRECAUTIONARY REPLACED PSEU-JAC A/C SWUNG GEAR CHECKED OK, NO FAULT MSGS. REPLACED SYSTEM 1 S 244 NOSE GEAR NOT COMPRESSED SWITCH. RETRACT AND EXTEND LANDING GEAR, OPS CHECKED NORMAL. 2L72 4F RTA1NM 20040226001482004022600148NM 2004 2 26 DL73S040115 120040128A5551 ATTACH FITTING BOEING737 737232 1384475NM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 THE STABILZER ATTACHMENT LUGS WERE FOUND WITH DAMAGE EXCEEDING THE LIMITS OF SB 737-55-1033. DAMAGE WAS REMOVED BY BLENDING AND OVERSIZING BORES PER ER/A 386108-14AD. 2L72 4F RTA16WE 20040226001512004022600151NM 2004 2 26 DL757040120 120040131A3350BPS73 POWER SUPPLY BOEING757 757232 1384965NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27602DL 22809 F/C SEATS EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2L72 4F RTA2NM 20040226001712004022600171NM 2004 2 26 DL738040140 120040208A3244 TIRE BOEING737 737832 13844CFNM MLG WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO273748Y 30489 CORD SHOWING ON NR 1 MLG TIRE. REPLACED NR 1 MAIN WHEEL ASSY. SPACER INSTALLED. 2L72 4F RTA16WE 20040226001802004022600180NM 2004 2 26 DL73S040149 120040211A5311654577055 FRAME BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 DURING INSPECTION OF THE BS 663 FRAME CRACKS WERE NOTED IN THE FRAME AT S3L, S2L AND S1. DURING INSTALLATION OF THE SRM FRAME REPAIR IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO ACCOMMODATE FRAME REPAIR FASTENERS. FRAME WAS REPAIRED PER SRM, SKIN REPAIRED PER ERA 386063-14. 2L72 4F RTA16WE 20040226001912004022600191NM 2004 2 26 DLM88040160 120040215A2432249701273 BATTERY DOUG MD88 MD88 3023688NM E AND E SMOKE A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27918DL 49583 FOUND BY ACS, SMOKE COMING OUT OF BATTERY VENT LINE BEHIND NOSE GEAR. REPLACED BATTERIES, CHARGER, AND CABLES. 2L72 4F RTA6WE 20040226001942004022600194CE 2004 2 26 DXTA200400243 120040214A3260 WARNING LIGHT CESSNA560 560XL 2076702CE MLG FALSE INDICATIONE DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07664QS 5605264 AFTER TAKEOFF MOVED GEAR HANDLE UP AND NOTICED THE UNLOCK LIGHT REMAINED ON. RECYCLED GEARS TWICE AND PROBLEM REMAINED THE SAME WITH HYDRAULIC PRESS LIGHT STAYING ON. ACCOMPLISHED AIR TURNBACK AND LANDED SAFELY. PLACED AIRCRAFT ON JACKS AND CYCLED LANDING GEAR SEVERAL CYCLES, COULD NOT DUPLICATE DISCREPANCY. INSPECTED UPLOCK SWITCHES RIGGING AND NO FAULT FOUND, OPERATIONAL CHECKS GOOD. REMOVED AIRCRAFT FROM JACKS, ALL WORK PERFORMED IAW CESSNA 560XL CHAPTER 32-30-00 AND 32-61-00. 2L72 4F RTA22CE 20040226001972004022600197CE 2004 2 26 DXTA200400246 120040216A2910 HYDRAULIC SYSTEM CESSNA750 750 2076810CE SYSTEM A LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07942QS 7500024 SHORTLY AFTER TAKEOFF OBSERVED AMBER HYDRAULIC SYSTEM-A LOW QUANTITY CAS MESSAGE, DISCOVER A-SYSTEM DECREASING IN QUANTITY. UNLOADED A-HYDRAULIC PUMP, HYDRAULIC QUANTITY DECREASED TO -0- AND ELECTED TO LAND IMMEDIATELY. DURING DESCENT PTU FAILED, NOTICED STRONG OIL ODOR IN CABIN. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20040227000092004022700009 2004 2 27 SCNA04003 420040128A2200 AUTOPILOT SYS BOEING737 737800* NM B SYSTEM MALFUNCTIONED A SCNAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL15PHHZC 28375 AT 410 AUTOPILOT B FLYING (LNAV/VNAV ENGAGED): AIRCRAFT BANKED LT AT APPROX 20 DEGREES/SECOND. IMMEDIATELY DISCONNTECTED AP. RECONNECTED AP B AFTER NOT FINDING ANY FMC ABNOMALITIES. NO FURTHER PROBLEMS WERE OBSERVED. PERFORMED DFCS BITE TESTS IAW 22-11-00 AND NO FAULTS FOUND. CHECKED GOOD. 2L72 4F RTA16WE 20040227000172004022700017WP 2004 2 27 MWEA040013 120040128A1430 BOLT DOUG DC9 DC981 3022081WP LANDING GEAR MISINSTALLED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31804ME 48030 DURING GEAR RETRACTION A LOUD NOISE COMING FROM THE NOSE GEAR AREA. LT FORWARD NOSE GEAR DOOR RETRACT LINK NOT LATCHED COMPLETELY, FOUND RELEASE HANDLE BOLT INSTALLED IMPROPERLY. REPOSITIONED BOLT CLOSED AND LOCKED FORWARD NOSE GEAR DOOR. 2L72 4F A6WE 20040227000212004022700021WP 2004 2 27 GTIA040040 120040128A2560 GLOWSTRIP DOUG DC9 DC982 3022082WP GALLEY LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 DTW - FLT 834 - AFT GALLEY FLOOR GLOW STRIP OFF. REINSTALLED GALLEY FLOOR AFT GLOWSTRIP. NO OTHER DEFECTS NOTED. (M) 2L72 4F A6WE 20040227000232004022700023WP 2004 2 27 GTIA040031 120040123A3220 LANDING GEAR DOUG DC9 DC982 3022082WP NOSE MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23804NK 49104 DTW - FLT 461 - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. SERVICE NOSE STRUT CHECKED SYSTEM, RIGGING AND PERFORMED NOSE GEAR RETRACTION. NO DEFECTS NOTED. (M) 2L72 4F A6WE 20040227000262004022700026WP 2004 2 27 GTIA040030 120040121A3213 STRUT DOUG DC9 DC982 3022082WP NLG DISCHARGED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23830NK 49932 ACY - FLT 1141 - DEPARTING ACY WITH GEAR HANDLE UP NOSE GEAR HAD UNSAFE INDICATION. RECYCLED GEAR, NOSE CAME UP NORMAL INDICATION REMAINDER OF FLIGHT. NOSE GEAR STRUT FOUND EXTENDED TOO FAR UPON ARRIVAL. SERVICED NOSE GEAR STUT TP PROPER LIMITS. NO LEAKS, DAMAGE OR FURTHER DEFECTS NOTED. (M) 2L72 4F A6WE 20040227000292004022700029WP 2004 2 27 GTIA040034 120040125A2120 ODOR DOUG DC9 DC983 3022083WP CABIN DETECTED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23826NK 49391 DTW - STRONG ODOR OF KEROSENE EXHAUST THROUGH OUT CABIN AND COCKPIT, ALL FLIGHT PHASES. CLEANED GROUND AIR CONDITIONING SUPPLY DUCT. AFTER CLEANING NOTED NO ODOR FROM RT PACK. (M) 2L72 4F RTA6WE 20040227000312004022700031WP 2004 2 27 GTIA040026 120040107A5320 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CABIN HAS CORROSION AT FLOOR SUPPORT STATION 200 TO STATION 160 LBL 55 INCHES. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FORWARD CABIN FLOOR SUPPORT. (M) 2L72 4F A6WE 20040227000402004022700040WP 2004 2 27 GTIA040046 120040127A215068347811 SWITCH DOUG DC9 DC983 3022083WP CABIN COOLING MALFUNCTIONED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP13815NK 49415 DTW - FLT 9815 - AFTER TAKEOFF LAS ABOUT 30 SECONDS A/C GOT VERY HOT IN THE CABIN SOME HAZE, TURN RIGHT PACK OFF A/C COOLED OFF NO HAZE, RIGHT PACK NEEDLE FLUCTUATED FROM 10-2 O'CLOCK POS BEFORE TURNING OFF SUPPLY TEMP ONLY INDICATED 140. TESTED CABIN TEMP CONTROL SYSTEM WITH LINE CHECKER, FOUND SYSTEM SHUTDOWN THERMAL SWITCH AND CABIN RATE OF CHANGE/HIGH LIMIT SENSOR (P/N 60730011 S/N 088C4219) BAD, REMOVED AND REPLACED BOTH UNITS. OPS CHECK GOOD. RAN ENGINES AT TAKEOFF POWER, VERIFIED SYSTEM OPERATES PROPERLY AT HIGH POWER. (M) 2L72 4F RTA6WE 20040227000772004022700077EU 2004 2 27 BAQA092353 120040123A6330L633M2010101 MOUNT UROCOPEC135 EC135P1 8680990EU GEARBOX INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME1058 0009 GEARBOX MOUNT PLUNGER RETRACTED. REPLACED WITH SERVICABLE UNIT. 01/28/2004 1G72 3U O H88EU 20040227000902004022700090WP 2004 2 27 ARWA20040106 120040127A2710 SWITCH DOUG DC8 DC862 3021970WP AILERONS INOPERATIVE A ARWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19810BN 45905 STARTED TAKE-OFF ROLL, AILERON POWER LIGHT CAME ON. REMOVED AND REPLACED MANUAL CONTROL IND SWITCH IAW MM 27-11-14; OPERATIONAL CHECK NORMAL IAW MM 27-11-14 AND 27-11-0. 2L74 4F 4A25 20040227000942004022700094NE 2004 2 27 020204 220040202A8500 ENGINE DOUG DC3 DC3C 3021457WP PWA R1830 R183090D 52020NE RIGHT FAILED E VLLAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL0536AP 291 13439 CP303375 IN CLIMB POWER IN ROUTE RT ENGINE BEGAN TO MISFIRE AND RUN ROUGH. OIL TEMP ALSO INCREASED. ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERTED. ENGINE WAS FOUND VERY HARD TO PULL THROUGH AND METAL FOUND IN SCREEN. SUSPECT CAM RING FAILURE. 2L72 4R4 R A669 5E4 20040301000232004030100023EU 2004 3 1 PG92004F00000 120040123A2910704A34412038 LINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE HYD SYSTEM LEAKING E PG9AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP19453NW 2475 AC LOST ALL HYDRAULIC FLIGHT CONTROL BOOST ASSIST DURING AIR TOUR FLIGHT. PILOT PERFORMED PRECAUTIONARY LANDING IAW MFG MM. MECHANIC DISPATCHED TO REMOTE SITE TO REPAIR AIRCRAFT. FOUND ALL BUT 1 CUP OF HYDRAULIC FLUID LEFT IN RESERVOIR. FOUND SUBJECT HIGH PRESSURE HYDRAULIC LINE WAS SEEPING FLUID, BUT NO APPARENT DEFECTS IN LINE WAS VISUALLY NOTICEABLE. REPLACED LINE WITH NEW AND AIRCRAFT WAS RETURNED TO SERVICE. THERE IS NO TIME REPLACEMENT ON THIS ITEM IAW AC MFG. (K) 1G71 3U3 U H9EU E19EU 20040301000672004030100067NM 2004 3 1 MEX2004040 120040130A2910 LINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENG HYD SYS LEAKING W ASMZO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM 26273 DURING PUSH BACK, FOUND HYDRAULIC LEAKAGE ON THE LT ENGINE WHEN IT WAS STARTED. AT REVISION WAS FOUND A BROKEN HYDRAULIC LINE, SUCH LINE WAS REPLACED BY AN ALTERNATE PN OF THE SAME PRESSURE CAPACITY AND SYSTEM TESTED IAW FIM. 2L72 4F4 FRTA2NM E17NE 20040301000812004030100081CE 2004 3 1 ESE2004F00000 120040125A269799120365 CONNECTOR CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE FIRE DETECTOR INOPERATIVE E ESEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11213JS3570 5500597 A FIRE WARNING OCCURRED DURING CLIMBOUT. ON THE RT ENGINE. NO EMERGENCY DECLARED. AIRCRAFT MADE A PRECAUTIONARY LANDING. NO SECONDARY INDICATION OF MALFUNCTION WERE EVIDENT. CREW COULD NOT DUPLICATE PROBLEM. RT ENGINE FIRE DETECTOR CONNECTOR. 1L72 4F4 F A22CE E1NE 20040301000902004030100090NM 2004 3 1 UIEA200400009 120040202A5730 SKIN BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING (D) CHECK, WING LOWER SKIN CORROSION FOUND AROUND SURGE TANK SUMP DRAIN VALVE AT WING STA 1487, BETWEEN STRINGERS S-5 AND S-6 LT SIDE. CORROSION DAMAGE IS REPAIRED BY BLEND OUT. REPAIR AREA IS SHOP PEENED AND HFEC INSPECTED. APPLIED ALODINE 1200 AND BMS 10-11 TYPE PRIMER. BLEND OUT AREA AROUND DRAIN VALVE FASTENER HOLE IS SPOT FACED. BACB30NW8 HILOK WITH BACC30N8 COLLAR IS INSTALLED WET WITH BMS 5 26 SEALANT IN .2460 TO .2480 INCHES DIAMETER HOLE. BMS 5 26 SEALANT IS APPLIED IN THE BLENDED CAVITY. 2L74 4F4 F A20WE E23EA 20040301000952004030100095NM 2004 3 1 GAIA04012OP 120040204A3260 PROXIMITY SENSOR BOEING727 727224 1384076NM PWA JT8 JT8D9 52048NE NLG OUT OF ADJUST A GAIAO OTHER N FALSE WARNING CLCLIMB 1 SW0769739 20667 AFTER TAKEOFF THE FLIGHT CREW NOTICED THAT THE NOSE GEAR RED AND GREEN LIGHTS STAYED ON AFTER GEAR RETRACTION. THE AIRCRAFT WAS REROUTED. A NORMAL LANDING WAS MADE. ADJUSTED NOSE GEAR POSITION SENSOR IAW MM. OPS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040301001322004030100132WP 2004 3 1 DHL2004806562 120040128A5320 SUPPORT DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 ITEM REF. NR. 2209: AFT CARGO COMPT. LT TUNNEL FLOORBEAM VERTICAL SUPPORT CORRODED, STA 1520.000. CORRODED. REMOVED CORROSION FROM FLOORBEAM VERTICAL SUPPORT STA 1520.000 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. REMOVED CORRODED SUPPORT IAW SRM 51-1-20D PG. 21. FABRICATED NEW SUPPORT (EXTRUSION 7075-T6 511) IAW SRM 53-2-0 PG. 1-2. CLEANED, TREATED AND PRIMED AREA AND NEW SUPPORT IAW SRM 51-1-8B. INSTALLED NEW FLOORBEAM VERTICAL SUPPORT IAW SRM 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040301001422004030100142CE 2004 3 1 58651 120040206A3210130909B38 MOUNT BEECH 1900 1900D 1154162CE DOWNLOCK SWITCH FAILED A AMWAO OTHER O OTHER LDLANDING 1 CE07174YV UE174 AFTER LANDING ON ROLL OUT CREW NOTICED RT MLG ANNUN FAIL/ INTERMITTENLY. AC WAS FERRIED, NO FURTHER INCIDENT. IS INST NEW BOLT, NUT, WASHER IN DOWNLOCK SW. 2L72 4T RTA24CE 20040301001492004030100149CE 2004 3 1 0407 120040113A76035038901229 THROTTLE CABLE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ2Y BHCJ2YF2 GL RT ENGINE BROKEN E BSYAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS APAPPROACH 1 GL07696BD TH352 ON APPROACH, RT ENGINE HAD NO RESPONSE, SHUT ENGINE DOWN LANDED NO PROBLEM. REMOVED AND REPLACED THROTTLE CABLE, OPS CHECK GOOD. 1L72 3O3 O 3A16 E5CE 5 CP37EA 20040301001522004030100152NM 2004 3 1 F3LA200400012 120040210A1430NAS1102E085 SCREW AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE FLAP TRACK MISSING A F3LAO OTHER O OTHER TXTAXI/GRND HDL 1 NM03922FR 2012 FLIGHT CREW REPORTED FASTENER MISSING FROM FLAP TRACK ON RT WING IB OF ENGINE PYLON. PLACED ON MAC 0001276. DETERMINED THIS DID NOT AFFECT SAFETY OF FLIGHT. ON 2/10/04, REPLACED SCREW. 2L72 4F4 FRTA28NM E2GL 20040301001562004030100156NM 2004 3 1 DHL2004780001 120040212A5270 ANNUNCIATOR BOEING727 727223 1384074NM PAX DOOR FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01780DH 22006 FORWARD ENTRY DOOR ANNUNCIATOR ILLUMINATED AFTER LANDING. CHECKED SWITCH AND DOOR. OPS NO FAULTS NOTED IAW MM 52-10. 2L73 4F A3WE 20040301001572004030100157NM 2004 3 1 DHL2004780002 120040213A5210 LOCK BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE PAX DOOR OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01780DH 22006 FORWARD ENTRY DOOR LIGHT ILLUMINATED AFTER LANDING. PREVIOUS WRITE-UP ON LOG PAGE NR 370580. RII REQUIRED. ADJUSTED DOOR LOCK MECHANISM TO ROLL OVER CENTER PAST LOCK FURTHER LOCK AND LIGHT SYSTEM. OPS CHECKED NORMAL ON GROUND IAW MM 52-11-01. 2L73 4F4 F A3WE E2EA 20040301001722004030100172EU 2004 3 1 2004UALA00113 120040210A3350 CONNECTOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29479UA 1538 AFT RT, LWR DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED CONNECTOR. CHECKS OK. 2L72 4F4 FRTA28NM E40NE 20040301001842004030100184NM 2004 3 1 DHL2004749003 120040207A8012 START VALVE BOEING727 7272J0 138407ENM NR 2 ENGINE OPEN A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01749DH 22013 NR 2 START VALVE OPEN ON TAKEOFF ROLL. TAKEOFF REJECTED PRIOR TO 80 KNOTS. AIRCRAFT WEIGHT = 149700 LBS, IAS = 70 KNOTS, OAT = 6 C, PA = 3740, BRAKE ENERGY ZONE NORMAL. REMOVED AND REPLACED START VALVE IAW M/M 80-10-00. GROUND RUN, FUNCTION CHECK OK. NOTE: PRESS SWITCH FROM ORIGINAL VALVE TRACKS TO REPLACEMENT VALVE. 2L73 4F RTA3WE 20040301001932004030100193WP 2004 3 1 GKZR200482308 120040217A5542 DOUBLER DOUG DC8 DC871F 302199DWP RUDDER CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 RUDDER BOTTOM SIDE FWD AT FILLET ON RT SIDE DOUBLER CRACKED AT RIVET IN NUT PLATE TO END OF DOUBLER. REMOVED SEALANT AND PAINT FROM AREA NO EVIDENCE OF A CRACK IAW DC-8 SRM 51-1-8. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND SEALED IAW DC-8 SRM 51-1-16 PG. 1-9. (CLOSED) 2L74 4F RT4A25 20040301001962004030100196NM 2004 3 1 AALA20040228 120040212A3350 LIGHT BOEING777 777223 1385213NM GALLEY BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21756AM 30264 DFW - LEFT HAND EMERGENCY LIGHT AT FIRST CLASS GALLEY BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY FOR LEFT HAND SIDE AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040301001992004030100199WP 2004 3 1 AALA20040239 120040216A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21432AA 49350 DEN - EMERGENCY LIGHT AT AFT CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHT AT AFT CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040301002062004030100206WP 2004 3 1 AALA20040234 120040215A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217547A 53029 ATL - OVERWING EMERGENCY LIGHTS AT ROW 20A AND 20F INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS FOR ROW 20A AND 20F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040301002192004030100219NM 2004 3 1 SWAA040465 120040214A53206545890 STRAP BOEING737 7373H4 1384600NM DOOR FRAME CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR CUTOUT AT UPPER AND LOWER HINGE STRAPS CRACKED. REMOVED AND REPLACED STRAPS PER SRM. 2L72 4F RTA16WE 20040301002232004030100223NM 2004 3 1 SWAA040469 120040214A53106546529 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 500D, BETWEEN STRINGER 26L AND STRINGER 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040301002242004030100224NM 2004 3 1 SWAA040470 120040214A53146545866 KEELBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 500D, STRINGER 28L. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20040301002252004030100225 2004 3 1 SWAA040471 420040214A25651061323 SLIDE BOEING737 7375H4 138449DNM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 L2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040301002272004030100227NM 2004 3 1 SWAA040473 120040215A3350BR2013 WIRE BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 EEPLS HAS WIRES EXPOSED. STOWED WIRES PER MM. 2L72 4F RTA16WE 20040301002282004030100228NM 2004 3 1 SWAA040474 120040215A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND INBOARD FRAME CHORD CRACKED AT BS 616, RBL 65, WL 204. REPAIRED FRAME CHORD PER ER. 2L72 4F RTA16WE 20040301002292004030100229NM 2004 3 1 SWAA040475 120040215A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FLOORBEAMS CRACKED AT BS 727B, RBL 25, WL 208 AND BS 727B, LBL 45, WL 208. REPAIRED BEAMS PER ER. 2L72 4F RTA16WE 20040301002302004030100230NM 2004 3 1 SWAA040476 120040215A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED IN AFT CARGO COMPARTMENT AT BS 767, RBL 8. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040301002332004030100233NM 2004 3 1 SWAA040479 120040215A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STRINGER 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040301002342004030100234NM 2004 3 1 SWAA040480 120040215A3350311500 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING FROM BULLNOSE AT 8D. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040301002352004030100235NM 2004 3 1 SWAA040481 120040215A5753KSBN8 BEARING BOEING737 7372H4 138448CNM LT WING WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING THRU FLIGHT CHECK, FOUND LINEAR MOVEMENT WHEN PUSHING UP ON LT INBOARD CARRIAGE ON OUTBOARD LT FLAP. REMOVED AND REPLACED LT NR 2 MID FLAP CARRIAGE SPHERICAL BEARING PER MM. 2L72 4F A16WE 20040301002382004030100238NM 2004 3 1 SWAA040444 120040212A76036555835 CABLE BOEING737 7372H4 138448CNM NR 2 ENGINE OUT OF ADJUST A SWAAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW29103SW 23109 ABORTED TAKEOFF, NR 2 THRUST LEVER MOVEMENT RESTRICTED. ADJUSTED NR 2 ENGINE THRUST REVERSER FOLLOW-UP CABLE PER MM. 2L72 4F A16WE 20040302000032004030200003WP 2004 3 2 AALA20040233 120040215A3350 SIGN DOUG DC9 DC983 3022083WP CABIN UNSERVICEABLE A AALAK NONE O OTHER ININSP/MAINT 1 SW21436AA 49454 DFW - LEFT HAND EMERGENCY LIGHT EXIT MARKER AT FORWARD OVERWING EXIT UNREADABLE. REPLACED LEFT HAND EMERGENCY LIGHT EXIT MARKER AT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040302000042004030200004NM 2004 3 2 SWAA040447 120040212A53126545819 PRESSURE PANEL BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND CRACK IN NOSE WHEEL WELL UNDER RT FWD NOSE PANEL BS 243. REPAIRED WEB PER EA. 2L72 4F A16WE 20040302000072004030200007NM 2004 3 2 SWAA040450 120040212A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND CORROSION ON WEB AT BS 1016, FWD SIDE OF BULKHEAD. REPAIRED WEB ER. 2L72 4F RTA16WE 20040302000092004030200009NM 2004 3 2 SWAA040452 120040212A53106546581 DOOR FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040302000102004030200010NM 2004 3 2 SWAA040453 120040212A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520 + 4, STRINGER 10R. REPAIRED FUSELAGE SKIN PER EA. 2L72 4F RTA16WE 20040302000122004030200012NM 2004 3 2 SWAA040426 120040210A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29086SW 22827 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 841, STRINGER 20L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040302000162004030200016NM 2004 3 2 SWAA040430 120040210A53116545815 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FRAME IN E/E COMPARTMENT CRACKED AT BS 344, BETWEEN STRINGERS 23L AND 24L. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040302000182004030200018NM 2004 3 2 SWAA040432 120040210A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND IN AFT CARGO COMPT STRINGER CLIP CORRODED AT BS727E, STRINGER 26R. REMOVED AND REPLACED STRINGER CLIP PER EA. 2L72 4F RTA16WE 20040302000202004030200020 2004 3 2 SWAA040434 420040210A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29769SW 30588 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040302000212004030200021NM 2004 3 2 SWAA040435 120040211A335065C27093 LIGHT BOEING737 7372H4 138448CNM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED AND IS PARTIALLY OUT OF RECEPTACLE. RESECURED LIGHT INTO RECEPTACLE PER MM. 2L72 4F A16WE 20040302000242004030200024NM 2004 3 2 SWAA040414 120040209A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 RED LENS MISSING FROM EEPLS AT OVERWING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20040302000252004030200025NM 2004 3 2 SWAA040415 120040209A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR OVERHEAD LIGHT PER MM. 2L72 4F A16WE 20040302000262004030200026NM 2004 3 2 SWAA040416 120040209A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 887 BETWEEN STRINGERS 20R AND STRINGER 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040302000282004030200028NM 2004 3 2 SWAA040418 120040209A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIP AT BS 807 STRINGER 26 R, CORRODED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040302000292004030200029NM 2004 3 2 SWAA040419 120040209A32116959886 FITTING BOEING737 7373H4 1384600NM LT AND RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT MLG FWD HANGER FITTINGS CORRODED. REPAIRED PER EA. 2L72 4F RTA16WE 20040302000302004030200030NM 2004 3 2 SWAA040420 120040209A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 480, STRINGER 4L AND BS 616, STRINGER 4R. REMOVED AND REPLACED TIE CLIP PER SRM. 2L72 4F RTA16WE 20040302000312004030200031NM 2004 3 2 SWAA040421 120040209A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040302000322004030200032NM 2004 3 2 SWAA040422 120040209A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040302000332004030200033 2004 3 2 SWAA040423 420040209A256563550 SLIDE BOEING737 7377H4 1384404NM L1,R1,R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29712SW 27846 DURING SCHEDULED C4 CHECK, FOUND R1, L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED ALL 3 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040302000342004030200034NM 2004 3 2 SWAA040424 120040208A575365464817 SPINDLE BOEING737 7372H4 138448CNM T/E FLAP BROKEN A SWAAK NONE F FLT CONT AFFECTED APAPPROACH 1 SW29086SW 22827 IN THE LANDING PHASE OF FLIGHT, WHEN FLAPS 30 WERE SELECTED, A LOUD POPPING/SNAPPING SOUND WAS HEARD, AND THE AIRCRAFT COMMENCED AN UNCOMMANDED ROLL TO THE RIGHT. NO ABNORMAL FLAP/LED INDICATIONS OBSERVED. 45 DEGREE YOKE DEFLECTION REQ'D TO LAND. FOUND OUTBOARD MID FLAP INBOARD CARRIAGE BROKEN AT SPINDLE. REMOVED FLAP ASSEMBLY, REMOVED AND REPLACED INBOARD CARRIAGE, INSPECTED OUTBOARD CARRIAGE VISUALLY, FOUND NO OTHER DAMAGE. REMOVED AND REPLACED SPINDLE AT INBOARD SIDE PER MM. 2L72 4F A16WE 20040302000352004030200035NM 2004 3 2 SWAA040364 120040205A53306545835 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKED AT NOSE WHEEL WELL, BOTH LT AND RT FORWARD ACCESS PANELS. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040302000362004030200036NM 2004 3 2 SWAA040365 120040205A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040302000372004030200037NM 2004 3 2 SWAA040366 120040205A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040302000392004030200039NM 2004 3 2 SWAA040368 120040205A57536546435 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20040302000402004030200040 2004 3 2 SWAA040369 420040205A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 R1 DOOR EVAC SLIDE LOOSE. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040302000432004030200043NM 2004 3 2 SWAA040372 120040205A53106547979 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CORRODED AT BS 948 TO BS 990 RBL 55, WL 208 CORRODED. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040302000452004030200045NM 2004 3 2 SWAA040257 120040127A335065C34691 LIGHT BOEING737 7373Y0 1384671NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 PASSENGER CABIN BULLNOSE EMERGENCY LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040302000462004030200046EU 2004 3 2 SWAA040258 220040126A7230332SW FAN BLADE BOEING737 7373H4 1384600NM CFMINTCFM56 CFM562AFR 13802EU ENGINE DAMAGED A SWAAE ENGINE SHUTDOWN E VIBRATION/BUFFET CLCLIMB 1 SW29386SW 26601 DECLARED EMERGENCY/AIR TURN BACK, INFLIGHT ENGINE SHUTDOWN. PASSING APPROX 8000 FEET, HEARD A POP AND FELT SLIGHT VIBRATION. ALL INSTRUMENTS SHOWED NORMAL. CLIMB SEEMED A LITTLE LOW FOR POWER SETTING. ISOLATED VIBRATION TO NR 2 ENGINE. REMOVED AND REPLACED NR 1 AND NR 2 FAN BLADE SETS PER MT. 2L72 4F4 FRTA16WE E21EU 20040302000482004030200048NM 2004 3 2 SWAA040260 120040127A3350PH22300L COVER BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 EEPLS FLOOR TRACK LIGHT COVER LOOSE AT ROW 8 DEF. REMOVED AND REPLACED EEPLS TRACK LIGHT COVER PER MM. 2L72 4F RTA16WE 20040302000512004030200051 2004 3 2 SWAA040263 420040127A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F A16WE 20040302000532004030200053WP 2004 3 2 AALA20040265 120040222A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - EMERGENCY EXIT SIGN AT AFT GALLEY EXIT DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT SIGN AT AFT GALLEY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000542004030200054WP 2004 3 2 AALA20040263 120040222A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - EMERGENCY EXIT SIGN AT RIGHT AND LEFT HAND OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY FOR EMERGENCY EXIT SIGN AT RIGHT AND LEFT HAND OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000552004030200055WP 2004 3 2 AALA20040268 120040222A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2173444 49470 DFW - EMERGENCY LIGHTS AT FORWARD ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000572004030200057WP 2004 3 2 AALA20040262 120040222A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - TAIL SECTION OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY FOR TAIL SECTION OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000582004030200058WP 2004 3 2 AALA20040269 120040223A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219677W 53627 STL - CEILING EMERGENCY LIGHTS AT ROWS 11 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACKS AT B5-102 AND B5-104 FOR CEILING EMERGENCY LIGHTS AT ROWS 11 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040302000592004030200059WP 2004 3 2 AALA20040270 120040223A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21571AA 49353 SEA - OVERHEAD EMERGENCY EXIT LIGHT IN AFT ENTRY AISLE INOPERATIVE. REPLACED BATTERY POWER SUPPLY AT B5-27 FOR OVERHEAD EMERGENCY EXIT LIGHTS IN AFT ENTRY AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040302000602004030200060NM 2004 3 2 AALA20040261 120040221A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21945AN 30085 SFO - EMERGENCY LIGHTING AT SEAT ROWS 7 THROUGH 10D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTING AT SEAT ROWS 7 THROUGH 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040302000612004030200061WP 2004 3 2 AALA20040266 120040222A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21553AA 53083 RDU - OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE AREA INOPERATIVE. RESEATED BATTERY AT POSITION B5-107 FOR OVERHEAD EMERGENCY LIGHTS AT AFT GALLEY SERVICE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000642004030200064WP 2004 3 2 AALA20040242 120040217A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217522A 49899 DFW - AFT EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000652004030200065WP 2004 3 2 AALA20040243 120040217A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217522A 49899 DFW - EMERGENCY PATH LIGHT ABOVE AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHT ABOVE AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000662004030200066WP 2004 3 2 AALA20040251 120040219A3350P4010051111 CONTROL MODULE DOUG DC9 DC982 3022082WP CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21424AA 49336 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FROM ROW 21 TO THE TAIL INOPERATIVE WHEN THE EMERGENCY LIGHT SWITCH IS IN THE ON POSITION. REPLACED THE BATTERY PACK AND CONTROL MODULE AB5-4 FOR THE EMERGENCY PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000672004030200067WP 2004 3 2 AALA20040252 120040219A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21424AA 49336 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 20D, 21D AND 28D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT 20D, 21D, AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000682004030200068WP 2004 3 2 AALA20040253 120040219A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21449AA 49475 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 4E INOPERATIVE. FOUND LOOSE CONNECTOR. RECONNECTED PLUG FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000712004030200071NM 2004 3 2 AALA20040226 120040209A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21654A 24612 MIA - EMERGENCY LIGHT AT L4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040302000732004030200073WP 2004 3 2 AALA20040260 120040221A3350 RELAY DOUG DC9 DC982 3022082WP CABIN FAILED A AALAK NONE J WARNING INDICATION ININSP/MAINT 1 SW21485AA 49678 SLC - BATTERY CHARGER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. REPLACED BATTERY CHARGER/BATTERY AND RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000772004030200077NM 2004 3 2 AALA20040257 120040220A3350 BATTERY PACK BOEING767 767223 1385123NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21302AA 22308 MIA - EMERGENCY LIGHT AT ROWS 16D AND 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 16D AND 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040302000792004030200079WP 2004 3 2 CALA0400143 120040220A5313S27779225 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2735832 49492 INSPECTION FOUND LONGERON 30 CORRODED FORWARD OF SPLICE IN FORWARD BAGGAGE BIN BETWEEN STA 484 AND 503. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A SPLICE AND LONGERON SECTION WERE INSTALLED IAW SRM 53-02, FIGURE 18. 2L72 4F A6WE 20040302000802004030200080NM 2004 3 2 CALA0400144 120040220A53206546586524 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND AFT PRESSURE BULKHEAD LOWER WEB AND STIFFENER CORRODED JUST AFT OF FS 1016, S23L. REPAIRED IAW ECRA 5311-01186. 2L72 4F RTA16WE 20040302000842004030200084NM 2004 3 2 CALA0400148 120040221A5330146N3531 SKIN BOEING757 757224 1384958NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717104 27294 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 1620-1640, S21R, JUST BELOW AND FORWARD OF R-3 DOOR. A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 214. A DIP WAS ISSUED TO INSPECT FASTENERS EVERY 1,000 FLIGHT CYCLES AND TO PERFORM A PERMANENT REPAIR AT 3,000 FLIGHT CYCLES. 2L72 4F RTA2NM 20040302000882004030200088NM 2004 3 2 CALA0400137 120040219A532065479573 WEB BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723657 28918 INSPECTION FOUND THE C-2 DOOR THRESHOLD WEB CORRODED. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040302000892004030200089NM 2004 3 2 CALA0400138 120040219A5210141A61501 SKIN BOEING737 737724 13844BYNM L1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR SKIN EDGE AT LOWER HINGE CUTOUT. THE DOOR SKIN WAS REPAIRED IAW ECRA 5210-01745. 2L72 4F RTA16WE 20040302000942004030200094NM 2004 3 2 CALA0400152 120040223A5320149A761415 STRUCTURE BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND A .75 INCH CRACK IN LOWER CHORD ON O/B WEB OF RT WHEEL WELL RING. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040302000962004030200096NM 2004 3 2 CALA0400154 120040223A5320149A761415 STRUCTURE BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND A 1 INCH CRACK IN LT MLG WHEEL WELL FAIRING ASSEMBLY O/B LOWER CHORD. THE CHORD WAS REMOVED AND REPLACED IAW EA 5310-04230. 2L72 4F RTA16WE 20040302000982004030200098NM 2004 3 2 CALA0400156 120040223A5510 ATTACH FITTING BOEING737 737524 1384721NM HORIZ STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723657 28918 INSPECTION FOUND HORIZONTAL STABILIZER FORWARD RIGHT LOWER ATTACH LUG GOUGED BY CLEVIS PIN FROM LOWER RIGHT SLIDER. THE GOUGE WAS BLENDED, FLAP PEENED, TREATED AND PRIMED IAW SRM 55-10-10 AND 51-20-06. 2L72 4F RTA16WE 20040302001002004030200100NM 2004 3 2 CALA0400158 120040223A5510180A16122 PIN BOEING737 737824 13844BZNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER PIN AND RT HORIZONTAL STABILIZER AFT MIDDLE PIN CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696A. 2L72 4F RTA16WE 20040302001012004030200101NM 2004 3 2 CALA0400159 120040223A5510180A16121 PIN BOEING737 737824 13844BZNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER PIN AND RT HORIZONTAL STABILIZER AFT UPPER PIN CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696A. 2L72 4F RTA16WE 20040302001032004030200103NM 2004 3 2 CALA0400129 120040217A5210141A6185 SKIN BOEING737 737724 13844BYNM L1 DOOR PEELING A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND THE UPPER RIGHT CORNER OF L-1 DOOR SKIN PEELING OFF. THE DOOR SKIN WAS REPAIRED IAW ECRA 5210-01744. 2L72 4F RTA16WE 20040302001042004030200104WP 2004 3 2 CALA0400130 120040217A5220 CABLE DOUG DC9 DC982 3022082WP TAILCONE OUT OF RIG A CALAK NONE O OTHER ININSP/MAINT 1 SW2735832 49492 THE TAIL CONE WOULD NOT DEPLOY USING AFT ENTRY DOOR HANDLE. THE TAIL CONE CABLES WERE RIGGED IAW MM 53-53-00. 2L72 4F A6WE 20040302001062004030200106NM 2004 3 2 CALA0400132 120040217A53306545775 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 875 BELOW S19R AFT OF C-2 DOOR. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 210. 2L72 4F RTA16WE 20040302001072004030200107NM 2004 3 2 CALA0400133 120040217A5320BAC1509100146705CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND AFT CARGO PIT RIGHT Z-CHANNEL CORRODED AT STA 760. THE Z-CHANNEL WAS REPAIRED IAW SRM 53-00-53, REPAIR 5. 2L72 4F RTA16WE 20040302001132004030200113EA 2004 3 2 COMA0460159 120040221A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01810CA 7370 FLIGHT 5706 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040227000192004022700019NM 2004 2 27 ASAA0410029 120040113A53156554896 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 847, RIGHT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 61 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040227000282004022700028WP 2004 2 27 GTIA040042 120040130A3220 LANDING GEAR DOUG DC9 DC982 3022082WP NLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23812NK 48021 PBI - FLT 833 - AFTER TAKEOFF, THE NOSE GEAR FAILED TO RETRACT. CYCLED GEAR DOWN, NOSE GEAR GREEN LIGHT ON INSTANTLY. RECYCLED GEAR UP. NOSE GEAR FAILED TO RETRACT. ABOUT 3 TO 4 MINUTES LATER THERE WAS A POP AND THE NOSE GEAR RETRACTED. AIRSPEED WAS MAINTAINED AT APPROX 180K THROUGH THIS. GEAR OPERATED NORMAL ON EXTENSION AT PBI. INSPECTED NOSE GEAR DID NOT FIND ANYTHING EXCEPT EXCESSIVE DIRTY GREASE AROUND BUNGIE CYL ROD END AND SWIVEL AREA. CLEANED OFF EXCESSIVE GREASE AND DEGREASED BUNGIE CYL. REGREASED STRUT AND JACKED NOSE GEAR. SWUNG GEAR MANY TIMES WITHOUT FAILURE, A/C OK FOR CONT SERVICE. (M) 2L72 4F A6WE 20040227000322004022700032NM 2004 2 27 ASAA0410028 120040113A532065671405 FLOOR SUPPORT BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOOR SUPPORT AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 24 CORRODED. REPAIRED FLOOR SUPPORT PER EA. (M) 2L72 4F A16WE 20040227000372004022700037WP 2004 2 27 GTIA040037 120040106A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND FORWARD PIT CEILING WEB CRACKED AT LAV DUMP FORWARD FEED THROUGH STATION 225 LBL 52. STOP DRILLED CRACK. FABRICATED WEB REPAIR DOUBLER. INSTALLED WEB REPAIR. (M) 2L72 4F RTA6WE 20040227000382004022700038 2004 2 27 GTIA040043 420040201A2565 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 MCO - FLT 1913 - L1 SLIDE FELL OUT OF DOOR PANEL. RE-INSTALLED L1 SLIDE PACK AND COVER. (M) 2L72 4F RT 20040227000432004022700043WP 2004 2 27 GTIA040044 120040127A2611 SMOKE DETECTOR DOUG DC9 DC983 3022083WP LAVATORY MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23815NK 49415 LAS - FLT 1108 - RETURN TO LAS, SMOKE IN CABIN AND LAVATORY ALARMS WENT OFF. INSPECTED CARGO BINS, TAIL CONE AREA AND CABIN, NO DEFECTS NOTED. RAN ENGINES NO DEFECTS NOTED. OPERATED PACKS NO DEFECTS NOTED, INSPECTED COALESCER SOCKS. NO DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040227000512004022700051WP 2004 2 27 GTIA040024 120040107A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FS DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD, RIGHT STATION 767-787 HAS MISSING EDGE FILLER, DAMAGED INSERTS, PEELING FIBERGLASS. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040227000522004022700052NM 2004 2 27 ASAA0410044 120040129A322065737622 LANDING GEAR BOEING737 7372Q8C 138448SNM NLG ICED A ASAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM01741AS 21959 ANC - DURING CLIMB-OUT KODIAK NOSE GEAR UNSAFE LIGHT INDICATION WAS OBSERVED AND NOSE GEAR DROPPED WITH GEAR HANDLE IN 'OFF' POSITION. REMOVED ICE FROM NOSE LANDING GEAR SKIN AREA, THEN LANDING GEAR, OPS CHECK NORMAL. (M) 2L72 4F A16WE 20040227000752004022700075EU 2004 2 27 BAQA092354 120040121A77141179406101 CONTROL UNIT BOLKMS117 BK117A1 5626010EU RPM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME6694 7243 ENGINE LOW WARNING LIGHT AND CHIME NOT WORKING. REPLACED WITH SERVICEABLE UNIT. 01/26/2004 1G72 3U H13EU 20040227000762004022700076EU 2004 2 27 BAQA092251 120040121A6410365A12002004 BLADE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY282 6529 TAIL ROTOR BLADE SUSPECTED TO BE CRACKED. HARDCARDS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 01/27/2004 1G72 3U3 U H10EU E19EU 20040227000872004022700087NM 2004 2 27 373PA0041 120040202A5320 GUSSET BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 AFT GUSSET CRACKED BETWEEN AIRSTAIR AND FUSELAGE DOOR CUTOUT. REPAIRED IAW SRM 53-10-15. 2L72 4F RTA16WE 20040227000882004022700088NM 2004 2 27 373PA0042 120040202A5315 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05373PA 23749 FLOORBEAM CORRODED AT BS 1006 RBL 14 AT SCREW HOLE. REPAIRED IAW SRM 53-00-51. 2L72 4F RTA16WE 20040227000922004022700092EA 2004 2 27 COMA0470012 120040127A5230 DOOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY OPEN A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO0110108 10108 FLIGHT 5289 AIRCRAFT WOULD NOT PRESSURIZE, HEARD RUMBLING NOISE FROM FLOOR AREA. FOUND CARGO DOOR OPEN, INSPECTED FOR DAMAGE AND CLOSED CARGO DOOR. 2L72 4F RTA21EA 20040227000972004022700097SO 2004 2 27 C2XA04SH019 120040117A531314528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714923 145318 DURING C CHECK THE T-REINFORCEMENT ON STRINGER 19 RT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040301000022004030100002NE 2004 3 1 JYD2004F00002 120040122A64206516100010041 ROTOR HEAD SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE TAIL ROTOR CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09194AC581 64017 DURING NORMAL AC INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET IS CRACKED 1.8125 INCH FROM THE TRAILING EDGE AND .25 INCH FROM THE TIP END. THE CRACK IS RUNNING SPAN WISE AND IS 6875 INCH LONG. PROBABLE CAUSE UNKNOWN. (MDR04-042) 2G72 4U4 U H4EA E15EA 20040301000262004030100026EU 2004 3 1 PG92004F00004 120040108A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TAIL ROTOR FAILED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19170PA 2637 TAIL ROTOR BEARING FAILED WITH ONLY 354 HOURS. (K) 1G71 3U H9EU 20040301000892004030100089EA 2004 3 1 F03050 120040123A5220 DOOR CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE EMERGENCY EXIT OUT OF ADJUST A FDKAO OTHER N FALSE WARNING CRCRUISE 1 SW07903FJ 15003 CREW REPORTED LT AFT EMERGENCY DOOR CAUTION LIGHT CAME ON DURING FLIGHT. THE MECHANIC CREW REPOSITION THE DOOR. OPS CHECKED GOOD. CONTROL NR 111418. 2L72 4F4 FRTA21EA E15NE 20040301000972004030100097NM 2004 3 1 GAIA04009OP 120040130A3150G6111 RELAY BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE WARNING HORN INOPERATIVE A GAIAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 SW07936PG 22441 DURING TAXI OUT, IT WAS DISCOVERED THAT THE TAKE OFF WARNING HORN WOULD NOT TEST. REMOVED AND REPLACED THE TIME DELAY RELAY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040301001032004030100103CE 2004 3 1 GLBA20030560 120040209A27101295210471 CONTROL CABLE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT AILERON FRAYED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03254GL UE254 LT AILERON CABLE FRAYED BETWEEN WS 124.58 AND 147.74 (LT WHEEL WELL), REMOVED AND REPLACED LT AILERON WING CABLE. OPS CK AND RIG CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040301001122004030100112EA 2004 3 1 SIMA200402602 120040124A3350 BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE EMERGENCY LIGHTSFAILED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21506AE 10056 EMERGENCY LIGHTS FAILED TO ILLUMINATE. RAI EMERGENCY BATTERY POWER PACKS NR 1 PN OFF 20131A SN OFF 12527, RAI NR 2 EMERGENCY BATTERY POWER PACK NR OFF 20131A SN OFF 74856. RAI NR 3 EMERGENCY BATTERY POWER PACK PN OFF 20131A SN OFF 74715. RAI NR 4 EMERGENCY BATTERY POWER PACK PN OFF 20131A SN OFF 74539, OPS CHECK GOOD. (SW21200403421) 2L72 4F4 FRTA21EA E15NE 20040301001182004030100118SO 2004 3 1 JGV2004F00001 120040129A34111159EL20500 PITOT LINE GULSTMG1159 G1159B 3953535SO RROYCESPEY SPEY50614 54519EU FS67.0-180.0 BROKEN B JGVRK NONE O OTHER ININSP/MAINT 1 CE0924YS 016 ORIGINAL PITOT/STATIC TUBING AND PLASTIC FITTINGS BRITTLE AND EASILY BROKEN. MOVING TUBING OR EVEN WIRE BUNDLES TOUCHING TUBING CAUSES LEAKS. THIS IS DUE TO ITS OLD AGE. IT NEEDS TO BE REPLACED WITH A NEWER, MORE FLEXIBLE TUBING. 2L72 4F4 FRTA12EA E2EU 20040301001352004030100135WP 2004 3 1 DHL2004806561 120040124A5751 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RT AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 ITEM REF. NR. 1305: RT IB AILERON L/E WITH 1.500 CRACK AROUND FASTENER HOLE STA XA 502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN (7075-T6AL 0.040) CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INNER SIDE. APPLIED PRC SEALANT TO FAYING SURFACES, INSTALLED NEW SKIN. FOR REBALANCING SEE NR 2427. 2L74 4F4 FRT4A25 E2GL 20040301001412004030100141NE 2004 3 1 58184 220040123A73141143890425 PUMP BEECH 1900 1900D 1154162CE PWA PT6 PT6A67 52043NE FUEL SYSTEM LEAKING A AMWAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 CE0713ZV UE13 AFTER ARRIVAL, CREW FOUND FUEL LEAK IN THE LT NACELLE AREA. REMOVED AND REPLACED LOW PRESSURE FUEL PUMP (PUMP, FUEL BOOST-LOW PRESS ENGINE D) P/N 143890425, S/N B-314. 2L72 4T4 TRTA24CE E26NE 20040301001432004030100143NM 2004 3 1 QXEA200400135 120040212A27113978001007 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 600 MALFUNCTIONED A QXEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM09409QX5177 4051 PDX FLIGHT NR 2417, ONCE AFTER TAKE OFF AND ONCE ENROUTE, AILERON TRIM WENT FULL SCALE RT WING DOWN. AUTO PILOT WAS ON BOTH TIMES. SELECTED AUTO PILOT OFF DID NOT HAPPEN AGAIN. REPLACED TRIM CONTROL PANEL AND TRIM ACTUATOR. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040301001452004030100145EA 2004 3 1 58159 220040122A73203032791 FUEL CONTROL BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT ENGINE LEAKING A AMWAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 CE07132YV UE132 CREW REPORTED FUEL LEAK LT NACELLE. REMOVED AND REPLACED LT FCU HIGH PRESSURE FUEL TUBE WHICH ATTACHES AFT SIDE OF FUEL FLOW TRANSMITTER. OPS CK NORMAL P/N 3032791. 2L72 4T3 TRTA24CE E2NE 20040301001482004030100148EU 2004 3 1 DHL2004365515 120040107A5347 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH 149 MAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 APPROX. RBL77 HAS SEVERAL SPOTS OF CORROSION. REMOVED ALL CORROSION POINTS AT SEAT TRACKGOES BETWEEN FRAME 20 AND 26 RBL77 FOUND AREA OUT OF LIMITS IAW A300 SRM 51-40-11 AND 53-10-00. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION IAW A300 SRM 51-40-12/51-30-30/51-10-40. SEAT TRACK P/N TMS 60-22457-7075T6511 LONG 13.5' PO 23488101. 2L72 4F4 FRTA35EU E23EA 20040301001662004030100166NM 2004 3 1 2004UALA00106 120040208A2120 ODOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29215UA 30221 FA REPORTED RUBBER BURNING ODOR NEAR 2L. THE REPORT OF BURNING ODOR WAS ON A FLT FROM SFO TO OGG. PROBLEM COULD NOT BE DUPLICATED AT OGG: OGGMM RAN MID GALLEY POWER, OVEN, CHILLERS, AND UPR & LWR RECIRCULATION FANS, CHECKED MID GALLEY CEILING, BUT NOTED NO BURNING ODOR OR SMOKE. AIRCRAFT RETURNED TO REVENUE SERVICE WITHOUT FURTHER SMOKE OR ODOR REPORTS. 2L72 4F4 FRTT0001SE E46NE 20040301001672004030100167EU 2004 3 1 2004UALA00107 120040206A3234 LEVER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29412UA 465 WHILE TRYING TO DROP GEAR ON APPROACH, ECAM MSG SHOWED LGCIU 1 AND 2 FAILURE. THIS WAS A POSITIONING FLIGHT. REPLACED LANDING GEAR LEVER. 2L72 4F4 FRTA28NM E40NE 20040301001702004030100170NM 2004 3 1 2004UALA00111 120040209A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY EXIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29650UA 25287 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE, 4TH LIGHT AFT OF OVERWING, LT SIDE. RELAMPED. CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20040301001972004030100197NM 2004 3 1 AALA20040229 120040213A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21659AA 24617 DFW - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 9 TO 15 INOPERATIVE. REPLACED SOCKET AT ROW 9 FOR EMERGENCY ESCAPE PATH LIGHTING FOR ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040301002002004030100200WP 2004 3 1 AALA20040230 120040214A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217546A 53028 DEN - AFT UPPER EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR AFT UPPER EMERGENCY LIGHTS BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040301002052004030100205WP 2004 3 1 AALA20040238 120040216A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217538A 49992 ATL - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040301002142004030100214NM 2004 3 1 SWAA040460 120040213A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND FUSEKAGE SKIN CRACK AT BS 520 + 4, STRINGER 10R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040301002162004030100216NM 2004 3 1 SWAA040462 120040213A5330 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR FRAME CUTOUT FORWARD LOWER HINGE INNER DOUBLER CRACKED. REMOVED AND REPLACED L1 DOOR CUTOUT DOUBLER PER SRM. 2L72 4F RTA16WE 20040301002322004030100232NM 2004 3 1 SWAA040478 120040215A3350101114 LAMP BOEING737 7373Q8 1384670NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040301002402004030100240NM 2004 3 1 SWAA040446 120040212A32601899 UPLOCK SENSOR BOEING737 7373H4 1384600NM LT MLG MALFUNCTIONED A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29352SW 24888 AIR TURNBACK, LT MLG (RED) LIGHT FAILED TO EXTINGUISH WITH GEAR IN THE UP POSITION. REMOVED AND REPLACED M988 CARD AND REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20040302000082004030200008NM 2004 3 2 SWAA040451 120040212A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 440 STRINGER 4R, AND BS 380, STRINGER 2L. REMOVED AND REPLACED STRINGER CLIPS SECTION PER SRM. 2L72 4F RTA16WE 20040302001142004030200114EA 2004 3 2 COMA0460160 120040222A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01810CA16207 7370 FLIGHT 5700 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20040302001152004030200115EA 2004 3 2 COMA0470024 120040217A3260 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA RT MLG FAULTY A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01331CA 10061 FLIGHT 9490 DURING CRUISE FLIGHT RECEIVED A GEAR DISAGREE CAUTION ASSOCIATED WITH A PROXIMITY SYSTEM FAULT AND MLG FAULT, CREW DECLARED AN EMERGENCY AND LANDED AT CVG SAFELY. REPLACED FAULTY CONNECTOR P614 FOR THE RIGHT MLG PROXIMITY SENSOR PX18. 2L72 4F RTA21EA 20040302001162004030200116EA 2004 3 2 COMA0470025 120040220A2781 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01379CA 10102 FLIGHT 5072 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER, OPERATION OF SLATS NORMAL. 2L72 4F RTA21EA 20040302001212004030200121WP 2004 3 2 DHL2004873003 120040210A2730 SPRING ASSY DOUG DC8 DC873F 302199FWP ELEVATOR DEFECTIVE A DHLAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO01873SJ 46091 DURING TAKEOFF, TAKEOFF TRIM SETTING OF 4.1 INITIAL ROTATION NORMAL AFTER GEAR RETRACTION ACFT PITCHED UP SLOWLY TO 20 DEG. PITCH UP & WAS REQUIRED TO PUT FWD PRESSURE ON CONTROL WHEEL TO APPROX 1.5 UNITS OF TRIM, LANDED WITH 4.0 UNITS OF TRIM. PERFORMED ELEVATOR CHECK. RIG CHECKED BOOST TABS, CONTROL TABS, PTC & LOAD FEEL MECHANISM. FOUND ELEVATOR CONTROL TABS OUT OF RIG. CORRECTED RIGGING. AFTER ROTATION A/C REQUIRED 1.2 DEG FORWARD TRIM TO HOLD V2+10. T/O TRIM SETTING 3.2, STABILIZED SETTING 2.0, CRUISE SETTING 2.0 AT 280 KIAS, APPROACH 3.0 AT 145 KIAS, LANDING 4.8 AT 129 KIAS. REMOVED & REPLACED ELEVATOR LOAD SPRING ASSY. AFTER REPLACEMENT OF ELEVATOR FEEL MECH, SYS CHECKS SERVICEABLE. 2L74 4F RT4A25 20040302001272004030200127NM 2004 3 2 SWAA040363 120040203A53306545700 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS AT FOLLOWING, BS 320, STRINGER 19R, BS 538, BETWEEN STRINGERS 2R AND 3R, BS1011, STRINGER 23R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040302001282004030200128 2004 3 2 SWAA040264 420040127A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040302001302004030200130NM 2004 3 2 SWAA040266 120040127A53116545811 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 320, LBL 53, WL 181. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040302001332004030200133 2004 3 2 SWAA040270 420040127A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1/R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM. 2L72 4F RTA16WE 20040302001382004030200138NM 2004 3 2 SWAA040275 120040128A256065C168209 HOOK BOEING737 7373H4 1384600NM L2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE HOOK LOOSE. REMOVED AND REPLACED FASTENERS SECURING SLIDE CONTAINER PER MM. 2L72 4F RTA16WE 20040302001412004030200141 2004 3 2 SWAA040278 420040128A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040302001432004030200143NM 2004 3 2 SWAA040280 120040128A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040302001472004030200147NM 2004 3 2 SWAA040297 120040130A335065C27095 BATTERY PACK BOEING737 7373Q8 1384670NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SPECIAL VISIT AT SAT AEROSPACE, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040302001482004030200148NM 2004 3 2 SWAA040298 120040130A2121215201 GASPER FAN BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29606SW 27926 AT CRUISE FL 35, FLIGHT ATTENDANTS REPORTED A METALLIC SMELL AT MID CABIN. TURNED GASPER FAN OFF SMELL IMPROVED. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20040302001522004030200152NM 2004 3 2 SWAA040302 120040130A5320BAC1503 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STIFFENER CORRODED IN MAIN WHEEL WELL, BS 663 TO BS 676, RBL 27. REMOVED AND REPLACED STIFFENER SECTION PER SRM. 2L72 4F RTA16WE 20040302001552004030200155NM 2004 3 2 SWAA040305 120040130A256065C19901 CABLE BOEING737 7373H4 1384600NM L2/R2 DOORS MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES CABLES MISROUTED. REROUTED BOTH DOOR EVAC SLIDE CABLES PER MM. 2L72 4F RTA16WE 20040302001562004030200156NM 2004 3 2 SWAA040306 120040130A57536546435 SKIN BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C2 CHECK, FOUND RT WING RT OUTBOARD AFT T/E FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040302001592004030200159NM 2004 3 2 SWAA040309 120040130A575465C26686 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED C3 CHECK, FOUND NR 1 L/E SLAT SKIN CRACKED OUTBOARD END. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040302001612004030200161NM 2004 3 2 SWAA040311 120040130A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040302001642004030200164NM 2004 3 2 SWAA040314 120040130A53116546658 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 907, STRINGER 9L. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040302001652004030200165NM 2004 3 2 SWAA040315 120040130A3350101114 LIGHT BOEING737 7375H4 138449DNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY AISLE LIGHT AT 4 DEF INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040302001662004030200166NM 2004 3 2 SWAA040316 120040130A53116546539 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME INBOARD CHORD CRACKED AT BS 616, RBL 64, WL 202. REMOVED AND REPLACED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040302001682004030200168NM 2004 3 2 SWAA040318 120040130A53116546555 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 867, STRINGER 9R. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040302001702004030200170NM 2004 3 2 SWAA040320 120040130A53116546549 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 767, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040302001732004030200173 2004 3 2 SWAA040376 420040207A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR MALFUNCTIONED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 L1 DOOR EVAC SLIDE PARTIALLY DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040302001792004030200179NM 2004 3 2 SWAA040382 120040207A256065C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20040302001802004030200180NM 2004 3 2 SWAA040383 120040207A3350101073 LENS BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040302001812004030200181NM 2004 3 2 SWAA040384 120040207A53116546552 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CORRODED AT BS 847, RBL 30 TO RBL 45. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040302001822004030200182NM 2004 3 2 SWAA040385 120040207A57126545445 RIB BOEING737 7373Y0 1384671NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND RT WING WBL 135, RIB LOWER CHORD CRACKED. REPAIRED CHORD PER ER. 2L72 4F RTA16WE 20040302001892004030200189NM 2004 3 2 SWAA040392 120040207A57536546434 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED PM CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20040302001952004030200195NM 2004 3 2 SWAA040398 120040207A533065618420 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT NLG WHEEL WELL BS 245.5, BELOW LT PRESSURE PANEL. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040302001972004030200197SO 2004 3 2 C2XA04SH108 120040226A532014524119007 SUPPORT EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 DURING C CHECK THE MAIN DOOR THRESHOLD SILL SUPPORT WAS FOUND TO BE CORRODED AT FRAME 15 TO 18 AND STRINGER 15 LT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL SUPPORT IAW AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040302001992004030200199SO 2004 3 2 C2XA04SH112 120040226A531514521700003 FLOORBEAM EMB 145 EMB145 3260210SO ALLSN AE3007AE3007C GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040302002002004030200200SO 2004 3 2 C2XA04SH072 120040220A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040303000012004030300001 2004 3 3 MEX2004028 420040121A3443026949 VANE DOUG MD88 MD88 3023688NM NR 2 ENGINE FAILED W ASMZO OTHER O OTHER NRNOT REPORTED 1 SW23160PL 49763 AC RETURN TO PLATFORM, AFTER ENGINES STARTING APPEARED (IRS NR 1 NO AIR IN EOAP) MESSAGE. AT PLATFORM IRU BREAKER WAS RESET BUT FAIL CONTINUE FAN VANE IRS NR 1 WAS REPLACED IAW MM-34-43-00, TESTS CORRECT. 2L72 4F RTA6WE 20040303000092004030300009NM 2004 3 3 F3LA200400013 120040213A2120 SMOKE AIRBUSA319 A319111 3930336NM COCKPIT DETECTED A F3LAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM03920FR 1997 AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN SHORTLY AFTER TAKEOFF, JUST AFTER APU BLEED WAS TURNED OFF. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH MM 71-00-00-810-802. PERFORMED OPS CHECK AND COULD NOT DUPLICATE DISCREPANCY ON GROUND. PERFORMED TEST FLIGHT. PERFORMED NORMAL BLEED-OFF TAKEOFF AND REINSTATED BLEED CONFIGURATION IAW NORMAL TAKEOFF/CLIMB PROCEDURES. MONITORED CABIN AND COCKPIT FOR SMOKE, MIST INDICATIONS. CHECKED NORMAL, NO DISCREPANCIES FOUND. 2L72 4F RTA28NM 20040303000122004030300012EA 2004 3 3 COMA0460148 120040216A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR ILLUMINATED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01986CA 7174 FLIGHT 5499, GEAR DISAGREE WARNING. CLEANED ICE FROM LANDING GEAR. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040303000162004030300016WP 2004 3 3 0390 120040217A57515719161501 HINGE FITTING DOUG DC8 DC863F 302198FWP LT AILERON CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 VISUALLY DETECTED LT OB AILERON CENTER HINGE FITTING CRACKED. 2L74 4F 4A25 20040303000202004030300020NM 2004 3 3 CALA0400128 120040217A532065528962 CHANNEL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724633 27901 INSPECTION FOUND A 1 INCH CRACK IN FLOORBOARD CHANNEL AT STA 537.45, BL 0 TO RBL 14. THE FLOORBOARD CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040303000212004030300021NM 2004 3 3 AWXA200400179 120040214A33971012721 WIRE BOEING737 737277 1384570NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING INSPECTION A BROKEN WIRE WAS FOUND ON THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 17 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040303000222004030300022NM 2004 3 3 AWXA200400180 120040215A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 35 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 DURING 8-DAY CHECK, MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 35 LT INOPERATIVE. REPAIRED BROKEN WIRE FOR THE EMERGENCY ESCAPE PATH LIGHT UNDER SEAT ROW 35 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040303000232004030300023EU 2004 3 3 AWXA200400182 120040214A5321D5367004100000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 DURING C-04 CHECK RT OB CABIN FLOOR PANEL (252VF) WAS FOUND DELAMINATED BETWEEN FR 60 AND FR 64, RBL 46 TO RBL 65. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL (252VF); FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG D53670041; INSTALLED NEW PANEL IAW A320 SRM 53-02-00, FIG. 209, PG. 233-236. 2L72 4F RTA28NM 20040303000242004030300024WP 2004 3 3 0479 120040217A572037048411 FITTING DOUG DC8 DC863F 302198FWP LT WING CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING FUEL TANK MAINTENANCE DETECTED LT WING NR 2 MAIN FUEL TANK CRACKED STRINGER END FITTING AT STA.XRS 78,S61. 2L74 4F 4A25 20040303000252004030300025WP 2004 3 3 GKZR200482304 120040217A5710 STRUCTURE DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 LT WING INSIDE NR 1A FUEL TANK FROM ACCESS PANEL 505B BETWEEN STA. 495.665 AND 508.977 LWR STRINGER NR 53 CRACKED. CUT AND REMOVED STRINGER NR 53 BETWEEN STA 495 AND 508 IAW DC-8 SRM 57-2-2. CUT AND INSTALLED REPLACEMENT STRINGER AND SPICES IAW DC-8 SRM 57-2-2. (CLOSED) 2L74 4F4 FRT4A25 E2GL 20040303000262004030300026NM 2004 3 3 QXEA200400153 120040208A2810 FUEL TANK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE RT WING LEAKING A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09356PH14505 502 FOUND FUEL LEAKING FROM OB SIDE OF NR 2 COWLING. MAINTENANCE INSPECTED AND FOUND THE LEAK TO BE COMING FROM THE BOTTOM OF THE WING BOX, AFT OF STATION YW 171.2. MAINTENANCE LOCATED THE SPECIFIC AREA OF THE LEAK AND APPLIED SEALANT TO THE SAME. THE FUEL TANK WAS FUELED, BOOST PUMPS WERE RUN AND NO LEAKS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040303000282004030300028WP 2004 3 3 MWEA040017 120040216A57305935852513 PANEL DOUG DC9 DC982 3022082WP WING CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 TOP PANEL IS CRACKED ON HORIZONTAL FLANGE. REMOVED AND REPLACED WITH FABRICATED TRAPEZOID PANEL. 2L72 4F A6WE 20040303000292004030300029NM 2004 3 3 P5CA0401035 120040203A573065B145967 PANEL BOEING747 7472D3B 1384805NM GE CF6 CF650* 30018NE LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23505MC 21251 LT WING UPPER LE PANEL CRACKED ON UPPER SURFACE (APPROX 30 INCHES,) LWR OB SURFACE HAS A 25 INCHES CRACK AND IS DISBONDED. PANEL REPLACED DURING FA-06 CHECK - NON-ROUTINE WORKCARD (T-160) NR 0034 REF. 2L74 4F4 FRTA20WE E23EA 20040303000332004030300033 2004 3 3 P5CA0401039 420040216A34182566A30A SENSOR BOEING747 747341 13848AMNM AOA FAILED A P5CAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 WP23355MC 23395 ON TAKEOFF AND TO CRUISE ALT 31.0, STICK SHAKER ON. RESET C/B, NO CHANGE. SHAKER STOPPED AT FL 31.0, AT CRUISE MACH, SAME ON APPROACH. REMOVED AND REPLACED AOA SENSOR, LT, IAW MM 27-37-01. OPS CK NORMAL. 2L74 4F RTA20WE 20040303000352004030300035WP 2004 3 3 0354 120040217A71102360006501 DUCT DOUG DC8 DC863F 302198FWP NR 2 ENGINE DELAMINATED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 769221414 46088 NR 2 ENGINE LT ENGINE COWL TRANSITION DUCT DELAMINATED ON INBOARD SIDE. 2L74 4F 4A25 20040303000432004030300043 2004 3 3 BAQA092515 420040203A34516226263001 TRANSCEIVER LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP DME SYS INOPERATIVE B BAQAK NONE O OTHER ININSP/MAINT 1 EA0340DK 2241 092 DME HAS AUDIO TONE ON ALL THE TIME. REPLACED WITH SERVICEABLE UNIT. 02/04/2004 2L72 4F4 F A10CE E6WE 20040303000452004030300045 2004 3 3 BAQA092463 420040129A3420501121001 GYRO AGUSTAA109 A109E 0260119EU COCKPIT INTERMITTENT B BAQAK NONE O OTHER ININSP/MAINT 1 EA03109UP222 11061 GYRO INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 02/04/2004 1G72 3U RTH7EU 20040303000492004030300049EA 2004 3 3 VNAA0402005 120040211A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT ACTIVATED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL07226JS 7895 IN FLIGHT, THE CREW RECEIVED A RIGHT HAND EMERGENCY DOOR CAS MESSAGE. AIRCRAFT PRESSURE STAYED NORMAL. MAINTENANCE CONTROL, WITH THE CREW, THEN DEFERRED THE DOOR WITH 52-70-03 CAT C. 2L72 4F4 FRTA21EA E15NE 20040303000612004030300061 2004 3 3 BAQA092602 420040211A3420501121001 GYRO AGUSTAA109 A109E 0260119EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109UP1452 11061 OFF FLAG STAYS IN VIEW. REPLACED WITH SERVICABLE UNIT. 02/16/2004 1G72 3U RTH7EU 20040303000632004030300063NM 2004 3 3 VNAA0402003 120040208A5270 SWITCH DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE GROUND/AIR DOOR DIRTY A VNAAO OTHER N FALSE WARNING CLCLIMB 1 GL07423JS 3032 DURING FLIGHT, THE CREW RECEIVED A GROUND AIR DOOR WARNING DURING CLIMBOUT AND RETURNED TO PIT. MAINTENANCE INSPECTED, CLEANED AND ACTUATED THE DOOR SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040303000662004030300066EU 2004 3 3 BAQA092645 120040206A77120177987030 CONTROL UNIT UROCOPEC135 EC135T1 5620026EU ENG TORQUE INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1226 0143 CONTROL UNIT INTERMITTENT, TQCNF/EXT THROUGH ECU ON NR 2 ENGINE. REPLACED BY SERVICEABLE UNIT. 02/11/2004 1G72 3U H88EU 20040303000682004030300068EU 2004 3 3 BAQA092647 120040202A249745043006 MASTER BOX UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03603ME115 0284 ELECTRICAL MASTER BOX CAME INSTALLED ON NEW AIRCRAFT N603ME/0284 AND FAILED AFTER 115.3 HOURS. REPLACE WITH SERVICABLE UNIT FROM ASSET (S/N 1135). 1G72 3U3 U H88EU E42NE 20040303000702004030300070 2004 3 3 SWIA200412925 420040218A3418607300001 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07587SW5579 5579 7062 STALL TEST SYSTEM WILL NOT TEST AND INTERMITTENT STALL FAIL MESSAGE ON EICAS. REMOVED AND REPLACED LEFT AND RIGHT MACH TRANSDUCERS IAW AMM 27-35-25. OPS CHECK GOOD IAW MM 27-35-25. P/N: 60730-000-1, RIGHT SIDE, S/N OFF: 180. 2L72 4F RTA21EA 20040303000722004030300072WP 2004 3 3 0378 120040217A53113754023 FRAME DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32R AND 33R. 2L74 4F4 F 4A25 1E8 20040303000732004030300073SO 2004 3 3 SWIA200412926 120040218A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE T/E FLAP LEAKING A SWIAA UNSCHED LANDING KFJFLUID LOSS FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07393SW9016 9016 120330 DURING APPROACH INTO MRY GOT A DISAGREEMENT WITH FLAP SELECTOR AT 25 FT THE NACELLE FLAPS WERE AT 0 DEGREES SHORTLY AFTER THE BLUE HYD QUANTITY AND PRESSURE WENT TO 0 AND ASSOCIATED LIGHTS. DIVERTED TO SFO. REPLACED LEAKING LEFT NACELLE FLAP ACTUATOR PER MM 27-50-08. OPS AND LEAK CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040303000752004030300075 2004 3 3 SWIA200412927 420040217A3418C818022 STICK SHAKER EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07223SW9031 9031 120291 F/O'S STICK SHAKER INOP. REPLACED RIGHT STICK SHAKER. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040303000772004030300077EU 2004 3 3 DHL2004364002 120040215A3260 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG INOPERATIVE A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01364DH 141 DURING INITIAL CLIMB, LANDING GEAR FAILED TO RETRACT. ABNORMAL PROCEDURES COMPLETED, LANDING GEAR RETRACTED. TRANSFERRED NR 1 LEVER LOCK SYSTEM TO DMI LOG IAW A/B MEL 32-31-02A CAT. (B) AS DMI NR 15736. REF. S/P 32-31-02A. VERIFY NR 2 LEVER LOCK SYSTEM OPS NORMAL IAW PREFLIGHT PROCEDURES. REF. DMI NR 15736 DURING INITIAL CLIMB, LANDING GEAR FAILED TO RETRACT. ABNORMAL PROCEDURE COMPLETED, LANDING GEAR RETRACTED (NR 1 SYSTEM) SEE S/P 32-31-02A. REPLACED 67GB PROXIMITY SENSOR ON LT GEAR IAW M/M 32-61-00. OPS CHECKED OK. THIS CLEARS DMI. 2L72 4F RTA35EU 20040303000782004030300078NM 2004 3 3 372PA0042 120040212A3350 LIGHT BOEING737 737306 13844BGNM GE CFM56 CFM56* 13802NE CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. CLEANED AND DRIED WATER FROM TRACK AND CONTACTS. OPS CHECKS NORMAL. 2L72 4F4 FRTA16NE E2GL 20040303000792004030300079EU 2004 3 3 DHL2004364003 120040218A3242 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG INTERMITTENT A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01364DH 141 BRAKES OCCASIONALLY RELEASES DURING TAXI AND NR 8 ANTI-SKID RELEASES INTERMITTENTLY. PERFORMED ANTI-SKID ADJ./TEST IAW MM 32-42-00. ANTI-SKID SYSTEM. OK FOR SERVICE. 2L72 4F RTA35EU 20040303000902004030300090NM 2004 3 3 04043402 120040212A2720 CONTROL CABLE DORNERDO32 DO328300 NM RUDDER FRAYED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27402FJ 3147 DURING INSPECTION THE RUDDER CONTROL CABLE WAS FOUND TO HAVE 4 BROKEN WIRES. THIS WAS DETERMINED TO BE WITHIN LIMITS. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2H72 4T RTA55NM 20040303000942004030300094SW 2004 3 3 2004F00079 120040216A5320 BRACKET BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL LIGHT CRACKED D K NONE O OTHER ININSP/MAINT 1 SW05518Z 3991 834616 RIVETED BRACKET, CONTAINING AIRCRAFT ATTACHING STUD, FOUND CRACKED IN BEND RADIUS. 1G71 3U3 U H2SW E4CE 20040303000952004030300095SW 2004 3 3 2004F00080 120040216A5320 BRACKET BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL LIGHT CRACKED D R45RK NONE O OTHER ININSP/MAINT 1 SW05518Z 3991 834616 RIVETED BRACKET, CONTAINING AIRCRAFT ATTACHING STUD, FOUND CRACKED IN BEND RADIUS. 1G71 3U3 U H2SW E4CE 20040303000962004030300096NE 2004 3 3 DHL2004783004 220040228A7320 POWER DRAIN VLV BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 3 ENGINE FAULTY A DHLAO OTHER X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 SO01783DH 21999 708917 DURING ENGINE START NR 3 ENGINE AUTO ROLL BACK AT 40 PERCENT N2. ATTEMPTED 2ND START PER MAINTENANCE CONTROL, HAD NO FUEL FLOW INDICATION. REMOVED AND REPLACED NR 3 ENGINE FUEL PRESSURE AND DUMP VALVE IAW ASTAR B-727 M/M 73-12-1. ENGINE START IAW ASTAR JRH 5.1.1. 2L73 4F4 F A3WE E2EA 20040303000972004030300097NM 2004 3 3 AALA20040249 120040219A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21920AN 29521 MIA EMERGENCY LIGHTS AT SEATS 12D, 13D, AND 14D INOPERATIVE. REPLACED BATTERY PACK M1695 FOR EMERGENCY LIGHTS AT SEATS 12D, 13D, AND 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA16WE 20040303000982004030300098NM 2004 3 3 DHL2004720002 120040228A5753 SKIN BOEING727 727228 1384083NM MID FLAP CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01720DH 19544 LEFT-HAND INBOARD MID FLAP LOWER SURFACE 2 AREAS OF SURFACE CORROSION. REMOVED CORROSION, TREATED AND PRIMED IAW B-727 SRM 51-10-2. 2L73 4F RTA3WE 20040303000992004030300099WP 2004 3 3 AALA20040248 120040218A3350 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21572AA 49458 EGRESS EMERGENCY LIGHT AT ROW 16 INOPERATIVE. SPLICED WIRES UNDER SEAT FOR EMERGENCY EGRESS LIGHT AT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED 2L72 4F RTA6WE 20040303001002004030300100NM 2004 3 3 AALA20040247 120040218A3350 BATTERY BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21189AN 32383 BULL NOSE EMERGENCY LIGHTS AT ROWS 11 THROUGH 14 AND R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHTS AT ROWS 11 THROUGH 14 AND R2 DOOR EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RTA2NM 20040301000692004030100069WP 2004 3 1 UO22004F00001 220040129A7210307217810 PLANETARY GEAR LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP GEARBOX FAILED B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL1935TJ 13594 137 P74120 1 EACH PLANETARY BEARING FAILED, CAUSING MASSIVE CHAIN REACTION FAILURE WITHIN FAN GEARBOX. 2L72 4F4 F A10CE E6WE 20040301000882004030100088EA 2004 3 1 F03052 120040125A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE MLG DEFECTIVE A FDKAO OTHER J WARNING INDICATION APAPPROACH 1 SW07504MJ882 801 10066 CREW REPORTED LANDING GEAR DISAGREE MESSAGE. EXTENDED GEAR UTILIZING ALTERNATE PROCEDURES. MECHANIC REMOVED AND REPLACED DEFECTIVE NLG SELECTOR VALVE. LK AND OPS CHECKED GOOD. CONTROL NR 111452 AND 111465, AFML LOG PG 46147, ITEM 4. 2L72 4F4 FRTA21EA E15NE 20040301001192004030100119SO 2004 3 1 HPF2004F00000 120040122A5280102156002 HINGE PIN PIPER PA46 PA46500TP 7104622SO PWA PT6 PT6* 52043EA NLG DOOR LOOSE B HPFRK NONE O OTHER ININSP/MAINT 1 WP09562HP227 4697139 NOSE GEAR DOOR FORWARD HINGE PIN MIGRATED AFT, NOT PROPERLY RETAINED. SUGGEST DRILLING HINGE TO ENABLE SAFETY WIRE OR COTTER PIN TO PREVENT HINGE PIN MIGRATION. LOSS OF HINGE PIN WOULD RESULT IN SIGNIFICANT DAMAGE TO NOSE GEAR DOOR. 1L71 3O3 TRTA25SO E2NE 20040301001252004030100125NM 2004 3 1 2004F00078 120040212A2621 INDICATOR BOEING737 737* NM GE CFM56 CFM56* 13802NE FIRE BOTTLE FALSE INDICATIONB K NONE N FALSE WARNING ININSP/MAINT 1 EA17889NC1085 29764EL 30070 REMOVED FIRE BOTTLE AND SENT FOR HYDROSTATIC RETEST, FILL AND LEAK CHECK. UPON RETURN OF BOTTLE REINSTALLED AND PERFORMED INSTALLATION TEST, OPS CHECK GOOD. APPROXIMATELY ONE WEEK LATER NOTICED CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. INSPECTION OF BOTTLE SHOWED CONTENTS OF BOTTLE HAD NOT BEEN DISCHARGED. 2L72 4F4 FRTA16WE E2GL 20040301001332004030100133WP 2004 3 1 DHL2004806564 120040123A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 ITEM REF. NR. 2249: RUDDER LT SKIN INTERNAL PART CORRODED STA ZR. 162.000-ZR 173.000 (MAJOR REPAIR). CORRODED, PERFORMED MAJOR REPAIR IAW MFG MSG NR DHL-CVG 04-0013H, DHL-CVG04-0015H, ED3583-1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG.12. REMOVED CORRODED SKIN AND FINGER DOUBLER IAW SRM 51-1-21 PG.1.FABRICATED NEW SKIN(2024-T3AL 0.032) IAW MFG MSG NR DHL-CVG04-0013H, DHL-CVG04-0015H, ED3583-1. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW SKIN IAW MFG MSG NR DHL-CVG04-0013H, DHL-CVG04-0015H, ED3583-1, SRM 51-1-21 PG.1. FOR REBALANCE SEE NR 2140. 2L74 4F RT4A25 20040301001472004030100147EU 2004 3 1 DHL2004365514 120040119A5311 FRAME AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01365DH REPAIR AT FR54, STR2L TO 5L DOES NOT CONFORM TO SRM. REMOVED REMAINING FASTENERS AND DOUBLER REPAIR FOR EVALUATION. PERFORMED NDT INSP OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR54, BETWEEN S-2L TO S-5L AND NO CRACKS NOTED. ACCOMPLISHED UT INSP, PROCEDURE C BY HFEC MANUAL HOLE PROBE, NO CRACKS NOTED AT THIS TIME. ACCOMPLISHED UT INSP AT FR54, STR 2L TO 5L AND NO DEFECTS NOTED AT THIS TIME. FABRICATED NEW REPAIR DOUBLER, DOUBLER SIZE 2'X 1'. INSTALLED REPAIR DOUBLER. NEW REPAIR DOUBLER FABRICATED. FILLER DOUBLER MADE OF 2024T3 .071 PO NR 83113526. ALODINED AND PRIMED. AERODYNAMIC CHAMFER. FILLING OF EXISTING COUNTERSINKS. FASTENERS HOLE AND DRILL HOLES. PAINTED REPAIR DOUBLER AT FRAME 54 STR 2L TO 5L. 2L72 4F4 FRTA35EU E23EA 20040301001582004030100158NM 2004 3 1 2004F00077 120040216A324631306 WHEEL BOEING727 727200 138407ENM MLG FRACTURED B D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO03 N481FE POSITION NR 3 OB WHEEL FLANGE SEPARATED FROM WHEEL, WHILE UNDER PRESSURE. 2L73 4F RTA3WE 20040301001612004030100161WP 2004 3 1 258160001 220040213A7261 OIL CAP BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP LT ENGINE MISINSTALLED E ERYAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE07803JL NA0436 P91433 DURING CRUISE FLIGHT, NOTICED FLUCTUATION IN OIL PRESSURE INDICATION ON LT ENGINE. INITIATED PRECAUTIONARY SHUTDOWN AND PROCEEDED WITHOUT INCIDENT. MAINTENANCE OPENED LOWER COWL AND FOUND IB OIL TANK SERVICE CAP DISLODGED AND LAYING IN LOWER COWLING. INSTALLED CAP AND LOCKWIRED, SERVICED OIL LEVEL AND WASHED ENGINE. PERFORMED ENGINE GROUND RUN, NO DISCREPANCIES FOUND. 2L72 4F4 FRTA3EU E6WE 20040301001652004030100165NM 2004 3 1 2004UALA00105 120040206A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE ROW 6,20 ABC INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29822UA 948 WHITE EEL LIGHTS ARE INOPERATIVE AT ROWS 6 ABC AND 20 ABC. REPLACED EEL LIGHTS. OPS CHECKED NORMAL. 2L72 4F4 FRTA28NM E40NE 20040301001712004030100171NM 2004 3 1 2004UALA00112 120040208A2910 LINE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HYDRAULIC SYSTEMFAILED A UALAO OTHER J WARNING INDICATION LDLANDING 1 WP29320UA 23952 LANDED UNDER AMBER ALERT DUE TO LOSS OF A SYSTEM HYDRAULICS. RIGID HYDRAULIC TUBE P/N 65C26809-1100 FAILED, ALLOWING THE A SYSTEM HYDRAULIC FLUID TO BLEED OUT. SUBSEQUENT INSPECTION FOUND THAT THE LINE HAD SHEARED ADJACENT TO WHERE IT WAS SECURED TO STRUCTURE WITH A CLAMP. THE HYDRAULIC LINE RUNS BETWEEN THE WING SPAR AND THE A SYSTEM EDP. THE HYDRAULIC LINE WAS REPLACED, NEW MOUNTING BRACKETS AND CLAMPS WERE INSTALLED, THE HYDRAULIC SYSTEM WAS SERVICED. 2L72 4F4 FRTA16WE E2GL 20040301001872004030100187NM 2004 3 1 DHL2004747003 120040211A5210 DOOR BOEING727 727224 1384076NM MAIN PAX OUT OF ADJUST A DHLAK NONE L NO TEST NRNOT REPORTED 1 SO01747DH 22253 MAIN ENTRY DOOR DIFFICULT TO CLOSE. ADJUSTED MAIN ENTRY DOOR IAW M/M 52-11-01. OPS CHECKED GOOD. 2L73 4F A3WE 20040301001922004030100192WP 2004 3 1 GKZR200482307 120040217A5313 SPLICE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 RIGHT LONGERON SPICE AT R34 STA 1490 CRACKED. REMOVED LONGERON SPLICE IAW DC-8 SRM 51-1-21. PERFORMED NDT FOUND NO CRACK IAW DC-8 SRM 51-5-2 TREATED AND PRIMED IAW DC-8 SRM. INSTALLED LONGERON SPLICE IAW DC-8 SRM 51-1-21. (CLOSED) 2L74 4F RT4A25 20040301002022004030100202WP 2004 3 1 AALA20040232 120040215A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21436AA 49454 DFW - FORWARD EMERGENCY LIGHT ARROW INOPERATIVE. REPLACED FORWARD EMERGENCY ARROW LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040301002092004030100209NM 2004 3 1 SWAA040455 120040213A3350BR9442 LIGHT BOEING737 7373Y0 1384671NM L1 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20040301002102004030100210NM 2004 3 1 SWAA040456 120040213A335065C27093 LIGHT BOEING737 7377H4 1384404NM R2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29418WN 29823 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20040301002112004030100211NM 2004 3 1 SWAA040457 120040213A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FORWARD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040301002122004030100212NM 2004 3 1 SWAA040458 120040213A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STRINGER 9L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040301002172004030100217 2004 3 1 SWAA040463 420040213A256563562 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040301002262004030100226NM 2004 3 1 SWAA040472 120040215A3350101073 LENS BOEING737 7372T4 1384492NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 L2 DOOR EMERGENCY EXIT LIGHT LENS COVER LOOSE. REINSTALLED LIGHT LENS PER MM. 2L72 4F A16WE 20040302001862004030200186NM 2004 3 2 SWAA040389 120040207A53126545409 PRESSURE PANEL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 45. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040303000022004030300002NM 2004 3 3 MEX2004029 120040122A275059370525001 CYLINDER DOUG MD80 MD83 3023681NM TE FLAP DAMAGED W ASMZO OTHER O OTHER NRNOT REPORTED 1 SW23831LF2554025540 53050 DURING TRANSIT CHECK WAS DETECTED EXCESSIVE FELT DOWN TO 33 DEGREES AND WHEN FLAPS ARE SELECTED, THERE ARE 5 DEGREE DIFFERENCE. AC WAS SENT TO HANGAR. DURING CHECK WAS DETECTED INTERNAL FLUID LEAKAGE IN EXTERIOR FLAP ACTUATOR. ACTUATOR AND PTU WERE REPLACED IAW MM. FLAPS BUS CABLE WAS ADJUSTED DUE TO BEING OUT OF TOLERANCE IAW MM AND FLAPS INDICATION WAS CHECKED IAW MM, ALL TESTS CORRECT. 2L72 4F RT 20040303000072004030300007NM 2004 3 3 AWXA200400177 120040106A551465475966 CLEVIS BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH POINT AT CENTER SECTION FITTING AFT CLEVIS, AFT FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH POINT, AFT FACE; OVERSIZED LOWER ATTACH POINT CENTER SECTION FITTING, AFT CLEVIS HOLE, AFT FACE; FABRICATED A NEW REPLACEMENT BUSHING IAW SRM 55-10-10, PG. 112; INSTALLED REPAIR PART IAW AWA E.R. 03-5512-04044-TB1. 2L72 4F4 FRTA16WE E2GL 20040303000082004030300008NM 2004 3 3 AWXA200400178 120040214A335032145410 EPSU AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE ZONE 221 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28801AW19355 889 EMERGENCY LIGHT SYSTEM TEST FAILED AT PUSH BUTTON ON FLIGHT ATTENDANT FORWARD PANEL. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20040303000132004030300013EA 2004 3 3 COMA0460149 120040215A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER N FALSE WARNING DEDESCENT 1 SO01491CA2939 7756 FLIGHT 5389 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20040303000172004030300017NM 2004 3 3 CALA0400125 120040216A5320 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714731 28799 INSPECTION FOUND AFT CARGO PIT LT Z-CHANNEL CORRODED FROM STA 727A-827. THE Z-CHANNEL WAS REMOVED AND A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040303000312004030300031NM 2004 3 3 P5CA0401036 120040213A2710 CIRCUIT CARD BOEING747 747236B 1384804NM AILERON CONTROL LOOSE A P5CAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 WP23924FT 21730 OB AILERONS LOCKED OUT, CYCLED FLAPS TWICE AND RESET C/B. NO HELP. RESEATED A1 CARD IN FLAP CONTROL CK AND VISUAL, OPS NORMAL IAW MM 27-10-00. 2L74 4F A20WE 20040303000342004030300034NM 2004 3 3 QXEA200400138 120040213A3260401020101 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA MLG MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09413QX 4060 PDX FLIGHT NR 2359 AFTER TAKE OFF AND RETRACTING LANDING GEAR, LT AMBER DOOR LIGHT AND RED GEAR LIGHT CYCLED, AND GEAR HANDLE LIGHT CYCLED. REPLACED LT HAND GEAR DOOR PROXIMITY SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040303000382004030300038EU 2004 3 3 BAQA092102 120040120A243523032022 COMMUTATOR BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101* NE STARTER GEN BURNED B BAQAK NONE O OTHER ININSP/MAINT 1 EA0339188175 7011 COMMUTATOR PITTED AND BURNED. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/02/2004 1G72 3U3 U H13EU E5NE 20040303000462004030300046EU 2004 3 3 BAQA092473 120040119A80129550178290 START VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE LEAKING B BAQAK NONE K FLUID LOSS ININSP/MAINT 1 EA03365S 899 6036 START VALVE LEAKS FUEL. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENG. S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE UNIT. 02/05/2004 1G72 3U3 U H10EU E19EU 20040303000502004030300050EU 2004 3 3 BAQA092553 120040121A71700174025120 DRAIN VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE IGNITION STICKS B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 899 6036 VALVE STICKS IN COLD WEATHER. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2. REPLACED WITH SERVICABLE UNIT. 02/05/2004 1G72 3U3 U H10EU E19EU 20040303000552004030300055NE 2004 3 3 BAQA092575 220040128A75320210027060 BLEED VALVE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE ENGINE WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC2094 7517 10849 WARRANTY. UNIT COVERED UNDER SUPPORT BY HOUR. UNIT EXTREMELY WORN. REPLACED WITH SERVICEABLE UNIT. 02/09/2004 1G72 3U3 UNCH13EU E19EU 20040303000562004030300056EA 2004 3 3 VNAA0402004 120040210A5270 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT EMER DOOR DIRTY A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07226JS 7895 DURING FLIGHT, THE CREW RECEIVED A RIGHT EMERGENCY DOOR ILLUMINATION AND YELLOW CAS MESSAGE. UPON ARRIVAL AT PHL, OUTSTATION MAINTENANCE FOUND CODE S42 IN THE PSEU. MAINTENANCE THEN CLEANED AND INSPECTED THE PROXY SENSOR AND TARGET IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00 AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040303000622004030300062EU 2004 3 3 BAQA092609 120040204A80129550178290 START VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03365KY1298 6529 START VALVE UNIT LEAKING FUEL. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1G72 3U3 U H10EU E19EU 20040303000642004030300064CE 2004 3 3 BAQA092610 120040123A2750 BRUSHES BEECH 90 C90 1152913CE PWA PT6 PT6* 52043EA FLAP MOTOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0390LF 10084 900 LJ852 MOTOR DELAYS, BRUSHES PROBABLY WORN OUT, SOUNDS WEAK. REPLACED WITH SERVICABLE UNIT. 02/13/2004 1L72 3T3 T 3A20 E2NE 20040303000652004030300065NE 2004 3 3 BAQA092612 220040120A73200164248840 FUEL CONTROL AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 851 6036 FUEL CONTROL PRODUCING FUEL VAPOR AFTER ENGINE SHUTS DOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 02/10/2004 1G72 3U3 U H10EU E19EU 20040303000692004030300069WP 2004 3 3 0375 120040217A5311 FRAME DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE FUSELAGE CORRODED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LONGERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F4 F 4A25 1E8 20040303000822004030300082SO 2004 3 3 SWIA200412930 120040220A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO CABIN DISCHARGED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07250YV298 298 120250 MERGENCY FLOOR LIGHTING, FRONT SECTION INOP. REPLACED FORWARD SECTION EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD. 2L72 4T RTA31SO 20040303000852004030300085NM 2004 3 3 DHL2004720001 120040217A33501000677 LIGHT BOEING727 727228 1384083NM PWA JT8 JT8D* NE PAX DOOR INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01720DH 19544 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY IAW B-727 M/M 33-50-111. OPS CHECKED GOOD. 2L73 4F4 FRTA3WE E2EA 20040303000862004030300086GL 2004 3 3 ALG2004F00002 220040116A72006895000 ENGINE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL FAILED E ALGAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION HOHOVERING 1 SW03206SL14481 45245 CAE860023 ENGINE START WAS NORMAL BROUGHT THE AIRCRAFT TO A 3 FT HOVER ALL ENGINE INDICATIONS NORMAL, AT THIS TIME THE PILOT HEARD A SLIGHT BANG FROM THE REAR OF THE AIRCRAFT FOLLOWED BY A LOUD GRINDING WHINE AND A HIGH FREQUENCY VIBRATION IN AIRFRAME. AC BEGAN A SLIGHT YAW AND NOTED N2 DECREASING. THE PILOT SET THE AIRCRAFT DOWN ON THE HELIDECK AND SHUT THE ENGINE DOWN. HE ALSO NOTED OIL COMING OUT OF ENGINE DECK DRAIN, HE ALSO OPENED THE ENGINE COWLING AND OBSERVED AN OIL PUDDLE IN THE ENGINE PAN. NOTIFIED MAINTENANCE. THE MECHANIC SUBSEQUENTLY REMOVED AND REPLACED ENGINE. (SW03200405257) 1G71 3U3 U H2SW E1GL 20040303000872004030300087SO 2004 3 3 C852004F00000 120040120A321067753000 PLATE PIPER PA28 PA28R201 7102816SO LYC O360 IO360A1A 41514EA MLG BROKEN B C85RO OTHER O OTHER NRNOT REPORTED 1 NE013628211129 28R7837271 DURING PREFLIGHT, SPRING WAS SEEN HANGING DOWN BY 1 END. THE SPRING ATTACHES TO THE PLATE. THE PLATE BROKE OFF THROUGH THE SPRING ATTACH HOLE. (THE SPRING IS THE EMERGENCY EXTENSION BACK UP SYSTEM, IF THE HYDRAULIC SYSTEM BECOMES INOPERATIVE) THE SQUAT SWITCH WIRES RUN THROUGH A HOLE IN THE PLATE, AND MAY HIDE THE FACT THE PLATE IS STARTING TO BEND OR BREAK, AS IT IS NOT EASILY VISABLE. FATIGUE OF THE PART IS ASSUMED TO BE THE CAUSE OF THE FAILURE. 1L71 3O3 O 2A13 1E10 20040303001012004030300101NM 2004 3 3 QXEA200400156 120040214A2611824PYX SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE LAVATORY FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09347PH15539 480 DURING CLIMBOUT AND PASSING 3000 FEET, THE LAVATORY SMOKE DETECTOR SOUNDED. THERE WAS NO SMOKE OR FUMES NOTED BY THE FLIGHT ATTENDANT. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040303001042004030300104WP 2004 3 3 ABXA040067 120040205A523099576442 INTERCOSTAL DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 FORWARD LOWER CARGO DOOR HAD CRACKED INTERCOSTAL AT AFT HINGE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040303001052004030300105WP 2004 3 3 ABXA040068 120040205A5230591014163 SKIN DOUG DC9 DC941 302207NWP FWD CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 FORWARD LOWER CARGO DOOR'S EXTERIOR SKIN WAS DAMAGED AT LOWER EDGE 3 PLACES. REPAIRED AREA IAW REA D952-49012. 2L72 4F A6WE 20040303001062004030300106WP 2004 3 3 ABXA040071 120040206A5320D0489835 WEB DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 CUSP WEB CRACKED FROM F.S. 1025-1039 APPROXIMATELY LT BUTT LINE 56. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040303001072004030300107WP 2004 3 3 04FDEA00456 120040219A3232 ACTUATOR DOUG DC10 DC1010 3022110WP RT MLG DOOR LEAKING A FDEAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25394FE 46628 AFTER T/O LAX, RT MAIN GEAR INDICATED UNSAFE AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY INDICATORS. RECYCLED PER QRH, NO CHANGE. DUMPED FUEL AND RETURNED FOR UNEVENTFUL LANDING. CHECKED: BUNGEE CYLINDER, EXTENSION RETRACTION ADJUSTMENT TEST, TARGET AND PROXIMITY SENSOR GAPS, BLED TRIM CYLINDER, TRUCK PIVOT RELATIVE MOVEMENT, LUBED GEAR, REPLACED RT GEAR DOOR ACTUATOR FOR BY-PASSING AND LEAKING. ALL ACCOMPLISHED AS PER MM. TEST FLEW AIRCRAFT WITH 3 LANDINGS. OK RETURNED TO SERVICE. 2L73 4F A22WE 20040303001092004030300109WP 2004 3 3 ABXA040073 120040205A5320592440710 SUPPORT DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 VERTICAL SUPPORT NR 7 CRACKED FORWARD SIDE OF FORWARD AUX TANK. REPLACED VERTICAL SUPPORT NR 7 IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20040303001122004030300112NM 2004 3 3 SWAA040548 120040222A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040303001132004030300113NM 2004 3 3 SWAA040549 120040222A575465C26603 WEDGE BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE IS DELAMINATED AT T/E. REMOVED AND REPLACED NR 4 SLAT PER MM. 2L72 4F RTA16WE 20040303001142004030300114NM 2004 3 3 SWAA040550 120040222A3350101114 LIGHT BOEING737 7373Y0 1384671NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C3 CHECK, FOUND FORWARD EMERGENCY EXIT LIGHT FIXTURE LOOSE. SECURED LIGHT FIXTURE PER MM. 2L72 4F RTA16WE 20040303001162004030300116NM 2004 3 3 SWAA040552 120040222A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED SPV, FOUND STRINGER CLIPS CRACKED AT BS 663.75, STRINGER 4R AND BS 683, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040303001182004030300118NM 2004 3 3 SWAA040554 120040222A53106545805 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR FRAME CUTOUT CRACKED AT FORWARD WEB. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20040303001202004030300120 2004 3 3 SWAA040556 420040223A2565D31354 SLIDE BOEING737 737317 138447PNM R2 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 R2 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040303001212004030300121 2004 3 3 SWAA040557 420040223A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29794SW 30605 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040303001242004030300124NM 2004 3 3 2004UALA00125 120040214A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 SMALL SKIN DENT BELOW AND FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040303001262004030300126NM 2004 3 3 2004UALA00127 120040213A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29595UA 28748 SKIN DENTS STA 600-640, AND STRINGER 14L-19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TRIPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040303001282004030300128NM 2004 3 3 2004UALA00130 120040215A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29376UA 24641 SHEAR TIES ARE CRACKED AT STA 616 STR 4L AND STA 344 STR 15R. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040303001332004030300133NM 2004 3 3 SWAA040531 120040220A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND WING CENTER SECTION BEADED WEB CRACKED AT RBL 38. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040303001342004030300134NM 2004 3 3 SWAA040532 120040220A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIES CRACKED AT BS 360, BETWEEN STRINGERS 13L, 14L AND 15L. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040303001352004030300135NM 2004 3 3 SWAA040533 120040220A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040303001362004030300136NM 2004 3 3 SWAA040534 120040220A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STRINGER 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040303001372004030300137NM 2004 3 3 SWAA040535 120040220A33507003661 BALLAST BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29430WN 33659 DURING SCHEDULED MV3 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT EMERGENCY EXIT LIGHT BALLAST. 2L72 4F RTA16WE 20040303001392004030300139NM 2004 3 3 SWAA040537 120040220A3350OL3070BEGPL LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29762SW 27876 DURING SCHEDULED MV3 CHECK, FOUND EEPLS TRACK LIGHT ROW 2 ABC INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040303001402004030300140 2004 3 3 SWAA040538 420040220A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040303001412004030300141 2004 3 3 SWAA040539 420040220A256563550 SLIDE BOEING737 7377AD 1384502NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040303001422004030300142NM 2004 3 3 SWAA040540 120040223A3350101114 LIGHT BOEING737 7377AD 1384502NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29798SW 28436 DURING SCHEDULED HC2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040303001432004030300143NM 2004 3 3 SWAA040541 120040221A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY AT R1 DOOR. 2L72 4F RTA16WE 20040303001452004030300145NM 2004 3 3 2004UALA00136 120040213A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 STRINGER ATTACH CLIP CRACKED AT BS 685 STR 3R. MAJOR REPAIR ACCOMPLISHED. REPLACED ATTACH CLIP. 2L72 4F4 FRTA16WE E2GL 20040303001462004030300146NM 2004 3 3 2004UALA00137 120040213A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 INTERCOSTAL CRACKED AT BS 294.5 STR 14L. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2GL 20040303001482004030300148NM 2004 3 3 2004UALA00139 120040216A2782 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29576UA 26690 ON FLAP RETRACTION THE L/E FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXCESSIVE TORQUE FORCES IN THE LE SLAT DRIVE SYSTEM INITIATED A LE SLAT DISAGREE FAULT WHICH WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT (FSEU) LE SLAT MOVEMENT IS AUTOMATICALLY INHIBITED BY HYDRAULIC BYPASS TO PREVENT DAMAGE TO ASSOCIATED LE SLAT DRIVE COMPONENTS. THE NR 6 AND 15 LE SLAT DRIVE ROTARY ACTUATORS WERE FOUND TO HAVE TRIPPED TORQUE OVERLOAD INDICATORS. THE NR 6 AND 15 LE SLAT DRIVE ACTUATORS WERE REPLACED. THE DRIVE TRANSMITTER IN THE LE SLAT POWER DRIVE UNIT (PDU) WAS ALSO REPLACED. 2L72 4F4 FRTA2NM E17NE 20040303001542004030300154NM 2004 3 3 2004UALA00146 120040217A2120 ODOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT DETECTED A UALAH DEACTIVATE SYST/CIRCUITS JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29197UA 26901 RIGHT ELEC UTIL EICAS MSG WITH ELECTRICAL ODOR IN GALLEY. AFTER SHUTTING DOWN RIGHT UTIL BUS, LEFT BUS TRIPPED. W/U STATES ELECTRIC BURNING ODOR FOLLOWED BY "ELEC UTILITY BUS R" AND THEN BY "ELEC UTILITY BUS L" BOTH UTILITY BUS SW'S SELECTED "OFF" PER FLT MAN IRRG 7-21 NO FURTHER RESET ATTEMPTED AND ODOR STOPPED. MAINTENENACE REPORTED THEY ACP ENGINE RUNS FOR APPROX 40 MIN; ALL ELECTRICAL SYSTEMS USED; NO CHAPTER 24 FAULTS FOUND OP CK'D OK, CHECK CABIN FOR ELECTRICAL ODOR NONE NOTED. RAN THE OVENS NO ODORS NOTED. 2L74 4F4 FRTA20WE E24NE 20040303001582004030300158WP 2004 3 3 ABXA040072 120040206A53119923409501 FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 EDDY CURRENT INDICATED LT MAIN FRAME AT FS 737 CRACKED AT AFT SIDE AT POINT J TO POINT G. REPAIRED IAW J.C. EA 53400110-001-2. 2L72 4F A6WE 20040303001592004030300159WP 2004 3 3 ABXA040074 120040206A53119919619506 FRAME DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 STA 775 AFT OVERWHEEL WELL FRAME WAS CRACKED BETWEEN POINTS E AND E IN AFT OB POCKET AND CRACKED BETWEEN POINTS H AND I IN AFT IB POCKET AND CRACKED IN FORWARD IB POCKET BETWEEN FASTENERS THAT ARE LOCATED BETWEEN POINTS H AND I. FORWARD IB POCKET CRACK EMINATES FROM OB FASTENER TOWARDS IB FASTENER APPROXIMATELY .5 INCH. REPLACED AFT FRAME AT STA. 775 IAW EA 53400326-001-5. 2L72 4F A6WE 20040303001612004030300161WP 2004 3 3 ABXA040078 120040218A335060030451 BATTERY DOUG DC9 DC941 302207NWP EMERGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX92 45728 OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH SEVICEABLE UNIT. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20040303001622004030300162WP 2004 3 3 ABXA040077 120040217A3350 BATTERY DOUG DC9 DC941 302207NWP EMRGENCY LIGHT DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 OVERHEAD EMERGENCY LIGHTS IN COCKPIT STAYED ON AFTER POWER SHUT DOWN. RESEATED BATTERIES IN EMERGENCY LIGHT POWER SUPPLY. LIGHTS FUNCTIONED NORMALLY IAW DC-9 MM. 2L72 4F A6WE 20040303001642004030300164NM 2004 3 3 AT0400003 120040218A3230MS288892 VALVE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE NLG LEAKING A ZZDAO OTHER J WARNING INDICATION CLCLIMB 1 SO15604AT 55128 WHILE RETRACTING GEAR, HAD A NOSE WHEEL RED LIGHT STAY ON. REMOVED AND REPLACED NOSE GEAR SCHRADER VALVE AND SERVICED NOSE STRUT IAW 32-21-01, PERFORMED NOSE GEAR RETRACTION SEVERAL TIMES. OPS CHECK GOOD IAW MM 32-00. 2L72 4F4 FTRA6WE E00057EN 20040303001662004030300166NM 2004 3 3 AWXA200400185 120040218A2530416000129 COFFEEMAKER AIRBUSA319 A319132 3930340NM FWD GALLEY ARCED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28816AW9416 2123 1350 BURNING ODOR, FLT 0395 EN ROUTE FLIGHT ATTENDANT OBSERVED A BURNING ELECTRICAL ODOR IN THE FORWARD GALLEY. MAINTENANCE FOUND THE NR 2 COFFEEMAKER IN THE FORWARD GALLEY ARCING, REMOVED AND REPLACED THE FORWARD GALLEY NR 2 COFFEEMAKER, OPERATIONAL CHECK WAS GOOD. PRELIMINARY INSPECTION OF COFFEE MAKER S/N 5361 COULD NOT CONFIRM REASON FOR REMOVAL. REPLACED UPPER & LOWER SPRINGS, FLOAT TIP, PROBES, AND RELAY (RL-119) PER AIRLINES REQUEST. 2L72 4F RTA28NM 20040303001672004030300167NM 2004 3 3 AWXA200400186 120040218A3350BR964411 LIGHT BOEING757 7572S7 1384962NM RROYCERB211 RB211* 54555NE SEAT ROW 16 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT LENS AT SEAT ROW 16 LT WAS FOUND MISSING. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA2NM A12EU 20040303001682004030300168NM 2004 3 3 AWXA200400187 120040219A33501012721 LIGHT BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE SEAT ROW 8 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 EEL, DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040303001692004030300169NM 2004 3 3 AWXA200400188 120040219A33501012721 LIGHT BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE SEAT ROW 19 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040303001702004030300170EU 2004 3 3 AWXA200400189 120040209A5347D53112092206 SEAT TRACK AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 DURING B-04 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR BEAM TEE CAP (SEAT TRACK) AT CLIP NUT LOCATIONS BETWEEN FR 17 AND FR 20, Y1292 RT. MAINTENANCE REMOVED DAMAGED SEAT TRACK BETWEEN BS 7830 AND BS 8000, Y1292 RT; FABRICATED 6 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-15, FIG. 204, PG. 222-227. 2L72 4F4 FRTA28NM E311NE 20040303001712004030300171EU 2004 3 3 AWXA200400190 120040209A5315D53472172201 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 DURING B-04 CHECK CORROSION WAS FOUND ON FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 66 AND FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-14, PG. 7-10, 12, AND 16-17. 2L72 4F4 FRTA28NM E311NE 20040303001722004030300172EU 2004 3 3 AWXA200400191 120040209A5315D5347172203 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 68, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 68, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG D53472189; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-14, 16 AND 17, PG. 7-10, 12. 2L72 4F4 FRTA28NM E311NE 20040303001732004030300173NE 2004 3 3 ANCF200400003 220040217A7200 ENGINE BOEING757 75728A 1384976NM PWA 4056 PW4056 NE RIGHT SURGES W ANCFA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO23517NA434924402 24260 30677 RT ENGINE SURGE DURING ACCEL (AFTER SELECTING CLIMB THRUST) AT 5000 FT ENG OPERATION ABNORMAL AFTER SURGE. ENG WAS NOT SHUTDOWN. BOROSCOPE INSPECTION WAS PERFORMED IAW AMM 71-00-00/601, FIM 71-06-00, FIG 105A NEGATIVE TEST, THE ENGINE WILL BE REPLACE ON FEBRUARY 20/2004 2L72 4F4 FRTA2NM E24NE 20040303001752004030300175SO 2004 3 3 C2XA04SH074 120040220A532014524131011 BRACKET EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C CHECK THE MAIN DOOR THRESHOLD AFT U BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040303001762004030300176EA 2004 3 3 MASA200400064 120040204A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ROW 10 DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 CREW REPORTED EMERGENCY FLOOR PROX LIGHTS AT ROW 10 INOPERATIVE AND CABIN DOOR FLOOR LEVEL EMERGENCY FLOOD INOPERATIVE. MECHANIC FOUND THE FLOOR PROX LIGHTS TO BE DISCONNECTED. MECHANIC RECONNECTED. OP CHECKS GOOD NO PARTS USED. 2L72 4F4 FRTA21EA E15NE 20040303001782004030300178EA 2004 3 3 MASA200400070 120040206A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717358 7358 DURING PREFLIGHT THE RT FORWARD EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MECHANIC RELAMPED. OPS CHECKS GOOD 2L72 4F RTA21EA 20040303001792004030300179EA 2004 3 3 MASA200400073 120040207A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA FRNKLN6A41506A4150* 27024EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0797314 108314 DURING PREFLIGHT THE RT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MECHANIC REPLACED BULB. 2L72 4F3 ORTA21EA E238 20040303001812004030300181SO 2004 3 3 MASA200400077 120040208A3397 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT UNSECURE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 EMERGENCY EXIT PATH LIGHTING INOPERATIVE. MECHANIC SECURED CONNECTION AT LIGHTING STRIP. OPS CHECKS GOOD. NO PARTS USED. 2L72 4T4 FRTT00011ATTE6CH 20040303001822004030300182SO 2004 3 3 MASA200400078 120040209A3350 BATTERY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07854MJ 145490 CREW WROTE-UP THE EMERGENCY EXIT LIGHT BATTERIES HAD LOW VOLTAGE. MECHANIC PERFORMED AN OP CHECK OF THE SYSTEM. MECHANIC COULD NOT DUPLICATE. NO PARTS USED. 2L72 4T4 FRTT00011ATTE6CH 20040303001832004030300183SO 2004 3 3 MASA200400079 120040209A33501317 BULB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 CEILING EMERGENCY EXIT LIGHT INOPERATIVE AT EXIT ROW. MECHANIC REPLACED BULB. OP CHECKS GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040303002012004030300201WP 2004 3 3 NACA20040012 120040220A281058832D CHECK VALVE DOUG DC6 DC6B 3021712WP FUEL SYSTEM STUCK A NACAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL037919C 43554 HEAVEY FUEL VAPOR IN CABIN DURING CLIMBOUT. REPAIRED AFT ONE WAY CHECK VALVE ON RT SIDE OF BULK FUEL VENT SYSTEM. 2L74 4R 6A4 20040303002082004030300208NM 2004 3 3 CALA0400194 120040301A551165479869 RIB BOEING737 7373T0 1384582NM HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND TWO LT HORIZONTAL STABILIZER L/E RIBS CRACKED AT DENTED AREA 72 INCHES TO 78 INCHES FROM I/B. THE CRACKS WERE 1 INCH LONG. THE RIBS WERE REMOVED AND REPLACED IAW SRM 51-40-02. THE DENT WAS REWORKED WITHIN ALLOWABLE LIMITS IAW SRM 55-10-01. 2L72 4F RTA16WE 20040303002092004030300209NM 2004 3 3 CALA0400195 120040301A5512 SKIN BOEING737 7373T0 1384582NM HORIZ STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND LT HORIZONTAL STABILIZER LOWER SKIN DENTED 57 INCHES FROM I/B EDGE AND 33 INCHES BACK FROM T/E. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-10-01. 2L72 4F RTA16WE 20040303002102004030300210NM 2004 3 3 CALA0400196 120040301A5320149A751116 WEB BOEING737 737724 13844BYNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 INSPECTION FOUND A .5 INCH CRACK IN AFT WEB ON RT MAIN WHEEL WELL RING ASSEMBLY. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW EA 5310-04230 AND SRM 51-40-02. 2L72 4F RTA16WE 20040303002122004030300212NM 2004 3 3 CALA0400198 120040301A5730 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2748127 28968 INSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT STA OSS 425. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20040303002142004030300214NM 2004 3 3 CALA0400200 120040301A534765C80736153 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND LT TIE DOWN RAIL LOWER FLANGE DAMAGED BY A SCREW JUST AFT OF STA 867 AND ABOVE STRINGER 27L. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040303002162004030300216NM 2004 3 3 2004UALA00123 120040215A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29175UA 24382 CORROSION WAS DISCOVERED ON THE UNDERSIDE OF THE FLOORBEAM LOCATED AT STA 1100 FROM LBL 17 TO LBL 30. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR STRAP. 2L74 4F4 FRTA20WE E24NE 20040303002182004030300218NM 2004 3 3 QXEA200400168 120040219A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY WILL NOT TEST A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09345PH1240 1240 476 PDX - FLIGHT 2138 - THE NR 1 BAGGAGE SMOKE DETECTOR WILL NOT TEST. MAINTENANCE REPLACED THE NR 1 CARGO SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040303002212004030300221NM 2004 3 3 04FDEA00436 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002262004030300226NM 2004 3 3 QXEA200400163 120040218A335061047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09364PH8893 82 524 PDX - AFT CABIN EMERGENCY LIGHT INOPERATIVE AND AFT RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. 2H72 4T RTA13NM 20040303002282004030300228SO 2004 3 3 SWIA200412858 120040204A2130 SWITCH EMB 120 EMB120ER 3260203SO CABIN PRESSURE FAILED A SWIAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 NM07214SW 120280 DURING CRUISE FLIGHT AT 27,000 FT, HAD A PRESSURE POP AND THEN A CABIN ALT WITH TRIPLE CHIME. PERFORMED PRECAUTIONARY EMERGENCY DESCENT TO 10,000 FT AT THAT POINT, WENT TO QRH. FOLLOWED PROCEDURE FOR LOSS OF CABIN PRESSURE. WENT TO MANUAL MODE ON PRESSURIZATION CONTROL AND WAS ABLE TO CONTROL CABIN. CONTINUED TO SLC AND LANDED WITHOUT INCIDENT. REPLACED AUTO-MAN DAMP SWITCH. OPS CHECK GOOD IAW 20-13-03 AND 21-30-00. 2L72 4T RTA31SO 20040303002292004030300229EA 2004 3 3 SWIA200412859 120040203A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 2 FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07461SW 7811 SPOILERON FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD. 2L72 4F RTA21EA 20040303002302004030300230 2004 3 3 SWIA200412860 420040205A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07293SW9033 9033 120320 COMPUTER FLAG ON F/O'S ADI INTERMITTENTLY. ASSOCIATED CAUTIONS AND A/P DISCONNECTED. RECEIVED ONE NOSE DOWN PITCH ABOUT 3 DEGREES AND THEN CORRECTED ITSELF. REMOVED AND REPLACED NR 2 A/P COMPUTER. OPS CHECKED GOOD ON GROUND TEST. P/N 622-8315-402, S/N ON 2468, S/N OFF 3300. 2L72 4T RTA31SO 20040303002312004030300231SO 2004 3 3 SWIA200412861 120040205A361032144143 SHUTOFF VALVE EMB 120 EMB120ER 3260203SO LT ENGINE MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07187SW9009 9009 120037 SMOKE IN COCKPIT AND CABIN WITH BOTH PACKS OFF. REMOVED AND REPLACED LT ENGINE PRESSURE REGULATOR SHUT OFF VALVE WITH SERVICEABLE UNIT IAW MM 36-10-04. OPS CHECKS GOOD AT THIS TIME. 2L72 4T RTA31SO 20040303002342004030300234NM 2004 3 3 DHL2004780003 120040228A7331 POWER SUPPLY BOEING727 727223 1384074NM FUEL FLOW FAILED A DHLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01780DH 22006 ALL THREE FUEL FLOW GAUGES WENT TO -0- CLIMBING THROUGH FL330, 28V DC AND 115 VAC FUEL FLOW CIRCUIT BREAKERS ARE POPPED. REPLACED FUEL FLOW POWER SUPPLY PER B-727 M/M 73-31-12. INDICATION NORMAL ON GROUND RUN-UP IAW JRH 5.2, AND GMM 20.4. 2L73 4F A3WE 20040303002382004030300238NM 2004 3 3 04FDEA00442 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002412004030300241NM 2004 3 3 04FDEA00445 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002422004030300242NM 2004 3 3 04FDEA00446 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002432004030300243NM 2004 3 3 04FDEA00447 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040304000022004030400002EU 2004 3 4 S9HA092987 120040219A6520350A33105803 BELLCRANK AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED B S9HAO OTHER O OTHER CRCRUISE 1 WP19358NT 1016 EMERGENCY ACTIONS EXC. ENGINE SHUTDOWN AT CRUISE AT APPROX. 110 KTS PILOT FELT THE AIRCRAFT YAW. PUSHING IN T/R PEDALS HAD NO EFFECT. PILOT CONTINUED STRAIGHT AND LEVEL FLIGHT TO MAIN BASE AND NOTIFIED COMPANY OF SITUATION. AFTER 5 ABORTED ATTEMPTS PILOT EXECUTED A RUN ON LANDING AND BROUGHT THE AIRCRAFT TO A STOP WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THE T/R GEAR BOX CONTROL LEVER HAD CRACKED, JUST AFT OF THE EXP PIN. 1G72 3U3 U H11EU E19EU 20040301002222004030100222NM 2004 3 1 SWAA040468 120040214A5311BAC1506 FRAME BOEING737 7373Q8 1384670NM BULKHEAD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND CHORD FORWARD OF THE PRESSURE BULKHEAD AT BS 1016, STRINGER 27R CORRODED. REMOVED AND REPLACED CHORD SPLICE PER SRM. 2L72 4F RTA16WE 20040301002312004030100231 2004 3 1 SWAA040477 420040215A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040301002362004030100236NM 2004 3 1 SWAA040482 120040215A27616544561 ACTUATOR BOEING737 7373Q8 1384670NM RT WING LEAKING A SWAAO OTHER K FLUID LOSS CRCRUISE 1 SW29689SW 23387 DECLARED EMERGENCY, A SYSTEM HYDRAULIC FAILURE, COMPLETE LOSS OF A SYSTEM HYDRAULIC FLUID AT FL 280, COMPLIED WITH QRH. REMOVED AND REPLACED NR 3 FLIGHT SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20040301002372004030100237NM 2004 3 1 SWAA040483 120040215A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STRINGER 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040301002392004030100239 2004 3 1 SWAA040445 420040212A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040304000062004030400006NE 2004 3 4 BAQA093233 220040117A73109550147560 SOLENOID VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE NR 1 ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 899 6036 2060 NR 1 ENGINE SMOKES ON SHUT DOWN. UNIT IS ORIGINAL EQUIPMENT ON ENGINE. ENG. TSI-898.6 REPLACED WITH SERVICEABLE UNIT. 02/24/2004 1G72 3U3 U H10EU E19EU 20040304000102004030400010 2004 3 4 BAQA092792 420040121A221041800468800 ACTUATOR AEROSPAS365 AS365N2 8680815EU ROLL INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 UNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 634) 1G72 3U RTH10EU 20040304000122004030400012EU 2004 3 4 BAQA092797 120040217A243523032048 STARTER GEN BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 STARTER GENERATOR WILL NOT START AIRCRAFT. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1G72 3U3 U H13EU E5NE 20040304000142004030400014EU 2004 3 4 BAQA092800 120040112A52101172427301 GUIDE BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE CREW DOOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1383 7243 GUIDE WORN BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1G72 3U3 U H13EU E5NE 20040304000152004030400015EU 2004 3 4 BAQA092801 120040112A521011724276101 GUIDE BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE CREW DOOR WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1383 7243 CREW DOOR GUIDE WORN BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1G72 3U3 U H13EU E5NE 20040304000162004030400016EU 2004 3 4 BAQA092802 120040217A7714645500071 TACH GENERATOR AEROSPAS365 AS365N2 8680815EU ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 TACH GENERATOR SCRAPPED, VELOCITY GENERATOR WAS SCRAPPED ON SITE IAW AEC, UNIT WAS REMOVED FOR NO NR INDICATION. REPLACED WITH UNIT FROM ASSET, ORDER TO REPLACE STOCK. 1G72 3U RTH10EU 20040304000192004030400019EU 2004 3 4 BAQA092757 120040202A2435 SHAFT UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03603ME115 Y20389 0284 STARTER GEN REMOVED FROM NR 2 ENG S/N PCEBJ108, HAS EXCESSIVE PLAY IN THE SHAFT. HARDCARD ENCLOSED REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1G72 3U3 U H88EU E42NE 20040304000512004030400051NM 2004 3 4 237TR0002 120040224A7931ST1042 TRANSMITTER BOEING737 737228 13844AGNM PWA JT8 JT8D15 52051NE NR 1 ENG OIL INOPERATIVE A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05237TR 23007 DURING TAKE OFF AT 90KTS. NR 1 ENGINE OIL PRESSURE DROPPED SLOWLY OUT OF THE GREEN ARC TO MID YELLOW. T/O ABORTED. OIL PRESSURE STABILIZED AT THE BOTTOM OF THE YELLOW ARC. 35PSI AT IDLE. REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW MM. OPS AND LEAK CHECK NORMAL. 2L72 4F4 FRTA16WE E2EA 20040304000522004030400052NM 2004 3 4 P5CA041045 120040224A3310 CIRCUIT CARD BOEING747 747341 13848AMNM INDICATOR LIGHTSLOOSE A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 INDICATOR LIGHTS PILOTS AND FLT ENGINEERS CIRCUIT BREAKER POPS AND WILL NOT RESET. RESEATED THE A-10 CARD IN THE MASTER DIM AND TEST BOX. SYS CKS OK IAW MM. 2L74 4F RTA20WE 20040304000562004030400056CE 2004 3 4 CED2004F00000 120040108A3244301336340 TIRE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NLG SEPARATED E CEDAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO05233CA 133 251414A ON CLIMB OUT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR NUMEROUS TIMES WITH NO CHANGE IN THE UNSAFE INDICATION, THEY THEN RETURNED WITHOUT INCIDENT AND NOTICED THE NOSE WHEEL TIRE WAS MISSING TREAD. UPON INSPECTION OF THE AIRCRAFT, FOUND THE TREAD FROM THE NOSE WHEEL TIRE HAD KEPT THE NOSE GEAR DOOR FROM CLOSING. REMOVED AND REPLACED THE NOSE WHEEL TIRE ASSEMBLY. SERVICED THE TIRE AND STRUT ASSEMBLIES. 2L72 4J4 J A10CE 1E16 20040304000572004030400057EU 2004 3 4 G1F2004F00001 120040209A7810FGFB582800D2 TAILPIPE AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 3 ENGINE CORRODED B G1FRK NONE O OTHER ININSP/MAINT 1 GL13312P 67 IT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC. THE PAINT HAS BEEN BUBBLING AND THE STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON AC, ALL OF THE CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. THE AREA OF CORROSION IS 19 INCHES LONG AND 7.5 INCH WIDE. THE CORRODED AREA IS AT THE 3 OCLOCK POSITION ON THE NR 1 ENGINE. VIEW LOOKING FORWARD, AT THE 12 OCLOCK POSITION ON THE NR 2 ENGINE, VIEW LOOKING FORWARD, AND THE 9 OCLOCK POSITION ON THE NR 3 ENGINE, VIEW LOOKING FORWARD. THE HEAT FROM THE ENGINE EXHAUST IS CAUSING THE PAINT TO PEEL, ALLOWING MOISTURE INTRUSION UNDER THE FASTENER HEADS. BLENDED AREA RESULTS SUBMITTED FOR REVIEW AND DISPOSITION. 2L73 4F4 FRTA46EU E1NM 20040304000622004030400062EA 2004 3 4 COMA0460165 120040216A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA LYC O360 O360A1D 41514EA LT WING DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01971CA 7145 FRETTING DAMAGE NOTED ON LT LOWER WING ACCESS HOLE CUTOUT AT 540CB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030. 2L72 4F3 ORTA21EA E286 20040304000642004030400064EA 2004 3 4 COMA0460167 120040222A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE MISLOCATED A COMAK NONE O OTHER ININSP/MAINT 1 SO01819CA 7415 FUSELAGE STATION 574 HAS A MISDRILLED HOLE AT STRINGER 14. COMPLIED WITH REO 601R-53-61-927 FOR REPAIR OF FUSELAGE STATION 574 AT STRINGER 14. PRIMED AND TOPCOATED IAW CRJ SRM 51-25-01. 2L72 4F RTA21EA 20040304000662004030400066EA 2004 3 4 COMA0460168 120040216A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01971CA 7145 LT FRAME FLANGE CRACKED BETWEEN STRINGERS 11 AND 12. REPAIRED REO 601R-53-61-193. 2L72 4F4 FRTA21EA E15NE 20040304000992004030400099EU 2004 3 4 MALA040206 120040205A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 FS 317 LT FUSELAGE 6 INCHES BELOW STR SL1632 DENT OUT OF LIMITS. CUT OUT DAMAGED AREA FABRICATED AND INSTALLED A DOUBLER REPAIR IAW EO NR S53005. A/C RELEASE DATE 2/26/04. REFER TO LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20040304001022004030400102EU 2004 3 4 MALA040208 120040210A5347 SEAT TRACK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 FS 294 LT SEAT TRACK HAS CORROSION. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW EO NR S53060. A/C RELEASE DATE 2/26/04. REFER TO LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20040304001122004030400112WP 2004 3 4 GTIA040120 120040111A5312 STANCHION DOUG DC9 DC983 3022083WP BULKHEAD CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND MID PIT BULKHEAD FRAME STANTION IS CRACKED LEFT. STOP DRILLED CRACK. FABRICATED REPAIR ANGLES. INSTALLED REPAIR ANGLES. (M) 2L72 4F RTA6WE 20040304001152004030400115WP 2004 3 4 GTIA040112 120040113A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND FLOOR PANEL OUTBOARD STATION 800 STIFFENER DEATTACHED IN 2 AREAS. REBONDED STIFFENER. (M) 2L72 4F RTA6WE 20040304001162004030400116WP 2004 3 4 GTIA040117 120040109A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND CORROSION ON CABIN FLOOR SUPPORT FS 200 55 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040304001172004030400117WP 2004 3 4 GTIA040121 120040115A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND RIGHT OUTBOARD FLOOR PANEL STATION 120 DELAMINATED AND THREE DAMAGED INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040304001192004030400119WP 2004 3 4 GTIA040100 120040108A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FLOOR PANEL UNDER F/O SEAT CORROSION AND GOUGE IN UPPER SURFACE. BROKEN TRIM SUPPORT. DISBONDED INNER SIDE STRIPS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040304001202004030400120WP 2004 3 4 GTIA040101 120040104A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP COCKPIT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01819NK 48016 GTIA - FOUND COCKPIT FLOOR PANEL 4411C CORRODED, CRACKED. BONDED CRACKED AREA. (M) 2L72 4F A6WE 20040304001232004030400123WP 2004 3 4 GTIA040107 120040113A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND FLOOR PANEL RIGHT OUTBOARD STATION 927 STIFFENER DETACHED AND CENTER STIFFENER 3 AREAS OF INCORRECT REPAIRS. REMOVED DAMAGED STIFFENER. FABRICATED NEW STIFFENER. INSTALLED NEW STIFFENER. (M) 2L72 4F RTA6WE 20040304001252004030400125WP 2004 3 4 GTIA040110 120040111A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND MAIN CABIN STATION 875 TO STATION 1309 LBL 22 INCHES INBOARD SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORRODED BARE METAL. SEAT TRACK OUT OF LIMITS STATION 937 TO 1022 LBL 22. REMOVED SEAT TRACK. FABRICATRED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F RTA6WE 20040304001262004030400126WP 2004 3 4 GTIA040111 120040115A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND CENTER FLOOR PANEL STATION 860 UPPER DOUBLER CRACKED AND BOTTOM LEFT AND RIGHT STIFFENERS CRACKED IN SEVERAL AREAS. REPLACED UPPER DOUBLER BOTTOM LEFT AND RIGHT STIFFENERS. (M) 2L72 4F RTA6WE 20040304001292004030400129WP 2004 3 4 GTIA040104 120040115A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE PEELING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD RIGHT AFT STATION 1307 PEELING FIBERGLASS. REQUIRES EDGE FILLER. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040304001302004030400130WP 2004 3 4 GTIA040108 120040115A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND LEFT CAPTAIN FLOOR PANEL BRACKET MISSING AND BOTTOM STIFFENERS DETACHED. REATTACHED BOTTOM STIFFENERS. INSTALLED NEW BRACKET. (M) 2L72 4F RTA6WE 20040304001312004030400131WP 2004 3 4 GTIA040109 120040115A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FOUND CENTER FLOOR PANEL STATION 800 BOTTOM LEFT AND RIGHT SUPPORT STIFFENERS CRACKED IN SEVERAL AREAS. REMVOED AND REPLACED SUPPORT STIFFENERS. (M) 2L72 4F RTA6WE 20040304001352004030400135WP 2004 3 4 GTIA040126 120040115A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND CENTER FLOOR PANEL STATION 927 DELAMINATED AND DAMAGED EDGE FILLER. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040304001422004030400142WP 2004 3 4 ASAA0480003 120040103A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 12 AND 13. RECONNECTED LOOSE LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040304001562004030400156WP 2004 3 4 GTIA040130 120040210A3260833703 SENSOR DOUG DC9 DC983 3022083WP MLG INDICATOR FAULTY A GTIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23833NK 49449 DTW - FOUND LEFT MAIN GEAR UNSAFE LIGHT ON AFTER GEAR RETRACTION-RECYCLED REMAINED IN UNTIL OUT AT 13000 FEET, NO OTHER ABNORMAL INDICATION SWITCH ON APPROACH CYCLED GEAR NO PROBLEM WITH LIGHTS, ALL NORMAL. T/A FOUND D1-26 L MAIN GEAR UP AND LATCHED SENSOR FAULTY, REMOVED AND REPLACED SENSOR. OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20040304001612004030400161WP 2004 3 4 GTIA040124 120040111A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND MAIN CABIN FS 1200 WEB CRACKED L18L. STOP DRILLED CRACK. FABRICATED, LOCATED AND DRILLED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20040304001702004030400170WP 2004 3 4 DHL2004806576 120040125A574057547052 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT INBOARD STUB WING FITTING CRACK 4.000 STA XW 223.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM PO201953, DWG 5754705. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW ATM PO201953, DWG 5754705. PERFORMED NDT INSPECTION IAW DC8 SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040304001742004030400174WP 2004 3 4 DHL2004806582 120040126A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT WING TOP PANEL PLATING CORROSION, STA XRS 204.000 S-9 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-11, DWG U80-R11. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED AREA IAW ED EDU80-11, DWG U80-R11. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (7075-T6AL 0.160) IAW ED EDU80-11, DWG U80-R11. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR DOUBLER IAW ED EDU80-11, DWG U80-R11, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040304001782004030400178WP 2004 3 4 DHL2004806581 120040127A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING OUTBOARD L/E LOWER PART CORRODED STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED EDU80-13, DWG U80-R13. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW ED EDU80-13, DWG U80-R13. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDU80-13, DWG U80-R13, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1.2L74 4F RT4A25 20040304001792004030400179WP 2004 3 4 DHL2004806586 120040205A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT FWD CTR SECTION FLOORBEAM CRACKED 0.500 STA 120.000, LBL 32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01-001. FABRICATED 1EA SPACER (7075-T6 0.142), 2EA FILLERS-FWD (7075-T6 0.071), SPACER AFT (7075-T6 0.071), 2EA SPLICE DOUBLER FWD-AFT ( 7075-T6 0.071), -T- FILLER (7075-T6 0.125) AND 2EA ANGLE DOUBLER FWD-AFT ( 7075-T6 0.160) IAW ED EDU80-5, DWG U80-R05. CLEANED, TREATED AND PRIMED AREA AND FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FABRICATED PARTS WITH NEW FASTENERS. 2L74 4F RT4A25 20040304001802004030400180WP 2004 3 4 DHL2004806588 120040205A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT FWD CENTER SECTION FLOORBEAM CRACKED 3.000 AT STA 140.000 LBL 32. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. INSPECTED FOR CRACK IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. FABRICATED 2EA ANGLE DOUBLER (7075-T6 0.160), 2EA FILLER-FWD/AFT ( 7075-T6 0.071), 2EA SPLICE DOUBLER-FWD/AFT (7075-T6 0.071), 1EA FILLER -T- (7075-T6 0.125), 1EA CLIP (7075-T6 0.090) AND 1EA SPACER (7075-T6 0.142) IAW ED EDU80-4, DWG U80-R04. CLEANED, TREATED AND PRIMED AREA AND FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED PARTS ON FLOORBEAM STA 140.000 LBL 32 WITH NEW FASTENERS. 2L74 4F RT4A25 20040304001832004030400183WP 2004 3 4 DHL2004806574 120040127A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FWD CARGO COMPT -A- BELLY DOOR LOWER PART EXTERNAL SKIN, STA 290.000 - 300.000, L31-L32R CRACKED 0.70 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDU80-10, DWG U80-R10. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMENT IAW ED-EDU80-10, DWG U80-R10 (7075-T6AL 0.050). CLEANED, TREATED AND PRIMED AREA AND NEW SKIN SEGMENT IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGMENT IAW ED-EDU80-10, DWG U80-R10, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040304001842004030400184WP 2004 3 4 DHL2004806547 120040115A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 INTERIM REPAIR ON RIGHT INBOARD FLAP UPPER SURFACE STA XW 104.000-122.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-T3AL 0.040) IAW SRM 57-7-1 FIG 1. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INNER SURFACE IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001862004030400186WP 2004 3 4 DHL2004806554 120040112A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING INBOARD FLAP UPPER SKIN WORN AT STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED WORN SKIN IAW SRM 51-1-21, SRM 51-3-0 PG 1. FABRICATED NEW SKIN (2024-T3AL 0.040) IAW SRM 57-7-1 FIG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SKIN WITH NEW FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001882004030400188WP 2004 3 4 DHL2004806553 120040112A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING OTBAORD L/E CORRODED AT STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2H. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. REMOVED EXISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW SRM 57-2-1 FIG 2H. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 2H, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040304001912004030400191WP 2004 3 4 DHL2004806559 120040111A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 4 FLOOR TRACK LUGS WORN (STA 1680.000-1702.000). REMOVED NR 4 FLOOR TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001922004030400192WP 2004 3 4 DHL2004806558 120040121A5347S4889185 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 UPPER CARGO COMPT NR 6 FLOOR TRACK LUGS WORN (STA 1570.000-1590.000). REMOVED DAMAGED TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK SEGMENT IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. 2L74 4F RT4A25 20040304001932004030400193WP 2004 3 4 DHL2004806560 120040110A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 NR 4 FLOOR TRACK LUG WORN STA 990.000-930.000 (MAIN CARGO COMPT). TRIMMED OUT DETERIORATED TRACK SEGMENT IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED SPLICES (7075-T6AL 0.100) (7075-T6AL 0.125) (7075-T6AL 0.160) IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED NEW TRACK SEGMENT AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001952004030400195NM 2004 3 4 SWAA040401 120040207A3350610478 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29415WN 29836 DURING SCHEDULED MV 1, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040304002022004030400202NM 2004 3 4 SWAA040286 120040129A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE BUSHING PER MM. 2L72 4F RTA16WE 20040304002062004030400206NM 2004 3 4 SWAA040290 120040129A5753 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040304002072004030400207NM 2004 3 4 SWAA040291 120040129A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACK AT BS 920, BETWEEN STRINGERS 24R AND 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040305000022004030500002NM 2004 3 5 AWXA200400172 120040211A3040233N32128 CONTROL PANEL BOEING757 757225 1384959NM WINDOW HEAT FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28914AW4508 653 22208 ON CLIMBOUT, RECEIVED FRM 30-41-02-03 EICAS MESSAGE, RT FORWARD WINDOW DISPLAYED INOPERATIVE LIGHT ILLUMINATED, WINDOW HEAT COULD NOT BE RESET, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL IAW BMM 30-41-02, SYSTEM OPERATIONAL CHECK WAS GOOD. VISUAL INSPECTION AND FUNCTIONAL TEST OF WINDOW HEAT CONTROL PANEL S/N D00016 WAS NO FAULT FOUND. UNIT WAS DISASSEMBLED AND INSPECTED FOR INTERNAL DAMAGE, NO DAMAGE WAS NOTE. REASSEMBLED UNIT, TESTED, AND RETURNED TO SERVICE IAW CMM 30-41-71, REV. 011. 2L72 4F RTA2NM 20040305000032004030500003NM 2004 3 5 AWXA200400173 120040212A3397BR963180 WIRE HARNESS BOEING737 7373S3 1384711NM SEAT ROW 1 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 PHX - EEL - DURING A-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 1 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040305000052004030500005NM 2004 3 5 SWAA040292 120040129A53206545409 WEB BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663.5, LBL 40. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040305000082004030500008NM 2004 3 5 SWAA040295 120040129A52426545830 SKIN BOEING737 7373H4 1384600NM E/E DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND E&E DOOR SKIN CRACKED NEAR AFT EDGE. REPAIRED DOOR SKIN PER SRM. 2L72 4F RTA16WE 20040305000092004030500009 2004 3 5 SWIA200412863 420040203A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07251YV4007 4007 120251 CAPTAIN AUTOPILOT FAILED, -E- ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED NR 1 APC-65 WITH SERVICEABLE UNIT IAW MM 22-10-00. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20040305000102004030500010 2004 3 5 SWIA200412864 420040204A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER DISCONNECTED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07946SW 7776 YAW DAMPER NR 1 WOULD NOT RESET AFTER IT DISCONNECTED. REPLACED NR 1 YAW DAMPER WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040305000122004030500012SO 2004 3 5 SWIA200412866 120040205A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT FAILED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07292SW6001 6001 120319 MID SECTION OF EMERGENCY LIGHTS FAILED TO TEST. REPLACED AND SECURED MID CABIN EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. 2L72 4T RTA31SO 20040305000132004030500013EA 2004 3 5 SWIA200412867 120040207A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07939SW77 77 7742 INBOARD GROUND SPOILER AND SPOILERON MESSAGE AFTER LANDING. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE UNIT IAW MM 27-61-05. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20040305000172004030500017EA 2004 3 5 SWIA200412871 120040206A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM ACT MALFUNCTIONED A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07449SW 7699 STAB CH 1 INOP, STATUS MESSAGE. WOULD NOT RE-ENGAGE DUE TO CIRCUIT BREAKER BEING POPPED. RETURNED TO SLC. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00 AND 27-42-01 AND 27-42-05. 2L72 4F RTA21EA 20040305000182004030500018SO 2004 3 5 SWIA200412872 120040207A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07561SW8359 1518 120335 EMERGENCY EXIT SIGN LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED MIDDLE ELBP WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040305000222004030500022EA 2004 3 5 SWIA200412876 120040209A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INTERMITTENT A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07588SW 7069 CAPTAIN'S TRIM SWITCH INTERMITTENT. REMOVED AND REPLACED CAPTAIN'S STAB TRIM SWITCH IAW 27-41-05. OPS CHECK GOOD. P/N 309-4334. 2L72 4F RTA21EA 20040305000232004030500023SO 2004 3 5 SWIA200412877 120040207A2422PC2511C INVERTER EMB 120 EMB120ER 3260203SO MALFUNCTIONED A SWIAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 NM07584SW9211 9211 120352 PILOT REPORTS SEVERAL AUTO PILOT FAILURES ON BOTH SIDES WITH ASSOCIATED FD AND OTHER FLAGS. REMOVED AND REPLACED NR 1 INVERTER DUE TO POSSIBLE A/C POWER PROBLEMS TO AHRS AND AUTOPILOT COMPUTERS. OPS CHECK OF INVERTER AND A/P GOOD. REF EMB MM 120 24-21-01. 2L72 4T RTA31SO 20040305000252004030500025NM 2004 3 5 DHL2004740002 120040217A29101711418CR0360 LINE BOEING727 7272Q9 138448MNM HYD SYSTEM LEAKING A DHLAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO01740DH 21930 B-SYSTEM BOTH LOW PRESSURE LIGHTS ILLUMINATED AT START OF TAKEOFF ROLL. PRESS DROPPED 200 LBS. OPENED BRAKE INTERCONNECT A-SYSTEM DROPPED TO 1 GALLON INTERCONNECT. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE NR 2 B-PUMP REF M/M 20-10-12, NO LEAKS NOTED. P/N: 171141-8CR0360. RTO, NO AIRSPEED, HAD JUST MOVED TRUST LEVER FORWARD WT: 136,620, NO AIRSPEED, -1C, AND PRESS ALTITUDE 5,000 FT. NOT REQUIRED DUE TO NO AIRSPEED IAW M/M 5-51-121. 2L73 4F RTA3WE 20040305000272004030500027EU 2004 3 5 AWXA200400184 120040218A3350 BATTERY PACK AIRBUS320 A320231 3930325EU ZONE 221 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28620AW3203712205 052 PHX - EEL - DURING 4-DAY CHECK EMERGENCY LIGHT TEST AT FORWARD FLIGHT ATTENDANT PANEL FAILED DISPLAYING MESSAGE -L COMM FAULT-. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY LIGHT BATTERY PACK AND EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040305000282004030500028WP 2004 3 5 04FDEA00431 120040218A2780894601 PROXIMITY SWITCH DOUG DC10 DC1030 3023501WP SLATS MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25312FE2784 2784 48300 ON TAKEOFF OUT OF OAK, SLATS DID NOT RETRACT. ALERT FOR SLAT DISAGREE. RAN THE QRH CHECKLIST AND RETURNED TO OAK. CYCLED TWICE. CHECKED PSEU & FCC 1 & 2. PERFORMED PSEU RTS, ALL NORMAL. TESTED SLAT SENSORS MM 27-84-02-5, ALL NORMAL. PERFORMED RTS OF SLAT SYS IN BOTH FCC-1 & 2, ALL NORMAL. NOTICED IN ACARS THAT ALL B-SENSORS SHOWED 0 WITH SLAT HANDLE IN RETRACT POS. FLIGHT CREW VERIFIED SLATS FOLLOWING COMMANDED POSITION, NO BUFFETING APPEARS A DISAGREEMENT INSIDE PSEU INDICATIONS MM 31-71-01-2 AND 45-45-01. REMOVED AND REPLACED PSEU RTS AND CONFIG CODE NORMAL. COMFIRMED BAD PSEU, PSEU SENSOR READOUT L2A NOW SHOWS OK (00) MM 31-71-01-2. 2L73 4F A22WE 20040305000292004030500029NM 2004 3 5 04FDEA00430 120040218A5320WSP0668501 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 FLOOR SUPPORT PLATE ASSY LOCATED BELOW LAVATORY AT STA 427 RT X=21 WAS CORRODED WITH A THRU HOLE. FLOOR SUPPORT AT STA 427 RT X = 21 REMOVED AND REPLACED IAW SRM 51-33-01 VOL II 2L73 4F RTA22WE 20040305000302004030500030NM 2004 3 5 04FDEA00429 120040218A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. LT WING - OUTBOARD TRAILING EDGE FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040305000312004030500031NM 2004 3 5 04FDEA00428 120040218A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING : OUTBOARD TRAILING EDGE FLAP STOP FITTING FOUND CRACK. RT WING OUTBOARD TRAILING EDGE FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II 2L73 4F RTA22WE 20040305000322004030500032NM 2004 3 5 04FDEA00427 120040218A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - NR 2 SLAT WITH CRACK AT 02 PLACES: 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLAT FROM SLAT TRAILING EDGE 3 INCHES FROM OUTBD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE 2 INCHES FROM OUTBD EDGE AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20040305000332004030500033NM 2004 3 5 04FDEA00426 120040218A5712ARB2850505 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING, CRACK FOUND ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM 51-33-01, VOL.II AND DRAWING ARB2873. COMPLIED WITH EA 1-5750-74325, WINGS - LT SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK. 2L73 4F RTA22WE 20040305000342004030500034NM 2004 3 5 04FDEA00425 120040218A5740ARB777296 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING: LOWER WINGLET AT FWD FITTING FOUND CRACKED. 2L73 4F RTA22WE 20040305000372004030500037NM 2004 3 5 04FDEA00421 120040218A5740 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING - LOWER WINGLET AT FORWARD FITTING FOUND CRACKED. 2L73 4F RTA22WE 20040305000382004030500038NM 2004 3 5 04FDEA00420 120040218A5754 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING NR 2 SLAT CRACK AT 02 PLACES; 2 INCHES FROM SLAT TRAILING EDGE, 3 INCHES FROM OUTBOARD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE, 2 INCHES FROM OUTBOARD EDGE. REMOVED CRACKED SEAL AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SEAL AT LT WING NR 2 SLAT FROM SLAT TRAILING EDGE 3" FROM OUTBD EDGE AND 3 INCHES FROM SLAT TRAILING EDGE 2 INCHES FROM OUTBD EDGE AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20040305000432004030500043NM 2004 3 5 DHL2004783002 120040218A7714 INDICATOR BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE ENGINE N2 MALFUNCTIONED A DHLAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 SO01783DH 21999 708917 DURING NR 3 ENGINE START, ENGINE ROLLED BACK AND SHUT ITSELF DOWN. N2 WAS AT 51 PERCENT AT THE TIME, 2ND START WAS NORMAL. INSPECTED INTAKE AND EXHAUST; NO OBVIOUS DEFECTS. SERV FUEL CONTROL BURNER PRESS BELLOWS PER P&W JT8D M/M 73-21-01. DURING ENGINE START FOUND NR 3 N2 INDICATOR SLOW TO RESPOND. REMOVED AND REPLACED NR 3 N2 INDICATOR PER BMM 77-12-0. RAN ENGINE SEVERAL TIMES PER DHL JRH CHAPTER 5. NO DEFECTS NOTED. 2L73 4F4 F A3WE E2EA 20040305000442004030500044EU 2004 3 5 AWXA200400192 120040209A5347D53472209201 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM SEAT RAIL AT FR 66, Y1292 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM SEAT RAIL AT FR 66, Y1292 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM SEAT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 9-14, 16 & 17, PG 7-10, 12. 2L72 4F RTA28NM 20040305000452004030500045EU 2004 3 5 AWXA200400193 120040209A5320D5348004320501 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SILL AT FR 66, Y1732 RT, FORWARD OF R-2 DOOR. MAINTENANCE REMOVED R-2 DOOR LOWER SILL AT FR 66, Y1732 RT; FABRICATED A NEW REPLACEMENT LOWER SILL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 9-14, 16 & 17, PG 6, 7-10 & 12. 2L72 4F RTA28NM 20040305000502004030500050NM 2004 3 5 AWXA200400198 120040215A2751 CONNECTOR BOEING737 73733A 1384673NM TE FLAP LOOSE A AWXAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28174AW 23633 PHX - EMERGENCY LANDING - FLT 0769 - ON APPROACH INTO PHX EN ROUTE FROM MZT TRAILING EDGE FLAPS WENT ASYMMETRIC BETWEEN FLAP POSITION 1 & 2. ABORTED APPROACH AND RECYCLED FLAPS WITH SAME RESULTS, ACCOMPLISHED TRAILING EDGE FLAP ASYMMETRICAL CHECKLIST AND AS A PRECAUTION DECLARED EMERGENCY, LANDED FLAPS 1. MAINTENANCE FOUND CONNECTOR LOOSE ON LT FLAP POSITION TRANSMITTER. CLEANED AND RE-SECURED CANNON PLUG, CYCLED FLAPS SEVERAL TIMES WITH NO FAULTS NOTED. 2L72 4F RTA16WE 20040305000512004030500051NM 2004 3 5 04FDEA00432 120040219A5754 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. 2L73 4F RTA22WE 20040305000532004030500053NM 2004 3 5 04FDEA00434 120040219A5754 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. 2L73 4F RTA22WE 20040305000542004030500054NM 2004 3 5 04FDEA00448 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000622004030500062SO 2004 3 5 C2XA04TY037 120040218A531514522459003 FLOORBEAM EMB 145 EMB145LR 3260212SO FRAME 20 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713553 145585 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOORBEAM RAMP ANGLE. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040305000632004030500063SO 2004 3 5 C2XA04TY038 120040218A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713553 145585 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040305000642004030500064SO 2004 3 5 C2XA04SH075 120040220A491014526850401 FIREWALL EMB 135 EMB135LR 3260305SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT VERTICAL SUPPORT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040305000662004030500066GL 2004 3 5 C2XA04IA013 220040218A7200 ENGINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 DEFECTIVE A C2XAEA ENGINE SHUTDOWN UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27139703956 145146 CAE312153 LCH-FLIGHT 970, THE CREW REPORTED SMOKE IN THE CABIN, THE CREW SHUT DOWN THE NR 2 ENGINE, AND DIVERTED TO LCH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040305000702004030500070NM 2004 3 5 04FDEA00461 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000712004030500071NM 2004 3 5 04FDEA00462 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000732004030500073NM 2004 3 5 04FDEA00464 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000742004030500074NM 2004 3 5 04FDEA00465 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000762004030500076NM 2004 3 5 04FDEA00467 120040220A5310 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN - BASE SECTION OF CHILLER COMPARTMENT AT GALLEY ASSEMBLY BULGING, CORROSION UNDERNEATH. 2L73 4F RTA22WE 20040305000782004030500078NM 2004 3 5 04FDEA00469 120040220A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 AFT CARGO WASTE TANK COMPARTMENT LT STA 1961, LONGERON 36 HAS CORROSION. 2L73 4F RTA22WE 20040305000792004030500079NM 2004 3 5 04FDEA00470 120040220A5310 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 AFT CARGO WASTE TANK COMPARTMENT LT STA 1961, LONGERON 37 HAS CORROSION. 2L73 4F RTA22WE 20040305000802004030500080WP 2004 3 5 04FDEA00477 120040220A5210 SEAL DOUG DC10 DC1030 3023501WP OOOR FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25304FE 46992 CLIMBOUT AT APPROXIMATELY FL 210, AIRCRAFT ALTITUDE WAS CLIMBING AT 1000 FPM. SECOND PACK BROUGHT ON LINE AND CABIN STILL CLIMBING AT 500 FPM, LEVELED AT FL 330. UNABLE TO STOP CABIN ALTITUDE FROM INCREASING TOWARD 10,000 FEET, RETURNED LAX AND LANDED WITHOUT INCIDENT. FOUND LARGE AIR LEAK COMING FROM L-3 PASSENGER PLUG DOOR. REMOVED DOOR AND FOUND ENTIRE BOTTOM PORTION OF DOOR SEAL MISSING. REMOVED AND REPLACED SEAL PER M/M 52-10-01-2. PRESSURIZED A/C, MUCH BETTER BUT STILL ON THE WEAK SIDE. FOUND OUTFLOW VALVE LEAKING PROFUSELY WHEN FULLY CLOSED. REMOVED AND REPLACED OUTFLOW VALVE PER M/M 21-31-08-2. PRESSURIZED A/C AND SYSTEM OPS CHECKS NORMAL PER M/M 21-31-05-2. 2L73 4F A22WE 20040305000812004030500081EA 2004 3 5 SWIA200412882 120040207A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07907SW 7511 RIGHT WING CENTER EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED RT WING CENTER EMERGENCY LAMP AS REQUIRED. OPS CHECK GOOD. 2L72 4F RTA21EA 20040305000852004030500085EA 2004 3 5 SWIA200412886 120040208A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07442SW 7609 OVERHEAD EMERGENCY LIGHT AT ROW 5 INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT LAMP. OPS CHECK GOOD. 2L72 4F RTA21EA 20040325001182004032500118EU 2004 3 25 BAQA092534 120040205A793153408 TRANSMITTER AEROSPAS365 AS365N2 8680815EU OIL PRESSURE READS HIGH B BAQAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA03915ME888 6417 OIL PRESS READ HIGH, INTERMITTENT. REPLACED WITH SERVICEABLE ASSET UNIT. 02/26/2004 1G72 3U RTH10EU 20040325001312004032500131EU 2004 3 25 BAQA092750 120040303A6210117151451 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR OUT OF TRACK B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03911TG178 7506 RETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, BLADE WOULD NOT TRACK. REPLACED WITH ANOTHER RENTAL BLADE (S/N 2413) 1G72 3U NCH13EU 20040325001322004032500132EU 2004 3 25 BAQA092751 120040303A6210117151451 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR OUT OF TRACK B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03911TG 7506 RENTAL 117-151451V001 S/N 2622 RENTAL CHARGE 36.75 HR REPLACEMENT VALVE RETURN OF RENTAL BLADE AFTER .4 HOURS OF USE, WOULD NOT TRACK REPLACED WITH ANOTHER RENTAL BLADE (S/N 2419) 1G72 3U NCH13EU 20040325001342004032500134EU 2004 3 25 BAQA093636 120040217A6210117151321 BLADE BOLKMSBK117 BK117C1 5626025EU MAIN ROTOR OUT OF TRACK B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG2814 7506 WARRANTY REPAIR/EXCHANGE : S/N 198 ; BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. SINCE FEBRUARY 21,200 BLADE HAS ACCUMULATED ONLY 279.8 HOURS BUT HAS BEEN REMOVED FROM SIX DIFFERENT AIRCRAFT FOR REPAIR WITH THIS BEING THE SEVENTH TIME. THIS TIME BLADE WAS INSTALLED FOR A TOTAL OF 1.8 HOURS ON N911TG/7506. LAST REPAIR 9-090000-65 S/N 2254 ; BLADE WILL NOT TRACK, CLIMBS AND DIVES FROM GROUND TO HOVER TO FLIGHT. WE RECEIVED BLADE ON EXCHANGE UNDER OUR PO 8-080107-53. BLADE WAS INSTALLED FOR A TOTAL OF 1.8 HOURS ON N911TG/7506. BLADE HAS ACCUMULATED ONLY 19.3 HOURS BUT HAS BEEN REPAIRED THREE TIMES SINCE 11/13/2001. 1G72 3U NCH13EU 20040325001522004032500152EU 2004 3 25 BAQA092788 120040212A28200319738350 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE FUEL SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME62 0143 30166 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. REPLACED WITH SERVICABLE UNIT. 02/19/2004 1G72 3U3 U H88EU E19EU 20040325001532004032500153EU 2004 3 25 BAQA092789 120040212A28200319738340 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1B2 60030NE FUEL SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME62 0143 30166 NR 1 ENGINE WILL NOT LIGHT OFF ON ALL START ATTEMPTS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/19/2004 1G72 3U3 U H88EU E19EU 20040326000062004032600006EU 2004 3 26 CX7A194J0418 120040318A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AO OTHER N FALSE WARNING NRNOT REPORTED 1 GL03307CE 340B204 AFTER FIRE TEST LEFT TAILPIPE HOT LIGHT STAYS ON. 2L72 4T RTA52EU 20040326000082004032600008NM 2004 3 26 MWEA040026 120040319A3230 VALVE BOEING717 717200 1383700NM ANTI-SKID SYS MALFUNCTIONED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31908ME 55172 ANTI-SKID FAIL ALERT ILLUMINATED. REMOVED AND REPLACED ANTI-SKID RETURN VALVE. 2L72 4F TRA6WE 20040326000112004032600011EA 2004 3 26 COMA0460205 120040317A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01498CA 7792 DAMAGED STRUCTURE ON RIGHT SIDE OF FUSELAGE AT FS 640 AND FS 672.2. REPAIRED STRUCTURE DAMAGE ON RIGHT SIDE FS 640 AND 672.2 IN ACCORDANCE WITH REO 601R-53-61-956. 2L72 4F RTA21EA 20040326000252004032600025NM 2004 3 26 2004UALA00237 120040315A5320 FLOOR SUPPORT AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29825UA 980 CABIN FLOOR SUPPORT CORRODED AT FRAME 66 AT RBL 40. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA28NM E40NE 20040326000262004032600026NM 2004 3 26 2004UALA00238 120040315A5320 FLOOR SUPPORT AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29825UA 980 CABIN FLOOR SUPPORT CORRODED AT FRAME 68 AT RBL 40. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA28NM E40NE 20040326000332004032600033NM 2004 3 26 2004UALA00245 120040313A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSLEAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 STRINGER, BS 380 STR 24L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SECTION & STRINGER SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040329000032004032900003EA 2004 3 29 ASOA04108 120040210A53206013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 621-625.30 NEAR STRINGERS 14L AND 14R WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTALS AT FS 621-625.30 NEAR STRINGERS 14L AND 14R. (M) 2L72 4F RTA21EA 20040329000072004032900007NE 2004 3 29 ASOA04097 220040207A72616087T04P05 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE CLOGGED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11866AS6503 7517 FLT 4553 - DURING CRUISE FROM DTW-DFW, AT APPROXIMATELY 31,000 FEET THE CREW RECEIVED A RIGHT ENGINE LOW OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE FLUCTUATED BETWEEN 25-33 PSI OCCASIONALLY DROPPING BELOW 25 PSI AND THEN SLOWLY DECREASING. OIL TEMPERATURE WAS SLIGHTLY ELEVATED ON THE RIGHT ENGINE TO AROUND 135 DEGREES. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO CVG, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LUBE AND SCAVENGER PUMP ON THE RIGHT ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040329001102004032900110EU 2004 3 29 CX7A194J0417 120040316A242031342001 GENERATOR SAAB SF340 340B 7860101EU LEFT FAILED A CX7AA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 GL03306CE145131 340B203 AFTER T/O LEFT AC GENERATOR LIGHT ILLUMINATED UNABLE TO RESET. 2L72 4T RTA52EU 20040329001152004032900115EA 2004 3 29 COMA0460210 120040318A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01934CA 7042 FLIGHT 5103, AFTER LANDING AT ATL RECEIVED A FLAP FAIL CAUTION WHEN EXISTING RUNWAY. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20040329001162004032900116EA 2004 3 29 COMA0460213 120040318A2613 SENSOR CNDAIRCL600 CL6002B19 1900309EA RT WING MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01917CA 7017 FLIGHT 5505 RECEIVED AN ANTI-ICE DUCT CAUTION DURING CLIMBOUT OF CVG, AIRCRAFT RETURNED TO THE FIELD. REPLACED 21 RIGHT WING HEAT SENSORS. 2L72 4F RTA21EA 20040329001232004032900123EU 2004 3 29 CX7A194J0409 120040120A7160 RING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE INV ACTUATOR MISSING A CX7AO OTHER O OTHER NRNOT REPORTED 1 GL03315CE 691 340B343 785192 RIGHT ENGINE IGV ACTUATOR RING MISSING PIN FOR 6 O'CLOCK POSITION IGV ACTUATING ARM. 2L72 4T4 TRTA52EU E8NE 20040329001252004032900125EA 2004 3 29 COMA0460204 120040317A2752854D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LT WING TE FLAP FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01729CA4218 7265 FLIGHT 5157 RECEIVED A FLAP FAIL MESSAGE DURING CLIMBOUT OF CMH. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE OUTBOARD ACTUATOR OF THE OUTER LEFT FLAP. 2L72 4F RTA21EA 20040329001412004032900141NM 2004 3 29 2004UALA00202 120040308A3213 SHOCK ABSORBER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE MLG FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29840UA 1522 RETURN TO FIELD DUE TO FAILURE OF LANDING GEAR TO RETRACT. LANDING GEAR SHOCK ABSORBER FAULT. LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) FAILED. THE LGCIU COMPONENT EXPERIENCED A HARD FAILURE DURING OUTPUT TESTS. REPLACED LGCIU. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040329001542004032900154NM 2004 3 29 2004UALA00213 120040308A2741 WARNING LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE STAB TRIM ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29660UA 27115 STABILIZER TRIM ADVISORY ILLUMINATED DURING TAKEOFF ROLL. UNABLE TO DUPLICATE DURING TROUBLE SHOOTING. ACCOMPLISHED ADDITIONAL TROUBLE SHOOTING AS A PRECAUTION. NO FAULTS FOUND. NO ADDITIONAL INCIDENTS NOTED. 2L72 4F4 FRTA1NM E24NE 20040329001572004032900157NM 2004 3 29 2004UALA00214 120040301A5754114N300357 WEDGE BOEING BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 5 SLAT SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29517UA A10294 24861 SEPARATION OF TRAILING EDGE WEDGE. REPLACED T/E WEDGE. REPAIRED LOWER SEAL PANELS. 2L72 4F4 FRTA2NM E17NE 20040329001812004032900181NM 2004 3 29 2004UALA00128 120040214A2133106120921 SAFETY VALVE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29947UA3328 26688 DIVERTED AFTER A RAPID CABIN DECOMPRESSION. THE INBOARD AND OUTBOARD SAFETY RELIEF VALVES FAILED OPERATIONAL TEST AND WERE REPLACED. THE CABIN PRESSURE CONTROLLER WAS ALSO REPLACED PRECAUTIONARY. 2L72 4F4 FRTA16WE E2GL 20040329001852004032900185NM 2004 3 29 2004UALA00140 120040216A323080602 CIRCUIT CARD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29338UA 24242 UNABLE TO RAISE THE LANDING GEAR AFTER TAKEOFF. REPLACED MAIN GEAR LOGIC CARD M991. 2L72 4F4 FRTA16WE E2GL 20040329001862004032900186NM 2004 3 29 2004UALA00174 120040227A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29511UA 24799 FUSELAGE SKIN AT BS 1460 HAS LIGHTNING STRIKE ADJACENT TO A FASTENER HOLE, ALONG PRODUCTION BUTT SPLICE BETWEEN STRINGER 24L & 25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040329001892004032900189NM 2004 3 29 2004UALA00179 120040301A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29397UA 24672 AFT CARGO PIT STATION 794 FWD LOWER DOOR FRAME WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW WEB. 2L72 4F4 FRTA16WE E2GL 20040329001982004032900198NM 2004 3 29 2004UALA00247 120040313A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 INTERCOSTAL BETWEEN FLOORBEAM 380 AND 400 AT BL 0 CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2GL 20040329001992004032900199WP 2004 3 29 MWEA040018 120040219A26110462 SMOKE DETECTOR DOUG DC9 DC932 3022066WP LAVATORY FALSE INDICATIONA MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31501ME 47132 LEFT LAVATORY SMOKE DETECTOR WENT OFF. INSPECTED LAVATORY COMPARTMENT, LIGHTING SOCKETS, LAVATORY TIMER, WATER HEATER, TRASH COMPARTMENT AND CYCLED LAVATORY MOTOR. REMOVED AND REPLACED SMOKE DETECTOR. 2L72 4F A6WE 20040330000042004033000004NM 2004 3 30 04FDEA00702 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE, BARREL NUT HOLE NR 7 MATING SURFACE CORRODED. LT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE, BARREL NUT HOLE NR 7 MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-09 AND DWG ARC0503 SHEET 2 ZONE 22. 2L73 4F RTA22WE 20040330000072004033000007NM 2004 3 30 DL76G040228 120040311A3246 NUT BOEING767 767332 1382001NM MLG WHEEL MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO271607B DL1109 30388 ON WALKAROUND FOUND TIE NUT MISSING FROM NR 3 MAIN LANDING WHEEL ASSEMBLY. REPLACED MLG TIRE ASSY IAW MM. 2L72 4F RTA1NM 20040330000302004033000030NM 2004 3 30 DLM88040242 120040316A2420249001278 GENERATOR DOUG MD88 MD88 3023688NM NR 2 ENGINE FAILED A DALAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO27982DL 53273 DURING T/O RIGHT GENERATOR FAILED, ACCOMPANIED BY AC CROSSTIE LOCKOUT. REPLACED RT GENERATOR AND CSD. 2L72 4F RTA6WE 20040330000352004033000035NM 2004 3 30 DL73S040248 120040312A5313 STRINGER BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27302DL 23047 STRINGER 4L DAMAGED IN LWR RADIUS AT STA 797. REPAIRED PER SRM 53-10-3 FIG 4. 2L72 4F RTA16WE 20040330000392004033000039NM 2004 3 30 DL75K040253 120040321A3230 PISTON BOEING757 757232 1384965NM TILT ACTUATOR SHEARED A DALAO OTHER O OTHER CRCRUISE 1 SO27649DL SA00301 24389 LANDING GEAR OVERRIDE HANDLE MOVING IN FLT. FOUND RT TRUCK TILT ACUATOR PISTON BROKE. REPLACED ACTUATOR. 2L72 4F RTA2NM 20040330000432004033000043NM 2004 3 30 DL73S040259 120040320A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27302DL 23047 INSPECTION OF THE SKIN LAPS PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE IN THE STRINGER 10R SKIN LAP SPLICE AT FS 432. A 1 X 6 INCH CUTOUT WAS MADE IN THE SKIN TO REMOVE THE CRACKED AREA. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER BAC B737 SRM AND PER ER/A 089002-14AD. 2L72 4F RTA16WE 20040330000522004033000052 2004 3 30 2004UALA00255 420040315A2565 DOOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE OVERWING SLIDE WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29596UA 28749 LEFT OVERWING SLIDE COMPARTMENT DOOR FAILED TO OPEN ON PNEUMATIC DEPLOYMENT TEST. NITROGEN SUPPLY REGULATOR USED FOR THE TEST WAS NOT CONFIGURED TO QUICKLY PROVIDE PRESSURE TO THE ACTUATOR TEST PORT. THE SUBSEQUENT, SUCCESSFUL, PNEUMATIC TEST WAS PERFORMED WITH A REGULATOR CONFIGURED TO QUICKLY DELIVER NITROGEN AT 1500 PSI TO THE ACTUATOR TEST PORT. AMM 25-65-00/501 'OFF-WING ESCAPE SYSTEM - ADJUSTMENT/TEST' HAVE INSTRUCTIONS TO QUICKLY APPLY PRESSURE TO 1500 PSI. THE CARRIAGE WILL NOT TURN OUT IF THE PRESSURE RELEASE IS SLOW. 2L72 4F4 FRTA2NM E17NE 20040330000572004033000057NM 2004 3 30 2004UALA00259 120040318A5320 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 STA 246 FLOORBEAM VERTICAL STIFFENER IS CRACKED AT LBL 23. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER. 2L72 4F4 FRTA1NM E24NE 20040330000672004033000067NM 2004 3 30 2004UALA00194 120040304A5340 SUPPORT FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG BEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29389UA 24664 LEFT MLG BEAM SUPPORT FITTING AFT SIDE 2 CRACK INDICATIONS AT HOLE C-AREA ON E AT 9 O`CLOCK POS UNDER WASHER RUNNING RADIALLY AT HOLE EDGE. ONE CRACK AT 12 O`CLOCK POS RUNNING UP AND DOWN. NOT EMANATING FROM HOLE, 3RD CRACK IS AT 6 O`CLOCK POS RUNNING DOWNWARD. MAJOR REPAIR ACCOMPLISHED. NOTCHED (BLENDED) OUT AFT SURFACE OF FITTING, INSTALLED TENSION PLATE DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040330000702004033000070 2004 3 30 04076316 420040316A31607011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU INOPERATIVE A VTZAO OTHER G MULTIPLE FAILURE DEDESCENT 1 EA27316UE 41055 DURING DESCENT OF FLIGHT 7794 CREW REPORTED CAPTAINS AHRU, VHF COMM, ADF, AND TRANSPONDER FAILURES. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE CLEARANCE DELIVERY UNIT, FCS SWITCHING RELAY, SYMBOL GENERATOR, AND NAV UNIT WERE REPLACED ON THE PILOTS SIDE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040330000722004033000072NM 2004 3 30 04FDEA00705 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE BARREL NUT HOLE NR 7 MATING SURFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-09 AND DWG ARC0503 SHEET 2 ZONE 22. 2L73 4F RTA22WE 20040330000772004033000077NM 2004 3 30 04FDEA00710 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75976, TRAILING EDGE AND TRAILING EDGE DEVICES, RT OUTBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000782004033000078NM 2004 3 30 04FDEA00543 120040302A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACKED. RIGHT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040330000942004033000094NM 2004 3 30 04FDEA00620 120040310A5713ARB31101 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING STRINGER 10 END SUSPECT CRACKED. LEFT WING STRINGER 10 REPAIRED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040330001002004033000100NM 2004 3 30 04FDEA00728 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001052004033000105NM 2004 3 30 04FDEA00733 120040323A522050797843 SKIN BOEING727 727200 138407ENM EMERGENCY EXIT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 LEFT AFT EMERGENCY EXIT DOOR EXTERNAL SKIN IS GOUGED AT LWR AFT CORNER. REMOVED DAMAGE AREA OF LEFT AFT EMERGENCY EXIT DOOR SKIN. FABRICATED REPAIR, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR AS PER SRM 52-00-2 AND INSTALLED ALL FASTENERS REMOVED FOR ACCESS IAW 51-30-2. 2L73 4F RTA3WE 20040330001072004033000107NM 2004 3 30 04FDEA00722 120040323A5753 MOUNT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD FORWARD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 AND DWG ARC0502 SHEET 4 ZONE 40. 2L73 4F RTA22WE 20040330001082004033000108NM 2004 3 30 04FDEA00723 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001182004033000118WP 2004 3 30 04FDEA00675 120040317A5330ABA7050U4 SKIN DOUG DC10 DC1010 3022110WP ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 LOWER FUSELAGE EXTERNAL INSPECTION, FOUND MANY DENTS (MAX DENT .044 EA) ON EXTERNAL SKIN STA 295 TO STA 330 SIDE AREA BETWEEN L33 TO L36. REMOVED AND REPLACED SKIN PANEL PER ABA 7050 AND SRM. 2L73 4F A22WE 20040331000032004033100003EA 2004 3 31 QXEA200400162 120040219A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - CENTER CHIMNEY IN FORWARD CARGO BAY HAS TORN SCREEN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040331000052004033100005EA 2004 3 31 QXEA200400159 120040218A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - MAINTENANCE FOUND A DENT IN LEFT SIDE OF FUSELAGE 8.5 INCHES AFT OF FS 379.00 AND 10 INCHES DOWN FROM BOTTOM OF WINDOW LINE. THE DENT WAS REPAIRED IAW EA R-53-198. 2L72 4F RTA21EA 20040331000062004033100006NE 2004 3 31 DHL2004784002 220040227A7261 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D17A 52049NE NR 2 OVERTEMP A DHLAE ENGINE SHUTDOWN KMJFLUID LOSS OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SO01784DH 22001 707258 OIL QUANTITY ENGINE NR 2 DROPPED TO 0, FOLLOWED BY LOOSE OF OIL PRESSURE ENGINE NR 2. PERFORMED OIL QUANTITY DECREASE AND IN-FLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURES. ENGINE SHUTDOWN AT 0436Z OIL QUANTITY: 0, OIL PRESSURE: 37 PSI. AFTER SHUTDOWN OIL PRESSURE: 4 PSI, OIL TEMPERATURE: 96 DEGREES CELSIUS. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY IAW ASTAR B-727 M/M 71.1. ENGINE FAILED TEST RUN (COMPRESSOR STALL) SEE ITEM 10M LOG PAGE 321384 FOR CORRECTIVE. DURING INITIAL ENGINE RUN #2 FOLLOWING ENGINE CHANGE. COMPRESSOR STALL AT PART POWER DURING STEADY STATE OPERATION. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY IAW ASTAR B-727 MTM 71.2. OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20040331000072004033100007 2004 3 31 UPS04141992 420040304A2565 CONNECTOR AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01142UP 0825 RED LIGHT ON EMERGENCY ESCAPE SLIDE TEST WILL NOT ILLUMINATE, BUZZER OPERATES NORMALLY. DEFERRED EVAC SLIDE WARNING LIGHT PER A300 MEL 52-73-01-1. PLACARD INSTALLED. CLOSING LP 146228 - RESET CONNECTOR ON AUTONOUMOUS POWER SUPPLY UNIT. OPS CK NORMAL, MEL 277035 CLEARED. 2L72 4F RTA35EU 20040331000082004033100008NM 2004 3 31 04FDEA00476 120040220A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 CORROSION ON STR 27L, STA 508, AROUND FASTENER, FWD CARGO BAY. REMOVED CORROSION ON STR 27L BS 508 AREA OF 1X1X.020 ORIG. 040. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER BS 490 - BS 510. FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1 AND 53-10-3 FIG 1. 2L73 4F RTA3WE 20040331000102004033100010NM 2004 3 31 04FDEA00401 120040212A5753ARC4230503 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT SUPPORT FOUND CRACKED. LT WING O/B FLAP I/B HINGE FAIRING (FLAP SIDE) AFT CRACKED SUPPORT REMOVED & FABRICATED AS PER DRWG ARC4230 (REF EARN 46) & INSTALLED AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040331000112004033100011NM 2004 3 31 04FDEA00400 120040212A5753ARC7668502 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING SUPPORT BRACKET BROKEN. RH WING I/B FLAP O/B HINGE FAIRING LOWEST O/B FAIRING BROKEN SUPPORT BRACKET REMOVED & REPLACED AS PER SRM 51-33-01 VOL2. 2L73 4F RTA22WE 20040331000132004033100013NM 2004 3 31 04FDEA00479 120040220A53116556120 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 950B, BETWEEN STR 26L & 25L. REPAIRED FRAME IAW FED EX EA 7-5310-55244 2L73 4F RTA3WE 20040331000142004033100014NM 2004 3 31 04FDEA00480 120040220A53116515932 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 DENT IN FRAME, STA 580, BETWEEN STR 22L AND STR 24L. REMOVED DAMAGED SECTION ON FRAME 580 B/N STR 22L & STR 24L. APPROX. 1.5 INCHES PER SRM 53-40-3. FABRICATED REPAIR PART PER SRM 51-40-3. ALODINED, PRIMED & PAINTED PER SRM 51-10-2. INSTALLED PER SRM 51-30-2. FED EX EA 7-5310-70628A. 2L73 4F RTA3WE 20040331000152004033100015NM 2004 3 31 04FDEA00482 120040220A53116516345 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1090, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX E.A. 7-5310-55241 2L73 4F RTA3WE 20040331000162004033100016NM 2004 3 31 04FDEA00483 120040220A53116516346 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1110, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55235 2L73 4F RTA3WE 20040331000172004033100017NM 2004 3 31 04FDEA00584 120040305A5320AKC753921 CLIP DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 FWD TAIL CONE LT AFT FRAME FOUND L-ANGLE BRACKET DAMAGED. FWD TAIL CONE LT AFT FRAME ANGLE BRACKET REMOVED AND REPLACED AS PER FEDEX EA 1-5340-75283 - FUSELAGE - AERODYNAMIC FAIRINGS - FORWARD TAILCONE ASSEMBLY - CLIP FABRICATION 2L73 4F RTA22WE 20040331000182004033100018NM 2004 3 31 04FDEA00586 120040305A5320AKC762017 PLATE DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 AFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RH FRAME 2 EA STOP PLATE REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER (TITLE : FUSELAGE AERODYNAMIC FAIRING AFT TAIL CONE ASSY PLATE FABRICATION) EA 1-5390-75285. 2L73 4F RTA22WE 20040331000192004033100019NM 2004 3 31 04FDEA00588 120040305A5740ARC4125501 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP STOP FITTING FOUND CRACKED. LT WING O/B FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040331000202004033100020NM 2004 3 31 04FDEA00585 120040305A5320AKC762013 CLIP DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 AFT TAIL CONE RT UPPER SUPPORT STRUCTURE BRACKET FOUND CRACKED. AFT TAIL CONE RH UPPER SUPPORT STRUCTURE BRACKET REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER (TITLE: FUSELAGE AERODYNAMIC FAIRING AFT TAIL CONE ASSY CLIP FABRICATION) EA 1-5390-75284. 2L73 4F RTA22WE 20040331000212004033100021NM 2004 3 31 UPS04541894 120040213A3040141T480150 HEATER BOEING757 75724APF 1384969NM COCKPIT WINDOW INOPERATIVE A IPXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01413UP 23853 EN ROUTE TO PHL, NOXIOUS FUMES WERE IN COCKPIT. NO EICASE, NO SMOKE. DIVERTED TO BDL. F/O R1 WINDOW HEAT SYSTEM AFT CORNER SMOKING WHEN WINDOW HEAT TURNED ON. AWAITING LP TO CLOSE, DEFERRED F/O R1 WINDOW HEAT SYSTEM D275899. R/R F/O'S R1 WINDOW PER MM 56-11-01-4, OPS CK GOOD. REFERENCE LP77516 8. 2L72 4F RTA2NM 20040331000232004033100023NM 2004 3 31 04FDEA00485 120040220A53116556124 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 950F, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55238 2L73 4F RTA3WE 20040331000242004033100024NM 2004 3 31 04FDEA00486 120040220A53116516344 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1070, BETWEEN STR 26L & 25L. REPAIRED I.A.W FED EX E.A. 7-5310-55239 2L73 4F RTA3WE 20040331000252004033100025NM 2004 3 31 04FDEA00487 120040220A53116516343 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1050, BETWEEN STR 26R & 25R. REPAIRED IAW FED EX EA 7-5310-55242 2L73 4F RTA3WE 20040331000262004033100026NM 2004 3 31 04FDEA00488 120040220A53116516343 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1050, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55242 2L73 4F RTA3WE 20040331000292004033100029NM 2004 3 31 04FDEA00391 120040210A5311AKC7539 FRAME DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 FWD TAIL CONE AFT LT FRAME FOUND CHAFED MARK. FWD TAIL CONE AFT LH FRAME REPAIR CARRIED OUT AS PER SRM 53-00-01 FIG 9 VOL1. 2L73 4F RTA22WE 20040331000312004033100031WP 2004 3 31 04FDEA00541 120040301A5420AVB705025 SUPPORT DOUG DC10 DC1010 3022110WP NR 2 NACELLE MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 NR 2 ENG CORE COWL FWD LT AND RT HINGE LINK/ROD SUPPORT FOUND MISSING. ALSO FOUND CRACKS AT LT AND RT VERTICAL STIFFENERS AT HINGE FITTING CUTOUTS FOR LINK ATTACHMENT. REPLACED LINK ASSY AND WELDED CRACKS. SUSPECT CRACKS CAUSED DUE TO MISSING ROD. 2L73 4F A22WE 20040331000342004033100034NM 2004 3 31 04FDEA00531 120040301A5320 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 TAIL TANK NR 26R BARREL NUT BORE EXCEEDED LIMIT DURING CORROSION REMOVAL. 2L73 4F RTA22WE 20040331000352004033100035NM 2004 3 31 04FDEA00533 120040301A5320AFA7761 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 INTERCOSTAL CRACKED AT LONGERON 7R, STA RT 1581 TO 1601. INTERCOASTAL CRACKED AT LONGERON 7R, STA RT 1581 TO 1601 CARRIED OUT REPAIR IAW SRM 53-00-01 VOL I FIG 5. 2L73 4F RTA22WE 20040331000372004033100037WP 2004 3 31 UPS04841955 120040222A5710 WING ROOT DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 RIGHT WING ROOT HAS CORROSION (EXFOLIATION). A/C FERRIED TO TCO DEFERRED (276424) AND TRANSFERRED TO NRC 469644 RMVD RH OVERWING EMERGENCY HATCH TO FOM. RMVD R/H OVERWING TO FUSELAGE FILLET PNL 292F TO FOM. RMVD CORRODED PAD FR R/H W/W IAW DC8-SRM 51-1 -20. RCVD NEW 2751738-2 FTG LOCATED & DRILLED IAW DC8 SRM 51-1-24. OK TO INSTALL. INSTALLED FTG, OK TO INSTALL PNL 292F IAW DC8-SRM-51-3- 0. OK TO INSTALL DOORWING EMERG HATCH. RMVD RH OVERWING EMERG HATCH P NL 292F. RMVD CORODED PAD FR RT WW & REINSTALLED PAD & PNL. 2L74 4F RT4A25 20040331000382004033100038NM 2004 3 31 04FDEA00521 120040225A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 STRINGER CORRODED AT BS 990 STR 28 LT. FOUND CORROSION ON STRINGER AT BS 990, STR 28 LT TO BE OUT OF LIMITS PER SRM 53-10- 1. REPAIRED STRINGER IAW SRM 53-10-3. 2L73 4F RTA3WE 20040331000392004033100039NM 2004 3 31 04FDEA00515 120040224A2841 INDICATOR DOUG MD11 MD11 3023602NM FUEL QTY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25596FE 48554 FUEL QTY/USED CHK ALERT. QRH COMPLETED/ INITIAL FUEL TOTAL 5K LOW. RAN SYSTEM IN MANUAL. ALERT WENT OUT IN 10 MIN LATER. LANDED TUL W/O INCIDENT. ACN RELEASED FOR SERVICE PER MEL/CDL: 28-01-01-02 CATEGORY: A EXPIRATION: 27FEB04, MEL 28-01-01-02. TANK NR 2 FUEL TANK SYNOPTIC QTY DISPLAY INOP. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 2 QTY W/FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPERATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LAT. TAIL FUEL MGMT - INOP. PER MEL 28-01-01-2, FUEL QTY IN TANK NR 2 IS 16,000L BS. A/C OK FOR SERVICE. REF WRI 28-40/4217 FOR WORK PERFORMED, FOUND WITH THE NR 2 TANK EMPTY THE SYNOPTIC DISPLAY SHOWED 2000 POUNDS. 2L73 4F RTA22WE 20040331000402004033100040NM 2004 3 31 QXEA200400151 120040217A6123 CONTROLLER DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS MALFUNCTIONED A QXEAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 NM09375PH 528 SEA - FLIGHT 2283 AT 60 KTS AUTOFEATHER DID NOT ARM. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE AUTOFEATHER CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040329001112004032900111EU 2004 3 29 CX7A194HJ0418 120040318A26121734362450 FIRE DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AO OTHER N FALSE WARNING NRNOT REPORTED 1 GL03307CE 340B204 AFTER FIRE TEST LEFT TAILPIPE HOT LIGHT STAYS ON. 2L72 4T RTA52EU 20040329001312004032900131EA 2004 3 29 COMA0460198 120040315A32204622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A COMAO OTHER O OTHER APAPPROACH 1 SO01914CA10468 7012 FLIGHT 5092 WHEN SELECTING GEAR DOWN DURING CVG APPROACH, RECEIVED A GEAR DISAGREE CAUTION. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040329001322004032900132EA 2004 3 29 COMA0460199 120040316A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01719CA 7253 FLIGHT 5158 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CLIMBOUT OF CVG. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGE. 2L72 4F RTA21EA 20040329001522004032900152NM 2004 3 29 2004UALA00211 120040305A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP2989UA 24664 BS 685 S4R HAS A CRACKED TEAR STRAP BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED BRACKET. 2L72 4F4 FRTA16WE E2GL 20040329001612004032900161NM 2004 3 29 2004UALA00215 120040309A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 SKIN AT STA 380 STR 24L CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER AND CLIPS. 2L72 4F4 FRTA16WE E2GL 20040329001722004032900172EU 2004 3 29 2004UALA00225 120040309A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29452UA 955 FLOOR SUPPORT CORRODED BETWEEN FR 66-70 RBL 34. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA28NM E40NE 20040329001732004032900173EU 2004 3 29 2004UALA00226 120040310A2611 CONTROL UNIT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SMOKE DETECTORS FAILED A UALAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29408UA 457 FLIGHT DIVERTED DUE TO AFT CARGO SMOKE ECAM MESSAGE. REPLACED SMOKE DETECTOR CONTROL UNIT (SDCU) AND FOUR AFT CARGO SMOKE DETECTORS. 2L72 4F4 FRTA28NM E40NE 20040329001882004032900188NM 2004 3 29 2004UALA00178 120040302A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29546UA 25367 SKIN DAMAGE AT STA 1701 AND STR 18 RT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040329001902004032900190WP 2004 3 29 MWEA040025 120040318A572059359412 ANGLE DOUG DC9 DC981 3022081WP TE FLAP CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 CORROSION ON ANGLE SUPPORT BRACKET ON RIGHT FLAP TRAILING EDGE AT RIGHT WING STATION XCW 104.5. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20040329001912004032900191NM 2004 3 29 2004UALA00231 120040310A5753 FITTING BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE TE FLAPS WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29603UA 21864 RIGHT WING INBOARD FLAP COLLAR FITTING WORN. MAJOR REPAIR ACCOMPLISHED. REPLACED RIGHT WING INBOARD FLAP COLLAR FITTING. 2L72 4F4 FRTA1NM E3NE 20040329001932004032900193WP 2004 3 29 AALA20040337 120040310A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21442AA 49468 DFW - EMERGENCY LIGHT IN COCKPIT IS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040329002002004032900200NM 2004 3 29 237TR0004 120040309A3350 BATTERY BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05237TR 23007 L2 DOOR OVERHEAD EMERGENCY LIGHT AND LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERIES IN BOTH UNITS. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040330000032004033000003NM 2004 3 30 04FDEA00701 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD HINGE, BARREL NUT HOLE NR 28 MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5740-75923, LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY. 2L73 4F RTA22WE 20040330000062004033000006NM 2004 3 30 DLM88040227 120040310A2910AS15308K025 LINE DOUG MD88 MD88 3023688NM HYDRAULIC SYS UNSERVICEABLE A DALAO OTHER K FLUID LOSS CLCLIMB 1 SO27944DL 49817 ON CLIMBOUT, RIGHT HYDRAULIC QTY WENT TO -0- FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. REPLACED RIGHT ENGINE PRESSURE LINE. 2L72 4F RTA6WE 20040330000222004033000022NM 2004 3 30 DL76S040223 120040307A3260 PIN BOEING767 767332 1382001NM RT MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27133DN 24982 WHILE WORKING A AIR GROUND DISAGREE PROBLEM. JACKED THE A/C PER THE SETUP AND FOUND THE RIGHT MAIN GEAR SWAYED FROM SIDE TO SIDE WHEN PUSHED INBOARD TO OUTBOARD. FOUND THE BOGIE PIN DAMAGED AND THE RIGHT TRUCK BUSHINGS WORN AND CRACKED. ALSO FOUND THE BOGIE BEAM BUSHINGS DAMAGED AND CRACKED. 2L72 4F RTA1NM 20040330000262004033000026NM 2004 3 30 DLM88040238 120040314A2560 MEGAPHONE DOUG MD88 MD88 3023688NM SAFETY EQUIPMENTINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27967DL 53116 AFT CABIN MEGAPHONE INOP. REPLACED MEGAPHONE. 2L72 4F RTA6WE 20040330000312004033000031NM 2004 3 30 DL757040243 120040316A5330141N33111 SKIN BOEING757 757232 1384965NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27608DA 22815 THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A 1.6 INCH CRACK IN THE SKIN WITH A SMALLER CRACK IN THE UNDERLYING BEARSTRAP. THE SKIN AND BEARSTRAP WERE LOCALLY CUTOUT TO REMOVE THE CRACK. THE AREA WAS REPAIRED WITH THREE EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 089063-14AD. 2L72 4F RTA2NM 20040330000412004033000041NM 2004 3 30 DLM88040255 120040322A3213 STRUT DOUG MD88 MD88 3023688NM NLG DISCHARGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27917DL 49573 ON DEPT WHEN GEAR HANDLE RAISED ALL GEAR IND IN TRANSIT AND MAIN GEAR WENT UP AND LOCKED EXCEPT NOSE GEAR STILL IND UNSAFE. GEAR DOOR OPEN LIGHT WAS OUT. REPLACED UP/LOCK SENSOR. 2L72 4F RTA6WE 20040330000452004033000045NM 2004 3 30 2004UALA00176 120040227A2420MR24121 IDG BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 2 MALFUNCTIONED A UALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29221UA149806325 30552 777112 RIGHT GEN EICAS MSG, DISCONNECTED RIGHT GEN AND STARTED APU. CREW OBSERVED EICAS ADVISORY MSG, ELECT GEN DRIVE R, WITH MAINT MSG (LOW FREQ & LOW OIL PRESS), WHICH ILLUMINATED GEN DRIVE LIGHT. DISCONNECTED IDG. SHOP RECORDS INDICATED OVERHAUL 4/02. ON-WING INSTALLATION ON 7/02. LOW FREQ & LOW OIL PRESS MAINT MSG OBSERVED WITH FAULT INDICATES LOW OIL QTY COULD CAUSE FREQ DROP. SHOP INDICATED SUFFICIENT OIL QTY & DIP TEST INDICATED NO LEAKS FROM UNIT, NOR ANY OTHER INTERNAL COMPONENT FOUND TO HAVE CAUSED LOW FREQ. UNIT WAS OIL SERVICED 2 DAYS PRIOR TO FAULT. SHOP FINDINGS WERE NFF AFTER 6,325 HRS IN OPERATION. UNIT WILL BE OH'ED, TEST STAND OPERATED AT VENDOR. SUBSEQUENT CORR ACT, REPLACE IDG. 2L72 4F4 FRTT0001SE E46NE 20040330000632004033000063NM 2004 3 30 2004UALA00186 120040303A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE OVERWING SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29302UA 23643 RIGHT AFT OVERWING SLIDE LIGHT IS INOPERATIVE. RELAMPED SLIDE LIGHT. 2L72 4F4 FRTA16WE E2GL 20040330000742004033000074NM 2004 3 30 04FDEA00707 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75979, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS 2L73 4F RTA22WE 20040330000842004033000084NM 2004 3 30 04FDEA00716 120040323A5753ARC2518502 STRAP DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING, INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD STRAP OUTBOARD SIDE SURFACE CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II 2L73 4F RTA22WE 20040330000912004033000091NM 2004 3 30 04FDEA00617 120040310A5311AFA79311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1601 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TITLE : FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILED IN THE WORK STEPS. 2L73 4F RTA22WE 20040330000962004033000096NM 2004 3 30 04FDEA00724 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001042004033000104WP 2004 3 30 04FDEA00732 120040323A5753ARC2177 SPINDLE DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 OUTBOARD FLAP - FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR P/N ARC2177. COMPLIED WITH EA 8-5750-75125. 2L73 4F A22WE 20040330001102004033000110NM 2004 3 30 04FDEA00735 120040323A5531 SPAR BOEING727 727200 138407ENM VERTICAL STAB CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 VERTICAL STAB MID SPAR CHAFED AT PANEL 9602 (RT SIDE). REPAIRED THE RT VERTICAL MID SPAR AT PANEL 9602 IAW FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3. 2L73 4F RTA3WE 20040331000012004033100001NM 2004 3 31 04FDEA00410 120040215A5753SK105700017007 FLAP TRACK DOUG MD11 MD11 3023602NM ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP VANE CENTER TRACK WORN. APPLIED A LIGHT COAT OF MIL-G-81322 (MOBILE 28) GREASE TO THE LOWER SURFACE OF CENTRE VANE SUPPORT TRACK OF THE I/B FLAP LT AS PER FEDEX EA 1-5750-74226 PT1. WINGS - TE FLAPS - I/B TE FLAP VANE - CENTRE VANE SUPPORT TRACK - REPAIR. 2L73 4F RTA22WE 20040331000092004033100009NM 2004 3 31 04FDEA00402 120040212A5720ARC4230504 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT WING O/B FLAP I/B HINGE AFT FAIRING (FLAP SIDE) AFT SUPPORT BRACKET FOUND CRACKED. RT WING O/B FLAP I/B HINGE AFT FAIRING - CRACKED AFT SUPPORT BRACKET REMOVED. FABRICATED AS PER DRWG ARC4230 (REF EARN 047) & INSTALLED AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040331000122004033100012NM 2004 3 31 04FDEA00478 120040220A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 CORROSION ON STR 27L, STA 580 AROUND FASTENER, FWD CARGO BAY. CORROSION ON STR 27 LT, STA 580 FWD CARGO BAY FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 53-10-3, 51-30-2. 2L73 4F RTA3WE 20040331000222004033100022NM 2004 3 31 04FDEA00484 120040220A53116556121 FRAME BOEING727 727200 138407ENM FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 FRAME BENT AT BS 950C, STR 26 RT. REPAIRED IAW FED EX EA 7-5310-55240 2L73 4F RTA3WE 20040331000362004033100036NM 2004 3 31 QXEA200400154 120040215A2750C1486561 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09414QX213 213 4061 ON TAKEOFF THE CREW RECEIVED A FLAP POWER CAUTION LIGHT WHEN THE FLAPS WERE SELECTED UP. THE CREW RESET THE C/B AS PER THE ABNORMAL CHECK LIST AND THE CAUTION LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT FLAP SYSTEMS AND REPLACE THE FLAP POWER CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040331000412004033100041NM 2004 3 31 04FDEA00563 120040303A5320ALC81211 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 TAIL TANK - NR 1L BARREL NUT BORE CORROSION REWORK OUT OF LIMIT. TAIL TANK - NR 1L BARREL NUT BORE CORROSION REMOVED AS PER EA 1-5510- 75912, STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/ REPAIR - AD 2003-22-08 2L73 4F RTA22WE 20040331000432004033100043NM 2004 3 31 QXEA200400155 120040214A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAILED A QXEAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 NM09358PH14046 506 YKA - BAGGAGE SMOKE WARNING TEST 2 FAILS TO TEST. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040331000442004033100044WP 2004 3 31 DHL2004809005 120040315A5753 RIB DOUG DC8 DC873F 302199FWP TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 LEFT-HAND INBOARD FLAP UNDER JOINT PANEL THERE IS A .75 INCH CRACK OUTBOARD RIB LOWER CORD 40 INCHES FROM TRAILING EDGE. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTER AS DMI 16040E. ONLY 2 REVENUE FLIGHTS WITH NOTED DAMAGE. REF. DMI 16040E LT INBOARD FLAP UNDER JOINT PANEL THERE IS A .75 CRACK OUTBOARD RIB LOWER CHORD 40 DEGREES FROM TRAILING EDGE (DAILY INSP.) DUE 20 MAR 04. REPLACED LEFT-HAND INBOARD FLAP ASSEMBLY IAW 27-51-1. PERFORMED INSPECT/CHECK IAW 27-51-1. PERFORMED ADJUSTMENT TEST IAW 27-50-0. NO DEFECTS NOTED. THIS CLEARS DMI 16040E. PLACARD REMOVED. 2L74 4F RT4A25 20040331000492004033100049NM 2004 3 31 SWAA040878 120040323A3350MS1557081 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29755SA 27871 DURING SCHEDULED C3 CHECK, FOUND RED EMERGENCY EXIT LIGHT AT MID CABIN INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040331000512004033100051NM 2004 3 31 SWAA040880 120040323A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 807, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331000522004033100052NM 2004 3 31 SWAA040847 120040320A3350610478 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT LT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED LT EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040331000532004033100053 2004 3 31 SWAA040848 420040321A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29105SW 23249 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040331000582004033100058 2004 3 31 SWAA040898 420040326A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29447WN 33720 R2 DOOR EVAC SLIDE LOOSE AT BOTTOM OF CONTAINER. RESECURED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040331000592004033100059NM 2004 3 31 SWAA040899 120040326A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 752, STRINGER 20L CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331000602004033100060NM 2004 3 31 SWAA040900 120040326A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 FWD ENTRY DOOR MISSING EMERGENCY LIGHT LENS COVER. INSTALLED LIGHT LENS COVER PER MM. 2L72 4F RTA16WE 20040331000612004033100061NM 2004 3 31 SWAA040901 120040326A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500B, STRINGER 16R CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040331000632004033100063NM 2004 3 31 SWAA040903 120040326A53206547957 WEB BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FWD CARGO COMPARTMENT WEB AT BS 840, BETWEEN STRINGERS 25L AND 26L, CORRODED. REMOVED AND REPLACED WEB SECTION PER ER. 2L72 4F RTA16WE 20040331000652004033100065NM 2004 3 31 SWAA040854 120040321A57436545321 FITTING BOEING737 7373Y0 1384671NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND LT MLG BEAM FITTING AT D-HOLE CRACKED. REMOVED AND REPLACED LT MLG FITTING PER ER. 2L72 4F RTA16WE 20040331000672004033100067NM 2004 3 31 SWAA040842 120040319A32606552811 ACCESSORY UNIT BOEING737 7372T4 1384492NM E/E BAY FAULTY A SWAAO OTHER O OTHER LDLANDING 1 SW29722WN 22698 ON LANDING GEAR EXTENSION 3 GREEN AND 3 RED LIGHTS ILLUMINATED. CYCLED GEAR, THEN NORMAL INDICATION FOR LANDING. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER MM. 2L72 4F A16WE 20040331000682004033100068 2004 3 31 SWAA040843 420040319A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040331000692004033100069NM 2004 3 31 SWAA040844 120040320A53106546811 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 992, RBL 47, WL 208, CORRODED. REPAIRED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040331000712004033100071NM 2004 3 31 SWAA040846 120040320A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 516, STRINGER 16L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331000722004033100072NE 2004 3 31 SWAA040828 220040316A7200332A1000 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE RIGHT FAULTY A SWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29315SW 23337 857573 INFLIGHT SHUTDOWN/AIRTURN BACK, NR 2 ENG OIL PRESSURE WENT TO ZERO AND OIL QUANTITY ALSO WENT TO ZERO. PERFORMED LOW OIL PRESSURE TEST AND ZONE A INSPECTION PER MM. ENGINE IS ON 50 CYCLE REINSPECT PER MX NOTE. 2L72 4F4 FRTA16WE E2GL 20040331000732004033100073NM 2004 3 31 SWAA040829 120040318A53126516300 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SPV, FOUND WEB AT BS 178, RBL 5.7, WL 188 TO WL 196, CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF WEB PER SRM. 2L72 4F A16WE 20040331000752004033100075NM 2004 3 31 SWAA040831 120040318A53106546569 SHEAR TIE BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SPV, FOUND SHEAR TIE AT BS 987, BL 0, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040331000792004033100079NM 2004 3 31 SWAA040835 120040318A335065C27093 LIGHT BOEING737 7372H4 138448CNM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED PM CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20040331000802004033100080NM 2004 3 31 SWAA040836 120040318A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331000822004033100082NM 2004 3 31 SWAA040838 120040318A53116547959 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AT BS 794, STRINGER 20R TO STRINGER 25R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040331000852004033100085NM 2004 3 31 SWAA040855 120040322A3210BAC24C05590EG CONTROL CABLE BOEING737 7372T4 1384492NM MLG OUT OF ADJUST A SWAAK NONE O OTHER LDLANDING 1 SW29722WN 22698 WHEN LANDING GEAR EXTENDED 3 GREEN AND 3 RED LIGHTS ILLUMINATED. CYCLED GEAR UP AND DOWN, NORMAL INDICATIONS. RIGGED LANDING GEAR CONTROL CABLES PER MM. 2L72 4F A16WE 20040331000872004033100087NM 2004 3 31 SWAA040857 120040322A53116520723 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME WEB CUTOUT AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME WEB PER ER. 2L72 4F RTA16WE 20040331000892004033100089NM 2004 3 31 SWAA040859 120040322A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND BS 500 + 16, STRINGER 23R, CORRODED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040331000902004033100090NM 2004 3 31 SWAA040861 120040322A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 500B, BETWEEN STRINGERS 27R AND 28R, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331000932004033100093NM 2004 3 31 SWAA040864 120040322A53106546529 SHEAR TIE BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500B, BETWEEN STRINGERS 27R AND 28R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040331000952004033100095NM 2004 3 31 SWAA040866 120040322A53126516300 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED SPV, FOUND 3 EACH CRACKS AT BS 178 BULKHEAD WEB, LBL .57 TO RBL 17.1, WL 178 TO WL 230. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20040331001012004033100101NM 2004 3 31 SWAA040890 120040325A53116546526 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 420, STR 25L TO STR 26L. REPAIRED FRAME PER ER AND SRM. 2L72 4F RTA16WE 20040331001042004033100104NM 2004 3 31 SWAA040881 120040324A3350101073 LENS BOEING737 7372H4 138448CNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 EMERGENCY EXIT OVERHEAD LIGHT LENS AT MID CABIN BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F A16WE 20040331001072004033100107NM 2004 3 31 04FDEA00738 120040324A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING, INBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75974, TRAILING EDGE & TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040331001092004033100109NM 2004 3 31 04FDEA00740 120040324A5713 LONGERON DOUG MD11 MD11 3023602NM WING TO FUSELAGECRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING TO FUSELAGE AT STA Y= 1491, LONGERON SPLICE FOUND CRACKED. RT WING TO FUSELAGE AT STA Y= 1491, CRACKED LONGERON SPLICE. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 53-10-00 VOL 1 FIG 2 2L73 4F RTA22WE 20040331001112004033100111NM 2004 3 31 SWAA040895 120040325A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE LT KEEL BEAM CORRODED AT BS 500D TO BS 540. REPAIRED KEEL BEAM SECTION PER ER. 2L72 4F RTA16WE 20040331001132004033100113NM 2004 3 31 SWAA040897 120040325A53106546529 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 460, STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040331001152004033100115NM 2004 3 31 04FDEA00642 120040312A5310AJC70213 FRAME DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 AFT FUSELAGE COMPARTMENT, UPPER FUSELAGE FRAME CLIP AT CANTED AREA STA 2046 FOUND CRACKED. CRACKED CLIP AT CANTED AREA STA 2046 AT AFT FUSELAGE COMPARTMENT UPPER FUSELAGE FRAME REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. COMPLIED EA 1-5340-75915, FUSELAGE, MAINFRAME OVERSIZED HOLE ON FRAME STATION 2046.00. 2L73 4F RTA22WE 20040331001172004033100117NM 2004 3 31 04FDEA00644 120040313A2913 PUMP DOUG MD11 MD11 3023602NM NR 3 HYD SYSTEM INOPERATIVE A FDEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25585FE 48481 IN CLIMB AT FL 350 HYD PUMP 3L OFF, ALERT ILLUMINATED FOLLOWED BY HYD PUMP 3R FAULT. ALERT WITH TEMP AMBER AT 97 DEG AND AMBER -T- ILLUMINATED ON BOTH PUMPS. BOTH PUMPS HAD OVERTEMPED. RELEASED FOR SERVICE PER MEL/CDL: 29-11-01-A, MEL 29-11-01-A: ENG NR 3 HYD PUMP INOP. PUMP REMOVED, RNR ENG NR 3 UPPER LEFT EDP PER MM REF 29-11-20-4-1. 2L73 4F RTA22WE 20040331001202004033100120NM 2004 3 31 04FDEA00647 120040314A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING FIXED LEADING EDGE LOWER SURFACE SKIN AT XORS 759 CRACKED. LT WING FIXED LEADING EDGE LOWER SURFACE SKIN AT XORS 759 SMOOTH END AND FOUND WITHIN LIMITS AS PER SRM 57-00-01 VOL 1 FIG 3 HFEC INSPECTION CARRIED OUT AS PER NDT SPM PART 06-10-01.001 REV 11. 2L73 4F RTA22WE 20040331001212004033100121NM 2004 3 31 04FDEA00655 120040315A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040331001222004033100122NM 2004 3 31 SWAA040904 120040326A53206545410 SUPPORT BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM SUPPORT AT BS 660, BL 0, CRACKED. REPAIRED FLOORBEAM SUPPORT PER EA. 2L72 4F RTA16WE 20040331001242004033100124NM 2004 3 31 04FDEA00657 120040316A5320A6A7115 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LONGERON SPLICE FOUND CORRODED AT STA 6-100 RIGHT LONGERON 45. COMPLIED WITH FEDEX EA 1-5310-75998, FUSELAGE - MAIN FRAME - CAC COMPARTMENT BODY STATION 6-100, LONGERON 45 RT SPLICE REPAIR 2L73 4F RTA22WE 20040401000032004040100003NM 2004 4 1 USAASB04011 120040121A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19425US 23992 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT SEAT ROW 11C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040401000042004040100004NM 2004 4 1 USAASB04010 120040121A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19560AU 23514 PHL - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040401000062004040100006NM 2004 4 1 USAABB04012 120040129A335020121 CHARGER BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19623AU 27244 CLT - FOUND CLASS DIVIDER OVERHEAD EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2L72 4F RTA2NM 20040401000072004040100007NM 2004 4 1 USAASB04009 120040118A2120 DUCT BOEING737 7373B7 1384580NM RT PACK BAY DETACHED A USAABG EMER. DESCENT O2 MASK DEPLOYED O OTHER CRCRUISE 1 EA19512AU 23595 CLE - FLT 232 - EN ROUTE FROM CLT TO CLE, CREW REPORTED THAT APPROXIMATELY 110 MILES SOUTH OF CLE AT FL250, THE AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSURE. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000 FEET AND CONTINUED ONTO CLE. OXYGEN MASK DID DEPLOY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. S/D - MAINTENANCE FOUND THE DUCTING AT THE RIGHT AIR CYCLE MACHINE DETACHED. REATTACHED DUCTING. REMOVED AND REPLACED RIGHT PACK FLOW CONTROL VALVE, P/N 396442-1, FOR FAILING SINGLE PACK CONFIDENCE CHECK. ALSO, REMOVED AND REPLACED THE RIGHT PACK 35 DEGREE SENSOR, P/N B7040-2, AND THE RIGHT WATER SEPARATOR P/N 183010-4, FOR BROKEN SCREEN INSIDE. REMOVED AND REPLACED OXYGEN GENERATORS2L72 4F RTA16WE 20040401000522004040100052EA 2004 4 1 A6WA200440017 120040202A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 FOUND FRAME 700 DAMAGED BETWEEN STRINGERS 16L AND 18L. REMOVED DAMAGED SECTION OF FRAME 700 FROM STRINGER 14L TO EXISTING SPLICE AT STRINGER 20L. FABRICATED SPLICE DOUBLER FROM 2024-T3 .040 INCH. INSTALLED SECTION OF FRAME P/N 600-360290-35 AND SPLICE DOUBLER IAW WVAC EO 601R-53-4653A. (M) 2L72 4F RTA21EA 20040401000552004040100055 2004 4 1 REXA04004 420040126A2562 G SWITCH CNDAIRCL600 CL6002B19 1900309EA ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258851D 0319 7851 ELT FAILS G-SWITCH TEST DURIG 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. MANUFACTURER HAS RECEIVED THE UNIT AND CONFIRMED A 'STICKING' G-SWITCH. THIS FAILURE IS THE 7TH OCCURRENCE OF THIS MODEL ELT FAILING THE G-SWITCH TEST ON ITS FIRST 12 MONTH INSPECTION. (M) 2L72 4F RTA21EA 20040401000582004040100058NM 2004 4 1 UIEA200400013 120040210A575365B08540202 PANEL BOEING747 747243B 1384830NM TE FLAP DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, FOUND TOP PANEL P/N 65B08540-202 DELAMINATED. AREA AFFECTED EXCEED SRM REPAIR LIMITS. THE DAMAGED SKIN WAS REMOVED AND DISCARDED. A METAL TO METAL HOT BOND REPAIR WAS ACCOMPLISHED PER 747 SRM 51-40-06 SECTION 3 REQUIREMENTS. DETAIL VISUALLY INSPECT AND TAP TEST THE REPAIR AREA FOR SIGNS OF DEGRADATION AT 2A CHECK INTERVALS, AND REPLACED THE PANEL WITHIN 18 MONTHS. ATLAS MCI A062 ISSUED TO REPLACE PANEL AT NEXT C-CHECK. (M) 2L74 4F A20WE 20040401000622004040100062NM 2004 4 1 AMTA200400103 120040131A2612710128 FIRE LOOP BOEING757 75723N 1384973NM LT ENGINE MALFUNCTIONED A AMTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL11515AT 27598 STATUS MESSAGE 'L ENGINE FIRE LP 1' APPEARED. REPLACED NR 1 LOOP NR 3 DETECTOR REF MM 26-11-01-4, SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040401000652004040100065NE 2004 4 1 AMTA200400134 220040206A7323FFGO22AD GOVERNOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT ENGINE FAILED A AMTAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL11522AT 29330 31604 ENGINE WILL NOT ACCELERATE BEYOND 30 PERCENT N1. REMOVED AND REPLACED LT ENGINE GOVERNOR PER MM 73-21-01-4. (M) 2L72 4F4 FRTA2NM E12EU 20040401000682004040100068NE 2004 4 1 TSAA0479020 220040205A7261697268811 BYPASS SWITCH BOEING737 737230 1384401NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE FAULTY A O OTHER J WARNING INDICATION CLCLIMB 1 WP13821AL 23155 NR 2 ENGINE OIL BYPASS LIGHT CAME ON. PERFORMED QRH PROCEDURES, ENGINE SHUTDOWN AND LANDED AT HNL. ACCOMPLISHED BREATHER PRESSURE CHECK PER FORM M-209. CHECK GOOD. DRAINED AND SERVICED OIL TANK AND GEARBOX. LEAK AND OPS CHECK GOOD. REPLACED THE NR 2 ENGINE OIL BYPASS SWITCH. RAN ENGINE, OPS CHECK OK. INSPECTED NR 2 ENGINE OIL FILTER AND REPLACED. IDLE RUN PERFORMED AND FILTER CHECKED CLEAN. MAINTENANCE DONE PER PW MM 72-00-00, PAGE 136. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTA16WE E2EA 20040401000692004040100069NM 2004 4 1 UIEA200400010 120040205A5714 SKIN BOEING747 747243B 1384830NM FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, CENTER WING TANK, LOWER SKIN ABOVE NR 1 ACM FOUND CORRODED. LEVEL 1. CORROSION WAS BLENDED OUT WITH A MACHINED FINISH. THE BLENDED AREA WAS HFEC INSPECTED AND FLAP/SHOP PEENED. ALODINE PRIMER AND BMS 3-23 CORROSION INHIBITING COMPOUND WAS APPLIED TO THE BLENDED AREAS PER 747 SRM 57-10-01 FIGURE 2. (M) 2L74 4F A20WE 20040401000732004040100073NM 2004 4 1 SWAA040907 120040327A275256970 ACTUATOR BOEING737 7373H4 1384600NM TE FLAPS INOPERATIVE A SWAAA UNSCHED LANDING O OTHER APAPPROACH 1 SW29309SW 22948 DIVERSION, ON FINAL APPROACH TO BUR T/E FLAPS WOULD NOT EXTEND PAST 5 DEGREES. T/E FLAPS WOULD NOT RETRACT, T/E FLAPS WOULD NOT RETRACT/EXTEND WITH ALT FLAP. REMOVED AND REPLACED HYDRAULIC FLAP DRIVE MOTOR PER MM. 2L72 4F RTA16WE 20040401000772004040100077NM 2004 4 1 SWAA040905 120040326A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29452WN 29846 DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040401000782004040100078NM 2004 4 1 SWAA040906 120040326A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 917, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040401000792004040100079NM 2004 4 1 04FDEA00648 120040315A2750 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000812004040100081NM 2004 4 1 04FDEA00650 120040315A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000822004040100082NM 2004 4 1 SWAA040912 120040327A3350OL3071BPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED PM CHECK, FOUND AFT BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM. 2L72 4F RTA16WE 20040401000832004040100083NM 2004 4 1 SWAA040913 120040327A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C3 CHECK, FOUND AFT LOWER FLASHLIGHT IND LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20040401000852004040100085NM 2004 4 1 SWAA040916 120040328A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 26L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040401000862004040100086 2004 4 1 SWAA040917 420040328A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040401000882004040100088NM 2004 4 1 SWAA040919 120040328A3350604222 BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED PM CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM. 2L72 4F RTA16WE 20040401000912004040100091NM 2004 4 1 04FDEA00635 120040310A5753ARC1984502 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP AFT MOUNT AFT BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000922004040100092NM 2004 4 1 04FDEA00634 120040310A5753ARC1984502 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP I/B HINGE BRACKET (FLAP SIDE) TOP O/B AFT BOLT HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281, WINGS - RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000932004040100093NM 2004 4 1 04FDEA00636 120040310A5753ARC199114 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B FWD MOUNT HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B FWD MOUNT HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75282 TITLE WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040401000942004040100094NM 2004 4 1 04FDEA00637 120040310A5753ARC199114 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B AFT MOUNT HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER O/B AFT MOUNT HOLE CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75282 TITLE: WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040401000952004040100095NM 2004 4 1 04FDEA00638 120040310A5753ARC199114 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT FWD HOLE FOUND CORROSION. RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE) UPPER AFT MOUNT FWD HOLE CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75282 TITLE: WINGS - RIGHT O/B FLAP, O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040401000982004040100098NM 2004 4 1 04FDEA00651 120040315A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000192004033000019NM 2004 3 30 DL73S040220 120040308A53306545775553 SKIN BOEING737 737232 1384475NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27318DL 23090 THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT STRINGER 22R. THE DAMAGE WAS REMOVED WITH A 1 X .75 INCH CUTOUT FROM THE DOOR CUTOUT EDGE. THE DAMAGE WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 088918-14, REV A. 2L72 4F RTA16WE 20040330000212004033000021NM 2004 3 30 DL767040222 120040308A3397 WIRE BOEING767 767232 1385132NM LT WING BROKEN A DALAH DEACTIVATE SYST/CIRCUITS M OVER TEMP NRNOT REPORTED 1 SO27108DL 22220 MCO LEFT WING ILLUMINATION LIGHT INOP. FOUND LIGHT ASSY TERMINAL BOARD BROKEN AND WIRES DAMAGED WITH EVIDENCE OF ARCING. NDS NEW ASSY TO INCLUDE TERMINAL BLOCK NOT SHOWN IN IPC. NDS MFG P/N 30-1543-1. NASI DAL, PULLED AND COLLARED C/B N-35 WING ILLUM ON P11-6 C/B PANEL. MCO SOB. MCO DOCUMENTED AS MRR. 2L72 4F RTA1NM 20040330000362004033000036NM 2004 3 30 DL76P040250 120040320A3350BPS73 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27144DA 27584 EMERGENCY PATH LIGHTS INOP IN FIRST CLASS. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. 2L72 4F RTA1NM 20040330000382004033000038NM 2004 3 30 DLM88040252 120040321A3230 CONDUIT DOUG MD88 MD88 3023688NM LT MLG WW DAMAGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27984DL 53311 AFTER T/O FROM RSW HAD A LT GEAR UNSAFE LIGHT. CYCLED GEAR HANDLE, NO HELP. DIVERTED TO MCO. FOUND LT GEAR CONDUIT DAMAGED AND INTERFERRING WITH GEAR. PINNED AND SAFTIED LANDING GEAR. MTC FERRY A/C TO ATL FOR GEAR MTC. 2L72 4F RTA6WE 20040330000482004033000048NM 2004 3 30 2004UALA00251 120040313A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 LIGHTNING STRIKE HOLE AT STA 867 STR 5L ELONGATED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040330000562004033000056NM 2004 3 30 2004UALA00180 120040301A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29397UA 24672 CORROSION FOUND AT ST 1016 RBL 18 RT STRINGER. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20040330000612004033000061EU 2004 3 30 2004UALA00261 120040318A3150 ANNUNCIATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT FAILED A UALAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 WP29416UA 479 ABORTED TAKEOFF AT 110 KNOTS DUE TO LOSING BOTH FLIGHT MODE ANNUNCIATORS. PROBLEM COULD NOT BE DUPLICATED ON GROUND. POST FLIGHT REPORT DID NOT INDICATE ANY FAULT. FMGC1 WAS REPLACED AS A PRECAUTION. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040330000692004033000069 2004 3 30 IXXA0400013O 420040309A23105220536016 COUPLER DOUG DC8 DC871F 302199DWP HF SYSTEM CORRODED A IXXAA UNSCHED LANDING O OTHER CRCRUISE 1 SW11822BX879492059 45813 DURING CRUISE HF SYS WAS NOT RECEIVING, ELECTED TO RETURN. MX FOUND INCORRECT P/N'S INSTALLED FOR ACCESS COUPLER & TUNER COUPLERS. REMOVED & REPLACED COUPLERS. MX FOUND RECEIVE LINES FOR HF 1 & 2 FROM LIGHT ARRESTOR TO ACCESS COUPLERS CORRODED & SHORTED TO OUTER SHIELD. RAN NEW TO COAX CABLE FROM ARRESTOR TO ACCESS & REPLACED COAX FOR HF 1 & 2 FROM LIGHTING ARRESTOR TO ACCESS COUPLER. INSTALLED NEW CONNECTORS ON BOTH ENDS OF COAX TESTED SYS & DISCOVERED HF NR 1 TUNER WOULD NOT CHANNELIZE, NR 2 WOULD NOT TRANSMIT, HF 2 COUPLER WOULD NOT RECEIVE. REINSTALLED ORIGINAL EQUIPMENT & SYSTEM CHECKS GOOD PER ALL APPLICABLE MANUALS. RECIEVE 5X5 BY DIEGO HF AND AIRCRAFT EN ROUTE. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 20040330000922004033000092NM 2004 3 30 04FDEA00618 120040310A5311AFA78141 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK RIGHT FRAME INNER EDGE FOUND DENTED AT STA 1681 STR 12. REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA, CRACK FREE CONDITION. FOR REPETITIVE INSPECTION, EA 1-5330-75320 TITLE: FUSELAGE - FRAME REPAIRS - DTR TRACKING - FOR VARIOUS FRAMES BETWEEN STATIONS 5-113 & 1721 LEFT AND RIGHT AS DETAILED IN THE WORK STEPS. 2L73 4F RTA22WE 20040330000932004033000093NM 2004 3 30 04FDEA00619 120040310A5713ARB75121 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING STRINGER 12 SUSPECT CRACKED. LEFT WING STRINGER 12 REPAIRED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040330000982004033000098NM 2004 3 30 04FDEA00726 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330000992004033000099NM 2004 3 30 04FDEA00727 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT WING OUTBOARD FLAP, INBOARD HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040330001032004033000103WP 2004 3 30 04FDEA00731 120040323A5753ARC0502502 BRACKET DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET CORROSION REPAIR P/N ARC0502-502. COMPLIED WITH EA 8-5740-75121. 2L73 4F A22WE 20040330001092004033000109NM 2004 3 30 04FDEA00734 120040323A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 CORROSION ON STUB FRAME SHEAR TIE STA 950E 4 BETWEEN STR 28R AND 29R. 2L73 4F RTA3WE 20040330001172004033000117EU 2004 3 30 04FDEA00674 120040316A21701879421 COALESCER BAG AIRBUS310 A310 EU CABIN COOLING DIRTY A FDEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25409FE 273 ON CLIMBOUT PASSING 17,000 FT RECEIVED AVIONICS SMOKE WARNING ALERT, JUST PRIOR SMELLED A MUSKY BURNING ODOR. THE ODOR SEEMED TO INCREASE AND DECREASE IN INTENSITY. THEN RECEIVED AVIONICS SMOKE ALERT. DECLARED EMERGENCY, RETURNED TO MEM. UNABLE TO COMPLY. REMOVED AND REPLACED COALESCER BAGS. REF A310 AMM CH 21-51-16-4. TOOK A/C TO HIGH POWER. PERFORMED AIR COOLING SYSTEM SERVICING (DUCT BURNOUT). REF A310 AMM CH 21-51-00-3. NO AVIONICS SMOKE LITE OR ANY ABNORMAL ODORS NOTED. REMOVED AND REPLACED COALESCER BAGS AFTER HIGH POWER. FOUND OLD BAGS VERY DIRTY AND WET. 2L72 4F RTA35EU 20040331000042004033100004NM 2004 3 31 2004UALA00162 120040223A2420AS11706H0236 HOSE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 CSD LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29948UA 26691 RETURNED TO ORD WITH A NR 1 CSD OIL PRESSURE LIGHT. FOUND FLEX LINE FROM CSD SERVICE PORT TO TEE FITTING ON CSD LEAKING AT FITTING. REPLACED FLEX LI NE. AS PRECAUTIONARY, REPLACED CSD AND GEN. 2L72 4F4 FRTA16WE E2GL 20040331000272004033100027NM 2004 3 31 04FDEA00489 120040220A53116516342 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BS 1030, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55236 2L73 4F RTA3WE 20040331000302004033100030NM 2004 3 31 04FDEA00491 120040220A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 CRACKED SKIN AT BS 692, BL 0, WL 148. COMPLIED WITH FED EX EA 7-5330-70630 ON THE CRACKED SKIN AT B.S. 692, BL 0, WL 148. 2L73 4F RTA3WE 20040331000322004033100032NM 2004 3 31 UPS04541961 120040227A5753 SKIN BOEING757 75724APF 1384969NM RT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01446UP 27735 RIGHT O/B TRAILING EDGE FLAP HAS A 3 INCH CRACK. DEFERRED AS PER EO 757-5750-8002 D INITIAL REPAIR IS C/W. COMPLY W/FINAL REPAIR AT OR BEFORE NEXT C CHECK. D276705 ASSIGNED. C/W REPLACEMENT OF PANEL PER BOEING DRAWING 113N3600 AND EO #B757-5720-20123-A 2L72 4F RTA2NM 20040331000422004033100042NM 2004 3 31 04FDEA00564 120040303A5330APB74411 SKIN DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CORROSION AT RT STA 1219 TO 1239 FROM RT X-8.5 - 27 ON CENTER WING UPPER SKIN. CORROSION AREA AS PER EA 1-5710-74330, WINGS - CENTER WING UPPER PANEL - SKIN CORROSION. 2L73 4F RTA22WE 20040331000462004033100046NM 2004 3 31 04FDEA00342 120040207A5340A5A71151 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CENTER CARGO - LT TUNNEL AREA LONGERON NR 41 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACK. CRACK SPLICE AT CENTER CARGO- LH TUNNEL AREA LONGERON 41 BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040331000472004033100047NM 2004 3 31 04FDEA00340 120040206A5320A5A7114515 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 CENTER CARGO LOWER BILGE AREA LONGERON 50 RT SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACK. CRACK SPLICE AT CENTER CARGO LOWER BILGE AREA LONGERON 50 RT BETWEEN STA 5-113 AND STA 1541 REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 51-33-01 VOL. II. 2L73 4F RTA22WE 20040331000482004033100048NM 2004 3 31 SWAA040877 120040323A57126545444 RIB BOEING737 7373Y0 1384671NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND RT WING AT WBL 114, S2, UPPER RIB CRACKED. REPAIRED RT WING RIB PER ER. 2L72 4F RTA16WE 20040331000562004033100056NM 2004 3 31 SWAA040851 120040321A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT BS 440, LOWER STOP CRACKED. REPAIRED FRAME PER T1-653-044. 2L72 4F RTA16WE 20040331000782004033100078 2004 3 31 SWAA040834 420040318A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040331000812004033100081NM 2004 3 31 SWAA040837 120040318A53106546812 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 960 TO BS 986, LBL 60 TO LBL 65, WL 208, CORRODED. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040331000842004033100084NM 2004 3 31 SWAA040840 120040318A55106552282 WEB BOEING737 7377H4 1384404NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 DURING SCHEDULED 5Y CHECK, FOUND LT HORIZONTAL STAB WEB AFT OF UPPER LUG CRACKED. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040331001032004033100103NM 2004 3 31 SWAA040894 120040325A531065C22909 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500D, OUTBOARD OF RT KEEL BEAM. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20040331001052004033100105NM 2004 3 31 SWAA040882 120040324A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT L2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040401000092004040100009NM 2004 4 1 USAABB04014 120040127A4900 APU BOEING767 7672B7 1385107NM APU BAY SHUTDOWN A K NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 EA19653US 24894 SJU - WITH THE LT IDG ON MEL, THE APU WAS OPERATING ON THE GROUND. APU PERFORMED AN AUTO SHUTDOWN. APU WAS RESTARTED AND SHUTDOWN AGAIN. AFTER SEVERAL ATTEMPTS AT REPLACING COMPONENTS, SURGE VALVE, ECU, LCIT SENSOR, THE APU WAS REPLACED. A VERIFICATION FLIGHT WAS PERFORMED SUCCESSFULLY ON 12 FEB 04. (M) 2L72 4F RTA1NM 20040401000102004040100010NM 2004 4 1 USAABB04011 120040125A2760340545 SHUTOFF VALVE BOEING767 7672B7 1385107NM LEFT WING LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19652US 24765 MCO - FLT 1123 - EN ROUTE CLT-CUN, CREW NOTED THE LEFT HYDRAULIC QUANTITY DROPPING TO ZERO, AND THE EICAS MESSAGES 'L HYD PRIM PUMP' AND 'STAB TRIM.' FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT WING AILERON AND SPOILER SHUTOFF VALVE LEAKING AND REPLACED IT. (M) 2L72 4F RTA1NM 20040401000542004040100054NM 2004 4 1 AMTA200400164 120040212A3350 LIGHT BOEING757 75723N 1384973NM ROWS 7-9FED INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 EMERGENCY EGRESS LIGHTING 7 THROUGH 9 FED INOPERATIVE. REMOVED AND REPLACED EGRESS PATH LIGHT ASSEMBLY REF AMM 33-51-09, OPS CHECK OK. (M) 2L72 4F RTA2NM 20040401000602004040100060EA 2004 4 1 A6WA200440016 120040201A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31428AW 7695 GEAR UP DISAGREE MESSAGE AFTER TAKEOFF 60 SECONDS. THREE HYDRAULIC PUMP FAILED LANDING GEAR SWING TIME TEST. REMOVED AND REPLACED 3A HYDRAULIC PUMP IAW 29-12093. OPS AND LEAK CHECK GOOD. LANDING GEAR SWING TEST GOOD IAW AMM 32-20-00. (M) 2L72 4F RTA21EA 20040401000612004040100061 2004 4 1 2004F00088 420040202A22107002800901 ACTUATOR CESSNA750 750 2076810CE YAW DAMPER INOPERATIVE A UG8AO OTHER J WARNING INDICATION CRCRUISE 1 GL235116 7500019 BLUE YAW DAMPER, FAIL LOWER 'B' CAS MESSAGE, AMBER YAW DAMPER OFF LOWER CAS MESSAGE AND PRI STAB TRIM FAIL AND MACH TRIM OFF CAS MESSAGE CAME ON DURING FLIGHT. CHANNEL 'B' YAW DAMP ACTUATOR FAILED TO OPERATE. REPLACED CHANNEL 'B' YAW DAMP ACTUATOR. OPERATIONAL CHECK NORMAL. (M) 2L72 4J RTT00007WI 20040401000762004040100076NM 2004 4 1 SWAA040910 120040327A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 DURING SCHEDULED MV2 CHECK, FOUND LT EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040401000992004040100099NM 2004 4 1 04FDEA00652 120040315A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RIGHT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401001012004040100101NM 2004 4 1 04FDEA00622 120040310A5753ARC25943 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING I/B FLAP O/B HINGE BRACKET MOST AFT UPPER BRACKET FOUND CRACKED. REPAIRED CARRIED OUT AT RIGHT WING I/B FLAP O/B HINGE AS PER EA 1-5750-75299, TITLE: WINGS - I/B T/E FLAP, O/B HINGE FAIRING (FLAP SIDE) UPPER AFT RIB - REPAIR. 2L73 4F RTA22WE 20040401001032004040100103WP 2004 4 1 04FDEA00683 120040320A5230 SEAL DOUG DC10 DC1030 3023501WP CARGO DOOR OUT OF POSITION A FDEAA UNSCHED LANDING GJSMULTIPLE FAILURE WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO25302FE 46801 APPROX 7,000 FT, ACFT FAILED PRESSURIZATION & CENTER ACCESS COMPT FLOW OFF LIGHT ILLUMINATED. RAN RED TABS ON AND AT APPROX 3K ACFT REGAINED PRESSURIZATION AND LIGHT WENT OUT. RETURNED TO BASE. PERFORMED ALL DOORS SEALS INSPECTION. AFTER PRESSURIZING A/C FOUND 2 FEET OF SEAL OUT OF TRACK ON FWD LOWER CARGO DOOR AFT CORNER, ALSO AROUND 10 INCHES OFF TRA CK FROM MAIN CARGO DOOR LWR AFT CORNER. RE-INSTALLED SEALS AND PERFORMED A/C PRESS PER JRH CHP 7-1. GROUND OPS CKS GOOD. 2L73 4F A22WE 20040401001042004040100104NM 2004 4 1 04FDEA00691 120040322A5320 INTERCOSTAL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 WHILE WORKING CARD N00237 FOUND CORROSION ON INTERCOSTAL BS 580-600 LBL 7. REMOVED & REPLACED INTERCOSTAL AT BS 580-600 LBL 7 IAW SRM 51-30-2, 51-20-1. 2L73 4F RTA3WE 20040401001062004040100106NM 2004 4 1 04FDEA00743 120040325A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENT AT FS Y= 1761 BETWEEN LONGERON 12L AND LONGERON 13L. COMPLIED WITH FEDEX EA 1-5310-76001, REPAIRED TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2L73 4F RTA22WE 20040401001082004040100108NM 2004 4 1 04FDEA00746 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1661 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3380. 2L73 4F RTA22WE 20040401001102004040100110NM 2004 4 1 04FDEA00748 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1701 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2L73 4F RTA22WE 20040401001122004040100112NM 2004 4 1 04FDEA00736 120040323A5531 SPAR BOEING727 727200 138407ENM VERTICAL STAB CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 VERTICAL STAB MID SPAR CHAFED AT PANEL 9601 (LT SIDE). REPAIRED DAMAGED AREA ON VERTICAL STAB MID SPAR BEHIND PANEL 9601 PER FED EX EA 7-5530-76229 AND SRM 55-30-6 FIG 3. 2L73 4F RTA3WE 20040401001162004040100116NM 2004 4 1 SWAA040868 120040323A3040830005602 WINDOW BOEING737 7373H4 1384600NM COCKPIT ARCED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29631SW 27706 AT FL 350 COCKPIT R2 OUTER PANE CRACKED WHILE ARCING. REMOVED AND REPLACED COCKPIT R2 WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20040401001172004040100117NM 2004 4 1 SWAA040869 120040323A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 RT OVERWING EMERGENCY EXIT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20040401001182004040100118NM 2004 4 1 SWAA040870 120040323A2910AS116080264 HOSE BOEING737 7373T5 1384608NM B HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW29667SW 23063 DIVERSION, HYD B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, QUANTITY ALMOST ZERO. REMOVED AND REPLACED HYD-B SYSTEM PRESSURE HOSE PER MM. 2L72 4F RTA16WE 20040401001192004040100119NM 2004 4 1 SWAA040871 120040323A3350BR2013 LIGHT BOEING737 7372H4 138448CNM OVERWING EXIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SPV, FOUND EEPLS AT OVERWING EXIT INOP. REPAIRED WIRE PER WPM. 2L72 4F A16WE 20040401001202004040100120NM 2004 4 1 SWAA040872 120040323A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHT AT LT OVERWING HATCH LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20040401001212004040100121NM 2004 4 1 SWAA040873 120040323A53306545765 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 500A + 5, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040401001222004040100122NM 2004 4 1 SWAA040874 120040323A53306545800 SKIN BOEING737 7373Y0 1384671NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 284, BETWEEN STRINGERS 23R AND 24R, CREASED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040401001232004040100123NM 2004 4 1 DHL2004749004 120040316A2510 SEAT BACK BOEING727 727200 138407ENM COCKPIT SEAT DAMAGED A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01749DH 22013 CAPTAINS SEAT BACK POPPING OUT OF LOCK POSITION WHEN MINIMAL PRESSURE APPLIED, IE TAKEOFF ACCELERATION, SETTING BRAKES. LUBED AND OPERATED CAPTAINS SEAT BACK IAW B-727 M/M 25-10-41. OPS CHECKED NORMAL NO DEFECTS NOTED. 2L73 4F RTA3WE 20040401001242004040100124 2004 4 1 MWEA040023 420040221A2565 PIN DOUG DC9 DC981 3022081WP SLIDE INOPERATIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 AFT SERVICE DOOR ESCAPE SLIDE PIN WILL NOT STAY IN POSITION. INSTALLED SLIDE COVER. 2L72 4F A6WE 20040401001252004040100125NM 2004 4 1 AALA20040357 120040316A33500201720001 LIGHT BOEING767 767323 1385205NM SEAT 40D LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21382AN 25451 SFO - EMERGENCY SEAT MOUNTED AISLE LIGHTING AT SEAT 40D LOOSE. REPLACED NUT PLATE AND LIGHT ASSEMBLY FOR EMERGENCY SEAT MOUNTED AISLE LIGHTING AT SEAT 40D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040401001272004040100127NM 2004 4 1 AALA20040353 120040315A33501703663 SOCKET BOEING757 757223 1384957NM EMERGENCYLIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21630AA 24588 BOS - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED WIRE CONTACT SOCKET FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040401001332004040100133EU 2004 4 1 PIV2004F00000 120040118A335059461 LAMP STBROSSD3 SD360 8100606EU PWA PT6 PT6A60A 52043NE EMERGENCY LIGHT BURNED OUT A PIVAO OTHER O OTHER NRNOT REPORTED 1 WP13711HJ SH3697 FWD BULKHEAD FLOOR AND LT WALL EXIT SIGNS. FLOOR PROXIMITY LIGHT NEEDS REPAIRED. ITEM HAD TO BE DISCONNECTED TO ALLOW FOR DOOR MODIFICATION INSTALLATION. FWD, TWO FLOOR PROXIMITY ESCAPE PATH TAPE BUSBAR SINGLE LAMP ARE BROKEN. REPLACED 1 EACH SINGLE TAPE BUSBAR, DUE TO DOOR MODIFICATION PROJECT. ALL CABIN EMERGENCY PROXIMITY LIGHTS REPLACED DUE TO UNCLEAR, BURNED OUT DURING THE DOOR MODIFICATION. 2H72 4T4 T A41EU E4EA 20040401001352004040100135NM 2004 4 1 JGV2004F00002 120040217A531025W342121431XVM4DOUBLER ISRAEL1125 1125 NM GARRTTTFE731TFE731* 01518WP WINDOW FRAME CRACKED B JGVRK NONE O OTHER ININSP/MAINT 1 CE09790FH3646 056 DURING C CHECK INSPECTION FOUND CABIN WINDOWS CRACKED. INSPECTED CABIN WINDOW FRAME DOUBLER. DISCOVERED CRACKS IN THE NUT PLATE HOLE. RT NR 3, NR 4, AND NR 5 AND LEFT NR 3 WINDOW POSITIONS. CAUSED FROM MINIMUM EDGE DISTANCE AND NUT PLATE HOLE ENLARGEMENT. (CE09200402199) 2L72 4F4 FRTA16NM E6WE 20040401001362004040100136CE 2004 4 1 WVE2004F00001 120040112A323324170161 ACTUATOR LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE NLG ACTUATOR CORRODED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09237FX4170 158 DURING 1200 HOUR INSPECTION OF NOSE LANDING GEAR FREE FALL ACTUATOR, FOUND ACTUATOR TO HAVE MAJOR CORROSION ON INSIDE OF ACTUATOR. WATER ENTERING ROD END OF ACTUATOR DUE TO LACK OF A MORE EFFECTIVE MOISTURE SEAL. MFG EVALUATION. (EA09200401492) 2L72 4F4 FRTA10CE E35NE 20040401001372004040100137EU 2004 4 1 QWP2004F00000 120040205A3213100A703029 STRUT BAG JETSTMJETSTM3201 1500217EU MLG CRACKED B QWPRO OTHER O OTHER NRNOT REPORTED 1 SO05488UE8433 8433 907 THE PISTON WAS FORCED OUT OF THE END OF THE SLIDE TUBE, SHEARING 2 GRUB SCREWS AND DAMAGING 2 OTHER GRUB SCREWS AND CRACKING THE SLIDE TUBE. THE SLIDE TUBE AND PISTON ARE NOT REPAIRABLE. CIRCUMSTANCES UNDER WHICH IT OCCURRED, UNKNOWN. PROBABLE CAUSE, UNKNOWN. 2L72 4T RTA56EU 20040401001382004040100138CE 2004 4 1 TCH2004F00001 120040211A7830713352 CONTROL VALVE LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE THRUST REVERSER INOPERATIVE E TCHAO OTHER O OTHER NRNOT REPORTED 1 GL03252RP541 235 LT REVERSER ARM LIGHT WOULD NOT EXTINGUISH. FOUND THAT A PRESSURE SWITCH ON THE CONTROL VALVE WAS NOT OPENING. PROBLEM WAS FOUND PRIOR TO DEPARTURE, ON THE RAMP AFTER ENGINE START. 2L72 4F4 FRTA10CE E35NE 20040401001462004040100146EU 2004 4 1 TRB2004F00007 120040104A3220C255890002 UPLOCK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE NLG UNLOCKED A TRBAO OTHER O OTHER LDLANDING 1 SO21248AT2947 248 A NOISE WAS HEARD UNDER THE CAPTAIN SEAT WHEN GEAR IS EXTENDED. REMOVED AND REPLACED UPLOCK BOX. 2H72 4T4 TRTA53EU E20NE 20040401001472004040100147NE 2004 4 1 TRB2004F00008 220040112A7230CT602 CHECK VALVE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COMPRESSOR FAILED A TRBAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO21434AT2787 434 1279 DURING TAKEOFF THE LT ENGINE ITT EXCEEDED THE LIMITS. REMOVED AND REPLACED THE LT ENGINE P2.5 CT CHECK VALVE. 2H72 4T4 TRTA53EU E20NE 20040401001482004040100148SW 2004 4 1 LDI2004F00000 120040209A3220 TRUNNION PIN GULSTM690TP 690B 7630516SW GARRTTTPE331TPE331* 01514WP NLG SEIZED E LDIAO OTHER O OTHER NRNOT REPORTED 1 SW0525RZ 4173 11518 NOSE GEAR WOULD NOT RETRACT. TRUNNION PINS HAD FROZEN UP. TRUNNION PINS DO NOT HAVE ANY LUBRICATION GREASE ZERTS WHICH COULD HAVE PREVENTED THE NOSE GEAR TRUNNION FROM FREEZING UP. 1H72 3T3 T 2A4 E2WE 20040401001492004040100149SO 2004 4 1 FPI2004F00001 220040217A741410357586 DISTRIBUTOR GEAR CESSNA210 T210M 2073451CE CONT O550 IO550* SO MAGNETO LOOSE E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO157398M850 0020A084 21062018 821030R DISTRIBUTOR GEAR FINGER LOOSENED UP AT SHAFT. 1H71 3O3 O 3A21 E3SO 20040401001512004040100151CE 2004 4 1 WK42004F00001 120040210A3244265K682 TIRE RKWELLNA265 NA26560 7630106CE PWA JT12 JT12A6A 52042NE MLG DAMAGED B WK4RO OTHER O OTHER NRNOT REPORTED 1 SO17353CA31 306028 CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT HAND TIRE. 2L72 4J4 JRTA2WE 1E9 20040401001542004040100154CE 2004 4 1 S1F2004F00000 120040211A24979536001215 BUSS BAR BEECH 58 58 1152740CE CONT O550 IO550* SO ELECTRICAL INOPERATIVE B S1FRO OTHER O OTHER NRNOT REPORTED 1 SO3387RG 679 TH1886 BUSS BAR ON EXTERNAL SUPPLY NEGATIVE POST HAD NO GROUND. BUSS BAR HAD MASKING TAPE ON IT WHEN FACTORY HAD PAINTED IT AND INSTALLED WITHOUT REMOVING TAPE. THEREFORE NO GROUND FOR EXTERNAL SUPPLY. 1L72 3O3 O 3A16 E3SO 20040401001562004040100156EU 2004 4 1 OWF2004F00001 120040214A5753S5701007900 BRACKET AEROSPATR42 ATR42300 8680920EU RT FLAP CRACKED B OWFRO OTHER O OTHER NRNOT REPORTED 1 CE05908FX28981 023 BRACKET CRACKED FROM CORRODED FOUND DURING C CHECK INSPECTION. UNIT REPLACED WITH NEW PART. 2H72 4T RTA53EU 20040401001682004040100168CE 2004 4 1 W6N2004F00000 120040223A2910572700258 LINE CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP RT HYDRAULIC SYSCRACKED B W6NRO OTHER O OTHER NRNOT REPORTED 1 GL25441LS 4410342 WHILE ON ROLL OUT PILOT REPORTED HYDRAULIC FLOW ENUNCIATOR CAME ON AIRCRAFT CIRCLED AROUND AND TAXIED UP TO REPAIR STATION AND MECHANICS FOUND CRACKED HYDRAULIC LINE ON THE RADIUS OF A BEND ON THE LINE. 1L72 3T3 TRTA28CE E2WE 20040406000052004040600005NM 2004 4 6 04FDEA00790 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76003. 2L73 4F RTA22WE 20040406000092004040600009NM 2004 4 6 CALA0400314 120040403A5347BAC15101355 CARGO TRACK BOEING737 737824 13844BZNM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND AFT CARGO FLOOR RAIL GOUGED AT STA 727J-5, RBL 3.0. REPAIRED IAW SRM 53-00-53, FIGURE 201, PAGE 202-203. 2L72 4F RTA16WE 20040406000172004040600017NM 2004 4 6 04FDEA00780 120040331A5753 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING STOP FITTING ASSEMBLY ON OUTBOARD FLAP CRACKED AT BARREL NUT BORE AREA. CRACKED STOP FITTING ASSY ON OUTBOARD FLAP AT RT WING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040406000182004040600018NM 2004 4 6 04FDEA00781 120040331A5753 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT WING STOP FITTING ASSEMBLY ON OUTBOARD FLAP CRACKED AT BARREL NUT BORE AREA. CRACKED STOP FITTING ASSY ON OUTBOARD FLAP AT LT WING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20040406000192004040600019NM 2004 4 6 04FDEA00782 120040331A5751 FITTING BOEING727 727200 138407ENM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 LEFT WING INBOARD AILERON HINGE FITTING AND WEB IS CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-1, REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-10-1 AND BOEING DWG 65-21709. 2L73 4F RTA3WE 20040406000202004040600020 2004 4 6 04FDEA00783 420040331A3443 IRU AIRBUS310 A310 EU NR 1 FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25410FE 356 AFTER T/O 1 IRU FAILED, 2 IRU WAS ALREADY MEL'D INOP. RETURN TO DFW. REMOVED AND REPLACED THE 1 IRU PER MM 34-25-00 -05-1, PERFORMED IRS SYS ADJ/TEST IN CONJUNCTION WITH WRI 34-43-6941 (IRU 3) AND WRI 34-43-6937 (IRU 2). ALL IRU'S TESTED NORMAL. PERFORMED AFS/LAND TEST, TEST PASSED. A/C CAT STATUS PLACED INTO A/C CAT II; AP1 & 2 CK CAT III. 2L72 4F RTA35EU 20040406000212004040600021NM 2004 4 6 04FDEA00785 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000222004040600022NM 2004 4 6 04FDEA00786 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000262004040600026NM 2004 4 6 04FDEA00685 120040322A533065545913 BEAR STRAP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25258FE 20940 MAIN FRAME, FWD LWR CARGO DOOR BEAR STRAP CORRODED (AD 98-11-03R1). COMPLIED WITH EA 7-5310-73889A FUSELAGE - MAIN FRAME, FWD LWR CARGO DOOR BEAR STRAP CORROSION REPAIR (AD 98-11-03 R1). 2L73 4F RTA3WE 20040406000272004040600027WP 2004 4 6 04FDEA00686 120040322A5751 FITTING DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 RIGHT INBOARD AILERON O/B HINGE SUPPORT FITTING CRACKED. REMOVED SUPPORT FITTING IAW M/M 53-23-01, RECEIVED SUPPORT FITTING WITH TRAVLER T4/414610, FIT AND DRILLED IAW SRM 51-35-01 AND INSTALLED SUPPORT FITTING IAW SRM 53-33-01. 2L73 4F A22WE 20040406000282004040600028NM 2004 4 6 04FDEA00687 120040322A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 CORROSION ON FWD CARGO STRINGER 28L BS 570. *S/D* REMOVED AND REPLACED FWD CARGO STRINGER 28L BS 570 TO BS 610 AND STRINGER CLIPS AT BS 580 AND BS 600 WITH WORK DONE IAW SRM 53-10-2, 53-10-3, 51-30-2. 2L73 4F RTA3WE 20040406000312004040600031NM 2004 4 6 04FDEA00692 120040322A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 WHILE WORKING CARD N00237 FOUND SKIN CORRODED BS 585-596 LBL 5 WL 148. REMOVED CORROSION ON SKIN BS 583 - 596 LBL 5 OF A AREA 17 X 2 INCHES WITH BLEND OUT LOWEST MEASUREMENT .042 OF ORIGINAL .098. FOUND OUT OF LIMITS IAW SRM 53-10-1. INSTALLED REPAIR DOUBLER IAW 53-30-3 FIG 3. 2L73 4F RTA3WE 20040302000152004030200015NM 2004 3 2 SWAA040429 120040210A3350100031 SIGN BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C4 CHECK, FOUND OVERWING OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20040302000382004030200038NM 2004 3 2 SWAA040367 120040205A3350612825 BATTERY BOEING737 7372H4 138448CNM CABIN FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EMERGENCY EXIT LIGHT FLICKERS INTERMITTENTLY. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040302000472004030200047NM 2004 3 2 SWAA040259 120040127A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 EMERGENCY EXIT LIGHT AT ROW 13 DEF SIDE LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20040302000492004030200049NM 2004 3 2 SWAA040261 120040127A3350101073 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29405WN 27893 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040302000502004030200050NM 2004 3 2 SWAA040262 120040127A57546573714 SLAT BOEING737 7372H4 138448CNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 SLAT CRACKED AT INBOARD END. REPAIRED SLAT CRACK PER RA. 2L72 4F A16WE 20040302000622004030200062NM 2004 3 2 AALA20040245 120040213A275118173819 TRANSMITTER BOEING737 737823 13844BZNM T/E FLAP FAILED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21976AN 30099 AFTER TAKEOFF FLAPS WOULD NOT RESPOND TO FLAP UP SETTING. WHEN ATTEMPTING TO SELECT FLAPS EXTENSION USING ALTERNATE FLAPS SWITCH AN ASYMMETRICAL FLAP INDICATION OCCURRED. FLAP HANDLE IN 2 DEG, RT INDICATOR 1.25 DEG, LT INDICATOR 1.5 DEG, L/E DEVICE INDICATORS ALL ILLUMINATED YELLOW. THERE WAS NO NOTICEABLE ROLL WHEN FLAP INDICATOR SHOWED AN ASYMMETRICAL CONDITION. PRIOR TO INITIATING PROCEDURE FLAP POSITION/SKEW SENSOR & INDICATOR CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, IT IMMEDIATELY POPPED AGAIN. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LAND CHECK, NO DEFECTS OR DAMAGE FOUND. REPLACED LT FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040302000752004030200075NM 2004 3 2 AALA20040258 120040220A2910 SEAL BOEING767 767323 1385205NM NR 1 SPOILER DAMAGED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21387AM 27184 LAX - INFLIGHT T192/20 AFTER TAKEOFF CENTER HYDRAULIC SYSTEM QUANTITY WENT TO ZERO WITH R/F SHOWING CENTER SYSTEM PRESSURE LIGHT ILLUMINATED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 SPOILER FILTER SEAL. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040302000762004030200076NE 2004 3 2 AALA20040259 220040221A731438430110 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED A AALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW21448AA 49474 725471 ATL INFLIGHT T593/21 ON ROTATION LEFT HAND ENGINE UNCOMMANDED SHUTDOWN. RETURNED TO ATL AND LANDED WITHOUT INCIDENT. REPLACED NUMBER 1 ENGINE FUEL CONTROL (76960612-HAMILTON SUNDSTRAND) AND FUEL PUMP. TRIMMED ENGINE TO PROPER PARAMETERS PER 71-00-00 PAGE 501. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20040302000782004030200078NM 2004 3 2 CALA0400142 120040220A575465C26793 SKIN BOEING737 7373T0 1384582NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND 0.2 INCH CRACKS AT THREE FASTENERS IN NR 3 SLAT LOWER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206. 2L72 4F RTA16WE 20040302000862004030200086NM 2004 3 2 CALA0400150 120040222A551018130006 FITTING BOEING737 737824 13844BZNM HORIZ STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND THE LT UPPER AFT EDGE OF HORIZONTAL STABILIZER BOX LUG GOUGED. THE GOUGE WAS REPAIRED IAW ECRA 5510-01721. 2L72 4F RTA16WE 20040302000972004030200097NM 2004 3 2 CALA0400155 120040223A5320149A761116 WEB BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND A 1 INCH CRACK IN LT WHEEL WELL FAIRING ASSEMBLY O/B WEB. THE WEB WAS REMOVED AND REPLACED IAW EA 5310-04230. 2L72 4F RTA16WE 20040302001082004030200108NM 2004 3 2 CALA0400134 120040218A532065C3397053 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723657 28918 INSPECTION FOUND A HOLE IN CABIN FLOOR INTERCOSTAL JUST FORWARD OF STA 360, BL 0. A REPAIR WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040302001092004030200109NM 2004 3 2 CALA0400135 120040219A5415313A1380134 ATTACH FITTING BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A .25 INCH CRACK IN NR 2 PYLON PANEL 5842 FORWARD ATTACH RAIL. THE ATTACH RAIL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040302001182004030200118EA 2004 3 2 COMA0460158 120040221A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAO OTHER O OTHER UKUNKNOWN 1 SO01484CA 7702 FLIGHT 5376 EMERGENCY LIGHTS AFT OF EXIT ROW ARE INOP. REPLACED FLEXIBLE LAMP SECTION. 2L72 4F RTA21EA 20040302001242004030200124NM 2004 3 2 DHL2004781002 120040225A7997 WIRE BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE OIL TEMP BROKEN A DHLAE ENGINE SHUTDOWN N FALSE WARNING NRNOT REPORTED 1 SO01781DH 21996 707130 ENGINE NR 3 OIL TEMPERATURE WENT ABOVE 165 DEGREES CELSIUS, NEEDLE STUCK OFF SCALE HIGH. ACCOMPLISHED ABNORMAL PROCEDURE. OIL TEMPERATURE ABOVE 165 DEGREES CELSIUS FOR 5 MINUTES BEFORE SHUTDOWN OF ENGINE. ACCOMPLISHED IN-FLIGHT FAILURE SHUTDOWN CHECK LIST. ENGINE NR 3 OIL PRESSURE AFTER SHUTDOWN WAS 40 PSI AND ENGINE SHUTDOWN FOR 20 MINUTES WITH N2 ABOVE 25 PERCENT. FOUND WIRE BROKEN BEHIND NR 3 ENGINE OIL TEMPERATURE BULB CONNECTOR. REPAIRED WIRE PER WDM 79-33-01. ALSO REMOVED AND REPLACED OIL TEMPERATURE BULB PER B-727 M/M 79-34-21. RAN ENGINE PER JRH. OPS CHECKED SERVICEABLE P/N: INSTALLED OF TEMPERATURE BULB 102-00002. 2L73 4F4 F A3WE E2EA 20040302001372004030200137NM 2004 3 2 SWAA040274 120040128A335010114 LENS BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040302001492004030200149NM 2004 3 2 SWAA040299 120040130A32336544610 ACTUATOR BOEING737 7373H4 1384600NM NLG FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29391SW 27378 AIRTURN BACK, ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RETURNED TO HOU WITH 3 GREEN GEAR LIGHTS. GEAR EXTENDED NORMALLY. REMOVED AND REPLACED NOSE GEAR RETRACT ACTUATOR PER MM. 2L72 4F RTA16WE 20040302001502004030200150NM 2004 3 2 SWAA040300 120040130A534365C10300 FITTING BOEING737 7372H4 138448CNM NLG CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND NOSE GEAR ACTUATOR UPPER SUPPORT FITTING AND BRACKET CRACKED AT CROSS BEAM INTERSECTION. REMOVED AND REPLACED FITTING AND BRACKET PER SRM. 2L72 4F A16WE 20040302001532004030200153NM 2004 3 2 SWAA040303 120040130A53116545812 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STRINGERS 20R AND 21R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040302001602004030200160NM 2004 3 2 SWAA040310 120040130A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BUSHINGS PER MM. 2L72 4F RTA16WE 20040302001672004030200167NM 2004 3 2 SWAA040317 120040130A53116546551 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULE D CHECK, FOUND FRAME CRACKED AT BS 807, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040302001742004030200174NM 2004 3 2 SWAA040377 120040208A52306547952 SEAL BOEING737 737317 138447PNM CARGO DOOR TORN A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29661SW 23173 DECLARED EMERGENCY, AIRCRAFT EXPERIENCED A MILD DEPRESSURIZATION AT 31,000 FEET NOTICED BY ALT. WARNING HORN GOING OFF. CABIN PRESSURE REACHED 10,00 FEET WENT TO STANDBY AND THEN MANUAL TO CONTROL CABIN. DESCENDED TO 14,000 WHERE STANDBY WORKED. REMOVED AND REPLACED AFT CARGO DOOR SEAL PER MM. 2L72 4F RTA16WE 20040302001752004030200175NM 2004 3 2 SWAA040378 120040207A3350101114 LENS BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 RT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20040302001842004030200184NM 2004 3 2 SWAA040387 120040207A32116582770 BEAM BOEING737 7373Y0 1384671NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND CORROSION ON RT MLG BEAM FASTENER HOLES LOWER BEAM. REPAIRED RT MLG BEAM PER ER. 2L72 4F RTA16WE 20040302001902004030200190NM 2004 3 2 SWAA040393 120040207A57536573732 FLAP BOEING737 7373T5 1384608NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 RT WING OUTBOARD AFT FLAP T/E DELAMINATED. REPAIRED RT WING T/E FLAP PER SRM. 2L72 4F RTA16WE 20040302001912004030200191 2004 3 2 SWAA040394 420040207A2565D31354 SLIDE BOEING737 7375H4 138449DNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 UNABLE TO SEE L2 DOOR EVAC SLIDE PRESSURE GAUGE AFTER MULTIPLE REINSTALL ATTEMPTS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040302001922004030200192 2004 3 2 SWAA040395 420040207A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040302001932004030200193NM 2004 3 2 SWAA040396 120040207A57536573732 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT FLAP T/E DELAMINATED. REPAIRED RT AFT T/E FLAP PER SRM. 2L72 4F RTA16WE 20040303000142004030300014EA 2004 3 3 COMA0470020 120040212A3260 TARGET CNDAIRCL600 CL6002C10 1390015EA NLG OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01641CA 10122 FLIGHT 5213, GEAR DISAGREE WARNING ADJUSTED THE NLG (CENTERED) PROXIMITY SENSOR TARGET. 2L72 4F RTA21EA 20040303000152004030300015EA 2004 3 3 COMA0470021 120040215A2781 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLATS ILLUMINATED A COMAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION LDLANDING 1 SO01378CA 10097 FLIGHT 5073, SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, NO FAULTS IN COMPUTER, OPERATIONAL TEST SATISFACTORY. 2L72 4F RTA21EA 20040303000182004030300018NM 2004 3 3 CALA0400126 120040216A53406545833212 ATTACH ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND ATTACH ANGLE FOR FLOOR PANEL AROUND GEAR DOWNLOCK VIEWER CORRODED AT AFT ATTACH ANGLE, BS 270, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01172. 2L72 4F RTA16WE 20040303000302004030300030NM 2004 3 3 P5CA0401038 120040216A2710 CONNECTOR BOEING747 747236B 1384804NM AILERON CONTROL LOOSE A P5CAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 WP23924FT 21730 NO AILERON MOVEMENT DURING FLT CONTROL CHECK. CLEANED AND RESECURED CONNECTOR D3296P AT J42-J-BOX. OPS CK OK, IAW MM 27-11-00. 2L74 4F A20WE 20040303000482004030300048NM 2004 3 3 VNAA0402008 120040216A3260 PSEU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE E/E BAY MALFUNCTIONED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07429JS 3043 DURING TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING FAIL AND PROXY SYSTEM FAILED AND THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. TAXI CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040303000522004030300052NE 2004 3 3 BAQA092556 220040119A7412HE402F GENERATOR AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE IGNITION SYS INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 899 6036 WARRANTY. UNIT INOPERATIVE. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE UNIT. 02/05/2004 1G72 3U3 U H10EU E19EU 20040303000802004030300080EA 2004 3 3 SWIA200412929 120040218A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 1 MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07720SW4 4 7297 SPOILERON FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SECU IAW CRJ MM 27-61-05 AND LEFT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPS CHECK GOOD. PCU P/N: 27000-7, S/N OFF: MAL-4191. 2L72 4F RTA21EA 20040303000832004030300083CE 2004 3 3 GNL2004F00001 120040209A3233508202085 ACTUATOR BEECH 90 E90 1152914CE PWA PT6 PT6A60A 52043NE NLG FAILED E GNLAK NONE O OTHER ININSP/MAINT 1 SW01304LG5770 LW231 NLG ACTUATOR FAILED ON RETRACTION, STRIPPED INTERNAL GEARS, IN THE SHAFT 5770 CYC/OH. 1L72 3T4 T 3A20 E4EA 20040303000842004030300084WP 2004 3 3 0400279862 120040129A5330 SKIN DOUG DC9 DC951 3022051WP PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01771NC 47769 DURING "L" CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 69.55 3.5 INCHES BELOW L14L. REPAIRED IAW EA 98-197450. 2L72 4F4 FRTA6WE E2EA 20040303001032004030300103WP 2004 3 3 ABXA040076 120040210A531399114279 LONGERON DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 STA. 1040 LONGERON 17 LT CRACKED. SPLICED IN NEW SECTION OF LONGERON IAW DC-9 SRM 53-02. 2L72 4F A6WE 20040303001102004030300110WP 2004 3 3 ABXA040066 120040205A57129919301506 RIB DOUG DC9 DC941 302207NWP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 RT WING LE HAD CRACKED RIB AT LOWER NUTPLATES FOR NR 2 IB SLAT TRACK RIB. FOUND 4 CRACKS, REPAIRED IAW REA D957-49005 AND INSTALLED NUTPLATES IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20040303001112004030300111 2004 3 3 QXEA200400160 420040216A34257003360941 AHRS DHAV DHC8 DHC8202 2809007NM E/E BAY MALFUNCTIONED A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09354PH13768353 498 PDX - ON FLIGHT 2126 HSI HEADING MISMATCH ON ADVISORY DISPLAY. PER CHECKLIST RESETS OK BUT REAPPEARS. REMOVED AND REPLACED NR 1 AHRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040303001172004030300117NM 2004 3 3 SWAA040553 120040222A57536573732 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED SERVICE CHECK, FOUND RT WING RT OUTBOARD T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM. 2L72 4F RTA16WE 20040303001232004030300123NM 2004 3 3 SWAA040530 120040220A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29632SW 27707 FORWARD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040303001302004030300130NM 2004 3 3 2004UALA00133 120040216A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29643UA 25093 EMERGENCY EXIT LIGHT AT NR 2AB ROW INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT, OPS OK. 2L72 4F4 FRTA1NM E24NE 20040303001312004030300131NM 2004 3 3 2004UALA00134 120040213A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 SKIN DAMAGE AT BS 847, BETWEEN STR 21R & 22R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR QUADRUPLER. 2L72 4F4 FRTA16WE E2GL 20040303001382004030300138NM 2004 3 3 SWAA040536 120040220A575369729901 WEDGE BOEING737 7377H4 1384404NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 DURING SCHEDULED 5Y CHECK, FOUND LT WING OUTBOARD AFT FLAP T/E WEDGE DELAMINATED. REPAIRED T/E WEDGE PER SRM. 2L72 4F RTA16WE 20040303001502004030300150NM 2004 3 3 2004UALA00142 120040216A5320 STRUCTURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29397UA 24672 CABIN UPPER LOBE BS 907 STR 4R AND 4L HAS CRACKS COMING FROM RIVET HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040303001512004030300151NM 2004 3 3 2004UALA00143 120040217A5311 FRAME BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 UPPER T-CHORD ON THE FRAME AT BS 720, APPROX RBL 15 HAS A DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLES, SHIMS AND FILLER. 2L74 4F4 FRTA20WE E24NE 20040303002072004030300207EU 2004 3 3 BAQA092790 120040212A28200319738330 MANIFOLD UROCOPEC135 EC135T1 5620026EU NR 1 ENG FUEL INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME62 0143 NR 1 ENGINE NOT LIGHTING OFF ON ALL START ATTEMPTS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/19/2004 1G72 3U H88EU 20040303002132004030300213NM 2004 3 3 CALA0400199 120040301A534765C80736153 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND LT TIE DOWN RAIL LOWER FLANGE DAMAGED BY A SCREW BETWEEN STA 747-767 ABOVE STRINGER 29L. A NEW TIE DOWN RAIL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040303002172004030300217NM 2004 3 3 2004UALA00124 120040215A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29595UA 28748 FUSELAGE SKIN IS DAMAGED AT BS 1440 AND SKIN LAP 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040303002202004030300220NM 2004 3 3 04FDEA00435 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002232004030300223NM 2004 3 3 04FDEA00438 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002272004030300227NM 2004 3 3 QXEA200400161 120040215A243523088008 STARTER GEN DHAV DHC8 DHC8202 2809007NM NR 2 MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM09360PH8900 545 515 SEA - ON FLIGHT 2108 UPON DC POWER APPLICATION, SMOKE CAME OUT OF NR 2 STARTER GENERATOR. REMOVED AND REPLACED STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040303002322004030300232SO 2004 3 3 SWIA200412862 120040120A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07190SW 120050 ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN ENTRYWAY. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040303002352004030300235NM 2004 3 3 SWAA040517 120040219A7830315A18975 BELLCRANK BOEING737 7373H4 1384600NM THRUST REVERSER STICKING A SWAAK NONE O OTHER LDLANDING 1 SW29354SW 25219 AFTER LANDING THE NR 1 THRUST LEVER WOULD NOT ADVANCE. REMOVED AND REPLACED THE NR 1 ENGINE INBOARD T/R ACTUATOR BELLCRANK AND THE FOLLOWUP CABLE PER MM. 2L72 4F RTA16WE 20040303002362004030300236NM 2004 3 3 04FDEA00441 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040304000032004030400003 2004 3 4 BAQA093101 420040218A221041800500001 ACTUATOR AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE TRIM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 5794 6036 TRIM ACTUATOR UNIT PITCH AUTO TRIM DECOUPLES. SELF TEST FAULT CODE 1. REPLACED WITH SERVICABLE UNIT. 02/23/2004 1G72 3U3 U H10EU E19EU 20040304000042004030400004 2004 3 4 BAQA093180 420040222A34516226263001 TRANSCEIVER LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP DME SYSTEM INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 70 092 DME TRANSCEIVER UNIT IS WEAK AND INTERMITTENT. UNIT ONLY LASTED 69.5 HOURS. REPLACED WITH SERVICEABLE UNIT. 02/24/2004 2L72 4F4 F A10CE E6WE 20040304000052004030400005EU 2004 3 4 BAQA093231 120040117A71700174078030 DRAIN VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE NR 1 ENGINE MALFUNCTIONED B BAQAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA03365S 298 6036 NR 1 ENGINE SMOKES ON SHUT DOWN. REPLACED WITH SERVICABLE UNIT. 02/24/2004 1G72 3U3 U H10EU E19EU 20040304000072004030400007EU 2004 3 4 BAQA092605 120040211A6320L632M1001966 TRANSMISSION UROCOPEC135 EC135P1 8680990EU MAIN ROTOR MAKING METAL B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME2226 0009 METAL CHIPS ON CHIP DETECTOR ARE PAST SERVICABLE LIMITS. *NOTE* FILTER REMOVED. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/18/2004 1G72 3U O H88EU 20040304000092004030400009EU 2004 3 4 BAQA092787 120040219A2140JBS8803 MIXING VALVE UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE HEATER INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME283 132 UNIT INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 02/23/2004 1G72 3U3 U H88EU E34NE 20040304000182004030400018 2004 3 4 BAQA092756 420040119A22117008138903 COMPUTER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE AUTOPILOT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME3425 7235 API LIGHT STAYS ON AND A/P WILL NOT TEST. REPLACED WITH SERVICABLE ASSET UNIT. 02/20/2004 1G72 3U3 U H13EU E5NE 20040304000222004030400022EA 2004 3 4 04049673 120040218A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27673BR 7599 DURING INSPECTION THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040304000332004030400033CE 2004 3 4 FPI2004F00000 120040128A7921654585 OIL COOLER CESSNA210 T210N 2073456CE CONT O550 IO550* SO ENGINE CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO152145U 21064776 821012R BOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION. 1H71 3O3 O 3A21 E3SO 20040304000392004030400039WP 2004 3 4 02240404WP 120040216A33501001191 LIGHT DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE ZONE 800 INOPERATIVE A A4JAK NONE L NO TEST ININSP/MAINT 1 SO35933JK 48159 L1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT IAW 33-53-0. OPERATIONAL CHECK GOOD. 2L72 4F4 F A6WE E2EA 20040304000732004030400073SO 2004 3 4 C2XA04SH109 120040226A531514522460013 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 DURING C CHECK THE CENTER FLOORBEAM FROM FRAME 18 TO FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040304000742004030400074SO 2004 3 4 C2XA04SH110 120040226A532014590082003 ANGLE EMB 145 EMB145 3260210SO ALLSN AE3007AE3007C GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 DURING C CHECK THE CENTER RAMP ANGLE FROM FRAME 18-20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040304000832004030400083SO 2004 3 4 GLBA20030574 120040227A575312034222009 RIB EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE NACELLE FLAP CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03297UX 120297 CRACK ON RIB LINK ALONG CENTER RIB ON LT NAC FLAP, REMOVED AND REPLACED RLB LINK PN 120-34222-009 ON NACCLLE FLAP. 2L72 4T4 TRTA31SO E20NE 20040304001002004030400100EU 2004 3 4 MALA040212 120040222A3350 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15427XJ 340B427 DURING TASK CARD OF OPS CHECKING OF EMERGENCY LIGHTING SWITCH JOB CARD NR 335003 THE EMERGENCY BATTERY PACKS FAILED DURING TEST (REPLACED PACK ) 21 LN LOCATION OF BATTERY PACK. REMOVED AND REPLACED SN AS REQUIRED. PERFORMED CHECKS IAW MFG MM. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040304001212004030400121WP 2004 3 4 GTIA040102 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND RIGHT CABIN FLOORBOARD STATION 200-256 MISSING FASTENERS NEEDS EDGE FILLER PEELING FIBERGLASS. FABRICATED NEW RIGHT CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040304001322004030400132WP 2004 3 4 GTIA040114 120040111A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND MAIN CABIN, RIGHT CUSP WEB AT FS 276-296 IS CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20040304001332004030400133WP 2004 3 4 GTIA040115 120040107A5522 SKIN DOUG DC9 DC983 3022083WP LT ELEVATOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND LEFT ELEVATOR INBOARD FORWARD EDGE SKIN CRACKED. FABRICATED LEFT ELEVATOR INBOARD FORWARD SKIN. INSTALLED FABRICATED SKIN. (M) 2L72 4F RTA6WE 20040304001342004030400134WP 2004 3 4 GTIA040116 120040110A2560 ESCAPE ROPE DOUG DC9 DC983 3022083WP COCKPIT DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND CAPTAINS AND F/O'S ESCAPE LINES DETERIORATED. REMOVED AND REPLACED CAPTAINS AND F/O'S ESCAPE LINES. (M) 2L72 4F RTA6WE 20040304001602004030400160WP 2004 3 4 GTIA040123 120040113A5321 DOUBLER DOUG DC9 DC983 3022083WP FLOOR PANEL MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND FLOOR PANEL OUTBOARD STATION 927 DOUBLER MISSING ON PANEL EDGE. FABRICATED NEW DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040304001682004030400168WP 2004 3 4 DHL2004806578 120040131A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LT WING INBOARD OUTER L/E CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80-14, DWG U80-R14. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW ED-EDU80-14, DWG U80-R14. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDU80-14, DWG U80-R14, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001692004030400169WP 2004 3 4 DHL2004806571 120040131A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 NOSE SECTION EXTERIOR SKIN WORN (STA 8.000 - 25.000, L-15L TO L-17L) HOLD OPEN HOOK COMPT (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 561-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80-17, DWG U80-R17. PERFORMED NDT INSPECTION IAW DCO NDT SPM PART 6-10-01-001. FABRICATED FILLER (7075-T6AL 0.050), 2 EA FINGER DOUBLER (7075-T6AL 0.032) AND DOUBLER (7075-T6AL 0.071) IAW ED-EDU80-17, DWG U80-R17. CLEANED, TREATED AND PRIMED AREA, FILLER, FINGER DOUBLERS AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, FINGER DOUBLERS AND DOUBLER IAW ED-EDU80-17, DWG U80-R17, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001722004030400172WP 2004 3 4 DHL2004806585 120040127A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAPS DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT OUTBOARD FLAP WITH INTERIM REPAIR ON UPPER FWD PLATING, STA XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-2, DWG U80-R02. REMOVED RIGHT OUTBOARD FLAP PLATING SEGMENT WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG 1. FABRICATED SPLICE (2024-T3 0.063) AND NEW SKIN SEGMENT (2024-T3 0.040) IAW ED EDU80-02, DWG U80-R02. PERFORMED CONTERSINK IN NEW SKIN SEGMENT IAW SRM 51-1-22 PG 1. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF SKIN SEGMENT AND SPLICE IAW SRM 51-1-8B. INSTALLED SPLICE, NEW SKIN SEGMENT AND NEW FASTENERS IAW DWG U80-R02, ED EDU80-2, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040304001812004030400181WP 2004 3 4 DHL2004806587 120040205A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 MAIN CARGO COMPT FLOORBEAM CRACKED 0.250 AT STA 180.000 LBL 32. PERFORMED MAJOR REPAIR. REMOVED FASTENERS. TRIMMED OUT DAMAGED AREA ON FLOORBEAM. INSPECTED FOR CRACKS. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA. FABRICATED ANGLE DOUBLERS 2EA (7075-T6AL 0.160), -T- FILLER (7075-T6AL 0.125), FILLER (7075-T6AL 0.071), SPLICE DOUBLERS 2EA (7075-T6AL 0.071), SPACER (7075-T6AL 0.142), CLIP (7075-T6AL 0.090), SPACER (7075-T6AL 0.071) IAW ED EDU80-6, DWG U80-R06. CLEANED, TREATED AND PRIMED REPAIR PARTS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED REPAIR PARTS ON FLOORBEAM AT STA 180.000 LBL 32 WITH NEW FASTENERS IAW ED EDU80-6, DWG U80-R06, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001822004030400182WP 2004 3 4 DHL2004806570 120040129A5720 INTERCOSTAL DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT WING T/E INTERCOSTAL LWR SURFACE 1.500 CRACK (STA XW0 - 5.000). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1, SRM 51-1-20D. FABRICATED INTERCOSTAL (7075-T6AL 0.090) IAW SRM 57-1-0. HEAT TREATED IAW SRM 51-1-1. CLEANED, TREATED AND PRIMED AREA AND INTERCOSTAL IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21 PG 1, SRM 51-1-20D. 2L74 4F RT4A25 20040304001872004030400187WP 2004 3 4 DHL2004806555 120040115A53405711283U501 ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 AFT CARGO COMPT ANCHOR PLATE SUPPORT FITTING CORRODED, STA 1440.000-1460.000, RBL 10. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANCHOR PLATE SUPPORT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040304001892004030400189WP 2004 3 4 DHL2004806557 120040120A57203755028504N CLIP DOUG DC8 DC873F 302199FWP NR 3 MAIN TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 NR 3 MAIN TANK CLIP CRACK 1.000 BETWEEN REAR SPAR AND S-51, XRS 22.750. REMOVED CRACKED CLIP (NR 3 MAIN TANK XRS 22.750). CLEANED, TREATED AND APPLIED COATING MATERIAL TO CLIP AND AREA IAW SRM 51-1-12 PG 7-21. INSTALLED NEW CLIP IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040304001902004030400190WP 2004 3 4 DHL2004806556 120040120A57545754705501N ATTACH FITTING DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING STUB WING INTERNAL PART FITTING CRACKED 4.000 AT STA XW 454.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001942004030400194NM 2004 3 4 SWAA040400 120040207A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 727 + 3, STRINGER 18R AND AT BS 766, STRINGER 22R. REPAIRED SKIN CRACKS PER SRM. 2L72 4F RTA16WE 20040304002002004030400200NM 2004 3 4 SWAA040284 120040129A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040304002032004030400203 2004 3 4 SWAA040287 420040129A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040305000142004030500014EA 2004 3 5 SWIA200412868 120040205A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07427SW7878 7878 7497 FLIGHT SPOILER CAUTION MESSAGE. REMOVED AND REPLACED NR 1 SECU WITH A SERVICEABLE UNIT. OPS CHECKS GOOD. WORK PERFORMED IAW AMM 27-61-05. 2L72 4F RTA21EA 20040305000162004030500016 2004 3 5 SWIA200412870 420040204A34256225798013 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07289YV7672 7672 120289 DURING FLIGHT, AUTO PILOT FAIL WHEN SELECTED TO F/O SIDE, YAW DISENGAGED. A - E ON AUTOPILOT PANEL AND FD FLAG ON EADI. CAPTAIN'S SIDE OPERATES NORMAL. REPLACED FCP65 ON F/O'S SIDE. GROUND CHECK OF AP SYSTEM GOOD. 2L72 4T RTA31SO 20040305000262004030500026EU 2004 3 5 AWXA200400183 120040217A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONE 221 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW2687321892 098 PHX - EEL - DURING 4-DAY CHECK EMERGENCY LIGHT TEST FAILED FOR MESSAGE 33-51-38 LOAD LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL) ABOVE L-1 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040305000362004030500036NM 2004 3 5 04FDEA00422 120040218A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 FLOOR SUPPORT PLATE ASSEMBLY LOCATED BELOW LAVATORY AT STA 427, RT X = 21 CORRODED WITH A THROUGH HOLE. FLOOR SUPPORT AT STA 427, RT X = 21 REMOVED AND REPLACED IAW SRM 51-33-01 VOL II 2L73 4F RTA22WE 20040305000392004030500039NM 2004 3 5 04FDEA00419 120040218A5754 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING CRACK ON NR 16 SLAT TRACK INBOARD SUPPORT RIB. REMOVED CRACKED SUPPORT RIB AS PER SRM 51-31-01, VOL.II AND FABICATED NEW SUPPORT RIB AS PER DRAWING ARB2850 AND ARB2873. INSTALLED FABRICATED RIB AT LT WING ON NR 16 SLAT TRACK INBOARD AS PER SRM 51-33-01, VOL.II AND DRAWING ARB2873. COMPLIED WITH EA 1-5750-74325, WINGS - LT SLAT - FABRICATION OF RIB FOR NR 16 SLAT TRACK. 2L73 4F RTA22WE 20040305000402004030500040NM 2004 3 5 04FDEA00418 120040218A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN FLOOR TRACK CRACKED AT STA 755, LT X = 27.5. FLOOR TRACK CRACKED AT STA 755, LT X = 27.5 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1. 2L73 4F RTA22WE 20040305000412004030500041WP 2004 3 5 04FDEA00416 120040217A5320NCA6042163 STIFFENER DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 ZONE 20, FS 475 FWD SIDE OF DOOR 115 AZ CLIPS AND ANGLES CORRODED FROM LBL 15 TO RBL 5. REMOVED AND REPLACED 2 STIFFENERS AND CLIPS IAW SRM 51-31-01 AT MAE ON N/R N00628. 2L73 4F A22WE 20040305000422004030500042WP 2004 3 5 04FDEA00415 120040217A5210ABA7163U4 FITTING DOUG DC10 DC1010 3022110WP L-1 DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 LOWER FWD AND AFT STOPS LUGS HAVE GOUGES ON L-1 DOOR. REMOVED DAMAGED LUGS AND INSTALLED SERVICABLE LUGS/STOPS IAW SRM 51-31-01 AND 51-33-01 AT MAE ON N/R N00825. 2L73 4F A22WE 20040305000592004030500059NM 2004 3 5 04FDEA00453 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000672004030500067NM 2004 3 5 04FDEA00458 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000692004030500069NM 2004 3 5 04FDEA00460 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000722004030500072NM 2004 3 5 04FDEA00463 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000772004030500077WP 2004 3 5 04FDEA00468 120040220A2840 WARNING SYSTEM DOUG DC10 DC1010 3022110WP FUEL QTY ACTIVATED A FDEAO OTHER J WARNING INDICATION DEDESCENT 1 SO25386FE 46620 AT 6000 FT ON DOWN WIND LEG WITH SLATS EXTENED AND 180 KTS,THE LEVEL 2 FUEL USED ALERT CAME ON. FUEL USED AND FUEL REMAINING EQUALLED DEPARTURE FUEL. APPROXIMATELY 5 MIN LATER, GOT A TANK NR 3 FUEL QTY LO ALERT. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. ALL ALERTS WENT AWAY AT 2500 FT ON FINAL. AT SHUTDOWN FUEL USED =17.7, 17.8, 18.0 FUEL TANKS 6.4, 6.7, 6.4 DEPARTURE FUEL WAS 73.0. PERFORM FUEL SYSTEM TEST ON ENTIRE FUEL SYSTEM WITH AIRCRAFT SYSTEM COMPUTER TWICE, ALL SYSTEM PASSED. PER MAINT PRACTICES. NO PREVIOUS HISTORY. 2L73 4F A22WE 20040305000842004030500084EA 2004 3 5 SWIA200412885 120040208A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07917SW 7641 ON APPROACH INTO DEN FLAPS FAIL CAUTION MESSAGE WHEN FLAPS ARE SELECTED FROM 0 TO 8 DEGREES. COMPLIED WITH QRH. REMOVED AND REPLACED POWER DRIVE UNIT. OPS CHECK GOOD. ALL WORK DONE IAW CRJ MM 27-52-01. 2L72 4F RTA21EA 20040305000862004030500086SO 2004 3 5 SWIA200412887 120040209A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07189SW2883 2883 120048 RECEIVED A CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25. RESET IAW QRH. REPLACED FLAP SELECTOR SWITCH WITH SERVICEABLE UNIT. OPERATED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD. 2L72 4T RTA31SO 20040305000882004030500088 2004 3 5 SWIA200412889 420040210A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO NR 1 AUTOPILOT MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 NM07271YV7723 7723 120271 CAPTAIN'S AUTOPILOT WILL CLIMB AND DESCEND 100 FT WHEN IN LEVEL FLIGHT. SWITCHED TO F/O'S AUTOPILOT. NO DISCREPANCIES. COULD NOT DUPLICATE. REPLACED NR 1 APC FOR TROUBLESHOOTING SYSTEM. OPS CHECKS GOOD IAW 22-10-00. 2L72 4T RTA31SO 20040308000012004030800001EU 2004 3 8 MALA040194 120040204A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15511XJ E2325 DURING C-CHECK INSPECTION IN LCQ, AFT CARGO COMPARTMENT FRAME 34 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED FRAME 34 IAW BAE 146 RJ-85 SRM 51-24-11. 2H74 4F RTA49EU 20040308000032004030800003SO 2004 3 8 C2XA04SH071 120040218A3350ML1317 LIGHT EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2748901 145501 SHV- DURING A ROUTINE CHECK THE COCKPIT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE DURING THE EMERGENCY LIGHT FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE BULB IAW EMB 145 AMM 33-50-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040308000072004030800007 2004 3 8 SWIA200412880 420040205A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT SYS FAULTY A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07563SW6145 6145 120338 AIRCRAFT OSCILLATES UP AND DOWN WITH NR 2 AUTOPILOT ENGAGED. COMMAND BARS MOVE AROUND. REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040308000082004030800008 2004 3 8 SWIA200412881 420040203A2210 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTOPILOT SYS DIRTY A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07290SW 120317 FIRST OFFICER'S AUTOPILOT FAILED WITH ASSOCIATED AUTOPILOT FAIL ON MAP AND T, A, R, E ON AUTOPILOT PANEL. INSPECTED AND CLEANED F/O'S AP COMPUTER RACK AND CONNECTORS, AP CONTROL PANELS AND AHRS COMPUTER CONNECTORS. TROUBLESHOT THE F/O'S AP SYSTEM. NO FAULTS FOUND. OPS CHECKED GOOD IAW MM 22-11-00. 2L72 4T4 TRTA31SO E20NE 20040308000092004030800009 2004 3 8 SWIA200412891 420040211A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO NR 2 FAULTY A SWIAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM07234SW7779 7779 120308 FIRST OFFICERS' AUTOPILOT FAILED AND THE ELEVATOR SERVO LIGHT ILLUMINATED. CHECKED ASSOCIATED WIRING ON CONNECTORS BEHIND APC NR 2, NO DEFECTS. REMOVED AND REPLACED APC NR 2. OPS CHECK GOOD ON GROUND OPERATIONS IAW MM 22-10-00. 2L72 4T RTA31SO 20040308000102004030800010 2004 3 8 SWIA200412892 420040214A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA STICK SHAKER PULLED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07908SW 7540 BOTH WIRES PULLED FROM CAPTAIN'S STICK SHAKER. REPAIRED BOTH WIRES ON CAPT'S STICK SHAKER AS NEEDED. PERFORMED OPS CHECK. ALL OPS CHECKS GOOD. 2L72 4F RTA21EA 20040308000122004030800012EA 2004 3 8 SWIA200412894 120040210A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILERON MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 NM07423SW8137 8137 7456 SPOILERONS FAULT MESSAGE. FLIGHT CONTROL PAGE SHOWS FAULT WITH RIGHT SPOILERON. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW AMM 27-62-01. SPOILERON SYSTEMS OPS CHECKS GOOD. LEAK CHECK GOOD. 2L72 4F RTA21EA 20040308000132004030800013EA 2004 3 8 SWIA200412895 120040211A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA CABIN FAILED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07934SW 7722 ROW 8 CEILING EXIT SIGN DOES NOT ILLUMINATE ON FORWARD SIDE. REPLACED AND SECURED BATTERY CHARGER ASSY AT SECTION 2 OF EMERGENCY BATTERY PACKS. OPS CHECK GOOD. 2L72 4F RTA21EA 20040308000142004030800014EA 2004 3 8 SWIA200412896 120040212A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07934SW2711 2711 7722 FORWARD OVERWING EMERGENCY EXIT SIGN INOP. INSTALLED SERVICEABLE BATTERY AND POWER SUPPLY. OPS CHECK GOOD. 2L72 4F RTA21EA 20040308000182004030800018SO 2004 3 8 C2XA04SH079 120040220A532014522460013 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000252004030800025SO 2004 3 8 C2XA04SH086 120040220A531514521700007 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 1SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000262004030800026SO 2004 3 8 C2XA04SH087 120040220A711014576057622 STRUCTURE EMB 135 EMB135ER 3260203SO NR 2 COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE AFT EDGE MEMBER ON THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000272004030800027SO 2004 3 8 C2XA04SH088 120040220A711014576057621 STRUCTURE EMB 135 EMB135ER 3260203SO NR 1 COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000282004030800028SO 2004 3 8 C2XA04SH089 120040221A711014576631621 STRUCTURE EMB 145 EMB145 3260210SO LT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000302004030800030SO 2004 3 8 C2XA04SH091 120040221A532014525422001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE LEFT FORWARD SILL IN THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000322004030800032SO 2004 3 8 C2XA04SH093 120040221A531314533823009 STRINGER EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV-DURING C-CHECK EXTERIOR STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000332004030800033EU 2004 3 8 MALA040202 120040202A5320 PANEL BAC 146 AVRO146RJ85A1500097EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15511XJ E2325 DURING C-CHECK INSPECTION, FUSELAGE PANEL 275CR IS CHAFED, BLENDED CHAFE WENT OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED FUSELAGE PANEL 275CR IAW MESABA EO A53154. A/C RELEASE DATE 2/20/04. 2H74 4F RTA49EU 20040308000352004030800035EU 2004 3 8 MALA040196 120040213A21507769106 ACM SAAB SF340 340B 7860101EU A/C BAY MALFUNCTIONED A MALAK NONE BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET NRNOT REPORTED 1 GL15454XJ 340B454 DURING APPROACH TO AIRPORT CREW COULD SMELL A BURNING ODOR IN FLIGHT DECK AND CABIN. PASSENGERS AND FLIGHT ATTENDANT REPORTED A STRONG VIBRATION AND NOISE COMING FROM THE FLOOR AFT ROW 6. PERFORMED QRH PROCEDURES. MAINTENANCE ISOLATED PROBLEM TO THE RIGHT AC PACK, INSPECT ACFT AND FOUND SAFE FOR ONE TIME FERRY FLT FROM LFT TO MEM FOR REPAIR WITH THE RIGHT AC PACK OFF. REMOVED AND REPLACED RIGHT ACM P/N 776910-6, S/N OFF 870613, S/N ON 900984, IAW JOB CARD 215181. OPS CHECK IS GOOD. 2L72 4T RTA52EU 20040308000382004030800038EU 2004 3 8 MALA040190 120040209A3260 CONNECTOR SAAB SF340 340B 7860101EU RT MLG WW LOOSE A MALAO OTHER N FALSE WARNING DEDESCENT 1 GL15442XJ 340B442 ON APPROACH TO LANDING RIGHT GEAR DOWN INDICATION DID NOT ILLUMINATE ON GEAR DOWN SELECTION. RIGHT GEAR DOWN LIGHT DID NOT ILLUMINATE. RAN QRH. NOTED LAMPS TEST OK, AND INTRANSIT LIGHT EXTINGUISHED (OPERATES NORMALLY). MAINTENANCE REPLACED BURNED-OUT BULBS IN INDICATOR AND RESECURED GEAR POSITION SWITCH CONNECTOR IN RT GEAR WELL. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040308000412004030800041EU 2004 3 8 MALA040201 120040202A5230 DOOR FRAME BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15511XJ E2325 DURING C-CHECK INSPECTION IN LCQ, AFT CARGO DOOR FRAME CRACKED IN TWO PLACES. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS, AND FILLERS BAE RJ-85 SRM 52-32-11. A/C RELEASE DATE 2/20/04. 2H74 4F RTA49EU 20040308000462004030800046SO 2004 3 8 C2XA04IA014 120040217A3350M8372375R1624N CONNECTOR EMB 145 EMB145ER 3260211SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712946 145052 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT AT SEAT 3B/C WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND FOUND THE ELECTRICAL CONNECTOR TO BE LOOSE. THE CONNECTOR WAS RESECURED AND THE LIGHT OPERATIONALLY TESTED. 2L72 4F RTT00011AT 20040302000192004030200019NM 2004 3 2 SWAA040433 120040210A53106546543 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT BELT FRAME SHEAR TIES CORRODED AT BS 727E, BETWEEN STRINGER 26R AND STRINGER 27R. REMOVED AND REPLACED SHEAR TIES PER EA. 2L72 4F RTA16WE 20040302000222004030200022NM 2004 3 2 SWAA040412 120040208A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2L72 4F RTA16WE 20040302000232004030200023NM 2004 3 2 SWAA040413 120040209A5320BAC1514 STIFFENER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND CHANNEL STIFFENERS CORRODED AT BS 1016, BL 0, WL 198. REPAIRED PER ACO AND AD. 2L72 4F RTA16WE 20040302000412004030200041NM 2004 3 2 SWAA040370 120040205A335007912 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 EEPLS STRIP COVER LOOSE AT ROW 1. SECURED EEPLS STRIP COVER PER MM. 2L72 4F RTA16WE 20040302000422004030200042 2004 3 2 SWAA040371 420040205A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29780SW 27885 L2 DOOR EVAC SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040302000522004030200052WP 2004 3 2 AALA20040264 120040222A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 12 AND 16 INOPERATIVE. REPLACED BATTERY FOR THE OVERHEAD EMERGENCY LIGHT AT ROWS 12 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000632004030200063NM 2004 3 2 AALA20040244 120040215A3350 BATTERY PACK BOEING757 757231 1384950NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21721TW 29954 DFW - BULLNOSE EMERGENCY LIGHT AT SEATS 14C AND 18C INOPERATIVE. REPLACED BATTERY PACK FOR BULLNOSE EMERGENCY LIGHT AT SEATS 14C AND 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040302000722004030200072WP 2004 3 2 AALA20040255 120040220A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217526A 49918 DEN - EMERGENCY LIGHT AT ROW 4 TO ROW 7 CEILING INOPERATIVE. REPLACED BATTERY AT OVERHEAD BIN ROW 6EF FOR ROWS 4 THROUGH 7 CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000832004030200083NM 2004 3 2 CALA0400147 120040221A53306545767130 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 400 BETWEEN S17L AND S18L. REPAIRED IAW ECRA 5331-01139. 2L72 4F RTA16WE 20040302000852004030200085NM 2004 3 2 CALA0400149 120040221A5280113A82322 DOOR BOEING737 737824 13844BZNM RT MLG CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND A .75 INCH CRACK IN RT MLG DOOR. THE CRACK WAS LOCATED ON THE FORWARD LOWER CORNER. THE RT MLG DOOR WAS REPAIRED IAW ECRA 5280-01316. 2L72 4F RTA16WE 20040302000872004030200087NM 2004 3 2 CALA0400151 120040222A5512 SKIN BOEING737 737524 1384721NM HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2752616 27329 INSPECTION FOUND TWO 1 INCH CRACKS IN RT LOWER HORIZONTAL STABILIZER SKIN AT REAR SPAR STA 100 AND 129. A REPAIR WAS INSTALLED IAW ECRA 5510-01724. 2L72 4F RTA16WE 20040302000902004030200090NM 2004 3 2 CALA0400139 120040219A532065528941 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723657 28918 INSPECTION FOUND FLOOR SUPPORTS CRACKED AT FASTENER HOLES AT STA 540, RBL 2 AND LBL 2. THERE WAS ONE CRACK IN EACH SUPPORT AND BOTH WERE TWO INCHES LONG. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-40-2. 2L72 4F RTA16WE 20040302000912004030200091NM 2004 3 2 CALA0400140 120040219A5720115A2982 BRACKET BOEING737 737724 13844BYNM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A .75 INCH CRACK IN BRACKET AT LT WING TRAILING EDGE JUST AFT OF NR 1 ENGINE PYLON BULB SEAL. A NEW BRACKET WAS INSTALLED IAW BOEING DRAWING 115A2982 AND SRM 51-40-02. 2L72 4F RTA16WE 20040302000932004030200093NM 2004 3 2 CALA0400161 120040224A5730114N2107 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719130 28970 INSPECTION FOUND A 3 INCH CRACK IN RT WING UPPER FIXED L/E SKIN LOCATED I/B OF SLAT NR 7 AT WS 418. REPAIRED IAW ECRA 5721-01119. 2L72 4F RTA2NM 20040302000952004030200095NM 2004 3 2 CALA0400153 120040223A5320149A761115 WEB BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND A 1 INCH CRACK IN O/B WEB ON RT WHEEL WELL RING. THE WEB WAS REMOVED AND REPLACED IAW BOEING DRAWING 149A7611 AND SRM 51-40-02. 2L72 4F RTA16WE 20040302001022004030200102NM 2004 3 2 CALA0400160 120040224A5730114N2107 SKIN BOEING757 757224 1384958NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719130 28970 INSPECTION FOUND TWO 3.5 INCH CRACKS IN LT WING UPPER L/E SKIN PANEL AT WS 539 BETWEEN NR 3 AND NR 4 SLATS. REPAIRED IAW ECRA 5721-01120. 2L72 4F RTA2NM 20040302001052004030200105NM 2004 3 2 CALA0400131 120040217A57536549509 ATTACH ANGLE BOEING737 7373T0 1384582NM T/E FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 1.2 INCH CRACK IN NR 2 FLAP TRACK FAIRING ATTACH ANGLE. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20040302001102004030200110NM 2004 3 2 CALA0400136 120040219A573065C26270 SKIN BOEING737 737524 1384721NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724633 27901 INSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER L/E SKIN AT NR 3 SLAT ACTUATOR. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-41-01. 2L72 4F RTA16WE 20040302001112004030200111EA 2004 3 2 COMA0460157 120040221A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01721CA11302 7259 FLIGHT 5108 FLAPS FAIL MESSAGE DURING TAXI. REPLACED THE PDU. 2L72 4F RTA21EA 20040302001122004030200112EA 2004 3 2 COMA0460155 120040217A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01491CA2942 7756 FLIGHT 5784 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040302001192004030200119EA 2004 3 2 COMA0460152 120040213A5210601R31881273 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01467CA5273 7637 PAX DOOR PRESSURE PANEL CABLE (ICE BREAK) IS BROKEN AT THE END OF THE CLEVIS DUE TO RUBBING ON THE FLAP (P/N 601R318122-3). PAX DOOR PRESSURE TO PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE (P/N 601R3188127_3). THE FLAP DECOMPRESSION PANEL NEEDS TO HAVE A RECESSION CUT INTO THE INTERIOR LIP TO ALLOW THE CABLE MORE ROOM AND TO PREVENT IT FROM BEING BROKEN FROM NORMAL USE. 2L72 4F RTA21EA 20040302001202004030200120EA 2004 3 2 COMA0460153 120040212A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01467CA 7637 CARGO BAY, LEFT AND RIGHT, FLOOR ANGLE SUPPORT CRACKED AT FS 621. REMOVED DAMAGED FLOOR ANGLE ON LEFT HAND AND RIGHT HAND SIDE OF 621 FLOOR ANGLE IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004. REPAIRED 621 FLOOR ANGLE, LEFT HAND AND RIGHT HAND SIDE, IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004. 2L72 4F RTA21EA 20040302001222004030200122NE 2004 3 2 DHL2004782006 220040211A7200JT8D17A ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D17A 52049NE NR 3 MALFUNCTIONED A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01782DH 21998 688763 AT FL310 DURING CRUISE A LOUD HUM ACCOMPANIED BY A VIBRATION OCCURRED ON ENGINE NR 3. PERFORMED ABNORMAL IN-FLIGHT ENGINE SHUTDOWN PROCEDURE PER 727 AOM. REMOVED AND REPLACED NR 3 ENGINE ASSEMBLY IAW ASTAR B-727 MTM 71.1. OPS CHECKED GOOD, OK FOR SERVICE. 2L73 4F4 F A3WE E2EA 20040302001262004030200126EU 2004 3 2 DHL2004367002 120040219A3240 MODULE AIRBUS300 A300B4203 3930306EU BRAKE SYS MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01367DH 265 AFTER GEAR RETRACTION MAX LIGHT REMAINED ILLUMINATED ON AUTO BRAKE PANEL. EXTENDED GEAR, RETRACTED GEAR. UPON RETRACTION HYD LIGHT ON MASTER WARNING PANEL ILLUMINATED & AIR PRESS LIGHT ON GREEN SYS ILLUMINATED THEN EXTINGUISHED. PULLED AUTO BRAKE C/B. DEFERRED AUTO BRAKE SYS DMI 15790 IAW MEL 32-42-07 CAT-C. PLACARD INSTALLED. REMOVED AND REPLACED AUTO BRAKE SELECTOR MODULE IAW M/M 32-42-55. GROUND OPS CHECKED OK. DMI 15790 CLEARED. PLACARD REMOVED. 2L72 4F RTA35EU 20040302001292004030200129NM 2004 3 2 SWAA040265 120040127A335090083 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED PM CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040302001342004030200134 2004 3 2 SWAA040271 420040127A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040302001392004030200139NM 2004 3 2 SWAA040276 120040128A256065C19901 CABLE BOEING737 7373H4 1384600NM R2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040302001542004030200154NM 2004 3 2 SWAA040304 120040130A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040302001722004030200172NM 2004 3 2 SWAA040375 120040207A57556573730 SPOILER BOEING737 7372H4 138448CNM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 THE NR 3 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 3 SPOILER PER MM. 2L72 4F A16WE 20040302001772004030200177NM 2004 3 2 SWAA040380 120040207A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040302001852004030200185NM 2004 3 2 SWAA040388 120040207A57536546430 FLAP BOEING737 7373Q8 1384670NM RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON RT WING INBOARD FORE FLAP INBOARD ATTACH ARM. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20040302001882004030200188NM 2004 3 2 SWAA040391 120040207A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 EMERGENCY EXIT LIGHT ON LT BULLNOSE MISSING LENS AT ROW 6 ABC. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040302001942004030200194NM 2004 3 2 SWAA040397 120040207A57536546430 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20040302001962004030200196NM 2004 3 2 SWAA040399 120040207A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040302001982004030200198SO 2004 3 2 C2XA04CL014 120040224A3350 CONNECTOR EMB 145 EMB145ER 3260211SO ALLSN AE3007AE3007C GL CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 FLIGHT NR 2103 THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED LOOSE CONNECTOR ON THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20040303000052004030300005NM 2004 3 3 AWXA200400175 120040214A21317612608 CONTROLLER BOEING737 7373Y0 1384671NM CABIN PRESSURE FAILED A AWXAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP28331AW274193346 23747 ON CLIMB OUT, AUTO PRESSURIZATION FAILED, CABIN PRESSURE CLIMBED QUICKLY, NO FAILURE LIGHT INDICATED. STABILIZED PRESSURIZATION IN STANDBY THEN RESELECTED AUTO, PRESSURIZATION WAS OK AT FIRST, BUT THEN FAILED AGAIN, STILL NO WARNING LIGHT. OUTFLOW VALVE INDICATED CLOSED, STABILIZED PRESSURIZATION IN STANDBY AT 12000 ALTITUDE AND ABLE TO CONTROL PRESSURIZATION SCHEDULE MANUALLY, TURNED BACK & LANDED WITHOUT EVENT. MAINT FOUND CIRCUIT BREAKER POPPED, R & R CABIN PRESSURE CONTROLLER, RESET CIRCUIT BREAKER, AND PERFORMED CABIN SAFETY PRESSURE AND RELIEF VALVE TEST IAW T/C F1B21001, TEST WAS GOOD. FUNCTIONAL CHECK OF CABIN PRESSURE CONTROLLER S/N FD37127 CONFIRMED FAILURE OF UNIT. 2L72 4F RTA16WE 20040303000062004030300006NM 2004 3 3 AWXA200400176 120040120A551465475966 CLEVIS BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER FORWARD CLEVIS, AT FORWARD LOWER FACE BS 1088, WL 256, RBL 30. MAINTENANCE REMOVED BUSHING FROM RT HORIZONTAL STABILIZER FORWARD CLEVIS; OVERSIZED CENTER SECTION CLEVIS FORWARD LOWER HOLE; FABRICATED A NEW REPLACEMENT BUSHING IAW B737-300 SRM 55-10-10, PG. 112; INSTALLED REPAIR PART IAW AWA E.R. 03-5512-04044-TB1. 2L72 4F4 FRTA16WE E2GL 20040303000322004030300032NM 2004 3 3 P5CA0401037 120040216A2710 CONNECTOR BOEING747 747236B 1384804NM AILERON CONTROL INOPERATIVE A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23924FT 21730 NO AILERON MOVEMENT INDICATION DURING FLIGHT CONTROL CHECK. CLEANED CONNECTOR ON AILERON INDICATOR IAW 27-10-00. OPS CK GOOD. 2L74 4F A20WE 20040303000392004030300039EU 2004 3 3 BAQA092499 120040204A2435 BRUSHES UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE STARTER GEN WORN B BAQAK NONE O OTHER ININSP/MAINT 1 EA03136MH 99161 0161 BRUSHES WORN IN UNIT. HARDCARD ENCLOSED. REPLACED BY SERVICABLE UNIT. 02/17/2004 1G72 3U3 U H88EU E34NE 20040303000412004030300041 2004 3 3 BAQA092509 420040204A34516226263001 TRANSCEIVER LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP INOPERATIVE B BAQAK NONE O OTHER ININSP/MAINT 1 EA0340DK 11545 092 UNIT WILL NOT LOCK-ON X CHANNELS. Y CHANNEL OKAY. REPLACED WITH SERVICEABLE UNIT. 02/06/2004 2L72 4F4 F A10CE E6WE 20040303000442004030300044 2004 3 3 BAQA092519 420040204A3444MI585351 INDICATOR LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP RADAR INOPERATIVE B BAQAK NONE O OTHER ININSP/MAINT 1 EA0340DK 11545 092 MODE BUTTONS ILLEGIBLE. REPLACED WITH SERVICABLE UNIT. 02/06/2004 2L72 4F4 F A10CE E6WE 20040303000512004030300051NE 2004 3 3 BAQA092555 220040119A7412HE402C EXCITER AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE IGNITION SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 1186 6036 WARRANTY. UNIT INOPERATIVE. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENG. S/N 2106 AND THE ENGINE WAS INSTALLED AT ACFTT 4578.5. REPLACED WITH SERVICABLE UNIT. 02/05/2004 1G72 3U3 U H10EU E19EU 20040303000532004030300053EA 2004 3 3 VNAA0402006 120040213A78301267588 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07215PS370 7880 IN FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE THRUST REVERSER UNLOCK INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 78-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040303000542004030300054NE 2004 3 3 BAQA092574 220040128A75320210027060 BLEED VALVE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE ENGINE WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC2094 7517 18050 WARRANTY- COVERED BY SUPPORT BY HOUR. UNIT EXTREMELY WORN. REPLACED WITH SERVICEABLE UNIT. 02/09/2004 1G72 3U3 UNCH13EU E19EU 20040303000582004030300058EU 2004 3 3 BAQA092577 120040202A76970301067400 WIRE HARNESS BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE ENGINE CONTROL DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC2106 7517 18049 FIRE DAMAGE, N2 WIRE OUTER INSULATION. REPLACED WITH SERVICEABLE UNIT 02/09/2004 1G72 3U3 UNCH13EU E19EU 20040303000592004030300059 2004 3 3 BAQA092578 420040204A34205050031904 GYRO BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101* NE STANDBY INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KC6216 7168 GYRO FLAG WILL NOT PULL, CARD ALSO STUCK. REPLACED WITH SERVICEABLE UNIT. 02/09/2004 1G72 3U3 UNCH13EU E5NE 20040303000742004030300074WP 2004 3 3 0471 120040214A5313 LONGERON DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT CORROSION ON LONGERON 30L AT FS 270 AND IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20040303001082004030300108WP 2004 3 3 ABXA040069 120040205A7110595915539 NOSE COWL DOUG DC9 DC941 302207NWP RT ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 NOSE COWL CRACKED 3 PLACES 6:00 POSITION AT NOSE COWL ANTI-ICE DUCT. INSTALLED ANTI-ICE DUCT IAW DC-9 MM 71-10-01-2-0001, REPLACED DOUBLER IAW DOUGLAS DWG 5959155. 2L72 4F A6WE 20040303001152004030300115 2004 3 3 SWAA040551 420040222A34142083111 INDICATOR BOEING737 7373G7 1384595NM COCKPIT FAULTY A SWAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW29683SW 24008 AIRTURN BACK, DUE TO AIRSPEED INDICATORS DID NOT AGREE. REMOVED AND REPLACED F/O AIRSPEED INDICATOR PER MM. 2L72 4F RTA16WE 20040303001192004030300119NM 2004 3 3 SWAA040555 120040222A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED AT THE AFT CARGO COMPARTMENT BS 745, LBL 8, WL 148. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20040303001252004030300125NM 2004 3 3 2004UALA00126 120040214A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 SKIN DENT STATION 1718 AND STRINGER 14L LAP JOINT. MAJOR REPAIR. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040303001272004030300127NM 2004 3 3 2004UALA00129 120040215A5320 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29376UA 24641 STA 344 END FITTING IS CRACKED AT STR 14L. MAJOR REPAIR ACCOMPLISHED. REPLACED END FITTING. 2L72 4F4 FRTA16WE E2GL 20040303001472004030300147NM 2004 3 3 2004UALA00138 120040213A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 CABIN FLOOR INTERCOSTAL CRACKED BS 344-360 LBL 11. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2GL 20040303001532004030300153NM 2004 3 3 2004UALA00145 120040217A3350 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE POWER SUPPLY BLOWN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 RIGHT OVERWING AFT 2 EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN POWER SUPPLY. CHECKS OK. 2L74 4F4 FRTA20WE E24NE 20040303001552004030300155NM 2004 3 3 2004UALA00147 120040218A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 EXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS AT BS 600-640, AND STR 14L TO 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN SPLICE DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040303001572004030300157WP 2004 3 3 ABXA040070 120040206A534039145901N FITTING DOUG DC9 DC941 302207NWP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 LONGERON 23 RT END CAP EXFOLIATED AT FS 1065. REPLACED LONGERON 23 RT END CAP USING P/N 3914590-1N IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040303001742004030300174NM 2004 3 3 F3LA200400014 120040219A5320 SILL BOEING737 7373S1 138447SNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED L1 DOOR MOP SILL CORRODED THE WIDTH OF THE DOORWAY AND EXTENDING AFT TO THE END OF THE CORD. REPLACED MOP SILL IAW SRM 53-10-15. 2L72 4F4 FRTA16WE E2GL 20040303001862004030300186NM 2004 3 3 04FDEA00457 120040219A2740 GEARBOX DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE STAB TRIM MAKING METAL A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25590FE 48505 AFTER T/O, PASSING 5000FT, CAPT NOTICED NOSE DOWN TRIM STUCK AT 2.2 ANU USING BOTH. CAPT AND F/O YOKE CONTROLS AND SUITCASE HANDLES TO TRIM NOSE DOWN. ALL UNSUCCESSFUL. ONCE A/C STARTED TO ACCELERATE, PASSING 10K , 310 KTS A/P WOULD DISENGAGE. AT FIRST TRIM WOULD TRIM NOSE UP TO 3.2. ATB TO MEM DURING APPROACH. TRIM STUCK AT 2.7 ANU, APPROX 30 LBS STICK PRESSURE REQ DURING INITIAL AND FINAL APPROACH AND LANDING. T/S STAB TRIM AND FOUND STAB GEAR BOX LOW ON OIL (NO OIL WAS ON DIPSTICK). REMOVED DRAIN PLUG DARK COLORED OIL AND SMALL METAL PIECES CAME OUT. STAB DID NOT MOVE WITH EITHER TRIM. REPLACED STAB TRIM GEARBOX, LT AND RT DRIVE MOTORS, LT AND RT BRAKE UNITS. ALL IAW MM 27-43-30-4, 04-4, 44-01-4. 2L73 4F4 FRTA22WE E13NE 20040303002062004030300206EA 2004 3 3 VNAA0402007 120040214A322016050115 STRUT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07218PS142 7885 IN FLIGHT,GEAR WOULD NOT RETRACT. DURING PUSHBACK FROM GATE, NOSE GEAR WAS TURNED PAST ITS LIMIT. NOSE WHEEL STEERING WAS THEN REPORTED INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED ELECTRO HYDRAULIC STEERING VALVE IAW MFG MM. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. AFTER TAKE OFF THE NOSE GEAR WOULD NOT RETRACT AND FLIGHT RETURNED. THE AIRCRAFT WAS THEN FERRIED WITH THE GEAR PINNED. MAINTENANCE INSPECTED AND REPLACE THE NOSE GEAR SHOCK STRUT ASSEMBLY IAW MFG MM. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040303002192004030300219NM 2004 3 3 QXEA200400167 120040220A2820 O-RING DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM LEAKING A QXEAK NONE K FLUID LOSS UKUNKNOWN 1 NM09375PH10493 529 PDX - A FUEL LEAK WAS NOTED ON THE NR 2 NACELLE AND APPEARS TO BE NEAR THE FUEL DOOR. MAINTENANCE REPLACED THE O-RINGS AT THE MASTER REFUEL/DEFUEL SHUTOFF VALVE AND ABOVE THE FILLER PORT. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040303002252004030300225NM 2004 3 3 04FDEA00440 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040304000012004030400001EU 2004 3 4 BAQA092554 120040119A71700174126090 VALVE AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE DRAIN STICKS B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365S 899 6036 WARRANTY. VALVE STICKS IN COLD WEATHER. UNIT WAS REMOVED AS ORIGINAL EQUIPMENT FROM ENGINE S/N 2060, AND THE ENGINE WAS INSTALLED AT ACFTT 4865.2 REPLACED WITH SERVICABLE UNIT. 02/05/2004 1G72 3U3 U H10EU E19EU 20040304000322004030400032NE 2004 3 4 E812004F00002 220040122A7261 BOSS CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE OIL FILTER CRACKED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL0322HP 674 S5500103 PCE102209 REMOVED OIL FILTER FROM NR 2 ENGINE DURING SCHEDULED PHASE (B) INSPECTION. FOUND RAISED BOSS ON BASE FOR O-RING SEAL CRACKED APPROXIMATELY .3333 OF THE WAY AROUND. NOTED (C) (17562), AND (10) MARKING EMBOSSED ON FILTER BASE ADJACENT TO PART NUMBER. 1L72 4F4 FRTA22CE E1NE 20040304000542004030400054CE 2004 3 4 DBC2004F00000 120040216A2750FL40 FUSE CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP FLAP CONTROL FAILED B DBCAO OTHER J WARNING INDICATION APAPPROACH 1 GL13202JK2119 6500100 ON APPROACH, FLAPS WOULD NOT EXTEND, LANDED UNEVENTFULLY. TROUBLESHOT AND FOUND FUSE F23 IN FLAP CONTROL SYSTEM BLOWN. APPARENT CAUSE WAS MOISTURE CONTAMINATION OF FLAP CONTROLLER CONNECTOR. REPLACED FUSE F23, OPERATIONS CHECKED GOOD. 2L72 4F4 F A9NM E6WE 20040304000652004030400065NE 2004 3 4 GLBA20030571 320040224A6110C7921 BEARING RACE BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3I NE PROP BEARINGS CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03 HJ447 ALL 4 MAIN BEARING (PROP) AND RACES WERE CRACKED AND DISINTEGRATED, REPLACED WITH IMPROVED BEARINGS IAW SERVICE BULLETIN 2L72 4T RTA24CE 5 CP10NE 20040304000752004030400075SO 2004 3 4 C2XA04SH111 120040226A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO ALLSN AE3007AE3007C GL FUSLEAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 DURING C CHECK THE GALLEY CENTER FLOORBEAM FROM FRAME 16-24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040304001362004030400136WP 2004 3 4 GTIA040125 120040111A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND MAIN CABIN FS 237-256 CORRODED ON CUSP AND WEB L18L. REMOVED CORROSION. FABRICATED NEW DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20040304001642004030400164WP 2004 3 4 GTIA040128 120040211A2560 HOLDER DOUG DC9 DC981 3022081WP FLASHLIGHT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 DTW - FOUND FORWARD LEFT EMERGENCY FLASHLIGHT HOLDER IS BROKEN. REMOVED AND REPLACED FORWARD LEFT EMERGENCY FLASHLIGHT HOLDER. (M) 2L72 4F A6WE 20040304001712004030400171WP 2004 3 4 DHL2004806580 120040131A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 VERTICAL STAB L/E HAS HOLES CORRODED STA ZFS 179.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG 3. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED EDU80-16, DWG U80-R16. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6AL 0.050) AND DOUBLER(7075-T6AL 0.063) IAW ED EDU80-16, DWG U80-R16. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER. 2L74 4F RT4A25 20040304001752004030400175WP 2004 3 4 DHL2004806583 120040131A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING CTR L/E CORRODED AT STA XW 257.000 (EXTERNAL SKIN). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED EDU80-15, DWG U80-R15. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (7075-T6AL 0.063) AND DOUBLER (7075-T6AL 0.071) IAW ED EDU80-15, DWG U80-R15. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDU80-15, DWG U80-R15, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001772004030400177WP 2004 3 4 DHL2004806579 120040126A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 RIGHT WING UPPER SKIN CORRODED AT STA XRS 202.000 S-12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-12, DWG U80-R12. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED AREAS IAW ED EDU8-12, DWG U80-R12. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (7075-T6AL 0.160) IAW ED EDU80-12, DWG U80-R12. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED REPAIR DOUBLER IAW ED EDU80-12, DWG U80-R12, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040304001972004030400197NM 2004 3 4 SWAA040403 120040207A3350100031 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED RON, FOUND LEFT EXIT SIDE WALL PANEL LIGHT INOP AT EMERGENCY EXIT DOOR. RELAMPED PER MM. 2L72 4F RTA16WE 20040304001982004030400198NM 2004 3 4 SWAA040404 120040207A2916V83533 CHECK VALVE BOEING737 7377H4 1384404NM HYD RESERVOIR FAULTY A SWAAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29723SW 27855 AIR TURNBACK, STRONG ODOR OF OIL OR HOT PLASTIC, MOST NOTICEABLE AT HIGH POWER SETTINGS. SWITCHED TO APU INFLIGHT, SLIGHT IMPROVEMENT. ALSO, SLIGHT IMPROVEMENT AT IDLE. NO VISIBLE SMOKE. REMOVED AND REPLACED A-SYSTEM HYDRAULIC RESERVOIR HEAD PRESSURE CHECK VALVE PER MM. 2L72 4F RTA16WE 20040305000042004030500004EU 2004 3 5 AWXA200400174 120040213A7711 WARNING SYSTEM AIRBUS320 A320231 3930325EU COCKPIT FALSE ACTIVATIONA AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28631AW 077 SEA - ABORTED TAKEOFF - FLT 0250 - DURING TAKEOFF AT SEA EN ROUTE FOR PHX AT APPROXIMATELY 80 KTS, SYNTHETIC VOICE CALLED FOR RETARD THROTTLES, EPR LOW AT 1.29, SHOULD BE 1.35 AT FLEX TEMP 40 DEGREES, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE RAN BOTH ENGINES TO FLEX AND TOGA POWER, NO FAULTS FOUND, EPR WITHIN LIMITS. 2L72 4F RTA28NM 20040305000152004030500015 2004 3 5 SWIA200412869 420040204A344580510001004 PROCESSOR EMB 120 EMB120ER 3260203SO NR 2 TCAS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07566SW2978 2978 120341 IN FLIGHT THE AP FAILED ON THE F/O'S SIDE, FOLLOWED BY A FLIGHT DIRECTOR FLAG ON THE F/O SIDE. THE 1 AMP CB ON AHRS 2 WAS POPPED. REPLACED AND SECURED TCAS PROCESSOR. OPS CHECKED OPERATION OF AUTOPILOT SYSTEM ON GROUND. ALL CHECKS GOOD AND CB'S REMAINED SET. 2L72 4T RTA31SO 20040305000202004030500020EA 2004 3 5 SWIA200412874 120040205A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07916SW 7634 RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED BULBS. OPS CHECK GOOD. 2L72 4F RTA21EA 20040305000242004030500024WP 2004 3 5 DHL2004809001 120040217A21215007025381 FAN DOUG DC8 DC873F 302199FWP COCKIT NOISY A DHLAO OTHER EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01604AL 46047 ON TAKEOFF AND AT CRUISE ALTITUDE, RECIRCULATION FAN IS LOUD & VIBRATION IS FELT UNDERFLOOR NEAR LAV NOISE DECREASES WITH FAN OFF. DEFERRED RECIRCULATION FAN, PLACARD INSTALLED. AT FL 330, 30 MINUTES INTO FLT, NOTED BURNING ODOR IN FLOOR AREA NEAR LAV MID CABIN TEMP INDICATED 95 DEG ON CABIN TEMP INDICATOR. SMELL WENT AWAY AFTER TURNING RT PACK OFF. CABIN STABILIZED AT 5000 FT. INSPECTED LT & RT PACKS. NO DEFECTS NOTED. OPERATED PACKS IN ALL RANGES & SETTINGS. OPS CHECKED OK. SMELL FROM RECIRCULATION FAN AT LOG ITEM 367524 - 1P. REMOVED AND REPLACED FAN ASSEMBLY, OPS CHECKED OK. DMI CLEARED, STICKER REMOVED. 2L74 4F RT4A25 20040305000472004030500047EU 2004 3 5 AWXA200400195 120040209A5315D53472208006 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 66, Y512 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 64 AND FR 67, Y512 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 9-14, 16 & 17, PG 6, 7-10, & 12. 2L72 4F RTA28NM 20040305000492004030500049EU 2004 3 5 AWXA200400197 120040208A5320D5367180500400 PANEL AIRBUS320 A320232 3930326EU ZONE 260 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL PANEL ASSEMBLY BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED AND REPLACED L-2 DOOR SILL PANEL ASSEMBLY IAW T/C O1D25310 & C1D25310. 2L72 4F RTA28NM 20040305000522004030500052NM 2004 3 5 04FDEA00433 120040219A5754 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000562004030500056NM 2004 3 5 04FDEA00450 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, - LEFT AND RIGHT OUTBAORD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000572004030500057NM 2004 3 5 04FDEA00451 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000582004030500058NM 2004 3 5 04FDEA00452 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000612004030500061NM 2004 3 5 04FDEA00455 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, TITLE :WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000652004030500065SO 2004 3 5 C2XA04SH076 120040220A541114576057621 STRUCTURE EMB 135 EMB135LR 3260305SO ENGINE NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV- DURING C-CHECK THE NUMBER ONE ENGINE UPPER COWLING AFT EDGE STRUCTURE WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE STRUCTURE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040305000682004030500068NM 2004 3 5 04FDEA00459 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040308000052004030800005EA 2004 3 8 SWIA200412878 120040209A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07443SW 7638 FLAPS HALFSPEED STATUS ON TAXI OUT. FOUND 3 OF THE 4 ACTUATORS FAILED TORQUE CHECK. REMOVED AND REPLACED ALL FLAP ACTUATORS LT AND RT SIDE IAW MM 27-53-01 AND 27-53-05. LEFT WING FLAP ACTUATORS - OPS CHECK GOOD. (RIGHT WING) RIGGING AND OPS CHECKS GOOD. LEFT NR 1 FLAP ACTUATOR S/N OFF: 3278, LEFT NR 2 FLAP ACTUATOR P/N: 852D100-19, S/N OFF: 3201, LEFT NR 3 FLAP ACTUATOR P/N: 853D100-19, S/N OFF: 1908, LEFT NR 4 FLAP ACTUATOR P/N: 854D100-19, S/N OFF: 1671 RIGHT NR 4 FLAP ACTUATOR P/N: 854D100-20, RIGHT NR 3 P/N: 853D100-20, S/N OFF: 1916, RIGHT NR 1 P/N: 852D100-19, S/N OFF: FRO361, RIGHT NR 2 P/N: 852D100-19, S/N OFF: FRO354. 2L72 4F RTA21EA 20040308000062004030800006 2004 3 8 SWIA200412879 420040204A34256226190204 AHRS EMB 120 EMB120ER 3260203SO E/E BAY MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM07215SW8280 3964 120281 INTERMITTENT COMPUTER FLAG ON CAPT ATTITUDE INDICATOR. AUTOPILOT DISENGAGED WITH FLAG. REPLACED AHRS, OPS CHECK GOOD. WORK DONE IAW MM 34-21-01. 2L72 4T RTA31SO 20040308000112004030800011EA 2004 3 8 SWIA200412893 120040213A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILERON MALFUNCTIONED A SWIAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07438SW1443 1443 7574 SPOILERONS FAULT STATUS MSG ON TAXI. PULLED CB`S PER MAINTENANCE CONTROL, NO EFFECT. RETURNED TO GATE. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW 27-61-01 CRJ MM. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. 2L72 4F RTA21EA 20040308000152004030800015 2004 3 8 SWIA200412897 420040212A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA STICK SHAKER BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07417SW 7400 LEFT STICK SHAKER INOP. REPAIRED BROKEN WIRE AT CANNON PLUG ON LEFT SHAKER. OPS TESTED GOOD. 2L72 4F RTA21EA 20040308000162004030800016SO 2004 3 8 C2XA04SH077 120040220A531314529180017 STRINGER EMB 135 EMB135ER 3260203SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 220 SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-24-02 AND EC 5320-01106. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000192004030800019SO 2004 3 8 C2XA04SH080 120040220A532014521725613 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000202004030800020SO 2004 3 8 C2XA04SH081 120040220A532014524131007 BRACKET EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE PASSENGER DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000292004030800029SO 2004 3 8 C2XA04SH090 120040221A532014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE LAVATORY CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000312004030800031SO 2004 3 8 C2XA04SH092 120040221A572024566289001 CHANNEL EMB 145 EMB145 3260210SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE RIGHT WING UPPER NUT PLATE CHANNEL ON SPAR 1 WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000342004030800034EU 2004 3 8 MALA040198 120040217A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN LCQ, FRAME AT STA 288 LBL 28 CRACKED. MAINTENANCE CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR IAW MESABA 30 NR S53108. A/C RELEASE DATE 2/20/04. 2L72 4T RTA52EU 20040308000362004030800036EU 2004 3 8 MALA040197 120040213A27307255201507 ELEVATOR SAAB SF340 340B 7860101EU LEFT DEFECTIVE A MALAK NONE FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL15408XJ 340B408 AFTER TAKEOFF LOST ELEVATOR EFFECTIVENESS, WENT TO A PITCH UP ATTITUDE. ELEVATOR CAUTION (ASSOC WITH AUTOPILOT) WENT TO AP/OFF AN1. MANUAL TRIM, NO STRONG VIBRATION BUT A BUFFETING HEAVY FEEL, NO ABNORMAL TRIM INPUTS TO FLY TRIM WERE SYNCED. WHEN OPERATING TRIM HEAVY FORCE NEEDED TO PUSH OR PULL ON WHEEL. RHYTMIC BUFFETING, NO VIBRATION. AC NEEDED EXCESSIVE FORCE TO MAINTAIN DESIRED PITCH ATTITUDE/ALTITUDE, AC CONTINUED TO OSCILLATE AT 200 RPM WITH THUMPING FEEL IN THE ELEVATOR SYSTEM. OSCILLATIONS OF 200 RPM NOTICED DURING ANY LEVEL FLIGHT CLR SKIES, LIGHT WINDS, CG NORMAL, AUTO PILOT OFF WITHIN 3 MIN OF LEAVING GROUND. AUTOPILOT ON MAYBE 1-2 MIN MAX. MAINTENANCE REPLACED LT ELEV ASSY, OPS CHECKS. 2L72 4T RTA52EU 20040308000392004030800039EU 2004 3 8 MALA040199 120040217A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN LCQ, LT I/B SEAT TRACK STA 297 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 2/20/04. 2L72 4T RTA52EU 20040308000452004030800045NM 2004 3 8 AWXA200400202 120040217A573065C262045 SKIN BOEING737 7373G7 1384595NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING AN UNSCHEDULED MAINTENANCE VISIT TO VENDOR REPAIR FACILITY, CORROSION WAS FOUND LT WING UPPER SKIN NEAR WING ROOT AT STR 1A, WBL 150. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; BLENDED DAMAGED AREA OF LT WING UPPER SKIN NEAR WING ROOT AND REMOVED STRINGER SEAL PAN AT STR 1A, WBL 150; FABRICATED 2 EACH REPAIR ANGLES, STRINGER SEAL PAN, AND A REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5724-04051-ES1. 2L72 4F RTA16WE 20040308000482004030800048SO 2004 3 8 C2XA04IA016 120040220A521014540853403 MECHANISM EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 DURING POSTFLIGHT INSPECTION THE MAIN PASSENGER DOOR WAS FOUND DIFFICULT TO OPERATE. MAINTENANCE LUBRICATED THE PASSENGER DOOR LOCKING MECHANISM AND OPERATIONALLY TESTED THE DOOR. 2L72 4T RTT00011AT 20040308000542004030800054NM 2004 3 8 04FDEA00472 120040220A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, MECHANICAL DAMAGE ON STRINGER CLIP, STR 25R, BS 1030. LOCATED & DRILLED HOLES ON NEW STRINGER CLIP AND REMOVED DAMAGE STRINGER CLIP AND INSTALLED NEW IAW SRM 51-30-2 AT BS 1030 25R STR. 2L73 4F RTA3WE 20040308000562004030800056NM 2004 3 8 04FDEA00474 120040220A53116515933 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 DENT IN FRAME, STA 600, BETWEEN STR 23L AND STR 24L. REMOVED DAMAGE AREA OF BS 600 FRAME. FABRICATED REPAIR AND INSTALL REPAIR IAW SRM 51-40-3. 2L73 4F RTA3WE 20040308000572004030800057NM 2004 3 8 04FDEA00475 120040220A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 DENT IN SKIN AT BS 1350 BELOW STR 6L. CUT OUT DAMAGED SKIN AT BS 1350 BELOW STR 6L AND INSTALLED REPAIR DOUBLER PER SRM 54-30-3. 2L73 4F RTA3WE 20040308000582004030800058NM 2004 3 8 04FDEA00481 120040220A53116515931 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 DENT IN FRAME, STA 560, BETWEEN STR 23L AND STR 25L. REMOVED DAMAGE AREA OF BS 560 FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3, EA 7-5310-70628. 2L73 4F RTA3WE 20040308000592004030800059NM 2004 3 8 04FDEA00492 120040220A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 FWD CARGO BAY TOP OF FRAME HAS MECHANICAL DAMAGE BS 580 BL 0 - RBL 4. REMOVED DAMAGE AREA OF BS 580 FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3. 2L73 4F RTA3WE 20040308000612004030800061NM 2004 3 8 04FDEA00494 120040220A53106515938 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 FOUND CORROSION ON SHEAR TIE AT BS 700 LBL 5 TO RBL 5. CUT AND REMOVED DAMAGE AREA OF SHEAR TIE BS 700 LBL 5 TO RBL 5. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-4 FIG 11. 2L73 4F RTA3WE 20040308000632004030800063NM 2004 3 8 VNAA0402009 120040220A2120 ODOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT DETECTED A VNAAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 GL07430JS 3044 THE CREW REPORTED RECEIVING A LAV SMOKE INDICATION WITH A FUNNY SMELL IN THE COCKPIT AND RETURNED TO THE GATE. ON THE WAY BACK TO THE GATE, THE LAV SMOKE INDICATION EXTINGUISHED BY ITSELF. MAINTENANCE INSPECTED THE LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECKS OF THE PACKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00 AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040308000642004030800064SO 2004 3 8 C2XA04CL012 120040223A3350 CONNECTOR EMB 135 EMB135ER 3260203SO CABIN LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 CLE FLIGHT 2152 THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND RESECURED THE CONNECTION ON THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTT00011AT 20040308000662004030800066NM 2004 3 8 QXEA200400165 120040222A3260301450201 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM RT MLG FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09414QX4997 4061 GEG - FLIGHT 2323 - CRUISING AT 25,000 FT, THE LEFT AND RIGHT MAIN GEAR DOORS WERE CYCLING. THE LEFT AND RIGHT YELLOW GEARS FLASHED ONE TIME. ONLY THE LEFT RED LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040308000672004030800067NM 2004 3 8 2004UALA00120 120040214A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29784UA 26951 TWO GOUGES IN EXTERIOR FUSELAGE SKIN AT STA 508 STR 47R-48R. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR. 2L72 4F4 FRTT0001SE E46NE 20040308000682004030800068NM 2004 3 8 2004UALA00121 120040214A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29212UA 30218 EXTERIOR EMERGENCY LIGHT INOPERATIVE AT DOOR 4R. REPLACED LAMP. OPS CHECKED OK. 2L72 4F4 FRTT0001SE E46NE 20040308000702004030800070EA 2004 3 8 QXEA200400169 120040219A2820 PIN CNDAIRCL600 CL6002C10 1390015EA CONNECTOR BACKED OUT A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09600QX5440 10005 PDX - FLIGHT 2543 - WHEN SELECTING RIGHT BOOST PUMP ON, NEITHER THE RIGHT OR LEFT BOOST PUMPS TURN ON. WHEN SELECTING LEFT BOOST PUMP ON, SYSTEM OPERATES NORMALLY. MAINTENANCE INSPECTED THE FUEL SYSTEM AND FOUND AN OPEN WIRE FROM THE FUEL CONTROL PANEL TO K56 RELAY X1. RESET PIN-J OF THE CANNON PLUG AND PERFORMED AN OPERATIONAL CHECK. THE CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040308000712004030800071NM 2004 3 8 AWXA200400203 120040223A56105893543109 WINDSHIELD BOEING737 7373G7 1384595NM COCKPIT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW29018 24711 PHX - AIR TURNBACK - FLT 0277 - ON CLIMBOUT OF PHX EN ROUTE FOR IAH THE CAPTAINS WINDSHIELD BEGAN ARCING, WINDSHIELD ALSO HAD EVIDENCE OF DELAMINATION ALONG TOP EDGE OF PANE, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW T/C R1B56001. AS A PRECAUTION ALSO REPLACED LT WINDOW HEAT CONTROL UNIT IAW BMM 30-40-11. VENDORS BENCH TEST OF WINDOW HEAT CONTROL UNIT S/N 2316 CONFIRMED FAILURE OF UNIT FOR FAILING OUTPUT TEST. TEARDOWN OF UNIT FOUND THE CONTACTS ON PC BOARD DIRTY, CLEANED CONTACTS AND RETESTED UNIT PER CMM 30-40-03, REV. 6. 2L72 4F RTA16WE 20040302001172004030200117EA 2004 3 2 COMA0460156 120040218A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS MALFUNCTIONED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 SO01938CA 7046 FLIGHT 5159 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040302001232004030200123WP 2004 3 2 DHL2004809002 120040227A5610 WINDSHIELD DOUG DC8 DC873F 302199FWP COCKPIT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01604AL 46047 F/O'S WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S FORWARD SIDE WINDOW IAW DC8 M/M 56-10-2, NO LEAKS NOTED. 2L74 4F RT4A25 20040302001252004030200125NM 2004 3 2 DHL2004745014 120040219A3260 SWITCH BOEING727 727224 1384076NM RT MLG OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 SELECTING GEAR HANDLE FROM UP TO OFF, RED DOORS LIGHT ON FRONT PANEL AND RIGHT GEAR DOORS LIGHT ON S/O'S PANEL ILLUMINATED. CYCLING GEAR HANDLE FROM UP TO OFF SEVERAL TIMES RE-ILLUMINATED THE LIGHTS. LIGHTS EXTINGUISHED WHEN GEAR HANDLE WAS MOVED TO OFF AT A HIGHER AIRSPEED. ADJUSTED RIGHT MAIN GEAR DOOR SWITCH IAW B-727 M/M 32-12-01. OPS CHECKED GOOD, LIGHT EXTINGUISHED. 2L73 4F A3WE 20040302001352004030200135NM 2004 3 2 SWAA040272 120040128A57556546451 SKIN BOEING737 7373H4 1384600NM LT SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 NR 2 FLIGHT SPOILER DEVELOPS BULGE ON TOP OF SPOILER DURING FLIGHT. REMOVED AND REPLACED NR 2 FLIGHT SPOILER PER MM. 2L72 4F RTA16WE 20040302001402004030200140NM 2004 3 2 SWAA040277 120040128A3350PH22300L STRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C2 CHECK, FOUND EEPLS FROM ROW 7 ABC TO ROW 11 ABC WORN. REMOVED AND REPLACED EEPLS LIGHTING AT ROW 7 ABC TO ROW 11 ABC PER MM. 2L72 4F RTA16WE 20040302001462004030200146NM 2004 3 2 SWAA040296 120040130A3350300432 BATTERY PACK BOEING737 7373Q8 1384670NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SPECIAL VISIT AT SAT AEROSPACE, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040302001572004030200157 2004 3 2 SWAA040307 420040130A2565D31354 BOTTLE BOEING737 7373H4 1384600NM EVAC SLIDE LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040302001582004030200158NM 2004 3 2 SWAA040308 120040130A575465C26686 SKIN BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED C3 CHECK, FOUND NR 2 L/E SLAT UPPER SKIN ON TRAILING EDGE INBOARD AFT CORNER DELAMINATED. REPAIRED L/E SLAT PER EA. 2L72 4F RTA16WE 20040302001622004030200162NM 2004 3 2 SWAA040312 120040130A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BUSHING PER MM. 2L72 4F RTA16WE 20040302001762004030200176NM 2004 3 2 SWAA040379 120040207A53106545855 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR CUTOUT FWD LOWER CORNER CRACKED. REPAIRED PER EA. 2L72 4F RTA16WE 20040302001782004030200178NM 2004 3 2 SWAA040381 120040207A256065C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE LATCH HOOK WITH TO LARGE OF A GAP. ADJUSTED L1 DOOR EVAC SLIDE HOOK PER MM. 2L72 4F RTA16WE 20040302001832004030200183NM 2004 3 2 SWAA040386 120040207A53106547979 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 638, LBL 64, WL 208. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040302001872004030200187NM 2004 3 2 SWAA040390 120040207A3350656C27093 LIGHT BOEING737 7372H4 138448CNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 FWD GALLEY EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. 2L72 4F A16WE 20040302002012004030200201SO 2004 3 2 C2XA04SH073 120040220A532014524131009 BRACKET EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 DURING C CHECK THE MAIN DOOR THRESHOLD FORWARD U BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040303000042004030300004NM 2004 3 3 P9RA20040007 120040214A2170 SEPARATOR BOEING727 727200 138407ENM CABIN AIR DIRTY A P9RAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11906PG 20728 AFTER TAKE OFF, THE AFT FLIGHT ATTENDANT REPORTED THE AFT CABIN WAS FILLING WITH SMOKE. RETURNED TO AIRPORT. PERFORMED TROUBLESHOOTING OF AIR CONDITIONING SYSTEM. FOUND DIRTY WATER SEPARATOR. CLEANED SAME. INSPECTED ALL INTERIOR PAX CABIN FOR EVIDENCE OF SMOKE. PRESSURIZED AIRCRAFT FOR 45 MINUTES. ALL CHECKED GOOD. CHECKED ALL LIGHTING AND BALLASTS. ALL GOOD. NO ELECTRICAL OR SMOKE ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20040303000102004030300010NM 2004 3 3 PCAA0402167 120040211A2612 RELAY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE FIRE DETECTION FAULTY A PCAAK NONE N FALSE WARNING ININSP/MAINT 1 EA13809EX 302 AIRCRAFT APU HAS A HISTORY OF THE FIRE FAULT AND CHECK FIRE DETECT LIGHTS ILLUMINATING AFTER SHUTTING DOWN THE APU. MAINTENANCE HAS COMPLIED WITH SEVERAL CHECKS AND HAS REPLACED THE RELAYS 2623-K1 AND 2622-K2.SYSTEM HAS NO HISTORY SINCE. SYSTEM OPERATIONAL CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20040303000112004030300011EA 2004 3 3 COMA0460147 120040215A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01518CA1803 7816 FLIGHT 5688 LANDING GEAR DISAGREE WARNING. REPLACED THE PSEU. 2L72 4F RTA21EA 20040303000192004030300019NM 2004 3 3 CALA0400127 120040216A291366087 PUMP BOEING737 737824 13844BZNM NR 1 ENG HYD SYSCRACKED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW277625412 30779 THE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WHILE ENROUTE TO CLE. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PUMP HAD FAILED INTERNALLY. THE PUMP WAS REPLACED IAW MM 29-11-11-00-803-001. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040303000602004030300060NM 2004 3 3 VNAA0402002 120040205A7160001A716E1000010 INTAKE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07462PS187552640 3084 DURING FLIGHT, THE CREW RECEIVED A LEFT HAND ENGINE INTAKE DE-ICE FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSPECTED AND REPLACED THE AIR INTAKE ASSEMBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040303000672004030300067EU 2004 3 3 BAQA092646 120040202A249745023502 MASTER BOX UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03603ME115 0284 ELECTRICAL MASTER BOX (S/N 1369) CAME INSTALLED ON NEW A/C N603ME/0284 AND FAILED AFTER 115.3 HOURS OF USE. REPLACED WITH SERVICABLE UNIT FROM STOCK (S/N 1108) 1G72 3U3 U H88EU E42NE 20040303000712004030300071WP 2004 3 3 0377 120040217A5330 DOUBLER DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT INTERIOR SKIN DOUBLER CORRODED AND CRACKED AT FS270 LONGERON 31L AND IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20040303001222004030300122NM 2004 3 3 SWAA040558 120040223A3040589354 CONTROLLER BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29717SA 27851 R1 WINDOW ARC WHEN WINDOW HEAT SELECTED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20040303001322004030300132NM 2004 3 3 2004UALA00135 120040213A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29386UA 24661 AFT CARGO PIT INTERCOSTAL CRACKED AT BS 867-887 STR 25R. MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2GL 20040303001442004030300144NM 2004 3 3 SWAA040543 120040221A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 EEPLS LIGHT COVER BROKEN. REMOVED AND REPLACED EEPLS LIGHT COVER PER MM. 2L72 4F RTA16WE 20040303001492004030300149NM 2004 3 3 2004UALA00141 120040216A5270 WARNING SYSTEM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE DOOR ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29330UA 24191 ABORTED TAKEOFF AT 110 KNOTS WITH AN AFT DOOR INDICATION. CHECKED AND CLEANED AFT ENTRY DOOR PROXIMITY SWITCH. 2L72 4F4 FRTA16WE E2GL 20040303001522004030300152NM 2004 3 3 2004UALA00144 120040217A5311 FRAME BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 UPPER T-CHORD ON THE FRAME AT BS 1780, APPROX RBL 27 HAS A DENT IN THE HORIZONTAL FLANGE OF THE CHORD. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE, SHIMS, INTERCOSTAL WEB & FILLERS. 2L74 4F4 FRTA20WE E24NE 20040303001562004030300156EU 2004 3 3 2004UALA00148 120040220A5320 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29410UA 463 AFT PASSENGER ENTRY DOOR (L2) DOOR SILL PLATE AT FRAME 68 IS CORRODED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NESTED ANGLE & FILLER REPAIR. 2L72 4F4 FRTA28NM E40NE 20040303001602004030300160WP 2004 3 3 ABXA040075 120040209A541299122433 BULKHEAD DOUG DC9 DC941 302207NWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 LT FORWARD PYLON BULKHEAD WAS CRACKED AT BOTTOM AT LT BUTT LINE 44.0. REPAIRED LT FORWARD PYLON BULKHEAD IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040303001802004030300180NM 2004 3 3 MASA200400076 120040208A3397 WIRE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07449YV 449 CREW REPORTED THE EMERGENCY LIGHT FLOOR PATH LIGHTS INOPERATIVE. MECHANIC TIGHTENED LEADS ON EMERGENCY LIGHTS. OPS CHECK GOOD. NO PARTS USED. 2H72 4T4 TRTA13NM E20NE 20040303001992004030300199NM 2004 3 3 2004UALA00150 120040210A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 FUSELAGE DENT NEXT TO DOUBLER AT FWD LOWER CORNER OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REMOVED & REPAIRED. 2L72 4F4 FRTA2NM E17NE 20040303002042004030300204CE 2004 3 3 EWG2004F00000 120040114A5730592211531 SKIN CESSNA425 425 2076018CE PWA PT6 PT6A135 52043NE MCAULY4HFR344HFR34C762 NE LT WING WRINKLED B EWGRO OTHER O OTHER NRNOT REPORTED 1 SO056845R4709 4250071 PCEZ0052 001790 IAW REQUIREMENTS OF FAR 145.63, SUBMITS THIS 8010-4. IN THE PROCESS OF PERFORMING A PHASE 2 AND 3 INSPECTION, DIAGONAL WRINKLES WERE DISCOVERED ON THE TOP LT WING PANEL BETWEEN THE AUX AND AFT SPARS IB OF THE NACELLE. AFTER CONTACT WITH AND REVIEW BY MFG ENGINEERING, MFG RECOMMENDED THE WING PANEL BE REPLACED. MFG STATED NO DIAGONAL WRINKLES WERE ACCEPTABLE IN THE PANEL IN QUESTION AND WAS AN INDICATION OF A HARD LANDING. MFG MM DOES NOT CALL FOR AN INSPECTION OF THE TOP WING PANEL DURING A HARD LANDING INSPECTION, ONLY THE BOTTOM PANELS. MFG HAD NO RECOMMENDATION FOR A REPAIR OR A FIX FOR THE PROBLEM ONLY REPLACEMENT OF THE PANEL. 1L72 3T4 TRTA7CE E4EA 6 C3PNE 20040303002052004030300205SO 2004 3 3 AEX2004F00000 120040122A32136531904 CYLINDER PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA LT MLG STRUT CRACKED B AEXRO OTHER O OTHER NRNOT REPORTED 1 WP092171D12361 287916146 UPPER TORQUE LINK ATTACH LUGS OF LT MAIN LANDING GEAR STRUT CYLINDER CRACKED OF DURING LANDING WITH RESULTING COLLAPSE OF GEAR. PROBABLE CAUSE WAS UNDETECTED PREVIOUS CRACK OR CRACKS. RECOMMEND THAT LANDING GEAR STRUT FAIRINGS TRAINING AIRCRAFT BE PERMANENTLY REMOVED FOR DAILY INSPECTION ACCESS. 1L71 3O3 O 2A13 E274 20040303002112004030300211WP 2004 3 3 CALA0400197 120040301A532059364423 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718833 49493 INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD WEB CRACKED IN TWO PLACES AT STA 1155 FORWARD SIDE OF DOOR CUTOUT. THE CRACKS WERE THREE INCHES LONG. REPAIRED WEB IAW ECRA 5310-04403. 2L72 4F A6WE 20040303002222004030300222NM 2004 3 3 04FDEA00437 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002242004030300224NM 2004 3 3 04FDEA00439 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002372004030300237NM 2004 3 3 QXEA200400170 120040223A5320 BRACKET DHAV DHC8 DHC8202 2809007NM FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09355PH 500 PDX - MAINTENANCE FOUND THE ENGINE DISCHARGE BLOW OUT DISK TUBE BRACKET CRACKED AT THE FUSELAGE. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-42-11. 2H72 4T RTA13NM 20040303002392004030300239NM 2004 3 3 04FDEA00443 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040303002402004030300240NM 2004 3 3 04FDEA00444 120040219A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040304000082004030400008 2004 3 4 BAQA092782 420040216A34205050031904 GYRO BOLKMSBK117 BK117C1 5626025EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG3105 7506 STANDBY GYRO CARD SLIPS IN DISPLAY. REPLACED WITH SERVICABLE UNIT. 02/20/2004 1G72 3U NCH13EU 20040304000112004030400011 2004 3 4 BAQA092793 420040121A221141800491350 COMPUTER AEROSPAS365 AS365N2 8680815EU AUTOPILOT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 UNIT IS BEING SENT TO AEC FOR WARRANTY REPAIR. REASON FOR REMOVAL, BOTH ROLL ACTUATORS WERE INOPERATIVE. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 545) 1G72 3U RTH10EU 20040304000172004030400017EU 2004 3 4 BAQA092803 120040212A77141179405303 INDICATOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE TRIPLE TACH FLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1163 7235 TRIPLE TACH NR 2 ENG N2 GOES LOW. REPLACED WITH SERVICEABLE ASSET UNIT. 02/20/2004 1G72 3U3 U H13EU E5NE 20040304000592004030400059EU 2004 3 4 TRB2004F00009 120040209A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU PWA PW120 PW124B NE EMERGENCY LIGHT FAULTY A TRBAK NONE L NO TEST ININSP/MAINT 1 SO21288AM 288 FLOOR EMERGENCY LIGHTS REMAIN ON. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. 2H72 4T4 TRTA53EU E2ONE 20040304000682004030400068EA 2004 3 4 COMA0460170 120040223A3241 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ANTI SKID SYS ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01781CA 7312 FLIGHT 5049 ANTI SKID MESSAGE DURING T/O. DEFERRED MAINTENANCE ON ANTI SKID IAW MEL. 2L72 4F4 FRTA21EA E15NE 20040304000762004030400076 2004 3 4 X072004F00000 420040202A2210065001790100 ACTUATOR CESSNA182 182S 2072701CE LYC O540 IO540* 41532EA ROLL INOPERATIVE B X07RO OTHER O OTHER NRNOT REPORTED 1 CE07973CF1136 18280253 PILOTS FOUND AILERON SYSTEM ROUGH ON PREFLIGHT. MECHANICS IN CHECKING OUT CAUSE, FOUND AILERON SYSTEM TO LOCKUP AND WOULD NOT FREE UP UNTIL SERVO WAS REMOVED. APPEARS BEARING IN GEAR BOX IS SLOPPY AND GEAR WILL BIND UP WHEN TURNED. 1H71 3O3 ONT3A13 1E4 20040304000842004030400084NE 2004 3 4 CX7A194J0408 220040113A7261 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE MAKING METAL A CX7AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL03303CE 3446 340B194 785358 ENGINE CHIP DETECT LIGHT ON. 2L72 4T4 TRTA52EU E8NE 20040304001132004030400113WP 2004 3 4 GTIA040103 120040114A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FS 1174 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL FS 1174 RBL 24-44 CORRODED AND TOP PRIMER REQ'D. FABRICATED FLOOR PANEL. (M) 2L72 4F A6WE 20040304001142004030400114WP 2004 3 4 GTIA040106 120040129A7160 NOSE COWL DOUG DC9 DC983 3022083WP NR 1 ENGINE WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - NR 1 ENGINE NOSE COWL HAS EXPOSED FIBERGLASS AFT OF INLET RING ENTIRE CIRCUMFERENCE. ON FURTHER INVESTIGATION FOUND NOSE COWL SKIN DELAMINATED. REPAIRED COWL. (M) 2L72 4F RTA6WE 20040304001272004030400127WP 2004 3 4 GTIA040119 120040127A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND LEFT FLOOR PANEL STATION 200-256 DELAMINATED AND TWO INSERTS MISSING. FABRICATED NEW PANEL. (M) 2L72 4F RTA6WE 20040304001992004030400199NM 2004 3 4 SWAA040283 120040129A335007912 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29767SW 29807 EEPLS FLOOR TRACK LIGHTING LENS MISSING. INSTALLED EEPLS LENS PER MM. 2L72 4F RTA16WE 20040305000062004030500006NM 2004 3 5 SWAA040293 120040129A3350BAC27DEL1157 BATTERY BOEING737 7377Q8 1384418NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29799SW 28209 DURING SCHEDULED MC, FOUND MID-CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040305000072004030500007NM 2004 3 5 SWAA040294 120040129A3350610478 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040305000112004030500011SO 2004 3 5 SWIA200412865 120040208A261147359713 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO AFT CARGO FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07299SW6 6 120329 SMOKE AURAL WARNING FOR CARGO SOUNDED. REPLACED AFT CARGO SMOKE DETECTOR. OPS CHECK GOOD. 2L72 4T RTA31SO 20040305000192004030500019 2004 3 5 SWIA200412873 420040203A3497 WIRE EMB 120 EMB120ER 3260203SO STALL WARNING DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07250YV 120250 CAPTAIN'S STALL WARNING SHAKER INOP ON TEST (PUSHER WORKS). REPAIRED WIRING AT NR 1 STALL SHAKER CONNECTOR. OPS CHECK GOOD. 2L72 4T RTA31SO 20040305000212004030500021 2004 3 5 SWIA200412875 420040206A34256226190204 COMPUTER EMB 120 EMB120ER 3260203SO E/E BAY MALFUNCTIONED A SWIAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 NM07268UE4407 4401 120207 ON ROTATION AUTO PILOT FAIL & TRIM FAIL, MAP ILLUMINATED WITH ASSOCIATED TRIPLE CHIME AND AURAL WARNING. BOTH FCP'S SHOWED TRIM AND AP WARNINGS. AUTOPILOT PANEL INDICATED T, AP, R, E, TRIM. WOULD NOT RESET. CAPTAIN'S EADI SHOWED FD. REMOVED AND REPLACED NR 2 AHRS COMPUTER WITH NEW AHRS COMPUTER IAW 32-21-00. OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA31SO 20040305000352004030500035NM 2004 3 5 04FDEA00424 120040218A5320ACA7104509 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN FLOOR TRACKS CRACKED AT STA 755, LT X=27.5. FLOOR TRACK CRACKED AT STA 755, LT X = 27.5 CARRIED OUT REPAIR IAW SRM 53-70-00 VOL I FIG 1 2L73 4F RTA22WE 20040305000822004030500082EA 2004 3 5 SWIA200412883 120040208A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIAD RETURN TO BLOCK JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07445SW4355 4355 7651 ON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON OUTBOARD PCU AND SECU NR 1. OPS CHECK SATISFACTORY. LEAK CHECK SATISFACTORY IAW MM 27-60-03. PCU P/N: 49-164-06, S/N OFF: 01389. 2L72 4F4 FRTA21EA E15NE 20040305000872004030500087 2004 3 5 SWIA200412888 420040209A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07441SW5716 5716 7602 STALL FAIL CAUTION SHORTLY AFTER TAKEOFF. FOLLOWED QRH PROCEDURES AND CONTINUED TO FAT. REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-00-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040305000892004030500089 2004 3 5 SWIA200412890 420040210A31706229820009 DCU CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW230 230 7578 NR 1 PFD WENT BLANK FOLLOWED BY A NR 1 YAW DAMPER DISCONNECT AND AUTO PILOT DISCONNECT. BOTH RE-ENGAGED. REMOVED AND REPLACED NR1 PFD IAW 31-61-4. OPS CHECK GOOD. RETURNED TO CAT II. REMOVED AND REPLACED NR 1 DCU FOR NUMEROUS DCU FAILS IN MDC IAW 31-41-04. PFD P/N: 622-9810-016, S/N OFF: 10DRR. 2L72 4F RTA21EA 20040308000022004030800002EU 2004 3 8 MALA040195 120040209A2612472326 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE CHAFED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15441XJ 340B441 DURING CLIMBOUT LEFT ENG FIRE DETECT LIGHT CYCLED ON AND OFF, OCCASIONALLY THE LT ENG FIRE T-HANDLE CAME ON AND OFF A FEW TIMES. AIR RETURN TO DTW. MAINTENANCE FOUND SENOR LOOP CHAFED, INSTALLED SERVICEABLE SENOR LOOP P/N 472326 IAW SF-340 MM 26-11-05-2. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040308000172004030800017SO 2004 3 8 C2XA04SH078 120040220A532014521699003 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000212004030800021SO 2004 3 8 C2XA04SH082 120040220A532014522459003 ANGLE EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000222004030800022SO 2004 3 8 C2XA04SH083 120040220A532013500374009 SPLICE EMB 135 EMB135ER 3260203SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK STRINGER 19 LEFT INTERNAL SPLICE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000232004030800023SO 2004 3 8 C2XA04SH084 120040220A532014525480003 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000242004030800024SO 2004 3 8 C2XA04SH085 120040220A531514521713005 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000372004030800037EU 2004 3 8 MALA040203 120040221A3010 BOOT SAAB SF340 340B 7860101EU HORIZ STAB DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15433XJ 340B433 BOOT TIMER LIGHT CAME ON IN FLT. TRIED TO MANUALLY INFLATE STAB BOOT, NO INDICATION THAT BOOTS INFLATED. LAMPS TEST OKAY. AIR RETURN TO DTW. MAINTENANCE PATCHED RIGHT HORIZ STAB AND REPLACED LT HORIZ STAB BOOT. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040308000432004030800043NM 2004 3 8 AWXA200400200 120040220A30204603KPS235 PRESSURE SWITCH BOEING757 7572S7 1384962NM NR 1 ENGINE DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28906AW5245533886 23568 AFTER TAKEOFF AT PHX EN ROUTE FOR MSP RECEIVED EICAS MESSAGE -L ENG ANTI-ICE- WITH NR 1 ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED. DUE TO ICING CONDITIONS AT MSP TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE, DID NOT CORRECT THE PROBLEM, REPLACED ENGINE ANTI-ICE LOW PRESSURE SWITCH IAW BMM 30-21-01. PERFORMED ENGINE RUN, ANTI-ICE VALVE OPERATED NORMALLY, NO LIGHT OR EICAS MESSAGES NOTED. FUNCTIONAL TEST OF ANTI-ICE LOW PRESSURE SWITCH S/N TR565 WAS NO FAULT FOUND, INSULATION, LEAKAGE, AND CALIBRATION TESTS WERE GOOD. 2L72 4F RTA2NM 20040308000512004030800051NM 2004 3 8 04FDEA00417 120040217A5230AFA80821 FITTING DOUG MD11 MD11 3023602NM CARGO DOOR SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CTR CARGO - DOOR SILL BETWEEN NR 1 & NR 2 FROM FWD ROLLER GUIDE FITTING SPOOL SCRATCHED MARKS. FEDEX EA 1-5230-74188 DOOR - CENTER CARGO 104 INCHES DOOR - ALIGNMENT PIN MODIFICATION HAS BEEN COMPLIED WITH & FOUND SATISFACTORY. 2L73 4F RTA22WE 20040308000522004030800052NM 2004 3 8 04FDEA00423 120040217A71102214110509 FITTING DOUG MD11 MD11 3023602NM NR 3 COWLING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 NR 3 ENG NOSE COWL (FAN COWL) GUIDE FITTING LT & RT FOUND WORN. ACCOMPLISHED AS PER EA 1-7110-74316 ENGINES, ENGINE COWLING - INCORPORATION OF P&W SB 71-120. 2L73 4F RTA22WE 20040308000602004030800060NM 2004 3 8 04FDEA00493 120040220A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232. 2L73 4F RTA3WE 20040308000692004030800069EA 2004 3 8 QXEA200400166 120040218A5240 SLIDE CNDAIRCL600 CL6002C10 1390015EA SERVICE DOOR DEFECTIVE A QXEAK NONE O OTHER UKUNKNOWN 1 NM09609QX5129 10031 PDX - CREW REPORTS, UNABLE TO OPEN SERVICE DOOR. THE HANDLE BINDS IN THE 12 O'CLOCK POSITION. MAINTENANCE REMOVED THE SERVICE DOOR INNER PANEL AND REASSEMBLED THE UPLOCK STRUT INNER TO OUTER SLIDE ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040308000732004030800073NM 2004 3 8 AWXA200400205 120040222A2560P4010021 BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040308000752004030800075EU 2004 3 8 AWXA200400207 120040211A5320D5347209800000 BEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON AUXILIARY BEAM Y912 LT AT FR 66. MAINTENANCE REMOVED AND REPLACED CORRODED AUXILIARY BEAM Y912 LT IAW A320 SRM 51-49-00, PG 5 & 6. 2L72 4F RTA28NM 20040308000762004030800076EU 2004 3 8 AWXA200400208 120040211A5315D5347217220090 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00, PG 5 & 6. 2L72 4F RTA28NM 20040308000782004030800078EU 2004 3 8 AWXA200400210 120040212A5347D53230463200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND IN TWO PLACES ON LT OUTBOARD SEAT TRACK AT FR 33, Y1292. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK AT FR 33, Y1292; FABRICATED A FILLER, DOUBLER, AND 2 EACH L-PROFILES; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-15, FIG 202 PG 207-211. 2L72 4F RTA28NM 20040308000802004030800080SO 2004 3 8 C2XA04BT023 120040221A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2722909 145459 DURING SERVICE AND ROUTINE INSPECTION MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHT AFT OF EMERGENCY EXIT AISLE TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY AISLE LIGHT IAW EMB145 MM 33-50-08. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040308000822004030800082EA 2004 3 8 QXEA200400164 120040222A361032912104 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09607QX5179 10024 SEA - FLIGHT 2454 DIVERSION TO PDX ON FLIGHT FROM SEA TO SBA LEFT HAND BLEED AIR VALVE CYCLES. REPLACED THE LOAD CONTROL VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040308000832004030800083SO 2004 3 8 C2XA04SH094 120040225A532014521721009 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000862004030800086SO 2004 3 8 C2XA04SH097 120040225A532014521725001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE LEFT HAND FLOOR SILL BETWEEN FRAMES 18 AND 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000872004030800087SO 2004 3 8 C2XA04SH098 120040225A532014521725613 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE RIGHT HAND FORWARD FLOOR SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000882004030800088SO 2004 3 8 C2XA04SH099 120040225A711014576057622 STIFFENER EMB 145 EMB145 3260210SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE RIGHT HAND ENGINE UPPER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE CHAFED AND EXCEEDED BLEND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000902004030800090SO 2004 3 8 C2XA04SH101 120040225A716014575001405 INTAKE EMB 145 EMB145 3260210SO NR 2 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000912004030800091EU 2004 3 8 DHL2004367003 120040225A5270 WARNING SYSTEM AIRBUS300 A300B4203 3930306EU COCKPIT ACTIVATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01367DH 265 MASTER WARNING PANEL (MWP) DOORS LIGHT ILLUMINATED WITH NO LIGHTS ON S/O'S DOORS PANEL ILLUMINATED. CYCLED CREW ENTRY DOORS IAW M/M 52-71-00. OPS CHECKED GOOD. 2L72 4F RTA35EU 20040308000922004030800092NE 2004 3 8 DHL2004805001 220040224A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 MALFUNCTIONED A DHLAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO01805DH 46125 ON TAKEOFF ROLL NR 1 ENGINE ROLLED BACKED TO IDLE. CHECKED NR 1 ENGINE MAIN ENGINE CONTROL (MEC) CONTROL RODS, INSPECTED INLET & EXHAUST, CHECKED SPECIFIC GRAVITY, FOUND OK IAW CFM M/M 72-00-00. PERFORMED POWER ASSURANCE CHECK IAW JRH 13.3, FOUND OK. UNABLE TO DUPLICATE. 2L74 4F4 FRT4A25 E2GL 20040308000932004030800093NM 2004 3 8 CALA0400162 120040224A5753113A270016 SKIN BOEING737 737724 13844BYNM T/E FLAP PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND RIGHT INBOARD T/E AFT FLAP PUNCTURED ON BOTTOM SIDE. THE FLAP WAS REPAIRED IAW SRM 51-70-10. 2L72 4F RTA16WE 20040308000942004030800094NM 2004 3 8 CALA0400163 120040225A57536546435333 FLAP BOEING737 7373T0 1384582NM LT WING DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND LEFT WING NR 1 AFT FLAP INBOARD T/E DELAMINATED. REPAIRED IAW SRM 51-70-10. 2L72 4F RTA16WE 20040308000952004030800095NM 2004 3 8 CALA0400164 120040225A5320143N5366 SILL BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714106 27296 INSPECTION FOUND THE FORWARD CARGO DOOR LOWER SILL UPPER SURFACE CORRODED AT AFT SECTION BEHIND THE SCUFF PLATE SUPPORT BRACKET, STA 580. REPAIRED IAW SRM 51-40-02. 2L72 4F RTA2NM 20040308000962004030800096NM 2004 3 8 QXEA200400171 120040223A2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8202 2809007NM HYD SYSTEM CONTAMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09359PH 514 PDX - FLIGHT 2170 - IMMEDIATELY AFTER SELECTING GEAR UP, THE NR 2 ENGINE HYDRAULIC PUMP CAUTION ILLUMINATED. THE GEAR DOORS DID NOT RETRACT AND THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT, BLED THE HYDRAULIC SYSTEM, CHECKED THE NR 2 LUBE DRAIN FILTER, VERIFIED PROPER OPERATION OF THE HYDRAULIC RESERVOIR, AND PERFORMED OPERATIONAL CHECKS OF THE EXTENSION AND RETRACTION SYSTEM. NO LEAKS WERE NOTED, AND THE GEAR OPERATIONAL CHECKS WERE GOOD. NO PARTS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040308000972004030800097EA 2004 3 8 QXEA200400172 120040223A274284897131 MOTOR CNDAIRCL600 CL6002C10 1390015EA HORIZ STAB FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09614QX321 10049 TUS - FLIGHT 2571 - IN FLIGHT, THE STAB CHANNEL INOP STATUS MESSAGE APPEARED WITH RUNAWAY TRIM CLACKER. MAINTENANCE INTERROGATED THE MAINTENANCE DIAGNOSTICS COMPUTER AND FOUND THE H-STAB RESOLVER FAILED. THE HSTA MOTOR WAS THEN REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040308000982004030800098EA 2004 3 8 QXEA200400173 120040224A26119847101505 SCREEN CNDAIRCL600 CL6002C10 1390015EA CARGO BAY DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX1208 10033 PDX - FLIGHT 2472 - GAPS WERE FOUND IN THE FORWARD CARGO SMOKE DETECTOR SCREEN. MAINTENANCE REPLACED THE FORWARD CARGO SMOKE DETECTOR SCREEN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040308001002004030800100NM 2004 3 8 04FDEA00518 120040225A5320 PLATE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 COCKPIT - ALUMINUM FLOOR BASE (PLATE) LOCATED BELOW CAPTAIN LEFT CONSOLE CORRODED. COCKPIT - ALUMINIUM FLOOR BASE (PLATE) LOCATED BELOW CAPTAIN LT CONSOLE CORROSION REMOVED BY HAND CLEAN AND REPROTECTED AS PER SRM 51-21-01 VOL II. REWORKED AREA FOUND WITHIN LIMITS AS PER SRM 53-00-01 VOL I. AREA PAINT TOUCHED UP AS PER SRM 51-21-01 VOL II. 2L73 4F RTA22WE 20040308001012004030800101NM 2004 3 8 04FDEA00516 120040224A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORROED. 2L73 4F RTA22WE 20040308001022004030800102NM 2004 3 8 04FDEA00517 120040225A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LT AND RT INBOARD TRAILING EDGE FLAP - HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040308001032004030800103NM 2004 3 8 04FDEA00513 120040223A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED 2L73 4F RTA22WE 20040308001042004030800104NM 2004 3 8 04FDEA00512 120040223A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-74322 - WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20040308001062004030800106NM 2004 3 8 04FDEA00510 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001092004030800109NM 2004 3 8 04FDEA00507 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001102004030800110NM 2004 3 8 04FDEA00506 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA #1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001132004030800113NM 2004 3 8 04FDEA00503 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001152004030800115NM 2004 3 8 04FDEA00501 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040308001162004030800116NM 2004 3 8 04FDEA00500 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC502. COMPLIED AS PER EA 1-5470-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040308001172004030800117NM 2004 3 8 04FDEA00499 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001182004030800118NM 2004 3 8 04FDEA00498 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001192004030800119NM 2004 3 8 04FDEA00497 120040220A5320 TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN - FLOOR TRACK AT STA 473 CTR, X = 0, CORRODED. FLOOR TRACK (CORRODED) AT STA 473 CTR X=0 REMOVED AND REPLACED AS PER SRM 51-33-01, VOL.II. 2L73 4F RTA22WE 20040308001202004030800120NM 2004 3 8 04FDEA00496 120040212A2740BACC2A4B25210B CONTROL CABLE BOEING727 727200 138407ENM HORIZ STAB OUT OF POSITION A FDEAK NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO25244FE 21647 AFTER LANDING, STABILIZER INOP IN BOTH CRUISE AND STAB MODE MANUAL HAND CRANK SHOWS NO RESISTANCE AS IF CABLE IS BROKEN. TROUBLESHOT TO STAB TRIM CABLES BEING OFF UPPER DRUM AND BOUND UP UNDERNEATH IT. REMOVED UPPER AND LOWER, LEFT AND RIGHT JACK SCREW ACCESS PANELS. CUT AND BLOCKED CABLES (TO THE BULKHEAD FORWARD OF JACKSCREW). REMOVED BOUND UP CABLE FROM AROUND BOTTOM OF DRUM. CRUISE AND STAB TRIM MOTOR C/B'S ARE PULLED AND TAGGED. REMOVED AND REPLACED STAB TRIM CABLES. COMPLETED INSTALLATION AND RIG OF STAB TRIM CABLES. ADJUSTED CHAIN TENSION AND INDICATOR PER B727-200 MM 27-40-000. 2L73 4F RTA3WE 20040308001242004030800124EU 2004 3 8 AWXA200400215 120040211A5320D53480043204 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON L-2 DOORWAY SILL INBOARD OF THE PROFILE ZEE BETWEEN FR 66 AND FR 68. MAINTENANCE CUT OUT DAMAGED AREA OF L-2 DOORWAY SILL FROM FR 66 TO FR 68; FABRICATED A FILLER & REPAIR STRAP; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 101 & 102 PG 101-103, 207-208, & 211-212. 2L72 4F RTA28NM 20040308001262004030800126EU 2004 3 8 AWXA200400218 120040211A5315D53472090005 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00, PG 5 & 6, TABLE 1. 2L72 4F RTA28NM 20040308001272004030800127EU 2004 3 8 AWXA200400219 120040211A5320D53480043205 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND UNDER R-2 DOOR FORWARD GIRT SPACER, AFT OF FR 66 AT Y1732 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF R-2 DOOR SILL BEAM AFT OF FR 66 AT Y1732 RT; FABRICATED A FILLER & REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 101 PG 103 & FIG 201 PG 201-203. 2L72 4F RTA28NM 20040308001282004030800128EU 2004 3 8 AWXA200400220 120040211A5753D5757005001052 SKIN AIRBUS320 A320231 3930325EU T/E FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK THE LT INBOARD FLAP WAS FOUND DELAMINATED AT REPAIR ON LOWER SURFACE, OUTBOARD OF NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR DOUBLER ON LOWER SURFACE, OUTBOARD OF NR 2 FLAP FAIRING; FABRICATED A NEW REPAIR DOUBLER; PERFORMED BOND REPAIR IAW A320 SRM 57-52-00 FIG 211 PG 248-256. 2L72 4F RTA28NM 20040308001332004030800133NM 2004 3 8 ASAA0410033 120040114A523065C352433 DOOR FRAME BOEING737 7372Q8C 138448SNM CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR NEEDS FRAME MODIFICATION. REPAIR IAW EA. (M) 2L72 4F A16WE 20040308001542004030800154NM 2004 3 8 ASAA0410016 120040108A53306545800150 SKIN BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STATION 344, STRINGER 19R. (M) 2L72 4F A16WE 20040308001552004030800155NM 2004 3 8 ASAA0410018 120040112A5315 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND AFTER ACCOMPLISHING A FLOORBEAM REPAIR, THE SHEAR WEB AT FUSELAGE STATION 500A, LEFT BUTTOCK LINE 24 HAS MISALIGNED HOLES. REPAIRED SHEAR WEB PER EA. (M) 2L72 4F A16WE 20040304000132004030400013EU 2004 3 4 BAQA092798 120040204A284481071370010 TRANSMITTER AEROSPAS365 AS365N2 8680815EU FUEL PRESS GAUGEFLUCTUATES B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME60 6417 FUEL PRESSURE GAUGE TRANSMITTER FLUCTUATING. REPLACED WITH SERVICEABLE ASSET UNIT. 1G72 3U RTH10EU 20040304000272004030400027CE 2004 3 4 AKG2004F00002 120040210A531250440041127 BULKHEAD BEECH 90 C90 1152913CE PWA PT6 PT6A60A 52043NE FUSELAGE DAMAGED B AKGRK NONE O OTHER ININSP/MAINT 1 CE05911CX6189 LJ830 IN COMPLETING AD, NOT ONLY WAS SCORING FOUND ACROSS THE MID SPAN, BUT ALSO ALL THE WAY AROUND WERE THE (U) FRAME LAYS ON TOP OF THE BULKHEAD WEB. THERE IS NOT A PATCH REPAIR FOR THIS. THE BULKHEAD WEB WILL AVE TO BE REPLACED. 1L72 3T4 T 3A20 E4EA 20040304000362004030400036WP 2004 3 4 02240402WP 120040201A302013277501 DUCT DOUG DC9 DC9 3022002WP PWA JT8 JT8D15A 52051NE LT ENGINE BROKEN A A4JAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO35934LK 48157 AFTER TAKEOFF THE RT ENGINE FIRE WARNING LOOP (A) LIGHT ILLUMINATED. SHORTLY, AFTER THE FIRE WARNING LOOP (B) ILLUMINATED WITH FULL ENGINE FIRE INDICATIONS. MAINTENANCE FOUND BROKEN COUPLING ON THE COWL ANTI-ICE DUCT, REMOVED AND REPLACED DUCT ASSEMBLY IAW MM 75-10-5. OPERATIONAL AND LEAK CHECK GOOD. 2L72 4F4 F A6WE E2EA 20040304000372004030400037EU 2004 3 4 GQR2004F00000 120040211A28222060F14 PUMP AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP LT FUEL BOOST WORN E GQRAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0581TX 600 81 DURING FLIGHT CREW NOTICED THERE WAS A LARGE DISCREPANCY BETWEEN INDICATED FUEL QUANTITY AND AMOUNT OF FUEL USED AS SHOWN ON FLIGHT MANAGEMENT SYSTEM. UPON LANDING CREW NOTICED FUEL DRIPPING FROM SEVERAL AREAS ON THE UNDERSIDE OF THE AIRCRAFT. FUEL WAS FOUND IN THE AFT BAGGAGE COMPARTMENT. WHILE TROUBLESHOOTING THIS PROBLEM, MAINTENANCE PERSONNEL DISCOVERED THAT WHEN THE LT FUEL BOOST PUMP WAS OPERATED IT WAS CONTINUOUSLY PUMPING FUEL OUT OF THE PUMP HOUSING OVERBOARD DRAIN. THE INTERNAL SEALS IN THIS PUMP HAD FAILED CAUSING THIS PROBLEM. DEFECTIVE PUMP WAS REPLACED WITH AN OVERHAULED UNIT AND AIRCRAFT WAS OPERATED WITH NO FURTHER PROBLEMS. 2L72 4F4 F A33EU E6WE 20040304000382004030400038WP 2004 3 4 02240403WP 120040205A3260 WARNING LIGHT DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE MLG FALSE INDICATIONA A4JAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO35932MJ 48156 AFTER TAKEOFF, RT MLG UNSAFE LIGHT AND DOOR LIGHT ILLUMINATED. MAINTENANCE JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS AND 1 MANUAL EXTENSION. NO DEFECTS NOTED. AFTER RETURN TO SERVICE. 2L72 4F4 F A6WE E2EA 20040304000402004030400040SO 2004 3 4 TZR2004F00002 220040129A74146320 MAGNETO CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO MCAULY3AF32C3AF32C* GL LEFT AND RIGHT CORRODED E TZRAO OTHER O OTHER NRNOT REPORTED 1 SW05110KS1035 402B1366 514857 PILOT REPORTED AN EXCESSIVE MAGNETO DROP ON LT AND RT MAGNETOS. UPON FURTHER INSPECTION FOUND THE MAGNETOS FULL OF CORROSION AT HARNESS CONNECTION AND IN THE AREA WHERE POINTS ARE LOCATED. THIS AIRCRAFT HAD NOT BEEN FLOWN IN A WHILE AND HANGARED FOR MOST OF THAT TIME. THIS AIRCRAFT HAS PRESSURIZED MAGNETOS AND BELIEVE THIS COULD BE THE SOURCE OF THE MOISTURE. 1L72 3O3 O A7CE E8CE 5 CP22EA 20040304000602004030400060NE 2004 3 4 TRB2004F00010 220040212A73208108001002 EEC AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE FAULTY A TRBAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO21429AT 429 C94050024 NO TORQUE INDICATION DURING TAKEOFF ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ELECTRONIC ENGINE CONTROL (EEC). 2H72 4T4 TRTA53EU E20NE 20040304000612004030400061WP 2004 3 4 UPS04841957 120040223A33505708458503 BATTERY PACK DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE: N/A AS REPORTED FROM THE FLIGHT CREW EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OK FOR SERVICE. 2L74 4F4 FRT4A25 E2GL 20040304000672004030400067EA 2004 3 4 COMA0460169 120040223A5230 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO BAY OPEN A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01982CA 7168 FLIGHT 5109 CARGO DOOR WARNING DURING T/O. CLOSED CARGO DOOR PROPERLY. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20040304001012004030400101EU 2004 3 4 MALA040207 120040207A5311 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 FS 583.0 FRAME BETWEEN STR SL1501 AND 1601 GOUGED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW EO NR S53152. A/C RELEASE DATE 2/26/04. REFER LOG PAGE NR 1264969 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20040304001032004030400103EU 2004 3 4 MALA040213 120040221A3260CM7715 BULB SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE MLG INDICATOR BURNED OUT A MALAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL15404XJ 340B404 TRANSIT LIGHT ON AFTER LIFT OFF, DURING GEAR RETRACTION (HYDRAULIC PUMP ON) TRANSIT LIGHT GOT BRIGHTER THEN REMAINED ON ALONG WITH RT GEAR LIGHT. LT AND RT NOSE GEAR LIGHTS WERE OUT. CYCLED GEAR DOWN, GOT 3 GREEN GEAR LIGHT BUT THE TRANSIT LIGHT REMAINED ON. FOUND TEST BUTTON TO BE ENGAGED SLIGHTLY CAUSING LIGHT TO STAY ON IN DIM MODE. CHANGED BULBS CM7715. PERFORMED GEAR SWINGS IAW MFG AMM CH 32-30-00-5 TO CHECK FOR GREEN LIGHT RT MAIN BEING OFF. GEAR SWINGS ALL CHECK GOOD AFTER 10 UP AND DOWN SWINGS. LIGHT (TRANSIT) DOES NOT STAY ON WITH GEAR IN UP OR DOWN POSITION. OK FOR SERVICE. 2L72 4T4 TRTA52EU E8NE 20040304001182004030400118WP 2004 3 4 GTIA040118 120040118A5522 SKIN DOUG DC9 DC983 3022083WP ELEVATOR GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND RIGHT ELEVATOR BOTTOM SIDE IS DENTED AND GOUGED NEAR OUTBOARD EDGE. REMOVED DAMAGED SECTION OF RIGHT ELEVATOR BOTTOM SIDE SKIN. FABRICATED TWO FINGER DOUBLERS. FABRICATED 1 SKIN SECTION APPROX 15 INCHES BY 16 INCHES. FABRICATED 1 GUSSET. INSTALLED TWO DOUBLERS, 1 GUSSET, ONE 15 INCHES BY 16 INCHES SKIN SECTION. (M) 2L72 4F RTA6WE 20040304001222004030400122WP 2004 3 4 GTIA040113 120040113A5320 CLIP DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND AFT PIT FS 1117 INTERCOSTAL CLIP RBL 13 CORRODED. REMOVED CLIP. FABRICATED CLIP. INSTALLED CLIP. (M) 2L72 4F RTA6WE 20040304001242004030400124WP 2004 3 4 GTIA040122 120040118A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND COCKPIT FLOOR PANEL FOR CONSOLE SKIN IS DEBONDED AND MISSING. REBONDED SKIN. (M) 2L72 4F RTA6WE 20040304001282004030400128WP 2004 3 4 GTIA040105 120040106A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FORWARD CABIN STATION 218 TO STATION 200 LEFT INBOARD SEAT TRACK HAS NICKS, GOUGED, CORROSION. REMOVED DAMAGED SEAT TRACK STATION 200-645. DRILLED AND LOCATED NEW TRACK AND SPLICES. INSTALLED SEAT TRACK LBL 24 STATION 200-645 AND 4 EACH SPLICE. (M) 2L72 4F A6WE 20040304001652004030400165WP 2004 3 4 GTIA040127 120040113A71105930645501 NOSE COWL DOUG DC9 DC983 3022083WP RT ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND TEMP REPAIR INSTALLED NR 2 NOSE COWL ACOUSTIC LINER. REMOVED AND RIGHT NOSE COWL. INSTALLED NOSE COWL. (M) 2L72 4F RTA6WE 20040304001662004030400166WP 2004 3 4 GTIA040129 120040210A2560 SIGN DOUG DC9 DC983 3022083WP G-4 GALLEY MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 DEN - FLT 367 - SAFETY GLOW EXIT SIGN AT G-4 GALLEY L-2 DOOR MISSING. FOUND PIECE SERVICABLE/REINSTALLED EXIT SIGN. (M) 2L72 4F RTA6WE 20040304001732004030400173WP 2004 3 4 DHL2004806584 120040127A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAPS DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 INTERIM REPAIR ON UPPER SURFACE OF RIGHT OUTBOARD FLAP, STA XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-1, DWG U80-R01. REMOVED SKIN SEGMENT WITH INTERIM REPAIR ON IT IAW ED EDU80-1, DWG U80-R01, SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.071) IAW ED EDU80-1, DWG U80-R01. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW SKIN SEGMENT IAW SR 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN SEGMENT IAW ED EDU80-1, DWG U80-R01, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040304001762004030400176WP 2004 3 4 DHL2004806577 120040127A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LEFT WING OTBD L/E UPPER & LOWER PART CORRODED AT STA XW 761.695. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIRS (3EA). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDU80-9, DWG U80-R09. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED FILLERS 2EA (7075-T6AL 0.050) AND DOUBLER (7075-T6AL 0.063) IAW ED-EDU80-9, DWG U80-R09. CLEANED, TREATED AND PRIMED AREA, FILLERS AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED-EDU80-9, DWG U80-R09, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001852004030400185WP 2004 3 4 DHL2004806589 120040205A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 FWD CARGO COMPT FLOORBEAM WITH 0.250 CRACK IN IT, STA 200.000 LBL 32 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. CUT OUT FLOORBEAM DAMAGED AREA. INSPECTED FOR CRACKS IAW DC8 NDT SPM PART 6-10-01-001. FABRICATED 2EA ANGLE DOUBLER FWD/AFT (7075-T6 0.160), 2EA SPACER (7075-T6 0.142, 0.171), CLIPS 2EA (7075-T6 0.090), 2EA FILLER (7075-T6 0.071), SPACER AFT (7075-T6 0.071), 2EA SPLICE DOUBLER FWD/AFT (7075-T6 0.071), T-FILLER (7075-T6 0.125) IAW ED EDU80-7, DWG U80-R07. CLEANED, TREATED AND PRIMED AREA AND FABRICATED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FABRICATED PARTS IAW ED EDU80-7, DWG U80-R07, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040304001962004030400196NM 2004 3 4 SWAA040402 120040207A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29744SW 29490 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS LIGHT COVERS CRACKED. REMOVED AND REPLACED EEPLS LIGHT COVERS PER MM. 2L72 4F RTA16WE 20040304002012004030400201NM 2004 3 4 SWAA040285 120040129A5753 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FLAP OUTBOARD CORNER DELAMINATED. REMOVED AND REPLACED INBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20040304002042004030400204NM 2004 3 4 SWAA040288 120040129A3350101073 LENS BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040304002052004030400205NM 2004 3 4 SWAA040289 120040129A575465C26602 WEDGE BOEING737 7373H4 1384600NM NR 5 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20040305000012004030500001 2004 3 5 AWXA200400170 420040211A2565D31042190 SLIDE BOEING757 7572S7 1384962NM L-4 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW626466532 23567 PHX - EES - DURING 4-DAY CHECK MAINTENANCE FOUND THE L-4 DOOR SLIDE BOTTLE PRESSURE IN RED ZONE. MAINTENANCE REMOVED AND REPLACED L-4 DOOR SLIDE ASSEMBLY IAW T/C R1C25602. 2L72 4F RTA2NM 20040305000462004030500046EU 2004 3 5 AWXA200400194 120040209A5315D53472209201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM AT FR 66, Y765 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM AT FR 66, Y765 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472209; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 9-14, 16 & 17, PG 6, 7-10 & 12. 2L72 4F RTA28NM 20040305000482004030500048EU 2004 3 5 AWXA200400196 120040209A5315D53472209201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28652AW 953 MCN - MAJOR REPAIR - DURING B-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM AT FR 70, Y765 RT. MAINTENANCE REMOVED DAMAGED FLOORBEAM BETWEEN FR 68 AND FR 70, Y765 RT; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472209; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 9-14, 16 & 17, PG 6, 7-10, & 12. 2L72 4F RTA28NM 20040305000552004030500055NM 2004 3 5 04FDEA00449 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000602004030500060NM 2004 3 5 04FDEA00454 120040219A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750- 74319, TITLE: WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040305000752004030500075NM 2004 3 5 04FDEA00466 120040220A5350 HINGE DOUG MD11 MD11 3023602NM TAIL CONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 AFT ACCESSORY COMPARTMENT, LT TAIL CONE LOWER HINGE FITTING SUPPORT FOUND CRACKED. AFT ACCESSORY COMPARTMENT, LT TAILCONE LOWER HINGE FITTING SUPPORT REPAIRED AS PER EA 1-5352-57900, FUSELAGE - TAILCONE/ ACTUATION PLATFORM - PART FABRICATION DEVIATION. CRACKED HINGE FITTING SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040305000832004030500083 2004 3 5 SWIA200412884 420040210A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AHRS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07965SW 7871 YAW DAMPER (YD) 1 TRIPPED OFF IN CRUISE. RESET (REPEATEDLY), GOT PROGRESSIVELY WORSE DOWN TO 2 SECONDS BETWEEN RESETS AND FAILS. ASSOCIATED: AP TRIPS OFF WITH YD1, AI NR 1 BLANKS OUT AND MAG FLAG APPEARS WITH YD1. VSI NR 1 ERRONEOUS INDICATIONS - SHOWS UP TO 1400 FPM DESCENT AND CLIMB WHILE IN LEVEL FLIGHT AND VSI NR 2 SHOWING 0 FPM UP/DOWN (IE LEVEL). STALL FAIL OCCURRED DESCENDING THROUGH 14,000 AT 3200. YD2 FAILED ON LANDING. REPLACED NR 1 AHRS COMPUTER. OPS CHECKS GOOD IAW CRJ MM 34-21-11. 2L72 4F4 FRTA21EA E15NE 20040308000042004030800004SO 2004 3 8 C2XA04IA012 120040215A3350 LIGHT EMB 145 EMB145 3260210SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714972 145151 DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHT ABOVE THE COCKPIT DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE POWER TO THE SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. 2L72 4F RTT00011AT 20040308000402004030800040EU 2004 3 8 MALA040200 120040211A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15511XJ E2325 DURING C-CHECK INSPECTION IN LCQ, LT FUSELAGE FRAME 20A STRINGER 17L HAS DENTS AND GOUGES. MAINTENANCE FABRICATED AND INSTALLED PERMANENT FUSELAGE REPAIR IAW MESABA EO A53133. A/C RELEASE DATE 2/20/04. 2H74 4F RTA49EU 20040308000422004030800042NM 2004 3 8 AWXA200400199 120040220A3350900835A BATTERY BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - EEL - DURING 4-DAY CHECK MAINTENANCE FOUND THE LT FORWARD AND MID CABIN SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT BATTERIES AT SEAT ROWS 4 AND 11, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040308000442004030800044NM 2004 3 8 AWXA200400201 120040222A3260893301 PROXIMITY SENSOR AIRBUSA319 A319132 3930340NM NLG DEFECTIVE A AWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28803AW 931 LAX - LANDING GEAR - FLT 0409 - ON DESCENT INTO LAX EN ROUTE FROM BOS WHEN LANDING GEAR WAS SELECTED DOWN, RECEIVED ECAM MESSAGE FOR LANDING GEAR NOT DOWN AND LOCKED. ALSO HAD 3 RED LIGHTS & LANDING GEAR DOOR OPEN INDICATIONS. RECYCLED LANDING GEAR HANDLE WITH SAME RESULT, THEN APPROXIMATELY 30 SECONDS LATER HAD NORMAL GEAR INDICATION. MAINTENANCE DOWNLOADED POST FLIGHT REPORT AND FOUND LGCIU NR 2 PROXIMITY SENSOR (39GA) TARGET POSITION MESSAGE. PER TSM 32-31-00-810-818, REMOVED AND REPLACED (SYSTEM 2) LT NOSE LANDING GEAR DOOR OPEN PROXIMITY SENSOR (39GA) IAW AMM 32-13-00-810-818, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20040308000532004030800053NM 2004 3 8 04FDEA00471 120040220A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 CORROSION (C53-111-01, 3) AFT CARGO BAY, ON STR 25R, BS 1045. REMOVED CORROSION ON AFT CARGO BAY ON STR 25R BS 1045, 1 INCH X 2 INCHES. MAXIMUM MATERIAL LOST .040. ORIGINAL THICKNESS .071. OUT OF LIMITS. CUT OUT STRINGER FROM BS 1040 TO BS 1060. FABRICATED REPAIR STRINGER AND HAT SECTION. ALODINED, PRIMED, PAINTED AND INSTALLED IAW SRM 51-10-6, SRM 53-10-1, SRM 53-10-3, SRM 51-30-2 FED EX MM 51-20-151-7. 2L73 4F RTA3WE 20040308000652004030800065SO 2004 3 8 C2XA04CL013 120040222A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2715572 145636 IAH FLIGHT 2611 THE CREW REPORTED THE RIGHT OVERWING UPPER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040308000722004030800072EU 2004 3 8 AWXA200400204 220040222A72301663M24P02 FAN BLADE BOEING737 73733A 1384673NM CFMINTCFM56 CFM562AFR 13802EU NR 2 ENGINE DAMAGED A AWXAK NONE C F.O.D. ININSP/MAINT 1 WP28164AW 23625 AUS - ENGINE FOD - DURING RON INSPECTION MAINTENANCE FOUND 33 FAN BLADES DAMAGED ON THE NR 2 ENGINE. SUSPECT DAMAGE WAS CAUSED BY MISSING ACOUSTIC LINER SCREWS. MAINTENANCE PERFORMED FOD INSPECTION IAW T/C I8M05030, BORESCOPED ENGINE IAW T/C I5M72025, REMOVED AND REPLACED ALL 38 FAN BLADES IAW T/C F5M72004 & S5M71001, AND PERFORMED SURVEY IAW T/C F1B77001. REPLACED DAMAGED INLET ACOUSTIC LINER PANELS AT 12:00, 1:00, 2:00, 6:00, 7:00, 8:00 O'CLOCK POSITIONS IAW MM 72-33-02. 2L72 4F4 FRTA16WE E21EU 20040308000772004030800077EU 2004 3 8 AWXA200400209 120040211A5315D53472188200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 10-12, PG 24, & 26- 28. 2L72 4F RTA28NM 20040308000812004030800081EU 2004 3 8 MALA040204 120040223A352011702803 SWITCH BAC 146 AVRO146RJ85A1500097EU OXYGEN SYS CONTAMINATED A MALAG O2 MASK DEPLOYED O OTHER TXTAXI/GRND HDL 1 GL15535XJ E2371 AFTER LANDING WHILE TAXIING TO GATE ALL PAX O2 MASKS IN CABIN DEPLOYED. INSPECTED NOTED LT FLT DECK PAX O2 OVERRIDE SWITCH CONTAMINATED WITH MOISTURE AND SHORTED OUT SWITCH. REPLACED SWITCH P/N S2802-002. ALSO NOTED 11AB, 13AB CHEMICAL O2 GENS ACTIVATED. REPLACED CANISTERS P/N 117028-03 11AB, S/N OFF NSN, S/N ON 9903986 13AB, S/N OFF NSN, S/N ON 9903984, SYS OPS TESTS GOOD. 2H74 4F RTA49EU 20040308000852004030800085SO 2004 3 8 C2XA04SH096 120040225A531014525480003 DOOR FRAME EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000892004030800089SO 2004 3 8 C2XA04SH100 120040225A716014575001405 INTAKE EMB 145 EMB145 3260210SO NR 1 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308000992004030800099NM 2004 3 8 04FDEA00519 120040225A5320 PLATE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 COCKPIT - ALUMINUM FLOOR BASE (PLATE) LOCATED BELOW FIRST OFFICER RIGHT CONSOLE CORRODED. ALUMINIUM FLOOR BASE (PLATE) LOCATED BELOW FIRST OFFICER RT CONSOLE CORROSION REMOVED BY HAND CLEAN AND REPROTECTED AS PER SRM 51-21- 01 VOL II. REWORK AREA FOUND WITHIN LIMIT AS PER SRM 53-00-01 VOL I. AREA PAINT TOUCHED UP AS PER SRM 51-21-01 VOL II. 2L73 4F RTA22WE 20040308001052004030800105NM 2004 3 8 04FDEA00511 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 0503, SHT 2. COMPLIED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001232004030800123EU 2004 3 8 AWXA200400214 120040211A5315D53472193200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y765 FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11 PG 1-2. 2L72 4F RTA28NM 20040308001292004030800129EU 2004 3 8 AWXA200400221 120040211A5315D53472189200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00 PG 5 & 6, TABLE 1. 2L72 4F RTA28NM 20040308001372004030800137NM 2004 3 8 ASAA0410034 120040114A53306545767 SKIN BOEING737 7372Q8C 138448SNM FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND SKIN PATH BELOW CARGO DOOR BENT. REPAIR IAW EA. (M) 2L72 4F A16WE 20040308001592004030800159NM 2004 3 8 ASAA0410017 120040108A53156554913505 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 947, LEFT BUTTOCK LINE 24.75, RIGHT BUTTOCK LINE 24.75 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040308001682004030800168NM 2004 3 8 ASAA0410019 120040112A533065458352 BEAR STRAP BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, REPLACED INTERIM REPAIR TO THE BEAR STRAP AT FUSELAGE STATION 259-277, LEFT BUTTOCK LINE 15.47. REPAIRED BEAR STRAP PER EA. (M) 2L72 4F A16WE 20040308001692004030800169NM 2004 3 8 ASAA0410020 120040112A5330654576943 SKIN PANEL BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE INTERNAL SKIN PANEL AT FUSELAGE STATION 382, STRINGER 28R-28L CORRODED. REPAIRED SKIN PANEL PER EA. (M) 2L72 4F A16WE 20040308001702004030800170NM 2004 3 8 ASAA0410021 120040112A54206570947 STRUCTURE BOEING737 7372Q8C 138448SNM NR 2 PYLON CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE NR 2 ENGINE PYLON AT FAIRING STATIONS 40 AND 62 CHAFED. REPAIRED PYLON PER EA. (M) 2L72 4F A16WE 20040308001712004030800171NM 2004 3 8 ASAA0410022 120040112A53476554968511 SEAT TRACK BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 370-446, RIGHT BUTTOCK LINE 45 PITTED AND GOUGED. REPLACED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040308001752004030800175NM 2004 3 8 ASAA0410006 120040106A53116545808524 FRAME BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, THE LOWER CHORD AT FUSELAGE STATION 294, STRINGER 25L HAD A FASTENER LOCATION TRIMMED OUT. REPAIRED LOWER CHORD PER EA. (M) 2L72 4F A16WE 20040308001762004030800176NM 2004 3 8 ASAA0410023 120040112A5315 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 727B, LEFT BUTTOCK LINE 60, RIGHT BUTTOCK LINE 41 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040308001772004030800177NM 2004 3 8 ASAA0410025 120040112A531565621571 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 360, RIGHT BUTTOCK LINE 19, RIGHT BUTTOCK LINE 52 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040308001792004030800179NM 2004 3 8 ASAA0410005 120040106A5347655496810 SEAT TRACK BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SEAT TRACK AT FUSELAGE STATION 480-520, RIGHT BUTTOCK LINE 25 CORRODED. REPAIRED SEAT TRACK PER SRM. (M) 2L72 4F A16WE 20040308001812004030800181NM 2004 3 8 ASAA0410009 120040107A53126941463506 FITTING BOEING737 7372Q8C 138448SNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE BULKHEAD FITTING AT FUSELAGE STATION 727, RIGHT BUTTOCK LINE 45.5 CRACKED. REPLACED FITTING PER EA. (M) 2L72 4F A16WE 20040308001822004030800182NM 2004 3 8 ASAA0410010 120040107A53156567140140 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, BUTTOCK LINE 0 CORRODED. REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040308001842004030800184NM 2004 3 8 ASAA0410013 120040107A533065458001 SKIN PANEL BOEING737 7372Q8C 138448SNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 350, STRINGER 24L DENTED. REPAIRED SKIN PANEL PER SRM. (M) 2L72 4F A16WE 20040308001862004030800186NM 2004 3 8 ASAA0410004 120040106A53156545833365 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 260, BUTTOCK LINE 0, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040308001882004030800188NM 2004 3 8 ASAA0410002 120040106A531565549055 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 480, RIGHT BUTTOCK LINE 5, RIGHT BUTTOCK LINE 59 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040308001892004030800189NM 2004 3 8 ASAA0410015 120040107A5315 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 540-727B, RIGHT BUTTOCK LINE 44 CORRODED. REPLACED FLOORBEAM PER SRM. (M) 2L72 4F A16WE 20040308001902004030800190NM 2004 3 8 ASAA04100012 120040107A55126573783503 SKIN BOEING737 7372Q8C 138448SNM HORIZ STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT STABILIZER STATION 156.55-159 GOUGED. REPAIRED HORIZONTAL STAB PER EA. (M) 2L72 4F A16WE 20040308001912004030800191NM 2004 3 8 ASAA0410011 120040107A531265458197 PRESSURE PANEL BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE PRESSURE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M) 2L72 4F A16WE 20040309000022004030900002EU 2004 3 9 MALA040192 120040209A302044730501 MODULE SAAB SF340 340B 7860101EU DE-ICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15424XJ 340B424 EN ROUTE TO STC W INBOARD LIGHT ILLUMINATED ON IT'S OWN FOLLOWED QRH LIGHT STAYED ON. AIR RETURN TO MSP. MAINTENANCE OHM CHECKED DUCT MATS AND THERMISTORS, OHM CHECKS GOOD. REMOVED AND REPLACED DEICE MODULE, PERFORMED 20 MIN OPS CHECKS, OPS CHECKS GOOD P/N 44730-501, S/N OFF A00072, S/N ON A00581. 2L72 4T RTA52EU 20040309000032004030900003EU 2004 3 9 MALA040193 120040214A3150006W500 WEU SAAB SF340 340B 7860101EU CENTRAL WARNING FAULTY A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15436XJ 340B436 DURING CLIMB, GOT A RT ENGINE FIRE ANNUNCIATOR FLICKERING AND A BITE LIGHT. AS PER MX DIRECTION, CYCLED CB'S E5, 6 AND L5. ALL LIGHTS WENT OUT WHEN CB'S WHERE PULLED BUT THE BITE LIGHT CAME BACK ON WHEN CB'S PUSHED IN. ON APPROACH THE BITE LIGHT THEN WENT OUT, NO OTHER ABNORMAL INDICATIONS. REPLACED WEU IAW AMM 31-50-05-4, OPS CHECK GOOD. P/N ON&OFF 006W500, S/N OFF 1596, S/N ON 1591. INSPECTED RIGHT FIRE WIRE, FOUND NO DISCREPANCIES. 2L72 4T RTA52EU 20040309000042004030900004EU 2004 3 9 MALA040189 120040206A2612 CONNECTOR SAAB SF340 340B 7860101EU FIRE WARNING CONTAMINATED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15441XJ 340B441 LEFT FIREBELL CAME ON FOR A SECOND, INFLIGHT. CRUISE FLT THE LEFT FIRE DETECT FAIL CWP CAUTION LIGHT REPEATEDLY CYCLED ON AND OFF IT WOULD GO OUT FOR 3 SECONDS AND COME BACK, QRH COMPLETE. MAINTENANCE FOUND CONTAMINATED CONNECTION AT ENGINE NACELLE. CLEANED AND SAFETIED OPS CHECK IAW SAAB 340 AMM CH 26-11. 2L72 4T RTA52EU 20040309000052004030900005EA 2004 3 9 04042653 120040211A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653BR 7438 DURING INSPECTION THE ANGLE CLIP AT FS 621 LONGERON 13 WAS FOUND CRACKED. THE ANGLE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4F RTA21EA 20040309000072004030900007EA 2004 3 9 04048677 120040217A33501314 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27677BR 7652 DURING INSPECTION THE RIGHT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040309000082004030900008EA 2004 3 9 04048426 120040217A3350321430 BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27426FJ 3190 DURING INSPECTION THE MIDDLE SECTION OF ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE BATTERY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION. 2L72 4F RTA21EA 20040309000102004030900010EA 2004 3 9 04048656 120040217A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27656BR 7485 DURING CLIMB OF FLIGHT 7375 CREW REPORTED A LAVATORY SMOKE INDICATION. THE SMOKE DETECTOR WAS FOUND TO BE PROVIDING A FALSE INDICATION AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000122004030900012EA 2004 3 9 04048640 120040217A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27640BR 7340 DURING INSPECTION THE RIGHT HAND AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040309000132004030900013EA 2004 3 9 04049710 120040218A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20040309000142004030900014NE 2004 3 9 MALA040168 220040204A7530216118218 BLEED BAND BAC 146 AVRO146RJ85A1500097EU GE CT7TP CT79B 30030NE NR 4 ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15505XJ E2313 ON CLIMBOUT AND LEVEL OFF THE EGT ON NR 4 ENGINE WAS CONTROLLED TO MAX CONTINUOUS POWER WITH N1 7 PERCENT LOWER THAN OTHER ENGINES INDICATIONS WERE IDENTICAL WHEN FADEC WAS TURNED OFF. N2 WAS ALSO SHOWING 3 PERCENT HIGHER. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 4 ENGINE BLEED BAND P/N 2-161-182-18, S/N ON 03246371277, P/N OFF 2-161-182-01, S/N OFF & UNKNOWN. 2H74 4F4 TRTA49EU E8NE 20040309000162004030900016EU 2004 3 9 04053303 120040222A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU EXTERIOR INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27303UE 41015 DURING INSPECTION THE RIGHT HAND EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4T RTA41NM 20040309000182004030900018EA 2004 3 9 04054673 120040223A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27673BR 7599 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING BETWEEN ROWS 9 THRU 12 WAS FOUND INOPERATIVE. A CONNECTOR WAS RESECURED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040309000202004030900020EA 2004 3 9 04051626 120040220A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE INDICATIONA VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27626BR 7225 DURING TAKEOFF CREW RECEIVED A LAVATORY SMOKE WARNING. CREW ABORTED TAKEOFF VERIFIED NO SMOKE WAS PRESENT AND FLIGHT CONTINUED UNEVENTFULLY. THE LAVATORY SMOKE DETECTOR WAS DEFERRED FOR FURTHER TROUBLESHOOTING. 2L72 4F RTA21EA 20040309000222004030900022EA 2004 3 9 04049687 120040218A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27687BR 7720 DURING INSPECTION THE AFT SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. A CONNECTOR WAS RESECURED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000232004030900023EA 2004 3 9 04050637 120040219A2752860D10018 PDU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAULTY A VTZAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 EA27637BR 7308 DURING APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE WITH FLAPS AT 37 DEGREES. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP POWER DRIVE UNIT AND FLAP ELECTRONIC CONTROL UNIT WERE FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000242004030900024EA 2004 3 9 04049710A 120040218A2750 ECU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FALSE ACTIVATIONA VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27710BR 7852 DURING APPROACH THE CREW REPORTED A FLAP FAIL MESSAGE AT 30 DEGREES. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. A SATISFACTORY OPERATIONAL CHECK OF THE FLAP SYSTEM WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000252004030900025EU 2004 3 9 AWXA200400222 120040211A5315D53472172201 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00 PG 5 & 6 TABLE 1. 2L72 4F RTA28NM 20040309000262004030900026WP 2004 3 9 AALA20040272 120040223A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21233AA 49180 DFW - CEILING EMERGENCY LIGHTS AT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040309000272004030900027NM 2004 3 9 AALA20040275 120040122A5330 SKIN BOEING757 757223 1384957NM FUSELAGE SCRATCHED A AALAK NONE O OTHER ININSP/MAINT 1 SW21637AM 24595 TUL - SCRATCH ON THE CROWN SKIN AT STATION 700 JUST INBOARD OF, AND ADJACENT TO, STRINGER 2L. AFTER SCRATCH WAS BLENDED THE DEPTH OF THE BLEND MEASURED 0.027 INCH. REPAIRED PER REPAIR DOUBLER ESO 90309. 2L72 4F RTA2NM 20040309000282004030900028NM 2004 3 9 AALA20040271 120040223A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21394AN 29431 JFK - EMERGENCY LIGHT AT SEAT 40H INOPERATIVE. FOUND CONNECTOR FOR EMERGENCY LIGHT LOOSE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040309000292004030900029EU 2004 3 9 AALA20040273 120040225A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217076A 610 MIA - EMERGENCY LIGHTS AT SEAT 32G INOPERATIVE. REPOSITIONED AND RESET CONNECTOR FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040309000302004030900030EU 2004 3 9 AALA20040276 120040219A5313 STRINGER AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - STRINGER 57 (BULK CARGO) CORRODED FROM FR65 TO FR67 IN AN AREA 0.5 BY 0.5 INCH AND A DEPTH OF 0.040 INCH. REPLACED STRINGER PER SRM 53-10-14. 2L72 4F RTA35EU 20040309000322004030900032NM 2004 3 9 AALA20040274 120040225A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21659AA 24617 MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHTS AT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040309000332004030900033WP 2004 3 9 CALA0400165 120040224A2797 WIRE DOUG DC9 DC982 3022082WP RUDDER SHORTED A CALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW2772825 49485 MACH TRIM INOP LIGHT ILLUMINATED AND AIRCRAFT BEGAN TO DUTCH ROLL AT 31,000 FEET EN ROUTE. QRH PROCEDURE COMPLETED, BUT NO CHANGE RESULTED. THERE WAS MINIMUM CONTROL WITH THE RUDDER. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE DFGS SW-B CIRCUIT BREAKER POPPED. TROUBLESHOOTING THE WIRING IAW MM 22-16-11 FOUND A SHORTED WIRE (RUDDER POSITION SENSOR WIRE, WIRE 2C610X22RD) IN TAIL COMPARTMENT BETWEEN S30-5 AND P10-429. THE WIRE WAS REPAIRED IAW STANDARD WIRING PRACTICES MANUAL 20-10-03. RUDDER WAS CHECKED FOR EXCESS FRICTION IAW MM 27-20-00 AND ALL CHECKED NORMAL. RETURN TO SERVICE TEST WAS PERFORMED ON NR 1 & 2 DFGS IAW MM 22-01-05 AND BOTH PASSED THE TEST. 2L72 4F A6WE 20040309000342004030900034NM 2004 3 9 QXEA200400174 120040219A33506104789 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09375PH11663332 529 SEA - ON FLIGHT 2281 EMERGENCY LIGHT CIRCUIT BREAKER IS TRIPPED AND POWER SUPPLY PS2, PS3, PS4, PS5 AND PS6 ARE DISCHARGED. REMOVED AND REPLACED ALL BATTERIES LISTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040309000352004030900035NM 2004 3 9 QXEA200400175 120040224A33506104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09360PH17182159 515 PDX - AFT UPPER EMERGENCY LIGHT AND AFT RIGHT HAND SIDE EGRESS LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED PS4 AND PS6 POWER SUPPLY. 2H72 4T RTA13NM 20040309000362004030900036SO 2004 3 9 C2XA04SH102 120040226A711014576631622 STIFFENER EMB 135 EMB135ER 3260203SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000372004030900037SO 2004 3 9 C2XA04SH103 120040226A711014576881043 SKIN EMB 135 EMB135ER 3260203SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE RIGHT HAND LOWER COWLING SKIN WAS FOUND TO BE CHAFED IN TWO AREAS BETWEEN STATIONS XN=2180.0 AND XN=2905.0. MAINTENANCE REMOVED THE DAMAGED AREAS AND PERFORMED DOUBLER REPAIRS IAW EMB 135 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000382004030900038SO 2004 3 9 C2XA04SH104 120040226A532013500469403 CROSSBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000402004030900040SO 2004 3 9 C2XA04SH106 120040226A532014521721009 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000422004030900042NM 2004 3 9 04FDEA00345 120040207A5753ARC050214 HINGE DOUG MD11 MD11F 3023600NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE RIGHT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040309000492004030900049NM 2004 3 9 AWXA200400228 120040211A532069774774 SUPPORT BOEING737 7373U3 13844CCNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 LCQ - MAJOR REPAIR - DURING C-5 CHECK CORROSION WAS FOUND MAIN CABIN FLOOR WEB SUPPORT AFT OF R-2 DOOR BETWEEN BS 986 AND BS 993, RBL 36 TO RBL 45. MAINTENANCE REMOVED CORRODED WEB SUPPORT FROM BS 986 TO BS 993, RBL 36 TO RBL 45; FABRICATED A NEW REPLACEMENT SUPPORT PER DWG 69-77477; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4. 2L72 4F RTA16WE 20040309000512004030900051NM 2004 3 9 AALA20040283 120040225A3350233T32101028 PANEL BOEING757 757223 1384957NM COCKPIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21655AA 24613 MEX - PREFLIGHT INSPECTION FOUND EMERGENCY -DISARMED- LIGHT INOPERATIVE. FERRIED FLIGHT FROM MEX TO MIA FOR REPAIR OF EMERGENCY LIGHT SWITCH. REPLACED EMERGENCY LIGHT PANEL ON COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040309000522004030900052 2004 3 9 AALA20040284 420040223A2565D31038201 SLIDE BOEING757 757223 1384957NM L1 DOOR FAILED A AALAK NONE O OTHER TXTAXI/GRND HDL 1 SW21660AM 25294 MIA - EMERGENCY ESCAPE SLIDE AT DOOR 1L FELL OFF ITS HOLDER AND DID NOT DEPLOY WHEN ARMED DOOR WAS OPENED. POWER ASSIST BOTTLE WAS BLOWN. JETBRIDGE WAS ATTACHED. REPLACED POWER ASSIST BOTTLE AND INSTALLED NEW SLIDE AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040309000532004030900053WP 2004 3 9 AALA20040281 120040225A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 ORD - OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040309000542004030900054WP 2004 3 9 AALA20040280 120040225A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21218AA 49168 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACKS FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040309000552004030900055NM 2004 3 9 AALA20040279 120040225A3350 CONNECTOR BOEING737 737823 13844BZNM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21906AN 29508 RDU - EMERGENCY PATH LIGHTS AT ROW 12D INOPERATIVE. SECURED LOOSE CONNECTOR AT PLUG FOR EMERGENCY PATH LIGHTS AT ROW 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040309000562004030900056NM 2004 3 9 AALA20040278 120040224A33500201991004 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21385AM 27059 LAX - EMERGENCY ESCAPE PATH LIGHTING AT SEAT 39H INOPERATIVE. REPLACED LAMP HOLDER ASSEMBLY FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040309000572004030900057NM 2004 3 9 AALA20040285 120040226A3350 COVER BOEING737 737823 13844BZNM CABIN DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21970AN 30096 MIA - RIGHT HAND AFT GALLEY ENTRY DOOR EMERGENCY LENS COVER AND BASE ASSEMBLY DAMAGED. REPLACED RIGHT HAND AFT GALLEY EMERGENCY EXIT DOOR LIGHTS ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040309000582004030900058WP 2004 3 9 AALA20040286 120040226A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21501AA 49738 DFW - EMERGENCY CEILING LIGHTS AT SEATS 7 THROUGH 10 INOPERATIVE. RELAMPED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEATS 7 THROUGH 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040309000622004030900062SO 2004 3 9 C2XA04BT022 120040220A33977287502611 WIRE HARNESS EMB 145 EMB145 3260210SO CABIN FAULTY A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2714960 145100 CREW REPORTED, SIDEWALL LAMP FLICKERING AND SMELL OF SMOKE IN SEAT 1A. MAINTENANCE REMOVED THE BULB AIRCRAFT RELEASED IAW MEL 33-20-00/1 CATEGORY-C ITEM CONTROL NUMBER 038985. AIRCRAFT ARRIVED EWR, MAINTENANCE REMOVED AND REPLACED HARNESS FOR LAMP INSERT SEATS 1A AND 2A, AND INSTALLED LAMP IAW EMB145 WM 33-21-50, OPS CHECKED GOOD. MEL REMOVED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040309000632004030900063EU 2004 3 9 MALA040214 120040225A3230HTE210014 ACTUATOR BAC 146 AVRO146RJ85A1500097EU LANDING GEAR FAILED A MALAO OTHER J WARNING INDICATION DEDESCENT 1 GL15533XJ E2367 UPON SELECTING LANDING GEAR DOWN GOT DISAGREEMENT LIGHT IN HANDLE AND NO GEAR DOWN IND AT THAT TIME GOT GREEN SYS HYD HI TEMP ON OVERHEAD PANEL. QRH'D GOT MAIN GEAR TO EXTEND WHEN SELECTING AC PUMP AND PTU AND NR 3 ENG PUMP OFF AND GOT NOSE GEAR TO EXTEND WHEN NR 3 ENG PUMP SW. TURNED BACK ON AND AC PUMP AND PTU SWITCHES TURNED BACK ON. REPLACED SELECTOR ACTUATOR IAW AMM 32-30-17. JACKED AC AND SWUNG GEAR SEVERAL TIMES. OPS CHECKS GOOD IAW 32-30-17 P/N HTE210014, S/N ON FRTR021AX, S/N OFF M253GB799. 2H74 4F RTA49EU 20040309000642004030900064NE 2004 3 9 MALA040209 220040218A7230 FAN BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 ENGINE SEIZED A MALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15531XJ E2365 NR 4 ENG 1ST START HOT, 2ND START HOT, GROUND PERSONNEL SAW NO ROTATION. QRH WAS FOLLOWED TEMP MAX 680 TRANSIENT. MX INSPECTED NR 4 ENG FOUND FAN SECTION SEIZED AND CHIP DETECTOR CONTAMINATED. INSTALLED 3 ENG FERRY KIT AS PER TASK CARD 3 ENG FERRY ON NR 4 ENG, A/C HAS BEEN INSPECTED AND FOUND SAFE FOR ONE TIME 3 ENG FERRY FROM DAY TO MSP. 2H74 4F4 FRTA49EU E6NE 20040309000662004030900066EU 2004 3 9 MALA040211 120040221A2751522858 INDICATOR SAAB SF340 340B 7860101EU COCKPIT FAULTY A MALAK NONE N FALSE WARNING APAPPROACH 1 GL15425XJ 340B425 WHEN PUTTING THE FLAPS DOWN FLAPS INDICATED A SPLIT POSITION. NO ABNORMAL AERODYNAMIC INDICATIONS. FOLLOWED SPLIT FLAP QRH. REMOVED AND REPLACED FLAP INDICATOR PER AMM 27-53-10-4, OPS CHECK GOOD PER 27-51-00. P/N ON/OFF 522858, S/N OFF 08870215, S/N ON 9703506. 2L72 4T RTA52EU 20040309000672004030900067EU 2004 3 9 MALA040205 120040205A5320 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15437XJ 340B437 FS 339 LEFT HD 11 INCHES BELOW STR SL1632 DENT FOUND TO BE OUT OF LIMITS. MX CUT OUT DAMAGED AREA FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53035. A/C RELEASE DATE 2/26/04. 2L72 4T RTA52EU 20040309000682004030900068NM 2004 3 9 AWXA200400229 120040226A33506104789 BATTERY PACK BOEING737 737277 1384570NM CARGO BAY DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - EEL - DURING 4-DAY CHECK FOUND THE L-1 & R-1 DOOR EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN FORWARD CARGO COMPARTMENT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040309000732004030900073EA 2004 3 9 04055643 120040224A27419960013 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB INTERMITTENT A VTZAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA27643BR 7363 DURING CLIMB OF FLIGHT 7624 CREW REPORTED A STABILIZER TRIM SYSTEM FAILURE. FLIGHT RETURNED TO FIELD AND LANDED UNEVENTFULLY. THE PITCH TRIM SWITCH WAS FOUND INTERMITTENT AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000742004030900074EA 2004 3 9 04056656 120040225A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA A/C BAY DIRTY A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27656BR 7485 DURING CLIMB OF 7790 CREW REPORTED A TOILET SMOKE MESSAGE. FLIGHT RETURNED TO FIELD AND LANDED UNEVENTFULLY. THE COALESCER BAG WAS FOUND DIRTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000752004030900075SO 2004 3 9 C2XA04IA017 120040223A792023065390 TUBE EMB 145 EMB145LR 3260212SO NR 1 ENGINE LEAKING A C2XAK NONE K FLUID LOSS CRCRUISE 1 SW2714950 145061 ON APPROACH INTO CUU THE NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE AIRCRAFT LANDED AT CUU WITHOUT INCIDENT WHERE THE AIRCRAFT WAS INSPECTED. THE OIL PRESSURE TUBE ASSEMBLY/REGULATING TEE, WAS FOUND TO BE LEAKING AND WAS REPLACED. THE NR 1 ENGINE OIL WAS SERVICED, LEAK CHECKED AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040309000762004030900076SO 2004 3 9 C2XA04SH113 120040227A33507287700509 CONTROL PANEL EMB 135 EMB135ER 3260203SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE EMERGENCY LIGHT PUSH BUTTON ON THE FLIGHT ATTENDANTS CONTROL PANEL WOULD NOT OPERATE THE EMERGENCY LIGHTING TEST. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANTS CONTROL PANEL IAW EMB 135 AMM II 25-27-09. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000862004030900086SO 2004 3 9 C2XA04SH123 120040227A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 1 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27125524321 4321 145583 SHV- DURING C-CHECK THE NR 1 ENGINE AIR INTAKE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000872004030900087SO 2004 3 9 C2XA04SH124 120040227A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000882004030900088SO 2004 3 9 C2XA04SH125 120040227A532014522460005 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000892004030900089SO 2004 3 9 C2XA04SH126 120040227A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000912004030900091EA 2004 3 9 SWIA200412898 120040112A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 193 LHS ELECTRICAL BAY FLOOR CRACKED. INSTALLED REPAIR IAW REO 601R-53-11-081 REV NC AND SKYWEST RII 53-401. 2L72 4F RTA21EA 20040309000932004030900093EA 2004 3 9 SWIA200412900 120040112A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 280 LT FLOORBEAM LBL 9.0 INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLES IAW CRJ SRM 51-40-11 AND CRJ REO 601R-53-11-171 REV NC (RII 53-401). P/N: 601R311011-73SA. 2L72 4F RTA21EA 20040308000552004030800055NM 2004 3 8 04FDEA00473 120040220A53116515938 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 FWD CARGO BAY FRAME IS DENTED BS 700 BETWEEN STR 24L & 25L. REMOVED DAMAGE AREA OF FRAME. FABRICATED REPAIR AND INSTALLED REPAIR IAW SRM 51-40-3. 2L73 4F RTA3WE 20040308000622004030800062NM 2004 3 8 04FDEA00495 120040220A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 WHILE WORKING FED EX WORK CARD, PUNCTURED BULKHEAD BS 227 LBL 21 WL 187. REPAIRED PUNCTURED BULKHEAD BS 227, LBL 21, WL 187 IAW SRM 51-40-2, 51-30-2 AND 51-10-2. 2L73 4F RTA3WE 20040308000842004030800084SO 2004 3 8 C2XA04SH095 120040225A532014522178005 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 21 AND 22. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040308001112004030800111NM 2004 3 8 04FDEA00505 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DWG ARC 0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001142004030800114NM 2004 3 8 04FDEA00502 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040308001212004030800121NM 2004 3 8 AWXA200400212 120040223A3510174660N5 OXYGEN MASK BOEING757 7572G7 1384963NM COCKPIT LEAKING A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28908AW7114 1553 24233 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CAPTAINS OXYGEN MASK WAS DEFECTIVE FRM 35-11-06-01. EMERGENCY, 100 PERCENT, AND NORMAL SELECTIONS ROTATE BEYOND EMERGENCY STOP VENTING MASK INTO COCKPIT AIR. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS OXYGEN MASK AND REGULATOR ASSEMBLY IAW BMM 35-11-51, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040308001252004030800125EU 2004 3 8 AWXA200400217 120040211A5315D53472094002 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOORBEAM Y512 LT, AT FR 66. MAINTENANCE REMOVED AND REPLACED CORRODED FLOORBEAM Y512 LT, AT FR 66 IAW A320 SRM 51-49-00 PG 5 & 6, TABLE 1. 2L72 4F RTA28NM 20040308001522004030800152NM 2004 3 8 ASAA0410027 120040113A53156554909501 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 807, LEFT BUTTOCK LINE 62.5- RIGHT BUTTOCK LINE 62.5 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040308001562004030800156NM 2004 3 8 ASAA0410032 120040114A53306545777 SKIN BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND REPAIR AT LEFT FUSELAGE SKIN AT STATION 907 AND STRINGER 10L REQUIRES REWORK. REPAIR IAW EA. (M) 2L72 4F A16WE 20040308001722004030800172NM 2004 3 8 ASAA0410024 120040112A53136545800114 STRINGER BOEING737 7372Q8C 138448SNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 24L AT FUSELAGE STATION 350 CRACKED. REPAIRED STRINGER PER SRM. (M) 2L72 4F A16WE 20040309000012004030900001EA 2004 3 9 04036629 120040205A76032100140007 GEARBOX CNDAIRCL600 CL6002B19 1900309EA RT ENGINE SEIZED A VTZAO OTHER O OTHER UKUNKNOWN 1 EA27629BR 7251 DURING FLIGHT THE CREW REPORTED THE RIGHT HAND ENGINE THROTTLE LEVER LOCKED UP. THE FLIGHT LANDED UNEVENTFULLY. THE THROTTLE GEARBOX ASSEMBLY WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000062004030900006EA 2004 3 9 04047637 120040216A5420 WEB CNDAIRCL600 CL6002B19 1900309EA RT NACELLE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27637BR 7308 DURING INSPECTION THE RIGHT HAND ENGINE SUPPORT BEAM LOWER OUTBOARD WEB WAS FOUND CRACKED. THE BEAM WAS TEMPORARILY REPAIRED IN ACCORDANCE WITH MANUFACTURERS DATA. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040309000602004030900060NM 2004 3 9 CALA0400174 120040226A53206945555Y9 SUPPORT FITTING BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2741135 29284 INSPECTION FOUND FORWARD CARGO DOOR CUTOUT LOWER SILL UPPER AFT SUPPORT FITTING CORRODED. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA2NM 20040309000652004030900065EU 2004 3 9 MALA040210 120040221A3412 PROBE SAAB SF340 340B 7860101EU EXTERIOR BIRD STRIKE A MALAK NONE O OTHER NRNOT REPORTED 1 GL15413XJ 340B413 BIRD STRIKE TO AIRCRAFT WAS DETERMINED TO BE MULTIPLE AREA OF IMPACT. COMPLETED GENERAL VISUAL INSPECTION OF THE AIRCRAFT EXTERIOR, LANDING GEAR, ALL FLT CONT BOTH ENG, PROPS. NOTED BIRD STRIKE TO RADOME. COMPLETED GENERAL INSPECTION OF AIRCRAFT. REMOVED & REPLACED TOTAL TEMP PROBE. CLEANED ALL BIRD STRIKE AREAS AND DETERMINED AIRCRAFT TO BE GOOD FOR SERVICE. 2L72 4T RTA52EU 20040309000702004030900070EU 2004 3 9 AWXA200400231 120040211A5313D53480047204 STRINGER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 31 RT, AFT OF FR 65. MAINTENANCE CUT OUT CORRODED AREA OF STRINGER 31 RT, AFT OF FR 65; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A SPLICE ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-13, FIG 201 PG 201-206. 2L72 4F RTA28NM 20040309000902004030900090SO 2004 3 9 C2XA04SH127 120040227A711014576631622 STRUCTURE EMB 145 EMB145LR 3260212SO RT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE RIGHT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309001002004030900100EA 2004 3 9 SWIA200412907 120040112A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 559 RT VERTICAL BEAM RBL 9 INBOARD & OUTBOARD LWR FLANGES CRACKED. BEAM REPAIRED IAW CRJ REO 601R-53-41-057 REV NC, RII 53-401. 2L72 4F RTA21EA 20040309001012004030900101EA 2004 3 9 SWIA200412908 120040112A5260 BRACKET CNDAIRCL600 CL6002B19 1900309EA PA X DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 PASSENGER DOOR CUTOUT LWR SILL AFT BRACKET ASSY FOR AIR STAIR HINGE ARM CORRODED. REPLACED BRACKET ASSY IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20040309001022004030900102EA 2004 3 9 SWIA200412909 120040112A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 409 + 128 LT VERTICAL BEAM LBL 27 LWR INBOARD FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401. 2L72 4F RTA21EA 20040309001042004030900104EA 2004 3 9 SWIA200412911 120040112A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 409 + 128 RT VERTICAL BEAM RBL 27 LWR INBOARD FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401. 2L72 4F RTA21EA 20040309001062004030900106EA 2004 3 9 SWIA200412913 120040112A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 SEAT TRACKS FS 409 + 128 AND FS 559 LBL 9 AND RBL 9 CORRODED. RT SEAT TRACK REPLACED IAW CRJ SRM 51-40-11, 51-41-02, 51-42-04. INSTALLED NEW LT SEAT TRACK IAW SRM 51-41-02, 51-41-04. P/N: 601R31032-7. 2L72 4F RTA21EA 20040309001092004030900109SO 2004 3 9 C2XA04SH129 120040229A532014525381001 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE LEFT BUTTSTRAP AT FRAME 65 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309001122004030900112WP 2004 3 9 AALA20040289 120040229A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21569AA 49351 MSP - OVERHEAD EMERGENCY LIGHTS AT ROWS 18-21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040309001132004030900113NM 2004 3 9 AALA20040290 120040229A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21653A 24611 LAX - FIRST CLASS AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS AREA EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040309001142004030900114NM 2004 3 9 AALA20040291 120040227A33501721651 CONNECTOR BOEING767 767323 1385205NM CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW217375A 25202 SFO - EMERGENCY LIGHT AT 37H INOPERATIVE. REPLACED CONNECTOR AT FOR EMERGENCY LIGHT AT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040309001152004030900115WP 2004 3 9 AALA20040292 120040227A3350 MODULE DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21572AA 49458 ORD - EMERGENCY PATH SEAT LIGHTING FROM SEATS 20D-29D IS DIM. REPLACED MODULE AND BATTERY FOR EMERGENCY PATH SEAT LIGHTING FROM SEATS 20D-29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040309001162004030900116WP 2004 3 9 GTIA040056 120040112A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND CORROSION ON RIGHT CUSP WEB FS 1193-1212 RIGHT. CUT OUT DAMAGED AREA. FABRICATED NEW DOUBLER REPAIR. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20040309001172004030900117WP 2004 3 9 GTIA040057 120040114A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND BROKEN INSERT AND DELAMINATION, CABIN FLOORBOARD FS 1140. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20040309001182004030900118 2004 3 9 GTIA040051 420040205A2565 LANYARD DOUG DC9 DC983 3022083WP EVAC SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FLL - FOUND R1 DOOR EVACUATION SLIDE LANYARD LOOSE. REINSTALLED R1 DOOR EVACUATION SLIDE LANYARD. (M) 2L72 4F RTA6WE 20040309001192004030900119WP 2004 3 9 GTIA040065 120040108A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 218 RIGHT SIDE OUTBOARD SEAT TRACK CORRODED. REMOVED SEAT TRACK RIGHT OUTBOARD STATION 200-247. FABRICATED NEW SECTION OF SEAT TRACK RIGHT OUTBOARD STATION 200-247. INSTALLED NEW SEAT TRACK. (M) 2L72 4F A6WE 20040309001212004030900121WP 2004 3 9 GTIA040068 120040114A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL STATION 1225 LEFT DETERIORATING NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040309001222004030900122WP 2004 3 9 GTIA040069 120040118A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CORROSION ON FLOORBOARD STATION 826 TO 1003 RBL 44 TO 54. UPON FURTHER INVESTIGATION CRACK FOUND AROUND SCREW HOLE. FABRICATED DOUBLER AND REMOVED CRACK. INSTALLED DOUBLER AND FILLER. (M) 2L72 4F A6WE 20040309001232004030900123WP 2004 3 9 GTIA040070 120040106A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND AFT LEFT STATION 1221-1287 SUB FLOOR WEB CRACKED. SUBFLOOR STATION 1221-1287, REMOVED AND REPLACED. (M) 2L72 4F A6WE 20040309001242004030900124WP 2004 3 9 GTIA040071 120040106A5320 ATTACH FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND AFT PIT LEFT STATION 1250-1271 SUBFLOOR CORRODED AT FLOORBEAM TO FUSELAGE ATTACH FITTING. FOUND THE FUSELAGE ATTACH FITTING AT STATION 1258 OUT OF LIMITS. REMOVED SUBFLOOR STATION 1250-1287. FABRICATED REPLACEMENT SUBFLOOR. LOCATED AND DRILLED REPLACEMENT FUSELAGE ATTACH FITTING. INSTALLED SUBFLOOR. INSTALLED REPLACEMENT FUSELAGE ATTACH FITTING. (M) 2L72 4F A6WE 20040309001252004030900125WP 2004 3 9 GTIA040072 120040108A5320 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND RIGHT AFT LAVATORY STATION 1322 STRINGER 18R FITTING CORRODED. REMOVED CORRODED FITTING. LOCATED, DRILLED AND INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20040309001262004030900126WP 2004 3 9 GTIA040073 120040107A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD FORWARD LAVATORY STATION 200-256 CRACKED IN SEVERAL AREAS. COMPOSITE SUPPORT CRACKED ON AFT END. REPAIRED CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040309001282004030900128WP 2004 3 9 GTIA040075 120040113A5321 SUPPORT DOUG DC9 DC981 3022081WP FLOOR PANEL CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOOR PANEL STATION 1174-1250 HAS CRACKED FLOOR SUPPORT. REPAIRED CRACKED FLOOR SUPPORT ON FLOOR PANEL. (M) 2L72 4F A6WE 20040309001292004030900129WP 2004 3 9 GTIA040076 120040107A5310 DOOR FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CORROSION ON JAMB BEAM BETWEEN FS 636-693 AROUND RIVETS AND DRILLED OFF SCREWS. FABRICATED 15 DOUBLER AND 9 SPACER. INSTALLED DOUBLER AND SPACER. (M) 2L72 4F A6WE 20040309001302004030900130WP 2004 3 9 GTIA040077 120040115A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL STATION 320-370 EDGES SPLIT-CRUSHED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040309001312004030900131WP 2004 3 9 GTIA040078 120040108A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CRACKED FRAME AT FS 1338 AND LONGERON 18R. CUT OUT DAMAGED AREA. FABRICATED FRAME SECTION AND REPAIR DOUBLER. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20040309001322004030900132WP 2004 3 9 GTIA040079 120040114A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL HAS CORROSION AT EDGES AND FAST HOLES, END OF STIFFENER CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR. INSTALLED REPAIR. (M) 2L72 4F A6WE 20040309001332004030900133WP 2004 3 9 GTIA040080 120040106A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CORROSION AND GOUGES ON SEAT TRACK STATION 788 TO 1309 RBL 44. REMOVED OUT OF LIMIT SEAT TRACK. FABRICATED REPLACEMENT SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F A6WE 20040309001352004030900135WP 2004 3 9 GTIA040083 120040115A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD STATION 1200, RBL 24-44 PEELING FIBERGLASS 349. REQUIRES EDGE FILLER. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040309001392004030900139WP 2004 3 9 GTIA040060 120040108A5320 PAN DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CARGO DOOR PAN HAS CORROSION AND CORRODED FASTENERS STATION 370-427 AND IS GOUGED AT STATION 379, DOOR STOP FITTINGS. CUT OUT DAMAGED. FABRICATED 04 EACH ANGLES. LOCATED AND DRILLED HOLES IN NEW FORWARD CARGO DOOR PAN. INSTALLED NEW FORWARD CARGO DOOR PAN. (M) 2L72 4F A6WE 20040309001402004030900140WP 2004 3 9 GTIA040061 120040106A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CORROSION ON SEAT TRACK STATION 788 TO 1309 LBL 24. REMOVED SEAT TRACK FROM LBL 24 STATION 936 TO 1309. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F A6WE 20040309001412004030900141WP 2004 3 9 GTIA040062 120040106A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND AFT PIT RIGHT STATION 1221-1287 SUB FLOOR WEB CRACKED. FABRICATED WEB. INSTALLED WEB. (M) 2L72 4F A6WE 20040309001422004030900142WP 2004 3 9 GTIA040063 120040106A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CORROSION AND GOUGES ON SEAT TRACK STATION 788 TO 1309 LBL 44. CUT OUT SEAT TRACK SECTION FROM STATION 1106-1309. LOCATED AND DRILLED TWO SECTION OF SEAT TRACK FROM STATION 1106-1183. LOCATED AND DRILLED TWO SEAT TRACK SPLICES. INSTALLED SEAT TRACK. (M) 2L72 4F A6WE 20040309001432004030900143WP 2004 3 9 GTIA040064 120040106A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CORROSION AND GOUGES ON SEAT TRACK STATION 788 TO 1309 RBL 24. REMOVED SEAT TRACK DAMAGED STATION 927 TO 1309. FABRICATED SEAT TRACK SPLICES. INSTALLED SEAT TRACK. (M) 2L72 4F A6WE 20040309001452004030900145WP 2004 3 9 GTIA040095 120040106A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND NLG WHEEL WELL CUTOUT AFT FRAME CORRODED AND CRACKED AT DOOR LANDING. REMOVED NLG WHEEL WELL AFT FRAME. LOCATED AND DRILLED NEW AFT FRAME. INSTALLED NEW AFT FRAME. (M) 2L72 4F A6WE 20040309001692004030900169WP 2004 3 9 GTIA040092 120040107A5230 FITTING DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND MID PIT DOOR AFT LOWER DOOR PAN AND ATTACH FITTING CRACKED AT DOOR STOP. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20040309001702004030900170WP 2004 3 9 GTIA040086 120040108A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND RIVETS PULLED THROUGH FLOORBOARD STATION 826 LBL 44 TO 54. UPON FURTHER INVESTIGATION FLOORBOARD STATION 826 LBL 44 TO 54 FOUND TO HAVE NUMEROUS BLOWN OUT HOLES, CRACKS, AND DELAMINATION. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20040309001712004030900171 2004 3 9 GTIA040087 420040116A2565D29982113 SLIDE DOUG DC9 DC981 3022081WP L1 DOOR UNSECURE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND L1 DOOR SLIDE IS COMING UNPACKED. REPLACED L1 DOOR SLIDE. (M) 2L72 4F A6WE 20040309001722004030900172WP 2004 3 9 GTIA040089 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW FOUND CABIN FLOORBOARD, RIGHT INBOARD STATION 180-200 SEVERAL INSERTS MISSING. PEELING FIBERGLASS REQUIRES EDGE FILLER. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040309001732004030900173WP 2004 3 9 GTIA040090 120040108A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD LEFT AFT FS 1257 SURFACE DELAMINATED MISSING INSERT. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040309001742004030900174WP 2004 3 9 GTIA040091 120040114A33505820A LIGHT DOUG DC9 DC981 3022081WP G4 GALLEY BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND G4 GALLEY HAS BROKEN EXIT LIGHT. REMOVED OLD BROKEN EXIT LIGHT. INSTALLED NEW EXIT LIGHT. (M) 2L72 4F A6WE 20040309001752004030900175WP 2004 3 9 GTIA040084 120040108A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND SCREW HEAD PULLED THROUGH FLOORBOARD STATION 250 LBL 44, AND PANEL CRACKED AT HOLE. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040309001762004030900176WP 2004 3 9 GTIA040093 120040113A5320 WEB DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CRACK IN SUBFLOOR PAX CABIN ENTRY AT FS 161, 24 INCHES LBL. REMOVED DAMAGED SUBFLOOR AREAS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040309001772004030900177WP 2004 3 9 GTIA040055 120040109A5320 TRIPLER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND MID CARGO DOOR JAMB BEAM CORRODED. REMOVED TRIPLER AFTER FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR TRIPLER. INSTALLED TRIPLER. (M) 2L72 4F RTA6WE 20040310000012004031000001NM 2004 3 10 UPS04241932 120040204A5712 RIB BOEING727 72722C 138400FNM WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLACED IAW SRM 51-30-2 & SPOILER OPERATION WITH STOP TESTED SATISFACTORY IAW MM 27-61-00. 2L73 4F A3WE 20040310000032004031000003NM 2004 3 10 UPS04241937 120040206A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C PARTIAL REPLACEMENT OF SKIN LOCATED AT BS 360-390 S4L-4R. REPLACED IAW UPS AUTHORIZATION B727-5330-19967-A. 2L73 4F A3WE 20040310000042004031000004NM 2004 3 10 UPS04241939 120040121A53206569742 FITTING BOEING727 72722C 138400FNM RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C RIGHT MLG WHEEL WELL, EVIDENCE OF CORROSION ON BS 870 FITTING O/B FLANGE AREA ABOVE STR 18A. FITTING REPLACED IAW DWG65C23231 AND 2BOF65-72710 AND UPS EO B727-5310-3056G. 2L73 4F A3WE 20040310000052004031000005NM 2004 3 10 UPS04241940 120040122A5320 BEAM BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C PRESENCE OF INTERGRANULAR CORROSION FOUND ON VARIOUS HOLES AND THE LOWER I-BEAM AT BS 1110 RBL 31 AS MARKED. REPAIRED IAW UPS AUTHORIZATION B727-53-21034. 2L73 4F A3WE 20040310000082004031000008EU 2004 3 10 UPS04141934 120040216A2560 POWER SUPPLY AIRBUSA300 A300F4622R 3930360EU CABIN MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01125UP 0809 INSPECTION TYPE:PFLT DOOR CABIN ESCAPE SLIDE WARNING LIGHT DID NOT TEST DURING PREFLIGHT. RESET AUTONOMOUS STANDBY POWER SUPPLY UNIT, WARNING LIGHT TESTS NORMALLY. 2L72 4F RTA35EU 20040310000142004031000014WP 2004 3 10 AALA20040294 120040228A3350P4010051111 CHARGER DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21572AA 49458 ORD - LAST ROWS OF EMERGENCY LIGHTS REMAIN ON WHEN A/C IS POWERED DOWN. REPLACED BATTERY PACK AND CHARGER FOR AFT SEAT LIGHTS AB-5. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040310000172004031000017WP 2004 3 10 AALA20040298 120040301A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21466AA 49596 DFW - RIGHT AFT EMERGENCY OVERWING EXIT LIGHT AT KNEE LEVEL FORWARD OF AFT RIGHT HAND OVERWING EXIT DOOR IS DIM. REPLACED THE UPPER CONTROL MODULE AND BATTERY PACK AT STATION 850 FOR RIGHT AFT EMERGENCY OVERWING EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040310000182004031000018NE 2004 3 10 AALA20040299 220040222A7230 COMPRESSOR BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE LT ENGINE STALLED A AALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW21782AN 30003 51238 JFK - INFLIGHT T0167/22 AT 175K LEFT HAND ENGINE COMPRESSOR STALLED WITH LOUD BANG AND AIRCRAFT YAW. FIVE SECONDS LATER SECOND COMPRESSOR STALL AND ENGINE STARTED TO ROLL BACK. ENGINE THRUST LEFT APPEARED MOMENTARILY. THROTTLE REDUCED AND STALL CLEARED. THE ENGINE THEN RAN NORMALLY. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE IN ACCORDANCE WITH WORKCARD 71-94-05 AND ACCOMPLISHED ENGINE CHANGE RUN-UP PER WORKCARD 71-95-19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTT00001SEE00050EN 20040310000192004031000019WP 2004 3 10 AALA20040297 120040301A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21466AA 49596 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 11D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040310000202004031000020WP 2004 3 10 AALA20040300 120040301A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21552AA 53034 DFW - CEILING EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040310000232004031000023NM 2004 3 10 AALA20040303 120040302A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21797AN 30012 DFW - EMERGENCY ESCAPE PATH AISLE LIGHTING AT 3R DOOR BATTERY LOW. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH AISLE LIGHTING AT 3R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040310000252004031000025EU 2004 3 10 AALA20040305 120040224A5320 SPLICE AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - STRINGER SPLICE AT STRINGER 51 RIGHT AND FRAME 71 HAVE 0.5 BY 0.5 INCH CORROSION AT DEPTH 0.030. INSTALLED NEW STRINGER SPLICE AT FRAME 71 PER SRM 51-75-10-2. 2L72 4F RTA35EU 20040310000262004031000026NM 2004 3 10 AALA20040308 120040220A5751113T1552 HINGE FITTING BOEING767 767323 1385205NM AILERON CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21378AN 25447 AFW - RIGHT HAND AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED WAS 1.24 INCHES AND FINAL MEASUREMENT IS 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PERMANENT REPAIR (CUP). REPAIR ANGLE (CUP) FABRICATED AND FASTENED TO AILERON RIB TO PROVIDE SUPPORT FOR FIXED TRAILING EDGE PANEL STIFFENER PER MRB 767-2560 DATED 2/18/04. 2L72 4F RTA1NM 20040310000282004031000028EU 2004 3 10 AALA20040306 120040224A5320 SPLICE AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - STRINGER SPLICE AT STRINGER 51 LEFT AT FRAME 71 HAS CORROSION AREA OF 0.5 BY 0.5 WITH A DEPTH OF 0.025. INSTALLED NEW STRINGER SPLICE AT STRINGER 51 AT FRAME 71 PER SRM 51-75-10-2. 2L72 4F RTA35EU 20040310000292004031000029NM 2004 3 10 AWXA200400232 120040228A335032145410 EPSU AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28816AW12228 1350 CMH - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT OVERWING EMERGENCY EXITS. MAINTENANCE REMOVED AND REPLACED RT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040310000302004031000030EU 2004 3 10 AWXA200400216 120040211A5315D53472172203 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1732 LT, FORWARD OF FR 68. UPON FURTHER EVALUATION CORROSION WAS FOUND ON 2 EACH REPAIR FILLERS. MAINTENANCE REMOVED CORRODED FILLERS ON FLOORBEAM Y1732 LT, FORWARD OF FR 68; FABRICATED 2 EACH REPLACEMENT REPAIR FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 51-41-14, FIG 201, PG 207-208, & 211-212. CORROSION LEVEL CHANGED FROM LEVEL 2 TO LEVEL 1 DUE TO PREVIOUS REPAIR. 2L72 4F RTA28NM 20040310000322004031000032SO 2004 3 10 C2XA04BT028 120040228A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2722909 145459 CREW REPORTED, FOUL SMELL THROUGHOUT CABIN AND FLIGHT DECK DURING ICE TEST, WENT AWAY AFTER TEST WAS COMPLETE. MAINTENANCE INSPECTED AIRCRAFT, OPS CHECKED ICE TEST SYSTEM IAW EMB145 MM 36-00-00. NO SMELL NOTED. 2L72 4T RTT00011AT 20040310000332004031000033SO 2004 3 10 C2XA04BT024 120040226A33501317 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711526 145410 CREW REPORTED TWO OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE RELAMPED BOTH EMERGENCY LIGHTS. OPS CHECKED BOTH GOOD IAW EMB135 MM 33-00-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040310000342004031000034SO 2004 3 10 C2XA04IA020 120040301A32201170C0000002 LANDING GEAR EMB 145 EMB145LR 3260212SO NLG UNDERSERVICED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714991 145278 DURING CLIMB THE CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE NOSE LANDING GEAR WAS UNDERSERVICED. THE LANDING GEAR WAS SERVICED AND THE AIRCRAFT TEST-FLOWN. THE TEST FLIGHT WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040310000392004031000039SO 2004 3 10 C2XA04BT025 120040226A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714998 145302 DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT ROW EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE RESECURED NR 3 EMERGENCY LIGHT BATTERY TO EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040310000462004031000046NM 2004 3 10 SWAA040544 120040221A21216454051 FAN BOEING737 7373T5 1384608NM FWD GALLEY FAULTY A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29694SW 23061 DURING CRUISE F/A REPORTS STRONG ACRID SMELL IN FORWARD GALLEY. GALLEY POWER WAS REMOVED SMELL WENT AWAY. REMOVED AND REPLACED RECIRC FAN PER MM. 2L72 4F RTA16WE 20040310000482004031000048NM 2004 3 10 SWAA040546 120040222A2560PH22300L STRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20040310000502004031000050NE 2004 3 10 SWAA040484 220040216A7320RP23500 SENSOR BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B22 13802NE NR 2 ENGINE FAULTY A SWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW29741SA 29277 AIRTURN BACK, DECLARED EMERGENCY, ON CLIMB-OUT NR 2 ENGINE SURGED BETWEEN 77 PERCENT AND 88 PERCENT N1. RETURNED TO BDL WITH NR 2 ENGINE AT IDLE. INSPECT ALL 3 CHIP DETECTORS, INTAKE AND EXHAUST. BORESCOPED ENGINE PER MM. PERFORMED EEC BITE CHECK FOUND FIT CODES 73-30902 AND 73-20812. REMOVED AND REPLACED T12 SENSOR PER MM. 2L72 4F4 FRTA16WE E00055EN 20040310000512004031000051NM 2004 3 10 SWAA040486 120040216A53306545819 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACK AT BS 245 BELOW FORWARD RT PRESSURE PANEL. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040310000522004031000052 2004 3 10 SWAA040487 420040216A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040310000532004031000053 2004 3 10 SWAA040488 420040216A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 L1 DOOR EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040310000542004031000054NM 2004 3 10 SWAA040489 120040216A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040310000582004031000058 2004 3 10 SWAA040493 420040216A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040310000602004031000060NM 2004 3 10 SWAA040495 120040217A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN CRACKED AT LT WHEEL WELL. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000622004031000062 2004 3 10 SWAA040498 420040217A2565D31354 SLIDE BOEING737 737301 1384611NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040310000652004031000065NM 2004 3 10 SWAA040502 120040217A32106549442 FITTING BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND LT MLG STABILIZER FORWARD FITTING CORRODED. REMOVED AND REPLACED LT MLG FORWARD FITTING PER BAC DRAWING. 2L72 4F RTA16WE 20040310000662004031000066NM 2004 3 10 SWAA040503 120040217A57206545326 WEB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND LT WING FSS 223, INBOARD OF FITTING (D) CRACKED AT WEB CHORD. REMOVED AND REPLACED WEB CHORD PER SRM AND ER. 2L72 4F RTA16WE 20040310000702004031000070NM 2004 3 10 SWAA040507 120040218A2530112251 COFFEEMAKER BOEING737 7377H4 1384404NM AFT GALLEY FAULTY A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29774SW 27882 F/A REPORTED SMELLING SMOKE IN AFT GALLEY AREA. TRACED ELECTRICAL BURNT ODOR TO COFFEEMAKER. PULLED COFFEEMAKER CB NO FURTHER ODOR. REMOVED AND REPLACED NR 2 COFFEEMAKER PER MM. 2L72 4F RTA16WE 20040310000712004031000071NM 2004 3 10 SWAA040508 120040218A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STRINGER 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000752004031000075NM 2004 3 10 SWAA040512 120040218A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, LBL 9 TO LBL 11, WL 234. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040310000762004031000076NM 2004 3 10 SWAA040513 120040218A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 FUSELAGE SKIN CRACKED BETWEEN BS 486 AND BS 500D, STRINGER 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000772004031000077NM 2004 3 10 SWAA040514 120040218A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STRINGER 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000782004031000078 2004 3 10 SWAA040515 420040218A2565D31354 SLIDE BOEING737 7373T5 1384608NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040310000802004031000080NM 2004 3 10 SWAA040485 120040216A3040286A2006001 COIL BOEING737 7377H4 1384404NM L2 WINDOW ARCED A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29412WN 29818 DIVERSION, WIRE BUNDLE CONNECTING CAPTAINS SIDE WINDOW HEAT WAS ARCHING AND BURNING. REMOVED AND REPLACED CAPTAINS WINDOW HEAT COIL PER MM. THIS IS AN AMENDED SDR ORIGINALLY SUBMITTED 02-17-04, REFLECTING A CORRECTED MFG PART NUMBER. 2L72 4F RTA16WE 20040310000812004031000081NM 2004 3 10 SWAA040518 120040219A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BS 482B + 17, STRINGER 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000832004031000083NM 2004 3 10 SWAA040520 120040219A57546573714 SKIN BOEING737 7372H4 138448CNM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT LOWER SKIN. REPAIRED NR 2 L/E SLAT PER RA. 2L72 4F A16WE 20040310000852004031000085NM 2004 3 10 SWAA040522 120040219A33501000679 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040310000862004031000086NM 2004 3 10 SWAA040523 120040219A335090083 BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED PM CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040310000872004031000087NM 2004 3 10 SWAA040524 120040219A33501000679 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED A1 CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040310000892004031000089NM 2004 3 10 SWAA040526 120040219A53306545700 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND CRACKS IN FUSELAGE SKIN AT BS 727E + 3, STRINGER 18R, AND BS 924, STRINGER 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000922004031000092NM 2004 3 10 SWAA040529 120040219A57536546435 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20040310000942004031000094NM 2004 3 10 SWAA040666 120040302A3350100067 LIGHT BOEING737 7372H4 138448CNM CABIN INTERMITTENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EMERGENCY EXIT LIGHT FLICKERING. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20040310000952004031000095 2004 3 10 SWAA040667 420040302A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040310000972004031000097 2004 3 10 SWAA040669 420040229A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20040310000982004031000098NM 2004 3 10 SWAA040670 120040302A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C4 CHECK, FOUND 3 IN LONG FUSELAGE SKIN CRACK AT BS 769, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040310000992004031000099NM 2004 3 10 SWAA040671 120040302A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM PANEL CRACKED BETWEEN BS 660 AND BS 724. REPAIRED KEEL BEAM PANEL PER SWA EA. 2L72 4F RTA16WE 20040310001002004031000100NM 2004 3 10 SWAA040672 120040302A531165C22908 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 25L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040310001032004031000103NM 2004 3 10 SWAA040675 120040302A55516551574 FITTING BOEING737 7373A4 1384585NM HORIZ STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION, LEFT AND RIGHT AFT SPAR CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER SRM. 2L72 4F RTA16WE 20040310001042004031000104 2004 3 10 SWAA040653 420040301A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F A16WE 20040310001052004031000105NM 2004 3 10 SWAA040654 120040229A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED A1 CHECK, FOUND 3 IN LONG FUSELAGE SKIN CRACK BETWEEN BS 500 -500A, STRINGER 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310001062004031000106NM 2004 3 10 SWAA040655 120040301A326065C2018 SWITCH BOEING737 7375H4 138449DNM NLG FAULTY A SWAAK NONE J WARNING INDICATION CLCLIMB 1 SW29528SW 26570 NOSE LANDING GEAR UNSAFE LIGHT INDICATION AFTER TAKE OFF. REMOVED AND REPLACED S845 SWITCH PER MM. 2L72 4F RTA16WE 20040310001072004031000107NM 2004 3 10 SWAA040656 120040301A53106547978 CREASE BEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 727B+. REPAIRED RT CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040310001092004031000109NM 2004 3 10 SWAA040658 120040301A534065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040310001102004031000110NM 2004 3 10 SWAA040660 120040301A53116546530 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 460, BETWEEN STRINGERS 26L AND 27L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040310001112004031000111NM 2004 3 10 SWAA040661 120040229A53306545760 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT LAP SEAM, BS 540, STRINGER 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040308000742004030800074EU 2004 3 8 AWXA200400206 120040211A5320D5347112420000 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT OUTBOARD SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AT STR 23 RT. MAINTENANCE REMOVED CORRODED RT OUTBOARD SHEAR PLATE WEB BETWEEN FR 69 AND FR 70, AT STR 23 RT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8 & 53 PG 7, 9, 22 & 28. 2L72 4F RTA28NM 20040308000792004030800079EU 2004 3 8 AWXA200400211 120040211A5320D53480048203 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND IN R-2 DOOR ENTRY WAY SHAPE SILL BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED DAMAGED R-2 DOOR SHAPE SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3 & 8 PG 7-9 & 22. 2L72 4F RTA28NM 20040308001072004030800107NM 2004 3 8 04FDEA00509 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20040308001122004030800112NM 2004 3 8 04FDEA00504 120040223A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHT 4. COMPLIED AS PER EA 1-5740-74323, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSY CORROSION. 2L73 4F RTA22WE 20040308001222004030800122EU 2004 3 8 AWXA200400213 120040224A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28652AW 953 PHX - EEL - DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1 LT AND 11 RT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED WIRE HARNESSES AT SEAT ROWS 1 LT AND 11 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040308001342004030800134WP 2004 3 8 ASAA0480064 120040201A33500105606 CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 1. REPLACED LIGHT MODULE CONNECTOR SOCKET. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040308001382004030800138WP 2004 3 8 ASAA0480043 120040129A335060030451 BATTERY DOUG DC9 DC983 3022083WP COCKPIT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01974AS 53450 ANC PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN TURNED ON. REPLACED ASSOCIATED BATTERY ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040308001572004030800157NM 2004 3 8 ASAA0410031 120040114A53156554906501 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OAK - DURING SCHEDULED D-CHECK, FOUND CABIN FLOORBEAM AT STATION 500A TOP SIDE CORRODED FROM RBL 4 TO RBL 23. REPAIR IAW EA. (M) 2L72 4F A16WE 20040308001732004030800173NM 2004 3 8 ASAA0410008 120040106A53306545769 SKIN PANEL BOEING737 7372Q8C 138448SNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 440-455, STRINGER 25R DENTED. REPAIRED SKIN PANEL PER EA. (M) 2L72 4F A16WE 20040308001742004030800174NM 2004 3 8 ASAA0410007 120040106A53306545778 SKIN BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, A PREVIOUS SKIN REPAIR WAS NOT CONFIGURED TO THE CURRENT AND REVISED SRM AT FUSELAGE STATION 927, STRINGER 20R. REMOVED PREVIOUS REPAIR AND REPLACED THE NEW REVISED SRM REPAIR. (M) 2L72 4F A16WE 20040308001832004030800183NM 2004 3 8 ASAA0410014 120040107A531165C335171 FRAME BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FRAME AT FUSELAGE STATION 685, STRINGER 13R-16R CORRODED. REPLACED FRAME PER SRM AND BOEING DRAWING. (M) 2L72 4F A16WE 20040308001872004030800187NM 2004 3 8 ASAA0410003 120040106A531565549063 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 520, RIGHT BUTTOCK LINE 60, LEFT BUTTOCK LINE 55 CORRODED. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040309000092004030900009NM 2004 3 9 04048500 120040217A3350 CONNECTOR DORNERDO32 DO328300 NM CABIN LOOSE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27500FJ 3197 DURING INSPECTION THE EMERGENCY LIGHTS AT SEAT 1A AND 1B WERE FOUND INOPERATIVE. THE CONNECTOR AND THE LIGHT ASSEMBLY WAS FOUND LOOSE AND RESECURED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2H72 4T RTA55NM 20040309000112004030900011NM 2004 3 9 04045423 120040214A291342152 PUMP DORNERDO32 DO328300 NM HYD SYSTEM FAILED A VTZAK NONE O OTHER UKUNKNOWN 1 EA27423FJ 3181 DURING AIRCRAFT OPERATION THE CREW REPORTED A HYDRAULIC PUMP-A FAILED. THE HYDRAULIC PUMP WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040309000152004030900015EU 2004 3 9 MALA040166 120040123A28208346 PRESSURE SWITCH SAAB SF340 340B 7860101EU FUEL SYSTEM LEAKING A MALAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15429XJ 340B429 FLIGHT ATTENDANT COMPLAINED OF JET FUEL SMELL IN GALLEY AND ROW 1 AREA, THROUGHOUT FLIGHT FROM DSM TO MSP. MAINTENANCE UNABLE TO DUPLICATE SQK. NO ABNORMAL SMELL OR ODOR NOTED IN CABIN OR COCKPIT WITH BLEED SYSTEM ON. INSPECTED WING AREA AND ENG COMPARTMENTS FOUND RIGHT FUEL STANDBY PSI SWITCH LEAKING. REPLACED P/N 8346 IAW SF340 AMM 28-22-10-4. OPS CHECK GOOD NO OTHER LEAKS NOTED. 2L72 4T RTA52EU 20040309000172004030900017EU 2004 3 9 04054322 120040223A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27322UE 41058 DURING INSPECTION THE RIGHT HAND FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4T RTA41NM 20040309000192004030900019NM 2004 3 9 04052424 120040221A4920 APU DORNERDO32 DO328300 NM APU BAY LEAKING A VTZAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UKUNKNOWN 1 EA27424FJ 3185 DURING AIRCRAFT OPERATION THE CREW RECEIVED A LAVATORY SMOKE MESSAGE. THE APU LOAD CONTROL VALVE WAS FOUND TO HAVE OIL RESIDUE CAUSING THE SMOKE. APU WAS DEFERRED FOR PARTS AND LATER REPAIRED. 2H72 4T RTA55NM 20040309000212004030900021EA 2004 3 9 04050648 120040219A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27648BR 7406 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040309000312004030900031EU 2004 3 9 AALA20040277 120040220A5320 SPLICE AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - STRINGER SPLICES CORRODED IN 0.7 BY 0.7 INCH AREA WITH DEPTH OF 0.032 INCH AT FR65 BULK AT STRINGERS 56L, 55L, 54L, 52L, 56R AND 55R. REPLACED CORRODED STRINGER SPLICES AT FR65 STRINGERS 56L, 55L, 54L, 56R AND 55R PER SRM 51-75-10. 2L72 4F RTA35EU 20040309000502004030900050WP 2004 3 9 AALA20040282 120040225A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21570AA 49352 ORD - FORWARD PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040309000592004030900059NM 2004 3 9 CALA0400173 120040226A5711654532422 SPAR BOEING737 7373T0 1384582NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 INSPECTION FOUND THE RT WING REAR SPAR UPPER CHORD CRACKED AT RSS 288. THE SPAR CHORD WAS REPAIRED IAW ECRA 5711-01055. 2L72 4F RTA16WE 20040309000612004030900061NM 2004 3 9 CALA0400175 120040226A532065C339702 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 344, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040309000772004030900077SO 2004 3 9 C2XA04SH114 120040227A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 52 AND FRAME 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309001202004030900120WP 2004 3 9 GTIA040067 120040116A5320 CUSP WEB DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND AFT PIT STATION 1193-1212 STRINGER 18L WEB CORRODED. REMOVED WEB FROM STATION 1174 TO STATION 1250. FABRICATED NEW WEB AND DOUBLER TWO MATERIAL LOSS ON FRAME FITTING OUT OF LIMITS. REMOVED FRAME FITTING. LOCATED AND DRILLED NEW FRAME FITTING. INSTALLED NEW FRAME FITTING. INSTALLED WEB. (M) 2L72 4F A6WE 20040309001442004030900144WP 2004 3 9 GTIA040094 120040108A5730 ACCESS PANEL DOUG DC9 DC981 3022081WP LT WING CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND LEFT WING ACCESS PANEL HAS SURFACE CORROSION AROUND FASTENERS ON EXTERIOR SIDE. REMOVED CORROSION. FABRICATED REPAIR PART. INSTALLED REPAIR PART. (M) 2L72 4F A6WE 20040309001462004030900146WP 2004 3 9 GTIA040096 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD, RIGHT, OUTBOARD STATION 160-200 MISSING EDGE FILLER, PEELING FIBERGLASS. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040309001472004030900147WP 2004 3 9 GTIA040097 120040112A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND LEFT FLOORBOARD STATION 1136-1193 DELAMINATED AND INSERTS CORRODED. FABRICATED NEW LEFT FLOORBOARD. (M) 2L72 4F A6WE 20040309001482004030900148WP 2004 3 9 GTIA040098 120040108A5320 ANGLE DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND RIGHT PASSENGER CABIN CUSP PLATE CORRODED AT STATION 207. CUT OUT CUSP ANGLE SECTION. FABRICATED 19 REPAIR ANGLE. FABRICATED 1 REPAIR CUSP ANGLE. INSTALLED REPAIR CUSP ANGLE AND 19 SPLICE ANGLE. (M) 2L72 4F A6WE 20040309001512004030900151WP 2004 3 9 GTIA040085 120040114A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL METAL EDGES BENT, CRACKED, WORN THROUGH. NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040309001532004030900153WP 2004 3 9 GTIA040099 120040114A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL STATION 1150-1250 LEFT, MISSING BROKEN INSERTS NO EDGE SEAL. UPON FURTHER EVALUATION FOUND PANEL AT STATION 1150-1250 TO BE DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040309001892004030900189SO 2004 3 9 RAIA00401044 120040126A532014525140023 SEGMENT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CK FOUND T-SECTION AT PAX DOOR AREA WITH CORROSION BEYOND BENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED T-SECTION. 2L72 4T RTT00011AT 20040309001912004030900191SO 2004 3 9 RAIA00401046 120040127A531514521719003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION CENTER FLOORBEAM AT RAMP SUPPORT. MAINTENANCE REPLACED CENTER FLOORBEAM. 2L72 4T RTT00011AT 20040309001932004030900193SO 2004 3 9 RAIA00401048 120040120A532014522459003 SUPPORT ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION AT SUPPORT ANGLE AT PAX DOOR. MAINTENANCE REMOVED AND REPLACED SUPPORT ANGLE. 2L72 4T RTT00011AT 20040309001952004030900195SO 2004 3 9 RAIA00401050 120040120A5315 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND LEFT HAND FLOORBEAM CORRODED. MAINTENANCE REPAIRED LEFT HAND FLOORBEAM IAW SRM 5321-10. 2L72 4T RTT00011AT 20040310000092004031000009NM 2004 3 10 UPS04441922 120040127A5230 DOUBLER BOEING747 747123 1384873NM CARGO DOOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C EO747-5330-13494-H REPAIR ASSESSMENT PROGRAM DURING MARK ACCOMPLISH, TAR 106855 REPAIR AGAIN AT BS 1905-1913 STR 42R AFT CARGO DOOR AFT EDGE AREA WHICH MAY INTERFERE WITH THE EXISTING REPAIR AT ITEM N672-46-26, BS 1915-1920 STR 41-42R. EXPENDED DOUBLER REPAIRED AS PER SRM 52-30-06 FIG 1 AT AFT CARGO DOOR AFT LWR CORNER BS 1905-1920 STR 41R-42R AREA. REPEAT INSPECTION REQUIRED AS PER SRM 52-30-06 FIG 1 SHT 12 TABLE II. REPEAT INSPECTION IS REQUIRED PER EO B747-5330-13494-H. 2L74 4F A20WE 20040310000222004031000022NM 2004 3 10 AALA20040302 120040229A3350 SIGN BOEING737 737823 13844BZNM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21901AN 29503 MIA - EMERGENCY EXIT SIGN AT 4R DOOR BROKEN. REPLACED EMERGENCY EXIT SIGN AT 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040310000272004031000027 2004 3 10 AALA20040307 420040224A25655A33073 SLIDE BOEING737 737823 13844BZNM SERVICE DOOR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21908AN 29510 TUL - EVACUATION SLIDE AT RIGHT HAND FORWARD SERVICE DOOR, STATION 312, FAILED TO STAY INFLATED DUE TO A HOLE IN THE SLIDE. REPLACED SLIDE AT FORWARD SERVICE DOOR PER WORKCARD 8814. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040310000312004031000031SO 2004 3 10 C2XA04TY039 120040222A33503325101 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2714991 145278 PILOT REPORT, PORT EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE PORT EMERGENCY EXIT LIGHT CONNECTOR. AIRCRAFT WAS RELEASED. 2L72 4T RTT00011AT 20040310000362004031000036SO 2004 3 10 C2XA04SH134 120040302A532014522461011 DOUBLER EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV- DURING C-CHECK THE RIGHT HAND FORWARD OMEGA BEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310000382004031000038SO 2004 3 10 C2XA04TY044 120040304A532014524131001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719554 145587 TYS DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR FWD SILL HAS AREAS OF CORROSION. MAINT BLENDED AFT AREA AND FOUND TO BE WITHIN LIMITS; ALODINED, PRIMED, PAINTED, BLENDED FWD AND FOUND TO BE OUT OF LIMITS, FABBED DOUBLER, ALODINED, PRIMED, PAINTED AND INSTALL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040310000402004031000040SO 2004 3 10 C2XA04IA018 120040226A3350 CONNECTOR EMB 145 EMB145 3260210SO CABIN DIRTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716961 145103 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDANTS JUMPSEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE FORWARD INVERTER, CLEANED THE CONNECTOR, AND RE-INSTALLED THE SAME UNIT. THE EMERGENCY LIGHTING SYSTEM OPERATIONALLY CHECK GOOD AND THE DISCREPANCY WAS CLEARED. 2L72 4F RTT00011AT 20040310000442004031000044SO 2004 3 10 C2XA04SH133 120040302A532014529150003 CROSSBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 BETWEEN THE CENTER OMEGA BEAM AND THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310000632004031000063NM 2004 3 10 SWAA040499 120040217A3350101114 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040310000642004031000064NM 2004 3 10 SWAA040500 120040217A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29737JW 27869 EEPLS COVER BROKEN AT FWD SECTION. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040310000682004031000068NM 2004 3 10 SWAA040505 120040217A531065353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 14R AND 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040310000792004031000079NM 2004 3 10 SWAA040516 120040218A33507003661 BALLAST BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29432WN 33715 DURING SCHEDULED MV3 CHECK, FOUND RT SIDE OVERWING EXIT DOOR LIGHT INOP. REMOVED AND REPLACED OVERWING EXIT DOOR LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20040310000912004031000091NM 2004 3 10 SWAA040528 120040219A53206516300 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND LT SHEAR WEB CORRODED AT BS 1016. REMOVED AND REPLACED SHEAR WEB PER SRM. 2L72 4F RTA16WE 20040310000962004031000096NM 2004 3 10 SWAA040668 120040302A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 4 LONG CRACK AT FUSELAGE SKIN AT BS 312, BETWEEN STR 17R AND STR 18R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040310001012004031000101NM 2004 3 10 SWAA040673 120040302A53116546567 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1016, LBL 5, WL 190.5. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040310001082004031000108NM 2004 3 10 SWAA040657 120040301A53206551698 SPLICE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE 4L CRACKED AT BS 360. REMOVED AND REPLACED SPLICE PER SRM. 2L72 4F RTA16WE 20040310001122004031000112NM 2004 3 10 SWAA040662 120040301A3350101114 LENS BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS ASSY PER MM. 2L72 4F RTA16WE 20040310001132004031000113NM 2004 3 10 SWAA040663 120040301A3350D71701100 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29423WN 29827 DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP BETWEEN ROWS 6 AND 10. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040310001142004031000114 2004 3 10 SWAA040664 420040301A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2/R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C4 CHECK, FOUND BOTH L2 AND R2 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDE ASSY'S PER MM. 2L72 4F A16WE 20040310001162004031000116EA 2004 3 10 04051636 120040220A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27636BR 7307 DURING INSPECTION THE RIGHT HAND AFT EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. A WIRE WAS FOUND BROKEN BENEATH THE FLOORBOARDS AND REPAIRED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040310001172004031000117 2004 3 10 04052660 420040221A3160 DISPLAY CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A VTZAO OTHER G MULTIPLE FAILURE NRNOT REPORTED 1 EA27660BR 7519 DURING OPERATION OF AIRCRAFT CREW REPORTED A MOMENTARY LOSS OF FLIGHT DISPLAYS, AUTOPILOT, FLIGHT DIRECTOR AND VHF COMM ON COPILOTS SIDE. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY AT DESTINATION. A SATISFACTORY OPERATIONAL CHECK OF ALL SYSTEMS WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040310001192004031000119EU 2004 3 10 RAIA00402026 120040227A2422559012A INVERTER AEROSPATR72 ATR72202 8680940EU NR 2 FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03723TE11026233 283 STL- RIGHT INVERTER FAULT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER. 2H72 4T RTA53EU 20040310001272004031000127SO 2004 3 10 RAIA00403003 120040305A3350 CONNECTOR EMB 145 EMB145LR 3260212SO COCKPIT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03818HK 145059 STL - EMERGENCY LIGHTS AT BOTTOM OF FLIGHT DECK INOP. MAINTENANCE RE-SECURED CANNON PLUG TO EMERGENCY LIGHT. 2L72 4T RTT00011AT 20040310001302004031000130EU 2004 3 10 RAIA00402003 120040202A33102LA06691300 LIGHT JETAIRJETSTMJETSTM4101 1500501EU COCKPIT SHORTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE03550HK 41039 COU - DURING LANDING AT STL CREW REPORTED SMOKE IN COCKPIT WITH NR 2 CONSOLE BACKLIGHTING C/B TRIPPED. MAINTENANCE INSPECTED AND DEFERRED CONSOLE NR 2 BACKLIGHTING, PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING CAPTAINS AFT LIGHTING ASSEMBLY. 2L72 4T RTA41NM 20040310001312004031000131GL 2004 3 10 RAIA00402004 320040202A6110B5JFR26C1103E PROPELLER JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR365JFR36C1003 GL NR 1 ENGINE FAULTY A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03561HK1269141 41077 020991 JLN - LEFT PROP HEAT INOP. MAINTENANCE DEFERRED PROP HEAT PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING NR 1 PROP. 2L72 4T RTA41NM 6 CP15NE 20040310001332004031000133SO 2004 3 10 C2XA04SH132 120040302A532014542773002 PANEL EMB 145 EMB145LR 3260212SO RT MLG WW CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE RIGHT HAND MAIN LANDING GEAR WHEEL WELL AFT RIB PANEL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PANEL IAW EMB 145 IPC 53-04-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310001342004031000134SO 2004 3 10 C2XA04TY043 120040304A532014521721005 PLATE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719554 145587 TYS DURING A SCHEDULED 1C INSPECTION THE FWD DIGITAL PLATE HAD AREAS OF CORROSION. MAINT CUT THE DAMAGED AREA OUT, FAB DOUBLERS AND DRILLED HOLES ON NEW FWD DIGITAL, INSTALL AND PRIMED DOUBLERS AND NEW DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040310001362004031000136SO 2004 3 10 C2XA04BT027 120040302A3260852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO RT MLG FAULTY A C2XAK NONE O OTHER CRCRUISE 1 SW2713956 145078 CREW REPORTED, EXPERIENCED SEVERAL UNUSUAL THUMPS WHILE INFLIGHT. NOISES SEEM TO BE COMING FROM THE NOSE OF THE AIRCRAFT. MAINTENANCE TROUBLESHOT AND FOUND RIGHT HAND LANDING GEAR UPLOCK CHANNEL-B FAULTY. REMOVED AND REPLACED LANDING GEAR PROXIMITY SWITCH-B AT RIGHTHAND LANDING GEAR UPLOCK IAW EMB145 AMM 32-61-01, SWUNG LANDING GEAR IAW EMB145 AMM 32-62-00 AND 32-30-00. OPS CHECKED GOOD, NO FURTHER NOISES OR FAULTS NOTED. 2L72 4F RTT00011AT 20040310001392004031000139SO 2004 3 10 C2XA04TY040 120040304A532014521725001 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 TYS DURING A SCHEDULED 2C INSPECTION THE LT WALL FLOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE LT FLOOR SILL AFT OF PAX DOOR IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040310001422004031000142SO 2004 3 10 C2XA04SH130 120040302A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 1 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV- DURING C-CHECK THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040311000012004031100001SO 2004 3 11 SWIA200412932 120040220A2730 PROXIMITY SWITCH EMB 120 EMB120ER 3260203SO LT & RT ELEVATORFAULTY A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07187SW 120037 FIRST FLIGHT AURAL WARNING TRIM CHECK FAILS. REMOVED LEFT AND RIGHT ELEVATOR TRIM PROX SWITCHES HAND SHAKE CONNECTORS AND REPLACED WITH ENVIRONMENTAL SPLICE CONNECTORS IAW EMB 120 WMM 20-21-00 AND 31-52-00, OPS CHECKED GOOD. 2L72 4T RTA31SO 20040311000062004031100006EA 2004 3 11 SWIA200412917 120040112A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 589 CARGO DOOR FLOOR LANDING PLATE TRANSVERSE BEAM ANGLE LBL 44 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. 2L72 4F4 FRTA21EA E15NE 20040311000072004031100007EA 2004 3 11 SWIA200412918 120040112A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040311000082004031100008EA 2004 3 11 SWIA200412919 120040112A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 605 CARGO DOOR LANDING PLATE TRANSVERSE BEAM LBL 44 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. 2L72 4F4 FRTA21EA E15NE 20040311000092004031100009EA 2004 3 11 SWIA200412920 120040214A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07926SW3388 3388 7687 AT CRUISE, RECEIVED A SPOILERONS CAUTION MSG ABOUT 1 MINUTE LATER, A FLT SPOILERS CAUTION MESSAGE ALONG WITH AN I/B GND SPLR FAULT MESSAGE. ON LANDING, THE SPOILERONS AND FLIGHT SPOILERS DEPLOYED ONLY, NO GROUND SPOILERS DEPLOYED. REMOVED AND REPLACED NR 2 SECU IAW CRJ 27-61-05. ALL OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040311000652004031100065NM 2004 3 11 QXEA200400158 120040217A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PANEL BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX - MAINTENANCE FOUND SEVERAL NUT PLATES BROKEN ON PANEL 122BR. REMOVED AND REPLACED BROKEN NUT PLATES IAW SRM 51-40-11. 2H72 4T RTA13NM 20040311000662004031100066SO 2004 3 11 C2XA04TY042 120040304A491014528650403 STIFFENER EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719554 145587 TYS DURING A SCHEDULED 1C INSPECTION THE RT UPPER STIFFENER ON THE APU FIREWALL WAS FOUND CRACKED. MAINT FABBED A DOUBLER AND STOPPED DRILL CRACK. INSTALL DOUBLER AT RT UPPER STIFFENER ON THE APU FIREWALL IAW EMB 135/145 SRM 55-32-13. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040311000682004031100068EA 2004 3 11 SWIA200412966 120040302A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07433SW 7550 OVERHEAD EMERGENCY LIGHT IN AFT CABIN INOP. REMOVED AND REPLACED EMERGENCY LAMP WITH A NEW LAMP IAW 33-00-00. OPS CHECK GOOD. P/N: 1317. 2L72 4F RTA21EA 20040311000702004031100070EA 2004 3 11 SWIA200412968 120040304A2701 CONTROL WHEEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT LACK OF LUBE A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07430SW 7523 AILERONS HESITATE, THEN MOVE A LOT WHEN TURNED TO LEFT. CANNOT DUPLICATE ON GROUND, ONLY INFLIGHT, FEELS LIKE THEY ARE RUBBING AGAINST SOMETHING. TORQUED FORWARD CONTROL WHEEL SHAFT NUT ON BOTH RIGHT AND LEFT CONTROL WHEELS AND LUBED BEARINGS PER MM 27-11-01. OPS CHECK GOOD PER MM 27-11-00. 2L72 4F RTA21EA 20040311000712004031100071 2004 3 11 SWIA200412969 420040301A22116229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS FAULTY A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07460SW 7803 AFTER SELECTING A NEW HEADING WHILE IN HDG MODE, THE A/C CONTINUED TURNING THROUGH THE NEW HEADING (OPPOSITE THE FLIGHT DIRECTOR COMMANDS) AND THEN JERKED SUDDENLY TO THE LEFT TWICE. THE A/P DISCONNECTED ON ITS OWN. REMOVED AND REPLACED FCC NR 1 IAW MM 22-12-1A. OP CHECKS GOOD. P/N 622-9815-704, S/N ON 642, S/N OFF 13N2T. 2L72 4F RTA21EA 20040311000732004031100073SO 2004 3 11 SWIA200412971 120040125A5411 FRAME EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER AFT FRAME IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1. 2L72 4T RTA31SO 20040311000742004031100074SO 2004 3 11 SWIA200412972 120040125A5411 FRAME EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 LEFT MLG, OUTBOARD LOWER NACELLE FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER NACELLE FRAME IAW 120 SRM 51-10-02 PG 3 SEC 3A & RII CARD 54-301. 2L72 4T RTA31SO 20040311000772004031100077NM 2004 3 11 CALA0400215 120040305A5347143A948535 CARGO TRACK BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724736 28803 INSPECTION FOUND LOWER RAIL IN FORWARD CARGO COMPARTMENT CORRODED AT STA 500D. THE RAIL WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040311000782004031100078NM 2004 3 11 CALA0400216 120040306A5320149A761115 WEB BOEING737 737724 13844BYNM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724736 28803 INSPECTION FOUND A 2 INCH CRACK IN WEB ON LT WHEEL WELL RING ASSEMBLY. A NEW WEB WAS INSTALLED WITH HI-LOKS AND RIVETS IAW SRM 51-40-02 AND 51-20-05. 2L72 4F RTA16WE 20040311000792004031100079NM 2004 3 11 CALA0400217 120040306A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0969351 23589 INSPECTION FOUND UPPER FLANGE OF MAIN CABIN FLOORBEAM CORRODED AROUND THREE FLOORBOARD ATTACH HOLES AT STA 312, RBL 36. A REPAIR STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20040311000802004031100080NM 2004 3 11 CALA0400218 120040306A5330 SKIN BOEING757 757224 1384958NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2748127 28968 THE PREVIOUS SKIN BLENDOUT AT STATIC PORT AREA, BS 540 BETWEEN S22R AND S23R WAS FOUND BEYOND LIMITS. THE DAMAGE WAS REPAIRED IAW SRM 53-00-01, FIGURE 209. A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 37,500 FLIGHT CYCLES AND AGAIN EACH SUBSEQUENT 12,000 FLIGHT CYCLES UNTIL SKIN REPLACED. 2L72 4F RTA2NM 20040311000832004031100083NM 2004 3 11 04FDEA00545 120040303A5753 SUPPORT DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RT WING OUTBOARD FLAP INBOARD HINGE BRACKET SUPPORT RIB (INTERIOR) FOUND CRACKED. RT WING O/B FLAP ASSY REMOVED & REPLACED AS PER AMM 27-50-30, OPERATION TEST & ADJUSTMENT CARRIED OUT FOUND SATIS AS PER AMM 27-50-00. COMPLIED WITH EA 1-5750-7529.1 TE FLAPS O/B RT FLAP - BUILDUP OF THE NRC6753-506 ASSY FOR USE IN PLACE OF THE NRC6753-502 ASSY. 2L73 4F RTA22WE 20040311000852004031100085EA 2004 3 11 COMA0460179 120040229A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN DISCONNECTED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01809CA 7366 FLIGHT 5600 EMERGENCY LIGHTS AT CABIN AND SERVICE DOORS ARE INOP. RECONNECTED LOOSE WIRE CONNECTION. 2L72 4F RTA21EA 20040311000862004031100086EU 2004 3 11 MALA040215 120040226A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15402XJ 340B402 DURING 4Y/2Y INSPECTION, RIGHT I/B SEAT TRACK AT STA 295 HAS CORROSION. REMOVED DAMAGED SEAT TRACK SECTION AT STA 295, CUT-DRILLED, DEBURR-TREATED, SEAT TRACK, INSTALLED NEW FABRICATED SEAT TRACK IAW EO S53060. A/C RELEASE DATE 3/1/04. 2L72 4T RTA52EU 20040311000892004031100089 2004 3 11 MALA040218 420040301A2213 COMPUTER BAC 146 AVRO146RJ85A1500097EU AUTOPILOT SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15508XJ E2318 JUST AFTER AIRBORNE LIGHTS ON ADVISORY PANEL FTC, EL TRIM, YD ILLUMINATED. AIR RETURN TO MSP. RERACKED DFGC. DFGS OP CHECKS GOOD IAW RJ-85 M/M CHAP 22. EXCEPT FOR AUTOTHROTTLE. 2H74 4F RTA49EU 20040311000942004031100094NM 2004 3 11 2004UALA00152 120040221A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29642UA 25092 EXTERIOR EMERGENCY LIGHT INOP AT LT FUSELAGE AFT OF TRAILING EDGE. RELAMPED, CHECKED OK. 2L72 4F4 FRTA1NM E24NE 20040311000952004031100095NM 2004 3 11 2004UALA00153 120040219A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29953UA 26700 EMERGENCY EXIT LIGHT INOP AFT OF WING. REPLACED EEL LIGHT STRIP IN FRONT OF GALLEY CARTS, GROUND CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040311000962004031100096NM 2004 3 11 2004UALA00154 120040226A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29586UA 26710 DOOR 1R EMERGENCY EXTERIOR LIGHT INOPERATIVE. RELAMPED, OPS CHECK NORMAL. 2L72 4F4 FRTA2NM E17NE 20040311000972004031100097NM 2004 3 11 2004UALA00155 120040222A4920 STATOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE APU MISINSTALLED A UALAO OTHER WEBINADEQUATE Q C VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29774UA 26936 INTERMITTENT ODOR AND HAZE IN CABIN. T2 STATOR ASSEMBLY OFTEN SUPPLIED BY THE VENDER AS COMPLETELY ASSEMBLED. SUBASSEMBLY HELD TOGETHER BY TWO WRAPS OF SAFETY WIRE FOR SHIPMENT. UNITED SHOP PROCEDURES DOES STATE TO REMOVE WIRE IF PRESENT (OEM CMM USED). UNITED APU SHOP MECHANICS MISSED REMOVING WIRE & DURING ENGINE OPERATION THE T2 BLADES GREW & HIT CONSTRAINED STATOR ASSEMBLY CAUSING HIGH VIBRATION & COMPRESSOR CARBON SEAL FAILURE WHICH RESULTED IN ODOR IN CABIN. JOB CARD WILL BE REVISED TO HAVE LEAD REMOVE ONE NOZZLE & CHECK FOR WIRE. OEM HAS BEEN CONTACTED TO USE ALTERNATIVE SHIPPING AIDE THAT WILL BURN AWAY AT INITIAL APU START. PREVENTING FAILURE. 2L72 4F4 FRTT0001SE E46NE 20040311000982004031100098NM 2004 3 11 2004UALA00156 120040221A2780 PDU BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLATS FAILED A UALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 WP29576UA 26690 FLIGHT RETURNED TO FIELD WITH A LEADING EDGE SLAT DISAGREEMENT MESSAGE. LEFT PDU TORQUE LIMITER TRIPPED. REPLACED LEFT LEADING EDGE POWER DRIVE UNIT. 2L72 4F4 FRTA2NM E17NE 20040311000992004031100099NM 2004 3 11 SWAA040589 120040225A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, STRINGERS 9L, 8L, 5L, 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040311001002004031100100NM 2004 3 11 SWAA040590 120040225A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A, STRINGERS 8L, 6L, 4L, 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040311001012004031100101NM 2004 3 11 SWAA040591 120040225A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727A, STRINGERS 7R, 6R, 4R, 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040311001022004031100102NM 2004 3 11 SWAA040592 120040225A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STRINGERS 8R, 7R, 6R, 3R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040308001782004030800178NM 2004 3 8 ASAA0410026 120040112A531365458955 STRINGER BOEING737 7372Q8C 138448SNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT FUSELAGE STATION 500B PLUS 15 CRACKED. REPAIRED STRINGER PER EA. (M) 2L72 4F A16WE 20040308001802004030800180NM 2004 3 8 ASAA0410001 120040106A531565549041 FLOORBEAM BOEING737 7372Q8C 138448SNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01741AS 21959 OKC - DURING SCHEDULED D-CHECK, FOUND THE FLOORBEAM AT FUSELAGE STATION 380, LEFT BUTTOCK LINE 11, RIGHT BUTTOCK LINE WITH ELONGATED HOLES. REPAIRED FLOORBEAM PER EA. (M) 2L72 4F A16WE 20040309000392004030900039SO 2004 3 9 C2XA04SH105 120040226A553012034077603 HINGE BRACKET EMB 135 EMB135ER 3260203SO VERTICAL STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE UPPER CENTER HINGE BRACKET ON THE VERTICAL STABILIZER TO THE RUDDER WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 AMM 20-10-01 AND EMB 135 IPC 55-31-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000412004030900041SO 2004 3 9 C2XA04SH107 120040226A531313500222001 STRINGER EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CENTER OMEGA BEAM STRINGER FROM FRAMES 22 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040309000432004030900043NM 2004 3 9 04FDEA00520 120040225A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 CORROSION (C53-224-01,1) ON FLOORBEAM BS 340 RBL 12 WL 208 AT FASTENER HOLE. CORROSION ON FLOORBEAM BS 340, RBL 12, WL 208 AT FASTENER HOLE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED & REPLACED FLOORBEAM BS 340 FROM BL 0 - RBL 65 PER SR DWG SR 27-53-007. 2L73 4F RTA3WE 20040309000442004030900044WP 2004 3 9 04FDEA00522 120040225A2497 WIRE DOUG DC10 DC1010 3022110WP MAIN BATTERY OUT OF POSITION A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25393FE 46627 REPEAT WRITE-UP. AT 1:45 HR INTO FLIGHT, RECEIVED LVL 1 ALERT BATTERY DISCHARGING FOR APPROX 20 SEC. ALERT THEN OUT FOR 1 MIN, CAME BACK ON AND OFF INTERMITTENTLY FOR NEXT 10 MIN. COMPLIED WITH QRH, LANDED AT DEN, NO OTHER PROBLEMS NOTED. INTERROGATED EPCU, FOUND SENSE FAULT. FOUND CELL SENSE WIRE COMING OFF OF CONNECTOR P1-1959 STRETCHED TAUNT, RELIEVED PRESSURE BY REMOVING TY-WRAPS AND MOVING WIRE INBOARD. REMOVED AND REPLACED BATTERY CHARGER PER MM 24-34-02-2, CHECKS NORMALLY. REMOVED AND REPLACED EPCU PER MM 24-08-01-4, CHECKS NORMALLY. PERFORMED BATTERY DISCHARGING ALERT OPS CHECK PER MM 24-00-01-6, CHECKS NORMALLY. 2L73 4F A22WE 20040309000452004030900045NM 2004 3 9 AWXA200400223 120040225A3350100865 POWER SUPPLY BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28155AW 23777 LAS - EEL - DURING B-1 CHECK THE EMERGENCY EXIT SIGN ABOVE R-2 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT AFT EMERGENCY POWER SUPPLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040309000462004030900046NM 2004 3 9 AWXA200400225 120040225A2560P4010021 BATTERY BOEING737 7373S3 1384711NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 DEN - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040309000472004030900047NM 2004 3 9 AWXA200400226 120040211A531065C807351 CREASE BEAM BOEING737 7373U3 13844CCNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 LCQ - MAJOR REPAIR - DURING C-5 CHECK EXFOLIATION CORROSION WAS FOUND ON RT CREASE BEAM BETWEEN BS 944 AND BS 998, RBL 54. MAINTENANCE REMOVED CORRODED SECTION OF RT CREASE BEAM BETWEEN BS 944 AND BS 998, RBL 54; FABRICATED A NEW REPLACEMENT SECTION OF CREASE BEAM; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-08 PG 1-4. 2L72 4F RTA16WE 20040309000482004030900048NM 2004 3 9 AWXA200400227 120040210A532065479573 WEB BOEING737 7373U3 13844CCNM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 LCQ - MAJOR REPAIR - DURING C-5 CHECK CORROSION WAS FOUND THROUGHOUT ENTIRE LENGTH OF AFT CARGO DOOR LOWER SILL FROM BS 793 TO BS 847, STR 24 RT TO STR 26 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR LOWER SILL; FABRICATED A NEW REPLACEMENT SILL PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-08, PARA 6. 2L72 4F RTA16WE 20040309000692004030900069EU 2004 3 9 AWXA200400230 120040211A5320D53480043205 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SILL BEAM Y1732 RT BETWEEN FR 66 AND FR 68. MAINTENANCE CUT OUT 2 EACH AREAS OF CORRODED SILL BEAM Y1732 RT BETWEEN FR 66 AND FR 68; FABRICATED 2 EACH FILLERS AND A REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14 FIG 101 & 201 PG 103 & 201-213. 2L72 4F RTA28NM 20040309000712004030900071NM 2004 3 9 04051401 120040220A291342152 PUMP DORNERDO32 DO328300 NM HYD SYSTEM FAILED A VTZAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27401FJ 3145 DURING TAXI OF FLIGHT 6153 CREW REPORTED A HYDRAULIC PUMP A FAIL AND RETURNED TO GATE. THE PUMP WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA55NM 20040309000722004030900072 2004 3 9 04052401 420040221A31607014300902 DISPLAY DORNERDO32 DO328300 NM COCKPIT FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27401FJ 3145 DURING CLIMB THE CREW REPORTED A PRIMARY FLIGHT DISPLAY FAILURE AND LOSS OF INFORMATION. THE DISPLAY UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040309000782004030900078SO 2004 3 9 C2XA04SH115 120040227A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000792004030900079SO 2004 3 9 C2XA04SH116 120040227A532014521713005 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000802004030900080SO 2004 3 9 C2XA04SH117 120040227A532014524131001 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD U-BRACKET AT FRAME 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000812004030900081SO 2004 3 9 C2XA04SH118 120040227A532014524131009 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE MAIN DOOR U-BRACKET AT FRAME 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000822004030900082SO 2004 3 9 C2XA04SH119 120040227A532014524125003 THRESHOLD EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000832004030900083SO 2004 3 9 C2XA04SH120 120040227A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000842004030900084SO 2004 3 9 C2XA04SH121 120040227A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT AND RIGHT UPPER APU MOUNTS. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000852004030900085SO 2004 3 9 C2XA04SH122 120040227A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 2 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27125524321 4321 145583 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE AFT FLANGE WAS FOUND TO BE GOUGED AROUND THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309000922004030900092EA 2004 3 9 SWIA200412899 120040112A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA E/E BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 193 RHS ELECTRICAL BAY FLOOR CRACKED. REPAIRED FLOOR IAW CRJ REO 601R-53-11-245 REV NC & RII 53-401. 2L72 4F RTA21EA 20040309000942004030900094EA 2004 3 9 SWIA200412901 120040112A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 280 RT FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ REO 601R-53-11-171 REV NC (RII 53-401). P/N: S6144-13. 2L72 4F RTA21EA 20040309000962004030900096EA 2004 3 9 SWIA200412903 120040112A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 484 RT INTERCOSTAL RBL 27 ANGLE CRACKED. ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. P/N: 601R31171-9. 2L72 4F RTA21EA 20040309000982004030900098EA 2004 3 9 SWIA200412905 120040112A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 280 PILOT'S BULKHEAD AFT FLOOR SUPPORT ANGLE RBL 11 CRACKED. REPAIR ANGLE IAW CRJ REO 601R-53-11-137 REV NC (RII 53-401). 2L72 4F RTA21EA 20040309001032004030900103EA 2004 3 9 SWIA200412910 120040112A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 409 + 128 LT VERTICAL BEAM LBL 18 LWR O/B FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401. 2L72 4F RTA21EA 20040309001052004030900105EA 2004 3 9 SWIA200412912 120040112A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 409 + 128 RT VERTICAL BEAM RBL 18 LWR O/B FLANGE CRACKED. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV NC & RII 53-401. 2L72 4F RTA21EA 20040309001072004030900107EA 2004 3 9 SWIA200412914 120040112A5411 RIB CNDAIRCL600 CL6002B19 1900309EA RT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 605 RT PYLON RIB CRACKED. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 54-401. P/N: 601-37004-86. 2L72 4F RTA21EA 20040309001112004030900111WP 2004 3 9 AALA20040288 120040229A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21569AA 49351 MSP - FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040309001822004030900182WP 2004 3 9 GTIA040059 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN FLOORBOARD, RIGHT STATION 197-229, DAMAGED INSERTS, MISSING EDGE FILLER, PEELING FIBERGLASS. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20040309001842004030900184 2004 3 9 GTIA040049 420040206A2565 LANYARD DOUG DC9 DC982 3022082WP EVAC SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FLL - FOUND R-1 DOOR EVACUATION SLIDE LANYARD LOOSE. RE-INSTALLED R-1 DOOR EVACUATION SLIDE LANYARD. (M) 2L72 4F A6WE 20040309001862004030900186WP 2004 3 9 GTIA040053 120040111A5320 DOUBLER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND FS 1136 L15L WEB DOUBLER HAS CORROSION. REMOVED WEB DOUBLER. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040310000022004031000002NM 2004 3 10 UPS04241933 120040122A5755 SUPPORT FITTING BOEING727 72722C 138400FNM NR 3 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C REPAIR PLATES ON NR 3 SPOILER PCU SUPPORT FITTING, REAR SPAR ATTACH ANGLES DO NOT CONFORM TO REQUIREMENTS OF SRM REPAIR 51-40-4 FIG 1 OR S/B 57-84 R1 CRITERIA. REPAIR CARRIED OUT IAW DRAWING 65-16201 & MM 28-11-20 & 28-11-21. 2L73 4F A3WE 20040310000102004031000010NM 2004 3 10 UPS04441923 120040125A5312 STRAP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C BS 1241 LEFT BULKHEAD SPLICE STRAP AFT HOLE FOUND CRACKS AT FWD AND AFT SIDE. BS 1241 LEFT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3). 2L74 4F A20WE 20040310000112004031000011NM 2004 3 10 UPS04441924 120040122A5320 STRAP BOEING747 747123 1384873NM RT WLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C RIGHT WLG W/W - BS 1241 SPLICE STRAP AFT HOLE CRACK. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107, RIGHT STA 1241 SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3). 2L74 4F A20WE 20040310000162004031000016NE 2004 3 10 AALA20040296 220040228A7200JT8D217C ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE NR 1 MAKING METAL A AALAA UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CRCRUISE 1 SW217535A 49989 MCO T/1219 EN ROUTE LGA-PBI ENGINE OIL PRESSURE AND LOW LIGHT ILLUMINATED ACCOMPANIED BY ZERO OIL PRESSURE AND ZERO OIL TEMPERATURE. REDUCED THRUST TO IDLE FROM 1348Z TO 1355Z, HEARD AND FELT VIBRATION AND SHUT DOWN ENGINE. LANDED MCO WITHOUT INCIDENT. FOUND MAGNETIC METAL IN SCREEN. OIL QUANTITY WAS OK. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20040310000212004031000021NM 2004 3 10 AALA20040301 120040301A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21795AN 30257 DFW - EMERGENCY LIGHT AT FLIGHT ATTENDANT SEAT BY 4R DOOR BROKEN AT MOLDING. REPLACED EMERGENCY LIGHT AT FLIGHT ATTENDANT SEAT BY 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040310000242004031000024EU 2004 3 10 AALA20040304 120040301A5311 FRAME AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 TUL - CORROSION ON FRAME 58 AT RIGHT HAND STR 46, AFT CARGO, IN 1 INCH BY 1 INCH AREA AND 0.030 INCH DEPTH. REPAIRED CORROSION FOR FRAME 58 AT RIGHT HAND STR 46 PER SRM 53-10-13-2. 2L72 4F RTA35EU 20040310000472004031000047NM 2004 3 10 SWAA040545 120040221A53126516300 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SPV, FOUND WEB CRACKED AT BS 178, WL 235 AND LBL 8, LBL 9, LBL 10 AND LBL 12.5. REPAIRED WEB PER SRM. 2L72 4F A16WE 20040310000552004031000055NM 2004 3 10 SWAA040490 120040216A53306555074 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER OUTBOARD CORNER OF THE NR 1 WINDOW. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000572004031000057NM 2004 3 10 SWAA040492 120040216A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM CORRODED BETWEEN BS 947 AND BS 987. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040310000672004031000067NM 2004 3 10 SWAA040504 120040217A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 767 + 3, AT STRINGER 19R. REPAIRED SKIN CRACK PER SRM. 2L72 4F RTA16WE 20040310000732004031000073NM 2004 3 10 SWAA040510 120040218A57536546434 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED ON T/E. REMOVED AND REPLACED LT WING INBOARD FLAP PER MM. 2L72 4F RTA16WE 20040310000742004031000074NM 2004 3 10 SWAA040511 120040218A5320BAC1514 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SPV, FOUND CORROSION ON BS 1016, VERTICAL STIFFENER AT 6 O'CLOCK POSITION. REPAIRED STIFFENER PER ACO. 2L72 4F RTA16WE 20040310000822004031000082NM 2004 3 10 SWAA040519 120040219A335007912 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 EEPLS STRIP COVER BROKEN AT ROW 17 ABC. REPAIRED PER MM. 2L72 4F RTA16WE 20040310000842004031000084 2004 3 10 SWAA040521 420040219A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040310000882004031000088NM 2004 3 10 SWAA040525 120040219A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE BULGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 727 + 13, STRINGER 27R. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040310000902004031000090NM 2004 3 10 SWAA040527 120040219A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 500D +16, STRINGER 15R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040310001262004031000126 2004 3 10 RAAI00403002 420040303A23507511001945 CONTROL PANEL JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03574HK* 6664 41093 STL - CAPTAIN'S HEADSET INOP. MAINTENANCE REMOVED AND REPLACED AUDIO CONTROL PANEL. 2L72 4T RTA41NM 20040310001352004031000135SO 2004 3 10 C2XA04SH131 120040302A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 2 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310001402004031000140SO 2004 3 10 C2XA04TY041 120040304A532014524131009 BRACKET EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 TYS DURING A SCHEDULED 2C INSPECTION THE PAX DOOR SILL BRACKETS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FORWARD AND AFT PAX DOOR SILL BRACKETS IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040310001442004031000144NM 2004 3 10 CALA0400189 120040229A5280 STRUCTURE BOEING737 737824 13844BZNM LT MLG DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND A .5 INCH AND .75 INCH CRACK IN LEFT MLG CENTER DOOR ON FORWARD LOWER CORNER. THE MLG DOOR WAS REPAIRED IAW ECRA 5280-01315, REV B. A DIP WAS ISSUED TO INSPECT THE DOOR EVERY 30 DAYS AND TO REPLACE THE DOOR WITHIN 24 MONTHS. 2L72 4F RTA16WE 20040311000022004031100002 2004 3 11 SWIA200412933 420040218A3497 WIRE EMB 120 EMB120ER 3260203SO STALL WARNING BROKEN A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07236SW 120312 NO STICK SHAKER RIGHT SIDE. REPAIRED BROKEN WIRE. OP CHECK OK. 2L72 4T RTA31SO 20040311000042004031100004EA 2004 3 11 SWIA200412915 120040112A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 625 LT INTERCOSTAL ANGLE CRACKED STR 14L. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040311000722004031100072EA 2004 3 11 SWIA200412970 120040302A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07592SW6297 6297 7279 RECEIVED A FLAPS FAIL WHEN SELECTING FLAPS 20 DURING APPROACH. REMOVED AND REPLACED LEFT BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD. P/N: 855D100-9, S/N ON: 316B, S/N OFF: 0811B. 2L72 4F RTA21EA 20040311000762004031100076SO 2004 3 11 SWIA200412974 120040125A5720 CLIP EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 LEFT WING SHEAR CLIP AT STATION YA-5825 CRACKED OUTBOARD OF FUEL PANEL 4 MIDDLE SECTION. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AND SEALED SHEAR CLIP IAW 120 SRM 51-10-02 AND RII CARD 28-301. 2L72 4T RTA31SO 20040311000842004031100084EA 2004 3 11 COMA0460178 120040302A32347455025 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01518CA1927 7816 FLIGHT 5870 WHEN LANDING GEAR SELECTED UP IT CYCLED BETWEEN UP AND INTRANSIT UNTIL THE CONTROL WAS RECYCLED. REPLACED THE GEAR SELECTOR CONTROL HANDLE. 2L72 4F RTA21EA 20040311000902004031100090EA 2004 3 11 04059655 120040228A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAULTY A VTZAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 EA27655BR 7457 DURING APPROACH OF FLIGHT TO BDL CREW REPORTED A FLAP FAIL WITH FLAPS AT 20 DEGREES ON APPROACH. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE BPSU WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040311000922004031100092EU 2004 3 11 2004UALA00057 120040124A2133VFT300A1 VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE DEFECTIVE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29439UA 683 RETURN TO FIELD DUE TO A PRESSURIZATION PROBLEM. INABILITY TO PRESSURIZE WAS RESULT OF A MALFUNCTIONING SKIN AIR OUTLET VALVE. THE DEFECTIVE UNIT WAS REPLACED AND VERIFIED FAULTY. NO FURTHER PRESSURIZATION PROBLEMS REPORTED SINCE UNIT REPLACEMENT. 2L72 4F4 FRTA28NM E40NE 20040311000932004031100093NM 2004 3 11 2004UALA00151 120040222A3350 INDICATOR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29791UA 26933 EXIT PATH LIGHTING INDICATOR LOOSE-BROKEN 11F. REPLACED AND TESTED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20040727000102004072700010EU 2004 7 27 04FDEA02153 120040722A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MAIN CABIN SEAT TRACK 2R FR 40/41 TO 6 INCHES AFT OF FR 45 IS 1 CORRODED AND CRACKED AT FR 43 ON THE I/B SIDE FLANGE AND 2 CORRODED IN THE SCALLOP AREA 10 INCHES AFT OF FR 44 (LEVEL 2). REMOVED AND REPLACED SEAT TRACK FROM FR40 TO FR 46 IAW SRM 51-72-10. 2L72 4F RTA35EU 20040309000952004030900095EA 2004 3 9 SWIA200412902 120040112A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 EXTERIOR HANDLE OF CREW ESCAPE HATCH HAS CORROSION DAMAGE. REPLACED CREW ESCAPE HATCH OUTER HANDLE WITH NEW ASSY. HANDLE OPS CHECKED OK. P/N: H3419-33. 2L72 4F RTA21EA 20040309000972004030900097EA 2004 3 9 SWIA200412904 120040112A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 280 PILOT'S BULKHEAD AFT FLOOR SUPPORT ANGLE LBL 9.0 CRACKED. REPAIR ANGLE IAW CRJ REO 601R-53-11-138 REV NC, RII 53-401. P/N: 7075T6 040, 600-34017-351. 2L72 4F RTA21EA 20040309000992004030900099EA 2004 3 9 SWIA200412906 120040112A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 559 LT VERTICAL BEAM LBL 9.0 INBOARD & OUTBOARD LWR FLANGES CRACKED. BEAM REPAIRED IAW CRJ REO 601R-53-41-057 REV NC, RII 53-401. 2L72 4F RTA21EA 20040309001082004030900108SO 2004 3 9 C2XA04SH128 120040229A532014521275605 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712552 145583 SHV-DURING C CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED AT FRAME 22, STRINGER 15 RIGHT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040309001102004030900110WP 2004 3 9 AALA20040287 120040229A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21462AA 49592 SAN - CEILING EMERGENCY LIGHTS BETWEEN TWO AFT LAVS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN TWO AFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040309001272004030900127WP 2004 3 9 GTIA040074 120040108A5312 DOOR FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND AFT PRESSURE BULKHEAD DOOR JAMB THRESHOLD SEAL TORN. AFTER REMOVED TORN SEAL FOUND CORROSION. CUT OUT DAMAGED AREA AT LOWER AFT DOOR JAMB. FORMED DOUBLER. FABRICATED FILLER. INSTALLED DOUBLER AND FILLER. (M) 2L72 4F A6WE 20040309001342004030900134WP 2004 3 9 GTIA040081 120040108A5320 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND LEFT AFT LAVATORY STATION 1322 STRINGER 18L FITTING CORRODED. REMOVED FITTING. INSTALLED NEW FITTING. (M) 2L72 4F A6WE 20040309001362004030900136WP 2004 3 9 GTIA040066 120040106A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FORWARD CABIN STATION 220-200 RIGHT SIDE INBOARD SEAT TRACK HAS GOUGED, NICKS, BARE METAL, LIGHT CORROSION. REMOVED DAMAGED SEAT TRACK STATION 200-265. LOCATED AND DRILLED SEAT TRACK. INSTALLED FASTENERS IN SEAT TRACK AT STATION 200-265. (M) 2L72 4F A6WE 20040309001382004030900138 2004 3 9 GTIA040050 420040206A2565 LANYARD DOUG DC9 DC982 3022082WP EVAC SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 RSW - FOUND R1 DOOR LANYARD OFF. RECONNECTED R1 DOOR SLIDE LANYARD. NO DEFECTS NOTED. (M) 2L72 4F A6WE 20040309001812004030900181WP 2004 3 9 GTIA040058 120040108A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND COCKPIT CENTER FLOORBOARD, BROKEN INSERTS AND SIDE DELAMINATIONS. FABRICATED NEW COCKPIT CENTER FLOORBOARD. (M) 2L72 4F A6WE 20040309001832004030900183 2004 3 9 GTIA040047 420040208A2565 LANYARD DOUG DC9 DC982 3022082WP EVAC SLIDE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FLL - R-1 DOOR EMERGENCY SLIDE GIRT BAR LANYARD ROUTED INCORRECTLY. RE-ROUTED R-1 DOOR SLIDE GIRT BAR LANYARD. (M) 2L72 4F A6WE 20040309001852004030900185WP 2004 3 9 GTIA040052 120040113A5311 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND MID PIT, BULKHEAD FRAME, FS 598, CRACKED IN THREE AREAS. STOP DRILLED CRACKS. FABRICATED TWO DOUBLERS. INSTALLED DOUBLERS. (M) 2L72 4F RTA6WE 20040309001872004030900187WP 2004 3 9 GTIA040054 120040113A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 FTW - FOUND CABIN CENTER FLOORBOARD FS 598 TO 636, INSERT BROKEN AND MATERIAL PEELING. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040309001882004030900188SO 2004 3 9 RAIA00401043 120040123A5320 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - PAX DOORSILL ANGLES HAVE CORROSION BEYOND BENDABLE LIMITS. MAINTENANCE REMOVED AND REPLACED PAX DOOR SILL ANGLES IAW EMB GST-1927/02A. 2L72 4T RTT00011AT 20040309001902004030900190SO 2004 3 9 RAIA00401045 120040127A532014522461011 DOUBLER EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION AT SERVICE DOOR ENTRY AREA DOUBLERS AT FRAME 19 AND 21. MAINTENANCE REMOVED AND REPLACED DOUBLERS. 2L72 4T RTT00011AT 20040309001922004030900192SO 2004 3 9 RAIA00401047 120040122A532014521719003 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND FORWARD FLOOR AT FRAME 14 TO FRAME 18 CENTER HAT BEAM CORROSION. MAINTENANCE REMOVED AND REPLACED HAT BEAM. 2L72 4T RTT00011AT 20040309001942004030900194SO 2004 3 9 RAIA00401049 120040120A531514521699003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION ON LEFT HAND DIGITAL. MAINTENANCE REMOVED AND REPLACED LEFT HAND DIGITAL. 2L72 4T RTT00011AT 20040310000122004031000012NM 2004 3 10 UPS04441925 120040129A5312 STRAP BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C BS 1241 RIGHT BULKHEAD SPLICE STRAP AFT HOLE CRACK FOUND RUNNING AFT APPROX .125 INCH. AFT BOLT HOLE REPAIRED AS PER RS R53-41-35107 BS 1241 RIGHT BULKHEAD SPLICE STRAP WILL BE REPLACED WITHIN 2 YEARS AFTER CRACK DISCOVERY AS PER EO B747-5310-0323 PARA D (3). 2L74 4F A20WE 20040310000132004031000013WP 2004 3 10 AALA20040293 120040227A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21438AA 49456 SEA - CEILING EMERGENCY LIGHTS FROM ROWS 17-21 INOPERATIVE. REPLACED BATTERY PACK B5-104 FOR CEILING EMERGENCY LIGHTS FROM ROWS 17-21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040310000152004031000015EU 2004 3 10 AALA20040295 120040228A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217062A 474 MIA - EMERGENCY LIGHTS AT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040310000352004031000035SO 2004 3 10 C2XA04IA021 120040222A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718556 145595 DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMP, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040310000372004031000037SO 2004 3 10 C2XA04SH136 120040303A532014528737001 STIFFENER EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712967 145133 SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/0718. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040310000412004031000041SO 2004 3 10 C2XA04IA019 120040229A32201170C000002 TUBE EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714991 6371 145278 FLIGHT 2766 - CREW REPORTED THAT THE LANDING GEAR FAILED TO RETRACT WITH AN ASSOCIATED LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE FOUND THE NOSE LANDING GEAR SLIDING TUBE TO BE LOCKING UP IN THE NOSE GEAR STRUT HOUSING. THE NOSE LANDING GEAR ASSEMBLY WAS REMOVED AND REPLACED, OPERATIONALLY TESTED, AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040310000422004031000042SO 2004 3 10 C2XA04SH135 120040302A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND UPPER APU SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310000432004031000043GL 2004 3 10 C2XA04CL015 220040226A7310P1081 FILTER EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 ENGINE DIRTY A C2XAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 SW2727962 145110 CLE FLIGHT 3231 THE CREW REPORTED A ENGINE NR 2 FUEL IMPENDING BYPASS WARNING. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND REPLACED THE FUEL FILTER AND IMPENDING BYPASS INDICATOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20040310000452004031000045SO 2004 3 10 C2XA04SH137 120040303A532014528737001 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV- DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310000492004031000049 2004 3 10 SWAA040547 420040222A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29784SW 29810 R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE R2 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2L72 4F RTA16WE 20040310000562004031000056NM 2004 3 10 SWAA040491 120040216A53156546815 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 986, RBL 24. REPAIRED PER SRM. 2L72 4F RTA16WE 20040310000592004031000059NM 2004 3 10 SWAA040494 120040216A3350OL3071BPEGL LIGHT BOEING737 7373Q8 1384670NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED 1/4D CHECK, FOUND ROW 6 ABC BULLNOSE EMERGENCY EXIT ESCAPE AISLE LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040310000612004031000061NM 2004 3 10 SWAA040497 120040217A33501000679 LIGHT BOEING737 7372H4 138448CNM R2 DOOR INTERMITTENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED R2 DOOR LIGHT PER MM. 2L72 4F A16WE 20040310000692004031000069NM 2004 3 10 SWAA040506 120040217A32116959886 FITTING BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED RON CHECK, FOUND RT MLG FORWARD HANGER FITTING PITTED. REPAIRED HANGER FITTING PER EA. 2L72 4F RTA16WE 20040310000722004031000072NM 2004 3 10 SWAA040509 120040218A53306545800 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 277 + 11.5, STRINGER 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310000932004031000093 2004 3 10 SWAA040665 420040302A3417HG480B13 ADC BOEING737 7372H4 138448CNM E/E BAY FAULTY A SWAAK NONE G MULTIPLE FAILURE CRCRUISE 1 SW29086SW 22827 NR 1 ASI FAILURE, MACH TRIM, GPWS AND WINDSHEAR FAIL LIGHTS ILLUMINATED, NR 1 AND NR 2 RADIO ALT'S INOP. ALL SYSTEMS CAME BACK SEVERAL MINUTES LATER. REMOVED AND REPLACED NR 1 ADC PER MM. 2L72 4F A16WE 20040310001022004031000102NM 2004 3 10 SWAA040674 120040302A534065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 727D, STR 7R, AND BS 727C, STR 7R. REMOVED AND REPLACED STR CLIPS PER SRM. 2L72 4F RTA16WE 20040310001152004031000115NM 2004 3 10 SWAA040583 120040225A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE BULGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN BULGED AT BS 795, BETWEEN STRINGER 26R AND STRINGER 27R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040310001182004031000118EU 2004 3 10 RAIA00401042 120040129A3230 LANDING GEAR JETAIRJETSTMJETSTM4101 1500501EU NLG COLLAPSED A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03567HK 41085 STL- ON APPROACH TO LANDING NOSE LANDING GEAR WOULD NOT FULLY EXTEND AND INDICATED UNSAFE. NOSE LANDING GEAR COLLAPSED ON LANDING. MAINTENANCE REMOVED AND REPLACED NLG, NR 2 ENGINE AND PROPELLER, REPAIRED DAMAGE TO FUSELAGE NOSE SECTION AND LANDING GEAR DOORS. 2L72 4T RTA41NM 20040310001222004031000122SO 2004 3 10 RAIA00401051 120040122A532014521725001 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND CORROSION LEFT HAND SILL. MAINTENANCE REMOVED AND REPLACED LEFT HAND SILL. 2L72 4T RTT00011AT 20040310001252004031000125SO 2004 3 10 RAIA00401054 120040120A532014521721009 STRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND FORWARD STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED FORWARD STRAP DIGITAL. 2L72 4T RTT00011AT 20040310001322004031000132EU 2004 3 10 RAIA00402005 120040203A21402974A000 SHUTOFF VALVE JETAIRJETSTMJETSTM4101 1500501EU CABIN HEAT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03554HK151863504 41067 STL - NO HEAT RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED NR 2 PRSOV. 2L72 4T RTA41NM 20040310001382004031000138SO 2004 3 10 C2XA04SH138 120040303A531214526850401 FIREWALL EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER SUPPORT ARM MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040310001432004031000143NM 2004 3 10 CALA0400188 120040229A5510180A16121 PIN BOEING737 737724 13844BYNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT UPPER FAILSAFE PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696, REV B, OP 1. 2L72 4F RTA16WE 20040311000032004031100003 2004 3 11 SWIA200412934 420040220A2210 PIN EMB 120 EMB120ER 3260203SO CONNECTOR BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW 120039 F/O'S ELECTRIC TRIM NOSE UP INOP. REPAIRED BROKEN PIN ON J2 PIN 1. RERACKED APC NR 2. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040311000752004031100075SO 2004 3 11 SWIA200412973 120040125A5411 FRAME EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 LEFT ENGINE FRAME NR 1 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FRAME NR 1 IAW EMB120 SRM 51-10-02 PG 3 SEC 3A AND S/B 120-54-0036 AND RII CARD 54-301. 2L72 4T RTA31SO 20040311000822004031100082NM 2004 3 11 04FDEA00544 120040303A5350 WEB DOUG MD11 MD11 3023602NM TAILCONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 TAIL CONE CENTER FWD WEB FOUND CRACKED. AFT TAILCONE CENTER FWD WEB REMOVED AND REPLACED AS PER SRM 51-35-01 VOL. II. 2L73 4F RTA22WE 20040311000912004031100091 2004 3 11 2004UALA00050 420040121A3441HG1150AC06 ADIRU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY FAILED A UALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP29425UA 508 FLIGHT DIVERTED DUE TO LOSS OF MULTIPLE NAVIGATION FUNCTIONS. ADIRU 3 WAS REMOVED AND TESTED. ADIRU 1 WAS MOVED TO NR 3 POSITION AND A REPLACEMENT UNIT INSTALLED IN POSITION NR 1. NR 1 IDG WIRING WAS CHECKED AS POSSIBLE CAUSE WITH NO FAULTS FOUND. ADIRU SYSTEM OPERATION HAS BEEN NORMAL TO DATE. TEST OF ADIRU NR 3 FOUND NO CURRENT FAULTS. A BITE MEMORY DUMP WAS ACCOMPLISHED AND SHOWED ALIGN IN AIR MESSAGE. UNIT SERVICEABLE. 2L72 4F4 FRTA28NM E40NE 20040315001882004031500188NM 2004 3 15 C1HA200478001 120040209A275040TP135 MOTOR BOEING727 727225 1384077NM TE FLAPS INOPERATIVE A C1HAA UNSCHED LANDING F FLT CONT AFFECTED LDLANDING 1 GL15818EA 22555 INBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND HYDROLICLY OR ELECTRICALLY ON LANDING. FOUND INBOARD ALTERNATE FLAP MOTOR BINDING INSTALLED SERVICEABLE ALTERNATE FLAP MOTOR REF MM 27-51-141 PG 401-402. OPS CHECKED GOOD. 2L73 4F A3WE 20040315001892004031500189 2004 3 15 PCAA0402164 420040212A34257003360941 AHRS DHAV DHC8 DHC8102 2809003NM NR 1 FAULTY A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13821EX218493219 173 FLIGHT 3929 CLIMBING OUT OF PHILADELPHIA HAD TO RETURN TO FIELD DUE TO THE AHRS ON THE CAPTAINS SIDE GOING INOP. THE PILOT ELECTED TO RETURN TO FIELD FOR MAINTENANCE. MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER AND ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040315001902004031500190NM 2004 3 15 PCAA0402165 120040210A612078249050 PCU DHAV DHC8 DHC8102 2809003NM NR 2 PROPELLER FAULTY A PCAAO OTHER L NO TEST TXTAXI/GRND HDL 1 EA13821EX19708444 173 FLIGHT 3998 MIDDLETOWN, PILOT REPORTED THAT THE NR 2 PROP DID NOT FEATHER DURING THE AUTOFEATHER TEST. MAINTENANCE REMOVED AND REPLACED THE NR 2 PROPELLER CONTROL UNIT. ALL OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040315001952004031500195NM 2004 3 15 UPS04441936 120040125A5415 FITTING BOEING747 747123 1384873NM NR 4 PYLON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 NR 4 PYLON DIAGONAL BRACE UNDERWING FITTING, HOLE NR 10 I/B ROW MOST AFT CORROSION FOUND ON BACKUP FITTING BORE AREA. DEFECTIVE AREA FASTENER HOLE CORROSION REPAIR CARRIED OUT AS PER HX RS R57-24-35102 AND EO B747-5740-19955-A. FINAL HOLE 0.562 INCH TO CLEAN UP CORROSION. 2L74 4F A20WE 20040315001972004031500197WP 2004 3 15 UPS04841916 120040129A5320577384443 SUPPORT DOUG DC8 DC871F 302199DWP INTERCOSTAL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, INTERCOSTAL SUPPORT CLIP IS CRACKED ON FWD SIDE OF AFT PRESSURE BULKHEAD STATION 1766 AT LONG 4L. REMOVED, FABRICATED AND REPLACED SUPPORT CLIP IAW DWG 5773844 AND SRM 51-1-20D. 2L74 4F RT4A25 20040315001982004031500198WP 2004 3 15 UPS04841917 120040201A53404758514509 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D. 2L74 4F RT4A25 20040315001992004031500199WP 2004 3 15 UPS04841918 120040129A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1731 LONG 14L IS CRACKED. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-2 FIG 12. 2L74 4F RT4A25 20040315002002004031500200WP 2004 3 15 UPS04841919 120040131A534037739062 SUPPORT FITTING DOUG DC8 DC871F 302199DWP CABIN SUBFLOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, FLOORBEAM SUPPORT FITTINGS ARE CRACKED AT STATION 798 AND 822 AT LBL 23. REMOVED, FABRICATED AND REPLACED FITTINGS IAW DWG 3773906 AND SRM 51-1-20D. 2L74 4F RT4A25 20040315002022004031500202WP 2004 3 15 UPS04841921 120040201A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STATION 1265 AT LONG 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040315002032004031500203WP 2004 3 15 UPS04841927 120040131A531047746541 SUPPORT DOUG DC8 DC871F 302199DWP A/C COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 A/C BAY CEILING SUPPORT ANGLE IS CRACKED AT STATION 55 LBL 30. REMOVED, FABRICATED AND REPLACED ANGLE FITTING IAW DWG 4774654 AND SRM 51-1-20D. 2L74 4F RT4A25 20040315002042004031500204WP 2004 3 15 UPS04841929 120040203A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1270 LONG 36 IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 1270 - 1310, FABRICATED AND INSTALLED STRAP DOUBLERS AND CHANNELS IAW UPS ENGINEERING FILE DC8-53-20393 AND SAA SK 703-514. 2L74 4F RT4A25 20040316000032004031600003WP 2004 3 16 UPS04841931 120040201A53204758514503 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1235, LONG 33R SUPPORT ANGLE IS CRACKED AND INTERCOSTAL IS GOUGED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE AND INTERCOSTAL IAW DWG 9754949, 4758514 AND SRM 51-1-20D. 2L74 4F RT4A25 20040316000302004031600030EA 2004 3 16 A6WA200440021 120040212A322016215105 BRACKET CNDAIRCL600 CL6002B19 1900309EA NLG BENT A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31402AW 7281 ON TAKEOFF, GEAR HANDLE UP NOSE GEAR UNSAFE AND GEAR DOOR OPEN WARNING MESSAGE. REMOVED AND REPLACED OLEO CENTER/PROXIMITY CENTER BRACKET. GEAR SWING OPS CHECK GOOD IAW AMM. (M) 2L72 4F RTA21EA 20040316000452004031600045WP 2004 3 16 GTIA040012 120040116A2612 CONNECTOR DOUG DC9 DC983 3022083WP LT ENG FIRE LOOPDAMAGED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23824NK 53015 DTW - FLT 1605 - FIRE DETECTOR LOOP CAUTION LIGHT FLICKERS WITH LEFT ENGINE LOOP A ILLUMINATED. REPAIRED CONNECTION ON UPPER LOOP. SYSTEM OP CHECKS GOOD. (M) 2L72 4F RTA6WE 20040316000462004031600046 2004 3 16 GTIA040013 420040117A2565 LANYARD DOUG DC9 DC982 3022082WP TAILCONE SLIDE OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 LGA - FOUND AFT TAILCONE SLIDE LEFT LANYARD NOT IN BRACKET. SECURED LANYARD IN BRACKET FOR TAILCONE SLIDE. OK FOR SERVICE. (M) 2L72 4F A6WE 20040316000472004031600047 2004 3 16 GTIA040015 420040118A2565 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FLL - FLT 980 - L1 AND L2 ESCAPE SLIDE GIRT BAR LANYARD ROUTED INCORRECTLY. REROUTED L1 AND L2 SLIDE GIRT BAR LANYARD. (M) 2L72 4F A6WE 20040316000492004031600049WP 2004 3 16 GTIA040017 120040106A5320 SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND AFT PIT STATION 1170 STRINGER 18L WEB SUPPORT CORRODED. REMOVED SUPPORT. INSTALLED WEB SUPPORT. (M) 2L72 4F A6WE 20040316000502004031600050WP 2004 3 16 GTIA040004 120040107A2120 ODOR DOUG DC9 DC983 3022083WP MID CABIN DETECTED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23832NK 49618 RSW - FLT 1605 - STRONG ODOR OF JET FUEL NOTED IN MID CABIN. AFTER REFUELING AND APU SHUTDOWN FUEL ODOR WENT AWAY. (M) 2L72 4F RTA6WE 20040316000522004031600052WP 2004 3 16 GTIA040006 120040105A3260 SWITCH DOUG DC9 DC983 3022083WP NLG CONTAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 ORD - FLT 1443 - RED NOSE GEAR LIGHT COMES ON AFTER NOSE GEAR RETRACTION. NOSE GEAR PIN IS RETRACTED. LIGHT GOES OUT IN MINUTES. CLEANED TARGET AND SWITCH OF DEBRIS. (M) 2L72 4F RTA6WE 20040316000532004031600053NM 2004 3 16 ASAA0440039 120040211A3397 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST TXTAXI/GRND HDL 1 NM01764AS 25101 FAI - FOUND FLOOR TRACK LIGHTING AT ROW 15 COVER DISLODGED CAUSING ONE SECTION OF WHITE LIGHTS TO FAIL. RECONNECTED WIRES AND REPLACED PROTECTIVE COVER AS REQUIRED. (M) 2L72 4F RTA16WE 20040316000552004031600055WP 2004 3 16 ASAA0480068 120040209A53219957918501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23976AS 53452 OKC - HV1 CHECK, FOUND CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FS 929-1003. REMOVED DAMAGED SECTION AND REPAIRED WITH FILLER AND SPLICE PER SRM 51-10-4, 53-01, AND 51-30-8. (M) 2L72 4F RTA6WE 20040316000562004031600056 2004 3 16 GTIA040008 420040108A2565 CLIP DOUG DC9 DC982 3022082WP GIRT BAR BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 DTW - FOUND GIRT BAR HOLD CLIP ON L2 DOOR BROKEN. REATTACHED GIRT BAR HOLD CLIP ON L2 DOOR. (M) 2L72 4F A6WE 20040316000572004031600057WP 2004 3 16 GTIA040010 120040107A2560 GLOWSTRIP DOUG DC9 DC983 3022083WP ROW 27 LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 DTW - FOUND SAFETY GLO FLOOR TRACK LIGHTING IS COMING UP AT ROW 27 ON RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED RETAINER ON SAFETY GLO PATH AT ROW 23. (M) 2L72 4F RTA6WE 20040316000582004031600058 2004 3 16 GTIA040014 420040118A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 ORD - FLT 478 - L1 SLIDE PACK FELL OFF DOOR UPON OPENING IN ORD. REINSTALLED SLIDE PACK. (M) 2L72 4F A6WE 20040316000592004031600059 2004 3 16 GTIA040002 420040102A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 LGA - FOUND L2 DOOR SLIDE DAMAGED AND ON THE RAMP FLOOR NEXT TO 2 BAGS OF GARBAGE. REMOVED AND REPLACED L2 DOOR SLIDE PACK, OK FOR SERVICE. (M) 2L72 4F A6WE 20040316000742004031600074EA 2004 3 16 ASOA04090 120040204A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11701EV 10020 DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040316000772004031600077EA 2004 3 16 ASOA04093 120040206A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING A GROUND INSPECTION IN ATL, THE RIGHT REAR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT REAR EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040316000792004031600079EU 2004 3 16 SIMA200402060 120040119A53117252813117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21339SB 340B339 ABI - DURING A 4000 HOUR INSPECTION, THE RT FUSELAGE FRAME AT STATION 668 WAS FOUND TO BE DENTED ABOVE THE FLOOR LINE. RECONTOURED THE DENTED AREA AND PERFORMED AN EDDY CURRENT INSPECTION OF REWORKED AREA. NO DEFECTS NOTED. FABRICATED A FLANGED REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006511 PARA 1. (M) 2L72 4T RTA52EU 20040316000802004031600080EU 2004 3 16 SIMA200402605 120040119A53117252814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21339SB 340B339 ABI - DURING A 400 HOUR INSPECTION, THE RT FUSELAGE FRAME AT STATION 686.888 WAS FOUND TO BE DENTED ABOVE THE FLOOR LINE. RECONTOURED THE DENTED AREA AND PERFORMED AN EDDY CURRENT INSPECTION OF REWORK AREA. NO DEFECTS NOTED. FABRICATED A FLANGED REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006511. (M) 2L72 4T RTA52EU 20040310001202004031000120SO 2004 3 10 RAIA00402027 120040228A3260 CONNECTOR EMB 145 EMB145LR 3260212SO WOW SWITCH DEFECTIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03815HK 145048 STL - AIR/GRN FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED THE WOW PROX SWITCH CONNECTOR. 2L72 4T RTT00011AT 20040310001212004031000121SO 2004 3 10 RAIA00403001 120040301A335078241 INVERTER EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03827HK 145021 STL - FRONT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER. 2L72 4F RTT00011AT 20040310001232004031000123SO 2004 3 10 RAIA00401052 120040120A532014522460013 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND CENTER FLOORBEAM GUSSET CORRODED. MAINTENANCE REMOVED AND REPLACED GUSSET. 2L72 4T RTT00011AT 20040310001242004031000124SO 2004 3 10 RAIA00401053 120040120A532014522460015 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03810HK 145231 STL - DURING BLOCK CHECK FOUND AFT STRAP CORRODED. MAINTENANCE REMOVED AND REPLACED AFT STRAP GUSSET. 2L72 4T RTT00011AT 20040310001282004031000128SO 2004 3 10 RAIA00403004 120040305A3010 LIGHT EMB 145 EMB145ER 3260211SO ANTI-ICE SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03827HK 145021 STL - WING ANTI-ICE OPEN LIGHT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED OPEN INDICATOR LAMP. 2L72 4F RTT00011AT 20040310001292004031000129 2004 3 10 RAIA00401056 420040125A22137021170951 CONTROL UNIT EMB 145 EMB145 3260210SO AUTOPILOT SYS MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03804HK2724 145082 STL - YAW DAMPER INOP INDICATION. MAINTENANCE DEFERRED PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING FLIGHT GUIDANCE CONTROL UNIT. 2L72 4F RTT00011AT 20040310001372004031000137SO 2004 3 10 C2XA04BT026 120040229A4900 ODOR EMB 145 EMB145 3260210SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2713964 145123 CREW REPORTED, STRONG ODOR OF FUEL/OIL IN COCKPIT AND CABIN AFTER EVERY APU START. MAINTENANCE INSPECTED, PERFORMED SEVERAL APU STARTS IAW EMB145 AMM 49-00-00. OPS AND LEAKED CHECKED GOOD. NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040310001412004031000141SO 2004 3 10 C2XA04IA022 120040301A32608005701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305SO NLG FAULTY A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2715527 145413 DURING CLIMB THE NOSE GEAR DOORS DID NOT RETRACT AFTER THE NOSE LANDING GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED TO XNA AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK PROXIMITY SWITCH. THE LANDING GEAR SYSTEM WAS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4F RTT00011AT 20040311000052004031100005EA 2004 3 11 SWIA200412916 120040112A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07409SW 7056 FS 662 LT FIRE WALL SHUT-OFF INTERCOSTAL ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040311000672004031100067EA 2004 3 11 SWIA200412965 120040212A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 42 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE AT FS 261 RIGHT REPAIRED IAW CRJ REO 601R-53-61-117 REV A AND RII 53-401. P/N: 601R53-61-117-4, 601R53-61-117-2. 2L72 4F RTA21EA 20040311000692004031100069 2004 3 11 SWIA200412967 420040227A3418 WARN PANEL EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07271YV 120271 STALL WARNING SYSTEM 2 FAILS TO TEST NORMALLY; STALL WARNING LAMP ILLUMINATES, WILL NOT EXTINGUISH ON MAP. REMOVED AND REPLACED STALL WARNING PANEL IAW 27-00-00, OPS CHECK OK. P/N 120-34428-505. 2L72 4T RTA31SO 20040311000812004031100081NM 2004 3 11 CALA0400219 120040308A5320 BRACKET BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718658 28919 INSPECTION FOUND A .75 INCH CRACK IN BRACKET AT BULKHEAD STA 727, RBL 3. A TYPICAL FORM SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20040311000872004031100087EU 2004 3 11 MALA040216 120040226A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15402XJ 340B402 DURING 4Y/2Y INSPECTION, LEFT I/B SEAT TRACK AT STA 295 HAS CORROSION. REMOVED DAMAGED SEAT TRACK SECTION AT STA 295, CUT-DRILLED, DEBURR-TREATED, SEAT TRACK, INSTALLED NEW FABRICATED SEAT TRACK IAW EO S53060. A/C RELEASE DATE 3/1/04. 2L72 4T RTA52EU 20040311000882004031100088EU 2004 3 11 MALA040217 120040301A3610 PERISEAL SAAB SF340 340B 7860101EU PNEUMATIC SYS LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15421XJ 340B421 LEFT BLEED AIR LEAK LIGHT ILLUMINATED IN FLIGHT, HIGH PRESS BLEEDS WERE OFF AT THE TIME. REMOVED AND REPLACED LT FLAP COVE DUCT PERI SEALS IAW SF340MM 36-10-00. PERFORMED OPERATIONAL TESTS IAW SF340MM 36-23-00-5. NO DEFECTS NOTED AT THIS TIME. 2L72 4T RTA52EU 20040727000092004072700009EU 2004 7 27 04FDEA02152 120040722A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MDC - SEAT TRACK L4 AT FR 16 HAS SEVERE LEVEL 3 CORROSION STARTING AT FR 16 AND GOING FORWARD 26 INCHES. REMOVED AND REPLACED TRACK IAW A310 SRM 51-40-20 AND 51-40-21. 2L72 4F RTA35EU 20040315001932004031500193NM 2004 3 15 UPS04441926 120040205A5230 DOUBLER BOEING747 747123 1384873NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, RAP ITEM N672 46-05 CRACK AT BS 1785 - 1792 STR 23L - 25L REMOVE FOR FURTHER ACTION. REPLACED REPAIR DOUBLER PER RS R52-32-35109 RELATED AREA SIDE CARGO DOOR RIGGING AND OPERATION CHECK DONE PER MM 52-32-00. SATISFACTORY AND EO B747-5230-19954-A. 2L74 4F A20WE 20040316000012004031600001EU 2004 3 16 MALA040191 120040208A33409111112163252 SOCKET SAAB SF340 340B 7860101EU EXTERIOR DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15421XJ 340B421 EN ROUTE TO STC W INBOARD LIGHT ILLUMINATED ON IT'S OWN. FOLLOWED QRH LIGHT STAYED ON. MAINTENANCE PERFORMED INDICATION ONLY REPLACED W INBOARD SOCKET, P/N 911-1112-1632-525 AT LOCATION 22HP, OPS CHECK GOOD. 2L72 4T RTA52EU 20040316000142004031600014EA 2004 3 16 A6WA200440023 120040219A4990 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU OIL TEMP ILLUMINATED A A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31409AW 7447 APU OIL TEMP CAUTION MESSAGE, DIVERTED TO ATL REF IDG NR 1 ON MEL. INTERROGATED ECU, TROUBLESHOT SYSTEM, REMOVED AND REPLACED HOT OIL TEMPERATURE SENSOR IAW AMM 49-91-25. RAN APU 15 MINUTES WITH LOADS APPLIED. NO DEFECTS NOTED, LEAK CHECK GOOD. (M) 2L72 4F RTA21EA 20040316000222004031600022NE 2004 3 16 A6WA200440022 220040214A7261 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE LEAKING A A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31424AW 7656 IN FLIGHT RIGHT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. COMPLIED WITH QRH. ALL OTHER ENGINE INDICATIONS NORMAL. LANDED WITH RT ENGINE AT IDLE AT MCI. INSPECTED AND FOUND OIL COMING FROM GANG DRAIN. R & R ACCESS B AND F CARBON SEAL IAW GE 34 RJ SEI ENG MM. GROUND RAN ENGINE, NO LEAKS NOTED. (M) 2L72 4F4 FRTA21EA E15NE 20040316000512004031600051WP 2004 3 16 GTIA040018 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLT COMP, FLOORBOARD DIRECTLY BEHIND CAPTAINS SEAT IS CRACKED. CUT OUT DAMAGE. FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. UPON FURTHER INVESTIGATION FOUND FIBERGLASS DOUBLERS SEPERATE. RECEMENTED FIBERGLASS DOUBLERS. (M) 2L72 4F A6WE 20040316000602004031600060WP 2004 3 16 GTIA040007 120040105A3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23833NK 49449 ON TAKEOFF OUT OF DCA, NOSE GEAR UNSAFE LIGHT ON. INDICATOR SHOWED UP NO NOISE FROM DOORS BEING OPEN, LIGHT WENT OUT PASSING FLIGHT LEVEL 200. ON DESCENT, AT 10,000 FT NOSE GEAR UNSAFE LIGHT CAME BACK ON THEN OUT AT 8000 FEET. PERFORMED VISUAL INSPECTION OF NOSE LANDING GEAR UP PROXIMITY SENSOR. REMOVED, INSPECTED, CLEANED AND REINSTALLED SENSOR CONNECTOR. CLEANED SENSOR AND TARGET, BOLTHEAD. PERFORMED BITE ON PSEU FOR BOTH SENSOR AND AUTO TEST, ALL CHECKED PASS REF. (M) 2L72 4F RTA6WE 20040316000622004031600062WP 2004 3 16 ASAA0480071 120040209A54145930640 SKIN DOUG DC9 DC983 3022083WP LT NACELLE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23976AS 53452 OKC - HV1 CHECK, FOUND LEFT ENGINE LOWER AFT COWL COMPOSITE MATERIAL IS SEPARATING AT FORWARD ATTACH HOOK. REBONDED COMPOSITE PER EA 7110-01220. (M) 2L72 4F RTA6WE 20040316000762004031600076WP 2004 3 16 ASAA0480069 120040209A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FS PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 OKC - HV1 CHECK, FOUND COCKPIT FLOOR PANEL UNDER CAPTAINS SEAT IS PUNCTURED. REMOVED DAMGAED SECTION AND INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20040316001082004031600108WP 2004 3 16 ASAA0480070 120040209A5230591014193N SKIN DOUG DC9 DC983 3022083WP CARGO BAY DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 OKC - HV1-CHECK, FOUND FORWARD CARGO BAY DOOR LOWER FORWARD AND AFT CORNERS ARE CHAFED. REMOVED DAMAGED SECTIONS. INSTALLED FILLERS AND DOUBLERS PER EA 5230-01226. (M) 2L72 4F RTA6WE 20040316001102004031600110NM 2004 3 16 C1HA200478002 120040218A3260 UPLOCK SENSOR BOEING727 727225 1384077NM RT MLG MALFUNCTIONED A C1HAO OTHER N FALSE WARNING APAPPROACH 1 GL15818EA 22555 ON APPROACH TO MSP WITH LANDING GEAR EXTENDED RIGHT MAIN GEAR HAD BOTH RED AND GREEN INDICATIONS. COMPLIED WITH COM PROCEDURES. REMOVED AND REPLACED MAIN GEAR UPLOCK SENSOR IAW 32-61-81, CHECKS GOOD. 2L73 4F A3WE 20040316001122004031600112WP 2004 3 16 UPS04841941 120040129A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, SUBFLOOR INTERCOSTAL IS CRACKED AT STATION 1736 RBL 35. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 3755032 AND SRM 51-1-20D. 2L74 4F RT4A25 20040316001132004031600113WP 2004 3 16 UPS04841942 120040201A53403755849U1 FITTING DOUG DC8 DC871F 302199DWP AFT CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1200 LONG 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755849 AND SRM 51-1-20D. 2L74 4F RT4A25 20040316001152004031600115WP 2004 3 16 UPS04841944 120040129A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 RIGHT STATION 1723 SHEAR TIE AND FRAME SECTION ARE CORRODED BEYOND LIMITS BETWEEN LONG 30R AND 31R. REMOVED, FABRICATED AND REPLACED SHEAR TIE AND FRAME SECTION IAW SRM 53-5-3 FIG 3 AND 53-2-0 FIG 2. 2L74 4F RT4A25 20040316001162004031600116WP 2004 3 16 UPS04841945 120040129A5755 RIB DOUG DC8 DC871F 302199DWP NR 1 SPOILER GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 LEFT WING TRAILING EDGE NR 1 SPOILER OUTBOARD DOWN STOP RIB IS GOUGED BEYOND LIMITS AT XW 90. BLENDED OUT GOUGE, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040316001182004031600118NM 2004 3 16 UPS04441954 120040222A5330 SKIN BOEING747 747256B 1384865NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 SKIN CORROSION AFT OF FWD LOWER CARGO DOOR. 2L74 4F RTA20WE 20040316001192004031600119NE 2004 3 16 UPS04541950 220040218A7200RB211535E4 ENGINE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE LEFT BIRD INGESTION A IPXAEA ENGINE SHUTDOWN UNSCHED LANDING CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01457UP 25478 31394 INSPECTION TYPE: ASE, ENGINE SHUT DOWN FOR BIRD STRIKE NR 1. REPLACED LT ENGINE ASSY PER TC 5002 (RR) PAGE 1-17 & TC5001 (RR) PAGES 1-41. 2L72 4F4 FRTA2NM E12EU 20040316001212004031600121WP 2004 3 16 UPS04841951 120040212A55105640810 BEARING DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LEFT HORIZONTAL STAB HINGE BEARING WILL NOT ACCEPT GREASE. DISASSEMBLED HINGE. FOUND STAB BEARING BORE CORRODED. REPAIRED PER SAA SK 703-677 AND UPS EO DC8-5510-19991-A. 2L74 4F RT4A25 20040316001232004031600123NM 2004 3 16 PCAA0402171 120040223A291082950010209 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM LEAKING A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 EA13981HA 378 FLIGHT 3969 HAD TO DECLARE AN EMERGENCY DUE TO THE CONTENTS OF THE NR 2 HYDRAULIC SYSTEM BEGINNING TO FALL WHILE 20 MILES OUT FROM LGA. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY AND TAXIED OFF THE ACTIVE RUNWAY, THEN WAS TOWED TO THE GATE. MAINTENANCE FOUND THE LANDING GEAR DOWN LINE IN THE RIGHT HAND TOP FUSELAGE AREA TO BE LEAKING. MAINTENANCE INSTALLED TEMP FLEX LINES AND REPLENISHED AND BLED SYSTEM. AIRCRAFT WAS GROUND RUN AND NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040316001252004031600125NM 2004 3 16 PCAA0402173 120040223A21507757352 ACM DHAV DHC8 DHC8102 2809003NM AIR CONDITIONINGFAULTY A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13826EX130642598 389 AIRCRAFT 826EX HAS SHOWN A SEVERAL DAY HISTORY OF THE LAVATORY SMOKE DETECTOR ALARMING. THE DETECTOR WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. THEN THE DETECTOR WOULD ALARM AT A LATER TIME. MAINTENANCE TROUBLESHOT IT DOWN TO THE AIR CYCLE MACHINE PRODUCING ENOUGH FUMES TO TRIP THE DETECTOR ALARM. AIR CYCLE MACHINE WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD. AIR CYCLE MACHINE IN QUESTION WAS ALSO DUE TIME CHANGE. 2H72 4T RTA13NM 20040316001262004031600126NM 2004 3 16 0400296307 120040220A2530 OVEN BOEING747 747451 1384940NM 1B GALLEY ODOR A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01667US 24222 DURING FLIGHT, A SMOKE ODOR EMITTED FROM THE RIGHT OVEN IN GALLEY 1B. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND THE OVEN CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040316001282004031600128NM 2004 3 16 0400306730 120040205A5312 PANEL BOEING747 7472J9F 1384806NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01630US 21668 DURING L-CHECK FOUND CRACK IN CANTED PRESSURE DECK CLOSURE PANEL AT BS 1241. REPAIRED PER EA 67-165097. 2L74 4F RTA20WE 20040316001292004031600129EA 2004 3 16 COMA0460161 120040222A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01819CA 7415 CARGO FLOOR ANGLE AT FS 621 RT SIDE CRACKED. REMOVED DAMAGED AREA OF RIGHT HAND CARGO FLOOR ANGLE. INSTALLED RIGHT HAND REPAIR ANGLE. ALL REPAIR AND FABRICATION WAS IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004, CRJ SRM 51-23-00, CRJ SRM 51-25-06 AND CRJ SRM 51-25-15. 2L72 4F RTA21EA 20040316001312004031600131EA 2004 3 16 COMA0460164 120040216A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01971CA 7145 FRETTING DAMAGE NOTED ON RIGHT LOWER WING ACCESS HOLE CUTOUT AT 650AB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030. 2L72 4F RTA21EA 20040316001322004031600132NM 2004 3 16 04FDEA00514 120040224A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR INOPERATIVE A FDEAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SO25479FE 21461 AFT AIRSTAIR LIGHT ILLUMINATED ON S/O PANEL. COMPLETED QRH. LIGHT WENT OUT AFTER 15 MIN. MEL 24FEB04 06:03 AC RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 05MAR04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2L73 4F RTA3WE 20040316001332004031600133 2004 3 16 SWAA040542 420040221A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR. DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 R2 DOOR EVAC SLIDE DEPLOYED WHEN DOOR WAS OPENED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040316001342004031600134NM 2004 3 16 04FDEA00524 120040227A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR INOPERATIVE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25209FE 22931 AFTER PASSING APPROXIMATELY 11,000 FEET, AFT AIRSTAIR LIGHT ILLUMINATED. AIRCRAFT BEGAN ACCELERATING THRU 250 KIAS. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 08MAR04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2L73 4F RTA3WE 20040316001362004031600136 2004 3 16 UPS04141964 420040226A2565 GIRT BAR AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE STIFF A IPXAK NONE O OTHER ININSP/MAINT 1 SO01149UP 0832 ENTRY DOOR ESCAPE SLIDE HANDLE IS DIFFICULT TO MOVE TO THE DISARM POSITION. ROUGH FEEL CHECK IAW MM 25-61-20-2. GIRT BAR CLEANED AND LUBRICATED, SATISFACTORY. 2L72 4F RTA35EU 20040316001372004031600137 2004 3 16 UPS04141966 420040226A2565 WARNING HORN AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01130UP 0815 INSPECTION TYPE:N/A LEVEL AT FL330 THE SLIDE WARNING HORN BUZZED CONTINUOUSLY. RESET C/B SLIDE WARNING HORN, CHECKS NORMAL. 2L72 4F RTA35EU 20040316001392004031600139NM 2004 3 16 UPS04541960 120040217A5321 FLOOR PANEL BOEING757 75724APF 1384969NM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01408UP 23730 INSPECTION TYPE: C, CORROSION ON MAIN DECK FLOOR WEB SURFACE BS 368-375 RBL 22 WL 208. REPAIRED PER SRM 51-70-13. 2L72 4F RTA2NM 20040316001402004031600140WP 2004 3 16 UPS04841958 120040225A3350 SOCKET DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT LOOSE A IPXAO OTHER L NO TEST ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: ASN, DOOR ENTRY AND EMERGENCY LIGHTING FIXTURE NOT SECURED. SECURED DOOR ENTRY AND EMERGENCY LIGHTING TO HOUSING. 2L74 4F RT4A25 20040316001422004031600142EA 2004 3 16 COMA0460171 120040226A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01979CA 7159 FLIGHT 5745 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040316001432004031600143EA 2004 3 16 COMA0460172 120040226A325016736103 SERVO VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01416CA 7450 FLIGHT 5975 NEW FAIL AND STEERING INOP MESSAGE DURING FLIGHT. REPLACED THE EHSU VALVE. 2L72 4F RTA21EA 20040316001442004031600144EA 2004 3 16 COMA0460173 120040224A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01934CA 7042 FLIGHT 5718 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040316001452004031600145EA 2004 3 16 COMA0470027 120040224A261147388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01368CA1154 10075 FLIGHT 5660 FORWARD AND AFT LAV SMOKE WARNING. REPLACED THE FIDEY CONTROL UNIT. 2L72 4F RTA21EA 20040316001492004031600149 2004 3 16 RAIA00402006 420040204A3197 CONNECTOR EMB 145 EMB145LR 3260212SO GROUND DAMAGED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03818HK 145059 DEN - CONFIG WARNING ON TAKEOFF. MAINTENANCE RESEATED GROUND CONNECTION TO BRAKE PRESSURE SWITCH. 2L72 4T RTT00011AT 20040316001522004031600152EU 2004 3 16 RAIA00402009 120040205A2432407817 BATTERY JETAIRJETSTMJETSTM4101 1500501EU NR 2 MAIN OVERHEATED A RAIAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 CE03571HK1121641 41090 STL - RIGHT BATTERY OVER TEMP INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 MAIN BATTERY. 2L72 4T RTA41NM 20040316001542004031600154SO 2004 3 16 RAIA00402011 120040207A3040 SPRING EMB 145 EMB145LR 3260212SO WINDSHIELD WIPEROUT OF ADJUST A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03814HK 145046 STL - F/O'S WINDSHIELD WIPER MOVING WHEN IN PARK. MAINTENANCE ADJUSTED SPRING TENSION ON F/O'S WIPER MECHANISM. 2L72 4T RTT00011AT 20040316001552004031600155SO 2004 3 16 RAIA00402012 120040208A2760852701 PROXIMITY SENSOR EMB 145 EMB145 3260210SO SPOILERS FALSE INDICATIONA RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03821HK6200 145068 STL- SPOILER OPEN INDICATION DURING TAXI. MAINTENANCE REMOVED AND REPLACED LEFT AFT SPOILER PROX SENSOR. 2L72 4F RTT00011AT 20040316001562004031600156EU 2004 3 16 RAIA00402013 120040209A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION FALSE ACTIVATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03565HK 41082 STL - TAKEOFF CONFIG WARNING FAIL INDICATION ON TAKEOFF. MAINTENANCE TROUBLESHOT BUT COULD NOT DUPLICATE MALFUNCTION. 2L72 4T RTA41NM 20040316001572004031600157EU 2004 3 16 RAIA00402014 120040209A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03573HK 41092 STL - EMERGENCY PATH LIGHTS INOP BETWEEN ROWS 2 TO 5. MAINTENANCE RESECURED LOOSE CONNECTOR AT PATH LIGHT STRIP. 2L72 4T RTA41NM 20040316001582004031600158EU 2004 3 16 RAIA00402015 120040210A2460A2105F PDU JETAIRJETSTMJETSTM4101 1500501EU RIGHT INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03574HK12725883 41093 STL - RIGHT ESSENTIAL BUSS FAILURE INDICATION. MAINTENANCE REMOVED AND REPLACE RIGHT PDU. 2L72 4T RTA41NM 20040316001592004031600159SO 2004 3 16 RAIA00402016 120040211A3260 PROXIMITY SWITCH EMB 145 EMB145 3260210SO RT MLG MALFUNCTIONED A RAIAO OTHER N FALSE WARNING LDLANDING 1 CE03803HK 145077 RIC - DURING LANDING AT BOS RIGHT MAIN GEAR INDICATED NOT LOCKED, RECYCLED AND GOT THREE GREEN INDICATIONS. MAINTENANCE REMOVED AND REPLACED DOWNLOCK PROX SWITCH AND PERFORMED GEAR SWING, CHECK OK. 2L72 4F RTT00011AT 20040316001622004031600162SO 2004 3 16 RAIA00402019 120040217A2810 VALVE EMB 145 EMB145LR 3260212SO RT WING VENT LEAKING A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03823HK 145475 IAD - FUEL LEAKING FROM RIGHT WING VENT DURING CLIMB. MAINTENANCE VERIFIED RIGHT WING VENT VALVE CLOSED. 2L72 4T RTT00011AT 20040316001632004031600163 2004 3 16 RAIA00402020 420040218A34177000700967 ADC JETAIRJETSTMJETSTM4101 1500501EU LEFT INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03550HK15198469 41039 STL - LEFT ADC INOP. MAINTENANCE REMOVED AND REPLACED NR 1 ADC. 2L72 4T RTA41NM 20040316001672004031600167SO 2004 3 16 RAIA00402025 120040223A2760852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO SPOILERS MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03815HK9143 145048 STL - SPOILER AND AIR/GRN FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED AIR/GRN PROX SWITCH. 2L72 4T RTT00011AT 20040316001682004031600168 2004 3 16 061041 420040228A34256229681001 INDICATOR BEECH 1900 1900D 1154162CE COCKPIT FAILED A NSVAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27191CJ UE19 ELECTRICAL FUMES IN COCKPIT, PILOTS EHSI WENT BLANK, TURNED EHSI OFF FUMES WENT AWAY. REMOVED AND REPLACED CAPT EHSI, UNIT HAD BURNED ODOR. NO OTHER DESCREPANCIES NOTED, OP CHECKED GOOD. 2L72 4T RTA24CE 20040316001692004031600169CE 2004 3 16 061042 120040227A5270 WARNING LIGHT BEECH 1900 1900D 1154162CE CARGO DOOR ILLUMINATED A NSVAD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 EA27171CJ UE71 CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT, AIRCRAFT RETURNED TO BLOCK. DEFERRED IN ACCORDANCE MEL 52-2. 2L72 4T RTA24CE 20040316001722004031600172NM 2004 3 16 C1HA20483004 120040227A3350900835A BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 AFT ENTRY PORTABLE EMERGENCY LIGHTS INOP. 2L73 4F A3WE 20040316001732004031600173NM 2004 3 16 UPS04241967 120040210A5752 CASTING BOEING727 72722C 138400FNM I/B RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, SURFACE CORROSION ON I/B RIGHT AILERON TAB HINGE BEARING SUPPORT CASTINGS (BOTH O/B AND MIDDLE CASTINGS). REMOVED I/B AILERON IAW MM 27-10-01. REPLACED CORRODED TAB HINGE SUPPORT CASTINGS IAW SRM 51-30-2. NO WEIGHT CHANGE OCCURRED TO AILERON DURING CASTING REPLACEMENT. 2L73 4F A3WE 20040316001742004031600174NM 2004 3 16 UPS04241968 120040211A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, FUSELAGE SKIN CRACKED AT BS 1354 RT. REPAIRED IAW SRM 51-40-2 FIG 1. 2L73 4F A3WE 20040316001752004031600175NM 2004 3 16 UPS04241969 120040212A5754 WEB BOEING727 72722C 138400FNM KRUGER FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, NR 1 KRUEGER FLAP ACTUATOR TRUNNION CAP SUPPORT WEB I/B & O/B CRACKED. NR 1 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAP SUPPORT WEB IAW SRM 51-20-1. INSTALLED 31 K-FLAP ACTUATOR TRUNNION SUPPORT CAP WEB PER BOEING DRAWING 65-16269. INSTALLED NR 1 K-FLAP ACTUATOR IAW MM 27-81-22. 2L73 4F A3WE 20040316001762004031600176NM 2004 3 16 UPS04241970 120040209A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, SUSPECT CRACK INDICATION AT BS 243.7 WL 216.5. AREA PAINT STRIPPED IAW MM 51-20-01. HFEC INSPECTION CARRIED OUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00. RESULT: CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3. 2L73 4F A3WE 20040316001782004031600178NM 2004 3 16 UPS04241972 120040223A5320 BRACKET BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, BROKEN BRACKET AT BS 1223 LBL 36 AFT AIRSTAIRS EQUIP AREA. REMOVED BROKEN BRACKET IAW OHM 20-50-01. BRACKET FABRICATED IAW SRM 51-20-01 AND INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20040316001792004031600179NM 2004 3 16 UPS04241973 120040213A5753 FLAP TRACK BOEING727 72722C 138400FNM NR 7 FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, NR 7 FLAP TRACK FAIRING I/B TRACK CRACKED. REPLACED TRACK IAW DRW 65-21796 & SRM 51-30-02. 2L73 4F A3WE 20040316001812004031600181NM 2004 3 16 UPS04241975 120040210A3270 SHOCK ABSORBER BOEING727 72722C 138400FNM TAIL SKID CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, TAIL SKID ABSORBER FOUND TO BE CRACKED. REPLACED TAIL SKIN ABSORBER IAW MM 32-71-41 & OHM 32-71-04. 2L73 4F A3WE 20040316001822004031600182NM 2004 3 16 UPS04241976 120040212A5347 SEAT TRACK BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE:C, CORROSION ON SEAT TRACK AT BEARSTRAP LOCK PIN LOCATION, BS 950 RBL 4 5.5. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5. REPAIR CARRIED OUT IAW SRM EO 2004-017-001 UPS ENGINEERING FILE 727-53-20136. 2L73 4F A3WE 20040316001832004031600183NM 2004 3 16 UPS04241977 120040211A5340 FITTING BOEING727 72722C 138400FNM TAIL SKID BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE:C, RIGHT LWR TERMINAL FITTING IN TAIL SKID BAY CRACKED. RIGHT LWR TERMINAL FITTING REPLACED IAW DWG 65-25992. 2L73 4F A3WE 20040316001842004031600184NM 2004 3 16 UPS04241978 120040212A7830 BRACKET BOEING727 72722C 138400FNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, ENGINE NR 1 THRUST REV O/B FAIRING MID SUPPORT BRACKET IS CRACKED. ENGINE NR 1 TR O/B FAIRING MID SUPPORT BRACKET REPLACED IAW MM 78-30-00. 2L73 4F A3WE 20040316001852004031600185NM 2004 3 16 UPS04241979 120040211A5340 FITTING BOEING727 72722C 138400FNM TAIL SKID BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY CRACKED. LEFT UPPER TERMINAL FITTING IN TAIL SKID BAY REPLACED IAW DWG 65-2 5992. 2L73 4F A3WE 20040316001882004031600188NM 2004 3 16 UPS04441981 120040211A5411 FRAME BOEING747 747212B 1384886NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACKS AT O/B FWD AND AFT FRAME WEB. FRAME WEB ATTACH PARTS REINSTALLED PER BS 54-53-34870 AND CONTINUE REPEAT INSPECTION PER RS OR UPS EO SINCE NO FURTHER CRACK PROPAGATION AFTER REPAIR PARTS REMOVED. 2L74 4F A20WE 20040316001932004031600193EU 2004 3 16 RAIA00402021 120040220A3150 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION FALSE ACTIVATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03565HK 41082 STL- TAKEOFF CONFIG WARNING INDICATION DURING TAKEOFF. MAINTENANCE TROUBLESHOT SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTA41NM 20040316001952004031600195NM 2004 3 16 CALA0400177 120040227A5321146A9401 SPLICE BOEING737 737724 13844BYNM FLOOR PANEL CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND AFT CARGO PIT FLOOR PANEL SPLICE CORRODED AT STA 727D. THE FLOOR PANEL SPLICE WAS REPLACED IAW IPC 53-42-11-26. 2L72 4F RTA16WE 20040316001962004031600196NM 2004 3 16 CALA0400178 120040227A5320UNK ANGLE BOEING737 7373T0 1384582NM FUSLEAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN FLOOR SHEAR WEB ANGLE AT STA 384, BL 0. THE SHEAR WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040316001972004031600197NM 2004 3 16 CALA0400179 120040227A573065C26714 SKIN BOEING737 737524 1384721NM RT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723657 28918 INSPECTION FOUND A 2.125 INCH CRACK IN RIGHT WING L/E SKIN AT NR 3 KRUEGER FLAP. THE AREA WAS REPAIRED IAW SRM 57-41-01, FIGURE 203. 2L72 4F RTA16WE 20040316002012004031600201NM 2004 3 16 CALA0400183 120040228A5510180A16121 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723707 28768 INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT TOP ATTACH PIN CORRODED. THE ATTACH PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040316002022004031600202NM 2004 3 16 CALA0400184 120040228A5510180A16121 PIN BOEING737 737724 13844BYNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723707 28768 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT TOP ATTACH PIN CORRODED. THE ATTACH PIN WAS REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040316002042004031600204NM 2004 3 16 CALA0400186 120040228A5510180A16122 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723707 28768 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER AND AFT MIDDLE ATTACH PINS CORRODED. THE ATTACH PINS WERE REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040316002052004031600205NM 2004 3 16 CALA0400187 120040229A5510180A16122 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT MIDDLE AND AFT LOWER FAILSAFE PINS CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696, REV B, OP 1. 2L72 4F RTA16WE 20040316002062004031600206NM 2004 3 16 CALA0400190 120040229A551265C27482 SKIN BOEING737 7373T0 1384582NM LT HOR STAB PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND LT HORIZONTAL STABILIZER LOWER TRAILING EDGE SKIN PANEL PUNCTURED JUST OUTBOARD OF ELEVATOR, BL 215.28. THE PANEL WAS REPAIRED IAW SRM 51-70-05. 2L72 4F RTA16WE 20040316002072004031600207NM 2004 3 16 CALA0400191 120040229A1430180A16112 BOLT BOEING737 737724 13844BYNM LT HOR STAB GALLED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723708 28769 INSPECTION FOUND UPPER BOLT GALLED ON LT HORIZONTAL STABILIZER FORWARD POSITION. THE BOLT WAS REPLACED IAW EA 5510-01696, REV B, OP 1. 2L72 4F RTA16WE 20040316002082004031600208NM 2004 3 16 CALA0400192 120040301A523069455559 STOP FITTING BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719136 29285 INSPECTION FOUND FORWARD CARGO DOOR LOWER STOP FITTINGS NR 2 AND NR 3 CORRODED AT STA 572. THE FITTINGS WERE REPLACED IAW SRM 51-40-02. 2L72 4F RTA2NM 20040315001942004031500194NM 2004 3 15 UPS04441935 120040124A5315 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D - BS 2150 RBL 108 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. CORROSION BLEND OUT 0.030 X 1 X 2 INCH, EXCEED SRM LIMIT. 2L74 4F A20WE 20040316000022004031600002WP 2004 3 16 UPS04841930 120040208A532048887551 ANGLE DOUG DC8 DC871F 302199DWP A/C COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 55, LBL 50 TWO INTERCOSTAL ANGLE SUPPORTS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE SUPPORTS IAW DWG 4888755, 4888754 AND SRM 51-1-21. 2L74 4F RT4A25 20040316000232004031600023NM 2004 3 16 UIEA200400018 120040219A5410 STRUT BOEING747 747243B 1384830NM NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 2 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT WITH CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NAC STATION 235 TO STATION 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F A20WE 20040316000482004031600048 2004 3 16 GTIA040016 420040115A2565 LANYARD DOUG MD80 MD83 3023681NM ESCAPE SLIDE DETACHED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 FLL - FLT 1443 - L1 SLIDE PACK NEEDS TO BE ATTACHED. REINSTALLED L1 SLIDE PACK LANYARD. (M) 2L72 4F RT 20040316000542004031600054WP 2004 3 16 ASAA0480067 120040209A532199365851 INSERT DOUG DC9 DC983 3022083WP FLOOR PANEL DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23976AS 53452 OKC - HV1-CHECK, FOUND CABIN FLOOR PANEL INSERT DAMAGED AT FS 927-1003. REPLACED FLOOR PANEL INSERT PER SRM 53-05. (M) 2L72 4F RTA6WE 20040316000692004031600069 2004 3 16 GTIA040001 420040101A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FGA - FLT 866 - L2 SLIDE PACK NEEDS REATTACHMENT. REATTACHED L2 SLIDE PACK. (M) 2L72 4F A6WE 20040316000702004031600070 2004 3 16 GTIA040003 420040101A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FLL - FLT 1581 - L2 SLIDE PACK CAME OFF DOOR UPON LANDING. L2 SLIDE PACK WAS REINSTALLED. (M) 2L72 4F A6WE 20040316000752004031600075EU 2004 3 16 ASOA04094 120040122A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11536AS 465 DURING A C-CHECK IN BNA, THE LEFT SEAT TRACK ON TOP AND BOTTOM BETWEEN FS 39 TO FS 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FS 39 TO FS 41 IAW SRM 51-25-02 AND 51-25-04. (M) 2H72 4T RTA53EU 20040316000782004031600078EU 2004 3 16 SIMA200402002 120040119A55127255150521 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. SKIN REPLACEMENT DONE IAW SAAB REPAIR STATEMENT 340-SDS-006500 AND STANDAR SRM PRACTICES. (M) 2L72 4T RTA52EU 20040316001142004031600114WP 2004 3 16 UPS04841943 120040131A532057585421 INTERCOSTAL DOUG DC8 DC871F 302199DWP AC. COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 55 LBL 50 INTERCOSTAL IS CRACKED BELOW CEILING. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5758542 AND SRM 51-1-20D. 2L74 4F RT4A25 20040316001242004031600124NM 2004 3 16 PCAA0402172 120040221A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY FAULTY A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13835EX205101003 289 FLIGHT 3982 CREW REPORTED THAT THE NR 2 BAGGAGE BAY SMOKE DETECTOR WOULD NOT TEST. ITEM WAS DEFERRED AFTER VERIFICATION THAT THE NR 1 WAS IN OPERATING ORDER. ONCE IN MAINTENANCE THE DETECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040316001272004031600127NM 2004 3 16 0400283141 120040214A2121EVT3454 COOLING FAN AIRBUSA319 A319114 3930350NM E/E BAY SEIZED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01341NB5144 5144 01738 RECEIVED VENT EXTRACT FAULT IN FLIGHT FOLLOWED BY SMOKE IN THE COCKPIT AND CABIN. FOLLOWED COCKPIT OPERATING MANUAL AND ECAM PROCEDURE. DIVERTED TO RNO AND LANDED WITHOUT INCIDENT. FOUND THE AVIONICS COOLING EXTRACT FAN SEIZED. APPLIED MEL 21-26-02A PROVISIONS AND RETURNED AIRCRAFT TO SERVICE. REPLACED THE EXTRACT FAN DURING OVERNIGHT LAYOVER AT MSP. 2L72 4F RTA28NM 20040316001352004031600135EU 2004 3 16 UPS04141963 120040226A3240 BRAKE AIRBUSA300 A300F4622R 3930360EU MLG INOPERATIVE A IPXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01150UP 0833 TAXIING TO PARK, NORMAL BRAKING FAILED. SWITCHED TO ALT BRAKE, BRAKE CAME ACTIVE RIGHT AWAY. TAXI WAY WAS COVERED WITH ICE. NORMAL BRAKE SYSTEM CHECK IAW MM 32-43-00-5 SATISFACTORY. 2L72 4F RTA35EU 20040316001412004031600141NM 2004 3 16 0400316314 120040226A2530 OVEN BOEING747 747451 1384940NM GALLEY SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01674NW 30269 DURING FLIGHT, SMOKE EMITTED FROM THE NR 3 OVEN IN THE NR 3 GALLEY CAUSING THE CIRCUIT BREAKER TO TRIP. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OVEN CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040316001482004031600148SO 2004 3 16 RAIA00401055 120040124A2150 WARNING LIGHT EMB 145 EMB145LR 3260212SO LT A/C PACK ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03812HK 145373 PIT - LEFT PACK OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 1 PACK, PER MEL. SUBSEQUENTLY CLEANED DMI BY CLEANING DE-ICE FLUID FROM APU BLEED SYSTEM. 2L72 4T RTT00011AT 20040316001512004031600151SO 2004 3 16 RAIA00402008 120040205A3020129482 PRESSURE SWITCH EMB 145 EMB145 3260210SO ANTI ICE SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03820HK349 145064 CLT - LEFT ENGINE ANTI-ICE VALVE FAILED TO OPEN ON TEST. MAINTENANCE DEFERRED NR 1 ENGINE ANTI-ICE PER MEL SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI-ICE PRESSURE SWITCH. 2L72 4F RTT00011AT 20040316001642004031600164EU 2004 3 16 RAIA00204021 120040220A3150 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CONFIGURATION FALSE ACTIVATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03565HK 41082 STL - TAKEOFF CONFIG WARNING INDICATION DURING TAKEOFF. MAINTENANCE TROUBLESHOT SYSTEM WITH NO DEFECTS NOTED. 2L72 4T RTA41NM 20040316001652004031600165SO 2004 3 16 RAIA00402022 120040222A2741 CONTROL UNIT EMB 145 EMB145LR 3260212SO STAB TRIM MALFUNCTIONED A RAIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE03825HK 145510 STL - MAIN PITCH TRIM INOP. MAINTENANCE RE-RACKED HORIZONTAL STAB CONTROL UNIT AND CHECKED OK. 2L72 4T RTT00011AT 20040316001702004031600170NM 2004 3 16 C1HA20043005 120040227A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT DISCHARGED A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 L-PORTABLE EMERGENCY LIGHTS INOP. 2L73 4F A3WE 20040316001772004031600177NM 2004 3 16 UPS04241971 120040212A5522 SKIN BOEING727 72722C 138400FNM RT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, X-RAY INSPECTION OF RIGHT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED ON PANEL ELEVATOR STA 136.5 TO 173.21. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-20-3, 51-40-5, 55-20-3, 51-30 -026, 51-10-02 & DRG 65-25638. 2L73 4F A3WE 20040316001902004031600190NM 2004 3 16 UPS04441983 120040210A5320 REVEAL BOEING747 747212B 1384886NM NR 4 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: C, M/D - LEFT NR 4 DOOR CUTOUT FWD LOWER BET S24-25L, CUTOUT REVEAL FOUND CRACK AS MARKED. CUTOUT REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84 AND HX RS R-53-62-35110, CRACKS STOPPED AT FASTENER HOLE FROM EDGE CONFIRMED BY NDT INSPECTION, SURROUNDING STRUCTURE IS CORROSION & DAMAGE FREE AFTER INSPECTED UPS ENGINEERING FILE 747-53-20171. 2L74 4F A20WE 20040316001912004031600191NM 2004 3 16 UPS04441984 120040219A5740 FITTING BOEING747 747212B 1384886NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: C, RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -A- FOUND CORROSION INSIDE FASTENER HOLE. CORROSION REMOVED AND HOLE -A- FREEZE PLUG INSTALLED AS PER RS R-57-12-35115 AND UPS EO B747-5710-20028-A. 2L74 4F A20WE 20040316001982004031600198NM 2004 3 16 CALA0400180 120040227A5320 FLOOR SUPPORT BOEING737 737724 13844BYNM CARGO BAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND FLOOR SUPPORT IN AFT PIT CORRODED AT STA 787-847, RBL 13.84. THE FLOOR SUPPORT WAS REPAIRED IAW ECRA 5321-01173. 2L72 4F RTA16WE 20040316002002004031600200NM 2004 3 16 CALA0400182 120040228A5320149A810921 FLOOR SUPPORT BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT BRACKET AT STA 867 IN AFT PIT. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-20. 2L72 4F RTA16WE 20040316002092004031600209NM 2004 3 16 CALA0400193 120040301A552265C25746142SP SKIN BOEING737 737524 1384721NM RT ELEVATOR PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724633 27901 INSPECTION FOUND A PUNCTURE IN THE RT ELEVATOR UPPER SKIN AT ELEVATOR STA 137.59. THE ELEVATOR SKIN WAS REPAIRED IAW ECRA 5520-01339. 2L72 4F RTA16WE 20040316002132004031600213 2004 3 16 SWIA200412924 420040215A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLIGHT CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07459SW6828 6821 7782 DURING CLIMBOUT YAW DAMPER 2 DISENGAGED AND WOULD RESET FOR 2 TO 5 MINUTES AND THEN DISENGAGE. REMOVED AND REPLACED FCC 2 IAW 22-12-14. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040316002142004031600214EA 2004 3 16 04058653 120040227A2701 YOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT INTERFERENCE A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27653BR 7438 DURING AIRCRAFT OPERATION THE CREW REPORTED A SLIGHT BUMP IN YOKE MOVEMENT WHEN ROTATING FROM LEFT TO RIGHT. A SATISFACTORY FUNCTIONAL CHECK OF THE YOKE WAS PERFORMED AND NO DEFECTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040316002152004031600215EA 2004 3 16 04058661 120040228A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27661BR 7520 DURING INSPECTION THE ORANGE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLY AND BATTERY WERE FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040316002162004031600216EA 2004 3 16 04058626 120040227A3320 BULB CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAILED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA27626BR 7225 DURING AIRCRAFT OPERATION THE CREW REPORTED A LAVATORY SMOKE WARNING. THE RETURN TO SEAT SIGN IN THE LAVATORY WAS FOUND TO BE MALFUNCTIONING AND THE BULB WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040316002172004031600217NM 2004 3 16 04058410 120040227A5610 SCREW DORNERDO32 DO328300 NM WINDSHEILD LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27410FJ 3165 DURING FLIGHT THE CREW REPORTED A LOUD WIND NOISE IN THE COCKPIT. THE FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE WINDSHIELD WAS INSPECTED AND A SCREW WAS FOUND LOOSE AND SUBSEQUENTLY TIGHTENED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040316002182004031600218EU 2004 3 16 04059315 120040228A3397 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27315UE 41033 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT ROW 8. A CONNECTOR WAS FOUND LOOSE AND TIGHTENED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040316002202004031600220NM 2004 3 16 2004UALA00157 120040223A7932 TRANSMITTER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 ENG OIL QTYMALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29804UA 759 FLIGHT DIVERTED DUE TO LOW NR 2 ENGINE OIL INDICATION. REPLACED OIL QUANTITY TRANSMITTER. 2L72 4F4 FRTA28NM E40NE 20040316002212004031600221NM 2004 3 16 2004UALA00158 120040223A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP2976UA 24641 HORIZONTAL WEB AT STA 194 AND STR 17 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20040316002242004031600224NM 2004 3 16 2004UALA00161 120040224A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29544UA 25322 AFT EXT FUSELAGE SKIN UNDER CARGO PIT DOOR AT STA 1420 STR 28R IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040317000012004031700001SO 2004 3 17 CHQA000434 120040203A3610CRA56320T COUPLING EMB 145 EMB145LR 3260212SO PNEUMATC SYS SEPARATED A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11562 4388 145451 DURING CLIMBOUT OF CMH PASSING THROUGH 3000 FT, ENTERED ICING CONDITIONS, ANTI-ICE SYSTEM CAME ON AND HEARD A LOUD THUD SOUND. BLD 2 LK APPEARED ON EICAS AND DID NOT GO OUT. SHUT NR 2 ENGINE DOWN IN FLIGHT. FLIGHT ATTENDANT ADVISED, SMELLED BURNING ODOR. DECLARED EMERGENCY AND RETURNED TO CMH. ON APPROACH GOT ANTI-ICE INOP, WG-ICE FAIL, AND STAB ICE FAIL MSGS. MADE OVERWEIGHT LANDING AND THEN EVACUATED AIRCRAFT. NO INJURIES. MAINTENANCE FOUND GAMAH COUPLING BLOWN OFF PNEUMATIC DUCT OVER RIGHT WING FAIRING. REMOVED AND REPLACED COUPLING. LEAK CHECK GOOD. OVERWEIGHT INSPECTION PERFORMED AND NO DAMAGE OR DEFECTS NOTED. ALL SYSTEMS CHECK GOOD. 2L72 4T RTT00011AT 20040317000022004031700002NM 2004 3 17 F3LA200400010 120040211A5330 SKIN BOEING737 7373S1 138447SNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED RT FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF R-1 DOOR CUTOUT. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-10-01 FIG 202. 2L72 4F RTA16WE 20040317000032004031700003NM 2004 3 17 372PA0041 120040216A3350 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. DRIED MOISTURE FROM FLOOR PATH LIGHTING AND OPS CHECKED OK. 2L72 4F RTA16NE 20040317000052004031700005NM 2004 3 17 249TR0023 120040219A3350S106CD BATTERY BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. OPS CHECKS NORMAL PER MM 33-51-51. 2L72 4F RTA16WE 20040317000062004031700006 2004 3 17 371PA0036 420040217A22102A72004 ACTUATOR BOEING737 737306 13844BGNM MACH TRIM MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05371PA 23543 DURING LEVEL CRUISE WITH AUTOPILOT A OR B ENGAGED, AIRCRAFT OCCASIONALLY GAINED 150 FT ALTITUDE WHILE ALTITUDE HOLD MODE ENGAGED. REPLACED MACH TRIM ACTUATOR PER MM 22-21-11. 2L72 4F RTA16NE 20040317000092004031700009NE 2004 3 17 P5CA0401042 220040219A7230 COMPRESSOR BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE STALLED A P5CAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP23920FT 22237 702114 NR 3 ENG COMPRESSOR STALL. ENG SHUTDOWN. REPLACED ENG PER WIC M7100-002 / M7100-011. ENG RUN & OPS CHECK NORMAL. 2L74 4F4 F A20WE E3NE 20040317000102004031700010NM 2004 3 17 P5CA0401043 120040221A34110856CC12 PITOT HEAD BOEING747 747283B 1384867NM RIGHT FAULTY A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23921FT 21575 RIGHT AUX PITOT PROBE FAULT LIGHT ON. REMOVED AND REPLACED RIGHT AUX PITOT PROBE GROUND TEST & LEAK CHECK OK. 2L74 4F A20WE 20040317000112004031700011NM 2004 3 17 219PA0012 120040220A33506104781 BATTERY PACK BOEING737 737222 1384473NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05219PA 19956 BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED OVERWING BATTERY PACKS. OPS CHECKS GOOD PER MM 33-50-00. 2L72 4F A16WE 20040317000122004031700012 2004 3 17 737DX0003 420040220A2210R1053M182 LIMITER BOEING737 737400 138449ANM AILERONS MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05737DX 24804 AILERON FORCE LIMITER FAILED LRU INTERFACE TEST 50 PERCENT OF THE TIME. REPLACED AILERON FORCE LIMITER PER MM 22-11-13. OPS CHECKS GOOD PER MM 22-11-13. 2L72 4F RTA16WE 20040317000132004031700013SO 2004 3 17 CHQA0000436 120040223A2120 UNKNOWN EMB 145 EMB145LR 3260212SO CABIN/COCKPIT ODOR A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11294 145497 BURNING RUBBER OR PLASTIC ODOR INFLIGHT FOR ABOUT 2 MINUTES. SMELLED IT IN COCKPIT FIRST AND FLIGHT ATTENDANT AND PASSENGERS SMELLED IT AS WELL. ONLY LASTED 2 MINUTES. WE WERE IN CLOUDS WITH LIGHTENING IN THE AREA. MCO MAINTENANCE THOROUGHLY CHECKED THE AIRCRAFT OUT FOR EVIDENCE OR CAUSE OF THE BURNING ODOR. NOTHING WAS FOUND AT ALL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040317000142004031700014NM 2004 3 17 F3LA200400015 120040220A5320 WEB BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED RT TOILET SUPPORT WEB CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-60-51. REMOVED RT AFT TOILET WEB SUPPORT. FABRICATED REPLACEMENT WEB PER BOEING DRAWING 65C72707. ALODINED REPLACEMENT WEB PER MM 51-21-41. PRIMED AND PAINTED PER SOPM 20-44-02. INSTALLED REPLACEMENT WEB PER SRM 51-40-02. 2L72 4F RTA16WE 20040317000152004031700015NM 2004 3 17 F3LA200400016 120040220A5320 WEB BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED LT TOILET SUPPORT WEB CORRODED. CORROSION FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-60-51. REMOVED DAMAGED LT AFT TOILET SUPPORT WEB. FABRICATED REPLACEMENT WEB PER BOEING DRAWING 65C32707. ALODINED REPLACEMENT LT AFT TOILET SUPPORT WEB PER MM 51-21-41. PRIMED AND PAINTED PER SOPM 20-44-02. INSTALLED REPLACEMENT WEB PER SRM 51-40-02. 2L72 4F RTA16WE 20040317000172004031700017NM 2004 3 17 757BJ0005 120040224A335020131A BATTERY PACK BOEING757 757236 1384971NM EMERGENCY LIGHTSINOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05757BJ 22176 R2 EMERGENCY EXIT LIGHTS INOP. REPLACED R2 DOOR EXIT LIGHT BATTERY PACK PER MM 33-51-07. OPS CHECKS GOOD. 2L72 4F RTA2NM 20040317000202004031700020NM 2004 3 17 2004UALA00164 120040223A5320 WEB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29376UA 24641 STA 194 HORIZ WEB AT STR 17 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20040317000242004031700024NM 2004 3 17 2004UALA00168 120040226A5230 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 AFT CARGO DOOR LOWER SKIN DAMAGED AT EDGE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FILLER AND DOUBLER. 2L74 4F4 FRTA20WE E24NE 20040317000252004031700025NM 2004 3 17 2004UALA00169 120040225A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29389UA 24664 LEFT FUSELAGE SKIN HAS 3 EA SMALL DENTS BETWEEN STA 1010 AND 1016 AND STR 12L &13L. MAJOR REPAIR ACCOMPLISHED. REPLACED FUSELAGE SKIN. 2L72 4F4 FRTA16WE E2GL 20040317000292004031700029NM 2004 3 17 2004UALA00173 120040227A5753 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29543UA 25698 TRAILING EDGE FLAPS SKIN HAS DAMAGE AND IS DELAMINATED. REPLACED THE TRAILING EDGE WEDGE. 2L72 4F4 FRTA2NM E17NE 20040317000332004031700033WP 2004 3 17 ABXA040085 120040227A2913AS66411LS666 PUMP DOUG DC9 DC932 3022066WP LT ENG HYD SYS INOPERATIVE A ABXAO OTHER S AFFECT SYSTEMS CRCRUISE 1 GL23900AX3047 47380 LEFT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT INTO BTV. REPLACED LEFT ENGINE HYDRAULIC PUMP ON LEFT ENGINE IAW DC-9 AMM 29-10-05-2-0001. OPS AND LEAK CHECKED GOOD. ALSO INSPECTED FLUID IN PUMP, ALL CLEAN, '0' CONTAMINANTS. REPLACED LEFT ENGINE CASE DRAIN FILLER ELEMENT AS PRECAUTIONARY IAW DC-9 AMM 29-10-24-0006. LEAK CHECKED GOOD. 2L72 4F A6WE 20040317000352004031700035WP 2004 3 17 ABXA040087 120040223A534037558471 FITTING DOUG DC8 DC861 3021952WP DOOR FRAME CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23853AX 46037 NR 3 PIT, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB FITTING WAS FOUND CRACKED DURING A LINE INSPECTION. REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F 4A25 20040317000372004031700037WP 2004 3 17 ABXA040080 120040217A5420591326211 ANGLE DOUG DC9 DC931 3022065WP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23908AX 47008 LEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04. 2L72 4F A6WE 20040317000392004031700039NE 2004 3 17 04FDEA00525 220040227A7200 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 3 VIBRATION A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO25223FE 20935 EXCESSIVE VIBRATION AND GRINDING SOUND ON NR 3 ENG POWER LEVER, INCREASES WITH SPEED AND ALTITUDE. ENGINE NR 3 USED 1 GALLON OF OIL DURING THE 1 HOUR PLUS 15 MIN FLIGHT. C/W ENGINE BORESCOPE PER W/C 7200-5005. NO DEFECTS NOTED. 2L73 4F4 FRTA3WE E2EA 20040317000402004031700040NM 2004 3 17 04FDEA00526 120040229A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) AT HINGE BRACKET AFT SIDE FOUND TEE CHORD CRACKED. REPAIR CARRIED OUT AS PER EA 1-5750-74329, WINGS - FLAP ASSEMBLIES - TEE CHORD FABRICATION. 2L73 4F RTA22WE 20040317000422004031700042NM 2004 3 17 04FDEA00528 120040229A5320 STIFFENER DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER HAVE CRACK LINE. COMPLIED FEDEX EA 1-3210-75908, LANDING GEAR - MAIN GEAR AND DOORS - PART FABRICATION. RT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040317000432004031700043NM 2004 3 17 04FDEA00530 120040229A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) NR 3 FRAME AFT FOUND SUPPORT BRACKET CRACKED. FABRICATED NEW TEE AS PER DRAWING NR ARC 0544. LT WING OUTBOARD TRAILING EDGE FLAP INBOARD HINGE (WING SIDE) 3 FRAME AFT SUPPORT BRACKET REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040317000492004031700049NM 2004 3 17 04FDEA00542 120040302A5754 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING SLAT TRACK 16 I/B SUPPORT RIB FOUND CRACKED. LT WING SLAT TRACK NR 16 I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. 2L73 4F RTA22WE 20040317000502004031700050WP 2004 3 17 0400339155 120040228A2133 LINE DOUG DC9 DC914 3022034WP OUTFLOW VALVE BROKEN A NWAAB EMER. DESCENT JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 GL018914E 45831 AT FL330, THE CABIN BEGAN TO CLIMB AT 500 FPM AND COULD NOT BE CORRECTED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT AND THEN WAS ABLE TO CLIMB BACK TO A HIGHER ALTITUDE IN STAGES. EVENTUALLY THE AIRCRAFT HAD TO DESCEND BACK DOWN TO 17,000 FT TO MAINTAIN CABIN PRESSURE. OUTFLOW VALVE WAS CLOSED AT ALL TIMES. MAINTENANCE FOUND A BROKEN SENSE LINE FROM THE RIGHT FLOW CONTROL VALVE AND REPLACED IT. ALSO, CLEANED THE CABIN TEMP SENSOR PICKUP. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040317000542004031700054NM 2004 3 17 04060411 120040229A3350 CONNECTOR DORNERDO32 DO328300 NM EMERGENCY LIGHT LOOSE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27411FJ 3166 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING AT ROW 9A WAS FOUND INOPERATIVE. A LOOSE CONNECTOR WAS FOUND AND RESECURED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040317000552004031700055EA 2004 3 17 04061673 120040301A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27673BR 7599 DURING INSPECTION THE RIGHT HAND FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040317000562004031700056EU 2004 3 17 04061303 120040301A5514 PANEL JETAIRJETSTMJETSTM4101 1500501EU EMPENNAGE CRACKED A VTZAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA27303UE 41015 DURING AIRCRAFT OPERATION THE CREW REPORTED A LOUD THUMPING ON THE RIGHT SIDE NOSE OF THE AIRCRAFT. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE LEFT HAND VERTICAL STABILIZER TO HORIZONTAL STABILIZER FILLET PANEL WAS FOUND CRACKED AND WAS REPAIRED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040317000572004031700057NM 2004 3 17 DL73S040162 120040217A33103186304951007 LIGHT BOEING737 737247 138448DNM INDICATOR BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27376DL 23603 WHILE WORKING MCO ON ANTI SKID LIGHTS STAYING ON DIM. FOUND WINDSHEAR AND ALTITUDE ALERT LIGHT ASSEMBLIES WITH ELECTRICAL BURNS AND ODOR. REPLACED ASSEMBLIES. 2L72 4F A16WE 20040317000582004031700058NM 2004 3 17 DLM88040163 120040216A2432203BC1021 CHARGER DOUG MD88 MD88 3023688NM E/E BAY UNSERVICEABLE A DALAH DEACTIVATE SYST/CIRCUITS MJ OVER TEMP WARNING INDICATION ININSP/MAINT 1 SO27994DL 53346 SMOKE FROM DRAIN HOLE OF E & E COMPARTMENT. FOUND BATTERIES BEING OVERCHARGED. REPLACED LEFT AND RIGHT BATTERIES, BATTERY CHARGER AND BATTERY CHARGER CIRCUIT BREAKER AS PER AMA BULLETIN 04-T1. PERFORMED BATTERY CHARGER SYSTEM TEST PER M/M 24-30-02-201, CHECK GOOD. 2L72 4F RTA6WE 20040317000642004031700064NM 2004 3 17 DL73S040170 120040218A533065458001206 SKIN BOEING737 737232 1384475NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 THE UPPER SKIN OF THE S19R WAS FOUND DENTED. DENTED WAS REMOVED AND REPAIR INSTALLED IAW 386089-14. 2L72 4F RTA16WE 20040317000662004031700066NM 2004 3 17 DL73S040173 120040218A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27380DL 23607 THE FUSELAGE SKIN WAS FOUND WITH A .25 INCH CRACK AT THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING (R2 DOOR). THE CRACK WAS REMOVED WITH A 1 INCH CUTOUT IN THE SKIN AND BONDED DOUBLER. THE CUTOUT WAS REPAIRED WITH EXTERNAL STEEL REPAIR DOUBLER PER ER/A 088604-14, REV B. 2L72 4F A16WE 20040317000672004031700067NM 2004 3 17 DL73S040175 120040219A5550 ATTACH FITTING BOEING737 737247 138448DNM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 CORROSION WAS NOTED ON THE VERT STAB ATTACH LUGS, ON THE AFT FACE OF THE NR 6 FIN LUG. CORROSION REMOVED AND LUG REWORKED PER ERA 386225-14. 2L72 4F A16WE 20040317000682004031700068NM 2004 3 17 DL76L040176 120040217A5730112T400037 SKIN BOEING767 767332 1382001NM LT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27171DN 24759 THE LOWER WING SKIN ON THE LT WING WAS FOUND WITH WEAR DAMAGE AT LBL 103 FROM THE REAR SPAR EXTENDING TO THE FRONT SPAR. THE WEAR WAS DUE TO CONTACT WITH UNDERWING FAIRING STRUCTURE. THE DAMAGE WAS MACHINED SMOOTH, INSPECTED, ROTO PEENED, AND SURFACE FINISHES RESTORED. THE REPAIR WAS ACCOMPLISHED PER ER/A 088560-14. 2L72 4F RTA1NM 20040317000722004031700072NM 2004 3 17 DL764040181 120040220A2781 WARNING LIGHT BOEING767 767432ER 1385134NM SLATS ILLUMINATED A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27839MH 29712 CREW DECLARED AN EMERGENCY DUE TO L/E SLAT ASSYM ON APPROACH INTO CVG. T/S PER FIM 27-81-00. PSEU HAS NO SENSOR FAULTS, RAN PSEU PER FIM 32-09-03. NO FAULTS SHOWN, DUE TO HISTORY OF S301 SENSOR FAULT, CKD RESISTANCE OF S301 AND FOUND WITHIN LIMITS. MEGGED WIRE FROM S301 TO PROX BOX NO SHORTS TO GND OR BETWEEN. REPLACED PSEU PER M/M. RAN FLAPS/SLATS, NO PROBLEMS NOTED. C/W MSU INSTALLED GOLD PINS IN POS 7 AND 8 ON D4378J, NO RII REQUIRED PER TOPP 40-30-05. 2L72 4F RTA1NM 20040317000732004031700073NM 2004 3 17 DL76L040183 120040220A2120 DUCT BOEING767 767332 1382001NM E/E BAY LOOSE A DALAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO27174DN 24802 IN CLIMBOUT AT FL270 OVERHEAT LIGHT CAME ON IN STAY-BY MODE AS PER QRH SWITCHED TO OVERRIDE. AFTER 2-3 MIN NO COOLING LIGHT CAME ON. FOUND DUCT SEPARATED FWD OF EQUIP COOLING SUPPLY CHECK VALVE LOCATED IN THE FWD CARGO COMPT LEFT SIDEWALL AREA. RESECURE DUCT OVERRIDE VLV V140 AND SYS INTERCONNECT VLV V90 CK OK I OVERRIDE MODE. STANDBY MODE CKD OK. ATLMA NOTIFIED. SEE ITE 005 THIS SVC FOR AUTO MODE OPS CK. 2L72 4F RTA1NM 20040317000772004031700077NM 2004 3 17 DLM88040187 120040223A3150 SWITCH DOUG MD88 MD88 3023688NM THROTTLE OUT OF ADJUST A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27955DL 49886 GEAR UNSAFE LIGHTS (3) WITH GEAR HANDLE UP AFTER TAKEOFF. AURAL WARNING TOO. AFTER LEVEL OFF AT 5000 FT WARNINGS INTERMITTANT. FOLLOWED POM GEAR UNSAFE LIGHT GEAR HANDLE UP CHECKLIST. GEAR LIGHTS 3 GREEN AFTER GEAR HANDLE RETURNED TO DOWN POSITION. FOUND RT THROTTLE SWITCH PACK OUT OF ADJUST. ADJUSTED PER AMM. SWUNG GEAR, CHECKS NORMAL. 2L72 4F RTA6WE 20040317000802004031700080NM 2004 3 17 DL73S040191 120040225A291772909 REGULATOR BOEING737 737232 1384475NM HYD RESERVOIR LEAKING A DALAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27329DL 23101 LOSS OF A-SYSTEM HYDRAULIC PRESSURE. FOUND NO RESERVOIR HEAD PRESSURE. REPLACED RESERVOIR PRESSURE REGULATOR AND BOTH CHECK VALVES. 2L72 4F RTA16WE 20040317000822004031700082NM 2004 3 17 DL73S040193 120040226A3230 ACCESSORY UNIT BOEING737 737232 1384475NM LT MLG FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27319DL 23091 ON T/O WHEN GEAR HANDLE RAISED LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ON. NO OTHER ABNORMAL INDICATIONS. REPLACED LANDING GEAR ACCESSORY UNIT. 2L72 4F RTA16WE 20040317000842004031700084NM 2004 3 17 DLM90040195 120040227A3350OL3071PEGL LAMP DOUG MD90 MD9030 3023690NM EMERGENCY LIGHT BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27909DA 53389 FIVE EMERGENCY TRACK LIGHTS AT SEAT 10 ABC INOPERATIVE. RELAMPED, CHECKS GOOD. 2L72 4F RTA6WE 20040317000872004031700087NM 2004 3 17 DL73S040198 120040228A2597 CONNECTOR BOEING737 737247 138448DNM COFFEEMAKER SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27238WA 223 23186 FLT ATTENDANT REPORTED EGG ODOR WHICH DEVELOPED INTO AN ELECTRICAL BURNING ODOR. ENGINES WERE OFF AND APU RUNNING WITH PACKS ON. FOUND ODOR EMINATING FROM AFT GALLEY COFFEE DISPENSER. REPLACED AND OPERATED BOTH DISPENSERS. FOUND NR 2 DISPENSER CONNECTOR SHORTED, NR 1 CHECKS OK. CAPPED CONNECTOR AND PULLED C/B FOR NR 2 DISPENSER, NEED CONNECTOR P/N 253204211 AND POTTING COMPOUND 033201107. WDM REF 25-31-94 FWD NR 2 DISPENSER TO MCO AND PLAC PER MEL 25-00-10A. 2L72 4F A16WE 20040317000902004031700090 2004 3 17 DL76L040202 420040229A3417341080159 ADC BOEING767 767332 1382001NM COCKPIT FAULTY A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27171DN 24759 F/O ALTIMETER OFF FLAG. SWITCHING TO ALTN ADC CLEARS PROBLEM. REPLACED RIGHT AIR DATA COMPUTER, OPS CHECK OK. 2L72 4F RTA1NM 20040317000912004031700091NM 2004 3 17 DL73S040203 120040301A53306546881119 SKIN BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 A TIME LIMITED REPAIR WAS REMOVED FROM BS 1025 NEAR S25R, NEARBY ADDITIONAL DAMAGE WAS NOTED (EG, DENTS AND GOUGES). DENTS AND GOUGES WERE CUTOUT AND A PERMANENT REPAIR INSTALLED PER ERA 386109-14. 2L72 4F A16WE 20040317000942004031700094NM 2004 3 17 DL73S040206 120040227A53306545770565 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27332DL 23104 THE STRINGER 4L & 4R SKIN LAP JOINTS WERE FOUND WITH SEVERAL CRACKS BETWEEN FS 540 & 727 WHEN INSPECTED PER AD 2003-08-15. THE CRACKED LAP JOINTS WERE CUTOUT IN THEIR ENTIRETY AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53A1177 AND PER ER/A 386137-14AD. 2L72 4F RTA16WE 20040317000992004031700099NM 2004 3 17 513NA0002 120040229A1430B757MLG BOLT BOEING757 7572T7 1384914NM WHEEL MISSING A PIDAK NONE O OTHER ININSP/MAINT 1 SO05513NA 23895 MAIN WHEEL BOLTS MISSING. REPLACED NR 8 MAIN TIRE (WHEEL ASSEMBLY) PER MM 32-45-01. 2L72 4F RTA2NM 20040317001022004031700102NM 2004 3 17 04FDEA00536 120040301A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25281FE 22348 GOUGE IN EXTERNAL FUSELAGE SKIN AT BS 1054 AT STRINGER 28R. REMOVED DAMAGE AREA OF SKIN. FABRICATED REPAIR DOUBLER. ALODINE AND PRIMED AREA OF SKIN COMMON TO REPAIR AND PRIMED REPAIR. INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F RTA3WE 20040317001032004031700103NM 2004 3 17 P5CA0401046 120040226A524565B1054626 DOOR BOEING747 747249F 1384849NM ACM SERVICE BROKEN A P5CAO OTHER O OTHER LDLANDING 1 WP23920FT 22237 RT SIDE FORWARD NR 3 ACM SERVICE DOOR OPENED ON APPROACH. REMOVED BROKEN DOOR, REPLACED WITH SERVICEABLE DOOR IAW 52-48-01 AMM. 2L74 4F A20WE 20040317001052004031700105NM 2004 3 17 UPS04241991 120040212A5520 SKIN BOEING727 72722C 138400FNM RT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, X-RAY INSPECTION OF RT ELEVATOR SHOWS 2 CRACK INDICATIONS ON BEADED SKIN, PREVIOUSLY STOP DRILLED ON PANEL ELEV STA 136.5 TO 173.21. HFEC CARRIED OUT. CRACKS CONTAINED WITHIN STOP DRILLED HOLES. REPAIR DOUBLERS FABRICATED IAW SRM 55-20-3. BONDED TO PANEL IAW SRM 51-40-5. REPAIRS RIVETED IAW SRM 55-20-3 FIG 3 AND SRM 51-30-026. RT ELEV BALANCE CALCULATED IAW SRM 51-80-07. 2L73 4F A3WE 20040317001062004031700106NM 2004 3 17 UPS04441990 120040209A5730 SKIN BOEING747 747212B 1384886NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: C, RIGHT WING UPPER SURFACE T/E RABBET AREA STRAP PNL BULGED UP AT 20 INCHES O/B OF ROOT AREA. CORROSION BLEND OUT 11.5 X 1, DEPTH .115 TO .62, ORI .332 TO .328. FPI C/O SOPM 20-20-02 AT REWORK AREA CORROSION FREE NDT INSPECTED, NIL FINDING. SHOT PEENING C/O. FASTENER REINSTALLED PER RS 57-25-35116. REINSPECTION TO BE ACCOMPLISHED AT 20000 FLIGHT CYCLES DUE TO THIS REPAIR IS AN INTERIM REPAIR UPS EO B747-5710-20053-A. 2L74 4F A20WE 20040317001072004031700107WP 2004 3 17 UPS04841989 120040223A572037517382 PAD DOUG DC8 DC873F 302199FWP RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01805UP 46117 DROP CORROSION ABOVE WING BOTTLE BOLT, LOCATED IN RIGHT W/W FWD BULKHEAD, UPPER O/B CORNER. REMOVED RIGHT OVERWING EMERGENCY HATCH AND PANEL 292F TO FOM. REMOVED CORRODED PAD FROM RIGHT WHEEL WELL IAW DC8 SRM 51-1-20D. INSTALLED PAD AND PANEL 292F IAW DC8 SRM 51-1-20D, 51-3-1, AND 51-3-0. INSTALLED RIGHT OVERWING EMERGENCY HATCH IAW DC8 SMM 52-20-02. 2L74 4F RT4A25 20040317001092004031700109NM 2004 3 17 F3LA200400018 120040303A5210 WEB BOEING737 7373S1 138447SNM L-2 DOOR CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED L-2 DOOR WEB CORRODED FROM STA 949 TO STA 991.5. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-40-02, 53-60-51, 53-60-15 AND DRAWING 65-45855. 2L72 4F RTA16WE 20040317001102004031700110NM 2004 3 17 CALA0400201 120040302A575465C26271 SKIN BOEING737 7373T0 1384582NM NR 6 SLAT GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND RT UPPER WING L/E SKIN GOUGED BETWEEN NR 5 AND NR 6 SLAT, AT WS 250. REPAIRED IAW SRM 51-70-17. 2L72 4F RTA16WE 20040317001112004031700111NM 2004 3 17 CALA0400202 120040302A5510180A16122 PIN BOEING737 737724 13844BYNM HORIZONTAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724715 28786 INSPECTION FOUND LT HORIZONTAL STABILIZER AFT LOWER FAILSAFE PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040317001122004031700112WP 2004 3 17 CALA0400203 120040302A7830 THRUST REVERSER DOUG DC9 DC982 3022082WP NR 2 ENGINE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718833 49493 INSPECTION FOUND A 10 INCH CRACK IN NR 2 ENGINE UPPER THRUST REVERSER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW 7830-01872. 2L72 4F A6WE 20040317001132004031700113NM 2004 3 17 CALA0400204 120040302A5730UNK SKIN BOEING757 757224 1384958NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2748127 28968 INSPECTION FOUND TWO CRACKS IN THE LT WING FIXED L/E SKIN AT OSS 421 T0 471. THE CRACKS WERE 3 INCH AND 5 INCH LONG. REPAIRED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20040317001152004031700115NM 2004 3 17 CALA0400206 120040303A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 THE L-2 DOOR EMERGENCY LIGHT BATTERY PACK FAILED RESTORE TEST. THE M1673 BATTERY PACK WAS REPLACED IAW WORK CARD 29-3350-1-7100. 2L72 4F RTA16WE 20040317001192004031700119NM 2004 3 17 F3LA200400020 120040303A5315 FLOORBEAM BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 947 CORRODED ALONG GOUGE 20 INCHES EITHER SIDE OF CENTER LINE. REPLACED T-CAP PER EA B3-53R-10330 AND SRM 51-40-02. 2L72 4F RTA16WE 20040317001202004031700120EA 2004 3 17 SWIA200412935 120040221A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07410SW 7066 F/O TRIM DISCONNECTS BOTH STABS AND MACH TRIMS. REMOVED AND REPLACED HSTA. FUNCTION CHECK SATISFACTORY IAW CRJ MM 27-42-01. 2L72 4F RTA21EA 20040317001212004031700121EA 2004 3 17 SWIA200412936 120040224A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AILERONS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07959SW 7840 AILERON TRIM MOVES RIGHT BUT NOT LEFT. REMOVED AND REPLACED AILERON TRIM CONTROL PANEL IAW CRJ MM 27-12-10. OPS CHECK GOOD. P/N: 601R51226-23SW. 2L72 4F RTA21EA 20040317001232004031700123EA 2004 3 17 SWIA200412938 120040222A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07417SW 7400 STAB TRIM 2 WILL NOT TEST CORRECTLY. ROCKER SWITCH DISENGAGES STAB 2. REMOVED AND REPLACED STAB MOTOR CONTROL UNIT AND HORIZONTAL ACTUATOR IAW MM 27-40-00, 27-48-00 & RII CARD 27-415. 2L72 4F4 FRTA21EA E15NE 20040317001262004031700126 2004 3 17 SWIA200412941 420040224A2210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER INTERMITTENT A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07964SW 7868 YD-2 MESSAGE APPEARS AND RESETS MOMENTARILY THEN DISENGAGES. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR PER WW 22-22-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20040317001282004031700128SO 2004 3 17 SWIA200412943 120040226A27315299 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07270YV 120270 ELEVATOR TRIM APPEARS TO HAVE FROZEN AT ALTITUDE 24,000 FT AND -34C DEGREES. WITH AUTOPILOT ON, TRIM WHEEL MADE AN ABNORMAL POP SOUND AND ROLLED BACK. ON DESCENT WITH AUTOPILOT OFF, TRIM WHEEL WOULD NOT TRIM NOSE DOWN PROPERLY, AND WOULD SPRING BACK. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM TAB ACTUATORS IAW EMB120 MM 27-32-02. OPS CHECK GOOD. P/N OFF: 5299, S/N OFF: 555. 2L72 4T RTA31SO 20040317001302004031700130NM 2004 3 17 F3LA200400022 120040303A5315 FLOORBEAM BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT GALLEY FLOORBEAM WEB CORRODED AT STA 986.5, LBL 42. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-60-51, 51-40-02, MM 51-21-41 AND BOLD DRAWING 65-46812. 2L72 4F RTA16WE 20040317001332004031700133 2004 3 17 SWIA200412945 420040227A341845150340 SENSOR CNDAIRCL600 CL6002B19 1900309EA AOA MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07592SW6287 6287 7279 STALL FAIL AFTER ROTATION. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040317001342004031700134SO 2004 3 17 SWIA200412946 120040229A2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07209SW 120269 TRIM AURAL WARNING SOUNDS CONTINUOUSLY WHEN TRIM IS IN GREEN BAND. REMOVED AND REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW EMB 120 MM 27-32-05. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040317001352004031700135 2004 3 17 SWIA200412947 420040227A2210 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE AUTOPILOT DIRTY A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07597SW 7293 CLIMBING OUT OF SLC, AUTOPILOT WOULD NOT ENGAGE ON EITHER CAPT'S OR F/O'S SIDE. F/O'S WORKED BOTH SIDES. NO WARNING OR CAUTION MESSAGE DISPLAYED. CLEANED AUTOPILOT DISENGAGE SWITCHES. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040317001362004031700136SO 2004 3 17 SWIA200412948 120040220A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07186SW6364 6364 120034 FLAP FAULTS INTERMITTENTLY IN AIR AND ON GROUND. REPLACED FLAP ANNUNCIATOR. OPS CHECKED GOOD. 2L72 4T RTA31SO 20040317001372004031700137SO 2004 3 17 SWIA200412949 120040216A5210 BELLCRANK EMB 120 EMB120ER 3260203SO PAX DOOR DAMAGED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07189SW 120048 FORWARD ENTRY DOOR WILL NOT OPEN. RESECURED BELLCRANK IAW EMB MM 52-11-05. OPS. CHECKS GOOD. 2L72 4T RTA31SO 20040317001382004031700138 2004 3 17 SWIA200412950 420040227A34178220372154 ADC CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07432SW3754 3754 7548 IN FLIGHT, RECEIVED EFIS COMP MON, STALL FAIL, MACH TRIM, IAS CAUTION MESSAGES AND ADC TEMP DISAGREE MESSAGE ON FMS. REPLACED NR 2 AIR DATA COMPUTER AND PURGED NR 1 AND NR 2 PITOT SYSTEM WITH NITROGEN. OPS AND LEAK CHECK GOOD IAW CRJ MM 34-11-00. P/N: 822-0372-154, S/N ON: 12FFG, S/N OFF: 2695 2L72 4F RTA21EA 20040317001402004031700140 2004 3 17 SWIA200412952 420040226A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07216SW8008 8008 120285 FIRST FLIGHT RUDDER CHECK NOT SMOOTH WITH HYDRAULICS ON AND OFF. REMOVED AND REPLACED NR 1 RUDDER SERVO IAW MM 22-10-09. P/N: 622-5734-002, S/N ON: 10055, S/N OFF: 7980. 2L72 4T4 TRTA31SO E20NE 20040317001412004031700141EA 2004 3 17 SWIA200412953 120040225A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07413SW 7102 ON TAXI-OUT, SPOILERON FAULT MESSAGE AND WHITE LT SPOILERON BOX. REPLACED LEFT INBOARD SPOILERON PCU WITH SERVICEABLE UNIT. LEAK, OPS CHECK GOOD. P/N: 27000-7, S/N OFF: 0590. 2L72 4F RTA21EA 20040315001912004031500191NE 2004 3 15 PCAA0402166 220040214A7261 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 LACK OF LUBE A PCAAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 EA13804EX 227 FLIGHT 3703 ITHACA, HAD TO ABORT TAKEOFF DUE TO NR 2 ENGIINE OIL PRESSURE LIGHT ILLUMINATING ON TAKEOFF ROLL. MAINTENANCE WAS NOTIFIED AND FOUND NR 2 ENGINE TO BE 3 QUARTS LOW ON OIL. MAINTENANCE SERVICED AND GROUND RAN AIRCRAFT. ALL OPERATIONAL CHECKS GOOD. 2H72 4T4 TRTA13NM E20NE 20040315001922004031500192NM 2004 3 15 PCAA0402168 120040216A29107591628101 MANIFOLD DHAV DHC8 DHC8102 2809003NM HYD SYSTEM BROKEN A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA13821EX1643 173 FLIGHT 4072 TO LGA REPORTED COMPLETE LOSS OF NR 2 HYDRAULIC CONTENTS IN FLIGHT. AIRCRAFT RAN FOR 20 MINUTES WITH NO FLUID IN AFFECTED SYSTEM. MAINTENANCE INSPECTED AND FOUND THE NR 2 HYDRAULIC PRESSURE MANIFOLD AT FAULT WITH A BROKEN OFF FITTING. MAINTENANCE REPLACED THE MANIFOLD AND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. THE CASE DRAIN FILTER WAS ALSO REPLACED. AIRCRAFT WAS GROUND RUN AND ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040315001962004031500196WP 2004 3 15 UPS04841915 120040211A532037592581 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1270 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040315002012004031500201WP 2004 3 15 UPS04841920 120040130A575336537812 SUPPORT FITTING DOUG DC8 DC871F 302199DWP TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT O/B FLAP HINGE 219 I/B SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3653781 AND SRM 51-1-20D. 2L74 4F RT4A25 20040316000242004031600024NM 2004 3 16 UIEA200400017 120040219A5410 STRUT BOEING747 747243B 1384830NM NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 1 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT HAD CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NAC STATION 235 TO STATION 254. THE RIB INSTALLATION AT NAC STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F A20WE 20040316000612004031600061WP 2004 3 16 GTIA040019 120040106A5321 FLOORBOARD DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND CABIN CENTER FLOORBOARD STATION 200-256, MISSING INSERTS, EDGE FILLER MISSING, PEELING FIBERGLASS. FABRICATED NEW CABIN CENTER FLOORBOARD. (M) 2L72 4F A6WE 20040316000652004031600065WP 2004 3 16 GTIA040005 120040107A4930 TRANSMITTER DOUG DC9 DC983 3022083WP APU FUEL LEAKING A GTIAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23826NK 49391 DTW - FLT 1605 - AFTER STARTING APU ON THE GROUND AFTER LANDING THERE IS A VERY STRONG ODOR OF JET FUEL THROUGHOUT THE CABIN APU AIR SWITCH OFF. FOUND EXTERNAL OIL LEAK ON LOW PRESSURE TRANSMITTER LEAKING INTO NON-RAM AIR DOOR. TIGHTENED B-NUTS AND NO LEAKS NOTED. (M) 2L72 4F RTA6WE 20040316000712004031600071EU 2004 3 16 ASOA04095 120040122A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 SO11536AS 465 DURING A C-CHECK IN BNA, THE LEFT AND RIGHT SEAT TRACKS ON THE TOP AND BOTTOM BETWEEN FS 36 TO FS 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FS 36 TO FS 39 IAW SRM 51-25-02 AND 51-25-04. (M) 2H72 4T RTA53EU 20040316000722004031600072EA 2004 3 16 ASOA04092 120040206A5210H341223 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 FLT 4954 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO CLOSE AND THE HANDLE WOULD NOT STAY IN THE CLOSED POSITION. MAINTENANCE LUBRICATED THE OUTSIDE AND INSIDE PASSENGER DOOR HANDLES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040316000732004031600073EA 2004 3 16 ASOA04091 120040206A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11885AS 7521 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS VERY DIFFICULT TO CLOSE AND STOW THE OUTER HANDLE. MAINTENANCE OPENED AND CLOSED THE MAIN PASSENGER DOOR TEN TIMES WITH NO FAULTS FOUND. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040316001302004031600130EA 2004 3 16 COMA0460162 120040216A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01971CA 7145 FRETTING DAMAGE NOTED ON LEFT LOWER WING ACCESS HOLE CUTOUT AT 550CB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030. 2L72 4F RTA21EA 20040316001382004031600138NM 2004 3 16 UPS04441959 120040212A53117075T60090IN FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: C, M/D - NR 5R MED CUTOUT BS 2231 FRAME AT S25R FOUND 1 FASTENER HOLE CRACK AT STRAP. M/D R5 DOOR FWD CUTOUT FRAME STRAP REPAIRED PER SRM 53-10-04 FIG 115. 2L74 4F A20WE 20040316001472004031600147EA 2004 3 16 04054651 120040223A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27651BR 7426 DURING APPROACH OF FLIGHT 7522 CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS A 8 DEGREES. FLIGHT LANDED UNEVENTFULLY. A SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040316001502004031600150 2004 3 16 RAIA00402007 420040204A3418 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU STALL WARNING ILLUMINATED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03558HK 41071 BOTH STALL WARNING LIGHTS ILLUMINATED. MAINTENANCE TROUBLESHOT AND WAS UNABLE TO DUPLICATE MALFUNCTION. PERFORMED MAINTENANCE TEST FLIGHT WITH NO SYSTEM MALFUNCTION. 2L72 4T RTA41NM 20040316001532004031600153NE 2004 3 16 RAIA00402010 220040206A7261 CHIP DETECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE CONTAMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03573HK 41092 SGF - RIGHT ENGINE OIL CONTAMINATE LIGHT ILLUMINATED. MAINTENANCE REMOVED SMALL FLAKE FROM RIGHT CHIP DETECTOR, CLEANED REINSTALLED AND GROUND RAN ENGINE WITH NO DEFECTS NOTED. 2L72 4T4 TRTA41NM E18NE 20040316001602004031600160SO 2004 3 16 RAIA00402017 120040213A3610AS568226 SEAL RING EMB 145 EMB145LR 3260212SO RT ENG BLEED LEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03816HK 145055 STL - RIGHT ENGINE BLEED LEAK. MAINTENANCE REMOVED AND REPLACED BLEED LINE SEAL UNDER CARGO BAY FLOOR. 2L72 4T RTT00011AT 20040316001662004031600166SO 2004 3 16 RAIA00402023 120040223A2760852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO SPOILERS FAULTY A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03815HK8619 145048 STL - SPOILER FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED AIR/GRN PROX SWITCH. 2L72 4T RTT00011AT 20040706001312004070600131SO 2004 7 6 RAIA00402024 120040624A3297 WIRE EMB 145 EMB145 3260210SO BRAKE SYS SHORTED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03807HK 145119 3551- RIC - "BRAKE OTBD INOP" WARNING MESSAGE. MAINTENANCE REPAIRED SHORTED WIRING BETWEEN CONNECTORS P1044AND J1055. 2L72 4F RTT00011AT 20040316001712004031600171NM 2004 3 16 C1HA20043003 120040227A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY SIGN INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 AFT EMERGENCY EXIT SIGN INOP. 2L73 4F A3WE 20040316001802004031600180NM 2004 3 16 UPS04241974 120040217A3210 YOKE BOEING727 72722C 138400FNM LT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, ON REMOVAL & BREAKDOWN OF LT SWING LINK, YOKE ASSY FOUND TO BE CORRODED. REPLACED SWING YOKE SUPPORT LT MLG SWING LINK IAW MM 57-15-01. 2L73 4F A3WE 20040316001872004031600187NM 2004 3 16 UPS04241985 120040209A5340 FITTING BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, SUSPECTED CRACK FOUND ON BS 940 FITTING LEFT ON FWD UPPER FLANGE. FITTING REPLACED IAW EO B727-5310-4501 AND DRW 65C15732. 2L73 4F A3WE 20040316002032004031600203NM 2004 3 16 CALA0400185 120040228A5510180A16122 PIN BOEING737 737724 13844BYNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723707 28768 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT CENTER AND AFT LOWER ATTACH PINS CORRODED. THE ATTACH PINS WERE REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040316002102004031600210EA 2004 3 16 SWIA200412921 120040214A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07912SW5334 5334 7595 DURING FFOD CHECK ON STAB TRIM CH 2 AND MACH TRIM, THE STAB TRIM 2 WOULD NOT STAY ENGAGED DURING THE TEST. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW RJ MM 27-42-01, 27-42-05 AND RII CARD 27-415. OPS CHECKS GOOD. ACTUATOR P/N: 8396-3, S/N OFF: 796. 2L72 4F4 FRTA21EA E15NE 20040316002122004031600212EA 2004 3 16 SWIA200412923 120040215A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07438SW518 518 7574 SPOILERON FAULT STATUS MESSAGE ON GROUND, UNABLE TO CLEAR WITH CIRCUIT BREAKERS. REMOVED AND REPLACED NR 1 SECU PER MM 27-61-05. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040316002232004031600223NM 2004 3 16 2004UALA00160 120040223A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29544UA 25322 FWD FUSELAGE SKIN DENTED AFT OF L2 DOOR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER, TRIPLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040317000072004031700007NM 2004 3 17 252TR0017 120040210A3233654610914L ARM BOEING737 737228 13844AGNM MLG CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 ULTRA SONIC NDT INSPECTION OF LEFT MAIN LANDING GEAR BEAM ARM INDICATION NOTED ON FWD LUG PER NDT MANUAL PART 4.32-10-02. REPLACED BEAM ARM PER MM 32-11-11. 2L72 4F RTA16WE 20040317000082004031700008NM 2004 3 17 P5CA0401041 120040221A3244314792 TIRE BOEING747 74746NF 13848BTNM NLG DAMAGED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23452PA 30810 RIGHT NOSE TIRE HAS LOOSE TREAD BELT. REPLACED TIRE PER MM 32-45-02, COMPLIED WITH TIRE TREAD LOSS INSPECTION PER MM 05-51-34. 2L74 4F RTA20WE 20040317000182004031700018 2004 3 17 757BJ0006 420040228A22106225391002 CONTROL PANEL BOEING757 757236 1384971NM AFCS INTERMITTENT A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05757BJ 22176 AFCS MODE CONTROL PANEL HAS INTERMITTENT FAILURE, RT SIDE, A/SPEED BUG GOES TO 300-350 WITHOUT COMMAND. REPLACED AFCS MODE CONTROL PANEL WITH SERVICEABLE UNIT PER MM 22-11-02. 2L72 4F RTA2NM 20040317000262004031700026NM 2004 3 17 2004UALA00170 120040226A2781 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLATS ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29677UA 30029 RETURNED TO FIELD DUE TO SLAT ASYMMETRY MESSAGE. OUTBOARD SLAT NR 10 POSITION SENSOR OUT OF LIMITS. ADJUSTED SENSOR. 2L72 4F4 FRTA1NM E24NE 20040317000272004031700027EU 2004 3 17 2004UALA00171 120040226A2750 FLAP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE WINGS FAILED A UALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP29410UA 463 FLIGHT LANDED SAFELY WITH ZERO FLAPS. ECAM FCTL FLAPS LOCKED WITH CFDS MSG FLP 1 OVERSPEED RT CHECK FLP MECH DRIVE. RT NR 1 FLAP ACTUATOR 6255CM SHAFT WAS FOUND LOOSE AND HAD MORE THAN 0.25 INCH OF RADIAL PLAY. THE CONNECTING U-JOINTS WERE ALSO FOUND LOOSE AND WORN. THE FAULTY FLAP ACTUATOR 6255CM AND THE U-JOINTS WERE REPLACED. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040317000302004031700030EA 2004 3 17 COMA0460174 120040228A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01937CA 7044 FLIGHT 5892 LEFT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040317000362004031700036NM 2004 3 17 ABXA040086 120040223A7120112T700610 FITTING BOEING767 767231 1385131NM NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23709AX 22572 DURING INSPECTION OF NR 2 ENGINE PYLON OUTBOARD SIDE LOAD FITTING PER AD 2001-08-23 AND SB 767-547A0070, HFEC INSPECTION REVEALED CRACK IN UPPER INBOARD RADIUS. INTERIM REPAIR ON REA B657-49099MR. 2L72 4F RTA1NM 20040317000412004031700041NM 2004 3 17 04FDEA00527 120040229A5320 STIFFENER DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER HAVE CRACK LINE.COMPLIED FEDEX EA #1-3210-75908, LANDING GEAR - MAIN GEAR AND DOORS - PART FABRICATION. LT MAIN LANDING GEAR WHEEL WELL OUTBOARD WEB STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040317000452004031700045WP 2004 3 17 04FDEA00537 120040301A5230 HANDLE DOUG DC10 DC1030 3023501WP CARGO DOOR MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 UPON A/C ARRIVAL FOUND COVER DOOR TO CENTER CARGO DOOR LOCKING HANDLE MISSING. ALSO MISSING HINGE ASSY. CENTER CARGO DOOR LOCK HANDLE COVER TEMP REPAIR PER EA LIMITED TO 2 FLT CYCLES COMPLIED WITH PART 1 OF EA 8-5350-76446. DOOR REPLACED. 2L73 4F A22WE 20040317000522004031700052NM 2004 3 17 04059429 120040228A5270 SENSOR DORNERDO32 DO328300 NM EMERGENCY DOOR DIRTY A VTZAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27429FJ 3194 DURING FLIGHT CREW RECEIVED AN EMERGENCY DOOR UNSAFE LIGHT. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE SENSOR FOR THE EMERGENCY EXIT DOOR WAS FOUND SOAKED WITH GLYCOL AND WAS CLEANED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2H72 4T RTA55NM 20040317000532004031700053NM 2004 3 17 PCAA0403174 120040228A612078249050 PCU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE STICKING A PCAAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA13811EX200117930 201 121318 FLIGHT 3870 HAD TO SHUTDOWN IT'S NR 2 ENGINE AND RETURN TO FIELD DUE TO THE AIRCRAFT YAWING AND THE NR 2 ENGINE AUTOFEATHERING AFTER ROTATION. AIRCRAFT RETURNED TO LGA WITHOUT INCIDENT. MAINTENANCE AND AVIONICS RESPONDED TO DISCREPANCY. AVIONICS DOWNLOADED FDR AS REQUIRED. MAINTENANCE REMOVED AND REPLACED THE NR 2 PROP ASSEMBLY, PROP CONTROL UNIT (DUE TO THE INTERNAL BETA SWITCH STICKING), OVERSPEED PUMP, PROP TRANSFER TUBE, AND INSPECTED CHIP DETECTORS AND OIL FILTERS AS NEEDED PER SITUATION REQUIREMENTS. 2H72 4T4 TRTA13NM E20NE 20040317000592004031700059NM 2004 3 17 DL78K040164 120040217A275018173810 TRANSMITTER BOEING737 737832 13844CFNM LT WING TE INOPERATIVE A DALAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 SO27398DA 30774 ON FLAP EXTENSION THRU 2 DEG FLAPS SPLIT AND LOCKED OUT. DIVERTED TO ORD FOR A 2 DEG FLAP LANDING. REPLACED LEFT FLAP POSITION TRANSMITTER. 2L72 4F RTA16WE 20040317000692004031700069NM 2004 3 17 DL73S040177 120040219A531265465682 BULKHEAD BOEING737 737247 138448DNM FUSELAGE CANNING A DALAK NONE O OTHER ININSP/MAINT 1 SO27380DL 23607 THE GORE WEB OF THE AFT PRESSURE DOME AT FS 1016 WAS FOUND WITH AN OIL CAN CONDITION BETWEEN STRINGER 2R & 3R NEAR THE OUTER -Y- CHORD OF THE DOME. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088605-14. 2L72 4F A16WE 20040317000752004031700075NM 2004 3 17 DL76S040185 120040220A2530 FILTER BOEING767 767332 1382001NM GALLEY CHILLER DIRTY A DALAO OTHER M OVER TEMP CRCRUISE 1 SO27120DL 23279 FLIGHT ATT REPORTS THAT FIRST CLASS GALLEY CHILLER HAS OVERHEATED. ALSO REPORTED AN ELECTIRICAL ODOR THAT APPEARED TO ORIGINATE NEAR THE TRASH BIN. INSPECTED FREEZER ASSY, COULD NOT SMELL ANY ELECTRIC ODOR, FOUND FREEZER FILTER EXTREMELY CLOGGED. CLEANED FILTER ASSY. OPERATED FREEZER, ALL GOOD. 2L72 4F RTA1NM 20040317000792004031700079NM 2004 3 17 DL738040190 120040224A27406355B000103 MOTOR BOEING737 737832 13844CFNM STAB TRIM INOPERATIVE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27371DA 29619 ON TAKEOFF ELECTRIC STAB TRIM WAS INOP. REPLACED RELAY J4 R64 AND STAB TRIM MOTOR PER MM. 2L72 4F RTA16WE 20040317000832004031700083NM 2004 3 17 DL76G040194 120040227A3830 DRAIN LINE BOEING767 7673P6 1385105NM E/E COMP CLOGGED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27152DL 24984 LEFT FWD LAV FLUID (2 GALS) CAME UP FROM UNDER FLOORBOARDS AT FWD ENTRY DOOR. FOUND FWD LAV, FWD GALLEY AND LEFT DOOR DRAIN LINE CLOGGED. CLEARED LINE, OPS CHECK GOOD. INSPECTED E/E COMP, ALL CHECK NORMAL. 2L72 4F RTA1NM 20040317000862004031700086NM 2004 3 17 DL73S040197 120040227A3350BPS73 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27316DL 23088 EMERGENCY PATH LIGHTS AT ROWS 22-25D INOP. REMOVED AND REPLACED POWER SUPPLY. 2L72 4F RTA16WE 20040317000922004031700092NM 2004 3 17 DL73S040204 120040301A5330654576988 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 SCRIBE MARKS WERE NOTED BETWEEN BS 360 TO BS 540 AT THE S26R LAP JOINT. LAP WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386165-14. 2L72 4F A16WE 20040317000932004031700093NM 2004 3 17 DL73S040205 120040301A5330654576988 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 SCRIBE MARKS WERE NOTED BETWEEN BS 360 AND BS 540 ALONG S26L LAP JOINT IN THE LOWER SKIN. LAP JOINT WAS REWORKED PER INSTRUCTIONS CONTAINED IN ERA 386161-14. 2L72 4F A16WE 20040317000952004031700095 2004 3 17 DL76L040207 420040229A3417341080159 ADC BOEING767 767332 1382001NM COCKPIT FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27171DN 24759 PASSING THROUGH 1800 FEET ON CLIMBOUT F/O ALTIMETER FAILED. SELECTED ALTN ON AIR DATA. ALTIMETER WORKED. REPLACED RT ADC AND FLUSHED STATIC LINES. 2L72 4F RTA1NM 20040317000972004031700097NM 2004 3 17 DL738040211 120040302A33500201820001 LIGHT BOEING737 737832 13844CFNM R1 DOOR INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO273768 29630 R1 EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. 2L72 4F RTA16WE 20040317001002004031700100NM 2004 3 17 04FDEA00534 120040301A5311 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 FRAME GOUGED BS 1130 JUST BELOW STR 7L. REMOVED GOUGE ON FRAME AT BS 1130, JUST BELOW STRINGER 7L. ORIGINAL MATERIAL THICKNESS .071 INCH. REMOVED .050 INCH, DAMAGE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REPAIRED DAMAGE IAW SRM 51-40-3. 2L73 4F RTA3WE 20040317001082004031700108NM 2004 3 17 F3LA200400017 120040303A5315 FLOORBEAM BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT GALLEY FLOORBEAM CORRODED ON WEB AND UNDER GALLEY ATTACH POINT, RT SIDE, STA 986, RBL 42. BLENDED CORROSION ON WEB AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-51. REMOVED DAMAGED SHEAR WEB AND COMMON SUPPORT ANGLES PER SRM 51-40-02. FABRICATED REPLACEMENT WEB, ALODINED, PRIMED AND PAINTED PER SOPM 20-41-02. INSTALLED REPLACEMENT WEB AND SUPPORT ANGLES PER SRM 51-40-02. 2L72 4F RTA16WE 20040317001142004031700114NM 2004 3 17 CALA0400205 120040302A5313654988621 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759338 23576 INSPECTION FOUND STRINGER 27L CORRODED IN FORWARD CARGO AREA AT STA 480-500B. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20040317001162004031700116NM 2004 3 17 CALA0400207 120040303A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 THE AFT LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED RESTORE TEST. THE M1670 BATTERY PACK WAS REPLACED IAW WORK CARD 29-3350-1-7100. 2L72 4F RTA16WE 20040317001172004031700117NM 2004 3 17 CALA0400208 120040303A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717244 28954 THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED RESTORE TEST. THE M1671 BATTERY PACK WAS REPLACED IAW WORK CARD 29-3350-1-7100. 2L72 4F RTA16WE 20040317001222004031700122EA 2004 3 17 SWIA200412937 120040221A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07454SW 7749 FLAP HALFSPEED MESSAGE DURING FLAP EXTENSION. REMOVED AND REPLACED FLAP PDU IAW 27-52-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20040317001242004031700124EA 2004 3 17 SWIA200412939 120040222A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07442SW5738 5738 7609 DURING CLIMBOUT OUTBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT ADVISORY MESSAGES ILLUMINATED. REMOVED & REPLACED NR 1 SECU PER AMM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20040317001252004031700125SO 2004 3 17 SWIA200412940 120040225A2721 CIRCUIT CARD EMB 120 EMB120ER 3260203SO RUDDER TRIM FAILED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07583SW 120351 RUDDER TRIM WHEEL, IN CLIMB AND CRUISE, VIBRATES AND FEELS RATCHETY. RETENSIONED RUDDER TRIM CABLE CIRCUIT AS REQUIRED REFERENCING MM 27-00-01 AND COMPLETED RII CARD 27-314. OPS CHECK GOOD. 2L72 4T RTA31SO 20040317001322004031700132NM 2004 3 17 F3LA200400023 120040303A5320 SILL BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED SILL PLATE AT L2 DOOR FLOOR CORRODED. REPLACED MOP SILL PER SRM 51-10-02. 2L72 4F RTA16WE 20040317001422004031700142EA 2004 3 17 SWIA200412954 120040229A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07919SW 7657 STAB CHANNEL 1 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW CL600 MM 27-41-01, OPS CHECK GOOD. 2L72 4F RTA21EA 20040317001432004031700143NM 2004 3 17 F3LA200400024 120040303A5315 FLOORBEAM BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 950, RBL 26 TO RBL 49, WL 208 CORRODED AT FLOORBOARD HOLES. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM PER SRM 53-60-51 AND 51-10-02. 2L72 4F RTA16WE 20040317001442004031700144EA 2004 3 17 SWIA200412955 120040228A27604916405 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07437SW6558 6558 7564 SPOILERONS FAULT MESSAGE (STATUS) APPEARED ON ED-2 SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE UNIT. ALSO REPLACED RIGHT INBOARD SPOILERON PCU IAW MM CH 27-62-01. OPS CHECK, LEAK CHECK GOOD. PCU P/N: 2700-7, S/N OFF: MAL4796. 2L72 4F RTA21EA 20040317001482004031700148SO 2004 3 17 SWIA200412959 120040121A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07190SW 120050 UNDER FLOOR PANEL 243 DF BRACKET BUCKLED AND CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FITTED AND INSTALLED NEW FLOOR SUPPORT BRACKET. P/N: 120-14243-001. 2L72 4T RTA31SO 20040317001502004031700150EA 2004 3 17 SWIA200412962 120040212A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 484 LEFT INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV A & RII 53-401. 2L72 4F RTA21EA 20040318000012004031800001 2004 3 18 ACE020604 420040206A3420 GYRO CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO COCKPIT SPINNING E YADAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 AL039957M 20700764 574487 PILOT REPORTED THAT TWO AIR DRIVEN GYROS BEGAN SPINNING AND THE ENGINE RPM INCREASED TO ABOVE RED LINE. WHEN UNABLE TO REDUCE RPM WITH PROP CONTROL, RETURNED TO THE AIRPORT. GROUND CHECKS COULD NOT DUPLICATE THE RPM PROBLEM. 1H71 3O3 O A16CE E5CE 20040318000022004031800002CE 2004 3 18 ACE020504 120040205A3710AA216CW PUMP CESSNA207 207A 2073604CE VACUUM SYS INOPERATIVE E YADAK NONE O OTHER ININSP/MAINT 1 AL039957M 20700764 PILOT REPORTED VACUUM PUMP INOP. MAINTENANCE REPLACED SEIZED (SHEARED SHAFT) PUMP. 1H71 3O A16CE 20040318000032004031800003 2004 3 18 YENA200408 420040211A23303042865102 CONTROL BOX AIRBUS320 A320232 3930326EU ENTERTAIN SYS FAULTY A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15504JB1653 1156 FOUR HOURS INTO FLIGHT RUBBER BURNING ODOR FROM ROW 7 LEFT, SMELL WAS INTERMITTENT. SHUT DOWN LTV AS A PRECAUTION, AIRINC WITH MCC NO OTHER ACTION TAKEN, ODOR DID NOT REOCCUR. FOUND ELECTRICAL BURNING ODOR AT SEB AT SEAT 9B. REPLACED SEB IAW LTV MM 23-39-00, OPS CHECK NORMAL. PERFORMED LTV INTEGRITY INSP IAW INFO NOTICE 2003-T050TRA. INSPECTED ALL LTV CABLE AND COMPONENTS IN ROW 7 THRU 11 ABC, OPS NORMAL. MEL CLEARED AND PLACARD REMOVED. 2L72 4F RTA28NM 20040318000042004031800004 2004 3 18 P9RA20040008 420040214A3454285T05545 SELECTOR PANEL BOEING757 757236 1384971NM VOR RECEIVER FAULTY A P9RAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11962PG 24119 WHILE AT CRUISE ALTITUDE; PVR-ORD, THE LEFT VOR RECEIVER BUTTON WAS PUSHED TO MANUAL MODE. THE UNIT STARTED TO EMIT A LITTLE SMOKE. THE QRH PROCEDURE WAS FOLLOWED AND THE SYSTEM WAS ISOLATED. BUTTON WAS PULLED OUT AND THE CIRCUIT BREAKER WAS PULLED AND THE SMOKE STOPPED. REMOVED AND REPLACED THE LEFT VOR DME CONTROL PANEL. OPS CHECKED GOOD. 2L72 4F RTA2NM 20040318000052004031800005SO 2004 3 18 LR7A04027 120040212A5310 WINDOW FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND PILOTS SIDE WINDOW FRAME CRACKED. REPAIRED IAW SMP583 FIG 53-30-25, FS 126 WL 251 LBL 40. 2H74 4T A1SO 20040318000062004031800006SO 2004 3 18 LR7A04028 120040212A5310 WINDOW FRAME LKHEED382 382G 526414USO COCKPIT CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND COPILOT SIDE WINDOW AFT LOWER FRAME CRACKED. REPAIRED IAW SMP583 FIG 53-30-32, FS 156 WL 231 RBL 45. 2H74 4T A1SO 20040318000072004031800007SO 2004 3 18 LR7A04029 120040212A5312 PRESSURE PANEL LKHEED382 382G 526414USO FUSLAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3202 RIGHT MLG BAY SIDE WALL (PRESSURE PANEL) SKIN CORRODED AT FS 537. REPAIRED IAW SMP583 FIG 53-40-10, FS 537 WL 156 RBL 62. 2H74 4T A1SO 20040318000082004031800008SO 2004 3 18 LR7A04030 120040212A5320 INTERCOSTAL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 768 4606 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3201 FOUND LT MLG BAY INTERCOSTAL BEAM TEE CRACKED AT FWD END AT WL 200 FS 477. REPAIRED IAW SMP583 FIG 53-40-43, FS 480 WL 200 LBL 64. 2H74 4T A1SO 20040318000092004031800009CE 2004 3 18 DXTA200400249 120040220A215073838426 ACM CESSNA500 560CESSNA 2076750CE AIR CON FAILED E DXTAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL07379QS3165 5600479 AFTER LANDING AT SLC, DURING SHUTDOWN COCKPIT FILLED WITH THICK HEAVY SMOKE. FOUND AIR CYCLE MACHINE TO BE AT FAULT, REMOVED DEFECTIVE ACM AND INSTALLED OVERHAULED UNIT IAW HAMILTON STANDARD AND CESSNA 560 MM CHAPTER 21-50-03 PG 201 & 202, OPS CHECKS GOOD. 2L72 4F RTA22CE 20040318000112004031800011SO 2004 3 18 LR7A04031 120040223A5320 STIFFENER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 698 4763 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB2703 FOUND LT FLAPWELL CWS 192 REAR BEAM STIFFENER CRACKED, FS 517, WL 259. REPLACED STIFFENER IAW SRM SMP583 51-60 & 51-70. 2H74 4T A1SO 20040318000132004031800013CE 2004 3 18 8313882 120040128A2731S3280 GEAR RAYTHN BEECH 1900 1900D 1154162CE ELE TAB DIAL SLIPPED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01831CA3652 UE395 WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TRIM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSED ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT. 2L72 4T RTA24CE 20040318000142004031800014CE 2004 3 18 8304771 120040212A2731S3280 GEAR RAYTHN BEECH 1900 1900D 1154162CE ELE TAB DIAL SLIPPED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01830CA6168 UE393 WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TRIM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSED ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT. 2L72 4T RTA24CE 20040318000172004031800017 2004 3 18 YENA200411 420040225A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ENTERTAIN SYS ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15579JB900 2132 ODOR FROM LTV OF ROW 20, WENT AWAY WHEN LTV SHUT OFF. PERFORMED INSP OF ALL LTV COMPONENTS AFT OF ROW 18 IAW JB INFO NOTICE 2003-T050TRA. FOUND SLIGHT ELECTRICAL ODOR ON SEB AT 26D. REMOVED AND REPLACED SEB AT SEAT 26D IAW AMM 23-39-00, SYSTEM OPS CHECK NORMAL. 2L72 4F RTA28NM 20040318000182004031800018SO 2004 3 18 LR7A04032 120040227A5320 WEB LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 113 4606 DURING A-CHECK INSPECTION PER JOB CARD HA1200 FOUND CENTER WING REAR BEAM WEB CRACKED APPROX 1.0 INCH AND TERMINATING AT ACCESS OPENING, AT CWS 45 LEFT, FS 597, WL 262. REPAIRED WEB IAW LAC MEA 382-57-04-024. LP 15001, ITEM M1. 2H74 4T A1SO 20040318000192004031800019EA 2004 3 18 SWIA200412964 120040212A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-52. 2L72 4F RTA21EA 20040318000202004031800020NM 2004 3 18 F3LA200400025 120040303A5320 CHANNEL BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 ZEE CHANNEL AT STA 993, LBL 30 TO LBL 40 CORRODED. FABRICATED AND INSTALLED REPLACEMENT Z-CHANNEL PER SRM 51-10-02, PAGE 37, SRM 51-30-01 AND SOPM 20-41-02. 2L72 4F RTA16WE 20040318000212004031800021WP 2004 3 18 ABXA040088 120040228A531056440111 SPAR CAP DOUG DC8 DC861 3021952WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23842AX 46015 STA 857 LEFT BUTTLINE 24, SPAR CAP CRACKED. REPAIRED SPAR CAP IAW DC-8 SRM 53-2-5, 51-1-8, 51-1-21, AND 51-3-1. 2L74 4F 4A25 20040318000222004031800022WP 2004 3 18 ABXA040089 120040215A53135750198501 FITTING DOUG DC8 DC861 3021952WP LONGERON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23842AX 46015 LEFT LONGERON 23 CRACKED AT STA 920. REPAIRED LONGERON IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-20D, 51-3-1, AND 51-3-0. 2L74 4F 4A25 20040318000232004031800023WP 2004 3 18 ABXA040090 120040214A533057749923 SKIN DOUG DC8 DC861 3021952WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23842AX 46015 FORWARD LOWER CARGO CORROSION FUSELAGE SKIN AT LONGERON 35 LEFT, FS 620. REPAIR ACCOMPLISHED IAW REA D853-48847MR AND DC-8 SRM 53-2-1, 51-1-20D, AND 51-1-8. 2L74 4F 4A25 20040318000242004031800024WP 2004 3 18 ABXA040091 120040301A3030DTK06123S059 CONNECTOR DOUG DC9 DC941 302207NWP PITOT SYSTEM BURNED A ABXAA UNSCHED LANDING JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23966AX 47510 AFTER TAKEOFF, CAPTAIN'S PITOT HEAT ANNUNCIATOR ILLUMINATED, MASTER CAUTION LIGHT ILLUMINATED. HEATER AMP METER READ -0-. CAPTAIN'S PITOT HEAT CIRCUIT BREAKER TRIPPED, ELECTRICAL SMOKE ODOR FILLED THE COCKPIT. AIRCRAFT RETURNED TO FAT. REPLACED CAPTAIN'S PITOT TUBE AND ELECTRICAL CONNECTOR IAW DC9 AMM 34-12-01-2-0001. OPS CHECK GOOD. 2L72 4F A6WE 20040318000252004031800025EA 2004 3 18 COMA0460175 120040229A3260172825 TARGET CNDAIRCL600 CL6002B19 1900309EA LT MLG LOOSE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01812CA 7381 FLIGHT 5173 GEAR DISAGREE WARNING, LT MLG INDICATES INTRANSIT. TIGHTENED THE PROX SWITCH TARGET ON THE LT MLG UPLOCK. 2L72 4F RTA21EA 20040318000282004031800028NM 2004 3 18 CALA0400209 120040303A1430BACB30LE5U16 BOLT BOEING767 767424ER 1385270NM KRUGER SEAL DR SHEARED A CALAK NONE O OTHER ININSP/MAINT 1 SW2766051 29446 THE LEADING EDGE DEVICE WAS FOUND HANGING ON RIGHT WING JUST INBOARD OF RIGHT ENGINE DURING WALKAROUND. MAINTENANCE FOUND BOLT FROM LINK SHEARED AND LINK DAMAGED AT KRUEGER SEAL DRIVE. THE LINK AND BOLT WERE REPLACED IAW MM 767-400-27-81-19, PAGE 401. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA1NM 20040318000292004031800029NM 2004 3 18 CALA0400210 120040303A5320149A761415 STRUCTURE BOEING737 737724 13844BYNM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 INSPECTION FOUND A .5 INCH CRACK IN LT WHEEL WELL AFT RING ASSEMBLY O/B LOWER CHORD. THE O/B LOWER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040318000322004031800032NM 2004 3 18 CALA0400213 120040116A531465621257 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776354 23592 MAINTENANCE DISCOVERED CRACKS ON THE LEFT HAND AND RIGHT HAND KEELBEAM LOWER CHORD AT STA 727 +14.40. THE NUMBER OF CRACKS AND LENGTH WAS NOT IDENTIFIED. THE EXISTING KEELBEAM LOWER CHORDS WERE CUT OUT AND NEW REPAIR SECTIONS WERE SPLICED IN IAW ECRA 5311-01184. 2L72 4F RTA16WE 20040318000332004031800033NM 2004 3 18 F3LA200400029 120040303A5320 WEB BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED SHEAR WEB CORRODED IN AFT GALLEY FROM STA 986.5 TO STA 1016, LBL 32.1 TO LBL 45.5. REMOVED SHEAR WEB AND SUPPORT ANGLES COMMON TO WEB. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-10-02, 51-40-02, 51-40-06, 51-21-01 AND SOPM 20-41-02. 2L72 4F RTA16WE 20040318000412004031800041WP 2004 3 18 04FDEA00546 120040303A5744ARC0502502 HINGE DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 REWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING AND FOUND BORE TO BE 2.322, OUT OF LIMITS IAW DC10 CMM 57-44-08. HEAT TREATED MATERIAL FOR BUSHING IAW DPS 5.00.2 & DPS 1.05.5. PERFORMED HFEC IAW DC10 NDT MANUAL PT6, NO CRACKS NOTED. FABRICATED OVERSIZED BUSHING IAW DC10 CMM 57-44-08. PERFORMED MPI IAW DPS 4.704 NO CRACKS, ETCHED BORE, NO CORROSION FOUND, PEENED HOLES IAW DC10 CMM 20-11-01 AND 20-11-02. CAD PLATED BUSHING IAW 57-44-08 PER QQP-416, TYPE 2 CLASS 2. PRIMED BORE AND INSTALLED BUSHING IAW CMM 57-44-08. FINAL BORE ID 2.2505. LEVEL 2 CORRODED BORE NR 4. 2L73 4F RTA22WE 20040318000422004031800042WP 2004 3 18 04FDEA00547 120040303A5744ARC0502502 HINGE DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 REWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING, REPAIRED HINGE PER FEDEX EA 8-5710-75067 DATED 01-23-04. 2L73 4F RTA22WE 20040318000432004031800043EU 2004 3 18 04FDEA00548 120040303A29133508806 PUMP AIRBUS330 A300* EU ZONE 400 DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25718FD 365 LOST GREEN SYS HYD FLUID AFTER FLAPS RETRACTED. NO HYDRAULIC OVERHEAT OCCURRED FOUND LINE BUSTED LT MLG UPLOCK. REMOVED & REPLACED LT MLG UPLOCK HOSE REF IPC 32-31-03-03 ITEM 30, NEEDS LEAK CHECK PAR 2C A300 MM 29-00-00-3. PUMP REMOVAL IN PROGRESS PER MM 29-11-32-4, A-300 MM-29-11-32-4. REMOVED AND REPLACED NR 2 ENG DRIVEN HYD PUMP PER A300- 600 M/M 29-11-32-4-01 NEEDS SERVICED AND LEAK CHECKED. REPLACED NR 1 GREEN SYS ENG DRIVEN HYD PUMP PER A300- 600 M/M 29-11-32-4-01. SERVICED GREEN SYS HYD FLUID. OPS & LEAK CHECK NORMAL. A/C OK FOR SERVICE. 2L72 4F RTA26NM 20040318000442004031800044WP 2004 3 18 04FDEA00549 120040303A5744ARC0502501 HINGE DOUG DC10 DC1030F 3023504WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25302FE 46801 LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REWORK LEFT OUTBOARD FLAP INBOARD FWD HINGE AT REAR SPAR OUTBOARD LWR MOUNT HOLE CORRODED AT BORE NR 3. REMOVED BUSHING AND CORROSION IAW CMM 57-44-8. FABRICATED AND INSTALLED OVERSIZED BUSHING IAW DC10 CMM 57-44-08 AND EA8-5710-75068. 2L73 4F RTA22WE 20040318000452004031800045WP 2004 3 18 04FDEA00550 120040303A5744ANB70166 MOUNT DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 DURING C-CHECK INSPECTION, CORROSION WAS FOUND IN THE CENTER BORE OF THE ANB7016-6 RT INBOARD FLAP DRIVE BEARING MOUNT BORE. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.0210 INCH DIA. REMOVED FITTING IAW DC10 SRM 51-31-00 VOL II. REMOVED CORROSION IAW DC10 SRM 57-20-00 VOL 1. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710-75080 AND DC10 SRM 57-20-00 VOL 1. CORROSION LEVEL 1. FITTING INSTALLATION COMPLETED ON FEDEX CARD N02040. 2L73 4F RTA22WE 20040318000462004031800046WP 2004 3 18 04FDEA00551 120040303A5744ARC0503 HINGE FITTING DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 RIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING AUCT MOUNT POINT HOLE HAS CORROSION AT BORE 5 A&B. DURING EO 8-5750-7-5000, CORROSION WAS FOUND IN THE 2 RT FLAP OUTBOARD HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1.192 AND 1.1908. REAMED BORES TO REMOVE CORROSION, FABRICATED AND INSTALLED OVERSIZED BUSHINGS IAW DC 10 CMM 57-44-09 AND EO 8-5710-75066. 2L73 4F RTA22WE 20040318000472004031800047WP 2004 3 18 04FDEA00552 120040303A5744ARC0538501 HINGE DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 RIGHT OUTBOARD FLAP INBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING C-CHECK INSPECTION CORROSION WAS FOUND IN THE INNER BORE OF ARC0538-501 OUTBOARD FLAP FORWARD CLEVIS FITTING. THE SUBJECT CORROSION WAS REMOVED BY OVERSIZING THE SUBJECT HOLE TO 1.220 INCH IN THE RIGHT FITTING AND 1.200 IN THE LT FITTING. REAMED FITTING MOUNT HOLES IAW DAC CMM 57-44-07 TO 1.220, ALL CORROSION REMOVED. FABRICATED REPAIR BUSHING IAW DWG 54928911N16-022 AND EO 8-5710-75084. 2L73 4F RTA22WE 20040318000482004031800048WP 2004 3 18 04FDEA00553 120040303A5744ARC053 HINGE DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 RIGHT OUTBOARD FLAP OUTBOARD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION. DURING EO 5750-7-5000, CORROSION WAS FOUND IN THE 2 RIGHT OUTBOARD FLAP HINGE FITTING NR 5 OUTBOARD MOUNTING HOLES. THE SUBJECT CORROSION WAS REMOVED TO A FINAL DIAMETER OF 1.192 INCH AND 1.908 INCH. REMOVED CORROSION, FABRICATED BUSHINGS AND INSTALLED BUSHINGS IAW DC10 CMM 57-44-09 AND EA 8- 5710-75066. 2L73 4F RTA22WE 20040318000512004031800051WP 2004 3 18 04FDEA00561 120040304A5311AJC702933 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 UPPER AFT FUSELAGE FRAME CRACKED CANT STA 2069. REMOVED AND REPLACED FRAME IAW SRM 51-35-02 AND SRM 51-33-01 AT MAE ON N/R N00320 W/O 25240. 2L73 4F A22WE 20040318000522004031800052WP 2004 3 18 04FDEA00562 120040304A5311AJC702817 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 UPPER AFT FUSELAGE FRAME CRACKED CANT STA 2092. REMOVED AND REPLACED FRAME IAW SRM 51-35-01 AND SRM 51-33-01 AT MAE ON N/R N00317 W/O 25240. 2L73 4F A22WE 20040318000532004031800053EU 2004 3 18 04FDEA00565 120040304A2170 COALESCER BAG AIRBUS310 A310 EU LT & RT A/C PACKODOR A FDEAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO25411FE 359 WHEN T/O POWER WAS APPLIED BOTH PILOTS NOTICED A VERY STRONG OIL BURNING ODOR. REJECTED T/O AT 90 KTS, COMPLETED QRH CHECK LIST AND TAXIED TO GATE. WHEN TAXIING IN POWER ODOR RETURNED. REMOVED AND REPLACED BOTH LT AND RT A/C PACK WATER SEPARATOR COALESCER BAGS IAW A310-200 AMM 21-51-16-3. PERFORMED HIGH POWER RUNS ON ENGINES NR 1 AND NR 2. ALSO ALTERNATED A/C PACKS AND BLEED AIR SOURCES FROM ENGINES IAW A300/A310 JET RUN HANDBOOK, NO OIL ODOR NOTED. OPS CHECK GOOD. 2L72 4F RTA35EU 20040318000552004031800055WP 2004 3 18 04FDEA00567 120040304A5744ARC0503 BRACKET DOUG DC10 DC1010 3022110WP LT WING FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 COMPLY WITH EA 8-5740-73884 WINGS - LT OUTBOARD FLAP, OUTBOAD HINGE BRACKET CORROSION REPAIR (P/N ARC0503). COMPLIED WITH EA 8-5740-73884 WINGS - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0503) AT MAE. 2L73 4F A22WE 20040318000562004031800056WP 2004 3 18 04FDEA00568 120040304A5730ARB0975523 ACCESS PANEL DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 PITTING INSIDE SEAL GROOVE/MATING SURFACE ON FUEL TANK ACCESS PANEL 638BB. PITTING OUT OF LIMITS. REPLACED PANEL 638BB IAW DC10 MM 28-00-00-2. 2L73 4F RTA22WE 20040318000582004031800058WP 2004 3 18 04FDEA00570 120040304A5312 BULKHEAD DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 FWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2. 2L73 4F RTA22WE 20040318000622004031800062WP 2004 3 18 04FDEA00574 120040304A5744ARC0503 HINGE DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 REWORK RT OUTBD FLAP OUTBD HINGE FITTING FWD ATTACH POINT BUSHING HAVE CORROSION WRITTEN FOR CLARIFICATION JPF. REMOVED BUSHING & CORROSION IAW DC10 CMM 57-44-09, FINAL HOLE SIZE 1.192, FOUND OUT OF LIMITS. FABRICATED BUSHING IAW DC10 CMM 57-44-09 AND EO 8-5710-75066. HEAT TREATED BUSHING IAW DPS 5.00.2 & DPS 1.05.5. MPI BUSHING IAW DPS 4.204, NO CRACKS NOTED. CAD PLATED BUSHING PER QQ P 416 TYPE Z CLASS 2 BY VENDOR PO433296. HFEC BORE IAW DC10 NDT MANUAL PT6, NO CRACKS NOTED. ETCH BORE IAW CMM 20-11-02, NO CORROSION NOTED. PEENED BORE IAW DC10 CMM 57044-09 & 20-11-01. PRIMED BORE IAW DC10 CMM57-44-09. INSTALLED REPAIR BUSHING IAW DC10 CMM 57-44-09 & EA 8-5710-75066. 2L73 4F RTA22WE 20040318000642004031800064EU 2004 3 18 MALA040219 120040225A2120 ODOR SAAB SF340 340B 7860101EU CABIN DETECTED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15410XJ 340B410 DURING DEPARTURE AIRCRAFT PULLED A LITTLE TO RIGHT DTV, DURING CLIMB STRONG ODOR OF BURNED RUBBER. ODOR INTENSIFIED THROUGH 10,000 FT. INSPECTED WHEEL, TIRES, BRAKES, ACMS, AND RUDDER, NO DISC FOUND. AIRCRAFT PASSES TEST FLIGHT. AIRCRAFT OK FOR RETURN TO SERVICE. 2L72 4T RTA52EU 20040318000652004031800065EU 2004 3 18 MALA040220 120040302A30206124300 SEPARATOR SAAB SF340 340B 7860101EU RT ENGINE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15370PX 340B300 RIGHT INTAKE LIGHT ILLUMINATES AFTER 15 MINUTES AND STAYS ON. AIR RETURN TO MSP. REPLACED RIGHT WHITE HARNESS P/N 7292533-602, NO HELP. REMOVED AND REPLACED RT PARTICLE SEPARATOR DUCT P/N 6124-300, S/N OFF 243, S/N ON 182, SYS OPS CHECKS GOOD. 2L72 4T RTA52EU 20040318000662004031800066 2004 3 18 MALA040221 420040302A22104068300904 COMPUTER BAC 146 AVRO146RJ85A1500097EU AUTOPILOT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15508XJ E2318 FTC/EL TRIM LIGHT ILLUMINATED DURING TAKEOFF ROLL. AIR RETURN TO MSP. REPLACED FGC. TESTS GOOD IAW AVRO MM CH 22. 2H74 4F RTA49EU 20040318000682004031800068NM 2004 3 18 SWAA040598 120040225A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 188, WL 207, RT SIDE 1 ABOVE FLOOR TO 1 BELOW FLOOR. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040318000712004031800071NM 2004 3 18 SWAA040601 120040226A2560PH22300L GLOWSTRIP BOEING737 7373Q8 1384670NM ROW 6-8 MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 PHOTOLUMINESCENT STRIP MISSING FROM ROW 6 TO ROW 8 LT SIDE. REINSTALLED NEW SECTION OF STRIP. 2L72 4F RTA16WE 20040318000722004031800072 2004 3 18 SWAA040602 420040226A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR DISLODGED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EVAC SLIDE INADVERTANTLY PULLED FROM DOOR. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318000732004031800073NM 2004 3 18 SWAA040603 120040226A53306545835 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT COOLING DUCT CUT OUT. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040318000742004031800074NM 2004 3 18 SWAA040604 120040226A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040318000752004031800075 2004 3 18 SWAA040605 420040226A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040318000762004031800076NM 2004 3 18 SWAA040606 120040226A3350100067 LIGHT BOEING737 7372H4 138448CNM RT GALLEY INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED PM CHECK, FOUND AFT RT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F A16WE 20040318000782004031800078NM 2004 3 18 SWAA040608 120040226A3350610478 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED A2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040318000792004031800079NM 2004 3 18 SWAA040609 120040226A3350OL3071BPEGPL BULB BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED A2 CHECK, FOUND 2 EACH EEPLS BULBS INOP. REMOVED AND REPLACED BULBS PER MM. 2L72 4F A16WE 20040318000812004031800081 2004 3 18 SWAA040611 420040226A2565D31354 SLIDE BOEING737 7372T4 1384492NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040318000822004031800082NM 2004 3 18 SWAA040614 120040226A143069681514 BOLT BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND LT MLG SIDE STRUT TO UNIVERSAL ATTACHMENT BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM. 2L72 4F RTA16WE 20040318000842004031800084NM 2004 3 18 SWAA040619 120040226A53116545805 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STRINGER 16L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040318000852004031800085NM 2004 3 18 SWAA040620 120040226A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 1016, LAP SPLICE 3 AND LAP SPLICE 4. REPAIRED BULKHEAD PER ER. 2L72 4F RTA16WE 20040318000882004031800088NM 2004 3 18 SWAA040623 120040226A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGERS 26L AND 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040318000892004031800089NM 2004 3 18 SWAA040624 120040226A5553 ATTACH FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR PRIMARY LUG AND AFT FACE CHAMFER CORRODED. REPAIRED VERTICAL STAB LUG PER ER. 2L72 4F RTA16WE 20040316001092004031600109NM 2004 3 16 PCAA0402169 120040218A3260XD4N RELAY DHAV DHC8 DHC8102 2809003NM MLG FAULTY A PCAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 EA13808EX 299 FLIGHT 3761 FROM ROCHESTER TO LGA, HAD TO RETURN TO FIELD DUE TO THE LANDING GEAR INOP LIGHT ILLUMINATING UPON GEAR UP SELECTION DURING CLIMBOUT. GEAR WAS EXTENDED MANUALLY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAYS 3261-K5, K6, K8, K11 AND OPERATIONAL CHECKS WERE ALL GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040316001112004031600111NE 2004 3 16 PCAA0402170 220040218A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LT & RT OUT OF RIG A PCAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA13844EX 339 FLIGHT 3915 SYRACUSE REPORTED THE AIRCRAFT DID NOT SLOW DOWN WHEN POWER LEVERS WERE SELECTED TO DISC. MAINTENANCE INSPECTED SYSTEMS AND RAN AND TAXIED THE AIRCRAFT, NO DEFECTS WERE NOTED. ITEM WAS THEN DEFERRED UNTIL AIRCRAFT REACHED MAINTENANCE AND ENGINE RIGGING WAS AGAIN CHECKED AND FOUND TO BE OUT OF ADJUSTMENT. BOTH ENGINES WERE RERIGGED. 2H72 4T4 TRTA13NM E20NE 20040316001172004031600117EU 2004 3 16 054041 120040221A3230D49412001 CONTROL UNIT SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A NSVAO OTHER J WARNING INDICATION APAPPROACH 1 EA27294CJ 340B294 DURING APPROACH, GEAR SELECTOR DOWN, TRANSIT LIGHT OFF, NO GREEN LIGHT INDICATION. EXECUTED MISSED APPROACH, COMPLETED ABNORMAL CHECKLIST, ON 3RD ATTEMPT GEAR OPERATED NORMAL. FERRIED AIRCRAFT TO HEF WITH GEAR PINNED. REPLACED GEAR CONTROL UNIT, PERFORMED FUNCTIONAL CHECK IAW 32-30-00, OPS NORMAL. 2L72 4T RTA52EU 20040316001202004031600120WP 2004 3 16 UPS04841946 120040213A2797 CABLE DOUG DC8 DC873F 302199FWP LT AILERON BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 AILERON BINDING ON RIGHT TURN. LEFT AILERON BUSSING CABLE BROKEN AT I/B OF AILERON. INSTALLED LEFT .125 INCH BUSS CABLE PER MM 27-13-22 UP TO STEP (H) ACCOMPLISHED REMAINING STOPS AND ADJUSTED PER MM 27-10-17-5. 2L74 4F RT4A25 20040316001222004031600122WP 2004 3 16 UPS04841952 120040217A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 25 CUSP WEB/INTERCOSTAL IS CRACKED AT LONG 21L. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. 2L74 4F RT4A25 20040316001462004031600146EA 2004 3 16 COMA0470028 120040226A5270 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA E/E DOOR ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01369CA 10079 FLIGHT 5073 AVIONICS BAY DOOR CAUTION MESSAGE DURING T/O. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2L72 4F RTA21EA 20040316001612004031600161SO 2004 3 16 RAIA00402018 120040215A32608065701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE03834HK RIC - NLG WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED WOW PROX SWITCH. 2L72 4T RTT00011AT 20040316001862004031600186NM 2004 3 16 UPS04241980 120040211A5754 WEB BOEING727 72722C 138400FNM KRUGER FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 INSPECTION TYPE: C, CRACKS ON NR 5 K-FLAP ACTUATOR I/B & O/B TRUNNION CAPS SUPPORT WEBS AT UPPER & LWR CORNERS. NR 5 K-FLAP ACTUATOR REMOVED PER MM 27-81-22. FABRICATED TRUNNION CAPS SUPPORT WEBS IAW SRM 51-20-1 & DRG 65-16269. INSTALLED TRUNNION CAPS SUPPORT WEB PER BOEING DRG 65-16249. INSTALLED NR 5 K-FLAP ACTUATOR IAW MM 27-81-22. 2L73 4F A3WE 20040316001892004031600189NM 2004 3 16 UPS04441982 120040210A5310 DOOR FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE: C, M/D - LEFT NR 4 DOOR FWD CUTOUT FWD FRAME APPROX S16L AREA, FRAME I/B FWD FACE FOUND CRACK AS MARKED. FWD FRAME CRACKED PORTION TRIMMED OFF, REPAIRED AS PER HX RS 53-62-35110. SURROUNDING STRUCTURE IS CORROSION AND DAMAGE FREE AFTER INSPECTED. NDT INSPECTED THE TRIMMED AREA, NO CRACK FOUND UPS ENGINEERING FILE 747-53-20171. 2L74 4F A20WE 20040316001922004031600192NM 2004 3 16 UPS04541986 120040227A3220 LANDING GEAR BOEING757 75724APF 1384969NM NOSE STUCK A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01426UP 25457 NOSE GEAR GREEN DN LGT FAILED TO ILUM W/GEAR HANDLE DN. EICAS MSG GEAR DISAGREE & GEAR DOORS DISPLAYED. DOORS & GEAR AMBER LGTS ILLUM. INDIC ATIONS WERE NORM AFTER ALTN GEAR EXT. REF LP 195912 R & R NLG RETRACT ACTUATOR PER MM VALVE & NOSE GEAR LOCK ACTUATOR PER MM 32-34-01. REMOVED NLG OPERATED SEQUENCE VALVE. INSTALLED NEW NOSE GEAR OPERATED SEQUENCE VALVE PER MM32-34-06 PERFORMED SUCCESSFUL N/G EXTEN AND RETRACT TEST. JACKED A/C, FOUND NO HYD LEAKS PER MM 7-1-02 MM32-34-00 PG 501-504 2L72 4F RTA2NM 20040316001942004031600194NM 2004 3 16 CALA0400176 120040227A5320143A948537 BRACKET BOEING737 737724 13844BYNM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717730 28798 INSPECTION FOUND FORWARD CARGO COMPARTMENT AFT BULKHEAD CENTER PANEL ATTACH BRACKET CORRODED. A NEW CENTER ATTACH BRACKET WAS INSTALLED IAW SRM 51-40-03 AND DRAWING 143A9485. 2L72 4F RTA16WE 20040316001992004031600199NM 2004 3 16 CALA0400181 120040228A53206546592 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND FLOOR STRAP CORRODED ALONG FASTENER HOLES AT BS 727D. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040316002222004031600222NM 2004 3 16 2004UALA00159 120040223A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP2976UA 24641 STA 706 STR 11 LT SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20040317000192004031700019NM 2004 3 17 2004UALA00163 120040224A5270 SENSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CARGO DOOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29853UA 1688 FLIGHT DIVERTED DUE TO FWD CARGO DOOR OPEN ECAM MESSAGE. FORWARD CARGO DOOR PROXIMITY SENSOR WAS REPLACED 28WV. THE FORWARD CARGO DOOR PROXIMITY TARGET WAS ALSO ADJUSTED. 2L72 4F4 FRTA28NM E40NE 20040317000312004031700031WP 2004 3 17 ABXA040081 120040217A5313527779223 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23908AX 47008 LONGERON 17 RIGHT HAD 2 CRACKS AT EACH LOCATION, FS 389, FS 408 AND FS 427. REPAIRED LONGERON 17 RIGHT FROM STA 388 TO 446 IAW DC-9 SRM 53-02. 2L72 4F A6WE 20040317000322004031700032WP 2004 3 17 ABXA040083 120040217A32329915510509 ACTUATOR DOUG DC9 DC931 3022065WP MLG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23908AX 47008 FITTING FORWARD OF DOOR ACTUATOR CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20040317000382004031700038WP 2004 3 17 ABXA040082 120040217A532039203201 FITTING DOUG DC9 DC931 3022065WP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23908AX 47008 SLANT PANEL INBOARD ANGLE FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-10-4, AND 51-30-1. 2L72 4F A6WE 20040317000442004031700044NM 2004 3 17 04FDEA00532 120040301A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 CABIN - INTERCOSTAL CRACKED AT LONGERON 7R, STA RT 1621 TO 1641. 2L73 4F RTA22WE 20040317000472004031700047WP 2004 3 17 04FDEA00539 120040301A5270 RELAY DOUG DC10 DC1030 3023501WP ANNUNCIATOR FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25309FE 48298 IN CRUISE FLIGHT AIR COND DOORS ANNUNCIATOR LIGHT ON S/O PANEL ILLUMINATED FOR APPROX 1 MIN THEN WENT OUT. RED TABS REQUIRED DIVERTING TO NEAREST SUITABLE AIRPORT. AIRCRAFT DIVERTED TO IND. TROUBLESHOT WITH TAFI 52-40-00AB FOUND RELAY R5-5431 BAD. REMOVED & REPLACED RELAY, OPS CHECK GOOD. 2L73 4F A22WE 20040317000652004031700065NM 2004 3 17 DL73S040172 120040218A534065465721 CLEVIS BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 CORROSION DAMAGE WAS NOTED ON THE NR 5, NR 6 AND NR 11 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW 386170-14. 2L72 4F RTA16WE 20040317000702004031700070NM 2004 3 17 DL73S040178 120040220A80122730426 START VALVE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE CONTAMINATED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27334DL 23105 709211 RIGHT ENGINE START VALVE OPEN LIGHT CAME ON DURING CLIMBOUT ISOLATION VALVE AND ENGINE BLEED VALVE WERE CLOSED. LIGHT WENT OUT AT LOW PWR SETTING. LIGHT STAYED OUT AT LOW PWR. FOUND F/F XMTR LEAKING AT HI PWR SETTING. REPLACED PACKING AND BACK UP RINGS. REPLACED START VALVE AND PRESS SWITCH. ALSO CLEANED CONNECTOR ALL FUEL SOAKED. 2L72 4F4 FRTA16WE E2EA 20040317000762004031700076NM 2004 3 17 DLM88040186 120040223A3220 STRUT DOUG MD88 MD88 3023688NM NLG UNDERSERVICED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27926DL 49713 NOSE GEAR FAILED TO RETRACT ON T/O. RED NOSE GEAR LIGHT ILLUMINATED. SERVICED STRUT PER M/M 12-15-041 PG 201. SWUNG NOSE GEAR CHECKED OK. 2L72 4F RTA6WE 20040317000782004031700078NM 2004 3 17 DL733040188 120040224A32206546221517 CYLINDER BOEING737 737347 1384647NM NLG SHEARED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27311WA 23597 WHILE TAKING THE RUNWAY IN A LEFT TURN, HEARD A BANG. THOUGH THE A/C FELT OK, ELECTED TO PULL OFF THE RUNWAY AND HAVE MAINT INSPECT THE AIRCRAFT. FOUND THE LEFT NOSE WHEEL AND AXLE BROKEN. REPLACED NOSE GEAR. 2L72 4F RTA16WE 20040317000812004031700081NM 2004 3 17 DL777040192 120040225A3350D71700201 POWER SUPPLY BOEING777 777232 1385232NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27866DA 29738 ZONE 3 SEAT MOUNTED EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK, OPS NORMAL. 2L72 4F RTT00001SE 20040317000852004031700085NM 2004 3 17 DLM90040196 120040227A256061020 BATTERY DOUG MD90 MD9030 3023690NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27909DA 53389 THE L1 DOOR EMERGENCY FLASHLIGHT OUTBOARD RED POWER LIGHT DOES NOT BLINK. REMOVED AND REPLACED BATTERY, OPS NORMAL NOW. 2L72 4F RTA6WE 20040317000892004031700089NM 2004 3 17 DLM88040201 120040228A3397 WIRE DOUG MD88 MD88 3023688NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27912DL 49543 ROW 1D & FWD GALLEY EMERGENCY LIGHT BURNED OUT. FOUND BAD WIRE TO GALLEY LIGHT HAD TO REWIRE. 2L72 4F RTA6WE 20040317000962004031700096NM 2004 3 17 DL76G040210 120040301A2410729825B IDG BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 ENGINE FAILED A DALAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO271607B 30388 704823 ON TAXI IN ATL, SHUT DOWN LT ENG AFTER COOLING. AFTER POWER TRANSFER, POWER STARTED TO TURN ON AND OFF APPROX THREE TIMES. FLIGHT ATTENDANT REPORTED SMOKE AND BURNING IN MAIN CABIN ALONG WITH FLICKERING LIGHTS. DOWN LOADED UTILITY BUSSES AND LT GEN CONTROL SWITCH. STARTED APU AND PROBLEM STOPPED, HAVE NOT RESET THE UTILITY BUSSES. RANG OUT FIELD WIRES AND ALL RESISTANCES WERE WITHIN LIMIT. REMOVED AND REPLACED NR 2 GCU, NO HELP. FOUND NO ELECTRICAL ODOR THROUGH OUT CABIN. REMOVED AND REPLACED RT IDG, OPS OK. 2L72 4F4 FRTA1NM E13NE 20040317001012004031700101NM 2004 3 17 04FDEA00535 120040301A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25281FE 22348 LONGITUDINAL BEAM, AT BS 760 TO BS 850, LBL 25 HAS NUMEROUS AREAS OF CORROSION ON EITHER SIDE OF THE SEAT TRACK. REMOVED CORROSION ON FLANGE OF LONGITUDINAL BEAM BS 760-850, LBL 25. ORIGINAL THICKNESS .100 INCH. REMOVED .030 INCH IN SEVERAL AREAS. FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1. REMOVED LONGITUDINAL BEAM BS 750-870 LBL 25. LOCATED & DRILLED UP NEW LONGITUDINAL BEAM. COUNTERSUNK APPLICABLE HOLES & DEBURRED, ALODINED & PRIMED ALL BAREMETAL AREAS. INSTALLED NEW LONGITUDINAL BEAM WITH FAYING SURFACE SEAL. ALL WORK ACCOMPLISHED IAW 727 SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2 & 51-20-4. 2L73 4F RTA3WE 20040317001272004031700127SO 2004 3 17 SWIA200412942 120040225A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07232SW7819 3939 120306 WHEN FIRST POWER UP A/C RECEIVED A CONTROL FAULT ON FLAP. REPLACED FLAP CONTROL UNIT PER MM 27-50-00. OPS CHECK OK. 2L72 4T RTA31SO 20040317001312004031700131SO 2004 3 17 CHQA000442 120040216A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11263 145199 LEFT WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT WING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. BULB P/N 1317. 2L72 4T RTT00011AT 20040317001392004031700139NE 2004 3 17 SWIA200412951 220040225A7250 TURBINE BLADES CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT ENGINE TORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07907SW7138 7138 7511 NUMEROUS RIGHT ENGINE 7TH STAGE ROTOR BLADES DAMAGED, TORN. REMOVED AND REPLACED RIGHT ENGINE IAW RII 71-401. 2L72 4F4 FRTA21EA E15NE 20040317001512004031700151EA 2004 3 17 SWIA200412963 120040212A5320 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 280 LEFT FLOORBEAM LBL 9.0 O/B ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-57. 2L72 4F RTA21EA 20040318000102004031800010 2004 3 18 YENA200409 420040218A2562 BATTERY HONEYWELL AIRBUS320 A320232 3930326EU ELT ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15584JB357 11513245344 2149 CREW NOTED THAT AN ODOR FROM ELT COMPARTMENT. ODOR WAS COMING FROM ELT BATTERY. REMOVED AND REPLACED ELT IAW MM 25-65-00. 2L72 4F RTA28NM 20040318000152004031800015 2004 3 18 YENA200410 420040220A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ENTERTAIN SYS MALFUNCTIONED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15507JB1739 1240 PAX REPORTED OF A BURNING ODOR NEAR ROW 25 IN THE CABIN. LIVE TV SHUT DOWN AS A PRECAUTION, BURNING ODOR NO LONGER PRESENT. PERFORMED INFO NOTICE 2003-T050TRA, LIVE TV SYSTEM INTEGRITY CHECK, NO EVIDENCE OF ELECTRICAL ODOR NOTED, VISUAL INSPECTION PERFORMED. AS A PRECAUTION REPLACED SEBS IN ROW 24B & 25B. 2L72 4F RTA28NM 20040318000372004031800037EA 2004 3 18 COMA0460177 120040302A339764645 BUSS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01937CA 7044 FLIGHT 5810 EMERGENCY FLOOR PATH LIGHTING, AFT OF ROW 8 IS INOP. REPLACED THE LIGHT STRIP. 2L72 4F RTA21EA 20040318000392004031800039SO 2004 3 18 CHQA000437 120040301A3350 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR EMER INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11292 145488 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT IAW EMB 145 MM 33-40. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040318000602004031800060WP 2004 3 18 04FDEA00572 120040304A5347 SEAT TRACK DOUG DC10 DC1030F 3023504WP ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 MAIN CABIN AT FS 835 - 870 AT LBL 8.5 SEAT TRACK HAS CORROSION AFT INBOARD FLANGE. REMOVED CORRECTED SECTION OF SEAT TRACK. FABRICATED NEW SECTION OF SEAT TRACK AND INSTALLED IAW DC10 SRM 53-42-01 VOL 1, DC10 SRM 53-70-00 VOL 1 AND DC10 SRM 51-21-01 VOL 2. 2L73 4F RTA22WE 20040318000612004031800061WP 2004 3 18 04FDEA00573 120040304A5744ARC0502 HINGE DOUG DC10 DC1030F 3023504WP TE FLAPS DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 REWORK BARREL NUT HOLE NR 10 IS LARGER THAN CMM LIMIT ON RT WING O/B-I/B FLAP HINGE FITTING. CLARIFICATION OF N01776. N01776 & N02167 REMOVED BUSHING & OPEN BORE TO .748 IAW DC10 MM 57-44-08, HEAT TREATED BUSHING MAT'L IAW DPS 5.00-2 & DPS 1.05.5, ETCHED BORE IAW DC10 CMM 20-11-02. HFEC BORE IAW DC 10 NDT MANUAL PT6 51-00-01 NO CRACKS, ROTO PEENED BORE IAW DC10 CMM 20-11-01, FABRICATED BUSHING IAW DC 10 CMM 57-44-08. INSTALLED BUSHING IAW DC10 CMM 57-44-08 AND EO 8-5710-75068. 2L73 4F RTA22WE 20040318000692004031800069NM 2004 3 18 SWAA040599 120040225A53206546957 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR WEB CORRODED BETWEEN BS 500 AND BS 500A, RT SIDE OF FUSELAGE. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040318000772004031800077NM 2004 3 18 SWAA040607 120040226A53126546547599 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED PM CHECK, FOUND BULKHEAD WEB CRACKED AT BS 727, LBL 13.5 AND LBL 14.5, 25 BELOW CEILING IN MAIN WHEEL WELL. REPAIRED WEB PER EA. 2L72 4F A16WE 20040318000802004031800080 2004 3 18 SWAA040610 420040226A2565D31354 SLIDE BOEING737 7372T4 1384492NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040318000902004031800090NM 2004 3 18 SWAA040625 120040226A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 360 TO BS 380, LBL 65, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040318000912004031800091NM 2004 3 18 SWAA040626 120040228A5210507945 DOOR BOEING737 7377H4 1384404NM L1 OUT OF ADJUST A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29752SW 29804 AIRTURN BACK, AFTER TAKEOFF FAILED TO PRESSURIZE AND THERE WAS A LOUD AIR NOISE AROUND L1 DOOR AREA. DOOR HANDLE WAS DOWN AND L1 DOOR LIGHT WAS OUT. ADJUSTED L1 DOOR PER MM. 2L72 4F RTA16WE 20040318000922004031800092NM 2004 3 18 SWAA040627 120040227A1100BAC29PPS0774 PLACARD BOEING737 7373H4 1384600NM L2 DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 L2 DOOR EVAC SLIDE MISSING PLACARD. INSTALLED PLACARD ON L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318000932004031800093NM 2004 3 18 SWAA040628 120040228A3350100031 SIGN BOEING737 7377H4 1384404NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29725SW 27857 MID CABIN CEILING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2L72 4F RTA16WE 20040318000952004031800095NM 2004 3 18 SWAA040630 120040227A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 52 TO RBL 52, WL 208. REPAIRED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040318000982004031800098NM 2004 3 18 SWAA040634 120040227A55116547985 RIB BOEING737 7373H4 1384600NM HORIZONTAL STAB DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB RIB CREASED AT STAB STATION 129.50, LOWER TEE CHORD. REPAIRED LT STAB RIB PER SRM. 2L72 4F RTA16WE 20040318000992004031800099NM 2004 3 18 SWAA040635 120040227A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 5L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040318001002004031800100NM 2004 3 18 SWAA040636 120040227A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, LBL 45.6. REPAIRED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040318001072004031800107NM 2004 3 18 SWAA040643 120040227A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 FORWARD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040318001082004031800108 2004 3 18 SWAA040644 420040227A2565D31354 SLIDE BOEING737 737301 1384611NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318001092004031800109 2004 3 18 SWAA040645 420040228A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318001102004031800110NM 2004 3 18 SWAA040647 120040228A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040318001112004031800111NM 2004 3 18 SWAA040648 120040229A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 AND BS 500A, STRINGER 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040318001132004031800113NM 2004 3 18 SWAA040650 120040229A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 918, STRINGER 22R. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040318001142004031800114NM 2004 3 18 SWAA040651 120040229A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FRAMES CRACKED AT BS 188, LT AND RT SIDES, WL 208. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20040318001162004031800116NM 2004 3 18 SWAA040559 120040223A5313BAC1498 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SPV, FOUND BS 1008, STRINGER 27L, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F A16WE 20040318001172004031800117NM 2004 3 18 SWAA040560 120040223A57536546481 SPINDLE BOEING737 7372H4 138448CNM RT WING TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SPV, FOUND RT WING NR 8 T/E FLAP SPINDLE WITH CRACK INDICATION. REMOVED AND REPLACED NR 8 FLAP SPINDLE PER MM. 2L72 4F A16WE 20040318001182004031800118NM 2004 3 18 SWAA040562 120040223A53116546533 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 500, BETWEEN STRINGERS 28L TO 28R. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040318001192004031800119NM 2004 3 18 SWAA040563 120040223A53106546581 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT FRAME CRACKED AT THE NR 6 AND NR 7 STOPS. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040318001212004031800121 2004 3 18 SWAA040565 420040223A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318001222004031800122NM 2004 3 18 SWAA040566 120040223A3350 COVER BOEING737 7373L9 1384470NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER CRACKED AT ROW 14 DEF. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040318001242004031800124 2004 3 18 SWAA040568 420040223A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318001302004031800130NM 2004 3 18 SWAA040574 120040224A53136551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 4L. REMOVED AND REPLACED STRINGER SLICE PER SRM. 2L72 4F RTA16WE 20040318001312004031800131 2004 3 18 SWAA040575 420040224A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318001332004031800133NM 2004 3 18 SWAA040577 120040224A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 259, LBL 11 AND RBL 11, WL 208. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040318001342004031800134NM 2004 3 18 SWAA040578 120040224A53116520723 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040318001352004031800135NM 2004 3 18 SWAA040579 120040224A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STRINGER 28 L AND STRINGER 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040318001372004031800137NM 2004 3 18 SWAA040581 120040225A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT DOOR EXIT LIGHT COVER LOOSE. SECURED EMERGENCY EXIT LIGHT COVER PER MM. 2L72 4F RTA16WE 20040318001382004031800138NM 2004 3 18 SWAA040582 120040225A3350604222 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INTERMITTENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 AFT GALLEY EMERGENCY EXIT LIGHT BLINKING. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040318001392004031800139 2004 3 18 234TR0015 420040301A22104038890948 CONTROL PANEL BOEING737 737228 13844AGNM COURSE SELECTOR MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05234TR 23004 COPILOT COURSE SELECTOR ON MCP WILL NOT ALLOW YOU TO SELECT 122 DEGREES. REPLACED MCP PER MM 22-11-341 AND OPS CHECKED. 2L72 4F RTA16WE 20040318001412004031800141NM 2004 3 18 ABXA040093 120040301A335020131A POWER SUPPLY BOEING767 767281 1385109NM EMERGENCY LIGHT INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23788AX 23021 EMERGENCY EXIT LIGHTS GO OUT AFTER 10 SECONDS. SWAPPED TO SPARE BATTERY. SYSTEM CHECKED GOOD. DEFERRED SPARE BATTERY PER MEL 33-51-1, CAT-C, CODE 11, MBCB 03-11-04. PLACARD INSTALLED. REPLACED SPARE BATTERY PER B767 AMM 33-51-07-2. PLACARD REMOVED. 2L72 4F RTA1NM 20040318001432004031800143 2004 3 18 200414 420040229A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15566JB1781 2042 ELECTRICAL ODOR AROUND ROW 13/14. TURNED OFF LIVE TV SYSTEM. ODOR SUBSIDED. INSPECTED PER INFORMATION NOTICE 2003-T050TRA ROW 11-14 R/L. NO DEFFECTS NOTED. REMOVED AND REPLACED SEB AT 13R AS PRECAUTION IAW AMM 23-39-00. OPERATIONS CHECK GOOD AT THIS TIME. RAN SYSTEM FOR 6 HOURS AND NO ODOR NOTED. 2L72 4F RTA28NM 20040318001452004031800145SO 2004 3 18 C2XA04CL016 120040229A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INTERMITTENT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 CVG FLIGHT 2931 THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL TEST AND NO DEFECTS WERE FOUND. WHEN AIRCRAFT GOT TO IAH THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INTERMITTENT WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040318001472004031800147 2004 3 18 YENA200414 420040229A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15566JB1781 2042 ELECTRICAL ODOR AROUND ROW 13/14. TURNED OFF LIVE TV SYSTEM. ODOR SUBSIDED. INSPECTED PER INFORMATION NOTICE 2003-T050TRA ROW 11-14 R/L. NO DEFFECTS NOTED. REMOVED AND REPLACED SEB AT 13 RT AS PRECAUTION IAW AMM 23-39-00. OPERATIONS CHECK GOOD AT THIS TIME. RAN SYSTEM FOR 6 HOURS AND NO ODOR NOTED. 2L72 4F RTA28NM 20040318001482004031800148NM 2004 3 18 249TR0025 120040206A5753654642835 FLAP TRACK BOEING737 7372K5 138448XNM TE FLAPS DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 ULTRASONIC INSPECTION OF LEFT I/B TRACK OF O/B FLAP SHOWS DEFECT IN UPPER PORTION OF AFT ATTACH BORE. REPLACED I/B TRACK OF O/B FLAP. 2L72 4F RTA16WE 20040318001492004031800149NM 2004 3 18 CALA0400214 120040304A5311 FRAME BOEING757 757224 1384958NM BS 1340 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2748127 28968 INSPECTION FOUND AFT CARGO COMPARTMENT RT SIDEWALL FRAME DENTED ON TOP SURFACE AT BS 1340, S26R. REPAIRED IAW SRM 51-70-11, FIGURE 1. 2L72 4F RTA2NM 20040318001502004031800150SO 2004 3 18 CHQ2004F00000 120040305A322014524475001 STRUT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NLG INOPERATIVE E CHQAO OTHER O OTHER NRNOT REPORTED 1 SO01262SK 145168 BEARING CAP SHIMS ARE MIGRATING OUT FROM CAP FACES. SOME SHIMS MIGRATE INTO BEARING LANDING, BETWEEN CAP AND BALL JOINT BEARING. THE TORQUE SPECIFICATIONS ARE FOR DRY TORQUE VALUES AND THE BOLTS ARE BEING INSTALLED WITH BOLTS ARE BEING INSTALLED WITH (CA-100) WET. THUS BOLTS ARE BEING UNDER TORQUED AT INSTALLATION. 2L72 4T4 FRTT00011ATTE6CH 20040318001532004031800153EU 2004 3 18 MALA040224 120040224A2750HP14161005 CONTROL VALVE SAAB SF340 340B 7860101EU TE FLAPS FAILED A MALAO OTHER O OTHER LDLANDING 1 GL15367PX 340B271 LANDING IN DTW CREW REPORTED FLAPS WOULD NOT EXTEND. COMPLETED ALL FLAPS LANDING. FLAPS WILL NOT EXTEND DN FLAPS 0 AT DTW ALL CB IN. REMOVED AND REPLACED FLAP CONTROL VALVE S/N ON 1168, S/N OFF 1588 IAW SAAB MM CHAP 27 SEE 409 CARD FOR DEATILS, ALL CHECKS GOOD. 2L72 4T RTA52EU 20040318001552004031800155EU 2004 3 18 MALA040230 120040225A3234 CONTROL HANDLE SAAB SF340 340B 7860101EU MLG FAILED A MALAO OTHER J WARNING INDICATION DEDESCENT 1 GL15414XJ 340B414 LEFT MLG LIGHT WOULD NOT COME ON AFTER GEAR EXTENSION. FOLLOWED QRH AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE, COMPLETED GEAR SWINGS AND ALL INDICATIONS CHECK GOOD IAW SAAB AMM 31-31-05-02. 2L72 4T RTA52EU 20040318001562004031800156EU 2004 3 18 MALA040226 120040228A3397 WIRE SAAB SF340 340B 7860101EU EMERGENCY LIGHT BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15450XJ 340B450 LEFT EMERGENCY FLOOR LIGHTING FROM 2A-4A LAYING IN AISLE WITH WIRES BROKEN OFF LIGHT STRIP. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHTING P/N 6636-2 IAW AMM 33-50-20-4. 2L72 4T RTA52EU 20040318001572004031800157EU 2004 3 18 MALA040231 120040227A3230 CONTROL UNIT SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15436XJ 340B436 LANDING GEAR TRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION. LAMP TESTS GOOD AND OPERATION NORMAL DURING GEAR EXTENSION. REMOVED AND REPLACED LANDING GEAR CONTROL UNIT PER SAAB MM 32-31-05-2, EXTENSION AND RETRACTION TEST GOOD PER SAAB MM 32-30-00-5. 2L72 4T RTA52EU 20040318001582004031800158CE 2004 3 18 DXTA200400254 120040303A7830 WARNING LIGHT CESSNA500 560CESSNA 2076750CE THRUST REVERSER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07324QS 5600423 ON TAKEOFF ROLL AT 50 KNOTS, THE LEFT ENGINE THRUST REVERSER ARMED LIGHT CAME ON. REJECTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040318001602004031800160EA 2004 3 18 COMA0460181 120040303A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01471CA 7655 FLIGHT 5263 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2L72 4F RTA21EA 20040318001612004031800161NM 2004 3 18 UPS04241995 120040304A2612 FIRE LOOP BOEING727 72725C 138400HNM NR 1 ENGINE OUT OF POSITION A IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01937UP 19302 INSPECTION TYPE:N/A ON CLIMBOUT ENG 1 STRUT OVERHEAT LIGHT ILLUM. CLOSED BLEED AIR SWITCH & PULLED NR 1 BLEED VALVE CB AS PER CHECKLIST. REDUCED THRUST TO IDLE, LIGHT REMAINED ILLUMINATED, OPERATED AT IDLE FOR 3 MIN LIGHT REMAINED ILLUM. SHUT DOWN ENGINE. RAN ENGINE, CHECKED FOR PNEUMATIC LEAKS IN NR 1 STRUT AREA. NO LEAKS NOTED. REPOSITIONED FWD & AFT LOOPS C/W ENG POWER RUN. NO OVERHEAT INDICATIONS NOTED. 2L73 4F A3WE 20040318001642004031800164NM 2004 3 18 04FDEA00557 120040303A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 STATIC DISCHARGE DAMAGE AT BS 433 BETWEEN STR 20 AND 21 R/T. *S/D* REPAIRED IAW FED EX EA 7-5330-70631. 2L73 4F RTA3WE 20040318001672004031800167NM 2004 3 18 04FDEA00577 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281. RT OUTBD FLAP INBD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040318001692004031800169NM 2004 3 18 04FDEA00579 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75281 TITLE WINGS - RT O/B FLAP I/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001702004031800170NM 2004 3 18 04FDEA00580 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040318001722004031800172NM 2004 3 18 04FDEA00582 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040318001732004031800173NM 2004 3 18 04FDEA00583 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75282 TITLE WINGS - RT O/B FLAP - O/B HINGE BRACKET PIVOT, ACTUATOR & MOUNTING BORE - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001742004031800174NM 2004 3 18 04FDEA00587 120040305A5350 FRAME DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 AFT TAIL CONE FWD RT FRAME FOUND 2 EA STOP PLATE WORN. AFT TAIL CONE FWD RT FRAME 2 EA STOP PLATE REMOVED, FABRICATED AS PER DWG AKC7620 & INSTALLED AS PER EA 1-5390-75285. FUSELAGE AERODYNAMIC FAIRING AFT TAILCONE ASSY PLATE. 2L73 4F RTA22WE 20040318001782004031800178SO 2004 3 18 C2XA04SH139 120040304A335078812 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712552 145583 SHV - DURING C-CHECK, THE NUMBER FIVE EMERGENCY AISLE PATH LIGHT WOULD NOT ILLUMINATE DURING AN OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE AISLE PATH LIGHT ASSEMBLY IAW EMB 145 SRM 33-50-12. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040318001802004031800180SO 2004 3 18 C2XA04SH143 120040304A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER END OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 6, FIGURE 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040318001812004031800181SO 2004 3 18 C2XA04SH141 120040304A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV - DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040318001822004031800182SO 2004 3 18 C2XA04SH142 120040304A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040318001882004031800188NM 2004 3 18 04FDEA00593 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. 2L73 4F RTA22WE 20040318001892004031800189NM 2004 3 18 04FDEA00594 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001952004031800195NM 2004 3 18 04FDEA00601 120040305A2750 O-RING BOEING727 727200 138407ENM FLAP CONTROL VALFAILED A FDEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25240FE 20978 A-SYSTEM HYDRAULICS FAILED IN FLIGHT. IN CRUISE FLT LVL 220, NOTICED A-SYSTEM QUANTITY DECREASING, LEAK CONTINUED TILL CHECKLIST DIRECTED A-PUMPS TO BE TURNED OFF. FOUND O-RING FAILURE AT UPPER PORT OF FLAP CONTROL VALVE. REPLACED O-RING PER 727-200 MM 20-10-011-4. CLEANED AREA, PRESSURIZED AND CHECKED FOR LEAKS, NONE NOTED. TWO GALLONS A-SYS HYDRAULIC FLUID REMAINING, SERVICED HYDRAULICS IAW MM 12-12-000. AIRCRAFT OK FOR CONTINUED SERVICE. 2L73 4F RTA3WE 20040318001962004031800196 2004 3 18 04FDEA00602 420040306A2230 AUTOTHROTTLE SYS AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE FAILED A FDEAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO25682FE 800 705276 ON FINAL APPROACH, NR 1 THROTTLE STUCK AT ABOUT 15 DEGREES. DECLARED EMERGENCY AND FINISHED APPROACH. AFTER LANDING, THROTTLE MOVED FREELY. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01 CATEGORY: C EXPIRATION: 16MAR04 MEL 22-30-01: AUTOTHROTTLE SYSTEM INOP. ALL THRUST MUST BE MANUALLY SET. NO OPS WITHIN METRIC AIRSPACE. DEBRIEFED CREW, APPROACH WAS MADE WITH AUTOTHROTTLES ENGAGED. AUTOTHROTTLE COUPLING UNIT REPLACED 2L72 4F4 FRTA35EU E13NE 20040318001992004031800199NM 2004 3 18 04FDEA00605 120040306A278210605582 ACTUATOR BOEING727 727200 138407ENM KRUGER FLAPS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO25481FE 21463 NR 3 KRUEGER FAILED TO EXTEND ON APPROACH TO KRST, C/W RED TABS DIVERT TO KMSP. REMOVED AND REPLACED THE NR 3 KRUEGER FLAP ACTUATOR AND THE L/E FLAP-SLAT POSITION CONTROL MODULE IAW MM 27-81-22 AND MM 27-82-031-4. 2L73 4F RTA3WE 20040318002002004031800200NM 2004 3 18 04FDEA00606 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR 2L73 4F RTA22WE 20040318002012004031800201NM 2004 3 18 04FDEA00607 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (WING SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75297 - WINGS - OUTBD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR 2L73 4F RTA22WE 20040318002022004031800202NM 2004 3 18 04FDEA00608 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER I/B SURFACE FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040318002042004031800204NM 2004 3 18 04FDEA00610 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B FWD SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040318002052004031800205NM 2004 3 18 04FDEA00611 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET LOWER O/B NUT SIDE SURFACE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040318002062004031800206NM 2004 3 18 04FDEA00612 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25617FE 48748 LT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040318002072004031800207NM 2004 3 18 04FDEA00613 120040308A5744 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (WING SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75296, WINGS - O/B TE FLAPS - I/B HINGE BRACKET (WING SIDE) - ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040318002082004031800208 2004 3 18 P9RA20040009 420040306A2565 SLIDE BOEING757 757236 1384971NM DISLODGED A P9RAK NONE O OTHER NRNOT REPORTED 1 SO11521NA 25592 PILOT REPORT; AT GATE IN PHL, L1 DOOR SLIDE FELL OUT OF ITS CASING. REINSTALLED L1 DOOR SLIDE PER MM 256601. 2L72 4F RTA2NM 20040318002102004031800210EU 2004 3 18 UPS04141994 120040228A5330A53986202200 SKIN AIRBUSA300 A300F4622R 3930360EU FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01145UP 0828 INSPECTION TYPE: C1, LOWER FUSELAGE SKIN IS DENTED FWD OF TAIL JACK PAD AT FRAME 86. BLENDED GOUGES, FOUND OUT OF LIMITS. REMOVED JACK PAD, FLOOR PANEL, WALK BOARD TO FOM; FABRICATED REPAIR DOUBLER; ALODINED & PRIMED; INSTALLED; ALL IAW A300 SRM 53-10-12, 51-21-10, AND 51-40-23. 2L72 4F RTA35EU 20040318002132004031800213NM 2004 3 18 UPS04442002 120040228A5740 FITTING BOEING747 747SR46 1384816NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, BS 1241 LT WING REAR SPAR UPPER SPLICE FITTING FOUND CRACKS AT HOLE NR 5. BS 1241 LT WING REAR UPPER SPLICE FITTING HOLE NR 5 REAMED TO REMOVE CRACKS. HFEC INSPECTED RESULT CRACK FREE. FINAL HOLE DIAMETER IS 1.000 INCH AND BUSHING INSTALLED AS PER EO B747-5740-17032-A APPENDIX -E-. 2L74 4F RTA20WE 20040318002142004031800214NM 2004 3 18 UPS04442003 120040226A5313 STRINGER BOEING747 747SR46 1384816NM FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, FWD CARGO COMPT, LT STA 580 - STA 600 STR 46 FOUND DENT MARK. FWD CARGO COMPT LT BS 580 - BS 600 STR 46L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. 2L74 4F RTA20WE 20040318002162004031800216NM 2004 3 18 UPS04442005 120040227A5310 BEAM BOEING747 747SR46 1384816NM NOSE WHEEL WELL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, NOSE WHEEL WELL, VERTICAL BEAM WEB RT BS 280 BETWEEN 1ST AND 2ND STIFFENER ONE INSULATION BLANKET STAND OFF HOLE CRACK FOUND APPROX 2 INCHES LONG AS MARKED (WL 160 TO 170). BEAM WEB REPAIRED AND REPAIRED PART INSTALLED AS PER SRM 51-40-02 FIG 1. 2L74 4F RTA20WE 20040318002172004031800217NM 2004 3 18 UPS04M41997 120040112A5347AFA7789545 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN AT STA 1841 LBL 107 MOST OUTBOARD SEAT TRACK FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34, ORIG THICKNESS 0.112 INCH, MAT REMOVED 0.032 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL 1. NEW SEAT TRACK INSTALLED PER SRM 53-70-00 FIG 7 VOL 1, SRM 51-31-01 & 51-35-01 STA 1751 TO 2007 LBL 107. 2L73 4F RTA22WE 20040318002192004031800219EA 2004 3 18 COMA0460180 120040219A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01819CA 7415 TWO DRAIN BOLT HOLES FORWARD OF FUEL ACCESS PANEL 610AB SHOW INDICATIONS OF CRACKS DURING EDDY CURRENT INSPECTION. PERFORMED REPAIR OF RIGHT WING LOWER PLANK FUEL DRAIN VALVE RETAINING HOLES JUST FORWARD OF PANEL 640AB IN ACCORDANCE WITH BOMBARDIER REO 601R-57-51-417. 2L72 4F RTA21EA 20040318002202004031800220EA 2004 3 18 COMA0460182 120040304A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01716CA 7250 FLIGHT 5088 FLAPS FAIL WARNING MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040318002212004031800221SO 2004 3 18 C2XA04SH144 120040308A335074441 LAMP EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712519 145366 SHV - DURING PREFLIGHT INSPECTION THE EXIT SIGN ABOVE THE FORWARD FLIGHT ATTENDANTS SEAT WOULD NOT ILLUMINATE DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE INOPERTIVE EXIT SIGN IAW EMB 135 AMM 33-50-14. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040318002222004031800222NM 2004 3 18 PCAA0403176 120040301A3244H31X97513 TIRE DHAV DHC8 DHC8102 2809003NM MLG FAILED A PCAAO OTHER O OTHER CRCRUISE 1 EA13848EX606 606 331 FLIGHT 3940 REPORTED EXTENSIVE DAMAGE TO REAR OF NR 2 NACELLE AND LOSS OF NR 2 HYDRAULIC CONTENTS DUE TO THE OUTBOARD RIGHT MAIN TIRE ASSEMBLY EXPLODING DURING FLIGHT. AN EMERGENCY WAS DECLARED AND THE CABIN WAS PREPPED FOR EMERGENCY. AIRCRAFT WILL BE INTERIM REPAIRED AND FERRIED FOR REPAIRS. 2H72 4T RTA13NM 20040318002232004031800223NM 2004 3 18 PCAA0403178 120040305A33506038443 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT FAILED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13818EX 235 MAINTENANCE CREATED DISCREPANCY DUE TO THE LEFT HAND AFT EGRESS EMERGENCY LIGHT NOT TESTING. IT WAS FOUND THAT THE ASSOCIATED BATTERY PACK WAS FAULTY. PACK WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 20040319000052004031900005NE 2004 3 19 HNAA0400012 220040221A7200 ENGINE DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 1 FAILED A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA07965HA112357847 450 AG0042 NR 1 ENGINE FAILED IN FLIGHT. PRIOR TO ENG NR 1 ENG OIL PRESS WARN LIGHT MOMENTARILY ILLUMINATED. WHEN ENGINE FAILED PROP DID NOT FX HAD TO USE ALT FX. AIRCRAFT WAS IN DESCENT, ENGINE AND PROP WERE IN A STABLE CONDITION. REMOVED AND REPLACED ENGINE. APPEARS ANGLE GEAR BOX FAILED ON AGB. 2H72 4T4 TRTA13NM E20NE 20040319000062004031900006 2004 3 19 5040022204 420040222A3418600591541 TRANSDUCER CNDAIRCL600 CL6002B16 1900305EA RT AOA OUT OF TOLERANCEE S4WAK NONE O OTHER ININSP/MAINT 1 WP07807Z 5093 5040 DURING COMPLETION OF AD 2003-22-12, FOUND RIGHT AOA TRANSDUCER OUT OF TOLERANCE. 2L72 4F RTA21EA 20040319000072004031900007 2004 3 19 5040022204A 420040222A3418600591541 TRANSDUCER CNDAIRCL600 CL6002B16 1900305EA LT AOA OUT OF TOLERANCEE S4WAK NONE O OTHER ININSP/MAINT 1 WP07807Z 5093 5040 DURING COMPLETION OF AD 2003-22-12, FOUND LEFT TRANSDUCER OUT OF TOLERANCE. 2L72 4F RTA21EA 20040319000102004031900010WP 2004 3 19 GKZR200482311 120040303A5310 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 LEFT UPPER CARGO COMP BETWEEN STA 902 & STA 920 FINGER DOUBLER ABOVE WHEEL WELL CORRODED AND RIVET HEAD SHEARED. CORRODED FINGER DOUBLER REMOVED, CORROSION ON PANEL REMOVED IAW DC-8 SRM 53-2-0. THICKNESS OF PANEL .063 CORRODED SECTION BEYOND LIMITS IAW DC-8 SRM 53-2-0. CORRODED SECTION CUT OUT AND REPAIR DONE IAW DC-8 SRM 53-2-1 FIG. 7 USING .071 2024T3 DOUBLER, .063 FILLER. AREA TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-21. (CLOSED) 2L74 4F RT4A25 20040319000112004031900011WP 2004 3 19 IXXA0400012O 120040303A3260H2024B SWITCH DOUG DC8 DC862F 3021972WP MLG DOOR BROKEN A IXXAO OTHER N FALSE WARNING CRCRUISE 1 SW11799AL73382147 45992335 DURING CRUISE FROM WSAP TO RJTY, DOORS NOT LATCHED LIGHT CAME ON. BOTH ALTERNATE LIGHTS STAYED OUT. MAINTENANCE REMOVED AND REPLACED RIGHT LATCH DOOR SWITCH PER ALL APPLICABLE MANUALS OPERATIONAL CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040319000122004031900012WP 2004 3 19 IXXA0400011O 120040303A2121 FAN DOUG DC8 DC862F 3021972WP COCKPIT BURNED OUT A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW11799AL73382147 45922335 DURING CRUISE FROM WSAP TO RJTY, SMOKE WAS IN COCKPIT. CREW TURNED OFF BOTH RECIRC FANS AND SMOKE CLEARED. CREW CONTINUED TO RJTY AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE TROUBLESHOT TO BAD RIGHT RECIRC FAN. THIS ITEM WAS TRANSFERRED TO THE DEFERRED MAINTENANCE ITEM LOG BOOK 29190 CAT -C- NO FLY DATE 3/15/04. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040319000152004031900015 2004 3 19 MALA040238 420040307A3440HG2001BC02 IRU BAC 146 AVRO146RJ85A1500097EU NR 1 FAILED A MALAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 GL15515XJ E2333 PASSING THROUGH 10,000 FEET LOST IRU ON CAPT SIDE. RETURNED TO DTW. REMOVED AND REPLACED NR 1 IRU ALL CHECKS GOOD IAW RJ-85 MM CHAP 34, P/N ON-OFF HG2001BC02, S/N OFF 97120734, S/N ON 97110762. 2H74 4F RTA49EU 20040319000162004031900016EU 2004 3 19 MALA040237 120040306A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15414XJ 340B414 AT 24 LN POWER SUPPLY EMERGENCY LIGHT PACK BAD. REMOVED AND REPLACED 24 LN POWER SUPPLY, P/N ON & OFF 3301-51, S/N ON 2006, S/N OFF 1412. ALL CHECKS ARE GOOD, ALL IAW SF340MM. 2L72 4T RTA52EU 20040319000172004031900017NE 2004 3 19 MALA040222 220040302A7320219333010 HMU BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 1 ENGINE FAILED A MALAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 GL15523XJ E2348 NR 1 ENGINE SHUTDOWN. NR 1 ENGINE FLAMED OUT UNCOMMANDED AFTER BEING STARTED FOR TAXI. RETURN TO GATE. CODES ON ESU NR 1 & 8 FADAM, CAUSE OF UNCOMMANDED SHUTDOWN TO BE HMU. REMOVED AND REPLACED HMU IWA AMM 73-20-01 401. PERFORMED OPS CHECKS IAW 71-00-00 & 72-00-00, ALL CHECKS GOOD. P/N ON/OFF 2-193-330-10, S/N ON 00AGU856; OFF 96AGU503C. A/C OKAY FOR CONTINUED SERVICE. 2H74 4F4 FRTA49EU E6NE 20040319000202004031900020EU 2004 3 19 MALA040236 120040307A27304068259902 SENSOR BAC 146 AVRO146RJ85A1500097EU ELEVATOR TRIM MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15511XJ E2325 ELECTRIC PITCH TRIM FAILED DURING FLAP RETRACTION (FTC-ILLUMINATED AS FLAPS WERE SELECTED FROM 18 DEG, TO UP THE FTC BEGAN TO TRIM UP AND IT FAILED HALFWAY TO 0 DEGREE FLAPS) VERIFIED. REMOVED AND REPLACED ELEV TRIM DUAL POSITION SENSOR. P/N OFF/ON 4068259-902, S/N OFF 97082193, S/N ON 96112330. ELECT PITCH & TRIM SYS TEST OF DFGC OPS CHECK GOOD IAW AMM 27-52-22 PAGE 201. 2H74 4F RTA49EU 20040319000222004031900022NM 2004 3 19 HNAA0400016 120040305A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07934HA 139 CORROSION ON STRINGER. 2H72 4T RTA13NM 20040319000232004031900023NM 2004 3 19 PCAA0403177 120040307A27202379003001 REGULATOR VALVE DHAV DHC8 DHC8102 2809003NM RUDDER FAULTY A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13809EX31505 302 FLIGHT 3996 HAD TO RETURN TO FIELD DUE TO HAVING THE NR 2 RUDDER HYDRAULIC, RUDDER PRESSURE, AND RUDDER FULL PRESSURE LIGHTS ILLUMINATE AFTER TAKEOFF. MAINTENANCE FOUND THE RUDDER PRESSURE REGULATOR VALVE TO BE AT FAULT. THE RUDDER PRESSURE REGULATOR VALVE WAS REPLACED AND THE SYSTEM OPERATIONAL CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040319000252004031900025 2004 3 19 PCAA0403180 420040306A34257003360941 COMPUTER DHAV DHC8 DHC8102 2809003NM NR 2 AHARS FAULTY A PCAAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 EA13984HA26858234 377 FLIGHT 3893 HAD TO RETURN TO FIELD DUE TO NR 2 ADI AND HSI FAILING ON INITIAL CLIMB. MAINTENANCE REMOVED AND REPLACED NR 2 AHARS COMPUTER AND OPERATIONAL CHECKED NR 2 HSI AND ADI, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040319000262004031900026SO 2004 3 19 C2XA04SH145 120040308A541114576056007 RIB EMB 145 EMB145LR 3260212SO LT NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV - DURING C-CHECK THE LEFT UPPER COWLING OUTBOARD REINFORCEMENT ANGLE WAS FOUND TO BE GOUGED BETWEEN STATION XN 2355 AND XN 3168. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040319000282004031900028WP 2004 3 19 0400371242 120040304A3350 BATTERY DOUG DC10 DC1030 3023501WP EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01242NW 47845 DURING LINE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND BATTERY. ALSO FOUND EMERGENCY LIGHT ARM CIRCUIT BREAKER BAD. REPLACED CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20040319000292004031900029NM 2004 3 19 0400386309 120040306A3350 POWER SUPPLY BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT AND BETWEEN DOOR 2R AND 3R. REPLACED THE POWER SUPPLY FOR THE LIGHTS ON THE LEFT SIDE OF THE AIRCRAFT AND REPLACED A LIGHT ASSEMBLY TO REPAIR THE LIGHTS BETWEEN DOOR 2R AND 3R. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040316002112004031600211 2004 3 16 SWIA200412922 420040216A22156224404101 SERVO CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AUTOPILOT FAILED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07411SW 7067 AUTOPILOT JERKS LEFT AND RIGHT MAINLY IN TURNS AND MOST PRONOUNCED WHEN SELECTING AND DE-SELECTING TURBULENCE BUTTON. REMOVED AND REPLACED RIGHT AUTO PILOT SERVO IAW 22-11-21. OPS CHECK GOOD. P/N: 622-4404-101, S/N OFF: 122. 2L72 4F4 FRTA21EA E15NE 20040316002192004031600219NM 2004 3 16 CHA200483002 120040227A335030767001 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 CEILING MOUNTED AREA LIGHT FOR EMERGENCY LIGHTS FWD ASSEMBLY INOP. 2L73 4F A3WE 20040317000162004031700016NM 2004 3 17 P5CA0401044 120040224A8097 CONNECTOR BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL START VALVE DIRTY A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23452PA 30810 706222 STATUS MESSAGE NR 1 ENG START VALVE, ENGINE START VALVE FAILED TO OPEN NORMALLY. CLEANED NR 1 ENGINE START VALVE CONNECTOR. RESECURED & OPS CHECK OK PER MM 80-11-00 PG 501. 2L74 4F4 FRTA20WE E23EA 20040317000212004031700021NM 2004 3 17 2004UALA00165 120040224A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29389UA 24664 STA 947 RBL 45.5 FLOORBEAM UPPER CAP HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20040317000222004031700022NM 2004 3 17 2004UALA00166 120040224A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 NEED REPAIR TO BS 178 FWD BULKHEAD. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB ON FWD BULKHEAD AT BS 178, LBL 5.7, WL 212. 2L72 4F4 FRTA16WE E2GL 20040317000282004031700028NM 2004 3 17 2004UALA00172 120040226A4910 APU BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU BAY FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29521UA 24891 DIVERTED DUE TO APU FAILURE WITH RT GENERATOR DRIVE LIGHT INOP. FOD ON LOAD COMPRESSOR. AT ENGINE DISSASSEMBLY FOUND LOAD COMPRESSOR LABRYNTH SEAL ABRADIBLE WITH HIGH WEAR CAUSING POOR PRESSURE BALANCE RESULTING IN HOC WEAR DUE TO VIBRATION FROM FOD. 2L72 4F4 FRTA2NM E17NE 20040317000342004031700034WP 2004 3 17 ABXA040084 120040218A5310591140311 STRUCTURE DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23908AX 47008 RIVET ROW FOUND CRACKED AT STA 76.550 UNDER CO-PILOT'S WINDSHIELD WIPER BETWEEN APPROXIMATELY LONGERON 3 AND 4 RIGHT. REPAIRED AREA IAW EA 53100075-003-2. 2L72 4F A6WE 20040317000462004031700046WP 2004 3 17 04FDEA00538 120040301A5270 RELAY DOUG DC10 DC1030 3023501WP ANNUNCIATOR FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25309FE 48298 IN CRUISE FLIGHT AIR COND DOORS ANNUNCIATOR LIGHT ON S/O PANEL ILLUMINATED FOR APPROX 1MIN THEN WENT OUT. RED TABS REQUIRED DIVERTING TO NEAREST SUITABLE AIRPORT. AIRCRAFT DIVERTED TO IND. TROUBLESHOT WITH TAFI 52-40-00AB FOUND RELAY R5-5431 BAD. REMOVED & REPLACED RELAY, OPS CHECK GOOD. 2L73 4F A22WE 20040317000512004031700051WP 2004 3 17 0400329969 120040302A2130 ANNUNCIATOR DOUG DC9 DC931 3022065WP CABIN PRESSURE ACTIVATED A NWAAB EMER. DESCENT JS WARNING INDICATION AFFECT SYSTEMS DEDESCENT 1 GL019333 47246 THE RED CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AT FL240 DURING DESCENT. CABIN WAS APPROACHING 10,000 FT, OUTFLOW VALVE INDICATED CLOSED, AND NO ASSOCIATED NOISE IN COCKPIT OR CABIN. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDED TO 10,000 FT MSL. AIRCRAFT LANDED IN MEM WITHOUT INCIDENT. MAINTENANCE BITE CHECKED PRESSURE CONTROLLERS, INSPECTED FOR DUCT LEAKS, AND RETURNED THE AIRCRAFT TO SERVICE WITH A PNEUMATIC TROUBLESHOOTING FORM PROVIDED. 2L72 4F A6WE 20040317000602004031700060NM 2004 3 17 DL73S040166 120040217A2780654496112 ACTUATOR BOEING737 737232 1384475NM GROUND SPOILER LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27323DL 23095 ON TAXI TO GATE POSTFLIGHT LOST A-SYSTEM HYDRAULICS, QUANTITY ZERO AND PRESSURE ZERO. REPLACED LEFT OUTBOARD SPOILER ACTUATOR FOR LEAKAGE. 2L72 4F RTA16WE 20040317000612004031700061NM 2004 3 17 DL764040167 120040217A3350D71702001 POWER SUPPLY BOEING767 767432ER 1385134NM SLIDE LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27829MH 29700 DURING PRE-DEPARTURE CHECK AFTER FLIGHT 225, FOUND 2L DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REBULBED, NO HELP. REPLACED POWER SUPPLY M6759. EXTERIOR EMERGENCY SLIDE LIGHT AT 2L CHECK OK. 2L72 4F RTA1NM 20040317000622004031700062NM 2004 3 17 DLM88040168 120040218A2432249701544 BATTERY DOUG MD88 MD88 3023688NM E/E BAY SMOKE A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27993DL 53345 AMT NOTICED SMOKE COMING OUT OF VENT BEHIND NOSE GEAR. REPLACED BATTERY, CHARGER, AND CIRCUIT BREAKER. 2L72 4F RTA6WE 20040317000632004031700063NM 2004 3 17 DL73S040169 120040218A534065469226 SUPPORT FITTING BOEING737 737232 1384475NM CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 CORROSION WAS NOTED ON BOTH THE LT AND RT BS 685 MLG SUPPORT FITTINGS IN THE LUG BORES AND FACES. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW ERA 386114-14. 2L72 4F RTA16WE 20040317000712004031700071NE 2004 3 17 DLM88040179 220040220A73207696912 BELLOWS DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENG FCU MALFUNCTIONED A DALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO27937DL 49810 725528 IN CRUISE FLT LVL 350 THREE HRS INTO FLT LT ENGINE WENT TO INCREASED THRUST 209 EPR 96 PERCENT N1 EGT 553, PULLED BOTH THROTTLES IDLE RT ENG RESPONDED, LT ENGINE STAYED AT HIGH THRUST FUEL HEAT ON AND ENGINE RETURNED TO NORMAL. INSPECTED MOISTURE TRAP AND SERVICED FUEL CONTROL BELLOWS. RAN ENGINE. UNABLE TO DUPLICATE. 2L72 4F4 FRTA6WE E9NE 20040317000742004031700074NM 2004 3 17 DLM88040184 120040222A2910 LINE DOUG MD88 MD88 3023688NM LT ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27914DL 49545 EN ROUTE TO EWR FROM ATL A/C SUFFERED HYDRAULIC FAILURE. CREW ELECTED TO DIVERT TO GSO AS A PRECAUTION. REPLACED LT ENGINE HYDRAULIC RETURN LINE FOR LEAKAGE. 2L72 4F RTA6WE 20040317000882004031700088NM 2004 3 17 DL757040200 120040228A33201C610F SWITCH BOEING757 757232 1384965NM LAV DOOR LIGHT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27662DN 24991 ON TAXI IN THE FLIGHT ATTENDANT IN THE MID SECTION DETECTED SMOKE FROM THE MID LAV. REPLACED LAV DOOR LATCH LIGHT SWITCH. 2L72 4F RTA2NM 20040317000982004031700098NM 2004 3 17 DLM88040212 120040302A3350RPS1B CHARGER DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27904DL 49535 EMERGENCY LIGHTS FROM SEAT 31 AND AFT INOPERATIVE. REPLACED BATTERY PACK. 2L72 4F RTA6WE 20040317001042004031700104NM 2004 3 17 P5CA0401047 120040302A5210 STOP BOEING747 747236B 1384804NM L-1 DOOR OUT OF ADJUST A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23924FT 21730 L-1 DOOR DIFFICULT TO CLOSE. ADJUSTED ALL STOPS AS REQ'D IAW MM 52-11-01, OPS CHECK NORMAL. 2L74 4F A20WE 20040317001182004031700118NM 2004 3 17 F3LA200400019 120040303A5320 SUPPORT BOEING737 7373S1 138447SNM GALLEY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED LT AFT GALLEY WALL SUPPORT CORRODED AT STA 989, LBL 44. REPLACED WALL SUPPORT PER SOPM 20-41-02 AND SRM 51-40-02. 2L72 4F RTA16WE 20040317001292004031700129NM 2004 3 17 F3LA200400021 120040303A531565C33367 FLOOR SUPPORT BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED AT NUT PLATE HOLES, RBL 51, STA 947 TO STA 967, WL 208. REPLACED FLOOR SUPPORT PER SRM 51-40-2 AND 53-60-51. 2L72 4F RTA16WE 20040317001492004031700149EA 2004 3 17 SWIA200412961 120040212A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07920SW 7660 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-58. 2L72 4F RTA21EA 20040318000262004031800026NM 2004 3 18 F3LA200400027 120040303A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM DAMAGE UNDER PHENOLIC BLOCK AT STA 986, LBL 45. REMOVED DAMAGED FLOORBEAM, LOCATED HOLES FOR NEW FLOORBEAM AND INSTALLED NEW BEAM PER SRM 51-40-02. 2L72 4F RTA16WE 20040318000272004031800027NM 2004 3 18 F3LA200400028 120040303A5320 SILL BOEING737 73736E 138443ANM FUSLAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED L-2 DOOR MOP SILL CORRODED. REPLACED MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20040318000362004031800036SO 2004 3 18 CHQA000453 120040102A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY SIGN DISCONNECTED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11561 145447 EMERGENCY EXIT SIGN (LOWER FWD) ON SERVICE DOOR INOP. UPON REMOVAL OF EMERGENCY EXIT SIGN FOUND A CONNECTOR NOT CONNECTED. RECONNECTED CONNECTOR AND OPS CHECK EMERGENCY EXIT SIGN. OPS CHECK WAS GOOD. ALL WORK IAW EMB 145 AMM CH 33-50. 2L72 4T RTT00011AT 20040318000402004031800040GL 2004 3 18 P5CA0401049 220040304A7200 ENGINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 3 LEAKING A P5CAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP23452PA 30810 706221 WHILE STARTING AT GATE NR 3 ENG LEAKING FUEL OUT OF THE BOTTOM MAST AFTER START. FOUND FUEL SUPPLY LINE CONNECTION AT PYLON WET. LOOSENED, REPOSITIONED AND TIGHTENED AS PER 73-11-10, OPS CHECKED ENG PER MM 72-00-00, NO LEAKS NOTED. 2L74 4F4 FRTA20WE E23EA 20040318000492004031800049WP 2004 3 18 04FDEA00559 120040303A3620 PRESSURE SWITCH DOUG DC10 DC1030 3023501WP PNEU MANIFOLD MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25319FE 47820 NR 3 MANIFOLD FAILURE LIGHT ILLUMINATED IN CRUISE AT FL 370. RED TABS FOLLOWED. T/S PER TAFI 36-23-00 FAULT CODE BC/YZ. PROBLEM DUPLICATED WITH OR WITHOUT PNEU SYS NR 3 PRESSURIZED. ACCOMPLISHED NR 3 PNEUMATIC SYSTEM DECAY CHECK PER DC-10 JRH TEST PASSED. WHEN DUPLICATING PROBLEM PNEU PRESSURE SWITCH FAULT BALL WOULD ILLUMINATE ON FAULT INDICATOR WITH FAIL LIGHT. REMOVED AND REPLACED NR 3 PNEUMATIC MANIFOLD FAILURE PRESSURE SWITCH PER MM 36-23-03-4. OPS CHECKED NORMAL. ITEM CLEARED, A/C OK TO CONTINUE. 2L73 4F A22WE 20040318000572004031800057WP 2004 3 18 04FDEA00569 120040304A5312 BULKHEAD DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 FWD NOSE WHEEL WELL BULKHEAD FWD SIDE HAS A CORRODED STRAP. REMOVED CORRODED STRAP. STRAP FOUND TO BE AN EXISTING REPAIR. FABRICATED REPAIR IAW DC10 SRM 53-00-01 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2, CORROSION FOUND TO BE LEVEL 2. 2L73 4F RTA22WE 20040318000592004031800059WP 2004 3 18 04FDEA00571 120040304A5310AGA318323 SHEAR TIE DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 AFT LWR CARGO COMPARTMENT FS 1971 AFT SIDE OF FRAME BETWEEN L-51L AND L-51R SHEAR TIE IS CORRODED. REMOVED SHEAR TIE, INTERCOSTAL, CLIPS AND SPLICE FRAME. CORROSION ON SHEAR TIE FOUND OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW SHEAR TIE, INTERCOSTAL CLIP AND SPLICE FRAME IAW DC10 SRM 51-35-01 VOL 2 AND 51-33-01 VOL 2. 2L73 4F RTA22WE 20040318000942004031800094NM 2004 3 18 SWAA040629 120040227A53436582770 SUPPORT BEAM BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND RT MLG SUPPORT BEAM CORRODED ON LOWER SURFACE. REPAIRED BEAM PER ER. 2L72 4F RTA16WE 20040318000962004031800096NM 2004 3 18 SWAA040631 120040227A53116546557 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 887, STRINGER 21R. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040318000972004031800097NM 2004 3 18 SWAA040632 120040227A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 418, RBL 70.53. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040318001042004031800104NM 2004 3 18 SWAA040640 120040227A3350101114 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 11DEF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER PER MM. 2L72 4F RTA16WE 20040318001052004031800105NM 2004 3 18 SWAA040641 120040227A53306552880 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT TOP AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040318001202004031800120NM 2004 3 18 SWAA040564 120040223A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040318001252004031800125 2004 3 18 SWAA040569 420040224A2565D31354 SLIDE BOEING737 737301 1384611NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED THE L1 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2L72 4F RTA16WE 20040318001282004031800128NM 2004 3 18 SWAA040572 120040224A53116547951 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT CRACKED AT FORWARD SIDE OF CUTOUT, BY CENTERING PAD. REPAIRED FUSELAGE FRAME PER EA. 2L72 4F RTA16WE 20040318001322004031800132NM 2004 3 18 SWAA040576 120040224A3350 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29794SW 30605 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS. 2L72 4F RTA16WE 20040318001442004031800144 2004 3 18 200413 420040218A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN SHORTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15571JB1270 2125 ELECTRICAL BURNING SMELL OBSERVED IN LAST 5 ROWS OF CABIN, LIVE TV TURNED OFF. PERFORMED INFORMATION NOTICE 2003-T050TRA LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR. FOUND SEB AT 24E EVIDENCE OF LIQUID SPILL. REMOVED AND REPLACED SEB AT 24E IAW LTV MM 23-39-00. SYSTEM OPERATION OK. 2L72 4F RTA28NM 20040318001522004031800152EU 2004 3 18 MALA040227 120040301A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 WHILE REMOVING EMERGENCY FLOOR TRACK LIGHTING STRIP, NOTED CORROSION ON LT AND RT CENTER AISLE SEAT TRACKS WEBS AT APPROXIMATELY STA 303. REMOVED CORROSION FROM LT & RT CENTER AISLE FWD SEAT TRACKS AND REPAIRED IAW 01-04031 CARD 210633 FOR DETAILS. 2L72 4T RTA52EU 20040318001542004031800154 2004 3 18 MALA040229 420040226A2330548315 CRADLE SAAB SF340 340B 7860101EU HANDSET DAMAGED A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15437XJ 340B437 FLIGHT ATTENDANT OVERHEAD PA, CALL AND EMERGENCY STATUS LIGHTS INOP. REPLACED FLIGHT ATTENDANT HANDSET CRADLE IAW SF340 AMM CHAPTER 23/30/05/4. ALL CHECKS GOOD. P/N ON&OFF 5483-1-5, S/N OFF 1050, S/N ON 648. 2L72 4T RTA52EU 20040318001592004031800159CE 2004 3 18 DXTA200400247 120040219A3234 SWITCH CESSNA500 560CESSNA 2076750CE MLG DIRTY E DXTAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL07396QS 5600396 DURING GEAR EXTENSION, HAD ONE RED AND NO GREEN INDICATION. COMPLIED WITH CHECKLIST, NOTICED CIRCUIT BREAKER DID NOT POP, MOVED HANDLE LEFT TO RIGHT SEVERAL TIMES WHICH FINALLY ACTIVATED THE GEAR EXTENSION PROCESS RESULTING IN A SAFE GEAR INDICATION. RECYCLED THE GEAR AND PROBLEM CAME BACK, ACCOMPLISHED AIR TURNBACK TO APF. OPS CHECKED LANDING GEAR AND COULD NOT GET PROBLEM TO DUPLICATE. FOUND DUST ON GEAR HANDLE, CLEARED GEAR HANDLE SWITCHES, SYSTEM OPS CHECK GOOD IAW 560 MM CHAPTER 32-01-00. 2L72 4F RTA22CE 20040318001622004031800162NM 2004 3 18 UPS04M41996 120040304A3350 BATTERY DOUG MD11 MD11F 3023600NM EMERGENCY LIGHTSDISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01250UP NR 1 EMERGENCY BATTERY LOW WARNING ILLUM. REMOVED AND REPLACED EMERGENCY BATTERY AS PER MM 33-51-01, OPS CHECK OK. 2L73 4F RTA22WE 20040318001682004031800168NM 2004 3 18 04FDEA00578 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75281. RT OUTBD FLAP INBD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040318001762004031800176NM 2004 3 18 04FDEA00590 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING I/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HOLE FOUND CORROSION. CORROSION REMOVED & REPLACED AS PER EA 1-5750-75312, TITLE : WINGS - I/B TE FLAP - RT O/B BRACKET (FLAP SIDE) - PIVOT BORE CORROSION - REPAIR. 2L73 4F RTA22WE 20040318001772004031800177SO 2004 3 18 C2XA04IA023 120040301A33507287580503 LIGHT EMB 145 EMB145LR 3260212SO CABIN BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713988 145265 DURING SCHEDULED MAINTENANCE ONE OF THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS WAS FOUND TO BE INOPERATIVE. THE AFFECTED STRIP WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040318001842004031800184NM 2004 3 18 C1HA200493001 120040303A335038931002 BATTERY PACK BOEING727 727212 138407GNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15293AS 21348 EMERGENCY EXIT LIGHT ABOVE AFT AIRSTAIRS INOP. 2L73 4F A3WE 20040318001852004031800185NE 2004 3 18 P5CA0401050 220040305A7597 CONNECTOR BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 1 BLEED VALVELOOSE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23505MC 21251 517343 NR 1 ENG WILL NOT START. MANUAL START UNSUCCESSFUL. FOUND CONNECTOR LOOSE ON NR 1 ENG BLEED AIR VALVE. RECONNECTED PLUG, OPS CHECK OK PER MM 36-11-00. 2L74 4F4 FRTA20WE E23EA 20040318001902004031800190NM 2004 3 18 04FDEA00596 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001982004031800198 2004 3 18 04FDEA00604 420040306A22202588838 SENSOR BOEING727 727200 138407ENM ZONE 300 FAILED A FDEAJBA DUMP FUEL EMER. DESCENT UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO25209FE6464 5426 22931 DURING CRUISE FLT AT FL330 AT .82 MACH THE A/C PERF U/C ROLL DOUBLETS (DUTCH ROLL MOTION). A/P AND STAB WAS OUT OF TRIM WITH A PITCH UP ATT DEV. TRIMMED THE STAB AND LEVELED A/C AND RECONN A/P. A/P WAS IN SYS-B. WHEN RECONN, THE A/P TRIMMED NOSE UP, HAD TO DISC A/P AND APPLY 20 LBS OF DOWN ELEV FORCE TO LEVEL A/C. TRIED SYS-A AND IT WAS WORSE. THE ELEV POS IND SHOWED A SPLIT STAB (LT HIGHER THAN RT). DECLARED AN EMERGENCY, DUMPED 9K OF FUEL AND WITH A/P OFF A/C TOOK MORE PRESS TO TURN RT THAN LT. CHECK PER MM 27-10-000-5, CHECKS NORMALLY. CHECKED ALL CABLES AND PULLEYS ASSOC WITH AILERONS, ALL CHECK NORMALLY. REMOVED LT ELEV POS SENS PER MM 22-11-071-5 REF WRI 22-10/7229 AND 22-30/7234. 2L73 4F RTA3WE 20040318002092004031800209CE 2004 3 18 069041 120040307A2751 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS FAILED A NSVAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27136MJ UE36 AIRCRAFT DEPARTED HYA UPON CALLING GEAR UP, THE GEAR HORN SOUNDED AND DID NOT STOP, THE INTRANSIT LIGHT ILLUMINATED AND DID NOT GO OUT, THE GEAR WAS EXTENDED AND RETRACTED AGAIN WITH THE SAME RESULTS, THE AIRCRAFT RETURNED TO HYA. MAINTENANCE REMOVED THE FLAP SWITCH AND FOUND SWITCH NOT MAKING CONTACT. ADJUSTED SWITCH, RE-INSTALLED FLAP SWITCH, OP CHECKED GOOD. 2L72 4T RTA24CE 20040318002112004031800211NM 2004 3 18 UPS04442000 120040228A5711 SPAR BOEING747 747SR46 1384816NM WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:C BS 1241 WING REAR SPAR LEFT UPPER CHORD FOUND CORROSION AT HOLE NR 9 APPROX 0.030 INCH DEPTH. BS 1241 WING REAR SPAR LEFT UPPER CHORD BOLT HOLE NR 9 CORROSION REMOVED NDT INSPECTED RESULT CORROSION FREE. BOLT HOLE BUSHING REPAIRED AS PER EO B747-5740-17032-A APPENDIX -E-. SEPARATE BUSHING INSTALLED IN INTERNAL SPLICE FITTING AND UPPER CHORD. 2L74 4F RTA20WE 20040318002152004031800215NM 2004 3 18 UPS04442004 120040227A5340 FITTING BOEING747 747SR46 1384816NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:C RT WING BS 1241 WING REAR SPAR UPPER SPLICE PLATE NR 4 FASTENER HOLE WAS CRACKED APPROX 0.040 INCH LONG RUNNING TOWARDS AFT (WL 180). BUSHING REPAIRED AS PER EO B747-5740-17032-A FINAL OVERSIZE FASTENER HOLE WAS 1.000 INCH AS PER APPENDIX -E-. 2L74 4F RTA20WE 20040319000022004031900002SO 2004 3 19 CHQA0000435 120040222A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11273 145331 DURING TAKEOFF OUT OF MCO ON FLIGHT 6451, NOTICED A BURNING ODOR FAINTLY COMING THROUGH THE COCKPIT. F/O AND FLIGHT ATTENDANT CONCURRED. F/A REPORTED A STRONG BURNING ODOR COMING FROM THE GALLEY, NO VISIBLE SMOKE OR FIRE. AIR TURNBACK INTO MCO AND LANDED WITHOUT INCIDENT. THE FIRE DEPARTMENT CHECKED THE AIRCRAFT AND DID NOT FIND INDICATION OF HOT SPOTS. MAINTENANCE THOROUGHLY CHECKED THE AIRCRAFT AND COULD NOT DETERMINE SOURCE OF REPORTED BURNING ODOR. THE ODOR COULD NOT BE CONFIRMED COMING FROM ANY COMPONENT OF THE AIRCRAFT. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040319000042004031900004NM 2004 3 19 HNAA0400011 120040212A3244 TIRE DHAV DHC8 DHC8102 2809003NM MLG WHEEL SEPARATED A HNAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07935HA 142 NR 2 MAIN TIRE APPEARED FLAT DURING TAXI OUT. AC ON TAXI WAY, MT GOING OUT TO A/C TO INSPECT A/C PRIOR TO TAXI BACK TO GATE. THE A/C BEHIND THIS A/C NOTICED SMOKE COMING FROM NR 2 BRAKE ASSY. F/A NOTICED TIRE CAME OFF RIM. 2H72 4T RTA13NM 20040319000082004031900008NM 2004 3 19 HNAA0400013 120040225A3231 DOOR DHAV DHC8 DHC8102 2809003NM MLG OUT OF RIG A HNAAO OTHER J WARNING INDICATION CRCRUISE 1 EA07937HA 148 UPON GEAR RETRACTION THE LEFT FORWARD GEAR DOOR DID NOT CLOSE. FOUND GEAR DOOR OUT OF RIGGING. RIGGGED DOOR, OPS CHECK, NO FURTHER DISCREPANCY. 2H72 4T RTA13NM 20040319000092004031900009WP 2004 3 19 GKZR200482310 120040303A1430 RIVET DOUG DC8 DC871F 302199DWP KEELBEAM SHEARED B GKZRK NONE O OTHER ININSP/MAINT 1 SW11823BX 46064 KEELBEAM AREA HAS SEVERAL RIVET HEADS SHEARED OFF BUTTLINE -0-. REMOVED FASTENERS AND DOUBLERS IAW DC-8 SRM 51-1-20. REMOVED CORROSION IAW DC-8 SRM 53-2-0 FOUND OUT OF LIMITS MORE THAN 20 PERCENT ORIGINAL MAT LOSS. FABRICATED DOUBLER REPAIR IAW DC-8 SRM 53-1-0 TREATED AND PRIMED. INSTALLED DOUBLERS IAW DC-8 SRM 51-1-20. (CLOSED) 2L74 4F RT4A25 20040319000332004031900033NM 2004 3 19 CALA0400223 120040309A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND RT I/B SEAT TRACK CORRODED AT STA 907-927. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040319000352004031900035NM 2004 3 19 C1HA200476001 120040229A2751 SWITCH BOEING727 727225 1384077NM TE FLAPS OUT OF ADJUST A C1HAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15676MG 22554 ADVANCED POWER LEVERS ABOVE 1.4 EPR AND TAKEOFF WARNING SOUNDED. OPS CHECK SYSTEM PER AD 88-22-09-01 STEP 9. ADJUSTED FLAP SWITCH. 2L73 4F A3WE 20040319000362004031900036NM 2004 3 19 C1HA200483002 120040227A335037067001 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 CEILING MOUNTED AREA LIGHT FOR EMERGENCY LIGHTS FWD ASSEMBLY INOP. 2L73 4F A3WE 20040319000382004031900038NM 2004 3 19 C1HA200483004 120040227A3350900835A BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 AFT PORTABLE EMERGENCY LIGHTS INOP. 2L73 4F A3WE 20040319000392004031900039NM 2004 3 19 C1HA200495001 120040227A3210 SUPPORT BRACKET BOEING727 727290 138408WNM NLG ACTUATOR BROKEN A C1HAO OTHER O OTHER APAPPROACH 1 GL15295AS 22147 NOSE GEAR FAILED TO EXTEND. COMPLIED WITH COM PROCEDURE, CRANKED ALL GEAR MANUALLY. 2L73 4F A3WE 20040319000412004031900041EU 2004 3 19 MALA040240 120040220A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 FS 363.0 LEFT UPPER FUSELAGE SKIN HAS DENTS. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MESABA EO S53009. A/C RELEASE DATE 3/8/04. 2L72 4T RTA52EU 20040319000432004031900043EU 2004 3 19 MALA040239 120040220A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 LEFT FUSELAGE NR 2 ICE SHIELD HAS DENTS. REMOVED ICE SHIELD, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A DOUBLER REPAIR, FABRICATED AND INSTALLED NEW ICE SHIELD IAW MESABA EO S53005. AC RELEASE DATE 3/8/04. 2L72 4T RTA52EU 20040319000452004031900045EU 2004 3 19 MALA040243 120040221A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 FS 295 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/8/04. 2L72 4T RTA52EU 20040319000472004031900047 2004 3 19 234TR0017 420040303A2297 CONNECTOR BOEING737 737228 13844AGNM CONTROL PANEL DIRTY A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05234TR 23004 MODE CONTROL PANEL SWITCHES AUTO PILOT ENGAGE INOP AND FLIGHT DIRECTOR INOPERATIVE. CLEANED AND RESEATED CONNECTOR. OPS CHECKS GOOD PER MM 22-15-0. 2L72 4F RTA16WE 20040319000482004031900048NM 2004 3 19 HNAA0400019 120040307A5330 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07934HA 139 MAJOR REPAIR DENTS AFT OF DITCHING HATCH .012 INCH DEEPEST DENT, WITH SKIN CUPPED .020 INCH. 2H72 4T RTA13NM 20040319000492004031900049NM 2004 3 19 HNAA0400020 120040227A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07934HA 139 CORROSION, RT SEAT RAIL FLOOR FLANGE FOR RT LOWER FLOOR PANEL IS CORRODED FROM X560 TO X600 WITH PREVIOUS BLENDING. 2H72 4T RTA13NM 20040319000502004031900050NM 2004 3 19 HNAA0400014 120040302A33506013211X BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT DISCHARGED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07914HA 53 FOUND LEFT EXIT EGRESS LIGHT (2), AFT CABIN OVERHEAD, PAX OVERHEAD EXIT SIGN IS INOP WHILE ATTEMPTING TO PERFORM SCHEDULED MX. W/C 33-50-03Q CLT MX FOUND SEVERAL EMERGENCY LIGHTS NOT WORKING, HAD TO CHANGE TWO BATTERIES. 2H72 4T RTA13NM 20040319000532004031900053NM 2004 3 19 HNAA0400022 120040309A5310 BEAM DHAV DHC8 DHC8102 2809003NM FUSELAGE CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07931HA 132 TRANSVERSE BEAM HAS A CRACK WHERE THE ALTERNATE RELEASE CABLE GOES THROUGH, ABOUT .4 INCHES LONG. REPAIRED PER EO 8-53-04-0148. 2H72 4T RTA13NM 20040319000552004031900055NM 2004 3 19 F3LA200400031 120040308A5315 FLOORBEAM BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CABIN FLOORBEAM AT STA 986 CORRODED. CORROSION ON FLOORBEAM TOP FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-60-31. REMOVED FLOORBEAM UPPER FLANGE, FABRICATED REPAIR T-CAP, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PER SRM 51-40-02 AND EA B3-53R-10331. 2L72 4F RTA16WE 20040319000562004031900056NM 2004 3 19 F3LA200400032 120040308A1430 SCREW BOEING737 7373S1 138447SNM RUDDER LOOSE A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED SCREWS F2 AND F4 WERE FOUND LOOSE PER RUDDER INSPECTION PERFORMED PER EO B3-55-00AD-0001-DY, PART 2, STEPS 2 AND 4. REPLACED BOLTS PER EO B3-55-00AD-004-DY. 2L72 4F RTA16WE 20040319000572004031900057NM 2004 3 19 P5CA0401053 120040309A3610 SEAL BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE N2 ENG DUCT BROKEN A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23921FT 21575 609184 LEFT WING L/E OVERHEAT LIGHT ON. REPLACED BROKEN SEALS ON L/E DUCT INBOARD OF NR 2 ENG AND BY THE NR 3 PDU OPS AND LEAK CHECK OK PER MM 36-11-01 AND 26-18-01. 2L74 4F4 F A20WE E3NE 20040319000592004031900059EA 2004 3 19 COMA0460184 120040305A274270608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A COMAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO01917CA20183 7017 FLIGHT 5492 STAB TRIM FAIL MESSAGE. REPLACED THE HSTCU. 2L72 4F RTA21EA 20040319000602004031900060EA 2004 3 19 COMA0460185 120040304A2410755469E IDG CNDAIRCL600 CL6002B19 1900309EA LEFT FAILED A COMAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO01466CA5622 7627 FLIGHT 5182 LEFT IDG TRIPPED OFF LINE. REPLACED THE LEFT IDG. 2L72 4F RTA21EA 20040319000612004031900061NE 2004 3 19 COMA0460186 220040304A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT VIBRATION A COMAA UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01976CA18635 7151 807332 FLIGHT 5883 RIGHT ENGINE N2 VIB WARNING, ENGINE ROLLBACK. REPLACED THE RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040319000632004031900063WP 2004 3 19 0400399851 120040214A5330 SKIN DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01760NC 47708 DURING L-CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 69.5 LBL 18. REPAIRED PER EA 98-197454. 2L72 4F RTA6WE 20040319000642004031900064WP 2004 3 19 ABXA040094 120040309A5610 WINDOW DOUG DC9 DC941 302207NWP COCKPIT OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23974AX 47623 CAPTAIN'S CLEARVIEW WINDOW INTERMITTENTLY JAMS AND CANNOT BE OPENED. ADJUSTED LOWER AFT HOOK ON CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-03. OPS CHECK GOOD. 2L72 4F A6WE 20040319000682004031900068NM 2004 3 19 P5CA0401055 120040308A71601960259501 INTAKE BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 2 NACELLE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 689184 NR 2 ENG INBOARD OUTSIDE FAN COWL REQ UPGRAGE, INTERNAL 84 X 20 INCH AREA DELAMINATED BEYOND LOCAL REPAIR. REPLACED COWLING. 2L74 4F4 F A20WE E3NE 20040319000702004031900070EA 2004 3 19 04066699 120040306A78301267588 PDU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27699BR 7801 DURING AIRCRAFT OPERATION THE CREW REPORTED THE RIGHT HAND THRUST REVERSER WOULD NOT DEPLOY. THE POWER DRIVE UNIT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY FUNTIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040319000712004031900071NM 2004 3 19 04048402 120040219A5311 FRAME DORNERDO32 DO328300 NM FUSLEAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27402FJ 3147 DURING INSPECTION FRAME 41 WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2H72 4T RTA55NM 20040319000722004031900072EA 2004 3 19 04041656 120040210A5310 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27656BR 7485 DURING INSPECTION A CRACK WAS FOUND AT STATION 621 WATER LINE 73 UNDER FLOOR PANEL 282. THE CRACK WAS REPAIRED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040319000732004031900073 2004 3 19 251TR0007 420040305A22104038890948 DISPLAY BOEING737 737228 13844AGNM CONTROL PANEL MALFUNCTIONED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 THE NUMBER 6 IS MISSING IN MODE CONTROL PANEL. PLACED ON MCO. 3/9/2004: REPLACED MODE CONTROL PANEL AND OPS CHECKED PER MM 22-11-341. 2L72 4F RTA16WE 20040319000762004031900076EA 2004 3 19 04066630A 120040306A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING HEAVY INSPECTION LEVEL 2 A CRACK WAS FOUND ON THE FLOORBEAM STRUCTURE AT FUSELAGE STATION 280 LBL 12. THE ANGLE WAS REPLACED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4F RTA21EA 20040319000772004031900077SO 2004 3 19 C2XA04BT030 120040306A335066368 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712519 145366 CREW REPORTED, FLOOR EMERGENCY LIGHT SECTION WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED FLOOR EMERGENCY LIGHT SECTION IAW EMB135 AMM 33-50-08. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040319000782004031900078EA 2004 3 19 04067667 120040307A2611PU9042R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA VTZAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 EA27667BR 7535 DURING AIRCRAFT OPERATION CREW RECEIVED A LAVATORY SMOKE INDICATION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE SMOKE DETECTOR WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040319000792004031900079NM 2004 3 19 CALA0400225 120040309A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 328, WL 208. A NEW FLOORBEAM SECTION WAS INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20040319000802004031900080NM 2004 3 19 CALA0400226 120040309A5320654681232 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 982, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040319000822004031900082SO 2004 3 19 C2XA04BT031 120040307A335020131A BATTERY EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715985 145248 CREW REPORTED, EMERGENCY LIGHTS, FORWARD STRIP, GALLEY AND MAIN EXIT DOOR EXIT INDICATORS INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP SEAT 1A IAW EMB 145 AMM 33-50-12. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040319000832004031900083EA 2004 3 19 04065630 120040305A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING HEAVY INSPECTION THE RIGHT SIDE FLOOR SUPPORT AT STA 621 WAS FOUND CRACKED. THE SUPPORT WAS REPLACED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040319000842004031900084EA 2004 3 19 04068630 120040306A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING HEAVY INSPECTION FLOOR SUPPORT LOWER FRAME AT STATION 280 RBL 11 AND RBL 14 WAS FOUND CRACKED. THE FRAME WAS REPAIRED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4F RTA21EA 20040319000872004031900087SO 2004 3 19 C2XA04IA025 120040306A3350 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714960 145100 DURING SCHEDULED MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EMERGENCY LIGHT ASSEMBLY CANNON PLUG LOOSE. THE CONNECTOR WAS RESET, THE LIGHT OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4F RTT00011AT 20040319000882004031900088SO 2004 3 19 C2XA04IA027 120040307A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715985 145248 THE CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FORWARD EMERGENCY LIGHT POWER SUPPLY TO BE INOPERATIVE. THE AFFECTED POWER SUPPLY WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040319000902004031900090SO 2004 3 19 C2XA04SH147 120040310A531514523186001 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319000912004031900091NM 2004 3 19 04070428 120040310A5250 DOOR DORNERDO32 DO328300 NM COCKPIT BROKEN A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27428FJ 3193 COCKPIT EMERGENCY DOOR BROKEN. 2H72 4T RTA55NM 20040319000952004031900095CE 2004 3 19 DXTA200400257 120040306A3230 CAP CESSNA560 560XL 2076702CE MLG BEARING LOOSE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07650QS 5605150 AFTER TAKEOFF RED GEAR UNLOCK LIGHT WILL NOT GO OUT WHEN GEAR HANDLE IS SELECTED UP. CYCLED GEAR 2 TIMES WITH NO CHANGE, ACCOMPLISHED AIR TURNBACK AND LANDED WITHOUT INCIDENTS. ACCOMPLISHED GEAR SWING AND FOUND NOSE GEAR NOT LOCKING, MEASURED STRUT EXTENSION AND FOUND TO BE OVER EXTENDED. REMOVED PISTON ASSEMBLY FROM TRUNNION AND FOUND UPPER BEARING CAP NOT FULLY SEATED ON PISTON. RETORQUED CAP AND ASSEMBLED STRUT AND SERVICED. SWUNG GEAR & CHECKED GOOD, ALL WORK DONE IAW CESSNA 560XL COMPONENT MM CHAPTER 32-20-01, OPS AND LEAK CHECK GOOD. 2L72 4F RTA22CE 20040319000982004031900098NM 2004 3 19 04FDEA00625 120040310A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25281FE 22348 DENT IN EXTERNAL FUSELAGE SKIN AT BS 365.5 AT STRINGER 18L. REPAIRED SKIN AT BS 365.5 AT STR 18L PER SRM 53-30-3 FIG 3 & FED EX EA 7-5330-70635. 2L73 4F RTA3WE 20040319001002004031900100 2004 3 19 371PA0037 420040310A22104051600913 COMPUTER BOEING737 737306 13844BGNM FLT CONTROL MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05371PA 23543 MACH TRIM INOP. UNABLE TO DUPLICATE. PERFORMED ALL MACH TRIM TESTS PER MM 22-11-01. PREVIOUS FAULTS FLAGGED NR 1 FCC. REPLACED NR 1 FCC PER MM 22-11-33 FOR TROUBLESHOOTING. OPS CHECKS GOOD. 2L72 4F RTA16NE 20040319001012004031900101SO 2004 3 19 C2XA04BT032 120040308A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT UNSECURE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722909 145459 CREW REPORTED, EMERGENCY LIGHT OVER ROW 12 FACING LAVATORY IS INOPERATIVE. MAINTENANCE RESECURED WIRING IAW EMB145 AMM 33-50-15. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040319001022004031900102NM 2004 3 19 CALA0400229 120040310A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 887-927. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040319001042004031900104NM 2004 3 19 CALA0400231 120040310A532065C807351 ANGLE BOEING737 7373T0 1384582NM R-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND R-2 DOOR THRESHOLD SUPPORT ZEE ANGLE CORRODED. THE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20040319001052004031900105NM 2004 3 19 CALA0400232 120040311A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-338. REPAIRED IAW SRM 53-00-52, FIGURE 202. 2L72 4F RTA16WE 20040319001072004031900107NM 2004 3 19 CALA0400234 120040310A5230 SKIN BOEING737 7373T0 1384582NM AFT CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769333 23571 INSPECTION FOUND A DENT IN AFT CARGO DOOR OUTER SKIN. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2L72 4F RTA16WE 20040319001082004031900108EA 2004 3 19 COMA0460188 120040301A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01914CA 7012 FUEL PANEL 550AB ACCESS HAS INDICATION OF POSSIBLE CRACK ON INBOARD FACE AT APPROXIMATELY 9 O`CLOCK POSITION. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-030. 2L72 4F RTA21EA 20040319001092004031900109EA 2004 3 19 COMA0460189 120040305A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01914CA 7012 CRACK FOUND AT LEFT AND LOWER WING PLANK AT WS 148.019. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-130, CRJ SRM 51-24-11, CRJ SRM 51-24-38, REO 601R-53-21-130 AND CRJ SRM 51-23-00. 2L72 4F RTA21EA 20040319001102004031900110EA 2004 3 19 COMA0460190 120040305A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01914CA 7012 CRACK FOUND AT LEFT HAND LOWER WING PLANK AT WS 148.019. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-130, CRJ SRM 51-24-11, CRJ SRM 51-24-38, REO 601R-53-21-130 AND CRJ SRM 51-23-00. 2L72 4F RTA21EA 20040319001132004031900113SO 2004 3 19 C2XA04SH150 120040311A531214526850401 FIREWALL EMB 145 EMB145 3260210SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319001152004031900115SO 2004 3 19 C2XA04SH152 120040312A716014575001405 INTAKE EMB 135 EMB135LR 3260305SO NR 2 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK, THE NR 2 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319001162004031900116NM 2004 3 19 237TR0003 120040309A33501000679 LIGHT BOEING737 737228 13844AGNM CABIN INOPERATIVE A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05237TR 23007 L-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED L-1 OVERHEAD DOOR LIGHT ASSEMBLY PER MM 33-50. OPS CHECK GOOD. 2L72 4F RTA16WE 20040319001182004031900118NM 2004 3 19 SWAA040737 120040309A53106557463 BRACKET BOEING737 7373Q8 1384670NM GIRT BAR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING PREFLIGHT CK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT MOUNTING FLOOR BRACKET MISSING. INSTALLED BRACKET PER MM. 2L72 4F RTA16WE 20040319001192004031900119NM 2004 3 19 SWAA040738 120040309A3246 BEARING BOEING737 7373H4 1384600NM RT MLG WHEEL BROKEN A SWAAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW29314SW 23336 DURING TAXI, FELT MLG WHEEL VIBRATION AND NR 4 MLG TIRE/WHEEL ASSY WAS CANTED AT AN ANGLE. FOUND NR 4 MLG WHEEL RIM ASSY AND INNER BEARING RACE BROKEN APART. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRE/WHEEL ASSY'S AND NR 4 BRAKE ASSY PER MM. 2L72 4F RTA16WE 20040319001202004031900120NM 2004 3 19 SWAA040739 120040309A55206959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW29388SW 26591 ACFT VIBRATION FELT ABOVE 250 KNOTS. REMOVED AND REPLACED RT ELEVATOR TAB INBD HINGE ATTACH BUSHING AND BOLT PER MM. 2L72 4F RTA16WE 20040319001212004031900121NM 2004 3 19 SWAA040740 120040309A5311BAC1517 FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SPECIAL VISIT, FOUND CRACKS INDICATION AT BS 727 FRAME FASTENERS HOLES, STR 18A LT AND STR 18A RT. REPAIRED FRAME PER SRM. 2L72 4F A16WE 20040319001222004031900122NM 2004 3 19 SWAA040741 120040309A5523 SKIN BOEING737 7373H4 1384600NM ELEVATOR TAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C1 CHECK, FOUND BOTH LT AND RT ELEVATOR TABS SKIN CRACKED AT NR 2 HINGE CUTOUTS. REMOVED AND REPLACED BOTH ELEVATOR TABS PER MM. 2L72 4F RTA16WE 20040319001232004031900123NM 2004 3 19 SWAA040742 120040309A53206547978 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND WEB CORRODED AT BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040319001242004031900124NM 2004 3 19 SWAA040743 120040309A575465C26656 SKIN BOEING737 7373H4 1384600NM WING SLATS DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND NR 2 AND NR 5 L/E SLAT TRAILING EDGES DELAMINATED. REPAIRED SLATS PER SRM. 2L72 4F RTA16WE 20040319001262004031900126NM 2004 3 19 SWAA040745 120040309A53106546500 SHEAR TIE BOEING737 7373A4 1384585NM KEELBEAM CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIES CORRODED AT BS 500D, LT AND RT KEEL BEAM, AND BS 520, LT KEELBEAM. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040319001272004031900127NM 2004 3 19 SWAA040746 120040309A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CRACKED AT BS 360, STR 14R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040319001282004031900128 2004 3 19 SWAA040700 420040304A34142083111 INDICATOR BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW29313SW 23335 F/O'S AIR SPEED IND C/B TRIPPED AND ACRID ODOR FOLLOWED. REMOVED AND REPLACED F/O'S MACH AIR SPEED IND PER MM. 2L72 4F RTA16WE 20040319001292004031900129NM 2004 3 19 SWAA040701 120040305A276165C268643 ACTUATOR BOEING737 7373H4 1384600NM LT WING SPOILER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED RON, FOUND NR 1 GROUND SPOILER HYD ACTUATOR CASING CRACKED. REMOVED AND REPLACED ACTUATOR PER MM. 2L72 4F RTA16WE 20040319001342004031900134NM 2004 3 19 SWAA040706 120040305A53126546568 BULKHEAD BOEING737 7377H4 1384404NM FUSELAGE CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED C4 CHECK, FOUND BS 1016 BULKHEAD PRESS BULKHEAD OIL CANNED AT STR 26. REPAIRED BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20040319001352004031900135NM 2004 3 19 SWAA040707 120040304A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 22L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040319001382004031900138NM 2004 3 19 SWAA040710 120040305A53306545877 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040319001392004031900139NM 2004 3 19 SWAA040711 120040305A53106545409 WEB BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND UPPER MLG W/W BEADED WEB CRACKED AT BS 665, OUTBD OF NR 2 SEAT TRACK. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20040319001402004031900140NM 2004 3 19 SWAA040712 120040305A53306550570 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040319001412004031900141NM 2004 3 19 SWAA040713 120040304A3350071700100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29706SW 27840 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PACK AT M1673 BALLAST PER MM. 2L72 4F RTA16WE 20040319001422004031900142NM 2004 3 19 SWAA040714 120040305A5320BCA1505 FLOOR SUPPORT BOEING737 7373H4 1384600NM AFT CARGO COMP CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 772, LBL 17 AND RBL 17. REPAIRED SUPPORTS PER SWA EA. 2L72 4F RTA16WE 20040319001442004031900144 2004 3 19 SWAA040716 420040305A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040319001492004031900149 2004 3 19 SWAA040691 420040304A2565D31354 SLIDE BOEING737 7373A4 1384585NM L1 DOOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040319001502004031900150NM 2004 3 19 SWAA040692 120040304A53126545668 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND CRACK INDICATION AT BS 1016 BULKHEAD, STR 15L. REPAIRED BULKHEAD PER ER. 2L72 4F RTA16WE 20040319001512004031900151NM 2004 3 19 SWAA040693 120040304A53106547978 CREASE BEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND RT CREASE BEAM CRACKED AT BS 520. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040319001552004031900155NM 2004 3 19 SWAA040699 120040304A53126545422 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND BS 727 BULKHEAD WEB CRACKED AT BL 0, WL 185. REPAIRED WEB PER SWA EA. 2L72 4F A16WE 20040319001592004031900159NM 2004 3 19 SWAA040679 120040303A53116546533 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, BETWEEN STR 26L AND STR 27L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040319001602004031900160NM 2004 3 19 SWAA040680 120040303A52406545871 FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT STOP FITTINGS. REMOVED AND REPLACED R1 DOOR PER MM. 2L72 4F RTA16WE 20040317001452004031700145 2004 3 17 SWIA200412956 420040301A2210 SPRING EMB 120 EMB120ER 3260203SO YOKE DAMAGED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07289YV 120289 CAPTAIN AP/TRIM INOP. REPLACED CAPTAIN'S YOKE RETURN SPRING WITH A SERVICEABLE SPRING. CAPT'S AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040317001462004031700146SO 2004 3 17 SWIA200412957 120040121A5311 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07190SW 120050 CRACK ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE IAW SRM 51-70-01. 2L72 4T4 TRTA31SO E20NE 20040317001472004031700147SO 2004 3 17 SWIA200412958 120040121A5411 FRAME EMB 120 EMB120ER 3260203SO NR 1 NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07190SW 120050 CHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SECTION OF CHANNEL FORWARD OF FRAME NR 1 ON RIGHT NACELLE IAW SRM 54-10-02. 2L72 4T RTA31SO 20040318000122004031800012CE 2004 3 18 8473735 120040128A2731S3280 GEAR BEECH 1900 1900D 1154162CE ELE TAB DIAL SLIPPED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01831CA3652 UE395 WHILE CHECKING ELEVATOR TRIM FOR FCD BE2703 DISCOVERED ELEVATOR TAB DIAL MECHANISM MOUNT ASSY HAD SLIPPED CAUSING THE TRIM INDEX MARK CALIBRATION TO CHANGE. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT THE SLIPPAGE WAS CAUSED BY A PRESSED ON GEAR IN THE ELEVATOR TAB DIAL MECHANISM MOUNT ASSY THAT HAD SLIPPED ON ITS SHAFT. 2L72 4T RTA24CE 20040318000162004031800016 2004 3 18 YENA200412 420040225A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ENTERTAIN SYS ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15579JB1146 2132 ELECTRICAL ODOR COMING FROM LIVE TV AROUND ROW 20. THE ITEM WAS PLACED ON MEL 25-22-03, CONTROL NUMBER L00361. UPON ARRIVAL AT JFK PERFORMED INSPECTION OF ALL LTV COMPONENTS FROM ROW 18ABC THRU 22ABC IAW JB INFO NOTICE 2003-T050TRA. FOUND NO EVIDENCE OF ELECTRICAL BURNING ODOR. REMOVED AND REPLACED SEB AT 20ABC AS PRECAUTION IAW LTV MM 23-39-00. MEL AND PLACARD REMOVED, MCC NOTIFIED, MX-4 UPDATED. 2L72 4F RTA28NM 20040318000302004031800030NM 2004 3 18 CALA0400211 120040303A5320149A761115 WEB BOEING737 737724 13844BYNM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 INSPECTION FOUND A .5 INCH CRACK IN LT WHEEL WELL AFT RING ASSEMBLY OUTER WEB. THE OUTER WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040318000312004031800031NM 2004 3 18 CALA0400212 120040303A5311 FRAME BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719136 29285 INSPECTION FOUND MAIN FRAME DENTED AT BS 1600, STRINGERS 23L TO 26L. A REPAIR WAS INSTALLED IAW ECRA 5311-01188. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 60 DAYS. 2L72 4F RTA2NM 20040318000342004031800034WP 2004 3 18 0400359860 120040228A278239200485511 ACTUATOR DOUG DC9 DC951 3022051WP RT WING SLAT MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01769NC 47757 ON APPROACH WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE BUT NO MENTION OF SLAT DISAGREEMENT ANNUNCIATOR STATUS. AS THE AIRCRAFT SLOWED TO 190 KTS, THE SLAT EXTEND LIGHT ILLUMINATED. IT WAS NOTED THAT THERE HAD BEEN NO PROBLEMS WITH THE SLAT POSITIONING DURING TAKEOFF AT DTW. LANDING WAS UNEVENTFUL AT MBS. MAINTENANCE COULD NOT FIND ANY PROBLEMS VISUALLY OR OPERATIONALLY WITH EITHER WING. THE SLAT ACTUATOR AND T-DUCT FOR THE RIGHT WING WERE REPLACED AS A PRECAUTION. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20040318000352004031800035NM 2004 3 18 F3LA200400030 120040303A5320 STRIP BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03316FL 1507 25264 DURING C-4 CHECK, INSPECTION REPORTED Z-STRIP AFT OF L-2 DOOR AT STA 1006, LBL 45, CORRODED. REMOVED Z-STRIP PER SRM 51-40-2. FABRICATED, TREATED, PRIMED AND PAINTED PER SRM 51-40-02, 51-10-02, 51-40-06, 51-20-01 AND SOPM 20-41-02. 2L72 4F RTA16WE 20040318000382004031800038SO 2004 3 18 CHQA000462 120040228A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281 145391 AFT GALLEY EMERGENCY EXIT SIGN INOP. INSTALLED SERVICEABLE SIGN IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040318000502004031800050WP 2004 3 18 04FDEA00560 120040303A5311AJC702119 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 UPPER AFT FUSELAGE FRAME CRACKED CANT STA 2046. REMOVED AND REPLACED FRAME IAW SRM 51-35-02 AND SRM 51-33-01 AT MAE ON N/R N00321 W/O 25240. 2L73 4F A22WE 20040318000542004031800054WP 2004 3 18 04FDEA00566 120040304A5744ARC05034 BRACKET DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25360FE 46636 COMPLY WITH EA 8-5740-73888 WINGS - RIGHT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF ACTUATOR LUG. COMPLIED WITH EA 8-5740-73888 WINGS - RIGHT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF ACTUATOR LUG AT MAE. 2L73 4F A22WE 20040318000632004031800063WP 2004 3 18 04FDEA00575 120040304A5730ARB0872507 ACCESS PANEL DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25302FE 46801 CORROSION ON FUEL TANK ACCESS 534CB, AT MATING SURFACE. RECEIVED NEW PANEL P/N ARB0872-507, TO BE INSTALLED ON WORK CARD 575I5503-01. 2L73 4F RTA22WE 20040318000672004031800067NM 2004 3 18 PCAA0403175 120040304A3240214663 BRAKE ASSY DHAV DHC8 DHC8102 2809003NM MLG LEAKING A PCAAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 EA13818EX8287 271 235 FLIGHT 4014 REPORTED AIRCRAFT VIBRATING WHEN USING RIGHT HAND BRAKE. MAINTENANCE FOUND THE INBOARD RIGHT HAND BRAKE ASSEMBLY LEAKING. THE BRAKE ASSEMBLY WAS REPLACED AND THE SYSTEM OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040318000702004031800070NM 2004 3 18 SWAA040600 120040225A53306545776 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STRINGER 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040318000832004031800083NM 2004 3 18 SWAA040618 120040226A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER 27L, BS 380 TO BS 391 AND BS 400B + 15 TO BS 495. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040318000862004031800086NM 2004 3 18 SWAA040621 120040226A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND DOUBLER CORRODED AT BS 442, BETWEEN STRINGERS 27R AND 28R. REPAIRED DOUBLER PER ER. 2L72 4F RTA16WE 20040318000872004031800087NM 2004 3 18 SWAA040622 120040226A5320BAC1517 CHANNEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND FLOOR ZEE CHANNEL CORRODED AT BS 270, FROM LBL 10 TO RBL 10, WL 208. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040318001122004031800112 2004 3 18 SWAA040649 420040229A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040318001232004031800123NM 2004 3 18 SWAA040567 120040223A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STRINGER 16L. REPAIRED FUSELAGE SKIN PER SRM. 2L72 4F RTA16WE 20040318001362004031800136NM 2004 3 18 SWAA040580 120040225A5753 SKIN BOEING737 7373K2 13844BANM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT T/E. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20040318001462004031800146 2004 3 18 YENA200413 420040228A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN SHORTED A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15571JB1270 2125 ELECTRICAL BURNING ODOR OBSERVED IN LAST 5 ROWS OF CABIN, LIVE TV TURNED OFF. PERFORMED INFORMATION NOTICE 2003-T050TRA LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR. FOUND SEB AT 24E EVIDENCE OF LIQUID SPILL. REMOVED AND REPLACED SEB AT 24E IAW LTV MM 23-39-00. SYSTEM OPERATION OK. 2L72 4F RTA28NM 20040318001662004031800166NM 2004 3 18 04FDEA00576 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. RT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75281 TITLE WINGS - RT O/B FLAP I/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001712004031800171NM 2004 3 18 04FDEA00581 120040304A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. COMPLIED WITH FEDEX EA 1-5750-75282 - WINGS - RT OUTBD FLAP - OUTBD HINGE BRACKET PIVOT, ACTUATOR AND MOUNTING BORE - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040318001792004031800179SO 2004 3 18 C2XA04SH140 120040304A531014530375001 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2726549 145571 SHV - DURING C-CHECK, THE L-BRACKET AFT OF THE CENTER BUTTSTRAP AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040318001832004031800183WP 2004 3 18 0400369911 120040305A5270 STRIKER DOUG DC9 DC931 3022065WP CARGO DOOR WARN OUT OF ADJUST A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01961N 47405 THE AFT CARGO DOOR OPEN WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 130 KTS AND THE AIRCRAFT EXITED THE RUNWAY WITHOUT INCIDENT. THE WARNING INDICATION EXTINGUISHED AS THE AIRCRAFT TURNED ONTO THE TAXIWAY. MAINTENANCE INSPECTED THE SECURITY OF THE DOOR AND PLACED THE SYSTEM ON MEL. LATER, THE AFT CARGO DOOR STRIKER PAD WAS READJUSTED AND THE MEL WAS REMOVED. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040318001872004031800187NM 2004 3 18 04FDEA00592 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001922004031800192NM 2004 3 18 04FDEA00598 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET I/B ACTUATOR HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288. WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001932004031800193NM 2004 3 18 04FDEA00599 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET O/B ACTUATOR HOLE CORROSION R & R AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318002032004031800203NM 2004 3 18 04FDEA00609 120040308A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 MAIN DECK SEAT TRACK AT STA 1239 RBL 27.5 WITH CROWN AREA EDGE CHIPPED. MAIN DECK STA 1239/ RBL 47.5 DAMAGED SEAT TRACK CARRIED OUT SECTIONAL REPAIR AS PER SRM 53-70-00 VOL 1. 2L73 4F RTA22WE 20040318002182004031800218NM 2004 3 18 UPS04M41998 120040112A5347AFA7789542 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN AT STA 1841 RBL 107 MOST OUTBOARD SEAT TRACK FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT STA 1841 RBL 107 MATERIAL REMOVED 0.040 INCH ORIG THK 0.112 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL 1. NEW SEAT TRACK & SPLICE INSTALLED PER SRM 53-70-00 FIG 1 & 7 VOL 1 REV 34. 2L73 4F RTA22WE 20040319000192004031900019EU 2004 3 19 MALA040234 120040305A3260 SWITCH BAC 146 AVRO146RJ85A1500097EU LT MLG MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15523XJ E2348 LEFT MLG RED INDICATION AND GEAR HANDLE LIGHT REMAINED ON AFTER GEAR RETRACTION. REMOVED AND REPLACED UNDERCARRIAGE SWITCH IAW AMM. PERFORMED SEVERAL GEAR SWINGS, ALL CHECKS WERE GOOD. 2H74 4F RTA49EU 20040319000242004031900024NM 2004 3 19 PCAA0403179 120040306A275144281508010 GAUGE DHAV DHC8 DHC8102 2809003NM TE FLAPS FAULTY A PCAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA13825EX10732254 388 FLIGHT 3711 REPORTED A HORN SOUNDING DURING TAKEOFF ROLL, POWER WAS AT 82 PERCENT AND SPEED APPROXIMATELY 60 KNOTS. MAINTENANCE FOUND THE FLAP GAUGE TO BE AT FAULT. GAUGE WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040319000312004031900031NM 2004 3 19 CALA0400221 120040308A534765C2084468 GALLEY TRACK BOEING737 7373T0 1384582NM STA 270-294 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND GALLEY TRACK CORRODED AT STA 270-294, RBL 14. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, PAGE 202, STEP 11 AND 12 AND SRM 51-10-02. 2L72 4F RTA16WE 20040319000442004031900044EU 2004 3 19 MALA040242 120040220A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 FS 295 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/8/04. 2L72 4T RTA52EU 20040319000542004031900054NM 2004 3 19 P5CA0401052 120040308A523060B003043 ACTUATOR BOEING747 74747UF 1384949NM DOOR LATCH MALFUNCTIONED A P5CAK NONE O OTHER TXTAXI/GRND HDL 1 WP23496MC 29257 MAIN DECK SIDE DOOR WILL NOT CLOSE IN ELECTRICAL OR MANUAL MODE. REMOVED AND REPLACED LATCH ACTUATOR PER MM 52-32-09. 2L74 4F RT1384945 20040319000742004031900074EA 2004 3 19 04066630 120040306A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING HEAVY INSPECTION LEVEL 2 CORROSION WAS IDENTIFIED AROUND THE FLOOR SUPPORT ANGLE HOLES AT FUSELAGE STATION 280 LBL AND RBL 3. THE ANGLE WAS REPAIRED AND AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4F RTA21EA 20040319000752004031900075EA 2004 3 19 04067630 120040307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING HEAVY INSPECTION LEVEL 2 CORROSION WAS IDENTIFIED AT FUSELAGE STATION 280 BETWEEN LBL 7 AND RBL 7 ON THE FORWARD FLOORBEAM ANGLE. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED. AIRCRAFT WILL BE RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4F RTA21EA 20040319000812004031900081NM 2004 3 19 CALA0400227 120040309A53156545815 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND MAIN CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 344, LBL 10. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 206. 2L72 4F RTA16WE 20040319000922004031900092CE 2004 3 19 DXTA200400256 120040308A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG INTERMITTENT E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07314QS 5600441 ON LANDING BRAKES FELT WEAK, DURING TAXI BRAKES FUNCTIONED INTERMITTENTLY UNTIL BRAKES FAILED COMPLETELY, USED EMERGENCY BRAKES TO STOP AIRCRAFT. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040319000992004031900099EU 2004 3 19 04FDEA00627 120040311A5511 SPAR AIRBUS310 A310 EU ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25450FE 162 RT HORIZONTAL STAB I/B END AT RIB 3 TO RIB 4 UPPER T/E EDGE OF SPAR FOR LENGTH OF 16 INCHES HAS SEVERE CORROSION WITH EXFOLIATION. RIGHT HORIZ STAB UPPER REAR SPAR CHORD FOR RIB 3 TO RIB 4 REMOVED CORROSION BY CUTTING OUT TEE CHORD AND INSTALLING NEW TEE CHORD SECTION AND SPLICING BY INSTALLING INTERNAL AND EXTERNAL SPLICE REPAIR ANGLES IAW A310 SRM 55-11-21 FIG 219. O/B OF RIB 5 TO RIB 6 REMOVED CORROSION, TREATED, LOCATED, DRILLED AND INSTALLED REPAIR STRAP IAW A310 SRM 55-11-21 FIG 211 AND 224. 2L72 4F RTA35EU 20040319001122004031900112SO 2004 3 19 C2XA04SH149 120040311A542014576631622 STIFFENER EMB 145 EMB145 3260210SO RT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE RIGHT HAND ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319001252004031900125NM 2004 3 19 SWAA040744 120040309A53116546540 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65, WL 200. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040319001312004031900131NM 2004 3 19 SWAA040703 120040305A27616549580 ACTUATOR BOEING737 7372H4 138448CNM RT WING SPOILER LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29095SW 23054 AIR TURNBACK, HYD A-SYS FAILURE. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR. 2L72 4F A16WE 20040319001362004031900136 2004 3 19 SWAA040708 420040304A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040319001472004031900147NM 2004 3 19 SWAA040688 120040304A53306545750 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED A1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 913, STR 10L, BS 783, STR 20L, AND BS 740, STR 19R. REPAIRED SKIN PER SRM AND SWA EA. 2L72 4F RTA16WE 20040319001532004031900153NM 2004 3 19 SWAA040697 120040304A335007312 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29420WN 29825 DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 4. REMOVED AND REPLACED TRACK COVER PER MM. 2L72 4F RTA16WE 20040319001582004031900158 2004 3 19 SWAA040678 420040303A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 R1 DOOR EVACUATION SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040319001612004031900161NM 2004 3 19 SWAA040681 120040303A3350101114 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20040319001622004031900162NM 2004 3 19 SWAA040682 120040303A52406969854 FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT STOP FITTING. REPAIRED FRAME PER BAC DRAWING. 2L72 4F RTA16WE 20040319001632004031900163NM 2004 3 19 SWAA040683 120040303A52106547952 SKIN BOEING737 7377H4 1384404NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SKIN CRACKED AT AFT UPPER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040319001642004031900164NE 2004 3 19 SWAA040684 220040302A72509995M22 TURBINE BLADES BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 ENG DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 858616 DURING SCHEDULED C1 CHECK, FOUND NR 1 ENG HPT BLADE DAMAGED AT L/E. REMOVED AND REPLACED NR 1 ENG PER MT. 2L72 4F4 FRTA16WE E2GL 20040319001652004031900165NE 2004 3 19 SWAA040685 220040303A7320JM44LC43 CLAMP BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 2 ENG OUT OF POSITION A SWAAK NONE O OTHER CRCRUISE 1 SW29353SW 24889 AT 35000FT, NR 2 ENG THRUST LEVER WAS DIFFICULT TO RETARD FROM CLIMB TRUST SETTING. REPOSITIONED 3 EA CLAMPS FROM PYLON TO THROTLE BOX. OPS CHECK GOOD PER MM. 2L72 4F4 FRTA16WE E2GL 20040319001662004031900166 2004 3 19 SWAA040717 420040307A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20040319001702004031900170NM 2004 3 19 SWAA040721 120040307A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986.5, LBL 5 TO RBL 5. REPAIRED BEAM PER T1-453-037. 2L72 4F RTA16WE 20040319001722004031900172NM 2004 3 19 SWAA040724 120040307A32116540107 FITTING BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND RT MLG FWD STABILIZER BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2L72 4F RTA16WE 20040319001732004031900173NM 2004 3 19 SWAA040725 120040307A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 208. REPAIRED FRAME PER T1-153-018. 2L72 4F RTA16WE 20040319001772004031900177NM 2004 3 19 SWAA040729 120040307A575465C26686 SKIN BOEING737 7375H4 138449DNM NR 3 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED 1/4D CHECK, FOUND NR 3 L/E SLAT LOWER SKIN SURFACE CRACKED 30 INCHES FROM INBD END. REPAIRED SLAT SKIN PER SRM. 2L72 4F RTA16WE 20040319001802004031900180 2004 3 19 SWAA040732 420040308A2565D31354 SLIDE BOEING737 7373A4 1384585NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040319001822004031900182 2004 3 19 SWAA040734 420040307A256565C19901 CABLE BOEING737 7373T5 1384608NM L2 & R2 DOORS MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C4 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE CABLES MISROUTED. REROUTED STRAP CABLES PER MM. 2L72 4F RTA16WE 20040319001832004031900183NM 2004 3 19 SWAA040735 120040307A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C4 CHECK, FOUND 2 FUSELAGE SKIN CRACKS AT BS 805, STR 22L AND BS 775, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040319001842004031900184NM 2004 3 19 SWAA040736 120040307A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29734SA 27866 EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS FWD SECTION PER MM. 2L72 4F RTA16WE 20040319001852004031900185NE 2004 3 19 VNAA0403009 220040309A7320 FITTING DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE HMU FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07441JS 3059 DURING FLIGHT, THE LEFT HAND ENGINE TORQUE WAS FLUCUATING AND FLIGHT 2434 RETURNED TO DAY. MAINTENEANCE INSPECTED AND FOUND A P-3 LINE FITTING LOOSE THEN TIGHTENED THE FITTING IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001872004031900187NM 2004 3 19 VNAA0403007 120040303A2430230GC02Y04 PANEL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE 1VE FAILED A VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07434JS3523 3051 THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED THE 1VE PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001902004031900190NM 2004 3 19 VNAA0403004 120040302A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAV FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07442JS 3060 THE CREW REPORTED RECEIVING A LAV SMOKE DETECT FAIL. MAINTENANCE INSPECTED AND DEFERRED THE APU IN ACCORDANCE WITH MEL 49-1 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001922004031900192NM 2004 3 19 VNAA0403003 120040103A3260 BULB DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG INDICATOR FAILED A VNAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07439JS 3057 ON APPROACH, THE CREW REPORTED A BURNED OUT LEFT HAND LANDING GEAR INDICATION. FLIGHT 2439 LANDED WITH NO FURTHER INCIDENTS. OUTSTATION MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND LANDING GEAR INDICATION BULB IN ACCORDANCE WITH 31-14-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001952004031900195NM 2004 3 19 VNAA0402011 120040228A2611SD942201 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAV FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07442JS173261806 3060 THE CREW REPORTED RECEIVING AN INTERMITTENT LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001962004031900196NM 2004 3 19 VNAA0402012 120040229A2611SD942201 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAV FAILED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07442JS 3060 THE CREW REPORTED RECEIVING A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND FOUND A LOOSE BACKSHELL TO THE LAV SMOKE DETECTOR AND TIGHTENED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040319001982004031900198SO 2004 3 19 C2XA04TY045 120040312A532014524131011 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714558 145598 TYS DURING A SCHEDULED 1C INSPECTION THE FWD AND AFT PAX DOOR THRESHOLD SUPPORT BRACKETS WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE THRESHOLD SUPPORT BRACKETS IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040319001992004031900199SO 2004 3 19 C2XA04TY046 120040312A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714558 145598 TYS DURING A SCHEDULED 1C INSPECTION THE LT OMEGA BEAM WAS FOUND CORRODED AT FR 20. MAINT CUT OUT THE CORRODED AREA, FABBED A NEW FILLER, SHIM AND DOUBLER, INSTALLED. ALODINED, PRIMED AND PAINTED IAW SRM 51-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040319002002004031900200SO 2004 3 19 C2XA04TY047 120040312A531514522459003 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 TYS DURING A SCHEDULED 2C INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AT THE GALLEY AREA. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040319002012004031900201SO 2004 3 19 C2XA04TY048 120040312A532014521725401 SILL EMB 135 EMB135ER 3260203SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 TYS DURING A SCHEDULED 2C INSPECTION THE SERVICE DOOR FWD SILL WAS FOUND CORRODED. MAINT BLENDED AND MEASURED AREA, FAB AND INSTALL DOUBLER IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040319002022004031900202SO 2004 3 19 C2XA04TY049 120040312A5320 CHANNEL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716510 145251 TYS DURING A SCHEDULED 2C INSPECTION A GOUGE WAS FOUND AT FR 15, STR 16L. MAINT REPAIRED CENTER FUSELAGE 1 AT LT FLOOR CROSSBEAM. ALODINED, PRIMED AND PAINTED IAW IC 2004-145/0816 AND CPM 51-21-04;05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040319002032004031900203NM 2004 3 19 CALA0400235 120040311A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040322000012004032200001EU 2004 3 22 AWXA200400234 120040229A3510 OXYGEN MASK AIRBUS320 A320231 3930325EU COCKPIT LEAKING A AWXAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 WP28633AW 082 MCI - DIVERSION - FLT 0285 - EN ROUTE FROM ORD TO PHX CREW OXYGEN LEAKED DOWN TO 60 PSI, DIVERTED TO MCI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE OBSERVERS MASK STOWED INCORRECTLY ALLOWING OXYGEN TO ESCAPE, RE-STOWED OBSERVERS MASK TO CORRECT POSITION, AND REPLACED CREW OXYGEN BOTTLE. 2L72 4F RTA28NM 20040322000022004032200002NM 2004 3 22 AWXA200400235 120040222A5751 SKIN BOEING737 73733A 1384673NM AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW HDH316 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE RT AILERON LEADING EDGE ACCESS PANEL LOWER LAND DELAMINATED 33.5 INCHES FROM THE INBOARD END. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-17, REPAIR 6, FIG 2, 6, 8 & 20. 2L72 4F RTA16WE 20040322000042004032200004NM 2004 3 22 AWXA200400237 120040221A5315655289416 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .25 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, LBL 45, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM LBL 25 TO LBL 45, WL 208; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SOPM 20-50-01 FIG 1 PG 1-8. 2L72 4F RTA16WE 20040322000062004032200006NM 2004 3 22 AWXA200400239 120040221A5315655289418 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .25 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, RBL 45, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM RBL 25 TO RBL 45, WL 208; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SOPM 20-50-01 FIG 1 PG 1-8. 2L72 4F RTA16WE 20040322000112004032200011NM 2004 3 22 AWXA200400243 120040306A2932501310000 PRESSURE SWITCH AIRBUSA319 A319132 3930340NM GREEN HYD SYS CRACKED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28827AW 1547 PHX - EMERGENCY LANDING - FLT 0154 - EN ROUTE FROM SFO TO PHX RECEIVED GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL INDICATION. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND NR 1 ENGINE (GREEN SYSTEM) HYDRAULIC PRESSURE SWITCH CRACKED AND LEAKING. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PRESSURE SWITCH IAW AMM 29-11-17, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040322000122004032200012NM 2004 3 22 AWXA200400244 120040303A575465C267937 SKIN BOEING737 7373G7 1384595NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 234.4. MAINTENANCE CUTOUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 234.4; FABRICATED A FILLER AND DOUBLER PER DWG 65C26603; INSTALLED REPAIR PARTS IAW 57-43-01 FIG 206, PG 216-219. 2L72 4F RTA16WE 20040322000142004032200014NM 2004 3 22 AWXA200400246 120040221A53106546551 SHEAR TIE BOEING737 73733A 1384673NM CRACKED CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, BL -0-. MAINTENANCE REMOVED DAMAGED SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, BL -0-; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 203, PG 207-209. 2L72 4F RTA16WE 20040322000162004032200016WP 2004 3 22 AALA20040325 120040308A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21228AA 49178 ORD EMERGENCY LIGHTS ABOVE ROW 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040322000182004032200018NM 2004 3 22 AWXA200400248 120040221A575465C266047 SKIN BOEING737 73733A 1384673NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 3 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 232.40. MAINTENANCE CUT OUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 232.40; FABRICATED A FILLER AND SPLICE PLATE PER DWG 65C26603; INSTALLED REPAIR PARTS IAW 57-43-01 FIG 206 PG 216-219. 2L72 4F RTA16WE 20040322000192004032200019NM 2004 3 22 AWXA200400249 120040223A52106555478502 GATE BOEING737 73733A 1384673NM L-2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND AT FASTENER HOLE ON L-2 DOOR LOWER GATE. MAINTENANCE REMOVED L-2 DOOR LOWER GATE ASSEMBLY FROM BS 960 TO BS 986.5, STR 16-17 LT; FABRICATED A NEW REPLACEMENT GATE ASSEMBLY; INSTALLED REPAIR PART IAW 53-13-61 FIG 401 PG 1-4. 2L72 4F RTA16WE 20040322000202004032200020NM 2004 3 22 AWXA200400250 120040221A57536546486 WEDGE BOEING737 73733A 1384673NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK THE RT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ON LOWER SURFACE APPROXIMATELY 36 INCHES FROM INBOARD END. MAINTENANCE CUT OUT DELAMINATED AREA OF MID FLAP TRAILING EDGE WEDGE AND FOUND NO CORE DAMAGE; FABRICATED FILLER & REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW 51-70-10 FIG 30 PG 88C-88E. 2L72 4F RTA16WE 20040322000212004032200021NM 2004 3 22 AWXA200400251 120040223A5753654643099 SKIN BOEING737 73733A 1384673NM LT WING TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK THE UPPER SURFACE OF LT WING INBOARD FORE FLAP WAS FOUND DISBONDED 34.75 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA OF LT WING INBOARD FORE FLAP; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW 51-70-10 FIG 30 PG 88C-88E. 2L72 4F RTA16WE 20040322000222004032200022NM 2004 3 22 AWXA200400252 120040223A53136545767 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER 16 LT AT BS 500C, AFT OF LEADING EDGE LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGED END OF STRINGER AT BS 500C; FABRICATED FILLER AND REPAIR CHANNEL; INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2L72 4F RTA16WE 20040322000232004032200023NM 2004 3 22 AWXA200400253 120040221A575465C267943 SKIN BOEING737 73733A 1384673NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 6 CRACKS WERE FOUND ON NR 1 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 445. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 1 SLAT LOWER SKIN WBL 445; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW 57-43-01 FIG 206 PG 216-219. 2L72 4F RTA16WE 20040322000252004032200025NM 2004 3 22 AWXA200400255 120040304A575465C2660399 SKIN BOEING737 7373B7 1384580NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND BETWEEN TWO RIVET HOLES ON LOWER EDGE OF NR 3 SLAT WS 321.5. MAINTENANCE CUT OUT DAMAGE ON LOWER EDGE OF NR 3 SLAT AT WS 321.5; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219. 2L72 4F RTA16WE 20040322000272004032200027NM 2004 3 22 AWXA200400257 120040228A531265175837 VERTICAL BEAM BOEING737 7373B7 1384580NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE ON VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195. MAINTENANCE REMOVED VERTICAL BEAM WEB AFT SIDE OF BS 178 BULKHEAD LBL 5.7, WL 195; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2L72 4F RTA16WE 20040322000292004032200029NM 2004 3 22 AWXA200400259 120040223A531065505683 CREASE BEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK CORROSION WAS FOUND ON L-2 DOOR ENTRY WAY CREASE BEAM UPPER OUTER CHORD BETWEEN BS 960 AND BS 983, LBL 55, WL 209. MAINTENANCE REMOVED CORRODED CREASE BEAM UPPER OUTER CHORD FROM BS 960 TO BS 983, LBL 55, WL 209; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 1 & 38. 2L72 4F RTA16WE 20040322000302004032200030NM 2004 3 22 AWXA200400260 120040310A3397BMS13311122 WIRE BOEING737 73733A 1384673NM SEAT ROW 15 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040322000312004032200031NM 2004 3 22 AWXA200400262 120040223A5311654580761 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 2 CRACKS WERE FOUND ON LOWER INBOARD RADIUS OF R-1 DOOR ENTRY WAY FORWARD STUB FRAME AT CREASE BEAM ATTACH POINT BS 294, RBL 59, WL 209. MAINTENANCE CUT OUT DAMAGE ON R-1 DOOR ENTRY WAY FORWARD STUB FRAME BS 294, RBL 59, WL 209; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED FILLER & REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5300-04062-SS1. 2L72 4F RTA16WE 20040322000372004032200037NM 2004 3 22 AWXA200400268 120040225A53206546812104 STRAP BOEING737 73733A 1384673NM LAVATORY FLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR STRAP BETWEEN BS 1020 AND BS 1025, RBL 27, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY FLOOR STRAP FROM BS 1020 TO BS 1025, RBL 27, WL 208; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 38. 2L72 4F RTA16WE 20040322000382004032200038NM 2004 3 22 AWXA200400269 120040225A53206546812104 STRAP BOEING737 73733A 1384673NM LAVATORY FLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR STRAP BETWEEN BS 1028, RBL 17, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY FLOOR STRAP FROM BS 1028, RBL 17, WL 208; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 PG 38. 2L72 4F RTA16WE 20040322000392004032200039NM 2004 3 22 AWXA200400270 120040303A53116546551 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 807, RBL 4. MAINTENANCE REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 807, RBL 4; FABRICATED A NEW REPLACEMENT SECTION OF SHEAR TIE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 210 SHEETS 1-4. 2L72 4F RTA16WE 20040322000402004032200040NM 2004 3 22 DHL2004755004 120040309A2612 FIRE LOOP BOEING727 727225 1384077NM NR 1 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01755DH 21857 NR 1 FIRE DETECTION GROUND CIRCUIT LIGHT ON. REPOSITIONED NR 1 ENGINE FIRE LOOP. OPS CHECKED NORMAL IAW 26-11-01. 2L73 4F A3WE 20040322000412004032200041NM 2004 3 22 DHL2004755005 120040310A3350 LIGHT BOEING727 727225 1384077NM EMERGENCY EXIT LOOSE A DHLAO OTHER O OTHER CRCRUISE 1 SO01755DH 21857 EMERGENCY EXIT LIGHTS FLASH ON AND OFF DURING TURBULENCE AND TAXI. FOUND LIGHT ASSEMBLY LOOSE. RESEATED SAME, PERFORMED OPS CHECK IAW M/M B-727 33-50-111. OPS CHECKED GOOD. 2L73 4F A3WE 20040322000422004032200042NM 2004 3 22 DHL2004741003 120040310A5320 INTERCOSTAL BOEING727 7272Q9 138448MNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 SURFACE CORROSION AT RT MLG STA 740 THRU 760 OUTBOARD OF FUEL SHROUD UPPER INTERCOSTAL. REMOVED SURFACE CORROSION, APPROXIMATELY .001 INCH, WITHIN LIMITS. TREATED AND PRIMED WITH ZINC CHROMATE IAW SRM 51-10-6. 2L73 4F RTA3WE 20040322000432004032200043NM 2004 3 22 DHL2004741004 120040310A5320 INTERCOSTAL BOEING727 7272Q9 138448MNM LT MLG WW CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 LT MLG WW SURFACE CORROSION AT STA 740 APPROXIMATELY INTERCOSTAL AREA OUTBOARD FUEL SHROUD. REMOVED SURFACE CORROSION APPROXIMATELY .001 INCH, WITHIN LIMITS. TREATED AND PRIMED WITH ZINC CHROMATE IAW SRM 51-10-6. 2L73 4F RTA3WE 20040322000442004032200044NM 2004 3 22 VNAA0403002 120040301A2120 UNKNOWN DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FUMES A VNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07462PS 3084 THE CREW REPORTED FUMES IN THE COCKPIT AND FLIGHT 2492 RETURNED TO PIT. THE CREW REPORTED THE FUMES DISPERSED AS THE FLIGHT WENT ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS AND THERE WERE NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040322000462004032200046NM 2004 3 22 CALA0400237 120040311A53116546539 BELTFRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A 3 INCH CRACK IN BELTFRAME AT STA 616 LEFT JUST BELOW FLOOR LINE. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20040322000512004032200051NM 2004 3 22 CALA0400242 120040312A531165C344121 BELTFRAME BOEING737 737524 1384721NM FUSELAGE BENT A CALAK NONE O OTHER ININSP/MAINT 1 SW2718658 28919 INSPECTION FOUND BELTFRAME IN FORWARD BAG BIN BENT AT STA 440 BETWEEN S28R AND 27R. REPAIRED BELTFRAME IAW SRM 53-00-07 FIGURE 205. 2L72 4F RTA16WE 20040322000522004032200052EA 2004 3 22 04067667A 120040307A3320 BULB CNDAIRCL600 CL6002B19 1900309EA LAVATORY WRONG PART A VTZAA UNSCHED LANDING WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27667BR 7535 DURING CLIMB FLIGHT CREW RECEIVED AN INDICATION FOR SMOKE IN LAVATORY WITH AN ACCOMPANIED BURNING ODOR. AIRCRAFT LANDED NORMALLY AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND THAT LAVATORY RETURN TO SEAT SIGN SHOWED SIGNS OF LOCAL OVER HEATING. FURTHER INVESTIGATION REVEALED THAT NUMEROUS INCORRECT P/N BULBS HAD BEEN INSTALLED IN THIS 28V LIGHT ASSEMBLY. THE COVER OF LIGHT ASSEMBLY WAS DISCOLORED DUE TO OVERHEATING, SEVERAL OF THE BULB BASES BAKED TO THE POINT OF FRACTURING. ISSUED A SMP REGARDING THIS EVENT AND AN FCD TO INSPECT THE FLEET FOR ANY LIKE CONDITION. INCLUDED IN PRE-SHIFT BRIEFS THAT SPECIAL CARE MUST BE TAKEN WHEN INSTALLING THESE BULBS TO INSURE THE PROPER BULB IS INSTALLED. 2L72 4F RTA21EA 20040322000532004032200053NM 2004 3 22 374PA0007 120040303A1430 BOLT BOEING737 73736M 138443BNM RUDDER LOOSE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 FOUND FIVE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER PARA (A) & (B) OF AD 2003-26-01 AND BOEING SB 737-55A1087. REPLACED HARDWARE AT LOCATIONS F1, F2, F3, F4, F10 PER BOEING SERVICE BULLETIN. 2L72 4F RTA16WE 20040322000572004032200057EA 2004 3 22 04068667B 120040308A3320 MOUNT CNDAIRCL600 CL6002B19 1900309EA LAVATORY LIGHT DIRTY A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27667BR 7535 DURING PUSHBACK A LAVATORY SMOKE INDICATION WAS RECEIVED. THE AIRCRAFT RETURNED TO THE GATE AND THE PASSENGERS DEPLANED NORMALLY. THERE WAS NO INDICATION OF SMOKE IN THE LAVATORY. CLEANED THE BACKING PLATE FOR THE LAVATORY LIGHT AND RETURNED THE RETURN TO SEAT LIGHT. PERFORMED AN OPS CHECK FOR 1.5 HOURS WITH NO FURTHER PROBLEMS EXPERIENCED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000582004032200058EA 2004 3 22 04067667C 120040307A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA VTZAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27667BR 7535 TOILET SMOKE MESSAGE WAS RECEIVED. NO INDICATION OF SMOKE FOUND IN THE LAVATORY. REPLACED SMOKE DETECTOR AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000592004032200059EA 2004 3 22 04067667B 120040307A3320 LIGHT CNDAIRCL600 CL6002B19 1900309EA LAVATORY OVERHEATED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27667BR 7535 DURING THE CLIMB THE FLIGHT CREW RECEIVED AN INDICATION FOR SMOKE IN THE LAVATORY WITH AN ACCOMPANIED BURNING ODOR. THE AIRCRAFT LANDED NORMALLY AND THE PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND THAT THE LAVATORY RETURN TO SEAT SIGN SHOWED SIGNS OF LOCAL OVER HEATING. THE SIGN WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000602004032200060EA 2004 3 22 04065651 120040305A27507455001 HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27651BR 7426 DURING FLAP EXTENSION, THE FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. THE MALFUNCTION DID NOT INTERFERE WITH THE SAFE OPERATION OF THE FLIGHT. THE FLIGHT WAS COMPLETED NORMALLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP CONTROL LEVER WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000622004032200062EA 2004 3 22 04065689 120040305A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27689BR 7737 THE FORWARD CABIN EMERGENCY LIGHT WAS INOP. REPLACED THE FORWARD CABIN EMERGENCY LIGHT BULB. AIRCRAFT RETURNED TO SERVICE WITH AN WORKING FORWARD CABIN EMERGENCY LIGHT. 2L72 4F RTA21EA 20040322000632004032200063EA 2004 3 22 04065710 120040305A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27710BR 7852 THE SECOND EMERGENCY LIGHT ON THE RIGHT SIDE OF THE AIRPLANE WAS INOP. THE LIGHT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000662004032200066EU 2004 3 22 04069316 120040309A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN FLOOR INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27316UE 41055 THE AFT EMERGENCY FLOOR LIGHTING WAS INOPERATIVE WHEN TESTED. THE AFT EMERGENCY FLOOR LIGHTING WAS REPAIRED AND OPERATION CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20040322000682004032200068EA 2004 3 22 04068667 120040308A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA AIR CON SYSTEM CONTAMINATED A VTZAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 EA27667BR 7535 LAVATORY SMOKE MESSAGE WAS RECEIVED BY THE FLIGHT CREW BUT THE RETURN TO SEAT LIGHT SELECTED WAS OFF. THE SMOKE DETECTOR AND COALESCER BAG WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000692004032200069EA 2004 3 22 04071669 120040311A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000712004032200071SO 2004 3 22 C2XA04IA029 120040309A2611 SMOKE DETECTOR EMB 145 EMB145ER 3260211SO CARGO BAY FALSE ACTIVATIONA C2XAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2714940 145033 CREW REPORTED THAT THE CARGO SMOKE WARNING INDICATION ILLUMINATED DURING FLIGHT. THE CREW ELECTED TO DISCHARGE THE CARGO BAY FIRE BOTTLES AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. THE SMOKE DETECTION SYSTEM WAS TESTED, THE FIRE BOTTLES WERE REPLACED, AND THE DISCREPANCY CLEARED. 2L72 4F RTT00011AT 20040322000722004032200072SO 2004 3 22 CHQA000465 120040308A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11292 145488 CENTER OVERHEAD EMERGENCY LIGHT LOCATED AT EMERGENCY EXITS (AFT SIDE) IS INOP. DROPPED CENTER OVERHEAD PANEL LOCATED AT EMERGENCY WING EXITS TO VERIFY CONNECTION OF LIGHT ASSY WIRES. WIRES CONNECTED. RESECURED OVERHEAD PANEL IAW EMB 145 AMM 25-22-04. OPS CHECKED EMERGENCY LIGHT SYSTEM IAW EMB AMM 33-50-00. OPS CHECK GOOD, ALL LIGHTS ILLUMINATE. 2L72 4T RTT00011AT 20040322000732004032200073EU 2004 3 22 AWXA200400271 120040311A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 221 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28632AW 81 CMH - EEL - DURING 4-DAY CHECK THE LT FORWARD CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040322000752004032200075 2004 3 22 AWXA200400273 420040309A3497 WIRE HARNESS BOEING737 7373G7 1384595NM COCKPIT BURNED A AWXAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 WP28158AW 23780 ON DESCENT INTO LAS EN ROUTE FROM MSP ARCING AND SMOKE APPEARED IN COCKPIT CEILING ABOVE CAPTAINS CIRCUIT BREAKER PANEL BS 259.5. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE IN WORK REPLACING WIRE HARNESS. MAINTENANCE FOUND WIRE HARNESS CHAFED ON CLAMP CAUSING A SHORT. REMOVED AND REPLACED 63 WIRES IN 7 WIRE RUNS FROM P6 CIRCUIT BREAKER PANEL TO DISCONNECT CONNECTOR BS 285. SYSTEMS AFFECTED BY DAMAGED WIRES INCLUDE; EQUIPMENT COOLING, PASSENGER READING LIGHTS, NO SMOKING/SEAT BELT SIGNS, LANDING LIGHTS, EXTERIOR LIGHTS, MACH AIRSPEED WARNING, STALL WARNING, PITOT STATIC, AND ENGINE/NOSE COWL ANTI-ICE. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040322000762004032200076SO 2004 3 22 CHQA000467 120040311A3350 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11283 145424 RIGHT FWD EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT. 2L72 4T RTT00011AT 20040322000772004032200077SO 2004 3 22 C2XA04SH153 120040312A531314528737001 STRINGER EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCING ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322000792004032200079SO 2004 3 22 C2XA04SH155 120040312A532014525480003 SILL EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT SILL WAS FOUND TO BE CORRODED FROM FRAME 65 TO 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322000802004032200080SO 2004 3 22 C2XA04SH156 120040312A541114576057622 RIB EMB 145 EMB145 3260210SO NR 2 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE AFT EDGE MEMBER OF THE NR 2 ENGINE UPPER COWLING WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322000862004032200086 2004 3 22 SWAA040764 420040311A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SPV, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040322000892004032200089NM 2004 3 22 SWAA040767 120040311A55236959227 BUSHING BOEING737 7373H4 1384600NM ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED NR 1 TO NR 4 ELEVATOR TAB HINGE BUSHINGS. 2L72 4F RTA16WE 20040322000912004032200091NM 2004 3 22 SWAA040769 120040311A53136551698 SPLICE BOEING737 7373Y0 1384671NM STRINGER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED A BS 907, STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040322000942004032200094NM 2004 3 22 SWAA040772 120040313A801135057165 STARTER BOEING737 7373H4 1384600NM NR 2 ENGINE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 WHILE STARTING NR 2 ENG, NOTICED SPARKS FROM COWLING. REMOVED AND REPLACED NR 2 ENG STARTER PER MM. 2L72 4F RTA16WE 20040322000952004032200095NM 2004 3 22 SWAA040773 120040313A3350BR9442 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040322000962004032200096NM 2004 3 22 SWAA040774 120040313A3350300432 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. RELAMPED AFT EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040322000982004032200098NM 2004 3 22 SWAA040777 120040313A531365C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STRINGER 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040322000992004032200099NM 2004 3 22 SWAA040778 120040313A53106547977 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 616 TO BS 639, RBL 63, WL 208. REMOVED AND REPLACED CREASE BEAM CHORD PER SRM. 2L72 4F RTA16WE 20040322001002004032200100NM 2004 3 22 SWAA040779 120040313A5510 STRUCTURE BOEING737 7373Y0 1384671NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND CORROSION ON RIGHT HORIZONTAL STAB CENTER SECTION FWD AND AFT SPAR, UPPER AND LOWER CLEVIS, FWD AND AFT LUG FACES. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20040322001012004032200101NM 2004 3 22 SWAA040780 120040312A7933162BL804A BULB BOEING737 7373H4 1384600NM NR 2 ENG OIL MALFUNCTIONED A SWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW29611SW 27697 DECLARED EMERGENCY, INFLIGHT SHUT DOWN, AIR TURNBACK. DURING CRUISE NR 2 ENG OIL TEMP IN YELLOW BAND, C/W QRH, OIL TEMP STILL IN YELLOW BAND, MOMENTARLY IN RED BAND, SHUT DOWN NR 2 ENG. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB PER MM. 2L72 4F RTA16WE 20040322001022004032200102 2004 3 22 SWAA040781 420040312A2565 INDICATOR BOEING737 7377H4 1384404NM SLIDE BOTTLE MALFUNCTIONED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 0219F 27867 L1 DOOR EVAC SLIDE LOW PRESS IND. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040322001032004032200103NM 2004 3 22 SWAA040782 120040312A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 EEPLS COVER AT ROW 2 ABC LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040322001052004032200105NM 2004 3 22 SWAA040784 120040312A53126517583 VERTICAL BEAM BOEING737 7373Y0 1384671NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED SPV, FOUND VERTICAL BEAM AT BS 180, RBL 17.1, WL 184 CRACKED. REPAIRED BEAM PER SRM. 2L72 4F RTA16WE 20040318001012004031800101NM 2004 3 18 SWAA040637 120040227A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 6L CRACKED FROM BS 360 TO BS 380. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040318001022004031800102NM 2004 3 18 SWAA040638 120040227A5753 SKIN BOEING737 7373K2 13844BANM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040318001032004031800103NM 2004 3 18 SWAA040639 120040227A5753 SKIN BOEING737 7373K2 13844BANM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040318001062004031800106NM 2004 3 18 SWAA040642 120040228A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT DETERIORATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 EEPLS COVER DETERIORATED AT THE RT SIDE OF AFT CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040318001152004031800115NM 2004 3 18 SWAA040652 120040229A53106546529 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED 1/4D CHECK, FOUND SHEARE TIE CORRODED AT BS 482, LOWER BILGE AREA. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040318001262004031800126NM 2004 3 18 SWAA040570 120040224A5311963820 FRAME BOEING737 7372H4 138448CNM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED SPV, FOUND FRAME CRACKED AT BS 178, WL 184, RBL 5.5 AND RBL 7. REPAIRED FRAME PER SRM. 2L72 4F A16WE 20040318001272004031800127 2004 3 18 SWAA040571 420040222A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040318001292004031800129NM 2004 3 18 SWAA040573 120040224A52406545871 FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR ASSEMBLY FRAME CRACKED AT NR 3 AFT STOP MOUNT. REMOVED AND REPLACED R1 DOOR PER MM. 2L72 4F RTA16WE 20040318001402004031800140 2004 3 18 234TR0016 420040304A2210 COMPUTER BOEING737 737228 13844AGNM COCKPIT MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05234TR 23004 MCP AUTOPILOT B INOP AND F/O FLIGHT DIRECTOR INOP. PLACED ON MEL 22-15-2. 2L72 4F RTA16WE 20040318001422004031800142NM 2004 3 18 750WL0002 120040301A3397 WIRE BOEING757 757200 1384950NM EMERGENCY LIGHTSBROKEN A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY LIGHTS BY -B- AND -C- LAVS INOP. SPLICED BROKEN WIRE PER SWPM 20-30-12. 2L72 4F RTA2NM 20040318001512004031800151 2004 3 18 MALA040225 420040226A2565 HANDLE BAC 146 AVRO146RJ85A1500097EU ESCAPE SLIDE MISROUTED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15510XJ E2323 MAIN PAX DOOR SLIDE PULL HANDLE ON EMERGENCY SLIDE NOT ROUTED CORRECTLY. REMOVED SLIDE PACK & RE-ROUTED SLIDE FLAP AS REQ'D FOR PROPER OPERATION & INSTALLATION. 2H74 4F RTA49EU 20040318001632004031800163NM 2004 3 18 04FDEA00556 120040303A53116516340 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY FRAME DENTED, BS 990, BETWEEN STR 26L & 25L. REPAIRED IAW FED EX EA 7-5310-55245. 2L73 4F RTA3WE 20040318001652004031800165NM 2004 3 18 04FDEA00558 120040303A53116556121 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25234FE 21328 AFT CARGO BAY, FRAME DENTED, BETWEEN STR 26L & 25L AT BS 950C. REPAIRED IAW FED EX EA 7-5310-55240. 2L73 4F RTA3WE 20040318001752004031800175NM 2004 3 18 04FDEA00589 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 RIGHT WING I/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER I/B HOLE FOUND CORROSION. CORROSION REMOVED AS PER EA 1-5750-75312, TITLE : WINGS - I/B TE FLAP - RT O/B BRACKET (FLAP SIDE) - PIVOT BORE CORROSION - REPAIR. 2L73 4F RTA22WE 20040318001862004031800186NM 2004 3 18 04FDEA00591 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LEFT WING O/B FLAP (FLAP SIDE) I/B HINGE BRACKET LOWER I/B HINGE HOLE FOUND CORROSION. CORROSION REMOVED & REPAIRED AS PER EA 1-5750-75287, TITLE : WINGS - LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001912004031800191NM 2004 3 18 04FDEA00597 120040305A5753 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25617FE 48748 LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE FOUND CORROSION. LT WING O/B FLAP (FLAP SIDE) O/B HINGE BRACKET LOWER O/B HINGE HOLE CORROSION REMOVED & REPLACED AS PER EA 1-5750-75288 TITLE WINGS - LT O/B FLAP O/B HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040318001942004031800194NM 2004 3 18 04FDEA00600 120040305A5260 LIGHT BOEING727 727200 138407ENM AIRSTAIR DOOR FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25204FE 22926 AFT AIRSTAIR LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF AT 4500 FT & 240 KNOTS. RETURNED BACK TO MEM & LIGHT WENT OUT AFTER LANDING. MEL 05MAR04 12:10. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 15MAR04. 2L73 4F RTA3WE 20040318001972004031800197EU 2004 3 18 04FDEA00603 120040306A7830 THRUST REVERSER AIRBUS310 A310 EU NR 1 ENGINE INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25447FE 251 NR 1 ENG REVERSER OPERATING LIGHT CAME ON (AMBER) AS TAKEOFF POWER WAS APPLIED AT ATL. THE LIGHT WENT OUT AFTER THE THROTTLE WAS BROUGHT BACK TO IDLE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 16MAR04 MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) 1 REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FWD THRUST POS. 2L72 4F RTA35EU 20040318002122004031800212NM 2004 3 18 UPS04442001 120040226A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, FWD CARGO COMPT, LEFT STA 980 FRAME FOUND CRACKED AT STRINGER 39 AREA. FRAME REPAIRED PER SRM 53-10-04 FIG 64. 2L74 4F RTA20WE 20040319000012004031900001WP 2004 3 19 IXXA0400010O 120040219A5610 WINDOW DOUG DC8 DC871F 302199DWP COCKPIT DELAMINATED A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11821BX846511754 45811 DURING TAKEOFF FROM KMCO F/O'S WINDOW STARTED DELAMINATION. CREW SHUTOFF WINDOW HEAT AND DELAMINATING STOPPED. CREW RETURNED AIRCRAFT TO KMCO AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. AFTER INSPECTION OF F/O'S WINDOW FOUND IT TO BE THE INNER WINDOW WITH THE DELAMINATION. FOUND IT WITHIN LIMITS PER ALL APPLICABLE MANUELS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040319000032004031900003EU 2004 3 19 2004F00084 120040226A3241 GENERATOR AMD FALC20FALCON 2720302EU ANTI-SKID SYS DEFECTIVE G O OTHER J WARNING INDICATION LDLANDING 1 GL23258PE 530 OCT85124E 163 UPON LANDING, AIRCRAFT DEPARTED RUNWAY. PILOT STATED THE LT BRAKES HAD FAILED. MIDCOAST AVIATION INSPECTED THE BRAKE SYSTEM, AND DISCOVERED THAT THE NR 1 ANTI-SKID GENERATOR HAD FAILED. MIDCOAST REPLACED THIS UNIT WITH A SERVICEABLE UNIT, FUNCTIOAL CHECK WAS SATISFACTORY. 2L72 4F A7EU 20040319000142004031900014EU 2004 3 19 MALA040233 120040205A2613 CONNECTOR SAAB SF340 340B 7860101EU RT TAILPIPE DAMAGED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15369PX 340B295 RIGHT TAILPIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO TVC AND LANDED OVERWEIGHT. MX REPLACED CONNECTOR. NO OTHER INFORMATION AT THIS TIME. 2L72 4T RTA52EU 20040319000182004031900018EU 2004 3 19 MALA040232 120040304A3260 UPLOCK ROLLER SAAB SF340 340B 7860101EU NLG CONTAMINATED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15425XJ 340B425 GEAR INTRANSIT LIGHT DID NOT EXTINGUISH AFTER TAKEOFF FROM JMS. CYCLED GEAR AS PER QRH BUT TRANSIT LIGHT DID NOT GO OUT. HYDRAULIC SYSTEMS INDICATIONS AND OPERATION WERE ALL NORMAL. CONTINUED FLIGHT TO DVL DUE TO VERY HEAVY ICE IN JMS AREA. GEAR OPERATED NORMALLY FOR LANDING. POST INSPECTION FOUND ICE ACCUMULATION ON NOSE GEAR ROLLER AND PLATE REA. REMOVED ICE ON UPLOCK ROLLER AND STRIKE PAD AREA. 2L72 4T RTA52EU 20040319000212004031900021NM 2004 3 19 HNAA0400015 120040305A3220MS21251B2L TURNBUCKLE DHAV DHC8 DHC8102 2809003NM NLG BENT A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07942HA 163 NOSE LANDING GEAR WOULD NOT RELEASE HAD TO BE MANUALLY RELEASED. WHEN GEAR HANDLE SELECTED DOWN NOSE UNSAFE LIGHT D/N ILLUMINATE, TRIED MANUAL EXTENSION, DID NOT WORK, TRIED AGAIN AND GEAR UNLOCKED. FOUND TURNBUCKLE BENT. REMOVED AND REPLACED TURNBUCKLE, OPS CHECK GOOD. 2H72 4T RTA13NM 20040319000302004031900030NE 2004 3 19 CALA0400220 220040306A7200 ENGINE BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE NR 1 MALFUNCTIONED A CALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW2712327 23457 720315 THE NR 1 ENGINE EXPERIENCED A POWER LOSS AT CRUISE WHILE EN ROUTE FROM MCO TO CLE. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED IAW MM 71-00-00. SHOP TEARDOWN REVEALED A FAILED NR 4 BEARING. 2L72 4F4 FRTA16WE E2GL 20040319000342004031900034NM 2004 3 19 CALA0400224 120040309A532065317876 ATTACH ANGLE BOEING737 7373T0 1384582NM L1 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND L-1 DOOR THRESHOLD ATTACH ANGLES CORRODED. NEW ANGLES WERE INSTALLED IAW SRM 51-40-01. 2L72 4F RTA16WE 20040319000372004031900037NM 2004 3 19 C1HA200483003 120040227A3350 BATTERY PACK BOEING727 7272S7 138407ZNM EMERGENCY LIGHT INOPERATIVE A C1HAK NONE L NO TEST ININSP/MAINT 1 GL15683CA 22490 AFT EMERGENCY EXIT SIGN INOP. FOUND BATTERY PACK INOPERATIVE. 2L73 4F A3WE 20040319000462004031900046NM 2004 3 19 219PA0013 120040303A3350 LAMP BOEING737 737222 1384473NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05219PA 19956 AFT CENTER AISLE EMERGENCY EXIT LIGHTS INOP. RELAMPED AND OPS CHECKS GOOD PER MM 33-51-02. 2L72 4F A16WE 20040319000512004031900051NM 2004 3 19 04FDEA00529 120040229A5744ARC05682 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 LEFT WING - OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT FOUND SUPPORT BRACKET CRACKED. REMOVED CRACKED BRACKET AS PER SRM 51-31-01, VOL II AND FABRICATED NEW TEE BRACKET AS PER DRAWING ARC0568. INSTALLED NEW TEE BRACKET AT LT WING OUTBOARD TRAILING EDGE FLAP OUTBOARD HINGE NR 3 FRAME FROM AFT AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040319000652004031900065SO 2004 3 19 C2XA04CL017 120040308A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716976 145171 CLE FLIGHT 2369 CREW REPORTED THAT 2 FLOOR PROXIMITY STRIPS WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH FLOOR PROXIMITY STRIPS. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040319000672004031900067NE 2004 3 19 P5CA0401054 220040308A7230773241 FAN BLADE BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 3 ENGINE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 689185 NR 3 ENG HAS ONE FAN BLADE TIP BENT, A SECOND FAN BLADE TIP BLADE FOUND DAMAGED & BROKEN. TWO BLADES REPLACED. 2L74 4F4 F A20WE E3NE 20040319000862004031900086SO 2004 3 19 C2XA04IA024 120040306A33507281000501 MODULE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAO OTHER L NO TEST CRCRUISE 1 SW2716541 145542 DURING CRUISE THE EMERGENCY LIGHT NOT ARMED CAUTION ADVISORY ILLUMINATED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LIGHTING CONTROL MODULE. OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040319000932004031900093CE 2004 3 19 DXTA200400251 120040222A3240 HOSE CESSNA500 560CESSNA 2076750CE BRAKE ASSY LEAKING E DXTAO OTHER K FLUID LOSS LDLANDING 1 GL07315QS 5600315 ON LANDING NOTICED NO BRAKING FORCE WITH THE RIGHT BRAKE PEDAL, ON POST FLIGHT INSPECTION FOUND BRAKE FLUID VISIBLY LEAKING FROM RIGHT MAIN WHEEL ASSEMBLY. JACKED AIRCRAFT AND FOUND WITH GEAR EXTENDED THE RIGHT HAND BRAKE HOSE LEAKING. REMOVED AND REPLACED BRAKE HOSE. BLEED BOTH LT AND RT BRAKE ASSEMBLY, OPS CHECK GOOD. LEAK CHECK GOOD IAW CESSNA 560 MM CHAPTER 32-42-01. 2L72 4F RTA22CE 20040319000962004031900096EU 2004 3 19 DXTA200400258 120040308A2120 ODOR ISRAELGALAXYGALAXY 4500307EU COCKPIT DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07700QS 052 AFTER 1.5 HOURS INTO FLIGHT, CREW NOTICED EXHAUST ODOR IN COCKPIT, SELECTED DIFFERENT AIR SUPPLY AND PROBLEM REMAINED. PRECAUTIONARY DIVERTED TO ABQ. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA53NM 20040319001172004031900117 2004 3 19 757BJ0007 420040310A2210 COMPUTER BOEING757 757236 1384971NM FLT CONTROL FAILED A PIDAO OTHER J WARNING INDICATION CRCRUISE 1 SO05757BJ 22176 FIRST OFFICER'S FLIGHT DIRECTOR BARS WENT ERRATIC IN CRUISE (INTERMITTENT). REPLACED RIGHT FCC COMPUTER PER MM 22-11-01. CHECKED BAD UPON INSTALLATION. REMOVED FCC COMPUTER, CLEANED AND RERACKED ORIGINAL FCC COMPUTER PER MM 22-11-01. OPS CHECKED OK. 2L72 4F RTA2NM 20040319001332004031900133NM 2004 3 19 SWAA040705 120040305A3350207330 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2L72 4F RTA16WE 20040319001372004031900137NM 2004 3 19 SWAA040709 120040305A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND BS 639 FRAME INBD CHORD CRACKED AT WL 208, RT SIDE. REPAIRED FRAME PER ERO. 2L72 4F RTA16WE 20040319001432004031900143NM 2004 3 19 SWAA040715 120040306A335065C27095 BATTERY BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED SPECIAL VISIT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 10 ABC, 8 DEF AND LT OVERWING. RECHARGED BATTERIES PER MM. 2L72 4F RTA16WE 20040319001452004031900145NM 2004 3 19 SWAA040686 120040304A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20040319001462004031900146 2004 3 19 SWAA040687 420040304A256561621469 SLIDE BOEING737 7375H4 138449DNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 L2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040319001482004031900148NM 2004 3 19 SWAA040689 120040304A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND KEELBEAM CRACKED AT BS 540, STR 28L AND STR 28R. REPAIRED KEEL BEAM PER ERO. 2L72 4F RTA16WE 20040319001522004031900152NM 2004 3 19 SWAA040696 120040304A53106546524 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040319001542004031900154NM 2004 3 19 SWAA040698 120040304A53126545422 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND BS 727 BULKHEAD WEB CRACKED AT BL 0, WL 185. REPAIRED WEB PER SWA EA. 2L72 4F A16WE 20040319001712004031900171NM 2004 3 19 SWAA040723 120040307A53106546533 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040319001782004031900178NM 2004 3 19 SWAA040730 120040308A57536547836 FITTING BOEING737 7373T5 1384608NM LT WING BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 LT WING OUTBD FORE FLAP ATTACH FITTING BROKEN. REMOVED AND REPLACED LT WING OUTBD FORE FLAP PER MM. 2L72 4F RTA16WE 20040319001792004031900179 2004 3 19 SWAA040731 420040308A256563550101 SLIDE BOEING737 7377H4 1384404NM L2 DOOR WRONG PART A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29796SW 27889 L2 DOOR EVACUATION SLIDE WOULD NOT ARM. FOUND INCORRECT SLIDE INSTALLED DURING MV2 CK ON THE PREVIOUS NIGHT TO THIS FLIGHT. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040319001812004031900181NM 2004 3 19 SWAA040733 120040308A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN FLOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29739GB 29275 EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20040322000092004032200009 2004 3 22 DHL2004783005 420040305A3414 INDICATOR BOEING727 727227 1384078NM NR 1 AIRSPEED MALFUNCTIONED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01783DH 21999 NR 1 WARNING HORN (CLACKER) SOUNDED DURING TAKEOFF ROLL. MACH AIRSPEED WARNING SYSTEM DEFERRED IAW MEL 34-4-3 CAT-B. DMI 15965. SP34-4 COMPLIED WITH CIRCUIT BREAKERS PULLED TO DEACTIVATE SYSTEM. REJECTED TAKEOFF BECAUSE OVER SPEED WARNING CLACKER SOUNDED. A/C WEIGHT = 136.2, IAS = 120, OAT = +6, PA 620, CAUTION ZONE. COMPLIED WITH DHL BOEING M/M HIGH ENERGY STOP SPECIAL INSPECTION CHECK PER 5-51-121. NO DEFECTS NOTED. BRAKE COOL DOWN PERIOD OF 38 MINUTES OBSERVED. REF ITEM 2P LOG PAGE 372821 FOR OVERSPEED WARNING CLACKER. REF DMI 15965 NR 1 WARNING HORN (CLACKER) SOUNDED DURING TAKEOFF ROLL. REPLACED NR 1 AIRSPEED INDICATOR OPS CHECKED GOOD PER M/M ADJUST/TEST 34-14-0. THIS CLEARS DMI 15965. 2L73 4F A3WE 20040322000152004032200015WP 2004 3 22 AALA20040324 120040306A3397 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW219619V 53566 DFW EMERGENCY ESCAPE PATH LIGHT MARKER AT FORWARD GALLEY WALL EXIT INOPERATIVE. RECONNECTED THE CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT THE FORWARD GALLEY WALL EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040322000322004032200032NM 2004 3 22 AWXA200400263 120040229A532069539711 CHANNEL BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A 2 INCH CRACK WAS FOUND ON AFT CARGO DOOR HOLD OPEN FITTING SUPPORT (CHANNEL) BETWEEN FLOORBEAM BS 787 AND BS 807, RBL 20. MAINTENANCE REMOVED DAMAGED AFT CARGO DOOR HOLD OPEN FITTING CHANNEL FROM BS 787 TO BS 807, RBL 20; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 FIG 2. 2L72 4F RTA16WE 20040322000332004032200033NM 2004 3 22 AWXA200400264 120040223A57536546431279 SKIN BOEING737 73733A 1384673NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP, 104 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A REPAIR CORE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 16, PG 67-69. 2L72 4F RTA16WE 20040322000362004032200036NM 2004 3 22 AWXA200400267 120040221A5754 SKIN BOEING737 73733A 1384673NM SLAT ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK THE NR 1 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED OUTBOARD OF THE INBOARD AUXILIARY TRACK. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 SLAT WEDGE LOWER SURFACE; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, REPAIR 21, 88C-88E. 2L72 4F RTA16WE 20040322000452004032200045NM 2004 3 22 CALA0400236 120040311A53156545818 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND FLOORBEAM CORRODED ON BOTTOM SIDE AT STA 360, BL 0. A DOUBLER WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20040322000492004032200049NM 2004 3 22 CALA0400240 120040311A5210UNK SKIN BOEING777 777224 1385225NM L-4 DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727015 28678 INSPECTION FOUND L-4 DOOR SKIN DENTED AT LOWER AFT CORNER. REPAIRED IAW SRM 52-10-01. 2L72 4F RTT00001SE 20040322000542004032200054EA 2004 3 22 04071710 120040311A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27710BR 7852 RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000552004032200055EA 2004 3 22 04070635 120040310A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27635BR 7295 EXTERNAL EMERGENCY LIGHTS FOUND INOP AT THE SERVICE DOOR. REPLACED THE BULB AND RESOLVED THE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322000562004032200056EU 2004 3 22 04071305 120040311A3350 BATTERY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27305UE 41019 EMERGENCY TRACK LIGHTS INOP. REPLACED THE NR 1 EMERGENCY BATTERY PACK AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040322000642004032200064NM 2004 3 22 04064420 120040304A2750 CONTROL UNIT DORNERDO32 DO328300 NM TE FLAPS INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27420FJ 3178 DURING FLIGHT THE CREW REPORTED A FLAP CONTROL FAILURE. THE FLAP ECU WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040322000652004032200065NM 2004 3 22 04069403 120040309A3350 BULB DORNERDO32 DO328300 NM LAVATORY BURNED OUT A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27403FJ 3149 LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE WHEN CHECKING. THE LIGHT WAS REPLACED AND RETURNED TO NORMAL SERVICE. 2H72 4T RTA55NM 20040322000742004032200074NM 2004 3 22 AWXA200400272 120040229A53306548240503 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN BELOW THE LT HORIZONTAL STABILIZER AFT OF ATTACH POINT AT BS 1138, STR 7 LT. MAINTENANCE REMOVED CRACKED SECTION OF SKIN BELOW THE LT HORIZONTAL STABILIZER AT BS 1138, STR 7 LT; FABRICATED A NEW REPLACEMENT SECTION OF SKIN PER DWG 65-48240; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1. 2L72 4F RTA16WE 20040322000842004032200084NM 2004 3 22 SWAA040761 120040311A326065C280342 LOCK SENSOR BOEING737 7373H4 1384600NM NLG FAULTY A SWAAO OTHER N FALSE WARNING CLCLIMB 1 SW29334SW 23938 AFTER GEAR RETRACTION, THE RED AND GREEN NLG LIGHTS STAYED ILLUMINATED IN BOTH THE UP AND OFF POSITION. CYCLED GEAR, NO IMPROVEMENT. REMOVED AND REPLACED NLG LOCK SENSOR PER MM. 2L72 4F RTA16WE 20040322000872004032200087 2004 3 22 SWAA040765 420040310A256565C168209 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20040322000922004032200092NM 2004 3 22 SWAA040770 120040313A335007912 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 FWD EEPLS COVER CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040322000932004032200093 2004 3 22 SWAA040771 420040313A2565D31354 SLIDE BOEING737 737301 1384611NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040322000972004032200097NM 2004 3 22 SWAA040775 120040313A3350311500 LENS BOEING737 737317 138447PNM ROW 16 & 17 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 AND 17 DEF. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040322001062004032200106NM 2004 3 22 SWAA040785 120040313A3350OL3071BPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 20 ABC INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040322001082004032200108EA 2004 3 22 04074710 120040314A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE RIGHT HAND OVERWING AND THE SERVICE DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322001092004032200109EA 2004 3 22 04074676 120040314A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27676BR 7644 DURING INSPECTION THE EMERGENCY LIGHT FOWARD OF THE SERVICE DOOR WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040322001102004032200110SO 2004 3 22 C2XA04IA030 120040307A335066903 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716961 145103 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT STRIP AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRIP, OPERATIONALLY TESTED THE LIGHTING, AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20040322001142004032200114EU 2004 3 22 MALA040245 120040309A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4Y/2Y INSPECTION, RIGHT I/B SEAT TRACK HAS CORROSION AT STA 294.5. REMOVED AND REPLACED RIGHT I/B SEAT TRACK AT STA 294 IAW MESABA EO S53060. A/C RELEASE DATE 3/13/2004. 2L72 4T RTA52EU 20040322001172004032200117EU 2004 3 22 MALA040244 120040309A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4Y/2Y INSPECTION IN LCQ, LEFT I/B SEAT TRACK HAS CORROSION AT STA 294. REMOVED AND REPLACED LEFT I/B SEAT TRACK AT STA 294 IAW MESABA EO S53060. A/C RELEASE DATE 3/13/04. 2L72 4T RTA52EU 20040322001182004032200118EU 2004 3 22 MALA040250 120040220A5711 SPAR SAAB SF340 340B 7860101EU RT WING GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 RIGHT O/B LEADING SPAR HAS GOUGES BETWEEN WS 2976 AND WS 3142. MX FABRICATED AND INSTALLED REPAIR ANGLE AND FILLERS IAW TIMCO REQ-L00725. A/C RELEASE DATE 3/8/2004. 2L72 4T RTA52EU 20040322001192004032200119EU 2004 3 22 MALA040251 120040307A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15414XJ 340B414 DURING COMPLETION J/C NR 335003 (OPS TEST OF EMERGENCY LIGHTING SYSTEM) THE POWER SUPPLIES FAULTED IN POSITION 20LN (S/N 1319) AND 24LN (S/N 1412) USING TEST BOX P/N TES-4052081. REMOVED AND REPLACED 24LN POWER SUPPLY. P/N ON AND OFF 3301-51, S/N ON 2006, S/N OFF 1412. ALL CHECKS ARE GOOD. ALL IAW SF340 MM. 2L72 4T RTA52EU 20040322001202004032200120EU 2004 3 22 MALA040248 120040302A3020ONNH24668165 DUCT SAAB SF340 340B 7860101EU INTAKE HEAT BURNED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL15428XJ 340B428 ON APPROACH LEFT INTAKE HEAT BURNED UP & SPARKING. REMOVED AND REPLACED LEFT LOWER DUCT IAW JOB CARD 7160-301. OPS CHECK GOOD P/N ON NH24668-165, S/N ON L180888, P/N OFF NH24668-169, S/N OFF L180871. REMOVED AND REPLACED LEFT INTAKE DEICE MODULE IAW ACT MM 30-21-03, P/N 44730-1, S/N OFF A00432, S/N ON A00142. 2L72 4T RTA52EU 20040322001212004032200121EU 2004 3 22 MALA040246 120040309A5320 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 DURING 4Y/2Y INSPECTION RIGHT STA 294 RBL 10 HAS CORROSION. REMOVED AND REPLACED WEB IAW SRM 51-40-21. A/C RELEASE DATE 3/13/04. 2L72 4T RTA52EU 20040322001232004032200123EU 2004 3 22 YENA200415 120040309A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT FAULTY A YENAK NONE L NO TEST ININSP/MAINT 1 EA15534JB8394 1705 EMERGENCY CABIN LIGHT TEST FAILS FOR EPSU AT EMERGENCY OVERWING RT SIDE. POWER SUPPLY REPLACED, OPERATION TEST GOOD PER AMM 33-51-38-401. 2L72 4F RTA28NM 20040322001242004032200124NM 2004 3 22 CALA0400243 120040312A5754 SKIN BOEING777 777224 1385225NM NR 6 SLAT DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727015 28678 INSPECTION FOUND LT WING NR 6 SLAT SKIN DENTED. REPAIRED IAW SRM 57-43-01, REPAIR 2. 2L72 4F RTT00001SE 20040322001272004032200127 2004 3 22 371PA0038 420040311A22104084042911 COUPLER BOEING737 737306 13844BGNM YAW DAMPER FAILED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 YAW DAMPER INOP. PLACED ON MEL 22-03. 03/12/2004: REPLACED YAW DAMPER COUPLER PER MM 22-13-31 PG 401. TESTS OK. 2L72 4F RTA16NE 20040322001282004032200128SO 2004 3 22 C2XA04CL019 120040307A3397 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DIRTY A C2XAK NONE L NO TEST UKUNKNOWN 1 SW2713936 145025 CLE FLIGHT 3451 THE CREW REPORTED THE EMERGENCY LIGHT SIGN AT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED CONNECTORS ON THE EMERGENCY EXIT SIGN AT SEAT 3BC. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040322001292004032200129SO 2004 3 22 C2XA04BT033 120040311A4900 APU EMB 145 EMB145LR 3260212SO TAILCONE ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2711544 145557 CREW REPORTED, STRONG ELECTRICAL ODOR WHEN SHUTTING DOWN APU. MAINTENANCE PERFORMED SEVERAL APU STARTS AND STOPS, NO ODOR NOTED. APU VISUAL INSPECTION GOOD. OPS CHECKED GOOD IAW EMB145 MM 49-00-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040322001302004032200130SO 2004 3 22 C2XA04CL020 120040312A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713936 145025 CLE FLIGHT 2193 THE CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040322001312004032200131NM 2004 3 22 DHL2004746003 120040312A3241 CONTROL UNIT BOEING727 727224 1384076NM ANTI SKID SYSTEMMALFUNCTIONED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO01746DH 22252 ON LANDING ROLL BELOW 100 KTS APPLIED BRAKES, HAD MINIMUM EFFECT, TOWER REPORTED SMOKE FROM MAINS ON LANDING. TRANSFERRED TO DMI 16023 IAW ASTAR MEL 32-5. PLACARD INSTALLED. MAINTENANCE NOTIFIED. REMOVED AND REPLACED ANTI-SKID (A/S) CONTROL UNIT PER M/M 32-42-61. OPS CHECKED PER M/M 32-42-00 SATISFACTORY. PLACARD REMOVED. THIS CLEARS DMI - 16023. 2L73 4F A3WE 20040322001322004032200132NM 2004 3 22 DHL2004745015 120040313A3260 POSITION SWITCH BOEING727 727224 1384076NM MLG DOOR FAILED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION RIGHT GEAR DOOR LIGHT REMAINED ILLUMINATED. RAN ABNORMAL, LIGHT REMAINED OUT WITH GEAR HANDLE IN UP POSITION. REMOVED AND INSTALLED RIGHT-HAND MAIN GEAR DOOR POSITION SWITCH IAW ASTAR M/M 32-62-11. SWITCH TEST OK. 2L73 4F A3WE 20040322001352004032200135EU 2004 3 22 AALA20040343 120040313A3397P4010051129 MODULE FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211413A 11376 MSP FRONT EMERGENCY FLOOR ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK/MODULE FOR FRONT EMERGENCY FLOOR ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040322001362004032200136WP 2004 3 22 AALA20040344 120040313A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21453AA 49558 DFW EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. FOUND LOOSE CONNECTORS. RESECURED CONNECTORS FOR EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040322001382004032200138SO 2004 3 22 C2XA04IA031 120040308A33507287577505 LIGHT EMB 135 EMB135LR 3260305SO PAX DOOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712519 145366 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT BY THE MAIN CABIN DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT, OPERATIONALLY CHECKED THE LIGHT, AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20040322001402004032200140EU 2004 3 22 AWXA200400275 120040314A3350P4010021 BATTERY AIRBUS320 A320231 3930325EU ZONE 900 - LAVATDISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28629AW 076 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT FORWARD JUMP SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040322001412004032200141EU 2004 3 22 AWXA200400276 120040314A2560P20700012015 FLASHLIGHT AIRBUS320 A320232 3930326EU ZONE 900 - LAVATDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28671AW 2077 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY LT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY LT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040322001432004032200143NE 2004 3 22 AWXA200400278 220040314A7530 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 OVERTEMP A AWXAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION APAPPROACH 1 WP28657AW218804674 1003 V10332 ON APPROACH, NR 2 ENG EGT 890 DEGREES, FUEL FLOW 1300 LBS & OIL PRESS & TEMP NORM. DISCONN AUTOTHROT & MOVED POWER LEVER, EGT REMAINED ABOVE 800 DEGREES FOR 4 MIN, SHUTDOWN ENG & DECLARED EMERGENCY. MX FOUND ENG 4TH STAGE VARIABLE STATOR VAIN ACT LINKAGE BRACKET BROKEN WITH BOLT MISSING. R & R NR 2 ENG IAW T/C. INVEST REPORT OF ENG, FOUND UPPER BOLT ATTACH 4TH STAGE VSV BRACKET IN UNISON RING & MATING DOWEL MISSING, OTHER BOLT STILL IN PLACE. VSV ACT LOADS APPLIED TO BRACKET CAUSED IT TO BEND & CRACK. BOLT MAY HAVE WORKED LOOSE DUE TO DAMAGED HELICOIL. TORQUE CHECK PERFORMED ON HELICOILS, HELICOIL THAT HAD MISSING BOLT HAD TORQUE OF LESS THAN 1 FT LB PER INCH, WHILE OTHER HAD TORQUE OF 2 FT LBS PER INCH. 2L72 4F4 FRTA28NM E40NE 20040322001452004032200145NM 2004 3 22 AWXA200400280 120040221A575465C267943 SKIN BOEING737 73733A 1384673NM NR 2 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK 4 CRACKS WERE FOUND ON NR 2 SLAT LOWER SKIN BELOW INBOARD AUXILIARY TRACK WBL 294.40. MAINTENANCE CUT OUT DAMAGE ON NR 2 SLAT LOWER SKIN WBL 294.40; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 201 PG 216. 2L72 4F RTA16WE 20040322001462004032200146NM 2004 3 22 AWXA200400281 120040223A5414 PANEL BOEING737 73733A 1384673NM LT PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .75 INCH CRACK WAS FOUND ON LT PYLON PANEL 5727L ACCESS OPENING LANDING NAC STA 211. MAINTENANCE STOP DRILLED CRACK ON LT PYLON PANEL 5727L ACCESS OPENING LANDING AT NAC STA 21; PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A DOUBLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5433-01037-DL1. 2L72 4F RTA16WE 20040322001502004032200150SO 2004 3 22 C2XA04IA032 120040312A2120 SMOKE EMB 145 EMB145XR 3260214SO COCKPIT DETECTED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2712135 145718 CREW REPORTED A STRONG ODOR OF SMOKE IN THE COCKPIT AND CABIN UPON TAKEOFF. THE CREW RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED TROUBLESHOOTING TO DETERMINE THE ORIGIN OF THE SMOKE. THE ENGINE AND BLEED SYSTEMS WERE RUN AND THE SMOKE ODOR COULD NOT BE DUPLICATED. THE DISCREPANCY WAS CLEARED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20040322001512004032200151SO 2004 3 22 C2XA04SH159 120040315A53101452246013 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE GOUGED AT FRAME 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001542004032200154NM 2004 3 22 SWAA040789 120040313A3350079123 COVER BOEING737 7377H4 1384404NM ROW 7 MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 EEPLS TRACK COVER MISSING AT ROW 7. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20040322001572004032200157NM 2004 3 22 SWAA040792 120040314A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 986, RT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040322001582004032200158NM 2004 3 22 SWAA040793 120040314A53116545805 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040322001592004032200159NM 2004 3 22 SWAA040794 120040314A53116545805 FRAME BOEING737 7373Y0 1384671NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040322001642004032200164NM 2004 3 22 SWAA040748 120040309A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 FWD CABIN EEPLS COVER BROKEN. REPAIRED FWD CABIN EEPLS COVER PER MM. 2L72 4F RTA16WE 20040322001662004032200166NM 2004 3 22 SWAA040750 120040310A53156546812 FLOORBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SPV, FOUND FLOORBEAM CHORD CORRODED AT BS 986, RBL 38, WL 208. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F A16WE 20040322001672004032200167NM 2004 3 22 SWAA040751 120040310A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STRINGER 23L. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040322001682004032200168NM 2004 3 22 SWAA040752 120040309A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001722004032200172NM 2004 3 22 SWAA040756 120040308A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 500 + 14. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040322001742004032200174 2004 3 22 SWAA040759 420040309A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED HC2, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040322001752004032200175SO 2004 3 22 C2XA04CL022 120040315A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714950 145061 CLE FLIGHT 3158 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040322001762004032200176SO 2004 3 22 CHQA000466 120040316A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281 145391 RIGHT OVERWING AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. BULB P/N GE1317. 2L72 4T RTT00011AT 20040322001772004032200177EA 2004 3 22 COMA0460191 120040311A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A COMAK NONE L NO TEST ININSP/MAINT 1 SO01809CA 7366 FLIGHT 5226 EMERGENCY LIGHTS AT CABIN AND SERVICE DOOR ARE INOP. REPAIRED BROKEN WIRES AND SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20040322001782004032200178EA 2004 3 22 COMA0460192 120040311A5230 DOOR CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR UNSECURE A COMAB EMER. DESCENT O OTHER CLCLIMB 1 SO01467CA 7637 FLIGHT 5917 CABIN ALTITUDE WARNING AND DISPLAY COOL CAUTION. COULD NOT DUPLICATE. INSPECTED AIRCRAFT, FOUND NO DEFECTS. SUSPECT CARGO DOOR NOT CLOSED PROPERLY. 2L72 4F RTA21EA 20040322001792004032200179EA 2004 3 22 COMA0460193 120040311A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01978CA 7158 FLIGHT 5690 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040322001802004032200180EA 2004 3 22 COMA0460194 120040311A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01986CA16595 7174 FLIGHT 5584 NLG DOOR OPEN CAUTION AFTER GEAR RETRACTION. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20040322001832004032200183EA 2004 3 22 COMA0460197 120040312A361022856030105 DUCT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE BLOWN A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01941CA 7050 FLIGHT 5200 RIGHT 14TH STAGE DUCT LEAK WARNING. FOUND 14TH STAGE BLEED DUCT BLOWN APART. REPLACED DUCT. 2L72 4F RTA21EA 20040322001842004032200184NM 2004 3 22 AWXA200400285 120040315A53302024T3071 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN 3 INCHES ABOVE LAP SEAM RT SIDE AT BS 767. MAINTENANCE CUT OUT DAMAGED SKIN 3 INCHES ABOVE LAP SEAM RT SIDE AT BS 767; FABRICATED 2 REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229 PG 334. 2L72 4F RTA16WE 20040322001862004032200186 2004 3 22 AWXA200400288 420040313A341746502003030314 ADC AIRBUSA319 A319132 3930340NM ZONE 123, NR 1 FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28824AW 1490 JFK - ABORTED TAKEOFF - FLT 0411 - ON TAKEOFF AT JFK EN ROUTE TO SFO RECEIVED NR 1 IR FAULT, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE ISSUED MEL 34-10-01, COND 2 IRS NR 1 NAV MODE INOP. ON 03/15/2004 MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA INERTIAL REFERENCE UNIT IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. VENDORS TEARDOWN REPORT OF ADIRU S/N 0987 CONFIRMED FAILURE OF THE UNIT. FOUND VIBRATION ISOLATORS SPLIT AND THE "Y" MULTI OSCILLATOR LASER GYRO UNMODELABLE. REPLACED MULTI OSCILLATOR LASER GYRO (P/N 517107-2, S/N 407913) AND REPLACED VIBRATION ISOLATORS WITH A MATCHED SET. PERFORMED THERMAL CALIBRATION AND TESTED UNIT IAW CMM TP1011, REV. 23. 2L72 4F RTA28NM 20040322001872004032200187NM 2004 3 22 AWXA200400289 120040303A5320654581246 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, RBL 35, WL 201. MAINTENANCE REMOVED CRACKED STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, RBL 35, WL 201; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040322001902004032200190SO 2004 3 22 C2XA04SH163 120040316A531014525523001 DOOR FRAME EMB 135 EMB135LR 3260305SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE LEFT T-SECTION AT THE CARGO DOOR CUT FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED SECTION IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001922004032200192SO 2004 3 22 C2XA04SH165 120040316A532014525480003 BEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001952004032200195NM 2004 3 22 SWAA040800 120040315A53306545771 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 645, STR 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001972004032200197NM 2004 3 22 SWAA040803 120040315A53136551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM. 2L72 4F RTA16WE 20040322001992004032200199SO 2004 3 22 2004F00082 120040314A760380237SHT77 CONTROL ROD GULSTMG159 G159 3952202SO RROYCEDART DART5298X 54507EU ROTOL R4304 R1844304 EU THROTTLE LOOSE E A UNSCHED LANDING O OTHER CLCLIMB 1 SO11197PA261932 93 18108 DRG4064 AIRCRAFT RELEASED FROM MAINTENANCE. DEPARTED VPC. CLIMBING OUT FROM 9,000 FT, RIGHT THROTTLE WOULD NOT RESPOND. RETURNED TO VPC WITH UNEVENTFUL LANDING. MAINTENANCE FOUND THE THROTTLE PUSH PULL ROD CAME LOOSE AT THE FIREWALL (ROD END SEPARATED FROM THE BARREL). MAINTENANCE INSPECTED AND RESECURED ROD END AND FUNCTIONAL CHECK PERFORMED SATISFACTORY. AIRCRAFT RELEASED AT THIS POINT. 2L72 4T4 T 1A17 E297 6 CP899 20040322002012004032200201SO 2004 3 22 CHQA000458 120040205A3350 LIGHT EMB 145 EMB145LR 3260212SO RT OVERWING INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 RIGHT WING OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT WING OVERWING EMERGENCY LIGHT. OPS CHECK GOOD IAW EMB 145 AMM 33-50-10. 2L72 4T RTT00011AT 20040323000022004032300002GL 2004 3 23 ERAA092666 220040113A723023057142 CASE HALF BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL COMPRESSOR DAMAGED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03134EH 635 COMPRESSOR CASE REC'D ON EXCHANGE WITH DAMAGED 6TH STAGE VANES. AS PER MR. GEORGE HICKS OF ALCOR, RETURNING REQUESTING WARRANTY EXCHANGE. RETURNING ON REPAIR ORDER RW-897299 1G72 3U3 U H3EU E4CE 20040323000032004032300003SW 2004 3 23 ERAA092667 120040120A6320412040785103 SPIDER GEAR BELL 412 412 1182202SW M/R HEAD CORRODED A ERAAO OTHER O OTHER NRNOT REPORTED 1 EA03169EH143 33064 SPIDER GEAR WITH ONLY 143.1 HRS HAS NITRITING BREAKING DOWN. TEETH FRETTING AND PITTING. RETURNING ON ERA PACK SLIP NR 5936 REQUESTING CREDIT. 1G72 4U H4SW 20040323000042004032300004SW 2004 3 23 ERAA092668 120040120A6320205040230003 SUN GEAR BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA M/R HEAD CORRODED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH143 33064 UPPER SUN GEAR WITH ONLY 143.1 HRS HAS NITRITING BREAKING DOWN, TEETH FRETTING AND PITTING. RETURNING ON ERA MMIR NR ERAA0001972 REQUESTING CREDIT. 1G72 4U4 U H4SW E22EA 20040323000052004032300005 2004 3 23 BAQA092565 420040204A3454066400703 CONTROL UNIT BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101* NE VOR SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KC6216 7168 DOES NOT CONVERT VOR COMPOSITE FOR SIN/COS ON HSI BEARING POINTER. REPLACED WITH SERVICABLE UNIT. 02/11/2004 1G72 3U3 UNCH13EU E5NE 20040323000062004032300006EU 2004 3 23 MHIA092672 120040203A3260455TSO1Y INDICATOR AEROSPAS365 AS365N2 8680815EU TMECA ARRIELARRIEL1 60030NE RT MLG INOPERATIVE B MHIAO OTHER P NO WARNING INDICATION CRCRUISE 1 EA25886TW 6413 RT LANDING GEAR LIGHT INOPERATIVE, REPLACED INDICATOR. 1G72 3U3 URTH10EU E19EU 20040323000072004032300007EU 2004 3 23 MHIA092673 120040209A5302 STRUCTURE AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE TAILBOOM CRACKED B MHIAK NONE O OTHER ININSP/MAINT 1 EA25401LH6351 3059 TAILBOOM CRACKED ON LOWER SURFACE AT RT BATTERY SUPPORT FOR AFT BATTERY INSTALLATION. CRACK STARTED AT FRAME 3035 AND WENT FOWARD 143MM MOVING UP THE TAIL BOOM RT SIDE TO 21MM FROM THE SIXTH RIVET FORWARD FROM FRAME 3035. AFTER DISCUSSION WITH MFG ENGINEERING DECIDED REPAIR COULD BE MADE IAW MM SECTIONS 53.10.40.701, 771 AND STANDARD PRACTICES MANUAL SECTION 20.03.05.407, 411. REPAIRS COMPLETED IAW THESE DOCUMENTS. RECOMMEND OPERATORS WITH STC SH5117NM RELOCATION OF THE BATTERY TO TAILBOOM INSPECT THE TAILBOOM SKIN AT THE LOWER FLANGE RIVET LINE OF LT BATTERY SUPPORT P/N G10101 AND RT SUPPORT G10102 AT 100 H. 1G72 3U3 U H11EU E19EU 20040323000082004032300008 2004 3 23 BAQA092697 420040213A2210 LIGHT LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP AUTOPILOT SYS INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11566 1134 092 SEVERAL LIGHTS INOPERATIVE ON UNIT. MRA NR 1155272-000020 REPLACED WITH SERVICABLE UNIT. 02/16/2004 2L72 4F4 F A10CE E6WE 20040323000102004032300010EU 2004 3 23 BAQA092490 120040130A28221176415103 PUMP BOLKMS117 BK117B1 5626012EU ALLSN 250C 250C47B GL FUEL BOOST INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 SW03213AE447 7219 EXCHANGE. FUEL PUMP OPERATING INTERMITTENTLY. REPLACED WITH SERVICALE UNIT. 02/02/2004 1G72 3U3 U H13EU E1GL 20040323000122004032300012 2004 3 23 BAQA091936 420040203A34214021541791 AHRS BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME400 7243 AUTO PILOT WOULD DECOUPLE. REPLACED WITH SERVICABLE UNIT. 02/03/2004 1G72 3U3 U H13EU E5NE 20040323000132004032300013 2004 3 23 BAQA092505 420040126A221041800478034 ACTUATOR AEROSPAS365 AS365N2 8680815EU YAW CHANNEL STICKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME221 6417 YAW ACTUATOR STICKING, TAP UNIT IT MOVES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 02/04/2004 1G72 3U RTH10EU 20040323000142004032300014 2004 3 23 BAQA092507 420040127A220041800561612 ACTUATOR AEROSPAS365 AS365N2 8680815EU AUTOFLIGHT FAILED B BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03915ME680 6417 FAILED MEGGER TEST. REPLACED WITH SERVICABLE UNIT. 02/04/2004 1G72 3U RTH10EU 20040323000182004032300018EU 2004 3 23 BAQA092537 120040128A77141179405303 INDICATOR BOLKMS117 BK117B1 5626012EU TRIPLE TACH FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117US 7175 ROTOR NEEDLE PEGS HIGH WHEN ELECTRICITY IS APPLIED. INSTALLED 10/23/2003, FAILED 01/28/2004. TSI-102.5. PLEASE SEE RO 9-090007-53 FOR MORE DETAILED HISTORY. REPLACED WITH SERVICABLE UNIT FROM OUR ASSET STOCK. 1G72 3U H13EU 20040319000322004031900032NM 2004 3 19 CALA0400222 120040309A5320654587512 ATTACH ANGLE BOEING737 7373T0 1384582NM R1 DOOR FRAME CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND R-1 DOOR JAMB THRESHOLD ATTACH ANGLE CORRODED. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040319000402004031900040SO 2004 3 19 CHQA000464 120040304A3350 BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11563 145509 EMERGENCY LIGHTS BATTERY INOP IN GALLEY. INSTALLED NEW BATTERY IAW EMB 145 AMM II CHAPT 33-50-04. 2L72 4T RTT00011AT 20040319000422004031900042EU 2004 3 19 MALA040241 120040220A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439XJ 340B439 FS 39.8 TO 370.0 HAS VARIOUS DENTS. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. REMOVED AND REPLACED ICE SHIELD IAW MESABA EO S53009. A/C RELEASE DATE 3/8/04. 2L72 4T RTA52EU 20040319000522004031900052EA 2004 3 19 HNAA0400021 120040308A291082970010477 LINE DHAV DHC8 DHC8311 1386006EA HYDRAULIC SYS LEAKING A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07335EN 375 AFTER TAKEOFF NR 2 HYD IOS C/L ILLUMINATED AND NR 2 HYD PRESSURE AND QTY DROPPED TO ZERO, FOLLOWED BY ILLUMINATION OF NR 2 ENG HYD PUMP, RUDDER PRESS, RUDDER FULL PRESS & OUTBD ROLL SPLR. C/L ILLUMINATED. LOST PRESSURE AT 0958 ENGINE SHUTDOWN AT 1040. INSTALLED TFL ON FWD SIDE OF NR 2 PRESSURE MANIFOLD SERVICED AND BLEED NR 2 HYD SYSTEM, GROUND RUN, LEAK CHECK. 2H72 4T RTA13NM 20040319000582004031900058EA 2004 3 19 COMA0460183 120040305A3411 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA PITOT STATIC SYSCONTAMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01958CA 7111 FLIGHT 5221 EFIS COMP MON WARNING DURING T/O. REMOVED WATER FROM PITOT SYSTEM, SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20040319000622004031900062EA 2004 3 19 COMA0460187 120040304A4990 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY OVERSERVICED A COMAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01966CA 7132 FLIGHT 5114 SMOKE IN COCKPIT COMING FROM COPILOTS SIDE PANEL. FOUND APU OVERSERVICED. SERVICED APU TO PROPER LEVEL AND CLEANED UP OIL MESS IN APU COMPARTMENT. 2L72 4F RTA21EA 20040319000662004031900066NM 2004 3 19 P5CA040154 120040308A5730 PANEL BOEING747 747283B 1384867NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LEFT WING UPPER LEADING EDGE PANEL CRACKED APPROX 18 INCHES BETWEEN STA WBL 470 & WBL 642. REPAIRED PANEL. 2L74 4F A20WE 20040319000692004031900069EA 2004 3 19 04066639 120040306A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27639BR 7313 DURING INSPECTION THE RIGHT HAND FORWARD AND AFT EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE LAMPS WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040319000852004031900085EA 2004 3 19 04068679 120040308A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM DISC FAILED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27679BR 7662 THE CREW REPORTED LOSS OF BOTH STABILIZER TRIM CHANNELS AND MACH TRIM AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE AIRPORT AND LANDED NORMALLY. THE PASSENGERS DEPLANED NORMALLY. THE CAPTAINS STABILIZER TRIM DISCONNECT SWITCH WAS REPLACED AND CHECKED OUT GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040319000892004031900089SO 2004 3 19 C2XA04SH146 120040310A531514530633003 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319000972004031900097CE 2004 3 19 DXTA200400252 120040224A2497 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE LAV ELECTRICAL MISPINNED E DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07840QS 258340 DURING PREFLIGHT INSPECTION, CREW SMELLED SMOKE IN CABIN AND DISCOVERED HAND TOWELS IN LAVATORY ON FIRE AND A SMALL PORTION OF THE SIDEWALL NEAR THE ELECTICAL OUTLET BEGINNING TO MELT. FOUND WIRING CONNECTOR BF MIS-PINNED. RE-PINNED CONNECTOR, BENCH CHECKED INVERTER, OPS CHECKED GOOD IAW HAWKER 800XP MM CHAPTER 25-40-14 REV 19, SEC 103. 2L72 4F RTA3EU 20040319001032004031900103NM 2004 3 19 CALA0400230 120040310A53206545875U70 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED AT STA 285-370. THE CORRODED SECTION OF Z-ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20040319001062004031900106NM 2004 3 19 CALA0400233 120040310A3297806002 CIRCUIT CARD BOEING737 7373T0 1384582NM MLG FAILED A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW2717326 23456 THE LANDING GEAR DID NOT RETRACT INITIALLY AFTER TAKEOFF FROM HAV. QRH WAS FOLLOWED AND LOCK OVERRIDE WAS USED TO RETRACT GEAR. THE FLIGHT WAS CONTINUED TO MIA WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE M991 LG LOGIC CIRCUIT CARD AT FAULT. THE M991 CIRCUIT CARD WAS REPLACED. AN OPERATIONAL TEST CHECKED GOOD IAW 32-09-20. 2L72 4F RTA16WE 20040319001112004031900111SO 2004 3 19 C2XA04SH148 120040311A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319001142004031900114SO 2004 3 19 C2XA04SH151 120040312A716014575001405 INTAKE EMB 135 EMB135LR 3260305SO NR 1 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK, THE NR 1 ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040319001302004031900130NM 2004 3 19 SWAA040702 120040305A335065C27095 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED SPECIAL VISIT AT SAT AERSPACE, FOUND EMERGENCY LIGHTS BATTERY PACKS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20040319001562004031900156NM 2004 3 19 SWAA040676 120040301A212164540501 FAN BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29611SW 27697 BURNING ODOR IN CABIN. REMOVED AND REPLACED RECIRCULATING FAN PER MM. 2L72 4F RTA16WE 20040319001572004031900157NM 2004 3 19 SWAA040677 120040303A335065C27093 LIGHT BOEING737 7373H4 1384600NM ROW 10 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 10 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20040319001682004031900168 2004 3 19 SWAA040719 420040306A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29440LV 29835 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20040319001742004031900174NM 2004 3 19 SWAA040726 120040307A53106546593 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040319001752004031900175NM 2004 3 19 SWAA040727 120040307A53116517582 FRAME BOEING737 7373A4 1384585NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND BS 178 BLKHD UPPER CHORD CRACKED AT WL 234, LBL 25. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20040319001862004031900186 2004 3 19 VNAA0403008 420040303A31607014300902 DISPLAY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL07434JS1961410616 3051 THE CREW REPORTED THAT A PRIMARY FUNCTION DISPLAY HAD FADED IN AND OUT TWICE. FLIGHT 2466 THEN DIVERTED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE PRIMARY DISPLAY UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040322000052004032200005NM 2004 3 22 AWXA200400238 120040303A3230114079017 SELECTOR VALVE AIRBUSA319 A319132 3930340NM ZONE 140 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28820AW164392533 1397 PHX - AIR TURNBACK - FLT 0251 - AFTER TAKEOFF FROM PHX EN ROUTE TO MSP RECEIVED ECAM MESSAGE LG LGCIU 2 FAULT, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL AND INTERFACE FACE UNIT (LGCIU) NR 2 (5GA2) IAW AMM 32-31-71. AIRMAN INDICATED A HARD FAULT FOR LANDING GEAR SELECTOR VALVE (40GA). REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-31-12. JACKED AIRCRAFT AND PERFORMED LANDING GEAR OPERATIONAL CHECK, CHECK WAS GOOD. 2L72 4F RTA28NM 20040322000132004032200013NM 2004 3 22 AWXA200400245 120040222A5310654587512 CREASE BEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF R-1 DOOR ENTRY WAY CREASE BEAM UPPER CHORD, UPPER LEG, FROM BS 305 TO BS 320, RBL 47, WL 209. MAINTENANCE REMOVED CORRODED UPPER ANGLE OF CREASE BEAM FROM BS 305 TO BS 320, RBL 47; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1 & 45. 2L72 4F RTA16WE 20040322000242004032200024NM 2004 3 22 AWXA200400254 120040223A53136545767 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER 16 RT AT BS 500C, AFT OF LEADING EDGE LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGED END OF STRINGER 16 RT AT BS 500C; FABRICATED FILLER AND REPAIR CHANNEL; INSTALLED REPAIR PARTS IAW AWA ER 03-5312-01094-DD1. 2L72 4F RTA16WE 20040322000342004032200034NM 2004 3 22 AWXA200400265 120040226A53136936600501 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 277, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 PG 1. 2L72 4F RTA16WE 20040322000352004032200035NM 2004 3 22 AWXA200400266 120040221A5753 SKIN BOEING737 73733A 1384673NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE LT WING TRAILING EDGE FORE FLAP DELAMINATED ON THE OUTBOARD LOWER SURFACE, APPROXIMATELY 2 INCHES FROM END. MAINTENANCE CUT OUT DELAMINATION ON LT WING TRAILING EDGE FORE FLAP; FABRICATED A REPAIR CORE AND DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 16 PG 67-69. 2L72 4F RTA16WE 20040322000472004032200047NM 2004 3 22 CALA0400238 120040311A53206562175133 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND MAIN CABIN FLOOR SUPPORT CORRODED ON UPPER SURFACE AT STA 294-312, RBL 12. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040322000482004032200048NM 2004 3 22 CALA0400239 120040311A5210UNK SKIN BOEING777 777224 1385225NM R-4 DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727015 28678 INSPECTION FOUND R-4 DOOR SKIN DENTED AT LOWER AFT CORNER. REPAIRED IAW SRM 52-10-01, REPAIR 8. 2L72 4F RTT00001SE 20040322000612004032200061NM 2004 3 22 251TR0008 120040311A1430 BOLT BOEING737 737228 13844AGNM RUDDER LOOSE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FOUND NINE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER AD 2003-26-01(A) (B) AND BOEING SB 737-55A1087. RETORQUED BOLTS F5, F6, F7, F8, F10 AND REPLACED BOLTS F1, F2, F3, F4 PER SB 737-55A1087. 2L72 4F RTA16WE 20040322000702004032200070NM 2004 3 22 DHL2004743003 120040308A532069678811 ANGLE BOEING727 727225 1384077NM AIRSTAIR ACT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 FOUND ANGLE AT STA 1273 UNDER AIRSTAIR ACTUATOR FITTING APPROXIMATELY 5 INCH CRACK IN LENGTH DURING OPERATIONAL CHECK. REMOVED AND REPLACED CRACKED ANGLE AT STA 1273 UNDER AIRSTAIR ACTUATOR (PART NUMBER 69-67881, PO NR 400025645) IAW B-727 SRM 51-30-2. 2L73 4F A3WE 20040322000782004032200078SO 2004 3 22 C2XA04SH154 120040312A5320 STRUCTURE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK, THE CROSS MEMBER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322000832004032200083NM 2004 3 22 SWAA040760 120040311A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STRINGER 14R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040322000852004032200085NM 2004 3 22 SWAA040762 120040310A53156546812 FLOORBEAM BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SPV, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED FLOORBEAM PER ER. 2L72 4F A16WE 20040322000902004032200090NM 2004 3 22 SWAA040768 120040311A53116546555 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 867, STRINGER 9L. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040322001222004032200122CE 2004 3 22 075041 120040312A5210 SEAL BEECH 1900 1900D 1154162CE CABIN DOOR FAILED A NSVAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27155CJ UE55 CABIN DOOR SEAL FAILED IN FLIGHT AT 18,000 FEET, AIRCRAFT RETURNED TO BUF. AIRCRAFT FERRIED TO ALB, INSTALLED NEW DOOR SEAL IAW MM 52-10-04. 2L72 4T RTA24CE 20040322001252004032200125NM 2004 3 22 CALA0400244 120040313A533065C35775 SKIN BOEING737 7373T0 1384582NM FUSLEAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2763305 23356 INSPECTION FOUND A 2 INCH CRACK IN RIGHT FUSELAGE SKIN AT BS 727E, S18R ABOVE EMERGENCY EXIT LIGHT AT WATERLINE. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2L72 4F RTA16WE 20040322001342004032200134WP 2004 3 22 AALA20040347 120040214A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21499AA 49737 DFW EMERGENCY LIGHTS AT SIDE IN TAIL COMPARTMENT INOPERATIVE. FOUND CHAFED AND CORRODED WIRING FOR EMERGENCY LIGHTS. REPLACED DAMAGED WIRE SPLICED NEW WIRING FOR EMERGENCY LIGHTS AT SIDE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040322001442004032200144NM 2004 3 22 AWXA200400279 120040305A572065C2802310 ANGLE BOEING737 73733A 1384673NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK .625 INCH CRACK WAS FOUND ON RT WING OUTBOARD EXHAUST GATE ANGLE WBL 205. MAINTENANCE REMOVED CRACKED RT WING OUTBOARD EXHAUST GATE ANGLE AT WBL 205; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW AWA ER 03-5752-04070-KB1. 2L72 4F RTA16WE 20040322001472004032200147NM 2004 3 22 AWXA200400282 120040303A572069177925 INTERCOSTAL BOEING737 7373G7 1384595NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND ON INTERCOSTAL IN NOSE WHEEL WELL BETWEEN BS 243.7 AND BS 251.6, STR 21 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL IN NOSE WHEEL WELL BETWEEN BS 243.7 AND BS 251.6, STR 21 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 14 PG 1, 38 & 56. 2L72 4F RTA16WE 20040322001522004032200152SO 2004 3 22 C2XA04SH160 120040315A531514522460015 STRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK THE AFT LEFT CENTER DIGITAL STRAP WAS FOUND TO BE CORRODED AT FRAME 16 TO FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001532004032200153 2004 3 22 SWAA040788 420040312A25656567380 WINDOW BOEING737 7377H4 1384404NM L1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 L2 DOOR EVACUATION SLIDE VIEWING WINDOW LENS LOOSE. SECURED WINDOW PER MM. 2L72 4F RTA16WE 20040322001602004032200160NM 2004 3 22 SWAA040795 120040314A53136551698 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE PER SRM. 2L72 4F RTA16WE 20040322001702004032200170NM 2004 3 22 SWAA040754 120040310A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, BETWEEN STRINGER 15L AND STRINGER 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040322001892004032200189SO 2004 3 22 C2XA04SH162 120040316A532014522178005 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES AT FRAME 21. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040322001932004032200193EU 2004 3 22 DHL2004363004 120040317A5411RIB RIB AIRBUS300 A300B4203 3930306EU NR 1 NACELLE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING A-CHECK, PYLON ENGINE NR 1 AT COWL HINGE FITTING INBOARD SIDE HAS A CRACK BELOW TEE BRACKET AT RIB 4. NR 4 RIGHT RIB HAS APPROXIMATELY A 3 INCH CRACK AT REVERSER HINGE AFT BRACKET (VISUALLY DETECTED). PERFORM EXTERNAL INSPECTION OF SIDE PANEL AND BOLT EVERY 200 FLIGHT HOURS AND THE REPAIR BEFORE 500 FLIGHT HOURS. DEFERRED REPAIR PER S/B A 300-54-068 PAGE 9 AND 10 AND GMM AND 3.5 INSPECT EVERY 200 FLIGHT HOURS AND REPAIR BEFORE 500 FLIGHT HOURS. 2L72 4F RTA35EU 20040323000092004032300009SW 2004 3 23 HEEA092745 120040125A6520406040400119FM GEARBOX CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C47B GL TAIL ROTOR CORRODED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03496PH3293 53398 REMOVED DUE TO EXCESSIVE CORROSION ON MAIN HOUSING IN AREA AROUND CHIP PLUG, AIR BREATHER VENT AND AT HOLES WHERE SAFETY WIRE IS ATTACHED TO HOUSING. GEARBOX WAS OVERHAULED AT T.T. 2575.00 ON FORM TRACKING AND W/O BH2122TN. SEND GEARBOX TO MFG FOR WARRANTY REPAIR DUE TO IMPROPER SURFACE PREPARATION WHEN IT WAS OVERHAULED AT A MFG OVERHAUL AND REPAIR FACILITY. RETURNED ON RO0056646. REFERENCE: MFG DMR NR 755847. 1Q71 3R3 U 2A6 E1GL 20040323000212004032300021EU 2004 3 23 BAQA092580 120040204A73321130021089 PRESSURE SWITCH AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL FUEL SYSTEM FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03652PM2 5179 PRESSURE SWITCH ONLY LASTED 1.5 HOURS REPLACED WITH SERVICABLE UNIT. 02/10/2004 1G72 3U3 U H11EU E4CE 20040323000222004032300022GL 2004 3 23 BAQA092581 220040204A732080030G VALVE AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL FUEL SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03652PM2 5179 VALVE ONLY LASTED 1.5 HOURS. SCRAPED ON SITE REPLACED WITH SERVICABLE UNIT. 02/10/2004 1G72 3U3 U H11EU E4CE 20040323000262004032300026EU 2004 3 23 BAQA092604 120040213A6321L635M1025229 BRAKE DISC UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR CHATTERING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME500 0009 BRAKE DISC PRODUCING EXCESSIVE CHATTER WHILE BRAKE APPLIED. REPLACED WITH SERVICABLE UNIT. 02/16/2004 1G72 3U3 UO H88EU E42NE 20040323000282004032300028EU 2004 3 23 BAQA092613 120040205A212119A2772 BLOWER BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE VENT FAN INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY657 7544 BLOWER INOPERATIVE, FAN ROTATES INTERMITTENTLY. REPLACED WITH SERVICEABLE UNIT. 02/13/2004 1G72 3U3 UNCH13EU E19EU 20040323000322004032300032EU 2004 3 23 BAQA092676 120040212A212119A2772 BLOWER BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE VENT FAN FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC 7517 BLOWER FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 02/12/2004 1G72 3U3 UNCH13EU E19EU 20040323000332004032300033 2004 3 23 BAQA092485 420040130A3160L316M30C1004 DISPLAY UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE COCKPIT INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH102 0069 CENTRAL DISPLAY UNIT INTERMITTENTLY BLACKS OUT WHEN POWER TURNED ON. REPLACED WITH SERVICABLE UNIT. 02/13/2004 1G72 3U3 UO H88EU E42NE 20040323000382004032300038EU 2004 3 23 I05R092764 120040115A6330L633M2010101 MOUNT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE M/R GEARBOX FAILED E I05RO OTHER O OTHER NRNOT REPORTED 1 WP07551BA1521 188 MAIN ROTOR GEARBOX MOUNT FAILED. REPLACED MOUNT. 1G72 3U3 UO H88EU E42NE 20040323000402004032300040EA 2004 3 23 SIMA200405001 120040217A33102LA00691307 LIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT SHORTED A SIMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21510AE 10105 LIT - FLT 3774 - DURING CRUISE FLIGHT, THE CRWE REPORTED SMOKE IN THE COCKPIT COMING FROM THE CAPTAINS FLOODLIGHT. FLOODLIGHT STOPPED SMOKING WHEN IT WAS TURNED OFF. MAINTENANCE REPLACED THE FLOODLIGHT IAW CRJ MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20040323000422004032300042EA 2004 3 23 ASOA04068 120040126A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE FORWARD PASSENGER AND SERVICE DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000432004032300043EA 2004 3 23 ASOA04080 120040131A5340 ATTACH BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INBOARD FLOORBEAM INTERCOSTAL ATTACH CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD FLOORBEAM INTERCOSTAL ATTACH CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-20. (M) 2L72 4F RTA21EA 20040323000442004032300044EA 2004 3 23 ASOA04077 120040130A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE TOP AND LOWER STEPS ON THE PASSENGER DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP AND LOWER STEPS ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040323000452004032300045EA 2004 3 23 ASOA04078 120040130A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE CARGO THRESHOLD FLOOR LANDING PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE REPAIRED THE CARGO THRESHOLD FLOOR LANDING PLATE IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20040323000462004032300046EA 2004 3 23 ASOA04085 120040202A7500 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA BLEED SYSTEM MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11877AS 7579 FLT 4582 - DURING CRUISE FROM ABE-ATL, AT APPROXIMATELY 28,000 FEET THE CREW RECEIVED A LEFT 14TH STAGE DUCT RED EICAS MESSAG FOLLOWED BY A TRIPLE CHIME AND MASTER WARNING, THEN RETARDED THE LT THRUST LEVER SLIGHTLY. IMMEDIATELY PRIOR TO INITIATING QRH PROCEDURES THE MASTER WARNING EXTINGUISHED. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW RETARDED THE LT THRUST LEVER TO IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO RIC, LANDING SAFELY. MAINTENANCE RESET THE LEFT BLEED CONTROL UNIT, BLEED LEAK TEST CIRCUIT BREAKERS AND PERFORMED A POWER RUN WITH NO MESSAGES APPEARING NOR ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040323000472004032300047EA 2004 3 23 ASOA04079 120040131A5340601R3111358 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11853AS 7374 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD FLOORBEAM CLIP AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLOORBEAM CLIP AT FS 280, RBL 9 IAW SRM 51-42-21. (M) 2L72 4F RTA21EA 20040323000492004032300049EU 2004 3 23 ASOA04071 120040128A3350301162 LENS AEROSPATR72 ATR72 EU EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11630AS 336 DURING HANGAR MAINTENANCE IN MCN, THE FLOOR EMERGENCY EXIT FLOOD LIGHT LENS AT THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY EXIT FLOOD LIGHT LENS AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040323000522004032300052EU 2004 3 23 ASOA04064 120040125A33501011309111 LIGHT AEROSPATR72 ATR72 EU ROW 5 INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11643AS 413 DURING A HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT STRIP AT ROW 5 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AND WIRING (P/N M22759/41-24-9) AT ROW FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040323000552004032300055EU 2004 3 23 USAASA04015 120040214A3397D9299200900000 WIRE HARNESS AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19117UW 1224 TPA - THE EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 21 LT. MAINTENANCE REPLACED THE SEAT HARNESS. OPERAITONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040323000582004032300058EA 2004 3 23 ASOA04066 120040126A5210601R3198067 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11702EV 10035 DURING A C-CHECK IN MCN, THE BOTTOM PASSENGER DOOR STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM PASSENGER DOOR STEP. (M) 2L72 4F RTA21EA 20040323000642004032300064EA 2004 3 23 ASOA04065 120040125A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 DURING A C-CHECK IN MCN, THE PASSENGER DOOR FRAME SILL AT FS 340 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FRAME SILL AT FS 340 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040323000672004032300067NM 2004 3 23 UPS04442039 120040301A531165B04349152 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:C AFT OF BULK CARGO COMPT- RT STA 2240 FRAME CRACKED BETWEEN STR R38 & STR R40 AREA. AFT OF BULK CARGO COMPT - RT STA 2240 FRAME STR 35R TO STR 40R REPLACED AS PER RS R53-62-35127 AND ENGINEERING FILE 747-53-20173. 2L74 4F RTA20WE 20040323000682004032300068NM 2004 3 23 UPS04442040 120040318A3350 LIGHT BOEING747 747123 1384873NM EMERGENCY SIGN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE DOOR INOP. REMOVED POWER PACK JPV 95678. REPLACED CREW SERVICE DOOR EMERGENCY EXIT SIGN BATTERY PACK PER MM 33-51-00. TESTS GOOD. 2L74 4F A20WE 20040323000692004032300069WP 2004 3 23 AALA20040356 120040315A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21516AM 49893 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FORWARD OF EMERGENCY OVERWING EXIT INOPERATIVE. REPLACED BOTH BATTERY PACK CHARGER MODULES FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FORWARD OF EMERGENCY OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040323000702004032300070NM 2004 3 23 AALA20040360 120040316A3350 BATTERY PACK BOEING757 757223 1384957NM FUSELAGE INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21631AA 24589 DFW - EMERGENCY EXIT LIGHT IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040323000722004032300072EU 2004 3 23 AALA20040361 120040312A5310 BEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2114056 463 TUL CRACK IN LOWER OUTBOARD FLANGE OF THE LEFT HAND GANTRY BEAM NR 4 AT FRAME 53. CRACK LENGTH IS 1.500 INCH. REPAIRED ACCORDING TO AIRBUS REPAIR TD 942.029285.004.2004, ISSUE B, DATED 10 MAR 2004 AND ESO 30595 DATED 12 MAR 2004. 2L72 4F RTA35EU 20040323000732004032300073WP 2004 3 23 ABXA040103 120040302A53205956034535 SUPPORT DOUG DC9 DC941 302207NWP SEAT TRACK CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 427 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20040323000742004032300074WP 2004 3 23 ABXA040104 120040302A53205956034535 SUPPORT DOUG DC9 DC941 302207NWP CARGO TRACK CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 365 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20040323000752004032300075WP 2004 3 23 ABXA040105 120040302A532029223681 BRACKET DOUG DC9 DC941 302207NWP SEAT TRACK CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 237 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040323000772004032300077WP 2004 3 23 ABXA040097 120040310A533059114003 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 FUSELAGE SKIN CRACKED AT LEFT AFT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED LEFT SKIN CRACK IAW DC-9 SRM 53-05. 2L72 4F A6WE 20040323000792004032300079WP 2004 3 23 ABXA040106 120040303A5755991574657 SUPPORT DOUG DC9 DC941 302207NWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 LEFT OUTBOARD SPOILER OUTBOARD SUPPORT TEE WAS CRACKED. REPLACED SUPPORT TEE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040323000802004032300080WP 2004 3 23 ABXA040099 120040301A571159113581 SPAR DOUG DC9 DC941 302207NWP LT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 ANGLE EXFOLIATED AND BULGED UPPER AFT FLANGE OF REAR SPAR UPPER TEE JUST OUTBOARD OF TRUNNION. REPLACED TEE ANGLE XRS 111.00 LEFT WING IAW DC-9 SRM. 2L72 4F A6WE 20040323000822004032300082NM 2004 3 23 UPS04442020 120040302A5313 STRINGER CLIP BOEING747 747SR46 1384816NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT - RT STA 2240 STRINGER 46 TIE CLIP FOUND CRACK. DEFECTIVE AREA STRINGER TIE CLIP REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F RTA20WE 20040323000862004032300086WP 2004 3 23 UPS04842028 120040312A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01807UP 46007 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01. 2L74 4F RT4A25 20040323000892004032300089NM 2004 3 23 UPS04242036 120040316A33501000679 LIGHT BOEING727 72725C 138400HNM FWD ENTRY INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01948UP 19357 FWD ENTRY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS. 2L73 4F A3WE 20040323000902004032300090WP 2004 3 23 UPS04842029 120040303A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:C2 STATION 1753 LONG 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION, INSTALLED STRAPS AND SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040323000912004032300091WP 2004 3 23 UPS04842030 120040302A5330 SKIN DOUG DC8 DC871F 302199DWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, FUSELAGE SKIN IS CRACKED AT STATION 1730 LONG 8L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040323000922004032300092WP 2004 3 23 UPS04842031 120040303A53403641126501 SUPPORT FITTING DOUG DC8 DC871F 302199DWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, STATION 780 FLOORBEAM SUPPORT FITTING IS CRACKED AT XC46R. REMOVED AND REPLACED FITTING IAW DWG 3641126 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040323000962004032300096SO 2004 3 23 C2XA04BT034 120040313A3234745550 LEVER EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716561 145610 CREW REPORT, LANDING GEAR FAILED TO RETRACT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. OPS CHECKED GOOD IAW EMB145 MM 32-32-02 AND 32-30-00. 2L72 4T RTT00011AT 20040323000982004032300098SO 2004 3 23 C2XA04BT037 120040315A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714543 145553 DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND THE LEFTHAND AND RIGHTHAND OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY POWER SUPPLY BOX IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040323000992004032300099SO 2004 3 23 C2XA04BT035 120040313A3350 CONTROL PANEL EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 CREW REPORTED, EMERGENCY LIGHTS WOULD NOT ARM, MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED COCKPIT CONTROL PANEL AND OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040323001032004032300103NM 2004 3 23 CALA0400249 120040317A573065C26272 SKIN BOEING737 737524 1384721NM WING DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713665 28926 INSPECTION FOUND LEADING EDGE SKIN UNDER NR 6 SLAT DENTED. A HOT BOND REPAIR WAS PERFORMED IAW SRM 51-70-04. 2L72 4F RTA16WE 20040323001042004032300104 2004 3 23 CALA0400250 420040317A2565 BOTTLE BOEING737 737524 1384721NM ESCAPE SLIDE DISCHARGED A CALAK NONE O OTHER ININSP/MAINT 1 SW271466843048 28928 INSPECTION FOUND R-2 DOOR SLIDE BOTTLE PRESSURE LOW. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-60. 2L72 4F RTA16WE 20040323001052004032300105NM 2004 3 23 P5CA0401057 120040311A7830 WARNING LIGHT BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE THRUST REVERSER ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23921FT 21575 686166 N4 T/R ARMED LIGHT ON DURING TAXI. OPENED MEL 78-06-A, CONFIRMED REVERSER STOWED. 2L74 4F4 F A20WE E3NE 20040323001062004032300106EU 2004 3 23 MALA040257 120040313A214013051002 HEATER SAAB SF340 340B 7860101EU CABIN ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15423XJ 340B423 CABIN AUX HEAT HAS AN ELECTRICAL BURNING ODOR. REMOVED AND REPLACED MID HEATER P/N 1305100-2, S/N ON 527, S/N OFF 131R, IAW AAR OKLAHOMA CMM OPS CHECK GOOD. REMOVED FROM DMR MXC NOTIFIED 4632. 2L72 4T RTA52EU 20040323001072004032300107EU 2004 3 23 MALA040253 120040309A2560P4010021 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU FLASHLIGHT DISCHARGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15513XJ E2329 FWD F/A EMERGENCY FLASHLIGHT IS NOT BLINKING. REMOVED AND REPLACED BATTERY PACK P/N P4-01-0021. OPS CHECK GOOD. 2H74 4F RTA49EU 20040323001082004032300108EU 2004 3 23 MALA040256 120040314A3350 COVER SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISLODGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15412XJ 340B412 ROW 1D EMERGENCY COVER OVER HANDLE FELL OFF, NEEDS TO BE RE-SAFTIED. RE-SAFTIED RIGHT FWD EMERGENCY EXIT DOOR HANDLE AS REQUIRED, SEC CHECKS GOOD. 2L72 4T RTA52EU 20040323001092004032300109EU 2004 3 23 MALA040259 120040312A3230 SELECTOR VALVE BAC 146 AVRO146RJ85A1500097EU MLG FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15533XJ E2367 GREEN SYSTEM HIGH TEMP LIGHT CAME ON INFLIGHT. AIR RETURN TO MEM. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW 32-30-17-05. LEAK CHECKS AND BLEED DOWN LEAK CHECKS GOOD. 2H74 4F RTA49EU 20040323001102004032300110EU 2004 3 23 MALA040258 120040312A3260GF4 RELAY BAC 146 AVRO146RJ85A1500097EU MLG INTERMITTENT A MALAO OTHER P NO WARNING INDICATION LDLANDING 1 GL15520XJ E2345 RIGHT MAIN GEAR LIGHT FAILED TO ILLUMINATE DURING FLIGHT WITH GEAR SELECTED DOWN. INDICATOR ILLUMINATED UPON LANDING. UNABLE TO DUPLICATE PIREP. REPLACED RELAY SOCKET FOR RELAY GF4 AND INSTALLED ORIGINAL GF4 RELAY COMPLETED NUMEROUS GEAR SWINGS IN HANGAR WITH NO DEFECTS. COMPLETED OPS TESTS OF LANDING GEAR PER AMM 32-30-00501. OPS CHECKS GOOD. 2H74 4F RTA49EU 20040323001112004032300111NE 2004 3 23 MALA040252 220040310A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MAKING METAL A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15443XJ 340B443 GEE785798 RIGHT CHIP DETECTOR LIGHT ILLUMINATED. AIR RETURN TO DTW. SFWI FOR REVIEW OF CHIP MATERIAL FOUND ON RIGHT ENGINE. PENDING LAB RESULTS AND ON SFWI FOR 40 FLT HOURS. MX REPLACED ENGINE. 2L72 4T4 TRTA52EU E8NE 20040323001122004032300112NM 2004 3 23 2004F00081 120040317A2530BS0063 COUPLER BOEING717 717200 1383700NM COFFEEMAKER INSTALLED B O OTHER O OTHER NRNOT REPORTED 1 SO15797 13124 MOD-16 (OPTO COUPLER) BEING INSTALLED BY MANUFACTURER. FOUND IT INCORRECTLY WIRED, CAUSING THE OVERTEMP PROTECTION CIRCUIT TO BECOME INOPERATIVE. 2L72 4F TRA6WE 20040323001142004032300114SO 2004 3 23 C2XA04SH170 120040317A532014524131007 SUPPORT BRACKET EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040323001162004032300116SO 2004 3 23 C2XA04TY052 120040317A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714558 145598 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND UNDER THE CARGO DOOR PROTECTIVE PLATE. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB-145 SRM 51-40-02 AND AMM-21-31-00. 2L72 4T RTT00011AT 20040323001172004032300117SO 2004 3 23 2XA04SH171 120040317A531514521721009 STRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714972 145151 SHV - DURING C-CHECK THE LEFT FORWARD DIGITAL STRAP FROM FRAME 15 TO FRAME 16.5 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040323001182004032300118EU 2004 3 23 MALA040266 120040312A3020 THERMISTER SAAB SF340 340B 7860101EU LT INTAKE HEAT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15412XJ 340B412 LEFT INTAKE HEAT CYCLES ON/OFF INFLIGHT. AIR RETURN TO DTW. MX SWAPPED LEFT NORMAL THERMISTER TO NR 4 RAN FOR 20 MIN, ALL CHECKS GOOD IAW MM 30. 2L72 4T RTA52EU 20040323001212004032300121WP 2004 3 23 ABXA040108 120040305A53435931960510 FITTING DOUG DC9 DC941 302207NWP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47608 FITTING CRACKED ON UPPER END OF KEEL VERTICAL SUPPORT, INBOARD OF BRAKE CONTROL VALVES. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20040323001262004032300126WP 2004 3 23 AALA20040335 120040309A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21259AA 49289 PHX - EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR EMERGENCY LIGHTS IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040323001282004032300128NM 2004 3 23 AALA20040336 120040310A3242260881211 BRAKE BOEING767 767323 1385205NM NR 5 MLG FAILED A AALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW21388AA 27448 MAN - DURING ROLLOUT, NR 5 MAIN LANDING GEAR WHEEL DEFAULTED. INSPECTION REVEALED NR 5 BRAKE REACTION PLATE SHEAR PINS FAILED AND CAUSED DAMAGE TO BRAKE AND WHEEL ASSEMBLY, INCLUDING THERMAL RELIEF PLUG CAUSING DEFLATION. REPLACED NR 5 BRAKE AND NR 5 AND NR 6 WHEELS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040323001302004032300130SO 2004 3 23 C2XA04SH169 120040317A532014524131005 BRACKET EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE PASSENGER DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040323001322004032300132EU 2004 3 23 MALA040261 120040223A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15532XJ E2366 DURING INSPECTION IN LCQ, SEAT TRACK NR 2 CORRODED FRAME 18-20. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 3/10/04. 2H74 4F RTA49EU 20040323001342004032300134EU 2004 3 23 MALA040262 120040223A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15532XJ E2366 DURING INSPECTION IN LCQ, SEAT TRACK NR 3 CORRODED FRAME 18-20. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 3/10/04. 2H74 4F RTA49EU 20040323001352004032300135SO 2004 3 23 C2XA04SH167 120040317A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER SHIM REPAIR IAW EMB 135 SRM 51-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040323001372004032300137 2004 3 23 ABXA040107 420040312A221057553865505 ACTUATOR DOUG DC8 DC863F 302198FWP YAW DAMPER BYPASSING A ABXAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL23811AX 46113 ON CLIMBOUT, THE AIRCRAFT EXPERIENCED A VIOLENT LATERAL FLUTTER. THE AUTOPILOT WAS OFF, YAW DAMPER ENGAGED. THE YAW DAMPER WAS DISENGAGED BY PILOT WITH NO NOTEABLE DIFFERENCE. DEPOWERED THE RUDDER HYDRAULICS AND THE FLUTTER STOPPED. FURTHER TROUBLESHOOTING VERIFIED THE RUDDER IN THE POWERED MODE CAUSED THE PROBLEM. ON PREFLIGHT, THE HYDRAULIC PRESSURE WITH AILERON AND RUDDER POWER OFF WAS 2920 PSI. WITH THE AILERON AND RUDDER POWER ON, THE PRESSURE WAS 2670 PSI. MAINTENANCE FOUND THE RUDDER HYDRAULIC POWER PACK BYPASSING FLUID. REPLACED THE RUDDER HYDRAULIC POWER PACK IAW DC8 MM 27-21-06. 2L74 4F 4A25 20040323001382004032300138NM 2004 3 23 DHL2004750008 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, UPPER CABIN RT SIDE BS 500 BETWEEN STR 17R AND 16R DENTED. CUT OUT DAMAGE AREA DIM 1 X .75 INCH IAW B727 SRM 51-40-3 FIG 1. FABRICATED DOUBLER REPAIR FROM MAT 7075-T6 .063 PO 900166 DIM 9 X 3.75 INCH IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR UPPER CABIN RT STA 500 BETWEEN STR 16R AND 17R IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040323001392004032300139NE 2004 3 23 DXTA200400265 220040315A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07305QS 5600261 ON TAKEOFF ROLL, THE RIGHT ENGINE N1 WAS 1/2 PERCENT BELOW TARGET, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20040323001402004032300140NM 2004 3 23 UPS04442012 120040226A5330 SEAL BOEING747 747SR46 1384816NM FUSE TO VERTICALCHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:C EMP AFT FUSELAGE TOP SKIN LT SIDE VERT FIN SEAL INTERFACE AREA FOUND MINOR CHAFE MARK FROM BS 2284-2360. BS 2284-2360 SKIN WEAR DAMAGE AREA SMOOTHED OUT AS PER SRM 51-10-01 & REPROTECTED AS PER SRM 51-10-02 WITHIN SRM 53-30-01 FIG 1. FLAGNOTED & EO 5330-18431-A ITEM 8 ALLOWABLE DAMAGE LIMITS. EXCEPT BS 2300-2320 & BS 2330-2360 EXCEEDED LIMITS. SKIN REPAIR C/O AS PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REPEAT INSPECTION REQ PER SRM 53-30-03 FIG 1 SHT 13. 2L74 4F RTA20WE 20040323001412004032300141NM 2004 3 23 UPS04542015 120040221A5310 SHEAR WEB BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01409UP 23731 INSPECTION TYPE: C3, CORROSION BS 1681 LBL 50 WL 208, CORROSION UPPER SURFACE OF SHEAR WEB. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER, ALL WORK DONE IAW SRM 51-70-13, 51-40-02 AND SRM 53-00-91 FIG 101. 2L72 4F RTA2NM 20040323001422004032300142WP 2004 3 23 UPS04842009 120040302A53133754473501N FITTING DOUG DC8 DC871F 302199DWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, LONGERON 31L SPLICE FITTING IS CRACKED BETWEEN STA 1260-1280. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D, 53-1-0. 2L74 4F RT4A25 20040323001432004032300143WP 2004 3 23 UPS04842010 120040303A5310 SHEAR TIE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:C2 STATION 1600 SHEAR TIE IS CRACKED BETWEEN LONGERONS 28L-29L. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2A. 2L74 4F RT4A25 20040323001442004032300144WP 2004 3 23 UPS04842011 120040302A5512 SKIN DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, RIGHT HORIZONTAL STAB L/E SKIN HAS INTERGRANULAR CORROSION AT XFS 178.750. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20040323001452004032300145WP 2004 3 23 UPS04842013 120040303A5313 LONGERON DOUG DC8 DC871F 302199DWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE: C2, STA 1733 LONG 14L IS CRACKED. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040324000012004032400001EU 2004 3 24 MALA040255 120040312A2750 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU TE FLAPS ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15521XJ E2346 FLAP FAULT 5 MINUTES AFTER FLAPS WERE BROUGHT UP. FLAP FAULT ILLUMINATED UNABLE TO RESET WITH POM PROCEDURE. AIR RETURN TO MSP. PER 27-50-00 RESET FLAPS RAN SYSTEM THRU 20 TIMES, NO FAIL. GREASED ALL 4 SCREW JACK BALLS AND OHM METER CHECKED SYSTEM WITH BREAKOUT BOX, ALL OHMS CHECKS GOOD. RAN SYSTEM ADDITIONAL CYCLES, OPS CHECKS GOOD. 2H74 4F RTA49EU 20040324000112004032400011WP 2004 3 24 MEX2004052 120040211A3150H05A00354 WARNING SYSTEM DOUG DC9 DC982 3022082WP CAWS FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW231003Y 48068 FLT 278 - MEX-CJS - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURNIG PUSH-BACK APU SHUTOFF AND APU FIRE, OVERSPEED, AND TAKEOFF ALARMS WERE ACTIVATED. AT PLATFORM, ALARM SYSTEM (CAWS) WAS RESET BUT FAIL CONTINUED. IT WAS REPLACED AND TESTED IAW MM 31-51-01, ALL CORRECT. DURING OVERNIGHT SERVICE, ALARMS SYSTEM WAS TESTED IN CAWS COMPUTER IAW MM 31-50-00, 31-51-01, ALL CORRECT. ADDITIONALLY FIRE DETECTION SYSTEM WAS TESTED IAW MM 26-00-00, ALL CORRECT. APU WAS OPERATING CORRECT IAW MM 49-00-00. (M) 2L72 4F A6WE 20040324000172004032400017WP 2004 3 24 MEX2004068 120040219A2420947F9453 GCU DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23838AM 49397 P718196 FLT 909 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE GENERATOR FAIL. THE APU WAS DEFERRED PREVIOUSLY SO THE GCU AND BCU WERE REPLACED BUT FAIL CHANGE TO LT ENGINE INDICATION. APU TRIM WAS ACCOMPLISHED AND IT WAS OPERATIVE. THE GCU WAS DEFERRED IAW MEL 24-1. DURING TRANSIT CHECK AT CUN STATION, THE GENERATOR WAS REPLACED IAW MM 24-20-07, TEST CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20040324000212004032400021NE 2004 3 24 MEX2004054 220040211A7230815331 BLADE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT ENGINE DAMAGED A K NONE C F.O.D. ININSP/MAINT 1 SW23160PL 49763 DURING TRANSIT CHECK IT WAS DETECTED LT ENGINE FAN BLADE WITH DAMAGE. DAMAGE WAS 4 INCHES DOWN OF THE BLADE ROOT ON THE ATTACH BORDER WITH /75 INCH LARGE AND .240 WIDE AN IT WAS BROKEN. BOROSCOPIC INSPECTION WAS PERFORMED ON 6 AND 7 STAGES BEING ALL CORRECT. BLADES SET WAS REPLACED IAW, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20040331000502004033100050NM 2004 3 31 SWAA040879 120040323A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29755SA 27871 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040331000542004033100054NM 2004 3 31 SWAA040849 120040321A53156546540 FLOORBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SPV, FOUND FLOORBEAM TOP CHORD AT BS 988, BL 0 TO RBL 45, WL 208 CORRODED. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F A16WE 20040331000622004033100062NM 2004 3 31 SWAA040902 120040326A5510 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT UPPER THRUST FITTING, UPPER AND LOWER ATTACH LUGS CORRODED. REPAIRED HORIZONTAL STAB PER ER. 2L72 4F RTA16WE 20040331000642004033100064 2004 3 31 SWAA040853 420040321A256565C19901 CABLE BOEING737 737301 1384611NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED 1/2D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040331000702004033100070NM 2004 3 31 SWAA040845 120040320A53106547973 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 985, RBL 49, WL 207, CORRODED. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040331000742004033100074NM 2004 3 31 SWAA040830 120040318A53156545815 FLOORBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SPV, FOUND FLOORBEAM AT BS 344, LBL 49, WL 208, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F A16WE 20040331000762004033100076NM 2004 3 31 SWAA040832 120040318A531265C28106 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SPV, FOUND PRESSURE BULKHEAD AT BS 1016, BL 0, CORRODED. REPAIRED PRESSURE WEB PER BOEING DRAWING. 2L72 4F A16WE 20040331000772004033100077NM 2004 3 31 SWAA040833 120040318A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SPV FOUND FUSELAGE SKIN AT BS 780, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040331000832004033100083NM 2004 3 31 SWAA040839 120040318A57436549442 FITTING BOEING737 7373Y0 1384671NM RT MLG CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D CHECK, FOUND RT MLG BEAM FITTING AT 5 O'CLOCK POSITION CRACKED. REMOVED AND REPLACED BEAM FITTING PER ER. 2L72 4F RTA16WE 20040331000912004033100091NM 2004 3 31 SWAA040862 120040322A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT BS 835, STRINGER 25L, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040331000922004033100092NM 2004 3 31 SWAA040863 120040322A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB AT BS 1016, STRINGER 6R, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040331000942004033100094NM 2004 3 31 SWAA040865 120040322A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331000962004033100096NM 2004 3 31 SWAA040867 120040322A335007912 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED MV2 CHECK, FOUND EEPLS FWD END CAP BROKEN. REMOVED AND REPLACED EEPLS END CAP PER MM. 2L72 4F RTA16WE 20040331000972004033100097NM 2004 3 31 SWAA040885 120040324A32601899 PROXIMITY SENSOR BOEING737 7373H4 1384600NM LT MLG FAULTY A SWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW29316SW 23338 LT MLG UNSAFE LIGHT ILLUMINATED. RECYCLED GEARS, NO HELP. REMOVED AND REPLACED LT MLG UPLOCK PROX SWITCH. OPS CK GOOD PER MM. 2L72 4F RTA16WE 20040331000982004033100098NM 2004 3 31 SWAA040886 120040325A3350101114 LENS BOEING737 7373Q8 1384670NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 LT AFT GALLEY AREA EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20040331000992004033100099NM 2004 3 31 SWAA040887 120040325A53306545769 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL A/C DOOR CUTOUT, FWD RT CORNER. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040331001002004033100100NM 2004 3 31 SWAA040888 120040325A53306552988 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 983, STR 21L, AND BS 947, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040331001022004033100102NM 2004 3 31 SWAA040893 120040325A551265C25727 SKIN BOEING737 7373A4 1384585NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB LOWER SKIN CRACKED AT IN SPAR STA 125. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040331001102004033100110NM 2004 3 31 04FDEA00741 120040324A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 LEFT WING TO FUSELAGE AT STA Y= 1491, LONGERON SPLICE FOUND CRACKED. LT WING TO FUSELAGE AT STA Y= 1491, CRACKED LONGERON SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER SRM 53-10-00 VOL 1 FIG 2 2L73 4F RTA22WE 20040331001122004033100112NM 2004 3 31 SWAA040896 120040325A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 480, STR 26L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040331001162004033100116NM 2004 3 31 04FDEA00643 120040312A5711ARB7411 SPAR DOUG MD11 MD11 3023602NM RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING - DURING ACCOMPLISHMENT OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGE TENSION STRAP SUPPORT REPLACEMENT, FOUND 2 EACH EXISTING HOLES OVERSIZED. REPAIR CARRIED AT RIGHT WING 2 EA EXISTING OVERSIZED HOLES OF OUTBOARD TRAILING EDGE FLAP INBOARD HINGE TENSION STRAP SUPPORT AS PER EA 1-5750-74333, WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE, TWO OVERSIZED HOLES FOUND. 2L73 4F RTA22WE 20040331001232004033100123NM 2004 3 31 04FDEA00656 120040315A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE WITH SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040331001252004033100125NM 2004 3 31 04FDEA00658 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000052004040100005 2004 4 1 USAABB04013 420040128A3460 COMPUTER BOEING767 7672B7 1385107NM FLT MANAGEMENT OUT OF ADJUST A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19651US 24764 FRA - FLT 193 - AFTER TAKEOFF, CREW NOTED THAT THE FMC'S WERE NOT UPDATING AND WERE APPROXIMATELY TEN MILES OFF IN POSITION. FLIGHT RETURNED TO FRA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REALIGNED THE IRU'S SEVERAL TIMES. BITE CHECK OF THE FMC'S WAS SATISFACTORY. (M) 2L72 4F RTA1NM 20040401000082004040100008NM 2004 4 1 USAASB04012 120040126A21317638104 CONTROLLER BOEING737 7373B7 1384580NM CABIN PRESSURE MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19385US9165 22958 PIT - FLT 385 - EN ROUTE FROM PHL-MSY, AT FL250, THE CABIN ALTITUDE BEGAN TO CLIMB MODERATELY. FLIGHT DESCENED TO 10,000 FEET WHERE CABIN WAS REGAINED. FLIGHT THEN DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE ACCOMPLISHED FUNCTIONAL TEST OF CABIN PRESSURE CONTROLLER. CONTROLLER FAILED STEP NR 12 OF TEST FOR LOW VOLTAGE. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. FUNCTIONAL TESTE AND OPERATIONAL TEST GOOD. (M) 2L72 4F RTA16WE 20040401000142004040100014NM 2004 4 1 USAABB04010 120040122A3350873100151REV12 LIGHT BOEING757 7572B7 1384964NM ROWS 23 & 33 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19628AU 27806 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 23 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. (M) 2L72 4F RTA2NM 20040401000562004040100056 2004 4 1 REXA04005 420040208A2562 G SWITCH CNDAIRCL600 CL6002B19 1900309EA ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258858D 01440 7858 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. MANUFACTURER HAS RECEIVED THE UNIT AND CONFIRMED A 'STICKING' G-SWITCH. THIS FAILURE IS THE 8TH OCCURRENCE OF THIS MODEL ELT FAILING THE G-SWITCH TEST ON ITS FIRST 12 MONTH INSPECTION. (M) 2L72 4F RTA21EA 20040401000592004040100059EA 2004 4 1 A6WA20040020 120040206A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 GL31403AW 7288 FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. (M) 2L72 4F RTA21EA 20040401000662004040100066NM 2004 4 1 AMTA200400113 120040127A5321 FLOOR PANEL BOEING757 75733N 1384931NM CARGO BAY CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11559TZ 32593 C2 PIT FLOOR PANEL HAS CORROSION FROM STATION 1330 TO 1200 RBL 20 TO LBL 20. CORROSION OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED NEW CARGO FLOOR PANEL IAW SRM 51-40-02-0 AND AMM 25-50-04-404-004. 2L72 4F RTA2NM 20040401000742004040100074NM 2004 4 1 SWAA040908 120040327A53126546568 BULKHEAD BOEING737 7377H4 1384404NM FUSELAGE CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29777QC 30592 DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD BETWEEN STRINGERS 3L AND 4L, OIL CANNED. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20040401000802004040100080NM 2004 4 1 04FDEA00649 120040315A2750 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401000972004040100097NM 2004 4 1 04FDEA00640 120040310A2170 COALESCER BAG BOEING727 727200 138407ENM CABIN AIR CONTAMINATED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25481FE 21463 AT FL310, 1 HOUR AFTER LEVEL-OFF, THE ENTIRE CREW AND JUMPSEATER NOTICED AN OBVIOUS ODOR OF SMOKE. ACCOMPLISHED EMERGENCY DESCENT AND LANDING. NO FURTHER SMOKE DETECTED AFTER LANDING, NORMAL SHUTDOWN. FAINT SMELL AGAIN NOTED, SEEMED TO BE FROM C/B PANELS IN LEFT REAR OF COCKPIT. FIRE CREW ALSO NOTICED A FAINT ODOR. NO CARGO OR APU OR FIRE SMOKE OR FIRE WARNING WENT OFF. ODOR WAS STRONGEST BEHIND AND RIGHT OF F/O BEHIND ENGINEERS PANEL. RAN APU WITH BOTH PACKS, RAN ENGINES WITH BOTH PACK PER JRH CHAPTERS 5 & 7. SMELLED MORE LIKE DEICING FLUID, CHANGED OUT COALESCER BAG PER REF 21-55 -051-4, ODOR HAS DISSIPATED, OK FOR RETURN TO SERVICE. 2L73 4F RTA3WE 20040401001302004040100130WP 2004 4 1 AALA20040358 120040317A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21468AA 49598 DFW - SEAT MOUNTED EMERGENCY LIGHT IN FORWARD SECTION ARE DIM. REPLACED NUMBER ONE CONTROL MODULE AND BATTERY AND REPLACED NUMBER TWO BATTERY FOR SEAT MOUNTED EMERGENCY LIGHT IN FORWARD SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040406000042004040600004NM 2004 4 6 04FDEA00789 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIRED. 2L73 4F RTA22WE 20040406000062004040600006NM 2004 4 6 04FDEA00791 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2L73 4F RTA22WE 20040406000082004040600008NM 2004 4 6 CALA0400313 120040403A5320143A987350 ANGLE BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND L-ANGLE STIFFENER FOR THE SUPPORT BULKHEAD PANEL CAMLOCK RAIL CORRODED AT STA 500I. THE L-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406000102004040600010NM 2004 4 6 04FDEA00778 120040330A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25619FE 48770 RT WING I/B FLAP I/B SIDE LOAD ROLLER FITTING ATTACHMENT IS CRACKED AT BASE RADIUS. REMOVED AND REPLACED R/H WING SIDELOAD ROLLER FITTING IAW M/M 20-50-02-2. 2L73 4F RTA22WE 20040406000162004040600016NM 2004 4 6 04FDEA00779 120040330A5712 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 16 FOUND CRACKED. LT WING LEADING EDGE RIB AT SLAT TRACK NR 16 REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. 2L73 4F RTA22WE 20040406000232004040600023NM 2004 4 6 04FDEA00787 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000252004040600025NM 2004 4 6 04FDEA00684 120040320A3230 CONTROL CABLE BOEING727 727200 138407ENM MLG OUT OF RIG A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25205FE 22927 WHEN GEAR HANDLE WAS SELECTED TO OFF POS AFTER GEAR RETRATION, ALL UNSAFE LIGHTS ILLUMINATED AND GEAR EXTENDED UNCOMMANDED. GEAR HANDLE WAS SELECTED TO DOWN POS AND ALL SAFE LIGHTS ILLUMINATED. PUT A/C ON JACKS PER 727 AMM 07-11-000-2. DURING GEAR RETRACT, DUPLICATED THE PILOT WRI. FOUND LANDING GEAR CONTROL CABLES LGVB AND LGVA OUT OF RIG, SO RIG PIN WILL NOT LINE UP WITH RIG HOLE IN BEARING RETAINER (ABOUT A .5 INCH OFF) SEE REF: AMM 32-31-000-5, FIG 502 SHEET 1. ADJ/ RIG PER 727 AMM 32-31-000-5, PERFORM GEAR RETRACTION. 2L73 4F RTA3WE 20040406000292004040600029NM 2004 4 6 04FDEA00688 120040322A5314 KEELBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 CORROSION ON LEFT KEELBEAM STA 950F 12 O/B FLANGE. REMOVED CORROSION FROM LEFT KEEL BEAM AT BS 950F 12 INCHES O/B FLANGE. MATERIAL LOSS WAS .030 DEEP X .5 X .5 INCH FROM AN ORIGINAL THICKNESS OF .150 AND IS OUT OF LIMITS IAW FED EX SR 27-53-023-A. REPAIRED KEEL BEAM IAW FED EX SR 27-53-023A. 2L73 4F RTA3WE 20040406000322004040600032NM 2004 4 6 04FDEA00744 120040325A3260Z3200502 BRACKET DOUG MD11 MD11 3023602NM ZONE 700 BROKEN A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25617FE 48748 UNSAFE GEAR INDICATION LEFT MLG DURING GEAR RETRACTION AT 230 KTS. UPON LANDING FOUND LEFT MLG ELECTRICAL HARNESS AND BRAKE HYD HOSES SUPPORT BRACKET ATTACHMENT TO TORSION LINK DAMAGED. SUPPORT BRACKET AND WIRE HARNESS REPLACEMENT CARRIED OUT REFER TO WRI 32-10/9350 AND 32-60/9357, 32-60/9358 FOR WORK DETAILS LANDING GEAR EXTENSION AND RETRACTION CARRIED OUT AS PER MM 32-31-00, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040406000342004040600034NM 2004 4 6 04FDEA00792 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2L73 4F RTA22WE 20040406000532004040600053NM 2004 4 6 04FDEA00761 120040327A5521 RIB DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 UPON REMOVAL OF RIGHT DETACHABLE ELEVATOR LOWER INBOARD ACCESS PANEL NR 345BB FOUND STA XE53.50 LOWER INBOARD MOUNTING FLANGE CRACKED. COMPLIED WITH FEDEX EA 1-5520-75973, STABILIZERS - ELEVATORS RT INBOARD ELEVATOR RIB REPAIR. 2L73 4F RTA22WE 20040406000552004040600055NM 2004 4 6 04FDEA00763 120040326A3610 CLAMP DOUG MD11 MD11 3023602NM PNEUMATIC DUCT LOOSE A FDEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO25623FE 48794 ON CLIMBOUT BETWEEN 5000 FT AND 10,000 FT, NR 2 ENG ANTI-ICE DUCT LEVEL 3 ALERT ILLUMINATED. QRH PROCEDURES FOLLOWED, RETURNED TO KMEM. LEVEL 3 WARNING DISAPPEARS AFTER THROTTLES RETURNED TO IDLE POWER. EMERGENCY EQUIPMENT REQUESTED, LANDING UNEVENTFUL. FOUND TWO VERY LOSE PNEUMATIC DUCT CLAMPS UPSTREAM OF PRSOV, TIGHTENED. OPS CHECKS GOOD PER JRH. 2L73 4F RTA22WE 20040406000602004040600060NM 2004 4 6 04FDEA00804 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000622004040600062NM 2004 4 6 04FDEA00806 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000642004040600064NM 2004 4 6 04FDEA00808 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000672004040600067WP 2004 4 6 04FDEA00678 120040317A1430 BOLT DOUG DC10 DC1010 3022110WP ZONE 500 UNDERTORQUED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25550FE 46521 BOLT FAILED TORQUES CHECK AT POSN 556GT LT OUTBOARD FLAP VANE. MX TORQUED PER FCD REQUIREMENTS. 2L73 4F A22WE 20040406000692004040600069WP 2004 4 6 04FDEA00680 120040317A1430 BOLT DOUG MD10 MD1010F 3022112WP ZONE 600 UNDERTORQUED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25550FE 46521 BOLT FAILED TORQUE CHECK ON POS 656GT RT OUTBOARD FLAP VANE. *S/D* MX TORQUED PER FCD REQUIREMENTS. 2L73 4F RTA22WE 20040406000712004040600071NM 2004 4 6 04FDEA00810 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1 2L73 4F RTA22WE 20040406000752004040600075EU 2004 4 6 04FDEA00816 120040401A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMPARTMENT CENTER CARGO TRACK AT CENTER LINE RT SIDE BETWEEN FRAME 77 AND 78, 2 EA AREAS OF CORROSION. CUT OUT DAMAGED SECTION OF CARGO TRACK AND INSTALLED NEW SECTION IAW SRM 53-10-16. 2L72 4F RTA35EU 20040406000862004040600086NM 2004 4 6 04FDEA00698 120040323A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, ACTUATOR ROD END HOLE NR 8 OUTBOARD FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-75923, LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040406000882004040600088NM 2004 4 6 04FDEA00700 120040323A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 LT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE, LOWER MOUNT HOLE NR 7, MATING SURFACE CORRODED. LT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE, LOWER MOUNT HOLE NR 7, MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 AND DWG ARC0502 SHEET 4 ZONE 40. 2L73 4F RTA22WE 20040406000902004040600090NM 2004 4 6 04FDEA00660 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406001062004040600106 2004 4 6 SWIA200413098 420040328A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER WILL NOT TEST A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07580SW9836 9836 120348 STALL STICK SHAKER NR 1 WON'T TEST. REMOVED AND REPLACED NR 1 STICK SHAKER. OPS CHECK GOOD. 2L72 4T RTA31SO 20040406001212004040600121NM 2004 4 6 CALA0400269 120040322A5320BAC1496377X7075TCHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND LEFT Z-CHANNEL IN AFT CARGO PIT CORRODED AT STA 727B-847. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040406001232004040600123NM 2004 4 6 CALA0400271 120040324A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714242 28805 INSPECTION FOUND RIGHT Z-CHANNEL IN AFT CARGO PIT CORRODED AT STA 727D-767. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40-02 AND 53-00-53. 2L72 4F RTA16WE 20040406001392004040600139EA 2004 4 6 SWIA200413063 120040319A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07935SW 7725 RIGHT WINDOW HAS MANY CRACKS ON THE INNER LAYER. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW CRJ MM 56-12-01 AND RII CARD 56-402. OPS CHECKS GOOD. P/N OFF: 601R33033-12, S/N OFF: 02241H4773. 2L72 4F RTA21EA 20040406001502004040600150 2004 4 6 SWIA200412987 420040304A2210 COMPUTER EMB 120 EMB120ER 3260203SO NR 2 AUTOPILOT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07293SW 120320 WHEN SELECTING AUTOPILOT TO FIRST OFFICER'S SIDE, THE TRIM FAILS WITH ALL ASSOCIATED WARNINGS. RERACKED NR 2 AUTOPILOT COMPUTER. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040406001522004040600152EA 2004 4 6 SWIA200412989 120040304A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07918SW 7645 MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED BULB, OPS CHECK GOOD. 2L72 4F RTA21EA 20040407000032004040700003CE 2004 4 7 EPUA300104A 120040130A534026111447 SUPPORT CESSNA208 208B 2073701CE ZONE 200 CRACKED E EPUAO OTHER O OTHER NRNOT REPORTED 1 AL03407GV 208B0616 PILOT REPORTED WHEN RETRACTING FLAPS ON ROLL-OUT THE FLAP CIRCUIT BREAKER TRIPPED. MX INSPECTED AND FOUND THE FLAP TRANSMISSION SUPPORT ASSY. CRACKED AND BUCKLED. THERE WAS NO EVIDENCE OF THE STANDBY FLAP SYSTEM BEING ACTIVATED. 1H71 3T A37CE 20040407000052004040700005EA 2004 4 7 ASOA04177 120040304A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11900EV 7608 FLT 9773 - DURING A GROUND INSPECTION IN DFW, THE NR 2 EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EXTERIOR EMERGENCY LIGHT LAMP ON THE RIGHT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000122004040700012EA 2004 4 7 ASOA04186 120040308A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING AN A-CHECK IN BTR, THE DOUBLER AT FS 640, STRINGER L10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBELR AT FS 640, STRINGER L10 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040407000182004040700018EA 2004 4 7 ASOA04164 120040229A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11706EV5786 10054 FLT 4908 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000202004040700020EA 2004 4 7 ASOA04162 120040228A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-21. (M) 2L72 4F RTA21EA 20040407000212004040700021EA 2004 4 7 ASOA04158 120040227A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11889AS 7538 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000442004040700044NM 2004 4 7 UIEA200400019 120040219A5410 STRUT BOEING747 747243B 1384830NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, DURING ZONAL INSPECTION IT WAS DISCOVERED THAT NR 3 ENGINE PYLON STRUT PRECOOLER EXHAUST VETN WITH CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NAC STATION 235 TO STATION 254. THE RIB INSTALLATION AT NAC STATION 248 WAS MODIFIED TO ACCOMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F A20WE 20040407000502004040700050SO 2004 4 7 SIMA200407201 120040307A27413621005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZONTAL STAB MALFUNCTIONED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW21648AE 145225 ORD - FLT 4098 - PITCH TRIM EICAS WARNING CAME ON. PITCH TRIM 12 INOPERATIVE BOTH MAIN AND BACKUP TRIM INOPERATIVE. REGAINED FULL CONTROL OF PITCH TRIM AFTER COMPLETING CHECK LIST. COMPLIED WITH ETN EM-27-028 R1 AND REPLACED THE HSCU PER THE ETN. (M) 2L72 4T RTT00011AT 20040407000512004040700051EA 2004 4 7 ASOA04155 120040224A5320601R950159 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURNIG A C-CHECK IN MCN, THE UPPER SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE UPPER SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY. (M) 2L72 4F RTA21EA 20040407000522004040700052EU 2004 4 7 SIMA200407903 120040306A53117253813007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21356SB 340B356 ABI - DURING AN MBV INSPECTION, THE GALLEY FLOOR RIGHT FRAME 272 WAS FOUND CORRODED BELOW SRM LIMITS. CUT OUT SECTION OF FRAME AND FABRICATED A FILLER, DOUBLER AND FOUR SHIMS. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, CHAPTER 53-70-30 AND 51-40-21. (M) 2L72 4T RTA52EU 20040407000532004040700053EU 2004 4 7 SIMA200407904 120040317A53302024T3 SKIN SAAB SF340 340B 7860101EU ICESHIELD DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21392AE 340B392 ABI - DURING AN MBV NISPECTION, FOUND A DEN IN THE RIGHT ICESHIELD WHICH EXCEEDED SRM LIMITS. REMOVED ICESHIELD WHERE DOUBLER WAS. REMOVED DAMAGED SKIN BY CREATING A CUTOUT. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079, 53-70-10 PAGE 215, FIG 209 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040407000552004040700055EU 2004 4 7 SIMA200407908 120040311A5311725313007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21356SB 340B356 ABI - DURING AN MBV INSPECTION, THE TOP FLANTE OF THE LOWER PORTION OF FRAME 258 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED AREA OF FLANGE BY CUTOUT. REMOVED EXISTING AFT ANGLE. FABRICATED A REPAIR ANGLE AND FILLER. FABRICATED TWO TRIPLERS ALSO. REPAIR DONE IAW SAAB 340SRM, 72LKS 3079 REV 420 53-70-30 PARA 5 FIG 209. (M) 2L72 4T RTA52EU 20040407000562004040700056NM 2004 4 7 USAA040013 120040208A5313 STRINGER BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19777AU36788 24979 PIT - FOUND STRINGER CRACKED 3.5 TO 4 INCHES LONG, STATION 1138 STRINGER 5A RIGHT SIDE. REPLACED STRINGER 5A LOWER CHORD PER TR 53-80-04, EA 77840, SRM 53-00-01. (M) 2L72 4F RTA16WE 20040407000612004040700061SO 2004 4 7 SIMA200407501 120040312A2720 CONTROL UNIT EMB 145 EMB145LR 3260212SO RUDDER CONTROL MALFUNCTIONED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 SW21630AE 145132 ORD - FLT 4244 - LOST RUDDER CONTROL DURING LANDING. EICAS DISPLAYED RUDDER 1-2 SYSTEM INOPERATIVE. PERFORMED TROUBLESHOOTING PROCEDURES FOR RUDDER 1-2 INOPERATIVE IAW EMB145 FAULT ISOLATION MANUAL. PERFORMED OPERATIONAL CHECK OF RUDDER IAW EMB 145 AMM 27-23-00. NO DEFECTS NOTED. COMPLIED WITH FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040407000632004040700063EU 2004 4 7 SIMA200407906 120040310A53117253813007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21393AE 340B393 ABI - DURING AN MBV INSPECTION OF THE TOP FLANGE OF THE LOWER PORTION OF FRAME 258.0 IT WAS FOUND THAT THE PREVIOUS REPAIR WAS CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED PREVIOUS REPAIR. INCREASED THE EXISTING CUT OUT TO ENCOMPASS HOLES WITH QUESTIONABLE EDGE DISTANCE. PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED AN 'L' SHAPED FILLER, REPAIR ANGLE, AND TWO TRIPLERS. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006771 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040407000652004040700065EU 2004 4 7 SIMA200407901 120040315A3230D49412001 CONTROL PANEL SAAB SF340 340B 7860101EU COCKPIT INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 SW21393AE 340B393 CLL - FLT 3397 - CREW REPORTED NO LANDING GEAR EXTENTION WHEN GEAR WAS SELECTED DOWN INTRANSIT LIGHT CAME ON BUT NO DOWN AND LOCK LIGHTS ILLUMINATED. RECYCLED LANDING GEAR SELECTOR AND AFTER TWO ATTEMPTS GEAR CAME DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL PANEL IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040407000672004040700067EA 2004 4 7 A6WA200340209 120040104A2612356024310 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA LT ENG PYLON MALFUNCTIONED A A6WAO OTHER N FALSE WARNING APAPPROACH 1 GL31401AW12628 7280 LEFT 14TH STAGE DUCT FAIL WARNING MESSAGE IN FLIGHT. REMAINED ILLUMINATED AFTER ENGINE SHUTDOWN 45 MINUTES. REMOVED AND REPLACED LEFT 14TH STAGE LOOP PYLON, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040407000692004040700069NM 2004 4 7 2004F00090 120040223A5310 STRUCTURE AIRBUSA319 A319132 3930340NM FUSELAGE VIBRATION Z A UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO23473TA 1140 FLT TAI 410 AT SAL, DURING CLIMB EXPERIENCED A STRONG VIBRATION IN ALL AIRCRAFT. THE AIRCRAFT WAS RETURNED TO SAL STATION FOR MAINTENANCE. THE AIRCRAFT REMAINS ON GROUND FOR INSPECTION. (M) 2L72 4F RTA28NM 20040407000702004040700070NM 2004 4 7 BJNA040202 120040224A3397 WIRE BOEING737 737282 13844ATNM EMERGENCY LIGHT LOOSE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 FORWARD FLOOR TRACK LIGHTING INOPERATIVE. INSPECTED THE EMERGENCY LIGHT POWER SUPPLY FOUND WIRE PULLED FROM THE CONNECTOR, REPLACED THE POWER SUPPLY, OPS CHECK OK. (M) 2L72 4F RTA16WE 20040407000832004040700083NM 2004 4 7 USAA040005 120040101A5314 KEELBEAM BOEING737 7373B7 1384580NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU50706 23701 PIT - FOUND KEEL BEAM CHAFING 16 INCH AREA, STATION 727 FORWARD TO 711 LEFT OUTBOARD FLANGE OF LT KEEL BEAM BY FASTENERS AND PANELS. INSTALLED DOUBLERS, STRAPS AND NUTPLATES PER TYPICAL REPAIR EA 77719, T/R 53-60-05. (M) 2L72 4F RTA16WE 20040407000852004040700085NM 2004 4 7 USAASB04015 120040206A33501317 BULB BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 ORD - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT OVERHEAD BIN BULLNOSE, SEAT ROW 25L, INOPERATIVE. MAINTENANCE FOUND THE BULB OUT OF POSITION. SECURED BULB IN PLACE. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040407000872004040700087WP 2004 4 7 AALA20040394 120040326A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21589AA 53252 SEA - EMERGENCY LIGHTS ON CEILING AT ROWS 8 THROUGH 12 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON CEILING AT ROWS 8 THROUGH 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040407000892004040700089NM 2004 4 7 AALA20040396 120040328A3242 BRAKE BOEING757 757223 1384957NM MLG DRAGGING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21604AA 27055 MIA - T1550 NEAR THE V1 SPEED THE AIRCRAFT YAWED TO THE LEFT ABOUT 5 DEGREES. THE TAKEOFF WAS CONTINUED AND A NORMAL ROTATION WAS ACCOMPLISHED. LANDED AT MIA WITHOUT INCIDENT. ACCOMPLISHED SPIN CHECK OF LEFT HAND MAIN GEAR AND FOUND NUMBER ONE BRAKE DRAGGING. REPLACED NUMBER ONE BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040407000912004040700091WP 2004 4 7 AALA20040393 120040326A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21447AA 49473 DFW - EMERGENCY LIGHT ON LOWER WALL OPPOSITE FORWARD LAVATORY IS INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON LOWER WALL OPPOSITE FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407000932004040700093WP 2004 4 7 AALA20040398 120040329A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21423AA 49335 DFW - SEAT MOUNTED EMERGENCY PATH LIGHTS IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY AT FORWARD END OF AFT EMERGENCY PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407000972004040700097WP 2004 4 7 AALA20040403 120040329A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 DFW - EMERGENCY LIGHTS AT STATION 1154 INOPERATIVE. FOUND PLASTIC BACK SHELL FOR PLUG FOR BATTERY PACK CONTROL MODULE AB5-4 AT STATION 1154 BROKEN. REPLACED PLASTIC BACK SHELL FOR PLUG FOR EMERGENCY LIGHT BATTERY PACK CONTROL MODULE AB5-4 AT STATION 1154. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407000992004040700099NM 2004 4 7 AALA20040399 120040331A3350 LIGHT BOEING757 757223 1384957NM CABIN MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21696AN 26976 STL - EMERGENCY LIGHT ASSEMBLY AT SEATS 28DEF MISSING. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLIES, BACK PLATE AND SHROUD FOR SEATS 28DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040407001012004040700101WP 2004 4 7 AALA20040405 120040329A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 DFW - LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ABOVE DOORS INOPERATIVE. REPLACED BATTERY PACK B5-105, RESECURED WIRE L799B16N TO TERMINAL 3, AND CORRECTED WIRE CONNECTION L1229F18 FROM TERMINAL 3 TO TERMINAL 5 FOR LEFT HAND AND RIGHT HAND OVERWING EMERGENCY EXIT SIGN LIGHTS ABOVE DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001042004040700104NM 2004 4 7 MWEA040049 120040405A532099294807 DOUBLER BOEING717 717200 1383700NM DOOR PAN GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31902ME 55166 AFT CABIN DOOR PAN IS GOUGED ON LEFT SIDE NEAR FLIGHT ATTENDANT SEAT, BOTTOM SNUBBER. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F TRA6WE 20040407001052004040700105NM 2004 4 7 AALA20040417 120040402A335002031461201 LIGHT BOEING737 737823 13844BZNM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21918AN 29519 ORD - WALL MOUNTED EMERGENCY EXIT LIGHT FIXTURE AT SEAT 14A BROKEN. REPLACED WALL MOUNTED EMERGENCY EXIT LIGHT FIXTURE AT SEAT 14A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040407001062004040700106NM 2004 4 7 AALA20040418 120040402A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21658AA 24616 EWR - AFT AIRCRAFT EMERGENCY LIGHTS ON FLOOR, RIGHT AND LEFT HAND EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK AT M736 AND M737 FOR AFT EMERGENCY LIGHTS ON FLOOR, RIGHT AND LEFT HAND EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040407001072004040700107 2004 4 7 AALA20040419 420040402A2565D29982125 SLIDE DOUG DC9 DC982 3022082WP CABIN FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21286AA 49298 ORD - GIRT BAR CABLE LOOSE. INSPECTED SLIDE PACK AND FOUND LANYARD FOR FIRING BOTTLE PULLED. SLIDE DID NOT DEPLOY. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001122004040700112WP 2004 4 7 MWEA040047 120040331A5544591025659 BRACKET DOUG DC9 DC981 3022081WP LOWER RUDDER CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 FOUR AREAS OF CORROSION ON LOWER RUDDER BRACKET. REMOVED AND REPLACED LOWER BRACKETS. 2L72 4F A6WE 20040407001142004040700114SO 2004 4 7 MASA200400111 120040226A2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY CONTAMINATED A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07852MJ 145567 CREW RETURNED TO FIELD FOR A LAV SMOKE DETECT MSG IN-FLIGHT. DCA MX REMOVED DEBRIS FROM SMOKE DETECTOR. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040407001152004040700115SO 2004 4 7 MASA200400112 120040226A3010 WARNING LIGHT EMB 145 EMB145LR 3260212SO ANTI ICE ILLUMINATED A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07838MJ 145384 CREW RETURNED TO FIELD FOR STAB ANTI-ICE FAIL MSG ON TAKEOFF. CLT MX OP CHECKED SYSTEM. MX COULD NOT DUPLICATE DISCREPANCY. NO PARTS USED. 2L72 4T RTT00011AT 20040407001162004040700116SO 2004 4 7 MASA200400117 120040229A3620 FILTER EMB 145 EMB145LR 3260212SO FAN AIR VALVE CONTAMINATED A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW07842MJ 145457 BLEED 2 OVERTEMP WARNING MSG ON EICAS IN-FLIGHT. MX CLEANED THE FAN AIR VALVE FILTER. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040407001192004040700119SO 2004 4 7 MASA200400132 120040309A3397 WIRE EMB 145 EMB145LR 3260212SO INVERTER LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07835MJ 145353 MID CABIN CEILING EMERGENCY EXIT SIGN INOP. RESECURED SIGN WIRING TO INVERTER WIRING CONNECTION. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040407001202004040700120WP 2004 4 7 AALA20040431 120040405A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT SHORTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21291AA 49303 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 21 THROUGH 31 AND TAIL CONE SIDEWALL EMERGENCY LIGHTS INOPERATIVE. FOUND WIRES IN TAIL COMPARTMENT SHORTED. REPAIRED WIRES FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 21 THROUGH 31 AND TAIL CONE SIDEWALL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001212004040700121WP 2004 4 7 AALA20040426 120040404A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW219627R 53597 LGA - CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. CLEANED CORROSION ON NUMBER 2 EMERGENCY BATTERY PACK IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040407001222004040700122NM 2004 4 7 2004UALA00262 120040319A5753 FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 RIGHT INBOARD T/E FLAP, MAIN FLAP INBOARD T/E HINGE FITTING SUPPORT CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCMENT REPAIR ANGLE TO HINGE FITTING. 2L72 4F4 FRTA1NM E24NE 20040407001232004040700123NM 2004 4 7 2004UALA00263 120040321A5753 SUPPORT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 RIGHT INBOARD FLAP, CENTER SUPPORT IS CRACKED ON THE LOWER INBOARD FLANGE AT THE MID FLAP ATTACH POINT. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR TO HINGE FITTING. 2L72 4F4 FRTA1NM E24NE 20040407001242004040700124NM 2004 4 7 2004UALA00264 120040321A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29643UA 25093 RIGHT EMERGENCY LIGHT PATH INOP FROM 15 THROUGH ROW 18. REPLACED EMERGENCY LIGHT BATTERY PACK, CHECKED OK. 2L72 4F4 FRTA1NM E24NE 20040407001302004040700130SO 2004 4 7 MASA200400081 120040213A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 EMERGENCY EXIT FLOOD LIGHT INOP. MX RESET LIGHTING SYSTEM. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409000012004040900001EU 2004 4 9 MALA040287 120040323A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 LEFT I/B SEAT TRACK HAS SEVERE CORROSION AT STA 297. REMOVED AND REPLACED SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/27/04. 2L72 4T RTA52EU 20040409000022004040900002EU 2004 4 9 MALA040288 120040328A5610 WINDSCREEN BAC 146 AVRO146RJ85A1500097EU COCKPIT SPARKS A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15522XJ E2347 DURING FLIGHT IN RAIN, A SPARK FLEW PAST THE F/O FROM WINDSCREEN WITH SLIGHT SMOKE. MEM MX SUSPECT STATIC DISCHARGE, INSPECTED WIRING AND CONDITION, NO APPARENT SIGNS OF SCREEN DAMAGE ETC, OPERATED WINDSHIELD HEAT SYSTEM CHECKS GOOD. OK FOR RETURN TO SERVICE. 2H74 4F RTA49EU 20040401001002004040100100NM 2004 4 1 04FDEA00653 120040315A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040401001022004040100102NE 2004 4 1 04FDEA00682 220040319A7321 LINE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE CDP CONTAMINATED A FDEAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO25595FE 48553 DURING DESCENT AT 6000 MSL, 250 KIAS IDLE THRUST ENG 2 RPM LO ALERT, FOLLOWED BY FLAMEOUT, EGT 75 DEG WITH IGNITION OVERRIDE ENGINE ACCELERATED TO NORMAL IDLE. ENGINE OPERATION DURING APPROACH, LANDING AND ROLLOUT WAS NORMAL. INSPECTED NR 2 ENG OIL MASTER CHIP DETECTOR IAW MM 79-36-01-61, NO CONTAMINATION FOUND. SYS AND FOUND CDP LINE FROM COMPRESSOR SECTION TO NR 2 ECU HAS WATER INSIDE, AND DRAIN PORT AT LOW POINT PLUGGED. OPENED CDP LINE AT ECU AND AT ENG AND BLEW DRY NIT THRU LINE TO CLEAN WATER AND DEBRIS. 2L73 4F4 FRTA22WE E13NE 20040401001052004040100105NM 2004 4 1 04FDEA00693 120040322A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 WHILE WORKING CARD N00237 FOUND FRAME TO BE CRACKED BS 600, LBL 7, WL 150. REPAIRED FRAME AT BS 600, LBL 7, WL 150 IAW SRM 53-10-4 FIG 13 AND PER EA 7-5310-70646. 2L73 4F RTA3WE 20040401001112004040100111NM 2004 4 1 04FDEA00749 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1681 BETWEEN LONGERONS 12L AND 13L. COMPLIED WITH FEDEX EA 1-5310-76001, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR 1-2520-7-3380. 2L73 4F RTA22WE 20040401001152004040100115NM 2004 4 1 04FDEA00752 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y=1601 BETWEEN LONGERONS 12L AND 13L. REPAIRED PER SRM 53-30-00 VOL I FIG 1. COMPLIED WITH FEDEX EA 1-5310-75999, REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2L73 4F RTA22WE 20040401001262004040100126NM 2004 4 1 AALA20040359 120040316A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM FUSELAGE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 DFW - EMERGENCY LIGHTS AT L4 INOPERATIVE. REPLACED COLLAR ON LIGHT ASSEMBLY AND REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040401001282004040100128NM 2004 4 1 AALA20040354 120040304A3350 LIGHT BOEING757 757223 1384957NM SEAT ROW 17D MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21646AA 24604 SFO - EMERGENCY LIGHT AT SEAT ROW 17D MISSING. INSTALLED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040401001292004040100129WP 2004 4 1 AALA20040355 120040315A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21971TW 53621 SEA - REMOVABLE EMERGENCY EXIT LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED REMOVABLE EMERGENCY EXIT LIGHT ASSEMBLY FOR FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040401001672004040100167CE 2004 4 1 UG12004F00000 120040220A3230481 MOTOR BEECH 200 B200 1152922CE MLG SHORTED B UG1RO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03989LA BB1310 REMOVED MOTOR DUE TO ARCING/ SHORTING TO CASE AND FAILURE. SHIPPED SAME AS CORE TO MFG. PART FAILURE OCCURRED IN FLIGHT AND EMERGENCY LANDING GEAR EXTENSION PERFORMED FOR LANDING WITHOUT INCIDENT. 1L72 4T A24CE 20040401001782004040100178CE 2004 4 1 DIN2004F00000 120040129A78974512245 WIRE LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP THRUST REVERSER MISMARKED B DINRK NONE W INADEQUATE Q C ININSP/MAINT 1 EA13127GT 5078 067 WE HAVE HAD THREE INSTANCES OF MISS-LABELED WIRES ON NEW DEPLOY SIGNAL SWITCHES (NR 45-12245) FOR MFG THRUST REVERSERS. TWO ON 9/16/98 AND ONE 1/14/04 (THIS SWITCH PURCHASED 8/10/03). ALL HAVE BEEN PURCHASED FROM MFG. THIS PLUNGER TYPE SWITCH HAS TWO CIRCUITS WITH SIX WIRES LABELED 1C, 2NC, 3NO FOR CIRCUIT NR 1 AND 4C, 5NO, GNC FOR CIRCUIT NR 2. WE HAVE FOUND THE NO (NORMALLY OPEN) AND NC (NORMALLY CLOSED) WIRE LABELS REVERSED FOR ONE CIRCUIT. EXAMPLE 5 NO WAS LABELED 6NC AND 6 NC WAS LABELED 5 NO. THIS PROBLEM CN BE DETERMINED WITH AN OHMMETER PRIOR TO INSTALLATION AND THE WIRE MARKERS SWAPPED TO THE CORRECT WIRES. 2L72 4F4 F A10CE E6WE 20040406000132004040600013NM 2004 4 6 04FDEA00818 120040401A7830 TRACK DOUG MD11 MD11 3023602NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 NR 3 ENG RIGHT REVERSER COWL OF TRANSLATING COWL MOST UPPER TRACK END FOUND WITH CRACK. NR 3 ENG RT REVERSER TRANSLATING COWL REMOVED AS PER AMM 78-31-16-4. REPAIRED AS PER FAA 8130-3/FA2004/0118, & REINSTALLED AS PER AMM 78-31-16-4. 2L73 4F RTA22WE 20040406000142004040600014NM 2004 4 6 04FDEA00819 120040401A5754 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. LT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040406000152004040600015NM 2004 4 6 04FDEA00820 120040401A5754 SLAT TRACK DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB FOUND CRACK. RT WING LEADING EDGE SLAT TRACK 16, I/B SUPPORT RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040406000452004040600045NM 2004 4 6 04FDEA00812 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000492004040600049NM 2004 4 6 04FDEA00755 120040325A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000512004040600051NM 2004 4 6 04FDEA00802 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000522004040600052NM 2004 4 6 04FDEA00759 120040326A5753 FITTING DOUG MD11 MD11 3023602NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25619FE 48770 LT WING INBOARD FLAP OUTBOARD HINGE SUPPORT FITTING AT PIVOT BEARING, FUSE PIN IS HEAVILY CORRODED. REMOVED & REPLACED HINGE PIN, BUSHING, WASHER, NUT & COTTER PIN AND INSTALLED IAW M/M 27-50-20-4. 2L73 4F RTA22WE 20040406000872004040600087NM 2004 4 6 04FDEA00699 120040323A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING - OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR ROD END HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5740-75923, LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSY. 2L73 4F RTA22WE 20040406000892004040600089NM 2004 4 6 04FDEA00659 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING OUTBOARD FLAP, INBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000972004040600097NM 2004 4 6 04FDEA00667 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000992004040600099NM 2004 4 6 04FDEA00669 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2L73 4F RTA22WE 20040406001012004040600101NM 2004 4 6 04FDEA00671 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75975, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406001102004040600110 2004 4 6 CALA0400318 420040404A2565UNK SLIDE BOEING757 757224 1384958NM RT OVERWING OUT OF RIG A CALAK NONE L NO TEST ININSP/MAINT 1 SW2758101 27291 CARRIER DEPLOYMENT WAS INTERMITTENT DURING RIGHT OFF WING SLIDE DEPLOYMENT FUNCTION TEST. THE RIGHT OFF WING SLIDE DOOR WAS RIGGED AND ADJUSTED IAW MM 25-65-09, PARAGRAPH 3D, ITEMS 9-14. 2L72 4F RTA2NM 20040406001122004040600112NM 2004 4 6 CALA0400286 120040326A5414311A145014 SKIN BOEING737 7373T0 1384582NM RT PYLON GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND RIGHT ENGINE PLYON SKIN GOUGED UNDER PANEL 5829R, NAC STA 234.25 AND 246.63. REPAIRED IAW ECRA 5431-01022. 2L72 4F RTA16WE 20040406001222004040600122NM 2004 4 6 CALA0400270 120040323A532065C3397335 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714660 28921 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT BETWEEN STA 312-328, LBL 46. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040406001242004040600124NM 2004 4 6 CALA0400272 120040324A5320 ANGLE BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714660 28921 INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT FORWARD BULKHEAD STA 727, RBL 3. A DOUBLER WAS INSTALLED ON THE ANGLE IAW SRM 51-70-11. 2L72 4F RTA16WE 20040406001272004040600127NM 2004 4 6 CALA0400307 120040401A5320143N54321 INTERCOSTAL BOEING757 757224 1384958NM BS CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 684, RBL 15. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, FIGURE 12. 2L72 4F RTA2NM 20040406001282004040600128NM 2004 4 6 CALA0400308 120040401A5315143N5014 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2758101 27291 INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT BS 680, RBL 16 TO LBL 16. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20040406001332004040600133EA 2004 4 6 SWIA200413036 120040220A5420 FAIRING CNDAIRCL600 CL6002B19 1900309EA RT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07426SW 7468 DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON LOWER STANG FAIRING 444BB CRACKED ON INBOARD SIDE. REPAIRED DAMAGE IAW SHORTS CMM 78-30-00, SRS 049. 2L72 4F RTA21EA 20040406001412004040600141EA 2004 4 6 SWIA200413066 120040315A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07913SW 7597 EMERGENCY LIGHT IN AFT OVERHEAD INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. 2L72 4F RTA21EA 20040406001422004040600142EA 2004 4 6 SWIA200413067 120040318A2731 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07588SW 7069 IMMEDIATELY AFTER LIFT-OFF, STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON. TRIM WOULD NOT RE-ENGAGE. REMOVED AND REPLACED PILOTS TRIM SWITCH IAW MM 27-41-05. SYSTEMS OPS CHECKS GOOD IAW CL600 MM 27-41-01. P/N: 996-0013. 2L72 4F RTA21EA 20040406001492004040600149NM 2004 4 6 CALA0400306 120040301A5320143A8126 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND RT Z-CHANNEL IN FORWARD CARGO COMPARTMENT CORRODED AT STA 490-500. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-30-15. 2L72 4F RTA16WE 20040407000292004040700029EA 2004 4 7 ASOA04169 120040302A5210601R3198041 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX STEP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN THE MCN, THE PASSENGER DOOR TOP STEP HINGE WAS FOUND TO BE CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASENGER DOOR TOP STEP HINGE. (M) 2L72 4F RTA21EA 20040407000312004040700031EU 2004 4 7 ASOA04183 120040307A33503011160 LIGHT AEROSPATR72 ATR72 EU GALLEY INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11643AS 413 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040407000462004040700046NM 2004 4 7 USAA040020 120040119A5347 SEAT TRACK BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 CLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 1 INCH AREA, BS 1626, LBL 24 LEFT INBOARD SEAT TRACK. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN BS 1540 AND 1640. (M) 2L72 4F RTA2NM 20040407000482004040700048EA 2004 4 7 ASOA04154 120040222A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURING A C-CHECK IN MCN, THE CARGO DOOR FORWARD RAIL LOWER SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR FORWARD RAIL LOWER SUPPORT BRAKET IAW SRM 51-42-06. (M) 2L72 4F RTA21EA 20040407000572004040700057EA 2004 4 7 SIMA200407504 120040313A3350YAD4F RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST ININSP/MAINT 1 SW21514AE 10119 CLE - FLT 4341 - MAINTENANCE FOUND THAT ALL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED RELAY K135. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA21EA 20040407000592004040700059SO 2004 4 7 SIMA200408202 120040321A27203621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZONTAL STAB INOPERATIVE A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SW21811AE 145529 ORD - FLT 3972 - ON FINAL RECEIVED PITCH TRIM 1/2 INOPERATIVE WARNING ON EICAS WITH MASTER WARNING. PERFORMED TROUBLESHOOTING PITCH TRIM 1/2 INOPERATIVE IAW FAULT ISOLATION MANUAL AND ETN EB-27-022R1. REPLACED HSCU EMB AMM 27-40-01. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040407000602004040700060EU 2004 4 7 SIMA200406802 120040305A2612472326 FIRE LOOP SAAB SF340 340B 7860101EU NR 2 ENGINE MALFUNCTIONED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21330AE 340B330 SBP - FLT 3004 - NR 2 FIRE WARNING INTEGRITY TEST FAILED. REPLACED NR 2 ENGINE AFT FIRE SENSOR LOOP IAW SAAB 340 AMM 26-11-05. OPS CHECK GOOD. (M) 2L72 4T RTA52EU 20040407000902004040700090WP 2004 4 7 AALA20040395 120040325A3397 LIGHT DOUG DC9 DC982 3022082WP ROW 28 MISWIRED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170529 49921 ORD - EMERGENCY OVERHEAD LIGHTS BETWEEN ROWS 28 AND 30 INOPERATIVE. FOUND B5-107 MISWIRED. REWIRED TO PROPER SYSTEM CONFIGURATION FOR EMERGENCY OVERHEAD LIGHTS BETWEEN ROWS 28 AND 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407000922004040700092WP 2004 4 7 AALA20040390 120040327A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW217520A 49897 DFW - EMERGENCY LIGHT ON LOWER WALL ACROSS FROM FORWARD LAVATORY IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT ON LOWER WALL ACROSS FROM FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407000942004040700094WP 2004 4 7 AALA20040402 120040331A335072761158 CIRCUIT BREAKER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT POPPED A AALAO OTHER O OTHER CRCRUISE 1 SW21288AA 49300 PHX - INFLIGHT T1418 AIRCRAFT BATTERY CHARGER CIRCUIT BREAKER POPPED. REPLACED BATTERY CHARGER AND CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407000962004040700096NM 2004 4 7 AALA20040401 120040330A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21399AN 29606 SFO - EMERGENCY ESCAPE PATH LIGHTING AT SEATS 21 AND 22AB INOPERATIVE. RESEATED LOOSE CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTING FOR SEATS 21 AND 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040407000982004040700098WP 2004 4 7 AALA20040397 120040329A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21423AA 49335 DFW - FORWARD EMERGENCY LIGHT ON AFT STAIRWELL SIDEWALL PANEL INOPERATIVE. RECONNECTED WIRES TO FORWARD EMERGENCY LIGHT ON AFT STAIRWELL SIDEWALL PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001032004040700103SO 2004 4 7 MASA200400034 120040115A2923848847 PUMP EMB 145 EMB145LR 3260212SO HYD FAILED A MASAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07829MJ 145228 UPON ARRIVAL IN HSV FOR RON, THE CREW REPORTED AN ELECTRICAL ODOR IN CABIN AT ROW 12C DURING FLIGHT. THE CREW REPORTED THAT THERE WAS NO VISIBLE SMOKE. MX FOUND THE NR 1 ELECTRIC HYD PUMP FAILED. MX REPLACED THE PUMP. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040407001172004040700117SO 2004 4 7 MASA200400119 120040301A2560P207009120 MOUNT EMB 145 EMB145LR 3260212SO FLASHLIGHT BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW07848MJ 145530 FWD CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN. MX REPLACED THE FLASHLIGHT MOUNT. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040407001182004040700118SO 2004 4 7 MASA200400130 120040308A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 MID CABIN CEILING EMERGENCY EXIT SIGN INOP. RESECURED CONNECTOR TO CABIN CONNECTION. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040407001262004040700126EA 2004 4 7 MASA200400170 120040328A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775998 7336 DURING AN RON, DISCOVERED THAT THE RT EXTERNAL EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS INOP. MX RELAMPED. 2L72 4F RTA21EA 20040407001272004040700127EA 2004 4 7 MASA200400172 120040330A3350BR9279013 SOCKET CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DEFECTIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 AFT CABIN EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT ASSEMBLY. OP CHECKS GOOD. 2L72 4F RTA21EA 20040407001322004040700132EA 2004 4 7 MASA200400094 120040220A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737228 7228 FLOOR EMERGENCY PATH LIGHTING WAS INOP FROM ROWS 9-13. MX FOUND LOOSE TERMINAL. MX RECONNECTED TERMINAL. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040409000042004040900004NM 2004 4 9 AWXA200400352 120040405A21337110033 OUTFLOW VALVE BOEING737 73733A 1384673NM CABIN PRESSURE FAILED A AWXABG EMER. DESCENT O2 MASK DEPLOYED G MULTIPLE FAILURE CRCRUISE 1 WP28166AW421432343 23627 AT FL 350 LOST CABIN PRESSURE, COULD NOT CONTROL IN ANY MODE. EXECUTED EMERGENCY DESCENT & MANUALLY DEPLOYED MASKS, DECLARED EMERGENCY. MX PERFORMED TEST OF OUTFLOW VALVE & FOUND HEATER GASKET INOP. R / R OUTFLOW VALVE, CABIN PRESS CONTROLLER AND CABIN PRESSURE CONTROL PANEL. CONFIRMED FAILURE OF CABIN PRESS CONTROL PANEL FINDING SWITCH DEFECTIVE, A BROKEN SWITCH SHAFT, CAPACITORS LEAKING, & OBSOLETE DRIVE BELTS. REPLACED DEFECTIVE PARTS, OVERHAULED UNIT IAW CMM. INCOMING TEST OF CABIN PRESS CONTROLLER CONFIRMED REASON FOR REMOVAL, UNIT FOUND TO HAVE A TRANSDUCER OUT OF TRIM. ALIGNED UNIT TO OEM SPECS, & PERFORMED CHECK OF OUTFLOW VALVE COULD NOT CONFIRM REASON FOR REMOVAL, UNIT PASSED ALL INCOMING TESTS. 2L72 4F RTA16WE 20040409000052004040900005NM 2004 4 9 AWXA200400353 120040405A3597W118201016 WIRE BOEING737 73733A 1384673NM SEAT ROW 11 RT BROKEN A AWXABG EMER. DESCENT O2 MASK DEPLOYED O OTHER CRCRUISE 1 WP28166AW 23627 PHX - EMERGENCY EQUIPMENT - DURING EMERGENCY DESCENT AND MANUAL OXYGEN MASK DEPLOYMENT, MASKS FAILED TO DEPLOY AT SEAT ROW 11 RIGHT. MAINTENANCE RE-TERMINATED BROKEN SPLICE AT PASSENGER OXYGEN LATCH MECHANISM SEAT ROW 11 RIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040409000062004040900006NM 2004 4 9 AWXA200400354 120040330A53306573742 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 PHX - MAJOR REPAIR - A .25 INCH CRACK WAS FOUND IN FUSELAGE SKIN LT SIDE AT LAP SEAM BETWEEN WINDOWS 11 & 12, BS 540, STR 14 LEFT. MAINTENANCE CUT OUT DAMAGED SECTION OF SKIN JUST BELOW WINDOW BELT BS 540, STR 14 LEFT; FABRICATED 4 EACH FILLERS, A DOUBLER & TRIPLER; INSTALLED REPAIR PARTS IAW B737-200 SRM 53-30-03 FIG 48, SHEET 58, DETAIL 31. 2L72 4F RTA16WE 20040409000122004040900012EU 2004 4 9 MALA040280 120040319A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15414XJ 340B414 DURING 4Y/2Y INSPECTION IN LCQ, FS 297 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/23/04. 2L72 4T RTA52EU 20040409000132004040900013EU 2004 4 9 MALA040281 120040316A3230 ROLLER SAAB SF340 340B 7860101EU MLG UPLOCK CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15362PX 340B258 UPON GEAR RETRACTION, 3 GREEN LIGHTS EXTINGUISHED, BUT GEAR UNSAFE LIGHT ILLUMINATED. RAN QRH WITH NO SUCCESS. AIR RETURN TO ELM. MX PST FLT INSP VISUALLY NOTED ALL 3 GEAR UPLOCK ROLLERS HEAVILY CAKED WITH SNOW AND ICE. CLEANED ALL 3 GEAR, GEAR DOORS, AND BAYS. OK FOR CONTINUED SERVICE. 2L72 4T RTA52EU 20040409000162004040900016NM 2004 4 9 AT0400008 120040407A3350 LIGHT BOEING717 717200 1383700NM TAIL COMP WILL NOT TEST A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15975AT 55035 TAIL COMPARTMENT EMERGENCY LIGHT DID NOT TEST ON A CHECK L2-738. CLEANED LIGHT TERMINALS, OPS CHECK GOOD IAW B717 MM 3353. 2L72 4F TRA6WE 20040409000172004040900017SO 2004 4 9 MASA200400099 120040222A3350 SIGN EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07844MJ 145481 EMERGENCY EXIT SIGN INOP ROW 12. MX SECURED CONNECTION AT LIGHT, OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040409000192004040900019EA 2004 4 9 MASA200400080 120040213A5210A410281 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW0775995 7361 MAIN CABIN EXTERNAL DOOR HANDLE WILL NOT STOW FROM THE INSIDE. MX REPLACED THE HANDLE ASSY. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409000202004040900020EA 2004 4 9 MASA200400084 120040214A2120 SMOKE CNDAIRCL600 CL6002C10 1390015EA CABIN DETECTED A MASAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW07510MJ 10101 A/C RETURNED TO THE FIELD DUE TO A REPORT OF ELECTRICAL SMOKE SMELL IN THE CABIN. MX INSPECTED CABIN AND LAV AREAS, TAXIED AND RAN THE A/C TO TAKEOFF POWER. NO DEFECTS NOTED. NO PARTS USED. 2L72 4F RTA21EA 20040409000212004040900021EA 2004 4 9 MASA200400090 120040217A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NR 2 ENGINE ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07570ML 7206 REJECTED TAKEOFF DUE TO THE NR 2 ENG REV ICON. MX PLACED T/R ON MEL 78-30-01. THE A/C CONTINUED SERVICE. 2L72 4F RTA21EA 20040409000222004040900022EA 2004 4 9 MASA200400098 120040222A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OVERSERVICED A MASAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SW0775995 7361 COULD NOT CLOSE THE PAX DOOR. CONTRACT MX REMOVED EXCESS GREASE FROM THE OUTER HANDLE FITTING AND THE DOOR OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2L72 4F RTA21EA 20040409000242004040900024SO 2004 4 9 MASA200400082 120040214A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07841MJ 145448 DURING A RON, DISCOVERED THE LEFT OVERWING EMERGENCY LIGHT WAS INOP. MX REPLACED THE LAMP. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409000252004040900025EA 2004 4 9 MASA200400087 120040215A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737228 7228 DURING PREFLIGHT THE PAX DOOR INTERIOR EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409000292004040900029SO 2004 4 9 MASA200400062 120040202A7830TY204103A CONTROL UNIT EMB 145 EMB145LR 3260212SO NR 2 ENGINE INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07831MJ6604 145273 ABORTED TAKEOFF DUE TO NR 2 ENGINE REV DISAGREE MESSAGE DURING TAKEOFF ROLL AND RETURNED TO GATE. MX PLACED THRUST REVERSER ON MEL. 2/08/2004. MX REPLACED THE ICU. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409000332004040900033WP 2004 4 9 AALA20040377 120040322A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 10D INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217550 53032 DFW - SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 10D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000352004040900035WP 2004 4 9 AALA20040382 120040323A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DEN - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000362004040900036 2004 4 9 MWEA040031 420040323A235055411 AUDIO PANEL BOEING717 717200 1383700NM COCKPIT INTERMITTENT A MWEAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL31916ME 55179 CAPTAIN'S AUDIO PANEL IS INTERMITTENT. REMOVED AND REPLACED AUDIO CENTRAL PANEL. 2L72 4F TRA6WE 20040409000392004040900039SO 2004 4 9 MASA200400151 120040319A3610S2U2226 O-RING EMB 145 EMB145LR 3260212SO BLEED DUCT BLOWN A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07827MJ 145217 DIVERTED TO CLT DUE TO BLEED NR 2 LEAK MSG IN-FLIGHT. MX REPLACED A BLEED DUCT GAMMA COUPLING O-RING AND THE SYSTEM OP CHECKED GOOD. 2L72 4T RTT00011AT 20040409000412004040900041SO 2004 4 9 MASA200400153 120040319A3350 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 RIGHT OVERWING INTERIOR EMERGENCY EXIT SIGN INOP. MX RESECURED THE SIGN AND IT OPERATED NORMALLY. NO PARTS USED. 2L72 4T RTT00011AT 20040409000422004040900042 2004 4 9 MASA200400157 420040321A22107003897925 CONTROLLER EMB 145 EMB145LR 3260212SO COCKPIT SMOKE A MASAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07833MJ 145327 FLIGHT GUIDANCE CONTROLLER STARTED SMOKING. MX REPLACED THE GUIDANCE CONTROLLER. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409000432004040900043SO 2004 4 9 MASA200400163 120040325A3350 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 CABIN CEILING EMERGENCY EXIT SIGN AT ROW 12 INOP ON THE BACKSIDE. MX ADJUSTED WIRING TO THE SIGN. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040409000442004040900044SO 2004 4 9 MASA200400164 120040325A3520 BOTTLE EMB 145 EMB145LR 3260212SO OXYGEN SYS OVERSERVICED A MASAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07832MJ 145310 AFT CABIN PORTABLE O2 BOTTLE OVERPRESSURIZED (GAUGE NEEDLE IN RED). MX INSPECTED BOTTLE AND FOUND TO BE WITHIN LIMITS FOR DISPATCH. NO PARTS USED. 2L72 4T RTT00011AT 20040409000472004040900047WP 2004 4 9 AALA20040381 120040323A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DEN - EMERGENCY LIGHT AT L1 DOOR AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L1 DOOR AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000482004040900048WP 2004 4 9 AALA20040378 120040322A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21516AM 49893 ATL - EMERGENCY LIGHTS FROM SEAT 1 THROUGH 20 INOPERATIVE. REPLACED CHARGER MODULE AND BATTERY PACK FOR EMERGENCY LIGHTS FOR SEATS 1 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000522004040900052SO 2004 4 9 MASA200400171 120040329A5210 LINKAGE EMB 145 EMB145LR 3260212SO PAX DOOR OUT OF RIG A MASAK NONE O OTHER ININSP/MAINT 1 SW07831MJ 145273 CREW REPORTED THE MAIN PAX DOOR HARD TO OPEN. MX RE-RIGGED AND LUBED THE PAX DOOR LINKAGE. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040409000532004040900053NM 2004 4 9 2004UALA00248 120040315A2120 SMOKE BOEING777 777222 1385219NM PWA PW4077PW4077 NE COCKPIT DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP29211UA 30217 SMOKE ORIGINATE MOMENTARILY AT BEGIN OF DESCENT ON CAPT'S SIDE IN COCKPIT. APU, SHOULDER-FOOT HEATERS OFF. THE REPORT OF SMOKE WAS ON A FLIGHT FROM LAX TO HNL. HNL MX CONDUCTED A COMPREHENSIVE CHECK OF NR 1 ENGINE FOR OIL LEAKS, BUT FOUND NONE. MAINTENANCE RAN THE ENGINES ON THE GROUND AND ISOLATED BOTH PACKS, BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT 2511 RETURNED TO REVENUE SERVICE WITHOUT FURTHER SMOKE OR SMELL REPORTS SINCE 3/16/04. 2L72 4F4 FRTT0001SE E46NE 20040409000572004040900057EU 2004 4 9 2004UALA00287 120040329A5270E00800208C CONNECTOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FWD CARGO DOOR DAMAGED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29479UA 1538 FWD CARGO DOOR OPEN INDICATION ON TAKEOFF. *S/D* REPAIRED DAMAGED CONNECTOR BACKSHELL ON DOOR WARNING SENSOR. 2L72 4F4 FRTA28NM E40NE 20040409000582004040900058NE 2004 4 9 SWIA200412993 220040307A7200 ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RIGHT LEAKING A SWIAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM07289YV8783 8783 120289 AFTER TAKEOFF THE CABIN FILLED WITH SMOKE SMELL AND THE SMOKE DETECTOR WAS SET OFF. AFTER LANDING FOUND EXCESSIVE OIL LEAKING FROM THE RIGHT ENGINE INLET. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY WITH SERVICEABLE ASSY. OPS CHECK GOOD, NO LEAKS NOTED AT THIS TIME IAW 72-00-00. RAN PACKS, NO SMOKE WAS DETECTED, OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040409000602004040900060EU 2004 4 9 AALA20040415 120040326A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170079 619 TUL - LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52.1 CRACKED. INSTALLED REPAIR FITTING PER ESO 30595 DATED 3/25/04 FOR LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52.1. 2L72 4F RTA35EU 20040409000612004040900061NM 2004 4 9 AALA20040411 120040317A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 AFW - CORROSION DISCOVERED ON THE TOP SURFACE OF THE UPPER FLOORBEAM AT STATION 1518. REMOVED CORROSION AND FABRICATED REPAIR STRAP FROM 0.050 INCH 301 1/2 H STAINLESS STEEL, MADE SURE STRAP COVERED THREE ROWS OF FASTENERS PAST DAMAGE. ALODINED ALL BARE ALUMINUM SERVICES AND FINISHED BLENDS AND REPAIRED STRAP WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS 5-92. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALANT AND USED HI-LOK OR EQUIVALENT FASTENERS. 2L72 4F RTA1NM 20040409000622004040900062EU 2004 4 9 AALA20040413 120040326A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170079 619 TUL - LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52 IS CRACKED. INSTALLED REPAIR FITTING PER ESO 30595 DATED 3-25-2004 FOR LEFT HAND GANTRY BEAM NUMBER 4 AT FRAME 52. 2L72 4F RTA35EU 20040409000632004040900063WP 2004 4 9 AALA20040412 120040326A5310 BEAM DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21207AA 49158 TUL - AFT CARGO DOOR BEAM CORRODED AT STATION 1160 - 1207. CORROSION WAS 6 INCHES BY 44 INCHES AND AT A DEPTH OF 0.034 INCHES. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-3 FIG 1. 2L72 4F A6WE 20040409000662004040900066NM 2004 4 9 2004UALA00289 120040328A3397 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29322UA 23954 EEL LIGHTS INOP AT SEAT ROWS 17-21. EEL CABLE REPLACED AND TESTED OK. 2L72 4F4 FRTA16WE E2GL 20040409000672004040900067 2004 4 9 2004UALA00290 420040329A2565 SQUIB BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE ESCAPE SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29648UA 25285 LEFT OVERWING ESCAPE SLIDE SQUIB TEST LIGHT DOES NOT WORK WHEN PRESSED TEST NR 1. RESEATED PLUGS ON BACK OF TEST PANEL - -TESTS OK. 2L72 4F4 FRTA1NM E24NE 20040409000692004040900069NM 2004 4 9 2004UALA00292 120040330A5313 SPLICE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE STRINGER CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 AFT CABIN NR 4R STR SPLICE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040409000772004040900077 2004 4 9 SWIA200413094 420040327A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07289YV6804 5861 120289 CAPTAIN SIDE RED TRIM AND AP LIGHTS ILLUMINATED ON FCP. REPLACED CAPTAIN'S AUTO-PILOT COMPUTER. CAPT'S AUTO-PILOT/FLIGHT DIRECTOR SYSTEM OPERATES NORMALLY PER MM 22-11-00. 2L72 4T4 TRTA31SO E20NE 20040409000782004040900078EA 2004 4 9 SWIA200412995 120040307A5520 BUSHING CNDAIRCL600 CL6002B19 1900309EA ELEVATOR DAMAGED A SWIAO OTHER E VIBRATION/BUFFET CRCRUISE 1 NM07413SW 7102 ELEVATOR SHUTTER DURING LEVEL FLIGHT AND INITIAL DESCENT AT APPROXIMATELY 290 KTS. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR OUTBOARD ACTUATOR TO CONTROL SURFACE BOLTS AND BUSHINGS IAW 27-33-01. INFLIGHT FUNCTIONAL CHECK OF ELEVATOR CONTROL SYSTEM GOOD. 2L72 4F RTA21EA 20040409000792004040900079EA 2004 4 9 SWIA200412996 120040307A2751855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07954SW1667 1667 7815 AFTER PASSENGER BOARDING, PRIOR TO START, RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED LEFT OUTBOARD BPSU AND PERFORMED RIGGING. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040409000812004040900081EA 2004 4 9 SWIA200412998 120040307A2741270007 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07916SW 7634 STAB TRIM CH 1 FAIL TO SET. DEPOWERED AND REPOWER AIRCRAFT. STAB TRIM RESET. REPLACED F/O'S PITCH TRIM DISCONNECT SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-30. 2L72 4F RTA21EA 20040409000822004040900082EA 2004 4 9 SWIA200412999 120040308A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM STICKING A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07437SW 7564 FIRST OFFICER'S TRIM SWITCH STICKY. REPLACED F/O'S TRIM SWITCH. OPS CHECK GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20040409000832004040900083NM 2004 4 9 AT040004 120040226A3220MS288892 SCHRADER VALVE BOEING717 717200 1383700NM NLG UNSERVICEABLE A ZZDAO OTHER J WARNING INDICATION CLCLIMB 1 SO15943AT 55006 AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR INDICATED UNSAFE, ALL QRH PROCEDURES ACCOMPLISHED, LANDING WEIGHT WAS 99,000 IBS, SINK RATE AT TOUCHDOWN 100 FPM. FOUND NOSE STRUT FLAT (ZERO PRESSURE), JACKED NOSE GEAR AND CYCLED SEVERAL CYCLES PER B717 AMM 32-30, NOSE GEAR FUNCTION CHECK NORMAL. AS PRECAUTIONARY REPLACED SCHRADER VALVE. 2L72 4F TRA6WE 20040409000842004040900084NM 2004 4 9 CALA0400296 120040330A5510180A16122 PIN BOEING737 737724 13844BYNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER MID MOUNT PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, STEP 10-13. 2L72 4F RTA16WE 20040409000862004040900086NM 2004 4 9 CALA0400298 120040330A5320BAC1496444 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND RIGHT ZEE CHANNEL CORRODED AT STA 500A-500I IN FORWARD PIT. THE Z-CHANNEL WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040409000872004040900087NM 2004 4 9 CALA0400299 120040330A5320BAC1496377 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND LEFT Z-CHANNEL CORRODED AT STA 727-847 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF ZEE CHANNEL WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040409000892004040900089NM 2004 4 9 2004UALA00296 120040327A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 AFT SIDE OF AFT CARGO DOOR CUTOUT NEEDS REPAIR. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040409000902004040900090NM 2004 4 9 2004UALA00297 120040330A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 BS 787 STR 23L SHEAR TIE CRACKED AFT CARGO COMPARTMENT. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040409000932004040900093EU 2004 4 9 2004UALA00300 120040319A5542D5547100200000 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RUDDER TIP DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29485UA 1617 UPPER RUDDER TIP MISSING. UPPER RIGHT & LEFT PANELS DAMAGED IN GFRP AREA. MAJOR REPAIR ACCOMPLISHED. REPLACED RUDDER TIP. INSTALLED NEW UPPER RIB, ATTACH ANGLE & FAIRING CAP TO RIGHT & LEFT PANELS. 2L72 4F4 FRTA28NM E40NE 20040409000942004040900094NE 2004 4 9 2004UALA00301 220040401A7297 CONNECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT ENGINE LOOSE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29659UA 27114 EICAS MESSAGE, RIGHT ENGINE FUEL FILTER DISPLAYED DURING CLIMBOUT. FUEL FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. THE SWITCH WAS TESTED IN THE SHOP, AND FOUND TO BE SLIGHTLY OUT OF CALIBRATION, BUT NOT ENOUGH TO CAUSE THE EVENT. AS A RESULT OF SHOP FINDINGS, THE MOST LIKELY CAUSE OF THIS EVENT IS A LOOSE CONNECTOR AT THE SWITCH (FIXED DURING SWITCH REPLACEMENT). 2L72 4F4 FRTA1NM E24NE 20040409000982004040900098WP 2004 4 9 MWEA040033 120040325A531599581561 LONGERON DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 WINDOW BELT CRACK VISUALLY DETECTED, STATION 408 LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR PARTS FABRICATED AND INSTALLED EACH LONGERON SPLICE, INSTALLED TITANIUM DOUBLER AND INSTALLED INTERCOSTAL. 2L72 4F A6WE 20040409000992004040900099WP 2004 4 9 MWEA04034 120040325A5311527779306 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 FRAME STATION 1307 BETWEEN LONGERON 29 LEFT AND 29 RIGHT HAS CORROSION. CUT OUT DAMADED SECTION OF FRAME, FABRICATED 13 PLATES AND INSTALLED 16 FASTENERS, REINSTALLED FRAME TO INTERCOSTAL. 2L72 4F A6WE 20040409001032004040900103EA 2004 4 9 SWIA200413073 120040314A2760 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07408SW 7055 ON TAXI OUT RECEIVED INBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW MM 27-61-01. OPS CHECK GOOD. P/N: 365-209D, S/N OFF: F0621A. 2L72 4F4 FRTA21EA E15NE 20040409001072004040900107SO 2004 4 9 SWIA200413077 120040316A275012064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07584SW3814 3814 120352 ON APPROACH GOT A CONTROL FAULT ON THE OUTBOARD FLAPS WHEN SELECTING 15 DEGREES. ALSO GOT 2 CONTROL FAULTS ON THE OUTBOARD FLAPS WHILE IN CRUISE. REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040409001082004040900108SO 2004 4 9 SWIA200413078 120040324A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07212SW9050 8531 120276 ON TAKEOFF ROLL FIRST OFFICER EXPERIENCED A STIFF RIGHT RUDDER INPUT THEN A TEMPORARY FREEZE (STOP) THEN UNCOMMANDED LEFT RUDDER INPUT/BUMP. ALL SYSTEMS OK DURING FLIGHT. REPLACED GREEN SYSTEM RUDDER ACTUATOR IAW MM 27-22-02. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040409001092004040900109NM 2004 4 9 CALA0400264 120040322A5320146A7502 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED FROM STA 727C TO 767. A NEW ZEE CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040409001102004040900110NM 2004 4 9 CALA0400265 120040322A5312UNK PRESSURE PANEL BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND PRESSURE DECK WEB CRACKED AT STA 665-675, RBL 35 TO RBL 45. REPAIRED IAW ECRA 5312-01025. 2L72 4F RTA16WE 20040409001112004040900111NM 2004 4 9 CALA0400266 120040317A533065C323596 SKIN PANEL BOEING737 737524 1384721NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718658 28919 INSPECTION FOUND FUSELAGE SKIN PANEL DENTED BELOW THE FORWARD CARGO DOOR CUTOUT BETWEEN STA 420 AND 440, S27L S26R. REPAIRED IAW ECRA 5311-01190. 2L72 4F RTA16WE 20040409001122004040900112EA 2004 4 9 SWIA200413079 120040324A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT FAILED A SWIAO OTHER O OTHER DEDESCENT 1 NM07958SW 7833 DESCEND THROUGH FL180 FIRST OFFICER'S WINDOW CRACKED, THEN CRACKED AGAIN THROUGH 13,000 FT. REPLACED FIRST OFFICER'S RIGHT WINDOW. OPS CHECK GOOD IAW RII 56-402 AND CRJ MM 56-00-00. P/N OFF NP134322-001. 2L72 4F4 FRTA21EA E15NE 20040409001132004040900113EU 2004 4 9 MALA040285 120040325A242031342001 GENERATOR SAAB SF340 340B 7860101EU AC SYSTEM FAILED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15451XJ 340B451 LEFT INTAKE LIGHT CYCLED DURING FLIGHT. MX REPLACED AC GEN P/N 31342-001, S/N ON 92009. ALL CHECKS GOOD OF INTAKE HEAT AND GEN. 2L72 4T RTA52EU 20040409001142004040900114NM 2004 4 9 CALA0400273 120040324A5753113A270018 SKIN BOEING737 737724 13844BYNM RT I/B AFT FLAP PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW27277346791 28949 INSPECTION FOUND A SMALL HOLE IN RIGHT WING I/B AFT FLAP APPROXIMATELY 20 INCHES FROM I/B EDGE. THE RIGHT WING I/B AFT FLAP ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-51-12-400-801. 2L72 4F RTA16WE 20040409001162004040900116NM 2004 4 9 CALA0400275 120040324A5320146A940121 STRAP BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND STRAP (CROSS TIE) BETWEEN STA 767 AND 787 CORRODED. A NEW STRAP WAS INSTALLED IAW SRM 51-20-01 AND 51-40-02. 2L72 4F RTA16WE 20040409001172004040900117 2004 4 9 CALA0400276 420040324A25651268128 ACTUATOR BOEING757 757224 1384958NM RT SLIDE INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW275810140330 27291 THE RIGHT OFF WING ESCAPE SLIDE CARRIER DID NOT DEPLOY WHEN 1500 PSI NITROGEN WAS APPLIED DURING TESTING. MAINTENANCE FOUND THE RIGHT WING ESCAPE SLIDE ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED AND A FUNCTIONAL CHECK WAS PERFORMED IAW MM 25-65-05, PARA 3A-D, ITEMS 1-18. 2L72 4F RTA2NM 20040409001192004040900119NM 2004 4 9 CALA0400278 120040325A53206547957U3 SILL BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714660 28921 INSPECTION FOUND AFT BAGGAGE BIN LOWER SILL CORRODED AT STA 794.3-847, S24R-25R. THE LOWER SILL WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20040409001242004040900124WP 2004 4 9 AALA20040387 120040324A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217508 49802 DEN - OVERHEAD EMERGENCY LIGHTS AT ROWS 14 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-102 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 14 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001252004040900125NM 2004 4 9 AALA20040389 120040325A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139356 24037 LAX - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. SECURED EMERGENCY LIGHT SIDEWALL CONNECTOR AT SEAT 29H AND J. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040409001272004040900127NM 2004 4 9 AT0400006 120040316A32205952241501 DEFLECTOR BOEING717 717200 1383700NM NLG DAMAGED A ZZDAO OTHER J WARNING INDICATION CLCLIMB 1 SO15969AT 55030 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED SPRAY DEFLECTOR. 2L72 4F TRA6WE 20040409001282004040900128WP 2004 4 9 MWEA040048 120040405A5210995575119 ANGLE DOUG DC9 DC981 3022081WP CABIN DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 MAIN CABIN DOOR, AFT LOWER CORNER ATTACH ANGLE IS CRACKED. FABRICATED AND INSTALLED NEW ATTACH ANGLE. 2L72 4F A6WE 20040409001292004040900129EA 2004 4 9 SWIA200413050 120040309A7120 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 CRACK FOUND ON LOWER WEB OF ENGINE SUPPORT BEAM AT LEFT ACCESS PANEL CUTOUT, OUTBOARD OF LBL 36.2, BETWEEN FS 625.3 AND FS 640.0. CARRIED OUT ENGINE SUPPORT BEAM REPAIR ON LH SIDE IAW BRAD REO 601R-43-61-366 REV. E. 2L72 4F4 FRTA21EA E15NE 20040409001302004040900130EA 2004 4 9 SWIA200413051 120040309A7120 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE SUPPORT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 CRACK FOUND ON LOWER WEB OF ENGINE SUPPORT BEAM AT RIGHT ACCESS PANEL CUTOUT, OUTBOARD OF RBL 36.2, BETWEEN FS 625.3 AND FS 640.0. CARRIED OUT ENGINE SUPPORT BEAM REPAIR RH SIDE IAW BRAD REO 601R-53-61-366 REV. E 2L72 4F4 FRTA21EA E15NE 20040409001312004040900131EA 2004 4 9 SWIA200413052 120040309A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, RIGHT FS 625 INTERCOSTAL ANGLE CRACKED. ANGLE REPLACED AT FS 625 RT STR 14 IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040409001332004040900133EA 2004 4 9 SWIA200413054 120040309A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, RIGHT SIDE FRAME STA 640 BETWEEN STR 9 AND STR 12 CRACKED. PARTS MADE IAW CRJ REO 601R-53-61-557. REPAIR PARTS INSTALLED IAW CRJ REO 601R-53-61-557 AT FR STA 640 BTWN STR 9 AND STR 12 RIGHT SIDE. 2L72 4F4 FRTA21EA E15NE 20040409001352004040900135 2004 4 9 SWIA200413056 420040318A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07583SW8382 8382 120351 CAPTAIN'S AUTOPILOT DISENGAGES DUE TO FD FLAG. REMOVED AND REPLACED NR 1 & 2 AUTOPILOT COMPUTERS. 2L72 4T RTA31SO 20040409001362004040900136WP 2004 4 9 AALA20040373 120040321A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21258AA 49288 DFW - FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 5E INOPERATIVE. REPLACED THE FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001372004040900137NM 2004 4 9 AALA20040376 120040321A2923849589 PUMP BOEING737 737823 13844BZNM HYD SYSTEM FAILED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21916AN 29517 DFW - INFLIGHT T2154/21 NUMBER 2 ENGINE HYDRAULIC LOW PRESSURE LIGHT CAME ON DURING CRUISE. SHORTLY AFTER LOST ALL OF SYSTEM B-HYDRAULIC PRESSURE. DECLARED EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE HYDRAULIC PUMP AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040406000352004040600035NM 2004 4 6 04FDEA00737 120040323A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25282FE 22349 DENT IN EXTERNAL SKIN OF NR 2 ENG INLET 12 INCHES FROM L/E AT 9 O'CLOCK POSITION. DENT IN EXTERNAL SKIN OF NR 2 ENGINE INLET 12 INCHES FROM L/E AT 9 O'CLOCK POSITION AREA 1.5 X .090 INCH DEEP A/Y=16.6, FOUND OUT OF LIMITS PER SRM 54-30-01. REPAIRED DENT PER SRM 54-30-03. 2L73 4F RTA3WE 20040406000362004040600036NM 2004 4 6 04FDEA00793 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1. 2L73 4F RTA22WE 20040406000372004040600037NM 2004 4 6 04FDEA00795 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000382004040600038NM 2004 4 6 04FDEA00796 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000392004040600039NM 2004 4 6 04FDEA00797 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000402004040600040NM 2004 4 6 04FDEA00798 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654. LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000412004040600041NM 2004 4 6 04FDEA00799 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000422004040600042NM 2004 4 6 04FDEA00800 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT LUG SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000432004040600043NM 2004 4 6 04FDEA00801 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76003. TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406000542004040600054NM 2004 4 6 04FDEA00762 120040327A324142307 CONTROL BOX BOEING727 727200 138407ENM ANTI SKID SYS INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25258FE 20940 MAIN GEAR ANTI SKID OUTBOARD INOP & INBD INOP LIGHTS INTERMITTEN ON TAKEOFF ROLL WITH NO BRAKES APPLIED. REMOVED AND REPLACED ANTI SKID CONTROL BOX, OPS CHECK AND SELF TEST GOOD AT THIS TIME IAW 727 MM 32-42-001-5. 2L73 4F RTA3WE 20040406000562004040600056NM 2004 4 6 04FDEA00764 120040327A5230B275307020 HINGE BOEING727 727200 138407ENM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25280FE 22347 MAIN CARGO DOOR, DOOR HINGE LUG MINOR GOUGE REPAIR BS 616.5. COMPLIED WITH EA 7-5230-75124 DOOR - MAIN CARGO DOOR DOOR HINGE LUG MINOR GOUGE REPAIR FS 616.5 AT MAE. 2L73 4F RTA3WE 20040406000582004040600058NM 2004 4 6 04FDEA00766 120040326A2840360112004 DCU DOUG MD11 MD11 3023602NM ZONE 200 MALFUNCTIONED A FDEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO25603FE 48459 AS PER MEL 28-01-02-02-A MEL HAS MAINTENANCE DEACTIVATE ALL AUX AND TAIL FUEL BOOST PUMP. TOP OF CLIMB NOTICED AUX UPPER RIGHT PUMP LOW ALERT. ALL INDICATION'S OF PUMP ON OVERHEAD AND SYNOPTIC DISPLAY INDICATE PUMP IS RUNNING, WHEN DEACTIVATED. R AND I DCU PER MM 28-41-91-4. REACTIVATE ALL C/B'S, CONNECTORS AND PERFORMED FSC RTS PER MM 28-08-01-5, ALL TEST PASSED. 2L73 4F RTA22WE 20040406000762004040600076NM 2004 4 6 04FDEA00760 120040327A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING, CORROSION OBSERVED ON UPPER SKIN SURFACE FROM XORS 264 TO 317 AND BETWEEN STRINGERS S10 TO S21. REMOVED PER SRM 57-10-00 VOL I FIG 32 2L73 4F RTA22WE 20040406000782004040600078EU 2004 4 6 04FDEA00771 120040330A3230BDM3003 PROXIMITY SENSOR AIRBUS300 A300F4605R 3930327EU MLG FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25661FE7224 7224 760 ON TAKEOFF AT BDL GEAR WOULD NOT RETRACT, COMPLIED WITH ECAM AND QRH PROCEDURES RETURNED TO KBDL UNEVENTFULL APPROACH AND LANDING. PERFORMED BITE CHECK ON PROX BOX PER TSM 32-61-00, FOUND BOX FAULT LIGHT ON. SENSORS ALL CHECK GOOD. CHECKED BOOGIE PITCH DAMPERS FOR PROPER SERVICE FOUND TO BE GOOD PER M/M 12-12-32. REMOVED AND REPLACED PROX BOX PER M/M 32-31-71-4, OPS CHECK GOOD. 2L72 4F RTA35EU 20040406000922004040600092NM 2004 4 6 04FDEA00662 120040316A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75275, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040406001082004040600108NM 2004 4 6 CALA0400316 120040403A5347BAC1509100688 CARGO TRACK BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND CARGO RAIL CORRODED AT STA 767, RBL 13.84. THE CARGO RAIL WAS REPAIRED IAW ECRA 5321-01177. 2L72 4F RTA16WE 20040406001152004040600115NM 2004 4 6 CALA0400289 120040328A2560ACREM1 MEGAPHONE BOEING737 7373T0 1384582NM FC CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 THE MEGAPHONE IN FIRST CLASS CABIN WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED. 2L72 4F RTA16WE 20040406001172004040600117NM 2004 4 6 CALA0400320 120040402A2780667901 VALVE BOEING757 757224 1384958NM DRIVE UNIT ASSY LEAKING A CALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714118 27560 THE FLIGHT ATTENDANTS REPORTED AN ELECTRICAL SMELL IN THE AFT CABIN WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE LEADING EDGE SLAT POWER DRIVE UNIT CONTROL VALVE MODULE LEAKING HYDRAULIC FLUID. THE ODOR OBSERVED IS SUSPECTED TO HAVE BEEN CAUSED BY THE FUMES FROM THE HYDRAULIC FLUID WHICH ENTERED THE PACK INLET. THE POWER DRIVE UNIT VALVE WAS REMOVED AND REPLACED IAW MM 27-81-06. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE ELECTRICAL SMELL COULD NOT BE DUPLICATED. THE RECIRCULATION AIR FILTERS WERE ALSO REMOVED AND REPLACED IAW MM 21-25-02. 2L72 4F RTA2NM 20040406001192004040600119NM 2004 4 6 CALA0400267 120040322A5313BAC1498156 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A .5 INCH CRACK IN STRINGER S23L AT STA 1040, FORWARD OF TAIL COMPARTMENT ACCESS DOOR. REPAIRED IAW SRM 53-00-03, FIGURE 202. 2L72 4F RTA16WE 20040406001402004040600140 2004 4 6 SWIA200413064 420040320A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA STICK SHAKER DISCONNECTED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07910SW 7566 FIRST OFFICER'S STICK SHAKER WIRE LEAD DISCONNECTED FROM SHAKER MOTOR. RECONNECTED WIRES ON FIRST OFFICER'S STICK SHAKER. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040407000042004040700004EU 2004 4 7 EPUA070304A 120040307A2612991034512 FIRE LOOP REIMS 406 F406 7535723EU PWA PT6 PT6A112 52043NE RT ENGINE CHAFED E EPUAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 AL03406GV F4060049 AS FLIGHT ENTERED DOWNWIND, THE RT FIRE WARNING LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN AND FLIGHT LANDED WITHOUT INCIDENT. MX FOUND THE AFT FIRE LOOP WAS CHAFFED UNDER CLAMP. 1L72 3T3 TRTA54EU E4EA 20040407000102004040700010EA 2004 4 7 ASOA04174 120040303A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR THRESHOLD SILL AT THE FORWARD LATCH FITTING, FS 562.72 - 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLORO THRESHOLD SILL AT THE FORWARD LATCH FITTING, FS 562.72 - 589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040407000142004040700014EA 2004 4 7 ASOA04184 120040308A3220521153 ARM CNDAIRCL600 CL6002C10 1390015EA NLG DISCONNECTED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11723EV 10132 FLT 4930 - DURING TAKEOFF FROM SNA-DFW, THE GEAR HANDLE WAS FOUND STUCK IN THE DOWN POSITION, FOLLOWED BY A SINGLE CHIME AND A WEIGHT ON WHEELS INPUT CAUTION MESSAGE. QRH PROCEDUES WERE COMPLEID WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED TO SNA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE UPPER AND LOWER NOSE LANDING GEAR NLG TORQUE ARM ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000192004040700019EA 2004 4 7 ASOA04163 120040228A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-71-00. (M) 2L72 4F RTA21EA 20040407000262004040700026EA 2004 4 7 ASOA04159 120040228A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000272004040700027EA 2004 4 7 ASOA04181 120040307A5210601R380741 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE INSPECTED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR AND FOUND THE CRACK TO BE WITHIN LIMITS. THE CRACK IS TO BE MONITORED AT EVER SERVICE CHECK AND THE ANCHOR FITTING IS TO BE REPLACED WITHIN 100 FLIGHT HOURS IAW REO 601R-52-11-272. AIRCRAFT OK FOR SERVICE. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040407000332004040700033EA 2004 4 7 ASOA04176 120040303A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11834AS 7254 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES ON THE LEFT AND RIGHT SIDES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLES ON THE LEFT AND RIGHT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040407000452004040700045NM 2004 4 7 USAA040019 120040119A5320 SILL BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 CLT - FOUND DOOR SILL CORRODED 1 INCH BY 1 INCH AREA, LBL 58, BS 310.5 TO BS 324 CABIN FLOOR LEVEL. REMOVED AND REPLACED LOWER DOOR SILL CHORD DOUBLER AND CHORD ANGLE PER BOEING DWG 141N8422, SM 51-10-02. (M) 2L72 4F RTA2NM 20040407000782004040700078NM 2004 4 7 USAA040012 120040201A5310 DOOR FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US51807 23313 PIT - FOUND FRAME CRACKED .5 INCH, LOWER AFT CORNER UNDER DOOR STOP FITTING. SPLICED IN NEW FRAME SECTION, REPLACED CORNER ANGLE AND DOUBLER PER SRM 51-70-11. (M) 2L72 4F RTA16WE 20040407000802004040700080NM 2004 4 7 USAA040014 120040113A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US49080 23319 CLT - FOUND SKIN CRACKED .008 INCH, FS 727E JUST BELOW S24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040407000822004040700082NM 2004 4 7 USAA040016 120040115A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19406US43801 23876 CLT - FOUND SKIN CRACKED .600 INCH CRACK, FS 727D JUST BELOW S23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 231. (M) 2L72 4F RTA16WE 20040407000842004040700084NM 2004 4 7 USAA040003 120040212A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU47922 23705 PIT - FOUND FORWARD BULKHEAD WEB CRACKED .5 INCH, 178 BULKHEAD WEB AT UPPER LEFT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664, PATCH, PER SRM 53-10-08 FIG 211. (M) 2L72 4F RTA16WE 20040407001112004040700111SO 2004 4 7 MASA200400036 120040116A5210 DOOR EMB 145 EMB145LR 3260212SO MAIN PAX OUT OF ADJUST A MASAK NONE O OTHER ININSP/MAINT 1 SW07837MJ 145367 CREW REPORTED THE MAIN CABIN DOOR HARD TO OPEN. MX TROUBLESHOT THE SYSTEM AND ADJUSTED THE DOOR LIFT ROD AND LUBRICATED ALL TRACK ROLLER BEARINGS. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040407001132004040700113SO 2004 4 7 MASA200400103 120040224A36208166243 SENSOR EMB 145 EMB145LR 3260212SO BLEED TEMP INOPERATIVE A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW07842MJ 145457 BLEED 2 OVERTEMP WARNING MESSAGE ON EICAS IN-FLIGHT. MX REPLACED THE NR 2 BLEED TEMP SENSOR. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040407001252004040700125EA 2004 4 7 MASA200400169 120040328A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777286 7286 A CEILING EMERGENCY LIGHT WAS INOP. MX RELAMPED. 2L72 4F RTA21EA 20040407001282004040700128EA 2004 4 7 MASA200400054 120040130A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747239 7239 EMERGENCY FLOOR LIGHTS AFT RT SIDE INOP. MX DEFERRED. 2/8/2004. MX REPLACED THE LAMP. OP CHECKS GOOD. 2L72 4F RTA21EA 20040407001292004040700129EA 2004 4 7 MASA200400067 120040205A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 CAPT REPORTED THE RIGHT HAND AFT OVER THE WING, EXTERIOR EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2L72 4F RTA21EA 20040409000032004040900003EU 2004 4 9 MALA040286 120040323A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 RIGHT I/B SEAT TRACK HAS SEVERE CORROSION AT STA 297. REMOVED AND REPLACED SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/27/04. 2L72 4T RTA52EU 20040409000082004040900008SO 2004 4 9 LR7A04033 120040401A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 400 4698 DURING A-CHECK INSPECTION PER JOB CARD HA1200 FOUND 3 INCH CRACK ON WEB LEFT FS 924. REPAIR CARRIED OUT IAW SMP583 53-50-04, REF FIG 51-140-17. 2H74 4T A1SO 20040409000092004040900009NE 2004 4 9 AWXA200400233 220040227A7532AC69924 BLEED VALVE AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28653AW17747 1003 ON CLIMBOUT AT APPROX 1500 FT HEARD A LOUD BANG & AC SHUTTERED, ECAM INDICATED NR 2 ENG STALL, AFTER ECAM MESSAGE ENG OPERATED NORMALLY. TURNED BACK & LANDED WITHOUT FURTHER EVENT. MX BORESCOPED HPC 3 & 6 STAGE, NO DEFECTS NOTED. PERFORMED PRESSURE BURNER SENSOR TEST, INSPECTED PRESSURE SENSOR TUBE. PERFORMED VARIABLE STATOR VANE RIG CHECK, INSPECTED VSV MECHANISM, AND LUBED VSV RINGS, NFF. PERFORMED BLEED VALVE SOLENOID TEST, TEST FAILED, REMOVED & REPLACED 7TH STAGE BLEED VALVE, AND 7TH STAGE BLEED SOLENOID VALVE. ENG RUN, TEST GOOD. PART NAME; VALVE, SOLENOID 7TH STAGE BLEED, MFG; DUNLOP AEROSPACE; P/N; AC69386, S/N; MN501, TT; 38554, TC; 17429, TSR; 9435. 2L72 4F4 FRTA28NM E311NE 20040409000102004040900010EU 2004 4 9 MALA040278 120040317A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 DURING 4Y/2Y INSPECTION IN LCQ, FS 297 LT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO NR S53060. A/C RELEASE DATE 3/22/04. 2L72 4T RTA52EU 20040409000152004040900015NM 2004 4 9 AWXA200400299 120040308A575465C26794 SKIN BOEING737 7373S3 1384711NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 PHX - MAJOR REPAIR - DURING 8-DAY CHECK SEVERAL CRACKS WERE FOUND PROGRESSING FROM RIVET HOLES ON LOWER LT EDGE OF NR 2 SLAT, SLAT STA 200. MAINTENANCE CUTOUT DAMAGE ON LOWER LT EDGE OF NR 2 SLAT, AT SLAT STA 200; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-01 FIG 206 PG 1. 2L72 4F RTA16WE 20040409000302004040900030EU 2004 4 9 MALA040282 120040322A5412216341205 FIRESHIELD BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 NACELLE CRACKED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15520XJ E2345 NR 4 ENGINE FIRE LIGHT ILLUMINATED. BLEW 1ST BOTTLE, LIGHT STILL ON, BLEW 2ND BOTTLE, LIGHT DID NOT EXTINGUISH FOR APPROXIMATELY 1 MINUTE. ABORTED TAKEOFF AT 95 KTS. NO VISIBLE INDICATION OF FIRE. INSPECTED BY FIRE DEPARTMENT. CREW DID NOT SWITCH LOOPS TO VERIFY FIRE INDICATION. MX REMOVED FDAMS CARD AND FORWARDED TO AVIONICS. MAINTENANCE CHANGED NR 4 FUEL MANIFOLD. WHILE CHANGING THE NR 4 FUEL MANIFOLD MAINTENANCE FOUND LOWER HALF OF FIRESHIELD CRACKED, AND BENT AT 6 O'CLOCK POSITION. INSTALLED FIRESHIELDS P/N 2-163-412-05, S/N 992463707662. 2H74 4F4 FRTA49EU E6NE 20040409000452004040900045NM 2004 4 9 AALA20040384 120040323A2560 LATCH HANDLE BOEING757 757223 1384957NM RAFT COMPARTMENTBROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21662AA 25296 CLO - RIGHT HAND AFT RAFT OVERHEAD COMPARTMENT LATCH HANDLE IS BROKEN. RAFT COMPARTMENT WILL NOT OPEN DURING NORMAL OR EMERGENCY PROCEDURES AND COULD NOT BE OPEN FOR SECURITY CHECKS. PARTS NOT IN STOCK AT CLO. FERRIED AIRCRAFT TO MIA FOR REPAIR PER SPOTTING MESSAGE 03-098 DATED 3/23/04. REPLACED RIGHT HAND LATCH HANDLE ASSEMBLY FOR RIGHT HAND AFT RAFT OVERHEAD COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040409000462004040900046WP 2004 4 9 AALA20040385 120040323A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 DFW - SEAT EMERGENCY PATH LIGHT AT ROW 8 INOPERATIVE. REPLACED SOCKET, BULBS, AND LENSE FOR SEAT EMERGENCY PATH LIGHT AT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000502004040900050NM 2004 4 9 AALA20040383 120040323A3350 LIGHT BOEING757 757223 1384957NM EXIT SIGN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21658AA 24616 DFW - EMERGENCY EXIT LIGHT AT DOOR 2L IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT DOOR 2L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040409000562004040900056SO 2004 4 9 MASA200400161 120040323A3397 WIRE EMB 145 EMB145LR 3260212SO EXIT SIGN OUT OF ADJUST A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 CABIN CEILING EMERGENCY EXIT SIGN IN ROW 12 INOP ON BACKSIDE. MX ADJUSTED WIRING TO SIGN. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040409000922004040900092NM 2004 4 9 2004UALA00299 120040330A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 BS 767 STR 22L AND STR 23L HAVE CRACKED SHEAR TIES. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040409001022004040900102EA 2004 4 9 SWIA200413072 120040314A2751855D1009 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07407SW4481 4481 7034 RECEIVED FLAPS FAIL, DID QRH. LANDED SLC 0 DEGREES FLAPS. REMOVED AND REPLACED LEFT BPSU IAW AMM 27-51-10 AND RIGGED FLAPS. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040409001062004040900106SO 2004 4 9 SWIA200413076 120040321A2750 CONTROL HANDLE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07233SW 120307 WHEN ON APPROACH, SELECTED FLAPS 25 GOT CONTROL FAULT. REPLACED FLAP HANDLE. OPS CHECK GOOD. P/N ON 120-54207-615, S/N OFF 120338. 2L72 4T4 TRTA31SO E20NE 20040409001232004040900123WP 2004 4 9 AALA20040386 120040325A4990 O-RING DOUG DC9 DC982 3022082WP APU CHIP DETECT INOPERATIVE A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21423AA 49335 JFK - INFLIGHT T1453 AFTER TAKEOFF FROM LGA, FLIGHT ATTENDANT AND FLIGHT CREW NOTICED ODOR. CABIN VISIBILITY REDUCED BY BLUE/GRAY SMOKE OBSCURING VISION FROM FORWARD TO AFT CABIN. TURNED OFF PACKS, GALLEY POWER, AND RECIRCULATING FANS WITH NO AFFECT. LANDED AT JFK WITHOUT INCIDENT. FOUND APU CHIP DETECTOR O-RING LEAKING. REPLACED APU CHIP DETECTOR O-RING, ACCOMPLISHED PACK BURN AND PLACARD APU PER MEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001342004040900134EA 2004 4 9 SWIA200413055 120040309A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION CARGO PIT; FLOORBEAM ANGLE IS CRACKED; FS 621.00 RBL 38.0. REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII 53-401. 2L72 4F RTA21EA 20040409001382004040900138NM 2004 4 9 AALA20040367 120040220A5751 FITTING BOEING767 767323 1385205NM AILERON HINGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21378AN 25447 AFW - RIGHT HAND INBOARD AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED AT 1.24 INCHES. FINAL MEASUREMENT AT 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PERMANENT REPAIR (CLIP). REPAIR ANGLE CLIP FABRICATED OUT OF 7075-T6 AND FASTENED TO AILERON RIB TO PROVIDE A SUPPORT FOR FIXED TRAILING EDGE PANEL STIFFENER PER MRB 767-2560 DATED 2/18/04. 2L72 4F RTA1NM 20040409001392004040900139NM 2004 4 9 AALA20040368 120040317A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 AFW - CORROSION REMOVED AT FLOORBEAM AT RIGHT BUTTOCK LINE 24, 30, 33, 45, 52, 56, 58, 60, 62, 65, 66, 68, 70, AND 73. LARGEST BLEND IS AT RIGHT BUTTOCK LINE 66 AND IS 1.0 INCH BY 0.050 INCH AND 0.050 INCH DEEP AT STATION 347. REMOVED CORROSION. FABRICATED REPAIR STRAP FROM 301 1/2H STAINLESS STEEL 0.050 INCH THICK. ENSURED AT LEAST TWO ROWS EITHER SIDE POST DAMAGE. ALODINED ALL BARE ALUMINUM SERVICES AND FINISHED BLENDS AND REPAIRED STRAP WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS 5-95. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALANT AND FASTENERS. 2L72 4F RTA1NM 20040409001402004040900140WP 2004 4 9 AALA20040364 120040317A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217542A 49996 DFW - EMERGENCY CEILING LIGHTS BETWEEN AFT LAVATORIES IS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY CEILING LIGHTS BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001422004040900142WP 2004 4 9 AALA20040372 120040321A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21407AA 49318 DFW - EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001432004040900143EU 2004 4 9 MALA040291 120040311A5520 ACCESS PANEL BAC 146 AVRO146RJ85A1500097EU RT ELEVATOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15512XJ E2326 DURING C-CHECK INSPECTION IN LCQ, PWI PER BAE FAX BARA/ARV/5805/02-DC, REPLACED RIGHT ELEVATOR ACCESS PANEL 336 C/B LANDING PLATE WITH NEW OR SERVICEABLE ITEM AT NEXT HEAVY CHECK. REMOVED, FABRICATED AND INSTALLED LANDING PLATE IAW MESABA EO NR A55233. A/C RELEASE DATE 3/30/04. 2H74 4F RTA49EU 20040409001442004040900144 2004 4 9 MALA040293 420040330A3410102CP2AF TAT PROBE SAAB SF340 340B 7860101EU MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15368PX 340B274 DURING FLIGHT OAT SHOWING -68, FLIGHT DIRECTOR OFF, AUTOPILOT OFF. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED TAT PROBE P/N ON&OFF 102CP2AF, S/N ON A18795, S/N OFF 90299, TAT PROBE OPS CHECKS GOOD IAW SF340 M/M CHAP 34. 2L72 4T RTA52EU 20040409001482004040900148 2004 4 9 SWIA200413057 420040317A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07224SW4800 4800 120294 WHEN A/P ON CAPTAIN'S SIDE, OCCASIONALLY THE A/P WOULD INITIATE A CLIMB, THEN DESCENT ON ITS OWN. A/P AURAL DID NOT COME ON, SEEMED LIKE AN ELEVATOR FLUCTUATION. REPLACED NR 1 APC-65B IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00. P/N: 622-8315-402, S/N ON: 2966, S/N OFF: 2947. 2L72 4T RTA31SO 20040409001492004040900149SO 2004 4 9 SWIA200413058 120040316A3397 SIGN EMB 120 EMB120ER 3260203SO ROW 9 INOPERATIVE A SWIAO OTHER LP NO TEST NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07196SW 120151 EXIT SIGN ABOVE ROW 9 WILL NOT ILLUMINATE. FOUND BROKEN WIRE AT EMERGENCY EXIT SIGN AT ROW 9. INSTALLED SPLICE AT WIRE. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040409001502004040900150EA 2004 4 9 SWIA200413059 120040318A27603G5209C LEVER CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07959SW 7840 ON APPROACH, GOT STATUS MESSAGES FLIGHT SPOILER FAULT AND OUTBOARD GROUND SPOILER FAULT. REMOVED AND REPLACED CONTROL LEVER. NO DEFECTS NOTED AT THIS TIME. OPS CHECKS GOOD IAW 27-61-01. S/N OFF G1007. 2L72 4F RTA21EA 20040409001512004040900151WP 2004 4 9 CALA0400281 120040324A29107936907665 LINE DOUG DC9 DC983 3022083WP RUDDER CON VLV LEAKING A CALAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW2714879 49526 THE RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED WHILE EN ROUTE FROM SFO TO IAH. THE LOSS WAS ACCOMPANIED BY HYDRAULIC FLUID FUMES AND HAZE IN THE CABIN WHEN THE HYDRAULIC FLUID WAS INJESTED INTO THE PACK SYSTEM. THE AIRCRAFT LANDED AT IAH AND PASSENGERS WERE EVACUATED VIA THE R-1 DOOR SLIDE AND TAIL CONE SLIDE. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE TO THE RUDDER CONTROL VALVE IN THE TAIL COMPARTMENT BROKEN. THE LINE WAS REMOVED AND REPLACED AND A PACK BURNOUT WAS ACCOMPLISHED. IN ADDITION, THE R-1 DOOR SLIDE AND TAIL CONE SLIDE WERE REMOVED AND REPLACED IAW MM 25-62-00 AND 25-62-01. 2L72 4F RTA6WE 20040409001542004040900154NM 2004 4 9 CALA0400284 120040326A335020131A BATTERY BOEING757 757224 1384958NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2734137 30229 THE R-2 DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. A NEW BATTERY PACK WAS INSTALLED IAW MM 33-51-07. 2L72 4F RTA2NM 20040409001552004040900155 2004 4 9 AT0400007 420040325A2565D29982225 SLIDE BOEING717 717200 1383700NM L1 DOOR UNSERVICEABLE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15954AT 55016 L1 DOOR EVACUATION SLIDE PRESSURE INDICATES JUST OUT OF GREEN ARC. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE PER B717 AMM 25-61-01. 2L72 4F TRA6WE 20040409001562004040900156EA 2004 4 9 MASA200400095 120040221A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717231 7231 THE LEFT WING EMERGENCY EXIT LIGHT WAS INOP. PLACED ON MEL 33-51-2. RELAMPED LIGHT. 2L72 4F RTA21EA 20040409001572004040900157SO 2004 4 9 MASA200400118 120040301A3350550531621 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07859MJ 145769 CABIN RIGHT SIDE OVERWING EXIT SIGN WILL NOT ILLUMINATE. MX REPLACE THE INVERTER. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409001592004040900159WP 2004 4 9 AALA20040428 120040403A2820 PUMP DOUG DC9 DC982 3022082WP FUEL TRANSFER INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21226AA 49176 DFW - INFLIGHT T1118 FUEL WOULD NOT FLOW FROM CENTER TANK AND ALL THREE AFT CENTER PUMP CIRCUIT BREAKERS WERE POPPED. LANDED WITHOUT INCIDENT AT DFW. RESET CIRCUIT BREAKERS, RAN PUMP AND TRANSFERRED FUEL. COULD NOT DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001602004040900160NM 2004 4 9 AALA20040429 120040405A3350 LIGHT BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21374AA 25201 SFO - EMERGENCY LIGHT AT LOWER END OF RIGHT HAND FIRST CLASS GALLEY HAS BROKEN BASE AND MISSING LENS COVER. REPLACED BASE AND LENS COVER FOR EMERGENCY LIGHT AT LOWER END OF RIGHT HAND FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040409001622004040900162NM 2004 4 9 AALA20040423 120040404A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21177AN 32396 ORD - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040409001632004040900163NM 2004 4 9 AALA20040427 120040404A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21973AN 29548 BOS - EMERGENCY LIGHTS IN FORWARD COACH SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD COACH SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040409001642004040900164EU 2004 4 9 AALA20040432 120040402A5311 FRAME AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2180057 465 TUL - SHEAR TIE ON FRAME 18 AT STATION 1340 HAS A 2 INCH BY 2 INCH SECTION OF CORROSION. REPAIRED FRAME 18 AT STATION 1340 PER SRM 53-10-13. 2L72 4F RTA35EU 20040409001692004040900169NM 2004 4 9 AALA20040370 120040321A3350P4010049 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219412W 53187 SEA - SEAT MOUNTED ESCAPE PATH LIGHTS AT ROWS 20 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT SEAT MOUNTED ESCAPE PATH AT ROWS 20 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040409001702004040900170NM 2004 4 9 CALA0400290 120040329A5320BAC1496377 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED AT STA 727-767 IN THE AFT CARGO COMPARTMENT. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040409001712004040900171NM 2004 4 9 CALA0400291 120040329A5210141A61503 SKIN BOEING737 737824 13844BZNM L-1 DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776269 31588 INSPECTION FOUND A CREASE IN SKIN AT AFT UPPER CORNER OF L-1 PASSENGER DOOR. REPAIRED IAW ECRA 5210-01756. 2L72 4F RTA16WE 20040409001722004040900172NM 2004 4 9 CALA0400292 120040328A2497UNK WIRE BOEING757 757224 1384958NM UTILITY BUS CHAFED A CALAK NONE AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2758101 27291 MAINTENANCE NOTICED SMOKE WHEN POWERING UP THE AIRCRAFT TO ACCOMPLISH A GEAR SWING WHILE THE AIRCRAFT WAS IN HEAVY CHECK AT YXX. WHEN MAINTENANCE FOUND THE SOURCE OF THE SMOKE THE FIRE HAD SELF EXTINGUISHED. EVIDENCE OF FIRE EXISTED FROM THE HEAT DAMAGE AND CHARRING IN THE AREA OF THE E2-1 RACK OUTBOARD, APPROXIMATELY STA 420-500. INITIAL INVESTIGATION REVEALED THAT THREE WIRES FROM THE LT AC UTILITY BUS CHAFED AGAINST THE E&E SUPPORT STRUCTURE AND THEN ARCING OCCURRED. HEAT DAMAGE TO THE STRUCTURE IS BEING EVALUATED. AN FCD WILL BE ISSUED TO INSPECT THE REST OF THE FLEET. 2L72 4F RTA2NM 20040409001752004040900175NM 2004 4 9 CALA0400295 120040330A5320143A7505 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND RIGHT Z-CHANNEL SUPPORT CRACKED AT SCREW HOLE IN FORWARD CARGO AREA AT STA 500F TO 500G. THE Z-CHANNEL SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-00-53 AND 53-30-53. 2L72 4F RTA16WE 20040409001762004040900176NM 2004 4 9 AALA20040371 120040321A3350 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY SIGN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219412W 53187 SEA - EMERGENCY EXIT SIGN AT SIDEWALL JUST FORWARD OF SEAT 21F INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT SIDEWALL JUST FORWARD OF SEAT 21F. SYSTEM CHECKED NORMAL OPERATION. 2L72 4F RT 20040409001802004040900180EA 2004 4 9 MASA200400124 120040302A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727318 7318 PILOT REPORTED THE OVERWING EXIT LIGHT WAS INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001812004040900181EA 2004 4 9 MASA200400125 120040303A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717337 7337 PAX DOOR EMERGENCY FLOOD LIGHT INOP. MX REPLACED BULB, OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001822004040900182EA 2004 4 9 MASA200400126 120040303A3350AE20131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747239 7239 ALL EMERGENCY LIGHTS WERE INOP. MX FOUND THE EMERGENCY LIGHT SWITCH HAD BEEN LEFT ON. ALL BATTERIES WERE DRAINED. MX REPLACED ALL 4 BATTERY PACKS. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001832004040900183EA 2004 4 9 MASA200400135 120040312A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727173 7173 RIGHT AFT EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001842004040900184SO 2004 4 9 MASA200400136 120040312A33501317 BULB EMB 145 EMB145LR 3260212SO FLOOD LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07832MJ 145310 AFT OVERHEAD EMERGENCY EXIT FLOOD LIGHT INOP. MX RELAMPED, OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409001862004040900186SO 2004 4 9 MASA200400139 120040312A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 CREW REPORTED THE EMERGENCY EXIT ROW LIGHT WAS INOP. MX RECONNECTED THE CONNECTOR TO THE LIGHT ASSY. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040409001872004040900187EA 2004 4 9 MASA200400140 120040313A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717275 7275 DURING PRE-FLIGHT, THE CREW FOUND THE EMERGENCY EXIT SIGN IN THE GALLEY WAS INOP. MX REPLACED THE BULBS. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001902004040900190EA 2004 4 9 MASA200400159 120040322A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777260 7260 CREW REPORTED THE PAX EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001912004040900191EA 2004 4 9 MASA200400167 120040327A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777278 7278 LEFT WING EMERGENCY LIGHT INOP. MX RELAMPED. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001922004040900192WP 2004 4 9 MWEA040036 120040326A5752 SKIN DOUG DC9 DC981 3022081WP AILERON TAB CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 LEFT AILERON UPPER SURFACE FORWARD INBOARD EDGE, STAINLESS STEEL CHAFE PLATE IS LIFTING UP ON THE AFT END, ALSO CORROSION IS EVIDENT ALONG THE INBOARD AND OUTBOARD EDGES AND SEEMS TO GO UNDER CHAFE PLATE. FABRICATED AND INSTALLED FILLER AND REPAIR STRIP. 2L72 4F A6WE 20040409001952004040900195WP 2004 4 9 MWEA040039 120040329A5553991183879 FRAME DOUG DC9 DC981 3022081WP VERTICAL STAB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 AFT ACCESSORY CANTED FRAME WEB HAS A CRACK LOCATED JUST RIGHT OF FORWARD VERTICAL STABILIZER FRONT ATTACH TANG. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040409001962004040900196WP 2004 4 9 MWEA040040 120040329A55429951485513 SKIN DOUG DC9 DC981 3022081WP LEFT RUDDER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RUDDER SKIN LEFT SIDE IS DENTED BETWEEN RIBS 12 AND 13 FROM TOP AT CENTER OF PANEL. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040409001982004040900198WP 2004 4 9 MWEA040043 120040329A53129936719125 BULKHEAD DOUG DC9 DC981 3022081WP FUSELAGE PUNCTURED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 STATION 218 AT LONGERON 27 RIGHT THE 218 BULKHEAD HAS A PUNCTURE APPROXIMATELY 6 INCHES ABOVE LONGERON 27 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040409001992004040900199WP 2004 4 9 MWEA040044 120040329A531099579457 DOOR FRAME DOUG DC9 DC981 3022081WP MID CARGO CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 MID CARGO PIT DOOR JAMB FORWARD HINGE, FORWARD SUPPORT IS CHAFED AT THE HINGE BOLT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040409002012004040900201WP 2004 4 9 MWEA040042 120040329A5313591140887 LONGERON DOUG DC9 DC981 3022081WP FUSLEAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 LONGERON 4 LEFT IS CRACKED AT FRAME STATION 541. FABRICATED AND INSTALLED LONGERON AND SPLICES. 2L72 4F A6WE 20040409002022004040900202WP 2004 4 9 MWEA040046 120040329A523059101419 ANGLE DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 CRACK ON DOOR PAN AFT SIDE OF PAN NEAR TORQUE TUBE END CAM FORWARD CARGO DOOR. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20040412000062004041200006EA 2004 4 12 ASOA04133 120040218A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040412000082004041200008EA 2004 4 12 ASOA04135 120040218A339764645 CABLE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 DURING HANGAR MAINTENANCE IN MCN, THE AFT EMERGENCY FLOOR LIGHT SECTION WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT CABLE ASSEMBLY AND CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040412000092004041200009EA 2004 4 12 ASOA04136 120040218A5210601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE FORWARD CABLE ANCHOR POINT ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CABLE ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040412000102004041200010EA 2004 4 12 ASOA04137 120040218A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA ENG SUPPORT BEAMCRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23865AS 7507 DURING A C-CHECK IN MCN, THE CLIPS BELOW THE ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDES AT FS 621 WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS BELOW THE ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDES AT FS 621. (M) 2L72 4F RTA21EA 20040412000112004041200011NM 2004 4 12 USAASB04019 120040217A3397 WIRE BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US 23985 MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO SEAT ROWS ON LEFT SIDE OF CABIN WERE INOPERATIVE. MAINTENANCE REPAIRED WIRING AT THE EMERGENCY LIGHTS ON SEAT ROWS 24 AND 25, LEFT SIDE. ALSO, REPLACED M1479 AND M1137 BATTERY PACKS, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040412000152004041200015EA 2004 4 12 ASOA04213 120040315A5320601R3117115 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, RBL APPROXIMATELY 28 AND 36 WERE FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, RBL APPROXIMATELY 28 AND 36 AND AT FS 484, BL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040412000162004041200016WP 2004 4 12 GTIA040205 120040219A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND MAIN CABIN F/B FS 1078-1155 LBL 30 IS DELAMINATED AND DAMAGED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040412000182004041200018WP 2004 4 12 GTIA040203 120040223A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND MAIN CABIN F/B FS 256-312 CENTER IS DAMAGED AND DELAMINATED AT INSERTS. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040412000192004041200019WP 2004 4 12 GTIA040204 120040228A5320 WEB DOUG DC9 DC983 3022083WP FS CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR WEB CRACKED STATION 218 RBL 44 UNDER SEAT TRACK. REMOVED DAMAGED SECTION OF WEB. DRILLED AND LOCATED REPAIR. INSTALLED REPAIR. (M) 2L72 4F RTA6WE 20040412000202004041200020WP 2004 4 12 GTIA040182 120040216A5553 ATTACH ANGLE DOUG DC9 DC982 3022082WP DORSAL FIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND LEFT SIDE DORSAL FIN ATTACH ANGLE CRACKED AND GOUGED THROUGH VERTICAL LEG INTO 1ST ROW OF HORIZONTAL. REMOVAL LEFT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND INNER ATTACH ANGLE LEFT SIDE CRACKED SEVERAL PLACES. REMOVED LEFT INNER ATTACH ANGLE. LOCATED AND DRILLED HOLES ON INNER ANGLE. LOCATED AND DRILLED HOLES ON OUTER ANGLE. INSTALLED INNER ATTACH ANGLE. INSTALLED OUTER ANGLE AND PLATE DOUBLER. (M) 2L72 4F A6WE 20040412000222004041200022WP 2004 4 12 GTIA040185 120040217A7830 DOOR DOUG DC9 DC982 3022082WP THRUST REVERSER CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND RIGHT THRUST REVERSER UPPER DOOR INBOARD SIDE CRACKED AND BENT. REMOVED DOUBLER. STOP DRILLED END OF CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040412000242004041200024 2004 4 12 GTIA040178 420040312A2565 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 LAS - FLT 1108 - L1 DOOR SLIDE PACK HAS SLIPPED DOWN OUT OF ITS JACKET. REINSTALLED SLIDE L-1 DOOR. (M) 2L72 4F RT 20040412000262004041200026WP 2004 4 12 GTIA040180 120040311A2612892809040003 AMPLIFIER DOUG DC9 DC983 3022083WP A-FIRE LOOP MALFUNCTIONED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FLT 705 - LGA - 'A' LOOP RIGHT ENGINE ON AFTER FIRE ENGINE TEST. T/S THE RIGHT ENGINE FIRE DETECTION 'A' LOOP SYSTEM, DETERMINED THE UPPER AND LOWER BARRIER AND ENGINE 'A' LOOP RES, CHECKS GOOD. REMOVED AND REPLACED THE FIRE DETECTOR AMP, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20040412000292004041200029NE 2004 4 12 GTIA040187 220040213A7230 NOSE COWL DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 2 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - NR 2 NOSE COWL LIP RING HAS OVERHEAT INDICATIONS. MEASUREMENTS OBTAINED EXCEEDED UPPER LIMIT FOR 2024-T42 MATERIAL. NR 2 ENGINE NOSE COWL S/N 099-362. REMOVED AND REPLACED SAS WO B00127-11N-00001. (M) 2L72 4F4 F A6WE E9NE 20040412000302004041200030WP 2004 4 12 GTIA040186 120040219A5532 PANEL DOUG DC9 DC982 3022082WP DORSAL FIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND DORSAL FIN PANEL FORWARD 9 EACH FASTENER HOLES CRACKED, CHAFED, AND BROKEN OUT. FABRICATED DOUBLER. BLENDED OUT CRACKED AREAS. INSTALLED DOUBLER. (M) 2L72 4F A6WE 20040412000312004041200031WP 2004 4 12 GTIA040200 120040213A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND RIGHT OUTBOARD SEAT TRACK CORRODED SEVERAL AREAS FROM FS 237-1309. FS 351-807 AND FS 1032-1309 OUT OF LIMITS. REMOVED SEAT TRACK BETWEEN STATION 351-798 AND STATION 1032-1309. FABRICATED SEAT TRACK SEC'S FS 200-807 AND REPAIR SPLICES. FABRICATE NEW SEAT RACK SECTION FS 1032-1309 AND REPAIR SPLICES. INSTALLED NEW SEAT TRACK SEC'S FS 200 AND 807 AND REPAIR SPLICES. INSTALLED NEW SEAT TRACK SEC FS 1032-1309 AND REPAIR SPLICES. (M) 2L72 4F RTA6WE 20040412000322004041200032WP 2004 4 12 GTIA040201 120040218A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK RBL 44 INCEHS STATION 200 TO 256 HAS CORROSION. SEAT TRACK RBL 44 STATION 200-245 OUT OF LIMITS. FABRICATED NEW SEAT TRACK SECTION AND SPLICE. INSTALLED SECTION OF SEAT TRACK AND SPLICE. (M) 2L72 4F RTA6WE 20040412000342004041200034WP 2004 4 12 GTIA040189 120040304A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR PANEL 200-237 STAINED, DETERIORATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000382004041200038WP 2004 4 12 GTIA040197 120040304A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FORWARD CABIN STATION 120 RBL 28, 34 INCHES, 38 INCHES, 45 INCHES HAS PUNCTURE/DAMAGED ON DIAPHRAM WEB PANEL. REMOVED DAMAGED AREAS. FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND FLOOR SUPPORT. FURTHER FOUND DAMAGED AT SUB FLOOR WEB STATION 120 RBL 12 INCHES. REMOVED DAMAGED WEB. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AT FLOOR WEB STATION 120 RBL 12 INCHES. INSTALLED DOUBLER AND FLOORBOARD SUPPORT AT STATION 120 RBL 28 TO 45. (M) 2L72 4F RTA6WE 20040412000392004041200039WP 2004 4 12 GTIA040194 120040305A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND COCKPIT CENTER FLOOR PANEL, CORNERS BROKEN OUT DRAIN PLATE CORRODED, DETERIORATING. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000412004041200041WP 2004 4 12 GTIA040196 120040305A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR PANEL BETWEEN AFT LAVS, STAINED, CORNER DELAMINATED. REPAIRED CORNER DELAMINATION. (M) 2L72 4F RTA6WE 20040412000432004041200043WP 2004 4 12 GTIA040191 120040304A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR PANEL STATION 160-200 LEFT OUTBOARD DELAMINATED, INSERTS MISSING, CRACKED, EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000442004041200044WP 2004 4 12 GTIA040199 120040213A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND LEFT INBOARD SEAT TRACK CORRODED SEVERAL AREAS FROM FS 297-1022. AFTER FURTHER INSPECTION FOUND LEFT INBOARD SEAT TRACK CORRODED AND OUT OF LIMITS FROM FS 1022 TO FS 1039. FABRICATED SEAT TRACK SECTION. INSTALLED SEAT TRACK SECTION AND SPLICE. (M) 2L72 4F RTA6WE 20040412000452004041200045WP 2004 4 12 GTIA040202 120040218A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK LBL 38 STATION 1136 TO STATION 1097 HAS CORROSION. REMOVED OUT OF LIMITS SEAT TRACK, LBL 38 STATION 1136-1097. FABRICATED NEW TRACK. INSTALLED TRACK. (M) 2L72 4F RTA6WE 20040412000462004041200046EA 2004 4 12 ASOA04212 120040315A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE CLIP AT FS 484, LBL APPROXIMATELY 28 AND 36 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL APPROXIMATELY 28 AND 36 AND ALSO REMOVED AND REPLACED THE INTERCOSTAL AT FS 484 ON THE LEFT SIDE AT BL 27 AND 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040412000472004041200047WP 2004 4 12 ASAA0480122 120040229A53305911410531 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND FUSELAGE SKIN DENTED AT FS 212-272. REPLACED EXISTING REPAIR DOUBLER AND FILLER PER SRM 50-04. (M) 2L72 4F RTA6WE 20040412000482004041200048WP 2004 4 12 ASAA0480123 120040229A532059360263 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND MID CARGO BAY DOOR JAMB FRAME INTERCOSTAL IS CORRODED ON FRAME SHEAR TIE AT FS 674. REPLACED INTERCOSTAL PER SRM 51-30-7. (M) 2L72 4F RTA6WE 20040412000492004041200049WP 2004 4 12 GTIA040207 120040302A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FORWARD CABIN STATION 176 RBL 26 INCHES SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040412000502004041200050WP 2004 4 12 ASAA0480116 120040229A571299375682 RIB DOUG DC9 DC983 3022083WP NR 5 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND RIGHT WING NR 5 SLAT OUTBOARD END CAP RIB IS CRACKED AT RIVET HOLE. REPLACED DAMAGED END CAP RIB PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040412000512004041200051WP 2004 4 12 ASAA0480117 120040229A532199365531 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED AND BENT INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040412000562004041200056WP 2004 4 12 ASAA0480135 120040229A5730ARB0975519 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1367 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040412000572004041200057WP 2004 4 12 ASAA0480141 120040301A5754 SKIN DOUG DC9 DC983 3022083WP NR 1 SLAT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6- CHECK - FOUND NR 1 SLAT FORWARD INBOARD PIN MATING SURFACE AND CASTING HOLE IS CORRODED. REAMED HOLE AND INSTALLED BUSHING EPR EA 5740-01382. (M) 2L72 4F RTA6WE 20040412000582004041200058WP 2004 4 12 ASAA0480151 120040302A532199366541 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD X=-44 STATION 1079-1155 HAS GOUGES AROUND EDGES AND IN SKIN. FABRICATED REPLACEMENT FLOORBOARDS IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040412000642004041200064NM 2004 4 12 AWXA200400316 120040303A575465C2668628 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 5 SLAT WEDGE WAS FOUND DISBONDED ON UPPER SURFACE ABOVE ACTUATOR. MAINTENANCE REMOVED EXISTING REPAIR ON UPPER SURFACE OF NR 5 SLAT WEDGE ABOVE ACTUATOR; FABRICATED A DOUBLER & REPAIR CORE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 23 PG 85J-85M. 2L72 4F RTA16WE 20040407000492004040700049EA 2004 4 7 ASOA04153 120040222A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURNG A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 280, RBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD CLIP AT FS 280, RBL 9. (M) 2L72 4F RTA21EA 20040407000542004040700054EU 2004 4 7 SIMA200407905 120040304A5414CRES30114 SKIN SAAB SF340 340B 7860101EU LEFT NACELLE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21393AE 340B393 ABI - DURING AN MBV INSPECTION, THE RIGHT NACELLE INBOARD WALL INNER SKIN PANEL WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED FILLR AND DOUBLER. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS006747 PARA 2 DATED MARCH 3, 2004. (M) 2L72 4T RTA52EU 20040407000582004040700058SO 2004 4 7 SIMA200408201 120040320A2740367051509 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZONTAL STAB MALFUNCTIONED A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21854AE 145743 DFW - FLT 3486 - ON APPROACH INTO DFW GOT PITCH BACKUP WARNING AND PITCH MAIN WARNING. REPLACED HSCU IAW ETN EB-27-022. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040407000622004040700062EU 2004 4 7 SIMA200407902 120040301A53157253707532 STRINGER SAAB SF340 340B 7860101EU FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21393AE 340B393 ABI - DURING AN MBV INSPECTION THE STRINGER AT SL 1501 AFT OF FRAME 363, WAS FOUND TO BE GOUGED. REMOVED DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB SRM, 72LKS 3079 REV 42, 51-70-20 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040407000642004040700064EU 2004 4 7 SIMA200407907 120040303A5414 SKIN SAAB SF340 340B 7860101EU RT NACELLE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21393AE 340B393 ABI - DURING A MBV INSPECTION THE RIGHT INBOARD NACELLE OUTER SKIN PANEL WAS FOUND CHAFED BELOW SRM LIMITS AT THE FILLET FAIRING SEAL CONTRACT POINT. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, CHAPTERS 54-10-10 FIG 207. (M) 2L72 4T RTA52EU 20040407000752004040700075NM 2004 4 7 AMTA200400020 120040106A335020121 BATTERY BOEING757 75728A 1384976NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11513AT 32449 EXTERIOR EMERGENCY LIGHT AT DOOR 1 RIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY IAW MM 33-51-07. OPS CEHCK NORMAL. (M) 2L72 4F RTA2NM 20040407000772004040700077NM 2004 4 7 USAA040011 120040202A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US51807 23313 PIT - FOUND SKIN CRACKED .5 INCH, BS 727D AND S22L. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBELR PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040407000792004040700079NM 2004 4 7 USAA040017 120040117A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US53730 22954 CLT - FOUND SKIN CRACKED .900 INCH, FS 727E JUST ABOVE S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DTAIL VI VII. (M) 2L72 4F RTA16WE 20040407000812004040700081NM 2004 4 7 USAA040015 120040106A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US49080 23319 CLT - FOUND SKIN CRACKED 6.250 INCH, FS 500D PLUS 3 INCHES JUST BELOW S15R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040407000862004040700086NM 2004 4 7 AALA20040391 120040328A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21915AN 29516 MIA - EMERGENCY LIGHTS AT ROWS 11D, 13D, AND 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR FOR EMERGENCY LIGHTS AT ROWS 11D, 13D, AND 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040407000882004040700088WP 2004 4 7 AALA20040392 120040326A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21447AA 49473 DFW - EMERGENCY LIGHT ON SEAT 7D INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY FOR EMERGENCY LIGHT ON SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001002004040700100WP 2004 4 7 AALA20040400 120040330A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21451AA 49477 RDU - OVERHEAD EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001022004040700102WP 2004 4 7 AALA20040404 120040329A3350P4010051111 CONTROL MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21490AA 49683 DFW - EMERGENCY EXIT SIGN AT AFT LEFT HAND SERVICE DOOR AT AL2-7 FORWARD OF DOOR NEAR FLOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK CONTROL MODULE AL2-7 AT AFT LEFT HAND SERVICE DOOR FORWARD OF DOOR NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040407001082004040700108NM 2004 4 7 AALA20040420 120040402A3040 HEATER BOEING757 757223 1384957NM WINDOW MALFUNCTIONED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21686AA 25343 ATL - INFLIGHT T2279 SMOKE IN COCKPIT AND CABIN. LANDED WITHOUT INCIDENT IN ATL. FOUND FIRST OFFICERS WINDSHIELD HEAT HIGH VOLTAGE TAP BAD. RAN ENGINES AT HIGH POWER SETTING. NO SMOKE OR ODOR NOTED. REPLACED R1 WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040407001092004040700109NM 2004 4 7 AALA20040416 120040402A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21677AN 29427 SNA - SEAT MOUNTED EMERGENCY LIGHT AT ROWS 16 THROUGH 27DEF INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT ROWS 16 THROUGH 27DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040407001102004040700110SO 2004 4 7 MASA200400038 120040118A3610 CLAMP EMB 145 EMB145LR 3260212SO BLEED SYSTEM LOOSE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07825MJ 145179 AIRCRAFT DIVERTED TO PIT FOR AN E-2 BLEED LEAK MSG. MX WAS CALLED AND TIGHTENED A LOOSE CLAMP. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040407001312004040700131SO 2004 4 7 MASA200400093 120040220A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07842MJ 145457 LEFT FWD EXTERIOR EGRESS LIGHT INOP. MX RELAMPED. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040407001332004040700133SO 2004 4 7 MASA200400097 120040222A3350744424 SIGN EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07859MJ 145769 EMERGENCY EXIT SIGN ROW 12 RIGHT SIDE INOP. MX REPLACED SIGN ASSY, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040409000232004040900023EA 2004 4 9 MASA200400092 120040219A5270 SWITCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A MASAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW07571ML 7209 AIR-DIVERT TO CLT AFTER PAX DOOR WARNING MSG IN CRUISE. MX ADJUSTED THE DOOR POX SWITCHES. A/C WILL DO A TEST FLIGHT. TEST FLIGHT SATISFACTORY. NO PARTS USED. 2L72 4F RTA21EA 20040409000272004040900027EA 2004 4 9 MASA200400089 120040216A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775991 7422 THE RIGHT WING EMERGENCY EXIT LIGHT WAS INOP DURING TEST. MX REPLACED THE BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409000282004040900028SO 2004 4 9 MASA200400083 120040214A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07827MJ 145217 FWD FLOOR PROX LIGHTING STRIP INOP. MX REPLACED THE BULB, OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409000322004040900032NM 2004 4 9 AALA20040369 120040317A5315141T5113 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21355AA 24036 AFW - CORROSION REMOVED AT FLOORBEAM AT RIGHT BUTTOCK LINE 8, 12.5, 17, 21.5, 23, 24, 28, 30 32, 34.5, 39,40, 43.5, 44.75, 46, 47.25, 51.25, 52, AND 54. LARGEST BLEND IS AT RIGHT BUTTOCK LINE 40 AND IS 1.0 INCH WIDE AND 0.039 INCH DEEP AT STATION 325. REMOVED CORROSION. FABRICATED REPAIR STRAP FROM 301 1/2 HARD STAINLESS STEEL 0.050 INCH THICK. ENSURED AT LEAST TWO ROWS EITHER SIDE POST DAMAGE. ALODINED ALL BARE ALUMINUM SERVICES AND FINISHED BLENDS AND REPAIRED STRAP WITH TWO COATS OF BMS 10-11 PRIMER. FILLED BLENDS WITH BMS 5-95. INSTALLED REPAIR STRAP WET WITH BMS 5-95 SEALENT, PROSEAL 870, PLUS BACB30NW6 OR EQUIVALENT FASTENERS. 2L72 4F RTA1NM 20040409000342004040900034WP 2004 4 9 AALA20040380 120040323A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 DFW - RIGHT AND LEFT HAND EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000402004040900040SO 2004 4 9 MASA200400152 120040319A2612M835362024M RELAY EMB 145 EMB145LR 3260212SO FIRE DETECTION INOPERATIVE A MASAK NONE J WARNING INDICATION ININSP/MAINT 1 SW07831MJ 145273 BAGGAGE FIRE SWITCH LIGHT WOULD NOT ILLUMINATE DURING THE FIRE DETECTION TEST. MX REPLACED THE TEST SWITCH RELAY. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040409000542004040900054EU 2004 4 9 2004UALA00285 120040327A2722SC47003 DAMPER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29413UA 470 GREEN HYDRAULIC SYSTEM FAILURE. QUANTITY ZERO, PRESSURE LOW. *S/D* YAW DAMPER NR 1 SEAL WAS FOUND LEAKING. THE FAULTY YAW DAMPER WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040409000642004040900064WP 2004 4 9 AALA20040414 120040401A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21287AA 49299 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 8D, 20D, 26D, AND 31D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT 8D, 20D, 26D, AND 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409000712004040900071NM 2004 4 9 2004UALA00294 120040330A5320 WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 STA 194 STR 17 RIGHT WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20040409000762004040900076EA 2004 4 9 SWIA200413093 120040326A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07941SW 7750 ONE AFT OVERHEAD AISLE EMERGENCY LIGHT INOP. RELAMPED AFT OVERHEAD EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD. 2L72 4F RTA21EA 20040409000802004040900080EA 2004 4 9 SWIA200412997 120040307A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERON LEAKING A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07947SW 7786 WHEN LEAVING THE RAMP, NOTICED A PUDDLE OF FLUID. CHECKED HYDRAULIC SYNOPTIC PAGE AND IT SHOWED A LOSS OF ALL HYDRAULIC SYSTEM NR 3 FLUID. REMOVED AND REPLACED NR 3 HYDRAULIC LEFT SPOILERON O/B PCU ACTUATOR WITH A SERVICEABLE UNIT IAW 27-62-01. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. 2L72 4F RTA21EA 20040409000852004040900085NM 2004 4 9 CALA0400297 120040330A5510180A16121 PIN BOEING737 737724 13844BYNM RH HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER MOUNT PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696, STEP 6-9. 2L72 4F RTA16WE 20040409000882004040900088NM 2004 4 9 CALA0400300 120040330A532065528941 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716339 23577 INSPECTION FOUND CABIN FLOOR SUPPORT CRACKED AT STA 540 JUST LEFT OF BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040409000952004040900095NM 2004 4 9 2004UALA00302 120040401A3810 POTABLE WATER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FAILED A UALAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29785UA 26954 POTABLE WATER IS NOT WORKING AND LAVS STARTING TO BACK UP. ONE HOUR OUT OF LHR WATER PRESSURE WENT TO NO PRESSURE. FOUND AIR COMPRESSOR HAD FAILED. WITH ENGINES/APU RUNNING, BLEED AIR SHOULD HAVE BEEN THE ONE PRESSURIZING THE SYSTEM. THE APU BLEED AIR CHECK VALVE INITIALLY FAILED CAUSING THE AIR COMPRESSOR TO TAKE ON THE LOAD AND CONTINUOUSLY RAN UNTIL IT ALSO FAILED. LHRMM REPLACED THE AIR COMPRESSOR, APU BLEED AIR CHECK VALVE, AND IN-LINE FILTERS. SYSTEM OPERATIONS NORMAL. NOTE: SEVERAL REPORTS FROM OTHER OPERATORS HAVE BEEN RECEIVED ON THE APU BLEED AIR CHECK VALVE FAILING. BOEING HAS A SERVICE BULLETIN TO REPLACED IT WITH A RE-DESIGNED VALVE. 2L72 4F4 FRTT0001SE E46NE 20040409000962004040900096NE 2004 4 9 2004UALA00303 220040402A7532 SOLENOID BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT BLEED VALVE FAILED A UALAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP29653UA 25391 RIGHT ENGINE COMPRESSOR STALLS. CREW REPORTED SURGE. AIRCRAFT SYSTEM DID NOT CONFIRM THE SURGE EVENT. ALL TROUBLESHOOTING WAS ACCOMPLISHED AND THE 2.9 BLEED SOLENOID WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20040409000972004040900097EA 2004 4 9 MASA200300091 120040218A1430ABY2 RIVET CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SHEARED A MASAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW0727191 7191 A/C WOULD NOT PRESSURIZE AFTER TAKEOFF, MX WAS CALLED. MX FOUND SHEARED RIVETS ON THE PAX DOOR VENT ACTUATOR ROD. MX REPLACED THE RIVETS, OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001002004040900100WP 2004 4 9 MWEA040035 120040325A575459374991 DOUBLER DOUG DC9 DC981 3022081WP LEFT WING SLAT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 LEFT WING LEADING EDGE HAS CORROSION 12 FT OUTBOARD OF NR 1 SLAT INBOARD IDLER ARM. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20040409001012004040900101EA 2004 4 9 SWIA200413071 120040320A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OUT OF RIG A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07454SW 7749 ON CLIMBOUT, FLAPS FAIL AT 8 DEGREES. RETURN TO SLC. RE-RIGGED FLAPS IAW 27-54-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040409001042004040900104EA 2004 4 9 SWIA200413074 120040314A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07912SW2731 2731 7595 AFTER LANDING IN BIL, STAB CH 1 INOP STATUS MESSAGE. REMOVED AND REPLACED HSTA AND MCU IAW CL 600 MM 27-42-01. OPS CHECKS GOOD. MCU P/N 7062-3, S/N OFF 943. 2L72 4F4 FRTA21EA E15NE 20040409001152004040900115NM 2004 4 9 CALA0400274 120040324A5320149A761415 STRUCTURE BOEING737 737724 13844BYNM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND A .75 INCH CRACK IN LEFT MAIN GEAR AFT SECTION OF WHEEL WELL RING ASSEMBLY CHORD. THE RING ASSEMBLY LOWER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040409001182004040900118NM 2004 4 9 CALA0400277 120040324A5755 SKIN BOEING737 737724 13844BYNM RT WING SPOILER DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND RIGHT GROUND SPOILER DELAMINATED IN TWO AREAS AND DENTED ON LOWER SURFACE. THE RIGHT GROUND SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-12. 2L72 4F RTA16WE 20040409001222004040900122NM 2004 4 9 AALA20040388 120040324A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21750AN 30259 DFW - TWO EMERGENCY LIGHTS AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACKS FOR TWO EMERGENCY LIGHTS AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040409001262004040900126NE 2004 4 9 AT0400005 220040316A7297 WIRE HARNESS BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LT ENGINE DAMAGED A ZZDAA UNSCHED LANDING BG SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CLCLIMB 1 SO15978AT 55037 AFTER TAKEOFF ON 26L ATL, LOST NR 6 DU AND LT GENERATOR FAIL ALERT, SMELLED ELECTRICAL SMOKE. EMERGENCY LANDING ON 9R AT APPROX 114,000 LBS FIRM LANDING. EMERGENCY EVACUATION CONDUCTED. ACCOMPLISHED REPLACEMENT OF THE LT ENGINE WIRING AND ALL CONNECTORS FROM THE LEFT ENGINE SENSOR TO THE LEFT PCDU AND OPS CHECK WAS SATISFACTORY. PERFORMED AC POWER GENERATION AND CONTROL ADJ AND TEST IAW B717 MM 24-21-00 WAS SATISFACTORY. 2L72 4F4 FTRA6WE E00061EN 20040409001322004040900132EA 2004 4 9 SWIA200413053 120040309A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07412SW 7101 DISCOVERED DURING C-CHECK INSPECTION, LEFT FS 625 INTERCOSTAL CRACKED. REPLACED LEFT FS 625 INTERCOSTAL IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040409001412004040900141NM 2004 4 9 AALA20040374 120040321A335002019242002 COVER BOEING737 737823 13844BZNM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21975AN 29549 DFW - EMERGENCY LIGHT COVER AT FORWARD ENTRY DOOR WILL NOT STAY IN PLACE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040409001652004040900165WP 2004 4 9 AALA20040422 120040403A3350 CHARGER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21970TW 53620 DFW - CEILING EMERGENCY LIGHTS AT ROW 25 ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040409001672004040900167NM 2004 4 9 AALA20040424 120040404A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21765AN 32879 DFW - EMERGENCY LIGHT OVER L3 DOOR INOPERATIVE. REPLACED BATTERY PACK M33406 FOR EMERGENCY LIGHT ABOVE 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040409001792004040900179WP 2004 4 9 AALA20040366 120040320A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 DFW - SEAT EMERGENCY ESCAPE PATH LIGHTS FROM ROW 20 AFT ARE INOPERATIVE. REPLACED TRACK LIGHT BATTERY PACK IN AFT GALLEY FOR IN SEAT EMERGENCY ESCAPE PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040412000042004041200004EA 2004 4 12 ASOA04138 120040218A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040412000052004041200005EA 2004 4 12 ASOA04139 120040219A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT ANGLE AT FS 621 IN THE LEFT AND RIGHT CORNERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040412000172004041200017WP 2004 4 12 GTIA040206 120040221A5310 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND AFT PIT SHEAR TIE CRACKED AT FS 1136 LONGERON 27R. REMOVED CRACKED SHEAR TIE. INSTALLED NEW SHEAR TIE. (M) 2L72 4F RTA6WE 20040412000252004041200025 2004 4 12 GTIA040179 420040312A2565 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DTW - FLT 565 - L2 DOOR SLIDE COVER LANYARD CAME OUT. REINSERTED L2 DOOR SLIDE COVER LANYARD. OPS CHECK GOOD. (M) 2L72 4F A6WE 20040412000282004041200028EA 2004 4 12 ASOA04211 120040315A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11915EV 7754 FLT 4912 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW TWO WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TWO. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040412000332004041200033WP 2004 4 12 GTIA040188 120040304A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FLOOR PANEL STATION 160-200 DELAMINATED, NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000402004041200040WP 2004 4 12 GTIA040195 120040305A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND COCKPIT FLOOR PANEL LEFT, PUNCTURED, FASTENER HOLES BROKEN OUT, CHAFED STRIP MISSING PLASTIC SHIELD BROKEN, EDGE CRACKED. COCKPIT FLOOR PANEL HAS PUNCTURE AND NUMEROUS CRACKS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000422004041200042WP 2004 4 12 GTIA040198 120040214A71605930645509 NOSE COWL DOUG DC9 DC983 3022083WP NR 1 ENGINE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND NR 1 ENGINE NOSE COWL LIPPING CORRODED AT 1:00 AND 5:00 O'CLOCK POSITION. FOUND CORROSION OUT OF LIMITS. REMOVED NOSE COWL. INSTALLED THE NR 1 ENGINE NOSE COWL. (M) 2L72 4F RTA6WE 20040412000552004041200055WP 2004 4 12 ASAA0480126 120040229A53209915554U16 INTERCOSTAL DOUG DC9 DC983 3022083WP FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND CORROSION ON NUT PLATES AND SEAT TRACK MID PIT STATION 769 TO 788 STRINGER 28R. REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW MD80 SRM 51-30-2. (M) 2L72 4F RTA6WE 20040412000652004041200065NM 2004 4 12 AWXA200400290 120040223A53136545767120 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 500C+4, FORWARD OF LEADING EDGE LIGHT. MAINTENANCE CUT OUT DAMAGE ON STRINGER 16 LT AND REMOVED STRINGER TIE CLIP AT BS 500C+4; FABRICATED A REPAIR CHANNEL, FILLER, AND NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PARTS IAW AWA ER 03-5331-04073-ES1. 2L72 4F RTA16WE 20040412000662004041200066NM 2004 4 12 AWXA200400291 120040317A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28157AW 23779 DEN - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040412000682004041200068NM 2004 4 12 AWXA200400293 120040223A5320654653949 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 MCN - MAJOR REPAIR - DURING C-20 CHECK FOUND A .625 INCH CRACK IN ANGLE BS 616, LBL 55, WL 208. MAINTENANCE CUT OUT DAMAGE IN ANGLE BS 616, LBL 55, WL 208; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20040412000692004041200069NM 2004 4 12 AWXA200400294 120040319A2910AS116080264 HYDRAULIC LINE BOEING737 7373Q8 1384670NM MLG WW CHAFED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28327AW 23507 LAS - AIR TURNBACK - FLT 0116 - ON CLIMBOUT OF LAS EN ROUTE FOR LAX B-SYSTEM HYDRAULICS FAILED, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE FOUND HYDRAULIC LINE LEAKING BETWEEN B-SYSTEM PRESSURE MODULE AND A/C DRIVEN PUMP. REMOVED AND REPLACED HYDRAULIC LINE IAW BMM 29-09-11. 2L72 4F RTA16WE 20040412000712004041200071 2004 4 12 AWXA200400343 420040402A2565D31517313 SLIDE AIRBUSA319 A319132 3930340NM R-2 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28824AW9842 1100 1490 R-2 DOOR EMERGENCY ESCAPE SLIDE RESERVOIR PRESSURE WAS BELOW SERVICEABLE LIMITS. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY ESCAPE SLIDE ASSEMBLY IAW T/C R1C25305. VENDORS CONFIRMED FAILURE OF EMERGENCY ESCAPE SLIDE ASSEMBLY S/N A9584, SLIDE WAS OVERHAULED IAW CMM 25-60-56, REV. 10. 2L72 4F RTA28NM 20040412000742004041200074 2004 4 12 AWXA200400346 420040403A344146502003030312 ADIRU AIRBUSA319 A319132 3930340NM NR 1 FAULTY A AWXAC ABORTED TAKEOFF IJ FLT. ATTITUDE INST. WARNING INDICATION TOTAKEOFF 1 WP28831AW4450 1576 ON TAKEOFF ROLL AT APPROX 90 KTS ATTITUDE & MAP NOT AVAILABLE, DISPLAYED ON CAPTS PRIMARY FLT DISPLAY & NAVIGATION DISPLAY, & NR 1 IR FAULT LIGHT ON, REJECTED TAKEOFF HIGH SPEED. AFTER REJECTED TAKEOFF BRAKE TEMP REACHED 990 DEG ON ALL FOUR BRAKES, AND NR 1 & 2 TIRES WENT FLAT WITH POSSIBLE LEAKS ON NR 3 & 4 TIRES. MX R & R NR 1 ADIRU IAW T/C R2A34304, OPS CHK GOOD. PERFORMED OVERTEMP INSP OF BOTH MLG AXLES, & R & R ALL FOUR MLG TIRES & BRAKE ASSY. BENCH TEST OF ADIRU COULD NOT VERIFY REASON FOR REMOVAL. SUSPECT PROBLEM WITH JFK RUNWAY 31L INDUCED FAULT OF Z QUANTIZER DC AMP FAILURE. THIS IS A KNOWN PROBLEM WITH JFK RUNWAY. 2L72 4F RTA28NM 20040412000752004041200075EU 2004 4 12 AWXA200400347 120040326A5321D53670033001 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND CABIN FLOOR PANEL 241JF DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 241JF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367033; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236. 2L72 4F RTA28NM 20040412000762004041200076EU 2004 4 12 AWXA200400348 120040326A5321D53670034000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 1 INCH CRACK WAS FOUND IN TWO PLACES ON CABIN FLOOR PANEL 241KF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 241KF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367034; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236. 2L72 4F RTA28NM 20040412000792004041200079NM 2004 4 12 AWXA200400317 120040303A53116546541504 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN FUSELAGE FRAME AT BS 663.75, STR 2 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE FRAME AT BS 663.75, STR 2 LT. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07 FIG 209 SHEETS 1-7. 2L72 4F RTA16WE 20040412000812004041200081NM 2004 4 12 AWXA200400319 120040302A52106545871523 SKIN BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .625 INCH CRACK WAS FOUND IN R-1 DOOR UPPER HINGE CUTOUT BS 303, STR 12 RT. MAINTENANCE CUT OUT DAMAGE IN R-1 DOOR UPPER HINGE CUTOUT. PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5241-04072-ES1. 2L72 4F RTA16WE 20040412000822004041200082NM 2004 4 12 AWXA200400320 120040302A53156546410163 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN CENTER FLOORBEAM UPPER CHORD AT BS 663.75, LBL 7. MAINTENANCE REMOVED DAMAGED SECTION CENTER FLOORBEAM UPPER CHORD AT BS 663.75, LBL 7. FABRICATED 2 REPAIR ANGLES AND 3 STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5702-04073-ES2. 2L72 4F RTA16WE 20040412000852004041200085NM 2004 4 12 AWXA200400181 120040215A32440397812 TIRE BOEING737 7373S3 1384711NM MLG FOD A AWXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP28316AW 23713 TIRE DEBRIS & MLG DOOR ON RUNWAY, NO ABNORMAL FLT CHARACT/INDICATIONS. LOWERED MLG & FLEW BY TOWER, EMER LANDING DECLARED. LANDED W/O INCID. MAINT FOUND NR 4 TIRE SHREDDED, RT MLG INNER DOOR MISSING. DAMAGED RT MLG CENTER DOOR, RT INBD T/E FORE FLAP AT MID SPAN, RT WING T/E INBD PANEL AFT OF RT MLG WW, NR 4 GROUND SPOILER ATTACH LUG. REPLACED RT MLG CENTER & INNER DOOR, RT INBD T/E FORE FLAP, RT WING T/E INBOARD PANEL, NR 4 GROUND SPOILER, ATTACH LUG, BOTH NR 3 & 4 MLG TIRES. NR 4 TIRE SENT TO MANUFACT FOR ANALYSIS. ANALYSIS OF TIRE FOUND 33 PERCENT OF TREAD WORN, NO SIGNS OF LONG TERM OVER DEFLECTION, CORD SEP, OR CORD FATIGUE. X-TYPE RUPTURE FOUND ON TREAD INDICATING CONTACT WITH A FOD, & REASON TIRE BURST.2L72 4F RTA16WE 20040412000862004041200086NM 2004 4 12 AWXA200400323 120040227A53116546539 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .75 INCH CRACK WAS FOUND ON INBOARD LOWER SIDE OF FUSELAGE FRAME AT BS 616, STR 17 LT. MAINTENANCE CUT OUT CRACKED FUSELAGE FRAME AT BS 616, STR 17 LT; FABRICATED A FILLER, DOUBLER & STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20040412000872004041200087NM 2004 4 12 AWXA200400324 120040321A5752654645522 TAB BOEING737 737301 1384611NM RT AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW 23260 MCN - MAJOR REPAIR - LOWER SURFACE OF RIGHT WING AILERON CONTROL TAB DELAMINATED AT WBL 456. MAINTENANCE PERFORMED BOND REPAIR ON RT WING AILERON CONTROL TAB AT WBL 456 IAW B737-300 SRM 51-70-16. 2L72 4F RTA16WE 20040412000882004041200088NM 2004 4 12 AWXA200400351 120040301A5330655298873 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN LOWER FORWARD CORNER OF L-2 DOOR CUTOUT BS 963. MAINTENANCE TRIMMED OUT DAMAGE IN LOWER FORWARD CORNER OF L-2 DOOR CUTOUT BS 963; PERFORMED REPAIR IAW AWA ER 03-5361-04079-ES1. 2L72 4F RTA16WE 20040412000892004041200089NE 2004 4 12 AWXA200400261 220040310A7532ETPU10002C TPU BOEING757 7572G7 1384963NM RROYCERB211 RB211* 54555NE NR 1 ENGINE MALFUNCTIONED A AWXAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 WP28910AW10042 24523 DURING DESCENT INTO LAS, WITH IDLE THRUST LEVERS THE NR 1 ENGINE SHUTDOWN. ENGINE RESTARTED AND OPERATED NORMALLY, RECEIVED STATUS MESSAGE LT ENG LP PUMP WITH ENGINE FAILURE FRM 73-11-05-01. DECLARED EMERGENCY, AND LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCE TROUBLESHOT IAW FIM 71-05-00, REMOVED AND REPLACED THE NR 1 ENGINE FUEL FLOW GOVERNOR IAW T/C R5M73603, AND REPLACED ENGINE TRANSIENT PRESSURE UNIT IAW BMM 75-32-15-004-001. HIGH PRESSURE FUEL PUMP WAS REMOVED AND REINSTALLED IAW T/C R5M73602, OPERATIONAL CHECK WAS GOOD. PART NAME; FUEL FLOW GOVERNOR, MFG; ROLLS-ROYCE, P/N; FFG021BH, S/N; 1947551, TT; 50415, TC; 19771, TSR; 439. 2L72 4F4 FRTA2NM A12EU 20040412000902004041200090NM 2004 4 12 AWXA200400356 120040408A3350BR964411 LIGHT BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040412000922004041200092NM 2004 4 12 AWXA200400358 120040407A5330654577678 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 PHX - MAJOR REPAIR - A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 747, STR 25 LT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 747, STR 25 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER & TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20040412000982004041200098 2004 4 12 SWIA200413082 420040320A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING FAULTY A SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07582SW 120350 LEFT STALL TEST LIGHT ILLUMINATES INTERMITTENTLY ON GROUND DURING TAXI. STALL TEST ON POWER UP IS SATISFACTORY. REPLACED NR 1 STALL WARNING COMPUTER WITH SERVICEABLE UNIT AS REQUIRED. SYSTEM OPS CHECK GOOD IAW EMB 120 MM 27-34-00. 2L72 4T RTA31SO 20040412000992004041200099SO 2004 4 12 SWIA200413083 120040323A3350 SIGN EMB 120 EMB120ER 3260203SO CABIN BROKEN A SWIAK NONE O OTHER TXTAXI/GRND HDL 1 NM07562SW 120336 FORWARD BULKHEAD EXIT SIGN IS BROKEN. REMOVED AND REPLACED BROKEN EXIT SIGN, OPS CHECK OK. P/N: 10-1301-15. 2L72 4T RTA31SO 20040412001022004041200102 2004 4 12 SWIA200413086 420040324A34256226190204 AHRS EMB 120 EMB120ER 3260203SO NR 1 MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07220SW6728 3560 120288 CAPTAIN'S AUTOPILOT FAILED FFOD CHECK AND COMPUTER FLAG STAYS IN VIEW. INSPECTED APC NR 1, NR 1 AHRS AND ADI NR 1 WIRING AND CONNECTORS. NO DEFECTS NOTED. CONTINUOUSLY TESTED AND NO FAULTS FOUND. REMOVED AND REPLACED NR 1 AHRS FOR TROUBLESHOOTING. OPS CHECK GOOD IAW MM 34-21-00 AND 22-10-00. 2L72 4T RTA31SO 20040412001062004041200106EU 2004 4 12 MALA040294 120040330A3020NF24668057 NOZZLE SAAB SF340 340B 7860101EU RT INTAKE FAULTY A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15407XJ 340B407 RIGHT INTAKE HEAT FAILED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED & REPLACED RIGHT INTAKE EXHAUST NOZZLE IAW SF340 AMM CHAP 71-60-10. ALL CHECKS GOOD AT THIS TIME. P/N ON&OFF NF24668-057, S/N ON L338514, S/N OFF NSN. 2L72 4T RTA52EU 20040412001082004041200108NM 2004 4 12 2004UALA00268 120040320A5320131W18111103 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE L4 DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29773UA40 26929 DOOR 4L WILL NOT OPEN FROM OUTSIDE OR INSIDE DOOR. FOUND GIRT BAR FITTING BROKEN. CAUSE DETERMINED TO BE THE THRESHOLD GIRT FLOOR FITTING OUT OF ADJUSTMENT, RESULTING IN A PRELOAD ON THE GIRT BAR AND THE GIRT BAR FITTING WHEN THE DOOR WAS CYCLED THROUGH ARM/DISARM. THE GIRT BAR FITTING WAS REPLACED. THE SAME FITTING CRACKED 6 DAYS EARLIER, BUT THE THRESHOLD GIRT FLOOR FITTING RIG WAS EVIDENTLY NOT CORRECT (SEE 2004UALA00234). 2L72 4F4 FRTT0001SE E46NE 20040412001102004041200110NM 2004 4 12 2004UALA00272 120040323A2425 WARNING SYSTEM BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE COCKPIT ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29223UA 30224 ON TAKEOFF ROLL LEFT GEN DRIVE LIGHT AT 60 KTS. TAKEOFF WAS ABORTED AND DRIVE LIGHT WENT OUT. MAINTENANCE FOUND ELECTRICAL GENERATOR DRIVE MESSAGE 24-31551 (FIM: IDG LEFT SHOWS LOW OIL PRESSURE. "THIS MAINTENANCE MESSAGE IS RELATED TO A LOW OIL LEVEL OR LOW OIL CHARGE PRESSURE IN THE IDG). MAINTENANCE SERVICED THE IDG TO FULL, PERFORMED OIL LEAK CHECK AFTER SUBSEQUENT ENGINE RUN AND FOUND NO LEAKS. BRAKES AND WHEELS WERE ALSO CHECKED AND FOUND SERVICEABLE. ENGINE RUN-UP CHECKED OK WITH FLIGHT CREW WITH NO RELATED MAINTENANCE MESSAGE. THE FLIGHT THEN CONTINUED UNEVENTFULLY. LH IDG REMOTE OIL LEVEL SENSOR WAS REPLACED SEVERAL FLIGHTS LATER AS PRECAUTIONARY. 2L72 4F4 FRTT0001SE E46NE 20040412001132004041200113WP 2004 4 12 AALA20040408 120040331A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21422AA 49334 DFW - AFT CABIN CEILING EMERGENCY LIGHTS AT L2-615, L2-671 AND L2-694 INOPERATIVE. REPLACED BATTERY PACK B5-27 AND RELAMPED AFT CABIN CEILING EMERGENCY LIGHTS AT L2-615, L2-671 AND L2-694. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040412001162004041200116NM 2004 4 12 CALA0400256 120040319A551165479886 RIB BOEING737 7373T0 1384582NM HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A .375 INCH CRACK IN RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040412001172004041200117EA 2004 4 12 QXEA200400152 120040210A2910MM67075294005 TUBE CNDAIRCL600 CL6002C10 1390015EA HYD SYSTEM CRACKED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09602QX5216 10010 THE CREW RECEIVED A HYDRAULIC 2 LO PRESSURE CAUTION. AFTER PERFORMING THE CHECKLIST, THEY RECEIVED A HYDRAULIC ENGINE DRIVEN PUMP 2A CAUTION MESSAGE, AND AFTER A FEW MINUTES, THE HYDRAULIC 2 LOW PRESSURE CAUTION RETURNED. THE HYDRAULIC SHUT OFF VALVE WAS SHUT OFF IAW THE CHECKLIST. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE PUMP PRESS LINE FROM THE AFT PRESSURE BULKHEAD TO THE NR 1 STS PRESS MANIFOLD. THE OPERATIONAL AND LEAK CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040412001182004041200118NM 2004 4 12 CALA0400257 120040320A5753654783866 SKIN BOEING737 7373T0 1384582NM NR 2 MIDFLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND NR 2 LEFT I/B MIDFLAP SKIN FOR EXHAUST GATE CONTROL ROD ON LEADING EDGE GOUGED AT WBL 163. REPAIRED IAW ECRA 5752-01151. 2L72 4F RTA16WE 20040412001212004041200121NM 2004 4 12 CALA0400260 120040320A5240 SKIN BOEING737 7373T0 1384582NM SERVICE DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND GROUND AIR SERVICE DOOR SKIN CORRODED. THE CORRODED SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040412001232004041200123NM 2004 4 12 CALA0400262 120040321A5510180A16122 PIN BOEING737 737724 13844BYNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND LEFT MIDDLE AND LEFT LOWER HORIZONTAL STABILIZER PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040412001252004041200125EU 2004 4 12 MALA040295 120040321A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN SHORTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 BATTERY POWER SUPPLY P/N 3301-51, S/N 1445, FAILED SCHEDULED CAPACITY CHECK. BATTERY P/N 3301-31 WAS FOUND SHORTED AND REPLACED ON IN HOUSE WORK ORDER 365069. UNIT PASSED RTS AND WAS RETURNED TO SERVICE ON 3/25/04. 2L72 4T RTA52EU 20040412001262004041200126EU 2004 4 12 MALA040296 120040321A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 BATTERY POWER SUPPLY P/N 3301-51, S/N 1442, FAILED SCHEDULED CAPACITY CHECK. BATTERY P/N 3301-51 WAS CHARGED IN SHOP ON IN HOUSE WO 365067, PASSED SUBSEQUENT CAP CHECK UNIT WAS RTS 3/25/04. 2L72 4T RTA52EU 20040412001292004041200129EU 2004 4 12 MALA040299 120040329A33506122751 BATTERY BAC 146 AVRO146RJ85A1500097EU CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15526XJ E2351 BATTERY PACK P/N 61-2275-1, S/N 0009407 WAS REMOVED FOR SCHEDULED MAINTENANCE ON 2/27/04. ON 3/29/04 THE BATTERY ASSEMBLY FAILED CAPACITY CHECK ON THE BENCH. BATTERY ASSEMBLY P/N 61-2275-1 WAS REPLACED AND UNIT WAS RTS ON 3/31/04. 2H74 4F RTA49EU 20040412001342004041200134 2004 4 12 2004UALA00281 420040325A2565MR25708 SLIDE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE L1 DOOR UNSERVICEABLE A UALAK NONE O OTHER ININSP/MAINT 1 WP29651UA 25389 DOOR 1 LEFT SLIDE RAFT PRESSURE AT 2500 PSI. REPLACED 1L DOOR ESCAPE SLIDE. 2L72 4F4 FRTA1NM E24NE 20040412001362004041200136NM 2004 4 12 2004UALA00283 120040325A2913 PUMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29589UA 28707 LT ENGINE HYDRAULIC PUMP FAILED. HYDRAULIC ENGINE PUMP EICAS MESSAGE DISPLAYED. PUMP IS ENROUTE TO VENDOR FOR EVALUATION. REPLACED PUMP AND FILTERS. FLUSHED SYSTEM, LEAK AND OPERATIONAL CHECK. 2L72 4F4 FRTA2NM E17NE 20040412001402004041200140NM 2004 4 12 AWXA200400335 120040228A531265175837 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .5 INCH CRACK WAS FOUND AT LIGHTNING HOLE IN BS 178 BULKHEAD VERTICAL WEB BEAM RBL 5, WL 195. MAINTENANCE REMOVED CRACKED SECTION OF BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 5, WL 195; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2L72 4F RTA16WE 20040412001412004041200141NM 2004 4 12 AWXA200400336 120040308A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 639, STR 3 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 639, STR 3 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46540; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2L72 4F RTA16WE 20040412001462004041200146NM 2004 4 12 AWXA200400339 120040302A534069414372 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 663, STR 10 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2L72 4F RTA16WE 20040412001482004041200148EU 2004 4 12 AWXA200400361 120040328A5311D5347112320300 FRAME AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF SUPPORT FRAME BETWEEN FR 69 AND FR 70, STR 24 RT. MAINTENANCE REMOVED CORRODED SUPPORT FRAME BETWEEN FR 69 AND FR 70, STR 24 RT; FABRICATED A NEW REPLACEMENT SUPPORT FRAME; INSTALLED REPAIR PART IAW AIRBUS A320 SRM 51-42-11. 2L72 4F RTA28NM 20040412001492004041200149NM 2004 4 12 AWXA200400309 120040325A1420BMS13311122 SPLICE BOEING737 737277 1384570NM CABIN BROKEN A AWXAO OTHER O OTHER ININSP/MAINT 1 WP28178AW 22645 PHX - EEL - FLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION, IN ON POSITION ALL EMERGENCY EXIT LIGHTS ILLUMINATED, AND IN OFF POSITION ALL EMERGENCY LIGHTS WERE OFF. MAINTENANCE FOUND OPEN SPLICE, REMOVED AND REPLACED SPLICE, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040412001502004041200150EU 2004 4 12 AWXA200400295 120040319A335032145410 EPSU AIRBUS320 A320232 3930326EU CABIN DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW9091 4176 762 PHX - EEL - EMERGENCY LIGHTS NEAR LT OVERWING EMERGENCY EXIT STAY ON AND FAIL TEST AT FORWARD ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040412001522004041200152NM 2004 4 12 AWXA200400297 120040302A57536546486131 WEDGE BOEING737 7373G7 1384595NM LT MID FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND LOWER SURFACE OF LT INBOARD MID FLAP WEDGE DELAMINATED 13.75 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DAMAGED SKIN AND CORE ON LOWER SURFACE OF LT INBOARD MID FLAP WEDGE; FABRICATED REPAIR CORE AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 16 PG 67-69. 2L72 4F RTA16WE 20040412001542004041200154NM 2004 4 12 AWXA200400325 120040330A2560P20700012015 FLASHLIGHT AIRBUSA319 A319132 3930340NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28821AW 1406 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY INBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD GALLEY INBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040412001552004041200155NM 2004 4 12 AWXA200400326 120040303A534569403521 GALLEY TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY LOWER OUTBOARD MOUNT TRACK AT BS 294, RBL 43, WL 208.5. MAINTENANCE REMOVED FORWARD GALLEY LOWER OUTBOARD MOUNT TRACK AT BS 294, RBL 43; FABRICATED A NEW REPLACEMENT MOUNT TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 16 PG 1-6. 2L72 4F RTA16WE 20040412001572004041200157NM 2004 4 12 AWXA200400328 120040324A321165C309313 SLEEVE BOEING737 7373G7 1384595NM LT MLG TRUNNION CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK PITTING CORROSION WAS FOUND INSIDE LT MAIN LANDING GEAR FORWARD TRUNNION BEARING SLEEVE, IN REAR SPAR. MAINTENANCE REMOVED CORRODED LT MAIN LANDING GEAR FORWARD TRUNNION BEARING SLEEVE; FABRICATED A NEW REPLACEMENT SLEEVE PER DWG 65-50768; INSTALLED REPAIR PART IAW DWG 65-50768, SHEET 4. 2L72 4F RTA16WE 20040412001592004041200159SW 2004 4 12 KBM2004F00019 120040127A2842EA4703987 SENSOR BELL 206 206B 1181511SW ALLSN 250C 250C* GL FUEL TANK FAULTY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 FUEL GAUGE PEGS OUT. REMOVED AND REPLACED WITH SERVICEABLE PART. 1G71 3U3 U H2SW E4CE 20040412001602004041200160EU 2004 4 12 KBM2004F00020 120040207A6730SC5084 SERVO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA165 2143 FORWARD AND AFT SERVO BINDING, REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040412001622004041200162EU 2004 4 12 KBM2004F00022 120040219A71700174078010 DRAIN VALVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING E KBMAO OTHER K FLUID LOSS ININSP/MAINT 1 WP19215LA 2143 START DRAIN VALVE, EXTERNAL LEAKING. 10 YR CALENDAR INSPECTION. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U3 U H9EU E19EU 20040412001632004041200163NM 2004 4 12 USA2004F00002 120040229A335020121 CHARGER BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19356US 23559 MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY PACK (PN 20131A). OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040412001642004041200164NM 2004 4 12 USAASB04017 120040214A3397 WIRE BOEING737 7374B7 1384702NM CABIN DAMAGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19783AU 25022 MCO - MAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REPAIRED WIRE TO THE OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040412001652004041200165NM 2004 4 12 GTIA040131 120040216A3350 SIGN DOUG MD80 MD83 3023681NM CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FLL - FLT 367 - DURING CABIN INSPECTION, FOUND L-2 DOOR AFT SAF-T-GLO EXIT SIGN DIRTY AND BROKEN. REMOVED AND REPLACED SAF-T-GLO EXIT SIGN AND END CAPS. (M) 2L72 4F RT 20040412001662004041200166WP 2004 4 12 GTIA040132 120040214A2560 SMOKE GOGGLES DOUG DC9 DC981 3022081WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 DTW - FOUND FIRST OFFICERS SMOKE GOGGLES CRACKED. REMOVED AND REPLACED FIRST OFFICERS SMOKE GOGGLES. (M) 2L72 4F A6WE 20040412001672004041200167NM 2004 4 12 GTIA040135 120040219A2530 COFFEEMAKER DOUG MD80 MD83 3023681NM GALLEY NOT SEATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 DTW - FLT 1874 - FLIGHT ATTENDANT REPORTED A SPARK FROM AFT COFFEE MAKER CB WHEN PULLED. RESEATED COFFEE MAKERS AND PERFORMED. OPS CHECK, NO DEFECTS NOTED AT THIS TIME. (M) 2L72 4F RT 20040412001682004041200168WP 2004 4 12 GTIA040136 120040217A3260 UPLOCK SENSOR DOUG DC9 DC983 3022083WP LT MLG LOOSE A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23833NK 49449 RED LEFT GEAR UNSAFE LIGHT ON AFTER RETRACTION, FOLLOWED QRH PROCEDURES AND LIGHT WENT OUT. FOUND LEFT GEAR UPLOCK SENSOR LOOSE. TIGHTENED SENSOR AND INSPECTED BRACKET AND SENSOR, INSTALLATION FOUND TO BE NORMAL. ALSO, PERFORMED PROX TEST OF UPLOCK SENSOR, PROX TEST SATISFACTORY AT THIS TIME, NO DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040412001702004041200170 2004 4 12 GTIA040143 420040102A2565D29982113 SLIDE DOUG DC9 DC983 3022083WP R1 DOOR UNSERVICEABLE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND R1 DOOR SLIDE REQUIRES REPACK. REMOVED R1 DOOR SLIDE. INSTALLED NEW R1 DOOR SLIDE. (M) 2L72 4F RTA6WE 20040412001712004041200171NM 2004 4 12 USAASB04014 120040205A33501012721 LIGHT BOEING737 7373B7 1384580NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19383US 22956 PIT - PILOT REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 7 AND 22, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS AT SEAT ROWS 7 AND 22, LEFT SIDE. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040412001732004041200173WP 2004 4 12 GTIA040145 120040122A5321 CHANNEL DOUG DC9 DC983 3022083WP FLOOR PANEL DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND PASSENGER CABIN METALLIC PANEL LEFT SIDE STATION 1174 TO 1260 HAS TWO HATS SECTION DISBONDED AND DAMAGE FORWARD END SECTION HAT. REPAIRED PANEL. (M) 2L72 4F RTA6WE 20040412001802004041200180WP 2004 4 12 GTIA040138 120040218A3260833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083WP LT MLG FAULTY A GTIAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 GL23833NK 49449 FLL - FLT 705 - AFTER LANDING GEAR RETRACTION LEFT MAIN RED UNSAFE LIGHT REMAINED ON FOR APPROX 2 MINUTES GEAR DOOR LIGHT WAS OUT. TROUBLESHOT LEFT MAIN GEAR INDICATION, RUNG OUT WIRES TO THE SENSOR. WIRES CHECKED OK ALSO RAN AST, ON PSEU AND MONITOR TEST OF LT SENSOR UPLOCK OK. MONITOR TEST OF DWN, ON PSEU, LOCK AND FAILED. REMOVED AND REPLACED LOCK SENSOR, ALSO SHIMMED UPLOCK SENSOR. (M) 2L72 4F RTA6WE 20040412001812004041200181 2004 4 12 GTIA040139 420040220A2565 SLIDE DOUG DC9 DC983 3022083WP L1 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 LAS - FLT 1874 - L1 DOOR SLIDE PACK FELL OFF. REINSTALLED L1 DOOR SLIDE PACK. (M) 2L72 4F RTA6WE 20040412001832004041200183WP 2004 4 12 GTIA040141 120040221A3260 WARNING LIGHT DOUG DC9 DC982 3022082WP COCKPIT ILLUMINATED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23820NK 49126 RSW - FLT 1605 - AFTER GEAR HANDLE SELECTED UP LT MAIN GEAR UNSAFE LIGHT (RED) REMAINED ON. CONSULTED QRH, GEAR UNSAFE LIGHT REMAINED ON ALL OTHER AIRCRAFT INDICATION NORMAL. INSPECTED LEFT MLG POSITION INDICATION SYSTEM. NO DEFECTS NOTED AT THIS TIME. (M) 2L72 4F A6WE 20040412001862004041200186EU 2004 4 12 ASOA04141 120040219A33503011160 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11531AS 454 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT AT ROW 3B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPOSITIONED THE EMERGENCY EXIT LIGHT AT ROW 3B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040412001872004041200187WP 2004 4 12 ASAA0480155 120040302A532199365451 INSERT DOUG DC9 DC983 3022083WP FLOORBOARD CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 160-200 HAS SEVERAL INSERTS CORRODED AND BENT. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M0 2L72 4F RTA6WE 20040412001882004041200188WP 2004 4 12 ASAA0480152 120040302A5320993033886 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CRACKED FLOOR WEB AT STATION 218, RBL 47 FORWARD CABIN. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 51-70-4. (M) 2L72 4F RTA6WE 20040412001922004041200192WP 2004 4 12 ASAA0480114 120040229A5230391227547 HINGE DOUG DC9 DC983 3022083WP CARGO DOOR WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND MID CARGO BAY DOOR HINGE BOLT HOLES ARE WORN FORWARD AND AFT. REPLACED DOOR HINGES PER OHM 52-30-1. (M) 2L72 4F RTA6WE 20040412001932004041200193WP 2004 4 12 ASAA0480115 120040229A532199365511 INSERT DOUG DC9 DC983 3022083WP FLOOR PANEL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED DAMAGED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040412001952004041200195WP 2004 4 12 ASAA0480142 120040301A575499558383 SLAT TRACK DOUG DC9 DC983 3022083WP L/E SLAT GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND NR 2 SLAT LEFT NR 8 TRACK HORN IS GOUGED ALONG LOWER EDGE. REMOVED DAMAGED SECTION AND PERFORMED HFEC REPAIR PER EA 5740-01380. (M) 2L72 4F RTA6WE 20040412001962004041200196WP 2004 4 12 ASAA0480143 120040301A3010593773321 TUBE DOUG DC9 DC983 3022083WP L/E SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, NR 5 SLAT LEFT BLOW TUBE CONNECTION END WORN ALONG EDGE. WELD-REPAIRED CHAFED AREA AND RECONTOURED TO ORIGINAL SHAPE PER EA 3010-01075. (M) 2L72 4F RTA6WE 20040412001972004041200197WP 2004 4 12 ASAA0480144 120040301A5730ABR0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M) 2L72 4F RTA6WE 20040412001992004041200199WP 2004 4 12 ASAA0480150 120040302A532199365461 INSERT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING CABIN FLOORBOARD STATION 160-200 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040412002002004041200200WP 2004 4 12 ASAA0480124 120040229A575359100436 VANE DOUG DC9 DC983 3022083WP T/E FLAP WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND RIGHT WING OUTBOARD FLAP VANE INBOARD AFT EDGE IS WORN. BLENDED OUTBOARD FLAP TRAILING EDGE. FOUND TO BE IN LIMITS IAW ASA EA 5750-01923, AND AAR EA 10283. (M) 2L72 4F RTA6WE 20040412002012004041200201WP 2004 4 12 ASAA0480125 120040229A532095200089 STRAP DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND MID PIT LOWER PAN, STRAP HAS CORROSION. REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED REPLACEMENT STRAP IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040412002022004041200202WP 2004 4 12 ASAA0480138 120040229A531056432241 WINDOW FRAME DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND FRAME AROUND AFT FRAME OF CAPTAINS SLIDING WINDOW CHAFED. BLENDED, TREATED, AND PRIMED CHAFED AREA PER EA 5310-02315. (M) 2L72 4F RTA6WE 20040412002032004041200203WP 2004 4 12 ASAA0480139 120040229A5730ABR0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, LEFT WING FUEL ACCESS PANEL 1363 HAS FRETTING CORROSION ON MATING FLANGE. REPLACED PANEL PER MM 28-00-00. (M) 2L72 4F RTA6WE 20040412002052004041200205WP 2004 4 12 ASAA0480127 120040229A5320993061287 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND FLOOR WEB CRACKED, FROM STATION 1287 TO 1309 AT 18R. REMOVED DAMAGED CUSP WEB, ORDERED AND INSTALLED NEW CUSP WEB IAW MD80 SRM 53-05 FIG 97. (M) 2L72 4F RTA6WE 20040413000012004041300001NE 2004 4 13 UG8A235JA 220040305A73201501KDC03005 EEC GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE RT ENGINE FAULTY E UG8AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23920DC1772 534 RT ENGINE ROLLED BACK AFTER TAKEOFF, ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CHANNEL B AND ENGINE OK. TROUBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICE EEC IAW MFG MM AND PERFORMED ENGINE OPERATIONAL CHECKS. ALL PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA12EA E00057EN 20040409000072004040900007NM 2004 4 9 AWXA200400355 120040407A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM SEAT ROW 5 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - EEL - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LEFT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040409000112004040900011EU 2004 4 9 MALA040279 120040317A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 DURING 4Y/2Y INSPECTION IN LCQ, FS 297 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 3/22/04. 2L72 4T RTA52EU 20040409000142004040900014NM 2004 4 9 AWXA200400298 120040320A276131077111 SERVO AIRBUSA319 A319132 3930340NM NR 4 SPOILER FAILED A AWXAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP28801AW19766 889 ON CLIMBOUT, RT WING NR 4 SPOILER WAS FLOATING CAUSING A/C TO ROLL LT AND BETA TARGET TO BE OUT TO RT. TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MX PLACED NR 4 SPOILER ON MEL 27-64-01, COND 3, & DEACTIVATED BOTH LT & RT WING NR 4 SPOILERS. R & R RT WING NR 4 SPOILER SERVO CONTROL (ACTUATOR) IAW AMM 27-64-51, OPS CK GOOD. FUNCTIONAL CHECK CONFIRMED FAILURE OF SPOILER SERVO CONTROL ACTUATOR. TEARDOWN OF UNIT FOUND INSULATION OUT OF LIMITS, SEALS & PACKINGS WORN, GROOVES IN PISTON, AND RING, LOCK NUT, & TRUNNION BUSHINGS DAMAGED. REPLACED SEALS & PACKINGS IN CUP VALVE AREA OF ACTUATOR ASSY, CLEANED FILTER, REWORKED PISTON, & REPLACED RING, LOCK NUT, & TRUNNION BUSHINGS. UNIT REPAIRED & TESTED IAW CMM. 2L72 4F RTA28NM 20040409000182004040900018EA 2004 4 9 MASA200400101 120040223A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BLOWN A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0717156 7156 THE PAX DOOR EXTERIOR AND LEFT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. ITEM WAS DEFERRED WITH THE CREW AND A/C DEPARTED WITHOUT FURTHER INCIDENT. MX RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20040409000262004040900026SO 2004 4 9 MASA200400088 120040216A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07857MJ 145765 DURING OVERNIGHT MX IT WAS DISCOVERED THAT THE RT FWD EXTERNAL EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB BUT THAT DID NOT FIX IT. MX PLACED ON MEL. 2L72 4T RTT00011AT 20040409000312004040900031NE 2004 4 9 MALA040283 320040321A6111 BLADE SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE PROPELLER DAMAGED A MALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15452XJ 340B452 NR 4 LEFT PROP BLADE DAMAGED. MAINTENANCE INSPECTED AND STATED IT APPEARED THE BLADE STRUCK SOMETHING DURING THE TAXI IN FROM NR 3321. MX REPLACED LEFT PROP, LEFT PROP ASSY IAW MAL TC NR 6110-303, P/N OFF&ON R390/4-123-F/27, S/N OFF DAP1403, S/N ON DAP0099, OPS CHECK GOOD AT THIS TIME. 2L72 4T RTA52EU 6 CP31NE 20040409000372004040900037WP 2004 4 9 MWEA040032 120040323A2913AS66411LS666 PUMP DOUG DC9 DC981 3022081WP ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 GL31812ME 48006 RIGHT ENGINE HYDRAULIC PUMP CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED ENGINE HYDRAULIC PUMP. 2L72 4F A6WE 20040409000382004040900038SO 2004 4 9 MASA200400150 120040319A2612 CONNECTOR EMB 145 EMB145LR 3260212SO FIRE DETECTION DIRTY A MASAK NONE L NO TEST ININSP/MAINT 1 SW07843MJ 145478 NO BELL DURING THE FIRE DETECTION TEST. MX REMOVED CLEANED CONNECTOR AND INSTALLED AURAL WARNING UNIT. THE SYSTEM OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040409000492004040900049WP 2004 4 9 AALA20040379 120040322A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219615W 53562 STL - CEILING EMERGENCY LIGHTS AT SEVERAL LOCATIONS THROUGHOUT CABIN AND FORWARD EXIT LIGHT AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACKS FOR CEILING EMERGENCY LIGHTS FOR VARIOUS LOCATIONS THROUGHOUT CABIN AND FOR FORWARD EXIT LIGHT AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040409000592004040900059 2004 4 9 SWIA200412994 420040307A2297 WIRE EMB 120 EMB120ER 3260203SO AUTOPILOT CHAFED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07583SW 120351 DURING AUTO PILOT FIRST FLIGHT OF THE DAY CHECKS, THE FIRST OFFICER'S AUTO PILOT DISCONNECTS ITSELF DURING TEST. INSPECTED AND FOUND CHAFED WIRE. REPAIRED WIRE AS REQUIRED. OPS CHECK GOOD, REPOSITIONED WIRING. 2L72 4T RTA31SO 20040409000652004040900065NM 2004 4 9 2004UALA00288 120040329A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 BULK CARGO COMPARTMENT SKIN DENTED FROM STRINGER 47L TO 46L AT STA 1936. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER & SPLICE REPAIR. 2L74 4F4 FRTA20WE E24NE 20040409000682004040900068NE 2004 4 9 2004UALA00291 220040329A7230 COMPRESSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE SEIZED A UALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP29473UA 1469 NR 1 ENGINE COMPRESSOR STALLED AND SUBSEQUENTLY SEIZED. OIL PRESSURE AND N2 WENT TO ZERO. NR 3 BEARING FAILED. OUTER RACE FRACTURED, BEARING CAGE DISINTEGRATED, ALL BALL BEARINGS WORN APPROXIMATELY 25 PERCENT ON OPPOSING SIDES. REPLACED ENGINE. CORRECTIVE ACTION ALREADY IN PLACE PER EXISTING AD NOTE, AND MCD CHIP RE-INSPECTION INTERVALS HAVE BEEN REDUCED FROM 125 FLIGHT HOURS TO 45 FLIGHT HOURS. 2L72 4F4 FRTA28NM E40NE 20040409000702004040900070NM 2004 4 9 2004UALA00293 120040330A5320 WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 STA 194 STR 17 LEFT HAS A CRACKED WEB. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20040409000732004040900073 2004 4 9 SWIA200413090 420040326A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07268UE1123 1123 120207 WHEN AUTOPILOT IS SELECTED TO FIRST OFFICER'S SIDE, AUTOPILOT TRIES TO CAPTURE LOCALIZER WHEN STILL FULL SCALE (AT LEAST 1.5 MILES OFF COURSE). REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040409000742004040900074 2004 4 9 SWIA200413091 420040325A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07298SW7527 6062 120328 RIGHT AFTER TAKEOFF TRIM FAIL LIGHT ILLUMINATED ON MAP AND TRIM LIGHT ON FCP AND SINGLE CHIME. ALL LIGHTS WENT OUT WHEN AUTOPILOT WAS SWITCHED TO FIRST OFFICER'S SIDE. ALL ILLUMINATED AGAIN WHEN SWITCHED BACK TO CAPTAIN'S SIDE. REMOVED AND REPLACED APC NR 1 WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040409000752004040900075EA 2004 4 9 SWIA200413092 120040326A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FALSE INDICATIONA SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07915SW 7615 AFTER TAKEOFF, FLAPS FAILED TO COME UP. FLAPS STOPPED 6-8 DEGREES WITH ASSOCIATED FLAPS FAIL CAUTION MESSAGE. RETURNED TO FIELD. PERFORMED A POWER DOWN/POWER UP ON AIRCRAFT. ALL OPS CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20040409000912004040900091NM 2004 4 9 2004UALA00298 120040330A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 BS 747 STR 22L AND STR 23L HAVE CRACKED SHEAR TIES. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040409001052004040900105EA 2004 4 9 SWIA200413075 120040308A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07934SW 7722 LEFT WINDOW CRACKED AT 17,000 FT. INSTALLED SERVICEABLE LEFT WINDOW ASSEMBLY IAW CRJ MM 56-12-01 AND RII 56-402. NO LEAKS NOTED. P/N OFF: NP139322-001, S/N OFF: 02218H3041. 2L72 4F4 FRTA21EA E15NE 20040409001202004040900120NM 2004 4 9 CALA0400279 120040325A53206916996 ATTACH ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND ATTACH ANGLES CORRODED UNDER RADAR R/T FORWARD OF STA 203.8. NEW ANGLES WERE INSTALLED IAW SRM 51-40-00 AND 51-10-02. 2L72 4F RTA16WE 20040409001212004040900121NM 2004 4 9 CALA0400280 120040325A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714242 28805 INSPECTION FOUND AFT CARGO LT ZEE CHANNEL CORRODED FROM STA 727-847. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040409001452004040900145EU 2004 4 9 MALA040289 120040311A5280 SKIN BAC 146 AVRO146RJ85A1500097EU MLG DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15512XJ E2326 DURING C-CHECK INSPECTION IN LCQ, LEFT MLG DOOR FWD UPPER EDGE CHAFED. BLENDED CHAFED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW MESABA EO A52036. A/C RELEASE DATE 3/30/04. 2H74 4F RTA49EU 20040409001462004040900146EU 2004 4 9 MALA040290 120040311A5280 SKIN BAC 146 AVRO146RJ85A1500097EU RT MLG DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15512XJ E2326 DURING C-CHECK INSPECTION IN LCQ, RIGHT MLG DOOR FWD UPPER EDGE CHAFED. BLENDED CHAFED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW MESABA EO NR A52037. A/C RELEASE DATE 3/30/04. 2H74 4F RTA49EU 20040409001522004040900152NM 2004 4 9 CALA0400282 120040326A532165458339 FLOOR PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A 1 INCH CRACK IN FLIGHT DECK FLOOR PANEL AT STA 257, RBL 1. REPAIRED IAW SRM 51-70-13. 2L72 4F RTA16WE 20040409001582004040900158NM 2004 4 9 AALA20040425 120040404A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21683A 25340 BOS - EMERGENCY LIGHT AT LEFT HAND OVERHEAD BIN AT L2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT HAND OVERHEAD BIN AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040409001612004040900161NM 2004 4 9 AALA20040430 120040405A3350 LIGHT BOEING757 757223 1384957NM L1 DOOR LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21616AA 24524 SFO - EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. SECURED EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040409001662004040900166WP 2004 4 9 AALA20040421 120040403A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21493AA 49731 MSP - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040409001682004040900168EU 2004 4 9 AALA20040433 120040402A5310 SHEAR TIE AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2180057 465 TUL - SHEAR TIE ON FRAME 18 AT STATION 1340 HAS 2 INCH BY 2 INCH SECTION OF CORROSION. REPAIRED FRAME 18 AT SECTION 1340 PER SRM 53-10-13. 2L72 4F RTA35EU 20040409001732004040900173NM 2004 4 9 CALA0400293 120040329A5320BAC1496377 CHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714735 28950 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED FROM STA 727 TO 767 IN AFT CARGO COMPARTMENT. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-00-53 AND 51-10-02. 2L72 4F RTA16WE 20040409001852004040900185EA 2004 4 9 MASA200400137 120040312A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777278 7228 PILOT REPORTED THE EMERGENCY LIGHT PANEL IN THE GALLEY WAS DISCONNECTED AND THE EMERGENCY EXIT SIGN WAS INOP. MX RECONNECTED THE PANEL AND REPLACED THE BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040409001932004040900193WP 2004 4 9 MWEA040037 120040326A573059305032 DOUBLER DOUG DC9 DC981 3022081WP RT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT WIND EXTERIOR BOTTOM AFT SKIN HAS A CORROSION SPOT AT STATION XRS234 STRINGER 17. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040409001942004040900194WP 2004 4 9 MWEA040038 120040326A143059305032 FASTENER DOUG DC9 DC981 3022081WP RIGHT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RIGHT WING EXTERIOR BOTTOM AFT SKIN HAS 3 EACH SPOTS OF CORROSION BETWEEN STATION XRS69 AND XRS91, ALL CORROSION SPOTS ARE WITHIN 14 INCHES OF AFT SPAR T. REMOVED CORROSION AND REMOVED AND REPLACED FASTENERS. 2L72 4F A6WE 20040409001972004040900197WP 2004 4 9 MWEA040041 120040329A5320593607111 INTERCOSTAL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 STATION 636 INTERCOSTAL BETWEEN LONGERON 30 AND 26 RIGHT HAS CORROSION. FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F A6WE 20040409002002004040900200WP 2004 4 9 MWEA040045 120040329A55425957485503 SKIN DOUG DC9 DC981 3022081WP RUDDER DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31806ME 48032 RUDDER SKIN ON LEFT SIDE IS DENTED BETWEEN RIB NR 14 AND 15 FROM TOP AT CENTER OF PANEL. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040409002032004040900203NM 2004 4 9 2004UALA00267 120040321A2120 ODOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29937UA 26668 RETURNED TO FIELD UNDER AMBER ALERT DUE TO A BURNING ODOR IN COCKPIT. CHECKED BEHIND P6-3 PANEL, FOUND WIRE ON R4 APPEARING TO BE BURNT. UPPER ROW OF WIRES THIRD FROM OTBD, WAS BLUE NOW BLACK. RELAY R4 AND REPAIRED BURNED CONNECTOR. 2L72 4F4 FRTA16WE E2GL 20040412000072004041200007EA 2004 4 12 ASOA04134 120040218A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23865AS 7507 DURING A C-CHECK IN MCN, THE RIGHT HYDRAULIC MANIFOLD INTERCOSTAL IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT HYDRAULIC MANIFOLD INTERCOSTAL IN THE AFT EQUIPMENT BAY. (M) 2L72 4F RTA21EA 20040412000142004041200014EA 2004 4 12 ASOA04225 120040319A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11823AS 7196 DURING AN A-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM AT BL 0 ON THE TOP SKIN AT THE FIRE LOOP ATTACH BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM AT BL 0 ON THE TOP SKIN AT THE FIRE LOOP ATTACH BRACKET IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040412000212004041200021WP 2004 4 12 GTIA040184 120040217A7830 THRUST REVERSER DOUG DC9 DC982 3022082WP RIGHT CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND RIGHT THRUST REVERSER UPPER SIDE PITTED HEAVILY. FOUND CRACK IN THE TOP SIDE UPPER DOOR. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040412000232004041200023EA 2004 4 12 ASOA04210 120040315A3397W2275934 WIRE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11723EV 10132 DURING AN A-CHECK IN BTR, THE FORWARD EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE WIRES TO THE FORWARD EMERGENCY LIGHT BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040412000362004041200036WP 2004 4 12 GTIA040192 120040304A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTB - FOUND LEFT OUTBOARD FLOOR PANEL STATION 258-313 HAS PUNCTURE. FOUND ADDITIONAL CRACK. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND HAT CHANNEL. INSTALLED HAT CHANNEL AND DOUBLER. (M) 2L72 4F RTA6WE 20040412000522004041200052WP 2004 4 12 ASAA0480118 120040229A53219932816504 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS CORRODED OUTBOARD OF OUTBOARD TRACK AT FS 256-313. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040412000542004041200054WP 2004 4 12 ASAA0480120 120040229A532099367184 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND RIGHT INTERCOSTAL IS CORRODED AT FS 1309-1322. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040412000602004041200060NM 2004 4 12 QXEA200400150 120040213A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA TE FLAPS ILLUMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 CREW RETURNED TO FIELD WHEN AFTER TAKE OFF THEY RECEIVED A FLAP POWER CAUTION AND THE FLAPS DID NOT RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND ASSOCIATED WIRING, OPERATED THE FLAPS SEVERAL TIMES. NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T4 TRTA13NM E00062EN 20040412000612004041200061NM 2004 4 12 2004UALA00110 120040207A29102724200103 LINE BOEING747 747422 1384935NM PWA 4056 PW4056 NE HYDRAULIC SYSTEMCHAFED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29128UA 30023 FLT HAS HAD NR 1 QTY INDICATION LOSS WITH PSBL HYD PRESS LOSS. AMBER ALERT DECLARED. LOSS OF FLUID DUE TO LANDING GEAR DOWN HYDRAULIC LINE PIN HOLE LEAK. PIN HOLE CAUSED BY CHAFING DUE TO BROKEN CLAMP BACC10CC-8 LOCATED AT STA 900. ACCOMPLISHED RYNGLOK REPAIR AT STA 900 AND RECLAMPED. 2L74 4F4 FRTA20WE E24NE 20040412000632004041200063NM 2004 4 12 AWXA200400301 120040322A335090055 CHARGER BOEING737 737277 1384570NM CABIN FAILED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28178AW 22645 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED AND REMAINED ON WITH THE FLIGHT DECK SWITCH IN ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AT BS 920 AND BATTERY PACKS AT SEAT ROWS 3, 11 & 17 LT AND FORWARD & AFT ENTRY WAY OVERHEADS. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. PART NAME; BATTERY, MFG; IDD AEROSPACE, P/N; 9008-3-5A, COND; LOST CHARGE. 2L72 4F RTA16WE 20040412000842004041200084NM 2004 4 12 AWXA200400322 120040324A5743656717217 FITTING BOEING737 7373G7 1384595NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON LT MAIN LANDING GEAR WALKING BEAM AFT ATTACH LUGS (STABILIZER FITTING) WBL 115.117. MAINTENANCE REMOVED AND REPLACED CORRODED LT MAIN LANDING GEAR WALKING BEAM STABILIZER FITTING IAW BMM 57-15-00. 2L72 4F RTA16WE 20040412000942004041200094NM 2004 4 12 AWXA200400341 120040301A5753654643099 DOUBLER BOEING737 7373G7 1384595NM LT FORE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND EXISTING REPAIR ON UPPER SURFACE OF LT INBOARD FORE FLAP DISBONDED 36 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED DISBONDED REPAIR ON UPPER SURFACE OF LT INBOARD FORE FLAP; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 31 PG 88F-88H. 2L72 4F RTA16WE 20040412001032004041200103SO 2004 4 12 SWIA200413087 120040325A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO LT FLAP FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07271YV7932 7932 120271 FLAP DISAGREEMENT AFTER RETRACTING FLAPS DURING AFTER-LANDING CHECK. REPLACED LEFT NACELLE ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECKS GOOD, LEAK CHECK GOOD. 2L72 4T RTA31SO 20040412001092004041200109NE 2004 4 12 2004UALA00269 220040319A7230 BLADE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 2 ENGINE CRACKED A UALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 WP29783UA 26950 NR 2 ENGINE COMPRESSOR STALLED IN CRUISE. POWER REDUCED TO IDLE. THE 6TH STAGE HPC INNER SHROUD ASSEMBLIES (PW IPC 72-35-00-17-001/-010) WERE FOUND TO HAVE BEEN INSTALLED BACKWARDS. THIS ALLOWED THE SEAL LAND TO MAKE INTERMITTENT CONTACT WITH THE TRAILING EDGE OF ALL OF THE 6TH STAGE BLADES NEAR THE AIRFOIL ROOT. A CRACK STARTED IN THE TRAILING EDGE OF ONE OF THESE BLADES, AND PROGRESSED IN FATIGUE TO THE AIRFOIL MID-CHORD. AT THAT POINT, THE REMAINDER OF THE BLADE FAILED IN STRESS RUPTURE. ALL 6TH STAGE BLADES, AND ALL OTHER HPC BLADES DOWNSTREAM OF THE 6TH STAGE, SUFFERED HEAVY RESULTANT DAMAGE. 2L72 4F4 FRTT0001SE E46NE 20040412001112004041200111NM 2004 4 12 2004UALA00273 120040324A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 FUSELAGE FRAME CRACKED STATION 520 STR 14R. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040412001122004041200112WP 2004 4 12 AALA20040407 120040331A3350 PIN DOUG DC9 DC982 3022082WP CABIN DETACHED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21457AA 49562 DFW - AIRSTAIR EMERGENCY CEILING LIGHT INOPERATIVE. REINSTALLED PIN AND QUICK DISCONNECT ON WIRE FOR AIRSTAIR EMERGENCY CEILING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040412001272004041200127EU 2004 4 12 MALA040297 120040326A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN MALFUNCTIONED A MALAK NONE O OTHER ININSP/MAINT 1 GL15527XJ E2352 BATTERY UNIT WAS REMOVED FOR SCHEDULED BENCH CHECK, IN HOUSE WO 365156, BATTERY FAIL CAPACITY CHECK, BATTERY PACK P/N 61-2275-1, S/N 9912223 FOR EMERGENCY LIGHT EVAC SYSTEM. PROBLEM WAS FOUND OFF AIRCRAFT IN SHOP ENVIRONMENT, A/C WAS NOT GROUNDED. BATTERY ASSEMBLY P/N 61-2275-1 WAS REPLACED, UNIT PASSED GMM TESTS AND WAS RETURNED TO SERVICE ON 3/30/04. 2H74 4F RTA49EU 20040412001452004041200145NM 2004 4 12 AWXA200400338 120040302A534069414372 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 663, STR 10 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2L72 4F RTA16WE 20040412001472004041200147NM 2004 4 12 AWXA200400340 120040303A53206545834523 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 311, BL 0. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 311, BL 0; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20040412001582004041200158EU 2004 4 12 G1F2004F00002 120040209A7810FGFB582800D2 TAILPIPE AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE NR 3 ENGINE CORRODED B G1FRK NONE O OTHER ININSP/MAINT 1 GL13312P 67 IT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC, PAINT HAS BEEN BUBBLING AND STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON THIS SPECIFIC AC, ALL OF CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. AREA OF CORROSION IS 19 INCHES LONG AND 7.5 INCHES WIDE. CORRODED AREA IS AT 3 O’CLOCK POSITION ON NR 2 ENGINE, VIEW LOOKING FORWARD AND 9 O’CLOCK POSITION ON THE NR 3 ENGINE, VIEW LOOKING FORWARD. THE HEAT FROM THE ENGINE EXHAUST IS CAUSING THE PAINT TO PEEL, ALLOWING MOISTURE INTRUSION UNDER THE FASTENER HEADS. BLENDED AREA RESULTS SUBMITTED TO MFG ENGINEERING FOR REVIEW AND DISPOSITION. 2L73 4F4 FRTA46EU E1NM 20040412001692004041200169WP 2004 4 12 GTIA040142 120040222A3260 UPLOCK HOOK DOUG DC9 DC983 3022083WP LT MLG LACK OF LUBE A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23833NK 49449 AFTER DEPARTURE LEFT GEAR LIGHT REMAINED RED WITH DOOR LIGHT OUT, COMPLIED WITH QRH. CYCLED GEAR, LIGHT WENT OUT. PERFORMED OPS CHECK OF PSEU AND FOUND NORMAL. CHECKED UPLOCK SENSOR ON MLG AND CHECKED 'GAP' AND FOUND NORMAL. LUBED UPLOCK HOOK MECH. (M) 2L72 4F RTA6WE 20040412001742004041200174EA 2004 4 12 ASOA04142 120040220A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11862AS 7476 DURING HANGAR MAINTENANCE IN BTR, THE LEFT REAR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT REAR OVERWING EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040412001822004041200182WP 2004 4 12 GTIA040140 120040221A2560 GLOWSTRIP DOUG DC9 DC981 3022081WP CABIN MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 DTW - FOUND SAFETY GLO FLOORPATH STRIP MISSING IN AFT GALLEY, L2 DOOR. RESECURED SAFETY GLO FLOORPATH LIGHTING. NO OTHER DEFECTS NOTED. (M) 2L72 4F A6WE 20040412001852004041200185EA 2004 4 12 ASOA04140 120040219A5320601R3117121 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES PRESSURE FLOOR SKIN AREA OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES PRESSURE FLOOR SKIN AREA OUTBOARD IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040412001982004041200198WP 2004 4 12 ASAA0480148 120040302A53219936582 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 946-1003 CENTER HAS DELAMINATION AROUND EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040412002042004041200204WP 2004 4 12 ASAA0480140 120040301A7110219006077 NOSE COWL DOUG DC9 DC983 3022083WP LT ENGINE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, LEFT ENGINE NOSE COWL IS CRACKED AT AFT FLANGE 7 O'CLOCK POSITION. REMOVED DAMAGED SECTION. REPAIRED WITH DOUBLER AND FILLER PER EA 7110-01221. (M) 2L72 4F RTA6WE 20040413000322004041300032WP 2004 4 13 CALA0400353 120040410A57309937512501 SKIN DOUG DC9 DC982 3022082WP LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772822 49482 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING SKIN JUST FORWARD OF PANEL 1196C UPPER LEFT WING AREA, STA XOS 286. REPAIRED IAW ECRA 5720-01946. 2L72 4F A6WE 20040413000342004041300034NM 2004 4 13 CALA0400355 120040411A5320 WEB BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715712 28783 INSPECTION FOUND A 4 INCH CRACK IN RIGHT MLG SKI JUMP O/B WEB. THE WEB WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040413000382004041300038NM 2004 4 13 CALA0400359 120040411A5330141A31125 SKIN BOEING737 737824 13844BZNM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO RIVET AT STA 328, L22L. REPAIRED IAW ECRA 5331-01141. 2L72 4F RTA16WE 20040414000012004041400001WP 2004 4 14 04FDEA00845 120040406A5270 SWITCH DOUG DC10 DC1010 3022110WP AC PACK DOOR MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO2540061 46973 THE AIR COND DOORS LIGHT ILLUMINATED CLIMBING OUT AT 7.5 PSID. THE LIGHT WENT OUT AT 4.0 PSID. FOLLOWED QRH PROCEDURES, RETURNED TO MEMPHIS. RELEASED FOR SERVICE PER MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 16APR04 MEL 52-04-04: AIR CONDITIONING DOOR CAUTION LIGHT INOP. VERIFY AND RECORD IN AML/EAML AIR CONDITIONING DOOR IS CLOSED AND LOCKED BY VISUAL INSPECTION PRIOR TO EACH DEPARTURE. VERIFIED DOORS CLOSED AND LOCKED PRIOR TO DEPARTURE. OK TO CONTINUE. MX REMOVED AND REPLACED LEFT AIR COND DOOR WARNING SWITCH P1- 1618. ALSO REPAIRED BROKEN WIRE AT TERMINAL STRIP S3-490. SYS OPS CHECK OK. 2L73 4F A22WE 20040414000032004041400003NM 2004 4 14 04FDEA00827 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654, LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000042004041400004NM 2004 4 14 04FDEA00828 120040403A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE HOLE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1 2L73 4F RTA22WE 20040414000072004041400007WP 2004 4 14 04FDEA00831 120040404A5311 FRAME DOUG DC10 DC1010 3022110WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 INSIDE ATTIC-TAIL SECTION CANTED FRAMES AT Y-2046.00 Y-2069.44 AND Y-2092.88 ARE CRACKED. REMOVED DAMAGED CLIPS IAW SRM 51-30-01 AND SRM 51-31-01. LOCATED AND INSTALLED REPAIR CLIPS IAW SRM 51-31-01 AND SRM 51-33-01. 2L73 4F A22WE 20040414000112004041400011EU 2004 4 14 MALA040308 120040404A33505521981 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL1579XJ 340A079 BATTERY PACK 61-0478-9 SN/ 38A, WAS REMOVED FOR A SCHEDULED CAPACITY CHECK. THE UNIT FAILED ON 4/4/04 AND BATTERY ASSEMBLY P/N 55-2198-1 WAS REPLACED. UNIT PASSED COMM TESTS AND WAS RETURNED TO SERVICE ON 4/7/04. 2L72 4T RTA52EU 20040414000122004041400012EU 2004 4 14 MALA040300 120040215A33506013211 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15361PX 340B249 EMERGENCY LIGHTS INOP OR LIGHTS ARE DIM. MAINTENANCE REPLACED BATTERY PACK P/N 60-1321-1, S/N 18158 WAS FOUND INOP ON BENCH, Q1, Q2, Q3, Q4 & Q5 ALONG WITH V1, SCR1, C1, C4 & C5 WERE REPLACED AND LENS ON C2 & C2 WERE RESOLDERED. VNH CHECKED GOOD IAW AMM, AND WAS RETURNED TO SERVICE 4/2/04. 2L72 4T RTA52EU 20040414000142004041400014EU 2004 4 14 MALA040304 120040331A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15450XJ 340B450 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 2137 WAS REMOVED FOR SCHEDULED BENCH CHECK ON 3/18/04. ON 3/31/04 UNIT FAILED BATTERY CAPACITY CHECK. BOTH BATTERY PACKS P/N 549-1324-06 WERE REPLACED AND UNIT WAS CHARGED. ALL SUBSEQUENT CHECKS WERE GOOD IAW CMM UNIT WAS RETURNED TO SERVICE 4/2/04. 2L72 4T RTA52EU 20040414000152004041400015EU 2004 4 14 MALA040305 120040402A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 RIGHT I/B SEAT TRACK HAS CORROSION AT STA 292. REPAIRED SEAT TRACK IAW MESABA EO S53060. A/C RETURNED TO SERVICE 4/2/04. 2L72 4T RTA52EU 20040414000162004041400016NM 2004 4 14 04FDEA00835 120040405A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 755 LBL 29 FOUND CRACKED. SEAT TRACK AT STA 745 TO STA 785 LBL 27.5 CUT AND REMOVED, CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20040414000182004041400018NM 2004 4 14 04FDEA00837 120040405A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT OUTBOARD FLAP NR 2 FLAP UP STOP BOLT FITTING FOUND CRACK AT THE STOP BOLT BARREL NUT AREA AT TWO PLACES. REMOVED IAW SRM 51-31-01 VOL II AND INSTALLED NEW FITTING IAW SRM 51-33-01 VOL II AND DWG ARC4125. 2L73 4F RTA22WE 20040414000192004041400019NM 2004 4 14 04FDEA00838 120040405A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT OUTBOARD FLAP NR 2 FLAP UP STOP BOLT FITTING SUSPECT CRACK AT THE STOP BOLT BARREL NUT AREA. REMOVED AS PER SRM 51-31-01 VOL II AND NEW STOP FITTING INSTALLED AS PER SRM 51-33-01 VOL II AND DRAWING ARC4125. 2L73 4F RTA22WE 20040414000212004041400021EU 2004 4 14 MALA040306 120040403A5210 DOOR SEAL SAAB SF340 340B 7860101EU PAX DOOR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15361PX 340B249 CABIN PRESSURE CWP MASTER WARNING ON. NO CONTROL IN MANUAL MODE, UNABLE TO CONTROL PRESS, WOULD NOT OPERATE IN AUTO AND WOULD ONLY WORK INTERMITTENTLY IN MANUAL. AIR RETURN TO DTW. MAINTENANCE FOUND PAX DOOR SEAL BLOWN OUT. REMOVED AND REPLACED PAX DOOR SEAL IAW SF340 AMM CH 52-10-15-4. LEAK CHECK GOOD. PERFORMED AUTO AND MANUAL PRESSURIZATION CHECKS, ALL CHECKS GOOD. 2L72 4T RTA52EU 20040414000222004041400022EU 2004 4 14 MALA040301 120040327A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 FS 280 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASED 3/31/04. 2L72 4T RTA52EU 20040414000232004041400023EU 2004 4 14 MALA040307 120040404A2612 FIRE DETECTOR SAAB SF340 340B 7860101EU LT ENGINE SHORTED A MALAC ABORTED TAKEOFF N FALSE WARNING TXTAXI/GRND HDL 1 GL15424XJ 340B424 LEFT FIRE DETECT FAIL CWP LIGHT IS ON. AFTER START LEFT FIRE DETECT FAIL LIGHT REMAINED ILLUMINATED. MAINTENANCE TROUBLESHOT PER SF3 MM 26-11-00-1 (FAULT ISOLATION 102). FOUND SHORT TO GROUND AT FIRE LOOP SENSOR 11WG. CLEANED MUCH DEBRIS FROM CENTER PIN ON EACH END OF LOOP. RE-INSTALLED, ALL CHECKS GOOD PER 26-11-00-5. LEFT FIRE DETECT FAIL TEST GOOD. LEFT FIRE TEST GOOD. A/C OK FOR SERVICE. 2L72 4T RTA52EU 20040414000272004041400027NM 2004 4 14 UPS04442099 120040324A5330 SKIN BOEING747 747121 1384871NM FUSELAGE BULGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, FX - LOWER FUSELAGE EXTERNAL SKIN FOUND BILGE UP AT STA 1000 STR 40L TO STR 41L. BS 980-998 BETWEEN STR 40L AND STR 41L SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION PER SRM 53-30-03 FIG 1 TABLE 4. 2L74 4F A20WE 20040414000282004041400028NM 2004 4 14 UPS04442100 120040325A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, TAIL FUSELAGE FWD OF 2360 S3L - S5L VERTICAL FIN LWR PANEL ATTACHMENT AREA CHAFE MARKS FOUND. BS 2335 - BS 2355 BETWEEN STR 4L AND STR 3L CHAFED SKIN REPAIRED PER SRM 53-30-03 FIG 1 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION PER SRM 53-30-03 FIG 1 TABLE 4. 2L74 4F A20WE 20040414000312004041400031NM 2004 4 14 UPS04M42091 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 20 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM, SURFACE MATERIAL REMOVED 0.019 INCH. BARREL NUT HOLE REPAIR PER EN1022-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000332004041400033WP 2004 4 14 UPS04842088 120040401A3350 LAMP DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 EMERGENCY LIGHTS ABOVE COCKPIT DOOR INOP. RELAMPED, OPS CHECK OK. 2L74 4F RT4A25 20040414000342004041400034NM 2004 4 14 UPS04M42084 120040130A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL RIGHT NR 01 NUT HOLE FOUND CORROSION ON BARREL NUT BEARING SURFACE (FWD & AFT) AND BOTTOM EDGE. CORROSION REMOVED AT NR 1 HOLE RIGHT BOTTOM SURFACE PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.060 INCH. BARREL NUT HOLE REPAIRED PER EN1009 -04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000362004041400036NM 2004 4 14 UPS04M42086 120040211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER LEFT NR 01 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED AT HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.094 INCH. BARREL NUT HOLE REPAIRED PER EN1033-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000372004041400037NM 2004 4 14 04FDEA00848 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT I/B FLAP, O/B HINGE I/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2L73 4F RTA22WE 20040414000382004041400038NM 2004 4 14 04FDEA00849 120040407A7800669472001 DUCT BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE NR 3 ENG FAN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25279FE 22346 COMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE. 2L73 4F4 FRTA3WE E2EA 20040414000392004041400039NM 2004 4 14 04FDEA00850 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT I/B FLAP, O/B HINGE O/B STRAP PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2L73 4F RTA22WE 20040414000412004041400041NM 2004 4 14 04FDEA00852 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000442004041400044NM 2004 4 14 04FDEA00878 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000452004041400045NM 2004 4 14 04FDEA00879 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000472004041400047NM 2004 4 14 04FDEA00881 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000482004041400048NM 2004 4 14 04FDEA00882 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000492004041400049NM 2004 4 14 04FDEA00855 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED. 2L73 4F RTA22WE 20040414000522004041400052NM 2004 4 14 04FDEA00858 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000552004041400055NM 2004 4 14 04FDEA00861 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000582004041400058NM 2004 4 14 04FDEA00863 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649,CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000592004041400059NM 2004 4 14 04FDEA00864 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000602004041400060NM 2004 4 14 04FDEA00865 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000612004041400061NM 2004 4 14 04FDEA00866 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000622004041400062NM 2004 4 14 04FDEA00867 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE INNER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000632004041400063NM 2004 4 14 04FDEA00868 120040408A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648. 2L73 4F RTA22WE 20040414000642004041400064NM 2004 4 14 04FDEA00869 120040408A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOT FACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMIT AS PER DRAWING ARC0502, SHT.4, ZONE 40. 2L73 4F RTA22WE 20040414000682004041400068EU 2004 4 14 04FDEA00925 120040412A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP 2ND CARGO TRACK FROM CENTER RT SIDE BETWEEN FRAMES 77 AND 78, 2 EA AREAS OF CORROSION, UPPER SURFACE. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT AND REMOVED DAMAGED SECTION OF CARGO TRACK, FABRICATED NEW SECTION OF CARGO TRACK, LOCATED AND DRILLED NEW SPLICES, INSTALLED CARGO TRACK AND SPLICES IAW A300-600 SRM 53-10-16 FIG 208. 2L72 4F RTA35EU 20040414000732004041400073NM 2004 4 14 04FDEA00900 120040412A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 AFT CARGO COMPARTMENT, RIGHT MOST O/B FLOOR SUPPORT UPPER & LOWER SURFACE FOUND WITH SEVERAL PLACES CORROSION. FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040414000752004041400075NM 2004 4 14 04FDEA00902 120040412A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN STA 475 CBL FOUND FLOORBEAM CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM ON FWD CABIN STA 475 CENTER BUTTOCK LINE AS PER AMM 53-21-04. 2L73 4F RTA22WE 20040414000772004041400077NM 2004 4 14 04FDEA00842 120040406A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643, TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040414000782004041400078WP 2004 4 14 04FDEA00843 120040406A5744ARC01540 HINGE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-75134 WINGS RIGHT INBOARD FLAP, HINGE ASSY ATTACH LUG REWORK. COMPLIED WITH EA 8-5740-75134. 2L73 4F RTA22WE 20040414000842004041400084NM 2004 4 14 04FDEA00874 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE I/B STRAP PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651. TRAILING EDGE FLAPS LT & RT INBOARD FLAP OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040414000862004041400086NM 2004 4 14 04FDEA00876 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000882004041400088NM 2004 4 14 CALA0400333 120040407A5510180A16121 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733714 28785 INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040414000922004041400092NM 2004 4 14 04FDEA00904 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040414000932004041400093NM 2004 4 14 04FDEA00905 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040414000942004041400094NM 2004 4 14 04FDEA00906 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040414000952004041400095NM 2004 4 14 04FDEA00907 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040409001472004040900147EU 2004 4 9 MALA040292 120040329A243023080031 STARTER GEN SAAB SF340 340B 7860101EU LT ENGINE FAILED A MALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15438XJ 340B438 THE LT STARTER FAILED DURING START. NO STARTER CUTOUT ON LEFT ENGINE, SAW SMOKE COMING OUT OF LEFT ENGINE INBOARD STARTER/GENERATOR VENT. MAINTENANCE VERIFIED DC STARTER/GENERATOR WAS INTERNALLY BURNED OUT, CAUSING SMOKE; NO OTHER FIRE OR DAMAGE EVIDENCE IN ENGINE NOTED. REPLACED LEFT DC STARTER/GEN P/N 23080-031, S/N ON-97381, S/N OFF-6925; ALSO REPLACED LEFT DC GCU, S/N ON-96582, S/N OFF-99700. RAN ENGINE, ALL CHECKS ARE GOOD. 2L72 4T RTA52EU 20040409001532004040900153NM 2004 4 9 CALA0400283 120040326A335020121 CHARGER BOEING757 757224 1384958NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2734137 30229 INSPECTION FOUND R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY CHARGER AT STA 340 (IN OVERHEAD AT FORWARD LAV & COCKPIT DOOR) WAS FOUND AT FAULT. THE CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07. 2L72 4F RTA2NM 20040409001742004040900174NM 2004 4 9 CALA0400294 120040330A5320143A7505 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND RIGHT INTERCOSTAL CRACKED AT STA 500C TO 500D IN FORWARD PIT. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-00-53 AND 53-30-53. 2L72 4F RTA16WE 20040409001772004040900177NM 2004 4 9 AALA20040365 120040319A3350 LIGHT BOEING757 7572Q8 1384972NM ROW 1 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21701TW 28160 DFW - EMERGENCY FLOOR TRACK LIGHTING AT FIRST CLASS ROW ONE INOPERATIVE. REPLACED POWER STRIP FOR EMERGENCY FLOOR TRACK LIGHTING AT FIRST CLASS ROW ONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040409001782004040900178 2004 4 9 AALA20040375 420040319A2565 BOTTLE BOEING767 767323 1385205NM ESCAPE SLIDE DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21366AA 25193 SFO - RIGHT HAND OVERWING SLIDE BOTTLE PRESSURE IS LOW. REPLACED RIGHT HAND OVERWING SLIDE BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040409001882004040900188EA 2004 4 9 MASA200400147 120040318A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747202 7202 CREW REPORTED RT SIDE EXTERIOR EMERGENCY LIGHT INOP. MX WAS CALLED. DURING THE RON MX REPLACED THE BULB. 2L72 4F RTA21EA 20040409001892004040900189EA 2004 4 9 MASA200400148 120040319A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775999 7361 THE CAPT REPORTED THE 3RD FROM THE FRONT OVERHEAD EMERGENCY EXIT LIGHT WAS INOP. MX REPLACED THE BULB. OP CHECKS GOOD. 2L72 4F RTA21EA 20040412000272004041200027WP 2004 4 12 GTIA040183 120040216A5553 ATTACH ANGLE DOUG DC9 DC982 3022082WP DORSAL FIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND RIGHT SIDE DORSAL FIN ATTACH ANGLE CRACKED THROUGH VERTICAL LEG AND INTO 1ST ROW OF FAST ON HORIZONTAL LEG AND GOUGED AND BROKEN FAST. DYE PEN INSPECTION SHOWS NO CRACKS. REMOVED RIGHT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND RIGHT INNER ATTACH ANGLE CRACKED IN SEVERAL PLACES. REMOVED RIGHT INNER ATTACH ANGLE AT DORSAL FIN. INSTALLED GUSSET PER MD80 SB DC0-53-223. INSTALLED RIGHT INBOARD ATTACH ANGLE AND OUTBOARD RIGHT ATTACH ANGLE PER MD80 SB NO DC9-53A223 RO2 AND SBDC9-223. (M) 2L72 4F A6WE 20040412000352004041200035WP 2004 4 12 GTIA040190 120040304A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP COCKPIT CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR PANEL FIRST OFFICERS SIDE, CORRODED, DISBONDED, STIFFENER BENT. REBONDED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000372004041200037WP 2004 4 12 GTIA040193 120040314A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR PANEL LEFT OUTBOARD STATION 1250-1309 HAT CHANNEL BROKEN OUT. REPAIRED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040412000532004041200053WP 2004 4 12 ASAA0480119 120040229A53305924802541 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND SKIN DENTED/GOUGED AT FS 351. INSTALLED FILLER AND DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040412000592004041200059WP 2004 4 12 ASAA0480154 120040302A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 927-1003 HAS CRACK IN SKIN AND DELAMINATION AROUND EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040412000622004041200062 2004 4 12 AWXA200400300 420040322A2350285T002239 SELECTOR PANEL BOEING757 7572S7 1384962NM COCKPIT SHORTED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28905AW41042365 23567 PHX - SMOKE - FLT 0052 - EN ROUTE FROM SJD TO PHX FLIGHT CREW NOTICED SMOKE EMANATING FROM BOOM / OXYGEN SWITCH ON NR 2 AUDIO SELECTOR PANEL, SMOKE STOPPED SHORTLY AFTER IT WAS NOTICED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AUDIO SELECTOR PANEL IAW BMM 23-51-01, OPERATIONAL CHECK WAS GOOD. VENDORS SHOP EVALUATION OF AUDIO SELECTOR PANEL S/N D00410 CONFIRMED REASON FOR REMOVAL FINDING RESISTOR (R1) AND CAPACITOR (C1) ON A2 CIRCUIT BOARD BURNED. REPLACED RESISTOR (R1) AND CAPACITOR (C1) ON A2 CIRCUIT BOARD, AND REPLACED OXYGEN / BOOM SWITCH PER E.O. 2350 01001. UNIT CLEANED, INSPECTED, AND TESTED IAW CMM 23-51-54, REV. 27. 2L72 4F RTA2NM 20040412000672004041200067NM 2004 4 12 AWXA200400292 120040318A53306595774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - MAJOR REPAIR - A 5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 23 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN BS 727E, STR 23 LT; FABRICATED REPAIR IAW B737-300 SRM 53-00-01 FIG 229, DETAILS 11 & 18. 2L72 4F RTA16WE 20040412000732004041200073NM 2004 4 12 AWXA200400345 120040404A2560P4010021 BATTERY BOEING737 737277 1384570NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040412000772004041200077EU 2004 4 12 AWXA200400349 120040327A5321D53670049001 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND 3 EACH CRACKS IN CABIN FLOOR PANEL 261EF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 261EF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367049; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236. 2L72 4F RTA28NM 20040412000802004041200080NM 2004 4 12 AWXA200400318 120040302A52106545871515 DOOR FRAME BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .4375 INCH CRACK WAS FOUND ON AFT FRAME OF R-1 DOOR AT 3RD STOP FITTING CUTOUT FROM THE BOTTOM BS 327, STR 13 RT. MAINTENANCE TRIMMED OUT DAMAGE IN AFT FRAME OF R-1 DOOR AT 3RD STOP FITTING CUTOUT FROM THE BOTTOM. PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW ER 03-5210-04081-SS1. 2L72 4F RTA16WE 20040412000832004041200083NM 2004 4 12 AWXA200400321 120040303A53156545812 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER CHORD OF FLOORBEAM AT BS 328, RBL 27 TO RBL 50, WL 208. MAINTENANCE REMOVED DAMAGED SECTION FLOORBEAM UPPER CHORD AT BS 328, FROM RBL 27 TO RBL 50. FABRICATED 5 REPAIR ANGLES AND NEW REPLACEMENT SECTION OF UPPER CHORD; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205, SHEETS 1-5. 2L72 4F RTA16WE 20040412000912004041200091NM 2004 4 12 AWXA200400357 120040407A533065C3579415 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 PHX - MAJOR REPAIR - A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 22 LT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 727E, STR 22 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20040412000952004041200095EU 2004 4 12 AWXA200400360 120040328A5320D5347112420100 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT OUTBOARD SHEAR PLATE, OUTBOARD OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED AND REPLACED RT OUTBOARD SHEAR PLATE IAW AIRBUS A320 SRM 51-42-11. 2L72 4F RTA28NM 20040412000972004041200097SO 2004 4 12 SWIA200413081 120040228A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07216SW 120285 LEFT NACELLE FRAME ONE IS CRACKED ON INBOARD AND OUTBOARD SIDES. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT NACELLE FRAME ONE IAW 120 SB 120-54-0036 & 120 SRM 51-10-02 PG 3 PAR 3. ACCOMPLISHED PART II OF SB 120-54-0036. 2L72 4T4 TRTA31SO E20NE 20040412001002004041200100 2004 4 12 SWIA200413084 420040322A2210 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT JAMMED A SWIAK NONE O OTHER TXTAXI/GRND HDL 1 NM07466SW 7856 YAW DAMPER NR 1 ENGAGE SWITCH JAMMED IN FLUSH POSITION. UNABLE TO ENGAGE YAW DAMPER 1. REMOVED AND REPLACED YAW DAMPER CONTROL PANEL. OPS CHECK GOOD. P/N: 601R51594-1. 2L72 4F RTA21EA 20040412001012004041200101 2004 4 12 SWIA200413085 420040323A3418 WARN PANEL EMB 120 EMB120ER 3260203SO STALL WARNING FAULTY A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07270YV 120270 FIRST OFFICER'S STALL WARNING INDICATOR WILL NOT TEST. REPLACED STALL WARNING TEST PANEL. OPS CHECKS GOOD. P/N: 120-34428-505, SN OFF: 120186. 2L72 4T RTA31SO 20040412001042004041200104EA 2004 4 12 SWIA200413088 120040324A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW 7497 PASSENGER DOOR SEAL STRIKER CRACKED AT FORWARD AND AFT PIN RECEPTACLES. DISCOVERED DURING B003 INSPECTION. REPAIRED IAW REO 601R-52-11-008. 2L72 4F4 FRTA21EA E15NE 20040412001052004041200105EA 2004 4 12 SWIA200413089 120040326A32347455025 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07967SW 7872 WHEN LANDING GEAR SELECTED DOWN, GEAR WOULD NOT LOWER. HANDLE HAD LESS RESISTANCE THAN NORMAL. FOLLOWED GEAR DOWN DISAGREE PROCEDURE TO LOWER MANUALLY. HYDRAULICS INDICATED NORMAL PRESSURE. PERFORMED EMERGENCY LANDING AT SFO. UPON LANDING, LOST NOSE WHEEL STEERING. REPLACED LANDING GEAR SELECTOR. OPS CHECKED GOOD. PERFORMED GEAR SWING. GEAR SWING CHECKED GOOD. 2L72 4F RTA21EA 20040412001072004041200107 2004 4 12 MWEA040030 420040322A34180861EWR TRANSDUCER DOUG DC9 DC982 3022082WP NR 2 FAULTY A MWEAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31809ME 48071 STALL INDICATION LIGHT CAME ON. CLEANED LEFT AND RIGHT FLAP POSITION TRANSMITTER CANNON PLUG, REMOVED AND REPLACED NUMBER TWO ANGLE OF ATTACK TRANSDUCER. 2L72 4F A6WE 20040412001142004041200114EU 2004 4 12 AALA20040409 120040331A3260BDM3003 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217083A 645 SJU - INFLIGHT T882 BOTH MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. NOSE GEAR RETRACTED. UNSAFE CONDITION ON BOTH MAIN GEAR AND DOOR OPEN LIGHTS ILLUMINATED. ECAM LANDING GEAR WILL NOT RETRACT. LANDED SJU WITHOUT INCIDENT. REPLACED PROXIMITY BOX. VISUALLY INSPECTED SENSOR AND TARGETS FOR GENERAL CONDITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040412001152004041200115NE 2004 4 12 AALA20040410 220040331A7250 TURBINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED A AALAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SW2176202 53292 717314 DFW - INFLIGHT T1573 RIGHT HAND ENGINE HAD A CONTAINED TURBINE FAILURE AT 5600 FEET. AIRCRAFT LANDED OVERWEIGHT. 2L72 4F4 FRTA6WE E9NE 20040412001202004041200120NM 2004 4 12 CALA0400259 120040320A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 INSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR FRAME UPPER CLOSE OUT WEB AT STA 847. A WEB REPAIR WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20040412001312004041200131NM 2004 4 12 2004UALA00275 120040323A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 STRINGER SPLICE AT BS 907 STR 4L IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRINGER SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040412001372004041200137NM 2004 4 12 2004UALA00284 120040325A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29193UA 26890 EMERGENCY LIGHTS FLASHING IN ALL ZONES. COULD NOT DUPLICATE. LIGHTS CHECKED GOOD. 2L74 4F4 FRTA20WE E24NE 20040412001392004041200139NM 2004 4 12 AWXA200400334 120040325A2497W9118814 WIRE BOEING737 7373Y0 1384671NM COCKPIT ARCED A AWXAO OTHER BJGSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION MULTIPLE FAILURE LDLANDING 1 WP28334AW 23747 ON TOUCHDOWN ARCING & SMOKE AT P6 C/B PANEL BEHIND F/O, NUMEROUS C/B'S POPPED. MX FOUND WIRE BUNDLES ARCED BEHIND P-6 (3) C/B PANEL. FOUND A SCREW SECURING GUSSET (BOTTOM OF P6 (3) PANEL) BS 254, RBL 21 CHAFED THROUGH BUNDLE, CLOSE PROXIMITY OF HARNESSES ARCING SPREAD FROM ONE BUNDLE TO OTHER. MX REPLACED 67 WIRES C/B'S ON P6 (2) & P6 (3) C/B PANELS TO VARIOUS CONNECTORS & RELAYS. REPLACED 7 C/B ON P6 (3) PANEL & GUSSET BEHIND P-6 (3) BS 254, RBL 21, ARCING DAMAGE. SYS AFFECTED BY DAMAGE: FLT CONTROL SHUTOFF VALVE, AUTO FLT CONTROL, ELECT HYD PUMP, AUDIO 1 & 2, (ENG 1 & 2 FIRE PROTECTION, SYNC-LOCK, IGNITION, IDLE CONTROL EGT, T/R CONTROL), FUEL QTY, COCKPIT LIGHTING & STAB TRIM ACTUATOR. 2L72 4F RTA16WE 20040412001842004041200184WP 2004 4 12 GTIA040137 120040219A33501001191 CLIP DOUG DC9 DC982 3022082WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 DTW - FOUND FORWARD ENTRY EMERGENCY EXIT LIGHT HAS BROKEN RETAINING CLIP. REMOVED AND REPLACED FORWARD ENTRY LIGHT ASSEMBLY. (M) 2L72 4F A6WE 20040412001892004041200189WP 2004 4 12 ASAA0480108 120040224A5753591004329 VANE DOUG DC9 DC983 3022083WP T/E FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HVC CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD CAM AND VANE LEADING EDGE ARE CHAFED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2 AND 57-03. (M) 2L72 4F RTA6WE 20040412001902004041200190WP 2004 4 12 ASAA0480109 120040224A531199115173 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND E/E COMPARTMENT FRAME CORRODED AT FS 200. REMOVED DAMAGED SECTION. INSTALLED SHIM, PLATE, AND ANGLE PER SRM 53-03. (M) 2L72 4F RTA6WE 20040412001942004041200194WP 2004 4 12 ASAA0480121 120040229A5320991555415 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND LEFT INTERCOSTAL IS CORRODED ON FLANGE AT FS 788. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040413000072004041300007NM 2004 4 13 CALA0400351 120040410A532065C32707Y WEB BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND LEFT AFT LAV WEB CORRODED AT STA 1006-1016. THE WEB WAS REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040413000352004041300035NM 2004 4 13 CALA0400356 120040411A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND LT ZEE CHANNEL CORRODED IN AFT PIT BETWEEN STA 727-847. THE ZEE CHANNEL WAS REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040413000372004041300037NM 2004 4 13 CALA0400358 120040411A532065C3397035 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717663 28924 INSPECTION FOUND A 1.5 INCH CRACK IN CABIN FLOOR INTERCOSTAL BETWEEN FS 344-360, LBL 12. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040414000052004041400005NM 2004 4 14 04FDEA00829 120040404A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT AFT (FLAP SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76645, PART 1, LT OUTBOARD FLAP INBD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BUSHINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000132004041400013EU 2004 4 14 MALA040303 120040329A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 FS 280 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 280 IAW MESABA EO S53060. A/C RELEASED 4/1/04. 2L72 4T RTA52EU 20040414000172004041400017NM 2004 4 14 04FDEA00836 120040405A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 755 RBL 29 FOUND CRACKED. SEAT TRACK AT STA 745 TO STA 816 RBL 27.5 CUT AND REMOVED, CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20040414000402004041400040NM 2004 4 14 04FDEA00851 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT I/B FLAP, O/B HINGE O/B LUG PIVOT HOLE FOUND WITH CORROSION. CORROSION REPAIRED. 2L73 4F RTA22WE 20040414000502004041400050NM 2004 4 14 04FDEA00856 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED. 2L73 4F RTA22WE 20040414000572004041400057NM 2004 4 14 04FDEA00862 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649. WING LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000692004041400069WP 2004 4 14 04FDEA00888 120040409A5753ARC2512 HINGE DOUG MD10 MD1010F 3022112WP RT IB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5750-75128 WINGS - RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR {P/N ARC2 512}. COMPLIED WITH EA 8-5750-75128, WINGS RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR (P/N ARC2512) AT MAE. 2L73 4F RTA22WE 20040414000702004041400070WP 2004 4 14 04FDEA00889 120040409A5753ARC0538501 BRACKET DOUG MD10 MD1010F 3022112WP LT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 5740-77336A WINGS - LT OUTBOARD FLAP - FWD CLEVIS BRACKET ASSY CORROSION REPAIR (P/N ARC0538-501). COMPLIED WITH EA 8-5740-77336A WINGS - LT OUTBOARD FLAP - FWD CLEVIS BRACKET ASSY CORROSION REPAIR (P/N ARC053 8-501) AT MAE. 2L73 4F RTA22WE 20040414000792004041400079WP 2004 4 14 04FDEA00844 120040406A5511 SPAR DOUG DC10 DC1010 3022110WP ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 COMPLY WITH EA 8-5510-75123 STABILIZER OVERSIZE HOLES IN HORIZ STAB CENTER SECTION AFT SPAR. COMPLIED WITH EA 8-5510-75123. 2L73 4F A22WE 20040414000832004041400083NM 2004 4 14 04FDEA00873 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE O/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2L73 4F RTA22WE 20040414000892004041400089NM 2004 4 14 04FDEA00886 120040407A2120 SMOKE DOUG MD11 MD11 3023602NM DETECTED A FDEAE ENGINE SHUTDOWN BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LDLANDING 1 SO25587FE 48489 AT 200 FT AGL ON LANDING IN SFS, GOT A CABIN SMOKE LVL 3 ALERT, IT WENT OUT SHORTLY. ALERT ON AGAIN DURING LANDING ROLL, THEN OUT. EMERGENCY DECLARED. ON TAXI IN, CABIN SMOKE LEVEL 3 ALERT ON STEADY. APU RUNNING. ENGINE SHUTDOWN. F/O SMELLED SMOKE. EMERGENCY EVACUATION DECLARED. REMOVED AND REPLACED SMOKE CARGO COMPT DETECTOR AFT CARGO DETECTOR 5 PER MM 26-14-01-4, OPS CHECK PER MM 26-14-01-5 PASSED. REMOVED AND REPLACED NR 2 FIREX ENG/APU CONTAINER. REMOVED AND REPLACED MSC, OPS TEST. REMOVED AND REPLACED NR 1, 2 AND 3 WATER SEPARATOR AMM 21-54-05-2. C/W MTSI ITEM NR 3 WRI 26-1/9032 AIR CONDITIONING PACK AND DISTRIBUTION DUCT ODOR CHECK PER MM 21-53-00-7 SATISFACTORY, A/C OK FOR SERVICE. 2L73 4F RTA22WE 20040414000972004041400097NM 2004 4 14 CALA0400335 120040407A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED BETWEEN BS 907 AND 947. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52. 2L72 4F RTA16WE 20040414001002004041400100WP 2004 4 14 CALA0400338 120040407A533059114123 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772822 49482 INSPECTION FOUND EXTERIOR FUSELAGE SKIN BULGED WITH RIVETS POPPING AROUND LOWER TCAS ANTENNA AND A 2 INCH CRACK WAS FOUND IN SKIN FORWARD OF TCAS ANTENNA AT STA 237. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12C. 2L72 4F A6WE 20040414001012004041400101NM 2004 4 14 CALA0400339 120040405A21216067723 FAN BOEING757 757224 1384958NM E/E BAY FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2719130 28970 THE FLIGHT CREW SMELLED A BURNING ODOR IN THE CABIN WHILE ON DESCENT INTO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT RECIRCULATION FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED IAW MM 21-25-01. 2L72 4F RTA2NM 20040414001022004041400102NM 2004 4 14 CALA0400340 120040407A53206552878U124 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 4 INCH CRACK IN ZEE ANGLE AT L-2 DOOR JAMB, STA 949. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040414001032004041400103NM 2004 4 14 CALA0400341 120040407A532065528781 WEB BOEING737 7373T0 1384582NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND WEB CORRODED AT FLOOR, STA 947 STRINGER 17L. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040414001042004041400104NM 2004 4 14 04FDEA00908 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040414001052004041400105NM 2004 4 14 CALA0400342 120040408A53206545805 ATTACH ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 1 INCH CRACK IN FORWARD ANGLE THAT ATTACHES TO FRAME AND SKIN AT STA 277 BETWEEN S15L AND S16L. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-00-07. 2L72 4F RTA16WE 20040414001072004041400107NM 2004 4 14 04FDEA00883 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE INNER & OUTER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414001102004041400110NM 2004 4 14 SWAA040920 120040329A3350610478 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29623SW 27933 DURING SCHEDULED A2 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT SIGN AND BOTH RT AND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AT MID CABIN LT SIDE. 2L72 4F RTA16WE 20040414001152004041400115NM 2004 4 14 SWAA040925 120040329A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 951, STRINGER 11R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040414001162004041400116NM 2004 4 14 SWAA040926 120040329A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS COVERS AT ROW 1 RT AND ROW 10 LT, BROKEN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040414001172004041400117 2004 4 14 SWAA040927 420040329A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040414001192004041400119WP 2004 4 14 04FDEA00821 120040402A5744ARC10451 BRACKET DOUG MD10 MD1010F 3022112WP LT O/B AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-75129 WINGS - OUTBOARD AILERON, BACKUP ACTUATOR BRACKET HOLE REWORK. COMPLIED WITH ENT BY: 484466 RPT BY: 484466. 2L73 4F RTA22WE 20040414001202004041400120NM 2004 4 14 04FDEA00822 120040403A5753 FLAP TRACK BOEING727 727200 138407ENM TE FLAPS BROKEN A FDEAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO25211FE 22933 OUTBOARD FLAPS STAYED AT 2 DEG WHEN FLAP HANDLE PUT TO 5 DEG. RAN QRH. LANDED UNEVENTFULLY. DECLARED AN EMERGENCY. IN WORK. RAN FLAPS TO 25 DEG. UPON VISUAL INSPECTION FOUND RIGHT OUTBD FOREFLAP BROKEN OFF OF FLAP TRACKS. EVALUATING DAMAGE AND PARTS AT THIS TIME. REMOVED AND REPLACED RIGHT O/B MIDFLAP AND I/B MIDFLAP TRACK, REMOVED AND REPLACED FOREFLAP. 2L73 4F RTA3WE 20040414001232004041400123WP 2004 4 14 04FDEA00825 120040403A5753ARB00292 BRACE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-75132 WINGS - RIGHT OUTBD FLAP - SIDE BRACE SUPPORT FITTING CORROSION REPAIR P/N ARB0 029-2. COMPLIED WITH EA 8-5740-75132 WINGS - RIGHT OUTBOARD FLAPS IDE BRACE SUPPORT CORROSION REPAIR P/N ARB0029-2. 2L73 4F RTA22WE 20040414001242004041400124NM 2004 4 14 SWAA040945 120040331A2701BACB10A325 BEARING BOEING737 7372T4 1384492NM CONTROL WHEEL BINDING A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29722WN 22698 AILERON CONTROL SLOPPY. LARGE DEAD BAND IN AILERONS. REMOVED AND REPLACED CAPT'S AILERON CONTROL WHEEL DRUM BEARINGS AND CAPT'S CONTROL COLUMN BEARINGS PER MM. 2L72 4F A16WE 20040414001272004041400127NM 2004 4 14 SWAA040948 120040331A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 744, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040414001282004041400128NM 2004 4 14 SWAA040949 120040331A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BS 500A, STRINGER 4R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040414001322004041400132 2004 4 14 SWAA040953 420040331A25656949956 CABLE BOEING737 7373H4 1384600NM L2/R2 DOORS MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C1 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES PER MM. 2L72 4F RTA16WE 20040414001332004041400133 2004 4 14 SWAA040954 420040331A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040414001342004041400134NM 2004 4 14 SWAA040955 120040331A335090083 BATTERY BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED RON, FOUND LT CENTER AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040414001352004041400135EU 2004 4 14 MALA040316 120040404A5210SOL2181BA LENS BAC 146 AVRO146RJ85A1500097EU PAX DOOR OBSTRUCTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 FWD PAX DOOR 1L FISH EYE LENS APPEARS TO BE OBSTRUCTED BY DEBRIS. INSTALLED NEW VIEWER INTO 1L, LEFT HAND PAX DOOR P/N SOL2181BA, OPS CHECK GOOD. ALL CHECKS GOOD. 2H74 4F RTA49EU 20040414001362004041400136NM 2004 4 14 SWAA040929 120040329A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT STRINGER 10R, BS 663, STRINGER 7R, BS 597, STRINGER 5R, BS 616, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040414001392004041400139 2004 4 14 SWAA040934 420040330A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE. 2L72 4F A16WE 20040414001412004041400141NM 2004 4 14 UPS04242079 120040331A3350 LAMP BOEING727 727185C 138406NNM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT HAS 1 LAMP INOP. RELAMPED AS REQUIRED, OPS CHECKS GOOD IAW M/M 33-50-01. 2L73 4F A3WE 20040414001432004041400143NM 2004 4 14 UPS04M42081 120040211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 36 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED AT HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.124 INCH. BARREL NUT HOLE REPAIR PER EN1031-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. 2L73 4F RTA22WE 20040414001442004041400144NM 2004 4 14 UPS04M42082 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 22 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM SURFACE, MATERIAL REMOVED 0.063 INCH. BARREL NUT HOLE REPAIRED PER EN1040-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414001452004041400145NM 2004 4 14 UPS04M42083 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HOZIZONTAL STABILIZER LEFT NR 26 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM, SURFACE MATERIAL REMOVED 0.071 INCH. BARREL NUT HOLE REPAIR PER EN 1029-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414001462004041400146EU 2004 4 14 UPS04142054 120040316A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY EXIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01142UP 0825 EMERGENCY EXIT LIGHT STAYS ON. ON GROUND WITH POWER REPEAT. INSTALLED M277614 C/W OPERATIONAL CHECKS PER TPCR PROCEDURES 3-33-MM-04-0360 MM 33-51-00-5 PAR F. CORRECTED PROCEDURES, RESULTS OPS CHECK GOOD. 2L72 4F RTA35EU 20040414001472004041400147EU 2004 4 14 UPS04142055 120040319A3320 LIGHT AIRBUSA300 A300F4622R 3930360EU LAVATORY INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01142UP 0825 LAV EMERGENCY LIGHT INOP. RELAMPED, WORKED OKAY. 2L72 4F RTA35EU 20040414001482004041400148NM 2004 4 14 UPS04242057 120040305A7120 MOUNT BOEING727 72730C 1384009NM NR 3 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B. 2L73 4F A3WE 20040414001492004041400149NM 2004 4 14 UPS04242058 120040311A5313 STRINGER BOEING727 72730C 1384009NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3. 2L73 4F A3WE 20040414001502004041400150NM 2004 4 14 UPS04242059 120040305A7120 MOUNT BOEING727 72730C 1384009NM NR 1 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A. 2L73 4F A3WE 20040414001512004041400151NM 2004 4 14 UPS04242060 120040309A5347 CARGO TRACK BOEING727 72730C 1384009NM CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8. 2L73 4F A3WE 20040414001522004041400152NM 2004 4 14 UPS04442053 120040311A5320 INTERCOSTAL BOEING747 747SR46 1384816NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, BELOW FLOOR INTERCOSTAL WEB CRACKED AT BS 2220 S-37R AS MARKED. BS 2220 S-37R BELOW FLOOR INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040414001532004041400153NM 2004 4 14 SWAA040936 120040330A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAMES AT BS 188, STRINGERS 17R AND 17L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040414001542004041400154NM 2004 4 14 SWAA040937 120040330A53116554892 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 336, BETWEEN STRINGERS 20L AND 21L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040414001552004041400155NM 2004 4 14 SWAA040938 120040330A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 639, STRINGER 15R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040414001562004041400156NM 2004 4 14 SWAA040939 120040330A53106547973 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 639, RBL 68, CRACKED. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20040414001572004041400157NM 2004 4 14 SWAA040941 120040330A55146547450 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB RT AND LT, AFT SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED HORIZONTAL STAB AFT SPAR CLEVIS PER ER. 2L72 4F RTA16WE 20040414001592004041400159NM 2004 4 14 SWAA040943 120040330A57536546430100 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E FOREFLAP PER MM. 2L72 4F RTA16WE 20040414001602004041400160NM 2004 4 14 SWAA040944 120040330A53146546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND SHEAR TIES AT RT KEEL BEAM BS 727E INBOARD, BS 727E OUTBOARD, BS 767 OUTBOARD, CRACKED. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040414001612004041400161NM 2004 4 14 SWAA040956 120040331A3350311498 REFLECTOR BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED PM CHECK, FOUND RT EXTERIOR EMERCENCY EXIT LIGHT INOP AFT OF WING TO BODY FAIRING. REMOVED AND REPLACED REFLECTOR PER MM. 2L72 4F RTA16WE 20040414001622004041400162NM 2004 4 14 SWAA040957 120040401A53306545767 SKIN BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 480, BETWEEN STRINGERS 27L AND 28L, BULGED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040414001632004041400163NM 2004 4 14 SWAA040958 120040401A33506556633 LIGHT BOEING737 7372H4 138448CNM LT OVERWING LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 CENTER EMERGENCY EXIT OVERWING LIGHT LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20040414001642004041400164NM 2004 4 14 SWAA040959 120040401A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 EMERGENCY EXIT NOT ARMED LENS FELL OUT. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20040414001652004041400165NM 2004 4 14 SWAA040960 120040401A55106551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION LT HINGE FITTING ON BOTH FACES CORRODED. REPAIRED FITTING PER ER. 2L72 4F RTA16WE 20040414001662004041400166NM 2004 4 14 SWAA040961 120040401A55306546872 FITTING BOEING737 7373H4 1384600NM VERTICAL FIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT LUG AFT FACE AND BORE CORRODED. REPAIRED VERTICAL FIN LUG PER ER. 2L72 4F RTA16WE 20040414001672004041400167NM 2004 4 14 SWAA040962 120040401A5321 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT FLOOR WEB AT BS 188 TO BS 196, STRINGERS 17 L AND 17R. REMOVED AND REPLACED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040414001682004041400168NM 2004 4 14 SWAA040963 120040401A53206516300 BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB AT BS 178, LBL 17.1, WL 182, CRACKED. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20040414001702004041400170NM 2004 4 14 SWAA040966 120040401A5312BAC1514 STIFFENER BOEING737 7373Q8 1384670NM BULKHEAD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND BS 1016, STIFFENER AT DRAIN HOLE CORRODED. REPAIRED STIFFENER PER EA. 2L72 4F RTA16WE 20040414001712004041400171NM 2004 4 14 SWAA040967 120040401A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 2, STRINGER 15R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040414001722004041400172WP 2004 4 14 UPS04842109 120040401A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT PNEUMATIC DUCT SUPPORT AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040414001742004041400174WP 2004 4 14 UPS04842111 120040331A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RT WING LEADING EDGE UPPER RIB IS CRACKED AT XFS 803.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040414001762004041400176NM 2004 4 14 SWAA040968 120040401A575465C26602223 SKIN BOEING737 7375H4 138449DNM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 2 LEADING EDGE SLAT DELAMINATED. REMOVED AND REPLACED LT WING NR 2 LEADING EDGE SLAT PER MM. 2L72 4F RTA16WE 20040414001782004041400178EU 2004 4 14 MALA040310 120040324A3234 CONTROL HANDLE SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAK NONE J WARNING INDICATION APAPPROACH 1 GL15443XJ 340B443 DURING APPROACH INTO ABN EXTENDED GEAR, LF MAIN DID NOT ILLUMINATE. UNSAFE LIGHT NOT ON, TEST ALL LIGHTS WORKED FINE, FOURTH CYCLE ALL GREEN. INSPECTED ALL ACCESSIBLE WIRING AND CANNON PLUGS FOR LEFT GEAR DOWN INDICATION. CLEANED CANNON PLUGS AND OPS CHECKED GEAR BY DOING MULTIPLE SWINGS. FOUND LEFT GREEN INDICATOR MALFUNCTIONING. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE WITH SERVICEABLE IAW SF 340 MM CHAP 32. 2L72 4T RTA52EU 20040414001792004041400179EU 2004 4 14 MALA040311 120040328A5710 STRUCTURE SAAB SF340 340B 7860101EU LT WING BIRD STRIKE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15456XJ 340B456 BIRD STRIKE LEFT INBOARD WING. REPLACED LEFT I/B LEADING EDGE ASSY P/N 7257500-787, S/N OFF NSN, S/N ON 206069 PER AMM 57-20-05-4, OPS AND LEAK CHECK GOOD. 2L72 4T RTA52EU 20040414001802004041400180EU 2004 4 14 MALA040312 120040329A2611 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU CARGO SMOKE ILLUMINATED A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15502XJ E2307 CARGO SMOKE LOOK UP LIGHT ILLUMINATED ON TAKEOFF PRIOR TO V1, ABORTED TAKEOFF. CARGO SMOKE LIGHT EXTINGUISHED DURING ABORT & REMAINED EXTINGUISHED. ABORT WAS NOT A HIGH ENERGY ABORT. INSPECTED FWD/AFT X SMOKE DETECTORS, ASSORTED CONNECTORS, OPS CHECKS. AFT/AFT CX SMOKE DETECTORS NO DEFECTS. VISUAL INSP BRACKET EAR PIN INDICATORS FUSEABLE PLUGS. 2H74 4F RTA49EU 20040414001812004041400181EU 2004 4 14 MALA040317 120040404A2611 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15442XJ 340B442 AVIONICS SMOKE DETECT LIGHT ILLUMINATED. MX REPLACED SMOKE DETECTOR. 2L72 4T RTA52EU 20040414001822004041400182EU 2004 4 14 MALA040313 120040401A564050L2181BA SIGHT GLASS BAC 146 AVRO146RJ85A1500097EU SERVICE DOOR CONTAMINATED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15532XJ E2366 RIGHT FORWARD SERVICE DOOR EMERGENCY EXIT SIGHT GLASS HAS CONDENSATION. REMOVED AND REPLACED EYE PIECE, P/N OFF AND ON 50L2181BA. 2H74 4F RTA49EU 20040414001832004041400183EU 2004 4 14 MALA040314 120040402A5220 COVER SAAB SF340 340B 7860101EU EMERGENCY EXIT DISLODGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15424XJ 340B424 FWD EMERGENCY EXIT COVER FOUND LAYING ON SEAT. MX RESAFTIED COVER SECURELY. 2L72 4T RTA52EU 20040414001842004041400184EU 2004 4 14 MALA040315 120040404A2560 COVER SAAB SF340 340B 7860101EU PBE DISLODGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15444XJ 340B444 AFT PBE COVER HAS BEEN REMOVED. REPLACED PBE P/N 119003-11, ALL GOOD AT THIS TIME. 2L72 4T RTA52EU 20040414001852004041400185NM 2004 4 14 CALA0400343 120040408A53136545800 STRINGER BOEING737 7373T0 1384582NM E/E BAY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND STRINGER 28L CORRODED AT STA 364, LBL 8 IN THE E&E COMPARTMENT. REPAIRED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040414001862004041400186NM 2004 4 14 CALA0400344 120040408A53106545805226 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 5 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN S15L AND S16L. A DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 207. 2L72 4F RTA16WE 20040414001872004041400187NM 2004 4 14 CALA0400345 120040408A5510180A16121 PIN BOEING737 737824 13844BZNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER AFT PIN CORRODED. REMOVED AND REPLACED PIN IAW EA 5510-01696. 2L72 4F RTA16WE 20040414001882004041400188NM 2004 4 14 CALA0400346 120040408A5510180A16121 PIN BOEING737 737824 13844BZNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT ATTACHMENT UPPER PIN CORRODED. REMOVED AND REPLACED PIN IAW EA 5510-01696. 2L72 4F RTA16WE 20040414001892004041400189NM 2004 4 14 CALA0400347 120040408A5510180A16122 PIN BOEING737 737824 13844BZNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND LEFT HORIZONTAL STABILIZER ATTACHMENT AFT PIN AND MIDDLE PIN CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040414001902004041400190NM 2004 4 14 CALA0400348 120040408A5510180A16122 PIN BOEING737 737824 13844BZNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER AFT ATTACHMENT MID PIN AND LOWER PIN CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040414001912004041400191NM 2004 4 14 CALA0400349 120040408A534265495598 FITTING BOEING737 7373T0 1384582NM VERTICAL STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND VERTICAL STABILIZER O/B AFT FUSELAGE FITTING CORRODED AT AFT BOTTOM SIDE OF HOLE CUTOUT, RIGHT AFT CLEVIS, STA 1088. REPAIRED IAW ECRA 5342-01021. 2L72 4F RTA16WE 20040414001922004041400192NM 2004 4 14 CALA0400350 120040408A53106545805226 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 3 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN S16L AND S17L. A NEW SHEAR TIE SECTION WAS INSTALLED IAW SRM 53-00-07, FIGURE 207. 2L72 4F RTA16WE 20040414001932004041400193NM 2004 4 14 AWXA200400329 120040324A574365C309314 SLEEVE BOEING737 7373G7 1384595NM MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK PITTING CORROSION WAS FOUND INSIDE RIGHT MAIN LANDING GEAR FORWARD TRUNNION SLEEVE INNER BORE AROUND ENTIRE CIRCUMFERENCE. MAINTENANCE REMOVED CORRODED RIGHT MAIN LANDING GEAR FORWARD TRUNNION SLEEVE; FABRICATED A NEW REPLACEMENT SLEEVE PER DWG 65-50768; INSTALLED REPAIR PART IAW DWG 65-50768, SHEET 4. 2L72 4F RTA16WE 20040414001942004041400194EU 2004 4 14 AWXA200400330 120040330A2932NAS16128 PACKING AIRBUS320 A320231 3930325EU HYD SYSTEM BURST A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28627AW 66 PHL - EMERGENCY LANDING - FLT 0256 - EN ROUTE FROM PHX TO PHL AT CRUISE RECEIVED CLASS 1 MESSAGE FOR GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL, MANUALLY EXTENDED LANDING GEAR AND DECLARED AN EMERGENCY. MAINTENANCE FOUND HYDRAULIC LEAK IN LEFT WHEEL WELL WHERE PRESSURE SWITCH (10CE1) IS INSTALLED IN MANIFOLD. REMOVED AND REPLACED O-RING PACKINGS ON FLIGHT CONTROL PRESSURE SWITCH (10CE1), LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA28NM 20040414001952004041400195NM 2004 4 14 04FDEA00695 120040323A5312AEA76211 WEB DOUG MD11 MD11 3023602NM ZONE 700 CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT VERTICAL WEBS IN CENTER LANDING GEAR WHEEL WELL FOUND OIL CANNING AT: (1) Y= 1391 TO Y= 1401, Z= -100 TO Z= -90, DEPTH= 0.074 INCH (2) Y= 1401 TO Y= 1411, Z= -100 TO Z= -90, DEPTH= 0.061 INCH (3) Y= 1411 TO Y= 1421, Z= -100 TO Z= -90, DEPTH= 0.069 INCH (4) Y= 1421 TO Y= 1431, Z= -90 TO Z= -70, DEPTH= 0.070 INCH. COMPLIED WITH FEDEX WITH EA 1-5310-75984, FUSELAGE - MAINFRAME - KEEL WEB / CENTER LANDING GEAR INSPECTION REQUIREMENTS. 2L73 4F RTA22WE 20040414001962004041400196NM 2004 4 14 04FDEA00753 120040325A5311AFA0027 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1661 BETWEEN LONGERONS 12R AND 13R. MID CABIN FRAME AT STA Y= 1661 BETWEEN STR 12R AND 13R DENT REPAIRED PER SRM 53-30-00 VOL I FIG 1. COMPLIED WITH FEDEX EA 1-5310-75999, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2L73 4F RTA22WE 20040414001972004041400197NM 2004 4 14 CALA0400322 120040405A5510180A16122 PIN BOEING737 737824 13844BZNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718220 28929 INSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER PIN CORRODED. A NEW PIN WAS INSTALLED IAW EA 5510-01696, REV C. 2L72 4F RTA16WE 20040414001982004041400198NM 2004 4 14 AWXA200400331 120040331A3350BR964411 LIGHT BOEING737 73733A 1384673NM SEAT ROW 22 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040412000702004041200070NE 2004 4 12 AWXA200400342 220040402A72614A7118 SCAVENGE PUMP AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE LEAKING A AWXAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 WP28801AW19870 889 BUR - TAILPIPE FIRE - FLT 0476 - NR 1 ENGINE HAD TAILPIPE FIRE AT ENGINE SHUTDOWN AFTER 5 MIN COOL DOWN. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL SCAVENGE PUMP IAW T/C R5M79301. RAN ENGINE AT IDLE, NO TAILPIPE FIRE AT SHUTDOWN, LEAK CHECK OF PUMP WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20040412000722004041200072NM 2004 4 12 AWXA200400344 120040402A291069547678 HYDRAULIC LINE BOEING737 737277 1384570NM LT MLG WW RUPTURED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28182AW 22649 SAT - AIR TURNBACK - FLT 0679 - ON CLIMBOUT OF SAT EN ROUTE FOR PHX LOST A-HYDRAULIC SYSTEM, FOLLOWED QRH AND TURNED BACK TO SAT. MAINTENANCE REMOVED AND REPLACED RUPTURED HYDRAULIC PRESSURE LINE BETWEEN A-SYSTEM MODULE AND LT MAIN LANDING GEAR ACTUATOR. REMOVED AND REPLACED NR 1 & 2 ENGINE A-SYSTEM HYDRAULIC PUMPS AND FILTERS DUE TO POSSIBLE PUMP CAVITATIONS FROM FLUID LOSS. ENGINE RUN OPERATIONAL & LEAK CHECKS WERE GOOD. 2L72 4F RTA16WE 20040412000782004041200078EU 2004 4 12 AWXA200400350 120040329A5321D53670022002 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND A 1 INCH CRACK IN CABIN FLOOR PANEL 251AF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 251AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10D5367022; INSTALLED NEW PANEL IAW A320 SRM 53-02-00 FIG 209 PG 233-236. 2L72 4F RTA28NM 20040412000932004041200093EU 2004 4 12 AWXA200400359 120040328A5320D5348002034300 WEB AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR WEB (TRAY) ON AFT SIDE OF L-2 DOOR WAY, OUTBOARD OF Y1732, BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CRACKED SHEAR WEB AFT OF L-2 DOORWAY Y1732, BETWEEN FR 68 AND FR 69; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20040412001192004041200119NM 2004 4 12 CALA0400258 120040320A5753113A37008 FLAP BOEING737 737824 13844BZNM RT WING DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW271824314323 28806 INSPECTION FOUND RIGHT WING O/B AFT FLAP I/B CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-22. 2L72 4F RTA16WE 20040412001222004041200122NM 2004 4 12 CALA0400261 120040321A575165C2592930 PANEL BOEING737 737524 1384721NM LT AILERON BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2715659 28920 INSPECTION FOUND LEFT AILERON PANEL 8106L BROKEN AT CENTER OF PANEL. REPAIRED IAW SRM 51-70-05. 2L72 4F RTA16WE 20040412001242004041200124NM 2004 4 12 CALA0400263 120040321A5510180A16111 PIN BOEING737 737724 13844BYNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727734 28949 INSPECTION FOUND LEFT UPPER HORIZONTAL STABILIZER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040412001282004041200128EU 2004 4 12 MALA040298 120040326A33506122751 BATTERY BAC 146 AVRO146RJ85A1500097EU CABIN FAULTY A MALAK NONE O OTHER ININSP/MAINT 1 GL15527XJ E2352 BATTERY UNIT WAS REMOVED FOR SCHEDULED BENCH CHECK, IN HOUSE WO 365157, BATTERY FAIL CAPACITY CHECK, BATTERY PACK P/N 61-2275-1, S/N 9710075 FOR EMERGENCY LIGHT EVAC SYSTEM. PROBLEM WAS FOUND OFF AIRCRAFT IN SHOP ENVIRONMENT, A/C WAS NOT GROUNDED. BATTERY ASSEMBLY P/N 61-2275-1 WAS REPLACED, UNIT PASSED GMM TESTS AND WAS RETURNED TO SERVICE ON 3/30/04. 2H74 4F RTA49EU 20040412001302004041200130NM 2004 4 12 2004UALA00274 120040324A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 STRINGER SPLICE AT STATION 907 STR 4R CRACKED. MAJOR REPAIR ACCOMPLISHED. NEW STRINGER SPLICE INSTALLED. 2L72 4F4 FRTA16WE E2GL 20040412001332004041200133NM 2004 4 12 2004UALA00280 120040324A3350582233 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29643UA 25093 EMERGENCY EXIT LIGHTS INTERMITTENT ROWS 15-18 LEFT SIDE. REPLACED EEL BATTERY POWER SUPPLY PACK. 2L72 4F4 FRTA1NM E24NE 20040412001352004041200135NM 2004 4 12 2004UALA00282 120040325A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 BEAR STRAP AT AFT SIDE OF AFT CARGO DOOR CUTOUT REQUIRED REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040412001382004041200138EU 2004 4 12 AWXA200400333 120040401A2560P20700012015 FLASHLIGHT AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST NRNOT REPORTED 1 WP28646AW 271 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT OUTBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040412001422004041200142NM 2004 4 12 AWXA200400337 120040303A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 639, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 639, STR 4 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-46540; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2 & 8. 2L72 4F RTA16WE 20040412001512004041200151NM 2004 4 12 AWXA200400296 120040320A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28160AW 23782 DEN - EEL - DURING A-1 CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 4 AND 7 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT SEAT ROWS 4 AND 7, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040412001532004041200153NM 2004 4 12 AWXA200400310 120040325A7722WL202EED6 INDICATOR BOEING737 7373B7 1384580NM COCKPIT FAULTY A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28332AW4189716857 23384 ON T/O ROLL 80 KTS NR 1 ENG EGT EXCEEDED 1100 DEG, REDUCED THRUST & EGT DROPPED TO 800DEG, AGAIN EGT SPIKED TO 1000 DEG, REJECTED T/O. TIME ABOVE MAX ON FIRST SPIKE WAS 2 SECONDS. MX INSPECTED EGT HARNESSES NR 1 ENG & EGT DISCONNECT D1208 FIREWALL, NO DEFECTS NOTED. OHMED HARNESS TB1012 TO FLT DECK IND, NO DEFECTS NOTED, OHMED HARNESS CONNECTOR BETWEEN EGT PROBES & TB1012 & RESISTANCE IND10.5 OHMS, SHOULD READ 2.5 OHMS. REPLACED HARNESS CONNECTOR BETWEEN EGT PROBES & TB1012, REPLACED NR 1 ENG EGT INDICATOR. PERFORMED EGT ACCURACY TEST NR 1 EGT, INDICATION WITHIN ACCURACY LIMITS. RAN ENG, ALL NORMAL AT ALL POWER SETTINGS. PART NAME; HARNESS, MFG; AUXITROL, P/N; CA130-00, POS; ENG 1. 2L72 4F RTA16WE 20040412001562004041200156NM 2004 4 12 AWXA200400327 120040303A53156545815 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 344, LBL 11, WL 208. MAINTENANCE CUT OUT DAMAGE ON UPPER SURFACE OF FLOORBEAM AT BS 344, LBL 11; FABRICATED A FILLER AND 2 REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205, SHEETS 1-5. 2L72 4F RTA16WE 20040412001912004041200191WP 2004 4 12 ASAA0480113 120040229A5320993053815 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CUSP WEB IS CORRODED AT FS 256. REMOVED DAMAGED SECTION. INSTALLED DOUBLER PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040413000332004041300033NM 2004 4 13 CALA0400354 120040410A5313BAC1498117 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND STRINGER 25L CORRODED IN E & E COMPARTMENT AT STA 351, LBL 32. A REPAIR WAS INSTALLED IAW SRM 53-00-03, DETAIL 7. 2L72 4F RTA16WE 20040414000062004041400006NM 2004 4 14 04FDEA00830 120040404A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 CENTER CARGO COMPARTMENT CRACKED ON LONGERON SPLICE 51L, STA 5- 123. CRACKED LONGERON SPLICE REMOVED AND REPLACED PER SRM 51-33- 01 VOL II 2L73 4F RTA22WE 20040414000092004041400009NM 2004 4 14 04FDEA00832 120040404A5730 PANEL DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH BULGE. COMPLIED WITH FEDEX EA 1-5710-76644. LEFT AND RIGHT HAND WING - AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000202004041400020NM 2004 4 14 04FDEA00839 120040406A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD LOWER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040414000242004041400024WP 2004 4 14 04FDEA00846 120040407A5753ARC0538 CLEVIS DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5750-75133 WINGS - RT OUTBOARD FLAP, OUTBOARD HINGE, REWORK OF FWD CLEVIS ARC0538. COMPLIED WITH EA 8-5750-75123 WINGS RIGHT OUTBOARD FLAP OUTBOARD HINGE REWORK OF FWD CLEVIS. 2L73 4F RTA22WE 20040414000262004041400026NM 2004 4 14 UPS04442098 120040330A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE SCRATCHED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C COCKPIT - BS 340-360 LEFT STR 2 AFT END AREA FOUND SCRATCH MARK. COCKPIT - BS 340-360 LEFT STR 2 STRINGER REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20040414000292004041400029NM 2004 4 14 UPS04M42089 120040214A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.044 INCH. BARREL NUT HOLE REPAIRED PER EN1043-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000352004041400035NM 2004 4 14 UPS04M42085 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 26 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM SURFACE AREA MATERIAL REMOVED 0.105 INCH. BARREL NUT HOLE REPAIRED PER EN1017-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000422004041400042NM 2004 4 14 04FDEA00853 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000432004041400043NM 2004 4 14 04FDEA00854 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE O/B ACTUATOR HOLE FOUND WITH CORROSION. CORROSION REMOVED AND REPAIRED. 2L73 4F RTA22WE 20040414000512004041400051NM 2004 4 14 04FDEA00857 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000562004041400056NM 2004 4 14 04FDEA00834 120040404A5210 SKIN DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FUSELAGE PAX DOOR 3 OFF CRACK ON INTERNAL PRIMARY DOUBLER OF LOWER FWD CORNER APPROXIMATELY .1875 INCH. CLEANED UP IAW SRM 53-00-01 FIG 1A VOL I. AND CARRIED OUT AS PER DAC NDT SPM PART 06-10-01-001 REV 11 AND FOUND NO CRACK EVIDENT. 2L73 4F RTA22WE 20040414000712004041400071WP 2004 4 14 04FDEA00890 120040409A5753NSC6053501 SUPPORT DOUG MD10 MD1010F 3022112WP LT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-77338 WINGS - OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM ARC2177. COMPLIED WITH EA 8-5740-77338 WINGS - OUTBOARD FLAP, REWORK OF CARRIAGE SUPPORT ARM ARC 2177 AT MAE. 2L73 4F RTA22WE 20040414000722004041400072EU 2004 4 14 04FDEA00899 120040411A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 SECOND SEAT TRACK FROM CENTER LEFT BETWEEN FRAMES F77 & F78, 2 EA AREAS OF CORROSION UPPER SURFACE, MAIN CARGO COMPT. REMOVED CORROSION IAW A300-600 SRM 51-74-10. REMOVAL OF CORROSION WAS VISUALLY OUT OF LIMITS IAW A300-600 SRM 51-74-10. LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20040414000762004041400076NM 2004 4 14 04FDEA00841 120040406A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040414000802004041400080NM 2004 4 14 04FDEA00870 120040408A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648. 2L73 4F RTA22WE 20040414000822004041400082NM 2004 4 14 04FDEA00872 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651. TRAILING EDGE FLAPS LT & RT INBOARD FLAP OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040414000902004041400090WP 2004 4 14 04FDEA00887 120040409A5753ARC0502501 BRACKET DOUG MD10 MD1010F 3022112WP LT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-77341 WINGS - LEFT OUTBOARD FLAP - FLAP INBOARD HINGE CORROSION REPAIR (P/N ARC0502-501). COMPLIED WITH EA 8-5740-77341 WINGS - LEFT OUTBOARD FLAP - FLAP INBOARD HINGE CORROSION REPAIR (P/N ARC0502-501) AT MAE. 2L73 4F RTA22WE 20040414000912004041400091NM 2004 4 14 04FDEA00903 120040412A5313 STRINGER DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT STA 1782 RIGHT STR 46 FOUND CRACKED. REPAIR ON LONGERON 46R BY BETWEEN STATION 1781 AND 1787. 2L73 4F RTA22WE 20040414001092004041400109NM 2004 4 14 04FDEA00885 120040408A243223013 CHARGER BOEING727 727200 138407ENM E & E BAY OVERHEATED A FDEAH DEACTIVATE SYST/CIRCUITS MSPOVER TEMP AFFECT SYSTEMS NO WARNING INDICATION NRNOT REPORTED 1 SO25236FE 21330 THE BATTERY CHARGER STARTED TO SMOKE AND THE BATTERY GOT VERY HOT 170 DEGREES. THE AIRCRAFT WAS IN THE HANGAR HAVING AN ALL LANDING GEAR CHANGE AND ON JACKS. 2L73 4F RTA3WE 20040414001132004041400113NM 2004 4 14 SWAA040923 120040329A53206545409 WEB BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND MLG UPPER DECK BEADED WEB AT BS 665 TO BS 673, LBL 30 TO LBL 35, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040414001142004041400114NM 2004 4 14 SWAA040924 120040329A57436552235 FITTING BOEING737 7373H4 1384600NM RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND RT MLG OUTBOARD STABILIZER FITTING CORRODED. REMOVED AND REPLACED RT MLG FITTING PER SRM. 2L72 4F RTA16WE 20040414001182004041400118NM 2004 4 14 SWAA040928 120040329A531365C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT STRINGER 11L, BS 706, BS 291.5, STRINGER 8L, BS 616, BS 578, STRINGER 7L, BS 597, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040414001222004041400122WP 2004 4 14 04FDEA00824 120040403A5753ARC1984 HINGE DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5750-75130 WINGS - LEFT OUTBOAD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-75130 - WINGS - LEFT OUTBOARD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR P/N ARC 1984. 2L73 4F RTA22WE 20040414001252004041400125NM 2004 4 14 SWAA040946 120040331A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29327SW 23691 DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040414001382004041400138NM 2004 4 14 SWAA040933 120040330A3350PH22300L LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 EEPLS STRIP LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20040414001402004041400140NM 2004 4 14 SWAA040935 120040330A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 597, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040414001422004041400142NM 2004 4 14 UPS04M42080 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 23 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED AT HOLE BOTTOM SURFACE, MATERIAL REMOVED 0.064 INCH PER SRM 51-21-01 VOL 2 REV 34. CARRY OUT BARREL NUT HOLE REPAIR PER EN1023-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409- D. 2L73 4F RTA22WE 20040414001772004041400177NM 2004 4 14 SWAA040969 120040401A57536546435282 SKIN BOEING737 7375H4 138449DNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20040414001992004041400199EU 2004 4 14 AWXA200400332 120040331A3243C245920001 MASTER CYLINDER AIRBUS320 A320231 3930325EU ZONE 122 OUT OF TOLERANCEA AWXAK NONE P NO WARNING INDICATION NRNOT REPORTED 1 WP28626AW46763 65 PHX - BRAKES - FLT 0576 - FLIGHT CREW REPORTED EMERGENCY MANUAL BRAKE PRESSURE WAS 200 ON LEFT, 500 ON RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED RIGHT BRAKE CONTROL MASTER CYLINDER (2626GM) IAW AMM 32-43-12-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040414002002004041400200NM 2004 4 14 CALA0400323 120040405A5320654587512 ANGLE BOEING737 7373T0 1384582NM R-1 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND R-1 DOOR LOWER CENTER SILL PLATE MOUNT ANGLE CORRODED. THE MOUNT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040414002012004041400201WP 2004 4 14 04FDEA00891 120040409A5753ARC0502 HINGE DOUG MD10 MD1010F 3022112WP LT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5750-77339 WINGS - LEFT O/B, I/B FWD HINGE ASSY (P/N ARC 0502) FWD CLEVIS REWORK. COMPLIED WITH EA 8-5750-77339 WINGS - LEFT O/B FLAP, I/B FWD HINGE ASSY (P/N ARC0502) FWD CLEVIS REWORK. 2L73 4F RTA22WE 20040414002032004041400203NM 2004 4 14 04FDEA00893 120040411A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 AND REPAIRED AS PER EA 1-5750-76657 PART 1. INBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (FLAP SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414002042004041400204SO 2004 4 14 SWIA200413070 120040324A5310 WINDOW POST EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07213SW 120277 ANGLE BRACKET UNDER PILOT'S WINDOWSILL IS CRACKED (FRAME 10). (DISCOVERED DURING C-CHECK INSPECTION)REMOVED AND REPLACED ANGLE BRACKET UNDER PILOT'S WINDOW SILL IAW SRM 51-10-02, 51-40-00. SEE RII 53-301. 2L72 4T4 TRTA31SO E20NE 20040414002062004041400206NM 2004 4 14 04FDEA00237 120040128A5315BAC1518338 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 CORROSION ON FLOOR BEAM AT FLOOR PANEL FASTENER HOLE BS 440, LBL 7.75 - 10.75 (100 PERCENT MATERIAL LOSS). REMOVED DAMAGE AREA OF TOP FLANGE OF FLOORBEAM AT BS 440. FABRICATED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 53-10-8. 2L73 4F RTA3WE 20040414002072004041400207WP 2004 4 14 04FDEA00414 120040217A5320 SUPPORT DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 STRUCTURE DAMAGE TO FORWARD SHUTTLE LOAD BAR TRANSMISSION SUPPORT AND ATTACHING FLOORBEAM STRUCTURE AT FUS. STA 879. REPAIRED LOWER FLOOR BEAM STA.879 AS PER SRM53-60-01 FIGUARE 3 AND AND EA 8-5310- 71818.REF WORD CARD SEQ0005. 2L73 4F4 F A22WE E23EA 20040414002092004041400209NM 2004 4 14 QXEA200400142 120040212A2120 ODOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 DETECTED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09348PH 484 SULFER ODOR IN COCKPIT AFTER LANDING. GROUND RAN AIRCRAFT ENGINES 1 AND 2 WITH BLEED ON, PACKS ON. ALL COCKPIT AND EXTERIOR LIGHTS ON. DC AND AC SYSTEMS CHECK GOOD. INVERTERS CHECK GOOD. NO ODOR NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040415000012004041500001EA 2004 4 15 O3O2004F00000 220040109A8510 SHAFT PIPER PA32 PA32260 7103206SO LYC O540 O540E4B5 41532EA IDLER ASSY BROKEN B O3ORO OTHER O OTHER NRNOT REPORTED 1 AL034798S504 321183 L669940 DISMANTLED THIS ENGINE DUE TO FUEL CONTAMINATION, FOUND THE PROP GOVERNOR IDLER SHAFT BROKEN AT THE KEYWAY AREA. ALSO THE IDLER GEAR SHAFT BOSS IN THE CRANKCASE WAS BROKEN. 1L71 3O3 O A3SO E295 20040415000022004041500002NE 2004 4 15 AC2A094057 220040403A732023075496 HMU BELL 430 430 1182150SW ALLSN 250C 250C40B 03032NE NR 2 MALFUNCTIONED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CH4037 49037 844110 M/ECU 2 ADVISORY LIGHT ILLUMINATED ON SHUTDOWN. VFMVFLT FAULT WAS RECORDED FOR ECU 2. REPLACED HMU. 1G72 3U3 URTH9SW E1GL 20040415000032004041500003NE 2004 4 15 BAQA093987 220040225A73100319738340 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE FUEL SYSTEM UNKNOWN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH190 0131 30187 200HR TIME CHANGE DUE, C/W AD 01-08-14(B). FUEL MANIFOLD, REPLACED WITH SERVICABLE UNIT. 03/30/2004 1G72 3U3 U H88EU E34NE 20040415000042004041500004EU 2004 4 15 BAQA094010 120040325A3150B19030GB03 DISPLAY UROCOPEC135 EC135T1 5620026EU COCKPIT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME1444 0143 UPPER SCREEN HAS "DEAD SPOTS," STARTING TO FAIL. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U H88EU 20040415000052004041500005NE 2004 4 15 HEEA094027 120040313A2697MS3476L106S CONNECTOR SKRSKYS76 S76A 8143006NE NR 2 ENGINE CORRODED E HEEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0322342 760096 WHILE IN CRUISE FLIGHT NR 2 ENGINE FIRE LIGHT ILLUMINATED. FOLLOWED EMERGENCY CHECK LIST FOR ENGINE FIRE LIGHT. RETURNED TO BASE. INSPECTED FOR SIGNS OF FIRE AND OR SMOKE, NONE FOUND. FOUND DEFECTIVE (CORRODED) CONNECTOR. REPLACED CONNECTOR. 1G72 3U H1NE 20040415000062004041500006EU 2004 4 15 HEEA094028 120040307A5610MBK117241001 WINDOW BOLKMS117 BK117A1 5626010EU COCKPIT DEPARTED E HEEAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW03911TL 7198 DURING FLIGHT, COPILOT SLIDING GLASS WINDOW DEPARTED WINDOW. WINDOW CAUSED SUBSEQUENT DAMAGE TO HORIZONTAL STABLIZER AND WINGLET. 1G72 3U H13EU 20040415000072004041500007SW 2004 4 15 AC2A093680 120040306A6710430010122101 STUD BELL 430 430 1182150SW MAIN ROTOR CRACKED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CM 49090 STUD IS CRACKED WHERE THREADS ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY. 1G72 3U RTH9SW 20040415000122004041500012GL 2004 4 15 W1J2004F00000 320040206A6110 RETAINING RING GULSTM690TP 690B 7630516SW HARTZLHCB3T HCB3TN5 GL LT PROPELLER OUT OF POSITION B W1JRE ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 WP01690RP 266 11493 ON 2/6/04 A NORMAL ENGINE RUN AND TAXI WAS BEING PERFORMED. AS WE ATTEMPTED TO TAXI OUT THE LT SIDE SEEMED TO HAVE NO THRUST OR MOVEMENT. WE HEARD A LOUD THUMP OR POP ON THE LT SIDE OF THE AIRCRAFT. AT THAT TIME WE ABORTED THE TAXI AND SHUT DOWN BOTH ENGINES IN ORDER TO INVESTIGATE THE PROBLEM. THE LEFT ENGINE PROP WAS FOUND IN THE FULL REVERSE POSITION AFTER ENGINE STOPPED ROTATING. INVESTIGATION AND PROP REMOVAL REVEALED A PLUG RETAINING RING WAS NOT IN PROPER POSITION AND THE PLUG HAD BEEN DISLODGED BY THE FEATHER SPRING. THE PROP WAS SENT TO A PROPELLER REPAIR STATION AND THE RETAINING RING WAS BELIEVED TO BE THE INCORRECT PN. (WP01200406679) 1H72 3T 2A4 6 CP15EA 20040415000242004041500024NE 2004 4 15 HEEA093674 120040225A7997 WIRE SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE OIL TEMP BULB BROKEN E HEEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03760PH 760078 NR 2 ENGINE OIL TEMPERATURE STARTED FLUCTUATING. MAINTENANCE REPAIRED A BROKEN WIRE NEAR THE NR 2 ENGINE OIL TEMPERATURE BULB. 1G72 3U3 U H1NE E19EU 20040415000252004041500025NM 2004 4 15 QXEA200400180 120040225A3260 CONNECTOR DHAV DHC8 DHC8202 2809007NM LT WING NOT SEATED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09357PH 504 RDM - FLIGHT 2128 - THE LANDING GEAR INOP CAUTION MESSAGE APPEARED IN FLIGHT AND THE LEFT MAIN GEAR AMBER LIGHT ILLUMINATED. THE CREW VISUALLY CHECKED AND VERIFIED THAT THE DOORS WERE OPEN. THE CREW COMPLIED WITH THE LANDING GEAR INOP CAUTION LIGHT CHECKLIST AND USED THE MANUAL GEAR EXTENSION. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CONNECTOR IN THE LEFT WING ROOT NOT FULLY SEATED. THE CONNECTOR WAS THEN CLEANED AND RECONNECTED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000282004041500028NM 2004 4 15 04FDEA00696 120040323A5320AEA76212 WEB DOUG MD11 MD11 3023602NM ZONE 700 CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 RT VERTICAL WEBS IN CENTER LANDING GEAR WHEEL WELL FOUND OIL CANNING AT: (1) Y= 1390 TO Y= 1401, Z= -100 TO Z= -90, DEPTH= 0.0090 INCH (2) Y= 1401 TO Y= 1411, Z= -100 TO Z= -90, DEPTH= 0.0070 INCH (3) Y= 1411 TO Y= 1421, Z= -100 TO Z= -90, DEPTH= 0.0072 INCH (4) Y= 1421 TO Y= 1431, Z= -90 TO Z= -70, DEPTH= 0.0068 INCH (4) Y= 1421 TO Y= 1431, Z= -90 TO Z= -70, DEPTH= 0.0180 INCH. COMPLIED WITH FEDEX EA 1-5310-75984, FUSELAGE - MAINFRAME - KEEL WEB / CENTER LANDING GEAR INSPECTION REQUIREMENTS. 2L73 4F RTA22WE 20040415000292004041500029EA 2004 4 15 QXEA200400185 120040226A26119847101505 SCREEN CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX - FORWARD CARGO BAY FORWARD ANGLED CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20040415000302004041500030EA 2004 4 15 HNAA0400008 120040128A3234574205A SELECTOR VALVE DHAV DHC8 DHC8311 1386006EA MLG FAILED A HNAAO OTHER J WARNING INDICATION LDLANDING 1 EA07328EN3481134811 281 WHEN LANDING GEAR SELECTED DOWN, NOSE AND MAIN LANDING GEAR DID NOT EXTEND. ALL RED GEAR UNSAFE LIGHTS ILLUMINATED. WHEN ALTERNATE EXTENDED GEAR OPS NORMAL, GEAR DOWN LOCKED (GREEN) ILLUMINATED. MADE UNEVENTFUL LANDING. ADDITIONAL INFO IS TO FOLLOW. 2H72 4T RTA13NM 20040415000342004041500034NM 2004 4 15 04FDEA00817 120040401A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25285FE 22622 FUSELAGE SKIN IS CRACKED AND EXFOLIATED AT BS 1060, STR 30. COMPLIED WITH FED EX EA 7-533070651 ON THE CRACKED AND EXFOLIATED SKIN AT BS 1060 STR 30. 2L73 4F RTA3WE 20040415000362004041500036NM 2004 4 15 QXEA200400191 120040305A2610 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM NACELLE & MLG DIRTY A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09416QX 4083 PDX - MAINTENANCE FOUND THAT WHEN THE ADVISORY LIGHT TEST IS PERFORMED, THE FIRE WARNING BELL IS TRIGGERED. AFTER INSPECTING THE SYSTEM, CLEANED THE RIGHT AND LEFT NACELLE ENGINE AND MAIN LANDING GEAR PRIMARY ZONE ADVANCE PNEUMATIC DETECTOR CANNON PLUGS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040415000372004041500037 2004 4 15 249TR0021 420040104A2210 BATTERY BOEING737 7372K5 138448XNM FLT DIRECTOR FAILED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 HEADING, IAS, COURSE BUGS WILL NOT CHANGE. A/P FLIGHT DIRECTOR SYSTEM TEST PERFORMED IAW MM 22-11-01. REPLACED BATTERY IAW MM 24-31-11. TEST OK. 2L72 4F RTA16WE 20040415000382004041500038NM 2004 4 15 QXEA200400194 120040304A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09405QX 4047 BOI - FLIGHT 2398 - DURING DESCENT, THE FLIGHT ATTENDANT REPORTED THE SMELL OF FUEL. MAINTENANCE INSPECTED THE NR 1 AND NR 2 ENGINE BAY AREAS, EXHAUSTS, AND THE SURROUNDING AREAS FOR EVIDENCE OF FUEL. NONE WAS FOUND. THE OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. COULD NOT DUPLICATE THE DISCREPANCY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000392004041500039NM 2004 4 15 QXEA200400195 120040305A2130 UNKNOWN BOMBDRDHC8 DHC8401 1390041NM UNKNOWN A QXEAO OTHER O OTHER DEDESCENT 1 NM09406QX 4048 SEA - FLIGHT 2329 - ON DESCENT AND AT 5000 FT, RAPID DEPRESSURIZATION OCCURRED. THE DIFFERENTIAL WENT TO ZERO AND MANUAL MODE/OPERATION MADE NO DIFFERENCE. MAINTENANCE INSPECTED THE AIRCRAFT. NO FAULT CODES WERE SHOWN IN THE CDS. FOUND THE ALTITUDE SET AT 4000 FT. OPERATIONAL CHECKS WERE PERFORMED AND WERE UNABLE TO DUPLICATE THE WRITE-UP. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000412004041500041NM 2004 4 15 QXEA200400198 120040308A6123 AUTOFEATHER SYS BOMBDRDHC8 DHC8401 1390041NM ENGINE UNKNOWN A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09406QX 4048 BOI - FLIGHT 2400 AT APPROXIMATELY 80 KTS ON TAKEOFF ROLL, THE AUTO FEATHER FAILED TO ARM. TAKEOFF ABORTED AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE. PERFORMED OPERATIONAL TEST OF AUTO FEATHER TEST. OPERATION TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000422004041500042NM 2004 4 15 04FDEA00238 120040128A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 N00260 CORROSION (C53-113-01(2)), AFT CARGO BAY, FRAME HAS CORROSION BY FASTENER COLLAR AT BS 1050 LBL 19 WL 150 (FASTENER COMMON TO FLOOR TO SIDEWALL SUPPORT AND FRAME) BLENDED CORROSION ON FRAME AT BS 1050 LBL 19 WL 150 IN AN AREA OF 3X1X.013 O.T. FOUND TO BE .063 DETERMINED TO BE OUT OF LIMITS AS PER SRM 53-10-1. ACCOMPLISHED FORMED SECTION REPAIR AS PER SRM 51-40-3 & FED EX E.A. 7-5310-55217. 2L73 4F RTA3WE 20040415000432004041500043NM 2004 4 15 QXEA200400196 120040305A7110 FITTING BOMBDRDHC8 DHC8401 1390041NM NR 1 COWLING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - NR 1 ENGINE FORWARD OUTBOARD SPINE COWL CLEAT CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-05 AND RD 8/4-71-032. 2H72 4T RTA13NM 20040415000442004041500044NM 2004 4 15 04FDEA00235 120040128A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 FWD CARGO BAY, FRAME DENTED STA 660 STR 24 LT. CUT OUT DENTED MATERIAL FROM FRAME AT BS 660, STR 24L AND PER SRM 51-40-3, 53-10-1, USING 7075-T6, .050 LOT #466242. CUT OUT WAS 1X1 2L73 4F RTA3WE 20040415000462004041500046NM 2004 4 15 2004UALA00270 120040317A7830315A1701123 THRUST REVERSER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE LT ENGINE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29903UA 25003 CRACKED HEAT SHIELD. INNER CORE SKIN DELAMINATED & CRACKED FROM FASTENER. CAUSED BY HEAT & VIBRATION. REPLACED INNER SKIN. OVERHAULED & RIGGED. 2L72 4F4 FRTA16WE E2GL 20040415000472004041500047NM 2004 4 15 QXEA200400200 120040308A213092147A020103 CONTROL PANEL BOMBDRDHC8 DHC8401 1390041NM COCKPIT FAILED A QXEAAI UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CRCRUISE 1 NM09413QX5148 4060 YYC - FLIGHT 2329 - CREW RETURNED TO FIELD WHEN THE CABIN PRESSURE MASTER WARNING LIGHT ILLUMINATED. CABIN PRESSURES WAS ABOVE 10,000 FT AND CLIMBING AT 500-700 FEET PER MINUTE. THE CREW WAS UNABLE TO CONTROL THE PRESSURE MANUALLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE CABIN PRESSURE CONTROL PANEL, AND THE CABIN PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000482004041500048NM 2004 4 15 2004UALA00271 120040322A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 DENT BELOW RIGHT AFT DOOR - DENT MEASURES 2.5 INCHES LONG BY 0.4 INCHES WIDE BY 0.210 DEEP. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER REPAIR INSTALLED. 2L72 4F4 FRTA16WE E2GL 20040415000512004041500051NM 2004 4 15 QXEA200400201 120040308A3320 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09401QX 4031 BZN - ON FLIGHT 2384, FLIGHT ATTENDANT REPORTED A HOT ELECTRICAL SMELL IN THE AREA OF THE PASSENGER SERVICE UNIT IN ROW 11 A/B. SIDEWALL LIGHTS TURNED OFF, AND SMELL AND HEAT DECREASED. PASSENGER SERVICE UNIT WAS ALSO HOT TO THE TOUCH. MAINTENANCE DEFERRED THE SYSTEM. MAINTENANCE RAN THE SIDEWALL LIGHTS FOR 7 HOURS, DROPPED THE PSU'S IN ROWS 10-12. ALL CHECKS NORMAL. NO SMELLS NOTED. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2H72 4T RTA13NM 20040415000522004041500052EU 2004 4 15 2004UALA00279 120040325A5610NP1653115 WINDSHIELD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29447UA20559 836 WINDSHIELD ON CAPTAIN'S SIDE STARTED TO CRACK & GOT PROGRESSIVELY WORSE. FLIGHT DIVERTED. WEATHER SEAL DETERIORATION LEAD TO DELAMINATION OF WINDOW ALLOWING WATER INGRESION CAUSING ARCING AT THE BUS BAR RESULTING IN CRACKING OF THE WINDSHIELD. THE WINDSHIELD WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040415000542004041500054EA 2004 4 15 QXEA200400181 120040227A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX - CHAFE MARK ON RIGHT HAND WING UNDER JUNCTION OF NR 1 AND NR 2 SLATS. REPAIRED IAW HORIZON AIR EA R-57-55. 2L72 4F RTA21EA 20040415000582004041500058NM 2004 4 15 QXEA200400206 120040310A5210502213 DOOR SEAL BOMBDRDHC8 DHC8401 1390041NM PAX DOOR TORN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09403QX6812 4037 GEG - FLIGHT 2337 - THE CREW RETURNED TO GATE WHEN THE MAIN CABIN DOOR SEAL WOULD NOT INFLATE. MAINTENANCE INSPECTED THE DOOR AND REPLACED THE MAIN CABIN DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000592004041500059EA 2004 4 15 QXEA200400212 120040311A261247388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA FIRE WARNING FAULTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09617QX3129 10130 DEN - CREW REPORTS FIRE SYSTEM FAULT STATUS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FIDEX CONTROL UNIT. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000612004041500061NM 2004 4 15 QXEA200400218 120040314A2421 CONNECTOR BOMBDRDHC8 DHC8401 1390041NM NR 1 GENERATOR LOOSE A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09410QX 4053 PDX - DURING FLIGHT 2419 NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. TURNED OFF NR 1 AC GENERATOR SWITCH, THEN BACK ON PER CHECKLIST. GENERATOR CAUTION LIGHT EXTINGUISHED. TIGHTENED CONTROL FIELD CONNECTOR ON AC GENERATOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000632004041500063EA 2004 4 15 QXEA200400220 120040314A2612474075 FIRE DETECTOR CNDAIRCL600 CL6002C10 1390015EA RIGHT FAILED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09617QX 10130 DEN - ON FLIGHT 4339 FIRE SYSTEM FAULT STATUS MESSAGE CAME ON 3-5 TIMES THROUGHOUT THE FLIGHT. REMOVED AND REPLACED RIGHT ENGINE UPPER FIRE DETECTION RAIL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000642004041500064EA 2004 4 15 QXEA200400221 120040316A2820 FUEL SYS CNDAIRCL600 CL6002C10 1390015EA FUEL TANK UNKNOWN A QXEAO OTHER O OTHER TOTAKEOFF 1 NM09611QX 10041 DEN - FLIGHT 4183 - ON TAKEOFF CLIMBOUT, FUEL MIGRATED TO THE CENTER TANK IN EXCESS OF 500 POUNDS. FUEL LEVEL RETURNED TO ZERO IN THE CENTER TANK WITHIN 5 MINUTES. MAINTENANCE INSPECTED THE SYSTEM AND FOUND NO FUEL LEAKS OR MIGRATION TO THE CENTER TANK. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2L72 4F RTA21EA 20040415000652004041500065EA 2004 4 15 QXEA200400223 120040317A3234533405 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA LANDING GEAR FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09611QX485 10041 DEN - FLIGHT 4339 - ON APPROACH, WITH THE GEAR SELECTED DOWN, THE GEAR DID NOT EXTEND. THE CREW ALSO NOTED GEAR DISAGREE WARNINGS WITH AN ASSOCIATED PROXY SYSTEM STATUS MESSAGE. THE CREW EXTENDED THE GEAR USING THE ALTERNATE RELEASE METHOD AND RECEIVED GOOD GEAR DOWN INDICATIONS. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000662004041500066EA 2004 4 15 QXEA200400225 120040318A3620 ELEMENT CNDAIRCL600 CL6002C10 1390015EA BLEED AIR SYS LOOSE A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09609QX 10031 PDX - FLIGHT 2555 RETURNED TO FIELD, RIGHT BLEED DUCT WARNING MESSAGE FOLLOWED BY RIGHT BLEED DUCT CAUTION MESSAGE. MAINTENANCE INSPECTED FOR BLEED LEAKS, NONE NOTED. RESECURED ELEMENTS AT MT144 AND MT204. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000712004041500071WP 2004 4 15 ASAA0480051 120040127A5313591142838 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND LONGERON 23R CORRODED AT FS 769-788. REMOVED CORROSION AND INSTALLED REPAIR U-CHANNEL PER SRM 53-02. (M) 2L72 4F RTA6WE 20040415000782004041500078WP 2004 4 15 ASAA0480087 120040221A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL IS GOUGED ALONG EDGE AT FS 905-977. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000792004041500079WP 2004 4 15 ASAA0480089 120040222A5320993663913 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL SIDE SUPPORT IS CRACKED AND DEFORMED AT FS 826-886. REPLACED SUPPORT PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040415000812004041500081WP 2004 4 15 ASAA0480091 120040222A532199365441 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS TORN EDGE AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000822004041500082WP 2004 4 15 ASAA0480092 120040222A532199365471 INSERT DOUG DC9 DC983 3022083WP FLOOR PANEL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 180-200. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000832004041500083WP 2004 4 15 ASAA0480093 120040222A532199365511 INSERT DOUG DC9 DC983 3022083WP FLOOR PANEL MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS NUMEROUS MISSING, BROKEN AND CORRODED INSERTS AT FS 200-256. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000842004041500084WP 2004 4 15 ASAA0480094 120040222A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS BROKEN INSERTS AND MISSING MATERIAL AT FS 465-541. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000852004041500085WP 2004 4 15 ASAA0480052 120040127A533059360215 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN CORRODED AT AFT LAVATORY SERVICE PANEL. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 5320-01635. (M) 2L72 4F RTA6WE 20040415000882004041500088WP 2004 4 15 ASAA0480177 120040310A5320993061285 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - HV CHECK, FOUND AFT CARGO BAY FLOOR WEB IS CRACKED AT FS 1287-1307. REPLACED WEB PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040415000892004041500089WP 2004 4 15 ASAA0480049 120040127A3830MD08050711 FLANGE DOUG DC9 DC983 3022083WP WASTE CHUTE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT AFT LAVATORY WASTE CHUTE MOUNTING FLANGE CRACKED. STOP-DRILLED CRACKS AND INSTALLED DOUBLER PER EA 2540-01116. (M) 2L72 4F RTA6WE 20040415000922004041500092WP 2004 4 15 ASAA0480172 120040307A53109957739157 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND SHEAR TIE CORRODED AT FS 1287. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 53-03. (M) 2L72 4F RTA6WE 20040415000932004041500093WP 2004 4 15 ASAA0480173 120040307A531359360501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND LONGERON IS CORRODED ON UNDERSIDE AT FS 1219. REMOVED DAMAGED SECTION AND INSTALLED SPLICE AND STRAP PER SRM 53-02. (M) 2L72 4F RTA6WE 20040415000952004041500095WP 2004 4 15 ASAA0480176 120040310A532199365491 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AT FS 148.5-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000972004041500097WP 2004 4 15 ASAA0480044 120040127A53305911432515 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 1398. INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040415000992004041500099WP 2004 4 15 ASAA0480179 120040310A531059360381 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR BEAM PREVIOUS REPAIR ANGLE/SKIN IS CORRODED UNDER FORWARD AND AFT LOWER DOOR STOP MOUNTS. REPLACED DOOR BEAM PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040415001002004041500100WP 2004 4 15 ASAA0480077 120040215A575449374491 SPLICE PLATE DOUG DC9 DC983 3022083WP L/E SLAT BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 OKC - DURING HV1 CHECK, FOUND RIGHT WING 0 TO 1 SLAT SPLICE PLATE UPPER END IS BENT. REPLACED SPLICE PLATE PER SRM 51-10-4 AND 57-50-13. (M) 2L72 4F RTA6WE 20040415001032004041500103WP 2004 4 15 ASAA0480088 120040221A532059360263 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO BAY DOOR BEAM INTERCOSTAL IS CORRODED AT FS 1193. REPLACED INTERCOSTAL PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040415001052004041500105WP 2004 4 15 ASAA0480166 120040307A531059128527 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND NLG RIGHT DOOR JAMB IS CRACKED AT LOWER END OF FRAME. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001062004041500106WP 2004 4 15 ASAA0480167 120040307A531359360501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND LONGERON 29R IS CORRODED AT FS 1295. REMOVED DAMAGE AND INSTALLED REPAIR CHANNEL PER SRM 53-02. (M) 2L72 4F RTA6WE 20040415001122004041500112WP 2004 4 15 ASAA0480107 120040224A52105956879501 WEB DOUG DC9 DC983 3022083WP L1 DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND FORWARD PAX L1 DOOR TORQUE BOX WEB IS CRACKED. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND SHIM PER SRM 53-01. (M) 2L72 4F RTA6WE 20040415001152004041500115SO 2004 4 15 C2XA04TY023 120040127A33501317 LAMP EMB 145 EMB145 3260210SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713964 145123 RT SIDE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED ON MEL 33-50-00/1, PLACARD NR 038565 FOR FURTHER TROUBLESHOOTING. MAINTENANCE RELAMPED THE EMERGENCY EXIT LIGHT, OPERATIONAL CHECKED GOOD. 2L72 4F RTT00011AT 20040413000312004041300031NM 2004 4 13 CALA0400352 120040410A5321143A8126 FLOORBOARD BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND RIGHT SIDEWALL TO FLOORBOARD WEB CORRODED BETWEEN STA 490 AND 500A. A NEW WEB WAS INSTALLED IAW SRM 51-40-20. 2L72 4F RTA16WE 20040413000362004041300036NM 2004 4 13 CALA0400357 120040411A5321146A8127 SHIELD BOEING737 737824 13844BZNM FLOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712238 28808 INSPECTION FOUND RIGHT FLOOR SHIELD CORRODED AT STA 767-787, S25R. THE FLOOR SHIELD WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND 53-60-15. 2L72 4F RTA16WE 20040414000082004041400008NM 2004 4 14 04FDEA00833 120040404A5730 PANEL DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH SEVERAL BULGES. COMPLIED WITH FEDEX EA 1-5710-76644 - WINGS - LEFT AND RIGHT HAND WING AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000102004041400010EU 2004 4 14 MALA040302 120040328A5347 SEAT TRACK SAAB SF340 340B 7860101EU CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 FS 292 FLOORBOARD SUPPORT AND RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED FLOORBOARD SUPPORT AND CORRODED SECTION OF SEAT AT FS 292 IAW SAAB 340 SRM 51-40-40, 51-40-21 AND MESABA EO S53060. A/C RELEASED 4/1/04. 2L72 4T RTA52EU 20040414000252004041400025NM 2004 4 14 04FDEA00847 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT I/B FLAP, O/B HINGE I/B STRAP PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2L73 4F RTA22WE 20040414000302004041400030NM 2004 4 14 UPS04M42090 120040213A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 19 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION AT BOTTOM OF RIGHT NR 19 HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.079 INCH. BARREL NUT HOLE REPAIR PER EN1039-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000322004041400032NM 2004 4 14 UPS04M42092 120040220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RIGHT NR 18 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING. CORROSION AT BOTTOM OF HOLE NR 18 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.053 INCH. BARREL NUT HOLE REPAIRED PER EN1055-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040414000462004041400046NM 2004 4 14 04FDEA00880 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, O/B HINGE I/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76652, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000532004041400053NM 2004 4 14 04FDEA00859 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF O/B PIVOT HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76650, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000542004041400054NM 2004 4 14 04FDEA00860 120040407A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, O/B HINGE I/B ACTUATOR HOLE FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-76649, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040414000652004041400065NM 2004 4 14 04FDEA00840 120040406A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BORE SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76643. TRAILING EDGE FLAPS, LT WING, OUTBOARD FLAP OUTBOARD HINGE PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040414000672004041400067EU 2004 4 14 04FDEA00926 120040412A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP 3RD CARGO TRACK RT SIDE FROM CENTER LINE AT FR 29 ONE EA AREA OF CORROSION. REPAIRED CORRODED AREA AS PER A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040414000812004041400081NM 2004 4 14 04FDEA00871 120040408A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76648. 2L73 4F RTA22WE 20040414000852004041400085NM 2004 4 14 04FDEA00875 120040408A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT I/B FLAP, O/B HINGE I/B LUG PIVOT HOLE FOUND WITH CORROSION. REPAIRED. 2L73 4F RTA22WE 20040414000872004041400087NM 2004 4 14 CALA0400332 120040407A5510180A16122 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733714 28785 INSPECTION FOUND LEFT HORIZONTAL STABILIZER AFT SPAR LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040414000992004041400099NM 2004 4 14 CALA0400337 120040407A53106545805 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 3 INCH CRACK IN FRAME SHEAR TIE AT STA 277 BETWEEN STRINGERS 14 AND 15L. THE CRACKED SECTION OF SHEAR TIE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-07, FIGURE 207. 2L72 4F RTA16WE 20040414001122004041400112NM 2004 4 14 SWAA040922 120040329A5310571769 WINDOW POST BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 DURING SCHEDULED 1/4D CHECK, FOUND COCKPIT NR 1 WINDOW LT POST, OUTBOARD UPPER CORNER CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20040414001212004041400121WP 2004 4 14 04FDEA00823 120040403A7160ATL702991 BELLMOUTH DOUG DC10 DC1010 3022110WP ZONE 400 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25389FE 46623 COMPLY WITH EA 8-7110-75131 ENGINE BELL-MOUTH RING ASSY INTERIM REPAIR A/C N389FE. COMPLIED WITH EA 8-7110-75131. 2L73 4F A22WE 20040414001262004041400126 2004 4 14 SWAA040947 420040331A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040414001302004041400130NM 2004 4 14 SWAA040951 120040331A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 996, STRINGER 27L, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040414001312004041400131NM 2004 4 14 SWAA040952 120040331A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L, AT BS 996, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040414001582004041400158NM 2004 4 14 SWAA040942 120040330A533065458790 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND L-1 DOOR CUTOUT FUSELAGE SKIN AFT UPPER SIDE CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040414002082004041400208 2004 4 14 XNOA1177 420040219A2250 COMPUTER AIRBUS300 A300B4203 3930306EU NR 1 YAW DAMPER DISENGAGED A XN0AD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL23373PC 218 NR 1 YAW DAMPER WILL NOT ENGAGE. ITEM TRANSFERRED TO DMI CONTROL NR 4107 IAW ENA MEL 22-21-01 CAT A PLACARDS INSTALLED. R&R NR 1 YAW DAMP CPU, OPS CK GOOD IAW A300 AMM 22-21-00. PLACARDS REMOVED. THIS ACTION CLEARS DMI #4107. (STATUS:SUPP/CLOSED) 2L72 4F RTA35EU 20040415000232004041500023NE 2004 4 15 HEEA093673 120040208A79210401272780 OIL COOLER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL NR 2 ENGINE CRACKED E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0322342 760096 IN CRUISE FLIGHT, THE NR 2 ENGINE OIL TEMPERATURE ROSE TO THE RED LINE. SECURED ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT JUNCTION OF THE OIL COOLER BLOWER DUCT CRACKED AND SPLIT OPEN. 1G72 3U3 U H1NE E1GL 20040415000272004041500027CE 2004 4 15 GLBA20030564 120040213A271050524531 IDLER GEAR BEECH 1900 1900D 1154162CE AILERON TRIM STICKING A GLBAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM03247GL UE247 AILERON TRIM CATCHES AND STICKS, R&R IDLER GEAR ASSY. OPS CK GOOD 2L72 4T RTA24CE 20040415000552004041500055NM 2004 4 15 QXEA200400203 120040309A3297471525 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG OUT OF TOLERANCEA QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX2319 4047 SEA - FLIGHT 2333 - THE AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE PSEU FAULT NW CENTERING FAULT 1. THE NOSE WHEEL CENTERING PROX SENSOR SHOWS BETWEEN TOO FAR AND FAR WITH THE NOSE LANDING GEAR AT CENTER. THE RVDT, AND STEERING HARNESS WAS REPLACED AND THE NOSE WHEEL STEERING SYSTEM WAS RIGGED. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000562004041500056EA 2004 4 15 QXEA200400204 120040310A2824T99A38603 EJECTOR CNDAIRCL600 CL6002C10 1390015EA LEFT CRACKED A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09608QX3040 10026 BOI - FLIGHT 4276 - THE CREW REPORTED THAT THE LEFT FUEL TANK WAS LEAKING INTO THE CENTER TANK AND RECEIVED A FUEL IMBALANCE CAUTION MESSAGE. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE LEFT PRIMARY EJECTOR CRACKED. THE EJECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000862004041500086WP 2004 4 15 ASAA0480047 120040127A532199366881 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL HAS DAMAGED CORE AT FS 655. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415000872004041500087WP 2004 4 15 ASAA0480048 120040127A53203914677507 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND STRUCTURAL SPLICE IS CORRODED AT FS 1212 IN AFT CARGO BAY AREA. REMOVED CORROSION AND TREATED PER EA 5310-02309. (M) 2L72 4F RTA6WE 20040415000912004041500091WP 2004 4 15 ASAA0480076 120040215A5532591216612N SKIN DOUG DC9 DC983 3022083WP VERTICAL STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 OKC - DURING HV1-CHECK, FOUND VERTICAL STABILIZER SKIN GOUGED JUST ABOVE HORIZONTAL STABILIZER RIGHT PIVOT POINT. REPLACED SKIN PER SRM 51-30-1 AND 51-30-2. (M) 2L72 4F RTA6WE 20040415001042004041500104WP 2004 4 15 ASAA0480165 120040307A533059114013 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND NLG LEFT DOOR AFT HINGE CUTOUT IS CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001072004041500107WP 2004 4 15 ASAA0480168 120040307A5320993033886 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND WEB CORRODED AT FS 294-313. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040415001192004041500119EA 2004 4 15 QXEA200400177 120040226A26119847101505 SCREEN CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - FORWARD CARGO BAY CENTER CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20040415001202004041500120NE 2004 4 15 QXEA200400179 220040226A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE WORN A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 NM09605QX4581 10022 GEE965274 MFR - FLIGHT 2557 ON FLIGHT FROM PDX TO ONT AIRCRAFT DIVERTED TO MFR DUE TO NR 1 ENGINE VIBRATION. REPLACED FAN BLADES SERIAL NUMBERS, IHI3069N, IHI3130N, IHI3140N, IHI3144N, IHI3149N, IHI3150N, IHI3156N, IHI3158N, IHI3160N, IHI3178N, IHI3180N, IHI3182N, IHI3186N, IHI3188N, IHI3190N, IHI3191N, IHI3192N, IHI3193N, IHI3194N, IHI3195N, IHI3196N, IHI3198N, IHI3200N, IHI3202N, IHI3203N, IHI3204N, IHI3206N, AND IHI3208N. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040415001232004041500123NM 2004 4 15 QXEA200400184 120040207A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09351PH1458614181 490 PDX - FORWARD CABIN ESCAPE EXIT LOWER EMERGENCY LIGHT EXIT SIGN INOP. MAINTENANCE REPLACED THE LENS AND LAMP ASSEMBLY WITH NO HELP. REPLACED THE PS5 POWER SUPPLY CONTROL BOX. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001252004041500125NM 2004 4 15 QXEA200400190 120040305A2610 DETECTOR BOMBDRDHC8 DHC8401 1390041NM NR 1 ENGINE DIRTY A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09416QX 4083 FCA - FLIGHT 2449 - WHEN THE ADVISORY TEST IS SELECTED, THE FIRE WARNING BELL IS TRIGGERED. MAINTENANCE INSPECTED THE SYSTEM AND CLEANED THE PEC ADVANCE PNEUMATIC DETECTOR AT THE NR 1 ENGINE. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040415001262004041500126NM 2004 4 15 QXEA200400192 120040307A5210 LEVER DHAV DHC8 DHC8202 2809007NM PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 SEA - FLIGHT 2065 - THE MAIN CABIN DOOR RELEASE LEVER IS STICKING WHILE ATTEMPTING TO OPEN THE DOOR. MAINTENANCE INSPECTED THE AIRCRAFT DOOR THEN CLEANED AND LUBRICATED THE DOOR LEVER MECHANISM AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001292004041500129NM 2004 4 15 QXEA200400208 120040313A2913570347001 PUMP DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE FAILED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09362PH13271 518 SEA - FLIGHT 2222 - AIRCRAFT RETURNED TO GATE AFTER RECEIVING A NR 2 ENGINE HYDRAULIC PUMP CAUTION INDICATION. THE NR 2 HYDRAULIC PRESSURE BLED TO 0 PSI. THE STANDBY HYDRAULIC PRESSURE WAS NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 ENGINE DRIVEN PUMP. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001302004041500130EU 2004 4 15 2004UALA00304 120040401A3233114095004 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT MLG CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29412UA 465 RIGHT MAIN LANDING GEAR LOCK STAY ACTUATOR CYLINDER FOUND WITH CORROSION ON THE PORT STATIC SEAL SURFACE. MAJOR REPAIR ACCOMPLISHED. CORROSION REMOVED BY MACHINING AREA AROUND PORT. FOUR LAYERS OF INTERFILL APPLIED TO REWORKED AREA. 2L72 4F4 FRTA28NM E40NE 20040415001332004041500133 2004 4 15 SWAA040989 420040405A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040415001352004041500135NM 2004 4 15 SWAA040990 120040405A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 597, STRINGER 8R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040415001372004041500137NM 2004 4 15 SWAA040991 120040405A33976573709 WIRE BOEING737 7373H4 1384600NM COCKPIT BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND L1 AND R1 DOOR EVAC SLIDE LIGHTS INOP. REPAIRED BROKEN WIRE AT OVERHEAD PANEL IN COCKPIT PER WDM AND MM. 2L72 4F RTA16WE 20040415001382004041500138NM 2004 4 15 SWAA040992 120040405A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 13L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001412004041500141NM 2004 4 15 SWAA040993 120040405A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727 + 5, BS 767 + 6, STRINGER 20L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001422004041500142NM 2004 4 15 SWAA040994 120040405A3350101073 LENS BOEING737 7373A4 1384585NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LENS PER MM. 2L72 4F RTA16WE 20040415001442004041500144NM 2004 4 15 SWAA040996 120040405A53206551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICE AT BS, 908, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040415001482004041500148NM 2004 4 15 SWAA040972 120040402A53306545760 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 470, STRINGER 17R, BS 500D, STRINGER 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001492004041500149NM 2004 4 15 SWAA040973 120040402A3350101114 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT SIGN MISSING LENS. INSTALLED EMERGENCY EXIT LENS PER MM. 2L72 4F RTA16WE 20040415001512004041500151NM 2004 4 15 SWAA040975 120040402A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C4 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EMERGENCY EXIT LENS PER MM. 2L72 4F RTA16WE 20040415001532004041500153NM 2004 4 15 SWAA040977 120040402A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C1 CHECK, FOUND EQUIPMENT COOLING DUCT EXHAUST CUT OUT SKIN CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040415001562004041500156NM 2004 4 15 SWAA040980 120040403A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040415001572004041500157NM 2004 4 15 SWAA040982 120040403A57536546435281 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20040415001592004041500159NM 2004 4 15 SWAA040984 120040403A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 908, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001612004041500161 2004 4 15 SWAA040986 420040404A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040415001622004041500162NM 2004 4 15 SWAA040987 120040404A533065C33757 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 275, BETWEEN STRINGERS 15L AND 16L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001632004041500163NM 2004 4 15 QXEA200400216 120040314A3040KCD4N RELAY BOMBDRDHC8 DHC8401 1390041NM COCKPIT FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09407QX6057 4049 SEA - ON FLIGHT NUMBER 2338, WINDSHIELD HOT CAUTION CAME ON DURING CRUISE FLIGHT WITH SWITCH SELECTED ON. COMPLIED WITH ABNORMAL CHECKLIST. CDS: NO ASSOCIATED FAULTS. REMOVED AND REPLACED 3041-K7 RELAY. COMPLIED WITH OPERATIONAL TEST OF PILOT/COPILOT WINDSHIELD ANTI ICE SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001662004041500166NM 2004 4 15 QXEA200400241 120040324A335061047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09345PH* 539 476 PDX - EMERGENCY TRACK LIGHTS AT FORWARD EMERGENCY EXIT ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACKS. 2H72 4T RTA13NM 20040415001692004041500169NM 2004 4 15 QXEA200400243 120040325A335082520977001 COVER DHAV DHC8 DHC8202 2809007NM CABIN MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09350PH 488 PDX - EMERGENCY PATH LIGHT COVER MISSING A SECTION AT ROW 1. REMOVED AND REPLACED LIGHTING ASSEMBLY. 2H72 4T RTA13NM 20040415001722004041500172NM 2004 4 15 QXEA200400213 120040312A271182740201003 SPRING DHAV DHC8 DHC8202 2809007NM AILERON TAB WORN A QXEAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM09357PH14368 504 PDX- ON FLIGHT 2131 ROLL CONTROL VERY STIFF AND SLUGGISH. MORE PRONOUNCED WHEN ROLLING TO THE LEFT. NOTICED DURING DESCENT THROUGH THE LANDING PHASES OF FLIGHT. MAINTENANCE INSPECTED THE SYSTEM AND RIGGED THE RIGHT AILERON TAB AND REPLACED THE TRIM TAB SPRINGS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001732004041500173NM 2004 4 15 QXEA200400224 120040311A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN MISSING A QXEAK NONE O OTHER UKUNKNOWN 1 NM09364PH 524 SEA - ON FLIGHT 2091 CABIN FLOOR TRACK LIGHTING IS MISSING AROUND ROW 1. REMOVED AND REPLACED FLOOR TRACK LIGHTING AT ROW 1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001742004041500174NM 2004 4 15 QXEA200400229 120040321A5420 BRACKET BOMBDRDHC8 DHC8401 1390041NM RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - RIGHT HAND FORWARD NACELLE UPPER INBOARD ANGLE BRACKET IS CRACKED AT RADIUS. REPAIRED IAW RD 8/4-71-032. 2H72 4T RTA13NM 20040415001752004041500175NM 2004 4 15 USAA04000A 120040103A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU47922 23705 FOUND BULKHEAD WEB CRACKED .5 INCH, 178 BULKHEAD WEB AT LOWER LT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664 PATCH AND SRM 53-10-08 FIG 211. (M) 2L72 4F RTA16WE 20040415001762004041500176NM 2004 4 15 QXEA200400072 120040123A2130 SEAL BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAK NONE O OTHER DEDESCENT 1 NM09406QX5914 4048 LOST CABIN PRESSURE ON DESCENT AT 7000 FEET. COULD NOT PRESSURIZE EVEN IN MANUAL. FLIGHT ATTENDANT NOTICED HISSING NOISE AT AFT AIR STAIRS DOOR. MANTENANCE INSPECTED ALL DOOR SEALS; CYCLED THE PASSENGER AND CARGO DOOR HANDLES; CLEANED AROUND THE AFT PASSENDER DOOR SEAL. MAINTENANCE PERFORMED AN OPERATIONAL CHECKS WITH ENGINES RUNNING. ALL CHECKS WERE GOOD. THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001772004041500177NM 2004 4 15 QXEA200400246 120040328A26114462531 SMOKE DETECTOR BOMBDRDHC8 DHC8401 1390041NM LAVATORY DEFECTIVE A QXEAK NONE N FALSE WARNING UKUNKNOWN 1 NM09407QX 4049 SEA - ON FLIGHT 2402 NO GREEN LIGHT ON LAVATORY SMOKE DETECTOR. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001782004041500178NM 2004 4 15 QXEA200400250 120040327A5414 PANEL BOMBDRDHC8 DHC8401 1390041NM RT NACELLE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - DENT ON RIGHT HAND NACELLE PANEL 422CT, LEFT HAND SIDE 14.5 INCHES AFT OF PANEL 422AL AND 11.5 INCHES ABOVE PANEL 422BL. REPAIRED IAW HORIZON AIR EA 6-54-293. 2H72 4T RTA13NM 20040415001792004041500179NM 2004 4 15 QXEA200400263 120040410A33506104789 BATTERY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09374PH10437345 528 PDX - EMERGENCY CEILING LIGHTS NR 1 AND NR 3 FORWARD AND AFT ARE INOPERATIVE. REMOVED AND REPLACED NR 1 AND NR 2 EMERGENCY LIGHT BATTERIES. 2H72 4T RTA13NM 20040415001822004041500182NM 2004 4 15 QXEA200400249 120040325A3350AC4LW LIGHT DHAV DHC8 DHC8202 2809007NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09355PH 500 PDX - EMERGENCY EXIT FAILS BETA LIGHT TEST. REMOVED AND REPLACED BETA LIGHTS. 2H72 4T RTA13NM 20040415001852004041500185NM 2004 4 15 USAA04000B 120040107A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US50290 23315 FOUND WEB CRACKED .5 INCH, BULKHEAD WEB BS 178, WL 218, RBBL 5.7. INSTALLED DOUBLER PER EO 5300V153. (M) 2L72 4F RTA16WE 20040415001872004041500187NM 2004 4 15 USAA04000C 120040212A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU47922 23705 FOUND FORWARD BULKHEAD CRACKED .5 INCH, 178 BULKHEAD WEB AT UPPER RIGHT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664, PATCH PER SRM 53-10-08 FIG 211. (M) 2L72 4F RTA16WE 20040415001902004041500190EA 2004 4 15 QXEA200400233 120040303A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 PDX - RIGHT HAND AND LEFT HAND TRAILING EDGES OF PYLON CAUSED SKIN ABRASIONS TO AIRCRAFT. REPAIRED IAW SRM 51-25-26. 2L72 4F RTA21EA 20040415001922004041500192NM 2004 4 15 QXEA200400234 120040320A5270 SWITCH BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DIRTY A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09409QX 4051 SEA - ENTERED AREA OF OCCASIONAL MODERATE TURBULENCE IN FLIGHT AND INTERNAL BAGGAGE DOOR CAUTION LIGHT ILLUMINATED. RAN CHECKLIST AND LIGHTS REMAINED ON FOR REMAINDER OF FLIGHT. CLEANED, LUBED INTERNAL BAGGAGE DOOR SWITCH/ROD. CYCLED BAGGAGE DOOR SEVERAL TIMES. CAUTION LIGHT ILLUMINATED AND EXTINGUISHED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040416000012004041600001NE 2004 4 16 A6WA2003400ZZ 220040105A7230 BLADE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ENGINE NICKED A A6WAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL31459AW 7863 873916 AFTER TAKEOFF, RIGHT ENGINE VIBRATION WENT TO 3.9, FELT AIRFRAME VIBRATION, WITH THRUST REDUCED VIBRATION INDICATION REDUCED TO GREEN RANGE. AIR RETURN, INSPECTED FAN IAW 72-20-00. BLENDED NICKS FROM SEVERAL BLADES IAW AMM TASK 72-20-00-300-801, ALL MINOR BLENDING. GROUND RAN CHECKED GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20040416000072004041600007NE 2004 4 16 QXEA200400238 220040324A7200CF348C1 ENGINE BOMBDRDHC8 DHC8401 1390041NM GE CF34 CF348C1 NE NR 2 MALFUNCTIONED A QXEAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09413QX5773 2248 4060 PCEFA0112 NR 2 ENGINE INFLIGHT SHUTDOWN, ON CLIMBOUT NR 2 PEC CAUTION LIGHT, NR 2 FADEC FAIL WARNING LIGHTS ILLUMINATED, NR 2 ENGINE AUTO FEATHER. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 FRTA13NM EOOO63EN 20040416000092004041600009NM 2004 4 16 QXEA200400237 120040324A7603 SWITCH DHAV DHC8 DHC8202 2809007NM POWER LEVER MALFUNCTIONED A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09365PH 526 SEA FLIGHT 2195 RETURN TO FIELD, NR 1 ENGINE INFLIGHT SHUTDOWN, TORQUE FLUCTUATION AT ALL POWER SETTINGS. MAINTENANCE REPLACED THE POWER LEVER SWITCH. OPERTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040416000102004041600010NM 2004 4 16 GAIA04032OP 120040221A27612145014 ACTUATOR BOEING727 727223 1384074NM LT WING SPOILER OUT OF ADJUST A GAIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SW07854AA 20995 AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. ADJUSTED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. GROUND OPS CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000122004041600012NM 2004 4 16 GAIA04033BOP 120040221A2612 FIRE LOOP BOEING727 727225 1384077NM NR 1 ENGINE OUT OF ADJUST A GAIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW07936PG 22441 NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. REPOSITIONED NR 1 ENGINE FIRE LOOP. GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000132004041600013NM 2004 4 16 GAIA04033AOP 120040221A2612 WARNING LIGHT BOEING727 727225 1384077NM NR 1 FIRE DETECTILLUMINATED A GAIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW07936PG 22441 NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. (M) 2L73 4F A3WE 20040416000152004041600015NM 2004 4 16 GAIA04026OP 120040205A3200 WARNING LIGHT BOEING727 727243 138408DNM TAIL SKID ILLUMINATED A GAIAO OTHER J WARNING INDICATION CLCLIMB 1 SW07579PE 21662 AFTER TAKEOFF, THE TAIL SKID LIGHT REMAINED ILLUMINATED. RECYCLED THE LANDING GEAR AND THE LIGHT WENT OUT. PERFORMED OPERATIONAL CHECK AND TEST OF THE TAIL SKID SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L73 4F RTA3WE 20040416000162004041600016NM 2004 4 16 GAIA04031OP 120040220A27612145014 ACTUATOR BOEING727 727223 1384074NM LT WING SPOILER MALFUNCTIONED A GAIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SW07854AA 20995 AIRCRAFT ROLLS TO THE LEFT WHEN THE SPEED BRAKES ARE EXTENDED. FOUND NR 3 SPOILER ACTUATOR BYPASSING. REMOVED AND REPLACED THE NR 3 SPOILER ACTUATOR IAW THE BOEING MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000172004041600017NM 2004 4 16 GAIA04024OP 120040219A2612 FIRE LOOP BOEING727 727224 1384076NM NR 3 ENGINE LOOSE A GAIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW0779748 22450 THE NR 3 ENGINE GROUND FAULT LIGHT CAME ON DURING TAXI AT SFO. INSPECTED AND CHECKED NR 3 ENGINE FIRE LOOP CLEANED AND RESECURED CONNECTORS. THE SYSTEM OPERATIONALLY CHECKED GOOD NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000182004041600018NM 2004 4 16 GAIA04023OP 120040219A2612 FIRE LOOP BOEING727 727225 1384077NM NR 1 ENGINE GROUNDED A GAIAO OTHER J WARNING INDICATION LDLANDING 1 SW07936PG 22441 THE NR 1 ENGINE GROUND FAULT LIGHT CAME ON AFTER LANDING IN FWA. NR 1 ENGINE FIRE LOOP WAS FOUND GROUNDED OUT. REPOSITIONED LOOP AND THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000192004041600019 2004 4 16 GAIA04022OP 420040206A22119030951901 COMPUTER BOEING727 727243 138408DNM AUTOPILOT SYS MALFUNCTIONED A GAIAO OTHER J WARNING INDICATION CRCRUISE 1 SW071269Y 21269 DURING CRUISE, THE AUTOPILOT OVER CORRECTS ON LOCALIZER. REMOVED AND REPLACED THE ROLL CHANNEL COMPUTER. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L73 4F RTA3WE 20040416000252004041600025 2004 4 16 GAIA04029OP 420040218A221125858056 COMPUTER BOEING727 727251 138408HNM AUTOPILOT SYS MALFUNCTIONED A GAIAO OTHER J WARNING INDICATION CRCRUISE 1 SW07278US 21157 DURING CRUISE THE AIRPLANE OCCASIONALLY TURNS RIGHT AND WILL NOT RESPOND BACK TO THE LEFT WITH FULL AUTOPILOT HEADING DEFLECTION TO THE LEFT. FLIGHT CONTINUED AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE AUTO PILOT ROLL CHANNEL COMPUTER. SYSTEM OPS CHECKS ON GROUND OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040416000282004041600028NM 2004 4 16 GAIA04025OP 120040205A2797 CONNECTOR BOEING727 727243 138408DNM RT WING L/E DIRTY A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW071269Y 21269 DURING CRUISE, THE NR 4 LEADING EDGE FLAP SHOWS EXTENDED WITH THE FLAPS RETRACTED. CLEANED AND RESEATED THE CONNECTOR ON THE NR 4 LEADING EDGE FLAP SWITCH. OPS CHECK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L73 4F RTA3WE 20040419000022004041900002WP 2004 4 19 ASAA0480040 120040126A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE TOOL DAMAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING INSPECTION, FOUND RIVET SET MARK AT STATION 398, LONGERON 30, ON SKIN. REPAIRED BY COLD WORKED AREA, COMPLIED WITH HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040419000062004041900006 2004 4 19 ASAA0480031 420040127A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA PREFLIGHT CHECK, FOUND AFT SERVICE DOOR L2 EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040419000072004041900007WP 2004 4 19 ASAA0480072 120040212A3350PA122261 LIGHT DOUG DC9 DC983 3022083WP COCKPIT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS 53079 SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD STANDBY EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED LIGHT SOCKET. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040419000102004041900010WP 2004 4 19 ASAA0480004 120040118A5610 WINDOW DOUG DC9 DC982 3022082WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 SEA - DURING PREFLIGHT CHECK, FOUND RIGHT F/O'S SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED OPERATING MECHANISM, WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040419000132004041900013WP 2004 4 19 ASAA0480001 120040101A33501001191 LIGHT DOUG DC9 DC983 3022083WP PAX CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS26995210 53453 PDX - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040419000142004041900014WP 2004 4 19 ASAA0480029 120040120A5320993061221 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND RIGHT CUSP WEB IS CRACKED AT FS 1204. REPLACED CRACKED SECTION, AND INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20040419000152004041900015WP 2004 4 19 ASAA0480023 120040120A53219936539503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE DAMAGE, UNSPECIFIED AT FS 148-160. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000232004041900023 2004 4 19 ASAA040002 420040101A25653961896501 LANYARD DOUG MD80 MD83 3023681NM ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01981AS 53472 LAS - DURING PREFLIGHT CHECK, FOUND AFT SERVICE L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RT 20040419000242004041900024WP 2004 4 19 ASAA0480041 120040126A5310993607339 SHEAR TIE DOUG DC9 DC983 3022083WP FS 1193 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING INSPECTION, FOUND AFT PIT STATION 1193 BETWEEN STRINGER 20 AND 29L SHEAR TIE CORRODED. REPAIRED BY REMOVED DAMAGE, FABRICATED REPAIR SHEAR TIE AND SPLICE IAW MD80 SRM 53-03. (M) 2L72 4F RTA6WE 20040419000272004041900027WP 2004 4 19 ASAA0480022 120040120A53219936547501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 175-196. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000282004041900028WP 2004 4 19 ASAA0480021 120040120A532199365461 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AROUND THREADED FASTENERS AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M0 2L72 4F RTA6WE 20040419000292004041900029WP 2004 4 19 ASAA0480020 120040120A53219957918501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 927-1003. INSTALLED FASTENER TO PLUG PUNCTURE PER SRM 53-01. (M) 2L72 4F RTA6WE 20040419000332004041900033WP 2004 4 19 ASAA0480024 120040120A532199366481 FLOOR PANEL DOUG DC9 DC983 3022083WP FS DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND EXISTING CABIN FLOOR PANEL REPAIR DOUBLER HAS DISBONDED AT FS 1155-1250. REBONDED DOUBLER EPR SRM 51-70-1. (M) 2L72 4F RTA6WE 20040419000352004041900035WP 2004 4 19 GTIA040154 120040227A215060714622 CONTROLLER DOUG DC9 DC981 3022081WP PACK AUTO TEMP MALFUNCTIONED A GTIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL23811NK 48017 ACY - FLT 1148 - AFTER TAKEOFF FROM ACY, THE AFT LEFT AND RIGHT DETECTORS WENT OFF AND FLIGHT ATTENDANT'S SAID AN OIL HAZE WAS IN THE AIR. LOOKED AT CABIN TEMP VALVE AND RIGHT VALVE WAS MAX TO THE RIGHT. PUT RIGHT VALVE TO MANUAL AND DROVE VALVE TO COLD. A/C CLEARED OF HAZE IN THE AFT AND DETECTORS WENT OFF. REMOVED AND REPLACED RIGHT AUTO TEMP CONTROLLER. SYSTEM CHECKS GOOD. (M) 2L72 4F A6WE 20040419000382004041900038 2004 4 19 GTIA040146 420040210A2565 SLIDE DOUG DC9 DC983 3022083WP R1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 DTW - FOUND R1 SLIDE PACK FELL OFF. RESECURED R1 DOOR SLIDE PACK, NO DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040419000412004041900041NE 2004 4 19 GTIA040152 220040222A7230 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 1 COMPRESSOR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 718528 DTW - FOUND SEVERAL C1 BLADES HAVE FOD DAMAGE NR 1 ENGINE. REMOVED AND REPLACED 12 EACH C1 BLADES. (M) 2L72 4F4 F A6WE E9NE 20040419000422004041900042NM 2004 4 19 USAABB04020 120040207A335020121 CHARGER BOEING767 7672B7 1385107NM R3 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19651US 24764 CLT - FOUND THE EXTERNAL SLIDE EMERGENCY LIGHTS INOPERATIVE AT THE R3 DOOR. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY. (M) 2L72 4F RTA1NM 20040419000432004041900043CE 2004 4 19 2004F00097 120040113A7830602HE66 SWITCH LEAR 60 60LEAR 5170707CE THRUST REVERSER DIRTY A DELAO OTHER J WARNING INDICATION NRNOT REPORTED 1 CE03660AS 191 LEFT UNLOCK LIGHT STAYED ON DURING THRUST REVERSER CHECK. CLEANED AND LUBED THRUST REVERSER POSITION SWITCHES AND OPS CHECKED GOOD. (M) 2L72 4F RTA10CE 20040419000442004041900044EU 2004 4 19 USAABA04002 120040210A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19675US 0370 PHL - FOUND BATTERIES FAILED AT EPSU'S 11WL, 13WL, AND 14WL. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20040419000462004041900046NM 2004 4 19 GAIA04042OP 120040227A2612 FIRE LOOP BOEING727 727225 1384077NM NR 1 ENGINE OUT OF POSITION A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07936PG 22441 FLT 714 - FWA-MIA - NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND DETECTOR CHAFING AT COWL DOOR. REPOSITIONED NR 1 ENGINE FIRE LOOP. GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000472004041900047WP 2004 4 19 GTIA040156 120040227A3260833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083WP MLG FAILED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23814NK 49619 LGA - FLT 706 - UNSAFE NOSE GEAR LIGHT STAYED ON WHEN GEAR HANDLE DOWN PIN WAS EXTENDED. FOUND NOSE GEAR SENSOR DOWN LOCK FAILED. REMOVED AND REPLACED NOSE GEAR DOWN SENSOR AND OPS CHECK GOOD, GEAR SWING GOOD. (M) 2L72 4F RTA6WE 20040419000482004041900048WP 2004 4 19 GTIA040155 120040229A3297 CONNECTOR DOUG DC9 DC983 3022083WP NLG UNSAFE LIGHTDAMAGED A GTIAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23814NK 49619 DTW - FLT 1923 - INTERMITTENT NLG UNSAFE LIGHT ON ARRIVAL. FOUND PUSHBACKED PIN 'B' ON CONNECTOR R5-1157. RESEATED AND RESECURED PUSHBACKED PIN 'B' ON CONNECTOR R5-1157. PERFORMED BITE, OPS CHECK ON PSEU. BITE OPS CHECK OK. NO FAULTS NOTED ON NLG DOWNLOCK SENSOR. (M) 2L72 4F RTA6WE 20040419000502004041900050NM 2004 4 19 USAA040031 120040228A5312 STIFFENER BOEING737 737301 1384611NM APBULKHEAD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 PIT - FOUND STIFFENER CORRODED, BS 1016 APBH CHANNEL STIFFENER RIGHT SIDE BOTTOM. CORRODED SECTIONS REPLACED PER EO 5302V112. (M) 2L72 4F RTA16WE 20040419000542004041900054 2004 4 19 GAIA04037OP 420040225A2211258580410 COMPUTER BOEING727 727224 1384076NM AUTOPILOT MALFUNCTIONED A GAIAO OTHER J WARNING INDICATION CRCRUISE 1 SW0779748 22450 FLT 578 - SFO-PHX-FWA - AUTOPILOT DIFFICULT TO ENGAGE IN CRUISE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000572004041900057NM 2004 4 19 UIEA200400026 120040302A5230 WEB BOEING747 747230B 1384889NM FWD CARGO DOOR DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15509MC 21221 LOWER FORWARD CARGO DORO HAS WEB DAMAGED AT TWO LOCATIONS, FORWARD AND AFT, ADJACENT TO POWER DOOR LOCK PUSH PULL RODS. REMOVED DAMAGED WEB FABRICATED NEW WEB AND INSTALLED NEW WEB AS PER SRM 51-30-02, 51-10-02 AND 52-30-02. (M) 2L74 4F A20WE 20040419000582004041900058CE 2004 4 19 2004F00098 120040120A5230541554226 CABLE LEAR 55 55LEAR 5170702CE PAX DOOR FRAYED A DELAO OTHER O OTHER NRNOT REPORTED 1 CE03723CC 036 SEVERAL STRANDS OF THE LOWER MAIN ENTRY DOOR CABLE WERE FOUND FRAYED. REMOVED AND REPLACED DOOR CABLE. (M) 2L72 4F A10CE 20040414002022004041400202WP 2004 4 14 04FDEA00892 120040409A5410 NUT PLATE DOUG DC10 DC1010 3022110WP NR 3 NACELLE DAMAGED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25366FE 46602 ON LANDING ROLLOUT NR 3 WOULD NOT GO INTO REVERSE. DID NOT GET ANY LIGHTS FOR INDICATION OF REVERSE PRESS OR UNLOCK. BY DIRECTION OF MAINT TRIED TO CYCLE REVERSER ON TAXI IN, NO JOY. MEL 09APR04. RELEASED FOR SERVICE PER MEL/CDL: 78-01-01-A CATEGORY: A EXPIRATION: 03JAN07 MEL 78-01-01-A: ENGINE NR 3 THRUST REVERSER INOP. TAKEOFF PERFORMANCE PENALTY MAY APPLY. DO NOT REACTIVATE ENGINE NR 3 THRUST REVERSER WITHOUT PRIOR AUTHORIZATION FROM POWERPLANT ENGINEERING (REF AD CHECK NR 3 T/R TRANSCOWL DO NOT OPERATE TAG NUT PLATES. FOUND NUT PLATES BAD ON INBOARD AND OUTBOARD TRANSLATING COWL. REMOVED AND REPLACED NUT PLATES IN REF TO DC-10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040415000082004041500008SW 2004 4 15 AC2A093681 120040306A6210412015303101 TRIM TAB BELL 430 430 1182150SW M/R BLADE CRACKED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CM 49090 TRIM TAB ON MAIN ROTOR BLADE IS CRACKED. REPLACED TRIM TAB. 1G72 3U RTH9SW 20040415000262004041500026NM 2004 4 15 QXEA200400182 120040220A2440 PIN BOMBDRDHC8 DHC8401 1390041NM EXTERNAL POWER DIRTY A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09410QX 4053 SEA - ON FLIGHT 2349 STATION PERSONNEL REPORTED WHEN DISCONNECTED THE GPU THERE WAS SMOKE COMING FROM THE AIRCRAFT GPU RECEPTACLE AND THE GPU CORD WAS HOT. COCKPIT ELECTRICAL SYSTEMS APPEARED NORMAL. INSPECTED GPU RECEPTACLE. CLEANED MATERIAL FROM PIN. CONNECTED GPU AND APPLIED GROUND POWER. DC EXTERNAL POWER ON INDICATED NORMAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000322004041500032SO 2004 4 15 DIN2004F000A 220040210A741410357586 GEAR CESSNA310 310R 2074245CE CONT O520 IO520MB 17032SO MAGNETO DAMAGED E DINAO OTHER O OTHER NRNOT REPORTED 1 EA135336C 421 310R1542 277915R A COMPLETE O/H OF THE ENGINE AND MAGNETOS WAS ACCOMPLISHED BY MFG ON 6/20/2002. THE PLASTIC GEAR (10-357583) DID NOT SEEM TO BIND WITH ANY FOREIGN MATERIALS. THE GEAR SEEMED FADDED TO A YELLOWISH COLOR. IT DOES NOT SEEM LIKE THIS GEAR WAS REPLACED AT O/H (421.3). IF THIS GEAR WAS REPLACED AT O/H MAYBE THERE WAS A BATCH OF BAD GEARS. THIS GEAR IS CRACKED AND MISSING ABOUT 8 TEETH IN 3 AREAS. 1L72 3O3 O 3A10 E5CE 20040415000332004041500033NM 2004 4 15 QXEA200400188 120040302A2130100314001 SERVO VALVE DHAV DHC8 DHC8202 2809007NM CABIN PRESSURE FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09365PH12402 526 BOI - FLIGHT 2202 - THE AIRCRAFT RETURNED TO FIELD TWICE WHEN AFTER TAKEOFF THE AIRCRAFT FAILED TO PRESSURIZE. ON THE FIRST RETURN, MAINTENANCE FOUND THE PRESSURE REGULATOR VALVE STICKING. REPLACED THE VALVE, PERFORMED OPERATIONAL CHECKS, AND RETURNED THE AIRCRAFT TO SERVICE. WHEN THE AIRCRAFT RETURNED BACK TO THE FIELD, MAINTENANCE INSPECTED THE AIRCRAFT AND PRESSURIZATION SYSTEMS AND REPLACED THE FLOW CONTROL SERVO. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000452004041500045NM 2004 4 15 QXEA200400197 120040307A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - FOUR DENTS ABOVE NR 12 WINDOW, LEFT SIDE OF AIRCRAFT, JUST AFT OF ICE SHIELD. REPAIRED IAW HORIZON AIR EA 6-53-330. 2H72 4T RTA13NM 20040415000492004041500049NM 2004 4 15 QXEA200400202 120040308A2843 BULB BOMBDRDHC8 DHC8401 1390041NM NR 1 FAULTY A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09413QX 4060 PDX - ON CLIMBOUT, NR 1 FUEL TEMPERATURE INDICATION ON ENGINE DISPLAY FLUCTUATED RAPIDLY FULL SCALE. ACCOMPLISHED ABNORMAL FUEL TEMPERATURE E/A CHECKLIST. MAINTENANCE INSPECTED AND WIGGLED FUEL TEMPERATURE BULB HARNESS FROM TEMPERATURE BULB TO FIREWALL CONNECTOR. NO DISCREPANCIES NOTED. REPLACED NR 1 FUEL TEMPERATURE BULB AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000572004041500057NM 2004 4 15 QXEA200400205 120040310A5210502213 DOOR SEAL BOMBDRDHC8 DHC8401 1390041NM PAX DOOR TORN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09406QX6180 4048 SEA - FLIGHT 2442 - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE AIRCRAFT FAILED TO PRESSURIZE. THE FLIGHT ATTENDANT STATED THAT A VERY LOUD NOISE WAS COMING FROM THE MAIN CABIN DOOR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN CABIN DOOR SEAL WAS BAD. MAINTENANCE REPLACED THE DOOR SEAL AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000602004041500060EA 2004 4 15 QXEA200400214 120040309A261247388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA FIRE WARNING FAULTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09617QX461 10130 DEN - FLIGHT 2165 - FIRE SYSTEM FAULT STATUS MESSAGE ON INTERMITTENTLY DURING CRUISE FLIGHT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE FIDEX CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000622004041500062EA 2004 4 15 QXEA200400219 120040314A261247388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA FIRE WARNING FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09617QX2582 2582 10130 BOI - FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED FIDEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000672004041500067EA 2004 4 15 QXEA200400211 120040311A2612 FIRE WARNING CNDAIRCL600 CL6002C10 1390015EA COCKPIT FALSE INDICATIONA QXEAO OTHER N FALSE WARNING ININSP/MAINT 1 NM09605QX 10022 BUR - FLIGHT 2555 - THE CREW RECEIVED AN INTERMITTENT FIRE WARNING FAULT STATUS MESSAGE. MAINTENANCE FOUND A MAINTENANCE DIAGNOSTIC COMPUTER FAULT: APU BOTTLE FAILED WIRING, LOW PRESSURE DETECTED. THE SYSTEM WAS PLACED ON MEL. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE APU FIRE EXTINGUISHER CONTAINER PRESSURE GAUGE, AND PERFORMED AN EXTINGUISHER WEIGHT CHECK. ALL CHECKS WERE GOOD. NO DISCREPANCIES NOTED. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415000682004041500068 2004 4 15 QXEA200400226 420040320A3442MI5853512 INDICATOR DHAV DHC8 DHC8202 2809007NM WEATHER RADAR DEFECTIVE A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NM09375PH6176 6176 529 SEA - ON FLIGHT 2195 DURING APPROACH, AN ELECTRICAL SMELL WAS NOTICED. WHEN ENGINES WERE SHUT DOWN, THE WEATHER RADAR WAS EMITTING A SIZZLING NOISE. REMOVED AND REPLACED RADAR INDICATION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415000702004041500070WP 2004 4 15 ASAA0480050 120040127A32115935812519 TRUNNION DOUG DC9 DC983 3022083WP LT MLG GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT MLG FORWARD TRUNNION FITTING IS GOUGED ON LOWER SIDE. REMOVED DAMAGE, PERFORMED HFEC, FLAP PEEN, AND TREATED AND PRIMED AREA PER EA5740-01373. (M) 2L72 4F RTA6WE 20040415000942004041500094WP 2004 4 15 ASAA0480174 120040311A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS492972995 53021 SEA LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040415000982004041500098WP 2004 4 15 ASAA0480045 120040127A532199366403 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED AT FS 886-927. REPLACED FLOOR PANEL PER SRM 51-01. (M) 2L72 4F RTA6WE 20040415001012004041500101WP 2004 4 15 ASAA0480083 120040221A532059360264 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT CARGO BAY DOOR BEAM INTERCOSTAL IS CORRODED AT FS 1165. REPLACED INTERCOSTAL PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040415001022004041500102WP 2004 4 15 ASAA0480175 120040309A532199366481 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL IS GOUGED AND DELAMINATED AT FS 1156-1250. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001092004041500109WP 2004 4 15 ASAA0480101 120040224A532199365461 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE DELAMINATED AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040415001212004041500121NM 2004 4 15 QXEA200400183 120040229A3020 HEATER BOMBDRDHC8 DHC8401 1390041NM NR 1 & 2 ENGINE MALFUNCTIONED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09400QX 4030 SEA - FLIGHT 2328 ENGINE ADAPT HEATER 1 CAUTION LIGHT ILLUMINATED. ENGINE INTAKE HEATER ON NR 1 SIDE (LIGHT) WENT DARK. COMPLIED WITH OPERATIONAL CHECK OF NR 1 AND 2 ENGINE INTAKE HEATERS IAW 400 MM-30-21-00 CHECKS GOOD. RESET CIRCUIT BREAKER. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001272004041500127EA 2004 4 15 QXEA200400193 120040307A2820T99A38601 EJECTOR CNDAIRCL600 CL6002C10 1390015EA FUEL TANK LEAKING A QXEAO OTHER J WARNING INDICATION UKUNKNOWN 1 NM09614QX3233 3233 10049 PDX - FLIGHT 2555 - CREW NOTED THE CENTER TANK FILLING WITH FUEL. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEM AND FOUND THE LEFT PRIMARY EJECTOR BAD. THE LEFT PRIMARY EJECTOR WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040415001452004041500145NM 2004 4 15 SWAA040981 120040402A575366232363 BOLT BOEING737 7373G7 1384595NM FLAP ROLLER BROKEN A SWAAK NONE O OTHER UKUNKNOWN 1 SW29690SW 23783 LT WING T/E FLAPS DO NOT RETRACT TO FULL UP POSITION. REMOVED AND REPLACED LT WING T/E FT INBOARD MID FLAP ROLLER ASSY BOLT. 2L72 4F RTA16WE 20040415001552004041500155NM 2004 4 15 SWAA040979 120040403A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 947, LBL 55.5, CRACKED. REPAIRED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040415001582004041500158NM 2004 4 15 SWAA040983 120040404A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND LT AND RT KEEL BEAM AT BS 767 TO BS 773, RT KEEL BS 727 + 13, AND RT BS 500D TO BS 540, CORRODED. REPAIRED KEEL BEAM PER ER. 2L72 4F RTA16WE 20040415001652004041500165NM 2004 4 15 QXEA200400217 120040314A3040 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM COCKPIT FALSE ACTIVATIONA QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09407QX 4049 GEG - ON FLIGHT NUMBER 2338, WINDSHIELD HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST. NO FAULTS IN CDS. INSPECTED TERMINALS ON PILOT & F/O'S WINDSHIELDS. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF PILOT WINDSHIELD ANTI ICE SYSTEM. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001702004041500170NE 2004 4 15 QXEA200400253 220040330A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE DAMAGED A QXEAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 NM09600QX5781 10005 GEE965221 TUS FLIGHT 2505 RETURN TO FIELD: NR 1 ENGINE VIBRATION 2.4 MILS. MAINTENANCE REPLACED FAN BLADES IHI1387N, IHI1392N, IHI1399N, IHI1429N, IHI1495N, IHI1501N, IHI1683N, IHI1693N, INI1702N, IHI1735N, IHI1737N IHI1739N, IHI1741N, IHI1744N, IHI1745N, IHI1747N, IHI1748N, IHI1751N, IHI1752N, IHI1754N, IHI1758N, IHI2178N, IHI2192N, IHI2193N, IHI2778N, IHI2874N, IHI3774N, IHI5186N. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040415001802004041500180NM 2004 4 15 QXEA200400264 120040409A33506138001 POWER SUPPLY BOMBDRDHC8 DHC8401 1390041NM CABIN DISCHARGED A QXEAK NONE L NO TEST UKUNKNOWN 1 NM09413QX5305 1443 4060 SEA - BOTH AFT OUTSIDE AND BOTH AFT EXIT DOOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED AFT LEFT HAND EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001832004041500183NM 2004 4 15 QXEA200400245 120040327A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAILED A QXEAK NONE O OTHER UKUNKNOWN 1 NM09353PH217956772 496 SEA - ON FLIGHT 2178 BAGGAGE SMOKE WARNING TEST 1 FAILED. REMOVED AND REPLACED AFT BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040415001882004041500188 2004 4 15 QXEA200400247 420040325A3418 STALL WARNING BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09414QX 4061 PDX - ON FLIGHT 2400 PUSHER SYSTEM FAIL CAUTION LIGHT ILLUMINATED ON TAXI IN. RAN ABNORMAL CHECKLIST, LIGHT STAYS ILLUMINATED. COMPLETED STALL TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040416000082004041600008NE 2004 4 16 QXEA200400239 220040324A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 ENGINE LACK OF LUBE A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09601QX4945 10009 GEE965316 DEN FLIGHT 4182 RETURN TO FIELD, NR 1 ENGINE VIBRATION. MAINTENANCE REPLACED FAN BLADES SERIAL NUMBERS IHI7274N, IHI7276N, IHI7280N, IHI7281N, IHI7289N, IHI7291N, IHI7297N, IHI7298N, IHI7302N, IHI7303N. OPERAITONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040416000112004041600011 2004 4 16 GAIA04030OP 420040218A22102588880901 COUPLER BOEING727 727224 1384076NM YAW DAMPER DAMAGED A GAIAO OTHER N FALSE WARNING CLCLIMB 1 SW0769739 20667 DURING TAXI, THE UPPER YAW DAMPER WAS CAUSING THE RUDDER TO SWING SIDE TO SIDE CAUSING VIBRATION. REMOVED AND REPLACED THE UPPER YAW DAMPER COUPLER. OPERATIONAL CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000592004041900059EA 2004 4 19 ASOA04101 120040208A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11847AS 7335 FLT 4382 - DURING A GROUND INSPECTION IN MGM, AN EMERGENCY CELING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040419000602004041900060CE 2004 4 19 2004F00099 120040206A324140911 TRANSDUCER LEAR 35 35A 5170602CE ANTI SKID SYS MALFUNCTIONED A DELAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 CE03360LJ 360 CREW REPORTED ERRATIC BRAKING WITH ANTI-SKID SYSTEM ENGAGED. FURTHER INVESTIGATION FOUND THAT THE ANTI-SKID 'OFF' LIGHTS WOULD FAIL TO COME ON AND WOULD NOT RESET. AN ELECTRICAL CONNECTOR ON THE ANTI-SKID INDICATION PANEL WAS FOUND LOOSE AND WAS REPAIRED. ALSO, THE NR 1 WHEEL SPEED TRANSDUCER HAD LOW RESISTANCE DURING FUNCTIONAL TESTING. THE LEFT OUTBOARD WHEEL SPEED TRANSDUCER WAS REMOVED AND REPLACED WITH AN OVERHAULED UNIT. (M) 2L72 4F A10CE 20040419000612004041900061NM 2004 4 19 GTIA040151 120040226A2797 WIRE DOUG MD80 MD83 3023681NM FLAP TO ELEVATORBROKEN A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23828NK 49823 FLL - FLT 262 - AFTER TAKEOFF RETRACTED SLATS, GOT DISAGREE LIGHT. CONFIRMED SLATS DEPLOYED AT 280 KTS OVERSPEED WARNING. ALSO AT LANDING, INDICATIONS WERE 40/40 AND TAKEOFF, GPWS WENT OFF. FOUND FLAP BUSS TO ELEVATOR SERVO FORCE LIMITER CABLE BROKEN. REMOVED AND REPLACED CABLE RUN 208B. (M) 2L72 4F RT 20040419000682004041900068NM 2004 4 19 GAIA04035BOP 120040225A2612 FIRE LOOP BOEING727 727251 138408HNM NR 3 ENGINE OUT OF ADJUST A GAIAK NONE N FALSE WARNING ININSP/MAINT 1 SW07279US 21158 FLT 875 - FWA-LAX - DURING PREFLIGHT, ENGINE NR 3 FIRE PROTECTION GROUND FAULT LIGHT REMAINS ILLUMINATED. ADJUSTED NR 3 ENGINE FIRE LOOP. CLOSED NR 3 COWL. NR 3 GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000692004041900069NM 2004 4 19 USAA040028 120040224A5240 DOOR FRAME BOEING737 7374B7 1384702NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU36522 25021 PIT- FOUND FRAME CRACKED 1 INCH, LOWER AFT CORNER FRAME FORWARD SERVICE DOOR. SPLCIED IN NEW SECTION PER SRM 51-70-11 DETAIL II. (M) 2L72 4F RTA16WE 20040419000712004041900071EA 2004 4 19 ASOA04207 120040313A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11836AS 7263 FLT 4324 - DURING A GROUND INSPECTION IN DFW, AN EMERGENCY CEILING LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040419000722004041900072EA 2004 4 19 ASOA04208 120040313A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040419000752004041900075EU 2004 4 19 ASOA04100 120040208A3397MS2275941249 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11637AS 383 DURING A HANGAR INSPECTION MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040419000772004041900077NM 2004 4 19 GAIA04035AOP 120040224A2612 FIRE LOOP BOEING727 727251 138408HNM NR 3 ENGINE MALFUNCTIONED A GAIAK NONE N FALSE WARNING ININSP/MAINT 1 SW07279US 21158 FLT 875 - FWA-LAX - DURING PREFLIGHT, ENGINE NR 3 FIRE PROTECTION GROUND FAULT LIGHT REMAINS ILLUMINATED. (M) 2L73 4F A3WE 20040419000852004041900085WP 2004 4 19 ASAA0480181 120040310A5311993607315 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND FRAME IS CORRODED AT FS 1211. REPLACED FRAME PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040419000862004041900086WP 2004 4 19 ASAA0480106 120040224A53219936581 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL EDGE SEAL MISSING FS 1007-1079. RESEALED PER DPS 1.901 AND DWG 9936584. (M) 2L72 4F RTA6WE 20040419000892004041900089WP 2004 4 19 ASAA0480103 120040224A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND SEAT TRACK IS CORRODED AT FS 236-313. REPLACED DAMAGED SECTION PER SRM 51-30-1 AND 51-30-5. (M) 2L72 4F RTA6WE 20040419000912004041900091WP 2004 4 19 ASAA0480183 120040309A53219957918502 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD IS CRACKED AND DELAMINATED AT FS 927-1003. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000932004041900093WP 2004 4 19 ASAA0480182 120040310A71205935710501 YOKE DOUG DC9 DC983 3022083WP ENGINE MOUNT DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND RIGHT ENGINE MOUNT YOKE UPPER ISOLATOR CAVITY CAD PLATING IS MISSING. REPLACED MOUNT YOKE PER MM 71-20-03. (M) 2L72 4F RTA6WE 20040419000982004041900098WP 2004 4 19 ASAA0480095 120040222A53219936640501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE SEALANT MISSING AT FS 864-886. RESEALED EFFECTED AREAS. (M) 2L72 4F RTA6WE 20040419000992004041900099WP 2004 4 19 ASAA0480097 120040222A532199365451 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001002004041900100WP 2004 4 19 ASAA0480096 120040222A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS EDGE SEALANT MISSING AT FS 826-864. RESEALED EFFECTED AREAS. (M) 2L72 4F RTA6WE 20040419001012004041900101WP 2004 4 19 ASAA0480046 120040127A53219936651519 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED AT FS 1041. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001042004041900104WP 2004 4 19 ASAA0480084 120040221A5320993658087 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR INTERCOSTAL CRACKED AND BENT AT FS 1045. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040419001052004041900105WP 2004 4 19 ASAA0480171 120040307A532199365511 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS SEVERAL DELAMINATED AREAS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001072004041900107WP 2004 4 19 ASAA0480164 120040307A53219936640501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND CABIN FLOOR PANEL HAS DELAMINATED AREAS AT FS 864-886. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001102004041900110WP 2004 4 19 ASAA0480157 120040302A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD STATION 200-256 X=14-X=22 HAS SEVERAL CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040419001112004041900111WP 2004 4 19 ASAA0480137 120040229A554259555313 SKIN DOUG DC9 DC983 3022083WP RUDDER WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND RUDDER LOWER HINGE SKIN HAS WORN ASTRO STRIKE. REPLACED ASTRO STRIKE PER SRM 51-70-1A. (M) 2L72 4F RTA6WE 20040419001182004041900118NM 2004 4 19 DHL2004750018 120040225A5754 FRAME BOEING727 7272M7 138407SNM SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, NR 3 SLAT AT ACT ROD END HAS OUTBOARD ATTACH FRAME IS CRACKED IN AFT RADIUS. REMOVED AND REPLACED NR 3 SLAT AT ACT ROD AND OUTBOARD ATTACH FRAME AFT 2 EA RIB SUPPORT PO 4136-27 P/N 65-17294-13 AND PO 413643 P/N 65-17294-14 IAW B727 SRM 51-30-2. ACCOMPLISHED SLATS OP'S CHECK, FOUND OK IAW B727 MM 27-81-0. 2L73 4F A3WE 20040419001192004041900119NM 2004 4 19 DHL2004750039 120040302A5320 WEB BOEING727 7272M7 138407SNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LWR VERTICLE LEADING EDGE LWR INTERNAL WEB CRACKS OUT AROUND BOLT FIN STA 55.9. REMOVED DAMAGED WEB AND FABBED NEW FROM 2024-T3 .032 PO 900534 DIM 12.75 X 12 INCH IAW 727 SRM 55-30-2 FIG 2. WEB TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-30-2. 2L73 4F A3WE 20040419001222004041900122NM 2004 4 19 DHL2004750040 120040307A5313 STRINGER BOEING727 7272M7 138407SNM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, STRINGER 19L CORRODED AT BS 720D & 10. REMOVED FASTENERS FOR ACCESS IAW 727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF STRINGER AND FABBED FILLER FROM BAC 1498-144 PO 3357 92 DIM 3.5 INCH SPLICE FROM BAC 1498-125 PO 335792 DIM 15.125 IAW 727 SRM 53-10-2 FIG 9 & 53-10-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20040419001232004041900123NM 2004 4 19 DHL2004750013 120040229A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 1130 ABOVE STR 26L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B-727-SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA SIZE 2 X 1.75 INCH AND FABRICATED DOUBLER FROM 2024-T3 .071 PO 900484 DIM 10 X 8.5 INCH STRUCTURAL FILLER FROM 2024-T3 .063 PO 900606 DIM 10 X 1.125 INCH IAW B-727-SRM 53-30-3 FIG 14. TREATED AND PRIMED PART AND AREA IAW B-727-SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B-727-SRM 53-30-3 FIG 14. 2L73 4F A3WE 20040419001282004041900128EA 2004 4 19 COMA0460255 120040413A7830864808 PSEU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01912CA1791 7011 FLIGHT 5728 RIGHT REVERSER UNSAFE CAUTION MESSAGE. REPLACED THE PSEU. 2L72 4F RTA21EA 20040419001292004041900129EA 2004 4 19 COMA0460256 120040413A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01495CA 7774 FLIGHT 5333 LEFT ANTI-ICE DUCT WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECK OF NORMAL AND STANDBY SYSTEM WAS SATISFACTORY. 2L72 4F RTA21EA 20040419001302004041900130EU 2004 4 19 DHL2004362002 120040405A3242 SERVO VALVE AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO01362DH 84 AFTER LANDING THE TOWER REPORTED SMOKE COMING FROM RIGHT MAIN GEAR. BRAKE TEMPERATURES WERE NORMAL, TILLER OPERATED NORMAL DURING TAXI. REMOVED AND REPLACED NR 8 TIRE SERVO VALVE, BRAKE ANTI-SKID & AUTO BRAKE CONTROL UNIT IAW M/M 32-42-48; M/M 32-42-72. ALSO DID WIRING CHECK PER M/M 32-42-12. CHECKED NORMAL. REMOVED AND REPLACED NR 7 TIRE ASSEMBLY DUE TO NR 8 TIRE FAILED ON LANDING. REMOVED AND REPLACED NR 7 MAIN LANDING GEAR TIRE ASSEMBLY PER A300 M/M12-37-32. CHECKED GOOD. NR 8 TIRE FAILED ON LANDING. REMOVED AND REPLACED NR 8 MAIN WHEEL TIRE ASSEMBLY IAW M/M 12-31-32 & CHECKED OK. 2L72 4F RTA35EU 20040419001342004041900134EA 2004 4 19 COMA0460221 120040328A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01818CA 7408 FLIGHT 5851 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040419001372004041900137EA 2004 4 19 COMA0460224 120040324A7110 COWLING CNDAIRCL600 CL6002B19 1900309EA RT ENGINE SEPARATED A COMAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO01781CA 7312 FLIGHT 5892 RT ENGINE COWLING SEPARATED FROM AIRCRAFT AFTER T/O. REPAIRED AND REPLACED ENGINE COWLING. 2L72 4F RTA21EA 20040419001392004041900139NM 2004 4 19 DHL2004750011 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 580. CUT OUT DAMAGED AREA 1 X .75 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .063 PO 900489 DIM 8 X 3.75 INCH IAW 727 SRM 53-10-2 FIG 1 & 51-40-3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-40-3. 2L73 4F A3WE 20040419001402004041900140NM 2004 4 19 DHL2004750012 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 560. CUT OUT DAMAGE AREA SIZE .5 X 1 INCH ON UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME BS 560 IAW B727 SRM 51-10-1. FABRICATED, REPAIR ANGLE FROM 7075T6 .063 SIDE 4.5 X 6 INCH PO 900166 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040419001452004041900145NM 2004 4 19 SWAA041051 120040413A573065C26279 SKIN BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING L/E SKIN AT WS 213, CRACKED. REPAIRED L/E SKIN PER ER. 2L72 4F RTA16WE 20040419001462004041900146NM 2004 4 19 SWAA041052 120040413A55536546872 FITTING BOEING737 7373H4 1384600NM TAIL CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB AFT SPAR RIGHT AND LEFT PRIMARY CLEVIS AFT LUGS, CORRODED. REPAIRED VERTICAL STAB LUGS PER ER. 2L72 4F RTA16WE 20040419001482004041900148NM 2004 4 19 SWAA041054 120040413A3350OL3071BPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29764SW 27878 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 3 DEF, INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040419001492004041900149NM 2004 4 19 SWAA041030 120040409A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN BEHIND LT WING TO BODY FAIRING AT BS 767, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419001502004041900150 2004 4 19 SWAA041031 420040410A2565 INDICATOR BOEING737 7372H4 138448CNM R1 DOOR SLIDE OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 19626780 23053 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040419001512004041900151NM 2004 4 19 SWAA041032 120040410A5311BAC1518 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 663, STRINGER 2L, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040419001532004041900153NM 2004 4 19 SWAA041034 120040410A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 500 + 2, STRINGER 12R, AND BS 500D + 18, STRINGER 12L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419001542004041900154NM 2004 4 19 DHL2004750022 120040229A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 1273 BELOW STR 14L. CUT OUT DAMAGED AREA DIM 1.875 X 1.25 INCH AND FABRICATED DOUBLER, MAT ID 2024T3 .071 PO 900484 DIM 8.25 X 10.875 IAW B727 SRM 53-30-3, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER ON LEFT FUSELAGE AT BS 1273 BELOW STR 14L IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040419001552004041900155NM 2004 4 19 SWAA041035 120040410A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419001572004041900157NM 2004 4 19 SWAA041038 120040410A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB FROM BS 328 TO BS 344, RBL 65, WL 208, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040419001582004041900158NM 2004 4 19 SWAA041039 120040411A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND CABIN FLOORBEAM AT BS 896, LBL 17 TO RBL 44, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040419001602004041900160EA 2004 4 19 COMA0460238 120040331A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA 3A UNRELIABLE A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01473CA4940 7668 FLIGHT 5153 GEAR DISAGREE WARNING. REPLACED THE 3A ACMP. 2L72 4F RTA21EA 20040419001612004041900161 2004 4 19 SWAA041041 420040411A2565D31354 SLIDE BOEING737 7373L9 1384470NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040419001652004041900165NM 2004 4 19 SWAA041043 120040412A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D + 6, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040419001692004041900169NM 2004 4 19 SWAA041048 120040412A335010107451 SIGN BOEING737 7373G7 1384595NM LT OVERWING LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EXIT SIGN LOOSE. SECURED LT OVERWING EXIT SIGN PER MM. 2L72 4F RTA16WE 20040419001702004041900170 2004 4 19 SWAA041049 420040412A25656949956 CABLE BOEING737 7373G7 1384595NM ESCAPE SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES GIRT CABLES MISROUTED. REROUTED EVAC SLIDES GIRT CABLES PER MM. 2L72 4F RTA16WE 20040419001752004041900175NM 2004 4 19 DHL2004750016 120040229A5210 SKIN BOEING727 7272M7 138407SNM L2 DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LEFT L2 DOOR HAS DENT BS 1050 STR 16L. REMOVED DAMAGE, CUTOUT IS .65 X .50 INCH IAW B727 SRM 52-00-3 FIG 3. FABRICATED DOUBLER FROM 2024T3 .063 PO 900606. DOUBLER IS .063, 6.5 X 7.2 INCH IAW B727 SRM 52-00-3 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 52-00-3 FIG 3. 2L73 4F A3WE 20040419001802004041900180NM 2004 4 19 2004UALA00307 120040403A2612 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO FIRE ILLUMINATED A UALAF ACTIVATE FIRE EXT. J WARNING INDICATION APAPPROACH 1 WP29177UA 24384 ON FINAL APPROACH FIRE CARGO AFT CAME ON. CREW USED ONE EXTINGUISHER BOTTLE. EMERGENCY EQUIPMENT STANDING BY. IN ADDITION TO THE "FIRE CARGO AFT" WARNING DURING DECENT, FLIGHT CREW OBSERVED STATUS MESSAGE "AFT CARGO 4 LP B". NRTMM FOUND STORED CMC FAIL MESSAGES FOR BOTH AFT CARGO 4 LP B AND AFT CARGO 3 LP A. FAILURES OF BOTH LOOP "A" AND "B" COULD ACCOUNT FOR FIRE CARGO AFT WARNING. GROUND INSPECTION FOUND NO EVIDENCE OF FIRE IN AFT CARGO PIT. 2L74 4F4 FRTA20WE E24NE 20040419001812004041900181EU 2004 4 19 MALA040321 120040405A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 4K INSPECTION, FS 272 FLOORBOARD SUPPORT ANGLE CORRODED. MX CUT OUT CORRODED AND DAMAGED AREA FABRICATED AND INSTALLED AN ANGLE REPAIR IAW MESABA EO S53102. A/C RELEASED 4/9/04. 2L72 4T RTA52EU 20040419001842004041900184NM 2004 4 19 SWAA041014 120040408A53306545770 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 737, STRINGER 20R, BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419001852004041900185NM 2004 4 19 SWAA041016 120040408A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND RT KEEL BEAM FLANGE BS 500D + 2, AND RT KEEL BEAM FLANGE BS 522, CORRODED. REPAIRED KEEL BEAM FLANGE PER EA. 2L72 4F RTA16WE 20040419001922004041900192NM 2004 4 19 SWAA041023 120040409A335007912 COVER BOEING737 7377H4 1384404NM ROW 1 ABC CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040419001932004041900193NM 2004 4 19 SWAA041024 120040409A3350101114 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20040419001962004041900196EU 2004 4 19 DHL2004364500 120040311A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN DECK COURIER AREA HAVE CORROSION EVIDENCE ON FLOOR PANEL SUPPORT/SEAT TRACK FROM APPROX FR 14 TO FR 15 RBL 0 TO RBL 20 (MARKED). REMOVED CORROSION FROM FR 14 TO FR 15 RBL 29, MAT LOSS .030, FOUND TO BE OUT OF LIMITS IAW A-300 SRM 53-10-00 FIG 612. REMOVED SEAT TRACK FROM FR 14 TO FR 19 RBL 20 IAW A-300 SRM 51-30-30. MATERIAL; USED P/N 60-22457 PO 23236312 TREATED, PRIMED AND POLYWHITE TRACK SECTION AS PER A-300 SRM 51-40-12. INSTALLED NEW SECTION OF SEAT TRACK IAW A-300 SRM 51-30-30 PAGE 8. 2L72 4F RTA35EU 20040419001972004041900197NM 2004 4 19 SWAA041027 120040409A531165C22908 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 500B, STRINGER 20L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040419001992004041900199NM 2004 4 19 SWAA041029 120040409A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT LT BS 907 TO LT BS 927, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER EA. 2L72 4F RTA16WE 20040419002062004041900206NM 2004 4 19 QXEA200400232 120040320A3040 HEATER BOMBDRDHC8 DHC8401 1390041NM WINDSHIELD MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09407QX4256 2856 802600 4049 SEA - FLIGHT NR 2326 RETURN TO FIELD, WINDSHIELD HOT & CAUTION ILLUMINATED. REPLACED FIRST OFFICER WINDSHIELD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040419002072004041900207NM 2004 4 19 SWAA040997 120040406A335007912 COVER BOEING737 7373T0 1384582NM EMERGENCY LIGHT BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29684WN 23941 RT FWD CABIN EEPLS COVER BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040419002082004041900208 2004 4 19 SWAA040998 420040406A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040419002092004041900209NM 2004 4 19 SWAA040999 120040406A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY PHOTOLUMINESCENT EXIT STRIP OUT OF POSITION. REPOSITIONED PHOTOLUMINESCENT EXIT STRIP PER MM. 2L72 4F RTA16WE 20040419002112004041900211EU 2004 4 19 MALA040309 120040328A5320 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 4K INSPECTION, FS 294 WEB CORRODED. REMOVED AND REPLACED WEB IAW SAAB 340 SRM 51-40. 2L72 4T RTA52EU 20040419002152004041900215EU 2004 4 19 MALA040320 120040408A242051634002 GCU SAAB SF340 340B 7860101EU AC GENERATOR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15402XJ 340B402 LEFT DC GEN CAUTION LIGHT ON INTERMITANTLY RESETS AFTER 10-15 SECONDS. AIR RETURN TO MSP. REMOVED AND REPLACED LEFT AC GEN GCU DUE TO DISCREPANCY IN COMMUNICATION WITH MXC/MX AND FLT CREW. P/N 51634-002, S/N OFF 97035, S/N ON 97031 IAW AMM 24-20-10-2. REMOVED AND REPLACED LEFT DC GCU IAW AMM 24-30-10 51539-007B, S/N OFF 98657 S/N ON 98114. OPS CHECKS GOOD. 2L72 4T RTA52EU 20040419002162004041900216EA 2004 4 19 COMA0460240 120040404A7720 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01721CA 7259 FLIGHT 5390 RIGHT ENGINE ITT OVERTEMP DURING T/O. COULD NOT DUPLICATE. GROUND RUN SATISFACTORY. NO DEFECT FOUND. 2L72 4F4 FRTA21EA E15NE 20040419002182004041900218 2004 4 19 COMA0460242 420040401A34326227194101 RECEIVER CNDAIRCL600 CL6002B19 1900309EA GLIDESLOPE MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01710CA10987 7241 FLIGHT 5837 COPILOTS GLIDESLOPE FLAG ON APPROACH. REPLACED THE NR 2 NAV RECEIVER. 2L72 4F RTA21EA 20040419002192004041900219NM 2004 4 19 DHL2004750009 120040222A5310 DOOR FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, DISCREPANCY AS FOLLOWS; C1 DOOR EXTERNAL HAS DENT IN BOTTOM CENTER OF DOOR U-CHANNEL. REMOVED DAMAGED ANGLE IAW B727 SRM 51-30-2, FABRICATED NEW ANGLE FROM BAC1496-383 PO 206631 DIM 44 X 2.75 INCH IAW B727 SRM 52-30-1, TREATED AND PRIMED ALL PARTS & AREA IAW B727 SRM 51-10-2. INSTALLED NEW ANGLE IAW B727 SRM 51-30-2, AT C1 DOOR, BOTTOM CENTER OF DOOR U-CHANNEL. 2L73 4F A3WE 20040419002202004041900220NM 2004 4 19 04FDEA00894 120040411A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD UPPER MOUNT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR 2L73 4F RTA22WE 20040419002242004041900224EU 2004 4 19 04FDEA00916 120040412A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 SEAT TRACK -0- [C/L] BETWEEN FRAMES 29-30 HAS CORROSION ON FLANGE NEAR FASTENER HOLE, MAIN CABIN FLOOR. REPAIRED SEAT TRACK AS PER A300-600 SRM 53-10-16 PG 210 FIG 202. 2L72 4F RTA35EU 20040420000012004042000001NM 2004 4 20 DHL2004755008 120040324A3260 WARNING LIGHT BOEING727 727225 1384077NM MLG DOORS ILLUMINATED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01755DH 21857 WHEN PLACING GEAR HANDLE FROM UP TO OFF FOLLOWING NORMAL GEAR RETRACTION FORWARD RED DOORS LIGHT ILLUMINATED WITH ASSOCIATED AMBER R GEAR DOOR LIGHT ON S/O'S PANEL. PERFORMED ABNORMAL PROCEDURE LIGHTS EXTINGUISHED WITH GEAR HANDLE IN UP POSITION. OPS CHECKED GEAR DOOR OPERATION AND INDICATION IAW B-M/M 32-62-00. NO DEFECTS NOTED. CHECKED GOOD. 2L73 4F A3WE 20040420000042004042000004EU 2004 4 20 04FDEA00918 120040412A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP CENTER SEAT AT CENTER LINE BETWEEN FRAME 74 TO 76, THREE EACH AREAS OF CORROSION ON UPPER SURFACE. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-16. CUT OUT SECTION OF SEAT TRACK .125 INCH LONG, FABRICATED AND INSTALLED REPLACEMENT SECTION PER SRM 53-10-16 AND 51-40-21. 2L72 4F RTA35EU 20040420000062004042000006NM 2004 4 20 QXEA200400259 120040407A5410 TRUSS DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - NR 1 ENGINE INBOARD UPPER TRUSS IS CHAFED. REPAIRED IAW DHC-8 RD 8-54-036, STEP 3. 2H72 4T RTA13NM 20040420000072004042000007EU 2004 4 20 04FDEA00920 120040412A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP RT SIDE NR 5 SEAT TRACK BETWEEN FR 24 AND 25 HAS TWO AREAS OF CORROSION UPPER SURFACE. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 PG 210 FIG 202, TREATED AREA AS PER A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20040420000112004042000011EA 2004 4 20 QXEA200400265 120040411A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA LT ENGINE LEAKING A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09609QX2692 1007 10031 DEN - FLIGHT 4339 - AT FL 330, THE CREW RECEIVED A MASTER CAUTION HYDRAULIC 1 LO PRESSURE AND ASSOCIATED OUTBOARD GROUND SPOILER, OUTBOARD SPOILERONS, AND OUTBOARD FLIGHT SPOILER MESSAGES. QUANTITY AND TEMPERATURE WERE GOOD BUT THE PRESSURE WAS DROPPING. ON THE LANDING FLARE THE CREW LOST NR 1 SYSTEM PRESSURE AND QUANTITY. THE ENGINE WAS SECURED. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NR 1 ENGINE DRIVEN PUMP, THE NR 1 HYDRAULIC SYSTEM PRESSURE FILTER, AND THE FORE AND AFT CASE DRAIN FILTERS. THE OPERATIONAL CHECKS AND THE LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040420000142004042000014NM 2004 4 20 2004UALA00308 120040405A2420 STATIC INVERTER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FWD E/E BAY OVERHEATED A UALAK NONE MABOVER TEMP FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29573UA 26685 STATIC INVERTER OVER-TEMPED IN FORWARD LOWER NOSE COMPARTMENT. STATIC INVERTER WAS REMOVED AND REPLACED. REMOVED UNIT SHIPPED TO MANUFACTURER TO DETERMINE ROOT CAUSE OF FAILURE. 2L72 4F4 FRTA2NM E17NE 20040420000162004042000016EA 2004 4 20 QXEA200400230 120040322A2710CC6710511143 TRIM PANEL CNDAIRCL600 CL6002C10 1390015EA COCKCPIT FAILED A QXEAO OTHER S AFFECT SYSTEMS CRCRUISE 1 NM09604QX5450 10019 SEA - FLIGHT 2181 - THE CREW REPORTED THAT THE AILERON TRIM WILL NOT TRIM OR MOVE TOWARDS RIGHT WING DOWN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER TRIM PANEL. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040420000172004042000017NM 2004 4 20 2004UALA00309 120040405A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME INNER FLANGE STA 1480 STR 25L HAS DENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR SPLICE. 2L72 4F4 FRTA2NM E17NE 20040420000202004042000020NM 2004 4 20 2004UALA00312 120040405A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 MAIN CABIN AT STA 294 STR 7R DOOR JAMB CORNER CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20040420000232004042000023EU 2004 4 20 2004UALA00315 120040407A5712 RIB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT WING DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29426UA 510 LEFT WING RIB 5 FITTING INBOARD REAR SPAR FASTENER 4 FROM THE TOP, NUT SHEARED OFF. BOLT LIKELY SHEARED AT THE TIME OF INSTALLATION. NO DAMAGE TO ADJACENT FASTENERS, FASTENER HOLES OR FITTING COMMON TO PROBLEM HOLE WAS NOTED INDICATING THAT SHEARING DID NOT OCCUR DUE TO OVERLOADING OF BOLT VIA GROUND OR FLIGHT LOADS. FASTENER WAS REPLACED WITH NEW OVERSIZE FASTENER AFTER ROUTINE ACCOMPLISHMENT OF COLD-WORKING. 2L72 4F4 FRTA28NM E40NE 20040420000242004042000024NM 2004 4 20 2004UALA00316 120040407A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG WW CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 WHEEL WELL PRESSURE DECK IS CRACKED AT STA 664 AND LBL 32. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20040420000252004042000025NM 2004 4 20 2004UALA00317 120040407A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 FLOORBEAM T-CAP AT STA 1640 RBL 60 IS CORRODED. REMOVED T-CAP. FABRICATED AND INSTALLED NEW T-CAP AND ANGLE. 2L72 4F4 FRTA2NM E17NE 20040420000272004042000027 2004 4 20 2004UALA00320 420040326A2330 POWER SUPPLY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE PROJECTOR OVERHEATED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29667UA 29239 ELECTRICAL ODOR IN PROJECTOR. REPLACED PROJECTOR. POWER SUPPLY OVERHEATED 2L72 4F4 FRTA1NM E24NE 20040420000322004042000032NM 2004 4 20 04FDEA00895 120040411A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD UPPER MOUNT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WINGS OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000332004042000033NM 2004 4 20 04FDEA00896 120040411A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, BARREL NUT BOLT HOLE AREA SPOT FACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76656, WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000342004042000034NM 2004 4 20 04FDEA00897 120040411A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD ACTUATOR BORE HOLE FOUND CORRODED. 2L73 4F RTA22WE 20040420000362004042000036NM 2004 4 20 04FDEA00909 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE INNER AND OUTER SURFACE OF I/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011, SUPPORT BRACKET CORROSION REMOVAL & REPAIR. 2L73 4F RTA22WE 20040420000372004042000037NM 2004 4 20 04FDEA00910 120040412A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT AFT O/B FLAP, I/B HINGE O/B PIVOT HOLE FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA 1-5750-76011. 2L73 4F RTA22WE 20040420000402004042000040EA 2004 4 20 COMA0460244 120040404A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01458CA15625 7613 FLIGHT 5123 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040420000412004042000041EA 2004 4 20 COMA0460245 120040407A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01518CA2242 7816 FLIGHT 5749 DURING GEAR RETRACTION, MLG CYCLED BETWEEN UP AND INTRANSIT. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20040415001162004041500116EA 2004 4 15 A6WA20034A 120040106A2721272613 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL31433AW8920 7289 RUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M) 2L72 4F RTA21EA 20040415001322004041500132NM 2004 4 15 SWAA040988 120040404A53116546561 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FRAME WEBS AT BS 951, STRINGER 11R AND STRINGER 10L, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040415001342004041500134CE 2004 4 15 GLBA20030545 120040128A2150 WARNING LIGHT BEECH 1900 1900D 1154162CE RT ENVIRO SYS ILLUMINATED A GLBAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM03170GL UE170 RT ENVIRO FAIL ANNC ILLUM, GROUND RAN ACFT AT FULL PWR SETTING WITH RAPID POWER ADVANCES AND ACCELERATION COULD NOT GET RT ENVIRO FULL OPS CK GOOD. 2L72 4T RTA24CE 20040415001432004041500143NM 2004 4 15 SWAA040995 120040405A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT SKIN AT BS 727 + 14, LBL 9, STRINGER 27L, CORRODED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040415001462004041500146NM 2004 4 15 SWAA040970 120040402A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 425, BS 452, STRINGER 16R, AND BS 390, STRINGER 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040415001472004041500147NM 2004 4 15 SWAA040971 120040401A53156935371 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM WEB AT BS 967, LBL 5, WL 208, CORRODED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040415001522004041500152NM 2004 4 15 SWAA040976 120040402A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 867, RT AFT CARGO COMPARTMENT TRACK TO FRAME CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040415001672004041500167NE 2004 4 15 QXEA200400222 220040315A7230 VALVE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 & 2 ENGINE MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09345PH 476 PCEAG0097 PDX - FLIGHT 2166 BURNING OIL SMELL REPORTED IN CABIN BY TWO CREW MEMBERS DURING DESCENT. NO VISIBLE SMOKE REPORTED. ALL INDICATIONS IN COCKPIT NORMAL. REPLACED NR 1 AND NR 2 ENGINE P2.5/P3 SWITCHING VALVE PER P&W MM 72-30-00. GROUND RAN AIRCRAFT AT VARIOUS POWER SETTINGS. NO DEFECTS NOTED AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040415001812004041500181NM 2004 4 15 QXEA200400251 120040327A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 PDX - NACELLE SKIN DAMAGE AT LOWER COWL HINGE POINTS. REPAIRED IAW HORIZON AIR EA 6-54-288A. 2H72 4T RTA13NM 20040415001842004041500184NM 2004 4 15 QXEA200400228 120040318A5720 ATTACH BRACKET BOMBDRDHC8 DHC8401 1390041NM RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - RIGHT HAND INBOARD WING TRAILING EDGE SUPPORT U-CHANNEL ATTACH ANGLE CRACKED AT WS YX135.25. REPAIRED IAW RD 8/4-57-177. 2H72 4T RTA13NM 20040415001892004041500189EA 2004 4 15 QXEA200400248 120040324A5210 ROLLER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR LACK OF LUBE A QXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09615QX 10065 BOI - ON FLIGHT 2544 PASSENGER DOOR IS HARD TO OPEN. CLEANED AND LUBED DOOR OPEN LEVER ROLLER AND REMOVED ICE FROM DOOR SILL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040416000262004041600026 2004 4 16 GAIA04020OP 420040129A22112585804 COMPUTER BOEING727 727214 138407RNM AUTOPILOT MALFUNCTIONED A GAIAO OTHER J WARNING INDICATION CRCRUISE 1 SW07750US 21512 DURING CRUISE, THE AIRCRAFT PITCHES UP AND DOWN WITH THE AUTOPILOT IN B-MODE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. OPS CHECK GOOD. AIRCRAFT WAR RELEASED FOR SERVICE. (M) 2L73 4F A3WE 20040416000292004041600029EU 2004 4 16 ASOA04089 120040204A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11634AS 370 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE PASSENGER DOOR EMEREGNCY LIGHT SOCKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040419000092004041900009WP 2004 4 19 ASAA0480028 120040122A33501001191 LIGHT DOUG DC9 DC983 3022083WP PAX CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS2618 2618 53076 OAK - DURING LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040419000302004041900030WP 2004 4 19 ASAA0480019 120040120A53219936582503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS SHREDDING AT FS 946-1003. REPLACED CHANNEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000512004041900051NM 2004 4 19 USAA040030 120040227A5312 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45084 23559 PIT - FOUND REAR PRESS BULKHEAD CORRODED 2 INCHES BY 4 INCHES, STATION 1016 BL 0 REAR PRESSURE BULKHEAD. CORRODED SECTIONS REPLACED PER EO 5302V112. (M) 2L72 4F RTA16WE 20040419000522004041900052NM 2004 4 19 USAA040029 120040228A5311 FRAME BOEING737 7373B7 1384580NM BULKHEAD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU47562 23857 PIT - FOUND FRAME CORRODED 6 INCHES BY 4 INCHES, BLO '0' AT Y FRAME STATION 1016 AT 6 O'CLOCK. Y FRAME LOWER LEGS AND WEB SKIN DOUBELR EPR EO 5302V112 AND SRM 51-20-01. (M) 2L72 4F RTA16WE 20040419000552004041900055NM 2004 4 19 GAIA04038OP 120040225A3350 LIGHT BOEING727 727223 1384074NM L1 DOOR INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07856AA 20997 ON POST FLIGHT INSPECTION, FOUND THE L1 EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000562004041900056NM 2004 4 19 GAIA04039OP 120040225A3210656021136 ACCESSORY UNIT BOEING727 727223 1384074NM E/E BAY INOPERATIVE A GAIAO OTHER J WARNING INDICATION DEDESCENT 1 SW07856AA 20997 FLT 211 - STL-FWA - ON DESCENT, THE AUTO PILOT DISENGAGED AND ALL INDICATOR TEST LIGHT ILLUMINATED. THE GEAR HANDLE WAS PLACED UP THEN OFF AND THE LIGHTS WENT BACK TO NORMAL. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040419000642004041900064NM 2004 4 19 USAASB04028 120040311A3397 WIRE BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19573US 23560 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ON BULLNOSE AT SEAT ROW 6, RIGHT SIDE INOPERATIVE. MAINTENANCE REPAIRED WIRING AT D2912 AND REPLACED BLOWN FUSE, P/N 21031-0005, IN POWER SUPPLY M1135. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040419000652004041900065NM 2004 4 19 USAASB04029 120040312A33501012623 SIGN BOEING737 7374B7 1384702NM EMERGENCY EXIT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19449US 24893 PIT - MAINTENANCE REPORTED THE AFT LEFT OVERWING EMERGENCY EXIT SIGN/LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040419000662004041900066NM 2004 4 19 USAASB04026 120040310A3350606171 SOCKET BOEING737 7373B7 1384580NM ROW 7 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU 23705 PIT - FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 7 INOPERATIVE. MAINTENANCE REPLACED THE SOCKET. (M) 2L72 4F RTA16WE 20040419000702004041900070NM 2004 4 19 USAA040027 120040224A5240 FITTING BOEING737 7374B7 1384702NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU36522 25021 PIT - FOUND FITTING CRACKED 1 INCH, LOWER AFT CORNER FITTING OF FORWARD SERVICE DOOR. REPLACED FITTING WITH MANUFACTURED FITTING PER SRM 51-70-11. (M) 2L72 4F RTA16WE 20040419000802004041900080WP 2004 4 19 ASAA0480098 120040224A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6-CHECK, FOUND CABIN FLOOR PANEL HAS MISSING EDGE SEAL AT FS 886-905. RESEALED PANEL PER DPS 1.901 AND DWG 9936584. (M) 2L72 4F RTA6WE 20040419000922004041900092WP 2004 4 19 ASAA0480102 120040224A532199365471 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL CORNER IS DELAMINATED AT FS 160-180. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000952004041900095WP 2004 4 19 ASAA0480178 120040310A531359364311 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND LONGERON 28L IS CORRODED AT FS 1231. REMOVED DAMAGED SECTION AND INSTALLED SPLICE PER SRM 53-02. (M) 2L72 4F RTA6WE 20040419001092004041900109WP 2004 4 19 ASAA0480158 120040302A532199365841 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - FOUND CABIN FLOORBOARD X=22 STATION 1117-1174 HAS GOUGES AND DELAMINATED EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040419001142004041900114EU 2004 4 19 DHL2004363005 120040412A3350312101 LIGHT AIRBUS300 A300B4203 3930306EU EXIT SIGN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01363DH 85 LF DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE ON TEST. REPLACED LIGHT ASSEMBLY AND POWER SUPPLY, OPS CHECKED GOOD IAW M/M 33-51-14 & 33-51-13. 2L72 4F RTA35EU 20040419001242004041900124NM 2004 4 19 QXEA200400258 120040405A5210 HANDLE BOMBDRDHC8 DHC8401 1390041NM PAX DOOR UNLATCHED A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09409QX 4051 GEG - FLIGHT 2387 - AIRCRAFT DIVERTED TO GEG WHEN AFTER TAKEOFF THE CREW RECEIVED AN AFT CARGO DOOR WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE CARGO DOOR HANDLE NOT LATCHED INTO THE RECESS. THE HANDLE WAS SECURED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040419001382004041900138EA 2004 4 19 COMA0460225 120040324A3150 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA RUDDER CONFIG ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01995CA 7229 FLIGHT 5158 RUDDER CONFIG WARNING DURING T/O. COULD NOT DUPLICATE. FOUND NO DEFECTS WITH CONFIG SYSTEM. 2L72 4F RTA21EA 20040419001522004041900152NM 2004 4 19 SWAA041033 120040410A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND 2 EACH BEAR STRAPS AT THE L1 DOOR UPPER AND LOWER HINGE CUTOUTS, CRACKED. REPAIRED BEAR STRAPS PER ER. 2L72 4F RTA16WE 20040419001662004041900166NM 2004 4 19 SWAA041045 120040412A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 360, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040419001762004041900176NM 2004 4 19 QXEA200400256 120040402A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM ZONE 100 STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH 484 PDX - PANELS 121AL, 121BL, 122BR, AND 122AR HAVE STRIPPED NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES AS REQUIRED IAW D-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040419002102004041900210 2004 4 19 SWAA041000 420040406A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE LOOSE. SECURED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040419002122004041900212EU 2004 4 19 MALA040323 120040405A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 4Y/2Y INSPECTION, CORROSION ON RIGHT I/B SEAT TRACK AT STA 294-295. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. A/C RELEASE DATE 4/9/04. 2L72 4T RTA52EU 20040419002142004041900214EU 2004 4 19 MALA040319 120040407A3240AE83011E SWIVEL SAAB SF340 340B 7860101EU BRAKE LINE LEAKING A MALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL15425XJ 340B425 LOST ALL HYDRAULIC FLUID DURING INITIAL DESCENT, LANDING GEAR EXTEND NORMALLY. ALL ACCUMULATORS HAD NORMAL PRESSURE; PERFORMED ZERO FLAP LANDING; NORMAL EXIT OFF RUNWAY (SANS NOSEWHEEL STEERING) TO GATE. FOUND RIGHT O/B BRAKE LINE SWIVEL LEAKING. REPLACED SWIVEL P/N AE83011E. ALL CHECKS GOOD SERVICED HYDRAULICS IAW AMM 12-10-29. 2L72 4T RTA52EU 20040420000032004042000003EU 2004 4 20 04FDEA00917 120040412A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP FLOOR, CENTER SEAT TRACK BETWEEN FRAME 66 AND 68, TWO EACH AREAS OF CORROSION. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. SPLICED IN NEW SECTION OF SEAT TRACK BETWEEN FRAMES 65.5 AND 68.5 IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040420000082004042000008EU 2004 4 20 04FDEA00921 120040412A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 SEAT TRACK AT C31 BETWEEN RIGHT NR 1 AND NR 2 SEAT TWO AREAS OF CORROSION. REMOVED DISCREPANT CLS ADAPTER AND REPLACED WITH NEW CLS ADAPTER IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040420000092004042000009EU 2004 4 20 04FDEA00922 120040412A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 SEAT TRACK AT C33 RIGHT NR 1 AND 2 SEAT TRACKS THREE AREAS OF CORROSION, MAIN CARGO COMPT. REMOVED DISCREPANT CLS ADAPTER AND REPLACED WITH NEW CLS ADAPTER IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040420000222004042000022NM 2004 4 20 2004UALA00314 120040406A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29390UA 24665 STA 420 STR 24L STRINGER CLIP HAS A PIECE MISSING. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20040420000292004042000029NM 2004 4 20 2004UALA00322 120040408A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 EXT FUSLAGE AT STA 265 BETWEEN STR 17L AND 18L DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA. FABRICATED & INSTALLED DOUBLER AND FILLER MATERIAL. 2L72 4F4 FRTA16WE E2GL 20040420000432004042000043NM 2004 4 20 DHL2004750025 120040225A5740 BRACKET BOEING727 7272M7 138407SNM FLAP ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, NR 5 L/E FLAP ACTUATOR TRUNNION BRACKETS SUPPORT BOTH I/B & O/B ARE CRACKED WS 171. REMOVED AND REINSTALLED NR 5 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED DAMAGED SUPPORT ANGLES 2EA AND FABBED NEW FROM 7075-T6, .063, PO 900226, DIM 8.875 X 6 INCH IAW B727 SRM 57-20-2 FIG 1. TREATED & PRIMED SUPPORTS ANGLES IAW B727 SRM 51-10-2. INSTALLED SUPPORT ANGLES IAW B727 SRM 51-30-2, PERFORMED OP'S & LEAK CK ON L/E FLAPS FOUND OK IAW B727 MM 27-81-00. 2L73 4F A3WE 20040420000452004042000045EA 2004 4 20 COMA0460243 120040401A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 2 GENERATOR FAILED A COMAC ABORTED TAKEOFF JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01967CA 7134 FLIGHT 5026 GENERATOR NR 2 FAILED DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040420000492004042000049NM 2004 4 20 DHL2004747004 120040316A3397 WIRE BOEING727 727224 1384076NM COCKPIT LIGHT FRAYED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01747DH 22253 CAPTAIN'S ADJUST LAMP CORD IS FRAYED AND IS ARCING. INSTALLED CLAMP AND TIGHTEN HARDWARE HOLDING GROUND WIRE PER M/M 20-80-1, OPS CHECKED NORMAL PER M/M 33-10-0. 2L73 4F A3WE 20040420000542004042000054NM 2004 4 20 AWXA200400362 120040401A5320655287823 STIFFENER BOEING737 7373G7 1384595NM DOOR SILL CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN STIFFENER ON BOTTOM OF THE L-2 DOOR SILL BS 976, LBL 56, WL 208. MAINTENANCE REMOVED CRACKED STIFFENER ON BOTTOM OF THE L-2 DOOR SILL BS 976, LBL 56; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-52878-23; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12 SHEETS 1-2. 2L72 4F RTA16WE 20040420000562004042000056NM 2004 4 20 AWXA200400364 120040401A532065C3267714 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT LAVATORY FLOOR STRAP FROM BS 1006 TO BS 1030, LBL 3, WL 208. MAINTENANCE REMOVED CORRODED FLOOR STRAP FROM BS 1006 TO BS 1030, LBL 3; FABRICATED A NEW REPLACEMENT FLOOR STRAP PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9 & 10. 2L72 4F RTA16WE 20040420000572004042000057WP 2004 4 20 UPS04842114 120040401A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040420000592004042000059WP 2004 4 20 UPS04842116 120040401A5720975329423 STIFFENER DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, LT WING I/B STUB WING HAS VERTICLE STIFFENER CRACKED AT LOWER END AT XS 256. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753294 AND SRM 51-1-20D. 2L74 4F RT4A25 20040420000612004042000061NM 2004 4 20 QXEA200400235 120040321A2611 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 ILLUMINATED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09375PH 529 PDX - ON FLIGHT NUMBER 2122, MASTER WARNING/SMOKE LIGHTS ILLUMINATED. BLINKS ON ABOUT EVERY 3 SECONDS LAST 10 MINUTES OF FLIGHT WITH NO ASSOCIATED INDICATION OF FIRE/SMOKE. PERFORMED OPERATIONAL CHECK OF BAGGAGE COMPARTMENT SMOKE DETECTORS, BOTH 1 AND 2 OPERATIONAL CHECKED GOOD. NO DEFECTS FOUND. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040420000622004042000062EA 2004 4 20 QXEA200400236 120040309A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 DENT IN LT SIDE FUSELAGE SKIN AT STATION FS 379.00 TO FS 394.00. REPAIRED IAW HORIZON AIR EA R-53-198. 2L72 4F RTA21EA 20040420000632004042000063NM 2004 4 20 QXEA200400215 120040314A33506138001 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09413QX805 805 4060 PDX - BOTH REAR EXTERIOR EMERGENCY LIGHTS AND ALL EMERGENCY LIGHTS IN GALLEY INOPERATIVE. REMOVED AND REPLACED RIGHT HAND 3 AND LEFT HAND 3 BATTERY PACKS. 2H72 4T RTA13NM 20040420000652004042000065NM 2004 4 20 UPS04442043 120040302A5310 BUSHING BOEING747 747SR46 1384816NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, REF EO B747-5310-1093-M RT SIDE BS 1241 FWD HOLE HAS BEEN OVERSIZED TO 1 INCH AND HAS A BUSHING INSTALLED. OLD BUSHING REMOVED AND HFEC INSPECTED RESULT CONFIRM CRACK FREE ON ALL LAYERS. BUSHING REPAIRED ON LONGERON AND ON SKIN. SPLICE STRAP AND FORGING PER RS R53-43-35119 AND BOLT BACB30US12K46, INSTALLED AS PER RS R53-43-35119, UPS-HKG-04-00059H EO B747-5310-1093-M AND EO B747-5310-20150-A. 2L74 4F RTA20WE 20040420000672004042000067NM 2004 4 20 UPS04442045 120040305A5711 STRAP BOEING747 747SR46 1384816NM LT WNG REAR SPARCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, BS 1241 LEFT WING REAR SPAR LOWER SPLICE FOUND CORROSION AT HOLE -A- ALL LAYERS APPROX 12 O/C POSITION AND APPROX 0.030 INCH DEEP. CORROSION REMOVED AND BOLT HOLE FINAL OVERSIZE TO 0.907 INCH PER EO B747-5710-12138-G, HFEC INSPECTED RESULT, NO CRACK AND CORROSION FOUND. BOLT BACB30US14K50Y INSTALLED PER EO B747-5710-12138-G APPENDICES -D- ITEM 7, FUEL LEAK CHECK CARRIED OUT SATISFACTORY. 2L74 4F RTA20WE 20040420000692004042000069NM 2004 4 20 UPS04442047 120040303A5711 FITTING BOEING747 747SR46 1384816NM RT WNG SPAR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:C RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. KICK FITTING HOLE -C- OVERSIZED TO 0.937 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE FASTENER HOLE BUSHING REPAIRED AND BOLT BACB30US14K45X INSTALLED PER RS R57-12-35122 AND EO B747-5710-20137-A REF UPS-HKG-04-00063F, UPS-HKG-04-00065H. 2L74 4F RTA20WE 20040420000702004042000070NM 2004 4 20 UPS04442048 120040303A5711 FITTING BOEING747 747SR46 1384816NM LT WING SPAR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:C LLEFT WING REAR SPAR LOWER KICK FITTING HOLE -C- FOUND CRACKED APPROX 0.040 INCH. LOWER KICK FITTING HOLE -C- OVERSIZED TO 1.000 INCH TO REMOVE CRACK. HFEC INSPECTED CONFIRM CRACK FREE. FASTENER HOLE BUSHING REPAIRED PER RS R-57-12-35122. BOLT P/N BACB30US14K45X INSTALLED. REF UPS-HKG-04-00063F, UPS-HKG-04-00065H, EO B747-5710-20137-A. 2L74 4F RTA20WE 20040420000712004042000071NM 2004 4 20 UPS04442050 120040321A3350 FUSE BOEING747 747123F NM EMERGENCY LIGHT BLOWN A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20324 AFT EMERGENCY LIGHT IN L1 DOOR INOP. TROUBLESHOT & FOUND BATTERY LOW FUSE BLOWN & BULB INOP. REPLACED BATTERY FUSE & RELAMPED IAW MM 33-51-00. OPS CHECK NORMAL AT THIS TIME. 2L74 4F A20WE 20040420000722004042000072WP 2004 4 20 UPS04842041 120040319A339711492010885 PANEL DOUG DC8 DC873F 302199FWP LANDING LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING TROUBLESHOOTING OF M277846 LANDING LIGHT INOP, MTC FOUND OVERHEAD LANDING LIGHT PANEL BURNED INTERNALLY AND WIRING SHORTED. OVERHEAD LIGHTING PANEL REMOVED & PLACED IN 5X STORES. REPLACED SWITCH 31-58, 51-59 & 51-61 AND ACCOMPANING WIRES TO DISCONNECTED PER SWPM. CHECKED REMAINING WIRES, ALL OKAY. 2L74 4F RT4A25 20040420000742004042000074NM 2004 4 20 QXEA200400210 120040311A2611473082 SMOKE DETECTOR BOMBDRDHC8 DHC8401 1390041NM FWD CARGO BAY WILL NOT TEST A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09414QX5166 4061 PDX - FLIGHT 2559 - THE FORWARD SMOKE DETECTOR DOES NOT TEST. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE FORWARD CARGO BAY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040420000772004042000077NM 2004 4 20 04FDEA00928 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP VANE, NR 2 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75928, LT AND RT OUTBOARD FLAP - NR 2 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000792004042000079NM 2004 4 20 DHL2004750031 120040225A5740 BRACKET BOEING727 7272M7 138407SNM LE FLAP ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, NR 6 L/E FLAP ACTUATOR TRUNNION BRACKETS SUPPORT BOTH I/B & O/B CRACKED WBL 304. REMOVED DAMAGED SUPPORTS AND FABBED NEW FROM 7075-T6, .063, PO 900226, DIM 7.5 X 3.5 INCH EA IAW B727 SRM 57-10-2 FIG 3. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED 2 EA BRACKETS IAW B727 SRM 51-30-2, PERFORMED OP'S AND LEAK CK ON NR 6 L/E FLAP ACTUATOR FOUND OK IAW B727 MM 27-81-0. 2L73 4F A3WE 20040420000802004042000080NE 2004 4 20 DHL2004807005 220040325A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 3 MALFUNCTIONED A DHLAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 SO01807DH 45990 693431 WHILE SHUTTING DOWN NR 2 ENGINE DURING BLOCK IN, THE NR 3 ENGINE SHUT DOWN ON ITS OWN. GROUND RAN NR 2 AND NR 3 ENGINES, AND SHUT DOWN TWO TIMES, OPS CHECKED OK IAW CFM MM 71-00-00 AND JRH 13.1 AND 11. 2L74 4F4 FRT4A25 E2GL 20040420000812004042000081NM 2004 4 20 04FDEA00945 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP I/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. 2L73 4F RTA22WE 20040420000822004042000082NM 2004 4 20 04FDEA00946 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP I/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040420000832004042000083NM 2004 4 20 04FDEA00947 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP O/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000842004042000084NM 2004 4 20 04FDEA00948 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP O/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000862004042000086NM 2004 4 20 04FDEA00950 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP O/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76663. WING OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000892004042000089NM 2004 4 20 04FDEA00930 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP VANE, NR 4 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75930. LEFT AND RIGHT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000942004042000094NM 2004 4 20 04FDEA00935 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP VANE, NR 4 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75930. LEFT AND RIGHT OUTBOARD FLAP NR 4 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000952004042000095NM 2004 4 20 04FDEA00936 120040413A5752 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP VANE, NR 5 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75931. LEFT AND RIGHT OUTBOARD FLAP NR 5 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000962004042000096NM 2004 4 20 04FDEA00937 120040413A5744 BRACE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP I/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000982004042000098NM 2004 4 20 04FDEA00939 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP I/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420000992004042000099NM 2004 4 20 DHL2004750030 120040225A5720 STIFFENER BOEING727 7272M7 138407SNM LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, LEFT WING FRONT SPAR & WBL 92.8 VERTICAL STIFFENER CRACK INDICATION FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW B727 SRM 51-30-2, STOPDRILLED CRACK AT LEFT WING FRONT SPAR VERTICAL STIFFENER IAW B727 SRM 51-10-1, FABRICATED ANGLE REPAIR FROM 7075-T6, .063 (7.0 X 1.25 X 6.5 INCH) PO 900489 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND WORKING AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-3 FIG 1. OP'S AND LEAK CHECK GOOD IAW B727 MM 28-10-02. 2L73 4F A3WE 20040420001012004042000101EU 2004 4 20 04FDEA00953 120040413A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP, 1ST SEAT TRACK FROM CENTER LINE RT SIDE BETWEEN FRAME 74 AND 75, 2 AREAS OF CORROSION UPPER SURFACE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SEAT TRACK SECTION PER A300-600 SRM 53-10-16 AND 51-40-21. 2L72 4F RTA35EU 20040420001042004042000104NM 2004 4 20 DHL2004740005 120040331A5711 SPAR BOEING727 7272Q9 138448MNM LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 PER DER RECOMMENDATION, INSTALLED DOUBLER REPAIR'S AS REQ AT LWS 198, FWD SPAR, LOWER CHORD PLATE IAW AERONAUTICAL SOLUTIONS REPORT 04-004IK. FABRICATED REPAIR DOUBLER & TRIPLER, TREATED & PRIMED, AND INSTALLED PER AERONAUTICAL SOLUTIONS REPORT 04-004IR, DATED 3/31/04. MATERIAL USED: 2024T3 X .100 INCH, PO 9911026 AND FASTENERS P/N: HL62PB 8-13. THIS IS A MAJOR REPAIR. 2L73 4F RTA3WE 20040420001062004042000106NM 2004 4 20 UPS04M42052 120040319A2560 TAPE DOUG MD11 MD11F 3023600NM SMOKE BARRIER UNSECURE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP 48774 RIGHT HAND UPPER SMOKE BARRIER HOOK AND LOOP TAPE NOT SECURED. SECURED SMOKE CURTAIN AT MAIN DECK RIGID BARRIER HOOK AND LOOP TAPE FASTENING. 2L73 4F RTA22WE 20040420001082004042000108NM 2004 4 20 04FDEA00942 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP I/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040420001092004042000109NM 2004 4 20 04FDEA00943 120040413A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP I/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. REMOVED AND REPAIRED AS PER CMM 57-44-08. FOUND REMAINING THICKNESS WITHIN TOLERANCE AS PER DWG ARC0502 SHT4. 2L73 4F RTA22WE 20040420001102004042000110NM 2004 4 20 04FDEA00944 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP I/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76665. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040420001132004042000113NM 2004 4 20 UPS04M42127 120040316A5753 BRACKET DOUG MD11 MD11F 3023600NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 INSPECTION TYPE: C, RIGHT WING I/B FLAP, O/B HINGE FOUND FWD FAIRING (O/B FACE) WITH AFT ATTACHMENT BRACKET CRACK. CRACKED ATTACHED BRACKET AT RIGHT WING I/B FLAP O/B HINGE REMOVED AS PER SRM 51-33-01 V2 R34. NEW BRACKET ARC7668, FABRICATED AS PER DWG ARC7668 FPI C/O IAW DPS4.707 AT 1/EA FABRICATED BRACKET, NO CRACK EVIDENT FOUND. FAB BRACKET PROTECTED AS PER SRM 51-21-01V2 R34. FAB BRACKET INSTALLED PER SRM 51-33-01 V2 R34. 2L73 4F RTA22WE 20040420001142004042000114NM 2004 4 20 UPS04M42130 120040316A5753ARC7717513 BRACKET DOUG MD11 MD11F 3023600NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP 48774 INSPECTION TYPE: C, LT WING O/B FLAP I/B HINGE SUSPECT L/E FAIRING ATTACH BRACKET (I/B & O/B) CRACKED. CRACKED BRACKET REMOVED AS PER SRM 51-33-01 V2 R34. NEW BRACKET FAB AS PER DWG ARC7717.FPI C/O IAW DPS 4.707 AT (1/EA) FAB BRACKET FOUND NO CRACK EVIDENT. FAB BRACKET PROTECTED PER SRM 51-21-01 V1 R 34. FAB BRACKET INSTALLED PER SRM 51-33-01 V2 R34. 2L73 4F RTA22WE 20040420001152004042000115 2004 4 20 AC2A094055 420040316A2561 BATTERY SKRSKYS76 S76A 8143006NE LIFE VEST SWOLLEN E AC2AK NONE O OTHER ININSP/MAINT 1 SO077266F 760273 BATTERY SWELLED. REPLACED WITH SERVICEABLE WATER ACTIVATED LIFE ASSEMBLY. 1G72 3U H1NE 20040420001182004042000118 2004 4 20 HE66094001 420040329A221141600297006 AUTOPILOT SYS UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT INTERMITTENT E HEEAO OTHER S AFFECT SYSTEMS CRCRUISE 1 SW03135CR 0164 AUTO PILOT FAILED INFLIGHT. AFTER RESETTING AUTOPILOT, IT WOULD FAIL AGAIN. 1G72 3U3 U H88EU E34NE 20040420001192004042000119NM 2004 4 20 UPS04442068 120040325A3350 BATTERY PACK BOEING747 747212B 1384886NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01526UP 21937 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN OVER UPPER DOCK ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY PACK PER AMM 33-31-04. OPS CHECKED GOOD. 2L74 4F A20WE 20040420001202004042000120WP 2004 4 20 UPS04842061 120040306A53203755822501N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:C2 STATION 270 BETWEEN LONG 35L-36 BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20040420001212004042000121WP 2004 4 20 UPS04842062 120040305A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:C2 STATION 257 LONG 36 RIGHT IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 250-290, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040420001222004042000122NE 2004 4 20 BAQA094030 220040324A73100319739560 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE LT INJECTION CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 32056 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U3 U H88EU E34NE 20040420001242004042000124NE 2004 4 20 BAQA094032 220040324A73100319739420 INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE PREFERENCE INJECCLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 32058 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U3 U H88EU E34NE 20040420001262004042000126EU 2004 4 20 ERAA094062 120040305A121023058147 IMPELLER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL THIN AIRFOIL MISMANUFACTURED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03153EH S572 IMPELLAR HAS THIN AIRFOIL. THIS IS NEW PART THAT WAS ISSUED TO AIRCRAFT BUT COULD NOT BE INSTALLED DUE TO THIN AIRFOIL. 1G72 3U3 U H3EU E4CE 20040420001282004042000128NE 2004 4 20 AWXA200400171 220040210A75307064004 SHAFT BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE SHEARED A AWXAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 WP28166AW4820010339 23627 DURING FULL THRUST TAKEOFF OAT AT 13 DEG, NR 2 ENG EXCEEDED MAX EGT LIMIT, RED EGT WARNING LIGHT ILLUMINATED & EGT 947 DEG FOR 5 SECONDS. ON CLIMB NR 2 ENG RAN 105 DEG HOTTER THAN NR 1 AT 877 DEG. AT CRUISE NR 2 ENG 100 DEG HOTTER THAN NR 1 AT 716 DEG. MX REQUESTED BOTH PMC'S BE SWITCHED OFF, THROTTLE SPLIT WENT FROM NR 2 THRUST LEVER BEING FORWARD OF NR 1 BY 1.5 INCHES TO A SPLIT OF 2.5 INCHES. DECLARED EMERGENCY, DIVERTED. FOUND NR 2 ENG MAIN FLEX SHAFT BROKEN BETWEEN VARIABLE BLEED VALVE GEAR MOTOR & BLEED VALVE STOP MECHANISM. R&R NR 2 ENG MASTER VBV GEAR MOTOR AND STOP MECHANISM, EGT PARAMETERS GOOD ON ENG RUN OPS CHECK. VENDORS TEST OF MASTER VARIABLE BLEED VALVE GEAR MOTOR, NO FAULT FOUND. 2L72 4F4 FRTA16WE E2GL 20040420001292004042000129WP 2004 4 20 UPS04842063 120040305A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:C2 STATION 257 LONGERON 34R I/B SIDE IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 230-290, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040420001382004042000138NM 2004 4 20 DHL2004750028 120040225A5720 ATTACH ANGLE BOEING727 7272M7 138407SNM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WS 130.7 INBOARD SIDE OF INT FRAME UPPER ATTACH ANGLE HAS 12 INCH CRACK IN RADIUS. REMOVED EXISTING ANGLE IAW B727 SRM 51-30-2. FABRICATED ANGLE FROM 2024-T3, .050, 7 X 2 INCH, PO 900641 IAW B727 SRM B727 SRM 57-20-2 FIG 1. TREATED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED ANGLE IAW B727 SRM 51-30-2. OP'S & LEAK CHECK GOOD, NO LEAKS NOTED IAW B727 MM 27-81-0 & 30-13-0. 2L73 4F A3WE 20040420001442004042000144NE 2004 4 20 BAQA094034 220040324A73100319739400 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE RT INJECTOR CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 32058 UNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U3 U H88EU E34NE 20040420001452004042000145EA 2004 4 20 COMA0470030 120040326A5744CC670171135 ATTACH FITTING CNDAIRCL600 CL6002C10 1390015EA RT SPOILER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01317CA3899 10055 THE RIGHT OUTBOARD MULTI-FUNCTION SPOILER OUTBOARD ATTACH FITTING (WS 216.9) IS CRACKED. REMOVED THE CRACKED ATTACH FITTING AND INSTALLED A NEW ATTACH FITTING P/N CC670-17113-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4790A. 2L72 4F RTA21EA 20040420001462004042000146NM 2004 4 20 UPS04242069 120040317A5320 FITTING BOEING727 72730C 1384009NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65-18420. 2L73 4F A3WE 20040420001492004042000149NM 2004 4 20 UPS04242073 120040310A5330 SKIN BOEING727 72730C 1384009NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG. 2L73 4F A3WE 20040420001512004042000151NM 2004 4 20 QXEA200400244 120040326A2162 WARNING SYSTEM BOMBDRDHC8 DHC8401 1390041NM CABIN TEMP MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09412QX 4059 GEG - ON FLIGHT 2427 BOTH FLIGHT COMPARTMENT AND CABIN PACK HOT LIGHTS CAME ON. NORMAL DUCT TEMPERATURES. LIGHTS EXTINGUISHED WHEN PACKS WERE TURNED OFF PER CHECKLIST. RESET ECS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040420001522004042000152EA 2004 4 20 COMA0460228 120040329A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01941CA 7050 CRACKS IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH. REPAIRED IN ACCORDANCE WITH REO 601R-53-11-539. 2L72 4F RTA21EA 20040420001542004042000154EA 2004 4 20 COMA0460231 120040329A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE ACTIVATIONA COMAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SO01709CA6672 7238 FLIGHT 5226 CARGO SMOKE WARNING, DISCHARGED CARGO FIRE BOTTLES. INSPECTED AND FOUND NO EVIDENCE OF OR CONDITION TO CAUSE SMOKE. REPLACED SMOKE DETECTORS. 2L72 4F RTA21EA 20040420001552004042000155NM 2004 4 20 AWXA200400311 120040329A2560P20700012015 FLASHLIGHT BOEING737 737301 1384611NM CABIN INOPERATIVE A AWXAK NONE L NO TEST NRNOT REPORTED 1 WP28325AW 23260 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040420001562004042000156 2004 4 20 BAQA094050 420040401A3421258719343 GYRO LEAR 55 55LEAR 5170702CE COCKPIT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11677 092 GYRO UNIT INOPERATIVE WHEN POWER SUPPLIED. REPLACED WITH SERVICABLE UNIT. 04/05/2004 2L72 4F A10CE 20040420001572004042000157NE 2004 4 20 AWXA200400312 220040327A7532AC69924 BLEED VALVE AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 2 ENGINE INOPERATIVE A AWXAO OTHER J WARNING INDICATION CRCRUISE 1 WP28818AW12366 1375 EN ROUTE FROM PHX TO SFO AT FL 350 DURING MODERATE TURBULENCE ECAM INDICATED NR 2 ENG STALL & FLT ATTENDANT REPORTED HEARING A LOUD THUMP. PERFORMED FCOM 3 PROCEDURE, ENG OPS NORMAL, DID NOT DECLARE EMERGENCY. MAINT COMPLIED WITH AMM 72-22-49, EEC TEST & VISUAL INSPECTION OF INLET & EXHAUST, NO DEFECTS NOTED. PERFORMED T/S TASK 71-00-00-810-809, STEPS 4B(2) D, E, & I; FOUND 7TH STAGE BLEED VALVE INOPERATIVE. R & R 7TH STAGE BLEED VALVE IAW AMM 75-32-04, OPS CHECK GOOD. FUNCTIONAL CHECK OF 7TH STAGE BLEED VALVE CONFIRMED REASON FOR REMOVAL. DISASSEMBLY FOUND TRIPLE SEALS WORN & SCORED & SPLIT BUSH GOUGED BEYOND REPAIR. REPLACED TRIPLE SEALS & REPLACED SPLIT BUSH ASSEMBLY PER CMM 75-32-52. 2L72 4F4 FRTA28NM E40NE 20040420001592004042000159NM 2004 4 20 AWXA200400313 120040303A575465C26685 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 3 SLAT WEDGE WAS FOUND DISBONDED ON THE UPPER SURFACE AT INBOARD CORNER. MAINTENANCE CUT OUT DISBONDED AREA OF SKIN ON UPPER SURFACE OF NR 3 SLAT WEDGE; FABRICATED A FILLER & DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 31 PG 88F-88H. 2L72 4F RTA16WE 20040420001602004042000160NM 2004 4 20 AWXA200400314 120040303A575465C2668722 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 6 SLAT WEDGE WAS FOUND DISBONDED ON UPPER SURFACE AT INBOARD END AND BETWEEN OUTBOARD MAIN & AUXILIARY TRACKS. SLAT BEYOND ECONOMICAL REPAIR, REMOVED AND REPLACED NR 6 SLAT. 2L72 4F RTA16WE 20040420001612004042000161NM 2004 4 20 AWXA200400315 120040303A575465C2668628 WEDGE BOEING737 7373G7 1384595NM L/E SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 MCN - MAJOR REPAIR - DURING C-15 CHECK THE NR 5 SLAT WEDGE WAS FOUND DISBONDED ON LOWER SURFACE ABOVE ACTUATOR. MAINTENANCE CUT OUT DAMAGED AREA OF NR 5 SLAT WEDGE; FABRICATED A DOUBLER & FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10 FIG 23 PG 85J-85M. 2L72 4F RTA16WE 20040420001642004042000164NM 2004 4 20 UPS04442077 120040329A3350 BATTERY PACK BOEING747 747256B 1384865NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01528UP 24071 INSPECTION TYPE:N/A LEFT EMERGENCY LIGHT IN DOOR FRAME OF UPPER DECK ESCAPE SLIDE INOP. REQUIRES BATTERY PACK ASSY DEFERRED PER MEL M278406. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK NORMAL. 2L74 4F RTA20WE 20040420001652004042000165WP 2004 4 20 UPS04842076 120040330A5610 SLIDING WINDOW DOUG DC8 DC873F 302199FWP COCKPIT BINDING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:PFLT F/O'S SLIDING WINDOW WILL NOT OPEN. CYCLED WINDOW, OPS CHECKS NORMAL. 2L74 4F RT4A25 20040420001662004042000166NM 2004 4 20 DHL2004745016 120040401A3260 WARNING SYSTEM BOEING727 727224 1384076NM COCKPIT MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 LANDING GEAR DOOR LIGHT ILLUMINATED, WHEN LANDING GEAR HANDLE WAS SELECTED TO OFF. DOOR ANNUNCIATOR PANEL INDICATED RIGHT GEAR DOOR PLACED GEAR HANDLE IN UP POSITION PER ABNORMAL PROCEDURE AND RED DOOR LIGHT EXTINGUISHED. CYCLED GEAR HANDLE SEVERAL TIMES WITH GEAR PINNED PER M/M 32-31-0. GEAR DOOR SYSTEMS INDICATION OPS CHECKED GOOD PER M/M 32-62-11. NO ABNORMAL INDICATIONS NOTED. COULD NOT DUPLICATE ON GROUND. 2L73 4F A3WE 20040420001672004042000167EA 2004 4 20 COMA0460233 120040318A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01920CA 7022 CARGO BAY FLOORBEAM LBL 27 HAS CORRODED SURFACE DAMAGE. REMOVED CARGO BAY FLOORBEAM CAP AT LBL 27, LOCATED HOLES IN A NEW FLOORBEAM CAP (P/N: 601R35031-3). INSTALLED NEW CAP WITH SERVICE HI LOKS RIVNUTS, AND CHERRY RIVETS IN ACCORDANCE WITH CRJ SRM 51-42-06, 51-42-21 AND 51-42-13. 2L72 4F RTA21EA 20040420001692004042000169EA 2004 4 20 COMA0460236 120040330A3260 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE ACTIVATIONA COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01917CA 7017 FLIGHT 5453 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. CLEANED NLG UPLOCK, EXTENSION AND RETRACTION CHECK SATISFACTORY. 2L72 4F RTA21EA 20040420001712004042000171NM 2004 4 20 CALA0400324 120040406A53206546568U520 STIFFENER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND AFT PRESSURE BULKHEAD RIGHT RADIAL STIFFENER CORRODED AT STA 1016, BL 0. THE CORRODED SECTION OF RADIAL STIFFENER WAS CUT OUT AND A NEW SECTION OF RADIAL STIFFENER WAS INSTALLED IAW BOEING DRAWING 65C28106, REV B. 2L72 4F RTA16WE 20040420001722004042000172NM 2004 4 20 CALA0400325 120040406A53206548689133 ATTACH BRACKET BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND TWO AFT WHEEL WELL PANEL I/B ATTACH BRACKETS CORRODED AT STA 727. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040420001732004042000173SW 2004 4 20 ALGA093984 120040321A6210206015001115 BLADE BELL 206 206L1 1182107SW ALLSN 250C 250C28 03013GL MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032611 2552 45417 FOUND MAIN ROTOR TRAILING EDGE EXTRUSION EXFOLIATED APPROXIMATELY 2.5. 1G71 3U3 U H2SW E1GL 20040420001752004042000175EA 2004 4 20 COMA0460239 120040402A3241428853 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ANTI-SKID SYS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01958CA11458 7111 FLIGHT 5322 ANTI SKID CAUTION DURING T/O. REPLACED THE ASCU. 2L72 4F RTA21EA 20040420001762004042000176EU 2004 4 20 BAQA093921 120040330A67101174143201 PITCH CONTROL BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE COLLECTIVE BROKEN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME6837 7243 COLLECTIVE PITCH CONTROL UNIT BROKEN NEAR BASE. REPLACED WITH SERVICABLE UNIT. 03/31/2004 1G72 3U3 U H13EU E5NE 20040420001772004042000177WP 2004 4 20 DHL2004805002 120040406A28226411194 PUMP DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE FUEL SYSTEM FAULTY A DHLAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO01805DH 46125 693535 NR 3 ENGINE FLAMED OUT AT 35,000, MACH .84. COMPLETED IN-FLIGHT ENGINE FAILURE CHECK LIST. COMPLETED IN-FLIGHT ENGINE START ABNORMAL PROCEDURE, AND IN-FLIGHT ENGINE SHUTDOWN CHECK LIST (5 PSI OIL). TROUBLESHOT PER CFM 56 M/M 71-00-00, FAULT 51. NO DEFECTS FOUND VISUALLY OR DURING ENGINE GROUND RUN TEST. REMOVED AND REPLACED FUEL BOOST PUMP PER M/M 73-10-2. LEAK CHECKED OK. PERFORMED MAX POWER ASSURANCE CHECK PER JRH, AND NO DEFECTS NOTED. ENGINE OPS CHECKED GOOD. OK TO CONTINUE. 2L74 4F4 FRT4A25 E2GL 20040420001782004042000178NM 2004 4 20 DHL2004748002 120040406A33501000677 LIGHT BOEING727 727225 1384077NM CABIN ILLUMINATED A DHLAK NONE O OTHER NRNOT REPORTED 1 SO01748DH 22440 EMERGENCY EXIT LIGHT IN FORWARD ENTRY ILLUMINATED IN FLIGHT. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT IAW B-727 M/M CHAPTER 33-50-00, OPS CHECK GOOD. 2L73 4F A3WE 20040420001792004042000179NM 2004 4 20 UPS04M42093 120040221A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 24 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 24 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.060 INCH. BARREL NUT HOLE REPAIRED PER EN1056-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040420001802004042000180NM 2004 4 20 UPS04M42094 120040219A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 21 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.039 INCH. BARREL NUT HOLE REPAIRED PER EN1054-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040420001822004042000182NM 2004 4 20 UPS04M42096 120040205A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RT NR 14 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION ON BOTTOM REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.010 INCH. BARREL NUT HOLE REPAIRED PER EN1025-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040420001852004042000185NM 2004 4 20 CALA0400328 120040406A532069353521 SUPPORT BRACKET BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 8L SUPPORT BRACKET AT STA 578. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040420001882004042000188NM 2004 4 20 CALA0400331 120040326A531065458053 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 MAINTENANCE DISCOVERED A SHEAR TIE CRACKED IN TWO PLACES ALONG THE FASTENERS ATTACHING IT TO THE FUSELAGE SKIN. THE CRACKS WERE LOCATED BETWEEN STRINGERS 9L AND 10L AND BETWEEN STRINGERS 10L AND 11L, STA 277. REPAIRED IAW ECRA 5311-01193. 2L72 4F RTA16WE 20040420001892004042000189EA 2004 4 20 COMA0460246 120040406A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01518CA2239 7816 FLIGHT 5442 GEAR DISAGREE WARNING, MLG CYCLED BETWEEN UP AND INTRANSIT. REPLACED HYDRAULIC RESERVOIR SYSTEM NR 3. 2L72 4F RTA21EA 20040420001922004042000192 2004 4 20 BAQA094012 420040402A34107002353913 SENSOR BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE AIR DATA INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 AIR DATA SENSOR WILL NOT HOLD (AIT) AFTER ABOUT 10 MINUTES OF FLIGHT TIME (NO VERTICAL MODES). REPLACED WITH SERVICABLE UNIT FROM AEC. 1G72 3U3 U H13EU E5NE 20040420001992004042000199EU 2004 4 20 ERAA093693 120040105A3212D24762101 FLOAT VALVE BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 FORWARD COMPARTMENT LEAKING AROUND TOP OFF VALVE REC'D FROM STOCK IN REPAIRED CONDITION. LEAK FOUND DURING INFLATION. REPAIRED IAW OHSO 100-1 AMD CW INSPECTION IAW 25-60-95. 1G72 3U3 U H3EU E4CE 20040420002042004042000204SW 2004 4 20 ERAA093702 120040113A6320412040002103 TRANSMISSION BELL 412 412 1182202SW MAIN ROTOR MAKING METAL A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 14992 TRANSMISSION MAKING METAL. LOCK MISSING FROM BEARING RETENTION NUT ON ACCY AND T/R DRIVE QUILL. CLIP WAS THE CAUSE OF METAL. PIECES OF FAME SPRAY FROM PREVIOUS CASE REPAIR ALSO IN OIL FILTER BUT WAS NOT CAUSE FOR CHIP LIGHT. UPPER SUN GEAR AND SPIDER GEAR SENT TO BELL TO EVALUATE PREMATURE WEAR ON GEAR TEETH.. ACTION TAKEN: REMOVED TOP CASE, UPPER AND LOWER PLANETARYS, SUMP CASE, ACCY AND T/R DRIVE QUILL, ROTOR BRAKE QUILL AND NR 2 HYD QUILL. REPAIRED ACCY AND T/R DRIVE QUILL, UPPER AND LOWER PLANETARIES, NR 1 HYD QUILL AND ARE ASSEMBLED IAW MFG 412-CR&O CH 63. COMPLIED WITH AD 94-18-09 AND ASB 412-93-72 N/A BY P/N. . 1G72 4U H4SW 20040506000912004050600091EU 2004 5 6 MALA040347 120040422A3520 SWITCH BAC 146 AVRO146RJ85A1500097EU PAX O2 FAILED A MALAG O2 MASK DEPLOYED S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL15522XJ E2347 ALL PASSENGER 02 MASKS DEPLOYED WHILE PARKED AT THE GATE. MAINTENANCE REPLACED ANEROID SWITCH. 2H74 4F RTA49EU 20040506000972004050600097NM 2004 5 6 CALA0400437 120040428A57206550820362 ANGLE BOEING737 737524 1384721NM LT WING WORN A CALAO OTHER O OTHER ININSP/MAINT 1 SW2714664 28925 LEFT WING TRAILING EDGE PANEL WORN JUST INBOARD OF NUMBER 3 FLAP TRACK FAIRING. REMOVED AND REPLACED ANGLE PER SRM 51-10-02. 2L72 4F RTA16WE 20040506000982004050600098NM 2004 5 6 CALA0400438 120040429A532065C807351 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714664 28925 R2 DOOR CUTOUT THRESHOLD Z-ANGLE CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. 2L72 4F RTA16WE 20040506001062004050600106NM 2004 5 6 CALA0400453 120040502A5280113A82004 DOOR BOEING737 737824 13844BZNM RT MLG CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712216 28776 INSPECTION FOUND A .75 INCH CRACK IN RIGHT MLG CENTER DOOR. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5280-01320. A DIP WAS ISSUED TO REINSPECT THE DOOR EVERY 30 DAYS AND TO REPLACE THE DOOR WITHIN 24 MONTHS. 2L72 4F RTA16WE 20040506001112004050600111NM 2004 5 6 CALA0400458 120040503A5350149A761416 FRAME BOEING737 737824 13844BZNM FAIRING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND A 5 INCH CRACK IN LOWER OUTBOARD AND LOWER I/B CHORDS ON RIGHT W/W AFT SKI JUMP FAIRING. THE CHORDS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040506001252004050600125EU 2004 5 6 MALA040333 120040408A5514 STRUCTURE SAAB SF340 340B 7860101EU HORIZ STAB DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING 4Y/2Y INSPECTION, RIGHT I/B UPPER STAB SPAR FASTENER HOLES FOUND TO BE IRREGULARLY SHAPED. COMPLIED WITH EO AD991921-03 PROCEDURE, FINAL REAMING OF HOLES, STEP 2 E-(1)-(2) 246 IAW MESABA EO AD991921-03. AIRCRAFT RELEASE DATE 4/16/2004. 2L72 4T RTA52EU 20040506001302004050600130WP 2004 5 6 ASAA0480129 120040229A575359304767 SKIN DOUG DC9 DC983 3022083WP T/E FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND STRIP, ANTI-ABRASION COATING AT OUTBOARD LOWER END OF LEFT INBOARD FLAP WEDGE AND EVALUATE 3 DENTS. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR SKIN IAW MD80 SRM 51-70-4. (M) 2L72 4F RTA6WE 20040506001312004050600131WP 2004 5 6 ASAA0480130 120040229A5313593643437 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND FORWARD CARGO COMPARTMENT STATION 247 CORROSION ON LONGERON 30. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICE IAW MD80 SRM 53-02. (M) 2L72 4F RTA6WE 20040506001322004050600132WP 2004 5 6 ASAA0480131 120040229A532059364423 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT PIT WEB AT DOOR CUTOUT BETWEEN STATION 1155 AND 1212 HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-10-4. (M) 2L72 4F RTA6WE 20040506001352004050600135NM 2004 5 6 ASAA0410054 120040208A575365478391 ACCESS PANEL BOEING737 737210C 1384459NM T/E FLAP DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE LEFT WING FLAP ACCESS PANEL AT WS 87.75-125.5 DISBONDED. REPAIRED PER EA. (M) 2L72 4F A16WE 20040506001362004050600136NM 2004 5 6 ASAA0410055 120040209A5313654577432 STRINGER BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 21L AT BS 847-900 CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040506001412004050600141WP 2004 5 6 ASAA0480186 120040314A53475930566 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK IS CHAFED AT FS 1212-1322. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20040506001432004050600143NM 2004 5 6 ASAA0410092 120040229A5310654654922 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND OVERSIZED HOLES AT SHEAR TIE AT STATION 767. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040506001452004050600145WP 2004 5 6 ASAA0480187 120040314A5320995821257 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND ATTACH ANGLE IS CORRODED AT FS 1007. REPLACED ANGLE PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040507000182004050700018 2004 5 7 BAQA094289 420040427A3421501121001 GYRO AGUSTAA109 A109E 0260119EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 1105 11502 UNIT CAUSES PILOT'S ADI TO TUMBLE. REPLACED WITH SERVICABLE UNIT. 04/29/2004 1G72 3U RTH7EU 20040507000412004050700041 2004 5 7 BAQA094215 420040430A3416375002241 ALTIMETER AEROSPSA365 SA365N 8680669EU COCKCPIT INACCURATE D BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 6425 ALTIMETER UNIT INACCURATE IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 05/01/2004 1G72 3U H10EU 20040507000592004050700059NE 2004 5 7 MDR04042 120040122A64106516100010141 BLADE SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE TAIL ROTOR CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09194AC581 64017 DURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND; THE OB SIDE OF THE POCKET IS CRACKED 1.8125 INCHES FROM THE TRAILING EDGE AND .25 INCH FROM THE TIP END. THE CRACK IS RUNNING SPAN WISE AND IS .6875 INCH LONG. PROBABLE CAUSE IS UNKNOWN. 2G72 4U4 U H4EA E15EA 20040507000692004050700069SO 2004 5 7 SWIA200413261 120040414A5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO WINDOW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07580SW 120348 SUPPORT BRACKET AFT CENTER OF PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT BRACKET, AFT CENTER OF PILOT'S DV WINDOW PER SRM 51-40-02 AND RII 53-301. 2L72 4T RTA31SO 20040507001132004050700113NM 2004 5 7 CALA0400432 120040427A534265538341 FITTING BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 VERTICAL STABILIZER AFT LEFT ATTACH LUG, AFT FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03. 2L72 4F RTA16WE 20040507001212004050700121NM 2004 5 7 CALA0400447 120040501A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 THE RIGHT I/B SEAT TRACK UPPER LOBE BROKE DURING REMOVAL AT STA 827. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040507001222004050700122WP 2004 5 7 CALA0400410 120040423A532059364423 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715841 49581 WEB CRACKED AT FWD LWR SIDE OF BAG BIN DOOR AT STA 636, LONG 27 LEFT. REMOVED AND REPLACED WEB PER ECRA 5310-04416. 2L72 4F A6WE 20040507001422004050700142 2004 5 7 CALA0400429 420040427A3418C072023 STICK SHAKER BOEING737 7373T0 1384582NM STALL WARNING WILL NOT TEST A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 CAPTAINS STICK SHAKER WILL NOT TEST. REPLACED STICK SHAKER PER AMM 27-32-31. 2L72 4F RTA16WE 20040507001532004050700153EA 2004 5 7 COMA0460286 120040423A2760 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01805CA 7354 FLIGHT 5450 DURING CRUISE FLIGHT, RECEIVED A SPOILER AND SPOILERON CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO DTW. PERFORMED RESET OF SPOILER ELECTRONIC CONTROL UNIT NR 1 AND NR 2. 2L72 4F RTA21EA 20040507001582004050700158EA 2004 5 7 COMA0460284 120040425A7910 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA NR 2 ENGINE OVERSERVICED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01729CA 7265 FLIGHT 5171 RECEIVED HIGH OIL TEMPERATURE INDICATION ON NR 2 ENGINE DURING CLIMBOUT OF ATL, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FOUND NR 2 ENGINE OIL OVERSERVICED, DRAINED EXCESS OIL AND PERFORMED ENGINE RUNS, OPERATION SATISFACTORY. 2L72 4F RTA21EA 20040507001712004050700171EA 2004 5 7 COMA0460273 120040414A5297601R576891 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR FAULTY A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01483CA 7689 FLIGHT 5259 PASSENGER DOOR WARNING, SERVICE DOOR CAUTION, AND OVERBOARD COOL FAIL MESSAGE. REPLACED THE CARGO DOOR WIRING HARNESS. 2L72 4F RTA21EA 20040507001722004050700172EA 2004 5 7 COMA0460272 120040413A2750860D10018ABCD ECU CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01954CA18832 7100 FLIGHT 5852 FLAPS FAILED CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040507001752004050700175EA 2004 5 7 COMA0460263 120040418A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01981CA 7163 FLIGHT 5890 APU SHUT DOWN DURING FLIGHT DUE TO HIGH TEMP, NR 2 IDG HAD BEEN DEFERRED. FLIGHT WAS DIVERTED TO SDF. INSPECTED APU ECU FOR FAULT CODES, NO CODES DISPLAYED. PERFORMED AN OPERATIONAL TEST OF APU, OPERATION OF APU SATISFACTORY. 2L72 4F RTA21EA 20040510000062004051000006SO 2004 5 10 SWIA200413226 120040418A2612 FIRE LOOP EMB 120 EMB120ER 3260203SO NR 2 ENGINE INOPERATIVE A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07579SW 120347 NR 2 ENGINE DETECTOR INOP. ENGINE WHEEL WELL LIGHT ILLUMINATED. REMOVED NR 2 ENGINE FIRE LOOP AND REPLACED WITH A SERVICEABLE LOOP IAW MM 26-21-01. OPS CHECK GOOD. P/N 3601-75-450/160C. 2L72 4T RTA31SO 20040510000182004051000018EA 2004 5 10 SWIA200413255 120040430A2613 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA OVERHEAT LOOP DIRTY A SWIAO OTHER LP NO TEST NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07594SW 7285 RIGHT JETPIPE LOOP B-INOP. REMOVED OVERHEAT AND FIRE DETECTOR CONTROL BOX CONNECTORS. CLEANED CONTACTS AND REINSTALLED CONNECTORS. OPS CHECK GOOD. 2L72 4F RTA21EA 20040510000412004051000041EU 2004 5 10 BTA2004F00001 120040328A3040 CONTROL VALVE HWKSLYDH125 BH125400A 4230138EU RROYCEVIPER VIPER522 54552EU DEMISTER INCORRECT E BTAAO OTHER O OTHER NRNOT REPORTED 1 GL23800TG NA780 REJECTED TAKEOFF, UNUSUAL BLEED AIR NOISE IN COCKPIT WHEN THROTTLES WERE ADVANCED FOR TAKE-OFF. TAKE-OFF ABORTED BEFORE 60 KNOTS, DISCOVERED COCKPIT WINDOW DEMISTER CONTROL VALVE IN FULL OPEN POSITION, REPOSITIONED CONTROL HANDLE TO NORMAL POSITION. SUBSEQUENT TAKEOFF, NO FURTHER PROBLEM. (NO DEFECT, VALVE IN WRONG POSITION FOR TAKE-OFF. PRECAUTIONARY REJECTED TAKEOFF BECAUSE OF UNUSUAL BLEED AIR NOISE) 2L72 4J4 J A3EU E3EU 20040510000442004051000044WP 2004 5 10 AALA20040525 120040504A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21207AA 49158 MSP CEILING EMERGENCY LIGHTS AT ROW 19 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000462004051000046NM 2004 5 10 AALA20040533 120040505A3350 LIGHT BOEING737 737823 13844BZNM ROW 12D BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21970AN 30096 DFW FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D BROKEN. REPLACED THE FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040510000612004051000061EU 2004 5 10 MALA040357 120040416A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15365PX 340B265 DURING CAPACITY CHECK BATTERY PACK P/N 61-0478-9, S/N 9712219 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/16/04 & 4/21/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK P/N 55-2198-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/25/04. 2L72 4T RTA52EU 20040510000692004051000069WP 2004 5 10 AALA20040532 120040505A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 ORD EMERGENCY FLOOR LIGHTING FLICKERING IN AFT CABIN. REPAIRED BROKEN WIRE IN AFT FUSELAGE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000702004051000070NM 2004 5 10 AALA20040527 120040505A3350P4010051112 MODULE BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21670AA 25335 JFK FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER MODULE FOR FIRST CLASS SEAT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20040510000752004051000075WP 2004 5 10 AALA20040519 120040503A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21587AA 53250 DEN OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510000772004051000077SO 2004 5 10 C2XA04SH271 120040507A532014521721009 BUTTSTRAP EMB 145 EMB145 3260210SO FUSLEAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED JUST UNDER THE COCKPIT STEP PANEL. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01115. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510000872004051000087SO 2004 5 10 C2XA04TY079 120040506A531514522461003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM TOP CAP. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-30-01, 51-20-03, 51-60-02, CPM 51-21-04, 51-21-06, 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040510000902004051000090SO 2004 5 10 C2XA04SH273 120040508A531214547494607 FIREWALL EMB 145 EMB145 3260210SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED IN TWO PLACES AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FIREWALL IAW EMB 145 SRM 51-40-02 AND EA 5340-01016 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510000912004051000091NM 2004 5 10 AALA20040524 120040430A3242 MODULE BOEING757 757223 1384957NM MLG INOPERATIVE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21604AA 27055 JFK INFLIGHT T1015/30 RIGHT SYSTEM HYDRAULIC QUANTITY EICAS STATUS PAGE INDICATED .42 QUANTITY. RETURNED TO JFK AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION WITH NO DAMAGE NOTED. SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. REPLACED RIGHT HAND ANTI SKID SHUTTLE VALVE MODULE AND ALTERNATE BRAKE SELECTOR VALVE. JACKED AIRCRAFT AND CHECKED ALL BRAKES FOR PROPER RELEASE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) PROPER RELEASE. 2L72 4F RTA2NM 20040510000932004051000093SO 2004 5 10 C2XA04SH274 120040508A711014576057621 RIB EMB 145 EMB145 3260210SO LT COWLING CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE LEFT UPPER ENGINE COWLING AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510000962004051000096NE 2004 5 10 AALA20040497 220040428A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RIGHT FAILED A AALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW21501AA 49738 717802 ABQ INFLIGHT T1508 ON TAKE OFF ON ROTATION HEARD A LOUD BANG FROM RIGHT ENGINE ACCOMPANIED BY POWER LOSS AND AIRCRAFT YAW. RETURNED FOR LANDING. NUMBER 1 AND NUMBER 2 HAD ROTATION OIL PRESSURE ALSO IN GREEN. RETURNED TO ABQ AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. CHANGED RIGHT HAND ENGINE DUE TO NUMBER 2 ENGINE TURBINE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040510001152004051000115WP 2004 5 10 AALA20040508 120040429A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 DFW AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001172004051000117WP 2004 5 10 AALA20040505 120040428A3213 PISTON DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21432AA 49350 DFW INFLIGHT T0617/28 AFTER TAKE OFF PILOT REPORTED UNABLE TO RETRACT LANDING GEAR. THE GEAR HANDLE BINDS APPROXIMATELY HALF WAY UP. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REMOVED FROM SERVICE FOR REPAIRS. ACCOMPLISHED SPECIAL ITEMS CARD 05-91-29 FOR OVERWEIGHT LANDING. REPLACED NOSE GEAR PISTON ASSEMBLY AND SEALS. SERVICED NOSE STRUT. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001212004051000121WP 2004 5 10 AALA20040513 120040501A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21406A 49317 ORD EMERGENCY LIGHTS FROM COCKPIT INOPERATIVE. REPLACED BATTERY PACKS AT SEAT 6EF, 9DEF, AND 20DEF FOR EMERGENCY LIGHTS FROM COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001222004051000122GL 2004 5 10 C2XA04CL041 220040424A720023070402 ENGINE EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XAK NONE EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 SW2714508 145220 CAE311106 CLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20040510001392004051000139SO 2004 5 10 C2XA04SH272 120040508A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716561 145610 SHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT THE COMPOSITE FIBER CROSS BEAM AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, PAGE 213, FIGURE 201, SHEET 3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040510001402004051000140NM 2004 5 10 AWXA200400479 120040421A53156546810 FLOORBEAM BOEING737 7373G7 1384595NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF CABIN FLOORBEAM AT BS 967, RBL 45. MAINTENANCE CUTOUT DAMAGED SECTION OF UPPER TEE CAP ON CABIN FLOORBEAM AT BS 967, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF UPPER TEE CAP, 2 EACH REPAIR STRAPS & NESTING ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG. 202. 2L72 4F RTA16WE 20040510001472004051000147SO 2004 5 10 C2XA04SH269 120040506A532014525422001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001542004051000154SO 2004 5 10 C2XA04SH262 120040501A27503631001007MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212SO T/E FLAP MALFUNCTIONED A C2XAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SW2716954 145072 SHV-IN FLIGHT 2523 FROM IAH TO DFW THE PILOT OBSERVED FLAP FAIL AND FLAP LOW SPEED INDICATION ON EICAS WHEN FLAP LEVER WAS MOVED TO THE 9 DEGREE POSITION. THE PILOT DECLARED AN EMERGENCY AND LANDED AT DFW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB 145 AMM 27-53-02. FLAP OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040510001762004051000176NM 2004 5 10 AWXA200400390 120040401A53156546811516 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF UPPER TEE AT BS 986, BL "0" TO RBL 9.5, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF UPPER TEE AT BS 986, BL "0" TO RBL 9.5, WL 208; FABRICATED A NEW REPLACEMENT SECTION OF TEE, 2 EACH SUPPORT ANGLES, AND 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG. 202, PG. 207-211. 2L72 4F RTA16WE 20040510001772004051000177NM 2004 5 10 AWXA200400391 120040401A53156546811516 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON UPPER SURFACE OF UPPER TEE AT BS 986, RBL 10 TO RBL 19, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF UPPER TEE AT BS 986, RBL 10 TO RBL 19, WL 208; FABRICATED A NEW REPLACEMENT SECTION OF TEE, 2 EACH SUPPORT ANGLES, & 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG. 202, PG. 207-211. 2L72 4F RTA16WE 20040510001802004051000180NM 2004 5 10 AWXA200400441 120040412A532069366564 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND IN UPPER ANGLE OF INTERCOSTAL BETWEEN BS 927 AND BS 947, BL "0". MAINTENANCE REMOVED CRACKED UPPER ANGLE ON INTERCOSTAL FROM BS 927 TO BS 947, BL "0"; FABRICATED A NEW REPLACEMENT UPPER INTERCOSTAL ANGLE PER DWG 69-36656 AND INSTALLED REPAIR PART. 2L72 4F RTA16WE 20040510001812004051000181NM 2004 5 10 AWXA200400407 120040425A57536546435235 SKIN BOEING737 737277 1384570NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW144363204 22653 FLIGHT CONTROL - DURING 4-DAY CHECK FOUND THE LT OUTBOARD TRAILING FLAP DELAMINATED AND SEPARATING ALONG TRAILING EDGE, APPROXIMATELY 12 INCHES BY 1 INCH, AND 3 INCHES BY 3/4 INCH WITH A 8 INCH SEPARATION. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD TRAILING FLAP IAW T/C R8M27002. 2L72 4F RTA16WE 20040510001852004051000185NM 2004 5 10 AWXA200400410 120040402A5311654653950 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK A 1 INCHES CRACK WAS FOUND IN FRAME FOOT AT BS 616, RBL 65, WL 202. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME FOOT AT BS 616, RBL 65, WL 202; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5311-01143-DD1. 2L72 4F RTA16WE 20040510001882004051000188EU 2004 5 10 AWXA200400414 120040328A5313D53480046203 SPLICE AIRBUS320 A320232 3930326EU STRINGER CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN FR 66 AND FR 67, STR 26 R/H. MAINTENANCE REMOVED CORRODED STRINGER SPLICE SECTION BETWEEN FR 66 AND FR 67, STR 26 R/H; FABRICATED A NEW REPLACEMENT SPLICE SECTION; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8 & 12. 2L72 4F RTA28NM 20040510001902004051000190EU 2004 5 10 AWXA200400416 120040330A5320D5347112320000 SUPPORT AIRBUS320 A320232 3930326EU FRAME CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FRAME SUPPORT, FORWARD OF FR 70 AT STR 23 LT. MAINTENANCE REMOVED CORRODED FRAME SUPPORT, FORWARD OF FR 70 AT STR 23 LT; FABRICATED A NEW REPLACEMENT FRAME SUPPORT; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2, 3, & 8. 2L72 4F RTA28NM 20040510001922004051000192NM 2004 5 10 AWXA200400444 120040420A57302024T3100 SKIN BOEING757 7572S7 1384962NM RT WING LE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 UPPER SURFACE OF RT FIXED WING LEADING EDGE DELAMINATED AT WS 421. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SURFACE OF R/H FIXED WING LEADING EDGE AT WS 421; FABRICATED A FILLER, NEW SECTION OF SKIN, AND A SPLICE PLATE; INSTALLED REPAIR PART IAW AWA E.R. 19-5700-00012-DD5. 2L72 4F RTA2NM 20040510001942004051000194NM 2004 5 10 AWXA200400446 120040414A143069367491 BOLT BOEING737 7373S3 1384711NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE LT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 LT. MAINTENANCE REMOVED AND REPLACED L/H VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B55002. 2L72 4F RTA16WE 20040510001952004051000195EU 2004 5 10 AWXA200400417 120040329A5347D5311281400000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 R/H, FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 R/H, FROM FR 12 TO FR 24, INSTALLED NEW REPLACEMENT SEAT TRACK IAW A320 SRM 51-42-11, FIG. 18. 2L72 4F RTA28NM 20040510001962004051000196NM 2004 5 10 AWXA200400469 120040503A561041600318003 COMPUTER AIRBUSA319 A319132 3930340NM ZONE 121 FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28805AW3682 1049 EN ROUTE, RECEIVED ECAM MESSAGE FOR ANTI-ICE LT WINDOW THEN HEARD A LOAD NOISE AS LT AFT SIDE WINDOW SHATTERED, PRESSURE WAS NOT LOST, DIVERTED TO GJT. MAINT R & R LT AFT SIDE WINDOW IAW AMM 56-11-12, & REPLACED LT WINDOW HEAT COMPUTER IAW AMM 30-42-34. OPS CHK OF WINDOW HEAT CONTROL UNIT GOOD. FUNCTIONAL CHECK OF WINDOW HEAT COMPUTER S/N 4160031800258 WAS NO FAULT FOUND. UNIT TESTED IAW CMM 30-42-36. 2L72 4F RTA28NM 20040510001982004051000198NM 2004 5 10 AWXA200400471 120040504A335020121 CHARGER BOEING757 7572G7 1384963NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 DURING INSPECTION FOUND THE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER FOR L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040510002022004051000202NM 2004 5 10 AWXA200400475 120040408A5313654577610 STRINGER BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 967. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 27 L/H AT BS 967; FABRICATED A 4 EACH ANGLES & SHIMS, 2 EACH CHANNELS, AND A HAT SECTION; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG. 201. 2L72 4F RTA16WE 20040510002032004051000203NM 2004 5 10 AWXA200400476 120040406A575465C2660298 SKIN BOEING737 7373S3 1384711NM SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK FOUND THE UPPER NO. 5 SLAT WEDGE DELAMINATED AT SS 147.5. MAINTENANCE REMOVED PREVIOUSLY INSTALLED REPAIR DOUBLERS ON NO. 5 SLAT WEDGE AT SS 147.5; FABRICATED NEW REPLACEMENT DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIG. 31. 2L72 4F RTA16WE 20040510002042004051000204EU 2004 5 10 AWXA200400418 120040328A5315D53472193200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT BETWEEN FR 66 AND FR 70. MAINTENANCE REMOVED CORRODED FLOORBEAM Y765 RT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8, 12, & 18. 2L72 4F RTA28NM 20040510002052004051000205EU 2004 5 10 AWXA200400419 120040328A5320D53480043205 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON INBOARD AFT R-2 DOOR SILL BETWEEN FR 66 AND FR 68, Y1800 R/H. MAINTENANCE CUTOUT CORRODED SECTION OF R-2 DOOR SILL FROM FR 66 TO FR 68 AT Y1800 R/H; PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED AN ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201 2L72 4F RTA28NM 20040510002072004051000207EU 2004 5 10 AWXA200400421 120040329A5315D53112066200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK STRESS CORROSION WAS FOUND ON FLOORBEAM Y765 LT AT FR 16. MAINTENANCE REMOVED CORRODED FLOORBEAM Y765 LT, FROM FR 12 TO FR 24, INSTALLED NEW REPLACEMENT FLOORBEAM IAW A320 SRM 51-42-11, FIG. 12 & 18. 2L72 4F RTA28NM 20040510002112004051000211NM 2004 5 10 UPS04M42247 120040217A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORR AT BOTTOM OF NR 25 RT HOLE REMOVED PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.044 INCH WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1043-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF UPS ENGINEERING FILE NR MD11-55-20012) 2L73 4F RTA22WE 20040510002122004051000212EU 2004 5 10 UPS04142326 120040430A3350 BATTERY AIRBUSA300 A300F4622R 3930360EU CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01128UP 0813 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. R&R EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY PER MM 33-51-14, CHECKS OK. 2L72 4F RTA35EU 20040510002152004051000215NM 2004 5 10 UPS04242320 120040414A5312 PRESSURE PANEL BOEING727 72722C 138400FNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE:C AIR LEAK FROM CRACK ON NWW WEB LHS BS 287. PAINT STRIPPED, HFEC INSPECTION C/O CRACKS CONFIRMED, CRACKED AREA CUT OUT, HFEC C/O AROUND CUT OUT AREA NDF, REMOVED SUPPORT STRUCTURE TO GAIN ACCESS, FABRICATED REPAIR PARTS, INSTALLED FABRICATED PARTS, REINSTALLED SUPPORT STRUCTURE, REPAIR PAINTED. 2L73 4F A3WE 20040510002172004051000217WP 2004 5 10 UPS04842322 120040403A5753 CHANNEL DOUG DC8 DC871F 302199DWP T/E FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE:C-1 RIGHT WING I/B FLAP O/B TRAILING EDGE IS CRACKED. REMOVED CRACKED CHANNEL. FAB NEW CHANNEL IAW DC8 SRM 57-7-1. ALODINED AND PRIMED CHANNEL IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-3-O,51-3-1,51-1-21 AND 51-1-21A 2L74 4F RT4A25 20040510002182004051000218WP 2004 5 10 UPS04842324 120040406A53203754065 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE:C-1 FWD LWR CARGO STA 300 TC 308 L33R TO L34R DOUBLER HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8. ORIG THICKNESS WAS .063 IAW DAC DWG 3754065. MATERIAL RMVD WAS .020 AND IS OUT OF LIMITS IAW DC8 SRM 53-2-0 FAB NEW DOUBLER FROM 7075-T6 .063 IAW DC8 51-1-24 & DAC DWG 3754065. ALODINED & PRIME DOUBLER IAW DC8 SRM 51-1-8. RMVD OLD & INSTALLED NEW D OUBLER IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20040510002192004051000219NM 2004 5 10 2004UALA00372 120040420A2750 FLAP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE WING MALFUNCTIONED A UALAB EMER. DESCENT FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 WP29948UA 26691 LANDED UNDER AMBER ALERT DUE TO A FLAP MALFUNCTION. AMT FOUND THAT THE TRAILING EDGE FLAP INDICATOR WAS STICKING AT 5 UNITS. VISUAL INSPECTION OF FLAP SYSTEM REVEALED NO OTHER DEFECTS. THE FLAP INDICATOR WAS REPLACED AND THE SYSTEM PASSED THE OPERATIONAL CHECK. TEAR DOWN AND INSPECTION OF THE FLAP INDICATOR VERIFIED THAT THE RIGHT POINTER WAS STICKING, WHICH WAS CAUSED BY MATERIAL BUILD-UP ON THE RIGHT SYNCHRO BRUSH. THE SYNCHROS (LEFT AND RIGHT) WERE CLEANED AND BEARINGS WERE REPLACED. UNIT WAS TESTED AND RETURNED TO STOCK. 2L72 4F4 FRTA16WE E2GL 20040510002212004051000221NM 2004 5 10 2004UALA00374 120040420A5240 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE L5 DOOR BUCKLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 MED 5L EXTERIOR SKIN AT FWD LOWER CORNER BUCKLED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20040510002222004051000222NM 2004 5 10 2004UALA00375 120040420A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 EXTERNAL FUSELAGE SKIN HAS DENT AT BS 2188 BTWN S29R & S30R. FABRICATED AND INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20040510002232004051000223NM 2004 5 10 2004UALA00376 120040420A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 LWR EXTERNAL FUSELAGE SKIN DENTED BS 1814 LBL 12.5. FABRICATED & INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20040510002262004051000226NM 2004 5 10 2004UALA00379 120040420A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 LT SIDE CABIN STRINGER TIE BRACKET CRACKED AT BS639 AND STRINGER 4L MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW CLIP. 2L72 4F4 FRTA16WE E2GL 20040510002272004051000227NM 2004 5 10 2004UALA00380 120040420A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 LT SIDE CABIN STRINGER TIE BRACKET CRACKED AT BS616 STR 4L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20040510002302004051000230EU 2004 5 10 2004UALA00362 120040417A5523D5528000100551 TAB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT ELEVATOR BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29453UA 1001 RT ELEVATOR UPPER ANTI-ROTATION TAB AT THE HINGE OUTBOARD OF THE INBD ACTUATOR IS BROKEN. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA28NM E40NE 20040510002342004051000234NM 2004 5 10 2004UALA00366 120040416A5315 FLOORBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29390UA 24665 STA 987 RBL 45.5 FLOOR BEAM HAS CORROSION ON TOP AND BOTTOM SIDE OF NUT PLATE HOLES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLES. 2L72 4F4 FRTA16WE E2GL 20040510002362004051000236NM 2004 5 10 2004UALA00368 120040417A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 EXTERNAL SKIN STA 847 RT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND QUAD REPAIR. 2L72 4F4 FRTA16WE E2GL 20040510002382004051000238NM 2004 5 10 2004UALA00387 120040421A2613 FIRE LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT WING OUT OF POSITION A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29311UA 23672 DIVERTED TO DFW DUE TO RIGHT WING-BODY OVERHEAT PROBLEM WITH ASSOCIATED NON-ICING RESTRICTION AND ICING CONDITIONS AT DEN. TROUBLESHOOT TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR, LOOP M1204 ABOVE NO. 2 ENGINE. FOUND LOOP SHORTED TO GROUND. REPLACED RIGHT HAND LEADING EDGE OVERHEAT LOOP M1204. 2L72 4F4 FRTA16WE E2GL 20040510002402004051000240NM 2004 5 10 F3LA200400041 120040414A5320 SILL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED R1 DOORWAY LOWER SILL WEB CORRODED ON UPPER AND LOWER SURFACE. REPLACED R1 DOOR SILL WEB PER SRM 51-40-02. 2L72 4F RTA16WE 20040510002432004051000243NM 2004 5 10 F3LA200400051 120040419A5320 SILL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON MOP SILL AT R2 DOOR. REPLACED MOP SILL PER SRM 51-40-02, 51-40-5 AND 51-40-08. 2L72 4F RTA16WE 20040510002452004051000245NM 2004 5 10 F3LA200400037 120040412A5320 WEB BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION UNDER C2 DOOR THRESHOLD. REPLACED C2 DOOR WEB AND CLEANED CORROSION SURROUNDING STRUCTURE PER SRM 51-10-2. LOCATED, DRILLED HOLES IN NEW WEB AND INSTALLED WEB PER SRM 51-40-02. 2L72 4F RTA16WE 20040510002462004051000246NM 2004 5 10 F3LA200400036 120040412A5320 ANGLE BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON LOWER RT TRANSITION ANGLE FROM C2 DOOR FWD. BLENDED CORROSION ON RT TRANSITION ANGLE, STA 727E TO STA 767, OUT OF LIMITS PER SRM 53-60-53. REPAIRED PER SRM 53-60-53, PAGE 208, AND SRM 51-40-02. 2L72 4F RTA16WE 20040510002482004051000248NM 2004 5 10 F3LA200400039 120040412A5320 SUPPORT ANGLE BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM SUPPORT ANGLE AT STA 294.5, RBL 39. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-2. FABRICATED AND INSTALLED REPLACEMENT REINFORCEMENT ANGLE PER SRM 53-10-8, 53-10-51 AND 51-40-02. 2L72 4F RTA16WE 20040510002492004051000249NM 2004 5 10 F3LA200400038 120040412A5320 STRAP BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED TAPERED STRAP INBD OF C-2 DOOR WEB SILL CORRODED. REPLACED STRAP PER SRM 51-40-02. 2L72 4F RTA16WE 20040510002502004051000250NM 2004 5 10 F3LA200400040 120040412A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FWD GALLEY FLOORBEAM AT STA 294.5, RBL 29.52. REPLACED FLOORBEAM SECTION PER SRM 53-10-51. 2L72 4F RTA16WE 20040510002532004051000253NM 2004 5 10 2004UALA00382 120040420A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 CABIN R1 DOOR SURROUND STRUCTURE INTERCOSTAL ANGLE HAS A CRACK AT BS 291 BETWEEN STR 13R AND 14R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20040510002562004051000256NM 2004 5 10 2004UALA00386 120040420A3350767 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29519UA 24872 LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP PN 767. 2L72 4F4 FRTA2NM E17NE 20040510002572004051000257NM 2004 5 10 2004UALA00388 120040418A2120 ODOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DETECTED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 WP29175UA 24382 FA REPORTED SMELLING PLASTIC BURNING SMELL/SMOKE. F/A USED A PLASTIC COVER WHILE HEATING FOOD. PLASTIC COVERED FOOD IS NOT LOADED INTO OVENS. F/A SHOULD REVIEW CORRECT PROCEDURES FOR RECON OVENS AND NEVER PLACE ANY PLASTIC ITEMS INTO OVENS. 2L74 4F4 FRTA20WE E24NE 20040510002582004051000258 2004 5 10 2004UALA00390 420040114A3414 INDICATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT FAULTY A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29597UA 28750 ABORTED TAKEOFF AT 100KTS DUE TO A CAPT AIRSPEED INDICATOR PROBLEM. THE CAPTAIN'S AIRSPEED INDICATOR WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20040510002592004051000259NM 2004 5 10 2004UALA00391 120040425A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29806UA 788 EMERGENCY LIGHTS FAIL 3SVC TEST. REPLACED EPSU RT & AFT UNITS AND AFT BATTERY. OPS CK GOOD. 2L72 4F4 FRTA28NM E40NE 20040510002652004051000265NM 2004 5 10 2004UALA00398 120040426A5313 STRINGER BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 LWR NOSE COMPT LT CRAWL WAY STRINGER 39 BTWN BS 280 AND BS 300 IS DEFORMED AND CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. 2L74 4F4 FRTA20WE E24NE 20040510002692004051000269NM 2004 5 10 2004UALA00402 120040423A5320 TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29390UA 24665 STRINGER TIE CRACKED AT BS 294.5 S23L. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER TIE. 2L72 4F4 FRTA16WE E2GL 20040510002732004051000273NE 2004 5 10 2004UALA00406 220040427A7200 SEAL BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 1 ENGINE FAILED A UALAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 WP29773UA 26929 NR 1 ENGINE N1 VIBRATIONS. 6TH STAGE TURBINE AIRSEAL FAILURE REF: PW4074/77 IPC (PN 51A346) 72-53-00 FIGURE 7, ITEM 70A. A 4-INCH AXIAL BY 6-INCH CIRCUMFERENTIAL PIECE OF THE SEAL HAD BROKEN OUT & WAS MISSING. THE REMAINDER OF THE LPT SUFFERED HEAVY DOWNSTREAM DAMAGE. THE SEAL WAS OF THE POST SERVICE BULLETIN PW4G-112-72-171 CONFIGURATION. THIS IS A NEW FAILURE MODE. THE 2ND SUCH FAILURE UA HAS SEEN. SEALS FROM BOTH FAILURES HAVE BEEN RETURNED TO PW & MTU FOR ROOT CAUSE ANALYSIS. 2L72 4F4 FRTT0001SE E46NE 20040510002742004051000274NM 2004 5 10 2004UALA00407 120040423A32116549488 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT MLG CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA40213 24662 THE LT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. FITTING WAS REPLACED. 2L72 4F4 FRTA16WE E2GL 20040510002762004051000276NM 2004 5 10 2004UALA00409 120040428A335058807 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29350UA 24301 EMERGENCY EXIT LIGHTING STRIP DAMAGED ON LT SIDE OF AFT GALLEY. REPLACED LIGHT ASSY AND SECTION OF PLASTIC COVER. 2L72 4F4 FRTA16WE E2GL 20040510002782004051000278NM 2004 5 10 2004UALA00411 120040427A335060243 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29585UA 26709 AFT EEL STRIP IN FRONT OF FWD, AFT LAV IS INOPERATIVE. REPLACED EEL STRIP. 2L72 4F4 FRTA2NM E17NE 20040510002802004051000280NM 2004 5 10 2004UALA00413 120040428A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29939UA 26672 FLOOR PROX EMERGENCY EXIT LIGHTING INOPERATIVE FROM ROW 14 AFT. REPLACED LIGHT CABLE AND AFT GALLEY FLOOR LIGHT. 2L72 4F4 FRTA16WE E2GL 20040510002822004051000282 2004 5 10 2004UALA00415 420040119A2565 SQUIB BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EVAC SLIDE BLOWN A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29659UA 27114 RT OVERWING SLIDE DOOR SQUIB BLOWN. SQUIB BLOWN IN CONJUNCTION WITH INADVERTANT SLIDE DEPLOYMENT. SQUIB REPLACED. 2L72 4F4 FRTA1NM E24NE 20040510002832004051000283NM 2004 5 10 2004UALA00416 120040429A2910 HYDRAULIC SYSTEM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE A SYSTEM MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29924UA 26645 FLIGHT RETURNED TO THE FIELD WITH A LOSS OF THE A SYSTEM HYDRAULIC PRESSURE. REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP. 2L72 4F4 FRTA16WE E2GL 20040510002842004051000284NM 2004 5 10 2004UALA00417 120040121A2820 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT ACTIVATED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29654UA 25392 FUEL CONFIGURATION LIGHT ON 1 HOUR INTO FLIGHT. FUEL IMBALANCE. 2L72 4F4 FRTA1NM E24NE 20040510002852004051000285NM 2004 5 10 2004UALA00418 120040318A1430 BOLT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NLG DOOR SHEARED A UALAK NONE O OTHER ININSP/MAINT 1 WP29618UA 21878 NOSE GEAR LT DOOR LINK ROD HINGE BOLT IS SHEARED. FOUND DURING NR 1 SERVICE. BOLT NOT RECOVERED, CAUSE OF FAILURE UNKNOWN. REPLACED BOLT. 2L72 4F4 FRTA1NM E3NE 20040510002892004051000289EU 2004 5 10 2004UALA00392 120040424A3240 BPSU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NLG BRAKES FAILED A UALAO OTHER O OTHER TXTAXI/GRND HDL 1 WP29494UA 1840 ON TAXI OUT, COMPLETE LOSS OF NOSE WHEEL STEERING AND BRAKING. ALSO EXPERIENCED UNCOMMANDED LEFT TURN. BRAKE SYSTEM CONTROL UNIT (BSCU) FAILED. BRAKE SYSTEM CONTROL UNIT (BSCU) REPLACED, NOSE WHEEL ANTISKID STEERING SWITCH REPLACED. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040511000012004051100001NM 2004 5 11 AWXA200400485 120040507A335020311A BATTERY BOEING737 73733A 1384673NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 DURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHTING AFT OF SEAT ROW 18 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT AFT EMERGENCY POWER SUPPLY BS 947, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040511000022004051100002EU 2004 5 11 AWXA200400486 120040507A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 11 RT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28654AW 1050 PHX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 R/H INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 11 R/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000032004051100003EU 2004 5 11 AWXA200400487 120040508A33501013081 LIGHT AIRBUS320 A320232 3930326EU SEAT ROW 22 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28604AW 1196 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 L/H WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPALCED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000052004051100005NM 2004 5 11 AWXA200400489 120040509A3397 WIRE BOEING737 7373Y0 1384671NM EMERGENCY LIGHT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28334AW 23747 DURING 8-DAY CHECK FOUND THE COCKPIT EMERGENCY DOME LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON RESISTOR MODULE FOR COCKPIT EMERGENCY DOME LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040511000102004051100010EU 2004 5 11 ERAA094453 120040404A3212D24873101 FLOAT BOLKMS105 BO105S 5626006EU LT MLG LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03298EH10739 CYLINDER BOTTLE LEAKING DOWN PRESSURE. SQUIB VALVE ON CYLINDER WAS CHECKED FOR LEAKS, LEAK WAS DISCOVERED AT SQUIB VALVE TO MANIFOLD JUNCTION. ACTION TAKEN: REMOVED SQUIB VALVE MANIFOLD ASSY FROM CYLINDER. REMOVED AND REPLACED O RING AND LEATHER BACK UP RING SEALING THE MANIFOLD TO THE SQUIB VALVE. RE-INSTALLED SQUIB VALVE ASSY TO THE CYLINDER AND RE PRESURIZED CYLINDER WITH NITROGEN. NO LEAKS DETECTED. CYLINDER RE INSTALLED ONTO FLOAT. 1G72 3U H3EU 20040511000152004051100015SW 2004 5 11 BAQA092500 120040422A2930222375016101 INDICATOR BELL 222 222U 1182140SW HYD OIL READS HIGH A BAQAO OTHER O OTHER NRNOT REPORTED 1 AL03587MG5419 47566 TEP GAUGE READS 50 DEGREES HIGH. ABOVE P.O. NR WAS CUT FOR A/C S/N 47534, BUT WAS USED ON A/C S/N 47566. REPLACED WITH SERVICABLE UNIT. 05/04/2004 1G72 3U H9SW 20040511000202004051100020NM 2004 5 11 UPS04242342 120040415A5347 CARGO TRACK BOEING727 72722C 138400FNM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, SECTION OF TIE DOWN RAIL IS CORRODED FROM BS530 TO BS480 IN LOWER FWD CARGO COMPARTMENT. CORRODED SECTION OF TIE DOWN RAIL REMOVED IAW SRM 51-30-2. TIE DOWN RAIL FABRICATED IAW DRG. NO.:66-01573 INSTALLED NEW TIE DOWN RAIL IAW SRM 51-30-2 2L73 4F A3WE 20040511000212004051100021NM 2004 5 11 DL76S040392 120040501A5551182T1306 FITTING BOEING767 767332 1382001NM HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27131DN 24852 INSPECTION OF THE HORIZONTAL STABILIZER PIVOT FITTING ATTACH FASTENER HOLE BORES REVEALED A CRACK INDICATION IN A SINGLE FASTENER HOLE COMMON TO THE FITTING SPLICE PLATES ON THE LT & RT SIDES. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS AND PROVIDE AND INSURANCE CUT. OVERSIZE BOLTS WERE INSTALLED IN THE HOLES. THE REPAIR WAS ACCOMPLISHED PER ER/A 089789-14, REV A. 2L72 4F RTA1NM 20040511000242004051100024WP 2004 5 11 UPS04842328 120040405A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, NLG RT CTR TUNNEL AREA (ACCESS THUR AFT PRESS PAL) FRAME & BRKT GOUGED JUST FWD OF PWR RECP BOX BLEND GOUGE IAW DC8 SRM 53-2-0, FIG 1F ORINGINAL THICKNESS .050 REMAIN ING MATERIAL OF .036 OUT OF LIMITS. ROUNDED GOUGE ON BRAKETT EDGE REPA IR ANGLES, 7075-0-03 PO 441313-2 MATERIAL ID FOR -35 FILLER .125 707 5T6 PO 424554-3 IAW DC8 TR 53-125 HEAT TREATED REPAIR ANGLES FAB AN GLES ALODINES & PRIMED & INSTALLED REPAIR ANGLES 51-1-8 & 51-1-20D 2L74 4F RT4A25 20040511000262004051100026NM 2004 5 11 DL738040393 120040504A2751S256A40450 TRANSMITTER BOEING737 737832 13844CFNM T/E FLAP DEFECTIVE A DALAO OTHER N FALSE WARNING APAPPROACH 1 SO273740C 30800 ON APPROACH INTO LA GUARDIA AT 1500 FEET FLAPS INITIALLY WERE SPLIT AT INDICATION 25. THE SPLIT IN THE NEEDLE THEN WENT AWAY BUT THE FLAPS WOULD MOVE NO FURTHER THAN 25 DEGREES. REPLACED FLAP POSITION TRANSMITTER. 2L72 4F RTA16WE 20040511000272004051100027NM 2004 5 11 DLM88040394 120040504A335060030451 BATTERY PACK DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27902DE 53379 CABIN SEAT EMERGENCY LIGHTING INOP ROW 18 THRU 23. REPLACED BATTERY PACK AND BATTERIES AT ROW 18. 2L72 4F RTA6WE 20040511000292004051100029WP 2004 5 11 UPS04842331 120040420A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, SEAT TRACK C/H STA 1120-1140 GOUGED, REMOVED GOUGES IAW DC8 SRM 53-2-0 & FOUND TO BE OUT OF LIMITS REMOVED FLOOR PANEL F90 & F94 FOR ACCESS. LOCATE NEW SEAT TRACK DRILLED EXISTING FASTENER HOLES ALODINE & PRIME IAW 51-1-8. LOCATE SEAT TRACK SPLICES & DRILLED FASTENERS HOLES IAW UPS EO 5320-8309. INSTALLED SEAT TRACK SPLICES & FLOOR BOARDS IAW 51-3-0 & UPS EO 5320-8309. 2L74 4F RT4A25 20040511000302004051100030NM 2004 5 11 DL73S040395 120040426A5755 SKIN BOEING737 737232 1384475NM RT SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 DENT & CRACK ON LWR SIDE OF I/B GROUND SPOILER 1.5 INCH FWD OF T/E AFT OF INBOARD ACTUATOR. 2L72 4F RTA16WE 20040511000312004051100031NM 2004 5 11 DL738040396 120040504A5350149A72551 FAIRING BOEING737 737832 13844CFNM FUSELAGE MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27379DA 30349 WING TO BODY FAIRING PANEL 192JL FOUND MISSING ON ARRIVAL. REPLACED PANEL 192JL. 2L72 4F RTA16WE 20040511000322004051100032WP 2004 5 11 UPS04842332 120040406A534047516251 FITTING DOUG DC8 DC871F 302199DWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, 680 LONGERON 11 LT LOWER AFT FITTING IS CRACKED, REMOVED CRACKED FITTING P/N 4751625-1 IAW DC8 SRM 51-3-0,51-1-20D & 51-1- 21 LOCATED AND DRILLED NEW FITTING IAW DAC DWG 4751625 AND DC8 SRM 51- 1-24 AND INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21, & 51-3-0 2L74 4F RT4A25 20040511000332004051100033WP 2004 5 11 UPS04842333 120040405A534736575041 SEAT TRACK DOUG DC8 DC871F 302199DWP COCKPIT WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, ENGINEER SEAT TRACKS HAVE ELONGATED HOLES. REMOVED F/E SEAT TRACKS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED FWD AND AFT TRACKS P/N 3657504-1 IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SR M 51-3-1 2L74 4F RT4A25 20040507000422004050700042SW 2004 5 7 ALGA094321 120040503A6320407340032101 BEARING BELL 407 407 1182206SW TRANSMISSION SPALLED D ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL A221 53243 TRANSMISSION DISASSEMBLED FOR METAL CONTAMINATION, FOUND BEARING BREAKING DOWN. REMOVED AND REPLACED BEARING. 1G71 3U O H2SW 20040507000642004050700064GL 2004 5 7 GO42004F00000 220040412A7320500N720155 CONTROL CABLE HUGHES500N 500N 3027374SW ALLSN 250C 250C20 03013GL FWD THRUST BROKEN B GO4RO OTHER O OTHER NRNOT REPORTED 1 WP13501HP1456 LN064 DURING DAILY INSP, THE THRUSTER ASSY SYSTEM WAS OPERATED TO CHECK THE OPERATION AND SMOOTHNESS OF THIS SYSTEM. A LOUD NOISE WAS HEARD AND THE THRUSTER CONE WAS DISCONNECTED FROM THE CONTROL SYSTEM. UPON REMOVING THE TAILBOOM FAIRING TO GET ACCESS TO THE INTERCONNECT CABLES, CLOSER LOOK AT THIS CABLE END AND IT APPEARS THAT THE CABLE END HAS CORROSION FROM THE INSIDE OUT. REQUESTED COPY OF METALLURGY TEST. (WP13200401531) 1G71 3U3 UNCH3WE E4CE 20040507000662004050700066SW 2004 5 7 ALGA094364 120040504A6230412040101129 MAST BELL 412 412EP 1182205SW MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XATTF2489 A723 36273 FOUND MAST ASSY. CORRODED IN AREA WHERE BEARING IS SEATED AND INSIDE VALLEY AREA ABOVE BEARING SEAT. CORROSION PITTING BEYOND 412 BHT CR&O LIMITS. SCRAPPED MAST. 1G72 4U H4SW 20040507001142004050700114NM 2004 5 7 CALA0400433 120040427A532065621257 ATTACH ANGLE BOEING737 7373T0 1384582NM LT MLG WW WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 DEEP WEAR AROUND FASTENERS ON LEFT AFT WHEEL WELL PANEL ATTACH ANGLE ON KEEL BEAM BETWEEN BS 715 & 272, 12 X 1 INCH. REPAIRED PER ECRA 5311-01195. 2L72 4F RTA16WE 20040507001252004050700125NM 2004 5 7 CALA0400413 120040424A335020121 CHARGER BOEING737 7373T0 1384582NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714337 23575 THREE EMERGENCY LIGHTS OVER EMERGENCY ESCAPE HATCH ARE INOP. REPLACED BATTERY CHARGERS AND BATTERIES PER MM 33-51-51. 2L72 4F RTA16WE 20040507001442004050700144EA 2004 5 7 COMA0460290 120040501A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01999CA 7230 FLIGHT 5884, 4 ROWS OF EMERGENCY LIGHTS ARE INOP. DEFERRED MAINT ON EMERGENCY LIGHTS PER MEL. 2L72 4F RTA21EA 20040507001452004050700145EA 2004 5 7 COMA0460264 120040417A274070608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB FAULTY A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01915CA14512 7013 FLIGHT 5344, AFTER TAKEOFF RECEIVED A STAB/MACH TRIM CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE DEPARTING CITY EVV. REPLACED THE HSTCU. 2L72 4F RTA21EA 20040507001472004050700147EA 2004 5 7 COMA0460275 120040422A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01989CA 7215 FLIGHT 5206 DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION AT 30 DEGREES WHEN SELECTED TO 45. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20040507001622004050700162EA 2004 5 7 COMA0460291 120040430A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01965CA 7131 FLIGHT 5005 LEFT THRUST REVERSER UNLOCKED CAUTION. SECURED AND DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040507001682004050700168EA 2004 5 7 COMA0460271 120040413A49901603662 OIL COOLER CNDAIRCL600 CL6002B19 1900309EA APU DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01416CA 7450 FLIGHT 5015 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL COOLER. 2L72 4F RTA21EA 20040510000022004051000002EA 2004 5 10 SWIA200413181 120040413A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 MAIN FUSELAGE PULLEY INTERCOSTAL CRACKED AT 2 LOCATIONS FS 484.00 RBL 27.0 AND RBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F4 FRTA21EA E15NE 20040510000042004051000004SO 2004 5 10 SWIA200413223 120040425A215022045404 ACM EMB 120 EMB120ER 3260203SO AIR CONDITIONER MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07561SW 120335 UNABLE TO COOL COCKPIT WITH ENGINE OR APU BLEED, LOW OR NORM SELECTED ON GROUND. SMOKE IN COCKPIT ASSOCIATED WITH DUCT OVERHEAT LIGHT. REPLACED AIR CYCLE MACHINE IAW MM 21-50-05, OPS CHECK GOOD. 2L72 4T RTA31SO 20040510000052004051000005SO 2004 5 10 SWIA200413225 120040424A3350 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07190SW 120050 REAR SECTION EMERGENCY LIGHTS DOES NOT ILLUMINATE. REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 17366-04-001, S/N OFF 397. 2L72 4T RTA31SO 20040510000082004051000008EA 2004 5 10 SWIA200413228 120040424A2697 TERMINAL CNDAIRCL600 CL6002B19 1900309EA LT ENG OVHT LOOPLOOSE A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07597SW 7293 LEFT JET OVERHEAT FAIL MESSAGE INTERMITTENTLY ILLUMINATED AND THEN STAYED ON STEADY EN ROUTE. THE MESSAGE STAYED ILLUMINATED WITH SELECTION OF BOTH A AND B LOOPS. MESSAGE CONTINUED TO CYCLE ON AND OFF. INSPECTED WIRING AT LEFT ENGINE JET PIPE, FOUND 3 LOOSE TERMINALS. REPAIRED LOOSE TERMINALS AS REQUIRED. OPS CHECK GOOD. 2L72 4F RTA21EA 20040510000102004051000010SO 2004 5 10 SWIA200413230 120040424A3350 PANEL EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07563SW 120338 EMERGENCY LIGHT PANEL ON FLOOR IN GALLEY BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT ON FLOOR AT GALLEY IAW EMB 120 MM 20-10-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20040510000142004051000014EA 2004 5 10 SWIA200413251 120040416A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 RIGHT BATT RIB AT WS 53.60 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. 2L72 4F RTA21EA 20040510000212004051000021EA 2004 5 10 SWIA200413258 120040426A3097 SCREW CNDAIRCL600 CL6002B19 1900309EA TERMINAL BLOCK LOOSE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07431SW 7536 LEFT WINDSHIELD SMELLED LIKE SULFUR, PUFF OF SMOKE JUST BEFORE CIRCUIT BREAKER POPPED. FOUND LOOSE SCREW ON LEFT WINDSHIELD HEAT TERMINAL BLOCK (P1). REPLACED WIRE CONNECTOR AND HARDWARE. OPS CHECK GOOD. 2L72 4F RTA21EA 20040510000232004051000023SO 2004 5 10 SWIA200413144 120040401A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07190SW 120050 ON THE GROUND WITH FLAP LEVER AT UP POSITION, CONTROL FAULT, FLAP AND ADVANCED SWS APPEAR INTERMITTENTLY. REPLACED FLAP ANNUNCIATOR IAW MM 20-21-00, MM 27-50-05. S/N OFF: 2151. REPAIRED AND REPOSITIONED WIRE W110-2909-2H WHICH WAS CHAFING AND SHORTING ON FLAP ANNUNCIATOR CASE IN OVERHEAD PANEL. 2L72 4T RTA31SO 20040510000252004051000025SO 2004 5 10 SWIA200413146 120040413A273152991 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM0758733 120197 ELEVATOR TRIM ACTUATOR FREEZES UP AT HIGH ALTITUDES. SIGNIFICANT SNAP-BACK WITH BOTH MANUAL AND ELECTRIC TRIM INPUTS, 17,000 FT AND HIGHER. REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS WITH SERVICEABLE UNITS IAW AMM 27-32-02. OPS CHECK GOOD. P/N: 5299-1. 2L72 4T RTA31SO 20040510000492004051000049NM 2004 5 10 AALA20040529 120040505A3397 WIRE BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21972AN 30097 MEX LEFT FORWARD OVERWING EMERGENCY LIGHTS CAME ON WITH NO POWER. REPLACED SPLICE SP828 CONNECTING WIRES W3142043720 WITH W3142PB AS PER STANDARD WIRING PRACTICE MANUAL. PERFORMED PROXIMITY SWITCH ELECTIC UNIT BITE FOR LEFT FORWARD OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040510000552004051000055EA 2004 5 10 COMA0460268 120040415A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01420CA 7451 FLIGHT 5688 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040510000652004051000065EU 2004 5 10 MALA040341 120040422A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU NR 3 ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15531XJ E2365 THE HYDRAULIC GREEN HI TEMP CAME ON CLIMBING THRU 25000 FT. QRH PROC ACCOMPLISHED AND THE GREEN HI TEMP LIGHT WENT OUT ABOUT 3-5 MIN LATER. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 ENG HYD PUMP P/N 521449, S/N OFF MX644694, S/N ON F9840810 PER AMM 29-10-17 201. RAN AC HYD SYSTEM DURING 1/2 ENGINE RUN AT RUN PAD, OPS AND LEAK CHECKS GOOD, NO DEFECTS NOTED. 2H74 4F RTA49EU 20040510000762004051000076SO 2004 5 10 C2XA04SH270 120040507A532014525422005 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE LEFT HAND AFT CARGO FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 68 TO FRAME 71. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510000792004051000079SO 2004 5 10 C2XA04BT059 120040419A2612M835366022M RELAY EMB 145 EMB145LR 3260212SO FIRE WARNING SYSFAILED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2713550 145575 SAV CO3462, CREW REPORTED, "FIRE LIGHT INDICATION ON CLIMBOUT IN BAGGAGE COMPARTMENT" DECLARED EMERGENCY, PERFORMED OVERWEIGHT LANDING, LANDED UNEVENTFULLY. MAINTENANCE PERFORMED INSPECTION OF BAGGAGE COMPARTMENT, PERFORMED OVERWEIGHT LANDING INSPECTION, AND PLACED BAGGAGE COMPARTMENT FIRE DETECTION ON MEL AIRCRAFT RETURNED TO SERVICE. AIRCRAFT ARRIVED IN EWR, MAINTENANCE REMOVED AND REPLACED RELAY KO625 IAW EMB145 MM #26-15-00, OPS CHECKED GOOD. REMOVED FROM MEL. AIRCRAFT RETURNED TO SERVICE. SDR CLOSED. 2L72 4T RTT00011AT 20040510000892004051000089NM 2004 5 10 AALA20040522 120040503A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21967AN 29545 BDL EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 7 THROUGH 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040510000992004051000099SO 2004 5 10 C2XA04SH254 120040429A532014521721009 STRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 14 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001022004051000102SO 2004 5 10 C2XA04BT056 120040428A3350110049 BATTERY PACK EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714947 145054 EWR-CO2528, CREW REPORTED, "EMERGENCY LIGHTS INOPERATIVE FROM FLIGHT ATTENDANTS CONTROL PANEL." MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK, OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040510001192004051000119NM 2004 5 10 AALA20040515 120040502A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21794AN 30256 LHR EMERGENCY LIGHT AT FIRST CLASS GALLEY BROKEN. REPLACED EMERGENCY LIGHT UNIT AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTT00001SE 20040510001262004051000126SO 2004 5 10 C2XA04BT057 120040428A33503025101 SOCKET EMB 145 EMB145ER 3260211SO CABIN DAMAGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 BTV-CO2248, DURING 4A INSPECTION, MAINTENANCE FOUND THE LEFTHAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP SOCKET ASSEMBLY. OPS CHECKED EMERGENCY LIGHTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040510001302004051000130NM 2004 5 10 AWXA200400437 120040408A532069353656 FLOOR SUPPORT BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD CABIN FLOOR SUPPORT ANGLE BETWEEN BS 380 AND BS 400, AT BL "0". MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE FROM BS 380 TO BS 400, AT BL "0"; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT ANGLE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3. 2L72 4F RTA16WE 20040510001322004051000132NM 2004 5 10 AWXA200400438 120040405A57536546431279 SKIN BOEING737 7373S3 1384711NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE L/H OUTBOARD AFT FLAP SEPARATING AT THE AFT INBOARD CORNER WS 230.68. MAINTENANCE PERFORMED A BOND REPAIR IAW B737-300 SRM 51-70-10, FIG. 10. 2L72 4F RTA16WE 20040510001412004051000141SO 2004 5 10 C2XA04SH268 120040506A532014525382001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE RIGHT HAND CENTER CARGO FLOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001462004051000146NM 2004 5 10 AWXA200400482 120040406A5755654645165 PANEL BOEING737 7373S3 1384711NM RT WING SPOILER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON NR 6 SPOILER PANEL ABOVE ACTUATOR AT WBL 245 RT. MAINTENANCE REMOVED AND REPLACED NR 5 SPOILER PANEL IAW AMM 27-62-11, FIG. 401, PG. 1-5. 2L72 4F RTA16WE 20040510001532004051000153NM 2004 5 10 AWXA200400398 120040406A53206545855 RETAINER BOEING737 7373Y0 1384671NM DOOR SEAL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF INNER CHORD AT R-2 DOOR LOWER FLOOR SEAL BS 990, STR 17 R/H, RBL 50. MAINTENANCE REMOVED DAMAGED INNER CHORD AT R-2 DOOR LOWER FLOOR SEAL BS 990, STR 17 R/H, RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040510001842004051000184NM 2004 5 10 AWXA200400409 120040402A5311654653949 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1" CRACK WAS FOUND IN FRAME FOOT AT BS 616, LBL 65, WL 202. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME FOOT AT BS 616, LBL 65, WL 202; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5311-01143-DD1. 2L72 4F RTA16WE 20040510001912004051000191NM 2004 5 10 AWXA200400443 120040405A57536546431279 SKIN BOEING737 7373S3 1384711NM FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 89.5 INCHES FROM INBOARD END WS 378 TO WS 386. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR ON LT OUTBOARD FORE FLAP FROM WS 378 TO WS 386; FABRICATED A REPAIR DOUBLER; BONDED REPAIR PART TO FORE FLAP IAW B737-300 SRM 51-70-10, FIG. 17. 2L72 4F RTA16WE 20040510002002004051000200NM 2004 5 10 AWXA200400473 120040428A5315146N53156 STIFFENER BOEING757 757225 1384959NM FLOORBEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 DURING C-07 CHECK EXFOLIATION CORROSION WAS FOUND ON TEE ANGLE STIFFENER UNDER SHEAR DECK BS 1716, BL "0". MAINTENANCE REMOVED CORRODED TEE ANGLE STIFFENER AT BS 1716, BL "0"; FABRICATED A NEW REPLACEMENT ANGLE STIFFENER PER DWG 146N5315; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-01, PARA. C. 2L72 4F RTA2NM 20040510002102004051000210EU 2004 5 10 AWXA200400424 120040327A5313D5348004720601 STRINGER AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 31 RT, AFT OF FR 65 BELOW OUTFLOW VALVE. MAINTENANCE REMOVED CORRODED SECTION OF STRINGER 31 RT AT FR 65+10; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12 & 18. 2L72 4F RTA28NM 20040510002142004051000214NM 2004 5 10 UPS04242318 120040414A5320 DOUBLER BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE:C OLD REPAIR DOUBLER HAS SIGNS OF INTERGRANULAR CORROSION IN LOWER NOSE COMPT, DOUBLER LOCATED ON VERTICAL INTERNAL STRUCTURE OF NWW RBL 14.6 B STA 314. REMOVED OLD REPAIR. HFEC CW NDF. NEW DOUBLER INSTALLED IAW SRM 51-10-02 AND 51-30-02. 2L73 4F A3WE 20040510002162004051000216NM 2004 5 10 UPS04242321 120040427A5320 SUPPORT BOEING727 72722C 138400FNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE:C CRACK ON SUPPORT STRUCTURE IN NWW RT FWD AREA. SUPPORT STRUCTURE REMOVED REF NRC NR 748078, SUPPORT STRUCTURE FABRICATE D IAW SRM 51-20-1, SUPPORT STRUCTURE INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20040510002202004051000220NM 2004 5 10 2004UALA00373 120040420A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 AFT PIT FLOOR FRAME T-CAP DENTED AT FRAME 1600 LBL 13. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW T-CAP. 2L74 4F4 FRTA20WE E24NE 20040510002372004051000237NM 2004 5 10 2004UALA00383 120040420A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 CABIN R1 DOOR SURROUND STRUCTURE INTERCOSTAL ANGLE HAS A CRACK AT BS 291 BETWEEN STR 9R AND 10R. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20040510002552004051000255NM 2004 5 10 2004UALA00385 120040421A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29772UA 26930 EMERGENCY LIGHT AT AISLE SEAT 24G INOPERATIVE. RELAMPED, OPS CK GOOD. 2L72 4F4 FRTT0001SE E46NE 20040510002602004051000260NM 2004 5 10 2004UALA00393 120040425A5210 DOOR FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE L1 DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 DOOR 1L MED FRAME CRACKED AROUND CENTER BOX. FABRICATED & INSTALLED REPAIR DOUBLER. 2L74 4F4 FRTA20WE E24NE 20040510002612004051000261NM 2004 5 10 2004UALA00394 120040425A5230 STRUCTURE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 FWD CARGO DOOR FWD EDGE 36 INCHES FROM TOP DENTED. FABRICATED & INSTALLED FILLER & DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20040510002702004051000270NM 2004 5 10 2004UALA00403 120040423A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29390UA 24665 STRINGER IS DENTED AT BS420 S24L. FABRICATED AND INSTALLED STRINGER REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20040510002772004051000277NM 2004 5 10 2004UALA00410 120040428A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 AFT PIT RT SIDE STA 2120 T-CAP FOR WASTE TANK SUPPORT FITTING CRACKED RBL 41 - 33. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW T-CAP SECTION. 2L74 4F4 FRTA20WE E24NE 20040510002862004051000286NM 2004 5 10 2004UALA00419 120040104A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29657UA 27112 EEL LIGHTS BLINKING FROM ROWS 20 TO 28 CHECKED SYSTEM PER WDM33-51-11 & 33-51-14, SPLICES SM42, SM41,SM5 OVER M1559 OK. SPLICES SM44, SM43 & SM45 OVER M1556 ALSO OK. 2L72 4F4 FRTA1NM E24NE 20040511000122004051100012EU 2004 5 11 ERAA094455 120040215A3212D24873101 FLOAT BOLKMS105 BO105S 5626006EU LT MLG LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03293EH 559 LT FLOAT ASSY DUE 6 MONTH INSPECTION. CYLINDER PN 2370039 SN 959 DUE HYDROTESTING 2-04. CHECK VALVES PN B17573-5 ON FLOAT BAG LEAKING. ELBOW CORRODED ACTION TAKEN: REPLACED CYLINDER SN 959 WITH SERVICEABLE CYLINDER SN 615. REMOVED AND REPLACED 2 EA CHECK VALVES AND REPLACED ELBOS PN B17794-1. CHECKED FOR COMPLIANCE WITH SB 120-813, 120-87-4, 120-82-4, 120-84-1, 802-25-1 & 802-25-2. 1G72 3U H3EU 20040511000172004051100017NM 2004 5 11 UPS04M42325 120040502A3260 WARNING LIGHT DOUG MD11 MD11 3023602NM MLG ILLUMINATED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01251UP DURING CLIMB GOT LT GEAR UNSAFE AFTER RETRACT. BOTH PRIMARY AND SECOND ARY GEAR INDICATIONS INDICATED UNSAFE. CYCLED GEAR NO HELP. UPON GEAR EXTENTION GOT ALL GREEN. REF WAN 888619 PER TECH SUPPOET REC R/R'D PSEU LT MLG ALT & #3 ENG LH EDP PER AMM 32 33 20 29 11 20 & 31 71 01 TS WIRES TO PROX SWS SWUNG GR W HYD TEST STAND OPS PRIMARY & SECONDARY INDICATION GOOD. 2L73 4F RTA22WE 20040511000232004051100023NM 2004 5 11 UPS04242344 120040426A5530 FRAME BOEING727 72722C 138400FNM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, VERT STAB JACKSCREW CUTOUT LT, FWD FRAME CRACKED AT FW STA 128 APPROX. CRACKED FRAME REMOVED IAW SRM 51-30-02. NEW FRAME INSTALLED IAW SRM 51-30-02 2L73 4F A3WE 20040511000282004051100028WP 2004 5 11 UPS04842330 120040422A53403750505502 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE:C-1 CORROSION AROUND FASTENER HOLE ON L35 RT STA 1040-1060 INTERNAL AFT PIT, REMOVED INTERCOSTAL & CLIP AT STA 1040 - 1060 RT L35 RT IAW DC8 SRM 51-1- 20D. FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-1 EVOL LONGERON SPLIC E 51-1-20D, FOUND TO BE CRACK, RECEIVED, LOCATED & DRILLED UP LONGERON SPLICE 3750545-502 IAW 51-1-24. INSTALLED LONGERON SPLICE IAW 51-1-2 0D,51-1-20D FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-0 2L74 4F RT4A25 20040511000342004051100034NM 2004 5 11 DLM88040397 120040505A5270BAN7024501 SWITCH DOUG MD88 MD88 3023688NM TAIL CONE FAILED A DALAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO27913DL 49544 FOUND DURING L/O CHECK WHILE LOOKING IN TAIL COMPARTMENT FOUND CABLE FREE FOR TAIL CONE DEPLOYMENT SYSTEM WITH NO LIGHT INDICATION IN COCKPIT OF TAIL CONE DEPLOYMENT. FOUND SWITCH S1-537 NOT ACTUATING / COMPLETING CIRCUIT. REPLACED SWITCH PER M/M, NOW LIGHT ILLUMINATES NORMALLY. 2L72 4F RTA6WE 20040511000372004051100037NM 2004 5 11 UPS04M42248 120040220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 12 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 12 RT REMOVED PER SRM51-21-01 VOL II REV 34 MATERIAL REMOVED 0.059 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1105-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2L73 4F RTA22WE 20040511000392004051100039NM 2004 5 11 DL73S040377 120040427A5330654576621 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10L LAP JOINT BETWEEN BS 360 AND 540. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 090052-14. 2L72 4F A16WE 20040511000402004051100040NM 2004 5 11 DLM88040378 120040425A5510279002350 STOP FITTING DOUG MD88 MD88 3023688NM HORIZ STAB BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27916DL 49591 DURING OP 5924 AD FOUND LOWER MECHANICAL STOP MADE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKEN OFF. REPLACED JACKSCREW AND STOP ASSY. ADJUSTED STABILIZER JACKSCREW CONTROL AND INDICATION PER M/M. RIG CHECKED AND OPS CKS GOOD. 2L72 4F RTA6WE 20040511000422004051100042NM 2004 5 11 UPS04M42249 120040225A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 5 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 5 RT REMOVED PER SRM 51-21-01 VOL II REV 34, MATERIAL REMOVED 0.018" IS WITHIN LIMITS PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1106-04. BUSHNG FABRICATED AND I NSTALLED PER EO MD11-5510-19409-D. (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2L73 4F RTA22WE 20040511000452004051100045EU 2004 5 11 AWXA200400491 120040508A7711 LINE AIRBUS320 A320231 3930325EU EPR CONTAMINATED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28621AW 053 PHX - ABORTED TAKEOFF - FLT 0743 - ON TAKEOFF AT PHX EN ROUTE FOR CMH RECEIVED EPR MODE FAULT ON NR 1 ENGINE WITH THRUST BUMP SELECTED, REJECTED TAKEOFF 70 KTS. ISSUED MEL 73-20-04 COND 1, EPR MODE INOP. ON 05/08/2004 IN PHX MAINTENANCE FLUSHED MOISTURE OUT THE P5 LINE WITH COMPRESSED AIR AND TIGHTENED A LOOSE B-NUT ON THE P5 LINE AT THE 6 O'CLOCK POSITION, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000472004051100047EU 2004 5 11 AWXA200400448 120040327A3350E0052R8B3APNE CONNECTOR AIRBUS320 A320232 3930326EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28640AW 448 MCN - EEL - DURING C-08 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED AT SEAT ROW 24 LT. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR AT EMERGENCY ESCAPE PATH LIGHT HARNESS SEAT ROW 24 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000482004051100048EU 2004 5 11 AWXA200400449 120040417A5321D53670048000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 6 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 261DF BETWEEN FR 66 AND FR 68, Y765 LT AND Y765 RT. MAINTENANCE REMOVED CRACKED FLOOR PANEL BETWEEN FR 66 AND FR 68, Y765 LT AND Y765 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70048, AND A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20040511000492004051100049NM 2004 5 11 AWXA200400450 120040414A143069367491 BOLT BOEING737 7373S3 1384711NM VETICAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT VERTICAL STABILIZER FORWARD SPAR TO BODY BOLT IAW T/C I6B5502. 2L72 4F RTA16WE 20040511000502004051100050NM 2004 5 11 AWXA200400451 120040413A143069702515 BOLT BOEING737 7373S3 1384711NM VERTICAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT BS 1085, STR 2 RT. MAINTENANCE REMOVED AND REPLACED RT AFT INBOARD VERTICAL STABILIZER ATTACH BOLT IAW T/C I6B55002. 2L72 4F RTA16WE 20040511000532004051100053NM 2004 5 11 AWXA200400454 120040421A575465C2660220 PANEL BOEING737 7373S3 1384711NM L/E SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN NR 5 SLAT OUTBOARD COVE PANEL SKIN AT STAB STA 255.7. MAINTENANCE REMOVED CRACKED NR 5 SLAT OUTBOARD COVE PANEL AT SS 255.7; FABRICATED A NEW REPLACEMENT PANEL PER DWG 65C26602; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-04 FIG 1. 2L72 4F RTA16WE 20040511000542004051100054NM 2004 5 11 UPS04M42251 120040225A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 16 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AN D BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 16 LT REMOVED PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.051 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1103-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20015) 2L73 4F RTA22WE 20040511000552004051100055EU 2004 5 11 AWXA200400455 120040429A5270 WARNING SYSTEM AIRBUS320 A320231 3930325EU CARGO DOOR FAULTY A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28633AW 082 ON TAKEOFF AT LAS EN ROUTE FOR SMF AT 60 KTS RECEIVED ECAM MESSAGE AFT CARGO DOOR OPEN REJECTED TAKEOFF AT 80 KTS AND RETURNED TO GATE. MAINTENANCE DETERMINED WARNING WAS CAUSED BY MALFUNCTION IN THE INDICATION SYSTEM, DOOR WAS SECURED. ISSUED MEL 52-70-1, COND 8, AFT CARGO DOOR INDICATION INOP. MAINTENANCE FOUND AFT CARGO DOOR LEVER ASSEMBLY AND BEARING WORN, REMOVED AND REPLACED ENTIRE AFT CARGO DOOR LOCKING MECHANISM IAW AMM 52-31-21, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000562004051100056NM 2004 5 11 AWXA200400456 120040423A532069432331 SUPPORT ANGLE BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL SUPPORT ANGLE AT BS 794.3, RBL 20. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL SUPPORT ANGLE, BS 794.3, RBL 20; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 2-3, 8, & 12. 2L72 4F RTA16WE 20040511000572004051100057NM 2004 5 11 AWXA200400457 120040430A2560P4010021 BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28175AW 23634 DEN - EMERGENCY EQUIPMENT - DURING A-01 CHECK FOUND THE FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040511000592004051100059 2004 5 11 AWXA200400459 420040502A2565D30665105 SLIDE AIRBUS320 A320231 3930325EU L2 DOOR DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW448984166 091 PHX - EEL/EES - DURING 4-DAY CHECK EMERGENCY LIGHT TEST FAILED WITH AFT LT BATTERY INDICATING FAULTS AT EXTERIOR LOADS. MAINTENANCE REMOVED AND REPLACED L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25301, LIGHT TEST WAS GOOD. 2L72 4F RTA28NM 20040511000612004051100061NM 2004 5 11 AWXA200400461 120040502A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 25 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT ROW 25 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040511000632004051100063NM 2004 5 11 UPS04M42252 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 19 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 19 LT REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMOVED 0.006 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1101-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20015) 2L73 4F RTA22WE 20040511000642004051100064NM 2004 5 11 AWXA200400463 120040406A561069264692 CAMSHAFT BOEING737 7373Y0 1384671NM COCKPIT WINDOW WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 LCQ - EES - DURING C-15 CHECK THE FIRST OFFICERS SLIDING WINDOW WOULD NOT OPEN USING THE EXTERNAL EMERGENCY HANDLE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS SLIDING WINDOW HANDLE SHAFT ASSEMBLY CAM IAW BMM 56-10-02, PG 602, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040511000662004051100066 2004 5 11 DL73S040382 420040430A344220412170416 TRANSCEIVER BOEING737 737247 138448DNM WX RADAR FAILED A DALAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SO27242WA 23516 WX RADAR FAILED ON T/O. REPLACED R/T UNIT. 2L72 4F A16WE 20040511000672004051100067NM 2004 5 11 UPS04M42254 120040217A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 28 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF NR 28 RT HOLE REMOVED PER SRM51-21-01 VOL II REV 34 MATERIAL REMOVED 0.036 INCHES IS WITHIN LIMIT PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1048-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018) 2L73 4F RTA22WE 20040511000682004051100068NM 2004 5 11 DLM88040383 120040430A2932ST107Q TRANSMITTER DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING A DALAK NONE K FLUID LOSS APAPPROACH 1 SO27945DL 49818 WHILE CONFIGURING THE AIRCRAFT FOR APPROACH, THE LEFT HYDRAULIC QUANTITY DECREASED TO 3 QUARTS. SERVICED SAME TO FULL. FOUND HYD PRESS TRANSMITTER LEAKING. REPLACED TRANSMITTER, RAN HYD AND NO LEAKS FOUND PER M/M. OPS CKS GOOD. 2L72 4F RTA6WE 20040511000692004051100069NM 2004 5 11 DL767040384 120040427A5753113T22012A STRUCTURE BOEING767 767232 1385132NM T/E FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27105DA 22217 RIGHT I/B FLAP ATTACH BOLTS HOLES CORRODED. REPAIRED PER ERA 089397-14MA REF NRC402 404 400 403 399 401. 2L72 4F RTA1NM 20040511000702004051100070NM 2004 5 11 DLM88040385 120040501A3320 BALLAST DOUG MD88 MD88 3023688NM CABIN FAULTY A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27922DL 49646 WISPY SMOKE REPORTED OVER SEAT 25DE. REPLACED BALLAST, CHECKS GOOD. 2L72 4F RTA6WE 20040511000712004051100071NM 2004 5 11 DL757040386 120040502A2121216001003 FAN BOEING757 757232 1384965NM CARGO BAY FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27615DL 22822 RT RECIRC FAN SHUTDOWN INFLIGHT AND PRODUCED AN ACRID SMELL. SMELL DISSIPATED AFTER FAN SWITCH SHUT OFF. REPLACED FAN. 2L72 4F RTA2NM 20040511000722004051100072NM 2004 5 11 DL76K040387 120040502A3350 BATTERY BOEING767 767332 1382001NM COCKPIT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27178DZ 30596 COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPS OK. 2L72 4F RTA1NM 20040511000742004051100074NM 2004 5 11 DL76L040389 120040502A3320 LIGHT BOEING767 767332 1382001NM AFT GALLEY MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27189DN 25990 ELECTRICAL ODOR COMING FROM RT SIDE AFT GALLEY (DUTYFREE CART AREA). REPLACED WORK LIGHT. 2L72 4F RTA1NM 20040511000752004051100075NM 2004 5 11 UPS04M42255 120040217A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 31 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMO VED 0.022 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1050-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. (REF. UPS ENGINEERING FILE NR MD11-55-20018) 2L73 4F RTA22WE 20040511000762004051100076NM 2004 5 11 UPS04M42256 120040223A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 4 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 04 LT REMOVED PER SRM 51-21-01 VOL II REV 34 MATERIAL REMOVED 0.058 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1064-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20014) 2L73 4F RTA22WE 20040511000792004051100079NM 2004 5 11 UPS04M42259 120040221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 22 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING. CORROSION AT BOTTOM OF HOLE NR 22 LT REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMOVED 0.045 INCHES IS WITHIN LIMIT PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1053-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409-D. (REF. UPS ENGINEERING FILE NR MD11-55-20015) 2L73 4F RTA22WE 20040511000812004051100081NM 2004 5 11 UPS04442362 120040507A3350 LIGHT BOEING747 747212B 1384886NM SERVICE DOOR INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01526UP 21937 UPPER DECK SERVICE DOOR FRAME EMERGENCY LIGHTS 2EA INOP. PANEL OPENED FOR ACCESS TO BATTERY PACK. APPLIED POWER TO A/C & ALLOWED EMERGENCY LIGHTS TO CHARGE SEVERAL HOURS. UPPER DECK DOOR LTS OPERATED NORMAL PER B747 MM 33-51-04 INSTALLED & SECURED PANEL. 2L74 4F A20WE 20040511000822004051100082NM 2004 5 11 UPS04242355 120040414A5320 RETAINER BOEING727 72722C 138400FNM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, FWD RT SEAT RETAINER ON NLG WW CUTOUT CORRODED SEAL RETAINER REMOVED, SEAL RETAINER FABRICATED IAW SRM 51-20-1, SEAL RETAINER INSTALLED MM 20-80-01 2L73 4F A3WE 20040511000832004051100083NM 2004 5 11 UPS04242356 120040415A5320 RETAINER BOEING727 72722C 138400FNM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, SEAL RETAINER ON NWW CUTOUT FWD LHS CORRODED SEAL RETAINER REPLACED IAW SRM 51-20-01 AND AMM 20-80-01 2L73 4F A3WE 20040511000842004051100084NM 2004 5 11 UPS04242357 120040413A5754 WEB BOEING727 72722C 138400FNM KREGUER FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, 5 FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB CRACKED. K FLAP ACTUATOR REMOVED, TRUNNION SUPPORT BOX I/B WEB REMOVED. WEB FABRICATED IAW DWG 65-16263. NEW K FLAP ACTUATOR TRUNNION SUPPORT BOX I/B WEB FITTED IAW SRM 51-30-02 2L73 4F A3WE 20040511000872004051100087NE 2004 5 11 UPS04442243 220040422A7200 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 2 FLAMED OUT A IPXAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO01676UP 20101 DURING CRUISE NR 2 ENG FLAMED OUT AT 37K DURING CROSSFEED FROM NR 3 TANK. OIL PRESS REMAINED 10PSI, N1 25 PERCENT, N2 28 PERCENT ENG WAS SHUTDOWN FOR APPROX 25MIN. CREW ATTEMPTED RESTART AT 33K PER QRH - NO JOY, CREW COMPLETED ENG SEVERE DAMAGE CHECKLIST. COMPLIED WITH MM 71-00-42 AND MM 72-00-00 NO DEFECTS NOTED. REF. ITEM 3 LOGPG 195499 SUSPECT CROSSFEED VALVE AT FAULT RAN ENG NR 2 NO DEFECTS NOTED. 2L74 4F4 F A20WE E20EA 20040511000882004051100088NM 2004 5 11 UPS04442261 120040423A2910 LINE BOEING747 747121 1384871NM NR 2 HYD SYS LEAKING A IPXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01681UP 19661 DURING INITIAL CLIMB LOST ALL QUANTITY AND PRESS IN HYD SYS NR 2. EMERGENCY DECLARED. FOUND NR 2 HYD SYS PRESSURE MODULE PRESSURE LINE LEAKING. REMOVED AND REPLACED NR 2 HYD SYS PRESSURE MODULE LINE LEAK. CHECKED GOOD AT THIS TIME. 2L74 4F A20WE 20040511000902004051100090WP 2004 5 11 UPS04842312 120040419A5347547553952400 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, UPPER CARGO PIT BETWEEN STA 822 TO 837 FLOORBEAM AT STA 822 AT SEAT TRACK (E) IS CORRODED. CUT SEAT TRACK REPAIR FLOORBEAM INSTALLED NEW SEAT TRACK AND 4 EACH FITTING SPLICE. 2L74 4F RT4A25 20040511000912004051100091NM 2004 5 11 UPS04M42311 120040429A5210 BOTTLE DOUG MD11 MD11F 3023600NM L1 PAX DOOR LOW A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP ON PREFLIGHT, FOUND DOOR IN DEPLOY HANDLE POSITION, FOR PNEUMATIC BOTTLE OPERATION. SERVICED L1 PAX DOOR EMERGENCY RELEASE BOTTLE IAW MD11 MM 12-25-04. PRESSURE HOLDING AT 1500 PSI. 2L73 4F RTA22WE 20040511000962004051100096WP 2004 5 11 UPS04842338 120040402A53139754913 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE:C-1 FWD PIT BETWEEN STA 200-300 LONGERON 34R CORRODED RMVD FASTENERS L34R FS 190-300 & FROM SHEARTIES & FRAMES AT FS 200& 220 AT L34R TO FOM. RMVD CORR FROM L34R AT FS 205-217. ORIG THICKNESS IS .092 MAT RMVD .030 MAT REMAINING.062 & IS OUT OF LIMITS. RMVD CORR FROM VER TICAL LEG L34R. ORIG THICNESS .063 MAT RMVD .027 MAT REMAINING .036 OU T OF LIMITS RMVD L STRAP SPLICED 2 EA HEAT TREATED INSTALLED. 2L74 4F RT4A25 20040511000972004051100097WP 2004 5 11 UPS04842339 120040401A53473772660 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSLEAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, SEAT TRACK STA 1700 LOBES BROKEN OFF. SEAT TRACK FOUND OUT OF LIMITS IAW DC8 SRM & UPS EO 5340-12053. REMOVED SEAT TRACK IAW 51-1-200 & 51-30 MAT ID SEAT TRACK P/N 3772660 IAW 53-7-1 LACATED & DRILLED HOLE IN SEAT TRACK F STA 1670-1710 IAW 51-1-24. ALODINE & PRIME IAW 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0 2L74 4F RT4A25 20040511000982004051100098WP 2004 5 11 UPS04842340 120040422A53475475539524000N SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, MAIN CABIN SEAT TRACK G & H AT FS 418 HAS EXFOLIATION. SEAT TRACK AREA DAMAGED RMVD LOCATED AND DRILLED NEW SEAT TRACK SPLICE FITTING AND SPLICE CHANNEL IAW EO DC8 5320-8309-D. INSTALLED IAW EO DC 8 5320-8309D. 2L74 4F RT4A25 20040511000992004051100099WP 2004 5 11 UPS04842345 120040407A53133750347503 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, LT MLG WW L34 BOTTOM SIDE GOUGED FWD STA 980. REMOVED ADF PANEL AND LONGERON IAW DC8 SRM 51-3-0 AND 51-1-20D. FABRIC ATED LONG -503 IAW DAC DWG 3750347. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -503 LONGERON IAW DC8 SRM 51-1-20D. INSTALLED ADF PANEL IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040511001002004051100100WP 2004 5 11 UPS04842347 120040406A53203754065 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, FWD LWR CARGO STA 300 TO 308 L33R DOUBLER WITHIN TORQUE BOX CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0 . FABRICATED NEW DOUBLER FROM 7075-T6 .063 IAW DC8 SRM 51-1-24 AND DAC DWG 3254065. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REMOVED OLD DOUBLER AND INSTALLED NEW DOUBLER IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040511001022004051100102WP 2004 5 11 UPS04842264 120040331A5743 FITTING DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER FWD. UPPER BOLT OF RIGHT MAIN LANDING GEAR RETRACT ACTUATOR UPPER MOUNT BRACKET SPOT FACED LUG,OVERSIZED HOLE,FABBED AND INSTALLED FILLER AND REPLACE- MENT BUSHING IAW E.O. DC8-5740-1636 2L74 4F RT4A25 20040511001032004051100103WP 2004 5 11 UPS04842265 120040331A5743 FITTING DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, EVIDENCE OF CORROSION UNDER BOLTS AND BRACKET AT LT MLG. RETRACT ACTUATOR LOWER BOLTS ON UPPER MOUNT BRACKET. OVERSIZED FWD. UPPER MOUNT HOLE FOR RETRACT ACTUATOR,FABRICATED AND INSTALLED BUSHING IAW E.O. DC8-5740-1636 2L74 4F RT4A25 20040511001062004051100106NM 2004 5 11 UPS04M42292 120040217A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 16 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.059 INCHES. BARREL NUT HOLE REPAIRER PER EN 1135-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20012). 2L73 4F RTA22WE 20040511001102004051100110NM 2004 5 11 04FDEA01171 120040510A5753 ACTUATOR DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. I/B ACTUATOR LUG HOLE REMOVED CORROSION AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001112004051100111NM 2004 5 11 04FDEA01172 120040510A5753 ACTUATOR DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.401, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.400 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001122004051100112NM 2004 5 11 04FDEA01173 120040510A5753 ACTUATOR DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001152004051100115NM 2004 5 11 04FDEA01176 120040510A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.502, MATERIAL REMOVED 0.004, REMAINING THICKNESS 0.498 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001172004051100117WP 2004 5 11 04FDEA01008 120040419A5711ARB0007501 SPAR CAP DOUG MD10 MD1010F 3022112WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH FEDEX EA 8-5710-77344 WINGS BASIC LEFT WINGS, LOWER AFT SPAR CAP REPAIR. COMPLIED WITH EA 8-5710-77344 WINGS - BASIC LEFT WING, LOWER AFT SPAR CAP REPAIR. 2L73 4F RTA22WE 20040511001182004051100118NM 2004 5 11 04FDEA01061 120040422A5320ABA8225505 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN STA 427 RBL 8.5 FLOOR PANEL SUPPORT CORRODED. FWD CABIN STA 427 RBL 8.5 FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040511001212004051100121NM 2004 5 11 CALA0400480 120040508A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 540, RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5331-01146. 2L72 4F RTA16WE 20040511001222004051100122NM 2004 5 11 UPS04M42295 120040220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.040 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1140-04 (UPS ENGINEERING FILE NR MD 11-55-20017). 2L73 4F RTA22WE 20040511001232004051100123NM 2004 5 11 UPS04M42296 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 33 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.028 INCH. BUSHINGS FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1137-04 (REF UPS ENGINEERING FILE NR MD11-55-20018). 2L73 4F RTA22WE 20040511001242004051100124NM 2004 5 11 UPS04M42297 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 05 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & S IDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.0006 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIR PER EN 1012-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2L73 4F RTA22WE 20040511001252004051100125NM 2004 5 11 UPS04M42298 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 8 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1013-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2L73 4F RTA22WE 20040511001272004051100127WP 2004 5 11 UPS04842349 120040331A534037558201 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, MAIN CABIN, FRAME FITTING CRACKED ON BOTH SIDES FS 427 L11L (DOT 6603). REMOVED TEE FITTING TO GAIN ACCESS TO CRACKED FITTING, REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING P/N 3755820- 1 IAW DC8 SRM 51-1-24 & DAC DWG 3755820 ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040511001282004051100128WP 2004 5 11 UPS04842350 120040401A5320 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, STA 1560-1580 L21L CUSP MEMBRANE GOUGED. REMOVED GOUGE ON CUSP TONGUE IAW DC8 SRM 53-2-0. OUT OF LIMITS. FABRICATED CUSP IAW DAD DWG 9750448. FABRICATED SPLICES IAW REO G09789. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP SECTION AND SPLICE ANGLES IAW DC8 SRM 51-1-20D INSTALLED FITTING IAW DC8 SRM 51-1-20D. INSTALLED DUCT IAW DC8 MM 20-11-00 & 36-11-01. 2L74 4F RT4A25 20040511001292004051100129WP 2004 5 11 UPS04842351 120040402A5321 FLOORBOARD DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, MAIN DECK FLOOR PANEL CORRODED STA 50 LBL 14. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS. FABBED SPLICE PLATES IAW DC8 SRM 53-2-3; LOCATED, DRILLED, AND COUNTERSUNK NEW FLOOR PANEL SECTION IAW DC8 SRM 51-1-24. ALOD & PRIMED IAW DC8 SRM 51-1-8. INSTALLED ROLLER TRAY FITTING IAW DC8 SRM 51-1-21A, INSTALLED FLOOR PANEL SECTION AND CEILING PANELS IN LOWER PIT A IAW DC8 SRM 51-3-0 & 51-3-1. 2L74 4F RT4A25 20040511001322004051100132NM 2004 5 11 UPS04242309 120040428A2160 A/C PACK BOEING727 727185C 138406NNM COCKPIT OVERTEMP A IPXAO OTHER O OTHER CRCRUISE 1 SO01940UP 19826 JUST AFTER T/O COCKPIT FILLED WITH FUMES, RIGHT PACK TEMP WAS 170'. TURNED OFF PAC FUMES STOPPED. ALL C/B'S CHECKED & IN PAC FAN OPS NORMAL. R/R 35 FT CONTROL VALVE PER AMM 21-51-42, OPS CHECK GOOD. 2L73 4F A3WE 20040511001342004051100134NM 2004 5 11 UPS04M42286 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 29 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AN D SIDEWALL SURFACE. CORROSION REMOVED AT BOTTOM SURFACE MATERIALS REMOVED 0.050 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19409D. 2)BARREL NUT HOLE REPAIRED PER EN 1027 3)BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409D (REF. UPS ENG INEERING FILE NR MD11-55-20017). 2L73 4F RTA22WE 20040511001362004051100136NM 2004 5 11 UPS04M42288 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 35 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & S IDEWALL SURFACE. CORROSION REMOVED PER SRM 51-2101 VOL2 REV34 MATERIAL REMOVED 0.0716. BARREL NUT HOLE REPAIRED PER EN 1016-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20018). 2L73 4F RTA22WE 20040511001402004051100140NM 2004 5 11 UPS04M42291 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 17 BARREL NUT HOLE FOUND WITH CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.054. BARREL NUT HOLE REPAIRED PER EN 1026-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20015). 2L73 4F RTA22WE 20040511001412004051100141NM 2004 5 11 UPS04M42268 120040223A5310 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. BOTTOM CORROSION AT HOLE NR 15 LT REMOVED PER SRM51-21-01 VOL II REV 34, M MATERIAL REMOVED 0.045 INCH IS WITHIN LIMIT PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1102-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20015). 2L73 4F RTA22WE 20040511001422004051100142NM 2004 5 11 UPS04M42300 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STAB LT NR 11 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.030. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1069-04 & EN 1014-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2L73 4F RTA22WE 20040511001432004051100143NM 2004 5 11 UPS04M42269 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 29 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION REMOVED AT NR 29 HOLE BOTTOM PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.027 FOUND WITHIN LIMIT AS PER EO MD11-5510-19409 D. BARREL NUT HOLE REPAIRED PER EN1018-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018). 2L73 4F RTA22WE 20040511001442004051100144NM 2004 5 11 UPS04M42270 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 11 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED AT NR 11 HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL II REV 34, MATERIAL REMOVED 0.030 FOUND WITHIN LIMIT PER EO MD11-5510-19409D . BARREL NUT HOLE REPAIRED PER EN1021-04. BUSHING FABRICATED A ND INSTALLED PER EO MD11-5510-19409D (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2L73 4F RTA22WE 20040511001452004051100145NM 2004 5 11 UPS04M42271 120040215A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 31 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. MINOR SURFACE CORROSION ON BOTTOM OF HOLE NR 31 REMOVED PER SRM 51-21-01 VO L II REV 34, MATERIAL REMOVED 0.008 WITHIN LIMITS OF EN1042-04. BARREL NUT HOLE REPAIRED PER EN1042-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2L73 4F RTA22WE 20040511001462004051100146NM 2004 5 11 UPS04M42272 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C HORIZONTAL STABILIZER RT NR 07 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 07 RT REMOVED PER SRM 51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.115 IS WITHIN LIMIT PER EN1052-04. 2. BARREL NUT HOLE REPAIRED PER EN1052-04. BUSHING FABRICATED AND INSTALLED P ER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2L73 4F RTA22WE 20040511001482004051100148NM 2004 5 11 UPS04M42274 120040220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 34 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 34 LT REMOVED PER SRM 51-21-01 VOL II REV 34 MATERIAL REMOVED 0.042 IS WITHIN LIMIT PER EN1060-04. 2. BARREL NUT HOLE REPAIRED PER EN1060-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017). 2L73 4F RTA22WE 20040511001562004051100156NM 2004 5 11 ASAA0440060 120040303A531065528780102 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FLOOR CREASE BEAM AT L2 JAMB CORRODED STATION 947 TO 1006. REMOVED AND REPLACED CREASE BEAM CHORD STATION 947-1006 LBL 50. (M) 2L72 4F RTA16WE 20040511001582004051100158NM 2004 5 11 ASAA0440057 120040303A532065C333672 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - AFT GALLEY AREA FORE TO AFT FLOOR SUPPORT CHORD HAS CORROSION STATION 947 TO 967 LBL 50. REMOVED AND REPLACED SUPPORT STATION 947-967 LBL 50. (M) 2L72 4F RTA16WE 20040511001622004051100162NM 2004 5 11 ASAA0440054 120040303A53476546813104 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND MAIN DECK SEAT TRACK AT STATION 344 LBL 26.5 UPPER SURFACES OF INBOARD AND OUTBOARD FLANGES CORRODED. REPAIRED SEAT TRACK AT STATION 344 LBL 26.5. (M) 2L72 4F RTA16WE 20040511001632004051100163NM 2004 5 11 ASAA0440044 120040225A531565C3394028 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND MAIN DECK FLOORBEAM AT FS 294.5 UPPER T-CAP UPPER SURFACE HAS SEVERAL AREAS OF CORROSION FROM LBL 24 TO RBL 50. REPAIRED UPPER CHORD AT STATION 294.5 FROM LBL 24 TO RBL 50. (M) 2L72 4F RTA16WE 20040510000192004051000019 2004 5 10 SWIA200413256 420040424A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AILERONS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07213SW8950 8950 120277 FEEL A BINDING WHEN MOVING AILERONS. REMOVED AND REPLACED AILERON SERVO WITH SERVICEABLE UNIT IAW EMB 120 MM CHAPTER 22-10-05. OPS CHECK GOOD. 2L72 4T RTA31SO 20040510000472004051000047WP 2004 5 10 AALA20040528 120040504A1420 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW219616 53563 MIA EMERGENCY LIGHTS AT SEAT 25D INOPERATIVE. RECONNECTED AND SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20040510000542004051000054NE 2004 5 10 COMA0470032 220040419A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NR 2 OVERHEATED A COMAC ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 SO01721CA13737 7259 807542 FLIGHT 5711 DURING TAKEOFF ROLL AT 80 KNOTS NR 2 ENGINE ITT REACHED 906C DEGREES, ABORTED T/O AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040510000562004051000056NM 2004 5 10 DL75A040390 120040503A2131211738813 CONTROLLER BOEING757 757212 1384951NM CABIN PRESSURE INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27757AT 23127 AT 37,000 FT CABIN ALTITUDE HORN CAME ON. SWITCHED TO AUTO 2 WITH NO IMMEDIATE ALT MOVEMENT, SO SWITCHED TO MANUAL. REPLACED NR 1 AUTO PRESSURE CONTROLLER. 2L72 4F RTA2NM 20040510000782004051000078SO 2004 5 10 C2XA04CL044 120040428A213122250N030301 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE FAILED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2714953 145071 BTV FLIGHT NR 2441 THE CREW REPORTED SMOKE COMING FROM THE DIGITAL PRESSURE CONTROLLER. MAINTENANCE REPLACED THE DIGITAL PRESSURE CONTROLLER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040510000942004051000094EU 2004 5 10 AALA20040502 120040426A2571 BATTERY BOX AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2180057 465 TUL CORROSION FOUND ON FORWARD SIDE OF AIRCRAFT EXTERNAL POWER BOX CENTERLINE BETWEEN FRAME 18 AND FRAME 19 AT STATION 1340. REPAIRED POWER BOX PER ESO 30595 DATED 4/26/04. (CLOSED) 2L72 4F RTA35EU 20040510001002004051000100SO 2004 5 10 C2XA04SH258 120040430A711014576526008 STRUCTURE EMB 145 EMB145LR 3260212SO NR 2 COWLING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712564 145618 SHV-DURING C CHECK THE NR 2 ENGINE LOWER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040510001012004051000101SO 2004 5 10 C2XA04SH259 120040503A532014522460013 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAME 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001082004051000108WP 2004 5 10 AALA20040506 120040428A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21279AA 49295 LAX LEFT AND RIGHT HAND OVERWING EMERGENCY EVACUATION EXTERIOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT HAND OVERWING EMERGENCY EVACUATION EXTERIOR LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20040510001142004051000114NM 2004 5 10 AALA20040507 120040429A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21691AA 25697 DFW EMERGENCY LIGHTS AT ROWS 27 THROUGH 36D INOPERATIVE. REPLACED BATTERY PACK M10801 FOR EMERGENCY LIGHTS AT ROWS 27 THROUGH 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20040510001162004051000116SO 2004 5 10 C2XA04SH255 120040430A531514522461015 DOUBLER EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV-DURING C CHECK THE DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040510001312004051000131SO 2004 5 10 C2XA04CL050 120040505A1430 SCREW EMB 145 EMB145XR 3260214SO EMERGENCY EXIT WRONG PART A C2XAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW2717146 145746 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE WRONG GRIP LENGTH SCREW INSTALLED ON THE DOOR SURROUND LINER. THE SCREW WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD OF THE DOOR. 2L72 4F RT 20040510001362004051000136SO 2004 5 10 C2XA04BT058 120040501A2120 ODOR EMB 145 EMB145XR 3260214SO COCKPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2712126 145693 GSO-CO3472, CREW REPORTED, "SMOKE SMELL IN COCKPIT DURING DESCENT." MAINTENANCE IN GSO INSPECTED THE AIRCRAFT. NO EVIDENCE OF SMOKE SMELL. ALL SYSTEMS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20040510001422004051000142NM 2004 5 10 AWXA200400480 120040405A534765468131 SEAT TRACK BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK EXFOLIATION CORROSION AND A 1 INCH CRACK WAS FOUND ON SEAT TRACK BS 420 TO BS 425, RBL 45. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK FROM BS 380 TO BS 480, RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK PER DWG 65-46813; INSTALLED REPAIR PART IAW B737-300 SRM 53-30-52, FIG. 1. 2L72 4F RTA16WE 20040510001432004051000143SO 2004 5 10 C2XA04IA052 120040503A3350M3902931229 PIN EMB 145 EMB145LR 3260212SO CONNECTOR LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715912 145439 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE PIN AT THE LIGHT CONNECTOR TO BE LOOSE. THE PIN WAS RE-INSERTED INTO THE AFFECTED CONNECTOR, THE LIGHT OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040510001452004051000145SO 2004 5 10 C2XA04TY078 120040506A532014522460015 PLATE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714516 145323 TYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT DIGITAL PLATE AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE AFT DIGITAL PLATE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040510001482004051000148NM 2004 5 10 AWXA200400394 120040401A521065458713 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK A 3/8 INCH CRACK WAS FOUND IN R-1 DOOR UPPER HINGE SKIN AT DRAIN HOLE. CRACK WAS FOUND CONTAINED AT HOLE, MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER IAW E.O. 52-00-02. 2L72 4F RTA16WE 20040510001552004051000155NM 2004 5 10 AWXA200400399 120040410A53126537607 VERTICAL BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 DURING C-15 CHECK 2 EACH 7/8 INCHES CRACKS WERE FOUND IN VERTICAL BEAM ON AFT SIDE OF BS 178 BULKHEAD AT LBL 5.7, WL 184. MAINTENANCE REMOVED DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL BEAM AT LBL 5.7, WL 184; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-08, FIG. 205. 2L72 4F RTA16WE 20040510001592004051000159NM 2004 5 10 AWXA200400401 120040410A531265175837 BULKHEAD BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND IN LT VERTICAL BEAM WEB ON AFT SIDE OF BS 178 BULKHEAD AT LBL 5.7, WL 190. MAINTENANCE REMOVED CRACKED L/H VERTICAL BEAM WEB ON AFT SIDE OF BS 178 BULKHEAD AT LBL 5.7, WL 190; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-17583; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-08, FIG. 1. 2L72 4F RTA16WE 20040510001632004051000163SO 2004 5 10 C2XA04CL047 120040505A32221170C000001 STRUT EMB 145 EMB145ER 3260211SO NLG FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714940147706957 145033 CLE FLIGHT NR 2676 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF FROM CLE. THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR STRUT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040510001692004051000169NM 2004 5 10 AWXA200400468 120040426A5320146N5318 SHEAR WEB BOEING757 757225 1384959NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 LCQ - MAJOR REPAIR - DURING C-07 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CABIN SHEAR DECK BETWEEN BS 1710 AND BS 1720, LBL 20 TO RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CABIN SHEAR DECK FROM BS 1710 TO BS 1720, LBL 20 TO RBL 20; FABRICATED A FILLER, DOUBLER, AND REPAIR HAT SECTION; INSTALLED REPAIR PARTS IAW B757-200, SRM 53-60-51, FIG. 203, PG. 1-5. 2L72 4F RTA2NM 20040510001712004051000171EU 2004 5 10 AWXA200400403 120040328A5315D53472192260 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM Y765 L/H FROM FR 66 AND FR 70; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-41-14, FIG. 1. 2L72 4F RTA28NM 20040510001782004051000178NM 2004 5 10 AWXA200400392 120040402A53206545834256 STIFFENER BOEING737 7373G7 1384595NM FLOOR SUPPORT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND AROUND FASTENER HOLES ON FLOOR SUPPORT STIFFENER BETWEEN BS 312 AND BS 328, RBL 11.05, WL 208.1. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR SUPPORT STIFFENER BETWEEN BS 312 AND BS 328, RBL 11.05, WL 208.1; FABRICATED A NEW REPLACEMENT SECTION OF STIFFENER PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12, PG. 1. 2L72 4F RTA16WE 20040510001822004051000182NM 2004 5 10 AWXA200400408 120040402A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 4 INCH CRACK WAS FOUND IN UPPER SURFACE OF CABIN FLOORBEAM UPPER CHORD AT BS 660, BL 0.07. MAINTENANCE REMOVED DAMAGED SECTION OF UPPER TEE BS 660, LBL 0.07; FABRICATED 2 EACH REPAIR STRAPS & SPLICE ANGLES; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5702-04110-SS1. 2L72 4F RTA16WE 20040510001932004051000193NM 2004 5 10 AWXA200400445 120040411A555169736972 BOLT BOEING737 7373S3 1384711NM HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON THE RT HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT BS 1088, WL 258. MAINTENANCE REMOVED AND REPLACED R/H HORIZONTAL STABILIZER FORWARD LOWER ATTACH BOLT IAW T/C I6C55038. 2L72 4F RTA16WE 20040510001972004051000197NM 2004 5 10 AWXA200400470 120040504A3397D9299200900200 WIRE HARNESS AIRBUSA319 A319132 3930340NM SEAT ROW 14 LT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 14 LT FROM WALL DISCONNECT 7260V TO SEAT CONNECTOR 5751VC-A, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040510001992004051000199 2004 5 10 AWXA200400472 420040504A2565D30665105 SLIDE AIRBUS320 A320231 3930325EU L-2 DOOR LEAKING A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28633AW6739 908 082 FLIGHT CREW REPORTED THE L-2 DOOR SLIDE PRESSURE WAS LOW. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040510002062004051000206EU 2004 5 10 AWXA200400420 120040329A5315D53472189200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 R/H FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9. 2L72 4F RTA28NM 20040510002082004051000208EU 2004 5 10 AWXA200400422 120040402A5347D53472176200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 LT, BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT, FROM FR 47 TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, FIG. 9-13, & 18. 2L72 4F RTA28NM 20040510002252004051000225NM 2004 5 10 2004UALA00378 120040419A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29848UA 1647 EMERGENCY EXIT LIGHTS ARE FLASHING IN ARMED POSITION. 2L72 4F4 FRTA28NM E40NE 20040510002282004051000228NM 2004 5 10 2004UALA00381 120040420A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 CABIN FUSELAGE FRAME CLIP CRACKED AT BS 400 STRINGER 4L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20040510002292004051000229NM 2004 5 10 2004UALA00266 120040319A2150123CH1B SENSOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE E/E BAY FAILED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29911UA 25255 RETURNED TO FIELD DUE TO EQUIPMENT COOLING FAN. FOUND EXHAUST FLOW SENSOR BAD AND REPLACED. 2L72 4F4 FRTA16WE E2GL 20040510002312004051000231EU 2004 5 10 2004UALA00363 120040416A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29453UA 1001 1 INCH BY 2 INCH HOLE PUNCTURED IN SKIN BETWEEN FRAME 20-21 AND STRINGERS 28-29 ON R-H SIDE OF FWD FUSELAGE APPROX 5 INCHES FWD OF AFT AVIONICS ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER. FABRICATED & INSTALLED EXTERNAL SKIN DOUBLER. 2L72 4F4 FRTA28NM E40NE 20040510002332004051000233NM 2004 5 10 2004UALA00365 120040418A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29390UA 24665 WHEEL WELL PRESSURE PANEL CRACKED AT STA 673 AND LBL 31. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND T-ANGLE STIFFENER. 2L72 4F4 FRTA16WE E2GL 20040510002352004051000235EU 2004 5 10 2004UALA00367 120040416A2920 LINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RAM AIR TURBINE LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29453UA 1001 RAM AIR TURBINE DEPLOYED BUT DID NOT PROVIDE BLUE HYDRAULIC PRESSURE DURING ROUTINE MAINTENANCE TEST. NO EMERGENCY GENERATOR POWER AVAILABLE VIA RAT. FOUND LOOSE B-NUT AT RAT MODULE, TIGHTEN LINE. REMOVED AND REPLACED RAT GROUND CHECK MODULE. OPERATIONS CHECK NORMAL 2L72 4F4 FRTA28NM E40NE 20040510002392004051000239NM 2004 5 10 2004UALA00389 120040108A2781 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 WP29574UA 26686 RETURNED TO THE FIELD WITH A SLAT DISAGREE MESSAGE. EXCESSIVE TORQUE LOAD IN SLAT DRIVE SYSTEM. ACCOMPLISHED SLAT LUBE AND PERFORMED BITE OF ALL THREE FSEU'S. FOUND NO CURRENT FAULTS. PREVIOUS FLIGHT FAULTS INDICATE LE SLAT DISAGREE WITH NO FAULTED UNIT. FOUND ROTARY ACTUATOR NR 5 INBD OVERLOAD INDICATOR POPPED. NR 5 ROTARY ACTUATOR REPLACED. 2L72 4F4 FRTA2NM E17NE 20040510002412004051000241EU 2004 5 10 F3LA200400053 220040419A7397 WIRE BOEING737 7373M8 1384615NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENGINE NICKED A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03303FL 25039 AIR TURN BACK. FLIGHT CREW REPORTED NR 2 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. FOUND A NICK IN WIRE INSULATION AT CLAMP. REPLACED WIRE AND CLAMP PER BWM 73-34-00. 2L72 4F4 FRTA16WE E21EU 20040510002422004051000242NM 2004 5 10 F3LA200400050 120040419A5320 FLOOR SUPPORT BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT SEGMENT AT STA 957, LBL 50. REPLACED FLOOR SUPPORT SEGMENT PER SRM 51-40-02, 53-60-51 AND BOEING DRAWING 65C33369. 2L72 4F RTA16WE 20040510002442004051000244NM 2004 5 10 F3LA200400057 120040416A3397 WIRE BOEING737 737300 1384610NM LT WING SHORTED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1214 23177 WHILE PERFORMING OPERATIONAL TEST OF LT OTBD LANDING LIGHT, FOUND SHORT IN LT WING WIRE BUNDLE, AFT SPAR INBD OF NR 1 ENGINE PYLON, AFT. RESPLICED W802-001-16 WIRE SECTION AT RSS 283 AND RSS 230 ON LT WING T/E PER WPM 20-10-13 AND 20-30-12. PERFORMED OPERATIONAL TEST OF LT WING INBD LANDING LIGHT AND CHECKED NORMAL PER MM 33-42-11. REPAIRED WIRING ON LT WING ENG PYLON FOR FUEL SHUTOFF, FLAP POSITION TRANSMITTER, AND NR 2 SPOILER SENSOR DUE TO SHORTED WIRING. 2L72 4F RTA16WE 20040510002522004051000252 2004 5 10 2004UALA00371 420040418A2565 CONNECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EVAC SLIDE LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29648UA 25285 LT OVERWING SLIDE SQUIB TEST FAILED. PROBLEM CAUSED BY LOOSE CONNECTORS. PROBLEM CLEARED BY RE-SEATING CONNECTORS ON BACK OF FLIGHT DECK PANEL. 2L72 4F4 FRTA1NM E24NE 20040510002622004051000262NM 2004 5 10 2004UALA00395 120040426A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29547UA 25368 EXTERNAL FUSELAGE SKIN AT BS600 STR 16L - 19L IS DAMAGED. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040510002632004051000263NM 2004 5 10 2004UALA00396 120040426A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29547UA 25368 FRAME AT BS 1681 WL 208 IS DAMAGED. INSTALLED FRAME DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040510002672004051000267 2004 5 10 2004UALA00400 420040426A3442 RADAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE WX RADAR FAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29653UA 25391 DIVERTED TO MIA DUE TO LOSS OF WEATHER RADAR. FLIGHT CREW REPORTED A GREEN BAND ON THE RADAR DISPLAY APPROX. 6.5 MILES IN FRONT OF AIRCRAFT. MAINTENANCE REPLACED C-BAND WX RADAR CONTROL PANEL. SHOP FOUND CONTROL PANEL TILT CONTROL MISADJUSTED TO 14.5 DEGREES DOWN WITH TILT CONTROL SET AT ZERO. IN FLIGHT, WITH THE TILT CONTROL SET TO ZERO, ANTENNA WOULD BE TILTED DOWN 14.5 DEGREES AND WOULD BE RECEIVING SIGNIFICANT GROUND RETURN. THIS WOULD SHOW UP AS A GREEN BAND ON THE RADAR DISPLAY. 2L72 4F4 FRTA1NM E24NE 20040510002682004051000268NM 2004 5 10 2004UALA00401 120040426A2920 HYDRAULIC SYSTEM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE B SYSTEM MALFUNCTIONED A UALAK NONE J WARNING INDICATION LDLANDING 1 WP29938UA 26671 FLIGHT LANDED UNDER AMBER ALERT DUE TO THE LOSS OF THE 'B' HYDRAULIC SYSTEM. NORMAL LANDING AND TAXI. AFTER ARRIVAL AT GATE, MAINTENANCE TECHNICANS FOUND THE B HYDRAULIC SYSTEM ACOUSTIC FILTER ASSEMBLY LEAKING. THE EMDP CASE DRAIN FILTER WAS INSPECTED BUT NO METALIC PARTICLES WERE FOUND. THE ACCOUSTIC FILTER ASSEMBLY WAS REPLACED AND AN EXTERNAL LEAK CHECK WAS PERFORMED. 2L72 4F4 FRTA16WE E2GL 20040510002712004051000271NM 2004 5 10 2004UALA00404 120040426A5512 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZ STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 L/E HORIZ STAB LE IS DENTED AT LE STA 115. TRIMED OUT DAMAGE, INSTALLED INTERNAL DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20040510002792004051000279NM 2004 5 10 2004UALA00412 120040428A5610 WINDOW BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT VIBRATES A UALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP29656UA 25394 RETURNED TO FIELD WITH A COCKPIT WINDOW VIBRATION. THE VIBRATION WAS CAUSED BY A LOOSE TAPE THAT WAS APPLIED ON WINDOW 3L TO PROTECT UNCURED (SOFT) SEALANT. THE SEALANT WAS APPLIED WHEN THE EXISTING NR 3L WINDOW WAS REPLACED, 2L72 4F4 FRTA1NM E24NE 20040510002882004051000288NM 2004 5 10 2004UALA00060 120040123A21317638101 CONTROLLER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN PRESSURE MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29911UA 25255 RETURNED TO THE FIELD WHEN UNABLE TO PRESSURIZE PLANE. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED LEAK CHECK. PRESSURIZED ACFT SEVERAL TIMES ON GROUND ACFT PRESSURIZED NORMAL. NO HARD FAULT WAS ISOLATED. ALL RESPECTIVE ATA SYSTEMS AND SUB-SYSTEMS WERE CHECKED. REPLACED CABIN PRESSURE CONTROLLER (CPC) AS PRECAUTIONARY. 2L72 4F4 FRTA16WE E2GL 20040511000042004051100004EU 2004 5 11 AWXA200400488 120040509A1420E0053R8B3ASNF CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 26 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 26 L/H. MAINTENANCE REPAIRED A BROKEN WIRES AT BULKHEAD CONNECTOR SEAT ROW 26 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000132004051100013EU 2004 5 11 ERAA094456 120040106A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU RT MLG LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03134EH9750 635 LEAKING. FLOAT BOTTLE CYLINDER PN 32370039 SN 765 DUE HYDRO 5/04. FLOAT BOTTLE SQUIB VALVE LEAKING IN BETWEEN VALVE AND MANIFOLD. ACTION TAKEN: REMOVED SQUIB VALVE. PN 609005 SN 1401 FROM CYLINDER SN 765. SENT CYLINDER OFF FOR HYDROTESTING. REPAIRED LEAK IN SQUIB VALE AND INSTALLED ONTO SERVICEABLE CYLINDER SN 808. PERFORMED REGULAR 6 MONTH INSPECTION ON REMAINDER OF FLOAT ASSY. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1G72 3U H3EU 20040511000162004051100016EU 2004 5 11 BAQA094310 120040503A771454487099111 INDICATOR BOLKMSBK117 BK117C1 5626025EU N1 RPM INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117NC2274 7517 GAUGE BACKLIGHTING INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 05/05/2004 1G72 3U NCH13EU 20040511000252004051100025WP 2004 5 11 UPS04842329 120040418A5532 SKIN DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, LEFT HORIZONTAL STAB LEADING EDGE INBD OF CENTER 3 EACH POPPED RIVETS REMOVED & INSTALLED LT HORIZONTAL STAP L/E 331F TO FOM IAW DC8 SRM 51-3 -0. RMVD FASTENERS IAW DC8 SRM 51-1-21A. FOUND SKIN TO BE CRACKED. CUT OUT DAMAGE & FAB REPAIR DOUBLER IAW DC8 SRM 55-2-1 FIG 4. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-2 1 & 51-1-21A. 2L74 4F RT4A25 20040511000362004051100036NM 2004 5 11 UPS04M42246 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 04 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 04 RT REMOVED PER SRM 51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.046 INCHES IS WITHIN LIMIT PER EO MD11-5510-19409D. REWORKED HOLE PER EN1051-04. BUSHING FABRICATED PER EO MD11-551 0-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20016) 2L73 4F RTA22WE 20040511000622004051100062NM 2004 5 11 AWXA200400462 120040502A30402312 CONTROL UNIT BOEING737 7373G7 1384595NM COCKPIT DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28156AW496931497 23778 AFTER TAKEOFF, LT FORWARD WINDOW OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH BUT LIGHT REMAINED ON, TURNED BACK DUE TO KNOWN ICING CONDITIONS AT MCI. MAINT FOUND A LOOSE WIRE IN TERMINAL LUG AT CIRCUIT BREAKER, RE-TERMINATED WIRE. R & R LT FWD WINDOW ANTI-ICE CIRCUIT BREAKER AND LT FORWARD WINDOW HEAT CONTROL UNIT IAW BMM, OPS CHK OF WINDOW ANTI-ICING SYSTEM GOOD. FUNCTIONAL TEST OF WINDOW HEAT CONTROL UNIT S/N 7103 CONFIRMED FAILURE OF UNIT FOR OUTPUT TEST. TEARDOWN OF UNIT FOUND TRANSFORMER T1 ARCING, REPLACED TRANSFORMER AND DEFECTIVE PARTS IAW CMM 30-40-02, REV. 14. 2L72 4F RTA16WE 20040511000732004051100073NM 2004 5 11 DLM88040388 120040502A2912 FITTING DOUG MD88 MD88 3023688NM CASE FILTER LEAKING A DALAE ENGINE SHUTDOWN K FLUID LOSS TXTAXI/GRND HDL 1 SO27901DE 53378 ON TAXI IN LOST ALL HYDRAULIC PRESSURE ON BOTH SIDES WITH ENGINES RUNNING AND ELECTRICAL PUMPS ON. QUANTITY WAS NORMAL. FOUND LT FWD CASE DRAIN FILTER LEAKING FROM OUTBOARD FITTING. TIGHTENED FITTING AND CLEANED AREA. PRESSURE AND INDICATIONS ALL NORMAL ON ENG RUN. 2L72 4F RTA6WE 20040511000922004051100092WP 2004 5 11 UPS04842334 120040405A534736575031 SEAT TRACK DOUG DC8 DC871F 302199DWP COCKPIT WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, ENGINEERS SEAT TRACKS HAVE ELONGATED HOLES. REMOVED FWD F/E'S SEAT TRACK IAW DC8 SRM 51-3-0 LOCATED AND DRILLED SE AT TRACK IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-3-1 2L74 4F RT4A25 20040511000952004051100095WP 2004 5 11 UPS04842337 120040402A534037558241 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1C, FWD PIT- FWD SIDE OF TORQUE BOX (APPROX STA 275) BETWEEN LONGERONS 33R -34 RT ZEE ANGLE CORRODED. REMOVED OLD FITTING PN 3755824-1 IAW DC8 SRM 51-1-20D. RECIVED NEW FITT ING PN 3755824-1 TAG 00702413 DRILLED UP FITTING IAW DC8 SRM 51-1- 24 INSTALLED FITTING IAW DC8 SRM 51-1-20D 2L74 4F RT4A25 20040511001042004051100104WP 2004 5 11 UPS04842266 120040401A57535614372503 FITTING DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CANOE FITTING I.A.W. DWG. 5614372,M/M.27-51-12, SAA SK 812-411,AND UPS ENGINEERING FILE NUMBER DC8-57-20109 2L74 4F RT4A25 20040511001082004051100108NM 2004 5 11 UPS04M42293 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 06 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AN D BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.013 INCH. BARREL NUT HOLE REPAIR PER EN 1138-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55-200 14). 2L73 4F RTA22WE 20040511001312004051100131WP 2004 5 11 UPS04842354 120040415A534037584981 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, LONGERON FITTING IS CRACKED. REMOVED FITTING, RECEIVED, LOCATED, AND DRILLED FITTING, INSTALLED FIT TING; ALL IAW DC8 SRM 51-1-20D, 51-1-24. 2L74 4F RT4A25 20040511001352004051100135NM 2004 5 11 UPS04M42287 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 23 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AN D SIDEWALL SURFACE. CORRSION REMOVED AT HOLE BOTTOM SURFACE PER SRM 51-21-01 VOL2 REV34 MATE RIALS REMOVED 0.093 INCH. BARREL NUT HOLE REPAIR PER EN 1024-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. (REF UPS ENGINEE RING FILE NR MD11-55-20015). 2L73 4F RTA22WE 20040511001512004051100151NM 2004 5 11 UPS04M42277 120040226A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 33 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLES NR 33 LT REMOVED PER SRM 51-21-01 VOL II REV 34. MATERIAL REMOVED 0.047 IS WITHIN LIMIT PER EN1065-04. BARREL NUT HOLE REPAIRED PER EN1065-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017). 2L73 4F RTA22WE 20040511001532004051100153NM 2004 5 11 04FDEA01088 120040424A5320ADA8424517 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE FOUND CORROSION. FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040511001602004051100160NM 2004 5 11 ASAA0440053 120040303A256065C161216 FITTING BOEING737 7374Q8 138447QNM L1 DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND L1 DOOR GIRT BAR FITTINGS AT STATION 312 AND 344 ARE CORRODED. REMOVED AND REPLACED ATTACH FITTINGS. (M) 2L72 4F RTA16WE 20040511001642004051100164NM 2004 5 11 ASAA0440045 120040227A33507024091007 SIGN BOEING737 7374Q8 138447QNM CABIN MISSING A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01796AS 28891 PDX - FOUND FLOOR EXIT SIGN MISSING NEAR L2 DOOR. REPLACED SIGN, OPS NORMAL. (M) 2L72 4F RTA16WE 20040511001662004051100166WP 2004 5 11 GTIA040256 120040317A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT COCKPIT FLOOR PANEL NR 1144 WOOD CRACKED, NO NONSKID. REPAIRED CRACKED WOOD. (M) 2L72 4F RTA6WE 20040511001672004051100167NM 2004 5 11 ASAA0440041 120040223A3397 WIRE BOEING737 7374Q8 138447QNM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01784AS 28199 DEN - FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE AT SEAT POSITION 22C. RECONNECTED LOOSE WIRE AND SECURED. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040511001682004051100168NM 2004 5 11 ASAA0440003 120040119A531565498843 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 967. REPAIR IAW EA. (M) 2L72 4F RTA16WE 20040511001712004051100171WP 2004 5 11 GTIA040255 120040313A5320 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MID CARGO DOOR SUPPORT ATTACHMENT ANGLE IS CRACKED. REMOVED SUPPORT ANGLE. FORMED NEW ANGLE. INSTALLED NEW SUPPORT ANGLE. (M) 2L72 4F RTA6WE 20040511001742004051100174WP 2004 5 11 GTIA040268 120040327A3350170239619 SIGN DOUG DC9 DC983 3022083WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND RIGHT AND LEFT EMERGENCY EXIT SIGNS BROKEN. REMOVED AND REPLACED RIGHT AND LEFT EMERGENCY EXIT SIGNS. (M) 2L72 4F RTA6WE 20040511001752004051100175WP 2004 5 11 GTIA040257 120040318A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND L1 DOOR TORQUE BOX WEB CRACKED AT STATION 207 LONGERON 15L. CUTOUT CRACKED AREA. FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20040511001772004051100177WP 2004 5 11 GTIA040259 120040401A2560 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FLL - FOUND L1 DOOR ESCAPE SLIDE LANYARD IS ROUTED INCORRECTLY. REROUTED L1 DOOR ESCAPE SLIDE LANYARD. (M) 2L72 4F A6WE 20040511001792004051100179NM 2004 5 11 ASAA0440049 120040229A532069434961 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 CYR - AFT BAG PIT LEFT TRANSITION Z-CHANNEL IS CORRODED IN NUMEROUS PLACES FROM STATION 797 TO 947. AFT CARGO PIT LEFT SIDE Z-CHANNEL REMOVED AND REPLACED 797 TO 947, 25L TO 25L. (M) 2L72 4F RTA16WE 20040511001822004051100182NM 2004 5 11 ASAA0440062 120040303A53106545875U70 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - R-1 DOOR LOWER THRESHOLD CREASEBEAM UPPER SURFACE HAS SEVERAL AREAS OF CORROSION BETWEEN STATION 294.5 AND 344 RBL 50. REMOVED AND REPLACED CREASEBEAM (CHORD) AT R1 DOOR 294.5 TO 344 RBL 50. (M) 2L72 4F RTA16WE 20040511001832004051100183NM 2004 5 11 ASAA0440061 120040303A53476546813104 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - MAIN DECK SEAT TRACK AT STATION 344 LBL 45.6 UPPER SURFACE OF INBOARD AND OUTBOARD FLANGES FOUND CORRODED. REPAIRED SEAT TRACK AT STATION 344 LBL 45.6 IAW SRM 737 53-00-52. (M) 2L72 4F RTA16WE 20040511001852004051100185NM 2004 5 11 ASAA0440047 120040229A53206553844 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - AFT BAG PIT RIGHT TRANSITION Z-CHANNEL IS CORRODED IN NUMEROUS PLACES FROM BS 867 TO 947. REMOVED AND REPLACED Z-CHANNEL STATION 867 TO 947, 25R. (M) 2L72 4F RTA16WE 20040511001872004051100187NM 2004 5 11 ASAA0440052 120040229A532065479576 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT PIT DOOR JAMB INBOARD BEAM AT FS 846 ABOVE STATION 25L CORRODED. REMOVED AND REPLACED WEB AT STATION 740-847 AT STRINGER 25R. (M) 2L72 4F RTA16WE 20040511001882004051100188NM 2004 5 11 ASAA0440046 120040229A532065465606 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT BAG PIT BS 947 FLOOR SUPPORT ANGLE IS CORRODED AT SEVERAL PLACES LBL 25 TO RBL 25. REMOVED AND REPLACED FLOOR SUPPORT ANGLES. (M) 2L72 4F RTA16WE 20040511001902004051100190NM 2004 5 11 ASAA0440065 120040303A5420311A11814 BUSHING BOEING737 7374Q8 138447QNM NR 2 PYLON WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - NR 2 PYLON LOWER SPAR FITTING INBOARD BUSHING MIGRATED. REMOVED AND REPLACED LOWER SPAR FITTING BUSHINGS. (M) 2L72 4F RTA16WE 20040511001932004051100193NM 2004 5 11 ASAA0440055 120040303A532065C353671 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - AFT GALLEY AREA FORE TO AFT FLOOR SUPPORT BEAM HAS CORROSION STATION 947 TO 967 RBL 50. REMOVED AND REPLACED FLOOR SUPPORT BEAM STATION 947 TO 967 RBL 50. (M) 2L72 4F RTA16WE 20040511001952004051100195NM 2004 5 11 ASAA0440072 120040303A531565468105 FLOORBEAM BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT GALLEY AREA, CORROSION ON STATION 967 FLOORBEAM LBL 28 AND RBL 18. REPAIRED FLOORBEAM AT STATION 967, LBL 28, RBL 18 TO LBL 27 WITHIN LIMITS. (M) 2L72 4F RTA16WE 20040511001962004051100196NM 2004 5 11 ASAA0440042 120040223A5330655053134 SKIN BOEING737 7374Q8 138447QNM FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND FUSELAGE EXTERNAL SKIN HAS SCRATCHES STATION 247, 10 INCHES ABOVE 24R. CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW 737-400 SRM 53-10-01. (M) 2L72 4F RTA16WE 20040511001992004051100199WP 2004 5 11 GTIA040261 120040402A3240 CABLE DOUG DC9 DC981 3022081WP RT MLG DEFECTIVE A GTIAK NONE O OTHER TXTAXI/GRND HDL 1 GL23811NK 48017 FLL - FLT 196 - DURING TAXI, RIGHT BRAKE LOCKED UP WITHOUT APPLYING BRAKES. REMOVED AND REPLACED RUN 97B BRAKE VALVE RETURN CABLE. (M) 2L72 4F A6WE 20040511002002004051100200WP 2004 5 11 GTIA040262 120040405A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 LAS - FLT 1103 - FOUND DAMAGE ON RIGHT SIDE OF A/C AT STATION 522-560 LONGERON 20 DUE TO DAMAGE. FUSELAGE EXTERNAL DOUBLER REPAIR INSTALLED AT FS 503-560, L19R-23R PER FLIGHT VEHICLES DRAWING 53-04162-1 EA 5310-0408. (M) 2L72 4F RTA6WE 20040512000012004051200001NM 2004 5 12 UPS04M42301 120040212A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 6 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.056. BARREL NUT HOLE REPAIRED PER EN 1034-004 (REF UPS ENGINEERING FILE NR MD11-55-20016). 3)BUSHING FABRICATED & INSTALLED PER EO MD11-5510 -19409-D. 2L73 4F RTA22WE 20040512000022004051200002NM 2004 5 12 UPS04M42302 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 03 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.092. BARREL NUT HOLE REPAIRED PER EN1035-04 (REF UPS ENGINEERING FILE NR MD11-55-20016). BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19 409-D. 2L73 4F RTA22WE 20040512000042004051200004NM 2004 5 12 UPS04M42304 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 14 BARREL NUT HOLE, FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.007. FITTING FABRICATED & INSTALLED PER EN 1015-04 (REF UPS ENGINEERING FILE NR MD11-55-20014). 2L73 4F RTA22WE 20040512000052004051200005NM 2004 5 12 UPS04M42305 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 02 BARREL NUT HOLES FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006. BARREL NUT HOLE REPAIRED PER EN 1011-04 (REF UPS ENGINEERING FILE NR MD11-55-20014) BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19 409-D. 2L73 4F RTA22WE 20040512000062004051200006NM 2004 5 12 UPS04M42306 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 10 BARREL NUT HOLE FOUND CORROSION ON SIDEWALL, BOTTOM & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.091. BARREL NUT REPAIRED PER EN 1036-04 (REF UPS ENGINEERING FILE MD11-55 -20016). BUSHING FABRICATED & INSTALLED PER EO MD11-55-19409-D. 2L73 4F RTA22WE 20040512000072004051200007NM 2004 5 12 UPS04M42307 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.032. BARREL NUT HOLE REPAIRED PER EN 1038-04 (REF UPS ENGINEERING FILE NR MD11-55-20015). BUSHING FABRICATED & INSTALLED PER EO MD11-5510-1 9409-D. 2L73 4F RTA22WE 20040512000092004051200009NM 2004 5 12 UPS04M42281 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STAB RT NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 AT HOLE BOTTOM SURFACE MATERIAL REMOVED 0.028 FOUND WITHIN LIMIT PER EO MD11-5510-19409-D. HEFC INSP CUTOUT IAW DAC NDT SPM REV10 CHAPTER 06.10.01.001 AT REWORK ED AREA & FOUND FOUND NO CRACK EVIDENT. REF TO UPS ENGINEERING FILE NR MD11-55-20018. REWORK TO BARREL NUT HOLE NR 30 RT PER EN1136-04. 2L73 4F RTA22WE 20040512000102004051200010WP 2004 5 12 UPS04842195 120040316A53151706317 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, MAIN CABIN FS 1727 FLOORBEAM AT RBL 34 & FLOOR SUPPORT CORRODED. REMVOED CORROSION FROM FLOORBEAM IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED TEE & L ANGLES IAW DAC DWG 575503. LOCATED AND DRILLED PARTS IAW DC8 SRM 51-1-24. INSTALLED FLOORBEAM AND SUPPORT AND ALL ATTACHING STRUCTURE THAT WAS REMOVED TO ACCESS IAW DC8 SRM 51- 1-20D, 51-3-0. ALOD & PRIME FLOORBEAM AND SUPPORT IAW DC8 SRM 51-1-8. 2L74 4F RT4A25 20040512000112004051200011WP 2004 5 12 UPS04842235 120040401A5320975402062 SUPPORT ANGLE DOUG DC8 DC873F 302199FWP FWD LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, TORQUE BOX SUPPORT ANGLE IS CORRODED BEYOND LIMITS AT STATION 280 LONG. 33R. REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. 9754020 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040512000132004051200013WP 2004 5 12 UPS04842237 120040402A5311 FRAME DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, STATION 1040 FRAME AND FRAME CAP ARE CORRODED BEYOND LIMITS AT LONG. 35L CUTOUT DAMAGED FRAME AT STATION 1040 LONG. 35L, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8-53A-010 AND REPLACED FRAME CAP IAW SRM. 53-1-0,51-1-20D,51-1-21 2L74 4F RT4A25 20040512000142004051200014WP 2004 5 12 UPS04842238 120040401A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, LEFT WING INBOARD STUB WING UPPER RIB IS CRACKED AT XS 250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED 2 ANGLE DOUBLERS IAW SRM. 57-2-0 FIG. 2 2L74 4F RT4A25 20040512000212004051200021WP 2004 5 12 ASMF 120040504A78300711346003 CONTROL VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE THRUST REVERSER LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23755RA 49727 725382 DURING TRANSIT CHECK, CAPTAIN INFORMED THAT REVERSER CONTROL VALVE WAS DETECTED WITH LEAK. LT REVERSER CONTROL VALVE WAS REPLACED IAW MM 78-31-04. DURING TEST, A LEAK WAS DETECTED IN PRESSURE NIPPLE. PACKING AND NIPPLE WERE REPLACED, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040512000322004051200032WP 2004 5 12 04FDEA01162 120040507A5753ARB00291 SUPPORT FITTING DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY EA 85740-77347- LEFT OUTBOARD BRACE SUPPORT FITTING CORROSION REPAIR. COMPLIED WITH EA 8-5740-77347. 2L73 4F A22WE 20040512000352004051200035GL 2004 5 12 04FDEA01165 220040507A7230CF66D CASE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 ENGINE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-7220-77402 ENGINE - GOUGES IN EXTERIOR OF NR 3 ENGINE AFT STATOR CASE. NO RESTRICTION NR 3 ENGINE AFT STATOR CASE HAS GOUGES, OK PER EA 8-7220-77402 IAW EA AFTER 50 FLIGHT CYCLES ACCOMPLISH AN INITIAL INSPECTION TO VERIFY THAT NO CRACKS EXIST UNDER 10X MAGNIFICATION. REPETITIVE INSPECTIONS WITHIN EVERY 200 FLIGHT CYCLES THEREAFTER, UNDER 10X MAGNIFICATION UNTIL TERMINATING ACTION AT NEXT ENGINE SHOP VISIT. 2L73 4F4 F A22WE E23EA 20040512000372004051200037NM 2004 5 12 04FDEA01167 120040508A5320 BRACKET BOEING727 727200 138407ENM RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 RIGHT MLG DOOR FORWARD HINGE SEAL SUPPORT THE AFT BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET, FABBED FROM 2024-T3 .040 BATCH 744347 AT MAE ON N/R N00389. 2L73 4F RTA3WE 20040512000402004051200040NM 2004 5 12 04FDEA01142 120040503A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 WHILE PERFORMING MAIN CARGO DOOR OPS CHECK FOUND AFT DOOR FRAME BS 618, WL 228 TO BE CRACKED. REMOVED DAMAGE IN MCD AFT FRAME BS 618, WL 228. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS AND FASTENERS REMOVED FOR ACCESS. ALL WORK DONE IAW SRM 51-40-3 AND 51-30-2. 2L73 4F RTA3WE 20040512000422004051200042NM 2004 5 12 04FDEA01144 120040504A5753ARB7411 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP, I/B HINGE FITTING TENSION STRAP SUPPORTS FOUND EXISTING CRACK ON HINGE HOLES BIGGER IN SIZE COMPARE TO EO 1-5750-7-5004 01 PT2 AS CALL OUT ON STEP 1B. COMPLIED WITH FEDEX EA 1-5750-75942 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE, TENSION STRAP FASTENER HOLES. 2L73 4F RTA22WE 20040512000432004051200043 2004 5 12 BAQA094402 420040430A34214021541671 INDICATOR BOLKMSBK117 BK117C1 5626025EU COCKPIT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG 7506 WHEN FLOWN WITH INDICATOR. WINGS LEVEL IN TRIM A/C MAKES SLOW RT TURN, INDICATOR IS DRIFTING. REPLACED WITH SERVICABLE UNIT. 05/05/2004 1G72 3U NCH13EU 20040512000442004051200044NM 2004 5 12 UIA9311 120040330A5711 SPAR DOUG MD90 MD9030 3023690NM RT WING CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017917 53572 DURING C 05 CHECK OF DATUM A/C: FOUND CORROSION ON UPPER SURFACE OF FRONT SPAR OF RT WING AT STA XRS 531. FOUND CORROSION ON UPPER SURFACES OF LOWER SKIN P/N:5935822-50 AND REAR SPAR LOWER CAP OF RT WING AT STA XRS=546. PERMANENT REPAIR ON FUSELAGE SKIN P/N:5924802-133 AT STA Y=237. FOUND CORROSIONS ON UPPER SURFACES OF LOWER SKIN P/N:5935822-505 OF WING AT STA XRS=546. SEVERE CORROSION WAS FOUND ON RT IB FLAP OB VANE P/N:5930495-51 TRAILING EDGE LOWER SURFACE. THIS REPAIR CAN BE CONSIDERED AS PERMANENT REPAIR. 2L72 4F RTA6WE 20040512000452004051200045SW 2004 5 12 ALGA094405 120040505A6220407010105101 STUD BELL 407 407 1182206SW M/R HUB ASSY CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03408AL A219 53491 FOUND 8 CRACKED STUDS. REPLACED WITH NEW STUDS. 1G71 3U O H2SW 20040512000502004051200050EU 2004 5 12 HXS2004F00001 120040325A5312350A2112470051 BULKHEAD SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAILBOOM CRACKED B HXSRK NONE O OTHER ININSP/MAINT 1 AL05913LP2151 2383 DURING ANNUAL INSPECTION, TAILBOOM BULKHEAD PN 350A2112470051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME PN ON WO NR 24-36502. 1G71 3U3 U H9EU E19EU 20040512000552004051200055NM 2004 5 12 ASMF200405002 120040501A2780833605 PROXIMITY SWITCH DOUG MD88 MD88 3023688NM STALL COMPUTER FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23158PL1296 49761 AIRCRAFT RETURNED TO PLATFORM. DURING ENGINE START THE (STALL INDICATION FAILURE) LIGHT TURNED ON. STALL COMPUTERS TESTS WERE PERFORMED AND SLATS FAILURE WAS DETECTED ON COMPUTER NR 2 AND (SIF) LIGHT TURNED ON ON BOTH COMPUTERS. PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) WAS TESTED DETECTING 620 CODE FAILURE ON ELECTRONIC CARD NR 15. PSEU WAS REPLACED IAW MM 32-09-10. 2L72 4F RTA6WE 20040512000562004051200056WP 2004 5 12 ASMF200405003 120040502A7930699151 STRAINER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE ENGINE OIL FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23216AM4091 49586 725948 AIRCRAFT RETURNED TO PLATFORM. (LT STRAINER CLOGGING) LIGHT TURNED ON AND INTERFERENCE PROBLEMS IN LT SPEAKER. OIL FILTER AND DIFFERENTIAL PRESSURE SWITCH WERE REPLACED IAW MM 79-20-06 AND 79-35-01, RESPECTIVELY, AND TEST WAS PERFORMED IAW MM 79-00-00, ALL CORRECT. LT AUDIO CONTROL BOX AND FLIGHT RECORDER WERE REPLACED IAW MM 23-50-02 AND 31-31-01, RESPECTIVELY, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040512000592004051200059SW 2004 5 12 ALGA094404 120040505A6220407010101101 YOKE BELL 407 407 1182206SW FUSELAGE DELAMINATED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03408AL6214 53491 FOUND DELAMINATION ON YOKE ARM. REPLACED WITH SERVICABLE PART. 1G71 3U O H2SW 20040512000602004051200060SW 2004 5 12 ALGA094414 120040506A6210406310405101 UNIVERSAL BELL 407 407 1182206SW MAIN ROTOR RATCHETING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03403AL363 53478 FOUND BEARING ROUGH AND RATCHETY. REPLACED WITH NEW PART. 1G71 3U O H2SW 20040512000622004051200062NM 2004 5 12 ASMF200405010 120040506A3260834503 PROXIMITY SENSOR BOEING757 7572Q8 1384972NM MLG DAMAGED W ASMFK NONE N FALSE WARNING ININSP/MAINT 1 SW23803AM 26268 DURING TRANSIT CHECK, (LANDING GEAR) AND (MAINTENANCE GEAR DOOR) LIGHTS TURNED ON. DURING MAINTENANCE REVISION, PSEU WAS DETECTED WITH DAMAGE ON SENSOR 076. PROXIMITY SWITCH WAS REPLACED IAW MM 32-61-02 AND TEST CORRECT IAW MM 32-61-00. 2L72 4F RTA2NM 20040512000652004051200065EU 2004 5 12 BAQA094395 120040430A284481071370010 INDICATOR AEROSPAS365 AS365N2 8680815EU FUEL PRESSURE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME166 6417 WILL NOT READ FUEL PRESSURE, NEEDLE AT ZERO. REPLACED WITH SERVICABLE UNIT. 05/10/2004 1G72 3U RTH10EU 20040512000682004051200068NM 2004 5 12 04FDEA01145 120040504A5753ANB70161 SUPPORT FITTING DOUG MD11 MD11 3023602NM T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B BUSHING BORE FOUND ELONGATED. COMPLIED WITH FEDEX EA 1-5750-75933, WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY. 2L73 4F RTA22WE 20040512000712004051200071NM 2004 5 12 04FDEA01146 120040504A5753ANB70161 SUPPORT FITTING DOUG MD11 MD11 3023602NM T/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B FWD EDGE FOUND WITH CHAFE MARKS. COMPLIED WITH FEDEX EA 1-5750-75933 - WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY. 2L73 4F RTA22WE 20040512000742004051200074NM 2004 5 12 04FDEA01123 120040430A5512 SKIN DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 HORIZONTAL STABILIZER UPPER FWD PLANK NR 8R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2L73 4F RTA22WE 20040512000762004051200076NM 2004 5 12 04FDEA01125 120040430A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. LT WING, O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. 2L73 4F RTA22WE 20040512000782004051200078NM 2004 5 12 04FDEA01127 120040430A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND O/B FLAP, I/B FWD HINGE ACTUATOR HOLE 8 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040512000802004051200080 2004 5 12 BAQA094415 420040503A2211117884141 CONTROL UNIT BOLKMSBK117 BK117C1 5626025EU AUTOPILOT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG 7506 STRONG LAT. INPUTS WITH YAW CSAS IN ON POSITON OR STANDBY POSITION, GOES AWAY WHEN SYSTEM IS TURNED OFF. UNIT LASTED 83.6 HOURS SINCE LAST REPAIR. LAST REPAIR, CJ RO 9-090006-17 ; INVOICE NR S29024201. 1G72 3U NCH13EU 20040512000812004051200081EU 2004 5 12 HXS2004F00000 120040325A6210355A11002011 BLADE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR CRACKED B HXSRO OTHER O OTHER NRNOT REPORTED 1 AL056094U4329 3935 2751 ON 3/25/04, MAIN ROTOR BLADE, SN 7530 REMOVED FROM AC DURING ANNUAL INSPECTION. 130MM SPANWISE CRACK FOUND AT 68.375. 1G71 3U3 UNCH9EU E19EU 20040512000822004051200082NM 2004 5 12 04FDEA01117 120040430A1430S49319171018 FASTENER DOUG MD11 MD11 3023602NM LT WING SHEARED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LT WING LOWER SURFACE I/B AREA, ONE FASTENER HEAD FOUND SHEARED OFF. LT WING LOWER SURFACE I/B AREA, ONE FASTENER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20040512000832004051200083NM 2004 5 12 04FDEA01118 120040430A1430S49319171015 FASTENER DOUG MD11 MD11 3023602NM RT WING SHEARED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF O/B FLAP I/B HINGE. RIGHT WING LOWER SURFACE - ONE FASTENER FORWARD OF O/B FLAP I/B HINGE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040512000842004051200084NM 2004 5 12 04FDEA01119 120040430A1430HLT4391012 FASTENER DOUG MD11 MD11 3023602NM RT WING SHEARED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING LOWER SURFACE, ONE FASTENER HEAD FOUND SHEARED OFF FORWARD OF PANEL 641KB. RIGHT WING LOWER SURFACE, ONE FASTENER FORWARD OF PANEL 641KB REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040512000882004051200088NM 2004 5 12 04FDEA01128 120040427A5730 PANEL DOUG MD11 MD11 3023602NM RT WING MISSING A FDEAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 SO25578FE 48458 PANEL ON TOP OF RIGHT WING MISSING. REPLACED WING PANEL USING APPROVED PARTS AND METHODS USING EA 1-5710-78268. PART NUMBER OF PANEL INSTALLED IS ARC0629-502 AND IS INK-STAMPED ACCORDINGLY REF MM CHAP 51 SRM. OK FOR SERVICE. INST ON A/C ONLY, NO REMOVAL ON MFG ARC0629-502. 2L73 4F RTA22WE 20040512000892004051200089NM 2004 5 12 04FDEA01129 120040430A3213NRG6221529 TRUCK DOUG MD11 MD11 3023602NM RT MLG BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25580FE 48471 RT MLG TRUCK BEAM HAS BROKEN PIVOT BORE SLEEVE AS VIEW THRU RT OUTBOARD AFT LUBE HOLE. UPON FURTHER INVESTIGATION NO DAMAGE WAS FOUND.OK TO CONTINUE SERVICE. RT MLG TRUCK WAS REMOVED & REINSTALLED IAW M/M 32-12-20-4. 2L73 4F RTA22WE 20040512000902004051200090WP 2004 5 12 04FDEA01130 120040501A7933 BULB DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 1 ENGINE FAULTY A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25312FE 48300 455217 ENG 1 OIL TEMP HIGH, TEMP 226; ABOVE RED LINE. READJUSTED POWER, TEMP REMAINED ABOVE RED LINE. SHUT DOWN NR 1 ENGINE AND LANDED. OIL TEMP SLOWLY RETURNED TO A LOWER SETTING. OIL PRESSURE & QTY NORMAL. NO VIBRATIONS. RAN ENG NR 1, OIL TEMP AT 4 MIN WAS 144 DEGREES. SHUT DOWN AND CHANGED TEMP BULB. RAN ENG AGAIN TEMP WAS 62 DEGREES AFTER 5 MIN. 2L73 4F4 FRTA22WE E23EA 20040512000932004051200093NM 2004 5 12 ASMF200405001 120040501A3350225BS1011 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT FAILED W ASMFK NONE L NO TEST ININSP/MAINT 1 SW23158PL9339 5890 49761 DURING TRANSIT CHECK CAPTAIN REPORTED THAT SOME EMERGENCY LIGHTS DO NOT WORK TURNED ON AND OTHERS WHEN SYSTEM WAS OFF THE LIGHTS TURNED ON. BATTERY WAS REPLACED IAW MM 33-53-00 AND VHF NAVIGATION SYSTEM WAS TESTED IAW MM 34-51-00 ALL CORRECT. DURING OVERNIGHT SERVICE THE SYSTEM WAS CHECKED, ALL CORRECT. 2L72 4F RTA6WE 20040512000972004051200097EU 2004 5 12 HXS2004F00002 120040316A5312350A2112470051 BULKHEAD SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAILBOOM CRACKED B HXSRO OTHER O OTHER NRNOT REPORTED 1 AL05618OT4015 1149 DURING ANNUAL INSPECTION, TAILBOOM BULKHEAD PN 350A2112470051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME PN ON WO 24-36502. REMOVED AND REPLACED BULKHEAD. 1G71 3U3 UNCH9EU E19EU 20040512001022004051200102SW 2004 5 12 ERAA094433 120040405A2435230461030 ARMATURE BELL 412 412 1182202SW STARTER GEN CHAFED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 ARMATURE THAT HAS SIGNS OF RUBBING AND GOT EXCESSIVELY HOT. RETURNING ON REPAIR ORDER NR RW-898494 REQUESTING WARRANTY EXCHANGE. 1G72 4U H4SW 20040510001792004051000179EU 2004 5 10 AWXA200400393 120040421A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 263 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW134821706 053 DURING INSPECTION THE LT AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040510001832004051000183NM 2004 5 10 AWXA200400442 120040405A57536546486129 WEDGE BOEING737 7373S3 1384711NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 DURING C-17 CHECK THE UPPER SURFACE OF LT INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 9 INCHES FROM INBOARD END. MAINTENANCE CUTOUT DAMAGED UPPER SKIN AND CORE ON LT INBOARD MID FLAP TRAILING EDGE AT WS 82 LT; FABRICATED A NEW REPLACEMENT CORE AND A REPAIR DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10, FIG. 16. 2L72 4F RTA16WE 20040510001862004051000186EU 2004 5 10 AWXA200400412 120040328A5315D5347219520200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y254 RT BETWEEN FR 68 AND FR 70. MAINTENANCE REMOVED CORRODED FLOORBEAM Y254 RT FROM FR 68 TO FR 70; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12 & 18. 2L72 4F RTA28NM 20040510001872004051000187EU 2004 5 10 AWXA200400413 120040328A5315D5347213320200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y765 RT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y765 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472-190; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12. 2L72 4F RTA28NM 20040510001892004051000189EU 2004 5 10 AWXA200400415 120040328A5315D53472172200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 L/H, FORWARD OF FR 68. MAINTENANCE CUTOUT CORRODED SECTION OF L-2 DOOR SILL FLOORBEAM Y1292 LT FROM FR 67 TO FR 69; PERFORMED HFEC INSPECTION OF CUTOUT; FABRICATED AN ANGLE AND SHIM; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201. 2L72 4F RTA28NM 20040510002012004051000201NM 2004 5 10 AWXA200400474 120040425A532065479574 WEB BOEING737 7373S3 1384711NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB IN SEVERAL LOCATIONS BETWEEN BS 794.3 AND BS 847, RBL 20. MAINTENANCE REMOVED CORRODED SECTION OF AFT CARGO COMPARTMENT DOOR SILL WEB FROM BS 794.3 TO BS 847, AT RBL 20; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A REPAIR SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG. 1. 2L72 4F RTA16WE 20040510002092004051000209EU 2004 5 10 AWXA200400423 120040329A5347D53112092206 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT, FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11, FIG. 12. 2L72 4F RTA28NM 20040510002132004051000213NM 2004 5 10 UPS04242316 120040426A2720 PULLEY BRACKET BOEING727 72722C 138400FNM RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE:C SUSPECT CRACKS ON RUDDER TRIM CABLE PULLEY BRACKET IN AIRSTAIRS AREA BS 1203 RT HFEC C/W, DERIVETED BRACKET, FAB BRACKET IAW SRM 51-20-01, BRACKET INSTALLED. 2L73 4F A3WE 20040510002242004051000224NM 2004 5 10 2004UALA00377 120040419A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29660UA 27115 EEL FLOOR PATH LIGHT STRIP AT MID GALLEY RT INOPERATIVE. REPAIRED DAMAGED SECTION. OPS CHK'D NORMAL. 2L72 4F4 FRTA1NM E24NE 20040510002322004051000232NM 2004 5 10 2004UALA00364 120040418A5314 KEELBEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 FASTENER HOLE ON RT SIDE OF KEEL BEAM AT STA 710 LOWER CHORD FLANGE, UPPER SURFACE ELONGATED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED STRAP AND FILLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040510002472004051000247NM 2004 5 10 F3LA200400056 120040425A5320 SILL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON R1 MOP SILL. REPLACED R1 MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20040510002642004051000264NM 2004 5 10 2004UALA00397 120040426A5320 STRUCTURE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29547UA 25368 STA 590 AND BS 638.5 STR 14L -19L IS DENTED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040510002662004051000266NM 2004 5 10 2004UALA00399 120040426A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29643UA 25093 FWD GALLEY EEL STRIP IS INOPERATIVE. REPAIRED EEL FEEDER. CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20040510002722004051000272NM 2004 5 10 2004UALA00405 120040426A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 AFT CARGO DOOR CUT OUT AFT SIDE BEAR STRAP HAD CORROSION AND GOUGES. DOUBLER/TRIPLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20040510002812004051000281NM 2004 5 10 2004UALA00414 120040424A5754114W41307 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE L/E SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29777UA 26916 T/E WEDGE DELAMINATED AT OTBD TRACK AREA LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE SKIN REPLACED & REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20040511000062004051100006NM 2004 5 11 AWXA200400490 120040507A3150 WARNING LIGHT BOEING737 7373G7 1384595NM PARK BRAKE ILLUMINATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28306AW 24633 ON TAKEOFF AT PDX EN ROUTE FOR LAS TAKEOFF WARNING CONFIGURATION HORN SOUNDED, REJECTED TAKEOFF AT 65 KTS, ALL SETTINGS IN PROPER PARAMETERS. MAINTENANCE TROUBLESHOT PROBLEM DOWN TO THE PARKING BRAKE VALVE AND ISSUED MEL 32-3, COND. 1, "PARKING BRAKE VALVE INOP". ON 05/08/2004 I PHX MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE TAKEOFF WARNING SYSTEM IAW T/C A1B31009 AND COULD NOT GET THE PROBLEM TO DUPLICATE. A FUP WAS WRITTEN TO REPLACE THE PARKING BRAKE VALVE. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE VALVE IAW T/C R4M32012, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA16WE 20040511000112004051100011EU 2004 5 11 ERAA094454 120040122A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU RT MLG LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03125EH11994 S562 6 MONTH INSPECTION DUE. CYLINDER 1EA PN 2370039 SN 946 DUE HYDRO TEST 4-04 SQUIB CHARGE 1 EA PN 94455 SN 1292 DUE RETIREMENT 4-04. CHECK VALVE ON AFT COMPARTMENT ON FLOAT BAG LEAKING. ACTION TAKEN: CHANGED 1 EA CYLINDER BOTTLE, CHANGED 1 EA SQUIB CHARGE, CHANGED 1 EA CHECK VALVE AND COMPLIED WITH 6 MONTH INSPECTION. VERIFIED COMPLIANCE WITH SB NUMBERS - 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1G72 3U H3EU 20040511000182004051100018 2004 5 11 UPS04142327 420040503A2565 LIGHT AIRBUSA300 A300F4622R 3930360EU DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01136UP 0820 CREW ENTRY DOOR EVAC SLIDE RELEASE WARNING SYSTEM LIGHTS WILL NOT TEST. BUZZERS OK. CLEANED DEBRIS FROM SWITCH NOW OPS GOOD PER MM 52-73-00. THIS CLEARS M280249. LP 234452 2L72 4F RTA35EU 20040511000192004051100019NM 2004 5 11 UPS04242341 120040416A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE:C CHAFING UNDER FAIRING AT BS1050 AND BS1070 JUST BELOW STR26L. AT BS1050 DAMAGE REMOVED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-1. AREA REPROTECTED IAW SRM51-10-02. AT BS1070 DAMAGE OUT OF LIMITS IAW SRM 53-30-1. REPAIR CARRIED OUT IAW SRM 53-30-02 FI G.2 2L73 4F A3WE 20040511000222004051100022NM 2004 5 11 UPS04242343 120040424A7830 SKIN BOEING727 72722C 138400FNM ENG.1 THRUST REVCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, ENGINE NR 1 THRUST REV. UPPER DOOR INNER RAMP SKIN CRACKED. DYE PENETRANT INSP. CARRIED OUT ON THE ABOVE AREA IAW MIL-STD-6866. CRACKS FOUND AND ENDS MARKED. STOP DRILLED CRACKS IAW MM 78-30-01. DYE PENETRANT INSP. CARRIED OUT AROUND STOP DRILLED AREA IAW MIL-STD-6 866. CRACKS CONTAINED WITHIN REPAIR AREA. FABRICATED REPAIR DOUBLER IA W SRM 78-30-01. CARRIED OUT REPAIR IAW SRM 78-30-01 2L73 4F A3WE 20040511000412004051100041NM 2004 5 11 DL76L040379 120040428A3246321003166 WHEEL BOEING767 767332 1382001NM NLG DEFECTIVE A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27171DN 24759 DURING TAXI-OUT WHILE ATTEMPTING LEFT TURN, AIRCRAFT DID NOT RESPOND TO TILLER INPUTS. CONTINUED STRAIGHT AHEAD AND SKID WAS NOTED. LEFT ENGINE WAS RUNNING AT TIME OF SKID. SPEED WAS 8-10 KNOTS, POWER WAS 78 PERCENT N2. A/C WEIGHT 292,400. TEST OF NOSE STEERING SYSTEM, FOUND OK. INSPECTED AXLES AND WHEEL BEARINGS, ALL FOUND OK. REPLACED BOTH NOSE WHEEL ASSY'S. LEFT NOSE TIRE WAS FLAT ON RETURN TO GATE. TAXIWAY WHERE SKID OCCURRED WAS JUST REPAVED ONLY HOURS BEFORE INCIDENT HAPPENED. LEFT ENGINE WAS ONLY ENGINE RUNNING WHEN GOING INTO LEFT TURN. 2L72 4F RTA1NM 20040511000432004051100043NM 2004 5 11 UPS04M42250 120040221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 27 BARREL NUT HOLE FOUND CORROSION ON BOTTOM ,SIDEWALL AND BEARING SURFACE. CORROSION ON BOTTOM OF HOLE NR 27 RT REMOVED PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.059 INCH IS WITHIN LIMIT PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1107-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018) 2L73 4F RTA22WE 20040511000462004051100046NM 2004 5 11 AWXA200400447 120040429A33501012721 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28155AW 23777 DEN - EEL - DURING A-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040511000522004051100052NM 2004 5 11 AWXA200400453 120040422A532065535944 REVEAL BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON R-1 DOOR CUTOUT UPPER AFT REVEAL AT FASTENER HOLE BS 336, STR 10 RT. MAINTENANCE REMOVED CORRODED R-1 DOOR UPPER AFT REVEAL AT BS 336, STR 10 RT; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3-4, & 6-8. 2L72 4F RTA16WE 20040511000652004051100065NM 2004 5 11 UPS04M42253 120040223A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 25 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 25 LT REMOVED PER SRM51-21-01 VOL II REV34, MATERIAL REMOVED 0.056 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1063-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF USP ENGINEERING FILE NR MD11-55-20015) 2L73 4F RTA22WE 20040511000852004051100085NM 2004 5 11 UPS04242358 120040415A524065957193 RIB BOEING727 72722C 138400FNM MID GALLEY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE: C, MID GALLEY DOOR UPPER GATE HINGE RIB CRACKED AT FWD CORNER. HINGE RIB REPLACED IAW DWG 65-16720 AND SRM 51-30-02 2L73 4F A3WE 20040511000862004051100086NM 2004 5 11 UPS04442359 120040506A5730 PANEL BOEING747 747200 1384847NM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 REF D277226 RT WING FIXED UPPER LEADING EDGE PANEL HAS DELAMINATION. ACCOMPLISH TEMP REPAIR. REMOVED PANEL FROM A/C. REPLACED RT WING UPPER LEADING EDGE PANEL AS PER SRM 51-30-02. THIS CLEARS D277226. 2L74 4F RTA20WE 20040511000892004051100089NE 2004 5 11 UPS04542310 220040429A7200ETPU10003C ENGINE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE LEFT FLAMED OUT A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 SO01458UP 25479 LT ENG FLAMED OUT ON FINAL APPROACH. DURING APPROACH RECEIVED L GEN EICAS FOLLOWED BY LT BUS FAIL, THEN 18 PSI & RED OIL PRESSURE INDICATION. PERFORMED IN FLIGHT SHUTDOWN LT ENGINE. INSP WIRE CLAMPS D1380 NO DMG NOTED, INSP ENG CHIP DET, DET CLEAN. INS P INLET & EXHAUST NO DMG NOTED. C/W TPU & BVCU BITE CK. FOUND FAULT NR 4 ON TPU & NR 04 ON BVCU. C/W FIM 75-32-00 4-1-A. REFERRED TO TABLE 1 03 FAULT. RPLCD TPU SENSOR PER MM. BITE CK ON LT/RT EEC FAULT 8A. INSP & CLEANED TAT PROBE PER FIM. 73-21-00 FIG 103 SHT 1. RAN ENG & BITE CK FOR TPU & BVCU & EE. ENG CK NORMAL 2L72 4F4 FRTA2NM E12EU 20040511000942004051100094WP 2004 5 11 UPS04842336 120040403A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, CORROSION AROUND NUTPLATES & FASTENER FROM STH 1480 TO 1540 AT CUSP LT SIDE OF AFT CARGO COMPT PUT A7763. REMOVED AIR GRILLS CUSP CLOSEOUT & FLOOR TO FOM REMOVED SEAT TRACK ORIG THICKNESS .090 IAW 51-2-0. REMOVED CORR IAW 51-1-8 AFTER BLEND .040 MATERIAL REMAINING OUT LIMITS IAW 53-2-3. LOCATED & DRILLED UP NEW SEAT TRACK FLOORBOARD CUSP CLOSEOUT & AIR GRILLS IAW DC8 SRM 51-3-0 2L74 4F RT4A25 20040511001052004051100105NM 2004 5 11 UPS04M42267 120040205A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 8 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE HOLE BOTTOM SURFACE AREA CORROSION REMOVED PER SRM51-21-01 VOL II R EV 34, MATERIAL REMOVED 0.005 INCH FOUND WITHIN LIMIT PER EO MD11-5510-194 09D. BARREL NUT HOLE REPAIRED PER EN1020-04. BUSHING FABRICA TED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR : MD11-55-20016) 2L73 4F RTA22WE 20040511001072004051100107NM 2004 5 11 04FDEA01170 120040507A5753 STOP FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED DAMAGED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LT WING O/B FLAP AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040511001092004051100109NM 2004 5 11 UPS04M42294 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 10 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORRORSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.047 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1139-04 (REF UPS ENGINEERING FILE NR 55-20014) 2L73 4F RTA22WE 20040511001132004051100113NM 2004 5 11 04FDEA01174 120040510A5753 ACTUATOR DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.403 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001142004051100114NM 2004 5 11 04FDEA01175 120040510A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001192004051100119NM 2004 5 11 04FDEA01062 120040422A5347AFA77957 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CABIN SEAT TRACK CORRODED STA 1830 & STA 1671 LBL 27. CABIN SEAT TRACK CUT AND REMOVED AT STA 1651 TO STA 1887 LBL 27.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040511001302004051100130WP 2004 5 11 UPS04842352 120040401A5320 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C1, AFT PIT RT CUSP EXTRUSION CORRODED BETWEEN STA 1000 AND 1020 LONG 21 RT. REMOVED DAMAGED CUSP SECTION IAW TR53-179 STA 990-1030 L21 RT. IAW DC8 SRM 51-1-20D. REC'ED, LOCATED AND DRILLED -3 & -5 REPAIR ANGLES, -7 D OUBLER AND -9 CUSP SECTION IAW DC8 SRM 51-1-24. FAB IAW TR 53-179 & RE PAIR DWG 2060296. ALODINED & PRIMED IAW DC8 SRM 51-1-8. AND INSTALLED -3,-5,-7, &-9 REPAIR MEMBERS IAW TR53-179 AND REPAIR DWG 3060296 2L74 4F RT4A25 20040511001332004051100133WP 2004 5 11 UPS04842308 120040428A1430 SCREW DOUG DC8 DC873F 302199FWP EMERGENCY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 TWENTY SCREWS & NUTPLATES CORRODED OUT OF BOTTOM OF LEFT REAR L1 TYPE DOOR. REPAIRED LEFT REAR TYPE 1 EXIT DOOR PER DC8 EO DC8-5220-19783F. 2L74 4F RT4A25 20040511001382004051100138NM 2004 5 11 UPS04M42289 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 09 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 AT HOLE AREA MATERIAL REMOVED 0.020. BARREL NUT HOLE REPAIRED PER EN 1037-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55-20014). 2L73 4F RTA22WE 20040511001392004051100139NM 2004 5 11 UPS04M42290 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB RT NR 32 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL2 REV34 MATERIAL REMOVED 0.034. BARREL NUT HOLE REPAIRED PER EN 1019-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D (REF UPS ENGINEERING FILE NR MD11-55- 20018). 2L73 4F RTA22WE 20040511001472004051100147NM 2004 5 11 UPS04M42273 120040224A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 28 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AN D BEARING SURFACE. BOTTOM OF HOLE NR 28 LT CORROSION REMOVED PER SRM 51-21-01 VOL II REV 34, MATERIAL REMOVED 0.015 IS WITHIN LIMITS PER EO 1104-04. BARREL NUT HOLE REPAIRED PER EN1104-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2L73 4F RTA22WE 20040511001502004051100150NM 2004 5 11 UPS04M42276 120040221A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 07 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 07 LT REMOVED PER SRM 51-21-01 VOL II REV 34 , MATERIAL REMOVED 0.060 IS WITHIN LIMITS PER EN1059-04. BARREL NUT HOLE REPAIRED PER EN1059-04. BUSHING FABRICATED AND INSTALLED P ER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20014) 2L73 4F RTA22WE 20040511001522004051100152NM 2004 5 11 UPS04M42278 120040217A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 34 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE RT NR 34 REMOVED PER SRM51-21-01 VOL II REV 34 MATERIAL REMOVED 0.089 FOUND WITHIN LIMITS PER EN1049-04. BARREL NUT HOLE REPAIRED PER EN1049-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20018). 2L73 4F RTA22WE 20040511001572004051100157NM 2004 5 11 ASAA0440058 120040303A531065458SSU122 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FLOOR CREASE BEAM AT R2 JAMB CORRODED STATION 947 TO STATION 990. REMOVED AND REPLACED CREASE BEAM STATION 947 TO 1006 RBL 50. (M) 2L72 4F RTA16WE 20040511001592004051100159NM 2004 5 11 ASAA0440056 120040303A53206546549 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - AFT BAG PIT BS 767 FRAME FAIL/SAFE CHORD ANGLE IS CORRODED FROM 26R TO BL 0. REPAIRED BS 767 FRAME FAIL/SAFE CHORD ANGLE. (M) 2L72 4F RTA16WE 20040511001692004051100169WP 2004 5 11 GTIA040253 120040319A5320 ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND AFT CARGO DOOR LATCH SUPPORT HOOK HAS CRACKED ANGLE AT AFT END. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2L72 4F RTA6WE 20040511001802004051100180NM 2004 5 11 ASAA0440066 120040303A5411S302TOOI219 BEARING BOEING737 7374Q8 138447QNM NR 2 PYLON LOOSE A K NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - NR 2 PYLON, UPPER SPAR ATTACH FITTING BEARING IS LOOSE IN LUG. REMOVED AND REPLACED CROWN BEAM BEARING. (M) 2L72 4F RTA16WE 20040511001812004051100181NM 2004 5 11 ASAA0440048 120040229A532069434961 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT BAG PIT RIGHT TRANSITION Z-CHANNEL IS CORRODED FROM STATION 847 TO 867. REMOVED AND REPLACED TRANSITION AT STATION 847 TO 867, 25 RT TO 25 RT. (M) 2L72 4F RTA16WE 20040511001892004051100189NM 2004 5 11 ASAA0440067 120040303A5411S302TOOI219 BEARING BOEING737 7374Q8 138447QNM NR 1 PYLON DEFECTIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND NR 1 ENGINE PYLON, UPPER LINK ATTACH POINT ROTATING IN UPPER SPAR FITTING. REMOVED AND REPLACED CROWN BEAM BEARING. (M) 2L72 4F RTA16WE 20040511001912004051100191NM 2004 5 11 ASAA0440064 120040303A5420311A11814 BUSHING BOEING737 7374Q8 138447QNM NR 1 PYLON WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - NR 1 ENGINE PYLON, DIAGONAL BRACE, LOWER SPAR ATTACH FITTING, INBOARD BUSHING MIGRATING. REMOVED AND REPLACED BUSHING. (M) 2L72 4F RTA16WE 20040511001922004051100192NM 2004 5 11 ASAA0440063 120040303A5320656571030 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - AFT CARGO PIT CENTER BELLY BETWEEN STATION 727D AND 727E, VHF ANTENNA SUPPORT STRUCTURE CORRODED. REMOVED AND REPLACED VHF ANTENNA SUPPORT STRUCTURE. (M) 2L72 4F RTA16WE 20040511001982004051100198WP 2004 5 11 GTIA040260 120040404A2560 LANYARD DOUG DC9 DC982 3022082WP EVAC SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FLLT - FLT 1751 - FOUND R1 SLIDE DEPLOYED WHEN CATERING OPENED DOOR. R1 SLIDE DID NOT DEPLOY, LANYARD CAME OFF COVER RESECURED LANYARD. (M) 2L72 4F A6WE 20040512000202004051200020NM 2004 5 12 UIA9306 120040224A5711 SPAR DOUG MD90 MD9030 3023690NM LT WING CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017923 53534 DURING S90M CHECK OF DATUM A/C, FOUND CORROSION, UPPER SURFACE OF FRONT SPAR LOWER CHORD OF LT WING AT STA XRS 509.2. LT WING (STA. XRS 115-601) AND RT WING (STA. XRS 73-477) UPPER SKIN. T/E ALUMINUM STRIP OF RUDDER THAT HAD PENETRATED THROUGH THE ENTIRE THICKNESS.4. NR 1-NR 2 ON LOWER WING SURFACE OF LT WING AT STA XRS=546.5. FUSELAGE FRAME LOWER TEE (P/N:9912246-115). THE CORROSION LOCATED STA 1437, L29R-L26R.6. PFM MAJOR REPAIR . 2L72 4F RTA6WE 20040512000312004051200031WP 2004 5 12 04FDEA01161 120040507A2750 FLAP DOUG DC10 DC1010 3022110WP WING MALFUNCTIONED A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25391FE 46625 ON FLAP RETRACTION AFTER T/O, GOT A FLAP DISAGREE LEVEL 2 ALERT. CONFIG PAGE SHOWED FLAPS STILL AT 18 DEG T/O SETTING. ACCOMPLISHED QRH PROCEDURES WITH RESULTS OF INABILITY TO RAISE OR LOWER FLAPS AT ALL. LANDED AT FLAPS 18 DEG/ EXT. CONFIG PAGE SHOWED FLAPS AT 19/21 & 20/19. FLAP HANDLE DURING TROUBLESHOOTING WAS RAISED TO 0 DEG/EXT AND LOWERED TO 35/EXT WITH NO CHANGE. FOUND DIAL-A-FLAP OUT OF SEQUENCE. RESET FLAP AND SLAT HANDLES REF MM 27-50-00-5. OPS CHECK NUMEROUS TIMES ALL NORMAL OPERATION. 2L73 4F A22WE 20040512000332004051200033WP 2004 5 12 04FDEA01163 120040507A5744ARC0502501 HINGE FITTING DOUG DC10 DC1010 3022110WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-5740-77348 WINGS - LEFT OUTBOARD FLAP HINGE BRACKET CORROSION REPAIR P/N ARC0502-501. COMPLIED WITH EA 8-5740-77348 WINGS LEFT OUTBOARD FLAP INBOARD HINGE BRACKET CORROSION REPAIR P/N ARC0502-501. 2L73 4F A22WE 20040512000342004051200034WP 2004 5 12 04FDEA01164 120040507A5753ARC27614 BRACKET DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-5740-77349 WINGS - RIGHT I/B FLAP REWORK OF TRACK/DRIVE BRACKET P/N ARC2761. COMPLIED WITH EA 8-5740-77349- WINGS RIGHT I/B FLAP, REWORK OF TRACK / DRIVE BRACKET. 2L73 4F A22WE 20040512000362004051200036WP 2004 5 12 04FDEA01166 120040508A5744ARC0538 BRACKET DOUG DC10 DC1010 3022110WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-5740-77350 WINGS - LEFT OUTBOARD FLAP-FWD CLEVIS BRACKET ASSY CORROSION REPAIR P/N ARC0538. REWORK OF BRACKET ASSY P/N ARC0538 ACCOMPLISHED PER EA 8-5740-77350. 2L73 4F A22WE 20040512000382004051200038NM 2004 5 12 04FDEA01168 120040507A5712 RIB DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT WING SLAT TRACK 16 I/B RIB FOUND CRACKED. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II & INSTALLED NEW RIB AT LT WING SLAT TRACK NR 16 AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040512000392004051200039NM 2004 5 12 04FDEA01169 120040507A5753 STOP FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RT WING O/B FLAP AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040512000472004051200047CE 2004 5 12 BAQA094409 120040505A324050030967 BRAKE ASSY LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP MLG WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 295 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2L72 4F4 F A10CE E6WE 20040512000532004051200053 2004 5 12 BAQA094422 420040504A342142000332430 INDICATOR UROCOPEC135 EC135P2 5620027EU AHRU INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03703ME25 0314 UNIT WOULD NOT CALIBRATE. S/N CURRENTLY INSTALLED WAS CANNED FROM AC S/N 0143. REPLACED WITH SERVICABLE UNIT. 05/07/2004 1G72 3U H88EU 20040512000572004051200057EU 2004 5 12 BAQA094312 120040504A2100625SMP5600BB1C DRIVE SHAFT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE AC DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH1183 0179 FLEX SHAFT DAMAGED IN CENTER SECTION. UNIT IS ORGINIAL EQUIPMENT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 05/10/2004 1G72 3U3 UO H88EU E42NE 20040512000792004051200079NM 2004 5 12 04FDEA01116 120040430A5712ARB2850506 RIB DOUG MD11 MD11 3023602NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING - NR 16 SLAT TRACK INBOARD RIB SUSPECTED CRACK AS MARKED. RIGHT WING - NR 16 SLAT TRACK INBOARD RIB REMOVED AND REPLACED AS PER SRM 51-31-01, VOL 2. 2L73 4F RTA22WE 20040512000852004051200085NM 2004 5 12 04FDEA01120 120040430A5512 SKIN DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 HORIZONTAL STAB LEFT UPPER FWD PLANK NR 14L BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATION. COMPLIED FEDEX EA NR 1-5510-76030, HORIZONTAL STABILIZER BARREL NUT BORE 14 LT FITTING FABRICATION. 2L73 4F RTA22WE 20040512000872004051200087NM 2004 5 12 04FDEA01121 120040430A5512 SKIN DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 HORIZONTAL STAB UPPER FWD PLANK NR 14R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76018, HORIZONTAL STABILIZER BARREL NUT BORE 14 RT FITTING FABRICATION. 2L73 4F RTA22WE 20040512000912004051200091NM 2004 5 12 04FDEA01043 120040422A5320A5A71141 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT, LEFT TUNNEL AT STA 5-113 TO STA 1541, STR 40 LONGERON SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT, LONGERON SPLICE REMOVED AS PER SRM 51-31-01 VOL 2 AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040512000942004051200094 2004 5 12 ASMF200405004 420040502A22302587781901 SERVO DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE AUTOTHROTTLE FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23216AM11743 49586 718411 DURING TRANSIT CHECK, CAPTAIN REPORTED A DIFFERENCE BETWEEN THROTTLES OF 1.5 INCHES. AUTOTHROTTLE SERVO UNIT WAS REPLACED IAW MM 22-31-01. TRIMMING WAS PERFORMED IAW MPCM 71-00-01 AND AUTOTHROTTLE CLUTCH DRUMS SERVICE WAS PERFORMED IAW MM 76-11-04, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040512001002004051200100NM 2004 5 12 CALA0400483 120040509A5330143N3521 SKIN BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714102 27292 INSPECTION FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 778 BETWEEN LBL 6 AND RBL 6. THE CORRODED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 204. 2L72 4F RTA2NM 20040512001012004051200101NM 2004 5 12 CALA0400484 120040509A5315BAC1518338 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714102 27292 INSPECTION FOUND FLOORBEAM CORRODED AT BS 740 FROM RBL 9 TO LBL 4. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20040512001042004051200104SW 2004 5 12 ERAA094434 120040417A6410212010750105FM BLADE BELL 412 412 1182202SW TAIL ROTOR PEELING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03421EH3732 33067 T/R BLADE SENT FOR REPAIR 5/29/2003. BLADE HAS ONLY 110.2 HRS SINCE REPAIR AND IS PEELING. RETURNING ON REPAIR ORDER RW-898678 REQUESTING WARRANTY REPAIR. 1G72 4U H4SW 20040512001072004051200107NE 2004 5 12 ERAA094438 120040118A262289113402 EXTINGUISHER SKRSKYS61 S61N 8142104NE CABIN INOPERATIVE A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03562EH 61257 UNIT HAS LOW PRESSURE, BARE METAL SHOWING, ID PLATE IS DAMAGED, WARNING LABEL IS DAMAGED, PRESSURE GUAGE IS 50 PSI OUT OF CALIBRATION. ACTION TAKEN: CLEANED, INSEPCTED, HYDROTESTED IAW CFR 49 180.205, BEAD BLAST AND PAINTED, OVERHAULED, REPLACED GUAGE, INSTALLED DECALS, FILLED, LEAK CHECKED, WT CHECKED (7.00 LBS W/ CARTRIDGES INSTALLED) IAW CMM 26-21-83 REV 4 2G72 4U 1H15 20040512001092004051200109SW 2004 5 12 ERAA094441 120040317A3212D24921119 COVER BELL 412 412 1182202SW MLG FLOAT LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03167EH 33089 FLOAT BAG HAS LEAK IN FORWARD CELL AT BLACK SEAM ACTION TAKEN: SENT TO OFFSHORE HELICOPTERRS FOR REPAIR. 14 HOLES FOUND 1 MISSING RELIEF VALVE. PATCHED 14 HOLES, REPLACE 1 MISSING RELIEF VALVE. C/W 6 MONTH INSPECTION IAW 41-SI-2. 1G72 4U H4SW 20040512001102004051200110SW 2004 5 12 ERAA094442 120040220A3212D24921119 COVER BELL 412 412 1182202SW FLOAT LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03412EH619 33001 FLOAT BAG HAS PIN HOLES ALL OVER AFT COMPARTMENT ACTION TAKEN: SENT TO OFFSHORE HELICOPTERS. FLOAT WAS REPAIRED IAW OHSS 100-1 AND C/W INOPERATIVE IAW 412-01-2. 1G72 4U H4SW 20040512001132004051200113NM 2004 5 12 04FDEA001112 120040428A5754651622292 SKIN BOEING727 727200 138407ENM L/E SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 COMPLY WITH EA 7-5750-77346; WINGS, LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE. 2L73 4F RTA3WE 20040512001152004051200115WP 2004 5 12 04FDEA01153 120040504A5753ARC1497505 FITTING DOUG DC10 DC1010 3022110WP RT FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT O/B FLAP NR3 VANE FITTING FWD BOLT HOLE IS CORRODED. REPLACED NR 3 VANE FITTING TO BE INSTALLED ON EO 8-5750-7-5000 C PT 4 AT MAE. 2L73 4F A22WE 20040512001162004051200116GL 2004 5 12 ALG2004F00020 220040420A732023078032 HMU BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL SYSTEM UNSERVICEABLE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03537AL3820 53230 CAE847018 FUEL FUMES WERE NOTED IN THE AFT RT PORTION OF THE PASSENGER COMPARTMENT. NOTED TO BE STRONG, SO DIVERTED TO HAVE IT CHECKED. MAINTENANCE REMOVED HAD BIN AND FUEL VALVE ACCESS PANEL. WITH BATTERY POWER ON, BOOST PUMPS RUNNING AND FUEL VALVE OPEN NOTED HEAVY FUEL DRIP ALMOST STREAMING FOR HMU CASE DRAIN. ENGINE PAN ACCUMULATING FUEL AND SEEPAGE CAUSING VAPORS IN HAT BIN AREA. REMOVED UNSERVICEABLE HMU, PART ON ORDER. 1G71 3U3 UO H2SW E1GL 20040512001182004051200118WP 2004 5 12 04FDEA01154 120040504A5753ARC1537509 SUPPORT DOUG DC10 DC1010 3022110WP RT FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT O/B FLAP VANE ASSY NR 4 VANE TRACK MOUNT AFT BOLT HOLE IS CORRODED. REPLACED SUPPORT ASSY TO BE INSTALLED AT MAE. 2L73 4F A22WE 20040512001192004051200119NM 2004 5 12 04FDEA001113 120040429A5712 RIB BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 RIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1. 2L73 4F RTA3WE 20040512001202004051200120NM 2004 5 12 04FDEA001114 120040429A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 FWD CARGO COMP'T FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4. 2L73 4F RTA3WE 20040512001212004051200121EA 2004 5 12 UIA9312 120040407A2910DH829111650 LINE DHAV DHC8 DHC8311 1386006EA HYD SYSTEM BROKEN Z B EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 TW00152395092 571 IN FLIGHT (NR 2 HYD PUMP CAUTION LIGHT COME ON AND ROLL SPLR OB HYD CAUTION LIGHT COME ON AND NR 2 PRESS IND. (0) AND QTY IND (0) AFTER A/C LANDED CHECK NR 2 HYD SYS FOUND RT OB SPLR PRESSURE TUBE BROKEN. IAW AMM 20-50-52 REPLACED FLEXIBLE HOSE FOR TEMPORALITY REPAIR . REPACED NR 2 EDP AND PRESSURE MANIFOLD FILTER AND RETURN MANIFOLD FILTER AND CASE DRAIN FILTER. ENG RUN-UP CHK BACK NML. 2H72 4T RTA13NM 20040512001222004051200122NM 2004 5 12 AWXA200400464 120040427A532069429494 SUPPORT ANGLE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN SUPPORT ANGLE (CLIP) OF AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE (CLIP) AT AFT CARGO COMPARTMENT DOOR SILL BS 807, RBL 30; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE (CLIP) PER DWG 69-42949; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4B. 2L72 4F RTA16WE 20040512001232004051200123EU 2004 5 12 AWXA200400433 120040329A5320D5348004320200 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK GALVANIC CORROSION WAS FOUND ON L-2 DOOR THRESHOLD DRAIN PAN SILL AT FR 68, Y1732 LT. MAINTENANCE REMOVED CORRODED L-2 DOOR THRESHOLD DRAIN PAN SILL AT FR 68, Y1732 LT; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 53-41-14 FIG 101. 2L72 4F RTA28NM 20040512001252004051200125NE 2004 5 12 115401 220040418A7261 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1735SZ 35SZ 357 DURING FLIGHT THE CREW RT ENGINE OIL PRESSURE DROPPED TO 30PSI WITH THE ASSOCIATED OIL PRESSURE WARNING ON THE CWP. CREW FOLLOWED THE QRH AND DIVERTED TO SCE. AFTER LANDING CREW CHECKED RH ENGINE OIL LEVEL. SIGHT GLASS SHOWED BELOW NORMAL. CREW NOTICED NO VISIBLE LEAKS. A/C TAKEN OUT OF SERVICE 4-18-04 AT 1915(LT) PIT MX SENT TO SCE TO ACCOMPLISH A C-SUMP. OPERATIONAL TEST AND LEAK CHECK GOOD. A/C RETURNED TO SERVICE 4-19-04 AT 1515(LT) 2L72 4T4 TRTA52EU E8NE6 20040512001272004051200127EU 2004 5 12 228551 120040419A3220 BUSHING SAAB SF340 SF340A 7850100EU NLG LOOSE A UHLACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL17123XS 123XS DURING TAKE-OFF ROLL AT AROUND 40 KNOTS THE A/C HAD A VIOLENT NOSE WHEEL SHIMMY. THE CREW ABORTED TAKE-OFF AND RETURNED TO THE GATE IN PIT. A/C TAKEN OUT OF SERVICE 4-19-04 AT 2245(LT) PIT MX TIGHTENED NOSE STEERING COLLAR BUSHING, PERFORMED TAXI CHECK. NO DEFECTS NOTED. A/C RETURNED TO SERVICE 4-20-04 AT 0845(LT) 2L72 4T RTA52EU 20040512001282004051200128EU 2004 5 12 AWXA200400426 120040402A5347D53472177200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 47 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 FIG 9-12. 2L72 4F RTA28NM 20040512001302004051200130EU 2004 5 12 236681 120040413A2613 WARNING LIGHT SAAB SF340 SF340A 7850100EU ENGINES ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL1714XS 340A014 ON TAKE-OFF ROLL, AIRCREW RECEIVED ON CWP TAILPIPE HOT LIGHT FOR BOTH ENGINES. AIRCREW REJECTED TAKE-OFF AND RETURNED TO THE GATE 2L72 4T RTA52EU 20040512001382004051200138EU 2004 5 12 181001 120040211A7930 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU TRIPPED A UHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL1735SZ 35SZ ON TAKE-OFF AIRCREW NOTICED OIL PRESSURE WENT TO ZERO AND OIL TEMP WENT TO -50 DEGREES C. AIRCREW REJECTED TAKE-OFF AND RETURNED TO THE GATE. AIRCREW FOUND CIRCUIT BREAKER POPPED. MAINTENANCE DISPATCHED TO A/C 2L72 4T RTA52EU 20040512001392004051200139EU 2004 5 12 178632 120040227A2933 INDICATOR SAAB SF340 SF340A 7850100EU HYD SYSTEM MALFUNCTIONED A UHLAO OTHER N FALSE WARNING DEDESCENT 1 GL1743SZ 340A043 APPROXIMATELY 40 MILES FROM PIT THE CREW NOTICED THE HYDRAULIC QUANTITY GUAGE WAS DROPPING. THEY ALSO INITIALLY NOTICED THE PRESSURE ALSO DROPPING. AFTER REFERENCING THE QRH THE PRESSURE STABILIZED BUT THE QUANTITY WAS STILL ERRATIC. THE CREW HAND PUMPED THE GEAR DOWN AND CONTACTED ATC TO ALERT THEM OF THEIR SITUATION. THE A/C LANDED WITHOUT INCEDENT AND TAXIED TO THE GATE NORMALLY. A/C TAKEN OUT OF SERVICE 2-27-04 AT 2000(LT). PIT MAINTENANCE INSPECTED THE FUSELAGE AND HYDRAULIC SERVICE AREA FOR SIGNS OF LEAKING AND FOUND NO DEFECTS. MAINTENANCE SERVICED THE HYDRAULIC SYSTEM, PERFORMED OPERATIONAL TESTS OF ALL ASSOCIATED SYSTEMS. NO DEFECTS WERE NOTED AT THAT TIME. A/C RETURNED TO SERVICE 2-27-04 AT 22L72 4T RTA52EU 20040512001412004051200141NE 2004 5 12 102831 220040321A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT MALFUNCTIONED A UHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL1735SZ 35SZ 357 DURING TAKE-OFF ROLL AT APPROXIMATELY 80-90 KNOTS THE CREW NOTICED THE RT ENGINE TORQUE FLUCTUATING FROM 70-115 PERCENT. THE CREW RETARDED THE POWER LEVERS AND ABORTED THE TAKE-OFF. A/C TAKEN OUT OF SERVICE 3-21-04 AT 1755 (LT) 2L72 4T4 TRTA52EU E8NE6 20040512001422004051200142EU 2004 5 12 109641 120040323A7720 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE ITT MALFUNCTIONED A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL17157SD 510 DURING TAKEOFF ROLLOUT AT ABOUT 50 KTS THE PILOT NOTICED THE DIGITAL ITT INDICATION WAS 999 AND THE ANALOG INDICATION WAS NORMAL, PILOT RETARDED POWER LEVERS AND RETURNED TO GATE. 2L72 4T4 TRTA52EU E8NE 20040512001432004051200143EU 2004 5 12 102201 120040311A3244 WHEEL SAAB SF340 SF340A 7850100EU NLG MALFUNCTIONED A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL17360SZ 340A006 ON TAKEOFF ROLL A/C EXPERIENCED A NOSE WHEEL SHIMMY AT 65KTS. AIRCREW ABORTED TAKE-OFF AND RETURNED SAFETY TO THE GATE. 2L72 4T RTA52EU 20040512001462004051200146EU 2004 5 12 011821 120040330A2613 WARNING LIGHT SAAB SF340 SF340A 7850100EU TAILPIPE ILLUMINATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1714XS 340A014 ON TAKE-OFF ROLL AIRCREW RECEIVED TAIL PIPE HOT LIGHT. AIRCREW REJECTED TAKE-OFF AND RETURNED TO THE GATE 2L72 4T RTA52EU 20040512001472004051200147EU 2004 5 12 094681 120040402A7931 WARNING SYSTEM SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE OIL PRESSURE ACTIVATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL17140CQ 140CQ ON TAKEOFF ROLLOUT AT ABOUT 70 KTS. THE PILOT HAD A CWP OIL PRESSURE WARNING ALONG WITH OIL PRESSURE INDICATOR IN THE YELLOW (20 PSI), PILOT ABORTED TAKEOFF AND RETURNED TO THE GATE. 2L72 4T4 TRTA52EU E8NE 20040512001482004051200148EU 2004 5 12 150711 120040502A2613 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE LT TAILPIPE ILLUMINATED A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1740SZ 40 E367503 DRG153688 AIRCRAFT HAD TAKEN OFF FROM LEX WHEN THE LT TAIL PIPE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO LEX WITHOUT INCIDENT. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040512001562004051200156EA 2004 5 12 COMA0460300 120040506A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01917CA4510 7017 FLIGHT 5228 GEAR DISAGREE WARNING. COULD NOT DUPLICATE - REPLACED THE PSEU 2L72 4F RTA21EA 20040512001582004051200158NM 2004 5 12 AWXA200400500 120040430A532065458078 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MAJOR REPAIR - DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 278, STR 14 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 278, STR 14 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL IAW DWG 65-45807; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3, 6, & 7. 2L72 4F RTA16WE 20040512001602004051200160EU 2004 5 12 AWXA200400483 120040506A3240E0415B3LM025 SWITCH AIRBUS320 A320232 3930326EU COCKPIT FAULTY A AWXAK NONE O OTHER LDLANDING 1 WP28653AW 1003 PHX - BRAKES - BRAKES MOMENTARILY GRABBED ON TOUCHDOWN, AUTO BRAKES WERE NOT SELECTED AND MANUAL BRAKES WERE NOT BEING APPLIED, BRAKES RELEASED AFTER ABOUT 1 SECOND. MAINTENANCE TROUBLESHOT PER TSM 32-42-00-810-889, AND REMOVED AND REPLACED PUSH BUTTON SWITCHES 7GG & 8GG, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040512001632004051200163WP 2004 5 12 04FDEA01155 120040506A5347FX4929147 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CARGO COMPT SEAT TRACK HAS AREAS OF ELONGATED SCALLOPS FROM F/S 1561-1651 RBL 8. REMOVED AND REPLACED SEAT TRACK AT FS 1561-1651 RBL-8 IAW SRM 51-31-01 & SRM 53-70-00 AT MAE. 2L73 4F A22WE 20040513000022004051300002CE 2004 5 13 DXTA200400304 120040430A3411CM2944612 PITOT LINE CESSNA750 750 2076810CE LEAKING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07935QS 7500135 POWER WAS ADVANCED ON TAKEOFF , SHORTLY AFTER AMBER CAS PITOT HEAT FAIL LT AND RT CAME ON, ABORTED TAKE OFF. TROUBLESHOT AND FOUND STATIC LINE LEAKING, REMOVED AND REPLACED STATIC LINE AND MICRO ADC, LEAK CHECK AND OP CHECK GOOD IAW MFG MM CHAPTER 34-11-08, FAR 91.411. 2L72 4J RTT00007WI 20040513000032004051300003CE 2004 5 13 DXTA200400306 120040503A2170 COALESCER BAG CESSNA750 750 2076810CE AIR DISTRIBUTIONCONTAMINATED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07936QS 7500036 WHILE ENROUTE PASSENGERS SMELLED A BURNING ODOR COMING FROM THE FORWARD PASSENGER SEATING AREA. THE ODOR WAS COMING AND GOING AND HAD AN ODOR OF BURNED INSULATION OR WIRING, DIVERTED AIRCRAFT. INSPECTED WIRING BEHIND THE METER CONTROL PANEL AND FOUND NO EVIDENCE OF BURNED WIRES, CLEANED COALESCER SOCK IAW MM, RAN AIRCRAFT NO FURTHER ODOR DETECTED. 2L72 4J RTT00007WI 20040513000042004051300004CE 2004 5 13 60633 120040416A3260 BULB BEECH 1900 1900D 1154162CE MLG INDICATOR INOPERATIVE A AMWAO OTHER N FALSE WARNING APAPPROACH 1 CE07144ZV UE144 NOSE GEAR DOWN/LOCKED ANNUN D/N ILLUM ON APPROACH. REMOVED AND REPLACED BOTH NOSE GEAR DOWN/LOCKED BULBS. 2L72 4T RTA24CE 20040513000092004051300009EU 2004 5 13 XNOA1182 120040407A5270 SWITCH AIRBUS300 A300B4203 3930306EU MLG DIRTY A XN0AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23371PC 157 DURING TAKEOFF ROLL, RT MAIN LANDING GEAR DOOR UNLOCK LT ILLUMINATED WITH GEAR DOWN LIGHT OUT. CLEANED DOOR SWITCH, OPS CK NORMAL ON GROUND IAW A300 MM 32-12-11. 2L72 4F RTA35EU 20040513000102004051300010WP 2004 5 13 MWEA040055 120040414A5320991014010 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 THE SUBFLOOR HAS A CRACK AT STATION 218 UNDER NR 4 SEAT TRACK. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040513000182004051300018EA 2004 5 13 SWIA200413284 120040503A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FS 280 LT FLOORBEAM LBL 9.0 I/B AND O/B ATTACH ANGLE CRACKED. (FOUND DURING C-CHECK INSPECTION). REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-23-00, AND RII 53-401. 2L72 4F RTA21EA 20040513000402004051300040NM 2004 5 13 USAA040062 120040315A5330 SKIN BOEING737 7373B7 1384580NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU51007 23702 FOUND SKIN CRACKED 3.5 INCH, FS 882 AND S25R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-00 FIG 229. (M) 2L72 4F RTA16WE 20040513000442004051300044NM 2004 5 13 USAA040061 120040315A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US52400 23311 FOUND SKIN CRACKED 2 INCHES, STATION 747, STRINGER 24R. INSTALLED DOUBLER PER EA 95275. (M) 2L72 4F RTA16WE 20040513000452004051300045NM 2004 5 13 USAA040067 120040329A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US51825 22957 FOUND SKIN CRACKED 1.25 INCH, BELOW S18R BS 751. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040513000472004051300047NM 2004 5 13 USAA040063 120040327A5321 FLOOR PANEL BOEING737 737301 1384611NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US46553 23557 FOUND FLOOR PANEL GOUGED 4 INCHES, STATION 992 RBL 39. MANUFACTURED OUT OF 2024 T3 020 PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20040513000492004051300049NM 2004 5 13 USAA040065 120040327A53201138864 FLOOR SUPPORT BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US46553 23557 FOUND FLANGE CRACKED 1.5 INCH FLOOR SUPPORT STATION 937 BL 0. REMOVED TOP FLANGE OF FLOOR SUPPORT, REPLACED WITH NEW PART EPN 1138864 PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20040513000502004051300050NM 2004 5 13 USAA040045 120040324A5330 SKIN BOEING737 737301 1384611NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US50373 23231 FOUND SKIN CRACKED 1 INCH, EXTERNAL FUSELAGE SKIN STATION 727D PLUS 2 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040513000512004051300051NM 2004 5 13 USAA040044 120040324A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US50373 23231 FOUND SKIN CRACKED 1.5 INCH, EXTERNAL FUSELAGE SKIN STATION 765 STRINGER 23R. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040513000532004051300053NM 2004 5 13 USAA040051 120040225A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU48278 23706 CLT - FOUND SKIN WITH 3 CRACKS, 2 INCHES, 2.5 INCHES AND .5 INCHES, BS 727D S23R-S24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040513000542004051300054NM 2004 5 13 USAA040052 120040302A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU50964 23856 CLT - FOUND SKIN CRACKED 2 INCHES, FS 885 JUST ABOVE STRINGER S25R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040511000382004051100038 2004 5 11 DL76L040376 420040427A2397 POWER CABLE BOEING767 767332 1382001NM CABIN SHORTED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27192DN 28449 AIRPHONE POWER CABLE SHORTED AT SEAT 4C-E LT SIDE FLOOR AREA. DISCONNECTED CANNON PLUGS IN FLOOR AREA. REPLACED CABLE. 2L72 4F RTA1NM 20040511000442004051100044 2004 5 11 DL777040380 420040428A34168220409201 ALTIMETER BOEING777 777232 1385232NM COCKPIT INOPERATIVE A DALAK NONE O OTHER CRCRUISE 1 SO27862DA 29734 STANDBY AIRSPEED INOP, STANDBY ALTIMETER INOP. MAT FAULTS MTC MSG 34-19908 AND 34-18893. REPLACED STANDBY ALTIMETER IND PER AMM. STANDBY ALT AND STANDBY A/S IND NOW CHECK OKAY. 2L72 4F RTT00001SE 20040511000512004051100051NM 2004 5 11 AWXA200400452 120040409A53306545768106 SKIN BOEING737 7373S3 1384711NM FUSELAGE BULGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR - DURING C-17 CHECK THE SKIN WAS FOUND BULGING BETWEEN FASTENERS INSIDE THE FORWARD CARGO COMPARTMENT AT A PREVIOUSLY INSTALLED REPAIR DOUBLER BS 370 TO BS 390, RBL 36. MAINTENANCE REMOVED REPAIR DOUBLER BS 370 TO BS 390, RBL 36 AND FOUND EVIDENCE OF WATER ENTRAPMENT, NO CORROSION. CLEANED AND TREATED SURROUNDING SKIN AREA; FABRICATED A DOUBLER, TRIPLER, AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20040511000582004051100058 2004 5 11 AWXA200400458 420040430A2230B546CCM0104 COMPUTER AIRBUSA319 A319132 3930340NM AUTOTHRUST SYS FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28813AW14844 1350 ON TAKEOFF AT PHX EN ROUTE FOR JFK MASTER CAUTION LIGHT ILLUMINATED WITH NO FAULTS DISPLAYED ON ECAM, REJECTED TAKEOFF AT APPROX 70 KNOTS. MX TROUBLESHOT PROBLEM TO AUTO THRUST FAILURE. ISSUED MEL 22-30-01, COND 1, AUTO THRUST FUNCTION INOP. ON 05/01/2004 WHEN AIRCRAFT RETURNED TO PHX, MAINTENANCE R & R NR 1 FMGC IAW T/C R2A22302, OPERATIONAL CHECK GOOD. FUNCTIONAL TEST OF FMGC CONFIRMED FAILURE. UNIT FAILED ARINC TEST ON AUTOMATIC TEST EQUIPMENT, BITE DATA INDICATED AUTOPILOT / AUTO THROTTLE FUNCTION FAILURE IN FLT. REPLACED INTEGRATED CIRCUIT GATE, INTEGRATED CIRCUIT H-CMOS INVERTER, INTEGRATED CIRCUIT FLIP-FLOP LATCH AND 2 EACH PROGRAMMABLE MEMORY CHIPS. UNIT WAS REPAIRED AND TESTED IAW CMM. 2L72 4F RTA28NM 20040511000602004051100060NM 2004 5 11 AWXA200400460 120040502A3397D9299200900000 WIRE AIRBUSA319 A319132 3930340NM CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 PHX - EEL - DURING INSPECTION FOUND A BROKEN WIRE IN HARNESS FOR EMERGENCY ESCAPE PATH LIGHT AT CONNECTOR 5751VC, SEAT ROW 8 RT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 8 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040511000772004051100077NM 2004 5 11 UPS04M42257 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 03 BARREL NUT HOLE FOUND CORROSION ON BOTTOM , SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 03 LT REMOVED PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.057 INCHES IS WITHIN LIMITS PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN1058-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF . UPS ENGINEERING FILE NR MD11-55-20014) 2L73 4F RTA22WE 20040511000782004051100078NM 2004 5 11 UPS04M42258 120040225A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 13 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 13 LT REMOVED PER SRM51-21-01 VOL II REV 34, MATERIAL REMOVED 0.051 INCHES IS WITHIN LIMIT PER EO MD11-5510-19409D. BARREL NUT HOLE REPAIRED PER EN1062-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20014) 2L73 4F RTA22WE 20040511000802004051100080 2004 5 11 UPS04142361 420040506A2565 LEVER AIRBUSA300 A300F4622R 3930360EU GIRT BAR FITTINGJAMMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01148UP 831 SLIDE LEVER JAMMED AND COULD NOT DISARM SLIDE. ADJUSTED GIRT BAR FITTING PER MM 52-10-11-5, OPS CK GOOD. 2L72 4F RTA35EU 20040511000932004051100093WP 2004 5 11 UPS04842335 120040403A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01748UP 45948 INSPECTION TYPE: C-1, STA 1240-1260 L35L INTERCOSTAL DENTED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-1-20D MATERIAL ID & FAB OF NEW PART IAW DAC DWG 49758507, HEAT TREATED PART REF LOAD HT041904 -3. ALODINE & PRIMED INTERCOSTAL IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040511001012004051100101WP 2004 5 11 UPS04842262 120040330A57305769857388 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RT WING CENTER LE. INNER SKIN IS CRACKED AT FASTENER HOLES XW408 TO XS520. REMOVED, FABRICATED AND REPLACED INNER SKIN AND DOUBLER IAW DWG. 5769759 AND 5769857 AND SRM. 51-1-20D,51-1-21 2L74 4F RT4A25 20040511001162004051100116NM 2004 5 11 04FDEA01177 120040510A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.095 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040511001202004051100120NM 2004 5 11 CALA0400479 120040507A5512 SKIN BOEING737 737524 1384721NM HORIZ STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727610 27323 INSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5510-01741. 2L72 4F RTA16WE 20040511001262004051100126NM 2004 5 11 UPS04M42299 120040206A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 32 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.070 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. BARREL NUT HOLE REPAIRED PER EN 1030-04 (REF UPS ENGINEERING FILE NR MD11-55-20017). 2L73 4F RTA22WE 20040511001372004051100137NM 2004 5 11 CALA0400481 120040508A53306545768 SKIN BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727610 27323 INSPECTION FOUND FUSELAGE SKIN CORRODED AFT OF FORWARD BAG BIN DOOR CUTOUT AT STA 452, S22R. A REPAIR WAS INSTALLED IAW ECRA 5330-03351. 2L72 4F RTA16WE 20040511001492004051100149NM 2004 5 11 UPS04M42275 120040218A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER LT NR 27 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 27 LT REMOVED PER SRM 51-21-01 VOL II REV 34 MATERIAL REMOVED 0.059 IS WITHIN LIMITS PER EN1057-04. 2. BARREL NUT HOLE REPAIRED PER EN1057-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2L73 4F RTA22WE 20040511001542004051100154NM 2004 5 11 04FDEA01090 120040424A5320ACA7150513 SPLICE DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040511001552004051100155NM 2004 5 11 04FDEA01103 120040425A534765441224 SPLICE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 COMPLY WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE CORRODED. COMPLIED WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE. 2L73 4F RTA3WE 20040511001612004051100161NM 2004 5 11 ASAA0440070 120040303A531065C335831 CREASE BEAM BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - RIGHT CREASE BEAM WEB AT STATION 986 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WEB. (M) 2L72 4F RTA16WE 20040511001722004051100172WP 2004 5 11 GTIA040266 120040323A33500105611001 LIGHT DOUG DC9 DC983 3022083WP VENTRAL STAIRS MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND LEFT VENTRAL STAIR PANEL SMALL LIGHT ASSEMBLY MISSING. REPLACED LEFT VENTRAL STAIR PANEL SMALL LIGHT ASSEMBLY. (M) 2L72 4F RTA6WE 20040511001732004051100173WP 2004 5 11 GTIA040267 120040302A5730 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND RIGHT WING LOWER FUEL ACCESS PANEL RL56C HAS CRACKED/DAMAGED AT FASTENER HOLES. REMOVED OLD FUEL ACCESS PANEL. INSTALLED NEW PANEL. (M) 2L72 4F RTA6WE 20040511001942004051100194NM 2004 5 11 ASAA0440071 120040303A532065C335821 WEB BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT GALLEY AREA HAS GOUGE IN FLOOR WEB STATION 1016, LBL 40. REMOVED AND REPLACED WEB. (M) 2L72 4F RTA16WE 20040511001972004051100197NM 2004 5 11 ASAA0440069 120040304A5315BAC14902865 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM PER SRM. (M) 2L72 4F RTA16WE 20040511002022004051100202WP 2004 5 11 GTIA040265 120040405A2560 LANYARD DOUG DC9 DC983 3022083WP EVAC SLIDE MISINSTALLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 DTW - FOUND R1 SLIDE COVER RELEASE LANYARD INSTALLED INCORRECTLY. CORRECTLY INSTALLED R1 SLIDE COVER RELEASE LANYARD. (M) 2L72 4F RTA6WE 20040512000032004051200003NM 2004 5 12 UPS04M42303 120040208A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STABILIZER RT NR 2 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING & SIDEWALL SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.014. BARREL NUT HOLE REPAIRED PER EN 1028-04 (REF UPS ENGINEERING FILE NR MD11-55-20016) BUSHING FABRICATED & INSTALLED PER EO MD11-5510-1940 9-D. 2L73 4F RTA22WE 20040512000222004051200022WP 2004 5 12 FE5F200400001 120040506A4930360800014 FUEL CONTROL DOUG DC9 DC982 3022082WP APU DETERIORATED W FE5FK NONE HB ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP03 9527 16 53167 DURING TRANSIT , APU RUNNING SUPPLIED BOTH ELEC.POWER AND AIR CONDITION, THE ELECTRICAL POWER ON / OFF INTERMITTENTLY, AND FINALLY ELEC.POWER DISCONNETED. AFTER THAT, THE SMOKE CAME OUT AT REAR CABIN AREA. MAINTENANCE CHECKED FOUND APU RPM WILL FLUCTUATED WHEN SUPPLIED BOTH ELEC. POWER AND PNEUMATIC. AFTER REPLACED THE APU FCU , CORRECT THE PROBLEM. MAINTENANCE ALSO CHECKED THE APU SUPPLIED ELEC.CIRCUIT, POWER RELAYS , NO ANOMALY FOUND. 2L72 4F A6WE 20040512000242004051200024NM 2004 5 12 S04421001 120040102A5270 SWITCH BOEING747 747400 NM PWA 4056 PW4056 NE E/E BAY DOOR MALFUNCTIONED W SAJFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP03 27965 ATB DUE TO MSG (DOOR ELEC MAIN). AFTER LANDING, GROUND CREW CONFIRMED MAIN E/E BAY DOOR WAS CLOSED PROPERLY. REVIEW CMC MESSAGE FOUND CMC MSG 52113 DOOR MAIN ELEC EQUIP ACCESS SW FAILED. NOT ANY CABIN PRESSURIZED RELATED MSG. WAS FOUND. GRD TEST CABIN PRESS CPC-A, CPC-B, MANUAL CABIN PRESSURIZE SYS CHECK NML. ALL CABIN DOORS AND CARGO DOORS VISUAL CK COND NML AND MAIN ELEC DOOR OPS AND IND. NML. FOR PRECAUTION PURPOSE, REPLACED MAIN EQUIPMENT DOOR WARNING SWITCH. PILOT REPORTED CABIN PRESSURE WAS NOT NORMAL AT LEVEL OFF FL260, QAR DATA SHOWS CABIN PRESSURE WAS NORMAL. MAIN ELEC DOOR IS PLUG-IN TYPE AND MAIN ELECTRICAL DOOR WAS CLOSED PROPERLY. QAR DIDN'T SHOW ANY ANOMALOUS DATA OF CABIN PRESSURE SYSTEM. 2L74 4F4 FRTA20WE E24NE 20040512000492004051200049CE 2004 5 12 BAQA094411 120040505A324050030967 BRAKE ASSY LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP MLG WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 295 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2L72 4F4 F A10CE E6WE 20040512000582004051200058SW 2004 5 12 BAQA094473 120040430A2841222375064103 INDICATOR BELL 222 222U 1182140SW LYC LTS101LTS101* NE FUEL QTY STICKS E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03223HX8056 47511 FUEL QYT INDICATOR RT NEEDLE STICKS ON UNIT. REPLACED WITH SERVICABLE UNIT. 05/10/2004 1G72 3U3 U H9SW E5NE 20040512000732004051200073EU 2004 5 12 04FDEA01152 120040504A5531 RIB AIRBUS310 A310203 3930313EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE 248 VERTICAL STABILIZER TRAILING EDGE ON RIGHT SIDE EDGE FOR ACCESS PANEL ATTACHMENT STRUCTURE, PROPAGATION OF CORROSION NOTED FROM RIB 12-17, AS MARKED. REMOVED CORROSION IAW A310-200 SRM 51-74-10. REPAIRED IAW FEDEX EA 6-5530-77658 AND SRM A310-200 51-74-10 AND 55-30-00. 2L72 4F RTA35EU 20040512000862004051200086WP 2004 5 12 ASMF200405006 120040503A7711LG80E1 TRANSMITTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE EPR FAILED W ASMFCD ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TOTAKEOFF 1 SW23751RA11652 49779 725412 AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF LOW TAKE OFF POWER ON RT ENGINE AND DURING TAXING RT ENGINE WITH STALLS. CAPTAIN REPORTED THAT PERFORMED TWO TAKE OFF INTENTS AND RT ENGINE DID NOT RESPOND. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE EPR TRANSMITTER WAS REPLACED IAW MM 77-11-02, TEST CORRECT. BOROSCOPE INSPECTION WAS PERFORMED ON 6A AND 7A STAGES OF HIGH COMPRESSOR, 1A AND 4A STAGES OF TURBINE SECTION AND IGV´S IAW MM 72-00-00, ALL CORRECT. REJECTED TAKE OFF INSPECTION WAS PERFORMED IAW MM 05-57-00 AND OPERATIONAL TESTS IN BOTH ENGINES WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040512000952004051200095WP 2004 5 12 CALA0400482 120040508A53205936469U1 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772825 49485 INSPECTION FOUND FITTING AT AFT LOWER CORNER OF AFT BAGGAGE BIN DOOR CUTOUT CORRODED. A NEW FITTING WAS INSTALLED IAW SRM 51-30-5. 2L72 4F A6WE 20040512001032004051200103NM 2004 5 12 CALA0400485 120040509A5315143N501555 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714102 27292 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 720 FROM RBL 58.2 TO LBL 58.2. REPAIRED IAW ECRA 5320-01753, SRM 51-10-02, FIGURE 12, PARAGRAPH 6 AND 51-40-02, FIGURE 3 AND 12. 2L72 4F RTA2NM 20040512001082004051200108NM 2004 5 12 04FDEA01115 120040429A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 LOWER FUSELAGE EXTERIOR SURFACE, SKIN CRACKED AT STATION 1010 AT APPROX STR 29R WITH CORROSION. CUT OUT DAMAGED SECTION OF SKIN IAW SRM 53-30-3 FIG 3A, FABRICATED AND INSTALLED (1) EA DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3A AT MAE. 2L73 4F RTA3WE 20040512001142004051200114SW 2004 5 12 ERAA094444 120040111A6730212076005101 SERVO BELL 412 412 1182202SW CYCLIC LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH4448 33004 SERVO LEAKING AND INPUT LEVER LOOSE. MAJOR SCORING ON UPPER PISTON UPPER PISTON SEVERELY SCORED, RUN OUT CHECK EXCEEDS ALL LIMITS .280. PERFORMED OVERHAUL INSPECTION TIMED AND TESTED. POST ASSEMNBLY RUN OUT CHECK .106. 1G72 4U H4SW 20040512001242004051200124NM 2004 5 12 AWXA200400411 120040424A5330654888233 SKIN BOEING737 7373G7 1384595NM FUSELAGE SCORED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK THE FUSELAGE SKIN WAS FOUND SCORED AT BS 1104 AND BS 1121, BETWEEN STR 3 RT AND STR 4 RT. MAINTENANCE PERFORMED A HFEC INSPECTION OF PREVIOUS BLEND OUT AND FOUND NO CRACKS. ENLARGED TRIM BY 0.04 INCH AS AN INSURANCE CUT; FABRICATED A REPAIR DOUBLER FROM 2024-T3 0.050; INSTALLED REPAIR PART IAW ER 03-5300-04115-ES3. 2L72 4F RTA16WE 20040512001262004051200126EU 2004 5 12 AWXA200400425 120040402A5347D53472177204 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 RT BETWEEN FR 47 AND FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT FROM FR 47 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF TRACK AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 51-42-11 FIG 9-13 & 18. 2L72 4F RTA28NM 20040512001322004051200132NE 2004 5 12 112161 220040330A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE SHUTDOWN A UHLAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL17148SD 340A148 462 DURING CLIMB OUT THE CREW HEARD A LOUD BANG FROM THE LH ENGINE WHICH THEN HAD AN UNCOMMANDED SHUTDOWN. THE PROP FEATHERED AS IT SHOULD, THE CREW DECLARED AN EMERGENCY AND LANDED BACK IN BUF SAFELY. AFTER LANDING THE CREW INSPECTED THE LT ENG FOR SIGNS OF FOD INTAKE NONE WAS NOTED BY THE CREW. 2L72 4T4 TRTA52EU E8NE6 20040512001332004051200133EU 2004 5 12 AWXA200400429 120040402A5347D5337111200000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 LT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 LT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9 & 18. 2L72 4F RTA28NM 20040512001362004051200136EU 2004 5 12 024251 120040423A3150 WARNING LIGHT SAAB SF340 SF340A 7850100EU TCAS ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL17157SD 157 JUST AFTER DEPARTURE AIRCREW RECEIVED TCAS FAILED INDICATION, THEN ATC NOTIFIED THEM THAT THEY COULD NOT BE SEEN. AIRCREW CYCLED THE TRANSPONDERS AND RECEIVED ANOTHER NOTICE FROM ATC. AIRCREW RETURN TO FIELD 2L72 4T RTA52EU 20040512001452004051200145EU 2004 5 12 111701 120040326A2613 SENSOR SAAB SF340 SF340A 7850100EU TAIL PIPE CONTAMINATED A UHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL1714 14 AIRCRAFT ON TAKE-OFF ROLL RECEIVED TAIL PIPE HOT LIGHT. AIRCREW REJECTED TAKE-OFF RETURNED TO GATE. MAINTENANCE REMOVE MOISTURE FROM TAIL PIPE, OPS CHECKED GOOD 2L72 4T RTA52EU 20040512001492004051200149 2004 5 12 109161 420040417A6122 GOVERNOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R390 R3904123F27 NE RIGHT MALFUNCTIONED A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL17360SZ 340A006 478 DRG1120690 AIRCRAFT ABORTED TAKE OFF WHEN THE RT POWER WOULD NOT SET. POWER LEVERS BROUGHT TO 80 PERCENT, CTOT SET TO 90 PERCENT. LT WENT TO 90 PERCENT, RT STAYED AT 80 PERCENT. 2L72 4T4 TRTA52EU E8NE6 6 CP31NE 20040512001502004051200150EU 2004 5 12 101171 120040218A3010 BOOT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE DEICE SYSTEM MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17118SD THE AIRCRAFT ENTERED ICING CONDITIONS AIRCREW SELECTED WING AND EMPENAGE DE-ICING. TIMER LIGHT ILLUMINATED IN SINGLE CYCLE, AIRCREW SELECTED CONTINUOUS CYCLE AND THE SAME RESULT FOLLOWED AND NO GREEN BOOT INFLATION LIGHTS. AIRCREW ATTEMPTED MANUAL INFLATION OF THE DE-ICE BOOTS, AGAIN NO INFLATION LIGHTS AND AIRCREW COULN'T TELL IF THE BOOTS WERE INFLATING VISUALLY. AIRCREW WAS INSTRUCTED TO RETURN TO PIT FOR FURTHER TROUBLESHOOTING. 2L72 4T4 TRTA52EU E8NE 20040512001612004051200161NM 2004 5 12 AWXA200400484 120040502A531065C807351 DOOR FRAME BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK INTERGRANULAR CORROSION WAS FOUND ON INNER CHORD AT R-2 DOOR BETWEEN BS 980 AND BS 995, RBL 63, RUNNING UNDER DOOR DRAIN. MAINTENANCE REMOVED CORRODED INNER CHORD AT R-2 DOOR FROM BS 980 TO BS 995, RBL 63; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PARA 7. 2L72 4F RTA16WE 20040513000062004051300006NM 2004 5 13 DHL2004760004 120040502A2823714810 VALVE BOEING727 7272B7 138407LNM PWA JT8 JT8D17A 52049NE FUEL SHUTOFF FAILED A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01760AT 21954 715301 ENGINE NR 1 AFTER ENGINE STARTED AND ACCELERATED TO 40 PERCENT N2 FUEL FLOW BEGAN TO FLUCUATED + OR - 200 WHEN ENGINE ACCELERATED TO 40 PERCENT N2 FUEL FLOW WENT TO ZERO AND ENGINE SHUTDOWN. COMPLETED ENGINE FAILURE EMERGENCY CHECKLIST. REMOVED AND REPLACED NR1 FUEL P+D VALVE IAW MM 73-12-01 AND NR 1 ENG FUEL SHUT-OFF VALVE. OPS CHECK GOOD AFTER GROUND RUN IAW JRH 5.2 AND 7.3 AND MM 28-22-1 2L73 4F4 F A3WE E2EA 20040513000112004051300011WP 2004 5 13 MWEA040056 120040414A53209915562 STIFFENER DOUG DC9 DC981 3022081WP LONGERON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 STIFFENER BELOW LONGERON 1 ON FORWARD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED. FABRICATED AND INSTALLED ANGLES. 2L72 4F A6WE 20040513000132004051300013NE 2004 5 13 P5CA0401068 220040403A7200 ENGINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 1 MALFUNCTIONED A P5CAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23920FT 22237 702264 NR 1 ENGINE UNABLE TO MAKE TAKEOFF POWER. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00-11 AND MM 71-00-02. ENGINE RUN NORMAL. 2L74 4F4 F A20WE E3NE 20040513000202004051300020 2004 5 13 HE66094420 420040507A3452C19252PCO8 COMPUTER UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE NR 2 UNSERVICEABLE E HEEAO OTHER G MULTIPLE FAILURE CRCRUISE 1 SW03135CR1439 0164 TRANSPONDER WOULD NOT WORK ABOVE 4000 FT AND NR 2 DME WOULD NOT WORK. AFTER HAVING THE TRANSPONDER REPAIRED SEVERAL TIMES AND FINALLY REPLACED PROBLEM STILL NOT CORRECTED. REPLACED NR 2 FCDM AND ALL PROBLEMS CORRECTED. 1G72 3U3 U H88EU E34NE 20040513000422004051300042WP 2004 5 13 GTIA040272 120040408A3350 SIGN DOUG DC9 DC982 3022082WP EXIT DISLODGED A GTIAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL23812NK 48021 EXIT SIGN AT AFT GALLEY FELL OFF ON TAKEOFF. RE-ATTACHED LUMINESCENT EXIT STRIP AT AFT GALLEY FLOOR AREA. (M) 2L72 4F A6WE 20040513000562004051300056NM 2004 5 13 USAA040050 120040220A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US46593 23556 FOUND SKIN CRACKED 2.5 INCHES, BS 520 S12R. INSTALLED DOUBLER PER EA 95192. (M) 2L72 4F RTA16WE 20040513000572004051300057NM 2004 5 13 USAA040054 120040308A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU51922 23228 FOUND STRINGER CRACKED TWO PLACES 1.5 INCH AND 1.25 INCH, STRINGER 24L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVED PER SRM 53-00-01 FIG 229 DETAIL XI. (M) 2L72 4F RTA16WE 20040513000592004051300059NM 2004 5 13 USAA040055 120040308A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU51922 23228 CLT - FOUND STRINGER CRACKED 1.25 INCH, AT STRINGER 23L BETWEEN BS 727E AND BS 747. INSTALLED DOUBLERS AFTER DAMAGE REMOVAL PER SRM 53-00-01 DETAIL XI FIG 229. (M) 2L72 4F RTA16WE 20040513000602004051300060EA 2004 5 13 COMA0460293 120040502A2130 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A COMABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01451CA 7562 FLIGHT 5096 CABIN ALTITUDE CAUTION DURING CLIMB. PERFORMED SYSTEM RESET OPERATIONAL CHECK OF PRESSURIZATION SYSTEM NORMAL. 2L72 4F RTA21EA 20040513000612004051300061WP 2004 5 13 04FDEA01156 120040506A5347 CARGO TRACK DOUG DC10 DC1010 3022110WP MAIN CARGO COMPTGOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CARGO COMPT CARGO TRACK HAS GOUGED AREAS FROM FS 899-919 LBL 47. REMOVED AND REPLACED CARGO TRACK AT FS 899-919 LBL 47 IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040513000632004051300063WP 2004 5 13 04FDEA01158 120040506A5347 CARGO TRACK DOUG DC10 DC1010 3022110WP MAIN CARGO COMPTGOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CARGO COMPT CARGO TRACK HAS GOUGED AREAS FROM FS 1441-1501 RBL 27. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-70-00 AT MAE. 2L73 4F A22WE 20040513000652004051300065EU 2004 5 13 04FDEA01160 120040507A5311 FRAME AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE 248 AVI BAY FROM FR 7 TO 10 STR 48L TO 48R E&E GROUND ACCESS DOOR CUTOUT SKIN SURFACE, FRAME ATTACHING SUPPORT ANGLES, PLATES, FITTINGS & FASTENERS HAVE CORROSION OVER ENTIRE CUTOUT AREA. REMOVED CORROSION AT AVI BAY FR 7 TO 10 STR 48L TO 48R, DOOR CUTOUT SKIN SURFACE, FRAME, SUPPORT ANGLES, PLATES, FITTINGS. ALL AREAS WITHIN LIMITS, FRAME SECTION NR 7 OUT OF LIMITS. REMOVED CORRODED SECTION OF FRAME NR 7 & ATTACHING PARTS. REINSTALLED NEW SECTION OF FRAME NR 7, RE-INSTALLED ATTACHING PARTS PER A310 SRM 51-40-21, 51-22-00, 51-74-10, 51-72-10. 2L72 4F RTA35EU 20040513000662004051300066NM 2004 5 13 04FDEA001107 120040428A5753 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. 2L73 4F RTA22WE 20040513000672004051300067NM 2004 5 13 04FDEA001108 120040428A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 I/B CORRODED. 2L73 4F RTA22WE 20040513000682004051300068NM 2004 5 13 04FDEA001109 120040428A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 O/B CORRODED. 2L73 4F RTA22WE 20040513000692004051300069NM 2004 5 13 04FDEA01178 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.505, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.503 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000742004051300074NM 2004 5 13 04FDEA01196 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.397 MATERIAL REMOVED: 0.001 REMAINING THICKNESS: 0.396 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000762004051300076NM 2004 5 13 04FDEA01198 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.410 MATERIAL REMOVED: 0.004 REMAINING THICKNESS: 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000782004051300078NM 2004 5 13 04FDEA01179 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.223 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000812004051300081NM 2004 5 13 04FDEA01182 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000822004051300082NM 2004 5 13 04FDEA01183 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.391 MATERIAL REMOVED: 0.002 REMAINING THICKNESS: 0.389 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000832004051300083NM 2004 5 13 04FDEA01184 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.127 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000852004051300085NM 2004 5 13 04FDEA01186 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.094 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000872004051300087NM 2004 5 13 04FDEA01200 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.487 MATERIAL REMOVED: 0.003 REMAINING THICKNESS: 0.484 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000882004051300088NM 2004 5 13 04FDEA01201 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.094. REPAIRED AS PER EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000892004051300089NM 2004 5 13 04FDEA01202 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.503 MATERIAL REMOVED: 0.002 REMAINING THICKNESS: 0.501 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000902004051300090NM 2004 5 13 04FDEA01203 120040510A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHEET 2. ORIGINAL THICKNESS =0.406, MATERIAL REMOVED =0.003, AND REMAINING THICKNESS =0.403. 2L73 4F RTA22WE 20040513000912004051300091NM 2004 5 13 04FDEA01204 120040510A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502 SHEET 2. ORIGINAL THICKNESS =0.476, MATERIAL REMOVED =0.002, AND REMAINING THICKNESS =0.474. 2L73 4F RTA22WE 20040513000922004051300092NM 2004 5 13 04FDEA01066 120040422A5320ADA8424501 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT, RIGHT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON SPLICE FOUND CRACKED. FWD CARGO COMPARTMENT, RIGHT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040513000932004051300093NM 2004 5 13 04FDEA01205 120040510A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221, AND REPAIRED AS PER EA 1-5740-75956, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040513000952004051300095EU 2004 5 13 04FDEA01004 120040418A3244Z3200202 TIRE AIRBUS310 A310222 3930315EU NLG FAILED A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO25421FE4973 616 342 ON T/O NOSE WHEEL TIRE FAILED AT V1=144 KTS, GW = 297.0. FOUND RIGHT TIRE BURST AND TORN TREAD. REMOVED AND REPLACED LT & RT NOSE TIRE ASSY PER MM 12-37-32-0-04. PREMATURE REMOVAL/INSTALLATION OFF MFG 286351003-1-51. 2L72 4F RTA35EU 20040513000972004051300097NM 2004 5 13 04FDEA01132 120040503A5511 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 HORIZONTAL STABILIZER, RIGHT UPPER FWD SPAR CAP NR 1R BARREL NUT BORE CORROSION BLEND-OUT EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2L73 4F RTA22WE 20040513000992004051300099NM 2004 5 13 04FDEA01134 120040503A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, OUTBOARD FLAP VANE NR 5 FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NRS 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK 2L73 4F RTA22WE 20040513001002004051300100NM 2004 5 13 04FDEA01135 120040503A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NRS 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK 2L73 4F RTA22WE 20040513001022004051300102NM 2004 5 13 04FDEA001105 120040426A534760822324 CARGO TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 MAIN CARGO COMPT CARGO TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACED CARGO TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2. 2L73 4F RTA3WE 20040513001032004051300103NM 2004 5 13 04FDEA01138 120040503A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20040513001072004051300107NM 2004 5 13 04FDEA001089 120040424A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON 44R SPLICE FOUND CRACKED. 2L73 4F RTA22WE 20040513001082004051300108NM 2004 5 13 04FDEA001090 120040424A5320ACA7150513 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. FWD CARGO COMPARTMENT STA 755-775 LONGERON 45L SPLICE CRACKED. REMOVED AND NEW SPLICE INSTALLED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040513001102004051300110WP 2004 5 13 04FDEA001092 120040424A5751 SKIN DOUG DC10 DC1010 3022110WP LT WING AILERON WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 LEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LIMITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALLED ON N00519. 2L73 4F A22WE 20040513001122004051300112NM 2004 5 13 04FDEA01137 120040503A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, OUTBOARD FLAP VANE NR 2 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBOARD FLAP NR 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20040513001132004051300113NM 2004 5 13 04FDEA001016 120040421A5347FXMACH0193 CARGO TRACK BOEING727 727200 138407ENM CARGO BAY GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 MAIN CARGO COMPT CARGO TRACK HAS GOUGED SCALLOPS AT FS 755 - 765 LBL 63. REMOVED AND REPLACED CARGO TRACK SECTION AT FS 755 - 765 LBL 63, IAW SRM 51-30-2 AT MAE. 2L73 4F RTA3WE 20040513001142004051300114NM 2004 5 13 04FDEA001017 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. 2L73 4F RTA22WE 20040513001152004051300115NM 2004 5 13 04FDEA001018 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. 2L73 4F RTA22WE 20040513001162004051300116NM 2004 5 13 04FDEA001019 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. 2L73 4F RTA22WE 20040513001192004051300119NM 2004 5 13 04FDEA001070 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. 2L73 4F RTA22WE 20040513001202004051300120NM 2004 5 13 04FDEA001071 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. 2L73 4F RTA22WE 20040513001212004051300121NM 2004 5 13 04FDEA001072 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE 8 OUTBOARD CORRODED. 2L73 4F RTA22WE 20040513001232004051300123NM 2004 5 13 04FDEA001074 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. 2L73 4F RTA22WE 20040513001242004051300124NM 2004 5 13 04FDEA001075 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE 8 OUTBOARD CORRODED. 2L73 4F RTA22WE 20040513001262004051300126NM 2004 5 13 04FDEA001077 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. 2L73 4F RTA22WE 20040513001272004051300127WP 2004 5 13 04FDEA001095 120040424A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 8.5 HAS BROKEN SCALLOP AT FS 755. REPLACED SECTION OF SEAT TRACK FROM FS 725 TO 785 AT RBL 8.5 IAW DC-10 SRM 53-70-00 VOL 1. 2L73 4F A22WE 20040513001312004051300131NM 2004 5 13 04FDEA001079 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. 2L73 4F RTA22WE 20040513001352004051300135NM 2004 5 13 04FDEA001083 120040424A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE 8 OUTBOARD CORRODED. 2L73 4F RTA22WE 20040514000012004051400001NM 2004 5 14 04FDEA001084 120040424A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO, STA 1671 RIGHT SIDE LONGERON 37 FASTENER HOLE SUSPECTED CRACK. 2L73 4F RTA22WE 20040514000022004051400002NM 2004 5 14 04FDEA001085 120040424A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO, STA 1671 RIGHT SIDE LONGERON 30 SUSPECTED CRACK. 2L73 4F RTA22WE 20040514000042004051400004NM 2004 5 14 04FDEA001086 120040424A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO, STA 1811 LEFT LONGERON 40 FOUND CRACKED. 2L73 4F RTA22WE 20040514000062004051400006NM 2004 5 14 04FDEA001021 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. 2L73 4F RTA22WE 20040514000072004051400007NM 2004 5 14 04FDEA001022 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. 2L73 4F RTA22WE 20040514000082004051400008NM 2004 5 14 04FDEA001023 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. 2L73 4F RTA22WE 20040514000092004051400009NM 2004 5 14 04FDEA001024 120040422A2752 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. 2L73 4F RTA22WE 20040514000102004051400010NM 2004 5 14 04FDEA001025 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. 2L73 4F RTA22WE 20040514000122004051400012NM 2004 5 14 04FDEA001027 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. 2L73 4F RTA22WE 20040514000132004051400013NM 2004 5 14 04FDEA001028 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. 2L73 4F RTA22WE 20040514000152004051400015NM 2004 5 14 CALA0400469 120040505A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND A 1.9 INCH CRACK IN FUSELAGE SKIN AT BS 767, S21R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090 AND 53-00-01. 2L72 4F RTA16WE 20040514000162004051400016NM 2004 5 14 CALA0400470 120040505A3350D71702030 CHARGER BOEING767 767424ER 1385270NM EMERGENCY LIGHTSINOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2776062 29457 THE EMERGENCY LIGHTS AT STA 368, WL 200 (SEAT ROW 1KL) DID NOT OPERATE DURING TEST OF BATTERY PACK. THE M730 EMERGENCY LIGHT CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 201. 2L72 4F RTA1NM 20040514000202004051400020NM 2004 5 14 CALA0400474 120040505A53206546812186 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND LT DIAGONAL FLOOR SUPPORT BEAM CORRODED AT FS 1006-1010. THE FLOOR SUPPORT BEAM WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040514000212004051400021NM 2004 5 14 CALA0400475 120040506A534069455512 ATTACH FITTING BOEING757 757224 1384958NM THRESHOLD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714118 27560 INSPECTION FOUND FORWARD CARGO DOOR CUTOUT LOWER SILL THRESHOLD FORWARD, SECOND, AND THIRD ATTACH FITTINGS AT LOWER FORWARD CORNER CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA2NM 20040514000222004051400022NM 2004 5 14 CALA0400476 120040506A5410313A11380 ANGLE BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00. 2L72 4F RTA16WE 20040514000262004051400026EA 2004 5 14 ASOA04280 120040411A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE AFT INTERCOSTAL BRACKET AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT INTERCOSTAL BRACKET AT FS 484, RBL 26 IAW ASA EO 600-0098. (M) 2L72 4F RTA21EA 20040514000272004051400027EA 2004 5 14 ASOA04273 120040407A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD. (M) 2L72 4F RTA21EA 20040514000282004051400028EA 2004 5 14 A6WA200440039 120040410A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 FOUND LEFT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. PERFORMED A MAJOR REPAIR TO LEFT FS 621 UNDERFLOOR SUPPORT ANGLE BY REMOVING DAMAGE AND INSTALLING REPAIR ANGLES IAW BOMBARDIER INC REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20040514000292004051400029WP 2004 5 14 GTIA040307 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 LEFT OUTBOARD DENTED, PUNCTURED, CORE CRUSHED, BROKEN INSERTS, COVERING PEELING AND DELAMINATED. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000302004051400030WP 2004 5 14 GTIA040308 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN STATION 541 TO 465 LBL 24 ICHES TO 44 INCHES FLOOR PANEL HAS CRACKED, DAMAGED ON EDGE. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040514000312004051400031WP 2004 5 14 GTIA040309 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSLAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 1155 TO 1250 METALLIC PANEL LEFT SIDE OUTBOARD HAS DISBONDED AT RUB STRIP/HAT CHANNEL. REBONDED RUBSTRIP HAT CHANNEL. (M) 2L72 4F RTA6WE 20040514000332004051400033WP 2004 5 14 GTIA040311 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND MAIN C/B STATION 1079 TO STATION 1117 RIGHT SIDE MID FLOOR PANEL HAS CRACKED/DAMAGED CORNER AND EDGE. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040514000372004051400037WP 2004 5 14 GTIA040303 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND CABIN FLOORBOARD STATION 150-160 CENTER INSERT BROKEN AND CORE DAMAGED. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000392004051400039WP 2004 5 14 GTIA040305 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PEELING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 150-160 LEFT OUTBOARD COVERING PEELING. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000402004051400040WP 2004 5 14 GTIA040306 120040318A5753 SKIN DOUG DC9 DC983 3022083WP RT TE FLAP LIGHTNING STRIKEA GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND RIGHT OUTBOARD FLAP INBOARD NR 2 TRAILING EDGE HAS LIGHTING STRIKE SEVERAL PLACES AT LOWER INBOARD SURFACE. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN. (M) 2L72 4F RTA6WE 20040514000412004051400041WP 2004 5 14 GTIA040312 120040327A5315 FLOORBEAM DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND FLOOR SUPPORT CRACKED AT FS 905 36 INCHES LBL. REMOVED CRACKED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040514000422004051400042WP 2004 5 14 GTIA040313 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND CABIN FLOORBOARD STATION 693-769 RIGHT OUTBOARD STRIPS DEBONDED. REBONDED STRIPS ON CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000452004051400045EA 2004 5 14 ASOA04277 120040411A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11864AS 7502 DURING AN A-CHECK IN BTR, THE LEFT WING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT WING EMERGENCY EXIT LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040514000462004051400046WP 2004 5 14 GTIA040314 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FS DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 769-826 RIGHT OUTBOARD HAT CHANNEL DEBONDED. BONDED THE DISBONDED HAT CHANNEL. (M) 2L72 4F RTA6WE 20040514000472004051400047WP 2004 5 14 GTIA040315 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 1174-1250 RIGHT OUTBOARD STRIPS DEBONDED. REBONDED STRIPS ON CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000482004051400048WP 2004 5 14 GTIA040317 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 1250 TO STATION 1309 LBL 24 TO 44 INCHES FLOOR PANEL HAS SOFT/MUSHEY SEVERAL INSERTS CORRODED. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000522004051400052EU 2004 5 14 USAA040075 120040330A5310D53472117220290 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW 0929 BFM - FOUND BEAM CORRODED 1.8 INCHES BY 1.4 INCHES BY .060 INCH AREA, FRAME 66-68, -Y1220, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040511001652004051100165NM 2004 5 11 ASAA0440059 120040303A532065479575 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - AFT PIT INTERCOSTAL AT STATION 787-790 STRINGER 25R CORRODED UPPER SURFACES. REMOVED AND REPLACED INTERCOSTAL STATION 767 TO 790 STRINGER 25R. (M) 2L72 4F RTA16WE 20040511001702004051100170WP 2004 5 11 GTIA040254 120040319A5320 ATTACH ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND FORWARD CARGO DOOR LATCH SUPPORT ATTACHMENT ANGLE IS CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M) 2L72 4F RTA6WE 20040511001762004051100176 2004 5 11 GTIA040258 420040402A2565D29982107 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR UNSERVICEABLE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 LGA - L1 DOOR SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE. (M) 2L72 4F A6WE 20040511001782004051100178NM 2004 5 11 ASAA0440050 120040229A531565538441 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 CYR - AFT CARGO PIT FLOORBEAM HAS CORROSION TOPSIDE WHERE FLOORPANEL SPLICE STRAP CROSSES, AFT OF 727F, LBL 16 TO RBL 16. REPAIRED AFT PIT FLOORBEAM AT STATION 727F, RBL 16. (M) 2L72 4F RTA16WE 20040511001842004051100184NM 2004 5 11 ASAA0440068 120040303A531465458661197 KEELBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - RIGHT KEEL BEAM CHORD AT STATION 502 HAS CORROSION. REPAIRED KEEL BEAM AT STATION 502. (M) 2L72 4F RTA16WE 20040511001862004051100186NM 2004 5 11 ASAA0440051 120040229A53106517688U165 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND L1 DOOR LOWER THRESHOLD CREASE BEAM UPPER HAS CORROSION FROM STATION 294.5 TO 344, LBL 50. REMOVED AND REPLACED CREASE BEAM. (M) 2L72 4F RTA16WE 20040511002012004051100201WP 2004 5 11 GTIA040264 120040407A3350 SIGN DOUG DC9 DC982 3022082WP CABIN MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 LGA - FOUND AFT GALLEY FLOOR EXIT GLOW SIGN MISSING. REPLACED MISSING AFT GALLEY FLOOR EXIT GLOW SIGN, OK FOR SERVICE. (M) 2L72 4F A6WE 20040512000082004051200008NM 2004 5 12 UPS04M42279 120040213A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, HORIZONTAL STAB LT NR 35 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM LT NR 35 HOLE REMOVED AS PER SRM51-21-01 VOL II REV 3 4, MATERIAL REMOVED 0.054 WITHIN LIMITS OF EN1041-04. BARREL NUT HOLE REPAIRED PER EN1041-04. BUSHING FABRICATED AND INSTALLED PER EO MD11-5510-19409D. (REF. UPS ENGINEERING FILE NR MD11-55-20017) 2L73 4F RTA22WE 20040512000122004051200012WP 2004 5 12 UPS04842236 120040331A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FWD LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 82 LONG. 31R REMOVED,FABRICATED AND REPLACED FINGER DOUBLER IAW DWG. 5779916 AND SRM. 51-1-20D,51-1-21 2L74 4F RT4A25 20040512000152004051200015WP 2004 5 12 UPS04842245 120040421A1420 CONNECTOR DOUG DC8 DC871F 302199DWP BATTERY PACK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01772UP 46072 EMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTOR LOOSE ON BATTERY PACK. RE INSTALLED SAME, SYSTEM TEST OK 2L74 4F RT4A25 20040512000412004051200041NM 2004 5 12 04FDEA01143 120040504A5753ARC2512504 BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT AFT I/B FLAP O/B HINGE, O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651 - WINGS - TRAILING EDGE FLAPS, LT & RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20040512000482004051200048CE 2004 5 12 BAQA094410 120040505A324050030967 BRAKE ASSY LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP MLG WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 295 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2L72 4F4 F A10CE E6WE 20040512000522004051200052 2004 5 12 ALGA094419 420040507A830023065470 COVER BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUSELAGE DEFECTIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBEM 53246 CAE847087 GEARBOX COVER REMOVED DUE TO IMPROPER REPAIRS AT TACH/GEN BORE. SENT PART TO VENDOR FOR WARRANTY REPAIR. 1G71 3U3 UO H2SW E1GL 20040512000672004051200067 2004 5 12 BAQA094260 420040504A3414L341M10C1001 INDICATOR UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE AIRSPEED INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH268 0069 INDICATOR LIGHTING DIM. REPLACED WITH SERVICABLE UNIT. 05/05/2004 1G72 3U3 UO H88EU E42NE 20040512000702004051200070 2004 5 12 BAQA094413 420040505A3421060001301 GYRO UROCOPEC135 EC135P1 8680990EU COCKPIT STICKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME304 0009 GYRO LIGHT, EHSI HEADING STICKING. REPLACED WITH SERVICABLE UNIT. 05/06/2004 1G72 3U O H88EU 20040512000722004051200072NM 2004 5 12 04FDEA01147 120040504A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 TRANSVERSE FRAME DENTED, RT SIDE STA Y= 1681, ALONG LONGERON 12R. DENTED AREA AT TRANSVERSE FRAME RT, STA Y= 1681, LONGERON 12R TRIMMED OUT AND REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. DAMAGE TOLERANCE INSPECTION REQUIREMENT CATEGORY B - INITIAL 14,500 CYCLES AND REPETITIVE 9,500 CYCLES. (TSN 44,468 AND CSN 8,723) COMPLIED EA NR 1-5310-76690, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NO.: 1-2520-7-33008. 2L73 4F RTA22WE 20040512000752004051200075NM 2004 5 12 04FDEA01124 120040430A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE BARREL NUT HOLE 2B MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040512000772004051200077NM 2004 5 12 04FDEA01126 120040430A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE ACTUATOR HOLE 8 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040512000962004051200096NM 2004 5 12 ASMF200405005 120040503A3620 WARNING LIGHT BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE COCKPIT ILLUMINATED W ASMFCD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW23802AM 26270 727115 AIRCRAFT SUSPENDED TAKE OFF AT 70 KTS AND RETURNED TO PLATFORM BECAUSE (L ENG BLEED OFF) LIGHT TURNED ON. (L ENG BLEED OFF) LIGHT WAS DEFERRED IAW MEL 36-11-1. FIM 36-10-00 PROCEDURE WAS PERFORMED AND SUSPENDED TAKE OFF INSPECTION WAS ACCOMPLISHED IAW MM 05-51-14, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20040512000992004051200099NE 2004 5 12 ASMF200405009 220040506A749744509 IGNITION LEAD DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE LT IGNITION DAMAGED W ASMFK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW23501AM 709877 709834 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT LT ENGINE IGNITION SYSTEM OUT OF SERVICE. IGNITION BOX, PLUG AND IGNITION CABLE WERE REPLACED IAW MM 74-10-01, 74-20-01 AND 74-20-02, RESPECTIVELY, AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE IGNITION CABLE WAS DETECTED WITH DAMAGE. IGNITION CABLE WAS REPLACED IAW MM 74-00-00, TEST CORRECT. 2L72 4F4 F A6WE E9NE 20040512001062004051200106GL 2004 5 12 ERAA094437 220040123A7320252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20 03013GL ENGINE FAILED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03153EH14716 702 GOVERNOR NOT HOLDING SINGLE ENGINE MAXIMUM BEEP RANGE. SENT FOR REPAIR. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A 1G72 3U3 U H3EU E4CE 20040512001112004051200111NM 2004 5 12 04FDEA01122 120040430A5512 SKIN DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 HORIZONTAL STAB RIGHT UPPER AFT PLANK NR 32R BARREL NUT BORE CORROSION BLEND OUT FOUND EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER, BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2L73 4F RTA22WE 20040512001172004051200117NE 2004 5 12 ASMF200405008 220040506A7230 BLADE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23755RA9369 9369 49727 725382 DURING OVERNIGHT SERVICE, FOD´S WERE DETECTED ON 15 BLADES OF LT ENGINE. BOROSCOPE INSPECTION WAS PERFORMED ON C6 AND C7 COMPRESSOR STAGE IAW MM 72-00-00 AND NO DAMAGE WAS DETECTED. ON FAN STAGE, 3 BLADES WERE DETECTED WITH DAMAGES AND C1 FAN STAGE WAS REPLACED IAW MM 72-33-02, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040512001352004051200135EU 2004 5 12 150141 120040412A1420 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT TAILPIPE DIRTY A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17150CN 150CN 434 DURING CLIMB OUTTHE LT TAILPIPE HOT LIGHT ILLUMINATED ON THE CWP. THE CREW FOLLOWED THE QRH AND SHUT THE ENGINE DOWN, DECLARED AN EMERGENCY AND LANDED SAFELY BACK IN PIT. A/C TAKEN OUT OF SERVICE 4-12-04 AT 1830 (LT) PIT MX INSPECTED AND CLEANED LH TAILPIPE HOT WIRING HARNESS CONNECTION. PERFORMED GROUND RUN OF LH ENGINE AT ALL POWER SETTINGS AND COULD NO DUPLICATE DISCREPANCY ON THE GROUND. A/C RETURNED TO SERVICE 4-12-04 AT 1905 (LT). 2L72 4T4 TRTA52EU E8NE6 20040512001442004051200144EU 2004 5 12 188441 120040220A3260 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE MLG MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1743SZ 340A043 AFTER RETRACTING THE LANDING GEA THE LEFT DOWN INDICATOR (GREEN) LIGHT ILLUMINATED, WITH NO LIGHT IN THE HANDLE, AND THE HANDLE IN THE UP POSITION. VISUAL INPECTION BY THE CREW CONFIRMED THE GEAR WAS RETRACTED. THE A/C RETURNED TO PITTBURGH AND THE TOWER DECLARED AN EMERGENCY. 2L72 4T4 TRTA52EU E8NE 20040512001572004051200157EA 2004 5 12 COMA0470039 120040507A5280CC670105723 CROSSBEAM CNDAIR CNDAIRCL600 CL6002C10 1390015EA MLG DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01355CA 10067 10067 LT MAIN GEAR DOOR CROSS MEMBER IS CRACKED. REMOVED AND REPLACED LT MAIN GEAR DOOR CROSS MEMER IAW MFG REPAIR ENGINEERING ORDER REO 670-52-82-014. 2L72 4F RTA21EA 20040512001592004051200159EU 2004 5 12 AWXA200400435 120040417A5321D53670047000 FLOORBOARD AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK A 4 INCH CRACK WAS FOUND IN CABIN FLOORBOARD (261NF). MAINTENANCE REMOVED CRACKED FLOORBOARD BETWEEN FR 64 TO FR 66; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBOARD IAW A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20040512001622004051200162NM 2004 5 12 04FDEA01001 120040417A53206519606178 WEB BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25279FE 22346 CENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE. 2L73 4F RTA3WE 20040513000012004051300001CE 2004 5 13 DXTA200400305 120040503A3150 WARNING SYSTEM CESSNA560 560XL 2076702CE COCKPIT ACTIVATED E DXTAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 GL07668QS 5605268 AFTER TAKEOFF THE GEAR WAS RETRACTED, THE THREE GREEN INDICATORS WENT OUT BUT THE RED LIGHT REMAINED ON, FLAPS AND STAB WERE NOT COMMANDED TO MOVE. RED LIGHT REMAINED ON AND THE HYDRAULIC PRESSURE LIGHT FLASHED, CYCLED GEAR SECOND TIME WITH SAME RESULTS. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040513000082004051300008NE 2004 5 13 0400651238 220040502A73218062826 FCU DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 3 ENGINE MALFUNCTIONED A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01238W 12043114 48267 517255 TAKEOFF WAS ABORTED AT 120 KTS WHEN THE NR 3 ENGINE FAILED TO REACH TAKEOFF TARGET NR 1. CREW ALSO REPORTED AN N2 EXCEEDANCE ON THE NR 3 ENGINE PRIOR TO ABORTING TAKEOFF. MAINTENANCE REPLACED THE MEC AND TRIMMED THE ENGINE. ALL ENGINE INDICATIONS WERE NORMAL. 2L73 4F4 F A22WE E23EA 20040513000412004051300041NM 2004 5 13 USAA040066 120040331A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US54183 22954 FOUND BULKHEAD SKIN CRACKED .25 INCH, BS 178 BULKHEAD LBL 5.7 WL 234. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER EO 5300V152C AND SRM 53-10-08 FIG 209 SHT 5. (M) 2L72 4F RTA16WE 20040513000522004051300052NM 2004 5 13 USAA040047 120040307A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US53965 22953 FOUND SKIN CRACKED .5 INCH, AFT SERVICE DOOR LOWER HINGE CUTOUT. CUT OUT DAMAGE AND INSTALLED DUOBLER PER SRM 53-60-01 FIG 208 AND EA 78095. (M) 2L72 4F RTA16WE 20040513000552004051300055NM 2004 5 13 USAA040053 120040303A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US39947 24554 CLT - FOUND SKIN CRACKED 1.5 INCH, FS 727E AT S24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040513000712004051300071NM 2004 5 13 04FDEA01193 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.093 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000792004051300079NM 2004 5 13 04FDEA01180 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.003, REMAINING THICKNESS 0.402. REPAIRED AS PER EA 1-5750-75954 - WINGS LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000842004051300084NM 2004 5 13 04FDEA01185 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.500 MATERIAL REMOVED: 0.008 REMAINING THICKNESS: 0.492 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513001012004051300101WP 2004 5 13 04FDEA001104 120040426A5410 SUPPORT DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE FIRE LOOP BROKEN A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25315FE35836 48313 ON TAKEOFF AT 1200 FT AGL THE EGT ON NR 1 ENG WENT TO 960 DEGREES INDICATED VERY RAPIDLY. TOOK 4 THROTTLE WIDTHS TO BRING THE EGT BACK INTO PARAMETERS AND ENG RUNNING SMOOTLY. DUMPED APPROX 20K LBS OF FUEL. INITIAL VISUAL INSPECTION REVEALED SEVERAL BROKEN PNEU DUCT SUPPORT STRUTS, MANY BROKEN CLAMPS, RUPTURED HIGH PRESSURE TURBINE COOLING DUCT AT 12 O'CLOCK POS BROKEN FIRE LOOP SUPPORT TUBE ETC AND METAL IN TAILPIPE. INTERROGATED NR 1 EGT INDICATOR, DATA SHOWED 975 DEG FOR 10 SEC. 2L73 4F4 F A22WE E23EA 20040513001182004051300118EU 2004 5 13 AWXA200400302 120040323A2121 BEARING TECHNOFAN AIRBUS320 A320231 3930325EU FAILED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 WP28646AW 1204 271 PHX - EMERGENCY LANDING - FLT 0272 - ON SHORT AND FINAL INTO PHX EN ROUTE FROM SNA ENCOUNTERED SMOKE AND A STRONG ELECTRICAL BURNING ODOR IN CABIN, DONNED MASKS AND DECLARED EMERGENCY. MAINTENANCE FOUND THE AVIONICS COOLING FAN (EXTRACT FAN) BEARINGS SEIZED CAUSING FAN TO OVERHEAT. REMOVED AND REPLACED AVIONICS COOLING FAN IAW AMM 21-26-51-000-001; OPERATIONAL CHECK WAS GOOD. *S/D* VENDOR CONFIRMED FAILURE OF AVIONICS COOLING FAN S/N 1204; UNIT WAS SEIZED. FRONT BEARING FAILED CAUSING IMPELLER TO BIND AGAINST BELLMOUTH. REPLACED FRONT & REAR BEARINGS, FRONT FLANGE, CENTER HOLE, AND BEARING FACE, BALANCED ROTOR AND MOTOR/IMPELLER, FUNCTIONAL TESTED UNIT IAW CMM 21-26-42. 2L72 4F RTA28NM 20040513001292004051300129WP 2004 5 13 04FDEA001097 120040424A7120AUB70251354104 MOUNT DOUG DC10 DC1010 3022110WP ZONE 400 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 NUMBER 1 PYLON AFT MOUNT BORE HAS CORROSION. REMOVE DAMAGE BY B/H IAW DRAWING AUB7025 AND AUB7034. LOCATED DRILLED AND DEBURRED NEW B/H PART NUMBER AUB7025-13 PO 440915.2 IAW DRAWING AUB7025 AND AUB7034. INSTALLED B/H PART NUMBER AUB7025-13 IAW DRAWING AUB7025 AND AUB7034. 2L73 4F A22WE 20040513001332004051300133NM 2004 5 13 04FDEA001081 120040424A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. 2L73 4F RTA22WE 20040514000032004051400003NM 2004 5 14 04FDEA001106 120040428A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE BARREL NUT HOLE 2B MATING SURFACE CORRODED. 2L73 4F RTA22WE 20040514000052004051400005NM 2004 5 14 04FDEA001087 120040424A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO, STA 1791 LT LONGERON 41 FOUND CRACKED. 2L73 4F RTA22WE 20040514000142004051400014NM 2004 5 14 04FDEA001029 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. 2L73 4F RTA22WE 20040514000182004051400018NM 2004 5 14 CALA0400472 120040505A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND AFT GALLEY FLOOR TRACK CORRODED AT STA 947.5. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52 AND ECRA 5321-01189. 2L72 4F RTA16WE 20040514000232004051400023NM 2004 5 14 CALA0400477 120040507A532069407653 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND FORWARD GALLEY FLOOR SUPPORT CORRODED BETWEEN STA 312 AND 344 BELOW L-1 DOOR. REPAIRED IAW ECRA 5321-01186. 2L72 4F RTA16WE 20040514000442004051400044EA 2004 5 14 ASOA04278 120040411A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGNECY LIGHT DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11901EV6043 2132 7616 FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040514000512004051400051EU 2004 5 14 USAA040074 120040330A5310D5347209001100 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND BEAM CORRODED 1.8 INCHES BY 1.4 INCHES BY .060 INCH AREA, FRAME 64, -Y1270, -Z240. REMOVED AND REPLACED BEAM. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040514000532004051400053EU 2004 5 14 USAA040076 120040330A5320D5348015800400 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND PLATE ASSEMBLY CORRODED 1.2 INCHES BY .8 INCHES BY .020 INCH AREA, FRAME 68, Y1502, -Z240. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 51-74-00, 51-42-11, 53-41-49. CORROSION LEVEL 2, TASK NR JA-160-53500. (M) 2L72 4F RTA28NM 20040514000552004051400055EU 2004 5 14 USAA040072 120040329A5320D53480042207 SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND SCUFF PLATE SUPPORT CORRODED .57 INCH DEEP BY .70 INCH WIDE BY 3 INCHES LONG, FS 68, Z=-240, Y=-1420. REMOVED AND REPLACED SCUFF PLATE SUPPORT PER SRM 51-74-00 AND 53-41-69. (M) 2L72 4F RTA28NM 20040514000572004051400057EA 2004 5 14 ASOA04275 120040409A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11850AS 7355 FLT 9768 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 11 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW ELEVEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040514000602004051400060EA 2004 5 14 A6WA200440040 120040410A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31427ZW 7685 FOUND RIGHT FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. PERFORMED A MAJOR REPAIR TO RIGHT FS 621 UNDER FLOOR SUPPORT ANGLE BY REMOVING DAMAGE AND INSTALLING REPAIR ANGLES IAW BOMBARDIER INC REO 601RR-53-61-117 REV B. (M) 2L72 4F RTA21EA 20040514000662004051400066 2004 5 14 KBM2004F00038 420040219A34245070020910 INDICATOR SNIAS 350 AS350BA 8680817EU TURN AND BANK INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TURN AND BANK INDICATOR, INOPERATIVE. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000722004051400072SO 2004 5 14 PNR2004F00000 120040412A532007A19474 ATTACH BRACKET PIPER PA28 PA28180 7102808SO LYC O360 O360A3A 41514EA ALTERNATOR CRACKED D PNRGO OTHER O OTHER NRNOT REPORTED 1 NM099265J360 283341 L2733736A U SHAPED ALTERNATOR TO ENGINE ATTACH BRACKET FOUND CRACKED. CRACK WAS TANGENTIAL TO THE REAR BOLT HOLE IN A MOSTLY LATERAL DIRECTION. IF CRACK HAD CONTINUED, IT WOULD HAVE EVENTUALLY CRACKED ALL THE WAS ACROSS BRACKET, BEHIND THE REAR BOLT HOLE, ALLOWING THE REAR SIDE OF THE ALTERNATOR TO BE UNSUPPORTED. PROBABLE CAUSE WAS AN UNBALANCED ARMATURE IN THE ALTERNATOR; PN 3656624. CAREFUL ANNUAL/100 HOUR INSPECTIONS OF THIS PART ARE RECOMMENDED TO DETECT THIS TYPE OF PROBLEM BEFORE IT DAMAGES OTHER PARTS. 1L71 3O3 O 2A13 E286 20040514000742004051400074CE 2004 5 14 E812004F00006 120040415A30972052111 CONNECTOR CESSNA500 S550 2076607CE ANTI ICE SYS LOOSE B E81RO OTHER O OTHER NRNOT REPORTED 1 GL0322HP 10214 S5500103 TROUBLESHOT INTERMITTENT ENGINE ANTI-ICING ANNUNCIATOR FAULT COMPLAINTS IAW MM AND TECH SUPPORT. FOUND (5) WORN/LOOSE PINS IN LT SIDEWALL AREA CONNECTOR P1289. REPLACED PINS AND REINSTALLED CONNECTOR. TKS/ENGINE ANTI-ICE SYSTEMS OPERATIONAL CHECKS, OK. SUSPECT RELATIVELY HIGH AC TT AND MAINT OPERATIONS IN AREA A POSSIBLE CASUAL FACTOR. 1L72 4F RTA22CE 20040514000762004051400076CE 2004 5 14 HYTA2004006 120040423A5313261310531 LONGERON CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA FUSELAGE CRACKED E HYTAO OTHER O OTHER NRNOT REPORTED 1 AL014365U13890 208B0253 LT LONGERON 261310531 AND RT LONGERON 261310528 WERE FOUND CRACKED AT THE LOWER AFTER CORNERS OF THE CUT-OUTS FOR THE CONTROL COLUMN TORQUE TUBE. THESE CUT-OUTS ARE LOCATED JUST FORWARD OF THE NOSE GEAR SPRING SUPPORT FITTINGS 26430633. RT LONGERON HAS ONE CRACK .3750 INCH LONG AND A SECOND CRACK .7500 INCH LONG EXTENDING DOWN AND AFT TO THE NEAREST RIVET. LT LONGERON HAS ONE CRACK .7500 INCH LONG EXTENDING DOWN AND AFT TO THE NEAREST RIVET. PROBABLE CAUSE IS LOADS IMPOSED BY THE NOSE GEAR SPRING SUPPORTS AT A POINT WHERE THE LONGERON WEB HAS BEEN MOSTLY REMOVED TO CLEAR THE CONTROL COLUMN TORQUE TUBE. THIS DAMAGE CAN BE REPAIRED WITH A RIVETED DOUBLER OF HEAVIER MATERIAL. 1H71 3T3 T A37CE E2NE 20040514000782004051400078SO 2004 5 14 BNG2004F00001 120040415A53206241102 CHANNEL PIPER PA28 PA28R200 7102811SO LYC O360 IO360A1A 41514EA FUSELAGE CRACKED B BNGRO OTHER O OTHER NRNOT REPORTED 1 GL19406974133 28R7435113 REAR CARRY THROUGH SPAR FRAME ASSY STA 128.237 CRACKED LT SIDE REAR WING ATTACH FITTING AREA. CHANNEL PN 62411-02 CRACKED COMPLETELY EXCEPT LAST .2500 INCH OF TOP FLANGE. AREA PARTIALLY COVERED BY ELECTRICAL TERMINAL STRIP AND COVER ASSY. 1L71 3O3 O 2A13 1E10 20040514000822004051400082EU 2004 5 14 KBM2004F00031 120040330A6730123668P BEARING SNIAS 350 AS350B2 8680813EU ROD END WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P LOWER ROD END BEARING ON RT SERVO WORN. REMOVED AND REPLACED. 1G71 3U H9EU 20040514000832004051400083EU 2004 5 14 KBM2004F00034 120040218A28406475100302 PROBE SNIAS 350 AS350B1 8680811EU FUEL SYSTEM STICKS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 FUEL PROBE INTERMITTENTLY STICKS BETWEEN APPROX. 25-35 PERCENT INDICATED. REMOVED AND REPLACED. 1G71 3U H9EU 20040514000842004051400084NE 2004 5 14 GW12004F00000 220040308A732049664002 CONTROL LEVER PIPER PA31T PA31T1 7103126SO PWA PT6 PT6A60A 52043NE FCU CRACKED B GW1RO OTHER O OTHER NRNOT REPORTED 1 EA03888AH4270 31T7904038 PCE10099 DURING RT ENGINE FUEL CONTROL UNIT (FCU) REPLACEMENT IT WAS DISCOVERED THE START/STOP CONTROL LEVER WAS FRACTURED AT THE FCU MOUNTING HOLE. THE BRACKET PN 49664002 WAS REPLACED. THE LT ENGINE BRACKET WAS REMOVED AND NDT INSPECTED AND REINSTALLED (NO DEFECTS NOTED). THIS IS THE SECOND OCCURRENCE OF THIS FRACTURE AT THIS REPAIR STATION SINCE JAN 15, 2004. MFG CONSIDER INSTALLING A SUPPORT GUSSET TO THE AFT AND/OR FWD SIDE OF THE BRACKET TO INCREASE FATIGUE LIFE. THE GUSSET WILL NOT INTERFERE WITH CONTROL CLEARANCE OR RIGGING. 1L72 3T4 T A8EA E4EA 20040514000862004051400086EU 2004 5 14 KBM2004F00024 120040304A6730123668P BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ROD END WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 LT LAT SERVO UPPER AND LOWER ROD END BALL, WORN. REMOVED AND REPLACED 1G71 3U3 U H9EU E19EU 20040514000892004051400089EU 2004 5 14 KBM2004F00030 120040321A6720704A34130184 CONTROL CABLE SNIAS 350 AS350BA 8680817EU TAIL ROTOR STIFF E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 TAIL ROTOR PEDALS STIFF WHEN THEY ARE AROUND THE (CENTER) POSITION. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000912004051400091EU 2004 5 14 KBM2004F00036 120040301A6420355A09103601 CASE SNIAS 350 AS350BA 8680817EU TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH981 2337 TAIL ROTOR HALF SHELLS WORN AND TORN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000932004051400093EU 2004 5 14 KBM2004F00032 120040427A21210500Y46 MOTOR SNIAS 350 AS350BA 8680817EU AIR CON BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 AIR CONDITIONER, 25 AMP CIRCUIT BREAKER FREQUENTLY POPS OFF, WILL STAY RESET 10-15 MINUTES. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000972004051400097EU 2004 5 14 KBM2004F00039 120040321A7931350A67400103AA INDICATOR SNIAS 350 AS350BA 8680817EU ENGINE OIL FLUCTUATES E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19230SH7565 2337 ENGINE OIL PRESSURE FLUCTUATES. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000982004051400098CE 2004 5 14 FCPR200400014 120040430A528005213115 FAIRING CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE LT MLG MISSING B FCPRO OTHER O OTHER NRNOT REPORTED 1 NM09591DK515 5600591 LT MAIN LANDING GEAR FAIRING DEPARTED AIRCRAFT IN FLIGHT DUE TO FAILURE OF 1 AN525-10R18 FASTENER THAT SECURES UPPER PART OF DOOR TO TRUNNION. THE HEAD OF THE FASTENER IS MISSING. PHILLIPS HEAD DESIGN SEEMS TO HAVE WEAKENED THE FASTENER. RECOMMEND A STRONGER FASTENER FOR THIS TENSION LOAD. 2L72 4F4 FRTA22CE E00053EN 20040514000992004051400099CE 2004 5 14 MW82004F00000 120040407A712071503 MOUNT BBAVIA8 8KCAB 2110612CE LYC O360 AEIO360* EA ENGINE CHAFED B MW8RO OTHER O OTHER NRNOT REPORTED 1 SO01912MA5 9482004 DURING A VISUAL INSPECTION OF THE NEW AC, ENGINE MOUNT WAS NOTED HAVING AN EXCESSIVE CHAFFING CAUSED BY A TINNERMAN NUT USED FOR WINTER BAFFLE ON IB SIDE OF OIL COOLER. SEVERAL OTHER AC HAVE BEEN NOTED WITH TINNERMAN NUTS ON THE OIL COOLERS BUT NO DAMAGE NOTED YET. INSP OF ENGINE MOUNT SHOULD BE DOEN AS SOON AS POSSIBLE AND IF NO DAMAGE TO THE ENGINE MOUNT IS NOTED, THE TINNERMAN NUT SHOULD BE REMOVED AND BOLT AND NUT SHOULD BE INSTALLED WHEN THE WINTER BAFFLE IS NEEDED. 1H71 3O3 O A21CE 1E10 20040514001022004051400102EU 2004 5 14 UO22004F00005 120040426A3260C2424500601 UPLOCK AMD FALC50FALCON900 2700160EU GARRTTTFE731TFE731* 01518WP NLG UNSERVICEABLE B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19900VL6449 60 UPLOCK BROKEN, INTERNAL, WOULD NOT ALLOW THE GEAR TO UPLOCK. 2L73 4F4 FRTA46EU E6WE 20040514001032004051400103NM 2004 5 14 HNAA0400050 120040511A531185320318 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 FRAME AT X 220 CORRODED AT STR 28S. REMOVED AND REPLACED FRAME 220 IAW EO 8-53-04-0316. 2H72 4T RTA13NM 20040514001052004051400105NM 2004 5 14 F3LA200400062 120040425A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD HOLE AT STA 986, LBL 30, FLOORBEAM UPPER CHORD. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG. 101, DETAIL VII. REPLACED UPPER CHORD OF FLOORBEAM FROM SKIN TO SKIN IAW EA B3-53R-10397, SRM 51-40-02, 51-40-05, 51-40-08 AND SOPM 20-41-02. 2L72 4F RTA16WE 20040514001062004051400106NM 2004 5 14 QXEA200400321 120040510A5720 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - RT WING FUEL ACCESS PANEL 622AT HAS BROKEN NUTPLATE AT FORWARD IB CORNER. REPAIRED IAW DHC-8-400 SRM 51-42-05 AND SRM 51-23-00. 2H72 4T RTA13NM 20040514001072004051400107NM 2004 5 14 QXEA200400318 120040510A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - PITTING ON LT IB SEAT TRACK BOTTOM CENTER FROM STATION X193.000 TO STATION X171.000. REPAIRED IAW HORIZON AIR EA 6-53-346. 2H72 4T RTA13NM 20040514001112004051400111SO 2004 5 14 C2XA04SH281 120040513A532014522460013 BUTTSTRAP EMB 145 EMB145 3260210SO FUSLEAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040514001182004051400118EU 2004 5 14 KBM2004F00041 120040304A80120174078030 DRAIN VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE STARTER LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV1311 3296 START DRAIN VALVE, INTERNAL LEAKING. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040514001202004051400120EU 2004 5 14 KBM2004F00043 120040207A6720350A21136324 BRACKET SNIAS 350 AS350B2 8680813EU T/R BELLCRANK CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 RT SIDE TAIL ROTOR PEDAL BELLCRANK BRACKET LOCATED UNDERNEATH CABIN FLOOR HAS CRACKS. REMOVED AND REPLACED. 1G71 3U H9EU 20040514001232004051400123NM 2004 5 14 ASMF200405013 120040508A3110 PITOT TUBE DOUG MD80 MD83 3023681NM PITOT STATIC FOD W ASMFD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW23945AS 49643 AIRCRAFT RETURNED OF FLIGHT, FLIGHT INSTRUMENTS WITH DAMAGE. DURING MAINTENANCE REVISION A FOD WAS DETECTED ON RIGHT PITOT TUBE AS CONSEQUENCE OF BIRD STRIKE. PITOT TUBE WAS CLEANED AND BRAKES WERE COOLED IAW MM 31-00-01. 2L72 4F RT 20040517000022004051700002EA 2004 5 17 SWIA200413285 120040503A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FS 484 LT INTERCOSTAL OB FLANGE LBL36 CRACKED. (FOUND DURING C-CHECK INSPECTION). INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. A, RII 53-401. 2L72 4F RTA21EA 20040517000052004051700005EU 2004 5 17 USAA040083 120040330A5315D5347218920200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH BY .050 INCH AREA, FRAME 68-69, -Y1210, -Z2240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040517000072004051700007EU 2004 5 17 USAA040080 120040329A5315D5347219020300 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOORBEAM CORRODED 1 INCH IN DIAMETER BY .030 INCH DEEP, LAV E MOUNTHOLE, -Y720, 10 INCHES AFT OF FRAME 64 ON BEAM ASSEMBLY. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040517000082004051700008EU 2004 5 17 USAA040087 120040331A5315D53474209001000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .048D AREA, FRAME 68 Y 1292 -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 51-74-00, 53-00-14 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040517000092004051700009EU 2004 5 17 USAA040088 120040331A5315D53471172220290 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH BY .02 AND .03, TWO AREAS, FS 66-68, Y1292, -Z240. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00 AND 51-42-11. (M) 2L72 4F RTA28NM 20040517000112004051700011EU 2004 5 17 USAA040093 120040401A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOOR PANEL CORRODED 5 INCHES LONG BY 3 INCHES WIDE BY .02 INCH DEEP AREA, MAIN CABIN 261FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M) 2L72 4F RTA28NM 20040517000122004051700012EU 2004 5 17 USAA040090 120040331A5315D5347218820400 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .039 INCH DEEP, FRAME 68, Y1162, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040517000132004051700013EU 2004 5 17 USAA040091 120040331A5321D5361060500100 FLOOR PANEL AIRBUSA319 A319112 3930323EU MAIN CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOOR PANEL CORRODED 1 INCH WIDE BY .015 DEEP ENTIRE LENGTH, MAIN CABIN, PNI 222FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20040517000152004051700015EU 2004 5 17 USAA040082 120040326A5320D5347209300000 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND LONGITUDINAL FLOOR SUPPORT CORRODED 2.3 INCHES LONG BY 1.7 INCHES WIDE BY .070 INCH DEEP AREA, BETWEEN FRAME 66/70, -Y 800MM. REPLACED LONGITUDINAL FLOOR SUPPORT PER SRM 51-42-11, SRM 53-00-14 AND SRM 51-74-00. CORRODED LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040517000162004051700016EU 2004 5 17 USAA040086 120040331A5320D5361042100000 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW 0929 BFM - FOUND PLATE ASSEMBLY CORRODED 5 INCHES BY 1.6 INCHES BY .020 INCH AREA, FRAME 20, -Z240, -Y765. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 53-11-14 AND 51-72-11. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040517000172004051700017EU 2004 5 17 USAA040089 120040330A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND SILL CORRODED .110 INCH BY .190 INCH BY .070 INCH DEEP, FRAME 68, Y1420, -Z240. REMOVED AND REPLACED SILL PER SRM 51-41-14. CORRODED LEVEL 2, TASK NR JA 260-53500. (M) 2L72 4F RTA28NM 20040517000182004051700018WP 2004 5 17 GTIA040281 120040325A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CORROSION ON SEAT TRACK LEFT INBOARD AT FS 200 PAX CABIN. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK AND SPLICE. INSTALLED NEW SEAT TRACK AND SPLICE. (M) 2L72 4F A6WE 20040517000202004051700020WP 2004 5 17 GTIA040291 120040324A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND FLIGHT CONTROL ACCESS PANEL BETWEEN F/O'S, CAPTAINS STATION 148 TO STATION 160 HAS CRACKED/DAMAGED ON EDGE, SOFT/MUSHEY. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040517000242004051700024WP 2004 5 17 GTIA040285 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN STATION 200 RBL 9 - RBL 44 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20040517000252004051700025WP 2004 5 17 GTIA040286 120040325A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSLEAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND DELAMINATION AND EDGE DAMAGED, CABIN FLOORBOARD FS 1309 LEFT OUTBOARD AFT SECTION. FABRICATED NEW FLOORBOARD. (M) 2L72 4F A6WE 20040517000262004051700026WP 2004 5 17 GTIA040287 120040316A5310 SHEAR TIE DOUG DC9 DC982 3022082WP AFT CARGO CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND AFT CARGO SHEAR TIE FROM LONGERON 26R-26L, CORRODED AND TOOL MARKS. FABRICATED NEW SHEAR TIE. (M) 2L72 4F A6WE 20040517000272004051700027EA 2004 5 17 A6WA200440050 120040419A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AW 7878 THE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. PERFORMED A MAJOR REPAIR TO RIGHT SIDE OF FUSELAGE SKIN AT FS 298.5 BETWEEN STRINGERS 13R AND 14R USING STANDARD SHOP PRACTICES. FABRICATED STIFFENER FROM 2024-T3 .063 INCH TO EXTEND BETWEEN TWO STRINGERS UNDER THE DENTED AREA IAW BRAS EO 601R-53-4835. (M) 2L72 4F RTA21EA 20040517000312004051700031EU 2004 5 17 SIMA200410107 120040330A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 ABI - DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. RECONTOURED DENTS AND PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA. NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS6852. (M) 2L72 4T RTA52EU 20040517000322004051700032WP 2004 5 17 GTIA040277 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN STATION 148-160 RBL 31 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20040517000342004051700034WP 2004 5 17 GTIA040279 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN STATION 198 LBL 16 - LBL 42 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20040517000372004051700037 2004 5 17 GTIA040273 420040409A2565 COVER DOUG DC9 DC982 3022082WP L1 DOOR SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FLT 223 - ORD - FOUND L1 SLIDE PACK AND COVER CAME LOOSE FROM ENTRY DOOR. NO DAMAGE NOTED, REINSTALLED L1 SLIDE PACK AND COVER. (M) 2L72 4F A6WE 20040517000382004051700038WP 2004 5 17 GTIA040274 120040410A3260833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23808NK 49504 FLL - FLT 1507 - NOSE GEAR UNSAFE LIGHT CAME ON IN CRUISE. COMPLIED WITH QRH, ACARS TO MAINTENANCE, LIGHT WENT OUT IN TURB. REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR. OPS CHECK OK ON GROUND. (M) 2L72 4F RTA6WE 20040517000402004051700040WP 2004 5 17 GTIA040276 120040410A3350 LIGHT DOUG DC9 DC982 3022082WP AFT GALLEY LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 ORD - FLT 1504 - AFT GALLEY AISLE EXIT LIGHTING TRACK CAME UP. RE-ATTACHED AFT GALLEY LUMINESCENT EXIT STRIP. (M) 2L72 4F A6WE 20040517000412004051700041EA 2004 5 17 A6WA200440048 120040418A5610NP1363216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A A6WAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31430AW3053 7719 FOUND RIGHT WINDSHIELD CRACKED RIGHT AFTER TAKEOFF. WINDSHEAR ENCOUNTERED DURING DEPARTURE ALSO, REMOVED AND REPLACED FIRST OFFICERS WINDSHIELD IAW AMM 56-11-01. (M) 2L72 4F RTA21EA 20040517000442004051700044WP 2004 5 17 GTIA040282 120040328A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND WEB AT FS 160 RBL 35 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED DOUBLER, FILLER. INSTALLED FABRICATED PARTS. (M) 2L72 4F A6WE 20040517000472004051700047SO 2004 5 17 JIKA200400005 120040422A7603555815 THROTTLE CABLE PIPER PA32 PA32R300 7103213SO ENGINE BROKEN E JIKAO OTHER O OTHER TXTAXI/GRND HDL 1 WP013609Q9680 53 32R7780319 AFTER LANDING PILOT ATTEMPTED TO ACCELERATE ENGINE TO TAXI TO THE RAMP AREA. THERE WAS NO RESPONSE FROM THE THROTTLE LEVER INPUTS, THE ENGINE WOULD NOT ACCELERATE ABOVE IDLE RPM. PILOT SHUT DOWN ENGINE AND THE AIRCRAFT WAS TOWED TO THE RAMP AREA. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE THROTTLE CABLE BROKEN APPROXIMATELY 3 INCHES FROM THE HOUSING END ON THE ENGINE FUEL INJECTION SERVO THROTTLE ATTACHMENT END. 1L71 3O A3SO 20040517000482004051700048NM 2004 5 17 PCAA0405204 120040513A2797 WIRE DHAV DHC8 DHC8102 2809003NM ELEVATOR TRIM BROKEN A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13814EX 318 FLIGHT NR 3828 LGA REPORTED THEIR STANDBY ELEVATOR TRIM AS BEING INOPERATIVE. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE FOUND THE GROUND AT TERMINAL BLOCK 2211 GS1 BROKEN. GROUND WAS REPAIRED AND ALL SYSTEMS OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040517000502004051700050EU 2004 5 17 00138 120040507A5270 SWITCH AMD FALC20FALCONE 2720305EU CARGO DOOR OUT OF ADJUST E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05285TW 285 PILOT REPORTED MAIN CARGO DOOR LIGHT CAME ON AND CABIN PRESS DUMPED, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. MAINTENANCE ADJUSTED SWITCH AND OPS CHECKED AIRCRAFT AND SYSTEM, RETURNED AIRCRAFT TO SERVICE. (CLOSED) 2L72 4F A7EU 20040517000512004051700051SO 2004 5 17 C2XA04SH282 120040513A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV-DURING C CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040517000522004051700052NM 2004 5 17 PCAA0405205 120040510A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM NR 2 INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13844EX167261407 339 FLIGHT NR 3937 REPORTED THEIR NR 2 SMOKE DETECTOR AS BEING INOPERATIVE DURING ROUTINE TEST. MAINTENANCE REMOVED AND REPLACED UNIT AND OPERATIONAL TEST SYSTEM, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040517000552004051700055EA 2004 5 17 QXEA200400314 120040509A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX5865 10010 PDX - THE AFT PRESSURE BULKHEAD HAS A CRACK APPROXIMATELY .3750 OF AN INCH LONG AT STATION 1098.20, ADJACENT TO THE LT HYDRAULING FITTING CUT-OUT. MAINTENANCE REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 670-53-61-034. 2L72 4F RTA21EA 20040517000642004051700064EA 2004 5 17 SWIA200413287 120040427A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 MAIN FUSELAGE IB AND OB BEAM CLIPS CRACKED FS280.00 RBL 9.0. (FOUND DURING C-CHECK INSPECTION). REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-40-11, 51-23-00, 51-42-21 AND RII53-401. 2L72 4F RTA21EA 20040517000662004051700066EA 2004 5 17 SWIA200413289 120040427A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 LBL 42.0. (FOUND DURING C-CHECK INSPECTION). REPAIRED CARGO PIT, FLOOR SUPPORT ANGLE AT FS 621.00 IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401. 2L72 4F RTA21EA 20040517000712004051700071 2004 5 17 371PA0040 420040327A2220 SENSOR BOEING737 737306 13844BGNM MACH TRIM INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 MACH TRIM INOPERATIVE. ADJUSTED NEUTRAL SHIFT SENSOR IAW MM 22-11-14. OPS CHECKS GOOD. 2L72 4F RTA16NE 20040517000722004051700072EU 2004 5 17 2004UALA00420 120040502A5270 SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR OBSTRUCTED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29427UA 512 RETURN TO FIELD DUE TO CARGO DOOR LIGHT INDICATION. CARGO NET WAS POSITIONED WHERE IT INTERFERED WITH DOOR PROXIMITY SENSOR. REPOSITIONED CARGO NET. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040517000732004051700073NM 2004 5 17 2004UALA00421 120040501A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOORBEAM WEB CRACKED AT UPPER SECTION RBL 13 WL 200. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED (T) ANGLE DOUBLER. 2L72 4F4 FRTA1NM E24NE 20040517000742004051700074 2004 5 17 2004UALA00422 420040501A2565 SQUIB BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE WING SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29669UA 30025 RT OFF WING SLIDE SQUIB TEST NR 1 FAILS. REPLACED RIGHT OFF WING SLIDE BATTERY CHARGER AND BATTERY PACK. LATER REPLACEMENT OF RELAY P/N XD4L015 SUGGESTS THAT INTERMITTENT RELAY PROBLEM MAY HAVE CONTRIBUTED TO THIS EVENT AS WELL. 2L72 4F4 FRTA1NM E24NE 20040517000752004051700075NM 2004 5 17 2004UALA00423 120040502A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT RBL 12 INCHES, T-ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED PULLEY SUPPORT ANGLE. 2L72 4F4 FRTA1NM E24NE 20040517000772004051700077NM 2004 5 17 2004UALA00425 120040502A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT RBL 16 INCHES IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA1NM E24NE 20040517000792004051700079NM 2004 5 17 AWXA200400493 120040504A53126517582 VERTICAL BEAM BOEING737 7373Y0 1384671NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3750 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB ON AFT SIDE RUNNING FROM BLANKET HOLE AT RBL 17.1, WL 184. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 184; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B737-300 SRM 53-70-13, FIG. 1. 2L72 4F RTA16WE 20040517000812004051700081NM 2004 5 17 AWXA200400495 120040428A5340146N874817 FITTING BOEING757 757225 1384959NM INTERCOSTAL CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 LCQ - MAJOR REPAIR - DURING C-07 CHECK A 2 INCH CRACK WAS FOUND IN AFT CABIN INTERCOSTAL FITTING AT BS 1681.8, BETWEEN STR 12 LT AND STR 13 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL FITTING AT BS 1681.8, BETWEEN STR 12 LT AND STR 13 LT; FABRICATED A NEW REPLACEMENT FITTING IAW DWG 146N8748; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 1. 2L72 4F RTA2NM 20040517000832004051700083NM 2004 5 17 AWXA200400497 120040427A5330654577627 SKIN BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 LCQ - MAJOR REPAIR, DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER FUSELAGE SKIN AT ANTENNA MOUNT BS 793, BL (0). MAINTENANCE REMOVED DAMAGED FUSELAGE SKIN AT ANTENNA MOUNT BS 793, BL (0); FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW SRM 53-00-01, FIG. 229. 2L72 4F RTA16WE 20040517000852004051700085NM 2004 5 17 AWXA200400499 120040409A533065457788 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR, DURING C-17 CHECK A .2500 CRACK WAS FOUND AT FASTENER HOLE IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF R-2 DOOR CUTOUT BS 981.8 TO BS 984.8, WL 198. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED AN INNER, MIDDLE, AND OUTER DOUBLERS; INSTALLED FREEZE PLUG IN STOP DRILL HOLE, INSTALLED DOUBLERS IAW SRM 53-60-01, FIG. 203, AND E.R. 03-5300-04128-HFIA. 2L72 4F RTA16WE 20040517000862004051700086NM 2004 5 17 QXEA200400279 120040420A2720682015 SWITCH BOMBDRDHC8 DHC8401 1390041NM RUDDER TRIM FAILED A QXEAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM09402QX6781 4032 GEG - CLIMBING OUT OF GEG, THE RUDDER TRIM STARTED MOVING TO THE LT WITHOUT PILOT INPUT. MAINTENANCE INSPECTED THE AIRCRAFT AND SYSTEMS AND REPLACED THE PEDESTAL RUDDER TRIM SWITCH. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040419000622004041900062CE 2004 4 19 2004F00100 120040119A2497MS2774317 MASTER RELAY LEAR 60 60LEAR 5170707CE RIGHT INOPERATIVE A DELAO OTHER O OTHER NRNOT REPORTED 1 CE03188TG 078 MULTIFUNCTION DISPLAY WAS INOPERATIVE. UPON FURTHER INVESTIGATION SEVERAL OTHER SYSTEMS HAD ALSO FAILED. FOUND RIGHT AVIONICS MASTER RELAY K3 TO BE DEFECTIVE. REPLACED RELAY AND OPS CHECKED GOOD. (M) 2L72 4F RTA10CE 20040419000742004041900074EA 2004 4 19 ASOA04099 120040208A5210600912251 CAM ROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11885AS 7521 FLT 4389 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE ADJUSTED AND LUBRICATED THE CAM ROD AT THE UPPER ROLLER ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040419000902004041900090WP 2004 4 19 ASAA0480184 120040310A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND FLOORBOARD IS CORRODED AND DELAMINATED AT FS 843-886. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000942004041900094WP 2004 4 19 ASAA0480180 120040310A534759305661 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419000962004041900096EA 2004 4 19 ASOA04087 120040203A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA OVERWING EXIT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11901EV 7616 FLT 4219 - DURING A GROUND INSPECTION IN DFW, THE FORWARD TWO EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE FORWARD TWO EXTERIOR OVERWING EMERGENCY EXIT LIGHTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040419001022004041900102WP 2004 4 19 ASAA0480086 120040221A53219936548501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001082004041900108WP 2004 4 19 ASAA0480163 120040307A533059114017 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV12 CHECK, FOUND NLG DOOR AFT HINGE CUTOUT IS CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-05. (M) 2L72 4F RTA6WE 20040419001122004041900112WP 2004 4 19 ASAA0480136 120040229A5730ARB0975519 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, - FOUND LEFT WING FUEL TANK ACCESS PANEL NR 1361 IS CORRODED ON MATING FLANGE. REPLACED PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040419001212004041900121NM 2004 4 19 DHL2004750038 120040302A5711 FRAME BOEING727 7272M7 138407SNM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 2ND FROM SPAR HAS UPPER END CRACKED. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024 T3 .032 PO 900534 DIM 3.75 X 2.5 INCH REPAIR ANGLE FROM 7075 T3 040 PO 900226 DIM 7 X 3.5 INCH IAW B727 SRM 51-40-3 FIG 1 52-20-2 FIG 1. PART TREATED & PRIMED IAW B727 SRM 51-10-2. PART INSTALLED IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040419001252004041900125NM 2004 4 19 DHL2004750019 120040225A5754 ROD END BOEING727 7272M7 138407SNM NR 2 SLAT ACT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME CRACKED IN FWD LOWER RADIUS. REMOVED AND REPLACED AT NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME BY FWD LOWER 2 EA RIB SUPPORT PO 413627 P/N 65-17310-4 AND PIL 413644 P/N 65-17310-3 IAW B727 SRM 51-30-2. ACCOMPLISHED SLATS OPS CHECK, FOUND OK IAW B727 MM 27-81-0. 2L73 4F A3WE 20040419001262004041900126EA 2004 4 19 QXEA200400261 120040411A5230 DOOR CNDAIRCL600 CL6002C10 1390015EA CARGO UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09602QX 10010 TUS - FLIGHT 4218 - CREW RETURNED TO FIELD WHEN AFTER TAKEOFF RECEIVED AN AFT CARGO DOOR WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE DOOR NOT SECURE. THE DOOR WAS SECURED AND OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHEKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040419001362004041900136EA 2004 4 19 COMA0460223 120040326A2797601R575101 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01967CA 7134 FLIGHT 5020 FLAPS FAILED CAUTION MESSAGE. REPLACED PDU WIRE HARNESS. 2L72 4F RTA21EA 20040419001412004041900141NM 2004 4 19 DHL2004750023 120040225A5320 FLOOR SUPPORT BOEING727 7272M7 138407SNM FUSELAGE BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, FWD CARGO FLOOR SUPPORT IS BENT BS 600 RBL 3. CUT OUT DAMAGED AREA SIZE 1 X 4 INCH ON FWD CARGO FLOOR SUPPORT BS 600 RBL 3 IAW B727 SRM 51-10-1. FABRICATED FILLER FROM 2024T3 .063 SIZE 1 X 4 INCH PO 900606 AND ANGLE FROM BAC 1506-1080 SIZE 21.75 X 2 INCH PO 3425287 IAW B727 SRM 51-40-4 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-4 FIG 1. 2L73 4F A3WE 20040419001422004041900142NM 2004 4 19 DHL2004750020 120040229A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LT FUSELAGE HAS A DENT BS 1070 BELOW STR 17L. REMOVED DAMAGE CUTOUT IS A 1.0 INCH CIRCLE IAW B727 SRM 53-30-3 FIG 1. FABRICATED DOUBLER FROM 2024T3 .090 PO 900103. DOUBLER IS 10.5 X 13.5 INCH IAW B727 SRM 53-30-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 53-30-3 FIG 1. 2L73 4F A3WE 20040419001472004041900147NM 2004 4 19 SWAA041053 120040413A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 360 TO BS 380, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040419001632004041900163NM 2004 4 19 DHL2004750015 120040229A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, LEFT FUSELAGE HAS A DENT BS 431 ABOVE STR 20L. CUT OUT DAMAGED AREA .75 INCH DIA AND FABBED FILLER, FROM 2024-T3 .063, PO 900606, DIA .75 INCH AND DOUBLER FROM 2024-T3, .071, PO 900484 DIA 3.25 INCH IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIG 13. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 13. 2L73 4F A3WE 20040419001672004041900167NM 2004 4 19 SWAA041046 120040412A5312BAC1518 PRESSURE PANEL BOEING737 7373L9 1384470NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C1 CHECK, FOUND FORWARD TEE STIFFENER WEB AT NLG W/W CEILING CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040419001722004041900172NE 2004 4 19 SWAA041010 220040409A7200332A1000XXX ENGINE BOEING737 7373K2 13844BANM GE CFM56 CFM563B1 13802NE LEFT FAULTY A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW29340LV 23738 721116 AIR TURNBACK, DECLARED EMERGENCY, ON TAKEOFF NR 1 ENGINE EGT FELL TO 350 DEGREES, AIRBORNE AT 800 FEET NR 1 ENGINE VIBRATION METER MAXED OUT AT 5 UNITS WITH AIRFRAME VIBRATION. NR 1 ENGINE WAS PUT IN IDLE POSITION AND VIBRATION STOPPED, EGT STILL LOW. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2L72 4F4 FRTA16WE E2GL 20040419001732004041900173 2004 4 19 SWAA041011 420040408A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29423WN 29827 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040419001832004041900183EA 2004 4 19 COMA0460257 120040413A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01713CA 7245 FLIGHT 5205 FLAP FAIL CAUTION AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040419001912004041900191NM 2004 4 19 SWAA041022 120040409A32601899 SENSOR BOEING737 7373Q8 1384670NM NLG FAULTY A SWAAK NONE J WARNING INDICATION NRNOT REPORTED 1 SW29672SW 23406 NOSE GEAR UNSAFE LIGHT ILLUMINATED, CYCLED GEAR NO HELP, VISUALLY CHECK NOSE GEAR DOWN AND LOCKED. ON FINAL GOT THREE GREEN LIGHTS FOR A SHORT PERIOD THEN RED NOSE GEAR LIGHT ILLUMINATED. REMOVED AND REPLACED LOGIC CARDS AND PROX SENSOR, PER MM. 2L72 4F RTA16WE 20040419001942004041900194NM 2004 4 19 SWAA041025 120040409A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419001982004041900198NM 2004 4 19 SWAA041028 120040409A53306546881 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 1016, STRINGER 7L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040419002002004041900200 2004 4 19 SWAA041002 420040407A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER SLIDE DID NOT INFLATE. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040419002132004041900213EU 2004 4 19 MALA040318 120040407A2720 CONTROL CABLE BAC 146 AVRO146RJ85A1500097EU RUDDER OUT OF POSITION A MALAO OTHER S AFFECT SYSTEMS NRNOT REPORTED 1 GL15526XJ E2351 CAPTAINS RUDDER PEDALS FEEL RESISTANCE/RUBBING WHEN EXERCISED TO FULL AND BACK. MX FOUND ONE RUDDER CABLE ON OUTSIDE OF HOLD DOWN PIN ON BELL CRANK AREA OF RUDDER CABLE SYSTEM. REPOSITIONED CABLE TO PROPER AREA, NO DAMAGE NOTED TO CABLE OR BELLCRANK, NO OTHER DEFECTS NOTED, CABLE TENSION IS CORRECT. ALL RUDDER TRAVEL MOVEMENT IS GOOD. 2H74 4F RTA49EU 20040420000022004042000002NM 2004 4 20 DHL2004755007 120040317A2120 ODOR BOEING727 727225 1384077NM COCKPIT DETECTED A DHLAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01755DH 21857 SLIGHT OIL ODOR IN COCKPIT DURING APU OPERATION ON GROUND. DEFERRED PER MEL 49-1 DMI 16065 PLACARD INSTALLED. REF DMI 16065 APU INOPERATIVE. CHECKED APU PER 49-00. CHECKED GOOD. RAN BOTH PACKS AT 115 PERCENT FOR 45 MINUTES, NO ODOR NOTED. CHECKED APU FOR LEAKS, NONE NOTED. CLEARED DMI 16065. PLACARD REMOVED. 2L73 4F A3WE 20040420000122004042000012WP 2004 4 20 DHL2004807006 120040407A5270 SWITCH DOUG DC8 DC873F 302199FWP MLG DOOR MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01807DH 45990 DOORS NOT LATCHED LIGHT FLICKER INTERMITTENT IN FLIGHT WITH GEAR RETRACTED. DOOR NOT LATCHED INDICATING LIGHT MAY BE INOPERATIVE PER MEL -B- 32-8 DMI 16255 PLACARD INSTALLED. DMI 16255 DOORS NOT LATCHED LIGHT FLICKERS INTERMITTENT IN FLIGHT WITH GEAR RETRACTED. REMOVED AND REPLACED LEFT GEAR DOOR TARGET SWITCH (DOOR WARNING) IAW DC8 WO 32-1-0, OPS CHECKED NORMAL IAW DC8 M/M 32-30-0. DMI CLEAR. 2L74 4F RT4A25 20040420000182004042000018NM 2004 4 20 2004UALA00310 120040404A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29567UA 26673 EXTERIOR EMERGENCY SLIDE LIGHT INOP AT DOOR 4L. REPLACED LAMP NR 767. 2L72 4F4 FRTA2NM E17NE 20040420000192004042000019NM 2004 4 20 2004UALA00311 120040405A5753 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE TE FLAP DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 LEFT OUTBOARD AFT FLAP ASSY DELAMINATED ALONG MOST INBOARD TRAILING EDGE AND CORNER OF FLAP. MAJOR REPAIR ACCOMPLISHED. REPLACED SKIN, AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040420000282004042000028EU 2004 4 20 2004UALA00321 120040409A5230 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29429UA 539 DAMAGE TO SKIN ON INSIDE OF AFT CARGO DOOR DIRECTLY BEHIND DOOR HANDLE HUB. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED ON DOOR INNER SKIN. 2L72 4F4 FRTA28NM E40NE 20040420000312004042000031NM 2004 4 20 DHL2004748001 120040318A143069396192 BOLT BOEING727 727225 1384077NM FLAP CARRIAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 LEFT-HAND OUTBOARD FLAP, OUTBOARD AFT FLAP CARRIAGE ECCENTRIC BOLT BROKEN AND ECCENTRIC MISSING. REPLACED BOLT AND ECCENTRIC AT LEFT-HAND OUTBOARD AFT TRAILING EDGE FLAP P/N: 69-39608-1 AND P/N: 69-39619-2 IAW B-727 M/M 27-51-11. OPS CHECKED NORMAL ON GROUND. 2L73 4F A3WE 20040420000462004042000046EU 2004 4 20 DHL2004362001 120040401A3242 BRAKE ASSY AIRBUS300 A300B4203 3930306EU NR 8 MALFUNCTIONED A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01362DH 84 BRAKES FEEL LIKE THEY ARE GRABBING ON TAXI. AS A PRECAUTION REMOVED AND REPLACED NR 8 BRAKE ASSEMBLY DUE TO NR 8 TIRE FAILURE, DUE TO SUSPECTING BRAKE WAS DRAGGING M/M 32-42-27. 2L72 4F RTA35EU 20040420000472004042000047NM 2004 4 20 DHL2004750026 120040301A5754 ROD END BOEING727 7272M7 138407SNM SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, NR 7 SLAT AT ACT ROD END HAS INBOARD ATTACH FRAME CRACKED IN LOWER FWD RADIUS. REMOVED CRACKED RIB, LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-3, PO 413646 IAW B727 SRM 51-30-2 FIG 1 & 2. ACCOMPLISHED L/E FLAPS OP'S CHECK FOUND OK IAW B727 MM 27-81-0. 2L73 4F A3WE 20040420000662004042000066NM 2004 4 20 UPS04442044 120040302A5330 SKIN BOEING747 747SR46 1384816NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE: C, REF EO - B747-5310-1093M LT BS 1241 AFT HOLE FOUND A BUSHING IN SKIN. LEFT BS 1241 AFT HOLE SKIN OLD BUSHING REMOVED. HFEC INSPECTED RESULT, NO CRACK FOUND. BUSHING FABRICATED AND INSTALLED PER RS R53-43-35119. BOLT BACB30US12K40 INSTALLED REF: SB747-53-2283 REV 4 FIG 14, EO B747-5310-1093-M AND EO B747-5310-20150-A, UPS-HKG-04-00059H. 2L74 4F RTA20WE 20040420000732004042000073NM 2004 4 20 DHL2004750021 120040229A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING C-CHECK, LT FUSELAGE FRAME HAS A DENT BS 1283 BELOW STR 22L. CUT OUT DAMAGED AREA .75 X .375 INCH LEFT FUSELAGE BS 1287 BETWEEN STR 22L FAB DOUBLER 2024-T3 PO 300606 DIM 6.5 X 12 INCH IAW B272 SRM 57-30-2 FIG 3, 53-30-3 FIG 3. ALODINED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER IAW B727 SRM 57-40-3 FIG 1. 2L73 4F A3WE 20040420000762004042000076EA 2004 4 20 QXEA200400240 120040321A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 PDX - MIDDLE CHIMNEY IS DAMAGED IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED CHIMNEY. 2L72 4F RTA21EA 20040420000882004042000088NM 2004 4 20 04FDEA00929 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP VANE, NR 3 FROM I/B VANE ATTACH FITTING HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75929. LT AND RT OUTBOARD FLAP NR 3 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420000912004042000091NM 2004 4 20 04FDEA00932 120040413A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP VANE, NR 1 FROM I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5750-75927. LEFT AND RIGHT OUTBOARD FLAP NR 1 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040420001072004042000107NM 2004 4 20 04FDEA00941 120040413A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT WING O/B FLAP I/B HINGE PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76664. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420001162004042000116NM 2004 4 20 DHL2004750017 120040225A5754 RIB BOEING727 7272M7 138407SNM L/E SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; NR 7 SLAT INTERIOR RIB O/B OF ACTUATOR ATTACH POINT CRACK INDICATION WS 640 NDT CONFIRMED. REMOVED CRACKED RIBS LOCATED, DRILLED AND INSTALLED NEW RIB P/N 65-17310-4, PO 410362 IAW B727 SRM 51-30-2, FIG 1 & 2. 2L73 4F A3WE 20040420001252004042000125NE 2004 4 20 BAQA094033 220040324A73100319739560 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE LT FUEL INJECTORCLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 32058 UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U3 U H88EU E34NE 20040420001352004042000135NM 2004 4 20 DHL2004750027 120040224A5311 FRAME BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME IS DENTED AT BS 540. CUT OUT DAMAGED AREA SIZE .75 X 1 INCH ON UPPER CABIN RIGHT SIDE BETWEEN STR 16R AND 17R FRAME AT BS 540 IAW B727 SRM 51-10-1, FABRICATED REPAIR ANGLE FROM 7075-T6 .063 SIZE 6 X 4.5 INCH PO 900166 IAW B727 SRM 51-40-3 FIG 1. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2, INSTALLED REPAIR ANGLE IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040420001392004042000139NM 2004 4 20 DHL2004750034 120040229A5330 SKIN BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT FUSELAGE HAS A DENT BS 1166 ABOVE STR 25L. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUT DAMAGED AREA DIM (1.25 X .75 INCH) & FAB DOUBLER FROM 2024 T3 .071 PO 900484 DIM 10.125 X 6.5 INCH IAW B727 SRM 53-30-3 FIG 1 & 53-30-2 FIG 2. DOUBLER & BARE METAL TREATED WITH ALODINE & PRIMER, FAB & INSTALLED REPAIR WASHER IAW B727 SRM 51-10-2 & 51-30-8. INSTALLED DOUBLER AT BS 1166 ABOVE STR 25L IAW B727 SRM 53-30-3 FIG 1. 2L73 4F A3WE 20040420001402004042000140NM 2004 4 20 DHL2004750035 120040229A5330 SKIN BOEING727 7272M7 138407SNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT FUSELAGE HAS A DENT BS 720E BELOW STR 17L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA (1.9375 X 1.875 INCH) AND FABBED DOUBLER FROM2024-T3 100 PO 900484 DIM 12.25 X 8.75 INCH & FILLER FROM 2024-T3 .090 PO 900103 DIM 1.875 X 1.875 INCH IAW 727 SRM 53-30-3 FIG 3. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2. REPAIR PARTS INSTALLED IAW 727 SRM 53-30-3 FIG 3. LEAK CHECK FOUND NO LEAKS IAW B727 MM 21-31-00. 2L73 4F A3WE 20040420001412004042000141NM 2004 4 20 DHL2004750037 120040302A5720 STIFFENER BOEING727 7272M7 138407SNM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01750DH 21951 DURING -C- CHECK, DISCREPANCY AS FOLLOWS; LEFT WING L/E CAVITY WBL 92 INT FRAME INBOARD SIDE UPPER STIFFENER 1ST FWD OF SPAR HAS UPPER END CRACKED. CUT OUT DAMAGE AREA & FABRICATED DOUBLER FROM 2024 T3 .040 PO 900226, 7 X 1.5 X 1.5 INCH, FILLER FROM 2024T3 .032 PO 900534 3.5 X 1 X 1 INCH IAW B727 SRM 51-40-3 FIG 1. TREATED & PRIMED IAW B727 SRM 51-10-2, INSTALLED DOUBLER & FILLER IAW B727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040420001422004042000142EA 2004 4 20 COMA0460226 120040324A339764643 POWER CABLE CNDAIRCL600 CL6002B19 1900309EA CABIN DEFECTIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01494CA 7765 FLIGHT 5822 EMERGENCY FLOOR LIGHTING IS DIM, ROW 5 FORWARD. REPLACED THE POWER STRIP. 2L72 4F RTA21EA 20040420001432004042000143EA 2004 4 20 COMA0460227 120040323A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAILED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01443CA5562 7539 FLIGHT 5232 GEAR DISAGREE WARNING AND HYDRAULIC SYSTEM 3 CAUTION. REPLACED THE SYSTEM 3A ACMP. 2L72 4F RTA21EA 20040420001472004042000147NM 2004 4 20 UPS04242070 120040312A5320 FITTING BOEING727 72730C 1384009NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420. 2L73 4F A3WE 20040420001482004042000148NM 2004 4 20 UPS04242072 120040309A5280 DOOR FRAME BOEING727 72730C 1384009NM TAIL SKID CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61. 2L73 4F A3WE 20040420001502004042000150EU 2004 4 20 BAQA093894 120040323A77970301037070 WIRE HARNESS AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE PYROMETRIC DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 1014 6425 12286 ENGINE, PROBES DAMAGED AT SOLDER JOINT. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H10EU E19EU 20040420001532004042000153EA 2004 4 20 COMA0460230 120040327A3234617501 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01958CA 7111 FLIGHT 5624 GEAR DISAGREE WARNING MLG DID NOT EXTEND. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20040420001582004042000158 2004 4 20 BAQA093967 420040329A3457 LIGHT BOLKMS117 BK117B1 5626012EU GPS INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME301 56111 7235 FACE WILL NOT ILLUMINATE. REPLACED WITH SERVICABLE UNIT. 04/05/2004 1G72 3U H13EU 20040420001622004042000162EU 2004 4 20 DHL2004363003 120040328A3242C200601004 BRAKE ASSY AIRBUS300 A300B4203 3930306EU NR 6 DRAGGING A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01363DH 85 ON TAKEOFF ROLL BRAKES HOT LIGHT ILLUMINATED ON MASTER WARNING PANEL (MWP). REJECTED TAKEOFF, COMPLETED ABNORMAL PROCEDURE. SPEED AT TIME OF RTO =<60 KIAS, A/C WEIGHT = 301,000, OAT = 23 DEGREES C, MAXIMUM BRAKE TEMPERATURE NR 6 260 DEGREES. CREW COMPLIED WITH REJECTED TAKEOFF (RTO) CRITERIA. BRAKE TEMPERATURES BELOW RTO CRITERIA OF 450 DEGREES PER A/B M/M 05-51-16. NR 6 MAIN BRAKE DRAGGING WITH PRESSURE SUPPLIED. DOES NOT DRAG WITHOUT PRESSURE. NR 6 MAIN BRAKE DEACTIVATED PER A300 MEL 32-42-09-01 CAT -C- AS DMI 16176. PLACARD INSTALLED, NR 6 MAIN BRAKE TRANSFERRED TO DMI LOG. REMOVED AND REPLACED NR 6 BRAKE PER 32-42-27. LEAK CHECKED OK. OPS CHECKED GOOD. 2L72 4F RTA35EU 20040420001632004042000163NM 2004 4 20 UPS04242075 120040308A2761 SUPPORT BOEING727 72730C 1384009NM NR 12 SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 INSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01. 2L73 4F A3WE 20040420001682004042000168EA 2004 4 20 COMA0460234 120040318A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01920CA 7022 LEFT WING FUEL ACCESS HOLE WS 136.676 HAVE INDICATIONS AT POSITION -A- FLAT HORIZONTAL SURFACE CHAMBER. REPAIRED AND ROTO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030. 2L72 4F RTA21EA 20040420001702004042000170EA 2004 4 20 COMA0460237 120040330A2910601R7528637 HYDRAULIC LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01785CA 7326 FLIGHT 5291 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, RESERVOIR INDICATED EMPTY. REPLACED HYDRAULIC SUCTION LINE IN AFT EQUIP BAY. 2L72 4F RTA21EA 20040420001742004042000174WP 2004 4 20 CALA0400326 120040406A5311 BELTFRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772822 49482 INSPECTION FOUND BELTFRAME UNDER TIEDOWN RAIL CORRODED AT STA 1231 BETWEEN STRINGER 27L AND 28L IN AFT BAGGAGE BIN. THE CORRODED AREA OF BELTFRAME WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-03, FIGURE 5. 2L72 4F A6WE 20040420001812004042000181NM 2004 4 20 UPS04M42095 120040220A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER RIGHT NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE NR 15 RIGHT REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.060 INCH. BARREL NUT HOLE REPAIRED PER EN1061-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040420001832004042000183NM 2004 4 20 UPS04M42097 120040129A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE:C HORIZONTAL STABILIZER BARREL NUT LEFT NR 36 HOLE FOUND CORROSION ON FWD & AFT WALL & GOUGE MARK ON O/B WALL DURING INSPECTION. HOLE BOTTOM SURFACE CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34. MATERIAL REMOVED 0.125 INCH. BARREL NUT HOLE REPAIRED PER EN1010-04. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-D. 2L73 4F RTA22WE 20040420001842004042000184NM 2004 4 20 CALA0400327 120040406A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 277 TO 294, RBL 45.6. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-02. 2L72 4F RTA16WE 20040420001862004042000186NM 2004 4 20 CALA0400329 120040407A5320694122616 SPLICE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND Z-ANGLE SPLICE CORRODED AT BS 1006 LEFT SIDEWALL. A NEW SPLICE WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040420001872004042000187NM 2004 4 20 CALA0400330 120040326A531465621257 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2769351 23589 MAINTENANCE DISCOVERED WEAR ON THE UPPER SURFACE OF THE LEFT KEEL BEAM LOWER CHORD OUTBOARD FLANGE BETWEEN STA 712 AND 727. THE WEAR WAS CAUSED BY THE WASHERS THAT ARE INSTALLED WITH THE LOWER WHEEL WELL FAIRING PANEL ATTACH FASTENERS. REPAIRED IAW ECRA 5311-01192. 2L72 4F RTA16WE 20040420001902004042000190EA 2004 4 20 COMA0460247 120040406A2750860D10018ABCD ECU CNDAIRCL600 CL6002B19 1900309EA E/E BAY MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01484CA2468 7702 FLIGHT 5460 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040420001912004042000191EA 2004 4 20 COMA0460248 120040406A32344622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01929CA10883 7035 FLIGHT 5596 GEAR DISAGREE WARNING, NLG INDICATED INTRANSIT. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040420001932004042000193EA 2004 4 20 COMA0460249 120040325A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01964CA 7129 RIGHT HAND 718.00 FRAME HAS CRACK IN RADIUS OF ATTACH FLANGE AT TOP OF STRINGER 11R. REPAIRED IN ACCORDANCE WITH REO 601R-53-61.969. 2L72 4F RTA21EA 20040420001942004042000194EA 2004 4 20 COMA0470031 120040406A3530 OXYGEN BOTTLE CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01354CA 10064 FLIGHT 5641 FWD CABIN 02 BOTTLE EMPTY. SERVICED 02 BOTTLE. 2L72 4F RTA21EA 20040420001952004042000195EU 2004 4 20 UPS04142103 120040407A5610 WINDSHIELD AIRBUSA300 A300F4622R 3930360EU COCKPIT CRACKED A IPXAK NONE O OTHER NRNOT REPORTED 1 SO01124UP 0808 INSPECTION TYPE:N/A ATB CAPT'S WINDSHIELD CRACKED WITH THE WINDOW HEAT LIGHT ILLUMINATED. REMOVED WINDSHIELD PANEL PER 56-11-11-4. BEGAN INSTALLATION TO STEP 2. REPLACED CAPT WINDSHIELD PER MM 56-11-11-4. OPS CHECK OK PER MM 30-42-00-5. 2L72 4F RTA35EU 20040420001962004042000196NM 2004 4 20 UPS04442101 120040326A5411 SPAR BOEING747 747121 1384871NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C NR 2 PYLON AFTER LOWER SPAR WEB NAC STA 240 AND NAC STA 256 I/B EDGE AREA CRACKS ARE FOUND AT 2 LOCATION AS MARK. NR 2 PYLON LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 2. 2L74 4F A20WE 20040420001972004042000197EU 2004 4 20 BAQA092588 120040309A6720L673M20A1005 ACTUATOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE CROSS FILLING LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03136MH2819 0161 ACTUATOR VALVE IS LEAKING EXCESSIVLY AND CROSS FILLING. REPLACED WITH SERVICABLE UNIT FROM AEC. 04/02/2004 1G72 3U3 U H88EU E34NE 20040420002032004042000203EU 2004 4 20 BAQA093959 120040330A6720 BEARING BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE BELLCRANK WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME274 550 7243 BEARINGS WORN AND ROUGH. TEFLON WORN IN BEARINGS. REPLACED WITH SERVICABLE UNIT. 04/05/2004 1G72 3U3 U H13EU E5NE 20040420002052004042000205 2004 4 20 HEEA093675 420040223A22117611112 AMPLIFIER SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1 60030NE YAW CHANNEL BURNED E HEEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03763P 760166 SMELLED ELECTRICAL FUMES DURING FLIGHT. LANDED AT MP299B. MAINTENANCE FOUND YAW CHANNEL AMP BURNED. 1G72 3U3 U H1NE E19EU 20040420002082004042000208WP 2004 4 20 UPS04842107 120040331A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040420002092004042000209WP 2004 4 20 UPS04842108 120040331A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 RIGHT WING L/E LOWER RIB IS CRACKED AT XS 429 AT I/B END OF SLOT HOUSING. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040420002102004042000210NE 2004 4 20 DHL2004752002 220040410A7230 COMPRESSOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE ENGINE STALLED A DHLAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO01752DH 22466 REJECTED TAKEOFF FOR INFORMATIONAL PURPOSES ONLY WT=152,000 LBS, TEMP=12.6, PRESS ALT=SEA LEVEL, AIRSPEED=60 KNOTS. SUSPECTED COMPRESSOR STALL WITH AN AUTO PACK TRIP. WIND WAS 89 AT CROSSWIND AT 10 KNOTS. ALSO FOR INFORMATIONAL PURPOSES ONLY. INSPECTED ENGINE INLETS, FOUND NO DEFECTS IAW M/M 71-00. 2L73 4F4 F A3WE E2EA 20040420002112004042000211GL 2004 4 20 HEEA093676 220040218A72000292005250 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL NR 2 MALFUNCTIONED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW03223422258 760096 DURING CRUISE FLIGHT NR 2 ENGINE TORQUE DROPPED TO 10 PERCENT AND NR 1 ENGINE TORQUE ROSE TO 99 PERCENT. ROTOR RPM DECREASED TO 104 PERCENT. MAINTENANCE REPLACED THE NR 1 ENGINE ASSEMBLY. 1G72 3U3 U H1NE E1GL 20040420002142004042000214EU 2004 4 20 SSHA093682 120040308A5302350A2112470051 FRAME AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE TAILBOOM CRACKED E SSHAK NONE O OTHER ININSP/MAINT 1 WP133607P11652 1249 INSPECTION OF AIRCRAFT REAR FRAME IAW ALERT SB 05.00.43 PARA. 2.B.1.A REVEALED JUNCTION FRAME TO BE CRACKED BEYOND LIMIT OF REPAIR OUTLINED IN THE MM. REMOVED UNSERVICABLE JUNCTION FRAME AND INSTALLED A SERVICABLE FRAME P/N 350A21-1247-0051 IAW MFG REPAIR SCHEME AND 8110-3. 1G72 3U3 U H11EU E19EU 20040420002152004042000215NM 2004 4 20 CALA0400373 120040410A3234UNK CONTROL LEVER BOEING737 737824 13844BZNM COCKPIT DIRTY A CALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW2733264 31584 WHEN GEAR WAS EXTENDED FOR LANDING INTO EWR, THREE GREEN AND THREE RED LIGHTS WERE RECEIVED ON THE MAIN PANEL AND THERE WERE THREE GREENS ON THE OVERHEAD. THE GEAR WAS CYCLED DURING A GO-AROUND AND THE GEAR EXTENDED NORMALLY WITH PROPER INDICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER DIRTY. THE CONTROL LEVER WAS CLEANED AND LUBRICATED. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA16WE 20040420002192004042000219 2004 4 20 BAQA093684 420040309A3452066011410101 TRANSPONDER BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE COCKPIT FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP45 7508 EXCHANGE. UNIT GIVING WRONG ALTITUDE, BAD WIRES IN UNIT. REPLACED WITH SERVICABLE UNIT. 03/15/2004 1G72 3U3 UNCH13EU E19EU 20040420002202004042000220NM 2004 4 20 04FDEA00960 120040414A5754 SKIN DOUG MD11 MD11 3023602NM L/E SLAT DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LT WING DENT MARK FOUND ON OUTBOARD NOSE SURFACE AREA OF SLAT NR 6. DENTED AREA AT LH WING OUTBOARD NOSE SURFACE OF SLAT NR 6 TRIMMED AS PER SRM 57-00-01, FIG.7, VOL. I. REPAIR PARTS FABRICATED & INSTALLED AS PER SRM 57-00-01, FIG.7, VOL.I & SRM 51-35-01, VOL.II. 2L73 4F RTA22WE 20040420002212004042000221NE 2004 4 20 BAQA093337 220040301A73200164248840 FUEL CONTROL AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE E BAQAO OTHER L NO TEST NRNOT REPORTED 1 EA03911UF1224 6338 5028 UNIT COULD NOT PASS FUEL CHECK. THIS IS ORIGINAL EQUIPMENT OFF OF THE ENGINE, TIMES DO MATCH UP TO OVERHAULS. REPLACED WITH SERVICABLE UNIT. 03/09/2004 1G72 3U3 U H10EU E19EU 20040420002222004042000222NM 2004 4 20 04FDEA00961 120040414A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, BARREL NUT BOLT BORE SPOTFACE FOUND CORRODED. SPOTFACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040420002232004042000223NM 2004 4 20 04FDEA00962 120040414A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, LOWER MOUNT SPOTFACE FOUND CORRODED. LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502, SHT.4, ZONE 40. 2L73 4F RTA22WE 20040420002252004042000225NM 2004 4 20 04FDEA00964 120040414A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, OUTBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658. 2L73 4F RTA22WE 20040420002282004042000228NM 2004 4 20 04FDEA00966 120040415A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION (C53-111-01, 3) ON SHEAR TIE BS 950E LBL 18 WL 141. CORROSION OUT OF LIMITS. REPAIRED SHEAR TIE BS 950E, LBL 18, WL 141 PER SRM 53-10-4 FIG 15 AND EA 7-5310-55285. 2L73 4F RTA3WE 20040420002302004042000230NM 2004 4 20 04FDEA00967 120040415A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 MAIN CARGO COMPARTMENT CORROSION ON FLOORBEAM BS 344 WL 208 BL 0 TO LBL 45. REMOVED CORROSION ON FLOORBEAM STA 344, LBL 38, 2 X 8 X .020 FOUND OUT OF LIMITS IAW SRM 51-10-1. REMOVED AND FABRICATED NEW FLOOR BEAM BS 344, WL 208, RBL 6 TO LBL 65 (SKIN) BAC 1505-29222 7075-T6511 LOT 540294 IAW SRM 51-30-5. FABRICATED 4 EACH SPLICE ANGLES BAC 1410-2773, 7075-T6 LOT 540292 IAW SRM 53-10-8 FIG 9. ALODINED AND PRIMED PER SOPM 20-41-02. INSTALLED UPPER CHORD AND 4EA SPLICE ANGLES IAW SRM 53-10-8 FIG 9. 2L73 4F RTA3WE 20040420002322004042000232EU 2004 4 20 I05R094206 120040308A63204649010008 TRANSMISSION UROCOPEC135 EC135P1 8680990EU MAIN ROTOR MAKING METAL B I05RK NONE O OTHER ININSP/MAINT 1 WP05552BA1834 190 TRANSMISSION MAKING METAL REPLACED PART. 1G72 3U O H88EU 20040421000012004042100001EU 2004 4 21 HXSD094143 120040316A5302350A2112470051 BULKHEAD AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1B 6OO30NE TAILBOOM CRACKED B HXSDK NONE O OTHER ININSP/MAINT 1 AL05618OT4015 1149 184 ON 3/16/06 DURING ANNUAL INSPECTION OF N6180T TAIL BOOM BULKHEAD P/N 350A21-1247-0051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME P/N ON WORK ORDER 24-36502. 1G72 3U3 U H11EU E19EU 20040421000022004042100002EU 2004 4 21 HXSD094146 120040325A5302350A2112470051 BULKHEAD AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1D1 NE TAILBOOM CRACKED B HXSDK NONE O OTHER ININSP/MAINT 1 AL05913LP2151 2383 9179 ON 3/25/04 DURING ANNUAL INSPECTION OF N913LP TAIL BOOM BULKHEAD P/N 350A21-1247-0051 WAS REMOVED DUE TO CRACK FOUND IN STRUCTURE. IT WAS REPLACED WITH A NEW COMPONENT, SAME P/N ON WORK ORDER 24-36502. 1G72 3U3 U H11EU E19EU 20040421000042004042100004NE 2004 4 21 HEEA094159 120040403A2913 SEAL SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL DRIVE SHAFT LEAKING B HEEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0322342 760096 NR 1 HYDRAULIC LIGHT ILLUMINATED DURING CRUISE FLIGHT FOLLOWED BY FLUCTUATING PRESSURE. SHUT DOWN NR 1 HYDRAULIC SYSTEM. MAINTENANCE FOUND NR 1 HYDRAULIC PUMP DRIVE SHAFT SEAL LEAKING AND NR 1 HYDRAULIC PUMP PRESSURE HOSE RUPTURED. REPLACED NR 1 HYDRAULIC PUMP PRESSURE HOSE P/N SS48C2C163000. 1G72 3U3 U H1NE E1GL 20040421000052004042100005SW 2004 4 21 ALGA094181 120040415A632023071895 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03537AL586 53230 CAE847257 GEAR HAS HEAVY SPALLING. REMOVED AND REPLACED W/SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20040421000062004042100006SW 2004 4 21 ALGA094182 120040415A63206893672 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03537AL586 53230 CAE847257 GEAR HAS HEAVY SPALLING. REMOVED AND REPLACED W/SERVICEABLE PART. 1G71 3U3 UO H2SW E1GL 20040421000072004042100007GL 2004 4 21 BAQA094018 220040401A731323077067 FUEL NOZZLE BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03302LE89 53572 REASON FOR REMOVAL STATES ENG HANG STARTS INTER. MEANS INTERMITTENT HUNG STARTS. I HAVE ENCLOSED A COPY OF THE ENGINE ASSY CARD. SO IT SHOWS YOU THAT THE REMOVED NOZZLE WAS INSTALLED 1/12/04 ENGINE TSN 8.1 REMOVED 3/24/04 ENGINE TSN 97. WHICH IT ONLY LASTED 88.9 TSN. 1G71 3U3 UO H2SW E1GL 20040421000132004042100013SW 2004 4 21 EOPR094205 120040415A2435200SGL111Q STARTER GEN BELL 407 407 1182206SW ALLSN 250C 250C20 03013GL ENGINE FAILED B EOPRO OTHER J WARNING INDICATION CRCRUISE 1 AL01847AL8371 CAE847125 53150 GENERATOR FAILED IN FLIGHT. LANDED AT NEXT OPPORTUNITY TO FIND GENERATOR BITS AND PIECES ON ENGINE DECK AND EVIDENCE OF OVERHEATING/MELTED METAL. REMOVED AND REPLACED STARTER WITH SERVICEABLE UNIT. CHECKED ENGINE CHIP DETECTORS FOR CONTAMINATION AND RAN ENGINE VIBRATION CHECK. 1G71 3U3 UO H2SW E4CE 20040421000152004042100015 2004 4 21 BAQA094141 420040415A3120B1894522281A CLOCK UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS1A NE COCKCPIT INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135LC300 0296 CLOCK WORKS INTERMITTENTLY AND THEN STOPS, WORKS THEN STOPS. REPLACED WITH SERVICABLE UNIT, 04/19/2004. 1G72 3U3 U H88EU E34NE 20040421000162004042100016NE 2004 4 21 BAQA094061 220040409A7314D240845 PUMP UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE FUEL SYSTEM FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH4 0069 FUEL PUMP FAILED OUT OF BOX (TSI 4.3 HOURS), RUNS FOR APPROX. 30 SECONDS THEN POPS CIRCUIT BREAKER. A REPLACMENT FOR THIS PUMP WAS ORDERED. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 UO H88EU E42NE 20040421000172004042100017 2004 4 21 BAQA093766 420040227A23109910951 RADIO UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE FM SYSTEM INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF351 0281 FM RADIO CHANNELS ARE FROZEN, WILL NOT CHANGE OR TRANSMIT. TFM-550 CAME FACTORY INSTALLED ON NEW EC135 ROTORWING AIRCRAFT PURCHASE FROM EUROCOPTER. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H88EU E34NE 20040421000212004042100021NE 2004 4 21 UPS04642147 220040416A7200 ENGINE BOEING767 76734AF 1385212NM GE CF6 CF680 30025NE RIGHT FLAMED OUT A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 SO01315UP 27743 INSPECTION TYPE: ETOP, RT ENGINE FLAMED OUT WHEN POWER WAS REDUCED FOR LANDING. OBVIOUSLY NO RE-START ATTEMPTED. NO ENG PARAMETER EXCEEDENCE OBSERVED. REPLACED RIGHT ENG PER TC 6002 & TC 6001 OP'S CHECK SATISFIED. 2L72 4F4 FRTA1NM E13NE 20040421000222004042100022WP 2004 4 21 UPS04842136 120040224A531156141605 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, AIR CONDITIONING ACCESSORY COMPT AT FS 56 ABOVE L24R FRAME IS CRACKED AT PNEUMATIC DUCT STANDOFF ATTACH BRACKET. REMOVED CRACKED FRAME SECTION. RECEIVED NEW -5 AND -17, -19 SPLICES. HEAT TREATED, LOCATED, DRILLED FRAME SECTION AND SPLICES. ALODINED AND PRIMED, INSTALLED FRAME SECTION AND SPLICES; ALL IAW DC8 SRM 51-1-20D, 21-1-21, 53-2-0 TR 53-125, 51-1-8, TPS-1003 REV A, AND DAC DWG 5614160. 2L74 4F RT4A25 20040421000232004042100023WP 2004 4 21 UPS04842137 120040224A531156141605 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AIR COND ACCESSORY COMPT AT FS 56 ABOVE L24L FRAME CRACKED AT PNEUMATIC DUCT STANDOFF ATTACH BRACKET. REMOVED CRACKED FRAME SECTION AT FS 56 LT FROM CUSP TO L26L, RECEIVED NEW - 5 FRAME SECTON AND SPLICES -17, -19; HEAT TREATED; LOCATED & DRILLED; ALODINED & PRIMED; INSTALLED FRAME SECTION AND SPLICES; ALL IAW DC8 SRM 51-1-20D, 21-1-21, 53-2-0 TR 53-125, 51-1-8, TPS 1003 REV A, AND DAC DWG 5614160. 2L74 4F RT4A25 20040421000242004042100024WP 2004 4 21 UPS04842138 120040224A531356138627 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, AIR COND ACCESSORY COMPT AT FS 56 L31R IS CORRODED. REMOVED CORROSION (ORIG MAT'L .090 REM .068) OUT OF LIMITS; FORMED REPAIR ANGLE IAW REO G09728. DYE PEN INSP; NO CRACKS NOTED; HEAT TREATED; LOCATED AND DRILLED; ALODINED AND PRIMED; INSTALLED ANGLE; ALL IAW DC8 SRM 51-1-8, 53-3-1, 51-2-0, 53-2-0 REO G09728, OHM 15-3-5, TPS 1003 REV A, AND 51-1-20D. 2L74 4F RT4A25 20040421000252004042100025WP 2004 4 21 UPS04842139 120040225A5730561135035 SKIN DOUG DC8 DC871F 302199DWP WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, FWD UPPER LT W/W AT STA 857-000 UPPER SPAR CAP AND PLATING HAVE CORROSION BULGING AREA LBL 46. REMOVED CORROSION; (ORIG .270, REM .141) OUT OF LIMITS. FABRICATED REPAIR FILLER, DOUBLER, TRIPLER, PRESSURE PANEL ASSEMBLY DOUBLER, SHIMS, PANEL (P/N 5646674-25), FLOOR SUPPORT ANGLE SPLICE; ALODINED & PRIMED; INSTALLED REPAIR PARTS; ALL IAW DC8 SRM 51-1-8, 57-2-0, AND TIMCO REO G09719. 2L74 4F RT4A25 20040421000272004042100027WP 2004 4 21 04FDEA00968 120040415A5410 PANEL DOUG DC10 DC1010 3022110WP NR 2 NACELLE MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 ON ARRIVAL WALKAROUND CHECK FOUND NR 2 ENGINE LEFT FWD LOWER PICKLE BARREL PANEL MISSING. RECEIVED PANEL AJC7077-1, PRE-DRILLED HOLES DO NOT LINE UP WITH STRUCTURES HOLES. COMPLIED WITH EA 8-5410-76625 PART 1. FLEW A/C TO IND FOR PERMANENT REPAIR. COMPLIED WITH EA 8-5410-76625 PART 2 AS REQUIRED. PNL 363AL UPPER HINGE HALF HAS ELONGATED HOLES, PERFORMED PERMANENT REPAIR TO HINGE HALF. CONNECTED TO PANEL. REPAIR REF EA 8-5410-76625. 2L73 4F A22WE 20040421000292004042100029WP 2004 4 21 04FDEA00970 120040413A7603 CONTROL CABLE DOUG DC10 DC1010 3022110WP NR 2 THROTTLE STUCK A FDEAE ENGINE SHUTDOWN S AFFECT SYSTEMS DEDESCENT 1 SO2568051 47805 NR 2 THROTTLES STUCK AT 91 PERCENT N1 FL310 SHUTDOWN ENGINE AT 6000 HIGH THROTTLE BROKE FREE ON TAXI IN. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE IN REF TO DC10 MM 76-11-01-2 RIG CHECKED GOOD. INSTALLED ALL SCREWS ON NR 2 ENGINE ACCESS PANELS, CLOSED WORK PLATFORM, AND PERFORMED AN ENGINE RUN FOR 5 MINUTES. MOVED THROTTLE TO BREAKAWAY THRUST AND THROTTLE MOVEMENT WAS SMOOTH AND RESPONDED WELL. ACFT OK FOR SERVICE. 2L73 4F A22WE 20040421000302004042100030EU 2004 4 21 04FDEA00971 120040415A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP BETWEEN 3 AND 4 SEAT TRACK FROM CENTER LINE, FLOOR PLATE PANEL HAS 3EA AREA OF CORROSION BETWEEN FR25 AND FR26. BLENDED OUT COROSION FOUND TO BE OUT OF LIMITS IWA A300-600 SRM 51-74-10 AND 53-10-00. REMOVED THRUST PLATE AND REINSTALLED OLD ANGLE FROM PLATE AND RE-INSTALLED ON NEW PLATE IAW A300-600 SRM 51-72-10 AND 51-40-21, AND INSTALLED NEW THRUST PLATE IAW A300-600 SRM 51-72-10 ABD 51-40-21. 2L72 4F RTA35EU 20040421000312004042100031EU 2004 4 21 04FDEA00972 120040415A5321A5378198422200 PLATE AIRBUS300 A300F4605R 3930327EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 METAL PNL AT NR 4 LEFT AND 5 LEFT SEAT TRACK BETWEEN C30 AND 31 HAS 4EA AREA'S OF CORROSION. REMOVED ANGLE FROM OLD THRUST PLATE AND INSTALLED ON NEW THRUST PLATE IAW A300-600 SRM 51-72-10 AND 51-40-30 AND INSTALLED NEW THRUST PLATE IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040421000322004042100032NM 2004 4 21 UPS04242177 120040403A5754 SKIN BOEING727 72731C 1384011NM KRUGER FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C NR 4 K-FLAP HAS CRACK ON INNER ANTI-ICE SKIN AROUND RIVET HOLE I/B OF O/B ACTUATION LINKAGE FOR BULLNOSE. REPAIR CARRIED OUT IAW SRM 51-30-2, 57-50-3. 2L73 4F A3WE 20040421000362004042100036NM 2004 4 21 UPS04242181 120040407A5753 CASTING BOEING727 72731C 1384011NM RT FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, RIGHT O/B FLAP I/B FLAP TRACK FAIRING HAS CRACKED CASTING/BRACKET. CRACKED BRACKET REMOVED IAW SRM 51-30-02 & STOP DRILLED IAW SRM 51-10-1. REPAIR SECTION FABRICATED IAW SRM 51-40-3 & INSTALLED IAW SRM 51-40-3. 2L73 4F A3WE 20040421000372004042100037NM 2004 4 21 UPS04242204 120040406A5510 BEAM BOEING727 72731C 1384011NM RT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM HAS CORROSION AFT OF BALANCE PANEL BAYS. BEAM REPLACED IAW SRM 51-30-2 AND DRG NR 65-22987. 2L73 4F A3WE 20040421000382004042100038NM 2004 4 21 UPS04242205 120040407A5753 FLAP TRACK BOEING727 72731C 1384011NM NR 6 FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, NR 6 FLAP TRACK FAIRING I/B TRACK IS CRACKED. FAIRING TRACK REPLACED IAW SRM 51-30-02. 2L73 4F A3WE 20040421000402004042100040NM 2004 4 21 UPS04442171 120040326A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C FWD CARGO LT STA 920 SLOPE PNL SUPPORT WEB CRACKED. FWD CARGO COMPT LT BS 920 BETWEEN STR 37L AND STR 38L FRAME REPAIR CARRIED OUT AS PER HX RS R53-22-35141, UPS ENGINEERING FILE NR 747-53-20178. 2L74 4F A20WE 20040421000412004042100041NM 2004 4 21 UPS04442172 120040326A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, FWD CARGO FX 880 FRAME CRACKED BETWEEN STR 37-38R. FWD CARGO COMPT BS 880 RT BETWEEN S37R AND S38R FRAME REPAIR CARRIED OUT AS PER HX RS R-53-22-35139, UPS ENGINEERING FILE NR 747-53-20177. 2L74 4F A20WE 20040421000442004042100044NM 2004 4 21 CALA0400392 120040418A552365C2638427A TAB BOEING737 737524 1384721NM LT ELEVATOR DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717663 28924 LEFT ELEVATOR TAB DELAMINATED (1 INCH SQ) AT OUTBOARD END OF TRAILING EDGE. REPAIRED LEFT ELEVATOR TAB PER SRM 51-70-04. 2L72 4F RTA16WE 20040421000472004042100047NM 2004 4 21 UPS04442175 120040326A5314 KEELBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, FX - KEELBEAM BOX INTERIOR LOWER WEB FOUND HEAVY CORROSION AT STA 1112 TO STA 1115 RBL 3 TO RBL 6. CORROSION BLEND OUT 0.039 X 2 X 2 INCH. KEEL BEAM BOX LOWER WEB REPAIRED AS PER HX RS R53-49-35142 AND UPS ENGINEERING FILE NR 747-53-20182, NRC 5728 FOR REPAIR DETAILS. 2L74 4F A20WE 20040421000482004042100048NM 2004 4 21 UPS04442176 120040325A5314 KEELBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, FX - KEELBEAM BOX LOWER EXTERNAL WEB ACCESS HOLE DOUBLER FOUND CORROSION CRACKED AT STA 1112 TO STA 1115 RBL 3 TO RBL 6. CORROSION BLEND OUT 0.050 X 2 X 2 INCH. DOUBLER, FILLER AND 2EA SPLICED ANGLE FABRICATED AND REPAIR PART INSTALLED AS PER RS 53-49-35142, UPS ENGINEERING FILE 747-53-20182. 2L74 4F A20WE 20040421000492004042100049NM 2004 4 21 UPS04442200 120040326A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, M/D - STA 360 S17L POSITION FRAME CRACK. M/S BS 360 STR 17L FRAME REPAIR CARRIED OUT AS PER HX RS R-53-12-35134 AND UPS EO B747-5310-20297. 2L74 4F A20WE 20040421000502004042100050NM 2004 4 21 UPS04442201 120040323A5330 SKIN BOEING747 747121 1384871NM FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, VISUAL INSPECTION OF FUSELAGE DENT .110 INCH DEEP MINOR AXIS 2.5 INCH AT FX 270 30 INCH BELOW FIRST OFFICER'S WINDOW. FUSELAGE BS 265-275 BETWEEN STR 9R AND STR 10R SKIN REPAIR CARRIED OUT AS PER SRM 53-30-03 FIG 1 CATEGORY A REPAIR. 2L74 4F A20WE 20040421000512004042100051NM 2004 4 21 UPS04442202 120040326A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C FWD CARGO FS 900 FRAME CRACKED BETWEEN STR 37-38R. FWD CARGO COMPT BS 900 BETWEEN STR 37R AND 38R FRAME REPAIR CARRIED OUT AS PER HX RS R-53-22-35140 AND UPS ENGINEERING FILE NR 53-20179. 2L74 4F A20WE 20040421000522004042100052NM 2004 4 21 UPS04442207 120040418A3350 LIGHT BOEING747 747212B 1384886NM EMERGENCY EXIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 EMERGENCY EXIT LIGHT AT ESCAPE DOOR ON FLIGHT DECK GOES OUT 3-5 SECONDS AFTER BEING TURNED ON. REPLACED LIGHT PACK ASSY, OPS CHECKS OK. 2L74 4F A20WE 20040421000542004042100054NM 2004 4 21 UPS04442209 120040417A3350 BATTERY PACK BOEING747 747121 1384871NM L1 DOOR INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01682UP 20349 AFT EMERGENCY LIGHT IN L1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-04, OPS CHECK GOOD. 2L74 4F A20WE 20040421000552004042100055WP 2004 4 21 UPS04842152 120040227A53476015176 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, MAIN CABIN FS 1220 SEAT TRACK -E- GOUGED ON SCALLOPS. BLENDED GOUGED AREA IAW DC8 SRM 53-2-0. OUT OF LIMITS IAW DC8 SRM 53- 2-3. REMOVED SEAT TRACK STA 1180-1280. RECEIVED NEW SEAT TRACK AND FITTING. CUT AND DRILLED SEAT TRACK AND FITTING IAW UPS EO DC8-5320-5167-C. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SEAT TRACK AND FLOORBOARDS IAW DC8 SRM 51-3-0 AND UPS EO DC8-5320-5167-C. 2L74 4F RT4A25 20040421000572004042100057NM 2004 4 21 CALA0400376 120040415A5313BAC1498117 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND STRINGER 25L CORRODED AT STA 967-996. A NEW STRINGER AND SPLICES WERE INSTALLED IAW SRM 53-00-03. 2L72 4F RTA16WE 20040421000582004042100058NM 2004 4 21 CALA0400377 120040415A5320655584311 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND AFT GALLEY DRAIN MAST HAT CHANNEL CORRODED AFT OF STA 986.5 BETWEEN S25L AND S26L. 2L72 4F RTA16WE 20040421000592004042100059NM 2004 4 21 CALA0400378 120040415A5510180A16211 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723721 28940 INSPECTION FOUND LEFT HORIZONTAL STABILIZER REAR SPAR UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421000602004042100060NM 2004 4 21 CALA0400379 120040415A5510180A16122 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723721 28940 INSPECTION FOUND THE LEFT HORIZONTAL STABILIZER REAR SPAR LOWER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421000632004042100063NM 2004 4 21 CALA0400382 120040416A5510180A16122 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723721 28940 INSPECTION FOUND LEFT HORIZONTAL STABILIZER MIDDLE PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421000642004042100064NM 2004 4 21 04FDEA00982 120040416A5313 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT AT STA 5-123 RIGHT STR 49 LONGERON SPLICE FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040421000652004042100065NM 2004 4 21 04FDEA00984 120040416A5410 STRIP BOEING727 727200 138407ENM PYLON TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 PANEL 5531 CHAFE STRIP IS TORN. REMOVED AND REPLACED STRIP IAW SRM 51-30-2 AT MAE. FABBED FROM 301-25 .012SS BATCH 000705488. 2L73 4F RTA3WE 20040421000682004042100068NM 2004 4 21 04FDEA00987 120040417A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN STA 427 LBL 53 - LBL 76 FOUND FLOOR SUPPORT BEAM CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040421000692004042100069NM 2004 4 21 04FDEA00988 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT I/B FLAP VANE I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED AS PER CMM57-52-03. 2L73 4F RTA22WE 20040421000712004042100071NM 2004 4 21 CALA0400384 120040417A53306545871 SKIN BOEING737 7373T0 1384582NM R1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 R1 DOOR LOWER HINGE CUTOUT UPPER SKIN PULLING AND CRACKED (1 INCH) ALONG RIVETS JUST ABOVE CUTOUT. FABRICATED AND INSTALLED REPAIR PER SRM 52-00-01. 2L72 4F RTA16WE 20040420002062004042000206WP 2004 4 20 UPS04842105 120040408A33506012335 BATTERY DOUG DC8 DC871F 302199DWP COCKPIT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, OP CHECKED GOOD. 2L74 4F RT4A25 20040420002072004042000207WP 2004 4 20 UPS04842106 120040331A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 304 AT PNEUMATIC DUCT SUPPORT. CUT OUT AND STOPDRILLED CRACKED AREA, NDT VERIFIED NO CRACKS AT STOPDRILLS AND CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040420002122004042000212SW 2004 4 20 HEEA093677 120040227A6340BAS212412100G PRESSURE SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA GEARBOX FLUCTUATES E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW032261D 33076 DURING CRUISE FLIGHT THE COMBINING GEARBOX OIL PRESSURE FLUCTUATED, LANDED. MAINTENANCE REPLACED THE OIL PRESSURE TRANSDUCER. 1G72 4U4 U H4SW E22EA 20040420002132004042000213SW 2004 4 20 HEEA093678 120040225A291070060T000Y255 HOSE BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE HYD SYSTEM RUPTURED E HEEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW038045T 28101 NR 1 HYDRAULIC SYSTEM FAILED IN FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOSE RUPTURED. REPLACED HOSE. ALSO REPLACED PUMP DUE TO RUNNING DRY. 2G72 4U4 U H10SW E8NE 20040420002172004042000217EU 2004 4 20 BAQA093683 120040307A7160430110217 ACTUATOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03912TG 7174 EXCHANGE - CORE RETURN FOR EXCHANGE PO 2-023236-05, ACTUATOR IS CAUSING COMPRESSOR STALLS. PLEASE NOTE THAT THIS ACTUATOR (S/N 2939) WAS INSTALLED ON ENGINE LE45512 FOR ONLY 7.2 HOURS, (DO NOT REPAIR AND RETURN S/N 2939). REPLACED WITH SERVICABLE UNIT. 03/18/2004 1G72 3U3 U H13EU E5NE 20040420002242004042000224NM 2004 4 20 04FDEA00963 120040414A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT FORWARD (WING SIDE) OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-76658. 2L73 4F RTA22WE 20040420002292004042000229EU 2004 4 20 BAQA092597 120040309A2741L209CCM2 ACTUATOR BOLKMSBK117 BK117C1 5626025EU TRIM FEEL INOPERATIVE B BAQAK NONE L NO TEST ININSP/MAINT 1 EA03117UP3241 7508 BENCH TEST FOR SERVICEABILITY. REPLACED WITH SERVICABLE UNIT. 03/09/2004 1G72 3U NCH13EU 20040421000082004042100008GL 2004 4 21 BAQA093729 220040310A7314 FILTER AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL FUEL PUMP FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03942MS T103451 5498 CAE841011 UNIT FAILED FILTER BY-PASS CHECK. THIS UNIT WAS ORIGINALLY ON THE ENGINE WHEN INSTALLED ON A/C S/N 5498. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1G72 3U3 U H11EU E4CE 20040421000102004042100010CE 2004 4 21 BAQA094195 120040416A242426800148 VOLT REGULATOR LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0330DK 10001 345 VOLTAGE REGUALTOR IS GIVING HIGH READINGS, WILL NOT REGULATE AMP GAUGE. REPLACED WITH SERVICABLE UNIT FROM JEARJET, 04/19/2004 2L72 4F4 F A10CE E6WE 20040421000122004042100012GL 2004 4 21 ALGA094199 220040419A725023053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30S 03013GL ENGINE OUT OF TOLERANCEE ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PARTO FOUND FLOW AREA BELOW MIN. RETURNING PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20040421000262004042100026WP 2004 4 21 UPS04842140 120040225A53403643758503 FITTING DOUG DC8 DC871F 302199DWP KEELBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, FITTING AT STA 902 IN RIGHT WHEEL WELL OVER KEELBEAM IS CRACKED. RECEIVED NEW PART P/N 3643758-503. LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND 51-3-1. 2L74 4F RT4A25 20040421000282004042100028WP 2004 4 21 04FDEA00969 120040415A5230 ACCESS PANEL DOUG DC10 DC1030 3023501WP CARGO DOOR MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25315FE 48313 DURING MAINT WALKAROUND FOUND CTR CARGO DOOR PRESSURE RELIEF ACCESS PANEL MISSING FROM A/C. INSTALLED PANEL PER MM 53-53-00. 2L73 4F A22WE 20040421000332004042100033NM 2004 4 21 UPS04242178 120040405A5315 FLOORBEAM BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328 RBL 24. REPAIR CARRIED OUT IAW SRM 53-10-8. 2L73 4F A3WE 20040421000342004042100034NM 2004 4 21 UPS04242179 120040405A5315 FLOORBEAM BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 344 LBL 24. REPAIR CARRIED OUT IAW SRM 51-20-1 FIG 7. 2L73 4F A3WE 20040421000352004042100035NM 2004 4 21 UPS04242180 120040406A5315 FLOORBEAM BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, FLOORBEAM FOUND CRACKED AT BS 328, RBL 44. REPAIR CARRIED OUT IAW SRM 53-10-8. 2L73 4F A3WE 20040421000392004042100039NM 2004 4 21 UPS04242206 120040406A5350 FRAME BOEING727 72731C 1384011NM FAIRING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE: C, FUSELAGE FAIRING 3430 HAS EXTENSIVE CORROSION TO THE FORMED FRAME HOLDING THE ANCHOR NUTS (FWD SIDE OF FAIRING). REPAIR CARRIED OUT IAW SRM 53-10-01, 51-20-01, 51-10-02 & 51-30-02. 2L73 4F A3WE 20040421000422004042100042NM 2004 4 21 CALA0400390 120040416A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 SEAT TRACK CORRODED (10 INCHES) BETWEEN FLOOR STATION 328 AND 346. REPLACED CORRODED SEAT TRACK PER SRM 53-00-52. 2L72 4F RTA16WE 20040421000432004042100043NM 2004 4 21 CALA0400391 120040418A531065498901 STOP FITTING BOEING737 737524 1384721NM R2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717663 28924 R2 DOOR STOP FITTING CRACKED (1 INCH) FORWARD UPPER FITTING SECOND FROM TOP. REMOVED AND REPLACED FITTING PER SRM 51-40-02. 2L72 4F RTA16WE 20040421000452004042100045NM 2004 4 21 UPS04442173 120040326A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C FWD CARGO LT STA 880 SLOPE PNL SUPPORT WEB CRACKED. FWD CARGO LT BS 880 BETWEEN S37L AND S38L FRAME REPAIR CARRIED OUT AS PER HX RS R53-22-35138, UPS ENGINEERING FILE NR 747-53-20176. 2L74 4F A20WE 20040421000462004042100046NM 2004 4 21 UPS04442174 120040329A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, AFT CARGO STA 1740 S42R STRINGER END CRACK. AFT CARGO COMPT BS 1740 STR 42R STRINGER REPAIR CARRIED OUT AS PER HX RS R53-61-35135, UPS ENGINEERING FILE NR 747-53-20181. 2L74 4F A20WE 20040421000532004042100053NM 2004 4 21 UPS04442208 120040418A3350 LIGHT BOEING747 747212B 1384886NM EMERGENCY EXIT MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01526UP 21937 EMERGENCY EXIT LIGHT AT POS 500 ON MCD HAS ONE LAMP INOP. REPLACED LAMP, OPS CHECKS OK. 2L74 4F A20WE 20040421000732004042100073NM 2004 4 21 CALA0400386 120040418A5313BAC1498162 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 STRINGER 27L HAS HEAVY CORROSION FROM STA 955 TO APB (5 FT). REMOVED AND REINSTALLED NEW STRINGER SECTION AT 27 LEFT STA 907 TO 1016 PER SRM 51-10-02. 2L72 4F RTA16WE 20040421000762004042100076NM 2004 4 21 CALA0400389 120040416A534565B578393 MOUNT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 FORWARD LAV MOUNT CORRODED AT STA 300 LBL 10. REMOVED AND REPLACED DAMAGED MOUNT PER SRM 51-10-02. 2L72 4F RTA16WE 20040421000772004042100077NM 2004 4 21 04FDEA001001 120040417A53216519606178 FLOOR PANEL BOEING727 727200 138407ENM CARGO COMPT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25279FE 22346 CENTER WEB AND CHORD IS CORRODED UNDER FLOOR PANEL AT BS 1176 FWD OF AFT AIR STAIRWAY IN MAIN CARGO COMPT. REMOVED AND REPLACED WEB AND CHORD IAW SRM 51-30-2 AT MAE. 2L73 4F RTA3WE 20040421000782004042100078EU 2004 4 21 04FDEA001004 120040418A3244 TIRE AIRBUS310 A310222 3930315EU MLG FAILED A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO25421FE4973 616 342 ON TAKEOFF, NOSE WHEEL TIRE FAILED AT V1=144 KTS, GW = 297.0. FOUND RIGHT TIRE BURST AND TORN TREAD. REMOVED AND REPLACED LT & RT NOSE TIRE ASSY PER MM 12-37-32-0-04. PREMATURE REMOVAL/INSTALLATION, OFF MFG 286351003-1-51, POS 1 SRL W1879A, TAG 542768, ON MFG 286351003-1-51, SRL W3039, TAG 462894, PREMATURE REMOVAL/INSTALLATION OFF MFG Z32-002-02, POS 2 SRL F243, TAG 542769, ON MFG 286351003-1-51, SRL 09920, TAG 998810. 2L72 4F RTA35EU 20040421000802004042100080NM 2004 4 21 04FDEA001006 120040418A5321 FLOOR PANEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN, STA 442 - STA 447 LBL 87 FOUND FLOOR CORRODED. 2L73 4F RTA22WE 20040421000812004042100081NM 2004 4 21 AWXA200400370 120040415A2131750A000002 VALVE AIRBUSA319 A319132 3930340NM ZONE 138 MALFUNCTIONED A AWXAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CRCRUISE 1 WP28818AW354008474 1375 AT FL 310 COULD NOT CONTROL CABIN PRESSURE, 250 FPM TO 10000, DESCENDED DOWN TO 12000 FT AND DIVERTED. PREVIOUS FLT A MEL WAS ISSUED FOR AFT CABIN TEMP & RT PACK FLOW CONTROL VALVE DE-ACTIVATED & LOCKED IN CLOSED POSITION. MEL ALSO REQUIRES FLOW SWITCH BE PLACED IN HIGH POSITION, AFTER DIVERSION SWITCH FOUND IN NORMAL. MX PERFORMED CABIN PRESSURIZATION CHECK USING PACKS 1 & 2 INDEPENDENTLY WITH FLOW SELECT SWITCH IN HIGH, COND 1, OPS NORMAL. RE-ACCOMPLISHED PROCEDURE USING BOTH PACKS TOGETHER & OPS NORMAL. PERFORMED BITE TEST OF CABIN PRESSURE CONTROLLERS 1 & 2, CHECKED GOOD. BITE TEST OF CFDS FAILED AFT CABIN TRIM AIR VALVE 13HK FOR AFT CABIN TEMP PROBLEM. R&R AFT CABIN TRIM AIR VALVE, OPS CHECK GOOD. 2L72 4F RTA28NM 20040421000822004042100082EU 2004 4 21 AWXA200400371 120040328A5315D53472172201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RIGHT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 9, PG 6-7 & 25. 2L72 4F RTA28NM 20040421000852004042100085NM 2004 4 21 AWXA200400372 120040402A575465C26794 SKIN BOEING737 7373G7 1384595NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING C-15 CHECK 6 EACH .3125 INCH CRACKS WERE FOUND IN NR 2 SLAT LOWER SKIN EMANATING FROM FASTENER HOLES BELOW THE INBOARD AUXILIARY TRACK AT FS 134.0 LEFT. MAINTENANCE REMOVED DOUBLER OUTBOARD OF DAMAGED AREA; CUT OUT CRACKED AREA OF NR 2 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW 737-300 SRM 57-43-01, FIG 206, PG 216-219. 2L72 4F RTA16WE 20040421000862004042100086NM 2004 4 21 AWXA200400367 120040414A53306545774575 SKIN BOEING737 737375 13844BNNM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28336AW 23707 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 1.74 INCH CRACK WAS FOUND IN FUSELAGE SKIN APPROXIMATELY 3 INCHES BELOW AND FWD OF RIGHT FUSELAGE AFT WING TO BODY FAIRING AND EMERGENCY EXIT LIGHT BS 727D, STR 21 & STR 22 RIGHT. MAINTENANCE REMOVED CRACKED SKIN AT BS 727D, BETWEEN STR 21 & STR 22 RIGHT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01 FIG 229, DETAIL 11. 2L72 4F RTA16WE 20040421000872004042100087EU 2004 4 21 AWXA200400375 120040416A28109813395 VALVE AIRBUS320 A320231 3930325EU RT WING FAULTY A AWXAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP28637AW45179 099 CMH - FUEL - FLT 0794 - WHILE TAXIING TO RUNWAY FOR DEPARTURE FUEL WAS REPORTED LEAKING FROM THE RIGHT WING, RETURNED TO GATE. MAINTENANCE FOUND FUEL LEAK COMING FROM RIGHT WING OUTBOARD SURGE TANK NACA INTAKE VENT. REMOVED AND REPLACED FUEL LEVEL SENSING CONTROL UNIT NR 1 PER TSM 28-21-00-810-825 & TSM 28-46-00-810-818. FUEL LEVEL SENSING SYSTEM BITE CHECK WAS GOOD, BUT DURING ENGINE RUN FUEL CONTINUED TO LEAK FROM NACA VENT. REMOVED AND REPLACED RIGHT WING AIR RELEASE VALVE IAW AMM 28-21-41-04, LEAK CHECK WAS GOOD. AIR RELEASE VALVE S/N FRTR200AB WAS DAMAGED BEYOND ECONOMICAL REPAIR; UNIT WAS SCRAPPED AT VENDOR. 2L72 4F RTA28NM 20040421000882004042100088NM 2004 4 21 AWXA200400376 120040416A5730114N2106 SKIN BOEING757 7572S7 1384962NM RT WING LE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 RIGHT FIXED WING LEADING EDGE UPPER SURFACE DISBONDED AT WS 397. MAINTENANCE REMOVED DAMAGE ON RIGHT FIXED WING LEADING EDGE UPPER SURFACE WS 397 AND PERFORMED BOND REPAIR PER AWA ER 19-5700-00012-DD4 & 757-200 SRM 51-70-17. 2L72 4F RTA2NM 20040421000892004042100089NM 2004 4 21 AWXA200400377 120040417A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 21 LT DETACHED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28156AW 23778 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT ROW 21 LEFT WILL NOT STAY ATTACHED TO SEAT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 21 LEFT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040421000912004042100091NM 2004 4 21 04FDEA00990 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP VANE I/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER CMM57-52-03. 2L73 4F RTA22WE 20040421000922004042100092NM 2004 4 21 04FDEA00991 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP VANE O/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER CMM57-52-03. 2L73 4F RTA22WE 20040421000932004042100093NM 2004 4 21 04FDEA00992 120040417A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP FWD I/B HINGE O/B SIDE SURFACE AROUND THE BRACE FITTING FOUND RUSTY AND PAINT WORK DETERIORATED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND REFER TO THE DWG TOLERANCE OF ARC0502 SHT 1. 2L73 4F RTA22WE 20040421000942004042100094NM 2004 4 21 04FDEA00993 120040417A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP FWD I/B HINGE O/B SIDE SURFACE AROUND THE FWD MOUNT AREA FOUND RUSTY AND PAINT WORK DETERIORATED. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC 0502 SHEET 2. 2L73 4F RTA22WE 20040421000952004042100095NM 2004 4 21 04FDEA00994 120040417A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT O/B FLAP FWD I/B HINGE O/B SIDE ABOVE PIVOT BORE SURFACE FOUND WITH CHAFE MARKS. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHEET 1. 2L73 4F RTA22WE 20040421000962004042100096NM 2004 4 21 04FDEA00995 120040417A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT O/B FLAP FWD I/B HINGE O/B SIDE ABOVE PIVOT BORE SURFACE FOUND WITH CHAFE MARKS. CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN TOLERANCE LIMIT AS PER DWG ARC0502 SHEET 1. 2L73 4F RTA22WE 20040421000972004042100097NM 2004 4 21 04FDEA00996 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT I/B FLAP VANE I/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2L73 4F RTA22WE 20040421000982004042100098EA 2004 4 21 COMA0460251 120040409A2740 MOTOR CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01492CA 7763 FLIGHT 5798 STAB TRIM FAILED DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF STAB TRIM NORMAL. 2L72 4F RTA21EA 20040421001002004042100100NM 2004 4 21 04FDEA00997 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT I/B FLAP VANE O/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2L73 4F RTA22WE 20040421001012004042100101NM 2004 4 21 04FDEA00998 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP VANE I/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION.CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2L73 4F RTA22WE 20040421001032004042100103EA 2004 4 21 COMA0460250 120040409A4990 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU OIL SYS ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01779CA 7306 FLIGHT 5051 APU OIL TEMP CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED OIL LEVEL AND CLEANED TEMP SWITCH. RUN CHECKS WERE NORMAL. 2L72 4F RTA21EA 20040421001082004042100108NM 2004 4 21 04FDEA00973 120040415A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 AFT FUSELAGE RT EXTERIOR SKIN FOUND WITH CORROSION AT STA Y 2007-2015 LONGERON STR 27. COMPLIED WITH FEDEX EA 1-5310-76666. REMOVAL AT RT FUSELAGE STATION 1997.75 LONGERON L-27R CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040421001092004042100109WP 2004 4 21 04FDEA00974 120040416A5510SB1055001617KIT PANEL DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 ON PANEL 7208-1 RT SIDE FOUND BY ULTRASONIC INSPECTION 1 HOLE WITH CRACK, L= .25 INCH AT 1 INCH FROM BOTTOM. REPLACED PANELS PER SB 55-16 FIG 3 GROUP 1 (EA -8-5510-70126) FEDEX P/N: SB10550016-17KIT, SB10550016-93KIT. THE P/N ITEM 5 IS A REPLACEMENT KIT. THE CORRECT P/N DEFECTED IS 7208-1. 2L73 4F A22WE 20040421001112004042100111EU 2004 4 21 04FDEA00976 120040416A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN CARGO DECK LEFT TRACK 5 HAS 8 EA AREAS OF CORROSION, 8 INCHES AFT OF FR 48, FR 49, 6 INCHES FWD OF FR 50, JUST FWD OF FR 51, JUST AFT OF FR 51, FWD OF FR 52, FR 53, FR 54. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN AREAS 1-4. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 BETWEEN FRAMES 48-51, BURNISHED AND TREATED DISCREPANCIES IN OTHER NOTED AREAS. 2L72 4F RTA35EU 20040421001122004042100112EU 2004 4 21 04FDEA00977 120040416A5320 PAN AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC FLOOR PAN BETWEEN TRACKS 2 & 3 RT FR 27 HAS 2 EA AREAS OF CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040421001152004042100115NM 2004 4 21 04FDEA00980 120040416A5320 WEB BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 SHEAR WEB CRACKED, AT BS 380-400, LBL 65, WL 208. REMOVED CRACKED SHEAR WEB BS 380-400, LBL 65, WL 208. FABRICATED NEW WEB AND INSTALLED IAW SRM 51-30-5, SRM 51-30-2 AND FED EX MM 51-20-151. 2L73 4F RTA3WE 20040421001162004042100116NM 2004 4 21 04FDEA00981 120040416A5330 SKIN BOEING727 727200 138407ENM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 UPPER FUSELAGE SKIN BULGE AT BS 380 BETWEEN STR 17L AND STR 18L. FOUND BULGE IN SKIN, BS 380 BETWEEN STR 17L & 18L, TO BE CREASED AND OUT OF LIMITS IAW SRM 53-30-1.CUT OUT DAMAGED SKIN 2 X 6 AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3. 2L73 4F RTA3WE 20040421001192004042100119EA 2004 4 21 COMA0460262 120040412A3230 UPLOCK HOOK CNDAIRCL600 CL6002B19 1900309EA MLG OUT OF ADJUST A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01929CA 7035 FLIGHT 5659 GEAR DISAGREE WARNING ON APPROACH. COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE NORMAL. ADJUSTED NLG UPLOCK HOOK TO M/M SPECS. 2L72 4F RTA21EA 20040421001202004042100120EA 2004 4 21 COMA0460259 120040410A326016600101 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01929CA25125 7035 FLIGHT 5870 GEAR DISAGREE WARNING ON APPROACH. REPLACED THE NLG UPLOCK. 2L72 4F RTA21EA 20040421001222004042100122NM 2004 4 21 04FDEA001003 120040417A5311 FRAME BOEING727 727200 138407ENM NLG SUPPORT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 COMPLY WITH EA 7-5310-77343; FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0, RBL 6.5 WL 153. COMPLIED WITH EA 7-5310-77343 FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0 RBL 6.5 WL 153 AT MAE. 2L73 4F RTA3WE 20040421001242004042100124WP 2004 4 21 04FDEA001007 120040419A5753ARC0502502 HINGE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH EA 8-5740-77340 WINGS RT OUTBOARD FLAP, FLAP INBOARD HINGE CORROSION REPAIR (P/N ARC0502-502). COMPLIED WITH EA 8-5740-77340 WINGS RT OUTBOARD FLAP, FLAP INBOARD HINGE CORROSION REPAIR P/N ARC 0502-502. 2L73 4F RTA22WE 20040421001262004042100126NM 2004 4 21 04FDEA00704 120040323A5753ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LEFT WING, OUTBOARD FLAP, OUTBOARD FORWARD HINGE, ACTUATOR ROD END HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5740-75913, WINGS LEFT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040421001292004042100129NM 2004 4 21 04FDEA00956 120040414A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP O/B HINGE ACTUATOR LUG I/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040421001312004042100131NM 2004 4 21 AWXA200400366 120040414A3350100865 POWER SUPPLY BOEING757 7572G7 1384963NM EMERGENCY LIGHT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 LAS - EEL - DURING 8-DAY CHECK THE L-1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M731 AT BS 369, LBL 5, WL 290, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040421001322004042100132NM 2004 4 21 AWXA200400368 120040414A7930SEL0C4W INDICATOR BOEING737 737301 1384611NM NR 2 ENG OIL FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28325AW17577 23260 ON TAKEOFF, NR 2 ENGINE OIL PRESSURE NEVER WENT ABOVE 21 PSI IN YELLOW RANGE, REJECTED TAKEOFF BETWEEN 100-110 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND INDICATOR IAW BMM 79-32-01 & 79-32-02, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST CONFIRMED FAILURE OF OIL PRESSURE INDICATOR. FOUND LAMPS RESTING ON POINTER'S HUB STEM, POINTER WAS LOOSE & APPEARED TO HAVE MELTED OFF HUB STEM, ALSO FOUND 3 OF 4 LAMPS INOPERATIVE. REMOVED & REPLACED GASKET 4 EA. O-RING, LAMPS 4 EA. & POINTER ASSY. REPAIRED &TESTING ACCOMPLISHED IAW CMM 31-00-31, REV. 2. 2L72 4F RTA16WE 20040421001332004042100133EU 2004 4 21 AWXA200400369 120040415A2560P4010021 BATTERY AIRBUS320 A320231 3930325EU ZONE 900 - LAVATDISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28624AW 55 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040421001352004042100135NM 2004 4 21 CALA0400360 120040412A532065C33970 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717663 28924 INSPECTION FOUND A 3 INCH CRACK IN CABIN FLOOR INTERCOSTAL BETWEEN FS 344-360, BL 0. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20040421001372004042100137NM 2004 4 21 CALA0400362 120040413A53306545767 SKIN BOEING737 7373T0 1384582NM FUSLEAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 380 + 17 BELOW STRINGER 17L. THE DENT WAS REPAIRED USING A DOUBLER IAW SRM 53-00-01, FIGURE 208. 2L72 4F RTA16WE 20040421001382004042100138NM 2004 4 21 CALA0400363 120040413A532069353656 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 380-400, BL 0. REPAIRED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040421001392004042100139NM 2004 4 21 CALA0400364 120040414A53306542988 SKIN BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND LEFT FUSELAGE SKIN GOUGED AT STA 986 JUST AFT OF DRAIN MAST, S25L. THE GOUGED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 229. 2L72 4F RTA16WE 20040421001402004042100140NM 2004 4 21 CALA0400367 120040414A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 40. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040421001412004042100141NM 2004 4 21 CALA0400368 120040414A5320654580562 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND FORWARD SUPPORT ANGLE THAT ATTACHES TO FRAME CRACKED IN SEVERAL PLACES AT STA 277, S14L TO S16L. THE CRACKED SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11, FIGURE 1. 2L72 4F RTA16WE 20040421001432004042100143NM 2004 4 21 CALA0400370 120040414A532065C161216 BRACKET BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND FLOOR BRACKET (GIRT BAR TIE DOWN) CORRODED AT STA 312, LBL 52. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040421001442004042100144NM 2004 4 21 CALA0400371 120040414A532065317875 CHANNEL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND L-1 DOOR CUTOUT CHANNEL CORRODED AT STA 312-344. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040421001452004042100145NM 2004 4 21 CALA0400372 120040414A5311146N103099 FRAME BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719136 29285 INSPECTION FOUND FRAME DENTED IN TWO PLACES AT BS 1600. THE DENTS WERE LOCATED BETWEEN S25L AND S26L AND BETWEEN S23L AND S24L. THE FRAME WAS REPAIRED IAW ECRA 5311-01188. 2L72 4F RTA2NM 20040421001462004042100146NM 2004 4 21 DHL2004755009 120040409A7312 O-RING BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE OIL/FUEL LEAKING A DHLAE ENGINE SHUTDOWN M OVER TEMP CLCLIMB 1 SO01755DH 21857 700311 ON CLIMBOUT NR 1 OIL TEMPERATURE EXCEEDED 120 DEGREES. ACCOMPLISHED ABNORMAL PROCEDURES. NR 1 FUEL HEAT WOULD NOT SHUT OFF. OIL QUANTITY BEGAN TO DECREASE. ALL ABNORMALS ACCOMPLISHED. SECURED NR 1 ENGINE PEAK TEMPERATURE 155 DEGREES FOR 5 MINUTES. FOUND NR 1 ENGINE FUEL OIL COOLER INLET LINE LEAKING OIL AT B-NUT. REPLACED O-RING WITH SERVICEABLE P/N: MS9388-016. MOTORED ENGINE PER JRH 5.2. NO LEAKS NOTED PER M/M 79-20-01. NR 1 FUEL HEAT WOULD NOT SHUT OFF. REMOVED AND REPLACED FUEL DE-ICING AIR VALVE IAW B-727 M/M 73-14-11. OPERATIONAL CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040421001472004042100147NM 2004 4 21 CALA0400365 120040412A5510180A16121 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716713 28784 INSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER AND MIDDLE PINS CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421001482004042100148NM 2004 4 21 UPS04442118 120040325A53207075T60071IN DOUBLER BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, M/D BS 270 RIGHT VERTICAL I/B SUPPORT ATTACH WEB FOUND CRACKED AS MARKED AT S-26R. WEB DOUBLER REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040421001492004042100149WP 2004 4 21 UPS04842120 120040401A53403649114U FITTING DOUG DC8 DC873F 302199FWP CABIN SUBFLOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, SUBFLOOR TO WEB FITTING IS CRACKED AT STA 925 AT LBL 63. REMOVED AND REPLACED FITTING IAW DWG 3649114 AND SRM 51-3-0, 51-1-20D. 2L74 4F RT4A25 20040421001522004042100152WP 2004 4 21 UPS04842123 120040331A5512 SKIN DOUG DC8 DC873F 302199FWP RT H-STAB. CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 91.25 TO XFS103.75, XFS 135-147, XFS 216-228. BLENDED OUT CORROSION, FABRICATED AND INSTALLED 3 REPAIR DOUBLERS IAW SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20040421001542004042100154WP 2004 4 21 UPS04842125 120040406A5320 WEB DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, STATION 1190 LONG 33L UPPER WEB IS CORRODED BEYOND LIMITS, WEB BELOW C-PIT DOOR. BLENDED OUT CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 25. 2L74 4F RT4A25 20040421001552004042100155EA 2004 4 21 ASOA04217 120040316A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11835AS 7258 DURING A C-CHECK IN MCN, THE EMERGENCY FLOOR LEVEL FLOOR LIGHT COVER ON THE AFT WALL BY THE PASSENGER DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LEVEL FLOOD LIGHT ASSEMBLY ON THE AFT WALL BY THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040421001562004042100156EA 2004 4 21 ASOA04218 120040316A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11835AS 7258 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT SIGN COVER BY THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040421001582004042100158EU 2004 4 21 ASOA04216 120040316A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11637AS 383 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040421001602004042100160EA 2004 4 21 ASOA04214 120040316A5330 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR DOOR FUSELAGE SKIN RADIUS AFT AREA LHS AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR DOOR FUSELAGE SKIN RADIUS AFT AREA LHS AT FS 235 IAW ASA EO 600-53-0122. (M) 2L72 4F RTA21EA 20040421001612004042100161EA 2004 4 21 ASOA04221 120040317A521060031535 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SEAL DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11881AS 7496 FLT 4499 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO LATCH. UPON INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SEAL STRIKER DAMAGED AND REPAIRED IT IAW REO 601R-52-11-008. MAINTENANCE ALSO LUBRICATED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040421001652004042100165NM 2004 4 21 GAIA04053OP 120040318A2612 FIRE LOOP BOEING727 727251 138408HNM NR 3 ENGINE SHORTED A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07279US 21158 FLT 602 - TOL-FWA - DURING CRUISE, NR 3 ENGINE FIRE PROTECTION GROUND FAULT LIGHT ILLUMINATED. FOUND SAFETY WIRE GROUNDING ON LOOP, REPOSTIIONED WIRE. NR 3 GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040421001662004042100166NM 2004 4 21 GAIA04048OP 120040310A2611100064901 SMOKE DETECTOR BOEING727 727223 1384074NM AFT LWR CARGO INOPERATIVE A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW076827 20180 LOWER CARGO FIRE WARNING ILLUMINATED SHORTLY AFTER TAKEOFF, RETURNED TO FWA. LIGHT WENT OUT BEFORE LANDING. BITE TEST CARRIED OUT. FOUND THREE SMOKE DETECTORS WEAK IN THE AFT CARGO. REMOVED AND REPLACED THREE WEAK SMOKE DETECTORS, RESET THE SYSTEM. OPS CHECK ON GROUND FOUND NORMAL ON FORWARD AND AFT LOWER CARGO. (M) 2L73 4F A3WE 20040421001672004042100167NM 2004 4 21 GAIA04050OP 120040317A2797 CONNECTOR BOEING727 727251 138408HNM LT WING DIRTY A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07252US 19971 AFTER TAKEOFF, THE NR 3 LEADING EDGE DEVICE DID NOT RETRACT ON FLAP RETRACTION. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. CLEANED CONNECTOR ON NR 3 LEADING EDGE DEVICE ACTUATOR. RAN FLAPS SYSTEM, OPS CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040421001682004042100168NM 2004 4 21 GAIA04047OP 120040309A2701 CONTROL COLUMN BOEING727 727224 1384076NM COCKPIT BINDING A GAIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW0779748 22450 DURING CRUISE FLIGHT, A BINDING OF THE CONTROL YOKE WAS NOTED IN A ROLL TO THE RIGHT. SPOILERS WERE CYCLED AND ABOVE PROBLEM WAS CORRECTED BUT LATER DID RETURN. FLT WAS COMPLETED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND CHECK FLIGHT CONTROLS AILERON AND SPEED BRAKE SYSTEM. LUBED AND OPS CHECK SYSTEM. COULD NOT DUPLICATE ON GROUND. OPS CHECKS GOOD ON GROUND. (M) 2L73 4F A3WE 20040421001692004042100169EU 2004 4 21 USAABA04004 120040303A274147148122 ACTUATOR AIRBUS330 A330323 3930335EU PITCH TRIM FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19677UW 0380 CREW REPORTED THAT THE AIRCRAFT PITCHED NOSE UP WITH EITHER AUTOPILOT ENGATED. FLIGHT RETURNED TO LGW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PITCH TRIM ACTUATOR. (M) 2L72 4F RTA46NM 20040421001702004042100170NM 2004 4 21 USAASB04033 120040318A3260 WARNING LIGHT BOEING737 737301 1384611NM MLG ILLUMINATED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19576US 23741 ON CLIMB-OUT FROM PHL, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M) 2L72 4F RTA16WE 20040421001712004042100171EU 2004 4 21 ASOA04224 120040319A3350 CIRCUIT BREAKER AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHTSTRIPPED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11530AS 453 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS REMAINED ON IN THE ARMED POSITION. MAINTENANCE RESET CIRCUIT BREAKER K-26. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040421001722004042100172NM 2004 4 21 GAIA04052OP 120040318A2797 CONNECTOR BOEING727 727243 138408DNM LT WING FLAPS DIRTY A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW071269Y 21269 ON TAKEOFF ROLL, AFTER FLAP RETRACTION THE NR 4 LEADING EDGE DEVICE INDICATED IN TRANSIT. NO ROLL WAS NOTED, THE AIRCARFT CONTINUED FLIGHT. CLEANED THE NR 4 LEADING EDGE FLAP SWITCH. RAN FLAPS SYSTEM OPS CHECKED NORMAL, THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040422000012004042200001EA 2004 4 22 ASOA04188 120040309A3260895001 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA MLG MISALIGNED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11723EV 10132 FLT 9950 - DURING CLIMB-OUT AFTER TAKEOFF FROM DFW-JFK, THE CREW SELECTED GEAR UP AND RECEIVED GEAR DISAGREE, NOSE STEERING INOPERATIVE AND WEIGHT ON WHEELS INPUT CAUTION MESSAGES. THE CREW COMPLIED WITH POH PROCEDURES AND DECLARED AND EMERGENCY. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE ADJUSTED BOTH NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSORS. OPS CHECKS GOOD. AIRCARFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000042004042200004EA 2004 4 22 ASOA04195 120040311A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040422000052004042200005EA 2004 4 22 ASOA04190 120040310A3350BM1006002 LIGHT CNDAIRCL600 CL6002B19 1900309EA LT OVERWING INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE LEFT OVERWING MIDDLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE LEFT OVERWING MIDDLE EMERGENCY LIGHT LAMP SOCKET. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20040422000062004042200006EU 2004 4 22 ASOA04194 120040311A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040422000072004042200007EA 2004 4 22 ASOA04192 120040310A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11900EV 7608 FLT 4512 - DURING A GROUND INSPECTIN IN BTR, THE EXTERIOR RIGHT MIDDLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR RIGHT MIDDLE EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000082004042200008EA 2004 4 22 ASOA04193 120040310A3350BF10044004 FIXTURE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURNG AN A-CHECK IN BTR, THE PASSENGER DOOR EMERGENCY EXIT LIGHT FIXTURE NEAR THE FLIGHT ATTENDANTS STATION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY EXIT LIGHT ASSEMBLY NEAR THE FLIGHT ATTENDANTS STATION. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000102004042200010EA 2004 4 22 ASOA04189 120040309A3350BC50334903 FIXTURE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11723EV 10132 DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHT AT FS 690 WAS FOUND NOT TO ILLUMINATE. MAINTENANCE CLEANED CORROSION INHIBITOR FROM UNDER THE LAMP GROUND LUG. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000112004042200011EA 2004 4 22 ASOA04204 120040312A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. (M) 2L72 4F RTA21EA 20040422000122004042200012EA 2004 4 22 ASOA04199 120040311A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURINGA C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040422000132004042200013EA 2004 4 22 ASOA04198 120040311A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA RT OVERWING INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11825AS 7207 DURING A GROUND INSPECTION FOLLOWING A ROUTINE OVERNIGHT IN DFW, THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD OVERWING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000142004042200014NE 2004 4 22 ASOA04209 220040314A7261 OIL CAP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE UNSECURE A ASOAO OTHER WKJINADEQUATE Q C FLUID LOSS WARNING INDICATION DEDESCENT 1 SO11533AS 460 127040 DURING DESCENT INITIATION INTO AGS FROM ATL, THE CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATING ALONG WITH THE CREW ALERT PANEL AND LOCAL ALERTS BEING NOTED. THE LOW OIL PRESSURE CHECKLIST WAS COMPLIED WITH AND TORQUE REDUCED ON THE LEFT ENGINE WHICH WAS FOLLOWED BY A DROP IN THE OIL PRESSURE BELOW 40 PSI. THE CREW THEN SHUT DOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN AGS. MAINTENANCE FOUND THE OIL CAP ON THE LEFT ENGINE UNSECURED, CLEANED AND SERVICED THE ENGINE WITH OIL AS PER ATR JIC 12-00-00. MAINTENANCE GROUND RAN THE LEFT ENGINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20040422000192004042200019EA 2004 4 22 ASOA04202 120040312A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE CLIPS AT THE AFT EQUIPMENT BAY BELOW THE ENGINE BEAM ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT THE AFT EQUIPMENT BAY BELOW THE ENGINE BEAM ON THE LEFT AND RIGHT SIDES IAW SRM 53-42-02. (M) 2L72 4F RTA21EA 20040422000212004042200021WP 2004 4 22 ASAA0480016 120040119A532199365501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAS CRACKED INSERT AT FS 196-256. REPLACED CHANNEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000232004042200023WP 2004 4 22 ASAA0480058 120040130A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 DURING 15K CHECK, FOUND LEFT INBOARD SEAT TRACK IS CORRODED AT FS 1098-1165. REPLACED SEAT TRACK PER SRM 51-10-4 AND 51-30-5. (M) 2L72 4F RTA6WE 20040422000242004042200024WP 2004 4 22 ASAA0480061 120040130A53133936474501 SPLICE DOUG DC9 DC983 3022083WP LONGERON CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND LONGERON SPLICE AT L1 AT FS 750-769 IS CORRODED. REPLACED SPLICE PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040422000252004042200025WP 2004 4 22 ASAA0480037 120040126A53219936584501 FLOORBOARD DOUG DC9 DC983 3022083WP FS DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 DURING INSPECTION FOUND FLOORBOARD STATION 769 TO 826, LBL 22-44 HAS SEVERAL AREAS OF EDGE DAMAGE. REPAIRED BY FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040422000302004042200030WP 2004 4 22 ASAA0480032 120040126A533059114003 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 DURING INSPECTION, FOUND SKIN CRACKED AT FORWARD HINGE RIGHT AFT NOSE GEAR DOOR EMINATING FROM RIVET HOLE FORWARD OF FORWARD HINGE CUTOUT. REPAIRED IAW SRM 51-10-2, 51-10-4 AND 51-30-2. (M) 2L72 4F RTA6WE 20040422000332004042200033SO 2004 4 22 SWIA200413120 120040317A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07234SW 120308 FRAME 36 RIGHT SIDE FLOOR STRAP CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME AT RIGHT SIDE FLOOR STRAP IAW SRM 120 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20040422000352004042200035SO 2004 4 22 SWIA200413142 120040415A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT FAULTY A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07197SW77 77 120186 IN CRUISE FLIGHT, FLAP ADV SWS, AND CONTROL FAULT LIGHTS ILLUMINATED. RESET THE SYSTEM PER QRH, 5 MINUTES LATER, FLAP ADV SWS, CONTROL FAULT, ASYMMETRY, AND FLAP DISAGREEMENT ALL ILLUMINATED. ALSO HAD ERRATIC READINGS ON FLAP INDICATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW EMB MM 27-50-05. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040422000382004042200038NM 2004 4 22 UPS04442215 120040329A575365B078791 RIB BOEING747 747121 1384871NM NR 8 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP I/B ARM I/B RIB ROTARY ACTUATOR NR 2, 8 MOUNTING BOLT HOLES CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 878 I/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH AND NR 8 MOUNTING BOLT HOLE OVERSIZED TO 0.371 INCH, BUSHINGS FABRICATED & INSTALLED. 2L74 4F A20WE 20040422000392004042200039NM 2004 4 22 UPS04442216 120040329A575365B078761 RIB BOEING747 747121 1384871NM NR 8 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP O/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 928 O/B ARM I/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH, BUSHINGS FABRICATED & INSTALLED. 2L74 4F A20WE 20040422000422004042200042WP 2004 4 22 ASAA0480055 120040130A533059530501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND FUSELAGE SKIN IS GOUGED AT STATION 235. REMOVED DAMAGED SECTION. REPAIRED WITH FILLER AND DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040422000472004042200047WP 2004 4 22 ASAA0480013 120040119A53219932816501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL CRACKED IN HAT CHANNELS AT FS 796-826. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000502004042200050WP 2004 4 22 ASAA0480014 120040119A532199579181 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL CRACKED AT FS 617-693. REPLACED CHANNEL PER SRM 51-10-4 AND 51-10-3. (M) 2L72 4F RTA6WE 20040422000532004042200053WP 2004 4 22 ASAA0480010 120040119A53219936639501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL SURFACE IS SHREDDING. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000552004042200055WP 2004 4 22 ASAA0480011 120040119A53219936639501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL CORNER IS CRACKED AT FS 886-927. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000562004042200056NM 2004 4 22 UPS04442233 120040329A575365B106251 RIB BOEING747 747121 1384871NM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 4 VC FLAP I/B RIB ROTARY ACTUATOR NR 3 & 4 MOUNTING BOLT HOLES CORRODED (LOOKS O/B COUNTS CLOCKWISE FROM TOP). LEFT WING NR 4 VC FLAP OLES 1277 I/B RIB ROTARY ACTUATOR NR 3 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH AND NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.371 INCH BUSHINGS FABRICATED & INSTALLED. 2L74 4F A20WE 20040422000572004042200057WP 2004 4 22 ASAA0480012 120040119A53219936640501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC 0 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL SURFACE IS DISBONDED AT FS 864-886. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000592004042200059WP 2004 4 22 ASAA0480039 120040126A53119919605501 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING INSPECTION, FOUND CORROSION ON AFT SIDE OF FRAME AT STATION 1271 AND LONGERON 30. REPAIRED BY REMOVING DAMAGE. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW MD80 SRM 53-03. (M) 2L72 4F RTA6WE 20040422000602004042200060WP 2004 4 22 UPS04842225 120040401A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 1746 LONG 15R IS CRACKED. CUT OUT DAMAGED LONGERON SECTION BETWEEN STATION 1736-1760, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED LONG SPLICE REPAIR IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040422000612004042200061WP 2004 4 22 ASAA0480007 120040119A53219936688503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 807-826. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000632004042200063WP 2004 4 22 UPS04842226 120040402A5320561214815 BRACKET DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 CIRCUMFERENTIAL TIE BRACKET IS CRACKED AT LONG 3L AND 3R AT APPROX STATION 1790. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 5612148 AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20040422000642004042200064WP 2004 4 22 ASAA0480035 120040126A5320593666065 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT ANGLE EXFOLIATED STATION 1212 BETWEEN 28R AND 27R. REPAIRED BY REMOVING DAMAGED SUPPORT AND INSTALLED NEW SUPPORT IAW MD80 SRM 51-30-4. (M) 2L72 4F RTA6WE 20040422000662004042200066WP 2004 4 22 UPS04842227 120040401A5320577270625 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 1766 LEFT SIDE THE LOWER ATTACH ANGLE AT UPPER CANTED BULKHEAD IS CRACKED BETWEEN LONGERON 9L AND 10L. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 5772706 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040422000672004042200067WP 2004 4 22 ASAA0480008 120040119A53219936651515 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS CORRODED AT FS 1003-1079. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000682004042200068WP 2004 4 22 UPS04842228 120040401A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 1734 LONG 15L IS CRACKED. CUT OUT DAMAGE LONGERON BETWEEN STATION 1710 TO 1760, FABRICATED AND INSTALLED LONGERON, STRAPS AND SPLICE FITTINGS IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040422000692004042200069WP 2004 4 22 ASAA0480009 120040119A532099525212 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL HAT CHANNEL IS CHAFED. REPLACED FLOOR PANEL HAT CHANNEL PER SRM 51-30-2, 51-10-4, AND 51-10-3. (M) 2L72 4F RTA6WE 20040422000712004042200071WP 2004 4 22 UPS04842229 120040402A532037584972N ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1140 AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D. 2L74 4F RT4A25 20040422000722004042200072WP 2004 4 22 UPS04842230 120040402A53204758514520N ATTACH FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1150 AT LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 4758514 AND SRM 51-1-20D. 2L74 4F RT4A25 20040422000732004042200073WP 2004 4 22 ASAA0480057 120040130A550059304973 TAB DOUG DC9 DC983 3022083WP ANTIFLOAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT ANTI-FLOAT TAB UPPER SURFACE IS DENTED. APPLIED FILLER PER SRM 55-04. (M) 2L72 4F RTA6WE 20040422000752004042200075WP 2004 4 22 ASAA0480059 120040130A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND WEB IS CORRODED AT LONGERON 18L NEAR L2 DOOR. REMOVED CORROSION. INSTALLED FILLER AND DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20040422000802004042200080CE 2004 4 22 CLS2004F00000 120040326A2910CM3690C60100 HOSE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO HYD SYSTEM LEAKING B CSLRK NONE K FLUID LOSS ININSP/MAINT 1 CE01678JS 414A0090 DURING 100 HOUR, INSPECTION FOUND LT MAIN LANDING GEAR HYDRAULIC ACTUATOR HOSE LEAKING HOSE WAS HARD AND NOT FLEXIBLE HOSE TAG SHOWS MFG DATE 3Q77 AND APPEARS TO BE ORIGNAL HOSE INSTALLED. AC MFG DATE 1978 WITH 7221.9 HOURS TT. RECOMMEND TO REPLACE FLEX HOSES EVERY 5 YEARS OR ON CONDITION. 1L72 3O3 O A7CE E8CE 20040422000822004042200082SO 2004 4 22 SWIA200413125 120040408A27223081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER FAILED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07289YV8116 7846 120289 DURING CLIMBOUT OF SEA, THE RIGHT RUDDER PEDAL TRAVEL WAS RESTRICTED TO ABOUT 2-4 INCHES THEN JAMMED AND WOULD NOT TRAVEL ANY FURTHER. A/C WAS ABOVE 120 KNTS ACCELERATING TO 180 KNTS. CONDUCTED RUDDER HEALTH CHECK IAW 27-22-00. TOP (BLUE) ACTUATOR FAILS. BOTTOM (GREEN) ACTUATOR CHECKS GOOD. REMOVED AND REPLACED TOP BLUE ACTUATOR. CONDUCTED HEALTH CHECK, PASSED. CONDUCTED LEAK AND RUDDER OPERATION CHECKS, GOOD IAW EMB120 MM 27-22-00. 2L72 4T RTA31SO 20040422000832004042200083SO 2004 4 22 SWIA200413126 120040408A213032144143 SHUTOFF VALVE EMB 120 EMB120ER 3260203SO A/C BAY STUCK A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07270YV 120270 APU BLEED OPEN, CROSSBLEED OPEN, LEFT PAC -LOW-, RIGHT PAC -OFF-, THE CABIN FILLED WITH SMOKE. FOUND RIGHT PACK PRESSURE SHUTOFF, VALVE STUCK OPEN ALLOWING CONTINUOUS AIRFLOW TO INOP PACK. REMOVED AND REPLACED VALVE IAW 21-50-01. OPS CHECKS GOOD. S/N OFF: 892. 2L72 4T RTA31SO 20040422000882004042200088WP 2004 4 22 UPS04842188 120040303A5330561386253 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 INNER DOUBLER FOR BELLY SKIN FOUND TO HAVE PREVIOUS DAMAGE (CUT) AT APPROX STA 22 L31L-33L. REMOVED SPLICE DOUBLER. FABRICATED -53 SPLICE DOUBLER IAW DAC DWG 5613 862. INSTALLED IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-1. 2L74 4F RT4A25 20040422000972004042200097 2004 4 22 UPS04M42210 420040418A2565 SWITCH DOUG MD11 MD11F 3023600NM R1 DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP INSPECTION TYPE:N/A R-1 DOOR ESCAPE SLIDE BATTERY PACK LT PUSH TO TEST SWITCH LT INOP. RELAMPED, NO HELP (BAD SWITCH). FOUND IND LAMP HOUSING BASE BROKEN FROM HOUSING. REPLACED DOOR SLIDE IND IN REF TO MD11 WDM 25-61-01. LIGHT TESTS NORMAL. 2L73 4F RTA22WE 20040422000982004042200098SO 2004 4 22 LR7A04034 120040408A5320 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 384 4606 DURING A-CHECK FOUND LEFT AFT VERTICAL BEAM CRACKED APPROX .4375 INCH AT FS 588 LT WL 198, LBL 67.5. REPAIRED LT AFT VERTICAL BEAM PER MEA NO 382-53-04-037 (SMP583 FIG 53-40-19). 2H74 4T A1SO 20040420002162004042000216NM 2004 4 20 CALA0400374 120040415A53206936656 SHEAR WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND A .5 INCH CRACK IN AFT CABIN SHEAR WEB AT STA 927-947.5, BL 0. A REPAIR WAS INSTALLED IAW BOEING DRAWING 69-36656. 2L72 4F RTA16WE 20040420002182004042000218NM 2004 4 20 CALA0400375 120040415A532065176884165 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 INSPECTION FOUND L-1 DOOR Z-ANGLE AT LOWER SILL CORRODED, STA 294-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040420002262004042000226EU 2004 4 20 CCHA093688 120040301A2422SPC10HD INVERTER UROCOPEC135 EC135T1 5620026EU NR 2 AC INTERMITTENT E O OTHER S AFFECT SYSTEMS NRNOT REPORTED 1 SO19911CK1776 0138 NR 2 AC INVERTER INTERMITTENT OPERATION. REPLACED AC INVERTER WITH NEW S/N 561. 1G72 3U H88EU 20040420002272004042000227NM 2004 4 20 04FDEA00965 120040414A5753 FITTING DOUG MD11 MD11 3023602NM T/E FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING OUTBOARD FLAP VANE T-FITTING (SECOND FROM INBOARD SIDE) FOUND WITH HOLES CORRODED. TEE FITTING (SECOND FROM INBOARD SIDE) REPAIRED AS PER EA 1-5750-76008. 2L73 4F RTA22WE 20040420002312004042000231EU 2004 4 20 BAQA092596 120040309A2741L309ABM2 ACTUATOR BOLKMSBK117 BK117C1 5626025EU FEEL AND TRIM FAILED B BAQAK NONE L NO TEST ININSP/MAINT 1 EA03117UP3241 7508 BENCH TEST FOR SERVICEABILITY. REPLACED WITH SERVICABLE UNIT. 1G72 3U NCH13EU 20040421000032004042100003SW 2004 4 21 HEEA094158 120040401A2435200SGL124Q STARTER GEN BELL 230 230 1182149SW ALLSN 250C 250C30 03013GL NR 2 FAILED B HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW03911RC2260 23037 DURING CRUISE FLIGHT, NR 2 DC GENERATOR LIGHT ILLUMINATED. PILOT FOLLOWED AIRCRAFT EMERGENCY CHECKLIST FOR SINGLE DC GENERATOR FAILURE AND LANDED AIRCRAFT. MAINTENANCE REPLACED NR 2 STARTER GENERATOR. 1G72 3U3 UNCH9SW E1GL 20040421000142004042100014 2004 4 21 BAQA094139 420040413A3160L316M30C1003 CDU UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE DISPLAY ERRATIC B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME 0009 DISPLAY SCREEN ON CDU IS ERRATIC (FLICKERING, LIGHT TO DARK, ON AND OFF). REPLACED WITH SERVICABLE UNIT, 04/13/2004. 1G72 3U3 UO H88EU E42NE 20040421000202004042100020NM 2004 4 21 UPS04442134 120040325A5320 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, M/D-CTR SECTION FLOOR SUPPORT WEB LWR CHORD FOUND CORROSION AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.055 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS. CHORD REPAIRED REFER SRM 51-40-04 FIG 3 CIC APPLIED IAW EO M-5100-2780E. 2L74 4F A20WE 20040421000562004042100056WP 2004 4 21 UPS04842182 120040311A53403779659501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE: C1, LONGERON 6L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING, LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM DC8 20-14-00. 2L74 4F RT4A25 20040421000612004042100061NM 2004 4 21 CALA0400380 120040415A5510180A16121 PIN BOEING737 737724 13844BYNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723721 28940 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER PIN CORRODED. THE PIN WAS REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421000622004042100062NM 2004 4 21 CALA0400381 120040415A5510180A16122 PIN BOEING737 737724 13844BYNM RT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723721 28940 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER REAR SPAR MIDDLE AND LOWER PINS CORRODED. THE PINS WERE REMOVED AND REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421000662004042100066NM 2004 4 21 04FDEA00985 120040416A5420 BRACKET BOEING727 727200 138407ENM NR 2 NACELLE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 NR 2 ENG RIGHT AFT COWL OVERBOARD DRAIN SUPPORT BRACKET & RIVET CHAFED. FABRICATED NEW SUPPORT BRACKET USING 2024-T3 .050C BATCH 742514 AND INSTALLED IAW SRM 51-30-2 AT MAE. 2L73 4F RTA3WE 20040421000672004042100067NM 2004 4 21 04FDEA00986 120040417A5410 SUPPORT BOEING727 727200 138407ENM NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 NR 2 RIGHT AFT COWL ENGINE DRAIN LINE SUPPORT CRACKED. FABRICATED DRAIN LINE SUPPORT FROM 2024-T3 .032C BATCH 715298 AND INSTALLED IAW SRM 51-30-2 AT MAE. 2L73 4F RTA3WE 20040421000702004042100070NM 2004 4 21 CALA0400383 120040417A5312149A761115 PRESSURE PANEL BOEING737 737824 13844BZNM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 OUTBOARD WEB CRACKED (3 INCH) LEFT HAND WHEEL WELL. REMOVED AND REPLACED WEB PER SRM 51-40-02. 2L72 4F RTA16WE 20040421000722004042100072NM 2004 4 21 CALA0400385 120040416A53306545767 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 DENT IN LEFT SIDE OF FUSELAGE AT BS 380 + 15 BELOW S-16LT. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED, INSTALLED REPAIR PER SRM 53-00-01 FIG 208. 2L72 4F RTA16WE 20040421000842004042100084NM 2004 4 21 AWXA200400374 120040404A53306545774575 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AFT OF EXTERIOR EMERGENCY EXIT LIGHT BS 727, STR 23 RIGHT. MAINTENANCE CUTOUT DAMAGED SKIN AT BS 727, STR 23 RIGHT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SKIN SECTION AND FORWARD & AFT FILLERS, DOUBLERS & TRIPLERS; INSTALLED REPAIR PARTS IAW DWG AW5361001. 2L72 4F RTA16WE 20040421001022004042100102NM 2004 4 21 04FDEA00999 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT I/B FLAP VANE O/B VANE SUPPORT ASSY FITTING FOUND HOLES WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. FOUND OUT OF LIMIT. SUPPORT FITTING REPLACED AS PER EO 1-5750-7-5005. 2L73 4F RTA22WE 20040421001052004042100105EA 2004 4 21 COMA0460253 120040410A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OPEN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01713CA 7245 FLIGHT 5219 CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND DOOR HANDLE IN OPEN POSITION. OPERATIONAL CHECK OF DOOR LATCH MECH WAS NORMAL. 2L72 4F RTA21EA 20040421001062004042100106EA 2004 4 21 COMA0460254 120040410A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01917CA 7017 FLIGHT 5719 GEAR DISAGREE WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE. GEAR RETRACTION CHECKS NORMAL. 2L72 4F RTA21EA 20040421001072004042100107NM 2004 4 21 04FDEA00784 120040401A53131D0542T LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FWD CARGO - EXFOLIATION CORROSION FOUND AT STA Y= 1019 LONGERON 46R. FWD CARGO - STA Y= 1019 LONGERON 46R REPAIRED AS PER SRM 53-10-00 VOL I. 2L73 4F RTA22WE 20040421001252004042100125WP 2004 4 21 04FDEA001008 120040419A5711ARB0007501 SPAR CAP DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 COMPLY WITH FEDEX EA 8-5710-77344 WINGS BASIC LT WINGS, LOWER AFT SPAR CAP REPAIR. COMPLIED WITH EA 8-5710-77344 WINGS BASIC LT WING, LOWER AFT SPAR CAP REPAIR. 2L73 4F RTA22WE 20040421001272004042100127NM 2004 4 21 04FDEA00954 120040414A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP O/B HINGE SIDE BRACE ATTACHMENT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040421001282004042100128NM 2004 4 21 04FDEA00955 120040414A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP O/B HINGE LOWER MOUNT MATING SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040421001342004042100134NM 2004 4 21 04FDEA00959 120040414A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION (C53-111-01) AFT CARGO BAY, FLOORBEAM HAS CORROSION LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29. *S/D* CORROSION ON AFT CARGO BAY FLOORBEAM LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29 FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR ANGLES AND FILLER ON LWR FLANGE BS 1148, WL 200, LBL 20 TO LBL 29 IAW SRM 53-10-8. 2L73 4F RTA3WE 20040421001422004042100142NM 2004 4 21 CALA0400369 120040414A532065C161215 BRACKET BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND FLOOR BRACKET (GIRT BAR LATCH TIE DOWN) AT STA 344, LBL 54 CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040421001512004042100151WP 2004 4 21 UPS04842122 120040331A5512 SKIN DOUG DC8 DC873F 302199FWP LEFT H-STAB. CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 LEFT HORIZONTAL STAB L/E UPPER SURFACE IS CORRODED BEYOND LIMITS XFS 153.75 TO XFS 161. BLENDED OUT CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20040421001532004042100153WP 2004 4 21 UPS04842124 120040402A5311 FRAME DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, STATION 1040 FRAME IS CORRODED AT LONG 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010. 2L74 4F RT4A25 20040421001572004042100157EU 2004 4 21 ASOA04222 120040318A33503011210 LIGHT AEROSPATR72 ATR72 EU FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11643AS 413 DURNG AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CEHCKS GOOD. AIRCARFT OK FOR SERVICE. (M) 2H72 4T RT 20040421001592004042100159EU 2004 4 21 ASOA04215 120040316A3350LP1670 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11637AS 383 DURING AN A-CHECK IN MCN, THE NEXT TO LAST EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NEXT TO LAST EMERGENCY FLOOR LIGHT STRIP LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040422000172004042200017EA 2004 4 22 ASOA04203 120040311A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING AN A-CHECK IN BTR, THE FS 640, FS 640 DOUBLER AND SKIN BUTT JOINT STRAP ON THE RIGHT SIDE AT STRINGER 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 640, FS 640 DOUBLER AND REPAIRING THE SKIN BUTT STRAP ON THE RIGHT SIDE AT STRINGER 9 IAW ASA EO 600-53-0107. (M) 2L72 4F RTA21EA 20040422000282004042200028WP 2004 4 22 ASAA0480073 120040215A53505961568501 RELEASE MECH DOUG DC9 DC983 3022083WP TAILCONE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 DURING HV1 CHECK, FOUND TAILCONE RELEASE MECHANISM BROKEN. REPLACED MECHANISM PER MM 53-53-02. (M) 2L72 4F RTA6WE 20040422000372004042200037NM 2004 4 22 UPS04442214 120040329A575365B078781 RIB BOEING747 747121 1384871NM NR 8 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP I/B ARM O/B RIB ROTARY ACTUATOR NR 4 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP HOLES 888 I/B ARM O/B RIB ROTARY ACTUATOR NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.328 INCH AS PER SRM 57-20-03 FIG 6 & NDT CHECKED NO CORROSION FOUND, REPAIR WITHIN SRM 57-20-03 FIG 6 LIMIT. 2L74 4F A20WE 20040422000452004042200045WP 2004 4 22 ASAA0480062 120040130A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND RIGHT INBOARD SEAT TRACK IS CORRODED AT FS 200-247. REPLACED SEAT TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000462004042200046WP 2004 4 22 ASAA0480005 120040119A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FS DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 826-864. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000512004042200051NM 2004 4 22 UPS04442222 120040420A53471A0970108766103 SEAT TRACK BOEING747 747256B 1384865NM FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 FIRST OFFICERS RIGHT AFT SEAT TRACK BROKEN. APPX 9 INCHES FROM AFT EDGE OF TRAVEL REMOVED FO'S SEAT FWD STOPS PB 77490 R/R FO'S SEAT TRACK PER MM 25-11-01. OPS CHECKS GOOD. OK FOR CONTINTED. SERVICE. 2L74 4F RTA20WE 20040422000542004042200054NM 2004 4 22 UPS04442232 120040329A575365B106211 RIB BOEING747 747121 1384871NM NR 5 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 5 VC FLAP I/B RIB ROTARY ACTUATOR NR 3 & 4 MOUNTING BOLT HOLES CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 5 VC FLAP OLES 1205 I/B RIB ROTARY ACTUATOR NR 3 MOUNTING BOLT HOLE OVERSIZED TO 0.341 INCH & WITHIN SRM 57-20-03 FIG 6 LIMITS. NR 4 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH BUSHING FABRICATED & INSTALLED. 2L74 4F A20WE 20040422000772004042200077CE 2004 4 22 FCPR200400012 120040326A28231013890255 SHUTOFF VALVE BEECH 90 C90A 1152911CE PWA PT6 PT6* 52043EA FUEL SYSTEM STUCK B FCPRO OTHER O OTHER NRNOT REPORTED 1 NM093263C1479 LJ1432 DURING TRAINING, PILOT CLOSED THE RT FIREWALL SHUTOFF VALVE AND WAS UNABLE TO OPEN IT. VALVE STUCK IN CLOSED POSITION. REPLACED VALVE, SYSTEM FUNCTION CHECK WAS NORMAL. (NM09200408137) 1L72 3T3 TRT3A20 E2NE 20040422000782004042200078 2004 4 22 SWIA200413122 420040404A22116229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AUTOPILOT SYS FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07924SW 7681 AT 28,000 FT MACH TRIM STAB TRIM CAUTIONS ON EICAS. UNABLE TO RESET. REMOVED AND REPLACED FCC CARD NR 2 WITH A SERVICEABLE UNIT IAW 22-10-00. OPS CHECKS GOOD. ALSO REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT ALONG WITH STAB TRIM/MACH TRIM ENGAGEMENT SWITCH PANEL ASSY IAW 27-40-00. OPS CHECKS GOOD. HSTCU P/N: 7060-9, S/N OFF: 1077. 2L72 4F4 FRTA21EA E15NE 20040422000792004042200079CE 2004 4 22 ABO2004F00000 120040303A5740501200734 FITTING BEECH 100 A100 1152915CE PWA PT6 PT6A60A 52043NE SPAR CRACKED E ABOAK NONE O OTHER ININSP/MAINT 1 GL1514CF 12665 B209 WHILE PERFORMING ROUTINE 36 MONTH/1000 HOUR WING BOLT INSPECTION, A CRACK WAS DISCOVERED USING DYE PENETRANT INSPECTION METHOD. THE CRACK WENT FROM WING BOLT HOLE, THROUGH THE RADIUS UP TO THE FITTING (FLAT AREA). 1L72 3T4 T A14CE E4EA 20040422000862004042200086WP 2004 4 22 UPS04842185 120040301A53472772660 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 CABIN STA 650 SEAT TRACK PITTED LBL 60. REMOVED CORRODED IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-3. ROUTED OUT DAMAGED IAW UPS DC8 SRM 53-2-3. LOCATED AND DRILLED HOLES IN SEAT TRACK TO LOCATE PLUG AND CHANNEL IAW UPS DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3 -0. 2L74 4F RT4A25 20040422000872004042200087WP 2004 4 22 UPS04842186 120040301A5330561386215N1 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 REMOVE AND REPLACE FWD LOWER SKIN AT STA 825, L36 IAW UPS EO DC8-5330- 8942. REMOVED AFT SECTION OF SKIN IAW UPS EO DC8-5330-8942. FABBED NEW -93 & -94 DOUBLERS AND FABBED -1 RT & LT DOUBLER IAW DAC DWG 5612627. ALODINED & PRIMED IAW DC8 SRM 51-1-8; CUT OUT SKIN, LOC & DRILL AND INSTALLED BELLY SKIN, -93, -94 DOUBLERS & -1 RT & LT SPLICE DOUBLERS ALL IAW UPS EO DC8-5330-8942, DC8 SRM 51-1-20D, 51-1-21, 51-3-0, 51-3-1. 2L74 4F RT4A25 20040422000932004042200093WP 2004 4 22 UPS04842197 120040327A53134615293 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AT APPROX STA 20, L34R CRACKED AT LOWER RADIUS. FAB, LONGERON LOCATED, DRILLED AND DEBURRED, ALODINED AND PRIMED NEW LONGERON IAW DC8 SRM 51-1-24, 51-1-8, AND DAC DWG 4615293. 2L74 4F RT4A25 20040422001002004042200100WP 2004 4 22 UPS04842143 120040225A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT PIT BETWEEN STA 1100 AND 1120 APPROX AT STR 33R INTERCOSTAL HAS CORROSION AROUND NUT PLATES. REMOVED CORROSION IAW DC8 SRM 51-1-8, ORIG THICKNESS .090, REMAINING THICKNESS .030. REMOVED INTERCOSTAL INQ DC8 SRM 51-1-20D. FABRICATED INTERCOSTAL IAW DAC DWG 9754949, ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-21 & 21-1-20D. 2L74 4F RT4A25 20040422001012004042200101WP 2004 4 22 UPS04842144 120040226A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1160 AT L33R INSIDE CROSS SLIDE DOOR TORQUE BOX BANANA FITTING IS CRACKED. REMOVED CORSS SLIDE DOOR TRACK TO FOM IAW DC8 SRM 51-3-0. REMOVED BANANA FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. REC'D LOCATED, AND DRILLED UP FITTING 3755847-2 IAW DC8 SRM 51-1-24, INSTALLED FITTING AND CROSS SLIDE DOOR TRACK IAW DC8 SRM 51-3-0 AND 51-1-20D. 2L74 4F RT4A25 20040422001022004042200102WP 2004 4 22 UPS04842145 120040226A532057519451 ATTACH ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 980 BULKHEAD LWR ATTACH ANGLE CRACKED ABOVE LONG 36. REMOVED ANGLE IAW DC8 SRM 51-1-20D & 51-3-0. REMOVED & REINSTALLED INTERCOSTAL STA 1000-980, 2 GUSSET AND 2 CLIPS, ATTACH ANGLE EXT FUSELAGE IAW DC8 SRM 51-1-20D, 51-1-21 & 51-3-0. REC'D, LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW DC8 SRM 51-1-20D, 51-3-0, AND 51-1-21. 2L74 4F RT4A25 20040422001032004042200103WP 2004 4 22 UPS04842146 120040226A53203755841501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1180 AT L33R Z-FITTING AND DOUBLER IS CRACKED. REMOVED Z-FITTING IAW DC8 SRM 51-1-20D, REC'D, LOCATED, AND DRILLED UP FITTING, REPAIR ANGLES, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 26. 2L74 4F RT4A25 20040422001062004042200106WP 2004 4 22 UPS04842150 120040226A53203750727519 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 KEELBEAM FS 856 (AS SEEN FROM LT ANTENNA PNL AREA) FITTING HAS VERTICAL CRACK IN RADIUS. REMOVED CRACKED FITTING, INSTALLED NEW FITTING, LOCATED DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20 AND 51-3-1. LEAK CHECK TO BE ACCOMPLISHED ON UPS TC 8000, ITEM 14. INSTALLED HYD LINES IAW DC8 MM 20-12-01. LEAK CHECK GOOD IAW DC8 MM 20-12-01. 2L74 4F RT4A25 20040422001072004042200107WP 2004 4 22 UPS04842151 120040227A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AIR COND COMPT FS 24-36 L24R IS CORRODED. REMOVED CORROSION FROM L24R IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2- 0; MAT ID 2597242-3 LONGERON PO 439263.1. LOCATED AND DRILLED LONGERON IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONGERON, END FITTINGS, STIFFENERS, INTERCOSTALS, AND DUCT CLAMP BRACKET IAW DC8 SRM 51-1-21, 51-3-0, 51-1-20D, AND 51-1-21A. 2L74 4F RT4A25 20040422001092004042200109WP 2004 4 22 UPS04842154 120040229A5313DC853B0097 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT STA 1560 STR 33L CRACKED. REMOVED LONGERON SECTION FS 1490-1550, REC'D NEW LONG LOCATED AND DRILLED IAW DC8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REMOVED 2EA LONG SPLICES, FOUND CRACKS REC'D NEW LONG SPLICES, LOCATED AND DRILLED IAW DC8 SRM 51-1-20D. INSTALLED LONG AND SPLICES IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040422001102004042200110WP 2004 4 22 UPS04842155 120040229A5315 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1580 LBL B7 FLOORBEAM HAS CORROSION DOT (A5 619). REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED ANGLE REPAIR IAW DAC TR 53-124, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FLOORBOARD IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040422001122004042200112WP 2004 4 22 UPS04842157 120040229A5313564532813 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1702 STR 28L CORRODED. REMOVED STR STA 1680-1740; REC'D NEW LONGERON, LOCATED AND DRILLED IAW DC 8 SRM 51-1-21 AND 51-1-20D; ALODINED AND PRIMED IAW DC8 SRM 51-1-8; REC'D NEW LONG SPLICE LOCATED AND DRILLED IAW DC8 SRM 51-1-20D, FAB STRAPS IAW DC8 SRM 53-2-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONG SPLICE AND STRAPS IAW DC8 SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20040422001132004042200113WP 2004 4 22 UPS04842159 120040229A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 MAIN CABIN SEAT TRACK DAMAGED AT STA 319 LBL 24 DOT A5804. BLEND CORROSION IAW DC8 SRM 51-1-8; OUT OF LIMITS IAW DC8 SRM 53-2-3; ROUTED OUT SEAT TRACK IAW DC8 SRM 53-2-3 FIG D; ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PLUG AND CHANNEL IAW UPS DC8 SRM 53-2-3 THEN REINSTALLED FLOORBOARD IAW UPS DC8 SRM 51-3-1. 2L74 4F RT4A25 20040422001162004042200116WP 2004 4 22 UPS04842162 120040401A57209753293 ANGLE DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 LEFT WING I/B STUB WING VERTICAL ANGLE IS CRACKED AT LOWER END AT XS 246.5. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D. 2L74 4F RT4A25 20040422001172004042200117WP 2004 4 22 UPS04842164 120040301A53203779659501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 LONGERON 3L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM 20-14-00. 2L74 4F RT4A25 20040422001212004042200121NM 2004 4 22 UIEA200400037 120040405A575365B39150602 HOUSING BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE TE FLAP CARRIAGECORRODED A UIEAO OTHER O OTHER NRNOT REPORTED 1 EA15522MC 21783 DURING D CHECK AT SIN, PITTED CORROSION FOUND OUTBOARD TRAILING EDGE MID-FLAP IB CARRIAGE BRG HOUSING. REMOVED LOCAL SURFACE DAMAGE FROM THE AFFECTED AREA OF HOUSING. NDT INSPECTED TO INSURE CRACK AND DEFECT FREE CONDITION. SMOOTH, BLENDED AND REFINISHED HOUSING TO DESIGN CONDITION. INSTALLED OVERSIZED BUSHING IAW REQUIREMENTS OF OHM 57-52-55. 2L74 4F4 FRTA20WE E23EA 20040422001262004042200126NE 2004 4 22 ALG2004F00011 120040223A6210 SCREW SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE M/R BLADE CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03862AL 760531 20608TEC ON DAILY INSPECTION, FOUND THREE SCREW HEADS CRACKED ON THE MAIN ROTOR BLADE TIP CAP INSTALLED ON THE BLUE BLADE. MAINTENANCE REMOVED AND REPLACED THE THREE SCREWS. DURING REPLACEMENT OF THE SCREWS MAINTENANCE FOUND TWO MORE SCREWS WITH CRACKS IN THE WITH NEW SCREWS THAT WERE SUPPLIED. 1G72 3U3 UNCH1NE E00054EN 20040422001282004042200128 2004 4 22 USA2004F00007 420040209A34207725005009 INDICATOR BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE ADI FAILED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19392US34970 23314 SHORTLY AFTER TAKEOFF, ENROUTE, THE F/O ADI FAILED. CREW REPORTED THE CIRCUIT BREAKER WAS TRIPPED AND THAT A SLIGHT ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FO ADI EMMITTING THE ELECTRICAL ODOR. REMOVED AND REPLACED ADI AND INSPECTED WIRING. NO PROBLEMS FOUND WITH WIRING. PERFORMED SATISFACTORY FUNCTIONAL CHECK. A SECOND ADI WAS REPLACED FOR THE SAME PROBLEM. WIRING CK OK. ATHIRD ADI WAS INSTALLED. HAVE BEEN NO REPEATS. 2L72 4F4 FRTA16WE E2GL 20040422001322004042200132SO 2004 4 22 A8X2004F00000 220040219A8530AEC631397 CYLINDER HEAD BEECH 58 58 1152740CE CONT O550 IO550C SO ENGINE SEPARATED B A8XRO OTHER O OTHER NRNOT REPORTED 1 SO05299GM147 TH1527 676333 THE HEAD SEPARATED FROM THE BARRELL. ENGINE OVERHAULED WITH THE NEW CYLINDERS ON 5/2/03. 1L72 3O3 O 3A16 E3SO 20040422001352004042200135NM 2004 4 22 GAIA04056OP 120040330A3260656021132 ACCESSORY UNIT BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE NLG INOPERATIVE A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW076831 20184 TAKE OFF, ON GEAR RETRACTION L-R-NOSE GEAR RED ILLUMINATE AND TAIL SKID STAY ILLUMINATED. RECYCLED GEAR W/3 DOWN GEAR LIGHTS BUT SAME INDICATIONS W/GEAR HANDLE UP AND OFF POSITIONS. RETURNED WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. INSTALLED GEAR PINS AND OPERATED GEAR HANDLE. ALL GEAR INDICATIONS NORMAL ON GROUND. RETURNED TO NORMAL CONFIGURATION AND REMOVED GEAR PINS. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040422001372004042200137CE 2004 4 22 E812004F00003 120040211A3211 MOUNT BEECH 2000 2000 1152000CE PWA PT6 PT6* 52043EA NLG UPLOCK CRACKED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL038158X NC42 DURING ROUTINE INSPECTION FOUND ANGLE ON NOSE GEAR LOCK LINK UPPER HALF THAT NOSE GEAR DOWN AND LOCKED SWITCH S190 IS MOUNTED TO, CRACKED AT RADIUS APPROX .7500 WAY THROUGH. FURTHER INVESTIGATION SHOWED THAT REAR END OF SWITCH ASSY WHERE WIRING AND STRAIN RELIEF EXIT SWITCH WERE HITTING LOWER HALF OF NOSE GEAR LOCK LINK ASSY WHEN RETRACTED. NO LANDING GEAR INDICATION FAULTS WERE REPORTED BY FLIGHT CREW, BUT IF HAD PROGRESSED FURTHER, WOULD HAVE CAUSED LOSS OF NLG DOWN AND LOCKED INDICATION. VERIFIED ADEQUATE CLEARANCE EXISTS WITH LOCK LINK ASSY WHEN NOSE GEAR RETRACTED. 1L72 4T3 TRTA38ACE E2NE 20040422001382004042200138NE 2004 4 22 ALG2004F00004 120040216A261230326E7 AMPLIFIER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL FIRE DETECTOR INOPERATIVE E ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03519AL 760058 CAE890416S FIRE WARNING LIGHT ON NR 2 ENGINE ILLUMINATED. NO FIRE WAS SEEN. MAINTENANCE REMOVED AND REPLACED FIRE DETECTOR CONTROL AMP. 1G72 3U3 U H1NE E1GL 20040422001392004042200139SW 2004 4 22 ALG2004F00006 120040204A634022A690 TACH GENERATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TRANSMISSION FAILED E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW032201W 3477 CAE834438 DURING TAKE OFF, TACH WENT TO ZERO, LOW ROTOR LIGHT ILLUMINATED WITH LOW ROTOR HORN. RETURNED, LANDED AND NOTIFIED MAINTENANCE AND CUSTOMER. MAINTENANCE REMOVED AND REPLACED ROTOR TACH GENERATOR. AIRCRAFT GROUND RUN LEAK CHECKED AND OPS CHECKED GOOD. 1G71 3U3 U H2SW E4CE 20040422001422004042200142EU 2004 4 22 TI92004F00000 120040324A2435230650181 STARTER GEN ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE73140 29001NE NR 2 ENGINE FAILED E T19AO OTHER M OVER TEMP NRNOT REPORTED 1 WP19676TC597 128 STARTER GENERATOR FAILED (OVERHEATED AND DROPPED OFF LINE). 2L72 4F4 FRTA16NM E1NM 20040422001432004042200143EU 2004 4 22 USA2004F00008 120040216A2121EVT3454H FAN AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE EXTRACT VALVE ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19119US11424 1268 ENROUTE, THE FLIGHT CREW NOTED A STRONG ELECTRICAL ODOR AT FL 330 DURING CLIMB. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE AIRCRAFT ON MEL AND RELEASED FOR SERVICE. MAINTENANCE REPLACED THE EXTRACT VALVE. OPS CHECKED OK. 2L72 4F4 FRTA28NM E2GL 20040422001442004042200144NM 2004 4 22 USA2004F00009 120040224A33501000679 LIGHT BOEING767 767201 1385125NM GE CF6 CF680 30025NE COCKPIT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 THE COCKPIT EMERGENCY LIGHT DID NOT TEST. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHT. OPERATIONALLY CHECKS, OK. 2L72 4F4 FRTA1NM E13NE 20040422001452004042200145EA 2004 4 22 A6WA200440027 120040308A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO SMOKE ILLUMINATED A D RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL31425AW 7663 SMOKE CARGO WARNING MESSAGE DURING TAXI. COMPLIED WITH IMMEDIATE ACTION CHECKLIST QRH. CARGO BOTTLE LOW CAUTION MESSAGE. MESSAGE SMOKE CARGO EXTINGUISHED. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SQUIBS IAW MM. REMOVED FROM MEL AND PLACARD. REMOVED AND REPLACED CARGO SMOKE DETECTOR. INSIDE SMOKE DETECTOR WAS DIRTY CAUSING INTERMITTENT ALARMS. CLEANED INSIDE DETECTOR. (M) 2L72 4F4 FRTA21EA E15NE 20040422001472004042200147EU 2004 4 22 BRM2004F00000 120040320A6320109040003109 TRANSMISSION AGUSTAA109 A109E 0260119EU TMECA ARRIUSARRIUS2K1 NE MAIN ROTOR CONTAMINATED E BRMAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM0791LF 11509 ENROUTE, (3-20-04, 11:38 PM) THE PILOT NOTED A MAIN ROTOR TRANSMISSION CHIP LIGHT. A PRECAUTIONARY LANDING WAS PERFORMED. UPON INSPECTION OF THE MAGNETIC PLUGS (UPPER AND LOWER) NO METAL WAS FOUND. A LIGHT COAT OF VERY FINE BLACK PARTICLES THAT LOOKED LIKE DUST WAS REMOVED FROM THE CHIP PLUGS. A109E MAINTENANCE MANUAL CHAPTER 63 PAGE 63-5 TABLE 63-1. CORRECTIVE ACTION FOR METAL PARTICLES CONTAMINATION STATES FUZZ, FINE HAIR LIKE PARTICLES, (NORMAL WEAR) AND IN THE CORRECTIVE ACTION COLUMN IT SAYS: BOTH MAGNETIC PLUGS WERE CLEANED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 URTH7EU E34NE 20040422001492004042200149SO 2004 4 22 2004F00083 120040210A2140 O-RING PIPER PA31T PA31T3 7103128SO PWA PT6 PT6* 52043EA FUEL NOZZLE MISSING E CSAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 AL05217CS 202 3975907 31T8275014 SMOKE ENTERED THE COCKPIT, (KEROSENE EXHAUST) DURING CLIMB. THE AIRCRAFT RETURNED. THE FORWARD HEATER WAS SLOW TO LIGHT OFF. DURING RECENT FUEL NOZZLE CLEANING, THE O-RING SEAL THAT SEALS THE NOZZLE TO COMBUSTION TUBE WAS NOT INSTALLED, OR FELL OUT DURING REASSEMBLY. COMPLETING A PRESSURE DECAY TEST AFTER THIS TYPE OF MAINTENANCE WOULD PREVENT THIS TYPE OF INCIDENT. 1L72 3T3 T A8EA E2NE 20040422001552004042200155GL 2004 4 22 ALG2004F00016 220040317A7200 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 OVERTEMP E ALGAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW031547N 760088 CAE892552S IN STRAIGHT AND LEVEL FLIGHT, NR 1 ENGINE OIL TEMPERATURE BEGAN TO CLIMB. AS IT APPROACHED, THE RED LINE WE BEGAN TO MONITOR CLOSELY. WHEN IT WENT ABOVE THE RED LINE, I FOLLOWED CKLIST PROCEDURES AND SHUT DOWN NR 1 ENGINE, MADE RUN ON LANDING. NO OTHER INDICATIONS OF PROBLEMS. MAINT REMOVED AND REPLACED NR 1 ENGINE FOR HIGH OIL TEMPERATURE. ALSO CHANGE THE OIL COOLER AND ITS THERMOSTAT. COMPLIED WITH OPS CHECK BOTH GROUND AND FLIGHT BOTH CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 1G72 3U3 U H1NE E1GL 20040422001562004042200156WP 2004 4 22 UPS04842165 120040330A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 FUSELAGE SKIN HAS A DENT AT STATION -48 LONG 20L. CUT OUT DAMAGE, FABRICATED FILLER, INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040422001572004042200157EU 2004 4 22 Y2PA04008 120040405A324695438091 WHEEL AMD FALC20FALCOND 2720304EU GE CF700 CF700* 30010NE MLG VIBRATION A Y2PAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL23811AA 273 187 ON TAKEOFF, CREW DETECTED VIBRATION ON RT MAIN GEAR. CREW HAD TOWER INSPECT RUNWAY TO FIND TIRE CAP AS SUSPECTED. AC DIVERTED, TO BURN FUEL AND OBTAIN EMERGENCY FACILITIES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. EMERGENCY WAS CANCELLED BY CREW UPON EXITING RUNWAY. MECHANIC WAS DISPATCHED TO EVALUATE AC. UPON INSPECTION, MECHANIC FOUND RT IB FLAP, RT OB GEAR DOOR, RT WING IB T/E, AND NR 2 ENGINE AFT COWL TO HAVE MINOR SHEET METAL DAMAGE (DENTS). ACCORDING TO CREW THE NR 4 TIRE STILL HAD PRESSURE ON LANDING AND ONLY DEFLATED DURING TAXI TO RAMP. THE AIRCRAFTS NR 3 AND NR 4 WHEEL AND TIRE ASSEMBLIES WERE REPLACED WITH SERVICEABLE UNITS. AIRCRAFT UNDERGOING REPAIRS FOR SHEET METAL DAMAGED. 2L72 4F4 F A7EU E7EA 20040422001622004042200162WP 2004 4 22 UPS04842168 120040408A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 786 TO 798 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 750 TO 810 IAW SRM 53-2-3 FIG 14. 2L74 4F RT4A25 20040422001632004042200163WP 2004 4 22 UPS04842169 120040401A5320 WEB DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 922 BLB 63 FINGER DOUBLER AND PRESSURE WEB IS CORRODED BEYOND LIMITS. REMOVED FINGER DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED FINGER DOUBLERS, FILLER SPLICE STRAP AND REPAIR DOUBLER IAW SRO8530026. 2L74 4F RT4A25 20040422001642004042200164NM 2004 4 22 USA2004F00001 120040219A3397 CONNECTOR BOEING737 737401 1384701NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19417US 23984 MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTING AT SEAT ROWS 6ABC THROUGH 9ABC INOPERATIVE. MAINTENANCE RESET SYSTEM AND TESTED CHARGER AND BATTERY. FOUND CANNON PLUG LOOSE. RESECURED CONNECTOR PLUG. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040422001682004042200168NM 2004 4 22 UPS04242219 120040405A2750 DRUM BOEING727 72731C 1384011NM LT MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C LEFT I/B MIDFLAP O/B AFT FLAP ACTUATING DRUM CORRODED. DRUM REPLACED IAW MM 27-51-01. 2L73 4F A3WE 20040422001692004042200169SO 2004 4 22 SIMA200405501 120040220A49204951830 FUEL NOZZLE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL APU BROKEN A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21849AE 145716 DISCOVERED FUMES IN CABIN AND COCKPIT SMELLS LIKE RAW JET FUEL. WALK AROUND INSPECTION REVEALED APU LEAKING FUEL. FOUND BROKEN FUEL NOZZLE. RAI APU FUEL NOZZLE IAW MFG MM. LEAK CHECKED APU, NO LEAKS NOTED AT THIS TIME. (SW21200404647) 2L72 4F4 FRTT00011ATTE6CH 20040422001742004042200174SO 2004 4 22 FTU2004F00000 120040325A3246 WHEEL PIPER PA23 PA23250 7102308SO LYC O540 TIO540* 41532EA MLG CRACKED B FTURD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NE057147C 274472 WHILE AIRCRAFT WAS TAXIING OUT TO THE RUNWAY FOR TAKE OFF. THE LT MAIN WHEEL TIRE WENT FLAT. AIRCRAFT WAS TOWED TO MAINTENANCE AND THE INNER WHEEL HALF RIM WAS FOUND CRACKED AT THE RIM RADIUS FOR APPROX. 5 INCHES ALONG THE RIM. THE TIRE WAS ALSO DAMAGED AND UNSERVICEABLE FOR FURTHER USE. NO OTHER DAMAGE FOUND THROUGHOUT THE LANDING GEAR. 1L72 3O3 O 1A10 E14EA 20040422001752004042200175NM 2004 4 22 UPS04442211 120040329A575365B078851 RIB BOEING747 747121 1384871NM NR 10 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 10 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOK O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 10 VC FLAP OLES 766 O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH & BUSHING FABRICATED & INSTALLED. 2L74 4F A20WE 20040422001772004042200177EU 2004 4 22 S642004F00000 120040325A29109603001153 POWERPACK PILATSPC12 PC1245 7090551EU PWA PT6 PT6A60A 52043NE HYD SYSTEM INOPERATIVE E S64AO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO17295PC865 295 SMOKING AT LT WING FAIRING EDGES. FAIRING PULLED, FOUND HYD PKG SOFT START RESISTOR SMOKED AS WELL AS LARGE BLACK AREA ON FUSELAGE BLACK. INSIDE OF WING FAIRING BURNED AND BUBBLED ON OUTSIDE. INSTALLED NEW RESISTOR AND NEW HYD UNIT SELECT RELAY. PULLED NR 4 CABIN CENTER LINE FLOOR. FOUND HYD UNIT 100-AMP CB POPPED. 100 AMP CB RESET. BATT SELECTED ON. PUMP DID NOT RUN AND RESISTOR STARTED HEATING. BATT OFF. CALLED TECH SUPPORT. HYD PKG AND ACCUMULATOR PULLED. CLEANED SIDE OF FUSELAGE AND FOUND ONLY SLIGHT DISCOLORATION TO PAINT. NO DAMAGE TO SKIN. REPLACED HYD CNTRL RELAY, HYD PKG, ACCUMULATOR, SOFT START RESISTOR, COMPLIED WITH SEVERAL GEAR SWINGS, NO PROBLEM NOTED. 1L71 3T4 TRTA78EU E4EA 20040422001782004042200178EU 2004 4 22 A6WA200460004 120040304A2131 CONTROLLER BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA CABIN PRESSURE MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31608AW E2049 PRESSURIZATION WAS ABNORMAL AFTER TAKEOFF, UNABLE TO CONTROL. CORRECTIVE ACTION IN PROGRESS. 2H74 4F4 F A49EU E6NE 20040422001792004042200179CE 2004 4 22 CMX2004F00000 120040330A8011PM2401 STARTER CESSNA172 172R 2072401CE BENDIX BROKEN B CMXRO OTHER O OTHER NRNOT REPORTED 1 CE05468CM3 17280860 BENDIX EXTENDED TOO FAR OUT (FORWARD) AND BROKE THE HOUSING. HAVE HAD 7 NEW STARTERS REPLACED WITHIN THE FIRST 50 HOURS OF USE ON 4 FACTORY OVERHAULED ENGINES SINCE DEC O4. ALL DUE TO BENDIX MALFUNCTIONS OF FAILURE TO EXTEND OR PREMATURE RETRACTION. 1H71 3O NT3A12 20040422001832004042200183SO 2004 4 22 SIMA200406803 120040305A2841 INDICATOR EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUEL QTY MALFUNCTIONED A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21822AE 145581 CREW NOTED AFTER TAKEOFF THAT THE RT FUEL TANK WAS LOOSING ABOUT 300LB PER MINUTE, SO THEY RETURNED FOR MAINTENANCE. INSPECTED RT FUEL SYSTEM AND FOUND NO LEAKS. ALSO CALCULATED FUEL BURN OF LT AND RT ENGINES FOUND TO BE NORMAL. NO DEFECTS NOTED. AC RETURNED TO SERVICE. (SW21200404944) 2L72 4F4 FRTT00011ATTE6CH 20040422001842004042200184CE 2004 4 22 FFS2004F00000 120040116A3397 WIRE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL NAV LIGHT SHORTED A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575Z 19581 UC136 WHEN PERFORMING BUSS SENSE TEST, LOW VOLTAGE (11V-18V) WAS STILL PRESENT ON CENTER BUSS WITH BUSS TIE RELAYS OPEN. IT WAS DETERMINED SOURCE OF VOLTAGE WAS RT GENERATOR BUSS. WHILE SYSTEMATICALLY OPENING CB POWERED OFF RT GENERATOR BUS, VOLTAGE ON CENTER BUSS DISAPPEARED WHEN THE ELEVATOR TRIM CB WAS PULLED. HOWEVER IT WAS DETERMINED THAT THE ELEVATOR TRIM MOTOR WOULD STILL RUN WHEN COMMANDED EVEN WITH ITS CB OPEN IF THE NAV LIGHTS WERE SELECTED ON. THE SHORT BETWEEN THE NAV LIGHT CIRCUIT (CENTER BUSS POWER) AND THE ELEVATOR TRIM CIRCUIT (RT GENERATOR BUS POWER) OCCURRED IN THE AFT PRESSURE BULKHEAD FEED THROUGH CONNECTOR. REPLACED FEED THROUGH FT393 AND PINS 2 AND 5 IN MATING PLUG P394. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20040422001922004042200192CE 2004 4 22 T2C2004F00000 120040204A2720265524057 CASTING RKWELLNA265 NA26560 7630106CE PWA JT12 JT12A6A 52042NE RUDDER CONTROL CRACKED B T2CRO OTHER O OTHER NRNOT REPORTED 1 WP01789SG4952 306121 DURING RUDDER RIGGING CHECK, FOUND CRACKED CASTING AT RUDDER PEDAL TORQUE TUBE SUPPORT, BELOW CO-PILOTS FLOOR. SUSPECT WIND GUST DAMAGE AS POSSIBLE CAUSE. ALSO NOTED RUDDER STOP BOLTS ON CASTING ADJUSTED BEYOND MAX TRAVEL LIMITS. RECOMMEND INSPECTING THIS AREA WHEN INSPECTING FOR WIND GUST DAMAGE. (WP01200406636) 2L72 4J4 JRTA2WE 1E9 20040422001952004042200195EA 2004 4 22 SWIA200413127 120040406A4930 FITTING CNDAIRCL600 CL6002B19 1900309EA APU LEAKING A SWIAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07418SW 7446 FUEL SMELL IN AIRCRAFT CABIN, ALSO FUEL LEAK FROM REAR OF AIRCRAFT. REPLACE FITTING AT APU FUEL CONTROL TO FUEL SHUTOFF VALVE. RAN APU, OPS CHECK AND LEAK CHECK GOOD. P/N: AP258S04. 2L72 4F RTA21EA 20040422001972004042200197SO 2004 4 22 CHQA000479 120040414A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO LAV SMOKE FALSE ACTIVATIONA CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11971 145426 AFTER TAKEOFF OUT OF PHL LAV SMOKE MESSAGE APPEARED ON EICAS. NO SMELL OR SIGHT OF SMOKE IN LAV. AIR TURNBACK INTO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED LAV SMOKE DETECTOR AND PERFORMED OPS CHECK IAW EMB 145 AMM 26-00-00. OPS CHECK OK. NO FAULTS FOUND. ACFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040422001992004042200199EA 2004 4 22 SWIA200413129 120040407A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07934SW 7722 EMERGENCY EXIT TIP LIGHTS INOP ON OVERHEAD SIGN AT ROW 8. REMOVED AND REPLACED TIP LIGHTS ON OVERHEAD SIGN AT ROW 8 IN REF TO AMM 33-51-00. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20040422002022004042200202SO 2004 4 22 CHQA000471 120040327A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 3-7 MALFUNCTIONED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286 145443 EMERGENCY EGRESS FLOOR LIGHTS AT ROW 3 THRU 7 ARE INOP. WHILE TROUBLESHOOTING EMERGENCY LIGHTS ROW 3 THRU 7, FOUND ALL EMERGENCY EGRESS FLOOR STRIP LIGHTS TO BE OPERATING NORMALLY. OPS CHECK GOOD IAW EMB 145 AMM 33-50-12. 2L72 4T RTT00011AT 20040422002032004042200203SO 2004 4 22 SWIA200413130 120040407A27523203001005 ACTUATOR EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07577345645 2202 120199 WHEN SELECTING FLAPS 45 FROM FLAPS 25 POSITION A FLAP DISAGREEMENT OCCURRED. AIRSPEED AT TIME OF DISAGREEMENT WAS 130 KIAS. REPLACED RIGHT I/B FLAP ACTUATOR WITH SERVICEABLE UNIT IAW AMM 27-50-07. OPS CHECK GOOD. 2L72 4T RTA31SO 20040422002052004042200205SO 2004 4 22 CHQA000473 120040404A3350 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378 145593 RT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT WING EMERGENCY LIGHT IAW EMB 140 MM CH 33-50-07. OPS CHECK GOOD. LAMP P/N GE1317. 2L72 4F RTT00011AT 20040422002092004042200209NM 2004 4 22 UIEA200400042 120040407A5414 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 3 PYLON DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING A MAINTENANCE INSP, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 3 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMAGE. NDT INSP, INCLUDING HFEC OF SKIN TRIMMED EDGES AND REPAIR FASTENER HOLES WAS ACCOMPLISHED TO ENSURE DAMAGE FREE CONDITION. A NEW SKIN REPAIR DOUBLER ASSEMBLY WAS INSTALLED FROM STA 286 TO STA316. THE REPAIR DOUBLER ASSEMBLY IS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED JUST AFT OF THE TITANIUM SKIN DOUBLER EXTENSION. THE REPAIR TITANIUM DOUBLERS ARE ATTACHED TO THE EXISTING TITANIUM DOUBLER EXTENSION WITH A NEW TITANIUM TRIPLER. 2L74 4F4 FRTA20WE E23EA 20040422002102004042200210NM 2004 4 22 AMTA200400377 120040328A5321 FLOOR PANEL BOEING737 73783N 13844HINM GE CFM56 CFM56* 13802NE AFT CARGO CORRODED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11308TZ 28244 CORROSION: AFT CARGO COMPARTMENT, FLOOR PANEL. FABRICATED PANEL 14 OBF IN C2 PIT IAW SRM, INSTALLED FLOORBOARD IAW AMM IN C-2 PIT. 2L72 4F4 FRTA16WE E2GL 20040422002122004042200212NM 2004 4 22 USA2004F00023 120040328A2572H313241 FORK BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE E32 RACK/EE BROKEN A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19512AU 23595 AFTER TAKEOFF, THE AUTO FAIL LIGHT ILLUMINATED. AIRCRAFT WOULD NOT PRESSURIZE AND THERE WAS NO PNEUMATIC PRESSURE FROM EITHER ENGINE. CABIN TEMPERATURE CLIMBED RAPIDLY. CREW BROUGHT APU ON LINE BUT STILL COULD NOT PRESSURIZE AIRCRAFT. PACKS WERE NOT WORKING. FLIGHT RETUNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT FOUND THE AIR CONDITIONING ACCESSORY UNIT HOLD DOWN LUG/FORK ASSY BROKEN AND UNIT NOT SEATED IN THE CONNECTOR RACK. INSTALLED ACCESSORY UNIT AND REPLACED FOR ASSEMBLY. PACK AND BLEED SYSTEM OPERATES NORMAL. 2L72 4F4 FRTA16WE E2GL 20040422002152004042200215NM 2004 4 22 UIEA200400041 120040407A5414 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 2 PYLON DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 DURING A MAINTENANCE INSPECTION, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 2 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CHORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMAGE. NDT INSPECTION, INCLUDING HFEC OF SKIN TRIMMED EDGES AND REPAIR FASTENER HOLES WAS ACCOMPLISHED TO ENSURE DAMAGE FREE CONDITION. A NEW SKIN REPAIR DOUBLER ASSEMBLY WAS INSTALLED FROM STA 286 TO STA 300. THE REPAIR DOUBLER ASSY IS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED JUS AFT OF THE TITANIUM SKIN DOUBLER EXTENSION. THE REPAIR TITANIUM DOUBLERS ARE ATTACHED TO THE EXISTING TITANIUM DOUBLER EXTENSION WITH A NEW TITANIUM TRIPLER. 2L74 4F4 FRTA20WE E23EA 20040422002162004042200216NM 2004 4 22 UIEA200400047 120040413A5414 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE ACCESS CUT OUT CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 1 PYLON PERCOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED AN ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER REPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040422002182004042200218EU 2004 4 22 AWXA200400380 120040328A5320D5348002034300 SHEAR WEB AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-08 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR WEB (TRAY) AFT SIDE OF R-2 DOORWAY, OUTBOARD OF Y1732 RT, BETWEEN FR 68 & FR 69. MAINTENANCE REMOVED CRACKED TRAY FROM Y1732 RT TO Y1800 RT, FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY PER DWG D53480020; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2 & 3 PG 7-10 & 12. 2L72 4F RTA28NM 20040422002202004042200220NM 2004 4 22 AWXA200400382 120040401A5320654797321 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN SHEAR WEB BETWEEN BS 616 AND BS 639, LBL 58, WL 208. MAINTENANCE REMOVED CRACKED SHEAR WEB BETWEEN BS 616 AND BS 639, LBL 58, WL 208; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-47973; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4 & 8 PG 26-28, 38. 2L72 4F RTA16WE 20040422002212004042200221NM 2004 4 22 AMTA200400243 120040304A7700 WARNING LIGHT BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE FALSE INDICATIONA AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11559TZ 32593 31869 AT 41,000 FT.790M, RT ENGINE EPR FLUCTUATES 1.60 TO 1.63 WITH A CORRESPONDING FLUCTUATION IN ALL OTER ENGINE INDICATIONS. ALSO, RT ENGINE BLEED DUCT PRESSURE FLUCTUATES 3 PSI. FOLLOWED FIM 71-06-00 FIG 102. NO FAULTS NOTED AT THIS TIME. OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20040422002242004042200224NM 2004 4 22 AWXA200400384 120040401A5320654797322 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FLOOR WEB UNDER RT OVERWING EMERGENCY HATCH BS 635, RBL 65, WL 208. MAINTENANCE REMOVED CRACKED FLOOR WEB AT BS 635, RBL 65, WL 208; FABRICATED A NEW REPLACEMENT FLOOR WEB PER DWG 65-47973; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4 & 8 PG 26-28, 38. 2L72 4F RTA16WE 20040422002252004042200225NM 2004 4 22 AWXA200400385 120040401A532065C326772 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON SHEAR WEB BETWEEN BS 986 AND BS 1016, LBL 36 AND LBL 45, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 986 TO BS 1016, LBL 36 TO LBL 45; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040422002262004042200226NM 2004 4 22 AWXA200400386 120040420A2560P4010021 BATTERY BOEING737 737375 13844BNNM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28336AW 23707 PHX - EMERGENCY EQUIPMENT - AFT CABIN EMERGENCY FLASHLIGHT DOES NOT TEST. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040422002272004042200227GL 2004 4 22 NF22004F00000 120040309A274111797004 MOTOR CIRRUSSR SR20 05628AJGL CONT IO360 IO360* 17025CE PITCH TRIM FAILED B NF2DO OTHER O OTHER NRNOT REPORTED 1 CE03267CD308 1284 PITCH TRIM MOTOR OUTPUT SHAFT SHEARED OFF ALLOWING TRIM CARTRIDGE AND ARM TO HANG LOOSELY IN THE TAIL POTENTIALLY JAMBING AND RESTRICTING ELEVATOR MOVEMENT. 1L71 3O3 ONTA00009CHE1CE 20040422002302004042200230EU 2004 4 22 PG92004F00012 120040302A6410 SPAR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE T/R BLADE CRACKED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19911KR819 9289 2094 DURING PERIODIC INSPECTION (500HR) AND COMPLIANCE OF ECF SB 05.11. FOUND CRACKED SPAR ON T/R BLADE SN 9289. THIS IS THE 3TH T/R BLADE WE HAVE REJECTED IN 6 MONTHS. ALL HAVE HAD THE EXACT SAME CRACK. SUGGEST MANUFACTURER REEVALUATE. THE MFG PROCESS OF THESE FLIGHT CONTROL ROTATING COMPONENTS. 1G71 3U3 UNCH9EU E19EU 20040422002312004042200231NM 2004 4 22 AWXA200400389 120040401A5320655287813 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SCUFF PLATE (ZEE ANGLE) BS 983, LBL 56, WL 209. MAINTENANCE REMOVED CORRODED ZEE ANGLE FROM BS 983, LBL 56, WL 209; FABRICATED A NEW REPLACEMENT ZEE ANGLE PER DWG 65-45878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040422002332004042200233SO 2004 4 22 SWIA200413131 120040401A2460 RELAY EMB 120 EMB120ER 3260203SO COCKPIT FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07293SW 120320 BURNING SMELL COMING FROM THE APU FEED PANEL (F/O'S SIDE). REMOVED AND REPLACED APU FEEDER PROTECTION RELAY AND CONNECTION BARS IAW EMB120 MM 20-00-00 AND WM 20-40-00. OPS CHECK. NO MORE ODOR. P/N: 25583-448258051-22, 120-24038-501, 120-24029-001. 2L72 4T RTA31SO 20040422002342004042200234CE 2004 4 22 EVT2004F00000 120040407A52601313232C15 PIN BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA AIRSTAIR BROKEN B EVTRO OTHER O OTHER NRNOT REPORTED 1 SO33130CT7670 BB578 FRONT AIRSTAIR TOP HOOK FOUND LOOSE WHEN OPENED. ON INSPECTION FOUND PIN BROKEN. HOOK REPLACEMENT AND INSPECTION. NOT DUE UNTIL 10,000 HOUR. 1L72 4T3 T A24CE E2NE 20040422002352004042200235SO 2004 4 22 OG52004F00000 120040325A55416354300 SPAR PIPER PA28 PA28R201 7102816SO LYC O360 IO360C1C6 41514EA MCAULY2D34C B2D34C213 GL RUDDER CRACKED B OG5RO OTHER O OTHER NRNOT REPORTED 1 GL21286ND2639 2844035 L88051A 011240 UPPER SPAR CRACKED ON BOTH SIDES FROM THE TOP TO THE BOTTOM ABOUT AN INCH IN LENGTH. THE CRACK IS ALL THE WAY THROUGH THE SPAR AND ALSO THE DOUBLER. 1L71 3O3 O 2A13 1E10 5 CP7EA 20040423000022004042300002NE 2004 4 23 UG82004F00003 220040305A7320 EEC GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE RT ENGINE FAULTY E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL23920DC 534 DURING CLIMB, RT ENGINE ROLLED BACK AFTER TAKE OFF ABOUT 20 DEGREES. SWITCHED DAU NR 1 TO CHANNEL B AND ENGINE OK. TROUBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICEABLE EEC IAW MFG MM AND PERFORMED ENGINE OPERATIONAL CHECKS. ALL PARAMETERS NORMAL. 2L72 4F4 FRTA12EA E00057EN 20040423000072004042300007WP 2004 4 23 Z3M2004F00000 120040212A2434ALX8421LS ALTERNATOR ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA ENGINE FAILED E Z3MAO OTHER O OTHER NRNOT REPORTED 1 CE037036J1026 0583 L2538140A ALTERNATOR FAILED TO PRODUCE ADEQUATE VOLTAGE UNDER HIGH LOADS. REPLACED ALTERNATOR. 1G71 3O3 O H11NM E295 20040423000092004042300009NE 2004 4 23 TRB2004F00013 220040229A720051653152 CONTROL UNIT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENG FIRE WARNINTERMITTENT A TRBAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO21407AT 407 127120 LT ENGINE FIRE WARNING INTERMITTENT. REPLACED FIRE CONTROL UNIT. 2H72 4T4 TRTA53EU E20NE 20040423000102004042300010EU 2004 4 23 USA2004F00011 120040307A3350321430 BATTERY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19766US 1378 THE EMERGENCY LIGHTS TEST FAULTS THE AFT EPSU BATTERY. MAINTNANCE REPLACED THE AFT EPSU BATTERY. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E2GL 20040423000172004042300017EU 2004 4 23 SDR2004016 120040302A2612 FIRE WARNING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE FALSE ACTIVATIONA TRBAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO21308AE 309 127094 LT ENGINE FIRE WARNING INDICATION CAME ON. CREW DEPLOYED THE FIRE BOTTLE AS A PRECAUTIONARY METHOD. NO EVIDENCE OF FIRE FOUND. LOOKS LIKE A TAIL WIND PROMOTE THE FALSE. ENGINE FIRE WARNING INDICATION. 2H72 4T4 TRTA53EU E20NE 20040423000182004042300018CE 2004 4 23 ID42004F00000 120040220A7120643042 MOUNT CESSNA303 T303 2073820CE CONT O520 TSIO520AE 17040SO ENGINE CRACKED B ID4RO OTHER O OTHER NRNOT REPORTED 1 SO09303NN T30300268 246194R DURING AN ANNUAL INSPECTION THE IB LOWER ENGINE MOUNT LEG WAS FOUND CRACKED ON THE LT ENGINE. AIRCRAFT TT WAS 4391.8. ENGINE TIME 685. THE CRACK WAS ABOUT 1.1250 INCHES LONG. STARTING AT LOWER EDGE 3 INCHES FROM ENGINE ATTACH POINT. HAS A SMALL POROSITY VOID .3750 INCH BACK FROM EDGE OF MOUNT LEG AND IN LINE WITH CRACK. 1L72 3O3 O A34CE E8CE 20040423000202004042300020EU 2004 4 23 SDR2004014 120040301A2612 FIRE WARNING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE FALSE INDICATIONA TRBAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO21399AT 399 127160 FIRE WARNING INDICATION ON RT ENGINE. VISUAL INSPECTION REVEALED NO FIRE EVIDENCE. OPERATIONAL CHECK OF THE SYSTEM FOUND SATISFACTORY. THIS HAPPENED WHILE HOLDING SHORT FOR TAKEOFF. LOOKS LIKE A TAIL WING ACTIVATED THE ENGINE WARNING LIGHT. 2H72 4T4 TRTA53EU E20NE 20040423000272004042300027NE 2004 4 23 RYNA50885 220040303A7200V2527A5 ENGINE AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE NR 1 FAILED A RYNAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 CE07381LF 460 V10225 DURING TAKEOFF ROLL OUT, A LOUD BANG SHUDDERED THE AIRCRAFT ACCOMPANIED BY AN IMMEDIATE AND EXCESSIVE YAW TO THE LEFT OF CENTER LINE. TAKEOFF WAS ABORTED AND AIRCRAFT TAXIED CLEAR OF THE ACTIVE RUNWAY WITHOUT INCIDENT. 2L72 4F4 FRTA28NM E40NE 20040423000282004042300028EU 2004 4 23 M7K2004F00004 120040122A5410TL100AXE12L50 FASTENER UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE HOOK SHEARED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19803MH422 3735 23069 ON THE ENGINE FAIRING 1 OF 4) LATCHING HOOK OF THE FASTENER SHEARED AT HOOK BASE AND CRYSTALIZATION OF THE METAL AT THE BREAK SEEMED APPARENT. NO SIGNIFICANT WEAR NOTED BEFORE THE BREAK OCCURRED THIS IS A TITAIUM MATERIAL. SUGGEST USING STAINLESS STEEL. 1G72 3U3 U H9EU E00054EN 20040423000292004042300029EU 2004 4 23 M7K2004F00005 120040109A1810350A21004828 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE CABIN CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19801MH217 3654 23007 RT CABIN ANTI-VIBRATOR TUNING HAMMER. SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORE AND AFT FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHINING OF THE PARTS SHOULD INCLUDE A MUCH GREATER RADIUS IN THE EFFECTED AREA OF CRACK OCCURRENCE. 1G72 3U3 U H9EU E00054EN 20040423000302004042300030CE 2004 4 23 PO82004F00000 120040301A2434E3FF10300AA ALTERNATOR CESSNA210 T210M 2073451CE CONT O520 TSIO520R 17040SO ENGINE FAILED B PO8RO OTHER O OTHER NRNOT REPORTED 1 NM096246B 134 21062721 293993R ALTERNATOR FAILED INFLIGHT AFTER 134 HOURS TSO. UNIT SENT OUT TO A CERTIFIED REPAIR STATION FOR REPAIR. TEARDOWN REPORT STATED ONE BAD BEARING AND A FAILED STATOR. PREVIOUS OVERHAULED ALTERNATOR LASTED FIVE MINUTES BEFORE AND THE OVERHAULED UNIT PRIOR TO THAT LASTED 398 HOURS. THIS AIRCRAFT HAS EXPERIENCED THREE FAILURES SINCE AUG 2001. 1H71 3O3 O 3A21 E8CE 20040423000322004042300032EU 2004 4 23 B3O2004F00000 120040223A6210355A11003000 BLADE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MAIN ROTOR DAMAGED B B3ORO OTHER O OTHER NRNOT REPORTED 1 SW035204Y933 3101 MAIN ROTOR BLADE RECEIVED FROM AEC WITH DAMAGE TO THE TRAILING EDGE OF THE NR 3 TRIM TAB. TRIM TABS RESET AT AEC PRIOR TO RECEIPT AEC WO NR W0078958. BLADE NOT ABLE TO FLY CORRECTLY ON TWO DIFFERENT AC. REQUEST EVALUATION OF BLADE. 1G71 3U3 U H9EU E19EU 20040423000332004042300033NM 2004 4 23 USAA040018 120040116A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US53730 22954 CLT - FOUND SKIN CRACKED 3.250 INCH, FS 753 JUST ABOVE STRINGER S23R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M) 2L72 4F RTA16WE 20040423000352004042300035EA 2004 4 23 ASOA04143 120040219A7120 BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE SUPPORT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE FORWARD INBOARD CORNER OF THE ENGINE SUPPORT BEAM AT APPROXIMATELY FS 625, BL 36.20 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD INBOARD CORNER OF THE ENGINE SUPPORT BEAM AT APPROX FS 625, BL 36.20 ON THE RIGHT SIDE IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20040423000362004042300036EA 2004 4 23 ASOA04144 120040219A3350BF50390901 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMEREGNCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR. OPS CHECKS GOOD. (M) 2L72 4F RTA21EA 20040423000372004042300037EA 2004 4 23 ASOA04145 120040220A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040421000742004042100074NM 2004 4 21 CALA0400387 120040416A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 PAX FLOOR STATION 312 FLOORBEAM STRAP HAS LITE CORROSION. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. 2L72 4F RTA16WE 20040421000752004042100075NM 2004 4 21 CALA0400388 120040416A534565B5783930 MOUNT BOEING737 7373T0 1384582NM LAVATORY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 FORWARD CABIN LAV MOUNT AT STATION 300 LBL 42 CORRODED. REMOVED AND REPLACED MOUNT PER SRM 51-10-02. 2L72 4F RTA16WE 20040421000792004042100079NM 2004 4 21 04FDEA001005 120040418A5753 SUPPORT DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT, CRACK FOUND ON LOWER HOLE AT 6 O' CLOCK POSITION FORWARD FACE. 2L73 4F RTA22WE 20040421000832004042100083NM 2004 4 21 AWXA200400373 120040408A53306545774575 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AFT OF LEFT WING TO BODY FAIRING BS 727E, STR 23 LEFT. MAINTENANCE CUT OUT DAMAGED SKIN AT BS 727E, STR 23 LEFT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SKIN SECTION AND FORWARD & AFT FILLERS, DOUBLERS & TRIPLERS; INSTALLED REPAIR PARTS IAW DWG AW5361001. 2L72 4F RTA16WE 20040421000902004042100090NM 2004 4 21 04FDEA00989 120040417A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RT I/B FLAP VANE O/B VANE ATTACH FITTING ASSY HOLES FOUND WITH CORROSION. ATTACH FITTING ASSY REMOVED AND REPLACED PER CMM57-52-03. 2L73 4F RTA22WE 20040421000992004042100099NM 2004 4 21 CALA0400366 120040412A5510180A16121 PIN BOEING737 737724 13844BYNM LT HOR STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716713 28784 INSPECTION FOUND LEFT HORIZONTAL STABILIZER UPPER PIN CORRODED. THE PIN WAS REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040421001042004042100104EA 2004 4 21 COMA0460252 120040409A32307455025 SELECTOR SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01507CA2253 7796 FLIGHT 5028 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. GEAR RETRACTION AND EXTENSION CHECKS NORMAL. REPLACED GEAR SELECTOR HANDLE FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20040421001102004042100110EU 2004 4 21 04FDEA00975 120040416A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 FIVE AREAS OF CORROSION ON SEAT TRACK FLANGE SEAT TRACK 1L BETWEEN FRAMES 26-28. REPAIRED SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201 WITH SPLICE REPAIR BETWEEN FRAMES 26.5 TO 29.5. 2L72 4F RTA35EU 20040421001132004042100113EU 2004 4 21 04FDEA00978 120040416A5320 PAN AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC FLOOR PAN BETWEEN TRACKS 2 & 3 RT FR 26 HAS 1 AREA OF CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040421001172004042100117EA 2004 4 21 COMA0460258 120040413A3020 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01912CA 7011 FLIGHT 5553 RIGHT COWL ANTI-ICE AND THRUST REVERSER UNSAFE CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA21EA 20040421001182004042100118EA 2004 4 21 COMA0460261 120040412A335059465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01934CA 7042 FLIGHT 5556 EMERGENCY FLOOR LIGHTS ARE INOP FROM ROW 8 AFT. REPLACED CONNECTOR WIRE AT ROW 8. 2L72 4F RTA21EA 20040421001212004042100121EA 2004 4 21 COMA0460260 120040410A49901603662 OIL COOLER CNDAIRCL600 CL6002B19 1900309EA APU MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01779CA 7306 FLIGHT 9466 APU OIL TEMP CAUTION. REPLACED THE APU OIL COOLER. 2L72 4F RTA21EA 20040421001232004042100123NM 2004 4 21 04FDEA001000 120040417A575565413312 BRACKET BOEING727 727200 138407ENM NR 8 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25279FE 22346 NR 8 SPOILER INBOARD STOP BRACKET LWR MOUNTING CRACKED. REMOVED AND REPLACED STOP BRACKET IAW SRM 51-30-2 AT MAE. 2L73 4F RTA3WE 20040421001362004042100136NM 2004 4 21 CALA0400361 120040413A53126546568 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE WRINKLED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 INSPECTION FOUND STRAP ON AFT FACE OF AFT PRESSURE BULKHEAD BULDGED/WRINKLED BETWEEN STRINGER 6L AND 8L, LBL 40. THE STRAP WAS REMOVED AND A REPAIR STRAP AND FILLER WERE INSTALLED IAW ECRA 5310-04310. 2L72 4F RTA16WE 20040421001502004042100150WP 2004 4 21 UPS04842121 120040404A5740 FITTING DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE: C3, LEFT WING FLAP HINGE 219 CANOE FITTING HAS PITTING CORROSION. MILLED OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLERS IAW SB 27-164. 2L74 4F RT4A25 20040421001622004042100162EA 2004 4 21 ASOA04220 120040317A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURNG A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040421001632004042100163EA 2004 4 21 ASOA04219 120040317A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7256 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040421001642004042100164EA 2004 4 21 ASOA04223 120040318A3350BF50122901 COVER CNDAIRCL600 CL6002B19 1900309EA EXIT SIGN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING HANGAR MAINTENANCE IN BTR, THE AFT CEILING EMERGENCY EXIT SIGN COVER WAS FOUND MISSING. MAINTENANCE REPLACED THE AFT CEILING EMERGENCY EXIT SIGN COVER. (M) 2L72 4F RTA21EA 20040421001732004042100173NM 2004 4 21 GAIA04051OP 120040318A2611302842 SMOKE DETECTOR BOEING727 727223 1384074NM MAIN CARGO COMP INOPERATIVE A GAIAO OTHER N FALSE WARNING CRCRUISE 1 SW07854AA 20995 DURING CRUISE, THE UPPER DECK CARGO SMOKE WARNING LIGHT CAME ON. NO SMOKE OBSERVED ON WALK THROUGH. CREW CONTINUED NORMAL OPERATIONS. REMOVED AND REPLACED CONTROL AMPLIFIER AND NR 6 SMOKE DETECTOR. OPS CHECK GOOD. AIRCRAF WAS RELEASED FOR SERVICE. (M) 2L73 4F A3WE 20040421001742004042100174EA 2004 4 21 ASOA04200 120040312A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE CLIP AT FS 280, RBL 9 OUTBOARD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 280, RBL 9 OUTBOARD IAW SRM 51-40-00. (M) 2L72 4F RTA21EA 20040422000022004042200002EA 2004 4 22 ASOA04197 120040311A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE AFT CARGO FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE AFT CARGO FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040422000032004042200003EA 2004 4 22 ASOA04196 120040311A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11865AS 7507 DURNG HANGAR MAINTENANCE IN MCN, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY CHARGER ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000092004042200009EU 2004 4 22 ASOA04191 120040310A5210S5217670000662 SPRING AEROSPATR72 ATR72212 8680945EU PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO11534AS 463 DURNG HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR WOULD NOT OPEN TO THE FULL OPEN POSITION. MAINTENANCE ADJUSTED THE SPRINGS ON THE PASSENGER DOOR IAW SERVICE BULLETIN ATR72-52-1027. (M) 2H72 4T RTA53EU 20040422000152004042200015EU 2004 4 22 ASOA04206 120040310A2751 WARNING LIGHT AEROSPATR72 ATR72212 8680945EU TE FLAPS ILLUMINATED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11635AS 372 DURING APPROACH INTO AVL FROM ATL, THE CREW RECEIVED A FLAP UNLOCK MESSAGE WITH A MASTER WARNING. A GO-AROUND WAS INITIATED AND THE CREW REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. A ZERO DEGREE FLAP LANDING WAS ACCOMPLISHED AND THE AIRCRAFT LANDED SAFELY IN AVL. MAINTENANCE INSPECTED THE FLAPS, ACTUATORS, SPOILERS AND HYDRAULIC SYSTEM FOR LEAKS. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040422000162004042200016EA 2004 4 22 ASOA04205 120040312A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED AND THE LOWER STEP SUPPORT ROD (P/N 601R317198-1) REQUIRING ADJUSTMENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP AND ADJUSTED THE LOWER STEP SUPPORT ROD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040422000182004042200018EA 2004 4 22 ASOA04201 120040312A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11866AS 7517 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, RBL 9 AND LBL 9 INBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, RBL 9 AND LBL 9 INBOARD IAW SRM 51-40-00. (M) 2L72 4F RTA21EA 20040422000202004042200020WP 2004 4 22 ASAA0480015 120040119A532199365521 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS DISBONDING AND HAS CORRODED FASTENERS AT FS 196-256. REPLACED CHANNEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000222004042200022WP 2004 4 22 ASAA0480017 120040119A532199366881 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 DURING HV-1 CHECK, FOUND CABIN FLOOR PANEL IS CRACKED ON UNDERSIDE AT FS 674-693. REPLACED CHANNEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000262004042200026WP 2004 4 22 ASAA0480042 120040126A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 DURING INSPECTION, FOUND AFT PIT LOWER FLANGE ON BEAM AT CARGO DOOR IS CORRODED AT STATION 1182. REPAIRED BY REMOVED DAMAGED BEAM, INSTALLED NEW BEAM IAW MD80 SRM 51-30-2, 51-30-5, 51-10-3. (M) 2L72 4F RTA6WE 20040422000272004042200027WP 2004 4 22 ASAA0480065 120040201A532199365501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 DURING HV1 CHECK, FOUND CABIN FLOOR PANEL IS CRACKED AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040422000292004042200029WP 2004 4 22 ASAA0480074 120040215A532059360717 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 OKC - DURING HV1-CHECK, FOUND INTERCOSTAL CORRODED AT FS 1212-1231. REPLACED INTERCOSTAL PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040422000312004042200031WP 2004 4 22 ASAA0480033 120040126A53219957918524 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING INSPECTION, FOUND CABIN FLOOR PANEL FOR STATION 693-769 BETWEEN RBL 44 AND RBL 54 HAT CHANNEL ON UNDERSIDE IS CRACKED. REPAIRED IAW MD80 SRM 51-70-5. (M) 2L72 4F RTA6WE 20040422000322004042200032WP 2004 4 22 ASAA0480034 120040126A53205936597529 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 DURING INSPECTION, FOUND AFT CARGO FLOOR SUPPORT STATION 1080 HAS EXFOLIATION ON UNDERSIDE AT NUTPLATES ABOVE LONGERON 30 TO 28L. REPAIRED BY REMOVING EXFOLIATED PART AND INSTALLED NEW PART PER MD80 SRM 51-10-4. (M) 2L72 4F RTA6WE 20040422000342004042200034 2004 4 22 SWIA200413141 420040411A3418C818171 TRANSDUCER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING DEDESCENT 1 NM07157327729 6368 120195 ON DESCENT, RECEIVED STALL WARNING AURAL AND MAP LIGHT FOR SYSTEM 1; ALSO HAD -SPD- FLAG ON EADI, INTERMITTENT THROUGH LANDING. REMOVED AND REPLACED AOA TRANSDUCER AND STALL WARNING COMPUTER. OPS CHECKS GOOD. STALL WARNING COMPUTER P/N OFF: C-81806-3, S/N OFF: 111. 2L72 4T RTA31SO 20040422000362004042200036EA 2004 4 22 SWIA200413143 120040220A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07923SW 7664 CRACKED INTERCOSTAL AT STA X484.00 BETWEEN LBL 27 AND LBL 36 (OUTBOARD). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV A. 2L72 4F4 FRTA21EA E15NE 20040422000402004042200040WP 2004 4 22 ASAA0480053 120040130A5320593607121 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND INTERCOSTAL IS CORRODED AT FS 1221. REPLACED INTERCOSTAL PER SRM 51-10-4, 51-10-2, AND 51-30-5. (M) 2L72 4F RTA6WE 20040422000412004042200041WP 2004 4 22 ASAA0480054 120040130A53135936667 STRINGER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND STRINGER IS CORRODED UNDER LOWER FLANGE AT FS 1212. REMOVED DAMAGED SECTION. REPLACED WITH SPLICE PER SRM 53-02, 51-10-3, AND 51-60-0. (M) 2L72 4F RTA6WE 20040422000432004042200043WP 2004 4 22 ASAA0480056 120040130A53305924802541 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURNG 15K CHECK, FOUND FUSELAGE SKIN IS DENTED AT FS 237. INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040422000442004042200044WP 2004 4 22 ASAA0480060 120040130A5347593056671 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS 53024 OKC - DURING 15K CHECK, FOUND LEFT OUTBOARD SEAT TRACK IS CORRODED AT FS 1106-1185. REPLACED DAMAGED TRACK PER SRM 51-10-4 AND 51-30-5. (M) 2L72 4F RTA6WE 20040422000482004042200048NM 2004 4 22 UPS04442217 120040329A575365B078751 RIB BOEING747 747121 1384871NM NR 8 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 8 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 8 VC FLAP OLES 938 O/B ARM O/B RIB ROTARY ACTUATOR NR 2 MOUNTING BOLT HOLE OVERSIZED TO 0.388 INCH, BUSHING FABRICATED & INSTALLED. 2L74 4F A20WE 20040422000492004042200049NM 2004 4 22 UPS04442218 120040329A575365B1014011 RIB BOEING747 747121 1384871NM NR 7 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP O/B ARM I/B RIB ROTARY ACTUATOR NR 2, 3, 4, 5, 7 BOLT HOLES CORRODED (LOOKS O/B, COUNTS CLOCKWISE FROM TOP). DUE CORROSION BLEND OUT EXCEED MAX DIA 0.371 INCH, LEFT WING NR 7 VC FLAP OLES 1015 O/B ARM I/B RIB REPLACED AS PER SRM 51-10-01 PG 8, VC FLAP R & I PER MM 27-81-02, RIGGING & OPERATION CHECK C/OUT PER MM 27-81-00, BUSHING FABRICATED & INSTALLED. 2L74 4F A20WE 20040422000522004042200052WP 2004 4 22 ASAA0480038 120040126A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING INSPECTION, FOUND MAIN CABIN STATION 628 X= -44 CORROSION ON SEAT TRACK. REPAIRED BY REMOVING DAMAGED SECTION. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK AND TWO SPLICES IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040422000582004042200058WP 2004 4 22 UPS04842224 120040403A5320559764631 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 25 AT LONG 21L ANGLE IN FWD ENTRY DOOR FWD JAMB IS CRACKED. REMOVED, CRACKED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL IAW DWG 5597646 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040422000622004042200062 2004 4 22 ASAA0480030 420040126A25653961896501 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01967AS 49103 SEA - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F A6WE 20040422000652004042200065WP 2004 4 22 ASAA0480036 120040126A5313593643923 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 OKC - DURING INSPECTION, FOUND MID CARGO PIT STATION 598-617 LONGERON 30 CORRODED AROUND FASTENERS. REPAIRED BY REMOVING CORROSION, SPOT FACED AREA, IAW EA 5310-02311 AND AAR EA 10234. (M) 2L72 4F RTA6WE 20040422000702004042200070 2004 4 22 ASAA0480075 420040218A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 SEA - FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040422000742004042200074WP 2004 4 22 UPS04842231 120040402A53203750545U501 SPLICE DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 LONG 35L SPLICE FITTING IS CRACKED STATION 1040-1060. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D. 2L74 4F RT4A25 20040422000762004042200076 2004 4 22 SWIA200413121 420040328A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AUTOPILOT SYS FAULTY A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07579SW9597 9597 120347 RATCHETING NOISE HEARD WITH SLIGHT NOTCH FEELING WHEN YOKE IS MOVED TO FULL AFT POSITION. MOVED YOKE THROUGH TRAVEL WITH A/P ON, SEEMED TO CLEAR PROBLEM. REPLACED AUTOPILOT ELEVATOR SERVO. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T4 TRTA31SO E20NE 20040422000812004042200081 2004 4 22 SWIA200413124 420040403A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING FAILED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07250YV 120250 BOTH STALL WARNING SYSTEMS WILL NOT TEST. THE RED STALL WARNING TEST LIGHTS STAY ILLUMINATED AFTER TESTING. REPLACED STALL WARNING COMPUTER WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040422000842004042200084WP 2004 4 22 UPS04842183 120040301A53203779659501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 LONGERON 3L BATHTUB FITTING CRACKED AT STA 902. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20 D, AND DC8 MM 20-1400. 2L74 4F RT4A25 20040422000852004042200085WP 2004 4 22 UPS04842184 120040301A5320377976U501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 LONGERON 7R BATHTUB FITTING CRACKED AT STA 680. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 5 1-1-24, AND INSTALLED FITTING IAW DC8 SRM 51-1-20D AND DC8 MM 20-14-00. 2L74 4F RT4A25 20040422000892004042200089WP 2004 4 22 UPS04842190 120040303A5720 CHANNEL DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 HAT CHANNEL FWD OF J-HOOK (FOR MLG DOOR RELEASE) IS CRACKED. REMOVED CRACKED HAT CHANNEL, FABRICATED NEW HAT CHANNEL IAW DAC DWG S-1 289798, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW HAT CHANNEL IAW DC8 SRM 51-3-1. 2L74 4F RT4A25 20040422000902004042200090WP 2004 4 22 UPS04842193 120040313A5315 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 MAIN CABIN FS 1660 FLOORBEAM AT LBL 20-LBL 30 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND PRE-EXISTING PLUG AT SEAT TRACK ATTACH HOLE OUT OF LIMITS. ROUTED OUT DAMAGE & FAB REPAIR ANGLE AND FILLER IAW DC8 SRM 51-2-1 FIG 1 SHT 7 TR 51-130. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-2-1 FIG 1 SHT 7 TR 53-138 AND DC8 SRM 51-1-20D FIG 4A. 2L74 4F RT4A25 20040422000912004042200091WP 2004 4 22 UPS04842194 120040406A53203641778 STIFFENER DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 2 EA DIAGONAL STIFFENERS FOR STA 8 BULKHEAD HAVE PREVIOUSLY CUTOUT DAMAGE ON LOWER ENDS. FABBED REPAIR ANGLE DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040422000922004042200092WP 2004 4 22 UPS04842196 120040320A53305644130 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 EXT FUSELAGE AT FS 1700 APPROX BETWEEN L16R AND L17R FASTENER HOLE CRACKED RUNNING FWD. CUT OUT DAMAGED AREA IAW DC8 SRM 53-2-1. FABBED DOUBLER, FINGER DOUBLER, AND FILLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040422000942004042200094WP 2004 4 22 UPS04842198 120040401A575557075344 BRACKET DOUG DC8 DC871F 302199DWP NR 2 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 RIGHT WING NR 2 SPOILER O/B MOUNT BRACKET CRACKED. REMOVED AND REPLACED RIGHT WING 32 SPOILER O/B MOUNT BRACKET IAW UPS DC8 SRM 51-1-21, 51-1-20D, AND 51-3-1. 2L74 4F RT4A25 20040422000952004042200095WP 2004 4 22 UPS04842199 120040303A53134615293 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AT APPROX STA 22 L34L FOUND TO HAVE PREVIOUS DAMAGE. REMOVED LONGERON IAW DC8 SRM 51-1-21. BLENDED GOUGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. RECEIVED NEW LONGERON, LOCATED, DRILLED IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040422000962004042200096WP 2004 4 22 UPS04842203 120040228A53203779659501N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 LONGERON 8L BATHTUB FITTING CRACKED AT STA 902. REMOVED CRACKED FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED SERVICEABLE FITTING IAW DC8 SRM 51-1-20D, AND DC8 MM 20-14-00. 2L74 4F RT4A25 20040422000992004042200099WP 2004 4 22 UPS04842141 120040225A532037502571 SPLICE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT PIT AT STA 1050 STR 31R LONGERON SPLICE CRACKED. REMOVED LONGER SPLICE IAW DC8 SRM 51-1-20D. RECEIVED, LOCATED AND DRILLED NEW SPLICE IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040422001112004042200111WP 2004 4 22 UPS04842156 120040229A53133898405 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT ACCESSORY COMPT AT STA 1545 STR 26R INSIDE AND OUTSIDE OF LONGERON HAS CORROSION. REMOVED DAMAGED SECTION IAW DC8 SRM 51-1-21. RECEIVED NEW LONGERON SECTION. LOCATED AND DRILLED NEW LONGERON SECTION AND SPLICE IAW DC8 SRM 51-1-24. INSTALLED LONGERON AND SPLICE IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040422001152004042200115WP 2004 4 22 UPS04842161 120040301A532037502711 SPLICE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 MAIN CABIN BETWEEN STA 1040 AND STA 1060 STR 1 SPLICE FITTING CRACKED. HFEC IAW DC8 NDT SPM 06-10-01.001. CRACK FOUND; REMOVED SPLICE FITTING AND REC'D NEW SPLICE LONGERON, LOCATED AND DRILL HOLES IAW DC8 SRM 51-1-24. INSTALLED NEW SPLICE LONGERON IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040422001202004042200120SW 2004 4 22 EAT2004F00002 120040311A3230 DRAG BRACE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP NLG CORRODED B EATRO OTHER O OTHER NRNOT REPORTED 1 GL09329BA TC238 DURING AN INSPECTION THE DRAG BRACE FOR THE NOSE LANDING GEAR WAS FOUND TO BE WORN BEYOND LIMITS. AFTER REMOVING THE DRAG BRACE THE PINS THAT ATTACH THE DRAG BRACE TO THE UPPER CYLINDER WERE FOUND PITTED AND INSIDE THE LUG BORE CORROSION WAS FOUND IN EXCESS OF .080 DEEP, WELL BEYOND ANY REPAIRABLE LIMITS. THIS AREA NEVER GETS PULLED APART UNLESS A PROBLEM THAT REQUIRES REMOVAL OF THE DRAG BRACE IS FOUND. THE GREASE ZERK ON THE LINK DOES NOT FORCE ANYTHING INTO THIS AREA TO REMOVE MOISTURE. IT WOULD BE ADVISABLE TO REMOVE THESE YEARLY TO CLEAN AND GREASE THEM TO PREVENT FUTURE CORROSION PROBLEMS. 2L72 4T3 TRTA8SW E2WE 20040422001222004042200122NM 2004 4 22 USA2004F00022 120040330A2120 ODOR BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE GALLEY DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19608AU 22204 CREW NOTED A BURNING ODOR IN THE AFT GALLERY. MAINTENANCE COULD NOT FIND A PROBLEM. AN ENGINE RUN WAS PERFORMED. THE CONDITION COULD NOT BE DUPLICATED. 2L72 4F4 FRTA2NM A12EU 20040422001232004042200123EU 2004 4 22 KBM2004F00018 120040122A7921MS5750V01 BLOWER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL COOLER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 OIL COOLER MOTOR INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE. 1G71 3U3 U H9EU E19EU 20040422001292004042200129SW 2004 4 22 ALG2004F00012 120040309A3050 WARNING LIGHT BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE ILLUMINATED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW033912Q 3271 CAE820628F AT TAKE OFF, DURING CLIMP OUT ENGINE CHIP LIGHT FLUCUATED ON AND OFF. MAINTENANCE REMOVED BOTH CHIP PLUGS, FOUND NOTHING ON EITHER. CLEANED CONNECTORS, REINSTALLED AND COMPLIED WITH OPERATIONAL GROUND RUN CHECK, CHECKED GOOD. 1G71 3U3 U H2SW E4CE 20040422001312004042200131SO 2004 4 22 AW42004F00000 220040323A8530SA643873 VALVE CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO NR2 CYLINDER BROKEN B AW4RA UNSCHED LANDING REJPARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 WP113911G950 340A0230 228542 DURING CRUISE, THE EGT INDICATION FOR THE NR 2 CYL OF THE RT ENGINE DROPPED TO ZERO. THIS WAS ACCOMPANIED BY VIBRATION, SLIGHT LOSS OF MANIFOLD PRESSURE AND A SLIGHT DECREASE IN THE CHT AND EGT INDICATIONS FOR CYLINDERS NR 4 AND NR 5. RETURNED TO DEPARTURE BASE. ENGINE WAS NOT SHUT DOWN. UPON COMPRESSION CHECK, NR 2 CYLINDER WAS FOUND WITH ZERO COMPRESSION. A BORESCOPE INSPECTION REVEALED A FAILURE OF THE EXHAUST VALVE. INSPECTION OF THE OTHER CYLINDERS ALSO SHOWED CONSIDERABLE DAMAGE TO NR 5 CYL AND MINOR DAMAGE TO SEVERAL OTHERS. WHEN INDUCTION SYSTEM BALANCE TUBE WAS REMOVED, A PIECE OF VALVE WAS FOUND. (WP272003B2874) 1L72 3O3 O 3A25 E8CE 20040422001342004042200134SW 2004 4 22 ALG2004F00015 120040320A2840407375006101 INDICATOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL FUEL QUANTITY FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL 53357 DURING TAKE OFF FUEL QUANTITY GUAGE LOST POWER, RECYCLED QUANTITY CIRCUIT BREAKER 3 TIMES, QUANTITY INDICATOR CAME ON AND AT THE SAME TIME RT TRANSFER PUMP CAUTION ILLUMINATED. RECYCLED RT PUMP CIRCUIT BREAKER BUT COULD NOT EXTINGUISH TRANSFER PUMP LIGHT. QUANTITY GUAGE FAILED AGAIN BEFORE LANDING. MAINTENANCE REPLACED FUEL QUANTITY INDICATOR PN 407375006101 SYSTEM CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20040422001412004042200141NE 2004 4 22 PA04001 220040305A73201501KDC03005 EEC GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE RT ENGINE INOPERATIVE E UG8AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23920DC 1772 534 RT ENGINE ROLLED BACK AFTER TAKE OFF ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CH. B AND ENGINE OK. 2L72 4F4 FRTA12EA E00057EN 20040422001502004042200150NE 2004 4 22 MDR04040 120040122A64106516100010041 BLADE SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE TAIL ROTOR CRACKED B JYDRK NONE O OTHER ININSP/MAINT 1 NM09229AC848 64018 DURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND: TWO SPANWISE CRACKS EXIST AT THE TRAILING EDGE ON THE OB SIDE. THE FIRST CRACK IS 7.25 INCH FROM OB END OF THE POCKET AND IS 1.25 INCH IN LENGTH. THE SECOND CRACK IS 14.5 INCHES FROM THE OB END OF THE POCKET AND IS 1.125 INCHES IN LENGTH. BOTH CRACKS ARE .375 INCH FROM THE TRAILING EDGE. THESE CRACKS ARE AT THE LEADING EDGE OF THE INSERT THAT RUNS THE LENGTH OF THE TRAILING EDGE. PROBABLE CAUSE IS UNKNOWN. 2G72 4U4 U H4EA E15EA 20040422001532004042200153CE 2004 4 22 GM0409 120040331A2611 SMOKE DETECTOR CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL BAGGAGE COMPT DIRTY E UG8AO OTHER N FALSE WARNING NRNOT REPORTED 1 GL235116 7500019 BAGGAGE SMOKE LIGHT(EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFT LANDING. BAGGAGE SMOKE DETECTER FOUND TO BE VERY DIRTY. INITATED A FLEET INSPECTION AND CLEANING OF DETECTERS. REMOVED SMOKE DETECTER AND CLEANED ALSO CLEANED COVER AND MOUNTING AREA. REINSTALLED AND PERFORMED FUNCTIONAL CHECK. SYSTEM CHECKED GOOD. 2L72 4J4 FRTT00007WITE6CH 20040422001542004042200154NE 2004 4 22 ALG2004F00014 120040305A261130326E7 AMPLIFIER SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL CARGO BAY INOPERATIVE E ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW03702AL 760243 CAE8900262S THE BAGGAGE SMOKE DETECTOR CAUTION LIGHT CAME ON 3 TIMES OVER A TWO MINUTE PERIOD. THERE WAS NO OTHER INDICATION OF FIRE OR SMOKE, WITH THE LIGHT OUT WE LANDED. MAINTENANCE REPLACED SMOKE DETECTOR CONTROL AMPLIFIER AND REPLACED CONNECTOR AT THE SMOKE DETECTOR. 1G72 3U3 U H1NE E1GL 20040422001582004042200158WP 2004 4 22 UPS04842166 120040402A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 1000 BETWEEN LONG 28L TO 29L SHEAR TIE IS CORRODED. REMOVED, FABRICATED AND REPLACED SPLICE PLATE AND FILLER IAW SRM 53-2-0 FIG 2A AND 2B. 2L74 4F RT4A25 20040422001592004042200159NM 2004 4 22 MXO2004F00000 120040401A3246LM522546 BEARING BOEING727 727233 138408ANM MAIN WHEEL CONTAMINATED E MXOAO OTHER E VIBRATION/BUFFET LDLANDING 1 WP01265FE116 21671 WHILE LANDING, THE FLIGHT CREW NOTICED A SHIMMY IN THE LANDING GEAR. BELIEVING THAT THEY HAD BLOWN A TIRE, THEY STOPPED ON A TAXIWAY AND NOTIFIED MAINTENANCE, INSPECTED THE LANDING GEAR. A BLOWN TIRE WAS NOT THE CASE AND MAINT RELEASED THE AC TO TAXI TO RAMP WHERE THE AC WAS THOROUGHLY INSPECTED. AFTER INSPECTING THE LANDING GEAR, BRAKES AND TORQUE LINKS, THE NR 1 AND NR 4 MAIN WHEEL ASSEMBLIES WERE INSPECTED AND WATER CONTAMINATION WAS FOUND IN THE BEARINGS OF THESE WHEEL ASSEMBLIES. MAINTENANCE REPLACED BOTH THE NR 1 AND NR4 MAIN WHEEL ASSEMBLIES AND INSPECTED NR 2 AND NR 3 MAIN WHEEL ASSEMBLIES AND THEY WERE FOUND SERVICEABLE. AIRCRAFT WAS DECLARED SERVICEABLE. NO FURTHER FAULTS WERE FOUND. 2L73 4F RTA3WE 20040422001612004042200161WP 2004 4 22 UPS04842167 120040402A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 STATION 1060 FRAME IS CORRODED BEYOND LIMITS AT LONG 35L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010. 2L74 4F RT4A25 20040422001662004042200166EU 2004 4 22 UPS04142234 120040420A2560321491 WARNING HORN AIRBUSA300 A300F4622R 3930360EU EVAC SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01126UP 0810 INSPECTION TYPE:N/A EVAC SLIDE WARNING BUZZER INOP M279503. REMOVED & REPLACED ASPSU PER AMM 52-73-18-4, CHECKED GOOD. 2L72 4F RTA35EU 20040422001672004042200167NM 2004 4 22 C7WA200400003 120040301A2612 WARNING LIGHT BOEING727 7272M7 138407SNM PWA JT8 JT8D9 52048NE CARGO FIRE ILLUMINATED A C7WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO17721RW 21200 LWR AFT CARGO FIRE LIGHT CAME ON AFTER TAKEOFF AND THEN EXTINGUISHED ON FINAL APPROACH BACK. ADDITIONALLY THE DUCT OVERHEAT LIGHT ON PILOTS OVERHEAD PANEL CAME ON AND REMAINED ON DURING FINAL APPROACH. TEMP PEGGED AT 250 DEGREES OR GREATER. OPS CHECK OF LOWER CARGO SMOKE DETECTION SYS NORMAL IAW MM. VISUALLY INSPECTED BLEED AIR DUCTS AND OVERHEAT SENSORS. PERFORMED HIGH POWER RUN NO LEAKS DETECTED. OVERHEAT SYSTEM TEST NORMAL IAW MM. 2L73 4F4 F A3WE E2EA 20040422001722004042200172NM 2004 4 22 UPS04242223 120040403A5754 RIB BOEING727 72731C 1384011NM L/E SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C NR 3 L/E SLAT, CRACK AT ACTUATOR ATTACH RIB (O/B RIB). REPAIR CARRIED OUT IAW SRM 51-30-02, 51-30-03, 57-50-03 & MM 28-81-11 & 27-00-00. 2L73 4F A3WE 20040422001732004042200173NE 2004 4 22 HCM2004F00001 220040407A7261 CHIP DETECTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE CONTAMINATED E HCMAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP13992BH 2889 9402 ON MARCH 20, 2004 WHILE ON A SIGHTSEEING FLIGHT, THE PILOT EXPERIENCED AN ENGINE CHIP LIGHT INDICATION. HE MADE A PRECAUTIONARY LANDING AT APPROXIMATELY 12:50 PM. A MECHANIC WAS DISPATCHED TO THE SITE AND INSPECTED ALL CHIP PLUGS. A SMALL SLIVER WAS FOUND AT THE OUTPUT OF THE OIL PUMP. NO FURTHER OCCURENCES WERE NOTED. 1G71 3U3 U H9EU E19EU 20040422001802004042200180EU 2004 4 22 BAQ2004F00000 120040326A672076CF8716 HOUSING UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE T/R CONTROL BROKEN B BAQRO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 THE TAIL ROTOR/ ANTI-TORQUE BALL BEARING CONTROL SYSTEM CONTROL CABLE HOUSING BROKE AND SEPARATED FROM THE ACTUATOR HOUSING NEAR THE AFT SUPPORT ON THE TAIL BOOM. THIS DISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION. 1G72 3U3 U H88EU E34NE 20040422001852004042200185SO 2004 4 22 AKG2004F00005 220040302A8530 CYLINDER PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO NR 6 FAILED B AKGRO OTHER O OTHER NRNOT REPORTED 1 CE05102RM4 347770069 THE NR 6 CYLINDER WAS FOUND CRACKED AROUND THE INSIDE OF THE STEEL PART ABOUT 1.5 INCHES FROM THE TOP WHERE IT SCREWED INTOTHE HEAD. THE CRACK IS ALMOST COMPLETELY AROUND THE CYLINDER. THIS CYLINDER IS A REPAIRED SERVICEABLE FROM ENGINE COMPONENTS WITH THE CERMINIL PROCESS. ENGINE WAS STILL RUNNING WHEN TAXIING TO THE RAMP, ONLY INDICATION PILOT HAD WAS BAD OIL LEAK. 1L72 3O3 O A7SO E9CE 20040422001872004042200187WP 2004 4 22 EOO2004F00001 120040227A6710369D27371 BUNGEE CYLINDER HUGHES369 369D 4470706WP M/R CONTROLS SLIPPED B EOORO OTHER O OTHER NRNOT REPORTED 1 AL03CFMAL 611010D COLLECTIVE WAS RATCHETY, FOUND THE BEARING ASSY (PN369D27371) WAS SPLIT ON ITS OUTER SLEEVE CAUSING INTERFERENCE BETWEEN IT AND THE INSIDE OF THE SPRING. REPLACED ENGIRE BUNGEE ASSY. 1G71 3U H3WE 20040422001892004042200189NM 2004 4 22 UIEA200400040 120040404A21216054578 FAN BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE FLIGHT DECK INOPERATIVE A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15516MC 22507 DURING TAXI IN, SMELL OF SMOKE FROM THE AIR CONDITIONING SYSTEM. FLIGHT DECK FAN SWITCHED OFF WITH NO FURTHER SMELL. AFTER SHUTDOWN, UNABLE TO SWITCH FAN BACK ON. CIRCUIT BREAKER PULLED AND ITEM TRANSFERRED DMI M04-064. REMOVED AND REPLACED FLIGHT COMPARTMENT RECIRCULATION FAN IAW MM. OPERATION CHECK NORMAL. GOOD FOR SERVICE. 2L74 4F4 F A20WE E23EA 20040422001902004042200190NM 2004 4 22 UIEA200400043 120040407A541065B8904942 FRAME BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE INSPECTION OF NR 3 PYLON, THE BULKHEAD UPPER ASSEMBLY RHS FORWARD ANGLE FRAME FLANGE WAS FOUND CRACKED AT THE END FASTENER HOLE COMMON TO THE FRONT SPAR FITTING AND STRUT CAP SKIN ASSY. FABRICATED A REPAIR ANGLE TO RESTORE THE DAMAGED ANGLE SECTION, EXCEPT EXTENDED IT TO MATCH THE EXISTING FRAME ANGLE. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040422001912004042200191NM 2004 4 22 USA2004F00017 120040301A49902380 TURBOCHARGER BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE APU BAY OVERSERVICED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19397US P34602 23319 ON DESCENT, CREW REPORTED STRONG EXHAUST FUMES IN THE AFT CABIN. NO SMOKE WAS NOTED. CREW TURNED RIGHT PACK TO HIGH AND RECIRCULATION FAN TO OFF WITH NO CHANGE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU OIL OVERSERVICED. REMOVED OIL TO PROPER LEVEL. OPERATIONAL CHECK OF APU NORMAL. 2L72 4F4 FRTA16WE E2GL 20040422001932004042200193NE 2004 4 22 MDR04041 120040122A64106516100010041 BLADE SKRSKYS64 S64E 8142604NE TAIL ROTOR CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09CGESG42069 64065 DURING NORMAL AIRCRAFT INSPECTIN, THE FOLLOWING WAS FOUND. THE OB SIDE OF THE POCKET HAS THREE CRACKS RUNNING SPANWISE APPROXIMATEL .398 INCH FROM THE TRAILING EDGE. THE FIRST CRACK IS 75 INCH FROM THE TIP END AND .835 INCH LONG. THE SECOND CRACK IS 9 INCH FROM THE TIP END AND .705 INCH LONG. THE THIRD CRACK IS 11.875 INCH FROM THE TIP END AND .684 INCH LONG. PROABABLE CAUSE IS UNKNOWN. 2G72 4U H4EA 20040422001942004042200194NM 2004 4 22 UPS04442213 120040329A575365B078731 RIB BOEING747 747121 1384871NM NR 7 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP I/B ARM O/B RIB ROTARY ACTUATOR NR 1, 3, 4, 5, 7, 8 MOUNTING BOLT HOLES CORRODED (LOOK O/B, COUNTS CLOCKWISE FROM TOP). LEFT WING NR 7 VC FLAP OLES 974 I/B ARM O/B RIB ROTARY ACTUATOR NR 1, 3, 4, 5, 7, 8 MOUNTING BOLT HOLES OVERSIZED TO 0.371 INCH, BUSHINGS FABRICATED & INSTALLED. 2L74 4F A20WE 20040422001962004042200196EA 2004 4 22 SWIA200413128 120040403A2751855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07907SW5632 5632 7511 EN ROUTE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. LANDED FLAPS 0 AT SLC. REPLACED LEFT SIDE BPSU PER CRJ MM 27-51-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20040422002012004042200201SO 2004 4 22 CHQA000478 120040408A3350 LIGHT EMB 145 EMB145LR 3260212SO RT WING INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11287 145460 RIGHT WING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT WING EMERGENCY EXIT LIGHT IAW EMB 145 MM CH 33-50. OPS CHECK GOOD. P/N 1317. 2L72 4T RTT00011AT 20040422002072004042200207GL 2004 4 22 CHQA000474 220040404A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ODOR A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11289 145463 AFTER ROTATION OUT OF IND, STARTED TO SMELL FUMES. THERE WAS NO EVIDENCE OF SMOKE IN THE CABIN BUT THE F/A REPORTED THE ODOR WAS STRONGER IN THE FRONT. DECISION WAS MADE TO RETURN TO IND. THE ODOR DID START TO DISSIPATE DURING LANDED. MAINTENANCE CHECKED THE AIRCRAFT AND ADVISED NR 1 ENGINE WAS JUST REPLACED AND THE ODOR POTENTIALLY WAS DUE TO THE NEW ENGINE. NO EVIDENCE AT ALL FOR ANY OTHER CAUSE OF THE SMELL. ACFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040422002142004042200214 2004 4 22 UIEA200400046 420040408A25657A14124 SLIDE BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE UPPER DECK MALFUNCTIONED A UIEAK NONE L NO TEST ININSP/MAINT 1 EA15808MC 21048 UPPER RT EMERGENCY DOOR SLIDE PARTIAL DEPLOYMENT; DURING UPPER RT EMERGENCY DOOR SLIDE RAFT ASSEMBLY DEPLOYMENT TEST, SLIDE/RAFT FAILED TO FULLY INFLATE. SEQUENCING MECHANISM RELEASED TO FACILITATE SLIDE RAFT REMOVAL AND DISPATCH TO STOP. NOTE: ACTUAL OR APPARENT CAUSE OF PARTIAL DEPLOYMENT IS BEEN INVESTIGATED DURING THE SLIDE OVERHAUL. 2L74 4F4 F A20WE E23EA 20040422002172004042200217NM 2004 4 22 USA2004F00024 120040328A2572806007 CIRCUIT CARD BOEING737 737301 1384611NM E11 SHELF/ FAULTY A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19576US 23741 ON CLIMBOUT, THE LT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE M987 PRINTED CIRCUIT CARD. ALSO, ADJUSTED UPLOCK SENSOR ON LT MAIN LANDING GEAR AND REPLACED WORN UPLOCK ROLLER ON STRUT. GEAR RETRACTION AND EXTENSION, POSITION INDICATING AND WARNING SYSTEM NORMAL IAW MM. 2L72 4F RTA16WE 20040422002192004042200219NM 2004 4 22 AWXA200400381 120040401A532065C326778 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 994, LBL 17.5, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 994, LBL 17.5, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7, STEP D. 2L72 4F RTA16WE 20040422002222004042200222NM 2004 4 22 AWXA200400383 120040401A532065528941 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN ANGLE AT BS 540, LBL 0.8, WL 208. MAINTENANCE REMOVED CRACKED ANGLE AT BS 540, LBL 0.8, WL 208; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-04 FIG 1 PG 2. 2L72 4F RTA16WE 20040422002232004042200223NM 2004 4 22 MYW2004F00000 120040129A2930 FILTER BOEING737 737* NM HYD SYSTEM INOPERATIVE A MYWAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO19GXLAC 29051 AT CRUISE, APPROX 2 HRS INTO FLIGHT GL511 SYSTEM (A) ELECTRIC HYDRAULIC OVERHEAT LIGHT ON. SWITCH TURNED OFF IAW PROCEDURES. LIGHT OUT IO APPROX 3 MINUTES. APPROX 3.5 HRS INTO FLT LOST SYSTEM (A) HYDRAULIC PRESSURE, DIVERTED. TROUBLESHOT SYSTEM IAW TASK 805 PARA E1D AND FOUND SYSTEM OPERATIONAL. REPLACED ELECTRIC HYD AND EDP CASE DRAIN FILTERS. FOUND METAL EDP CASE DRAIN FILTER. REPLACED FILTERS. MAINTENANCE FERRIED AIRCRAFT. REMOVED AND REPLACED NR 1 EDP IAW MM. SYSTEM OPERATIONAL CK NORMAL. LEAK CK OK. RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA16WE 20040422002292004042200229NM 2004 4 22 AWXA200400388 120040401A5320654585512 SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SCUFF PLATE (ZEE ANGLE) BS 967 TO BS 981, RBL 56, WL 209. MAINTENANCE REMOVED CORRODED ZEE ANGLE FROM BS 967 TO BS 981, RBL 56, WL 209; FABRICATED A NEW REPLACEMENT ZEE ANGLE PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040422002322004042200232SO 2004 4 22 SIMA200405902 120040225A27303621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMAO OTHER O OTHER LDLANDING 1 SW21731BE 145356 AFTER LANDING, DURING TAXI, CREW REPORTED THE PITCH TRIM 1 AND 2 INOPERATIVE ILLIMINATED. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200404646) 2L72 4F4 FRTT00011ATTE6CH 20040422002372004042200237EA 2004 4 22 SWIA200413132 120040409A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA T/E FLAP BROKEN A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07409SW 7056 FLAPS FAILED AT 17 DEGREES AFTER TAKEOFF AT SLC. RETURNED TO SLC. FOUND WIRE BROKEN AT PIN -K- ON CANNON PLUG 2P2CE TO RT BPSU AND CANNON PLUG SOCKETS CORRODED. REPLACED CANNON PLUG 2P2CE WITH A SERVICEABLE UNIT IAW CRJ WM 20-17-80. FLAPS SYSTEM OPERATES NORMALLY. P/N: D38999-26WC98SN. 2L72 4F RTA21EA 20040422002382004042200238 2004 4 22 SWIA200413133 420040408A3418 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07915SW 7615 DURING STALL TEST -STALL FAIL- CAUTION MESSAGE APPEARED. REPAIRED BROKEN WIRE ON STICK SHAKER ON FIRST OFFICER'S YOKE AS REQUIRED. OPS CHECKED GOOD IAW MM 27-35-00. 2L72 4F4 FRTA21EA E15NE 20040423000032004042300003CE 2004 4 23 YNO2004F00000 120040412A323399121112 ACTUATOR CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE RT MLG WORN A YNOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA1162NS 3330 S5500072 10214S DEPARTED AIRPORT, WHEN GEAR WAS SELECTED UP THE RT MAIN GEAR WOULD NOT COME UP AND LOCK. THE PILOTS COMPLETED THE CHECKLIST THE GEAR WAS SELECTED DOWN AND HAD AN ALL GEAR SAFE CONDITION. THE AIRCRAFT DIVERTED AND LANDED WITH NO PROBLEM. I AM REQUESTING A ONE TIME FERRY PERMIT FOR THIS AIRCRAFT TO FLY FOR TROUBLESHOOTING AND REPAIRS. THE GEAR WILL BE LEFT DOWN, VFR DAY OLY. I HAVE PERSONALLY LOOKED OVER THE ENTIRE AIRCRAFT AND CAN FIND NO DAMAGE. I BELIEVE THE AIRCRAFT IS SAFE FOR THE FERRY TRIP. 1L72 4F4 FRTA22CE E1NE 20040423000052004042300005EA 2004 4 23 MW22004F00000 220040304A8530 STUD PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA NR 3 CYLINDER BROKEN B MW2RO OTHER O OTHER NRNOT REPORTED 1 GL175481T 327240107 L992948 NR 3 CYLINDER OFF ENGINE. ALL 8 CLY HOLD DOWN STUDS BROKE, ROD OFF CRACKSHAFT. FLIGHT OK TIL TURN TO DOWN WIND TO LAND, ENGINE FAILED AND AIRCRAFT LANDED SAFELY. 1L71 3O3 O A3SO 1E4 20040423000132004042300013EU 2004 4 23 RYNA54233 120040303A7540GA554912 TRANSDUCER AIRBUS320 A320233 3930329EU IAE V2500 V2500A1 NE NR 1 ENG PYLON FAULTY A RYNAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE07941LF 461 DURING CRUISE FLIGHT, ECAM DISPLAYED (LEFT WING AIR LEAK) MESSAGE. PERFORMED ECAM ACTION. RETURNED, AS A HEAVY WEIGHT LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE BLEED PRESSURE TRANSDUCER. 2L72 4F4 FRTA28NM E311NE 20040423000192004042300019SO 2004 4 23 AKV2004F00000 220040316A8530649168 CYLINDER BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO ENGINE CRACKED B AKVRA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CE05413J 2590 1607 TC831 CS1922308LP AIRCRAFT WAS AT A CRUISING ALTITUDE OF 6000 FT MSL WHEN PILOT HEARD A LOUD BANG AND FELT SEVERE VIBRATION. PILOT STATED THAT WHEN HE LOOKED OUT AT THE LEFT ENGINE HE SAW SMOKE AND OIL COMING FROM THE COWLING; AT WHICH TIME HE ELECTED TO SHUT THAT ENGINE DOWN. AFTER LANDING, VISUAL INSPECTION OF THE LT ENGINE VERIFIED THAT THE NR ONE CYLINDER BARREL WAS CRACKED. CAUSE OF FAILURE, UNKNOWN. 1L72 3O3 ORT3A16 3E1 20040423000212004042300021EU 2004 4 23 SDR2004011 120040217A612330048000018 AUTOFEATHER SYS AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE INOPERATIVE A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO21429AT 429 DURING TAKEOFF THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) DIS NOT ARM. CREW ABORTED THE TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE AUTO FEATHER UNIT. 2H72 4T4 TRTA53EU E20NE 20040423000252004042300025 2004 4 23 C7WA200400001 420040127A3422258733513 GYRO BOEING727 7272M7 138407SNM PWA JT8 JT8D9 52048NE COCKPIT INOPERATIVE A C7WAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO17721RW 21200 ABORTED TAKEOFF AT APPROX 80 KTS DUE TO FAILURE OF F/O DIRECTIONAL GYRO. REMOVED AND REPLACED VIRTICAL GYRO IAW MM. 2L73 4F4 F A3WE E2EA 20040423000382004042300038NM 2004 4 23 USAA040008 120040120A5320 STIFFENER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19587US 23932 PIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH, BS 1016 APBH BL-0. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER BOEING DWG 65C28106 REF EO 5302V112A. (M) 2L72 4F RTA16WE 20040423000392004042300039NM 2004 4 23 USAA040009 120040125A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19573US 23560 PIT - FOUND STRINGER WITH 5 INCH CORROSION, S25L AT STATION 356 VERTICLE LEG OF STRINGER. CORROSION LEVEL 2, TASK NR C53-201-01. REMOVED STRINGER DAMAGE, INSTALLED SPLICE SECTION PER EA 77521. (M) 2L72 4F RTA16WE 20040423000402004042300040NM 2004 4 23 USAA040007 120040109A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US50290 23315 PIT - FOUND FRAME CRACKED 1 INCH, BS 178 LEFT SIDE FRAME AT WL 207. SPLICED FRAME AT WL 212 EPR EO 5300V157 PART F. (M) 2L72 4F RTA16WE 20040423000422004042300042EU 2004 4 23 USAASA04025 120040316A3350321430 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19184US 1651 BDL - FOUND THE EMERGENCY POWER SUPPLY UNIT BATTERY WEAK AT THE R3 DOOR LOCATION. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POWER SUPPLY UNIT AT THE R3 DOOR LOCATION. (M) 2L72 4F RTA28NM 20040423000482004042300048 2004 4 23 GTIA040161 420040306A2565D29985107 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 ORD - FLT 433 - SLIDE PACK FELL OFF L2 DOOR. REMOVED AND REPLACED L2 DOOR SLIDE PACK. REMOVED SHIPPING PIN AND ATTACHED PULL CABLE. (M) 2L72 4F A6WE 20040423000492004042300049EA 2004 4 23 ASOA04187 120040308A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11839AS 7284 DURING A C-CHECK IN MCN, THE NR 1 EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY FLOOR LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040423000512004042300051EU 2004 4 23 USAASA04023 120040310A3350321430 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19764US 1369 LGA - THE EMERGENCY LIGHT TEST GAVE 'EPSU EMER R' MESSAGE ON TEST. MAINTENANCE REPLACED BATTERY FOR MID-CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040423000532004042300053WP 2004 4 23 GTIA040165 120040123A5753 VANE DOUG DC9 DC981 3022081WP TE FLAPS DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND TWO DENTS ON UPPER OF INBOARD RIGHT FLAP DENTS ARE ON VANE ASSEMBLY 31 INCHES FROM INBOARD EDGE. DENT IS OUT OF LIMITS. ON FURTHER INVESTIGATION FOUND EXTERNAL DOUBLER DISBONDED, SKIN DELAMINATION. REPAIRED DENTS. REPAIRED DOUBLER AND DELAMINATED AREA. (M) 2L72 4F A6WE 20040423000542004042300054WP 2004 4 23 GTIA040166 120040108A5753 FITTING DOUG DC9 DC981 3022081WP LT WING TE FLAP CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND LEFT WING INBAORD FLAP INBOARD ACTUATOR ATTACHED FITTING CRACKED. REMOVED LEFT INBOARD FLAP INBOARD ACTUATOR ATTACH FITTING. LOCATED AND DRILLED ATTACH FITTING. INSTALLED LEFT INBOARD FLAP INBOARD ACTUATOR ATTACH FITTING. (M) 2L72 4F A6WE 20040423000552004042300055WP 2004 4 23 GTIA040167 120040107A5755 SKIN DOUG DC9 DC981 3022081WP FLIGHT SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 RT WING INBOARD FLIGHT SPOILER DELAMINATED. REPAIRED DELAMINATED AREA. (M) 2L72 4F A6WE 20040423000592004042300059NE 2004 4 23 A6WA200460003 220040224A7321 FUEL CONTROL BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 2 ENGINE MALFUNCTIONED A A6WAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL31608AW E2049 NR 2 ENGINE FLAMED OUT DURING CRUISE FLIGHT. EMERGENCY CHECKLIST COMPLIED WITH. ENGINE WINDMILLED FOR 10 TO 15 MINUTES. REMVOED AND REPLACED FUEL CONTROL IAW AMM 73-20-01-401. REMOVED AND REPLACED OVERSPEED VALVE, UNDER FURTHER INVESTIGATION. (M) 2H74 4F4 F A49EU E6NE 20040423000602004042300060EU 2004 4 23 USAABA0404 120040303A274147148122 ACTUATOR AIRBUS330 A330323 3930335EU PITCH TRIM FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19677UW14265 0380 LGW - FLT 95 - CREW REPORTED THAT THE AIRCRAFT PITCHED NOSE UP WITH EITHER AUTOPILOT ENGAGED. FLIGHT RETURNED TO LGW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PITCH TRIM ACTUATOR. (M) 2L72 4F RTA46NM 20040423000622004042300062EA 2004 4 23 ASOA04150 120040222A5320601R3501163 SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR SILL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL SUPPORT AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL SUPPORT AT FS 562-72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040423000632004042300063EA 2004 4 23 ASOA04152 120040224A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA AIR CONDITIONER ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11919EV 7780 FLT 4650 - DURING DESCENT INTO DFW AND MLU, THE CREW NOTICED A BURNING ODOR DURING POWER CHANGES WITH THE PACK ON THE ENGINE BLEEDS AND WHEN SWITCHING BLEEDS FROM ENGINES TO THE AUXILIARY POWER UNIT. THE ODOR WAS STRONG DURING POWER CHANGES OR BLEED SWITCHING FOR A FEW SECONDS AND THEN DIMINISHED. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040423000642004042300064WP 2004 4 23 GTIA040164 120040114A5321 FLOOR PANEL DOUG DC9 DC981 3022081WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND FLOOR PANEL STATION 1079-1155 DETERIORATING. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040423000682004042300068SO 2004 4 23 C2XA04BT045 120040403A335020131A BATTERY PACK EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 CREW REPORTED, EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY ASSEMBLIES. OPS CHECKED GOOD IAW EMB145 AMM 33-50-04. AIRCRAFT RETURNED TO SERVICE. P/N OFF 2013-1A; S/N OFF 56460, 72238, 77815, AND 82294. 2L72 4F RTT00011AT 20040423000722004042300072GL 2004 4 23 C2XA04CL038 220040419A720023070401 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LEFT FAILED A C2XABA EMER. DESCENT UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CRCRUISE 1 SW2714991116656098 145278 CAE311147 THE CREW REPORTED NR 1 ENGINE VIBRATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO DAYTON AND LANDED. AFTER LANDING THE NR 1 ENGINE HAD A SMALL FIRE OUT THE BACK OF THE ENGINE. THE FIRE WAS EXTINGUISHED AND NO OTHER INCIDENT OCCURRED. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040423000732004042300073WP 2004 4 23 ABXA040136 120040331A531059114113 DOOR FRAME DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23972AX 47631 TWO CRACKS EMANATED FROM FASTENER ON FORWARD LOWER CARGO DOOR JAMB UPPER FORWARD CORNER, 6 INCHES ABOVE UPPER FORWARD DOOR STOP AT FS 372, BETWEEN LONGERONS 20 AND 21 RIGHT. FORWARD CRACK LENGTH WAS .0937 INCH LONG, AFT CRACK LENGTH WAS .1562 INCH LONG. REPAIRED AREA IAW EA 53100110 AND SERVICE REWORK DRAWING SR09530117. 2L72 4F A6WE 20040426000012004042600001WP 2004 4 26 ABXA040138 120040403A5320 CHANNEL DOUG DC9 DC932F 3022067WP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 FOUND BOLT PULLED OUT OF C-CHANNEL AT NR 11 9G NET ARM AT STA 207. DAMAGE WAS AT PREVIOUSLY REPAIRED AREA. REPAIRED DAMAGED AREA IAW REA D953-49568MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0. 2L72 4F A6WE 20040426000062004042600006SO 2004 4 26 C2XA04SH207 120040407A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO RT ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27185564383 145595 DURING C-CHECK THE RIGHT ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000072004042600007SO 2004 4 26 C2XA04IA050 120040419A335020133A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715985 145248 DURING PREFLIGHT INSPECTION THE FORWARD SECTION OF EMERGENCY LIGHTING ON THE FLOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LIGHTING STRIP BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040426000082004042600008SO 2004 4 26 C2XA04SH227 120040415A531514522459003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000102004042600010SO 2004 4 26 C2XA04SH229 120040415A532014525480003 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715555 145594 SHV- DURING C-CHECK THE CARGO DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040422001042004042200104WP 2004 4 22 UPS04842148 120040226A532037558411 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1200 BETWEEN L33R-34R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0; REMOVED DAMAGED FITTING, REC'D, LOCATED, AND DRILLED UP FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2G. 2L74 4F RT4A25 20040422001052004042200105WP 2004 4 22 UPS04842149 120040226A532037558412 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 AFT CARGO PIT AT FS 1230 AT L33R Z-FITTING IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMAGED FITTING IAW DC8 SRM 51-1-20D, REC'D, LOCATED AND DRILLED UP FITTING IAW DC8 SRM 53-2-0 FIG 2G, AND 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 2G. 2L74 4F RT4A25 20040422001082004042200108WP 2004 4 22 UPS04842153 120040228A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 IN CABIN AT FWD SIDE OF STA 680 L8R END FITTING IS CRACKED. REMOVED CRACKED LONGERON END FITTING, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D AND DC8 MM 20-14-00. 2L74 4F RT4A25 20040422001142004042200114WP 2004 4 22 UPS04842160 120040301A5320 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 857 L9R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D AND MM 20-14-00. 2L74 4F RT4A25 20040422001182004042200118SO 2004 4 22 LAT2004F00000 120040203A8011 STARTER PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA RT ENGINE FAILED E LATAO OTHER O OTHER NRNOT REPORTED 1 AL03357SA 802 318052162 L202768A UPON REACHING 1ST LEG OF TRIP, RT ENGINE WOULD NOT START. DISPATCHED MECHANIC TO AND REPLACED STARTER WITH NEW ASSEMBLY. AIRCRAFT RETURNED TO BASE. (AL03200412386) 1L72 3O3 O A20SO E14EA 20040422001302004042200130EU 2004 4 22 ULX2004F00004 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE SPOTLIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01225LA2653 3308 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATIONS- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U3 U H9EU E19EU 20040422001402004042200140NE 2004 4 22 UG82004F00000 220040305A73201501KDC03005 EEC GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE RT ENGINE FAULTY E UG8AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23920DC 534 RT ENGINE ROLLED BACK AFTER TAKE OF ABOUT 20 PERCENT. SWITCHED DAU NR 1 TO CH B AND ENGINE, OK. TROUBLESHOOTING REVEALED A FAULTY NR 2 EEC (ELECTRONIC ENGINE CONTROLLER). INSTALLED A SERVICEABLE EEC IAW MDG MM AND PERFORMED ENGINE OPERATIONAL CHECKS. ALL PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA12EA E00057EN 20040422001652004042200165WP 2004 4 22 UPS04842170 120040401A5320577384411 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CENTER POST UPPER ATTACH ANGLE IS CRACKED STATION 1766 BL 0. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773844 AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20040422001712004042200171NM 2004 4 22 UPS04242220 120040403A5754 RIB BOEING727 72731C 1384011NM L/E SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C NR 2 L/E SLAT CLOSURE RIB AT INBOARD END OF SLAT CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-20-1 & MM 20-10-05. 2L73 4F A3WE 20040422001762004042200176NM 2004 4 22 UPS04442212 120040329A575365B078701 RIB BOEING747 747121 1384871NM NR 7 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C LEFT WING - NR 7 VC FLAP O/B ARM O/B RIB ROTARY ACTUATOR NR 4, 5 MOUNTING BOLT HOLES CORRODED (LOOKS O/B COUNTS CLOCKWISE FROM TOP). LEFT WING NR 7 VC FLAP OLES 1024 O/B ARM O/B RIB ROTARY ACTUATOR NR 4, 5 MOUNTING BOLT HOLES OVERSIZED TO 0.388 INCH, BUSHINGS FABRICATED & INSTALLED. 2L74 4F A20WE 20040422001822004042200182NE 2004 4 22 AMTA200400244 220040304A7323FFG052AE GOVERNOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE ENGINE MALFUNCTIONED A AMTAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 GL11560TZ2263 33525 31877 DURING ENGINE RUNS, NR 1 ENGINE FLAMED OUT, CHECKED ENGINE, RESTARTED OK. LT ENGINE SURGE ON EICAS AFTER SHUTDOWN. REMOVAL AND INSTALLATION OF FUEL FLOW GOVERNOR AS REQUIRED IAW AMM. 2L72 4F4 FRTA2NM E12EU 20040422001882004042200188NM 2004 4 22 UIEA200400038 120040406A5330 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE FUSELAGE DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 DURING D CHECK, SKIN DENT FOUND ON FWD CARGO DOOR CUTOUT. A SKIN GOUGE ON THE SKIN OF THE FORWARD CARGO DOOR CUTOUT AFT SKIN EDGE, BS670, BETWEEN S-37 AND S-38 WAS REPAIRED BY TRIMMING OUT THE GOUGE. A HFEC AND DETAILED VISUAL INSPECTION WITHIN 20 INCHES WAS ACCOMPLISHED. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040422001982004042200198SO 2004 4 22 CHQA000470 120040322A3350 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11292 145488 AFT CEILING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040422002002004042200200GL 2004 4 22 CHQA000477 220040408A7230 COMPRESSOR EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 2 ENGINE DAMAGED A CHQAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL11841 145737 CAE312428 FLT 6490 DFW - OKC: JUST AFTER TAKEOFF THROUGH ACCELERATION ALTITUDE WITH ALL ENGINE INDICATIONS NORMAL, NR 2 ENGINE FLAMED-OUT. CREW ADVISED PRIOR TO V1, HEARD A POP. AN EMERGENCY WAS DECLARED AND NR 2 ENGINE WAS SECURED. THE AIRCRAFT RETURNED TO DFW, MADE NORMAL APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE BOROSCOPED THE ENGINE AND FOUND EXCESSIVE DAMAGE TO COMPRESSOR AND INLET GUIDE VANES. ENGINE CHANGE IS IN PROGRESS. INDICATIONS WERE NORMAL. 2L72 4F4 FRTT00011ATTE6CH 20040422002042004042200204SO 2004 4 22 CHQA000475 120040403A7930 TRANSDUCER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 ENG OIL MALFUNCTIONED A CHQAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING DEDESCENT 1 GL11267 145268 FLT 3099 SDF - DCA: CREW REPORTS ENG 2 OIL PRESS WENT DOWN TO 47 PSI, INTO RED RANGE ON LOW SIDE, THEN WENT TO AMBER DASHES, THEN SPIKED UP INTO TOP OF HIGH SIDE RED RANGE, BUT DID NOT GET EXACT PSI READING. OIL QUANTITY INDICATED 12 QTS AND THERE WERE NO EICAS MESSAGES REPORTED. CREW THEN ELECTED TO SHUT ENGINE DOWN AND DIVERT INTO IAD. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT IAD WITHOUT INCIDENT. MAINTENANCE FOUND THE OIL PRESSURE TRANSDUCER WAS A FAULT. REMOVED AND REPLACED ENGINE OIL PRESSURE TRANSDUCER AND THE SYSTEM OPS AND LEAK CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040422002062004042200206NM 2004 4 22 AWXA200400378 120040419A2560P4010021 BATTERY BOEING737 7373G7 1384595NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER NRNOT REPORTED 1 WP28308AW 24710 MKE - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY WAS WEAK. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040422002082004042200208NM 2004 4 22 AWXA200400379 120040416A3397BMS13311122 WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28904AW 23566 LCQ - EEL - DURING C-09 CHECK FOUND THE L-4 & R-4 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE RE-TERMINATED A TERMINAL AT THE AFT CABIN EMERGENCY LIGHT TEST SWITCH IAW SWPM 20-30-15, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040422002112004042200211NM 2004 4 22 AMTA200400379 120040331A5321 FLOOR PANEL BOEING737 73783N 13844HINM GE CFM56 CFM56* 13802NE CARGO BAY CORRODED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11308TZ 28244 CORROSION: AFT CARGO COMPARTMENT, FLOOR PANEL. DUE TO OLD SEALANT A ROUND CARGO TIEDOWNS WAS NOT REMOVED CAUSING BULGE IN NEW PANEL. NEW SEALANT NOT APPLIED EITHER. ALSO INCORRECT MM REF USED. INSTALLED PANEL IAW SRM. REMOVED OLD SEALANT AROUND CARGO TIE DOWNS, APPLIED NEW SEALANT IAW SRM. 2L72 4F4 FRTA16WE E2GL 20040422002132004042200213NM 2004 4 22 UIEA200400045 120040408A571065B155026 BEAM BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE RT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, CRACKS WERE FOUND AT RT WING LE LOWER OUTBOARD BEAM LOCATIONS AT ILES 414.50 AND 543.93. TRIMMED OUT CRACKED PORTIONS OF BEAM NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONDITION. SPLICED IN REPLACEMENT SECTIONS OF BEAM BETWEEN TRIM LINES AND PRODUCTION SPLICES. REFINISHED BEAM TO DESIGNED CONDITION. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040422002282004042200228NM 2004 4 22 AWXA200400387 120040401A532065C327074 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON THE LT AFT LAVATORY SUBFLOOR SHEAR WEB BETWEEN BS 1016 AND BS 1028, LBL 6 TO LBL 32, WL 208. MAINTENANCE CUT OUT CORRODED SECTION OF LT AFT LAVATORY SUBFLOOR SHEAR WEB FROM BS 1016 AND BS 1028, LBL 0 TO LBL 37, WL 208; FABRICATED A FILLER, DOUBLER, AND NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13 FIG 1 PG 1-3. 2L72 4F RTA16WE 20041028000042004102800004NE 2004 10 28 BAQ2004F00001 220040928A7200L311M10765102 SWITCHING UNIT UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE INSTRUMENT PANELMALFUNCTIONED A BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03868ME709 0288 NR 1 ENGINE WENT TO IDLE DURING FLIGHT. NR 2 ENGINE OEI AT 129 PERCENT TQ MAX FOR 30 SECONDS. NR 1 ENGINE RESET ITSELF TO (FLY). NO FURTHER INCIDENTS TILL LANDING SHUTDOWN. 1G72 3U3 U H88EU E42NE 20040423000042004042300004WP 2004 4 23 G2W2004F00000 220040308A7321307080022 FCU LEAR 35 31 5170530CE GARRTTTFE731TFE73123B WP LT ENGINE FAULTY A G2WAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 WP23555VR 033C P99251 THE AIRCRAFT WAS DECENDING THROUGH 10,000 FT TRASITIONING FROM THE ENROUTE TO APPROACH PHASE OF FLIGHT. IT WAS AT THIS TIME THAT THE CAPTAIN NOTICED THE LT ENGINE INDICATIONS ROLLED BACK SHOWING A DEAD ENGINE. THE CAPTAIN MOVED THE LT THROTTLE TO SEE IF THE ENGINE WAS PRODUCING ANY THRUST AND IT WAS DETERMINED THAT THE ENGINE WAS NOT RUNNING. THE CREW INITIATEE THE EMEGENCY CHECKLIST AND ENGINE SHUT DOWN PROCEDURES IN FLIGHT. THE CREW THEN DETERMINED THAT THEIR WAS NO APPARENT CAUSE FOR INFLIGHT AIR START AND THE ENGINE STARTED NORMALLY AND RAN WITHOUT INCIDENT TO THE DESTINATION AIRPORT OF AIRPORT. DETERMINED THAT THE CAUSE WAS A FAULTY FUEL PUMP/FUEL CONTROL. REMOVED AND REPLACED. F/T OK. 2L72 4F4 FRTA10CE E6WE 20040423000062004042300006EU 2004 4 23 M7K2004F00002 120040102A5610350A25900100 WINDSCREEN UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE COCKPIT CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19802MH505 3707 23036 WINDSCREEN DEVELOPED 3 INCH CRACK IN LT UPPER CORNER NOTICED UPON LANDING DURING POST FLIGHT CHECK. MFG METHOD OF BONDING OF WINDSCREEN TO AIRFRAME CAUSES EXPANSION AND CONTRACTION TO DEVELOP STRESS IN THE LEXAN MATERIAL LENDING TO CRACKING DEFECTS. 1G72 3U3 U H9EU E00054EN 20040423000152004042300015EU 2004 4 23 M7K2004F00003 120040110A1810350A21004828 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE SUPPORT BEARING CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19803MH113 3735 23069 FITTING, RT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED LARGER RADIUS MACHINING OR TO BE OF GREATER STRENGTH. 1G72 3U3 U H9EU E00054EN 20040423000222004042300022EU 2004 4 23 SDR2004024 120040404A2612CG7G010 SMOKE DETECTOR AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CARGO BAY FAULTY A TRBAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO21499AT 499 JUST BEFORE TAXIING, WITH BOTH ENGINES RUNNING, A STRONG ELECTRICAL BURNING ODOR WAS FELT INSIDE THE FLIGHT DECK. REMOVED AND REPLACED ELECTRICAL SMOKE DETECTOR. 2H72 4T4 TRT E20NE 20040423000232004042300023 2004 4 23 USA2004F00021 420040329A2565 STATIC LINE BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE ESCAPE SLIDE LOOSE A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19630AU 0912RP 27808 CREW HAD DIFFICULTY IN ARMING THE R1 DOOR. MAINTENANCE FOUND THE SLIDE STATIC LINE LOOSE AND RESECURED THE END LOOP AROUND THE GIRT BAR. 2L72 4F4 FRTA2NM A12EU 20040423000242004042300024EU 2004 4 23 M7K2004F00007 120040110A1810350A21004827 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE CABIN CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19803MH113 3735 RT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED TO BE OF GREATER STRENGTH AND MACHINED RADIUS INCREASED. 1G72 3U3 U H9EU E00054EN 20040423000342004042300034EU 2004 4 23 USAABA04003 120040226A5270893301 SWITCH AIRBUS330 A330323 3930335EU AFT CARGO DOOR OUT OF ADJUST A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19678US 0388 PHL - FLT 002 - WHILE CLIMBING OUT OF PHL, THROUGH 8,000 FEET, CREW RECEIVED ECAM WARNING 'DOOR AFT CARGO'. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RELEASED AIRCRAFT ON MEL 52-7101B1. MAINTENANCE FOUND THE 28MJ AND 26MJ SWITCHES OUT OF ADJUSTMENT. THE 26MJ SWITCH WAS REPLACED AND BOTH SWITCHES ADJUSTED. THE LATCHING MECHANISM WAS ALSO LUBRICATED. (M) 2L72 4F RTA46NM 20040423000462004042300046NM 2004 4 23 USAA040006 120040112A5314 KEELBEAM BOEING737 7373B7 1384580NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU50706 23701 PIT - FOUND KEELBEAM CHAFFING 16 INCH AREA, STATION 727 FORWARD TO 711 RT OUTBOARD FLANGE OF LT KEELBEAM BY FAIRING AND ATTACH FAST. INSTALLED DOUBLERS, STRAP AND NUT PLATES PER TYPICAL REPAIR 53-60-05 AND EA 77518. (M) 2L72 4F RTA16WE 20040423000472004042300047WP 2004 4 23 GTIA040088 120040107A5230 PAN DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND MID PIT DOOR FORWARD LOWER DOOR PAN AND ATTACH FITTING CRACKED AT DOOR STOP. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED FITTINGS. REMOVED CRACKED T-ANGLE. STOP DRILLED CRACKED PAN 4 PLACES. FABRICATED TWO EACH -5 DOUBLERS. FABRICATED T-ANGLE. INSTALLED T-ANGLE. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F A6WE 20040423000522004042300052WP 2004 4 23 GTIA040162 120040305A57555910055523 SKIN DOUG DC9 DC981 3022081WP LT WING SPOILER DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23805NK 48058 DTW - FOUND LEFT WING INBOARD FLIGHT SPOILER DAMAGED DUE TO CHAFE STRIP COMING LOOSE AND RUBBING HALF WAY THROUGH SPOILER. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER. (M) 2L72 4F A6WE 20040423000562004042300056EU 2004 4 23 USAASA04022 120040309A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT WILL NOT TEST A USAAK NONE L NO TEST ININSP/MAINT 1 EA19728UW 1155 PIT - THE EMERGENCY LIGHT SYSTEM WOULD NOT TEST. MAINTENANCE REPLACED THE MID CABIN, RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040423000652004042300065EA 2004 4 23 ASOA04147 120040221A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11909EV 7658 DURING A GROUND INSPECTION IN ATL, THE AFT OVERWING EMERGENCY EXIT LIGHT ON THE RIGHT SIDE WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OVERWING EMERGENCY EXIT LIGHT LAMP ON THE RIGHT SIDE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040423000662004042300066EA 2004 4 23 ASOA04149 120040222A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040423000672004042300067WP 2004 4 23 ABXA040139 120040401A531499155101 KEELBEAM DOUG DC9 DC931 3022065WP LT WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 LEFT KEELBEAM TO VERTICAL WEB ATTACH FITTING CRACKED AT BOTTOM OF WING ATTACH POINT APPROXIMATELY STA 693 FORWARD OF GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20040423000712004042300071NM 2004 4 23 CALA0400405 120040421A5320656571023 CLIP BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 A/B/B ANTENNA U-CHANNEL FORWARD RIGHT ATTACH CLIP CRACKED AT STATION 727D (3 INCHES). REPLACED CRACKED ATTACH CLIP PER SRM 51-40-02. 2L72 4F RTA16WE 20040426000022004042600002SO 2004 4 26 C2XA04SH205 120040407A531014522460009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000032004042600003SO 2004 4 26 C2XA04SH206 120040407A532014522178005 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000042004042600004SO 2004 4 26 C2XA04SH208 120040407A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO LT ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27185564383 145595 SHV- DURING C-CHECK THE LEFT ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000112004042600011SO 2004 4 26 C2XA04TY071 120040420A531514526437001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712921 145354 TYS - DURING A SCHEDULED 2C INSPECTION THE RT LAV FLOORBEAM CAP OVERFLOW WATER AND LINE FITTINGS, PLUS THE RIVETS AND NUTS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE FLOORBEAM CAP AFTER COUNTERSINKING RIVETS WITH A NEW FLOORBEAM. REPLACED RIVETS AND NUTS IAW EMB 135/145 SRM 51-40-02; 03; 06 AND 51-20-03. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED. 2L72 4T RTT00011AT 20040426000132004042600013SO 2004 4 26 C2XA04SH232 120040418A532014521725613 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE FORWARD SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000142004042600014EU 2004 4 26 04FDEA001015 120040421A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 A 2 INCH CRACK ON INBOARD FLANGE LEFT NR 2 SEAT TRACK FWD OF FRAME 30, MAIN CABIN. REMOVED DAMAGED SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED AND TOP COATED NEW SEAT TRACK SECTION IAW A300-600 SRM 51-20-23. INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SRM 51-20-23. 2L72 4F RTA35EU 20040426000152004042600015SO 2004 4 26 C2XA04SH226 120040415A531514532636401 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK, THE LEFT FLOORBEAM FLANGE WAS FOUND TO BE CORRODED AROUND THE CARBON CROSS BEAM AT FRAME 24. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000162004042600016SO 2004 4 26 C2XA04CL027 120040324A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 CLE FLIGHT 2031, THE CREW REPORTED THE EMERGENCY EXIT SIGN NEXT TO MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN AND RESECURED THE INVERTER CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426000172004042600017SO 2004 4 26 C2XA04BT050 120040419A33507013348 DAU EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2714952 145067 CREW REPORTED, ELECTRICAL EMERGENCY ABNORNAL WITH EMERGENCY LIGHTS NOT ARMED AFTER SHUTTING DOWN APU ON AFTER TAKEOFF CHECKLIST. AIRCRAFT DIVERTED BACK TO EWR AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE NR 1 DAU IAW EMB145 MM 31-41-01. OPS CHECKED SYSTEM GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040426000182004042600018SO 2004 4 26 C2XA04SH237 120040422A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717560 145605 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 5, FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000202004042600020SO 2004 4 26 C2XA04TY061 120040402A3350301 LIGHT EMB 145 EMB145LR 3260212SO OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 IAH - A/C 12540 WAS FOUND WITH AN INOP OVERWING EXIT LIGHT. MAINT REMOVED AND REPLACED THE LIGHT AND OPS CHECK WAS GOOD. A/C RELEASED TO SERVICE. 2L72 4T RTT00011AT 20040426000222004042600022SO 2004 4 26 C2XA04SH236 120040421A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717560 145605 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000242004042600024SO 2004 4 26 C2XA04SH234 120040421A531014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717560 145605 SHV- DURING C-CHECK THE LEFT FLOORBEAM BUTTSTRAP WAS FOUND TO BE DENTED BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000252004042600025SO 2004 4 26 C2XA04SH235 120040421A541014576599003 STIFFENER EMB 145 EMB145LR 3260212SO LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717560 145605 SHV- DURING C-CHECK THE LEFT HAND ENGINE LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000272004042600027EA 2004 4 26 SWIA200413136 120040411A2751855D10011 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07915SW1120 1120 7615 FLAPS FAIL CAUTION MESSAGE APPROX 30 SEC. AFTER SELECTING 0 DEGREES AFTER DEPARTURE. FLIGHT CONTROL PAGE SHOWS FLAPS 0 DEGREES YELLOW OUTLINE. REMOVED AND REPLACED RIGHT BPSU AND RIGGED IAW CRJ MM CHAPTER 27-51-10. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040426000292004042600029 2004 4 26 SWIA200413138 420040412A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07908SW 7540 DURING STALL TEST SYSTEM WENT TO PUSHER AND -SHAKER- AT THE SAME TIME WITH NO DELAY IN BETWEEN. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK GOOD IAW 27-35-01. P/N: 3995100208, S/N OFF: 752. 2L72 4F RTA21EA 20040426000302004042600030EA 2004 4 26 SWIA200413139 120040416A276052C52610A1 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILER MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07459SW 7782 INBOARD AND OUTBOARD GROUND SPOILER FAULT DURING TAKEOFF ROLL. REMOVED AND REPLACED OUTBOARD GROUND SPOILER MANIFOLD PER AMM 27-63-05. OPS AND LEAK CHECK GOOD. S/N OFF 0100T. 2L72 4F RTA21EA 20040426000322004042600032SO 2004 4 26 C2XA04SH222 120040412A716014576711401 COWLING EMB 145 EMB145LR 3260212SO LT ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 DURING C-CHECK THE LT LOWER ENGINE COWLING WAS FOUND TO BE GOUGED ON THE INNER SKIN AT STATION XN1485.0. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 54-10-01 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000342004042600034SO 2004 4 26 C2XA04TY069 120040412A532014521725613 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712921 145354 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040426000352004042600035SO 2004 4 26 C2XA04TY063 120040411A531514521721005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712563 145612 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD FLOORBEAM AT FRAME 16. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040426000372004042600037SO 2004 4 26 C2XA04TY062 120040405A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO MAINS INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716976 145171 BNA - A/C MADE AN AIR RETURN FOR LANDING GEAR, WOULD NOT RETRACT. OVERWEIGHT LANDING. MAINT CYCLED GEAR SEVERAL TIMES, NO CMC OR EICAS MESSAGES NOTED, NO DEFECTS NOTED IAW 32-30-00 AND THE OVERWEIGHT SINKRATE WAS FOUND TO BE WITHIN LIMITS IAW AMM 5-50-02. ALL WORK WAS ACCOMPLISHED AND AC RELEASED FOR SERVICE. NO PARTS WERE REPLACED. 2L72 4T RTT00011AT 20040426000382004042600038SO 2004 4 26 C2XA04IA036 120040321A3350MS277891A SWITCH EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INTERMITTENT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711544 145557 DURING POSTFLIGHT INSPECTION THE EMERGENCY LIGHTS WERE FOUND TO TURN ON INTERMITTENTLY WITH AN EMERGENCY LIGHTS NOT ARMED MESSAGE DISPLAYED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040426000392004042600039SO 2004 4 26 C2XA04TY066 120040412A53201452172561 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712921 145354 TYS - DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT SILL WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL IAW EMB SRM 51-40-02 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040426000442004042600044WP 2004 4 26 ABXA040124 120040318A5330577331153 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 AFT ACCESSORY INNER SKIN AT LONGERON 27 RIGHT, LONGERON 26 RIGHT, STA 1660 - 1680 WAS CORRODED. REPAIRED AREA IAW REA D853-4866MR. 2L74 4F 4A25 20040426000472004042600047NM 2004 4 26 CALA0400406 120040421A552365C2638427 TAB BOEING737 737524 1384721NM LT ELEVATOR DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717663 28924 LEFT ELEVATOR TAB DELAMINATED OUTBOARD END AT TRAILING EDGE WEDGE (1 INCH). REPAIRED LEFT ELEVATOR TAB PER SRM 51-70-04. 2L72 4F RTA16WE 20040426000512004042600051SO 2004 4 26 C2XA04IA047 120040411A3097 BUSS EMB 145 EMB145 3260210SO WINDSHEILD BURNED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2716963 8317 145116 DURING CRUISE THE PILOT REPORTED A SMOKE ODOR IN THE COCKPIT. THE AIRCRAFT DIVERTED TO MGM WHERE MAINTENANCE COULD NOT DUPLICATE THE SMOKE ODOR. THE AIRCRAFT WAS REPOSITIONED TO IAH WHERE MAINTENANCE FOUND THE CAPTAINS WINDSHIELD BUSS BLOCK TO HAVE EVIDENCE OF OVERHEATING. THE CAPTAINS WINDSHIELD WAS REPLACED AND THE DISCREPANCY CLEARED. 2L72 4F RTT00011AT 20040426000522004042600052SO 2004 4 26 C2XA04SH214 120040408A531514522460015 STRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE AFT FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 16 TO 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000542004042600054GL 2004 4 26 C2XA04TY070 220040415A726123073567 CARBON SEAL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A C2XAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2714514 145303 CAE311418 AIR RETURN, FERRIED TO TYS FROM EWR, FOR LAV SMOKE ON EICAS, STRONG ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED THE ZERO CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKED GOOD IAW RR MM 72-25-40, 72-25-25, 72-21-05, 72-21-15, 72-50-00 AND EC7250-01018. 2L72 4F4 FRTT00011ATTE6CH 20040426000552004042600055WP 2004 4 26 ABXA040112 120040323A32607000010101ABX SWITCH DOUG DC9 DC933F 302207AWP NLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23934AX189 47462 AFTER GEAR HANDLE SELECTED DOWN, NOSE GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR WITH SAME RESULT. CHECKED GEAR DOWN VISUAL (PEEP HOLE) AND NOSE LIGHT ILLUMINATED AT 500 FT AGL ON FINAL. FOUND WIRING HARNESS KINKED BEHIND DOWNLOCK SWITCH CANNON PLUG. RE-ROUTED HARNESS TO PROVIDE CLEARANCE. NO DEFECTS ON WIRES OR PLUG. REPLACED DOWNLOCK SWITCH AS PRECAUTION. 2L72 4F A6WE 20040426000592004042600059NM 2004 4 26 04FDEA001010 120040421A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. 2L73 4F RTA22WE 20040426000602004042600060NM 2004 4 26 04FDEA001011 120040421A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. 2L73 4F RTA22WE 20040426000612004042600061NM 2004 4 26 04FDEA001012 120040421A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. 2L73 4F RTA22WE 20040426000632004042600063EU 2004 4 26 04FDEA001014 120040421A5320A5378198422000 BRACKET AIRBUS300 A300F4605R 3930327EU SUBFLOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 TWO AREAS OF CORROSION ON SUBFLOOR AFT OF FRAME 28 BETWEEN SEAT TRACKS 3L AND 4L, MAIN CABIN. REMOVED AND REPLACED THRUST BRACAKET IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040426000662004042600066SO 2004 4 26 C2XA04CL030 120040331A5697163500111 WINDSHIELD EMB 145 EMB145 3260210SO COCKPIT SHORTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2727962 145110 DTW FLIGHT 2136, THE CREW REPORTED SMOKE IN THE COCKPIT WHEN WINDSHIELD HEAT TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426000672004042600067SO 2004 4 26 C2XA04SH211 120040408A532014524131011 BRACKET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000702004042600070SO 2004 4 26 C2XA04BT044 120040401A335020131A BATTERY EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714925 145004 CREW REPORTED, THE LT AND RT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER PACK IAW EMB145 MM 33-50-11, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040426000712004042600071SO 2004 4 26 C2XA04SH173 120040320A532014521725001 SILL EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV- DURING C-CHECK THE LT FLOOR SILL BETWEEN FRAMES 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426000772004042600077WP 2004 4 26 ABXA040122 120040318A532097558041 WEB DOUG DC8 DC863F 302198FWP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN FS 280 AND RIGHT CUSP HAD CORROSION. REPAIRED AREA IAW REA D853-48860MR. 2L74 4F 4A25 20040426000782004042600078WP 2004 4 26 ABXA040123 120040318A571157446784 SPAR CAP DOUG DC8 DC863F 302198FWP CENTER WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 TOP SIDE OF CENTER WING BOX, STA 857, LEFT BUTT LINE 24, UPPER SPAR CAP HAD A 3 INCH CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 31-3-1. 2L74 4F 4A25 20040426000842004042600084NM 2004 4 26 ABXA040079 120040224A5740112T700610 FITTING BOEING767 767231 1385131NM NR 2 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23709AX 22572 MX INSPECTED O/B PITCH LOAD FITTING LOCATED ON NR 2 ENG PYLON MANDATED BY AD 2001-08-23 & S/B 767-57A0070. HFEC INSPECTION REVEALED A CRACK INDICATION IN FITTING. CRACK WAS LOCATED IN UPPER I/B RADIUS OF FITTING, APPROX 1.25 INCH LONG RUNNING FORWARD AND AFT. HFEC AND FLUORESCENT PENETRANT INSPECTION INDICATED CRACK IS IN INBOARD RADIUS ONLY AND DOES NOT EXTEND ONTO FORWARD FACE OF FITTING OR THROUGH ENTIRE THICKNESS OF FITTING. CRACK WAS BLENDED AND DEFERRED PER REA-B657-49099-MR AND ABX GMM CHAPTER 1, SECTION 07.04 FOR MX TRACKING. A/C INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLT FROM ILN TO GSO FOR PERMANENT REPAIR OR REPLACEMENT OF NR 2 ENG O/B PITCH LOAD FITTING. FERRY PERMIT ISSUED. 2L72 4F RTA1NM 20040426000852004042600085NM 2004 4 26 AT0400009 120040413A33508039251 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT UNSERVICEABLE A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15935AT 55069 CABIN CEILING EMERGENCY LIGHTS FOR ROWS 1-15 DISCHARGE AND SHUT OFF AFTER APPROXIMATELY 10 SECONDS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY R5-227 IAW AMM 33-51-03. OPS CHECK NORMAL IAW MM 33-51-00. 2L72 4F TRA6WE 20040426000872004042600087NE 2004 4 26 ABXA040110 220040317A7532563883 BLEED VALVE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE DEFECTIVE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23812AX 2625 46126 669330 AFTER TAKEOFF 2000 FEET, HEARD SHARP LOUD BANG/POP. NR 2 EPR DROPPED .18 AND BACK. FELT SLIGHT LEFT YAW. REPLACED NR 2 ENGINE COMPRESSOR BLEED VALVE AND CONTROL IAW 75-30-03-2-0002. NR 2 ENGINE LOW PRESSURE BLEED VALVE CHECKED GOOD IAW DC8 AMM 71-00-00. REPLACED LOW PRESSURE FUEL FILTER. LEAK CHECKED GOOD ON ENGINE RUN. 2L74 4F4 F 4A25 1E8 20040426000892004042600089 2004 4 26 SWIA200413101 420040329A22116228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07229SW7959 7959 120305 FIRST OFFICER'S SIDE AUTO PILOT HAD SEVERAL -TRIM FAIL- AURAL WARNINGS WITH ASSOCIATED RED -TRIM- FAIL LIGHTS. REPLACED FIRST OFFICER'S AUTO PILOT COMPUTER. OPS CHECK GOOD. 2L72 4T RTA31SO 20040426000902004042600090SO 2004 4 26 SWIA200413102 120040324A2150 SELECTOR SWITCH EMB 120 EMB120ER 3260203SO RT A/C PACK FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM0758733 120197 SMOKE IN CABIN DURING TAXI OUT. REPLACED RCCB FOR RIGHT GROUND COOLING FAN AND REPLACED MODE SELECTOR SWITCH FOR RIGHT PACK IAW MM 21-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20040426000932004042600093SO 2004 4 26 SWIA200413105 120040403A2730 SPRING EMB 120 EMB120ER 3260203SO ELEVATOR FAILED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07561SW 120335 FLIGHT CONTROLS FOR ELEVATOR FEEL EXCEPTIONALLY LITE. REPLACED FIRST OFFICER'S ELEVATOR RETURN SPRING WITH SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040426001002004042600100 2004 4 26 2004UALA00191 420040303A2211 COMPUTER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE AUTOPILOT MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 WP29224UA 30225 LIGHTNING STRIKE ON FWD RADOME AND F/O WINDSHIELD WITH STATIC DISCHARGE. POSSIBLE RADIOS/NAVIGATION INTERMITTENT. ON APPROACH TO ICN, CREW REPORTED THE AUTOPILOT DISCONNECTED, IT WAS RESET BY CREW AND TRIPPED AGAIN. THERE WERE ALSO ABNORMAL ILS INDICATIONS. SEVERE WEATHER CONDITIONS WERE REPORTED IN THE AREA. ACFT DIVERTED TO CJU. GROUND MAINTENANCE AT ICN & CJU COMPLETED AN OPERATIONAL CHECK OF ILS SYSTEM WITHOUT ANY ABNORMAL FINDINGS. THERE WAS NO REPLACEMENT OF PARTS AND BOTH ILS AND AUTOPILOT SYSTEMS OPERATIONAL CHECKED NORMAL. AS OF 4/13/2004, NO ABNORMAL AUTOPILOT OR ILS PROBLEMS HAVE BEEN REPORTED SINCE ABOVE EVENT. 2L72 4F4 FRTT0001SE E46NE 20040426001012004042600101WP 2004 4 26 ABXA040115 120040318A5310 STRUCTURE DOUG DC9 DC941 302207NWP FUSELAGE VIBRATION A ABXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL23974AX 47623 VIBRATION FELT IN AIRCRAFT (YOKE, FLOOR, & SEAT) ABOVE 320 KTS. NO CHANGE IN INTENSITY UNTIL SLOWED BELOW 320 KTS. VIBRATION STARTS AND STOPS ABRUPTLY. DEFERRED MACH TRIM SYSTEM IAW DC9 MEL. CLEARED MACH TRIM SYSTEM AFTER PERFORMING ADJ/TEST PROCEDURES IAW DC9 MM 22-20-01-2. NO DEFECTS FOUND. INSPECTED ALL LANDING GEAR DOORS, ALL FLIGHT CONTROL SYSTEMS AND PERFORMED OPERATIONAL CHECK OF FLIGHT CONTROL SYSTEMS. NO DEFECTS FOUND. 2L72 4F A6WE 20040426001022004042600102WP 2004 4 26 ABXA040113 120040310A7120 VIBE ABSORBER DOUG DC9 DC941 302207NWP NR 1 ENGINE LOOSE A ABXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL23974AX 47623 VIBRATION WAS NOTED DURING CLIMB & DESCENT ABOVE 320 KTS. CREW STATED, FELT NOT VIBRATION IN FLIGHT CONTROLS OR THROTTLES. INSPECTED ALL DOORS & FLIGHT CONTROLS FOR CONDITION AND SECURITY. NO DEFECTS FOUND. INSPECTED ENGINE VIBRATION ABSORBERS ON NR 1 & NR 2 ENGINES. FOUND NR 1 ENGINE FORWARD UPPER VIBRATION ABSORBER LOOSE. SECURED ABSORBER IAW DC9 MM 71-20-03-2-02-1. 2L72 4F A6WE 20040426001032004042600103WP 2004 4 26 ABXA040114 120040313A5350 FAIRING DOUG DC9 DC941 302207NWP FUSELAGE LOOSE A ABXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL23974AX 47623 LOW FREQUENCY VIBRATION CAN BE HEARD AND FELT ON FLOOR PANELS. BEGINS AT 320 KTS, BELOW 320 KTS VIBRATION CEASES. TIGHTENED LOOSE FLAP TO BODY FAIRING ON LEFT FLAP ASSY AND ADJUSTED NOSE LANDING GEAR DOOR PRELOAD PER DC9 MM 32-22-01. INSPECTED TABS AND ANTENNA'S FOR SECURITY. NO DEFECTS NOTED. 2L72 4F A6WE 20040426001052004042600105EU 2004 4 26 2004UALA00325 120040410A2910 PRESSURE SWITCH AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN HYD SYS MALFUNCTIONED A UALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 WP29424UA 506 GREEN HYDRAULIC SYSTEM RSVR LO LVL ECAM DISPLAYED. GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH FAILED, REPLACED GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH, OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040426001082004042600108NM 2004 4 26 2004UALA00328 120040412A2120 ODOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29811UA 847 VERY STRONG ELECTRIC BURNING ODOR IN COCKPIT AND AFT CABIN AREA AT CRUISE ALTITUDE. NO CAUSE IDENTIFIED. CHECKED CABIN AND LAV LIGHTING AND TRASH AREAS, NO DEFECTS. OPERATED BOTH PACKS USING APU AND ENGINES, RAN TRIM VALVES FULL HOT & COLD. OPERATED ENGINES AT FLEX POWER FOR 5 MINUTES, NO DEFECTS NOTED. 2L72 4F4 FRTA28NM E40NE 20040426001112004042600111NM 2004 4 26 04FDEA00958 120040414A5310 TRUNNION BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION ON RIGHT TRUNNION UPPER TEE CHORD FWD UNDERSIDE, STA 295 WL 169 RBL 15. CORROSON ON NLG RT TRUNNION UPPER TEE CHORD STA 295, WL 169, RBL 15 FOUND TO BE OUT OF LIMITS. REPLACED CORRODED TEE CHORD AND INSTALLED NEW TEE CHORD PER 727 SRM 53-10-1, 51-30-2, 51-10-1. 2L73 4F RTA3WE 20040426001122004042600112NM 2004 4 26 2004UALA00331 120040412A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 18G/23G INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29798UA 26928 EMERGENCY LIGHT INOP AT AISLE SEATS 18G AND 23G. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20040426001142004042600114NM 2004 4 26 2004UALA00333 120040408A5320 SILL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 AFT CARGO DOOR LWR SILL BEAM UPPER STRAP FROM STA 807 TO 847 HAS CORROSION AROUND SCREW HOLES. MAJOR REPAIR ACCOMPLISHED. REPLACED SILL BEAM AND STRAP. 2L72 4F4 FRTA16WE E2GL 20040426001162004042600116NM 2004 4 26 2004UALA00335 120040413A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME INNER FLANGE STA 1480 HAS A DENT AT STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040426001182004042600118NM 2004 4 26 2004UALA00337 120040413A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME INNER FLANGE HAS DENT STA 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040426001192004042600119SO 2004 4 26 C2XA04SH239 120040423A532014524131009 BRACKET EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE PASSENGER DOOR FORWARD THRESHOLD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001212004042600121SO 2004 4 26 C2XA04SH241 120040423A531514521713005 FLOORBEAM EMB 135 EMB135ER 3260203SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 18 TO 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001222004042600122SO 2004 4 26 C2XA04SH243 120040424A531514521700007 FLOORBEAM EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001232004042600123SO 2004 4 26 C2XA04SH244 120040424A532014525480003 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001242004042600124SO 2004 4 26 C2XA04SH245 120040424A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717560 145605 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001292004042600129SO 2004 4 26 C2XA04SH178 120040321A532014521718003 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE LEFT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED ANGLE, FABRICATED AND INSTALLED A NEW RAMP ANGLE IAW EMB 135 SRM 51-30-01 AND EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001312004042600131SO 2004 4 26 C2XA04SH213 120040408A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001332004042600133SO 2004 4 26 C2XA04CL026 120040322A49204951680 BLEED VALVE EMB 135 EMB135LR 3260305SO APU FAULTY A C2XAO OTHER O OTHER CRCRUISE 1 SW2714522 145383 CLE FLIGHT 2906, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT AFTER THE APU WAS STARTED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426001342004042600134SO 2004 4 26 C2XA04BT029 120040302A2150 A/C PACK EMB 145 EMB145LR 3260212SO AIR CONDITION ODOR A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW27229096359 6359 CREW REPORTED, DURING ICE TEST FOUL ODOR NOTED, WENT AWAY AFTER ICE TEST. F/A INFORMED SAME ODOR BETWEEN ROWS 3-7. PACK NR 2 SELECTED OFF, ODOR DISSIPATED NEVER CAME BACK. ODOR LIKE BURNING PAPER. MX FOUND NR 2 ECU DUCT LINE CONNECTED TO CONDENSER/MIXER AND RAM AIR VALVE TO BE DISCONNECTED. MX REINSTALLED LINES, RAN ENGINES AND PACKS, COULD NOT DUPLICATE ODOR & OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT FLEW ONE ROUNDTRIP AND ARRIVED BACK IN EWR, CREW REPORTED, BURNING ODOR DURING ICE TEST, PREVIOUS WRITEUP. TROUBLESHOT ENG AND BLEED SYSTEMS, FOUND NR 2 ENG PRODUCING BURNING ODOR. AIRCRAFT FERRIED FOR MAINTENANCE. REMOVED & REPLACED NR 2 ENG, OPS CHECKS & LEAK CHECKS GOOD. 2L72 4T RTT00011AT 20040426001352004042600135SO 2004 4 26 C2XA04TY054 120040320A335072875787 LENS EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT CRACKED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715932 145015 TYS A/C 932 WAS IN FOR A SERVICE CHECK AND MAINTENANCE FOUND THE LEFT CABIN WALL EXIT LIGHT DAMAGE. MAINTENANCE REMOVED AND REPLACED THE EXIT WALL LENS IAW 145 AMM 33-50-13. OPS CHECK GOOD ALL WORK WAS COMPLIED WITH AND RELEASED. 2L72 4F RTT00011AT 20040426001362004042600136SO 2004 4 26 C2XA04SH177 120040321A532014525480003 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001372004042600137SO 2004 4 26 C2XA04BT047 120040407A3260852701 PROXIMITY SWITCH EMB 145 EMB145ER 3260211SO MLG DIRTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2714947 145054 CREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE APPEARED AFTER TAKEOFF, MESSAGE WENT AWAY AFTER 5 SECONDS. MAINTENANCE FOUND NOSE LANDING GEAR STRUT OVERSERVICED, SERVICED STRUT TO PROPER LEVEL; AND CLEANED RIGHTHAND MAIN LANDING GEAR FORWARD WEIGHT ON WHEELS SWITCH CONNECTOR. OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040426001392004042600139SO 2004 4 26 C2XA04BT049 120040411A3350209 LIGHT EMB 145 EMB145ER 3260211SO COCKPIT DOOR FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714947 145054 CREW REPORTED, EMERGENCY LIGHT BELOW COCKPIT DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BELOW COCKPIT DOOR IAW EMB145 MM 33-50-13. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040426001402004042600140SO 2004 4 26 C2XA04TY055 120040323A533012041320071 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE BIRD STRIKE A C2XAO OTHER C F.O.D. CRCRUISE 1 SW2716954 145072 TYS, BIRD STRIKE ON RIGHT FORWARD FUSELAGE NOSE OF AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SKIN IAW-EMB-IC2004-145/1098 AND IC2004-145-1103. 2L72 4T RTT00011AT 20040426001412004042600141SO 2004 4 26 C2XA04SH191 120040403A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND SUPPORT ROD BRACKET. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001442004042600144SO 2004 4 26 C2XA04SH197 120040405A3350375901 LIGHT EMB 135 EMB135LR 3260305SO CABIN BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 233 BLC WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-15. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001452004042600145SO 2004 4 26 C2XA04SH198 120040405A531514521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01112. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001472004042600147SO 2004 4 26 C2XA04SH196 120040405A335074441 LIGHT EMB 135 EMB135LR 3260305SO CABIN BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 234ARC FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW EMB 135 AMM 33-50-14. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001482004042600148SO 2004 4 26 C2XA04SH194 120040403A531514522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001492004042600149SO 2004 4 26 C2XA04SH199 120040405A532013500322001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001502004042600150SO 2004 4 26 C2XA04SH216 120040409A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001512004042600151SO 2004 4 26 C2XA04SH218 120040411A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001522004042600152SO 2004 4 26 C2XA04IA048 120040412A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715985 145248 DURING PREFLIGHT INSPECTION THE AFT FLOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040426001532004042600153SO 2004 4 26 C2XA04SH230 120040416A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27185564437 2681 145595 SHV- DURING C-CHECK WHILE PERFORMING A FUNCTIONAL OF THE EMERGENCY LIGHTING SYSTEM, THE FLOOR PROXIMITY LIGHT STRIP AT THE OVERWING EMERGENCY EXITS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AND OPERATIONALLY CHECKED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001572004042600157SO 2004 4 26 C2XA04SH215 120040409A531514521721009 STRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED THE DAMAGED AREAS AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001582004042600158SO 2004 4 26 C2XA04SH180 120040324A531514522460015 STRAP EMB 135 EMB135ER 3260203SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE AFT FLOORBEAM AT FRAME 17 TO 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001592004042600159SO 2004 4 26 C2XA04CL024 120040319A33501317 LAMP EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719503 145176 DURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP FOR THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426001612004042600161SO 2004 4 26 C2XA04CL035 120040415A27503634001025 DRIVE SHAFT EMB 145 EMB145XR 3260214SO RIGHT FLAP SEIZED A C2XAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SW2717115 145666 CLE FLIGHT 2221, THE CREW REPORTED A FLAP FAIL IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT FLAP NR 4 FLEX SHAFT. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040426001622004042600162SO 2004 4 26 C2XA04CL036 120040416A3260852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO NLG CRACKED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2712967 145133 CLE FLIGHT 2826, THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426001642004042600164SO 2004 4 26 C2XA04BT038 120040321A3350 RELAY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716541 145542 CREW REPORTED, EMERGENCY LIGHT NOT ARMED, EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAY K0275 AND PERFORMED WIRING CHECKS IAW EMB145 33-50-50 AND RELAY IAW EMB145 WM 20-13-02. OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20040426001662004042600166SO 2004 4 26 C2XA04SH220 120040411A531514522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001672004042600167SO 2004 4 26 C2XA04TY056 120040323A531112304811001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE BIRD STRIKE A C2XAO OTHER C F.O.D. CRCRUISE 1 SW2716954 145072 TYS, BIRD STRIKE ON RIGHT FORWARD FUSELAGE, FRAME 4 ON FORWARD FUSELAGE 1 WAS FOUND DAMAGED. MAINTENANCE CUT OUT THE DAMAGED SECTION, FABRICATED AN L-CHANNEL (2 ON EACH SIDE) AND INSTALLED IAW EMB-IC2004-145/1098 AND SRM 53-00-04 FIG 201. 2L72 4T RTT00011AT 20040426001682004042600168SO 2004 4 26 C2XA04SH224 120040412A532014522178005 THRESHOLD EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715555 145594 SHV- DURING C-CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001702004042600170SO 2004 4 26 C2XA04SH219 120040411A531514522461011 GUSSET EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715555 145594 SHV- DURING C-CHECK RIGHT HAND AFT FLOORBEAM DOUBLER WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001712004042600171SO 2004 4 26 C2XA04IA039 120040326A33507287580505 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713929 145009 EMERGENCY LIGHT STRIP AT SEAT 1A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20040426001722004042600172SO 2004 4 26 C2XA04IA049 120040414A335020133A BATTERY EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS ON THE FLOOR WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE FLOOR EMERGENCY LIGHTS, OPERATIONALLY TESTED THE SYTEM, AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20040426001732004042600173SO 2004 4 26 C2XA04IA040 120040329A3350BC10020002 LIGHT EMB 145 EMB145XR 3260214SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711121 145683 THE EMERGENCY LIGHT AT THE PASSENGER DOOR ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ASSEMBLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4F RT 20040426001782004042600178SO 2004 4 26 C2XA04CL028 120040325A3350 LIGHT EMB 145 EMB145LR 3260212SO ROWS 8-9 INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713979 145181 CLE FLIGHT 2623, THE CREW REPORTED THE EMERGENCY AILSE PATH LIGHTS WERE INOPERATIVE AT ROW 8-9. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 33-20-00. 2L72 4T RTT00011AT 20040426001792004042600179SO 2004 4 26 C2XA04CL029 120040322A4930 APU EMB 135 EMB135LR 3260305SO APU BAY ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2712530 145533 CLE FLIGHT 2888 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT WHEN THE APU WAS STARTED. MAINTENANCE PLACED THE APU ON MEL. 2L72 4F RTT00011AT 20040423000412004042300041NM 2004 4 23 USAA040010 120040201A5753 SKIN BOEING737 7374B7 1384702NM FLAP CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19777AU 24979 PIT - FOUND FLAP DEEP CHAFED 4 INCHES BY .125 INCH BY .025 INCH DEEP, LEFT OUTBOARD MID FLAP INBOARD LEADING EDGE. INSTALLED SKIN REPLACEMENT DOUBLER PER SRM 57-53-01. (M) 2L72 4F RTA16WE 20040423000582004042300058 2004 4 23 GTIA040163 420040306A2565 CABLE DOUG DC9 DC982 3022082WP L2 DOOR SLIDE MISROUTED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23804NK 49104 FLL - L2 DOOR ESCAPE SLIDE GIRT BAR CABLE ROUTED INPROPERLY. REROUTED CABLE. (M) 2L72 4F A6WE 20040423000692004042300069SO 2004 4 23 C2XA04SH231 120040417A533014520595005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715555 145594 SHV- DURING C-CHECK THE EXTERIOR SKIN WAS FOUND TO BE GOUGED AT FRAME 11 BETWEEN STRINGERS 20L AND 21L. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-10-01, STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000052004042600005SO 2004 4 26 C2XA04CL034 120040409A3397 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713935 145022 CLE FLIGHT 2006, THE CREW REPORTED THE EMERGENCY LIGHT ABOVE 3A DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND REPAIRED THE EMERGENCY LIGHT CONNECTOR AT SEAT 3A. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426000092004042600009SO 2004 4 26 C2XA04SH228 120040415A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE LEFT FLOORBEAM FLANGE WAS FOUND TO BE CORRODED AROUND THE CARBON FIBER CROSS BEAM. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORM A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000212004042600021SO 2004 4 26 C2XA04IA034 120040317A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27149916914 2406 145278 DURING PREFLIGHT INSPECTION THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. THE AIRCRAFT WAS INSPECTED AND THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND DISCHARGED. THE AFFECTED PACK WAS REMOVED AND REPLACED, THE LIGHTING SYSTEM OPERATIONALLY TESTED, AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040426000232004042600023SO 2004 4 26 C2XA04SH233 120040421A716014575001405 INTAKE EMB 145 EMB145LR 3260212SO RT ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE RIGHT HAND ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE UPPER COWLING ALIGNMENT HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMBRAER IC 2004-145/1466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000282004042600028EA 2004 4 26 SWIA200413137 120040414A2697 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA WW OVERHEAT DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07441SW 7602 MLG BAY OVERHEAT WILL NOT TEST. REMOVED AND REPLACED LT AND RT WHEEL BIN WIRING HARNESSES. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040426000312004042600031SO 2004 4 26 SWIA200413140 120040410A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER PL NO WARNING INDICATION NO TEST TXTAXI/GRND HDL 1 NM07578SW 120346 ROW 6 SEAT -A- EMERGENCY LIGHT POD DOES NOT ILLUMINATE. REMOVED AND REPLACED LAMP AT SEAT 6A. EMERGENCY LIGHT OPS CHECKS GOOD. 2L72 4T RTA31SO 20040426000452004042600045WP 2004 4 26 ABXA040142 120040421A5250 LATCH DOUG DC9 DC931 3022065WP COCKPIT DOOR JAMMED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23908AX 47008 COCKPIT DOOR LATCH JAMMED. DISASSEMBLED COCKPIT DOOR LATCH ASSEMBLY, FOUND HANDLE JAMMED. FREED JAM AND REASSEMBLED. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20040426000572004042600057SO 2004 4 26 C2XA04SH212 120040408A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED FROM FRAME 17 TO 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000722004042600072SO 2004 4 26 C2XA04SH174 120040320A530014522460015 BUTTSTRAP EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426000732004042600073WP 2004 4 26 ABXA040127 120040318A53103648280 ATTACH ANGLE DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 ATTACH ANGLE TO UPPER PRESSURE DECK FLOOR FROM STA 960 - 980, 100 INCHES FROM RIGHT CUSP, HAD CORROSION. REPAIRED AREA IAW REA D853-48865MR. 2L74 4F 4A25 20040426000762004042600076WP 2004 4 26 ABXA040121 120040318A531256453325 PRESSURE PANEL DOUG DC8 DC863F 302198FWP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 RIGHT WHEEL WELL, CORROSION ON SPOILER CABLE BRACKET FOOT END AROUND ATTACH BOLTS, JUST ABOVE LONGERON 24, FS 920. REPAIRED AREA IAW DC-8 REA D853-48868MR. 2L74 4F 4A25 20040426000922004042600092SO 2004 4 26 SWIA200413104 120040402A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM07196SW1774 1774 120151 DURING TAKEOFF ROLL FLAP AND ADVANCED SWS ILLUMINATED ON MAP WITH ASSOCIATED CONTROL FAULT ON FLAP WARNING INDICATION PANEL. COMPLIED WITH QRH RESET. OPERATED NORMALLY REMAINDER OF FLIGHT. REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040426000972004042600097SO 2004 4 26 SWIA200413109 120040402A2121EVAC2322C2 FAN EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT PACK FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07197SW781 781 120186 LEFT PACK EMITTING SMOKE THROUGH VENTS WHILE ON GROUND. REPLACED LEFT PACK GROUND COOLING FAN. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040426000982004042600098SO 2004 4 26 LR7A04035 120040403A5320 WEB LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 4 4763 DURING CARGO RAMP CLOSURE, CARGO DOOR LEADING EDGE WEB CRACKED AND STIFFENER ANGLE BROKEN BY CONTACT WITH RAMP SUPPORT STOOL AT FS 869, LBL 15 AND 32, WL 200. REPAIRED IAW LAC MEA 382-52-04-036. 2H74 4T A1SO 20040426000992004042600099WP 2004 4 26 ABXA040141 120040416A5610 WINDOW DOUG DC9 DC932 3022066WP COCKPIT STUCK A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23988AX 47084 FIRST OFFICER'S SIDE WINDOW WAS STUCK SHUT. INSTALLED A MISSING NUT AT ROD END AT TOP OF WINDOW AND SECURED LOOSE LOCK BAR TRIM. WINDOW OPERATES NORMALLY. 2L72 4F A6WE 20040426001042004042600104NM 2004 4 26 2004UALA00324 120040409A33201013273 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 10-11 OVERHEATED A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29510UA 24780 SIDEWALL LIGHT AT ROW 10-11 LT SIDE EMITTING ODOR. REPLACED LIGHT ASSEMBLY. 2L72 4F4 FRTA2NM E17NE 20040426001062004042600106NM 2004 4 26 2004UALA00326 120040413A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT BILGE STA 1464 TO 1472, RBL 3, LOWER SKIN ANTENNA DOUBLER CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW ANTENNA INTERNAL DOUBLER. 2L72 4F4 FRTA2NM E17NE 20040426001102004042600110NM 2004 4 26 2004UALA00330 120040412A5743 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT MLG CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 RT MLG OB FITTING WAS FOUND CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED RT MLG OB FITTING. 2L72 4F4 FRTA16WE E2GL 20040426001132004042600113 2004 4 26 2004UALA00332 420040412A2565 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN TORN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 SLIDE FAILED PROOF PRESSURE TEST AFTER 3 MINUTES AT 4.2 PSI. THE SEAM BELOW THE GIRT TORE. SLIDE WAS RETURNED TO OEM FOR ANALYSIS, BUT SPECIFIC CAUSE FOR FAILURE WAS INDETERMINATE. INFLATABLE PORTION OF SLIDE WAS SCRAPPED. 2L74 4F4 FRTA20WE E24NE 20040426001202004042600120SO 2004 4 26 C2XA04BT051 120040422A3350110049 BATTERY PACK EMB 145 EMB145LR 3260212SO GALLEY AREA WEAK A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715985 145248 CREW REPORTED, EMERGENCY LIGHTS IN FORWARD PART OF CABIN ARE WEAK. MAINTENANCE REMOVED AND REPLACED GALLEY EMERGENCY LIGHT BATTERY PACK IAW EMB145 MM 33-50-04. OPS CHECKED EMERGENCY LIGHTS GOOD. 2L72 4T RTT00011AT 20040426001262004042600126SO 2004 4 26 C2XA04SH240 120040423A532014524131011 BRACKET EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE PASSENGER DOOR THRESHOLD AFT BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001282004042600128SO 2004 4 26 C2XA04SH176 120040321A531514522460015 BUTTSTRAP EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE AFT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001322004042600132SO 2004 4 26 C2XA04CL031 120040330A49204951680 BLEED VALVE EMB 145 EMB145LR 3260212SO APU FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2710575 145640 EWR FLIGHT 2060, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00. ON 3/31/04 MAINTENANCE REPLACED THE APU BLEED AIR VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040426001802004042600180NM 2004 4 26 2004UALA00338 120040413A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME STA 1580 INNER FLANGE HAS 2 DENTS BETWEEN STR'S 25R-26R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040426001852004042600185SO 2004 4 26 C2XA04SH184 120040327A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001892004042600189NM 2004 4 26 DLM88040263 120040324A4940 STARTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE APU FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27971DL12717 53214 P80536 ELECTRICAL ODOR THROUGHOUT AIRCRAFT. REPLACED APU. 2L72 4F4 FRTA6WE E2EA 20040426001902004042600190NM 2004 4 26 DL75K040264 120040324A3350 FUSE BOEING757 757232 1384965NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27643DL 23997 SEATS 2-8 EMERGENCY LIGHTS INOP. REPLACED BAD FUSE. 2L72 4F RTA2NM 20040426001912004042600191NE 2004 4 26 ABXA040116 220040324A7200 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 DEFECTIVE A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23811AX 1 46113 671250 UPON INITIAL CLIMBOUT, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 2 ENGINE OIL PRESSURE WAS NOTED TO BE 28 PSI AND OIL QUANTITY DECREASING. SHUT DOWN ENGINE AT 0424Z. N1 AND N2 RPM'S NOTED: 22/35. ENGINE OIL PRESSURE IN CRUISE: 3 PSI. REPLACED NR 2 ENGINE. 2L74 4F4 F 4A25 1E8 20040426001952004042600195NM 2004 4 26 2004UALA00341 120040413A5320 SILL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 CABIN R-2 DOOR SILL ATTACH ANGLE AND SIDE FRAME ATTACH ANGLE CORRODED STA 1690 AND APPROX RBL 60. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040426001972004042600197NM 2004 4 26 2004UALA00342 120040413A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT CARGO PIT STA 1300, STR 20L-21L, SHEAR TIE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20040426001982004042600198NM 2004 4 26 2004UALA00343 120040413A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 EXTERIOR FUSELAGE DENTED BELOW DOOR 1L BETWEEN STR 19L AND 20L AT STA 300. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND TRIPLER. 2L72 4F4 FRTA16WE E2GL 20040426002002004042600200NM 2004 4 26 2004UALA00346 120040413A2910 HYDRAULIC SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29645UA 25280 RETURNED TO THE FIELD DUE TO HYDRAULIC FLUID LOSS AND UNSUITABLE WEATHER. ACTUAL FLUID LOSS UNDETERMINED, NO SIGNIFICANT LEAKS FOUND AND NO FURTHER LOSS OF FLUID. 2L72 4F4 FRTA1NM E24NE 20040426002012004042600201NM 2004 4 26 2004UALA00347 120040413A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 FUSELAGE FRAME IS CRACKED AT STA 616 BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040426002062004042600206NM 2004 4 26 2004UALA00353 120040413A5310 DOOR FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 MAIN CABIN AT STA 294 STR 7R DOOR JAM CORNER CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040426002072004042600207SO 2004 4 26 C2XA04IA045 120040402A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715985 145248 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHT AT THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040426002082004042600208SO 2004 4 26 C2XA04IA043 120040401A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 DURING PREFLIGHT INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND THE BULB TO BE BURNED OUT. THE AFFECTED BULB WAS REPLACED AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20040426002092004042600209SO 2004 4 26 C2XA04IA044 120040401A3350REBC410J2000CB LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711544 145557 DURING PREFLIGHT INSPECTION THE FORWARD FLOOR EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RELAY K0275, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040426002112004042600211SO 2004 4 26 C2XA04BT048 120040409A3350276005 FUSE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714543 145553 DURING SERVICE AND ROUTINE INSPECTION, MAINTENANCE FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY POWER FUSE IAW EMB145 WM 33-50-50. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040426002152004042600215SO 2004 4 26 C2XA04TY060 120040328A335066367 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713979 145181 A/C 979 WAS IN FOR A SERVICE CHECK AND MAINT FOUND ONE OF THE EMERGENCY LIGHT AISLE STRIPS INOP NR 4. MAINT REPAIRED THE BROKEN WIRE AT EMERGENCY STRIP NR 4 IAW EMB 145 AMM 20-21-00, OPS CHECK GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED TO SERVICE. 2L72 4T RTT00011AT 20040427000012004042700001EU 2004 4 27 KBM2004F00017 120040122A6420350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R HUB WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 TAIL ROTOR HUB LAMINATED RUBBER HINGE BEARING ARE WORN BEYOND LIMITS. REMOVED AND REPLACED WITH NEW. 1G71 3U3 U H9EU E19EU 20040427000022004042700002EU 2004 4 27 KBM2004F00023 120040219A6220126891P BALL JOINT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE STARFLEX DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 BALL JOINT, BOTH WORN AND DAMAGE STAKE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040427000042004042700004NE 2004 4 27 ALG2004F00005 120040209A7697 SWITCH SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE THROTTLE DIRTY E ALGAE ENGINE SHUTDOWN G MULTIPLE FAILURE NRNOT REPORTED 1 SW03862AL 760531 20054TEC DURING APPROACH TO CM243, WHILE CHECKING DECU FAULTS PRIOR TO LANDING, NOTICED A NR 2 DECU (FLY GATE FAULT). PROCEED TO ICY AND SHUTDOWN NR 2 ENGINE IN MIXED MODE. MAINTENANCE CLEANED SWITCHES ON NR 2 THROTTLE IN QUADRANT AND CLEANED AND INSPECTED CONNECTORS ON NR 2 ENGINE DECU AND ON ENGINE DECK. CYCLED BATTERY AND FAULTS HAD TURNED WHITE. HAD PILOT RUN AIRCRAFT, FAULTS CLEARED, RETURNED TO SERVICE. 1G72 3U3 UNCH1NE E19EU 20040427000052004042700005 2004 4 27 ALG2004F00007 420040216A3197 WIRE BELL 407 407 1182206SW ALLSN 250C 250C47B GL TEMP BULB DAMAGED A ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03697AL 53374 CAE847158 WHILE LIFTING OFF FOR TAKE OFF, THE TRANSMISSION TEMPERATURE GAUGE FLUCTUATED FROM 0 TO MAX AND REMAINED AT MAX AFTER THROTTLE REDUCED TO IDLE. MAINTENANCE FOUND SHAFTED WIRE NUMBER E629A22 INSIDE CONNECTOR AT TRANSMISSION TEMPERATURE BULB. REPAIRED WIRE AND GROUND OPS CHECKED GOOD. 1G71 3U3 UO H2SW E1GL 20040427000132004042700013SW 2004 4 27 JJWA0055059 120040214A6210206010200133 BLADE BELL 206 206B 1181511SW ALLSN 250C 250C* GL MAIN ROTOR DEFECTIVE E JJWAK NONE O OTHER ININSP/MAINT 1 SO175005N3 1931 INSTALLED 2 NEW BLADES WITH HIGH VISIBILITY PAINT FROM MFG. ABLE TO PERFORM SPAN AND LATERAL BALANCE TO LESS THAN .02IPS. UNABLE TO REDUCE VERTICAL VIBRATION TO ACCEPTABLE LEVELS IN HOVER TO 120 MPH. INSTALLED ANOTHER WARRANTY BLADE AND WAS ABLE TO TRACK TO MORE ACCEPTABLE VERTICAL VIBRATION LEVELS. 1G71 3U3 U H2SW E4CE 20040427000142004042700014SW 2004 4 27 JJWA0055058 120040210A3212206050168009 FLOAT BELL 206 206B 1181511SW ALLSN 250C 250C* GL MLG MISINSTALLED E JJWAO OTHER O OTHER NRNOT REPORTED 1 SO175005N 1931 ORDERED NEW FLOAT BAGS FROM FLOATS AND FUEL CELLS, ONE MFG DATE MAY 2003, OTHER FEB 2004, BOTH MANUFACTURED WITH AFT BELT AND BUCKLE ASSEMBLIES INSTALLED UPSIDE DOWN. HAD TO SEND FOR REPAIRS TO NEW BAGS. 1G71 3U3 U H2SW E4CE 20040427000152004042700015EU 2004 4 27 SDR2004012 120040223A6123ACE0002 SWITCH AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CENTER PEDESTAL FAILED A TRBAO OTHER HG ELECT. POWER LOSS-50 PC MULTIPLE FAILURE LDLANDING 1 SO21447AM 447 DURING LANDING WHEN POWER LEVERS WERE MOVED FROM GROUND IDLE POSITION TO REVERSE, THE ENGINE NH WENT BELOW 71 PERCENT. AIRCRAFT AC POWER WAS LOST THEREFORE, NO HYDRAULIC POWER AVAILABLE. UNABLE TO TAKE OFF POWER CONTROL SYSTEM (ATPCS) SWITCH. THIS IS NOT A TIME CONTROLLED COMPONENT THEREFORE, THERE IS INFO PERTAINING TO THE PART TT NOR THE TSO. 2H72 4T4 TRT E20NE 20040427000162004042700016NM 2004 4 27 HALA0400278 120040226A5312991183915 BULKHEAD BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE FUSELAGE CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13484HA 55129 DURING 2A CHECK, TWO CRACKS MEASURING 2.0 INCHES AND 1.5 INCHES WERE FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD AT STA 1178.225 AT LONGERON 17L, IN THE CAPS FORWARD FLANGE. REPAIR IN WORK. 2L72 4F4 FTRA6WE E00057EN 20040427000202004042700020NM 2004 4 27 IUEA200400028 120040308A2612 CONNECTOR BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 1 ENGINE DIRTY A IUEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15506MC 21252 517718 GT8971/5 DNA/BKK ATB AND IFSD DUE TO NR 1 ENGINE FALSE FIRE WARNING: NR 1 ENGINE FIRE INDICATION DURING CLIMB, ALL OTHER SYSTEMS NORMAL EXCEPT (B) LOOP WAS DEFERRED. (A) LOOP WAS INDICATION FAULT AND FIRE. ENGINE SHUTDOWN ACCOMPLISHED AND FUEL JETTISON 28.3K. PERFORMED THROUGH INSPECTION OF ENGINE FIRE LOOPS. FOUND TWO CONNECTORS AT CORE SECTION LOOSE. CLEANED AND SECURED THEM. CLEANED AND REINSTALLED AFT FIREWALL CONNECTORS. PERFORMED ENGINE RUN, ALL CHECKED NORMAL IAW MM 26-11-00. 2L74 4F4 FRTA20WE E23EA 20040427000212004042700021NM 2004 4 27 UIEA200400029 120040308A3310245904 TRANSFORMER BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL P7 PANEL BURNED A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15499MC 29260 GT603/6 HSV/PIK BURNT ODOR IN COCKPIT: AIRCRAFT HAS A BURNT ODOR DURING ENTIRE FLIGHT. TRACED TO TRANSFORMER T44, REMOVED AND REPLACED SAME IAW MM 33-11-05. NO CIRCUIT BREAKER AVAILABLE, ISOLATED WIRING AND TRANSFERRED TO DMI M04-014 IAW MEL 33-11-01 CAT C. CB WAS REMOVED AND REPLACED, AND OPERATION CHECK NORMAL. 2L74 4F4 FRT1384945 E23EA 20040427000222004042700022GL 2004 4 27 UIEA200400031 220040308A7200 ENGINE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 4 SURGES A UIEAJA DUMP FUEL UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA15498MC 29259 CI 351/8 ATL/ANC ATB DUE TO NR 4 ENGINE STALL: AT SPEED V2 AFTER TAKEOFF, ENGINE NR 4 BEGAN SURGING FOLLOWED BY STALLING AND AIRFRAME SHUDDER. ENGINE NR 4 THRUST LEVER WAS RETARDED TO STABILIZE THE ENGINE. FUEL DUMPED TO 302 KG AND RETURNED FOR LANDING 27R ATC. NO ENGINE EXCEEDANCE NOTED. REMOVED AND REPLACED NR 4 ENGINE IAW WO A717101GTI. 2L74 4F4 FRT1384945 E23EA 20040427000262004042700026NM 2004 4 27 USA2004F00005 120040226A2120 ODOR BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE COCKPIT DETECTED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19604AU 22199 DURING MAINTENANCE FERRY FLIGHT, CREW REPORTED A SMOKE ODOR IN THE FLIGHT DECK. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN PERFORMED AN ENGINE RUN WITH THE PACKS ON. THE CONDITION COULD NOT BE DUPLICATED. 2L72 4F4 FRTA2NM A12EU 20040427000292004042700029EA 2004 4 27 A6WA200440026 120040306A322016154101 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31434AW8573 7322 NOSE LANDING GEAR DOOR OPEN AND CAUTION DISAGREE MESSAGES, ACCOMPANIED BY WOW INPUT AND STEERING INOPERATIVE CAUTION MESSAGE ON DEPARTURE. RAN QRH FOR NLG DOOR OPEN, GEAR DISAGREE REMOVED WITH GEAR DOWN, RAN QRH FOR CAUTIONS. RECONNECTED TORQUE LINKS, REMOVED AND REPLACED LOWER TORQUE LINK, RETRACTION CHECK GOOD. 2L72 4F RTA21EA 20040427000342004042700034 2004 4 27 GTIA040160 420040305A2565D29982113 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE R1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 R1 DOOR SLIDE FOUND ON GALLEY FLOOR DURING DAILY INSPECTION. REMOVED AND REPLACED R1 SLIDE PACK. 2L72 4F4 F A6WE E2EA 20040427000362004042700036NE 2004 4 27 AMTA200400235 220040303A7200 ENGINE BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LEFT MALFUNCTIONED A A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL11560TZ 33525 31877 LT ENGINE UNABLE TO ACHIEVE MAX CLIMB THRUST AT FL 390 MAX AVAILABLE EPR=1.67. SHOULD HAVE BEEN 1.76. ENGINE PRODUCED MAX CLIMB AT FL350. REMOVED AND REPLACED NR 1 ENGINE FFG PER MM 73-21-01-4, TAKEOFF EPR REACHED. PERFORMED NR 1 ENGINE THRUST POWER TEST NR 9 AND NR 10. ENGINE PARAMATERS IN LIMITS PER MM 71-00-00-5. (M) 2L72 4F4 FRTA2NM E12EU 20040427000382004042700038NM 2004 4 27 AMTA200400241 120040304A5220 WARNING LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE EMERGENCY EXIT FALSE ACTIVATIONA AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11519AT 27975 EICAS MSG. RT EMERGENCY DOOR. COULD NOT DUPLICATE FAULT, OPENED DOOR AND INSPECTED SWITCH. COMPLIED WITH NR3 DOOR WARNING SYSTEM TEST. N O DEFECTS NOTED. RESECURED DOOR AND SLIDE. REF MM 52-71-00 AND W/C 222R2509. 2L72 4F4 FRTA2NM A12EU 20040427000402004042700040EA 2004 4 27 SIMA200406402 120040229A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE EMERGENCY LIGHT DAMAGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21507AE 10059 DURING PREFLIGHT THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR TO BE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING NEAR THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200404816) 2L72 4F4 FRTA21EA E15NE 20040427000412004042700041SO 2004 4 27 SIMA200406806 120040306A27303621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMAO OTHER J WARNING INDICATION CLCLIMB 1 SW21731BE 145356 PITCH NR 1 AND NR 2 INOPERATIVE. COMPLIED WITH ETN EB 27-0022R1 AND REPLACED HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (SW21200404960) 2L72 4F4 FRTT00011ATTE6CH 20040427000442004042700044SW 2004 4 27 ALG2004F00009 120040227A7931 CONNECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANSDUCER FAILED A ALGAA UNSCHED LANDING N FALSE WARNING HOHOVERING 1 SW03607AL 53264 WHEN AIRCRAFT WAS PICKED UP TO A HOVER. AS AIRCRAFT CAME TO A HOVER, ENGINE OIL PRESSURE WENT HIGH. AIRCRAFT WAS LANDED BACK ON PAD, SHUT DOWN AND CONTACTED MAINTENANCE. MAINTENANCE REPLACED ENGINE OIL PRESSURE TRANSDUCER, DID NOT FIX PROBLEM. THEN REPLACED ENGINE OIL PRESSURE TRANSDUCER CONNECTOR PLUG. OPS CHECKED GOOD. 1G71 3U3 UO H2SW E1GL 20040427000452004042700045SW 2004 4 27 ALG2004F00010 120040229A6730206076031021 SERVO BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FLT CONTROLS BINDING E ALGAO OTHER J WARNING INDICATION HOHOVERING 1 SW03198H 3647 CAE832754 WHILE PICKING UP TO A HOVER. FIRST FLIGHT OF THE DAY, WHILE PICKING UP TO A HOVER FELT BINDING IN CYCLIC. SET AIRCRAFT DOWN AND CHECKED FRICTION AND HYDRAULIC SWITCH, MADE SECOND ATTEMPT TO PICKUP TO A HOVER WITH SAME STIFFNESS IN CYCLIC. SHUTDOWN AND NOTIFIED MAINTENANCE. MAINTENANCE REMOVED RT CYCLIC SERVO AND INSTALLED RT SERVO. 1G71 3U3 U H2SW E4CE 20040427000502004042700050NE 2004 4 27 BAQA094029 220040326A73130319739420 INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ENGINE CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 32056 INJECTOR REMOVED DUE TO SUSPECTED CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004 1G72 3U3 U H88EU E34NE 20040427000562004042700056EU 2004 4 27 BAQA093992 120040220A249745043006 MASTER BOX UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ELECTRICAL WILL NOT TEST D BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME2410 132 BOX DOES NOT SELF TEST AND GENERATOR DISCONNECT LIGHT ILLUMINATED. S/N 1334 WAS THE UNIT THAT WAS USED FROM ASSET, YET TO RECEIVE THE REPLACEMENT FROM AEC. REPLACED WITH SERVICEABLE UNIT. 04/14/2004 1G72 3U3 U H88EU E34NE 20040427000572004042700057EU 2004 4 27 BAQA094174 120040401A212119A2772 BLOWER BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE AIR DISTRIBUTIONNOISY B BAQAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA03117KY 7544 BLOWER IS EXCESSIVELY NOISY OPERATION AND INTERMITTENT STARTING AND STOPPING. S/N 105 WAS TAKEN FROM ASSET STOCK AND INSTALLED ON A/C. YET TO RECEIVE THE REPLACEMENT FROM AEC AS OF 04/15/2004. REPLACED WITH SERVICEABLE UNIT FROM ASSET (S/N 105). 04/15/2004 1G72 3U3 UNCH13EU E19EU 20040427000592004042700059EU 2004 4 27 BAQA092753 120040315A28221176415103 PUMP BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101* NE FUEL BOOST SHORTED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KC 7168 BOOST PUMP IS NOT PUMPING FUEL (INTERNAL SHORT). CANNING INVOLVED BETWEEN PBH 7243 AND 7168 WHICH IS WHY THIS PUMP WAS REMOVED OFF OF A/C 7168. REPLACED WITH SERVICABLE UNIT FROM AEC, 04/15/2004 1G72 3U3 UNCH13EU E5NE 20040427000612004042700061EU 2004 4 27 BAQA094194 120040401A5210L563M10X2001 PANEL UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE DOOR CRACKED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME2336 0144 PANEL HAD STRESS CRACK IAW SITE MECHANIC, UPON REMOVAL, PANEL SHATTERED AND MECHANIC SCRAPPED ON SITE. REPLACED WITH SERVICEABLE PANEL FROM AEC, 04/16/2004 1G72 3U3 U H88EU E34NE 20040427000652004042700065SW 2004 4 27 HEEA094229 120040412A2420 GENERATOR BELL 412 412 1182202SW NR 1 INOPERATIVE E HEEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03108X 33115 ON SHORT FINAL TO GC-158, THE NR 1 GENERATOR KICKED OFF LINE, HAD LIGHT SMOKE IN THE CABIN, AND SEVERAL CIRCUIT BREAKERS POPPED. FOUND SEVERAL CHAFED WIRES AT THE TOP OF THE WINDSHIELD CENTER POST WHERE THE BUNDLE SPLITS TO GO THE CIRCUIT BREAKER PANEL. 1G72 4U H4SW 20040427000662004042700066EU 2004 4 27 HEEA094230 120040406A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SWITCH DEFECTIVE E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW03800PH S800 IN CRUISE FLIGHT, HYDRAULIC BLOCK LIGHT CAME ON, FOLLOWED BY NR 1 HYDRAULIC LIGHT ILLUMINATION. RETURNED TO BASE. FOUND DEFECTIVE SWITCH ON GUIDE ASSEMBLY. REPLACED HYDRAULIC GUIDE ASSEMBLY. 1G72 3U H3EU 20040427000672004042700067 2004 4 27 BAQA094232 420040416A312050380067 LOAD METER BEECH 100 100BEECH 1152916CE PWA PT6 PT6A27 52043EA COCKPIT UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 10364 B144 INDICATOR STICKS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1L72 3T4 T A14CE E4EA 20040427000682004042700068SW 2004 4 27 ALGA094233 120040422A3241206020110103 SKID BELL 407 407 1182206SW ALLSN 250C 250C47B GL VERTICAL STAB BROKEN B ALGAK NONE O OTHER ININSP/MAINT 1 SW03617AL5075 BP2119 53265 THE TAIL SKID BROKE AT RETAINING HOLE AND A PORTION OF SKID DEPARTED AIRCRAFT. FATIGUE CRACK APPEARS TO HAVE STARTED AT RETAINING HOLES AND PROGRESSED AROUND BETWEEN 2.25. 1G71 3U3 UO H2SW E1GL 20040427000702004042700070 2004 4 27 BAQA094006 420040401A2312064105430 TRANSCEIVER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE WEAK E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA035405G 7179 TRANSCEIVER IS WEAK AND UNREADABLE. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1G72 3U3 U H13EU E5NE 20040427000712004042700071EU 2004 4 27 BAQA094235 120040320A243523081057 STARTER GEN UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH 0179 STARTER GEN WILL NOT ROTATE ENGINE, BRUSHES ARE WORN. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1G72 3U3 UO H88EU E42NE 20040427000722004042700072GL 2004 4 27 BAQA094236 220040331A73136890917 FUEL NOZZLE AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL FUEL SYSTEM DIRTY E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS550 5495 CAE840418 REQUIRES CLEANING AND FLOW CHECK. FUEL NOZZLE IS ORIGINAL EQUIPMENT OFF OF ENG. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1G72 3U3 U H11EU E4CE 20040427000782004042700078EU 2004 4 27 BAQA094193 120040422A28221C441 PUMP AEROSPAS355 AS355F2 8680812EU ALLSN 250C 250C20 03013GL FUEL BOOST FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03942MS1165 5498 PUMP FAILS TO PROVIDE SUFFICIANT PRESSURE. REPLACED WITH SERVICABLE UNIT. 04/26/2004 1G72 3U3 U H11EU E4CE 20040427000812004042700081NM 2004 4 27 DL73S040266 120040325A53306545866585 SKIN BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 CORROSION WAS FOUND ON THE KEEL BEAM LOWER SKIN PANEL. LOWER SKIN PANEL WAS REPLACED PER ERA 386233-14. 2L72 4F A16WE 20040427000842004042700084NM 2004 4 27 DL73S040271 120040325A2120 ODOR BOEING737 737247 138448DNM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27375DL 23602 ON CLIMBOUT, F/A REPORTED STRONG ODOR IN AFT CLOSET AND LAV AREA AT FL 310 ODOR DISSIPATED. INSPECTED COCKPIT AND CABIN, NO PROBLEMS NOTED. INSPECTED BEHIND COFFEEMAKERS, NO ODORS PRESENT. CYCLED CABIN LIGHTING, ALL LIGHTS OPS NORMAL. RAN BOTH ENGINES AT PWR WITH PACKS, NO ODORS NOTED. A/C OK FOR SERVICE. 2L72 4F A16WE 20040427000852004042700085NM 2004 4 27 DL73S040272 120040326A5330UNK SKIN BOEING737 737247 138448DNM FUSELAGE FATIGUED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 CRACK INDICATIONS WERE NOTED DURING MFEC INSPECTION OF THE S4R LAP. DURING REPAIR ACCOMPLISHMENT PER SRM 53-30-3, FIG 42, 12 MORE ADDITIONAL CRACK INDICATIONS WERE NOTED. CRACK INDICATIONS WERE REMOVED, ADDITIONAL INSPECTIONS ACCOMPLISHED AS PER ERA 386164-14AD. 2L72 4F A16WE 20040427000862004042700086NM 2004 4 27 DL73S040273 120040324A5330 SKIN BOEING737 737232 1384475NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27315DL 23087 THE FUSELAGE WAS INSPECTED AND FOUND TO HAVE EVIDENCE OF SCRIBING ALONG THE LOWER SKIN OF SEVERAL SKIN LAP JOINTS BETWEEN FS 360 & 1016 IN THE UPPER FUSELAGE BETWEEN STRINGERS 14L & 14R. THE BUTT JOINTS OF THE FUSELAGE WERE ALSO FOUND WITH SCRIBE INDICATIONS. THE SKIN LAPS WERE CUT AND REPLACED WITH ALUMINUM DOUBLERS AND THE BUTT JOINT SPLICES REPLACED. THE WORK WAS SUMMARIZE PER ER/A 088408-14. 2L72 4F RTA16WE 20040427000882004042700088NM 2004 4 27 DL76L040275 120040328A2560P20700030 FLASHLIGHT BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27177DN 25122 DURING PDC FOUND FWD CABIN LEFT JUMPSEAT BY 1L DOOR FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT, TEST OK. 2L72 4F RTA1NM 20040427000902004042700090 2004 4 27 DL777040277 420040328A2330 COVER BOEING777 777232 1385232NM SEAT 54H UNSECURE A DALAO OTHER O OTHER CRCRUISE 1 SO27860DA 29951 SEAT 54H GETS AN ELECTRICAL SHOCK ON FOOT FROM ENTERTAINMENT UNIT UNDER SEAT 53H. CAUSED PROBLEM TO OTHER DISPLAYS IN AREA. FOUND PLASTIC COVER ON AVU UNDER SEAT 53H AND 1 EA CONNECTOR ON AVU UNSECURE. SECURED SAME. VIDEO / AUDIO, NOW OPS NORMAL. PERFORMED INSPECTION VISUAL OF OTHER IFE WIRING UNDER 53H. NO OTHER TROUBLE FOUND. 2L72 4F RTT00001SE 20040427000952004042700095NM 2004 4 27 DL764040282 120040329A793041809104 TRANSMITTER BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 2 ENG OIL MALFUNCTIONED A DALAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 SO27838MH 29711 704857 ON APPROACH TO ATL RT ENG OIL PRESS WENT TO 0 AND ENG WAS SHUTDOWN. ALL OTHER PARAMETERS WERE NORMAL. FOUND RT ENG OIL PRESSURE TRANSMITTER FAILED PER FIM 79-11-00 PAGE 105. REPLACED TRANSMITTER AND ACCOMPLISHED POST WINDMILL INSP PER M/M 72-00-00-206-096-HOO PAGE 4. ENGINE PARAMETERS NORMAL, A/C OK FOR SERVICE. 2L72 4F4 FRTA1NM E13NE 20040427000972004042700097NM 2004 4 27 DLM88040284 120040310A5753VTB00680 BEARING DOUG MD88 MD88 3023688NM FLAP HINGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27990DL 53342 DURING HMV IN ATL FOUND 3 FLAP HINGE BOLTS TO BE ROTATING AND WITH THE COTTER PINS SHEARED AT THE NUT. POSITIONS FOUND WERE THE RIGHT O/B FLAP I/B HINGE AT AFT ATTACH POINT, RIGHT O/B FLAP CENTER HINGE AT AFT ATTACH POINT, AND THE LEFT O/B FLAP CENTER HINGE AT THE AFT ATTACH POINT. TWO HINGE FITTINGS WERE REPLACED INCLUDING BEARINGS AND ONE HAD THE BEARING REPLACED ONLY. 2L72 4F RTA6WE 20040427000982004042700098NM 2004 4 27 DLM88040285 120040331A3244 TIRE DOUG MD88 MD88 3023688NM MLG FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27961DL 49980 ON TAKEOFF FROM LGA, NR 1 TIRE BLEW OUT. DAMAGED 2 HYD LINES ON GEAR STRUT, DAMAGED GEAR STRUT DOOR AND DAMAGED SPLASH DEFLECTOR. DIVERTED TO JFK. NR 2 TIRE REMAINED INFLATED. REPAIRED OR REPLACED DAMAGED PARTS. 2L72 4F RTA6WE 20040427001002004042700100NM 2004 4 27 DL75A040287 120040401A3244B757M TIRE BOEING757 757212 1384951NM MLG SEPARATED A DALAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 SO27750AT 23126 NR 4 AND NR 8 MAIN TIRES BLOWN/DEFLATED CONFIRMED BY GROUND PERSONNEL ON TAKEOFF AT LGA. NR 8 TIRE LOST CAP, NR 4 TIRE FLAT. REPLACED ALL 4 WHEEL ASSYS ON RIGHT TRUCK. ALSO REPLACED NR 8 BRAKE LINE AND NR 4 AND 8 BRAKE ASSYS DAMAGED BY TIRE CAP. REPLACED NR 7 SPOILER PANEL DUE TO DAMAGE. 2L72 4F RTA2NM 20040427001022004042700102NM 2004 4 27 DL73S040289 120040401A5330654577245 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4L LAP JOINT BETWEEN BS 727 AND BS 908. DAMAGE WAS REMOVED AND REPAIRED PER ERA 088665-14. 2L72 4F A16WE 20040427001052004042700105NM 2004 4 27 DL73S040292 120040401A53116546541504 FRAME BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 BS 663 FRAME WAS FOUND CRACKED NEAR S7R. CRACK WAS REMOVED AND REPAIRED PER ERA 089232-14. 2L72 4F A16WE 20040427001062004042700106NM 2004 4 27 DL767040293 120040401A3350 BATTERY BOEING767 767232 1385132NM EMERGENCY LIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27107DL 22219 EMERGENCY EXIT SIGNS INOP AT RT AND LT OVERWING EXIT DOORS. REPLACED EMERGENCY PWR SUPPLY BATTERIES AT M737, M732 PER M/M, NOW OPS NORMAL. 2L72 4F RTA1NM 20040427001082004042700108NM 2004 4 27 DL757040295 120040401A5420H30717 KEEPER BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE BROKEN A DALAO OTHER O OTHER CRCRUISE 1 SO27617DL 22907 716541 AFT LATCH OR CORE COWL ON NR 1 ENGINE BROKEN. REPLACED LATCH CATCH NR 1 ENGINE CORE COWL AFT POSITION PER M/M. 2L72 4F4 FRTA2NM E17NE 20040427001092004042700109NM 2004 4 27 DL73S040296 120040402A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 THE FUSELAGE SKIN LAP JOINTS AND BUTT JOINTS WERE FOUND WITH NUMEROUS AREAS OF SCRIBE DAMAGE FROM FS 259.5 TO 1016 IN THE JOINTS FROM STRINGER 14 AND ABOVE. THE AFFECTED LAP JOINTS WERE CUT OUT AND ALUMINUM REPAIR DOUBLERS INSTALLED TO RESTORE THE JOINTS. THE BUTT JOINT STRAPS WERE REMOVED AND REPLACED. THE REPAIRS ARE SUMMARIZED ON ER/A 386200-14. 2L72 4F A16WE 20040427001102004042700110 2004 4 27 DL76L040297 420040402A3450 IRU BOEING767 767332 1382001NM OUT OF ADJUST A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27184DN 27111 FMC WAS NOT PROVIDING GOOD NAV ORIENTATION IMMEDIATELY AFTER T/O. ALL DATA WAS OFF BY APPROX 300 MILES. UPON LANDING AT SNN POS SHOWED AIRCRAFT AT GATE IN HAM. RESET AND BITE CHECK OF BOTH FMCS, NO TROUBLE. CHECKED NAV DATA BASE FOR FMC, DATABASE CORRECT. CHECKED SENSORS AND READOUT ON FMC, CDU ALL OK. CHECKED ADCS, NO FAULT FOUND. REALIGNED IRU. NO FURTHER TROUBLE. FOUND A/C TO BE IN CORRECT WORKING ORDER. 2L72 4F RTA1NM 20040427001112004042700111NM 2004 4 27 DLM88040298 120040402A2560P4010021 BATTERY DOUG MD88 MD88 3023688NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27961DL 49980 AFT F/A AND FWD F/A EACH HAD ONE EMERGENCY FLASHLIGHT THAT WAS NOT FLASHING THE RED LIGHT. REPLACED BATTERY ON BOTH, OPERATION NORMAL. 2L72 4F RTA6WE 20040427001142004042700114 2004 4 27 DL76S040301 420040403A2330 ODOR BOEING767 767332 1382001NM VIDEO EQUIP DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27122DL 23436 ELECTRICAL SMOKE ODOR FROM VIDEO EQUIP RACK, WHEN SHUT OFF SMOKE DISSIPATED. RAN VCP 1 AND VCP 2 FOR 15 MINUTES EACH, NO SMOKE ODOR NOTICED. REMOVED VCP 1 AND VCP 2 AND FOUND NO EVIDENCE OF SMOKE. REINSTALLED VCP 1 AND VCP 2, RAN GASPER AND RECIRC FANS. NO ODOR NOTICED. 2L72 4F RTA1NM 20040427001162004042700116NM 2004 4 27 DL73S040304 120040405A5330654577886 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S14R LAP JOINT BETWEEN BS 908 AND BS 960. DAMAGE WAS REMOVED AND REPAIRED PER ERA 088728-14. 2L72 4F A16WE 20040427001172004042700117NM 2004 4 27 DL73S040305 120040405A533065458001189 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4R LAP JOINT BETWEEN BS 259.9 AND BS 360. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089005-14. 2L72 4F A16WE 20040427001202004042700120NM 2004 4 27 DL73S040308 120040405A53306560552501 STRAP BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE BUTT JOINT AT BS 360 BETWEEN S13L AND S28R. DAMAGE WAS REMOVED AND REPAIRED PER ERA 088793-14. 2L72 4F A16WE 20040427001222004042700122NM 2004 4 27 DL73G040310 120040405A53306545768267 SKIN BOEING737 73735B 13844BMNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27223DZ 23972 DAMAGE WAS NOTED TO THE FUSELAGE SKIN AT THE FWD EDGE OF THE C1 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089422-14. 2L72 4F RTA16WE 20040427001232004042700123NM 2004 4 27 DL733040311 120040405A3520 PSU BOEING737 737347 1384647NM 19DEF INOPERATIVE A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO27309WA 23442 PAX SEAT 19DEF 02 MASKS DID NOT DEPLOY WHEN SWITCH IN COCKPIT PUSHED. REPLACED PSU. 2L72 4F RTA16WE 20040427001252004042700125NM 2004 4 27 DL733040313 120040403A5330654577572 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303WA 23183 THE FUSELAGE SKIN WAS FOUND WITH 2 CRACKS ALONG THE BONDED DOUBLER EDGES AT STRINGERS 22R & 23R. AN EXISTING REPAIR FOR A SIMILAR CRACK WAS LOCATED AT STRINGER 24R. THE EXISTING REPAIR WAS REMOVED, ALL CRACKS REMOVED WITH CUTOUTS, AND THE CUTOUTS REPAIRED WITH A SINGLE ALUMINUM DOUBLER/TRIPLER REPAIR. THE REPAIR WAS ACCOMPLISHED PER ER/A 089558-14, REV A. 2L72 4F RTA16WE 20040427001272004042700127NE 2004 4 27 DL757040316 220040408A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 FAILED A DALAE ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 SO27630DL37995 22920 716581 ENGINE FAILURE ON LEFT ENGINE WITH T/O POWER SET, BOTH FIRE BOTTLES DISCHARGED INTO ENGINE MAX EGT 762 DEG FOR 3.06 MINUTES. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20040428000012004042800001EA 2004 4 28 SWIA200413134 120040410A2721AL00102 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07410SW1144011440 7066 RUDDER TRIM CB 2F6 POPPED. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW MM 27-22-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20040428000032004042800003 2004 4 28 DL76L040315 420040407A3420211002542 HSI BOEING767 767332 1382001NM COCKPIT MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27184DN 27111 ON ARRIVAL AT GATE CREW REPORTED A PUNGENT ODOR IN COCKPIT AND CAPT HSI BRIGHTNESS FLUCTUATING. ON INSPECTION NOTICED SIMILAR ODOR FROM CAPT FWD CONSOLE AND E/E EXHAUST AREA. REPLACED CAPT HSI AND CONFIRMED COOLING FLOW GAINED ACCESS TO EQUIP. COOLING SUPPLY FAN FOUND INLET GRILL CLOGGED. CLEANED GRILL AND INSTALLED NEW SUPPLY FAN PER MM. RETURNED A/C TO NORMAL, NO ODORS IN COCKPIT, OK FOR SERVICE. 2L72 4F RTA1NM 20040428000042004042800004NM 2004 4 28 DL73S040319 120040407A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 INSPECTION OF THE STRINGER 10L LAP JOINT BETWEEN FS 360 & 540 REVEALED A CRACKED FASTENER HOLE AT FS 380. THE CRACKED HOLE WAS REMOVED WITH A 1 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC 737 SRM 53-30-3, FIG 42. THE REPAIR WAS DOCUMENTED PER ER/A 089541-14AD. 2L72 4F RTA16WE 20040428000072004042800007NM 2004 4 28 DL777040322 120040408A3350 FUSE BOEING777 777232 1385232NM BATTERY PACK BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27861DA 29952 EMERGENCY LIGHTING AT ROWS 30D-44E AND 30F-44G INOP. REPLACED FUSE IN BATTERY PACK. EMERGENCY LIGHT CHECK OK. 2L72 4F RTT00001SE 20040428000082004042800008NM 2004 4 28 DL76S040323 120040409A2910NAS161208A O-RING BOEING767 767332 1382001NM RUDDER PCA DAMAGED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27117DL 23276 LOSS OF CENTER HYD FLUID. FOUND O-RING ON RUDDER PCA DAMAGED. REPLACED O-RING. 2L72 4F RTA1NM 20040428000122004042800012WP 2004 4 28 ASAA0480082 120040224A33501001191 LIGHT DOUG DC9 DC983 3022083WP PAX CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS271544091 53022 LAX - LINE CHECK - FOUND PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20040428000132004042800013WP 2004 4 28 ASAA0480146 120040301A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01958AS 53024 SEA - PREFILGHT CHECK, FOUND FIRST FIVE EMERGENCY TRACK LIGHTS TESTS INOPERATIVE, TWICE. RECONNECTED MODULE CONNECTOR, TWICE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040428000142004042800014WP 2004 4 28 ASAA0480145 120040301A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP COCKPIT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01964AS 53078 SEA - PREFLIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHTS DID ILLUMINATE DURING CHECK. REPLACED ASSOCIATED POWER SUPPLY BATTERY PACK. LIGTHS THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20040428000162004042800016NM 2004 4 28 ASAA0440021 120040204A33978100022602 WIRE BOEING737 7374Q8 138447QNM EMERGENCY EXIT INOPERATIVE A ASAAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM01754AS 25095 GYR - FOUND FLOOR TRACK LIGHTING SYSTEM AT THE OVERWING EMERGENCY EXIT HAS 6 WHITE LIGHTS THAT ARE NOT ILLUMINATED AND HAS EXPOSED WIRES. RECONNECTED WIRES. REINSTALLED COVER RAIL, FLOOR TRACK LIGHTING OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040428000192004042800019WP 2004 4 28 ASAA0480111 120040227A33500105606 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 16. REPLACED MISSING MODULE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040428000212004042800021WP 2004 4 28 GTIA040175 120040218A5320 STRUCTURE DOUG DC9 DC983 3022083WP SUBFLOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND CABIN SUBFLOOR CORRODED FS 1173-1213 RBL 54. SUBFLOOR STATION 1183 TO 1188 IS OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040428000232004042800023EU 2004 4 28 A6WA200460005 120040306A7500226368001 LINE BAC 146 146200A 1500266EU BLEED AIR BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31292UE E2087 NR 1 ENGINE ANTI-ICE PIPE FRACTURED. ASSOCIATED CLAMP BRACKET ALSO BROKE. FRACTURED AT 90 DEGREE ELBOW AT FORWARD END. REPLACED PIPE ASSEMBLY AND BRACKET PIPE ASSEMBLY P/N 2-263-680-01. (M) 2H74 4F A49EU 20040428000242004042800024WP 2004 4 28 GTIA040170 120040216A5730 PANEL DOUG DC9 DC982 3022082WP LT WING CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND LEFT WING PANEL 1163C SCRATCHED LIGHT SURFACE CORRODED. REMOVED CORROSION FROM LEFT PANEL 1163C. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F A6WE 20040428000282004042800028WP 2004 4 28 GTIA040222 120040322A3297 CONDUIT DOUG DC9 DC983 3022083WP UPLOCK SENSOR KINKED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23833NK 49449 DEPARTING LAS AFTER GEAR RETRACTION NOSE GEAR RED LIGHT REMAINED ILLUMINATED. ACCOMPLISHED QRH PROCEDURE WHICH RECTIFIED THE PROBLEM NO FURTHER DEFECTS NOTED. FOUND NLG LOCKED SENSOR CONDUIT KINKED AND SPLICES IN PROX WIRING. REMOVED AND REPLACED NLG LOCKED SENSOR (D1-32). ALSO REMOVED AND REPLACED NOSE GEAR DOWN SWITCH S1-412 AS PRECAUTIONARY. ALSO, REMOVED AND REPLACED PROX SWITCH ELECTRONIC UNIT AS PRECAUTIONARY. NLG SWING OPS CHECK GOOD WITH NO DISCREPANCIES. (M) 2L72 4F RTA6WE 20040428000312004042800031GL 2004 4 28 BAQA094005 220040402A732023070606 FUEL CONTROL AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL ENGINE FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911KY 5101 WARRANTY / EXCHANGE - CORE RETURN FOR WARRANTY/EXCHANGE PO 202317205. CORE S/N 333014 WAS RECEIVED UNDER EXCHANGE PO 202267101 AND INSTALLED ON ENGINE S/N 841012 ON 02/26/2004 AND FAILED 04/02/2004 FOR A TOTAL TSO OF 9.4 HOURS. PLEASE ADVISE WARRANTY MANAGER ON WARRANTY STATUS OF FUEL CONTROL S/N 333014 REPLACED WITH SERVICEABLE CONTROL, 04/20/2004. 1G72 3U3 U H11EU E4CE 20040428000332004042800033 2004 4 28 BAQA094048 420040414A34516226263001 TRANSCEIVER BELL 222 222U 1182140SW LYC LTS101LTS101* NE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03222LF751 47528 EXCHANGE - CORE RETURN FOR EXCHANGE PO 202342803, DMF INOPERATIVE ON CORE,IS NOT RECEIVING A SIGNAL. REPLACED WITH SERVICEABLE UNIT FROM AVGROUP, 04/22/2004 1G72 3U3 U H9SW E5NE 20040428000342004042800034 2004 4 28 BAQA093902 420040419A3454066107810 RECEIVER AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE NAV RECEIVER UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03199SM 6396 RENTAL - RETURN OF RENTAL UNIT S/N 10327 IN SERVICEABLE CONDITION REPLACED WITH UNIT BACK FROM REPAIR, 04/21/2004 1G72 3U3 U H10EU E19EU 20040428000352004042800035EU 2004 4 28 BAQA094099 120040403A80129550178290 START VALVE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE ENGINE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY610 7544 WARRANTY - CORE RETURN FOR WARRANTY PO 202317606, ENG S/N 18167, VALVE WAS REMOVED IN THE TROUBLESHOOTING PROCESS OF HAR STARTING NR 1 ENGINE. REPLACED WITH SERVICEABLE UNIT FROM MFG, 04/21/2004 1G72 3U3 UNCH13EU E19EU 20040428000372004042800037NE 2004 4 28 BAQA094226 220040329A7421SC1821 IGNITER UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ENGINE UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 WARRANTY. ELECTRODE GONE IN UNIT. REPLACED WITH SERVICEABLE ASSET UNIT. 04/26/2004 1G72 3U3 U H88EU E34NE 20040428000392004042800039NE 2004 4 28 BAQA093879 220040317A73100319739400 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE RT INJECTION CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH474 0273 WARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 03/19/2004 1G72 3U3 U H88EU E19EU 20040423000502004042300050EA 2004 4 23 ASOA04146 120040221A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11864AS 7502 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040423000572004042300057WP 2004 4 23 GTIA040168 120040106A5730 SKIN DOUG DC9 DC981 3022081WP LT WING CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FTW - FOUND LEFT WING LOWER SKIN PANEL UPPER SURFACE HAS 4 INCH BY 5 INCH DIAMETER EXFOLIATION AT XCW 121 9 INCHES AFT OF WING REAR SPAR AND 9 INCHES MLG TRUNNION FITTING. WING SKIN FSXCW 121 OUTBOARD OF TRUNNION FOUND OUT OF LIMITS. ALT SPAR FS XCW 121 FORWARD BRACKET FOUND TO BE CRACKED. REMVOED BRACKET. FABRICATED NEW ANGLE. LOCATED AND DRILL NEW REPAIR DOUBLER. INSTALL REPAIR DOUBLER. INSTALLED NEW ANGLE. WORK WAS ACCOMPLISHED PER SPIRIT AIRLINE EA 5730-0401. (M) 2L72 4F A6WE 20040423000612004042300061EA 2004 4 23 ASOA04148 120040221A3350BF10044004 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11864AS 7502 DURING A C-CHECK IN MCN, AN EMERGENCY EXIT ILGHT LENS AND TRIM WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING AN EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2L72 4F RTA21EA 20040423000702004042300070WP 2004 4 23 CALA0400404 120040420A5313993607329 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2715841 49581 A/B/B SHEAR TIE CORRODED AT LONGERON 30 AND 28 RIGHT AT STATION 1193. FABRICATED AND INSTALLED SHEAR TIE REPAIR SPLICE BETWEEN LONG 30 AND 29 RIGHT PER SRM 53-03 FIG 3. 2L72 4F A6WE 20040423000742004042300074WP 2004 4 23 ABXA040137 120040405A5315 FLOORBEAM DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23813AX 46136 MAIN CABIN STA 920 FLOORBEAM LOWER FLANGE FORWARD SIDE WAS CORRODED APPROXIMATELY 5 INCHES INBOARD OF CUSP LEFT SIDE. REPAIRED AREA IAW REA D853-49122MR. 2L74 4F 4A25 20040426000122004042600012SO 2004 4 26 C2XA04CL032 120040402A3350 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713935 145022 ORD FLIGHT 2210, THE CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. THE CREW PERFORMED A RESET AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426000192004042600019SO 2004 4 26 C2XA04IA035 120040323A32501170A350001 POTENTIOMETER EMB 145 EMB145XR 3260214SO NLG STEERING ERRATIC A C2XAO OTHER S AFFECT SYSTEMS LDLANDING 1 SW2741104 145646 UPON LANDING THE NOSE WHEEL STEERING SYSTEM FAILED CAUSING THE AIRCRAFT TO DEPART THE RUNWAY. THE AIRCRAFT WAS INSPECTED AND DAMAGE WAS NOT FOUND TO THE LANDING GEAR OR AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR STEERING POTENTIOMETER, OPERATIONALLY TESTED THE STEERING SYSTEM, AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4F RT 20040426000362004042600036SO 2004 4 26 C2XA04TY064 120040411A531514521700001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712563 145612 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER AISLE FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040426000422004042600042 2004 4 26 ABXA040134 420040330A2250 A/C PACK BOEING767 767231 1385131NM AIR CONDITIONINGSHUTDOWN A ABXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL23708AX 22571 DURING APPROACH TO RUNWAY 22L AT MHR, WHEN LANDING GEAR WAS LOWERED, RIGHT PACK SHUT OFF AND LOC FAILED. MISSED APPROACH EXECUTED, GEAR CYCLED UP AND DOWN AND EVERYTHING SEEMED TO WORK AGAIN. MAINTENANCE AT MHR COMPLIED WITH MCDP GROUND TEST 30. NO CURRENT FAULTS NOTED. A/C RELEASED TO CAT 2 CHECK CAT 3B. 2L72 4F RTA1NM 20040426000562004042600056SO 2004 4 26 C2XA04CL033 120040408A32201172C000002 DRAG STRUT EMB 135 EMB135ER 3260203SO NLG SEIZED A C2XAO OTHER J WARNING INDICATION APAPPROACH 1 SW27275126998 145274 CLE FLIGHT 2127 THE CREW REPORTED ON APPROACH THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. THE CREW FOLLOWED THE QRH AND ACCOMPLISHED LANDING GEAR EXTENSION. ALL GEAR INDICATED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR MAIN DRAG STRUT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426000582004042600058NM 2004 4 26 04FDEA001009 120040421A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. 2L73 4F RTA22WE 20040426000652004042600065SO 2004 4 26 C2XA04SH201 120040406A531514522461011 DOUBLER EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE RIGHT FLOORBEAM DOUBLERS AT FRAME 20 AND 22 WERE FOUND TO BE CORRODED AROUND THE SCREW HOLES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000742004042600074WP 2004 4 26 ABXA040130 120040318A53156513301503 FLOORBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 RIGHT PRESSURE DECK MAIN CABIN LOWER SIDE OF FLOORBEAMS AT STA 920 AND 940 ARE EXFOLIATED. REPAIRED AREA IAW REA D853-48871MR AND REA D853-48873MR. 2L74 4F 4A25 20040426000752004042600075WP 2004 4 26 ABXA040120 120040318A53134375221 FITTING DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 AIR CONDITION ACCESSORY COMPARTMENT AT STA 70, LONGERON 34 RIGHT TO LONGERON 35 RIGHT, BULKHEAD ATTACH FITTING CORRODED. REPAIRED CHORD AND LONGERON FITTING IAW DC-8 SRM 51-1-24, 53-2-5 AND 51-1-8. 2L74 4F 4A25 20040426000832004042600083WP 2004 4 26 ABXA040119 120040318A53135750198 LONGERON DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 LONGERON 24 LEFT CRACKED, LOWER INNER FLANGE OF BOTTLE BOLT CAVITY. REPAIRED LONGERON 23 LEFT IAW DC-8 SRM 53-2-2 AND REA D853-48861MR. 2L74 4F 4A25 20040426001302004042600130SO 2004 4 26 C2XA04SH210 120040408A532014524131009 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE MAIN DOOR THRESHOLD FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001382004042600138SO 2004 4 26 C2XA04BT043 120040401A335020131A BATTERY EMB 145 EMB145 3260210SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716961 145103 CREW REPORTED DURING PREFLIGHT INSPECTION, EMERGENCY EXIT LIGHT BY PASSENGER DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD IAW EMB145 MM 33-50-00. 2L72 4F RTT00011AT 20040426001432004042600143SO 2004 4 26 C2XA04IA042 120040328A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711539 145536 DURING SCHEDULED MAINTENANCE THE RIGHT CENTER FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED THE LIGHT, AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040426001462004042600146SO 2004 4 26 C2XA04SH192 120040403A532014521725015 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01111. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001552004042600155SO 2004 4 26 C2XA04CL023 120040319A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN WILL NOT TEST A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713935 145022 CLE FLIGHT 2041, THE CREW REPORTED THE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040426001602004042600160SO 2004 4 26 C2XA04SH217 120040411A532014521725613 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715555 145594 SHV- DURING C-CHECK THE RIGHT HAND SILL FORWARD OF THE SERVICE DOOR WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION FROM THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001632004042600163SO 2004 4 26 C2XA04SH221 120040411A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001652004042600165SO 2004 4 26 C2XA04SH202 120040404A3097 WIRE HARNESS EMB 145 EMB145ER 3260211SO WINDSHIELD HEAT PINCHED A C2XAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW2714942 145037 IAH - FLIGHT 2064 THE CREW REPORTED A STRONG ELECTRIC BURNING ODOR WHEN THE WINDSHIELD HEAT WAS SELECTED ON. THE AIRCRAFT LANDED AT IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE WINDSHIELD HEAT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT SHV WHERE MAINTENANCE FOUND A WIRE BUNDLE PINCHED AND ARCING UNDER FLOOR PANEL 222AF. MAINTENANCE REPAIRED THE AFFECTED WIRING, AND REMOVED AND REPLACED THE AFFECTED FLOOR PANEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001742004042600174SO 2004 4 26 C2XA04SH225 120040413A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001752004042600175SO 2004 4 26 C2XA04BT040 120040327A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 CREW REPORTED, SERVICE DOOR EMERGENCY LIGHT BULB BURNED OUT. MAINTENANCE REMOVED AND REPLACED LIGHT BULB IAW EMB145 AMM 33-50-06. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040426001772004042600177SO 2004 4 26 C2XA04BT041 120040324A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 DURING ROUTINE INSPECTION MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040426001872004042600187NM 2004 4 26 DLM88040261 120040324A3320 LIGHT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE GALLEY ODOR A DALAB EMER. DESCENT BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27920DE 53423 725365 APPROACHING CRUISE ALTITUDE OF 330 CABIN CREW AS WELL AS FLIGHT CREW SMELLED ELECTRICAL ODOR, NO SMOKE. REPLACED FIRST CLASS GALLEY OVER LIGHT ASSY 339101074. 2L72 4F4 FRTA6WE E9NE 20040426001882004042600188NM 2004 4 26 DL76L040262 120040324A2530811150417 COFFEEMAKER BOEING767 767332 1382001NM GALLEY UNSERVICEABLE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271200K 28457 ELECTRIC BURNING ODOR NEAR LOCATION 409. FOUND HOTPLATE CONNECTION ON NR 2 COFFEEMAKER BROKEN. REPLACED COFFEEMAKER, OPS NORMAL. 2L72 4F RTA1NM 20040426001992004042600199NM 2004 4 26 2004UALA00344 120040413A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 STR 15L IS CRACKED AT STA 380. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040426002052004042600205NM 2004 4 26 2004UALA00352 120040413A5320 SILL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 MAIN CABIN AT R1 DOOR SILL ANGLE SUPPORT HAS CORROSION BETWEEN BS 300 AND 330. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040427000172004042700017NE 2004 4 27 HALA0400286 220040228A7320114E6112G1 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE LT ENGINE FAILED A HALAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 WP13485HA 55130 LT FADEC FAIL CAME ON INFLIGHT. LT ENGINE FAILED ON FINAL VFR CONDITIONS JUST OUTSIDE EWABE NORMAL LANDING. HAL3392 FIM/MRM CODE: 732145. CURRENT FAULTS/ 732115, 732116, AND 732145 REPLACED NR 1 EEC IAW MM. GROUND RUN CHECK, OK. HAL580/4884 PN OFF 114E6112G1 SN OFF LHBR0208 PN ON 114E6112G120 SN ON LHBR0293 TIME REMOVED: 0430 FAULT CODE: 732145. 2L72 4F4 FTRA6WE E00057EN 20040427000182004042700018NM 2004 4 27 UIEA200400027 120040304A5230 PANEL BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE DOOR LATCH LOOSE A UIEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA15518MC 23476 MXP/BOM ATB DUE TO SIDE CARGO DOOR OPEN LIGHT ON: SIDE CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF AND REMAINED ON AFTER TAKEOFF. FOUND SECURING PANEL ON LATCH DOOR MECHANISM WITH LOOSE SCREWS. TIGHTENED SCREWS, EXERCISED DOOR AND CHECKED OPERATION, FOUND NORMAL. PERFORMED PRESSURIZATION CHECK IAW MM 21-31-00, ALL NORMAL. AIRCRAFT WAS DEPRESSURIZED AND FUEL DUMPED PRIOR TO LANDING. 2L74 4F4 F A20WE E23EA 20040427000192004042700019NM 2004 4 27 UIEA200400025 120040301A5280 RETAINER BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL MLG DOOR SEAL CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15408MC 29261 CORROSION FOUND IN PORTION OF MISSING SEAL RETAINER. FORM OF CORROSION (FLAKING, PITTING) FOUND. CORROSION CLEANED UP IAW SRM 51-10-02 ALODINE 1200 APPLIED AND REPROTECTED WITH BMS 10-11 TY1. 2L74 4F4 FRT1384945 E23EA 20040427000232004042700023EU 2004 4 27 USA2004F00000 120040225A2120 ODOR AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19725UW 1135 ENROUTE PIT-IAH. DURING FLIGHT, NOTICED OILY ODOR AT MID-CABIN. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATED THE AIR CONDITIONING PACKS WITH THE APU. NO ODOR DETECTED. CHECKED APU AREA. NO OIL DRAINAGE NOTED. FOUND AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20040427000302004042700030EA 2004 4 27 A6WA200440029 120040310A3220161XX101 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG DISCONNECTED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31446AW1694 7806 AFTER TAKEOFF SELECTED GEAR UP, GOT GEAR UP DISAGREE. RAN THROUGH CHECKLIST AND RETURNED. ALSO, GOT NWS INOPERATIVE, WOW INPUT CAS MESSAGE. INSPECTED AND FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED TORQUE LINKS (PN 16144-101UPPER, 16154-101 LOWER). 2L72 4F4 FRTA21EA E15NE 20040427000322004042700032WP 2004 4 27 GTIA040157 120040301A2560 SIGN DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE CABIN MISSING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23832NK 49618 SAF T GLO EMERGENCY EXIT SIGN MISSING L2 DOOR AFT POSITION. LOCATED SIGN UNDER GALLEYS CART, CLEANED AREA, REPLACED BROKEN EXIT SIGN, REINSTALLED WITH DOUBLE SIDED TAPE. 2L72 4F4 FRTA6WE E2EA 20040427000332004042700033WP 2004 4 27 GTIA040158 120040110A716059306451 NOSE COWL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RT ENGINE MISSING A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23834NK 49847 RT ENGINE NOSE COWL SN 49123 ACOUSTIC LINING MISSING ON LOWER HALF OF PERFORATED INTERIOR. REMOVED NOSE COWL. INSTALLED RT NOSE COWL. 2L72 4F4 FRTA6WE E2EA 20040427000352004042700035NM 2004 4 27 AMTA200400200 120040224A7712ETPU30001 SENSOR BOEING757 75733N 1384931NM RROYCERB211 RB211* 54555NE RT ENGINE MALFUNCTIONED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11556TZ14282 32590 31865 RT ENGINE NR 2 WENT TO O/S 103.4 4SEC. REMOVED AND REPLACED TPSU IAW AMM. OPS CHECK IAW 71-00-00-5 TEST 3. OK FOR SERVICE. 2L72 4F4 FRTA2NM A12EU 20040427000372004042700037NM 2004 4 27 AMTA200400266 120040306A7720 WARNING LIGHT BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE FALSE ACTIVATIONA AMTAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL11556TZ 32590 31865 RT TURBINE OVHT DET 2 STATUS MESSAGE APPEARED AND THEN CLEARED. PERFORMED TURBINE OVERHEAT DET SYSTEM BITE. IAW FIM 26-13-00 FIG 103 SHEET 1 THRU 3. NO FAULTS NOTED. NO MESSAGES DISPLAYED. SYSTEM OPERATION OK. 2L72 4F4 FRTA2NM E12EU 20040427000582004042700058EU 2004 4 27 BAQA094069 120040401A6420 BEARING BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE FORK LINK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 3742 7243 FORK LINK BEARING WORN PREMATURELY. S/N 3040 WAS TAKEN FROM ASSET AND USED ON PBH. REC'D S/N 3675 FROM AEC TO REPLACE ASSET STOCK. REPLACED WITH SERVICABLE UNIT FROM AEC. 1G72 3U3 U H13EU E5NE 20040427000632004042700063EU 2004 4 27 BAQA093756 120040412A6330L633M2010104 MOUNT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE TRANSMISSION LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03601FH127 0069 GEARBOX MOUNT IS LEAKING EXCESSIVLEY (FLAT). REPLACED WITH SERVICABLE UNIT FROM AEC, 04/19/2004 1G72 3U3 UO H88EU E42NE 20040427000792004042700079 2004 4 27 BAQA094207 420040421A3442071015190101 RADAR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME880 7235 TRANSMITTER FAULT/PAINTS ON ONE SIDE/TX FLT/ANT FLT. REPLACED WITH SERVICEABLE UNIT, 04/22/2004 1G72 3U3 U H13EU E5NE 20040427000802004042700080NM 2004 4 27 DLM90040265 120040324A2420 GENERATOR DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 1 ENGINE BROKEN A DALAO OTHER O OTHER CLCLIMB 1 SO27913DN215574200 53393 020017 LT GEN FAILED IN CLIMB WITH GEN OFF, LIGHT ILLUMINATED. RESET ONCE UNSUCCESSFUL. VERBAL FROM CREW VIBRATION FELT IN A/C AND YOKE. FOUND GENERATOR BROKEN IN 2 PIECES WITH GEARBOX CONTAMINATED WITH METAL MATERIAL. WILL REQUIRE ENGINE REPLACEMENT. 2L72 4F4 FRTA6WE E40NE 20040427000832004042700083NM 2004 4 27 DL73S040268 120040325A5320654541041 FLOOR SUPPORT BOEING737 737247 138448DNM FUSELAGE FATIGUED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 A CRACKED WAS NOTED IN THE BBL 0.07 LONGITUDINAL FLOOR SUPPORT AT BS 715. CRACKED REMOVED AND FLOOR SUPPORT REPAIRED PER ERA 386095-14AD. 2L72 4F A16WE 20040427000872004042700087NE 2004 4 27 DL75K040274 220040325A7230 COMPRESSOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27685DA46908 27588 716519 HIGH SPEED ABORT LEFT ENGINE APPARENT COMPRESSOR STALL, MAX AIRSPEED 99 KIAS. AFTER STOPPED LT ENG OIL PRESSURE IND WENT RED AND EGT WENT ABOVE RED LIMIT INDICATOR. LEFT ENG SHUTDOWN, MAX BRAKE TEMP -4- ON NR 6. FOUND METAL IN TAILPIPE. BORESCOPED HPC EXTENSIVE DAMAGE BEYOND M/M LIMITS, ENGINE CHANGE REQUIRED. REPLACED NR 1 ENG PER ROUTINE CARD DECK. ALSO C/W HIGH ENERGY CONDITIONAL INSPECTION PER M/M 05-51-14. 2L72 4F4 FRTA2NM E17NE 20040427001032004042700103NM 2004 4 27 DL73S040290 120040401A533065458001178 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4L LAP JOINT BETWEEN BS 259.5 AND BS 360. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089308-14. 2L72 4F A16WE 20040427001042004042700104NM 2004 4 27 DL73S040291 120040401A5210 INTERCOSTAL BOEING737 737247 138448DNM SERVICE DOOR MISINSTALLED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 DURING ACCOMPLISHMENT OF EO03-055852-03AD, THREE INTERCOSTALS WERE NOTED AS BEING DISCREPANT AS NOTED IN THE INTRODUCTION OF ERA 089386-14. DISCREPANCIES WERE DISPOSTIONED PER ERA 089386-14. 2L72 4F A16WE 20040427001122004042700112NE 2004 4 27 DL757040299 220040402A7261 B-NUT BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE STRIPPED A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27652DL 24392 716587 RT ENGINE SHUTDOWN BY CREW DUE TO LOSS OF OIL PRESSURE. CONTRACT MTC IN SMF HAS IDENTIFIED NR 5 BEARING SCAVENGE TUBE B-NUT IS STRIPPED AT LUBE OIL SCAVENGE PUMP FITTING. REPLACED TUBE. 2L72 4F4 FRTA2NM E17NE 20040427001192004042700119NM 2004 4 27 DL73S040307 120040405A533065458001172 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10L LAP JOINT BETWEEN BS 259.5 AND BS 303.9. DAMAGE WAS REMOVED AND REPAIRED PER ERA 088638-14. 2L72 4F A16WE 20040427001242004042700124NM 2004 4 27 DL75K040312 120040405A2121 FAN BOEING757 757232 1384965NM FWD BB AFT WALL INOPERATIVE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO276706Q 30422 IN DESCENT THRU FLT LEVEL 200 RT RECIRC FAN INOP, LIGHT ILLUMINATED WITH MSG, DETECTED FUMES IN CABIN. FOLLOWED CHECK LIST ODOR WENT AWAY. REMOVED FWD BB AFT WALL, PERFORMED VISUAL INSPECTION OF RT RECIRC FAN AND ASSOCIATED WIRING. REPLACED FAN. 2L72 4F RTA2NM 20040428000102004042800010WP 2004 4 28 ASAA0480147 120040303A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 PDX - FOUND LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 16. REPAIRED DAMAGED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040428000112004042800011WP 2004 4 28 GTIA040221 120040318A7160 LINER DOUG DC9 DC982 3022082WP NR 2 ENG INTAKE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 ACY - NR 2 ENGINE INTAKE LINER LOOSE FOUND ON WALKAROUND. REMOVED DAMAGED ACOUSTIC PANEL LINER. INLET COWL INSPECTION AND REPAIR OF THE DYNA ROHR ACOUSTIC PANELS ACOUSTIC LINING MISSING BETWEEN 4 O'CLOCK AND 8 O'CLOCK POSITION NOSE COWL TO BE REPLACED ON C/O 146482-2. (M) 2L72 4F A6WE 20040428000172004042800017WP 2004 4 28 ASAA0480081 120040220A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01976AS 53452 PHX - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FIRST 7 INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR. LIGTHS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040428000322004042800032CE 2004 4 28 BAQA094035 120040416A2841CMF8014 MONITOR BEECH 100 100BEECH 1152916CE PWA PT6 PT6A27 52043EA FUEL QTY INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 10364 B144 EXCHANGE - CORE RETURN FOR EXCHANGE PO 202350203, INDICATING INTERMITTENT. REPLACED WITH SERVICABLE MONITOR., 04/20/2004 1L72 3T4 T A14CE E4EA 20040428000412004042800041NE 2004 4 28 BAQA093881 220040317A73130319739420 INJECTOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE ENGINE CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH474 0273 WARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/19/2004 1G72 3U3 U H88EU E19EU 20040428000422004042800042NE 2004 4 28 BAQA093896 220040319A7310 LINE BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE FUEL MANIFOLD DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE247 1UV04119 7219 EXCHANGE. ENG S/N LE45573. MANIFOLD HAS TUBE DAMAGE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/23/2004 1G72 3U3 U H13EU E5NE 20040428000482004042800048NM 2004 4 28 DLM88040373 120040426A2740591096257 ACTUATOR DOUG MD88 MD88 3023688NM EMPENNAGE BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27916DL 49591 DURING OPN 5924AD FOUND LOWER MECHANICAL STOP MAKE CONTACT WITH JACKSCREW STOP. LOWER STOP BROKE OFF. REPLACED JACKSCREW ASSEMBLY. 2L72 4F RTA6WE 20040428000542004042800054NM 2004 4 28 SWAA041074 120040415A5320BAC1509100146 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FLOOR SUPPORT AT BS 774 TO BS 777, LBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040428000562004042800056 2004 4 28 SWAA041076 420040415A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE LOOSE. SECURED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040428000582004042800058NM 2004 4 28 SWAA041078 120040415A53116546920 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND FRAME WEB AT BS 639, RT OVERWING EXIT DOOR, CRACKED. REPAIRED FRAME WEB PER ER. 2L72 4F RTA16WE 20040428000602004042800060NM 2004 4 28 SWAA041088 120040416A53136551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER SPLICES AT STRINGER 4R, BS 360, AND BS 908, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20040428000622004042800062NM 2004 4 28 SWAA041090 120040417A53126545409 PRESSURE PANEL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESSURE WEB AT BS 663, LBL 40, CRACKED. REPAIRED WEB PER ER. 2L72 4F RTA16WE 20040428000642004042800064 2004 4 28 SWAA041092 420040417A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428000662004042800066NM 2004 4 28 SWAA041067 120040415A2910272A4451130 LINE BOEING737 7377H4 1384404NM A-HYD SYS LOOSE A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29742SW 29278 AIR TURNBACK, A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. RETORQUED A-SYSTEM HYDRAULIC RESERVOIR RETURN LINE PER MM. 2L72 4F RTA16WE 20040428000682004042800068NM 2004 4 28 SWAA041056 120040414A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 EEPLS COVER AT OVERWING EMERGENCY EXIT BROKEN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040428000702004042800070NM 2004 4 28 SWAA041058 120040414A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND BS 1016, AFT PRESSURE BULKHEAD WEB, AT DOME CAP RBL1, CRACKED. REPAIRED WEB PER ER. 2L72 4F RTA16WE 20040428000722004042800072NM 2004 4 28 SWAA041060 120040414A5320BAC1509100146 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM FROM, BS 727 + 10 TO BS 780, AT RBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040428000742004042800074NM 2004 4 28 SWAA041062 120040414A53106545810 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 291.5 TO BS 332, RBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040428000782004042800078NM 2004 4 28 SWAA041066 120040414A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 428 + 13, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428000812004042800081NM 2004 4 28 SWAA041070 120040415A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 375, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428000832004042800083NM 2004 4 28 SWAA041104 120040418A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29782SA 29808 DURING SPV, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040428000852004042800085NM 2004 4 28 SWAA041106 120040419A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 EEPLS COVER AT RT OVERWING EXIT, MISSING. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040428000872004042800087NM 2004 4 28 SWAA041094 120040418A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 FUSELAGE SKIN AT BS 780, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428000892004042800089NM 2004 4 28 SWAA041127 120040421A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND STRINGER 26L, BS 727 + 5, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040428000912004042800091NM 2004 4 28 SWAA041129 120040421A531265C28106 STIFFENER BOEING737 7373H4 1384600NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016, RT RADIAL STIFFENER CRACKED. REPAIRED STIFFENER PER BAC DRAWING. 2L72 4F RTA16WE 20040428000932004042800093NM 2004 4 28 SWAA041131 120040421A53306545778 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040428000952004042800095 2004 4 28 SWAA041079 420040416A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428000972004042800097 2004 4 28 SWAA041081 420040416A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428000992004042800099NM 2004 4 28 SWAA041083 120040416A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FLOORBEAM AT BS 727D + 5, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040428001012004042800101NM 2004 4 28 SWAA041085 120040416A3350101114 LAMP BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED C2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040428001042004042800104NM 2004 4 28 SWAA041098 120040418A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SPV, FOUND STRINGER 25R, AT BS 896, CRACKED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040428001252004042800125NM 2004 4 28 DL738040334 120040412A3010CFM567 VALVE BOEING737 737832 13844CFNM GE CFM56 CFM56* 13802NE NR 2 ANTI ICE FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO273767 7018 888736 30821 888736 ON TAKEOFF ROLL BELOW 80 KTS NR 2 ENG COWL ANTI-ICE LIGHT ILLUM. DISCONTINUED TAKEOFF. REPLACED NR 2 ENG COWL A/I VALVE PER MM. 2L72 4F4 FRTA16WE E2GL 20040428001282004042800128NM 2004 4 28 DL738040338 120040413A335002031461201 LENS BOEING737 737832 13844CFNM LT OVERWING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27381DA 30350 LEFT OVERWING EMERGENCY EXIT PATH LIGHT LENS BROKEN WON`T STAY ON LIGHT ASSY. REPLACED LENS. 2L72 4F RTA16WE 20040428001292004042800129NM 2004 4 28 DL73S040339 120040414A2697 WIRE BOEING737 737247 138448DNM PACK BAY DAMAGED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27379DL 23606 LEFT WING BODY OVERHEAT LIGHT STARTED BLINKING AFTER T/O. REPAIRED WIRING. 2L72 4F A16WE 20040428001302004042800130NM 2004 4 28 SWAA041109 120040419A575465C26686 SKIN BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND LT WING, NR 2 L/E SLAT LOWER SKIN AT AFT ROW OF RIVETS, CRACKED. REPAIRED NR 2 L/E SLAT SKIN PER SRM. 2L72 4F RTA16WE 20040428001312004042800131NM 2004 4 28 SWAA041110 120040419A53116547959 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SPV, FOUND AFT CARGO DOOR FRAME CUTOUT AT BS 847, STRINGER 25R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040428001322004042800132NM 2004 4 28 SWAA041112 120040419A53156545410 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040428001342004042800134NM 2004 4 28 SWAA041114 120040419A53306547955 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BAY SKIN BETWEEN BEARSTRAP AND INTERCOSTAL LOWER FLANGE AT BS 844, RBL 17, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040428001362004042800136NM 2004 4 28 SWAA041100 120040418A5315BAC1509100146 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL3, CORRODED. REPAIRED BEAM PER EA. 2L72 4F RTA16WE 20040428001382004042800138 2004 4 28 SWAA041117 420040420A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040428001402004042800140 2004 4 28 SWAA041119 420040420A2565D31354 SLIDE BOEING737 7372T4 1384492NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040428001422004042800142NM 2004 4 28 SWAA041121 120040420A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 947, RBL 10, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040428001432004042800143NM 2004 4 28 SWAA041123 120040420A53106545871 DOOR FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR, FORWARD DOOR FRAME CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20040428001462004042800146NM 2004 4 28 SWAA041101 120040418A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM SECTION PER EA. 2L72 4F RTA16WE 20040428001482004042800148 2004 4 28 SWAA041143 420040423A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428001502004042800150NM 2004 4 28 SWAA041145 120040423A53306545835 SKIN BOEING737 7372T4 1384492NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED C3 CHECK, FOUND E/E ACCESS DOOR CUTOUT AT BS 352, AFT LT CORNER CORRODED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040428001522004042800152NM 2004 4 28 SWAA041147 120040423A53126545808 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD AT BS 294.5, STRINGER 11L, FIFTH STOP, CRACKED. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20040428001542004042800154NM 2004 4 28 SWAA041149 120040423A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29711HK 27845 DURING SCHEDULED MV1 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED AFT LT BATTERY PACK PER MM. 2L72 4F RTA16WE 20040428001562004042800156NM 2004 4 28 SWAA041151 120040424A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001572004042800157NM 2004 4 28 DLM88040340 120040414A3230MS288892 SCHRADER VALVE DOUG MD88 MD88 3023688NM NLG MALFUNCTIONED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27967DL 53116 ON TAKEOFF ROLL, NOSE GEAR BOTTOMING OUT. TRIED TO RAISE GEAR NOSE, GEAR DISAGREEMENT AND AUDIO NOISE INDICATED PARTIALLY DOWN OR DOORS OPEN. RAN CHECKLIST, LOWERED GEAR TO 3 GREEN, LANDING UNEVENTFUL AT 136,000 LBS, TOUCHDOWN AT LESS THAN 300 FPM. FOUND SHRADER VALVE O-RING LEAKING. REPLACED SHRADER VALVE AND SERVICED NOSE STRUT PER M/M. SWUNG NOSE GEAR SEVERAL TIMES. OPS CHECKS NORMAL. OK FOR SERVICE. 2L72 4F RTA6WE 20040428001602004042800160NM 2004 4 28 DL73S040344 120040416A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 THE FUSELAGE SKIN LAP JOINTS AND BUTT JOINTS WERE FOUND WITH SEVERAL AREAS OF SCRIBE MARK DAMAGE IN THE PRESSURIZED FUSELAGE AREA BETWEEN FS 360 & 1016, IN THE UPPER PORTION BETWEEN STRINGERS 14L & 14R. THE DAMAGE LAP JOINTS ARE CUT AND REMOVED AND REPAIRED WITH ALUMINUM DOUBLERS. THE DAMAGED BUTT JOINT STRAPS ARE REMOVED AND NEW SECTIONS INSTALLED. THE REPAIRS ARE DOCUMENTED IN ER/A 089653-14. 2L72 4F A16WE 20040428001622004042800162NM 2004 4 28 DL73S040346 120040415A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 INSPECTION OF THE STRINGER 10R SKIN LAP JOINT FROM FS 360 TO 540 PER AD 2003-08-15, REVEALED A SINGLE CRACK AT FS 370. THE CRACK WAS REMOVED WITH A 1 X 4.25 INCH CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3 AND PER ER/A 089539-14AD. 2L72 4F RTA16WE 20040428001762004042800176NM 2004 4 28 DL73S040352 120040419A53306545768134 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089710-14. 2L72 4F A16WE 20040428001782004042800178NM 2004 4 28 DL73S040354 120040419A5330654576535 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089713-14. 2L72 4F A16WE 20040428001802004042800180NM 2004 4 28 DL73S040356 120040419A5330654577245 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089715-14. 2L72 4F A16WE 20040428001812004042800181NM 2004 4 28 DL73S040357 120040419A5330654577246 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089716-14. 2L72 4F A16WE 20040428001832004042800183NM 2004 4 28 DL73S040359 120040417A5330654577416 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 727B+2 ALONG THE BONDED DOUBLER LINE JUST BELOW STRINGER 18L. THE CRACK IS TYPICAL OF BAC S/B 737-53-1065. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE S/B AND PER ER/A 089524-14. 2L72 4F RTA16WE 20040428001852004042800185NM 2004 4 28 DL76L040361 120040418A3397 WIRE BOEING767 767332 1382001NM SEAT 1A SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27199DN 28456 DURING LAYOVER FOUND EMERGENCY LIGHTS AT THE FIRST 5 ROWS ARE INOP. FOUND SHORT IN WIRING AT SEAT 1A. REPAIRED WIRING, CHECKS OK. 2L72 4F RTA1NM 20040428001872004042800187 2004 4 28 DL757040363 420040420A3430341080155 RECEIVER BOEING757 757232 1384965NM E/E BAY OVERHEATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27666DN 25034 CREW REPORTED FUMES IN CABIN AND FLIGHT DECK DURING CRUISE. TURNING OFF UTILITY BUSSES ALLOWED ODOR TO DISSIPATE. CREW ELECTED TO DIVERT INTO IAD (ATL-PVD FLIGHT). DL MTC AND FLT CREW REPORTED FINDING LT ILS RECEIVER CIRCUIT BREAKER TRIPPED. FURTHER MTC INSPECTION OF ILS RECEIVER SHOWED UNIT TO HAVE FAILED/SMOKED AND EMINATING STRONG ODOR. REPLACED TRANSCEIVER. 2L72 4F RTA2NM 20040428001892004042800189NM 2004 4 28 DL757040366 120040421A3397 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27671DN 25332 ON INSPECTION FOUND EMERGENCY LIGHTS INOP ON AFT RIGHT LAVATORY. REPAIRED THREE BROKEN WIRES UNDER AISLE CARPET AT RT AFT LAVATORY PER WSPM. OPN OF LIGHTS NORMAL. 2L72 4F RTA2NM 20040428001912004042800191SO 2004 4 28 C2XA04IA037 120040325A335066367 LIGHT EMB 145 EMB145LR 3260212SO ROW 1-7 INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713979 145181 DURING PREFLIGHT INSPECTION THE FLOOR PROXIMITY LIGHT AT ROWS 1 THROUGH 7 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040428001942004042800194EU 2004 4 28 2004UALA00355 120040414A2497 WIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEAT 25B SHORTED A UALAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 WP29428UA 523 ON FINAL APPROACH WIRES UNDER SEAT 25B SPARKED ELECTRICAL SMOKE. HALON FIRE EXTINGUISHER USED. CAUSE OF ELECTRICAL SPARK WAS IDENTIFIED TO ORIGINATE FROM THE SEAT-TO-SEAT CABLE, WHICH CONNECTS BOTH PES AND PSS DATA. THIS CABLE ALSO CARRIES 110 VAC. PER AIRCRAFT SAFETY, A CUSTOMER (ESCORTED IN PROTECTIVE CUSTODY) WAS KICKING THE SEAT IN FRONT OF HIM, CONTACTING THE SEAT-TO-SEAT CABLE RESULTING IN THIS INCIDENT. REPLACED THE SEAT-TO-SEAT CABLE AND PERFORM AN OPERATIONAL CHECK. 2L72 4F4 FRTA28NM E40NE 20040428001982004042800198 2004 4 28 2004UALA00361 420040414A2565 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DEPLOYED A UALAK NONE O OTHER ININSP/MAINT 1 WP29506UA 24627 AFT LEFT DOOR SLIDE PARTIALLY DEPLOYED WHEN DOOR OPENED FROM OUTSIDE. OPENING DOOR FROM OUTSIDE DID NOT INITIATE DEPLOYMENT. WHEN DOOR WAS OPENED, ONE SIDE OF SLIDE DROPPED BELOW DOOR DUE TO A LOOSE RESTRAINT STRAP. SAME SLIDE WAS REINSTALLED. 2L72 4F4 FRTA2NM E17NE 20040428001992004042800199NM 2004 4 28 CALA0400393 120040419A5330656571034 SUPPORT BOEING737 7373T0 1384582NM ANTENNA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 ANTENNA SUPPORT CORRODED BETWEEN STA 727D AND 727E. REPLACED U-CHANNEL FOR ANTENNA IAW SRM 51-10-02. 2L72 4F RTA16WE 20040429000332004042900033NE 2004 4 29 M7K2004F00000 220040122A7261350A54113800 TUBE UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE ANTI ROTATION CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19802MH163 3707 23036 ENGINE OIL AIR VENT TUBE POSITIONED ALONG THE RT SIDE OF THE ENGINE WITH THE AFT END CURVED UPWARD INTO THE ENGINE EXHAUST AS TO AID THE VENTURI SECTION OF THE OIL AIR VENTING HAS A WELDED CLAMP SUPPORTED BY A STRAP HANGING FROM THE ENGINE TAILPIPE TO PREVENT TUBE ROTATION OUT OF THE GAS/EXHAUST PATH. THIS CLAMP IS ROUTINELY CRACKING DUE TO FATIGUE. NO TUBE ROTATION HAS OCCURRED 3RD FAILURE THIS AC. 1G72 3U3 U H9EU E00054EN 20040429000342004042900034EU 2004 4 29 M7K2004F00001 120040122A1430TL100AXE12L50 FASTENER UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE ENGINE FAIRING SHEARED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19802MH529 3707 23036 1 OF 4 LATCHES ON THE ENGINE FAIRING, THE LATCH HOOK SHEARED AT THE BASE OR CONTACT POINT IN THE HOOK AND EXAMINATION SHOWED NO APPARENT WEAR JUST A SHEAR BREAK LINE WITH SOME CRYSTALIZATION APPARENT MUCH LIKE A FATIGUE FAILURE. THE HOOK IS OF TITANIUM MATERIAL. AN OLDER STAINLESS STEEL VARIENT OF THE LATCH WAS MUCH MORE DURABLE AND WOULD WEAR SLOWLY AND NEVER SHEARED EXCEPT DUE TO WEAR. 1G72 3U3 U H9EU E00054EN 20040426000262004042600026 2004 4 26 SWIA200413135 420040411A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07581SW 120349 AFTER INITIAL POWER-UP AND -AURAL UNIT OKAY-, THE NR 2 STALL SHAKER, CLACKER AND PUSHER ACTIVATED CONTINUOUSLY (AOA VANES WERE CENTERED). REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL. OPS CHECK GOOD AT THIS TIME. P/N: 120-34428-505. 2L72 4T RTA31SO 20040426000332004042600033SO 2004 4 26 C2XA04SH223 120040412A532014521725615 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000402004042600040SO 2004 4 26 C2XA04TY065 120040411A531014522460007 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712563 145612 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GUSSET TOP CAP AT FRAME 20. MAINTENANCE ACCOMPLISHED THE BLEND-OUT REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04, 05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040426000412004042600041SO 2004 4 26 C2XA04BT042 120040330A33503025103 LIGHT EMB 145 EMB145LR 3260212SO FUSELAGE FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716918 145397 DURING 4A INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT OVER RIGHTHAND WING TO BE INOPERATIVE. REMOVED AND REPLACED RIGHTHAND OVERWING EMERGENCY LIGHT IAW EMB145 MM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040426000432004042600043WP 2004 4 26 ABXA040129 120040318A533058911231 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MAIN CABIN CENTER WING BOX HAD CORROSION AT LEFT BUTT LINE 8, STA 850. REPAIRED AREA IAW REA D857-48869MR. 2L74 4F 4A25 20040426000482004042600048NM 2004 4 26 CALA0400407 120040421A55116547534 RIB BOEING737 7373T0 1384582NM RT HORIZ STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 RIGHT HORIZONTAL STAB LEADING EDGE RIBS (4 EACH) DAMAGED AT LOWER AFT EDGE. FIRST FOUR RIBS FROM INBOARD SIDE. TRIMMED OUT DAMAGED AREA ON ALL FOUR RIB WEBS. FABRICATED AND INSTALLED DOUBLERS AND FILLERS TO ALL FOUR RIBS PER SRM 51-70-13. 2L72 4F RTA16WE 20040426000492004042600049SO 2004 4 26 C2XA04SH195 120040403A531514522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000502004042600050WP 2004 4 26 ABXA040135 120040401A2710 LINKAGE DOUG DC8 DC861 3021952WP AILERONS LACK OF LUBE A ABXAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL23848AX 46032 COULD NOT MOVE AILERON TRIM WHEEL DURING DESCENT INTO ILN. LUBED AND INSPECTED LT, RT AND WHEEL WELL AILERON LINKAGES. OPERATED AILERON TRIM THROUGH NUMBEROUS TIMES. OPERATED NORMAL. 2L74 4F 4A25 20040426000532004042600053SO 2004 4 26 C2XA04SH209 120040408A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718556 145595 SHV- DURING C-CHECK STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01265. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000622004042600062NM 2004 4 26 04FDEA001013 120040421A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 SKIN CHAFE DAMAGE FOUND AT BS 950E 12 TO 950E 19 BETWEEN STR 25L TO STR 26L. SKIN CHAFE FOUND TO BE OUT OF LIMITS FROM BS 950E 12 - 950E 19. REPAIRED DAMAGED SKIN FROM 950E 12 TO 950E 19 BETWEEN STR 25L TO 26L PER SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20040426000642004042600064SO 2004 4 26 C2XA04SH200 120040406A491014547494043 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426000682004042600068SO 2004 4 26 C2XA04SH172 120040320A531514521721009 BUTTSTRAP EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714514 145303 SHV- DURING C-CHECK THE FORWARD FLOORBEAM BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426000692004042600069SO 2004 4 26 C2XA04SH175 120040321A491014526850401 FIREWALL EMB 135 EMB135LR 3260305SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT HAND UPPER APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426000792004042600079WP 2004 4 26 ABXA040128 120040318A53405750198 FITTING DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 LONGERON 24 LEFT, STA 980, UPPER LIP CRACKED. REPAIRED AREA IAW REA D853-48872MR. 2L74 4F 4A25 20040426000802004042600080WP 2004 4 26 ABXA040126 120040318A1430 FASTENER DOUG DC8 DC863F 302198FWP FLOOR SUPPORT WRONG PART A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 ATTACH ANGLE TO FLOOR SUPPORT CENTER WING BOX, RIGHT SIDE 857, ANGLE HAD IMPROPER FASTENER INSTALLED. REPAIRED AREA IAW REA D857-48854MR. 2L74 4F 4A25 20040426000812004042600081WP 2004 4 26 ABXA040125 120040318A53115754671502 FRAME DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 AFT LOWER CARGO STA 1140, ABOVE LONGERON 35 RIGHT, RIVNUT INSTALLED THROUGH PORTION OF FASTENER HEAD. REPAIRED AREA IAW REA D853-48864MR. 2L74 4F 4A25 20040426000822004042600082WP 2004 4 26 ABXA040118 120040318A53145750043 KEELBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 MID SHIP ACCESSORY COMPARTMENT, FS 640 - 660, L-36 KEEL BEEM EXTENSION CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ABX REA D853-48863MR, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. 2L74 4F 4A25 20040426000882004042600088 2004 4 26 SWIA200413100 420040324A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER INOPERATIVE A SWIAD RETURN TO BLOCK LP NO TEST NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07229SW9150 9150 120305 NR 2 STALL SHAKER INOP. REPLACED FIRST OFFICER'S STICK SHAKER SERVO PER MM 27-00-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20040426000912004042600091 2004 4 26 SWIA200413103 420040326A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07214SW 120280 STALL WARNING LIGHT ILLUMINATES ON THE MAP. REMOVED AND REPLACED STALL PANEL. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040426000942004042600094EA 2004 4 26 SWIA200413106 120040330A2750 FLAP CNDAIRCL600 CL6002C10 1390015EA OUT OF RIG A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07703SK 10139 FLAPS HALF SPEED MSG ON EICAS. RIGGED FLAPS IAW MM 27-52-00-802-A01, TR 27-0190. 2L72 4F RTA21EA 20040426000952004042600095EA 2004 4 26 SWIA200413107 120040401A2780766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07702SK 10136 SLATS HALF SPEED MESSAGE. REMOVED AND REPLACED LEFT SLAT/FLAP CONTROLLER. OPS CHECK GOOD IAW 27-51-05. 2L72 4F RTA21EA 20040426000962004042600096 2004 4 26 SWIA200413108 420040402A34256226190204 COMPUTER EMB 120 EMB120ER 3260203SO E/E BAY MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07583SW7656 2784 120351 AP DISCONNECTED, ASSOCIATED WITH -FD- ANNUNCIATOR ON CAPTAIN'S EADI AND -ERRATIC BEHAVIOR- FROM F/O'S FLIGHT DIRECTOR DISPLAY, IT DISCONNECTED WHILE AP WAS ON F/O'S COMPUTER. INSTALLED SERVICEABLE AHRS COMPUTER ON CAPTAINS SIDE. AUTOPILOT AND AHRS OPS CHECK GOOD PER 34-21-00. 2L72 4T RTA31SO 20040426001072004042600107NE 2004 4 26 2004UALA00327 220040409A7200 ENGINE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 MALFUNCTIONED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29929UA 26652 RETURNED TO FIELD DUE TO NR 2 ENGINE POWER PROBLEM. DOWNLOAD FROM FLIGHT DATA RECORDER (FDR) FOUND POWER LOSS ON THE NR 1 ENGINE. FOUND NR 1 POSITION SPAR VALVE WIRING W802-002-18 & W802-005-20 SHORTED TOGETHER UNDER CLAMP, 65 INCHES FROM CONNECTOR D5162P AND REPAIRED WIRING. AS PERCAUTIONARY, ACCOMPLISHED NR 1 ENGINE POWER ASSURANCE RUN & ACCELERATION CHECKS. 2L72 4F4 FRTA16WE E2GL 20040426001092004042600109NM 2004 4 26 2004UALA00329 120040412A2613 WARNING LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 ENGINE ILLUMINATED A UALAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 WP29921UA 25388 ON APPROACH AT APPROX 4000 FT, NR 2 ENG HAD AN OVERHEAT WARNING. PULLED THROTTLE BACK. LIGHT STAYED ON, THEN SHUT DOWN ENG. LIGHT STAYED ILLUMINATED AND CAPT FIRED THE LEFT FIRE BOTTLE. INDICATION PROBLEM IN THE FIRELOOP SYSTEM. FIRELOOP (A) WAS INOPERATIVE PER MEL 2611 THE PREVIOUS DAY ELIMINATING REDUNDANCY FEATURE OF THE FIRELOOP SYSTEM. FIRELOOP (B) FAILED CAUSING OVERHEAT LIGHT TO GO ON. REPLACED BOTH ENGINE CORE DETECTOR ELEMENTS M1122 DUE TO FAILURE OF MINIMUM 40 MEGOHMS RESISTANCE CHECK. 2L72 4F4 FRTA16WE E2GL 20040426001252004042600125SO 2004 4 26 C2XA04SH238 120040423A531313500377005 STRUCTURE EMB 135 EMB135ER 3260203SO STRINGER GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE STRINGER REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001272004042600127SO 2004 4 26 C2XA04SH242 120040423A491014547494403 FIREWALL EMB 135 EMB135ER 3260203SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP OF THE RIGHT VERTICAL STIFFENER. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001422004042600142SO 2004 4 26 C2XA04SH193 120040403A531514526437001 BUTTSTRAP EMB 145 EMB145LR 3260212SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001542004042600154SO 2004 4 26 C2XA04SH179 120040324A531514590321301 STRAP EMB 135 EMB135ER 3260203SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE FORWARD FLOORBEAM AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DIGITAL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001562004042600156SO 2004 4 26 C2XA04SH181 120040324A541114576056007 RIB EMB 135 EMB135ER 3260203SO NR 1 NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE NR 1 ENGINE UPPER COWLING, AFT OUTBOARD RIB WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001692004042600169SO 2004 4 26 C2XA04TY068 120040412A531514521713003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712921 145354 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLISHED THE DOUBLER REPAIR IAW EMB SRM 53-21-10 AND CPM 51-21-04,05 AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040426001762004042600176SO 2004 4 26 C2XA04BT039 120040324A2910TY204103A CONTROL UNIT EMB 135 EMB135LR 3260305SO HYD SYSTEM LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW27175077938 7938 145215 CREW REPORTED NR 1 HYDRAULIC QUANTITY LOW LEVEL INFLIGHT. AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO EWR. EWR MAINTENANCE REMOVED AND REPLACED NR 1 ICU IAW EMB135 AMM 78-33-01. SERVICED HYDRAULICS, OPS CHECKED AND LEAK CHECKED GOOD. PERFORMED OPERATIONAL CHECK OF HYDRAULIC SYSTEM IAW EMB135 AMM 29-10-00. OPS CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040426001812004042600181NM 2004 4 26 2004UALA00339 120040413A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME STA 1400 INNER FLANGE HAS A DENT AT STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040426001832004042600183SO 2004 4 26 C2XA04TY058 120040328A532014521725001 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729515 145309 TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOOR SUPPORT FRAME WAS CORRODED AT FR 20 AND FR 21. MAINT REMOVED AND REPLACED THE LEFT FORWARD SILL IN THE AFFECTED AREA IAW EMB 135/145 SRM 51-40-02; 51-40-06 AND 51-20-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040426001842004042600184SO 2004 4 26 C2XA04SH182 120040327A542014576631621 STIFFENER EMB 135 EMB135LR 3260305SO NR 1 NACELLE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE NR 1 LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001942004042600194SO 2004 4 26 C2XA04TY057 120040328A531514521699003 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729515 145309 TYS DURING A SCHEDULED 2C INSPECTION THE LEFT FLOORBEAM CAP HAD AREAS OF CORROSION AT FR 19-23. MAINT REMOVED AND REPLACED THE LEFT FLOORBEAM TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040426002022004042600202NM 2004 4 26 2004UALA00348 120040413A5347 SEAT TRACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 SEAT TRACK BETWEEN BS 639 AND 706 LBL 44 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK SECTION. 2L72 4F4 FRTA16WE E2GL 20040426002102004042600210SO 2004 4 26 C2XA04IA046 120040405A3350 SWITCH EMB 145 EMB145 3260210SO EMERGENCY LIGHT MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716961 145103 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT ARMING SWITCH AND THE LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. THE DISCREPANCY WAS THEN CLEARED. 2L72 4F RTT00011AT 20040426002142004042600214NM 2004 4 26 2004UALA00354 120040401A575469735491 SUPPORT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 3 SLAT BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29333UA 24228 TIE DUCT FLANGE & SUPPORT BRACKET BROKEN. REMOVED AND REPAIRED BROKEN TAI DUCT FLANGE AND BROKEN SUPPORT, REINSTALLED. 2L72 4F4 FRTA16WE E2GL 20040427000062004042700006SW 2004 4 27 TZ02004F00000 120040213A57512709 HINGE BBAVIA8 8GCBC 1220803SW LYC O360 O360C1E 41514EA HARTZLHCC2Y HCC2YR1 GL AILERON CRACKED B TZ0RK NONE O OTHER ININSP/MAINT 1 NM055060M770 32679 L2722636A CH24356 CONDUCTED ANNUAL INSPECTION ON AIRCRAFT. FOUND BOTH LEFT AND RT AILERON CONTROL ROD ATTACH POINTS TO CONTROL SURFACES TO BE CRACKED. SPECULATE DAMAGE MAY HAVE BEEN INDUCED BY WIND ACTION AND LACK OF USE OF CONTROL SURFACE LOCK. 1H71 3O3 O A21CE E286 5 CP920 20040427000102004042700010SW 2004 4 27 ALG2004F00008 120040223A6320 CHIP DETECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANSMISSION CONTAMINATED E ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03627AL 53284 DURING TAKEOFF, TRANSMISSION LIGHT CAME ON FOR 30 SECONDS THEN IT WENT OFF. MAINTENANCE FOUND CARBON PARTICLES ON PLUG, CHANGED FILTER AND OIL GROUND RAN LEAKED CHECK GOOD. 1G71 3U3 UO H2SW E1GL 20040427000392004042700039SO 2004 4 27 SIMA200405901 120040222A524712024234039 ACCESS DOOR EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL TAILCONE MISSING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21840AE 145656 DURING POSTFLIGHT WALKAROUND, CREW REPORTED THE APU TAILCONE ACCESS DOOR TO BE MISSING. MAINTENANCE FOUND NO DAMAGE OTHER THAN MISSING PAINT AROUND ACCESS DOOR. THE DOOR WAS REPLACED IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200404665) 2L72 4F4 FRTT00011ATTE6CH 20040427000422004042700042SO 2004 4 27 SIMA200606403 120040304A2120 ODOR EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL COCKPIT DETECTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21701MH 145162 CREW NOTED BURNING ODOR IN COCKPIT DURING TAXI. PERFORMED GVI OF FORWARD AVIONICS AND UNDER FLOOR COMPARTMENTS. PERFORMED OPERATIONAL CHECKS OF WINDSHIELD HEAT, ANTI-ICE, AIR CONDITIONING AND ENGINES WITH NO DESCREPANCIES NOTED. AC RETURNED TO SERVICE. (SW21200404961) 2L72 4F4 FRTT00011ATTE6CH 20040427000552004042700055EU 2004 4 27 BAQA092601 120040225A3340 MOTOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101* NE LANDING LIGHT SEIZED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117CJ 63482 7051 LANDING LIGHT MOTOR SEIZED IN UNIT. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1G72 3U3 U H13EU E5NE 20040427000602004042700060EU 2004 4 27 BAQA093958 120040330A6720 BEARING BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE PITCH LINK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 TAIL ROTOR PITCH LINK BEARINGS PREMATURELY WORN. REPLACED WITH SERVICABLE UNIT FROM AEC. 04/16/2004 1G72 3U3 U H13EU E5NE 20040427000692004042700069EA 2004 4 27 BAQA094234 220040422A7314913800033 PUMP BEECH 100 100BEECH 1152916CE PWA PT6 PT6A27 52043EA FUEL PUMP LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03999G 10364 B144 FUEL PUMP LEAKING. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1L72 3T4 T A14CE E4EA 20040427000742004042700074EU 2004 4 27 BAQA093828 120040217A243523081057 STARTER GEN UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH2074 0179 STARTER GEN WOULD NOT START ENGINE. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 UO H88EU E42NE 20040427000762004042700076 2004 4 27 BAQA093850 420040227A3416066306403 ALTIMETER BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101* NE COCKPIT MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WS494 7068 ENCODING ALTIMETER LAGGING AND LACKING BY 600 FT. REPLACED WITH SERVICEABLE UNIT. 03/23/2004 1G72 3U3 U H13EU E5NE 20040427000822004042700082NM 2004 4 27 DL73S040267 120040325A55516573781501 ATTACH FITTING BOEING737 737247 138448DNM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 CORROSION WAS NOTED ON THE LUGS OF THE HORIZONTAL STABILIZER CENTER SECTION REAR SPAR HINGE AND HOUSING FITTING. CORROSION REMOVED AND FITTINGS REWORKED IAW ERA 386232-14. 2L72 4F A16WE 20040427000892004042700089NM 2004 4 27 DLM88040276 120040328A2120 ODOR DOUG MD88 MD88 3023688NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27959DL 49978 PASSING THRU 10,000 MSL NOTICED ELECTRICAL ODOR, NO SMOKE OR HAZE NOTED. PERFORMED DUCT BURNOUT AND INSPECTED AIRCRAFT. 2L72 4F RTA6WE 20040427000922004042700092NM 2004 4 27 DL73S040279 120040326A5330654577895 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27239WA 23187 DAMAGED HOLES FOUND IN STR 20R LAP SPLICE FASTENER ROWS. DURING REPLACEMENT OF UPPER SKIN PANEL BETWEEN STA 916-990. REPAIRED PER ERA 386177-14. 2L72 4F A16WE 20040427000932004042700093NM 2004 4 27 DL73S040280 120040329A5330654577646 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S25L LAP JOINT BETWEEN BS 727 AND BS 908. DAMAGE WAS REMOVED AND REPAIRED PER ERA 088651-14. 2L72 4F A16WE 20040427000942004042700094NM 2004 4 27 DL764040281 120040330A3260849704 PSEU BOEING767 767432ER 1385134NM E1 RACK MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27839MH 29712 IN CRUISE MASTER WARNING SOUNDED AND MASTER CAUTION ILLUMINATED WITH GEAR DISAGREE CAUTION AND INTRANSIT INDICATIONS FOR BOTH MAIN/NOSE GEAR NORMAL UP INDICATION. AIR/GROUND AND NOSE DISAGREE STATUS MSG. GEAR RETRACTION NORMAL AT T/O. NO ABNORMAL CONDITIONS DURING CLIMBOUT/CRUISE. NO VIBRATION NOTED AIR TURNBACK WAS RECOMMENDED TO LAX. REPLACED PSEU PER M/M AND CHECKS NORMAL. MSG CLEARED. 2L72 4F RTA1NM 20040427000992004042700099NM 2004 4 27 DLM88040286 120040401A492038005041 APU DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE APU BAY FAILED A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27979DL14744 53266 P80354 SMOKE IN CABIN FROM PACKS WHEN FIRST APPLIED FROM APU ON TAKEOFF. NORMAL POWER WITH EGT QUITE HIGH, ABOUT 585 DEG, GOT A BURNING ODOR THAT SET OFF SMOKE DETECTORS IN AFT LAV LASTED ONLY A SHORT TIME. REPLACED APU PERFORMED DUCT BURNOUT AND REPLACED WATER BAGS. 2L72 4F4 FRTA6WE E2EA 20040427001182004042700118NM 2004 4 27 DL73S040306 120040405A5330655298878 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S14L LAP JOINT BETWEEN BS 908 AND BS 960. DAMAGE WAS REMOVED AND REPAIRED PER ERA 088591-14. 2L72 4F A16WE 20040427001212004042700121NM 2004 4 27 DL73G040309 120040405A5711654532421 SPAR BOEING737 73735B 13844BMNM RT WING FATIGUED A DALAK NONE O OTHER ININSP/MAINT 1 SO27223DZ 23972 THE LEFT WING REAR SPAR CHORD WAS FOUND TO BE CRACKED AT APPROX RSS 223. THE SUBJECT HOLE IS COMMON TO THE MLG BEAM ATTACH FITTING. DAMAGE WAS REMOVED AND REWORKED PER ERA 386257-14. 2L72 4F RTA16WE 20040427001262004042700126NE 2004 4 27 DL73S040314 220040405A7200 ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15 52051NE NR 2 MALFUNCTIONED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27307DL45578 23079 709216 ABORTED T/O DCA DUE TO NR 2 ENG EPR HUNG AT 1.6, N1, N2, EGT, FF LOWER THAN NR 1. CLEARED RUNWAY, RAN ENG TO FULL POWER OK. SUSPECT CROSSWIND FOR THE LEFT AFFECTED NR 2. DID STATIC RUNUP PRIOR TO 2ND T/O, NR 2 SLOWER TO ACCEL TO T/O THAN NR 1, BUT DID REACH T/O. ALL PARAMETERS THE SAME EXCEPT N1, NR 1, 87 PERCENT, NR 2, 92 PERCENT. REMAINDER OF FLT, ALL INST NORMAL. REPLACED NR 2 EPR TRANSMITTER AND SERVICED BELLOWS ON NR 2 ENGINE FUEL CONTROL. RAN ENG TO T/O POWER, ALL INDICATIONS NORMAL. 2L72 4F4 FRTA16WE E2EA 20040428000022004042800002NM 2004 4 28 DLM88040368 120040423A4990491201119 OIL CAP DOUG MD88 MD88 3023688NM APU LEAKING A DALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27973DL 53241 ON TAKEOFF AFT LAV SMOKE DETECTOR WENT OFF, WITH SLIGHT ODOR IN CABIN AND COCKPIT, AFTER 30 SEC ODOR WENT AWAY AND ALARM CEASED. REPLACED LEAKING APU OIL CAP AND PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20040428000092004042800009WP 2004 4 28 ASAA0480079 120040219A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01976AS 53452 PHX - FOUND EMEREGNCY FLOOR TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040428000272004042800027 2004 4 28 GTIA040173 420040302A2565 CLIP DOUG DC9 DC982 3022082WP GIRT BAR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 LGA - FLT 197 - FOUND GIRT BAR RETAINER CLIP ON AFT GALLEY SERVICE DOOR HARD TO SET GIRT BAR IN. ADJUSTED AFT GALLEY SERVICE DOOR GIRT BAR HOLDER CLIPS. (M) 2L72 4F A6WE 20040428000432004042800043EA 2004 4 28 VNAA0403019 120040331A33502013BR POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL07209PS685 7874 AIRCRAFT N209PS WAS A SPARE AIRCRAFT IN DAY. THE NR 1 EMERGENCY BATTERY POWER SUPPLY WAS FOUND TO BE BAD. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY BATTERY POWER SUPPLY IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040428000452004042800045NM 2004 4 28 DL777040370 120040424A3350 FUSE BOEING777 777232 1385232NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27862DA 29734 EMERGENCY LIGHTS AT SEATS 44 THROUGH 55 INOP. REPLACED BATTERY PACK FUSE. 2L72 4F RTT00001SE 20040428001032004042800103NM 2004 4 28 SWAA041097 120040418A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESSURE WEB AT BS 673, RBL 36, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040428001052004042800105 2004 4 28 SWAA041099 420040418A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428001062004042800106NM 2004 4 28 DLM90040325 120040409A3244 TIRE DOUG MD90 MD9030 3023690NM NR 2 CUT A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27911DA 53391 ITEM CUT IN NR 2 MAIN TIRE. REPLACED NR 2 MAIN WHEEL ASSY PER M/M. 2L72 4F RTA6WE 20040428001072004042800107NM 2004 4 28 DL76S040326 120040409A3320 LIGHT BOEING767 767332 1382001NM MID GALLEY SPARKS A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27117DL 23276 FLIGHT ATTENDANT REPORTED BURNING EMBER FELL OUT OF OVERHEAD AREA IN MID GALLEY. MTC PULLED CEILING PNLS DOWN IN MID GALLEY AREA. INSPECTED LIGHTING FIXTURES AND WIRING. INSPECTED C/B PANEL AND COFFEMAKERS AND WIRING. NO PROBLEMS FOUND. A/C OK FOR SERVICE. 2L72 4F RTA1NM 20040428001082004042800108NM 2004 4 28 DL76L040327 120040409A2120 ODOR BOEING767 767332 1382001NM GALLEY DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27179DN 25144 ON DESCENT INTO JFK CREW NOTICED A PECULIAR ODOR DIRTY SOCKS OR LAV ODOR, THEN DEAD HEADING CREW REPORTED SMELLING ELECTRICAL SMOKE. NO VISIBLE SIGN OF SMOKE OBSERVED. 2L72 4F RTA1NM 20040428001092004042800109NM 2004 4 28 DL764040329 120040410A2120 ODOR BOEING767 767432ER 1385134NM AFT CABIN DETECTED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27826MH 29697 DURING TAXI OUT, F/A AND PASSENGERS REPORT ELECTRICAL ODOR IN AFT CABIN CAPT SIDE. ODOR DISSIPATED BUT CAME BACK DURING TAXI IN. CHECKED ABOVE ROW 46 AND 47 CEILING PANELS AFT CARGO COMPARTMENT IFE RACKS, RAN CHILLERS AND OVENS TURNED ON ALL LIGHTS, CHECKED BREAKERS IN E/E AND AFT CARGO, ALL NORMAL. TAXIED AIRCRAFT AND PULLED POWER ON ENGINES, NO ODOR NOTED. OK FOR SERVICE. 2L72 4F RTA1NM 20040428001102004042800110NM 2004 4 28 DL73G040330 120040412A5330654577572 SKIN BOEING737 73735B 13844BMNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27223DZ 23972 A DENT AND GOUGE WERE NOTED IN THE UPPER SKIN AT BS 807 NEAR S25R. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 089247-14. 2L72 4F RTA16WE 20040428001112004042800111NM 2004 4 28 DL73G040331 120040412A531565C339503 FLOORBEAM BOEING737 73735B 13844BMNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27223DZ 23972 CORROSION WAS NOTED ON THE UPPER CAP OF THE BS 986.5 FLOORBEAM. UPPER CAP REMOVED AND NEW SECTION SPLICED IN PER ERA 089197-14. 2L72 4F RTA16WE 20040428001122004042800112NM 2004 4 28 DL73G040332 120040412A53306545767130 SKIN BOEING737 73735B 13844BMNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27223DZ 23972 TWO DENTS WERE NOTED IN THE FUSELAGE SKIN JUST ABOVE S16L, NEAR BS 384 AND 400. DAMAGE WAS REWORKED PER ERA 089089-14. 2L72 4F RTA16WE 20040428001132004042800113NM 2004 4 28 SWAA041132 120040422A33501000679 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29073SW 22673 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040428001142004042800114NM 2004 4 28 SWAA041133 120040422A335090083 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 EEPLS AT ROW 10 DEF AND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040428001152004042800115NM 2004 4 28 SWAA041134 120040422A2560P4010021 BATTERY BOEING737 7373Y0 1384671NM FLASHLIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040428001162004042800116NM 2004 4 28 SWAA041135 120040422A3350311500 LENS BOEING737 7372T4 1384492NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 3 DEF. SECURED LIGHT LENS PER MM. 2L72 4F A16WE 20040428001172004042800117 2004 4 28 SWAA041136 420040422A2565D31354 SLIDE BOEING737 7372T4 1384492NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040428001182004042800118NM 2004 4 28 SWAA041137 120040422A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 805, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001192004042800119NM 2004 4 28 SWAA041138 120040422A5310BAC15172294 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FWD FRAME CUTOUT AT AFT STOP FITTINGS CRACKED. REPAIRED DOOR CUTOUT FRAME PER SRM. 2L72 4F RTA16WE 20040428001202004042800120NM 2004 4 28 SWAA041139 120040422A5552183A8410 BUSHING BOEING737 7373H4 1384600NM ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PUSHROD BUSHINS PER MM. 2L72 4F RTA16WE 20040428001212004042800121NM 2004 4 28 SWAA041140 120040422A3350101114 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C2 CHECK, FOUND LT EMERGENCY EXIT HATCH LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040428001222004042800122NM 2004 4 28 SWAA041141 120040422A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 14, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040428001232004042800123NM 2004 4 28 DL75A040333 120040410A5330146N37505 SKIN BOEING757 757212 1384951NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27752AT 23128 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1645, JUST BELOW STRINGER 19R. THE DENT WAS REMOVED WITH A 3.5 X 3.2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 089688-14, REV A. 2L72 4F RTA2NM 20040428001242004042800124 2004 4 28 SWAA041108 420040419A2565411N20873 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20040428001262004042800126NM 2004 4 28 DL764040335 120040413A2120 ODOR BOEING767 767432ER 1385134NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27828MH 29699 ON GROUND STRONG ELECTRICAL ODOR CAN BE SMELLED IN AFT SECTION OF PAX CABIN. LEFT REAR, CENTER LEFT AND RIGHT FRONT DOORS WERE OPEN. NO ODOR DECTECTED. CK'ED ALL BREAKERS IN AFT GALLEY TO SEE IF ANY WERE POPPED, NO C/B'S OPENED. CK'ED LAV FOR DISCHARGED FIRE EXTINGUISHERS, NONE WERE DISCHARGED 2L72 4F RTA1NM 20040428001272004042800127NE 2004 4 28 DL76L040337 220040413A7261 CARBON SEAL BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE LEAKING A DALAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27176DN39451 25061 724688 MID CABIN SMOKE DETECTORS AND AFT CABIN SMOKE DETECTORS CAME ON SHORTLY AFTER T/O, NOTICED MUSTY ODOR AND AGAIN AT TOD IN PASSENGER CABIN. ATL MAINT ALSO FOUND OIL LEAK AT NR 2 ENG INLET. FOUND 100 CCS OIL IN NR 2 ENG INTAKE. SUSPECT FROM FRAME LE OIL CONSUMPTION HIGHER THAN NR 1 FOR LAST 30 DAYS. OPENED AND REMOVED NOSE COWL. REPLACED NR 1 AND 1.5 CARBON SEALS A SEATS ON NR 2 ENG PER DAJIC M522. RT NOSE COWL INSTALLED PER M/M. RAN ENG PER PFM, OPS NORMAL. 2L72 4F4 FRTA1NM E24NE 20040428001452004042800145NM 2004 4 28 SWAA041125 120040420A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001472004042800147NM 2004 4 28 SWAA041142 120040423A2560P4010021 BATTERY BOEING737 7372H4 138448CNM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F A16WE 20040428001492004042800149NM 2004 4 28 SWAA041144 120040423A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 765, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001512004042800151NM 2004 4 28 SWAA041146 120040423A53106545469 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 26R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040428001532004042800153NM 2004 4 28 SWAA041148 120040423A3350101073 LENS BOEING737 7373TO 138447GNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT DOOR LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040428001552004042800155 2004 4 28 SWAA041150 420040424A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428001582004042800158NE 2004 4 28 DLM88040341 220040414A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FIRE A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO27969DL34155 53172 725527 ON TAXI OUT ANOTHER AIRCRAFT REPORTED SMOKE AND OR FIRE ON NR 2 ENGINE. REPLACED ENGINE. 2L72 4F4 FRTA6WE E9NE 20040428001592004042800159 2004 4 28 DL76S040343 420040415A3440 SWITCH 13206001 BOEING767 767332 1382001NM MODULE OVERHEATED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27125DL NA 24075 ON DESCENT STARTED TO DETECTED A SLIGHT BURNING ODOR, ELECTRICAL ODOR. CREW DECLARED AN EMERGENCY. FOUND GPWS MODULE OVERHEATED. REMOVED MODULE AND FORWARDED TO MCO AND PLACARD. 2L72 4F RTA1NM 20040428001612004042800161NM 2004 4 28 DL73S040345 120040414A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 540 & 727 PER AD 2003-08-15, REVEALED 15 CRACK INDICATIONS. THE ENTIRE LAP JOINT WAS CUT OUT AND REPLACED WITH ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ER/A 089523-14AD. 2L72 4F RTA16WE 20040428001632004042800163NM 2004 4 28 DL75K040347 120040416A335020131A BATTERY PACK BOEING757 757232 1384965NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27644DL 23998 FWD ZONE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK FOR FWD ZONE AND TESTED GOOD. 2L72 4F RTA2NM 20040428001642004042800164NM 2004 4 28 SWAA041152 120040424A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 986 TO BS 1006, STRINGER 27L, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001662004042800166NM 2004 4 28 SWAA041154 120040424A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, LBL 17, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040428001682004042800168NM 2004 4 28 SWAA041156 120040424A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C4 CHECK, FOUND PHOTOLUMINESCENT STRIPS AT 10 D AND 15 C, WORN. REMOVED AND REPLACED STRIPS PER MM. 2L72 4F RTA16WE 20040428001702004042800170NM 2004 4 28 SWAA041158 120040425A335020131A BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY AND FWD SERVICE EXTERIOR EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040428001712004042800171NM 2004 4 28 SWAA041160 120040425A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001732004042800173NM 2004 4 28 DL73S040349 120040417A3350340638500 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27316DL 23088 EMERGENCY INSEAT LIGHTING SEATS 21-24 INOP. REPLACED FUSE IN PWR SUPPLY M9013. CHECKS OK. 2L72 4F RTA16WE 20040428001752004042800175NM 2004 4 28 DL73S040351 120040419A5330654577247 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089708-14. 2L72 4F A16WE 20040428002012004042800201NM 2004 4 28 CALA0400395 120040419A551065C26389 CLIP BOEING737 7373T0 1384582NM LT ELEVATOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 LEFT ELEVATOR O/B SIDE HINGE PANEL SUPPORT CRACKED. INSTALLED CLIP PER SRM 55-20-02 FIG 1; 51-30-01 FIG 2. 2L72 4F RTA16WE 20040429000482004042900048GL 2004 4 29 ALGA093964 220040326A726023071895 GEAR BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032618 1081 45503 CAE895112 FOUND HEAVY SPALLING ON GEAR TEETH. 1G71 3U3 U H2SW E1GL 20040429000492004042900049EU 2004 4 29 YLYL093965 120040316A8011 COMMUTATOR UROCOPEC120 EC120B 8680987EU TMECA ARRIELARRIEL2B NE STATIC INVERTER FAILED L YLYLK NONE O OTHER ININSP/MAINT 1 WP19130GC427 9193 3562 BRUSHES FAILED PREMATURELY. DAMAGED COMUTATOR. 1G72 3U3 UNCR0001RD E00054EN 20040429000502004042900050SW 2004 4 29 ALGA093730 120040311A6210206015001115 BLADE BELL 206 206L1 1182107SW ALLSN 250C 250C30 03013GL MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03272M 2063 45365 TRAILING EDGE EXTRUSION HAS AREA APPROX. 5. 1G71 3U3 U H2SW E1GL 20040429000512004042900051SW 2004 4 29 ALGA093731 120040311A6210206010200133 BLADE BELL 206 206B3 1181506SW ALLSN 250C 250C* GL MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03116AL2922 2389 MAIN ROTOR BLADE TRAILING EDGE EXTRUSION EXFOLIATED AT STA. 179.0. DAMAGE IS CONSIDERED A MATERIAL DEFECT. 1G71 3U3 U H2SW E4CE 20040429000522004042900052SW 2004 4 29 ALGA093732 120040311A6210206015001115 BLADE BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL MAIN ROTOR CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03175AL2239 52117 MAIN ROTOR BLADE TRAILING EDGE EXTRUSION EXFOLIATED AT STA. 98 AND 130. DAMAGE IS CONSIDERED A MATERIAL DEFECT. 1G71 3U3 UNCH2SW E1GL 20040429000602004042900060EU 2004 4 29 BAQA093300 120040224A243523081043 STARTER GEN BOLKMSBK117 BK117C1 5626025EU ENGINE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY697 7544 WOULD NOT START ENGINE. REPLACED WITH SERVICEABLE UNIT. 03/10/2004 1G72 3U NCH13EU 20040429000612004042900061EU 2004 4 29 BAQA093656 120040201A7714430106202 PICKUP UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE ENGINE INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME28 0009 NO GAGE INDICATION. REPLACED WITH SERVICABLE ASSET UNIT. 03/10/2004 1G72 3U3 UO H88EU E42NE 20040429000622004042900062 2004 4 29 BAQA092512 420040204A3420109290 GYRO BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE COCKPIT NOISY E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP 7508 UNIT MAKING NOISE WHEN INSTALLED ON AIRCRAFT. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1G72 3U3 UNCH13EU E19EU 20040429000642004042900064 2004 4 29 BAQA093733 420040202A3420109290 GYRO BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP3236 7508 UNIT MAKING NOISE WHEN INSTALLED ON AIRCRAFT. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1G72 3U3 UNCH13EU E19EU 20040429000652004042900065EU 2004 4 29 BAQA093735 120040316A672041800876800 ACTUATOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH474 0273 ACTUATOR FAILED, NO REFERENCE VOLTAGE FOR ACT. POSITION. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/17/2004 1G72 3U3 U H88EU E19EU 20040429000662004042900066 2004 4 29 BAQA093736 420040304A22117008138903 COMPUTER BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE AUTOPILOT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME474 7243 AUTOPILOT FAILS SELF-TEST. CODE 1E17. REPLACED WITH SERVICABLE ASSET UNIT. 03/12/2004 1G72 3U3 U H13EU E5NE 20040429000692004042900069EU 2004 4 29 BAQA093188 120040220A672011731822 BEARING BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE PITCH LINK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 BEARINGS PREMATURELY WORN. REPLACED WITH SERVICABLE PITCH LINKS. 03/12/2004 1G72 3U3 U H13EU E5NE 20040429000722004042900072EU 2004 4 29 BAQA093339 120040310A7714L771M40C1010 INDICATOR UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE TRIPLE RPM INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135WJ77 0287 BOTH N2 NEEDLES INOPERATIVE ON TRIPLE RPM INDICATOR. REPLACED WITH SERVICABLE UNIT. 03/12/2004 1G72 3U3 U H88EU E42NE 20040429000752004042900075EU 2004 4 29 BAQA093759 120040324A6330L633M2010101 MOUNT UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE M/R GEARBOX LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03522ME2325 0144 LEAKING FLUID, AND RETRACTED ALL THE WAY INTO UNIT. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1G72 3U3 U H88EU E34NE 20040429000762004042900076EU 2004 4 29 BAQA093774 120040322A3150L315M5003101 WARNING SYSTEM UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT NOISY E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03533ME2608 132 EXCESSIVE ICS BACKGROUND NOISE, AND EXCESSIVELY LOUD WARNING TONES. REPLACED WITH SERVICABLE UNIT. 03/22/2004 1G72 3U3 U H88EU E34NE 20040429000772004042900077EU 2004 4 29 BAQA091987 120040303A6730L673M40A1001 ACTUATOR UROCOPEC135 EC135T1 5620026EU FENESTRON LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03135MH1967 0131 ACTUATOR SHAFT SEAL LEAKING. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/17/2004 1G72 3U H88EU 20040429000782004042900078 2004 4 29 BAQA093829 420040312A2210117884141 CONTROL UNIT BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE AUTOPILOT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG 7506 YAW CSAS MADE UNCOMMANDED YAW OSCILLATIONS IN NORMAL AND STANDBY MODE AT APPROX. TWO SECOND INTERVALS. UNIT WAS INSTALLED 02/16/2004 AT A/C TT 5145.8 AND WAS REMOVED 03/12/2004 AT A/C TT 5172.2 FOR A TOTAL OF 26.4 HOURS. LAST REPAIR REF RO 9-090006-18 MMIR CLAIM NR 91640 (ALSO A WARRANTY REPAIR FOR UNIT FAILING OUT OF BOX). THIS WILL BE THE THIRD REPAIR ON THIS UNIT IN 8 MONTHS. 1G72 3U3 UNCH13EU E19EU 20040429000812004042900081EU 2004 4 29 BAQA093892 120040309A2140JBS8803 EJECTOR UROCOPEC135 EC135T1 5620026EU HEATER INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH392 0131 EJECTOR INOPERATIVE, WON'T BLOW HEAT. REPLACED WITH SERVICABLE UNIT. 03/22/2004 1G72 3U H88EU 20040429000832004042900083EU 2004 4 29 BAQA092349 120040319A6330L633M2010104A004MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03522ME2325 0144 UNIT LEAKING FLUID AND PLUNGER RETRACTED. ABOVE P.O. IS MEANT FOR A/C S/N 0132, BUT ONE WAS CANNED OFF OF A/C S/N 0144. PERMISSION GIVEN TO RETURN THIS UNIT. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1G72 3U H88EU 20040429000862004042900086 2004 4 29 BAQA093925 420040322A3120B1794127000A CLOCK BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE COCKPIT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME1890 7243 UNIT WILL NOT RUN AND WILL NOT KEEP CORRECT TIME. P.O NR 202198408 WAS CUT FOR A/C S/N 7235, BUT ENDED UP BEING USED ON A/C S/N 7243. OK TO RETURN ON RMA NR R045364. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1G72 3U3 U H13EU E5NE 20040429000872004042900087 2004 4 29 BAQA093939 420040318A3120621396231 COMPASS UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE COCKPIT BROKEN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH474 0273 WARRANTY. ADUSTMENT SCREW ON UNIT IS BROKEN. REPLACED WITH SERVICABLE UNIT. 03/25/2004 1G72 3U3 U H88EU E19EU 20040426001822004042600182NM 2004 4 26 2004UALA00340 120040413A5320 SILL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 DOOR 1R LOWER SILL CORRODED ATTACH ANGLE CORRODED STA 375-377, RBL 61. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040426001922004042600192SO 2004 4 26 C2XA04SH183 120040327A532014521725613 SILL EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AT FRAME 19 TO FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426001932004042600193SO 2004 4 26 C2XA04SH186 120040327A532014521725613 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE RIGHT HAND SILL FORWARD OF THE SERVICE DOOR WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION FROM THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 AND EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426001962004042600196SO 2004 4 26 C2XA04SH185 120040327A531013500469401 CROSSBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715509 145238 SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 22 BETWEEN THE RIGHT SILL AND THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040426002042004042600204NM 2004 4 26 2004UALA00351 120040413A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 GOUGE IN STRINGER 23R AT STA 727D+6. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040426002122004042600212SO 2004 4 26 C2XA04SH187 120040327A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 2 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE NR 2 ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040426002132004042600213SO 2004 4 26 C2XA04TY059 120040328A5315 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716559 145603 TYS DURING A SCHEDULED 1C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED AT FR 20. MAINT CUT OUT THE EFFECTED AREA, FAB DRILLED AND COUNTERSUNK A NEW REPAIR PART, ALODINED, PRIMED, PAINTED AND INSTALL THE NEW PART IAW EMB 135/145 SRM 53-21-10; 51-20-03-06 AND CPM 51-21-04; 05; 06, SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040427000092004042700009CE 2004 4 27 S1F2004F00001 120040211A24979536001215 BUSS BAR BEECH 58 58 1152740CE CONT O550 IO550* SO W23 MISMANUFACTURED B S1FRO OTHER O OTHER NRNOT REPORTED 1 SO3387RG 679 TH1886 BUSS BAR ON EXTERNAL SUPPLY NEGETIVE POST HAD NO GROUND. BUS BAR HAD MASKING TAPE ON IT WHEN FACTORY HAD PAINTED IT AND INSTALLED WITHOUT REMOVING TAPE. THEREFORE NO GROUND FOR EXTERNAL SUPPLY. 1L72 3O3 O 3A16 E3SO 20040427000272004042700027 2004 4 27 USA2004F00006 420040224A2565D30654122 SLIDE BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE PAX DOOR DEFLATED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19619AU326648923 27198 DURING THE OPERATIONAL CHECK OF THE RIGHT FRONT PASSENGER DOOR SLIDE, THE SLIDE DEPLOYED BUT DID NOT HOLD PRESSURE. THE LOWER SUPPORT CHAMBERS DID NOT RECEIVE ENOUGH PRESSURE, AND THE ENTIRE SLIDE HAD LOST MOST OF ITS PRESSURE WITHIN FIVE MINUTES OF BEING DEPLOYED. MAINTENANCE REPLACED THE SLIDE. OK FOR SERVICE. 2L72 4F4 FRTA2NM A12EU 20040427000312004042700031EA 2004 4 27 A6WA200440028 120040310A3230 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT MLG TRUNNION LOOSE A O OTHER O OTHER NRNOT REPORTED 1 GL31424AW 7656 LT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED AND REPLACED LEFT MLG AFT TRUNNION BUSHING USING FIRST OVERSIZE BUSHING P/N 601R-5721003-21 IAW CRJ SB 601R-32-054 REV B PART B STEP 3A-3E. (M) 2L72 4F4 FRTA21EA E15NE 20040427000512004042700051EU 2004 4 27 BAQA094041 120040323A26970301037070 WIRE HARNESS AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE FIRE DETECTOR DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 1040 6425 12104 WIRE HARNESS HAS DAMAGED SOLDER JOINTS ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/02/2004 1G72 3U3 U H10EU E19EU 20040427000622004042700062NE 2004 4 27 BAQA094196 220040406A7314D240845 PUMP UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE FUEL SYSTEM INTERMITTENT B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601FH698 0069 FUEL PUMP HAS INTERMITTENT OPERATION, POPPING CIRCUIT BREAKER. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/19/2004 1G72 3U3 UO H88EU E42NE 20040427000642004042700064SW 2004 4 27 HEEA094228 120040412A6320222342480101 BEARING BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE ROTOR BRAKE FAILED E HEEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW0359806 28140 TRANSMISSION CHIP LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AT POINT SU FUR. MAINTENANCE FOUND BEARINGS IN THE ROTOR BRAKE QUILL HAD FAILED. 2G72 4U4 U H10SW E8NE 20040427000772004042700077NE 2004 4 27 BAQA094242 220040213A7530430110212 MODULATOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101* NE AIR FLOW FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911WS 7068 AIRFLOW MODULATOR FAILED OUT OF BOX, WILL NOT OPEN COMPLETELY. LAST REPAIR 8-080113-84, TSO 0.0 HOURS. 1G72 3U3 U H13EU E5NE 20040427000912004042700091NM 2004 4 27 DL738040278 120040329A5210 DOOR BOEING737 737832 13844CFNM L1 UNSECURE A DALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO27388DA 30375 L(1) DOOR DID NOT SEAL ON CLIMB-OUT PREVENTING AIRCRAFT FROM PRESSURIZING. FOUND DOOR NOT SHUT PROPERLY. INSPECTED DOOR AND OPS CHECKS GOOD. 2L72 4F RTA16WE 20040427000962004042700096NM 2004 4 27 DL73S040283 120040330A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 CORROSION ON AFT SIDE OF FORMER STA 827 O/B OF STR 27R. INSTALLED PERMANENT REPAIR PER SRM 53-10-4 FIG 6. COMPLETED AND SENT SSI DATA RETRIEVAL. 2L72 4F RTA16WE 20040427001012004042700101NM 2004 4 27 DL73S040288 120040401A5330654577246 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S4R LAP JOINT FROM BS 727 - 908. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 088676-14. 2L72 4F A16WE 20040427001132004042700113 2004 4 27 DL75K040300 420040403A344220412170403 TRANSCEIVER BOEING757 757232 1384965NM RADAR UNIT BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27645DL 24216 FAINT ELECTRICAL ODOR IN COCKPIT AFTER ENGINES SHUT DOWN. ISOLATED TO BAD WX RADAR R/T WHICH FAILED ON TAXI IN. DEACT R/T BY PULLING C/BS AND DISPATCHED WITH RADAR INOP PER MEL 34-43-01A. REPLACED R/T UNIT. 2L72 4F RTA2NM 20040427001152004042700115NM 2004 4 27 DL73S040303 120040405A5330654580026 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 SCRIBE MARKS WERE NOTED AT S14L BETWEEN BS 259.5 AND 303.9. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089014-14. 2L72 4F A16WE 20040427001282004042700128NM 2004 4 27 DL757040317 120040405A5330146N64103 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27630DL 22920 THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN STRINGERS 18L & 19L, JUST FWD OF THE FS 1618 SKIN BUTT SPLICE. THE DENTED AREA WAS REMOVED WITH A CUT OUT AND REPAIRED WITH TWO ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 089586-14, REV A. 2L72 4F RTA2NM 20040427001292004042700129NM 2004 4 27 DL73S040318 120040407A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 INSPECTION OF THE STRINGER 14L SKIN LAP JOINT PER AD 2003- 08-15, REVEALED A CRACKED FASTENER HOLE AT FS 500A+10 & ANOTHER AT FS 500B+15. THE CRACKS WERE REMOVED WITH SKIN CUTOUTS (1 X 4 & 1 X 7 INCH RESPECTIVELY). THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER BAC 737 SRM 53-30-3 FIG 42 AND DOCUMENTED PER ER/A 089542-14. 2L72 4F RTA16WE 20040428000052004042800005NM 2004 4 28 DL73S040320 120040407A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15, REVEALED A TOTAL OF 9 CRACKED FASTENER HOLES AT THREE LOCATIONS IN THE JOINT. THE CRACKS WERE REMOVED WITH CUTOUTS OF 15.5 X 1 INCH AND TWO CUTOUTS OF 7.25 X 1 INCH. THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER BAC 737 SRM 53-30-3, FIG 42 AND DOCUMENTED PER ER/A 089522-14AD. 2L72 4F RTA16WE 20040428000062004042800006NM 2004 4 28 DL757040321 120040408A3350 WIRE HARNESS BOEING757 757232 1384965NM EMERGENCY LIGHT DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27692DL 29724 ON INSPECTION FOUND SEAT TRACK LIGHTS OUT. REPLACED LIGHT ASSY HARNESSES. 2L72 4F RTA2NM 20040428000152004042800015NM 2004 4 28 ASAA0440002 120040114A3397 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01754AS 25095 ONT - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIV AT ROW 16. RESECURED AND CONNECTED FLOOR TRACK WIRING. OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040428000182004042800018NM 2004 4 28 ASAA0480161 120040306A33500105606 MODULE DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS 53471 PHX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE IN FIRST CLASS CABIN. RECONNECTED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040428000202004042800020NM 2004 4 28 ASAA0440001 120040112A33508100022607 LIGHT BOEING737 737490 1384715NM ROW 3-7 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 LAS - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROWS 3-7. RESECURED AND CONNECTED FLOOR TRACK WIRING. OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040428000222004042800022WP 2004 4 28 GTIA040169 120040219A5320 INTERCOSTAL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND CABIN STATION 807-826 STRINGER 1 INTERCOSTAL CORRODED. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2L72 4F A6WE 20040428000252004042800025WP 2004 4 28 GTIA040171 120040216A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND LEFT CABIN INBOARD SEAT TRACK CORRODED AND WORN STATION 200-1307. REMOVED CORROSON LEFT CABIN INBOARD SEAT TRACK STATION 200-1307. REMOVED SEAT TRACK STATION 200 TO SPLICE STATION 260. LOCATED AND DRILLED NEW SEAT TRACK STATION 200 TO SPLICE STATION 260. INSTALLED SEAT TRACK STATION 200 TO SPLICE STATION 260. (M) 2L72 4F A6WE 20040428000262004042800026WP 2004 4 28 GTIA040172 120040221A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND MAIN CABIN FLOORBOARD FS 200-256 LEFT INBOARD CENTER HAS MISSING AND DAMAGED INSERTS AND DAMAGED ON END. FABRICATED NEW CABIN FLOORBOARD STATION 200-256. (M) 2L72 4F A6WE 20040428000362004042800036EU 2004 4 28 BAQA094225 120040413A671041800847100 ACTUATOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE OUTPUT SHAFT WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03554ME2473 0154 EXCHANGE. OUTPUT SHAFT HAS EXCESSIVE SIDE PLAY. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/22/2004 1G72 3U3 U H88EU E34NE 20040428000462004042800046NM 2004 4 28 DLM88040371 120040426A33508039001 BATTERY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27901DL 49532 SEAT TRACK EMERGENCY LIGHTS FROM ROW 1 TO ROW 14 INOP. ALONG WITH FLIGHT DECK EMERGENCY LIGHT. REPLACED BATTERY PWR SUPPLY AND BATTERY FOR SEAT EMERGENCY LIGHTS LOC AT STA 386. REPLACED BATTERY PWR SUPPLY AND BATTERIES AT STA 211. 2L72 4F RTA6WE 20040428000472004042800047NM 2004 4 28 DL73S040372 120040423A531265465682 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304DL 23076 INSPECTION OF THE AFT P-DOME WEB PER AD 99-08-23 REVEALED CRACKS IN THE WEB COMMON TO THE BULKHEAD Y-CHORD NEAR STRINGER 5R. THE CRACKED AREA OF WEB WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 089561-14AD. 2L72 4F RTA16WE 20040428000492004042800049NE 2004 4 28 DL764040374 220040426A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 2 SHUTDOWN A DALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 SO27831MH10630 29702 706164 AT 2000 FEET RIGHT ENG ROLLED BACK HAD HIGH FUEL FLOW AND HIGH VIBS ENG NOT RESPONDING TO THROTTLE INPUTS. AFTER LANDING ENG SHUTDOWN DUE HIGH VIBS. METAL FOUND IN TAILPIPE. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20040428000502004042800050NM 2004 4 28 DL73S040375 120040427A5330654577892 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10R LAP JOINT BETWEEN BS 908 AND 960. DAMAGE WAS REMOVED AND THE AREA REPAIRED PER ERA 089670-14. 2L72 4F A16WE 20040428000512004042800051NM 2004 4 28 SWAA041071 120040415A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428000522004042800052NM 2004 4 28 SWAA041072 120040415A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND R2 DOOR UPPER HINGE CUTOUT REPAIR DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER SRM. 2L72 4F RTA16WE 20040428000532004042800053NM 2004 4 28 SWAA041073 120040415A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29327SW 23691 DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040428000552004042800055 2004 4 28 SWAA041075 420040415A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1/R1 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040428000592004042800059NM 2004 4 28 SWAA041087 120040416A53126546568 BULKHEAD BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB AT BS 1016, FROM STRINGER 6R TO STRINGER 6L, STRINGER 23R, CRACKED. REPAIRED WEB PER ER. 2L72 4F RTA16WE 20040428000612004042800061NM 2004 4 28 SWAA041089 120040416A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND BUTT STRAP AT BS 908, STRINGER 4R, CRACKED. REPAIRED STRAP PER SRM. 2L72 4F RTA16WE 20040428000632004042800063NM 2004 4 28 SWAA041091 120040417A531165C25229 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT BS 727D, STRINGER 26R AND STRINGER 27R, CORRODED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040428000652004042800065NM 2004 4 28 SWAA041093 120040418A3350100885 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29778SW 27883 DURING SCHEDULED MV1 CHECK, FOUND EEPLS AT ROWS 1 TO 4, INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2L72 4F RTA16WE 20040428000672004042800067NM 2004 4 28 SWAA041055 120040414A335057771 CAP BOEING737 7372T4 1384492NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS MISSING END CAP. INSTALLED END CAP PER MM. 2L72 4F A16WE 20040428000692004042800069 2004 4 28 SWAA041057 420040414A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2/R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C3 CHECK, FOUND BOTH L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F A16WE 20040428000712004042800071NM 2004 4 28 SWAA041059 120040414A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 395, BETWEEN STRINGER 15L AND STRINGER 16L, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040428000732004042800073NM 2004 4 28 SWAA041061 120040414A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 663, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040428000752004042800075NM 2004 4 28 SWAA041063 120040414A5321 FLOOR PANEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND MANUAL GEAR EXTENSION ACCESS DOOR AND FLOOR STRUCTURE AT BS 243 TO BS 253, RBL 6 TO RBL 12, CORRODED. REPAIRED FLOOR STRUCTURE PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040428000772004042800077NM 2004 4 28 SWAA041065 120040414A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT BS 867, STRINGER 26 R, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040428000792004042800079NM 2004 4 28 SWAA041068 120040415A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 EEPLS COVER LOOSE AT OVERWING EXIT ROW. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040428001332004042800133NM 2004 4 28 SWAA041113 120040419A531265C35740 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING WEB AT LT AND RT BRAKE PAD AFT MOUNTS, CRACKED. REPAIRED NLG W/W CEILING WEB PER EA. 2L72 4F RTA16WE 20040428001352004042800135NM 2004 4 28 SWAA041115 120040419A3350D71701100 BATTERY BOEING737 7377H4 1384404NM R2 DOOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040428001372004042800137NM 2004 4 28 SWAA041116 120040420A3260806007 CIRCUIT CARD BOEING737 7373Y0 1384671NM E/E BAY FAILED A SWAAO OTHER N FALSE WARNING CLCLIMB 1 SW29682SW 23496 AFTER TAKEOFF AND MOVING GEAR LEVER TO OFF POSITION BOTH RED AND RT MLG LIGHT ILLUMINATED. MOVED GEAR LEVER TO UP THEN OFF, LIGHTS EXTINGUISHED. REMOVED AND REPLACED RT MLG DOWNLOCK LOGIC CARD, ADJUSTED UPLOCK SENSOR, PER MM. 2L72 4F RTA16WE 20040428001392004042800139NM 2004 4 28 SWAA041118 120040420A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29326SW 23690 FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED OUTBOARD FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040428001922004042800192SO 2004 4 28 C2XA04IA038 120040326A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2711535 145518 DURING CLIMB THROUGH 15,000 FT, THE CREW REPORTED THE ODOR OF SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. ENGINE RUNS WERE PERFORMED OPERATING THE PRESSURIZATION, AIR CONDITIONING, AND BLEED SYSTEMS AND THE ODOR COULD NOT BE DUPLICATED. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY WITH NO ODOR OF SMOKE IN THE CABIN OR FLIGHT DECK. 2L72 4T RTT00011AT 20040428001932004042800193NM 2004 4 28 AT0400010 120040418A33506011779 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15936AT 55058 OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY SUPPLY REF 717 AMM 33-51-06, OPS CHECK GOOD (IN AFT CARGO COMPARTMENT). 2L72 4F TRA6WE 20040428001952004042800195NM 2004 4 28 2004UALA00356 120040414A5312 BULKHEAD BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 DAMAGE TO AFT PRESS BULKHEAD & SKINS STA 1620-1787 STR 19-25L. MAJOR REPAIR ACCOMPLISHED. STA 1720 BREAK RING REPLACED FROM WL 191 TO BL 0 STA 1720 BULKHEAD 2 INCH DENT REPAIRED. SKINS REPLACED STA 1620-1720 STR 19-25L. STRINGERS AND ASSOC FITTINGS REPLACED STA 1720-1787 STR 19-25L. 2L72 4F4 FRTA2NM E17NE 20040428001962004042800196NE 2004 4 28 2004UALA00357 220040414A7200 ENGINE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 VIBRATION A UALAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP29648UA 25285 REPORTS OF VIBRATION NR 2 ENGINE. DUE TO REPORTS OF ENGINE VIBRATION THE ENGINE WAS BOROSCOPED, CHIP DETECTORS INSPECTED AND INLET AND EXHAUST CHECKED. NO DEFECTS NOTED. THE ENGINE THEN HAD A TRIM BALANCE AND RETURNED TO SERVICE. 2L72 4F4 FRTA1NM E24NE 20040428001972004042800197NM 2004 4 28 2004UALA00359 120040413A5311 FRAME AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29842UA 1569 DENT FOUND BETWEEN FR1 & FR2 JUST FWD OF FWD E&E DOOR. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA28NM E40NE 20040526000352004052600035NM 2004 5 26 SWAA041368 120040513A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND PHOTOLUMINESCENT STRIP BETWEEN BS 336 AND BS 948, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER ACO. 2L72 4F RTA16WE 20040429000012004042900001EU 2004 4 29 BAQA092614 120040126A291011745020 MODULE BOLKMSBK117 BK117C1 5626025EU HYDRAULIC INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP111 7508 REASON FOR REMOVAL FAILED HYSTERESIS CHECK SUSPECTED AUTO PILOT PROBLEM. THE PROBLEM WAS WHEN THIS AIRCRAFT WAS DELIVERED THE HYD PACK HAD ANOTHER MFG SERVO ON IT. AND THE AUTO PILOT SYSTEM NEVER WORKED. SO FINALLY WE GOT THE RIGHT HYD PACK WITH THE FWM SERVO'S ON IT. WE ARE ASKING FOR WARRANTY ON THE ONE THAT WAS REMOVED AND THE NEW ONE THAT WAS INSTALLED. HARD CARDS ARE ENCLOSED. 1G72 3U NCH13EU 20040429000432004042900043NE 2004 4 29 ALGA093898 120040323A6320SB2559101 BEARING SKRSKYS76 S76A 8143006NE M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBCT536 760109 MAIN GEARBOX DISASSEMBLED FOR METAL CONTAMINATION, FOUND BEARING BREAKING DOWN. 1G72 3U H1NE 20040429000452004042900045NE 2004 4 29 BAQA093911 220040310A7530430110212 MODULATOR BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE AIR FLOW INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LG 7032 LE45239 UNIT REMOVED FOR OVERHAUL. PART WAS INSTALLED ON ENG S/N LE45239, BUT ENGINE WAS ORIGINALLY INSTALLED ON A/C S/N 7068. INSTALLED ON 5/4/99 AT ENG TT 3407.8 AND REMOVED ON 08/24/200 AT 4181.0, THEN REINSTALLED ON 08/24/2000 AT 4182.0, AND REMOVED CURRENTLY ON 03/10/2004 AT 5808.0. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1G72 3U3 U H13EU E5NE 20040429000532004042900053SW 2004 4 29 ALGA093891 120040322A6510407340339107 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL T/R DRIVE DAMAGED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL253 53240 FOUND GREASE DISCOLORATION ON NR 2 BEARING HBVM LIGHT. 1G71 3U3 UO H2SW E1GL 20040429000552004042900055EU 2004 4 29 BAQA093653 120040119A7714430106202 PICKUP UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE E BAQAO OTHER O OTHER APAPPROACH 1 EA03603ME91 0284 WILL NOT READ NRO. REPLACED WITH SERVICABLE ASSET UNIT. 03/08/2004 1G72 3U3 U H88EU E42NE 20040429000582004042900058EU 2004 4 29 BAQA093660 120040308A249745023502 MASTER SWITCH UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE MAIN FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF368 0281 FAILED SEVERAL TIMES ON AIRCRAFT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/09/2004 1G72 3U3 U H88EU E34NE 20040429000682004042900068EU 2004 4 29 BAQA093742 120040229A771454487099111 INDICATOR BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE N1 RPM INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY711 7544 DIGITS UNREADABLE AT NIGHT. REPLACED WITH SERVICABLE ASSET UNIT. 03/12/2004 1G72 3U3 UNCH13EU E19EU 20040429000732004042900073EU 2004 4 29 BAQA093755 120040317A2140JBS8803 MIXING VALVE UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE HEATER INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME2352 0144 THIS UNIT'S MOTOR RUNS CONSTANTLY. REPLACED WITH SERVICABLE UNIT. 03/29/2004 1G72 3U3 U H88EU E34NE 20040429000892004042900089EU 2004 4 29 BAQA093947 120040312A5610L563M28X2001 WINDOW UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE COCKPIT CRACKED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH473 0273 WINDOW CRACKED NEAR HANDLE. REPLACED WITH SERVICEABLE UNIT. 03/25/2004 1G72 3U3 U H88EU E19EU 20040429000902004042900090EU 2004 4 29 BAQA093950 120040312A3340117897341 LAMP BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE STROBE SHORTED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY735 7544 STROBE LAMP ASSY HAS AN INTERNAL SHORT, WILL NOT FLASH. REPALCED WITH SERVICABLE UNIT 03/26/2004 1G72 3U3 UNCH13EU E19EU 20040429000922004042900092EU 2004 4 29 BAQA093658 120040210A6330L633M2010103 MOUNT UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE GEARBOX LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03137MH933 0179 WARRANTY. FLAT ON STOP, LEAKED GLYCOL. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1G72 3U3 UO H88EU E42NE 20040429000942004042900094 2004 4 29 BAQA093968 420040326A3444066304401 INDICATOR UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE COCKPIT BURNED OUT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135ME 0009 INSTRUMENT LIGHTING IS BURNED OUT. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 UO H88EU E42NE 20040429001042004042900104NM 2004 4 29 AALA20040486 120040424A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21634AA 24592 SFO - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 8DEF BROKEN. REPLACED LIGHT SOCKET FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 8DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040430000012004043000001WP 2004 4 30 ASMF200403009 120040315A2752 WARNING HORN DOUG DC9 DC987 3022087WP COCKPIT ACTIVATED W ASMFD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML 49726 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF TAKEOFF ALARM ACTIVATED. TECHNICAL PERSONNEL PERFORMED TESTS TO THE PROXIMITY SWITCH STALL COMPUTER AND STATUS TEST PANEL, BEING ALL CORRECT. DURING OVERNIGHT SERVICE AT MEX WIRING WAS REPAIRED ON S30-111 LEAD (PIN 29X) IN ACCORDANCE WITH MM 27-52-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000022004043000002NM 2004 4 30 ASMF200403020 120040331A2410696233B CSD DOUG MD80 MD83 3023681NM ENGINE FAILED W ASMFH DEACTIVATE SYST/CIRCUITS MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW23831LF47177327 53050 CAPTAIN REPORTED HIGH TEMPERATURE ON CSD DURING CLIMB, SO IT WAS DEACTIVATED. DURING TRANSIT CHECK AT MEX, THE CHIP DETECTOR WAS CKECKED AND CSD WAS DRAINED AND SERVICED IAW MM 12-12-02, TEST CORRECT. DURING OVERNIGHT SERVICE, THE RIGHT CSD AND HEAT EXCHANGER WERE REPLACED IAW MM 24-20-01 AND 24-10-03 RESPECTIVELY, TEST CORRECT. 2L72 4F RT 20040430000032004043000003NM 2004 4 30 ASMF200404011 120040414A3260 SWITCH DOUG MD88 MD88 3023688NM MLG MALFUNCTIONED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23158PL 49761 DURING TRANSIT CHECK AT MEX, THE LANDING GEAR ALARM WAS ACTIVATED AND IT WAS NOT POSSIBLE TO TURNED OFF. TECHNICAL PERSONNEL REPLACED THE SWITCH S1-92 AND TESTED THE SYSTEM ACCORDANCE WITH MM 32-60-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000042004043000004NM 2004 4 30 ASMF20040404 120040405A2130825011 CHECK VALVE DOUG MD88 MD88 3023688NM AIR CONDITIONINGLEAKING W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23160PL102912869 49763 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION FAILS. CAPTAIN REPORTED THAT LEFT AIR CONDITIONING PACKAGE WAS INOPERATIVE AND RIGHT AIR CONDITIONING PACKAGE WITH A FEW FLOW. AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIGHT SERVICE BOTH PACKAGES WERE CHECKED BY LEAKS IAW MM 36-00-00 AND A LEAK WAS DETECTED IN GROUND PNEUMATIC VALVE. GROUND PNEUMATIC VALVE WAS REPLACED IAW MM 21-32-00, TEST CORRECT. 2L72 4F RTA6WE 20040430000052004043000005WP 2004 4 30 ASMF200403003 120040307A3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP MLG FAILED W ASMFO OTHER N FALSE WARNING TOTAKEOFF 1 SW23491SH 49150 DURING TRANSIT CHECK THE RIGHT AIR CONDITIONING TEMPERATURE CONTROL WAS OUT OF SERVICE. ADDITIONALLY, DURING TAKEOFF THE NOSE LANDING GEAR RED LIGHT WAS NOT TURNED OFF. THE PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) WAS TESTED AND FAIL CODES 510 AND 580 APPEARED. THE PSEU WAS REPLACED AND TEST CORRECT IAW MM 32-60-00. 2L72 4F A6WE 20040430000062004043000006WP 2004 4 30 ASMF200403004 120040309A3110 CONTROL PANEL DOUG DC9 DC987 3022087WP COCKPIT FAILED W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SW23216AM 49586 AIRCRAFT RETURNED OF FLIGHT DUE TO ESDP RIGHT PANEL WAS OUT OF SERVICE AND WITHOUT INFORMATION. TEST PANEL WAS PERFORMED BUT FAIL CONTINUED. T34 CIRCUIT BREAKER WAS RESET, CORRECTING THE POWER SUPPLY TO THE RIGHT SIDE. CONNECTORS WERE CLEANED, ALL CORRECT. DURING TRANSIT CHECK AT MEX, THE 91970 CIRCUIT BREAKER WAS REPLACED AND TESTS WERE PERFORMED IN ACCORDANCE WITH MM 31-61-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000072004043000007WP 2004 4 30 ASMF200403007 120040314A3260833605 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP NLG FAILED W ASMFO OTHER N FALSE WARNING CRCRUISE 1 SW23501AM411367921 49188 CAPTAIN REPORTED THAT DURING FLIGHT NOSE LANDING GEAR RED LIGHT TURNED ON OCCASIONALLY. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE PROXIMITY SENSOR D1-32 AND PROXIMITY UNIT WERE REPLACED IN ACCORDANCE WITH MM 32-60-04 PAGE 201 AND 32-60-01, TEST CORRECT. 2L72 4F A6WE 20040430000082004043000008WP 2004 4 30 ASMF200403011 120040320A7931 PRESSURE SWITCH DOUG DC9 DC983 3022083WP LT ENG OIL MALFUNCTIONED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23583MD 49659 DURING TRANSIT CHECK THE LEFT OIL LOW PRESSURE LIGHT TURNED ON. THE SWITCH WAS DEFERRED IAW MEL 79-2. DURING OVERNIGHT SERVICE THE LOW PRESSURE SWITCH WAS REPLACED IAW MM 79-34-01, TEST CORRECT. 2L72 4F RTA6WE 20040430000112004043000011WP 2004 4 30 AALA20040496 120040427A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217528A 49920 DFW - EMERGENCY EXIT SIGN AT FORWARD GALLEY INOPERATIVE. REPLACED WIRE FROM FORWARD GALLEY TO SIDEWALL FOR EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000152004043000015SO 2004 4 30 C2XA04SH251 120040429A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712564 145618 SHV- DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040430000182004043000018WP 2004 4 30 ASMF200403005 120040312A3340 LIGHT DOUG DC9 DC987 3022087WP TAXI INOPERATIVE W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23204AM 49404 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF NOSE LANDING GEAR LIGHTS DID NOT TURN ON. NOSE LANDING GEAR TAXI LIGHTS WERE REPLACED IN ACCORDANCE WITH MM 33-41-01 WITHOUT ENGINES SHUTOFF. 2L72 4F RTA6WE 20040430000192004043000019WP 2004 4 30 ASMF200403012 120040321A7930 WARNING LIGHT DOUG DC9 DC982 3022082WP ENGINE OIL ILLUMINATED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF OIL STRAINER CLOGGING LIGHT TURNED ON. PRESSURE SWITCH AND STRAINER CLOGGING OIL SWITCH WERE CHECKED AND LEAK TEST WAS PERFORMED, ALL CORRECT. THE LEFT FILTER WAS REMOVED, CLEANED AND INSTALLED, TEST WAS CORRECT IAW MM 79-20-06. DURING OVERNIGHT SERVICE THE FILTER WAS REPLACED IAW MM 79-20-06, TEST CORRECT. 2L72 4F A6WE 20040430000212004043000021NM 2004 4 30 ASMF200404006 120040410A2410696233B CSD DOUG MD88 MD88 3023688NM LT GENERATOR FAILED W ASMFK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SW23158PL219449433 49761 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSHBACK THE LEFT CSD OIL PRESSURE LIGHT TURNED ON. CSD WAS DISCONNECTED AND DEFERRED IN ACCORDANCE WITH MEL 24-1-1. DURING OVERNIGHT CHECK, THE CSD AND THE OIL HEAT EXCHANGER WERE REPLACED IN ACCORDANCE WITH MM 24-10-01, TESTS CORRECT. 2L72 4F RTA6WE 20040430000222004043000022WP 2004 4 30 ASMF200404012 120040415A793042D1091A PRESSURE SWITCH DOUG DC9 DC982 3022082WP LT ENG OIL DAMAGED W ASMFDE RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 SW23501AM14231226 49188 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF L OIL STRAINER CLOGGING LIGHT TURNED ON. THE ABNORMAL PROCEDURE WAS PERFORMED AND LEFT ENGINE WAS SHUTDOWN. THE FILTER AND SWITCH PRESSURE FILTER WERE REPLACED IAW 72-61-54 AND TEST CORRECT IAW MM 79-35-01. 2L72 4F A6WE 20040430000232004043000023 2004 4 30 ASMF200404010 420040413A3432 CONNECTOR DOUG DC9 DC983 3022083WP LT VHF SYSTEM DAMAGED W ASMFO OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SW23838AM 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT THE LEFT VHF SYSTEM WAS OUT OF SERVICE. TECHNICAL PERSONNEL REPLACED RX VOR ILS AND CONTROL PANEL, BUT FAIL CONTINUED. WIRING WAS CHECKED DETECTING THE LINE 1RN11A22 OF THE CONNECTOR P10-407 (PIN H) DAMAGED. REPAIRED WIRING IN ACCORDANCE WITH WDM 34-32-01 AND TESTED IN ACCORDANCE WITH MM 34-32-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000242004043000024WP 2004 4 30 ASMF200403001 120040303A2121251301 COOLING FAN DOUG DC9 DC987 3022087WP CABIN DAMAGED W ASMFK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW23751RA 49779 DURING OVERNIGHT SERVICE THE FAN CIRCUIT BREAKER WAS OFF. FANS WERE REPLACED IN ACCORDANCE WITH MM 21-50-03 AND SMOKE ODOR WAS DETECTED ON PASSENGER CABIN. AIRCRAFT WAS VENTILED AND WATER SEPARATOR COVERS WERE REPLACED. AFTER, AIR CONDITIONING SYSTEM WAS WORKING CORRECT. 2L72 4F RTA6WE 20040430000252004043000025NM 2004 4 30 ASMF200403010 120040317A7920699151 STRAINER DOUG MD80 MD83 3023681NM LT ENG OIL CLOGGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS36878 49643 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF L OIL STRAINER CLOGGING LIGHT TURNED ON AFTER ENGINE START. MAIN OIL FILTER AND SWITCH OIL FILTER WERE REPLACED, IN ACCORDANCE WITH MM 79-20-00 AND 79-30-00, ALL CORRECT. 2L72 4F RT 20040430000262004043000026NM 2004 4 30 ASMF200403015 120040325A5730 PANEL DOUG MD80 MD83 3023681NM WING DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23831LF 53050 DURING TRANSIT CHECK THE FUEL PANEL WAS DETECTED WITH DAMAGE OF 2.5 INCHES AND LEADING EDGE WITH CRACK OF 1.5 INCH IN STATION XRS 220. THE FUEL PANEL WAS REPAIRED IAW SRM 52-01 AND RIGHT WING LEADING EDGE WAS REPAIRED IAW SRM 57-06. 2L72 4F RT 20040430000292004043000029NM 2004 4 30 ASMF200404007 120040412A27806010N000103 ACTUATOR DOUG MD88 MD88 3023688NM SLATS FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23160PL33496 49763 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXIING THE AUTO SLAT FAIL LIGHT TURNED ON. AT PLATFORM, THE TECHNICAL PERSONNEL PERFORMED A TEST TO THE SYSTEM GETTING THE SAME RESULTS WITH FAIL CODE IN BOTH COMPUTERS. AIRPLANE WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE BOTH AUTO SLAT ACTUATORS WERE REPLACED IN ACCORDANCE WITH MM 27-80-08. ADDITIONALLY S1-467 SWITCH AND ATTACK ANGLE WERE REPLACED IN ACCORDANCE WITH MM 27-80-07 AND 34-19-01, TESTS WERE PERFORMED IN ACCORDANCE WITH MM 27-80-08 AND 34-19-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000302004043000030NM 2004 4 30 ASMF200404008 120040412A2410696233B CSD DOUG MD88 MD88 3023688NM LT ENGINE FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23162PL5542915534 49765 DURING TRANSIT CHECK, CAPTAIN REPORTED LEFT CSD OIL PRESSURE LIGHT TURNED ON AND HIGH TEMPERATURE RESTRICTION. TECHNICAL PERSONNEL REPLACED THE LEFT CSD AND AIR/OIL HEAT EXCHANGER IN ACCORDANCE WITH MM 24-10-00, TESTS CORRECT IN ACCORDANCE WITH MM 24-10-03. 2L72 4F RTA6WE 20040430000312004043000031NM 2004 4 30 ASMF200404009 120040412A2910 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23168PL 53174 DURING TRANSIT CHECK HYDRAULIC FLUID LEAK WAS DETECTED IN A LINE LOCATED AT THE UPPER SECTION OF THE AFT CARGO DOOR. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE LEAK WAS DETECTED IN THE RIGHT HYDRAULIC PUMP RETURN LINE, IT WAS ADJUSTED IN ACCORDANCE WITH MM 29-00-00 PAGES 201 AND 208, TESTS CORRECT. 2L72 4F RTA6WE 20040430000322004043000032WP 2004 4 30 ASMF200403008 120040315A213121171801 CONTROLLER DOUG DC9 DC987 3022087WP CABIN PRESSURE MALFUNCTIONED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23214AM8259 49585 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB AT 33,000 FEET, AFT CARGO DOOR AND AFT STAIRWAY DOOR LIGHTS TURNED ON AND CABIN STARTED TO DEPRESSURIZE. CARGO COMPARTMENT DOORS WERE CHECKED, ALL CORRECT. AIRCRAFT WAS PRESSURIZED WITH A GROUND PNEUMATIC UNIT NO LEAK WAS FOUND. ENGINES PRESSURIZATION TESTS WAS PERFORMED, ALL CORRECT. AS A PREVENTIVE ACTION PRESSURIZATION CONTROLLER NR ONE WAS REPLACED. DURING OVERNIGHT SERVICE TESTS TO PRESSURIZATION SYSTEM WERE PERFORMED IN ACCORDANCE WITH MM 21-32-03, 52-31-00 AND 52-63-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000332004043000033NM 2004 4 30 ASMF200403017 120040329A3320 CONNECTOR DOUG MD88 MD88 3023688NM LAV LIGHT SHORTED W ASMFK NONE BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW23161PL 49764 DURING TRANSIT CHECK A BURNED ODOR WAS DETECTED IN AFT LEFT LAVATORY. ELECTRICAL CIRCUIT WAS CHECKED IAW WDM 33-23-12 AND THERE WERE DETECTED A TRANSFORMER T1-2 AND CONNECTOR R5-2403 WITH SHORT CIRCUIT. THE CONNECTOR AND TRANSFORMER WERE REPLACED IAW WDM 33-23-12, TESTS CORRECT. 2L72 4F RTA6WE 20040430000342004043000034NE 2004 4 30 ASMF200403016 220040325A732076960615 FCU DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFDE RETURN TO BLOCK ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW23945AS9026 9016 49643 725486 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE DID NOT ACCELERATE. PARAMETERS WERE CHECKED AND WERE NORMAL IAW MM 71-00-01. ENGINE WAS SHUTOFF AND PURGE VALVES WERE CHECKED IAW MM 75-31-01. RIGHT FUEL CONTROL UNIT WAS REPLACED IAW MM 73-20-01 AND ACCELERATION TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRT E9NE 20040430000372004043000037 2004 4 30 ASMF20040403 420040405A344220412140413 TRANSCEIVER DOUG DC9 DC982 3022082WP RADAR FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW231003Y9746 9736 48068 AIRCRAFT ARRIVED WITH FOLLOWING REPORTS: RADAR ANTENNA TURNED TO RIGHT. RADAR CONNECTOR WAS RESEATED AND CLEANED IAW MM 34-41-01. L ICE PROTECT TEMP HIGH LIGHT TURNED ON. LEAK WAS CORRECTED AND CLAMPS WERE TIGHTENED IAW MM 30-10-07. LEFT WINDSHIELD WIPER DOES NOT WIPE. LEFT WINDSHIELD WIPER WAS ADJUSTED IAW MM 30-42-03. HEAD PHONE AND SPEAKER COMES ALL THE TIME A MORSE CODE. AUDIO BOX CONNECTORS WERE CHECKED AND CLEANED IAW MM 23-40-00. DURING OVERNIGHT SERVICE THE ANTENNA AND RADAR TRANSCEIVER, ANTICIPATOR AND THERMOSTAT, AND AUDIO CONTROL BOX WERE REPLACED IAW MM 34-41-01, 34-41-04, 36-10-6, 36-10-7, AND 23-50-02 RESPECTIVELY. 2L72 4F A6WE 20040430000402004043000040EU 2004 4 30 AALA20040447 120040410A3397 WIRE AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2119059 469 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. FOUND EMERGENCY LIGHT DISCONNECTED UNDERNEATH SEAT. RECONNECTED EMERGENCY LIGHT UNDERNEATH SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040430000412004043000041WP 2004 4 30 AALA20040441 120040408A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21975TW 53625 TWO AFT EMERGENCY LIGHTS ON CEILING BETWEEN LEFT AND RIGHT HAND LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR TWO AFT EMERGENCY LIGHTS ON CEILING BETWEEN LEFT AND RIGHT HAND LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040430000422004043000042NM 2004 4 30 AALA20040448 120040410A3350BPS73 MODULE BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 ORD - EMERGENCY EXIT LIGHTS AT ROWS 31HJ TO 40HJ INOPERATIVE. REPLACED POWER MODULE M734 FOR EMERGENCY EXIT LIGHTS AT ROWS 31HT TO 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000442004043000044WP 2004 4 30 AALA20040444 120040409A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219619V 53566 RDU - EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040430000472004043000047NM 2004 4 30 ASMF200404014 120040421A213039613011 FLOW VALVE DOUG MD88 MD88 3023688NM CABIN PRESSURE FAILED W ASMFBA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23160PL9918 1472 49763 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO AS A CONSEQUENCE OF DURING FLIGHT AT 370 FT AIRCRAFT WAS DEPRESSURIZED AND DESCENDED AT 150 FT WITH CABIN ALTITUDE OF 11,000 FT AND ORAL ALARM. THE OXYGEN MASKS WAS NOT NECESSARY ACTIVATED DUE TO PRESSURE WAS STABLE. DURING OVERNIGHT SERVICE FLOW CONTROL VALVE WAS REPLACED IAW MM 21-31-00 AND BOTH SYSTEMS WERE CHECKED BY LEAKS IAW MM 21-00-00 TO 7.7 PSI, ALL CORRECT. 2L72 4F RTA6WE 20040430000492004043000049WP 2004 4 30 AALA20040454 120040322A49975D00862 TERMINAL DOUG DC9 DC983 3022083WP APU OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21563AA 49345 TUL - THREE WIRE RING TERMINALS SHOW SIGNS OF OVERHEATING AT RESISTER R4-9. REPLACED THREE EACH WIRE RING TERMINALS AT RESISTER R4-9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040430000502004043000050WP 2004 4 30 AALA20040453 120040326A4997 WIRE DOUG DC9 DC983 3022083WP APU OVERHEATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21563AA 49345 TUL - AUXILLARY POWER UNIT WIRE FEEDER CABLES, NUMBERS 3X2CAB, 3X2D2B, 3X1D2A AND 3X1C2A SHOWS SIGNS OF OVERHEATING. PLASTIC ADELON WIRE NUMBER 3X1C2A SHOWED SIGNS OF OVERHEATING. REPLACED AUXILLARY POWER UNIT WIRE FEEDER CABLES 3X2C2B, 3X2D2B, 3X1D2A, AND 3X1C2A AND ADEL CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040430000512004043000051NM 2004 4 30 AALA20040452 120040411A3350 COVER BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21399AN 29606 MIA - EMERGENCY EXIT LIGHT COVER MISSING MID GALLEY. FOUND ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000542004043000054WP 2004 4 30 AALA20040465 120040415A3411 PITOT LINE DOUG DC9 DC982 3022082WP AIRSPEED LEAKING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW217518A 49895 MIA - INFLIGHT T518 AT ROTATION AND LIFT OFF RUDDER RATIO LIGHT AND MACH INDICATOR LIGHT CAME ON. CAPTAIN AND FIRST OFFICER AIR SPEED NOT RELIABLE. CENTER GOOD. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. COMPLETED RUDDER RATIO TEST/ADJUSTMENT AND NO FAULTS FOUND ON RUDDER RATIO MODULES. FOUND LEAKING PITOT LINE. SECURED PITOT LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000562004043000056NE 2004 4 30 AALA20040464 220040415A7230 COMPRESSOR BOEING767 767223 1385123NM GE CF680 CF680A2 NE ZONE 600 STALLED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW21324AA 22325 580324 ORD - DURING CRUISE AT FL370 EXPERIENCED THREE COMPRESSOR STALLS. ALL ENGINE INDICATIONS REMAINED NORMAL, NO VARIATIONS. FLIGHT ATTENDANTS REPORTED SPARKS COMING OUT OF RIGHT HAND ENGINE. SPARKS CONTINUED INTERMITTANTLY DURING DECENT WHENEVER POWER WAS CHANGED. REPLACED RIGHT HAND ENGINE PER WORKCARDS 71-94-01 AND 71-95-18 AND ALL ATTACHMENTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20040430000572004043000057WP 2004 4 30 AALA20040439 120040407A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114551 53033 DEN - AFT ACCESSORY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-28 FOR AFT ACCESSORY OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000582004043000058WP 2004 4 30 AALA20040438 120040407A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114551 53033 DEN - AFT OVERHEAD EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-105 FOR AFT OVERHEAD EMERGENCY EXIT DOOR LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000612004043000061WP 2004 4 30 AALA20040481 120040421A3397 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217538A 49992 MIA - EMERGENCY ESCAPE PATH LIGHT AT 7D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000632004043000063NM 2004 4 30 VNAA0404001 120040401A3240AC69965 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PARKING BRAKE FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07431JS1084310760 3028 THE CREW REPORTED GETTING A EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040430000642004043000064NE 2004 4 30 VNAA0403018 220040331A73208111804004 ECU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LT ENGINE FAILED A VNAAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL07438JS18477 3056 WHILE ON APPROACH, THE LEFT HAND ENGINE TORQUE SURGED FROM 90 TO 10 PERCENT AND WAS UNCONTROLLABLE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND SHUT THE ENGINE DOWN. FLIGHT 2558 THEN LANDED AT PIT. MAINTENANCE INSPECTED AND REPLACED THE ENGINE CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040430000652004043000065 2004 4 30 VNAA0403017 420040328A3421 INDICATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ATTITUDE INOPERATIVE A VNAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07229PS 7898 AIRCRAFT N229PS HAD ITS STANDBY ATTITUDE INDICATOR MEL'D. THE DESTINATION CITY, PHL, WAS REPORTING FOG. THEREFORE, FLIGHT 2233 HAD TO DIVERTED TO PIT DUE TO WEATHER. 2L72 4F4 FRTA21EA E15NE 20040430000662004043000066WP 2004 4 30 AALA20040455 120040413A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 EMERGENCY OVERHEAD LIGHT AT ROW 29D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY OVERHEAD LIGHT AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000672004043000067NM 2004 4 30 AALA20040456 120040413A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21624AA 24582 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040430000682004043000068WP 2004 4 30 AALA20040457 120040413A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170401 49312 DFW - CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK AT B5-100 FOR CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000702004043000070EU 2004 4 30 AALA20040491 120040422A5730 SKIN AIRBUS300 A300B4605R 3930308EU RT WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW217082A 643 TUL - TWO INCH BY FOUR INCH AREA OF CORROSION ON RIGHT HAND LOWER WING SKIN UPPER SURFACE AT NUMBER 10 SLAT TRACK OPENING. CORROSION HAS A DEPTH OF 50 PLUS PERCENT. REPAIRED NUMBER 10 SLAT TRACK OPENING LOWER WING SKIN PER ESO 40-572000-3322 DATED 4/21/2004. 2L72 4F RTA35EU 20040430000712004043000071EU 2004 4 30 AALA20040492 120040422A5730 SKIN AIRBUS300 A300B4605R 3930308EU RT WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW217083A 645 TUL - TWO INCH BY FOUR INCH AREA OF CORROSION ON RIGHT HAND LOWER WING SKIN UPPER SURFACE AT NUMBER NINE SLAT TRACK OPENING. CORROSION HAS DEPTH OF 50+ PERCENT. REPAIRED NUMBER NINE SLAT TRACK OPENING LOWER WING SKIN PER ESO 40-572000-3322 DATED 4/21/2004. 2L72 4F RTA35EU 20040430000722004043000072NM 2004 4 30 AALA20040489 120040426A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21607AM 27058 BOS - EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040430000742004043000074WP 2004 4 30 AALA20040437 120040407A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217535A 49989 PHX - CEILING EMERGENCY LIGHTS AND SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGERS B5-27 AND B5-28 FOR EMERGENCY CEILING LIGHTS AND SLIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040428000402004042800040NE 2004 4 28 BAQA093880 220040317A73100319739560 MANIFOLD UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE LT INJECTION CLOGGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911NH474 0273 WARRANTY. ENG S/N 32047. UNIT REMOVED DUE TO CLOGGING OF NOZZLES. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/19/2004 1G72 3U3 U H88EU E19EU 20040428000442004042800044NM 2004 4 28 DL764040369 120040424A1430114T41457 BOLT BOEING767 767432ER 1385134NM L/E SLAT 9 FAILED A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO27828MH 29699 LEADING EDGE SLAT ASYM EICAS MESSAGE DURING FLAP EXT FOR TAKEOFF. BITE TESTED PSEU. FAULTED TARGET 303 ON 9 SLAT INBOARD END. FOUND TARGET AND BOLT MISSING. REPLACED MISSING PARTS. CLEARED PS CYCLED FLAPS AND SLATS. NO MESSAGES APPEARED. SYSTEM CHECKS GOOD AT THIS TIME. 2L72 4F RTA1NM 20040428000802004042800080NM 2004 4 28 SWAA041069 120040415A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 1000, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428000822004042800082NM 2004 4 28 SWAA041102 120040418A53126545819 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED RON, FOUND NOSE W/W WEB AT LT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040428000842004042800084 2004 4 28 SWAA041105 420040419A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428000862004042800086NM 2004 4 28 SWAA041107 120040419A3350 LIGHT BOEING737 7373Q8 1384670NM EXIT SIGN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29317WN 24068 DURING SPV, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040428000882004042800088NM 2004 4 28 SWAA041126 120040421A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM CARGO BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM AT BS 727 + 18, RBL 44, CRACKED. REPAIRED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040428000902004042800090NM 2004 4 28 SWAA041128 120040421A32601899 UPLOCK SENSOR BOEING737 7373Q8 1384670NM LT MLG MALFUNCTIONED A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29317WN 24068 AIR TURNBACK, DURING POSITION FERRY FROM PAE TO PHX, AFTER LAP INSPECTION, DUE TO LT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR 4 TIMES, LIGHT REMAINED ON IN THE UP POSITION. REMOVED AND REPLACED LT, MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20040428000922004042800092NM 2004 4 28 SWAA041130 120040421A33506556633 LIGHT BOEING737 7373H4 1384600NM OVERWING EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040428000942004042800094NM 2004 4 28 SWAA041095 120040418A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428000962004042800096NM 2004 4 28 SWAA041080 120040416A1430 RIVET BOEING737 7373H4 1384600NM GIRT BAR SHEARED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29654SW 28399 R2 DOOR EVAC SLIDE GIRT BAR FWD FITTING HAS SHEARED RIVET. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR RIVET PER MM. 2L72 4F RTA16WE 20040428000982004042800098 2004 4 28 SWAA041082 420040416A2565D31354 SLIDE BOEING737 7373L9 1384470NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428001002004042800100 2004 4 28 SWAA041084 420040416A25656557463 GIRT BAR BOEING737 7375H4 138449DNM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR FWD FITTING RIVET, LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR FWD FITTING RIVET PER MM. 2L72 4F RTA16WE 20040428001022004042800102NM 2004 4 28 SWAA041086 120040416A53306546881 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001412004042800141 2004 4 28 SWAA041120 420040420A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040428001442004042800144NM 2004 4 28 SWAA041124 120040420A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001652004042800165NM 2004 4 28 SWAA041153 120040424A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040428001672004042800167NM 2004 4 28 SWAA041155 120040424A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772.5, RBL 2.5 TO LBL 2.5, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040428001692004042800169NM 2004 4 28 SWAA041157 120040424A53306545890 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN BELOW L1 DOOR BS 335, LT LOWER SIDE, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040428001742004042800174NM 2004 4 28 DL73S040350 120040419A53306545767531 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089703-14. 2L72 4F A16WE 20040428001772004042800177NM 2004 4 28 DL73S040353 120040419A5330654577274 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089712-14. 2L72 4F A16WE 20040428001792004042800179NM 2004 4 28 DL73S040355 120040419A5330654576537 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089714-14. 2L72 4F A16WE 20040428001822004042800182NM 2004 4 28 DL73S040358 120040419A5330654576622 SKIN BOEING737 737247 138448DNM S10R, BS360-540 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089757-14. 2L72 4F A16WE 20040428001842004042800184NM 2004 4 28 DL76L040360 120040419A324026124121A BRAKE BOEING767 767332 1382001NM MLG LOOSE A DALAO OTHER O OTHER LDLANDING 1 SO27189DN 25990 FOUND NR 5 BRAKE ROTOR/STATORS LOOSE. REPLACED NR 5 BRAKE ASSY PER M/M. 2L72 4F RTA1NM 20040428001862004042800186NM 2004 4 28 DL76L040362 120040420A3350333780100 BATTERY BOEING767 767332 1382001NM EMERGENCY LIGHT DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO271200K 28457 EMERGENCY LIGHT ASSY M9009 INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER BASE. EMERGENCY LIGHT OPS CHECK NORMAL. 2L72 4F RTA1NM 20040428001882004042800188NM 2004 4 28 DLM90040364 120040421A2900 CIRCUIT BREAKER DOUG MD90 MD9030 3023690NM HYD SYSTEM TRIPPED A DALAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO27915DN 53395 RIGHT HYD SYSTEM FAILURE. DECLARED EMERGENCY LANDING, NO HYD. FOUND RIGHT INSTR TRANSFER C/B POPPED. RESET L9 C/B, ALL INDICATIONS. OPERATED PUMPS SYSTEM, CHECKS OK. NO LEAKS FOUND. 2L72 4F RTA6WE 20040428001902004042800190 2004 4 28 DL76L040367 420040422A23301301273111 VIDEO UNIT BOEING767 767332 1382001NM SEAT 6CE INOPERATIVE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27190DN 28447 FLIGHT ATTENDANTS DETECTED FAINT ELECT ODOR IN MID GALLEY AREA. ALL GALLEY C/B'S DEACT. AS A PRECAUTION. ODOR DEC. ALTHOUGH STILL DETECTABLE, NO VISIBLE SMOKE. FOUND J4 CONX WITH MISSING & BENT PINS AT SEAT 6CE. DEACT AVU AT 6CE AND MOVED TERM PLUG TO SEAT 5CE. FWD AVU AT SEAT 6CE TO MCO / PLACARD PER MEL 25-20-01K. 2L72 4F RTA1NM 20040428002002004042800200NM 2004 4 28 CALA0400394 120040419A5310143A948535 SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 SUPPORT FRAME AT FWD PIT STA 500 IS CORRODED. INSTALLED NEW FRAME IAW SRM 51-40-02. 2L72 4F RTA16WE 20040429000352004042900035EU 2004 4 29 M7K2004F00006 120040109A5340350A21004827 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE SUPPORT BEAM CRACKED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19801MH217 3654 RT CABIN ANTI VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME, THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHING OF THE PARTS SHOULD INCLUDE A MUCH GREATER DESIGN RADIUS IN THE AREA OF CRACK OCCURRENCE. 1G72 3U3 U H9EU E00054EN 20040429000562004042900056EU 2004 4 29 BAQA093663 120040222A243523032027 STARTER GEN BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 UNIT INOP, WILL NOT COME ON LINE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1G72 3U3 U H13EU E5NE 20040429000572004042900057EU 2004 4 29 BAQA093665 120040304A6330L633M2010105 MOUNT UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE M/R GEARBOX LEAKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF92 0281 UNIT LEAKING AND FAILED. REPLACEMENT UNIT SENT. REPLACED WITH SERVICABLE UNIT. 03/08/2004 1G72 3U3 U H88EU E34NE 20040429000592004042900059 2004 4 29 BAQA093306 420040305A3120MC7004NVG COMPASS UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE COCKPIT OUT OF ADJUST B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03584AE212 0288 20 DEGREE DEVIATION OF ACTUAL POSITION. REPLACED WITH SERVICEABLE UNIT. 03/09/2004 1G72 3U3 U H88EU E42NE 20040429000792004042900079EU 2004 4 29 BAQA093860 120040315A3150 WARNING LIGHT UROCOPEC135 EC135P2 5620027EU STATIC INVERTER ILLUMINATED E BAQAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA03584AE235 0288 (INVERTER) CAUTION LIGHT ON CPDS. REPLACED WITH SERVICABLE UNIT. 03/22/2004 1G72 3U H88EU 20040429000912004042900091EU 2004 4 29 BAQA093954 120040310A793153408 TRANSMITTER AEROSPAS365 AS365N2 8680815EU OIL PRESSURE INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 PRESSURE TRANSMITTER IS CAUSING GUAGE FLUCTUATIONS (TOP-BOTTOM). REPLACED WITH SERVICABLE UNIT FORM ASSET. 1G72 3U RTH10EU 20040429001052004042900105WP 2004 4 29 ASMF200403002 120040304A3610 CLAMP DOUG DC9 DC987 3022087WP BLEED AIR LEAKING W ASMFK NONE M OVER TEMP ININSP/MAINT 1 SW23803ML 49726 DURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON TAIL CONE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AUGMENTATION VALVE AND REGULATOR PRESSURE VALVE CLAMPS WERE REPLACED IAW MM 20-10-11, GASKET AND NIPPLE OF 13A STAGE BLEED VALVE WERE REPLACED IAW MM 20-10-13, ENGINE RUN WAS PERFORMED AND TEST CORRECT IAW MM 71-00-00. OVER TEMPERATURE TAIL CONE LIGHT WAS CORRECT. 2L72 4F RTA6WE 20040430000092004043000009SO 2004 4 30 C2XA04IA051 120040423A3040 HEATER EMB 145 EMB145 3260210SO WINDSHEILD SMOKE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2714959 4214DE 145091 DURING DESCENT THE CREW REPORTED THAT THE WINDSHIELDS FOGGED UP WITH A BURNING ODOR. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE DEFERRED THE WINDSHIELD HEATING SYSTEM. THE FIRST OFFICER'S WINDSHIELD WAS LATER REMOVED AND REPLACED AND THE DEFERRAL CLEARED. 2L72 4F RTT00011AT 20040430000162004043000016WP 2004 4 30 ASMF200403013 120040322A2913AS66411LS666 PUMP DOUG DC9 DC987 3022087WP HYD SYSTEM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23754RA228043725 49641 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC PRESSURE ON LEFT ENGINE REACHED 4000 PSI AND DROPPED TO ZERO. THE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, TEST CORRECT. 2L72 4F RTA6WE 20040430000352004043000035WP 2004 4 30 ASMF200403019 120040330A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23505MD 49149 CAPTAIN REQUESTED A CHECK FOR DENTS IN RIGHT SIDE OF FUSELAGE NEAR TO THE STATIC PORTS. AIRCRAFT WAS CHECKED BY DENTS IAW SRM 53-04 AND DENTS WERE WITHIN LIMITS. 2L72 4F A6WE 20040430000382004043000038WP 2004 4 30 AALA20040442 120040409A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217514A 49891 THREE EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AT B5-27 AND B5-28 FOR THREE EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000522004043000052NM 2004 4 30 AALA20040451 120040412A3397 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT OVERSIZED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21372AA 25199 SFO - EMERGENCY LIGHT AT SEAT 5B INOPERATIVE. FOUND CONNECTION ON AFT LIGHT OVERSIZED. RESIZED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000552004043000055NM 2004 4 30 AALA20040463 120040414A3397 PIN BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW217375A 25202 LAX - EMERGENCY ESCAPE PATH LIGHTING AT 37H INOPERATIVE. FOUND PUSH BACK PIN AT CONNECTOR NEXT TO SIDEWALL. RESECURED PINS FOR EMERGENCY ESCAPE PATH LIGHTING AT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000692004043000069WP 2004 4 30 AALA20040458 120040413A3397 WIRE HARNESS DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219681B 53631 TPA - EMERGENCY PATH SEAT MOUNTED LIGHTING AT SEAT 22DEF INOPERATIVE. FOUND AREA WHERE LIGHT MODULE MOUNTS TO SEAT AND WIRING HARNESS RETAINING FIXTURE ARE DAMAGED. SEAT NEEDS REPLACED. SEAT NOT IN STOCK AT TPA. PLACARD EMERGENCY ESCAPE PATH LIGHTING SYSTEM PER MEL 33-17, AUTHORITY 4-1313-C. REPLACED WIRE HARNESS AND SECURED TO SEAT FIXURE FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 22DEF. CLEARED MEL 04-1313-C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040430000762004043000076WP 2004 4 30 AALA20040435 120040406A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21403A 49314 DFW - CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 30 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 28 THROUGH 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000772004043000077WP 2004 4 30 AALA20040436 120040406A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21295AA 49307 DFW - CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK B5-102 FOR CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000802004043000080EU 2004 4 30 AALA20040470 120040415A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 MIA - ALL THREE EMERGENCY LIGHTS AT R1 DOOR IS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY 110WL2 FOR ALL THREE EMERGENCY LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040430000812004043000081EU 2004 4 30 AALA20040471 120040415A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 MIA - EMERGENCY SEAT LIGHTS BETWEEN SEATS 1G AND 5G INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY 110WL2 FOR EMERGENCY SEAT LIGHTS BETWEEN SEATS 1G AND 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040430000822004043000082NM 2004 4 30 AALA20040472 120040418A5320 INSULATION BOEING767 767323 1385205NM CABIN DISPLACED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21343AN 33082 POP - INFLIGHT T2058 ENROUTE DFW TO SJU AT FL370, DETECTED SMOKE IN COCKPIT AND CABIN. SMOKE APPEARS TO COME FROM AIR CONDITIONING SYSTEM. COMPLETED EMERGENCY CHECKLIST AND LANDED WITHOUT INCIDENT AT POP. FOUND INSULATION BLANKET CONTACTING PNEUMATIC DUCTS AT AIR MIX MANIFOLD COMPARTMENT. REMOVED INSULATION BLANKET FROM CONTACT WITH PNEUMATIC DUCTS AT AIR MIX MANIFOLD COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000832004043000083NM 2004 4 30 AALA20040468 120040418A33500201720001 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21943AN 30599 MIA - EMERGENCY LIGHT ASSEMBLY AT SEAT 19D INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040430000852004043000085EA 2004 4 30 VNAA0404002 120040401A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ANTI ICE SYSTEM ILLUMINATED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07229PS 7898 DURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. AS THE POWER LEVERS WERE RETARDED, THE MESSAGE CLEARED BY ITSELF AND FLIGHT 2228 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2L72 4F4 FRTA21EA E15NE 20040430000862004043000086NM 2004 4 30 VNAA0403016 120040328A5297 ROD DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE GALLEY DOOR DAMAGED A VNAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL07423JS 3032 THE CREW REPORTED THAT THE GALLEY DOOR WAS VIBRATING IN FLIGHT OVER 150 KNOTS. FLIGHT 2470 THEN DIVERTED TO BWI. THE AIRCRAFT WAS THEN FERRIED TO CAK. MAINTENANCE INSPECTED AND FOUND A SPLICE IN THE STABILZER ROD OF THE GALLEY DOOR. MAINTENANCE REMOVED AND REPAIRED THE SPLICE AND WIRE IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040430000932004043000093NM 2004 4 30 ASMF200404016 120040424A793356B17 SENSOR DOUG MD80 MD83 3023681NM OIL TEMP DAMAGED W ASMFA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 SW23831LF9272 53050 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT HMO AS A CONSEQUENCE OF ENGINE NR 1 WITH OIL TEMPERATURE OSCILLATIONS BETWEEN 110 AND 137 DEGREES F AND OIL PRESSURE OF 47 PSI. DURING CRUISE THE OIL TEMPERATURE WAS 120 DEGREES F, DURING DESCENT THE OIL TEMPERATURE WAS 160 DEGREES F, APPROXIMATELY TO SHUTDOWN TEMPERATURE, AND OIL PRESSURE WAS BETWEEN 45 AND 50 PSI. THE TEMPERATURE SENSOR WAS REPLACED AND FAIL CONTINUE. CABLES WERE CHECKED AND SENSOR AND INDICATOR CABLES WERE GROUNDED. CABLES WERE ISOLATED AND ENGINE RUNNING WAS PERFORMED. DURING OVERNIGHT SERVICE LEFT TEMPERATURE SENSOR WAS REPLACED IAW MM 79-32-01 AND ENGINE RUNNING WAS PERFORMED IAW MM 71-00-00. CABLES WERE REPAIRED. 2L72 4F RT 20040430000942004043000094WP 2004 4 30 ASMF200404017 120040425A2161 WIRE DOUG DC9 DC987 3022087WP SENSOR DAMAGED W ASMFI CABIN DEPRESSURIZATION H ELECT. POWER LOSS-50 PC DEDESCENT 1 SW23751RA 49779 CAPTAIN REPORTED THAT DURING DESCENT WITH ENGINES ON IDLE, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT TURNED ON. PROCEDURE WAS ACCOMPLISHED TURNING OFF THE LIGHT, BUT WITH AIR CONDITIONING SYSTEM ON, HP BLEED OF FLOW LIGHT TURNED ON AND AT 5000 FEET, AIRCRAFT WAS DEPRESSURIZED. DURING TEST ON GROUND BOTH PACKAGES WERE OUT OF SERVICE WITH DUCTS COVERS BROKEN AND WITH THE WIRING SENSOR TEMP HIGH LOOSEN DUE TO A PNEUMATIC LEAKAGE. DUCT WAS CORRECTLY INSTALLED AND WIRING WAS REPAIRED, TESTS WERE PERFORMED IN ACCORDANCE WITH MM 30-10-00 AND 21-00-00, ALL CORRECT. 2L72 4F RTA6WE 20040430000952004043000095WP 2004 4 30 ASMF200404018 120040425A528039567851 LINK DOUG DC9 DC982 3022082WP MLG DOOR DAMAGED W ASMFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW23501AM565771132 49188 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF STRONG VIBRATION ON NOSE LANDING GEAR. DURING CHECK, IT WAS DETECTED THAT THE NOSE LANDING GEAR RIGHT DOOR WAS OPEN. DOOR MECHANISM WAS LUBRICATED AND BRAKES WERE COOLED. OPERATIONAL CHECK WAS PERFORMED TO DOOR MECHANISM BEING CORRECT IN ACCORDANCE WITH MM 32-20-00. DURING TRANSIT CHECK AT MEX, NOSE LANDING GEAR DOORS WERE CHECKED DETECTING THAT THE FASTENER DID NOT OPERATE CORRECTLY, IT WAS REPLACED AND ACTUATOR WAS ADJUSTED IN ACCORDANCE WITH MM 32-22-01, TESTS CORRECT. 2L72 4F A6WE 20040430000962004043000096NM 2004 4 30 VNAA0404016 120040419A2720 PIN DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE RUDDER INSTALLED A VNAAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 GL07429JS 3043 FLIGHT 2597 RETURNED TO GATE WITH RUDDER PEDDLES JAMMED. MAINTENANCE INSPECTED AND REMOVED RIG PIN FROM RUDDER PEDDLES IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040430000972004043000097EA 2004 4 30 VNAA0404017 120040420A3610GG670803203 GASKET CNDAIRCL600 CL6002B19 1900309EA GROUND AIR FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07702PS37 10135 FLIGHT 2292 RETURNED TO GATE WITH ANTI ICE DUCT MESSAGE, BLEED LOOP FAIL. MAINTENANCE INSPECTED AND REPLACED THE GROUND AIR CONNECTION GASKET IN ACCORDANCE WITH THE BOMBARDIER MAINTENANCE MANUAL 36-17-01-400-801-A01. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040430000982004043000098EA 2004 4 30 VNAA0404013 120040415A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA LEFT OUT OF RIG A VNAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL07220PS 7887 AFTER TAKEOFF, FLAPS FAILED AT 8. FLIGHT 2270 RETURNED TO PHL. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND RIGGED LEFT HAND AND RIGHT HAND FLAPS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 27-54-00-803-801. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040430001002004043000100NM 2004 4 30 VNAA0404015 120040416A6120D11992 CONTROL UNIT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE RT PROPELLER FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07440JS21660613 3058 ON TAKEOFF, RIGHT HAND ENGINE TORQUE SPIKED TO 125. FLIGHT 2540 ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040430001012004043000101NE 2004 4 30 VNAA0403021 220040328A73208111804004 ECU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LT ENGINE FAILED A VNAAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL07438JS18477 3056 DURING CLIMBOUT AND ENROUTE, THE CREW REPORTED THAT THE LEFT HAND ENGINE LOST 30 PERCENT TORQUE AND THE AIRCRAFT YAWED BOTH TIMES. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE INSPECTED AND ADJUSTED BLADE ANGLES, RETRIMMED THE ENGINES, SWAPPED ECU'S AND REPLACED THE HYDROMECHANICAL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. GROUND RUNS AND THEN A OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040430001032004043000103NM 2004 4 30 AALA20040480 120040420A3350 SIGN BOEING737 737823 13844BZNM EMERGENCY LIGHT DISLODGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21937AN 30082 MEX - FORWARD GALLEY EMERGENCY EXIT SIGN OUT OF PLACE. REINSTALLED FORWARD GALLEY EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040430001052004043000105NM 2004 4 30 DL757040365 120040421A3350276005 FUSE BOEING757 757232 1384965NM EMERGENCY LIGHT BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27671DN 25332 ON INSPECTION FOUND EMERGENCY LIGHTS FWD OF 1R AND 1L DOOR INOP. REPLACED FUSE AT AFFECTED POWER SUPPLY PER MM. OPN OF LIGHTS NORMAL. 2L72 4F RTA2NM 20040430001062004043000106NM 2004 4 30 ASAA0410119 120040317A5347655496921 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK AT STATION 887 TO 947 CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040430001092004043000109NM 2004 4 30 ASAA0410149 120040323A531565549055 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON FLOORBEAM STATION 480. REPAIR IAW EA. (M) 2L72 4F A16WE 20040430001122004043000112EU 2004 4 30 USAA040041 120040228A5321D536716500000 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND FLOOR PANEL DELAMINATED 1.5 SQUARE INCH, TOP SURFACE FLOOR PANEL 241EF, FRAME 36-42. FABRICATED NEW FLOOR PANEL PER SRM 53-02-00. (M) 2L72 4F RTA28NM 20040430001132004043000113EU 2004 4 30 USAA040033 120040226A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW 0949 BFM - FOUND R2 DOOR SILL CORRODED 3.75 INCH BY 2 INCH BY .10 INCH DEEP, +X 2780, -Y 155 CM, Z = 0. CORROSON LEVEL 1, TASK/CARD NR JA 260-53500. DEFECTIVE REPLACED WITH IDENT PART NR PER SRM 51-42-11, 53-41-14, FIG 101. (M) 2L72 4F RTA28NM 20040430001152004043000115EU 2004 4 30 USAASA04033 120040401A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT WILL NOT TEST A USAAK NONE L NO TEST ININSP/MAINT 1 EA19753US 1326 RI - FOUND AN EMERGENCY LIGHT THAT WOULD NOT TEST. MAINTENANCE REPLACED THE FORWARD EPSU. (M) 2L72 4F RTA28NM 20040430001192004043000119NM 2004 4 30 USAABB04029 120040320A335020131A BATTERY PACK BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19627AU 27805 PHL - FOUND R1 DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F RTA2NM 20040430001202004043000120NM 2004 4 30 USAASB04039 120040330A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19784AU 25023 PIT - MAINTENANCE REPORTED THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTING AT SEAT ROWS 24 AND 25, LEFT SIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 20131A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040430001212004043000121EA 2004 4 30 ASOA04226 120040320A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURNG A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR TOP STEP IAW SRM 51-73-00. (M) 2L72 4F RTA21EA 20040430001222004043000122EU 2004 4 30 USAA040032 120040223A5320D5361042200000A0SPLICE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND SPLICE CORRODED 4 INCH BY 2 INCH BY .02 INCH AREA, FRAME 20, Y-765 - Y-254. CORROSION LEVEL 1, TASK/CARD NR JA-220-53500. DEFECTIVE PART REPLACED WITH IDENT PART NUMBER. (M) 2L72 4F RTA28NM 20040503000022004050300002EA 2004 5 3 ASOA04229 120040321A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE SERVICE DOOR INTERCOSTAL ON BOTH SIDES WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR INTERCOSTAL ON BOTH SIDES IAW SRM 51-24-21. (M) 2L72 4F RTA21EA 20040503000042004050300004EU 2004 5 3 USAA040043 120040312A5321D5367175601000 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19706US 0946 BFM - FOUND FLOOR DELAMINATED 10 INCHES BY 24 INCHES, AFT CABIN RIGHT SIDE BETWEEN FRAME 68-70 AT FORWARD END OF PANEL. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M) 2L72 4F RTA28NM 20040503000082004050300008NM 2004 5 3 USAASB04036 120040326A33501010731 LIGHT BOEING737 7374B7 1384702NM AFT ENTRY DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19430US 24552 PIT - MAINTENANCE REPORTED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040503000092004050300009NM 2004 5 3 USAASB04041 120040330A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19527AU 23862 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10, INCLUDING THE ARROW SIGNS, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK, P/N 2013-1A AT BODY STATION 400. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040503000132004050300013NM 2004 5 3 ASAA0410096 120040301A5313654655413 STRINGER BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 21L AND FRAME 847. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000152004050300015NM 2004 5 3 ASAA0410101 120040302A53136546552 STRINGER BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 21L AND STATION 827. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000162004050300016EU 2004 5 3 USAA040040 120040305A5320D53471124200 PLATE AIRBUSA319 A319112 3930323EU FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND PLATE SHEAR CORRODED 5 LOCATIONS 1-2 SQUARE INCHES, .032 INCH DEEP, FS 69-70, -Y1292, Z=0. REMOVED AND REPLACED PLATE WITH IDENT PART NR PER SRM 53-41-17, SRM 51-42-11. (M) 2L72 4F RTA28NM 20040503000172004050300017EU 2004 5 3 USAA040039 120040227A5310D5347219620000 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND BEAM CORRODED .9 INCH BY .8 INCH, 2 HOLES BLOWN, FORWARD LEFT FRAME 64-66 PLUS Y1292 Z=0. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14 PAGE 106, FIG 102. (M) 2L72 4F RTA28NM 20040503000182004050300018NM 2004 5 3 GAIA04066ST 120040326A5320BAC15141617 ANGLE BOEING727 727223 1384074NM FS CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND AN ANGLE WAS CRACKED ON THE AFT AIRSTAIR ACTUATOR ATTACH POINT FS 1263 WL 200 RBL 22. INSTALLED ANGLE REPAIR IAW BOEING B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503000202004050300020EU 2004 5 3 USAA040036 120040227A5320D5347217220300 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW 0949 BFM - FOUND FLOOR SUPPORT BEAM CORRODED 1 INCH BY .8 INCH, 3 HOLES, RT AFT FRAME 68-70 Z=0. CORROSION LEVEL 2, TASK/CARD NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14 FIG 102, PAGE 106. (M) 2L72 4F RTA28NM 20040503000212004050300021NM 2004 5 3 ASAA0440011 120040122A2612 MODULE BOEING737 7374Q8 138447QNM APU FIRE DETECT MALFUNCTIONED A ASAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM01763AS 25100 GYR - AFTER TAKEOFF APU FIRE DETECTION FAULT LIGHTS ON FIRE WARNING PANEL ILLUMINATED. AIRCRAFT RETURNED TO GYR AND LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. REPLACED FIRE DETECTION ELECTRONICS RACK MODULE. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040503000222004050300022WP 2004 5 3 ASAA0480189 120040315A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 9-14. RECONNECTED LOOSE CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040503000232004050300023NM 2004 5 3 ASAA0440018 120040203A33508100022601 LIGHT BOEING737 7374Q8 138447QNM ROW 15-16 DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 FOUND EMERGENCY EXIT FLOOR LIGHTING AT ROW 15-16 HAVE COME APART AND UNPLUGGED. INSTALLED LAMP ASSEMBLY AT ROW 16 PER AMM 33-51-02. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040503000242004050300024WP 2004 5 3 ASAA0480099 120040224A33970105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 LAX - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FORWARD CABIN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040503000252004050300025WP 2004 5 3 ASAA0480110 120040227A33970105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 SEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN TWO FORWARD CABIN LOCATIONS. RECONNECTED CONNECTORS IN BOTH LOCATIONS. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040503000262004050300026WP 2004 5 3 ASAA0480112 120040228A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 LAX - DURING PREFLIGHT CHECK, FOUND FIRST CLASS CABIN EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE, BROKEN. RECONNECTED CONNECTOR. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20040503000312004050300031EU 2004 5 3 MALA040363 120040423A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REMOVED AND REPLACED ICE GUARD NR 7 IAW SAAB 340 SRM 53-70-10-2 AND MESABA EO S53005. A/C RELEASE DATE 4/25/04. 2L72 4T RTA52EU 20040503000332004050300033EU 2004 5 3 MALA040360 120040422A5230 STRUCTURE SAAB SF340 340B 7860101EU CARGO DOOR GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED FWD LOWER CORNER GOUGE AREA OF CARGO DOOR IAW SAAB SRM 52-10-10 PARAGRAPH 1 AND MESABA EO S52028. A/C RELEASE DATE 4/25/04. 2L72 4T RTA52EU 20040503000342004050300034SO 2004 5 3 C2XA04SH252 120040429A532014521725015 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040503000352004050300035NM 2004 5 3 ASAA0410147 120040322A33508731002142 LIGHT BOEING737 737290C 138448VNM SMOKE BARRIER INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING MAINTENANCE, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED ILGHT ASSEMBLY. (M) 2L72 4F A16WE 20040503000362004050300036NE 2004 5 3 A6WA200460006 220040310A72502141057R60 TURBINE WHEEL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 4 ENGINE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 NR 4 ENGINE, 4TH TURBINE WHEEL LOST HEAD OF RIVET WHICH HOLDS BLADE IN PLACE, CAUSING IMPACT DAMAGE TO 4TH NOZZLE CONTAINMENT RIGHT. MAINTENANCE REMOVED AND REPLACED 4TH T-WHEEL ASSEMBLY. (M) 2H74 4F4 FRTA49EU E6NE 20040503000372004050300037EU 2004 5 3 MALA040338 120040418A3350 LIGHT SAAB SF340 340B 7860101EU CABIN MALFUNCTIONED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15426XJ 340B426 EMERGENCY LIGHTS - UNARMED CAUTION LIGHT CAME ON IN FLT, EMERGENCY LIGHTS CAME ON IN CABIN. CYCLED SWITCH FROM OFF TO ARMED AND RESET C/B L7 AND L8 NEITHER WORKED. AIR RETURN TO MSP. MAINTENANCE CYCLED AC PWR EMERGENCY LIGHTS OPS CHECKS GOOD IAW SF340 MM CH33. 2L72 4T RTA52EU 20040503000382004050300038 2004 5 3 MALA040339 420040420A344220412220435 DISPLAY BAC 146 AVRO146RJ85A1500097EU COCKPIT FAULTY A MALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL15506XJ E2314 RADAR IN TURB MODE GOES FROM 0 TO +2.5, CAPTAINS SCREEN WOBBLES 80NM SCALE & BELOW AND WITHIN 30 NM OF LEVEL 4 DID NOT PAINT PRECIPITATION. AIR RETURN TO MSP. MAINTENANCE REPLACED RADAR DISP AND R/T. R/T P/N ON&OFF 204-1217-0414, S/N ON 7203, S/N OFF 7462, DISPLAY P/N ON&OFF 2041222-0435, S/N ON 4699, S/N OFF 5000. WX RADAR SYSTEM TEST GOOD IAW RJ MM CHAPT 34. 2H74 4F RTA49EU 20040503000402004050300040EU 2004 5 3 MALA040337 120040417A261289905202 FIRE DETECTOR SAAB SF340 340B 7860101EU LT ENGINE FAULTY A MALAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15366PX 340B267 AFTER ENGINE START, LEFT ENGINE FIRE WARNING ON CWP AND LEFT FIRE HANDLE ILLUMINATED, ALONG WITH FIRE BELL. LIGHTS AND WARNING WERE ON BRIEFLY, THEN EXTINGUISHED. TESTED THE LEFT FIRE SYSTEM ON TEST PANEL, TEST GOOD. THEN THE FIRE INDICATION OCCURRED AGAIN. MAINTENANCE REMOVED AND REPLACED FIRE DETECTOR P/N 899052-02, S/N ON 0840, S/N OFF 0620, AND WEU P/N 006W00, S/N ON 1581, S/N OFF 1623, IAW AMM 31-50-05 AND 26-11-10. OPS CHECK GOOD. 2L72 4T RTA52EU 20040503000412004050300041SO 2004 5 3 C2XA04SH246 120040427A532014522178005 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040503000452004050300045SO 2004 5 3 C2XA04SH248 120040427A532014521725001 SILL EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV - DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040503000462004050300046SO 2004 5 3 C2XA04SH249 120040427A531514522461011 DOUBLER EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040503000472004050300047SO 2004 5 3 C2XA04BT052 120040425A212014520385405 DUCT EMB 145 EMB145XR 3260214SO A/C BAY DAMAGED A C2XAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2718102 145643 LAV SMOKE WARNING AFTER T/O, DECLARED EMERGENCY, QRH COMPLETED, AIR RETURNED TO IAD. COOKING SMELL NOTED FOR 2 MIN. WARNINGS WENT AWAY AFTER C/B PULLED. FWD GALLEY SMOKE DETECTOR ACTIVATED. MX OPS CHECKED ALL PAX CABIN LIGHTS, OPS CHECKED GOOD. NO BURNING SMELL. ALL SOCKETS FOR FLUORESCENT LIGHT TUBES GOOD. OPERATED BLEED AIR SYS FOR CABIN DISTRIBUTION, COULD NOT DUPLICATE. NEXT ATTEMPTED T/O ABORTED, WITH STRONG BURNT COOKING SMELL. SMELL DISSIPATED BUT LINGERED TO GATE. MX INSPECTED NR 1 PACK SYS, FOUND LOOSE INSULATION & RESECURED INSULATION; RAN BOTH ENG 5 MIN, NO BURNING SMELL. PACK NR 1 PLACED ON MEL. REMOVED & REPLACED AIR CONDITIONING DUCT AFT OF DUAL HEAT EXCHANGER. REMOVED FROM MEL. 2L72 4F RT 20040503000502004050300050EU 2004 5 3 A6WA200460007 120040310A14305L443440 RIVET BAC 146 146200A 1500266EU FUSELAGE BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 6TH RIVET ABOVE PAX WINDOW AT FRAME STATION 755.48, RIVET MISSING HEAD. MAINTENANCE INSTALLED BLIND CHERRY-MAX FASTENER. (M) 2H74 4F A49EU 20040503000522004050300052SO 2004 5 3 C2XA04CL039 120040423A3350 LIGHT EMB 145 EMB145 3260210SO CABIN MALFUNCTIONED A C2XAK NONE O OTHER UKUNKNOWN 1 SW2714974 145161 CLE FLIGHT 2114 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT AFTER TESTING. MAINTENANCE PERFORMED A RESET OF THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040503000532004050300053SO 2004 5 3 C2XA04CL040 120040423A335078241 INVERTER EMB 145 EMB145ER 3260211SO CABIN FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM THE AFT EMERGENCY EXIT TO THE LAV. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040503000542004050300054SO 2004 5 3 CHQA000481 120040427A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST UKUNKNOWN 1 GL11286 145443 TWO EMERGENCY LIGHT STRIPS REPORTED INOPERATIVE. MAINTENANCE REPLACED 2 EA EMERGENCY LIGHT FLOOR STRIPS. OPS CHECK GOOD IAW EMB-145MM 33-50-08. 2L72 4T RTT00011AT 20040503000582004050300058GL 2004 5 3 C2XA04TY074 220040428A720023074962 ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27181021834 1834 145643 TYS - FLIGHT 2110 PERFORMED AIR RETURN DUE TO ABNORMAL SMELL FROM NR 2 PACK. A/C WAS RELEASED IAW MEL 21-51-00/2 CAT-C CONTROL 041491 TO TYS WHERE MAINT REMOVED AND REPLACED THE NR 2 ENG IAW ROLL ROYCE MM 72-00-00. ALL WORK WAS ACCOMPLISHED WITH LEAK, VIBES AND OPS CHECKS GOOD. A/C RELEASED TO SERVICE AFTER ALL WORK WAS C/W. 2L72 4F4 FRT TE6CH 20040503000592004050300059NM 2004 5 3 CALA0400396 120040419A5320BAC149644 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 FWD CARGO RIGHT Z-CHANNEL CORRODED FROM STA 500-500I. INSTALLED NEW CHANNEL IAW SRM 53-00-53. 2L72 4F RTA16WE 20040503000602004050300060NM 2004 5 3 CALA0400397 120040419A5320146A7502 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 AFT CARGO FLOOR Z-CHANNEL CORRODED FROM STA 727G-794. INSTALLED Z-CHANNEL IAW SRM 53-60-53. 2L72 4F RTA16WE 20040503000612004050300061NM 2004 5 3 CALA0400398 120040419A5320146A7502 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 AFT CARGO RIGHT Z-CHANNEL CORRODED FROM STA 727 TO 727G. INSTALLED NEW CHANNEL IAW SRM 53-60-53. 2L72 4F RTA16WE 20040503000622004050300062EA 2004 5 3 A6WA200440033 120040318A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31451AW 7832 STRANGE ODOR NOTED IN CABIN. REVIEWED HISTORY IN ATA 21-24-33-36-49, NO HISTORY ASSOCIATED WITH CABIN ODOR, INSPECTED CABIN, EXTERIOR, MLG BAGS, CARGO BAY, AFT EQUIPMENT BAY AND AVIONICS BAY. NO DEFECTS NOTED. COULD NOT DUPLICATE WITH PASSENGERS DEBOARDED. (M) 2L72 4F RTA21EA 20040503000632004050300063NM 2004 5 3 CALA0400399 120040419A5320BAC146377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 AFT CARGO LEFT Z-CHANNEL CORRODED FROM STA 727+4 TO 827. INSTALLED Z-CHANNEL IAW SRM 53-00-53. 2L72 4F RTA16WE 20040503000692004050300069WP 2004 5 3 ASAA0480066 120040206A33500105606 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 OAK - DURING PREFLIGHT CHECK, FOUND LAST TWO EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RECONNECTED CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040503000752004050300075NM 2004 5 3 ASAA04101010 120040306A53136935352 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AT STATION 887. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000762004050300076NM 2004 5 3 ASAA0410137 120040317A14306546533 NUT PLATE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT FRAME AT STATION 500 NUT PLATES CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000782004050300078NM 2004 5 3 AALA20040477 120040419A3397 WIRE BOEING757 757223 1384957NM EXIT SIGN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21635AA 24593 DFW - RIGHT HAND EMERGENCY EXIT SIGN AT ROW 17 INOPERATIVE. RECONNECTED RIGHT HAND EMERGENCY EXIT SIGN WIRES AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040503000792004050300079WP 2004 5 3 AALA20040473 120040419A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217548A 53030 MIA - CEILING EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503000802004050300080WP 2004 5 3 AALA20040474 120040419A3350 CONTACTOR DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219619V 53566 DFW - EMERGENCY DIRECTIONAL LIGHT MOUNTED ON FORWARD GALLEY WALL INOPERATIVE. REPINNED QUICK DISCONNECT CONTACT FOR EMERGENCY LIGHT MOUNTED ON FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040503000812004050300081WP 2004 5 3 AALA20040475 120040419A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21555AN 53085 DFW - AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR AFT GALLEY EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503000842004050300084SO 2004 5 3 C2XA04CL025 120040320A33507281000501 CONTROL MODULE EMB 145 EMB145LR 3260212SO CABIN INTERMITTENT A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2711544 145557 MSN FLIGHT 2152, THE CREW REPORTED A EMERGENCY LIGHTS WOULD NOT ARM MESSAGE. THE CREW RESET AND OPERATIONAL CHECKS WERE GOOD. AFTER AIRCRAFT ARRIVED IN CLE MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040503000892004050300089EA 2004 5 3 SWIA200413111 120040404A27604916406 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07447SW3794 3794 7677 ON TAXI, RECEIVED FLIGHT SPOILERS FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE UNIT IAW 27-00-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040503000902004050300090EA 2004 5 3 SWIA200413112 120040403A2751 INDICATOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07590SW 7077 GEAR/FLAP ANNUNCIATED AT FL330. WHITE BAR WENT FROM FLAPS 2 DEGREES - 3 DEGREES - 6 DEGREES - 8 DEGREES. FLIGHT CONTROL PAGE SHOWS FLAPS 10 DEGREES LEFT, 0 DEGREES RIGHT - NO ADVERSE HANDING CHARACTERISTICS. REMOVED AND REPLACED FLAP POSITION INDICATOR AS REQ. OPS CHECK GOOD IAW MM 27-55-01. 2L72 4F RTA21EA 20040503000912004050300091EA 2004 5 3 SWIA200413113 120040405A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07587SW 7062 STAB AND MACH TRIM DISENGAGED DURING FLIGHT. REMOVED AND REPLACED CAPTAIN'S PITCH DISCONNECT SWITCH IAW MM 27-41-30. OPS CHECK GOOD. 2L72 4F RTA21EA 20040503000932004050300093NM 2004 5 3 ASAA0410109 120040306A5311654656733 FRAME BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FRAME AT STATION 1006 HAS MECHANICAL DAMAGE AT STRINGER 1006. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000942004050300094NM 2004 5 3 ASAA0410102 120040303A5313654577432 STRINGER BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED STRINGER 21L FORWARD OF FRAME STATION 727-787 AND 887. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000952004050300095WP 2004 5 3 ABXA040117 120040326A32607000010101ABX1 DOWNLOCK SWITCH DOUG DC8 DC861 3021952WP NLG CORRODED A ABXAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL23853AX 5989 46037 AFTER GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT COME ON. NO RED UNSAFE LIGHT ON. REPLACED BULBS, NO HELP. CREW PERFORMED A GO-AROUND, CYCLED GEAR. VISUALLY CHECKED NOSE GEAR DOWN AND LOCKED, MADE NORMAL LANDING. GEAR PINNED AFTER LANDING AND AIRCRAFT TAXIED TO GATE. NOSE GEAR GREEN LIGHT CAME ON AFTER BLOCK IN AT GATE. FOUND NOSE GEAR DOWNLOCK SWITCH AND CONNECTOR CORRODED AND CAUSING INDICATION PROBLEMS. REPLACED CONNECTOR IAW DC-8 MM 20-50-01-2. REPLACED SWITCH IAW DC8 MM 32-60-00. OPS CHECKED GOOD. 2L74 4F 4A25 20040503000982004050300098NM 2004 5 3 ASAA0410107 120040306A5313693535261 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND DENT ON STRINGER CLIP AT STATION 727A AND STRINGER 23L. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000992004050300099GL 2004 5 3 C2XA04SH253 220040426A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 DAMAGED A C2XAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW27185564438 4438 145595 SHV - FLIGHT 2806 FROM IAH TO MEM CREW REPORTED LOW OIL QUANTITY AND HIGH OIL TEMPERATURE 25 MINUTES AFTER TAKEOFF AT CRUISE ALTITUDE. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE IAW CONTINENTAL EXPRESS TASK CARD 6271001. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040503001012004050300101NM 2004 5 3 ASAA0410116 120040308A53306545778 SKIN BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND DENT ON LOWER FUSELAGE SKIN 6 INCHES. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040429000442004042900044NE 2004 4 29 ALGA093899 120040323A632023076252 GEAR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03702AL1032 760243 CAE890304S FOUND HEAVY SPALLING ACROSS GEAR TEETH OF PTO GEAR. 1G72 3U3 U H1NE E1GL 20040429000462004042900046EU 2004 4 29 BAQA093957 120040317A6710 ROD END UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ACTUATOR EXCESS PLAY E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME2359 355 0144 EXCESSIVE LATERAL PLAY IN ACTUATOR ROD END. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1G72 3U3 U H88EU E34NE 20040429000542004042900054SW 2004 4 29 ALGA093945 120040325A6220406310405101 BEARING BELL 407 407 1182206SW M/R DRIVE BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL246 53265 BEARING ROUGH AND BINDING. 1G71 3U O H2SW 20040429000632004042900063 2004 4 29 BAQA092513 420040204A3420109290 GYRO BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE COCKPIT NOISY E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117UP3241 7508 UNIT MAKING NOISE WHEN INSTALLED ON AIRCRAFT. REPLACED BY SERVICABLE UNIT. 03/11/2004 1G72 3U3 UNCH13EU E19EU 20040429000672004042900067EU 2004 4 29 BAQA093737 120040316A2914L290M20A1014 PUMP UROCOPEC135 EC135T1 5620026EU TMECA ARRIELARRIEL1 60030NE HYD PUMP LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03911NH474 0273 HYDRAULIC PUMP IS LEAKING AT SHAFT. REPLACED WITH SERVICABLE UNIT. 03/17/2004 1G72 3U3 U H88EU E19EU 20040429000802004042900080 2004 4 29 BAQA093886 420040315A3120B1894522281A CLOCK UROCOPEC135 EC135T1 5620026EU COCKPIT INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03522ME 0144 LIGHT WAS INSTALLED ON 01/19/2004 AND FAILED 03/15/2004 FOR A TOTAL OF 80.4 FLIGHT HOURS. INTERNAL LIGHTING IS INOPERATIVE. CLOCK WAS PURCHASED OUTRIGHT ON OUR PO 2-022166-05. 1G72 3U H88EU 20040429000822004042900082EU 2004 4 29 BAQA093189 120040319A2422PC251123E INVERTER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1971 7235 WARRANTY. UNIT DISPLAYS INVERTER LIGHT. REPLACED WITH SERVICABLE UNIT. 03/23/2004 1G72 3U3 U H13EU E5NE 20040429000842004042900084 2004 4 29 BAQA092498 420040310A3421C17027AA01 INDICATOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ATTITUDE FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03136MH2469 0161 UNIT READS 80' OFF. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1G72 3U3 U H88EU E34NE 20040429000852004042900085EU 2004 4 29 BAQA092236 120040310A6730L673M40A1001 ACTUATOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE TAIL ROTOR LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03136MH 0161 ACTUATOR LEAKS IN DIFFERENT POSITIONS. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/24/2004 1G72 3U3 U H88EU E34NE 20040429000882004042900088 2004 4 29 BAQA093941 420040308A3120B1894522281A CLOCK UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT FAILED D BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH 0131 CLOCK WILL NOT HOLD CORRECT TIME, RUNNING FAST. REPLACED WITH UNIT PURCHASED OUTRIGHT THROUGH AEC (PO 2-023000-06) 1G72 3U3 U H88EU E34NE 20040429000932004042900093 2004 4 29 BAQA093963 420040316A3120B1894522281A CLOCK UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03575ME1 0157 UNIT FAILED OUT OF BOX, BACKLIGHTING IS INOPERATIVE. P.O. NR ABOVE REFERENCES A/C S/N 0284, BUT UNIT WAS INSTALLED ON A/C S/N 0157, OK TO RETURN. 03/26/2004 1G72 3U3 U H88EU E34NE 20040430000272004043000027NM 2004 4 30 ASMF200404002 120040401A5350100910033 RADOME DOUG MD88 MD88 3023688NM FUSELAGE CRACKED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23162PL 49765 DURING TRANSIT CHECK WAS DETECTED A FOD IMPACT ON RADOME. RADOME HAS AN APPROXIMATELY CRACK OF 24 INCHES PER 20 INCHES. RADOME WAS REPLACED IN ACCORDANCE WITH MM 53-51-00. 2L72 4F RTA6WE 20040430000282004043000028 2004 4 30 ASMF200403006 420040312A3421111702 MONITOR DOUG MD80 MD83 3023681NM FMA FAILED W ASMFK NONE J WARNING INDICATION CRCRUISE 1 SW23861LF8167 8167 49826 CAPTAIN REPORTED THAT MONITOR LIGHT HINGE ON BOTH FMA'S. TECHNICAL PERSONNEL RESTED THE LIGHT BUT IT CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR DUE TO IT HAS APU INOPERATIVE. DURING OVERNIGHT SERVICE FMA MONITOR WAS REPLACED AND TESTED IN ACCORDANCE WITH MM 32-29-01AND BREAKER B10-19 OF VERTICAL GYRO NR 1 WAS REPLACED IN ACCORDANCE WITH WDM 34-24-01, ALL CORRECT. 2L72 4F RT 20040430000392004043000039NM 2004 4 30 AALA20040446 120040410A3397 CONNECTOR BOEING737 737823 13844BZNM CABIN DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21928AN 29528 EMERGENCY ESCAPE PATH LIGHT AT ROW 19D INOPERATIVE. FOUND PIN PUSHED BACK AT SIDEWALL CONNECTOR. RECONNECTED PIN AT SIDEWALL CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT ROW 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040430000482004043000048NM 2004 4 30 AALA20040449 120040410A2520 MOTOR BOEING777 777223 1385213NM SEAT SHORTED A AALAK NONE O OTHER CRCRUISE 1 SW21792AN 30253 LHR - BELT CAUGHT IN SEAT TRACK AT 4J AND SHORTED TRACKING AND SWIVEL MOTORS OUT. SMOKE WAS PRESENT. PULLED CIRCUIT BREAKER FOR SEAT 4J AND PLACARD PER 25-04D AUTHORITY 4-105DC-C. REPLACED LEFT BACK SUPPORT ARM ADJUSTED SWIVEL CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040430000592004043000059WP 2004 4 30 AALA20040440 120040407A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217519A 49896 DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 22 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK AT B5-106 FOR CABIN CEILING EMERGENCY LIGHTS AT ROWS 22 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000602004043000060NE 2004 4 30 AALA20040482 220040421A7261 SEAL AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE LT ENGINE LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2170073 516 695221 SDQ - INFLIGHT T9621/20 SJU-MIA LEFT HAND ENGINE OIL QUANTITY LOSS. AT CRUISE NUMBER 1 OIL QUANTITY SLOWLY DECREASED. PULLED ENGINE TO IDLE AND LEAK CONTINUED. SHUT ENGINE DOWN AT 6 QUARTS. ENGINE WINDMILLED AT ABOUT 15 PERCENT WITHOUT OIL QUANTITY OR PRESSURE FOR APPROXIMATELY 20 MINUTES DURING DIVERT TO SDQ. ALL OTHER ENGINE INDICATIONS WERE NORMAL PRIOR TO SHUTDOWN. FOUND OIL LEAK ON THE PRESSURE LINE COMING FROM THE OIL COOLER. REPLACED A GASKET SEAL ON THE PRESSURE LINE COMING FROM THE OIL COOLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20040430000882004043000088 2004 4 30 VNAA0403014 420040326A3418 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AOA FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL THEN ABORTED TAKEOFF. AS THE AIRCRAFT PULLED OFF OF THE RUNWAY IT CORRECTED ITSELF, THE CREW REPORTED VERY WINDY CONDITIONS. THE AIRCRAFT WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040430000892004043000089NM 2004 4 30 VNAA0403013 120040325A335051122803 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07462PS21803959 3084 THE CREW REPORTED THAT THE EMERGENCY BATTERY TEST FAILED. MAINTENANCE INSPECTED AND REPLACED THE AFT EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040430000902004043000090NE 2004 4 30 VNAA0403012 220040320A720041590200 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT ENGINE FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07434JS22637 3051 DURING FLIGHT, THE RIGHT HAND ENGINE ITT INDICATED 100 DEGREES HOTTER THAN THE LEFT HAND ENGINE AND THE CREW RETURNED TO DCA. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND ENGINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED BAD. MAINTENANCE THEN INSPECTED AND CHANGED THE HIGH PRESSURE COMPENSATOR VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040430000922004043000092NM 2004 4 30 ASMF200404015 120040423A2780 CONTROL CABLE DOUG MD88 MD88 3023688NM SLAT DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23160PL 49763 DURING TRANSIT CHECK SLAT NR 5 ON LEFT WING DID NOT RETRACT. A CYCLE OF SLAT WAS PERFORMED WITHOUT POSITIVE RESULTS. PANEL WAS REMOVED AND A CABLE WAS DETECTED WITH DAMAGE. THE LEFT SLAT NR 5 CABLE AND PULLEY WERE REPLACED IAW MM 27-80-01, ALL CORRECT. 2L72 4F RTA6WE 20040430001162004043000116EU 2004 4 30 USAA040034 120040227A5315D5347118820400 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND FLOORBEAM CORRODED 1.1 INCH BY 1.0 INCH, THREE BLOWN OUT HOLES, AFT LEFT FRAME 68-70, +Y 1292, Z=0. CORROSION LEVEL 2, TASK/CARD NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14, PAGE 106, FIG 102. (M) 2L72 4F RTA28NM 20040430001172004043000117EU 2004 4 30 USAASA04014 120040209A2120 ODOR AIRBUSA319 A319112 3930323EU COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA19711UW 1033 SJU - FLT 1266 - EN ROUTE PHL-SJU - DURNIG APPROACH, A BURNING ODOR WAS DETECTED IN BOTH THE CABIN AND COCKPIT. NO SMOKE WAS OBSERVED. THE AUTOPILOT DISCONNECTED AND THE GPS WAS LOST. FROM 7,000 FEET UNTIL TOUCHDOWN, NOTICED THE ODOR IN THE COCKPIT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED THE AVIONICS VENTILATION TEST. A TEST OF THE ADIRU SYSTEMS, CPC 1 AND 2 TESTS, AND A CAT 3 TEST. NO FAULTS WERE FOUND DURNG ANY OF THE TESTING. (M) 2L72 4F RTA28NM 20040430001232004043000123EU 2004 4 30 USAA040035 120040227A5320D53472209223 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND FLOOR SUPPORT CORRODED .6 INCH BY .8 INCH, 1 BLOWN HOLE AT FS 64-66 RIGHT Y1292 Z=0. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14 FIG 102, PAGE 106. (M) 2L72 4F RTA28NM 20040430001242004043000124EU 2004 4 30 USAASA04030 120040330A335032145410 PSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19121UW 1294 PHL - THE RIGHT, MID-CABIN EMERGENCY EXIT LIGHT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE RIGHT SIDE, MID CABIN POSITION. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040503000052004050300005EA 2004 5 3 ASOA04232 120040321A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE OUTBOARD FLOORBEAM ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE OUTBOARD FLOORBEAM ANGLES AT FS 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040503000072004050300007NM 2004 5 3 USAASB04040 120040330A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19371US 22950 PIT - MAINTENANCE REPORTED THE MID CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLCED THE BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040503000142004050300014NM 2004 5 3 ASAA0410115 120040308A5310654652512 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND SHEAR TIE CORRODED AT STATION 380. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000192004050300019EU 2004 5 3 USAA040038 120040227A5320D5347208900200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND FLOOR SUPPORT CORRODED .5 INCH BY .7 INCH, RIGHT CENTER FS 66-68 -Y1292 Z=0. CORROSION LEVEL 2, TASK/CARD NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14 PAGE 106, FIG 102. (M) 2L72 4F RTA28NM 20040503000282004050300028 2004 5 3 GTIA040220 420040319A2565 LANYARD DOUG DC9 DC983 3022083WP L2 DOOR SLIDE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FLL - FOUND L2 DOOR SLIDE LANYARD ROUTED INCORRECTLY. RE-ROUTED L2 DOOR SLIDE LANYARD CORRECTLY. (M) 2L72 4F RTA6WE 20040503000302004050300030EU 2004 5 3 MALA040351 120040420A214013051002 HEATER SAAB SF340 340B 7860101EU CABIN SPARKS A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL15425XJ 340B425 AUX HEAT SYSTEM - F/A NOTICED SMALL SPARKS COMING FROM FWD HEATER BOX DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED FWD HEATER ASSY. P/N OFF&ON 1305100-2, S/N OFF 4401, S/N ON 382 IAW AAR CMM. REMOVED FROM DMR, MXC NOTIFIED. 2L72 4T RTA52EU 20040503000322004050300032EU 2004 5 3 MALA040359 120040421A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED DENT AT RIGHT FUSELAGE STA 358 WL 87 IAW DSAAB 340 SRM 53-70-10 AND MESABA EO S53009. A/C RELEASE DATE 4/25/04. 2L72 4T RTA52EU 20040503000432004050300043SO 2004 5 3 C2XA04SH247 120040427A532014521699003 BUTTSTRAP EMB 135 EMB135ER 3260203SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727512 145274 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040503000482004050300048SO 2004 5 3 C2XA04BT053 120040426A2611FDS765A2 SMOKE DETECTOR EMB 135 EMB135LR 3260305SO LAVATORY FAULTY A C2XAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW2727523 145389 CREW REPORTED, LAV SMOKE WARNING AFTER TAKEOFF FROM NEWARK, CONDITION CLEARED WHEN CIRCUIT BREAKER PULLED PER QRH, WITH SMELL IN THE CABIN. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB135 AMM 26-14-01. OPS CHECKED GOOD. NO SMOKE NOTED. 2L72 4F RTT00011AT 20040503000552004050300055SO 2004 5 3 C2XA04TY072 120040428A575114569009408 BRACKET EMB 135 EMB135ER 3260203SO RT AILERON GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716511 145267 TYS - DURING A SCHEDULED 2C INSPECTION THE RT AILERON PCA ATTACH BRACKET WAS FOUND GOUGED. MAINT REMOVED AND REPLACED THE AILERON PCA BRACKET PRIMED AND PAINTED IAW SRM 51-20-03 AND EA 2710-01017. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040503000712004050300071SO 2004 5 3 C2XA04SH190 120040330A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER/SHIM REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040503000722004050300072NM 2004 5 3 CALA0400401 120040419A5320149A761115 WEB BOEING737 737824 13844BZNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 RIGHT WHEEL WELL WEB CRACKED 2 INCHES. INSTALLED NEW WEB IAW SRM 51-40-02. 2L72 4F RTA16WE 20040503000822004050300082WP 2004 5 3 AALA20040476 120040419A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW - EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS FORWARD FLIGHT STATION TO OVERWING INOPERATIVE. REPLACED BATTERY PACK AT OVERWING FOR EMERGENCY LIGHTS FROM FLIGHT ATTENDANTS FORWARD FLIGHT STATION TO OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503000872004050300087SO 2004 5 3 C2XA04CL037 120040419A32347455503 CONTROL HANDLE EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716559 145603 CLE FLIGHT 2221, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, AND DID NOT RECEIVE A LEVER DISAGREE ON THE EICAS. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR LEVER CONTROL HANDLE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040503000922004050300092SO 2004 5 3 SWIA200413114 120040302A5320 BRACKET EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07213SW 120277 LEFT COCKPIT SIDE LATERAL BRACKET IN COCKPIT IS CRACKED AT LIGHTENING HOLE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED CRACKED BRACKET AT LEFT COCKPIT FRAME 12 AFT OF DV WINDOW. INSTALLED SERVICEABLE BRACKET. 2L72 4T RTA31SO 20040503001002004050300100NM 2004 5 3 ASAA041017 120040308A5313655162812 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER 27R CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001072004050300107WP 2004 5 3 ABXA040133 120040322A532059114335 STRUCTURE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 FS 775, INBOARD OF STRINGER NR 3 LEFT AT FASTENER HOLE, 1 EA CRACK INDICATION. REPAIRED AREA IAW DC-9 SRM 53-04. 2L72 4F A6WE 20040503001082004050300108WP 2004 5 3 ABXA040131 120040315A531049179231 STOP FITTING DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 UPPER RIGHT VENTRAL DOOR STOP FITTING ON AFT PRESSURE BULKHEAD WAS CRACKED. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 20040503001102004050300110SO 2004 5 3 SWIA200413115 120040302A5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07213SW 120277 SUPPORT BRACKET UNDER PILOT WINDOW CRACKED (MARKED). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED SUPPORT BRACKET UNDER PILOT WINDOW IAW SRM 53-00-04. 2L72 4T RTA31SO 20040503001112004050300111SO 2004 5 3 SWIA200413116 120040302A5310 SHEAR TIE EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07213SW 120277 CRACK FOUND ON SHEAR CLIP ON RIGHT SIDE OF CARGO PIT WALL AT FLOOR LEVEL 2ND RIB FORWARD OF AFT BULKHEAD. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SHEAR TIE AT FRAME 46 FLOORBOARD LEVEL RIGHT SIDE PER EMB120 SRM 51-40-02. P/N: 120-04984-002. 2L72 4T RTA31SO 20040503001122004050300112SO 2004 5 3 SWIA200413117 120040317A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07234SW 120308 CABIN FLOORBOARD FRAMES HAVE CORROSION AT FRAME 38. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME AT CABIN FLOOR IAW SRM 120 51-10-02 PG 3 SEC 3.A. 2L72 4T RTA31SO 20040503001132004050300113SO 2004 5 3 SWIA200413118 120040317A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07234SW 120308 CORROSION ON LEFT FLOOR SEAT TRACK IN VARIOUS SPOTS. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FORWARD AND AFT SECTIONS OF LEFT FLOOR SEAT TRACK WITH NEW IAW EMB120 MM 53-01-05. 2L72 4T RTA31SO 20040503001142004050300114SO 2004 5 3 SWIA200413119 120040317A5230 FRAME EMB 120 EMB120ER 3260203SO CARGO DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07234SW 120308 CARGO DOOR UPPER FORWARD INBOARD FRAME CRACKED AT BACKSTOP BRACKET SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM120 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20040503001172004050300117WP 2004 5 3 AALA20040487 120040425A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FOR AFT HALF OF COACH CABIN INOPERATIVE. REPLACED FORWARD BATTERY (DME CORP P4010049) AND AFT MODULE ASSEMBLY FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FOR AFT HALF OF COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503001182004050300118 2004 5 3 AALA20040488 420040425A2565D29982125 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR FAILED A AALAK NONE O OTHER TXTAXI/GRND HDL 1 SW2114551 53033 PHL - WHEN GROUND CREW WAS PREPARING TO TOW AIRCRAFT TO THE GATE THE RIGHT 1 GALLEY DOOR WAS OPENED BY GROUND CREW FROM THE INSIDE AND THE SLIDE FELL OUT. SLIDE DEPLOYED BY ONLY PARTIALLY INFLATING. FERRIED AIRCRAFT TO DFW FOR SLIDE REPLACEMENT. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503001192004050300119NM 2004 5 3 AALA20040483 120040423A3350 PIN BOEING757 757223 1384957NM CONNECTOR BACKED OUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW21654A 24612 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24D INOPERATIVE. FOUND PIN PUSHED BACK AT CONNECTOR. RESECURED PIN FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040503001222004050300122WP 2004 5 3 AALA20040461 120040414A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21443AA 49469 DFW - EMERGENCY CEILING LIGHTS AT ROWS 18 THROUGH 20 INOPERATIVE. REPLACED CENTER BATTERY PACK AT ROW 20 FOR EMERGENCY CEILING LIGHTS ROWS 18 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503001252004050300125EU 2004 5 3 AALA20040459 120040414A3350 PIN AIRBUS300 A300B4605R 3930308EU CONNECTOR BACKED OUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170072 515 MIA - FORWARD ENTRY EMERGENCY LIGHT AT DOOR 3R INOPERATIVE. REPLACED PUSH BACK PIN AT CONNECTION FOR FORWARD ENTRY EMERGENCY LIGHT AT DOOR 3R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040503001262004050300126NM 2004 5 3 AALA20040460 120040414A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959AN 30828 SJC - MID CEILING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT LOWER RIGHT HAND SIDEWALL AT ROW 13 FOR CEILING EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040503001332004050300133NM 2004 5 3 ASAA0410094 120040229A5320654655011 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND HOLE OVERSIZED AT STATION 787. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001362004050300136NM 2004 5 3 ASAA0410100 120040302A53206551525 SPLICE BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND GOUGED AT STATION 727 AND STRINGER 24L. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001382004050300138NM 2004 5 3 ASAA0410111 120040306A53206935352 TIE CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND STRINGER TIE CLIP CORRODED AT STATION 907. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001482004050300148 2004 5 3 GTIA040224 420040319A2565 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 DTW - FLT 417 - L1 SLIDE PACK FELL FROM DOOR. REINSTALLED SAME SLIDE PACK A REQUIRED. (M) 2L72 4F RT 20040503001502004050300150 2004 5 3 GTIA040225 420040323A2565 SLIDE DOUG DC9 DC981 3022081WP L1 DOOR UNSECURE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 ACY - FLT 330 - L1 SLIDE PACK NEEDS SECURING. REINSTALLED PACK. (M) 2L72 4F A6WE 20040503001642004050300164NM 2004 5 3 ASAA0410132 120040317A53206935352 TIE CLIP BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CRACKED AT FS 747. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001712004050300171WP 2004 5 3 GTIA040174 120040310A3350 CAP DOUG DC9 DC981 3022081WP CABIN MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 DTW - FLT 1689 - FOUND SAFETY GLOW FLOOR TRACK RIGHT AT EXIT ROW 26 MISSING END CAP AND INSERT ASSEMBLY. FOUND MISSING ASSEMBLY IN CABIN RESECURED. (M) 2L72 4F A6WE 20040503001742004050300174EU 2004 5 3 ULX2004F00000 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP23223LA 3366 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U H9EU 20040503001762004050300176EU 2004 5 3 A6WA200460008 120040311A5280HC528B0039002 HINGE BRACKET BAC 146 146200A 1500266EU RT MLG DOOR BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 RIGHT MLG DOOR HINGE BROKEN MAINTENANCE REPLACED RIGHT MLG DOOR AFT HINGE BRACKET. RETRACTION CK COMPLIED WITH ON W/C. (M) 2H74 4F A49EU 20040503001852004050300185 2004 5 3 HE66094217 420040416A2212C013S611 BUTTON UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ATTITUDE CONTROLBROKEN E HEEAO OTHER O OTHER CRCRUISE 1 SW03135CR1400 0164 WHEN ACTIVATING ALT HOLD, THE LIGHT WOULD NOT IGNITE CONFIRMING ALT HOLD WAS ENGAGED. 1G72 3U3 U H88EU E34NE 20040503002052004050300205SW 2004 5 3 YTRR094256 120040424A6330 BUSHING BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL MOUNT WORN B YTRAK NONE O OTHER ININSP/MAINT 1 SW03521921028 52192 WORN BUSHING ON RESTRAINT MOUNT AT LATERAL SPRING ATTACH POINT. 1G71 3U3 UNCH2SW E1GL 20040503002132004050300213EU 2004 5 3 BAQA093191 120040407A291011745020V002 MODULE BOLKMS117 BK117B1 5626012EU HYDRAULIC SYS LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME6420 7235 UNIT LEAKING HYRO FLUID. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/23/2004 1G72 3U H13EU 20040503002142004050300214EA 2004 5 3 A6WA200440031 120040313A2710 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A A6WAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 GL31437AW 7744 ABORTED TAKEOFF DUE TO AILERON MISCONFIGURATION WARNING MESSAGE ABOVE 80 KNOTS. BTMS READINGS 03, 03, 04, 06 REPORTED WEIGHT 52,000 LBS. COMPLIED WITH SPECIAL INSPECTION PROCEDURE IAW 5-51-27, ABORTED TAKEOFF. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRES. OPS CHECKED ANTI-SKID, PROX SENSOR, FLT CONTROLS, BRAKES, TRIM SYSTEM. OPS CHECK GOOD. INTERROGATED MDC, NO FAULTS. AIRCRAFT RETURN TO SERVICE. (M) 2L72 4F RTA21EA 20040503002252004050300225EU 2004 5 3 ULX2004F00003 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP23228LA808 3316 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U3 U H9EU E19EU 20040503002272004050300227NM 2004 5 3 ASAA0410113 120040306A532065465601 TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CORRODED AT STATION 947 AND STRINGER 18R. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002282004050300228EU 2004 5 3 BAQA094250 120040422A243523032048 STARTER GEN BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03955ME 7243 STARTER GEN WILL NOT CRANK. REPLACED WITH SERVICEABLE UNIT. 1G72 3U3 U H13EU E5NE 20040503002312004050300231NM 2004 5 3 ASAA0410098 120040301A5320654655112 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 22L AND STATION 807. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002342004050300234EU 2004 5 3 BAQA093775 120040224A6220E1T302301A FREQ ADAPTER AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR CRACKED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03365KY1330 6529 UNITS CRACKED BEYOND LIMITS. REPLACED WITH SERVICABLE ASSET UNIT. 03/17/2004 1G72 3U3 U H10EU E19EU 20040503002352004050300235NM 2004 5 3 ASAA0410097 120040301A5320654654912 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 21L AND STATION 767. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002382004050300238NM 2004 5 3 ASAA0410133 120040317A532065465578 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLE OVERSIZED AT SHEAR TIE AT STATION 887. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002392004050300239NM 2004 5 3 ASAA0410138 120040317A531565498851 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT CABIN FLOORBEAM UPPER T-CHORD CORRODED AT STATION 986.5. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002442004050300244NM 2004 5 3 ASAA0410135 120040317A532069353523 TIE CLIP BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CRACKED TIE CLIP AT STATION 727B. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002542004050300254WP 2004 5 3 GTIA040227 120040219A5330 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND LEFT ALTERNATE STATIC PORT INTERNAL DOUBLER CORRODED. REMOVED INTERNAL DOUBLER. LOCATED AND DRILLED NEW DOUBLER. INSTALLED INTERNAL DOUBLER. (M) 2L72 4F A6WE 20040503002552004050300255NM 2004 5 3 ASAA0410136 120040317A53116546532 FRAME BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT FRAME 494 GOUGED BETWEEN STRINGER 18 AND 19. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002572004050300257NM 2004 5 3 ASAA0410143 120040317A5320654681215 INTERCOSTAL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND INTERCOSTAL ASSEMBLY L ANGLE IS CORRODED AT FS 1016. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002582004050300258NM 2004 5 3 ASAA0410124 120040317A53156546548504 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC DURING MAINTENANCE, FOUND AFT PIT CABIN FLOORBEAM T-CHORD CORRODED AT FS 747. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002592004050300259NM 2004 5 3 ASAA0410125 120040317A531165465641 FRAME BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FRAME OVERSIZED HOLES AND CORROSION AT STATION 986. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040430000102004043000010SO 2004 4 30 C2XA04TY075 120040428A3260852701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214SO NLG CRACKED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2711107 145654 TYS FLIGHT 2797, AFTER TAKEOFF THE NOSE GEAR DOORS REMAINED OPEN. A/C WAS FERRIED TO TYS WHERE MAINT REMOVED AND REPLACED THE NLG SEQUENCE SWITCH IAW EMB 145XR MM 32-63-03. OPS CHECK GOOD. A/C RELEASED TO REVENUE SERVICE. 2L72 4F RT 20040430000122004043000012WP 2004 4 30 AALA20040495 120040427A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21278AA 49294 DEN - EMERGENCY LIGHT OVER RIGHT WING ILLUMINATED DURING FLIGHT. REPLACED BATTERY PACK FOR RIGHT HAND OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000132004043000013WP 2004 4 30 AALA20040493 120040427A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21291AA 49303 IAD - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 20 BACK TO REAR OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACKS FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 20 TO REAR OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000142004043000014NM 2004 4 30 AALA20040494 120040427A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 LAX - AISLE PATH EMERGENCY LIGHT AT SEAT ROWS 31H THROUGH 40H INOPERATIVE. REPLACED BATTERY PACK AT SEAT 39HJ FOR AISLE PATH EMERGENCY LIGHTS AT SEAT ROWS 31H THROUGH 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000172004043000017NM 2004 4 30 ASMF200403014 120040316A3260833605 PROXIMITY SWITCH DOUG MD80 MD83 3023681NM NLG FAILED W ASMFO OTHER J WARNING INDICATION CLCLIMB 1 SW23831LF475462768 53050 DURING CLIMB AND CRUISE AT SEVERAL TIMES RUDDER TRAVEL UNRESTRICTED LIGHT TURNED ON, FLASHING MODE ALL THE FLIGHT. CHECKED BY LEAK AND ADJUSTED RUDDER THROW LIMITER IAW MM 27-20-00. PROXIMITY SWITCH WAS REPLACED IAW MM 32-60-04, TEST CORRECT. 2L72 4F RT 20040430000202004043000020WP 2004 4 30 ASMF200404001 120040401A7620LG8OE1 COMPUTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE ENGINE FAILED W ASMFCD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW23214AM1383 49585 718205 AIRCRAFT SUSPENDED TAKE OF AT 100 KTS AND RETURNED TO PLATFORM AS A CONSEQUENCE OF THE RIGHT ENGINE DID NOT REACH THE TAKE OF THRUST, IT ONLY REACHED 1.6 OF EPR. AT MEX PLATFORM, TECHNICAL PERSONNEL PERFORMED AN ACCELERATION TEST REACHING ONLY 1.7 OF EPR'S. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE RIGHT ENGINE EPR'S COMPUTER ASSY WAS REPLACED IN ACCORDANCE WITH MM 77-11-02. ENGINE RUN TEST WAS PERFORMED IN ACCORDANCE WITH MM 72-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040430000362004043000036NM 2004 4 30 ASMF200404005 120040406A7711 HOSE DOUG MD88 MD88 3023688NM LT ENG PT2 DAMAGED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23168PL 53174 DURING TRANSIT CHECK CAPTAIN REPORTED A DIFFERENCE OF 0.09 BETWEEN EPR´S, BEING LEFT BIGGER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE LEFT ENGINE PT2 HOSE WAS REPLACED AND CHECKED BY LEAKS IAW MM 77-11-01, TEST CORRECT. 2L72 4F RTA6WE 20040430000432004043000043EU 2004 4 30 AALA20040443 120040409A3350 COVER FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW211403M 11354 ORD - FIRST CLASS EMERGENCY TRACK LIGHTING IS BROKEN. REPAIRED LIGHT STRIP AND REPLACED COVER AT AFT END OF FIRST CLASS FOR EMERGENCY TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040430000452004043000045NM 2004 4 30 AALA20040445 120040409A3397 PIN BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 ORD - EMERGENCY ESCAPE PATH LIGHT AT SEAT 40B INOPERATIVE. PLACARD PER MEL 33-16D AUTHORIZATION 4-197-C. FOUND PUSHED PIN ON EMERGENCY ESCAPE PATH LIGHT SYSTEM. REPAIRED PIN FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT SEAT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000532004043000053 2004 4 30 AALA20040450 420040412A256529985103 SLIDE DOUG DC9 DC982 3022082WP GALLEY DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21457AA 49562 DFW - AFT LEFT HAND GALLEY DOOR IN ARMED POSITION AND WHEN DOOR OPENED BY CABIN SERVICES SLIDE PARTIALLY DEPLOYED AND CAME OUT OF SLIDE CASE BUT DID NOT INFLATE. REPLACED SLIDE FOR AFT LEFT HAND GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000622004043000062EA 2004 4 30 VNAA0404003 120040401A2612 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE OUT OF POSITION A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07229PS 7898 DURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. MAINTENANCE WAS DISPATCHED FROM DAY TO CLE. MAINTENANCE THEN INSPECTED AND FOUND THE LEFT HAND FIRE LOOP PUSHED DOWN ON THE BLEED DUCT. MAINTENANCE RELOCATED THE FIRE LOOP AWAY FROM THE DUCT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040430000732004043000073WP 2004 4 30 AALA20040490 120040426A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21207AA 49158 ORD - EMERGENCY LIGHTS AT TAIL CONE OVERHEAD CATWALK INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT TAIL CONE OVERHEAD CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000752004043000075WP 2004 4 30 AALA20040434 120040406A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2133414 49325 DFW - EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY WALL INOPERATIVE. REPAIRED WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT FORWARD GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040430000792004043000079EU 2004 4 30 AALA20040469 120040415A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 MIA - EMERGENCY FLOOD LIGHT AT BULKHEAD FORWARD OF SEAT 1G IS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY 110WL2 FOR EMERGENCY FLOOD LIGHT AT BULKHEAD FORWARD OF SEAT 1G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040430000842004043000084 2004 4 30 AALA20040466 420040414A22114040800912 COMPUTER BOEING767 767223 1385123NM AUTOPILOT INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21328AA 22328 LAX - INFLIGHT T032 RETURNED TO LAX DUE TO AILERON LOCKOUT, RUDDER RATIO EICAS MESSAGE AND ALL THREE AUTOPILOTS INOPERATIVE. LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED LEFT AND RIGHT HAND AIR DATA COMPUTERS (4040800912 FROM HONEYWELL), LEFT AND RIGHT HAND STABILIZER TRIM, AILERON MODULE (285T0015117MODD FROM BOEING) AND AUTOPILOT MODE CONTROL PANEL (8221492102 FROM ROCKWELL COLLINS). SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000872004043000087NM 2004 4 30 VNAA0403015 120040326A2120 SMOKE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT DETECTED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL07430JS 3044 THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM AND HX FANS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040430001022004043000102NM 2004 4 30 AALA20040479 120040420A3350 LIGHT BOEING757 757223 1384957NM ROW 25DEF INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21692AA 26972 JFK - EMERGENCY ESCAPE PATH LIGHTING AT ROW 25DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY ESCAPE PATH LIGHTING AT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040430001042004043000104EU 2004 4 30 AALA20040478 120040417A27207345003 COMPUTER AIRBUS300 A300B4605R 3930308EU FEEL LIMITER INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2114061 471 SJU - INFLIGHT T661 ON CLIMB FLIGHT RECEIVED A DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. NO EMERGENCY AND NOT OVERWEIGHT. REPLACED NUMBER 1 FEEL LIMITER COMPUTER AND RESET NUMBER 2 COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. SECOND AIR INTERRUPT ON DEPARTURE FOR DUAL RUDDER LIMITER FAULT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBERS 1 AND 2 FEEL LIMITER COMPUTERS AND RELAYS AND VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040430001082004043000108EA 2004 4 30 ASOA04237 120040321A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11824AS 7203 FLT 4586 - DURING APPROACH INTO LIT FROM DFW, THE CRWE RECEIVED A FLAPS FAIL MASTER WARNING WHEN THEY SELECTED THE FLAPS TO EIGHT DEGREES. THE QRH WAS COMPLIED WITH THE CREW REQUESTED EMERGENCY EQUIPMENT TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN LIT. MAINTENANCE RESET THE FLAP SYSTEM IAW AD98-20-01 AND ASA EO 600-27-0004. SYSTEM RESET AND OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040430001102004043000110EA 2004 4 30 ASOA04227 120040321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE FORWARD INBOARD CORNER LEADING TO THE NUTPLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20040430001112004043000111EU 2004 4 30 USAASA04032 120040331A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19752US 1319 BOS - THE LEFT EMERGENCY LIGHT POWER SUPPLY FAULTED DURING TEST. MAINTENANCE REPLACED THE LEFT, MID CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040430001142004043000114EU 2004 4 30 USAA040042 120040228A5321D536106250000 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW14308 0949 BFM - FOUND FLOOR PANEL 222EF CRACKED 1 INCH, FRAME 16-20 EDGE OF TOP SURFACE. FABRICATED NEW FLOOR PANEL PER SAMPLE PER SRM 53-002-00. (M) 2L72 4F RTA28NM 20040430001252004043000125EA 2004 4 30 ASOA04230 120040321A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL IAW SRM 51-40. (M) 2L72 4F RTA21EA 20040503000012004050300001NM 2004 5 3 GAIA04067ST 120040326A551065224008 FITTING BOEING727 727223 1384074NM HORIZ STAB CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, THE HORIZONTAL STABILIZER FRONT SPAR GIMBAL A FRAME RIGHT UPPER FORWARD AND AFT CLEVIS HOLES WERE FOUND CRACKED. REMOVED AND REPLACED A FRAME GIMBAL SUPPORT IAW BOEING 727 AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503000032004050300003EA 2004 5 3 ASOA04228 120040321A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE FRAME FS 718, STRINGERS 10-12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING FRAME FS 718, STRINGERS 10-12 ON THE RIGHT SIDE IAW ASA EO 600-53-0067A. (M) 2L72 4F RTA21EA 20040503000062004050300006EA 2004 5 3 ASOA04231 120040321A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE RACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-40. (M) 2L72 4F RTA21EA 20040503000102004050300010NM 2004 5 3 USAASB0402 120040331A3350110049 POWER SUPPLY BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19527AU 23862 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 5 THROUGH 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT POWER SUPPLY. OPS CHECK OF EMERGENCY LIGHTS GOOD. (M) 2L72 4F RTA16WE 20040503000112004050300011NM 2004 5 3 ASAA0410118 120040317A53306545778 SKIN BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND 4 INCH CREASE IN SKIN BELOW RIVET AT BS 1000. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000122004050300012EU 2004 5 3 USAA040037 120040227A5310D5347219020400 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19707UW 0949 BFM - FOUND BEAM CORRODED 1.2 INCH BY .9 INCH, 3 BLOWN OUT, CENTER LEFT FS 66-68, +Y 1292, Z=0. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-14, PAGE 106, FIG 102. (M) 2L72 4F RTA28NM 20040503000272004050300027WP 2004 5 3 ASAA0480162 120040306A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 SEA - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 10. RECONNECTED CONNECTOR WIRE. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20040503000292004050300029EU 2004 5 3 MALA040352 120040407A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15507XJ E2316 BATTERY PACK P/N 61-2275-1, S/N 9902954 REMOVED FOR SCHEDULED CAPACITY CHECK, UNIT FAILED CAP CHECK ON 4/7/04. UNIT WAS RECHARGED AND CAP CHECK PASSED. UNIT RE-CHARGED AND RETURNED TO SERVICE ON 4/14/04. 2H74 4F RTA49EU 20040503000392004050300039EU 2004 5 3 MALA040340 120040421A3520 OXYGEN MASK BAC 146 AVRO146RJ85A1500097EU CABIN DEPLOYED A MALAG O2 MASK DEPLOYED O OTHER NRNOT REPORTED 1 GL15525XJ E2350 OXYGEN MASK DEPLOYED IN FLIGHT. OXYGEN AND PRESSURIZATION ALL NORMAL. MAINTENANCE STOWED PAX 02 MASKS IAW JOB CARD 0501. 2H74 4F RTA49EU 20040503000442004050300044SO 2004 5 3 C2XA04SH250 120040427A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712564 145618 SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040503000492004050300049SO 2004 5 3 C2XA04BT054 120040427A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714573 145638 CREW REPORTED EMERGENCY LIGHTS FLASHING ON AND OFF DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS IAW EMB145 MM 33-50-04, OPS CHECKED GOOD IAW EMB 145 33-50-00. PART NUMBER: 2013-1A, SERIAL NUMBERS: 81656, 84256, 73652, AND 84568. 2L72 4T RTT00011AT 20040503000642004050300064WP 2004 5 3 GTIA040176 120040217A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND CABIN STATION 522-560 STRINGER 18L FLOOR WEB CORRODED. FLOOR WEB AT STATION 527 IS OUT OF LIMITS. REMOVED DAMAGE AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20040503000652004050300065NM 2004 5 3 CALA0400400 120040419A5320BAC1496377 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 FWD CARGO RIGHT INTERCOSTAL IN FLOOR AREA STA 500D TO 500E CRACKED. REPLACED INTERCOSTAL IAW SRM 51-20-01 AND 51-40-02. 2L72 4F RTA16WE 20040503000662004050300066WP 2004 5 3 GTIA040177 120040213A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP COCKPIT WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND COCKPIT FLOOR PANEL 4411A BOTTOM DISBONDED NON-SKID WORN. FOUND BOTTOM SKIN CRACKED. REMVOED BOTTOM SKIN. FABRICATED NEW BOTTOM SKIN. INSTALLED BOTTOM SKIN. (M) 2L72 4F RTA6WE 20040503000672004050300067WP 2004 5 3 ASAA0480080 120040220A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 SJD - PREFLIGHT CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. RESEATED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040503000682004050300068NM 2004 5 3 ASAA0410035 120040116A335086210144 BATTERY BOEING737 737298C 1384490NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REPLACED REMOTE ASSEMBLY BATTERY, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040503000742004050300074NM 2004 5 3 CALA0400403 120040419A572065C8073530 HINGE FITTING BOEING737 7373T0 1384582NM RT WING BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2718350 23588 RT WING DOOR LWR HINGE FITTING IS BROKEN AT NR 6 FLAP TRACK. REPLACED DOOR HINGE IAW SRM 51-40-02. 2L72 4F RTA16WE 20040503000852004050300085SO 2004 5 3 C2XA04IA041 120040328A32608005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214SO MLG OUT OF ADJUST A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2713123 145688 DURING CLIMB THE CREW REPORTED THAT THE LANDING AIR/GROUND FAIL MESSAGE ILLUMINATED AND THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE ADJUSTED THE MAIN LANDING GEAR PROXIMITY SWITCHES. THE GEAR WAS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4F RT 20040503000882004050300088SO 2004 5 3 SWIA200413110 120040403A3397 WIRE EMB 120 EMB120ER 3260203SO CABIN CHAFED A SWIAO OTHER O OTHER CRCRUISE 1 NM07189SW 120048 EMERGENCY LIGHTS FLICKERED ON AND OFF DURING FLIGHT. FOUND CHAFED WIRE AT FIRST TRACK LIGHTING. REPAIRED AS REQUIRED. OPS CHECK GOOD. 2L72 4T RTA31SO 20040503002072004050300207SW 2004 5 3 ALGA094222 120040421A6220406310405101 UNIVERSAL BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03697AL534 53374 FOUND EXCESSIVE AXIAL PLAY. REMOVED AND REPLACED WITH NEW PART IN FIELD. 1G71 3U3 UO H2SW E1GL 20040503002122004050300212EU 2004 5 3 BAQA093768 120040331A6720 BEARING BOLKMS117 BK117B1 5626012EU WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME1411 7235 BEARINGS PREMATURELY WORN. REPLACED WITH SERVICABLE UNIT FROM AEC, 04/23/2004 1G72 3U H13EU 20040503002232004050300223NM 2004 5 3 ASAA0410114 120040306A53136552928607 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER 27R CORRODED AT STATION 986. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002362004050300236EU 2004 5 3 BAQA091939 120040112A7900365A32276002 SIGHT GAUGE AEROSPAS365 AS365N2 8680815EU ENGINE OIL DIRTY E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03915ME 6417 SIGHT IS UNREADABLE, NEEDS CLEANING. REPLACED WITH SERVICABLE UNIT. 1G72 3U RTH10EU 20040503002372004050300237NM 2004 5 3 ASAA0410130 120040317A5340693535219 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CORRODED AT STRINGER 967. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002472004050300247NM 2004 5 3 ASAA0410129 120040317A531565549054 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT CEILING FLOORBEAM AT STATION 460 CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002602004050300260NM 2004 5 3 ASAA0410126 120040317A53156568940 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON T-CHORD AT STATION 1115-1125. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002652004050300265NM 2004 5 3 ASAA0410142 120040317A53136552928604 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER CORRODED AT STATION 946. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002662004050300266CE 2004 5 3 N4J2004F00006 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE T/R ACTUATOR CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15601GG1187 192 RT IB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2L72 4F4 FRTA10CE E35NE 20040503002672004050300267NM 2004 5 3 ASAA0410127 120040317A53136552928604 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER 27L CORRODED AT FS 946-950. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002682004050300268NM 2004 5 3 ASAA0410145 120040317A534765549694 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORRODED SEAT TRACK FLANGE AT FS 727B. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002692004050300269NM 2004 5 3 ASAA0410140 120040317A534765549698 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK CORROSION AT STATION 847. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002722004050300272NM 2004 5 3 ASAA0410156 120040323A5754655553615 SKIN BOEING737 737290C 138448VNM L/E SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE CHECK, FOUND NR 2 SLAT UPPER TRAILING EDGE SKIN DENTED AT TRACK AREA WING STATION 505. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002742004050300274SW 2004 5 3 ALGA094108 120040412A6510407340339107 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL T/R DRIVE DEFECTIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL403 53240 HBMV FAULT LIGHT NR 2 BEARING (AFT) REMOVED AND REPLACED WITH NEW PART. 1G71 3U3 UO H2SW E1GL 20040503002792004050300279NM 2004 5 3 ASAA0410120 120040317A533065457787 SKIN BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND GOUGE AND DENT BELOW RIGHT STAB ICE LIGHT AT STATION 964. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002842004050300284EA 2004 5 3 WVE2004F00004 120040420A5514601R5531002 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HORIZ STAB LACK OF LUBE B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09408SW 7055 LT VERTICAL STABILIZER PIVOT FITTING FOR THE HORIZONTAL STABILIZER HAS BUSHING (PN 601R55310025) MIGRATED AT WL 235.00, LBL 4.10. PROBABLE CAUSE: PIVOT PIN LUBRICATION NOT ADEQUATE. (EA09200401997) 2L72 4F4 FRTA21EA E15NE 20040503002852004050300285EA 2004 5 3 WVE2004F00008 120040419A5320601R311719 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERK NONE O OTHER NRNOT REPORTED 1 EA09408SW 7055 FS 484 WATERLINE 73 RBL 27 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS 2L72 4F4 FRTA21EA E15NE 20040503002862004050300286WP 2004 5 3 GTIA040208 120040317A1430 SCREW DOUG DC9 DC983 3022083WP COCKPIT LOOSE A GTIAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23831NK 49617 FLL - FLT 1123 - WHEN SELECTING L WING LIGHT ON DURING APPROACH CHECKLIST SMOKE AND SPARKS SHOT OUT FROM UNDER GLARE SHIELD. TIGHTENED SCREW ON L WING SWITCH THAT WAS LOOSE, OPS CHECKED NORMAL. (M) 2L72 4F RTA6WE 20040503002882004050300288WP 2004 5 3 GTIA040210 120040318A2560 LANYARD DOUG DC9 DC981 3022081WP R1 DOOR DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 LGA - FLT 703 - FOUND DOOR R1 SLIDE LANYARD CABLES NOT ATTACHED. ATTACHED CABLE TO GIRT BAR. (M) 2L72 4F A6WE 20040503002892004050300289WP 2004 5 3 GTIA040211 120040219A2560 HOOK DOUG DC9 DC982 3022082WP L2 DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND L2 DOOR HAS SEVERAL CRACKS AT SLIDE COVER AND LINER/GIRT BAR HOOK IS BROKEN. INSTALLED NEW GIRT BAR HOOK. (M) 2L72 4F A6WE 20040503002902004050300290WP 2004 5 3 GTIA040239 120040327A2560 CABLE DOUG DC9 DC983 3022083WP L2 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FLL - FLT 679 - FOUND L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE MISPOSITIONED. INST CABLE ON GIRT BAR. (M) 2L72 4F RTA6WE 20040503002922004050300292WP 2004 5 3 GTIA040233 120040218A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK RBL 24 INCHES STATION 200 TO 256 HAS CORROSION. REMOVED SEAT TRACK STATION 200 TO 265. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F RTA6WE 20040503002952004050300295WP 2004 5 3 GTIA040235 120040308A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND DENT ON SKIN AT FS 427 LONGERON 21L. CUTOUT DAMAGE. UPON FURTHER EVALUATION FOUND HIDDEN DAMAGE ON LONGERON 21. FABRICATED REPAIR FILLER. FABRICATED AND DRILLED REPAIR DOUBLERS. FABRICATED LONGERON. FABRICATED SPLICE. INSTALLED REPAIR PARTS, FILLER, DOUBLERS, LONGERON AND SPLICE. (M) 2L72 4F RTA6WE 20040503002962004050300296WP 2004 5 3 GTIA040232 120040312A5320 WEB DOUG DC9 DC982 3022082WP RT MLG CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND RIGHT MLG AFT SUPPORT WEB CORRODED AT INBOARD SIDE. FABRICATED PLATE. FABRICATED 4 EACH L ANGLES AND 4 EACH BRACKETS. INSTALLED RIVETS IN REPAIR PARTS. (M) 2L72 4F A6WE 20040503002972004050300297WP 2004 5 3 GTIA040234 120040311A5753 SKIN DOUG DC9 DC983 3022083WP T/E FLAP DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND LEFT OUTBOARD FLAP UPPER SKIN DAMAGED. REMOVED DAMAGED UPPER SKIN AND DOUBLER. FABRICATED NEW SKIN AND DOUBLER. INSTALLED NEW SKIN AND DOUBLER. (M) 2L72 4F RTA6WE 20040503002982004050300298WP 2004 5 3 GTIA040241 120040321A324250078981 BRAKE DOUG DC9 DC983 3022083WP NR 1 MLG WORN A GTIAK NONE E VIBRATION/BUFFET NRNOT REPORTED 1 GL23831NK 49617 ACY - FLT 1296 - AT SLOW SPEEDS BRAKING IS VERY ROUGH VIBRATION CHALTER. FOUND NR 1 MAIN GEAR WHEEL BRAKES WORN BEYOND LIMITS. REMOVED AND REPLACED MAIN GEAR WHEEL BRAKES NR 1. LEAK CHECKED NORMAL. (M) 2L72 4F RTA6WE 20040503002992004050300299NM 2004 5 3 GAIA04063ST 120040326A5320 ANGLE BOEING727 727223 1384074NM AFT AIRSTAIRS CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND A Z-ANGLE CRACKED ON THE AFT AIRSTAIR TORQUE BOX FS 1273 RBL 20. INSTALLED Z-ANGLE REPAIR IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503003002004050300300NM 2004 5 3 GAIA04060ST 120040326A5315 FLOORBEAM BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND CORROSION ON THE FLOORBEAM AT FS 1130 RIGHT SIDE LOWER CHORD. INSTALLED REPAIR IAW BOEING 727 SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503003012004050300301NM 2004 5 3 GAIA04059ST 120040326A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND CORROSION ON THE STRINGER JUST FORWARD OF FS 294.5 RIGHT SIDE FORWARD OF E/E AND NOSE WHEEL WELL. INSTALLED REPAIR IAW BOEING 727 SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503003022004050300302WP 2004 5 3 GTIA040242 120040327A323459164605509 CONTROL VALVE DOUG DC9 DC982 3022082WP MLG DEFECTIVE A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23801NK 48048 AFTER TAKEOFF RIGHT RED GEAR LIGHT STAYED ON. AMBER DOOR LIGHT WAS OUT, A/C PRESS NORMAL QRH PROCEDURE AFTER APPROX 10 MINUTES GEAR DOOR OPEN LIGHT CAME ON REF QRH. CABIN PRESS STILL NORMAL AFTER 20 MINUTES DOOR LIGHT OUT AT 1200 FT AND 260 KNOTS RED GEAR LIGHT WENT OUT. REMOVED AND REPLACED MAIN LANDING GEAR CONTROL VALVE. PERFORMED OPS AND LEAK CHECK, OPS AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 20040503003042004050300304NM 2004 5 3 GAIA04064ST 120040326A5320 ANGLE BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND AN ANGLE CRACKED ON A PREVIOUS REPAIR TO THE AFT AIRSTAIR TORQUE BOX FS 1273 RBL 20. INSTALLED L ANGLE REPAIR IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503003072004050300307SO 2004 5 3 SIMA200408603 120040325A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO E/E BAY MALFUNCTIONED A SIMAK NONE J WARNING INDICATION LDLANDING 1 SW21805AE 145489 DFW - FLT 3574 - DURING LANDING ROLL CREW RECEIVED PITCH TRIM 1/2 INOPERATIVE MESSAGE AFTER A/P DISCONNECT. NO PROBLEMS WITH A/P SWITCH BEING STUCK. CREW DID NOT RESET C/B'S. MAINTENANCE REMOVED AND REPLACED THE HORIZ STABILIZER CONTROL UNIT IAW EMB MM AFTER COMPLYING WITH ETN EB-27-022. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040503003082004050300308NM 2004 5 3 GAIA04057ST 120040326A5210 SKIN BOEING727 727223 1384074NM R1 DOOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND CRACK ON THE FORWARD LOWER CORNER OF THE R1 DOOR SKIN. INSTALLED FILLER AND DOUBLER REPAIR IAW BOEING 727 SRM 52-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503003092004050300309SO 2004 5 3 SIMA200409101 120040329A27403621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO E/E BAY MALFUNCTIONED A SIMAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW21733KR 145368 LGA- FLT 4877 - DURING CLIMB CREW REPORTED PITCH TRIM 1/2 FAILURE WHEN CLIMBING THROUGH 160 KTS. TRIM WORKED THROUGH 2 UNITS FROM +8 TO +6 BEFORE FAILING. REGAINED TRIM AFTER PULLING AND RESETTING CIRCUIT BREAKER. MAINTENANCE COMPLIED WITH ETN EB-27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040503003102004050300310WP 2004 5 3 GTIA040216 120040218A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND MAIN CABIN SEAT TRACK LBL 24 INCHES STATION 1307 TO STATION 1130 HAS CORROSION. REMOVED SEAT TRACK SECTION STATION 1068-1307. FABRICATED NEW SEAT TRACK. FABRICATED NEW SEAT TRACK. FABRICATED SPLICE SECTION REPAIR STATION 1140 AND 1260. INSTALLED SEAT TRACK AND SPLICE. (M) 2L72 4F RTA6WE 20040503003122004050300312WP 2004 5 3 GTIA040229 120040130A5320 ANGLE DOUG DC9 DC983 3022083WP LT MLG WW CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND LEFT MLG W/W FORWARD OUTBOARD EDGE OF DOOR CUTOUT HAS 1 CRACKED ANGLE. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED ANGLE. (M) 2L72 4F RTA6WE 20040503003142004050300314WP 2004 5 3 GTIA040237 120040326A261259585701 FIRE LOOP DOUG DC9 DC982 3022082WP LT ENGINE FAULTY A GTIAO OTHER N FALSE WARNING APAPPROACH 1 GL23803NK 48087 DTW - FLT 631 - ON FINAL INTO TPA, NR 1 ENGINE A-LOOP FLICKERED WITH NO ASSOCIATED WARNING EXCEPT M-CAUTION FLICKERED ONCE FOR 2 SECONDS, SELECTED B-LOOP AND EXECUTED TEST. TEST WAS NORMAL. REMOVED AND REPLACED LEFT ENGINE FIRE LOOP. (M) 2L72 4F A6WE 20040503003152004050300315WP 2004 5 3 GTIA040212 120040224A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND MIDPIT LONGERON 30 CORRODED AT FS 664 AROUND FASTENER HOLE. REMOVED LONGERON SECTION L30 FROM STATION 585-665. FABRICATED LONGERON. LONGERON REPAIR PER SPIRIT EA 5310-0403. INSTALLED LONGERON, INSTALLED SPLICE AT STATION 665. (M) 2L72 4F A6WE 20040503003162004050300316WP 2004 5 3 GTIA040214 120040309A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND SEAT TRACK FLANGE CORRODED AT STATION 1251 LBL 44. REMOVED SEAT TRACK AT STATION 1231-1301. LOCATED AND DRILLED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F RTA6WE 20040503003192004050300319NM 2004 5 3 ASAA0410106 120040306A53206935352 TIE CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CORRODED AT FS 967. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503003212004050300321NM 2004 5 3 ASAA0410104 120040306A532065515254 SPLICE BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER END SPLICE GOUGED AT STATION 727. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503003222004050300322WP 2004 5 3 GTIA040248 120040110A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND MAIN CABIN STATION 256 TO 875 RBL 22 INCHES INBOARD SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORROSION, BARE METAL. AFTER FURTHER INSPECTION DISCOVERED SEAT TRACK RBL 22 INCHES INBOARD STATION 693 CRACKED. MATERIAL LOSS WITHIN LIMITS FOR SEAT TRACK RBL 22 INCHES INBOARD STATION 465-692 AND STATION 798-875. CUT DAMAGE AREA SEAT TRACK RBL 22 INBOARD STATION 665 TO 798. LOCATED AND DRILLED SEAT TRACK STATION 665-798 AND SPLICES. INSTALLED SEAT TRACK STATION 665 TO 798 RBL 22 AND SPLICES TWO EACH. (M) 2L72 4F RTA6WE 20040504000052004050400005EU 2004 5 4 BAQA093969 120040329A672076CF8716 CABLE UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE BALL BEARING CONDISCONNECTED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MF400 0281 WARRANTY. CABLE UNWEDGED FROM AFT CABLE. REPLACED WITH SERVICABLE UNIT. 04/07/2004 1G72 3U3 U H88EU E34NE 20040504000192004050400019NM 2004 5 4 QXEA200400262 120040411A561080260008 WINDSHIELD BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CRACKED A QXEAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 NM09407QX4924 113 4049 FLIGHT DIVERTED INTO GEG WHEN THE FIRST OFFICERS WINDSHIELD CRACKED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT WINDSHIELD. OPERATIONAL AND LEAK CHECKS WERE PERFOMED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040504000222004050400022NM 2004 5 4 ASAA20041 120040120A3350 LIGHT BOEING737 7372X6C 1384552NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 SEA - DURING INSPECTION FOUND MID CABIN OVERHEAD EXIT SIGN INOPERATIVE AND FLOOR TRACK LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. REPLACED MID CABIN OVERHEAD SIGN BATTERY P/N 86210144 PACK AND TRACK LIGHTING CONTROL MODULE P/N 873203041 THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040504000242004050400024NM 2004 5 4 ASAA20042 120040119A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 8 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040504000252004050400025EA 2004 5 4 ASOA04236 120040321A5320 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE RIGHT SIDE FS 640 DOUBLER AT STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT SIDE FS 640 DOUBLER AT STRINGER 9 IAW ASA EO 600-53-0075. (M) 2L72 4F RTA21EA 20040504000282004050400028WP 2004 5 4 GTIA040246 120040111A55235930497402 SKIN DOUG DC9 DC983 3022083WP RT ELEVATOR TAB DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB DENTED ON BOTH SIDES NUMEROUS PLACES. REMOVED RIGHT ELEVATOR ANTI-FLOAT TAB. INSTALLED RIGHT ELEVATOR ANTI-FLOAT TAB. (M) 2L72 4F RTA6WE 20040504000292004050400029WP 2004 5 4 GTIA040247 120040225A33500105611001 LIGHT DOUG DC9 DC983 3022083WP AFT AIRSTAIRS BROKEN A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND AFT AIRSTAIRS EMERGENCY LIGHTS SEVERAL LIGHTS NOT WORKING. REMOVED BROKEN AFT AIRSTAIR EMERGENCY LIGHT. INSTALLED NEW LIGHT ASSEMBLY. (M) 2L72 4F RTA6WE 20040504000312004050400031WP 2004 5 4 GTIA040219 120040323A3260833703 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP LT MLG FAULTY A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23801NK 48048 FTW - FOUND DOOR MLG LIGHT CAME ON DURING CLIMB FOR APPROX 2 MINUTES STAYED OFF THE REST OF FLIGHT. FOUND LEFT MAIN GEAR DOOR PROX SWITCH D1-30. REMOVED AND REPLACED LEFT MAIN GEAR OPEN PROX SWITCH, OPS CHECK GOOD. (M) 2L72 4F A6WE 20040504000322004050400032 2004 5 4 GTIA040243 420040326A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 LGA - FLT 1174 - L1 DOOR SLIDE PACK FELL OFF OF DOOR WHEN DOOR WAS CLOSED. REINSTALLED FORWARD CABIN DOOR SLIDE ASSEMBLY AND COVER. (M) 2L72 4F A6WE 20040504000352004050400035NM 2004 5 4 ASAA0410122 120040317A53106554956506 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND SHEAR TIE AT FS 520 CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000362004050400036NM 2004 5 4 ASAA0410148 120040323A53206545768 DOUBLER BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND INTERNAL DOUBLER AT FS 375 AND STRINGER 14R REQUIRES REPAIR REWORK. REPAIR IAW EA. (M) 2L72 4F A16WE 20040504000412004050400041NM 2004 5 4 ASAA0410157 120040323A5210654587139 SKIN BOEING737 737290C 138448VNM R1 DOOR CRACKED A K NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 DURING MAINTENANCE, FOUND R-1 DOOR INTERIOR SKIN CRACKED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000442004050400044NM 2004 5 4 ASAA0410123 120040317A5320655162820 TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND STRINGER TIE IS CORRODED AT FS 947. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000462004050400046NM 2004 5 4 ASAA0410121 120040317A531165465251 FRAME BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORRODED FRAME AT STATION 380 AND LEFT STRINGER 26. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000472004050400047 2004 5 4 GTIA040249 420040329A2565 SLIDE DOUG DC9 DC981 3022081WP L2 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 ACY - FLT 1141 - AFT SLIDE PACK AT GALLEY L-2 DOOR FELL OFF. REINSTALLED SLIDE PACK AND COVER. NO DEFECTS NOTED. (M) 2L72 4F A6WE 20040504000482004050400048NM 2004 5 4 GTIA040250 120040329A2560 CABLE DOUG MD80 MD83 3023681NM TAILCONE OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 DTW - FOUND VERIFY TAILCONE SLIDE INSTALLATION. REPOSITIONED KEVLAR CABLE AND TAILCONE COVER STRAP CLIPS. (M) 2L72 4F RT 20040504000492004050400049NM 2004 5 4 ASAA0410154 120040323A5320654868720 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND RIGHT MAIN WHEEL WELL CRACKED AT FRAME STATION 685. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000602004050400060NE 2004 5 4 S04472025 220040220A7200 ENGINE BOEING747 747400 NM PWA 4056 PW4056 NE NR 1 SURGES W SAJFA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP03 24311 744 B18273, DURING FINAL APPROACH, AT ALT 4000 FT, AUTO THROTTLE WAS ENGAGED. WHEN THROTTLE ADVANCE FROM IDLE, ENG 1 SURGE AND SPOOL DOWN.C/A: REPLACE ENG 1 VSV ACT. PERFORM MAINT ACTION IAW FIM 71-00-00. CHECK NML. 2L74 4F4 FRTA20WE E24NE 20040504000612004050400061EU 2004 5 4 SIMA200410112 120040324A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 AIRCRAFT SUSTAINED HAIL DAMAGE 8 IN FORWARD OF FRAME 583.0 AT SL 1606 THAT REQUIRED A REPAIR, THE PREVIOUS REPAIR AT THIS LOCATION SWAS FOUND TO BE INCORRECT. DENT WAS INSPECTED BY ULTRASONIC BOND TEST WITH NO DEFECTS NOTED. DENT RECONTOURED IAW MFG SRM. FABRICATED A REPAIR DOUBLER AND TRIPLER. 2L72 4T4 TRTA52EU E8NE 20040504000622004050400062EU 2004 5 4 SIMA200410109 120040401A55117253707014 SPAR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE HORIZ STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 DURING AN MBV INSPECTION AND COMPLIANCE OF AD COLD WORK EXPANSION OF HOLES IN FRONT SPAR OF LT AND RT HORIZONTAL STABILIZERS. DURING THE EDDY CURRENT INSPECTION OF THE RT STABILIZER HOLES THE UPPER IB HOLE SHOWED REJECTABLE INDICATIONS. OVERSIZED AND COLD WORKED HOLE TO ACCEPT OVERSIZED OF .277. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. WORK DONE IAW REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000642004050400064EU 2004 5 4 SIMA200410108 120040328A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 DURING AN MBV INSPECTION, ONE DENT WAS FOUND ON THE TOP SKIN PANEL BETWEEN FRAME STA 339 AND 363.0, STRINGER 1501 AND 1601 THAT WAS BEYOND SRM LIMITS. COMPLETELY REMOVED THE DAMAGED AREA BUT CREATING A CUTOUT. FABRICATED A REPAIR DOUBLER AND FORMED TO FUSELAGE CONTOUR. REPAIR DONE IAW SRM. 2L72 4T4 TRTA52EU E8NE 20040504000652004050400065SO 2004 5 4 SIMA200410702 120040412A27503632001003 PDU EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007C GL T/E FLAP MALFUNCTIONED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21716AE 145264 DURING APPROACH WHEN CREW SELECTED FLAPS FROM 22 DEGREES TO 9 DEGREES. THE FLAPS FAILED AT 9 DEGREES. MAINTENANCE REMOVED AND REPLACED THE FLAP DRIVE UNIT IAW MM. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406012) 2L72 4F4 FRTT00011ATTE6CH 20040504000662004050400066EU 2004 5 4 SIMA200410113 120040329A5330AL2024T3 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON REPAIR STATEMENT, DENT ID AS NR 7, 4.5 INCH AFT OF STA 339 AND 2.7 INCH ABOVE LS 1605 WAS FOUND TO BE BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THIS LOCATION WAS FOUND TO BE INCORRECT. FABRICATED A NEW REPAIR DOUBLER. REPAIR DONE IAW MFG STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000682004050400068EU 2004 5 4 SIMA200410111 120040328A5311 FRAME SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 DURING AN MBV INSPECTION MAINTENANCE FOUND DENT ON CARGO FRAME 658.5 BEYOND SRM LIMITS. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. RECONTOURED TO NORMAL AND DID ADDITIONAL NDT INSPECTION. FABRICATED A REINFORCEMENT DOUBLER. REPAIR DONE IAW REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040430000782004043000078NM 2004 4 30 AALA20040467 120040418A33500201922001 LIGHT BOEING767 767323 1385205NM SEAT 24B BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 LAX - EMERGENCY LIGHT ASSEMBLY AT SEAT 24B BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040430000992004043000099EA 2004 4 30 VNAA0404014 120040415A3610285051 SWITCH CNDAIRCL600 CL6002B19 1900309EA WING FAILED A VNAAO OTHER N FALSE WARNING LDLANDING 1 GL07229PS376 7898 AFTER LANDING, ANTI ICE DUCT WARNINGS ILLUMINATED THEN CLEARED. AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED WING LEADING EDGE THERMEL SWITCHES IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 36-21-07-710-801. OPERATIONAL CHECKS WERE DONE AND AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040430001072004043000107NM 2004 4 30 ASAA0410152 120040323A5313654576717 STRINGER BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT STRINGER GOUGED AT STATION 500A. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040430001182004043000118EU 2004 4 30 USAAEM04001 120040321A5280 DOOR EMB ERJ170ERJ170100 EU NLG OPEN A USAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA19804MD 17000016 PIT - DURING FLIGHT INTERMITTENT NOSE LANDING DOOR OPEN AFTER GEAR RETRACTION. INSPECTED NOSE LANDING DOOR LINKAGES. NO DEFECTS NOTED. CHECKED AND ADJUSTED GAP ON DOOR PROX SENSORS. (M) 2L74 4F RTA56NM 20040503000422004050300042SO 2004 5 3 C2XA04TY073 120040428A575114569009408 BRACKET EMB 135 EMB135ER 3260203SO RT AILERON WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716511 145267 TYS - DURING A SCHEDULED 2C INSPECTION THE RIGHT PCS AILERON O/B BRACKET BUSHING WAS FOUND MIGRATING. MAINT REMOVED AND REPLACED THE RIGHT AILERON PCA ATTACH BRACKET IAW EA-2710-01017 AND 51-20-03; 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040503000512004050300051SO 2004 5 3 C2XA04BT055 120040427A27503634001021 CABLE EMB 135 EMB135LR 3260305SO T/E FLAP BINDING A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW2724517 145332 CREW REPORTED, FLAP FAIL INFLIGHT DURING DESCENT AT APPROXIMATELY 9000 MSL, APPROXIMATELY 240 KNOTS, SPEED BRAKE DEPLOYED OPEN. FLAP INDICATOR ON EICAS AMBER WITH DASHED LINE. QRH FLAP FAILURE CHECKLIST COMPLETED. ZERO FLAP LANDING PERFORMED. MAINTENANCE REMOVED AND REPLACED LEFT HAND INBOARD FLEXIBLE SHAFT CABLE IAW EMB135 AMM 27-51-04. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040503000562004050300056SO 2004 5 3 CHQA000480 120040425A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 DURING OPERATIONAL CHECK THE 1ST AISLE EMERGENCY LIGHT WAS OUT. REMOVED AND REPLACED 1ST AISLE EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-4. 2L72 4T RTT00011AT 20040503000572004050300057NM 2004 5 3 AALA20040484 120040424A3350 LIGHT BOEING757 7572Q8 1384972NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21709TW 28168 LAS - SECTION OF EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B BROKEN. REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHTING AT SEAT 1B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040503000702004050300070SO 2004 5 3 C2XA04SH189 120040330A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE BLENDED OUT THE AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040503000732004050300073NM 2004 5 3 CALA0400402 120040419A5311149A761416 FRAME BOEING737 737824 13844BZNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717245 28955 RIGHT WHEEL WELL O/B CHORD CRACKED 2 FT. REPLACED CHORD IAW SRM 51-40-01. 2L72 4F RTA16WE 20040503000772004050300077NM 2004 5 3 ABXA040140 120040412A3213161T11551 BEARING BOEING767 767281 1385109NM RT MLG STRUT MISINSTALLED A ABXAA UNSCHED LANDING O OTHER APAPPROACH 1 GL23794AX 23144 EN ROUTE TO SJC, RIGHT MAIN LANDING GEAR FAILED DOWN AND LOCK WITH GEAR DOOR OPEN. OBSERVED BY ATC TOWER, HELICOPTER. ACCOMPLISHED NON NORMAL, DID NOT SOLVE PROBLEM. SEVERAL NEGATIVE AND POSITIVE G'S MANEUVERS AND GEAR CAME DOWN. AIRCRAFT WAS RE-ROUTED TO MHR WHERE IT LANDED WITHOUT FURTHER INCIDENT. UPON LANDING, GEAR WAS PINNED AND AIRCRAFT TOWED TO GATE. OPENED WORK PACK W/O 600196580. STRUT REPACKED IAW B767 AMM 32-11-25-2. ACCOMPLISHED LANDING GEAR ALTERNATE EXTEND CONDITION. ACCOMPLISHED SEVERE OR UNUSUAL TURBULANCE INSPECTION. NO DEFECTS NOTED. REWORKED AREA ON RIGHT MAIN LANDING GEAR UPLOCK FITTING. ROTOPEEN IAW REA B 632-49613, REF ABX PROCESS STANDARDS MANUAL 900-4, NUMBER 10. 2L72 4F RTA1NM 20040503000832004050300083SO 2004 5 3 C2XA04TY067 120040412A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712921 145354 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040503000862004050300086SO 2004 5 3 C2XA04SH188 120040328A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718557 145596 SHV- DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040503000962004050300096NM 2004 5 3 ASAA0410112 120040306A531565549101 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AT AFT PIT FLOORBEAM AT STATION 847. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503000972004050300097NM 2004 5 3 ASAA0410108 120040306A5313654688337 STRINGER BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 22L AND STATION 787. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001092004050300109WP 2004 5 3 ABXA040132 120040315A5312591013013 BULKHEAD DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 AXIAL CRACK IN AFT PRESSURE BULKHEAD AT RIGHT UPPER CORNER OF VENTRAL DOOR CUT OUT. REPAIRED AREA IAW REA D953-49498MR. 2L72 4F A6WE 20040503001292004050300129SO 2004 5 3 C2XA04SH204 120040407A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE T-REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040503001342004050300134NM 2004 5 3 ASAA0410099 120040302A53136552928595 STRINGER BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 22L AND STATION 847. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503001592004050300159NM 2004 5 3 ASAA0410131 120040317A53206546579552 TEE FITTING BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON T-CHORD IN APU COMPARTMENT RIGHT STATION 1115-1125 BELOW AIR DUCT CUTOUT. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002462004050300246EU 2004 5 3 PG9R118900 120040302A6410355A12004008 BLADE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19911KR819 2094 TAIL ROTOR BLADE HAS SPAR CRACK. (RMA NR R047450) 1G71 3U3 UNCH9EU E19EU 20040503002532004050300253WP 2004 5 3 GTIA040226 120040216A5310 BEAM DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND MID PIT DOOR JAMB IS CORRODED STATION 636 TO 623 ON EDGE AND AROUND FASTENERS. REMOVED JAMB BEAM. DRILLED AND LOCATED NEW JAMB BEAM. INSTALLED JAMB BEAM. (M) 2L72 4F A6WE 20040503002622004050300262NM 2004 5 3 ASAA0410141 120040317A534765549696 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK CORROSION AT STATION 857. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002732004050300273SW 2004 5 3 ALGA094103 120040408A6220406310405101 UNIVERSAL BELL 407 407 1182206SW ALLSN 250C 250C* GL M/R DRIVE RATCHETING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03436AL598 53069 ROUGH AND RATCHETY. REMOVED AND REPLACED WITH NEW PART. 1G71 3U3 UO H2SW E4CE 20040503003182004050300318WP 2004 5 3 GTIA040213 120040308A33504TL115 SWITCH DOUG DC9 DC981 3022081WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FTW - FOUND FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH BROKEN. REPLACED FORWARD LIGHT ATTENDANT EMERGENCY LIGHT SWITCH. (M) 2L72 4F A6WE 20040503003202004050300320NM 2004 5 3 ASAA0410105 120040306A53206552928595 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND HOLES OVERSIZED AT STRINGER 241 AND STATION 847. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503003252004050300325WP 2004 5 3 GTIA040245 120040111A55235930497401 SKIN DOUG DC9 DC983 3022083WP LT ELEVATOR TAB DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND LEFT ELEVATOR ANTI-FLOAT TAB DENTED ON BOTH SIDES NUMEROUS PLACES. REMOVED LEFT ELEVATOR ANTI-FLOAT TAB. INSTALLED LEFT ELEVATOR ANTI-FLOAT TAB. (M) 2L72 4F RTA6WE 20040504000342004050400034 2004 5 4 GTIA040218 420040321A2565 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR UNLATCHED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 DTW - FLT 709 - SLIDE PACK FELL OFF DOOR WHEN DOOR SHUT FOR PUSH-LATCH CAME UNDONE. FOUND SLIDE PACK STILL INSTALLED, LATCH CAME UNDONE. RELATCHED, NO OTHER DEFECTS NOTED. (M) 2L72 4F RT 20040504000372004050400037 2004 5 4 ASAA0410155 420040323A2300654576989 ANTENNA BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AT LOWER ANTENNA AT STATION 470. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000402004050400040NM 2004 5 4 ASAA0410158 120040323A531165469461 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CRACKED FRAME AT FS 927. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000432004050400043NM 2004 5 4 ASAA0410128 120040317A531065469486 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT SHEAR TIE CORRODED AT FS 967 AT STRINGER 19L-20L. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000692004050400069EU 2004 5 4 SIMA200410114 120040329A5330AL2024T3 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON MFG REPAIR STATION DENT ID NR 6510.0 IN FORWARD OF FRAME 389 AND 4.0 IN ABOVE SL 1603 WAS FOUND BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THE LOCATION WAS FOUND INCORRECT. REMOVED PREVIOUS DOUBLER AND FABRICATED A NEW DOUBLER. REPAIR DONE IAW SRM. 2L72 4T4 TRTA52EU E8NE 20040504000712004050400071EU 2004 5 4 SIMA200410117 120040329A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. MFG REPAIR STATEMENT DENT ID AS NR 43, 4.5 IN AFT OF STATION 319 AT SL 1602 WAS FOUND BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THIS LOCATION WAS DETERMINED TO BE INCORRECT. REMOVED PREVIOUS REPAIR DOUBLER THAT WAS INSTALLED FABRICATED REPAIR DOUBLER. REPAIR DONE IAW MFG REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000722004050400072EU 2004 5 4 SIMA200410116 120040323A53117253813007 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 DURING AN MBV INSPECTION, THE GALLEY FRAME 258.0 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A 23.0 CUTOUT OF THE DAMAGED AREA OF FRAME 258 AND TREATED THE BARE METAL EDGES. FABRICATED A DOUBLER, SHIMS AND TRIPLER FOR REPAIR. REPAIR DONE IAW MFG SRM. 2L72 4T4 TRTA52EU E8NE 20040504000742004050400074EU 2004 5 4 SIMA200410101 120040323A53117252814417 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21392AE 340B392 DURING AN MBV INSPECTION A PREVIOUS REPAIR ON GALLEY FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED EXISTING REPAIR PARTS AND PERFORMED A CUTOUT OF FRAME 258. FAB SHIM, DOUBLER AND TWO TRIPLER FOR REPAIR. REPAIR DONE IAW MFG REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000752004050400075EU 2004 5 4 SIMA200410104 120040320A53117252813485 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 DURING AN MBV INSPECTION A GALLEY AREA FRAME 225 WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT DAMAGED SECTION . CLEANED AND TREATED THE BARE METAL EDGES OF THE CUTOUT. FABRICATED A FILLER, SPACER AND REPAIR ANGLE. REPAIR DONE IAW SRM. 2L72 4T4 TRTA52EU E8NE 20040504000772004050400077EU 2004 5 4 SIMA200410103 120040406A53117253813 FRAME SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 DURING AN MBV INSPECTION FRAME 258.0 TOP FLANGE WAS FOUND CORRODED BELOW SRM LIMITS. DURING HIDDEN DAMAGE INSPECTION FOUND PREVIOUS. REPAIR ON FRAME 258 TO HAVE IMPROPER FASTENER EDGE DISTANCE ON SEVEN HOLES. REMOVED PREVIOUS REPAIR, AND CUT OUT THE ROW OF SEVEN HOLES. FABRICATED A FILLER, TWO TRIPLERS AND REPAIR ANGLE. REPAIR DONE IAW MFG REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000792004050400079EA 2004 5 4 WVE2004F00006 120040419A5320601R3117117 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09408SW 7055 FS 484 WATERLINE 73 LBL 27 OB INTERCOSTAL ATTACHMENT ANGLE (PN 601R3117117) IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997) 2L72 4F4 FRTA21EA E15NE 20040504000802004050400080EA 2004 5 4 WVE2004F00007 120040419A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERK NONE O OTHER NRNOT REPORTED 1 EA09408SW 7055 FUSELAGE SKIN IS CRACKED AT THE CORNERS OF THE NOSE LANDING GEAR CUT OUT AT FS 235, RBL 6 AND LBL 6, STINGERS 26 R AND 26L. PROBABLE CAUSE: STRESS (EA09200401997) 2L72 4F4 FRTA21EA E15NE 20040504000832004050400083NM 2004 5 4 USA2004F00025 120040410A21337110033 OUTFLOW VALVE BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19591US49097 23936 ON CLIMB OUT, ENROUTE, THE AUTO MODE OF THE PRESSURIZATION CONTROLLER FAILED AT FL230. THE AUTO FAIL LIGHT ILLUMINATED AND THE CABIN PRESSURE WARNING HORN ACTIVATED AS CABIN ALTITUDE REACHED 12,000 FEET. THE OUTFLOW VALVE WAS NOTED AS BEING CLOSED. FLIGHT DESCENDED TO 10,000 FEET WHERE PRESSURIZATION WORKED NORMALLY IN STANDBY MODE. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS DEPLOYED. MAINT REMOVED AND REPLACED THE AFT OUTFLOW VALVE ASSY IAW MM. ACCOMPLISHED JOB CARD AND AUTO PRESSURIZATION SYSTEM CHECK IAW MM. SYSTEM CHECKS GOOD 2L72 4F4 FRTA16WE E2GL 20040504000862004050400086NE 2004 5 4 USA2004F00029 220040320A7200 ENGINE AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE NR 1 FAILED A USAAO OTHER JY WARNING INDICATION ENGINE STOPPAGE APAPPROACH 1 EA19709UW 0997 ENROUTE, DURING APPROACH, AT 12,000 FEET, RECEIVED (ENG 1 OIL FILTER CLOG) ECAM MESSAGE. THEN THE NUMBER ONE ENGINE BEGAN TO FLUCTUATE, VIBRATE AND SURGE UNTIL IT QUIT. CREW ACCOMPLISHED THE SHUT DOWN PROCEDURES GIVEN BY ECAM ACTIONS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 18 MINUTES. MAINTENANCE REPLACED THE NUMBER ONE ENGINE. OPERATIONALLY AND LEAK CHECKED OK. 2L72 4F4 FRTA28NM E2GL 20040504000882004050400088 2004 5 4 USA2004F00016 420040224A2565D30654122 SLIDE BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE R1 DOOR LEAKING A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU 27198 DURING ANNUAL SLIDE OPERATIONAL CHECK, THE R1 DOOR SLIDE DEPLOYED PROPERLY, BUT FAILED TO HOLD PRESSURE. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA2NM A12EU 20040504000892004050400089NM 2004 5 4 USA2004F00018 120040305A2120 ODOR BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE CABIN DETECTED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA19530AU 24412 ON APPROACH, THE FLIGHT ATTENDANTS REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE AFT CABIN. CREW SHUT OFF GALLEY POWER AND WENT TO FULL COLD ON THE PACKS. NO FAULTS WERE NOTED IN THE ELECTRICAL SYSTEM AND NO OBVIOUS SOURCE OF SMOKE WAS FOUND IN THE CABIN. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT TAXIED TO THE GATE AND THE PASSENGERS DEPLANED NORMALLY. MAINT RAN ALL ELEC SYSTEMS AND LIGHTING IN THE CABIN AND GALLEYS. ALL OPERATIONALLY CHECKED GOOD WITH NO ODOR NOTED. RAN ENGINES, APU AND PACKS. NO ODORS NOTED. CHECKED E AND E COMPARTMENT. NO ODOR FOUND. CHECKED ALL CIRCUIT BREAKERS. ALL CHECK GOOD. RAN HYDRAULIC SYSTEM, SYSTEM CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA16WE E2GL 20040504000902004050400090EU 2004 5 4 USA2004F00010 120040306A3350321431 BATTERY AIRBUS330 A330323 3930335EU PWA 4052 PW4052 52119NE CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19672W 333 EPSU 15WL FAILED CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERY. 2L72 4F4 FRTA46NM E24NE 20040505000012004050500001 2004 5 5 PAI2004F00000 420040419A2562CI2485 ANTENNA CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE AFT FUSELAGE CRACKED B PAIRO OTHER O OTHER NRNOT REPORTED 1 SO15500UB 5600052 IN JANUARY, AN ELT WAS INSTALLED WITH ANTENNA CI 248-5 INSTALLED WITH A DOUBLER. THE DOUBLER WAS TIED INTO THE EXISTING 2 STRINGERS ON THE LT AND RT. 3 MONTHS LATER THE SKIN AND DOUBLER CRACKED AROUND THE BASE OF THE ANTENNA AND UPON LANDING THE ANTENNA DEPARTED THE AIRCRAFT. IT REMAINED ATTACHED BY THE COAX CABLE. THE ANTENNA WAS UNDAMAGED, A DER WAS BROUGHT IN AND A FLUSH PATCH INSTALLED. A NEW DOUBLER WAS FABRICATED AND THE NEW DOUBLER TIED INTO THE 2 STRINGERS ALONG WITH THE FWD AND AFT FRAMES. 2L72 4F4 FRTA22CE E25EA 20040505000022004050500002EU 2004 5 5 PG9R118894 120040131A7160350A54108004 INTAKE UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE AIR INTAKE CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19131GC186 3691 AIR INTAKE HAS A CRACK. (RMA NR R046894) 1G72 3U3 U H9EU E00054EN 20040505000032004050500003EA 2004 5 5 A6WA200440044 120040414A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WINGS INOPERATIVE A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31418AW 4887 FLAP FAIL MESSAGE. FLAPS AT ZERO, COMPLIED WITH QRH-WEIGHT AT TOUCHDOWN 41,800 LBS, APPROXIMATE SPEED 115 KNOTS. BRAKE APPLICATION 55 MAX BRAKE TEMP 2. RESET FLAPS IAW SUPPLEMENT 98-18 FLAPS OPERATE NORMAL AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20040505000062004050500006NE 2004 5 5 ASO2004F00003 220040402A7200 ENGINE CNDAIRCL215 CL2151A10 1900320EA GE CF34 CF34* NE CONTAMINATED A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27717EV 10088 DURING CLIMB OUT, THE CREW RECEIVED A FORWARD LAVATORY SMOKE MESSAGE ACCOMPANIED BY SMOKE INTO THE COCKPIT ALONG WITH AN ODOR IN THE COCKPIT AND CABIN. THE SMOKE DISSIPATED FOLLOWING COMPLIANCE WITH THE LAVATORY SMOKE CHECKLIST. AN EMERGENCY WAS DECLARED WITH FIRE AND RESCURE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED, LANDING SAFELY. UPON MAINT INSP OF THE AIRCRAFT AND REVIEW OF THE MAINT HISTORY. IT WAS DETERMINED THE SMOKE HAD BEEN CAUSED BY RESIDUE FROM AN ENGINE WASH MIXTURE IN THE BLEED AIR SYSTEM. MAINT PERFORMED DRYING OF THE INTERNAL ENGINE AIRFLOW COMPONENTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4R4 FRTA14EA E15NE 20040505000072004050500007EA 2004 5 5 A6WA200440043 120040413A3230601R850071 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TRUNNION FAILED A O OTHER O OTHER NRNOT REPORTED 1 GL31427ZW3404 7685 WHILE REMOVING RT MLG FOR FITTING REPLACEMENT, IT WAS DISCOVERED THAT RT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 2ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCH ALL WORK DOEN IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-054 REV B, PART B. (M) 2L72 4F4 FRTA21EA E15NE 20040505000082004050500008EA 2004 5 5 ASO2004F00002 120040413A3260 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE MLG ILLUMINATED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27724EV 10138 DURING TAKEOFF, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSISTION. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFELY. MAINT FOUND MAINTENANCE DIAGNOSTIC COMPUTER (MDC) FAULTS FOR ALL THREE GEAR UPLOCK FAR. MAINT PERFORMED TWENTY GEAR SWINGS AND ALSO INSPECTED THE DOWN AND UPLOCKS, GEAR SELECTOR VALVE, ELECTRICAL AND HADRAULIC CONNECTIONS FOR SECURITY. NO DEFECTS WERE NOTED. THE MDC SHOWED NO FURTHER FAULTS IN OPERATION. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040505000092004050500009NM 2004 5 5 UIEA200400068 120040422A36109790181 VALVE BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE NR 3 ENGINE INOPERATIVE A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15536MC 21576 455889 AZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BACK TO IDLE LIGHT WILL EXTINGUISH. BUT LIGHT WILL COME BACK ON IF PUSH THRUST LEVER FORWARD MORE THAN 70 PERCENT N1. NR 3 THRUST LEVER USED IN IDLE FOR REMAINING OF FLIGHT. NR 3 ENGINE PNEUMATIC DUCT LEAK CHECK CARRIED OUT, NIL LEAKS. FAN AIR MODULATING VALVE SENSE LINES LEAK CHECK NIL. FAN AIR MODULATING VALVE REPLACED IAW AMM. TEMPERATURE SENSOR BODY AND PLUG CLEANED. HIGH POWER RUN CARRIED OUT ALL NORMAL. DUMPED 30.0 KG FULE TO MEET MAX LANDING WEIGHT. 2L74 4F4 F A20WE E23EA 20040505000122004050500012EU 2004 5 5 PG9R117586 120040331A2435150S61229 STARTER GEN UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE ENGINE FAILED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19135PH704 3695 UNIT FAILED TO START AIRCRAFT. (RMA NR R047877) 1G72 3U3 U H9EU E00054EN 20040505000132004050500013EU 2004 5 5 PG9R117581 120040119A5340350A21004827 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE FUSELAGE CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19135PH509 3695 FITTINGS CRACKED. (RMA NR R046607) 1G72 3U3 U H9EU E00054EN 20040505000152004050500015EU 2004 5 5 PG9A117580 120040119A5340350A21004827 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE FUSELAGE CRACKED B PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19130PH663 3670 REAR FITTINGS CRACKED. (RMA NR R046607) 1G72 3U3 U H9EU E00054EN 20040505000212004050500021EA 2004 5 5 ASOA04244 120040327A5730CC67017351 SKIN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27709EV 10068 DURING HANGER MAINTENANCE, THE SKIN UNDER THE RT IB MULTIFUNCTIONAL SPOILER AT THE IB BRACKET WAS FOUND CRACKED. MAINT IS TO PERFORM A DETAILED VISUAL INSP FOR PROGRESSION OF THE CRACK AT EVERY SUBSEQUENT SERVICE CHECK, UP TO A MAX OF 100 FLIGHT HRS IAW REO 670-57-73-008, AT WHICH TIME THE PERMANENT REPAIR IS TO BE PERFORMED. 2L72 4F4 FRTA21EA E15NE 20040505000242004050500024NM 2004 5 5 CW1R075K 120040210A3010F2MA726103 TUBE AMD FALC50FALCON2000 2730170NM RT WING CRACKED B CW1RO OTHER O OTHER NRNOT REPORTED 1 EA11790L 15 FITTING FOR PRESSURE SENSOR CRACKED ON IB WING ANTI-ICE TUBE. CRACK WAS IN WELD AREA. POSSIBLY HOT AIR FROM DUCT COULD DAMAGE CONTROL PUSH PULL ROD. CHECK AREA CAREFULLY BY REMOVING LAGGING AROUND TUBE DURING INSPECTION. 2K73 4F RTA50NM 20040505000252004050500025EU 2004 5 5 A6WA200460013 120040415A3213 AXLE BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA MLG VIBRATION A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31608AW E2049 AIRCRAFT EXPERIENCED VIBRATION AFTER LANDING. MAINTENANCE REMOVED AND REPLACED RT MLG AXLE. 2H74 4F4 F A49EU E6NE 20040505000272004050500027CE 2004 5 5 KW32004F00000 120040401A3260444EN2REN3R SQUAT SWITCH LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP RT MAIN GEAR INOPERATIVE B KW3RK NONE O OTHER ININSP/MAINT 1 WP07404MK 2003 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT ONE EACH SET SCREW MISSING FROM LT OB, RT IB, AND RT OB LEVER ARMS AND 2 EACH SET SCREWS MISSING FROM LT IB LEVER ARM. PROBABLE CAUSE; UNKNOWN AT THIS TIME. MISSING SET SCREWS (PN 632UNC-2A) MUST BE INSTALLED IAW MFG MM. 2L72 4F4 FRTT00008WIE6WE 20040505000282004050500028EU 2004 5 5 USA2004F00026 120040416A323490337B0001012 CONTROL LEVER EMB ERJ170ERJ170100 EU GE CF34 CF34* NE COCKPIT MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19802MD233 17000013 CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE (UP) POSITION AFTER TAKEOFF. FLIGHT RETURNED WITHOUT INCIDENT. MAINTENANCE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATISFACTORY. 2L74 4F4 FRTA56NM E15NE 20040505000292004050500029 2004 5 5 USA2004F00028 420040413A2312 ANTENNA EMB ERJ170ERJ170100 EU GE CF34 CF34* NE VHF COMM LIGHTNING STRIKEA USAAK NONE O OTHER CLCLIMB 1 EA19803MD 17000015 PILOT LOST VHF 1, 2 AND 3 SHORTLY AFTER TAKEOFF. PILOT REPORTED STATIC DISCHARGE AT 12,000 FT. MAINTENANCE FOUND LIGHTENING STRIKE THAT DAMAGED VHF 1, 2 AND 3 ANTENNA`S. MAINTENANCE ACTION: COMPLIED WITH LIGHTENING STRIKE INSPECTION. REPAIRED VHF 1 AND 2 ANTENNAS TO MAINTENANCE FERRY FOR DAMAGE REPAIR. 2L74 4F4 FRTA56NM E15NE 20040505000352004050500035EU 2004 5 5 UO22004F00002 120040301A213022201N071000 SELECTOR AMD FALC50FALCON50MYST2730106EU CABIN PRESSURE ERRATIC B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19450K 14 186 AUTO SELECTOR, SENDS ERRATIC SIGNALS TO THE TORQUE MOTOR OF THE ELECTRO PNEUMATIC VALVE. 2L73 4F A46EU 20040505000362004050500036NM 2004 5 5 UO22004F00004 120040416A3010BA562041 CLAMP AMD FALC50FALCON2000 2730170NM ANTI-ICE SYS BROKEN B UO2RO OTHER O OTHER NRNOT REPORTED 1 GL19722JB 13 CLAMP T LOCK BROKE AND SAFETY LATCH DID NOT STAY LATCHED ALLOWING BLEED AIR TO FILL THE AREA WHENEVER WING ANTI-ICE WAS SELECTED. 2K73 4F RTA50NM 20040505000382004050500038NM 2004 5 5 UIEA200400044 120040408A542065B9412511 STIFFENER BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE OF NR 1 PYLON, THE LHS NR 5 STIFFENER END WAS FOUND CRACKED AT NAC STA 288.0 WL 146.5. TRIMMED OFF THE CRACKED STIFFENER END. FABRICATED A REPAIR PLATE TO MATCH THE TRIMMED OFF PORTION OF THE STIFFENER ATTACHING FLANGE. FABRICATED TWO REPAIR ANGLES AND A HORIZONTAL WEB FILLER. THE REPAIR PARTS WERE INSTALLED WITH HI-LOK FASTENERS. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040505000392004050500039NM 2004 5 5 UIEA200400032 120040314A524565B1054625 DOOR BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE NR 1 ACM MISSING A UIEAO OTHER E VIBRATION/BUFFET CLCLIMB 1 EA15537MC 22403 BIRD STRIKE: VIBRATION OF ENTIRE AIRFRAME ON CLIMB OUT. SUDDEN VIBRATION AT APPROXIMATELY 16,000 FT AND 300K IAS. PERFORMED BIRD STRIKE INSP MM. FOUND DAMAGE TO THE FORWARD NR 1 ACM INLET LEFT SIDE AREA AND NR 1 ACM DOOR MISSING. REPAIRED DAMAGED AREA IAW SRM PROCEDURES AND REPLACED MISSING DOOR. 2L74 4F4 F A20WE E23EA 20040505000432004050500043NM 2004 5 5 UIEA200400049 120040413A5414 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 3 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED A ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER REPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040505000452004050500045WP 2004 5 5 UG82004F00001 220040329A7510 SWITCH CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP LT ENGINE STUCK E UG8AK NONE L NO TEST TXTAXI/GRND HDL 1 GL235117 6507064 DURING PILOTS PREFLIGHT, TRIP CANCELLED, LT ENGINE ANTI-ICE LIGHT DID NOT STAY ON DURING OPERATIONAL TEST OF SYSTEM. TROUBLESHOOTING POINTED TO THE LT NACELLE COOLING AIR INLET ANTI-ICING SENSOR (SWITCH). THE CONTACTS IN THE SENSOR WERE FOUND STUCK. REPLACED THE FAULTY SENSOR (SWITCH). OPERATIONAL TEST OF ANTI-ICE SYSTEM SHOWED NO FURTHER DISCREPANCIES. 2L72 4F4 F A9NM E6WE 20040505000462004050500046CE 2004 5 5 UG82004F00002 120040331A2611 SMOKE DETECTOR CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL CARGO BAY DIRTY E UG8AO OTHER N FALSE WARNING DEDESCENT 1 GL235116 7500019 DURING DESCENT, BAGGAGE SMOKE LIGHT (EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFTER LANDING. BAGGAGE SMOKE DETECTOR FOUND TO BE VERY DIRTY. REMOVED SMOKE DETECTOR AND CLEANED COVER AND MOUNTING AREA. REINSTALLED AND PERFORMED FUNCTIONAL CHECK. SYSTEM CHECKED GOOD. INITIATED A FLEET INSPECTION AND CLEANING OF DETECTORS. 2L72 4J4 FRTT00007WITE6CH 20040505000472004050500047SO 2004 5 5 PA04002 120040419A31501159SCAV35431 CIRCUIT CARD GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU WARNING SYSTEM DIRTY E UG8AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23473KT 438 AURAL OVERSPEED WARNING CAME ON DURING TAKEOFF ROLL, LOW SPEED ABORT. THERE WAS A MALFUNCTION WITHIN THE OVERSPEED WARNING SYSTEM. THE AUDIBLE TONE GENERATOR WAS REMOVED. THE NR 2 CHANNEL CARD WAS REMOVED, INSPECTED, CLEANED AND REINSTALLED. THE OVERSPEED SYSTEM WAS OPERATIONALLY CHECKED IAW THE MM AND FOUND TO PERFORM WITHIN MFG SYS TOLERANCES. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 F A12EA E2EU 20040505000482004050500048CE 2004 5 5 TZR2004F00005 120040310A81204066109025 TURBOCHARGER CESSNA401 401 207590CCE CONT O520 TSIO520EB 17040SO ENGINE FAILED E TZRAE ENGINE SHUTDOWN KR FLUID LOSS PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW05403TE 464 4010008 14590271E PILOT REPORTED LOSS OF TURBO BOOST AND OIL PRESSURE, SHUT DOWN ENGINE AND FEATHERED PROPELLER IN FLIGHT. LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. DURING POST FLIGHT INSPECTION OF TURBO OIL WAS OBSERVED IN THE EXHAUST OVERBOARD PIPE INDICATING SEAL FAILURE. BEARING FAILURE WILL CAUSE LACK OF BOOST AND ATTRIBUTED TO SEAL FAILURE. 1L72 3O3 O A7CE E8CE 20040505000512004050500051EU 2004 5 5 TRB2004F00014 120040301A2612 FIRE WARNING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE MALFUNCTIONED A TRBAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO21342AT 345 127137 ON GROUND, WITH PROP IN FEATHER POSITION, THE LT ENGINE FIRE INDICATION LIGHT CAME ON. AFTER ENGINE SHUTDOWN THE WARNING LIGHT EXTINGUISHED. STRONG TAILWIND WAS PRESENT. PERFORMED ENGINE FIRE SYSTEM OPERATION TEST AND FOUND SYSTEM WORKING SATISFACTORY. LOOKS LIKE THE STRONG TAIL WIND WAS THE CONTRIBUTOR FACTOR. (SDR2004015) 2H72 4T4 TRTA53EU E20NE 20040505000532004050500053CE 2004 5 5 WK42004F00003 120040210A3244265K682 TIRE RKWELLNA265 NA26560 7630106CE PWA JT12 JT12A6A 52042NE MLG DAMAGED B WK4RO OTHER O OTHER NRNOT REPORTED 1 SO17353CA31 306028 CENTER TREAD CHUNKED AFTER 23 LANDINGS ON RT TIRE. THE REVISION IS TO THE SN OF THE TIRE WHICH HAS THE DAMAGE TO IT. THE PREVIOUS SN WAS TO THE WHEEL ASSY ITSELF AND NOT THE DEFECTIVE PART(TIRE). 2L72 4J4 JRTA2WE 1E9 20040505000552004050500055SW 2004 5 5 Q8L2004F00000 120040226A321354530011 HOUSING SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP LT MLG CRACKED B Q8LRK NONE O OTHER ININSP/MAINT 1 NM11160WA TC399 DURING A 50 HOUR FLUORESCENT PENETRANT INSPECTION OF THE LT AND RT MAIN LANDING GEAR STRUT HOUSINGS, A CRACK WAS FOUND ON THE LT MLG HOUSING. THE CRACK IS .125 INCHES LONG AND IS LOCATED .125 INCHES FROM THE FORWARD EDGE ON THE OB SIDE. THE INSPECTION IS COVERED IN MFG SB 226-32-033. THE HOUSING HAD PREVIOUSLY BEEN REWORKED AND CANNOT BE REWORKED ANY FURTHER , IT IS NOT ALLOWED ANY CRACKS. THE PROBABLE CAUSE IS SERVICE INDUCED FATIGUE CRACKING. CONTINUE 50 HOUR INSPECTION INTERVALS SHOULD DETECT THE INITIATION OF CRACKS IN REWORKED HOUSINGS. 2L72 4T3 TRTA8SW E2WE 20040505000562004050500056NE 2004 5 5 04100401 220040409A753231B575601 BLEED VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE COMPRESSOR INTERMITTENT A VTZAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 EA27401FJ 3145 PCECD0091 DURING APPROACH OF FLIGHT 6253 TO BOS CREW REPORTED A COMPRESSOR STALL AND ITT INDICATION RISE ON THE LEFT HAND ENGINE. THE LEFT HAND ENGINE WAS SHUT DOWN AS A PRECAUTION AND FLIGHT LANDED UNEVENTFULLY. SEVERAL BLEED OVER VALVES WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 FRTA55NM E35NE 20040505000572004050500057EU 2004 5 5 Q752004F00000 120040223A278210609008 ACTUATOR AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP L/E SLAT LEAKING E Q75AA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO03569DW7486 220 DURING CLIMB OUT, SLATS RETRACTED NORMALLY. THEN A MASSIVE HYDRAULIC LEAK APPEARED ON OB LEFT WING. NR 1 HYDRAULIC SYSTEM BEGAN TO EMPTY. LANDING GEAR WAS LOWERED AND LANDING WAS MADE NORMALLY. AFTER INVESTIGATING PROBLEMS WAS LT, OB SLAT ACTUATOR. THE RETRACTION SWIVEL END FROZE AND IT CAUSED THE HYDRAULIC LINE IN THE LE OF THE OB WING TO BREAK CAUSING THE LEAK. SB 212 ADDRESSED THIS PROBLEM AND WAS ACCOMPLISHED AT THE FACTORY. MFG IS LOOKING INTO THE PROBLEM. 2L72 4F4 F A33EU E6WE 20040505000612004050500061EA 2004 5 5 04102655 120040411A210070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27655BR 7457 DURING CRUISE OF FLIGHT 7387 CREW REPORTED A STAB/MACH TRIM FAILURE. THE CREW DIVERTED TO NEAREST SUITABLE FIELD AND FLIGHT LANDED UNEVENTFULLY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040505000642004050500064 2004 5 5 04080669 420040320A22106225027101 SERVO CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27669BR 7545 DURING FLIGHT CREW REPORTED AN UNCOMMANDED DISCONNECT OF THE AUTOPILOT SYSTEM. THE ELEVATOR SERVO WAS REPLACED AND IAPS LIGHTING PROTECTION CARD WAS FOUND LOOSE AND TIGHTENED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040505000652004050500065EA 2004 5 5 04088663 120040328A33501317 BULB CNDAIRCL600 CL600* EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27663BR 7527 DURING INPSECTION THE PASSENGER DOOR ENXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000662004050500066CE 2004 5 5 Q2A2004F00000 120040217A7603 LINKAGE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE RT THROTTLE LACK OF LUBE B Q2ARO OTHER O OTHER NRNOT REPORTED 1 SW17101SG BB1785 PILOT REPORTED RT THROTTLE LOCKED IN FLIGHT. NON EVENTFUL LANDING. INSPECTION FOUND DRY FUEL CONTROL LINKAGE CAUSING BINDING. LUBRICATED IAW MM, FUNCTION CHECKS OK. NO PRESENCE OF LUBE SINCE NEW. 1L72 4T4 T A24CE E4EA 20040505000672004050500067EA 2004 5 5 04117622 120040426A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27622BR 7187 DURING INSPECTION THE LEFT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000682004050500068EU 2004 5 5 04106321 120040415A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27321UE 41045 DURING INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4T RTA41NM 20040505000692004050500069EU 2004 5 5 PG9R118897 120040211A5610350A25902500 WINDSHIELD UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE COCKPIT CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19135PH553 3695 WINDSHIELD CRACKED. SCRAPPED (RMA NR R047070) 1G72 3U3 U H9EU E00054EN 20040505000702004050500070EA 2004 5 5 04105651 120040414A33503071BPEGL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27651BR 7426 DURING INSPECTION THE FOWARD FLOOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000712004050500071EU 2004 5 5 04107324 120040416A33503022471 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27324UE 41017 DURING INSPECTION THE RIGHT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040505000722004050500072EU 2004 5 5 04093329 120040402A3350FU248 FUSE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27329UE 41097 DURING INSPECITON THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE FUSE AND PASSENGER DOOR FLOOR EMERGENCY EXIT SIGN WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED 2L72 4T RTA41NM 20040505000732004050500073NM 2004 5 5 P762004F00004 120040219A552465229907 BRACKET BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE LT ELEVATOR CRACKED A P76AO OTHER O OTHER NRNOT REPORTED 1 SO17894AA59612 22010 LEFT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLES THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES AND CRACKED AND BENT. 2L73 4F4 FRTA3WE E2EA 20040505000772004050500077NM 2004 5 5 P762004F00000 120040219A552469222959 BRACKET BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE LT ELEVATOR CRACKED A P76AO OTHER O OTHER NRNOT REPORTED 1 SO17894AA59612 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2L73 4F4 FRTA3WE E2EA 20040505000782004050500078NM 2004 5 5 P762004F00001 120040219A552469222958 BRACKET BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE LT EVEVATOR CRACKED A P76AO OTHER O OTHER NRNOT REPORTED 1 SO17894AA 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2L73 4F4 FRTA3WE E2EA 20040505000792004050500079EA 2004 5 5 04082654 120040422A3350110049 CHARGER CNDAIRCL600 CL600* EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27654BR 7454 DURING INSPECTION THE LEFT AND RIGHT HAND EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040505000802004050500080NM 2004 5 5 04112451 120040421A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27451FJ 3205 DURING INSPECTION THE LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. 2H72 4T RTA55NM 20040505000812004050500081EA 2004 5 5 04113642 120040422A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27642BR 7356 DURING INSPECTION THE ROW 10C EMERGENCY ESCAPE PATH LIGHTING WAS FOUDN INOPERATIVE. THE LAMP WAS REPLACED AND A SATISFACTORY OEPRATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000822004050500082EA 2004 5 5 04108659 120040417A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27659BR 7509 DURING INSPECTION THE RIGHT HAND AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000852004050500085EA 2004 5 5 04113634 120040422A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27634BR 7287 DURING INSPECTION THE FOWARD RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE AND THE BULB WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000872004050500087EA 2004 5 5 04088706 120040327A33503071BPEGL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27706BR 7553 DURING INSPECTION THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OEPRATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000902004050500090EA 2004 5 5 04112621 120040421A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27621BR 7186 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000922004050500092EA 2004 5 5 OEZ2004F00000 120040311A2150SZ430031A MOTOR DHAV DHC6 DHC6300 2802606EA PWA PT6 PT6A60A 52043NE AIR CONDITIONINGFAILED A OEZAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP19228SA 253 PILOT REPORTED BURNING SMELL ON LOG BOOK ENTRY. MAINTENANCE ACTIONS FOUND THAT THE AIR CONDITIONING COMPRESSOR MOTOR WAS THE SOURCE OF THE ODOR. A NEW AIR CONDITIONING COMPRESSOR WAS INSTALLED. 1H72 3T4 TRTA9EA E4EA 20040505001022004050500102EA 2004 5 5 SWIA200413186 120040413A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, FUSELAGE LEFT VERTICAL BEAM LOWER INBOARD AND OUTBOARD FLANGE CRACKED AT 409 + 128 LBL 27. REPAIRED LT VERTICAL BEAM LWR IB FLANGE AT 409+120 LBL 27. REF. CRJ REO 601R-53-41-056 REV. NC, RII 53-401. 2L72 4F RTA21EA 20040505001032004050500103EA 2004 5 5 SWIA200413187 120040413A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT TRANSVERSE BEAM ATTACH CLIPS FOR CARGO DOOR STOP FITTINGS CRACKED AT FS 589.00 AND FS 605.00, LBL 42.0. ATTACH CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, AMM 20-21-00 AND RII 53-401. 2L72 4F RTA21EA 20040505001042004050500104CE 2004 5 5 MCI2004F00000 120040407A1430AN17613AM ATTACH BOLT BEECH 100 B100 1152919CE GARRTTTPE331TPE3315 01514WP HORIZ STAB DAMAGED B MCIRK NONE O OTHER ININSP/MAINT 1 WP11236CP BE9 PERFORMED INSPECTION ON HORIZONTAL STABILIZER ATTACH FITTINGS AND FOUND BOLT HEAD MISSING ON ONE BOLT ON LT AFT ATTACH POINT. REMOVED BOLT AND FOUND IT TO BE WORN AND CORRODED. REPLACED LT AND RT AFT ATTACH BOLTS, BOTH WERE WORN AND CORRODED. BOLT HEAD SHOWS SIGNS OF CORROSION AND POSSIBLY HAD BEEN CRACKED FOR SOME TIME. 1L72 4T4 T A14CE E4WE 20040505001062004050500106SO 2004 5 5 SWIA200413189 120040422A2797 WIRE EMB 120 EMB120ER 3260203SO CONTROL COLUMN BROKEN A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07284YV 120284 FIRST OFFICER'S STALL WARNING SHAKER INOP. REPAIRED BROKEN WIRE NEAR SHAKER CONNECTOR ON CONTROL COLUMN OF FIRST OFFICER'S SIDE. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040505001072004050500107EA 2004 5 5 SWIA200413190 120040416A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 CARGO PIT; TRANSVERSE BEAM ATTACH ANGLES FOR DOOR STOP FITTINGS ARE CRACKED; FS 589.00 AND FS 605.00 LBL 42.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16 AND RII 53-401. 2L72 4F RTA21EA 20040505001132004050500113EA 2004 5 5 SWIA200413194 120040416A5312 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 559 PRESSURE WEB AT RBL 10 AND 18 CRACKED AT AILERON BELLCRACK MOUNTING POINTS. (DISCOVERED DURING C-CHECK INSPECTION) WEB REPAIRED IAW CRJ REO 601R-53-41-207 REV. NC AND RII53-401. 2L72 4F RTA21EA 20040505001152004050500115EA 2004 5 5 SWIA200413196 120040416A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 409 AND 128 RIGHT VERTICAL POST RBL 27 LOWER INBOARD FLANGE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) MADE REPAIR PART AND INSTALLED IAW CRJ REO 601R-53-41-056 REV. NC. REF. RII 53-401. 2L72 4F RTA21EA 20040505001162004050500116EA 2004 5 5 SWIA200413197 120040416A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 MAIN FUSELAGE; PRESSURE FLOOR WEB CRACKED; FS 469.00 LBL 9.0 TO RBL 9.0. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED PRESSURE FLOOR CUTOUT IAW CRJ REO 601R-53-41-102 REV. NC. 2L72 4F RTA21EA 20040505001172004050500117EA 2004 5 5 SWIA200413198 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 MAIN FUSELAGE; PULLEY INTERCOSTAL INBOARD REMOTE ANGLE IS CRACKED AT FS 484.00 LBL 27.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLE IAW CRJ REO 601R-53-41-059 REV. A AND RII 53-401. 2L72 4F RTA21EA 20040505001212004050500121EA 2004 5 5 SWIA200413200 120040416A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 364 STR 8R IS CRACKED FROM FASTENER HOLES ON UPPER AND LOWER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPECTION) FABRICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC. 2L72 4F4 FRTA21EA E15NE 20040505001232004050500123EA 2004 5 5 SWIA200413202 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 625 LEFT INTERCOSTAL STR 14L IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INTERCOSTAL REPLACED AT FS625 STR 14LH IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040505001242004050500124EA 2004 5 5 SWIA200413203 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 625 RIGHT INTERCOSTAL STR 14R IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) INTERCOSTAL REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040505001252004050500125EA 2004 5 5 SWIA200413204 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 RT FIREWALL SHUTOFF VALVE SUPPORT INTERCOSTAL AFT ANGLE IS CRACKED FS 654 ADJACENT STR 9. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLE IAW CRJ SRM 51-40-11, AND 51-42-06. 2L72 4F RTA21EA 20040505001262004050500126EA 2004 5 5 SWIA200413205 120040416A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 CARGO PIT FLOORBEAM ANGLE REPAIR ANGLE CRACKED AT FS 621.00 LBL 42.0. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED REPAIR ANGLE IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401. 2L72 4F RTA21EA 20040505001272004050500127EA 2004 5 5 SWIA200413206 120040416A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DISTORTED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 CARGO PIT FLOORBEAM SIDE WEB BUCKLED AND DISTORTED; FS 589.00 - FS 605.00; LBL 27.0; OUTBOARD SIDE. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED WEB IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-25-16, AND REO 601R-53-61-989 REV., RII 53-401. 2L72 4F RTA21EA 20040505001292004050500129EA 2004 5 5 SWIA200413235 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 MAIN FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE FS 484.00 LBL 36.0. (DISCOVERED DURING C-CHECK INSPECTION). REPAIRED DAMAGE AT FS 484, LBL 36, IAW CRJ REO 601R-53-41-059 REV. A. REF. RII53-401. 2L72 4F RTA21EA 20040505001312004050500131EA 2004 5 5 SWIA200413236 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL STR 14 R CRACKED. INTERCOSTAL REPAIRED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040505001332004050500133CE 2004 5 5 IJA2004F00000 120040127A324207515500 PLATE BEECH 90 B90 1152912CE PWA PT6 PT6A60A 52043NE LT BRAKE BROKEN E IJAAO OTHER O OTHER LDLANDING 1 CE07777KU LJ377 ON LANDING PILOT NOTICED LT BRAKE WAS SOFT. AFTER SHUT DOWN PILOT NOTICED THAT THE LT AFT BRAKE CALIPER WAS BROKEN IT APPEARS THAT THE LT BRAKE TORQUE PLATE LOWER AFT CALIPER ATTACH POINT BROKE WHEN THE BRAKES WERE APPLIED. 1L72 3T4 T 3A20 E4EA 20040505001352004050500135EA 2004 5 5 SWIA200413239 120040423A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 280 LEFT FLOORBEAM LBL 9.0 ATTACH ANGLE OUTBOARD CRACKED. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, AND RII 53-401. 2L72 4F RTA21EA 20040505001362004050500136EA 2004 5 5 SWIA200413240 120040423A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ANGLE REPLACED AT FS280, RBL 9.0 IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21, 51-23-00, 51-21-11, AND RII53-401. 2L72 4F RTA21EA 20040505001392004050500139EA 2004 5 5 SWIA200413242 120040423A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 625 LEFT INTERCOSTAL STR 14 LT CRACKED. 2L72 4F RTA21EA 20040505001412004050500141EA 2004 5 5 SWIA200413244 120040423A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE RBL41 CRACKED. ACCOMPLISHED REPAIR ON FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV. A. REF. RII53-401. 2L72 4F RTA21EA 20040505001432004050500143EA 2004 5 5 SWIA200413154 120040228A5210 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, PAX DOOR; STAIR SIDEWALL ATTACH ANGLE IS CRACKED BY DOOR POWER ASSIST PULLEY BRACKET (FS 341.00). CUT AWAY DAMAGED SECTION AND REPAIRED IAW REO 601R-52-11-456. 2L72 4F RTA21EA 20040505001452004050500145CE 2004 5 5 HYTA2004003 120040317A143026222442 BOLT CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA FUSELAGE CORRODED E HYTAK NONE O OTHER ININSP/MAINT 1 AL014365U13890 208B0253 WHILE CONDUCTING INITIAL INSPECTION, BOTH AFT WING TO FUSELAGE ATTACH BOLTS WERE FOUND SLIGHTLY RUSTED. DAMAGE WAS NEGLIGIBLE. THESE BOLTS AS WELL AS FORWARD ATTACH BOLTS AND UPPER AND LOWER STRUT ATTACH BOLTS WERE APPARENTLY INSTALLED DRY. THIS HARDWARE SHOULD ALL BE INSTALLED WITH A RUST INHIBITOR OR GREASE. 1H71 3T3 T A37CE E2NE 20040503001202004050300120WP 2004 5 3 AALA20040485 120040424A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217514A 49891 DEN - EMERGENCY LIGHTS ON CEILING FROM SEAT ROWS 17 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AT B5-104 FOR EMERGENCY LIGHTS ON CEILING FROM SEAT ROWS 17 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040503001272004050300127 2004 5 3 AALA20040462 420040412A25655A33073 SLIDE BOEING737 737823 13844BZNM ENTRY DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21972AN 30097 TUL - EVACUATION SLIDE AT FORWARD ENTRY DOOR FAILED TO DEPLOY AUTOMATICALLY OR MANUALLY. REPLACED EVACUATION SLIDE AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040503001282004050300128SO 2004 5 3 C2XA04SH203 120040407A532014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712922 145338 SHV- DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040503001462004050300146WP 2004 5 3 GTIA040223 120040322A3260 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP NLG DIRTY A GTIAK NONE N FALSE WARNING CLCLIMB 1 GL23833NK 49449 DTW - FLT 1874 - DURING CLIMB AFTER GEAR RETRACTION, THE RED NOSE GEAR LIGHT STAYED ON. PERFORMED QRH PROCEDURE AND THE INDICATION CORRECTED ITSELF, NOSE LANDING GEAR PIN IN COCKPIT WAS DOWN WITH HANDLE UP. FOUND PROX SWITCH DIRTY CLEANED TARGET ALSO LUBED RETRACTION HANDLE DUE TO STICKY FEEL ON TEST CHECKS GOOD. (M) 2L72 4F RTA6WE 20040503001752004050300175EU 2004 5 3 ULX2004F00002 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP23226LA433 3310 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE, AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U H9EU 20040503001772004050300177GL 2004 5 3 JJWA0055791 220040412A72406870992 COMBUST CHAMBER BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE CRACKED E JJWAO OTHER O OTHER NRNOT REPORTED 1 SO175005N7664 1931 NOTICE HIT TOT ON A NORMALLY COOL RUNNING TURBINE, OVER A PERIOD OF A FEW FLIGHTS TOT CLIMBED MORE. PERFORMED NORMAL BARFIELD TOT TESTING AND BLEED VALVE CLOSURE TESTS, THEN DID THE HAND FEEL TEST DURING START AND IDLE AND FOUND AIR LEAKAGE AT LEFT AFT AIR TUBE AREA. FOUND CRACK IN REINFORCED AIMPIT AREA OF COMBUSTION CASE. NO DAMAGE TO LINER AND GOOD PATTERN FROM FUEL NOZZLE. ORDERED COMBUSTION CASE FOR REPLACEMENT. 1G71 3U3 U H2SW E4CE 20040503002022004050300202SW 2004 5 3 YTRR094255 120040422A6330 BUSHING BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL RESTRAINT WORN B YTRAK NONE O OTHER ININSP/MAINT 1 SW0352192 52192 WORN BUSHINGS ON RESTRAINT MOUNT AT LATERAL SPRING ATTACH POINTS. 1G71 3U3 UNCH2SW E1GL 20040503002062004050300206SW 2004 5 3 ALGA094218 120040421A6220406310405101 UNIVERSAL BELL 407 407 1182206SW ALLSN 250C 250C20 03013GL MAIN ROTOR RATCHETING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03457AL285 53151 FOUND EXCESS AXIAL PLAY AND RATCHETY. UNIT REPLACED WITH NEW BY FIELD MAINT. 1G71 3U3 UO H2SW E4CE 20040503002102004050300210EU 2004 5 3 BAQA093765 120040421A3242AHA1121MOD12345 CALIPER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE WEAK E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME2611 7235 CALIPER IS WEAK, SPONGY AND LEAKING EXCESSIVELY. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/21/2004 1G72 3U3 U H13EU E5NE 20040503002112004050300211 2004 5 3 BAQA094113 420040412A34215040122902 INDICATOR UROCOPEC135 EC135P1 8680990EU ATTITUDE MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF1089 0140 BACKLIGHTING OUT ON UNIT. REPLACED WITH SERVICABLE UNIT. 04/22/2004 1G72 3U O H88EU 20040503002292004050300229EU 2004 5 3 BAQA094251 120040404A249745023502 MASTER SWITCH UROCOPEC135 EC135T1 5620026EU PWA PW206 PW206A NE COCKPIT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135WJ1584 0298 WARRANTY. NR 2 BUS TIE OPEN ON UNIT. THIS UNIT WAS INSTALLED BY HDS AT 11.4 HRS. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/26/2004 1G72 3U3 U H88EU E42NE 20040503002412004050300241NM 2004 5 3 ASAA0410134 120040317A53156546811504 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM AT STATION 1006 CORRODED ON UPPER CHORD. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002562004050300256NM 2004 5 3 ASAA0410139 120040317A5347655496914 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CABIN SEAT TRACK BOTTOM SIDE CORRODED AT STATION 907. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002612004050300261NM 2004 5 3 ASAA0410146 120040317A53156546568145 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM UPPER CHORD IS CORRODED AT STATION 1016. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002802004050300280NM 2004 5 3 ASAA0410151 120040323A5320655162822 STRUCTURE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND OVERSIZED HOLE AT STRINGER 23L. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002912004050300291WP 2004 5 3 GTIA040240 120040327A2560 FLASHLIGHT DOUG DC9 DC983 3022083WP FWD GALLEY OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 LGA - FLT 709 - FOUND FORWARD GALLEY FLASHLIGHT FELL OUT OF ITS HOLDER. RESECURED FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT ASSEMBLY. NO FURTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040503002932004050300293 2004 5 3 GTIA040230 420040104A2565 PIN DOUG DC9 DC983 3022083WP TAILCONE OUT OF POSITION A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND TAILCONE SLIDE WILL NOT DEPLOY WHEN TAILCONE IS RELEASED. REPOSITIONED CLEVIS TOGGLE PINS ON AFT EMERGENCY EXIT SLIDE. (M) 2L72 4F RTA6WE 20040503003032004050300303SO 2004 5 3 SIMA200408802 120040326A27403621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO E/E BAY FAULTY A SIMAK NONE J WARNING INDICATION DEDESCENT 1 SW21720AE 145279 BNA- FLT 4856 - CREW REPORTED A DUAL PITCH TRIM FAIL ON DESCENT. AUTOPILOT WAS ON AND DID NOT TOUCH ANYTHING. RECEIVED FAILURE OF MAIN AND BACK UP PITCH TRIM AND 16000 FT. AFTER LANDING CYCLED C/B AND FAILURE WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040503003062004050300306SO 2004 5 3 SIMA200408601 120040322A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZ STAB MALFUNCTIONED A SIMAK NONE J WARNING INDICATION APAPPROACH 1 SW21813AE 145539 YYZ- FLT 4904 - DURING APPROACH WHEN AUTO PILOT WAS DISCONNECTED, PITCH TRIM 1-2 INOPERATIVE MESSAGE CAME ON EICAS. STAYED ON FOR A FEW SECONDS THEN WENT OUT. BOTH PITCH TRIM SWITCHES WORKED. LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE COMPLIED WITH ETN EB 27-022. THE HSCU WAS REMOVED AND REPLACED IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040503003172004050300317WP 2004 5 3 GTIA040215 120040229A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FLOOR SUPPORT CORRODED AT STATION 1251 LBL 40. REMOVED DAMAGED FLOOR SUPPORT. LOCATE AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040503003232004050300323EA 2004 5 3 ASOA04235 120040321A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE OUTBOARD CLIP AND INTERCOSTAL AT FS 484, RBL 27, IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040504000012004050400001EA 2004 5 4 A6WA200440045 120040417A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE DENTED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31463AW 7878 FORWARD SERVICE DOOR JAMMED. TWO DENTS FORWARD OF RT FORWARD SERVICE DOOR. DENTS OUT OF LIMITS. COMPLIED WITH REPAIR BRAS EO 601R-53-4835 STEPS 1, 2, 3, 4 AND 5. PERFORMED REPAIR OF SERVICE DOOR STRINGER 16/17 OF FIG 245 AND STRINGER 13/14 FIG 295. (M) 2L72 4F4 FRTA21EA E15NE 20040504000262004050400026EA 2004 5 4 ASOA04240 120040323A335058351 COVER CNDAIRCL600 CL6002B19 1900309EA CABIN DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 FLT 4413 - DURING A GROUND INSPECTION IN ATL, THE REAR EMERGENCY FLOOR LIGHT STRIP AND COVER WERE FOUND DAMAGED. MAINTENANCE RECONNECTED THE REAR EMERGENCY FLOOR LIGHT STRIP AND REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT COVER (P/N 5835-1). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040504000302004050400030EA 2004 5 4 ASOA04239 120040322A3250 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA STEERING SYS MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11702EV 10035 FLT 4195 - DURING CLIMB-OUT FROM DFW-DCA, UPON GEAR RETRACTION THE CREW RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE RESET THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT AND THE MESSAGE CLEARED. MAINTENANCE ALSO PERFORMED OPS CHECKS OF THE STEERING SYSTEM AND PERFORMED GEAR RETRACTIONS/EXTENSIONS WITH THE STEERING ENGAGED. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040504000522004050400052CE 2004 5 4 IL32004F00000 120040318A5330 DOUBLER BEECH 55 T42A CE FUSELAGE MISINSTALLED B IL3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP0712VB ANTENNA WAS SECURED ON UPPER FUSELAGE SKIN WITH FOUR SCREWS. ONE OF SCREWS WENT THROUGH SKIN AND 6 INCH WIDE HAT SEC STRUCTL DBLR. SCREW HOLE WAS DRILLED THRU DBLR RISER RADIUS. NUT HAD LG GAP UNDER IT ON SIDE AWAY FROM RADIUS. SCREW HOLE WAS DRILLED THROUGH SKIN, VERY CLOSE TO DBLR RISER. WHEN INSTALLED SCREW (2 IN TOO LONG), BENT RISER STIFFENER OUT OF WAY TO SCREW WOULD CLEAR IT. RISER STIFFENER WAS CRACKED WHERE BENT, PLIER MARKS. USED LONG SCREW, BENT RISER STIFFENER BECAUSE HOLE WAS SO CLOSE TO RISER, COULD NOT GET NUT STARTED ON SHORT SCREW. OTHER TWO SCREWS WERE INSTALLED THROUGH SKIN AND .0625 PIECE TEFLON. THREADS OF SCREW WERE HALF WAY THROUGH NUT. OTHER SCREW WAS 2 OR 3 THREADS SHORT. 1L72 3O 3A16 20040504000782004050400078EA 2004 5 4 WVE2004F00009 120040419A5320601R311719 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A WVERK NONE O OTHER ININSP/MAINT 1 EA09408SW 7055 FS 484 WATERLINE 73 RBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R311719 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997) 2L72 4F4 FRTA21EA E15NE 20040504000852004050400085 2004 5 4 USA2004F00013 420040228A3417HG480B42 ADC BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE E/E BAY FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19356US40307 23559 SHORTLY AFTER TAKEOFF, ENROUTE, ALL THE CAPTAINS AIR AND FLIGHT INSTRUMENTS FAILED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AIR DATA COMPUTER. PERFORMED SATISFACTORY FUNCTIONAL CHECK IAW MM AND LAND VERIFY TEST IAW R5 JOB CARD. 2L72 4F4 FRTA16WE E2GL 20040505000102004050500010EU 2004 5 5 PG9R118895 120040205A7160350A54108005 INTAKE UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE AIR INTAKE CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19135PH531 3695 AIR INTAKE CRACKED WITH ONLY 531.8 HOUR. (RMA NR R046964) 1G72 3U3 U H9EU E00054EN 20040505000142004050500014EU 2004 5 5 PG9R117581A 120040119A5340350A21004828 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE FUSELAGE CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19135PH509 3695 FORWARD FITTINGS CRACKED. (RMA NR R046607) 1G72 3U3 U H9EU E00054EN 20040505000172004050500017CE 2004 5 5 GM0408 120040413A3411 PITOT TUBE CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP PITOT/STATIC SYSOBSTRUCTED E UG8AO OTHER P NO WARNING INDICATION CLCLIMB 1 GL235117 6507064 AFTER ROTATION, CREW NOTICED A LOSS OF AIRSPEED INDICATION ON THE PILOT`S INDICATOR ONLY. FLAP OVERSPEED LIGHT ILLUMINATED. ALSO THE AUTOPILOT AND YAW DAMPENER WOULD NOT ENGAGE. TROUBLESHOOTING POINTED TO A LACK OF AIRSPEED INDICATION FROM THE LT SIDE AIR DATA COMPUTER. THE PITOT TUBE AND ASSOCIATED TUBING WERE CLEARED OF DEBRIS. A PITOT/STATIC CHECK WAS PERFORMED WITH NO ABNORMALITIES NOTED. OPERATION OF ALL ASSOCIATED SYSTEMS WERE NORMAL. AC WAS RELEASED FOR FLIGHT. 2L72 4F4 F A9NM E6WE 20040505000182004050500018CE 2004 5 5 N4J2004F00000 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE T/R ACTUATOR CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15600GG2381 115 T/R ACTUATOR SUPPORT BEAM CRACKED. PART WAS REPLACED MAY 2002. 2L72 4F4 FRTA10CE E35NE 20040505000342004050500034EU 2004 5 5 UO22004F00003 120040301A28222070C11 PUMP BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP FUEL SYSTEM FAILED B UO2RO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL1946WC NA0334 RT BOOST PUMP FAILED AND LOW FUEL PRESSURE LIGHT CAME ON. PUMP HAD APPROXIMATE 1500 HOURS SINCE LAST OVERHAUL. PROBABLE CAUSE WAS DETERIORATED BRUSHES IN PUMP. 2L72 4F4 F A3EU E6WE 20040505000372004050500037CE 2004 5 5 UJJ2004F00000 120040217A531297524030711 ADAPTER BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA AFT BULKHEAD CRACKED B UJJRK NONE O OTHER ININSP/MAINT 1 WP01160SF3918 BB32 WHILE INVESTIGATING CABIN PRESSURE LEAKS, IT WAS FOUND THAT BOTH AFT PRESSURE BULKHEAD RUDDER CARRY THROUGH SEAL ADAPTERS WERE CRACKED IN SEVERAL PLACES. THESE ADAPTERS ARE MADE OF THERMOFORMED (ABS) PLASTIC, RIVETED INTO PLACE USING A METAL DOUBLER, AND HAVE A METAL BRACKET RIVETED TO THEM. MOST OF THE CRACKS BEGAN AT THE OUTER RIVET HOLES AND PROCEEDED TOWARDS THE CENTER HOLE AREA, SEVERAL NEARLY CONVERGING. APPEARS THAT RIVETS ARE CONTRIBUTING TO THE FORMATION OF CRACKS WHEN THEY ARE DRIVEN OR SQUEEZED INTO PLACE, EXPANDING IN THE HOLES, AND DIMPLING THE PLASTIC. IF CRACKS CONVERGED, LARGE CHUNKS OF THE PLASTIC COULD HAVE BLOWN OUT DUMPING CABIN PRESSURE. (WP01200407837) 1L72 4T4 T A24CE E4EA 20040505000582004050500058EA 2004 5 5 04102709 120040411A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA STAB TRIM INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27709BR 7352 DURING CRUISE OF FLIGHT 7352 CREW REPORTED STAB/MACH TRIM FAIL MESSAGES. CREW DIVERTED TO NEAREST SUITABLE LANDING FIELD AND FLIGHT LANDED UNEVENTFULLY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT AND TRIM ACTUATOR WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040505000632004050500063NE 2004 5 5 04111415 220040420A753231B1575601 BLEED VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE COMPRESSOR INOPERATIVE A VTZAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 EA27415FJ 3170 CD0066 DURING CLIMB OF FLIGHT 6138 CREW REPORTED A LOUD BANG FROM THE RIGHT HAND ENGINE WITH N1 AND N2 INDICATIONS SLOWLY DECREASING. THE ENGINE WAS SHUTDOWN AND EMERGENCY DECLARED. THE FLIGHT LANDED UNEVENTFULLY AND PAASENGERS DEPLANED NORMALLY. THE PRELIMNARY CAUSE IS SUSPECTED TO BE A COMPRESSOR STALL CAUSED BY AN ENGINE BLEED OVER VALVE FAILURE. AIRCRAFT IS CURRENTLY UNDER MAINTENANCE REPAIR TO DETERMINE EXACT CAUSE OF ENGINE FAILURE A SUPPLEMENTAL REPORT WILL BE SUBMITTED 2H72 4T4 FRTA55NM E35NE 20040505000762004050500076NM 2004 5 5 P762004F00002 120040219A552465229905 BRACKET BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE LT ELEVATOR CRACKED A P76AO OTHER O OTHER NRNOT REPORTED 1 SO17894AA59612 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2L73 4F4 FRTA3WE E2EA 20040505000832004050500083EA 2004 5 5 04096624 120040405A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 DURING INSPECTION THE LEFT HAND FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000862004050500086EA 2004 5 5 04109685 120040418A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27685BR 7712 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000892004050500089EA 2004 5 5 04111710 120040420A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE RIGHT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND INOEPRATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000932004050500093NE 2004 5 5 O2G2004F00000 220040127A7260 GEARBOX LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE RT ENGINE FAILED E O2GAO OTHER J WARNING INDICATION DEDESCENT 1 NE0314TU 026 RT ENGINE CHIP LIGHT FLICKERED JUST PRIOR TO DECENT. AC LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW PULLED RT ENGINE CHIP DETECTOR AND FOUND BOLT AND LOCK RING RESTING IN CHIP DETECTOR SCREEN ENCLOSURE. REPLACED ACCESSORY GEARBOX. (NE03200407105) 2L72 4F4 FRTA10CE E35NE 20040505000952004050500095CE 2004 5 5 N4J2004F00001 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE THRUST REVERSER CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15600GG2381 115 RT OB T/R ACTUATOR SUPPORT BEAM CRACKED. PART WAS REPLACED MAY 2002. 2L72 4F4 FRTA10CE E35NE 20040505000982004050500098CE 2004 5 5 N4J2004F00005 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE THRUST REVERSER CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15601GG1187 192 RT OB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2L72 4F4 FRTA10CE E35NE 20040505000992004050500099EA 2004 5 5 SWIA200413184 120040413A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, FUSELAGE LEFT VERTICAL BEAM LOWER OUTBOARD FLANGE CRACKED AT FS 409 + 128 LBL 18. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 REV. NC, RII53-401. 2L72 4F RTA21EA 20040505001012004050500101EA 2004 5 5 SWIA200413185 120040413A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE ATTACH CLIP CRACKED FS 280.00 RBL 9 OUTBOARD. REPLACED CLIP IAW CRJ REO 601R-53-11-171 REV. NC AND RII53-401. 2L72 4F RTA21EA 20040505001342004050500134EA 2004 5 5 SWIA200413238 120040416A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 DISCOVERED DURING C-CHECK INSPECTION, FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 CRACKED. ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII53-401. 2L72 4F RTA21EA 20040505001372004050500137EA 2004 5 5 SWIA200413241 120040423A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 484 INTERCOSTAL OUTBOARD FLANGE LBL36 CRACKED. ACCOMPLISHED REPAIR IAW CRJ REO 601R-53-41-059 REV. A. REF. RII 53-401. 2L72 4F RTA21EA 20040505001502004050500150EA 2004 5 5 SWIA200413208 120040416A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT; FUSELAGE FRAME AT FS 605.00 HAS 2 CRACKED FLANGES THAT ATTACH TO STR 18L. 2L72 4F RTA21EA 20040505001512004050500151CE 2004 5 5 HYTA2004005 120040317A321026410143 SPRING CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA MLG WORN A HYTAO OTHER O OTHER NRNOT REPORTED 1 AL014365U13890 208B0253 FLEXING OF MLG CENTER SPRING PN 2641014-3 CAUSES CENTER SPRING TO CONTACT MLG COVER PN 2611103-10 WHICH IS LOCATED BENEATH THE CENTER SPRING. CHAFING HAD WORN THROUGH THE PAINT ON THE LOWER SURFACE OF CENTER SPRING. TWO RIVETS HAD WORN INTO THE LOWER SURFACE OF THE CENTER SPRING. THESE RIVETS ARE THE CENTER IB RIVETS THAT FASTEN A FAIRING AT EACH END OF THE COVER. SUGGEST ELIMINATING THE CENTER RIVET AND INSTALL TWO RIVETS FURTHER OB AND OFF CENTER. ALSO APPLY CHAFE TAPE TO LOWER SURFACE OF CENTER SPRING. 1H71 3T3 T A37CE E2NE 20040505001562004050500156CE 2004 5 5 GUU2004F00002 120040227A2697 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA FIRE BOTTLE DIRTY A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1787555 UE234 DURING FLIGHT, NR 2 ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS INTERMITTENTLY, CONTINUED. INSPECTED AND CLEANED WIRES ON NR 2 FIRE BOTTLE. COULD NOT DUPLICATE. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E4EA 20040505001572004050500157NM 2004 5 5 GTIA040318 120040424A5321 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23836NK 53045 MAIN CB STA 446 TO 466 RT SIDE MID FLOOR PANEL HAS CRACKED/DAMAGE ON EDGE. 2L72 4F RT 20040505001582004050500158NM 2004 5 5 GTIA040319 120040322A5320 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23836NK 53045 LT MAIN CABIN CUSP WEB STA 229 IS CRACKED. REMOVED CUSP WEB SECTION. FABRICATED NEW CUSP WEB. INSTALLED CUSP WEB. 2L72 4F RT 20040505001592004050500159NM 2004 5 5 GTIA040316 120040414A5321 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23836NK 53045 MAIN CB STA 1079 TO STA1136, LBL 24 INCH TO 44 INCHES FLOOR PANEL HAS CRACKED ON EDGE/ SEVERAL INSERTS CORRODED. 2L72 4F RT 20040505001632004050500163CE 2004 5 5 FTU2004F00002 120040407A272112606421 CHAIN CESSNA206 T206H 2073303CE LYC O540 TIO540* 41532EA RUDDER TRIM MISINSTALLED B FTURK NONE O OTHER ININSP/MAINT 1 NE05989MD442 T20608091 FIRST TIME AC WAS IN OUR SHOP DURING AN ANNUAL INSP, THE RUDDER TRIM CHAIN IN THE CENTER PEDESTAL WAS FOUND NOT INSTALLED CORRECTLY. WERE THE CHAIN IS SUPPOSE TO RIDE OVER THE IDLER TENSIONING SPROCKET, IT WAS FOUND OFF THE SPROCKET AND JUST RESTING ON THE SPROCKET SHAFT. IDLER TENSION WAS CORRECT AND TRIM SYSTEM WAS WORKING. NO APPARENT DAMAGE WAS FOUND CHAIN REINSTALLED CORRECTLY AND SYSTEM OPS CHECKED GOOD. 1H71 3O3 ORTA4CE E14EA 20040505001642004050500164SO 2004 5 5 FPI2004F00002 220040325A8520821016R CRANKCASE CESSNA210 T210N 2073456CE CONT O550 IO550* SO ENGINE CRACKED E FPIAO OTHER O OTHER NRNOT REPORTED 1 SO154702C 21063591 821016R RT CASE CRACKED AT CYLINDER NR 1. 7TH STUD LOWER RECESS IN CASE. 1H71 3O3 O 3A21 E3SO 20040505001652004050500165CE 2004 5 5 FMAA2004001 120040330A1430NAS464PA42 BOLT CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO NLG BROKEN E FMAAO OTHER O OTHER NRNOT REPORTED 1 AL01734GW500 U20604832 567534 THE HEAD OF THE BOLT ATTACHING THE REAR OF THE NOSE GEAR DRAG LINK TO THE AIRCRAFT WAS FOUND LAYING IN THE NOSE GEAR WELL. THIS BOLT IS IN A SHEAR LOAD AND SHOULD NOT HAVE BEEN SUBJECT TO ANY FORCES THAT WOULD FORCE THE HEAD OF THE BOLT TO THE POINT OF CRACKING OFF. 1H71 3O3 O A4CE E5CE 20040505001662004050500166CE 2004 5 5 FIP2004F00000 120040416A7921654585 FLANGE CESSNA210 T210N 2073456CE CONT O550 IO550* SO OIL COOLER CRACKED E FIPAO OTHER O OTHER NRNOT REPORTED 1 CE032145U 21064776 821012R TOP MOUNT EAR AND IB BAFFLE FLANGE CRACKED UNDER NORMAL OPERATING CONDITIONS. 1H71 3O3 O 3A21 E3SO 20040505001672004050500167SO 2004 5 5 ET72004F00000 120040331A71101159P204272 HEAT SHIELD GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU RT COWLING DELAMINATED E ET7AO OTHER O OTHER NRNOT REPORTED 1 WP01668JT10889 162 NOTED HEAT SHIELD HAS DISBONDED FROM RT FIX COWL OUTER SKIN AT APPROX FS 596.0 TO NACELLE STATION 179.0 (OIL CAN). INSPECTION OF FIX COWL INTERIOR (INNER SKIN CORE) AT FS 596.0 TO NACELLE STATION 179.0. NO DEFECTS NOTED. FOUND DELAMINATION ON INNER SKIN CORE AT NACELLE STATION 140.0 TO NACELLE STATION 179.0 APPROX. DELAMINATION IS APPROX 20.0 INCHES X 8.0 INCHES. END 2L72 4F4 FRTA12EA E2EU 20040505001682004050500168WP 2004 5 5 ESU2004F00000 220040229A7261 CARBON SEAL LEAR 35 35A 5170602CE GARRTTTFE731TFE7312B WP NR 1 ENGINE LEAKING E ESUAO OTHER K FLUID LOSS NRNOT REPORTED 1 CE03274JS 274 P73192 UPON COMPLETION OF A FOUR POINT RUN AND CASE PRESSURE CHECK IT WAS NOTED THAT THE NR 3 AND NR 4, CARBON SEALS WERE LEAKING. THIS REQUIRED AND ENGINE CHANGE OF NR 1 ENGINE. 2L72 4F4 F A10CE E6WE 20040505001712004050500171CE 2004 5 5 E812004F00004 120040315A5730101120017119 SKIN PANEL BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA LT WING DAMAGED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL03355TW7458 BB521 NOTED LOOSE/DAMAGED RIVETS ATTACHING LT WING CENTER SECTION UPPER LEADING EDGE SKIN PANEL. UPON REMOVAL FOR SKIN PANEL REPLACEMENT, NOTED PANEL ATTACHED IN SEVERAL PLACES WITH MS20426AD TYPE RIVETS WHERE NAS1097 RIVETS ATTACHED ORIGINALLY. SKIN RIVET ATTACH HOLES WORN/ELONGATED. ALSO NOTED MINOR CRACKING IN WS 46.50, WS 56.00, WS 65.50, AND WS 75.50 WEBS IN UPPER FLANGES AT INTERSECTION WITH PN 101120017115 UPPER STRINGER. SUSPECT CAUSED BY COMBINATION OF NORMAL FATIGUE STRESS IN PROP BLAST AREA COMBINED WITH WORN/OVER COUNTERSUNK ATTACH FASTENER HOLES. PROP OUT OF BALANCE CONDITION MAY AGGRAVATE SITUATION. 1L72 4T3 T A24CE E2NE 20040505001742004050500174NM 2004 5 5 ASAA0440012 120040122A531565498843 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING SCHEDULED MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT BS 967. REPAIR IAW EA. (M) 2L72 4F RTA16WE 20040505001752004050500175NM 2004 5 5 ASAA0410083 120040216A531165465251 FRAME BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE, FOUND CORROSION IN E/E BAY AT FS 380. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040505001762004050500176NE 2004 5 5 MALA040342 220040422A7320219333010 HMA BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 ENGINE FAILED A MALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL15530XJ E2364 NR 3 ENGINE SHUTDOWN INFLIGHT. NR 3 ENG FAILED AT 270 NO WARNINGS OR FAULT BEFORE OR AFTER FAILURE RIGHT LOW FEED LEVEL ILLUMINATED JUST BEFORE LANDING. MAINTENANCE REPLACED HMA P/N ON 2-193-330-10. OPS CHECK GOOD. 2H74 4F4 FRTA49EU E6NE 20040505001772004050500177NE 2004 5 5 MALA040343 220040424A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT OVERTEMP A MALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15416XJ 340B416 LEFT ENGINE OVER TEMPED INFLIGHT. CLIMBING THROUGH 8000 FT LEFT ENG FAILED APPEARED TO HAVE COMPRESSOR STALL. TORQUE WAS LESS THAN 10 PERCENT ITT WAS 1200-1300C (QRH COMPLETE WITH SHUTDOWN ENG) AIR RETURN TO MSP. REMOVED AND REPLACED ENG IAW JC 7100-301. P/N ON/OFF CT7-9B, S/N OFF GE-E 785765, S/N ON GE-E785567, OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20040505001792004050500179NM 2004 5 5 ASAA0410077 120040215A533065468823 SKIN BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DENTS BELOW STRINGER 24L AND STATION 1076. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001802004050500180NM 2004 5 5 ASAA0410078 120040215A533065468823 SKIN BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DENT AT STATION 1037. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001812004050500181NM 2004 5 5 ASAA0410079 120040215A533065468813 SKIN BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DENT AT STATION 1038. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001822004050500182NM 2004 5 5 ASAA0410081 120040216A53306545800742 SKIN BOEING737 737210C 1384459NM FS DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND EXISTING REPAIR AT STATION 280 TO 312 AND STRINGER 19R DAMAGED. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001842004050500184NM 2004 5 5 ASAA0410070 120040215A533065468811 SKIN PANEL BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 1050-1060, STRINGER 27L-27R DENTED. REPAIRED PER SRM AND EA. (M) 2L72 4F A16WE 20040505001862004050500186NM 2004 5 5 ASAA0440033 120040204A5315BAC14902857 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND STATION 360 RBL 39 TO RBL 55 FLOORBEAM HAS CORROSION TOP AND BOTTOM AROUND SCREW HOLES, GALLEY AND SEAT TRACK FITTINGS. REMOVED CORROSION AND CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. FABRICATED 2 AND 3 AND FILLER PARTS PER SRM 53-30-51 AT STATION 360, RBL 89 TO RBL 55. (M) 2L72 4F RTA16WE 20040505001872004050500187NM 2004 5 5 ASAA0440037 120040204A5320654795766 WEB BOEING737 7374Q8 138447QNM FS GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - AFT CARGO PIT DOOR SILL SUPPORT WEB HAS TOOLING MARKS ON OUTBOARD SIDE. REPLACED WEB PER SRM 53-60-15. (M) 2L72 4F RTA16WE 20040505001882004050500188NM 2004 5 5 ASAA0410084 120040216A53306545778 SKIN BOEING737 737210C 1384459NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND DAMAGE TO EXISTING REPAIR AT STATION 867. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001932004050500193NM 2004 5 5 ASAA0410088 120040216A53306546595532 SKIN BOEING737 737210C 1384459NM FUSELAGE BULGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SKIN BULGE AT STRINGER 27L AND STATION 727. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001962004050500196NM 2004 5 5 ASAA0410076 120040215A53116545829 FRAME BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND CHORD DAMAGE BULGE CORROSION AT STATION 327. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040505001972004050500197NM 2004 5 5 ASAA0410071 120040215A53306546881 SKIN PANEL BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 1016-1040, STRINGER 26L-27R DENTED. REPAIRED PER SRM AND EA. (M) 2L72 4F A16WE 20040505001992004050500199NM 2004 5 5 ASAA0410073 120040215A53116547955528 FRAME BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT BS 807, STRINGER 26L-26R CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002002004050500200NM 2004 5 5 ASAA0410059 120040210A533065458001 SKIN PANEL BOEING737 737210C 1384459NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 244-252, STRINGER 24R DENTED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002022004050500202NM 2004 5 5 ASAA0410060 120040210A5313655292857 STRINGER BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 20L AT BS 847 CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002032004050500203NM 2004 5 5 SWAA041247 120040503A53106545810 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT R1 DOOR BELOW THE SILL, CORRODED. REMOVED AND REPLACED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040505002052004050500205NM 2004 5 5 SWAA041249 120040503A575465C26610218 WEDGE BOEING737 737317 138447PNM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F RTA16WE 20040505002092004050500209NM 2004 5 5 ASAA0410058 120040209A53306545830120 SKIN PANEL BOEING737 737210C 1384459NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE SKIN PANEL AT BS 328-344, STRINGER 28R-28L CHAFED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002122004050500212NM 2004 5 5 ASAA0410050 120040206A53106546526501 SHEAR TIE BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 400, STRINGER 17L CRACKED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002152004050500215NM 2004 5 5 ASAA0410067 120040213A3350900542 BATTERY BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC - DURING INSPECTION, FOUND THE EXIT IDENTIFIER IN THE MID CABIN INOPERATIVE. REPLACED BATTERY AND REPAIRED WIRE, THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040505002162004050500216NM 2004 5 5 ASAA0410061 120040210A5313654576717 STRINGER BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 25L AT BS 470-500B PLUS 10 CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002182004050500218NM 2004 5 5 ASAA0410064 120040210A53116547955528 FRAME BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE FRAME AT BS 887, STRINGER 24L-25L CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002492004050500249NM 2004 5 5 SWAA041217 120040429A5311CLAD7075T6 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 297, STRINGER 17R, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040505002512004050500251NM 2004 5 5 SWAA041219 120040429A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE AT BS 827, LBL 6 TO RBL 6, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040505002532004050500253NM 2004 5 5 SWAA041221 120040429A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 360, ABOVE AND BELOW STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002552004050500255NM 2004 5 5 SWAA041223 120040429A3350101114 LIGHT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20040505002572004050500257NM 2004 5 5 SWAA041225 120040429A3350311500 LENS BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT BULLNOSE LENS BETWEEN ROWS 16 DEF AND 17 DEF, LOOSE. SECURED BULLNOSE LIGHT LENS PER MM. 2L72 4F RTA16WE 20040505002592004050500259NM 2004 5 5 SWAA041168 120040426A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT MLG WHEEL WELL CEILING BEADED PRESSURE WEB AT BS 663 TO BS 672, LBL 32, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20040505002612004050500261NM 2004 5 5 SWAA041170 120040426A532065C30926 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL BEAM FITTING AT BS 727, LBL 18, CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20040505002632004050500263NM 2004 5 5 SWAA041172 120040426A531465621257 KEELBEAM BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM AT BS 510 TO BS 520, CORRODED. REPAIRED KEEL BEAM PER EA. 2L72 4F RTA16WE 20040505002652004050500265NM 2004 5 5 SWAA041174 120040426A52306547952 SKIN BOEING737 7373Y0 1384671NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN AT UPPER AFT CUTOUT FOR HANDLE, CRACKED. REPAIRED CARGO DOOR SKIN PER EA. 2L72 4F RTA16WE 20040505002672004050500267NM 2004 5 5 SWAA041176 120040426A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D CHECK, FOUND KEEL BEAM CHORD AT BS 727 TO BS 727 + 15, RBL 8 TO LBL 8, CORRODED. REPAIRED KEEL BEAM CHORD PER ER. 2L72 4F RTA16WE 20040505002692004050500269NM 2004 5 5 SWAA041179 120040426A25606557463 FITTING BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FITTINGS CORRODED. REPAIRED GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20040505002702004050500270NM 2004 5 5 SWAA041182 120040426A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FWD CARGO COMPARTMENT AT BS 500 B + 16, TO 430, STRINGER 27 L, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040505002712004050500271NM 2004 5 5 SWAA041183 120040426A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 500 D, STR 8 R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040505002722004050500272NM 2004 5 5 SWAA041161 120040423A533065621258 SKIN BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 28R, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040505002732004050500273NM 2004 5 5 SWAA041162 120040426A33501103229 COVER BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 L1 DOOR LOWER EMERGENCY LIGHT COVER LOOSE. SECURED LIGHT COVER PER MM. 2L72 4F RTA16WE 20040505002742004050500274NM 2004 5 5 SWAA041163 120040426A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 787, RBL 9, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040505002752004050500275NM 2004 5 5 SWAA041164 120040426A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT AT BS 867 TO BS 907 STRINGER 26R, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040505002762004050500276NM 2004 5 5 SWAA041165 120040426A3350311500 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 9 DEF. SECURED LENS PER MM. 2L72 4F RTA16WE 20040505002772004050500277NM 2004 5 5 SWAA041166 120040426A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 907, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040505002782004050500278NM 2004 5 5 SWAA041185 120040426A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 1006, LBL 6, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040505002792004050500279NM 2004 5 5 SWAA041186 120040426A53206553698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 907, STR 21L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040505002802004050500280NM 2004 5 5 SWAA041196 120040428A335065C27093 LIGHT BOEING737 7372T4 1384492NM CABIN OUT OF POSITION A SWAAK NONE O OTHER NRNOT REPORTED 1 SW29722WN 22698 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT FELL OUT IN FLIGHT. INSTALLED OVERHEAD LIGHT PER MM. 2L72 4F A16WE 20040505002822004050500282NM 2004 5 5 SWAA041198 120040428A3350101114 COVER BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 LEFT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2L72 4F RTA16WE 20040505002842004050500284NM 2004 5 5 SWAA041200 120040428A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 11R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040505002912004050500291NM 2004 5 5 SWAA041191 120040427A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002922004050500292 2004 5 5 SWAA041192 420040427A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040505002932004050500293NM 2004 5 5 SWAA041193 120040427A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 520, LBL 64, CRACKED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040505002942004050500294NM 2004 5 5 SWAA041194 120040427A575465737145 SKIN BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT SKIN AT INBOARD EDGE CRACKED. REPAIRED SLAT SKIN PER EA. 2L72 4F RTA16WE 20040505002952004050500295NM 2004 5 5 SWAA041195 120040427A53106545810 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT L1 DOOR CUTOUT, LOWER STOP FITTING CRACKED. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20040503002712004050300271NM 2004 5 3 ASAA0410144 120040317A5340693535219 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STRINGER TIE CLIP CORRODED AT FS 967. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040503002822004050300282EA 2004 5 3 WVE2004F00003 120040319A5320601R3117127 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERK NONE O OTHER NRNOT REPORTED 1 EA09408SW 7055 FS 484 WATERLINE 73 LBL 9 OB INTERCOSTAL ATTACHMENT ANGLE PN 601R3117127 IS CRACKED .2500 INCH. PROBABLE CAUSE: STRESS (EA09200401997) 2L72 4F4 FRTA21EA E15NE 20040503002832004050300283EA 2004 5 3 WVE2004F00005 120040420A53466013500661 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERK NONE O OTHER NRNOT REPORTED 1 EA09408SW 7055 ENGINE SUPPORT BEAM LEFT UPPER ATTACHMENT ANGLE (PN 6013500661) AT FS 640, WL 115, LBL 45, STRINGER 9 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200401997) 2L72 4F4 FRTA21EA E15NE 20040503002872004050300287WP 2004 5 3 GTIA040209 120040318A2560 PIN DOUG DC9 DC983 3022083WP L1 DOOR OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 ACY - FLT 259 - FOUND L1 DOOR SLIDE PACK GIRT BAR RELEASE PIN NEEDS TO BE RESET. REINSTALLED GIRT BAR RELEASE PIN. SLIDE DID NOT COME OFF DOOR. (M) 2L72 4F RTA6WE 20040503002942004050300294WP 2004 5 3 GTIA040231 120040224A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND MIDPIT LONGERON 28R CORRODED AT FS 617 AROUND FASTENER HOLE. REMOVED LONGERON 28R STATION 588 TO 628. FABRICATED LONGERON. INSTALLED LONGERON. (M) 2L72 4F A6WE 20040503003052004050300305NM 2004 5 3 GAIA04058ST 120040326A532065317731 SUPPORT BOEING727 727223 1384074NM FUSELAGE CORRODED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 DURING C-CHECK, FOUND CORROSION ON THE REINFORCEMENT CHORD AT FUSELAGE STATION 1176.9 RBL 62.5. REMOVED AND REPLACED REINFORCEMENT CHORD IAW BOEING 727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040503003112004050300311NM 2004 5 3 GTIA040228 120040305A2560 COVER DOUG MD80 MD83 3023681NM L1 DOOR OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 FLL - FLT 702 - FOUND L1 DOOR SLIDE LOOSE. ADJUSTED L1 DOOR SLIDE COVER. OK FOR SERVICE. (M) 2L72 4F RT 20040503003132004050300313WP 2004 5 3 GTIA040236 120040115A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 FTW - FOUND LEFT FLOOR PANEL STATION 200-256 DELAMINATED AND TWO EACH INSERTS MISSING. FABRICATED NEW PANEL. (M) 2L72 4F RTA6WE 20040503003242004050300324EA 2004 5 3 ASOA04234 120040321A5320601R31171179 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 28 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 484, LBL 28 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040504000042004050400004EU 2004 5 4 ULX2004F00001 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01217LA2391 3311 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE-AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION-USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U3 U H9EU E19EU 20040504000272004050400027EA 2004 5 4 ASOA04238 120040322A33504871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN UNSECURE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01853AS 7374 FLT 4583 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS TWO THROUGH SEVEN WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT CONNECTORS BETWEEN ROWS TWO THROUGH SEVEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040504000382004050400038NM 2004 5 4 ASAA0410160 120040323A53126546568 BULKHEAD BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PRESSURE BULKHEAD CORRODED ALONG AFT SIDE OF FRAME 1016. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000392004050400039NM 2004 5 4 ASAA0410159 120040323A5347655496921 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND SEAT TRACK CORROSION AT STATION 867-920. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000422004050400042EA 2004 5 4 ASOA04233 120040321A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM AT BL 0 FIRE LOOP BRACKET IS CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040504000452004050400045NM 2004 5 4 ASAA0410153 120040323A532069407771 INTERCOSTAL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT INTERCOSTAL CORRODED AT STRINGER 21L. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040504000502004050400050WP 2004 5 4 GTIA040244 120040111A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23834NK 49847 TW - FOUND MAIN CABIN STATION 875 TO 1309 LBL 44 INCHES SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORROSION, BARE METAL. SEAT TRACK AT STATION 1031 TO 937 WAS FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F RTA6WE 20040504000552004050400055EU 2004 5 4 TRB2004F00012 120040306A2613RP17100 OVERHEAT SENSOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT NACELLE FAULTY A TRBAO OTHER N FALSE WARNING TOTAKEOFF 1 SO21438AT 438 DURING TAKEOFF ROLL THE RT ENGINE NACELLE OVERHEAT WARNING CAME ON. REMOVED AND REPLACED RT ENGINE NACELLE OVERHEAT SENSOR. (SDR2004017) 2H72 4T4 TRTA53EU E20NE 20040504000762004050400076EU 2004 5 4 SIMA200410115 120040329A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON REPAIR STATEMENT DENT, FWD OF FRAME 512 AT SL 1603 WAS FOUND BEYOND SRM LIMITS. THE PREVIOUS REPAIR AT THIS LOCATION WAS DETERMINED TO BE INCORRECT. REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED A NEW DOUBLER REPAIR DONE IAW REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000812004050400081SO 2004 5 4 WVB2004F00000 120040325A792120010A OIL COOLER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT ENGINE RUPTURED E WVBEEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 AL0159764707 448 317652037 ON 24 MAR 04, AC DEPARTED, AT APPROX 50 MILES FROM DEPARTURE, PILOT NOTICED A LOSS OF MANIFOLD PRESSURE AND A LOSS OF OIL PRESSURE ON THE LT ENGINE, FEATHERED THE LT PROPELLER, SHUT DOWN THE LT ENGINE AND RETURNED TO DEPARTURE. A MAINTENANCE INSPECTION REVEALED THAT THE LT OIL COOLER HAD RUPTURED, LEAKING OIL FREELY. MAINT HAS ELECTED TO REPLACE THIS ENGINE. 1L72 3O3 O A20SO E14EA 20040504000872004050400087NM 2004 5 4 USA2004F00015 120040303A4920380029816 APU BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE APU BAY LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19626AU33274 27303 ENROUTE, CREW RECEIVED THE EICAS MESSAGE (R GEN DRIVE) AND THE ASSOCIATED LIGHT. THE IDG WAS DISCONNECTED. THE APU WAS BROUGHT ON LINE, BUT SUBSEQUENTLY PERFORMED AND AUTO SHUTDOWN. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE GCU FOR THE IDG PROBLEM. THE APU WAS FOUND TO HAVE SHUTDOWN DUE TO A MASSIVE OIL LOSS. THE APU WAS REPLACED. 2L72 4F4 FRTA2NM A12EU 20040505000112004050500011NE 2004 5 5 PG9R118892 220040202A7261350A54113800 TUBE UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE OIL AIR VENT CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19130PH627 3670 TUBE OIL AIR VENT CRACKED. (RMA NR R046856) 1G72 3U3 U H9EU E00054EN 20040505000192004050500019CE 2004 5 5 N4J2004F00002 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE T/R ACTUATOR CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15600GG2381 115 LT OB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED MAY 2002. 2L72 4F4 FRTA10CE E35NE 20040505000222004050500022EU 2004 5 5 SIMA200410102 120040330A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DENTED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21374AE 340B374 DURING MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON MFG REPAIR STATEMENT DENT ID AS NR 10. BETWEEN FUSELAGE STA 535, 560 AND SL 1504 AND 1505 FOUND TO BE BEYOND SRM LIMITS. COMPLETELY REMOVED DAMAGE BY CREATING A CUTOUT. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW MFG STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040505000232004050500023CE 2004 5 5 GUU2004F00003 120040418A21971143641407 CIRCUIT BOARD BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA BLEED AIR SHORTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO1717541 UE203 DURING FLIGHT, SMELLED ELECTRICAL ODOR IN COCKPIT. SELECTED LT BLEED AIR ENVIRONMENTAL OFF. CONTINUED TO NAS. LANDED WITHOUT INCIDENT. MAINTENANCE FERRY. REPAIRED CHAFFED WIRE FROM PRESSURE REGULATOR PIN F. REMOVED AND REPLACED BLEED AIR PC BOARD A317. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040505000402004050500040NM 2004 5 5 UIEA200400050 120040413A5414 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 4 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 4 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSEMBLY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED AN ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER REPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040505000422004050500042NM 2004 5 5 UIEA200400048 120040413A5414 SKIN BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 D CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 2 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED AN ALUMINUM FILLER OF 2024-T3. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEAL LOWER REPAIR ANGLE FROM STA 235 TO STA 254. THE RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040505000522004050500052NM 2004 5 5 UIEA200400051 120040415A5750 BUSHING BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE WING WORN A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 (D) CHECK, DURING SCHEDULE MAINTENANCE, NR 8 MOVEABLE CANOE AFT SECTION SECONDARY DOOR ASSEMBLY LOWER BEARING FOUND MIGRATED. THE LUG BORES ARE OVERSIZED TO 0.7827 INCH DIAMETER TO REMOVE DAMAGE. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE. AN ALUMINUM REPAIR SLEEVE WAS INSTALLED, COMPLETE WITH A NEW DESIGN TYPE BEARING. 2L74 4F4 FRTA20WE E23EA 20040505000542004050500054CE 2004 5 5 QCW2004F00000 120040315A8120369100265 HEAT SHIELD BEECH 36 B36TC 1151609CE CONT O520 TSIO520* 17040SO TURBOCHARGER CHAFED E QCWAO OTHER O OTHER NRNOT REPORTED 1 NM01671TC56 EA671 527463 THE TURBO HEAT SHIELD CHAFED 30 PERCENT THROUGH THE LT INDUCTION ELBOW DUE TO ENGINE VIBRATION. STRICT ATTENTION SHOULD BE PAID TO THE AFT IB SIDE OF HEAT SHIELD. THE HEAT SHIELD HAD TO BE ALTERED TO PREVENT FURTHER REOCCURRENCE OF THIS SITUATION. 1L71 3O3 O 3A15 E8CE 20040505000592004050500059 2004 5 5 04103650 420040412A222070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27650BR 7418 DURING CRUISE OF FLIGHT 7823 CREW REPORTED A STAB/MACH TRIM FAILURE. CREW DIVERTED TO NEAREST SUITABLE AIRPORT AND FLIGHT LANDED SAFELY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20040505000602004050500060EA 2004 5 5 04098670 120040407A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER INOPERATIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27670BR 7561 DURING CLIMB OF FLIGHT 7351 CREW REPORTED A RIGHT HAND THRUST REVERSER UNLOCK MESSAGE AND RETURNED TO DEPARTURE FIELD. FLIGHT LANDED UNEVENTFULLY. THE RIGHT HAND THRUST REVERSER STOW SWITCH WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040505000622004050500062EU 2004 5 5 04107332 120040416A2730 CONTROL CABLE JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR OUT OF RIG A VTZAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA27332UE 41100 DURING TAKEOFF AND APPROACH CREW REPORTED ELEVATOR FLUTTERS. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE AILERON CABLE TENSION WERE FOUND TO BE OUT OF ADJUSTMENT AND WERE READJUSTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2L72 4T RTA41NM 20040505000742004050500074NM 2004 5 5 P762004F00003 120040219A552465229908 BRACKET BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE LT ELEVATOR CRACKED A P76AO OTHER O OTHER NRNOT REPORTED 1 SO17894AA59612 22010 LT NR 3 ELEVATOR BALANCE PANEL AREA. FORWARD BRACKET THAT HOLDS THE FORWARD HINGE ATTACH POINT. STIFFENER BRACKETS AND ANGLES CRACKED AND BENT. 2L73 4F4 FRTA3WE E2EA 20040505000752004050500075EA 2004 5 5 04074664 120040315A335078279015 ACM CNDAIRCL600 CL6002B19 1900309EA CABIN COOLING INOPERATIVE A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA27664BR 7528 DURING AIRCRAFT OPERATION THE RIGHT HAND PAC TEMPERATURE CONTROL BECAME INOPERATIVE. THIS RESULTED IN A REPORT OF SMOKE IN THE CARGO AREA AND CABIN. THE AIR CYCLE MACHINE WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. 2L72 4F RTA21EA 20040505000882004050500088EA 2004 5 5 04107687 120040416A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27687BR 7720 DURING INSPECTION THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND INOEPRATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505001102004050500110EA 2004 5 5 SWIA200413192 120040416A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 280 RIGHT FLOORBEAM RBL 9 OUTBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-40-13, 51-42-21, 51-23-00, 51-25-00, AND 51-24-36 2L72 4F RTA21EA 20040505001122004050500112NM 2004 5 5 ATC0388 120040203A3320L8161516 LIGHT BOEING737 7374Y0 1384705NM GE CFM56 CFM56* 13802NE LAVATORY A WRONG PART B LH6YK NONE W INADEQUATE Q C ININSP/MAINT 1 EA35239CT 23980 ROUTINE C CHECK INSPECTION AND FUNCTIONS ON LAVATORY A LIGHTING THE DOME LIGHT ASSY WAS FOUND DETACHED FROM MODULE CEILING. ALL 3 SECURING LUGS HAD DETACHED FROM SUPPORT RING DUE TO SEVERE OVERHEATING OF DOME LIGHT AND SURROUNDING AREA. ON INVESTIGATION IT WAS FOUND THAT LAMP, PN GE 1691 WAS FITTED IAW LABEL OF BODY OF DOME LIGHT BUT IPC 33-26-00 REQUIRES A PN 303AF TO BE FITTED. PN 1691 LAMPS ARE RATED 28V 0.61 AMPS AND PN 303 AF LAMP AT 28V 0.31 AMPS. FURTHER INVESTIGATION FOUND INCORRECT RATED LAMPS FITTED TO BOTH REAR LAVATORIES. LAVATORY A LIGHT ASSY, REPLACED. LAMPS REPLACED IN REAR LAV. NO DAMAGE FOUND ON ADJACENT WIRE BUNDLE AND SOUND PROOFING. SMOKE DETECTOR PLUG REPLACED. (EA35200401324) 2L72 4F4 FRTA16WE E2GL 20040505001192004050500119EA 2004 5 5 SWIA200413199 120040416A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FRAME SECTOR AT FS 349 BETWEEN STR 24 LT AND 24 RT IS CORRODED BEYOND LIMITS. FRAME SECTOR REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND RII 53-401. (DISCOVERED DURING C-CHECK INSPECTION) 2L72 4F RTA21EA 20040505001202004050500120CE 2004 5 5 LBW2004F00001 120040310A2612 FIRE WARNING LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE731* 01518WP ENGINE FAULTY E LBWAF ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 EA25815DD 35A414 LT FIRE WARNING LIGHT ILLUMINATED, CHEW ACTUATED FIRE BOTTLE. AFTER LANDING MAINTENANCE CREW NOTED FIRE WARNING TEST INOPERATIVE ON BOTH ENGINES AND MASTER CAUTION WILL NOT EXTINGUISH. PROBLEM TO BE DETERMINED. 2L72 4F4 F A10CE E6WE 20040505001302004050500130CE 2004 5 5 LBW2004F00000 120040310A3297 WIRE LEAR 60 60LEAR 5170707CE LT MLG WW CUT E LBWAO OTHER O OTHER NRNOT REPORTED 1 EA25126KD 262 CUT WIRE FOUND ON LT GEAR DOWN AND LOCKED SWITCH WHICH CAUSED THE IB GEAR DOORS NOT TO RETRACT IN THE GEAR DOWN POSITION. THIS WAS THE FIRST FLIGHT BACK AFTER MAINTENANCE WAS PERFORMED BY MFG. THE LT GEAR ACTUATOR WAS REPLACED AND THE DOWN AND LOCK SWITCH TRANSFERRED TO THE NEW ACTUATOR. CUT WIRE WAS REPAIRED. 2L72 4F RTA10CE 20040505001422004050500142CE 2004 5 5 HYTA2004004 120040317A3397 WIRE CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA TAILCONE MISROUTED E HYTAO OTHER O OTHER NRNOT REPORTED 1 AL014365U13890 208B0253 FLASHING BEACON WIRE IN TAILCONE WAS ROUTED OVER THE BALLAST RESISTOR WHERE THERE IS LESS THAN .5 INCH CLEARANCE TO STRUCTURE. WIRE WAS NOT TOUCHING BALLAST RESISTOR OR AIRPLANE STRUCTURE, BUT INSULATION WAS BURNED CLEAR THROUGH TO BARE WIRE. WIRE SHOULD HAVE BEEN ROUTED UNDER AND AWAY FROM RESISTOR. 1H71 3T3 T A37CE E2NE 20040505001522004050500152CE 2004 5 5 HYI2004F00000 120040206A551150320023 SPAR CAP CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO HORIZ STAB CORRODED E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE016875D18886 402C0511 CORRODED SPAR CAP LOCATION, REAR SPAR ON HORIZONTAL STABILIZER, LOWER CAP. CORRODED AT LEFT, IB HINGE, 12 INCHES OB OF IB HINGE. (NE01200401202) 1L72 3O3 O A7CE E8CE 20040505001532004050500153EA 2004 5 5 SWIA200413209 120040416A5320 STIFFENER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS621 BULKHEAD LEFT VERTICAL STIFFENER LBL 18 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401. 2L72 4F RTA21EA 20040505001542004050500154EA 2004 5 5 SWIA200413210 120040416A5320 STIFFENER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS621 BULKHEAD LEFT VERTICAL STIFFENER LBL 9.0 UPPER ATTACH CLIP CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII 53-401. 2L72 4F RTA21EA 20040505001782004050500178NM 2004 5 5 ASAA0440036 120040204A5315BAC14902734 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND STATION 344 LBL 12 TO LBL 24 FLOORBEAM HAS CORROSION TOP AND BOTTOM SIDES. REPAIRED PER SRM 51-70-12 FIG 1. (M) 2L72 4F RTA16WE 20040505001912004050500191NM 2004 5 5 ASAA0410087 120040216A5310654654842 SHEAR TIE BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE, FOUND SHEAR TIE CORRODED AT STATION 747. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040505001922004050500192EU 2004 5 5 MALA040365 120040410A5230 DOOR FRAME BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, AFT CARGO DOOR UPPER FRAME CRACKED. MAINTENANCE FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR IAW MESABA EO A52040. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040505002062004050500206NM 2004 5 5 ASAA0410074 120040215A53106560552501 TEAR STRAP BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND TEAR STRAP AT STATION 360 AND STRINGER 28L CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040505002072004050500207NM 2004 5 5 ASAA0410085 120040216A531065465502 SHEAR TIE BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SHEAR TIE AT STATION 787 CORRODED. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505002082004050500208NM 2004 5 5 ASAA0410080 120040216A53306545800599 SKIN BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SKIN CORRODED AT STATION 360 AND STRINGER 28L. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505002102004050500210NM 2004 5 5 ASAA0410052 120040206A5313 STRINGER BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 24L AT BS 907, CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002112004050500211NM 2004 5 5 ASAA0410051 120040206A531369353502 STRINGER CLIP BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE STRINGER CLIP AT BS 727A, STRINGER 19L CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002132004050500213NM 2004 5 5 ASAA0410049 120040206A53106546529501 SHEAR TIE BOEING737 737210C 1384459NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 440, STRINGER 17L CRACKED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040505002192004050500219EU 2004 5 5 BAQA092494 120040330A6240430106202 PICKUP UROCOPEC135 EC135P1 8680990EU SPEED FLUCTUATES E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03577LF1054 0140 CORE RETURN FOR WARRANTY PO 202294001, CAUSING NEEDLE FLUCTUATIONS AND LIGHT REPLACED WITH SERVICABLE UNIT FROM AEC, 04/28/2004. 1G72 3U O H88EU 20040505002202004050500220NM 2004 5 5 SWAA041250 120040503A575465C26601302 WEDGE BOEING737 737317 138447PNM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT UPPER WEDGE PANEL DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2L72 4F RTA16WE 20040505002222004050500222 2004 5 5 SWAA041252 420040503A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29700GS 27835 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040505002242004050500224 2004 5 5 SWAA041254 420040503A25656567380 LENS BOEING737 7377H4 1384404NM EVAC SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29783SW 29809 R2 DOOR EVAC SLIDE PRESSURE GAUGE VIEWING LENS LOOSE. SECURED R2 DOOR LENS PER MM. 2L72 4F RTA16WE 20040505002262004050500226NM 2004 5 5 SWAA041231 120040501A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040505002282004050500228NM 2004 5 5 SWAA041233 120040502A335007912 COVER BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 EEPLS COVER AT RT ROW 6 TO ROW 8, MISSING. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040505002302004050500230NM 2004 5 5 SWAA041235 120040502A531465621265 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM CHORD AT RT BS 727 A, AND LT BS 727, CORRODED. REMOVED AND REPLACED KEEL BEAM CHORD PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040505002322004050500232NM 2004 5 5 SWAA041237 120040502A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 492, RBL 45, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040505002342004050500234NM 2004 5 5 SWAA041239 120040502A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927 + 5, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002362004050500236NM 2004 5 5 SWAA041227 120040501A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500 D, STRINGER 12R, AND STRINGER 12L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002382004050500238NM 2004 5 5 SWAA041229 120040501A3350311500 LENS BOEING737 7375H4 138449DNM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED PM CHECK, FOUND BULLNOSE LIGHT LENS AT ROW 8 ABC CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040505002402004050500240NM 2004 5 5 SWAA041240 120040502A574365C3291818 FITTING BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING RON CHECK, FOUND RT MLG FWD INBOARD STABILIZER FITTING CORRODED. REPAIRED RT MLG INBOARD FITTING PER EA. 2L72 4F RTA16WE 20040505002422004050500242NM 2004 5 5 SWAA041242 120040502A53126516300 BULKHEAD BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SPV, FOUND BULKHEAD WEB AT BS 178, LBL 7 TO LBL 8, CRACKED. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20040505002442004050500244NM 2004 5 5 SWAA041244 120040502A3350612825 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29741SA 29277 DURING SPV, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040505002462004050500246NM 2004 5 5 SWAA041213 120040429A5315BAC150539042 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 219, LBL 16, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040505002472004050500247NM 2004 5 5 SWAA041215 120040429A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 8L, AND STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040505002482004050500248NM 2004 5 5 SWAA041216 120040429A5311BAC15061653 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME WEB AT BS 303.9, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2L72 4F RTA16WE 20040505002502004050500250NM 2004 5 5 SWAA041218 120040429A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002522004050500252NM 2004 5 5 SWAA041220 120040429A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E + 16, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002542004050500254NM 2004 5 5 SWAA041222 120040429A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 908, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040505002562004050500256NM 2004 5 5 SWAA041224 120040429A25606949956 CABLE BOEING737 7373G7 1384595NM L2/R2 DOORS MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE CABLES PER MM. 2L72 4F RTA16WE 20040505002582004050500258NM 2004 5 5 SWAA041167 120040426A2560P4010021 BATTERY PACK BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040505002812004050500281NM 2004 5 5 SWAA041197 120040428A335007912 COVER BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040505002832004050500283NM 2004 5 5 SWAA041199 120040428A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM CHORD AFT CARGO COMPARTMENT, AT BS 727 TO BS 730, LBL 12, CORRODED. REPAIRED KEEL BEAM PER EA. 2L72 4F RTA16WE 20040505002852004050500285NM 2004 5 5 SWAA041201 120040428A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002872004050500287NM 2004 5 5 SWAA041203 120040428A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002892004050500289 2004 5 5 SWAA041205 420040428A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29413WN 29819 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040505002902004050500290NM 2004 5 5 SWAA041190 120040427A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 737, BETWEEN STRINGER 18R AND 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002982004050500298NM 2004 5 5 SWAA041189 120040427A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505003002004050500300 2004 5 5 SWAA041207 420040428A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040505003022004050500302NM 2004 5 5 SWAA041209 120040429A1430 FASTENER BOEING737 7373H4 1384600NM R2 DOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 L2 DOOR EVAC SLIDE DOOR GIRT BAR HOOK MISSING FASTENER. INSTALLED FASTENER IN R2 DOOR EVAC SLIDE HOOK PER MM. 2L72 4F RTA16WE 20040506000012004050600001EU 2004 5 6 BAQA094288 120040428A6720741C000005 ACTUATOR BOLKMS117 BK117B1 5626012EU TAIL ROTOR LEAKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME 7235 ACTUATOR LEAKING AND BUSHINGS WORN. REPLACED WITH SERVICABLE UNIT. 04/29/2004 1G72 3U H13EU 20040506000032004050600003EU 2004 5 6 BAQA094294 120040419A642010513241 BEARING BOLKMS117 BK117B1 5626012EU FORK LINK WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME286 7235 BEARINGS WORN IN FORK LINK. REPLACED WITH SERVICABLE ASSET UNIT. 04/29/2004 1G72 3U H13EU 20040506000062004050600006 2004 5 6 BAQA094210 420040430A34165035P2P42 ALTIMETER AEROSPSA365 SA365N 8680669EU COCKPIT INACCURATE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0389SM 6425 UNIT INACCURATE WHEN IN FLIGHT. REPLACED WITH SERVICABLE UNIT. 04/30/2004 1G72 3U H10EU 20040506000072004050600007EU 2004 5 6 BAQA094322 120040429A641011731743 BLADE BOLKMS117 BK117B1 5626012EU TAIL ROTOR DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03945ME3515 7235 UNABLE TO BALANCE BLADES AND PAINT IS STARTING TO PEEL. 1G72 3U H13EU 20040506000082004050600008NM 2004 5 6 ANCF200400006 120040409A5350 RADOME DOUG MD80 MD83 3023681NM FUSELAGE BIRD STRIKE W ANCFA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO23632CT 49632 BIRD STRIKE AT AIRPLANE'S DOME, THE AIRCRAFT DID NOT SHOW ANY ABNORMAL INDICATION, RADAR WAS TURN OFF AS A PRECAUTIONARY MEASURE. THE RADOME WAS REPLACED IAW AMM 53-51-00 PAG 401 AND ANTENNA TILT POSITION WAS CHECKED AND PERFORMED TEST IAW AMM 34-41-00 PAG 201-202. P/N ON AND OF 5910091-27 S/N OF: 01215 S/N ON: 1063. 2L72 4F RT 20040506000102004050600010EU 2004 5 6 2004F00102 120040428A6220129010160115 STRAP AGUSTAA109 A119 0261102EU PWA PT6 PT6* 52043EA M/R BOND BROKEN E O OTHER O OTHER NRNOT REPORTED 1 SO07521RC20 14019 PCEPU0007 MAIN ROTOR BONDING STRAP BROKEN. THIS IS A CONSTANT PROBLEM, PORTION OF THE STRAP WHICH CONTINUES TO BREAK IS MADE OF COPPER. THIS END OF THE STRAP BOLTS TO A STAINLESS STEEL CONNECTION WHICH NEVER BREAKS. THE ENDS OF THE BONDING STRAPS SHOULD BE MADE OF A STAINLESS STEEL MATERIAL OR SOMETHING MORE RELIABLE THAN A COPPER FITTING. 1G72 3U3 T H7EU E2NE 20040506000122004050600012NM 2004 5 6 ASMF200404022 120040428A2420696233B CSD DOUG MD80 MD83 3023681NM GENERATOR FAILED W ASMFA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW23831LF169756482 53050 AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF LT GENERATOR LIGHT TURNED ON AND CSD WAS OUT OF SERVICE. ENGINE WAS SHUTDOWN TO ENGAGED CSD. THE CONTROL BOX WAS RESET AND ENGINE WAS STARTED WITH SWITCH ON "RESET" POSITION WITHOUT VOLTAGE AND FREQUENCY INDICATION. LT GENERATOR CONTROL BOXES WERE INTERCHANGED WITH APU CONTROL BOXES WITH NEGATIVE RESULTS. CONTROL BOXES WERE RETURNED TO THE ORIGINAL POSITIONS AND APU WAS STARTED OPERATING WITH LT BUS. AIRCRAFT WAS REFUELED AND LT GENERATOR WAS DEFERRED IAW MEL 24-1-1. DURING OVERNIGHT SERVICE CSD, GENERATOR AND OIL HEAT EXCHANGER WERE REPLACED IAW MM 24-10-03, 24-20-00 AND 24-10-01, RESPECTIVELY, TESTS CORRECT. 2L72 4F RT 20040506000132004050600013NM 2004 5 6 ASMF200404023 120040429A3097 WIRE DOUG MD88 MD88 3023688NM ANTI ICE SYSTEM GROUNDED W ASMFO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SW23169PL 53175 CAPTAIN REPORTED THAT DURING TAKE OFF (AIRFOIL ICE PROTECT PRESS ABNORMAL) LIGHT TURNED ON. CABLES WERE CHECKED AND A LINE WAS GROUNDED IN SENSOR S1-46. (AIRFOIL ICE PROTECT PRESS ABNORMAL) LIGHT WIRING WAS REPAIRED IAW WDM 30-11-01, TEST CORRECT. 2L72 4F RTA6WE 20040506000142004050600014NM 2004 5 6 ASMF200404024 120040429A2910 TUBE BOEING757 7572Q8 1384972NM HYD SYS DAMAGED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23804AM 26271 DURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED ON LT ENGINE. DURING MAINTENANCE REVISION AN HYDRAULIC TUBE (P/N 316N3100-28) WAS DETECTED WITH DAMAGE. PROVISIONAL FLEXIBLE HOSE WAS INSTALLED, LEAK TEST WAS PERFORMED, NO LEAK WAS DETECTED. DURING OVERNIGHT SERVICE PROVISIONAL HOSE WAS REPLACED, LEAK TESTS WERE CORRECT. 2L72 4F RTA2NM 20040506000152004050600015WP 2004 5 6 ASMF200404020 120040427A32443910097543 TIRE DOUG DC9 DC987 3022087WP MLG FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23205AM3305 49405 DURING TRANSIT CHECK CAPTAIN REPORTED THAT AIRCRAFT TURNED TO THE LT DURING TAXING AND NOSE LANDING GEAR INDICATOR PIN EXTENDED ALL THE TIME. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE NOSE LANDING GEAR TIRES WERE REPLACED IAW MM 32-40-02 AND NOSE LANDING GEAR VISUAL INDICATOR WAS ADJUSTED IAW MM 32-60-06, TEST CORRECT. 2L72 4F RTA6WE 20040506000162004050600016NM 2004 5 6 ASMF200404021 120040427A2410729825G IDG ALIDSG GTCP331200 BOEING757 7572Q8 1384972NM APU FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23802AM2254011460 P2086 26270 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MTY AS A CONSEQUENCE OF APU WAS SHUTDOWN IN FLIGHT AND LT IDG WAS PREVIOUSLY DEFERRED. BITE TO ECU WAS PERFORMED IAW FIM 49-11-00 AND "NO FAME" MESSAGE WAS SHOWN IN FAULT DISPLAY. APU OIL LEVEL WAS VERIFIED AND FOUND ALMOST EMPTY. APU OIL SERVICE WAS PERFORMED IAW MM 12-13-04. LT IDG WAS REPLACED IAW MM 24-11-01 AND APU GCU WAS SWAPPED WITH LT GENERATOR IAW MM 24-22-02, TEST CORRECT. 2L72 4F RTA2NM 20040506000212004050600021EU 2004 5 6 BAQA094266 120040421A212107140370001 MOTOR BOLKMS117 BK117B2 5626013EU BLOWER FAN FAILED E BAQAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 EA03296GL6388 7222 COOLING BLOWER VERY LOUD DURING OPERATION. REPLACED WITH SERVICABLE UNIT. 04/27/2004 1G72 3U NCH13EU 20040506000222004050600022EU 2004 5 6 BAQA094252 120040422A2435 SHAFT AEROSPAS355 AS355F2 8680812EU STARTER GEN SEVERED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS 1820 5495 SHAFT SEVERED ON UNIT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004 1G72 3U H11EU 20040506000482004050600048EU 2004 5 6 MALA040370 120040411A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, SEAT TRACK NR 3 CORRODED OUT OF LIMITS. CUT OUT CORRODED SECTION OF NR 3 SEAT TRACK, LOCATED, DRILLED AND INSTALLED NEW SECTION NR 3 SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040506000492004050600049EU 2004 5 6 MALA040367 120040410A5280 DOOR BAC 146 AVRO146RJ85A1500097EU LT MLG CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, LEFT MLG DOOR FWD UPPER EDGE CHAFED. CUT OUT CHAFED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW MESABA EO A52041. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040506000502004050600050EU 2004 5 6 MALA040364 120040423A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED DENTS IAW MESABA EO S53009. REMOVED AND REPLACED NR 1 ICE GUARD IAW SAAB 340 SRM 53-70-10-2. A/C RELEASE DATE 4/25/04. 2L72 4T RTA52EU 20040506000522004050600052EU 2004 5 6 MALA040368 120040411A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, FWD CABIN FLOORBEAM FRAME 18 HAS CORROSION OUT OF LIMITS. MAINTENANCE CUT OUT CORRODED SECTION OF FRAME 18, FABRICATED AND INSTALLED NEW SECTION OF FLOORBEAM IAW MESABA EO A53168. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040506000542004050600054EU 2004 5 6 MALA040361 120040422A5230 STRUCTURE SAAB SF340 340B 7860101EU CARGO DOOR GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, MX REPAIRED GOUGED LOWER CORNER OF CARGO DOOR IAW SAAB 340 SRM 52-10-10 PARAGRAPH 1 AND MESABA EO S52028. A/C RELEASE DATE 4/25/04. 2L72 4T RTA52EU 20040506000552004050600055EU 2004 5 6 MALA040362 120040422A5230 SKIN SAAB SF340 340B 7860101EU CARGO DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15406XJ 340B406 DURING 4K INSPECTION IN LCQ, REPAIRED UPPER O/B SKIN CHAFED AREA ON CARGO DOOR IAW SAAB SRM 52-10-10, PARAGRAPH 1 AND MESABA EO S52028. A/C RELEASE DATE 4/25/2004. 2L72 4T RTA52EU 20040506000562004050600056EU 2004 5 6 MALA040371 120040411A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, SEAT TRACK NR 4 CORRODED OUT OF LIMITS. CUT OUT CORRODED SECTION OF NR 4 SEAT TRACK, LOCATED, DRILLED AND INSTALLED NEW SECTION OF NR 4 SEAT TRACK IAW MESABA EO A53026. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040506000582004050600058EU 2004 5 6 KC82004F00001 120040426A5610MY20267109 WINDSHIELD AMD FALCONFALCON20 2730103EU GE CF700 CF700* 30010NE COCKPIT CRACKED E KC8AO OTHER O OTHER NRNOT REPORTED 1 GL2370CK 128 CAPTAINS SIDE WINDSHIELD INNER LAMINATE CRACKED DUE TO INNER HEATING ELEMENTS SHORTING. WINDSHIELD WAS REPLACED WITH NEW WINDSHIELD IAW MM. 2L72 4F4 FRTA7EU E7EA 20040506000592004050600059EU 2004 5 6 A6WA200460011 120040331A2750 FLAP BAC 146 146200A 1500266EU LYC ALF502ALF502* 41580EA WING MALFUNCTIONED A A6WAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL31181US E2042 ON CLIMB OUT, FLAP INOPERATIVE/ FLAP MWS ILLUMINATED IMMEDIATELY AFTER SELECTING 24-18 DEGREES, COMPLIED WITH QRH, DIVERTED. CHECKED ECU (4) ONLY ILLUMINATED, RESET FLAP SYSTEM IAW MM, SYSTEM RESET AND OPS CHECK NORMAL ON GROUND AT THIS TIME. 2H74 4F4 F A49EU E6NE 20040506000602004050600060CE 2004 5 6 AC02004F00000 120040220A561010138402518 WINDSHIELD BEECH 200 B200 1152922CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED B ACORB EMER. DESCENT O OTHER CRCRUISE 1 SO05300ET4479 BB1381 DURING FLIGHT, AT FLIGHT LEVEL, 21,000 FT, COPILOTS WINDSHIELD INNER PANEL CRACKED. PILOT IMMEDIATELY DESCENDED TO A SAFE ALTITUDE AND LANDED AS SOON AS POSSIBLE. UPON INSPECTION, FOUND NO DAMAGE TO OUTER PANEL. WINDSHIELD HEAT WAS OPERATING NORMALLY. NO REASON FOUND OR DETECTED FOR FAILURE. 1L72 4T4 T A24CE E4EA 20040506000632004050600063CE 2004 5 6 T8B2004F00000 120040423A7830225006503 DOOR BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE THRUST REVERSER CRACKED B T8BDO OTHER O OTHER NRNOT REPORTED 1 SO25711EC3670 RK167 THE UPPER LEFT THRUST REVERSER DOOR IS CRACKED APPROXIMATELY 11 INCHES. THE CRACK IS LOCATED BEHIND THE MIDDLE ROW OF RIVETS, APPROXIMATELY .5 INCH BEHIND THE RIVET CENTER LINE AND IS PERPENDICULAR TO LINE OF FLIGHT. THE DOOR HAS BEEN RETURNED TO THE MFG FOR REPAIR. 2H72 4F4 FRTA16SW E25EA 20040506000642004050600064SO 2004 5 6 AKG2004F00006 220040315A8520 NUT BEECH 36 B36TC 1151609CE CONT O520 TSIO520UB 17040SO NR 4 CYLINDER LOOSE B AKGRK NONE O OTHER ININSP/MAINT 1 CE0574MT 121 EA659 527558 WHILE COMPLETING AN ANNUAL INSPECTION. ONE OF THE CYLINDER RET BASE NUTS FOR THE NR 4 CYLINDER WAS MISSING. NUT WAS FOUND BETWEEN CYLINDER. TORQUE CHECK MADE OF THE OTHER NUTS FOUND 3 MORE LOOSE. WE CHECKED THE OTHER CYLINDER AND FOUND THEN TO BE OK. ALL OF THE CYLINDER NUT DID HAVE INSPECTION TORQUE SEAL ON THEM. THIS ENG BUILD DATA WAS 2/6/02. NO RECORD OF CYLINDER WORK COMPLETED ON THIS ENGINE. 1L71 3O3 O 3A15 E8CE 20040506000662004050600066NM 2004 5 6 AMTA200400440 120040414A36101074944 CONTROLLER BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE BLEED AIR SYS MALFUNCTIONED A AMTAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TOTAKEOFF 1 GL11517AT 27973 ON TAKEOFF LT ENGINE BLEED OFF LIGHT ILLUMINATER. RESET UPON ARRIVAL AT KMDW SYSTEM NORMAL . REMOVED AND REPLACED REVERSE FLOW CHECK CONTROLLER IAW AMM 2L72 4F4 FRTA2NM A12EU 20040506000712004050600071SO 2004 5 6 HYI2004F00002 220040419A8520632893 GEAR CONT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO RT ENGINE FAILED E HYIAK NONE O OTHER TXTAXI/GRND HDL 1 NE0126514312 Z03JA202 402C0344 828682 UPON START, RT ENGINE FAILED TO TURN. MECHANIC FOUND PROP COULD NOT BE TURNED BY HAND EITHER. LATER INSPECTION FOUND CRANKSHAFT LARGE GEAR MISSING TEETH, AND STARTER ADAPTER MISSING TEETH ON DRIVE GEAR. MECHANIC TO REMOVE AND REPLACE ENGINE. 1L72 3O3 O A7CE E8CE 20040504000702004050400070SO 2004 5 4 SIMA200406401 120040221A335020131A BATTERY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN FAILED A O OTHER O OTHER NRNOT REPORTED 1 SW21617AE 145093 SUBMITTED OPEN AWAITING DISCREPANCY AND TIMES AND CYCLES AND SERIAL NUMBER. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040504000732004050400073EU 2004 5 4 SIMA200410118 120040329A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21398AM 340B398 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON MFG REPAIR STATEMENT DENT ID AS NR 33, 6.9 IN FORWARD OF STA 319 AT SL 1502 WAS FOUND TO BE BEYOND SRM LIMITS. PREVIOUS REPAIR AT THIS LOCATION WAS FOUND TO BE INCORRECT. REMOVED PREVIOUS REPAIR DOUBLER THAT WAS INSTALLED. FABRICATED NEW REPAIR DOUBLER. REPAIR DONE IAW MFG REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040504000822004050400082CE 2004 5 4 WK42004F00002 120040315A3244265K682 TIRE RKWELLNA265 NA26565 7630107CE LANDING GEAR DAMAGED B WK4RO OTHER O OTHER NRNOT REPORTED 1 SO174CS 26 46527 CENTER TREAD CHUNKED AFTER 54 LANDINGS ON LT TIRE. 2L72 4J A2WE 20040504000842004050400084EU 2004 5 4 USA2004F00012 120040304A3350321430 BATTERY AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19109UW 1065 THE RT SIDE MID-CABIN EMERGENCY LIGHT BATTERY FAULTED DURING TEST. MAINTENANCE REPLACED THE RT SIDE MID-CABIN EMERGENCY LIGHT BATTERY. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E2GL 20040505000042004050500004EA 2004 5 5 DAT2004F00000 220040410A7314310733801 LINE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA P3 FILTER CRACKED A DATAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13390GA SH3077 LEAVING 4400 FEET, THE RT ENGINE TORQUE FELL FROM 3200 LBS TO 2000 LBS THEN TO 1500 LBS THEN STABILIZED AT 2000 LBS FOR A WHILE THEN WENT BACK TO 3000 LBS. THE FLIGHT CREW TURNED BACK AND CALLED DEC TO TELL THEM OF THE SITUATION. THE FLIGHT CREW ADVISED THE ATC THEY NEEDED TO RETURN, DUE TO A POSSIBLE MAINTENANCE PROBLEM. AC LANDED WITHOUT INCIDENT. AC WAS PUT IN HANGAR AND DECOWLED WITH NO VISIBLE PROBLEMS FOUND. MECHANICS FOUND A CRACKED LINE COMING OFF THE P3 FILTER. LINE WAS REMOVED AND REPLACED IAW MFG MM. OPS CHECK AND ENGINE RUNS GOOD. AC WAS RETURNED TO SERVICE. 2H72 4T4 T A41EU E4EA 20040505000052004050500005CE 2004 5 5 FTU2004F00001 120040407A32201018100321 TORQUE KNEE BEECH 300 300BEECH 1152930CE PWA PT6 PT6* 52043EA MLG GOUGED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05145NA FA145 DURING A 6 YEAR/ 8,000 CYCLE LANDING GEAR INSPECTION, DAMAGE WAS FOUND ON ALL 4 MAIN LANDING TORQUE KNEE`S AT THE UPPER (PN 101-8100321) AND LOWER (PN1018100327) KNEE`S ATTACH POINT. ITS SUSPECTED THAT IN THE PAST, SOMEONE HAD ATTACHED SOME KIND OF HOOK CLAMPING DEVICE TO THE TWO TORQUE KNEE`S SO WHEN JACKING THE WING THE STRUT WOULDN’T EXTEND AND YOU ONLY NEEDED TO JACK A SHORT DISTANCE, UNFORTUNATELY THE HOOKS SEVERELY DAMAGED THE TORQUE KNEE`S TO A POINT WHERE THEY WERE CONSIDERED UNSERVICEABLE BY MFG. ALL MAIN LANDING GEAR TORQUE KNEE`S WERE REPLACED WITH NEW PARTS PURCHASED FROM MFG. THESE KNEE`S ARE NOT CHEAP, SO THAT SHORT CUT WAS A COSTLY MISTAKE. RECOMMENDATIONS ARE TO FOLLOW AIRCRAFT MM. 2L72 4T3 T A24CE E2NE 20040505000162004050500016SW 2004 5 5 EAT2004F00004 120040326A5311263106510 FRAME SWRNGNSA227 SA227* SW GARRTTTPE331TPE331* 01514WP FUSELAGE CRACKED B EATRK NONE O OTHER ININSP/MAINT 1 GL09370AE AC506 DURING INSPECTION FRAME (PN262106510) WAS FOUND CRACKED AT THE CONTROL COLUMN BEARING MOUNT ON THE RT SIDE. THIS WAS THE IMPROVED BEARING MOUNT SETUP AS CALLED OUT IN AD AND SB TO PREVENT CRACKING. THE CRACKS ARE OCCURING RT AT THE TOP OF THE IMPROVED (PN 2621352007P) DOUBLER ASSY. BELOW THE RADIOUS ON THE (26-21065-10) FRAME. MFG HAD SB CONCERNING THIS AREA THAT CHANGES THE MOUNTING AGAIN AND MAKING THE DOUBLER LONGER TO SPREAD OUT THE LOAD BETTER TO THE FRAME. 2L72 4T3 TRTA5SW E2WE 20040505000202004050500020CE 2004 5 5 N4J2004F00003 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE T/R ACTUATOR CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15601GG1187 192 LT IB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2L72 4F4 FRTA10CE E35NE 20040505000262004050500026EA 2004 5 5 A6WA200440042 120040413A3230601R850071 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TRUNNION FAILED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31427ZW3404 7685 WHILE REMOVING LT MLG FOR FITTING REPLACEMENT IT WAS DISCOVERED THAT LT MLG AFT TRUNNION BUSHING IS MIGRATED. REMOVED MIGRATED BUSHING, INSTALLED 1ST OVERSIZE BUSHING AND LINE REAMED TO 2.4379 INCHES ALL WORK DONE IAW BRAS EO 601R-32-4827 AND MFG SB 601R-32-054, REV B, PART B. (M) 2L72 4F4 FRTA21EA E15NE 20040505000412004050500041NM 2004 5 5 UIEA200400039 120040406A5315 FLOORBEAM BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE FUSELAGE DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15522MC 21783 DURING D CHECK, FOUND UPPER DECK FLOORBEAM, ONE ELONGATED HOLE WITH A SHORT EDGE MARGIN WAS FOUND COMMON TO STA 360 UPPER DECK FLOORBEAM UPPER CORD. THIS AIRCRAFT WAS MODIFIED TO A SPECIAL FREIGHTER CONFIGURATION. OVERSIZED SME HOLE TO 0.250 INCH DIAMETER (CLOSE REAM ACCEPTABLE) USED OPEN-HOLE HFEC INSPECTION TO CONFIRM ALL HOLES COMMON TO THE MODIFICATION/ REINFORCING STRAP ARE CRACK FREE. FORM 8110-3 ISSUED. 2L74 4F4 FRTA20WE E23EA 20040505000842004050500084SO 2004 5 5 OG52004F00001 120040329A612089307000 ROD END PIPER PA28 PA28R201 7102816SO LYC O360 IO360C1C6 41514EA MCAULY2D34C B2D34C213 GL PROP GOVERNOR WORN B OG5RO OTHER O OTHER NRNOT REPORTED 1 GL21384ND678 2844095 L3081251A 020899 PROP GOVERNOR CONTROL ROD END CAME APART FROM THE PROP GOVERNOR, CAUSING A LACK OF CONTROL TO THE PITCH OF THE AC PROPELLER. WORN AREAS THAT CAUSED TO OCCUR ARE THE BASE OF THE BALL JOINT AND WEAR AT THE END OF THE SPRING LOADED RETAINER ASSY. (GL21200402103) 1L71 3O3 O 2A13 1E10 5 CP7EA 20040505000912004050500091EA 2004 5 5 04107632 120040416A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING INSPECTION THE LEFT HAND WING FOWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. 2L72 4F RTA21EA 20040505000962004050500096EA 2004 5 5 SWIA200413183 120040413A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 DISCOVERED DURING C-CHECK INSPECTION, FUSELAGE RIGHT VERTICAL BEAM LOWER INBOARD AND OUTBOARD FLANGE CRACKED AT FS 559 LBL 9. REPAIRED BEAMS IAW CRJ REO 601R-53-41-057 REV. NC AND IAW RII 53-401. 2L72 4F RTA21EA 20040505000972004050500097CE 2004 5 5 N4J2004F00007 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE THRUST REVERSER CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15601GG 192 LT OB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED JULY 2002. 2L72 4F4 FRTA10CE E35NE 20040505001002004050500100CE 2004 5 5 N4J2004F00004 120040329A7830266016503 SUPPORT BEAM LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE THRUST REVERSER CRACKED E N4JAO OTHER O OTHER NRNOT REPORTED 1 WP15600GG2381 115 LT IB T/R ACTUATOR SUPPORT BEAM CRACKED AT GUIDE ROD ATTACH POINT. PART WAS REPLACED MAY 2002. 2L72 4F4 FRTA10CE E35NE 20040505001052004050500105EA 2004 5 5 SWIA200413188 120040420A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07432SW7093 7093 7548 LEFT FLIGHT SPOILER WHITE BOX W/FLIGHT SPOILERS FAULT STATUS MSG. REMOVED AND REPLACED INBOARD PCU ON LEFT SPOILER IAW MM 27-62-01. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20040505001092004050500109EA 2004 5 5 SWIA200413191 120040416A5315 FITTING CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 MAIN FUSELAGE; FS 460 RBL 9.0 OB FLOORBEAM FITTING CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED FITTING IAW CRJ SRM 51-40-11, 51-41-06, 51-23-00, 51-42-06, 51-23-00, 51-42-21, 51-21-11, 51-25-16, AND RII 53-401. 2L72 4F RTA21EA 20040505001112004050500111EA 2004 5 5 SWIA200413193 120040416A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 280 LEFT FLOORBEAM RBL 9 INBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-06, 51-42-21, 21-23-00, 51-25-00, 51-42-36 AND 51-21-11 AND RII 53-401. 2L72 4F RTA21EA 20040505001142004050500114EA 2004 5 5 SWIA200413195 120040416A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 559 VERTICAL POST LBL 9.0 INBOARD AND OUTBOARD LOWER FLANGES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED POST IAW CRJ REO 601R-53-41-057 REV. NC. REF. SKYWEST RII 27-414 AND RII 53-401. 2L72 4F RTA21EA 20040505001222004050500122EA 2004 5 5 SWIA200413201 120040416A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 379 STR 8R IS CRACKED FROM FASTENER HOLE IN UPPER FRAME TO SKIN FLANGE. (DISCOVERED DURING C-CHECK INSPECTION) FABRICATED, FIT, DRILLED AND INSTALLED ALL THE REPAIR PARTS IAW CRJ REO 601R-53-21-501 REV. NC. 2L72 4F RTA21EA 20040505001282004050500128EA 2004 5 5 SWIA200413234 120040427A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07406SW 7030 AFTER TAKEOFF WHILE TRIMMING, STAB TRIM AND MACH TRIM MESSAGES ILLUMINATED. RETURNED TO LAND, AS MESSAGES REAPPEARED AND TRIMS INOPERATIVE.REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT AS PER RII27-415, MM 27-42-01 AND 27-42-05. OPS. CHECKS GOOD. 2L72 4F RTA21EA 20040505001322004050500132EA 2004 5 5 SWIA200413237 120040416A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07447SW 7677 DISCOVERED DURING C-CHECK INSPECTION, FS 625 LEFT INTERCOSTAL STR 14 L CRACKED. INTERCOSTAL REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040505001382004050500138GL 2004 5 5 15HA0458004 220040221A72306828400 COMPRESSOR CVAC 440 440 2422902WP ALLSN 501D 501D13D 03004GL LT ENGINE DAMAGED A I5HAO OTHER O OTHER DEDESCENT 1 GL23582P 475 501042 DURING THE DESCENT, AT APPROX 12,000 FT, THE CREW HEARD A LOUD BANG A MOMENT LATER, THE LT FIRE WARNING LIGHT ILLUMINATED AND THE CREW (E) HANDLED THE ENGINE. THE AC MADE AN UNEVENTFUL LANDING. INSPECTION OF THE LT ENGINE HAS REVEALED THE PRESENCE OF A PIECE OF METAL LODGED IN THE FIRST STAGE OF THE COMPRESSOR. THERE ARE BENT AND DAMAGED FIRST AND SECOND STAGE COMPRESSOR BLADES AND THE ENGINE CANNOT BE TURNED BY HAND. FIFTH AND TENTH STG BLADES APPEAR TO BE UNDAMAGED AS DOES THE TURBINE. ENGINE DETERMINED TO HAVE FOD DAMAGE AND WAS REMOVED AND REPLACED. RETURNED TO SERVICE. 2L72 4R4 T 6A6 E282 20040505001402004050500140EA 2004 5 5 SWIA200413243 120040423A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07924SW 7681 DISCOVERED DURING C-CHECK INSPECTION, FS 625 RIGHT INTERCOSTAL STR 14R CRACKED. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00. 2L72 4F RTA21EA 20040505001442004050500144EA 2004 5 5 SWIA200413155 120040228A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 LT WING; LOWER WING PLANK FUEL ACCESS HOLES HAVE CORROSION ON REBATES. (DISCOVERED DURING C-CHECK INSPECTION.)REPAIRED AREA IAW CRJ REO 601R-57-21-030 REV. ''C'' AND SB 601R-57-030 REV. ''C''. 2L72 4F RTA21EA 20040505001472004050500147EA 2004 5 5 SWIA200413157 120040306A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, FORWARD EQUIPMENT COMPARTMENT FS 193.00 RIGHT SIDE FLOOR WEB CRACKED BY FRAME. REPAIRED IAW CRJ REO 601R-53-11-245 REV. NC. 2L72 4F RTA21EA 20040505001482004050500148EA 2004 5 5 SWIA200413158 120040306A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07406SW 7030 DISCOVERED DURING C-CHECK INSPECTION, WING BOX PRESSURE FLOOR SKIN CRACKED AT FS460, LBL2 - LBL8 AND RBL2 - RBL8, 4 CRACKS TOTAL. PRESSURE FLOOR REPAIRED IAW CRJ REO 601R-53-41-102 REV. NC, RII 53-401. 2L72 4F RTA21EA 20040505001602004050500160CE 2004 5 5 GNL2004F00002 120040326A324650300010109 WHEEL BEECH 90 E90 1152914CE PWA PT6 PT6A27 52043EA LANDING GEAR CRACKED E GNLAK NONE O OTHER ININSP/MAINT 1 SW0144GK LW298 ON PREFLIGHT INSPECTION A DARK HAIR LINE CRACK EXTENDED FROM A BOLT HOLE ON THE IB SIDE OF THE WHEEL HALF. REMOVED WHEEL, APPLIED DYE PENT AND CONFIRMED THE CRACK. THE WHEEL HALF IS CONDEMNED AND REMOVED FROM SERVICE. 1L72 3T4 T 3A20 E4EA 20040505001612004050500161EA 2004 5 5 SWIA200413211 120040416A5312 STIFFENER CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 DISCOVERED DURING C-CHECK INSPECTION, FS 621 BULKHEAD VERTICAL STIFFENER BL 0 UPPER CLIP CRACKED. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-21, 51-23-00. REF. RII53-401. 2L72 4F RTA21EA 20040505001622004050500162CE 2004 5 5 G1IA2004001 120040323A7540 WARNING SYSTEM BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA COCKPIT ACTIVATED E G1IAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 AL0125KA BB783 LT BLEED AIR FAIL LIGHT ILLUMINATED DURING FLIGHT. SECURED BLEED AIR FOR AFFECTED SIDE AND LANDED AT SCHEDULED DESTINATION. MAINTENANCE DEPT INSPECTED ALL BLEED DUCTS AND EVA TUBING, WITH NO DEFECTS NOTED. PURGED SYSTEM WITH COMPRESSED AIR CLEARING POSSIBLE OBSTRUCTION. PERFORMED OPERATION CHECK OF SYSTEM AND CHECK FLIGHT OF AIRCRAFT. NO FURTHER DISCREPANCIES NOTED. 1L72 4T4 T A24CE E4EA 20040505001852004050500185NM 2004 5 5 ASAA0440016 120040202A53156546811 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 FOUND BS 986 FLOORBEAM HAS CORROSON AROUND CLIPNUT HOLES AT NUMEROUS PLACES FROM LBL 46 TO RBL 46, TOP AND BOTTOM SURFACES. REPAIRED IAW EA 5310-02303. (M) 2L72 4F RTA16WE 20040505001892004050500189NE 2004 5 5 MALA040344 320040425A6110R3904123F PROPELLER SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE LT ENGINE FAULTY A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15367PX 340B271 LEFT PROP DEICE ANNUNCIATION ILLUMINATES IN NORM AND MAX INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED & REPLACED LEFT PROP IAW JC 6110-303. P\N OFF R390/4-123/F27. P\N ON R389/4-123/F26. S/N ON DAP0199, S/N OFF DAP/0003/92. ALL CHECKS GOOD. 2L72 4T RTA52EU 6 CP61GL 20040505001902004050500190NM 2004 5 5 ASAA0410086 120040216A53306545800599 SKIN BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING MAINTENANCE CHECK, FOUND SKIN HAS CORROSION AT STATION 360. REPAIR IAW EA. (M) 2L72 4F A16WE 20040505001942004050500194 2004 5 5 MALA040374 420040430A34426227337001 TRANSCEIVER SAAB SF340 340B 7860101EU WX RADAR FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15436XJ 340B436 AFTER TAKEOFF THE WEATHER RADAR FAILED, WOULD NOT PAINT KNOWN WEATHER. AIR RETURN TO MEM. REMOVED & REPLACED WEATHER RADAR TRANSCEIVER/TRANSMITTER IAW SF340 AMM CHAP 34-42-05-4. ALL CHECKS GOOD AT THIS TIME. P/N ON&OFF 622-7337-001, S/N ON 4553, S/N OFF 4623. 2L72 4T RTA52EU 20040505002212004050500221NM 2004 5 5 SWAA041251 120040503A575366546486129 WEDGE BOEING737 737317 138447PNM T/E FLAP DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE PANEL DISBONDED. REMOVED AND REPLACED LT WING INBOARD MID FLAP PER MM. 2L72 4F RTA16WE 20040505002232004050500223NM 2004 5 5 SWAA041253 120040503A3350612825 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29766SW 29806 DURING SPV, FOUND EMERGENCY EXIT LIGHTS AT R1, R2 AND L1 DOORS, INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PER MM. 2L72 4F RTA16WE 20040505002252004050500225NM 2004 5 5 SWAA041245 120040503A3350BR2013 LIGHT BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 EEPLS LIGHT AT ROW 8 DEF LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040505002272004050500227NM 2004 5 5 SWAA041232 120040501A52306547952 SKIN BOEING737 737317 138447PNM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN FWD SIDE AT CABLE ATTACH BOLT, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20040505002292004050500229NM 2004 5 5 SWAA041234 120040502A531165C27709 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND BULKHEAD CHORD AT BS 727 BBL 0, CORRODED. REMOVED AND REPLACED BULKHEAD CHORD PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040505002312004050500231NM 2004 5 5 SWAA041236 120040502A53106520723 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME WEB AT BS 492, LOWER STOP FITTING, CRACKED. REPAIRED FRAME WEB PER SB AND ER. 2L72 4F RTA16WE 20040505002332004050500233NM 2004 5 5 SWAA041238 120040502A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM AT BS 957 TO BS 986, CORRODED. REMOVED AND REPLACED BEAM PER SRM. 2L72 4F RTA16WE 20040505002352004050500235NM 2004 5 5 SWAA041226 120040501A3350101114 LENS BOEING737 7373Y0 1384671NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040505002372004050500237NM 2004 5 5 SWAA041228 120040501A5523183A8410 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE HARDWARE PER MM. 2L72 4F RTA16WE 20040505002392004050500239NM 2004 5 5 SWAA041230 120040501A532065C28106 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM VERTICAL WEB AT BS 727 + 7 TO BS 727 + 8, CORRODED. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040505002412004050500241NM 2004 5 5 SWAA041241 120040502A574369378775 FITTING BOEING737 7373H4 1384600NM RT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING RON CHECK, FOUND RT MLG WALKING BEAM FWD FITTING CORRODED. REPAIRED RT MLG WALKING BEAM FITTING PER EA. 2L72 4F RTA16WE 20040505002432004050500243NM 2004 5 5 SWAA041243 120040502A335090083 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29711HK 27845 DURING SPV, FOUND RT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040505002452004050500245NM 2004 5 5 SWAA041212 120040429A53106547951 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND L2 DOOR FRAME LOWER HINGE CUTOUT CRACKED. REPAIRED L2 DOOR CUTOUT PER ER. 2L72 4F RTA16WE 20040505002602004050500260NM 2004 5 5 SWAA041169 120040426A53106977035 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT BS 294.5, RBL 45, CORRODED. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040505002622004050500262NM 2004 5 5 SWAA041171 120040426A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040505002642004050500264NM 2004 5 5 SWAA041173 120040426A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18 R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505002662004050500266NM 2004 5 5 SWAA041175 120040426A53116546581 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT BS 992, RBL 45, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040505002682004050500268NM 2004 5 5 SWAA041178 120040426A5315BAC150518884 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 39, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040505002962004050500296NM 2004 5 5 SWAA041187 120040427A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 FUSELAGE SKIN AT BS 500 D, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040505003032004050500303NM 2004 5 5 SWAA041210 120040429A5751654645424A SKIN BOEING737 7372H4 138448CNM RT AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED RON, FOUND RT WING AILERON OUTBOARD LOWER SURFACE, DELAMINATED. REMOVED AND REPLACED RT WING AILERON PER MM. 2L72 4F A16WE 20040506000512004050600051EU 2004 5 6 MALA040366 120040410A5280 DOOR BAC 146 AVRO146RJ85A1500097EU RT MLG CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15533XJ E2367 DURING C1 & C2 INSPECTION IN LCQ, RIGHT MLG DOOR FWD UPPER EDGE CHAFED. CUT OUT CHAFED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW MESABA EO A52042. A/C RELEASE DATE 4/29/04. 2H74 4F RTA49EU 20040506000672004050600067EU 2004 5 6 R6U2004F00001 120040415A7120307107126 MOUNT BRAERODH125 HS125700A 4230170EU LT ENGINE CRACKED E R6URK NONE O OTHER ININSP/MAINT 1 GL03418RD11539 NA0210 CRACKED AREA WAS BOUND BY MAG PARTICLE INSPECTION DURING ENGINE CHANGE. THE CRACK WAS LOCATED IN THE WEBBING AREA. THE PROBABLE CAUSE WAS A LACK OF RADIUS IN THE WEB AREA, AS THE SPOT FACE USED TO PROVIDE THE FLAT SURFACE FOR THE BEARING HAD AN EXTREMELY SHARP RADIUS IF ANY. SUGGEST USING A SPOT FACE WITH A RADIUS. (R2001) 2L72 4F A3EU 20040506000722004050600072CE 2004 5 6 HYI2004F00001 120040419A801099103971 RELAY CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO STARTER SYS OVERHEATED E HYIAO OTHER M OVER TEMP TXTAXI/GRND HDL 1 NE01106CA 402C1020 PILOT ATTEMPTED START OF LEFT ENGINE, ENGINE DID NOT TURN. MECHANIC FOUND START RELAY OVERHEATED AND DISCOLORED REMOVE AND REPLACED RELAY AND STARTER AS A PRECAUTION AIRCRAFT RELEASED BACK TO SERVICE. 1L72 3O3 O A7CE E8CE 20040506000732004050600073CE 2004 5 6 BLB2004F00000 120040401A80111108249 STARTER CESSNA182 182L 2072726CE CONT O470 O470R 17026SO ENGINE FAILED E BLBAK NONE O OTHER ININSP/MAINT 1 GL1742275 18258937 13288116R TWO OVERHAULED STARTER WERE INSTALLED ON OVERHAULED ENGINE. BOTH STARTERS FAILED TO TURN OVER ENGINE, REINSTALLED OLD STARTER AND ENGINE STARTED AS NORMAL. 1H71 3O3 ONT3A13 E273 20040506000832004050600083NM 2004 5 6 UPS04242241 120040406A5310 DOOR FRAME BOEING727 72731C 1384011NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 INSPECTION TYPE:C LWR FWD CARGO DOOR CUTOUT FRAME, CRACK INDICATION IN AREA NR 4 FWD DOOR STOP. REPAIR CARRIED OUT IAW SMRO EO 2004-027-01 UPS ENGINEERING FILE NR B727-5310-20302-A 2L73 4F A3WE 20040506000852004050600085NM 2004 5 6 UPS04442240 120040329A5330 SKIN BOEING747 747121 1384871NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE:C FUSELAGE BS 835 - 845 STR 39R FOUND PREVIOUSLY REPAIR PATCH LOWER ROW FASTENERS SHORT EDGE MARGIN. EXISTING SKIN CUTOUT ENLARGED PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-10-02 SKIN REPAIR CARRIED AS PER SRM 53-30-03 FIG 11 CATEGORY B REPAIR REQUIRE REPEAT INSPECTION AS PER SRM 53-30-03 FIG 11 TABLE II. 2L74 4F A20WE 20040506000872004050600087EU 2004 5 6 MALA040350 120040425A3520WF11 SWITCH BAC 146 AVRO146RJ85A1500097EU PSU FAILED A MALAG O2 MASK DEPLOYED O OTHER TXTAXI/GRND HDL 1 GL15525XJ E2350 RIGHT SIDE O2 MASKS DROPPED DOWN DURING TAXI OUT OF LEX. MAINTENANCE REPLACED WFI AND PAX DROP SWITCH WF11, REPLACED ROW 10 AND ROW 13 RIGHT GENERATORS. 2H74 4F RTA49EU 20040506000882004050600088EU 2004 5 6 MALA040346 120040421A3250708572 MOTOR SAAB SF340 340B 7860101EU NLG STEERING MALFUNCTIONED A MALAD RETURN TO BLOCK F FLT CONT AFFECTED LDLANDING 1 GL15362PX 340B258 ON TAXI AFTER CLEARING RUNWAY, NOSEWHEEL STEERING BECAME STIFF AND INEFFECTIVE HYD. PRESSURE GOOD. MAINTENANCE REPLACED STEERING NOSE WHEEL MOTOR IAW SF340 MM 32-50-25-4 ALSO COMPLIED WITH SERVICE BULLETIN 340-32-101. ALL CHECKS GOOD. P/N ON/OFF 70857-2, S/N ON C01919G, S/N OFF 0221G. 2L72 4T RTA52EU 20040506000922004050600092NE 2004 5 6 MALA040373 220040429A7320 ECU BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 ENGINE FAILED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 GL15532XJ E2366 DURING APPROACH NR 3 ENGINE EGT EXCEEDED LIMITS, 690 FOR ABOUT 5 SECONDS BEFORE SHUTTING ENGINE DOWN. AFTER ENGINE SHUTDOWN EGT CONTINUED TO OVERTEMP AND INDICATE VARIABLE AS POWER WOULD INCREASE OR DECREASE. WHEN FADEC WAS TURNED ON EGT APPEARED NORMAL FOR A SHUTDOWN EVENT. MAINTENANCE REPLACED ECU AND AS A PRECAUTION REPLACED HMA. FADAMS DOWNLOAD REVEALED ENGINE DID NOT OVERTEMP, INDICATION ERROR ONLY. 2H74 4F4 FRTA49EU E6NE 20040506000932004050600093NE 2004 5 6 MALA040372 320040429A614010223N01R00 INDICATOR SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE LT PROP RPM INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15403XJ 340B403 AFTER TAKEOFF LEFT PROP RPM INDICATOR INDICATED ZERO CYCLED C/B J-8, INDICATOR STILL INDICATED ZERO. WHILE RETURNING TO DTW INDICATOR WORKED INTERMITTENTLY. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED GAUGE P/N 10223N01R00, S/N OFF 117, S/N ON BG05. 2L72 4T RTA52EU 6 CP61GL 20040506000952004050600095EU 2004 5 6 MALA040328 120040401A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION WHILE REMOVING NR 7 ICE SHIELD, FOUND DAMAGED SKIN BENEATH ICE SHIELD. MAINTENANCE REPAIRED DAMAGED SKIN IAW MESABA EO S53009. AIRCRAFT RELEASE DATE 4/16/04. 2L72 4T RTA52EU 20040506000962004050600096EU 2004 5 6 MALA040324 120040403A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION, RIGHT SIDE OF FUSELAGE AT STA 741-768 HAS HEAVY CHAFES FROM HORIZONTAL STAB SEAL. MAINTENANCE REPAIRED DAMAGED AREA IAW MESABA EO S53066. AIRCRAFT RELEASE DATE 4/16/2004. 2L72 4T RTA52EU 20040506000992004050600099NM 2004 5 6 CALA0400408 120040422A3320 SOCKET BOEING757 757224 1384958NM CABIN FAULTY A CALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2717128 27567 PASSENGERS IN ROW 21 - 23 AIRCRAFT LEFT AND RIGHT REPORTED A FAINT SMELL OF RUBBER WHICH COMES AND GOES. FOUND BURNED CONTACT AT FLUORESCENT FIXTURE AT 21 ABC. PULLED AND COLLARED C/B AND PLACARD LIGHT SYSTEM. 2L72 4F RTA2NM 20040506001002004050600100NM 2004 5 6 CALA0400409 120040423A532065457832 MOUNT BRACKET BOEING737 7373T0 1384582NM NR 2 VHF ANTENNACRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 CRACK (3.5 INCH) IN MOUNT FOR NUMBER TWO VHF ANTENNA IN FORWARD CARGO COMPARTMENT. REPLACED MOUNT PER SRM 51-40-02. 2L72 4F RTA16WE 20040506001022004050600102NM 2004 5 6 CALA0400449 120040502A5320143A948523 SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND LEFT STANCHION SUPPORT ASSEMBLY IN FORWARD PIT AT AFT BULKHEAD CORRODED AT STA 500I. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040506001042004050600104NM 2004 5 6 CALA0400451 120040502A5320143A7510 INTERCOSTAL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND RIGHT INTERCOSTAL UNDER Z-CHANNEL IN FORWARD CARGO PIT CORRODED AT STA 500D AND 500E. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 143A7510. 2L72 4F RTA16WE 20040506001072004050600107NM 2004 5 6 CALA0400454 120040503A53306545774 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND A 2.5 INCH CRACK IN RIGHT FUSELAGE SKIN JUST AFT OF AFT WING FAIRING, 27 INCHES AFT OF STA 727E. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 229, SHEET 21. 2L72 4F RTA16WE 20040506001082004050600108NM 2004 5 6 CALA0400455 120040503A5350149A761115 WEB BOEING737 737824 13844BZNM FAIRING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND A CRACK IN O/B WEB OF LEFT W/W AFT SKI JUMP FAIRING. THE WEB WAS REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040506001092004050600109NM 2004 5 6 CALA0400456 120040503A5350149A761413 FRAME BOEING737 737824 13844BZNM FAIRING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND A 5 INCH CRACK IN LOWER I/B CHORD AND IN LOWER O/B CHORD ON LEFT W/W AFT SKI JUMP FAIRING. NEW CHORDS WERE INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040506001102004050600110NM 2004 5 6 CALA0400457 120040503A5350149A761116 WEB BOEING737 737824 13844BZNM FAIRING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND A 5 INCH CRACK IN O/B WEB ON RIGHT W/W AFT SKI JUMP FAIRING. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040506001122004050600112NM 2004 5 6 CALA0400459 120040503A5315 FLOORBEAM BOEING757 757224 1384958NM STA 1640 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714102 27292 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1640 BETWEEN LBL 9 AND RBL 14, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20040506001132004050600113NM 2004 5 6 CALA0400460 120040503A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344. REPAIRED IAW SRM 51-70-12. 2L72 4F RTA16WE 20040506001152004050600115NM 2004 5 6 CALA0400462 120040504A5320143A750114 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN FORWARD CARGO PIT. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040506001172004050600117NM 2004 5 6 CALA0400464 120040504A53206548607 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE FOR RIGHT RAM AIR INLET AT BS 540, S22R. THE CRACKED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11. 2L72 4F RTA16WE 20040506001192004050600119 2004 5 6 CALA0400466 420040504A2340285T000169 CIRCUIT CARD BOEING757 757224 1384958NM INTERPHONE SYS FAULTY A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW271210935840 27299 THE FLIGHT ATTENDANTS REPORTED SMOKE/HAZE AND SMOKEY ODOR IN CABIN WHILE AT CRUISE. THE QRH PROCEDURE FOR SMOKE IN CABIN WAS COMPLETED AND THE GALLEY AND VIDEO EQUIPMENT CIRCUITS WERE DEACTIVATED. THE HAZE CEASED, BUT THE ODOR REMAINED. THE AIRCRAFT LANDED AT ITS SCHEDULED STATION IN IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE INTERPHONE AUDIO ACCESSORY UNIT AT FAULT. THE UNIT HAD A BURNED AMP CARD. THE AUDIO ACCESSORY UNIT WAS REPLACED IAW MM 23-42-01. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20040506001202004050600120NM 2004 5 6 CALA0400467 120040505A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 328. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-12. 2L72 4F RTA16WE 20040506001212004050600121EU 2004 5 6 MALA040331 120040403A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION, LEFT SIDE OF FUSELAGE AT STA 741-768 HAS HEAVY CHAFES FROM HORIZONTAL STAB SEAL. MAINTENANCE REPAIRED DAMAGED AREA IAW MESABA EO S53066. AIRCRAFT RELEASE DATE 4/16/2004. 2L72 4T RTA52EU 20040506001222004050600122EU 2004 5 6 MALA040334 120040407A33506104789 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15363PX 340B260 BATTERY PACK P/N 61-0478-9, S/N 1875 WAS REMOVED ON 4/3/04 FOR SCHEDULED CAPACITY CHECK. UNIT FAILED CAP CHECK ON 4/7/04. UNIT WAS DEEP CYCLED AND RECHARGED UNIT THEN PASSED CMM TESTS ON 4/10/04. 2L72 4T RTA52EU 20040506001232004050600123EU 2004 5 6 MALA040326 120040331A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION, RIGHT SIDE OF FUSELAGE HAS SEVERAL DENTS AT STA 340 FROM SL1632-1634. MAINTENANCE REPAIRED DENTS IAW MESABA EO S53009. AIRCRAFT RELEASE DATE 4/16/2004. 2L72 4T RTA52EU 20040506001242004050600124EU 2004 5 6 MALA040325 120040331A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 LEFT SIDE OF FUSELAGE HAS SEVERAL DENTS AT STA 340 FROM 1532-1534. REPAIRED DENTS IAW MESABA EO S53009, AIRCRAFT RELEASE DATE 4/16/04. 2L72 4T RTA52EU 20040506001262004050600126EU 2004 5 6 MALA040327 120040331A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 DURING INSPECTION, LEFT SIDE OF FUSELAGE HAS SEVERAL DENTS AT STA 340 FROM SL1632-1634. MAINTENANCE REPAIRED DENTS IAW MESABA EO S53035. AIRCRAFT RELEASE DATE 4/16/2004. 2L72 4T RTA52EU 20040506001282004050600128WP 2004 5 6 ASAA0480132 120040229A5313993607313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND AFT PIT STATION 1212 LONGERON 26L HAS CORROSION ON TOP OF SPLICE PLATE. REMOVED DAMAGED PLATE, FABRICATED AND INSTALLED REPLACEMENT PLATE IAW MD80 SRM 51-10-4. (M) 2L72 4F RTA6WE 20040506001332004050600133NM 2004 5 6 ASAA0410048 120040206A534069353521 STRINGER CLIP BOEING737 737210C 1384459NM FUSELAGE GOUGED A K NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER CLIP AT BS 907, STRINGER 25L GOUGED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040506001342004050600134NM 2004 5 6 ASAA0410047 120040206A53136546526 STRINGER BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 28R AT BS 400 CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040506001372004050600137NM 2004 5 6 ASAA0470001 120040223A33508100022601 BATTERY PACK BOEING737 737790 13844CNNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01617AS 30542 SEA - DURING MAINTENANCE CHECK, FOUND FLOOR TRACK LIGHT INOPERATIVE AT ROW 15C. REPLACED BATTERY PACK, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040506001382004050600138WP 2004 5 6 ASAA0480192 120040214A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP COCKPIT NOT SEATED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01964AS 53078 SEA - DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY FLOOD LIGHTS INOPERATIVE. RESEATED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 20040506001392004050600139WP 2004 5 6 ASAA0480185 120040312A2560220123101 GIRT BAR DOUG DC9 DC982 3022082WP L1 DOOR OUT OF POSITION A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS 49235 PHX - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE GIRT BAR PULLED FROM FABRIC SLEEVE. RESECURED BAR TO SLIDE FABRIC SLEEVE. (M) 2L72 4F A6WE 20040506001402004050600140NM 2004 5 6 ASAA0480191 120040316A33501001191 LIGHT DOUG MD80 MD83 3023681NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS470486549 53471 PDX - FOUND DURING LINE CHECK, PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040506001472004050600147NM 2004 5 6 ASAA0410046 120040206A5414657094715 PANEL BOEING737 737210C 1384459NM NR 1 PYLON PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND THE NR 1 ENGINE PYLON PANEL NR 5140 PUNCTURED. REPAIRED PER EA. (M) 2L72 4F A16WE 20040506001482004050600148NM 2004 5 6 ASAA0410057 120040209A5313654577741 STRINGER BOEING737 737210C 1384459NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 OKC - DURING SCHEDULED C-CHECK, FOUND STRINGER 25L AT BS 907-947 CORRODED. REPAIRED PER SRM. (M) 2L72 4F A16WE 20040506001522004050600152NM 2004 5 6 ASAA0410069 120040214A335086210144 BATTERY BOEING737 737290C 138448VNM SMOKER BARRIER DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY EXIT SIGN ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN LIGHT TESTED NORMAL. (M) 2L72 4F A16WE 20040506001552004050600155WP 2004 5 6 ASAA0480133 120040229A532059364423 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV6 CHECK, FOUND PIT CORROSION ON TOP AND BOTTOM OF WEB BETWEEN STATION 1211 AND 1212 LONGERON 30 TO 28R. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-10-4. (M) 2L72 4F RTA6WE 20040507000062004050700006GL 2004 5 7 S04472017 220040301A7230 BLADE BOEING747 747400 NM GE CF6 CF680C2* GL NR 2 ENGINE MISSING W SAJFD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 WP03 30765 747F B18708 A/C GTB DUE TO HEAVY SNOW AT LUX. ENG-2 SURGED AND FLAMEOUT DURING T/O ROLL (GROUND SPEED<45 KNOTS), GTB AGAIN. GROUND INSP FOUND METAL DEBRIS IN ENG-2 TAIL PIPE. BORESCOPE ALL 4 ENGINES, FOUND ENG-3 4 EA HPC 1ST STAGE BLADES L/E AND T/E TIP MATERIAL MISSING WHICH ARE OUT OF LIMIT. NR 1 AND NR 4 ENGINE BSI RESULTS WERE NORMAL. NR 2 AND NR 3 ENGINES WERE REPLACED BY AOG TEAM. ENGINE RUN UP AND TEST FLIGHT NORMAL. 2L74 4F4 FRTA20WE E23EA 20040507000122004050700012NE 2004 5 7 ANCF200400007 220040418A7532AC69178 SOLENOID BOEING757 757236 1384971NM RROYCERB211 RB211535E4 54555NE RT BLEED VLV INOPERATIVE W ANCFC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO23506NA 24771 30737 TAKE OFF WAS DISCONTINUED AT 90KNS RT ENG EGT WAS IN YELLOW BAND, CONTINUE RAISING. ENG EGT WAS MORE THAN LIMIT WAS ACCOMPLISHED BLOCK 5.2,11,17 AND 24 TEST NR 3 LP/HP COMPR AIRFLOW CONTROL TEST IAW AMM. TAKE OFF PWR WAS PERFORMED IP BLEED V/VS SOLENOID AND HP BLEED V/VS SOLENOIDS SWAP WITH ENG LT PERFORMED BITE TEST TO BVCU AND TPU PERFORMED TEST NR3 COMPR AIR FLOW CNTRL TEST WAS OK, EGT AT 1,796EP WAS 772ºC AMM. LT HP3 BLEED V/V SOLENOID P/N AC67960 ON Y OFF S/N EFV202 S/N RU058 RT HP3 BLEED V/V SOLENOID P/N AC69178 ON Y OFF S/N MR316 S/N RX286 HP2 BLEED V/V SOLENOID P/N AC67960 ON Y OFF S/N MO349 S/N PJ078 P BLEED V/V SOLENOID P/N AC67760 ON Y OFF S/N MQ278 S/N RX295 LT IP BLEED V/V SOLENOID ON Y . 2L72 4F4 FRTA2NM E12EU 20040507000132004050700013EU 2004 5 7 BAQA094102 120040423A2822P94C16602 PUMP AEROSPAS355 AS355F1 8680810EU FUEL BOOST INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03652PM75 5179 FUEL PRESSURE DROPPED TO ZERO, AND FUSE BLOWN. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/28/2004 1G72 3U H11EU 20040507000152004050700015SW 2004 5 7 HEEA094283 120040419A7722212075067113 INDICATOR BELL 412 412 1182202SW ITT FLUCTUATES E HEEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03108X 33115 SHORTLY AFTER TAKEOFF, THE NR 1 ITT INDICATOR FLUCTUATED. RETURNED. MAINTENANCE REPLACED ITT INDICATOR. 1G72 4U H4SW 20040507000172004050700017GL 2004 5 7 ALGA094285 220040428A72106893672 GEAR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL FUSELAGE TOP SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03519AL591 760058 CAE890585S FOUND SPALLING AND GALLING ON PINION GEAR TEETH. SENT TO VENDOR FOR WARRANTY CREDIT. 1G72 3U3 U H1NE E1GL 20040507000192004050700019EU 2004 5 7 BAQA094105 120040427A3233 ACTUATOR AEROSPSA365 SA365N 8680669EU DRAG STRUT LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03365S 5879 19 6036 ACTUATOR IS LEAKING. REPLACED WITH SERVICABLE UNIT. 04/28/2004 1G72 3U H10EU 20040507000282004050700028EU 2004 5 7 ULX2004F00005 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP23223LA1022 3278 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION: USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U H9EU 20040507000302004050700030EU 2004 5 7 ULX2004F00008 120040310A3340017601 HOUSING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE SPOT LIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP23221LA647 3220 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U3 U H9EU E19EU 20040512001292004051200129EU 2004 5 12 AWXA200400427 120040402A5347D5323046720000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12 & 18. 2L72 4F RTA28NM 20040512001312004051200131EU 2004 5 12 AWXA200400428 120040402A5347D5337111000800 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 LT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 LT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11, FIG 12 & 18. 2L72 4F RTA28NM 20040512001372004051200137EU 2004 5 12 024461 120040428A3260 WARNING LIGHT SAAB SF340 SF340A 7850100EU MLG MALFUNCTIONED A UHLAO OTHER N FALSE WARNING LDLANDING 1 GL17157SD 157 ON APPROACH TO PIT THE LANDING GEAR WAS SELECTED DOWN. AIRCREW DID NOT RECEIVE THE LIGHT FOR THE LEFT MAIN GEAR DOWN AND LOCKED. AIRCREW CYCLED THE GEAR THREE TIMES WITH THE SAME OUTCOME. THE TRANSIT LIGHT WAS OUT AND THE GEAR APPEARED DOWN. AIRCREW PREFORMED A FLY BY TO VERIFY THE GEAR IS DOWN. AIRCRAFT LANDED SAFELY IN PIT 2L72 4T RTA52EU 20040512001512004051200151EU 2004 5 12 AWXA200400430 120040402A5347D5337111200100 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 RT BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 41 TO FR 47; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12 & 18. 2L72 4F RTA28NM 20040512001522004051200152EU 2004 5 12 AWXA200400431 120040402A5347D5323046320000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y1292 LT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 LT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9 & 18. 2L72 4F RTA28NM 20040512001532004051200153EU 2004 5 12 AWXA200400432 120040402A5347D5323046420000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 LT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 LT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 12. 2L72 4F RTA28NM 20040512001542004051200154EU 2004 5 12 AWXA200400434 120040402A5347D5323046420000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28640AW 448 MCN - MAJOR REPAIR - DURING C-8 CHECK FRETTING CORROSION WAS FOUND ON CABIN SEAT TRACK Y765 RT BETWEEN FR 24 AND FR 35. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT FROM FR 24 TO FR 35; RECEIVED AND INSTALLED A NEW REPLACEMENT SECTION OF SEAT TRACK IAW A320 SRM 51-42-11 FIG 9-12, & 18. 2L72 4F RTA28NM 20040512001552004051200155NM 2004 5 12 0400686316 120040507A3350 CONNECTOR BOEING747 747451 1384940NM EMERGNECY LIGHT LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01676NW 33002 DURING LINE CHECK, FOUND LT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-65. SECURED LOOSE CONNECTION ON LIGHT SOCKET. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040513000052004051300005NM 2004 5 13 DHL2004764004 120040430A2760 SPOILER BOEING727 727264 138408MNM ZONE 500 OUT OF ADJUST A DHLAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO01764AT 22984 A PULSATING HIGH FREQUENCY VIBRATION IS FELT THROUGH THE YOKES AND THRUST LEVERS. THE VIBRATION IS MORE INTENSE DURING CLIMB THAN IN CRUISE, AND IS MORE INTENSE IN CAPTAINS YOKE. SUSPECT THE VIBRATION IS ENGINE RELATED. ALL ENGINE GAUGES INDICATE NORMALLY. WITH THRUST LEVERS AT IDLE ON DESCENT VIBRATION DECREASES. GRND RAN ENG'S FROM IDLE TO 1.90 EPR NO VIBRATION NOTED. PERFORMED COMP. BLEED VALVE CHECK IAW JRH 7.2, NO DEFECTS NOTED ON ALL ENG'S. FOUND NR 2 GROUND SPOILER OUT OF ADJ. IN RETRACT POS. ADJ SPOILER AND STOP IAW M/M 27-62-1, CHECKED FLAP ECCENTRICS IAW M/M 27-51-12 NO DEF NOTED. CHECKED COVE PANELS, NO DEFECTS NOTED. 2L73 4F A3WE 20040513000072004051300007 2004 5 13 COMA0460296 420040502A3440 TRANSCEIVER CNDAIRCL600 CL6002B19 1900309EA RADAR MALFUNCTIONED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01507CA709 189BC 7796 FLIGHT 5026 RADAR FAILED, REPLACED THE RADAR RECEIVER/TRANSMITTER. 2L72 4F RTA21EA 20040513000122004051300012NM 2004 5 13 P5CA0401069 120040413A4950 BLEED VALVE BOEING747 747341 13848AMNM APU FAILED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 APU BLEED AIR VALVE FAILED ON PUSHBACK ENGINE START. DEFERRED APU BLEED AIR IAW MEL 49-1-1. 2L74 4F RTA20WE 20040513000142004051300014NM 2004 5 13 252TR0021 120040503A3350ML81 LAMP BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS NORMAL. 2L72 4F RTA16WE 20040513000152004051300015 2004 5 13 106041 420040413A3410066500013104 DISPLAY BEECH 1900 1900C 1154161CE VSI INOPERATIVE A NSVAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27119CJ UC19 CAPTAINS VSI DISPLAY UN-USEABLE AND DISCHARGING BURNED ODORS IN CABIN REMOVED AND REPLACED CAPTAINS VSI PERFORMED SATISFACTORY STATIC CHECK IAW AMM 34-10-06. 2L72 4T RTA24CE 20040513000162004051300016WP 2004 5 13 DHL2004801005 120040509A2750 DRIVE LINK DOUG DC8 DC873F 302199FWP TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 DURING NDT INSPECTION OF RT IB FLAP DRIVE LINK FOUND CRACK OUT OF LIMITS ON LINK. REMOVED AND REPLACED RT IB FLAP DRIVE LINK IAW M/M 27-51-4. OPS CHECKED OK. 2L74 4F RT4A25 20040513000172004051300017EA 2004 5 13 SWIA200413283 120040503A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (FOUND DURING C-CHECK INSPECTION). REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-21-11, AND 51-42-21. REF. RII 53-401. 2L72 4F RTA21EA 20040513000432004051300043NM 2004 5 13 USAA040049 120040212A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US 23558 FOUND SKIN CRACKED 2 INCHES, 727D AND S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040513000462004051300046NM 2004 5 13 USAA040068 120040329A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US51825 22957 FOUND SKIN CRACKED 2.5 INCHES, BETWEEN BS 727 D/E BELOW STATION AT 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040513000482004051300048NM 2004 5 13 USAA040064 120040327A53201134849 SHEAR WEB BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US 23557 FOUND SHEAR WEB CORRODED 3 INCHES BY 10 INCHES, TOP AND LOWER SURFACE OF FLOOR PAN AT AFT PRESS BULKHEAD, RBL 0-15. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-2. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20040513000582004051300058NM 2004 5 13 USAA040046 120040307A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US53965 22953 FOUND SKIN CRACKED .5 INCH, FUSELAGE SKIN AND BEAR STRAP BS 957 S-14R SERVICE DOOR LOWER HINGE. INSTALLED DOUBLER PER SRM 53-60-01 AND EA 78095. (M) 2L72 4F RTA16WE 20040513000622004051300062WP 2004 5 13 04FDEA01157 120040506A5347 CARGO TRACK DOUG DC10 DC1010 3022110WP MAIN CARGO COMPTELONGATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CARGO COMPT CARGO TRACK HAS AREAS OF ELONGATED SCALLOPS FROM FS 999-1029 RBL 47. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-70-00 FROM STA 989 TO 1009 AT MAE. 2L73 4F A22WE 20040513000642004051300064EU 2004 5 13 04FDEA01159 120040507A5510 STRUCTURE AIRBUS310 A310203 3930313EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE 248 LEFT HORIZONTAL STABILIZER FIXED LEADING EDGE, ZONE 330 (FWD SPAR) UPPER LIP UPPER SECTION APPROX STA 158 RIB 5, 4 EA AREAS 1.0 INCH L ,(.200 INCH W AREA 2 & 3 AS MARKED), (.100 INCH W AREA 1 & 4 AS MARKED). UNABLE TO DETERMINE DEPTH WITHOUT BLENDOUT, CORROSION AT THIS TIME MEETS LEVEL 1 CORROSION, WITHOUT MATERIAL AND SURFACE PROTECTION REMOVAL. CHORD FLANGE, BLENDED CORROSION IAW SRM 51-74-10 & FOUND UPPER T-CHORD OUT OF LIMITS. CUT & REMOVED DAMAGED SECTION OF UPPER TEE CHORD IAW A310 SRM 55-11-21, PARA 6(E) 2 FIG 205 & 210. APPLIED ALODINE AND PRIMER & TOP COAT TO ALL REPAIR SURFACES IAW A310 SRM 51-21-00 & 51-23-00. INSTALLED REPAIR IAW A310 SRM 55-11-21 FIG 205 & 210. 2L72 4F RTA35EU 20040513000702004051300070NM 2004 5 13 04FDEA01192 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.500, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.498 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000732004051300073NM 2004 5 13 04FDEA01195 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000862004051300086NM 2004 5 13 04FDEA01187 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.502 MATERIAL REMOVED: 0.002 REMAINING THICKNESS: 0.500 AND REPAIRED AS PER FEDEX EA 1-5750-75954. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513001052004051300105NM 2004 5 13 04FDEA01140 120040503A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, OUTBOARD FLAP VANE NR 2 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20040513001112004051300111NM 2004 5 13 04FDEA01136 120040503A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, OUTBOARD FLAP VANE NR 3 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NR 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK 2L73 4F RTA22WE 20040513001222004051300122NM 2004 5 13 04FDEA001073 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. 2L73 4F RTA22WE 20040513001282004051300128WP 2004 5 13 04FDEA001096 120040424A7120NSL60235 MOUNT DOUG DC10 DC1010 3022110WP ZONE 400 WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 NR 3 ENGINE AFT MOUNT BEARING MIGRATING. REMOVED AND REPLACED NUMBER 3 ENGINE AFT MOUNT IAW DC-10 MM 71-20-02-2. 2L73 4F A22WE 20040513001302004051300130NM 2004 5 13 04FDEA001078 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. 2L73 4F RTA22WE 20040513001342004051300134NM 2004 5 13 04FDEA001082 120040424A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. 2L73 4F RTA22WE 20040514000112004051400011NM 2004 5 14 04FDEA001026 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. 2L73 4F RTA22WE 20040514000172004051400017NM 2004 5 14 CALA0400471 120040505A5415 SUPPORT ANGLE BOEING737 7373T0 1384582NM NACELLE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND A 3 INCH CRACK IN SUPPORT ANGLE AT RT NACELLE STA 363.65 ON I/B SIDE RADIUS. A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 54-50-71 AND 51-40-02. 2L72 4F RTA16WE 20040514000192004051400019NM 2004 5 14 CALA0400473 120040505A53206546812187 BRACKET BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND RT DIAGONAL SUPPORT BRACKET CORRODED AT STA 992-1018. THE SUPPORT BRACKET WAS REPLACED IAW MM 51-21-31 AND SRM 51-40-02. 2L72 4F RTA16WE 20040514000322004051400032WP 2004 5 14 GTIA040310 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND MAIN C/B STATION 1174 TO STATION 1193 RIGHT SIDE MID HAS CRACKS AND DAMAGED ON EDGE. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000362004051400036NM 2004 5 14 HALA0400438 120040409A212173251C FAN BOEING767 76733AER 1385230NM CABIN ODOR A HALAO OTHER O OTHER DEDESCENT 1 WP13584HA 25531 BURNING ODOR ON DESCENT INTO HNL AFTER SELECTING TERRAIN ON THE CAPTAINS SIDE. ODOR WENT AWAY AFTER DESELECTING, ELECTRICAL ODOR IN NATURE. TERRAIN SYSTEM CHECK OK PER MM 34-46-00-5. REPLACED FORWARD RACK COOLING FAN PER MM 21-58-06. LEAK AND OPERATIONAL OK. REINSTALLED SIDE WALL PANEL. (M) 2L72 4F RTA1NM 20040514000432004051400043EA 2004 5 14 ASOA04279 120040411A5210601R3170767 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11705EV 10051 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR BOTTOM STEP AIW SRM 51-73-00. (M) 2L72 4F RTA21EA 20040514000502004051400050EU 2004 5 14 USAA040073 120040330A5320D53480048202 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW 0929 BFM - FOUND SILL SHAPE CORRODED 2 INCHES BY .50 INCH BY .02 INCH AREA, BETWEEN FRAME 66 AND 68, Y +1732, -Z240. REMOVED AND REPLACED SILL SHAPE PER SRM 51-74-00 AND 53-41-79. (M) 2L72 4F RTA28NM 20040514000562004051400056EU 2004 5 14 USAA040077 120040327A5347D5347209000200 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND SEAT TRACK ASSEMBLY CORRODED .1 INCH BY 1 INCH BY .49 INCH DEEP, FS 66 Y765, -Z35. REMOVED AND REPLACED SEAT TRACK ASSEMBLY PER SRM 51-74-00, 53-00-14, 51-42-00 AND 51-23-01. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040514000632004051400063NE 2004 5 14 KBM2004F00025 220040318A72300292005220 GUIDE VANE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE CRACKED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19115SH107 3141 9666 REMOVAL OF ENGINE FOR DISC REPLACEMENT. FOUND CRACK ON 1ST STG NOZZLE GUIDE VANES. DURING 2ND STAGE TURBINE WHEEL AND BLADE REPLACEMENT 263 SB. REMOVED AND REPLACED ENGINE WITH RENTAL. 1G71 3U3 U H9EU E19EU 20040514000642004051400064EU 2004 5 14 KBM2004F00026 120040330A6510704A33640014 BUSHING SNIAS 350 AS350BA 8680817EU DRIVE LINK WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 REMOVED AND REPLACED LOWER STATIONARY DRIVE LINK BUSHING WORN. 1G71 3U NCH9EU 20040514000702004051400070EA 2004 5 14 WVE2004F00010 120040426A57206001020428 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT WING CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09408SW 7055 RT WING STA 48.30 ANGLE PN 600-1020428 IS CRACKED , 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040514000752004051400075CE 2004 5 14 FCPR200400013 120040419A3242 BRAKE ASSY BEECH 90 C90A 1152911CE PWA PT6 PT6* 52043EA LT MLG CRACKED B FCPRO OTHER O OTHER NRNOT REPORTED 1 NM09691AS3054 LJ1240 TORQUE PLATE BROKE WHEN APPLYING BRAKES, APPEARS THAT CRACK STARTED UNDER BUSHING THAT CARRIES THE CALIPER PINS, DOES NOT HAVE A PROCEDURE TO REMOVE BUSHINGS TO CHECK FOR CRACKS. 1L72 3T3 TRT3A20 E2NE 20040514000772004051400077EA 2004 5 14 WVE2004F00012 120040426A5320601R31148 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CORRODED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09408SW 7055 LT FLOOR SILL PN 601R3114863 BETWEEN FS 364 AND FS 379 IS SEVERELY CORRODED. PROBABLE CAUSE: POSSIBLE WATER INTRUSION. (EA09200402076) 2L72 4F4 FRTA21EA E15NE 20040514000812004051400081EU 2004 5 14 KBM2004F00029 120040307A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P1022 2347 REMOVED AND REPLACED BEARINGS, WORN OUT. 1G71 3U NCH9EU 20040514000852004051400085NM 2004 5 14 K5S2004F00000 120040420A24972803500000 CONNECTOR GULSTM200 200 4500308NM PWA 306 PW306B NE WIRE HARNESS FAILED B K5SRO OTHER O OTHER NRNOT REPORTED 1 NM07363GA 063 J2 CONNECTOR FAILED TO LOCK. 2L72 4F4 FRTA53NM E35NE 20040514000902004051400090SW 2004 5 14 KBM2004F00033 120040319A2841 FLOAT BELL 206 206B 1181511SW FUEL CELL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV64 6325 2704 FLOAT DOES NOT FLOAT, FILLS UP WITH FUEL. REMOVED AND REPLACED. 1G71 3U H2SW 20040514001042004051400104NM 2004 5 14 HNAA0400054 120040511A531185320937 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 SKIN CORRODED UNDER FRAME X252 BETWEEN STR 31S AND 30S, REMOVED AND REPLACED FRAME IAW EO 8-53-04-0315 CLEANED AND TREATED SKIN CORROSION. 2H72 4T RTA13NM 20040514001092004051400109NM 2004 5 14 QXEA200400317 120040510A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - PITTING ON LT IB SEAT TRACK IN BOTTOM CENTER FROM STATION X217.000 TO STATION X223.000. REPAIRED IAW EA 6-53-346. 2H72 4T RTA13NM 20040517000042004051700004EU 2004 5 17 USAA040084 120040330A5347D2353342650000 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND SEAT TRACK/BEAM ASSEMBLY CORRODED 1 INCH LONG BY .040 INCH WIDE BY .119 INCH DEEP, FRAME 24, -Y 1292, -Z 240. INSTALLED SEAT TRACK SPLICE/DOUBLER REPAIR PER SRM 53-00-15 AND SRM 42-11, 53-43-1. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040517000142004051700014EU 2004 5 17 USAA040094 120040401A5321D5367180500500 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOOR PANEL CORRODED 3 INCHES LONG BY 2 INCHES WIDE BY .02 INCH DEEP, MAIN DECK FLOOR PANEL 262FF. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-72-11 AND 51-42-11. (M) 2L72 4F RTA28NM 20040517000192004051700019WP 2004 5 17 GTIA040288 120040309A5310 DOUBLER DOUG DC9 DC982 3022082WP DOOR BEAM CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CORROSION ON MID PIT DOOR BEAM REPAIR DOUBLER FROM STATION 636 TO 693 AND ON FRAME AT STATION 693. REMOVED REPAIR STRAP. FABRICATED NEW REPAIR STRAP. INSTALLED REPAIR DOUBLER. (M) 2L72 4F A6WE 20040517000282004051700028EA 2004 5 17 A6WA200440049 120040419A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AW 7878 THE RIGHT FUSELAGE SKIN WAS DAMAGED WHEN THE SERVICE DOOR WAS OPENED WHILE PRESSURIZED. FUSELAGE SKIN WAS DENTED BETWEEN STRINGERS 13/14 APPROX 3.5 INCHES AFT OF FS 295 AND DENTED WITH A CREASE BETWEEN STRINGERS 16/17 AT FS 295. TRIMMED OUT SKIN PANEL AND FRAME FLANGE. ALL CRACKS REMOVED. REPAIRED FRAME FLANGE BY FABRICATING REPAIR ANGLE. ALL WORK DONE IAW BRAS EO 601R-53-4835. (M) 2L72 4F RTA21EA 20040517000332004051700033WP 2004 5 17 GTIA040278 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN STATION 180 RBL 9 RBL 44 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20040517000392004051700039 2004 5 17 GTIA040275 420040410A2565 CLIP DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 RSW - FOUND L1 DOOR SLIDE PACK LANYARD CLIP FELL OFF. INSTALLED SLIDE PACK LANYARD CLIP. CLIP SECURE. (M) 2L72 4F A6WE 20040517000452004051700045SO 2004 5 17 C2XA04CL053 120040507A2120 ODOR EMB 145 EMB145XR 3260214SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2712126 145693 IAH FLIGHT NR 2039, THE CREW REPORTED A STRONG BURNING ODOR WHEN THE ANTI-ICE SYSTEM WAS ON. MAINTENANCE INSPECTED AND PERFORMED ANTI-ICE TEST. NO DEFECTS OR EVIDENCE OF A BURNING ODOR. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RT 20040517000462004051700046EU 2004 5 17 DHL2004364507 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, N/R 5527 CABIN, 10TH SEAT TRACK FROM LT. SIDE, HAS CORROSION ON IB AND OB LOWER FLANGES BETWEEN FRAME 19-24 AND HEAVY CORROSION INSIDE TRACK OF FRAME 20. CUT OUT SEAT TRACK AT FR. 23 1/2 AND REMOVED SEAT FROM FR. 19 TO 23 1/2 IAW A-300 SRM 53-10-10 FIG. 724. 2) TRIMMED TO FIT NEW SEAT TRACK FROM FR. 19 TO 23 1/2 (8.5 FEET) AND REPAIR ANGLES ( 4 EACH ) AT 23 1/2 IAW A-300 SRM 53-10-10 MATERIAL USED AS FOLLOWS. SEAT TRACK- 60-22457, (4 EACH) REPAIR ANGLES - 60-12336. TREATED, PRIMED, AND POLYWHITE SEAT TRACK AND REPAIR ANGLES IAW A-300 SRM 51-40-12 AND INSTALLED SEAT TRACK AND REPAIR ANGLES BETWEEN FR. 19-FR.24, 10TH FROM LT. 2L72 4F RTA35EU 20040517000492004051700049WP 2004 5 17 MWEA040075 120040512A217017946081 SEPARATOR DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE CABIN AIR INOPERATIVE A MWEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31804ME 48030 STRONG FUMES IN CABIN. REMOVED AND REPLACED WATER SEPARATOR. 2L72 4F4 F A6WE E9NE 20040517000592004051700059NM 2004 5 17 20040513 120040430A2710BACB10BW21 BEARING BOEING727 727227 1384078NM AILERON DETERIORATED A SQ7AO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO018642653159100 21364 DURING LOW SPEED FLIGHT, WHEN TURNING RIGHT, AS WHEEL PASSES 30-35 INDEX MARK, VIBRATION OCCURS. REMOVED AND REPLACED LT IB AILERON QUADRANT BEARINGS AND ADJUSTED AILERON SYSTEM IAW MM. 2L73 4F A3WE 20040517000602004051700060NM 2004 5 17 04FDEA01141 120040503A2750ARC70531 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, OUTBOARD FLAP, VANE NR 1 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20040517000612004051700061NM 2004 5 17 DHL2004755013 120040513A2612 MODULE BOEING727 727225 1384077NM APU FIRE DETECT MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01755DH 21857 APU FIRE LIGHT AND BELL CAME ON. FIRE HANDLE PULLED LIGHT OUT AND BELL SILENCED. TRANSFERRED TO DMI NR 16580 IAW MEL 49-1 CAT. (C) PLACARD INSTALLED FIRE HANDLE PULLED. APU FIRE LIGHT AND BELL CAME ON FIRE HANDLE PULLED. LIGHT OUT AND BELL SILENCED. REMOVED AND REPLACED APU MODULE ASSEMBLY, RUNS, ADJUSTMENT, AND TEST PER B-727 M/M 49-00 & 26-15-0. OPS CHECKED NORMAL. THIS CLEAR DMI 16580. PLACARD REMOVED. 2L73 4F A3WE 20040517000782004051700078EU 2004 5 17 AWXA200400492 120040510A3610 TRANSDUCER AIRBUS320 A320232 3930326EU NR 2 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28657AW 1003 ON CLIMB OUT, EN ROUTE, RECEIVED ECAM MESSAGE (AIR ENG 2 BLEED ABNORMAL PRESSURE), BLEED VALVE INDICATED CLOSED WITH (0) PSI, TURNED BACK & LANDED WITHOUT FURTHER EVENT. MAINT R & R NR 2 ENG BLEED PRESSURE REGULATOR VALVE CONTROL SOLENOID (10HA2) IAW AMM, AND BLEED REGULATED PRESSURE TRANSDUCER (8HA2) IAW AMM, OPS & LEAK CHECKS GOOD. TEST OF TEMPERATURE LIMITATION SOLENOID THERMOSTAT S/N 2652 CONFIRMED FAILURE OF UNIT FOR LEAKAGE OUT OF TOLERANCE. SOLENOID WAS FOUND LEAKING & STICKING OPEN AND THE DIAPHRAGM HOLES WHERE ENLARGED. REPLACED BASE, SOLENOID CORE, DIAPHRAGM, SOLENOID SEAT, AND CLAPPER. UNIT TESTED GOOD IAW CMM 36-11-43. 2L72 4F RTA28NM 20040517000802004051700080NM 2004 5 17 AWXA200400494 120040504A53126517582 VERTICAL BEAM BOEING737 7373Y0 1384671NM BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB ON AFT SIDE RUNNING FROM BLANKET HOLE AT LBL 5.7, WL 180. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL BEAM WEB AT LBL 5.7, WL 180; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, FIG. 1. 2L72 4F RTA16WE 20040517000822004051700082NM 2004 5 17 AWXA200400496 120040420A5311BAC1517705 FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 LCQ - MAJOR REPAIR, DURING C-14 CHECK CORROSION WAS FOUND ON BOTH SIDES OF FRAME AT BS 1064 AROUND S87 ACCESSORY LIGHT SWITCH. MAINTENANCE REMOVED CORROSION ON FRAME AT BS 1064, STR 29 LT; FABRICATED 2 EACH REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG. 201, PG. 202-206. 2L72 4F RTA16WE 20040517000842004051700084NM 2004 5 17 AWXA200400498 120040406A53206517688167 ANGLE BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 MCN - MAJOR REPAIR, DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR SILL IB STIFFENER ANGLES AT SCREW HOLES BS 328, LBL 60. MAINTENANCE REMOVED 2 EACH CORRODED STIFFENER ANGLES AT BS 328, LBL 60; FABRICATED 2 EACH NEW REPLACEMENT ANGLES IAW DWG 65-17688; INSTALLED REPAIR PARTS IAW SRM 51-40-02, FIG. 12. 2L72 4F RTA16WE 20040517000872004051700087NM 2004 5 17 250TR0031 120040419A3350900835A BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 FORWARD CABIN CENTER AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED OK. 2L72 4F RTA16WE 20040517000882004051700088SW 2004 5 17 040401 120040419A32602782186017 INDICATOR SWRNGNSA227 SA227AC 8780603SW MLG FAILED A PNSAL ABORTED APPROACH P NO WARNING INDICATION LDLANDING 1 AL0341NE 741 AIRCRAFT WAS ON APPROACH, WHEN THE PILOT SELECTED GEAR DOWN THERE WAS NO GEAR INDICATOR LIGHTS, CYCLED GEAR STILL NO INDICATION LIGHTS. THE FLIGHT DIVERTED DUE TO BETTER WEATHER CONDITIONS, A FLYBY THE TOWER WAS MADE, THE GEAR APPEARED TO BE DOWN AND AN UNEVENTFUL LANDING WAS MADE. MAINT DISCOVERED THAT THE LANDING GEAR INDICATOR HAD FAILED GIVING A NO GEAR INDICATION TO THE PILOTS. 2L72 4T RTA8SW 20040517000912004051700091SO 2004 5 17 RAIA00404007 120040416A324221624 BRAKE EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03816HK132 145055 LT OB BRAKE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY. 2L72 4T RTT00011AT 20040517000922004051700092SO 2004 5 17 RAIA00404008 120040418A2611 ODOR EMB 145 EMB145 3260210SO CABIN DETECTED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03804HK 145082 LAV SMOKE MESSAGE. MAINTENANCE CHECKED LAV IN CABIN FOR EVIDENCE OR ODOR, RAN LT AND RT PACKS IN AUTO AND MANUAL, UNABLE TO DUPLICATE. 2L72 4F RTT00011AT 20040517000942004051700094WP 2004 5 17 MWEA040068 120040511A53159910078169 FLOORBEAM DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 STATION 180 FLOORBEAM IS DENTED APPROXIMATELY 4 INCHES RT OF THE AIRCRAFT CENTERLINE. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F A6WE 20040517000962004051700096EU 2004 5 17 USAA040114 120040401A5321D5367016100000 ANGLE AIRBUSA319 A319112 3930323EU FLOOR DECK CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW1630716307 0929 MAIN DECK SEAL ANGLES AT PNL 262GF AND 262EG CRACKED AT WELDS. REMOVED AND REPLACED SEAL ANGLES PER SRM 51-72-11 AND 51-42-11. (M) 2L72 4F RTA28NM 20040517000972004051700097NM 2004 5 17 2004UALA00277 120040325A3097MS27212215 TERMINAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE WINDOW HEAT BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29506UA 24627 NO POWER AT PHASE A OF CB C391 WINDOW HEATER 1L AND CB C336 RECIRC FAN L. DURING TROUBLESHOOTING OF WINDOW HEAT AND RECIRCULATING FAN PROBLEMS, WIRES WERE FOUND WITH OVERHEAT DAMAGE ON TB5031 AT THE P-31 LT GEN. PANEL. THE TERMINAL STRIP TB5031 (P/N MS27212-2-15), WAS FOUND OVERHEATED, POSSIBLY CAUSED BY A BAD CONTACT ON THE WIRE TERMINAL (BACT12AC15). THE OVERHEAT PROPAGATED THE DAMAGE TO WIRES W1130-0028-08 AND W4508-0001-08 (BMS13-51) AND CAUSED THE STUD TO GET LOOSE FROM THE TERMINAL STRIP. NO COMPONENT INVOLVED, WIRES W1130-0028-08 , W4508-0001-08 AND THE TERMINAL STRIP MS27212-2-15 WERE REPLACED. 2L72 4F4 FRTA2NM E17NE 20040517000992004051700099 2004 5 17 GLBA20030552 420040203A3421 EADI BEECH 1900 1900D 1154162CE COCKPIT FROZEN A GLBAO OTHER S AFFECT SYSTEMS CRCRUISE 1 NM03219GL UE219 NR 1 EADI FROZE 10 DEG BANK, INSP EADI & ENVIROMENTAL SYS OPS CK GOOD 2L72 4T RTA24CE 20040517001002004051700100CE 2004 5 17 RK256001 120040131A7110 COWLING BEECH MU300 400A 1155402CE RIGHT MISSING E ERYAO OTHER C F.O.D. CLCLIMB 1 CE0726PA 1741 RK256 AFTER TAKEOFF, DEPARTURE INSTRUCTIONS WERE TO CLIMB TO 2000 FEET AND TURN LEFT TO HEADING 120. A LEFT TURN WAS INITIATED A 1000 FEET AND AT APPROXIMATELY 1300 FEET AND HEADING 180 IN LIGHT TURBULENCE, A BUMP WAS FELT BY BOTH PIC AND SIC. PIC VERIFIED FLIGHT CONTINUITY AND NORMAL ENGINE INDICATIONS...ALL NORMAL. AFTER LANDING AT DESTINATION AIRPORT (PBI), CREW FOUND DURING POSTFLIGHT THAT RT ENGINE LOWER COWLING WAS MISSING AND EVIDENCE OF BIRD STRIKE ON RT ENGINE UPPER COWLING. 2H72 4F RTA16SW 20040517001042004051700104SO 2004 5 17 GLBA20030554 120040206A5297 WIRE EMB 120 EMB120ER 3260203SO DOOR ANNUNCIATORDAMAGED A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03293UX 120293 FWD DOOR ANNUNCIATOR ILLUMINATED AT 29000 FT, REPAIRED SOLDER JOINTS ON DOOR OPEN SWITCH OPS CK GOOD 2L72 4T RTA31SO 20040517001062004051700106WP 2004 5 17 NACA20040011 120040212A7160247779 INTAKE PIPE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE RUPTURED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS APAPPROACH 1 AL032907F1546 1546 533265 33553 NR 4 ENGINE BACKFIRING ON FINAL AND UPON LANDING. ENGINE SHUT DOWN AFTER LANDING. REPLACED NR 4 ENGINE, NR 15 & 16 Y-PIPE DUE TO BEING RUPTURED. CHECKED GOOD ON RUN. 2L74 4R4 R A781 5E8 20040517001082004051700108CE 2004 5 17 RB570001 120040211A5270 POSITION SWITCH RAYTHN390 390 7150030CE PAX DOOR OUT OF ADJUST E ERYAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07488PC349 RB57 JUST NORTH OF PXR CLIMBING THROUGH FL310, GOT A "CABIN DOOR UNLOCKED" CAUTION LIGHT. RAN THE CHECKLIST, COMMUNICATED WITH ATC AND ASKED FOR LOWER (12000 FT). BRIEFED THE PAX, AND PROCEEDED ON TO VNY. ON ENGINE SHUTDOWN, VISUALLY INSPECTED THE CABIN DOOR AND DETERMINED THAT IT WAS LOCKED AND LATCHED FIRMLY 17 2 3F RTA00010WI 20040517001092004051700109WP 2004 5 17 020104 120040217A53103754023IN FITTING DOUG DC8 DC863F 302198FWP CARGO DOOR CORRODED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 315 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A PIT) DOOR STRUCTURE FITTING CORRODED-TASK CARD #0323. 2L74 4F 4A25 20040517001102004051700110WP 2004 5 17 0324 120040217A531037540231N FITTING DOUG DC8 DC863F 302198FWP CARGO DOOR CORRODED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 EXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 324 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A-PIT) DOOR STRUCTURE FITTING CORRODED. 2L74 4F 4A25 20040517001122004051700112WP 2004 5 17 0355 120040217A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK 5600-0551 FOUND AFT ACCESSORY COMPARTMENT FS 1640 BETWEEN LONGERON 32R AND 33R. FASTENERS PULLING THROUGH FUSELAGE SKIN AND IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20040517001152004051700115NM 2004 5 17 04005 120040216A2612 WARNING LIGHT BOEING747 747209B 138489BNM CARGO FIRE WILL NOT TEST A KCSAA UNSCHED LANDING L NO TEST CRCRUISE 1 GL23714CK 22446 AFT BULK FIRE "B" LIGHT ON, "A" LIGHT WOULD NOT TEST. 2L74 4F RTA20WE 20040517001162004051700116NM 2004 5 17 04006 120040219A2612 WARNING LIGHT BOEING747 747132 1384882NM APU FIRE WARNINGILLUMINATED C KCSAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL23709CK 20247 ON TAKE-OFF ROLL, APU FIRE WARNING CAME ON--ABORTED TAKE-OFF. 2L74 4F A20WE 20040517001202004051700120WP 2004 5 17 02240401WP 120040208A3260801801 PROXIMITY SENSOR DOUG DC9 DC9 3022002WP MLG MALFUNCTIONED A A4JAO OTHER N FALSE WARNING LDLANDING 1 SO35933J 48159 ON LANDING INTO ABE DURING GEAR EXTENSION LEFT MAIN GEAR UNSAFE LIGHT CAME ON WITH NO GREEN DOWN AND LOCK LIGHT ON. WENT THROUGH CHECK LIST AND LANDED. REPLACED LEFT GEAR DOWN LOCK PROXIMITY SENSOR IAW DC9 MM 32-60-01. OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 20040517001222004051700122EU 2004 5 17 U30A200400003 120040221A339758799 LEAD AIRBUS320 A320214 3930316EU EMERGENCY LIGHT DAMAGED A U30AK NONE L NO TEST ININSP/MAINT 1 EA17GBXKA 0714 PRIOR TO DEPARTURE OF FLT 712 IN DTW, MAINTENANCE NOTED THE EMERGENCY FLOOR LIGHTING INOP AT SEATS 16 AND 21. DEFERRED PER MEL 33-50-03-3. NOTE: ON FEB 23, 2004 MAINTENANCE TROUBLESHOT THE PROBLEM TO A DEFECTIVE LEAD ASSY-CABLE (7260VC6) DUE TO FAULTY PINS IN CONNECTOR. LEAD ASSY-CABLE WAS REPLACED I/A/W AMM 31-51-12, OPS CK OK. 2L72 4F RTA28NM 20040517001242004051700124SO 2004 5 17 GLBA20030575 120040227A571212034222010 LINK EMB 120 EMB120ER 3260203SO WING CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03297UX 120297 RIB LINK CRACKED ON RT NAC FLAP, R&R RT RIB LINK ON NACCLLE FLAP PN 120-34222-010 2L72 4T RTA31SO 20040517001312004051700131CE 2004 5 17 60267022704 120040226A7930 PUMP LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE OIL SYSTEM SEIZED E J7SAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0550558 267 PCECA0386 DURING CLIMBOUT FROM KBED, FLIGHT CREW OBSERVED A LEFT ENGINE LOW OIL PRESSURE WARING LIGHT AND A SIMULTANEOUS DECREASE IN INDICATED OIL PRESSURE. THE ENGINE WAS IMMEDIATELY SHUTDOWN AND THE AIRCRAFT DIVERTED TO KBDL. THE LT ENGINE HAS BEEN REMOVED BY MAINTENANCE AND A LOANER ENGINE INSTALLED. PRATT & WHITNEY SUSPECTS A SEIZED OIL PUMP. A TEARDOWN REPORT HAS BEEN REQUESTED. 2L72 4F4 FRTA10CE E35NE 20040517001342004051700134GL 2004 5 17 690A0220004MT 320040220A6110HCB3TN5FL PROPELLER GULSTM690TP 690A 0141722SW HARTZLHCB3T HCB3TN5 GL NR 2 INCORRECT B JBZRK NONE O OTHER ININSP/MAINT 1 WP27677WA 143 11243 THE NR 1 PROPELLER WAS REMOVED TO FACILITATE ENGINE MAINTENANCE. WHILE THE PROP WAS OFF IT WAS SENT TO A REPAIR STATION TO HAVE THE BLADES RETURNED TO FEATHER. THE PROP WAS THEN INSPECTED AND TESTED. PROPELLER INSPECTION FOUND THAT THE BLADE ANGEL SETTING FROM BLADE TO BLADE WAS OUT OF TOLERANCE, THE BLADE TWIST WAS OUT OF TOLERANCE, THE PROP WAS OUT OF BALANCE, AND THE CYLINDER WAS WORN. THE NR 2 PROP ( S/N BVA7651), WHICH HAD BEEN OVERHAULED BY THE SAME FACILITY AT THE SAME TIME, WAS THEN REMOVED FOR EVALUATION. BLADE ANGLE AND TWIST WERE OUT OF TOLERANCE, AND ONE CLAMP WAS CORRODED INTERNALLY AND COULD NOT BE REWORKED. BOTH PROPS WERE OVERHAULED ON 1/3/2001 AND HAD 143.1 HOURS SINCE OVERHAUL. 1H72 3T 2A4 6 CP15EA 20040518000032004051800003NM 2004 5 18 USAABB04039 120040425A3397 SOCKET BOEING767 767201 1385125NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 PHL - THE FLOOR EMERGENCY LIGHTING FROM SEAT ROWS 9 AB THROUGH 13AB, LEFT SIDE, WAS FOUND INOPERATIVE. MAINTENANCE LOCATED AND REPAIRED A BAD BULB SOCKET. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA1NM 20040518000042004051800004NM 2004 5 18 USAA040119 120040409A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US52179 23312 CLT - FOUND SKIN WITH TWO CRACKS .5 INCH AND 2 INCHES LONG, STATION 727E +4 AT STRINGER 22R, RIGHT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040518000052004051800005NM 2004 5 18 USAA040105 120040409A5512 SKIN BOEING757 7572B7 1384964NM HORIZONTAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU36733 27199 PIT - FOUND HORIZONTAL STABILIZER SKIN WITH 8 INCH REPAIR, JUST AFT OF FSS 145 RT HORIZONTAL STABILIZER LOWER SKIN. COMPOSITE LAY UP REPAIR PER SRM 51-70-10. (M) 2L72 4F RTA2NM 20040518000062004051800006NM 2004 5 18 USAA040104 120040409A5753 SKIN BOEING757 7572B7 1384964NM TE FLAP DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU36733 27199 PIT - FOUND AFT FLAP WITH 6 INCH REPAIR, LOWER SKIN OUTBOARD AFT FLAP AT WS 537 LT WING. COMPOSITE LAY UP REPAIR PER SRM 51-70-17. (M) 2L72 4F RTA2NM 20040518000072004051800007NM 2004 5 18 USAA040122 120040422A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19588US47523 23933 CLT - FOUND SKIN CRACKED 3.5 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT, STATION 344.47, WL 207.5. INSTALLED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 202. (M) 2L72 4F RTA16WE 20040518000102004051800010NM 2004 5 18 USAA040117 120040409A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US52179 23312 FOUND SKIN CRACKED 2.5 INCHES, STATION 727E AT STRINGER 18R, RT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040518000112004051800011EU 2004 5 18 USAABA04010 120040425A335032146210 EPSU AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 0388 PHL - EPSU 16WL FAILED SYSTEM TEST. MAINTENANCE REMOVED AND REPLACED THE EPSU. SYSTEM TEST NORMAL. (M) 2L72 4F RTA46NM 20040518000122004051800012 2004 5 18 REXA04008 420040407A2562 G SWITCH CNDAIRCL600 CL6002B19 1900309EA ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258790A 01467 7790 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. THIS FAILURE IS THE 9TH OCCURRENCE OF THIS MODEL ELT FAILING THE G-SWITCH ON ITS FIRST 12 MONTH INSPECTION. PINNACLE AIRLINES REACHED THE 12 MONTH INVERVAL ON ONLY 16 AIRCRAFT EQUIPPED WITH THIS MODEL ELT PRIOR TO THIS FAILURE. THE MANUFACTURER HAS CONFIRMED THE G-SWITCH FAILURE ON THE OTHER 8 UNITS. (M) 2L72 4F RTA21EA 20040518000132004051800013EU 2004 5 18 USAABA04007 120040421A2420590897417 GCU AIRBUS330 A330323 3930335EU RT GENERATOR FAULTY A USAAA UNSCHED LANDING GB MULTIPLE FAILURE SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19677UW18492 0380 PHL - FLT 196 - EN ROUTE PHKL-MAN, THE RIGHT IDG BECAME INOPERATIVE. THE PAU WAS STARTED, HOWEVER IT WAS REPORTED THAT THE ELECTRICAL SYSTEM WAS UNSTABLE. THE FCU HEADING FROZE AND NEW HEADINGS WERE NOT ACCEPTED BY THE AUTOPILOTS NOR THE FLIGHT DIRECTOR. IN ADDITION, THE CREW REPORTED AN ELECTRICAL ODOR IN THE MID GALLEY. ALL GALLEY EQUIPMENT WAS SECURED AND THE ODOR ABATED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FCU FOR THE NAVIGATION PROBLEM. NO CAUSE WAS FOUND FOR THE MID GALLEY ODOR. THE MAIN CAUSE FOR THIS EVENT WAS THE ELECTRICAL PROBLEM. THE RIGHT GCU AND RIGHT ENGINE WC-1 WIRING HARNESS WRE REPLACED. (M) 2L72 4F RTA46NM 20040518000152004051800015NM 2004 5 18 USAA040109 120040402A5330 SKIN BOEING757 757225 1384959NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU61617 22196 FOUND SKIN WITH SCAB PATCH 6.5 INCHES BY 7.25 INCHES, STATION 1420, S29L. DOUBLER REPAIR PER SRM 53-00-01, FIG 201. (M) 2L72 4F RTA2NM 20040518000172004051800017NM 2004 5 18 USAA040103 120040409A5753 SKIN BOEING757 7572B7 1384964NM TE FLAP DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU36733 27199 PIT - FOUND RIGHT OUTBOARD AFT FLAP HAS 6 INCH REPAIR, LOWER SKIN IN OUTBOARD AFT FLAP. COMPOSITE LAY UP REPAIR PER SRM 51-70-17. (M) 2L72 4F RTA2NM 20040518000192004051800019NM 2004 5 18 USAA040102 120040409A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU36733 27199 PIT - FOUND FLOORBEAM CORRODED 2 INCH AREA, .025 INCH DEEP, FLOORBEAM UPPER SURFACE BS 700 LBL 55. BLENDED AREA TO REMOVED CORROSION, INSTALLED REPAIR ANGLES PER EA 78224. (M) 2L72 4F RTA2NM 20040518000212004051800021WP 2004 5 18 GTIA040337 120040423A5340 SUPPORT DOUG DC9 DC982 3022082WP GIRT BAR BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 DTW - FOUND AFT GALLEY SERVICE DOOR, ONE GIRT BAR SUPPORT TAB BROKEN. INSTALLED NEW GIRT BAR SUPPORT TAB ON AFT GALLEY SERVICE DOOR. (M) 2L72 4F A6WE 20040518000232004051800023WP 2004 5 18 GTIA040299 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 218-237 LT OUTBOARD COVER TORN, EXPOSED CORE. COVER DELAMINATED AND BLUE WATER STAINS IN CORE. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040518000242004051800024EA 2004 5 18 A6WA200440051 120040422A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31433AW 7289 RIGHT FS 718 BETWEEN STRINGERS 11 AND 12 HAS CRACK ON FRAME FLANGE, WORK ORDER 63453 MAINTENANCE WORKCARD 24. TRIMMED OUT SECTION OF FRAME FLANGE, PERFORMED LPI OF CUT LINES. FABRICATED FILLER FROM 2024-T3 .040 INCH, WVAC PO NR 33626/1. FABRICATED REPAIR ANGLE FROM P/N 600-36030-24 AND INSTALLED REPAIR PARTS IAW 601R-61-143 REV A. (M) 2L72 4F RTA21EA 20040518000252004051800025WP 2004 5 18 GTIA040298 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 LEFT INBOARD NO EDGE FILLER AND COVERING SPLINTERED. FABRICTED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040518000272004051800027WP 2004 5 18 GTIA040335 120040423A7120K22199SA31 ISOLATOR DOUG DC9 DC982 3022082WP NR 1 ENGINE OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 NR 1 ENGINE FORWARD LOWER VIBRATION ISOLATION MOUNT OUT OF LIMITS. REMOVED AND REPLACED FORWARD LOWER VIBRATION ISOLATOR. (M) 2L72 4F A6WE 20040518000282004051800028WP 2004 5 18 GTIA040333 120040415A1420 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FOUND TAIL COMPARTMENT EMERGENCY EXIT IDENTIFIER IS NOT LIGHT ON TEST. SECURED CONNECTOR, OPS CHECK. (M) 2L72 4F A6WE 20040518000292004051800029EA 2004 5 18 A6WA200440053 120040426A5320 CHANNEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31433AW 7289 MWC 69 - Z-MEMBER IS CHAFED IN AFT EQUIPMENT BAY AT FS 625, BL0, WL 136, ON AFT SIDE OF AFT PRESSURE BULKHEAD. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION. FABRICATED AND INSTALLED A REPAIR ANGLE IAW BRAS EO 601R-53-4884A. (M) 2L72 4F RTA21EA 20040518000302004051800030WP 2004 5 18 GTIA040294 120040325A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN FLOOR SUPPORT CORRODED STATION 1155 AT L2 DOOR OPENING. REMOVED DAMAGED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F A6WE 20040518000322004051800032 2004 5 18 GTIA040338 420040426A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FLL - FLT 433 - FOUND SLIDE PACK FELL OUT OF R1 DOOR INTO CABIN. SECURED SLIDE AT R1 DOOR. (M) 2L72 4F A6WE 20040518000342004051800034 2004 5 18 GTIA040330 420040417A2565 RETAINER DOUG DC9 DC982 3022082WP SLIDE COVER BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FLL - FOUND LEFT AFT SLIDE PACK COVER GIRT BAR RETAINING CLIP BROKEN. REMOVED AND REPLACED LEFT AFT SLIDEPACK COVER GIRT BAR RETAINING CLIP. OPS CHECK GOOOD. (M) 2L72 4F A6WE 20040518000412004051800041CE 2004 5 18 2004F00106 120040220A2730115610010325 TORQUE TUBE BEECH 100 100BEECH 1152916CE RT ELEVATOR CRACKED E HSRAK NONE O OTHER ININSP/MAINT 1 NM05102LF5468 549 B65 DURING PRE-FLIGHT FOUND EXCESSIVE PLAY BETWEEN ELEVATOR TRAILING EDGES. AIRCRAFT DID NO DISPATCH. REMOVED ELEVATOR, DISASSEMBLED LEFT TORQUE TUBE. FOUND TORQUE TUBE CRACKED ALMOST 3/4 OF THE WAY AROUND THE CIRCUMFRANCE OF THE TORQUE TUBE SURFACE. INSTALLED NEW TORQUE TUBE ASSEMBLY. TORQUE TUBE TOTAL TIME 5468 HOURS. INSPECTION INTERVAL IS 1000 HOURS. NEXT INPSECTION DUE IN 451 HOURS PER SERVICE BULLETIN 21-45. 1L72 3T A14CE 20040518000432004051800043WP 2004 5 18 1965 120040228A278037701431 CRANK ASSY DOUG DC8 DC863F 302198FWP LE FLAPS FRACTURED I U2RBO OTHER J WARNING INDICATION DEDESCENT 1 GL23921R 6747317652 46145 FLIGHT CREW REPORTED WING SLOT LIGHT ON WITH FLAPS EXTENDED. FOUND RIGHT AHND EXTENDED LEADING OOUTBOARD SLOT DOOR INOPERATIVE DUE TO FRACTURED AND BROKEN CRANK ASSEMBLY AT STA.XS476 2L74 4F 4A25 20040518000442004051800044 2004 5 18 GLBA20030577 420040229A2300 RADIO BEECH 1900 1900D 1154162CE COMM SYSTEM MALFUNCTIONED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03247GL UE247 STATIC IN BOTH COMM'S BOTH NAVS FAILED PRECIP, R & R STATIC WICKS 2L72 4T RTA24CE 20040518000462004051800046NM 2004 5 18 XNOA1178 120040225A2910 LINE BOEING727 727173C 1384059NM HYD SYSTEM LEAKING A XN0AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23704A 19504 LOSS "A" SYSTEM PRESSURE & QUANTITY. INSTALLED TEMP FLEX LINE IAW B727 MM 20-10-12 & ENA GMM CHAPTER 5, PRESSURE LEAK CK GOOD. TRANSFERRED TO CARRY-OVER ITEM 1388 PLACARD INSTALLED.(STATUS:ORIG/OPEN) R & R TEMP FLEX HOSE FROM NOSE L/G ACTUATOR IAW B727 MM 20-10-12. PRESSURE LEAK CK GOOD. PLACARD REMOVED. THIS ACTION CLEARS C/O 1388. (STATUS:SUPP/CLOSED) 2L73 4F A3WE 20040518000492004051800049NE 2004 5 18 00131 220040210A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05888TW 292 249SC104A PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL 370. WILL UPDATE THIS SDR AFTER MAINTENANCE. LT ENGINE REMOVED FOR HSI INSPECTION NO ABNORMAL WEAR REPORTED, PERFORMANCE RUN COMPLETED, ENGINE AND AIRCRAFT RETURN TO SERVICE. 2L72 4J4 J A10CE 1E16 20040518000542004051800054WP 2004 5 18 0024 220040220A732030707222 SENSOR LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP EEC SHORTED E CIEAO OTHER J WARNING INDICATION CRCRUISE 1 NM03244LJ3531 190 244 P74689 THE LEFT ENGINE COMPUTER LIGHT ILLUMINATED IN CRUISE, DEEC (DIGITAL ELECTRONIC ENGINE CONTROL) DROPPED OFF-LINE. DEEC SUCCESSFULLY RESET ONCE DURING DESCENT (N2 AT 55 PERCENT). THE DEEC DROPPED OFF-LINE AGAIN ON APPROCH WHEN ENGINE WAS POWERED ABOVE 75 PERCENT N2. AIRCRAFT LANDED WITHOUT INCIDENT. FAULT CODE USING THE FLASHING LIGHT PROCEDURE, INDICATED THERE WAS A PROBLEM WITH THE N2 MONOPOLE. MAINTENANCE DOWNLOADED THE INFORMATION IN THE DEEC AND THE FAULT CODE WAS VERIFIED AS A N2 MONOPOLE SHORTED TO GROUND. THE MONOPOLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE TOTAL TIME ON THE MONOPOLE USING THE ENGIEN LOGS, INDICATES IT IS THE SAME AS THE ENGINE TOTAL TIME. 2L72 4F4 F A10CE E6WE 20040518000562004051800056WP 2004 5 18 NAFA20040002 120040304A3260BZ3YT DOWNLOCK SWITCH DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE MLG DIRTY I N32BA UNSCHED LANDING N FALSE WARNING LDLANDING 1 AL017780B 45372 UNSAFE NOSE WHEEL INDICATION. REMOVED NOSE GEAR DOWN & LOCK SWITCH ASSEMBLY, CLEANED CONTACTS, REASSEMBLED, RIGGED AND SWUNG NOSE GEAR. OP CHECK GOOD. (CLEANED INSPECTION WINDOW). 2L74 4R4 R 6A3 5E8 20040518000592004051800059NE 2004 5 18 XNOA1179 220040305A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 2 MALFUNCTIONED A XN0AC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL2376752 21248 666134 NR 2 ENGINE WILL NOT ACHIEVE TAKE-OFF POWER. PERFORMED NR 2 ENGINE RUN. NR 2 ENGINE MAKES ITS TARGET POWER IAW P&W JT8D MM 72-00-00. NO DEFECTS NOTED. (STATUS: ORIG/CLOSED) 2L73 4F4 F A3WE E2EA 20040518000612004051800061SO 2004 5 18 DEBAGA11591 120040305A2430A700AH RELAY GULSTMG1159 G1159 3953505SO APU FAILED E DEBAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 CE03900BF 1 206 WITH AIRCRAFT ON GROUND WITH APU RUNNING, THE ESSENTIAL AND MAIN BUSS VOLTAGES DROPPED TO 19VDC. TROUBLESHOT SYSTEM AND FOUND THAT THE REVERSE CURRENT RELAY A700AH SN L13232 DID NOT PROPERLY SERVE AS A REVERSE CURRENT RELAY AND IT FED POWER TO THE DC GENERATOR RELAY. THIS RELAY HAD 1 HOUR AND 3 CYCLES SINCE INSTALLATION AS AN OVERHAULED PART. 2L72 4F RTA12EA 20040518000692004051800069EU 2004 5 18 WRNA200400001 120040311A2780CHA1063007B BRAKE ASSY AIRBUS300 A300B4203 3930306EU LE SLATS FAILED A WRNAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 SO05368DH 207 SLATS WOULD NOT RETRACT AFTER TAKE-OFF. DUMP FUEL AND RETURNED TO AIRPORT. LANDING NORMAL. TROUBLESHOT SLAT SYSTEM. OPS CHECK OK. INSPECTED SYSTEM FOUND NR 2 & 3 SCREWJACK RT WING TRIPPED. RESET TRIP INDICATORS. CHECK BOTH LT AND RT WING FRICTION BRAKES FOR SLAT SYSTEM. FOUND RT WING BRAKE FAIL TORQUE CHECK. R & R RT WING FRICTION BRAKE IAW MM 27-81-47 OPS CHECK SLAT SYSTEM OK. LUBED SLAT SCREWJACK AND TRACKS FOR PRECAUTION IAW 12-13-27. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA35EU 20040518000702004051800070EU 2004 5 18 WRNA200400002 120040311A2780CHA1063007B BRAKE ASSY AIRBUS300 A300B4203 3930306EU ZONE 600 FAILED A WRNAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 SO05368DH 207 SLATS WOULD NOT RETRACT AFTER TAKE-OFF. DUMP FUEL AND RETURNED TO AIRPORT. LANDING NORMAL. TROUBLESHOT SLAT SYSTEM. OPS CHECK OK. INSPECTED SYSTEM FOUND NR 2 & 3 SCREWJACK RT WING TRIPPED. RESET TRIP INDICATORS. CHECK BOTH LT AND RT WING FRICTION BRAKES FOR SLAT SYSTEM. FOUND RT WING BRAKE FAIL TORQUE CHECK. R & R RT WING FRICTION BRAKE IAW MM 27-81-47 OPS CHECK SLAT SYSTEM OK. LUBED SLAT SCREWJACK AND TRACKS FOR PRECAUTION IAW 12-13-27. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA35EU 20040518000722004051800072WP 2004 5 18 258160002 220040229A7261 CARBON SEAL BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP RT ENGINE DAMAGED E ERYAO OTHER J WARNING INDICATION DEDESCENT 1 CE07803JL 1147 NA0436 P91423 ON DESCENT TO KBCT, ENGINE POWER WAS REDUCED TO IDLE. OIL PRESSURE ON NR 2 ENGINE DROPPED TO RED LINE. POWER INCREASED ON NR 2 ENGINE AND OIL PRESSURE INCREASED. FOUND NR 1 CARBON SEAL RUNNER RETAINER DAMAGED. REPLACED RETAINER AND CARBON SEAL WITH NEW. INSTALLED NEW OIL PUMP. PERFORMED GROUND RUN, OIL PRESSURE ADJUSTMENT, VIBE SURVEY, AND OIL SYSTEM FLUSH. 2L72 4F4 FRTA3EU E6WE 20040518000742004051800074SO 2004 5 18 RAIA00403005 120040302A21508152403 COMPRESSOR EMB 145 EMB145LR 3260212SO LT ACM MALFUNCTIONED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03815HK10141 145048 SMOKE IN COCKPIT. APPEARS TO BE CONNECTED WITH NR 1 PACK. MAINTENANCE TROUBLE SHOT AND DEFERRED LT PACK IAW MEL. SUBSEQUENTLY MAINTENANCE CLEARED DMI BY REMOVING AND REPLACING LT AIR CYCLE MACHINE. 2L72 4T RTT00011AT 20040518000762004051800076SO 2004 5 18 RAIA00403007 120040307A324239807 VALVE EMB 145 EMB145LR 3260212SO BRAKE ASSY INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK7954 145256 EICAS MESSAGE BRAKE OTBD INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE O/B BRAKE CONTROL VALVE. 2L72 4T RTT00011AT 20040518000792004051800079NM 2004 5 18 EIA2004008 120040122A3397 CONNECTOR BOEING747 747273C 1384896NM EMERGENCY LIGHT LOOSE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471EV 20651 EXIT LIGHTS AT L5 AND R5 DOORS INOP DURING "A" CHECK. RESEATED CONNECTOR ON POWER SUPPLY OPS CHECK GOOD. 2L74 4F RTA20WE 20040518000812004051800081NM 2004 5 18 EIA2004007 120040120A3310 ODOR BOEING747 747132 1384882NM MAP LIGHT DETECTED A EIAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09481EV 19896 CAPTAINS MAP LIGHT EMITS ELECTRIAL ODOR WHEN TURNED ON. DEACTIVATED CIRCUIT AND ENTERED DMI 279 PER MEL 33-1. 2L74 4F A20WE 20040518000832004051800083CE 2004 5 18 59623 120040311A5210 CABLE BEECH 1900 1900D 1154162CE PAX DOOR HANDLE LOOSE A AMWAO OTHER O OTHER TOTAKEOFF 1 CE0726YV UE26 WHEN CREW ARRIVED IN SHV. FOR THE DEPARTURE THE PAX DOOR WOULD NOT OPEN WITH THE OUTSIDE HANDLE. TURNED FWD CABLE UPPER 1 1/2 TURNS. 2L72 4T RTA24CE 20040518000872004051800087NE 2004 5 18 PCAA0403181 220040316A7260311859701 GARLOCK SEAL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE MISALIGNED A PCAAB EMER. DESCENT O OTHER DEDESCENT 1 EA13844EX 339 MADE AN EMERGENCY LANDING DUE TO THE NR 2 OIL PRESSURE FLUXUATING ON DESCENT. NR 2 ENGINE WAS FEATHERED AND CABIN WAS PREPPED FOR EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 DC GENERATOR GARLOCK SEAL IMPROPERLY SEATED. GARLOCK WAS REMOVED AND REPLACED AND THE AIRCRAFT OPERATIONAL CHECK AND LEAK CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040518000892004051800089WP 2004 5 18 2004000003 120040316A21503961969 VALVE DOUG DC10 DC1030 3023501WP FLOW CONTROL MALFUNCTIONED A CNMAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07540AX 46595 AFTER T/O AND FIRST PWR REDUCTION NR 2 AC PACK OFF LIGHT ON. NR 2 AC PACK WOULD NOT FUNCTION IN MANUAL OE AUTO. INFLIGHT WITH NR 3 AC PACK IN AUTO, TEMP DRIVES TO FULL HOT WORKS OK IN MANUAL. REPLACED NR 2 FLOW CONTROL VALVE AND REPLACED NR 3 PACK TEMP INDICATOR. 2L73 4F A22WE 20040518000902004051800090NM 2004 5 18 F3LA200400033 120040315A2750693534759 SPINDLE BOEING737 737300 1384610NM FLAP CARRIAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 2361 23177 INSPECTION REPORTED RT OTBD FLAP CARRIAGE SPINDLE SHOWED CRACK INDICATION ON ULTRASOUND INSPECTION (REF. AD 2003-24-08, FRONTIER WORK CARD 9-5702). REMOVED SPINDLE AND FOUND NO CRACK, BUT FOUND HEAVY CORROSION AT SADDLE. REPLACED CARRIAGE SPINDLE. 2L72 4F RTA16WE 20040518000912004051800091CE 2004 5 18 GLBA20030589 120040313A21201143800595 SHUTOFF VALVE BEECH 1900 1900D 1154162CE RT ENVIRO FAILED A GLBAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM03201GL4463 UE201 RT ENVIRO FAIL ANN ILLUMINATED, R&R RT PRSOV PN 114-380059-5 MM OPS AND LEAK CK GOOD 2L72 4T RTA24CE 20040513000722004051300072NM 2004 5 13 04FDEA01194 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.514, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.513 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000752004051300075NM 2004 5 13 04FDEA01197 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000772004051300077NM 2004 5 13 04FDEA01199 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040513000942004051300094NM 2004 5 13 04FDEA01206 120040510A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE FOUND CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.222, AND REPAIRED AS PER EA 1-5740-75956. LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040513000962004051300096WP 2004 5 13 04FDEA01131 120040501A5720 STRIP DOUG MD10 MD1010F 3022112WP RT WING LE TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25372FE 46610 RIGHT WING DLE CHAFE STRIP TORN WITH MISSING SECTION. REMOVED, FABRICATED CHAFE STRIP AND INSTALLED IAW DPS 4.710 & SRM 51-31-01 AT MAE. 2L73 4F RTA22WE 20040513000982004051300098NM 2004 5 13 04FDEA01133 120040503A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 HORIZONTAL STABILIZER, RIGHT UPPER CENTER PLANK NR 15R BARREL NUT BORE CORROSION BLEND-OUT EXCEEDED EO 1-5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-76025. HORIZONTAL STABILIZER BARREL NUT BORE REWORK/REPAIR A.D. 2003-22-08. 2L73 4F RTA22WE 20040513001042004051300104NM 2004 5 13 04FDEA01139 120040503A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILING EDGE DEVICES RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK. 2L73 4F RTA22WE 20040513001062004051300106NM 2004 5 13 04FDEA001088 120040424A5320ADA8424517 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE FOUND CORROSION. FWD CARGO COMPARTMENT STA 1119 TO 6-10 LONGERON L46 SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040513001092004051300109WP 2004 5 13 04FDEA001091 120040424A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 MAIN CABIN SEAT TRACK AT LBL 107, FS 1476-1479 CORROSION CENTER OF TRACK. REMOVE CORROSION IAW DC-10 SRM 51-21-01 VOL 2. FOUND TO BE OUT OF LIMITS, MATERIAL FOR NEW CHANNEL 7075 T651, .750 PLATE, PO 401641.2 AND FABRICATED CHANNEL IAW DC-10 SRM 53-70-00 VOL 1. INSTALLED REPAIR CHANNEL IAW DC-10 SRM 51-31-01 VOL 1. 2L73 4F A22WE 20040513001172004051300117NM 2004 5 13 04FDEA001020 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. 2L73 4F RTA22WE 20040513001252004051300125NM 2004 5 13 04FDEA001076 120040423A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. 2L73 4F RTA22WE 20040513001322004051300132NM 2004 5 13 04FDEA001080 120040424A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, BARREL NUT HOLE 2B MATING SURFACE CORRODED. 2L73 4F RTA22WE 20040514000252004051400025EA 2004 5 14 ASOA04281 120040405A5320601R9501511 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET. (M) 2L72 4F RTA21EA 20040514000342004051400034EU 2004 5 14 USAA040070 120040329A5320D53471124201 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 PIT - FOUND SHEAR PLATE WORN/CHAFED 1 INCH BY 1 INCH IN FOUR AREAS, FRAME 69-70 Y1292, Z-240. REPLACED SHEAR PLATE PER SRM 53-41-17 AND 51-42-11. LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040514000352004051400035EU 2004 5 14 USAA040069 120040328A5315D5347217320000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 FOUND FLOORBEAMBEAM WORN 1 INCH BY 1 INCH BY .070 INCH, FRAME 66 Y-254, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040514000382004051400038WP 2004 5 14 GTIA040304 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 RIGHT OUTBOARD NO EDGE FILLER, MISSING INSERT AND COVERING TORN. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040514000492004051400049 2004 5 14 USAASA04035 420040415A2565 LANYARD AIRBUSA319 A319112 3930323EU ESCAPE SLIDE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW 0972 BFM - THE SLIDE GIRT BAR LANYARD CABLE BALLS DISENGAGED UPON INSTALLATION OF ESCAPE SLIDE ONTO AIRCRAFT. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040514000542004051400054EU 2004 5 14 USAA040071 120040330A5320D53471124200 PLATE AIRBUSA319 A319112 3930323EU FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND PLATE CORRODED 2 INCHES BY 1 INCH BY .17 INCH DEEP, FS 69-70, -Y1292, -Z240. REMOVED AND REPLACED SHEAR PLATE PER SRM 53-41-17, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040514000802004051400080EU 2004 5 14 KBM2004F00027 120040307A7920J26109 HOSE SNIAS 350 AS350BA 8680817EU ENG OIL LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP191188P 2347 ENGINE OIL HOSE RETURN LINE. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000872004051400087 2004 5 14 KBM2004F00037 420040305A3452066106200 TRANSPONDER SNIAS 350 AS350BA 8680817EU COCKPIT UNSERVICEABLE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 UNABLE TO RECEIVE SIGNAL FROM TRANSPONDER. REMOVE AND REPLACED WITH SERVICEABLE TRANSPONDER. 1G71 3U NCH9EU 20040514001102004051400110NM 2004 5 14 QXEA200400320 120040510A5320 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - PANEL 522AT HAS TWO STRIPPED NUT PLATES. REPAIRED IAW DHC-8-400 SRM 51-42-05. AND SRM 51-23-00. 2H72 4T RTA13NM 20040514001192004051400119EU 2004 5 14 KBM2004F00042 120040304A6420350A33215001 BALL SNIAS 350 AS350B2 8680813EU T/R SPIDER EXCESS PLAY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 TAIL ROTOR PC SPIDER END BALL BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED. 1G71 3U H9EU 20040517000032004051700003EU 2004 5 17 USAA040081 120040326A5347D5311282600201 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW 0929 BFM - FOUND TRACK CORRODED 2.7 INCHES BY 1.1 INCH BY .053 INCH DEEP, FRAME 15, Y=503.2, Z=-240. REMOVED AND REPLACED TRACK PER SRM 53-11-14, FIG 106, 51-42-11, 51-74-00. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040517000062004051700006EU 2004 5 17 USAA040085 120040330A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND SILL CORRODED 2 INCHES BY 1.3 INCHES BY .070 INCH DEEP, FRAME 66, Y 1502, -Z240. REMOVED AND REPLACED SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA 260-53500. (M) 2L72 4F RTA28NM 20040517000212004051700021WP 2004 5 17 GTIA040293 120040315A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND AFT PIT STATION 1155-1124 VHF ANTENNA HAS TEMP REPAIR DOUBLER ON IT. REMOVED TEMP REPAIR DOUBLER. FABRICATED PERM REPAIR DOUBLER AND FINGER DOUBLER. INSTALLED DOUBLER AND FINGER DOUBLER. (M) 2L72 4F A6WE 20040517000222004051700022WP 2004 5 17 GTIA040283 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN STATION 200 LBL 9 - LBL 13 FLOOR SUPPORT CORRODED AND LBL 5 - RBL 5 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT AT STATION 200 LBL 9 - LBL 13. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20040517000232004051700023WP 2004 5 17 GTIA040284 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CABIN STATION 200-227 LBL 15 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F A6WE 20040517000292004051700029EU 2004 5 17 SIMA200410105 120040402A531172528814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 ABI - DURIG AN MBV INSPECTION A GALLEY AREA FLOOR FRAME 272 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE FRAME. CLEANED AND TREATED THE BARE METAL EDGE. FABRICATED FILLER, DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 53-70-30, 51-20-50, 51-40-21, 51-40-40, 51-40-60, 51-20-41 AND 52-10-43. (M) 2L72 4T RTA52EU 20040517000302004051700030EU 2004 5 17 SIMA200210106 120040331A5330AL2024T3 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 ABI - DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. ON PREVIOUS STATEMENT ID 69 DENT BETWEEN STATION 487 AND 512 AND BETWEEN SL 1601 AND 1602. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS006572, PARA 1, 3, 8. (M) 2L72 4T RTA52EU 20040517000562004051700056NM 2004 5 17 QXEA200400316 120040507A52108521003001 DOOR DHAV DHC8 DHC8202 2809007NM MAIN CABIN BINDING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09360PH14094 515 THE MAIN CABIN DOOR BINDS DURING OPENING. DOOR MUST BE MANUALLY MOVED TO THE OPEN POSITION. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR HINGES AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040517000582004051700058GL 2004 5 17 DXTA200400312 220040514A7310 WARNING LIGHT CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL BYPASS ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07986QS 7500086 CAE330189 ON TAKE-OFF AT 60 KNTS, (FUEL FILTER BYPASS L) CAS MESSAGE CAME ON, ABORTED TAKE-OFF. ITEM IS UNDER INVESTIGATION. 2L72 4J4 FRTT00007WITE6CH 20040517000622004051700062NM 2004 5 17 DXTA200400313 120040513A2161 CONTROLLER GULSTM200 200 4500308NM CABIN COOLING MALFUNCTIONED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07720QS 085 DURING FLIGHT THE COCKPIT AUTO TEMP MESSAGE ILLUMINATED, AFTER SWITCHING COCKPIT TEMP CONTROLLER TO MANUAL, SYSTEM WAS NORMAL AS LONG AS THE TEMP CONTROL KNOB WAS FULL COLD. PLACED TEMP CONTROL KNOB TO WARM AND NOTICED FUMES OF HOT MELTING PLASTIC, FOLLOWED BY THE COCKPIT DUCT TEMP, HI MESSAGE. RETURNED COCKPIT TEMP CONTROL KNOB TO FULL COLD AND THE WARNING WENT OUT. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA53NM 20040517000672004051700067EA 2004 5 17 SWIA200413290 120040427A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FLOOR SUPPT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. (FOUND DURING C-CHECK INSPECTION). ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII53-401. 2L72 4F RTA21EA 20040517000692004051700069NM 2004 5 17 DHL2004745017 120040429A2613 FIRE LOOP BOEING727 727224 1384076NM NR 1 ENGINE MISROUTED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01745DH 20665 NR 1 ENGINE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED TO DMI 16463 IAW MEL 26-9 PLACARD INSTALLED. REF DMI NR 16463 NR 1 ENG DETECTION CIRCUIT GROUNG LIGHT ILLUMINATED. FOUND ENG FIRE LOOP TOUCHING CASE, REROUTED FIRE LOOP, OPS CHECKS GOOD IAW B727 MM 26-11-012. THIS CLEARS DMI NR 16463. PLACARD REMOVED MXC NOTIFIED. 2L73 4F A3WE 20040517000702004051700070 2004 5 17 HNAA0400039 420040420A34177000700975 COMPUTER DHAV DHC8 DHC8102 2809003NM ADC NR 1 FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07933HA 134 AFTER TAKEOFF ADC 1 FAILED. NR 1 ALTIMETER AND IVSI FLAGGED, TRANSPONDER FAILED, OVERSPEED WARNING HORN SOUNDED AND GPWS C.L. OVERSPEED WARNING HORN SILENCED WHEN ADC 1 CB PULLED. REMOVED AND REPLACED DADC, SELF TEST GOOD. 2H72 4T RTA13NM 20040517000902004051700090NM 2004 5 17 F3LA200400052 120040419A2821 FILTER BOEING737 7373M8 1384615NM FUEL SYSTEM INOPERATIVE A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03303FL 25039 AIR TURN BACK. FLIGHT CREW REPORTED NR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REINSTALLED C/P D404 ON NR 2 ENGINE FIREWALL. INSPECTED NR 2 ENGINE FUEL FILTER. NO DEBRIS NOTED. SYSTEM CHECKED OKAY. NORMAL TAKEOFF POWER IAW MM 73-34-00. 2L72 4F RTA16WE 20040517000932004051700093 2004 5 17 RAIA00404009 420040418A34207011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU LT ADC FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03555HK9352 3141 41072 3661-RIC- LT ADC FAILED DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 SYMBOL GENERATOR. 2L72 4T RTA41NM 20040517000952004051700095WP 2004 5 17 MWEA040071 120040511A5320593659216 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 FLOOR SUPPORT ANGLE AT STATION 540 BETWEEN LONGERON 27 LT AND 27 RT HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INSTALLED NEW SUPPORT ANGLE AND SHIM. 2L72 4F A6WE 20040517001052004051700105EU 2004 5 17 U30A200400002 120040206A2710B372BAM0509 COMPUTER AIRBUS320 A320214 3930316EU ZONE 127 FAULTY A U30AK NONE J WARNING INDICATION ININSP/MAINT 1 EA17GBXKA 0714 DURING PRE-FLIGHT OF FLT 718 DTW-ACA, THE CREW NOTED NR 1 SEC (SPOILER ELEVATOR COMPUTER) ON ECAM FAULTED AND ON OVERHEAD PUSHBUTTON SWITCH.MAINTENANCE SWAPPED THE NR 1 SEC AND THE NR 3 SEC. NR 3 SEC (S/N 5601) WAS DEFERRED PER MEL 27-94-01. ALL MAINTENEANCE PROCEDURES AND CHECKS C/W. NOTE: REPLACED SEC (S/N 5601)ON 2/7/04. 2L72 4F RTA28NM 20040517001132004051700113WP 2004 5 17 0369 120040217A53205894282501 CLIP DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK 5690-0551 AFT CARGO FS 1210 LONGERON 33R CORRODED AND CRACKED 2 EACH FITTING CLIPS AND INDENTIFED AS LEVEL 2 CORROSION 2L74 4F 4A25 20040517001142004051700114WP 2004 5 17 0370 120040217A53203755843501 FITTING DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 DURING CPCP TASK 5590-0551 AFT CARGO FS 1160 LONGERON 35R AND 34R FITTING CRACKED AND IDENTIFIED AS LEVEL 2 CORROSION. 2L74 4F 4A25 20040517001182004051700118 2004 5 17 GLBA20030568 420040219A34141303800057 INDICATOR BEECH 1900 1900D 1154162CE AIRSPEED STUCK A GLBAO OTHER O OTHER TOTAKEOFF 1 NM03247GL UE247 FO'S ASI STUCK AT ZERO, PREFORMED PITOT CK OPS CK GOOD 2L72 4T RTA24CE 20040517001192004051700119CE 2004 5 17 GLBA20030569 120040223A282011892000033 LINE BEECH 1900 1900D 1154162CE FUEL SYSTEM LEAKING A GLBAK NONE K FLUID LOSS ININSP/MAINT 1 NM03210GL UE210 FUEL LINE PN 118920000330 CHAFED ON ACM DUCT ASSY COUPLING CREATING A FUEL LEAK, CHANGED FUEL LINE AND REPOSITIONED DUCT COUPLING AND SPIRAL WRAPPED FUEL LINE 2L72 4T RTA24CE 20040517001212004051700121WP 2004 5 17 02340405WP 120040216A3350AD4002P BATTERY DOUG DC9 DC931 3022065WP EMERGENCY LIGHT OUT OF TOLERANCEA A4JAK NONE L NO TEST ININSP/MAINT 1 SO35934LK 48157 EMERGENCY PORTABLE LIGHT AT FWD L1 DOOR INOPERATIVE. R&R RECHARGEABLE BATTERIES IAW 33-53-0. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 20040517001292004051700129CE 2004 5 17 58784 120040212A30801293840091 PRESSURE SWITCH BEECH 1900 1900D 1154162CE DEICE SYSTEM INOPERATIVE A AMWAO OTHER J WARNING INDICATION CLCLIMB 1 CE07182YV UE182 AFTER DEPARTING FROM MSS. CREW CLIMBED THROUGH INCING CONDITIONS AND FOUND TAIL DE-ICE TO BE INOP. IN BOTH MODES. THEY DIVERTED TO DUJ. UNDER A DISPATCH DECLARED EMERGENCY AND LANDED SAFELY WITH NOT FURTHER INCIDENTS.CORRECTIVE ACTION THAT WAS TAKEN IS R&R'D TAIL DE-ICE PRESSURE SWITCH. PERFORMED GRND RUN. OPS CK GOOD. P/N 129-384009-1 2L72 4T RTA24CE 20040517001302004051700130CE 2004 5 17 AMWA121 120040213A5312114410026113 BULKHEAD BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0726YV UE26 THREE CRACKS WERE FOUND IN FWD BULKHEAD FROM A SINGLE RIVET. CRACKS WERE APPROXIMATELY 1/2" OR SHORTER. PERFORMED EDDY CURRENT INSPECTION AND REPAIRED CRAKCS BY INSTALLING DOUBLER AND SHIME IN ACCORDANCE WITH RAYTHEON AIRCRAFT FR- CO-01004 2L72 4T RTA24CE 20040517001332004051700133NM 2004 5 17 SROM200400013 120040226A5310655496027 SHEAR TIE BOEING737 737205 1384456NM ZONE 200 CRACKED C SROMK NONE O OTHER ININSP/MAINT 1 AL03733PA339637874 23466 DURING D CHECK INSPECTION FOUND CRACKED SHEAR TIE AT STA 360 BETWEEN STR 14 & 15 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 SRM 53-10-4. 2L72 4F RTA16WE 20040518000332004051800033WP 2004 5 18 GTIA040334 120040423A7160 ACCOUSTIC LINER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 708500 DTW - FOUND ACCOUSTIC LINE DAMAGE AT 12 O'CLOCK POSITION ON NR 1 ENGINE REAR FAN CASE SECTION. REMOVED AND REPLACED NR 1 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20040518000382004051800038WP 2004 5 18 GTIA040296 120040315A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND FORWARD CARGO COMPARTMENT, CARGO TRACK SUPPORTS AND INTERCOSTAL BETWEEN L27R-L28R STATION 218-237 CORRODED. REMOVED INTERCOSTAL. FABRICATED INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2L72 4F A6WE 20040518000482004051800048WP 2004 5 18 G6OA022404 120040224A75001555M40G01 AIR DUCT DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE 14 STA ENG DUCT BLOWN A G6OAC ABORTED TAKEOFF RM PARTIAL RPM/PWR LOSS OVER TEMP TOTAKEOFF 1 EA27612GC 47840 455319 ON TAKEOFF CREW REPORTED A LOSS OF POWER ON NR 3 ENGINE THEY ABORTED TAKEOFF AT THIS TIME. A VISUAL INSPECTION IDENTIFIED THE 14 STAGE DUCT HAD BLOWN. 2L73 4F4 FRTA22WE E23EA 20040518000502004051800050EU 2004 5 18 00130 120040210A3260 UPLOCK AMD FALC20FALCON 2720302EU MLG OUT OF ADJUST E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05158TW 158 PILOT REPORTED AFTER DEPARTURE FROM STL GEAR INDICATION RED AFTER SELECTING GEAR UP, RETURN TO STL THREE GREEN AFTER SELECTING GEAR DOWN, WILL UPDATE AFTER MAINTENANCE. AFTER NUMEROUS ATTEMPTED FLIGHTS THE AIRCRAFT WAS RELOCATED VIA SPECIAL FLIGHT PERMIT TO ANOTHER MAINTENANCE FACILITY, R & R LT MLG UPLOCK ASSY AND ADJUSTED STRIKER PLATE, SYSTEM OPS CHECK GOOD, NO FURTHER PROBLEM ON SUBSEQUENT FLIGHTS. 2L72 4F A7EU 20040518000512004051800051CE 2004 5 18 CNQD20040001 120040301A5610NP1397223 WINDOW CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL COCKPIT CRACKED B CWQRA UNSCHED LANDING O OTHER CLCLIMB 1 WP05200AP2042 7500003 330002 THE COCKPIT LEFT SIDE WINDOW OUTER PLY SHATTERED ON CLIMB OUT FROM LAX. THE CREW DEPRESSURIZED THE AIRCRAFT AND DIVERTED TO LGB. 2L72 4J4 FRTT00007WITE6CH 20040518000522004051800052CE 2004 5 18 58817 120040213A3242 KNOB BEECH 1900 1900D 1154162CE RT BRAKE RELEASEUNSECURE A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07218YV UE218 RT BRAKE WILL NOT RELEASE. RESECURED BRAKE PARKING KNOB, LUBED ACT. 2L72 4T RTA24CE 20040518000572004051800057NE 2004 5 18 GLBA20030581 220040304A7200 ENGINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RIGHT OUT OF RIG A GLBAO OTHER J WARNING INDICATION APAPPROACH 1 NM03299UX 120299 RT ENGINE INADVERTENT AUTO FEATHER IN FLT, CHECKED ENGINE RIGGING & ADJUSTED AUTO FEATHER ARM SW. 2L72 4T4 TRTA31SO E20NE 20040518000602004051800060WP 2004 5 18 WRLA200410 120040228A2131 CONTROLLER GARRETTLTD DOUG DC10 DC1030F 3023504WP A/C PACK INTERMITTENT A WRLAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO11303WL 118C124 46917 SMOKE IN COCKPIT AFTER TAKE OFF TURNED NR 2 PACK OFF. SMOKE STOPED.RETURNED TO BGR. NOTE INSPECTED PACK & ON OPS TEMP DISCHARGE TEMP 95 PERCENT PACK AUTO OFF PLACED NR 2 PACK ON DMI M21FE2704-124 MEL 21-1 CAT C.. CLEARED DMI M21FE2704 REMOVED AND REPLACED NR 2 PACK TEMP CONTROLLER RAN NR 2 PACK ON GROUND FOR MAINY HOURS & PACK TEMP OPS NORMAL ALL PARAMETERS SHOW NORMAL AT THIS TIME ON GROUND. 2L73 4F RTA22WE 20040518000622004051800062SO 2004 5 18 ENHA2004C2070 220040207A8500 ENGINE CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO SHUTDOWN E ENHAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 AL039728M 20700721 570052 ON TAKE OFF AT 300 FT AGL PILOT EXPERIENCED ENGINE LOSS OF POWER, ENGINE QUIT. PILOT EMERGENCY ACTION IN ACCORDANCE WITH AFM RESTORED ENGINE OPERATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. L FUEL TANK HAD APPROX 25 GALS FUEL, R FUEL TANK HAD APPROX 25 GALS FUEL. COMPANY MAINTENANCE INSPECTED FUEL SYSTEM AND ENGINE IGNITION SYSTEM, PERFORMED ENG PERFORMANCE FUNCTIONAL TESTS, ENGINE GROUND OPERATION NORMAL, NO DISCREPANCIES NOTED, AIRCRAFT RELEASED FOR TEST FLIGHT. 1H71 3O3 O A16CE E5CE 20040518000642004051800064EA 2004 5 18 N401MA 220040214A7200 ISOLATION MOUNT BELL 412 412 1182202SW PWA PT6 PT6B36 52043EA REDUCTION GB DEBONDED E A1UAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE03401MA5565 1982 CPCB2463 33060 ENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAINTENANCE FOR REPAIRS. AFTER TROUBLESHOOTING FOUND LATERAL ISOLATION MOUNT DEBONDED. REMOVED AND INSTALLED SERVICEABLE UNIT. 1G72 4U4 U H4SW E4EA 20040518000712004051800071CE 2004 5 18 BIER200401059 120040312A2436B003871 VOLT REGULATOR BEECH 58 58 1152740CE FAILED B BSYAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS BHGSMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC MULTIPLE FAILURE CLCLIMB 1 EA211859 TH1299 SMELLED SMOKE IN COCKPIT, CIRCUIT BREAKER POPPED, SHUT-DOWN ALL POWER TO AIRCRAFT. FOUND OVERVOLTAGE CIRCUIT DID NOT DISABLE WHEN REGULATOR ALLOWED VOLTAGE TO CLIMB ABOVE 32V, TOOK OUT ALL ELECTRICAL EQUIPMENT ON. 1L72 3O 3A16 20040518000732004051800073SO 2004 5 18 RAIA00402028 120040227A33207287501519 SOCKET EMB 145 EMB145 3260210SO CABIN LIGHT BURNED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03805HK 145096 FUMES IN MAIN CABIN WITH SMOKE COMING FROM SEAT 1A CEILING LIGHT AREA. MAINTENANCE FOUND WINDOW WASH LIGHT HOLDER AT 1A BURNED AND DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI REMOVING AND REPLACING WINDOW WASH LIGHT HOLDER. 2L72 4F RTT00011AT 20040518000752004051800075SO 2004 5 18 RAIA00403006 120040305A3350RP51B POWER SUPPLY EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03821HK 145068 EMERGENCY FLOOR PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 2 POWER SUPPLY. 2L72 4F RTT00011AT 20040518000772004051800077SO 2004 5 18 RAIA00403008 120040309A3350RP51B BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03822HK 145069 MX - STL - FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS NR 1,2,3 & 4. 2L72 4T RTT00011AT 20040518000782004051800078NM 2004 5 18 EIA2004009 120040125A3340 SCREW BOEING747 747212B 1384886NM LANDING LIGHT LOOSE A EIAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09486EV 20888 DURING COCKPIT CHECK NOTICED ELECTRICAL ODOR. FOUND ONE SCREW HAD COME LOOSE ON LT OB LDG LIGHT SWITCH CAUSING ARCHING. UNABLE TO TIGHTEN SCREW REQUIRES NEW SWITCH. DEACTAVATED CIRCUIT AND ENTERED DMI 483. SWITCH ORDERED. 2L74 4F A20WE 20040518000932004051800093CE 2004 5 18 6026702272004 120040227A793030B445001 GEARSHAFT LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE RIGHT ENGINE LEAKING E J7SAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW055055855 60267 CA0386 FOUR MINUTES AFTER TAKEOFF THE MAIN OIL PRESSURE WARNING LIGHT CAME ON FOLLOWED SIX SECONDS LATER BY THE OIL PRESSURE DROPPING TO ZERO. ENGINE SHUTDOWN INTITIATED AND THE AIRCRAFT WAS DIVERTED TO BDL. ENGINE OIL WAS DISCOVERED ON THE FUSELAGE, TAIL, AND THE INNER AND OUTER ENGINE COWLINGS. IT WAS FOUND THAT ONLY EIGHT OUNCES OF OIL WERE IN THE RESERVOIR. ENGINE WAS REMOVED AND SENT TO PWC FOR REPAIR. THE TEARDOWN REPORT FOUND THAT AN OIL GALLERY PLUG PN ST3744 WAS NOT PROPERLY SWAGGED IN PLACE AND HAD COME LOOSE ALLOWING OIL TO ENTER THE STARTER/GENERATOR GEARSHAFT, ESCAPE INTO THE STARTER DRAIN AND SUBSEQUENTLY OUT THE DRAIN MAST. 2L72 4F4 FRTA10CE E35NE 20040518000952004051800095NE 2004 5 18 TSAA0479034 220040317A726169726881 BYPASS SWITCH BOEING737 737282C 13844AUNM PWA JT8 JT8D9A 52048NE NR 2 ENGINE FAILED A TSAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 WP13826AL 23051 ON DESCENT, OIL FILTER BYPASS LIGHT ILLUMINATED AND STAYED ON. SHUT DOWN ENGINE. REPLACED NR 2 FILTER BYPASS SWITCH FOR ILLUMINATION DUE TO FILTER CONTAMINATION. IDLE CHECK OK. REPLACED NR 2 ENGINE OIL FILTER FOR CONTAMINATION IAW 79-61-00. IDLE CHECK OK. DRAINED AND SERVICED NR 2 ENGINE OIL IAW 79-11-01. IDLE CHECK OK. 2L72 4F4 FRTA16WE E2EA 20040518000962004051800096NM 2004 5 18 C1HA200483005 120040222A3220 LANDING GEAR BOEING727 7272S7 138407ZNM NOSE LACK OF LUBE A C1HAO OTHER J WARNING INDICATION APAPPROACH 1 GL15683CA 22490 DURING GEAR EXTENTION, NOSE GEAR DID NOT COME. RECYCLED GEAR PER CHECKLIST OPERATED NORMAL. LUBRICATED NOSE GEAR PER MM 12-21-11 PERFORMED NOSE GEAR EXTENTION AND RETRACTION PERMM 32-33-00 .CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED 2L73 4F A3WE 20040518000972004051800097NE 2004 5 18 NAFA20040003 220040317A7414DLN10 MAGNETO DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE ENGINE SHORTED I N32BE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL017780B1809 1809 45372 37306 NR 2 ENGINE PRECAUTIONARY SHUT DOWN DUE TO LOSS OF LEFT DISTRIBUTOR. REPLACED NR 2 ENGINE MAGNETO. CHECK GOOD. 2L74 4R4 R 6A3 5E8 20040518000982004051800098NM 2004 5 18 PCAA0403182 120040315A494063D49845521 CONTROL PANEL DHAV DHC8 DHC8102 2809003NM APU SMOKE A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA13814EX 318 REPORTED A PUFF OF SMOKE FROM THE AUXILLARY POWER UNIT CONTROL PANEL WHEN THE GENERATOR SWITCH WAS SELECTED ON.MAINTENANCE CONFIRMED THAT THE CONTROL PANEL WAS AT FAULT AND DISCONNECTED THE PANEL CONNECTOR, ISOLATED THE UNIT, AND COMPLIED WITH MEL PROCEDURES UNTIL PARTS WERE OBTAINED. ONCE PARTS WERE AVAILABLE THE CONTROL PANEL WAS REMOVED AND REPLACED AND THE SYSTEM WAS OPERATIONAL CHECKED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040518000992004051800099NM 2004 5 18 PCAA0403183 120040318A5532CVR121 SEAL DHAV DHC8 DHC8102 2809003NM ZONE 300 LOOSE A PCAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA13846EX 326 REPORTED A VIBRATION IN CRUISE FLT. THE CREW ELECTED TO MAKE A PRECAUTIONARY LANDING AT WILLIAMSPORT DUE TO BEING OVERHEAD THE AIRPORT AT THE TIME. MAINTENANCE FOUND THE SEAL ON THE LEFT HAND SIDE OF THE VERTICAL STABILIZER TO HORIZONTAL STABILZER LOOSE. THE SEAL WAS REATTACHED AND THE AIRCRAFT RETUNED TO SERVICE. MAINTENANCE ALSO COMPLIED WITH INSPECTION OF THE ENGINE MOUNTS AND PROPELLAR ASSEMBLIES, ALL CHECKS GOOD. 2H72 4T RTA13NM 20040518001002004051800100SO 2004 5 18 RAIA00402029 120040225A277080951 SOLENOID EMB 145 EMB145 3260210SO RUDDER GUST LOCKDEFECTIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03833HK 145240 GUST LOCK WILL NOT DISENGAGE. MAINTENANCE DEFERRED SYSTEM IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE RUDDER GUST LOCK SOLENOID. 2L72 4F RTT00011AT 20040518001022004051800102NM 2004 5 18 C1HA200485001 120040318A324431395 TIRE BOEING727 7272S7 138407ZNM MLG SMOKE A C1HAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15685CA 22492 DURING GEAR RETRACT LAS THERE WAS ODOR OF BURNED RUBBER IN COCKPIT AND FWD CABIN AREA, AN AUDIBLE SQUEEL WAS HEARD ORIGTINATING FROM BELOW FLIGHT DECK, JUST PRIOR TO ROTATION LAS THE NOSE WHEEL SHOOK ABNORMALLY. INBOUND INTO MSP DECLARED EMERGENCY AND LANDED SAFELY AFTER GEAR CONCERNS. BOTH NLG TIRES PROPERLY INFLATED AND NO VISUAL DEFECTS IN/ON NLG WILL CHANGE BOTH TIRES AS A PRECAUTION. 2L73 4F A3WE 20040518001032004051800103NM 2004 5 18 C8GA20040002 120040317A2910BACH8B04NN0157 LINE BOEING727 727223 1384074NM HYD SYSTEM RUPTURED A C8GAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO15715AA 22470 FLT 202 FROM MDSD TO KMIA. ENROUTE TO KMIA OBSERVED A COMPLETE LOSS OF "B" SYSTEM HYDRAULIC FLUID FOLLOWED BY BOTH "B" SYSTEM LOW-PRESSURE LIGHTS ILLUMINATING. BRAKE PRESSURE BEGAN A SLOW DROP TO 1400 POUNDS. A PHONE PATCH WAS MADE TO COMPANY, ADVISED ATC IN MIAMI AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT OUR FINAL DESTINATION IN KMIA WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND A RUPTURE FLEX LINE TO HYD POWER UNIT FOR THE RIGHT HAND ELEVATOR. REPLACED FLEX HOSE ASSEMBLY AT ELEVATOR POWER UNIT, SERVICED “A” AND “B” HYDRAULIC SYSTEMS AND SYSTEM LEAK CHECK GOOD IAW B727 MM 12-12-0, 29-00 AND 27-30-81. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20040518001042004051800104SO 2004 5 18 RAIA00403009 120040312A2740 WARNING LIGHT EMB 145 EMB145LR 3260212SO PITCH TRIM ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 CE03811HK 145256 PRIMARY AND STANDBY PITCH TRIM FAIL INDICATION. EVENTUALLY REGAINED PRIMARY PITCH TRIM. MAINTENANCE PERFORMED OPERATIONAL CHECK OF PRIMARY AND STANDBY PITCH TRIM SYSTEMS. UNABLE TO DUPLICATE FAULT, OPS CHECK GOOD. 2L72 4T RTT00011AT 20040518001052004051800105 2004 5 18 RAIA00403011 420040315A2350AX40 HEADSET JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03550HK 41039 5542-STL- CAPTAIN'S HEADSET INOP. MAINTENANCE REMOVED AND REPLACED CAPTAIN'S HEADSET. 2L72 4T RTA41NM 20040518001062004051800106EU 2004 5 18 RAIA00403012 120040315A3097 WIRE AEROSPATR42 ATR42300 8680920EU RT PROP DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03426TE 228 RIGHT PROP DE-ICE FAILED. MAINTENANCE REMOVED AND REPLACED FAULTY WIRE AT RIGHT PROP ASSEMBLY. 2H72 4T RTA53EU 20040518001072004051800107EU 2004 5 18 RAIA00403014 120040316A3060B40183616 BOOT JETAIRJETSTMJETSTM4101 1500501EU RT PROP INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03550HK 41039 5537-JLN- RIGHT PROP HEAT FAILED. MAINTENANCE REMOVED AND REPLACED PROP BOOT. 2L72 4T RTA41NM 20040518001082004051800108EU 2004 5 18 RAIA00403016 120040317A2150 A/C PACK AEROSPATR72 ATR72202 8680940EU CABIN COOLING INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03723TE 283 LEFT PACK NO FLOW. MAINTENANCE TIGHTENED LOOSE CLAMP ON HEAT EXCHANGER. 2H72 4T RTA53EU 20040518001102004051800110WP 2004 5 18 IXXA0400017O 120040321A5280 ARM DOUG DC8 DC862 3021970WP MLG DOOR BENT A IXXAO OTHER J WARNING INDICATION CRCRUISE 1 SW11799AL73457222 45922335 IN CRUISE "DOORS NOT LATCHED LIGHT" CAME ON FOR 10 MINUTES. MAINTENANCE FOUND LT LANDING GEAR DOOR LATCH ROLLER ARMS BENT. REMOVED AND REPLACED LATCH ROLLER ARMS. WITH DOORS CLOSED FOUND LT DOOR LATCH ROLLER STOP BOLT SPACER CONTACTING RAIL ASSEMBLY. PERFORMED MAIN GEAR DOOR UPLACTH MECHANISM ADJUSTMENT/TEST TO PROVIDE A MINIMUM 1/8 INCH CLEARANCE BETWEEN STOP BOLT SPACER AND RAIL ASSEMBLEY. PERFORMED LANDING GEAR DOOR SWITCH TEST. OPERATIONAL CHECK WAS GOOD PER ALL MAINTENANCE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040518001122004051800112CE 2004 5 18 4514503112004 120040311A2613LJ01317002 SWIVEL VALVE LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP HYD SYSTEM BYPASSING E J7SAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW05421FX2386 45145 P116285 RIGHT PYLON OVERHEAT WARNING INDICATION ON TAKE-OFF. PILOT REDUCED POWER ON ENGINE TO IDLE AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO ORIGINATION POINT. MAINTENANCE REPLACED DAMAGED HP FIREWALL BLEED AIR SEALS. PROBLEM HAS RE-OCCURRED AND IS UNDER INVESTIGATION.CONTINUED 03.22.2004: REPLACED SWIVEL DUCT ASSEMBLY, 4 E-SEALS, 2 EACH PYLON OVERHEAT SENSORS AND MADE PERMANENT REPAIR TO THE R/H ENGINE EXHAUST INNER BYPASS DUCT. GROUND RUNS AND TEST FLIGHT CONDUCTED SATISFACTORILY. AIRCRAFT HAS MADE SUBSEQUENT FLIGHTS WITHOUT FURTHER DISCREPANCIES. 2L72 4F3 TRTT00008WIAEXJ STC 20040518001142004051800114NE 2004 5 18 WRNA200400003 220040319A7200 ENGINE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 1 FAILED A WRNAEC ENGINE SHUTDOWN ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO05502TA7475 3950 075 455454 DURING TAKEOFF ROLL AT 110KTS, LOUD BANG AND FLASH, COMPRESSOR STALL, NR 1 ENGINE. ABOURTED TAKEOFF AND PERFORMED ENGINE SHUTDOWN. EGT HAD EXCEEDED MAXIUM LIMIT, 935 DEGREES. BOROSCOPE OF HOT SECTION ENTAILED, REVIELED NO DAMAGE. ENGINE R & R IAW ENGING CHANGE PROCEDURES DUE TO OVERTEMP REPORTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20040518001152004051800115NM 2004 5 18 P5CA0401061 120040319A1420 CONNECTOR BOEING747 747236B 1384804NM AILERON INDI DIRTY A P5CAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 WP23924FT 21730 DURING FLIGHT CONTROL CHECK, NO INDICATION OF AILERON MVMT. CLEANED CONNECTOR D3297J AT J-BOX IN RT WHEEL WELL. PERFORMED FLIGHT CONTROL CHECK. ALL OPS AND INDICATIONS NORMAL PER MM 27-11-16. 2L74 4F A20WE 20040518001212004051800121EU 2004 5 18 0400483230 120040323A2910BHC106004 PRIORITY VALVE AIRBUS320 A320211 3930320EU PTU MANIFOLD LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS APAPPROACH 1 GL01330NW 307 JUST PRIOR TO APPROACH, RECEIVED ECAM MESSAGE 'HYD Y RSVR LO LVL'. FOLLOWED COM AND LANDED UNEVENTFULLY. ECAM INDICATED NEAR TOTAL LOSS OF FLUID. FOUND PRIORITY VALVE AT PTU MANIFOLD LEAKING. REPLACED PRIORITY VALVE AND SERVICED YELLOW HYDRAULIC RESERVOIR. LEAK AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040518001222004051800122EU 2004 5 18 YENA200419 120040323A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15531JB 1650 ODOR OF ELECTRICAL SMOKE REPORTED BY F/A IN G5 GALLEY. PER JB INFORMATION NOTICE 2003-T050TR A, INSPECTED ROWS 24-26 L/R SEBS, SEB CONNECTIONS, IN-SEAT WIRING, ARMREST/DPCU AREA WIRING, LIVE TV SIDEWALL RACKS(TO INCLUDE MRMS, RACK COMPONENTS, NO FAULTS/ABNORMALITIES NOTED AT THIS TIME. COULD NOT DUPLICATE ELECTRICAL ODOR. LIVE TV SYS OPERATES NORMAL AS PER LTV AMM 23-39-00. INSPECTION OF GALLEY FOUND COFFEEE POT WITH BURNT COFFEE IN IT. 2L72 4F RTA28NM 20040518001232004051800123NE 2004 5 18 WRLA200412 220040322A7200PW4462 ENGINE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 2 VIBRATION A WRLAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SO11274WA 48633 723945 ENGINE NR 2 HAS LEVEL 2 VIBRATION HI ALERT, ENGINE SHUTDOWN INFLIGHT AS A PRECAUTIONARY MEASURE FLIGHT FROM RKSI TO PANC, NR 2 ENGINE WILL BE CHANGE ON PANC 2L73 4F4 FRTA22WE E24NE 20040518001242004051800124NM 2004 5 18 HNAA0400025 120040319A291082910009119 LINE DHAV DHC8 DHC8201 2809001NM HYDRAULIC SYS LEAKING A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA07965HA 450 NR 2 HYD. QTY, LOST QTY IN TAKEOFF AND LANDING PHASE OF FLT. HYD PRESS STAYED AT 3000 PSI AT ALL TIMES. FOUND HYD LINE TO NLG DOOR SEQUENCE VALVE SOLENOID LEAKING, INSTALLED TFL AT THIS TIME. 2H72 4T RTA13NM 20040518001312004051800131NM 2004 5 18 WRLA200411 120040315A3350604413 BATTERY PACK DOUG MD11 MD11 3023602NM EMERGENCY LIGHT DISCHARGED A WRLAK NONE L NO TEST ININSP/MAINT 1 SO11804DE 48475 L4 OVERWING EMERGENCY BATTERY PACK TEST LOW, REMOVED AND REPLACED WITH A NEW BATTERY S/N#1037,OP'S CHECK GOOD. 2L73 4F RTA22WE 20040518001332004051800133NM 2004 5 18 C1HA200481001 120040320A215039608831 CONTROL VALVE BOEING727 7272S7 138407ZNM RT A/C PACK FAILED A C1HAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15681CA 22020 UPON APPLING TAKEOFF POWER AT 20 KNOTS. RIGHT PACK TRIPPED OFF. ABORTED AND RETURNED TO GATE. LOW SPEED INSPECTED AND RESCHEDULED PER MEL 21-1-1 CAT C06019. INFORMED MXC PLACARDS INSTALLED. (ITEM RESOLVE UNDER MDDR: C06019) REPLACED FLOW CONTROL MOD AND S/O VALVE PER M/M 36-12-61. OPS GOOD. REMOVED FROM MEL. 2L73 4F A3WE 20040519000012004051900001NM 2004 5 19 C1HA200475001 120040321A2120 CAP BOEING727 727225 1384077NM COALESCER DUCT LOOSE A C1HAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15816EA 22553 PRESSURIZATION WOULD NOT HOLD SCHEDULED CABIN ALTITUDE AT 6.3CC FOR FL370 CABIN SLOWLY CLIMB TO 10,000 FT WHEN CLOSED CARGO HEAT OUTFLOW CABIN DESCENDED TO 8,00 STABLE PLACED ON MEL 21-16-2A CABIN PRESSURE CONTROL SYSTEM AUTO INOP PER FORMED DDG C06028 INFLIGHT UNABLE TO CONTROL CABIN ALTITUDE IN BOTH STANDBY AND MANUAL MODE. MAINTENANCE REPAIRED LEAK BY TIGHTENING CLAP AT COALESCER DUCT OPS CHECKED GOOD REF 21-30-00 2L73 4F A3WE 20040519000032004051900003 2004 5 19 RAIA00403013 420040315A3460E535E100 FDAU EMB 145 EMB145LR 3260212SO COCKPIT FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03812HK306 145373 3545-RIC- FDAU FAILED. MAINTENANCE REMOVED AND REPLACED FDAU. 2L72 4T RTT00011AT 20040519000052004051900005SO 2004 5 19 RAIA00403017 120040324A28102810051102 VALVE EMB 145 EMB145ER 3260211SO FUEL SYSTEM LEAKING A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03827HK2481 145021 STL FUEL LEAK/VENTING. TOWER REPORTED LARGE AMOUNT OF WHITE SMOKE COMING FROM AIRCRAFT. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT WING FUEL VENT VALVES. 2L72 4F RTT00011AT 20040519000072004051900007SO 2004 5 19 RAIA00403019 120040322A3040163500122 HEATER EMB 145 EMB145LR 3260212SO WINDSCREEN SHORTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE03822HK2438 145069 5762 - OKC - UPON DECENT INTO STL SMOKE IN COCKPIT. MAINTENANCE TROUBLE SHOT AND DEFERRED FO'S WINDOW HEAT PER MEL. SUBSEQUENTLY CLEARED MEL REMOVING AND REPLACING FO'S WINDSCREEN. 2L72 4T RTT00011AT 20040519000092004051900009SO 2004 5 19 RAIA00403021 120040323A2760 SWITCH EMB 145 EMB145 3260210SO THRUST LEVER DIRTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03802HK 145066 3538 - PIT - "SPD BRK LVR DISAGREE" MESSAGE. MAINTENANCE CLEANED THRUST LEVER SWITCHES. HIGH SPEED TAXI CHECKS OK. 2L72 4F RTT00011AT 20040519000102004051900010CE 2004 5 19 4010 120040320A32306046H39A RELAY BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO HARTZLHCJ3Y PHCJ3YR2 GL MLG INTERMITTENT E BSYAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL072027V TH965 298902R ED4124A (CLE) GEAR WOULD NOT COME DOWN, CYCLED GEAR SELECTOR MANY TIMES THEN GEAR FINALLY CAME DOWN, PILOT ELECTED TO FLY GEAR DOWN TO (CMH). MAINT. FOUND BOTH THE CIRCUIT BREAKER AND THE DYNAMIC BRAKE RELAY INTERMITTENT,REMOVED AND REPLKACED BOTH UNITS OPS. CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20040519000112004051900011SO 2004 5 19 4012 120040321A3230487862 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCC4Y HCC4YR2 GL ZONE 700 INTERMITTENT E BSYAO OTHER J WARNING INDICATION LDLANDING 1 GL07711LH 318152174 L173868A FH848 INTERMITTENT LEFT GEAR DOWN AND LOCK LIGHT.FOUND DOWN AND LOCK SWITCH BAD, REMOVED AND REPLACED SWITCH OPS. CHECKS GOOD. 1L72 3O3 O A20SO E14EA 5 CP52GL 20040519000122004051900012NM 2004 5 19 757BJ0008 120040319A5230 RETAINER BOEING757 757236 1384971NM CARGO DOOR SEAL CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 NR 1 CARGO DOOR AFT FRAME WEB CRACKED AT I/B SEAL RETAINER ATTACH HOLE. REPAIRED DAMAGE PER SRM 53-00-07. 2L72 4F RTA2NM 20040519000162004051900016 2004 5 19 372PA0043 420040321A2230735SUE1012 COMPUTER BOEING737 737306 13844BGNM AUTO THROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05372PA 23546 AUTO THROTTLE WILL NOT ARM. RELEASED ON MEL 22-4. 03/23/2004: REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-10. BITE CHECKS GOOD. 2L72 4F RTA16NE 20040519000182004051900018 2004 5 19 GLBA20030597 420040325A34141303800057 INDICATOR BEECH 1900 1900D 1154162CE AIRSPEED STUCK A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03247GL2519 UE247 NR 2 ASI STUCK AT ZERO, R&R NR 2 ASI PN 130-380005-7 2L72 4T RTA24CE 20040519000192004051900019NM 2004 5 19 0400496740 120040324A3240 WARNING LIGHT BOEING747 747251F 1384898NM BRAKE OVERHEAT FALSE INDICATIONA NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01640US 23888 DURING TAKEOFF, THE BRAKE OVERHEAT LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF AT 120 KNOTS AND RETURNED TO THE GATE WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED THE BRAKING SYSTEM WITH NO FAULTS FOUND. 2L74 4F A20WE 20040519000202004051900020EU 2004 5 19 DXTA200400271 120040319A5720 TAPE BRAERO1000 HAWKER1000 7450005EU RT WING TIP LOOSE E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07550QS 259050 CLIMBING THROUGH APPROXIMATELY FL280, EXPERIENCED A SEVERE LONGITUDINAL OSCILLATION. THE YOKE OSCILLATED LEFT AND RIGHT RAPIDLY AND WINGS WERE FLEXING 4 TO 6 INCHES, DISCONNECTED AUTOPILOT WITH NO POSITIVE AFFECT, CONDITION IMPROVED BY SLOWING DOWN THE AIRCRAFT FROM 275 TO 250-255 KTS, ACCOMPLISHED AIR TURN BACK. - VISUALLY INSPECTED BOTH WINGS, FOUND CHAFED TAPE COMING LOOSE ON THE RIGHT WING LENSE TIP. REMOVED CHAFED TAPE FROM LEFT AND RIGHT WING TIP LENSE, NO OTHER DISCREPANCIES FOUND IAW HAWKER 1000 AMM CHAPTER 20. 2L72 4F RTA3EU 20040519000222004051900022NM 2004 5 19 WRLA200413 120040318A2497 WIRE DOUG MD11 MD11F 3023600NM PDU BURNED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11275WA 48631 CENTER CARGO COMPT. PDU WIRE BUNDLE HAVE 6 WIRES BURNED AND BROKEN (WIRE NO:G110-663-20, G110-667-20, G110-665-20, G110-668-20, G110-666-20 AND G110-094-16) REPAIR THE WIRES WITH SPLICE PER SWPM 20-10-03. WIRES CONTINUITY AND INSULATION CHECK PER WDM 30-29-01 & 2552-05.CAUSE ANALYSIS: FORE, AND AFT DOUBLE FACED RESTRAINT LATCH ROD BROKEN AND CHAFING WITH WIRES AT (STA. 1721) 2L73 4F RTA22WE 20040519000232004051900023CE 2004 5 19 DXTA200400174 120040324A5300 STRUCTURE CESSNA500 560CESSNA 2076750CE AIRFRAME NOISY E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07373QS 5600373 CLIMBING THROUGH 12,000 FT AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLOWED DOWN BELOW 250 KNOTS THEN THE PROBLEM STOPPED, RE-ACCELERATED IT HAPPENED AGAIN. LOWERED THE GEAR NORMALLY AND DIVERTED TO ACY. - ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040519000242004051900024CE 2004 5 19 DXTA200400272 120040321A3260602751 DOWNLOCK SWITCH CESSNA750 750 2076810CE MLG INOPERATIVE E DXTAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL07952QS 7500200 WHEN GEAR HANDLE WAS PUT IN DOWN POSITION 3 GREEN AND RED GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR HANDLE AND CONDITION WAS THE SAME PER EMERGENCY CHECK LIST, GEAR HORN CAME ON WITH FULL FLAPS. DIVERTED TO SWF AND LANDED SAFELY. VISUALLY INSPECTED THE RT MAIN GEAR UP-LOCK AND DOWN LOCK ASSY'S, NO DEFECTS NOTED. TROUBLESHOT AND FOUND RT MAIN LANDING GEAR DOWN LOCK INOP. REPLACED DOWN LOCK SWITCH REF CESSNA 750 MM CHAPTER 32-30-04. RESET SHUTTLE ON GEAR CONTROL VALVE AND PERFORMED GEAR SWINGS TO PURGE AIR. SYSTEM GROUND OPERATIONAL CHECK GOOD 2L72 4J RTT00007WI 20040519000252004051900025CE 2004 5 19 DXTA200400273 120040322A1420 CONNECTOR CESSNA500 560CESSNA 2076750CE ANTI SKID SYS CONTAMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07302QS6882 5600402 400 FEET ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED. - BLED AIRCRAFT BRAKE SYSTEM IAW CESSNA 560 MM CHAPTER 32-42-00. SERVICED EMERGENCY BRAKE BOTTLE IAW CESSNA 560 MM CHAPTER 12-13-01, FOUND ANTI-SKID CONTROL BOX CONNECTOR TO HAVE HYDRAULIC FLUID INSIDE CONTROL BOX AND NOTICED A BURN ODOR. CHECKED ALL HYDRAULIC LINES FOR LEAKS, REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20040519000262004051900026SO 2004 5 19 RAIA00403022 120040323A1420 CONTROL UNIT EMB 145 EMB145LR 3260212SO TRIM SYSTEM MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03814HK8057 1230 145046 5677 -STL - PITCH TRIM 1 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STAB UNIT. 2L72 4T RTT00011AT 20040519000282004051900028EU 2004 5 19 RAIA00403025 120040325A3244AH52688 TIRE JETAIRJETSTMJETSTM4101 1500501EU NLG WORN A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03562HK 41078 3657 - BWI - AIRCRAFT HARD TO HOLD ON CENTER LINE. MAINTENANCE REMOVED AND REPLACED BOTH NLG TIRES. 2L72 4T RTA41NM 20040519000352004051900035NM 2004 5 19 HNAA0400030 120040326A3010 TAPE DHAV DHC8 DHC8102 2809003NM LEADING EDGE DEBONDED A HNAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA07934HA 139 LEFT I/B BOOT LOOSE. PHL WILL SECURE WITH SPEED TAPE WE'LL MEL A/F DEICE AND FLY REVENUE TO SBY. SCURED LOOSE DEICE BOOT WITH SPEED TAPE I/A/W SPECIAL PROCEDURE 20.2 AND PLACED AIRFRAME DEICE ON MEL. R&R LEFT INBOARD DEICE BOOT LEADING EDGE. 2H72 4T RTA13NM 20040519000362004051900036 2004 5 19 371PA0041 420040326A221075130 TRANSFER VALVE BOEING737 737306 13844BGNM YAW DAMPER INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05371PA 23543 YAW DAMPER INOPERATIVE. RELEASED ON MEL. 03/29/2004: REPLACED RUDDER POWER CONTROL UNIT TRANSFER VALVE PER MM 22-12-21. OPS CHECKS GOOD. 2L72 4F RTA16NE 20040519000372004051900037EU 2004 5 19 CX7A194J0421 120040328A26131734362450 DETECTOR SAAB SF340 340B 7860101EU TAIL PIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03318CE 340B358 DURING TAKEOFF ROLL, RECEIEVED TAILPIPE HOT INDICATION (ABORTED TAKEOFF) WARNING IMMEDIATELY EXTINGUISHED. 2L72 4T RTA52EU 20040519000402004051900040NM 2004 5 19 TSAA0456033 120040315A56105893543129 WINDSHIELD BOEING737 7372T4 1384492NM COCKPIT FAILED A TSAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP13808AL 23445 CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED. RETURNED TO HNL. REMOVED AND REPLACED CAPTAIN'S NR 1 WINDOW IAW AMM 56-11-11, PAGES 401-411 AND 580. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20040519000422004051900042EA 2004 5 19 HNAA0400031 120040330A5542 SKIN DHAV DHC8 DHC8311 1386006EA RUDDER CRACKED A HNAAO OTHER E VIBRATION/BUFFET CRCRUISE 1 EA07336EN 336 SEVERE TURBULENCE JOLT OCCURRED AT 17,000 FT. LOST 200 FEET. INSPECTED IAW W/C 05-50-21I ONE DEFECT NOTED FOUND CRACK IN FORE RUDDER. REPAIRED IAW EO 8-55-04-0222 2H72 4T RTA13NM 20040519000432004051900043NE 2004 5 19 04013 220040331A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 MALFUNCTIONED A KCSAEA ENGINE SHUTDOWN UNSCHED LANDING EMJVIBRATION/BUFFET OVER TEMP WARNING INDICATION CRCRUISE 1 GL23712CK54196 19754 685652 SHUTDOWN NR 2 ENGINE IN FLIGHT; AT APPROX. 4000 FT AGL NR 2 ENGINE SURGED AND BANGED FOLLOWED WITH HIGH EGT 1150 DEG.C. RETURNED TO VHHH AND ALL OTHER ENGINE PARMETERS NOT EXCEEDED. 2L74 4F4 F A20WE E20EA 20040519000442004051900044NM 2004 5 19 P5CA0401064 120040330A272025EN556 SWITCH BOEING747 747236B 1384804NM TE FLAPS FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23924FT 21730 OUTBOARD AILERONS FAILED TO UNLOCK AFTER FLAPS 20 DEG SELECTED. FOUND FLAP LIMIT SWITCH S216 FAILED. R & R SWITCH, ALL OPS NORMAL. 2L74 4F A20WE 20040519000462004051900046WP 2004 5 19 7357 120040329A5313609458 STRINGER DOUG DC3 DC3 3021401WP FUSELAGE CORRODED E JRAAK NONE O OTHER ININSP/MAINT 1 GL11376A 27047 STRINGER CORROSION FOUND DURING PHASE INSPECTION ON RIGHT FUSELAGE BELOW FLOOR AT STATION 312.5 TO 450.5, THE STRINGER WAS REMOVED AND REPLACED. 2L72 4R A669 20040519000492004051900049EU 2004 5 19 YENA200420 120040330A2780 COMPUTER AIRBUS320 A320232 3930326EU SLATS MALFUNCTIONED A YENAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA15536JB 1784 FLAPS LOCKED WITH ALIGNMENT FAULT BETWEEN 0 & 1; SLATS NORMAL EXTENSION. RESET BOTH SFCC'S AND PERFORMED TSM TASK 27-51-00810-818 PAR 4. A. (5), NO FAULTS NOTED. AIRCRAFT IS SATISFACTORY FOR SERVICE. 2L72 4F RTA28NM 20040519000522004051900052EA 2004 5 19 X6PA000042004 220040331A8500IO540K1A5 ENGINE PIPER PA32 PA32300 7103212SO LYC O540 IO540K1A5 41532EA LEAKING E X6PAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SO33130BW 3240963 L1076048A SHORTLY AFTER TAKE OFF FROM RDU MARCH 31,2004, AT 1:45PM N130BW LOST OIL PRESSURE. THE PILOT TURNED BACK TOWARD THE FIELD; HOWEVER, BEING SHORT OF THE RUNWAY HE EMERGENCY LANDED ON A ROAD NEXT TO RDU. NO DAMAGE TO THE AIRCRAFT OR PILOT. UPON INSPECTION THE ENGINE STILL CONTAINED 9 QUARTS OF OIL, AND THE CASE WAS PENITRATED JUST ABOVE THE NR 6 CYLINDER. NO CAUSE FOR LOSS OF OIL PRESSURE HAS BEEN DETERMINED AT THIS TIME. 1L71 3O3 O A3SO 1E4 20040519000532004051900053EU 2004 5 19 00134 120040331A5230 DOOR AMD FALC20FALCON 2720302EU CARGO BAY OPEN E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05232TW 32 PILOT REPORTED CARGO DOOR OPENED INFLIGHT AT APPROX 500FT AGL, RETURN TO DEPARTURE AIRPORT FOR UNEVENTFUL LANDING. DOOR WAS INSPECTED PER THE AVTEC MANUAL AND OPS CK NORMAL. AIRCRAFT RETURNED TO SERVICE. TRIP WAS COMPLETED WITH NO FURTHER PROBLEMS. 2L72 4F A7EU 20040519000552004051900055NM 2004 5 19 EIA2004013 120040318A3350 BATTERY PACK BOEING747 747132 1384882NM EMERGENCY LIGHT DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09479EV 19898 EMERGENCY ESCAPE LIGHT ABOVE FIRE WARNING CARD MODULE INTERMITTENT. RECHARGED BATTERY PACK. OPERATIONS CHECK OK. 2L74 4F A20WE 20040519000562004051900056NE 2004 5 19 EIA2004014 220040328A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 4 FLAMED OUT A EIAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 NM09482EV 20713 662971 CLIMBING THROUGH 38500 FT NR 4 ENGINE FLAMED OUT. INFLIGHT RESTART NORMAL. INSPECTED INTAKE AND EXHAUST NO DEFECTS NOTED INSPECTED BLEED SCREENS NO FOREIGN OBJECTS NO DEFECTS. REPLACED MAIN FUEL FILTERS, SUMPED NR 4 FUEL DRAIN NO WATER FOUND. FUEL PUMP PRESSURE CHECKED AT FP-12 PRESSURE ABOVE 300 PSI. PERFORMED OPS CHECK OF FUEL CONDITION ACTUATOR NO DEFECT FOUND. NR 4 SYSTEM OPS CHECKED NORMAL PER MM 71-00-40, 71-00-42,71-00-46. CHECKED WATER DRAIN AT EVC PT3 NO DEFECT. 2L74 4F4 F A20WE E20EA 20040519000572004051900057NM 2004 5 19 250TR0028 120040331A5330 SKIN BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CRACK IN THE FUSELAGE SKIN AT THE LEFT AFT ENTRY DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED DAMAGE PER SRM 53-30-3 FIG. 24. 2L72 4F RTA16WE 20040519000602004051900060 2004 5 19 GLBA20030601 420040401A3420F0030 FUSE EMB 120 EMB120ER 3260203SO NR 2 AHRS LOOSE A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM03297UX 120297 NR 2 AHRS FAILED IN FLIGHT, FOUND FUSE F0030 NOT SEATED RESEATED FUSE OPS CK & RUN GOOD 2L72 4T RTA31SO 20040519000612004051900061CE 2004 5 19 DXTA200400274 120040324A326025WS4055AD UPLOCK CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07373QS 5600373 CLIMBING THROUGH 12,000 FEET AT 280 KNOTS, NOTICED A "THUMPING NOISE" FOLLOWED BY AN INTERMITTENT GEAR UNSAFE LIGHT. SLOWED DOWN BELOW 250 KNOTS THEN THE PROBLEM STOPPED, RE-ACCELERATED IT HAPPENED AGAIN. LOWERED THE GEAR NORMALLY AND DIVERTED TO ACY. FOUND NOSE GEAR UP-LOCK ROLLER NOT SEATED IN HOOK WHEN GEAR WAS RETRACTED. ADJUSTED UP-LOCK ASSEMBLY PER CESSNA 560 MM CHAPTER 32-31-05, PERFORMED NUMEROUS LANDING GEAR SWINGS WITH NO PROBLEMS. 2L72 4F RTA22CE 20040519000642004051900064NE 2004 5 19 NACA20040015 220040331A8530356993 CYLINDER HEAD DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03438721019 1019 533294 P34219 NR 4 ENGINE FEATHERED DUE TO BACKFIRING, RUNNING ROUGH, AND LOSS OF POWER. REPLACED NR 4 ENGINE, NR 2 CYLINDER DUE TO CRACKED HEAD. 2L74 4R4 R A781 5E8 20040519000662004051900066EU 2004 5 19 RAIA00403026 120040326A3260AIR135668 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03554HK 41067 GEAR HANDLE LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED AND REPLACED UPLOCK SWITCH. 2L72 4T RTA41NM 20040519000672004051900067GL 2004 5 19 RAIA00403027 220040327A7200AE3007A ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RIGHT OVERTEMP A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03817HK9559 145058 311246 RIGHT ENGINE HIGH ITT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. 2L72 4T4 FRTT00011ATTE6CH 20040519000682004051900068EU 2004 5 19 RAIA00403028 120040331A2797 WIRE JETAIRJETSTMJETSTM4101 1500501EU STICK SHAKER FAULTY A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03553HK 41066 TAKE OFF CONFIGURATION WARNING FAULT DURING TAXI. MAINTENANCE REPAIRED BROKEN WIRE AT STICK SHAKER, RESET POWER AND OPS CK OK. 2L72 4T RTA41NM 20040519000702004051900070CE 2004 5 19 DXTA200400286 120040401A30209945363 VALVE CESSNA750 750 2076810CE ANTI ICE SYSTEM MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07964QS 7500164 ABORTED TAKEOFF FOR "HP DUCT O PRES - RIGHT" CAS MESSAGE. REMOVED AND REPLACED RIGHT ENGINE HIGH PRESSURE ANTI-ICE SHUT OFF VALVE IAW CESSNA 750 MM CHAPTER 36-10-00, OPS CHECK GOOD. 2L72 4J RTT00007WI 20040519000712004051900071CE 2004 5 19 DXTA200400287 120040401A2710 AILERON CESSNA560 560XL 2076702CE WINGS VIBRATION E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07625QS 5605319 AFTER TAKE OFF WITH GEAR UP ABOVE 180 KNOTS IAS, YOKE DEVELOPED AN AILERON SHIMMY/ VIBRATION OF APPROX. 1 TO 2 VIBRATIONS PER SECOND. INTENSITY INCREASED UP TO 300 KNOTS IAS, VIBRATIONS DECREASED ON DESCENT AND BELOW 170 KNOTS IAS. - PERFORMED FREE PLAY CHECK ON AILERON CONTROL TRIM TAB. INSPECTED ALL FLIGHT SURFACES FOR LOOSE, DAMAGED OR MISSING PARTS. INSTALLED HYDRAULIC TESTER AND RAN FLAPS AND STAB, RAN ALL TRIM AND FLIGHT CONTROLS I/A/W 560XL MM 27-10-00 & 27-00-00, NO DEFECTS NOTED 2L72 4F RTA22CE 20040519000742004051900074 2004 5 19 00135 420040331A3422 GYRO AMD FALC20FALCON 2720302EU COCKPIT STUCK E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05165TW 65 PILOT REPORTED CAPT'S DG STUCK ON RUNWAY HEADING, RETURN TO DEPARTURE AIRPORT, MAINTENANCE COULD NOT DULICATE,, CK GOOD ON ALL HEADINGS IAW WITH FALCON 20 M/M. 2L72 4F A7EU 20040519000762004051900076NM 2004 5 19 PCAA0405187 120040405A2710LA11A2118 ACTUATOR DHAV DHC8 DHC8102 2809003NM AILERON TRIM INOPERATIVE A PCAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA13811EX107893696 201 LGA REPORTED AILERON TRIM INOP.MAINTENANCE REPLACED THE AILERON TRIM ACTUATOR.SYSTEM CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519000782004051900078 2004 5 19 251TR0009 420040403A22101061984158 CONTROL PANEL BOEING737 737228 13844AGNM AUTOFLIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05251TR 23792 MODE CONTROL PANEL IS INOPERATIVE. REPLACED MODE CONTROL PANEL PER MM 22-11-341. OPS CHECKS GOOD. 2L72 4F RTA16WE 20040514000582004051400058EA 2004 5 14 ASOA04276 120040409A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED TEH PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040514000592004051400059EU 2004 5 14 A6WA200460012 120040412A5420 ANGLE BAG BAE146BAE146300A 1500267EU NR 4 PYLON CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 FOUND CRACK IN THE NR 4 PYLON AT THE FORWARD END OF THE CENTER ANGLE JUST AFT OF RIB NR 3. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 615-18830001. (M) 2H74 4F RTA49EU 20040514000612004051400061EU 2004 5 14 USAA040078 120040328A5347D5311281520200 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND TRACK CORRODED 1.3 INCHES BY 1.1 INCHES BY .043 INCH AREA, MAIN DECK SEAT TRACK, FRAME 16, Y 1252, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11, SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040514000622004051400062EU 2004 5 14 USAA040079 120040328A534705311281520202 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND TRACK CORRODED 1.6 INCHES LONG BY 1.0 INCH WIDE BY .068 INCH DEEP AREA, BETWEEN FRAME 12-24 BL Y765. REMOVED AND REPLACED SEAT TRACK PER SRM 51-42-11, 51-74-00, 53-11-14. CORROSION LEVEL 2 TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040514000652004051400065EU 2004 5 14 KBM2004F00035 120040301A6220MA4373 BALL SNIAS 350 AS350BA 8680817EU SPIDER ASSY WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 BALL END ON SPIDER ASSY IS WORN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514000682004051400068EA 2004 5 14 WVE2004F00011 120040426A57206001020427 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT WING CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09408SW 7055 LT WING STA 48.30 ANGLE PN 600-1020427 IS CRACKED 1 INCH IN RADIUS. PROBABLE CAUSE: STRESS. REMOVE AND REPLACE ANGLE IAW CRJ 200 SRM 51-42-21 AND 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040514000792004051400079EU 2004 5 14 KBM2004F00028 120040307A6420AS350BA BEARING SNIAS 350 AS350BA 8680817EU T/R BLADE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P14078 2347 TAIL ROTOR BLADE HALF SHELL BEARING WORN OUT. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040514001012004051400101EU 2004 5 14 KBM2004F00040 120040326A792147750 MOTOR SNIAS 350 AS350BA 8680817EU BLOWER OVERHEATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH1045 2337 OIL TEMP HIGH WHEN SITTING ON THE GROUND (100 DEGREE (C)). REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U NCH9EU 20040514001082004051400108NM 2004 5 14 QXEA200400319 120040504A5720 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX 4037 PDX - RT WING FUEL PANEL 623AT HAS ONE BROKEN NUTPLATE. REPAIRED IAW Q400 AMM TASK 57-11-01-400-801, PARAGRAPH 1, 2, 3 AND 4C. 2H72 4T RTA13NM 20040514001132004051400113NE 2004 5 14 ASMF200405011 220040507A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RIGHT MALFUNCTIONED W ASMFC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW231003Y 48068 P708437 AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM, LOW POWER ON RT ENGINE. INLET AND OUTLET OF RT ENGINE WERE CHECKED, ALL CORRECT. FUEL CONTROL UNIT WAS REPLACED AND PT2, PT7 AND OIL FILTER WERE CHECKED. TRIM TO BOTH ENGINES WAS PERFORMED AND EGT REACHED 630 DEGREES, THEREFORE PYD AND PRBC VALVES WERE REPLACED. AFTER REPLACEMENT, EGT REACHED 640 DEGREES, SO PYD AND PRBC WERE REINSTALLED IN THE ORIGINAL POSITIONS. ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. 2L72 4F4 F A6WE E9NE 20040517000012004051700001EU 2004 5 17 DHL2004367004 120040428A2780861CAH SENSOR AIRBUS300 A300B4203 3930306EU ANGLE OF ATTACK FAILED A DHLAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO01367DH3197 3197 265 SLAT/FLAP LEVER WOULD NOT MOVE AFTER TAKEOFF COMPLETED THE SLAT/FLAP LEVER LOCK FAILURE ABNORMAL PROCEDURE. REMOVED AND REPLACED NR 1 AOA SENSOR IAW MM 22-23-39. CHECKED GOOD. PERFORMED OPERATIONAL TEST OF SLAT RETRACTION INTERLOCK IAW MM 27- 81-00. TESTED GOOD 2L72 4F RTA35EU 20040517000102004051700010EU 2004 5 17 USAA040092 120040331A5321D5361060500000 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW16307 0929 BFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 1 INCH WIDE BY .02 INCHES DEEP AREA, MAIN CABIN, PANEL 221FF. REPLACED WITH NEW PANEL PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20040517000352004051700035 2004 5 17 USAASA04036 420040415A256561639103 BOTTLE AIRBUSA321 A321211 3930370EU ESCAPE SLIDE INOPERATIVE A K NONE O OTHER ININSP/MAINT 1 EA19166US 1436 FAILURE MESSAGE 'SLIDE BOTTLE MID R'. MAINTENANCE REPLACED THE MID RIGHT DOOR SLIDE INFLATION RESERVOIR. THE SHOP FOUND SOME LEAKING AT THE O-RING AT THE SLIDE BOTTLE NECK. REPLACED THE O-RING. (M) 2L72 4F RTA28NM 20040517000362004051700036WP 2004 5 17 GTIA040292 120040310A5311 FRAME DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND CORROSION AND CRACKED FRAME 'L' ANGLE AFT SUPPORT FS 731 MID CARGO L30 AND L29R. REMOVED CRACKED AND CORRODED FRAME 'L' ANGLE LOCATED AND DRILLED NEW ANGLE. INSTALLED ANGLE. (M) 2L72 4F A6WE 20040517000422004051700042EA 2004 5 17 A6WA200440046 120040417A4930 LINE CNDAIRCL600 CL6002B19 1900309EA APU FUEL LEAKING A A6WAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 GL31457AW 7854 AT FL310, STRONG ODOR OF JET FUEL FUMES, FLIGHT ATTENDANT ALSO HAD SAME SMELL FROM ROW 2 FORWARD TO GALLEY. NO ODOR AT REAR OF CABIN, DESCENDED TO FL280, SAME ODOR, DESCENDED TO FL240 ODOR WENT AWAY. IN DESCENT CENTER TANK QTY FLUCTUATING BETWEEN 0-20 LBS. INSPECTED AND FOUND FUEL LEAK AT FUEL APU, ATTEMPTED TO TIGHTEN FITTINGS. ALL WERE TIGHT. CLEANED RESIDUAL FUEL, RAN APU AND VERIFIED LEAK. DISCOVERED FUEL LEAK IN APU FUEL SUPPLY LINE AND CRACKED FUEL MANIFOLD. (M) 2L72 4F RTA21EA 20040517000432004051700043WP 2004 5 17 GTIA040280 120040326A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW- FOUND CABIN STATION 160-200 LBL 7 FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT. FORMED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M0 2L72 4F A6WE 20040517000532004051700053NM 2004 5 17 QXEA200400313 120040511A27202379003001 REGULATOR DHAV DHC8 DHC8202 2809007NM RUDDER FAULTY A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09364PH7967 524 PDX - FLIGHT 2173 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF, THE CREW RECEIVED A RUDDER FULL PRESSURE CAUTION LIGHT, NR 1 RUDDER HYDRAULIC CAUTION LIGHT, AND RUDDER PRESSURE CAUTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RUDDER DUAL PRESSURE REGULATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040517000542004051700054WP 2004 5 17 DHL2004805004 120040513A33505708458505 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01805DH 46125 A/C EMERGENCY POWER BATTERY PACK DISCHARGED. REMOVED AND REPLACED A/C EMERGENCY BATTERY PACK, OPS CHECKED GOOD IAW DC-8 MM. 2L74 4F RT4A25 20040517000632004051700063EA 2004 5 17 SWIA200413286 120040503A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 FS 625 RT SIDE INTERCOSTAL ANGLE STR 14R CRACKED. (FOUND DURING C-CHECK INSPECTION). 2L72 4F RTA21EA 20040517000652004051700065EA 2004 5 17 SWIA200413288 120040427A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07925SW 7682 MAIN FUSELAGE PULLEY INTECOSTAL HAS OB FLANGE CRACKED FS 484.00 RBL 36.0. (FOUND DURING C-CHECK INSPECTION). MANUFACTURED AND INSTALLED ANGLE AS REQUIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20040517000682004051700068EA 2004 5 17 SWIA200413291 120040503A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 FS 625 RT OBLIQUE ANGLE P/N 601-35012-52 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-21-16, 51-23-00, AND 52-42-06. SEE RII53-401. 2L72 4F RTA21EA 20040517000982004051700098CE 2004 5 17 59458 120040305A24359036102331 STARTER GEN BEECH 1900 1900D 1154162CE RIGHT INOPERATIVE A AMWAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 CE07138YV UE138 SHORTLY AFTER DEPARTING, THE RT GENERATOR FELL OFF-LINE. CREW DECIDED TO RETURN TO FIELD, LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED HALL EFFECT DEVINE. REPAIRED SENSE LINE ON LT STARTER/GENERATOR. OPS CK NORMAL. 2L72 4T RTA24CE 20040517001072004051700107CE 2004 5 17 GLBA20030562 120040212A2120 SMOKE BEECH 1900 1900D 1154162CE COCKPIT DETECTED A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM03240GL UE240 CREW SMELLED ELECTRICAL SMOKE IN COCKPIT, INSP ELECTRICAL RAN A/C FOUND NO DISCREPANCIES OPS CHECK FLIGHT SATISFACTORY 2L72 4T RTA24CE 20040517001112004051700111WP 2004 5 17 0380 120040217A5414UNKNOWN SKIN DOUG DC8 DC863F 302198FWP NR 2 PYLON CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23865F 7692219701 46088 VISUALLY DETECTED CRACK IN PREVIOUS DOUBLER LEFT WING LEADING EDGE AT NR 2 ENGINE PYLON CUTOUT. 2L74 4F 4A25 20040517001172004051700117 2004 5 17 GLBA20030566 420040218A34141303800057 INDICATOR BEECH 1900 1900D 1154162CE AIR SPEED SMOKE A GLBAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 NM03247GL363 UE247 NR 2 ASI STAYED AT ZERO & TOWER REPORTED OF SMOKE ON TAKE OFF ROLL, R&R NR 2 ASI GROUND RAN ACFT INSP ENG NO PROBLEMS NOTED 2L72 4T RTA24CE 20040517001252004051700125CE 2004 5 17 GLBA20030570 120040224A5270 WARNING LIGHT BEECH 1900 1900D 1154162CE AIRSTAIR DOOR ILLUMINATED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03201GL UE201 CABIN DOOR ANNUNCIATOR CAME ON,R&R AIRSTAIR DOOR FWD LATCH HANDLE SWITCH PN V3-10108 OPS CK GOOD 2L72 4T RTA24CE 20040517001262004051700126CE 2004 5 17 GLBA20030565 120040217A21301013840287 PRESSURE SWITCH BEECH 1900 1900D 1154162CE CABIN PRESSURE MALFUNCTIONED A GLBAO OTHER J WARNING INDICATION CLCLIMB 1 NM03220GL UE220 CABIN ALT HIGH ILLUMINATED, R&R CABIN ALT HIGH PRESS SWITCH PN 101-384028-7 2L72 4T RTA24CE 20040518000012004051800001NM 2004 5 18 USAA040120 120040324A5314 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US46553 23557 FOUND KEELBEAM CORRODED AND PITTING 1 INCH BY 4 INCH AREA, RT KEELBEAM LOWER SURFACE STATION 663.75 TO 727. INSTALLED REPAIR STRAP PER EA 78097. LEVEL 1 TASK NR C53-212-01. (M) 2L72 4F RTA16WE 20040518000022004051800002NM 2004 5 18 USAA040108 120040402A5330 SKIN BOEING757 757225 1384959NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU 22196 CLT - FOUND SKIN SCAB PATCH 9.25 INCH BY 9.75 INCH, STATION 1320-1340, S25L-S27L. DOUBLER REPAIR PER EA 65019B. (M) 2L72 4F RTA2NM 20040518000082004051800008NM 2004 5 18 USAA040106 120040409A5532 SKIN BOEING757 7572B7 1384964NM VERTICAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU 27199 PIT - FOUND VERTICAL STABILIZER SKIN WITH 6 INCH REPAIR, 15 INCHES AFT OF FSS 170. COMPOSITE LAY UP REPAIR PER SRM 51-70-10. (M) 2L72 4F RTA2NM 20040518000092004051800009NM 2004 5 18 USAA040118 120040410A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US52179 23312 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 933 STRINGER 24R. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040518000222004051800022WP 2004 5 18 GTIA040300 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-200 CENTER EDGE BROKE. COVER TORN CORE EXPOSED AND CORROSION ON INSERTS. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040518000312004051800031WP 2004 5 18 GTIA040295 120040319A5320 FITTING DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND AFT CARGO STATION 1117 LONGERON 28R DOOR BEAM END FITTING CORRODED. REMOVED CLIP FROM END FITTING. FABRICATED CLIP. INSTALLED CLIP. (M) 2L72 4F A6WE 20040518000352004051800035WP 2004 5 18 GTIA040302 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 150-160 RIGHT OUTBOARD COVERING TORN. FABRICATED NEW CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040518000472004051800047 2004 5 18 GLBA20030578 420040229A23001013800539 STATIC WICK BEECH 1900 1900D 1154162CE COMM SYSTEM DAMAGED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03247GL UE247 STATIC IN BOTH COMM'S BOTH NAV'S FAILED IN PRECIP, R&R STATIC WICKS PN 101-380053-9 2L72 4T RTA24CE 20040518000532004051800053CE 2004 5 18 0025 120040303A3230CR105 DIODE LEAR 35 35A 5170602CE MLG DISCONNECTED E CIEAO OTHER J WARNING INDICATION DEDESCENT 1 NM0349BE 15073 192 DURING DESCENT INTO DESTINATION AIRPORT, THE PILOT WAS UNABLE TO GET THE GEAR TO EXTEND. AFTER ATTEMPTING A COUPLE OF TIMES AND AFTER PULLING AND RESETING THE GEAR CONTROL CIRCUIT BREAKER, THE GEAR WAS EXTENDED USING THE EMERGENCY GEAR EXTENSION PROCEDURE AND THE GEAR EXTENDED AND A NORMAL LANDING WAS MADE. THE AIRCRAFT WAS JACKED AND THE GEAR SYSTEM WAS BLEED OF THE NITROGEN AND TROUBLE SHOOTING FOUND A DIODE IN THE COPILOT CIRCUIT BREAKER PANEL AREA, AT CONNECTION CR105, TO BE DISCONNECTED. THE DIODE WAS RESOLDERED TO ITS CONNECTOR. THE GEAR OPERATION WAS CHECKED PER THE LEAR JET MAINTENANCE MANUAL CHAPTER 32-41-00 AND CHECKED GOOD. 2L72 4F A10CE 20040518000552004051800055NE 2004 5 18 NACA20040014 220040304A8500R2800CB3 ENGINE DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 LEAKING A NACAE ENGINE SHUTDOWN RKJPARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION DEDESCENT 1 AL03993302232 2232 43576 P31943 NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND DOUBLE SHORTED SECONDARIES ON MOST CYLINDERS. REPLACED NR 2 ENGINE DUE TO BLOWER SEAL LEAKING. 2L74 4R4 R 6A3 5E8 20040518000632004051800063SO 2004 5 18 2004F00107 220040310A85006461401 STUD CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C505 GL CRANKCASE LOOSE G BIGABEA EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CLCLIMB 1 NM04114BH 340A1230 503082 020379 DURING CLIMB OUT, THE PILOT NOTICED THE RIGHT ENGINE OIL PRESSURE GAGE INDICATING A SIGNIFICANT INCREASE IN PRESSURE. WHEN THE RIGHT ENGINE STARTED TO RUN ROUGH THE ENGINE WAS SECURED AND THE PROPELLER WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURNED TO THE AIRPORT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEMS. AFTER THE RIGHT COWLING WAS REMOVED TO INVESTIGATE THE ROUGH RUNNING ENGINE, IT WAS FOUND THAT THE ENGINE HAD BLOWN THE NUMBER 4 CYLINDER OFF OF THE CRANKCASE, ALLOWING THE PISTON TO COCK IN THE CYLINDER BARREL AND THROWING THE NUMBER 4 ROD, DAMAGING THE CRANKCASE. THE ENGINE CANNOT BE ROTATED BY HAND. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20040518000662004051800066SW 2004 5 18 N406MA 120040218A7933MS280343 DETECTOR BELL 222 222B 1182124SW LYC LTS101LTS101750C1 41560NE NR 2 ENG OIL BROKEN E A1UAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE03406MA 47134 4711447162 WHILE ENROUTE TO A SCENE CALL, CLIMBING THROUGH 3800 FT EAST OF ROMNA, CA. I NOTICED NR 2 ENGINE OIL TEMP PEGGED ABOVE MAX. TEMP HAD BEEN NORMAL ON LAUNCH AND THROUGH THE FIRST 10 MIN. OF FLIGHT. ABORTED MISSION AND RETURNED TO BASE. DUE TO TERRAIN AND ABSENCE OF SECONDARY INDICATIONS, ELECTED TO KEEP NR 2 ENGINE RUNNING. REVIEWED POH AND MADE UNEVENTFUL MINIMUM POWER LANDING TO OUR USUAL TAXI WAY. NO EMERGENCY DECLARED WITH ATC. NO UNUSUAL NOISES, VIBRATION, OR SMELL. DURING TROUBLESHOOTING, FOUND NR 2 OIL TEMP BULB CAUSED INDICATION TO READ AT LEAST 40 DEGREES HIGH ALSO FOUND NR 2 BLOWER BEARINGS SEIZED AND SHAFT SHEARED. REPLACED TEMP BULB AND BLOWER. OPS CHECKED GOOD, RETURNED TO SERVICE. 1G72 3U3 U H9SW E5NE 20040518000672004051800067SO 2004 5 18 GLBA20030586 120040310A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MISINSTALLED A GLBAK NONE L NO TEST ININSP/MAINT 1 NM03297UX 120297 LT FWD OVER WING EMERGENCY LIGHT INOPERATIVE, FOUND WIRES MISINSTALLED, REWIRED OPS CK GOOD 2L72 4T RTA31SO 20040518000682004051800068NE 2004 5 18 N406MA0204 220040227A7297 WIRE BELL 222 222B 1182124SW LYC LTS101LTS101750C1 41560NE CHIP DETECTOR CHAFED E A1UAO OTHER J WARNING INDICATION NRNOT REPORTED 1 CE03406MA 47134 DURING FLIGHT TAIL ROTOR CAUTION LIGHT ILLUMINATED. RETURNED TO BASE. FOUND POWER WIRE TO CHIP DETECTOR WAS FOUND TO HAVE CHAFED THROUGH AND SHORTED. REPAIRED WIRE. 1G72 3U3 U H9SW E5NE 20040518000842004051800084CE 2004 5 18 GLBA20030590 120040314A2131 CONTROLLER BEECH 1900 1900D 1154162CE CABIN PRESSURE MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03254GL UE254 ACFT WILL NOT PRESSURIZE IN FLT. 2L72 4T RTA24CE 20040518000862004051800086WP 2004 5 18 2004000002 120040316A215020497511 ACM DOUG DC10 DC1030 3023501WP NR 1 FAILED A CNMAJA DUMP FUEL UNSCHED LANDING O OTHER CRCRUISE 1 SW07630AX 46596 LITTLE TO NO AIRFLOW FROM NR 1 PACK, LITTLE TO NO AIRFLOW FROM NR 2 PACK. NOTE: UNABLE TO HOLD PRESSURIZATION WITH BOTH NR 1 & 2 PACKS. REMOVED AND REPLACED NR 1 ACM. FOUND LOOSE BOLT ON NR 2 PACK TURBINE BYPASS VALVE. 2L73 4F A22WE 20040518000922004051800092GL 2004 5 18 2004000001 220040309A7261 SEAL DOUG DC10 DC1030 3023501WP GE CF6 CF650A 30018GL NR 2 ENGINE LEAKING A CNMAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 SW0759083 47926 NR 2 ENGINE OIL QUANITY STEADILY DECREASED DURING CRUISE. LOST 2.5 QTS IN 50 MINUTES. SHUTDOWN ENGINE TO PRESERVE OIL QTY. RESTARTED ENGINE AT ALT. FL 240, QTY HELD OK FOR APPROACH AND LANDING. FROM PREVIOUS ENGINE DRIVEN HYD PUMP REMOVAL AND BLOCKOUT FOUND SPLINE LOCKOUT TOOL SEAL DAMAGED. REPLACED SEAL LEAK CHECK GOOD 2L73 4F4 F A22WE E23EA 20040518000942004051800094CE 2004 5 18 0026 120040312A561010138402518 WINDSHIELD BEECH 200 B200 1152922CE COCKPIT CRACKED E CIEAO OTHER O OTHER CRCRUISE 1 NM03203LG1991 BB926 DURING CRUISE THE COPILOTS WINDSHIELD INNER PANE SHATTERED. NO DEBRIS FELL INTO THE CABIN OTHER THAN DUST. THE OUTER PANE STAYED IN TACT. THE PILOT DESENDED TO A LOWER ALTITUDE AS RECOMMANDED BY THE AIRCRAFT FLIGHT MANUAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. 1L72 4T A24CE 20040518001112004051800111CE 2004 5 18 GLBA20030594 120040321A77141303800445 INDICATOR BEECH 1900 1900D 1154162CE N1 FROZEN A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03154GL UE154 RT N1 INDICATOR SPIKED & FROZE AT 98 PERCENT, PREFORMED OPS CK FOUND NO DEFECTS SWAPPED GAUGES PN 130-380044-5 CND 2L72 4T RTA24CE 20040518001132004051800113WP 2004 5 18 IXXA0400018S 120040224A5330 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C-CHECK CORROSION WAS DETECTED ON RT WING OUTBOARD LEADING EDGE INNER SECTION UPPER SKIN SURFACE. MAINTENANCE REMOVED DAMAGED SKIN, FABRICATED DOUBLER, CLEANED, TREATED AND PRIMED AREA AT INNER FACE OF DOUBLER. MAINTENANCE THEN INSTALLED DOUBLER AND NEW FASTENERS IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL TEMPORARY REPAIR REVISION 57-102. 2L74 4F RT4A25 20040518001202004051800120CE 2004 5 18 ACE032304 120040322A2822 DIAPHRAGM BEECH 1900 1900C 1154161CE FUEL PUMP RUPTURED E YADAO OTHER K FLUID LOSS NRNOT REPORTED 1 AL03114AX 1384 B667 UC36 FOUND DIAPHRAGM LEAKING (RUPTURED) - THIS PUMP WAS BEING INSPECTED DUE TO AN ABORTED TAKEOFF AFTER ENGINE FLAME OUT. 1384 HOUR & 6 MONTHS AFTER INSTALL. 2L72 4T RTA24CE 20040518001252004051800125NM 2004 5 18 HNAA0400024 120040319A612078249050 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF7 NE PROPELLER INOPERATIVE A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07931HA 132 DURING CLIMB PROP AT 1050 PROP JUMPED BETWEEN 1020 & 1080 AIRCRAFT RETURNED TO FIELD, CAPT REPORTED THE PROP SYNC WAS ON AT THE TIME AND THEY DID NOT TURN IT OFF. R & R NR 2 PCU. 2H72 4T RTA13NM 6 CP7NE 20040518001272004051800127NM 2004 5 18 HNAA0400026 120040325A534785320798133SP SEAT TRACK DHAV DHC8 DHC8201 2809001NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07969HA 468 SEAT TRACK CORRODED JUST INBOARD OF PAX DOOR R & R SEAT TRACK IAW RD8-53-3074, RD8-53-2295,RD8-53-1102 2H72 4T RTA13NM 20040518001292004051800129 2004 5 18 GLBA20030596 420040324A2300 CONNECTOR BEECH 1900 1900D 1154162CE HEADSETS DIRTY A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03257GL UE257 NO SIDE TONE IN HEADSETS, CLEANED & ADJUSTED MIC JACKS OPS CK GOOD 2L72 4T RTA24CE 20040519000042004051900004SO 2004 5 19 RAIA00403015 120040317A801135059106 STARTER EMB 145 EMB145LR 3260212SO RT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03817HK9333 145058 5755-DCA- RIGHT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED RIGHT TURBINE STARTER. 2L72 4T RTT00011AT 20040519000142004051900014NM 2004 5 19 757BJ0009 120040319A5310 DOOR FRAME BOEING757 757236 1384971NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 NR 2 CARGO DOOR FRAME AFT WEB CRACKED AT NR 6 DOOR STOP FASTENER LOCATION. REPAIRED DAMAGE PER SRM 53-00-07. 2L72 4F RTA2NM 20040519000212004051900021CE 2004 5 19 DXTA200400270 120040318A3260 WARNING LIGHT CESSNA500 560CESSNA 2076750CE MLG FALSE ACTIVATIONE DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07366QS 5600466 UPON GEAR RETRACTION THE GEAR UNLOCKED LIGHT WOULD NOT EXTINGUISH, GEAR EXTENDED NORMALLY ON RECYCLE WITH 3 GREEN LIGHTS, ACCOMPLISHED AIR TURN BACK TO TEB. PERFORMED GEAR SWING AND FOUND GEAR UNSAFE LIGHT EXTINGUISHED WITH EVERY RETRACTION AND EXTENSION OF LANDING GEAR. SYSTEM OPERATES NORMAL AT THIS TIME, ALL WORK PERFORMED IAW CE560 MM. CHAPTER 7-10-00 & 32-01-00. 2L72 4F RTA22CE 20040519000292004051900029CE 2004 5 19 DXTA200400277 120040326A3260531762 SQUAT SWITCH CESSNA750 750 2076810CE NLG OUT OF ADJUST E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07960QS 7500160 AFTER TAKE OFF FROM BED AND ESTABLISHED A POSITIVE RATE OF CLIMB, SELECTED GEAR UP AND THE GREEN NOSE GEAR LIGHT REMAINED ILLUMINATED. PLACING GEAR SELECTOR TO THE EXTEND POSITION ALL THREE GREEN GEAR LIGHTS ILLUMINATED AND THE UNLOCKED LIGHTS EXTINGUISHED. THE GEAR SELECTOR COULD NOT BE BROUGHT OUT OF THE EXTEND POSITION, DIVERTED AIRCRAFT TO SWF. - TROUBLESHOT SYSTEM, ALL THREE GREEN LIGHTS ILLUMINATED AND THE UNLOCKED LIGHT EXTINGUISHED, CONFIRMED THE GEAR SELECTOR COULD NOT BE BROUGHT OUT OF THE EXTEND POSITION. FOUND NOSE GEAR SQUAT SWITCH OUT OF ADJUSTMENT, RIGGED NOSE SQUAT SWITCH PER CESSNA 750 MM CHAPTER 32-60-00, GROUND OPS CHECKED GOOD. 2L72 4J RTT00007WI 20040519000332004051900033NM 2004 5 19 PCAA0403185 120040326A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY FALSE INDICATIONA PCAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA13814EX1423554 318 REPORTED RECEIVING THE WARNING LIGHT FOR THE NR 1 BAGGAGE SMOKE DETECTOR.NO SMOKE OR FIRE PRESENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 DETECTOR AND OPERATIONAL CHECKS WERE GOOD. 2H72 4T RTA13NM 20040519000392004051900039NM 2004 5 19 0402001 120040217A2497 GROUND STUD BOEING737 737200 1384453NM BATTERY DETACHED A MJYAK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW07737TW 20257 BATTERY VOLTS BELOW MINIMUMS FOUND GROUND LUG DETACHED FROM FORMED SECTION REPAIRED FORMED SECTION IAW BOEING SRM 51-40-3 PG 5 FIG 1 SHEETS 1-5. 2L72 4F A16WE 20040519000502004051900050EU 2004 5 19 YENA200421 120040331A2750 APPU AIRBUS320 A320232 3930326EU TE FLAPS OUT OF ADJUST A YENAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA15536JB 1784 ON APPROACH FLIGHT CONTROL LOCKED - ALIGNMENT PROBLEM - SLATS 2 & FLAPS < 1. PERFORMED FLAP RIGGING IAW MM 27-54-00-501 AND ADJUSTED RT ASYMMENTRY POSITION PICKOFF UNIT (APPU )IAW MM 27-51-18-401. PERFORMED OPERATIONAL CHECK, CHECKS NORMAL. 2L72 4F RTA28NM 20040519000512004051900051CE 2004 5 19 X6PA200400003 120040325A5312511201144 BULKHEAD CESSNA402 402C 207590RCE FUSELAGE CRACKED E X6PAK NONE O OTHER ININSP/MAINT 1 SO33350RC15246 402C0469 BOTTOM CENTER OF BULKHEAD FOUND CRACKED AT THE REAR TIE DOWN HOOK ATTACH POINT. CRACK APPEARS TO ORIGINATE FROM OLD REPAIR. 1L72 3O A7CE 20040519000542004051900054NM 2004 5 19 EIA2004012 120040317A3350S1356B37 LIGHT BOEING747 747SR46 1384816NM CARGO DECK INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09478EV 21033 MAIN CARGO DECK EMERGENCY EXIT LIGHT GOES OUT AFTER 10 SECONDS. REPLACED LIGHT ASSY. 2L74 4F RTA20WE 20040519000622004051900062CE 2004 5 19 DXTA200400268 120040318A3241S289930 CIRCUIT BREAKER CESSNA500 560CESSNA 2076750CE ANTI SKID SYS TRIPPED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07302QS 5600402 APPROX 100 FT ABOVE TOUCHDOWN THE "POWER BRAKE LOW PRESS." AND "ANTISKID INOP." ANNUNCIATOR LIGHTS ILLUMINATED AND THE ANTI SKID CIRCUIT BREAKER POPPED. LANDING WAS UNEVENTFUL, USED BACKUP PNEUMATIC SYSTEM TO STOP AIRCRAFT. - RE-SET CIRCUIT BREAKER WITH NO SUBSEQUENT POPPING, INSPECTED LT CIRCUIT BREAKER PANEL WITH NO FAULTS NOTED. BLED BRAKE SYSTEM TWICE TO REMOVE ALL AIR IAW CESSNA 560 MM CHAPTER 32-42-00. OPS CHECK & LEAK CHECK GOOD, SERVICED PNEUMATIC GEAR BOTTLE IAW CESSNA 560 MM CHAPTER 12-13-01. 2L72 4F RTA22CE 20040519000632004051900063NM 2004 5 19 513NA0003 120040401A3246 BOLT BOEING757 7572T7 1384914NM WHEEL MISSING A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05513NA 23895 NR 7 TIRE ASEMBLY MISSING 3 BOLTS. REPLACED NR 7 MAIN TIRE PER MM 32-45-01. 2L72 4F RTA2NM 20040519000692004051900069SO 2004 5 19 RAIA00403029 120040331A301083552 TRANSDUCER EMB 145 EMB145 3260210SO ANIT ICE SYSTEM DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03820HK 145064 WING ANTI-ICE TEST FAILED. MAINTENANCE REMOVED AND REPLACED BURST TRANSDUCER. 2L72 4F RTT00011AT 20040519000772004051900077WP 2004 5 19 0400519933 120040325A5313 SPLICE DOUG DC9 DC931 3022065WP LONGERON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011334U 47280 DURING "M" CHECK FOUND CRACK IN LONGERON 30 SPLICE FITTING FROM BS 580 TO BS 604. REPAIRED PER EA 99-198614. 2L72 4F A6WE 20040519000792004051900079CE 2004 5 19 097041 120040406A261224412886 FIRE DETECTOR BEECH 1900 1900D 1154162CE RT ENGINE DAMAGED A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27124CJ UE24 IN CRUISE RT FIRE HANDLE ILLUMINATED FOR 4 SECONDS AND WENT OUT. REMOVED AND REPLACED RT ENGINE FIRE DETECTION CABLE IAW 26-10-01 OPS CHECKED GOOD 2L72 4T RTA24CE 20040519000802004051900080NE 2004 5 19 NACA20040016 220040405A7261 LINE BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE ENGINE LOOSE A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 AL03992AJ 562 19428 654023 NR 2 ENGINE SHUT DOWN DUE TO OIL QUANTITY AND PRESSURE WENT TO ZERO. FOUND NR 2 ENGINE OIL PRESSURE TRANSMITTER PRESSURE LINE LOOSE. REMOVED AND INSPECTED LINE, NO DEFECTS FOUND. RE-INSTALLED PRESSURE LINE. LEAK & OP CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040519000812004051900081NM 2004 5 19 P5CA0401067 120040403A3411856CC11 PITOT TUBE BOEING747 747236B 1384804NM FUSELAGE DAMAGED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23924FT 21730 AT DEPARTURE TIME, CAPT'S MAIN PITOT LIGHT STAYED ON WITH SWITCH IN ON POSITION. R&R CAPT'S PITOT PROBE. OPS AND LEAK CHECK OK PER MM 34-11-01. 2L74 4F A20WE 20040519000822004051900082 2004 5 19 P5CA0401065 420040331A3454G692503 CONTROL PANEL BOEING747 747341 13848AMNM VHF NAV SMOKE A P5CAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP23355MC 23395 SPARKS AND SMOKE CAME FROM BEHIND FO VOR ON LANDING. R & R NR 2 VHF CONTROL PANEL. 2L74 4F RTA20WE 20040519000862004051900086NM 2004 5 19 C1HA200485003 120040405A2780 FLAP BOEING727 7272S7 138407ZNM NR 4 KRUGER INOPERATIVE A C1HAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL15685CA 22492 NR 4 KRUGER FLAP WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT CURRENTLY IN HEAVY CHECK AND CORRECTIVE ACTION WILL FOLLOW WITH C CHECK FINDING AND RESOLUTION. 2L73 4F A3WE 20040519000872004051900087CE 2004 5 19 GLBA20030598 120040328A2797 WIRE BEECH 1900 1900D 1154162CE CONTROL YOKE BROKEN A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03154GL UE154 LOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOOD 2L72 4T RTA24CE 20040519000882004051900088EA 2004 5 19 HNAA0400032 120040328A531085320686101 DOOR FRAME DHAV DHC8 DHC8311 1386006EA PAX DOOR CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07330EN 274 LIP AT PAX DOOR ENTERANCE WAY IS CORRODED ENTIRE LENGTH OF FLANGE, R&R AIRSTAIR DOOR THRESHOLD 2H72 4T RTA13NM 20040519000902004051900090EA 2004 5 19 HNAA0400034 120040407A5610NP15790213 WINDOW DHAV DHC8 DHC8311 1386006EA COCKPIT CRACKED A HNAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA07337EN 284 CAPT'S LEFT WINDOW (SIDE) CRACKED IN FLIGHT R & R CAPT'S SIDE WINDOW, OPS CHECK GOOD 2H72 4T RTA13NM 20040519000912004051900091NM 2004 5 19 HNAA0400035 120040407A21507827906 ACM DHAV DHC8 DHC8102 2809003NM CABIN COOLING SEIZED A HNAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07912HA461911438 040 ACM SEIZES UP AND SMOKED UP CABIN 2H72 4T RTA13NM 20040519000922004051900092 2004 5 19 DXTA200400289 420040401A3460700549901 CDU CESSNA750 750 2076810CE NR 1 FMS FAILED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07924QS 7500124 DURING CRUISE AT FL430, NR 1 FMS WENT BLANK WITH RED FMS NR 1 DISPLAYED ON CAPTAIN’S MFD. ABOUT 30 MINUTES LATER A FAINT ODOR OF BURNED INSULATION NOTICED, ODOR STAYED CONSTANT FOR THE REST OF THE FLIGHT. REMOVED AND REPLACED NR 1 FMS CDU, OP-CHECK GOOD PER CESSNA 750 MM CHAPTER 34-60-01. 2L72 4J RTT00007WI 20040519000932004051900093NE 2004 5 19 NACA20040017 220040407A7421RHB32E SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 CYLINDER CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL032907F 35 533265 28737 NR 2 ENGINE SHUT DOWN DUE TO LOW COMPRESSION INDICATION ON NR 2 CYLINDER. REPLACED BOTH SPARK PLUGS ON NR 2 CYLINDER DUE TO CRACKED CERAMICS. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040519000942004051900094NM 2004 5 19 0400526306 120040403A3350 BULB BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK, FOUND THE RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21-41. REPLACED BULBS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040519000952004051900095NM 2004 5 19 0400536642 120040404A3350 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01642NW 21942 DURING LINE CHECK, FOUND 'E' ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040519000992004051900099 2004 5 19 251TR0006 420040302A2210 WARNING HORN BOEING737 737228 13844AGNM AUTO PILOT INOPERATIVE A PIDAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO05251TR 23792 AUTO PILOT DISCONNECT AURAL WARNING INOP. MECHANIC STATED THAT WHEN HE ARRIVED IN CONTROL CABIN, THE AURAL WARNING C/B WAS OUT. THE C/B WAS RESET AND AN OPERATIONAL CHECK OF THE AURAL WARNING PERFORMED SATISFACTORILY PER MM 22-11-01. THERE HAVE BEEN NO FURTHER WRITE-UPS RELATED TO AUTO PILOT DISCONNECT AURAL WARNING. 2L72 4F RTA16WE 20040519001012004051900101NM 2004 5 19 TSAA0449036 120040401A492038007021 APU BOEING737 73773A 1384606NM FAILED A TSAAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 WP13738AL147553380 28499 APU LOW OIL PRESSURE LIGHT CAME ON. FAULT 49-911007, INSPECTED APU, NO OIL IN TANK. ADDED 5 QTS. EVIDENCE OF OIL LEAK ON APU SHROUD. REMOVED AND REPLACED APU IAW M-715 AND CONFORMED WITH TASK CARDS 49-152-00-01, 49-040-00-01, AND 49-030-00-01. VERIFIED OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040519001032004051900103GL 2004 5 19 RAIA00403030 220040319A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03814HK 145046 311020 5622 - DEN - ATTCS NO MARGIN INDICATION NR 2 ENGINE. MAINTENANCE DEFERRED ATTCS PER MEL 73-22-02. SUBSEQUENTLY CLEARED DMI BY PERFORMING THRUST ASSURANCE RUN WITH NO MESSAGES NOTED. 2L72 4T4 FRTT00011ATTE6CH 20040519001042004051900104SO 2004 5 19 RAIA00403031 120040328A2120 FILTER EMB 145 EMB145 3260210SO AIR DIST DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03820HK 145064 5717 - STL - BLEED 2 OVER-TEMP MESSAGE. MAINTENANCE CLEANED FAN AIR VALVE FILTER. 2L72 4F RTT00011AT 20040519001052004051900105 2004 5 19 RAIA00404001 420040405A34180861DT5MOD1 VANE EMB 145 EMB145ER 3260211SO LT AOA FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03808HK10405 145157 AOA FAILURE ON TAKE OFF. MAINTENANCE REMOVED AND REPLACED LT AOA VANE. 2L72 4F RTT00011AT 20040519001062004051900106 2004 5 19 AIA00404002 420040406A3418 COMPUTER EMB 145 EMB145 3260210SO STALL WARNING MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03801HK 145053 3512 - LGA - DURING R/O ROLL GOT SPOILERS FAIL MESSAGE. MAINTENANCE RESET STALL PROTECTION COMPUTER AND OPS CHECKED OK. 2L72 4F RTT00011AT 20040519001082004051900108WP 2004 5 19 MWEA040050 120040409A53109915558191 ANGLE DOUG DC9 DC981 3022081WP DOOR FRAME SCRATCHED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 AFT CABIN DOOR JAMB AREA, LEFT SIDE OF AFT CABIN DOOR ANGLE HAS A DEEP SCRATCH IN RADIUS, IN BAY LONGERON 3. -- FABRICATED AND INSTALLED NEW ANGLE. 2L72 4F A6WE 20040519001092004051900109WP 2004 5 19 MWEA040051 120040409A5347593056675 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 NR 2 SEAT TRACK HAS AREA OF CORROSION IN CENTER CHANNEL AT STATION 1265. FABRICATED AND INSTALLED SEAT TRACK. 2L72 4F A6WE 20040519001122004051900112NM 2004 5 19 C8GA20040004 120040409A7933162BL704D INDICATOR BOEING727 7272A1 138407FNM PWA JT8 JT8D17 52049NE NR 2 ENGINE OIL FAILED A C8GABE EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO15287SC5217 21345 688275 FLT 1815 FROM KEWR TO KTOL. AT FL310 NR 2 ENGINE DISPLAYED EXCESSIVELY HIGH OIL TEMPERATURE, DESCENDED TO FL240 AND RAN ALL APPLICABLE CCIA CHECKLIST. IN-FLIGHT SHUT DOWN OF THE NR 2 ENGINE AS A PRECAUTIONARY, ADVISED ATC AND DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT AT FINAL DESTINATION IN TOL. AIRCRAFT WAS INSPECTED AND THE NR 2 ENGINE OIL TEMPERATURE INDICATOR WAS REPLACED. RAN NR 2 ENGINE AND THE OIL TEMPERATURE INDICATION SYSTEM CHECK NORMAL IAW MM 79-34-11 AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040519001132004051900113SO 2004 5 19 MASA200400181 120040402A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 EMERGENCY EXIT ROW OVERHEAD LIGHT SIGN INOP. MX SECURED WIRING AT LIGHT ASSY. OP CHECKS GOOD. NO PARTS USED 2L72 4T RTT00011AT 20040519001142004051900114SO 2004 5 19 MASA200400182 120040402A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 LT WING EMERGENCY EXIT SIGN INOP. MX SECURED WIRING AT LIGHT ASSY. OP CHECKS GOOD. NO PARTS USED 2L72 4T RTT00011AT 20040519001162004051900116SO 2004 5 19 MASA200400188 120040407A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DAMAGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07837MJ 145367 DCA CREW REPORTED EMERGENCY LIGHT AT ROW 12 O/H INOP ON FORWARD SIDE. MX REPAIRED WIRING AT CONNECTOR. OP CHECKS GOOD. NO PARTS USED 2L72 4T RTT00011AT 20040519001182004051900118CE 2004 5 19 DXTA200400292 120040410A2750 HANDLE CESSNA500 560CESSNA 2076750CE TE FLAPS BROKEN E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07293QS 5600293 FLAPS HANDLE STUCK AT FLAP 7 DEGREES POSITION, COULD NOT RETRACT FLAP AFTER TAKEOFF AND FLAP INDICATOR BROKEN. REPOSITION FLAP HANDLE AND RESECURED PLASTIC FLAP INDICATOR IAW CE560 MM CHAPTER 20-32; PERFORMED FUNCTIONAL CHECK OF FLAP SYSTEM IAW MM CHAPTER 27-51-00, OPS CHECK NORMAL. 2L72 4F RTA22CE 20040519001212004051900121WP 2004 5 19 MWEA040052 120040412A5320993061285 WEB DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LT HAND CUSP MEMBRANE FRAME STATION 1300 HAS A CRACK FROM LIGHTENING HOLE TO LIGHTENING HOLE APPROXIMATELY 4 INCHES. -- FABRICATED AND INSTALLED CUSP MEMBRANE. 2L72 4F A6WE 20040519001232004051900123NM 2004 5 19 N171QS04001 120040329A1420CA6628750 CONNECTOR BOEING737 7377BC 1384509NM CFMINTCFM567CFM567B2US 13802NE NR 2 IDG ARCED E BJ6AA UNSCHED LANDING BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CRCRUISE 1 NE03171QS1625 30572 877251 NR 2 IDG DROPPED OF LINE. APU USED TO SUPPLY POWER TO BUS. CREW ELECTED TO DIVERT TO PBI FOR REPAIRS. AIRCRAFT ON FAR 91 POSITIONING FLIGHT. REPLACED AFFECTED NR 2 IDG HARNESS AND CONNECTOR. OPS CHECKED SATISFACTORY. SENT HARNESS AND CONNECTOR TO THE BOEING COMPANY FOR ANALYSIS. BOEING ENGINEERING ANALYSIS CONCLUDED THAT THE ELECTRICAL CONTACT PIN AND SOCKET FAILED AS A RESULT OF HEAT GENERATED BETWEEN THE PINS AND SOCKETS. 2L72 4F4 FRTA16WE E2GL 20040519001242004051900124CE 2004 5 19 ESPA691D 120040404A3244178K431 TIRE LEAR 35 36LEAR 5170601CE MLG BLOWN E ESPAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO1171PG 013 ON TAKE-OFF ROLL THE RIGHT OUTBOARD TIRE EXPERIENCED A BLOW OUT. THE CREW ABORTED THE TAKE-OFF AND APPLIED MAXIMUM BRAKING. THE REMAINING 3 MAIN TIRE BLEW AS A RESULT OF THE HEAT GENERATED FROM THE BRAKING ACTION. 2L72 4F A10CE 20040519001252004051900125NM 2004 5 19 04016 120040411A2612 WARNING LIGHT BOEING747 747200F 1384866NM PWA JT9 JT9D7R4G2 52054NE NR 4 ENGINE ILLUMINATED A KCSAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23704CK 22299 725343 AFTER TAKEOFF AT 500 FT AGL, THE NR 4 ENGINE FIRE INDICATION ILLUMINATED AND THE FIRE BELL SOUNDED. PERFORMED APPROPRIATE CHECKLIST AND LANDED WITHOUT INCIDENT. 2L74 4F4 FRTA20WE E3NE 20040519001262004051900126CE 2004 5 19 GLBA20030608 120040409A561010138402522 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A GLBAO OTHER A FLAME/FIRE CRCRUISE 1 NM03210GL2718 UE210 FO'S WINDSHIELD CRACKED AND CAUGHT ON FIRE, R&R WINDSHIELD PN 101-384025-22 2L72 4T RTA24CE 20040519001292004051900129NM 2004 5 19 EIA2004017 120040402A5313 STRINGER BOEING747 747212B 1384886NM FUSLEAGE DENTED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 STRINGER 38R STA. 535 DENTED. REMOVED DAMAGED STR. FABBED AND INSTALLED NEW STRINGER PER B747 SRM 51-30-02,51-20-01, 51-20-01, & 51-10-02 2L74 4F A20WE 20040519001302004051900130NM 2004 5 19 EIA2004018 120040324A278065B8039033 DRIVE SHAFT BOEING747 747132 1384882NM LE SLATS SHEARED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 DURING WALKAROUND FOUND LE FLAPS NR 15 & 16 EXTENDED WITH DRIVE SHAFT SHEARED OFF. REMOVED AND REPLACED TORQUE TUBE IAW B747 MM 27-81-05. OPS CHECKED NORMAL. 2L74 4F A20WE 20040519001322004051900132NM 2004 5 19 250TR0029 120040409A3350 LAMP BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 LOW LEVEL EMERGENCY LIGHTS INOP AT ROWS 5DEF, 11DEF, 20DEF. RELAMPED AND OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040519001362004051900136NM 2004 5 19 0400543134 120040410A2121EV13454H FAN AIRBUSA319 A319114 3930350NM AVIONICS BAY FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01334NB6475 6475 1659 RECEIVED AVIONICS VENT BLOWER FAULT AND A PUFF OF SMOKE. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY AT LBF (NORTH PLATTE, NEBRASKA). FOUND AVIONICS BLOWER FAN SEIZED. SWAPPED WITH EXTRACT FAN AND APPLIED MEL PROVISIONS FOR EXTRACT FAN. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040519001372004051900137WP 2004 5 19 WRLA200414 120040411A7110NTL6012 COWL DOOR DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NACELLE MISSING A WRLAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO1114075 46922 517623 AIRCRAFT N14075 DEPT. FROM LIRN TO KNGU AT 2100Z WHILE AIRCRAFT CRUISING AFTER 5 HOURS AND 40 MIN.APPROX. 0240Z (ACCORDING TO THE CAPTAIN REPORT) THE ACFT. SHUDDERED AND BOUNCED FOR APPROX. 1/2 SECOND, THEN RETURNED TO STABLE FLIGHT, ACFT. CONTINUE TO KNGU AND HAD NORMAL LANDING AND NO CONTROL PROBLEMS. THE GROUND CREW NOTED THE NR 2 ENGINE COWL DOOR LT & RT SIDE WAS MISSING, SIGNIFICANT DAMAGE TO R/H INBOARD ELEVATOR WITH THE TAILCONE DISPLACED BUT ATTACHED. 2L73 4F4 F A22WE E23EA 20040519001392004051900139EU 2004 5 19 RAIA00404004 120040410A3260AIR140034 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG DEFECTIVE A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03569HK 41088 RED LIGHT IN GEAR HANDLE AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED NLG UP-LOCK SWITCH. 2L72 4T RTA41NM 20040519001402004051900140NM 2004 5 19 EIA2004020 120040412A3350 LIGHT BOEING747 747132 1384882NM EMERGENCY EXIT INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09479EV 19898 EMERGENCY EXIT LIGHT DOOR 5L INOP. REPLACED LIGHT ASSY OPS CHECKED NORMAL. 2L74 4F A20WE 20040519001412004051900141NM 2004 5 19 EIA2004021 120040412A3350 FUSE BOEING747 747132 1384882NM BATTERY FAILED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09479EV 19898 EMERGENCY LIGHT ON CEILING LT SIDE STA 2160 INOPERATIVE. REPLACED FUSE IN BATTERY. PACK OPS CHECKED GOOD IAW B747 MM 33-51-00 PAGE 101 2L74 4F A20WE 20040519001422004051900142NE 2004 5 19 NACA20040018 220040413A8550 ENGINE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4 LEAKING A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL0343872 533294 P34219 NR 4 ENGINE SHUT DOWN DUE TO OIL LOSS. REPLACED NR 4 ENGINE DUE TO INTERNAL FAILURE. 2L74 4R4 R A781 5E8 20040519001432004051900143CE 2004 5 19 DXTA200400275 120040325A3241MS2416602 RELAY CESSNA500 560CESSNA 2076750CE ANTI SKID SYS FAILED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07302QS 5600402 400 FT ABOVE TOUCHDOWN THE POWER BRAKE LOW PRESSURE AND ANTI-SKID INOP ANNUNCIATOR LIGHTS INOP LIGHTS ILLUMINATED AND THE ANTI-SKID CB POPPED, AND BRAKES BECME INEFFECTIVE - TESTED ANTI-SKID SYSTEM, BREAKER WOULD NOT TRIP, METERED ALL ANTI-SKID WIRES, FOUND NO SHORTS. INSPECTED ALL ANTI-SKID COMPONENTS, NO DEFECT NOTED, REPLACED SKID MOTOR CONTROL RELAY, SKID CONTROL RELAY, AND SKID CONTROL BREAKER IAW CESSNA 560 MM. CHAPTER 32-40-01. BLED BRAKE SYSTEM IAW CESSNA 560 MM CHAPTER 32-42-00, SERVICED EMERGENCY BRAKE BOTTLE IAW CESSNA 560 MM CHAPTER 12-13-01 BRAKE SYSTEM OPS CHECK GOOD. 2L72 4F RTA22CE 20040519001462004051900146CE 2004 5 19 DXTA200400280 120040328A3230 RELEASE CABLE CESSNA750 750 2076810CE MLG DAMAGED E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 GL07989QS 7500089 CLIMBING THROUGH FL250, CREW HEARD A LOUD THUMP FOLLOWED BY A LANDING GEAR UNLOCK LIGHT INDICATION. DURING DESCENT THROUGH 4000 FT, HEARD A THUMP FOLLOWED BY THE “UNLOCK” LIGHT GOING OUT. FOLLOWED CHECKLIST TO LOWER AND BLOW DOWN GEARS, HAD NORMAL GEAR INDICATIONS 3 GREEN AND NO RED, AIRCRAFT LANDED WITHOUT INCIDENTS. TROUBLESHOT GEAR SYSTEM AND FOUND EMERGENCY GEAR UP-LOCK RELEASE CABLE TENSION TOO TIGHT. RE-RIGGED UP-LOCK EMERGENCY GEAR CABLE TENSIONS AND PERFORMED EMERGENCY GEAR UP-LOCK RELEASE IAW CESSNA 750 MM CHAPTER 32-30-05 FOR MAIN GEAR AND 33-70-06 FOR NOSE GEAR. SERVICED PNEUMATIC BOTTLE IAW CESSNA 750 MM CHAPTER 12-19-36, OPERATIONAL CHECKED GOOD. 2L72 4J RTT00007WI 20040519001502004051900150NM 2004 5 19 F3LA200400042 120040414A532065529103 REVEAL BOEING737 73736E 138443ANM DOOR FRAME CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED INBD EDGE OF R1 DOOR LOWER FWD REVEAL CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-15. REPLACED REVEAL PER SRM 51-40-2 AND 51-10-2. 2L72 4F RTA16WE 20040519001512004051900151NM 2004 5 19 371PA0042 120040414A3411106145818 PROBE BOEING737 737306 13844BGNM PITOT STATIC SYSDAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 REFERENCE PREVIOUS HISTORY OF MACH TRIM FAULTS AT .77 MACH. REPLACED UPPER RIGHT PITOT/STATIC PROBE PER MM 34-11-11, ALSO RIGGED NEUTRAL SHIFT SENSOR PER MM 22-11-14 AND RIGGED ELEVATOR POSTIONN SENSOR. SYSTEMS CHECK GOOD PER LAND VERIFY SYSTEM TEST. 2L72 4F RTA16NE 20040519001522004051900152NM 2004 5 19 250TR0030 120040404A3350 POWER SUPPLY BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST NRNOT REPORTED 1 SO05250TR 22597 EMERGENCY PATH LIGHTING INOP. REPLACED POWER SUPPLY. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040519001552004051900155 2004 5 19 C1HA200476002 420040413A3432 GLIDE SLOPE BOEING727 727225 1384077NM BOTH ERRATIC A C1HAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL15817EA 22554 BOTH GLIDE SLOPES ERRATIC CAUSING GO-AROUND. SUSPECT GROUND PROBLEM. PERFORMED TEST ON BOTH ILS SYSTEMS. NO DEFECT NOTED IAW MM 34-31-00. 2L73 4F A3WE 20040519001572004051900157NM 2004 5 19 PCAA0404188 120040409A335082410162001 CONTROL BOX DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT MALFUNCTIONED A PCAAO OTHER N FALSE WARNING CRCRUISE 1 EA13817EX 191 REPORTED EMERGENCY LIGHTS COMING ON AND NOT EXTIGUISHING. LIGHTS WERE REPORTED AS CYCLING ON AND OFF. FOR TROUBLESHOOTING MAINTENANCE REPLACED BATTERY POWER PACKS, NO FIX. THE EMERGENCY LIGHT CONTROL BOX WAS REPLACED AND SYSTEM CHECK GOOD.AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001622004051900162NM 2004 5 19 F3LA200400045 120040415A5320 SUPPORT BOEING737 73736E 138443ANM STA 990 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON GALLEY SUPPORT ZEE AT STA 990, LBL 45 TO LBL 35. FABRICATED AND INSTALLED REPLACEMENT SUPPORT PER SRM 51-40-02, 51-30-02 AND 51-30-01. 2L72 4F RTA16WE 20040519001632004051900163EU 2004 5 19 RAIA00404005 120040407A2910 LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM CRACKED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03572HK 41091 LOST HYDRAULIC PRESSURE AFTER TAKEOFF. MAINTENANCE FOUND BRAKE IN HYDRAULIC TUBE AND SWAGED TUBE. 2L72 4T RTA41NM 20040519001652004051900165 2004 5 19 P9RA20040011 420040417A2565D30656126 SLIDE BOEING757 757236 1384971NM R4 DOOR DEPLOYED A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO11521NA 25592 AIRCRAFT OVERNIGHT IN JFK. MAINTENANCE DISCOVERED R4 SLIDE DEPLOYED. EXACT CAUSE NOT KNOWN. SUSPECT OVERNIGHT CLEANING/CATERING CREW. REMOVED AND REPLACED SLIDE. 2L72 4F RTA2NM 20040519001662004051900166NM 2004 5 19 F3LA200400044 120040415A5320 SILL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L2 MOP SILL AT DOOR OPENING. REMOVED MOP SILL, LOCATED AND DRILLED HOLES, AND INSTALLED PER SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20040519001682004051900168NM 2004 5 19 513NA0005 120040415A1430 BOLT BOEING757 7572T7 1384914NM WHEEL MISSING A PIDAK NONE O OTHER ININSP/MAINT 1 SO05513NA 23895 THREE TIE BOLTS MISSING ON THE NR 5 MAIN WHEEL ASSEMBLY. REPLACED LEFT OUTBOARD TIRE ASSEMBLY PER MM 32-45-01. 2L72 4F RTA2NM 20040519001702004051900170NM 2004 5 19 QXEA200400269 120040414A3350 LENS BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 LENS LOOSE ON CEILING EMERGENCY LIGHT AT ROW 13. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001712004051900171NM 2004 5 19 QXEA200400270 120040418A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09360PH 515 ON FLIGHT 2193 FORWARD EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED FORWARD SECTION OF AISLE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT REUTNED TO SERVICE. 2H72 4T RTA13NM 20040519001722004051900172NM 2004 5 19 QXEA200400272 120040418A3010 BOOT BOMBDRDHC8 DHC8401 1390041NM ZONE 500 INOPERATIVE A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09403QX 4037 ON FLIGHT 2348 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED DURING DESCENT IN ICING CONDITIONS. RAN CHECKLIST AND OBSERVED SECOND PANEL FROM LT WINGTIP DID NOT INFLATE AND RIGHT SIDE PRESSURE 10-12 PSI. GROUND RAN AIRCRAFT, OPERATED BOOTS THROUGH 3 CYCLES. DE-ICE PRESSURE AND BOOTS NORMAL. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001732004051900173CE 2004 5 19 DXTA200400290 120040406A801135059723 STARTER CESSNA750 750 2076810CE ENGINE FAILED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07951QS2335 7500151 AFTER TAKE-OFF FROM TEB, AT 1500 FT LEFT ENGINE FIRE INDICATION CAME ON, PULLED LEFT THROTTLE BACK AND INDICATION IMMEDIATELY EXTINGUISHED. DECLARED EMERGENCY AND LANDED SAFELY. – INITIAL INSPECTION NOTICED THE LT ENGINE COWLING HAS HEAT DAMAGE WITH A DELAMINATED AREA ABOUT 12 INCHES WIDE, ALSO FOUND BLACK SOOT INSIDE OF COWLINGS. FURTHER INVESTIGATION FOUND THE AIR STARTER DID NOT DISENGAGE AND APPEARED TO BE ON FIRE. REMOVED AIR TURBINE STARTER AND INSTALLED REPAIRED UNIT SERVICED WITH MOBIL JET II IAW CESSNA 750 MM CHAPTER 80-10-00 OPS AND LEAK CHECK GOOD. PERFORMED ONE TIME FERRY FLIGHT TO ICT FOR ENGINE CHANGE. 2L72 4J RTT00007WI 20040519001742004051900174NM 2004 5 19 F3LA200400046 120040308A5320 SUPPORT BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED LT AFT GALLEY WALL SUPPORT CORRODED AT STA 989, LBL 44. REPLACED SUPPORT PER SOPM 20-41-02 AND SRM 51-40-02. 2L72 4F RTA16WE 20040519001752004051900175EA 2004 5 19 QXEA200400266 120040413A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PASSENGER DOOR INNER SKIN NEXT TO LOWER FORWARD LATCH CHAFE DAMAGE FROM UPPER FORWARD DOOR SOP. REPAIRED IAW CRJ SRM 52-11-01-101-AC1. 2L72 4F RTA21EA 20040519001762004051900176EA 2004 5 19 QXEA200400267 120040413A5230 DEFLECTOR CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR BENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 PDX - FORWARD BAG DOOR WIND DEFLECTOR ATTACHED TO EXTERIOR SKIN IS BENT OUTWARD INTO SLIP STREAM, WITH DOOR CLOSED. REPLACED DEFLECTOR IAW CRJ 700 SRM 51-42-06 2L72 4F RTA21EA 20040519001782004051900178NM 2004 5 19 PCAA0404192 120040417A521085210116003 HANDLE DHAV DHC8 DHC8102 2809003NM CARGO DOOR BENT A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13835EX 289 REPORTED THAT THE OUTSIDE AIRSTAIR DOOR HANDLE WAS BENT AND WOULD NOT ALLOW THE DOOR TO BE CLOSED. MAINTENANCE REOMVED AND REPLACED THE HANDLE AS REQUIRED AND THE DOOR WAS RIGGED AS NEEDED. SYSTEM OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001802004051900180NM 2004 5 19 PCAA0404194 120040419A21607786971 VALVE DHAV DHC8 DHC8102 2809003NM CABIN TEMP FAULTY A PCAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA13845EX2733910959 344 RETURNED TO FIELD DUE TO ENGINE BLEEDS CAUSING HOT AIR TO ENTER THE AIRCRAFT REGARDLESS OF ENVIROMENTAL SETTINGS. MAINTENANCE REMOVED AND REPLACED THE TEMPERATURE TRIM VALVE. SYSTEM OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETUNED TO SERVICE. 2H72 4T RTA13NM 20040519001832004051900183NM 2004 5 19 TSAA0436037 120040414A36001074925 REGULATOR BOEING737 73776N 13844CHNM NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13746AL12129 29905 NR 2 ENGINE BLEED GIVES NO DUCT PRESSURE WITH ISOLATION VALVE IN AUTO OR CLOSED. RETURNED TO DEPARTURE AIRPORT, EXECUTED LOW SINK RATE LANDING. REMOVED AND REPLACED NR 2 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03-4. ENGINE NR 2 BLEED SYSTEM OPS CHECKS NORMAL. IAW MAINTENANCE CONTROL HNL PERFORM PRECAUTIONARY CHANGE OF WIRE HARNESS MW0311, REF: 737NG FTD-36-00001. REMOVED AND REPLACED MW0311 WIRE HARNESS IAW AMM 73-21-06-4. FADEC SYSTEM TEST PERFORMED IAW AMM 73-21-00-5. SYSTEM PASSED TEST. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040519001852004051900185NM 2004 5 19 F3LA200400048 120040419A5320 SUPPORT BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON GALLEY SUPPORT ZEE AT STA 990, LBL 35-45. REPLACED GALLEY SUPPORT ZEE PER SRM 51-40-2. 2L72 4F RTA16WE 20040519001862004051900186NM 2004 5 19 F3LA200400049 120040419A5320 FLOOR SUPPORT BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT SEGMENT BETWEEN STA 967 AND STA 986, LBL 16. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT SEGMENT PER SRM 51-10-02, 53-60-51, 51-20-01, 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA16WE 20040519001872004051900187NM 2004 5 19 PCAA0404195 120040419A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY FALSE ACTIVATIONA PCAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA13814EX768 768 318 FLIGHT NR 3763 REPORTED THE SMOKE WARNING LIGHT ILLUMINATING WHILE GROUND HANDLING. NO SMOKE WAS PRESENT FROM THE BAGGAGE COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 SMOKE DETECTOR IN THE BAGGAGE COMPARTMENT AND OPERATIONAL TEST THE SYSTEM. ALL CHECKS GOOD. 2H72 4T RTA13NM 20040519001882004051900188EU 2004 5 19 0400563306 120040418A3150 WARNING LIGHT AIRBUS330 A330323 3930335EU COCKPIT FALSE ACTIVATIONA NWAAO OTHER N FALSE WARNING CRCRUISE 1 GL01806NW 00578 DURING CRUISE, RECEIVED MASTER CAUTION AND MOMENTARY ECAM WARNINGS FOR SMOKE IN THE IN-FLIGHT ENTERTAINMENT BAY, AFT CARGO COMPARTMENT, AND AVIONICS VENT. WARNINGS CLEARED WITHOUT CREW ACTION AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RESET THE PASSENGER SYSTEM PUSH BUTTON. BITE TEST OF SDCU GOOD. 2L72 4F RTA46NM 20040519001892004051900189NM 2004 5 19 0400576301 120040417A3350 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51-63JK. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040519001902004051900190NM 2004 5 19 HNAA0400040 120040420A5280 DOOR DHAV DHC8 DHC8102 2809003NM NLG OUT OF ADJUST A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07975HA 176 NLG DOOR AMBER C/L ILLUMINATED AFTER GEAR RETRACTED, ADJUSTED NOSE GEAR DOOR PROXIMITY SWITCH IAW AC MM PERFORMED PSEU. GROUND OPS CHECK, OPS CHECK GOOD. 2H72 4T RTA13NM 20040517000892004051700089WP 2004 5 17 IXXA0400016O 120040318A3260 UPLOCK DOUG DC8 DC871F 302199DWP MLG CORRODED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11821BX847901893 45811 DURING UPLATCH CHECK AFTER TAKE OFF, GEAR DOORS AND GEAR UNSAFE LIGHTS CAME ON. CREW PERFORMED UNSATISFACTORY UPLATCH CHECK (WARNING LIGHTS ON) CHECK WAS STILL UNSATISFACTORY. CREW RETURNED AIRCRAFT AND LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE TROUBLESHOT LANDING GEAR EXTENSION/ RETRACTION IN ENTIRETY. FOUND RT MAIN LANDING GEAR UPLATCH MECHANISM CORRODED. MAINTENANCE CLEANED THE MECHANISM ALONG WITH THE ATTACHING PARTS AND JACKED THE AIRCRAFT IAW ALL APPLICABLE MANUALS. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040517001012004051700101NE 2004 5 17 WRLA200409 220040206A7250 TURBINE BLADES DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 1 ENGINE FAILED A WRLAJA DUMP FUEL UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO11352WL 47838 517423 NR 1 ENGINE COMPRESSOR STALLED / FAILED AT A/C ROTATION COMPLETED EMERGENCY & ABNORMAL CHECK LISTS. REMOVED AND REPLACED ENGINE ASSY. 2L73 4F4 F A22WE E23EA 20040517001022004051700102NE 2004 5 17 NACA20040009 220040206A7421RHB32E SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE FOULED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL03779TA99 99 45529 P34011 NR 3 ENGINE SHUT DOWN DUE TO NR 14 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED SPARK PLUGS, SHORT LEADS AND RESET VALVE CLEARANCES. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040517001032004051700103NM 2004 5 17 NACA20040010 120040206A2750BACB10ET04 BEARING BOEING727 72723 1384004NM TE FLAPS SEIZED A NACAJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AL03992AJ 19428 OUTBOARD FLAPS STUCK AT 3.5 DEGREES DURING FLAP RETRACTION. REPLACED BEARINGS IN RIGHT HAND OUTBOARD SEQUENCING CARRIAGE, SEQUENCING TOGGLES. 2L73 4F A3WE 20040517001232004051700123CE 2004 5 17 0409 120040225A3220 WARNING LIGHT LEAR 35 35A 5170602CE MLG INOPERATIVE E BSYAO OTHER J WARNING INDICATION APAPPROACH 1 GL0781FR 081 GOING INTO ATL HAD NO NOSE GEAR DOWN AND LOCK LIGHT LANDED NO PROBLEM. 2L72 4F A10CE 20040517001272004051700127 2004 5 17 58644 420040206A2230130909B22 SOLENOID BEECH 1900 1900D 1154162CE PROP WORN A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07165YV UE165 AFTER ARRIVAL TO PIT ON FLIGHT 5528. RIGHT PROP WENT INTO GROUND FINE. CORRECTIVE ACTION TAKEN R/R LOW PITCH SOLENOID CLEVIS HARDWARE RIGGED. 2L72 4T RTA24CE 20040517001282004051700128CE 2004 5 17 58728 120040210A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS STUCK A AMWAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE07178YV UE178 AFTER TAKEOFF FLAPS STUCK AT A PLACE IN BETWEEN 17 DEGREES & 34 DEGREES. CREW THEN DECIDED TO RETURN TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENTS. CLEANED LT / RT SPLIT FLAP SWITCHES OPS CK NORMAL. 2L72 4T RTA24CE 20040517001322004051700132EA 2004 5 17 UIA9307 120040227A561017180003 WINDOW DHAV DHC8 DHC8311 1386006EA COCKPIT CRACKED Z B EMER. DESCENT O OTHER CRCRUISE 1 TW0015223 404 IN FILGHT,FILGHT COMPARTMENT CAPTAIN SIDE WINDOW CRACK.A/C LANDING AFTER IAW M/M 56-10-16 REPLACED CAPTAIN SIDE WINDOW AND IAW M/M 30-41-00 OPERATIONAL TEST NORMAL. 2H72 4T RTA13NM 20040518000142004051800014EA 2004 5 18 REXA04007 120040405A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA LT MLG FAILED A REXAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SO258837B 7783 LEFT MAIN GEAR FAILED TO EXTEND WHEN GEAR SELECTED DOWN. EMERGENCY DECLARED, QRH PROCEDUERS FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED MAIN LANDING GAR PRIORITY VALVE IAW AMM 32-32-15. (M) 2L72 4F RTA21EA 20040518000162004051800016NM 2004 5 18 USAA040116 120040407A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU50349 23551 CLT - FOUND SKIN CRACKED .700 INCH, 3 INCHES AFT OF FS 727D ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040518000182004051800018 2004 5 18 USAABB04038 420040419A2565D30656126 SLIDE BOEING757 7572B7 1384964NM R4 DOOR OUT OF ADJUST A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 CLT - THE R4 DOOR EVACUATION SLIDE WILL NOT ARM. MAINTENANCE READJUSTED THE SLIDE AND LUBED THE GIRT BAR. (M) 2L72 4F RTA2NM 20040518000262004051800026WP 2004 5 18 GTIA040336 120040425A3350 SIGN DOUG DC9 DC983 3022083WP AFT GALLEY DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FLL - FOUND AFT GALLEY EXIT SIGN FELL OFF WALL. RESECURED EXIT SIGN. (M) 2L72 4F RTA6WE 20040518000362004051800036WP 2004 5 18 GTIA040301 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 160-180 RIGHT INBOARD NO EDGE FILLER AND INSERTS CORRODED. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040518000372004051800037WP 2004 5 18 GTIA0040297 120040310A5313F LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND MID CARGO FS 769 L28L, LONGERON AND ATTACHED HARDWARE CORRODED. FABRICATED LONGERON REPAIR CHANNEL. INSTALLED NEW LONGERON. SUPPORT CHANNEL. (M) 2L72 4F A6WE 20040518000392004051800039WP 2004 5 18 GTIA040340 120040422A2810 VENT DOUG DC9 DC983 3022083WP RT WING UNSECURE A GTIAK NONE WK INADEQUATE Q C FLUID LOSS ININSP/MAINT 1 GL23832NK 49618 FOUND RIGHT OUTBOARD WING LEAKING FUEL FROM WEEP HOLE. FOUND FASTENER TO VENT PORT NOT PROPERLY SECURED. (M) 2L72 4F RTA6WE 20040518000402004051800040NM 2004 5 18 2004F00105 120040212A2621 INDICATOR BOEING737 7377AV 1384506NM GE CFM56 CFM56* 13802NE FIRE BOTTLE FALSE INDICATIONB K NONE O OTHER ININSP/MAINT 1 EA17889NC1085 29621EL 30070 REMOVED FIRE BOTTLE AND SENT TO REPAIR STATION FOR HYDROSTATIC RETEST,FILL AND LEAK CHECK. UPON RETURN OF BOTTLE REINSTALLED AND PERFORMED INSTALLATION TEST PER BOEING CARD NO.26-350-00-00 OPS CHECK GOOD. APPROXIMATELY ONE WEEK LATER NOTICED CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. INSPECTION OF BOTTLE SHOWED CONTENTS OF BOTTLE HAD NOT BEEN DISCHARGED. THIS PROBLEM WAS NOTICED ON TWO OTHER AIRCRAFT. 2L72 4F4 FRTA16WE E2GL 20040518000422004051800042NE 2004 5 18 NAFA20040001 220040228A853033641 PUSHROD PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE CYLINDER BENT I N32BE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS APAPPROACH 1 AL017780B1544 1544 227101 45372 NK510101 NR 3 ENGINE PRECAUTIONARY SHUT DOWN DUE TO NR 3 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED BOTH INTAKE AND EXHAUST PUSH RODS AND ADJUSTED VALVES. OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20040518000452004051800045NE 2004 5 18 NACA20040013 220040228A726131359407200335 FITTING BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE NR 2 ENGINE LEAKING A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03992AJ 19428 654023 NR 2 ENGINE SHUT DOWN DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY. REPLACED NR 2 ENGINE OIL LINE FITTING AT LT SIDE OF GEARBOX. INSPECTED NR 2 ENGINE CHIP DETECTORS AND MAIN OIL SCREEN. OP AND LEAK CHECK GOOD. 2L73 4F4 F A3WE E2EA 20040518000582004051800058CE 2004 5 18 GLBA20030579 120040301A5270 WARNING SYSTEM BEECH 1900 1900D 1154162CE CARGO DOOR ILLUMINATED A GLBAO OTHER N FALSE WARNING CRCRUISE 1 NM03202UX UE202 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLT, ADJUSTED DOOR AJAR SW. 2L72 4T RTA24CE 20040518000822004051800082NM 2004 5 18 EIA2004011 120040305A5410 SHIELD BOEING747 747SR46 1384816NM NR 4 PYLON TORN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 NR 4 ENGINE LOWER I/B PYLON SKIRT FIRE SHEILD WORN THROUGH FROM NAC STA. 180.00 TO NAC STA. 265.94. NR 4 ENG LWR I/B SKIN REPAIRED PER SRM 54-30-03 FIG 35 & 36 PG 111-118. 2L74 4F RTA20WE 20040518000852004051800085CE 2004 5 18 GLBA20030591 120040314A3230 MOTOR BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03257GL UE257 BOTH LOAD METER PEG WHEN GEAR MOTOR CYCLES WITH GEAR UP, PENDING CORRECTIVE ACTION. 2L72 4T RTA24CE 20040518000882004051800088SO 2004 5 18 4008 120040317A81204091709001 TURBOCHARGER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LT ENGINE SMOKE E BSYAA UNSCHED LANDING RB PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL0735871 318052123 L861761A DJ7998 LOST LEFT TURBO AFTER DEPARTURE. NOTIFIED DEPARTURE OF ENGINE PROBLEM, RETURNED TO (SDF) HAD SMOKECOMING OUT OF TURBINE. REMOVED AND REPLACED TURBO CHARGER. 1L72 3O3 O A20SO E14EA 5 CP33EA 20040518001182004051800118NM 2004 5 18 PCAA0403184 120040319A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM NR 1 INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13814EX6209 1246 318 IN SYRACUSE REPORTED THE NR 1 SMOKE DETECTOR AS BEING INOP DURING TEST. MAINTENANCE REMOVED AND REPLACED THE DETECTOR AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040518001262004051800126NM 2004 5 18 HNAA0400027 120040325A54148541280 PANEL DHAV DHC8 DHC8201 2809001NM NR 1 NACELLE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07969HA 468 NR 1 NACELLE REAR DECK UNDER FINGERNAIL HAS SURFACE CORROSION, R & R REAR DECK 2H72 4T RTA13NM 20040518001282004051800128CE 2004 5 18 GLBA20030595 120040323A77003053995CL10 TRIM STICK BEECH 1900 1900D 1154162CE NR 1 ENGINE MALFUNCTIONED A GLBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM03153GL UE153 NR 1 ENG WON'T MAKE TAKEOFF POWER, R & R TRIM STICK PN 3053995CL10. 2L72 4T RTA24CE 20040518001302004051800130NM 2004 5 18 2004F00095 120040325A3246313061 WHEEL BOEING727 727 UTILSYSNM MLG CRACKED B K NONE O OTHER ININSP/MAINT 1 SO25495 4994 333 495 RETURNED, TO REPAIR SHOP, WHEEL/ TIRE ASSY REMOVED FOR LOSS OF TIRE PRESSURE ,CAUSED BY SEVERE CRACK TO OUTBOARD WHEEL HALF.(REURNING FRACTURED PART TO MFG. FOR ANALYSIS) 2L73 4J RTA3WE 20040518001322004051800132NM 2004 5 18 2004F00096 120040325A324626094712 WHEEL DOUG MD11 MD11F 3023600NM MLG FRACTURED B K NONE O OTHER ININSP/MAINT 1 SO25584 584 WHEEL/ BRAKE ASSEMBLY RETURNED TO SHOP SEIZED, FOUND THAT 11 WHEEL ROTOR DRIVE KEYS WERE FRACTURED (SENDING DRIVE KEYS 2609731 TO MFG. FOR ANALYSIS) 2L73 4F RTA22WE 20040519000022004051900002SO 2004 5 19 RAIA00403010 120040315A801135059106 STARTER EMB 145 EMB145 3260210SO NR 1 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03806HK10914 145112 LT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AIR TURBINE STARTER. 2L72 4F RTT00011AT 20040519000062004051900006SO 2004 5 19 RAIA00403018 120040321A28102930003102 VALVE EMB 145 EMB145ER 3260211SO FUEL SYSTEM LEAKING A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03827HK10511 145021 5642 - STL - TOWER REPORTED FUEL LEAKING FROM AIRCRAFT. MAINTENANCE REMOVED AND REPLACED DE-FUEL SHUTOFF VALVE. 2L72 4F RTT00011AT 20040519000132004051900013 2004 5 19 249TR0024 420040303A2565 BOTTLE BOEING737 7372K5 138448XNM ESCAPE SLIDE LOW A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 DURING A-CHECK FOUND L-1 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED L-1 DOOR SLIDE WITH SERVICEABLE UNIT PER MM 25-61-311. 2L72 4F RTA16WE 20040519000272004051900027 2004 5 19 RAIA00403024 420040325A34257003110901 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03569HK171703951 41088 5534 - STL - FO`S EHSI WENT BLANK. MAINTENANCE REMOVED AND REPLACED FOS EHSI. 2L72 4T RTA41NM 20040519000312004051900031NM 2004 5 19 583CC0003 120040324A33501000677 LIGHT BOEING737 737291 138448WNM COCKPIT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05583CC 21069 COCKPIT EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY PER MM 33-51-101 & OPS CHECKS NORMAL. 2L72 4F A16WE 20040519000322004051900032NM 2004 5 19 HNAA0400028 120040329A61207895431 BULKHEAD HAMSTD DHAV DHC8 DHC8201 2809001NM HAMSTD14SF 14SF23 NE PROP ASSY CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07997HA1049210492 980513 507 980515 DURING THE MAJOR INSPECTION OF PROPELLER ACTUATOR PARTS, THE PISTON BULKHEAD WAS FOUND CRACKED DURING FLUORSCENT PENNENTRANT INSPECTION. THIS HAS BEEN A COMMON FIND WITH THIS PART. 2H72 4T RTA13NM 6 CP7NE 20040519000342004051900034NM 2004 5 19 HNAA0400029 120040327A3260 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM MLG MALFUNCTIONED A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07906HA 9 AFTER TAKEOFF NLG RED LIGHT TOOK LONGER TO EXTINGUISH THAN NORMAL. THEN CYCLED ON AND OFF SEVERAL TIMES WITH ASSOCIATED THUMP FROM NLG AREA. DOOR LITES DID NOT ILLUMINATE. CHECKED PSEU FOR FAULTS NONE FOUND CHECKED UPLOCK SENSOR NO FAULTS RERACKED PSEU AND PERFORMED SYSTEM TEST CHECKS GOOD. PERFORMED FLIGHT TEST OPS CHECK GOOD. 2H72 4T RTA13NM 20040519000472004051900047CE 2004 5 19 DXTA200400283 120040329A2910 LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL07603QS 5605203 UPON GEAR RETRACTION SEVERAL LOUD BANGS WERE HEARD AND FELT, GEAR LIGHTS EXTINGUISHED, HYDRAULIC PRESSURE LIGHT STARTED FLASHING. PULLED C/B AND ANOTHER BANG HEARD AND FELT ALONG WITH RED GEAR UNSAFE LIGHT, RESET C/B AND GEAR EXTENDED NORMALLY. - PERFORMED 15 FAULT FREE GEAR SWING PER CESSNA 560XL MM CHAPTER 32-01-00, NO AIR NOTED IN RETURN SIGHT OF HYDRAULIC POWER CART. INSPECT GEAR INSTALLATIONS AROUND NEW NOSE GEAR UPLOCK HOOK ACTUATOR AND SWITCH, ACCESSED HOOK RIG PIN HOLES AND VERIFIED PROPER HOOK RIGGING PER 32-30-05 NO FAULTS FOUND. 2L72 4F RTA22CE 20040519000592004051900059WP 2004 5 19 0400509620 120040327A5312 BULKHEAD DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01620NW 47533 DURING "H" CHECK FOUND CRACKS IN BULKHEAD WEB AT BS 756. REPAIRED PER EA 96-198613. 2L72 4F A6WE 20040519000722004051900072CE 2004 5 19 DXTA200400288 120040404A7603 CONTROL CABLE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENGINE OUT OF RIG E DXTAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 GL07352QS 5600352 PCE500209 LEFT ENGINE FLAMED OUT AFTER DOING PREFLIGHT WING SPOILER CHECK. INSPECTED LEFT ENGINE CONTROLS AT FUEL CONTROL UNIT AND ACCOMPLISHED ENGINE POWER CONTROLS CHECK. PERFORMED ADJUSTMENT AND RIGGING CHECK IAW CESSNA 560 MM CHAPTER 76-11-00 PG. 501 NO DISCREPANCIES NOTED. 2L72 4F4 FRTA22CE E25EA 20040519000732004051900073NM 2004 5 19 C1HA200485002 120040402A27821U1110 ACTUATOR BOEING727 7272S7 138407ZNM KRUGER FLAP MALFUNCTIONED A C1HAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL15685CA 22492 NR 4 KRUGER FLAP WOULD NOT RETRACT AFTER T/O. R&R NR 4 KRUGER FLAP ACTUATOR PER M.M. 27-81-22. ACTUATOR OPS CHECKS GOOD. 2L73 4F A3WE 20040519000982004051900098NM 2004 5 19 513NA0004 120040406A335020131A BATTERY PACK BOEING757 7572T7 1384914NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05513NA 23895 MID CABIN FLOOR ILLUMINATION LIGHTS AND R3 DOOR AND OVERWING EMERGENCY LIGHTS INOP. REPLACED M734 EMERGENCY LIGHT BATTERY PACK PER MM 33-51-0. 2L72 4F RTA2NM 20040519001022004051900102EU 2004 5 19 RAIA00403023 120040325A3320BC0072001 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN BURNED A RAIAD RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 CE03552HK 41057 FIRE ABOVE SEAT 8A, POSSIBLE WASH LIGHTING. MAINTENANCE TROUBLE SHOT, AND DEFERRED WINDOW WASH LIGHT SYSTEM PER MEL. SUBSEQUENTLY REMOVED AND REPLACED WASH LIGHT FIXTURE. 2L72 4T RTA41NM 20040519001172004051900117SO 2004 5 19 MASA200400189 120040408A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07829MJ2130 145228 2 CABIN FLOOR PROX LIGHTING STRIPS INOP. MX REPLACED THE BATTERY PACK. OP CHECKS GOOD 2L72 4T RTT00011AT 20040519001192004051900119CE 2004 5 19 DXTA200400291 120040408A3230 RELEASE CABLE CESSNA750 750 2076810CE NLG OUT OF RIG E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07946QS 7500195 AT FL410 THERE WAS A LOUD THUMP IN THE NOSE GEAR AREA AND THE GEAR UNLOCK RED LIGHT ILLUMINATED, THERE WAS ANOTHER THUMP AND THE LIGHT EXTINGUISHED. LANDING GEAR BLOW DOWN HANDLE WAS PULLED. JACKED AIRCRAFT AND PERFORMED GEAR BLOW DOWN AND OPS CHECK, RESET GEAR BLOW DON AND SERVICED NITROGEN IAW 750 MM CHAPTER 12-00-01. FOUND NOSE GEAR UP LOCK RELEASE WAS HOLDING UP LOCK FROM FULLY ENGAGING ROLLER. RE-RIGGED NOSE GEAR RELEASE AND OPS CHECKED SYSTEM, OPERATIONAL CHECK OF SYSTEM GOOD. ALL WORK DONE IAW 750 MM CHAPTER 32-30-06. 2L72 4J RTT00007WI 20040519001332004051900133NM 2004 5 19 XNOA1183 120040413A5270 SWITCH BOEING727 727227 1384078NM CARGO DOOR OUT OF ADJUST A XN0AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL2376752 21248 DURING CLIMB, MAIN CARGO DOOR LIGHT ILLUMINATED. ADJUSTED DOOR CLOSED SWITCH IAW HAMILTON-TIMCO SUPPLEMENTAL MM 7-11-1. OPS CHECKS GOOD IAW HAMILTON TIMCO-SUPPLEMENTAL MM 4.1.1 2L73 4F A3WE 20040519001342004051900134WP 2004 5 19 IXXA0400020O 120040412A2133 LINKAGE DOUG DC8 DC862F 3021972WP OUTFLOW VALVE LOOSE A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW1171CX 64050343 45961 DURING FLIGHT CABIN CLIMBING AT 1000' PER MINUTE- AIRCRAFT ALTITUDE FL200- UNALBE TO CAUSE CABIN TO DESCEND TO NORMAL ALTITUDE- CROSSFEED OPEN. MAINTENANCE INSPECTED PNEUMATIC DUCTING AND PERFORMED LEAKS CHECK. NO DEFECTS NOTED. MAINTENANCE THEN PERFORMED GROUND PRESSURIZATION PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED CABIN AIR OUTFLOW VALVE FOUND DRIVE ROD LINKAGE LOOSE, CAUSING VALVE TO STICK OPEN. ADJUSTED LINK PER ALL MANUALS,OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040519001482004051900148NM 2004 5 19 HNAA0400036 120040410A3230574205A SELECTOR VALVE DHAV DHC8 DHC8201 2809001NM MLG WEAK A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07985HA 479 LANDING GEAR WILL NOT RETRACT AFTER T/O, RETURN TO FIELD, GEAR WAS CONFIRMED DOWN, INSPECTED GEAR, L/G INHIBIT SWITCH AND L/G ALTERNATE DOORS, ALL INSP NORMAL, R&R PSEU SAME BITE CODES INDICATED BITE CODE 40 28 VDC POWER CHECKED ALL POWER INTO PSEU AND GROUNDS, NO DEFECT NOTED. C/W OPS CHECK OF LANDING GEAR SELECTOR PANEL PER MM32-31-05 OPS CHECK GOOD L/G SELECTOR VALVE SOLENOID WAS VERY WEAK. R&R LANDING GEAR SELECTOR VALVE. 2H72 4T RTA13NM 20040519001492004051900149NM 2004 5 19 P5CA0401070 120040414A2910272U1200747 TUBE BOEING747 74746NF 13848BTNM HYD SYSTEM LEAKING A P5CAO OTHER K FLUID LOSS LDLANDING 1 WP23451PA 30809 STATUS MESSAGE, "HYD PRESSURE ENG 2." INSTALLED FLEX LINE IN PLACE OF RIGID LINE AND SECURED, OPS AND LEAK CHECK OK IAW MM 29-00-00 AND SERVICED HYD LEVEL TO FULL. 2L74 4F RTA20WE 20040519001612004051900161NM 2004 5 19 F3LA200400043 120040415A5320 SILL BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L1 MOP SILL. REPLACED L1 MOP SILL PER SRM 51-40-02 AND 53-10-15. 2L72 4F RTA16WE 20040519001912004051900191NM 2004 5 19 NACA20040019 120040421A301080034 GASKET PWA BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE SHUTOFF VALVE WORN A NACAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03992AJ262 262 B3750 19428 649589 NR 1 ENGINE STRUT OVERHEAT LITE CAME ON DURING CLIMB. RETARDED THROTTLES AND LITE WENT OUT. RE-APPLIED CLIMB POWER AND LITE CAME BACK ON. REPLACED WING ANTI-ICE HIGH PRESSURE SHUT-OFF VALVE GASKETS. CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040519001922004051900192NM 2004 5 19 P5CA0401071 120040415A324426070812 TIRE BOEING747 7472D3B 1384805NM MLG SEPARATED A P5CAO OTHER O OTHER LDLANDING 1 WP23505MC 21251 TOWER REPORTED LOST TIRE ON LANDING. REPLACED NR 3 TIRE AND BRAKE, NR 4 TIRE. 2L74 4F RTA20WE 20040519001952004051900195NM 2004 5 19 QXEA200400273 120040420A26114462531 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER CRCRUISE 1 NM09347PH 480 SEA-ON FLIGHT NUMBER 2021, FLIGHT ATTENDANT REPORTED LAVATORY SMOKE DETECTOR, GREEN LIGHT, NOT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001982004051900198NM 2004 5 19 PCAA0404190 120040415A793125890 FLOW DIVIDER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 OIL PRESS LEAKING A PCAAE ENGINE SHUTDOWN P NO WARNING INDICATION CLCLIMB 1 EA13840EX8480 3 327 121211 REPORTED A POWER LEVER SPLIT AND TORQUE GRADUALLY DECREASING AFTER TAKEOFF. THE NR 2 OIL PRESSURE WENT TO ZERO AND THE OIL PRESSURE LIGHT ILLUMINATED. CREW SHUTDOWN THE NR 2 ENGINE AND RETURNED TO RICHMOND. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LEAKING FROM THE NR 2 ENGINE FLOW DIVIDER,ENOUGH THAT THE ENGINE WAS SHUTTING DOWN DUE TO FUEL STARVATION. THE FLOW DIVIDER WAS REMOVED AND INSPECTED AND REINSTALLED. AIRCRAFT HAD GROUND RUN UP PERFORMED AND ALL LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040519001992004051900199CE 2004 5 19 DXTA200400296 120040418A3230 LANDING GEAR CESSNA560 560XL 2076702CE MAINS MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07690QS 5605090 SELECTED GEAR UP ON TAKEOFF, GEAR FAILED TO RETRACT, INDICATION SHOWED 3 GREEN 1 RED UNLOCK LIGHT . SELECTED GEAR DOWN, 3 GREENS RED EXTINGUISHED, ACCOMPLISHED AIR TURN BACK AND LANDED SAFELY. ACTUATED EMERGENCY GEAR EXTENSION HANDLE, RESTORED AND SERVICED PNEUMATIC BOTTLE IAW CESSNA 560XL MM CHAPTER 12-13-01. JACKED AIRCRAFT, CYCLED GEAR NUMEROUS TIMES, SYSTEM OPS CHECKED GOOD, MAINTENANCE PERFORMED IAW CESSNA 560XL MM CHAPTER 32-30-00. 2L72 4F RTA22CE 20040519002002004051900200NM 2004 5 19 DXTA200400297 120040418A2420524PCZ CIRCUIT BOARD AMD FALC50FALCON2000 2730170NM NR 2 ALTERNATOR FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07222QS 122 DURING FLIGHT THE RIGHT GENERATOR FAILED AFTER TAKEOFF, GENERATOR SWITCH REMAINED CLOSED. GENERATOR VOLT METER INDICATED 0 VOLTS, ACCOMPLISHED AIR TURN BACK AND LANDED OVERWEIGHT. - REMOVED AND REPLACED NR 2 ALTERNATOR PRINTED CIRCUIT BOARD (524PCZ) IAW FALCON 2000 MM 24-306, OPERATIONALLY CHECKED GOOD. 2K73 4F RTA50NM 20040519002022004051900202CE 2004 5 19 DXTA200400293 120040415A3150 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE FUEL FILTER ILLUMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07893QS 258393 ON TAKE OFF ROLL AT 40 KNTS "ENGINE NR 1 FUEL" LIGHT ILLUMINATED, ABORTED TAKE OFF - SUMPTED FUEL FROM AIRCRAFT AND CHECKED FOR WATER CONTAMINATION, NONE FOUND. INSPECTED THE LEFT ENGINE FUEL FILTER AND NO DEBRIS NOTED. REPLACED FILTER AND PERFORMED ENGINE GROUND RUN, SYSTEM OPS AND LEAK CHECKED GOOD IAW RAYTHEON MM CHAPTER 71-00-00. 2L72 4F RTA3EU 20040519002042004051900204WP 2004 5 19 MWEA040058 120040419A5347593056671 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 NR 1 SEAT TRACK HAS LIGHT CORROSION AROUND SCREW HOLE, UPPER AND LOWER SIDES STATION 1136-1165. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2L72 4F A6WE 20040519002052004051900205WP 2004 5 19 MWEA040059 120040419A5347593056671 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 NR 2 SEAT TRACK IS CORRODED AT STATION 1155-1179. FABRICATED AND INSTALLED NEW SEAT TRACK. 2L72 4F A6WE 20040519002062004051900206WP 2004 5 19 MWEA040060 120040419A5347593056671 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 CORROSION FOUND UNDER G3 FORWARD GALLEY FOOT, FOUND ON NR 2 SEAT TRACK AT FRAME STATION 1100. REMOVED AND REPLACED SEAT TRACK. 2L72 4F A6WE 20040519002092004051900209 2004 5 19 304AW0005 420040418A22104084042911 COUPLER BOEING737 7373G7 1384595NM YAW DAMPER DAMAGED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05304AW 24011 YAW DAMPER POPS DC CIRCUIT BREAKER. PLACED ON MEL 22-3-1 AND PERFORMED RUDDER PRESSURE REDUCER SYSTEM TEST PER MM 22-12-01. 04/22/2004: REPLACED YAW DAMPER COUPLER PER MM 22-12-13. SYSTEM CHECKS NORMAL PER ADJUSTMENT/TEST. 2L72 4F RTA16WE 20040519002102004051900210NE 2004 5 19 QXEA200400278 220040421A7230 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 ENGINE STUCK A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 NM09600QX 10005 GEE965303 ON FLIGHT FROM BOI TO SJC. NR 2 ENGINE N1 VIBRATION. AIRCRAFT RETURNED TO FIELD AND MAINTENANCE FREED STUCK BLADE. NO PARTS REPLACED OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040519002112004051900211NM 2004 5 19 QXEA200400277 120040421A3040SYLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09359PH11778 514 ON FLIGHT FROM PDX TO LMT CREW RECEIVED A WINDSHIELD HOT CAUTION LIGHT, DUE TO ICING CONDITIONS A DECISION WAS MADE TO RETURN TO PDX. MAINTENANCE REPLACED THE FIRST OFFICER WINDSHIELD TEMPERATURE CONTROLLER. OPERATIONAL CHECK GOOD. AIRCRAFRT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519002132004051900213NM 2004 5 19 EIA2004023 120040421A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 STA 360 LT UPPER DECK FLOORBEAM, TO FRAME INTERFACE HAS (4) ELONGATED HOLES. OVERSIZED ELONGATED HOLES AT STA 360 LT UPPER DECK FLOORBEAMS TO FRAME INTERFACE TO ROUND CONDITION. HFEC & 1OX VISUAL INSP SHOWS HOLES TO BE CRACK AND CORROSION FREE. (SEE ECRA 486-53-025-2). REMOVED EXISTING FREEZE PLUGS AT HOLES NR 2 AND NR 4 & INSTALLED NEW FREEZE PLUGS. INSTALLED (1) REPAIR STRAP AT BS 340 RT FLOORBEAM TO FRAME INTERFACE PER ECRA486-53-025-2. 2L74 4F A20WE 20040519002142004051900214NM 2004 5 19 EIA2004024 120040421A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 STA 340 RT UPPER DECK FLOORBEAM TO FRAME INTERFACE HAS ELONGATED HOLES. OVERSIZED, ELONGATED HOLES TO ROUND CONDITION. HFEC & 1OX VISUAL INSPECTION SHOWS HOLES TO BE CRACK AND CORROSION FREE. (SEE ECRA 486-53-025-2) REMOVED EXISTING FREEZE PLUGS AT HOLES NR 2 & 4 & INSTALLED NEW FREEZE PLUGS. INSTALLED 1 REPAIR STRAP AT BS 340 R/H FLOORBEAM TO FRAME INNER INTERFACE PER ECRA 486-53-25-2. 2L74 4F A20WE 20040519002172004051900217NM 2004 5 19 EIA2004027 120040421A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 LEFT HAND AFT INNER CHORD CRACKED AT STA 2598 AT SHEAR DECK. FABRICATED AND INSTALLED SPLICE ANGLES LT AFT INNER CHORD STA 2598 AT SHEAR DECK, PER B747 SRM 53-10-04, FIG 72. 2L74 4F A20WE 20040519002182004051900218NM 2004 5 19 EIA2004029 120040421A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 STA 360 LT UPPER DECK FLOORBEAM UPPER CHORD HAS NUMEROUS HOLES WITH SHORT EDGE MARGIN BETWEEN LBL 55 & LBL 82. REPAIRED STA 360 LH UPPER DECK FLOORBEAM UPPER CHORD SHORT EDGE MARGIN HOLES, LBL 55-LBL 82, PER ECRA #486-53-025-2, PART "C" 2L74 4F A20WE 20040519002192004051900219NM 2004 5 19 252TR0018 120040328A2121215201 FAN BOEING737 737228 13844AGNM AIR DISTRIBUTIONFAILED A PIDAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO05252TR 23001 SMOKE/MORE LIKE ELECTRICAL FUMES/CABIN & FLIGHT DECK. RECIRCULATION (GASPER) FAN PLACED IN OFF POSITION. QUICK REFERENCE HANDBOOK COMPLETED, FUMES SUBSIDING. CHECKED SYS PER MM 21-00-01. ALL SYSTEMS CHECK OK, INCLUDING "RECIRCULATION" GASPER FAN. NO FUMES NOTED. SIX SEGMENTS FLOWN, APX. 9 HRS FLT TIME. GASPER FAN INOPERATIVE. REPLACED GASPER FAN PER MM 21-42-21. UPON REMOVAL, VERBALLY CONFIRMED BY MX THAT THE BEARINGS IN THE GASPER FAN MOTOR WERE ROUGH & BINDING. THE GASPER FAN IS PRESENTLY BEING PROCESSED INTO REPAIR SHOP WITH A TEAR DOWN REPORT FORTHCOMING. RECEIVED THE TEAR DOWN REPORT: FAN WAS DIRTY, BEARINGS WERE WORN TO FAILURE CAUSING IMPELLER TO RUB THE INLET SHROUD. ROTOR RUBBED THE STATOR. 2L72 4F RTA16WE 20040519002202004051900220WP 2004 5 19 MWEA040063 120040422A575359304941 VANE DOUG DC9 DC981 3022081WP TE FLAP CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LEFT HAND INBOARD FLAP SECTION CHAFED ON THE LEADING EDGE OF THE INBOARD FIXED VANE. -- FABRICATED AND INSTALLLED INBOARD FIXED VANE. 2L72 4F A6WE 20040519002212004051900221CE 2004 5 19 60413 120040408A5753 LINK BEECH 1900 1900D 1154162CE TE FLAPS STUCK A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE07132YV UE132 ON TAKEOFF OUT OF HII FLAPS WERE SELECTED UP BUT THEY STUCK AT 17 DEGREES. AFTER TALKING WITH THE COMPANY ALL DECIDED AIRCRAFT SHOULD RETURN TO FIELD. RETURNED WITH NO FURTHER INCIDENT. R&R FLAP FLIP SWITCH LINK, BUSHING & CAM OPS CK NORMALP/N 101-521030-3 2L72 4T RTA24CE 20040519002242004051900224CE 2004 5 19 59816 120040318A3242 NUT BEECH 1900 1900D 1154162CE BRAKE ROD LOOSE A AMWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE07176YV UE176 ON TAKE OFF ROLL CREW NOTED A LACK OF PROPER ACCELERATION. ABORTED TAKE OFF RETURNED TO GATE. FOUND BRAKE ROD NUT LOOSE. IT WAS TIGHTENED. 2L72 4T RTA24CE 20040519002262004051900226CE 2004 5 19 60014 120040326A5220 MECHANISM BEECH 1900 1900D 1154162CE EMERGENCY EXIT LACK OF LUBE A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07159YV UE159 EMERG/EXIT 6C HANDLE ON EXT/PARTLY OPEN W/IN/CLOSE. CLEANED & LUBED EMERG/EXIT 6C L/MECHANISM. 2L72 4T RTA24CE 20040519002282004051900228CE 2004 5 19 60135 120040329A32601143640681 PRESSURE SWITCH BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER LDLANDING 1 CE07173YV UE173 UPON GETTING READY TO LAND IN PKB. CREW EXTENDED LANDING GEAR WITH CAUSE LANDING GEAR C/B TO POP AND NOT RESET. CREW CALLED AND DID A FLY BY TO VERIFY GEAR WAS DOWN. TOWER CALLED OUT EQUIPMENT AND THEY LANDED SAFELY WITH NO FURTHER INCIDENT THERE. R/R JACK AC/CYCD/RR A316 CARD/S1 PRESS SWITCH. 2L72 4T RTA24CE 20040519002302004051900230NM 2004 5 19 04232004SO35 120040422A21613218581 VALVE DOUG MD88 MD88 3023688NM AC SYS FAILED A A4JAGB O2 MASK DEPLOYED EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO3512FQ 49766 DURING INITIAL CLIMB SMOKE ENTERED COCKPIT AND REAR PORTION OF CABIN.TROUBLE SHOT AND FOUND LEFT HAND TEMP CONTROL VALVE STUCK OPEN TO FULL HOT. REMOVED AND REPLACED LEFT HAND TEMP CONTROL VALVE IAW MD80 MM 21-61-01. OPERATIONAL AND LEAK CHECKS GOOD.AS A PRECAUTION REMOVED AND REPLACED LEFT HAND COALESER BAG IAW MD80 MM 21-20-02. OPERATIONAL AND LEAK CHECK GOOD.PERFORMED OPERATIONAL CHECK OF PACK OVER TEMP AUTO-SHUTOFF SYSTEM PER MM21-60-00. SYSTEM TEST GOOD. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA6WE 20040519002312004051900231NM 2004 5 19 DHL2004755010 120040421A2197 SPLICE BOEING727 727225 1384077NM SENSOR BROKEN A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01755DH 21857 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON. NOTED DUCT OVER HEAT LIGHT. PLACED LT PACK ON MEL IAW 21-1-1, CONTROL 16378, CAT. "C", PLACARD INSTALLED. REF. DMI 16378 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON. NOTED DUCT OVER HEAT. FOUND BROKEN SPLICE FROM 35 DEGREE SENSOR TO 35 DEGREE CONTROLLER. REPLACED SPLICE PER STANDARD PRACTICES. PACK OPERATES NORMAL PER M/M 21-11-00. THIS CLEARS DMI #16378. MAINTENANCE CONTROL NOTIFIED. 2L73 4F A3WE 20040519002322004051900232NM 2004 5 19 DHL2004755011 120040422A2150 VALVE BOEING727 727225 1384077NM LT PACK FAILED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01755DH 21857 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON TEMPERATURE APPROXIMATELY 170 DEGREES. SEE PREVIOUS WRITE-UP LOG PAGE 000717. DMI 16389 MAINTENANCE CONTROLLER DIFFERED PER MEL 21-1-1 CATEGORY "C". REF. DMI 16389 SMOKE IN COCKPIT WHEN LEFT PACK WAS TURNED ON TEMPERATURE APPROXIMATELY 170 DEGREES. SEE PREVIOUS WRITE-UP LOG PAGE 000717. OPERATED PACKS SEVERAL TIMES WITH APU AND ENGINE BLEEDS. CHANGED PACK VALVE PRECAUTIONARY IAW M/M 21-55-71. INSPECTED PREVIOUS SPLICE REPAIR NO FAULTS. TESTED PACK COOLING FAN OPERATION NO FAULTS PER M/M 21-11-00. THIS CLEARS DMI 16389. 2L73 4F A3WE 20040519002332004051900233NM 2004 5 19 DHL2004763005 120040423A2612 WARNING LIGHT BOEING727 727264 138408MNM CARGO BAY ILLUMINATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01763AT 22983 LOWER CARGO COMPARTMENT DETECTION LIGHT ILLUMINATED PRIOR TO DEPARTURE. RESET CIRCUIT BREAKER. VERIFIED AFT AND FORWARD PITS FREE OF SMOKE-FIRE. OPS CHECKED GOOD. 2L73 4F A3WE 20040519002362004051900236NM 2004 5 19 04FDEA001031 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002382004051900238NM 2004 5 19 04FDEA001033 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002412004051900241NM 2004 5 19 04FDEA001036 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002422004051900242NM 2004 5 19 04FDEA001037 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002442004051900244NM 2004 5 19 04FDEA001039 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002452004051900245NM 2004 5 19 04FDEA001040 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002462004051900246NM 2004 5 19 04FDEA001041 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002482004051900248NM 2004 5 19 04FDEA001044 120040422A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN, STA 442 RBL 30 FOUND FLOORBEAM CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002502004051900250EU 2004 5 19 04FDEA001046 120040422A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN CABIN FR 41 UP TO FR 44, NR 4 RT SEAT TRACK NOTED CORROSIONS ON FOUR AREAS AS MARKED REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21 2L72 4F RTA35EU 20040519002512004051900251EU 2004 5 19 04FDEA001047 120040422A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC 5TH SEAT TRACK FROM CENTERLINE RT SIDE BETWEEN FR 26 AND FR 27 1 EA AREA OF CORROSION CLEANED OUT CORROSION, FOUND TO BE OUT OF LIMITS, AND REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 2L72 4F RTA35EU 20040519002532004051900253EU 2004 5 19 04FDEA001049 120040422A5320 BRACKET AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 FLOOR PAN PANEL BETWEEN RT SIDE OF 3 AND 4 SEAT TRACK AT FR 27 HAS FOUR EACH AREAS OF CORROSION UPPER SURFACE CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10 2L72 4F RTA35EU 20040519002542004051900254EU 2004 5 19 04FDEA001050 120040422A5320 PLATE AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 N01291 MDCC FLOOR PAN PANEL BETWEEN 3 AND SEAT TRACK 4 AT FR 26 RT SIDE HAS 3 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10 2L72 4F RTA35EU 20040519002552004051900255EU 2004 5 19 04FDEA001051 120040422A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 3RD SEAT TRACK FROM CENTERLINE JUST FWD OF FR 27 ONE EA AREA OF SURFACE CORROSION UPPER SURFACE. REPAIRED SEAT TRACK 3 LT FR 26-27 TO FR 27-28 AE PER A300-600 FREIGHTER SRM 53-10-16 PARA 4 FIG 201. 2L72 4F RTA35EU 20040520000022004052000002NM 2004 5 20 UIEA200400058 120040422A5730 PANEL BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING TOP SKIN. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER APPLIED IAW 57-30-01. (M) 2L74 4F A20WE 20040520000032004052000003EU 2004 5 20 USAASA04037 120040417A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19721UW10741 1095 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040520000062004052000006NM 2004 5 20 UIEA200400066 120040422A5720 ANGLE BOEING747 747243B 1384830NM RT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RIGHT WING T/E UPPER FIXED PANEL HORIZONTAL SUPPORT BEAM L-ANGLE CRACKED AT WING STATION 400. REPLACED CRACKED ANGLE WRT SRM 51-30-02. (M) 2L74 4F A20WE 20040520000072004052000007NM 2004 5 20 UIEA200400061 120040422A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SKIN CORROSON WS 323.82.00 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520000082004052000008NM 2004 5 20 UIEA200400062 120040422A5720 BUSHING BOEING747 747243B 1384830NM LT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING WALKING BEAM SUPPORT FITTING ASSEMBLY. FORWARD BEARING HOUSING OUTBOARD UPPER/FWD BOLT HOLE LOCATION ON REAR SPAR STIFFENER WAS FOUND WITH A CRACKED BUSHING HOLE AND BUSHING WAS ALSO FOUND WORN. CRACKED HOLE REPAIRED AS PER SB 747-57-2226 REV 6. CRACKED HOLE REAMED TO REMOVED CRACK. HOLE HFEC INSPECTED AND COLD WORKED TO .748 INCH AND NEW BUSHING INSTALLED. (M) 2L74 4F A20WE 20040520000132004052000013NM 2004 5 20 USAABB04034 120040411A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655US 25257 PHL - FOUND SECTION 2 OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING. (M) 2L72 4F RTA1NM 20040520000142004052000014EU 2004 5 20 USAASA04038 120040417A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19721UW12054 1095 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040520000152004052000015NM 2004 5 20 UIEA200400053 120040421A5730 CAP BOEING747 747243B 1384830NM RT WING LE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RT WING LEADING EDGE NOSE CAP AT LES 1042 FOUND 4.25 INCH LONG SPANWISE CRACK PROPERGATED FROM WING ANTI-ICE DUCT. RIGHT WING LEADING EDGE NOSE BEAM CRACKED WEB REPAIRED AS PER FAA FORM 8110-3 REF SJC NR A00063. (M) 2L74 4F A20WE 20040520000182004052000018NM 2004 5 20 UIEA200400055 120040421A5712 RIB BOEING747 747243B 1384830NM RT WING LE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RT WING LEADING EDGE RIB AT ILES 330 FOUND WITH A 1.25 INCH LONG CRACK ON THE WEB ALONG THE LOWER ANGLE AT AFT EDGE. REPLACED CRACKED LEADING EDGE RIB WEB WRT SRM 51-30-02. (M) 2L74 4F A20WE 20040520000202004052000020NM 2004 5 20 UIEA200400077 120040423A5311 FRAME BOEING747 747243B 1384830NM BULKHEAD CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RT WING GEAR WHEEL WELL BS 1350 BULKHEAD LOWER CHORD HORIZONTAL FLANGE AT RBL 50, LOWER SURFACE CORRODED. CORROSION REMOVED IAW SRM 51-10-01 FOUGN TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 1. AREA REPROTECTED IAW SRM 51-10-02. REMAINING THICKNESS 1.140 INCH. ORIGINAL THICKNESS 1.225 INCH. MATERIAL REMOVED .085 INCH. (M) 2L74 4F A20WE 20040520000212004052000021NM 2004 5 20 UIEA200400057 120040422A5730 PANEL BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING STOP SKIN. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPORTECTED AND PRIMER APPLIED IAW 57-30-01. (M) 2L74 4F A20WE 20040520000222004052000022NM 2004 5 20 UIEA200400056 120040421A5730 PANEL BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SKIN FIXED T/E FIBERGLASS PANEL BULGING AT RABBET AREA AFT OF REAR SPAR BETWEEN WBL 198.6 TO 204.6. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520000242004052000024NM 2004 5 20 UIEA200400079 120040423A5720 ANGLE BOEING747 747243B 1384830NM RT WING TE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RT WING T/E LOWER ACCESS PANEL SUPPORT BEAM AFT L-ANGLE CRACK AT WS 670. REPLACED CRACKED PANEL SUPPORT BEAM ATTACH CLIP 'L' ANGLE WRT SRM 51-30-02. (M) 2L74 4F A20WE 20040520000262004052000026NM 2004 5 20 USAABB04033 120040410A3397W83200916 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19645US 23897 FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE W832-009016. (M) 2L72 4F RTA1NM 20040520000302004052000030EU 2004 5 20 USAAEM04005 120040416A32301701941B MODULE EMB ERJ170ERJ170100 EU COCKPIT INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19802MD 17000013 CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE 'UP' POSITION AFTER TAKEOFF. FLIGHT RETURNED EWR WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATISFACTORY. (M) 2L74 4F RTA56NM 20040520000312004052000031EU 2004 5 20 USAABA04009 120040423A33501013083 LIGHT AIRBUS330 A330323 3930335EU LAVATORY WALL INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19672UW 0333 THE AISLE EMERGENCY LIGHT MOUNTED ON THE L73 LAVATORY WALL WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA46NM 20040520000322004052000032NM 2004 5 20 USAASB04044 120040412A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19384US 22957 PIT - MAINTENANCE REPORTED THE AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY FOR THE AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20040520000332004052000033NM 2004 5 20 USAASB04046 120040425A2424915F2125 GCU BOEING737 7374B7 1384702NM NR 1 GENERATOR OVERHEATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19448US5521216385 24892 NR 1 GENERATOR CONTROL UNIT BEGAN TO SMOKE IN FLIGHT. AFTER TRIPPING OFF LINE, SMOKE STOPPED. FLT LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 GENERATOR CONTROL UNIT. RAN ENGINE. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040520000342004052000034NM 2004 5 20 USAA040101 120040401A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US47550 23739 FOUND SKIN CRACKED .375 INCH, TOP HINGE CUTOUT AFT SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-60-01. (M) 2L72 4F RTA16WE 20040520000352004052000035NM 2004 5 20 USAA040107 120040405A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US53322 22952 FOUND SKIN CRACKED 1.250 INCH LONG, INSTALLED DOUBLER PER SRM. 53-00-01, FIG 229. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040520000362004052000036NM 2004 5 20 USAA040113 120040405A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US53322 22952 FOUND SKIN CRACKED 1.250 INCH LONG, 3 INCHES FORWARD OF FS 727E ADJACENT TO S-24L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040520000382004052000038NM 2004 5 20 USAA040112 120040405A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US53322 22952 FOUND SKIN CRACKED .600 INCH LONG, S-23L AT FS 744. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040520000402004052000040NM 2004 5 20 USAA040097 120040330A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US47550 23739 PIT - FOUND CHORD CORRODED 4 SQUARE INCHES, FORWARD SIDE AT Y-CHORD. CLEANED CORROSION PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20040520000452004052000045NE 2004 5 20 USAABA04008 220040421A729752U397 WIRE HARNESS AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE SHORTED A USAAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 EA19677UW 0380 THE RIGHT IDG BECAME INOPERATIVE. THE APU WAS STARTED, HOWEVER IT WAS REPORTED THAT THE ELECTRICAL SYSTEM WAS UNSTABLE. THE FCU HEADING FROZE AND NEW HEADINGS WERE NOT ACCEPTED BY THE AUTOPILOTS NOR THE FLIGHT DIRECTOR. IN ADDITION, THE CREW REPORTED AN ELECTRICAL SMELL IN THE MID GALLEY. ALL GALLEY EQUIPMENT WAS SECURED AND THE SMELL ABATED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED GHE FCU FOR THE NAVIGATION PROBLEM. NO CAUSE WAS FOUND FOR THE MID GALLEY ODOR. THE MAIN CAUSE FOR THIS EVENT WAS THE ELECTRICAL PROBLEM. THE RIGHT GCU AND RIGHT WC-1 WIRING HARNESS WERE REPLACED. (M) 2L72 4F4 FRTA46NM 20040520000462004052000046NM 2004 5 20 USAA040098 120040401A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19576US50106 23741 PIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, FROM AFT EDGE TO INBOARD FASTENER LEFT 18A SHELF. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) 2L72 4F RTA16WE 20040520000472004052000047SO 2004 5 20 C2XA04CL054 120040514A52207137011509 LINER EMB 135 EMB135ER 3260203SO EMERGENCY DOOR MISALIGNED A C2XAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW2727512 145274 DURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE LT OVERWING INNER DOOR LINER TO BE MISALIGNED. MAINTENANCE REALIGNED LINER AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040520000482004052000048NM 2004 5 20 QXEA200400322 120040512A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAULTY A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09375PH10974 529 AT 10,000 FT MSL OVER OLY, CREW GOT AN INTERMITTENT MASTER WARNING/SMOKE LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH CARGO SMOKE DETECTORS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520000502004052000050NM 2004 5 20 CALA0400491 120040515A532065C3397053 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723661 28922 INSPECTION FOUND A 2 INCH CRACK IN UPPER FLANGE OF INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 65C33970. 2L72 4F RTA16WE 20040520000522004052000052NM 2004 5 20 04FDEA01070 120040423A5753ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OB FLAP OB FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. LT WING, OB FLAP OB FWD HINGE BARREL NUT HOLE NR 7 MATING SURFACE CORROSION REMOVED IAW CMM 57-44-09 PAGE 9 AND FOUND WITHIN LIMITS IAW DWG ARC0503. 2L73 4F RTA22WE 20040520000542004052000054EA 2004 5 20 541804062004 120040406A2750KD4L050 RELAY CNDAIRCL604 CL604 1900301EA FLAPS FAILED E J7SAA UNSCHED LANDING SFJAFFECT SYSTEMS FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW05319FX 5418 FLAPS WOULD NOT RETRACT AFTER TAKE-OFF. (FLAPS WERE SET AT 20 DEGREES).MAINTENANCE IN PROGRESS - MAINTENANCE TROUBLESHOOTING CONFIRMED K2CE RELAY WAS AT FAULT. RELAY REPLACED AND OPS CHECKS PERFORMED SATISFACTORILY. 2L72 4F RTA21EA 20040520000602004052000060NM 2004 5 20 0400765515 120040426A5320 INTERCOSTAL BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 23203 DURING H-CHECK FOUND CRACK IN INTERCOSTAL AT BS 660 S14 RT. REPAIRED IAW EA 55-199015. 2L72 4F RTA2NM 20040520000612004052000061NM 2004 5 20 QXEA200400323 120040514A521085217003001 DOOR BOMBDRDHC8 DHC8401 1390041NM MAIN CABIN OUT OF ADJUST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09404QX6765 4046 CREW REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE DOOR UP AND DOWN LIMIT STOPS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520000622004052000062NM 2004 5 20 04FDEA01074 120040423A5753ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OB FLAP, OB FWD HINGE, ACTUATOR HOLE 8 IB CORRODED. COMPLIED WITH EA 1-5750-76024 , WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OB FLAP OB HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040520000632004052000063NM 2004 5 20 04FDEA01075 120040423A5753ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OB FLAP, OB FWD HINGE ACTUATOR , HOLE 8 OB CORRODED. COMPLIED WITH EA 1-5750-76024 - WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OB FLAP OB HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040520000652004052000065NM 2004 5 20 04FDEA01076 120040423A5753ARC2512504 FLAP DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. COMPLIED WITH EA NR1-5750-76023, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. RT IB FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040520000662004052000066NM 2004 5 20 DHL2004743004 120040515A5754 RIB BOEING727 727225 1384077NM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 LT WING NR 2 LEADING EDGE SLAT RIBS AT ROD END HAS 2 SMALL CRACKS. ONE ON EACH SIDE OF ROD END. REPAIRED BRACKETS IAW B-727 SRM 51-40-3, MATERIAL USED 2024T3, .051, RIVETS USED: CR3223-5-2, 10 EA, NAS 517-3-5 SCREWS, 2 EA. PO NR 400004986. . 2L73 4F A3WE 20040520000672004052000067EA 2004 5 20 MASA200400166 120040326A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07515MJ 10117 SUPP ASH 7119 BNA RT OVERWING EXTERNAL EMERGENCY EGRESS LIGHT INOPERATIVE. MECHANIC DEFERRED. 3/26/2004. MECHANIC RELAMPED. OP CHECKS GOOD. 2L72 4F RTA21EA 20040520000682004052000068EA 2004 5 20 MASA200400195 120040413A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW0737342 7342 SUPP ASH 7177 DEN-ABQ. AT PREFLIGHT, CREW FOUND THE FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PLACED ON MEL. 4/15/2004. MECHANIC RELAMPED. 2L72 4F RTA21EA 20040520000722004052000072EA 2004 5 20 MASA200400220 120040422A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775983 7481 CREW REPORTED EMERGENCY EXIT LIGHT INOPERATIVE. MECHANIC REPLACED THE LIGHT. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040520000732004052000073EA 2004 5 20 MASA200400226 120040426A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW077291Z 7291 CAPTAIN REPORTED THAT THE AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. MECHANIC REPLACED THE BULB AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20040520000742004052000074EA 2004 5 20 MASA200400228 120040427A3350BR9279106 SIGN CNDAIRCL600 CL6002B19 1900309EA OVERWING EXIT BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW0775983 7481 ASH 7188 IN BNA, DURING PREFLIGHT WALK THE CREW NOTICED THE SERVICE DOOR OVERWING EXIT SIGN LENS BROKEN. THE PLANE FERRIED AND MECHANIC REPLACED THE SIGN ASSY. 2L72 4F RTA21EA 20040520000762004052000076EA 2004 5 20 MASA200400255 120040510A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747239 7239 EMERGENCY FLOOR PROXIMITY LIGHT 3RD FROM AFT INOPERATIVE. ITEM WAS PLACED ON DEFERRAL IAW MEL 33-51-01-5 CAT C. MECHANIC RESECURRED CONNECTOR AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040520000772004052000077NM 2004 5 20 MASA200400259 120040511A33501317 BULB DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07988HA 426 EXIT SIGN ABOVE SEAT 1D INOPERATIVE. MECHANIC REPLACED THE BULBS IN THE SIGN. NO FURTHER FAULTS NOTED. 2H72 4T RTA13NM 20040520000802004052000080SO 2004 5 20 C2XA04SH278 120040510A541114576631622 RIB EMB 145 EMB145 3260210SO ENGINE NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV-DURING C CHECK THE RIGHT ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040520000812004052000081NM 2004 5 20 AWXA200400501 120040428A5320654581211 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN STIFFENER FORWARD OF BS 328, LBL 34. MAINTENANCE REMOVED CRACKED STIFFENER AT BS 328, LBL 34; FABRICATED A NEW REPLACEMENT STIFFENER IAW DWG 65-45834; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 12. 2L72 4F RTA16WE 20040520000822004052000082WP 2004 5 20 UPS04842378 120040514A2420 CONTROL PANEL DOUG DC8 DC873F 302199FWP NR 4 FAILED A IPXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01812UP 46112 N/A DURING TAXI OUR AND JUST BEFORE TAKEOFF, WE GOT A BUSS POWER FAIL LIGHT AND NR 4 GEN UNPARRALLED LIGHT ON. SMOKE BEGAN TO ACCUMULATE IN THE COCKPIT. TAXIED BACK TO RAMP. FOUND NR 4 GCP TO HAVE A HARD FAILURE. SUSPECT NR 4 GCP AS CAUSE OF SMOKE. RAN A/C PNEUMATIC SYSTEM, CHECKS NORMAL. REMOVED AND REPLACED NR 4 GCP IAW MM 24-20-0 6-2. PERFORMED OPERATIONAL CHECK IAW MM 24-20-00-0, OPS CHECKS GOOD. 2L74 4F RT4A25 20040518001012004051800101WP 2004 5 18 1982 120040318A7931E6 WIRE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 1 ENG DIFF SWSHORTED I U2RBE ENGINE SHUTDOWN F FLT CONT AFFECTED CRCRUISE 1 GL23921R 599061128 46145 669628 NR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENGINE AT 2245Z, OIL PRESSURE 45PSI,OIL TEMP 95 DEGREES C, WINDMILLING OIL PRESSURE 32 PSI. 2L74 4F4 F 4A25 1E8 20040518001092004051800109CE 2004 5 18 4009 120040311A5230 DOOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YR2 GL FWD CARGO BAY OPEN E BSYAD RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL0726CC TH136 ON TAKEOFF OUT OF DAL NOSE BAGGAGE DOOR POPPED OPEN, PILOT RETURNED TO BASE SECURED NOSE BAGGAGE DOOR AND CONTINUED WITH SCHEDULED RUN, NO FURTHER ACTION TAKEN. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20040518001162004051800116NM 2004 5 18 P5CA0401062 120040321A1420 CONNECTOR BOEING747 747236B 1384804NM AILERON CONTROL DIRTY A P5CAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 WP23924FT 21730 ON TAXI OUT FLIGHT CONTROL CHECK, NO O/B AILERON INDICATION. RECONNECTED AND CLEANED CONNECTOR S313 SWITCH. OPS CK NORMAL PER MM 27-10-00. 2L74 4F A20WE 20040518001192004051800119EA 2004 5 18 ACE032204 220040322A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA NR 2 FLAMED OUT E YADAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 AL03114AX UC36 32601 NR 2 ENGINE FLAMED OUT ON TAKEOFF. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE. 2L72 4T4 TRTA24CE E4EA 20040519000082004051900008SO 2004 5 19 RAIA00403020 120040323A276014533022405 CONTROL UNIT EMB 145 EMB145 3260210SO SPOILERS MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03802HK9776 145066 3563 - PWM - WHEN THRUST LEVERS ARE ADVANCED SPEED BRAKE LEVER DISAGREE MESSAGE IS DISPLAYED. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT. 2L72 4F RTT00011AT 20040519000152004051900015NM 2004 5 19 757BJ0010 120040319A5310 DOOR FRAME BOEING757 757236 1384971NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05757BJ 22176 NR 2 CARGO DOOR FWD FRAME AT STA.1380 WEB CRACKED AT SEAL RETAINER FASTENER LOCATION BETWEEN STR 25 RT AND STR26 RT. REPAIRED DAMAGE PER SRM 53-00-07. 2L72 4F RTA2NM 20040519000172004051900017NM 2004 5 19 P5CA0401063 120040323A27821267481 DRIVE UNIT BOEING747 747283B 1384867NM NR 1 LE FLAP MALFUNCTIONED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23921FT 21575 NR 1 L/E FLAP REQUIRES ALTERNATE PROCEDURE TO EXTINGUISH IN TRANSIT LIGHT. R&R NR 1 L/E DRIVE UNIT PER MM 27-81-03. 2L74 4F A20WE 20040519000382004051900038EU 2004 5 19 XNOA1180 120040330A29136506606 PUMP AIRBUS300 A300B4203 3930306EU HYD SYSTEM MALFUNCTIONED A XN0AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23372PC 1805 196 NR 2 ENG GREEN PUMP LOW PRESSURE IN FLIGHT. R&R NR 2 GREEN SYSTEM ENGINE DRIVEN PUMP IAW A300 AMM 29-11-32. OP'S CHECK GOOD. NO LEAKS NOTED. (STATUS: ORIG/CLOSED) 2L72 4F RTA35EU 20040519000412004051900041NM 2004 5 19 TSAA0453035 120040213A5244141A3722 ACCESS DOOR BOEING737 73776N 13844CHNM EXTERNAL POWER CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13745AL 29904 FOUND EXTERNAL POWER ACCESS DOOR DAMAGED. TRIMMED OUT CRACK OR DAMAGED AREA TO 1/2 INTERNAL RADIUS. HFEC VERIFIED TRIMMED OUT AREA. ALODINED AND PRIMED. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IN ACCORDANCE WITH ECO 7-0170. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040519000482004051900048NE 2004 5 19 IXXA0400019O 220040329A7320 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 1 FLAMED OUT A IXXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW11606AL908142566 46044 693534 DURING FLIGHT AT 34.0 FL AT 88 PERCENT N1, RPM FLUXED APPROX. 8 PERCENT ROM 80 TO 88 PERCENT ON NR 1 ENGINE, ENGINE FLAMED OUT. DESCENDED TO FL250 ATTEMPTED RESTART WITH PMC ON ENG WOULD NOT RESTART, SECOND ATTEMPT WITH PMC OFF ENGINE RELIGHTED, CONTINUED REMAINDER OF FLIGHT WITH PMC OFF. CREW LANDED IN KNGU WITHOUT INCIDENT. MAINTENANCE DEFERRED THIS ITEM PER MEL 73-01.CAT-C WITH NO FLY DATE 04/09/04. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20040519000582004051900058 2004 5 19 04014 420040331A3400 PANEL BOEING747 747209B 138489BNM COCKPIT SMOKE A KCSAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23714CK 22446 SMOKE IN COCKPIT ORIGINATING FROM BENEATH P-10 PANEL 2L74 4F RTA20WE 20040519000652004051900065NM 2004 5 19 F3LA200400035 120040311A3350 BATTERY BOEING737 7373M8 1384615NM L2 SLIDE LIGHT DISCHARGED A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03303FL 2961 25039 DURING C-5 CHECK, INSPECTION REPORTED L2 DOOR SLIDE LIGHTS INOP., BATTERY WAS DEAD. REPLACED L2 DOOR SLIDE. 2L72 4F RTA16WE 20040519000752004051900075NM 2004 5 19 PCAA0404186 120040404A335061047811 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13840EX 327 WHILE IN LGA, MAINTENANCE REPORTED THAT THERE WERE SEVERAL FLOOR AND SIDE EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2H72 4T RTA13NM 20040519000832004051900083NE 2004 5 19 P5CA0401066 220040403A7320 CABLE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 1 ENGINE DISCONNECTED A P5CAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 WP23355MC 23395 455430 NR 1 ENGINE ACCELERATES EXTREMELY SLOW. THE N2, EGT, AND FUEL FLOW ARE NOT ALIGNED WITH OTHER ENGINES. N1 GAUGE REMAINED AT IDLE. CORRECTIVE ACTION: DISCONNECTED MEC VSB/VBV, FEEDBACK CABLES EXERCISED MEC. RECONNECTED VSV/VBV FEEDBACK CABLES. PERFORMED ENGINE RUN, CK OK. 2L74 4F4 FRTA20WE E23EA 20040519000842004051900084EU 2004 5 19 YENA200422 120040406A21501263A000003 ACM AIRBUS320 A320232 3930326EU NR 1 SEIZED A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15509JB1098656 1270 AFTER TAKE OFF AT LGB, ON CLIMB SMELL AND VISIBLE INDICATION OF SMOKE IN CABIN PASSING THRU 10K/FT. AIR TURN BACK TO LGB. FOUND LT NR 1 PACK AIR CYCLE MACHINE SEIZED PER TSM 26-15-00-810-804. REMOVED & REPLACED NR 1 AIR CYCLE MACHINE IAW AMM 21-52-21. LEAK CK & OPS CK OK. 2L72 4F RTA28NM 20040519000852004051900085NE 2004 5 19 GLBA20030603 220040405A7261 OIL SYSTEM BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 1 ENGINE LOW A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03254GL UE254 OIL PRESSURE IN YELLOW ON NR 1 ENGINE, SERVICED ENGINE OIL 2L72 4T4 TRTA24CE E26NE 20040519000892004051900089NM 2004 5 19 HNAA0400033 120040406A531085311883 BEAM DHAV DHC8 DHC8102 2809003NM FUSELAGE CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 TRANSVERSE BEAM CRACKED AT RELEASE CABLE HOLE AT R/H SIDE IN NLG BAY APPROX .3 INCH LONG, REPAIRED IAW EO 8-53-04-0241 2H72 4T RTA13NM 20040519001072004051900107EU 2004 5 19 RAIA00404003 120040406A3234877701 SELECTOR JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03558HK1614 553 41071 RED LIGHT IN GEAR HANDLE. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE. 2L72 4T RTA41NM 20040519001102004051900110CE 2004 5 19 GLBA20030606 120040408A79311013890235 TRANSDUCER BEECH 1900 1900D 1154162CE LT OIL PRESSURE MALFUNCTIONED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM03253GL24177 UE253 LT ENG OIL PRESSURE INDICATOR FLUCUATING OFF SCALE, R&R LT OIL PRESSURE TRANSDUCER 2L72 4T RTA24CE 20040519001152004051900115EA 2004 5 19 MASA200400187 120040406A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727172 7172 GALLEY EMERGENCY EXIT LIGHT INOP. MX REPLACED THE BULB. OP CHECKS GOOD 2L72 4F RTA21EA 20040519001202004051900120NM 2004 5 19 P9RA20040010 120040409A3220 CABLE BOEING727 7272J0 138407ENM NLG OUT OF RIG A P9RAO OTHER J WARNING INDICATION CRCRUISE 1 SO11919PG 22604 WITH GEAR HANDLE IN THE OFF POSITION WHILE IN LIGHT TURBULENCE, NOSE GEAR LIGHT ILLUMINATED. (PIE TO SYR) CRUISE FLIGHT. FOUND NOSE GEAR WHEEL WELL DOOR CABLES WITH LOW TENSION. ADJUSTED PER M/M 32-22. CLEANED AND LUBRICATED NOSE GEAR. OPERATIONALLY CHECKED GOOD. 2L73 4F RTA3WE 20040519001222004051900122WP 2004 5 19 MWEA040053 120040412A53203936190 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 SPLASH GUARD FOR G-1 GALLEY AT STATION 160 APPEARS TO BE CORRODED IN SEVERAL AREAS. FABRICATED AND INSTALLED FITTINGS,FILLER AND PANEL 21. 2L72 4F A6WE 20040519001282004051900128NM 2004 5 19 EIA2004016 120040401A5312 BULKHEAD BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 RT WING LANDING GEAR BAY CANTED BULKHEAD STA. 1261 RBL 0 UPPER INBD CORNER (TEE CHORD) HAS CORROSION. REMOVED AND REPLACED TEE CHORD AT STA. 1261 RBL 0 PER 747 SRM 51-10-02 PG 1, 51-30-05 PAGES 6-9, 51-30-02 PAGES 8-9 AND 51-10-16 PAGES 1-30. 2L74 4F A20WE 20040519001312004051900131NM 2004 5 19 EIA2004019 120040408A3350 LIGHT BOEING747 747121 1384871NM EMERGENCY EXIT INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09480EV 20348 EMERGENCY EXIT LIGHT AT STA. 2200 LT INOP. REPLACED EMERGENCY LIGHT AT STATION 2200 LT PER B747 MM 33-51-07. OPS CHECKED OK PER 33-51-00 2L74 4F A20WE 20040519001352004051900135NE 2004 5 19 MASA200400162 220040324A72616087T04P05 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CLOGGED A MASAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW077728614916 7286 872204 A/C RETURNED TO FIELD REPORTING THAT THE CAPT PERFORMED AN IN-FLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE. MX REPLACED THE LUBE SCAVENGE PUMP. OP CHECKS GOOD ON TEST FLIGHT. 2L72 4F4 FRTA21EA E15NE 20040519001382004051900138EU 2004 5 19 RAIA00403032 120040330A2761TY176302A ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU RT SPOILERS MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03556HK178234718 41073 RT SPOILER SHOWS UNLOCK. MAINTENANCE DEFERRED SPOILER SYSTEM PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING THE RIGHT SPOILER ACTUATOR. 2L72 4T RTA41NM 20040519001472004051900147NM 2004 5 19 F3LA200400034 120040331A2612 FIRE DETECTOR BOEING737 737317 138447PNM APU BAY MALFUNCTIONED A F3LAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03EICHH 23177 CLIMBING THROUGH 5,000 MSL, FLIGHT CREW REPORTED APU FIRE INDICATION. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. REPLACED APU FIRE BOTTLE PER MM 26-22-11, PAGE 401-406. PLACARDED APU AND APU FIRE DETECTION SYSTEM PER MEL 26-8A. COMPLIED WITH SP 26-8. NO EVIDENCE OF FIRE WAS FOUND. AN ADDENDUM TO THIS SDR WILL BE SUBMITTED UPON REMOVAL OF THE PLACARD. ADDENDUM: ON 4/9/04, REPLACED BOTH APU EXHAUST FIRE DETECTOR ELEMENTS PER MM 26-15-14, PERFORMED OPERATIONAL CHECK AND CHECKED OKAY. REPLACED EXHAUST OVERHEAT ELEMENT, P/N 896768, S/N 217. REPLACED EXHAUST FIRE ELEMENT, P/N 896767, S/N 2178. 2L72 4F RTA16WE 20040519001562004051900156NM 2004 5 19 C1HA200476003 120040415A3230 ACCESSORY UNIT BOEING727 727225 1384077NM LT MLG MALFUNCTIONED A C1HAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15817EA 22554 LEFT MAIN GEAR RED UNSAFE LIGHT ON AFTER RETRACTION. FOLLOWED COM PROCEDURE & RETURNED TO LAX. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. OPS CHECKED GOOD IAW AMM 32-09-121. 2L73 4F A3WE 20040519001592004051900159NM 2004 5 19 PCAA0404187 120040405A2710LA11A2118 ACTUATOR DHAV DHC8 DHC8102 2809003NM AILERONS INOPERATIVE A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13811EX107893696 201 LGA REPORTED AILERON TRIM INOP. MAINTENANCE REPLACED THE AILERON TRIM ACTUATOR.SYSTEM CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001672004051900167NM 2004 5 19 HNAA0400037 120040418A5610PR1425 SEALANT DHAV DHC8 DHC8102 2809003NM WINDSHIELD DETACHED A HNAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA07930HA 126 NOTED LOUD FLAPPING NOISE INFLT FROM CAPT WINDSHIELD AFTER T/O RETURN TO FIELD. FOUND LOOSE WINDSHIELD SEAL, EXCESS WAS REMOVED AND APPLIED SPEED TAPE. SEALED AT NEXT RON PER EO 8-56-04-0273 2H72 4T RTA13NM 20040519001792004051900179NM 2004 5 19 PCAA0404193 120040418A3320F18T5WWRS LIGHT DHAV DHC8 DHC8102 2809003NM ROW 8 & 9 SMOKE A PCAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13839EX 226 REPORTED SMOKE FROM THE OVERHEAD LIGHT ABOVE SEATS IN ROW 8 AND 9.MAINTENANCE COMPLIED WITH MEL AND REMOVED THE LAMP AND PULLED AND BANDED ASSOCIATED CIRCUIT BREAKER. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001942004051900194NM 2004 5 19 QXEA200400274 120040419A2760 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM SPOILERS ILLUMINATED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09414QX 4061 GEG-ON FLIGHT NUMBER 2356, ROLL SPOILER OUTBOARD GROUND CAUTION LIGHT ILLUMINATED UPON CLEARING RUNWAY AFTER LANDING. FLIGHT/TAXI SWITCH FOR SPOILERS STILL IN FLIGHT POSITION. PFCS INDICATES OUTBOARD SPOILERS IN RETRACTED POSITION. PLACED ON MEL. THE OUTBOARD SPOILER LOWER LIFT DUMP VALVE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001962004051900196 2004 5 19 YENA200423 420040415A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ENTERTAIN SYS ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15506JB2967 1923 1235 ODOR OF SMOKE REPORTED BY FA'S 1HR INTO FLIGHT AT OR AROUND ROW 17. UPON FURTHER INVESTIGATION ODOR WAS GONE. NO EVEDENCE OF SMOKE / HEAT ETC. NO ECAMS. TV'S WERE NOT TURNED OFF. NO FURTHER REPORTS DURING FLIGHT. PERFORMED TSM 24-00-00-810-823 NO FAULTS FOUND. ALSO PERFORMED INFO NOTICE 2003-TO5OTR A. SMELL NOT REPORTED AROUND ROW 17 ABC, PROCEEDED TO PART B OF INFO NOTICE AND FOUND NO ABNORMALITIES. ITEM WAS DEFERRED PER MEL 25-22-03. UPON ARRIVAL AT MCO REMOVED AND REPLACED SEB PER INFO NOTICE 2003-T050TR A. OPERATION CHECK GOOD IAW LTV AMM 23-39-00. 2L72 4F RTA28NM 20040519002012004051900201CE 2004 5 19 DXTA200400295 120040417A3260327 LIGHT CESSNA560 560XL 2076702CE MLG INDCATOR INOPERATIVE E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07690QS 5605090 DURING APPROACH SELECTED GEAR DOWN AND DID NOT GET A SAFE GEAR INDICATION FOR THE RIGHT MAIN GEAR. PERFORMED THE EMERGENCY CHECKLIST AND BLEW GEAR DOWN BY PNEUMATICS, LANDED SAFELY AT JAX. - TROUBLESHOT LANDING GEAR SYS. FOUND THE RH MLG SAFE LIGHT BURNT OUT, REMOVED AND REPLACED BULB OPS CHECKED GOOD. JACKED AIRCRAFT AND CHECKED LANDING GEAR RETRACTION, FOUND ALL INDICATIONS NORMAL. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 32-30-00, SERVICED PNEUMATIC BOTTLE IAW CESSNA 560XL CHAPTER 12-13-0.1 2L72 4F RTA22CE 20040519002032004051900203WP 2004 5 19 MWEA040057 120040419A5347593056671 SEAT TRACK DOUG DC9 DC981 3022081WP STA CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 NR 1 SEAT TRACK SECTION STA 1165-1240 HAS NUMEROUS AREAS OF BARE METAL AND CORROSION. NOTE THAT SOME OF THE CORROSION IS ON THE BOTTOM SIDE OF SCREW HOLE. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK. 2L72 4F A6WE 20040519002072004051900207WP 2004 5 19 MWEA040061 120040421A5320993061275 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 SUBFLOOR MEMBRANE SKIN HAS 2 HOLES ENLONGATED AT FRAME STATION 1222, JUST BELOW SEAT TRACK NR 1. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040519002082004051900208WP 2004 5 19 MWEA040062 120040402A5320993061275 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 SUBFLOOR MEMBRANE SKIN HAS 2 HOLES ELONGATED AT FRAME STATION 1234 JUST BELOW SEAT TRACK NR 1. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040519002162004051900216NM 2004 5 19 EIA2004026 120040421A5320 WEB BOEING747 747212B 1384886NM FUSELAGE GOUGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 AFT PIT STA 1500 BETWEEN STR 41-42 LEFT FWD SIDE OF WEB HAS DEEP GOUGE. FABRICATED AND INSTALLED FRAME SECTION & DOUBLER PER B747 SRM 51-4-003, PAGES 7-12 AT STA 1500 STR 41-42 L DUE TO GOUGE EXCEEDING LIMIT PER B747 SRM 53-10-01, PAGE 1-4. MTL ID 7075T6,.063 PER B747 SRM 53-11-25, PG 1,2,26. FABRICATED FRAME & DOUBLER PER B747 SRM 51-30-02, PG 2-3&8-9 ALONDINED PER B747 SRM 51-10-02 & PRIMED PER BSOPM 20-41-02, PGS 7-9. 2L74 4F A20WE 20040519002222004051900222CE 2004 5 19 60371 120040407A3240 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07165YV UE165 CREW CALLED REPORTING BRAKES FELT SOFT. MAINTENANCE CALLED PIT. 2L72 4T RTA24CE 20040519002372004051900237NM 2004 5 19 04FDEA001032 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002392004051900239NM 2004 5 19 04FDEA001034 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040520000102004052000010NM 2004 5 20 UIEA200400064 120040422A531365B8904410 RIB BOEING747 747243B 1384830NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND KEELBEAM VERTICAL SUPPORT ANGLES AT STATION 1000 LT AND RT SIDES CRACKED. SUPPORT ANGLES REPLACED IAW SRM 51-10-01 AND SRM 51-30-02. (M) 2L74 4F A20WE 20040520000112004052000011NM 2004 5 20 UIEA200400059 120040422A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LT WING TOP SKIN CORROSION WS 1280 STRINGER 14. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520000192004052000019NM 2004 5 20 UIEA200400060 120040422A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SKIN CORROSION WS 1280 STRINGER 18. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520000252004052000025NM 2004 5 20 UIEA200400078 120040423A5314 KEELBEAM BOEING747 747243B 1384830NM FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RIGHT WING GEAR WHEEL WELL KEELBEAM TOP SURFACE AT BS 1265, CORRODED AROUND FASTENERS LOCATION. KEEL BEAM CORRODED TOP WEB SURFACE REPLACEMENT CARRIED OUT AS PER SRM 51-10-01 AND SRM 51-30-02. (M) 2L74 4F A20WE 20040520000292004052000029NM 2004 5 20 USAA040095 120040113A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19354US46309 23557 FOUND SKIN WITH 3 INCH STRESS CRACK, FORWARD OF AFT BAGGAGE PIT DOOR BS 727E S18R. STRESS CRACK REPAIR PER SRM 53-00-01 FIG 201, AND OM-7 NR 27801. (M) 2L72 4F RTA16WE 20040520000372004052000037NM 2004 5 20 USAA040110 120040403A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US53322 22952 FOUND SKIN CRACKED 1.450 INCH LONG, FS 891 ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040520000492004052000049SO 2004 5 20 C2XA04CL055 120040514A33501317 BULB EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727512 145274 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 9BC (IN PSU) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040520000552004052000055NE 2004 5 20 AALA20040552 220040513A7260 GEARBOX BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE RT ENGINE LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21791AN 30254 51244 FRA INFLIGHT T071/13, THREE HOURS INTO FLIGHT STATUS MESSAGE DISPLAYED WITH RT ENGINE N3 READING 0 OIL QUANTITY AND RT ENGINE OIL PRESSURE STARTED DROPPING. CREW SHUT DOWN RT ENGINE AND DIVERTED. LANDED OVERWEIGHT AND WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY ONE HOUR. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. REPLACED RT ENGINE GEAR BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTT00001SEE00050EN 20040520000562004052000056NE 2004 5 20 AALA20040551 220040511A7314 PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUEL SYSTEM INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21418AA 49329 725560 DURING CLIMB RT ENGINE REDUCED TO 30 PERCENT WITH ACCOMPANING YAW. SHUT DOWN ENGINE AND RETURNED TO ELP. LANDED OVERWEIGHT WITHOUT INCIDENT. PERFORMED OVERWEIGHT LANDING INSPECTION. REPLACED RT ENGINE DRIVEN FUEL PUMP IAW MM 73-12-01 AND RT ENGINE FUEL CONTROL IAW WORK CARD 73-91-99. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040520000692004052000069EA 2004 5 20 MASA200400200 120040414A33502013ASMI BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07650ML 7137 ASH NR 2917. CLT-BNA. OPERATIONS LEFT THE EMERGENCY LIGHTS ON AND RAN DOWN THE BATTERIES. MECHANIC REPLACED THE BATTERIES. OP CHECKS GOOD. 2L72 4F RTA21EA 20040520000842004052000084EU 2004 5 20 04FDEA001052 120040422A5320 BRACKET AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 N01236 MDCC LT SIDE BETWEEN SEAT TRACK 3 AND 4 FROM CENTER LINE AT FR 27 FLOOR PANEL HAS 2 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 2L72 4F RTA35EU 20040520000852004052000085EU 2004 5 20 04FDEA001053 120040422A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC LT SIDE NR 4 SEAT TRACK FROM CENTER LINE JUST FWD OF FR 27, 2 EA AREAS OF CORROSION, UPPER SURFACE. REPAIRED SEAT TRACK NR 4 LT FROM FR 26-27 TO FR 27-28 IAW A300-600 FREIGHTER SRM 53- 10-16 FIG 201 2L72 4F RTA35EU 20040520000872004052000087NM 2004 5 20 04FDEA001063 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040520000882004052000088NM 2004 5 20 04FDEA001064 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040520000892004052000089NM 2004 5 20 04FDEA001065 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040520000902004052000090NM 2004 5 20 04FDEA001067 120040423A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO, STA 1181 LT LONGERON 37 FOUND CRACK. **** S/D COMING **** 2L73 4F RTA22WE 20040520000912004052000091NM 2004 5 20 04FDEA001068 120040423A5330 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 AFT CARGO LONGERON SPLICE AT STA 1867-1887 RT LONGERON 40 FOUND CRACK. **** S/D COMING **** 2L73 4F RTA22WE 20040520000932004052000093NM 2004 5 20 QXEA200400280 120040421A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH127224495 510 TEST 1 POSITION ON THE FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR IS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520000942004052000094NM 2004 5 20 P5CA0401075 120040415A3260827932 PROXIMITY SWITCH BOEING747 7472D3B 1384805NM MLG FAILED A P5CAO OTHER N FALSE WARNING LDLANDING 1 WP23505MC 21251 LEFT "WING GEAR" ELECTRICAL HARNESS INSPECTION. REPLACED LEFT WING O/B (PRIM) PROX SWITCH (TILT) AND REPLACED LEFT WING GEAR INBD (ALT) TILT SWITCH. SECURED INBD PROX SWITCH MOUNT. CLEARANCE OK ON GEAR SWING. 2L74 4F RTA20WE 20040520000952004052000095NM 2004 5 20 P5CA0401072 120040414A29146606808 PUMP BOEING747 74746NF 13848BTNM HYD SYSTEM FAILED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23454PA 30812 AFTER STARTING ENG 1 & 4, OPERATING CONRTOL CHECK HYD PSI NR 3 FELL TO 80PSI, VERY SLOW TO COME UP, SPI VERY SLOW TO RESPOND. HYD SYSTEM FAULT LIGHT LOW PSI LIGHT CAME ON. DEFERRED NR 3 DEMAND PUMP, ON 4/17/04 R&R NR 3 ACMP, OPS AND LEAK CK OK. 2L74 4F RTA20WE 20040520000962004052000096NM 2004 5 20 P5CA0401073 120040415A5280 DOOR BOEING747 7472D3B 1384805NM LT WING DAMAGED A P5CAO OTHER O OTHER LDLANDING 1 WP23505MC 21251 LT WING GEAR LWR O/B STRUT DOOR DAMAGED. REMOVED AND ROUTED TO SHOP, OK TO INSTALL. INSTALLED DOOR PER MM. 2L74 4F RTA20WE 20040520000972004052000097EA 2004 5 20 QXEA200400281 120040421A2810 O-RING CNDAIRCL600 CL6002C10 1390015EA ZONE 100 MISSING A QXEAK NONE O OTHER UKUNKNOWN 1 NM09601QX6005 10009 A LEAK WAS NOTED COMING FROM THE CENTER FUEL TANK DURING THE POST FLIGHT WALK AROUND. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE O-RING MISSING ON THE FUEL MANIFOLD TUBE FITTING. A NEW O-RING WAS INSTALLED, OPERATIONAL AND LEAK CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040520000982004052000098NM 2004 5 20 QXEA200400282 120040413A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 OUT OF ADJUST A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09410QX5506 4053 SEVERAL TIMES DURING THE FLIGHT, THE LT AND RT GEAR DOOR MAIN UNSAFE AND GEAR HANDLE LIGHTS ILLUMINATED. A LOUD THUMP WAS HEARD FROM THE MAIN GEAR AREA, THEN THE LIGHTS WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE LANDING GEAR UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520001002004052000100WP 2004 5 20 ARWA20040301 120040317A53435753054502 FITTING DOUG DC8 DC863F 302198FWP NR 3 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YN 300 APPROX. FOOT STOOL FITTING LEFT SIDE WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING FROM NR 3 PYLON IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-000084, DATED 22-MAR-04, DOUGLAS AOL 8-854, S/B 57-84, DRAWING NUMBER TUI5753054-501/-502 SF1, DRAWING NR 5613906, 5753029 AND 5802738. 2L74 4F 4A25 20040520001022004052000102NM 2004 5 20 WRLA200415 120040407A2910 LINE DOUG MD11 MD11 3023602NM HYD SYSTEM BROKEN A WRLAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11273WA 48519 ACCORDING TO THE CAPTAIN'S REPORT: AFTER THE TAKEOFF FROM SBEG, DURING CLIMB AND AFTER SLAT RETRACTION,THE (HYD 3 FAIL)ALERT WAS ANNUNCIATED, AND COMPLETE LOSS OF SYSTEM 3 HYD. FLUID WAS NOTED,NO ACTION WAS POSSIBLE,PROCEEDED TO KFLL AND FOLLOWED CKECKLIST FOR NORMAL LANDING. FOUND HYD LINE BROKEN, AT KFLL REPAIRED THE LINE PER MD-11 MM 20-10-01 LEAKED CHECK GOOD, RETURN AIRCRAFT BACK TO SERVICE 2L73 4F RTA22WE 20040520001032004052000103 2004 5 20 IXXA0400021O 420040421A3418C25640643 COMPUTER DOUG DC8 DC871F 302199DWP STALL WARNING MALFUNCTIONED A IXXAC ABORTED TAKEOFF J WARNING INDICATION CLCLIMB 1 SW11820BX850802392 46065 AT V1, 121 KNOTS STALL WARING (SHAKER STICK) WENT OFF. HIGH SPEED ABORT 122 KNOTS BRAKE CHART 28 MILLION FT. LBS. 2.5 HOURS COOLING TIME REQUIRED. CREW RETURNED TO BLOCKS. AN INSPECTION IS ON GOING. AS SOON INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED LIFT COMPUTER. SYSTEM OPERATIONAL CHECK GOOD PER ALL APPLICABLE MANUALS. MAINTENANCE ALSO PERFORMED ATI JOB CARD 13.01-5 REJECTED TAKE OFF INSTPECTION. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040520001062004052000106EU 2004 5 20 RAIA00404011 120040420A3244AH52688 TIRE JETAIRJETSTMJETSTM4101 1500501EU NLG DEFLATED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03570HK 41089 LEFT NOSE TIRE FLAT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES. TIRE SHOP PEOPLE REPORT: TIRE SHOWED NO PUNCTURE, WHEEL BLOW OUT PLUG AND VALVE STEM OK. WHEEL HALF SEAL APPEARED GOOD. 2L72 4T RTA41NM 20040520001072004052000107SO 2004 5 20 RAIA00404010 120040419A5210 ROD EMB 145 EMB145 3260210SO PAX DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03807HK 145119 LOUD SQUEAL COMING FROM PAX DOOR. MAINTENANCE FOUND EXTERNAL DOOR ROD OUT OF RIG AND ADJUSTED ROD. GROUND RAN AND DID CABIN PRESSURE CK. 2L72 4F RTT00011AT 20040520001092004052000109WP 2004 5 20 MWEA040064 120040426A5330593271749 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LIGHTNING STRIKE ON UPPER CROWN AT STATION 1041 LONGERON LT. FABRICATED AND INSTALLED SKIN AND DOUBLER. 2L72 4F A6WE 20040520001102004052000110WP 2004 5 20 MWEA040065 120040426A55245930497501 BUSHING DOUG DC9 DC981 3022081WP LT ELEVATOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 LEFT ELEVATOR FORWARD SPAR AT STATION XE204, EYE BOLT MOUNT HAS CORROSION. -- FABRICATED AND INSTALLED BUSHING. 2L72 4F A6WE 20040520001112004052000111NM 2004 5 20 F3LA200400054 120040421A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM AT STA. 328, RBL 15 TO RBL 35. REMOVED DAMAGED TOP CHORD OF FLOOR BEAM, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-51 AND EA B3-53R10393. 2L72 4F RTA16WE 20040520001122004052000112NM 2004 5 20 F3LA200400055 120040425A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION AT FLOORBOARD HOLE AT STA 986, LBL 30, FLOOR BEAM UPPER CHORD. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-51, FIG. 101, DETAIL VII. REPLACED UPPER CHORD OF STA 986 FLOOR BEAM FROM SKIN TO SKIN PER EA B3-53R-10397, SRM 51-40-02, 51-40-05, 51-40-08 AND SOPM 20-41-02. 2L72 4F RTA16WE 20040520001142004052000114NM 2004 5 20 HNAA0400043 120040425A534785320490 SEAT TRACK DHAV DHC8 DHC8201 2809001NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07965HA 450 RIGHT HAND SEAT RAIL CORRODED IN AREA FRONT OF LAV.SPLICED IN SEAT RAIL IAW RD 8-53-3074. 2H72 4T RTA13NM 20040520001152004052000115NM 2004 5 20 04FDEA001054 120040422A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 FUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3. 2L73 4F RTA3WE 20040520001162004052000116NM 2004 5 20 04FDEA001055 120040422A5311651766445 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 FRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO .023 INCHES DEEP. FRAME THICKNESS IS .050 OUT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. ISNTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51-30-5. 2L73 4F RTA3WE 20040520001172004052000117NM 2004 5 20 04FDEA001056 120040422A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 LWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5. 2L73 4F RTA3WE 20040520001182004052000118NM 2004 5 20 04FDEA001057 120040422A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 EXTERNAL FUSELAGE SKIN CHAFE DAMAGED UNDER FAIRING CONTACT AREA, BS 950D 15 - 990, STR 23L - 26L. SKIN CHAFE FOUND OUT OF LIMITS BS 973-989 IAW SRM 53-30-1. REPAIRED SKIN IAW SRM 53- 30-3 FIG 3. BLEND OUT FROM 950D 15 - 950E 12, AND 950E 18 TO 973 FOUND TO BE WITHIN LIMITS PER 727 SRM 53-30-1. BLEND OUT FROM BS 950E 12 TO 950E 18 FOUND TO BE OUT OF LIMITS AND TO BE REPAIRED ON N01061. 2L73 4F RTA3WE 20040520001202004052000120NM 2004 5 20 04FDEA001059 120040422A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION STA 760 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS BS 760 DELTA BEAM LWR ANGLE. REMOVED AND INSTALLED NEW B S760 DELTA BEAM LWR ANGLE IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2L73 4F RTA3WE 20040520001222004052000122 2004 5 20 2419TR0026 420040424A3414 INDICATOR BOEING737 7372K5 138448XNM AIRSPEED MALFUNCTIONED A PIDAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO05249TR 22598 NO AIRSPEED INDICATION ON TAKE OFF ROLL - SPEED FLAG ON ADI. ELECTRICAL (BATTERY & APU GENERATOR) RESET PREFORMED. ADI OPSERATIONAL TEST PERFORMED SATISFACTORILY PER MM 34-22-0. ADC'S SWAPPED FOR TROUPBLE-SHOOTING PURPOSES AND SELF TEST PERFORMED SATISFACTORILY PER MM 34-12-0 2L72 4F RTA16WE 20040520001252004052000125 2004 5 20 249TR0026 420040424A3414 INDICATOR BOEING737 7372K5 138448XNM AIRSPEED INOPERATIVE A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05249TR 22598 NO AIRSPEED INDICATION ON TAKE OFF ROLL - SPEED FLAG ON ADI. ELECTRICAL (BATTERY & APU GENERATOR) RESET PERFORMED. ADI OPERATIONAL TEST PERFORMED SATISFACTORILY PER MM 34-22-0. ADC'S SWAPPED FOR TROUBLE-SHOOTING PURPOSES AND SELF TEST PERFORMED SATISFACTORILY PER MM 34-12-0 2L72 4F RTA16WE 20040520001262004052000126NM 2004 5 20 04FDEA001098 120040424A2780 DRUM DOUG DC10 DC10 N/A-SDRNM ZONE 500 WRONG PART A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 LT SLAT DRIVE MECHANISM FOLLOWUP CABLW DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACE DRUM FOR LEFT HAND SLAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9. 2L73 4F RTA22WE 20040520001282004052000128 2004 5 20 04FDEA001100 420040424A34166224563008 ALTIMETER DOUG DC10 DC10 N/A-SDRNM ZONE 200 MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. REMOVED AND REPLACED FIRST OFFICERS RADIO ALTIMETER INDICATOR IAW DC-10 MM 34-42-02. REPAIRED BROKEN WIRE AT CONNECTOR P1-1009 PIN J IAW DC-10 WDM 34-42-02. OPS CHECK OF RADIO ALTIMETER IAW DC-10 MM 34-42-00 GOOD. 2L73 4F RTA22WE 20040520001292004052000129NM 2004 5 20 04FDEA001101 120040424A5751 SKIN DOUG DC10 DC10 N/A-SDRNM ZONE 600 ERODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 RT OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUTOUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1. 2L73 4F RTA22WE 20040520001302004052000130NM 2004 5 20 04FDEA001102 120040424A323060008924 CONTROL UNIT DOUG DC10 DC10 N/A-SDRNM ZONE 700 FAILED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 ANTISKID FAILS (MULTIPLE REPEATS) REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTROL WIRING, FOUND SHORT AT RECEPTACLE R5-264, REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTISKID CONTROL UNIT FAULTY, REPLACED CONTROL UNIT, PERFORMED OPS CHECK, SYSTEM OPS CKECK GOOD, INSTALLED HUB CAPS, ALL IAW DC-10 MM 32-45-00 AND SWPM 20-31-03. 2L73 4F RTA22WE 20040520001312004052000131NM 2004 5 20 DHL2004764001 120040423A3350 BATTERY BOEING727 727264 138408MNM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01764AT 22984 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR BATTERY IS DEAD. REMOVED AND REPLACED L1 ENTRY DOOR LIGHT ASSEMBLY. OPS SERVICEABLE IAW M/M 33-50-71. 2L73 4F A3WE 20040520001322004052000132NE 2004 5 20 DHL2004760002 220040425A7200 ENGINE BOEING727 7272B7 138407LNM PWA JT8 JT8D17A 52049NE NR 1 SHUTDOWN A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01760AT 21954 715301 PERFORMED HUNG START PROCEDURES FOR THE NR 1 ENGINE DUE TO AFTER N2 WENT TO 40 PERCENT THE FUEL FLOW WENT TO 0 AND THE ENGINE SHUTDOWN. 2ND ATTEMPT SUCCESSFUL EXCEPT THE FUEL FLOW INITIALLY WENT TO 1700 THEN DROPPED TO NORMAL START PARAMETERS. RAN NR 1 ENGINE PER JRH 5.2, NO DEFECTS NOTED, ALL PARAMETERS ARE WITHIN LIMITS. 2L73 4F4 F A3WE E2EA 20040520001332004052000133WP 2004 5 20 2006 120040423A78305751935503 TRACK DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE THRUST REVERSER DAMAGED I U2RBK NONE P NO WARNING INDICATION ININSP/MAINT 1 GL23921R 6762031 46145 669644 POST FLIGHT INSPECTION NR 2 THRUST REVERSER AND TRANSLATING RING DAMAGED.LOWER T/R TRACK STOP AND ATTACHING HARDWARE MISSING. DOUGLAS SERVICE BULLETIN 78-100 IDENTIFIES THIS PROBLEM. 2L74 4F4 F 4A25 1E8 20040520001342004052000134NM 2004 5 20 QXEA200400283 120040421A335010126271 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 LT EMERGENCY EXIT LIGHT AT SIDE WALL INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520001382004052000138NE 2004 5 20 04017 220040426A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 FAILED A KCSAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL23712CK 19754 AT 100 FT AFTER TAKEOFF THE NR 2 ENGINE FAILED. 2L74 4F4 F A20WE E20EA 20040520001412004052000141NM 2004 5 20 C1HA200485004 120040426A5754 WEDGE BOEING727 7272S7 138407ZNM SLAT GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 NR 6 SLAT CRACK AT FASTNER HOLE/2 GOUGES IN WEDGE EXTRUSION 2L73 4F A3WE 20040520001432004052000143NM 2004 5 20 PCAA0404197 120040425A33506038443 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A PCAAO OTHER L NO TEST ININSP/MAINT 1 EA13808EX 299 WHILE IN MAINTENANCE IT WAS FOUND THAT THE FRONT TWO EMERGENCY EXIT LIGHTS DID NOT OPERATE DURING SYSTEM TEST. MAINTENACE FOUND BATTERY AT POSITION 500 AT FAULT. BATTERY REPLACED AND SYSTEM OPERATIONAL CHECK WAS GOOD. 2H72 4T RTA13NM 20040520001442004052000144NM 2004 5 20 PCAA0404198 120040425A3260 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003NM MLG MISRIGGED A PCAAO OTHER WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA13804EX 227 REPORTED HAVING THE RIGHT HAND AMBER GEAR DOOR LIGHT ILLUMINATE WHEN THE GEAR WAS RETRACTED. LIGHT WENT OUT WHEN GEAR WAS SELECTED DOWN. MAINTNANCE PERFORMED GEAR SWING AND CHECKED ADJUSTMENTS OF PROXIMITY SENSORS. MAINTENANCE FOUND THE RIGHT HAND MAIN LANDING GEAR FORWARD DOOR PROXIMITY SWITCH TO BE OUT OF RIG. SYSTEM WAS RIGGED AND THE GEAR SYSTEM OPERATIONAL CHECKED. ALL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520001452004052000145NE 2004 5 20 MWEA040066 220040426A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE RIGHT INOPERATIVE A MWEAC ABORTED TAKEOFF YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 GL31809ME 48071 P716739D RT ENGINE POWER LOSS AND VIBRATION ON TAKEOFF ROLL. N1, N2, AND EGT APPEARED NORMAL. EPR WOULD ACCELERATE ABOVE IDLE ON TAXI BACK. REMOVED AND REPLACED RT ENGINE. 2L72 4F4 F A6WE E9NE 20040520001462004052000146EU 2004 5 20 118041 120040427A3350 LIGHT SAAB SF340 340B 7860101EU SEAT 3A INOPERATIVE A NSVAK NONE L NO TEST ININSP/MAINT 1 EA27346CJ 346 INTERIOR LIGHTING SYSTEM, OVERHEAD EMERGENCY LIGHT INOP SEAT 3A. LIGHT MEL PER 33-52-2 2L72 4T RTA52EU 20040520001472004052000147EU 2004 5 20 XNOA1181 120040331A2420 GENERATOR AIRBUS300 A300B4203 3930306EU NR 2 INOPERATIVE A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23473AS 203 AT PUSHBACK IN SCK NR 2 GEN NO VOLT'S AND FREQ'S. SHUT DOWN ENG AND RETURNED TO THE GATE. R&R NR 2 GENERATOR CONTROL UNIT IAW A300 AMM 24-21-12 OPS CHECK GOOD. (STATUS:SUPP/CLOSED) 2L72 4F RTA35EU 20040520001482004052000148NM 2004 5 20 DHL2004783007 120040426A3350 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01783DH 21999 ON PRE-DEPARTURE, FOUND MAIN ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REM0VED AND REPLACED MAIN ENTRY ENTRY DOOR EMERGENCY EXIT LIGHT & OPS CHECKED GOOD PER B-727 M/M 33-50-01. LOANER EMERGENCY EXIT LIGHT P/N: 10-0067-9, S/N: 16213 INSTALLED ON MAIN ENTRY POSITION. TRANSFERRED TO DMI 16430L IAW ASTAR GMM 3.5 CAT. II. PLACARD INSTALLED. GREEN SHEET COMPLIED WITH. REF. DMI 16430, LOANER EMERGENCY EXIT LIGHT (ENTRY DOOR). REMOVED AND REPLACED ENTRY DOOR EMERGENCY EXIT LIGHT PER M/M 33-50-101, OPS CHECKED NORMAL IAW THIS CLEARS DMI 16430L. PLACARDS REMOVED. 2L73 4F A3WE 20040520001502004052000150WP 2004 5 20 ABXA040151 120040409A5315991224359 FLOORBEAM DOUG DC9 DC932 3022066WP AFT CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 FLOORBEAM CORRODED AT RIGHT BUTT LINE 44 STA. 965. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05. 2L72 4F A6WE 20040520001512004052000151WP 2004 5 20 ABXA040146 120040408A5330591141253 DOUBLER DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 ANTENNA SUPPORT CORRODED BETWEEN STA. 465 - 446 LONGERON 30 - 29 LT. REPLACED DOUBLER 5911412-53 AND 5911412-55 AIW DC-9 SRM 51-30-2 AQND 51-30-5. 2L72 4F A6WE 20040520001522004052000152WP 2004 5 20 ABXA040147 120040408A5330591141253 DOUBLER DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 ANTENNA SUPPORT CORRODED BETWEEN STA. 522 - 503, LONGERON 30 - 29 LT. REPLACED DOUBLERS AROUND THE ANTENNA IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20040520001532004052000153WP 2004 5 20 ABXA040148 120040408A53304912772505 DOUBLER DOUG DC9 DC932 3022066WP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 CORROSION AT STA. 226, LONGERON 18 RIGHT ON ANGLE DOUBLER. REPLACED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20040520001572004052000157WP 2004 5 20 ABXA040143 120040408A5320591412161 PAN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 MAIN ENTRY DOOR PAN CRACKED AT FORWARD LOWER STOP. REPAIRED DOOR IAW DC-9 SRM. 2L72 4F A6WE 20040520001582004052000158WP 2004 5 20 ABXA040144 120040408A53109957663503 BEAM DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 CRACK INDICATION FOUND ON FORWARD LOWER CARGO DOOR NR 2 BEAM TEE FORWARD END AT SKIN RIVET. REPAIRED AREA IAW DC-9 SRM K05159 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 20040520001592004052000159WP 2004 5 20 ABXA040145 120040408A53159912243127 FLOORBEAM DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 STA 965 FLOORBEAM STRAP CORRODED. REMOVED DAMAGED FLOORBEAM AT STA. 965 FROM LBL 54 - RBL 54. FABRICATED NEW FLOORBEAM IAW DACO DWG. 9912243. 2L72 4F A6WE 20040520001602004052000160WP 2004 5 20 ABXA040150 120040409A531199115057 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 ANGLE FORWARD OF CENTER WINDSHIELD AT LOWER RT OUTBOARD CORNER CRACKED. APPROXIMATE LENGTH 1.5 INCHES. REPAIRED ON REA D953-49620MR. 2L72 4F A6WE 20040520001612004052000161WP 2004 5 20 ABXA040154 120040414A53209910079209 ANGLE DOUG DC9 DC932 3022066WP FUSLAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 SPLICE ANGLE CORRODED AT STA 229, LONGERON 18 RIGHT. REPLACED SPLICE ANGLE IAW REA D953-49615. 2L72 4F A6WE 20040520001622004052000162WP 2004 5 20 DHL2004802004 120040427A574056423421 FITTING DOUG DC8 DC873 302199CWP LT WING CRACKED B DHLAK NONE O OTHER ININSP/MAINT 1 SW11802DH 46076 LT X3 WING TO FUSELAGE FITTING CRACKED. REMOVED AND REPLACED LT STA. X3 WING TO FUSELAGE FITTING IAW DOUGLAS DRAWING 589477 AND DC-8 SRM 51-1-20. 2L74 4F RT4A25 20040520001632004052000163NM 2004 5 20 0400596631 120040424A3350 BATTERY PACK BOEING747 747251B 1384892NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01631US 23111 DURING LINE CHECK, FOUND 'D' ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040520001642004052000164NM 2004 5 20 XNOA1185 120040427A3234 HOUSING BOEING727 727227 1384078NM SELECTOR VALVE CRACKED A XN0AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL2379754 21363 ON DEPARTURE LOST SYSTEM A HYDRAULIC FLUID. FOUND RT MAIN GEAR SELECTOR VALVE HOUSING CRACKED, R & R VALVE, OPS AND LEAK CHECK GOOD DURING GEAR SWING IAW B727 MM 32-33-31. (STATUS:ORIG/CLOSED) 2L73 4F A3WE 20040520001652004052000165NE 2004 5 20 2004UALA00370 220040419A7200 ENGINE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LEFT MALFUNCTIONED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29620UA 21880 DIVERTED DUE TO LOSS OF LT ENGINE POWER. ENGINE HUNG DURING ACCELERATION. TSI WAS 10 HRS. FOUND PCB 3.5, PTT2 TOTAL AIR TEMP AND PIR INTERSTAGE RETURN PSI TUBE FROM TT2 SENSOR LOOSE. ALL WERE SECURED AND SAFETIED. 2L72 4F4 FRTA1NM E3NE 20040520001662004052000166NM 2004 5 20 TSAA0427038 120040424A27823818001003 ACTUATOR BOEING737 73773A 1384606NM LE SLAT FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13738AL14854 28499 L/E FLAP TRANSIT LIGHT ON AFTER FLAP RETRACTION. SOME LEADING EDGE DEVICES REMAIN EXTENDED. OVERWEIGHT LANDING 151,300 LBS AT 50 FEET PER MINUTE. PHASE 1A REF 05-51-35-2, LANDING SINK RATE WAS LOW TO MODERATE, INSPECTION COMPLETE, NO DEFECTS NOTED. REPLACED EXTEND HYDRAULIC FUSE IAW AMM 27-81-61-4. GROUND OPS CHECK GOOD. REPLACED RETRACT HYDRAULIC FUSE IAW AMM 27-81-61-4. GROUND OPS CHECK GOOD. REPLACED NR 6 L/E SLAT ACTUATOR IAW AMM 27-81-41. OPS AND LEAK CHECK GOOD IAW AMM 27-81-00-700-802 AND 27-81-00-710-801. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040520001672004052000167NM 2004 5 20 TSAA0421039 120040425A21315483766 CONTROLLER BOEING737 73776N 13844CHNM A/C PACKS FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13740AL10983 28640 BOTH PACKS TRIPPED WHILE CLIMBING THROUGH 10,000 FT. SELECTED WARMER TEMP, RESET, BOTH PACKS TRIPPED AGAIN. LANDING WEIGHT 151,000 LBS. OVERWEIGHT LANDING INSPECTION PERFORMED IAW AMM 05-51-35-2, NO DEFECTS NOTED. ISOLATED TO CABIN TEMPERATURE CONTROLLER (FIM 21-52-00-810-834, SUBTASK 800-330) CONTROLLER REPLACED IAW AMM 21-61-01-4. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040520001692004052000169EU 2004 5 20 XNOA1184 120040426A3230 VALVE AIRBUS300 A300B4203 3930306EU MLG FAILED A XN0AL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL23371PC 157 ON APPROACH WHEN LANDING GEAR HANDLE EXTENDED GEAR DID NOT COME DOWN. MISSED APPROACH COMPLETED CHECK-LIST. L/G GRAVITY EXTENSION. ALL GEAR EXTENDED & LOCKED. NORMAL LANDING COMPLETED. R & R LANDING GEAR ELECTRO VALVE (3GA) OPS CK SYSTEM NORMAL IAW A300 AMM 32-31-12 (STATUS:SUPP/CLOSED). 2L72 4F RTA35EU 20040520001702004052000170CE 2004 5 20 GLBA20030617 120040426A3200 CIRCUIT BREAKER BEECH 1900 1900C 1154161CE MLG TRIPPED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03122GL UC122 GEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOOD 2L72 4T RTA24CE 20040520001712004052000171CE 2004 5 20 GLBA20030605 120040407A52301145140461 LATCH BEECH 1900 1900D 1154162CE CARGO DOOR DAMAGED A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03170GL UE170 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, R & R SAFETY LATCH PN 114-514046-1 OPS CK GOOD 2L72 4T RTA24CE 20040520001722004052000172EU 2004 5 20 MTNA20044 120040427A2612D1384N FIRE LOOP FOKKERF27 F27MK500 4990629EU LT ENGINE OPEN A MTNAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 SO33721FE 10460 AFTER TOUCHING DOWN IN IND FLIGHT 7201 BNA-IND THE LEFT ENGINE FIRE WARNING ILLUMINATED.THE CREW TAXIED THE AIRCRAFT OFF THE RUNWAY STOPPED THE AIRCRAFT PERFORMED THE ON GROUND EMERGENCY PROCEDURES AND DECLARED AND EMERGENCY WIHT ATC.NO EVIDENCE OF A FIRE WAS FOUND. THE AIRCRAFT TAXIED TO THE RAMP ON THE RIGHT ENGINE. MAINTENANCE FOUND A DEFECTIVE SECTION OF THE FIRE LOOP. THE SECTION WAS REPLACED ALONG WITH ONE FIRE BOTTLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T A817 20040520001742004052000174EA 2004 5 20 QXEA200400287 120040421A3244 TIRE CNDAIRCL600 CL6002C10 1390015EA NR 3 SEPARATED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09608QX 10026 THE CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF THE NR 3 MAIN TIRE RECAP CAME OFF. THIS SDR WILL REMAIN IN AN OPEN STATUS PENDING COMPLETION OF MAINTENANCE. THE NUMBER 3 MAIN TIRE WAS REPLACED WITH NEW. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. NOTE: THIS TIRE WAS AT RECAP LEVEL 1. RECAPPED TIRES ARE NO LONGER BEING. 2L72 4F RTA21EA 20040520001772004052000177EU 2004 5 20 KBM2004F00056 120040105A6320579069G BEARING SNIAS 350 AS350B2 8680813EU M/R GEARBOX WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 REMOVED MGB CROSSBEAM SUPPORT BAR DUE TO 2 EA. LAMINATED BEARINGS BEING WORN. REMOVED AND REPLACED. 1G71 3U H9EU 20040520001792004052000179EU 2004 5 20 KBM2004F00055 120040105A6320579065H BEARING SNIAS 350 AS350B2 8680813EU M/R GEAROBOX WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 REMOVED MGB CROSSBEAM SUPPORT BAR DUE TO 2 EA. LAMINATED BEARINGS ARE WORN OUT. REMOVED AND REPLACED. 1G71 3U H9EU 20040520001812004052000181EU 2004 5 20 KBM2004F00047 120040428A24507271825 CIRCUIT BREAKER SNIAS 350 AS350BA 8680817EU COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 25 AMP CONDENSOR CIRCUIT BREAKER (POPS) WHEN RUNNING AIR CONDITIONER. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040520001832004052000183EU 2004 5 20 KBM2004F00053 120040430A6220123668P BEARING SNIAS 350 AS350BA 8680817EU MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 BEARING FOUND WORN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040520001852004052000185EU 2004 5 20 KBM2004F00057 120040105A6420355A09103601 HOUSING SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV691 3296 TAIL ROTOR LAMINATED HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U H9EU 20040520001872004052000187EU 2004 5 20 KBM2004F00044 120040503A21210500847 MOTOR SNIAS 350 AS350BA 8680817EU BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P29 2347 BLOWER MOTOR, INOPERATIVE, CAUSING BELT TO BURN UP. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040520001892004052000189 2004 5 20 KBM2004F00051 420040429A2312069102409 SWITCH SNIAS 350 AS350B1 8680811EU VHF COM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA48 2143 NR 2 VHF VOLUME SWITCH, INOPERATIVE. REMOVED AND REPLACED. 1G71 3U H9EU 20040520001922004052000192NM 2004 5 20 QXEA200400288 120040423A1430 SCREW DHAV DHC8 DHC8202 2809007NM ZONE 800 LOOSE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09345PH16285 476 MAIN CABIN DOOR CATCHES ON OPENING. APPEARS TO BE CATCHING ON LOOSE HINGE SCREW. MAINTENANCE TIGHTENED SCREW ON MAIN CABIN DOOR HANDLES. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520001942004052000194NM 2004 5 20 QXEA200400290 120040426A1430 DOME NUT BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 MAINTENANCE FOUND A BAD DOME NUT ON PANEL 122BR. THE DOME NUT WAS REMOVED AND REPLACED IAW Q400SRM 51-42-05. 2H72 4T RTA13NM 20040520001952004052000195NM 2004 5 20 0400606303 120040423A2530 OVEN BOEING747 747451 1384940NM G2B GALLEY SMOKE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01663US 23818 DURING FLIGHT, SMOKE EMITTED FROM THE NBR 2 OVEN IN GALLEY 2B. PULLED CIRCUIT BREAKERS AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OVEN CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040520001982004052000198EA 2004 5 20 ASOA04274 120040407A5210601R317011 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STICKING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11880AS 7606 DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR STICKS DURING OPENING. MAINTENANCE INSPECTED THE PASSENGER DOOR AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520001992004052000199EU 2004 5 20 ASOA04271 120040405A3350E0062B1A4AC0A SWITCH AEROSPATR72 ATR72 EU EMERGENCY LIGHT SHORTED A ASOAO OTHER O OTHER CRCRUISE 1 SO11641AS 387 DURING FLIGHT FROM AGS-ATL, THE EMERGENCY EXIT LIGHTS ILLUMINATED IN THE ARMED POSITION AND EXTINGUISHED WHEN THE DISARMED POSITION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040520002002004052000200NM 2004 5 20 UIEA200400074 120040423A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1454 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520002012004052000201NM 2004 5 20 UIEA200400071 120040423A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORROSION WSTA 697 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520002022004052000202NM 2004 5 20 UIEA200400073 120040423A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORROSION WS 1434 STRINGER 13. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520002042004052000204NM 2004 5 20 UIEA200400076 120040423A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING LOWER SKIN CORROSION AROUND SURGE TANK SUMP DRAIN VALVE AT WS 1487. CORROSION BLENDED OUT AND REPAIRED AS PER FAA FORM 8110-3 DATED 19 JAN 2004, COPY ATTACHED FOR DETAILS OF HFEC INSPECTION REF COPY OF ATTACHED SJC A00064. (M) 2L74 4F A20WE 20040520002062004052000206NM 2004 5 20 UIEA200400072 120040423A5730 SKIN BOEING747 747243B 1384830NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND WING TOP SIDE SKIN CORROSION WSTA 440.62 STRINGER 19. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520002082004052000208NM 2004 5 20 UIEA200400069 120040423A5411 RIB BOEING747 747243B 1384830NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND INTERIOR RIB CRACKED AT NAC STA 318.20 RIGHT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TARNSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M) 2L74 4F A20WE 20040519000962004051900096CE 2004 5 19 3117504062004 120040406A5210 SWITCH LEAR 35 31 5170530CE PAX DOOR OUT OF RIG E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05131FX3499 31A175 DOOR WARNING LIGHT WOULD NOT EXTINGUISH. THE DOOR WAS VERIFIED AS PINNED AND THE ITEM WAS DEFERRED. ON TAKE-OFF, THE DOOR SEAL SQUEALED EXCESSIVELY AND THE AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT. SUBSEQUENT MAINTENANCE FOUND THE AFT DOOR PIN WAS MISSALIGNED AND HAD BROKEN THE DOOR LIGHT ACTUATING SWITCH. THE SWITCH WAS REPLACED AND THE DOOR RE-RIGGED. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA10CE 20040519000972004051900097CE 2004 5 19 6018203312004 120040331A3241 CONTROL BOX LEAR LEAR 60 60LEAR 5170707CE ANTI SKID SYS FAILED E J7SACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW05245FX J714B 60182 ON TAKE-OFF ROLL, ALL 4 ANTI-SKID LIGHTS ILLUMINATED. TAKE-OFF WAS ABORTED. AS AIRCRAFT SLOWED, LIGHTS EXTINGUISHED ONE BY ONE. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA10CE 20040519001002004051900100 2004 5 19 372PA0044 420040407A2210AR6460M2 ACTUATOR BOEING737 737306 13844BGNM AUTOPILOT SYS SHORTED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 DFCS HISTORY SHOWS AUTO-PILOT TRIM SERVO HAS NO RESPONSE. AUTO-PILOT COLUMN SWITCHING MODULE CHECKS OK PER MM 27-41-00. FOUND OPEN IN AUTO-PILOT STABILIZER TRIM ACTUATOR. REPLACED AUTO-PILOT STABILIZER TRIM SERVO AND OPS CHECKED PER MM 22-11-81. 2L72 4F RTA16NE 20040519001272004051900127NM 2004 5 19 EIA2004015 120040329A1420 PIN BOEING747 747132 1384882NM CONNECTOR DIRTY A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 EMERGENCY LIGHTS POWER PACK NOT CHARGING. PIN NR 10 AND 11 ON POWER PACK CLEANED AND RESEATED OPS CHECKED AS PER MM 33-51-05 2L74 4F A20WE 20040519001442004051900144CE 2004 5 19 DXTA200400278 120040327A3411 PITOT TUBE CESSNA750 750 2076810CE DAMAGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07919QS 7500224 ON TAKEOFF ROLL WITH UPPER AND LOWER YAW DAMPERS AND MACH TRIM IN A-CONFIGURATION, THE LOWER YAW DAMPER FAILED BETWEEN 50 AND 70 KTS, AMBER "YD OFF LOWER" EICAS MESSAGE APPEARED. REPLACED PITOT LINE TO NR 1 ADC PER 750 MM CHAPTER 34-11-01 LEAK CHECK GOOD. COMPLIED WITH PITOT / STATIC CHECK PER FAR 91.411, NO LEAKS NOTED, TIGHTENED LOOSE TERMINAL ON STANDBY POWER SWITCH, SYSTEM OP CHECK GOOD. 2L72 4J RTT00007WI 20040519001452004051900145CE 2004 5 19 DXTA200400279 120040328A27809914532 CONTROL VALVE CESSNA750 750 2076810CE SLATS LEAKING E DXTAA UNSCHED LANDING K FLUID LOSS DEDESCENT 1 GL07948QS 7500149 UPON GEAR EXTENSION HYDRAULIC FLUID LEVEL DROPPED BELOW 16 PERCENT, DIVERTED AIRCRAFT TO APA AND LANDED SAFELY. FOUND SLAT SPOOL VALVE LEAKING, REMOVED AND REPLACED VALVE, BLED A/B SYSTEM RESERVOIRS WITH (2) GALLONS OF SKYDROL EACH. LEAK CHECKED GOOD IAW THE CESSNA 750 MM CHAPTER 27-80-01. 2L72 4J RTT00007WI 20040519001532004051900153CE 2004 5 19 GLBA20030610 120040414A2120 SMOKE BEECH 1900 1900D 1154162CE COCKPIT DETECTED A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM03245GL UE245 SMOKE IN COCKPIT, CK ALL ACFT SYSTEMS CND 2L72 4T RTA24CE 20040519001542004051900154NE 2004 5 19 GLBA20030611 220040414A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LEFT OVERTEMP A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03247GL UE247 LT ENGINE TEMP LIMITED AT TAKE OFF, PREFORMED GROUND RUN ALL PARAMETERS WITHIN LIMITS 2L72 4T4 TRTA24CE E26NE 20040519001582004051900158NE 2004 5 19 PCAA0404189 320040414A6140V319 SWITCH DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF* NE POWER LEVER FAULTY A PCAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA13834EX 285 UPON ROTATION NOTED PROPELLAR RPM FLUCTUATION. CHECKLIST WAS FOLLOWED AND NORMAL OPERATION WAS RESTORED. CREW ELECTED TO RETURN TO LGA DUE TO PROXIMITY AND WEATHER. FLIGHT LANDED WITHOUT INCIDENT.LGA MAINTENANCE COMPLIED WITH MEL.ONCE AIRCRAFT IN MIDDLETOWN MAINTENANCE REMOVED AND REPLACED POWER LEVER SWITCH 6141-S3. SYSTEM OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 6 CP7NE 20040519001602004051900160NE 2004 5 19 00132 220040319A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE RIGHT FLAMED OUT E HAEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05233TW 24B221 251210A PILOT REPORTED RT ENGINE FLAMMED OUT CLIMBING THROUGH FL 39.5 AIRCRAFT DIVERTED TO GRI. MAINTENANCE DISPATCHED FROM ADS, FOUND NO FOD DAMAGE OR LEAKS, RESTRICTED AIRCRAFT 39K ALT AND HAD AIRCRAFT FLOWN TO ADS. WILL UPDATE AFTER FURTHER MAINTENANCE. CORRECTION MADE TO SERIAL NUMBER OF ENGINE 03/23/2004 ON THIS ENGINE. ENGINE REMOVED 04/06/2004 FOR INSPECTION. A DETAILED TEAR DOWN OF THE ENGINE FAILED TO ESTABLISH ANY ABNORMALITIES OR DEFECTS. BASED ON CONTINUED HISTORY OF THE ENGINE IT WAS REMOVED FROM THE SERVICE POOL AND PARTED OUT. 2L72 4J4 J A10CE 1E16 20040519001642004051900164SO 2004 5 19 RAIA00404006 120040415A27201170A80001 POTENTIOMETER EMB 145 EMB145LR 3260212SO RUDDER MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03834HK 145269 AIRCRAFT PULLS TO RIGHT ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED RUDDER POT. OPS CK GOOD OF HIGH SPEED TAXI WITH CREW. 2L72 4T RTT00011AT 20040519001692004051900169NM 2004 5 19 QXEA200400268 120040416A33506138001 POWER SUPPLY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09403QX4943 1457 4037 WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM, LIGHTS AT THE AFT CABIN DOORS AND REAR EGRESS DID NOT WORK. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001772004051900177NM 2004 5 19 PCAA0404191 120040415A5330 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13809EX 302 MAINTENANCE REPORTED A HOLE IN FUSELAGE AFT OF AIRSTAIR DOOR AT STATION 264.THE HOLE WAS REPAIRED PER CALLAHAN RD CAS-AAL170, WHICH REQUIRED THE DAMAGE BE REMOVED AND CRACK CHECKED THEN INSTALLING A BOLT WASHER AND NUT AND SEALING SAME WITH PRC.DAMAGE DRAWING WAS SUBMITTED TO BOMBARDIER FOR TOLERANT ANALYSIS. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519001812004051900181WP 2004 5 19 0400559605 120040417A21312075301AA CONTROLLER DOUG DC9 DC932 3022066WP CABIN PRESSURE FAILED A NWAAB EMER. DESCENT JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 GL01605NW 47223 DURING CRUISE AT FL350 THE CABIN BEGAN AN UNCONTROLLED CLIMB. MANUAL CONTROL HAD NO EFFECT SO THE FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. IT IS NOTED THE CREW WAS ABLE TO REGAIN MANUAL CONTROL DURING THE DESCENT. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BITE WHICH FAULTED THE NR 1 CONTROLLER. AFTER REPLACEMENT OF THE FAILED CONTROLLED BITE OF BOTH CONTROLLERS SHOWED NO FAULTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 20040519001822004051900182NM 2004 5 19 F3LA200400047 120040308A5311 FRAME BOEING737 7373S1 138447SNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED BODY FRAME CRACKED AND BENT IN FWD CARGO COMPARTMENT AT STA 460, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-00-07, FIG. 203. 2L72 4F RTA16WE 20040519001842004051900184EU 2004 5 19 U30A200400004 120040418A2760 SPOILER AIRBUS320 A320214 3930316EU WINGS MALFUNCTIONED A U30AL ABORTED APPROACH E VIBRATION/BUFFET APAPPROACH 1 EA17266AV 1152 DURING APPROACH, THE CREW SELECTED FULL FLAPS AND THE AIRPLANE STARTED TO VIBRATE. THE CREW ELECTED TO PERFORM A GO-AROUND AND PERFORM THE LANDING USING FLAPS IN CONFIGURATION 3. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. NOTE: THE NR 1 SPOILER HAD PREVIOUSLY FAULTED EARLIER THIS DAY AND WAS DEFERRED PER MEL 27-64-01. THIS MEL PROCEDURE REQUIRES THE DEACTIVATION OF BOTH NR 1 SPOILERS. DEACTIVATION PROCEDURE IS CURRENTLY UNDER REVIEW AND INVESTIGATION. THIS SDR IS OPEN STATUS, AWAITING FURTHER INFORMATION. 2L72 4F RTA28NM 20040519001972004051900197NM 2004 5 19 QXEA200400276 120040420A3010 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 ILLUMINATED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09346PH 477 ON FLIGHT 2219 DURING DESCENT WITH BOTH POWER LEVERS AT FLIGHT IDLE, THE DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. AS POWER WAS ADVANCED CAUTION LIGHT WOULD EXTINGUISH. THIS OCCURED WEATHER FAST OR SLOW CYCLE WAS SELECTED AND ALSO AFTER ISO VALVE WAS SELECTED TO ISO AS PER THE CHECKLIST. PRESSURE ON BOTH NEEDLES ON THE DE-ICE PRESSURE GUAGE WAS 10 PSI AT FLIGHT IDLE. COMPLIED WITH AMM TASK 30-10-00-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519002152004051900215NM 2004 5 19 EIA2004025 120040421A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 STA 340 LT UPPER DECT FLOORBEAM TO FRAME INTERFACE HAS ELONGATED HOLES. OVERSIZED ELONGATED HOLES AT BS 340 LT FLOORBEAM TO FRAME INTERFACE TO ROUND CONDITION PER ECRA 486-53-25-2, PART B, STEP 2. HFEC & 10X VISUAL INSP SHOWS HOLES ARE CRACK AND CORROSION FREE. (ECRA 486-53-025-2,PART B, STEPS 2-3) 2L74 4F A20WE 20040519002252004051900225CE 2004 5 19 60013 120040326A5220 MECHANISM BEECH 1900 1900D 1154162CE EMERGENCY EXIT LACK OF LUBE A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07159YV UE159 EMERG/EXIT 4C HANDLE NOT FLUSH ON EXT/W/INT FLUSH. CLEANED & LUBED EMERG/EXIT 4C MECHANISM 2L72 4T RTA24CE 20040519002292004051900229CE 2004 5 19 60146 120040330A5260 AIRSTAIR BEECH 1900 1900D 1154162CE FUSELAGE DAMAGED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07163YV UE163 AIRCRAFT DOOR WOULD NOT LOCK PROPERLY FROM THE INSIDE. MAINTENANCE CALL AND AIRCRAFT WAS MOVED TO THE HANGAR FOR REPAIRS. PERFORMED AIRSTAIR DOOR HONYECOMB INSERT. REPAIR AND SERVICE BULLENTIN 52-3099. RIGGED DOOR. P/N MS2469AS71 2L72 4T RTA24CE 20040519002352004051900235NM 2004 5 19 04FDEA001030 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002402004051900240NM 2004 5 19 04FDEA001035 120040422A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002472004051900247NM 2004 5 19 04FDEA001042 120040422A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTRE CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 TO STA 1541, STR 38 LONGERON SPLICE FOUND CRACKED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002522004051900252EU 2004 5 19 04FDEA001048 120040422A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 4TH SEAT TRACK RT SIDE FROM CENTER LINE AT FR 27 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED DAMAGED SECTION IAW A300-600 SRM 53-10-16 FIG 201 2L72 4F RTA35EU 20040520000012004052000001NM 2004 5 20 UIEA200400054 120040421A5712 RIB BOEING747 747243B 1384830NM LT WING LE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING LE PARTIAL RIB AT ILES 414.5 HAS A 4.5 INCH CRACK LONGITUDAL ACROSS ITS WEB JUST BEHIND THE FORWARD RIB SECTION. CRACKED WEB REPAIRED PER SRM 51-40-02. (M) 2L74 4F A20WE 20040520000042004052000004NM 2004 5 20 UIEA200400052 120040421A5347 SEAT TRACK BOEING747 747243B 1384830NM FUSELAGE DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 UPPER DECK SEAT TRACK CROWN HAS 2 OF THE LIPS SHEARED OFF AT STATION 660 LBL 46.65. DAMAGED SEAT TRACK SECTION TRIMMED OUT AND REPAIR SECTION SPLICED ON IAW SRM 53-10-05. (M) 2L74 4F A20WE 20040520000092004052000009NM 2004 5 20 UIEA200400063 120040422A5711 SPAR BOEING747 747243B 1384830NM LT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA155700 23300 FOUND LEFT WING UPPER MID SPAR WEB SURFACE FROM MSS 446.41 TO MSS 475.62 FOUND 2 CRACKS OF 5MM AND 16MM IN LENGTH REF TO NDT REPORT NR 276/03. CARRIED OUT HFEC INSPECTION ON THE CUTOUT SURFACE WEB AS PER NTM PART 6 51-00-00 FIG 4. NIL CRACK INDICATED. CRACKED MID SPAR WEB REPAIRED AS PER SRM 57-10-06 FIG 5. (M) 2L74 4F A20WE 20040520000122004052000012NM 2004 5 20 USAA040096 120040401A5312 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19576US50106 23741 FOUND AFT PRESSURE BULKHEAD CORRODED 2 FEET BY 2 INCH AREA, FROM LBL .5 TO RBL 5 INCHES IN FRONT OF CHANNEL STIFFENER. INSTALLED FILLERS, DOUBLERS AND STIFFENERS PER BAC DWG 65C28106, SRM 51-40-02, 53-80-08, EA 781171. (M) 2L72 4F RTA16WE 20040520000172004052000017EU 2004 5 20 USAABA04006 120040413A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHTSINOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19676UW 0375 PHL - FOUND L1 DORO EPSU BATTERIES FAILED ON OPERATIONAL CHECK, AND THE EPSU BATTERIES AT DOORS L2, R2 AND R4 FAILED ON THE CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERIES AT THE FOUR EPSU'S. (M) 2L72 4F RTA46NM 20040520000232004052000023NM 2004 5 20 UIEA200400080 120040423A5730 ANGLE BOEING747 747243B 1384830NM RT WING TE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND RT WING T/E UPPER FIXED PANEL LONGITUDINAL SUPPORT BEAM FORWARD L-ANGLE CRACK AT WBL 130.0. REPLACED CRACKED SUPPORT ANGLE WRT SRM 51-30-02. (M) 2L74 4F A20WE 20040520000282004052000028NM 2004 5 20 USAA040111 120040404A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19373US 22952 CLT - FOUND SKIN CRACKED .600 INCH LONG, S22R 12 INCHES AFT OF FS 727D. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040520000392004052000039NM 2004 5 20 USAABB04035 120040416A2560SG9601 GLOWSTRIP BOEING757 757225 1384959NM CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 CLT - FOUND EMERGENCY LIGHT PHOTOLUMINESCENT STRIPS MISSING AT ROW 1 AND BETWEEN ROWS 2 AND 3. MAINTENANCE REPLACED THE STRIPS. (M) 2L72 4F RTA2NM 20040520000422004052000042NM 2004 5 20 USAABB04037 120040421A335020131A BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19627AU 27805 TPA - FOUND EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE FORWARD AISLE. OPS CHECKS OK. (M) 2L72 4F RTA2NM 20040520000432004052000043NM 2004 5 20 USAA040099 120040401A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19576US50106 23741 PIT - FOUND SHELF CRACKED 2 INCHES IN LENGTH, AFT END OF RIGHT 18A SHELF INTO FIRST FASTENER. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M) 2L72 4F RTA16WE 20040520000442004052000044EU 2004 5 20 USAAEM04004 120040416A32349037B0001012 CONTROL LEVER EMB ERJ170ERJ170100 EU MLG INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19802MD 17000013 CREW WAS UNABLE TO MOVED THE LANDING GEAR LEVER TO THE 'UP' POSITION AFTER TAKEOFF. FLIGHT RETURNED TO EWR WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE. OPERATIONALLY CHECKS SATISFACTORY. (M) 2L74 4F RTA56NM 20040520000512004052000051NM 2004 5 20 CALA0400492 120040516A531565C33947 FLOORBEAM BOEING737 737524 1384721NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723661 28922 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 927, BL 0, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53-60-51, FIGURE 203. 2L72 4F RTA16WE 20040520000572004052000057NM 2004 5 20 MWEA040078 120040514A53305953050137 SKIN BOEING717 717200 1383700NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31916ME 55179 HOLE IN FUSELAGE SKIN MEASURING 12 INCHES X 4 INCHES AT STATION 422 BETWEEN LONGERON 26 LT AND 24 LT. SPLICE IN NEW SECTION OF SKIN. 2L72 4F TRA6WE 20040520000642004052000064NM 2004 5 20 04FDEA01087 120040424A53131D1104T7150 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO STA 1791 LT LONGERON 41. REPAIR CARRIED OUT IAW SRM 53-10-00 VOL. I. 2L73 4F RTA22WE 20040520000702004052000070EA 2004 5 20 MASA200400212 120040420A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747239 7239 SUPP ASH 7173. TUS CREW REPORTED 2 NON-ADJACENT CEILING EMERGENCY LIGHTS INOPERATIVE. MECHANIC PLACED ON MEL. MECHANIC RELAMPED. OPS CHECK GOOD. 2L72 4F RTA21EA 20040520000792004052000079NE 2004 5 20 227681 220040517A7261 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F25 NE RIGHT MALFUNCTIONED A UHLAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17123XS 123 207 DRG438589 ON 05-17-04 APPROX. 1500 (UTC), FLT 9407, DURING CLIMB, THE CREW NOTICED RT OIL PRESSURE LIGHT ILLUMINATED IN CLIMB. RT ENGINE WAS SHUTDOWN, CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040520001012004052000101WP 2004 5 20 ARWA20040202 120040202A5320 WEB DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE INTERIOR BETWEEN STA 1060.000 AND STA 1080.000 LT CUSP WITH CORROSION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING ROD SKETCH 04-05-18-001. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR. 2L74 4F 4A25 20040520001052004052000105SO 2004 5 20 RAIA00404012 120040420A3350548318 HANDSET EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03827HK6829 145021 CABIN CALL AND CABIN EMERGENCY LIGHT WILL NO EXTINGUISH. MAINTENANCE REMOVED AND REPLACED CABIN FORWARD HANDSET. 2L72 4F RTT00011AT 20040520001232004052000123WP 2004 5 20 DHL2004873004 120040423A5610 WINDSHIELD DOUG DC8 DC873F 302199FWP COCKPIT CRACKED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 RT WINDSHIELD (R1) HAS A 6 INCHES CRACK IN THE LOWER LT CORNER. CRACK IS IN OUTER PANE. CRACK DOES NOT OBSTRUCT VIEW. R & R RT WINDSHIELD IAW M/M 56-10-2. WINDSHIELD HEAT TESTED OK. 2L74 4F RT4A25 20040520001362004052000136NM 2004 5 20 QXEA200400285 120040423A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 PDX- DENT ON LT SIDE OF FUSELAGE 6 INCHES AFT OF ICE SHIELD AND 3 INCHES ABOVE STRINGER 13. REPAIRED IAW Q400 RD 8/4-53-666. 2H72 4T RTA13NM 20040520001372004052000137EA 2004 5 20 QXEA200400286 120040422A2150 EXHAUST LOUVER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09614QX 10049 RT ACM EXHAUST LOUVER MISSING FROM EXHAUST DUCT. INSTALLED RIGHT HAND ACM EXHAUST DUCT POUVER ASSEMBLY IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20040520001402004052000140NM 2004 5 20 C1HA200485005 120040426A5752 WEDGE BOEING727 7272S7 138407ZNM AILERON DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 LT OTBRD AILERON TRAILING EDGE WEDGE DELAMINATED 2L73 4F A3WE 20040520001542004052000154WP 2004 5 20 ABXA040149 120040408A531099115033 SHEAR TIE DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 CORROSION ON SHEAR TIE STA 851 ABOUT 6 INCHES ABOVE LONGERON 15 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM. 2L72 4F A6WE 20040520001552004052000155WP 2004 5 20 ABXA040152 120040409A531199196192 FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 RIGHT AFT MAIN FRAME AT STA. 737 WAS CRACKED AT POINTS E TO D AND G TO J. REPAIRED MAIN FRAME STA. 737 RIGHT IAW EA 30686. 2L72 4F A6WE 20040520001562004052000156WP 2004 5 20 ABXA040153 120040412A532099105035 WEB DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 LT CUSP WEB CRACKED AT FS 965. REPAIRED LT CUSP WEB AT FS 965. 2L72 4F A6WE 20040520001732004052000173WP 2004 5 20 MWEA040067 120040427A5522593055713 SKIN DOUG DC9 DC981 3022081WP LT ELEVATOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 LEFT ELEVATOR, UPPER SKIN MOST FORWARD INBOARD SECTION HAS A CRACK EMANATING OUT OF ATTACHMENT HOLE 3/4 INCH. FABRICATED AND INSTALLED FAIRING (UPPER INBOARD SKIN). 2L72 4F A6WE 20040520001762004052000176EU 2004 5 20 KBM2004F00046 120040127A3150KW9 HORN SNIAS 350 AS350BA 8680817EU LOW ROTOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 LOW ROTOR WARNING, INOPERATIVE, DURING RUN UP CHECK. REMOVED AND REPLACED WITH NEW. 1G71 3U NCH9EU 20040520001972004052000197NM 2004 5 20 2004F00109 120040428A3240 BRAKE HONEYWELL BOEING727 727200 138407ENM LANDING GEAR DAMAGED A K NONE O OTHER ININSP/MAINT 1 SO25 B4874B4837 N216FE NEWLY MANUFACTURED, BRAKES WERE REMOVED, AFTER MAINTENANCE INSPECTION REVEALED BRAKE WAS COMING APART BETWEEN HEAT STACK AND PISTON HOUSING ASSEMBLY INTERFACE.REVIEW AT REPAIR FACILITY FOUND: 7 OF 8 TIE BOLTS WERE MISSING OF BRAKE SERIAL B4874. POSITION NR 1. 8 OF 8 SAFETY CABLES WERE BROKEN AND ALL 8 TIE BOLTS WERE LOOSE ON SERIAL B4837 POSITION NR 2. BRAKES WILL BE REVIEWED BY MANUFACTURE FOR ROOT CAUSE DETERMINATION. 2L73 4F RTA3WE 20040520002032004052000203EA 2004 5 20 ASOA04282 120040410A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11877AS 7579 FLT 4732 - DURING AN A-CHECK IN BTR, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520002052004052000205NM 2004 5 20 UIEA200400075 120040423A5730 SKIN BOEING747 747243B 1384830NM FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1392 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M) 2L74 4F A20WE 20040520002072004052000207NM 2004 5 20 UIEA200400070 120040423A5411 RIB BOEING747 747243B 1384830NM NR 3 NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND INTERIOR RIB CRACKED AT NAC STA 300 LEFT SIDE NR 3 PYLON LOWER AREA. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING SEP-SIN-04-00049H. (M) 2L74 4F A20WE 20040520002162004052000216WP 2004 5 20 GTIA040323 120040325A3201 SPLASH GUARD DOUG DC9 DC983 3022083WP NOSE WHEEL BENT A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND NOSE WHEEL SPLASH GUARD RIGHT BENT AND SEPARATING AT RUBBER SEAL LEFT BENT AND RUST ON RUB PLATE. REMOVED RUB PLATES. FABRICATE NEW NOSE WHEEL RUB PLATES. INSTALLED NOSE WHEEL RUB PLATES. (M) 2L72 4F RTA6WE 20040520002182004052000218 2004 5 20 GTIA040326 420040415A2565 CABLE DOUG DC9 DC981 3022081WP EXIT SLIDE DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 0610 48017 FOUND DOOR 1R EMERGENCY EXIT SLIDE HAS CABLES PROTRUDING FROM COVER. REPLACED SLIDE ASSEMBLY, DOOR 1R. (M) 2L72 4F A6WE 20040520002192004052000219 2004 5 20 GTIA040327 420040415A2565 HINGE DOUG DC9 DC983 3022083WP L2 DOOR SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 DTW - FLT 844 - FOUND L2 DOOR SLIDE PACK GIRT BAR HANDLE HINGES ARE LOOSE AND DO NOT HOLD GIRT BAR. FOUND GIRT BAR RETAINING BRACKET ON SLIDE COVER TO NEED ADJUSTING. ADJUSTED RETAINING BRACKET. NO FURTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040520002242004052000224EA 2004 5 20 ASOA04256 120040330A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040520002252004052000225EA 2004 5 20 ASOA04255 120040330A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER WEB NEAR BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER WEB NEAR BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040520002262004052000226WP 2004 5 20 GTIA040320 120040322A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND LEFT MAIN CABIN CUSP WEB STATION 515, STATION 520, STATION 525, STATION 550, STATION 570, STATION 572, STATION 565 AND STATION 580 HAS CORROSION. REMOVED CORRODED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M) 2L72 4F RTA6WE 20040520002282004052000228WP 2004 5 20 GTIA040322 120040322A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND LEFT MAIN CABIN CUSP WEB STATION 612, 625, 630, 664, CORRODED, STATION 645 HAS BARE METAL, STATION 668 IS PUNCTURED. REMOVED CORRODED WEB. FABRICATED NEW WEB. INSTALLED NEW WEB. (M) 2L72 4F RTA6WE 20040520002292004052000229EA 2004 5 20 ASOA04254 120040330A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE LT AND RT CARGO COMPARTMENT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT CARGO COMPARTMENT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040520002342004052000234EA 2004 5 20 ASOA04251 120040329A3350BF50390901 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20040520002352004052000235EA 2004 5 20 ASOA04252 120040329A3350BF50357901 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE FORAWRD CEILING EMERGENCY EXIT LIGHT LENS WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CEILING EMERGENCY EXI LIGHT LENS. (M) 2L72 4F RTA21EA 20040520002372004052000237EA 2004 5 20 ASOA04253 120040330A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE ELFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RLB 9. (M) 2L72 4F RTA21EA 20040520002382004052000238 2004 5 20 USAAEM04002 420040408A2565 SLIDE EMB ERJ170ERJ170100 EU PAX DOOR DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19801MA 17000012 PHL - SLIDE ON MAIN ENTRY DOOR BECAME UNRAVELED. (M) 2L74 4F RTA56NM 20040520002402004052000240EA 2004 5 20 ASOA04269 120040405A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE LEFT WING BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT WING BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20040520002422004052000242EA 2004 5 20 ASOA04267 120040405A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL WAS FOUND CORRODED AND CRACKED ON THE FORWARD EDGE BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR SILL. (M) 2L72 4F RTA21EA 20040520002572004052000257EA 2004 5 20 ASOA04266 120040405A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11870AS 7530 FLT 4755 - DURING A GROUND INSPECTION IN DFW, AN EMEREGNCY OVERWING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY OVERWING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520002582004052000258EA 2004 5 20 ASOA04258 120040330A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER ATTACH ANGLE AT THE FASTENER HOLE WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ENGINE SUPPORT BEAM UPPER ATTACH ANGLE IAW SRM 51-42-20. (M) 2L72 4F RTA21EA 20040520002592004052000259EA 2004 5 20 ASOA04265 120040404A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11858AS 7417 FLT 4887 - DUIRNG A GROUND INSPECTION IN DFW, THE OVERHEAD EMERGENCY LIGHTS AT ROWS FIVE AND FOURTEEN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT LAMPS AT ROWS FIVE AND FOURTEEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520002602004052000260EU 2004 5 20 ASOA04257 120040330A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11536AS 465 DURING A HANGAR CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040520002612004052000261WP 2004 5 20 GTIA040321 120040319A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - PASSENGER CABIN STATION 712-731 STRINGER 18R WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. FABRICATED REPAIR CUSP WEB. INSTALLED REPAIR AND REPAIR SPLICE. (M) 2L72 4F RTA6WE 20040520002632004052000263EA 2004 5 20 ASOA04264 120040404A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 FLT 4667 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520002642004052000264EU 2004 5 20 ASOA04263 120040403A3350 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN MALFUNCTIONED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11533AS 460 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHTS ILLUMINATED WHILE IN THE ARMED POSITION. MAINTENANCE OPERATED THE EMERGENCY FLOOR LIGHTS SYSTEM AND NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040520002652004052000265EA 2004 5 20 ASOA04261 120040331A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP PANEL WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP ASSEMBLY. (M) 2L72 4F RTA21EA 20040520002662004052000266EA 2004 5 20 ASOA04260 120040331A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11907EV 7648 FLT 4242 - DURING A GROUND INSPECTION IN BTR, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520002672004052000267EA 2004 5 20 ASOA04259 120040329A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP IAW SRM 51-74-06. (M) 2L72 4F RTA21EA 20040520002702004052000270EU 2004 5 20 KBM2004F00059 120040323A5310350A07272071 CROSSBEAM SNIAS 350 AS350B2 8680813EU FUSELAGE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV3971 3296 CROSSBEAM LAMINATED BEARING. REMOVED AND REPLACED. 1G71 3U H9EU 20040520002712004052000271EU 2004 5 20 KBM2004F00065 120040118A2150050143 MOTOR SNIAS 350 AS350B2 8680813EU EVAPORATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 OVERHEAD VENTS DO NOT BLOW AIR WHEN THE AC OR FAN ACTIVATED. AFT EVAPORATOR MOTOR INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H9EU 20040520002722004052000272EU 2004 5 20 KBM2004F00061 120040503A7921MS5750V01 MOTOR SNIAS 350 AS350B2 8680813EU OIL COOLER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 OIL COOLER HARD TO TURN. REMOVED AND REPLACED. 1G71 3U H9EU 20040520002732004052000273EU 2004 5 20 KBM2004F00064 120040514A5280 PIN SNIAS 350 AS350B2 8680813EU LT MLG DOOR UNLATCHED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 LT MAIN DOOR POPPED OPEN IN FLIGHT, TOP PIN UNLATCHED. FILED DOWN A GROVE AND THE UPPER STAPLE AS NEEDED. 1G71 3U H9EU 20040520002742004052000274EU 2004 5 20 KBM2004F00066 120040503A6420350A33215001 BALL END SNIAS 350 AS350B2 8680813EU T/R SPIDER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 TAIL ROTOR SPIDER END BEARINGS WORN, REQUS REPLACEMENT. REMOVED AND REPLACED. 1G71 3U H9EU 20040520002752004052000275NE 2004 5 20 KBM2004F00062 220040503A7314P94B12209 PUMP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE FUEL SYSTEM INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV4182 3296 FUEL PUMP, UNIT INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040520002762004052000276EU 2004 5 20 KBM2004F00067 120040407A6711704A34130184 CONTROL BOX SNIAS 350 AS350B2 8680813EU T/R CABLE CNTRL CHAFED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 ANTI-TORQUE PEDALS FEELS AS IF A COMPONENT IS SCRAPING. REMOVED AND REPLACED. 1G71 3U H9EU 20040520002772004052000277EU 2004 5 20 KBM2004F00058 120040204A77145007155 PICKUP SNIAS 350 AS350B2 8680813EU NR INDICATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 NR NEEDLE WENT TO ZERO IN FLIGHT. REMOVED AND REPLACED. 1G71 3U H9EU 20040520002782004052000278NE 2004 5 20 KBM2004F00063 220040504A75329560154920 COUPLER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE BLEED VALVE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 BLEED VALVE WILL NOT CLOSE AT 96-100 PERCENT NG. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040520002792004052000279EU 2004 5 20 KBM2004F00060 120040323A24359560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU STARTER GEN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 STARTER GEN FLANGE MAGNETIC SEAL IS LEAKING. REMOVED AND REPLACED. 1G71 3U H9EU 20040520002812004052000281SO 2004 5 20 RAIA00404014 120040423A243132248001 BATTERY EMB 145 EMB145 3260210SO NR 1 OVERHEATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK820 137 145068 BAT 1 OVHT MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY. 2L72 4F RTT00011AT 20040520002832004052000283SO 2004 5 20 RAIA00404016 120040426A36104800112 SWITCH EMB 145 EMB145 3260210SO BLEED VALVE INOPERATIVE A RAIAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 CE03809HK 145187 UNABLE TO CROSS START - CROSS BLEED VALVE WOULD NOT OPEN. MAINTENANCE REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH. 2L72 4F RTT00011AT 20040520002852004052000285 2004 5 20 304AW0006 420040425A22104051601938 PANEL BOEING737 7373G7 1384595NM MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05304AW 24011 MODE CONTROL PANEL SWITCHES, N1, SPD, VNAV, LNAV, ALT HLD & V/S INDICATORS INOP. PLACED ON MEL 22-15-8. NOTE: MAINTENANCE INDUCED PROBLEM WHILE REPLACING ONE LIGHT BULB IN PANEL. 04/26/2004: REPLACED MCP AND OPS CHECKED PER MM 22-11-34. CLEARED MEL. 2L72 4F RTA16WE 20040520002872004052000287EU 2004 5 20 DHL2004364501 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, 9TH SEAT TRACK HAS HEAVY CORROSION IN TRACK & FLANGES FRAME 20. REMOVED CORROSION FROM SEAT TRACK FLANGE & CENTER SECTION AT FR. 19-20, RBL 57, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION FROM FR. 18.5-20.5, RBL 57. TRIMMED NEW SEAT TRACK SECTION. TREATED PRIMMED AND POLYWHITED NEW PARTS IAW A-300 SRM. FOUND CAP FWD OF SEAT TRACK AT APPROX. FR. 18.5 CORRODED ON UPPER SURFACE. REPLACED LAP FWD OF SEAT TRACK FR. 18.5 PER A-300 SRM. CABIN 9TH SEAT TRACK FROM LT. SIDE HEAVY CORROSION IN TRACK & FLANGES FRAME 20. REPLACED SEAT TRACK NR 9 FROM LT SIDE FROM FR. 18.5 TO 20.5 IAW A-300 SRMS. 2L72 4F RTA35EU 20040520002882004052000288EU 2004 5 20 DHL2004364502 120040316A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN CARGO COMPT SEAT TRACK FLANGE HAS CORROSION AT FR. 23. LBL. 37. REMOVED CORROSION FROM SEAT TRACK FLANGE AT FR. 23, LBL 37, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SEAT TRACK SECTION FROM FR. 23.5 TO FR. 15. TRIMED TO FIT NEW SEAT TRACK SECTION FROM FR.23.5 TO FR. 15 AND SPLICES ANGLES AT FR. 235. TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SECTION AND REPAIR ANGLES. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES AT FR. 23.5 IAW A300 SRM. 2L72 4F RTA35EU 20040520002892004052000289EU 2004 5 20 DHL2004364503 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, SEAT TRACK, 4TH FROM LT. SIDE HAS CORROSION AFT. OF FRAME 20, AND LOWER FLANGE CRACKED. REMOVED CORRODED SEAT TRACK SECTION FROM FR. 23.5 TO FR. 15. TRIMED TO FIT NEW SEAT TRACK SECTION FROM FR. 23.5 TO FR. 15 AND SPLICED ANGLES AT FR. 23.5. TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SECTION AND REPAIR ANGLES. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES AT FR. 23.5 IAW A300 SRM. 2L72 4F RTA35EU 20040520002912004052000291NM 2004 5 20 DHL2004764002 120040429A2612 FIRE LOOP BOEING727 727264 138408MNM NR 3 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01764AT 22984 NR 3 DETECTOR INOP LIGHT ILLUM IN FLIGHT, REWORKED/READJUSTED LOOP ELEMENT AWAY FROM NR 3 ENG COWL-LOWER IAW MM 26-14-00 NO FURTHER FAULTS NOTED OPS CK GOOD. 2L73 4F A3WE 20040520002922004052000292NM 2004 5 20 DHL2004764003 120040428A2612 FIRE LOOP BOEING727 727264 138408MNM ENGINE LOOSE A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01764AT 22984 NR 3 DETECTOR INOPERATIVE LIGHT ILLUMINATED IN FLIGHT. FOUND LOOSE CLAMP ON FIRE LOOP, RE-SECURED AND RAN ENG. PER JRH 5.2. OPS CHECK GOOD ON GROUND. 2L73 4F A3WE 20040520002932004052000293EU 2004 5 20 WRNA200400004 120040428A1420P68016 CONNECTOR AIRBUS300 A300B4203 3930306EU EGT LOOSE A WRNAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO05368DH 207 DURING FLIGHT CREW REPORTED NR 1 ENGINE EGT INDICATOR FLUCUATION. DIVERTED TO GSO FOR NORMAL LANDING. MAINTENANCE TROUBLE SHOOTING FOUND CANNON PLUG ON ENGINE EGT HARNESS LOOSE. TIGHTENED CANNON PLUG IAW STANDARD PRACTICES. INDICATOR OP'S CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20040521000012004052100001EU 2004 5 21 DHL2004364504 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN CARGO COMPARTMENT SEAT TRACK FLANGE HAS CORROSION BETWEEN FR. 32 AND FR. 36 LBL 36. REMOVED CORROSION FROM SEVERAL SPOTS BETWEEN FR 32-36, LBL 36. MATERIAL LOSS FROM 35.5 TO FR 36 0.003 FOUND TO BE WITHIN LIMITS , FOUND TO BE OUT OF LIMITS IAW A-300 SRM. CUT OUT CORRODED SEAT TRACK SECTION FROM FR. 32 TO FR 36 LBL 36, TRIMED TO FIT NEW TRACK SECTION. TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SECTION AND REPAIR ANGLES IAW A-300 SRM. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES AT FR. 3 AND FR 36 A300 SRM. 2L72 4F RTA35EU 20040521000022004052100002CE 2004 5 21 0027 120040426A3242244234 STATOR BFGOODRICH BEECH 90 E90 1152914CE BRAKE BROKEN E CIEAO OTHER O OTHER LDLANDING 1 NM0363BV 202 G5381 LW256 AFTER LANDING THE PILOT WROTE UP, RIGHT BRAKE HAS INTERMITTENT RAPID CYCLES OF, ON AND OFF BRAKE PRESSURE. ALSO INDICATED, APPEARS TO BE LEAKING HYDRAULIC FLUID. MAINTENANCE INSPECTED THE BRAKE AND FOUND THE INNER BRAKE CARRIER LINING BROKEN. THE PIECE OF THE INNER CARRIER LINING ASSEMBLY, APPROXIMATELY 3 INCHES LONG HAD BROKEN OFF AND WAS BECOMING WEDGED BETWEEN THE BRAKE HOUSING AND THE WHEEL ASSEMBLY. THE BROKEN PIECE HAD DAMAGED THE INNER WHEEL HALF ENOUGH TO CAUSE REJECTION OF THE WHEEL FORM FURTHER SERVICE. VISUAL INSPECTION OF THE BROKEN PIECE INDICATES IT HAD BECOME HOT AT SOME POINT IN TIME. IF THE BRAKE HAD NOT BEEN INSPECTED AT THIS TIME THE WHEEL MAY HAVE SEPARATED AT THE INNER WHEEL BEAD AREA1L72 3T 3A20 20040521000032004052100003NM 2004 5 21 QXEA200400291 120040428A21309672032501 PANEL BOMBDRDHC8 DHC8401 1390041NM AFT CARGO DISLODGED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09408QX6355 4050 FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF, AND DURING THE CLIMB, THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BLOW OUT PANEL DISLODGED. THE PANEL WAS RESEATED AND OPERATIONAL CHECKS WERE PERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040521000052004052100005WP 2004 5 21 G6OA042704 120040427A2170 COALESCER BAG DOUG DC10 DC1030F 3023504WP CABIN AIR CONTAMINATED A G6OAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27602GC 47923 SMOKE IN COCKPIT FROM PILOT AND COPILOT FOOT WELL. 2L73 4F RTA22WE 20040521000062004052100006 2004 5 21 249TR0027 420040425A2230734SVE23 COMPUTER BOEING737 7372K5 138448XNM AUTOTHROTTLE INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO THROTTLE COMPUTER INOPERATIVE. PLACED ON MEL 22-4. 04/27/2004: REPLACED AUTO THROTTLE COMPUTER AND OPS. CHECKED PER MM 22-31-01. CHECKS GOOD. CLEARED MEL. 2L72 4F RTA16WE 20040521000072004052100007NM 2004 5 21 252TR0019 120040429A7600 THROTTLE BOEING737 737228 13844AGNM RT ENGINE MALFUNCTIONED A PIDAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO05252TR 23001 ON TAKE OFF ROLL, LEFT THROTTLE WAS 2 KNOBS AHEAD OF RIGHT ENGINE THROTTLE. ABORTED TAKE OFF. MAINTENANCE FOUND RIGHT ENGINE PT2 LINE CLOGGED AT NOSE DOME. OBSTRUCTION WAS APPROX. 3 INCHES INSIDE OF OPEN END OF PT2 LINE. CLEARED PT2 LINE AND ACCOMPLISHED ENGINE RUN AND TRIM PER MM 71-09-200. ALL ENGINE PARAMETERS CHECK OK. 2L72 4F RTA16WE 20040521000132004052100013CE 2004 5 21 DXTA200400302 120040502A3220 LANDING GEAR CESSNA560 560XL 2076702CE NOSE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07626QS 5605126 AFTER TAKE OFF FROM FFC NOSE LANDING GEAR WOULD NOT RETRACT, DIVERTED TO ATL AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20040521000142004052100014CE 2004 5 21 DXTA200400301 120040428A275062384002 CONTROL UNIT CESSNA650 650 2076802CE TE FLAPS MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS CRCRUISE 1 GL07782QS1915 6507082 AT FL410, MACH .78, NOSE PITCHED DOWN -3 TO -5º, AUTOPILOT WAS "ON", FLAPS OVERSPEED LIGHT ILLUMINATED. FLAPS INDICATED 7º THEN 20º, VISUALLY FLAPS APPEARED TO BE BETWEEN 0 - 7º. - FOUND BITS 1, 2, 7, 8 SET ON CONTROLLER, SUSPECT A BAD FLAP CONTROLLER DUE TO FAULT CODES. REPLACED CONTROLLER CHECKED MECHANICAL AND ELECTRICAL PER CESSNA 650 MM CHAPTER 27-54-00. 2L72 4F A9NM 20040519001932004051900193NM 2004 5 19 QXEA200400275 120040413A2611 SMOKE DETECTOR BOMBDRDHC8 DHC8401 1390041NM CARGO BAY WILL NOT TEST A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09416QX 4083 FORWARD BAGGAGE SMOKE DETECTOR WILL NOT TEST. FORWARD BAGGAGE SMOKE DETECTOR TESTS NORMALLY AFTER AIRCRAFT POWER CYCLE. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040519002122004051900212NM 2004 5 19 EIA2004022 120040419A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 STA 340, 360 RT UPPER DECK FLOORBEAM HAS NUMEROUS HOLES WITH SHORT EDGE MARGIN BETWEEN RBL 55-80. STA 340 AND 360 RT UPPER DECK FLOORBEAM WITH SHORT EDGE MARGIN HOLES REPAIRED PER ECRA 3486-53-025-2 2L74 4F A20WE 20040519002232004051900223CE 2004 5 19 60419 120040408A3260 DOWNLOCK SWITCH BEECH 1900 1900D 1154162CE MLG DIRTY A AMWAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CE07178YV UE178 ON LANDING APPROACH IN EYW. AIRCRAFT LOST ALL INDICATION ON POSITION OF RT LANDING GEAR. CREW ABORTED LANDING. CYCLED GEAR AND GOT THREE DOWN AND LOCKED INDICATION. LANDED SAFELY WITH NO FURTHER INCIDENT. CLEANED DOWNLOCK SWITCHES. JACKED AIRCRAFT AND PERFORMED GEAR RETRACTION TEST. COULD NOT DUPLICATE AFTER MANY CYCLES. OPS CK NORMAL 2L72 4T RTA24CE 20040519002272004051900227CE 2004 5 19 60064 120040328A26121293640455 FIRE DETECTOR BEECH 1900 1900D 1154162CE CABIN FALSE ACTIVATIONA AMWAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 CE07133YV UE133 ON TAXI FIRE WARNING WAS INDICATED AT NR 2 ENGINE FOR APPROX 20 SECONDS THEN NORMAL. NO FIRE NOTICED BY CREW. RETURNED TO GATE WITH NO FURTHER INCIDENT. R&R'D FIRE DETECT/CONTROL BOX&A-319 PCB. 2L72 4T RTA24CE 20040519002342004051900234NM 2004 5 19 USAA040121 120040409A5320 SPLICE BOEING757 7572B7 1384964NM CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19620AU3673336733 27199 CORROSION ON SPLICE PLATE APPROX. 6 INCHES IN LENGTH BY 2 INCHES IN WIDTH AT BS 1401 BETWEEN S29L AND S29R. TRIM OUT CORRODED AREA, SPLICED IN NEW SECTION WITH EXTERNAL REPAIR SPLICE PER EA 78190. CORROSION LEVEL 1, TASK NR C52-155-02. (M) 2L72 4F RTA2NM 20040519002432004051900243NM 2004 5 19 04FDEA001038 120040422A5753 ROD END DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. **** S/D COMING **** 2L73 4F RTA22WE 20040519002492004051900249EU 2004 5 19 04FDEA001045 120040422A5320 BRACKET AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 N01279 MDCC FLOOR PAN PANEL BETWEEN SEAT TRACKS 1 AND 2 RT OF CENTERLINE FR 25 HAS CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10 2L72 4F RTA35EU 20040520000052004052000005NM 2004 5 20 UIEA200400065 120040422A541165B940512 RIB BOEING747 747243B 1384830NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND INTERIOR RIB CRACKED AT NAC STATION 220 RIGHT SIDE. DEFECT RECTIFIED AS PER TRANSIT W/O 71181467000001 IAW BOEING DRAWING 65B94117 REV E, 65B89043 REV D, 65B89044 REV B, AND BOEING RES SIN-04-00049H. (M) 2L74 4F A20WE 20040520000162004052000016NM 2004 5 20 UIEA200400067 120040422A5313 STRINGER BOEING747 747243B 1384830NM FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 FOUND AFT CARGO STRINGER AT STATION 1750 RIGHT SIDE STRINGER 44 FOUND CORRODED. STRINGER REPAIRED AT STATED LOCATION CARRIED OUT AS PER SRM 53-10-03 FIG 1. (M) 2L74 4F A20WE 20040520000272004052000027NM 2004 5 20 USAABB04036 120040416A2560SG9602 GLOWSTRIP BOEING757 757225 1384959NM CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU 22199 FOUND EMERGENCY LIGHT PHOTOLUMINESCENT STRIPS MISSING AT ROW 1 AND BETWEEN ROWS 2 AND 3. MAINTENANCE REPLACED THE STRIPS. (M) 2L72 4F RTA2NM 20040520000412004052000041NM 2004 5 20 USAA040100 120040119A5330 SKIN BOEING737 737301 1384611NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19573US50196 23560 PIT - FOUND SKIN WITH SCRIBE MARKS 260 INCHES IN LENGTH, STRINGER 10 LEFT BS 360-540. ACCOMPLISHED CUT-OUT AND INSTALLATION OF REPAIR DOUBLER PER EA 77471. (M) 2L72 4F RTA16WE 20040520000532004052000053NM 2004 5 20 04FDEA01073 120040423A5753ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OB FLAP, OB FWD HINGE BARREL NUT HOLE 7 MATING SURFACE CORRODED. COMPLIED WITH EA 1-5750-76024 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OB FLAP OB HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040520000582004052000058 2004 5 20 COMA0460318 420040512A22206629968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPNER MALFUNCTIONED A COMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO01965CA24668 7131 FLIGHT 5405 RUDDER FLUTTER DURING FLIGHT. REPLACED THE YAW DAMPNER ACTUATOR. 2L72 4F RTA21EA 20040520000592004052000059NM 2004 5 20 0400775515 120040514A5347 SEAT TRACK BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 23203 DURING AN H-CHECK FOUND CORROSION ON SEAT TRACK SUPPORT BEAM AT BS 377 RBL 46. REPAIRED IAW EA 198879. 2L72 4F RTA2NM 20040520000752004052000075EA 2004 5 20 MASA200400249 120040506A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAK NONE O OTHER ININSP/MAINT 1 SW0775992 7401 THE CAPTAIN REPORTED THE FORWARD TWO EMERGENCY FLOOR PROXIMITY LIGHTING STRIPS INOPERATIVE. MECHANIC TROUBLESHOT THE SYSTEM AND FOUND TWO CONNECTORS DISCONNECTED. THE CONNECTORS WERE RECONNECTED THE SYSTEM WAS OPERATIONALY TESTED AND CHECKED GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040520000862004052000086NM 2004 5 20 04FDEA001060 120040422A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT. AT STA 5-123 TO STA 1561 LT LONGERON 48, FOUND CORROSION. **** S/D COMING**** 2L73 4F RTA22WE 20040520000922004052000092NM 2004 5 20 04FDEA001069 120040423A5330 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 AFT CARGO LONGERON SPLICE AT STA 1847-1867 RT LONGERON 38 FOUND CRACK. **** S/D COMING **** 2L73 4F RTA22WE 20040520001082004052000108NM 2004 5 20 HNAA0400038 120040419A291082910010207 LINE DHAV DHC8 DHC8102 2809003NM HYDRAULIC SYS LEAKING A HNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA07938HA 152 NR 2 HYD QYT DROPPED TO 1 QT INFLT, AIR TURNBACK, INSTALLED TFL FROM BULKHEAD TO T FITTING UNDER GRAVEL GUARD IN NOSE WHEEL WELL, LEAK CHECK GOOD. R&R HYDRAULIC LINE. 2H72 4T RTA13NM 20040520001192004052000119NM 2004 5 20 04FDEA001058 120040422A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION STA 780 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS BS 780 DELTA BEAM LWR ANGLE. ACCESS LWR WEB. REMOVED, INSTALLED NEW BS 780 DELTA BEAM LWR ANGLE AND INSTALLED LWR WEB SUPPORT BEACON PANEL IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2L73 4F RTA3WE 20040520001212004052000121NM 2004 5 20 AT0400011 120040421A3397 WIRE BOEING717 717200 1383700NM EMERGENCY LIGHT BROKEN A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15955AT 55017 DURING EMERGENCY LIGHT OPS CHECK, WHILE PERFORMING SERVICE CHECK, SEAT ROW 20 DEF LIGHT FAILS TO LIGHT. REPAIRED WIRING AT SEAT ASSY. PER B717 SWPM 20-30-12 AND SWPM 20-10-13, AND WDM 33-51-14 OPS CHECK NORMAL IAW AMM 33-51-00. 2L72 4F TRA6WE 20040520001272004052000127NM 2004 5 20 04FDEA001099 120040424A5751 SKIN DOUG DC10 DC10 N/A-SDRNM ZONE 600 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 RT OUTBOARD AILERON INBOARD SUDE HAS SKIN SEPERATING AND CRACKED. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIGHT AND BALANCE, AILERON WITHIN 60-110 LIMIT AT 87 INCH POUNDS IAW DC-10 CMM 57-51-02. 2L73 4F RTA22WE 20040520001422004052000142NM 2004 5 20 PCAA0404196 120040426A332016405080 SOCKET DHAV DHC8 DHC8102 2809003NM CABIN LIGHTS ARCED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13805EX 228 REPORTED ELECTRICAL ODOR FROM AROUND OVERHEAD LIGHTS AT ROW 1AC. MAINTENANCE INSPECTED AND FOUND LIGHT SOCKET AT ROW 1AC AT FAULT. BULB WAS REMOVED AND MEL COMPLIED WITH.AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040520001492004052000149NM 2004 5 20 DHL2004783008 120040426A33501000677M LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01783DH 21999 COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT & OPS CHECKED GOOD PER B-727 M/M 33-50-1. 2L73 4F A3WE 20040520001682004052000168CE 2004 5 20 2004F00108 120040428A7500621465649 PRECOOLER CESSNA650 650 2076802CE BLEED AIR SYS BROKEN E K NONE O OTHER ININSP/MAINT 1 EA01750FB4086 6507049 DURING INSPECTION FOUND THE LINK ASSEMBLIES BROKEN AND CRACKED AT THE WELDS. INSPECTING MECHANIC FOUND THE SAME CONDITION ON BOTH SIDES (I.E. TWO SEPARATE BLEED AIR PRECOOLER ACTUATORS). BROKEN PARTS ARE MADE OUT OF ALUMINUM AND MECHANIC REPORTS THAT HE BELIEVES THAT BECAUSE THE LINK IS 'PULLING' ON A VERY STOUT SPRING, MATERIAL SHOULD BE CONSTRUCTED FROM STEEL OR STAINLESS RATHER THAT FROM ALUMINUM. REPORTER HAS ALSO SUGGESTED THIS TO CESSNA TECHNICAL SUPPORT. 2L72 4F A9NM 20040520001752004052000175NE 2004 5 20 DHL2004760003 220040427A7320 FUEL CONTROL BOEING727 7272B7 138407LNM PWA JT8 JT8D17A 52049NE NR 1 ENGINE MALFUNCTIONED A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01760AT 21954 715301 DURING ENG START, AFTER N2 WENT TO 40 PERCENT FUEL FLOW FLUCTUATING 700 TO 1400 PPH & THEN IMMEDIATELY FUEL FLOW WENT TO 0 PPH NR 1 ENG SHUTDOWN. REPLACED NR 1 ENG FUEL CONTROL & FUEL PUMP. OPS CHECKED GOOD IAW 73-21-02 & 73-11-01 OF THE JT8D MM. NR 1 ENG FUEL CONTROL REMOVED. REPLACED NR 1 ENGINE FUEL CONTROL IAW 73-21-02 OF JT8D MM LEAK & OPS CHECKED GOOD. NR 1 ENG FUEL PUMP REMOVED. REPLACED NR 1 ENG FUEL PUMP IAW 73-11-01 OF MM, LEAK & OPS CHECKED GOOD. NR 1 ENG TRIM REQUIRED AFTER FUEL PUMP & FUEL CONTROL CHANGE IAW MM 73-11-01, 73-21-02. RAN NR 1 ENG IAW ASTAR JRH 5.2 PERFORMED NR 1 ENG TRIM IAW JRH 7.9 MM 72-00-00 POWER ASSURANCE RAN AND TRIM SHEET COMPLETED OPS CHECK AND LEAK CHECKS ARE GOOD. 2L73 4F4 F A3WE E2EA 20040520001912004052000191 2004 5 20 DJFA2004002 420040411A34256226189002 COMPENSATOR BEECH MU300 400BEECH CE FLT DIRECTOR MALFUNCTIONED E DJFAA UNSCHED LANDING O OTHER CRCRUISE 1 EA23755TA2443 RK324 DURING FLIGHT AIRCRAFT EXPERIENCED A PFD FAILURE AND LOST BOTH PF'S. PILOTS CONTACTED CENTER AND RECIEVED VECTORS TO CAS WERE THEY LANDED WITH NO FURTHER PROBLEMS. 2H72 4F RTA16SW 20040520001932004052000193EA 2004 5 20 QXEA200400289 120040426A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA AFT CARGO INTERMITTENT A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09607QX6432 10024 CREW RECEIVED AN AFT CARGO DETECTOR CAUTION MESSAGE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE AFT CARGO DETECTOR SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY. THE AFT NR 1 SMOKE DETECTOR WAS REPLACED AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040520001962004052000196SO 2004 5 20 BIER200401060 220040428A8530AEC631397 CYLINDER HEAD CESSNA414 414 2075908CE CONT O520 TSIO520NB 17040SO RT ENGINE CRACKED B BIERA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA21236A 200 4140805 514728 LOW MP INDICATION. RT ENGINE, NR 1 CYLINDER, HEAD SEPERATED FROM CYLINDER. AD 2004-08-10 N/A TO CYLINDER DUE TO S/N. CYLINDER MANUF BY ECI, INC. BUT THEY ARE NOT LISTED BELOW. 1L72 3O3 ORTA7CE E8CE 20040521000122004052100012NE 2004 5 21 DXTA200400303 220040502A7421CH346593 IGNITER CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE ENGINE FAILED E DXTAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 GL07335QS 5600335 PCE500168 ON FIRST ATTEMPT RT ENGINE WOULD NOT LIGHT, ON SECOND ATTEMPT ENGINE LIGHT OFF AND STARTED. AFTER ENGINE START, WHILE AT IDLE THE RT ENGINE FLAMED OUT PRIOR TO TAXI. FOUND IGNITER FIRES INTERMITTENTLY REPLACED INBOARD IGNITER AND FOUND THROTTLE NOT RIGGED CORRECTLY, RE-RIGGED THROTTLE AND ALL OPS CHECK GOOD. ALL WORK DONE IAW JT15D-5D MM CHAPTER 74-20-02 AND CESSNA 560MM CH 76-11-00. 2L72 4F4 FRTA22CE E25EA 20040521000162004052100016 2004 5 21 DXTA200400269 420040318A2300360011 AMPLIFIER ISRAELGALAXYGALAXY 4500307EU OVERHEATED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07700QS124 052 DURING FLIGHT CREW DETECTED SMOKE IN THE COCKPIT, NOTICED SMOKE COMING OUT FROM BEHIND THE BOTTOM FORWARD 2 DRAWS. TURNED THE GALLEY POWER OFF AND AFTER A FEW MINUTES THE SMOKE STOPPED. CONTINUED FLIGHT TO DESTINATION WITHOUT INCIDENTS. - INSPECTED GALLEY AREA AND FOUND THE AIRSHOW SPEAKER AMPLIFIER HAD SIGNS OF OVERHEATING. REPLACED DEFECTIVE AIRSHOW SPEAKER AMPLIFIER WITH A REPAIRED UNIT, OPS CHECKED SATISFACTORY. 2L72 4F RTA53NM 20040521000182004052100018NM 2004 5 21 237TR0005 120040501A7710 TRANSMITTER BOEING737 737228 13844AGNM LT ENGINE LOOSE A PIDAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO05237TR 23007 LT ENGINE WOULD NOT MAKE TARGET EPR ON TAKE OFF ROLL. FOUND B-NUT ON EPR TRANSMITTER LOOSE. REINSTALLED/TORQUED LINE. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040521000192004052100019WP 2004 5 21 041204SO3501 120040412A2611915 BATTERY DOUG DC9 DC9 3022002WP SMOKE DETECTOR DAMAGED A A4JAO OTHER N FALSE WARNING TOTAKEOFF 1 SO35935D BOTH LAVATORY SMOKE DETECTORS WENT OFF DURING TAKE-OFF. FOUND DETECTOR BROKEN AND TAMPERED WITH. R & R RT AND LT AFT LAVATORY SMOKE DETECTOR BATTERIES. 2L72 4F A6WE 20040521000212004052100021WP 2004 5 21 DHL2004805003 120040502A2750 SWITCH DOUG DC8 DC873F 302199FWP TE FLAPS MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01805DH 46125 TAKEOF WARNING HORN SOUNDED AFTER ADVANCING THRUST FOR TAKEOFF. REJECTED TAKEOFF PER S.O.P. A/C WEIGHT 206200, IAS 0, OAT CEL 10, PRESS ALTITUDE 833, BRAKE ENERGY ZONE NORMAL FOUND BUILDUP OF DEBRIS ON FLAP/SWITCH FOLLOWUP CAM. CLEANED AND OPS CHECKED FLAP TAKEOFF WARNING SYS, OK IAW DC-8 MM 27-52-1. BRAKE ENERGY AND RTO NOTED BY MX. 2L74 4F RT4A25 20040521000232004052100023 2004 5 21 YENA200425 420040428A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN MALFUNCTIONED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15581JB1571 2141 LIVE TV SYSTEM INOP, TRIED ONE RESET BUT FAILED. (FLIGHT CREW REPORTED ODOR BY ROW 18 ABC DURING RESET). REMOVED AND REPLACED LTV SEB AT 18 ABC IAW INFO NOTICE 2003-T050TR A. OPERATION CHECK NORMAL REF MM 23-39-00. 2L72 4F RTA28NM 20040521000242004052100024EU 2004 5 21 DHL2004362004 120040430A3242 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01362DH 84 AUTO BRAKES IN "MED" BRAKES WOULD NOT RELEASE WITHIN + - 10SEC., RENGAGED TWICE AFTER THEY RELACED. PERFORMED AUTO BRAKE CONTROL UNIT FUNCTIONAL TEST IAW M/M 32-42-54. OPS CK GOOD. 2L72 4F RTA35EU 20040521000252004052100025 2004 5 21 KBM2004F00069 420040104A231206410543C DISPLAY SNIAS 350 AS350BA 8680817EU VHF COMMS FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH316 2957 DISPLAY WENT BLANK IN COM TWICE DURING FLIGHT. HAD TO TUN OFF SWITCH TO RESET DISPLAY. REMOVED AND REPLACED WITH SERVICEABLE. 1G71 3U NCH9EU 20040521000272004052100027WP 2004 5 21 IXXA0400042S 120040303A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING CENTER SECTION UPPER FLOORBEAM FLANGE CORRODED, STA. 980.000 RBL 10 INCHES. REPAIR ARE ACCOMPLISHED, PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG. 1, REMOVED CORROSION FROM UPPER FLOORBEAM FLANGE, STA 980.000 RBL. 10 INCHES IAW DC8 SRM 51-1-8 PG. 18, FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2M, CUT OUT DAMAGED SECTION, FABRICATED FILLER & DOUBLER IAW SRM 51-2-1 FIG. 1, PERFORMED NDT INSP. IAW NDT SPM PART 08-00-02/07 CLEANED, TREATED AND PRIMED AREA, FILLER, DOUBLER IAW DC8 SRM 51-1-8B INSTALLED FILLER, DOUBLER IAW DC8 SRM 51-2-1 FIG. 7, DC8 SRM 51-1-20D PG. 9, DC8 SRM 51-1-21 PG.7, DC8 SRM 51-3-0 PG. 1. 2L74 4F RT4A25 20040521000292004052100029WP 2004 5 21 IXXA0400044S 120040214A5330 SKIN DOUG DC8 DC873F 302199FWP FUSLAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C-CHECK RT FUSELAGE FORWARD LOWER CARGO COMPARTMENT FWD DOOR PLATING LOWER SIDE INTERIM REPAIR BETWEEN STA FS 280.00 AND FS 340.00. REPAIR ACCOMPLISHED. REMOVED TEMPORARY REPAIR IAW DC8 SRM 51-1-21 PG 1. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-001, FABRICATED NEW SKIN SEGMENT IAW DWG V22-R13. CLEANED, TREATED AND PRIMED AREA, NEW SKIN, SPLICE( INTERNAL) IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON SPLICE & SKIN AND INSTALLED IAW DWG V22-R13, DC8 SRM 51-1-21 PG1, SRM 51-1-15 , SRM 51-1-20D PG 9, SRM 51-1-21A PGS 1-4. LEAK CHECK ACCOMPLISHED. 2L74 4F RT4A25 20040521000342004052100034NM 2004 5 21 ASMF200405016 120040514A213339271411 REGULATOR VALVE DOUG MD88 MD88 3023688NM CABIN PRESSURE FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23162PL107577907 49765 AIRCRAFT RETURNED OF FLIGHT WHEN FAIL IN RIGHT AIR CONDITIONING SYSTEM AND ADVERSE WEATHER CONDITIONS. AIRCRAFT FLIGHT WITH RT AIR CONDITIONING SYSTEM DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE, RT PRESSURE REGULATOR VALVE WAS REPLACED IAW MM 21-31-06, TEST CORRECT. 2L72 4F RTA6WE 20040521000352004052100035 2004 5 21 ASMF200405018 420040515A3497 BUSS DOUG DC9 DC982 3022082WP DFGC NR 1 LOOSE W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23505MD 49149 AIRCRAFT RETURNED TO PLATFORM BECAUSE BUSS WERE LOOSEN. GCU´S WERE CHECKED, ALL CORRECT. FLIGHT DIRECTOR BUSS WAS CHECKED AND IT WAS DETECTED WITH FAIL. DFGC NR 1 WAS RESEATED AND BOTH DFGC´S WERE TESTED IAW MM 22-00-00, CORRECTING THE FAIL. 2L72 4F A6WE 20040521000362004052100036NE 2004 5 21 ASMF200405019 220040515A73207434968 SOLENOID VALVE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23161PL 49764 718075 AIRCRAFT RETURNED TO PLATFORM BECAUSE AFTER LT ENGINE STARTED PARAMETERS WERE N2 70 PERCENT, EGT 422 DEGREES, N1 42 PERCENT, EPR 1.10 AND 21 °C. DURING CHECK, IDLE SOLENOID WAS REPLACED IAW MM 73-20-05, TEST CORRECT. DURING TAXING, SYSTEM FAILED AGAIN RETURNING TO PLATFORM. TECHNICAL PERSONNEL DEFERRED THE FAILURE IAW MEL 73-7. 2L72 4F4 FRTA6WE E2EA 20040521000372004052100037WP 2004 5 21 ASMF200405017 120040515A2133 PRESSURE VALVE DOUG DC9 DC987 3022087WP CABIN PRESSURE FAILED W ASMFAG UNSCHED LANDING O2 MASK DEPLOYED GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SW231075T 49724 AIRCRAFT RETURNED FLIGHT BECAUSE IN AUTOMATIC MODE THE PRESSURIZATION SYSTEM HAD OSCILLATIONS AND IN MANUAL MODE THE PRESSURE VALVE COULD NOT BE CLOSED. DURING MAINTENANCE REVISION, THE SWITCH WAS PLACED IN MANUAL POSITION AND VALVE WAS CLOSED, THE SYSTEM OPERATED CORRECTLY. DUE TO OXYGEN MASKS AND OXYGEN GENERATORS WERE DEPLOYED AIRCRAFT WAS SENT TO THE HANGAR AND LEAK TEST WAS PERFORMED IAW MM 21-00-00, PRESSURE RELIEF VALVES WERE CHECKED OPENING AT 8 PSI, AND OPERATING CORRECTLY. OXYGEN MASKS AND OXYGEN GENERATORS WERE REPLACED, ALL TESTS WERE CORRECT. 2L72 4F RTA6WE 20040521000402004052100040EU 2004 5 21 KBM2004F00071 120040124A6420350A33215300 BEARING SNIAS 350 AS350BA 8680817EU T/R HINGE SHEARED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH817 2957 TAIL ROTOR HUB HINGE SPHERICAL LAMINATED BEARING IS SHEARED. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040521000412004052100041EU 2004 5 21 KBM2004F00068 120040104A6420355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1846 2957 TAIL ROTOR LAMINATED HALF BEARINGS WORN. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U NCH9EU 20040521000452004052100045EU 2004 5 21 KBM2004F00076 120040109A6420355A09103601 BEARING SNIAS 350 AS350B1 8680811EU TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 831 2009 HALF SHELL BEARING IS WORN BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U H9EU 20040521000462004052100046EU 2004 5 21 DHL2004367005 120040430A5270 WARNING LIGHT AIRBUS300 A300B4203 3930306EU PAX DOOR ILLUMINATED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01367DH 265 JUST AFTER TAKEOFF, DOOR LIGHT ON MWP ILLUMINATED MOMENTARILY WITH A CHIME. DID NOT SEE A LIGHT ON DOOR PANEL. CYCLED ALL A/C DOORS PERFORMED OPERATIONAL CK PER M/M 52-70-11. DOOR WARNING SYST. PRESSURIZE A/C TO 7 PSI NO FAULTS NOTED PER M/M 05-53-00. 2L72 4F RTA35EU 20040521000482004052100048NE 2004 5 21 2004000004 220040501A7261 GASKET DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 ENGINE LEAKING A CNMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0749082 47927 517258 NR 3 ENGINE OIL LOSS, APPROXIMATELY 2 QTS. PER HOUR. MX ADVISED CREW TO RETURN TO BWI FOR REPAIRS. REPLACED GASKET ON OIL VENT LINE FOR B-SUMP AND OIL TANK. RAN ENGINE AT POWER. NO FURTHER LEAKING NOTED. 2L73 4F4 F A22WE E23EA 20040521000492004052100049NM 2004 5 21 WRLA200418 120040423A29136506606 PUMP DOUG MD11 MD11 3023602NM NR 1 ENG HYD FAILED A WRLAO OTHER J WARNING INDICATION CRCRUISE 1 SO11272WA 48437 NR 1 HYDRAULIC SYSTEM FAIL INFLIGHT, THE CREWS CONTINUED TO DESTINATION AND FOLLOWED STANDARD EMERGENCY PROCEDURE. AT KBWI MAINTENANCES FOUND NR 1 ENGINE RT HYD. DRIVEN PUMP INOP. THEY REMOVED AND REPLACED NR 1 ENGINE BOTH RT & LT EDP. OP'S & LEAKS CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA22WE 20040521000522004052100052NM 2004 5 21 PCAA0405201 120040430A3260855401 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003NM MLG LOOSE A PCAAO OTHER J WARNING INDICATION CLCLIMB 1 EA13817EX 191 FLIGHT #4069 REPORTED THE RIGHT MAIN GEAR DOOR AMBER ADVISORY LIGHT REAMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR DOORS WERE VISUALLY CONFIRMED CLOSED. MAINTENANCE FOUND THE FORWARD GEAR DOOR PROXIMITY SWITCH LOOSE. SWITCH HAS BEEN RESECURED AND ADJUSTED.PROXIMITY SWITCH TEST COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040521000532004052100053NM 2004 5 21 PCAA0405202 120040501A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM NR 1 INOPERATIVE A PCAAO OTHER L NO TEST NRNOT REPORTED 1 EA13834EX236172564 285 REPORTED THE NR 1 SMOKE DETECTOR AS BEING INOPERATIVE DURING TEST.MAINTENANCE REMOVED AND REPLACED THE UNIT AND OPERATIONAL TESTED THE SYSTEM . SYSTEM TEST GOOD. AIRCRAFT RETUNED TO SERVICE. 2H72 4T RTA13NM 20040521000552004052100055EU 2004 5 21 DHL2004364506 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, 7TH SEAT TRACK FROM LT SIDE, INBD LOWER FLANGE CRACKED AFT OF FRAME 20 AND CORROSION ON FLANGES BETWEEN FRAME 19-21. REMOVED CORROSION AT SIDE OF SEAT TRACK IAW SRM, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SEAT TRACK SECTION. TRIMMED TO FIT NEW SEAT TRACK SECTION AND SPLICE ANGLES IAW SRM TREATED, PRIMED, AND POLYWHITE NEW SEAT TRACK SECTION AND REPAIR ANGLES IAW SRM. INSTALLED NEW SEAT TRACK AND REPAIR ANGLES IAW SRM. 2L72 4F RTA35EU 20040521000572004052100057EU 2004 5 21 RAIA00405001 120040502A3010 BOOT JETAIRJETSTMJETSTM4101 1500501EU ANTI ICE SYSTEM LEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03569HK 41088 AIRFRAME DE-ICE FAULT AUTO AND MANUAL. MAINTENANCE INSTALLED DE-ICE BOOT PATCHES ON THE LT WING AND LT HORIZONTAL STAB DE-ICE BOOTS. 2L72 4T RTA41NM 20040521000582004052100058NM 2004 5 21 2820404 120040407A332010618921 LIGHT BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE CABIN BURNED A SQ7AO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01282US60362100 21161 DURING DESCENT, SOME SMOKE IN CABIN AT SEAT 15 ABC. THE "FASTEN SEAT BELT, NO SMOKING" CIRCUIT BREAKER POPPED. FOUND LIGHT BAR MELTED. DISCONNECTED AND STOWED WIRES. SEAT BELT, NO SMOKING SYSTEM PLACED ON MEL 33-3. 2L73 4F4 F A3WE E2EA 20040521000592004052100059NM 2004 5 21 2820504 120040430A3350 BATTERY PACK BOEING727 727251 138408HNM EMERGENCY LIGHT INOPERATIVE A SQ7AK NONE L NO TEST ININSP/MAINT 1 SO01282US60439100 21161 EMERGENCY LIGHT FAILURE AT RIGHT OVERWING EXIT. REPLACED BATTERY PACK AND SYSTEM CHECKS NORMAL. 2L73 4F A3WE 20040521000602004052100060NM 2004 5 21 P5CA0401077 120040425A7830 ROD BOEING747 747341 13848AMNM NR 3 ENG T/R LOOSE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 NR 3 ENG HAS ROD STICKING OUT OF T/R SLEEVE AT 3:00 POSITION. REMOVED DAMAGED ROD, INSPECTED AREA, FOUND NO FURTHER DAMAGE. DEACTIVATED PER MEL 78-01-05. 2L74 4F RTA20WE 20040521000612004052100061NM 2004 5 21 P5CA0401080 120040427A5320 WEB BOEING747 7472D3B 1384805NM FUSELAGE DAMAGED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23505MC 21251 ON POST FLIGHT INSPECTION, FOUND FAIRING OVER RIGHT WING ROOT OPEN AND FOUND WEB PANEL DAMAGED. ACCOMPLISHED REPAIR OF WEB PANEL PER SRM 51-40-02. SURROUNDING AREA CLEANED AND INSPECTED. NO FURTHER DAMAGE. 2L74 4F RTA20WE 20040521000622004052100062NM 2004 5 21 P5CA0401081 120040429A2797 WIRE BOEING747 747230B 1384889NM ELEVATOR BROKEN A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23508MC 21644 ON ENGINE START, ELEVATOR FEELS LIGHT. DID NOT COME ON WITH HYD SYST NR 2 PRESSURIZED AND SYST 3 UNPRESSURIZED. FOUND BROKEN WIRE AT MISOI, REPAIRED IAW 20-10-13. PERFORMED SYST CHECK PER 27-31-00, SYST OPS NORMALLY. 2L74 4F A20WE 20040521000632004052100063NE 2004 5 21 P5CA0401078 220040426A7510 LINE BOEING747 747236B 1384804NM PWA JT9 JT9D7Q 52054NE FUEL SYSTEM LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23924FT 21730 NR 2 ENGINE FUEL LEAK FROM DRAIN MAST FOUND DURING PREFLIGHT. FOUND PSO LINE AT EVC LEAKING. INSTALLED NEW FERRULE AND RESEATED LINE. PERFORMED IDLE RUN AND LEAK CHECK PER MM 71-00-80. TEST NR 3 NO LEAKS EVIDENT. 2L74 4F4 F A20WE E3NE 20040521000652004052100065NM 2004 5 21 P5CA0401076 120040425A80107265747 START VALVE BOEING747 747236B 1384804NM NR 4 ENGINE FAILED A P5CAED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23924FT 21730 START VALVE NR 4 ENG ILLUM DURING TAXI. ENGINE SHUTDOWN AND RETURN TO RAMP. R&R STARTER VALVE IAW AMM 80-04-01. 2L74 4F A20WE 20040521000662004052100066EA 2004 5 21 MASA200400238 120040501A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR SEPARATED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777331 7331 ASH 7173 THE PAX DOOR HANDLE CAME OFF. MX IN THE PROCESS OF REPLACING THE HANDLE. REPLACED HANDLE ASSY AND SWITCH PLUNGER 2L72 4F RTA21EA 20040521000672004052100067NE 2004 5 21 MASA200400237 220040430A72004147T70P01 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE INOPERATIVE A MASAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW071733718992 7337 872560 CREW REPORTED RT ENGINE FAILED IN FLIGHT. THE ENGINE SHUTDOWN UNCOMMANDED INFLT. MX CHANGED THE RT FCU. OPS CHECK GOOD 2L72 4F4 FRTA21EA E15NE 20040521000702004052100070EA 2004 5 21 MASA200400234 120040429A27505913000 BPSU CNDAIRCL600 CL6002D24 1390016EA TE FLAPS INOPERATIVE A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07918FJ142 15018 DECLARED EMERGENCY WITH FLAPS FAILED AT 4 DEGREES ON APPROACH TO PHX. AIRCRAFT OUT OF SERVICE FOR MECHANICAL FLAP RIGGING. MX REPLACED THE RIGHT HAND BPSU. OPS CHECK GOOD 2L72 4F RTA21EA 20040521000722004052100072EA 2004 5 21 MASA200400231 120040428A27505913000 BPSU CNDAIRCL600 CL6002C10 1390015EA TE FLAPS INOPERATIVE A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07510MJ2494 10101 DECLARED AN EMERGENCY AND LANDED IN LAX DUE TO A FLAP FAIL AT ZERO CONDITION. MX WENT TO LAX AND CHANGED THE BPSU. 2L72 4F RTA21EA 20040521000782004052100078NE 2004 5 21 MASA200400044 220040125A72303901T93G06 FAN BLADE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE VIBRATION A MASAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SW07759914633 75991 872783 CREW REPORTED NR 1 ENGINE HIGH VIBE DURING TAKE-OFF. A/C RETURNED TO THE FIELD AND MX WAS CALLED. MX BORESCOPED THE ENGINE AND WAS GOOD. MX NOTICED SEVERAL FAN BLADES WITH CHIPS. MX REPLACED THE FAN BLADES. OP CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040521000802004052100080 2004 5 21 MASA200400050 420040127A3418 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA STALL WARNING ILLUMINATED A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW0777195 7195 RETURNED TO GATE FOR STALL FAIL MESSAGE ON TAXI-OUT. MX RESET SYSTEM. OP CHECKS GOOD. NO PARTS USED 2L72 4F RTA21EA 20040521000832004052100083EA 2004 5 21 MASA200400059 120040201A5210BLC3BC11SL5C4 SHEAR PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE FAILED A MASAK NONE O OTHER ININSP/MAINT 1 SW0775998 75998 PAX DOOR STOW HANDLE CAME OFF WHEN F/A CLOSED THE DOOR. A/C WAS FERRIED TO PHL. MX REPLACED THE SHEAR PIN. OP CHECKS GOOD. 2L72 4F RTA21EA 20040521000852004052100085EA 2004 5 21 MASA200400100 120040223A77326233M30A ACCELEROMETER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE UNSERVICEABLE A MASAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SW0777302 7302 872479 ABORTED T/O DUE TO NR 1 ENG N2 VIB ICON ON EICAS. MX REPLACED THE NR 1 EVM AND A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F4 FRTA21EA E15NE 20040521000862004052100086EA 2004 5 21 MASA200400102 120040224A5210 INDICATOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0775995 7361 CAPT REPORTED THE MAIN CABIN DOOR OUTER HANDLE STOWED INDICATOR WAS NOT DISPLAYED. MX REPOSITIONED INDICATOR. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040521000892004052100089EA 2004 5 21 MASA200400108 120040224A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07591ML5766 7388 RT FS 625 OBLIQUE ANGLE IS CRACKED. REPLACED CRACKED OBLIQUE ANGLE IAW BOMB CRJ SRM 51-42.21 2L72 4F RTA21EA 20040521000902004052100090 2004 5 21 P9RA20040012 420040413A2565146110016DME SLIDE BOEING727 727200 138407ENM LEAKING A P9RAK NONE O OTHER ININSP/MAINT 1 SO11288SC 20765 SLIDE REMOVED FOR SCHEDULED CHANGE. REPAIR STATION TEARDOWN INDICATED THE INFLATABLE TUBE IS POROUS AND WILL NOT PASS TEST. UNIT IS NOT REPAIRABLE. LAST OVERHAUL WAS MAY 31 2001. 2L73 4F RTA3WE 20040521000932004052100093 2004 5 21 MASA200400115 420040228A3418 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA STALL WARNING FALSE ACTIVATIONA MASAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW07506MJ 10073 A/C DIVERTED TO LAX AFTER CREW GOT A STALL FAIL CAUTION MSG. MX RESET SYSTEM. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040521000942004052100094WP 2004 5 21 ABXA040156 120040429A3260 PROXIMITY SWITCH DOUG DC9 DC931 3022065WP MLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23947AX 47004 GO AROUND-MISSED APPROACH-GEAR RECYCLE. UPON PLACING MLG HANDLE IN THE DOWN POSITION FOR LANDING, MLG DOWN LIGHT FAILED TO ILLUMINATE. AFTER RUNNING ABNORMALS, DISCOVERED THE MLG WARNING CIRCUIT BREAKER WAS OUT. RESET CIRCUIT BREAKER AND EXTENDED MLG. AFTER SECOND EXTENSION, THREE GREEN LIGHTS ILLUMINATED. AND MLG CHECKED DOWN ALSO ON USING MAIN GEAR PROXIMITY SWITCHES. LANDING SOUNDED AND APPEARED TO WORK NORMALLY THE ENTIRE FLIGHT. FOUND WIRE AT P1-132 PIN 7 OPEN TO S3-65 TERMINAL 2, REPAIRED WIRE 1G206D24. WHILE PULLING IN WIRE, WIRE G207K24 AND 1G205C24 BROKE AT ENVIRONMENT SPLICES IN CONDUIT. REPAIRED WIRES IAW DC-9 WDM 32-41-00 LEFT LANDING GEAR OPS CHECKED GOOD IAW DC-9 AMM 32-60-00. 2L72 4F A6WE 20040521000972004052100097CE 2004 5 21 DXTA200400285 120040331A2120 ODOR CESSNA750 750 2076810CE COCKPIT DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07947QS 7500047 AT FL410 STRONG ODOR OF SMOKE IN CABIN AND THE COCKPIT, SMOKE WAS COMING FROM BEHIND THE CAPTAIN’S CIRCUIT BREAKER PANEL AND OUT THE DEFROST HOLES JUST BELOW THE LEFT SIDE WINDOW. DEPLOYED O2 MASKS AND LANDED SAFELY. INSPECTED THE FOLLOWING AREAS FOR SIGNS OF BURNING OR ARCING: LT CIRCUIT BREAKER PANEL, PILOTS SIDE PANELS, BAR, CLOSET, LT PCB J-BOX, PSU LIGHTING, BEHIND INSTRUMENT PANEL, INSIDE PEDESTAL AND AFT CLOSET, EVERYTHING CHECKED GOOD. RAN AIRCRAFT WITH BOTH ENGINES & APU, PERFORMED OPERATIONAL CHECK OF ENVIRONMENTAL CONTROL SYSTEM, COCKPIT & CABIN PACKS- OPS CHECKS GOOD IAW CESSNA MM CHAPTER 24-51-00 AND 21-51-00. 2L72 4J RTT00007WI 20040521000982004052100098WP 2004 5 21 0400649969 120040501A2913AS19593C PUMP DOUG DC9 DC931 3022065WP HYD SYSTEM LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL019333 47246 ON BASE LEG DURING APPROACH FOR LANDING, THE RIGHT HYDRAULIC SYSTEM LOST ALL FLUID AND FAILED. COMPLIED WITH COM PROCEDURES AND LANDING GEAR WAS EXTENDED MANUALLY. LANDING WAS NORMAL AT BNA ALTHOUGH THE GEAR DOORS DID HIT. GROUND CREW PINNED THE GEAR AND DOORS PRIOR TO TAXI. MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP, THE AUXILIARY HYDRAULIC PUMP, AND THE RIGHT HYDRAULIC SYSTEM FILTERS. LEAK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040521000992004052100099WP 2004 5 21 0400659620 120040501A272037723745503 VALVE DOUG DC9 DC932 3022066WP RUDDER CONTROL CRACKED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01620NW 47533 WHEN THE HYDRAULIC PUMPS WERE TURNED ON DURING DESCENT, THE RIGHT HYDRAULIC SYSTEM FAILED COMPLETELY LOSING PRESSURE AND QUANTITY. CREW COMPLIED WITH COM PROCEDURES: LOSS OF RIGHT HYDRAULIC SYSTEM AND EMERGENCY GEAR EXTENSION. LANDING WAS NORMAL AND UNEVENTFUL AT DTW. MAINTENANCE FOUND THAT THE RUDDER POWER SHUTOFF VALVE AT THE PRESSURE PORT WAS CRACKED. REPLACED THE SHUTOFF VALVE AND SERVICED THE SYSTEM. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040521001012004052100101EA 2004 5 21 MASA200400131 120040309A32314622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG DOOR LEAKING A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07372285476 7228 A/C RETURNED TO FIELD FOR NLG DOOR MASTER CAUTION WITH NR 3 PUMP MESSAGES UPON RETRACTION. PILOT ALSO HAD NR 3 PRESS LOW MASTER CAUTION MSG UPON EXTENTION. MX REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. OP CHECKS GOOD. 2L72 4F RTA21EA 20040521001032004052100103EA 2004 5 21 MASA200400134 120040311A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LAV SMOKE FALSE INDICATIONA MASAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW0775995 7361 THE CAPT REPORTED A "SMOKE IN LAV" MSG. NO SMOKE OR FIRE WAS OBSERVED. MX COULD NOT DUPLICATE THE PROBLEM ON THE GROUND. NO PARTS USED. 2L72 4F RTA21EA 20040521001062004052100106EA 2004 5 21 MASA200400145 120040316A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FALSE ACTIVATIONA MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0775995 7361 A/C RETURNED TO THE FIELD AFTER A "FLAPS FAIL" CAUTION MSG WAS ILLUMINATED ON EICAS. PHL MX PERFORMED PART "A" INSPECTION. NO DEFECTS NOTED. 3/17/2004. MX PERFORMED PART "B" AND NO DEFECTS WERE NOTED. NO PARTS USED. 2L72 4F RTA21EA 20040521001072004052100107EA 2004 5 21 MASA200400146 120040317A32342322H000004 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG LEAKING A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07507MJ 10077 CREW DECLARED AN EMERGENCY FOR GEAR DISAGREE IN THE AIR. GEAR WAS LOWERED MANUALLY AND THE PLANE LANDED WITHOUT FURTHER PROBLEMS. MX REPLACED THE GEAR HANDLE AND THE SELECTOR VALVE. OP CHECKS GOOD ON TEST FLIGHT. NOMEN: GEAR HANDLE P/N 7-45502-3 S/N UNK. 2L72 4F RTA21EA 20040521001082004052100108EA 2004 5 21 MASA200400154 120040319A2120GG670950601 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0717275 7275 A/C RETURNED TO FIELD. CREW REPORTED A LT PACK HI PRESS EICAS MSG IN-FLIGHT. THE RT PACK WAS PREVIOUSLY DEFERRED. THE A/C FLEW TO PHX. MX REPLACED THE BLEED AIR CHECK VALVE. OP CHECKS GOOD. 2L72 4F RTA21EA 20040521001102004052100110EA 2004 5 21 MASA200400158 120040319A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07592ML6784 7410 DURING HEAVY CHECK. LEFT FS 621 UNDER FLOOR SUPPORT ANGLE P/N 601R35031-239 HAS A .5 INCH LONG CRACK. REPAIRED CRACK IN FS 621 UNDER FLOOR UNDER FLOOR SUPPORT ANGLE IAW BOMBARDIER REPAIR EO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20040521001112004052100111EA 2004 5 21 MASA200400160 120040323A2697 TERMINAL CNDAIRCL600 CL6002B19 1900309EA FIRE LOOP OUT OF POSITION A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0777260 7260 RETURNED TO GATE AFTER REJECTED TAKE-OFF. CREW RECIEVED A LT JETPIPE OVERHEAT WARNING LIGHT. MX REPOSITIONED TERMINALS FOR BOTH LOOPS A & B GROUNDING. MX REPOSITIONED THEM. OP CHECKS GOOD ON HIGH POWER RUN. NO PARTS USED 2L72 4F RTA21EA 20040521001122004052100112SW 2004 5 21 KBM2004F00080 120040429A6510327211 DISC PACK BELL 206 206B 1181511SW TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 ENGINE TAIL ROTOR DRIVE SHAFT, COUPLING HAS CRACKS. REMOVED AND REPLACED. 1G71 3U H2SW 20040521001132004052100113EU 2004 5 21 KBM2004F00078 120040514A7120206062101102 MOUNT SNIAS 350 AS350B1 8680811EU ENGINE CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 RT FWD ENGINE COWLING SUPPORT LEG CRACKED AT MGB DECK HWD IAW STANDARD PRACTICES. REPAIRED RT ENGINE SUPPORT LEG W/STAINLESS STEEL BRACKET DOUBLER W/ EXISTING. 1G71 3U H9EU 20040521001142004052100114SW 2004 5 21 KBM2004F00079 120040121A8000MS250893C SWITCH BELL 206 206B 1181511SW STARTER INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 START SWITCH INTERMITTENT. REMOVED AND REPLACED. 1G71 3U H2SW 20040521001152004052100115EU 2004 5 21 KBM2004F00083 120040109A5270SP381210 SWITCH SNIAS 350 AS350B2 8680813EU CARGO DOOR INOPERATIVE E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19884SH 2884 LT BAGGAGE DOOR OPEN LIGHT COMES ON IN FLIGHT. REMOVED AND REPLACED DOOR SWITCH. 1G71 3U H9EU 20040521001182004052100118GL 2004 5 21 KBM2004F00082 220040109A72619560137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL ENGINE LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19751H 3403 MO 5 OUTPUT SHAFT MAGNETIC SEAL IS LEAKING OIL. REMOVED AND REPLACED. 1G71 3U3 U H9EU E4CE 20040521001202004052100120EU 2004 5 21 KBM2004F00085 120040503A6730123668P ROD END SNIAS 350 AS350B2 8680813EU MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 FORE/AFT SERVO LOWER ROD END HAS EXCESSIVE PLAY. REMOVED AND REPLACED. 1G71 3U H9EU 20040521001212004052100121EU 2004 5 21 KBM2004F00087 120040407A792147750 MOTOR SNIAS 350 AS350B2 8680813EU OIL COOLER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH207 2884 OIL COOLER MOTOR INOPERATIVE. REMOVED AND REPLACED. 1G71 3U H9EU 20040521001242004052100124EA 2004 5 21 MASA200400193 120040413A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775995 7361 FORWARD CABIN DOOR WILL NOT CLOSE. MX CLOSED THE DOOR. NO PARTS USED 2L72 4F RTA21EA 20040521001272004052100127EA 2004 5 21 MASA200400203 120040415A5210 ROLLER CNDAIRCL600 CL6002C10 1390015EA PAX DOOR LACK OF LUBE A MASAK NONE O OTHER ININSP/MAINT 1 SW07509MJ 10094 THE CREW CALLED IN WITH PAX DOOR WILL NOT OPEN. MX TROUBLESHOT AND FOUND THE UPPER ROLLERS NEEDED LUBRICATION. MX GREASED ROLLERS IAW THE AMM. DOOR OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040521001292004052100129EA 2004 5 21 MASA200400207 120040417A2741 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA STAB TRIM MALFUNCTIONED A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW07512MJ 10109 DECLARED AN EMERGENCY DURING LANDING DUE TO STAB TRIM W/N RE-ENGAGE. MX WAS CALLED. MX COULD NOT DUPLICATE DISCREPANCY. NO PARTS USED 2L72 4F RTA21EA 20040521001332004052100133NM 2004 5 21 04FDEA001043 120040422A5320A5A71141 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 TO STA 1541, STR 40 LONGERON SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT LONGERON SPLICE REMOVED AS PER SRM 51-31-01 VOL II AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040521001352004052100135NM 2004 5 21 04FDEA001062 120040422A5347AFA77957 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CABIN SEAT TRACK CORRODED STA 1830 & STA 1671 LBL 27. CABIN SEAT TRACK CUT AND REMOVED AT STA 1651 TO STA 1887 LBL 27.5. REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040521001362004052100136CE 2004 5 21 GLBA20030621 120040504A31501293640919 CIRCUIT BOARD BEECH 1900 1900D 1154162CE ANNUNCIATOR MALFUNCTIONED A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03192GL UE192 AFX ANNUNCIATOR WILL NOT EXTINGUISH WHEN AUTO FEATHER IS ARMED, R&R PCB A123 PN 129-364091-9 2L72 4T RTA24CE 20040521001372004052100137WP 2004 5 21 ABXA040157 120040414A5754991932629 CLIP DOUG DC9 DC933F 302207AWP LT WING LE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 WING LEADING EDGE SPLICE ANGLE AND DOUBLER CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK. REPLACED ANGLE / DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040521001412004052100141WP 2004 5 21 ABXA040161 120040416A53409911840166 ATTACH FITTING DOUG DC9 DC933F 302207AWP FUSELAGE BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 ATTACH FITTING AND ANGLE AFT SIDE OF FRAME 1087 AT 12:30 POSITION, BROKEN. REPLACED IAW DC-9 SRM 51-30-1, 51-30-5 AND 51-30-2. 2L72 4F A6WE 20040521001442004052100144NM 2004 5 21 QXEA200400296 120040502A3260401020101 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM09406QX 4048 AFTER TAKEOFF AND SELECTED GEAR HANDLE UP, 3 GREEN LIGHTS REMAINED ILLUMINATED ALONG WITH 3 RED GEAR UNSAFE LIGHTS. GEAR DID NOT RETRACT. CYCLED LANDING GEAR SELECTOR PER CHECKLIST AND SAME SCENARIO OCCURRED FOR 15 SECONDS. GEAR RETRACTED AND INDICATION RETURNED TO NORMAL WITH NO CAUTION LIGHTS. HYDRAULIC PRESSURE AND QUANTITIES NORMAL. REMOVED AND REPLACED PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040521001452004052100145NM 2004 5 21 QXEA200400297 120040502A3260301450301 PSEU BOMBDRDHC8 DHC8401 1390041NM ZONE 200 MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09408QX5986 5986 4050 AFTER TAKEOFF, AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. COMPLIED WITH CHECKLIST. AFTER GEAR EXTENSION RED NOSE GEAR AND AMBER LIGHT REMAINED ILLUMINATED. COMPLETED ALTERNATE GEAR EXTENSION CHECKLIST. REMOVED AND REPLACED PSEU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040521001462004052100146EA 2004 5 21 QXEA200400298 120040503A2612 CIRCUIT BREAKER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 TRIPPED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09604QX 10019 FIRE SYSTEM FAULT. FOUND N2 FIRE DETECT B CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040521001472004052100147EA 2004 5 21 QXEA200400299 120040501A261247388904 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 MALFUNCTIONED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09607QX6478 6478 10024 FIRE SYSTEM FAULT STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED FIRE DETECTION AND EXTIGUISHING CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040521001482004052100148EA 2004 5 21 QXEA200400300 120040501A2121P196305 FILTER CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CLOGGED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09605QX 10022 "DISPLAY COOL" CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. EXTINGUISHED PER CHECKLIST. REILLUMINATED AFTER LANDING AND EXTINGUISHED AFTER CHECKLIST. FOUND DISPLAY FAN FILTER CLOGGED. REMOVED AND REPLACED FILTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040521001492004052100149EA 2004 5 21 QXEA200400294 120040502A5320 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 RIGHT HAND FUSELAGE INTERCOASTAL AT STATION 1084.2 IS CRACKED AT HYDRAULIC PRESSURE FEED LINE. REPAIRED IAW HORIZON AIR EO R-29-08 "B". 2L72 4F RTA21EA 20040521001502004052100150EA 2004 5 21 QXEA200400295 120040503A2612 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 LOOSE A QXEAK NONE N FALSE WARNING ININSP/MAINT 1 NM09603QX 10011 "FIRE SYSTEM FAULT" STATUS MESSAGE. FOUND J650 1.5 TURNS FROM TIGHT. TIGHTENED AND PERFORMED OPERATIONAL TEST OF THE FIDEX SYSTEM PER CRJ AMM TASK 26-10-00-710-801-A01. TESTED GOOD. NO PARTS REPLACED. 2L72 4F RTA21EA 20040521001522004052100152NM 2004 5 21 PCAA0405203 120040504A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM NR 2 INOPERATIVE A PCAAO OTHER L NO TEST NRNOT REPORTED 1 EA13839EX32399997 226 NR 2 SMOKE DETECTOR INOPERATIVE DURING TEST. MAINTENANCE REMOVED AND REPLACED NR 2 UNIT AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040521001552004052100155CE 2004 5 21 DXTA200400307 120040504A32601EN114N119 SQUAT SWITCH RAYTHNDH125 HAWKER800XP 7150012CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07824QS 258523 AFTER TAKE OFF OUT OF DAL GEAR WOULD NOT RETRACT, HANDLE WOULD COME UP. ACCOMPLISHED AIR TURN BACK - JACKED AIRCRAFT AND TROUBLESHOT SYSTEM, FOUND LEFT GEAR WEIGHT ON WHEEL SWITCH TO BE DEFECTIVE. REMOVED AND REPLACED SWITCH, PERFORMED OPERATIONAL CHECK, ALL CHECKED GOOD IAW HAWKER 800XP MM CHAPTER 32-30-01. 2L72 4F RTA3EU 20040521001572004052100157WP 2004 5 21 ABXA040169 120040428A57539955813509 FITTING DOUG DC9 DC931 3022065WP LT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 LEFT FLAP HAD CRACKED FITTING AT SPLICE BETWEEN NR 4 AND 5 REMOVEABLE TRAILING EDGE SEGMENTS. REPLACED 2 EACH NEW FITTINGS IAW DC-9 SRM 51-30-2 AND 51-30-1. P/N: 9955813-509 AND -507. 2L72 4F A6WE 20040521001592004052100159WP 2004 5 21 ABXA040162 120040422A57539957576501 PANEL DOUG DC9 DC931 3022065WP LT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 LEFT FLAP LOWER OUTBOARD SURFACE HAD NUMEROUS PLACES WITH SURFACE CORROSION AND EVIDENCE OF INNER CORROSION. SKIN BULGED AROUND RIVET HEADS. REPAIRED TRAILING EDGE SEGMENT IAW DC-9 SRM. 2L72 4F A6WE 20040521001602004052100160WP 2004 5 21 ABXA040163 120040423A5310591015915 DOOR FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 ANGLE CRACKED ON FORWARD SIDE OF LEFT FORWARD OVERWING EXIT DOOR JAMB AT FS 617, LONGERON 15 LT. REPLACED ANGLE IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20040521001612004052100161WP 2004 5 21 ABXA040164 120040423A55229918480501 SKIN DOUG DC9 DC931 3022065WP LT ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 LEFT ELEVATOR LOWER SKIN WAS BULGED AND CORRODED AROUND FASTENERS AND DOUBLER. REPAIRED ELEVATOR IAW DC-9 SRM. 2L72 4F A6WE 20040521001632004052100163WP 2004 5 21 ABXA040166 120040426A53135920319508 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 LONGERON 29 LT CRACKED AT STA. 588. REPAIRED LONGERON 29 LT IAW DC-9 SRM 53-02 AND REA D953-49676MR. 2L72 4F A6WE 20040521001652004052100165WP 2004 5 21 ABXA040168 120040427A5532591218849 PANEL DOUG DC9 DC931 3022065WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 LT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. P/N: 5912188-49 AND -50. 2L72 4F A6WE 20040521001662004052100166WP 2004 5 21 DHL2004802003 120040421A5720 FLANGE DOUG DC8 DC873 302199CWP WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 STA 966 INBOARD VERTICAL FLANGE OF SUPPORT, THERE IS A CRACK 2.5 INCHES LONG, FORWARD OF AFT BOLT. ACCOMPLISHMENT OF PERMANENT REPAIR REQUIRED BY 30 APR 04. STA. 966 XW3 THE INBOARD VERTICAL FLANGE OF THE SUPPORT, THERE IS A CRACK 2.5 INCH LONG, FORWARD OF AFT BOLT. INSTALLED *TEMPORARY REPAIR PER FAA FORM 8110-3 DATED 23 APR 04, BOEING MSG 1-DFUSS. TEMPORARY REPAIR GOOD FOR 7 REVENUE FLIGHT DAYS. REMOVED AND REPLACED LT STA NR 3 WING/FUSELAGE FITTING IAW DOUG DRAWING 589477 AND DC8 SRM 51-1-20. 2L74 4F RT4A25 20040521001672004052100167CE 2004 5 21 ACE050504 120040505A28221143890425 PUMP BEECH 1900 1900C 1154161CE FUEL SYSTEM LEAKING E YADAO OTHER K FLUID LOSS NRNOT REPORTED 1 AL03112AX 1267 UC45 PILOT REPORTED FUEL LEAKING FROM ENGINE DRAIN. MAINTENANCE REPLACED LOW PSI FUEL PUMP. 2L72 4T RTA24CE 20040521001682004052100168CE 2004 5 21 60211 120040401A5210MS212561 CABLE BEECH 1900 1900D 1154162CE PAX DOOR DAMAGED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07163YV UE163 UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR TO OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THUR EMERGENCY EXIT AT SEAT 6A ALL WERE DEPLANED WITH NO FURTHER INCIDENT. REINSTALLED PASS/DOOR FWD CABLE ON UPPER END. 2L72 4T RTA24CE 20040521001702004052100170EA 2004 5 21 QXEA200400302 120040502A3620 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ILLUMINATED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09615QX 10065 WHEN POWER MOVED FROM TOGO TO CLIMB, RIGHT BLEED DUCT WARNING MESSAGE (RED), AFTER 5 SECONDS, WARNING OUT AND REPLACED WITH RIGHT BLEED DUCT CAUTION MESSAGE (YELLOW). COMPLIED WITH ALL CHECKLISTS. MAINTENANCE INTERROGATED MDC, NO CURRENT FAULTS. NO CURRENT CAS MESSAGES. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERIVE. 2L72 4F RTA21EA 20040521001712004052100171NM 2004 5 21 04FDEA01006 120040418A5347ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN, STA 442 - 447 LBL 87 FOUND SEAT TRACK CORRODED. FWD CABIN SEAT TRACK AT STA 442 - 447 LBL 87 REMOVED AND INSTALLED IAW SRM 51-33-01 VOL II AND DWG NBA6022. 2L73 4F RTA22WE 20040521001722004052100172NM 2004 5 21 04FDEA01042 120040422A5320A5A7114517 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT, LT TUNNEL AT STA 5-113 - 1541, STR 38 SPLICE FOUND CRACKED. CENTER CARGO COMPARTMENT LT TUNNEL AT STA 5-113 - 1541, STR 38 SPLICE REMOVED AS PER SRM 51-31-01 VOL II AND INSTALLED NEW SPLICE AS PER SRM 51-33- 01 VOL II. 2L73 4F RTA22WE 20040521001732004052100173NM 2004 5 21 04FDEA01044 120040422A5315ABA8305501 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN STA 442 RBL 30, FOUND FLOORBEAM CORRODED. FWD CABIN STA 442 RBL 30 FLOORBEAM REMOVED AND INSTALLED AS PER SRM 51-33-01 VOL II AND DWG ABA8305. 2L73 4F RTA22WE 20040521001742004052100174NM 2004 5 21 04FDEA01060 120040422A5313AFA77751 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 CENTER CARGO COMPARTMENT AT STA 5-123 - 1561 LT LONGERON 48 FOUND CORROSED. CENTER CARGO COMPARTMENT AT STA 5-123 - 1561 LT LONGERON 48 REMOVED AND INSTALLED NEW LONGERON AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040521001762004052100176CE 2004 5 21 60684 120040419A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE ENGINES DAMAGED A AMWAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE07133YV UE133 ON TAXI OUT RT FIRE WALL T-HANDLE ILLUMINATED. BOTH ENGINES SHUT DOWN. PAX DEPLANED. AIRCRAFT WAS TOWED BACK TO GATE WITH NO FURTHER INCIDENT. FOUND & ELIMINATED LEAK, R&R FWD FIRE LOOP. 2L72 4T RTA24CE 20040521001772004052100177CE 2004 5 21 60658 120040418A2612 WARNING LIGHT BEECH 1900 1900D 1154162CE RT ENG FIRE FALSE ACTIVATIONA AMWAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE07133YV UE133 UPON TAXI RT FIREWALL FUEL VALVE ILLUMINATED. NO FIRE WAS VISUALLY NOTED AT NR 2 ENG. LT & RT FIRE EXTINGUISHING BOTTLES WERE DISCHARGED TO NR 2 ENG. AIRCRAFT SHUTDOWN ON TAXI WAY. PAX EVACUATED ON TAXI WAY. R & R FIRE BOTTLES SQUIBS. 2L72 4T RTA24CE 20040521001782004052100178 2004 5 21 66527 420040412A2300 RADIO BEECH 1900 1900D 1154162CE NR 1 & 2 NOISY A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07144ZV UE144 LOUD SQUEELING NOISE HEARD ON BOTH COMM NR 1 & 2. RERACKED NR 1 & 2 COMMS C/N DUP CKS GOOD. 2L72 4T RTA24CE 20040521001792004052100179CE 2004 5 21 60796 120040423A3297 WIRE BEECH 1900 1900D 1154162CE MLG DAMAGED A AMWAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 CE07135YV UE135 WITH GEAR SELECTED DOWN LT DOWN AND LOCK INDICATOR DID NOT ILLUMINATE. EMERGENCY DECLARED GEAR PUMPED DOWN. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REPAIRED WIRE W/SPLICE IN LT NACELLE TB 2L72 4T RTA24CE 20040521001802004052100180CE 2004 5 21 60795 120040423A32601293640797 ANNUNCIATOR BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER N FALSE WARNING APAPPROACH 1 CE07131YV UE131 ON APPROACH TO DRO WHEN GEAR WAS EXTENED. 3 GREENS WOULD NOT ILLUM LANDING GEAR IND C.B. POPPED GREEN NOTIFIED. MX CTRL ADVISED TO RETURN TO FMN. AIRCRAFT THEN RETURNED TO FMN DECLARED EMERGENCY AND LANDED WITH NO FURTHER INCIDENT. R & R ANNUNCIATOR PWR SOURCE PCB & WIRES ON HARN. P/N 129-364079-7. S/N 842A93 2L72 4T RTA24CE 20040521001832004052100183SO 2004 5 21 RAIA00405002 120040504A3397 WIRE EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCONNECTED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03804HK 145082 EMERGENCY EGRESS LIGHT AT ROW 8 INOP. MAINTENANCE REPAIRED WIRE AT LIGHT ASSY. 2L72 4F RTT00011AT 20040521001852004052100185SO 2004 5 21 LR7A04036 120040403A5320341973R FITTING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 FOUND RT MLG WHEEL WELL FS 497 BOW BEAM UPPER FITTING CRACKED AT RBL 62, WL250. FITTING REPLACED IAW SRM SMP 583 51-60 & 51-70. NR 2085. 2H74 4T A1SO 20040521001862004052100186SO 2004 5 21 LR7A04037 120040403A5310 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 FOUND RMLG WHEEL WELL BEAM ASSY CRACKED AT FS 530 AND 569, RBL 62, WL 240. REPLACED BEAM IAW SRM SMP 583 51-60 AND 51-70. NR 2086 2H74 4T A1SO 20040521001872004052100187SO 2004 5 21 LR7A04038 120040403A5230 STIFFENER LKHEED382 382G 526414USO CARGO DOOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5212 FOUND CARGO DOOR FS 1013 AFT BULKHEAD STIFFENERS CRACKED AT LBL 38 AND RBL 38. REPLACED STIFFENERS IAW SRM SMP 583 51-60 AND 51-70. NR 2119. 2H74 4T A1SO 20040521001882004052100188SO 2004 5 21 LR7A04039 120040403A5343370031 FITTING LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3215 FOUND NLG WHEEL WELL FS 196 DRAG BRACE MOUNTING FITTINGS WITH FRETTING CORROSION AT MOUNT HOLES LBL 8 AND RBL 8, WL 144. REPLACED FITTINGS IAW SRM SMP 583 51-60 AND 51-70. NR 2136. 2H74 4T A1SO 20040521001902004052100190SO 2004 5 21 LR7A04041 120040403A5315 FLOORBEAM LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED URINAL DRAIN LINE HOLES IN FS 817E FLOORBEAM WEB AT LBL 30 AND RBL 30, WL 140. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-17. NR 2155. 2H74 4T A1SO 20040521001912004052100191SO 2004 5 21 LR7A04042 120040403A5312 DOUBLER LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5317 FOUND FS 880 RT BULKHEAD WEB DOUBLER CRACKED AT RBL 62, WL 190. REPLACED DOUBLER IAW SRM SMP 583 51-60 AND 51-70. NR 2158. 2H74 4T A1SO 20040521001942004052100194SO 2004 5 21 LR7A04045 120040403A5340 ATTACH ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST5323 FOUND FS 848 FRAME ATTACH ANGLE CRACKED AT LBL 63, WL 182. REPAIRED IAW SRM SMP 583 53-50-10. NR 2171. 2H74 4T A1SO 20040521001952004052100195SO 2004 5 21 LR7A04046 120040403A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 FOUND RT MLG WHEEL WELL AFT BULKHEAD FS 617 PANEL RISER CRACKED AT RBL 73, WL 189. REPAIRED IAW SRM SMP 583 53-40-10. NR 2175. 2H74 4T A1SO 20040520000992004052000099WP 2004 5 20 ARWA20040201 120040202A5347 CARGO TRACK DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45688 DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT BETWEEN STA 940.000 AND STA 1500.000, RBL 58.5 INCHES TRACK WR SECTION WITH CORROSION. REMOVED CORROSION IN ACCORDANCE WITH DC-8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH DC-8 SRM 53-2-3; REMOVED FLOOR PANELS FROM MAIN CARGO COMPARTMENT IN ACCORDANCE WITH DC-8 MM 53-21-2, CUT OUT TRACK SECTION AND PREPARED NEW TRACK SECTION AND FABRICATED SPLICES IN ACCORDANCE WITH DC-8 SRM 53-2-3, TREATED AND PRIMED REPAIR AREA AND PARTS IN ACCORDANCE WITH DC-8 SRM 51-1-8; INSTALLED PARTS IN ACCORDANCE WITH SRM 53-2-3; REINSTALLED FLOOR PANELS IN ACCORDANCE WITH MM 53-21-2. 2L74 4F 4A25 20040520001132004052000113NM 2004 5 20 HNAA0400042 120040424A5270 WARNING LIGHT DHAV DHC8 DHC8201 2809001NM PAX DOOR ILLUMINATED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07985HA 479 AIRCRAFT LANDED 400 LBS OVER WEIGHT DUE TO RETURN TO FIELD, SEE ITEM ONE FOR MORE INFO. "LAV SERVICE DOOR POPPED OPEN." FERRIED AIRCRAFT TO SALISBURY FOR HARD LANDING INSPECTION AS PER POH 4.37.0 AND MM 05-50-00. SBY MAINTENANCE PERFORMED HARD LANDING GEAR INSPECTION IAW W.C. 05-50-11I. NO DEFECTS NOTED. 2H72 4T RTA13NM 20040520001242004052000124 2004 5 20 YENA200424 420040416A233010233940007 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15506JB1933 1235 F/A SMELLED BURNING ORANGE ODOR SHUT DOWN TV'S CALLED MX. PERFORMED INSPECTION OF LIVE TV & RECHECKED COMPONENTS IN ROW 12 THROUGH 17 AS NOTED BY THE FLIGHT CREW PER AMM 24-00-00-810-823 & INFO NOTICE 2003-T050TR A. NO DEFECTS NOTED. PRECAUTIONARY REASONS DEFERRED LIVE TV SYSTEM ON MEL 25-22-03. UPON ARRIVAL AT LGB INSPECTED LIVE TV COMPONENTS FROM ROW 10 THRU 19 IAW JB INFO NOTICE 2003-T050TR A. NO BURNING ODORS NOTICED IN CABIN. DURING INSPECTION OF SEB CONNECTIONS AT ROW 10B, NOTICED DISCOLORED PIN ON SEB CONNECTOR J2 AND ON MATING SEAT TO SEATCABLE P2 CONNECTOR. REMOVED AND REPLACED SEB AND SEAT TO SEAT CABLE AT 10B IAW AMM 23-39-00. LEFT LIVE TV OPERATING FOR 2 HOURS. ALL OPERATION NORMAL. CLEAR2L72 4F RTA28NM 20040520001352004052000135NM 2004 5 20 QXEA200400284 120040422A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09410QX 4053 DENT 18 INCHES AFT AND BELOW LEFT STRAKE. REPAIRED IAW Q400 TASK 25-32-00-400-801. 2H72 4T RTA13NM 20040520001392004052000139NM 2004 5 20 C1HA200485006 120040426A5752 SKIN BOEING727 7272S7 138407ZNM AILERON TAB DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15685CA 22492 LT INBD AILERON TAB 4 DENTS BEYOND SRM LIMITS HOT BOND REPAIRED, WEIGH AND BALANCE REQUIRED 2L73 4F A3WE 20040520001782004052000178EU 2004 5 20 KBM2004F00048 120040429A36100301027300 PIPE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE FREE TURBINE CHAFED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 4126 ENGINE P2 AIR PIPE SUPPLYING AIR TO MODULE 5 BEARING HAS DEEP CHAFE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040520001802004052000180 2004 5 20 KBM2004F00045 420040127A3420350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P878 2342 TAIL ROTOR SPHERICAL. LAMINATE BEARINGS WORN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040520001822004052000182EU 2004 5 20 KBM2004F00050 120040411A7931642790041 TRANSMITTER SNIAS 350 AS350B1 8680811EU OIL PRESSURE FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 FLUCTUATION IN OIL PRESSURE. REMOVED AND REPLACED. 1G71 3U H9EU 20040520001842004052000184 2004 5 20 KBM2004F00054 420040505A34215040017901 GYRO SNIAS 350 AS350BA 8680817EU ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH604 2337 (ATT GYRO) ATT INDICATOR FLAG STAYS UP. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040520001862004052000186EU 2004 5 20 KBM2004F00049 120040218A2840647510033 PROBE SNIAS 350 AS350B1 8680811EU FUEL SYSTEM STICKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 FUEL PROBE, INTERMITTENTLY STICKS BETWEEN APPROX 25-35 PERCENT INDICATED. REMOVED AND REPLACED. 1G71 3U H9EU 20040520001882004052000188 2004 5 20 KBM2004F00052 420040202A3120271600 GAUGE SNIAS 350 AS350BA 8680817EU OAT INACCURATE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 OAT GAUGE IS INACCURATE. REMOVED AND REPLACED WITH NEW GAUGE. 1G71 3U NCH9EU 20040520001902004052000190EU 2004 5 20 KMB2004F00000 120040202A71601206502A ACTUATOR SNIAS 350 AS350BA 8680817EU AIR INTAKE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 ENGINE ALTERNATE AIR INTAKE DOORS WILL NOT ACTUATE, OPEN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040520002902004052000290WP 2004 5 20 0400629855 120040426A2913AS19593C PUMP DOUG DC9 DC951 3022051WP RT HYD SYSTEM FAILED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 GL01764NC 47717 PILOT REPORTED THE LOSS OF HYDRAULIC FLUID FROM THE RIGHT HYDRAULIC SYSTEM. LANDING WAS WITHOUT INCIDENT AND MAINTENANCE FOUND THE ELECTRICAL AUXILIARY PUMP LEAKING FROM A SPLIT DRAIN LINE. THE ELECTRIC AUXILIARY PUMP AND THE RIGHT ENGINE DRIVEN PUMP WERE REPLACED, THE CASE DRAIN FILTER WAS CHECKED, AND A FUNCTIONAL LEAK CHECK WAS ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20040521000042004052100004SO 2004 5 21 RAIA00404017 120040405A32420123AFU1 SENSOR EMB 145 EMB145LR 3260212SO RT BRAKE FLUCTUATES A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03823HK2901 145475 RT INBOARD BRAKE TEMP INDICATION FLUCTUATES. MAINTENANCE DEFERRED RT I/B BRAKE TEMP INDICATION SYSTEM PER MEL 32-40-1. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE RT I/B BRAKE TEMP SENSOR. 2L72 4T RTT00011AT 20040521000082004052100008SO 2004 5 21 GLBA20030619 120040429A3210 LANDING GEAR EMB 120 EMB120ER 3260203SO LEFT MALFUNCTIONED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM0396ZK 120096 LT MLG WOULD NOT RETRACT, PREFORMED GEAR SWING NO DEFECTS NOTED OPS CK GOOD 2L72 4T RTA31SO 20040521000092004052100009NM 2004 5 21 QXEA200400292 120040429A335061047811 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09347PH504 504 480 FLOOR TRACK EMERGENCY LIGHTING STRIP AT ROW 7 AND LT EMERGENCY EXIT MARKER AT ROW 3 IS INOPERATIVE. REMOVED AND REPLACED BATTERY. 2H72 4T RTA13NM 20040521000202004052100020NM 2004 5 21 04FDEA001066 120040422A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT RT TUNNEL STR 38 AT STA 1119 - STA 6-10 LONGERON SPLICE FOUND CRACKED. **** S/D COMING **** 2L73 4F RTA22WE 20040521000222004052100022EU 2004 5 21 DHL2004362003 120040430A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU CARGO BAY WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01362DH 84 ELEC. CARGO SMOKE DETECTION WILL NOT TEST. RESET SYSTEM OPS CKS GOOD IAW M/M 26-14-00. 2L72 4F RTA35EU 20040521000382004052100038EU 2004 5 21 KBM2004F00074 120040315A2150507 COMPRESSOR SNIAS 350 AS350BA 8680817EU AIR CONDITIONER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH3 2957 AIR CONDITIONER, INOPERATIVE. COMPRESSOR FAILED. REMOVED AND REPLACED COMPRESSOR. 1G71 3U NCH9EU 20040521000442004052100044EU 2004 5 21 KBM2004F00077 120040406A792147750 MOTOR SNIAS 350 AS350B1 8680811EU OIL COOLER SHORTED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2350 2009 OIL COOLER MOTOR HAS AN INTERNAL SHORT. REMOVED AND REPLACED. 1G71 3U H9EU 20040521000542004052100054EU 2004 5 21 DHL2004364505 120040313A5347602245 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, CABIN-SEAT TRACK, 3RD FROM SIDE HAS HEAVY CORROSION AFT OF FRAME 20. REMOVED CORROSION FROM SEAT TRACK FRAME 20 LBL 57. FOUND TO BE OUT OF LIMITS IAW SRM. CUT OUT SEAT TRACK SECTION FROM FR. TO 21.5 LBL 57 IAW SRM. TRIMMED TO FIT NEW SEAT TRACK SECTION IAW SRM. TREATED, PRIMED, AND POLIWHITE NEW TRACK SECTION AND SPLICES IAW SRM. INSTALLED SEAT TRACK SECTION FROM FR. 19 TO 21.5 LBL 57 IAW SRM. 2L72 4F RTA35EU 20040521000562004052100056NE 2004 5 21 ARWA20040401 220040417A7532S633883 BLEED VALVE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 3 ENGINE SURGES A ARWAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO19906R 46087 ON TAKEOFF ROLL NR 3 ENGINE EPR INDICATOR SUDDENLY INCREASED TO 2.02 UNITS AFTER ALL ENGINES HAD BEEN SPOOLED AND STABLE AND ALL POWER LEVERS ALIGNED. EGT ALSO INCREASED TO MAX TAKEOFF LIMITS. ABORTED TAKEOFF AT 80 KIAS AND REJECTED TAKEOFF CHECKLIST WAS ACCOMPLISHED. CHECKED NR 3 ENGINE AT BLAST FENCE; PERFORMED RUN UP AND TROUBLE-SHOOTING INDICATES EPR SYSTEM ERRONEUS; ALL OTHER PARAMETERS FOUND NORMAL IAW MM. ENTERED NR 3 EPR SYSTEM ON DMI 18494 AS PER MEL 77-1-2 CATEGORY A. CLEARED DMI 18494 ON 4/17/04; DURING RUN-UP FOUND COMPRESSOR BLEED VALVE OUT OF SCHEDULE (STICKING) REMOVED & REPLACED NR 3 SURGE BLEED VALVE IAW MM 75-30-3. OPERATIONAL CHECK NORMAL, ALL PARAMETERS OK. 2L74 4F4 F 4A25 1E8 20040521000742004052100074EA 2004 5 21 MASA200400219 120040421A2730 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM LOOSE A MASAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW07650ML 7137 DURING CRUISE, THE STAB TRIM MOVED UN-COMMANDED. MX OP CHECKED SYSTEM AND FOUND NO FAULTS. DURING OVER NIGHT MX THE FO'S TRIM SWITCH WAS FOUND TO BE LOOSE IN THE YOKE AND WAS REINSTALLED. OP CHECKS GOOD. NO PARTS USED 2L72 4F RTA21EA 20040521000792004052100079NE 2004 5 21 MASA200400045 220040125A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT HOT START A MASAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SW0717217 7217 873138 CREW REPORTED LEFT ENGINE HOT START. MX DRY MOTORED AND THAN STARTED THE ENG. OP CHECKS GOOD. NO PARTS USED 2L72 4F4 FRTA21EA E15NE 20040521000912004052100091EA 2004 5 21 MASA200400109 120040224A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07591ML5766 7388 LT FS 625 OBLIQUE ANGLE IS CRACKED. REPLACED 625 OBLIQUE ANGLE IAW BOMB CRJ SRM 51-42-21. 2L72 4F RTA21EA 20040521000922004052100092EA 2004 5 21 MASA200400114 120040226A5753 FLAP CNDAIRCL600 CL6002B19 1900309EA CONTAMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0737208 7208 AFTER TAKE-OFF THE FLAPS WOULD NOT RETRACT, THE LANDING GEAR WOULD NOT RETRACT PROPERLY AND SEVERAL WING ANTI-ICE MSGS APPEARED. THE A/C RETURNED TO THE FIELD WERE MX FOUND ICE FOULING THE FLAPS AND LANDING GEAR. AFTER RESETTING THE FLAPS AND CLEARING THE ICE FROM THE A/C EVERYTHING CHECKED OK. NO PARTS USED 2L72 4F RTA21EA 20040521000962004052100096CE 2004 5 21 DXTA200400284 120040331A326065430087 UPLOCK SWITCH CESSNA500 560CESSNA 2076750CE MLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07333QS 5600333 RT MLG WOULD NOT RETRACT ON DEPARTURE, LANDING GEAR EMERGENCY T-HANDLE PULLED AND MLG PNEUMATIC BOTTLE DISCHARGED. TROUBLESHOT RIGHT MAIN GEAR, JACKED AIRCRAFT AND PERFORMED RETRACTION CHECK FOUND RT MLG UP-LOCK FAILED. REMOVED AND REPLACED UP-LOCK SWITCH PER CESSNA 560 MM CHAPTER 32-31-05, OPS CHECKED GOOD. 2L72 4F RTA22CE 20040521001092004052100109EA 2004 5 21 MASA200400155 120040319A2120P196305 FILTER CNDAIRCL600 CL6002B19 1900309EA AIR CONDITIONERSODOR A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0717231 7231 A/C RETURNED TO FIELD. CREW REPORTED A LAV SMOKE DETECTION AND ELECTRICAL SMOKE ODOR IN CABIN. MX INSPECTED THE A/C LAV AREA BUT COULD NOT FIND EVIDENCE OF A PROBLEM. MX PERFORMED ENGINE RUNS AND THE ODOR WAS COMING THROUGH THE AIR CONDITIONING SYSTEM. MX REPLACED THE DUCT FILTERS. OP CHECKS GOOD. 2L72 4F RTA21EA 20040521001192004052100119EU 2004 5 21 KBM2004F00086 120040409A77129550176240 TRANSMITTER SNIAS 350 AS350B2 8680813EU ENGINE TORQUE READS HIGH E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19884SH 2884 TORQUE READING 10-15 PERCENT HIGH AND FUNCTUATING. REMOVED AND REPLACED. 1G71 3U H9EU 20040521001232004052100123EA 2004 5 21 MASA200400190 120040407A5240 HANDLE CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775987 5987 CREW REPORTED SERVICE DOOR STOW HANDLE BROKEN INSIDE. MX RESECURED. NO PARTS USED 2L72 4F RTA21EA 20040521001252004052100125EA 2004 5 21 MASA200400194 120040413A52103864110N503 COVER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HINGE BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW071721715629 7217 CREW REPORTED THE PAX DOOR HINGE BROKEN WILL NOT ALLOW DOOR TO OPEN FROM THE OUTSIDE. A/C WILL FERRY TO OKC FOR REPAIR.4/14/2004. MX REPLACED THE HINDGE COVER. 2L72 4F RTA21EA 20040521001282004052100128EA 2004 5 21 MASA200400206 120040417A216035002300 CHECK VALVE CNDAIRCL600 CL6002B19 1900309EA FAN INOPERATIVE A MASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0717231 7231 DURING TAXI, THE FLIGHT ATTENDANT SAW AND SMELLED SMOKE COMING FROM THE AFT INSIDE CABIN OUT OF THE FLOOR VENTS. THE CREW DECLARED A GROUND EMERGENCY. MX WAS CALLED AND FOUND THE RIGHT PACK HAD OVERTEMPED. MX PLACED IT ON MEL. MX PERFORMED ENGINE RUNS. MX REPLACED FAN BY-PASS CHECK VALVE NO FURTHER DISCREPANCIES FOUND. 2L72 4F RTA21EA 20040521001312004052100131EA 2004 5 21 MASA200400216 120040421A2741 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A MASAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW07650ML 7173 DURING FLIGHT THE STAB TRIM MOVED UNCOMMANDED IN SMALL INCREMENTS. MX INSPECTED AND RESET THE SYSTEM BUT COULD NOT DUPLICATE THE PROBLEM. NO PARTS USED 2L72 4F RTA21EA 20040521001382004052100138WP 2004 5 21 ABXA040160 120040416A5347591076928 SEAT TRACK DOUG DC9 DC933F 302207AWP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 SEAT TRACK UPPER INBOARD FLANGE CORRODED AROUND FASTENER HOLES AT FS 908 - 945, RBL 44 AND FLANGE CRACKED AT FS 945. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1 AND 53-05. 2L72 4F A6WE 20040521001402004052100140WP 2004 5 21 ABXA040159 120040415A5310991224314 SHEAR TIE DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 SHEAR TIE CRACKED FS 965 AT LONGERON 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040521001512004052100151NM 2004 5 21 WRLA200419 120040427A2430SM600BA40N24 RCCB DOUG MD11 MD11F 3023600NM NR 3 DC BUS INOPERATIVE A WRLAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11276WA 48632 INFLIGHT LOST NR 3 DC BUSS, WORLD AIRWAYS DIRECTED THE CREWS TO RETURN TO THE POINT OF TAKEOFF (RCTP), THE CREWS THEY HAD TO DUMP FUEL TO FACILITATE THE MAX GROSS LANDING WEIGHT. REMOVED AND REPLACED THE RCCB RELAY NR 3 DC BUSS CHECKED NORMAL AIRCRAFT BACK TO THE SERVICE. 2L73 4F RTA22WE 20040521001582004052100158 2004 5 21 ABXA040170 420040504A2565 SPRING BOEING767 767231 1385131NM ESCAPE SLIDE FAILED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23702AX 22566 MAIN ENTRY DOOR ESCAPE SLIDE DEPLOYMENT BAR WOULD NOT STAY UP. REPLACED DEPLOYMENT BAR GAS SPRINGS. OPS CHECKED GOOD IAW B767 AMM 26-66-01. 2L72 4F RTA1NM 20040521001812004052100181CE 2004 5 21 60830 120040425A3297 WIRE BEECH 1900 1900D 1154162CE DOWNLOCK DAMAGED A AMWAO OTHER N FALSE WARNING APAPPROACH 1 CE07138YV UE138 ON APPROACH NLG VISUAL TO CONFIRM GEAR DOWN. LANDED NO FURTHER INCIDENT. NSP'D NLG REPAIRED WIRES ON DOWNLOCK 2L72 4T RTA24CE 20040521001892004052100189SO 2004 5 21 LR7A04040 120040403A5320 STIFFENER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3215 FOUND NLG WHEEL WELL FS 196 STIFFENER CRACKED AT BL 0, WL 144. REPLACED STIFFENER IAW SRM SMP 583 51-60 AND 51-70. NR 2137. 2H74 4T A1SO 20040521001932004052100193SO 2004 5 21 LR7A04044 120040403A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HST5323 FOUND FS 836 FRAME BRACKET CRACKED AT RBL 70, WL 190. REPAIRED IAW SRM SMP 583 51-140-19. NR 2170. 2H74 4T A1SO 20040521001982004052100198SO 2004 5 21 LR7A04049 120040403A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED INS TEMP PROBE AT FS 228, LBL 60, WL 245. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-10. NR 2186. 2H74 4T A1SO 20040521001992004052100199SO 2004 5 21 LR7A04050 120040403A5512 DOUBLER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5511 FOUND FS 1063 LOWER HORIZONTAL STABILIZER DOUBLER CRACKED AT RH HSS 61, WL 280. REPLACED DOUBLER IAW SRM SMP 583 51-60 AND 51-70. NR 2190. 2H74 4T A1SO 20040521002002004052100200SO 2004 5 21 LR7A04051 120040403A5320 CHANNEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5314 FOUND FS 836 LT BULKHEAD CHANNEL CRACKED AT LBL 70, WL 185. REPAIRED IAW SRM SMP 583 51-140-19. NR 2191. 2H74 4T A1SO 20040524000022004052400002WP 2004 5 24 IXXA0400053S 120040328A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA XW 485.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT DWG V22-R02, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, 51-1-20D PAGE 21, 51-3-0 PAGE 1, REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGE 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 TRIMMED OUT THE DAMAGED AREA IAW DWG V22-RO2, PERFORMED NOT INSPECTION IAW DC8 NOT SPM PART 6-10-01.001, CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED A REPAIR DOUBLER AND A FILLER. 2L74 4F RT4A25 20040524000052004052400005SO 2004 5 24 GLBA20030626 120040518A612078249046 PCU EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE NR 1 ENGINE INOPERATIVE A GLBAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM0396ZK 11203 120096 NR 1 ENG LOSS OF OIL PRESSURE, REMOVED AND REPLACED NR 1 ENG PCU. 2L72 4T4 TRTA31SO E20NE 20040524000062004052400006EA 2004 5 24 SWIA200413292 120040503A53206013501251 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 FS 625 LT OBLIQUE ANGLE P/N 6013501251 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-21-16, 51-23-00, AND 52-42-06. SEE RII53-401. 2L72 4F RTA21EA 20040524000072004052400007WP 2004 5 24 DHL2004803529 120040412A57203645611U BRACKET DOUG DC8 DC873 302199CWP FWD BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 4 ALT. TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET IAW DC8 SRM 51-1-20D PG. 21,9. REFER TO NR. 0341 FOR LEAK CHECK 2L74 4F RT4A25 20040524000082004052400008WP 2004 5 24 DHL2004803507 120040324A5712 RIB DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT OUTER WING OB. L/E FORMER CRACKED 0.250 AT XFS 760.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-20D PG.9, SRM 57-2-0 PG. 9-10. 2L74 4F RT4A25 20040524000092004052400009WP 2004 5 24 DHL2004803508 120040324A5712 RIB DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT OUTER WING OB L/E FORMER CRACKED 0.250 AT XFS 822.000 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. FABRICATED DOUBLER (2024-T3 AL 0.032) IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PG. 9-10, SRM 51-1-20D PG. 9 2L74 4F RT4A25 20040524000102004052400010WP 2004 5 24 DHL2004803502 120040320A5315 FLOORBEAM DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 ITEM REF. NR. 1122: MAIN CARGO COMPT. NR 7 FLOORBEAM LUGS WORN, STA. 1120.000. CUT OUT NR 7 FLOORBEAM DAMAGE SECTION IAW SRM 53-2-3 PG.17 FIG. 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND FLOORBEAM PLUG IAW SRM 51-3-0 PG.1, SRM 53-2-3 PG. 17-19 2L74 4F RT4A25 20040524000112004052400011WP 2004 5 24 DHL2004803506 120040324A5330 SKIN DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 EXTERNAL FUSELAGE SKIN CRACKED 0.500 AT STA.1747.000,L15 TO L16R. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG. 7 REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 PAGES 103, 104 FIG.7, SHEET 3. FABRICATED FILLER (7075T6 0.063) FINGER DOUBLER (7075T6 0.040) DOUBLER (7075T6 0.071) IAW SRM 53-2-1 PAGES 99,100 FIG.7 SHEET 1.CLEANED, TREATED AND PRIMED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER, FINGER DOUBLER AND DOUBLER IAW SRM 53-2-1 PAGES 99, 100 SRM 51-1-21 PAGE1. SRM 51-1-20D PAGE 9 (WITH NEW FASTENERS). 2L74 4F RT4A25 20040524000122004052400012WP 2004 5 24 DHL2004803511 120040324A5712 RIB DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT OUTER WING OB L/E FORMER CRACKED 0.250 (UPPER PART) STA XFS. 835.000 REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1 FABRICATED DOUBLER (2024T3 AL,0.032) IAW SRM 57-2-0 PAGES 9, 10. CLEANED TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PAGES 9, 10, SRM 51-1-20D PAGE 9. 2L74 4F RT4A25 20040524000132004052400013WP 2004 5 24 DHL2004803512 120040319A5531 RIB DOUG DC8 DC873 302199CWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 VERTICAL STABILIZER L/E FORMER CRACKED 0.500 STA. XFS 110.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (2024-T3AL 0.032) UAW SRN 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG. 7-8, SRM 51-1-20D PG. 9. 2L74 4F RT4A25 20040524000142004052400014WP 2004 5 24 DHL2004803537 120040422A5730 SKIN DOUG DC8 DC873 302199CWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RT WING CTR L/E EXTERIOR SURFACE SHOWS CORROSION AT STA. XW 257.500. PERFORMED MAJOR REPAIR IAW ED NR EDV43-5, DWG V43-R05. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.11. TRIMMED OUT CORRODED SECTION IAW ED EDV43-5, DWG V43-R05. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.071) IAW ED EDV43-5, DWG V43-R05. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS. 2L74 4F RT4A25 20040524000152004052400015WP 2004 5 24 DHL2004803538 120040422A5754 VANE DOUG DC8 DC873 302199CWP LT WING LE FLAP ELONGATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING IB. VANE SLOR HOLES ELONGATED STA XS 247.000. PERFORMED MAJOR REPAIR IAW ED EDV43-9, DWG V43-R09. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1, SRM 51-1-20D PG.21. TRIMMED OUT DAMAGED SECTION IAW ED ECV43-9, DWG V43-R09. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6AL 0.063) AND DOUBLER (7075-T6AL 0.071) IAW ED EDV43-9, DWG V43-R09. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS IAW ED EDV43-9, DWG V43-R09, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2L74 4F RT4A25 20040524000222004052400022EU 2004 5 24 MALA040390 120040429A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15511XJ E2325 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN 61-2275-1, SN/9808677 WAS REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/20/04. UNIT FAILED CAP CHECK ON 4/29/04. MAINTENANCE REPLACED BATTERY PACK CELL PN 61-2274-1 UNIT CHARGED AND PASSED COMM TESTS. A/C RELEASE DATE 5/01/2004 2H74 4F4 FRTA49EU E6NE 20040524000232004052400023EU 2004 5 24 MALA040398 120040430A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 DURING 4K INSPECTION IN LCQ, FS 364 RT FUSELAGE HAS DENTS. CUT OUT DENTED AREA FABRICATED, LOCATED DRILLED AND INSTALLED AN EXTERNAL DOUBLER REPAIR IAW EO NR S53009. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2L72 4T RTA52EU 20040524000242004052400024EU 2004 5 24 MALA040393 120040429A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15452XJ 340B452 EMERGENCY POWER SUPPLY PN 3301-51 SN/1331 REPORTEDLY DO NOT HOLD CHARGE. REPLACED BATTERY ASSEMBLY 3301-31 AND UNIT PASSED CMM CHECKS ON 5/6/04. REFER TO IN HOUSE WO NR 367478 FOR ADDITIONAL DETAIL. 2L72 4T RTA52EU 20040524000252004052400025EU 2004 5 24 MALA040400 120040505A3350 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15422XJ 340B422 DURING CAPACITY TEST EMERGENCY BATTERY FAILED TEST. REPLACED 20LN AND 24LN OPS CHECK GOOD SEE JOB CARD 335003 WO NR 367398 FOR DETAILS REPLACED 20LN AND 24LN. OPS CHECK GOOD, SEE JOB CARD 335003 WO NR 367398 FOR DETAILS. 2L72 4T RTA52EU 20040524000262004052400026EU 2004 5 24 MALA040397 120040430A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 DURING 4K INSPECTION IN LCQ, BS 362 LT FUSELAGE HAD DENTS. CUT OUT DENTED, FABRICATED, LOCATED, DRILLED AN EXTERNAL DOUBLER REPAIR IAW MESABA EO NR S53009. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2L72 4T RTA52EU 20040524000272004052400027EU 2004 5 24 MALA040399 120040508A5511 SPAR SAAB SF340 340B 7860101EU HORIZONTAL STAB DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15362PX 340B258 DURING 4K INSPECTION IN LCQ, HORIZONTAL STABILIZER FWD SPAR COLD WORKING. COLD WORKED FASTENER HOLES ON THE HS FWD SPAR IAW SB 340-55-034, DATED 16 OCT 1998. TERMINATING ACTION FOR AD 99-19-21. REPAIRED IAW EO NR AD991921-03. A/C RELEASE DATE 5/10/04. REFER TO LOG PAGE NR 1204180 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040524000292004052400029EU 2004 5 24 MALA040392 120040429A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15361PX 340B249 DURING CAPACITY CHECK, BATTERY PACK EMERGENCY POWER SUPPLY WAS REMOVED FOR SCHEDULED DISCHARGE CHECK ON 4/16/04. CAP CHECK FAILED ON 4/29/04. REPLACED BOTH CELL PACKS PN 549-1324-06 AND UNIT THEN PASSED CMM CHECKS. A/C RETURNED TO SERVICE 5/6/04. REFER TO IN HOUSE WO NR 366385 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040524000312004052400031SO 2004 5 24 C2XA04CL052 120040511A3350 LIGHT EMB 145 EMB145XR 3260214SO ROW 12 INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 CLE FLIGHT NR 2021 THE CREW REPORTED THE ROW 12 EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. 2L72 4F RT 20040524000332004052400033WP 2004 5 24 IXXA0400050S 120040212A5320 PLATE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND CORROSION AND CRACK DAMAGE IN FUSELAGE FORWARD CTR. SECTION LOWER PLATING STA. 580.00 L-36. REPAIR WAS ACCOMPLISHED. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG2M. REMOVED FASTENERS AND DAMAGED SECTION IAW DWG V22-R10. PERFORMED NDT INSPECTION IAW DC8 NDT PART 6-10-01-001. FABRICATED FILLER, FINGER DOUBLER IAW DWG V22-R10.CLEANED, TREATED AND PRIMED AREA. FINGER DOUBLER & FILLER AND INSTALLED. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG9. 2L74 4F RT4A25 20040524000342004052400034WP 2004 5 24 IXXA0400051S 120040211A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND LT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA.XW. 485.000. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED AREA IAW DWGV22-R01 INCLUDING FASTENERS AND CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-21 PG.1, 51-1-20D PG. 21 AND SRM 51-1-8 PG. 17-18. NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01.001 AREA WAS CLEANED, TREATED AND PRIMED. FABRICATED A REPAIR DOUBLER AND FILLER . CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND THE FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DCI SRM 51-1-11 PG 9. INSTALLED THE REPAIR DOUBLER AND FILLER USING THE NEW FASTENERS IAW DWG. V22-R01 AND DC8 SRM 51-1-21 PG 1 AND 51-1-20D P2L74 4F RT4A25 20040524000392004052400039NM 2004 5 24 ASMF200405023 120040519A7920 WARNING LIGHT DOUG MD88 MD88 3023688NM ENGINE OIL ILLUMINATED W ASMFO OTHER M OVER TEMP CLCLIMB 1 SW23158PL 49761 AIRCRAFT RETURNED OF FLIGHT, HIGH OIL TEMPERATURE ON LT ENGINE WITH 160 DEGREES C AND 60 PSI. DURING MAINTENANCE REVISION, OIL QUANTITY ON BOTH ENGINES WERE CHECKED AND WAS DETECTED, ENGINE NR 1 WITH 18 QUARTERS AND ENGINE NR 2 WITH 1 QUARTER, CHIPS DETECTORS, FUEL CONTROL VALVE AND CSD OIL LEVEL WERE CHECKED, ALL CORRECT. LT ENGINE OIL SERVICE WAS PERFORMED IAW MM 12-12-04, ALL CORRECT. 2L72 4F RTA6WE 20040524000402004052400040NE 2004 5 24 ASMF200405020 220040517A7261 SEAL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE CRACKED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23881LF 53051 726001 DURING TRANSIT CHECK AN OIL LEAK WAS DETECTED ON RT ENGINE. CHIPS DETECTORS, OIL FILTER, N1 AND N2 WERE CHECKED AND OIL QUANTITY WAS 4 QUARTERS. SEAL OF BEARING NR 6 WAS DETECTED WITH CRACK AND SEAL WAS REPLACED IAW MM 72-53-40, TEST CORRECT. 2L72 4F4 FRT E9NE 20040524000412004052400041WP 2004 5 24 ASMF200405022 120040519A2751 SWITCH DOUG DC9 DC982 3022082WP TAKEOFF WARNING OUT OF ADJUST W ASMFD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23491SH 49150 AIRCRAFT RETURNED TO PLATFORM, (TAKE OFF) WARNING FLAG SHOWS, DURING TAKE OFF CONFIGURATION. DURING MAINTENANCE REVISION, FLAPS WERE OPERATED AND FAIL CONTINUE. VISUAL INSPECTION WAS PERFORMED AND WAS DETECTED THAT THE FLAP LEVER DOES NOT ACTUATE THE TAKE OFF SWITCH. AIRCRAFT WAS SENT TO THE HANGAR AND TAKE OFF WARNING SWITCH WAS ADJUSTED IAW MM 27-53-01 AND TESTED IAW MM 27-00-00, ALL CORRECT. 2L72 4F A6WE 20040524000432004052400043SO 2004 5 24 C2XA04TY085 120040523A532014521725613 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712567 145623 DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINT. REMOVED THE REPLACED THE SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02 AND IC-2004145/2152. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040524000452004052400045EU 2004 5 24 AWXA200400557 120040521A7711005RL03 RELAY AIRBUS320 A320231 3930325EU NR 1 ENGINE FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28636AW3999526325 098 ABORTED TAKEOFF, FLT 0018, ON TAKEOFF AT PHX EN ROUTE FOR JFK AT 60 KTS NR 1 ENGINE INDICATED 1.390 EPR AND RT ENGINE INDICATED 1.401 EPR, TARGET TOGO WAS 1.401, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE RELAY BOX (4100KS) IAW AMM 71-51-49-04, OPERATIONAL CHECK WAS GOOD. TEARDOWN/FUNCTIONAL CHECK OF RELAY BOX S/N 1044 PRODUCED NO DISCREPANCIES. UNIT WAS OPENED, INSPECTED, AND TESTED UNDER ALL TEMPERATURE CYCLES PER CMM 71-51-49, REV. 3, NO FAULTS NOTED. 2L72 4F RTA28NM 20040524000462004052400046NM 2004 5 24 AWXA200400558 120040430A53116545810 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MAJOR REPAIR, DURING C-17 CHECK A .6875 INCH CRACK WAS FOUND IN FRAME END ABOVE THE L-1 DOOR AT BS 312, STR 6 LT. MAINTENANCE TRIMMED OUT THE CRACK IN FRAME END AT BS 312, STR 6 LT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND REPAIR CHANNEL, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG. 101. 2L72 4F RTA16WE 20040524000482004052400048NM 2004 5 24 AWXA200400560 120040505A322010621955 BEARING BOEING737 7373Y0 1384671NM TRUNNION CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LANDING GEAR, DURING C-15 CHECK CORROSION WAS FOUND ON THE NOSE LANDING GEAR (NLG) DRAG BRACE RT TRUNNION BEARING. MAINTENANCE REMOVED AND REPLACED CORRODED NLG DRAG BRACE RT TRUNNION BEARING IAW BMM 32-21-61-4. 2L72 4F RTA16WE 20040524000512004052400051WP 2004 5 24 UPS04842394 120040507A57403704841501 FITTING DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, NR 3 MAIN FUEL TANK HAS STRINGER 51 END FITTINGS CRACKED AT XRS 74. REMOVED AND REPLACED FITTINGS IAW DWG. 3704841 AND SRM. 51-1-20D, 51-3-0 2L74 4F RT4A25 20040524000522004052400052WP 2004 5 24 UPS04842395 120040509A5313 LONGERON DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 680 LONG. 9L IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 650-680,FABRICATED AND INSTALLED LONGERON SECTION IAW SRM. 53-2-2 FIG. 10. 2L74 4F RT4A25 20040524000532004052400053WP 2004 5 24 UPS04842396 120040507A534037558451N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 34L TO 35L. REMOVED AND REPLACED FITTING IAW DWG. 3755845 AND SRM. 53-2-0 FIG. 2D. 2L74 4F RT4A25 20040524000562004052400056EU 2004 5 24 EHA2004F00001 120040314A71700174038010 DRAIN VALVE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1E 60030NE NR 1 ENGINE LEAKING E EHAAO OTHER O OTHER NRNOT REPORTED 1 AL03141LG 7503 18019 PILOT REPORTED EXCESSIVE FUEL SMELL AFTER STARTING NR 1 ENGINE PILOT SHUT DOWN ENGINE DURING RESTART OBSERVED LARGE AMOUNT OF FUEL POURING OVER ENGINE FROM THE TOP SIDE OF ENGINE. UPON INVESTIGATION FOUND START DRAIN VALVE LEAKING. REPLACED START DRAIN VALVE, LEAK CHECKED GOOD AC RETURNED TO SERVICE. 1G72 3U3 UNCH13EU E19EU 20040524000572004052400057SW 2004 5 24 R322004F00000 120040427A6410206016201131 BLADE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TAIL ROTOR DEBONDED E R32AO OTHER O OTHER NRNOT REPORTED 1 EA21206TH1673 4217 TAIL ROTOR BLADES, NO MECHANICAL DIFFICULTIES NOTED ON PREFLIGHT. UPON LANDING, SHUTDOWN AIRCRAFT. AFTER EXITING AIRCRAFT, NOTICED TAIL ROTOR BLADE (C5-4834) HAD DEBONDED FROM SKIN. DEFECT IN MFG PROCESS. 1G71 3U3 U H2SW E4CE 20040524000612004052400061WP 2004 5 24 DHL2004803536 120040422A5730 SKIN DOUG DC8 DC873 302199CWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING OB L/E OUTER SECTION CORRODED, STA. XFS 710.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.9. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-2, DWG V43-R02. PERFORMED NDT INSP. IAW DC8 NDT SPM 6-10-01.001. FABRICATED FILLER AND DOUBLER IAW DWG V43-R02, ED EDV43-2. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS IAW ED EDV43-2, DWG V43-R02, SRM 51-1-21 PG. 1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2L74 4F RT4A25 20040524000622004052400062NE 2004 5 24 CX7A194J0426 220040520A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MALFUNCTIONED A CX7AE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL03307CE 340B204 TORQUE INDICATION FOR RT ENGINE DROPPED TO ZERO. PROP RPM INDICATION DROPPED FROM 1270-1000 DURING CRUISE. NO CHANGES WERE NOTICED TO ACTUAL TORQUE OR ACTUAL RPM. AT THE TIME TO BRING CONDITION LEVER MAX FOR LANDING THE RIGHT RPM DROPPED MASSIVELY CAUSING THE AIRCRAFT TO YAW. ELECTED TO SHUTDOWN THE RT ENGINE. 2L72 4T4 TRTA52EU E8NE 20040524000632004052400063WP 2004 5 24 IXXA0400058S 120040212A5730 PLATE DOUG DC8 DC873F 302199FWP RT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C CHECK INSPECTION FOUND RT INNER WING CTR. LE SLOT OUTER PLATING CORRODED. STA.XW257.000-XFS 310.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-21 PG. 1, 51-3-0 PG.1, 51-1-20D PG. 9, 51-1-8 PG.17-18, 57-2-1 PG. 11 AND DWG V22-R14. NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01-001. FABRICATED DOUBLER & 2 FILLERS IAW DC8 DRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG. 9. INSTALLED DOUBLER & FILLERS AND NEW FASTENERS IAW DWG V22-R14, DC8 SRM 51-1-21 PG 1, 51-3-0 PG. 1 51-1-20D PG. 9. 2L74 4F RT4A25 20040524000652004052400065WP 2004 5 24 IXXA0400060S 120040214A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING C CHECK INSP FOUND LT WING IB LE UPPER SKIN SURFACE CORRODED STA XFS 207.00-212.00. REPAIR WAS ACCOMPLISHED. DAMAGED SKIN ALONG WITH FASTENERS AND CORROSION WERE REMOVED AND FOUND OUT OF LIMITS IAW DC8 SRM. AN NDT INSPECTION WAS PERFORMED IAW DC8 NDT SPM PART 6-10-01.001, CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND TWO FILLERS IAW DWG V22-R17. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW DC8 SRM 51-1-8B. PRC SEALANT WAS APPLIED ON FAYING SURFACES IAW DC8 SRM 51-1-11PG 1. INSTALLED DOUBLER & FILLERS USING NEW FASTENERS IAW DWG V22-R17 AND DC8 SRM 51-1-21 PG 1, AND 51-3-0PG. 1. 2L74 4F RT4A25 20040524000672004052400067WP 2004 5 24 IXXA0400062S 120040214A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND RT FUSELAGE AFT LOWER CARGO COMPARTMENT FWD DOOR PLATING LOWER SIDE CRACKED AND WEAR DAMAGE BETWEEN STA 1160.00 TO 1220.00.REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R12. REMOVED DAMAGE SKIN SEGMENT AND EXTERNAL SPLICE DOUBLER IAW DWG V22-R12, DC8 SRM 51-1-21 PG 1, 51-1-20D PG 21. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01-0001. FABRICATED NEW SKIN SEGMENT + INTERNAL SPLICE DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN SEGMENT + SPLICE DOUBLER ( INTERNAL) + NEW FASTENERS IAW DWG V22-R12, DC9 SRM 51-1-21 PG 1, 51-1-20D PG 9. 2L74 4F RT4A25 20040524000692004052400069EU 2004 5 24 KBM2004F00091 120040219A6230126891P BALL JOINT SNIAS 350 AS350BA 8680817EU MAIN ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 MAIN ROTOR BLUE PITCH LINK UPPER ROD WORN. MAIN ROTOR RED PITCH LINK UPPER ROD WORN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000702004052400070EU 2004 5 24 KBM2004F00090 120040321A6230126891P ROD END SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 BLUE AND RED MAIN ROTOR PITCH CHARGE LINK UPPER END ROD BEARING STAKE HAS DAMAGE MARK. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040524000712004052400071WP 2004 5 24 IXXA0400063S 120040212A5730 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND LT OB WING LE OB SECTION SKIN CORRODED STA XW 761.000. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS AND CORROSION ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG 21, 51-1-21 PG.1, 51-3-0 PG.1, 51-1-8 PG 17-18, 57-2-1 PG. 11 AND DWG V22-R07. NDT INSPECTION WAS PERFORMED IAW NTD SPM PART 6-10-01-001. FABRICATED FILLER & DOUBLER IAW DWG V22-R07. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER & DOUBLER IAW DC8 SRM 51-1-8B. PRC SEALANT WAS APPLIED TO FAYING SURFACES IAW DC8 SRM 51-1-11. PG 9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS IAW DWG V22-R07, SC8 SRM 51-1-21 PG ., 51-1-20D PG 9 AND 51-3-0 PG.1 2L74 4F RT4A25 20040524000722004052400072 2004 5 24 DHL2004746004 420040506A3414 INDICATOR BOEING727 727224 1384076NM COCKPIT MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01746DH 22252 MACH AIRSPEED WARNING ACTIVATED AT 90 KTS DURING TAKE-OFF ROLL. T/O REJECTED AT 110 KTS, 145.200 TOW, TEMP +19 C, PA 100', RWY 36L, AND BRAKE ENERGY CAUTION ZONE. TRANSFERRED TO DMI NR 16523 IAW ASTAR MEL 34-4-3 MACH AIRSPEED WARNING SYSTEM DEACTIVATED FOR FLIGHT. REF. DMI NR 16523 (MACH AIRSPEED WARNING ACTUATED AT 90 KTS. DURING TAKE-OFF ROLL. T/O REJECTED AT 110 KTS, 145,000 TOW, TEMP +19 C, PA 100', RWY 36L, AND BRAKE ENERGY "CAUTION ZONE".) REMOVED AND REPLACED F/O'S MACH AIRSPEED INDICATOR, PERFORMED ADJUSTMENT/TEST (PITOT STATIC TEST) IAW B-M/M 34-14-0 PAGE 501. SYSTEM OPS NORMAL. NO LEAKS NOTED. THIS CLEARS DMI NR 16523. PLACARDS REMOVED. 2L73 4F A3WE 20040524000742004052400074SO 2004 5 24 C2XAO4SH279 120040511A531114524191002 FRAME EMB 145 EMB145 3260210SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 DURING C-CHECK FRAME 22 WAS FOUND TO BE CRACKED BETWEEN STRINGER 21 LT AND 21 RT. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EMB 145 SRM 53-00-04, PG. 205, FIG. 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040524000752004052400075EU 2004 5 24 KBM2004F00092 120040227A3150E659 WARNING HORN SNIAS 350 AS350BA 8680817EU COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 LOW RPM AURAL WARNING HORN IS NOT FUNCTIONING (SUSPECTED HOR FREQUENCY DETECTOR IS INOPERATIVE. 1G71 3U NCH9EU 20040524000762004052400076 2004 5 24 KBM2004F00096 420040327A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU VHF SYSTEM INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH322 2957 VHF RADIO BREAKS SQUELCH INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE RADIO. 1G71 3U NCH9EU 20040524000772004052400077 2004 5 24 KBM2004F00095 420040309A34215040017901 GYRO SNIAS 350 AS350BA 8680817EU ATTITUDE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 ATTITUDE INDICATOR TUMBLES IN FLIGHT. REMOVED AND REPLACED ATTITUDE GYRO. 1G71 3U NCH9EU 20040524000792004052400079EU 2004 5 24 KBM2004F00093 120040308A21210500211 MOTOR SNIAS 350 AS350BA 8680817EU BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH576 2957 FORWARD AC BLOWER DOES NOT BLOW HIGH AND NOT VERY GOOD. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000802004052400080EU 2004 5 24 KBM2004F00094 120040309A7931APTE176S150G TRANSMITTER SNIAS 350 AS350BA 8680817EU OIL PRESS INTERFERENCE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH3548 2957 OIL PRESSURE GAUGE INTERMITTENTLY READS ZERO. REMOVED AND REPLACED TRANSMITTER. 1G71 3U NCH9EU 20040524000812004052400081EU 2004 5 24 KBM2004F00098 120040211A7931704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817EU OIL PRESS READS HIGH E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 ENGINE OIL PRESSURE GAUGE READS HIGH. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000822004052400082SO 2004 5 24 LR7A04054 120040403A5311 FRAME LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE CANTED SKIN CRACKED AT RT FS 847 FRAME, RBL 72, WL 170. REPAIRED IAW LAC MEA 382-53-01-080 R1 & ED 01-058-1 REV A. NR 2004. 2H74 4T A1SO 20040524000832004052400083SO 2004 5 24 LR7A04055 120040403A5320LS5112 ANGLE LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND LH CHINE ANGLE CORRODED FS 247-252 AT LBL 62, WL 142. REPAIRED IAW LAC MEA 382-53-04-028. NR 2161. 2H74 4T A1SO 20040524000852004052400085NM 2004 5 24 249TR0028 120040503A335020131A BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 EMERGENCY EXIT LIGHT OVER L2 DOOR INOP. REPLACED BATTERY PACK PER MM 33-51-51. OPS NORMAL. 2L72 4F RTA16WE 20040524000872004052400087EU 2004 5 24 MALA040377 120040425A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15443XJ 340B443 DURING 4Y/2Y INSPECTION IN LCQ, RT IB SEAT TRACK WITH CORROSION AT STA 294-310. REMOVED AND REPLACED RT IB SEAT TRACK AT STA 296-326. IAW MESABA EO S53060. A/C RELEASE DATE 4/29/04. REFER TO LOG PG 770575 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040524000882004052400088EU 2004 5 24 MALA040379 120040426A760082180 CONDITION LEVER SAAB SF340 340B 7860101EU COCKPIT DAMAGED A MALAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL15436XJ 340B436 RT CONDITION LEVER WILL NOT CONTROL PROP INTO MIN MAX RANGE. PILOT REPORTED DIFFICULTY IN THE MIN/MAX RANGE. MAINTENANCE REMOVED AND REPLACED RT CONDITION AIRFRAME CABLE PN 82180 PERFORMED MASTER RIG TEST RAN ALL CHECKS GOOD. 2L72 4T RTA52EU 20040524000892004052400089EU 2004 5 24 MALA040380 120040502A2930152581 SWITCH BAC 146 AVRO146RJ85A1500097EU HYD PRESS BROKEN A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL15514XJ E2330 HYDRAULIC FUMES NOTED IN CABIN ON MX WALK AROUND. MAINTENANCE FOUND A BROKEN PRESSURE SWITCH LEAKING NEAR RECIRCULATION FAN. MX REMOVED & REPLACED GREEN HYD PRESS SWITCH PN 15258-1 SN ON 3777TW SN/OFF 3680 ALL CHECKS GOOD. ALL CHECK GOOD. 2H74 4F RTA49EU 20040524000922004052400092EU 2004 5 24 KBM2004F00103 120040420A21210500847 BLOWER SNIAS 350 AS350BA 8680817EU AIR CONDITIONER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 AMP METER IN THE RED WITH AC ON. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000932004052400093 2004 5 24 KBM2004F00104 420040414A34215040032902 INDICATOR SNIAS 350 AS350B1 8680811EU ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 359 2009 INDICATOR WILL NOT HOLD ATTITUDE. REMOVED AND REPLACED. 1G71 3U H9EU 20040524000942004052400094EU 2004 5 24 KBM2004F00100 120040311A7931 GAUGE SNIAS 350 AS350BA 8680817EU OIL PRESS ERRATIC E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 OIL PRESSURE GAUGE READS ERRATIC. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000952004052400095EU 2004 5 24 KBM2004F00101 120040320A21210500847 MOTOR SNIAS 350 AS350BA 8680817EU BLOWER NOISY E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 1024 2300 7 INCH BLOWER MOTOR, MAKING LOUD NOISE AND VIBRATION IN THE CABIN. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000962004052400096EU 2004 5 24 KBM2004F00102 120040418A2425704A47270101 GAUGE SNIAS 350 AS350BA 8680817EU COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 AMP METER DOES NOT MOVE TILL REACHES 65, THEN PEGS OUT TOO FAR RT SIDE THEN COMES BACK SLOWLY TO REGULAR VOLTAGE. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000972004052400097NM 2004 5 24 SWAA041255 120040430A2121215201 GASPER FAN BOEING737 7373H4 1384600NM E/E BAY OVERHEATED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29387SW 26602 ON DESCENT, ACRID ODOR REPORTED IN CABIN BY F/A'S. NO ODOR NOTED IN COCKPIT. ODOR DISSIPATED AFTER TURNING OFF GASPER FAN. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20040524000982004052400098NM 2004 5 24 SWAA041256 120040504A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29777QC 30592 CREW REPORTS EEPLS FWD RED LIGHT INOP. REPAIRED EEPLS LIGHT PER MM. 2L72 4F RTA16WE 20040524000992004052400099 2004 5 24 SWAA041257 420040504A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040524001002004052400100NM 2004 5 24 SWAA041258 120040504A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FWD BULLNOSE EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040524001012004052400101NM 2004 5 24 SWAA041259 120040504A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND KEELBEAM AT RT BS 500C + 18, AND LT BS 500C + 18, INBOARD FLANGE, CORRODED. REPAIRED KEEL BEAM LT AND RT CHORD PER MM. 2L72 4F RTA16WE 20040524001022004052400102NM 2004 5 24 SWAA041260 120040504A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB AT BS 1016, STRINGER 6R, CRACKED. REPAIRED BULKHEAD PER ER. 2L72 4F RTA16WE 20040524001032004052400103NM 2004 5 24 SWAA041261 120040504A5551 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND LT AND RT, FWD AND REAR SPAR, HORIZONTAL STAB CENTER SECTION LUG FACES CORRODED. REPAIRED STAB PER SRM. 2L72 4F RTA16WE 20040524001042004052400104NM 2004 5 24 SWAA041262 120040504A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES AT BS 188, STRINGER 17R AND STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040524001052004052400105NM 2004 5 24 SWAA041263 120040504A53206517591 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 188 TO BS 198, STRINGER 17R, AND BS 188 TO BS 196, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2L72 4F RTA16WE 20040524001062004052400106NM 2004 5 24 SWAA041264 120040504A533065457600 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 5L, AND BS 482, STRINGER 16L, CRACKED. REPAIRED FUSELAGE SKIN PER SRM. 2L72 4F RTA16WE 20040524001072004052400107NM 2004 5 24 SWAA041265 120040504A3350612825 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29402WN 29814 DURING SPV, FOUND SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOP. DEEP CYCLED AIRCRAFT EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040524001082004052400108NM 2004 5 24 SWAA041266 120040505A2560PH22300L GLOWSTRIP BOEING737 7373G7 1384595NM ROW 7 DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 PHOTOLUMINESCENT STRIP AT ROW 7 ABC, DELAMINATED. REMOVED AND REPLACED FLOOR STRIP PER MM. 2L72 4F RTA16WE 20040524001092004052400109NM 2004 5 24 SWAA041267 120040505A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 311, BETWEEN STRINGER 19R AND STRINGER 20R, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040524001102004052400110NM 2004 5 24 SWAA041268 120040505A53406535357 FITTING BOEING737 7373H4 1384600NM KEELBEAM CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND BULKHEAD TEE FITTING AT BS 727, LBL 6, CRACKED. REMOVED AND REPLACED T-FITTING PER SRM. 2L72 4F RTA16WE 20040524001122004052400112NM 2004 5 24 SWAA041308 120040508A53306545765 SKIN BOEING737 7377H4 1384404NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN AT BS 500 + 8, FWD AIRPHONE ANTENNA, CRACKED. REPAIRED FUSELAGE SKIN PER SRM. 2L72 4F RTA16WE 20040524001132004052400113NM 2004 5 24 SWAA041309 120040508A3350D71702030 BATTERY BOEING737 7377Q8 1384418NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29799SW 28209 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHTS AT LT OVERWING EXIT AND OVERHEAD CEILING, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040524001142004052400114 2004 5 24 SWAA041280 420040506A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001152004052400115 2004 5 24 SWAA041281 420040504A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED RON, L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, SLIDE DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001162004052400116NM 2004 5 24 SWAA041282 120040506A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED RON, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040524001172004052400117NM 2004 5 24 SWAA041270 120040505A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER 26R, BETWEEN BS 814 AND BS 821, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040524001182004052400118NM 2004 5 24 SWAA041271 120040505A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 787, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040524001192004052400119NM 2004 5 24 SWAA041272 120040505A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 380, RBL 56, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040524001202004052400120NM 2004 5 24 SWAA041273 120040505A53116545812 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 328, BETWEEN STRINGER 20R AND STRINGER 21R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040524001212004052400121NM 2004 5 24 SWAA041274 120040505A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 827, LBL 8, WL 149, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040524001222004052400122NM 2004 5 24 SWAA041275 120040505A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 951, LOWER RT LAP SEAM, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040524001232004052400123NM 2004 5 24 SWAA041276 120040505A5330907822 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR CUTOUT, LOWER HINGE, CRACKED. REPAIRED L1 DOOR CUTOUT PER SRM. 2L72 4F RTA16WE 20040524001242004052400124 2004 5 24 SWAA041277 420040505A256565C19901 CABLE BOEING737 7375H4 138449DNM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE DOOR CABLE PER MM. 2L72 4F RTA16WE 20040524001252004052400125 2004 5 24 SWAA041278 420040505A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29756SA 27872 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001262004052400126NM 2004 5 24 SWAA041279 120040505A53206547690 SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND NR 3 VHF ANTENNA SUPPORT STRUCTURE AT BS 727D TO BS 727E, BL 0, CORRODED. REMOVED AND REPLACED ZEE SUPPORT SECTION PER SRM. 2L72 4F RTA16WE 20040524001272004052400127NM 2004 5 24 SWAA041283 120040506A53206545833 WEB BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SPV, FOUND FLOOR STRUCTURE WEB AT BS 180, RBL 24, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040520002172004052000217NM 2004 5 20 GTIA040325 120040408A5321 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 FOUND CENTER AILSE FLOOR PANEL APPEARS TO BE SPONGY BETWEEN SEAT ROW 16 AND 17. REINFORCED FLOOR PANEL. (M) 2L72 4F RT 20040520002332004052000233EA 2004 5 20 ASOA04250 120040329A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20040520002362004052000236EA 2004 5 20 ASOA04249 120040329A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11877AS 7579 FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040520002392004052000239EA 2004 5 20 ASOA04270 120040405A5320601R950159 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY RAM AIR INLET SPIDER DUCT BRACKET. (M) 2L72 4F RTA21EA 20040520002412004052000241EA 2004 5 20 ASOA04268 120040405A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040520002822004052000282SO 2004 5 20 RAIA00404015 120040424A3610S2U2230 O-RING EMB 145 EMB145LR 3260212SO BLEED AIR LEAKING A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03814HK 145046 RT BLEED LEAK MESSAGE. MAINTENANCE REMOVED AND REPLACED O-RINGS IN THE NR 2 ENGINE BLEED LINE IN CARGO COMPARTMENT. 2L72 4T RTT00011AT 20040520002842004052000284NM 2004 5 20 250TR0032 120040422A3350 BATTERY BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE C F.O.D. ININSP/MAINT 1 SO05250TR 22597 FWD CABIN AFT SECTION OF EMERGENCY LIGHTS INOP. REPLACED BATTERY. SYSTEM CHECKS NORMAL. 2L72 4F RTA16WE 20040520002862004052000286NM 2004 5 20 0400615532 120040428A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01532US 24263 DURING "H" CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 25. REPAIRED PER EA 55-198777. 2L72 4F RTA2NM 20040521000102004052100010SO 2004 5 21 RAIA00404018 120040429A32608005707 SQUAT SWITCH EMB 145 EMB145ER 3260211SO MLG DEFECTIVE A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03826HK 145016 LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MLG WOW SWITCH. 2L72 4F RTT00011AT 20040521000112004052100011WP 2004 5 21 ABXA040155 120040427A32600080004003 CONTROL BOX DOUG DC8 DC863 302198AWP MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23825AX 648 46115 AFTER TAKEOFF, GEAR WARNING LIGHT REMAINED ON. LANDING GEAR AND DOOR INDICATOR PANEL SHOWED NOSE GEAR. RECYCLED, SAME RESULT. CONSULTED ABNORMAL AND PROCEEDED TO DESTINATION. MAINTENANCE AT ILN: DURING SELF TEST OF PROX SWITCH CONTROL BOX, NOSE GEAR UP LIMIT FAILED IN B POSITION. REPLACED PROX CONTROL BOX IAW DC8 MM 32-60-00. NOSE GEAR UP LIMIT TESTED GOOD IN POSITION A AND B. NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR UP. INSTALLED NOSE LANDING GEAR UP LIMIT PROX SWITCH AND ADJUSTED IAW DC-8 MM. COMPLIED WITH POSITION WARNING SYSTEM TEST IAW DC8 MM 32-60-00-2. 2L74 4F 4A25 20040521000152004052100015NM 2004 5 21 0400636313 120040501A3350 POWER SUPPLY BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01673US 30268 DURING LINE CHECK, FOUND ZONE 'A' AND 'B' RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040521000282004052100028WP 2004 5 21 IXXA0400043S 120040216A5320 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK FOUND A-CARGO DOOR FITTING CORRODED AT STA 300.00 L34R TO L33R. REPAIR ACCOMPLISHED. REMOVED CORROSION ON CARGO DOOR FITTING STATION 300.00 IAW 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG.2M, REMOVED FITTING, FABRICATED NEW FITTING IAW REPAIR SPECIFICATION NR 2003-05 DWG ED-3622. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02-07. FABRICATED DOUBLER IAW SRM 53-2-0 PG 17-18 FIG. 2D CLEANED, TREATED AND PRIMED DOUBLER AND FITTING IAW SRM 51-1-8B. INSTALLED FITTING AND DOUBLER IAW SRM 51-1-20DPG.9 SRM 53-2-0 PG 17-18 FIG 2D. 2L74 4F RT4A25 20040521000302004052100030WP 2004 5 21 IXXA0400045S 120040304A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND FWD FUSELAGE EXTERNAL SKIN HAS IMPROPER REPAIR IAW DWG V22-R19. REPAIR ACCOMPLISHED. TEMPORARY REPAIR WAS REMOVED. FABRICATION AND INSTALLATION OF FINGER DOUBLER FILLER AND DOUBLER IAW STRUCTURAL REPAIR MANUAL. CLEANED, TREATED AND PRIMED. PRC SEALANT WAS APPLIED TO FAYING SURFACES. NEW FASTNERS FOR FINGER DOUBLER, FILLER, AD DOULBER WERE ISNTALLED IAW DWG V22-R19, SRM 51-1-21 PG 1, SRM 51-1-20DPG 9. 2L74 4F RT4A25 20040521000312004052100031WP 2004 5 21 IXXA0400046S 120040225A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK INSPECTION FOUND RT HORIZONTAL STAB L/E SURFACE SHOWS CORROSION AND A 1 INCH CRACK. REPAIR ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW DWG V22-R18. REMOVED FASTENERS , REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE DAMAGED AREA IAW DWG V22-R18, PERFORMED NDT INSECTION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER AND TWO FILLERS. CLEANED TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLERS IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED THE REPAIR DOUBLER AND FILLERS WITH THE NEW FASTENERS IAW DWG V22-R18 AND DC8 SRM 51-1-20D,51-1-21 AND 51-3-0 PG 1. 2L74 4F RT4A25 20040521000322004052100032NE 2004 5 21 KBM2004F00070 220040124A74219550175400 IGNITER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE RT ENGINE DEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 RT ENGINE IGNITER TIP IS DEFECTIVE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040521000392004052100039EU 2004 5 21 KBM2004F00073 120040423A2110507 COMPRESSOR SNIAS 350 AS350BA 8680817EU AIR CONDITIONER SEIZED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH801 2957 A/C BELT MELTED ON COMPRESSOR. COMPRESSOR FOUND SEIZED. REMOVED AND REPLACED COMPRESSOR. 1G71 3U NCH9EU 20040521000422004052100042EU 2004 5 21 KBM2004F00072 120040124A24359566015450 MAGNETIC SEAL SNIAS 350 AS350BA 8680817EU STARTER GEN LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 STARTER GEN FLANGE TO ENGINE ACCESSORY GEAR BOX MAGNETIC SEAL IS LEAKING OIL. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040521000472004052100047EU 2004 5 21 00136 120040429A28222060B PUMP AMD FALCONFALCON20 2730103EU GE CF700 CF7002D2 30010NE FUEL BOOST FAILED E HAEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW05699TW 050 PILOT REPORTED RT BOOST PUMP FAILURE AND TROUBLE KEEPING FUEL BALANCED AIRCRAFT IN MAINTENANCE AT THIS TIME WILL UPDATE THIS SDR WHEN FURTHER INFORMATION IS AVA.MAINTENANCE REPLACED RT BOOST PUMP AND PERFORMED OPERATIONAL CHECKS GOOD AT THIS TIME AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA7EU E7EA 20040521000692004052100069EA 2004 5 21 MASA200400235 120040430A361032895902 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA ENGINE INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07759831598 5983 THE CREW ABORTED T/O DUE TO AN WING OVERHEAT MESSAGE. MX IN THE PROCESS OF TROUBLESHOOTING. MX REPLACED 14TH STAGE SOV OPS CHECKED GOOD 2L72 4F RTA21EA 20040521000752004052100075EA 2004 5 21 MASA200400209 120040419A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0797325 7325 A/C ABORTED T/O DUE TO SPOILER CAUTION MSG. MX WAS CALLED OUT AND DEPOWERED AND REPOWERED A/C SO THEY CAN RESEAT THE SSCU. OP CHECKS NORMAL. NO PARTS USED 2L72 4F RTA21EA 20040521000772004052100077EA 2004 5 21 MASA200400043 120040125A5753 FLAP CNDAIRCL600 CL6002B19 1900309EA TE FLAPS CONTAMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0747239 7239 AFTER DEPARTURE THE CREW RECIEVED A FLAP FAIL MSG. A/C RETURNED TO THE FIELD AND MX WAS CALLED. MX REMOVED ICE FROM THE FLAPS. OP CHECKS GOOD. NO PARTS USED 2L72 4F RTA21EA 20040521000812004052100081EA 2004 5 21 MASA200400051 120040127A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF ADJUST A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0717175 7175 AIRCRAFT RETURNED TO FIELD FOR A RIGHT THRUST REVERSER UNLOCK MESSAGE IN-FLIGHT. MX PLACED T/R ON MEL. 1/31/2004. MX RERIGGED THE SWITCH. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040521000882004052100088EA 2004 5 21 MASA200400107 120040224A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07591ML5766 7388 FS 621, RBL 40, WL 73 UNDER FLOOR SUPPORT ANGLE FROM RBL 32 TO RBL 44. FABRICATED REPAIR ANGLES IAW BOMB REO 601R-53-61-117 REV B 2L72 4F RTA21EA 20040521000952004052100095 2004 5 21 DXTA200400281 420040328A3140 WARNING LIGHT CESSNA750 750 2076810CE COCKPIT ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07983QS 7500083 DURING TAKE-OFF ROLL BELOW 80 KTS, NO TAKE-OFF CAS MESSAGE ILLUMINATED, MACH TRIM OFF, PRIMARY STAB TRIM FAILED, YAW DAMPER FAIL LOWER, YAW DAMPER NOT CENTERED, FGC A FAIL CAS MESSAGES ILLUMINATED. NOSE WHEEL SHIMMY VERY STRONG ALSO, ABORTED TAKE-OFF. PERFORMED HONEYWELL DOWNLOAD FOR ICAS MESSAGES AND PERFORMED NO-TAKEOFF FUNCTIONAL TEST, OPS CHECK GOOD IAW CESSNA 750 MM CHAPTER 31-52-00. REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLY DUE TO TIRES BEING FLAT SPOTTED, OPS CHECKED GOOD IAW CESSNA 750 MM CHAPTER 32-41-01. 2L72 4J RTT00007WI 20040521001002004052100100EA 2004 5 21 MASA200400129 120040306A7930 LINE CNDAIRCL600 CL6002B19 1900309EA LT ENG OIL LOOSE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0777278 7278 CREW AIR DIVERTED DUE TO LT ENGINE OIL PRESSURE MSG. MX WAS CALLED. MX TIGHTENED SERVICE LINE. NO PARTS USED. 2L72 4F RTA21EA 20040521001022004052100102EA 2004 5 21 MASA200400133 120040310A2730 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA ELEVATORS FALSE INDICATIONA MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07914FJ 15014 AIRCRAFT RETURNED TO FIELD W/AN ELEVATOR SPLIT CAUTION MSG. MX SHUT DOWN THE A/C AND REPOWERED AND THE MSG CLEARED. MX PERFORMED THE ELEVATOR OPS CHECK AND DIDA VISUAL INSP OF THE ELEVATOR AND FOUND NO DEFECTS. NO PARTS USED 2L72 4F RTA21EA 20040521001042004052100104EA 2004 5 21 MASA200400138 120040312A4990 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY LEAKING A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0787353 7353 THE CREW RETURNED TO THE FIELD BECAUSE THEY SMELLED SMOKE COMING FROM THE PACKS DUE TO THE APU OIL SPRAYED IN THE APU COMPARTMENT AND THE PACKS. MX RAN ENGINES AND PACKS AT A HIGH TEMP TO DISIPATE THE OIL. OP CHECKS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040521001052004052100105EA 2004 5 21 MASA200400143 120040315A5210 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE INDICATIONA MASAK NONE N FALSE WARNING ININSP/MAINT 1 SW0737208 7208 MAIN CABIN DOOR W/N OPEN. MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USED 2L72 4F RTA21EA 20040521001172004052100117EU 2004 5 21 KBM2004F00084 120040416A2170050085 BLOWER SNIAS 350 AS350B2 8680813EU EVAPORATOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 AC BACK BLOWER INOPERATIVE. REMOVED AND REPLACED BLOWER. 1G71 3U H9EU 20040521001392004052100139WP 2004 5 21 ABXA040158 120040415A5534591214129 ATTACH ANGLE DOUG DC9 DC933F 302207AWP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 LEFT VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC-9 SRM. 2L72 4F A6WE 20040521001422004052100142NE 2004 5 21 HNAA0400041 220040423A7321324485318 FUEL CONTROL DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 1 ENGINE INOPERATIVE A HNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA07335EN4584 4584 375 123128 LOSS OF POWER ON NR 1 ENG IN CLIMB. ENG DID REMAIN RUNNING. A/C RETURNED TO FIELD & DECLARED EMERGENCY, DID NOT SHUTDOWN ENG UNTIL ON FIELD. A/C CLIMB THROUGH 7000 FT. ENG PARAM: TQ 0, WF 230, NH 71, NL 59, ITT 447, OIL PRESS GOOD, PROP RPM STABL & CONTROLLABLE W/ COND LEVER. ECU SELECTED TO MAN & BACK, NO EFFECT. MX LOOKING FOR DEFECTS & WILL RUN IF NONE FOUND. SELECTED BOOST PUMP ON, NO EFFECT. AFTER INSPECT, MX TRIED ENG START. RUNS, BUT UNRESPONSIVE TO POWER LEVER INPUTS WITH ECU ON OR OFF. R & R MFC. TRIM RUN COMPLETE. DUPLICATED ON GROUND RUN R & R NR 1 MFC. PERFORMED RIG CHECK PER WC 76-00-02Q AND TRIMMED PER -8 OPERATING MANUAL LEAK AND OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20040521001532004052100153NM 2004 5 21 P5CA0401085 120040430A3242 ACCUMULATOR BOEING747 747243B 1384830NM BRAKE SYSTEM LEAKING A P5CAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23516MC 22507 AFTER ENG START, NR 1 AND 4 LOST HYD SYSTEM QTY. REPLACED BRAKE ACCUMULATOR AS PER MM 32-41-23. OPS AND LEAK CK NORMAL. RESTARTED NR 1 AND 4, HYD SYSTEM TO PROPER LEVEL. 2L74 4F A20WE 20040521001562004052100156CE 2004 5 21 60159 120040330A2750 FLAP BEECH 1900 1900D 1154162CE WINGS MALFUNCTIONED A AMWAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE0715YV UE15 AFTER TAKING OFF IN MIA CREW COULDN'T GET FLAPS TO COME UP SO CALL DISPATCH AND WE TOLD THEM TO RETURN TO GATE THEY LANDED SAFELY WHEN THEY GOT TO GATE THEY TRY FLAPS AGAIN AND THEY CAME UP MAINT. THEN DEFERED THEM WITH NO FURTHER INCIDENT 2L72 4T RTA24CE 20040521001692004052100169CE 2004 5 21 60212 120040401A5210 DOOR BEECH 1900 1900D 1154162CE MAIN PAX STUCK A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07163YV UE163 UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THRU THE EMERGENCY EXIT AT 6A. REMOVED & REINSTALLED EMERGENCY EX/DOOR 2L72 4T RTA24CE 20040521001922004052100192SO 2004 5 21 LR7A04043 120040403A5320LS5112 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND RT FS 746E CHINE ANGLE CORRODED AT RBL 62 WL 142. REPLACED CHINE ANGLE FS 737E - 817E IAW SRM SMP 583 51-60 AND 51-70. NR 2162. 2H74 4T A1SO 20040521002012004052100201SO 2004 5 21 LR7A04052 120040403A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED OMEGA ANTENNEA DOUBLER AT FS 862, LBL 45, WL 285. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-10. NR 2200. 2H74 4T A1SO 20040524000012004052400001WP 2004 5 24 IXXA0400048S 120040212A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK FUSELAGE EXTERIOR SKIN WITH 1INCH CRACK AND CORROSION IN IT, STA 1080.000 L-34R. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS ALONG WITH THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. REMOVED THE DAMAGED SECTION IAW DWG V22-R09, PERFORMED NDT INSP INAW DC8 NDT SRM PART 6-10-01-001. FABRICATED FILLER AND DOUBLER IAW DWG V22-R09 CLEANED TREATED AND PRIMED AREA. FILLER DOUBLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED FILLER, DOUBLER & NEW FASTENERS IAW SRM 51-1-20D, SRM 51-1-21 PG 7. 2L74 4F RT4A25 20040524000042004052400004WP 2004 5 24 IXXA0400054S 120040328A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION LT OB WING L/E IB SECTION LWR SKIN SURFACE CORRODED, STA XFS. 710.000. REPAIRS WERE ACCOMPLISHED IAW APPROVAL DOCUMENT, REMOVED FASTENERS, REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 REMOVED DAMAGED AREA, PERFORMED NDT INSPECTION IAW NOT SPM PART 6-10-01-001, CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND REPAIR DOUBLER AND TWO FILLERS IAW DWG V22-RO4, CLEANED TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FAYING SURFACES IAW SRM 51-1-11 PAGE 4, INSTALLED DOUBLER + FILLERS USING NEW FASTENERS IAW DWG V22-R04, SRM 51-1-21 PAGE 1, 51-1-20D PAGE 9 AND 51-3-0 PAGE. 1. 2L74 4F RT4A25 20040524000192004052400019EU 2004 5 24 MALA040391 120040429A3350 FUSE SAAB SF340 340B 7860101EU EMERGENCY LIGHT BLOWN A MALAK NONE L NO TEST ININSP/MAINT 1 GL15448XJ 340B448 A/C WOULD NOT SUPPLY POWER AFTER REPLACING LT EXIT EMERGENCY LIGHTS EXIT LIGHT ASSEMBLY. MAINTENANCE REPLACED TWO BLOWN FUSES, PASSED AMM CHECKS AND WAS RETURNED TO SERVICE 5/1/04. REFER TO WO NR 367101 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040524000212004052400021EU 2004 5 24 MALA040396 120040430A5315 FLOORBEAM SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 DURING 4K INSPECTION IN LCQ, FS 363.0 FLOORBEAM CRACKED. CUT OUT DAMAGED AREA OF FLOORBEAM, FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR IAW EO NR S53108. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2L72 4T RTA52EU 20040524000282004052400028EU 2004 5 24 MALA040394 120040430A33506104789 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15369PX 340B295 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK 61-0478-9 SN/ELB026 FAILED 4/30/04. MECHANIC RECHARGED AND UNIT PASSED CMM TESTS ON 5/6/04. REFER TO IN HOUSE WO NR 367019 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040524000352004052400035WP 2004 5 24 IXXA0400052S 120040212A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED , STA. XW 485.000. REPAIR WAS ACCOMPLISHED. CORROSION, FASTENERS AND THE DAMAGED AREA WAS REMOVED IAW DC8 SRM 51-1-21 PG1, 51-1-20D PG21,51-3-0 PG.1, 51-1-8 PG 17-18, 57-2-1 PG.11, AND DWG. V22-R02. NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01.001. AREA WAS CLEANED, TREATED AND PRIMED. FABRICATED A REPAIR DOUBLER AND FILLER IAW DWG V22-R02. THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER WAS CLEANED, TREATED AND PRIMED IAW APPLICABLE MANUALS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER AND FILLER USING NEW FASTENERS IAW DWG V22-R02 AND SRM 51-1-21 PG 1 51-1-20DPG 9 AND 51-3-0 PG 1. 2L74 4F RT4A25 20040524000372004052400037WP 2004 5 24 IXXA0400057S 120040212A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C CHECK RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA IAW SRM 51-1-20D PG 21., 51-3-0 PG. 7, 51-1-21 PG 1. AN NDT INSPECTION WAS PERFORMED IAW NDT SPM PART 6-10-01-011. FABRICATED FILLER & DOUBLER IAW DWG. V22-R15 CLEANED, TREATED AND PRIMED AREA, INNER FACE OF FILLER & DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT ( PRC) TO FAYING SURFACES IAW DC8 SRM. 51-1-11 PG. 9 INSTALLED FILLER & DOUBLER AND NEW FASTENERS IAW DWG. V22-R15. SRM 51-1-21 PG.1, 51-2-20D PG. 9, 51-3-03 PG.1 2L74 4F RT4A25 20040524000382004052400038NM 2004 5 24 ASMF200405021 120040518A282040885 VALVE BOEING757 7572Q8 1384972NM LT FUEL SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23801AM576 25624 DURING REFUELING A FUEL LEAK WAS DETECTED IN LT MAIN GEAR DOOR. LT CENTRAL TANK VALVE WAS DETECTED WITH LEAK AND FUEL VALVE WAS REPLACED IAW MM 28-10-00, TEST CORRECT. 2L72 4F RTA2NM 20040524000502004052400050WP 2004 5 24 UPS04842393 120040505A541057567901 FITTING DOUG DC8 DC871F 302199DWP NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, NR 1 PYLON UPPER AFT END HAS PN 57567901 CRACKED AT YN 384.942. REMOVED CRACK FROM FITTING BY REMOVING INTEGRAL STIFFNER IAW UPS. ENGINEERING FILE NR DC8-54-20038 AND SAA SK 730-344. 2L74 4F RT4A25 20040524000582004052400058GL 2004 5 24 ALG2004F00021 220040428A73136899001 FUEL NOZZLE BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ENIGNE INOPERATIVE E ALGAO OTHER RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SW03414LV13540 52006 ON START UP, UNABLE TO START ENGINE, THE ENGINE FLAMED OUT DURING THE START SEQUENCE. ATTEMPTED THREE STARTS WITH NO SUCCESS. CONTACTED BASE MANAGER AND MAINTENANCE FOR HELP. MAINTENANCE REMOVED AND REPLACED FUEL NOZZLE AND SHIMMED AS REQUIRED, REMOVED AND REPLACED BATTERY AND ADJUSTED FUEL CONTROL START/ACCELERATION. THE AIRCRAFT OPS CHECKED GOOD. 1G71 3U3 UNCH2SW E1GL 20040524000602004052400060WP 2004 5 24 UPS04842398 120040506A5310577384419 SHEAR TIE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, AFT OF STATION 1766 J-FRAME TO LONG. 13L SHEAR TIE IS CRACKED REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG.5773844 AND SRM. 51-1-20D. 2L74 4F RT4A25 20040524000732004052400073 2004 5 24 COMA0460324 420040516A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAILED A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01783CA 7315 FLIGHT 5364 STALL FAIL CAUTION MESSAGE. RESET THE STALL COMPUTER, NO DEFECTS FOUND. 2L72 4F RTA21EA 20040524001422004052400142NM 2004 5 24 SWAA041310 120040509A53116547951 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AT LOWER STOP FITTING, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040524001432004052400143NM 2004 5 24 SWAA041311 120040509A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 14R, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040524001442004052400144NM 2004 5 24 SWAA041312 120040509A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 965, STRINGER 6R, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040524001452004052400145NM 2004 5 24 SWAA041313 120040510A5343BAC1517 ANGLE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT MLG VERTICAL ANGLE AT BS 695, STRINGER 18R, CRACKED. REMOVED AND REPLACED MLG ANGLE PER SRM. 2L72 4F RTA16WE 20040524001462004052400146NM 2004 5 24 SWAA041314 120040509A575465C26603 SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND NR 2 L/E SLAT, OUTBOARD END DELAMINATED. REPAIRED NR 2 SLAT PER SRM. 2L72 4F RTA16WE 20040524001472004052400147NM 2004 5 24 SWAA041315 120040509A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 188, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040524001482004052400148NM 2004 5 24 SWAA041316 120040509A5511 SPAR BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION FWD SPAR LT AND RT CLEVIS FWD AND AFT LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20040524001492004052400149NM 2004 5 24 SWAA041317 120040509A5312963820 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SPV, FOUND RT BULKHEAD FRAME AT BS 178, WL 207, CRACKED. REMOVED AND REPLACED RT FRAME PER ACO. 2L72 4F RTA16WE 20040524001502004052400150NM 2004 5 24 SWAA041318 120040509A534365C10300 FITTING BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED A2 CHECK, FOUND NLG ACTUATOR ATTACH FITTING GUSSET, CRACKED. REMOVED AND REPLACED NLG FITTING PER SRM. 2L72 4F RTA16WE 20040524001512004052400151NM 2004 5 24 SWAA041319 120040508A575465C26603 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND RT NR 4 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20040524001522004052400152 2004 5 24 SWAA041320 420040510A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001532004052400153NM 2004 5 24 SWAA041298 120040507A57536546486 WEDGE BOEING737 737317 138447PNM RT WING FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD MID FLAP WEDGE, CRACKED. REPAIRED RT WING MID FLAP WEDGE PER SRM. 2L72 4F RTA16WE 20040524001542004052400154NM 2004 5 24 SWAA041299 120040507A575365C30462 SKIN BOEING737 7377H4 1384404NM RT WING FOREFLAPCRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD FOREFLAP L/E, CRACKED. REPAIRED L/E FOREFLAP PER EA. 2L72 4F RTA16WE 20040524001552004052400155NM 2004 5 24 SWAA041300 120040507A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29707SA 27841 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT FWD GALLEY, ROW 11 DEF, AND ROW 16 ABC. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040524001562004052400156 2004 5 24 SWAA041301 420040508A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001572004052400157NM 2004 5 24 SWAA041302 120040508A33506114789 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29085SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND AFT FUSELAGE EXTERIOR EMERGENCY EXIT LIGHTS AT L2 AND R2 DOORS, INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY EXIT LIGHTS BATTERY PER MM. 2L72 4F A16WE 20040524001582004052400158 2004 5 24 SWAA041303 420040508A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001592004052400159NM 2004 5 24 SWAA041321 120040510A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040524001612004052400161NM 2004 5 24 SWAA041323 120040510A53116520723 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT LOWER STOP FITTING, BS 492, BETWEEN STRINGER 24R AND STRINGER 25R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040524001632004052400163NM 2004 5 24 SWAA041325 120040510A53126546568 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, RBL 2 TO LBL 2, CORRODED. REPAIRED PRESSURE WEB PER ER. 2L72 4F RTA16WE 20040524001652004052400165NM 2004 5 24 SWAA041327 120040510A3350604222 BATTERY BOEING737 737301 1384611NM R2 DOOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29659SW 23229 DURING SPV, FOUND R2 DOOR EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040524001672004052400167NM 2004 5 24 SWAA041304 120040508A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR FRAME UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED DOOR FRAME CUTOUT LOWER RADIUS PER EA. 2L72 4F RTA16WE 20040524001692004052400169NM 2004 5 24 SWAA041306 120040508A53126516300 STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SPV, FOUND BULKHEAD STRAP AT BS 178, RBL 6 TO RBL 25, CRACKED. REMOVED AND REPLACED STRAP PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040524001712004052400171EU 2004 5 24 KBM2004F00106 120040113A6420350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 TAIL ROTOR PITCH LINK, CRACKED BUSHING. REMOVED AND REPLACED. 1G71 3U H9EU 20040524001722004052400172EU 2004 5 24 KBM2004F00109 120040314A2197540028C2A ELECTRICAL BOX SNIAS 350 AS350B2 8680813EU AIR CONDITIONER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 642 3403 AIR CONDITIONER BLOWS WARM. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H9EU 20040524001732004052400173 2004 5 24 KBM2004F00107 420040309A2312064105430 TRANSCEIVER KY196A SNIAS 350 AS350B2 8680813EU COMMS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 REMOVED COMM, KY 196A, SN:8965 FOR TROUBLESHOOTING. REMOVED AND REPLACED. 1G71 3U H9EU 20040524001742004052400174EU 2004 5 24 KBM2004F00110 120040130A77129550176240 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TORQUE UNRELIABLE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 TORQUE GAUGE SHOWING UNRELIABLE READINGS DURING THE FLIGHT. ON GROUND IT ROTATES CLOCKWISE. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040524001762004052400176EU 2004 5 24 KBM2004F00111 120040205A772256375600010 INDICATOR SNIAS 350 AS350B2 8680813EU COCKPIT MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 INCORRECT READING DURING FLIGHT. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H9EU 20040524001792004052400179EU 2004 5 24 MALA040378 120040425A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15443XJ 340B443 DURING 4Y/2Y INSPECTION IN LCQ, LT IB SEAT TRACK WITH CORROSION AT STA 294-310. REMOVED AND REPLACED LT IB SEAT TRACK AT STA 294-310. IAW MESABA EO S53060. A/C RELEASE DATE 4/29/04. REFER TO LOG PG 770575 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040524001822004052400182WP 2004 5 24 0400679954 120040429A1430 SCREW DOUG DC9 DC931 3022065WP HYD PUMP SHEARED A NWAAO OTHER K FLUID LOSS DEDESCENT 1 GL01921RW 06305 47164 DUIRING DESCENT FOR LANDING, THE CREW NOTICED THE LOSS OF ALL OF THE LEFT HYDRAULIC SYSTEM FLUID. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HOUSING SCREWS SHEARED ON THE ALTERNATE GEAR PUMP AND REPLACED THE PUMP. ALSO, FOUND THAT THE LEFT INBOARD UPPER ACCUMULATOR WOULD NOT HOLD PRESSURE AND REPLACED IT AS WELL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040524001832004052400183EU 2004 5 24 04097637 120040502A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGNECY LIGHT WORN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27309UE 41022 DURING INSPECTION THE AFT SECTION OF FLOOR EMERGENCY LIGHTING WAS FOUND INOPERATIVE. THE CONNECTOR WAS FOUND WORN AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040524001842004052400184NM 2004 5 24 DHL2004740006 120040506A5755 SKIN BOEING727 7272Q9 138448MNM NR 6 SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 LOWER SURFACE OF NR 6 SPOILER PREVIOUS REPAIR CRACKED. REPLACED NR 6 SPOILER PANEL OPS CHECKED NORMAL IAW B727 M/M 27-60-0. 2L73 4F RTA3WE 20040524001862004052400186EA 2004 5 24 04118668 120040427A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27668BR 7544 DURING INSPECTION THE LEFT HAND EXTERIOR FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS REUTNRED TO SERVICE 2L72 4F RTA21EA 20040524001882004052400188EA 2004 5 24 04117656 120040426A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27656BR 7485 DURING INSPECTION THE CEILING EMERGENCY LIGHT A ROW 8 WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040524001902004052400190EU 2004 5 24 04126307 120040505A3397PT2112 WIRE JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT WORN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27307UE 41021 DURING INSPECTION THE FOWARD SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE. THE PIGTAIL WAS FOUND WORN AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE, 2L72 4T RTA41NM 20040524001912004052400191NM 2004 5 24 QXEA200400303 120040506A3620 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 ILLUMINATED A QXEAO OTHER N FALSE WARNING DEDESCENT 1 NM09407QX 4049 SEA FLIGHT 2391 ON SHORT FINAL, GOT NR 2 BLEED HOT CAUTION LIGHT, SHUT BLEED OFF PER CHECKLIST. LIGHT WENT OUT, DID NOT REOCCUR. MAINTENANCE INTERROGATED CDS, NO FAULTS RECORDED. GROUND RAN NR 2 ENGINE FOR 30 MINUTES WITH BLEED ON AND PACKS ON AT VARIOUS POWER SETTINGS. NO CAUTION LIGHT. NO FAULT FOUND. AIRCRAFT OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20040524001932004052400193NM 2004 5 24 04125426 120040504A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27426FJ 3190 DURING INSPECTION THE FOWARD DOME EMERGENCY LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA55NM 20040524001942004052400194EU 2004 5 24 04125321 120040504A335010126243 SIGN JETAIRJETSTMJETSTM4101 1500501EU CABIN INTERMITTENT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27321UE 41045 DURING INSPECTION THE FOWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20040524001972004052400197 2004 5 24 ARWA20040501 420040505A341619769101 INDICATOR DOUG DC8 DC863F 302198FWP STANDBY ALT MALFUNCTIONED A ARWAO OTHER N FALSE WARNING CRCRUISE 1 SO19784AL 46135 STANDBY ALTITUDE INDICATOR FAILED IN FLIGHT. REMOVED STANDBY INDICATOR & REPLACED WITH SERVICE STANDBY ATT. INDICATOR. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DACO DC-8 MM 24-3-3. 2L74 4F 4A25 20040525000012004052500001NM 2004 5 25 QXEA200400305 120040503A5210D5D592395926 STRUT DHAV DHC8 DHC8202 2809007NM ZONE 800 FAILED A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09361PH21 21 516 MAIN CABIN DOOR ASSIST STRUTS ARE NOT OPERATING. MAIN CABIN DOOR VERY DIFFICULT TO OPEN AND CLOSE. WHEN DOOR DOES OPEN IT DROPS VERY RAPIDLY. REMOVED AND REPLACED PASSENGER DOOR GAS STRUTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040525000042004052500004EU 2004 5 25 DHL3642004508 120040316A53476022417 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, SEAT TRACK FLANGE HAS CORROSION AT FR 26 - 30 RBL 37. REMOVED CORROSION FROM SEAT TRACK FLANGES BETWEEN FR 26 - 30, RBL 37 IAW A300 SRM 51-40-11. CUT OUT DAMAGE SEAT TRACK SECTION FROM FR. 26 1/2 TO FR. 32 1/2-123 IAW A-300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO HI IAW A300 SRM 53-10-10 FIG. 724. 51-27-00, MATERIAL USED SEAT TRACK PO 2403961 P/N 60-22417, LENGHT, SPLICES. P/N 60-12336, PO 24072359, 4 FT. LENGHT. TREATED AND PRIMED, POLIWHITE NEW PARTS IAW A300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION FR. 26.5 TO 32 1/2 1231 LENGHT IAW A300 SRM 53-10-10 FIG. 724. 2L72 4F RTA35EU 20040525000062004052500006WP 2004 5 25 LO62004F00001 120040506A711131954 ACTUATOR CVAC 340 34032 2422706WP PWA R2800 R2800* 52026NE COWL FLAPS INOPERATIVE D LO6BO OTHER O OTHER NRNOT REPORTED 1 SW173427 4155 90 RT SIDE, COWL FLAP ACTUATOR BECAME INTERMITTENT. FINALLY COWL FLAPS STOPPED PART WAY OPEN. REPLACED ACTUATOR WITH OVERHAULED UNIT. 2L72 4R4 R 6A6 5E8 20040525000082004052500008EU 2004 5 25 E812004F00007 120040430A3040 HEATER BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE731* 01518WP WINDSCREEN INOPERATIVE B E81RO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL03833CW L292207 258033 PILO RPORTED LT WINDSCREEN OVERHEAT ANNUNCIATOR LIGHT, WOULD NOT RESET. LT (A) WINDSCREEN WOULD NOT DISSIPATE PRECIPITATION, VISUAL APPEARANCE (WAVY). FOUND RESISTANCE BETWEEN (A) SCREEN P1 AND P2 TERMINALS AT 25 OHMS, SERVICE LIMIT 35.15 TO 47.55 OHMS. REPLACED (A) SCREEN ASSY. WITH REPAIRED UNIT IAW MM 56-10-11. OPERATIONAL CHECKS ON GROUND, OK. AIRCRAFT MAINT HISTORY UNAVAILABLE. 2L72 4F4 FRTA3EU E6WE 20040525000142004052500014NM 2004 5 25 SWAA041348 120040511A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29711HK 27845 DURING SPV, FOUND RT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040525000162004052500016 2004 5 25 SWAA041330 420040511A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040525000182004052500018 2004 5 25 SWAA041332 420040511A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED PM CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040525000192004052500019NM 2004 5 25 SWAA041333 120040511A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040525000202004052500020NM 2004 5 25 SWAA041334 120040511A5340907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED L1 DOOR UPPER HINGE BOX FITTING PER EA. 2L72 4F RTA16WE 20040525000212004052500021NM 2004 5 25 SWAA041336 120040511A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040525000222004052500022NM 2004 5 25 SWAA041337 120040511A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040525000232004052500023NM 2004 5 25 SWAA041338 120040511A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND BS 296, STRINGER 10L, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040525000242004052500024NM 2004 5 25 SWAA041339 120040511A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040525000262004052500026NM 2004 5 25 SWAA041341 120040511A53116546593 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 500 A, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040525000272004052500027NM 2004 5 25 SWAA041342 120040511A53116546534 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 520, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040525000302004052500030NE 2004 5 25 LX52004F00000 120040506A29300711311820 INDICATOR SKRSKYS76 S76B 8143007NE PWA PT6 PT6* 52043EA HYD SYSTEM INOPERATIVE E LX5AO OTHER O OTHER NRNOT REPORTED 1 GL19761LL 760379 THE NR 2 HYDRAULIC SYS RETURN FILTER BYPASS INDICATOR WAS FOUND EXTENDED (POPPED) ON PREFLIGHT CHECK. WHEN WE REMOVED THE FILTER TO CHANGE IT, A SMALL PIN WAS FOUND IN THE FILTER BOWL. UPON FURTHER INVESTIGATION, A HOLE WAS FOUND ON THE SIDE OF THE BYPASS INDICATOR. WE INSPECTED A NEW BYPASS INDICATOR AND DETERMINED THE PIN THAT WAS FOUND IN THE FILTER BOWL SHOULD BE INSTALLED IN THE HOLE IN THE SIDE OF THE INDICATOR. RECOMMEND STAKING THE PIN AFTER IT IS INSTALLED IN THE SIDE OF THE INDICATOR. 1G72 4U3 T H1NE E2NE 20040525000522004052500052EA 2004 5 25 VNAA0405002 120040501A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07250PS 7929 DURING FLIGHT, THE EMERGENCY DOOR MASTER CAUTION CAME ON AT 24,000 FEET, PRESSURE REMAINED GOOD. MAINTENANCE CONTROL DEFERRED WITH CREW, 52-70-03-C. 2L72 4F4 FRTA21EA E15NE 20040525000542004052500054NM 2004 5 25 VNAA0405004 120040503A5210 DOOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MAIN PAX OPEN A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07441JS 3059 AFTER TAKEOFF, THE MAIN CABIN DOOR OPENED, AND FLIGHT 2447 RETURNED TO ABE, AIRCRAFT N441JS WAS THEN FERRIED TO CAK. THIS IS CURRENTLY STILL UNDER INVESTIGATION. AN UPDATED ODR WILL BE PROCESSED WHEN THE INVESTIGATION HAS BEEN COMPLETED. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040525000562004052500056EA 2004 5 25 VNAA0405006 120040507A5220 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE OVERWING FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07245PS 7919 THE CREW RECEIVED A RIGHT HAND OVERWING EMERGENCY EXIT CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REINSTALLED THE RIGHT HAND OVERWING EMERGENCY DOOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040525000582004052500058 2004 5 25 VNAA0405008 420040512A34178220372445 ADC CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT FAILED A VNAAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 GL07247JS84 7922 DURING TAKEOFF, THE CAPTAIN'S SIDE AIR SPEED INDICATOR, VERTICAL SPEED INDICATOR, AND MACH TRIM HAD NO INFORMATION DISPLAYED. MAINTENANCE THEN REPLACED THE NR 1 AIR DATA COMPUTER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040525000602004052500060 2004 5 25 VNAA0405010 420040515A34178220372445 ADC CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07251PS84 7931 DURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE AIR DATA COMPUTER IN ACCORDANCE WITH 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040525000612004052500061NM 2004 5 25 VNAA0405012 120040522A2611 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL05434JS 3051 THE CREW REPORTED GETTING A LAV SMOKE FAIL CAS MESSAGE. MAINTENANCE DEFERRED THE LAV SMOKE DETECTION SYSTEM WITH THE CREW PER 26-3 CODE C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040525000622004052500062NM 2004 5 25 VNAA0405011 120040518A261251653151 CONTROL UNIT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FIRE WARNING FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL05426JS23533 3038 THE CREW REPORTED THAT A FIRE SQUIB WAS FAILING TO TEST. MAINTENANCE INSPECTED AND REPLACED THE FIRE WARNING CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040525000662004052500066NM 2004 5 25 MWEA040070 120040509A5220 CLIP BOEING717 717200 1383700NM TAILCONE DEFECTIVE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31903ME 55167 TAILCONE WOULD NOT DROP USING AFT ENTRY DOOR EMERGENCY RELEASE MECHANISM. ADJUSTED SPRING CLIPS FOR PIN 12. RETESTED OPERATIONS CHECKED GOOD. 2L72 4F TRA6WE 20040525000672004052500067NM 2004 5 25 HNAA0400044 120040506A27515908353 TRANSMITTER DHAV DHC8 DHC8102 2809003NM TE FLAPS DEFECTIVE A HNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA07931HA 132 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL, ABORTED TAKE-OFF R&R RT RVDT 2H72 4T RTA13NM 20040525000682004052500068SO 2004 5 25 C2XA04CL051 120040508A323122250100003 SOLENOID VALVE EMB 135 EMB135LR 3260305SO NLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2727523 145389 CLE FLIGHT 2234 THE CREW REPORTED NOISE AND VIBRATION COMING FROM THE NOSE OF THE AIRCRAFT. RECYCLED LANDING GEAR WITH NO CHANGE. AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, FOUND NOSE GAER DOORS WOULD NOT CLOSE. REMOVED AND REPLACED NOSE GEAR DOOR SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20040525000722004052500072SO 2004 5 25 GLBA20030623 120040505A3350D36604001375 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A GLBAO OTHER O OTHER CRCRUISE 1 NM03108UX6261 120108 EMERGENCY EXIT LIGHTS IN ROW 5A DIM, R & R EMERGENCY BATTERY PACK PN D366-04-001 2L72 4T RTA31SO 20040525000732004052500073EU 2004 5 25 DHL2004364511 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, CABIN-8TH SEAT TRACK FROM LT SIDE, HEAVY CORROSION ON LOWER FLANGES AND IN SEAT TRACK BETWEEN FRAME 20-21. REMOVED CORROSION AT I/B SIDE OF SEAT TRACK IAW A300 SRM 51-40-11 PAGE 701. MATERIAL REMOVED .040 ORIGINAL THICKNESS .090. FOUND TO BE OUT LIMITS IAW A300 SRM 53-10-00 PAGE 619. CUT OUT CORRODED SEAT TRACK AT FR. 22 1/2 (RBL 36) AND REMOVED SECTION FROM FR 19-22 1/2 IAW A300 53-10-10, FIG. 724. TRIMMED TO FIT NEW SEAT TRACK SECTION BETWEEN FR 19-22 1/2 (6 1/2 FEET) AND 4 EACH REPAIR ANGLES (1 FT EACH) AT FR 22 1/2 IAW A300 SRM 53-10-10, FIG. 724 MATERIAL USED AS FOLLOWS SEAT TRACK = 60-22457, PO 24030161 4 EACH REPAIR ANGLES = 60-12336, PO 24072359. TREATED, PRIMED, AND POLIWHITED SEAT 2L72 4F RTA35EU 20040525000742004052500074WP 2004 5 25 ABXA040171 120040402A5320 SUPPORT DOUG DC9 DC932F 3022067WP FUSELAGE FAILED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 ON POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED 1 9G NET SUPPORT PULLED FROM FUSELAGE MOUNT. REPAIRED DAMAGED AREA IAW REA D953-49569MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0. 2L72 4F A6WE 20040525000752004052500075WP 2004 5 25 ABXA040173 120040428A5542 SKIN DOUG DC8 DC863 302198AWP RUDDER TE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 RUDDER TRAILING EDGE TIP HAS METAL MISSING. REPAIRED ARE IAW DC-9 SRM 55-2-0, 51-1-2, 51-1-21A, 51-4-8 AND REA D855-49316MR. 2L74 4F 4A25 20040521000172004052100017NM 2004 5 21 252TR0020 120040429A3350900835A BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTING WILL NOT HOLD CHARGE. REPLACED BATTERY PACK FOR HATCH LIGHTING. OPS CHECKS OK. 2L72 4F RTA16WE 20040521000262004052100026WP 2004 5 21 IXXA0400041S 120040308A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION MAIN CARGO COMPT FRAME CRACKED 3 INCHES STAT. 1580.000, L-21R, MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING IAW DC8 SRM 53-2-0 PAGE2 OF 2 FIG 2, REMOVED DAMAGED AREA IAW SRM 53-2-0 PAGES 2 OF 2 FIG. 2, FABRICATED FRAME IAW SRM 53-2-0 PAGES 2 OF 2 FIG. 2, PERFORMED HEAT TREATMENT IAW SRM 51-1-1, PAGES 1, 13, 17 CLEANED, TREATED AND PRIMED AREA + FRAME + SPLICES IAW SRM 51-1-8B INSTALLED FRAME + SPLICES IAW SRM 51-1-20D. 2L74 4F RT4A25 20040521000332004052100033WP 2004 5 21 ASMF200405015 120040514A215020495054 COOLING TURBINE DOUG DC9 DC987 3022087WP CABIN COOLING FAILED W ASMFK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW23753RA5522585 49587 DURING TRANSIT CHECK SMOKE IN CABIN WAS REPORTED WHEN GROUND PNEUMATIC UNIT WAS CONNECTED AND LT AIR CONDITIONING SYSTEM WAS ACTIVATED. THE SYSTEM WAS CHECKED AND NO SMOKE EVIDENCE WAS DETECTED. BOTH AIR COOLING TURBINES WERE CHECKED AND LT AIR CONDITIONING SYSTEM WAS DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE AT GDL, LT TURBINE COOLING WAS REPLACED IAW MM 21-51-1, TEST CORRECT. 2L72 4F RTA6WE 20040521000432004052100043EU 2004 5 21 KBM2004F00075 120040501A71700174078030 DRAIN VALVE SNIAS 350 AS350B1 8680811EU ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 ENGINE WILL NOT START. NO RISE ON T4. REMOVED AND REPLACED. 1G71 3U H9EU 20040521000512004052100051NE 2004 5 21 PCAA0405200 220040501A7397 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE SENSING BULB CHAFED A PCAAD RETURN TO BLOCK N FALSE WARNING NRNOT REPORTED 1 EA13814EX 318 REPORTED THE NR 2 ENGINE FUEL TEMPERATURE AS ERRATIC. WHILE MAINTENANCE WAS REPLACING THE FUEL TEMPERATURE SENSING BULB IT WAS NOTICED THAT THE WIRE GOING FROM PIN B TO GROUND ON THE TEMPERATURE SENSING BULB'S CONNECTOR WAS CHAFED. WIRE WAS REPAIRED AND SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040521000642004052100064 2004 5 21 P5CA0401079 420040429A256560B50072 SLIDE BOEING747 747249F 1384849NM CABIN DEPLOYED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 UPPER DECK CREW RH DOOR ESCAPE SLIDE DEPLOYED. SLIDE REMOVED AND DEFERRED PER MEL 25-11-3. 2L74 4F A20WE 20040521000682004052100068EA 2004 5 21 MASA200400236 120040428A2711 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM OUT OF ADJUST A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0775998 7336 CREW REPORTED IN LEVEL FLIGHT A/C HAS TO BE TRIMMED WING DOWN OUT OF GREEN LIMITS. MX ADJUSTED THE AILERON ACTUATOR OPS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040521000712004052100071EA 2004 5 21 MASA200400232 120040428A2760855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW07759946473 7367 DIVERTED TO IAD BUT WAS ORIGINALLY GOING TO DCA. CREW REPORTED THE FLAPS FAIL AT 20 DEGREES. A/C IS CURRENTLY OUT OF SERVICE AND MX IS TROUBLESHOOTING. MX FROM CLT WENT TO IAD BUT COULD NOT CLEAR FAULT. A/C FERRIED TO PHL AND BOTH BPSU'S WERE CHANGED OPS CHECKED GOOD 2L72 4F RTA21EA 20040521000732004052100073EA 2004 5 21 MASA200400230 120040428A5210HSP115B094900 PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07592ML 7410 THE CAPTAIN REPORTED THE CREW ENTRANCE DOOR (PAX DOOR) INTERIOR PULL HANDLE TO STOW THE OUTER HANDLE PULLED OFF. MX REPLACED ROLLER PIN IN DOOR HANDLE OPS CHED GOOD 2L72 4F RTA21EA 20040521000762004052100076 2004 5 21 MASA200400035 420040116A31706229820009 DCU CNDAIRCL600 CL6002B19 1900309EA RT ELEVATOR INOPERATIVE A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW0777278 7228 NO INDICATION OF MOVEMENT ON THE RIGHT ELEVATOR. MX PLACED ITEM ON MEL 27-34-01 1/20/2004. MX REPLACED THE DCU. OP CHECKS GOOD 2L72 4F RTA21EA 20040521000822004052100082EA 2004 5 21 MASA200400058 120040201A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0717175 7175 CREW ABORTED TAKE-OFF DUE TO CONFIG SPOILER WARNING MESSAGE. MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USED 2L72 4F RTA21EA 20040521000842004052100084EA 2004 5 21 MASA200400071 120040206A302024403615 SENSING ELEMENT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM CHAFED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775995 7361 AIRCRAFT ABORTED TAKE-OFF WITH ANTI-ICE DUCT WARNING MSG ON T/O. MX TROUBLE SHOT. MX REPLACED THE FIRE WARNING ELEMENT. OP CHECKS GOOD 2L72 4F RTA21EA 20040521000872004052100087EA 2004 5 21 MASA200400106 120040224A5320601R35031239 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW07591ML5766 7388 FS 621, LBL 40, WL 73 UNDER SUPPORT ANGLE IS CRACKED. FABRICATED REPAIR ANGLES FROM P/N 601R-53-61-004-1 AND 601R-53-61-004-5 AND INSTALLED IAW BOMB REO 601R-53-61-117 REV B 2L72 4F RTA21EA 20040521001162004052100116 2004 5 21 KBM2004F00081 420040121A342495550A INDICATOR BELL 206 206B 1181511SW TURN & SLIP STICKS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 TURN AND SLIP INDICATOR NEEDLE STICKS. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 1G71 3U H2SW 20040521001222004052100122EU 2004 5 21 KBM2004F00088 120040123A5270SP381210 SWITCH SNIAS 350 AS350B2 8680813EU CARGO DOOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH59 2884 LT SIDE BAGGAGE DOOR WARNING LIGHT, INOPERATIVE. ADJUSTED MICROSWITCH FOR LT SIDE BAGGAGE DOOR. OPS CHECKED GOOD. 1G71 3U H9EU 20040521001262004052100126NE 2004 5 21 MASA200400201 220040414A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A MASAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW071723115246 7231 872304 CREW REPORTED NR 2 ENGINE ITT 84 DEG HIGHER THAN THE NR 1 ENGINE. MX PERFORMED AN ENG COMP WASH AND PWR ASSURANCE CHECKS. MX BORESCOPED NR 2 ENGINE AND REJECTED IT. MX REPLACED NR 2 ENGINE. OP CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040521001302004052100130EA 2004 5 21 MASA200400214 120040420A2120 ODOR CNDAIRCL600 CL6002D24 1390016EA CABIN DETECTED A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07902FJ 15002 RETURNED TO FIELD DUE TO A REPORT OF A SMOKEY/OILY ODOR IN THE CABIN. IN THE COCKPIT THE LAV SMOKE WARNING MESSAGES WERE DISPLAYED. MX WAS CALLED. MX CONFIRMED THE PRESENCE OF THE ODOR, BUT WAS UNABLE TO DUPLICATE THE PROBLEM WHILE RUNNING THE ENGINES. MX COULD NOT DUPLICATE. NO PARTS USED 2L72 4F RTA21EA 20040521001342004052100134NM 2004 5 21 04FDEA001061 120040422A5320ABA8225505 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CABIN STA 427 RBL 8.5 FLOOR PANEL SUPPORT CORRODED. FWD CABIN STA 427 RBL 8.5 FLOOR SUPPORT REMOVED AND REPLACED IAW SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040521001432004052100143NM 2004 5 21 AT0400012 120040503A3397 WIRE BOEING717 717200 1383700NM ROW 3F BROKEN A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15940AT 55004 EMERGENCY LIGHTS AT ROW 3F INOPERATIVE. RETERMINATED BROKEN WIRE AT SEAT ROW 3 DISCONNECT IAW SWPM 20-31-00. FUNCTIONAL CHECK NORMAL IAW AMM 33-51-00. 2L72 4F TRA6WE 20040521001542004052100154 2004 5 21 P5CA0401086 420040504A3441 WARNING LIGHT BOEING747 747249F 1384849NM COCKPIT ILLUMINATED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23920FT 22237 NR 2 INS WARNING LIGHT ON AFTER DOOR CLOSED. CLEAN AND REALIGNED INU. OPS CK NORMAL AS PER 34-41-00. 2L74 4F A20WE 20040521001622004052100162WP 2004 5 21 ABXA040165 120040426A53135920319513 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 LONGERON 30 CRACKED, STA. 588. REPAIRED LONGERON 30 IAW REA D953-49676MR. REPAIRED FRAME AT FS 579 IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040521001642004052100164WP 2004 5 21 ABXA040167 120040426A531039536262 DOOR FRAME DOUG DC9 DC931 3022065WP BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23941AX 47419 AFT PRESSURE BULKHEAD DOOR JAMB LEFT UPPER STOP FITTING CRACKED ON HORIZONTAL LEG. REPLACED FITTING IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20040521001752004052100175NM 2004 5 21 04FDEA01089 120040424A5320ADA8424513 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 FWD CARGO COMPARTMENT STA 1119 - 6-10 LONGERON 44 RT SPLICE FOUND CRACKED. FWD CARGO COMPARTMENT STA 1119 - 6-10 LONGERON 44 RT SPLICE REMOVED AS PER SRM 51-33-01 VOL II AND INSTALLED NEW SPLICE AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040521001822004052100182 2004 5 21 61027 420040502A2300437003 AMPLIFIER BEECH 1900 1900D 1154162CE NR 2 COMMS NOISY A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07144ZV UE144 WHILE IN ROUTE TO TPA FROM PFN. COMMS NR 1 & 2 DEVELOPED LOUD SQUEAK. AIRCRAFT RETURNED TO PFN MAINTENANCE WAS CALLED. R&R FO'S AUDIO AMP & NR 2 RADIO AMP. P/N 437-003. S/N 508 2L72 4T RTA24CE 20040521001842004052100184WP 2004 5 21 0028 220040427A753295881271 BLEED VALVE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP LT ENGINE DEFECTIVE E CIEAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NM03553V 10189563 35A141 P74430C DURING TAKEOFF ROLL, PILOT UNABLE TO GET PROPER N1 INDICATION REQUIRED FOR TAKEOFF & ENGINE THEN STARTED ROLLING BACK ON POWER. TAKEOFF ABORTED & AIRCRAFT STOPPED WITHOUT INCIDENT. MX INSPECTED ENGINE & PERFORMED A GROUND RUN, UNABLE TO DUPLICATE PROBLEM. DEEC (DIGITAL ELECTRONIC ENGINE COMPUTER) DOWNLOADED & CHECKED. DOWNLOAD INDICATED A MOMENTARY OVERTEMP ON ITT. NO OTHER FAULTS NOTED. MODIFICATION OF SDR A COMPLETE FUNCTIONAL CHECK OF SURGE BLEED VALVE PERFORMED & UNIT FOUND TO NOT PERFORM WITHIN SPECIFICATIONS. UNIT REPLACED PER SB TFE731-76-3072. ENGINE RUN & CHECKED ON GROUND. 2L72 4F4 F A10CE E6WE 20040524000162004052400016WP 2004 5 24 DHL2004803528 120040412A57203804001508 CLIP DOUG DC8 DC873 302199CWP FUEL TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 4 ALT TANK (1EA) CRACKED CLIP BETWEEN STA XW 495.665 AND CTR WING SPAR CORNER. REMOVED AND REPLACED CRACKED CLIP BETWEEN STA XW 495.665 AND CTR. WING SPAR (NR 4 ALT TANK) IAW DC8 SRM 51-1-20D PG. 21-9. REFER TO NR 0341 FOR LEAK CHECK. 2L74 4F RT4A25 20040524000182004052400018WP 2004 5 24 DHL2004803539 120040422A5330 SKIN DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 FUSELAGE EXTERIOR SKIN SURFACE WORN (STA FS. 314.000-327.000, L-31R TO L-32R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW ED EDV43-4, DWG V43-R04. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21, SRM 51-3-0 PG.1. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-4, DWG V43-R04. PERFORMED NDT INSP. IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED 2EA FILLERS (7075-T6 0.071) AND DOUBLER (7075-T6 0.080) IAW ED EDV43-4, DWG V43-R04. CLEANED, TREATED AND PRIMED FILLERS AND DOUBLER IAW SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLERS, DOUBLERS AND NEW FASTENERS IAW ED EDV43-4, DWG V43-R04, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. 2L74 4F RT4A25 20040524000202004052400020EU 2004 5 24 MALA040395 120040430A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 DURING 4K INSPECTION IN LCQ, FS 294-319 RT IB SEAT TRACK CORRODED. REMOVED AND REPLACED RT IB SEAT TRACK FROM FS 294-FS 319 IAW MESABA EO NR S53060. REFER TO LG PG. NR 1270902 FOR ADDITIONAL INFORMATION. A/C RETURNED TO SERVICE 5/12/04. 2L72 4T RTA52EU 20040524000302004052400030WP 2004 5 24 MWEA040079 120040519A57535910042510 DOUBLER DOUG DC9 DC981 3022081WP RT FLAP DELAMINATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 RIGHT OUTBOARD FLAP CENTER FIXED VANE HAS A 5.2500 INCH SQUARE DELAMINATION 2.7500 INCH FORWARD OF TRAILING EDGE AT OB EDGE LOWER SURFACE. FABRICATED AND INSTALLED REPAIR FITTINGS AND DOUBLER. 2L72 4F A6WE 20040524000322004052400032WP 2004 5 24 IXXA0400055S 120040328A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND LT WING OB L/E OUTER SECTION LWR SKIN SURFACE CORODED, STA. XFS 710.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTERNERS IAW DC8 SRM 51-120D PG. 21, SRM 51-1-21 PG. 1, SRM 51-3-0 PG.1, REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PG. 11, REMOVED DAMAGED SECTION IAW DWG: V22-R05, PERFOMRED NDT INSP. IAW NDT SPM PART 6-10-01-001 FABRICATED FILLER + DOUBLER IAW DWG: V22-RO5 CLEANED, TREATED AND PRIMED AREA + INNER FACE OF FILLER + DOUBLER IAW SRM 51-1-8B APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9 INSTALLED FILLER + DOUBLER + NEW FASTNERS IAW DWG: V22 RDS, SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG. 1. 2L74 4F RT4A25 20040524000362004052400036WP 2004 5 24 IXXA0400056S 120040328A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIRS WERE ACCOMPLISHED BY REMOVING FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-3-0 PG. 1, SRM 51-1-21 PG. 1, REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18 FOUND OUT OF LIMITS IAW SRM 57-2-1 PG. 11 REMOVED DAMAGED SECTION IAW DWG: V22-R15, PERFORMED NDI INSP. IAW DC8 NDI SPM PART 6-10-01-001 FABRICATED FILLER + DOUBLER IAW DWG: V22-R15 CLEANED, TREATED AND PRIMED AREA + INNER FACE OF FILLER + DOUBLER IAW DC8 SRM , 51-1-8B APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9, INSTALLER FILLER, DOUBLER & NEW FASTENERS IAW DWG: V22-R15 SRM 51-1-21 PG. 1, DC8 SRM 51-120D PG. 9 SRM 51-3-0. 2L74 4F RT4A25 20040524000422004052400042WP 2004 5 24 IXXA0400047S 120040212A5700 VANE DOUG DC8 DC873F 302199FWP RT WING LE CORRODED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11603AL9190 2910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING L/E OB VANE CORRODED, ELONGATED HOLES AROUND STA. XOLDS 6.224. REPAIRS WERE ACCOMPLISHED IAW DWG V22-RO6, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21, REMOVED CORROSION IAW SRM 51-1-8 PAGE 11 17.18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PAGE 11 REMOVED DAMAGED AREA IAW DWG V22-R06, PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 6-10-01 001 FABRICATED FILLER & DOUBLER IAW DWG V22-RO6 CLEANED, TREATED AND PRIMED AREA, FILLER, DOUBLER & INTERNAL PARTS IAW SRM 51-1-8B APPLIED PRC SEALANT TO FAHING SURFACES IAW SRM 51-1-11 PAGE 9 INSTALLED KILLER DOUBLER WITH NEW FASTENERS IAW DWG V22-R06 IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9, SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20040524000442004052400044EU 2004 5 24 AWXA200400556 120040520A2150763A000003 ACM AIRBUS320 A320231 3930325EU ZONE 190 MALFUNCTIONED A AWXAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28625AW 02321 064 AIR TURN BACK ON CLIMB OUT, RECEIVED ECAM MESSAGE FOR PACK 1, NR 2 FAULT WITH ASSOC PACK 2 OVERHEAT. PASSING THROUGH FL 250 ECAM DIRECTED NR 2 PACK BE TURNED OFF, NR 1 PACK ALREADY ON MEL, AS A/C DESCENDED BELOW 10000 FT, NR 2 PACK TURNED OFF & OVERHEAT CONDITION CLEARED, TURNED NR 2 PACK BACK ON & SYS WORKED OK FOR REMAINDER OF FLT, BUT NR 2 PACK TEMP REMAINED HOT. MAINT TROUBLESHOT AC PACKS 1, 2, PREFLT REPORT INDICATED PACK 2 BYPASS VALVE & OUTLET TEMP SENSOR (35HH). R & R PACK 2 OUTLET TEMP SENSOR (35HH) IAW AMM, & BYPASS VALVE, LEAK & OPS CHECK GOOD. REPLACED FLOW CNTRL VALVE FOR PACK NR 1, PROBLEM STILL EXISTS, SYS REMAINS ON MEL. TEARDOWN ANALYSIS OF AIR CYCLE MACHINE S/N 01404 CONFIRMED FAILURE OF UNIT.2L72 4F RTA28NM 20040524000472004052400047NM 2004 5 24 AWXA200400559 120040502A53206552894 FLOOR SUPPORT BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN CABIN FLOOR SUPPORT AT BS 540, LBL 1. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT AT BS 540, LBL 1; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT IAW DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA. 9. 2L72 4F RTA16WE 20040524000902004052400090EU 2004 5 24 MALA040383 120040506A3260MS2740017 RELAY BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15523XJ E2348 LT GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR LIGHT REMAINED ON AFTER RETRACTION. AIR RETURN TO DTW. MAINTENANCE JACKED A/C AND SWUNG GEAR NUMEROUS TIMES COULD NOT DUPLICATE ORIGINAL DISCREPANCY. CHANGED RELAY GF2 FOR PRECAUTIONARY MEASURES WITH SUBSEQUENT SWINGS. ALL CHECKS GOOD AT THIS TIME. PN MS27400-17 ALL IAW AVRO MM CHAP 12 & 32. 2H74 4F RTA49EU 20040524001112004052400111NM 2004 5 24 SWAA041269 120040505A53116516302 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 198, STRINGER 17R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040525000092004052500009 2004 5 25 SWAA041343 420040511A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040525000112004052500011NM 2004 5 25 SWAA041345 120040511A575365C30462 SKIN BOEING737 737317 138447PNM RT FORE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REPAIRED RT WING INBOARD FORE FLAP PER SRM. 2L72 4F RTA16WE 20040525000122004052500012 2004 5 25 SWAA041346 420040511A25656949956 CABLE BOEING737 7375H4 138449DNM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040525000652004052500065NM 2004 5 25 DHL2004765003 120040507A5321 FLOOR PANEL BOEING727 727264 138408MNM CARGO BAY CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01765AT 23014 AFT LOWER CARGO COMPARTMENT FLOOR COMPARTMENT B9 & B10 HAS LIQUID SPILL THAT IS CAUSING SURFACE CORROSION & MINOR PITTING ON FLOOR PANELS. REMOVED CORROSION AND TREATED WITH ARODINE IAW SRM 51-10-2 AND SRM 51-10-6. MATERIAL LOSS LESS THAN .001, WITHIN LIMITS PER SRM 53-10-1 FIGURE 7. 2L73 4F A3WE 20040525000762004052500076NE 2004 5 25 ABXA040172 220040507A7261 OIL TANK DOUG DC9 DC932F 3022067WP PWA JT8 JT8D9A 52048NE NR 2 ENGINE CRACKED A ABXAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23904AX 47040 665919 AIR DIVERSION, EMERGENCY DECLARED, IN FLIGHT SHUT DOWN. AIRCRAFT DIVERTED TO SHV AFTER DEPARTURE FROM SAT WITH REPORT OF OIL PRESSURE LOSS ON NR 2 ENGINE. ENGINE OIL QUANTITY DROPPED TO ZERO, OIL TEMPERATURE BEGAN TO CLIMB. OIL PRESSURE DROPPED TO 35 PSI. NR 2 ENGINE SHUTDOWN. AIR DIVERT TO SHV. FOUND CRACK IN OIL TANK ADJACENT TO OIL QUANTITY PROBE. REMOVED AND REPLACED OIL TANK IAW DC-9 MM 79-10-01-2-0001. REMOVED OIL SCREEN ELEMENTS AND INSPECTED FOR METAL AND FOREIGN MATTER, NONE FOUND. ACCOMPLISHED IAW P&W 72-00. PERFORMED ENGINE RUN IAW DC-9 MM 71-00-00-5-007. NO LEAKS NOTED. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20040525000772004052500077NM 2004 5 25 P5CA0401088 120040507A1420 CONNECTOR BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE EGT INDICATOR DAMAGED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23534MC 21832 517539 AFTER PUSH BACK ON ENGINE START, NR 2 ENGINE EGT GAUGE HAD FLAG IN VIEW. T/S FOUND BROKEN PIN IN CONNECTOR, REPLACED, ALL INDICATIONS NORMAL. 2L74 4F4 F A20WE E23EA 20040525000802004052500080EA 2004 5 25 COMA0460297 120040506A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO01805CA 7354 FLIGHT 5796 SPOILER AND FLIGHT SPOILER CAUTION MESSAGE. COULD NOT DUPLICATE. RESET SECU, SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20040525000822004052500082EA 2004 5 25 COMA0460299 120040507A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA1567 7043 FLIGHT 9475 GEAR DISAGEREE WARNING. COULD NOT DUPLICATE, REPLACED THE PSEU. 2L72 4F RTA21EA 20040525000832004052500083EA 2004 5 25 COMA0460301 120040506A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01940CA9274 7048 FLIGHT 5579 GEAR DISAGREE WARNING, REPLACED THE NLG PRIORITY VALVE 2L72 4F RTA21EA 20040525000852004052500085EA 2004 5 25 COMA0460303 120040510A5320601R3520549 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01427CA9080 7460 CARGO FLOOR SILL IS TORN WHERE THE FOLD DOWN PROTECTIVE EDGE ATACH BRACKET IS LOCATED AT STATION FS 574.0. C/W 601R-53-61-690. 2L72 4F RTA21EA 20040525000872004052500087EU 2004 5 25 YENA200426 120040506A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15508JB 1257 SHORTLY AFTER TAKE OFF (2 MINUTES)INFLIGHT CREW REPORTED AN ODOR LIKE "BURNED PLASTIC" WITH NO VISUAL INDICATION OF SMOKE THRU ENTIRE CABIN. NO ODOR WAS APPARENT IN COCKPIT. LIVE TV WAS TURNED OFF AND PACK FLOW TURNED TO HIGH. ODOR DISSIPATED AFTER 2-3 MINUTES. CREW REKPORTED SLIGHT ODOR ON LANDING. PER TSM 24-00-00-810-823 CHECKED AIRCRAFT FOR ANY SIGN OF BURNING ODOR OR FUMES IN CABIN. FOUND NO SIGNS OR INDICATIONS OF BURNING ODOR. AS A PRECAUTIONARY POWERED OFF LIVE TV SYSTEM AND PLACED ON MEL. LATER INSPECTED LIVE TV SYSTEM AS PER PROCEDURES IN INFO NOTICE 2003-T050TR A. FOUND NO DISCREPANCIES, SYSTEM OPERATING NORMAL IAW LTV MM 23-39-00, MEL CLEARED, LIVE TV SYSTEM ACTIVATED. 2L72 4F RTA28NM 20040525000882004052500088SO 2004 5 25 SWIA200413263 120040414A5720 CLIP EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07580SW 120348 2 ND FROM AFT LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED 2ND FROM AFT LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07. 2L72 4T RTA31SO 20040525000892004052500089SO 2004 5 25 SWIA200413264 120040414A5720 CLIP EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07580SW 120348 MIDDLE LOWER SKIN CLIP CRACKED AT RIB 16, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED MIDDLE LOWER SKIN CLIP AT RIB 16 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07. 2L72 4T RTA31SO 20040525000912004052500091EA 2004 5 25 SWIA200413266 120040413A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 RIGHT PRESSURE FLOOR HAS CORROSION AS MARKED AT FS 409+128 TO 559, RBL 36 TO RBL 48.REPAIRED IAW CRJ REO 601R-53-41-206 REV. NC. 2L72 4F RTA21EA 20040525000922004052500092EA 2004 5 25 SWIA200413267 120040413A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 RIGHT FIREWALL HYDRAULIC SHUTOFF VALVE SUPPORT INTERCOSTAL IS WORN AT AFT BULKHEAD FITTING FS 661 / ADJACENT STR 9.REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F RTA21EA 20040525000932004052500093 2004 5 25 SWIA200413268 420040503A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07405SW815 815 7029 MACH TRIM WILL NOT ENGAGE. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK SATISFACTORY IAW CRJ MM 27-35-01 AND WM 34-13-00. 2L72 4F RTA21EA 20040525000942004052500094EA 2004 5 25 SWIA200413269 120040504A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA LT ENGINE FALSE ACTIVATIONA SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07405SW 7029 LEFT JET OVERHEAT CAUTION MESSAGE. INSTALLED SERVICEABLE JET PIPE ON LT ENG. LT PIPE OVERHEAT TESTS GOOD LOOPS ''A & B''. 2L72 4F RTA21EA 20040525000952004052500095EA 2004 5 25 SWIA200413270 120040506A2752852B1621 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 NR 3 ACTUATOR ON LEFT WING HAS EXCESSIVE PLAY IN FLAP SIDE ATTACH POINT INBOARD BUSHING ON GIMBLE PIN ATTACH POINT. REMOVED AND REPLACED NR 3 ACTUATOR ON LT WING I/B GIMBLE ATTACH BUSHING BLOCK IAW CRJ MM 27-53-05 AND CMM 27-50-12. P/N 2L72 4F RTA21EA 20040525000962004052500096EA 2004 5 25 SWIA200413271 120040506A2750855D1009 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07408SW704 704 7055 RECEIVED A FLAPS FAIL CAUTION MESSAGE UPON ARRIVAL AT SLC. COULD NOT RAISE FLAPS FROM THE 45 DEGREE POSITION. REMOVED AND REPLACED RT BPSU IAW MM 27-51-10. RIGGED RT BPSU IAW CRJ MM 27-51-10 AND REINSTALLED FLEX DRIVE AND SAFETIED IAW CRJ MM 27-54-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040525000972004052500097EA 2004 5 25 SWIA200413272 120040505A261247259702 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU FIRE WILL NOT TEST A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07442SW6282 6282 7609 APU FIRE WARNING AND APU FIRE PUSH LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT IAW CL-600 MM 26-10-01. OPS CHECKS GOOD IAW MM 26-12-00 AT THIS TIME. 2L72 4F RTA21EA 20040525000982004052500098SO 2004 5 25 SWIA200413273 120040505A3350 SOCKET EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07580SW 120348 1ST 3 LIGHTS OF THE FLOOR LEVEL EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. INSTALLED INSULATING BOOT ON E-LIGHT SOCKET OVER PAX DOOR ENTRANCE. EMERGENCY LIGHTS OPS CHECK NORMAL. ALL PANELS AND ITEMS REMOVED FOR ACCESS SECURED. 2L72 4T RTA31SO 20040525001002004052500100EA 2004 5 25 SWIA200413275 120040508A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07441SW 7602 CO-PILOT'S WINDOW CRACKED WHILE INFLT. REMOVED AND REPLACED RIGHT WINDOW IAW CRJ MM 51-00-00. OPS AND LEAK CHECK GOOD. P/N: NP139322-2 S/N OFF: 03133H3843. 2L72 4F RTA21EA 20040525001022004052500102 2004 5 25 SWIA200413277 420040505A22156225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07251YV6001 6001 120251 CAPTAIN'S AUTOPILOT CONTINUOUS AURAL TRIM FAIL MESSAGE AND TRIM FAIL ON MAP, AND AP PANEL. REPLACED ELEVATOR TRIM SERVO SVO-65. CAPT'S AUTOPILOT OPS CK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040525001032004052500103EA 2004 5 25 SWIA200413278 120040508A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07403SW6690 6690 7028 STAB TRIM CH 1 INOP. WOULD NOT RE-ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HORIZONTAL STAB ACTUATOR IAW AMM 27-40-00, 27-42-05. OPS CHECK OK. MCU P/N: 7062-3 S/N OFF: 942 2L72 4F RTA21EA 20040525001042004052500104EA 2004 5 25 SWIA200413279 120040505A2700601R5122623SW CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AIL/RUDER INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07452SW 7716 LT WING DOWN AILERON TRIM IS INOPERATIVE. REMOVED AND REPLACED THE AILERON/RUDDER TRIM PANEL ASSEMBLY. BOTH SYSTEMS CHECK GOOD. 2L72 4F RTA21EA 20040525001052004052500105SO 2004 5 25 SWIA200413280 120040505A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07292UX9366 9366 120292 ON CLIMBOUT THE OUTBOARD FLAPS INDICATED A SINGLE BAR ASSEMETRY. RETURNED TO FAT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-00. OPS CHECK GOOD. 2L72 4T RTA31SO 20040525001062004052500106EA 2004 5 25 SWIA200413281 120040507A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA STALL WARNING DAMAGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07441SW 7602 STALL PROTECTION PUSHER SHAKER WILL NOT WORK. REMOVED AND REPLACED CAPT'S SHAKER CONNECTOR. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040525001092004052500109NM 2004 5 25 C1HA200494001 120040508A3230 LATCH BOEING727 727290 138408WNM MLG FAILED A C1HAO OTHER J WARNING INDICATION CLCLIMB 1 GL15294AS 22146 GEAR LEVER FAILED TO MOVE UP AT DEPARTURE AT CANCUN COM 2.32.23 RUN CONFIRMED FAILURE OF MECHANIC LATCH. PERFORMED LEVER LOCK TEST MM 32-31-11 OPS CHECKS GOOD 2L73 4F A3WE 20040525001102004052500110NM 2004 5 25 P5CA0401089 120040506A77978TK34ACA2 WIRE HARNESS BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 2 ENGINE DAMAGED A P5CAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP23534MC 21832 517539 DURING ENGINE NR 2 START AT GATE, CREW REPORT THAT ENGINE NR 2 EGT NO INDICATION & FLAG IN VIEW. TROUBLE SHOT, FOUND RT UPPER HARNESS AT FAULT. REMOVED AND REPLACE ENGINE HARNESS, ENGINE RUN OPS CHECK OK. 2L74 4F4 F A20WE E23EA 20040525001112004052500111CE 2004 5 25 DXTA200400308 120040510A2821230618826 FUEL FILTER CESSNA750 750 2076810CE ENGINE CONTAMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07950QS 7500050 ON TAKE OFF THE FUEL FILTER BYPASS R-CAS MESSAGE CAME ON, ABORTED TAKE OFF. RESET ELECTRICAL BYPASS INDICATOR IAW ALLISON/ROLLS MM TASK 73-3000-990-801, REMOVED AND REPLACED RIGHT ENGINE FUEL FILTER IAW ALLISON/ROLLS MM CHAPTER 73-21-10 RUN UP LEAK CHECK GOOD, FULL POWER CHECK GOOD. 2L72 4J RTT00007WI 20040525001132004052500113NM 2004 5 25 DHL2004765004 120040511A2170 COALESCER BAG BOEING727 727264 138408MNM LT & RT CONTAMINATED A DHLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01765AT 23014 ON ROTATION NOTICED ODOR AT 500 FT AGL IT SUBSIDED BUT RETURNED 30 SECONDS LATER AND INCREASED 4 MINUTES FROM ROTATION SAW SMOKE IN COCKPIT. DECLARED EMERGENCY. COMPLETED SMOKE IN COCKPIT CHECKLIST. RETURNED TO MCO. INSPECTED E & E BAY WIRING FOR DEFECTS NONE NOTED. INSPECTED LT & RT ACM'S NO DEFECTS NOTED IAW B-727 M/M 21-55-11. PERFORMED OPERATIONAL CHECK OF LT & RT PACKS NO DEFECTS NOTED IAW B-727 M/M 21-55-0. PRESSURIZED AIRCRAFT TO 7 PSI NO DEFECTS NOTED IAW ASTAR JRH CHAPTER 6.3. REMOVED AND REPLACED LT & RT WATER SEPARATOR SOCKS IAW B-727 M/M 21-55-51 (PRECAUTIONARY PER MAINTENANCE (MXC)). 2L73 4F A3WE 20040525001142004052500114NM 2004 5 25 371PA0043 120040507A3350 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 FORWARD SECTION AND AFT SECTION OF EMERGENCY EXIT LIGHTS ARE OUT. CLEANED LUMINET STRIPS, INSTALLED NEW TOP COVER, OPS CHECKS GOOD PER MM 33-51-21. 2L72 4F RTA16NE 20040525001152004052500115NM 2004 5 25 513NA0006 120040506A3246 BOLT BOEING757 7572T7 1384914NM NR 2 MLG MISSING A PIDAK NONE O OTHER ININSP/MAINT 1 SO05513NA 23895 NR 2 MAIN LANDING GEAR TIRE HAS TWO WHEEL BOLTS MISSING. REPLACED NO. TWO MAIN LANDING GEAR WHEEL/TIRE ASSEMBLY PER MM 32-45-01. 2L72 4F RTA2NM 20040525001162004052500116NM 2004 5 25 DHL2004783006 120040424A5753652163586 SKIN BOEING727 727227 1384078NM TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 RT WING OTBD TE FLAP HAS AREA OF DELAMINATION APPROXIMATELY 5 FT FROM INBD END. TEMPORARY REPAIR INSTALLED IAW B-727 SRM 51-40-20 PERMANENT REPAIR TO BE DONE IN 150 FLIGHT HOURS. 2L73 4F A3WE 20040525001182004052500118 2004 5 25 BAQA094573 420040513A342142000332430 INDICATOR UROCOPEC135 EC135T1 5620026EU AHRU FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME 0143 UNIT FAILED OUT OF BOX, BLOWS CIRCUIT BREAKER. REPLACED WITH SERVICABLE UNIT. 05/19/2004 1G72 3U H88EU 20040525001192004052500119NE 2004 5 25 BAQA093854 220040505A7314 SHAFT SEAL BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101* NE FUEL PUMP LEAKING E BAQAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA03117CJ 2AFP701B6 7051 SHAFT SEAL IS LEAKING. REPLACED WITH SERVICABLE UNIT FROM ITS, 05/19/2004 1G72 3U3 U H13EU E5NE 20040525001232004052500123 2004 5 25 BAQA094582 420040513A342041800876250 INDICATOR AEROSPAS355 AS355F2 8680812EU COCKPIT INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03703ME54 0314 ACTUATION LIGHT ON CAD AMBER RT ON HSI INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 1G72 3U H11EU 20040525001242004052500124 2004 5 25 BAQA094213 420040421A3444066304401 INDICATOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE COCKPIT INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03213AE 7219 RADAR ALTIMETER HAS INTERMITTENT OPERATION, SELF TEST AND FACE GLASS LOOSE. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H13EU E5NE 20040525001252004052500125EU 2004 5 25 BAQA094262 120040428A2435 SPLINE BOLKMS117 BK117A3 5626015EU STARTER GEN WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911BK 15836 7099 SPLINE WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE UNIT, 05/20/2004 1G72 3U H13EU 20040525001282004052500128CE 2004 5 25 VJ32004F00000 120040505A3297SM50D7 RELAY BEECH 33 F33A 1151425CE CONT O520 IO520BB 17032SO MLG INTERMITTENT B VJ3RO OTHER O OTHER NRNOT REPORTED 1 WP075581T154 CE1350 820457R PILOT REPORTED THAT LANDING GEAR FAILED TO EXTEND WHEN GEAR SWITCH SELECTED TO DOWN POSITION. AFTER GEAR HANDLE CYCLED SEVERAL TIMES GEAR CAME DOWN. UPON TROUBLE SHOOTING OF THE LANDING GEAR SYSTEM FOUND LANDING GEAR DYNAMIC RELAY INTERMITTENT. 1L71 3O3 O 3A15 E5CE 20040525001292004052500129EU 2004 5 25 RO32004F00002 120040505A1430NAS517V32XA SCREW AMD FALC50FALCON50MYST2730106EU LT WING CHAFED B RO3RO OTHER O OTHER NRNOT REPORTED 1 CE0330FT 271 24TH SCREW IB OF RIB 20 ON LT WING IS CHAFFING ON OB SLAT HYDRAULIC LINE. DOORS, UPPER FIXED STRUCTURE BOX, RIB 7 TO RIB 13. 2L73 4F A46EU 20040526000022004052600002SO 2004 5 26 SIMA200407503 120040315A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21642AE 145193 FOUND FLOOR EMERGENCY LIGHTING INOPERATIVE FROM ROWS 7-12 INCLUDING EXIT ROW LIGHTS. REPLACED NR 3 POWER SUPPLY. OPS CHECK GOOD. (M) 2L72 4T RTT00011AT 20040526000032004052600003SO 2004 5 26 SIMA200404603 120040214A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21649PP 145234 CMH - FLT 4401 - CRWE REPORTED THE EMERGENCY CABIN LIGHTS IN THE LAST THREE ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040526000042004052600004CE 2004 5 26 2004F00142 120040302A261224403915 ELEMENT LEAR 60 60LEAR 5170707CE LT ENGINE MALFUNCTIONED E DELAK NONE O OTHER ININSP/MAINT 1 CE03660AS 191 DURING PREFLIGHT PROCEDURES, THE LT ENGINE FIRE TEE HANDLE DID NOT ILLUMINATE VIA PRESS TO TEST. SYSTEM TROUBLESHOOTING REVEALED THAT THE LT ENGINE ACCESSORY GEARBOX FIRE SENSING ELEMENT, PIN U WAS SHORTED BETWEEN THE CENTER CONDUCTOR AND SHIELDING. REPLACEMENT OF THE FIRE SENSING ELEMENT CORRECTED THE PROBLEM. (M) 2L72 4F RTA10CE 20040526000082004052600008SO 2004 5 26 SIMA200405002 120040218A3350110049 INVERTER EMB 135 EMB135LR 3260305SO NR 2 INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21718AE 145275 LGA - FOUND MAINTENANCE REPORTED THE SERVICE DOOR AREA LIGHT AND EMERGENCY LIGHTS GO DIM WHEN SELECTED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040526000102004052600010SO 2004 5 26 SIMA200410404 120040412A335020131A BATTERY EMB 145 EMB145LR 3260212SO NR 1 INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21615AE 145087 ORD - FLT 3956 - FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 1 EMERGENCY BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040526000112004052600011SO 2004 5 26 SIMA200410401 120040411A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO NR 1 INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21615AE 145087 BNA - NR 1 EMERGENCY LIGHTNG SYSTEM INOPERATIVE. REPLACED NR 1 EMERGENCY BATTERY SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040526000132004052600013SO 2004 5 26 SIMA200408801 120040326A335020131A POWER SUPPLY EMB 135 EMB135LR 3260305SO NR 2 INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21735TS 145386 DURING PREFLIGHT, CREW REPORTED THE FORWARD EMERGENCY LIGHT WOULD STAY ON FOR ONLY 2 SECONDS. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHT BATTERY PACK IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040526000152004052600015SO 2004 5 26 SIMA200407202 120040309A3397 WIRE EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DAMAGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21728AE 145328 NR 3 AND 4 EMERGENCY LIGHT STRIPS ARE INOPERATIVE. REPAIRED WIRE SPLICE IAW AMM 70-03-03. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20040526000172004052600017EA 2004 5 26 ASOA04284 120040419A5610NP1393226 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11925EV 7831 FLT 4266 - DURING DESCENT INTO DFW FROM CAE, AT APPROXIMATELY 20,000 FT THE INTERIOR PANE ON THE FIRST OFFICERS RIGHT WINDOW CRACKED. THE CRACK CONTINUED TO PROPAGATE AND AN EMERGENCY WAS DECLARED AS A PRECAUTION. NO PRESSURIZATION OR OTHER PROBLEMS OCCURRED. THE CREW COMPLIED WITH THE QRH AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS RIGHT WINDOW. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040526000182004052600018EA 2004 5 26 ASOA04285 120040419A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11861AS 7445 DURING AN A-CHECK IN BTR, THE RT SIDE FS 640 DOUBLER BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT SIDE FS 640 DOUBLER BETWEEN STRINGERS 9 AND 12 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040526000192004052600019EU 2004 5 26 ASOA04286 120040420A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11633AS4052 939 344 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040526000202004052600020EA 2004 5 26 ASOA04292 120040424A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 UNDER THE CLIPS RIGHT SIDE HOLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGIEN SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040526000222004052600022EA 2004 5 26 ASOA04290 120040424A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING A C-CHECK IN MCN, THE CARGO BAY LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040526000242004052600024EA 2004 5 26 ASOA04247 120040328A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE PASSENGER DORO FORWARD AND AFT HAND RAIL SUPPORT ARM ATTACH ANGLE SILL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD AND AFT HAND RAIL SUPPORT ARM ATTACH ANGLE SILL. (M) 2L72 4F RTA21EA 20040526000272004052600027SO 2004 5 26 SIMA200406801 120040305A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO NR 4 DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21649PP 145234 FLIGHT ATTENDANTS REPORTS REAR HALF OF EMERGENCY FLOOR EGRESS LIGHTS STAYS ON FOR 1-2 SECONDS AND THEN DIMS COMPLETELY DURING TEST. REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK, OPS CHECKED GOOD. (M) 2L72 4T RTT00011AT 20040526000312004052600031NE 2004 5 26 ASOA04287 220040420A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE LOW A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11851AS 7360 DURING CLIMB-OUT FROM DFW-MEM, PASSING THROUGH 21,000 FT THE CREW RECEIVED AN ENGINE OIL PRESSURE WARNING MESSAGE FOR APPROXIMATELY TWO SECONDS ON THE RT ENGINE AND THEN IT EXTINGUISHED. THE OIL PRESSURE WAS MONITORED WHICH FLUCTUATED RAPIDLY BETWEEN 25 TO 45 PSI. THE CREW COMPLIED WITH THE QRH, PULLING THE POWER TO IDLE AND THE OIL PRESSURE STABILIZED AT 42 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE SERVICED THE RT ENGINE OIL TO THE PROPER LEVEL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040526000322004052600032SO 2004 5 26 SIMA200409701 120040404A272015793101 PRESSURE SWITCH EMB 145 EMB145 3260210SO NR 2 RUDDER MALFUNCTIONED A SIMAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW21612AE 145079 RUDDER 1/2 INOP EICAS. FOLLOWED CHECKLIST, MECHNICAL CONTROL NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 RUDDER PRESSURE SWITCH IAW AMM. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040526000332004052600033NM 2004 5 26 SWAA041329 120040507A528065C28176 DOOR BOEING737 7373H4 1384600NM MLG DAMAGED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29642WN 27715 AIR TURNBACK, AFTER GEAR RETRACTION ON TAKEOFF, RT GEAR LIGHT ILLUMINATED RED. CYCLED GEAR, NO HELP. FOUND BOTH RT CENTER AND INNER GEAR DOORS DAMAGED. REMOVED AND REPLACED BOTH RT GEAR DOORS PER MM. 2L72 4F RTA16WE 20040526000362004052600036NM 2004 5 26 SWAA041369 120040513A53106545810 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 330, LBL 55, CRACKED. REPAIRED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040526000392004052600039 2004 5 26 SWAA041362 420040513A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040526000442004052600044NM 2004 5 26 SWAA041350 120040512A2612894092 ELEMENT BOEING737 7372T4 1384492NM NR 2 ENGINE FAULTY A SWAAO OTHER N FALSE WARNING CRCRUISE 1 SW29722WN 22698 DURING CRUISE FLIGHT NR 2, ENGINE FIRE LIGHT ILLUMINATED, AND FIRE BELL SOUNDED FOR 15 TO 20 SECONDS. ALL ENGINE INDICATIONS APPEARED NORMAL. SYSTEM FIRE TEST ACCOMPLISHED ALL NORMAL. CLEANED CONNECTORS D1204P/D414P AND REPOSITIONED A FIRE LOOP. 2L72 4F A16WE 20040526000472004052600047NM 2004 5 26 SWAA041353 120040512A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 10 ABC, MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040526000482004052600048NM 2004 5 26 SWAA041354 120040512A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STA 133, FWD OF REAR SPAR, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040526000512004052600051NM 2004 5 26 SWAA041358 120040512A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 380, STRINGER 28 R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040526000522004052600052NM 2004 5 26 SWAA041359 120040512A5315BAC1509100146 FLOORBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727C + 7, LBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040526000532004052600053NM 2004 5 26 SWAA041360 120040512A53116546546 FRAME BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, BELT FRAME AT BS 827, RBL 9, CORRODED. REPAIRED BELT FRAME PER SRM. 2L72 4F RTA16WE 20040526000542004052600054 2004 5 26 SWAA041361 420040512A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040526000572004052600057NM 2004 5 26 04FDEA01301 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.496, MATERIAL REMOVED AT O/B FACE: 0.004, I/B FACE: 0.005, REMAINING THICKNESS OF LUG: 0.487. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526000602004052600060NM 2004 5 26 04FDEA01054 120040422A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 FUSELAGE SKIN DENTED AT BS 1080 STR 7R. FUSELAGE SKIN DENT AT BS 1080 STR 7R FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3. 2L73 4F RTA3WE 20040526000612004052600061NM 2004 5 26 04FDEA01055 120040422A5311651766445 FRAME BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 FRAME GOUGED AT STR 22L BS 520. FOUND GOUGE ON FRAME AT BS 520 STR 22 LT TO .023 INCH DEEP. FRAME THICKNESS IS .050 OUT OF LIMITS. REMOVED FRAME SECTION FROM STR 21L - 25L, BS 520. INSTALLED NEW FRAME IAW SRM 53-10-1/SRM 51-30-2/SRM 51-30-5. 2L73 4F RTA3WE 20040526000622004052600062NM 2004 5 26 04FDEA01056 120040422A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 LWR FUSELAGE SKIN DENTED BS 1125 BELOW LAP AT STR 20L. DENT ON SKIN AT BS 1125 BELOW LAP AT STR 20L WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER SRM 53-30-3 FIG 5. 2L73 4F RTA3WE 20040526000652004052600065NM 2004 5 26 04FDEA01059 120040422A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION STA 760 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS BS 760 DELTA BEAM LWR ANGLE. REMOVED AND INSTALLED NEW BS 760 DELTA BEAM LWR ANGLE IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2L73 4F RTA3WE 20040526000672004052600067NM 2004 5 26 04FDEA01085 120040424A5313AFA7797501 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO - STA 1671 RT LONGERON 30 SUSPECTED CRACK. CENTER CARGO - STA 1671 RT LONGERON 30 SPLICE END FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2 AND DWG AFA7797. 2L73 4F RTA22WE 20040526000712004052600071WP 2004 5 26 H592004F00000 120040228A6510 SPLINE HUGHES269 269C 4470504WP LYC O360 HIO360D1A 41514EA DRIVE SHAFT SLIPPED E H59AO OTHER O OTHER NRNOT REPORTED 1 EA1775070 S2019 1404 L2486951A LEVEL FLIGHT, THE TAIL ROTOR DRIVESHAFT STARTED SLIPPING. TAIL ROTOR DRIVESHAFT SPLINES STRIPED. ON FRONT HALF OF SHAFT, STUDENT ENTERED AN AUTOROTATION AND AIRCRAFT LANDED HARD AND RECEIVED SUBSTANTIAL DAMAGE. 1G71 3O3 O 4H12 1E10 20040526000732004052600073 2004 5 26 BAQA094670 420040513A342041600298010 GYRO UROCOPEC135 EC135T1 5620026EU COCKPIT BURNED OUT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME 0143 LIGHTS ARE OUT ON UNIT. REPLACED WITH SERVICABLE UNIT. 05/21/2004 1G72 3U H88EU 20040526000762004052600076SW 2004 5 26 ALGA094690 120040521A6320206375202101 TACH GENERATOR BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL MAIN ROTOR WORN E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03266AL884 52281 FOUND SPLINES INSIDE ARMATURE AND ON DRIVSHAFT WORN. DISCREPANCY FOUND ON 900 HR INSPECTION. RETURNING PART TO VENDOR FOR WARRANTY. 1G71 3U3 UNCH2SW E1GL 20040526000792004052600079EU 2004 5 26 BAQA094586 120040517A63406505A3053 INDICATOR BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE TRIPLE TACH INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601EH 7181 TACH INOPERATIVE, NO N/R. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 U H13EU E5NE 20040526000812004052600081EU 2004 5 26 BAQA094649 120040520A3150C19209VG11 DISPLAY UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206B 0 NE COCKPIT INTERMITTENT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TS1194 0167 SCREEN INTERMITTELY FAILS ON START UP DISK. FLASHES F. 1G72 3U3 UO H88EU E42NE 20040526000842004052600084EU 2004 5 26 BAQA094704 120040422A6720 BEARING BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE PITCH LINK ASSY WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY206 24922513 7544 BEARINGS WORN AND SLOPPY. REPLACED WITH SERVICABLE UNIT. 05/24/2004 1G72 3U3 UNCH13EU E19EU 20040526000862004052600086NM 2004 5 26 04FDEA01107 120040428A5753ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. LEFT WING, O/B FLAP, I/B FWD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. 2L73 4F RTA22WE 20040526000882004052600088NM 2004 5 26 04FDEA01109 120040428A5753ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 O/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040526000902004052600090NM 2004 5 26 04FDEA01288 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. SPOTFACED, CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.405, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.403. REWORKED AREA REPAIRED AS PER EA 1-5750-76670, LT OUTBOARD FLAP INBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526000912004052600091NM 2004 5 26 04FDEA01289 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL LUG THICKNESS: 0.403, MATERIAL REMOVED: 0.005, REMAINING THICKNESS OF LUG: 0.398 REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526000942004052600094NM 2004 5 26 04FDEA01084 120040424A5313NFA631313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO STA 1671 RT LONGERON 37 FASTENER HOLE SUSPECTED CRACK. CENTER CARGO - STA 1671 RT LONGERON 37 REPAIR CARRIED OUT AS PER SRM 53-10-00 VOL I FIG 2. 2L73 4F RTA22WE 20040526000952004052600095NM 2004 5 26 04FDEA01291 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526000992004052600099NM 2004 5 26 04FDEA01293 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.095. REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001012004052600101NM 2004 5 26 04FDEA01295 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.494, MATERIAL REMOVED: 0.004, REMAINING THICKNESS OF LUG: 0.490. REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001042004052600104NM 2004 5 26 04FDEA01298 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671, LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001062004052600106NM 2004 5 26 04FDEA01300 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. O/B ACTUATOR ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.395, MATERIAL REMOVED: 0.002, REMAINING THICKNESS: 0.393. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001082004052600108NM 2004 5 26 04FDEA01304 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.092. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001112004052600111NM 2004 5 26 04FDEA01307 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001132004052600113NM 2004 5 26 04FDEA01309 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.408, MATERIAL REMOVED: 0.007, REMAINING THICKNESS: 0.401. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001162004052600116WP 2004 5 26 04FDEA01255 120040513A5740ARC08311 STOP DOUG DC10 DC1010F 3022111WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LT WING O/B FLAP, O/B FLAP TRACK STOP GOUGED. REMOVED AND REPLACED TRACK STOP IAW MM 20-50-02-2. 2L73 4F A22WE 20040526001192004052600119WP 2004 5 26 04FDEA01258 120040513A5320FXABA71597 INTERCOSTAL DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN DECK L-1 DOOR AFT JAMB STRUCTURE 2ND ACCESS HOLE FROM THE FLOOR FRAME STRUCTURE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-33-01 AT MAE. 2L73 4F A22WE 20040521001962004052100196SO 2004 5 21 LR7A04047 120040403A532033170964 FITTING LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION NR 2053 ACCOMPLISHMENT FOUND FS 738E TROOP DOOR RT LONGERON END FITTING CORRODED AND TOOL MARKED AT RBL 62, WL 142. BLENDOUT AND TREATMENT IAW SRM SMP 583 51-30 AND LMAC SES GLD-1720 TN 0031. REINSTALLED IAW SMP 581 91-00-10. NR 2183. 2H74 4T A1SO 20040521001972004052100197SO 2004 5 21 LR7A04048 120040403A53133339142 FITTING LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION NR 2053 ACCOMPLISHMENT FOUND FS 816E RT LONGERON AFT END FITTING TOOL MARKED AT RBL 62, WL 142. REPLACED FITTING IAW SRM SMP 583 51-60 AND 51-70. NR 2184. 2H74 4T A1SO 20040521002022004052100202SO 2004 5 21 LR7A04053 120040403A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DAMAGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 2658 5025 DURING SCHEDULED C4 INSPECTION IDENTIFIED UNUSED FORMATION LIGHT PORT AT FS 379, BL 0, WL 285. REPAIRED WITH DOUBLER IAW SRM SMP 583 51-140-10. NR 2201. 2H74 4T A1SO 20040524000032004052400003WP 2004 5 24 IXXA0400049S 120040213A5730 PLATE DOUG DC8 DC873F 302199FWP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND CORROSION ON RT OUTER WING IB L/E OUTER PLATING AROUND STA XFS 710.00. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, 51-1-21 PG. 1,51-3-0 PG 1. THE CORROSION AND DAMAGED SKIN WAS REMOVED AND FOUND OUT OF LIMITS. IAW DWG V22-R03 AND SRM 57-2-1 PG. 11. NDT INSPECTION WAS PERFORMED PER NDT SPM PART 6-10-01.001. CLEANED, TREATED AND PRIMED AREA, FABRICATED A REPAIR DOUBLER AND FILLER IAW DWG. V22-R03. THE REPAIR DOUBLER WAS CLEANED, TREATED AND PRIMED. PRC SEALANT WAS APLIED ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER AND FILLER USING NEW FASTENERS IAW DWG V22-R03 AND SRM 51-1-20D PG 9, 51-1-21 PG. 1 AND 51-3-0 PG. 1.. 2L74 4F RT4A25 20040524000172004052400017WP 2004 5 24 DHL2004803530 120040412A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 FWD ACCESSORY COMPT. FRAME CRACK 1.000, STA. 55.000 L-24L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG.2. TRIMMED OUT DAMAGED FRAME SEGMENT AND FABRICATED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT (ALCLAD 7075-0 0.071) IAW DC8 SRM 53-2-0 FIG.2. HEAT TREATED IAW DC8 SRM 51-1-1 PG. 1,13,17. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT IAW DC8 SRM 51-1-21 PG.1, DC8 SRM 51-1-20D PG.9. 2L74 4F RT4A25 20040524000492004052400049WP 2004 5 24 UPS04842392 120040503A53403779762U1 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, AFT SIDE OF STATION 680 FRAME LONG. 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 3779762 AND SRM. 51-1-20D 2L74 4F RT4A25 20040524000542004052400054WP 2004 5 24 UPS04842397 120040503A53403775762U501 FITTING DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 STATION 680 END FITTING FWD. SIDE OF FRAME IS CRACKED AT LONG. 9L. REMOVED AND REPLACED FITTING IAW DWG. 3775762 AND SRM. 51-1-20D 2L74 4F RT4A25 20040524000642004052400064WP 2004 5 24 IXXA0400059S 120040214A5512 PLATE DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE EXTENAL PART CORRODED STA XFS 341.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG1, 51-1-21 PG. 1, 51-1-8 PG. 17-18, 55-2-1 PGS. 15,16 AND DWG V22-R08. AN NDT INPSECTION WAS PERFORMED IAW NDT SPM PART 6-10-01-001. FABRICATED FILLER & DOUBLER IAW DWG V22-R08. CLEANED TREATED AND PRIMED AREA, FILLER & DOUBLER IAW DC8 SRM 51-1-8B. PRC SEALANT WAS APPLIED ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG. 9. INSTALLED FILER & DOUBLER AND FASTENERS IAW DWG. V22-R08,DC8 SRM 51-1-21 PG. 1,51-3-0 PG.1 AND 51-1-20D PG 9. 2L74 4F RT4A25 20040524000662004052400066WP 2004 5 24 IXXA0400061S 120040214A5754 PLATE DOUG DC8 DC873F 302199FWP LT SLOT VANE ELONGATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING A ROUTINE C-CHECK INSPECTION FOUND LT OB SLOT VANE UPPER SURFACE ELONGATEED HOLES STA X0200 67.000 (ON REPAIR DOUBLER). REPAIR WAS ACCOMPLISHED. FASTENERS AND THE EXISTING REPAIR DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1 AND 51-3-0 PG 1. DAMAGED SKIN WAS REMOVED IAW DWG. V22-R16. NDT INSPECTION WAS PERFORMED IAW DC8 SPM PART 6-10-01-001 CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. FABRICATED A REPAIR DOUBLER AND FILLER IAW DWG V22-12. CLEANED TREATED AND PRIMED THE REPAIR DOUBLER AND THE FILLER. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG1. INSTALLED DOUBLER AND FILLER USING NEW FASTENERS IAW DWG V22-R16 AND DC8 SRM 51-1-21PG 1 AND 51-3-0 PG.1 2L74 4F RT4A25 20040524000682004052400068EU 2004 5 24 KBM2004F00089 120040321A2913POLYV597K4 BELT SNIAS 350 AS350B2 8680813EU HYD PUMP SPLIT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH675 3345 HYD PUMP V BELT HAS SPLIT. REMOVED AND REPLACED. 1G71 3U H9EU 20040524000782004052400078 2004 5 24 KBM2004F00097 420040331A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU VHF SYSTEM FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 WILL NOT CHANGE FREQUENCY. REMOVED AND REPLACED. 1G71 3U NCH9EU 20040524000862004052400086EU 2004 5 24 SA04043 120040507A3350321430 BATTERY PACK AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT DISCHARGED A USAAK NONE J WARNING INDICATION ININSP/MAINT 1 EA19767UW 1382 EPSU BATTERY MESSAGE CREATED BY CIDS. MAINTENANCE REPLACED THE RIGHT EPSU BATERY PACK. 2L72 4F RTA28NM 20040524001282004052400128NM 2004 5 24 SWAA041284 120040506A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER AT ROW 11 ABC AND ROW 12 ABC, WORN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040524001302004052400130NM 2004 5 24 SWAA041286 120040506A5523183A8410 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR NR 1, NR 3, NR 4, TAB HINGE BUSHINGS PER MM. 2L72 4F RTA16WE 20040524001322004052400132NM 2004 5 24 SWAA041288 120040507A5340907822 FITTING BOEING737 7373H4 1384600NM L1 DOOR FRAME CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR JAMB LOWER FWD HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER EA. 2L72 4F RTA16WE 20040524001342004052400134NM 2004 5 24 SWAA041290 120040507A335065C27093 LIGHT BOEING737 7377H4 1384404NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 FWD SERVICE DOOR LOWER EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040524001362004052400136NM 2004 5 24 SWAA041292 120040507A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 1121, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040524001382004052400138NM 2004 5 24 SWAA041294 120040507A3350101114 LIGHT BOEING737 7373H4 1384600NM ROW 10 INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED PM CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT ROW 10 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040524001402004052400140NM 2004 5 24 SWAA041296 120040507A3350612825 BATTERY BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29661SW 23173 DURING SCHEDULED SERVICE CHECK, FOUND L1 AND R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040524001602004052400160NM 2004 5 24 SWAA041322 120040510A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 328, STRINGER 28R, CRACKED. REPAIRED SKIN PER ACO. 2L72 4F RTA16WE 20040524001622004052400162NM 2004 5 24 SWAA041324 120040510A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SPV, FOUND BULKHEAD PRESSURE WEB AT BS 1016, BETWEEN SRTINGER 27L AND STRINGER 26L, CORRODED. REPAIRED PRESSURE WEB PER ER. 2L72 4F RTA16WE 20040524001642004052400164NM 2004 5 24 SWAA041326 120040510A335090083 BATTERY BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29659SW 23229 DURING SPV, FOUND EMERGENCY EXIT LIGHTS RT MID CABIN, INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040524001662004052400166NM 2004 5 24 SWAA041328 120040510A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 970, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040524001682004052400168 2004 5 24 SWAA041305 420040508A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001702004052400170NM 2004 5 24 SWAA041307 120040508A335065C34691 LIGHT BOEING737 7373Q8 1384670NM ROW 3 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 3 ABC, LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040524001782004052400178EU 2004 5 24 MALA040382 120040505A2730M835362024M RELAY SAAB SF340 340B 7860101EU PITCH TRIM MALFUNCTIONED A MALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL15408XJ 340B408 ON CLIMBOUT OF MEM, THE FO'S PITCH TRIM ON YOKE WOULD NOT WORK. ALL CIRCUIT BREAKERS WERE IN AND BOTH SIDES WERE BEING MOVED. CAPT SIDE WORKED NORMAL. STARTED TO WORK ON APPROACH. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED RELAYS 15CC & 17CC. PN FOR BOTH M83536-2-024M. TESTED MAIN AND STANDBY TRIM-ALL TESTS ARE GOOD. 2L72 4T RTA52EU 20040524001812004052400181NE 2004 5 24 0400661238 220040502A73218062826 FUEL CONTROL DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 3 ENGINE MALFUNCTIONED A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01238W 12043114 48267 517255 TAKEOFF WAS ABORTED AT 120 KTS WHEN THE NR 3 ENGINE FAILED TO REACH TAKEOFF TARGET N1. CREW ALSO REPORTED AN N2 EXCEEDANCE ON THE NR 3 ENGINE PRIOR TO ABORTING TAKEOFF. MAINTENANCE REPLACED THE MEC AND TRIMMED THE ENGINE. ALL ENGINE INDICATIONS WERE NORMAL. 2L73 4F4 F A22WE E23EA 20040524001852004052400185EA 2004 5 24 04118683 120040427A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27683BR 7692 DURING INSPECTION THE LEFT NR 1 AND 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERAITONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040524001872004052400187EA 2004 5 24 04117668 120040417A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27668BR 7544 DURING INSPECTION THE PASSNEGER DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040524001892004052400189EA 2004 5 24 04121624 120040430A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27624BR 7211 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND IOPERATIVE AND REPLACED. A SATISFACTRY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040524001922004052400192EA 2004 5 24 04122669 120040501A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27669BR 7545 DURING INSPECTION THE PASSENGER DOOR EMERGENCY FLOOR FLOOD LIGHT WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040524001952004052400195NM 2004 5 24 WRLA200420 120040505A2497 WIRE DOUG MD11 MD11 3023602NM COCKPIT PANEL BURNED A WRLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11273WA 48519 AIRCRAFT N273WA DEPARTED KSEA TO RKSO (OSAN-KOREA) AFTER APPROXIMATELY 8 HOURS ACRID SMELL WAS DETECTED AND INTERMITTENT FUMES WERE NOTICED JUST OUTSIDE THE DOOR TO THE CREW BUNK ,NEAR THE AFT C/B PANEL, AND NEAR THE COCKPIT ENTRY AREA, THE CREW MADE DECISION TO DIVERT THE AIRCRAFT TO RJTY (YOKOTA), AT RJTY FOUND WIRES OF EMERGENCY LIGHTING BATTERY CHARGER IN COCKPIT OVERHEAD PANEL CHAFFED AND BURNT,REPAIRED WIRES IAW SWP 20-10-03 THE SYSTEM CHECKED OK, AIRCRAFT DEPARTED FROM RJTY TO OSAN AND BEFOR LANDING ON OSAN THE ACRID RESURFACED FOLLOWED BY A POPPING OF THE COCKPIT DOOR LOCK C/B,ITEM ENTRED ON MEL, AT KSEA REMOVED AND REPLACED THE COCPIT DOOR LOCK SOLENOID 2L73 4F RTA22WE 20040525000032004052500003EU 2004 5 25 DJFA2004004 120040404A7930326180120013 REGULATOR VALVE AMD FALC50FALCON50MYST2730106EU ALIDSGTFE731TFE7313AR WP ENG OIL PUMP FAILED E DJFAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA23551CW3000 3000 51 DURING THE CLIMB THE PILOTS NOTICED THE NR 3 ENGINE OIL PRESSURE LIGHT ILUMINATED. OIL PRESSURE WAS DESCENDING THREW 25 PSI. AT THAT POINT THE PILOTS SHUT DOWN THE NR 3 ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. 2L73 4F4 F A46EU E6WE 20040525000102004052500010NM 2004 5 25 SWAA041344 120040511A57536546434302 SKIN BOEING737 737317 138447PNM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040525000152004052500015 2004 5 25 SWAA041349 420040511A25656567380 COVER BOEING737 7373H4 1384600NM R1 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 R1 DOOR EVAC SLIDE PRESSURE IND LENS COVER CRACKED. REMOVED AND REPLACED LENS COVER PER MM. 2L72 4F RTA16WE 20040525000252004052500025NM 2004 5 25 SWAA041340 120040511A53136551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REPAIRED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040525000592004052500059EA 2004 5 25 VNAA0405009 120040515A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07251PS 7931 DURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE CONFIG AND THE MESSAGE CLEARED. FLIGHT 2377 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. 2L72 4F4 FRTA21EA E15NE 20040525000632004052500063WP 2004 5 25 MWEA040069 120040509A2420976J2544 GENERATOR DOUG DC9 DC981 3022081WP ENGINE INOPERATIVE A MWEAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL31804ME 48030 LEFT GENERATOR LIGHT CAME ON, WAS ABLE TO RESET LEFT GENERATOR, THEN FOURTY-FIVE MINUTES LATER LEFT GENERATOR LIGHT CAME ON AGAIN, STARTED AUXILIARY POWER UNIT, BUT UNABLE TO POWER LEFT SIDE OF ELECTRICAL POWER SYSTEM. REMOVED AND REPLACED GENERATOR CONTROL UNIT. 2L72 4F A6WE 20040525000712004052500071NM 2004 5 25 04FDEA01191 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040525000782004052500078EU 2004 5 25 DHL2004364512 120040313A53476022417 SEAT TRACK AIRBUS300 A300B4203 3930306EU CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING "C" CHECK, 5TH SEAT TRACK FROM LT SIDE, INBD LOWER FLANGE CRACKED, OUTBOARD FLANGE HAS CORROSION AFT. OF FRAME 20. REMOVED CORROSION AT FLANGE OF SEAT TRACK IAW A300 SRM 51-40-11 PAGE 1 MATERIAL (REMOVED .030. FOUND TO BE OUT LIMIT IAW A300 SRM 53-10-00. PAGE 619. CUT OUT DAMAGED SEAT TRACK SECTION FROM FR 19 TO 21.5 IAW A300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO FIT IAW A300 SRM 53-10-10 FIG 724 AND 51-27-00 MAT. USE SEAT TRACK: PO24030161, P/N 60-22417, 5 FT. LENGHT, SPLICES, P/N 60-12336, PO 24072359 4 FT. LENGHT. TREATED, PRIMED, AND POLIWHITE NEW PARTS IAW A300 51-40-12. INSTALLED NEW SEAT TRACK SECTION IAW A300 SRM 53-10-10 FIG. 724. 2L72 4F RTA35EU 20040525000792004052500079EU 2004 5 25 DHL3642004510 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN CARGO COMPARTMENT SEAT TRACK FLANGES HAVE SEVERAL AREAS OF CORROSION BETWEEN FR. 32 AND FR. 38.2, LBL 18. REMOVED CORROSION FROM SEAT TRACK FLANGES BETWEEN FR 32 TO 38.2, LBL 18 IAW A300 SRM 51-40-11. MAT. LOSS FROM FR 32 TO 33 = 0.003, FOUND TO BE WITHIN LIMITS IAW A300 SRM 53-10-00, FIG. 612. MAT.LOSS BETWEEN FR 33 TO 38.2 APPROX. 0.020 TO 0.050, FOUND TO BE OUT OF LIMITS IAW A300 SRM 53-10-00, FIG. 612 (NOMINAL THICKNESS 0.090). CUT OUT DAMAGE SEAT TRACK SECTION FROM FR 32.5 TO 38.2 LBL 18 IAW A300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO FIT IAW A300 SRM 53-10-10 FIG. 724 AND 51-27-00. MAT. USED SEAT TRACK PO 24030161, P/N 60-22457, LENGHT 13.5 FT, SPLICES. P/N 60412336, PO=242L72 4F RTA35EU 20040525000812004052500081EA 2004 5 25 COMA0460298 120040505A2720601R5122623 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA INST PANEL MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01479CA 7675 FLIGHT 5644 RUDDER TRIM INOP. REPLACED THE TRIM SWITCH PANEL. 2L72 4F RTA21EA 20040525000842004052500084EA 2004 5 25 COMA0460302 120040505A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01717CA16630 7017 FLIGHT 5672 LANDING GEAR DISAGREE WARNING. COULD NOT DUPLICATE, REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20040525000862004052500086EA 2004 5 25 COMA0470040 120040507A5280CC670105724 CROSSBEAM CNDAIR CNDAIRCL600 CL6002C10 1390015EA MLG DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01355CA 10067 10067 RIGHT HAND MAIN GEAR DOOR CROSS MEMBER IS CRACKED. REMOVED AND REPLACED RIGHT MAIN GEAR DOOOR CROSS MEMBER IAW BOMBARDIER AEROSPACE REPAIR ENGINEERING ORDER REO 670-52-82-014 2L72 4F RTA21EA 20040525001262004052500126 2004 5 25 BAQA094314 420040506A34165035P2P42 ALTIMETER BOLKMS117 BK117B1 5626012EU COCKPIT UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03601EH 7181 ALTIMETER PRODUCING A MODE C-ERROR, REPLACED WITH SERVICABLE UNIT FROM QAI, 05/20/2004 1G72 3U H13EU 20040526000092004052600009SO 2004 5 26 SIMA200311204 120040413A5310163500110 WINDOW POST EMB 145 EMB145 3260210SO COCKPIT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21613AE11641 145081 WHILE CHANGING THE CO-PILOTS WINDSHIELD TWO FASTENER HOLES IN THE LOWER AFT CORNER OF THE AIRFRAME OPENING WERE FOUND TO BE CORRODED. ONE OF THE FASTENER HOLES REMAINED WITHIN MANUFACTURERS LIMITS AFTER REMOVAL OF CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THIS HOLE. REMOVED NUTPLATE FROM SECOND HOLE AND REAMED WINDSHIELD LOWER BEAM AND BELT STRAP TO .313 IN. FABRICATED A BUSHING WITH 100 DEGREE COUNTERSINK TO FILL THE REAMED HOLE. REPAIR DONE IAW AMERICAN EAGLE ENGINEERING TECHNICAL NOTICE EM-53-039 AND EMB REPAIR STATEMENT 1C2004-145/1439. (M) 2L72 4F RTT00011AT 20040526000162004052600016EA 2004 5 26 ASOA04246 120040328A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS DURING A C-CHECK IN MCN, THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 36 AFT CLIP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 36 AFT CLIP BRACKET IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040526000212004052600021EA 2004 5 26 ASOA04291 120040424A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040526000232004052600023EA 2004 5 26 ASOA04248 120040328A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11876AS 7576 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. ARICRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040526000292004052600029EA 2004 5 26 ASOA04288 120040422A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO COMPT MALFUNCTIONED A ASOAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO11839AS 7284 DURING TAXI OUT FROM ATL-CRW, A SMOKE CARGO WARNING MESSAGE WAS RECEIVED AND THE NR 1 AND NR 2 FIRE BOTTLES DISCHARGED. THE CREW COMPLIED WITH QRH PROCEDURES AND PERFORMED AN EMERGENCY EVACUATION OF THE AIRCRAFT. ALL PASSENGERS WERE DEPLANED SAFELY THROUGH THE MAIN PAX DOOR. THERE WERE NO INJURIES AND NO AIRCRAFT DAMAGE. THE AIRCRAFT WAS INSPECTED AND RELEASED BY THE ATL FIRE SERVICES. MAINTENANCE ALSO INSPECTED THE AIRCRAFT AND IT WAS RETURNED TO THE GATE SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND ALSO REMOVED AND REPLACED THE NR 1 AND NR 2 FIRE BOTTLE CARTRIDGES. OPS CHECKS GOOD. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040526000402004052600040 2004 5 26 SWAA041363 420040513A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040526000502004052600050 2004 5 26 SWAA041356 420040512A25656557463 FITTING BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FITTINGS, CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20040526000582004052600058NM 2004 5 26 04FDEA01302 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.498, MATERIAL REMOVED: 0.002, REMAINING THICKNESS: 0.496. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526000632004052600063NM 2004 5 26 04FDEA01057 120040422A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 EXTERNAL FUSELAGE SKIN CHAFE DAMAGED UNDER FAIRING CONTACT AREA, BS 950D 15 - 990, STR 23L - 26L. SKIN CHAFE FOUND OUT OF LIMITS BS 973-989 IAW SRM 53-30-1. REPAIRED SKIN IAW SRM 53-30-3 FIG 3. BLEND OUT FROM 950D 15 - 950E 12, AND 950E 18 TO 973 FOUND TO BE WITHIN LIMITS PER 727 SRM 53-30-1. BLEND OUT FROM BS 950E 12 TO 950E 18 FOUND TO BE OUT OF LIMITS AND TO BE REPAIRED ON N01061. 2L73 4F RTA3WE 20040526000662004052600066NM 2004 5 26 04FDEA01286 120040423A324326011825 BRAKE BOEING727 727200 138407ENM MLG BLOWN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25216FE299 299 22937 ON BLOCK, FOUND NR 1 BRAKE ASSY BLOWN APART. 2L73 4F RTA3WE 20040526000692004052600069 2004 5 26 ASMF200405024 420040521A23406861000002 HANDSET DOUG MD88 MD88 3023688NM INTERPHONE FAILED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23160PL40417 49763 AIRCRAFT RETURNED TO PLATFORM, AFT MICROPHONE FAILURE AND CONSTANT CHIME BETWEEN FLIGHT DECK AND PASSENGER CABIN. REPORT WAS DEFERRED IAW MEL 23-8 CAT (B). DURING TRANSIT CHECK AT MEX, AFT MICROPHONE WAS REPLACED IAW MM 23-40-04, TESTS CORRECT. 2L72 4F RTA6WE 20040526000752004052600075SW 2004 5 26 ALGA094571 120040518A6710406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C* GL UNIVERSAL RATCHETING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03436AL735 53069 EXCESSIVE AXIAL PLAY AND RATCHETY.REPLACED WITH NEW PART. 1G71 3U3 UO H2SW E4CE 20040526000962004052600096NM 2004 5 26 04FDEA01292 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.125. REPAIRED AS PER EA 1-5750-76670. LT O/B FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001032004052600103NM 2004 5 26 04FDEA01297 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), O/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. O/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.190. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001122004052600112NM 2004 5 26 04FDEA01308 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.093. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001142004052600114NM 2004 5 26 04FDEA01310 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.402, MATERIAL REMOVED: 0.003, REMAINING THICKNESS: 0399. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001202004052600120WP 2004 5 26 04FDEA01259 120040513A5710FXARL050022 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AND BROKEN AT XORS 683 INBOARD SIDE. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040526001212004052600121WP 2004 5 26 04FDEA01260 120040513A5320FXADA00595 SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN DECK LT STA 1079 LONGERON 20 FRAME SUPPORT CRACKED. REMOVED AND REPLACED FRAME TEE SUPPORT IAW SRM 51-31-01 AND SRM 51-33-01 AT MAE. 2L73 4F A22WE 20040526001222004052600122WP 2004 5 26 04FDEA01261 120040513A5720FXARL050030 CHANNEL DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT WING VENT PIPE SUPPORT BRACKET CRACKED INSIDE 635 BT. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040526001232004052600123WP 2004 5 26 04FDEA01262 120040513A5720FXARL0500239 CLIP DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LT WING VENT PIPE SUPPORT BRACKET BROKEN INSIDE 538AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040526001252004052600125NM 2004 5 26 04FDEA01038 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS, RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040526001342004052600134NM 2004 5 26 C1HA200494002 120040509A3230 ACCESSORY UNIT BOEING727 727290 138408WNM MLG DAMAGED A C1HAO OTHER O OTHER CLCLIMB 1 GL15294AS 22146 ON DEPARTURE MBJ, GEAR LEVER FAILED TO MOVE TO UP COM 2.32.23 FOLLOWED. CONFIRMED LEVER LATCH FAILURE. R/R LANDING GEAR ACCESSORY UNIT MM 32-09-121 OPS CHECKS OF SYSTEM OK. 2L73 4F A3WE 20040526001352004052600135WP 2004 5 26 AALA20040541 120040510A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21589AA 53252 EMERGENCY LIGHTS AT SERVICE DOOR AND AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK P4010049 (MFR DME CORP) FOR EMERGENCY LIGHTS AT AFT SERVICE DOOR AND BATTERY PACK 60030451 FOR EMERGENCY LIGHTS AT FORWARD AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20040526001392004052600139EU 2004 5 26 AALA20040544 120040510A3234 SELECTOR VALVE AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW2190070 513 MIA ON APPROACH UNABLE TO LOWER GEAR. CREW CYCLED GEAR HANDLE BUT NO INDICATION OR SOUND OF GEAR LOWERING. CREW LOWERED GEAR MANUALLY. LANDED MIA WITHOUT INCIDENT. REPLACED LANDING GEAR SELECTOR VALVE AND LANDING GEAR CONTROL LEVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA35EU 20040526001422004052600142EU 2004 5 26 AALA20040543 120040510A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211405J 11356 ORD EMERGENCY CEILING LIGHT AT ROW 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHT AT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RT 20040526001442004052600144NM 2004 5 26 2004UALA00426 120040502A5320 BRACKET BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT LBL IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED TEE ANGLE. 2L72 4F4 FRTA1NM E24NE 20040526001462004052600146NM 2004 5 26 2004UALA00428 120040502A5320 PULLEY BRACKET BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOOR BEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT LBL 2 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT ANGLE. 2L72 4F4 FRTA1NM E24NE 20040526001522004052600152NE 2004 5 26 2004UALA00435 220040502A7261 O-RING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE LEAKING A UALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29390UA 24665 AIRCRAFT DIVERTED TO AMA DUE TO HIGH OIL CONSUMPTION IN NR 1 ENGINE. FOUND STARTER SHAFT O-RING MISSING. STARTER WAS REPLACED PREVIOUS DAY. REPLACED STARTER SHAFT O-RING AND SERVICED ENGINE OIL . 2L72 4F4 FRTA16WE E2GL 20040526001532004052600153NM 2004 5 26 2004UALA00436 120040504A2910 B-NUT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE A-HYD SYSTEM LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29376UA 24641 CAPTAIN DECLARED AMBER ALERT, LOOSING A SYSTEM HYDRAULICS, UPON INSPECTION AT MSP, THE B-NUT ON THE SYSTEM A-EMDP ACOUSTIC FILTER WAS FOUND LOOSE AND LEAKING. THE B-NUT WAS TIGHTENED AND AN EXTERNAL HYDRAULIC LEAK CHECK WAS PERFORMED TO ENSURE THE LEAK WAS CORRECTED. HYDRAULIC FLUID LEVELS WERE CHECKED AND SERVICED. 2L72 4F4 FRTA16WE E2GL 20040526001542004052600154 2004 5 26 2004UALA00437 420040427A3442 DISPLAY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE WX RADAR MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29653UA 25391 WX RADAR GREEN BAND RING DISPLAY AT APPROX 6.5 MILE IN FRONT OF ACFT. RADAR DISPLAYS A GREEN ARC THAT SEEMS TO MOVE WITH RADAR TILT. 2L72 4F4 FRTA1NM E24NE 20040526001582004052600158NM 2004 5 26 2004UALA00447 120040507A2760 CONTROL MODULE BOEING757 757222 1384956NM PWA 2037 PW2037 NE SPOILERS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29553UA 25277 DURING CLIMB EICAS SPOILER MESSAGE DISPLAYED. FAULTED NR 3 RIGHT SPOILER CONTROL MODULE (SCM) REPLACED NR 7 RIGHT SCM 2L72 4F4 FRTA2NM E17NE 20040526001632004052600163EA 2004 5 26 SWIA200413297 120040503A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484 LBL 27 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED CRACKED CLIP AT LBL 27 BS 484 IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20040526001642004052600164SO 2004 5 26 C2XA04SH280 120040511A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716561 145610 SHV-DURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT UPPER SUPPORT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040526001652004052600165NM 2004 5 26 DL73S040398 120040506A5311VARIOUS FRAME BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 MULTIPLE DENTS WERE NOTED IN ADJACENT FUSELAGE FRAMES IN THE AFT BAG BIN AREA. DAMAGES WERE REPAIRED IAW ERA 090120-14. 2L72 4F A16WE 20040526001662004052600166NM 2004 5 26 DL73S040399 120040506A5330654577518 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 A CRACK APPROXIMATELY 2.3 INCHES LONG WAS NOTED IN THE FUSELAGE SKIN APPROX. 1 INCH AFT OF BS 727B JUST BELOW S18R. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089987-14. 2L72 4F A16WE 20040526001672004052600167NM 2004 5 26 DL73S040400 120040506A531165479602 FRAME BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 CORROSION WAS NOTED ON THE BS 847 FRAME JUST ABOVE S25R. DAMAGE WAS REMOVED AND REPAIRED AS PER ERA 089931-14. 2L72 4F A16WE 20040527000012004052700001NM 2004 5 27 04FDEA01421 120040524A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO STR 26 RT STA 720B CORRODED. REMOVED DAMAGE AREA OF STRINGER AND STIN AT BS 720B. FABRICATED AND INSTALLED REPAIRS IAW SRM 53-30-3, 53-10-3. 2L73 4F RTA3WE 20040527000032004052700003NM 2004 5 27 04FDEA01423 120040524A531365453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 STRINGER CLIP CRACKED STA 950A STR 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 6R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040527000052004052700005 2004 5 27 SWAA041375 420040514A2565D31354 SLIDE BOEING737 7377H4 1384404NM L2 DOOR LOW A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 L2 DOOR EVAC SLIDE PRESSURE LOW PRESSURE INDICATION. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040527000062004052700006NM 2004 5 27 SWAA041376 120040514A335010107451 SIGN BOEING737 7375H4 138449DNM EMERGENCY EXIT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29521SW 25320 RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED OVERWING SIGN PER MM. 2L72 4F RTA16WE 20040527000082004052700008NM 2004 5 27 SWAA041378 120040514A335010107451 SIGN BOEING737 7377H4 1384404NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 RT OVERWING EMERGENCY EXIT SIGN MISSING. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040527000092004052700009 2004 5 27 SWAA041379 420040514A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040527000112004052700011 2004 5 27 SWAA041381 420040514A25656949956 CABLE BOEING737 7372T4 1384492NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F A16WE 20040527000132004052700013 2004 5 27 SWAA041383 420040514A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040527000162004052700016NM 2004 5 27 SWAA041386 120040514A53306545765 SKIN BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29738CB 27870 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN AT BS 500+8, FWD AIR PHONE ANTENNA, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040527000172004052700017NM 2004 5 27 SWAA041387 120040515A3350101073 COVER BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 FWD SERVICE DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LIGHT COVER PER MM. 2L72 4F RTA16WE 20040527000182004052700018NM 2004 5 27 SWAA041388 120040515A335065C27093 LIGHT BOEING737 7373Q8 1384670NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT ENTRY DOOR LIGHT PER MM. 2L72 4F RTA16WE 20040527000192004052700019NM 2004 5 27 SWAA041389 120040515A53126545409 PRESSURE PANEL BOEING737 737317 138447PNM LT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND LT MLG BEADED PRESSURE WEB AT BS 664, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA. 2L72 4F RTA16WE 20040527000202004052700020NM 2004 5 27 SWAA041390 120040515A53306545877 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT, LOWER FORWARD CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040527000232004052700023NM 2004 5 27 SWAA041393 120040516A53206551698 SPLICE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND STRINGER SPLICES AT BS 908, STRINGER 4R AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20040527000242004052700024 2004 5 27 DL73S040402 420040506A34544034559901 RMI BOEING737 737232 1384475NM COCKPIT SMOKE A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27302DL 23047 NR 2 RMI STARTED TO SMOKE. REPLACED SAME 2L72 4F RTA16WE 20040527000272004052700027NM 2004 5 27 DLM88040405 120040506A52203913359547 CABLE DOUG MD88 MD88 3023688NM TAILCONE UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27957DL 49976 WORKING MSU TO VERIFY TAILCONE RELEASE SYSTEM LOCKING CABLE FOUND ONE CABLE BROKEN REF IPC 53-50-00-25A REPLACED CABLE 2L72 4F RTA6WE 20040527000282004052700028NM 2004 5 27 DL733040406 120040507A261251211 CONTROL UNIT BOEING737 7373B7 1384580NM FWD CARGO BAY MALFUNCTIONED A DALAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 SO27947WP 23376 ON LANDING ROLLOUT WITH AFT CARGO B SYSTEM LOOP INOPERATIVE, GOT FALSE AFT CARGO FIRE INDICATION AND BOTTLE WAS DISCHARGED. AFTER CONFIRMATION THAT NO FIRE EXISITED AIRCRAFT TAXIED TO GATE. REPLACED CARGO FIRE DETECTOR CONTROL UNIT 2L72 4F RTA16WE 20040527000292004052700029NM 2004 5 27 DL76S040407 120040507A2432 CHARGER BOEING767 767332 1382001NM MAIN E&E BAY MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SO27135DL 25145 MAIN BATTERY CHARGER STATUS MSG. REPLACED MAIN BATTERY CHARGER PER M/M, NO HELP. REPLACED MAIN SHIPS BATTERY PER M/M. ALL CKS NORMAL PER M/M. 2L72 4F RTA1NM 20040527000312004052700031NM 2004 5 27 DL76L040410 120040507A5512 SKIN BOEING767 767332 1382001NM HORIZONTAL STAB LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27182DN 25987 FOUND ON ARRIVAL LIGHTING STRIKE AND DAMAGE ON LT HORIZONTAL STAB, L1 DOOR AREA. REPAIRED SAME 2L72 4F RTA1NM 20040527000332004052700033NM 2004 5 27 DL73S040412 120040507A335020131A BATTERY BOEING737 737232 1384475NM EMERGENCY LIGHTSINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27311DL 23083 FWD BULLNOSE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. CHECKS OK. 2L72 4F RTA16WE 20040527000362004052700036NM 2004 5 27 DL75K040415 120040509A3350 FUSE BOEING757 757232 1384965NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO276704Z NA 30396 ON LAYOVER FOUND EMERENGCY EXIT LIGHTS AT FWD RT OVERWING EXIT, OVERHEAD LIGHT AT 20DEF-26ABC-33ABC INOPERATIVE. FOUND BULB SHORTED AT 20DEF AND REPLACED FUSE IN AFT GALLEY BATTERY PACK 2L72 4F RTA2NM 20040527000372004052700037NM 2004 5 27 DL764040416 120040506A3260S238T00626 PSEU BOEING767 767432ER 1385134NM E/E BAY FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27839MH 29712 ON CLIMB OUT GEAR DISAGREE FOLLOWED BY GEAR NOT DOWN CAUTION AND WARNING. AIR RETURN TO LAS. REPLACED PSEU. ALL CHECKS GOOD. 2L72 4F RTA1NM 20040527000382004052700038NM 2004 5 27 DL757040417 120040510A3297 WIRE BOEING757 757232 1384965NM ANTI SKID XDUCERDAMAGED A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27682DA 26958 ANTI-SKID CYCLES ON REPEATEDLY. OVERHEAD ANTI-SKID ILLUMINATED ON STATUS PAGE. NORMAL AND ALT ANTI-SKID ARE ON. RESET C/BS TESTED NORMAL FOR 5 MIN THEN CAME BACK ON. BITE ON ANTI-SKID BOX SHOWS BOX1-5 AND TRANSDUCER NR 1. PULLED OUT TRANSDUCER 1 AND CHECKED WIRING. RED WIRE TO PIN 1 OF TRANSDUCER PLUG BROKEN. REPAIRED WIRING AND REPLACED ANTI-SKID/AUTOBRAKE CONTROL UNIT PER MM OPS CHECKS OK. 2L72 4F RTA2NM 20040527000402004052700040NM 2004 5 27 DLM88040419 120040510A33506011779 RACK DOUG MD88 MD88 3023688NM BATTERY PACK MALFUNCTIONED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27909DE 53418 OVERWING EMERGENCY LIGHTS WOULD NOT SHUT OFF AFTER TEST.REPLACED BATTERY PACK RACK UNIT. OPS NORMAL 2L72 4F RTA6WE 20040527000432004052700043NM 2004 5 27 DL76S040425 120040508A5330141T3331 SKIN BOEING767 767332 1382001NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27119DL 23278 THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP AT FS 340. THE CRACK WAS REMOVED WITH A 4 X 5 INCHES CUTOUT THROUGH BOTH MEMBERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 090194-14, REV A. 2L72 4F RTA1NM 20040527000442004052700044NM 2004 5 27 DL73S040426 120040428A5330 SKIN BOEING737 737232 1384475NM C2 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 3/16 INCH CRACK IN FUSELAGE OUTER SKIN AT C2 DOOR CUTOUT UPPER AFT CORNER , FASTENER REPAIR PER SRM 53-30-3 FIG 6 2L72 4F RTA16WE 20040527000452004052700045EU 2004 5 27 04FDEA01052 120040422A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMPARTMENT, LT SIDE BETWEEN SEAT TRACK 3 AND 4 FROM CENTERLINE AT FR 27 FLOOR PAN PANEL HAS 2 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040527000462004052700046EU 2004 5 27 04FDEA01053 120040422A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC LT SIDE NR 4 SEAT TRACK FROM CENTER LINE JUST FWD OF FR 27, 2 EA AREAS OF CORROSION, UPPER SURFACE. REPAIRED SEAT TRACK NR 4 LEFT FROM FR 26-27 TO FR 27-28 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201. 2L72 4F RTA35EU 20040527000482004052700048 2004 5 27 SWAA041455 420040522A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29524SW 26566 R2 DOOR EVAC SLIDE HIGH PRESSURE INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040527000492004052700049NM 2004 5 27 SWAA041456 120040522A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29717SA 27851 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20040527000502004052700050NM 2004 5 27 SWAA041457 120040522A53146545866 PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C3 CHECK, FOUND RT KEELBEAM PANEL AT BS 700, CRACKED. REPAIRED PANEL PER SRM. 2L72 4F RTA16WE 20040527000512004052700051NM 2004 5 27 SWAA041458 120040522A335065C34691 COVER BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT COVER AT ROW 2 ABC OUT OF POSITION. REPOSITIONED BULLNOSE LIGHT COVER PER MM. 2L72 4F RTA16WE 20040527000532004052700053NM 2004 5 27 SWAA041460 120040523A531565C33940 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 294, RBL 18 TO RBL 50, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. 2L72 4F RTA16WE 20040527000552004052700055NM 2004 5 27 SWAA041463 120040523A3350311500 LENS BOEING737 7375H4 138449DNM ROW 11ABC BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 11 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040527000572004052700057NM 2004 5 27 SWAA041450 120040521A3350101114 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040527000582004052700058NM 2004 5 27 SWAA041451 120040521A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 504, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040527000602004052700060WP 2004 5 27 04FDEA01099 120040424A5751UNK SKIN DOUG DC10 DC1010 3022110WP ZONE 600 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 RT OUTBOARD AILERON INBOARD SIDE HAS SKIN SEPARATING AND CRACKED. VERIFIED MATERIAL ID FOR SKIN .032 INCH 2024-T3 PO 427557.2 AND DOUBLER .040 INCH 2024-T3 PO 434977.1 IAW DC-10 SRM 57-51-01 VOL 3. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIGHT AND BALANCE, AILERON WITHIN 60-110 LIMIT AT 87 INCH POUNDS IAW DC-10 CMM 57-51-02. 2L73 4F A22WE 20040527000632004052700063NM 2004 5 27 SWAA041473 120040524A531565C33940 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 294, RBL 55, CORRODED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040527000652004052700065NM 2004 5 27 SWAA041476 120040524A53116554892 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 303.9, LBL 57.5, CRACKED. REPAIRED FRAME SECTION PER SB. 2L72 4F RTA16WE 20040527000662004052700066NM 2004 5 27 SWAA041478 120040524A531165C25228 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040527000682004052700068NM 2004 5 27 SWAA041466 120040524A3350100031 SIGN BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 AFT ENTRY DOOR EMERGENCY EXIT LENS LOOSE. REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY EXIT SIGN BASE PER MM. 2L72 4F RTA16WE 20040527000692004052700069NM 2004 5 27 SWAA041467 120040524A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 740, STRINGER 18L, BS 792, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040527000702004052700070 2004 5 27 SWAA041468 420040524A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040527000712004052700071NM 2004 5 27 SWAA041469 120040524A5520REP4M6 BEARING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C4 CHECK, RT AND LT ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AND LT ELEVATOR INPUT ROD BEARINGS PER MM. 2L72 4F RTA16WE 20040527000722004052700072NM 2004 5 27 SWAA041453 120040521A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040527000732004052700073NM 2004 5 27 SWAA041454 120040522A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040527000742004052700074NE 2004 5 27 SWAA041464 220040523A7261332A10000XXX ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE LT WING LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW29653SW 28398 725928 ON TAKEOFF FROM SEA HAD AN OILY ODOR WENT AWAY IMMEDIATLEY. ON DESCENT INTO LAS OIL SMELL WAS WORSE. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY PER MM. 2L72 4F4 FRTA16WE E2GL 20040527000752004052700075NM 2004 5 27 SWAA041470 120040524A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT BS 639, STRINGER 2R, STRINGER 3L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040527000772004052700077NM 2004 5 27 SWAA041481 120040524A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 380, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040527000802004052700080EA 2004 5 27 LKL2004F00000 220040430A7200PT6A41 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA LEFT FAILED E LKLAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL1144US 2550 BB56 PCE80104 AIRCRAFT WAS IN CRUISE FLIGHT AT 26,000 FT WHEN PILOT HEARD A BANG FROM THE LT ENGINE. THE LT ENGINE CAME TO A STOP AND THE PILOT PERFORMED A SINGLE ENGINE LANDING WITH OUT INCIDENT. INITIAL OBSERVATION BY THE PILOT SHOWED METAL FLAKES IN THE EXHAUST AND OIL SPILLING ON THE GROUND. THE ENGINE WAS REMOVED AND SENT FOR EXAMINATION. 1L72 4T4 T A24CE E4EA 20040524001292004052400129 2004 5 24 SWAA041285 420040506A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040524001312004052400131NM 2004 5 24 SWAA041287 120040506A30405717623122 WINDOW BOEING737 7373H4 1384600NM COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29613SW 27931 IN FLIGHT THE R2 WINDOW ARCED, COMPLIED WITH QRH. REMOVED AND REPLACED R2 WINDOW PER MM. 2L72 4F RTA16WE 20040524001332004052400133 2004 5 24 SWAA041289 420040507A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED RON, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040524001352004052400135NM 2004 5 24 SWAA041291 120040507A55116547994 RIB BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB L/E RIB AT STAB STA 243, CRACKED. REMOVED AND REPLACED HORIZONTAL STAB RIB PER SRM. 2L72 4F RTA16WE 20040524001372004052400137NM 2004 5 24 SWAA041293 120040507A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED C3 CHECK, FOUND RT AFT END EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040524001392004052400139NM 2004 5 24 SWAA041295 120040507A3397145005920 WIRE BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT AT R1 DOOR, INOP. SECURED GROUND WIRE PER MM. 2L72 4F RTA16WE 20040524001412004052400141NM 2004 5 24 SWAA041297 120040507A53146561215 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO KEELBEAM WEB AT BS 807 TO BS 827, RBL 7, CORRODED. REMOVED AND REPLACED KEEL BEAM WEB PER SRM. 2L72 4F RTA16WE 20040524001752004052400175EU 2004 5 24 KBM2004F00112 120040220A21200500847 MOTOR SNIAS 350 AS350B2 8680813EU CONDENSER BLWR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH3284 2884 CONDENSOR BLOWER INOPERATIVE. QUIT DURING GROUND RUN. REMOVED AND REPLACED. 1G71 3U H9EU 20040524001772004052400177EU 2004 5 24 KBM2004F00108 120040310A6730SC5084 SERVO SNIAS 350 AS350B2 8680813EU FLT CONTROLS LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19751H 3403 SERVO UNIT IS LEAKING. REMOVED AND REPLACED. 1G71 3U H9EU 20040524001802004052400180GL 2004 5 24 109050504 220040505A7200 ENGINE AGUSTAA109 A109 0260109EU ALLSN 250C 250C20B 03013GL NR 1 SMOKE B JBZRA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP2721RX 6012 817 7131 CAE820563 AFTER LANDING AT A REMOTE FIRE STATION TO PICK UP A PATIENT, THE CREW CHIEF NOTICED HEAVY WHITE SMOKE COMING FROM THE NR 1 ENGINE EXHAUST. THE AIRCRAFT WAS SHUT DOWN AND REMAINED ON SIGHT OVERNIGHT. THE FOLLOWING DAY MAINTENANCE CONFIRMED THE PROBLEM AND THE ENGINE WAS REPLACED. THE ENGINE WAS RETURNED TO THE OVERHAUL VENDER AND AS YET NO CAUSE HAS BEEN REPORTED. THE ENGINE HAD 817.5 TSO AND HAD AN ENHANCED TURBINE. 1G72 3U3 U H7EU E4CE 20040524001962004052400196WP 2004 5 24 ARWA20040502 120040505A7997NPN WIRE DOUG DC8 DC863F 302198FWP NR 1 ENGINE DAMAGED A ARWAO OTHER N FALSE WARNING CRCRUISE 1 SO19784AL 46135 NR 1 OIL TEMPERATURE ERRATIC AND UNREALIABLE IN-FLIGHT. REPAIRED WIRE AT PIN U NR 1 ENGINE PYLON MAIN DISCONNECT PLUG IN ACCORDANCE WITH DACO DC-8 MM 20-50-1. RAN ENGINE FOR 20 MINUTES. OPERATIONAL CHECK GOOD IAW DACO DC-8 MM 71-00-00 2L74 4F 4A25 20040524001982004052400198EA 2004 5 24 QXEA200400301 120040505A261147359719 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAK NONE N FALSE WARNING ININSP/MAINT 1 NM09607QX477 59 10024 FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR. 2L72 4F RTA21EA 20040525000022004052500002NM 2004 5 25 QXEA200400306 120040505A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09415QX 4081 GOUGE IN SKIN INBOARD OF STRINGER 32 AT STATION 68.8. REPAIRED IAW Q400 TASK 53-10-31-350-802. 2H72 4T RTA13NM 20040525000052004052500005WP 2004 5 25 LO62004F00000 120040506A242028E04 GENERATOR CVAC 340 34032 2422706WP PWA R2800 R2800* 52026NE LEFT INOPERATIVE D LO6BO OTHER O OTHER NRNOT REPORTED 1 SW173427 90 LEFT AC GENERATOR OPERATION INTERMITTENT AND UNSTEADY IAW VOLTMETER. REPLACED GEN WITH OVERHAULED UNIT. 2L72 4R4 R 6A6 5E8 20040525000072004052500007CE 2004 5 25 KZ52004F00000 120040506A792153E22144 VALVE CESSNA150 150J 2071820CE LYC O720 IO720A1B 41546EA OIL COOLER INOPERATIVE D KZ5RO OTHER O OTHER NRNOT REPORTED 1 GL155078626 15069552 PILOT REPORTED HIGH OIL TEMP 210 DEGREES-220 DEGREES F., REMOVED VALVE AND TESTED SIDE BY SIDE WITH NEW VALVE, OLD VALVE DID NOT CLOSE AT THE SAME REATE AS NEW VALVE AND OIL TEMP DECREASED TO. 1H71 3O3 O 3A19 1E15 20040525000132004052500013NM 2004 5 25 SWAA041347 120040511A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29434WN 32454 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXTERIOR EXIT LIGHT AT R2 DOOR INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040525000172004052500017NM 2004 5 25 SWAA041331 120040511A3350900835A BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 EEPLS LIGHTS ILLUMINATED EN ROUTE. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2L72 4F A16WE 20040525000532004052500053EA 2004 5 25 VNAA0405003 120040502A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ADC NR 1 FALSE ACTIVATIONA VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07247JS17 7922 DURING TAKEOFF, THE CREW RECEIVED AN ADC NR 1 FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AIR REFERENCE PANEL IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040525000572004052500057EA 2004 5 25 VNAA0405007 120040511A4930N6421073 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU FUEL FAILED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL07249PS 7926 APPROXIMATELY 20 MINUTES FROM PHL, THE CREW RECEIVED A FUEL IMBALANCE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND SHUTDOWN THE LEFT HAND ENGINE AND LANDED AT PHL. MECHANICS WERE SENT FROM DAY. MAINTENANCE THEN INSPECTED AND REPLACED THE APU PUMP IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040525000692004052500069NM 2004 5 25 04FDEA01188 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.405 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040525000702004052500070NM 2004 5 25 04FDEA01190 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.405 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040525001072004052500107EA 2004 5 25 SWIA200413282 120040506A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 NM07410SW 7066 ON DESCENT INTO SLC THE A/C PITCHED UP AND GAVE A AP PITCH TRIM & NOSE UP TRIM CAUTION. STAB TRIM AND MACH TRIM DROPPED OFF 3 TIMES. NOTE: WITH AUTO PILOT OFF THE TRIM WAS NOT MOVING AND THE STAB TRIM KICKED OFF. REMOVED AND REPLACED THE HSTCU IAW MM 27-41-01. OPERATION CHECKS SATISFACTORY AT THIS TIME. NO DEFECTS NOTED. S/N OFF: 175. 2L72 4F RTA21EA 20040525001082004052500108EA 2004 5 25 QXEA200400307 120040508A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 700 MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09602QX2077 133 10010 AIRCRAFT RETURNED TO FIELD FOR GEAR DID NOT RETRACT AFTER TAKEOFF. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR SELECT VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040525001122004052500112NM 2004 5 25 P5CA0401090 120040509A793141809104 TRANSMITTER BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 4 ENG OIL MALFUNCTIONED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23453PA 30811 706365 NR 4 ENGINE OIL PRESSURE 155 PSI AT IDLE POWER, WITH POWER INCREASE OIL PRESSURE REMAINS HIGH. REMOVED AND REPLACE NR 4 ENGINE OIL TRANSMITTER IAW AMM 79-32-01. OPS CHECK & LEAK CHECK OK. 2L74 4F4 FRTA20WE E23EA 20040525001212004052500121 2004 5 25 BAQA094574 420040514A221041600297006 AUTOPILOT SYS UROCOPEC135 EC135P2 5620027EU COCKPIT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03703ME26 0314 UNIT REMOVED DUE TO AUTOPILOT HARD FAILURE. REPLACED WITH SERVICABLE UNIT. 05/19/2004 1G72 3U H88EU 20040526000012004052600001NE 2004 5 26 CP22004F00000 220040331A853011640 CYLINDER DAMPER NAMER T6 AT6G 6400434CE PWA R1340 R1340AN1 52016NE ROCKER BOX CRACKED B CP2RO OTHER O OTHER NRNOT REPORTED 1 SW155115D 60 493330A 20218 A CRACK STARTED AT EXHAUST VALVE ROCKER SHAFT BUSHING AND PROCEEDED AROUND THE FRONT SIDE OF ROCKER BOX CASTING AND AFT TO THE VALVE COVER PARTING SURFACE. THIS WAS UNDER NORMAL OPERATING CONDITIONS. 1L71 3R3 R A2575 5E2 20040526000072004052600007SO 2004 5 26 SIMA200406805 120040306A335014532341401 MODULE EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21820AE 145576 NOTIFIED BY MAINTENANCE, EMERGENCY LIGHTS DO NOT TURN OFF AFTER F/A TESTS WITH BATTERIES ON AND EMERGENCY LIGHT ARMED ALSO SHOWING 'EMER LT NOT ARMED' ON EICAS. REPLACED EMERGENCY LIGHT OVERHEAD PANEL MODULE ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20040526000142004052600014EA 2004 5 26 ASOA04289 120040422A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURNG AN A-CHECK IN BTR, THE LT AND RT FS 640 AT BL 45 DOUBLERS WERE FOUND CRACKED. UPON REMOVAL OF THE DOUBLERS MAINTENANCE FOUND FS 640 AT BL 45 TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMVOED AND REPLACED FS 640 AT BL 45. (M) 2L72 4F RTA21EA 20040526000282004052600028CE 2004 5 26 2004F00143 120040316A3260404EN876 SWITCH LEAR 35 35A 5170602CE RT MLG FAILED A DELAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 CE03360LJ 360 DURING TAXI, WITH ANTI-SKID SYSTEM ON, HYDRAULIC PRESSURE WAS PRESENT BUT NO BRAKING ACTION OCCURRED. FURTHER INVESTIGATION REVEALED THAT THE RIGHT MLG DOWN SAFETY SWITCH FAILED. SWITCH REPLACEMENT CORRECTED THE PROBLEM. (M) 2L72 4F A10CE 20040526000302004052600030SO 2004 5 26 SIMA200409901 120040407A1430 CONNECTOR EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT LOOSE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21832AE 145627 EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE AT SEAT 16A, ISSUED MEL 33-27. FOUND CONNECTION OF STRIP LIGHTING LOOSE. RE-SECURED AS REQUIRED IAW EMB AMM, MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040526000372004052600037NM 2004 5 26 SWAA041371 120040513A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040526000412004052600041NM 2004 5 26 SWAA041364 120040513A5314656215 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND KEELBEAM AT BS 727 - 19, STRINGER 27R, AND BS 727 + 9, STRINGER 27L, CORRODED. REPAIRED KEEL BEAM PER EA. 2L72 4F RTA16WE 20040526000422004052600042 2004 5 26 SWAA041365 420040513A25656557463 FITTING BOEING737 7373H4 1384600NM L2/R1 DOORS CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND L2 AND R1 DOOR EVAC SLIDES FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED EVAC SLIDE GIRT BAR FITTINGS PER MM. 2L72 4F RTA16WE 20040526000432004052600043NM 2004 5 26 SWAA041366 120040513A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND RT MLG WHEEL WELL CEILING BEADED PRESSURE WEB AT BS 671, RBL 41, CRACKED. REPAIRED RT MLG PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20040526000462004052600046NM 2004 5 26 SWAA041352 120040512A3350101114 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F A16WE 20040526000492004052600049NM 2004 5 26 SWAA041355 120040512A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 986, RBL 43, CORRODED. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20040526000642004052600064NM 2004 5 26 04FDEA01058 120040422A5310 BEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 CORROSION STA 780 DELTA BEAM LWR ANGLE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS BS 780 DELTA BEAM LWR ANGLE. ACCESS LWR WEB. REMOVED, INSTALLED NEW BS 780 DELTA BEAM LWR ANGLE AND INSTALLED LWR WEB SUPPORT BEACON PANEL IAW SRM 51-30-2, 51-10-6 STEP 7, 51-10-1 FIG 1, 51-30-5. 2L73 4F RTA3WE 20040526000782004052600078EU 2004 5 26 BAQA094575 120040506A6730L673M40A1001 ACTUATOR UROCOPEC135 EC135T1 5620026EU TAIL ROTOR UNSERVICEABLE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03511ME823 0143 EXCESSIVE PLAY IN BEARING ON CONTROL ROD. REPLACED WITH SERVICABLE UNIT. 05/19/2004 1G72 3U H88EU 20040526000822004052600082EU 2004 5 26 BAQA094100 120040430A243245033502 BATTERY UROCOPEC135 EC135T1 5620026EU MASTER MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03582AE1713 0298 NR 1 ENGINE GENERATOR WILL NOT CONNECT UNTIL NR 2 ENGINE AT IDLE. CORE S/N 1092 WAS CANNED OFF OF A/C 0278 ON 01/20/04 AND INSTALLED ON 0298 AT A/C TT 11.4 REPLACED WITH SERVICABLE UNIT FROM AEC, 05/21/2004 1G72 3U H88EU 20040526000832004052600083EU 2004 5 26 BAQA094505 120040426A6340L771M40C1014 INDICATOR UROCOPEC135 EC135T1 5620026EU TRIPLE TACH STICKING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03582AE181 0298 HR NEEDLE STICKS. REPLACED WITH SERVICABLE UNIT. 05/24/2004 1G72 3U H88EU 20040526000852004052600085NM 2004 5 26 04FDEA01106 120040428A5753ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND O/B FLAP, I/B FWD HINGE BARREL NUT HOLE 2B MATING SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040526000872004052600087NM 2004 5 26 04FDEA01108 120040428A5753ARC050213 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND O/B FLAP, I/B FWD HINGE, ACTUATOR HOLE 8 I/B CORRODED. COMPLIED WITH FEDEX EA 1-5750-76028, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040526000932004052600093NM 2004 5 26 04FDEA01081 120040424A5753ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE LOWER MOUNT HOLE 7 MATING SURFACE CORRODED. RIGHT WING, OUTBOARD FLAP, INBOARD FWD HINGE LOWER MOUNT HOLE NR 7 MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08, AND FOUND WITHIN LIMITS AS PER DWG ARC 0502. 2L73 4F RTA22WE 20040526001102004052600110NM 2004 5 26 04FDEA01306 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002, REMAINING THICKNESS: 0.501. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001152004052600115EU 2004 5 26 04FDEA01254 120040513A2720 ACTUATOR AIRBUS300 A300F4605R 3930327EU RUDDER FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25669FE 774 DURING FLAP/SLAT RETRACTION AFTER TAKEOFF, SYSTEM 1 & 2 RUDDER TRAVEL FAULT LIGHTS ILLUMINATED. SELECTED BOTH OFF, WAITED ONE MINUTE AND TRIED RE-SET. LIGHTS RE-ILLUMINATED SELECTED BOTH SWITCHES OFF. FAULT LIGHTS STAYED OUT. FOLLOWED QRH AND RETURNED TO TAKEOFF AIRPORT. UPON FURTHER T/S FOUND THAT THE STOP VARIABLE ACTUATOR WAS BAD. REMOVED AND REPLACED ACTUATOR PER M/M 27-23-23-4, PERFORMED ADJUSTMENT/TEST PER M/M 27-23-00-5 AND ALL SYSTEMS CHECK GOOD AT THIS TIME. 2L72 4F RTA35EU 20040526001182004052600118WP 2004 5 26 04FDEA01257 120040513A5713ARB21762 STRINGER CLIP DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT WING STRINGER TO RIB TIE CLIP CRACKED INSIDE 634 AT- S 37. REMOVED AND REPLACED CLIP IAW SRM 51-31-01 AND SRM 51-33-01 AT MAE. 2L73 4F A22WE 20040526001242004052600124WP 2004 5 26 04FDEA01263 120040513A5720FXARL05008 CHANNEL DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED IN 2 PLACES AT XORS 738 INSIDE PANEL 636BB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040526001452004052600145NM 2004 5 26 2004UALA00427 120040502A5320 BRACKET BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSLEAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOORBEAM FWD SIDE PULLEY BRACKET SUPPORT ANGLE AT LBL 4 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT ANGLE. 2L72 4F4 FRTA1NM E24NE 20040526001592004052600159EA 2004 5 26 SWIA200413293 120040503A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 RT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED DAMAGE AND INSTALLED REPAIR PARTS DOUBLER AND FILLER IAW REO 601R-57-51-046 REPAIR 1. 2L72 4F RTA21EA 20040527000152004052700015NM 2004 5 27 SWAA041385 120040514A5530 CLEVIS BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB REAR SPAR CLEVIS FWD AND AFT LUG FACES, CORRODED. REPAIRED VERTICAL STAB PER ER. 2L72 4F RTA16WE 20040527000212004052700021NM 2004 5 27 SWAA041391 120040516A335010107451 LENS BOEING737 7375H4 138449DNM EXIT SIGN LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29521SW 25320 RT OVERWING EMERGENCY EXIT SIGN LENS, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040527000252004052700025NM 2004 5 27 DL73G040403 120040506A335081 BULB BOEING737 73735B 13844BMNM LT OVERWING INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27225DL 25069 LEFT OVERWING EMERGENCY LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SAME PER A.M.M. - OPS CKS GOOD 2L72 4F RTA16WE 20040527000302004052700030NM 2004 5 27 DL76S040408 120040506A5330141T33315 SKIN BOEING767 767332 1382001NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27119DL 23278 CRACK REPAIR THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A 5 X 4 INCHES CUTOUT THROUGH BOTH LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 090194-14. 2L72 4F RTA1NM 20040527000342004052700034NM 2004 5 27 DLM88040413 120040509A7930 INDICATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ENG OIL SYSTEM MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27964DL 49983 726931 PASSING 20K LT ENGINE OIL QTY DECREASED ALL THE WAY TO ZERO. ENGINE POWER REDUCED TO IDLE.ON DECENT ALL INDICATIONS RETURNED TO NORMAL. CHECKED OIL AT TANK, FULL. INSPECTED OIL TEMP DECALS AND EXAUST AREA, OK. CREW REPORTED OIL PRESSURE DID NOT DECREASE. A/C OK FOR CONTINUED SERVICE. FWD LT ENGINE OIL QTY INDICATION DEFERRED PER MEL 79-00-03. 2L72 4F4 FRTA6WE E9NE 20040527000422004052700042NM 2004 5 27 DL73S040422 120040511A5311VARIOUS FRAME BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 MULTIPLE FRAMES WERE FOUND TO BE DENTED IN THE FWD CARGO BIN AREA. THE DENTED FRAMES ARE LOCATED BETWEEN BS 400 AND 440. THE DAMAGE WAS DISPOSITIONED AS PER INSTRUCTIONS IN ERA 090192-14. 2L72 4F A16WE 20040527000472004052700047WP 2004 5 27 04FDEA01091 120040424A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 MAIN CABIN SEAT TRACK AT LBL 107, FS 1476-1479 CORROSIN CENTER OF TRACK. REMOVE CORROSION IAW DC-10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS, MATERIAL FOR NEW CHANNEL 7075 T651, .750 PLATE, PO 401641.2 AND FABRICATED CHANNEL IAW DC-10 SRM 53-70-00 VOL 1. INSTALLED REPAIR CHANNEL IAW DC-10 SRM 51-31-01 VOL 1. 2L73 4F A22WE 20040527000542004052700054NM 2004 5 27 SWAA041462 120040523A575465C26602 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F RTA16WE 20040527000562004052700056NM 2004 5 27 SWAA041449 120040521A3350101114 LAMP BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 RT RED OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM. 2L72 4F A16WE 20040527000612004052700061NM 2004 5 27 SWAA041471 120040524A55306552490 BEAM BOEING737 7373H4 1384600NM RUDDER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND VERTICAL STAB T/E BEAM AT LT RUDDER STATION 13.3 TO RUDDER STATION 121.64, CRACKED. REMOVED AND REPLACED VERTICAL STAB BEAM PER SRM. 2L72 4F RTA16WE 20040527000622004052700062NM 2004 5 27 SWAA041472 120040524A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 440, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040527000672004052700067NM 2004 5 27 SWAA041465 120040523A5311907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX AFT LEG, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR UPPER HINGE PER EA. 2L72 4F RTA16WE 20040527000792004052700079CE 2004 5 27 WTW2004F00000 120040512A71119632405535 CHANNEL BEECH 58 58 1152740CE CONT O520 IO520* 17032SO COWL FLAP BROKEN D WTWAO OTHER O OTHER NRNOT REPORTED 1 GL13666198388 TH1070 PILOTS REPORTED COWL FLAP HANDLE BROKE IN THEIR HAND WHEN THE COWL FLAPS WERE CLOSED. INSPECTION REVEALED THE LEVER PN 96324055-33 WORE AGAINST THE DETENT PLATE PN 96-324055-163 AND CUT A GROOVE IN THE LEVER. FURTHER INSPECTION REVEALED THE CHANNEL PN 96-324055-35 HAD CRACKED IN 3 PLACES. THE OTHER LEVER HAD A WEAR MARK STARTING IN IT FROM THE DETENT PLATE. 1L72 3O3 O 3A16 E5CE 20040527000812004052700081CE 2004 5 27 JZ22004F00000 120040421A3230H111499 SWITCH CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP MLG INTERMITTENT B JZ2RA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL03600JD 6500236 AFTER TAKEOFF, GEAR HANDLE COULD NOT BE MOVED TO THE (GEAR UP) POSITION. AIRCRAFT RETURNED TO DEPARTURE POINT AND LANDED UNEVENTFULLY (MLI). MAINTENANCE STAFF JACKED AIRCRAFT AND ATTEMPTED TO RETRACT GEAR. GEAR HANDLE COULD NOT BE RAISED, DUPLICATING THE CONDITION FOUND IN THE AIR. THE NOSE WHEEL WAS MOVED LT AND RT AND THE NOSE GEAR CENTERING SWITCH ACTUATED CAUSING A RELAY TO ENERGIZE THAT WAS AUDIBLE TO MAINTENANCE STAFF. GEAR HANDLE COULD THEN BE RAISED TO THE (GEAR UP) POSITION AND THE GEAR RETRACTION SEQUENCE FUNCTIONED NORMALLY. THE NOSE GEAR CENTERING SWITCH WAS REPLACED AND THE RETRACTION SEQUENCE TESTED IN VARIOUS SIDE LOAD CONDITIONS AND FUNCTIONED FLAWLESSLY. 2L72 4F4 F A9NM E6WE 20040527000842004052700084NM 2004 5 27 SCNA04007 120040504A3350D71701100 BATTERY PACK BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15806SY 28215 FORWARD LEFT BATTERY PACK FOR EMERGENCY LIGHTS DEAD 2L72 4F RTA16WE 20040527000852004052700085SO 2004 5 27 RAIA00405003 120040507A272015793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO RUDDER INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03814HK 145046 CREW REPORTER RUDDER 1/2 FAIL INDICATION AND WHEN RUNNING CHECK LIST FELT ABRUPT YAW WHEN SYSTEM TURNED OFF, DID NOT REENERGIZE RUDDER HYDRAULIC SYSTEM AND RETURNED TO STL. MAINTENANCE INSPECTED THE RUDDER INTERCONNECT RODS IN THE RUDDER AREA WITH NO DEFECT NOTED. REMOVED AND REPLACED RUDDER SYSTEM 2 PRESSURE SWITCH. 2L72 4T RTT00011AT 20040527000862004052700086SO 2004 5 27 RAIA00405004 120040508A32608005701 SQUAT SWITCH EMB 145 EMB145LR 3260212SO LT MLG MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03815HK18 145048 LANDING GEAR DID NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MLG WOW SWITCH AND OPS CHECKED GOOD DURING RETRACTION CHECK. 2L72 4T RTT00011AT 20040527000892004052700089EU 2004 5 27 MALA040387 120040508A2930IPT6110003000S TRANSDUCER SAAB SF340 340B 7860101EU HYD PRESSURE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15366PX 340B267 SHORTLY AFTER T/O CLIMBING THROUGH ABOUT 6000 FT GOT HYD CAUTION LIGHT ON CWP TURNED PUMP OFF NOTICED MAIN WAS NORMAL EMERG WAS LOW DOWN TO ALMOST 0 QTY AND O/B INDICATORS WAS NORMAL ABOUT A MIN TO 90 SEC IT STARTED TO PUMP BACK UP JUMPING UP NAD DOWN THEN BACK TO NORMAL. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED EMERG ACC PRESSURE TRANSDUCER IAW AMM 29-32-05-4 OPS CHECKS GOOD PN IPT61-1000-3000SG SN OFF 645-8-175 SN ON 560-7-264. 2L72 4T RTA52EU 20040527000902004052700090EU 2004 5 27 MALA040385 120040507A242031342003 GENERATOR SAAB SF340 340B 7860101EU LEFT AC FAILED A MALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15416XJ 340B416 DURING TAXI OUT, LT AC GEN FAILED TO COME ON LINE. PAX REPORTED SMOKE AND FLAMES EXIT A/C OF EXHAUST HOLE. A/C RETURNED TO GATE. MAINTENANCE REPLACED LT AC GEN. ALL CHECKS GOOD DONE IAW SF340MM CHAP 24. 2L72 4T RTA52EU 20040527000912004052700091EU 2004 5 27 MALA040386 120040508A3320 SOCKET SAAB SF340 340B 7860101EU CABIN LIGHTS BURNED A MALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15364PX 340B262 AT DEPARTURE CREW REPORTED SMOKE COMING FROM SIDEWALL AREA AROUND ROW 9. MAINTENANCE FOUND BAD LIGHT SOCKET. REMOVED SOCKET AND CAP AND STOWED WIRING. DEFERRED SIDEWALL LIGHT. 2L72 4T RTA52EU 20040527000932004052700093EA 2004 5 27 COMA0460304 120040508A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01916CA18859 7014 FLIGHT 5851 GEAR DISAGREE WARNING, COULD NOT DUPLICATE. REPLACED THE NLG DOORS SELECTOR VALVE. 2L72 4F RTA21EA 20040527000942004052700094EA 2004 5 27 COMA0460305 120040508A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01957CA21055 7109 FLIGHT 5417 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20040527000952004052700095EA 2004 5 27 COMA0460306 120040510A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01934CA12751 7042 FLIGHT 5050 RT WINDSHIELD CRACKED. REPLACED WINDSHIELD 2L72 4F RTA21EA 20040527000982004052700098NM 2004 5 27 CALA0400486 120040511A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714219 28781 INSPECTION FOUND THE EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06-960-805. 2L72 4F RTA16WE 20040527000992004052700099NM 2004 5 27 CALA0400487 120040510A3230UNK CABLE BOEING737 7373T0 1384582NM MLG OUT OF ADJUST A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2718350 23588 THE GEAR HANDLE WOULD NOT MOVE BEYOND THE OFF POSITION WHEN RAISING GEAR AFTER TAKEOFF FROM EWR. THE GEAR WAS CYCLED AND RETRACTION WAS NORMAL. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE TELEFLEX CABLE OUT OF ADJUSTMENT. THE CABLE WAS ADJUSTED IAW MM 27-65-51. AN ADJUSTMENT/TEST OF THE AIR/GROUND SENSORS WAS PERFORMED IAW MM 32-09-01. THE GEAR WAS CYCLED SEVERAL TIMES AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040527001002004052700100NM 2004 5 27 CALA0400488 120040511A7830315A100138 SLEEVE BOEING737 737524 1384721NM THRUST REVERSER CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714664 28925 INSPECTION FOUND A 1.6" CRACK IN I/B THRUST REVERSER SLEEVE. THE SLEEVE WAS REPAIRED IAW SRM 51-70-17. 2L72 4F RTA16WE 20040527001032004052700103NE 2004 5 27 COMA0460310 220040506A7200CF343A1 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT OVERTEMP A COMAC ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 SO01403CA9771 7428 807635 FLIGHT 5678 LT ENGINE ITT OVERTEMP DURING T/O. REPLACED LT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040527001052004052700105NM 2004 5 27 QXEA200400312 120040505A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNSECURE A QXEAC ABORTED TAKEOFF WJ INADEQUATE Q C WARNING INDICATION TOTAKEOFF 1 NM09400QX7012 4030 SEA - FLIGHT 2442 - THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WHEN A BAGGAGE DOOR WARNING WAS RECIEVED. MAINTENANCE INSPECTED THE AIRCRAFT AND BAGGAGE DOOR AND FOUND THE BAGGAGE DOOR HANDLE NOT SECURE. THE DOOR HANDLE WAS SECURED PROPERLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040527001072004052700107NM 2004 5 27 04FDEA01010 120040421A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001092004052700109NM 2004 5 27 04FDEA01012 120040421A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019, TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001132004052700113NM 2004 5 27 04FDEA01019 120040422A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001152004052700115WP 2004 5 27 04FDEA01101 120040424A5522 SKIN DOUG DC10 DC1010 3022110WP ZONE 600 ERODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 RIGHT HAND OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUT OUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1. 2L73 4F A22WE 20040527001182004052700118EU 2004 5 27 04FDEA01051 120040422A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC 3RD SEAT TRACK FROM CENTERLINE JUST FWD OF FR 27 ONE EA AREA OF SURFACE CORROSION UPPER SURFACE. REPAIRED SEAT TRACK 3 LEFT FR 26-27 TO FR 27-28 AE PER A300-600 FREIGHTER SRM 53-10-16 PARA 4 FIG 201. 2L72 4F RTA35EU 20040527001192004052700119EU 2004 5 27 04FDEA01045 120040422A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC FLOOR PAN PANEL BETWEEN SEAT TRACKS 1 AND 2 RT OF CENTERLINE FR 25 HAS CORROSION. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040528000012004052800001EU 2004 5 28 YENA200417 120040313A33509BG40450300 HOUSING AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE CABIN DEFECTIVE A YENAK NONE O OTHER UKUNKNOWN 1 EA15564JB 2020 LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. FOUND RECEPTACLE AT FAULT. REPLACED LIGHT HOUSING ASSY. 2L72 4F4 FRTA28NM E311NE 20040528000032004052800003NM 2004 5 28 DL764040429 120040511A2140283137 HEATER BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE CABIN ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27828MH 29699 HEATER AT 2L GIVES OFF BURNING RUBBER SMELL. WENT AWAY WHEN CB WAS PULLED, C FWD TO MCO HEATER DEACT. ETOPS CATEGORY (E) PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F4 FRTA1NM E13NE 20040528000042004052800004NM 2004 5 28 DL73S040430 120040512A5753 SKIN BOEING737 737232 1384475NM PWA JT8 JT8D* NE T/E FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 NR 2 AFT FLAP AFT SKIN SEPARATED/DELAMINATED AT IB END. REPAIRED IAW SRM 51-40-20 FIG 10. 2L72 4F4 FRTA16WE E2EA 20040528000052004052800005NM 2004 5 28 DLM88040431 120040512A2910 HYDRAULIC LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE HYD SYSTEM LOOSE A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27981DL 53268 718140 RT HYD SYS QUANTITY DROPPED TO ONE WITH GOOD PRESSURE INDICATED. SHUTOFF RT ENGINE DRIVEN PUMP AND EXECUTED MANUAL GEAR EXTENSION AND EMERGENCY LANDING. FOUND RIGID LINE LEAKING ON RT ENGINE HYDRAULIC PUMP. TIGHTENED SAME LEAK, CKS GOOD. 2L72 4F4 FRTA6WE E9NE 20040528000072004052800007NM 2004 5 28 DL73S040434 120040513A335020131A BATTERY PACK BOEING737 737232 1384475NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27323DL 23095 R1 EXIT DOOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2L72 4F RTA16WE 20040528000102004052800010NM 2004 5 28 DHL2004781003 120040522A33501000679 LIGHT BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01781DH 21996 EXIT LIGHT OVER L1 DOOR INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT OVER L1 DOOR IAW MM 33-50-101. OPS CHECKED NORMAL. 2L73 4F4 F A3WE E2EA 20040528000122004052800012NM 2004 5 28 C1HA200483008 120040522A5751 STRUCTURE BOEING727 7272S7 138407ZNM LT AILERON DENTED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15683CA 22490 LT IB AILERON, DENTS BEYOND SRM LIMITS IAW SRM HOT BOND REPAIR, WEIGH AND BALANCE REQUIRED. 2L73 4F A3WE 20040528000132004052800013NM 2004 5 28 C1HA200492014 120040522A5320 BEAM BOEING727 727212 138407GNM PWA JT8 JT8D* NE FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 FS 1183 LBL 36 CRACK IN VERTICAL BEAM. 2L73 4F4 F A3WE E2EA 20040528000142004052800014NM 2004 5 28 C1HA200483007 120040522A5751 WEDGE BOEING727 7272S7 138407ZNM LT AILERON DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15683CA 22490 LT OB AILERON, TRAILING EDGE WEDGE DELAMINATED, REPLACED LOWER SKIN, 8110-3 ISSUED. 2L73 4F A3WE 20040528000152004052800015WP 2004 5 28 0400879868 120040520A27805919526507 DUCT DOUG DC9 DC951 3022051WP L/E SLAT LACK OF LUBE A NWAAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL01777NC 47787 FLIGHT CREW NOTICED A LT ROLLING MOTION AFTER SLAT EXTENSION ALONG WITH A SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PROCEDURES AND NORMAL HYDRAULIC PRESSURE OF 3000 PSI WAS CONFIRMED. CAPTAIN DECLARED AN EMERGENCY WITH ATC, HAD CFR CALLED OUT, AND ACCOMPLISHED A 40 DEGREE FLAP AND NO SLAT LANDING AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND A (T) DUCT CHATTERING AND LUBRICATED ALL (T) DUCTS ON THE AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20040528000162004052800016SO 2004 5 28 CHQA000498 120040523A3097 WIRE EMB 135 EMB135KL 3260302SO ANTI-ICE SYSTEM BURNED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11371 145535 RECEIVED A PITOT 3 INOP EICAS MSG IN THE PROCESS OF COMPLETING THE QRH CHECKLIST. WE SMELLED A DISTINCT ELECTRICAL BURNING SMELL. AT THAT POINT THE FLIGHT ATTENDANT NOTIFIED US OF SMOKE IN THE CABIN AREA. WE DECLARED AN EMERGENCY AND LANDED. MAINTENANCE INVESTIGATED THE CAUSE OF THE SMOKE AND REPORTED THE FOLLOWING. AFTER REMOVAL OF K57 RELAY, FOUND SOCKET XK0057 CHARRED AT PINS C1 AND X1 AND A1 HEAT DAMAGED WIRE W102-0268-16 BURNED REF EMB WM 30-31-50, REPLACED WIRE IAW EMB 145 AMM 20-00-05 AND SOCKET IAW EMB 145MM 20-50-01. T/S RELAY K58 FOUND X1 AND X2 SHOWED OPEN MIN 260-2. REPLACED RELAYS K57 AND K58 IAW EMB 145MM 20-13-02. OPS CHECK GOOD. 2L72 4F RTT00011AT 20040528000212004052800021 2004 5 28 ARWA20040506 420040521A34222589201901 GYRO DOUG DC8 DC862 3021970WP PWA JT3D JT3D* 52039NE COCKPIT FAULTY A ARWAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19810BN 45905 CAPTAIN'S COMPASS FAILED IN FLIGHT. REMOVED AND REPLACED CAPTAIN'S PICTORIAL DEVIATION INDICATOR (PDI) AND DIRECTIONAL GYRO (DG) IAW MM 31-10-1 AND MM 34-21-1. SWAPPED INSTRUMENT AMPS IAW 34-00. SYSTEM GROUND TEST NORMAL IAW 34-21-0, 34-52-0 AND 34-28-0. 2L74 4F4 F 4A25 1E8 20040528000232004052800023EU 2004 5 28 MALA040410 120040506A3350 BATTERY PACK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 BATTERY PACK (PN 61-0478-9) SN ON /OFF 010, WAS REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. UNIT WAS RECHARGED AND SUBSEQUENTLY CAPACITY CHECK PASSED. UNIT WAS TESTED IAW CONN AND RETURNED TO SERVICE 5/13/04. 2L72 4T4 TRTA52EU E8NE 20040528000252004052800025EU 2004 5 28 MALA040408 120040505A3350330131 BATTERY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 UNIT FAILED ON WING SCHEDULED CAPACITY CHECK. BATTERY POWER SUPPLY PN 3301-31 SN/2009 BATTERY FAILED CAPACITY CHECK ON BENCH. MAINTENANCE REMOVED AND REPLACED BATTERY ASSEMBLY PN 3301-31. UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 5/7/2004. 2L72 4T4 TRTA52EU E8NE 20040528000282004052800028NM 2004 5 28 PCAA0405209 120040524A323282910016009 ACTUATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NLG DOOR FAULTY A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13812EX31495 312 FLIGHT NR 3845 REPORTED NOSE DOOR CAUTION LIGHT REMAINING ILLUMINATED WITH A NOISE COMING FROM NOSE AREA AFTER GEAR RETRACTION. THE GEAR WAS CYCLED IAW CHECKLIST AND THE LIGHT EXTINGUISHED AND THEN ILLUMINATED AGAIN. FLIGHT RETURNED. MAINTENANCE REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR AND INSPECTED THE ASSOCIATED NOSE GEAR DOOR SENSORS. OPERATIONAL CHECKS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040528000312004052800031WP 2004 5 28 UPS04842407 120040508A57205644972501 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 NR 1 ALT. TANK AT XRS 440 APPROX. STRINGER 59 FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW DWG.5644972, 3645612 AND SRM. 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040528000322004052800032WP 2004 5 28 UPS04842408 120040508A532037558241 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 300 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 33R-34R. REMOVED AND REPLACED FITTING IAW DWG. 3755824 AND SRM. 53-2-0 FIG. 2D. 2L74 4F4 FRT4A25 E2GL 20040528000332004052800033WP 2004 5 28 UPS04842409 120040507A532036431112 ANGLE DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 781 LOWER HORIZONTAL ANGLE AT LBL 60 APPROX IS CRACKED OVER WING BOX. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG.3643111 AND SRM. 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040528000342004052800034WP 2004 5 28 UPS04842410 120040507A57205644973502 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 NR 4 ALT TANK HAS STRINGER 59 FITTING CRACKED AT XRS 428 AND XRS 440 REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 5644973 AND SRM. 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040528000372004052800037WP 2004 5 28 UPS04842413 120040511A5320 STRAP DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 440 AT LBL 12 HAS STRAP BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633853 AND SRM. 51-1-21. 2L74 4F4 FRT4A25 E2GL 20040528000382004052800038WP 2004 5 28 UPS04842414 120040506A5310577384458 SHEAR TIE DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 STATION 1766 AFT SIDE LONG 17R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5773844 AND SRM. 51-3-0. 2L74 4F4 FRT4A25 E2GL 20040528000402004052800040WP 2004 5 28 UPS04842416 120040508A53203755822503N FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 300 BETWEEN LONG 34L-35L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG. 2D. 2L74 4F4 FRT4A25 E2GL 20040528000412004052800041WP 2004 5 28 UPS04842417 120040507A53203755843502N FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 1160 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D. 2L74 4F4 FRT4A25 E2GL 20040528000442004052800044EU 2004 5 28 CX7A194J0427 120040523A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LAVATORY MALFUNCTIONED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03304CE 340B198 ON TAKEOFF ROLL, HAD LAV SMOKE INDICATION, ABORTED TAKEOFF, RAN CHECKLIST, REMAINED ILLUMINATED. 2L72 4T4 TRTA52EU E8NE 20040528000502004052800050CE 2004 5 28 421C052404MT 120040524A781053551084 EXHAUST STACK CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO NR 2 ENGINE CRACKED B JBZRK NONE O OTHER ININSP/MAINT 1 WP2727RX 421C0404 825036 ON THE DAILY INSPECTION, EXHAUST STAINS WERE NOTED ON THE IB SIDE OF THE NR 2 ENGINE COWL. ON FURTHER INSPECTION A CRACK WAS DISCOVERED ON THE EXHAUST STACK AT THE NR 6 RISER. THE 9 INCH CRACK APPEARS TO HAVE STARTED ON THE WELD BETWEEN THE RISER AND STACK ON THE OB SIDE, PROGRESSED DOWN AROUND THE STACK AND UP THE BACKSIDE, ENDING ON THE AFT SIDE OF THE RISER. THE BELLOWS ALSO WAS REPLACED DUE TO DETERIORATION OF THE INTERIOR LINER. 1L72 3O3 O A7CE E7CE 20040528000512004052800051NM 2004 5 28 QXEA200400339 120040521A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA FUSELAGE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX- FORWARD LT AND RT NUTPLATES ARE BROKEN ON UPPER RED ANTI-COLLISION LIGHT ASSEMBLY ATTACH HARDWARE. REMOVED FORWARD ANGLE, REPLACED NUTPLATES AND REINSTALLED ANGLE IAW Q400 SRM 51-42-75. 2H72 4T4 TRTA13NM E00062EN 20040528000532004052800053NM 2004 5 28 QXEA200400341 120040519A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX- PANEL 121BL HAS A BAD NUTPLATE ON LOWER ROW. DOME SEALED NUT PLATE IAW DHC-8 SRM 51-23-00. 2H72 4T4 TRTA13NM E20NE 20040528000562004052800056WP 2004 5 28 ARWA20040507 120040521A2830 ACTUATOR DOUG DC8 DC862 3021970WP PWA JT3D JT3D* 52039NE FUEL SYSTEM MALFUNCTIONED A ARWAJA DUMP FUEL UNSCHED LANDING O OTHER CRCRUISE 1 SO19810BN 45905 UNABLE TO EXTEND FUEL DUMP CHUTES ELECTRICALLY, MOTOR STOPPED APPROXIMATELY 3300 FULL EXTENDED. TRANSFERRED TO DMI NR 18536 CATEGORY (C) IAW MEL 28-9-1. INSTALLED CAT (C) PLACARD; PENDING CLOSING OF DMI. PERFORMED OPERATIONAL CHECK OF FUEL DUMP CHUTE ELECT MOTOR ACTUATOR IAW MM 28-30-2. OPERATIONAL CHECK NORMAL. THIS CLEARS DMI NR 18536. 2L74 4F4 F 4A25 1E8 20040528000592004052800059WP 2004 5 28 GTIA040418 120040319A5310 STOP FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 FWD CARGO DOOR FUSELAGE SIDE, DOOR STOP CORRODED/ FROZEN. REMOVE DOOR STOP. INSTALLED NEW DOOR STOP. 2L72 4F4 F A6WE E2EA 20040528000602004052800060NM 2004 5 28 GTIA040423 120040426A2560 FLASHLIGHT DOUG MD80 MD83 3023681NM AFT LAVATORY MISSING A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23836NK 53045 RT AFT LAV AFT SIDE MISSING 2 EA EMERGENCY LIGHTS. RT AFT LAV EMERGENCY FLASHLIGHTS ARE INSTALLED. 2L72 4F RT 20040528000612004052800061NM 2004 5 28 GTIA040427 120040406A78305938050503 ACOUSTIC LINER DOUG MD80 MD83 3023681NM THRUST REVERSER BOWED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23836NK 53045 NR 2 T/R, SN 49785 ACOUSTIC LINER BOWED. REMOVED NR 2 T/R INSTALLED NR 2 T/R. 2L72 4F RT 20040528000632004052800063WP 2004 5 28 GTIA040419 120040411A5313 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 AFT PIT LONGERON 30 STA 1236 HAS CORROSION UNDER LIP IN RADIUS. REMOVED DAMAGED LONGERON FROM STA 1236-1309. FABRICATED NEW LONGERON. INSTALLED LONGERON. 2L72 4F4 F A6WE E2EA 20040528000702004052800070NM 2004 5 28 GTIA040426 120040319A3350BR9661116 LIGHT DOUG MD80 MD83 3023681NM R1 DOOR MISSING A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23836NK 53045 FWD RT GALLEY SERVICE DOOR LINER EXIT LIGHT ASSY MISSING. INSTALLED NEW LIGHT ASSY. 2L72 4F RT 20040528000722004052800072WP 2004 5 28 GTIA040430 120040324A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 CABIN FLOORBEAM UPPER FLOOR SUPPORT EXTRUSION CORRODED STA 1309. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. 2L72 4F A6WE 20040528000732004052800073WP 2004 5 28 GTIA040432 120040311A5754 FITTING DOUG DC9 DC982 3022082WP L/E SLAT CRACKED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 RT NR 5 SLAT OB SEAL TORN. (EDGE SEAL) FURTHER INVESTIGATION FOUND END FITTING CRACKED. REMOVED RT NR 5 SLAT OB END FITTING. INSTALLED END FITTING. 2L72 4F A6WE 20040528000742004052800074WP 2004 5 28 GTIA040433 120040321A5320 WEB DOUG DC9 DC982 3022082WP COCKPIT CRACKED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 COCKPIT UNDER FIRST OFFICER KICK PANEL WEBBING CRACKED AFT END OF FWD TRACK. REMOVED WEB. DRILLED NEW PART. INSTALLED NEW WEB. 2L72 4F A6WE 20040528000752004052800075WP 2004 5 28 GTIA040434 120040317A5330 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE BULGED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 FUSELAGE LT SIDE AT STA 218 BETWEEN LONG 21L AND 22L SKIN IS BULGING AT REPAIR. FOUND TO BE OUT OF LIMIT OF INTERNAL DOUBLER. FABRICATED INTERNAL DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F A6WE 20040528000762004052800076NM 2004 5 28 GTIA040438 120040504A3350 SIGN DOUG MD80 MD83 3023681NM CABIN INOPERATIVE A GTIAK NONE L NO TEST NRNOT REPORTED 1 GL23828NK 49823 G-4 GALLEY AREA L-2 EXIT SAF-T-GLO SIGN FOUND IN AISLE WAY. INSTALLED NEW EXIT SIGN ASSY. INSTALLED NEW EXIT SIGN ASSY. 2L72 4F RT 20040528000782004052800078 2004 5 28 GTIA040441 420040510A2565 SLIDE DOUG MD80 MD83 3023681NM R1 DOOR OUT OF POSITION A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 R1 SLIDE FELL OFF DOOR WHEN OPENED BY CATERING. REINSTALLED SLIDE. 2L72 4F RT 20040528000792004052800079WP 2004 5 28 GTIA040446 120040511A2560 PIN DOUG DC9 DC981 3022081WP EVAC SLIDE OUT OF POSITION A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23819NK 48016 CHECK L1 DOOR SLIDE PACK. FOUND LANYARD AND UNFURLING PINS OUT. REMOVED SLIDE FROM DOOR AND REINSTALLED UNFURLING PINS. REINSTALLED PACK BACK ON L1 DOOR AND LANYARD. NO FURTHER DEFECTS NOTED. 2L72 4F A6WE 20040528000802004052800080WP 2004 5 28 GTIA040440 120040508A3260 WARNING LIGHT DOUG DC9 DC982 3022082WP COCKPIT ILLUMINATED A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23801NK 48048 AFTER T/O NOSE GEAR UNSAFE LIGHT ON FOLLOWED QRH AND LANDED. PERFORMED NOSE GEAR EXTENSION AND RETRACTION OPERATIONAL CK. OPS CK OK. 2L72 4F A6WE 20040528000812004052800081WP 2004 5 28 GTIA040422 120040420A33501001191 LIGHT DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE L1 DOOR BROKEN A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 EMERGENCY LIGHT AT L1 DOOR HOLDER IS BROKEN. REMOVED EMERGENCY LIGHT. INSTALLED SERVICEABLE EMERGENCY LIGHT. 2L72 4F4 F A6WE E2EA 20040528000822004052800082WP 2004 5 28 GTIA040435 120040323A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 STA 229 LT CUSP MEMBRANE HAS CORROSION. REMOVED DAMAGED AREA. FABRICATED WEB. INSTALLED NEW WEB. 2L72 4F A6WE 20040528000832004052800083WP 2004 5 28 GTIA040442 120040508A3350 SIGN DOUG DC9 DC982 3022082WP AFT GALLEY DEFECTIVE A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23804NK 49104 FLOOR EXIT SIGN IN AFT GALLEY UNREADABLE. REPLACED FLOOR EXIT SIGN (SAFETY GLOW) IN AFT GALLEY. 2L72 4F A6WE 20040528000852004052800085WP 2004 5 28 GTIA040421 120040420A3350 LIGHT DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE AFT STAIRWELL BROKEN A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 5 EA EMERGENCY LIGHTS BROKEN IN AFT STAIRWELL. REMOVED BROKEN LIGHTS. INSTALL 5 EA NEW LIGHTS. 2L72 4F4 F A6WE E2EA 20040528000872004052800087 2004 5 28 P5CA0401096 420040523A3441 INU BOEING747 747341 13848AMNM GE CF6 CF650E2B 30018NE NAV SYSTEM MALFUNCTIONED A P5CAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP23355MC 23395 AFTER TAKEOFF, POSITION ERROR IN INS, UNABLE TO UPDATE MANUALLY OR AUTOMATICALLY. INS SYSTEM OPERATIONAL CHECK NORMAL AS IAW MM 34-41-00, DME SYSTEM OPERATIONAL CHECK NORMAL IAW MM 34-55-00. 2L74 4F4 FRTA20WE E23EA 20040525000902004052500090EA 2004 5 25 SWIA200413265 120040413A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 LEFT PRESSURE FLOOR HAS CORROSION AS MARKED AT FS 409+128 TO 559, LBL 36 TO LBL 48.REPAIRED IAW CRJ REO 601R-53-41-206 REV. NC. 2L72 4F RTA21EA 20040525000992004052500099SO 2004 5 25 SWIA200413274 120040508A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS LEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 NM07296SW 120325 ENROUTE, AT ALTITUDE, FLAP SYSTEM EXPERIENCED A CONTROL FAULT ON THE OUTBOARD SEGMENT. WHEN LANDING, FLAPS 45 DEGREES, WE EXPERIENCED ANOTHER CONTROL FAULT. WE RESET THE SECOND ONE AFTER LANDING. BOTH WERE ON THE OUTBOARD SEGMENTS. REPLACED RIGHT OUTBOARD FLAP ACTUATOR DUE TO CONTROL FAULTS AND HYDRAULIC FLUID ON ROD END AREA. OPS CHECKED GOOD. DONE IAW MM 27-50-09. S/N OFF: 0294. 2L72 4T RTA31SO 20040525001012004052500101 2004 5 25 SWIA200413276 420040507A34446222855011 TRANSCEIVER CNDAIRCL600 CL6002C10 1390015EA NR 2 RADAR ALT MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07705SK 10145 DURING TAXI OUT, GLD UNSAFE CAUTION MESSAGE APPEARED. RETURNED TO GATE. MDC INDICATES SSCU2 FAILED. RAD ALT RANGE FAULT COMP ID A13.REMOVED AND REPLACED NR 2 RAD ALT TRANSCEIVER. OPS CHECK GOOD IAW CRJ 700 MM 34-44-01. 2L72 4F RTA21EA 20040525001202004052500120EA 2004 5 25 WVE2004F00013 120040420A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09408SW 7055 BULKHEAD FS 202.75 LBL 24 BETWEEN STRINGERS 20L AND 21L IS CRACKED PROTRUDING FROM CUTOUT FOR PARKING BRAKE CONTROL ROD. VIBRATION AND STRESS FROM CABLE ARE THE PROBABLE CAUSE. INSTALL DOUBLER ON BULKHEAD. 2L72 4F4 FRTA21EA E15NE 20040525001222004052500122 2004 5 25 BAQA094539 420040519A3421060002600 GYRO AEROSPAS355 AS355F2 8680812EU COCKPIT FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS 5495 GYRO FAILED. REPLACED WITH SERVICABLE UNIT. 1G72 3U H11EU 20040525001272004052500127EU 2004 5 25 BAQA094679 120040517A7712642519032 TRANSMITTER AEROSPAS355 AS355F2 8680812EU TORQUE IND FAILED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03941MS 5495 TORQUE TRANSMITTER UNIT FAILED OUT OF BOX, WILL NOT ADJUST. RETURNED TO TRADEWIND INTERNATIONAL. 1G72 3U H11EU 20040526000052004052600005SO 2004 5 26 SIMA200410701 120040413A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT MALFUNCTIONED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21615AE 145087 CREW REPORTED THE FORWARD EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK (P/N 20131A) IAW EMB 145 AMM 33-50-06. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040526000062004052600006SO 2004 5 26 SIMA200406201 120040228A335070131A BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21725AE 145312 FOUND FORWARD FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED NR 1 AND NR 2 BATTERY PACKS IAW W/C 33-100-19. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20040526000122004052600012SO 2004 5 26 SIMA200407502 120040314A33507287100509 CONTROL PANEL EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21639AE 145182 EMERGENCY LIGHTS WILL NOT WORK FROM THE FLIGHT ATTENDANTS PANEL. REPLACED FLT ATTENDANT CONTROL PANEL IAW EMB 145 AMM 33-21-00. OPS CHECKED GOOD. (M) 2L72 4T RTT00011AT 20040526000252004052600025EA 2004 5 26 ASOA04272 120040406A5320601R3501111 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11836AS 7263 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT ANGLE UNDER THE FLOORBOARD AT THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT ANGLE UNDER THE FLOORBOARD. (M) 2L72 4F RTA21EA 20040526000262004052600026EA 2004 5 26 ASOA04293 120040424A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-42-00. (M) 2L72 4F RTA21EA 20040526000342004052600034NM 2004 5 26 SWAA041367 120040513A5312BAC1514 STIFFENER BOEING737 7373H4 1384600NM BULKHEAD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED AND REPLACED BULKHEAD STIFFENER PER ACO. 2L72 4F RTA16WE 20040526000382004052600038NM 2004 5 26 SWAA041373 120040513A53306545877 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CUTOUT AT UPPER STOP CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040526000452004052600045NM 2004 5 26 SWAA041351 120040512A3350OL3071BPEGPL BULB BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED PM CHECK, FOUND EEPLS LIGHT AT ROW 1ABC, INOP. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20040526000592004052600059NM 2004 5 26 04FDEA01013 120040421A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25243FE 21480 SKIN CHAFE DAMAGE FOUND AT BS 950E 12 TO 950E 19 BETWEEN STR 25L TO STR 26L. SKIN CHAFE FOUND TO BE OUT OF LIMITS FROM BS 950E 12 - 950E 19. REPAIRED DAMAGED SKIN FROM 950E 12 TO 950E 19 BETWEEN STR 25L TO 26L PER SRM 53-30-3 FIG 1. 2L73 4F RTA3WE 20040526000742004052600074CE 2004 5 26 BAQA089380 120040405A28231013890255 SHUTOFF VALVE BEECH 90 C90 1152913CE FUEL SYSTEM MALFUNCTIONED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0390LF 10147 LJ852 SHUTOFF VALVE DOES NOT OPERATE PROPERLY. REPLACED WITH SERVICABLE UNIT. 05/24/2004 1L72 3T 3A20 20040526000772004052600077SW 2004 5 26 ALGA094697 120040521A6320206375202101 TACH GENERATOR BELL 407 407 1182206SW MAIN ROTOR WORN E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBFG887 52274 FOUND SPLINES INSIDE ARMATURE AND ON DRIVSHAFT WORN. DISCREPANCY FOUND ON 900HR. INSPECTION.RETURNING PART TO VENDOR FOR WARRANTY. 1G71 3U O H2SW 20040526000802004052600080EU 2004 5 26 BAQA094647 120040426A6410L621M1010056 BLADE UROCOPEC135 EC135P2 5620027EU MAIN ROTOR PEELING E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03603ME346 0284 EC135 M/R BLADE S/N 1573, INTERGRATED PU FILM PEELING OFF. 1G72 3U H88EU 20040526000892004052600089EU 2004 5 26 04FDEA01287 120040518A5312 BULKHEAD AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 AFT PRESSURE BULKHEAD FR 80 RIGHT WEB ASSY HAS AREAS OF CORROSION. INSTALLED NEW WEB ON ATTACH ANGLE IAW SRM 51-40-21. WORK PERFORMED ON NRC N00272. 2L72 4F RTA35EU 20040526000922004052600092NM 2004 5 26 04FDEA01290 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP INBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526000972004052600097EU 2004 5 26 RO32004F00001 120040228A1430NAS517V32XA SCREW AMD FALC50FALCON50MYST2730106EU RT WING CHAFED B RO3RO OTHER O OTHER NRNOT REPORTED 1 CE0330FT 271 39TH SCREW IB OF RIB 20 ON RT WING UPPER FIXED STRUCTURE BOX RIB 13 TO 20 IS CHAFFING ON HYDRAULIC RETURN LINE FOR RT AILERON SERVO. 2L73 4F A46EU 20040526000982004052600098CE 2004 5 26 JAC006RR 120040510A779730224410 WIRE HARNESS BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA RT ENGINE FAILED B MZ2RO OTHER O OTHER NRNOT REPORTED 1 GL13200CJ2463 BB143 PCE80320 RT ENGINE ITT INDICATION FAILED IN FLIGHT, PROBLEM WAS DETERMINED BY MAINT TO BE AN ENGINE HARNESS FAILURE. AC FERRIED HOME, WHERE THE T5 HARNESS ASSY WAS REPLACED. CORRECTING DISCREPANCY. THE FAULT WAS NOT DETECTABLE THROUGH NORMAL INSPECTION PROCEDURES, SUGGEST HARNESS REPLACEMENT BE ACCOMPLISHED DURING EACH ENGINE HOT SECTION INSPECTION. 1L72 4T4 T A24CE E4EA 20040526001002004052600100NM 2004 5 26 04FDEA01294 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.503, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.501. REWORKED AREA REPAIRED AS PER EA 1-5750-76670. LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001022004052600102WP 2004 5 26 04FDEA01296 120040518A5753ARC1496 SUPPORT DOUG DC10 DC1010 3022110WP LT OB FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 ARC1496 FLAP VANE SUPPORT CORROSION REWORK IAW EA 8-5750-77409. COMPLIED WITH EA 8-5750-77409 WINGS ARC1496 FLAP VANE SUPPORT CORROSION REWORK AT MAE. 2L73 4F A22WE 20040526001052004052600105NM 2004 5 26 04FDEA01299 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), I/B ACTUATOR ATTACHMENT SPOTFACE FOUND CORRODED. I/B ACTUATOR ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.392, MATERIAL REMOVED: 0.002, REMAINING THICKNESS: 0.390. REPAIRED AS PER EA 1-5750-76671, LT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001072004052600107NM 2004 5 26 04FDEA01303 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.094, FINAL DIAMETER: 1.096. REPAIRED AS PER EA 1-5750-76671. LT OUTBOARD FLAP, OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001092004052600109NM 2004 5 26 04FDEA01305 120040518A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL THICKNESS OF LUG: 0.492, MATERIAL REMOVED AT O/B FACE: 0.021, I/B FACE: 0.023, REMAINING THICKNESS OF LUG: 0469. REPAIRED AS PER EA 1-5750-76672, RT OUTBOARD FLAP, O/B FLAP SIDE HINGE BRACKET PIVOT BEARINGS. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040526001172004052600117WP 2004 5 26 04FDEA01256 120040513A5347FXSRM537000ST SEAT TRACK DOUG DC10 DC1010F 3022111WP ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CARGO DECK SEAT TRACK GOUGED AT LBL 47.25 FS 1740. REMOVED AND REPLACED DAMAGED TRACK AT FS 1740 LBL 47.25 IAW SRM 53-70-00 FIG 1 & 51-31-01 AT MAE. 2L73 4F A22WE 20040526001312004052600131NM 2004 5 26 0400705515 120040507A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 23203 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 24. REPAIRED PER EA 55-198768. 2L72 4F RTA2NM 20040526001362004052600136NM 2004 5 26 AALA20040537 120040510A3350 FUSE BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21789AN 30252 EMERGENCY LIGHT AT SEAT ROWS 30 THROUGH 44 INOPERATIVE. REPLACED FUES IN BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30 THROUGH 44. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTT00001SE 20040526001432004052600143NM 2004 5 26 AALA20040538 120040508A3350 LIGHT BOEING767 767323 1385205NM SEAT 24G INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21399AN 29606 DFW EMERGENCY LIGHT AT SEAT 24G DAMAGED. REPAIRED EMERGENCY LIGHT ASSEMBLY FOR SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20040526001472004052600147NM 2004 5 26 2004UALA00429 120040502A5753113T22703 HINGE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RT INBD FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16876 30024 RT INBD FLAP CENTER EXTERNAL HINGE IS CRACKED ON THE OUTBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLES. 2L72 4F4 FRTA1NM E24NE 20040526001482004052600148NM 2004 5 26 2004UALA00430 120040502A5320 PULLEY BRACKET BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 FWD RT TUNNEL, BS 246 FLOORBEAM, FWD SIDE PULLEY BRACKET SUPPORT ANGLE CRACKED AT BL0. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT ANGLE. 2L72 4F4 FRTA1NM E24NE 20040526001502004052600150NM 2004 5 26 2004UALA00432 120040430A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 35CD INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29220UA 30223 EMERGENCY EEL LIGHT AT SEAT 35CD IS INOP. REPLACED LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20040526001512004052600151NM 2004 5 26 2004UALA00433 120040430A2120 FLUID BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE NR 1 A/C PACK DETECTED A UALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP29670UA 29240 FOUL, STRONG ODOR ON TAKEOFF AND LANDING. REMAINS THROUGHOUT DEPARTURE CLIMB AND BEG IN AGAIN BELOW 20,000 ON ARRIVAL. FLT ATTENDANTS AND PAX COMPLAINING. AFTER LANDING ODOR MADE EYES WATER IN AFT CABIN. SMOKE ALARMS IN AFT LAVS SOUNDED SHORT TIME. DEICING FLUID WAS FOUND DRIPPING FROM THE NR 1 ENGINE. IT WAS REMOVED AND BOTH ENGINES WERE RUN, AN A/C PACK BURNOUT ACCOMPLISHED TO REMOVE ANY REMAINING RESIDUE TRAPPED IN THE SYSTEM. 2L72 4F4 FRTA1NM E24NE 20040526001552004052600155NM 2004 5 26 2004UALA00438 120040504A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29541UA 25253 FLT DIVERTED DUE TO ELECTRICAL ODOR IN COCKPIT. LT RECIRC FAN REMOVED AS SUSPECT. NO FAULT FOUND. BOTH RECIRC FAN HEPA FILTERS REPLACED. COOLING FANS AIR BARRIER FILTER REPLACED. 1 HOUR TEST FLIGHT COULD NOT DUPLICATE ODOR. NO DISCREPANCIES FOUND. 2L72 4F4 FRTA2NM E17NE 20040526001572004052600157NM 2004 5 26 2004UALA00443 120040505A2530 COFFEEMAKER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29944UA 26683 RETURNED TO YYZ DUE TO F-A REPORTED SPARKS AND POPPING COMING FROM FWD GALLEY CEILING ABOVE COFFEE MAKER. MECHANIC INSPECTING AIRCRAFT FOUND NO SIGNS OF ARCING OR MOISTURE ABOVE COFFEEMAKER. SUBJECT COFFEEMAKER FOUND TO FUNCTION PROPERLY. FURTHER ANALYSIS BY ORIGINAL MANUFACTURER REVEALED NO SIGNS OF ELECTRICAL ARCING AT TOP OF UNIT, BUT DID VERIFY SIGNS OF ELECTRICAL ARCING BENEATH UNIT AT CONNECTION TO HOTPLATE ELEMENT. TYPICAL CAUSE IS MOISTURE INGRESSION OF THERMAL INSULATION AND ARCING TO UNPROTECTED TERMINAL. OSV FOR COFFEEMAKER MAINTENANCE, ADVISED AND INSTRUCTED TO INSPECT FOR UNPROTECTED HOTPLATE TERMINALS AND APPLY CORRECTIVE ACTION, AS NEEDED. 2L72 4F4 FRTA16WE E2GL 20040526001602004052600160EA 2004 5 26 SWIA200413294 120040503A5712 RIB CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 LT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). COMPLIED WITH 1 THROUGH 9 OF REO 601R-57-51-046. FAB. PARTS FROM 56144-4 ANGLE .063 AND 7075T6 .050, PO 358501/1. PERFORMED REPAIR NR 1. 2L72 4F RTA21EA 20040526001622004052600162EA 2004 5 26 SWIA200413296 120040503A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 FLOOR SUPPORT ANGLES AT FS 280, RBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 IB AND OB AND LBL 9 IB AND OB IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND EO 601R-53-4942. SEE RII 53-401. 2L72 4F RTA21EA 20040526001682004052600168NM 2004 5 26 DL73S040401 120040504A2761 HOUSING BOEING737 737232 1384475NM SPOILER ACTUATORCRACKED A DALAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO27331DL 0413 23103 LOST A HYDRAULIC SYSTEM ON TAXI IN TO GATE AT ORD. FOUND NR 8 GROUND SPOILER ACTUATOR BODY CRACKED. REPLACED NR 8 GROUND SPOILER PER AMM 27-62-101, PB 401. LEAK AND OP. CHECK GOOD. RII PERFORMED. 2L72 4F RTA16WE 20040527000022004052700002NM 2004 5 27 04FDEA01422 120040524A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FLOORBEAM TOP TEE CORRODED STA 1030 LBL 25 - RBL 25 WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMGE AREA PER SRM 53-10-8. 2L73 4F RTA3WE 20040527000142004052700014NM 2004 5 27 SWAA041384 120040514A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT E/E COMPARTMENT EQUIPMENT COOLING DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040527000222004052700022NM 2004 5 27 SWAA041392 120040516A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND STRINGER 4R AT BS 639, CRACKED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040527000352004052700035NM 2004 5 27 DL757040414 120040509A4950331200 APU BOEING757 757232 1384965NM APU BAY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27629DL10025 22919 FA'S REPORT MUSTY/DUSTY ODOR THROUGHOUT A/C ON DESCENT. PASSENGERS ALSO COMPLAINED. RAN APU OVERNIGHT TO PURGE DUCTS, NO ODOR NOTED. 2L72 4F RTA2NM 20040527000392004052700039NM 2004 5 27 DL73S040418 120040510A5522 SKIN BOEING737 737232 1384475NM LT ELEVATOR DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 WHILE WORKING N/R 13 FOUND LT ELEVATOR UPPER SURFACE DELAMINATED UNDER CONDUCTIVE FRAME REPAIRED PER SRM 55-20-03 FIG 1 TABLE 1. 2L72 4F RTA16WE 20040527000412004052700041NM 2004 5 27 DL757040421 120040510A5750 SKIN 114N4005177 BOEING757 757232 1384965NM NR 4 SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27662DN A10324 24991 ACCOMPLISHED METAL BOND REPAIR TO UPPER INBOARD SKIN ON THE NUMBER 4 SLAT. 2L72 4F RTA2NM 20040527000592004052700059NM 2004 5 27 SWAA041452 120040521A575465C26602217 SKIN BOEING737 7373G7 1384595NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED A1 CHECK, FOUND LT WING L/E NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20040527000642004052700064NM 2004 5 27 SWAA041475 120040524A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR CUTOUT UPPER TORQUE FITTING BEAR STRAP CRACKED. REPAIRED BEAR STRAP PER ER. 2L72 4F RTA16WE 20040527000762004052700076NM 2004 5 27 SWAA041480 120040524A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040527000832004052700083NM 2004 5 27 SCNA04006 120040504A3350 FUSE BOEING737 7378Q8 13844BXNM POWER SUPPLY BLOWN A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15804SY 16942 30689 FORWARD LEFT POWER SUPPLY FOR EMERGENCY LIGHTS INOP. 2L72 4F RTA16WE 20040527000922004052700092GL 2004 5 27 MASA200400253 220040507A7250AE3007A1 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 HOT START A MASAE ENGINE SHUTDOWN M OVER TEMP TXTAXI/GRND HDL 1 SW07830MJ6047 145259 CAE311929 ASH 2767 CLT. CREW REPORTED THE NR 2 ENGINE EXPERIENCED HUNG START WITH EXCESSIVE TAILPIPE FLAME. MX INVESTIGATED AND FOUND ACCORDING TO CMC THAT THE ITT MAXIMUM LIMITS WERE EXCEEDED AT 927 DEGREES C FOR 9 SECONDS AND N1 & N2 WERE OVERSPEED. MX CHANGED NR 2 ENGINE AND THRUST REVERSER WAS ALSO CHANGED DUE TO EXCESSIVE HEAT. 2L72 4T4 FRTT00011ATTE6CH 20040527001042004052700104EA 2004 5 27 COMA0470041 120040508A5230 DOOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY OPEN A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01398CA 10112 FLIGHT 5091 CABIN ALTITUDE CAUTION MESSAGE. FOUND AFT CARGO DOOR NOT CLOSED PROPERLY. CLOSED DOOR, NO DEFECTS FOUND. 2L72 4F RTA21EA 20040527001082004052700108NM 2004 5 27 04FDEA01011 120040421A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001122004052700112NM 2004 5 27 04FDEA01018 120040422A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001142004052700114 2004 5 27 04FDEA01100 420040424A34166224563008 ALTIMETER DOUG DC10 DC1010 3022110WP ZONE 200 MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 FIRST OFFICERS RADIO ALTIMETER FLAG IN VIEW. AIRCRAFT CONTINUES TO DEVELOPE HISTORY OF RADIO ALTIMETER FAULTS. CLEANED RADIO ALTIMETER COOLING FANS AND R/T IAW DC10 MM 20-10-10. REMOVED AND REPLACED COOLING FAN IAW DC-10 MM 21-85-05. REMOVED AND REPLACED FIRST OFFICERS RADIO ALTIMETER INDICATOR IAW DC-10 MM 34-42-02. REPAIRED BROKEN WIRE AT CONNECTOR P1-1009 PIN J IAW DC-10 WDM 34-42-02. OPS CHECK OF RADIO ALTIMETER IAW DC-10 MM 34-42-00 GOOD. 2L73 4F A22WE 20040528000022004052800002EU 2004 5 28 00139 120040513A3260 SQUAT SWITCH AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE RT MLG OUT OF RIG E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05204TW 204 PILOT REPORTED CABIN WOULD NOT PRESSURIZE. CABIN LIGHT CAME ON, RETURN TO DEPARTURE AIRPORT ADS FOR MAINTENANCE. MAINTENANCE FOUND SQUAT SWITCH ON RT MLG OUT OF RIG, ADJUSTED AND PERFORMED OP CHECKS, AIRCRAFT RETURNED TO SERVICE. (CLOSED) 2L72 4F4 F A7EU E7EA 20040528000112004052800011NM 2004 5 28 C1HA200483006 120040522A5754 SLAT BOEING727 7272S7 138407ZNM NR 6 CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15683CA 22490 NR 6 SLAT CRACK AT FASTENER HOLE AND 2 GOUGES IN WEDGE EXTRUSION. 2L73 4F A3WE 20040528000182004052800018NE 2004 5 28 MALA040402 220040518A73216071T20P18 CONTROL UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 GL15422XJ 340B422 RT PROP RPM, TORQUE AND ENGINE OIL PRESSURE FLUCTUATING AFTER TAKEOFF. AIR RETURNED. MAINTENANCE REMOVED AND REPLACED DEC PN 6071T20P18 SN ON LMDT2171 SN OFF LMDT2223. OPS CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20040528000242004052800024 2004 5 28 MALA040409 420040424A25629521000020 BATTERY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ELT DISCHARGED A MALAK NONE O OTHER NRNOT REPORTED 1 GL15370PX 340B300 ELT REMAINS ON PN 95210000-20, SN/0343. UNIT WAS FOUND TO HAVE NO TROUBLE . UNIT WAS FOUND TO HAVE NO THROUGH. MAINTENANCE REPLACED BATTERY DUE TO DISCHARGED STATE. UNIT PASSED MFG MM CHECKS AND WAS RETURNED TO SERVICE 5/6/04. 2L72 4T4 TRTA52EU E8NE 20040528000262004052800026EU 2004 5 28 MALA040406 120040506A3350501171202 BATTERY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 POWER SUPPLY PN 501-1712-02 SN 2065, WAS REMOVED FOR SCHEDULED DISCHARGE CHECK, UNIT FAILED DISCHARGE CHECK. BATTERY ASSEMBLIES (2 EA) PN 549-1324-06 WERE REPLACED AND UNIT PASSED ALL CMM CHECKS. UNIT WAS RETURNED TO SERVICE 5/13/04. FOR ADDITIONAL INFORMATION REFER TO WO#366903. 2L72 4T4 TRTA52EU E8NE 20040528000352004052800035WP 2004 5 28 UPS04842411 120040512A574456423421 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 LT WING FLAP LINK SUPPORT ASSY IS CRACKED AT FLAP HINGE 3. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM. 51-1-20D, 51-3-0. 2L74 4F4 FRT4A25 E2GL 20040528000422004052800042WP 2004 5 28 UPS04842418 120040507A53203755843U501 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 STATION 1152 OB OF LONG 35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D. 2L74 4F4 FRT4A25 E2GL 20040528000472004052800047NM 2004 5 28 AWXA200400562 120040521A2560P4010021 BATTERY BOEING737 73733A 1384673NM GE CFM56 CFM56* 13802NE FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28175AW 23634 LCQ - EMERGENCY EQUIPMENT - DURING C-19 CHECK FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040528000522004052800052NM 2004 5 28 QXEA200400340 120040519A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX- RT FORWARD FUSELAGE PANEL 122AR HAS TWO BAD NUTPLATES. DOME SEALED NUTPLATES IAW DHC-8 SRM 51-23-00. 2H72 4T4 TRTA13NM E20NE 20040528000552004052800055NM 2004 5 28 QXEA200400343 120040518A5410 STRUT DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NACELLE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX- UPPER OB STRUT PROTECTIVE COATING IS WORN OFF 14 INCHES FORWARD OF FIREWALL ON IB SIDE. APPLIED EPOXY PRIMER IAW RD 8-54-036. 2H72 4T4 TRTA13NM E20NE 20040528000582004052800058SO 2004 5 28 IS42004F00000 120040407A214088D932EL TUBE PIPER PA23 PA23250 7102308SO LYC O540 IO540* 41532EA HEATER CRACKED B IS4RK NONE O OTHER ININSP/MAINT 1 SO0926FT 277754059 RECEIVED HEATER CORE FROM CUSTOMER. THE COMBUSTION TUBE END PLATE HAS TWO VISUAL CRACKS. ONE AT THE TWO O’CLOCK POSITION AND ONE AT THE SEVEN O’CLOCK POSITION. THIS HEATER IS THE (FR) SERIES THAT HAS THE CERAMAKOTE COMBUSTION TUBE WITH NO AD AGAINST IT. BY LOOKING AT THE HEATER SN THIS HEATER WAS MFG IN MARCH, 1999. CAUSE OF THE CRACK IS PROBABLY CAUSED BY METAL FATIGUE DUE TO TIME IN SERVICE OR RUNNING THE HEATER TOO HOT. THERE IS NOTHING THAT CAN BE DONE TO PREVENT THESE CRACKS. ALL AIRCRAFT HEATER COMBUSTION TUBES AT SOME POINT IN TIME ARE GOING TO FAIL/CRACK. A PRESSURE TEST OF THE COMBUSTION TUBE WILL FIND THESE FAILURES. 1L72 3O3 O 1A10 1E4 20040528000622004052800062WP 2004 5 28 GTIA040444 120040509A2560 LANYARD DOUG DC9 DC981 3022081WP EVAC SLIDE DISENGAGED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23811NK 48017 L1 DOOR PACK SLIDE LANYARD DISENGAGED FROM DOOR (SLIDE DID NOT FALL OFF OF DOOR). REINSTALLED LANYARD. 2L72 4F A6WE 20040528000642004052800064NM 2004 5 28 GTIA040424 120040416A3350 LIGHT DOUG MD80 MD83 3023681NM CABIN MISSING A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23836NK 53045 SEVERAL EMERGENCY EXIT IDENTIFIERS LIGHTS MISSING. INSTALLED 4 EA NEW EMERGENCY EXIT IDENTIFIERS. 2L72 4F RT 20040528000662004052800066WP 2004 5 28 GTIA040443 120040507A2560 LANYARD DOUG DC9 DC982 3022082WP R1 DOOR MISINSTALLED A GTIAK NONE W INADEQUATE Q C NRNOT REPORTED 1 GL23817NK 49141 R1 GALLEY SERVICE DOOR, LANYARD NEED TO BE REINSTALLED. REINSTALLED LANYARD AT R1 GALLEY SERVICE DOOR. OPS CK GOOD. 2L72 4F A6WE 20040528000712004052800071WP 2004 5 28 GTIA040428 120040326A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 CABIN STA 200-229 RBL 21 SEAT TRACK CORRODED AT FASTENER HOLES. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK. INSTALLED NEW SEAT TRACK IN CABIN STA 200-220. 2L72 4F A6WE 20040528000772004052800077WP 2004 5 28 GTIA040439 120040425A2560 STRAP DOUG DC9 DC982 3022082WP EVAC SLIDE MISINSTALLED A GTIAK NONE W INADEQUATE Q C NRNOT REPORTED 1 GL23812NK 48021 TAIL SLIDE COVER HOLD DOWN STRAPS NOT INSTALLED CORRECTLY. INSTALLED TAIL CONE EMERGENCY SLIDE COVER STRAPS CORRECTLY. 2L72 4F A6WE 20040528000882004052800088CE 2004 5 28 E712004F00000 120040326A7931APTE304200G TRANSDUCER CESSNA525 525A 2076615CE WILINTFJ44 FJ442A GL LT ENGINE FAILED E E71AE ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA1712GS 406 525A0127 WHILE CLIMBING THROUGH FL180, PILOTS NOTICED A CONTINUAL DECLINE IN OIL PRESSURE ON THE LT ENGINE. PROCEDURE REQUIRED SHUTDOWN AND SECURING LT ENGINE IN FLIGHT. AT THAT TIME THE AIRCRAFT WAS 20 MIN FROM INTENDED DESTINATION. PILOTS MADE A NORMAL DESCENT TO 40N AND LANDED WITH ONE ENGINE, WITHOUT INCIDENT. EXCHANGED PRESSURE TRANSDUCERS FROM SIDE TO SIDE, TEST RAN, COULD NOT DUPLICATE PROBLEM. REPLACED SUSPECT TRANSDUCER, MOC-OK. 1L71 4F4 FRTA1WI E3GL 20040528000902004052800090SO 2004 5 28 FFK2004F00004 220040427A73146462102A1 PUMP CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE FAILED B FFKRO OTHER O OTHER NRNOT REPORTED 1 SO0510QP 3 402B0831 183547R AFTER INSTALLING AN ENGINE WITHIN 3 FLIGHT HOURS THE ENGINE DRIVEN FUEL PUMP SHAFT FAILED. PUMP FAILED ON TAKEOFF AND QUIT RUNNING. 1L72 3O3 O A7CE E8CE 20040601000022004060100002NM 2004 6 1 DL73S040433 120040513A5320 FITTING BOEING737 737247 138448DNM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 DURING ACCOMPLISHMENT OF EO 3-085220-03, CORROSION DAMAGE WAS NOTED WHICH EXCEEDED THE ALLOWABLE LIMITS OF THE SUBJECT EO ON THE NR 6 AND NR 12 LUGS LOCATED AT BS 1088. CORROSION REMOVED AND DAMAGE REWORKED IAW ERA 089944-14. 2L72 4F4 F A16WE E2EA 20040601000042004060100004CE 2004 6 1 EWC2004F00000 120040518A2170991206913 SEPARATOR CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE A/C BAY MISALIGNED E EWCRK NONE O OTHER NRNOT REPORTED 1 SO0552CK 8038 S5500076 CABIN PRESSURE LOSS BECAUSE OF A COUPLING BLOWING LOOSE BETWEEN TWO MISALIGNED PARTS, THE WATER SEPARATOR PN 9912069-13 AND THE (Y), PN 6515326-28. THE MISALIGNMENT IS A DESIGN PROBLEM. 1L72 4F4 FRTA22CE E1NE 20040601000052004060100005CE 2004 6 1 EWC2004F00001 120040518A2130651532628 DUCT CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE TAIL CONE LOOSE E EWCRK NONE O OTHER NRNOT REPORTED 1 SO0552CK S5500076 CABIN PRESSURE LOSS BECAUSE OF A COUPLING BLOWING LOOSE BETWEEN TWO MISALIGNED PARTS, THE WATER SEPARATOR PN 9912069-13 AND THE (Y), PN6515326-28. THE MISALIGNMENT IS A DESIGN PROBLEM. 1L72 4F4 FRTA22CE E1NE 20040601000072004060100007CE 2004 6 1 S5M2004F00000 120040427A3710ADV212CW PUMP BEECH 36 A36TC 1151603CE CONT O520 TSIO520* 17040SO VACUUM SYSTEM FAILED B S5MRO OTHER O OTHER CRCRUISE 1 GL153671S346 EA95 THE PILOT WAS FLYING IN CLEAR WEATHER. SUDDENLY HE LOST ALL INSTRUMENT AIR PRESSURE. THIS IS A DUAL PUMP AND BOTH PUMPS FAILED AT THE SAME TIME. WHEN PUMP WAS REMOVED, THE DRIVE SHAFT COULD BE PULLED OUT OF THE PUMP ABOUT 2 INCHES. WHEN SPOKE WITH THE MFG PRIOR TO PURCHASING THIS SYSTEM, WERE TOLD THAT IT WAS NOT POSSIBLE FOR BOTH PUMPS TO FAIL AT THE SAME TIME. HAD THE PLANE BEEN IN IFR CONDITIONS, WOULD HAVE LOST HIS GYROS. (SO17200410222) 1L71 3O3 O 3A15 E8CE 20040601000142004060100014NM 2004 6 1 PCAA0405212 120040523A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NR 1 INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13812EX279103988 312 DURING ROUTINE TEST THE FLIGHT CREW REPORTED THE NR 1 SMOKE DETECTOR AS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 SMOKE DETECTOR UNIT. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040601000162004060100016WP 2004 6 1 ASMF200405025 120040524A1430 FASTENER DOUG DC9 DC987 3022087WP FUSELAGE LIGHTNING STRIKEW ASMFK NONE O OTHER ININSP/MAINT 1 SW23216AM 49586 DURING TRANSIT CHECK, A LIGHTING STRIKE WAS DETECTED ON THE FUSELAGE LT SIDE, FORWARD OF THE WING WITH SOME FASTENERS DAMAGED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT. FASTENERS WERE REPLACED IAW MM 43-04 FIG 38 TABLE B CONDITION 2. PENDING FOR FURTHER INFORMATION, IT WILL BE SENT AS SUPPLEMENT. 2L72 4F RTA6WE 20040601000172004060100017NM 2004 6 1 ASMF200405026 120040527A56105912290506 WINDSHIELD DOUG MD88 MD88 3023688NM COCKPIT CRACKED W ASMFK NONE O OTHER CRCRUISE 1 SW23160PL150 49763 CAPTAIN INFORMED THAT DURING FLIGHT RT WINDSHIELD PANEL CRACKED (EXTERNAL SIDE). WINDSHIELD PANEL ASSY WAS REPLACED IAW MM 56-10-2, TESTS CORRECT. 2L72 4F RTA6WE 20040601000182004060100018EA 2004 6 1 ASOA04327 120040415A3350364911 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27910EV 7727 DURING A (C) CHECK, THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD 3 SECTIONS OF EMERGENCY FLOOR LIGHT STRIPS. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040601000192004060100019EA 2004 6 1 ASOA04330 120040504A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27872AS 7542 DURING HANGER MAINTENANCE, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK THE SERVICE. 2L72 4F4 FRTA21EA E15NE 20040601000202004060100020EA 2004 6 1 ASOA04329 120040503A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EXTERIOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27853AS 7374 DURING A GROUND INSPECTION, THE LT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040601000222004060100022EA 2004 6 1 ASOA04326 120040501A783022858400801 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE THRUST REVERSER OUT OF RIG A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27908EV 7654 CF343B1 DURING CRUISE, AT APPROXIMATELY 26,000 FEET THE CREW RECEIVED A LT REVERSER UNLOCK MESSAGE. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT DIVERTED. FIRE AND RESCUE VEHICLES WERE REQUESTED TO BE ON STAND BY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE LT LOWER OB THRUST REVERSER OUT OF RIG AND RERIGGED IT. MAINTENANCE ALSO REMOVED AND REPLACED THE IB FLEXIBLE CABLE, LT ENGINE BLOCKER DOOR IN THE TWELVE AND 3 O’CLOCK POSITIONS, AND THE LT ENGINE THRUST REVERSER STOW SWITCH CONNECTOR BRACKET FOR PREVENTATIVE MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040601000262004060100026CE 2004 6 1 SDR2004027 120040428A5610NP1588014 WINDSHIELD CESSNA414 414 2075908CE COCKPIT CRACKED A TRBAO OTHER O OTHER CRCRUISE 1 SO21414AF 4140167 DURING CRUISE AT 17,000 FT, THE F/O WINDSHIELD INNER LAYER CRACKED. CREW DECLARED EMERGENCY. REMOVED AND REPLACED WINDSHIELD ASSY. 1L72 3O RTA7CE 20040601000272004060100027EU 2004 6 1 SDR2004026 120040427A5610NP1588012 WINDSHIELD AEROSPATR72 ATR72212 8680945EU COCKPIT CRACKED A TRBAD RETURN TO BLOCK O OTHER CRCRUISE 1 SO21414WF20110 414 F/O`S OUTER LAYER OF WINDSHIELD CRACKED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD. 2H72 4T RTA53EU 20040601000292004060100029CE 2004 6 1 Z5F2004F00001 120040504A3240 LINE CESSNA500 550 2076604CE BRAKE SYSTEM CONTAMINATED E Z5FAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NE03317CS1799 5501019 WHEN TAXIING OUT OF THE CHOCKS, THERE WAS A LOSS OF BRAKING POWER ON THE LT BRAKE, BOTH PILOT AND COPILOT SIDE. SUSPECTED AIR IN BRAKE LINES AFTER MAINTENANCE WAS PERFORMED (LT MASTER CYLINDER). BRAKES WERE BLED. 1L72 4F A22CE 20040601000312004060100031NM 2004 6 1 GAIA04069OP 120040420A3610 CLAMP BOEING727 727251 138408HNM NR 1 ENGINE LOOSE A GAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07252US 19971 NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON JUST AFTER TAKE-OFF. CREW RETURNED AIRCRAFT TO DEPARTURE AERODROME (FWA) WHERE AN UNEVENTFUL LANDING WAS MADE. DUPLICATED PROBLEM DURING GROUND ENGINE RUN. TIGHTENED SEVERAL CLAMPS ON BLEED LINES AND (B) NUT ON SENSE LINES. RE-ADJUSTED STRUT OVERHEAT LOOP. OPS CHECK GOOD ON GROUND DURING ENGINE RUN. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20040601000322004060100032NM 2004 6 1 GAIA04070OP 120040427A3260656021136 ACCESSORY UNIT BOEING727 727223 1384074NM E/E BAY FAULTY A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW076833 20186 GEAR UNSAFE LIGHTS AND TAIL-SKID EXTENDED LIGHT DID NOT EXTINGUISH WHEN LANDING GEAR WAS CYCLED UP. FLIGHT ORIGINALLY SCHEDULED, DIVERTED WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LANDING GEAR ACCY UNIT. SYSTEM CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20040601000332004060100033NM 2004 6 1 04FDEA01478 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000342004060100034NM 2004 6 1 04FDEA01479 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.409, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.407. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000352004060100035NM 2004 6 1 04FDEA01480 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.140. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000382004060100038NM 2004 6 1 04FDEA01483 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.512, MATERIAL REMOVED= 0.003, REMAINING THICKNESS= 0.409. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000392004060100039NM 2004 6 1 04FDEA01484 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.492, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.490. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000412004060100041NM 2004 6 1 04FDEA01486 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG.THK. OF LUG: 0.504, MATERIAL REMOVED: 0.007, REMAINING THK.OF LUG: 0.497. REPAIR CARRIED - OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000422004060100042NM 2004 6 1 04FDEA01487 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.093, FINAL DIAM.: 1.125, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000432004060100043NM 2004 6 1 04FDEA01488 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.397, MATERIAL REMOVED: 0.002, REMAINING THK. OF LUG: 0.395. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000442004060100044NM 2004 6 1 04FDEA01498 120040527A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01,3) FLOORBEAM STA 1110 WL 208 CORRODED UPPER CHORD. REMOVED CORROSION FROM BS 1110 FLOOR BEAM, FOUND TO BE OUT OF LIMITS PER SRM 53- 10-1. ACCESSED AREA, REPLACED UPPER CHORD PER FED EX EA 7-5310-77727, RESTORED ACCESS PER SRM 51-30-2 AND SOPM 20-50-1. 2L73 4F RTA3WE 20040601000452004060100045NM 2004 6 1 04FDEA01499 120040527A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO COMPARTMENT STA 520, WL 163, LBL 39 FRAME DENTED. REMOVED DAMAGE ON FRAME B.S. 520, WL 163, LBL 39 IN A 1 1/2 X 17 1/2 AREA. FABRICATED REPAIR DOUBLER USING 7075-T6 .050 LOT 553781. ALODINED, PRIMED AND INSTALLED IAW 727 SRM 51-30-2, 51-40-3 SH3 AND EA 7-5310-70665. 2L73 4F RTA3WE 20040601000462004060100046GL 2004 6 1 04FDEA01500 220040527A7532 VALVE AIRBUS300 A300F4605R 3930327EU GE CF6 CF66D 30020GL NR 2 ENGINE FAULTY A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25657FE 748 705245 NR 2 ENGINE FAILURE WARNINGS APPEARED ON ECAM ON TAKEOFF AT 70 KTS. REJECTED TAKEOFF. TRIED ANOTHER TAKEOFF, SAME PROBLEM, REJECTED TAKEOFF AGAIN. NR 2 ENGINE WOULD NOT SHUT DOWN IN BLOCKS WITH FUEL LEVER. PULLED NR 2 FIRE HANDLE AND ENGINE WOULD NOT SHUT DOWN FOR 2 MINUTES. PERFORMED ENGINE FIRE TEST ON NR 2 ENGINE, WHEN HP VALVE WAS RAISED LIGHT IN HANDLE DID NOT ILLUMINATE. HP VALVE WILL REQUIRE CHANGE. R&R HMU (P/N 441790) RAN ENG OPS CK . MEM MX. 2L72 4F4 FRTA35EU E23EA 20040601000492004060100049WP 2004 6 1 04FDEA01503 120040527A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT SEALING AREA FOR PANEL 636CB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-42-04 AT MAE. 2L73 4F A22WE 20040601000502004060100050NM 2004 6 1 04FDEA01504 120040528A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND LOWER MOUNT MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-404. ORIG. THK.: 0.514, MATERIAL REMOVED: 0.008, REMAINING THK.: 0.506. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040601000512004060100051NM 2004 6 1 04FDEA01505 120040528A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE OUTBOARD CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-404. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040601000522004060100052NM 2004 6 1 04FDEA01506 120040528A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.221, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040601000532004060100053NM 2004 6 1 04FDEA01507 120040528A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD INBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG. 402-407. ORIG. THK.: 0.415, MATERIAL REMOVED: 0.004, REMAINING THK.: 0.411. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76718 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040601000552004060100055WP 2004 6 1 04FDEA01470 120040526A5414 PANEL DOUG DC10 DC1010 3022110WP NACELLE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 PNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAINER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01. 2L73 4F A22WE 20040601000572004060100057WP 2004 6 1 04FDEA01472 120040526A5753ARC1495510 VANE DOUG DC10 DC1010 3022110WP FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-5750-77429 WINGS ARC1455-510 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77429. 2L73 4F A22WE 20040601000582004060100058WP 2004 6 1 04FDEA01096 120040424A7120NSL60235 MOUNT DOUG DC10 DC1010 3022110WP NR 3 ENGINE OUT OF POSITION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25365FE 46601 NUMBER 3 ENGINE AFT MOUNT BEARING MIGRATING. REMOVED AND REPLACED NUMBER 3 ENGINE AFT MOUNT IAW DC-10 MM 71-20-02-2. 2L73 4F A22WE 20040601000612004060100061WP 2004 6 1 04FDEA01092 120040424A5751ARC12837 SKIN DOUG DC10 DC1010 3022110WP LT AILERON WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25365FE 46601 LEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LIMITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALLED ON N00519. 2L73 4F A22WE 20040601000652004060100065NM 2004 6 1 04FDEA01063 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040601000662004060100066NM 2004 6 1 04FDEA01064 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936, WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040601000672004060100067NM 2004 6 1 04FDEA01065 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040601000682004060100068EU 2004 6 1 04FDEA01046 120040422A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN CABIN FR 41 UP TO FR 44, NR 4 RIGHT SEAT TRACK NOTED CORROSIONS ON FOUR AREAS AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040601000702004060100070EU 2004 6 1 04FDEA01048 120040422A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC 4TH SEAT TRACK RT SIDE FROM CENTER LINE AT FR 27 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED DAMAGED SECTION IAW A300-600 SRM 53-10-16 FIG 201. 2L72 4F RTA35EU 20040601000712004060100071EU 2004 6 1 04FDEA01049 120040422A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC FLOOR PAN PANEL BETWEEN RT SIDE OF 3 AND 4 SEAT TRACK AT FR 27 HAS FOUR EACH AREAS OF CORROSION UPPER SURFACE. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040601000722004060100072EU 2004 6 1 04FDEA01050 120040422A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC FLOOR PAN PANEL BETWEEN 3 AND SEAT TRACK 4 AT FR 26 RT SIDE HAS 3 EA AREAS OF CORROSION UPPER SURFACE. REMOVED AND REPLACED THRUST PLATE IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040601000732004060100073NM 2004 6 1 SWAA041408 120040517A143065C16820 FASTENER BOEING737 7375H4 138449DNM GIRT BAR HOOK LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE HOOK FASTENERS PER MM. 2L72 4F RTA16WE 20040601000742004060100074NM 2004 6 1 SWAA041410 120040507A3350604222 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29421LV 32452 DURING SPV, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040601000752004060100075NM 2004 6 1 SWAA041409 120040517A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29421LV 32452 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT R2 DOOR INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040601000762004060100076NM 2004 6 1 SWAA041411 120040517A3350D71701100 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29730SW 27862 DURING SCHEDULED 5Y CHECK, FOUND EMERGENCY EXIT LIGHTS AT R1 AND L1 DOORS INOP. REMOVED AND REPLACED R1 AND L1 EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040601000772004060100077 2004 6 1 SWAA041505 420040527A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 R1 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040601000822004060100082NM 2004 6 1 SWAA041510 120040527A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT LOWER FRAME, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040601000842004060100084NM 2004 6 1 SWAA041488 120040525A3397BR2013 WIRE BOEING737 7372T4 1384492NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS WIRES BROKEN AND EEPLS COVERS LOOSE AT OVERWING EXIT. REPAIRED EEPLS WIRES AND SECURED COVERS PER MM. 2L72 4F A16WE 20040601000852004060100085 2004 6 1 SWAA041489 420040525A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040601000862004060100086 2004 6 1 SWAA041490 420040525A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE LOW PRESSURE, IND. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040526001322004052600132NM 2004 5 26 0400696718 120040505A5312 BULKHEAD BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING H-CHECK FOUND CRACK IN BULKHEAD CHORD AT BS 1000 FROM 36L TO 40L. REPAIRED PER EA 67-165121. 2L74 4F A20WE 20040526001332004052600133NM 2004 5 26 QXEA200400310 120040506A524085247255003 SEAL BOMBDRDHC8 DHC8401 1390041NM ZONE 800 MISINSTALLED A QXEAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09539DS3507 4016 BOTH FLIGHT ATTENDANTS WERE UNABLE TO OPEN OR CLOSE THE REAR SERVICE DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE SEAL PROTRUDING ON BOTH THE FORE AND AFT EDGES. THE DOOR SEAL WAS TRIMMED AS REQUIRED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040526001372004052600137NM 2004 5 26 AALA20040539 120040508A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 EMERGENCY LIGHT AT SEAT 6E INOPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA2NM 20040526001382004052600138NM 2004 5 26 AALA20040540 120040510A1420 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21370AA 25197 MIA EMERGENCY ESCAPE LIGHT AT SEAT 29H INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED LOOSE CONNECTOR FOR EMERGENCY ESCAPE LIGHT AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20040526001402004052600140EU 2004 5 26 AALA20040542 120040510A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211405J 11356 EMERGENCY LIGHT ON CEILING AT ROW 9 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON CEILING AT ROW 9 PER WORKCARD 0910. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RT 20040526001412004052600141NM 2004 5 26 AALA20040545 120040510A3350 FUSE BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21750AN 30259 LT FLOOR PROXIMITY LIGHTS FROM ROWS 20 TO 26 INOPERATIVE. FOUND FUSE BLOWN IN MODULE 33404 BATTERY PACK. REPLACED FUSE IN MODULE 33404 BATTERY PACK FOR FLOOR PROXIMITY LIGHTS FROM ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTT00001SE 20040526001492004052600149NM 2004 5 26 2004UALA00431 120040502A5230451T16042 SUPPORT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 FWD PIT CARGO DOOR LOWER SUPPORT IS CRACKED AT APPROX BS 610. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT. 2L72 4F4 FRTA1NM E24NE 20040526001562004052600156NM 2004 5 26 2004UALA00439 120040505A2612 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO FIRE ILLUMINATED A UALAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP29177UA 24384 TOP OF DESCENT CREW GOT AFT CARGO FIRE INDICATOR LIGHT. DECLARED EMERGENCY. USED ONE FIRE BOTTLE AND LIGHT DID NOT EXTINGUISH. NORMAL LANDING. PROBABLE CAUSE A COMBINATION OF AN INTERMITTENT SMOKE DETECTOR AND MOISTURE FROM THE CARGO. SMOKE DETECTOR WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 20040526001612004052600161EA 2004 5 26 SWIA200413295 120040503A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07597SW 7293 FLOOR SUPPORT ANGLES AT FS280, LBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 INBOARD AND OUTBOARD AND LBL 9 INBOARD AND OUTBOARD IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, AND EO 601R-53-4942. SEE RII 53-401. 2L72 4F RTA21EA 20040527000042004052700004NM 2004 5 27 SWAA041374 120040513A5240651647 GATE BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR UPPER GATE CRACKED. REMOVED AND REPLACED R1 DOOR UPPER GATE PER MM. 2L72 4F RTA16WE 20040527000072004052700007NM 2004 5 27 SWAA041377 120040514A3350OL3071BPEGPL LAMP BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C3 CHECK, FOUND LAST LIGHT ON RT EEPLS INOP. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20040527000102004052700010NM 2004 5 27 SWAA041380 120040514A53306545767 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29104SW 23110 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 437, AFT OF RADIO ALT ANTENNA, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040527000122004052700012NM 2004 5 27 SWAA041382 120040514A575465C26603 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND NR 4 L/E SLAT DELAMINATED. REPAIRED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20040527000262004052700026NM 2004 5 27 DL76K040404 120040506A2132SETLOC420M INDICATOR BOEING767 767332 1382001NM COCKPIT FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27171DZ 29690 IRR // AUTO 1 AND AUTO 2 WENT INOP AT 1000 FT AGL. UNABLE TO READ CABIN PRESSURE OR RATE WHEN IN MANUAL - CABIN DIFF PRESSURE OK AND OUTFLOW VALVE WAS OK IN MANUAL, RESET C/B W/MAINT CONCURENCE NO HELP - DIVERTED TO MCO. REPLACED CABIN PRESSURIZATION PANEL INDICATOR. BIT BOTH AUTO CONTROLLERS WITH NO FAULTS SHOWN ON EITHER CONTROLLER. PRESSURIZED A/C SEVERAL TIMES. DIFF IND, CABIN RATE AND CABIN ALT ALL CK OK PER MM 21-33-01 2L72 4F RTA1NM 20040527000322004052700032NM 2004 5 27 DL73S040411 120040507A3350276005 FUSE BOEING737 737232 1384475NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27311DL 23083 AFT LT BULLNOSE EMERGENCY LIGHTS INOPERATIVE, REPLACED BATTERY. NO HELP. REPLACED FUSES ON CHARGER. CHECKS GOOD. 2L72 4F RTA16WE 20040527000522004052700052NM 2004 5 27 SWAA041459 120040522A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED RON, FOUND R1 DOOR CUTOUT UPPER AFT STOP SKIN CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040527000822004052700082NM 2004 5 27 DL76G040427 120040510A3260 PROXIMITY SENSOR BOEING767 767332 1382001NM MLG DIRTY A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO271605 30198 GEAR DISAGREE WITH GEAR DOORS EICAS MESSAGE AFTER RAISING GEAR LEVER AND THE THREE GEAR LIGHTS EXTINGUISHED. CYCLED GEAR DOWN THEN UP. AGAIN SAME INDICATIONS. GEAR DOWN LOCKED OK. CLEANING PROXIMITY SWITCHES ALL GEARS AND PERFORMED OPERATIONAL TEST OF MAIN AND NOSE LANDING GEAR NORMAL. EXTENSION AND RETRACTION CHECKED ALL DOORS ALIGNED WITH THE BODY CONTOUR. BITE PSEU. NO FAULTS. REPLACED PSEU AS A PRECAUTION PER M.M. 32-09-04 AND TESTED GOOD. 2L72 4F RTA1NM 20040527000872004052700087SO 2004 5 27 RAIA00405005 120040508A1420D3899926FA98SN CONNECTOR EMB 145 EMB145LR 3260212SO MLG DETERIORATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03815HK 145048 5697 -STL - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NLG WOW SWITCH CONNECTOR AND OPS CHECKED GOOD DURING RETRACTION CHECK. 2L72 4T RTT00011AT 20040527000882004052700088CE 2004 5 27 61073 120040503A1420MS3476W2241 CONNECTOR BEECH 1900 1900D 1154162CE ANNUCIATOR BURNED A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE07126YV UE126 CREW REPORTED ON APPROACH ANNUNICATOR C.B. TRIPPED. IT WAS RESET AND POPPED AGAIN. THERE WAS A FAINT BURNED ODOR IN THE CABIN. LANDED WITH NO FURTHER INCIDENT. R&R FEED THRU CONNECTOR. 2L72 4T RTA24CE 20040527000962004052700096NM 2004 5 27 QXEA200400311 120040510A3260401020101 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM NLG FAULTY A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09410QX5710 4053 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE GEAR FAILED TO RETRACT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NOSE LANDING GEAR PROXIMITY SENSOR. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040527000972004052700097EA 2004 5 27 COMA0460307 120040510A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA MAINS MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01951CA 7091 FLIGHT 5081 GEAR DISAGREE WARNING ON EXTENSION. COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS NORMAL. 2L72 4F RTA21EA 20040527001172004052700117WP 2004 5 27 04FDEA01095 120040424A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25365FE 46601 MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 8.5 HAS BROKEN SCALLOP AT FS 755. REPLACED SECTION OF SEAT TRACK FROM FS 725 TO 785 AT RBL 8.5 IAW DC-10 SRM 53-70-00 VOL 1. 2L73 4F A22WE 20040528000062004052800006NM 2004 5 28 DL73S040432 120040513A53156546800508 FLOORBEAM BOEING737 737247 138448DNM PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 CRACKS WERE NOTED IN THE BS520 FLOORBEAM UPPER RADII WHERE THE SEAT TRACKS CROSS OVER THE BEAM. DAMAGE WAS REMOVED AND THE FLOORBEAM REPAIRED IAW ERA 089860-14. 2L72 4F4 F A16WE E2EA 20040528000092004052800009EA 2004 5 28 2004F00144 220040517A7414 BREAKER POINTS SLICK M3637 PIPER PA32 PA32300 7103212SO LYC O540 IGO540* 41532EA MAGNETO BROKEN D O OTHER O OTHER NRNOT REPORTED 1 AL058127K10 03060080 327940268 SLICK MAG MODEL NUMBER M3637 CONTACT POINTS BROKE. 10 HOURS SINCE NEW. 1L71 3O3 O A3SO 1E11 20040528000192004052800019WP 2004 5 28 ABXA040181 120040519A216160714621 CONTROLLER DOUG DC9 DC933F 302207AWP CABIN TEMP DEFECTIVE A ABXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23931AX407 47384 ON TAXI, LEFT PACK CYCLED ON AND OFF A FEW TIMES, BUT OPS NORMALLY BEFORE TAKE-OFF. AT 3500 FT LEFT PACK SHUTDOWN, AT 4000 FT RIGHT PACK SHUTDOWN. THEY BOTH CYCLED ON AND OFF. AT 10000 FT TURNED EACH PACK OFF PER ABNORMAL. ONE AT A TIME TO COOL DOWN. AFTER TURNING THE PACKS ON AGAIN, COCKPIT FILLED UP WITH SMOKE THAT HAD AN OILY SMELL. TURNED BOTH PACKS OFF AND RETURNED TO CLT AIRPORT. REPLACED BOTH WATER SEPARATOR BAGS, BOTH DIRTY. CHECKED BOTH ENGINES INLET AND EXHAUST, CHECKED BOTH ACM'S FOR OIL SERVICING. FOUND LEFT PACK INTERMITTENT IN AUTO POSITION. REMOVED AND REPLACED LEFT TEMP CONTROLLER IAW DC-9 MM 21-60-00-2. OPS CHECKED GOOD IAW DC-9 MM 21-60-00-2-0001. 2L72 4F A6WE 20040528000202004052800020CE 2004 5 28 GLBA20030629 120040519A52101294000321 STRUCTURE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA CABIN DOOR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03202UX UE202 CABIN DOOR HAS CORRODED AREA BY BUTTON, REPAIRED. 2L72 4T3 TRTA24CE E2NE 20040528000292004052800029SO 2004 5 28 C2XA04CL057 120040521A2120 SMOKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2713992 145284 STL FLIGHT NR 2364 THE CREW REPORTED A STRONG ODOR/LIGHT SMOKE IN THE CABIN WITH BOTH APU BLEEDS AND ENGINE BLEEDS ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF BOTH PACKS. NO DEFECTS WERE FOUND. 2L72 4T4 FRTT00011ATTE6CH 20040528000302004052800030EU 2004 5 28 MALA040411 120040514A351035916D52 OXYGEN MASK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT LEAKING A MALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15426XJ 340B426 ON TAXI OUT THE O2 DEPLETED FROM 500 TO 50 RAPIDLY AND O2 LIGHT ILLUMINATED. THE MASK SEEM TO BE HOLDING PRESSURE. SERVICED O2 TO 1600PSI. AFTER 20MIN O2 BLED DOWN TO 1500PSI. DISCONNECTED O2 MASKS AND WAITED 20 MIN. PRESSURE REMAINED AT 1500PSI, REPLACED CAPT AND F/OS MASKS. CAPT S/N OFF 1815 S/N ON 7604. S/N OFF 3745 S/N ON 3581. P/N BOTH OFF/ON 359-16D52. RESERVICED TO 1600 PSI. LEAK CHECK GOOD. 20 MIN. CHECK SERVICED IAW SF340 MM CHP 12. 2L72 4T4 TRTA52EU E8NE 20040528000462004052800046EU 2004 5 28 AWXA200400561 120040521A3350Z040H0004110 DEU AIRBUS320 A320231 3930325EU CABIN FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW38215 271 PHX - EEL DURING 4-DAY CHECK: FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FAILED AT CIDS PANEL. MAINTENANCE REMOVED AND REPLACED DECODER ENCODER UNIT (DEU) B (300RH5) IAW AMM 23-73-47, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040528000482004052800048NM 2004 5 28 AWXA200400563 120040515A5320D5347112420000 PLATE AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 MCN - MAJOR REPAIR - DURING B-03 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE AT THE AFT END OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-3, 8, & 14-17. 2L72 4F4 FRTA28NM E311NE 20040528000692004052800069WP 2004 5 28 GTIA040420 120040411A5313 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 AFT PIT STA 1256 LONGERON 28R CORROSION UNDER LIP OF LONGERON. REMOVED DAMAGED LONGERON FROM STA 1255-1338. FABRICATED NEW LONGERON. INSTALLED LONGERON. 2L72 4F4 F A6WE E2EA 20040528000892004052800089NM 2004 5 28 UPS04542419 120040523A4990 OIL SYSTEM BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE APU OVERSERVICED A IPXAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 SO01414UP 23854 INSPECTION TYPE:N/A ATB - APU FAILED IN FLT W/RT ENG GEN ON MEL. FOUND OIL OVER SERVICED. NO FAULTS FOUND ON APU CONTROLLER GROUND. RAN APU A/C OK FOR SERVICE. 2L72 4F4 FRTA2NM E17NE 20040601000032004060100003NE 2004 6 1 DXTA200400314 220040523A72003050005 ENGINE AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE NR 1 MALFUNCTIONED E DXTAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL07269QS2181 169 P105136 AT FL370 NR 1 ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. PRECAUTIONARY SHUT DOWN NR 1 ENGINE AND DIVERTED TO IA, AIRCRAFT LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2K73 4F4 FRTA50NM E44NE 20040601000102004060100010SO 2004 6 1 CHQA000499 120040526A3350 CONNECTOR EMB 135 EMB135LR 3260305SO CABIN DISCONNECTED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11842 145661 ROW 1 EXIT LOCATOR SIGN IS INOP. RECONNECTED CONNECTOR PLUG IAW AMM 33-50-15. OPS CHECK GOOD. 2L72 4F RTT00011AT 20040601000132004060100013NM 2004 6 1 PCAA0405211 120040525A323454C546349 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NLG FAULTY A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13812EX31502 312 FLIGHT NR 3920 REPORTED THEIR NOSE GEAR DOOR LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION WITH AN ASSOCIATED LOUD NOISE FROM THE NOSE GEAR AREA. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR SOLENOID SEQUENCE VALVE AND RELAY 3261-K7. SYSTEM WAS OPERATIONAL CHECKED AND ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040601000212004060100021EA 2004 6 1 ASOA04325 120040501A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27863AS 7487 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT NEAR ROW 8 WAS FOUND MISSING. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT NEAR ROW 8. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040601000252004060100025EU 2004 6 1 SDR2004025 120040420A275070481 CONTROL SWITCH AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT FAILED A TRBAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO21420AT 420 FLAPS DID NOT EXTEND AND DECLARED EMERGENCY LANDING. REMOVED AND REPLACED FLAP CONTROL SWITCH. 2H72 4T4 TRTA53EU E20NE 20040601000282004060100028CE 2004 6 1 Z5F2004F00000 120040505A3240 LINE CESSNA500 550 2076604CE PWA 530 PW530A NE BRAKE SYSTEM CONTAMINATED E Z5FAK NONE O OTHER LDLANDING 1 NE03317CS 5501019 WHEN LANDING, THERE WAS A LOSS OF BRAKING POWER ON THE LT BRAKE, COPILOTS SIDE. THE PEDAL WENT TO THE WALL. PILOT APPLIED BRAKES TO STOP THE AIRCRAFT. PILOT REPORTED HIS BRAKE WAS 2-3 INCHES FORWARD OF RT BRAKE PEDAL. SUSPECTED AIR STILL IN BRAKE LINES AND OR COMPONENTS. BRAKES WERE BLED AGAIN. 1L72 4F4 F A22CE E00053EN 20040601000302004060100030NM 2004 6 1 GAIA04068OP 120040401A575165217232 SKIN PANEL BOEING727 727251 138408HNM RT AILERON MISSING A GAIAK NONE O OTHER ININSP/MAINT 1 SW07279US 21158 ON POST FLIGHT INSPECTION FOUND RT OB AILERON DAMAGE AT IB LOWER SURFACE EDGE IB PANEL MISSING FROM AILERON. AIRCRAFT LANDED WITHOUT INCIDENT. INSTALLED MISSING PANEL AT IB HINGE LEADING EDGE. REPAIRED DAMAGED IB LOWER SURFACE EDGE IAW SRM, SHEET (5) PG 169. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20040601000472004060100047WP 2004 6 1 04FDEA01501 120040527A5340ANB7393501 SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5310-77427 FUSELAGE MAIN FRAME STRUCTURE ASSY INBOARD FLAP SUPPORT CORROSION REPAIR, P/N A NB7393-501. COMPLIED WITH EA 8-5310-77427 FUSELAGE MAIN FRAME STRUCTURE ASSY INBOARD FLAP SUPPORT CORROSION REPAIR P/N ANB7393-501 AT MAE. 2L73 4F A22WE 20040601000592004060100059WP 2004 6 1 04FDEA01097 120040424A7120AUB70251354104 MOUNT DOUG DC10 DC1010 3022110WP NR 1 ENGINE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25365FE 46601 NUMBER 1 PYLON AFT MOUNT BORE HAS CORROSION. REMOVED DAMAGE BY B/H IAW DRAWING AUB7025 AND AUB7034. LOCATED DRILLED AND DEBURRED NEW B/H PART NUMBER AUB7025-13 PO 440915.2 IAW DRAWING AUB7025 AND AUB7034. INSTALLED B/H PART NUMBER AUB7025-13 IAW DRAWING AUB7025 AND AUB7034. 2L73 4F A22WE 20040601000622004060100062NM 2004 6 1 04FDEA01039 120040422A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040601000782004060100078 2004 6 1 SWAA041506 420040527A2565D31354 SLIDE BOEING737 7372H4 138448CNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED PM CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040601000802004060100080NM 2004 6 1 SWAA041508 120040527A53106546809 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 946, STRINGER 17R, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20040601000812004060100081NM 2004 6 1 SWAA041509 120040527A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, BL 0, CRACKED. REPAIRED DOME CAP PER EA. 2L72 4F RTA16WE 20040601000832004060100083 2004 6 1 SWAA041487 420040525A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 L2 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040601000872004060100087NM 2004 6 1 SWAA041491 120040525A53146545866 PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C4 CHECK, FOUND LEFT KEELBEAM PANEL AT BS 660, BS 700, CRACKED. REPAIRED KEELBEAM PANEL PER SRM. 2L72 4F RTA16WE 20040601000882004060100088NM 2004 6 1 SWAA041492 120040525A57536546430190 SKIN BOEING737 7373H4 1384600NM RT FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040601000912004060100091NM 2004 6 1 SWAA041495 120040525A53116546540 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND FRAME AND FRAME WEB AT BS 639, STRINGER 17R, CRACKED. REPAIRED FRAME AND FRAME WEB PER ER. 2L72 4F RTA16WE 20040601000922004060100092NM 2004 6 1 SWAA041482 120040524A256065659723 PLATE BOEING737 7373H4 1384600NM CABIN CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FLOOR MOUNT PLATES CORRODED. REMOVED AND REPLACED GIRT BAR MOUNT PLATES PER SRM AND MM. 2L72 4F RTA16WE 20040601000932004060100093NM 2004 6 1 SWAA041483 120040524A53156546812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040601000942004060100094NM 2004 6 1 SWAA041484 120040524A53116545808 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294.5, RBL, 54, WL 209, CORRODED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040601000952004060100095NM 2004 6 1 SWAA041485 120040524A53116546538 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 616, RBL 65, WL 202, CRACKED. REPAIRED FRAME CHORD PER ER. 2L72 4F RTA16WE 20040601000962004060100096NM 2004 6 1 SWAA041486 120040524A55116547508 RIB BOEING737 7373H4 1384600NM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND LEFT HORIZONTAL STAB RIB CHORD AT STAB STATION 120, CRACKED. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040601000982004060100098NM 2004 6 1 SWAA041414 120040518A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED RON, FOUND LOWER KEELBEAM CHORD AT BS 727 + 2, STRINGER 27R, CORRODED. REMOVED AND REPLACED LOWER KEELBEAM CHORD PER EA. 2L72 4F RTA16WE 20040601000992004060100099NM 2004 6 1 SWAA041415 120040518A256065C19901 CABLE BOEING737 7372H4 138448CNM L1 & R1 DOOR MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C1 CHECK, FOUND L1 AND R1 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L1 AND R1 DOOR EVAC SLIDE CABLES PER MM. 2L72 4F A16WE 20040601001032004060100103EA 2004 6 1 ASOA04328 120040503A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE T/E FLAP MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO27923EV1898 7826 DURING APPROACH, THE CREW RECEIVED A FLAPS FAIL AMBER CAUTION MESSAGE. THE FLAPS INDICATED ZERO DEGREES ON THE PRIMARY EICAS AND SYNOPTIC PAGES AND THE FLAPS HAD NOT BEEN CALLED FOR PRIOR TO THE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT DIVERTED, PERFORMING A ZERO FLAP LANDING AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT FLAP BRAKE POSITION SENSOR UNIT (BPSU) AND RIGGED THE FLAPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040601001042004060100104SO 2004 6 1 C2XA04SH323 120040527A532014528737001 STIFFENER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE T REINFORCEMENT ON EXTERNAL STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040601001062004060100106WP 2004 6 1 04FDEA01468 120040526A2560ABE702021 MOUNT BRACKET DOUG DC10 DC1010 3022110WP COCKPIT BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 CAPTAINS ESCAPE ROPE MOUNT BRACKET IS BENT. CLOSING ACTION ON 05/25/04 ON N/R N00025. REMOVED AND REPLACED CAPTAINS ESCAPE ROPE MOUNT BRACKET IAW SRM 51-31-01. 2L73 4F A22WE 20040601001082004060100108NM 2004 6 1 04FDEA01475 120040526A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20040601001092004060100109NM 2004 6 1 04FDEA01476 120040526A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING - OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - L/H OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20040601001112004060100111NM 2004 6 1 04FDEA01489 120040526A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING OB FLAP AFT OB HINGE, FOUND OB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.196, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20040601001122004060100112NM 2004 6 1 04FDEA01490 120040526A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. THK. OF LUG: 0.402, MATERIAL REMOVED: 0.002, REMAINING THK.OF LUG: 0.400. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20040601001132004060100113NM 2004 6 1 04FDEA01491 120040526A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. DIA: 1.062, FINAL DIA: 1.191. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F4 FRTA22WE E13NE 20040601001142004060100114WP 2004 6 1 04FDEA01492 120040526A5753ANB70821 FITTING DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-77425 WINGS-LT IB FLAP, ROLLER FITTING ATTACH HOLES CORRODED AT MAE(PART 1 INTIAL IS COMPLIED WITH AND WILL REQUIRE A FOLLOW UP ACTION TO BE COMPLIED WITH. COMPLIED WITH AS STATED IN UPDATE. 2L73 4F4 F A22WE E23EA 20040601001172004060100117WP 2004 6 1 04FDEA01495 120040527A5753ARC0154 HINGE BRACKET DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5740-77418 WINGS RT INBD FLAP, FWD HINGE ASSY PIVOT BORE CORROSION. COMPLIED WITH EA NR 8-5740-77418 WINGS-LT IB FLAP, FWD HINGE ASSY PIVOT BORE CORROSION, PART 1 ONLY. COMPLIED WITH AS STATED IN UPDATE. 2L73 4F4 F A22WE E23EA 20040601001222004060100122NM 2004 6 1 UPS04242427 120040512A5754 BRACKET BOEING727 72725C 138400HNM L/E SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE: C BRACKET INSIDE NR 7 SLAT AT OB TRACK CRACKED. REPAIRED IAW SRM 57-50-3. 2L73 4F A3WE 20040601001232004060100123NM 2004 6 1 UPS04242428 120040511A2560 RING BOEING727 72725C 138400HNM EVAC SLIDE DISCONNECTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE: C SLIDE LATCH RING ON FWD E DOOR ESCAPE SLIDE AND GIRT BAR TO SLIDE COMPARTMENT LATCH CHAIN FOUND DISCONNECTED. REPLACED RING AND CONNECTED CHAIN TO SLIDE LATCH IAW 25 -60-04. 2L73 4F A3WE 20040601001252004060100125NM 2004 6 1 UPS04242431 120040511A5330 LAP JOINT BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C CORROSION AT LAP JOINT, STR 6L, BS 695 - BS 718. REPAIRED IAW SRM 53-30-3, FIG 4. 2L73 4F A3WE 20040601001262004060100126NM 2004 6 1 UPS04242432 120040511A5312 PRESSURE PANEL BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C NWW PRESSURE WEB HAS A CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT BS 290 RT. REPAIRED IAW SRM 51-40-02. 2L73 4F A3WE 20040601001272004060100127NM 2004 6 1 UPS04242433 120040511A5347 SEAT TRACK BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C CORROSION ON SEAT TRACK FLANGE AT BS 495, RBL 62.5. REPAIRED IAW SRM 53-10-5, FIG 1. 2L73 4F A3WE 20040601001312004060100131NM 2004 6 1 UPS04242437 120040514A7120 MOUNT BOEING727 72725C 138400HNM PWA JT8 JT8D5 52046NE NR 1 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C NR 1 ENG FWD MOUNT HOLES HAVE PITTING CORROSION IN BOTH IB HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592. 2L73 4F4 F A3WE E2EA 20040601001322004060100132NM 2004 6 1 UPS04242438 120040514A7120 MOUNT BOEING727 72725C 138400HNM PWA JT8 JT8D5 52046NE NR 3 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT HOLE HAVE PITTING CORROSION IN BOTH I/B HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592. 2L73 4F4 F A3WE E2EA 20040601001342004060100134NE 2004 6 1 NACA20040022 220040527A8530356994 CYLINDER PWA CB3 DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE DEFECTIVE A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL0399330450 450 P34459 43576 P34459 DISCREPANCY: NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND BACK FIRING AT CRUISE. NR 1 CYLINDER LT SIDE SHORTED SECONDARY. REPLACED NR 1 CYLINDER DUE TO FAILED RINGLAND. 2L74 4R4 R 6A3 5E8 20040601001352004060100135NM 2004 6 1 QXEA200400370 120040526A5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - RIGHT WING LE UPPER ATTACH BRACKET IS CRACKED IN THE RADIUS. MOUNTED ON FORWARD SPAR ST WS YW138.000. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T4 TRTA13NM E20NE 20040601001372004060100137NM 2004 6 1 QXEA200400371 120040526A5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - RT WING LE LOWER ATTACH BRACKET IS CRACKED IN THE RADIUS, MOUNTED ON FORWARD SPAR AT WS YW 138.000. REPAIRED IAW DHC-9 SRM 51-40-00. 2H72 4T4 TRTA13NM E20NE 20040601001382004060100138NM 2004 6 1 QXEA200400372 120040526A5730 PLATE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE RT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - LIGHT CHAFING ON LADDER PLATE UNDER STRESS PANEL 622AT AT IB END, ON REAR SIDE FROM YW90 TO YW106 AND ON FORWARD SIDE FROM YW90 TO YW139. REPAIRED IAW DHC-8-200 MM 20-32-02 AND 20-34-08. 2H72 4T4 TRTA13NM E20NE 20040601001402004060100140NM 2004 6 1 QXEA200400374 120040526A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - SEAT TRACK 4 HAS CORROSION ON OB FLANGE FROM STATION X202 TO X210 AROUND RIVET HEADS. REPLACED NR 4 SEAT TRACK. 2H72 4T4 TRTA13NM E20NE 20040601001422004060100142NM 2004 6 1 QXEA200400367 120040526A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - SEAT TRACK 4 HAS LIGHT CHAFE THROUGH PRIMER FROM STATION X315 TO X328. REPLACED NR 4 SEAT TRACK. 2H72 4T4 TRTA13NM E20NE 20040601001442004060100144NM 2004 6 1 QXEA200400365 120040526A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - SEAT TRACK NR 4 HAS CORROSION ON TOP OF TRACK AT APPROXIMATELY STATION X253. REPLACED NR 4 SEAT TRACK. 2H72 4T4 TRTA13NM E20NE 20040601001462004060100146NM 2004 6 1 QXEA200400368 120040526A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - SEAT TRACK NR 4 HAS AREA OF CORROSION IN CENTER OF TRACK AT STATION X377. REPLACED NR 4 SEAT TRACK. 2H72 4T4 TRTA13NM E20NE 20040601001472004060100147NM 2004 6 1 QXEA200400360 120040524A1430 RIVET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE CARGO DOOR LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX-AFT CARGO DOOR SKIN HAS NUMEROUS RIVETS SHOWING WORK TRAILS AND MISSING PAINT INDICATING RIVET MOVEMENT. REPAIRED IAW D-8 200 SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040601001492004060100149WP 2004 6 1 AALA20040591 120040526A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E2EA 20040601001522004060100152NM 2004 6 1 AALA20040594 120040528A3350 CONNECTOR BOEING767 767323 1385205NM GE CF6 CF680 30025NE CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21357AA 24038 EMERGENCY LIGHT AT SEAT 35H INOPERATIVE. FOUND LOOSE CONNECTOR. TIGHTENED AND SECURED EMERGENCY LIGHT CONNECTOR AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20040601001552004060100155SO 2004 6 1 C2XA04SH332 120040529A533014520554001 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 19A AND STRINGER 12L. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-22-01 STEP 6 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040601001572004060100157NE 2004 6 1 DHL2004805005 220040528A7314 PUMP DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 1 ENGINE MALFUNCTIONED A DHLAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO01805DH 46125 693219 25 MIN AFTER SETTING CRUISE THRUST, FL 360, ENGINE NR 1 FLAMED OUT. ENGINE INSTRUMENTS NORMAL, DESCENDED TO FL 240 AND INITIATED IN-FLIGHT ENGINE START PROCEDURE, ENGINE START NORMAL, CLIMBED BACK TO FL 360. ALL ENGINE INDICATIONS NORMAL. COMPLETED ALL EMERGENCY CHECKLIST AND ABNORMAL PROCEDURES IAW SOP. REPLACED NR 1 ENGINE DRIVEN FUEL PUMP IAW M/M 73-10-1. ALSO REPLACED FUEL FILTER (MAIN) IAW M/M 73-11-10 (P/N: NR CH0697101552M00 FILTER) PERFORMED SUCCESSFUL LEAK CHECK AND MAX. POWER ASSURANCE RUN (ALL PARAMETERS WITHIN LIMITS) IAW JRH 11.8 AND 13.3. AIRCRAFT OK FOR SERVICE. 2L74 4F4 FRT4A25 E2GL 20040601001602004060100160EU 2004 6 1 MALA040417 120040526A2932 PRESSURE SWITCH SAAB SF340 SF340A 7850100EU HYD SYSTEM INOPERATIVE A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15106XJ 340A106 HYDRAULIC LIGHT ILLUMINATED AFTER SELECTING GEAR RETRACTION. MAIN PRESSURE DROPS TO 1800 PSI FOR 3-5 SECONDS THEN GOES UP. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE SWITCH 9ML IAW SF 340 MM 29-10-45 OPS AND LEAK CHECKS GOOD ALSO REPAIRED GROUND WIRE AT MAIN HYDRAULIC PRESSURE TRANSDUCER CONNECTOR PLUG. ALL OPS CHECKS GOOD. 2L72 4T RTA52EU 20040601001612004060100161EU 2004 6 1 MALA040421 120040528A3350 SIGN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN MISSING A MALAK NONE O OTHER NRNOT REPORTED 1 GL15370PX 340B300 EXIT SIGN ABOVE SEAT 6A IS MISSING. MAINTENANCE REPLACED MISSING COVER WITH SERVICEABLE ONE AS NEEDED. SECURITY CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20040601001632004060100163EU 2004 6 1 MALA040420 120040526A2560 CAP BAC 146 AVRO146RJ85A1500097EU PAX DOOR DIRTY A MALAK NONE O OTHER ININSP/MAINT 1 GL15508XJ E2318 CABIN DOOR FORWARD RT SIDE DOES NOT SHOW YELLOW MARKINGS ON GIRT BAR WHEN DOOR IS ARMED. MAINTENANCE INSPECTED RT FWD CABIN SERVICE DOOR GIRT BAR AND SLIDE ASSEMBLY. OPERATES NORMALLY. CLEANED GIRT BAR END CAPS AND CYCLED SEVERAL TIMES, OPERATION NORMAL AND ACCEPTABLE. 2H74 4F RTA49EU 20040601001652004060100165WP 2004 6 1 P9RA20040013 120040528A7312773482 FUEL HEATER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE RUPTURED A P9RAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO11135NJ 49440 717379 IN CRUISE FLIGHT, CZM-IAH, NR1 ENGINE FIRE WARNING ANNUNCIATED. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO CZM WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE FUEL HEAT MANIFOLD, FIRE BOTTLE AND BOTTLE SQUIBS. 2L72 4F4 F A6WE E9NE 20040601001672004060100167NM 2004 6 1 SWAA041417 120040518A531069353656 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND SHEAR TIES AT BS 360, BELOW AND ABOVE STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040601001692004060100169NM 2004 6 1 SWAA041419 120040518A534065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND STRINGER CLIPS AT BS 500C AND BS 500D, STRINGER 9L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040601001702004060100170NM 2004 6 1 SWAA041420 120040518A5313BAC1498 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND STRINGER 20L AT BS 727D + 4, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040602000042004060200004NM 2004 6 2 04FDEA01512 120040528A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED ALLOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2L73 4F RTA22WE 20040602000052004060200005EU 2004 6 2 04FDEA01513 120040528A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK NR 4L SECTION FROM FR 74 TO FR 80/82 HAS 3 EA AREAS OF CORROSION, INCLUDING ON AND UNDER SCALLOPS, BETWEEN FR 74 AND FR 75, 10 INCHES AFT OF FR 75, 3 INCHES FWD OF FR 76. REMOVED CORROSION FROM SEAT TRACK, MAT'L LOSS AT AREAS AND ARE OUT OF LIMITS IAW SRM 53-10-16. REMOVED DAMAGED SECTION SEAT TRACK, LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK SECTION FROM FR 74 TO FR 76/77 IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040602000072004060200007EU 2004 6 2 04FDEA01515 120040528A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 TRACK 3L SECTION FROM 10 INCHES AFT OF FR 71 TO 10 INCHES FWD OF FR 74 HAS 4 AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS, AT FR 72, BETWEEN FR 72 AND 73, 2 INCHES AFT OF FR 74. REMOVED SEAT TRACK, FABRICATED REPLACEMENT TRACK, TREATED, PRIMED AND TOP COATED SEAT TRACK, INSTALLED PER B/P 1853278295 AND A300-600 SRM 51-75-10 AND 51-40-21. 2L72 4F RTA35EU 20040602000082004060200008NM 2004 6 2 04FDEA01456 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.410, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.408. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000092004060200009NM 2004 6 2 04FDEA01457 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIRED AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000112004060200011NM 2004 6 2 04FDEA01459 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.092. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000192004060200019WP 2004 6 2 04FDEA01467 120040526A5720ARB116414 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT WING L/E LOWER L/E SUPPORT BRACKET IS CRACKED AT IT'S AFT END RT WS XORS 835. REMOVED AND REPLACED RT WING L/E SUPPORT BRACKET AT WS XORS 835 INBOARD OF SLAT TRACK 15 IAW SRM 51-31-01 AND SRM 51-35-01. 2L73 4F A22WE 20040602000212004060200021NM 2004 6 2 04FDEA01450 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.510, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.508. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000232004060200023WP 2004 6 2 04FDEA01264 120040513A5720FXARL050016 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED IN 3 PLACES AT XORS 714 INSIDE ACCESS PANEL 636 AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040602000242004060200024NM 2004 6 2 04FDEA01311 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.2195. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000252004060200025NM 2004 6 2 04FDEA01312 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4 FIG 1. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.1895. REPAIRED AS PER EA 1-5750-76672. RT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE BRACKET PIVOT BEARINGS CORROSSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000262004060200026WP 2004 6 2 04FDEA01313 120040518A5720ARL050015 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AT XORS 714 INSIDE ACCESS 536AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040602000342004060200034NM 2004 6 2 04FDEA01321 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.504, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.502. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000352004060200035NM 2004 6 2 04FDEA01032 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040602000362004060200036NM 2004 6 2 04FDEA01326 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.220. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000372004060200037NM 2004 6 2 04FDEA01327 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER: 1.219. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000382004060200038NM 2004 6 2 04FDEA01328 120040518A5730 SKIN DOUG MD11 MD11 3023602NM LT WING CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 FIXED LEADING EDGE SKIN BEHIND NR 3 SLAT CHAFED. REPAIRED AS PER SRM 57-10-00 FIG 15 VOL I. 2L73 4F RTA22WE 20040602000392004060200039NM 2004 6 2 04FDEA01329 120040518A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 FWD PIT - STA 720E - 720F, STR 27L EXFOLIATED. CUT OUT STRINGER DAMAGE IAW SRM 53-10-3 FIG 1, FABRICATED NEW SECTION STRINGER & REPAIR SPLICES FROM MAT BAC 1498-147, BATCH 32659 & BAC 1498-131 BATCH 54832 IAW SRM 53-10-3. INSTALLED STRINGER & SPLICES IAW SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20040602000402004060200040NM 2004 6 2 04FDEA01330 120040518A2761 SUPPORT ANGLE BOEING727 727200 138407ENM NR 5 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE HAS A CRACK. REMOVED AND REPLACED NR 5 SPOILER ACTUATOR I/B SUPPORT ANGLE IAW SRM 51-30-2, ON NON ROUTINE N00606. 2L73 4F RTA3WE 20040602000412004060200041NM 2004 6 2 04FDEA01331 120040518A5313FXSRM514231A STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 RIGHT MLG W/W - CRACK IN STR 18 AT APPROX STA 908. STOP DRILLED CRACK AS PER SRM 53-10-1 FIG 1. FABRICATED REPAIR ANGLES ON MAE TRAVELER T4/428590. INSTALLED REPAIR ANGLES IAW SRM 51-30-2, ON NON ROUTINE N00097. 2L73 4F RTA3WE 20040602000422004060200042WP 2004 6 2 04FDEA01332 120040519A5753ANB74341 MOUNT DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT I/B FLAP SIDE LOAD ROLLER FITTING MOUNT IS CORRODED. REPLACED ASSY ON WC E 8-5750-7- 5002 AT MAE. 2L73 4F A22WE 20040602000442004060200044WP 2004 6 2 04FDEA01334 120040519A5753ANB74341 FITTING DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT I/B FLAP SIDE LOAD ROLLER FITTING HAS CORROSION IN BORES AND IS CHAFED. REPLACED FITTING ON W/C E8-5750-7-5002 PT 1 AT MAE. 2L73 4F A22WE 20040602000452004060200045WP 2004 6 2 04FDEA01335 120040519A78309036RR79PO1 BRACKET DOUG DC10 DC1010 3022110WP THRUST REVERSER CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 NR 3 ENG O/B TR FEED BACK YOKE BRACKET CHAFED. REMOVED AND REPLACED FEEDBACK YOKE IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040602000462004060200046WP 2004 6 2 04FDEA01336 120040519A5230ADG7010507 DAMPENER DOUG DC10 DC1010 3022110WP CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LWR FWD CARGO DOOR COUNTER BALANCE DAMPENER IS CORRODED. REMOVED AND REPLACED COUNTER BALANCE DAMPENER IAW MM 52-31-07-2 AT MAE. 2L73 4F A22WE 20040602000472004060200047NM 2004 6 2 SWAA041421 120040518A53106546529 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND SHEAR TIE AT BS 500C, STRINGER 16R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040602000482004060200048NM 2004 6 2 SWAA041422 120040518A335065C34691 LIGHT BOEING737 7373Q8 1384670NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 10 DEF, LOOSE. SECURED BULLNOSE LIGHT PER MM. 2L72 4F RTA16WE 20040602000492004060200049NM 2004 6 2 SWAA041423 120040518A53306545768 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 350, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040602000502004060200050NM 2004 6 2 SWAA041424 120040518A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040602000512004060200051NM 2004 6 2 SWAA041425 120040518A53306545857 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR CUTOUT SKIN AT LOWER FWD CORNER, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040602000542004060200054EU 2004 6 2 04FDEA01374 120040520A5320 ANGLE AIRBUS310 A310203 3930313EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 AFT PRESSURE BULKHEAD FR80 OUTER ANGLE LABELED LEFT NR 8 HAS INCOMING ELONGATED HOLES. FABBED REPLACEMENT ANGLE P/N A5398182321000 IAW ACFT DRAWING A53981823 ANGLE TO BE INSTALLED ON N CARD N00035 REF SDR 04-1346. 2L72 4F RTA35EU 20040602000552004060200055NM 2004 6 2 04FDEA01375 120040520A2620ARL0402563 SUPPORT BRACKET DOUG MD11 MD11 3023602NM NR 3 PYLON MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25580FE 48471 NR 3 PYLON ENGINE FIREX SUPPLY LINE IS RIDING HARD AND WORN THROUGH AGAINST PYLON STRUCTURE AFT OF PYLON FWD BULKHEAD LOOKING THRU ACCESS PANEL 487FL. THE DAMAGE IS MEASURED AS 1.125 X .125 INCHES ). REMOVED AND REPLACED A SECTION OF FIREX PERMANENT LINE BETWEEN FIRE BOTTLE AND UPPER PILLOW CONNECTION PER M/M 20-10-01-2. BLENDED BULB SEAL SUPPORT BRACKET. FOUND THAT DAMAGE TO FIREX LINE WAS DUE TO MISSING SUPPORT BRACKET HARDWARE. 2L73 4F RTA22WE 20040602000572004060200057NM 2004 6 2 04FDEA01377 120040520A5320FXFAB35407FS FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 FWD PIT - STA 715 FLOOR SUPPORT R3 - EXFOLIATED AT NUT PLATE HOLES. FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-4, INSTALLED IAW SRM 51-30-2, ON NON ROUTINE N00637 AT MAE. 2L73 4F RTA3WE 20040602000592004060200059WP 2004 6 2 04FDEA01379 120040520A7830 BRACKET DOUG DC10 DC1010 3022110WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 NR 3 ENGINE LEFT T/R TRANSLATING SLEEVE, FWD LOWER SLIDER CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-31-01 & 51-35-01. FAB NEW BRACKET IAW CF6-6 ENGINE MANUAL. INSTALLED IAW ENGINE MANUAL CF6-6 & SRM 51-31-01. 2L73 4F A22WE 20040602000602004060200060WP 2004 6 2 04FDEA01380 120040521A5720ARK0067 BRACKET DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT WING T/E, HYD LINE SUPPORT IS BROKEN OFF SPOILER ACTUATOR NR 5. REMOVED AND FAB NEW BRACKET IAW DWJ ARK 0067 & DPS 3069 AND REINSTALLED NEW BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040602000612004060200061WP 2004 6 2 04FDEA01381 120040521A5320NCA6042 STIFFENER DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 VERTICAL STIFFENER FASTENER HOLES ELONGATED, UNDER DOOR SILL 115AZ INSIDE AVIONICS COMP. REMOVED VERTICAL STIFFENER & T-CLIPS. REC FROM FAB ON T4/429922. VERTICAL STIFFENER LOCATED & DRILLED. FAB 2 CLIPS FROM 60.8060.20MST000955 1 & 2 CLIP FROM 60.2781420MST0008469. LOCATED, DRILLED, TREATED, PRIMED & INSTALLED VERTICAL STIFFENER & 2 CLIPS IAW SRM 51-33-01 & DRG NCA6042 AT MAE. 2L73 4F A22WE 20040602000632004060200063WP 2004 6 2 04FDEA01383 120040521A5712ALC7204501N PANEL DOUG DC10 DC1010 3022110WP HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 MAJOR REPAIR DURING C-CHECK, AND PASSENGER TO FREIGHTER CONFIG BY ULTRASONIC INSPECTION, FOUND 1 PANEL CRACKED ON THE HORIZONTAL STABILIZER. P/N REMOVED ALC7204-1. REMOVE AND REPLACE PANEL WITH P/N ALC7204-501N PER EA 8-5510-70126. 2L73 4F A22WE 20040602000642004060200064NM 2004 6 2 SWAA041427 120040518A29106544654 HYDRAULIC LINE BOEING737 7372H4 138448CNM LT WING BROKEN A SWAAK NONE K FLUID LOSS APAPPROACH 1 SW29095SW 23054 DECLARED EMERGENCY, ON APPROACH AFTER FLAPS EXTENDED TO 5 DEGREES, A SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. ALSO LOST SYSTEM PRESSURE. REMOVED AND REPLACED BROKEN HYDRAULIC RETURN LINE ON NR 2 L/E SLAT ACTUATOR PER MM. 2L72 4F A16WE 20040602000662004060200066NM 2004 6 2 04FDEA01033 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040602000672004060200067NM 2004 6 2 04FDEA01034 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040527001012004052700101EA 2004 5 27 COMA0460308 120040510A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01927CA 7031 FLIGHT 5802 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040527001022004052700102 2004 5 27 COMA0460309 420040510A3140 COMPUTER CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01468CA 7649 FLIGHT 5343 IAPS DEGRADED STATUS MESSAGE DURING T/O. RESET THE NR 2 DCU, SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20040527001062004052700106NM 2004 5 27 04FDEA01009 120040421A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001102004052700110NM 2004 5 27 04FDEA01016 120040421A5347FXMACH0193 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 MAIN CARGO COMPT. SEAT TRACK HAS GOUGED SCALLOPS AT FS 755 - 765, LBL 63. REMOVED AND REPLACED SEAT TRACK SECTION AT F/S 755-765, LBL 63, IAW SRM 51-30-2. 2L73 4F RTA3WE 20040527001112004052700111NM 2004 5 27 04FDEA01017 120040422A5720ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019. TRAILING EDGE AND TRAILING EDGE DEVICES LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040527001162004052700116WP 2004 5 27 04FDEA01102 120040424A324060008924 CONTROL UNIT DOUG DC10 DC1010 3022110WP ZONE 700 WILL NOT TEST A FDEAO OTHER L NO TEST NRNOT REPORTED 1 SO25365FE 46601 ANTI-SKID FAILS (MULTIPLE REPEATS). REMOVED HUBCAPS, PERFORMED RINGOUT OF ALL WHEEL SPEED TRANSDUCERS, VALVES AND CONTROL WIRING. FOUND SHORT AT RECEPTACLE R5-264. REPLACED R5-264, PERFORMED OPS CHECK, FOUND ANTI-SKID CONTROL UNIT FAULTY. REPLACED CONTROL UNIT, PERFORMED OPS CHECK, SYSTEM OPS CKECK GOOD. INSTALLED HUB CAPS, ALL IAW DC-10 MM 32-45-00 AND SWPM 20-31-03. 2L73 4F A22WE 20040528000082004052800008NM 2004 5 28 DL73S040435 120040513A53146562125 KEELBEAM BOEING737 737247 138448DNM PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 FUSELAGE KEEL LT LOWER CHORD FS 727A SPLICE. THE LT LOWER KEEL CHORD WAS FOUND WITH CORROSION AT THE FACTORY SPLICE LOCATION AT FS 727A. THE CORROSION WAS REMOVED WITH CUTOUTS IN THE CHORD FLANGES AND LOCAL BLENDS. THE REMOVED MATERIAL WAS REPAIRED WITH ALUMINUM STRAPS AND NEW SPLICE ANGLES IAW ER/A 090184-14. 2L72 4F4 F A16WE E2EA 20040528000172004052800017 2004 5 28 MALA040403 420040518A3416641413701 ALTIMETER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT STICKS A MALAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL15415XJ 340B415 STANDBY ALTIMETER STICKS AND THEN JUMPS DOES NOT RUN SMOOTHLY. AIRCRAFT DIVERTED. MAINTENANCE REPLACED STANDBY ALTIMETER IAW AMM 34-13-25-2 P/N ON/OFF 64141-370-1 SN ON 2516 SN OFF 1112 REMOVED. 2L72 4T4 TRTA52EU E8NE 20040528000222004052800022EU 2004 5 28 MALA040404 120040519A36107063200 PERISEAL BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE BLEED AIR SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15517XJ E2335 L ZONE HIGH TEMP ILLUMINATED DURING CRUISE. AIR RETURN. MAINTENANCE REPLACED PERI-SEALS (PN 706-3-200), ADJACENT TO PYLON O/H SWITCH IN LEADING EDGE. OPS AND LEAK CHECK GOOD IAW AMM CHPT 36. 2H74 4F4 FRTA49EU E6NE 20040528000392004052800039WP 2004 5 28 UPS04842415 120040506A5310577384458 SHEAR TIE DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 AFT SIDE STATION 1766 J-FRAME TO LONGERON LONG 19R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5773844 AND SRM 51-3-0. 2L74 4F4 FRT4A25 E2GL 20040528000452004052800045EU 2004 5 28 CX7A194J0428 120040523A2611CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101EU CARGO BAY ACTIVATED A CX7AF ACTIVATE FIRE EXT. J WARNING INDICATION TXTAXI/GRND HDL 1 GL03316CE 340B348 ON TAXI TO GATE, CARGO SMOKE CWP. BLEW CARGO FIRE EXTINGUISHER NR 1. 2L72 4T RTA52EU 20040528000492004052800049NM 2004 5 28 AWXA200400564 120040515A5315D53472090000200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 MC - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR BEAM Y765 FORWARD OF FR 66. MAINTENANCE REMOVED CORRODED BEAM Y765 FORWARD OF FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11, FIG. 101. 2L72 4F RTA28NM 20040528000542004052800054NM 2004 5 28 QXEA200400342 120040518A5410 STRUT DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NACELLE SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX- UPPER IB STRUT PROTECTIVE COATING IS SCRATCHED 24 INCHES FORWARD OF FIREWALL. APPLIED EPOXY PRIMER IAW RD 8-54-036. 2H72 4T4 TRTA13NM E20NE 20040528000652004052800065WP 2004 5 28 GTIA040429 120040324A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 SEAT TRACK LT IB SIDE CORRODED. PAX CABIN AT FS 1117-1250. REMOVED SEAT TRACK AT FS 115-1117. LOCATED AND DRILLED SEAT TRACK. INSTALLED NEW SEAT TRACK. 2L72 4F A6WE 20040528000672004052800067WP 2004 5 28 GTIA040445 120040511A2560 CABLE DOUG DC9 DC982 3022082WP EVAC SLIDE MISINSTALLED A GTIAK NONE W INADEQUATE Q C NRNOT REPORTED 1 GL23800NK 49144 L-1 DOOR ESCAPE SLIDE GIRT BAR CABLE IMPROPERLY INST. REPOSITIONED CABLE ON GIRT BAR. 2L72 4F A6WE 20040528000682004052800068NM 2004 5 28 GTIA040425 120040315A5523 TAB DOUG MD80 MD83 3023681NM LT ELEVATOR DELAMINATED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23836NK 53045 LT ELEVATOR ANTI FLOAT TAB DELAMINATED, 2 EA. REMOVED LT ELEVATOR ANTI FLOAT TAB. INSTALLED SERVICEABLE ANTI FLOAT TAB. 2L72 4F RT 20040528000842004052800084NE 2004 5 28 GTIA040447 220040426A7200JT8D219 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 1 FAILED A GTIAA UNSCHED LANDING O OTHER CLCLIMB 1 GL23800NK 49144 718528 AIR RETURN, NR 1 ENGINE FAILED AFTER TAKEOFF AT 1000 AGL-FLEX PWR T/O AT 1000 AGL. WE HAD AN ABRUPT BANG AND VIBRATION AND NR 1 ENGINE ROLLED BACK. ENGINE WINDMILLED N1 30 PERCENT TILL LAND-EGT WAS OK. DID NOT NOTICE OIL PRESSURE. DID NOT TRY TO RESTART ENGINE. NO SMOKE OR FLAME NOTICED. REMOVED AND REPLACED NR 1 ENGINE. OPS AND LEAK CK OK. 2L72 4F4 F A6WE E9NE 20040528000862004052800086WP 2004 5 28 GTIA040431 120040329A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP COCKPIT DELAMINATED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23817NK 49141 COCKPIT FLOOR PANEL BROKEN INSERTS AND EDGE OF PANEL DELAMINATED. FABRICATED COCKPIT FLOOR PANEL. 2L72 4F A6WE 20040601000242004060100024NE 2004 6 1 AMTA200400544 220040511A7321 EEC BOEING757 757* NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED A AMTAK NONE O OTHER CRCRUISE 1 GL11512TZ 26635 30873 LT ENGINE POWER FLUCTUATES. ENGINE STABLE WITH EEC OFF. 2L72 4F4 FRTA2NM E12EU 20040601000362004060100036NM 2004 6 1 04FDEA01481 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.507, MATERIAL REMOVED= 0.006, REMAINING THICKNESS= 0.501. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000372004060100037NM 2004 6 1 04FDEA01482 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.091. REPAIRED AS PER FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601000542004060100054WP 2004 6 1 04FDEA01469 120040526A5414 PANEL DOUG DC10 DC1010 3022110WP NACELLE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 PNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAINER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01. 2L73 4F A22WE 20040601000632004060100063NM 2004 6 1 04FDEA01040 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040601000892004060100089NM 2004 6 1 SWAA041493 120040525A256065C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER SRM. 2L72 4F RTA16WE 20040601000902004060100090 2004 6 1 SWAA041494 420040525A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED RON, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040601001002004060100100 2004 6 1 SWAA041416 420040518A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040601001152004060100115WP 2004 6 1 04FDEA01493 120040527A5753ARC01821 FITTING DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-77424 WINGS LT IB FLAP-OB HINGE BRACKET SIDE BRACE REPAIR (P/N ARC0182-1) COMPLIED WITH EA 8-5750-77424 (WINGS-LT IB FLAP- OB HINGE BRACKET SIDE BRACE REPAIR (PN ARC 018 2-1) AT MAE. 2L73 4F4 F A22WE E23EA 20040601001282004060100128NM 2004 6 1 UPS04242434 120040512A5330 LAP JOINT BOEING727 72725C 138400HNM PWA JT8 JT8D5 52046NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C MATERIAL LOSS (LAP JOINT CORROSION) AT S-6L BS 685. REPAIRED IAW UPS EO B727-5330-0509 APPX C, AND SRM 53-3 0-1, FIG 5. 2L73 4F4 F A3WE E2EA 20040601001292004060100129NM 2004 6 1 UPS04242435 120040511A5720 INTERCOSTAL BOEING727 72725C 138400HNM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C LT WING LE CAVITY INTERCOSTAL JUST OB OF NR 1 LEADING EDGE FLAP CENTER HINGE CASTING CRACKED AT IB LOWER FASTENER HOLE. REPLACED INTERCOSTAL IAW DRG 65-17356. 2L73 4F A3WE 20040601001362004060100136NM 2004 6 1 QXEA200400363 120040527A5330 SKIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - LT LOWER AFT FUSELAGE HAS AN AREA OF NICKS BELOW PREVIOUS PATCH AT LOWER FORWARD CORNER OF BAGGAGE DOOR OPENING. REPAIRED IAW DHC-8-200 SRM 51-20-51 AND SRM 51-20-36. 2H72 4T4 TRTA13NM E20NE 20040601001412004060100141NM 2004 6 1 QXEA200400369 120040527A3230 STRUCTURE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE MLG DRAG STRUT CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - MAIN LANDING GEAR DRAG STRUT UPPER CROSS MEMBER CHAFED ON OB END WHERE SIDESTAY PROX HARNESS HAS BEEN RUBBING AGAINST IT. REPAIRED IAW CMM 32-10-02. 2H72 4T4 TRTA13NM E20NE 20040601001432004060100143NM 2004 6 1 QXEA200400364 120040526A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - SEAT TRACK 4 HAS CORROSION ON FLANGE AND ON EDGE OF NUTPLATE FLANGE AT STATION X240 ON OB SIDE. REPLACED SEAT TRACK. 2H72 4T RTA13NM 20040601001532004060100153NM 2004 6 1 AALA20040590 120040526A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21921AN 29522 BDL SEAT EMERGENCY LIGHTS AT ROWS 5 THROUGH 8 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY LIGHTS AT ROWS 5 THROUGH 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA16WE E2GL 20040601001682004060100168NM 2004 6 1 SWAA041418 120040518A53206545768 BUTTSTRAP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND BUTT STRAP AT BS 360, STRINGER 14L, CRACKED. REPAIRED STRAP PER SRM. 2L72 4F RTA16WE 20040602000012004060200001NM 2004 6 2 04FDEA01509 120040528A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.481, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.479, MINIMUM ALLOWABLE THICKNESS OF LUG: 0.408. WITHIN ALLOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2L73 4F RTA22WE 20040602000102004060200010NM 2004 6 2 04FDEA01458 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.508, MATERIAL REMOVED= 0.001, REMAINING THICKNESS= 0.507. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000142004060200014NM 2004 6 2 04FDEA01462 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.403, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.401. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000222004060200022NM 2004 6 2 04FDEA01105 120040426A534760822324 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 MAIN CARGO COMPT SEAT TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACED SEAT TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2. 2L73 4F RTA3WE 20040602000272004060200027WP 2004 6 2 04FDEA01314 120040518A5320AFA387155 FLOOR SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 AFT CARGO COMPT FLOOR SUPPORT IS CORRODED ON LOWER SURFACE STA 1781 LBL 27 TO LBL 42. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040602000292004060200029WP 2004 6 2 04FDEA01316 120040518A5720ANB707011 CLIP DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 STA 1278 - STA 1441 LEFT WING OVERWING PANEL SUPPORT FRAME LOWER MOUNT CLIPS ARE CRACKED. REMOVED AND REPLACED CLIPS IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040602000302004060200030NM 2004 6 2 04FDEA01317 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.093, FINAL DIAMETER: 1.188. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000322004060200032NM 2004 6 2 04FDEA01319 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.477, MATERIAL REMOVED: 0.027, REMAINING THICKNESS OF LUG: 0.450. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000432004060200043WP 2004 6 2 04FDEA01333 120040519A5753ANB72545 BRACKET DOUG DC10 DC1010 3022110WP T/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT I/B SIDE LOAD ROLLER BRACKET IS WORN/CHAFED. REPLACED BRACKET ON W/C E8-5750-75002 PT 2 AT MAE. 2L73 4F A22WE 20040602000652004060200065WP 2004 6 2 04FDEA01384 120040521A5712 RIB DOUG DC10 DC1010 3022110WP CENTER WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 MAJOR REPAIR DURING C-CHECK, PASSENGER TO FREIGHTER CONFIG, FOUND RIB XCW/81 BETWEEN LONGERON 21 AND 22, UPPER CORD RADIUS HAS .5 INCH CRACK CENTER WING RIB. REPAIRED AREA WITH A FAB ANGLE, PER EA 8-5710-70141. 2L73 4F A22WE 20040602000682004060200068NM 2004 6 2 04FDEA01035 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040602000692004060200069NM 2004 6 2 04FDEA01036 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040602000712004060200071EU 2004 6 2 04FDEA01351 120040519A5312 PRESSURE BLKHD AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 AFT PRESSURE BULKHEAD FR 80 LEFT WEB ASSY HAS AREAS OF EXCESSIVE CORROSION. FABRICATED NEW WEB IAW AIRBUS DRWG A53981860, INSTALLED NEW WEB ASSY IAW A310 SRM 51-40-21 ON ATTACH ANGLE. WORK PERFORMED ON NRC N00269. 2L72 4F RTA35EU 20040602000722004060200072WP 2004 6 2 04FDEA01355 120040519A5320FXSRM531601 FLOOR SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 AFT CARGO FLOOR SUPPORT BEAM IS CORRODED STA 1841 LBL 18 TO RBL 36. REPLACED SUPPORT BEAM IAW SRM 51-33-01 AND SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040602000732004060200073WP 2004 6 2 04FDEA01356 120040519A5754ARB139420 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT WING NR 3 SLAT TRACK LOWER FAIRING OUTBOARD SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-31-01 AND AMM 27-80-01-4 AT MAE. 2L73 4F A22WE 20040602000742004060200074NM 2004 6 2 04FDEA01357 120040520A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), O/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIAMETER: 1.217, MAX ALLOWABLE DIAMETER: 1.220, WITHIN ALLOWABLE LIMIT AS PER CMM 57-52-03 PAGE 446. REPAIRED AS PER EA 1-5750-76679. TRAILING EDGE FLAPS RT INBOARD FLAP OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000762004060200076NM 2004 6 2 04FDEA01359 120040520A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 44 RT STA 1541 FOUND CRACK. CRACK SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040602000802004060200080NM 2004 6 2 04FDEA01364 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - O/B FLAP I/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED. ORIGINAL LUG THICKNESS: 0.393, MATERIAL REMOVED: 0.003, REMAINING THICKNESS OF LUG: 0.390 REWORKED AREA REPAIRED AS PER EA 1-5750-76674. LT O/B TRAILING EDGE FLAP - INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS - REPAIR. 2L73 4F RTA22WE 20040602000812004060200081NM 2004 6 2 04FDEA01365 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 1. ORIGINAL THICKNESS OF LUG: 0.459, MATERIAL REMOVED: 0.004, REMAINING THICKNESS OF LUG: 0.455 WITHIN LIMIT AS PER DRAWING ARC0502. 2L73 4F RTA22WE 20040602000832004060200083NM 2004 6 2 04FDEA01367 120040520A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.218, EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76675. OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2L73 4F RTA22WE 20040602000882004060200088EU 2004 6 2 04FDEA01386 120040521A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MAIN CABIN SEAT TRACK NR 3 RIGHT, BETWEEN FR 50-52, MULTIPLE SPOTS OF CORROSION ALONG SEAT TRACK HOLES AND BOTH SIDES OF FLANGE TOP TO BOTTOM AS MARKED. REMOVED SEAT TRACK, FABBED NEW SEAT TRACK, DRILLED AND REAMED HOLES, TREATED PRIMED AND TOP COATED, AND INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 AND 51-71-10. 2L72 4F RTA35EU 20040602000902004060200090NM 2004 6 2 04FDEA01388 120040521A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 STRINGER CLIP CRACKED STA 950D STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 7R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040602000922004060200092NM 2004 6 2 04FDEA01390 120040521A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 SEAT TRACK FOUND CRACKED AT STA 902-914 RIGHT 28 INCHES. SEAT TRACK CUT AND REMOVED AT STA 869 TO STA 969 RBL 27.5 AND REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040602000932004060200093NM 2004 6 2 SWAA041428 120040519A33500L3071BPEGPL LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29702ML 22054 EEPLS LIGHT AT ROW 14 ABC INOP. RELAMPED EEPLS PER MM. 2L72 4F A16WE 20040602000962004060200096NM 2004 6 2 SWAA041431 120040519A335010107451 SIGN BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040602000972004060200097NM 2004 6 2 SWAA041432 120040519A53306560552 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 285, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040602000982004060200098NM 2004 6 2 SWAA041433 120040519A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040602001012004060200101NM 2004 6 2 ASAA0410178 120040327A5753654795987 SKIN BOEING737 737290C 138448VNM T/E FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT OUTBOARD MID FLAP LOWER SKIN IS CHAFED AT IMMEDIATE OUTBOARD OF INBOARD PUSHROD. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001032004060200103NM 2004 6 2 ASAA0410161 120040327A53156554906501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON FLOORBEAM AT STATION 500A. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001062004060200106NM 2004 6 2 ASAA0410165 120040327A531565549091 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM UPPER CHORD CORRODED AT STATION 807. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001082004060200108NM 2004 6 2 ASAA0410167 120040327A533065C80736833 SKIN BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT AFT SIDE SKIN AT STATION 727 HAS DAMAGE, DENTS NICKS. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040602001092004060200109NM 2004 6 2 ASAA0410053 120040208A3350900542 BATTERY BOEING737 7372X6C 1384552NM CABIN NOT SEATED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 ANC - DURING INSPECTION, FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER IN THE MID CABIN INOPERATIVE. RESEATED THE BATTERY, THEN EXIT IDENTIFIER OPERATED NORMAL. (M) 2L72 4F RTA16WE 20040602001102004060200110NM 2004 6 2 ASAA0440089 120040326A33508100022601 LIGHT BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 ANC - FOUND FORWARD GALLEY ENTRANCE RED FLOOR TRACK LIGHT UNPLUGGED. REINSTALLED FORWARD GALLEY RED FLOOR TRACK LIGHT, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040602001132004060200113NM 2004 6 2 ASAA0410163 120040327A53126546568 PRESSURE BLKHD BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION IN AFT CARGO BAY AFT PRESSURE BULKHEAD AT STRINGER 0. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040602001172004060200117NM 2004 6 2 ASAA0410173 120040327A531565549011 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON UPPER CHORD BEAM AFT FLANGE AT STATION 947. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001192004060200119NM 2004 6 2 ASAA0410174 120040327A531569335403 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT CARGO PIT CABIN FLOORBEAM LOWER CHORD CORRODED AT STATION 767. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001222004060200122NM 2004 6 2 ASAA0410177 120040327A54146570947 SKIN BOEING737 737290C 138448VNM NR 1 PYLON CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND NR 1 ENGINE PYLON INBOARD SKIN CHAFED FORWARD OF PANEL 5143. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001242004060200124NM 2004 6 2 ASAA0410180 120040327A5753657190218 STRUCTURE BOEING737 737290C 138448VNM T/E FLAP CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND RIGHT WING INBOARD MID FLAP CENTER FOREFLAP TRACK CUT OUT CRACKED .375 INCH. REPAIRED IAW EA. (M) 2L72 4F A16WE 20040602001252004060200125NM 2004 6 2 ASAA0410181 120040327A53116547959501 FRAME BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND STATION 794 FRAME UPPER FLANGE IS GOUGED. REPAIRED IAW. (M) 2L72 4F A16WE 20040602001272004060200127NM 2004 6 2 ASAA0410183 120040327A531565549011 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT STATION 947 CABIN FLOORBEAM CORRODED ALONG TOP T-CHORD. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001292004060200129NM 2004 6 2 ASAA0410206 120040424A5340693535222 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND STRINGER CLIP AT STATION 986, STRINGER 23L IS CORRODED. REMOVED DAMAGED STRINGER CLIP AND INSTALLED REPLACEMENT STRINGER CLIP IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040603000032004060300003NM 2004 6 3 04FDEA01394 120040521A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK R1 DOOR WAY SEAT TRACK FOUND CORROSION AT STA 440 RT 86 INCHES. REMOVED IAW SRM 51-33-01 VOL II. NEW SEAT TRACK HOLES TRANSFERRED IAW SRM 51-31-01 VOL II, PROTECTED IAW SRM 51-21-01 VOL II AND INSTALLED IAW SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040603000042004060300004NM 2004 6 3 04FDEA01395 120040521A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK, FLOOR SUPPORT CORRODED AT STA 409, RBL 14. FLOOR SUPPORT CORRODED AT STA 409, RBL 14 REMOVED IAW SRM 51-33-01 VOL II, NEW FLOOR SUPPORT HOLES TRANSFERRED IAW SRM 51-31-01-VOL II AND INSTALLED IAW SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040603000082004060300008WP 2004 6 3 04FDEA01322 120040518A5753ARC70071 STOP FITTING DOUG DC10 DC1010 3022110WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING O/B FLAP O/B STOP WORN AND MISSING. REMOVED AND REPLACED STOP AT MAE. 2L73 4F A22WE 20040603000092004060300009NM 2004 6 3 04FDEA01210 120040510A5754 BRACKET DOUG MD11 MD11 3023602NM L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. INBD BRACKET REMOVED AS PER SRM 51-31-01-VOL II AND INSTALLED NEW BRACKET AS PER SRM 51-33-01 VOL II & SRM 51-35-01 VOL II. CARRIED OUT OPERATION CHECK AS PER AMM 27-80-00 AND FOUND SATISFACTORY. 2L73 4F RTA22WE 20040603000102004060300010NM 2004 6 3 04FDEA01211 120040510A5744ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE O/B ACTUATOR LUG HOLE CORROSION. REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH AND REPAIRED AS PER FEDEX EA 1-5740-75955 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040603000122004060300012NM 2004 6 3 04FDEA01213 120040510A5744ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407 ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH AND REPAIRED AS PER FEDEX EA 1-5740-75955 - WINGS - LEFT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040603000152004060300015WP 2004 6 3 04FDEA01265 120040513A5347FXSRM537000SH SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CABIN SEAT TRACK LBL 27 FS 1119 IS CRACKED. REPLACED SEAT TRACK IAW SRM 53-70-00 AT MAE. 2L73 4F A22WE 20040603000162004060300016WP 2004 6 3 04FDEA01266 120040513A2550AWJ70061 CLIP DOUG DC10 DC1010 3022110WP CARGO BAY BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 CTR PIT ROLLER BRACKET BROKEN STA 1705 RBL 57. REMOVED AND REPLACED ROLLER AND CLIP IAW SRM 51-31-01AT MAE. 2L73 4F A22WE 20040603000172004060300017NM 2004 6 3 04FDEA01267 120040514A5311AFA00283 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 FOUND DAMAGED. UPPER CARGO COMPARTMENT, RIGHT UPPER FRAME ASSY AT STA 1681 CARRIED OUT REPAIR ON DAMAGED AREA AS PER SRM 53-30-00 VOL I FIG 1. FOR REPETITIVE INSPECTION TRACKING, REFER TO FEDEX EA 1-5310-75963 - FUSELAGE - MAINFRAME - TRACKING OF CATEGORY B REPAIRS ON FRAME. 2L73 4F RTA22WE 20040603000182004060300018WP 2004 6 3 04FDEA01323 120040518A5753ARC2166505 SPINDLE DOUG DC10 DC1010 3022110WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT O/B FLAP I/B ROLLER SPINDLE IS WORN AND IS CORRODED. REMOVED AND REPLACED SPINDLE ON W/C E 8-5750-7-5000 PT 3. 2L73 4F A22WE 20040603000202004060300020NM 2004 6 3 04FDEA01325 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR I/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.403, MATERIAL REMOVED: 0.003, REMAINING THICKNESS OF LUG: 0.400. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040603000242004060300024WP 2004 6 3 04FDEA01339 120040519A7110ASL00402 RUB STRIP DOUG DC10 DC1010 3022110WP NR 2 COWLING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 NR 2 ENGINE RIGHT CORE COWL FWD CHAFE STRIP IS WORN. REPLACED RUB STRIP IAW SRM 51-31-01AT MAE. 2L73 4F A22WE 20040603000272004060300027NM 2004 6 3 04FDEA01342 120040519A49909698664 SWITCH DOUG MD11 MD11 3023602NM APU DEFECTIVE A FDEAO OTHER O OTHER CRCRUISE 1 SO25590FE 48505 APU AUTO SHUTDOWN IN FLIGHT TWICE, CFDS FAULTED OIL PRESS LO. REMOVED AND REPLACED APU LOP SWITCH AS PER AMM 49-94-01-4. OPS TEST OF APU CARRIED OUT AS PER 49-10-00. FOUND SATISFACTORY. 2L73 4F RTA22WE 20040603000292004060300029NM 2004 6 3 04FDEA01344 120040519A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO STA 629 FRAME DENTED LBL 6 STR 28. CUT OUT DAMAGED PORTION OF FRAME AT BS 720 LBL 6 STR 28 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3. 2L73 4F RTA3WE 20040603000302004060300030EU 2004 6 3 04FDEA01346 120040519A5312 PRESSURE BLKHD AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 REAR PRESSURE BULKHEAD FWD FACE ON THE AFT SIDE OF FR 82 FROM S38L TO S38R HAS AREAS OF CORROSION. LEVEL 2 CORROSION. REF N CARD N00035. COMPLIED WITH EA 6-5310-78353 PT1 2L72 4F RTA35EU 20040603000342004060300034EU 2004 6 3 04FDEA01349 120040519A5320 FITTING AIRBUS310 A310203 3930313EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 STRINGER 57 O/B END FITTING AT FRAME 80 HAS TWO ELONGATED HOLES. .300 X .280. .225 X .190. FABBED REPLACEMENT PART IAW AIRBUS DWG A53981973 ANGLE (END FITTING). ANGLE INSTALLED ON WORK CARD NON ROUTINE N00035. 2L72 4F RTA35EU 20040603000362004060300036WP 2004 6 3 04FDEA01219 120040511A5620NAA6049509 WINDOW DOUG DC10 DC1010 3022110WP CABIN SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 SIDE OF FUSELAGE FWD OF RIGHT WING FWD WINDOW HAS SCRATCHES. REMOVED AND REPLACED RT CABIN WINDOW FWD OF WING IAW MM 56-20-00-2 AT MAE. 2L73 4F A22WE 20040603000382004060300038WP 2004 6 3 04FDEA01221 120040511A5347FXMACH1550 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CARGO DECK SEAT TRACK GOUGED AT STATION 820 TO 970 LBL 47.25. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040603000392004060300039WP 2004 6 3 04FDEA01222 120040512A5230FXADA77611 PLATE DOUG DC10 DC1010 3022110WP CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FWD LWR CARGO DOOR FWD JAMB CENTER ANTI-CHAFE PLATES GOUGED. REMOVED AND REPLACED ANTI-CHAFE PLATES IAW SRM 51-31-01AT MAE. 2L73 4F A22WE 20040603000402004060300040WP 2004 6 3 04FDEA01223 120040512A5753ARC3093505 STOP FITTING DOUG DC10 DC1010 3022110WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT INBOARD FLAP STOP PAD FITTING FWD OF O/B HINGE FASTENER HOLES ELONGATED AND WORN. REPLACED ANTI FRICTION UPSTOP PAD IAW MM 20-50-02-2 AT MAE. 2L73 4F A22WE 20040603000412004060300041WP 2004 6 3 04FDEA01224 120040512A5753ARC14711 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT WING O/B FLAP NR 2 TRACK HAS GOUGE. REMOVED AND REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE. 2L73 4F A22WE 20040603000442004060300044EU 2004 6 3 04FDEA01350 120040519A5320 FITTING AIRBUS310 A310203 3930313EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 STRINGER 57 I/B END FITTING AT FRAME 80 HAS TWO ELONGATED HOLES. .300 X .200. .225 X .190. NO ACTION REQUIRED OLD PART IS BEING REPLACED AT STR 57 FR 80 REF DRAWING R53970100 ITEM 40 PART A5398020620300 REF N00035 FOR INSTALLATION OF END FITTING. 2L72 4F RTA35EU 20040603000452004060300045WP 2004 6 3 04FDEA01227 120040512A5753ARC14751 FLAP TRACK DOUG DC10 DC1010 3022110WP NR 1 FLAP VANE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT O/B FLAP NR 1 VANE TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 TA MAE. 2L73 4F A22WE 20040603000462004060300046WP 2004 6 3 04FDEA01352 120040519A21501879009 HEAT EXCHANGER DOUG DC10 DC1010 3022110WP A/C BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 NR 3 HEAT EXCHANGER HAS CRACK ON INSIDE. REPLACED HEAT EXCHANGER IAW MM 21-53-01-2 AT MAE. 2L73 4F A22WE 20040603000472004060300047WP 2004 6 3 04FDEA01229 120040512A5753ARC15631 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT WING O/B FLAP NR 3 TRACK TOP COATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE. 2L73 4F A22WE 20040603000482004060300048WP 2004 6 3 04FDEA01230 120040512A5753ARC1563503 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP VANE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT O/B FLAP NR 3 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 AT MAE. 2L73 4F A22WE 20040603000492004060300049WP 2004 6 3 04FDEA01231 120040512A5230ADA746227N GUARD DOUG DC10 DC1010 3022110WP CARGO DOOR BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FWD LWR CARGO DOOR VENT DOOR GRILL BENT GOUGED AND BROKEN. REMOVED AND REPLACED VENT DOOR GUARD IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040603000512004060300051WP 2004 6 3 04FDEA01353 120040519A5753ARC20031 CARRIAGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT O/B FLAP BOTH I/B AND O/B ROLLER CARRIAGES HAVE WORN AREAS AND CORROSION. REPLACED CARRIAGES ON W/C E 8- 5750-7-5000 PT 3 AT MAE. 2L73 4F A22WE 20040603000522004060300052WP 2004 6 3 04FDEA01354 120040519A2752ARC2531502 DRIVE ASSY DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT I/B FLAP DRIVE ARM I/B BEARING FACE IS PITTED. REPLACED DRIVE ARM ON WC E8-5750-7-5002 PT 2 AT MAE. 2L73 4F A22WE 20040603000542004060300054NM 2004 6 3 04FDEA01361 120040520A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 38 LEFT STA 1541. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040603000552004060300055NM 2004 6 3 04FDEA01412 120040522A5755 BRACKET BOEING727 727200 138407ENM SPOILER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 WINGS - SPOILERS - SPOILER DOWN STOP BRACKET GOUGE REPAIR. COMPLIED WITH EA 7-5740-77411. BLENDED GOUGE, HFEC NO CRACKS NOTED. 2L73 4F RTA3WE 20040603000592004060300059NM 2004 6 3 04FDEA01372 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.452, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.450. REPAIRED AS PER EA 1-5750-76676. LEFT HAND OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2L73 4F RTA22WE 20040603000602004060300060NM 2004 6 3 04FDEA01233 120040512A3260 WARNING LIGHT BOEING727 727100 1384036NM COCKPIT ILLUMINATED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25190FE 19083 NOSE GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR LOWERED, CAME ON AFTER NOSE GEAR PIN INSTALLED. ADDITIONAL INFO FROM DEBRIEFING CREW. EXTREME PRECIPITATION LEAVING MSY UPON ARRIVAL INTO SHV, NOSE GEAR SHOWED UNSAFE. CYCLED HANDLE GREEN LIGHT ILLUMINATED. UPON ARRIVAL AT AFW COULD NOT GET GREEN LIGHT AFTER NUMEROUS ATTEMPTS. DID GO-AROUND TWICE TO ALLOW TOWER TO OBSERVE GEAR POSITION. TOWER INFORMED GEAR DOWN. UPON LANDING HAD MAINTENANCE INSTALL NOSE GEAR PIN PRIOR TO TAKE TO RAMP AND GATE. 2L73 4F RTA3WE 20040603000652004060300065NM 2004 6 3 04FDEA01285 120040518A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING NR 1 FUEL TANK - XORS 757 - ACCESS PANEL 536BB. SUSPECT CRACK ON NR 10 STRINGER. SLOTTED OUT CRACK AS PER SRM 51-31-01 VOL II. REPAIR ANGLES INSTALLED AS PER SRM 51-33-01 VOL II AND EA 1-5710-76680. UPPER WING STRINGERS 10 & 11 LEFT - CRACK REPAIR. 2L73 4F RTA22WE 20040603000672004060300067NM 2004 6 3 04FDEA01029 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040603000692004060300069NM 2004 6 3 04FDEA01067 120040423A5313NFA631325 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO - STA 1181 LEFT LONGERON 37 FOUND CRACK. CENTER CARGO - STA 1181 LEFT LONGERON 37 REPAIRED AS PER SRM 53-10-00 VOL I FIG 2. 2L73 4F RTA22WE 20040603000702004060300070NM 2004 6 3 04FDEA01416 120040524A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK FRAME FOUND TWO CHAFED MARKS AT STA 535 LEFT BETWEEN 9G NET ATTACH YOKE. DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2L73 4F RTA22WE 20040603000712004060300071EU 2004 6 3 04FDEA01385 120040521A5320 TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 CROSS TRACK AT FR 33 BETWEEN TRACKS 2R AND 3R HAS CORROSION ON WHOLE TRACK. REMOVED AND REPLACED CROSS TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040603000732004060300073NM 2004 6 3 04FDEA01419 120040524A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 SEAT TRACK LBL 8.5 CORRODED AT STA 1119 TO STA 6-50. REMOVED AND REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040603000752004060300075 2004 6 3 YENA200431 420040529A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN MALFUNCTIONED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15556JB4005 2346 1904 BURNING SMELL IN CABIN AT ROW 11. COMPLIED WITH INFO NOTICE 2003-T050TR A. NO ABNORMALITY NOTED. AS A PRECAUTION REMOVED AND REPLACED SEB AT 10B AND 10E. RAN SYSTEM FOR 1 HOUR AND OPERATION IS GOOD. 2L72 4F RTA28NM 20040603000762004060300076EA 2004 6 3 WVE2004F00017 120040510A5320601R3111358 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09597SW 7293 FLOOR SUPPORT ANGLES AT FS280, RBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2L72 4F RTA21EA 20040603000772004060300077EA 2004 6 3 COMA0460337 120040528A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 WORK IN PROGRESS ON DMI 848101, LONG CRACK AT RT WING LOWER PLANK AT WS 148.019. REPAIRED LOWER RT WING PLANK WS 148.019R IAW REO 601R-57-21-130 2L72 4F4 FRTA21EA E15NE 20040603000792004060300079WP 2004 6 3 UPS04842441 120040511A5330577991639 SPLICE PLATE DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 210 FINGER DOUBLER AND SPLICE PLATE ARE CORRODED BEYOND LIMITS BETWEEN LONG 21L TO 31L AND STATION 210 LONG 25R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER, SPLICE PLATE AND SPLICE FITTING IAW DWG 5779916,4653726 AND SRM 51-1-20D, 51-1-21 2L74 4F4 FRT4A25 E2GL 20040603000802004060300080WP 2004 6 3 UPS04842442 120040513A531097555105 SHEAR TIE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 1320 SHEAR TIE IS CRACKED BELOW LONG 21L. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 9755510 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040603000812004060300081WP 2004 6 3 UPS04842443 120040504A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2 FUSELAGE SKIN CORRODED ALONG LONGERON 21R AT FS 8 AND FS55 EO DC8-5330-19540-A INSTALLED TEMP REPAIR, INSTALL PERMANENT REPAIR AT NEXT C- CHECK. GEN AND RECEIVED RFTS N818UP-1-20760. REMOVED FASTENERS STA-9 TO STA-70 L2OR -L24 RMVD TEMP REPAIR AND L22R STA-70 TO STA-8. REMOVED DAMAGED SECTION OF P/N 5613861-347 INNER DOUBLER, REMOVED CORRODED FROM INTERIOR OF SKIN P/N5613861 FOUND WITHIN LIMITS. FAB AND INSTALLED NEW SEC SKIN REPAIRED DOUBLER, FILLER AND FINGER DOUBLER REINSTALLED ALL FASTENERS. SRM53-2-1F7 2L74 4F4 FRT4A25 E2GL 20040603000822004060300082WP 2004 6 3 UPS04842444 120040513A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 JUST BELOW LOWER CUTOUT OF MAIN CARGO DOOR, FUSELAGE SKIN HAS TWO DENTS. REMOVED FASTENER IN SKIN FS 200-220, RMVD DAMAGE SECTION OF SKIN AT FS 210 MATERIAL ID FOR DOUBLER REPAIR EXTERNAL DOUBLER 7075-T6.080 PO 43557 21 FILLER 2024-T-3,071 PO 442960.1 FINGER DOUBLERS 7075-T6 PO 433440.5 DC8-SRM-53-2-1 FAB DOUBLER, FITTER, AND FINGER DOUBLER. ALODINED AND PRIMED. INSTALLED DOUBLER IAW SRM-53-2-1. 2L74 4F4 FRT4A25 E2GL 20040603000852004060300085WP 2004 6 3 UPS04842448 120040508A532037505450502 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35R HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION STA 1040-1080. NO MATERIAL LOSS IAW SRM 53-4-1 AND DAC DWG 9758507. FOUND WITHIN LIMITS. LONGERON SPLICE FOUND TO BE CRACKED. REC'D LOCATED AND DRILLED NEW LONGERON SPLICE. INTERCOSTAL STA 1040-1060 AND STRAP STA 1050 L35R IT IAW SRM 51-1-20D & 51-3-0 2L74 4F RT4A25 20040603000872004060300087WP 2004 6 3 UPS04842450 120040512A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 CORROSION ON FRAME AT FS 180 L35L-35R. REMOVED CORROSION, FOUND BLENDOUT BEYOND ALLOWABLE LIMITS IAW SRM 53-2-0 FIG 1F. FAB -9 DOUBLER, -11 FILLER IAW EO 11728-B AND UPS DWG 53A-011A. INSTALLED PARTS IAW EO AND DWG. ALODINED AND PRIMED IAW SRM-51-1-8. 2L74 4F RT4A25 20040603000882004060300088WP 2004 6 3 UPS04842451 120040508A532047723981 SPLICE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 FWD OR AFT PRESSURE BULKHEAD AT BS 1766 30L SPLICE FITTING HAS CORROSION. REMOVED FITTING. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS AND CRACKED. REC'D FITTING P/N 4772398-1 PO 446277. LOCATED AND DRILLED AND DEBURR FITTING INSTALLED FITTING P/N 4772398-1. ALL IAW SRM 53-2-0,51-1-21, AND 5 1-1-20D 2L74 4F RT4A25 20040603000892004060300089WP 2004 6 3 UPS04842477 120040529A5310 WINDOW FRAME DOUG DC8 DC873F 302199FWP COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:N/A SEVERAL AREAS OF CORROSION ON CTR WINDSHIELD LOWER FRAME. CHECKED CORROSION PITTING WITH DIAL DEPTH GAUGE, DEEPEST FITTING IS .020 REMOVED ALL PITTING IAW SRM 51-1-4-8. ULTRASOUND AREAS. FOUND .077 REMAINING. BLEND CORROSION IAW SRM 53-02-00 FIG 1F WITHIN LIMITS 2L74 4F RT4A25 20040603000912004060300091EA 2004 6 3 COMA0460338 120040528A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 LT SIDE OF FUSELAGE CHAFED BY PYLON FROM FS 700.00 TO FS 755.00. REPAIRED CHAFFING ON LT SIDE OF FUSELAGE AT FS 700-755 IAW REO 601R-53-61-269. 2L72 4F RTA21EA 20040603000982004060300098NM 2004 6 3 QXEA200400377 120040527A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PANEL 122AR ON RT FORWARD FUSELAGE HAS TWO BAD NUTPLATES. REMOVED AND REPLACED NUTPLATES IAW DHC-8 SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040603001052004060300105NE 2004 6 3 ALG2004F00022 220040511A732076370034 HMU BELL 214 214* 1182103SW GE CT7TS CT71 30030NE NR 1 ENGINE FAILED A ALGAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW03391AL 28103 NR 1 ENGINE FAILED DURING TAKE OFF, AIRCRAFT RETURNED TO PLATFORM. MAINT REMOVED NR 1 ENGINE HMU AND INSTALLED SERVICEABLE HMU ALSO REMOVED NR 1 ENGINE ECU AND INSTALLED SERVICEABLE ECU. 2G71 4U4 U H6SW E8NE 20040603001072004060300107SO 2004 6 3 LR7A04057 120040526A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW JOB CARD HB5301 FOUND RT SIDE FS 428 FUSELAGE SKIN CRACKED AT ESCAPE HATCH CUTOUT LOWER AFT CORNER, RBL 85, WL 195. REPAIRED IAW SRM SMP 583 53-40-50, REPAIR B. NR 0002. 2H74 4T4 T A1SO E282 20040603001092004060300109SO 2004 6 3 LR7A04059 120040526A5714 WEB LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CENTER WING BOX CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 8715 4606 DURING SCHEDULED B3 INSPECTION NR 02/REP/51/2 REPAIR ACCOMPLISHMENT FOUND CENTER WING FWD BEAM WEB CRACKED .75 IN AT 2 EA. FASTENER HOLES AT CWS 72R, FS 517, WL 258 AND 282. REPAIRED IAW LAC MEA 382-57-04-041 AND SRM SMP 583 57-30-22. NR 0124. 2H74 4T4 T A1SO E282 20040603001122004060300112WP 2004 6 3 ASAA0480303 120040422A532199365451 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040603001142004060300114WP 2004 6 3 ASAA0480305 120040422A53219957918501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CRACKED AND DISBONDED ON LOWER SURFACE AT FS 977-1003. REPLACED DAMAGED HAT CHANNEL PER MM 20-20-1. (M) 2L72 4F RTA6WE 20040603001162004060300116WP 2004 6 3 ASAA0480307 120040422A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED ON LOWER SURFACE AT FS 826-864. REPLACED FLOOR PANEL PER SRM. 53-05. (M) 2L72 4F RTA6WE 20040601000012004060100001NM 2004 6 1 DL75K040428 120040511A2751 WARNING SYSTEM BOEING757 757232 1384965NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A DALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO276716C 30838 SELECTED FLAPS 25 TO 30 AT APPROX 170 KTS. FLAT LOAD RELIEF ACTIVATED AND EICAS MSG ( FLAP LOAD RELIEF) CAME ON. FLAP LEVER WAS RESET TO 25 AND FLAPS RETRACTED TO 20, MSG CLEARED SHORTLY AFTER (LE SLAT DISAGREE AND TE DISAGREE) EICAS MSG. PERFORMED QRH (LEADING EDGE SLAT DISAGREE) PROCEDURE PG, NNC.9.6 EICAS MSG CLEARED. DFDR SHOWS SPEED OF 182 KTS WITH FLAPS AT 30 DEG. FLAP OVERSPEED INSPECTION COMPLETED, NO PROBLEMS FOUND. 2L72 4F4 FRTA2NM E17NE 20040601000112004060100011NM 2004 6 1 PCAA0405210 120040525A5270 PROXIMITY SWITCH DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE PAX DOOR DIRTY A PCAAI CABIN DEPRESSURIZATION N FALSE WARNING CRCRUISE 1 EA13981HA 378 FLIGHT NR 3723 NOTED ILLUMINATION OF THE CABIN DOOR WARNING LIGHT DURING CRUISE. CREW COMPLIED WITH CHECKLIST AND MOVED PASSENGER'S AWAY FROM DOOR AREA, INITIATED DESCENT AND DEPRESSURIZED, LIGHT EXTINGUISHED. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBED THE DOOR PROXIMITY SWITCH ON THE DOOR CONTROL ARM. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040601000232004060100023EU 2004 6 1 SDR2004028 120040509A3320S0003014000000 CIRCUIT BOARD AEROSPATR72 ATR72212 8680945EU CABIN SHORTED A TRBAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO21447AM 447 DISCREPANCY: WHILE CRUISING AT 17,000 FT, THE CREW HEARD A RELAY CLICKING SOUND FOLLOWED BY CIRCUIT BREAKERS POPPING OUT FOR SEAT BELT, NO SMOKING, CALL SYSTEM AND RT CABIN READING LIGHTS. FLIGHT ATTENDANT REPORTED ELECTRIC SPARKS AND SMOKE COMING FROM THE PASSENGER SERVICE UNIT (PSU) 8 C/D. AIRCRAFT DIVERTED. 2H72 4T RTA53EU 20040601000482004060100048WP 2004 6 1 04FDEA01502 120040527A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT SEALING AREA FOR PANEL 637AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-42-04 AT MAE. 2L73 4F A22WE 20040601000602004060100060WP 2004 6 1 04FDEA01098 120040424A2780 DRUM DOUG DC10 DC1010 3022110WP SLAT DRIVE WRONG PART A FDEAK NONE O OTHER ININSP/MAINT 1 SO25365FE 46601 LEFT HAND SLAT DRIVE MECHANISM FOLLOW UP CABLE DRUM IS THE WRONG PART NUMBER. REMOVED AND REPLACED DRUM FOR LEFT HAND SLAT DRIVE MECHANISM IAW DAC CMM 27-83-11 PAGE 505 ITEM 9. 2L73 4F A22WE 20040601000642004060100064NM 2004 6 1 04FDEA01041 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040601000692004060100069EU 2004 6 1 04FDEA01047 120040422A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MDCC 5TH SEAT TRACK FROM CENTERLINE RT SIDE BETWEEN FR 26 AND FR 27 1 EA AREA OF CORROSION. CLEANED OUT CORROSION, FOUND TO BE OUT OF LIMITS, AND REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040601000792004060100079NM 2004 6 1 SWAA041507 120040527A57536546435318 STRUCTURE BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED A1 CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040601000972004060100097NM 2004 6 1 SWAA041496 120040525A55341765A310126 BRACKET BOEING737 7377H4 1384404NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED HC1 CHECK, FOUND VERTICAL STAB SPRING BRACKET AT BS 1016, RBL 11, CRACKED. REPAIRED VERTICAL STAB SPRING BRACKET PER EA. 2L72 4F RTA16WE 20040601001012004060100101SO 2004 6 1 2004F00145 220040526A8550629360 IDLER GEAR CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO LT ENGINE BROKEN E EA ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE07420SS273 0562 826288R FOLLOWING TAKE OFF, THE PILOT NOTICED THAT THE LT ENGINE WAS TRAILING SMOKE AND OIL. THE ENGINE WAS SHUT DOWN AND SECURED AND THE AIRCRAFT RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION IT WAS DETERMINED THAT DURING START UP, THE ENGINE EXPERIENCED A (KICK BACK) AND THE IDLER GEAR WHICH DRIVES THE OIL SCAVENGE PUMP FAILED. THIS ALLOWED OIL TO BUILD UP IN THE AIR/OIL SEPARATOR OF THE ENGINE BREATHER UNTIL IT SPILLED OVERBOARD INTO THE ENGINE NACELLE. 1L72 3O3 O A7CE E8CE 20040601001052004060100105NM 2004 6 1 DXTA220400317 120040531A3260327 LIGHT AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE COCKPIT INOPERATIVE E DXTAO OTHER N FALSE WARNING APAPPROACH 1 GL07298QS 98 ON APPROACH LOWERED GEAR HANDLE AND DID NOT RECEIVE GREEN LIGHT, PERFORMED EMERGENCY GEAR EXTENSION AND DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR SWING, FOUND BOTH RT GREEN LIGHTS BURNED OUT, REPLACED BULBS AND SYSTEM OPS CHECKED GOOD IAW MM CHAPTER 32-002. 2K73 4F4 FRTA50NM E44NE 20040601001072004060100107NM 2004 6 1 04FDEA01474 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RT WING - OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED = 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040601001102004060100110NM 2004 6 1 04FDEA01477 120040526A5753 HINGE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING OB FLAP AFT IB HINGE, FOUND IB ACTUATOR HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS= 0.400, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.398. COMPLIED WITH FEDEX EA 1-5750-76716, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR 2L73 4F4 FRTA22WE E13NE 20040601001162004060100116WP 2004 6 1 04FDEA01494 120040527A5753ARC0503 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5740-77431 WINGS-RT OB FLAP, OUTBD HINGE ASSY P/N ARC0503 PIVOT BORE REWORK. COMPLIED WITH EA 8-5740-77431 WINGS-RT OB FLAP, OB HINGE ASSY P/N ARC0503 PIVOT BORE REWORK AT MAE. 2L73 4F A22WE 20040601001212004060100121NM 2004 6 1 UPS04242426 120040510A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C CRACK ON FUSELAGE SKIN AT BS235.8, LT SIDE, WL 222. REPAIRED IAW SRM 53-30-3, FIGURE 3. 2L73 4F A3WE 20040601001542004060100154SO 2004 6 1 C2XA04SH326 120040527A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040601001562004060100156EA 2004 6 1 COMA0460333 120040524A329717300130 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA RT MLG BROKEN A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01708CA 7235 FLIGHT 5436 ANTI SKID CAUTION DURING T/O. REPLACED THE RT MLG OB WIRE HARNESS. 2L72 4F RTA21EA 20040601001642004060100164 2004 6 1 P9RA20040014 420040531A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR OUT OF POSITION A P9RAK NONE O OTHER UKUNKNOWN 1 SO1114816 49370 AT GATE IN CZM, THE L1 DOOR SLIDE FELL OUT OF ITS COVER. REINSTALLED L1 DOOR SLIDE COVER. 2L72 4F A6WE 20040602000152004060200015NM 2004 6 2 04FDEA01463 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000172004060200017NM 2004 6 2 04FDEA01465 120040526A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CRACKED STRINGER CLIP, STA 950C, STRINGER 3L. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3L IAW SRM 51-30-2. 2L73 4F RTA3WE 20040602000202004060200020NM 2004 6 2 04FDEA01449 120040525A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - INBOARD FLAP AFT OUTBOARD HINGE - FOUND INBOARD PIVOT BORE HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 - 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.252. COMPLIED WITH FEDEX EA 1-5750-76714, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040602000312004060200031NM 2004 6 2 04FDEA01318 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN O/B ATTACHMENT BORE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL DIAMETER: 1.063, FINAL DIAMETER HOLE REAMED TO 1.093. REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000532004060200053 2004 6 2 SWAA041412 420040517A2565D31354 SLIDE BOEING737 7373A4 1384585NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040602000562004060200056NM 2004 6 2 04FDEA01376 120040520A5320FXFAB35411FS FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 FWD PIT - STA 715 - FLOOR SUPPORT L2 EXFOLIATED AT NUT PLATE HOLES. FABBED NEW FLOOR SUPPORT ON TRAVELER T4/430748 & INSTALLED REPAIR IAW SRM 51-40-4 AND 51-30-2, ON NON ROUTINE N00641 AT MAE. 2L73 4F RTA3WE 20040602000582004060200058NM 2004 6 2 04FDEA01378 120040520A5310FXSRM53104 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 AFT CARGO COMPT HAS A CORRODED SHEAR TIE AT FS 970 STR 28L - 29L. FABRICATED SHEAR TIE ON TRAVELER T4/432278 & FABRICATED FLOOR SUPPORT ON TRAVELER T4/430988. REPAIRED & INSTALLED SHEAR TIE AT FS 970 STR 28L - 29L IAW SRM B727 SRM 53-10-4 PAGE 46. 2L73 4F RTA3WE 20040602000622004060200062NM 2004 6 2 04FDEA01382 120040521A531069436834 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-111-01, 2) FWD CARGO BAY SHEAR TIE ON FRAME 720 STR 26 LT IS CORRODED. REMOVED CORROSION ON SHEAR TIE ON FRAME STA 720, STR 26 LT, FWD CARGO BAY. REMOVED .017 3 X 1 INCH FROM .050, OUT OF LIMITS. REMOVED DAMAGED SHEAR TIE, LOCATED, DRILLED, INSTALLED NEW SHEAR TIE IAW SRM 53-10-1, 51-10-6, 51-30-02, FED EX MM 51-20-021-7, 51-20-151-7. 2L73 4F RTA3WE 20040602000702004060200070NM 2004 6 2 04FDEA01037 120040422A5753ARC198414 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75936 - WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040602000792004060200079NM 2004 6 2 04FDEA01363 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.220, EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76674. LT OUTBOARD TRAILING EDGE FLAP INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS. REPAIR. 2L73 4F RTA22WE 20040602000842004060200084NM 2004 6 2 04FDEA01368 120040520A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.450, MATERIAL REMOVED: 0.002, REMAINING THICKNES OF LUG: 0.448. REPAIRED AS PER EA 1-5750-76675 - WINGS - OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2L73 4F RTA22WE 20040602000862004060200086NM 2004 6 2 04FDEA01370 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76676. LT OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2L73 4F RTA22WE 20040602000912004060200091WP 2004 6 2 04FDEA01389 120040521A5730 SKIN DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT WING DROOPED LEADING EDGE O/B L/E HAS GOUGE. REPAIRED LEFT WING DROOPED L/E IAW SRM 57-00-01. GOUGE FOUND OUT OF LIMITS BY NTSPM 04-00-03 .070 BEFORE .045 AFTER. REMOVED & REPLACED BROKEN BRACKET ON O/B RIB IAW SRM 57-00-01, REMOVED AND REPLACED WORN BULB SEAL IAW DPS 3.579. DROOP L/E ON LEFT WING WAS REMOVED AND REINSTALLED ON DOCUMENT N01336. WORK DONE AT MAE. 2L73 4F A22WE 20040602000952004060200095NM 2004 6 2 SWAA041430 120040519A2910312A10104 HYDRAULIC LINE BOEING737 7373H4 1384600NM NR 2 ENGINE LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29635SW 27708 AIR TURNBACK, DECLARED EMERGENCY. DURING CLIMB NR 2 ENGINE HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, ACCOMPANIED BY HYDRAULIC FLUID QUANTITY INDICATING 1/3 FULL. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE PER MM. 2L72 4F RTA16WE 20040602000992004060200099NM 2004 6 2 SWAA041434 120040519A33506104789 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED PM CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040602001022004060200102NM 2004 6 2 ASAA0440077 120040310A33978100022601 WIRE BOEING737 7374Q8 138447QNM CABIN BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01778AS 25110 PDX - FOUND AFT TWO RED EMERGENCY LIGHTS ARE NOT WORKING. REPLACED ONE SECTION BROKEN WIRE. (M) 2L72 4F RTA16WE 20040602001112004060200111NM 2004 6 2 ASAA0410168 120040327A5311 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FRAME IS CRACKED UNDER FLOOR SUPPORT STRUCTURE AT STATION 440. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040602001142004060200114NM 2004 6 2 ASAA0410170 120040327A531565548944 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT CABIN FLOORBEAM LOWER T-CHORD IS CORRODED. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001162004060200116NM 2004 6 2 ASAA0410172 120040327A531565549055 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FORWARD PIT CABIN FLOORBEAM LOWER AREA AT STATION 480 CORRODED. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001232004060200123NM 2004 6 2 ASAA0410179 120040327A575365479307 SKIN BOEING737 737290C 138448VNM LT MID FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT OUTBOARD MID FLAP LOWER SKIN IS CHAFED OUTBOARD OF OUTBOARD CARRIAGE. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001302004060200130NM 2004 6 2 04FDEA01391 120040521A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK FLOOR SUPPORT FOUND CORROSION AT STA 457 LT 87 INCHES. REMOVED IAW SRM 51-31-01 VOL II, NEW SUPPORT MACHINED AS PER DWG ABA8356 AND INSTALLED IAW SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040603000022004060300002NM 2004 6 3 04FDEA01393 120040521A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK - SEAT TRACK FOUND CRACKED AT STA 902-914 RT 28 INCHES. REMOVED AT STA 459 TO STA 535 RBL 27.5 IAW SRM 51-33-01 VOL II, REPAIR TRACK FABRICATED AND INSTALLED IAW SRM 53-70-00 FIGURE 1 VOL I. 2L73 4F RTA22WE 20040603000052004060300005EU 2004 6 3 04FDEA01207 120040510A5534 ATTACH ANGLE AIRBUS310 A310203 3930313EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE 248 RT SIDE OF VERTICAL STAB T/E, AT RIB 26 TOP FLANGE (PANEL ATTACHMENT ANGLE BRACKET) HAS CORROSION ON INNER SIDE OF FLANGE. REPAIRED IAW EA 6-5530-77670A RT SIDE OF VERTICAL STAB T/E AT RIB 26 TOP FLANGE. 2L72 4F RTA35EU 20040603000252004060300025WP 2004 6 3 04FDEA01340 120040519A5320AFA016320 SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 STA 1561 LGN 38R RT LWR UNDERWING FAIRING PANEL SUPPORT FRAME IS CRACKED. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-35-01 AND SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040603000322004060300032EU 2004 6 3 04FDEA01347 120040519A5320 ANGLE AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 AFT PRESSURE BULKHEAD FR 80 INNER ANGLE LABELED LT NR 2 AND SHIM ARE CORRODED [EXFOLIATED]. REPLACED ANGLE AND SHIM ON FR 80 INNER ANGLE LT NR 2 IAW A310 SRM 51-72-10 AND 53-19-17. 2L72 4F RTA35EU 20040603000422004060300042WP 2004 6 3 04FDEA01225 120040512A5753ARC14731 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE. 2L73 4F A22WE 20040603000502004060300050WP 2004 6 3 04FDEA01232 120040512A78309077M89G01 ROD DOUG DC10 DC1010 3022110WP THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 ENGINE NR 3 OUTBOARD T/R HOLD OPEN ROD SAFETY PIN IS ELONGATED. REMOVED AND REPLACED ENGINE NR 3 RT T/R HOLD OPEN ROD IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040603000532004060300053WP 2004 6 3 04FDEA01228 120040512A5753ARC14731 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT WING O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE. 2L73 4F A22WE 20040603000572004060300057 2004 6 3 04FDEA01216 420040510A31404059027903 CONTROLLER DOUG MD11 MD11 3023602NM COCKPIT MALFUNCTIONED A FDEAA UNSCHED LANDING GE MULTIPLE FAILURE VIBRATION/BUFFET CRCRUISE 1 SO25607FE 2868 48547 AT ALTITUDE LOST GOOD AIRSPEED INDICATIONS ON CADC2 AND STBY AIRSPEED INDICATORS CAPT HAD SWAPPED TO CADC2 EARLIER, GOT STICK SHAKER FOLLOWED BY BUFFET. CORRECTED FOR HIGH SPEED, SITUATION WORSENED. LOST ALL AIRSPEED INDICATIONS ON F/O, CAPT, AND STBY INDICATORS. CORRECTED FOR STALL AND STARTED TO GET BETTER. CAPT WENT BACK TO CADC 1 AND GOT GOOD INFO AGAIN. DIVERTED TO CYYC. FOUND ALL HEATING ELEMENTS GOOD, RANG ALL WIRING, VERIFIED ALL SWITCHING FOR GND SHIFT CIRCUITS. FOUND NO FAULTS WITH WIRING. REPLACED RELAY'S R2-5111, R2-5102, AND R2-5109, HAD TROUBLE COMMUNICATING WITH MSC REPLACED MSC, COMPARISON TESTS GOOD AFTER PURGE AND RR OF MSC. 2L73 4F RTA22WE 20040603000622004060300062EU 2004 6 3 04FDEA01234 120040512A5511 SPAR AIRBUS310 A310203 3930313EU HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 RIGHT HORIZONTAL UPPER TRAILING EDGE SPAR I/B OF RIB 5 HAS LEVEL 2 CORROSION, APPROX 6 INCHES L X .800 INCH W, NOTE: PREVIOUS STRAP REPAIR INSTALLED I/B OF DAMAGE TO RIB 3. REMOVED PREVIOUS REPAIR, REMOVED CORROSION, MAT'L LOSS GREATER THAN 10 PERCENT, FABRICATED NEW REPAIR ANGLE. INSTALLED NEW REPAIR ANGLE AND TREATED, PRIMED AND APPLIED TOP COATING IAW A310 SRM 55-11-21, 51-23-20, AND 51-74-10. 2L72 4F RTA35EU 20040603000632004060300063NM 2004 6 3 04FDEA01283 120040518A5320NPB67685 STIFFENER DOUG MD11 MD11 3023602NM RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT MAIN LANDING GEAR WHEEL WELL FWD STIFFENER AT STA X= -74 FOUND CRACKED. RIGHT MAIN LANDING GEAR WHEEL WELL FWD STA X= -74 CRACKED STIFFENER REMOVED, FABRICATED AND NEW STIFFENER INSTALLED AS PER FEDEX EA 1-5310-76007. FUSELAGE - MAINFRAME - CENTER WING STRUCTURE/INTERIM REPAIR. 2L73 4F RTA22WE 20040603000662004060300066NM 2004 6 3 04FDEA01373 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 0.593, MAX ALLOWABLE DIAMETER: 0.667, FINAL DIAMETER: 0.661 WITHIN LIMIT. REPAIRED AS PER EA 1-5750-76676. LEFT HAND OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2L73 4F RTA22WE 20040603000782004060300078NM 2004 6 3 ASMF200405028 120040528A77112047021 INDICATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE COCKPIT FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23881LF2400 53051 725563 DURING TRANSIT CHECK RT ENGINE EPR INDICATOR WAS DETECTED OUT OF SERVICE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIGHT SERVICE PT2 HOSE WAS REPLACED IAW MM 77-11-01 AND LEAK CHECK WAS PERFORMED, ALL CORRECT. ENGINE RUNNING WAS PERFORMED AND PNEUMATIC LEAK WAS DETECTED ON 13A STAGE VALVE DUCT CLAMP AND PT2 HOSE WAS BURNED. CLAMP WAS REPLACED AND LEAK TEST WAS CORRECT, EPR INDICATOR WAS REPLACED AND TRIM PROCEDURE WAS PERFORMED IAW MM 71-00-01 AND 77-10-00, ALL CORRECT. 2L72 4F4 FRT E9NE 20040603000832004060300083WP 2004 6 3 UPS04842445 120040506A5753 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE T/E FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 LW OB FLAP UPPER SURFACE DOUBLER GOUGED AT I/B ICE BREAKER GUIDE TRACK STA XF219. REMOVED DAMAGED DOUBLER FAB NEW DOUBLER ALODINED AND PRIMED INSTALLED NEW DOUBLER. 2L74 4F4 FRT4A25 E2GL 20040603000902004060300090EA 2004 6 3 WVE2004F00015 120040510A5712601R1020328 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT WING CRACKED E WVERK NONE O OTHER ININSP/MAINT 1 EA09597SW 7293 RT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2L72 4F4 FRTA21EA E15NE 20040603000922004060300092SO 2004 6 3 C2XA04SH339 120040601A532014521725403 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 7 FIG 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040603000942004060300094NM 2004 6 3 AWXA200400581 120040530A2560P2070001214 FLASHLIGHT BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28326AW 23258 EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CABIN FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040603001002004060300100EA 2004 6 3 QXEA200400379 120040530A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 FORWARD BAGGAGE COMPARTMENT ENTRY-WAY OVERHEAD CHIMNEY HAS A TEAR IN THE METAL WEBBING. REMOVED AND REPLACED CHIMNEY ASSEMBLY. 2L72 4F RTA21EA 20040603001022004060300102EA 2004 6 3 WVE2004F00016 120040510A5320601R3111357 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09597SW 7293 FLOOR SUPPORT ANGLES AT FS280, LBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2L72 4F4 FRTA21EA E15NE 20040603001042004060300104SO 2004 6 3 C2XA04SH341 120040601A531514522461011 DOUBLER EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C CHECK THE RT OMEGA BEAM AFT DOUBLER WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040603001062004060300106NE 2004 6 3 ALG2004F00023 220040511A73217046M95G03 ECU BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE NR 1 ENGINE FAILED A ALGAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW03391AL 28103 NR 1 ENGINE FAILED DURING TAKE OFF, AIRCRAFT RETURNED TO PLATFORM. MAINT REMOVED NR 1 ENGINE HMU AND INSTALLED SERVICEABLE HMU. ALSO REMOVED NR 1 ENGINE ECU AND INSTALLED SERVICEABLE ECU. 2G72 4U4 U H10SW E8NE 20040603001082004060300108SO 2004 6 3 LR7A04058 120040526A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW JOB CARD HB5301 FOUND RT SIDE FS 405 FUSELAGE SKIN CRACKED AT ESCAPE HATCH CUTOUT UPPER FWD CORNER, RBL 82, WL 226. REPAIRED IAW SRM SMP 583 53-40-50, REPAIR H. NR 0003. 2H74 4T4 T A1SO E282 20040603001182004060300118WP 2004 6 3 ASAA0480291 120040420A5730ARB0975535 PANEL DOUG DC9 DC983 3022083WP WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FUEL PANEL IS CORRODED. REPLACED PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040603001202004060300120WP 2004 6 3 ASAA0480350 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1357C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001222004060300122WP 2004 6 3 ASAA0480347 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1363C RUBSTRIP DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001242004060300124WP 2004 6 3 ASAA0490343 120040421A533059360331 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND AFT PIT SKIN BETWEEN STATION 1149 AND 1155, LONGERON 29L-30 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER EA 5330-01774. (M) 2L72 4F RTA6WE 20040603001302004060300130NM 2004 6 3 ASAA0410205 120040424A5340693535222 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND STRINGER CLIP AT STATION 986, STRINGER 24L IS CORRODED. REMOVED DAMAGED CLIP AND INSTALLED REPLACEMENT CLIP IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040603001312004060300131WP 2004 6 3 04FDEA01268 120040514A5753ARC2512502 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP - AFT HINGE ASSY ARC2512 PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP AFT HINGE ASSY ARC 2512 PIVOT BORE CORROSION AT MAE. 2L73 4F A22WE 20040603001332004060300133NM 2004 6 3 04FDEA01270 120040514A5320 TRANSITION PANEL BOEING727 727200 138407ENM CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 FWD PIT - LT TRANS PANEL STR 675 - 2 NUT PLATE HOLES EXFOLIATED. REMOVED & REPLACED TRANS ANGLE IAW SRM 51-30-2. ORIGINAL TRANS ANGLE .050. REMOVED .050 IAW SRM 51-10-6. REMAINING .000 OUT OF LIMITS IAW SRM 53-10-1 FIG 1 PG 2. FABRICATED NEW TRANS ANGLE FROM 7075-T6 .050C BATCH 8R00071001 IAW SRM 51-20-1 AND SRM 51-30-5. TREATED AND PRIMED BARE METAL IAW SRM 51-10-2. 2L73 4F RTA3WE 20040604000022004060400002NM 2004 6 4 04FDEA01274 120040514A3350S106 BATTERY BOEING727 727200 138407ENM CABIN DISCHARGED A FDEAK NONE L NO TEST ININSP/MAINT 1 SO25266FE 21672 FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. INSTALLED RECHARGED BATTERIES INTO EMER LIGHT UNIT IAW PART 33-50-00 OF AMM. OPS CHECK NORMAL. 2L73 4F RTA3WE 20040604000032004060400003NM 2004 6 4 04FDEA01275 120040515A3350S106 BATTERY BOEING727 727200 138407ENM CABIN DISCHARGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25491FE 21529 COCKPIT EMERGENCY EXIT LIGHT REMAINS ON. INSTALLED NEW BATTERIES IN COCKPIT EMERGENCY LIGHT ASSY PER STD MX PRAC & SECURED LIGHT BRACKET WHICH WAS STARTING TO COME LOOSE. EMERGENCY LIGHTS OPS CHECK NORMAL. 2L73 4F RTA3WE 20040604000042004060400004EU 2004 6 4 04FDEA01276 120040515A2611 SMOKE DETECTOR AIRBUS300 A300B4622R 3930312EU CARGO BAY FAULTY A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25719FD 388 INFLIGHT AVIONIC SMOKE WARNING AT FL 310 SEVERAL WARNINGS ON AND OFF DURING ICING CONDITIONS THEN OFF WHEN CLEAR FOR SEVERAL MIN THEN ON CONTINUOUSLY. DIVERTED INTO DEN 170NM OUT, FOLLOWED ECAM PROCEDURES NEVER NOTICED ANY SMOKE. UNEVENTFUL LANDING AND TAXI IN. TROUBLESHOT PER TSM261500 P101, REMOVED AND REPLACED CARGO SMOKE DETECTOR 13WA PER AMM-2619124. OPS CHECK NORMAL. CREW ADVISED SNIFFER USED, NO SMOKE DETECTED. MX CHECKED AND CONFIRMED NO SMOKE DURING OPS CHECK. 2L72 4F RTA35EU 20040604000052004060400005WP 2004 6 4 04FDEA01277 120040516A2540AWD0012 PAN DOUG DC10 DC1010 3022110WP FWD LAVATORY DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 C/W EA 8-2540-77416 FWD LAV FLOOR PAN REPAIR. FWD LAV FLOOR PAN REPAIRED IAW EA 8-2540-77416 ON MAE TRAVLER T4/431252. 2L73 4F A22WE 20040604000102004060400010EU 2004 6 4 04FDEA01440 120040525A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 3R (FROM 14 INCHES FWD OF FR 59 TO FR 69) HAS 5 EA AREAS OF CORROSION, INCLUDING ON AND UNDER SCALLOPS. 8 INCHES AFT OF FR 64, 10 INCHES FWD OF FR 65, 8 INCHES AFT OF FR 65, 6 INCHES FWD OF FR 65, AND 8 INCHES AFT OF FR 67. REMOVED SEAT TRACK FROM FR 62 TO FR 69 AND REPLACED WITH REPLACEMENT TRACK. TREATED, PRIMED, TOP COATED, REPAIRED AND ASSEMBLED PER SRM A300-600 51-21-10 AND 53-10-16 PG 205 FIG 201. 2L72 4F RTA35EU 20040604000112004060400011EU 2004 6 4 04FDEA01441 120040525A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 3R SECTION (10 INCHES FWD OF FR 74 TO JUST AFT OF FR 80/82) HAS 6 EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 6 INCHES FWD OF FR 74, BETWEEN FR 74 AND FR 75, BETWEEN FR 75 AND 76, 1 INCH FWD OF FR 76, 1 INCH AFT OF FR 76, AND 7 INCHES AFT OF FR 76. REMOVED SEAT TRACK, REPLACEMENT TRACK FABBED FROM 7075-T6511, TREATED, PRIMED, TOP COATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM A300-600 51-21-10, 51-74-10, 53-10-16 PG 205 FIG 201. 2L72 4F RTA35EU 20040604000152004060400015NM 2004 6 4 04FDEA01445 120040525A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FLOOR FRAME DENTED. FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FRAME DENTED OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665. 2L73 4F RTA3WE 20040604000192004060400019NM 2004 6 4 SWAA041538 120040530A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727B, BETWEEN STRINGER 27L AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SKIN PER ER. 2L72 4F RTA16WE 20040604000222004060400022NM 2004 6 4 SWAA041541 120040531A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 847 TO BS 867, LBL 65 TO LBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20040604000252004060400025NM 2004 6 4 SWAA041529 120040531A53306545800219 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SERVICE CHECK, FOUND FUSELAGE SKIN BELOW R1 DOOR AT TEXAS PATCH, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040604000272004060400027NM 2004 6 4 SWAA041531 120040601A278265446519 ACTUATOR BOEING737 7372H4 138448CNM L/E SLAT FAILED A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29073SW 22673 AIR TURNBACK, NR 2 L/E SLAT WOULD NOT RETRACT, VISUALLY CONFIRMED. REMOVED AND REPLACED NR 2 L/E SLAT ACTUATOR PER MM. 2L72 4F A16WE 20040604000312004060400031NM 2004 6 4 SWAA041545 120040602A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 2 ABC, LOOSE. SECURED OVERHEAD LIGHT LENS PER MM. 2L72 4F RTA16WE 20040604000322004060400032 2004 6 4 SWAA041546 420040602A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040604000332004060400033NM 2004 6 4 04FDEA01417 120040524A5311ACA71231 FRAME DOUG MD11 MD11 3023602NM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK - FRAME FOUND TWO CHAFED MARK AT STA 535 LT BETWEEN 9G NET ATTACH YOKE. MAIN DECK - FRAME AT STA 535 LT BETWEEN 9G NET ATTACH YOKE DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2L73 4F RTA22WE 20040604000362004060400036NM 2004 6 4 04FDEA01561 120040602A5311 FAILSAFE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01, 2) ON FRAME, STA 760, RBL 70, WL 207. FOUND CORROSION ON FRAME FAIL SAFE STRAP AT BS 760 RBL 70, WL 207 TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED DAMAGED SECTION OF FAIL SAFE STRAP. FABRICATED REPAIR SECTION OF STRAP AND DOUBLER PER SRM 51-10-4 FIGURE 1 AND INSTALLED PER SRM 51-30-2. 2L73 4F RTA3WE 20040604000382004060400038NM 2004 6 4 SWAA041547 120040602A5330654576972 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT E/E COOLING DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040604000402004060400040NM 2004 6 4 SWAA041549 120040602A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C1 CHECK, FOUND STRINGER 19R AT BS 735, CRACKED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040604000412004060400041NM 2004 6 4 SWAA041550 120040602A3260285A16004 PSEU BOEING737 7377H4 1384404NM E/E BAY FAULTY A SWAAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW29762SW 27876 AIR TURNBACK, AFTER TAKEOFF FROM MDW WITH GEAR AND FLAPS RAISED THE TAKEOFF WARNING HORN GOES OFF WITH POWER REDUCTION. REMOVED AND REPLACED PSEU PER MM. 2L72 4F RTA16WE 20040604000432004060400043NM 2004 6 4 SWAA041552 120040602A53106547955 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR AFT FRAME CUTOUT AT NR 5 DOOR STOP, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040604000442004060400044NM 2004 6 4 SWAA041553 120040602A531265C32677 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB AT BS 1016, BBL 0, BS 1016, LBL 2, CORRODED. REMOVED AND REPLACED WEB SECTIONS PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040604000482004060400048NM 2004 6 4 SWAA041557 120040602A575465C26686 WEDGE BOEING737 7373H4 1384600NM L/E SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT T/E WEDGE, DELAMINATED. REPAIRED T/E WEDGE PER SRM. 2L72 4F RTA16WE 20040604000502004060400050NM 2004 6 4 SWAA041559 120040602A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040604000512004060400051NM 2004 6 4 SWAA041560 120040602A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727D, STRINGER 8R AND STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20040604000542004060400054 2004 6 4 SWAA041534 420040601A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040604000592004060400059NM 2004 6 4 SWAA041515 120040530A3350110049 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND EEPLS AT OVERWING EXITS INOP. REMOVED AND REPLACED EEPLS BATTERY PER MM. 2L72 4F A16WE 20040604000602004060400060NM 2004 6 4 SWAA041516 120040530A33506104791 BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND FWD ENTRY AND FWD SERVICE DOORS OVERHEAD EMERGENCY EXIT LIGHTS, INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040604000622004060400062 2004 6 4 SWAA041518 420040531A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040604000632004060400063NM 2004 6 4 SWAA041519 120040531A532065C346701 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING, CRACKED. REPAIRED HINGE BOX FITTING PER EA. 2L72 4F RTA16WE 20040604000662004060400066NM 2004 6 4 SWAA041522 120040531A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 307, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040604000682004060400068NM 2004 6 4 SWAA041524 120040531A3350582240 POWER SUPPLY BOEING737 7373K2 13844BANM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED A2 CHECK, FOUND LT AND RT EMERGENCY EXIT MARKERS WILL NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY PER MM. 2L72 4F RTA16WE 20040604000722004060400072NM 2004 6 4 SWAA041528 120040530A278265447641 ACTUATOR BOEING737 7377H4 1384404NM L/E SLAT FAILED A SWAAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 SW29785SW 30602 AIR TURNBACK, ON TAKEOFF WITH FLAP RETRACTION L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS UP. CONFIRMED PARTIALLY EXTENDED. REMOVED AND REPLACED ALL EIGHT L/E SLAT ACTUATORS PER MM. 2L72 4F RTA16WE 20040604000732004060400073NM 2004 6 4 SWAA041436 120040519A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29642WN 27715 DURING RON CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 14 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040604000742004060400074NM 2004 6 4 SWA041437 120040520A2612896768 FIRE LOOP BOEING737 7373H4 1384600NM APU BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29326SW 23690 AIR TURNBACK, DURING CLIMBOUT, APU FIRE INDICATION, C/W QRH AND RETURNED TO IND. REMOVED AND REPLACED APU FWD FIRE LOOP PER MM. 2L72 4F RTA16WE 20040604000752004060400075NM 2004 6 4 SWAA041438 120040520A52306547952524 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR, FWD FRAME AT SPRING TENSION PLATE, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20040604000772004060400077NM 2004 6 4 SWAA041440 120040520A335007912 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29764SW 27878 EEPLS COVER MISSING LEFT FWD SIDE. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040604000782004060400078NM 2004 6 4 SWAA041441 120040520A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 L2 DOOR EMERGENCY EXIT OVERHEAD LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040604000792004060400079EA 2004 6 4 WVE2004F00014 120040510A5712601R1020327 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT WING CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09597SW 7293 LEFT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE; STRESS. RECOMMENDATION: REPAIR IAW MFG REPAIR EO. (EA09200402314) 2L72 4F4 FRTA21EA E15NE 20040604000832004060400083EU 2004 6 4 USAA040163 120040424A5320D5347219020300 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW 0936 FLOOR SUPPORT BETWEEN FRAME 68 AND 69 AT Y1244.6, Z240. CORROSION: LEVEL 2; TASK NR JA-250-53500. REMOVED AND REPLACED NEW FLOORBEAM. 2L72 4F4 FRTA28NM E2GL 20040604000852004060400085EU 2004 6 4 USAA040168 120040424A5320D5347219020300 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOOR SUPPORT, 3 INCHES X 1.5 INCHES W X .020 INCH D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 FLOOR SUPPORT BETWEEN FR 68 AND 69 AT Y1244.6, Z240. REMOVED AND REPLACED NEW FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14. 2L72 4F4 FRTA28NM E2GL 20040604000862004060400086EU 2004 6 4 USAA040167 120040426A5347D53112782202 SEAT TRACK AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 SEAT TRACK, 2 INCHES X 1 INCH X .100 INCHES AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y-1292, Z240. REMOVED AND REPLACED TRACK IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040604000902004060400090EU 2004 6 4 USAA040166 120040427A5320D5347209000300 TRACK AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 TRACK, 3.5 INCHES X 3.5 INCHES X .170 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 64 TO 70, Y736.6, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-14, 51-42-11, 51-71-12. 2L72 4F4 FRTA28NM E2GL 20040604000912004060400091SO 2004 6 4 O2G2004F00001 120040516A27401159C2008029 CONTROL CABLE GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU PITCH TRIM BROKEN E O2GAK NONE F FLT CONT AFFECTED TOTAKEOFF 1 NE03929WT 1317 CREW CALLED IN TO SAY PITCH TRIM JAMMED 2 DEGREES NOSE UP. FOUND PITCH TRIM CABLE BROKEN AT PULLEY IN RT HORIZONTAL STAB. FOUND CABLE WAS RUBBING AGAINST THE PULLEY BOLT, WHERE THE CABLE WAS NOT IN THE PULLEY GROVE CAUSING IT TO FRAY, WEAR AND BREAK. REPLACED TRIM CABLE. 2L72 4F4 FRTA12EA E25NE 20040604000922004060400092NE 2004 6 4 MDR04048 120040412A64106516100010041 BLADE SKRSKYS64 S64E 8142604NE TAIL ROTOR CRACKED A JYDRK NONE O OTHER ININSP/MAINT 1 NM09CGESG 64V13981435 64065 DURING ROUTINE INSPECTION, THE POCKET (PN 6516100010041) WAS FOUND CRACKED ON THE OB SIDE APPROX 6 INCHES FROM THE LE AND 56.5 INCHES FROM THE TIP END. THE CRACK RUNS UNDER THE STIFFENER ON THE POCKET. THE CRACK IS APPROXIMATELY 1.25 INCHES IN LENGTH. PROBABLE CAUSE IS ROUGH EDGES ON SKIN. 2G72 4U H4EA 20040604000962004060400096CE 2004 6 4 GUU2004F00005 120040505A2840 WARNING LIGHT BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA FUEL SYSTEM INTERMITTENT A GUUAO OTHER N FALSE WARNING CRCRUISE 1 SO1748544 UE183 DURING FLIGHT, LT FIREWALL FUEL VALVE LIGHT FLICKERED. INSPECTED LT FIREWALL SYSTEM. NO DEFECTS NOTED. 2L72 4T3 TRTA24CE E2NE 20040604000972004060400097CE 2004 6 4 GUU2004F00004 120040504A3240 LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA BRAKE SYSTEM CONTAMINATED A GUUAO OTHER O OTHER TXTAXI/GRND HDL 1 SO1781538 UE199 DURING TAXI, VERY POOR BRAKING ACTION ON RT PEDAL. BLED RT BRAKE SYSTEM. OPS CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040604000982004060400098NM 2004 6 4 GAIA04072 120040506A323065402391 ROD BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE LT MLG UNSERVICEABLE A GAIAA UNSCHED LANDING O OTHER CLCLIMB 1 SW076806 19481 AT DEPARTURE, LT MAIN GEAR FAILED TO RETRACT. THIS WAS VERIFIED BY THE TOWER. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED AFT RADIUS ROD ON OB DOOR LT MAIN WHEEL WELL. DOOR FIT AND OPS CHECK, OK. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040604000992004060400099EU 2004 6 4 USAA040173 120040425A5315D5347218920200 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOORBEAM, 1.0 INCH L X 1.5 INCH W X .022 INCH D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 65-68, -Y 1244.6, Z240. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-00-14 & 51-42-11. 2L72 4F4 FRTA28NM E2GL 20040604001002004060400100EU 2004 6 4 USAA040183 120040505A5320D5367175301800 PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW15976 0904 PANEL, 5 INCHES LONG, CRACKED, FR64, Y1732, Z240. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. 2L72 4F4 FRTA28NM E2GL 20040604001012004060400101EU 2004 6 4 USAA040177 120040429A5320D5347112420000 WEB AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 WEB, 3 INCHES L X 2INCHES W X .020 INCHES D, CORROSION, LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 69-70 + Y1244.6, Z240. REMOVED AND REPLACED WEB IAW SRM 51-74-00, 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E2GL 20040604001032004060400103EU 2004 6 4 USAA040175 120040429A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOOR SUPPORT, 1.9 INCHES X .6 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2, TASK NR JA-220-53500, FR 22, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER, REMOVED DAMAGE IAW SRM 51-74-00, 51-21-11, 51-75-12. 2L72 4F4 FRTA28NM E2GL 20040604001082004060400108EU 2004 6 4 USAA040184 120040506A5320D5348015900500 PLATE AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW15976 0904 PLATE, 2.00 INCH LONG X .05 INCH AREA, EXFOLIATED CORROSION; LEVEL 2; TACK NR JA-260-53500 R2 DOOR, AFT GIRT BAR PLATE ASSY, FR 68-Y1292. INSTALLED NEW PLATE IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040604001102004060400110WP 2004 6 4 AMTA200400555 120040514A33505165744 CHARGER LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE CABIN MALFUNCTIONED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 RT AFT PWR PACK FOR EMERGENCY LIGHT DOES NOT FLASH. LIGHT IS ON SOLID. REMOVED AND REPLACED POWER PACK IAW MM. OPERATION NORMAL AT THIS TIME. 2L73 4F4 F A23WE A12EU 20040604001132004060400113WP 2004 6 4 GTIA040400 120040331A78305938050503 THRUST REVERSER DOUG DC9 DC983 3022083WP NR 1 ENGINE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND NR 1 ENG ESN P725858D S/N 49356 THRUST REVERSER HAS HEAT DAMAGE ON INTERIOR SURFACE OF TRAILING EDGE. REMOVED NR 1 ENGINE THRUST REV. INSTALLED NR 1 ENGINE THRUST REVERSER. (M) 2L72 4F RTA6WE 20040604001152004060400115WP 2004 6 4 GTIA040402 120040403A5320 CHANNEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND AFT PIT ENLARGED HOLE ON SUPPORT CHANNEL STATION 1212, L27R. UPON FURTHER INVESTIGATION SUPPORT CHANNEL FOUND TO HAVE CORROSION. REMOVED SUPPORT CHANNEL. FABRICATED REPAIR SUPPORT CHANNEL. INSTALLED REPAIR SUPPORT CHANNEL. (M) 2L72 4F RTA6WE 20040604001162004060400116WP 2004 6 4 GTIA040403 120040401A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND E/E COMPARTMENT STATION 1212 STRINGER 29R SUPPORT CORRODED. UPON FURTHER INVESTIGATION, FOUND SUPPORT TO BE INTERCOSTAL. CENTER DOUBLER IS OUT OF LIMITS. FABRICATED NEW DOUBLER. INSTALLED INTERCOSTAL AND DOUBLER. (M) 2L72 4F RTA6WE 20040604001172004060400117WP 2004 6 4 GTIA040404 120040407A5753 VANE DOUG DC9 DC983 3022083WP T/E FLAP DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND LEFT NR 5 OUTBOARD FLAP OUTBOARD VANE GOUGED, CHAFED AND CORRODED. REPAIRED FLAP VANE. (M) 2L72 4F RTA6WE 20040604001202004060400120WP 2004 6 4 GTIA040407 120040401A5753 DOUBLER DOUG DC9 DC983 3022083WP RT FLAP VANE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND DISBOND OF PREVIOUS REPAIR ON UPPER SURFACE OF RIGHT NR 2 INBOARD FLAP VANE. REMOVED PREVIOUS REPAIR. REPAIRED AREA. (M) 2L72 4F RTA6WE 20040604001232004060400123WP 2004 6 4 GTIA040411 120040409A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND AFT PIT INTERCOSTAL ASSEMBLY STATION 1150 BETWEEN L28R AND L29R HAS CORROSION. LOCATED AND DRILLED NEW INBOARD AND OUTBOARD T-CLIPS. (M) 2L72 4F RTA6WE 20040604001242004060400124WP 2004 6 4 GTIA04412 120040409A5320 CLIP DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND INBOARD T-CLIP JAM BEAM FS 1155 FASTENER HOLES ELONGATED, CORROSION. LOCATED AND DRILLED NEW INBOARD T-CLIP. (M) 2L72 4F RTA6WE 20040604001262004060400126WP 2004 6 4 GTIA040414 120040409A5320 ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND AFT PIT DOOR BEAM TO SKIN ANGLE SUPPORT STATION 1155 CORRODED. ANGLE WAS FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED HOLES ANGLE SUPPORT. (M) 2L72 4F RTA6WE 20040604001272004060400127WP 2004 6 4 GTIA040397 120040503A3350 SIGN DOUG DC9 DC983 3022083WP CABIN MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FLL - FLT 367 - FOUND L-2 DOOR AFT EXIT SAFETY GLO SIGN MISSING. INSTALLED NEW EXIT SAFETY GLO SIGN. (M) 2L72 4F RTA6WE 20040604001282004060400128WP 2004 6 4 GTIA040417 120040311A55235930497502 TAB DOUG DC9 DC982 3022082WP RT ELEVATOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB DELAMINATED AND HAS NUMEROUS DENTS. REMOVED FLOAT TAB. INSTALLED FLOAT TAB. (M) 2L72 4F A6WE 20040604001292004060400129NM 2004 6 4 ASAA0440043 120040221A3397 WIRE BOEING737 7374Q8 138447QNM CABIN EXPOSED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 ANC - FOUND FLOOR TRACK LIGHTING WIRING COMPLETELY EXPOSED AND DISCONNECTED AT ROWS 9-10. RECONNECTED WIRING AND INSTALLED PROTECTIVE COVER ON TRACK ROWS 9-10. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040604001352004060400135NM 2004 6 4 ASAA0410189 120040411A531565549073 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND CORROSION ON FLOORBEAM RPR STRAP AT FS 767. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-01465. (M) 2L72 4F A16WE 20040604001362004060400136NM 2004 6 4 ASAA0410188 120040411A531565549072 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND CORROSION ON FLOORBEAM RPR STRAP AT FS 747. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-01466. (M) 2L72 4F A16WE 20040601001202004060100120NM 2004 6 1 04FDEA01508 120040528A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING OB FLAP IB HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 FIG 1, PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.429, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.427. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS I/B HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE REPAIR. 2L73 4F RTA22WE 20040601001242004060100124NM 2004 6 1 UPS04242430 120040510A5280 DOOR BOEING727 72725C 138400HNM RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE: C RT MLG DOOR HAS DEEP INTERGRANULAR CORROSION ON A STRUCTURAL SKIN ELEMENT NEAR THE FWD HINGE AREA. ON REMOVAL OF SKIN, TWO CRACKS FOUND ON TOP AND BOTTOM OF SKIN. REPAIRED IAW SRM 52-80-2 FIG 2. 2L73 4F A3WE 20040601001302004060100130NM 2004 6 1 UPS04242436 120040508A5330 SKIN BOEING727 72725C 138400HNM PWA JT8 JT8D5 52046NE FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE:C 2 DENTS IN SKIN AT BS 1245, STR 19R . REPAIRED IAW SRM 53-30-3, FIG 13A. 2L73 4F4 F A3WE E2EA 20040601001392004060100139NM 2004 6 1 QXEA200400373 120040526A5320 CLIP DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - AFT CARGO DOOR FORWARD TRACK OB BRACE HAS A CRACKED SUPPORT CLIP. REPAIRED IAW MM SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040601001452004060100145NM 2004 6 1 QXEA200400366 120040526A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE FUSELAGE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - SEAT TRACK NR 4 HAS CHAFE IN CENTER OF TRACK FROM STATION X285 TO X298. REPLACED NR 4 SEAT TRACK. 2H72 4T4 TRTA13NM E20NE 20040601001502004060100150WP 2004 6 1 AALA20040592 120040526A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW LT AND RT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B549 FOR EMERGENCY LIGHTS AT LT AND RT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E2EA 20040601001582004060100158NM 2004 6 1 DHL2004780004 120040528A33501315 LIGHT BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE CABIN LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 EMERGENCY EXIT LIGHT OVER FORWARD ENTRY REQUIRES REINSTALLATION. LIGHT WILL NOT STAY SECURED. RE-LAMPED AND REINSTALLED EMERGENCY EXIT LIGHT IAW M/M 33-50-91, OPS CHECKED GOOD. BULB P/N: 1315 (2 EA.) 2L73 4F4 F A3WE E2EA 20040601001592004060100159NM 2004 6 1 DHL2004741006 120040529A3231 DOOR BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE NLG OUT OF ADJUST A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01741DH 21931 AT 260 MACH .78 A THUMPING NOISE WAS HEARD IN THE NOSE GEAR AREA ACCOMPANIED WITH RED DOORS LIGHT AND YELLOW NOSE DOOR LIGHT S/O'S PANEL ILLUMINATED. COMPLETED ABNORMAL, GEAR HANDLE MOVED TO UP POSITION THUMPING NOISE STOPPED. ADJUSTED NOSE GEAR WHEEL WELL DOORS IAW BMM CHAPTER 32-22-01. OPS CHECKED GOOD ON GROUND. 2L73 4F4 FRTA3WE E2EA 20040601001622004060100162EU 2004 6 1 MALA040419 120040530A3020 THERMOSTAT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE FAULTY A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15402XJ 340B402 RT ENGINE INTAKE LIGHT CYCLED ON AND OFF NUMEROUS TIMES; RAN QRH--NO CHANGES. IT CYCLED FOR THE REMAINDER OF FLIGHT. AIR RETURN TO DTW. MAINTENANCE FOUND NR 3 THERMOSTAT ON LOWER DUCT OPEN--SWAPPED TO NR 4 POSITION. COMPLETED OP'S CK'S IAW AMM. ALL CHECKS GOOD. SEE 409 NR 131454 FOR DETAILS. 2L72 4T4 TRTA52EU E8NE 20040601001662004060100166NM 2004 6 1 QXEA200400375 120040526A3260401020101 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA LT MLG DOOR OUT OF ADJUST A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09414QX5763 4061 SEA - FLIGHT 9999 - WITH THE GEAR RETRACTED AND IN LEVEL FLIGHT, THE LT MAIN GEAR DOOR CYCLED. ALSO, THE LT MAIN GEAR INDICATED UNSAFE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LT GEAR DOOR CLOSED PROXIMITY GAP SENSOR TOO FAR. MAINTENANCE RE-RIGGED THE PROX SENSORS AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040602000022004060200002NM 2004 6 2 04FDEA01510 120040528A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), UPPER I/B MOUNTING BOLT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 0.879, FINAL DIAMETER: 0.952, MAX ALLOWABLE DIAMETER: 0.944, EXCEED ALLOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2L73 4F RTA22WE 20040602000032004060200003NM 2004 6 2 04FDEA01511 120040528A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED ALLOWABLE LIMIT AS PER CMM 57-44-08 PAGE 407 FIG 401. REPAIRED AS PER EA 1-5750-76678. RT OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, UPPER I/B ATTACHMENT FLANGE AND BORE. REPAIR. 2L73 4F RTA22WE 20040602000062004060200006EU 2004 6 2 04FDEA01514 120040528A5320 TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MAIN CABIN CROSS TRACK AT FR 57.1 BETWEEN TRACKS 2 AND 3R HAS ONE EA AREA OF CORROSION. REMOVED AND REPLACED CABIN CROSS TRACK AT FR 57.1 BETWEEN TRACKS 2 AND 3R IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040602000122004060200012NM 2004 6 2 04FDEA01460 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS= 0.503, MATERIAL REMOVED= 0.005, REMAINING THICKNESS= 0.498. COMPLIED WITH FEDEX EA #1-5750-76723, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000132004060200013NM 2004 6 2 04FDEA01461 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.125. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76723, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000162004060200016NM 2004 6 2 04FDEA01464 120040526A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FRAME UPPER CHORD DENTED BS 1010, RBL 30 ABOVE STR 26R. CUT OUT DAMAGED AREA OF FRAME AT BS 1010, RBL 30 ABOVE STR 26R IN 1.75 X 1.5 DIAMETER AREA. FABRIATED TYPICAL FORMED SECTION REPAIR. ALODINED, PRIMERED AND INSTALLED IAW SRM 51-40-3 FIGURE 1, SRM 51-10-2 AND SRM 51-30-2. 2L73 4F RTA3WE 20040602000182004060200018WP 2004 6 2 04FDEA01466 120040526A5420AUH70301 SUPPORT DOUG DC10 DC1010 3022110WP NR 3 PYLON CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 ENGINE NR 3 THROTTLE CABLE PYLON SUPPORT IS CHAFING AGAINST THE ENGINE CASING. REMOVED AND REPLACED CABLE SUPPORT GUIDE P/N AUH7030-1 IAW SRM 51-33-01. 2L73 4F A22WE 20040602000282004060200028NM 2004 6 2 04FDEA01315 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), FOLLOW UP SYSTEM PUSH-PULL ROD ATTACHMENT HORN, MOUNTING BOLT HOLE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. RIGINAL DIAMETER: 0.257, FINAL DIAMETER HOLE REAMED TO 0.325. HOLE REPAIRED AS PER EA 1-5750-76673. RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000332004060200033WP 2004 6 2 04FDEA01320 120040518A5720ARB00313 SUPPORT FITTING DOUG DC10 DC1010 3022110WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT O/B FLAP O/B HINGE REAR SPAR SUPPORT FITTING ATTACHED TO SPAR IS CORRODED IN AND AROUND BARREL NUT HOLE. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-33-01, SRM 51-31-01 AND SRM 51-41-01 AT MAE. 2L73 4F A22WE 20040602000522004060200052NM 2004 6 2 SWAA041426 120040518A53306545760 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040602000772004060200077NM 2004 6 2 04FDEA01360 120040520A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 46 LT STA 1541 CRACKED. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AT CENTER CARGO COMPARTMENT BILGE AREA SPLICE FITTING AT LONGERON 46 LT STA 1541 AS PER SRM 51-33-01 VOL II AND FABRICATED NEW SPLICE FITTING AS PER DWG A5A7114 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33- 01 VOL II. 2L73 4F RTA22WE 20040602000782004060200078NM 2004 6 2 04FDEA01362 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.220, EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76674. LT OUTBOARD TRAILING EDGE FLAP INBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS. REPAIR. 2L73 4F RTA22WE 20040602000822004060200082NM 2004 6 2 04FDEA01366 120040520A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 1.187, MAX ALLOWABLE DIAMETR: 1.190, FINAL DIAMETER: 1.250, EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76675. OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2L73 4F RTA22WE 20040602000942004060200094 2004 6 2 SWAA041429 420040519A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040602001002004060200100NM 2004 6 2 SWAA041435 120040519A3350OL3071BPEGL LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 5 DEF, 2 ABC, INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20040602001052004060200105NM 2004 6 2 ASAA0410164 120040327A5753657190218 STRUCTURE BOEING737 737290C 138448VNM T/E FLAP CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CRACK .25 INCH ON RIGHT WING INBOARD MID FLAP INBOARD FORE FLAP TRACK CUT OUT. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001072004060200107NM 2004 6 2 ASAA0410166 120040327A53156554910502 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORRODED T-CHORD AT STATION 867. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001202004060200120NM 2004 6 2 ASAA0410175 120040327A53156554894502 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND FLOORBEAM CORRODED AT STATION 747. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040603000012004060300001NM 2004 6 3 04FDEA01392 120040521A278140173 POSITION SWITCH BOEING727 727200 138407ENM L/E FLAP FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25276FE 22041 NR 1 L/E FLAP FAILED TO RETRACT AFTER T/O. FOLLOWED RED TABS AND RETURNED TO LAND. REMOVED AND REPLACED NR 1 L/E FLAP POSITION SWITCH PER MM 27-82-001-4. OPS CHECK GOOD PER MM. ACFT OK FOR SERVICE. 2L73 4F RTA3WE 20040603000132004060300013EU 2004 6 3 04FDEA01214 120040511A5511 RIB AIRBUS310 A310203 3930313EU HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE 248 RIGHT HORIZONTAL STAB END RIB UPPER AND LOWER FORMER PROFILE CORRODED. REMOVED CORROSION FROM RIGHT HORIZONTAL STAB, END RIB UPPER & LOWER FORMER PROFILES IAW A310-200 SRM 51-74-10. FABRICATED REPAIR STRAP & INSTALLED IAW EA 6-5510-77671. 2L72 4F RTA35EU 20040603000192004060300019NM 2004 6 3 04FDEA01324 120040518A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR O/B ATTACHMENT SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 FIG 1, PAGES 2 TO 4. ORIGINAL THICKNESS OF LUG: 0.404, MATERIAL REMOVED: 0.004, REMAINING THICKNESS OF LUG: 0.400. REPAIRED AS PER EA 1-5750-76673, RT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040603000222004060300022NM 2004 6 3 04FDEA01217 120040511A5320 CLIP BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 FWD PIT - STA 720D, FRAME FOR BULKHEAD PANEL, BOTTOM SIDE CLIP CORRODED RBL 4. REMOVED CLIP IAW SRM 51-30-2, FABRICATED NEW CLIP IAW SRM 51-20-1, MAE MATERIAL ID 04074,7075-T6 .032 BATCH 671070, INSTALLED NEW CLIP IAW SRM 51-30-2, AT MAE. 2L73 4F RTA3WE 20040603000232004060300023WP 2004 6 3 04FDEA01338 120040519A25508063410 ROLLER TRAY DOUG DC10 DC1010 3022110WP MAIN CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN DECK BALL MAT AT STA 695-775 LBL 60-108 HAS DENT AND IS TORN. REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040603000282004060300028EU 2004 6 3 04FDEA01343 120040519A5320 ANGLE AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 AFT PRESSURE BULKHEAD FR 80 INNER ANGLE {LABELED NR 3} HAS EXFOLIATED CORROSION. REPLACED ANGLE ON FR 80 INNER ANGLE NR 3 LT IAW A310 SRM 51-72-10 AND 53-19-17. 2L72 4F RTA35EU 20040603000332004060300033EU 2004 6 3 04FDEA01348 120040519A5320 WEB AIRBUS310 A310203 3930313EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 WEBBING AT FRAME 80 HAS THREE ELONGATED HOLES COMMON TO STRINGER 57. .300 X .280 HOLE WITH ED OF .250 FROM CENTER. ELONGATED HOLE .225 X .190. ELONGATED HOLE .225 X .180. 2L72 4F RTA35EU 20040603000352004060300035WP 2004 6 3 04FDEA01218 120040511A7830FXFAB2504CDS PANEL DOUG DC10 DC1010 3022110WP THRUST REVERSER MISSING A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 NR 3 ENGINE TR UPPER AFT CLOSE OUT PANEL MISSING A SECTION. REMOVED AND REPLACED CLOSE OUT PANEL FABBED ON MAE TRAV 428784 AT MAE. 2L73 4F A22WE 20040603000582004060300058WP 2004 6 3 04FDEA01414 120040522A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN CARGO COMP SEAT TRACK HAS AREAS OF ELONGATED SCALLOPS FROM FS 1129-1530 LBL 8 AND IS CRACKED AT FS 1179 APPROX 4 INCHES LONG. NDT AT LBL 8 FS 1179 NO CRACK NOTED IAW NTSPM 06-10-01. BLENDED OUT DAMAGED AREAS AT LBL 8 FS 1129-1530 IAW SRM 53-70-00. STA 1129-1249 FOUND IN LIMITS IAW SRM 53-70-00. TREAT & PRIME AREA 1129-1249 IAW SRM 51-21-01, REINSTALLED FS 1129-1249 IAW SRM 51-34-01. FS 1249-1530 IS OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED FS 1249-1530 SEAT TRACK IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040603000682004060300068NM 2004 6 3 04FDEA01031 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040603000722004060300072NM 2004 6 3 04FDEA01418 120040524A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 MAIN DECK - FRAME FOUND TWO CHAFED MARK AT STA 535 RIGHT BETWEEN 9G NET ATTACH YOKE. DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2L73 4F RTA22WE 20040603000742004060300074EU 2004 6 3 04FDEA01420 120040524A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 3R HAS FIVE AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 2 INCHES FWD OF FR 74, BETWEEN FR 74 AND 75, 0.5 INCH AFT OF FR 75, BETWEEN FR 76 AND 77, AND 1 INCH AFT OF FR 77. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS AT ALL LOCATIONS. REMOVED AND REPLACED SEAT TRACK FROM FRAME 73.5 TO 77.5 IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040603000842004060300084WP 2004 6 3 UPS04842447 120040507A532047731501 CLIP DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 MAIN CABIN RT CUSP AT LWR FWD CORNER OF R2 DOOR (FS 1620) EXFOLIATION CORROSION. REMOVED CORROSION ON CLIP IAW DC8-SRM 51-1-8, OUT OF LIMITS. MAT ID AND FAB CUSP CLIP IAW DAC DWG 4773150 PERFORMED DYE PEN TEST. ALODINE AND PRIME CUSP CLIP IAW DC8-SRM 51-1-8 INSTALLED CLIP IAW SRM 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040603000862004060300086WP 2004 6 3 UPS04842449 120040513A53472772 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 MAIN CABIN FS AT 995 SEAT TRACK "E" HAS CORROSION BETWEEN LUGS. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT SEAT TRACK EO DC8-5320-5167C DWG DC8-53B-003. LOCATED, DRILL AND DEBURRED SEAT TRACK PLUS 2 SPLICE FITTING SEAT TRACK. ALODINED AND PRIMED SEAT TRACK. INSTALLED SEAT TRACK PLUS 2 SPLICE FITTING IAW DC8 SRM 51-3-0 AND 51-3-1. 2L74 4F RT4A25 20040603001192004060300119WP 2004 6 3 ASAA0480351 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1379 RUBSTRIP IS DISBONDED. REAMED HOLES. INSTALLED PRP BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001212004060300121WP 2004 6 3 ASAA0480349 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1355C RUBSTRIP IS DISBONED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001232004060300123WP 2004 6 3 ASAA0480346 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1367C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001252004060300125WP 2004 6 3 ASAA0480292 120040420A531199581881 FRAME DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FRAME FASTENER HOLE IS WORN OUT OF ROUND AT FS 1322. REMOVED DAMAGE. INSTALLED REPAIR ANGLE, FILLER, AND SHIM PER SRM 53-05. (M) 2L72 4F RTA6WE 20040603001262004060300126WP 2004 6 3 ASAA0480352 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1371C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001272004060300127WP 2004 6 3 ASAA0480348 120040421A57205930502501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1303 RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUB STRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040604000012004060400001NM 2004 6 4 04FDEA01272 120040515A5754ARB16803 PANEL DOUG MD11 MD11 3023602NM L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING - NR 3 L/E SLAT INBOARD SIDE PANEL FOUND WITH CRACK ACROSS LIGHTENING HOLE. LEFT WING - NR 3 L/E SLAT INBOARD SIDE CRACKED PANEL REMOVED AND NEW PANEL INSTALLED AS PER SRM 51-35-01 VOL 2 & SRM 51-35-02 VOL 2. 2L73 4F RTA22WE 20040604000072004060400007EU 2004 6 4 04FDEA01437 120040524A5347A5361251820002 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MDC AT FRAME 14B SEAT TRACK L2 HAS CORROSION. REMOVED FLOOR DRAIN PANS, REMOVED SEAT TRACK, DRILLED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK AND REINSTALLED FLOOR DRAIN PANS IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040604000082004060400008EU 2004 6 4 04FDEA01438 120040524A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MDCC ON L4 SEAT TRACK BETWEEN FR 40 TO 44, 4 EA SPOT OF CORROSION ON TOP INNER CHANNEL AND SIDE OF SEAT TRACK. REMOVED CORRODED SEAT TRACK, SPLICED IN NEW SECTION BETWEEN FRAMES 40 TO 44.5 IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040604000132004060400013NM 2004 6 4 04FDEA01443 120040525A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO BAY STA 660 FRAME DENTED AT STR 24 LT. REPAIRED DENTED FRAME AT FWD CARGO BAY STA 660, STR 24L IAW EA 7-5310-70665 AND SRM 51-40-3. 2L73 4F RTA3WE 20040604000162004060400016NM 2004 6 4 SWAA041535 120040601A276165C28127 CASTING BOEING737 7372H4 138448CNM LT SPOILER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD NR 5 GROUND SPOILER ACTUATOR CASTING, CRACKED. REMOVED AND REPLACED NR 5 ACTUATOR CASTING PER MM AND SRM. 2L72 4F A16WE 20040604000182004060400018NM 2004 6 4 SWAA041537 120040601A5755654645170A SPOILER BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 4 SPOILER DELAMINATED. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2L72 4F RTA16WE 20040604000202004060400020NM 2004 6 4 SWAA041539 120040530A53206920158 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT LT AND RT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2L72 4F RTA16WE 20040604000232004060400023NM 2004 6 4 SWAA041542 120040601A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040604000262004060400026NM 2004 6 4 SWAA041530 120040601A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040604000292004060400029 2004 6 4 SWAA041533 420040601A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29419WN 29824 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040604000352004060400035WP 2004 6 4 04FDEA01555 120040601A5320ACA7561 PLATE DOUG DC10 DC1010 3022110WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CARGO DOOR CUTOUT AFT JAMB UPPER SCUFF PLATE IS GOUGED. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040604000422004060400042NM 2004 6 4 SWAA041551 120040602A53206546812 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 986, LBL 38, BS 1002, RBL 41, CORRODED. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20040604000452004060400045NM 2004 6 4 SWAA041554 120040602A53116546559 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 927, BBL 0, STRINGER 29L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040604000462004060400046NM 2004 6 4 SWAA041555 120040602A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 25R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040604000472004060400047NM 2004 6 4 SWAA041556 120040602A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 380 + 16, STRINGER 17L, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040604000532004060400053NM 2004 6 4 SWAA041562 120040602A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040604000562004060400056NM 2004 6 4 SWAA041512 120040529A5311963089 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SPV, FOUND CHORD AT RT BS 178 ABOVE AND BELOW FLOOR, CRACKED. REMOVED AND REPLACED CHORD AT RT BS 178 PER ACO. 2L72 4F RTA16WE 20040604000572004060400057NM 2004 6 4 SWAA041513 120040529A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R AND STINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040604000582004060400058NM 2004 6 4 SWAA041514 120040530A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 942.5, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040604000822004060400082NM 2004 6 4 USAA040056 120040225A5320 ATTACH ANGLE BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19645US 23897 FWD CABIN FLOOR UPPER ATTACH ANGLE, WEB STA 287-303, RBL 40, CRACKED. FABRICATED NEW ANGLE AND FILLER AND INSTALLED IAW SRM 51-10-02. 2L72 4F4 FRTA1NM E13NE 20040604000842004060400084EU 2004 6 4 USAA040165 120040428A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW 0936 FLOOR SUPPORT, 1.3 INCHES X .90 INCH X .021 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON - FR 16, Y-254. INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-11-14, FIG 201. 2L72 4F4 FRTA28NM E2GL 20040604000932004060400093NE 2004 6 4 MDR04046 120040315A6320643520017019 HOUSING SKRSKYS64 CH54B 8142610NE MAIN GEARBOX CRACKED A JYDRO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09158AC 253 A6167 64081 MAIN GEAR BOX (SN A6167) WAS INSTALLED ON AIRCRAFT AND REQUIRED REMOVAL DUE TO A POSSIBLE CRACK FOUND ON THE UPPER HOUSING ON THE RT SIDE. HOUSING APPEARED TO BE SEEPING OIL FROM SUSPECTED CRACK IN THE ARMPIT OF THE UPPER HOUSING. THE SUSPECT AREA WAS LOCALLY BLENDED. ETCHED AND FPI WAS ACCOMPLISHED. CRACK WAS FOUND IN THE RT ARMPIT AND APPEARED TO BE APPROX 2 INCHES LONG. PROBABLE CAUSE IS FATIGUE AT THE WELD IN THE CASTING. 2G72 4U H6EA 20040604001112004060400111EU 2004 6 4 A6WA200460015 120040512A5753 FLAP TRACK BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502* 41580EA T/E FLAP WORN A K NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES .033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REMOVED LOWER CARRIAGE NR 2 LEFT. ROLLERS REPLACED IAW CMM 57-50-22. CARRIAGE REINSTALLED IAW AMM 27-50-64. FUNCTION TESTED SERVICEABLE. BLACKLASH MEASURED AT 8 MM. OK TO REMAIN IN SERVICE AT THIS TIME. REF BAE FAX BARA/AVR/6741/04-MK. (M) 2H74 4F4 FRTA49EU E6NE 20040604001222004060400122WP 2004 6 4 GTIA040410 120040409A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND AFT PIT INTERCOSTAL ASSY STATION 1155, L28R TO L29R CORRODED. FABRICATED NEW INTERCOSTAL. (M) 2L72 4F RTA6WE 20040604001312004060400131WP 2004 6 4 GTIA040415 120040409A5310 STOP FITTING DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND AFT PIT DOOR STOP FITTINGS CORRODED AND RUSTY STATION 1193 FORWARD AND AFT. LOCATED AND DRILLED TWO NEW DOOR STOP FITTINGS. (M) 2L72 4F RTA6WE 20040604001342004060400134NM 2004 6 4 ASAA0410090 120040223A33508821004 BATTERY BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, FOUND PALLET 8-2 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040604001372004060400137NM 2004 6 4 ASAA0410187 120040410A33508821004 BATTERY PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 FOUND SMOKE BARRIER LIGHTS WEAK WHEN ACTIVATED. CHANGED OUT SMOKE BARRIER BATTERY PACK. TESTS OK. (M) 2L72 4F RTA16WE 20040604001382004060400138WP 2004 6 4 ASAA0480271 120040412A33970105606 WIRE DOUG DC9 DC983 3022083WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01976AS 53452 LAX - PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS 'BROKEN' INOPERATIVE AT ROW 3. RECONNECTED WIRE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040604001392004060400139NM 2004 6 4 ASAA0480270 120040407A33500105606 CONNECTOR DOUG MD80 MD83 3023681NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS 53471 DURING SEA LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE. RECONNECTED CONNECTOR AT ROW 3. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040604001402004060400140NM 2004 6 4 ASAA0440020 120040131A3397 WIRE BOEING737 7374Q8 138447QNM CABIN BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01791AS 28886 FOUND FLOOR TRACK LIGHT INOPERATIVE AT AFT LEFT BIFFY. REPAIRED BROKEN WIRE, TRACK LIGHT CHECKS GOOD. (M) 2L72 4F RTA16WE 20040604001412004060400141NM 2004 6 4 ASAA0440013 120040123A33508100022607 CONNECTOR BOEING737 7374Q8 138447QNM CABIN UNSECURE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 BUR - DURING MAINTENANCE, FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT ROW 20-23. RE-SECURED AND CONNECTED FLOOR TRACK WIRING. OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA16WE 20040604001422004060400142NM 2004 6 4 ASAA0410191 120040411A5320655056810 THRESHOLD BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND L2 DOOR THRESHOLD WEB IS CORRODED AND GOUGED. REMOVED DAMAGED WEB AND INSTALLED REPLACEMENT WEB IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040604001432004060400143NM 2004 6 4 ASAA0410190 120040411A534765549693 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND SEAT TRACK IS NICKED AND GOUGED AT STATION 600-616, LBL 25. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT FLOOR TRACK SECTION IAW SRM 53-10-5. (M) 2L72 4F A16WE 20040604001442004060400144WP 2004 6 4 GTIA040396 120040503A3350 SIGN DOUG DC9 DC983 3022083WP CABIN BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01809NK 49503 FLL - FOUND L-2 DOOR FORWARD EXIT SAFETY GLO SIGN BROKEN. INSTALLED NEW EXIT SAFETY GLO. (M) 2L72 4F RTA6WE 20040607000032004060700003WP 2004 6 7 04FDEA01606 120040603A2720AJH70891 PULLEY BRACKET DOUG DC10 DC1010 3022110WP RUDDER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RUDDER CABLE QUADRANT INSIDE ACCESS PNL 364BR UPPER AND LOWER ARMS GUIDE PIN HOLES ELONGATED AND PINS FALLING OUT/MISSING. REMOVED AND REPLACED PULLEY BRACKET AND PULLEY IAW MM 20-50-02-2, CHECKED TENSIONS IAW MM 27-20-00-5 AND MM 27-20-00-6 AT MAE. 2L73 4F A22WE 20040607000042004060700004WP 2004 6 7 04FDEA01607 120040603A3411ACP803047 STATIC PORT DOUG DC10 DC1010 3022110WP PITOT/STATIC SYSOUT OF TOLERANCEA FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RT PRIMARY STATIC PORT FAILED THE CONVEXITY AND CONCAVITY CHECK ALONG PLANE LINE-A. REMOVED AND REPLACED RT STATIC PORT PRIMARY IAW MM 34-11-02 AT MAE. 2L73 4F A22WE 20040607000052004060700005WP 2004 6 7 04FDEA01608 120040603A7110ASL00401 RUB STRIP DOUG DC10 DC1010 3022110WP NR 3 COWLING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 NR 3 ENG LT CORE COWL FWD RUB STRIP WORN. REMOVED AND REPLACED RUBSTRIP IAW SRM 51-31-01 AND SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000062004060700006WP 2004 6 7 04FDEA01609 120040603A5524FX55220117 STRUCTURE DOUG DC10 DC1010 3022110WP RT ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT ELEVATOR DROOP T/E OUTBOARD T/E CORNER IS CRACKED. REMOVED AND REPLACED T/E SECTION IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000092004060700009NM 2004 6 7 04FDEA01563 120040602A5340 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO COMPARTMENT STA 520 WL 150 RBL 21 STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 520, WL 150, RBL 21, STR 26R. REMOVED DAMAGE 1 X 5 INCH FROM EDGE OF CLIP. ALODINED AND PRIMED BARE METAL IAW SRM 51-30-2, 51-10-01, 51-10-2. 2L73 4F RTA3WE 20040607000112004060700011NM 2004 6 7 04FDEA01565 120040602A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01) FLOORBEAM UPPER FLANGE LWR SURFACE IS GOUGED AND CORROSION STA 400 LBL 2-8 WL 208. REPAIRED FLOORBEAM AT BS 400, LBL 2-8, WL 208 IAW SRM 53-10-8 FIG 3, 51-40-3, 51-10-3, FED EX MM 51-20-000-7, 51-20-021-7, SRM 51-30-2. ORIGINAL MATERIAL THICKNESS = .125 INCH. DEPTH OF DAMAGE = .080 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. 2L73 4F RTA3WE 20040607000122004060700012EU 2004 6 7 04FDEA01567 120040602A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE SEAT TRACK 5L 4 INCHES FWD OF FRAME 23 HAS CHIPPED SCALLOP. REMOVED DAMAGED SECTION OF TRACK, FABBED REPAIR SPLICE IAW SRM 53-10-16, AND INSTALLED SPLICE IAW SRM'S 51-10-08, 51-35-00, AND 51-40-21. 2L72 4F RTA35EU 20040607000132004060700013EU 2004 6 7 04FDEA01568 120040602A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE NR 2 RT TRACK BETWEEN FR 45 & 54, LEVEL 2 CORROSION IN TRACK, AND FR 47 & 48, 2EA AREAS, FR 46 & 47 2EA AREAS OF LEVEL 2 CORROSION, FR 48 & 49 2EA AREAS BROKEN RIVETS AND BARE METAL ALONG FLANGE. REMOVED DAMAGED TRACK, FABBED NEW TRACK AND INSTALLED IAW SRM'S 53-10-16, 51-25-00, AND 51-35-00 INCLUDING RIVETS. 2L72 4F RTA35EU 20040607000172004060700017WP 2004 6 7 04FDEA01572 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RETAINER BALL UNIT CRACKED STA 745-785. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000192004060700019WP 2004 6 7 04FDEA01574 120040602A5753ARC2541504 RUB STRIP DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT INBOARD FLAP OUTBOARD HINGE FITTING FWD FAIRING CHAFE STRIP IS DAMAGED. REMOVED AND REPLACED CHAFE STRIP IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040607000202004060700020WP 2004 6 7 04FDEA01575 120040602A5320ANB7203103 BRACKET DOUG DC10 DC1010 3022110WP RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT MLG W/W AFT O/B WEB VERT STIFFENER UPPER END BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040607000212004060700021WP 2004 6 7 04FDEA01576 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINER UNIT CRACKED STA 1501. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000222004060700022WP 2004 6 7 04FDEA01556 120040601A5320ANB7203 SUPPORT ANGLE DOUG DC10 DC1010 3022110WP RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT MLG W/W AFT WEB FWD BULB SEAL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED ANGLE SUPPORT AND WEB IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000232004060700023NM 2004 6 7 04FDEA01566 120040602A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 970 LBL 12 WL 200 LOWER FLOORBEAM CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED FLOORBEAM LOWER CHORD 1 X 4.25 INCHES. FABRICATED & INSTALLED REPAIR ANGLES (2 EA) & FILLER, AND RESTORED ALL ACCESS PER SRM 53-10-1, 53-10-8 FIG 8. 2L73 4F RTA3WE 20040607000262004060700026WP 2004 6 7 04FDEA01559 120040601A53474929147 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CARGO SEAT TRACK IS CORRODED AROUND FLOOR BOARD FASTENER HOLES STA 1219 RBL 74-86. REMOVED AND REPLACED SECTION OF SEAT TRACK AND SPLICES IAW SRM 53-20-00-01 AT MAE. 2L73 4F A22WE 20040607000272004060700027EU 2004 6 7 04FDEA01560 120040602A5270 WARNING SYSTEM AIRBUS310 A310203 3930313EU COCKPIT FAULTY A FDEAIA CABIN DEPRESSURIZATION UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25445FE 297 ON CLIMBOUT PASSING 6800 FT GOT LEFT FWD COMP DOOR UNLOCK LIGHT (AMBER INDICATION). RETURNED TO LAS. ON APPROACH AT 4000 FEET LIGHT TURNED GREEN (DE-PRESSURIZED AT THIS POINT). LWR FD DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOP. LWR FD DOOR VISUALLY CHECKED CLOSED & LOCKED. INSPECTED AT 0331 Z. 2L72 4F RTA35EU 20040607000282004060700028WP 2004 6 7 04FDEA01577 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RETAINER BALL UNIT CRACKED STA 615-675. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000302004060700030WP 2004 6 7 04FDEA01579 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RETAINER BALL UNIT CRACKED STA 635-695. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000312004060700031WP 2004 6 7 04FDEA01580 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINER UNIT CRACKED STA 615 TO 635 13 EA. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000322004060700032WP 2004 6 7 04FDEA01581 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RETAINER BALL UNIT IS CRACKED STA 610 TO 635. REMOVED AND REPLACED RETAINER STA 610 TO 635 IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000342004060700034WP 2004 6 7 04FDEA01583 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINER UNIT CRACKED STA 615 - 775. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000372004060700037WP 2004 6 7 04FDEA01588 120040602A25508156912 ROLLER TRAY DOUG DC10 DC1010 3022110WP CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 CONVEYOR ASSY ON BOTTOM SIDE CORRODED. REPLACED CONVEYOR IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000382004060700038NM 2004 6 7 04FDEA01589 120040602A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.426, MATERIAL REMOVED =0.002, REMAINING THICKNESS =0.424, WITHIN LIMIT AS PER DWG NR ARC0503. 2L73 4F RTA22WE 20040607000392004060700039NM 2004 6 7 04FDEA01590 120040602A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER =1.188, FINAL DIAMETER =1.217. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76721, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040607000402004060700040NM 2004 6 7 04FDEA01591 120040602A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER =1.188, FINAL DIAMETER =1.252. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76721, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP / OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040607000412004060700041WP 2004 6 7 04FDEA01585 120040602A5320ADA71211 FLOOR SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MCD FLOOR SUPPORT CORRODED AT FS 1300 LBL 80. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040607000432004060700043NM 2004 6 7 04FDEA01592 120040602A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS= 0.418, MATERIAL REMOVED= 0.002, REMAINING THICKNESS= 0.416. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040607000452004060700045NM 2004 6 7 04FDEA01446 120040525A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 STRINGER CLIP CRACKED STA 950B STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 950B, STR 7R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040607000472004060700047EU 2004 6 7 04FDEA01448 120040525A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 UPPER FUSELAGE STA 1870 FR 28 I/B SIDE OF TRACK 5R UNDER FLOOR PANEL 232VH LEVEL 1 CORROSION 1.2 L X 1.0 INCH W. DEPTH UNDERMINE WITHOUT BLENDOUT, ALSO FR 29 LIGHT SURFACE CORROSION 1 EA AREA, BETWEEN FR 30 & 31, 1 EA AREA LIGHT SURFACE CORROSION, FR 38 AND FR 38.2 HAVE 1 EA AREAS OF LIGHT SURFACE CORROSION. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 FIG 201 FR 26/27 TO FR 32/33, REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10 AT FR 38 TO 38.2 2L72 4F RTA35EU 20040607000482004060700048EU 2004 6 7 04FDEA01014 120040421A5320A5378198422000 BRACKET AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 TWO AREAS OF CORROSION ON SUBFLOOR AFT OF FRAME 28 BETWEEN SEAT TRACKS 3L AND 4L, MAIN CABIN. REMOVED AND REPLACED THRUST BRACKET IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040607000492004060700049WP 2004 6 7 04FDEA01278 120040516A5753ARC2512502 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 C/W EA8-5740-77406, RIGHT INBOARD FLAP, AFT HINGE ASSY ARC 2512, PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77406 RIGHT INBOARD FLAP, AFT HINGE ASSY, PIVOT BORE CORROSION CW PT1 ONLY. 2L73 4F A22WE 20040607000622004060700062NM 2004 6 7 04FDEA01020 120040422A5753ARC199113 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76019 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000652004060700065NM 2004 6 7 04FDEA01023 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000672004060700067NM 2004 6 7 04FDEA01025 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000702004060700070NM 2004 6 7 04FDEA01028 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000712004060700071NM 2004 6 7 04FDEA01030 120040422A5753ARC199114 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP OUTBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75937, WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040607000732004060700073EU 2004 6 7 04FDEA01516 120040528A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 5R FROM 8 INCHES FWD OF FR 45 TO FR 54 HAS 3 EA AREAS OF CORROSION, ONE AREA OUTBOARD FLANGE WITH GOUGES AT FR 47, AND 7 AREAS OF ELONGATED HOLES WITH GOUGES ON INBOARD FLANGE BETWEEN FR 48 TO FR 51. REMOVED CORROSION AND GOUGES IAW A300-600 SRM 51-74-10, MAT'L LOSS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM FRAME 44/45 TO FRAME 51 IAW SRM 53-10-16. 2L72 4F RTA35EU 20040607000752004060700075WP 2004 6 7 04FDEA01518 120040528A5753ARB37992 HINGE BRACKET DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 C/W 8-5710-77408, WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR, P/N ARB3799-2. COMPLIED WITH EA 8-5710-77408 WINGS - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET MOUNT HOLE REPAIR P/N 3799-2 AT MAE. 2L73 4F A22WE 20040607000762004060700076WP 2004 6 7 04FDEA01519 120040528A5720ARB21761 CLIP DOUG DC10 DC1010 3022110WP LT FUEL TANK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 TWO CLIPS CRACKED INSIDE FUEL TANK PLATE 534AT. REMOVED AND REPLACED CLIPS IAW SRM 51-33-01 AT MAE. 2L73 4F A22WE 20040607000772004060700077WP 2004 6 7 04FDEA01520 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 536CB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000782004060700078WP 2004 6 7 04FDEA01521 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 538BB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000792004060700079WP 2004 6 7 04FDEA01522 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 537AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000822004060700082WP 2004 6 7 04FDEA01525 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL. REMOVED AND REPLACED IAW SRM 51-31-01AT MAE. 2L73 4F A22WE 20040607000832004060700083WP 2004 6 7 04FDEA01526 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 638BB. REMOVED AND REPLACED IAW SRM 51-42-01 AT MAE. 2L73 4F A22WE 20040607000842004060700084WP 2004 6 7 04FDEA01527 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP RT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 638AB. REMOVED AND REPLACED IAW SRM 51-42-01 AT MAE. 2L73 4F A22WE 20040607000852004060700085WP 2004 6 7 04FDEA01528 120040528A5720ARB21762 CLIP DOUG DC10 DC1010 3022110WP RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 TWO CLIPS CRACKED INSIDE NR 3 FUEL TANK PLATE 634AT. REMOVED AND REPLACED CLIPS IAW SRM 51-33-01 AT MAE. 2L73 4F A22WE 20040607000862004060700086WP 2004 6 7 04FDEA01529 120040528A78309019M14L06 GUIDE DOUG DC10 DC1010 3022110WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 NR 2 ENGINE RIGHT REVERSER LWR FWD T-TRACK GUIDE CRACKED LWR ATTACHMENT. REMOVED AND REPLACED BRACKET IAW SRM 51-35-01. 2L73 4F A22WE 20040607000872004060700087WP 2004 6 7 04FDEA01539 120040529A5712ARB1868 RIB DOUG DC10 DC1010 3022110WP RT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5710-77424 WINGS - REWORK OF RIGHT NR 7 SLAT TRACK OUTBOARD RIB ARB1868. COMPLIED WITH EA 8-5710-77434. 2L73 4F A22WE 20040607000882004060700088WP 2004 6 7 04FDEA01540 120040529A5753NRC6053501 STOP FITTING DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-77430 WINGS - OUTBOARD FLAP INBOARD UP-STOP FITTING CORROSION REWORK, LEFT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-77430. 2L73 4F A22WE 20040602000852004060200085NM 2004 6 2 04FDEA01369 120040520A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING O/B FLAP O/B HINGE (WING SIDE), FWD ATTACHMENT FORK, I/B HOLE SPOTFACE CORRODED. RT WING O/B FLAP O/B HINGE (WING SIDE), FWD ATTACHMENT FORK, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.385, MATERIAL REMOVED: 0.014. REMAINING THICKNES OF LUG: 0.371 EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76675. OUTBOARD TRAILING EDGE FLAPS OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS, REPAIR. 2L73 4F RTA22WE 20040602000872004060200087NM 2004 6 2 04FDEA01371 120040520A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LIMIT. REPAIRED AS PER EA 1-5750-76676. LT OUTBOARD TRAILING EDGE FLAPS - OUTBOARD HINGE BRACKET (WING SIDE) ACTUATOR ATTACHMENT LUGS AND TENSION STRAP INTERFACE - REPAIR. 2L73 4F RTA22WE 20040602000892004060200089NM 2004 6 2 04FDEA01387 120040521A5712 RIB BOEING727 727200 138407ENM WING DAMAGED A FDEAO OTHER K FLUID LOSS ININSP/MAINT 1 SO25241FE 20979 COMPLY WITH EA 7-5720-77412 WING - SPOILER DOWN STOP RIB REPAIR. COMPLIED WITH EA 7-5720-77412. WORKED IN CONJUNCTION WITH EA 7-5720-77423. 2L73 4F RTA3WE 20040602001042004060200104NM 2004 6 2 ASAA0410162 120040327A5313 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION ON STRINGER 27R FLANGE AT STATION 351 E/E DOOR CUTOUT. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001122004060200112NM 2004 6 2 ASAA0410169 120040327A53156554910502 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND CORROSION AFT CARGO PIT STATION 887 LOWER FLOORBEAM AT CLIP NUTS. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001152004060200115NM 2004 6 2 ASAA0410171 120040327A531565549011 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND AFT PIT AT STATION 947 FLOORBEAM CORRODED AT BOTTOM T-CHORD. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001182004060200118NM 2004 6 2 ASAA0410103 120040306A33508821004 BATTERY BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 6-10 EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040602001212004060200121NM 2004 6 2 ASAA0410176 120040327A57536571940 SKIN BOEING737 737290C 138448VNM LT MID FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT INBOARD MID FLAP UPPER SURFACE IS CHAFFED AT WING STATION 108 TO 123. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001262004060200126NM 2004 6 2 ASAA0410182 120040327A575365575091020 SKIN BOEING737 737290C 138448VNM LT MID FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND LEFT OUTBOARD MID FLAP LOWER SKIN IS CHAFED IMMEDIATE INBOARD OF INBOARD PUSH ROD. REPAIR IAW EA. (M) 2L72 4F A16WE 20040602001282004060200128NM 2004 6 2 ASAA0410207 120040424A3350 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING MAINTENANCE CHECK, FOUND FLOOR PROX EMERGENCY LIGHTS, PALLET 9-3, OUT. CHANGED OUT BATTERY PACK, OPS CHECK OK. (M) 2L72 4F A16WE 20040603000062004060300006WP 2004 6 3 04FDEA01208 120040510A2120ACM70191 DUCT DOUG DC10 DC1010 3022110WP A/C BAY BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-2150-77351 AIR/CONDITIONING NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019. REMOVED NR 3 AC PACK EXHAUST DUCT IAW MM 20-50-02-2 AND 21-62-09-2 EA 8-2150-77351. COMPLIED WITH ON MAE TRAVLER T4/428578. INSTALLED NR 3 AC PACK EXHAUST DUCT IAW MM 20-50-02-2 AND 21-62-09-2. 2L73 4F A22WE 20040603000072004060300007NM 2004 6 3 04FDEA01209 120040510A5754 BRACKET DOUG MD11 MD11 3023602NM L/E SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING LEADING EDGE NR 16 SLAT TRACK ASSY INBOARD BRACKET WEB CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II AND BUSHING REPAIR CARRIED OUT AS PER EA 1-5710-76771 - WINGS - LEADING EDGE SLAT SUPPORT NR 16 (LT) - BUSHING REPAIR. 2L73 4F RTA22WE 20040603000112004060300011NM 2004 6 3 04FDEA01212 120040510A5744ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2 AND CMM 57-44-09. ORIGINAL THICKNESS =0.446 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.444 INCH. 2L73 4F RTA22WE 20040603000142004060300014EU 2004 6 3 04FDEA01215 120040511A5534 ATTACH BRACKET AIRBUS310 A310203 3930313EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE 248 RIGHT SIDE OF VERTICAL STAB FROM RIB 22 TO 26 OF REAR SPAR HAS SEVERAL AREAS OF CORROSION ON FLANGES (PANEL ATTACH BRACKET). REMOVED CORROSION AT RT SIDE OF VERTICAL STAB REAR SPAR AREA, 3 AREAS NEEDED REWORK. FABRICATED & INSTALLED REPAIRS IAW EA 6-5530-77658A. 2L72 4F RTA35EU 20040603000212004060300021WP 2004 6 3 04FDEA01337 120040519A25508064010 ROLLER TRAY DOUG DC10 DC1010 3022110WP MAIN CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 MAIN DECK 2C BALL MAT HAS SEVERAL MISSING RETAINERS AND BALLS. REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040603000262004060300026EU 2004 6 3 04FDEA01341 120040519A7830 WARNING SYSTEM AIRBUS310 A310203 3930313EU COCKPIT ACTIVATED A FDEAK NONE J WARNING INDICATION APAPPROACH 1 SO25409FE 273 ENGINE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED IN FLT, IT DID NOT FEEL AS IF THE REVERSER WAS DEPLOYED. COMPLIED WITH ECAM/PROCEDURES AND LANDED AT TUL. LIGHT WENT OUT AFTER ENGINE SHUTDOWN ON THE GROUND. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-B CATEGORY: C EXPIRATION: 29MAY04 MEL 78-30-01-B: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. 2L72 4F RTA35EU 20040603000312004060300031NM 2004 6 3 04FDEA01345 120040519A5313655612910 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION ON STRINGER 27R BS 955. REMOVED AND REPLACED STR 27 RT IN ACCORDANCE WITH FED EX E.A #7-5310-55318. 2L73 4F RTA3WE 20040603000372004060300037WP 2004 6 3 04FDEA01220 120040511A5753ARC2166505 SPINDLE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT O/B FLAP I/B ROLLER SPINDLE WORN AND HAS CORROSION. REMOVED AND REPLACED SPINDLE IAW W/C E 8-5750-7-5000 AT MAE. 2L73 4F A22WE 20040603000432004060300043WP 2004 6 3 04FDEA01226 120040512A5753ARC14711 FLAP TRACK DOUG DC10 DC1010 3022110WP NR 2 FLAP VANE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RIGHT O/B FLAP NR 2 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE. 2L73 4F A22WE 20040603000562004060300056WP 2004 6 3 04FDEA01413 120040522A5753NRC6053501 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 WINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE. COMPLIED WITH EA 8-5750-77415, WINGS - OUTBOARD FLAP, REWORK OF POSITION INDICATOR HOLE IN ARC1984 HINGE. 2L73 4F A22WE 20040603000642004060300064NM 2004 6 3 04FDEA01284 120040518A5713 STRINGER DOUG MD11 MD11 3023602NM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING NR 1 FUEL TANK - XORS 717 - ACCESS PANEL 536AB. SUSPECT CRACK ON NR 11 STRINGER. SLOTTED OUT CRACK AS PER SRM 51-31-01 VOL II AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II, & EA 1-5710-76680. UPPER WING STRINGERS 10 & 11 LT - CRACK REPAIR. 2L73 4F RTA22WE 20040603000932004060300093NM 2004 6 3 AWXA200400580 120040530A3350900835A BATTERY BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 LAS - EEL - DURING 4-DAY CHECK THE L-1 AND R-1 DOOR EMERGENCY SLIDE LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2EA 20040603000952004060300095NM 2004 6 3 AWXA200400582 120040531A3397BMS13311122 WIRE HARNESS BOEING737 7373Y0 1384671NM GE CFM56 CFM56* 13802NE CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28323AW 23684 DURING THRU-FLIGHT INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT WIRE HARNESS AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040603000962004060300096NM 2004 6 3 AWXA200400583 120040528A3260893301 PROXIMITY SENSOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE LT MLG FAULTY A AWXAO OTHER N FALSE WARNING APAPPROACH 1 WP28802AW 924 EMERGENCY LANDING - FLT 0280 - ON APPROACH, EN ROUTE WITH LANDING GEAR SELECTED DOWN GEAR DID NOT EXTEND, MANUALLY SELECTED GEAR DOWN AND DECLARED EMERGENCY. MAINTENANCE PERFORMED WIRING CHECK AND FOUND RESISTANCE ON LT MAIN LANDING GEAR (MLG) DOOR OPEN PROXIMITY SENSOR HIGH, REMOVED AND REPLACED LT MLG DOOR PROXIMITY SENSOR IAW AMM 32-31-73, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20040603000972004060300097NM 2004 6 3 AWXA200400584 120040529A2133VFT300A1 OUTFLOW VALVE AIRBUSA319 A319132 3930340NM CABIN PRESSURE FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28803AW440341610 931 AIR TURN BACK - FLT 0051 - ON CLIMB OUT OF LAS EN ROUTE, RECEIVED AVIONICS VENT SYSTEM FAULT, AIRCRAFT PRESSURIZED NORMALLY, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE ISSUED MEL 21-26-04 COND 1, "SKIN AIR OUTLET VALVE INOP". ON 05/31/2004 IN BOS: MAINTENANCE REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM TASK 21-26-53-000-001, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF SKIN AIR OUTLET VALVE S/N 47 WAS NO FAULT FOUND. REMOVED ACTUATOR (S/N 188) AND TESTED ON ACTUATOR BENCH, NO FAULTS FOUND, REINSTALLED ACTUATOR. RETESTED UNIT AND RETURNED TO SERVICE IAW CMM 21-26-53, REV. 6. 2L72 4F RTA28NM 20040603000992004060300099NM 2004 6 3 QXEA200400378 120040529A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN BROKEN A QXEAK NONE O OTHER UKUNKNOWN 1 NM09375PH 529 ON FLIGHT 2112- NR 2 EMERGENCY FLOOR TRACK LIGHTING IS BROKEN. REMOVED AND REPLACED TRACK LIGHTING ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040603001012004060300101SO 2004 6 3 C2XA04SH338 120040601A532014521721005 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C CHECK THE CENTER BUTTSTRAP AT FRAME 14 WAS FOUND TO BE CORRODED AROUND THE NUTPLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01118. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040603001032004060300103SO 2004 6 3 C2XA04SH340 120040601A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040603001102004060300110SO 2004 6 3 LR7A04060 120040526A5343 CAP LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL RT MLG CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW JOB CARD HB3202 FOUND RT FS 517 MLG BEAM CRACKED AT RBL 66, WL 160. REPLACED OUTER BEAM CAP IAW DWG 388392. NR 02/REP/51/2. 2H74 4T4 T A1SO E282 20040603001112004060300111NM 2004 6 3 ASAA0410204 120040424A526065596586 TORQUE BOX BOEING737 737290C 138448VNM AIR STAIRS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND AIRSTAIR TORQUE BOX, BTM SIDE AT STATION 980-986, LBL 50 IS CORRODED. REMOVED DAMAGED WEBS AND INSTALLED REPLACEMENT WEBS IAW BOEING DWG 65-59658. (M) 2L72 4F A16WE 20040603001132004060300113WP 2004 6 3 ASAA0480304 120040422A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PEELING A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SURFACE IS PEELING AT SEVERAL LOCATIONS BETWEEN FS 826-864. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040603001152004060300115WP 2004 6 3 ASAA0480306 120040422A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND FLOOR PANEL IS DELAMINATED AT SEVERAL LOCATIONS FROM FS 927-1003. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040603001172004060300117WP 2004 6 3 ASAA0480290 120040420A53119912246503 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FRAME CORRODED ON UPPER SURFACE AT FS 1338. REPLACED DAMAGED SECTION AND INSTALLED REPAIR ANGLE PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040603001282004060300128WP 2004 6 3 ASAA0480345 120040421A57205930503501 RUB STRIP DOUG DC9 DC983 3022083WP WING PANEL DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND WING PANEL 1361C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M) 2L72 4F RTA6WE 20040603001292004060300129WP 2004 6 3 ASAAO480180 120040310A534759305661 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING HV CHECK, FOUND SEAT TRACK CHAFED AT FS 1212. REPLACED DAMAGED SECTION OF TRACK PER SRM 53-05. (M) 2L72 4F RTA6WE 20040603001322004060300132WP 2004 6 3 04FDEA01269 120040514A5330AYB70223 DOUBLER DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 RADIO ALTIMETER NR 1 & 2 AFT FUSELAGE STRUCTURE CORRODED. REMOVED AND REPLACED LT AND RT RADIO ALT DOUBLERS IAW SRM 51-31-01 AND SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040604000122004060400012NM 2004 6 4 04FDEA01442 120040525A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO STA 680 FRAME DENTED AT STR 24 RT. CUT OUT DAMAGE ON FRAME INNER CHORD BS 680, STR 24 RT. DRILLED UP REPAIR DOUBLER AND INSTALLED PER SRM 51-40-3 FIG 1 AND FED EX EA 7-5310-70665. 2L73 4F RTA3WE 20040604000172004060400017NM 2004 6 4 SWAA041536 120040601A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SPV CHECK, FOUND FUSELAGE SKIN AT BS 790 TO BS 796, STRINGER 19L, CRACKED. REMOVED AND REPLACED SKIN SECTION PER SRM. 2L72 4F RTA16WE 20040604000282004060400028NM 2004 6 4 SWAA041532 120040601A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 PHOTO LUMINESCENT STRIP LOOSE AT RT ROW 7 AND RT ROW 8. SECURED STRIP PER MM. 2L72 4F RTA16WE 20040604000372004060400037WP 2004 6 4 04FDEA01273 120040515A2421 GENERATOR DOUG DC10 DC1030 3023501WP NR 2 & NR 3 CONTAMINATED A FDEAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO25318FE 46837 AT ROTATION (MAIN WHEEL LIFTOFF), CAPTAIN LOST ALL INSTRUMENTS. THE FOLLOWING LIGHTS ILLUMINATED ON S/O PANEL: GEN 1 OFF, L EMER AC BUS OFF, AC BUS 1 OFF, AC BUS TIE 1 ISOL, L EMER DC BUS OFF, DC BUS 1 OFF. SEVERAL WARNING HORNS GOING OFF THAT COULD NOT BE SILENCED. ON T/O ROLL, ALL ENGINES WERE PRODUCING THRUST, BUT IT TOOK ENGINE NR 1 N2 GAUGE UNTIL 100 KNOTS TO SHOW A PROPER INDICATION, IT WAS CYCLING PRYOR TO THAT. WHILE FLYING BACK TO KIND, GEN NR 1 KEPT COMING ON LINE DROPING OFF. EVENTUALLY IT FIXED ITSELF JUST PRIOR TO LANDING, EVEN PARALLELED THE GENS. HEAVY RAIN CAME THROUGH WHILE A/C SAT ON RAMP. DRIED VISIBLE WATER, FACT 1, NR 2, NR 3 ENG AC GENERATOR ADJ/TEST GOOD PER MM. 2L73 4F A22WE 20040604000552004060400055NM 2004 6 4 SWAA041511 120040529A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 757, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040604000642004060400064NM 2004 6 4 SWAA041520 120040531A532065C360751 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX FITTING, CRACKED. REPAIRED HINGE BOX FITTING PER EA. 2L72 4F RTA16WE 20040604000692004060400069NM 2004 6 4 SWAA041525 120040531A335020131A BATTERY PACK BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED PM CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED FWD BATTERY PACK PER MM. 2L72 4F RTA16WE 20040604000702004060400070NM 2004 6 4 SWAA041526 120040531A33506104789 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29458WN 33857 DURING SCHEDULED PM CHECK, FOUND RT OVERWING EXTERIOR ESCAPE LIGHT INOP. REMOVED AND REPLACED ESCAPE LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040604000802004060400080EA 2004 6 4 WVE2004F00018 120040510A5320601R3117117 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09597SW 7293 FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484, LBL 27 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314) 2L72 4F RTA21EA 20040604000812004060400081EU 2004 6 4 USAA040164 120040428A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOOR SUPPORT, 1.8 INCH X .70 INCH X .037 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON-FR 20, Y-254. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-14, FIG 204. 2L72 4F4 FRTA28NM E2GL 20040604000882004060400088NM 2004 6 4 USAA040060 120040228A5315 FLOORBEAM BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19645US 23897 TOP OF FLOORBEAM, STA 287, RBL 26, RBL53 CORROSION (3 AREAS). INSTALLED CAP IN FLOORBEAM IAW SRM 53-00-51, FIG 201. 2L72 4F4 FRTA1NM E13NE 20040604000892004060400089EU 2004 6 4 USAA040169 120040425A5320D5347217220390 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOOR SUPPORT, 1.5 INCH L X 1 INCH W X .030 INCHES D AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 TWO AREAS FLOOR SUPPORT, FR 64-68 AT Y1244.6, Z240. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E2GL 20040604000952004060400095CE 2004 6 4 GUU2004F00006 120040509A55201016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO171654017470 UE172 AT SCHEDULED ROUTINE MAINTENANCE, TR OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040604001022004060400102EU 2004 6 4 USAA040172 120040428A5321D5367161300000 FLOOR PANEL AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW 0936 FLOOR PANEL, 6 INCHES X .2500 INCH W, DELAMINATION, FLOOR PANEL NR 241 AF, FR 34 AND 35 AT Y24, Z240. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. 2L72 4F4 FRTA28NM E2GL 20040604001062004060400106EU 2004 6 4 USAA040176 120040429A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOOR SUPPORT, .8 INCH X .6 INCH X .030 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-74-00, 53-11-14, 51-21-11, 51-75-12. 2L72 4F4 FRTA28NM E2GL 20040604001072004060400107EU 2004 6 4 USAA040178 120040429A5347D5311281520200 SEAT TRACK AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 SEAT TRACK, 1.5 INCH X 1.3 INCH X .032 INCH DEEP. CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y765, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11. 2L72 4F4 FRTA28NM E2GL 20040604001122004060400112WP 2004 6 4 GTIA040399 120040329A5753 SKIN DOUG DC9 DC983 3022083WP LT FLAP VANE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND LEFT NR 3 OUTBOARD FLAP INBOARD VANE METAL GOUGED. REMOVED COVER SKIN. LOCATED AND DRILLED HOLES AT NEW COVER SKIN. INSTALLED NEW SKIN. (M) 2L72 4F RTA6WE 20040604001192004060400119WP 2004 6 4 GTIA040406 120040401A5753 VANE DOUG DC9 DC983 3022083WP T/E FLAP DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND RIGHT NR 4 OUTBOARD FLAP VANE FULL OF WATER AND ATTACHING HARDWARE IS CORRODED. UPON FURTHER INSPECTION FOUND DELAMINATED AT LEADING EDGE. REPAIRED DELAMINATION. (M) 2L72 4F RTA6WE 20040604001302004060400130NM 2004 6 4 ASAA0440040 120040219A33508100022601 LIGHT BOEING737 7374Q8 138447QNM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 SEA - FOUND FIRST TWO ROWS OF EMERGENCY LIGHTS INOPERATIVE. RELAMPED AND SECURED LOOSE WIRES AND INSTALLED MISSING COVER AT SEAT ROW 1AC. (M) 2L72 4F RTA16WE 20040604001322004060400132WP 2004 6 4 GTIA040416 120040418A2560 LANYARD DOUG DC9 DC983 3022083WP EVAC SLIDE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND R1 DOOR SLIDE HAS BROKEN LANYARD. REMOVED BROKEN LANYARD. INSTALLED NEW LANYARD. (M) 2L72 4F RTA6WE 20040604001332004060400133NM 2004 6 4 ASAA0410091 120040227A33508821004 BATTERY BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 9-5 EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. (M) 2L72 4F A16WE 20040607000072004060700007WP 2004 6 7 04FDEA01611 120040603A7110ATL0052501 RUB STRIP DOUG DC10 DC1010 3022110WP NR 2 COWLING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 NR 2 ENG RIGHT FAN COWL AFT EDGE RUB SEAL WORN. REMOVED AND REPLACED RUB SEAL STRIP IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040607000102004060700010NM 2004 6 7 04FDEA01564 120040602A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01, 3) FLOORBEAM STA 1130 LWR CHORD FWD FLANGE UPPER SURFACES CORRODED LBL 1-45 WL 200 AROUND NUT PLATE. REMOVED CORROSION ON 1130 FLOORBEAM, LOWER CHORD, FWD FLANGE UPPER AND LOWER SURFACES LBL 1 - LBL 45, WL 200 AROUND FASTENER HOLES. ORIGINAL THICKNESS .163 INCH. REMAINING THICKNESS AFTER CORROSION REMOVAL FOUND TO BE .116 INCH AT LBL 16.5, .103 INCH AT LBL 19.5 AND .138 INCH AT LBL 34.5. FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1. REPLACED LOWER CHORD OF BS 1130 FLOORBEAM IAW EA 7-5310-55302. 2L73 4F RTA3WE 20040607000162004060700016WP 2004 6 7 04FDEA01571 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINERS UNIT IS CRACKED 2EA STA 1600 TO 1681. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000182004060700018WP 2004 6 7 04FDEA01573 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINER UNIT IS CRACKED STA 615 - 775. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33. 2L73 4F A22WE 20040607000242004060700024WP 2004 6 7 04FDEA01557 120040601A5753ARC2499509 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT I/B FLAP TRACK MOUNT HOLES CORRODED. REMOVED AND REPLACED FLAP TRACK IAW CMM 57-52-01 AT MAE. 2L73 4F A22WE 20040607000292004060700029WP 2004 6 7 04FDEA01578 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINING UNIT CRACKED STA 615 TO 775. REMOVED AND REPLACED RETAINER IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000462004060700046NM 2004 6 7 04FDEA01447 120040525A7312 CONNECTOR BOEING727 727200 138407ENM PWA JT8 JT8D1 52044NE FUEL HEAT VALVE DISCONNECTED A FDEAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION DEDESCENT 1 SO25281FE 22348 689890 DURING DESCENT AT FL 280 NR 2 ENGINE OIL TEMP INCREASED TO 135, FOLLOWED QRH PROCEDURES FOR HIGH OIL TEMP, OIL TEMP REMAINED IN YELLOW BAND. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AFTER 15 MINUTES WITH OIL TEMP STILL IN YELLOW BAND. NR 2 ENGINE WAS SHUTDOWN FOR APPROX 20 MINUTES. AFTER SHUTDOWN OIL TEMP INCREASED TO 165. DURING TROUBLESHOOTING FOUND FUEL HEAT VALVE HAD CONNECTOR REMOVED AND TIED BACK AND VALVE WAS IN OPEN POSITION. RECONNECTED CONNECTOR AND SAFETIED. REMOVED AND REPLACED MAIN ENGINE OIL FILTER IN (NOTE: NO BURNT OIL SMELL OR PARTICLES IN OIL FILTER), PER JRH 6-67. DRAINED OIL, RESERVICED WITH FRESH OIL. THE ANIT-ICE VLV WAS DEFERRED INOP AT THE PREVIOUS STN. 2L73 4F4 FRTA3WE E2EA 20040607000502004060700050NM 2004 6 7 04FDEA01279 120040517A5514ALC8100 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 TAIL TANK - NR 28L BARREL NUT BORE CORROSION REMOVAL EXCEEDED LIMIT. COMPLIED AS PER FEDEX EA 1-5510-76711 - STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE REWORK / REPAIR - AD 2003-22-08. 2L73 4F RTA22WE 20040607000512004060700051NM 2004 6 7 04FDEA01280 120040517A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 CTR CARGO COMPT BILGE AREA SPLICE FITTING AT LONGERON 44 LEFT STA 1541. SUSPECT CRACK ORIGINATING FROM THE RIVET AREAS. CRACK SPLICE FITTING REMOVED AT CENTER CARGO COMPARTMENT BILGE AREA SPLICE FITTING AT LONGERON 44 LT STA 1541 AS PER SRM 51-33-01 VOL II AND FABRICATED NEW SPLICE FITTING AS PER DWG A5A7116 AND NEW SPLICE FITTING INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040607000582004060700058EU 2004 6 7 04FDEA01618 120040604A5320 FLOOR SUPPORT AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 AT FRAME 51 BETWEEN SEAT TRACKS 1 AND 2L FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-00, FABRICATED NEW PART IAW DWG A53812989, INSTALLED FABBED PART IAW SRM 53-40-21. 2L72 4F RTA35EU 20040607000602004060700060NM 2004 6 7 04FDEA01281 120040517A5753ARC4125501 STOP FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. LEFT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2. 2L73 4F RTA22WE 20040607000682004060700068NM 2004 6 7 04FDEA01026 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000692004060700069NM 2004 6 7 04FDEA01027 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000802004060700080WP 2004 6 7 04FDEA01523 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED FOR PANEL 538AB. REMOVED AND REPLACED RUB STRIP IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000892004060700089EU 2004 6 7 04FDEA01541 120040531A760332827562 CABLE AIRBUS310 A310222 3930315EU PWA JT9 JT9D* NE NR 2 THROTTLE OUT OF RIG A FDEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO25453FE2932 1132 267 715406 ON TAKEOFF NR 2 THROTTLE WOULD NOT GO PAST V2WAY, DUE TO BINDING. ABORTED BELOW 70 KTS. RETURNED TO GATE. THROTTLE LEVER FEEDBACK CABLE MECHANISM FOUND OUT OF RIGGING RANGE. T/L FEEDBACK MECHANISM RIGGED IAW MM 78-31-38-2. 2L72 4F4 FRTA35EU E20EA 20040607000902004060700090EU 2004 6 7 04FDEA01542 120040601A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 4R HAS 1 EA AREA ON AND UNDER SCALLOP WITH CORROSION 10 INCHES AFT OF FR 74. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MAT'L LOSS OUT OF LIMITS. REMOVED DAMAGED SECTION SEAT TRACK, LOCATED DRILLED, AND INSTALLED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16 P205/206. 2L72 4F RTA35EU 20040607000912004060700091EU 2004 6 7 04FDEA01543 120040601A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 1 (CENTER TRACK) HAS 6 EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS. 1) 10 INCHES AFT OF FR 71 AT PRODUCTION BREAK. 2) BETWEEN FR 73 & FR 74. 3) BETWEEN FR 75 & FR76. 4 & 5) BETWEEN FR 75 & 76. 6) 2 INCHES AFT OF FR 78. REMOVED DISCREPANT SEAT TRACK AREA, FABRICATED AND INSTALLED REPAIR SEAT TRACK IAW A300-600 SRM 53-10-16, 51-21-10, AND 51-40-21. 2L72 4F RTA35EU 20040607000922004060700092EU 2004 6 7 04FDEA01544 120040601A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MAIN DECK CARGO COMP BETWEEN FR 45 AND FR 54, L4 SEAT TRACK HAS 6 AREAS OF CORROSION. 1) 6 INCHES AFT OF FR 45. 2) 12 INCHES AFT OF FR47. 3) 5 INCHES FWD OF FR49. 4) 2 INCHES FWD OF FR50. 5) 7 INCHES FWD OF FR 53. 6) 12 INCHES AFT OF FR53. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MEASURED MAT'L LOSS AND CHECKED LIMITS AS PER SRM 53-10-16. AREAS 1-5 WITHIN LIMITS, AREA 6 OUT OF LIMITS. REPAIRED SEAT TRACK AS PER A300-600 SRM 53-10-16 FIG 205. 2L72 4F RTA35EU 20040607000932004060700093EU 2004 6 7 04FDEA01545 120040601A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 BETWEEN FR 28 AND FR 29 AT TRACK 2L THERE IS AREAS OF CORROSION (MAIN CARGO) AND FROM FR 30 TO FR 38, 12 EA AREA OF CORROSION. REMOVED CORROSION IAW A300-600 SRM 51-74-10, MEASURED MAT'L LOSS, CHECKED MAT'L LIMITS PER SRM 53-10-16 FIG 102, REPAIRED SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16 FIR 201. 2L72 4F RTA35EU 20040607000942004060700094WP 2004 6 7 04FDEA01546 120040601A5720ARC0744 CLIP DOUG DC10 DC1010 3022110WP RT WING BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT OUTBOARD FLAP, INBOARD WING MOUNTED HINGE, FWD OUTBOARD FAIRING SUPPORT STR CLIP BROKEN. REMOVED AND REPLACED CLIP RIGHT OUTBOARD INBOARD HINGE FWD OUTBOARD FAIRING SUPPORT IAW SRM 51-31-01, 51-25-01, DPS 3.69 REV E DWG ARC0744 2020T- 3 .071. 2L73 4F A22WE 20040607000962004060700096NM 2004 6 7 04FDEA01079 120040423A5753ARC0512503 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76022, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040607000972004060700097NM 2004 6 7 04FDEA01080 120040424A5753ARC050214 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, BARREL NUT HOLE NR 2B MATING SURFACE CORRODED. RIGHT WING OUTBOARD FLAP INBOARD FWD HINGE BARREL NUT HOLE NR 2B MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN LIMITS AS PER DWG ARC0502. 2L73 4F RTA22WE 20040607000982004060700098NM 2004 6 7 04FDEA01082 120040424A5753ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE NR 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76029, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040607001002004060700100WP 2004 6 7 04FDEA01547 120040601A5720ARC074812 RETAINER DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT O/B FLAP O/B WING MOUNTED HINGE, AFT I/B BULB SEAL RETAINER ARE DAMAGED ON BULLET FAIRING. FAB NEW RETAINER ON MAE TRAVLER T4/433934. INSTALLED NEW RETAINER AND SEAL IAW SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040607001012004060700101WP 2004 6 7 04FDEA01548 120040601A5720ARC074812 RETAINER DOUG DC10 DC1010 3022110WP RT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT O/B FLAP, O/B WING MOUNTED HINGE, AFT O/B BULB SEAL RETAINER ON BULLET FAIRING ARE WORN. FAB NEW RETAINER ON MAE TRAVLER T4/434038, INSTALLED NEW RETAINER AND SEAL IAW SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040607001042004060700104EU 2004 6 7 04FDEA01551 120040601A5315 FLOORBEAM AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 FWD CARGO OVERHEAD FLOORBEAM AT FR 27, 27 INCHES RIGHT OF CENTERLINE ON THE FWD SIDE IS CRACKED ON UPPER VERTICAL LEG. REWORKED CRACK AT FR 27 IAW A300-600 SRM 51-27-00, NDT VERIFIED CRACK, REMOVED CRACK IN WEB IAW 53-10-15 P207. NDT VERIFIED NO CRACK FOUND. FABRICATED REPAIR PARTS IAW 53-10-15, SHOT PEEN REPAIR PARTS IAW PMS 01-01-13. LOCATED AND DRILLED PARTS IAW SRM 53-10-15, TREATED, PRIMED AND TOP COATED PARTS IAW SRM 51-35-00. INSTALLED REPAIR PARTS IAW SRM 53-10-15 FIG 207. 2L72 4F RTA35EU 20040607001052004060700105WP 2004 6 7 04FDEA01552 120040601A5753ANB70822 FITTING DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK. COMPLIED WITH EA 8-5750-78218 WINGS - RIGHT INBOARD FLAP, ROLLER FITTING REWORK AT MAE. 2L73 4F A22WE 20040607001112004060700111NM 2004 6 7 04FDEA01072 120040423A5753ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76021, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040607001122004060700112NM 2004 6 7 04FDEA01077 120040423A5753ARC2512504 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76023, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040607001142004060700114NM 2004 6 7 04FDEA01086 120040424A5313NFA631325 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 CENTER CARGO - STA 1811 LT LONGERON 40 FOUND CRACKED. CENTER CARGO - STA 1811 LT LONGERON 40 REPAIRED AS PER SRM 53-10-00 VOL I FIG 2. 2L73 4F RTA22WE 20040607001152004060700115NM 2004 6 7 04FDEA01148 120040504A5311AFA0022 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 TRANSVERSE FRAME DENTED, LT SIDE STA Y= 1561, ALONG LONGERON 12L. DENTED AREA AT TRANSVERSE FRAME LT, STA Y= 1561, LONGERON 12L TRIMMED OUT AND REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. DAMAGE TOLERANCE INSPECTION REQUIREMENT CATEGORY B - INITIAL 14,500 CYCLES AND REPETITIVE 9,500 CYCLES. COMPLIED EA 1-5310-76689, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2L73 4F RTA22WE 20040607001162004060700116 2004 6 7 SWAA041442 420040520A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 & R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C4 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F A16WE 20040607001192004060700119NM 2004 6 7 SWAA041445 120040520A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 524, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040607001212004060700121NM 2004 6 7 SWAA041447 120040520A335007912 COVER BOEING737 7377H4 1384404NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER DAMAGED AT MID CABIN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040607001222004060700122NM 2004 6 7 SWAA041448 120040520A3350311500 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 1 ABC, BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20040607001232004060700123NM 2004 6 7 SWAA041413 120040518A32601899 UPLOCK SENSOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAK NONE N FALSE WARNING CLCLIMB 1 SW29301SW 22941 LEFT MLG RED LIGHT FLICKERED AND THEN REMAINED STEADY AFTER GEAR RETRACTION. CYCLED GEAR, NO HELP. LIGHT WENT OUT AFTER 30 MINUTES. RIGHT MLG UPLOCK SENSOR RESISTANCE OUT OF RANGE. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR. 2L72 4F RTA16WE 20040607001252004060700125NM 2004 6 7 SWAA041400 120040516A3260655825029 CIRCUIT CARD BOEING737 7375H4 138449DNM E/E BAY FAULTY A SWAAK NONE N FALSE WARNING CLCLIMB 1 SW29526SW 26568 AFTER TAKEOFF THE RIGHT MLG RED WARNING LIGHT REMAINED ON, AND WITH MLG LEVER IN OFF POSITION BOTH RIGHT MLG RED AND GREEN LIGHTS ILLUMINATED. CREW CYCLED GEAR, ALL INDICATIONS NORMAL. CHECKED RESISTANCE ON PINS FROM GEAR LOGIC SHELF TO UPLOCK AND DOWNLOCK SENSORS, NO DEFECTS NOTED. REMOVED AND REPLACED CIRCUIT CARD M986 PER MM. 2L72 4F RTA16WE 20040607001262004060700126NM 2004 6 7 SWAA041401 120040517A3211654610918 PIN BOEING737 7375H4 138449DNM RT MLG BROKEN A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29526SW 26568 AIR TURNBACK, AFTER TAKEOFF RIGHT MLG RED WARNING LIGHT ILLUMINATED, AND WITH GEAR LEVER IN OFF POSITION BOTH RED AND GREEN LIGHTS ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED RIGHT MLG TRUNNION PIN PER MM. 2L72 4F RTA16WE 20040607001282004060700128NM 2004 6 7 SWAA041403 120040517A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SPV, FOUND SHEAR TIE AT BS 520, RBL 7, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040607001292004060700129NM 2004 6 7 SWAA041404 120040517A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040607001302004060700130NM 2004 6 7 SWAA041405 120040517A57536546435 FLAP BOEING737 7373H4 1384600NM RT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED PM CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20040607001312004060700131NM 2004 6 7 SWAA041406 120040517A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 5, STRINGER 21L AND BS 767, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040607001322004060700132NM 2004 6 7 SWAA041407 120040517A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 5, STRINGER 19R AND BS 732, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040607001332004060700133NM 2004 6 7 SWAA041394 120040516A531069353656 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040607001342004060700134NM 2004 6 7 SWAA041395 120040516A57536546434 FLAP BOEING737 7373H4 1384600NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 LEFT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20040607001372004060700137NM 2004 6 7 SWAA041398 120040516A53146562125 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND KEELBEAM CHORD AT BS 500D + 2, RBL 6, CORRODED. REPAIRED KEELBEAM CHORD PER EA. 2L72 4F RTA16WE 20040607001422004060700142WP 2004 6 7 GTIA040269 120040218A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE WRINKLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND FUSELAGE EXTERIOR STATION 37-58.7 SKIN WRINKLED FROM STRINGER 18L TO 24 INCHES BELOW STRINGER. CUTOUT DAMAGED AREA AT STATION 50.67.5 FROM STRINGER 18L AND 14.4 INCHES DOWN. CUT OUT AREA. FABRICATED ONE EACH 49 SPLICE DOUBLER. FABRICATED ONE EACH 7, 9, 11 AND 47 DOUBLER. INSTALLED REPAIR. (M) 2L72 4F RTA6WE 20040607001432004060700143WP 2004 6 7 GTIA040398 120040407A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND CORROSION AT AFT PIT THRESHOLD BETWEEN SKIN AND DOUBLER. UPON FURTHER NOTICE, FOUND AFT DOOR JAMB BEAM CORRODED AND OUT OF LIMITS. REMOVED DOOR JAMB BEAM. REMOVED CORROSION FROM BETWEEN SKIN AND DOUBLER AT AFT THRESHOLD. FOUND SKIN TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW BEAM. FABRICATED REPAIR DOUBLERS. INSTALLED DOOR JAMB BEAM. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20040607001452004060700145WP 2004 6 7 ASAA0480362 120040427A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01964AS 53078 PDX LINE CHECK, FOUND PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M) 2L72 4F RTA6WE 20040607001462004060700146NM 2004 6 7 ASAA0440075 120040309A531565C339481 FLOORBEAM BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT GALLEY AREA STATION 947.5 FLOORBEAM HAS CORROSION AT FASTENER HOLES LBL 16 TO RBL 16. REPAIRED FLOORBEAM. (M) 2L72 4F RTA16WE 20040607001472004060700147NM 2004 6 7 ASAA0440078 120040314A801135057166 STARTER BOEING737 737490 1384715NM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01706AS34614 28894 725629 OAK - FOUND INSPECTED NR 2 ENGINE, FOUND THE NR 2 STARTER HAD COME APART AND WAS DAMAGED. REMOVED AND REPLACED THE NR 2 ENGINE STARTER PER AMM. (M) 2L72 4F4 FRTA16WE E2GL 20040607001492004060700149NM 2004 6 7 ASAA0440074 120040309A5315654681189 FLOORBEAM BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND CABIN FLOORBEAM STATION 986.5 CORRODED RBL 48 TO LBL 48. REPLACED FLOORBEAM. (M) 2L72 4F RTA16WE 20040607001502004060700150NM 2004 6 7 ASAA0440073 120040308A531165C323061 FRAME BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND AFT CARGO PIT FRAME AT STATION 727G FORWARD SIDE HAS CORROSION BETWEEN STRINGER 26R-27R LOWER ANGLE. REPAIR FRAME, STATION 26R TO 27R. (M) 2L72 4F RTA16WE 20040607001512004060700151NM 2004 6 7 ASAA0440093 120040401A531565C3394016 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND MAIN DECK FLOORBEAM AT FS 294.5 APPROX LBL 12 TO RBL 50, UPPER T-CAP HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE. BLENDED CORROSION CK OUT OF LIMITS. REMOVED 'T' AND FABRICATED NEW 'T' AND INSTALLED 'T' AND REPAIR ANGLE PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20040607001532004060700153NM 2004 6 7 ASAA0440111 120040430A532045204831 STIFFENER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 OAK - FOUND LOWER FUSELAGE INTERNAL STATION 540-1016 PRESS BULKHEAD CHANNEL STIFFENER AT BL 0 HAS CORROSION. REMOVED CORRODED SECTION OF CHANNEL STIFFENER. INSTALLED FILLER AND REPAIR SPLICE ANGLES AT STATION 1016 PRESS BULKHEAD. (M) 2L72 4F RTA16WE 20040607001542004060700154NM 2004 6 7 ASAA0440110 120040430A532065C28106 STIFFENER BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 OAK - FOUND LOWER FUSELAGE INTERNAL STATION 540-1016 PRESS BULKHEAD CHANNEL STIFFENER AT BL 0 HAS GOUGE. REMOVED CORRODED SECTION OF CHANNEL STIFFENER. INSTALLED FILLER AND REPAIR SPLICE ANGLES AT STATION 1016 PRESSURE BULKHEAD. (M) 2L72 4F RTA16WE 20040607001552004060700155NM 2004 6 7 ASAA0440087 120040323A5310654582545 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND R1 DOOR THRESHOLD CREASEBEAM AT STATION 294.5 APPROX RBL 55, CORRODED IN NUMEROUS AREAS OF UPPER SURFACE. REMOVED AND REPLACED R1 DOOR THRESHOLD CHORD STATION 262 TO 380 RBL 55 PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20040608000042004060800004NM 2004 6 8 ASAA0440038 120040209A533065C33757 SKIN BOEING737 737490 1384715NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01794AS 28889 GYR - FOUND TEMP REPAIR TO DENT IN EXTERIOR SKIN. REPAIRED DENT IN FUSELAGE SKIN AT STATION 279 BETWEEN STRINGER 18L-19L IAW SRM. (M) 2L72 4F RTA16WE 20040608000052004060800005NM 2004 6 8 ASAA0440112 120040504A5714654543925 SUPPORT BOEING737 7374Q8 138447QNM CNTR WING BOX CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01776AS 25109 GYR - FOUND LEFT AC BAY HEAT EXCHANGER DUCT MOUNTING FLANGE CORRODED AT APPROX BS 580 LBL 36. REPAIRED LEFT CENTER WING SUPPORT WEB AT STATION 587 PER EA NR 5710-01104. (M) 2L72 4F RTA16WE 20040608000072004060800007NM 2004 6 8 ASAA0440086 120040323A531565C83940 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - MAIN DECK FLOORBEAM AT STATION 294.5 APPROX LBL 12 TO RBL 50, UPPER T-CAP HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE. BLENDED CORROSION CK OUT OF LIMITS. REMOVED 'T' AND REPAIR ANGLE EPR SRM 53-10-51. (M) 2L72 4F RTA16WE 20040608000092004060800009NM 2004 6 8 ASAA0440096 120040401A5315AND101362404 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND MAIN DECK FLOORBEAM STATION 294.5 HAS CORROSION FROM LBL 12 TO RBL 50. REPAIRED FLOORBEAM T-CAP CHORD. (M) 2L72 4F RTA16WE 20040608000122004060800012NM 2004 6 8 ASAA0440032 120040204A533065C323564 SKIN BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND FUSELAGE SKIN DENT/GOUGED AT BS 847 BETWEEN S-24R AND S-25R. REPAIRED IAW EA 5330-01688. (M) 2L72 4F RTA16WE 20040608000132004060800013NM 2004 6 8 ASAA0440034 120040204A5414311A145017 SKIN BOEING737 7374Q8 138447QNM LT PYLON CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND LEFT ENGINE PYLON OUTBOARD SKIN CHAFFED AT WING INTERFACE. REPAIRED IAW EA 5430-01128. (M) 2L72 4F RTA16WE 20040608000152004060800015NM 2004 6 8 ASAA0440094 120040401A533065C377672 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND DENT IN FUSELAGE SKIN, AF6 OF L-1 DOOR 8 FEET ABOVE VERTICAL. REPAIRED DENT IN FUSELAGE STATION 360 TO 380, STRINGER 17L AND 18L REF SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20040608000172004060800017NM 2004 6 8 ASAA0440029 120040204A5315BAC1480836 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND FLOORBEAM HAS SCREW HOLES WITH CORROSION. REPAIRED FLOORBEAM IAW SRM 53-10-01. (M) 2L72 4F RTA16WE 20040608000182004060800018NM 2004 6 8 ASAA0440030 120040204A533065516241 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND AFT PIT, CORROSION ON SKIN DOUBLER STATION 1006. REPAIRED IAW EA 5330-1743. (M) 2L72 4F RTA16WE 20040608000202004060800020NM 2004 6 8 04FDEA01149 120040504A5311AFA0029 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 TRANSVERSE FRAME DENTED, RT SIDE STA Y= 1761 ALONG LONGERON 12R. DENTED AREA AT TRANSVERSE FRAME RT, STA Y= 1761, LONGERON 12R TRIMMED OUT AND REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. DAMAGE TOLERANCE INSPECTION REQUIREMENT CATEGORY B - INITIAL 14,500 CYCLES AND REPETITIVE 9,500 CYCLES. COMPLIED EA 1-5310-76690, FUSELAGE - MAINFRAME - REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO 1-2520-7-3308. 2L73 4F RTA22WE 20040608000212004060800021NM 2004 6 8 04FDEA01150 120040504A5347ACA76921 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 MAIN DECK SEAT TRACK (RT SIDE) FOUND CORROSION, FS Y = 1235.0, X = -27.50. MAIN DECK FS Y=1235.0, X= -27.5 RT CORROSION SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040608000222004060800022NM 2004 6 8 04FDEA01151 120040504A5347ACA76921 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 MAIN DECK SEAT TRACK (RT SIDE) FOUND CROWN DAMAGED: FS Y = 1235.0, X = -47.50. MAIN DECK FS Y = 1235.0, X = -47.50 RT SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040608000232004060800023NM 2004 6 8 04FDEA01253 120040513A5230 HINGE BOEING727 727200 138407ENM MAIN CARGO DOOR WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 COMPLY WITH EA 7-5210-77407; DOORS - MAIN CARGO DOOR HINGE WEAR REPAIR P/N B27-53-070-03. COMPLIED WITH EA 7-5210-77407. MAIN CARGO DOOR HINGE REPAIR P/N B27-53-070-03. 2L73 4F RTA3WE 20040608000242004060800024EU 2004 6 8 04FDEA01252 120040513A5312 BULKHEAD AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25431FE 316 REAR PRESSURE BULKHEAD FWD FACE ON THE AFT SIDE OF FR 80/82 FROM S38L TO S38R HAS AREAS OF CORROSION. COMPLIED WITH EA 6-5310-78353 PT1. 2L72 4F RTA35EU 20040608000252004060800025NM 2004 6 8 04FDEA01112 120040428A5754651622292 STRUCTURE BOEING727 727200 138407ENM L/E SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 COMPLY WITH EA 7-5750-77346; WINGS - LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE. 2L73 4F RTA3WE 20040608000262004060800026NM 2004 6 8 04FDEA01113 120040429A5712 RIB BOEING727 727200 138407ENM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 RIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1. 2L73 4F RTA3WE 20040608000272004060800027NM 2004 6 8 04FDEA01114 120040429A5320 FLOOR SUPPORT BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25206FE 22928 FWD CARGO COMPT FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4. 2L73 4F RTA3WE 20040608000282004060800028NM 2004 6 8 04FDEA01236 120040512A5347ADA7321519 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 MAIN CARGO DECK STA 810 LEFT HAND SEAT TRACK REF X=27.5 SEAT TRACK DENTED. DENTED SEAT TRACK AT MAIN CARGO DECK STA 810 LEFT HAND SIDE X=27.5 REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040608000292004060800029NM 2004 6 8 04FDEA01237 120040512A5744ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CM 57-44-09 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0503 SHT 2. ORIGINAL THICKNESS =0.430 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.428 INCH. 2L73 4F RTA22WE 20040608000312004060800031NM 2004 6 8 04FDEA01594 120040603A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.220. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040603001342004060300134WP 2004 6 3 04FDEA01271 120040515A5753ARC1497505 FITTING DOUG DC10 DC1010 3022110WP FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT O/B FLAP NR 3 VANE FITTING FWD BOLT HOLE HAS CORROSION. AFT BOLT HOLE BUSHING IS CORRODED AND FITTING HAS NUMEROUS AREAS OF CORROSION. RECEIVED NEW NR 3 VANE FITTING TO BE INSTALLED ON WORK CARD E8-5750-7- 5000 PT 3 AT MAE. 2L73 4F A22WE 20040604000062004060400006EU 2004 6 4 04FDEA01436 120040524A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MAIN DECK CARGO COMP, ONE EACH SPOT OF CORROSION BETWEEN FR 54 AND 54.1 ON SEAT TRACK L5. REMOVED AND REPLACED DUMMY SEAT TRACK IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20040604000142004060400014NM 2004 6 4 04FDEA01444 120040525A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 STA 600 FRAME DENTED BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY. FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY DENT FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665. 2L73 4F RTA3WE 20040604000212004060400021NM 2004 6 4 SWAA041540 120040530A53156546810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 947, LBL 53.5, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F RTA16WE 20040604000242004060400024NM 2004 6 4 SWAA041543 120040601A53106554892 STOP FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND BS 303.9 DOOR CUTOUT FRAME FWD STOP FITTING, CRACKED. REPAIRED DOOR CUTOUT FRAME FWD STOP FITTING PER SB. 2L72 4F RTA16WE 20040604000302004060400030NM 2004 6 4 SWAA041544 120040601A324426015711 TIRE BOEING737 7372H4 138448CNM LT MLG BLOWN A SWAAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SW29087SW 22903 AIR TURNBACK, NR 1 TIRE BLEW ON TAKEOFF DAL. REMOVED AND REPLACED NR 1 AND NR 2 MAIN WHEEL AND TIRE ASSEMBLIES PER MM. 2L72 4F A16WE 20040604000342004060400034WP 2004 6 4 04FDEA01554 120040601A5320ACA7561 PLATE DOUG DC10 DC1010 3022110WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CARGO DOOR CUTOUT FWD JAMB UPPER SCUFF PLATE IS GOUGED. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-21-02 AT MAE. 2L73 4F A22WE 20040604000392004060400039 2004 6 4 SWAA041548 420040602A2565D31591478 SLIDE BOEING737 7373H4 1384600NM R1 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040604000492004060400049NM 2004 6 4 SWAA041558 120040602A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040604000522004060400052NM 2004 6 4 SWAA041561 120040602A53116546555 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 867, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040604000612004060400061 2004 6 4 SWAA041517 420040530A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040604000652004060400065NM 2004 6 4 SWAA041521 120040531A3350101114 LENS BOEING737 7373A4 1384585NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 RT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20040604000672004060400067NM 2004 6 4 SWAA041523 120040531A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 5, STRINGER 15R, BS 500C + 5, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040604000712004060400071NM 2004 6 4 SWAA041527 120040531A291065C26809 HYDRAULIC LINE BOEING737 7373A4 1384585NM RT MLG LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29674AA 23252 DECLARED EMERGENCY/DIVERSION, NR 1 ENGINE A SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED RT MLG UPLOCK HYDRAULIC LINE PER MM. 2L72 4F RTA16WE 20040604000762004060400076NM 2004 6 4 SWAA041439 120040520A291065C2680101150 HYDRAULIC LINE BOEING737 7373H4 1384600NM NR 2 ENGINE LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29635SW 27708 AIR TURNBACK, NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM QUANTITY DROPPED TO 1/4 FULL. REMOVED AND REPLACED NR 2 ENGINE B-SYSTEM HYDRAULIC SUPPLY LINE PER MM. 2L72 4F RTA16WE 20040604000872004060400087EU 2004 6 4 USAA040170 120040428A5321D5367175301800 FLOOR PANEL AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 FLOOR PANEL, 4.5 INCH X 5.5 INCH OB AFT CORNER, DELAMINATION FR 66, Y1182, FLOOR PANEL 261 HG. NEW PANEL FABRICATED IAW SRM 53-02-00, FIG 309. 2L72 4F4 FRTA28NM E2GL 20040604000942004060400094EA 2004 6 4 HJB2004F00000 120040123A1430 SCREW DHAV DHC3 DHC3 2800202EA PWA R1340 R1340* 52016NE IDU DEFECTIVE B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL05336AK 333 BAD LOCKING SCREW. 1H71 3R3 R A815 5E2 20040604001052004060400105EU 2004 6 4 USAA040174 120040429A5320D5348004320401 SILL AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW13655 0936 SILL, 4.25 INCHES X 2.5 INCHES X .042 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66, Z240, Y1972. REMOVED AND REPLACED SILL IAW SRM 51-74-00, 53-41-14, 51-42-11. 2L72 4F4 FRTA28NM E2GL 20040604001092004060400109EU 2004 6 4 USAA040185 120040507A5320D5347218920200 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW15976 0904 BEAM, 3 INCH X 1.5 INCHES X .032 INCH DEEP AREA, CORROSION; LEVEL 2; TASK JA-260-53500 BETWEEN FR 68, 69, Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040604001142004060400114WP 2004 6 4 GTIA040401 120040403A5754 RIB DOUG DC9 DC983 3022083WP L/E SLAT DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND RIGHT WING NR 5 SLAT OUTBOARD EDGE SEAL IS TORN. OUTBOARD RIB NR 5 SLAT REMOVED. FOUND RIB TO BE DAMAGED BEYOND REPAIR. NEW RIB SEAL AND RETAINER INSTALLED. (M) 2L72 4F RTA6WE 20040604001182004060400118WP 2004 6 4 GTIA040405 120040401A5753 VANE DOUG DC9 DC983 3022083WP T/E FLAP DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND RIGHT NR 3 OUTBOARD VANE FULL OF WATER AND HAS CORROSION ON HARDWARE. UPON FURTHER INSPECTION FOUND DELAMINATION AT OUTBOARD TRAILING EDGE. REPAIRED DELAMINATED AREA. (M) 2L72 4F RTA6WE 20040604001212004060400121WP 2004 6 4 GTIA040408 120040419A3350010561001 LIGHT DOUG DC9 DC983 3022083WP A/C BAY BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND TWO EMERGENCY LIGHT ASSEMBLIES IN AFT ACCESSORY COMP BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTS ASSEMBLY. (M) 2L72 4F RTA6WE 20040604001252004060400125WP 2004 6 4 GTIA040413 120040413A3350 PIN DOUG DC9 DC983 3022083WP PORTABLE LIGHT DAMAGED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND PORTABLE EMERGENCY LIGHT, FLASHLIGHT, DOES NOT WORK. REMOVED AND REINSTALLED NEW PINS FOR PLUG. (M) 2L72 4F RTA6WE 20040607000012004060700001WP 2004 6 7 04FDEA01610 120040603A5320FXSRM531501 FLOOR SUPPORT DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 AFT CARGO COMPT DOOR SILL FLOOR BOARD SUPPORT IS CORRODED STA 1801 TO 1841. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-01 AND SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040607000142004060700014WP 2004 6 7 04FDEA01569 120040602A5320AWE867621 CLIP DOUG DC10 DC1010 3022110WP CARGO BAY BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MCD, RT VENT PNL FAIRING CLIPS BROKEN AT STA 615. REMOVED AND REPLACED BROKEN CLIPS IAW SRM 51-21-02 AT BFM/MAE. 2L73 4F A22WE 20040607000632004060700063NM 2004 6 7 04FDEA01021 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000662004060700066NM 2004 6 7 04FDEA01024 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END OUTBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000742004060700074WP 2004 6 7 04FDEA01517 120040528A5753ARC01542 HINGE BRACKET DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5740-77420 WING - RIGHT INBOARD FLAP - OUTBOARD HINGE BRACKET CORROSION REPAIR (P/N ARC0154-2). COMPLIED WITH EA 8-5740-77420 LEFT INBOARD FLAP - O/B HINGE BRACKET CORROSION REPAIR (P/N ARC 0154-2) FABRICATED BUSHING ON TRAV 432592 AT MAE. 2L73 4F A22WE 20040607001102004060700110NM 2004 6 7 04FDEA01071 120040423A5753ARC050311 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, OUTBOARD FLAP, OUTBOARD FWD HINGE, ACTUATOR HOLE 8 INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76021, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES, LEFT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040607001202004060700120NM 2004 6 7 SWAA041446 120040520A53126545409 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 40, CRACKED. REPAIRED BEADED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20040607001272004060700127NM 2004 6 7 SWAA041402 120040517A531465621257 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SPV, FOUND KEELBEAM CHORD AT BS 727 +2.5, AT RBL 7, CORRODED. REMOVED AND REPLACED KEELBEAM CHORD PER EA. 2L72 4F RTA16WE 20040607001362004060700136NM 2004 6 7 SWAA041397 120040516A53156545410 FLOORBEAM BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 660, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040607001402004060700140WP 2004 6 7 GTIA040394 120040419A2560 CABLE DOUG DC9 DC983 3022083WP TAIL SLIDE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 DTW - FOUND TAIL SLIDE COVER KEVLAR CABLE NOT ROUTED CORRECTLY. INSTALLED KEVLAR CABLE CORRECTLY. (M) 2L72 4F RTA6WE 20040607001412004060700141WP 2004 6 7 GTIA040395 120040428A2560 CABLE DOUG DC9 DC981 3022081WP EVAC SLIDE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 DTW - FLT 955 - FOUND L-2 DOOR ESCAPE SLIDE CABLE TO GIRT BAR INCORRECTLY ATTACHED. REPOSITIONED CABLE. (M) 2L72 4F A6WE 20040607001442004060700144NM 2004 6 7 ASAA04100248 120040504A33506013211 BATTERY PACK BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT L2, R2 DOORS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS IAW 33-51-51. (M) 2L72 4F A16WE 20040607001482004060700148NM 2004 6 7 ASAA0440076 120040309A5310654587547 CREASE BEAM BOEING737 737490 1384715NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 GYR - FOUND CREASE BEAM WEB AT STATION 304, R1 DOOR HAS DEEP GOUGE JUST INBOARD OF CREASE BEAM INNER CHORD. REMOVED AND REPLACED WEB. (M) 2L72 4F RTA16WE 20040607001522004060700152NM 2004 6 7 ASAA0440092 120040401A5310654582545 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND R1 DOOR THRESHOLD CREASEBEAM AT STATION 294.5 APPROX RBL 55, CORRODED IN NUMEROUS AREAS OF UPPER SURFACE. REMOVED AND REPLACED R-1 DOOR THRESHOLD CHORD STATION 262 TO 380 RBL 55 PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20040608000022004060800002NM 2004 6 8 ASAA0440105 120040415A5712654544555 RIB BOEING737 7374Q8 138447QNM LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01773AS 25106 GYR - FOUND LEFT WING INTERNAL RIB AT STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOWER CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M) 2L72 4F RTA16WE 20040608000032004060800003NM 2004 6 8 ASAA0440017 120040130A5320654769015 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01784AS 28199 FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT LEFT Z-ANGLE HAS CORROSION BETWEEN STATION 727G AND 770, MARKED. REPAIRED IAW SRM 53-60-53 PAGE 209. (M) 2L72 4F RTA16WE 20040608000082004060800008NM 2004 6 8 ASAA0440079 120040315A531065465349 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND FORWARD CARGO COMPARTMENT, STATION 520 RBL 3, LOWER FRAME SHEAR TIE 100 PERCENT EXFOLIATED. FABRICATED AND INSTALLED 65-46534-9 SHEAR TIE. (M) 2L72 4F RTA16WE 20040608000322004060800032NM 2004 6 8 04FDEA01595 120040603A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL DIAMETER= 1.187, FINAL DIAMETER= 1.221. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040608000332004060800033NM 2004 6 8 04FDEA01596 120040603A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND SIDE LINK MATING SURFACE CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS =0.446, MATERIAL REMOVED =0.003, REMAINING THICKNESS =0.443, WITHIN LIMIT AS PER DWG NR ARC0503. 2L73 4F RTA22WE 20040608000352004060800035NM 2004 6 8 04FDEA01598 120040603A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND OUTBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407. ORIG. DIAM.: 1.187, FINAL DIAM.: 1.222, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76724 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040608000362004060800036NM 2004 6 8 04FDEA01600 120040603A5312AEA76211 PRESSURE PANEL DOUG MD11 MD11 3023602NM FUSELAGE CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT HAND WHEEL WELL - OIL CANNING FOUND AT STA: Y= 1395-1401, Z= -90 TO -100, DEPTH= 0.0549 INCH Y= 1401-1411, Z= -90 TO -100, DEPTH= 0.0941 INCH Y= 1411-1421, Z= -90 TO -100, DEPTH= 0.0921 INCH Y= 1421-1431, Z= -90 TO -100, DEPTH= 0.0976 INCH Y= 1431-1441, Z= -70 TO -90, DEPTH= 0.1430 INCH. COMPLIED FEDEX EA 1-5310-76719, FUSELAGE - MAINFRAME - KEEL WEB / CENTER LANDING GEAR INSPECTION REQUIRMENTS, PART I. 2L73 4F RTA22WE 20040608000402004060800040NM 2004 6 8 04FDEA01238 120040512A5744ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED, FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCH, AND REPAIRED AS PER EA 1-5740-75958 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040608000422004060800042NM 2004 6 8 04FDEA01240 120040512A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - SPOTFACE AT BARREL NUT AREA FOUND CORRODED. LEFT FWD O/B FLAP I/B HINGE SPOTFACE AT BARREL NUT AREA CORROSION REMOVED AS PER CMM 57-44-08 PG 402-407, ORIG THK 0.382 INCH, MATERIAL REMOVED 0.002 INCH, REMAINING THK 0.380 INCH AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040608000432004060800043NM 2004 6 8 04FDEA01241 120040512A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AS PER CM 57-44-08 PAGES 402-407, AND FOUND WITHIN LIMITS AS PER DWG ARC0502. ORIGINAL THICKNESS =0.468 INCH, MATERIAL REMOVED =0.002 INCH, REMAINING THICKNESS =0.466 INCH. 2L73 4F RTA22WE 20040608000442004060800044NM 2004 6 8 04FDEA01242 120040512A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR I/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR I/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.221 INCH, AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040608000452004060800045NM 2004 6 8 04FDEA01243 120040512A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - ACTUATOR O/B LUG HOLE FOUND CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE ACTUATOR O/B LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-08 PG 402-407, ORIG DIA 1.187, FINAL DIA 1.221 INCH, AND REPAIRED AS PER EA 1-5740-75956 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040608000472004060800047WP 2004 6 8 04FDEA01245 120040512A5320D10250732 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CABIN RIGHT UPPER GILLINER SUPPORT BRACKETS ATTACHED TO FRAMES FS 635 AND 655 ARE BROKEN. REMOVED AND REPLACED CLIPS AT STA 635 AND 655 IAW SRM 51-35-01, FABBED FROM 2024-T3 .063C BATCH 702499 DRWG D10-25-073 AT MAE. 2L73 4F A22WE 20040608000492004060800049NM 2004 6 8 04FDEA01424 120040524A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 STRINGER CLIP CRACKED STA 950C STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 7R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040608000502004060800050NM 2004 6 8 04FDEA01425 120040524A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 STRINGER CLIP CRACKED STA 950A STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 7R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040608000512004060800051NM 2004 6 8 04FDEA01426 120040524A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO STA 660 FRAME DENTED AT STR 24 RT. TRIMMED OUT DENT DAMAGE FROM FLANGE ON FRAME STA 660, STR 24R, LOCATED AND DRILLED FASTENER HOLES IN REPAIR DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7-5310-70665. ALODINED, PRIMERED AND INSTALLED FASTENERS PER SRM 51-20-1 AND 51-30-2. APPLIED BMS3-29 TO REPAIR AREA. 2L73 4F RTA3WE 20040608000542004060800054WP 2004 6 8 04FDEA01430 120040524A5753ARC1984 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-77413 WING - RT OUTBOARD FLAP - FLAP MOUNTED HINGE POSITION INDICATOR HOLE REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-77412. 2L73 4F A22WE 20040608000552004060800055WP 2004 6 8 04FDEA01431 120040524A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5310-77410 FUSELAGE MAIN FRAME - MINOR DEVIATION TO SRM SEAT TRACK SPLICE. COMPLIED WITH EA 8-5310-77410. 2L73 4F A22WE 20040608000572004060800057NM 2004 6 8 04FDEA01433 120040524A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CRACKED STRINGER CLIP, STA 950C, STRINGER 5R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 5R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040608000582004060800058NM 2004 6 8 04FDEA01434 120040524A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CRACKED STRINGER CLIP, STA 950D, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 6R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040608000592004060800059NM 2004 6 8 04FDEA01435 120040524A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01) ON FLOORBEAM UPPER SURFACE BS 380 RBL 25 TO 35 WL 208. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA RBL 25.75 TO 27.75 AND RBL 46 TO 48 AT BS 380, WL 208. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS, BOTH LOCATIONS, IAW SRM 53-10-1 AND 53-10-8 FIG 8. 2L73 4F RTA3WE 20040608000602004060800060NM 2004 6 8 04FDEA01451 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.094. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040608000612004060800061WP 2004 6 8 04FDEA01247 120040512A5753ARC20031 CARRIAGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 RIGHT O/B FLAP BOTH I/B AND O/B CARRIAGES HAVE CORROSION IN ROLLER MOUNT HOLES. REPLACED I/B AND O/B ROLLER CARRIAGES TO BE INSTALLED ON EO 8-5750-7-5000 AT MAE. 2L73 4F A22WE 20040608000622004060800062NM 2004 6 8 04FDEA01452 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.506, MATERIAL REMOVED : 0.007, REMAINING THICKNESS OF LUG: 0.506. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040608000632004060800063WP 2004 6 8 04FDEA01248 120040512A5230ADA36751 BRACKET DOUG DC10 DC1010 3022110WP CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 FORWARD LWR CARGO DOOR LATCH SPOOL FITTING CORRODED AND SPOOL PITTED. REPLACED BRACKET AND SPOOL IAW MM 52-31-00-5 AT MAE. 2L73 4F A22WE 20040608000652004060800065WP 2004 6 8 04FDEA01250 120040513A5753ARC2700501 FLAP TRACK DOUG DC10 DC1010 3022110WP T/E FLAP VANE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 LEFT INBOARD FLAP VANE NR 2 TRACK HAS DEEP WEAR MARKS ON LOWER & UPPER SURFACE. REPLACED NR 2 LEFT I/B TRACK TO BE INSTALLED ON EO 8-5750-7-5002 AT MAE. 2L73 4F A22WE 20040608000672004060800067NM 2004 6 8 04FDEA01453 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.093, FINAL DIAMETER =1.129. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040608000692004060800069NM 2004 6 8 04FDEA01455 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING OUTBOARD FLAP AFT INBOARD HINGE, FOUND INBOARD PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER =1.062, FINAL DIAMETER =1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040608000702004060800070NM 2004 6 8 SWAA041574 120040604A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT RT BS 400, WL 208. REPAIRED SKIN CRACKS PER SRM. 2L72 4F RTA16WE 20040608000712004060800071NM 2004 6 8 SWAA041575 120040604A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 787, STRINGER 18L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040608000722004060800072 2004 6 8 SWAA041576 420040604A256563550101 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040608000732004060800073 2004 6 8 SWAA041577 420040604A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040608000762004060800076NM 2004 6 8 SWAA041580 120040604A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 500C, STRINGER 26R, CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM. 2L72 4F RTA16WE 20040608000782004060800078NM 2004 6 8 SWAA041582 120040604A256065C19901 CABLE BOEING737 7373H4 1384600NM EVAC SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040608000802004060800080NM 2004 6 8 SWAA041584 120040604A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, LBL 7, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040608000822004060800082NM 2004 6 8 SWAA041586 120040604A52306547952524 WEB BOEING737 7375H4 138449DNM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD LOWER CORNER WEB, CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2L72 4F RTA16WE 20040608000852004060800085NM 2004 6 8 CALA0400495 120040428A53156545410200 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770353 23591 A CRACK WAS FOUND IN THE LONGITUDINAL FLOORBEAM UPPER CHORD AT ITS ATTACHMENT TO THE TRANSVERSE FLOORBEAM AT STA 727B, RBL 45. THE CRACK WAS LOCATED ON THE I/B SIDE OF THE LONGITUDINAL FLOORBEAM AT THE SECOND HI-LOK FASTENER HOLE FORWARD OF STA 727B. THE CRACK RAN FROM THE I/B EDGE OF THE LONGITUDINAL FLOORBEAM TO THE HI-LOK FASTENER HOLE. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01187. 2L72 4F RTA16WE 20040608000862004060800086NM 2004 6 8 CALA0400496 120040426A5320 SILL BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND THE L-1 DOOR LOWER SILL CHORD CORRODED AT BS 318, LBL 57. THE AREA WAS REPAIRED IAW ECRA 5321-01186. 2L72 4F RTA16WE 20040608000872004060800087NM 2004 6 8 CALA0400497 120040520A5420313N505228 STRUCTURE BOEING757 757224 1384958NM NR 2 PYLON GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714102 27292 INSPECTION FOUND THE NR 2 ENGINE PYLON STRUCTURE LOWER CHORD GOUGED IN TWO PLACES AT STA 260. THE AREA WAS REPAIRED IAW ECRA 5450-01565. 2L72 4F RTA2NM 20040608000882004060800088NM 2004 6 8 CALA0400498 120040520A531565C33950 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769602 27315 INSPECTION FOUND AFT MAIN CABIN FLOORBEAM CORRODED AT FS 986, LBL 46. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-31, FIGURE 203. 2L72 4F RTA16WE 20040608000912004060800091NM 2004 6 8 CALA0400508 120040522A5320BAC1496444 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2736247 28807 INSPECTION FOUND FORWARD CARGO LT Z-CHANNEL CORRODED FROM STA 490-500I. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53 AND 51-40-02. 2L72 4F RTA16WE 20040608000942004060800094NM 2004 6 8 CALA0400511 120040526A3350D71702030 CHARGER BOEING767 767424ER 1385270NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2777066 29461 THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT STA 841, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07. 2L72 4F RTA1NM 20040608000982004060800098WP 2004 6 8 CALA0400502 120040523A53202929169 CHANNEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND RIGHT HAT SECTION CORRODED AT STA 148-200, RBL 12. A NEW HAT SECTION WAS INSTALLED IAW SRM 53-14-01, 51-10-04, AND 51-30-01. 2L72 4F A6WE 20040608001032004060800103WP 2004 6 8 CALA0400514 120040528A5320993638102N ANGLE DOUG DC9 DC982 3022082WP RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND A 1 INCH CRACK IN RIGHT WHEEL WELL FORWARD END ANGLE AT KEEL BEAM, STA 984. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2L72 4F A6WE 20040608001052004060800105NM 2004 6 8 CALA0400516 120040529A3397 WIRE BOEING737 7373T0 1384582NM CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW2776354 23592 THE ROW 8ABC EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW MM 20-20-00 AND 33-51-21. 2L72 4F RTA16WE 20040608001062004060800106NM 2004 6 8 CALA0400517 120040530A335020131A BATTERY PACK BOEING757 757224 1384958NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2719136 29285 INSPECTION FOUND FIRST CLASS CABIN EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-07. 2L72 4F RTA2NM 20040608001072004060800107NM 2004 6 8 CALA0400518 120040530A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2733286 31600 INSPECTION FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20040608001082004060800108NM 2004 6 8 CALA0400519 120040530A253072067002 OVEN BOEING757 757224 1384958NM FWD GALLEY MALFUNCTIONED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW271412120264 27563 THE FLIGHT ATTENDANT'S REPORTED SMOKE AROUND THE FORWARD GALLEY APPROXIMATELY 10 MINUTES AFTER TAKEOFF FROM IAH. THE SMOKE DISSIPATED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A SMOKE INSPECTION WAS PERFORMED AND NOTHING ABNORMAL WAS FOUND. MAINTENANCE FOUND THAT THE FORWARD GALLEY INBOARD OVEN GOT MUCH HOTTER THAN THE OTHERS. THE OVEN WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. NO OTHER DISCREPANCIES WERE NOTED. 2L72 4F RTA2NM 20040608001102004060800110NE 2004 6 8 CALA0400493 220040519A7310405744 SHUTOFF VALVE BOEING737 737524 1384721NM GE CFM56 CFM563B1 13802NE NR 1 ENGINE SHORTED A CALAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SW271463918556 28900 856821 THE AUTOTHROTTLE DISCONNECTED AND THE NR 1 ENGINE AUTO SHUTDOWN ON FINAL APPROACH TO IAH. NO RESTART WAS ATTEMPTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND CANNON PLUG D05162P SHORTED WHICH CAUSED THE NR 1 ENGINE FUEL S/O VALVE TO POWER CLOSED. THE FUEL S/O MOTOR WAS ALSO SHORTED. THE FUEL S/O VALVE WAS REPLACED IAW MM 28-22-11. THE D05162P AND D05162J CANNON PLUGS WERE REMOVED AND REPLACED IAW STANDARD PRACTICES WIRING MANUAL 20-00-01. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E2GL 20040608001132004060800113WP 2004 6 8 CALA0400490 120040513A5347SRO95301157001 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714840 49580 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT GALLEY MOUNTS, STA 1174 AND 1212. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-05. 2L72 4F A6WE 20040608001142004060800114WP 2004 6 8 CALA0400522 120040604A5313S1242886 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND LONGERON 22L CORRODED AT STA 1287. REPAIRED IAW SRM 53-02, FIGURE 18. 2L72 4F A6WE 20040608001152004060800115NM 2004 6 8 CALA0400523 120040604A532065C3397053 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714662 28923 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT NUT PLATE HOLES, STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20040608001172004060800117NM 2004 6 8 CALA0400525 120040605A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2739728 28944 INSPECTION FOUND THE R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. THE FORWARD EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040608001182004060800118NM 2004 6 8 CALA0400521 120040603A523065C36183 SKIN BOEING737 737524 1384721NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769602 27315 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR OUTER SKIN DENTED 15 INCHES FROM TOP AND 18 INCHES FROM AFT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203. 2L72 4F RTA16WE 20040608001192004060800119EU 2004 6 8 MALA040430 120040519A3350549132406 BATTERY SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15457XJ 340B457 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1510 FAILED CAPACITY CHECK. MAINTENANCE REPLACED (2EA) BATTERY ASSEMBLY P/N 549-1324-06 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04. 2L72 4T RTA52EU 20040608001212004060800121EU 2004 6 8 MALA040433 120040515A3350 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1987 FAILED CAPACITY CHECK. MAINTENANCE REPLACED (2 EA) CELL PACKS P/N 549-1324-06 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/2004. 2L72 4T RTA52EU 20040608001222004060800122EU 2004 6 8 MALA040432 120040513A33505521981 POWER SUPPLY SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL1599XJ 340A099 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N ELB410 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04. 2L72 4T RTA52EU 20040608001232004060800123EU 2004 6 8 MALA040422 120040601A302044730501 CONTROL MODULE SAAB SF340 340B 7860101EU DEICE SYSTEM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15424XJ 340B424 RIGHT INTAKE LIGHT ILLUMINATED CYCLED ON AND OFF AFTER TAKEOFF. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DEICE CONTROL MODULE PER AMM 30-20-15 P/N 44730-501, S/N ON A00012, S/N OFF A00432. 2L72 4T RTA52EU 20040608001262004060800126EU 2004 6 8 MALA040427 120040527A3350330131 BATTERY SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 DURING CAPCACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 1394 FAILED ON WING CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 5/29/04. 2L72 4T RTA52EU 20040608001272004060800127EU 2004 6 8 MALA040428 120040527A3350330131 BATTERY SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446XJ 340B446 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2206 FAILED ON WING CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/30/04. 2L72 4T RTA52EU 20040608001282004060800128EU 2004 6 8 MALA040429 120040520A335055219801 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 UNIT WAS REMOVED FOR MISSING CAMLOCK, P/N 61-0478-9, S/N ELB082. WHILE UNDERGOING BENCH CHECK, UNIT FAILED CAPACITY CHECK. REPLACED CELL PACK P/N 55-219801 AND UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/27/04. 2L72 4T RTA52EU 20040608001292004060800129EU 2004 6 8 MALA040425 120040525A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15457XJ 340B457 DURING 4Y/2Y INSPECTION IN LCQ, FS 300 RT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05. 2L72 4T RTA52EU 20040608001302004060800130EU 2004 6 8 MALA040431 120040513A33506104789 POWER SUPPLY SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A MALAK NONE O OTHER ININSP/MAINT 1 GL1599XJ 340A099 DURING CAPACITY CHECK IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N ELB103 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/21/04. 2L72 4T RTA52EU 20040608001312004060800131EU 2004 6 8 MALA040415 120040524A243523080031 STARTER GEN SAAB SF340 340B 7860101EU RIGHT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15406XJ 340B406 RIGHT DC GEN FELL OFF LINE AND WOULD NOT RESET. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED RIGHT DC STARTER GENERATOR IAW SF 340 AMM 24-31-05-4. ALL CHECKS GOOD. P/N ON OFF 23080-031, S/N ON 7552, S/N OFF 98149. 2L72 4T RTA52EU 20040608001332004060800133EU 2004 6 8 USAA040218 120040512A5320D5347218820200 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 BEAM, 1.0 INCH X 1.0 INCH X .020 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500 FR 68, Y 1292, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001352004060800135EU 2004 6 8 USAA040226 120040506A5320D5347209000200 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 BEAM, 1.0 INCH X 1.50 INCH X .090 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME Y765 AND CROSSBEAM C66, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001372004060800137EU 2004 6 8 USAA040186 120040507A5347D5347217220390 SEAT TRACK AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW15976 0904 SEAT TRACK, 2 INCHES X 1.6 INCHES X .038 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR68, Y1292, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001382004060800138EU 2004 6 8 USAA040193 120040507A5320D534721220290 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW 0904 BEAM, 2.0 INCHES L X 1.5 INCHES W X .055 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500, BEAM, FR 68, Y1292, Z240. REPLACED BEAM. 2L72 4F4 FRTA28NM E2GL 20040608001392004060800139EU 2004 6 8 USAA040219 120040512A5320D5347217220290 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 BEAM 1.0 INCH X 2.0 INCH X .020 INCH, CORROSION; LEVEL 2; TASK NR JA-160-53500. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001402004060800140EU 2004 6 8 USAA040192 120040507A5347D5300282600101 TRACK AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW 0904 TRACK, 2.5 INCHES X 1.5 INCHES X .090 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR14, Y503.2, Z240. REMOVED AND REPLACED TRACK IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001422004060800142EU 2004 6 8 USAA040217 120040512A5321D5367151200100 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 FLOOR PANEL, .9 INCH CRACK, MAIN CABIN, FLOOR PANEL 242 MF. FABRICATED FLOOR PANEL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001442004060800144EU 2004 6 8 USAA040195 120040508A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW15976 0904 SILL, 1 INCH X .75 INCH X .052 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, L-2 DOOR SILL PLATE FRAME 66-68, Z240. REMOVED AND REPLACED SILL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001452004060800145EU 2004 6 8 USAA040197 120040508A5320D5348004320501 PLATE AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW15976 0904 DOOR SEAL PLATE, 1 INCH X .8 INCH X .50 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500, BEAM C66, Y1732, Z240. REMOVED AND REPLACED SCUFF PLATE. 2L72 4F4 FRTA28NM E2GL 20040608001462004060800146NM 2004 6 8 USAA040207 120040426A5315 FLOORBEAM BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US68850 23898 FLOORBEAM, 2 INCHES X 2 INCHES AREA, CORROSION; NO TASK/ LEVEL, CABIN FLOOR, TOP OF FLOORBEAM STA 1502, LBL 28. SPLICE REPAIR INSTALLED IAW SRM. 2L72 4F4 FRTA1NM E13NE 20040608001482004060800148NM 2004 6 8 USAA040209 120040429A5320 WEB BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US 23898 WEB CUTOUT, .75 INCH LONG EACH, CRACKS (2) SEAT TRACK AT BS 785, RBL 55 CABIN FLOOR LEVEL. SPLICED IN FABRICATED TEE CAP IAW 53-00-51, FIG 203. 2L72 4F4 FRTA1NM E13NE 20040608001492004060800149EU 2004 6 8 USAA040212 120040512A5320D5348015800500 SUPPORT AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 GIRT BAR FITTING SUPPORT, 1.5 INCHES X 1.0 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 68 BL-Y 1732. REMOVED AND REPLACED SUPPORT IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001502004060800150EU 2004 6 8 USAA040214 120040513A5320D53480043001 SILL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 SILL, 1.0 INCH X 1.0 INCH X .07 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500, Z240, BTW FR 66 AND FR 68 BL-Y 1732. REMOVED AND REPLACED SILL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001532004060800153EU 2004 6 8 USAA040215 120040513A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 SILL, 1.0 INCH X 1.0 INCH X .08 INCH AREA, CORROSION; LEVEL 2 TASK NR JA-260-53500, Z240 BET FR 66,FR68J BL Y1732. REMOVED AND REPLACED SILL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001542004060800154EU 2004 6 8 USAA040213 120040512A5320D5348015900500 SUPPORT AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 GIRT BAR FITTING SUPPORT, 1.0 INCH X 1.0 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66 BL, Y 1732, Z240. REMOVED AND REPLACED SUPPORT IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001552004060800155EU 2004 6 8 USAA040221 120040512A5320D5437217220390 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 BEAM, 1.5 INCH X 1.5 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 67, BL-Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM 53-00-14, FIG 102. 2L72 4F4 FRTA28NM E2GL 20040608001572004060800157EU 2004 6 8 USAA040222 120040512A5320 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 BEAM, 3.0 INCH X 1.0 INCH X 0.25 INCH CORROSION; LEVEL 2; TASK NR JA-260-53500, FR66, BL-Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM 53-00-14, FIG 102. 2L72 4F4 FRTA28NM E2GL 20040608001592004060800159EU 2004 6 8 USAA040227 120040506A5320D5347209200000 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 BEAM, 1.0 INCH X 2.0 INCH X .025 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME Y765, CROSSBEAM C68 AND C70, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001602004060800160EU 2004 6 8 USAA040225 120040506A5320D5347219320000 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 BEAM, 1.0 INCH X 1.5 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR-Y765, BETWEEN CROSSBEAM C66, C67, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001612004060800161EU 2004 6 8 USAA040228 120040506A5320D5347112420100 WEB AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 WEB, 7 INCH X 3 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, WEB BETWEEN FRAME 69, 70, Y1292. REPLACED PART IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001622004060800162SO 2004 6 8 C2XA04SH328 120040527A521014524131011 BRACKET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040608001632004060800163SO 2004 6 8 C2XA04SH325 120040527A531514530375001 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE SHELL PLATE ON TOP OF THE CENTER OMEGA BEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040608001652004060800165SO 2004 6 8 CHQA000448 120040121A3350 POWER SUPPLY EMB 135 EMB135LR 3260305SO LYC O320 O320* 41508EA CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844 145620 AFT EMERGENCY LIGHTS OUT. REMOVED AND REPLACED 1, 2, 3, AND 4 EMERGENCY POWER PACKS IAW 135 AMM CH 33-50-04. OPS CHECK GOOD. 2L72 4F3 ORTT00011ATE274 20040608001682004060800168SO 2004 6 8 CHQA000460 120040208A3397 WIRE EMB 145 EMB145LR 3260212SO CONT IO360 IO360* 17025CE CABIN EXPOSED A CHQAK NONE O OTHER ININSP/MAINT 1 GL11262 145144 PROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-08-4. 2L72 4T3 ORTT00011ATE1CE 20040608001702004060800170SO 2004 6 8 CHQA000443 120040215A3350 LIGHT EMB 145 EMB145LR 3260212SO CONT IO360 IO360* 17025CE CABIN MALFUNCTIONED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11264 145221 NO POWER LEFT TO EMERGENCY LIGHTS. MECHANIC TESTED LIGHTS IAW EMB-145 MM 33-50-00. FOUND TO BE WORKING OK. 2L72 4T3 ORTT00011ATE1CE 20040608001712004060800171SO 2004 6 8 CHQA000446 120040125A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11841 145737 RT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. LAMP PN 1317. 2L72 4F RTT00011AT 20040608001732004060800173SO 2004 6 8 CHQA000455 120040118A3397 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A CHQAK NONE O OTHER ININSP/MAINT 1 GL11261 145144 NR 1 PROXIMITY STRIP WIRE FOUND BROKEN. REPAIRED IAW STANDARD PRACTICES CHAPT 20-10. 2L72 4T RTT00011AT 20040608001752004060800175SO 2004 6 8 CHQA000450 120040115A3350 CONNECTOR EMB 145 EMB145LR 3260212SO LYC O360 AEIO360* EA CABIN LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11292 145488 EMERGENCY EXIT LOCATOR SIGN ROW 12 OVERHEAD POSITION INOPERATIVE. RESECURED CONNECTION TO EXIT LIGHT ASSY. OPS CHECK GOOD REF 145 AMM 33-50-01. 2L72 4T3 ORTT00011AT1E10 20040608001762004060800176SO 2004 6 8 CHQA000451 120040113A3350 BULB EMB 135 EMB135KL 3260302SO CONT A75 A75* 17005SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378 145593 RT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F3 ORTT00011ATE213 20040608001772004060800177SO 2004 6 8 CHQA000452 120040114A3397 WIRE EMB 135 EMB135KL 3260302SO CONT A75 A75* 17005SO CABIN BROKEN A CHQAK NONE O OTHER ININSP/MAINT 1 GL11378 145593 FLOOR PROXIMITY LIGHT STRIP HAS BROKEN WIRES. REPAIRED LIGHT STRIP IAW EMB145 WM 20-21-00 AND EMB145 AMM 33-56-12. 2L72 4F3 ORTT00011ATE213 20040609000022004060900002NM 2004 6 9 AALA20040613 120040603A33970201875001 WIRE HARNESS BOEING737 737823 13844BZNM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21971AN 29547 RNO - ROW 16 DEF EMERGENCY PATH LIGHT WIRE BROKEN. REPLACED WIRE HARNESS FOR ROW 16DEF EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040609000042004060900004NM 2004 6 9 AALA20040615 120040604A3350 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 MIA - LEFT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED LEFT AFT OVERWING EMERGENCY EXIT SIGN BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609000052004060900005NM 2004 6 9 AALA20040616 120040605A3350 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21670AA 25335 MIA - EMERGENCY LIGHTS IN CABIN ON INTERMITTENTLY. REMOVED AND REPLACED CENTER BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040607000022004060700002NM 2004 6 7 04FDEA01605 120040603A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION ON FLOORBEAM AT BS 950 RBL 27.5 WL 208 UPPER FLANGE. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-6 AND FED EX EA 7-5310-55308. 2L73 4F RTA3WE 20040607000082004060700008NM 2004 6 7 04FDEA01562 120040602A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO COMPARTMENT STA 560 WL 155 LBL 35 FLOOR FRAME DENTED. CUT OUT DAMAGE IN FRAME AT BS STA 560 WL 155 LBL 35 AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20040607000152004060700015WP 2004 6 7 04FDEA01570 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINING UNIT CRACKED STA 615 TO 775. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000252004060700025WP 2004 6 7 04FDEA01558 120040601A53127075T6032 PRESSURE BLKHD DOUG DC10 DC1010 3022110WP LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT MLG W/W AFT BULKHEAD IS CORRODED. REMOVED AND REPLACED AFT BULKHEAD SKIN PANEL IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040607000332004060700033WP 2004 6 7 04FDEA01582 120040602A25508002810 RETAINER DOUG DC10 DC1010 3022110WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL RETAINER UNIT CRACKED STA 699-745. REMOVED AND REPLACED RETAINERS IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000352004060700035WP 2004 6 7 04FDEA01584 120040602A5753 PANEL DOUG DC10 DC1010 3022110WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5740-77422 WINGS - INBOARD FLAP, OVERSIZED HOLE IN ROLLER FITTING SUPPORT PANEL ASSY. COMPLIED WITH EA 8-5740-77422 WINGS - FLAP, OVERSIZED HOLE IN ROLLER FITTING SUPPORT PANEL ASSY. 2L73 4F A22WE 20040607000362004060700036WP 2004 6 7 04FDEA01587 120040602A25508063510 ROLLER TRAY DOUG DC10 DC1010 3022110WP CARGO BAY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 BALL MAT IS DAMAGED AT STA 615 TO 775 MCD. REMOVED AND REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000422004060700042WP 2004 6 7 04FDEA01586 120040602A25508046410 LOCK DOUG DC10 DC1010 3022110WP CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 TWO EA 80464-10 LOCK ASSY CORRODED. REMOVED AND REPLACED LOCK ASSY IAW ANCRA MM 25-50-33 AT MAE. 2L73 4F A22WE 20040607000442004060700044WP 2004 6 7 04FDEA01473 120040526A5270 PROXIMITY SENSOR DOUG DC10 DC1010 3022110WP CARGO DOOR FAULTY A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25399FE 48262 ON EXT FINAL TO MEM RECEIVED AN ALERT INDICATING THE MAIN CARGO DOOR WAS OPEN (B-LOOP). DOOR WAS VERIFIED CLOSED BY FIRE/RESCUE PERSONNEL AFTER LANDING. RELEASED FOR SERVICE PER MEL/CDL: 52-40-01-06 CATEGORY: B EXPIRATION: 29MAY04 MEL 52-40-01-06: CARGO DOOR UPPER B ALERT INOP. VERIFY DOOR IS CLOSED AND LOCKED PRIOR TO BLOCK-OUT. REPLACED CARGO DOOR PROX SENSOR IAW MM 52-70-06-2. OPS CHECKS GOOD. 2L73 4F A22WE 20040607000612004060700061NM 2004 6 7 04FDEA01282 120040517A5753ARC4125502 STOP FITTING DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING - OUTBOARD FLAP STOP FITTING FOUND CRACKED. RIGHT WING - OUTBOARD FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL 2 AND SRM 51-35-01 VOL 2. 2L73 4F RTA22WE 20040607000642004060700064NM 2004 6 7 04FDEA01022 120040422A5753ARC198413 SUPPORT BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND OUTBOARD FLAP INBOARD AFT HINGE ACTUATOR ROD END INBOARD HOLE SPOTFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76020 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LEFT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040607000722004060700072EU 2004 6 7 04FDEA01015 120040421A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 A 2 INCH CRACK ON INBOARD FLANGE LEFT NR 2 SEAT TRACK FWD OF FRAME 30, MAIN CABIN. REMOVED DAMAGED SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16. LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINE, PRIMED AND TOP COATED NEW SEAT TRACK SECTION IAW A300-600 SRM 51-20-23. INSTALLED NEW SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. TOP COATED FASTENERS IAW A300-600 SRM 51-20-23. 2L72 4F RTA35EU 20040607000812004060700081WP 2004 6 7 04FDEA01524 120040528A5720ARB09721 RUB STRIP DOUG DC10 DC1010 3022110WP LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT WING FUEL TANK ACCESS RUB STRIP GOUGED AT PANEL 533AT. REMOVED AND REPLACED RUB STRIP IAW SRM 51-31-01AT MAE. 2L73 4F A22WE 20040607000992004060700099NM 2004 6 7 04FDEA01083 120040424A5753ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE, ACTUATOR HOLE NR 8 OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-76029, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040607001022004060700102EU 2004 6 7 04FDEA01549 120040601A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 SEAT TRACK 3R HAS 6 EA AREAS OF CORROSION. 1) 8 INCHES FWD OF FR27. 2) 4 INCHES FWD OF FR27. 3) 6 INCHES AFT OF FR30. 4) 8 INCHES AFT FR32. 5) 10 INCHES AFT OF FR33. 6) 4 INCHES AFT OF FR38.1. REMOVED CORROSION 6 AREAS IAW A300-600 SRM 53-10-16, AREA 3 FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED NEW SEAT TRACK, SPLICE AND INSTALLED NEW SEAT TRACK AND SPLICES IAW A300-600 SRM 53-10-16 FIG 201. 2L72 4F RTA35EU 20040607001032004060700103EU 2004 6 7 04FDEA01550 120040601A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25650FE 726 MAIN CABIN TRACK 3R: 1) A WORN SCALLOP AT FR 24. 2) GOUGES ON TOP OF SCALLOPS AT FR 22. 3) GOUGED SCALLOPS AT FR 20 TO 21. BLENDED AREAS 2 AND 3 IAW A300-600 SRM 51-73-10, WITHIN LIMITS PER SRM 53-10-16. FOR AREA 1 AT FR 24 REF EA 6-5320-78360 FOR REPAIR, TREAT AND TOP COAT ALL REPAIRS IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20040607001082004060700108NM 2004 6 7 04FDEA01068 120040423A5313AGA70481 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 AFT CARGO LONGERON AT STA 1867-1887 RIGHT LONGERON 40 FOUND CRACK. AFT CARGO LONGERON AT STA 1867-1887 RIGHT LONGERON 40 REPAIR CARRIED OUT AS PER SRM 53-10-01 VOL I FIG 2. 2L73 4F RTA22WE 20040607001092004060700109NM 2004 6 7 04FDEA01069 120040423A5313AGA70261 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 AFT CARGO LONGERON AT STA 1847-1867 RIGHT LONGERON 38 FOUND CRACK. AFT CARGO STA 1847-1867 RIGHT LONGERON 38 CRACK REPAIRED AS PER SRM 53-10-00 VOL I. 2L73 4F RTA22WE 20040607001132004060700113NM 2004 6 7 04FDEA01189 120040510A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIG DIA 1.062 INCH, FINAL DIA 1.189 INCH AND REPAIRED AS PER FEDEX EA 1-5750-74315 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040607001352004060700135NM 2004 6 7 SWAA041396 120040516A531365C27314 STRINGER CLIP BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP AT BS 787, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040608000012004060800001NM 2004 6 8 ASAA0440103 120040411A5712654544555 RIB BOEING737 7374Q8 138447QNM WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND WING RIB LOWER CHORD IS CRACKED APPROXIMATELY .5 INCH LONG, CHORD TO SKIN ATTACH TEE AFT OF STRINGER. REPLACED DAMAGED RIB LOWER CHORD. (M) 2L72 4F RTA16WE 20040608000062004060800006NM 2004 6 8 ASAA0440107 120040417A53126516300511 BULKHEAD BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01705AS 29318 GYR - FOUND STATION 178 WEB DAMAGED WL 219, LBL 18.1. REPAIRED DAMAGE IAW ASA EA NR 5310-02343 PG 3 STEP 3. (M) 2L72 4F RTA16WE 20040608000102004060800010NM 2004 6 8 ASAA0440090 120040401A531065465349 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND FORWARD CARGO COMPARTMENT, STATION 520 RBL 3, LOWER FRAME SHEAR TIE 100 PERCENT EXFOLIATED. FABRICATED AND INSTALLED 65-46534-9 SHEAR TIE. (M) 2L72 4F RTA16WE 20040608000112004060800011NM 2004 6 8 ASAA0440097 120040401A5315BAC1518338 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND MAIN DECK FLOORBEAM UPPER T-CAP STATION 360 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE. REPAIRED FLOORBEAM. (M) 2L72 4F RTA16WE 20040608000162004060800016NM 2004 6 8 ASAA0440028 120040204A531565C339481 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND CORROSION ON UPPER T-CAP FLOORBEAM. REPAIRED IAW ASA EA 5310-02310. (M) 2L72 4F RTA16WE 20040608000302004060800030NM 2004 6 8 04FDEA01593 120040603A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP FORWARD INBOARD HINGE, FOUND LOWER MATING SURFACE CORRODED. SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 - 407. ORIGINAL THICKNESS= 0.464, MATERIAL REMOVED= 0.031, REMAINING THICKNESS= 0.433. COMPLIED WITH FEDEX EA 1-5750-76725, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040608000412004060800041NM 2004 6 8 04FDEA01239 120040512A5744ARC050312 HINGE BRACKET DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE FOUND CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED FOUND EXCEEDED LIMITS AS PER CMM 57-44-09 PG 402-407, ORIG DIA 1.187 INCH, FINAL DIA 1.220 INCH, AND REPAIRED AS PER EA 1-5740-75958 - WINGS - RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040608000462004060800046WP 2004 6 8 04FDEA01244 120040512A5350NAS6406U31D THRU BOLT DOUG DC10 DC1010 3022110WP TAIL CONE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 TAIL CONE RIGHT HINGE HAS EXCESSIVE PLAY. REMOVED AND REPLACED TAIL CONE RIGHT HINGE THRU BOLT IAW MM 53-52-00-2 AT MAE. 2L73 4F A22WE 20040608000522004060800052NM 2004 6 8 04FDEA01428 120040524A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01), ON FLOORBEAM LWR FLANGE STA 600 RBL 49 TO 60 WL 201. REMOVED CORROSION ON LOWER FLANGE FLOORBEAM CHORD AT BS 600, RBL 49-60, WL 201. FOUND TO BE OUT OF LIMITS. ACCESSED AREA AND CUT LOWER CHORD FROM RBL 35 TO END OF FLOORBEAM. FABRICATED LOWER CHORD, (2) SUPPORT ANGLES, (2) REINFORCEMENT STRAPS, (4) SHIMS. ALODINED AND PRIMERED. INSTALLED ALL REPAIR PARTS AND FASTENERS THAT WERE REMOVED FOR ACCESS IAW SRM 53-10-1, 51-10-6, 53-10-8, 51-30-2 AND FED EX M/M 51-20-151-7. 2L73 4F RTA3WE 20040608000562004060800056NM 2004 6 8 04FDEA01432 120040524A534065453136 STRINGER CLIP BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CRACKED STRINGER CLIP, STA 950C, STRINGER 3R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3R IAW SRM 51-30-2. 2L73 4F RTA3WE 20040608000752004060800075NM 2004 6 8 SWAA041579 120040604A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER TIE CLIP AT BS 807, STRINGER 18L, CRACKED. REMOVED AND REPLACED STRINGER TIE PER SRM. 2L72 4F RTA16WE 20040608000772004060800077NM 2004 6 8 SWAA041581 120040604A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT R2 DOOR, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040608000812004060800081NM 2004 6 8 SWAA041585 120040604A5311BAC1509100146 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND FRAMES AT BS 770, STRINGER 8L AND STRINGER 12L, CORRODED. REPAIRED FRAME SECTIONS PER EA. 2L72 4F RTA16WE 20040608000832004060800083NM 2004 6 8 UIEA200400088 120040505A5270602EN6016 WARNING SWITCH BOEING747 7472D7B 1384803NM CARGO DOOR OUT OF ADJUST A UIEAIA CABIN DEPRESSURIZATION UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA15526MC 22337 CARGO DOOR LIGHT ANNUNCIATOR LIGHT CAME ON IN FLIGHT AS WELL AS FORWARD CARGO LIGHT ON F/E PANEL. FHB PROCEDURE CARRIED OUT. ADJUSTED DOOR WARNING SWITCH. OPERATED DOOR SEVERAL TIMES, DOOR LIGHTS NORMAL, ALL OFF WHEN DOOR CLOSED MM 52-34-00/501. AIRCRAFT WAS DIVERTED TO DXB/IST. (M) 2L74 4F RTA20WE 20040608000952004060800095NM 2004 6 8 CALA0400499 120040522A5320143A948535 SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2736247 28807 INSPECTION FOUND FORWARD CARGO AFT BULKHEAD PANEL LOWER SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040608000972004060800097NM 2004 6 8 CALA0400501 120040523A5320146A8127 ANGLE BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2736247 28807 INSPECTION FOUND RIGHT Z-ANGLE CORRODED AT STA 767-787. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-60-15 AND 51-40-02. 2L72 4F RTA16WE 20040608001002004060800100WP 2004 6 8 CALA0400504 120040524A531327779223 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND A .25 INCH CRACK IN LONGERON 4L AT STA 160. A LONGERON SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18. 2L72 4F A6WE 20040608001012004060800101WP 2004 6 8 CALA0400505 120040525A5320 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 168.7 AND 200, 14 INCHES INSIDE FORWARD SERVICE DOOR. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2L72 4F A6WE 20040608001042004060800104WP 2004 6 8 CALA0400515 120040528A5230 SKIN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND A 6 INCH CRACK IN FORWARD BAGGAGE BIN DOOR INNER SKIN AT BOTTOM AFT SIDE. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 52-05, FIGURE 26A. 2L72 4F A6WE 20040608001112004060800111NM 2004 6 8 CALA0400494 120040518A551265C27494 SKIN BOEING737 737524 1384721NM HORIZ STAB PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723661 28922 INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN PUNCTURED AT STAB STA 203. THE PUNCTURED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW 55-10-01. 2L72 4F RTA16WE 20040608001202004060800120EU 2004 6 8 MALA040426 120040525A5347 CARGO TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15457XJ 340B457 DURING 4Y/2Y INSPECTION IN LCQ, FS 630.112 CARGO COMPARTMENT CENTER SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05. 2L72 4T RTA52EU 20040608001242004060800124EU 2004 6 8 MALA040423 120040602A36102985A000003 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU BLEED AIR SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15531XJ E2365 NR 2 ENGINE AIR FAULT LIGHT CAME ON AFTER TAKEOFF. AIR RETURN TO MEM. MAINTENANCE REPLACED ISOLATION / PRESSURE REDUCING VALVE FOR NR 2 ENG IAW AVRO AMM 36-11-11. OPS AND LEAK CHECK GOOD. P/N ON 2985A000-003, P/N OFF 2985A000-002, S/N ON 923048-3, S/N OFF 760291-5. 2H74 4F RTA49EU 20040608001252004060800125EU 2004 6 8 MALA040424 120040525A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15457XJ 340B457 DURING 4Y/2Y INSPECTION IN LCQ, FS 300 LEFT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT FS 300 I/B IAW MESABA EO S53060. A/C RELEASE DATE 6/4/05. 2L72 4T RTA52EU 20040608001362004060800136EU 2004 6 8 USAA040220 120040512A5320 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW 0896 BEAM, 3.0 INCH X 3.0 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 68, BI-Y1292, Z240. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001472004060800147NM 2004 6 8 USAA040208 120040426A5315 FLOORBEAM BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US68850 23898 FLOORBEAM 16 INCHES X 2 INCH AREA, CORROSION; NO LEVEL/ TASK AFT CABIN FLOOR STA 1480, LBL 27-43. INSTALLED REPAIR IAW SRM. 2L72 4F4 FRTA1NM E13NE 20040608001512004060800151EU 2004 6 8 USAA040216 120040512A5321 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 FLOOR PANEL, 1.2 INCH CRACK, MAIN CABIN FLOOR PANEL 261 HG. FABRICATED FLOOR PANEL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001582004060800158EU 2004 6 8 USAA040223 120040512A5320D5347209001000 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 BEAM, 1.0 INCH X 1.0 INCH X 0.025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; Z240, FR66 BLY1292. REMOVED AND REPLACED IAW 53-00-14, FIG 102. 2L72 4F4 FRTA28NM E2GL 20040608001642004060800164SO 2004 6 8 C2XA04SH327 120040527A521014524131009 BRACKET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV-DURING C CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040608001662004060800166SO 2004 6 8 CHQA000456 120040118A3397 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A CHQAK NONE O OTHER ININSP/MAINT 1 GL11261 145144 NR 3 PROXIMITY STRIP WIRES BROKEN. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB-145 AMM II CHAPTER 33-50-12. 2L72 4T RTT00011AT 20040609000062004060900006NM 2004 6 9 AALA20040617 120040605A3350P4010051112 MODULE BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21193AN 32387 MIA - EMERGENCY LIGHTS FOR ROWS 9 THROUGH 15 INOPERATIVE. REMOVED AND REPLACED MODULE AND BATTERY FOR EMERGENCY LIGHTS FOR ROWS 9 THROUGH 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609000092004060900009EU 2004 6 9 MALA040401 120040502A3010MS2740017 RELAY BAC 146 AVRO146RJ85A1500097EU ANTI-ICE SYSTEM DEFECTIVE A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15502XJ E2307 BREAKER F26 POPS WHEN OUTER WING ANTI-ICE VALVE IS SELECTED. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED RELAYS HH10 AND HH8 P/N MS27400-17 IAW AMM 30-11-00-1. FOUND COFFEE ALL OVER RELAY HH10. OP CHECKS GOOD. 2H74 4F RTA49EU 20040609000102004060900010EU 2004 6 9 MALA040413 120040523A302044730501 CONTROL MODULE SAAB SF340 340B 7860101EU DEICE SYSTEM DEFECTIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15449XJ 340B449 THE RT INTAKE HEAT FAILED IN FLIGHT. INFLIGHT, RIGHT INTAKE CAUTION LIGHT ILLUMINATED, IT WENT OUT AFTER 20 SECONDS AND THEN ILLUMINATED AGAIN EVERY 3-5 MINUTES. DIVERTED TO CWA. MAINTENANCE REMOVED AND REPLACED DEICE CONTROL MODULE P/N 44730-501, S/N ON A00112, S/N OFF A00031, OPS CHECK GOOD. WORK DONE IAW SAAB MM. 2L72 4T RTA52EU 20040609000112004060900011EU 2004 6 9 MALA040412 120040523A3020NH24668153 DUCT SAAB SF340 340B 7860101EU RT INTAKE FAILED A MALAA UNSCHED LANDING O OTHER UKUNKNOWN 1 GL15410XJ 340B410 DIVERTED TO CWA AFTER THE RIGHT INTAKE HEAT FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RIGHT DUCT P/N NH24668-153, S/N ON L219890, S/N OFF L219863. 2L72 4T RTA52EU 20040609000122004060900012EU 2004 6 9 MALA040414 120040524A3230 STRIKER BAC 146 AVRO146RJ85A1500097EU NLG OUT OF ADJUST A MALAO OTHER O OTHER DEDESCENT 1 GL15513XJ E2329 THE NOSE GEAR WOULD NOT EXTEND FOR LANDING AT JAN. MAINTENANCE T/S FOUND NOSE GEAR UPLOCK BRACKET AT FAULT. REMOVED 1 SHIM FROM BRACKET STRIKER PLATE. ALL CHECKS GOOD IAW AMM32-20-27 AND OPS CHECK IAW AMM32-30-00. NO FURTHER ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2H74 4F RTA49EU 20040609000132004060900013EU 2004 6 9 04FDEA01111 120040428A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE MAIN CABIN FLOOR SUPPORT FROM FR14 TO 15A JUST I/B OF Y1456 IS CORRODED. REMOVED FAB AND INSTALLED FLOOR SUPPORT IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20040609000152004060900015WP 2004 6 9 04FDEA01530 120040529A5751NRC6041505 SKIN DOUG DC10 DC1010F 3022111WP LT AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 LEFT WING OUTBOARD AILERON LOWER SKIN BULGED /CORRODED AT CENTER HINGED POINT. REMOVED AND REPLACED LEFT OUTBOARD AILERON IAW DC10 AMM 27-10-02-4. AILERON RIG TO BE ACCOMPLISHED ON FEDEX ROUTINE OPERATION E 8-5710-7-5005A PT 1. 2L73 4F A22WE 20040609000162004060900016WP 2004 6 9 04FDEA01531 120040529A5751NRC6041505 SKIN DOUG DC10 DC1010F 3022111WP LT AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 LEFT WING OUTBOARD AILERON LOWER SKIN BULGED /CORRODED AT CENTER HINGED POINT. REMOVED AND REPLACED LEFT OUTBOARD AILERON IAW DC10 AMM 27-10-02-4. AILERON RIG TO BE ACCOMPLISHED ON FEDEX ROUTINE OPERATION E 8-5710-7-5005A PT 1. 2L73 4F A22WE 20040609000172004060900017WP 2004 6 9 04FDEA01532 120040529A5310ADA00553 DOOR FRAME DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD CARGO DOOR CUTOUT, FORWARD LOWER CORNER WEB IS CORRODED FS 895, RBL 52. REMOVED DAMAGED FRAME AREA IAW DC10 SRM 53-50-00 VOL 1. FABRICATED SPLICE PLATE AND INSTALLED REPAIR DOUBLERS AND SPLICE PLATE IAW DC10 SRM 53-50-00 VOL 2. 2L73 4F A22WE 20040609000182004060900018WP 2004 6 9 04FDEA01533 120040529A5315 FLOORBEAM DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25054 47808 T-CAP CORRODED IN FORWARD PIT AT FS 909 RBL 30. REMOVED DAMAGED T-CAP, LOCATED DRILLED AND SIZED NEW EXTRUSION IAW DC10 SRM 51-31-01 AND INSTALLED NEW T-CAP IAW DC10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040609000202004060900020WP 2004 6 9 04FDEA01537 120040529A5311 FRAME DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD PIT AT APPROX FS 980 AT LONGERON 52 FRAME HAS CORROSION. REMOVED CORRODED AREA, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC10 SRM 53-00-01 FIG 8 VOL 1 AND 52-21-01 VOL 2 AND 51-33-01 VOL 2. 2L73 4F A22WE 20040609000232004060900023WP 2004 6 9 04FDEA01536 120040529A2550 ROLLER TRAY DOUG DC10 DC1010F 3022111WP CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 LOWER FORWARD CARGO COMPARTMENT, CORROSION ON BOTTOM SIDE OF ROLLER TRAY AT FS 875 AT LBL 28. CORROSION FOUND TO BE INTERGRANULAR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW DC10 SRM 53-42-01 VOL 3. 2L73 4F A22WE 20040609000242004060900024NM 2004 6 9 04FDEA01427 120040524A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-01), ON FLOORBEAM BS 344 LBL 33 TO 60 WL 208 AROUND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM, BS 344. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, RBL 65 - LBL 65, WL 208. ALL WORK DONE PER SRM 53-10-8 FIG 9, 51-10-2, 51-30-2, 51-30-5, 51-30-8. 2L73 4F RTA3WE 20040609000252004060900025WP 2004 6 9 04FDEA01397 120040522A5315 FLOORBEAM DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 T-CAP CORRODED IN FORWARD PIT AT STATION 909 RBL 30. REMOVED AND REPLACED T-CAP IAW DC10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040609000262004060900026WP 2004 6 9 04FDEA01398 120040522A5310ADA00553 DOOR FRAME DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD CARGO DOOR CUTOUT, AFT LOWER CORNER, WEB CORRODED, APPROX FS 1002, RBL 52. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. INSTALLED NEW FRAME SECTION AND REPAIR DOUBLERS AND ANGLE SPLICES IAW DC10 SRM 53-13-01 VOL 3. 2L73 4F A22WE 20040609000312004060900031WP 2004 6 9 04FDEA01403 120040522A3411 STATIC PORT DOUG DC10 DC1010F 3022111WP PITOT/STATIC SYSOUT OF ADJUST A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 RIGHT HAND ALTERNATE STATIC PORT FAILS HIGH/LOW MISMATCH CHECK AT AFT SIDE OF PORT. SKIN HAS .005 INCH DIFFERENCE IN HEIGHT (.002 INCH MAX ALLOWED). ADJUSTED RIGHT HAND STATIC PORT IAW DC10 MM 34-11-01-2, PARAGRAPH B (4). ALL TOLERANCES ARE WITHIN SPECIFIED LIMITS WITH TOP .001, BOTTON .003, FORE .001 AND AFT AT .001 IAW DC10 MM 34-11-01-2. 2L73 4F A22WE 20040609000332004060900033WP 2004 6 9 04FDEA01405 120040522A5347 SEAT TRACK DOUG DC10 DC1010F 3022111WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 MAIN CARGO APPROX STATION 910 SEAT TRACK AT RBL 27 IS CRACKED. REMOVED CRACKED SEAT TRACK SECTION, LOCATED AND DRILLED REPAIR SECTION AND INSTALLED SEAT TRACK REPAIR IAW DC10-10 SRM 53-70-00 VOL 1 AND DC10-10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040609000342004060900034WP 2004 6 9 04FDEA01406 120040522A5311 FRAME DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD PIT APPROX STATION 980 LONGERON 52 FRAME HAS CORROSION. REMOVE CORROSION IAW DC10 SRM 51-21-01 VOL 2, ORIGINAL THICKNESS .071 IAW DC10 SRM 53-13-01 FIG 8 VOL 3. MATERIAL REMOVED .032 INCH, MATERIAL REMAINING .039 INCH. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW DC10 SRM 53-00-01, VOL 1, FIG 8 AND DC10 SRM 51-33-01 VOL 2. 2L73 4F A22WE 20040609000352004060900035WP 2004 6 9 04FDEA01407 120040522A5320 CUSP WEB DOUG DC10 DC1010F 3022111WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 CENTER ACCESSORY COMPARTMENT UPPER RIGHT HAND CUSP WEB HAS CRACKS AROUND LIGHTING HOLES BETWEEN FS 1139 AND FS 1156. FABRICATED REPAIR DOUBLER AND INSTALLED WEB REPAIR AND DOUBLERS IAW DC10 SRM 51-35-01 VOL 2. 2L73 4F A22WE 20040609000372004060900037WP 2004 6 9 04FDEA01409 120040522A5347 SEAT TRACK DOUG DC10 DC1010F 3022111WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 MAIN CARGO AREA FS 925 SEAT TRACK RBL 47 EDGE IS CRACKED. REMOVED CRACKED SEAT TRACK SECTION, FABRICATED REPAIR PARTS, AND SLICE PLATES IAW DC10 SRM 53-70-00 VOL 1 AND INSTALLED IAW DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040609000392004060900039WP 2004 6 9 04FDEA01411 120040522A5310SR10530048177 DOOR FRAME DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD CARGO PIT AT DOOR CUTOUT STATION 1002 CHORD FOUND CORRODED INSIDE TORQUE BOX. REMOVED CORROSION IAW DC10 SRM 53-00-01 VOL 2, FOUND TO BE OUT OF LIMITS, FABRICATED ANGLE IAW DC10 SRM 51-21-01 VOL 1 AND 53-50-00 VOL 2. INSTALLED TWO STRAPS AND INTERCOSTALS AND BRACKETS REMOVED TO FACILITATE, INSTALLED SR 10530048-17 AND -7 PARTS IAW DC10 53-50-00 VOL 1. 2L73 4F A22WE 20040609000402004060900040WP 2004 6 9 AALA20040618 120040605A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21595AA 53285 DFW - B2-28 BATTERY PACK INOPERATIVE. REMOVED AND REPLACED B2-28 BATTERY PACK PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000412004060900041WP 2004 6 9 AALA20040619 120040605A3397 WIRE DOUG DC9 DC983 3022083WP A/C BAY DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21595AA 53285 DFW - AFT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING FROM TAIL CONE LIGHT TO AFT CATWALK EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000432004060900043WP 2004 6 9 AALA20040621 120040606A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21249AA 49269 DFW - AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED B5-10 BATTERY PACK FOR AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000442004060900044WP 2004 6 9 AALA20040622 120040606A33500201720003 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21558AA 53088 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000462004060900046NM 2004 6 9 AALA20040562 120040516A3350 SOCKET BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21343AN 33082 SFO - EMERGENCY EXIT LIGHT AT R4 DOOR INOPERATIVE. FOUND BULB HOLDER LOOSE. TIGHTENED BULB HOLDER FOR EMERGENCY EXIT LIGHT AT R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609000472004060900047NM 2004 6 9 AALA20040561 120040515A3397 WIRE BOEING777 777223 1385213NM CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21786AN 30250 DFW - AFT COACH SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPAIRED SHORT IN WIRING AT SEAT 31G FOR AFT COACH SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040609000482004060900048NM 2004 6 9 AALA20040567 120040517A3350P4010051112 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21691AA 25697 LAX - EMERGENCY LIGHTS FROM 27D TO BACK OF AIRCRAFT INOPERATIVE. REPAIRED SHORT NEAR L4 DOOR LIGHT AT L759 AND REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS FROM 27D TO BACK OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609000492004060900049NM 2004 6 9 AALA20040563 120040516A3350 CONNECTOR BOEING757 757223 1384957NM CABIN NOT SEATED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21622AA 24580 SFO - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. RESEATED CONNECTOR FOR INSEAT EMERGENCY ESCAPE PATH LIGHT AT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609000512004060900051WP 2004 6 9 AALA20040568 120040517A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21459AA 49564 LAX - EMERGENCY LIGHTS AT AFT SERVICE DOOR DROP CEILING PANEL AT STATION 1133 AND CEILING LIGHTS AT STATIONS 1209 RIGHT AND 1152 LEFT INOPERATIVE. REPLACED BATTERY PACK B5107 AT STATION 1190 FOR EMERGENCY LIGHTS AT AFT SERVICE DOOR DROP CEILING PANEL AT STATION 1133 AND CEILING LIGHTS AT STATIONS 1209 RIGHT AND 1152 LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000522004060900052 2004 6 9 AALA20040564 420040516A2565D29982125 SLIDE DOUG DC9 DC982 3022082WP CABIN UNSERVICEABLE A AALAK NONE O OTHER ININSP/MAINT 1 SW21232AA 49179 PHX - FORWARD SERVICE DOOR SLIDE PRESSURE BELOW GREEN ARC. REPLACED SLIDE AT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000552004060900055WP 2004 6 9 AALA20040570 120040519A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219622A 53593 DFW - AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000562004060900056NM 2004 6 9 AALA20040577 120040510A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 AFW - FLOORBEAM AT STATION 325 AT RBL 86 (VERY OUTBOARD END) BROKEN OFF, AREA IS 1 INCH SQUARE. SMOOTHED AND BLENDED BROKEN EDGE OF CHORD. TWO REPAIR ANGLES MACHINED, EXTRUSION INSTALLED. ANGLES ATTACHED WITH FLUSH HI-LOKS (UPPER FASTENER) AND PROTRUDING HI-LOKS IN LOWER HOLE LOCATIONS. EXISTING FASTENER LOCATIONS REPLACED WITH SAME TYPE AND SIZE AS ORIGINAL. 2L72 4F RTA1NM 20040609000592004060900059NM 2004 6 9 AALA20040574 120040510A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 AFW - FLOORBEAM AT STATION 347 AT G1 GALLEY AREA HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 2 INCH BY 1 INCH AND A DEPTH OF 0.55 INCHES. REMOVED CORROSION AND VERIFIED FABRICATED REPAIR STRAP, ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS AND REPAIR STRAP WITH PRIMER. FILLED BLENDS WITH BMS 595 SEALANT AND INSTALLED REPAIR STRAP WITH SEALANT PROSEAL 870 AND FASTENERS. 2L72 4F RTA1NM 20040609000602004060900060NM 2004 6 9 AALA20040573 120040506A5330 SKIN BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21352AA 24033 AFW - FUSELAGE SKIN AT STATION 1582 AT 539L ON THE FORWARD SIDE OF PRODUCTION SPLICE HAS CORROSION. THE AREA OF CORROSION IS 8 INCHES BY 3 AND .75 INCH AND THE CRACK LENGTH IS APPROXIMATELY 0.75 INCH. REMOVED AREA OF SKIN DAMAGE PER SRM 53-00-01 AND REPAIRED USING STACKED DOUBLERS PER THE SRM. REPAIR FASTENERS IN NEW LOCATIONS ARE .1875 INCH STAINLESS SHEAR HEAD HI-LOKS. 2L72 4F RTA1NM 20040609000622004060900062WP 2004 6 9 AALA20040580 120040520A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW2114551 53033 DFW - ENTRY AISLE AND FORWARD GALLEY CEILING EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK AT B523 FOR OVERHEAD ENTRY AISLE AND FORWARD GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000652004060900065WP 2004 6 9 AALA20040579 120040520A3397 CABLE DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21513AA 49890 MIA - SEAT EMERGENCY LIGHT AT 29DEF INOPERATIVE. FOUND CABLE UNPLUGGED. PLUGGED CABLE IN FOR SEAT EMERGENCY LIGHT AT 29DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000672004060900067WP 2004 6 9 AALA20040581 120040520A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114551 53033 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000682004060900068WP 2004 6 9 AALA20040595 120040527A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21457AA 49562 DFW - EMERGENCY LIGHTS IN CEILING AT ROW 8 ARE INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS IN CEILING AT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000732004060900073WP 2004 6 9 AALA20040604 120040531A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW213515 49892 DFW - EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FLIGHT DECK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000742004060900074WP 2004 6 9 AALA20040605 120040531A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW213515 49892 DFW - LEFT AND RIGHT HAND EMERGENCY EXIT SIGN AT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR LEFT AND RIGHT HAND EMERGENCY EXIT SIGN AT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000762004060900076WP 2004 6 9 AALA20040608 120040601A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21563AA 49345 LGA - EMERGENCY PATH LIGHTING AT ROW 20D TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY PATH LIGHTING AT ROW 20D TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000772004060900077WP 2004 6 9 AALA20040597 120040529A3397 WIRE DOUG DC9 DC982 3022082WP CABIN PINCHED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 DFW - SEAT MOUNTED EMERGENCY LIGHT FROM EXIT ROW FORWARD INOPERATIVE. FOUND PINCHED WIRE AT ROW 17. REPAIRED PINCHED WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000792004060900079NM 2004 6 9 AALA20040624 120040607A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21923AN 29524 DFW - LIGHT ASSEMBLY IN LEFT AFT EMERGENCY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IN LEFT AFT EMERGENCY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040609000822004060900082WP 2004 6 9 AALA20040603 120040531A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21976TW 53626 SEA - OVERHEAD EMERGENCY LIGHTS AT FORWARD LIFE RAFT BIN INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR OVERHEAD EMERGENCY LIGHTS AT FORWARD LIFE RAFT BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000832004060900083WP 2004 6 9 AALA20040606 120040531A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 LGA - EMERGENCY LIGHT AT FORWARD AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000852004060900085NM 2004 6 9 04FDEA01604 120040603A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 1070, LBL 25 TO RBL 60, WL 200 LOWER FLOORBEAM FWD SIDE CORRODED. REPAIRED FLOOR BEAM BS 1070 PER FED EX EA 7-5310-55306. 2L73 4F RTA3WE 20040609000862004060900086NM 2004 6 9 XNOA1187 120040525A2611 WARNING SYSTEM BOEING727 727227 1384078NM COCKPIT ACTIVATED A XN0AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL2373751 21247 MAIN CARGO AND LOWER CARGO WARNING IN FLIGHT WITH LIGHT AND BELL. 2L73 4F A3WE 20040609000872004060900087EU 2004 6 9 184591 120040529A3220 LANDING GEAR SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE NLG VIBRATION A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL17152CQ ON TAKE OFF ROLL OUT ENCOUNTERED EXCESSIVE NOSE WHEEL SHIMMY AT ABOUT 50 KTS AND PILOT ABORTED TAKE OFF. 2L72 4T4 TRTA52EU E8NE 20040609000892004060900089SO 2004 6 9 SWIA200413346 120040520A27503069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07196SW 120151 (CONTROL FAULT) ILLUMINATED ON FLAP PANEL AND MAP. REPLACED FLAP ANNUNCIATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040609000902004060900090EA 2004 6 9 SWIA200413347 120040522A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT MLG FAULTY A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07594SW 7285 INFLIGHT RECEIVED (MLG OVHT FAIL) MESSAGE. REPLACED LT GEAR FIRE LOOP AND WIRE HARNESS, MLG OVHT OPS CHECKS GOOD. P/N: 244-03615. 2L72 4F4 FRTA21EA E15NE 20040609000912004060900091EA 2004 6 9 SWIA200413348 120040522A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE COCKPIT DIRTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07427SW 7497 IN FLIGHT (STAB) AND (MACH) TRIM CAUTION MESSAGES ILLUMINATED. CLEANED CAPTAIN'S STAB TRIM DISCONNECT SWITCH. OPS CKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040609000942004060900094EU 2004 6 9 RAIA00405010 120040513A261251228532 CONTROL UNIT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP FIRE DETECTION FAULTY A RAIAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 CE03560HK 41076 5559-STL- RT ENGINE FIRE INDICATION UPON DESCENT TO SGF. MAINTENANCE REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT. 2L72 4T3 TRTA41NM E2WE 20040609000952004060900095SO 2004 6 9 RAIA00405011 120040515A3240 CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL BRAKE SYSTEM MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03818HK 145059 5675-STL- OB BRAKE INOPERATIVE INDICATION. MAINTENANCE RERACKED BRAKE CONTROL UNIT. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040609000962004060900096NM 2004 6 9 ASAA01100MM 120040124A3350BACC18Z2R CIRCUIT BREAKER BOEING737 7372X6C 1384552NM BREAKER PANEL INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 DURING INSPECTION, FOUND THE EMERGENCY FLOORPATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION.RESET THE EMERGENCY FLOORPATH LIGHTING CIRCUIT BREAKER THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040609001002004060900100NM 2004 6 9 QXEA200400326 120040516A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE PANEL STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX- FOUR NUTPLATES ON PANEL 121AL ARE STRIPPED OUT. REMOVED AND REPLACED NUTPLATE IAW DHC-8 SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040609001012004060900101NM 2004 6 9 374PA0008 120040517A5320 ANGLE BOEING737 73736M 138443BNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 CORROSION ON LT TRANSITION ANGLE IN AFT CARGO BIN FROM BS 727E TO AFT END. FABRICATED AND INSTALLED REPLACEMENT TRANSITION ANGLE IAW SRM 53-60-53. 2L72 4F4 FRTA16WE E2GL 20040609001032004060900103EU 2004 6 9 MALA040418 120040524A2450 RELAY SAAB SF340 SF340A 7850100EU GE CT7TP CT79B 30030NE AC POWER SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15110XJ 340A110 AFTER DEPARTURE FROM MSP, CREW REPORTED RT AVIONICS FAILURE. AIR RETURN TO MSP. MAINTENANCE REPLACED RELAY 4PP RT AVIONICS BUSS. CHECKS GOOD IAW CHAP 24. 2L72 4T4 TRTA52EU E8NE 20040609001052004060900105SO 2004 6 9 LR7A04061 120040526A1430 RIVET LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE LOOSE A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 686 4606 DURING SCHEDULED B3 INSPECTION IAW SB 382-53-42 FOUND APPROX 400 EA LOOSE FASTENERS AT FS 245 AND FS 345E FUSELAGE SKIN. REPLACED RIVETS IAW SRM SMP 583 51-70 AND SB 382-53-42. NR 02SB382-53-42. 2H74 4T4 T A1SO E282 20040609001092004060900109WP 2004 6 9 UPS04842424 120040507A53115764343U507 FRAME DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 STATION 1120 FRAME CAP IS CORRODED BEYOND LIMITS AT LONG 36. REMOVED AND REPLACED FRAME CAP IAW DWG 5764343 AND REPAIRED FRAME IAW DWG DC8-53A-010, EO DC8-5310-11728-A, SRM 51-1-20D, 51-1-21 2L74 4F4 FRT4A25 E2GL 20040609001122004060900112NM 2004 6 9 DHL2004741005 120040528A3231 DOOR BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE NLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01741DH 21931 ON CLIMB OUT AT 330 KIAS A RATTLING SOUND CAME FROM THE NOSE GEAR AREA ACCOMPANIED BY RED (DOORS) LIGHT ON F/O'S PANEL AND (NOSE GEAR DOOR) LIGHT ON S/O'S PANEL. LIGHTS CYCLED ON AND OFF RAPIDLY IN SYNCHRONIZATION WITH THE BANGING SOUND. CREW PERFORMED THE (LANDING GEAR OR DOOR WILL NOT STAY UP WITH GEAR LEVER OFF) ABNORMAL PROCEDURE AND ABNORMAL INDICATIONS CEASED. ADJUSTED NOSE GEAR WHEEL WELL DOORS IAW BMM REF 32-22-01, OPS CHECKED GOOD ON GROUND. 2L73 4F4 FRTA3WE E2EA 20040609001132004060900113NM 2004 6 9 DHL2004750042 120040530A2613 WARNING SYSTEM BOEING727 7272M7 138407SNM PWA JT8 JT8D* NE COCKPIT MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01750DH 21951 ENGINE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED MOMENTARILY AFTER T/O. LIGHT EXTINGUISHED BEFORE ABNORMAL PROCEDURE WAS BEGUN. INSPECTED AND RAN NR 3 IAW JRH 5.2 WITH NO DEFECTS NOTED 26-14-00. 2L73 4F4 F A3WE E2EA 20040609001152004060900115NM 2004 6 9 DL73S040462 120040525A3397276005 WIRE BOEING737 737232 1384475NM PWA JT8 JT8D* NE CABIN PINCHED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27315DL 23087 ROW 11-16 EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE PINCHED UNDER FLOOR TRACK COVER, REPLACED FUSE IN POWER PACK AND REPAIRED WIRE UNDER SEAT TRACK COVER. 2L72 4F4 FRTA16WE E2EA 20040609001172004060900117NM 2004 6 9 DL738040464 120040526A5753113A21123 SPAR BOEING737 737832 13844CFNM GE CFM56 CFM56* 13802NE T/E FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27390DA 30536 RT IB MAIN FLAP FRONT SPAR LOWER CHORD FOUND TO BE DAMAGED. DAMAGE WAS LOCATED BETWEEN 26 INCHES AND 34 INCHES FROM THE IB END OF SPAR. DAMAGE WAS REMOVED AND REPAIR INSTRUCTION ISSUED IAW ERA 090294-14. 2L72 4F4 FRTA16WE E2GL 20040609001212004060900121NM 2004 6 9 DL757040468 120040524A5330141N33131 SKIN BOEING757 757232 1384965NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27603DL 22810 FUSELAGE SKIN ASSY L1 DOOR CUTOUT UPPER FWD CORNER : CRACK REPAIR, INSPECTION OF THE FUSELAGE SKIN AT THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT REVEALED A CRACK. THE CRACK IS TYPICAL OF AD 2004-09-32. THE CRACK WAS CUTOUT OF THE SKIN AND UNDERLYING BEARSTRAP. THE CUTOUT WAS REPAIRED WITH THREE EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 090671-14AD. 2L72 4F RTA2NM 20040609001232004060900123EA 2004 6 9 COMA0460344 120040529A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN LOOSE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01494CA 7765 EMERGENCY FLOOR PATH LIGHTING, ROW 8 AFT, IS INOPERATIVE. SECURED LOOSE CONNECTION. 2L72 4F4 FRTA21EA E15NE 20040609001242004060900124EA 2004 6 9 COMA0460345 120040531A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING MALFUNCTIONED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01983CA 7169 FLIGHT 5746 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20040609001262004060900126SO 2004 6 9 CHQA000457 120040208A3397 WIRE EMB 145 EMB145LR 3260212SO CONT IO360 IO360* 17025CE CABIN EXPOSED A CHQAK NONE O OTHER ININSP/MAINT 1 GL11262 145168 PROXIMITY STRIP HAS EXPOSED WIRES ON CONNECTOR AT261BF. REMOVED AND REPLACED PROXIMITY STRIP LIGHT IAW EMB 145 AMM 33-50-08-4. 2L72 4T3 ORTT00011ATE1CE 20040609001282004060900128SO 2004 6 9 CHQA000445 120040210A3350 LIGHT EMB 145 EMB145LR 3260212SO CONT E185 E185* 17014SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11273 145331 EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECK GOOD IAW EMB 145 AMM 33-25-01. 2L72 4T3 ORTT00011ATE246 20040609001292004060900129SO 2004 6 9 C2XA04SH330 120040529A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040609001302004060900130SO 2004 6 9 C2XA04SH331 120040529A532014528737001 STIFFENER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040609001312004060900131SO 2004 6 9 C2XA04SH292 120040518A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 AND EC 5310-01270. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040609001322004060900132EU 2004 6 9 022001A 120040526A2611 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE ILLUMINATED A UHLAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL17152CQ 152CQ 300 FLIGHT 4644 PIT-BUF. DURING CRUISE AT 17K IFR ON TOP. THE RT ENGINE FIRE WARNING ON CWP ILLUMINATED ALONG WITH MASTER WARNING AND ASSOCIATED FIRE HANDLE ILLUMINATION. CREW FOLLOWED QRH AND PULLED RH FIRE HANDLE. THE CREW DID NOT NEED TO FIRE THE BOTTLE AS THE LIGHTS EXTINGUISHED ONCE THE HANDLE WAS PULLED. CREW DECLARED EMERGENCY SINGLE ENGINE LANDING. A/C LANDED SAFELY. TAKEN OUT OF SERVICE 5-26-04 AT 1805 LT. 2L72 4T4 TRTA52EU E8NE6 20040609001332004060900133SO 2004 6 9 C2XA04SH294 120040518A716014575183003 SKIN EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 INTAKE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040609001472004060900147WP 2004 6 9 AALA20040611 120040603A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21409AA 49320 DFW - EMERGENCY LIGHTS ABOVE SEAT 20D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001482004060900148NM 2004 6 9 AALA20040609 120040602A3397 WIRE BOEING757 757223 1384957NM CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21694AN 26974 BOS - EMERGENCY LIGHTS FROM L2 AND R2 TO SEAT ROW 15 INOPERATIVE. REPAIRED SHORTED WIRE AT SEAT 15DEF FOR EMERGENCY LIGHTS FROM L2 AND R2 TO SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609001502004060900150NM 2004 6 9 AALA20040584 120040523A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21692AA 26972 LAX - EMERGENCY LIGHTS AT SEAT ROWS 16D THROUGH 25D AND EMERGENCY EXIT LIGHT OVER RIGHT AND LEFT HAND WING INOPERATIVE. REPLACED BATTERY PACK M10953 FOR EMERGENCY LIGHTS AT SEAT ROWS 16D THROUGH 25D AND EMERGENCY EXIT LIGHTS OVER RIGHT AND LEFT HAND WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609001512004060900151NM 2004 6 9 AALA20040586 120040522A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21352AA 24033 CDG - EMERGENCY EXIT SIGN AT 4L AND 4R INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT 4L AND 4R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040607001062004060700106WP 2004 6 7 04FDEA01553 120040601A5320ACA7561 PLATE DOUG DC10 DC1010 3022110WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 MAIN CARGO DOOR CUTOUT AFT JAMB HAS A GOUGED SCUFF PLATE. REMOVED AND REPLACED SCUFF PLATE IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040607001072004060700107NM 2004 6 7 04FDEA01005 120040418A5753ARB0029509N STRAP DOUG MD11 MD11 3023602NM T/E FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 RIGHT WING - OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACK FOUND ON LOWER HOLE AT 6 O'CLOCK POSITION FORWARD FACE. RIGHT WING - OUTBOARD FLAP INBOARD HINGE TENSION STRAP SUPPORT CRACK LOWER HOLE REPAIRED AS PER E 1-5750-7-5004 REV 1 PART 2. WINGS TRAILING EDGE DEVICES INSPECT/REPLACE OUTBOARD FLAP INBOARD TENSION STRAP SUPPORTS. 2L73 4F RTA22WE 20040607001172004060700117NM 2004 6 7 SWAA041443 120040520A256065C19901 CABLE BOEING737 7372H4 138448CNM L2 DOOR MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F A16WE 20040607001182004060700118NM 2004 6 7 SWAA041444 120040520A5523183A8410 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C1 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RIGHT ELEVATOR HINGE BUSHING PER MM. 2L72 4F RTA16WE 20040607001242004060700124NM 2004 6 7 SWAA041399 120040516A53306545774 DOUBLER BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE DOUBLER AT BS 727D, BL 0, CORRODED. REMOVED AND REPLACED DOUBLER PER SRM. 2L72 4F RTA16WE 20040607001382004060700138WP 2004 6 7 GTIA040252 120040224A5320 CLIP DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 FTW - FOUND MID PIT JAM BEAM FORWARD END CLIP CORRODED AT FS 598 AROUND FASTENER. FABRICATED MID PIT JAM BEAM FORWARD END CLIP. (M) 2L72 4F A6WE 20040607001392004060700139WP 2004 6 7 GTIA040270 120040213A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 FTW - FOUND CORROSION AFT CARGO DOOR LOWER DOOR JAMB FS 1155-1211. REMOVED JAMB BEAR. DRILLED AND LOCATED NEW JAMB BEAM. INSTALLED AFT CARGO PIT JAMB. (M) 2L72 4F RTA6WE 20040608000142004060800014NM 2004 6 8 ASAA0440095 120040401A532065C161216 ATTACH FITTING BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 GYR - FOUND ATTACH FITTING CORRODED. REPLACED ATTACH FITTING. (M) 2L72 4F RTA16WE 20040608000192004060800019NM 2004 6 8 ASAA0440031 120040204A5315BAC14902734 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND FLOORBEAM HAS CORROSION AT STATION 294.5 TOP AND BOTTOM SIDES. REPAIRED IAW SRM 53-10-51 FIG 205. (M) 2L72 4F RTA16WE 20040608000342004060800034NM 2004 6 8 04FDEA01597 120040603A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP FORWARD OUTBOARD HINGE, FOUND INBOARD ACTUATOR HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 PG. 402-407 ORIG. DIAM.:1.187 FINAL DIAM.: 1.222. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76724 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040615000622004061500062NM 2004 6 15 ASAA0410218 120040426A53476554968523 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND DURING C-CHECK, SEAT TRACK AT STATION 480-400, RBL 62 IS NICKED AND WORN. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW 51-30-5. (M) 2L72 4F A16WE 20040608000392004060800039NM 2004 6 8 04FDEA01603 120040603A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 BS 990 FRAME LT PREVIOUS REPAIR CRACKED ON BOTTOM. FOUND DAMAGE TO BS 990 FRAME, STR 24 LT TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 51-40-3 AND FED EX EA 7-5310-55307. 2L73 4F RTA3WE 20040608000482004060800048WP 2004 6 8 04FDEA01246 120040512A5320ANB720389 STIFFENER DOUG DC10 DC1010 3022110WP RT MLG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 STA 1450 RIGHT MAIN LANDING GEAR W/W AFT OUTBOARD WEB VERTICAL STIFFENER LOWER END CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040608000532004060800053WP 2004 6 8 04FDEA01429 120040524A5753ARC1991 HINGE DOUG DC10 DC1010 3022110WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-77414, WING - OUTBOARD FLAP, REWORK OF POSITION INDICATION HOLE IN ARC1991 HINGE. COMPLIED WITH EA 8-5750-77414. 2L73 4F A22WE 20040608000742004060800074NM 2004 6 8 SWAA041578 120040604A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 813, STRINGER18L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040608000892004060800089NM 2004 6 8 CALA0400506 120040430A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2754241 28953 THE INTERIOR AND EXTERIOR LIGHTS ON L-1 DOOR WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06 AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040608000922004060800092NM 2004 6 8 CALA0400509 120040526A3350D71702030 CHARGER BOEING767 767424ER 1385270NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2777066 29461 THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT STA 401, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 206. 2L72 4F RTA1NM 20040608000962004060800096NM 2004 6 8 CALA0400500 120040522A5320143A948535 SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2736247 28807 INSPECTION FOUND FORWARD CARGO AFT BULKHEAD LEFT PANEL LOWER SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040608000992004060800099WP 2004 6 8 CALA0400503 120040524A53206044887075T6 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 200 FROM SIX INCHES I/B OF LEFT I/B SEAT TRACK TO CENTER SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2L72 4F A6WE 20040608001022004060800102NM 2004 6 8 CALA0400513 120040528A5312 PRESSURE PANEL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2723661 28922 INSPECTION FOUND A 3 INCH CRACK IN PRESSURE WEB AT STA 727, RBL 17, FORWARD SIDE IN WHEEL WELL. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5330-03352. 2L72 4F RTA16WE 20040608001092004060800109NM 2004 6 8 CALA0400520 120040524A272010622202 TRIM SWITCH BOEING737 737924 13848A1NM COCKPIT FAULTY A CALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SW2731412 30129 THE ELECTRIC RUDDER TRIM FAILED IN OPERATION TO THE LEFT WHILE IN CRUISE PORTION OF FLIGHT FROM TPA TO EWR. OPERATION TO THE RIGHT WAS NORMAL. IF MOVED TO THE RIGHT THE TRIM COULD NOT BE RETURNED TO THE LEFT AT ALL. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RUDDER TRIM SWITCH AT FAULT. THE RUDDER TRIM SWITCH WAS REMOVED AND REPLACED IAW MM 27-11-94 AND FUNCTIONAL CHECKS WERE GOOD. 2L74 4F RTA16WE 20040608001162004060800116WP 2004 6 8 CALA0400524 120040605A5311S27779306 BELTFRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND BELTFRAME CORRODED AT STA 1287, LONGERON 23L. A NEW SECTION OF FRAME WAS SPLICED IN IAW SRM 53-03, FIGURE 2A. 2L72 4F A6WE 20040608001322004060800132EU 2004 6 8 USAA040198 120040510A5320D5347219021100 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW 0904 BEAM, 2.5 INCH X 1.5 INCH X .031 INCH AREA, CORROSION, LEVEL 2; TASK NR JA-260-53500 FLOOR SUPPORT, FRAME 66, Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040608001692004060800169SO 2004 6 8 CHQA000461 120040205A3350 LIGHT EMB 145 EMB145LR 3260212SO LYC O480 GO480* 41527EA CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 RT WING OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT WING OVERWING EMERGENCY LIGHT. OPS CHECK GOOD IAW EMB 145 AMM 33-50-10. 2L72 4T3 ORTT00011ATE275 20040608001722004060800172SO 2004 6 8 CHQA000454 120040107A3350 CONNECTOR EMB 145 EMB145LR 3260212SO LYC O540 O540* 41532EA CABIN BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260 145128 ONE CONNECTOR FOUND BROKE OFF AT SEAT 14 EMERGENCY PROXIMITY LIGHT. SPLICED WIRES BACK TOGETHER IAW CMM 20-21-00 AND OPS CHECKED GOOD IAW AMM 33-50-12. 2L72 4T3 ORTT00011ATE295 20040608001742004060800174SO 2004 6 8 CHQA000449 120040120A3350RPS1B BATTERY EMB 145 EMB145LR 3260212SO LYC O540 O540* 41532EA CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260 145128 AFT SECTION OF EMERGENCY LIGHTING OUT. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTING BATTERY IAW EMB 145 AMM II 33-50-04. 2L72 4T3 ORTT00011ATE295 20040609000072004060900007NE 2004 6 9 MALA040388 220040510A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED A MALAEA ENGINE SHUTDOWN UNSCHED LANDING RJBPARTIAL RPM/PWR LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15441XJ 340B441 DURING CLIMBOUT FROM MEM AT APPROXIMATELY 700 FT AGL ON FLIGHT 3323, ENGINE HAD A STAGE ONE TURBINE BLADE SEPARATION EVENT. HEARD SMALL COMPRESSOR STALL IN RT ENG NOTED R TQ & NG ZERO W/ITT REDLINED & RT OVERTEMP LIGHT ON ITT BEGAN DECREASING THEN ENG WAS SHUTDOWN. NOTED SLIGHT BURNING SMELL IN COCKPIT & CABIN W/BLDS OFF A/C PERFORMED AIR RETURN AFTER SHUTTING DOWN THE RT ENGINE. REMOVED AND REPLACED RT ENG IAW GE MANUAL JC 7100-301 P/N ON & OFF CT7-9B, S/N ON GE-E785696 OFF GE-E785179. ALL ENG RUNS PERFORMED AND LEAK CHECKS PERFORMED IAW ALL JC. A/C GOOD FOR SERVICE. ALL ENG PARAMETERS GOOD. 2L72 4T4 TRTA52EU E8NE 20040609000192004060900019WP 2004 6 9 04FDEA01534 120040529A5320 CHANNEL DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 CORROSION ON NUT PLATE CHANNEL AT FORWARD LOWER CARGO UNDERFLOOR BETWEEN FS 859 AND 879 AT RBL 28. CORROSION FOUND TO BE INTERGRANULAR AND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW DC10 SRM 53-00-01 VOL 1. 2L73 4F A22WE 20040609000222004060900022WP 2004 6 9 04FDEA01535 120040529A5320 FITTING DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD CARGO DOOR SILL FITTING CORRODED AT APPROX FS 919 AT RBL 56. REMOVED CORRODED AREA, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC10 SRM 51-21-01 VOL 2 AND 51-31-01 VOL 2. 2L73 4F A22WE 20040609000272004060900027WP 2004 6 9 04FDEA01399 120040522A5347 SEAT TRACK DOUG DC10 DC1010F 3022111WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 MAIN CARGO AREA STATION 925 SEAT TRACK AT LBL 47 EDGE IS CRACKED. CUT OUT DAMAGE SECTION OF TRACK, FABRICATED SEAT TRACK, SPLICE PLATE AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-70-00 VOL 1 AND DC10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040609000322004060900032WP 2004 6 9 04FDEA01404 120040522A5330 SKIN DOUG DC10 DC1010F 3022111WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 RIGHT HAND ALTERNATE STATIC PORT FAILS WAVINESS INSPECTION AT POSITIONS 4, 4A AND 4W. REMOVED ALTERNATE STATIC PORT AND AVIONICS PRESSURE SWITCH FLEX HOSE IAW DC10 MM 34-11-01-2 AND DC10 MM 33-11-00. REWORKED SKIN AROUND STATIC PORT IAW DC10 SRM 53-20-00 VOL 1. REINSTALLED ALTERNATE STATIC PORT AND AVIONICS FLEX HOSE IAW DC10 MM 34-11-01-2, PERFORMED LEAK CHECK OF ALTERNATE STATIC SYSTEM IAW DC10 MM 34-11-00, NO LEAKS. 2L73 4F A22WE 20040609000382004060900038WP 2004 6 9 04FDEA01410 120040522A5753ARC25171 STRAP DOUG DC10 DC1010F 3022111WP T/E FLAP OUT OF LIMITS A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 LEFT WING, INBOARD FLAP, OUTBOARD HINGE, INBOARD STRAP P/N ARC 2517-1 IS OUT OF LIMITS IAW DC10 CMM 57-52-01. REMOVED OUT OF LIMITS STRAP, LOCATED AND DRILLED HOLES IN NEW STRAP IAW DAC DWG ARC 2512. LOCATED BUSHING HOLE IAW DAC DWG ARC 2512 AND EA 8-5710-77549. INSTALLED NEW STRAP IAW DAC DWG ARC 2512 AND DC10-10 MM 20-50-02-2. 2L73 4F A22WE 20040609000422004060900042NM 2004 6 9 AALA20040620 120040606A3397 WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21616AA 24524 SFO - FORWARD GALLEY EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ALONG WIRE RUN AT RIGHT SIDE WALL AT SEAT 1 EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609000452004060900045WP 2004 6 9 AALA20040623 120040605A2410 CSD DOUG DC9 DC983 3022083WP NR 1 ENGINE FAILED A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW21571AA 49353 BNA EN ROUTE ORD - ATL DURING CLIMBOUT LEFT CSD OIL PRESSURE LOW LIGHT ILLUMINATED FOLLOWED BY LEFT GENERATOR TRIPPED OFF. CONFIRMED CSD OVERTEMP AND DISCONNECTED. ALSO APU GENERATOR WOULD NOT GO ONLINE AFTER INFLIGHT START. RESET, NO HELP. LANDED BNA WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE CSD AND OIL COOLER AND APU GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000542004060900054WP 2004 6 9 AALA20040566 120040517A3350 CONTACTOR DOUG DC9 DC982 3022082WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21488AA 49681 AUS - AFT EMERGENCY OVERHEAD LIGHTS AT L2 DOOR AND AFT AISLE INOPERATIVE. CLEANED BATTERY CONTACTS AND REINSTALLED BATTERIES FOR AFT EMERGENCY LIGHTS AT L2 DOOR AND AFT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000582004060900058NM 2004 6 9 AALA20040576 120040510A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 AFW - FLOORBEAM AT STATION 325 (G1 GALLEY AREA) HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIMITS. AREA IS 1 INCH BY 1 INCH AND DEPTH IS 0.23 INCH. REMOVED CORROSION AND VERIFIED. FABRICATED REPAIR STRAP, ALODINED ALL BARE ALUMINUM SURFACES AND FINISHED BLENDS AND REPAIR STRAP WITH PRIMER. FILLED BLENDS WITH BMS595 SEALANT AND INSTALLED REPAIR STRAP WITH SEALANT PROSEAL 870 AND FASTENERS. 2L72 4F RTA1NM 20040609000662004060900066WP 2004 6 9 AALA20040578 120040519A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21556AA 53086 DFW - RIGHT AND LEFT HAND EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT HAND EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000722004060900072NM 2004 6 9 AALA20040600 120040529A3350 CONNECTOR BOEING737 737823 13844BZNM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21928AN 29528 ORD - SEAT MOUNTED EMERGENCY LIGHT AT ROW 19DEF INOPERATIVE. SECURED LOOSE CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 19DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040609000782004060900078WP 2004 6 9 AALA20040601 120040529A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219616G 53563 DFW - EMERGENCY EXIT LIGHTS ON CEILING AT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS ON CEILING AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000972004060900097NM 2004 6 9 ASAA01100NN 120040124A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040609000982004060900098NM 2004 6 9 ASAA01100LL 120040123A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 DURING INSPECTION FOUND THE EMERGENCY FLOORPATH LIGHTING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040609001142004060900114NM 2004 6 9 DLM88040461 120040525A3244MD88M TIRE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE NR 3 MLG DAMAGED A DALAK NONE C F.O.D. TXTAXI/GRND HDL 1 SO27919DL 49584 NR 3 MAIN TIRE HAS FOD DAMAGE. REPLACED NR 3 MAIN TIRE. 2L72 4F4 FRTA6WE E2EA 20040707000022004070700002NM 2004 7 7 RJEF598HA 120040511A2720810A000005 CONTROL UNIT AIRBUSA319 A319132 3930340NM IAE V2527 V2527EA5 NE RUDDER SERVO LOOSE W RJEFA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO23472TA 1113 DURING CRUISE, AC DIVERTED, PILOT REPORT OF MOD STRUCTURAL VIBRATION. ON GROUND, TECH FOUND THE FWD SEAL AT RT NLG OUT OF POSITION, IT WAS ADJUSTED IAW AMM. DAMAGED SEAL ON PANEL 191 AB LOOSE, INSTALLED SPEED TAPE IAW TSM. INSP OF RUDDER SERVO CONTROLS, HINGE LINE BRGS. FOUND THAT 3 SERVO CNTRL ACTUATORS OUT OF LIMITS. THE 3 ACTUATORS WERE REPLACED. ADJUSTED AND TESTED IAW MM. RESULTS NORMAL. INSP ELEV SERVO CONTROLS AND HINGE LINE BRGS, FOUND NORMAL. NO OSCILLATIONS WERE NOTED ON THE ELEVATORS. CKD OVERWEIGHT LANDING REPORT IAW MM, LOAD REPORT FROM AIDS SYSTEM NOT SHOWN, INSP WAS NOT REQUIRED. TEST FLIGHT WAS CONDUCTED, VIBRATION WERE NOT NOTED AND AC RETURNED TO NORMAL OPS. 2L72 4F4 FRTA28NM E40NE 20040609001342004060900134SO 2004 6 9 C2XA04SH297 120040518A532014533897003 STIFFENER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713566 145622 DURING C CHECK THE T REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040609001522004060900152NM 2004 6 9 AALA20040585 120040521A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21382AN 25451 SFO - EMERGENCY PATH LIGHT AT 31B INOPERATIVE. FOUND CONNECTOR AT 31B SIDEWALL DISCONNECTED. RECONNECTED EMERGENCY LIGHT CONNECTOR AT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609001532004060900153NM 2004 6 9 AALA20040587 120040523A3350 CONNECTOR BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21398AN 29605 GRU - EMERGENCY AISLE LIGHTING AT SEAT ROWS 30H THROUGH 32H INOPERATIVE. FOUND CONNECTOR UNDER SEAT 29J DISCONNECTED. RECONNECTED EMERGENCY AISLE LIGHTING CONNECTOR AT SEAT 29J FOR EMERGENCY AISLE LIGHTING AT ROWS 30H THROUGH 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609001552004060900155EU 2004 6 9 AALA20040589 120040521A3350 SWITCH AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2140064 507 JFK - EMERGENCY LIGHTS ASSEMBLY AT L1 DOOR IS INOPERATIVE. FOUND SWITCH LOOSE BEHIND L1 DOOR EMERGENCY LIGHT. REINSTALLED SWITCH FOR EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040609001562004060900156WP 2004 6 9 AALA20040555 120040513A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21210AA 49161 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 20D IS BROKEN. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001572004060900157NM 2004 6 9 AALA20040556 120040513A5242 DOOR SEAL BOEING737 737823 13844BZNM E/E BAY DOOR LEAKING A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21936AN 29532 DFW - CABIN PRESSURIZATION PROBLEMS DURING CLIMB. REPEAT PROBLEM. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. LEFT HAND PACK WAS PLACARD INOPERATIVE DURING BOTH EVENTS. FOUND LOWER ELECTRICAL ACCESSORY COMPARTMENT (E&E COMPARTMENT) DOOR LEAKING. REPAIRED LOWER E AND E DOOR SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040609001582004060900158NM 2004 6 9 AALA20040557 120040514A2520 POWER SUPPLY BOEING737 737823 13844BZNM CABIN DEFECTIVE A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21933AN 30080 LAX - PASSENGER ADAPTER APPEARED TO SMOKE AFTER A FEW MINUTES OF USE. UNABLE TO DETERMINE IF POWER PORT OR ADAPTER WAS THE PROBLEM. PASSENGER STOPPED USING POWER PORT AND SMOKE WENT AWAY. REPLACED POWER SUPPLY AND JUNCTION BOX. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040609001612004060900161WP 2004 6 9 AALA20040558 120040514A3350P2010031302 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21460AA 49565 LAX - EMERGENCY FLOOD LIGHT AT G2 GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY FLOOD LIGHT AT G2 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001632004060900163WP 2004 6 9 AALA20040554 120040513A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 TPA - EMERGENCY LIGHTS AT THE AFT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHTS AT THE AFT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001642004060900164WP 2004 6 9 AALA20040550 120040512A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219615W 53562 SNA - LEFT AND RIGHT EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK AT B5103 FOR LEFT AND RIGHT HAND EMERGENCY EXIT LIGHTS AT FORWARD OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609001662004060900166WP 2004 6 9 AALA20040547 120040511A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21406A 49317 DFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001672004060900167NM 2004 6 9 AALA20040548 120040510A3350 FUSE BOEING777 777223 1385213NM CABIN BLOWN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21784AN 29588 DFW - FIRST CLASS GALLEY WALL MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE FOR FIRST CLASS GALLEY BATTERY PACK FOR WALL MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040609001682004060900168 2004 6 9 AALA20040549 420040405A25651061323 SLIDE BOEING737 737823 13844BZNM SERVICE DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21910AN 29512 TUL - AUTO INFLATION FAILED FOR SLIDE AT FORWARD SERVICE DOOR. MANUAL INFLATION PASSED. REPLACED SLIDE AT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040610000192004061000019NM 2004 6 10 DHL2004754006 120040511A5753 STRUCTURE BOEING727 727223 1384074NM T/E FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT WING OUTBD AFT FLAP SHOW SPOTS 2 EA OF DISBOND OF WBL 279 & WBL 395. T/E UPPER SIDE. CUT OUT DELAMINATED AREAS AT RT OUTBD AFT FLAP APPROX 1.25 X 10 INCH AND 1.5 X 1.5 INCH. APPLIED ADHESIVE PRIMER AND FABRICATED FILLERS 1.5 X 1.5 INCH AND 1.25 X 10 INCH AND DOUBLERS 3 X 3 INCH AND 2.5 X 12 INCH FROM .016 INCH 2024 T3 PO 9912030. BONDED REPAIR PARTS, CURED, CLEANED, PRIMED AND SEALED IAW B-727 SRM 57-50-2 FIG 4 AND 51-40-20 FIG 30. 2L73 4F A3WE 20040610000222004061000022NM 2004 6 10 DHL2004754004 120040510A5310 DOOR FRAME BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; E&E AFT DOOR LOCK FRAME RT SIDE DENTED. CUT OUT DAMAGED AREA, FABBED DOUBLER FROM 7075 T6 .063 PO 900861 DIM 6.0625 X 1.8750 X 1.125 INCH, AND FILLER FROM 7075-T6 .050 PO 900780 DIM 3.055 X .75 X 1.25 X .25 INCH IAW 727 SRM 53-10-2 FIG 3 RM 171 51-40-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040610000232004061000023NM 2004 6 10 DHL2004754007 120040511A5310 STOP FITTING BOEING727 727223 1384074NM LT MLG WW LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT WHEEL WELL BS 950 AFT DOOR STOP BRACKET IS LOOSE FROM WEB ATTACH ANGLES. REMOVED HYD LINES 4EA FOR ACCESS FOR S/M REPAIR IAW B-727-M/M 20-10-5. REMOVED BRACKETS 2EA ON LT WHEEL WELL BS 950 AFT DOOR STOP FROM WEB AND ACCESS PANEL IAW B-727-SRM 51-30-2. FABRICATED 2EA BRACKETS DIM 19.5 X 5 INCH PO 900576 MAT. 2024-T3 .050 IAW B-727-SRM 51-40-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B-727-SRM 51-10-2. INSTALLED 2EA BRACKETS IAW B-727-SRM 51-30-2. REINSTALLED 4EA HYD LINES AND ACCESS PANEL IAW B-727 M/M 20-10-5. 2L73 4F A3WE 20040610000242004061000024NM 2004 6 10 DHL2004754009 120040511A5320 ANGLE BOEING727 727223 1384074NM RT MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT W/W STA 870 RBL 12 VERTICAL ANGLE IS CRACKED. REMOVED & REPLACED DAMAGED ANGLE P/N 65-18636-378 PO 422352 IAW 727 SRM 51-30-2. 2L73 4F A3WE 20040610000282004061000028EU 2004 6 10 DHL2004364007 120040603A3260BED201 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU LANDING GEAR FAULTY A DHLAO OTHER O OTHER CLCLIMB 1 SO01364DH 141 UPON GEAR RETRACTION GEAR WOULDN'T RAISE. LANDING GEAR HANDLE CANNOT BE RAISED. COMPLETED ABNORMAL, GEAR RAISED NORMALLY. LANDING GEAR LEVER LOCK WAS IN POSITION NR 1 TO BEGIN. REPLACED PROXIMITY BOX IAW M/M 32-61-12. OPS CHECKED GOOD AT THIS TIME. 2L72 4F RTA35EU 20040610000292004061000029WP 2004 6 10 DHL2004803541 120040422A5754 SKIN DOUG DC8 DC873 302199CWP L/E SLOT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RT WING INBOARD SLOT L/E UPPER SKIN CORRODED AT XILD 42.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG V43-R03, ED EDV43-3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED AREA IAW DWG V43-R03, ED EDV43-3. PERFORMED NDT INSPECTION IAW NDT SPM PART 6-10-01.001. FABRICATED FILLER (AL 7075-T6 0.063) AND DOUBLER (AL 7075-T6 0.071) IAW DWG V43-R03, ED EDV43-3. CLEANED, TREATED AND PRIMED AREA, DOUBLER AND FILLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ED EDV43-3, DWG V43-R03, SRM 51-1-21 PG 1M, SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040610000542004061000054NM 2004 6 10 DHL2004781004 120040603A3350 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01781DH 21996 ON SERVICE CHECK FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER M/M 33-50-101. 2L73 4F A3WE 20040610000612004061000061NM 2004 6 10 SWAA041587 120040606A793042D107A1 BYPASS SWITCH BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAULTY A SWAAE ENGINE SHUTDOWN N FALSE WARNING NRNOT REPORTED 1 SW29073SW 22673 687784 INFLIGHT SHUTDOWN, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. OIL TEMPERATURE IN RED PRIOR TO SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE OIL TEMP BULB, BYPASS SWITCH AND OIL FILTER. REMOVED AND REPLACED NR 1 ENGINE OIL FILTER, CLEANED GROUNDING FLANGE CONNECTOR, PER MM. 2L72 4F4 F A16WE E2EA 20040610000622004061000062NM 2004 6 10 SWAA041589 120040605A3350101073 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 DURING SCHEDULED C4 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040610000632004061000063NM 2004 6 10 SWAA041590 120040605A3350100885 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED MV2 CHECK, AFT GALLEY EMERGENCY EXIT LIGHTS EXTINGUISHED AFTER 60 SECONDS. REMOVED AND REPLACED AFT RT BATTERY PER MM. 2L72 4F RTA16WE 20040610000672004061000067NM 2004 6 10 SWAA041594 120040605A575465C266021 STRUCTURE BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA. 2L72 4F RTA16WE 20040610000702004061000070NM 2004 6 10 SWAA041597 120040605A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 15L, CRACKED. REPAIRED SKIN PER SRM AND EA. 2L72 4F RTA16WE 20040610000712004061000071NM 2004 6 10 SWAA041598 120040606A2560PH22300L STRIP BOEING737 7375H4 138449DNM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 EEPLS PHOTOLUMINESCENT STRIP AT ROW 7 ABC, LOOSE. SECURED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20040610000722004061000072 2004 6 10 SWAA041599 420040606A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29779SW 27884 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610000792004061000079NM 2004 6 10 SWAA041604 120040606A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 378.5, LBL 2.8, EQUIPMENT COOLING AIR EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040610000822004061000082NM 2004 6 10 SWAA041606 120040606A53306545890 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR CUTOUT AFT LOWER CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040610000832004061000083 2004 6 10 SWAA041607 420040607A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610000852004061000085 2004 6 10 SWAA041609 420040607A2565D31591478 SLIDE BOEING737 7373Y0 1384671NM R1 DDOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610000862004061000086NM 2004 6 10 SWAA041610 120040607A335090083 BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED RON, FOUND RT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040610000872004061000087NM 2004 6 10 SWAA041611 120040607A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 500B, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040610000892004061000089NM 2004 6 10 SWAA041573 120040603A256065C19901 CABLE BOEING737 7373A4 1384585NM L2 DOOR MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040610000942004061000094NM 2004 6 10 SWAA041615 120040608A339765C27093 GROUND WIRE BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER NRNOT REPORTED 1 SW29358SW 26595 THREE AFT EMERGENCY EXIT DOOR LIGHTS FLICKERED DURING FLIGHT. SECURED LOOSE GROUND WIRE PER MM. 2L72 4F RTA16WE 20040610000952004061000095NM 2004 6 10 SWAA041616 120040608A256065C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20040610000972004061000097 2004 6 10 SWAA041618 420040608A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610001012004061000101NM 2004 6 10 SWAA041567 120040603A3350311500 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 20 ABC, MISSING. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040610001032004061000103NM 2004 6 10 SWAA041569 120040603A256065C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE FWD HOOK LOOSE. SECURED L1 DOOR EVAC SLIDE FWD HOOK PER MM. 2L72 4F RTA16WE 20040608000372004060800037NM 2004 6 8 04FDEA01601 120040603A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION (C53-224-04) ON FLOORBEAM AROUND NUT PLATE HOLES BS 1130, LBL 27 - LBL 43, WL 207. CORROSION OUT OF LIMITS. REPAIRED 1130 FLOORBEAM UPPER CHORD LBL 27-43 WL 207 IAW SRM 53-10-8 FIG 10. 2L73 4F RTA3WE 20040608000382004060800038NM 2004 6 8 04FDEA01602 120040603A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 SIDE FRAME DENTED BS 460 RBL 65 STR 16R. FOUND DENT IN 460 FRAME, STR 16R TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665A. 2L73 4F RTA3WE 20040608000642004060800064WP 2004 6 8 04FDEA01249 120040512A2550 ROLLER TRAY DOUG DC10 DC1010 3022110WP CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 CENTER CARGO CENTER LINE ROLLER TRAY IS CORRODED STA 1621 AND STA 1681. REPLACED ROLLER TRAY IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040608000662004060800066NM 2004 6 8 04FDEA01251 120040513A5320 INTERCOSTAL BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25241FE 20979 AFT CARGO COMPT FS 1147 - 1164 STR 27L - STR 28L INTERCOSTAL HAS LIGHT CORROSION AND MISSING NUT PLATES ON LWR SURFACE OF CHORD. REMOVED CORROSION IAW SRM 51-10-6, OUT OF LIMITS IAW SRM 53-10-1, REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-1, MATERIAL ID 04091 7075-T6 .050C BATCH 8R00071001. INSTALLED NEW ANGLE IAW SRM 51-30-2. INSTALLED NUT PLATES IAW SRM 51-30-2. 2L73 4F RTA3WE 20040608000682004060800068NM 2004 6 8 04FDEA01454 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 RIGHT WING - OUTBOARD FLAP AFT INBOARD HINGE, FOUND OUTBOARD ACTUATOR. HOLE OUT SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS OF LUG: 0.390, MATERIAL REMOVED : 0.002, REMAINING THICKNESS OF LUG: 0.388. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76713, TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040608000792004060800079NM 2004 6 8 SWAA041583 120040604A573065C26700 SKIN BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C3 CHECK, FOUND RT WING L/E SKIN CUTOUT AT WS 210, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040608000902004060800090WP 2004 6 8 CALA0400507 120040525A53209930612 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND A 1 INCH CRACK IN LT CUSP MEMBRANE AT STA 1271. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 96. 2L72 4F A6WE 20040608000932004060800093NM 2004 6 8 CALA0400510 120040526A3350D71702030 CHARGER BOEING767 767424ER 1385270NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2777066 29461 THE EMERGENCY LIGHTS DID NOT ILLUMINATE AT STA 533, WL 204, RBL 95 DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-07, PAGE 206. 2L72 4F RTA1NM 20040608001122004060800112NM 2004 6 8 CALA0400489 120040512A5210141N62443 SKIN BOEING757 757224 1384958NM R1 DOOR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714102 27292 INSPECTION FOUND R-1 DOOR INTERIOR SKIN GOUGED AT BS 354, WL 245. THE SKIN WAS REPAIRED IAW ECRA 5210-01769 AND A DIP WAS ISSUED TO REINSPECT THE AREA ON OR BEFORE 37,500 CYCLES AND TO PERFORM A REPEAT INSPECTION EVERY 12,000 CYCLES THEREAFTER. 2L72 4F RTA2NM 20040608001342004060800134EU 2004 6 8 USAA040224 120040506A5320D5347209000300 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 BEAM, .75 INCH X .75 INCH X .050 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR Y765, BETWEEN CROSSBEAM C64 AND C65 AFT END OF SEAT TRACK. REMOVED AND REPLACED BEAM IAW SRM. 2L72 4F RTA28NM 20040608001432004060800143EU 2004 6 8 USAA040196 120040508A5320D5347219021000 BEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW 0904 BEAM, 2.5 INCH X 1.5 INCH X .028 INCH, CORROSION; LEVEL 2, TASK NR JA-260-53500, BL Y1292, FR 66, Z240. DEFECTIVE PART REPLACED WITH IDENT PN IAW EA 95469 AND SRM. 2L72 4F4 FRTA28NM E2GL 20040608001522004060800152NM 2004 6 8 USAA040210 120040428A5320 WEB BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US68850 23898 SEAT TRACK WEB, .75 INCH LONG EACH, CRACKED (2) WEB CUTOUT UNDER SEAT TRACK BS785, LBL 55. REPAIRED IAW SRM. 2L72 4F4 FRTA1NM E13NE 20040608001562004060800156EU 2004 6 8 USAA040229 120040506A5320D5347112420000 WEB AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19702UW16155 0896 WEB, 1.5 INCH X 1.5 INCH X .015 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500. WEB BETWEEN FR69, 70, Y1292, Z240. 2L72 4F4 FRTA28NM E2GL 20040608001672004060800167SO 2004 6 8 CHQA000459 120040106A3350 LIGHT EMB 145 EMB145LR 3260212SO WRIGHTR3350 981TC18EA1 67038EA EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286 145443 RT AFT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT AFT WING EMERGENCY LIGHT IAW 145 MM 33-50-07. OPS CHECKS GOOD. LAMP PN 1713. 2L72 4T4 RRTT00011ATE287 20040609000032004060900003NM 2004 6 9 AALA20040614 120040604A3350 BATTERY PACK BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21388AA 27448 MIA - RIGHT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR RIGHT AFT OVERWING EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609000142004060900014EU 2004 6 9 04FDEA01110 120040428A5320A53611646223000 CROSSBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25428FE MAIN CABIN FLOOR SUPPORT CROSSBEAM AT FR14A FROM Y953 TO Y1456 IS CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW A310-200 SRM 51-40-21. 2L72 4F RTA35EU 20040609000212004060900021WP 2004 6 9 04FDEA01538 120040529A2550 SUPPORT DOUG DC10 DC1010F 3022111WP CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 CORROSION AT FORWARD LOWER CARGO ROLLER TRAY AT RBL 28, FS 889 ON TOP PLATE, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION, FABRICATED T-SUPPORT, DOUBLERS AND INSTALLED IAW DC10 SRM 51-31-01 VOL 2. 2L73 4F A22WE 20040609000292004060900029WP 2004 6 9 04FDEA01401 120040522A5347 SEAT TRACK DOUG DC10 DC1010F 3022111WP FUSELAGE INCORRECT A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 SEAT TRACK ON WL 27R BETWEEN 615-670 MAIN UPPER CARGO HAS A BIG GAP TWO PLACES. REMOVED SEAT TRACK SECTION AND INSTALLED NEW TRACK SECTION IAW DC10 SRM 51-31-01 VOL 2 AND DC10 SRM 51-21-01 VOL 2. 2L73 4F A22WE 20040609000302004060900030WP 2004 6 9 04FDEA01402 120040522A5753ARC291425 FLAP TRACK DOUG DC10 DC1010F 3022111WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 LEFT HAND INBOARD FLAP TRACK HAS SIGNS OF WEAR (6 PLACES), MARKED. CHECKED LIMITS ON LEFT HAND INBOARD FLAP TRACK NUMBER 2 IAW DC10-10 F/E MM 27-50-03-2, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW DC10-10 MM 27-50-03-2 STEP 4B (2) (A). 2L73 4F A22WE 20040609000502004060900050WP 2004 6 9 AALA20040569 120040519A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219622A 53593 DFW - CEILING EMERGENCY LIGHT FROM ROW 15 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 15-17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040609000532004060900053EU 2004 6 9 AALA20040565 120040516A5610PPGD20543406 WINDSHIELD FOKKERF28 F28MK0100 4990807EU COCKPIT CRACKED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW211427A 11412 ORD - FIRST OFFICER WINDSHIELD CRACKED AND ARCING. REPLACED FIRST OFFICER WINDSHIELD IN ACCORDANCE WITH MM 56-11-00-4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040609000572004060900057NM 2004 6 9 AALA20040571 120040430A307030431101680 TAPE BOEING767 767323 1385205NM ANTI-ICE SYS BURNED A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 AFW - HEATER TAPE FOR WATER OR DRAIN LINE WAS BURNT IN HALF. INSULATION WRAPPER WAS SLIGHTLY CHARRED. WATER AND DRAIN LINE ARE WRAPPED TOGETHER WITH 2 RIBBONS (PART NUMBER 304311040280 MFR COX AND COMPANY), AREA WAS .5 INCH BY 16 INCHES AT AFT CARGO AT STATION NUMBER 1410 THROUGH 1420 ABOVE STRINGER 536R. CAPPED AND STOWED HEATER TAPE POWER WIRE. REMOVED BURNT SECTION OF HEATER TAPE AND WRAPPED NEW INSULATION AROUND DRAIN LINE AND WATER LINE PER PATTERN CARD 1231 STEP 3 NOTE 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609000632004060900063NM 2004 6 9 AALA20040583 120040521A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21670AA 25335 LGA - EMERGENCY EXIT LIGHT AT R2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609000702004060900070NM 2004 6 9 AALA20040598 120040529A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219630A 53561 DFW - EMERGENCY ESCAPE LIGHT IN CEILING ABOVE SEAT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE LIGHT IN CEILING ABOVE SEAT ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040609000712004060900071NM 2004 6 9 AALA20040599 120040529A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21915AN 29516 BOS - EMERGENCY EGRESS LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND ROW 7 FOR EMERGENCY EGRESS LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040609000882004060900088SO 2004 6 9 SWIA200413345 120040520A3397 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE CABIN BROKEN A SWIAK NONE L NO TEST TXTAXI/GRND HDL 1 NM07569SW 120344 ONE EMERGENCY LIGHT IS INOP (LEFT SIDE OF AISLE).REPLACED BROKEN WIRE. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040609000922004060900092EU 2004 6 9 RAIA00405007 120040507A3241 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP ANTI-SKID SYS MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03556HK 41073 3646-RIC- ANTI-SKID LIGHT ILLUMINATED. MAINTENANCE PLACED ANTI-SKID SYSTEM ON DEFERRAL IAW MEL 32-6. SUBSEQUENTLY CLEARED DMI BY OPS CHECK ANTI-SKID SYSTEM-OPS CHECK OK. 2L72 4T3 TRTA41NM E2WE 20040609000932004060900093SO 2004 6 9 RAIA00405009 120040512A3240429512 CONTROL UNIT EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL BRAKE SYS DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK3349 145068 5701-STL- BRAKE DEGRADE MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT. 2L72 4F4 FRTT00011ATTE6CH 20040609000992004060900099EA 2004 6 9 QXEA200400356 120040525A3260895001 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE NLG OUT OF ADJUST A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09600QX6199 10005 FLIGHT 2465 - THE CREW REPORTED THAT AFTER TAKE-OFF, THE GEAR FAILED TO RETRACT. THE FLIGHT CONTINUED ON TO PDX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE WHEEL CENTERING PROX SENSORS OUT OF ADJUSTMENT. THE SENSORS WERE ADJUSTED, OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040609001042004060900104EU 2004 6 9 MALA040416 120040524A2560 COVER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN OUT OF POSITION A MALAO OTHER O OTHER ININSP/MAINT 1 GL15441XJ 340B441 FA PBE COVER FELL OFF. UPON INSPECTION FOUND PBE COMPROMISED. REPLACED PBE. 2L72 4T4 TRTA52EU E8NE 20040609001072004060900107WP 2004 6 9 UPS04842422 120040504A5712 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 LT WING LE UPPER RIB IS CRACKED AT XFS 641. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2 2L74 4F4 FRT4A25 E2GL 20040609001082004060900108WP 2004 6 9 UPS04842423 120040507A532097540552 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 AFT TORQUE BOX UPPER FRAME IS CRACKED AT STATION 1220 LONGERON 34L TO 35L. REMOVED AND REPLACED FRAME GUIDE FITTING IAW DWG 9754055 AND SRM 51-3-0 2L74 4F4 FRT4A25 E2GL 20040609001102004060900110NM 2004 6 9 FX72004F00000 120040501A7312320115 VALVE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 2 DEFECTIVE A FX7AO OTHER O OTHER NRNOT REPORTED 1 SO1979749 22451 NR 2 ENGINE SHUT-DOWN DURING FLIGHT DUE TO HIGH OIL TEMP IN YELLOW ARC. TROUBLESHOT AND FOUND FUEL HEAT VALVE OPEN. CLOSED MANUALLY AND SAFETY WIRED SHUT. RAN ENGINE ALL PARAMETERS NORMAL AND AIRCRAFT RETURNED TO SERVICE WITH FUEL HEAT VALVE ON DMI. NO FURTHER INCIDENTS. 2L73 4F4 F A3WE E2EA 20040609001112004060900111EA 2004 6 9 F03053 120040425A5210 MECHANISM CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE PAX DOOR LACK OF LUBE A FDKAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07906FJ1972 1659 15006 MAINTENANCE WAS CALLED OUT TO THE PLANE BECAUSE THE CREW COULD NOT GET THE MAIN CABIN DOOR REOPENED AFTER CLOSING IT. MAINTENANCE DISASSEMBLED THE DOOR, LUBED AND CLEANED, REASSEMBLED AND ALL FUNCTIONAL AND OPS CHECKS GOOD. CONTROL NR 112617. 2L72 4F4 FRTA21EA E15NE 20040609001192004060900119NM 2004 6 9 DL73S040466 120040525A5753 ROLLER BOEING737 737232 1384475NM PWA JT8 JT8D* NE T/E FLAP OUT OF POSITION A DALAK NONE F FLT CONT AFFECTED CLCLIMB 1 SO27305DL 23077 DURING ROTATION A STRONG RT WING UP FORCE WAS ENCOUNTERED AS THE AIRCRAFT BECAME AIRBORNE. SUBSTANTIAL RT AILERON WAS NECESSARY TO KEEPS WINGS LEVEL. FOUND LT OB FLAP IB TRACK WITH BELLCRANK ROLLER OUT OF CAMTRACK. REPLACED BELLCRANK. 2L72 4F4 FRTA16WE E2EA 20040609001222004060900122NM 2004 6 9 DL73S040469 120040526A2740 SPRING BOEING737 737232 1384475NM STAB TRIM OUT OF LIMITS A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27306DL 23078 MANUAL TRIM AND AUTO PILOT TRIM INOPERATIVE THROUGHOUT FLIGHT. CYCLED BOTH STAB TRIM CUTOUT SWITCHES, NO HELP, REPLACED STAB TRIM BRAKE LEAF SPRINGS AND PERFORMED BRAKE CHECKS IAW M/M. 2L72 4F RTA16WE 20040609001252004060900125EA 2004 6 9 COMA0470044 120040524A3234533443 CONTROL HANDLE CNDAIRCL600 CL6002C10 1390015EA COCKPIT FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01340CA4412 10062 FLIGHT 5287 GEAR DISAGREE WARNING. REPLACED THE GEAR SELECTOR LEVER. 2L72 4F RTA21EA 20040609001272004060900127EU 2004 6 9 BAQ2004F12345 120040513A7120109032530101 BRACKET AGUSTAA109 A109E 0260119EU PWA PW206 PW206A NE LT ENGINE CRACKED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037UC 1797 11088 NR 1 ENGINE LT OB FORWARD ENGINE SUPPORT BRACKET FOUND CANCELLED DURING ROUTINE MAINTENANCE. PART IS VISABLE AFTER INSPECTION PANEL IS REMOVED INSIDE ENGINE COMPARTMENT. PANEL NR 109-0322-10-527. 1G72 3U3 URTH7EU E42NE 20040609001592004060900159WP 2004 6 9 AALA20040559 120040515A3397 WIRE DOUG DC9 DC982 3022082WP CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21555AN 53085 DFW - EMERGENCY SEAT MOUNTED AND LEFT AND RIGHT HAND OVERWING EXIT LIGHTS AT ROW 20 TO TAIL CONE INOPERATIVE. REPAIRED SHORTED WIRE FOR EMERGENCY SEAT MOUNTED AND LEFT AND RIGHT HAND OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040610000692004061000069NM 2004 6 10 SWAA041596 120040605A3350101114 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040610000802004061000080NM 2004 6 10 SWAA041605 120040606A5310BAC15172294 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR CUTOUT AFT FRAME DOOR, CRACKED. REPAIRED DOOR FRAME PER SRM. 2L72 4F RTA16WE 20040610000902004061000090NM 2004 6 10 SWAA041563 120040603A57536546434 STRUCTURE BOEING737 7373H4 1384600NM T/E FLAP SEPARATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 LT WING OUTBOARD AFT FLAP T/E, SEPARATED. REPAIRED LT OUTBOARD AFT T/E FLAP PER SRM. 2L72 4F RTA16WE 20040610000922004061000092NM 2004 6 10 SWAA041614 120040606A323365448255 ACTUATOR BOEING737 7373H4 1384600NM RT MLG FAILED A SWAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SW29352SW 24888 DIVERSION, AFTER GEAR HANDLE UP, INDICATED UP. AFTER GEAR HANDLE OFF, RT MLG INDICATED DOWN AND LOCKED. GEAR HANDLE DOWN, ALL 3 GEARS INDICATED DOWN AND LOCKED, VISUALLY CHECKED MLG DOWN AND LOCKED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20040610000982004061000098 2004 6 10 SWAA041619 420040608A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED C4 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F A16WE 20040610000992004061000099NM 2004 6 10 SWAA041565 120040603A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040610001072004061000107NM 2004 6 10 DLM88040492 120040531A2910AS15308K0254 HYDRAULIC LINE DOUG MD88 MD88 3023688NM HYD SYSTEM CHAFED A DALAD RETURN TO BLOCK KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27953DL 49884 ON TAXI OUT SMOKE WAS SEEN COMING OUT OF RIGHT REAR OF A/C. RIGHT HYDRAULIC PRESSURE 0, RIGHT HYDRAULIC QUANTITY 2. PINNED GEAR, TAXIED BACK TO GATE. INSP RIGHT REAR OF A/C, NO EVIDENCE OF SMOKE OR FIRE. FOUND RT ENG HYDRAULIC FLEX LINE BETWEEN PYLON AND FILTER ASSY CHAFED THROUGH ON FASTENER. REPLACED LINE AND SERVICED HYDRAULIC RSVR TO FULL. RAN ENGS PER PFHB, LEAK CHECK NORMAL, QTY NORMAL, A/C OK FOR SERVICE. 2L72 4F RTA6WE 20040610001352004061000135NE 2004 6 10 DL76L040494 220040601A7210 FLANGE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27178DN53980 25143 724168 NR 1 ENGINE FLANGE CRACK FOUND DURING ROUTINE BORESCOPE. REPLACING ENGINE. 2L72 4F4 FRTA1NM E24NE 20040610001382004061000138NM 2004 6 10 DL73S040495 120040601A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 APPROX 3 INCH LONGITUDINAL CRACK IN FUSELAGE SKIN STA 944 ABOVE STR 24R. REPAIRED PER SRM. 2L72 4F RTA16WE 20040610001392004061000139NM 2004 6 10 DL76S040496 120040601A5751 SKIN BOEING767 767332 1382001NM RT AILERON DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27118DL 23277 RIGHT OUTBOARD AILERON OUTBOARD END LOWER AND UPPER SKIN AND SPAR DELAMINATED APPROXIMATELY 14 INCHES LONG AT END OF PART. REPAIRED PER ER/A 090481-14. 2L72 4F RTA1NM 20040610001412004061000141NM 2004 6 10 DL73S040498 120040531A3350BPS73 PIN BOEING737 737232 1384475NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27311DL 23083 FOUND ON SERVICE CHECK, AISLE LIGHTS AT SEAT 22L AND 24L INOP. FOUND PIN BROKE ON M1136 AT STATION L753. REPLACED AND TESTED PER M/M. 2L72 4F RTA16WE 20040610001422004061000142NE 2004 6 10 DL76L040499 220040601A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 MALFUNCTIONED A DALAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO27195DN33540 28452 727654 HARD TO START AND OIL IN THE TAIL PIPE. CHANGED ENGINE. 2L72 4F4 FRTA1NM E24NE 20040610001432004061000143NM 2004 6 10 DL73S040500 120040602A5313 STRINGER BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27316DL 23088 FOUND ON W-2 LETTER CHECK STRINGER 27 LEFT CORRODED STA 967-1006. REPAIRED PER SRM 53-10-3 FIG 1. 2L72 4F RTA16WE 20040610001452004061000145NM 2004 6 10 DL757040502 120040601A5310146N851225 DOOR FRAME BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27662DN 24991 FUSELAGE C2 DOOR OPENING FRAME AND SILL FS 1440, SILL CHORD REPLACEMENT AND FRAME SPLICE REPAIR. THE OUTER CHORD OF THE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS FOUND WITH SEVERAL AREAS OF CORROSION AND REQUIRED REPLACEMENT. TO FACILITATE REPLACEMENT, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER SECTIONS REMOVED. THE SILL CHORD WAS REPLACED AND THE FRAME SECTION SPLICED BACK WITH ALUMINUM REPAIR DOUBLERS PER ER/A 090314-14, REV A. 2L72 4F RTA2NM 20040610001652004061000165NM 2004 6 10 DL73S040474 120040528A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 CORROSION ON FWD AND AFT SIDE OF FRAME STA 827 BETWEEN STR 27 LT AND RT. REPAIRED PER SRM 53-10-04. 2L72 4F RTA16WE 20040610001682004061000168NM 2004 6 10 DL764040477 120040529A3350 LENS BOEING767 767432ER 1385134NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27841MH 29714 EMERGENCY LIGHT LENS MISSING AT SEAT 20B. INSTALLED SAME. 2L72 4F RTA1NM 20040610001702004061000170NM 2004 6 10 DL76G040479 120040529A3040561701280 CONTROLLER BOEING767 7673P6 1385105NM E/E BAY FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27156DL 25354 CAPT FWD WINDSHIELD STARTED TO SMOKE ACCOMPANIED WITH FUMES. BOTTOM LEFT CONNECTOR MELTED, FOUND J5 CONNECTOR AT L1 WINDOW BURNT, WINDOW NOT DAMAGED. REPLACED WINDSHIELD HEAT CONTROLLER. 2L72 4F RTA1NM 20040610001712004061000171NM 2004 6 10 DLM88040480 120040530A4990 OIL SYSTEM DOUG MD88 MD88 3023688NM APU LOW A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27913DE13362 49956 P80424 A/C 9013 DIVERTED TO LGA FROM ATL EN ROUTE TO ALB DUE TO APU FAULT LIGHT ILLUMINATED AFTER LEFT ENGINE CSD DISCONNECTED. SERVICED APU OIL TO FULL. 2L72 4F RTA6WE 20040610001722004061000172NM 2004 6 10 DLM88040481 120040530A3350 CONNECTOR DOUG MD88 MD88 3023688NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27923DL 49705 SEAT EMERGENCY LIGHT INOP AT 24D. REPAIRED BROKEN CONNECTOR AT SEAT TO SIDEWALL DISCONNECT. 2L72 4F RTA6WE 20040610001742004061000174NM 2004 6 10 DL76S040483 120040529A3397 WIRE BOEING767 767332 1382001NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27128DL 24078 SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 26F INOP. REPAIRED BROKEN WIRES AT CONNECTOR, CHECKS GOOD. 2L72 4F RTA1NM 20040610001772004061000177NM 2004 6 10 DLM88040487 120040531A2121349101527 FAN DOUG MD88 MD88 3023688NM CARGO BAY FAULTY A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27933DL 49720 ODOR REPORTED MID CABIN BY SEVERAL PAX. FOUND NR 1 LOW RANGE ALT FAN AS CAUSE OF ODOR. DEACTIVATED FAN, NR 1 LRRA INOP. REPLACED SAME. 2L72 4F RTA6WE 20040610001822004061000182 2004 6 10 DL76L040488 420040531A31604058650931 CDU BOEING767 767332 1382001NM COCKPIT FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27199DN 28456 NR 2 RIGHT CDU SCREEN WENT BLANK ONE HOUR INTO FLIGHT. RECYCLED CIRCUIT BREAKER E29. DISPLAY RETURNED FOR APPROX 45 MINUTES THEN FAILED AGAIN. AIRCRAFT RETURNED TO JFK. REMOVED AND REPLACED RIGHT FMS CDU PER M/M 34-61-02. OP CHECKS GOOD AT THIS TIME. 2L72 4F RTA1NM 20040610001832004061000183NM 2004 6 10 DL73S040489 120040531A5610 WINDOW BOEING737 737232 1384475NM COCKPIT CRACKED A DALAK NONE O OTHER DEDESCENT 1 SO27334DL 23105 R1 WINDOW CRACKED INFLT DESCENDING THROUGH 25,000 FT AT 280 KT. REPLACED SAME. 2L72 4F RTA16WE 20040716000762004071600076NM 2004 7 16 CALA0400562 120040702A5313BAC1498156 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND STRINGER 27L CORRODED AT STA 986.5. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A NEW STRINGER, HAT SECTIONS, FILLER, AND SHIMS WERE INSTALLED IAW SRM 53-00-03, DETAIL 6. 2L72 4F RTA16WE 20040610001902004061000190NM 2004 6 10 DL764040491 120040531A3244 TIRE BOEING767 767432ER 1385134NM MLG DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO27841MH 29714 NR 8 MLG TIRE HAS FOD DAMAGE. SCREW WAS STUCK IN TREAD. REPLACED WHEEL ASSY. 2L72 4F RTA1NM 20040610001952004061000195NM 2004 6 10 DL767040506 120040304A7697 WIRE BOEING767 767232 1385132NM GE CF680 CF680A2 NE NR 1 ENGINE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27103DA42131 22215 580319 DURING HMV IN GSO FOUND NR 1 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRING AND PLUGS. 2L72 4F4 FRTA1NM E13NE 20040610001982004061000198NM 2004 6 10 DL73S040437 120040512A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27380DL 23607 THE FUSELAGE SKIN WAS INSPECTED FOR SCRIBE LINES. SCRIBES WERE FOUND IN THE LOWER SKIN OF SEVERAL LAP JOINTS, IN THE BUTT JOINTS, AND AROUND FAIRING PANELS FROM FS 360 TO 908, PRIMARILY IN THE UPPER FUSELAGE. THE SCRIBED LAP JOINTS WERE CUT OUT AND REPAIRED WITH ALUMINUM DOUBLERS. THE BUTT JOINT STRAPS WERE REPLACED. THE FAIRING SCRIBES WERE BLENDED AND REPAIRED WITH ALUMINUM DOUBLERS. 2L72 4F A16WE 20040610002002004061000200NM 2004 6 10 DLM90040439 120040515A21216459401 FAN DOUG MD90 MD9030 3023690NM CABIN SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27902DA 53382 SMOKE AND FUMES IN CABIN, TURNED OFF RIGHT PACK AND GALLEY POWER SMOKE STOPPED. FOUND J9 C/B POPPED ON RECIRCULATION FAN. REPLACED SAME. 2L72 4F RTA6WE 20040610002012004061000201NM 2004 6 10 DL76G040440 120040515A5753113T1226 FITTING BOEING767 7673P6 1385105NM T/E FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27152DL 24984 DURING PSV IN ATLANTA, FOUND A HOLE CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 089397-14MA REVISION A, REPAIR NR 1. 2L72 4F RTA1NM 20040610002022004061000202NM 2004 6 10 DL76G040441 120040516A5753113T2252 FITTING BOEING767 7673P6 1385105NM T/E FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27152DL 24984 DURING PSV IN ATLANTA, FOUND HOLES CORRODED WHILE ACCOMPLISHING ME 02 OF EA 01-085672-12 AD, REV C. REPAIRED PER ERA 089397-14MA REVISION A, REPAIR NR 4. 2L72 4F RTA1NM 20040610002042004061000204NM 2004 6 10 DL738040509 120040607A3510174660N3 OXYGEN MASK BOEING737 737832 13844CFNM COCKPIT LEAKING A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO273764D 30818 ACFT OFF SCHEDULED ORD DUE TO C/P 02 MASK WOULD NOT SHUT OFF AND WAS DEPLETING 02 BOTTLE. REPLACED MASK. 2L72 4F RTA16WE 20040610002232004061000223NM 2004 6 10 DLM88040458 120040524A3350 CONNECTOR DOUG MD88 MD88 3023688NM CABIN LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27902DE 53379 SEVERAL EMERGENCY SEAT LIGHTS INOP AFTER ROW 17. SECURED LOOSE CONNECTOR AT ROW 17. 2L72 4F RTA6WE 20040610002242004061000224NM 2004 6 10 DL76L040436 120040514A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27194DN 28451 PLASTIC SMELLING FUMES BRIEFLY NOTED FOR 1 MIN INFLT NEAR ROW 15 SEATS A AND B. CHECKED AREA OF SEAT 15 A AND B. FOUND NO EVIDENCE OF SMELL OR BURNING. OK FOR SERVICE. 2L72 4F RTA1NM 20040610002282004061000228NM 2004 6 10 SWAA041620 120040608A335065C27093 LIGHT BOEING737 7373K2 13844BANM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040610002302004061000230NM 2004 6 10 SWAA041621 120040608A33506128251 BATTERY BOEING737 7373K2 13844BANM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040610002312004061000231NM 2004 6 10 SWAA041622 120040608A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 18 ABC TO ROW 20 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20040610002342004061000234NM 2004 6 10 SWAA041625 120040608A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 20, CORRODED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040610002352004061000235NM 2004 6 10 SWAA041626 120040608A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT LEFT BS 296, WL 209, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040609000082004060900008EU 2004 6 9 MALA040384 120040507A215011341041 MOTOR SAAB SF340 340B 7860101EU CABIN COOLING FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL15453XJ1964 340B453 CABIN FILLED WITH SMOKE. A/C EVACUATED ALL ELECTRICAL SWITCHES OFF. SMOKE APPEARED TO COME FROM REAR OF CABIN. SUSPECT SUPPLEMENTAL A/C. NO ENGINE RUNNING, ON EXTERNAL POWER. MAINTENANCE FOUND SUPPLEMENTAL A/C COMPRESSOR MOTOR TO BE BURNED UP. REMOVED AND REPLACED COMPRESSOR MOTOR P/N 1134104-1, S/N ON 1425, S/N OFF 480 IAW CMM 9, 2, 1. OPS CHECKS GOOD. 2L72 4T RTA52EU 20040609000282004060900028WP 2004 6 9 04FDEA01400 120040522A5411 RIB DOUG DC10 DC1010F 3022111WP NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 NUMBER 2 ENGINE INLET STRUCTURE RIB CRACKED AT SPLICE AT 1 O’CLOCK POSITION, ACCESS THROUGH PANEL 362JR. REMOVED SPLICE, INTERCOSTAL AND STIFFENER SECTION IAW DC10 SRM 51-35-01 VOL 2, FORMED STIFFENER AND SPLICE IAW DC10 SRM 51-10-00 VOL 2, INSTALLED REPAIR PARTS IAW DC10 SRM 54-10-00 VOL 1 AND 54-35-01 AND 54-33-01 VOL 2. 2L73 4F A22WE 20040609000362004060900036WP 2004 6 9 04FDEA01408 120040522A5320 FITTING DOUG DC10 DC1010F 3022111WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 FORWARD CARGO DOOR SILL FITTING IS CORRODED AT APPROX FS 919 AT RBL 56. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL 1. TRIMMED OUT DAMAGE FLANGE IAW DC10 SRM 53-50-00 FIG 11. FABRICATED REPAIR ANGLE IAW DC10 SRM 53-50-00 FIG 11 VOL 1. INSTALLED IAW DC10 SRM 51-33-01 VOL 2 AND 53-50-00 FIG 11 VOL 1. 2L73 4F A22WE 20040609000612004060900061NM 2004 6 9 AALA20040575 120040510A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21381AN 25450 AFW - FLOORBEAM AT STATION 287 AT RBL 86 AT VERY OUTBOARD END HAS CRACK ON H3 FLANGE. AREA OF FLANGE CONTAINING CRACK WAS REMOVED. TWO REPAIR ANGLES MACHINED FROM 0,063 INCH 7075T6 EXTRUSION AND FILLER WERE INSTALLED WITH STAINLESS HI-LOKS. 2L72 4F RTA1NM 20040609000642004060900064WP 2004 6 9 AALA20040582 120040520A3350 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21574AA 53151 DFW - EMERGENCY PATH LIGHT AT SEAT 14D INOPERATIVE. FOUND LOOSE CONNECTION UNDER SEAT 14D. REPAIRED LOOSE CONNECTION FOR EMERGENCY PATH LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000692004060900069WP 2004 6 9 AALA20040596 120040530A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21410AA 49321 DEN - OVERHEAD EMERGENCY LIGHTS AT AFT OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT AFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000752004060900075NM 2004 6 9 AALA20040607 120040531A3397 WIRE BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21374AA 25201 DFW - EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD GALLEY INOPERATIVE. FOUND LOOSE WIRE. RECONNECTED WIRE FOR EMERGENCY EXIT LIGHT AT RIGHT HAND FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609000802004060900080WP 2004 6 9 AALA20040625 120040607A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217508 49802 DFW - SEAT MOUNTED EMERGENCY EXIT PATHWAY LIGHTING AT 22D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY EXIT PATHWAY LIGHTING ASSEMBLY AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609000812004060900081NM 2004 6 9 AALA20040602 120040531A2910 MODULE BOEING767 767223 1385123NM HYD SYSTEM FAILED A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21321AA 22322 MCI - INFLIGHT T003 FROM JFK TO LAX LOST CENTER HYDRAULIC SYSTEM QUANTITY APPROXIMATELY TWO HOURS INTO FLIGHT. LANDED MCI WITHOUT INCIDENT. REPLACED HYDRAULIC MODULE AND DELTA P O-RINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040609001022004060900102NM 2004 6 9 304AW0007 120040519A5330 SKIN BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE LIGHTNING STRIKEA PIDAK NONE O OTHER NRNOT REPORTED 1 SO05304AW 24011 SEVERAL LIGHTENING STRIKES IN THE CROWN OF THE FUSELAGE SKIN NEAR STATION 259 BETWEEN STR 2 AND 3 LEFT. REPAIRED IAW SRM 53-00-01 AND EA NR 53-171. 2L72 4F4 FRTA16WE E2GL 20040609001062004060900106NM 2004 6 9 UPS04242439 120040511A5330 SKIN BOEING727 72725C 138400HNM PWA JT8 JT8D5 52046NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 INSPECTION TYPE: C CRACK IN SKIN AT FWD CARGO DOOR CUTOUT AT FWD LWR CORNER. REPAIRED IAW AAAE EO 2004-050-001. REFERENCE UPS EO B72 7-5330-20497-A. 2L73 4F4 F A3WE E2EA 20040609001182004060900118NM 2004 6 9 DL757040465 120040526A2530811150417 COFFEEMAKER BOEING757 757232 1384965NM PWA 2037 PW2037 NE MID GALLEY OVERHEATED A DALAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27683DA 27103 MID GALLEY COFFEE MAKER OVERHEATED, REPLACED COFFEE MAKER. 2L72 4F4 FRTA2NM E17NE 20040609001202004060900120NM 2004 6 9 DL78K040467 120040526A2780 FSEU BOEING737 737832 13844CFNM GE CFM56 CFM56* 13802NE E/E BAY FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27399DA 30379 RETURN TO ATL, WITH LEADING EGDE SLAT NR 1 AND LEADING EDGE FLAPS NR 1 AND NR 4, REMAINING ILLUMINATED AMBER ON AFT OVERHEAD ANNUNCIATOR, LE FLAP TRANSIT REMAINED ILLUMINATED CREATING LE LOCKOUT NO ADVERSE ROLL. REPLACED FSEU FOR FAULT CODE 27-51105. 2L72 4F4 FRTA16WE E2GL 20040609001462004060900146NM 2004 6 9 AALA20040610 120040602A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21794AN 30256 DFW - EMERGENCY LIGHT ON RIGHT HAND SIDE AT AFT FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT RIGHT HAND SIDE AT AFT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040609001492004060900149NM 2004 6 9 AALA20040612 120040602A5330 SKIN BOEING757 757223 1384957NM FUSELAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21674AN 29424 TUL - REPAIR OF TEMPORARY REPAIR OF FUSELAGE SKIN AT STRINGER 26L TO 27L AT STATION 500. CUT OUT AREA WAS 4.5 INCHES BY 6.25 INCHES. REPAIRED TEMPORARY REPAIR PER ESO 09309 AND SRM 53-30-01. 2L72 4F RTA2NM 20040609001542004060900154WP 2004 6 9 AALA20040588 120040524A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 PHL - EMERGENCY LIGHTS ON RIGHT SLIDE OF AIRCRAFT FROM SEAT ROW 20 FORWARD AND OVERWING EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACKS AT SEAT ROW 20 AND FOR FORWARD ENTRY OVERHEAD AND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001622004060900162NM 2004 6 9 AALA20040553 120040513A3397 POWER CABLE BOEING757 7572Q8 1384972NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21701TW 28160 DFW - EMERGENCY ESCAPE PATH LIGHT AT LEFT HAND AISLE FORWARD OF SEATS 1AB INOPERATIVE. FOUND EMERGENCY LIGHT POWER CABLE BROKEN IN FIRST CLASS. REPLACED EMERGENCY PATH LIGHT POWER CABLE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040609001692004060900169 2004 6 9 SWAA041588 420040605A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610000302004061000030NM 2004 6 10 DHL2004754010 120040512A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; STRINGER 28R CORRODED AT BS 1050. CUT OUT DAMAGED AREA OF STR 28R BS 1040 TO BS 1078 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STR REPAIR FROM BAC 1498-145 SIZE 38.5 PO 900878 AND 2EA SPLICES FROM BAC 1498-131 SIZE 10 INCHES PO3323107 IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2, INSTALLED STR REPAIR IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20040610000332004061000033NM 2004 6 10 DHL2004754013 120040515A5754 SUPPORT BRACKET BOEING727 727223 1384074NM L/E FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; NR 2 L/E FLAP ACTUATOR TRUNNION BRACKET SUPPORT IS CRACKED O/B SIDE. REMOVED DAMAGED BRACKET IAW B727 SRM 51-30-2, FABRICATED NEW BRACKET DIM 6.125 X 8.75 FROM 7075T6.063 PO 900861 IAW B727 SRM 57-20-2 FIG 1, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED NEW BRACKET ON NR 2 L/E FLAP O/B SIDE IAW B727 SRM 51-30-2 AND 57-20-2 FIG 2, OPS & LEAK CHECKED. NR 2 KRUEGER FLAP IAW B727 MM 27-81, OPS CHECKED GOOD. 2L73 4F A3WE 20040610000682004061000068NM 2004 6 10 SWAA041595 120040605A575465C266011 STRUCTURE BOEING737 7373H4 1384600NM L/E SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E SLAT, CRACKED. REPAIRED L/E SLAT PER EA. 2L72 4F RTA16WE 20040610000772004061000077NM 2004 6 10 SWAA041600 120040606A552365C26384 HINGE BRACKET BOEING737 7373H4 1384600NM ELEVATOR TAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED THRU CHECK, FOUND RT AND LT ELEVATOR TAB CONTROL ROD HINGE ATTACH EAR CRACKED. REMOVED AND REPLACED RT AND LT ELEVATOR TABS PER MM. 2L72 4F RTA16WE 20040610000882004061000088NE 2004 6 10 SWAA041612 220040607A75307064004 MOTOR BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE FAILED A SWAAK NONE EF VIBRATION/BUFFET FLT CONT AFFECTED NRNOT REPORTED 1 SW29312SW 23334 722235 AT 8000 FT AND BELOW EXPERIENCED SEVERAL LOUD BUMPS WHICH SHOOK. THE AIRCRAFT SOURCE SEEMED TO BE FROM RIGHT, SIDE SLIGHT YAW (NOT IN PEDALS). REMOVED AND REPLACED NR 2 ENGINE VBV MOTOR AND BLEED VALVE, PER MM. REMOVED AND REPLACED NR 2 ENGINE MEC AND CIT SENSOR PER MM. 2L72 4F4 FRTA16WE E2GL 20040610001042004061000104NM 2004 6 10 SWAA041570 120040603A57536546431 STRUCTURE BOEING737 7373H4 1384600NM LT FOREFLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW296021W 27953 DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD FORE FLAP L/E, CRACKED. REMOVED AND REPLACED LT FORE FLAP PER MM. 2L72 4F RTA16WE 20040610001442004061000144NE 2004 6 10 DL76S040501 220040530A7250 TURBINE BLADES BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 2 ENGINE DAMAGED A DALAK NONE M OVER TEMP TOTAKEOFF 1 SO27135DL45415 25145 580362 RT ENGINE EGT 950 ON TAKEOFF FOR LESS THAN ONE MINUTE. FOUND LPT BLADES DAMAGED AND BROKEN PER FIM. REPLACED NR 2 ENGINE PER JIC CARD DECK 1T145. C/W NR 2 ENGINE PREFLIGHT AND LEAK CHECKS, NO DISCREPANCIES NOTED. 2L72 4F4 FRTA1NM E13NE 20040610001472004061000147NM 2004 6 10 DL73S040503 120040602A5311 FRAME BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27316DL 23088 FOUND ON W-2 LETTER CHECK CORROSION LOWER FRAME INBOARD OF STR 27L AT STA 1006. REPAIRED PER SRM 53-10-4 FIG 10. 2L72 4F RTA16WE 20040610001512004061000151NM 2004 6 10 DLM88040470 120040527A3240S4916997BS65008 CONTROL CABLE DOUG MD88 MD88 3023688NM BRAKE SYSTEM BROKEN A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27993DL 53345 RT BRAKE PEDAL HAS EXCESSIVE PLAY, FEELS LIKE ONE OF THE RIGHT BRAKES IS LOCKED. IT TOOK 80 PERCENT N1 TO TAXI IN WITH ONLY 123K LBS WEIGHT. FOUND RIGHT BRAKE CONTROL CABLE BROKEN AT LEFT BRAKE CONTROL VALVE. REPLACED SAME. 2L72 4F RTA6WE 20040610001632004061000163NM 2004 6 10 DL76S040472 120040527A49405198588 ECU BOEING767 767332 1382001NM GE CF6 CF680 30025NE APU MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27122DL33374 23436 P253 MCO - APU STARTER CONTINUOUSLY POWERED CAUSING OVERHEATING AND SMELL IN APU AIR. REPLACED ECU AND K117 CONTACTOR. 2L72 4F4 FRTA1NM E13NE 20040610001642004061000164NM 2004 6 10 DL757040473 120040527A4990 OIL SYSTEM BOEING757 757232 1384965NM APU LOW A DALAO OTHER J WARNING INDICATION CRCRUISE 1 SO27608DA29878 22815 P1175 APU FAULT LIGHT AND APU SHUTDOWN FOLLOWED WITH APU OIL QTY MESSAGE. SERVICED OIL. 2L72 4F RTA2NM 20040610001942004061000194NM 2004 6 10 DLM88040504 120040606A3260MS250081 POSITION SWITCH DOUG MD88 MD88 3023688NM COCKPIT FAILED A DALAO OTHER N FALSE WARNING APAPPROACH 1 SO27979DL 53266 PUT LANDING GEAR HANDLE DOWN, 3 RED BELOW 1500 FT, GEAR UNSAFE AURAL WARNING. ACCOMPLISHED CHECKLIST. EMERGENCY GEAR HANDLE PULLED 3 GREEN. EMERGENCY GEAR STOWED, 3 RED. COMPLETED CHECKLIST, STOPPED STRAIGHT AHEAD. REPLACED GEAR HANDLE POSITION SWITCH 21-89. JACKED A/C AND CYCLED GEAR THRU SEVERAL TIMES, ALL INDICATIONS NORMAL. A/C OK FOR SERVICE. 2L72 4F RTA6WE 20040610001962004061000196NM 2004 6 10 DL767040507 120040304A7697 WIRE BOEING767 767232 1385132NM NR 2 ENGINE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27103DA65081 22215 580376 DURING HMV IN GSO FOUND NR 2 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRES AND PLUGS. 2L72 4F RTA1NM 20040610001992004061000199NM 2004 6 10 DL76G040438 120040514A24210MP25059 COUPLING BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 IDG LEAKING A DALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO271607B 30388 704823 RIGHT GENERATOR DRIVE ILLUMINATED. COMPLIED WITH QRH. BPCU BITE OK, SERVICE IDG, IDG OVERFLOW PORT LEAKING. REPLACED OVERFLOW COUPLING FILTER AND CHECKED CHIP DET DRAINED AND RESERVICED IDG. RAN ENG FOR 20 MIN, OPS CHECK/LEAK CHECK OK. 2L72 4F4 FRTA1NM E13NE 20040610002222004061000222NM 2004 6 10 DLM88040457 120040524A335060030451 BATTERY PACK DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27923DL 49705 AFT EMERGENCY EXIT IDENTIFIER LIGHTS INOP. REPLACED BATTERY PACK, NOW CHECKS NORMAL. 2L72 4F RTA6WE 20040610002322004061000232NM 2004 6 10 SWAA041623 120040608A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN DEFECTIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 DURING SCHEDULED RON, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 17 ABC, DIM. REMOVED AND REPLACED BULLNOSE LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040610002332004061000233NM 2004 6 10 SWAA041624 120040608A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB AT BS 672, LBL 31, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040610002372004061000237NM 2004 6 10 SWAA041628 120040608A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1040, STRINGER 23R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040610002442004061000244WP 2004 6 10 GTIA040378 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 656-856 CORRODED AND GOUGED. REMOVED DAMAGED SECTION OF TRACK STATION 656-856. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M) 2L72 4F RTA6WE 20040610002452004061000245WP 2004 6 10 GTIA040387 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 693 TO STATION 769 LEFT SIDE OUTBOARD METALLIC PANEL CRACKED AT HAT SECTION, DISBONDED AT RUB STRIPS. RE-BONDED RUB STRIP. REMOVED HAT CHANNEL. INSTALLED HAT CHANNEL. (M) 2L72 4F RTA6WE 20040610002472004061000247WP 2004 6 10 GTIA040391 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 617-693 RIGHT OUTBOARD STRIPS DEBONDED, HAT CHANNEL DEBONDED, FLOORBOARD CRACKED. FABRICATED NEW BOARD. (M) 2L72 4F RTA6WE 20040610002482004061000248WP 2004 6 10 GTIA040377 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 1056-1136 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 1056-1136. LOCATED AND DRILLED SEAT TRACKS. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACKS AND SPLICES. (M) 2L72 4F RTA6WE 20040610002522004061000252WP 2004 6 10 GTIA040380 120040402A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CENTER CABIN FLOORBOARD STATION 256-313, CREASED ALONG UPPER SKIN, PUNCTURED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040610002532004061000253WP 2004 6 10 GTIA040381 120040402A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN CENTER FLOORBOARD STATION 579-617 HAS PEELING FIBERGLASS. FABRICATED CABIN CENTER FLOORBOARD. (M) 2L72 4F RTA6WE 20040610002582004061000258WP 2004 6 10 GTIA040385 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL STATION 541 TO 617 HAS CRACKED AND DAMAGED AT HAT CHANNEL TWO RUB STRIP MISSING ONE DISBONDED. REMOVED HAT CHANNEL. INSTALLED HAT CHANNEL. (M) 2L72 4F RTA6WE 20040610002592004061000259WP 2004 6 10 GTIA040389 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 617 TO STATION 541 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED/DAMAGED FORWARD AND AFT EDGE. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040610002602004061000260WP 2004 6 10 GTIA040363 120040317A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK 1136-1309 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 1136-1309. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. (M) 2L72 4F RTA6WE 20040610002612004061000261WP 2004 6 10 GTIA040364 120040317A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 1176-1309 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK AT STATION 1176-1309. FABRICATED SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACKS AND SPLICES. (M) 2L72 4F RTA6WE 20040610002622004061000262WP 2004 6 10 GTIA040369 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK RIGHT INBOARD STATION 436-636. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2L72 4F RTA6WE 20040610002642004061000264WP 2004 6 10 GTIA040372 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK CORRODED AND GOUGED FS 1036-1309. REMOVED DAMAGED TRACK RIGHT INBOARD STATION 1036-1309. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED TRACK SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2L72 4F RTA6WE 20040610002682004061000268WP 2004 6 10 GTIA040370 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 636-836 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK INBOARD RIGHT STATION 636-836. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED TRACK SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2L72 4F RTA6WE 20040610002722004061000272WP 2004 6 10 GTIA040359 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 1155 TO STATION 1250 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS BROKEN HALF/SEVERAL INSERTS CORRODED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040610002752004061000275WP 2004 6 10 GTIA040360 120040312A5312 BULKHEAD DOUG DC9 DC983 3022083WP FUSELAGE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND FORWARD PIT STATION 218 FORWARD BULKHEAD HAS CRACKED SUPPORT CHANNEL AND DENT LBL 7 INCHES. CUT OUT DAMAGED AREA ON WEB. FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. LOCATED AND DRILLED UPPER SUPPORT. INSTALLED UPPER SUPPORT. (M) 2L72 4F RTA6WE 20040610002772004061000277WP 2004 6 10 GTIA040362 120040317A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 200-256 CORRODED, GOUGED. REMOVED DAMAGED SECTION OF TRACK STATION 200-256. LOCATED AND DRILLED NEW SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED SEAT TRACK AND SPLICES. (M) 2L72 4F RTA6WE 20040610002802004061000280EA 2004 6 10 ASO2004F00012 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE CLIPS AT FS 280, LBL9 AND RBL9 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 AND RBL 9 ON THE LT AND RT SIDES IAW SRM. (ASOA04344) 2L72 4F4 FRTA21EA E15NE 20040610002812004061000281EA 2004 6 10 ASO2004F00013 120040507A3350BF50390901 LENS CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27707EV 10057 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR. (ASOA04337) 2L72 4F4 FRTA21EA E15NE 20040610002822004061000282EU 2004 6 10 ASO2004F00010 120040307A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK, THE LT AND RT SIDE Z-FLOOR SUPPORT WAS FOUND CORRODED BEYOND LIMITS AFT OF FRAME 39. MAINTENANCE REMOVED AND REPLACED THE CORRODED Z-FLOOR SUPPORTS IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21,2004. (ASOA04367) 2H72 4T4 TRT E20NE 20040614000542004061400054NM 2004 6 14 ASAA0440010 120040119A53206545855103 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND R-2 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 947-997. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040614000552004061400055NM 2004 6 14 ASAA0440004 120040119A5414311A145017 SKIN BOEING737 7374Q8 138447QNM NR 1 PYLON CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, NR 1 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257. REPAIR IAW EA. (M) 2L72 4F RTA16WE 20040614000572004061400057NM 2004 6 14 ASAA0440026 120040204A5414311A145017 SKIN BOEING737 7374Q8 138447QNM NR 1 PYLON CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - NR 1 PYLON SKIN CHAFED OUTBOARD SIDE AT WING INTERFACE. REPAIRED NR 1 PYLON OUTBOARD SKIN IAW ASA EA 5430-01128. (M) 2L72 4F RTA16WE 20040614000612004061400061NM 2004 6 14 ASAA0440023 120040204A532065C3397257 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND STATION 376, RBL 11, FLOOR SUPPORT SCREW HOLE HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT STATION 376, RBL 11, IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20040614000642004061400064NM 2004 6 14 ASAA0440006 120040119A53306545776106 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND SKIN CREASE AT STATION 792 TO 803 AND STRINGER 25R TO 27L. (M) 2L72 4F RTA16WE 20040614000702004061400070NM 2004 6 14 ASAA0440015 120040202A532065468861 STRUCTURE BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 AIRCRAFT DENTED AT TAIL JACK PAD AREA STATION 1088. REPAIRED IAW EA 9330-01741. (M) 2L72 4F RTA16WE 20040614000772004061400077NM 2004 6 14 ASAA0440008 120040119A53206552878U102 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND L2 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 947 TO 986. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040614001042004061400104NM 2004 6 14 ASAA0440024 120040204A5210654587512 ANGLE BOEING737 7374Q8 138447QNM R1 DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - FOUND R-1 DOOR 'L' ANGLE HAS CORROSION THE FULL LENGTH OF THE ANGLE. REMOVED AND REPLACED THE 'L' ANGLE PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20040614001092004061400109GL 2004 6 14 SIMA200413803 220040514A7200 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 1 VIBRATION A SIMAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW21834AE 145631 BOS - FLT 4669 - UNUSUAL ABNORMAL VIBRATION AND NOISE FROM NR 1 ENGINE AT 40 PERCENT N1 AND BELOW, CAN BE FELT THROUGH FLOOR, YOKE AND RUDDER PEDALS. ALSO, IN CABIN AREA. ENGINE INSTRUMENTS READ NORMAL. REPLACED NR 1 ENGINE ASSEMBLY IAW W/C 72-000-00. LEAK AND OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20040614001102004061400110SO 2004 6 14 SIMA200413501 120040513A491014526850401 FIREWALL EMB 135 EMB135KL 3260302SO APU CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21805AE 145489 SAW - FOUND CRACKS ALONG APU FIREWALL WHEN INSTALLING APU. REPLACED APU FIREWALL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040614001172004061400117GL 2004 6 14 SIMA200413201 220040509A7200 ENGINE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMABA EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SW21707EB 145195 PWM - FLT 4645 - A/C LEVEL AT 21K FT JUST ABOUT TO SET CRUISE MODE FELT YAW AND HEARD LOUD BANG NOISE. NR 1 ENGINE UNCOMMANDED SHUTDOWN. AIRCRAFT DECLARED EMERGENCY AND LANDED IN PWM. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20040614001182004061400118SO 2004 6 14 SIMA200413801 120040512A246014521325117 CONTROL PANEL EMB 145 EMB145LR 3260212SO COCKPIT SHORTED A SIMAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW21626AE 145117 MEM - FLT 3954 - THUMPING NOISE LOUD AND ABRUPT COMING FROM GEAR AREA. LOWERED GEAR AND NOISE WENT AWAY, DECLARED EMERGENCY LANDED SAFELY. DURING TAXI TO MAINTENANCE, RECEIVED ELECTRICAL EMERGENCY ABNORMAL MESSAGE. FOUND NR 2 BATTERY SWITCH INTERNALLY SHORTING IN GROUND CAUSING INTERMITTENT RAPID BUS SWITCHING RESULTING IN VARIOUS EICAS MESSAGES INCLUDING LEGU AIR GROUND FAULTS. REMOVED AND REPLACED ELECTRICAL CONTROL PANEL 22ETC. OPS CHECK GOOD IAW W/M 24-30 AND 24-61. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040614001192004061400119SO 2004 6 14 SIMA200413802 120040513A5610NP15131111 WINDOW EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21618AE 145097 ORD - FLT 4233 - CREW REPORTED SMOKE SMELL IN COCKPIT WHEN USING CAPTAIN WINDOW HEAT. REPLACED CAPTAIN WINDOW IAW AMM 56-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040614001202004061400120EU 2004 6 14 USAA040146 120040419A5320 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND BEAM CORRODED 2.8 IN BY 1.2 INCH BY .050 INCH DEEP AREA, FRAME 16, -Y1292, -Z240. CORROSION LEVEL 2, TASK NR JA-220-53500. FABRICATED AND INSTALLED ANGLE, DOUBLER, FILLER PER SRM 53-11-14, 53-1-14, 51-42-11. (M) 2L72 4F RTA28NM 20040609001602004060900160WP 2004 6 9 AALA20040560 120040515A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21556AA 53086 DEN - FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-23 FOR FORWARD ENTRY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040609001652004060900165NE 2004 6 9 AALA20040546 220040511A7532 TPU BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE LT ENGINE MALFUNCTIONED A AALAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SW21612AA 24488 31040 MCO - INFLIGHT T1208/11 LEFT ENGINE FLAMED OUT AT IDLE DURING APPROACH AT 3000 FEET. CLIMBED TO ALTITUDE AND PERFORMED SUCCESSFUL RESTART. EMERGENCY DECLARED. LANDED MCO WITHOUT INCIDENT. REPLACED TPU BVCU AND DEDICATED GENERATOR ROTOR AND STATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20040610000642004061000064NM 2004 6 10 SWAA041591 120040605A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 944, RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040610000652004061000065NM 2004 6 10 SWAA041592 120040605A53156546806 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29641SW 27714 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 860 LBL 17 TO RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040610000662004061000066NM 2004 6 10 SWAA041593 120040605A5753654643099 STRUCTURE BOEING737 7373H4 1384600NM LT FOREFLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20040610000782004061000078NM 2004 6 10 SWAA041602 120040606A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 9L, CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040610000842004061000084 2004 6 10 SWAA041608 420040607A256563562 SLIDE BOEING737 7373G7 1384595NM L1 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610000912004061000091NM 2004 6 10 SWAA041564 120040603A335007912 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29737JW 27869 EEPLS COVER AT ROW 1 ABC, MISSING. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040610000962004061000096 2004 6 10 SWAA041617 420040608A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. DISCREPANCY ALSO OCCURRED AT SJC ON SAME DAY. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040610001002004061000100NM 2004 6 10 SWAA041566 120040603A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SPV, FOUND BULKHEAD WEB AT BS 1016, BL 0, CORRODED. REPAIRED BULKHEAD WEB PER ER. 2L72 4F RTA16WE 20040610001022004061000102NM 2004 6 10 SWAA041568 120040603A573065C27045 SKIN BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED C3 CHECK, FOUND LOWER WING SKIN OUTBOARD NR 1 ENGINE, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040610001052004061000105NM 2004 6 10 SWAA041571 120040603A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 807, LBL 7, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040610001062004061000106NM 2004 6 10 SWAA041572 120040603A256065C168209 HOOK BOEING737 7373A4 1384585NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20040610001622004061000162NM 2004 6 10 DL76S040471 120040527A3397 WIRE BOEING767 767332 1382001NM CABIN SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27137DL 25306 RED EMERGENCY LIGHTS AT 25AB INOP. FOUND WIRING SHORTED AT PAX SEAT 25AB BETWEEN LWR SIDEWALL PANEL AND SEAT TRACK. REPLACED BLOWN FUSES IN M9009 AND M9010 ESCAPE PATH PWR SUPPLIES. REINSTALLED ALL LWR KICK PNLS. EMERGENCY LIGHTS ESCAPE PATH SYS OP CHECKS GOOD PER AMM. REPAIRED WIRING PER CHAP 20. 2L72 4F RTA1NM 20040610001672004061000167NM 2004 6 10 DL73S040476 120040529A26117213000000 SMOKE DETECTOR BOEING737 737247 138448DNM AFT LAVATORY DEFECTIVE A DALAK NONE N FALSE WARNING TOTAKEOFF 1 SO27243WA 23517 AFT LAV SMOKE DETECTOR CHIMES ONLY ONCE DURING TEST. REPLACED SMOKE DETECTOR. 2L72 4F A16WE 20040610001692004061000169NM 2004 6 10 DL76S040478 120040529A3350 COVER BOEING767 767332 1382001NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27128DL 24078 SEAT 4EF MISSING EMERGENCY LIGHT COVER ASSY. INSTALLED COVER ASSY. 2L72 4F RTA1NM 20040610001732004061000173NM 2004 6 10 DL764040482 120040530A3350 LENS BOEING767 767432ER 1385134NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27831MH 29702 MID GALLEY EMERGENCY PATH LIGHT MISSING LENS. INSTALLED LENS, OPS CHECK OK. 2L72 4F RTA1NM 20040610001762004061000176NM 2004 6 10 DL738040485 120040519A5753 SPAR BOEING737 737832 13844CFNM T/E FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27390DA 30536 REPAIR OF RIGHT INBOARD MAIN FLAP FRONT SPAR LOWER CHORD. 2L72 4F RTA16WE 20040610001882004061000188NM 2004 6 10 DLM88040490 120040531A2421976J2528 GENERATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27943DL 49816 725373 ABORTED TAKEOFF AT 85 KNOTS DUE TO RIGHT GENERATOR FAIL. FOUND RT GEN GCU LOOSE IN RACK. RESECURED AND RAN ENGINE GEN, STILL WOULD NOT COME ON LINE AND CAUSED X-TIE LOCKOUT. SWAPPED APU AND RIGHT GEN GCUS PER MM 24-20-07-401. RIGHT GEN STILL INOP ON RUN. X-TIE MSG RESET AFTER RIGHT CSD DISCONNECTED. APU GEN POWERS RIGHT BUS OK. X-TIE SYS CHECKED OK PER MM 24-20-00-201 TEST H. 2L72 4F4 FRTA6WE E9NE 20040610002032004061000203NM 2004 6 10 DL76S040442 120040515A2750113T200061 LINK BOEING767 767332 1382001NM T/E FLAP CORRODED A DALAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SO27117DL 23276 NR 2 LEFT I/B TRAILING EDGE FLAP I/B TORQUE TUBE LOWER ATTACH LINK CORRODED IN AFT O/B HOLE. COMPLIED WITH ERA089397-14MA REV A TIME LIMITED REPAIR NR 5. 2L72 4F RTA1NM 20040610002152004061000215NM 2004 6 10 DL76K040453 120040520A3246767300M HEAT SHIELD BOEING767 767332 1382001NM MLG CONTAMINATED A DALAF ACTIVATE FIRE EXT. BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TXTAXI/GRND HDL 1 SO27171DZ 29690 AFTER ARRIVAL AT GATE NUMBER 8 WHEEL AND BRAKE ASSY STARTED TO SMOKE HEAVILY AND SMALL FLAME FLARED UP. FOUND EXCESSIVE GREASE BUILD-UP INSIDE OF WHEEL HEAT SHIELD. REPLACED WHEEL ASSY. 2L72 4F RTA1NM 20040610002192004061000219NM 2004 6 10 DL73S040454 120040521A3350 CONNECTOR BOEING737 737232 1384475NM CABIN NOT SEATED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27301DL 23073 EMERGENCY EXIT LIGHT COME ON AND GO OUT OFF WITHOUT A POWER FAILURE. RESET PLUG ON E-PATH POWER SUPPLY. NO OCCURRENCE NOTED. 2L72 4F RTA16WE 20040610002362004061000236NM 2004 6 10 SWAA041627 120040608A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAME AT RIGHT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040610002492004061000249WP 2004 6 10 GTIA040376 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 856-1056 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 856-1056. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M) 2L72 4F RTA6WE 20040610002502004061000250WP 2004 6 10 GTIA040384 120040326A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND FORWARD CABIN STATION 200 TO 160 LBL 55 INCH SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABRICATED AND LOCATED HOLES. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040610002552004061000255WP 2004 6 10 GTIA040386 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL BARE METAL AT HAT CHANNEL DISBONDED AT RUB STRIPS ONE MISSING RUB STRIP STATION 617-693. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040610002562004061000256WP 2004 6 10 GTIA040392 120040322A5312 BULKHEAD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND FORWARD CARGO FORWARD BULKHEAD FS 218 L27L-L28L LOWER BRACKET AND B/H SKIN, BOTH HAVE CRACK. CUT OUT DAMAGED/CRACKED AREA ON B/H SKIN. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M) 2L72 4F RTA6WE 20040610002572004061000257WP 2004 6 10 GTIA040393 120040322A5531 RIB DOUG DC9 DC983 3022083WP VERTICAL STAB CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND VERTICAL STAB LOWER DORSAL FIN ACCESS PANEL SUPPORT MATING SURFACES CORRODED, SEVERAL NUTPLATES CORRODED AND MISSING. AFTER FURTHER EVALUATION, FOUND RIB CRACKED. DORSAL FIN PANEL SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED NEW PANEL SUPPORT. INSTALLED NEW PANEL SUPPORT. REMOVED AND REPLACED FORMER. (M) 2L72 4F RTA6WE 20040610002652004061000265WP 2004 6 10 GTIA040382 120040402A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN CENTER FLOORBOARD STATION 541-579 HAS PEELING FIBERGLASS. DAMAGED INSERTS. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040610002662004061000266WP 2004 6 10 GTIA040361 120040317A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 200-256 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SEAT TRACK SPLICES. INSTALLED NEW TRACKS AND SPLICES. (M) 2L72 4F RTA6WE 20040610002672004061000267WP 2004 6 10 GTIA040365 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. SEAT TRACK STATION 436-570 IS OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK AND SPLICES. (M) 2L72 4F RTA6WE 20040610002692004061000269WP 2004 6 10 GTIA040374 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 1036-1136 CORRODED AND GOUGED. REMOVED SEAT TRACK LEFT OUTBOARD STATION 1036-1136. FABRICATED SEAT TRACKS. FABRICATED SPLICES. INSTALLED LEFT OUTBOARD SEAT RACKS AND SPLICES. (M) 2L72 4F RTA6WE 20040610002712004061000271WP 2004 6 10 GTIA040383 120040326A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN RBL 55, SUBFLOOR WEB FROM STA 1136 TO 1212 IS CORRODED. FOUND STATION 1150, 1185, AND 1205 TO BE OUT OF LIMITS. FABRICATED TWO SECTION CUSP WEBS. INSTALLED CUSP WEB STATION 1098-1250. (M) 2L72 4F RTA6WE 20040610002782004061000278WP 2004 6 10 GTIA040366 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. FOUND STATION 480-636 TO BE OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATE SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M) 2L72 4F RTA6WE 20040614000672004061400067NM 2004 6 14 ASAA0440014 120040202A5311BAC1505100261 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 AFT PIT STUB FRAME HAS CORROSION AROUND NUT PLATE BS 792 BL 18R. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20040614000732004061400073NM 2004 6 14 ASAA0440007 120040119A5320654587U70 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND R-1 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 306-350. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040614001222004061400122NM 2004 6 14 USAA040187 120040429A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53435 22955 CLT - FOUND SKIN CRACKED 1.35 INCHES, STATION 760 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040614001232004061400123NM 2004 6 14 USAA040191 120040507A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU52223 23228 PIT - FOUND SKIN CRACKED 4 INCHES, FORWARD SERVICE DOOR LOWER AFT CORNER STATION 328, APPROX STRINGER 16R. INSTALLED DOUBLER, TRIPLER AND FILLERS PER EA 78356. (M) 2L72 4F RTA16WE 20040614001272004061400127NM 2004 6 14 USAA040180 120040503A5743 SUPPORT FITTING BOEING737 737301 1384611NM LT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US 23930 PIT - FOUND MLG SUPPORT FITTING CRACKED .25 INCH LONG, LEFT MLG SUPPORT FITTING REAR SPAR OF LEFT WING. REPLACED LEFT MLG SUPPORT FITTING PER EA 78221. (M) 2L72 4F RTA16WE 20040614001282004061400128EU 2004 6 14 USAA040133 120040415A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND FLOOR PANEL CORRODED 2.20 INCHES LONG BY 2.40 INCHES WIDE, FRAME 66-68 AT ENTRY L-2 DOOR, NR 261FF. CORROSION LEVEL 2, TASK NR JA-260-53100. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11. (M) 2L72 4F RTA28NM 20040614001302004061400130EU 2004 6 14 USAA040134 120040416A5321D5367175302070 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND PANEL DELAMINATED APPROX 6 SQUARE INCHES TOTAL, PANEL 262HG AFT CABIN FLOOR. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M) 2L72 4F RTA28NM 20040614001312004061400131EU 2004 6 14 USAA040135 120040416A5321D536771756001000FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND PANEL DELAMINATED AND CORRODED 7 SQUARE INCHES TOTAL, PANEL 261EG AFT CABIN FLOOR. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M) 2L72 4F RTA28NM 20040614001322004061400132NM 2004 6 14 USAA040179 120040503A5320 WEB BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US50060 23930 PIT - FOUND FLOOR WEB CRACKED 1 INCH AND 1.5 INCHES, BETWEEN STATION 559 AND 578 AT STRINGER 17L. REPLACED FLOOR WEB PER SRM 51-10-2. (M) 2L72 4F RTA16WE 20040614001352004061400135NM 2004 6 14 USAA040181 120040503A5743 SUPPORT FITTING BOEING737 737301 1384611NM RT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US50060 23930 PIT - FOUND MLG SUPPORT FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING REAR SPAR OF RIGHT WING. REPLACED RIGHT MLG SUPPORT FITTING PER EA 78221. (M) 2L72 4F RTA16WE 20040614001362004061400136NM 2004 6 14 USAA040141 120040417A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU52619 23512 CLT - FOUND SKIN CRACKED 1.5 INCHES, BS 727D S-23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040614001382004061400138NM 2004 6 14 USAA040188 120040420A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US52314 23313 CLT - FOUND SKIN CRACKED 2.5 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT STATION 344.47 WL, 207.5. INSTALLED DOUBLER EPR SRM 53-00-01. (M) 2L72 4F RTA16WE 20040614001402004061400140EU 2004 6 14 USAA040147 120040423A5347D5347217220390 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND SEAT TRACK CORRODED 1.5 INCHES BY 2.4 INCHES BY .067 INCHES DEEP AREA, BETWEEN FRAME 67 AND 68, -Y1732, -Z24. CORROSION LEVEL 2, TASK NR JA-260-53500. REMOVED AND REPLACED SEAT RACK PER SRM 53-00-15, 51-74-00, 51-42-00, 53-00-14. (M) 2L72 4F RTA28NM 20040614001412004061400141NM 2004 6 14 XC42004F00000 120040518A2400P502986 ROTOR DORNERDO32 DO328100 2996000NM EXCITER DEFECTIVE B XC4RO OTHER O OTHER NRNOT REPORTED 1 SO35353SK8253 3122 ROTOR EXCITER FAILED, DAMAGING MAIN STATOR WINDINGS. PROBABLE CAUSE: POOR DESIGN OF ROTOR ASSEMBLY. 2H72 4T RTA45NM 20040614001422004061400142GL 2004 6 14 ULX2004F00018 220040301A7323 FLYWEIGHT BENDIX BELL 206 206B 1181511SW ALLSN 250C 250C20J 03013GL GOVERNOR MALFUNCTIONED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01212LA 85400039 3957 CAE270320 N2 RPM UNSTABLE. WILL NOT HOLD N2 RPM STABILIZED. PROBABLE CAUSE: FLYWHEEL WEIGHT MALFUNCTION. 1G71 3U3 U H2SW E4CE 20040614001452004061400145WP 2004 6 14 UPS04842367 120040504A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 341. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040614001462004061400146WP 2004 6 14 UPS04842368 120040503A53203779762U1 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 680 AFT SIDE LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D & 51-3-0. 2L74 4F RT4A25 20040614001472004061400147WP 2004 6 14 UPS04842369 120040504A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 358. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040614001492004061400149EU 2004 6 14 ULX2004F00017 120040301A2435 COMMUTATOR SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE STARTER GEN INOPERATIVE B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01229LA2205 202 3317 NO OUTPUT, COMMUTATOR BAR LIFTED, BRUSHES DESTROYED. 1G71 3U3 U H9EU E19EU 20040614001502004061400150NM 2004 6 14 DL73S040510 120040608A335020131A BATTERY PACK BOEING737 737232 1384475NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27301DL 23073 FORWARD EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2L72 4F RTA16WE 20040614001522004061400152NM 2004 6 14 DL76G040511 120040608A3350 TERMINAL BOEING767 767332 1382001NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO271605 30198 SEAT 20A EMERGENCY EXIT SIGN INOP. FOUND BROKEN GROUND TERMINAL. RE-TERMINATED, CHECK GOOD. 2L72 4F RTA1NM 20040614001582004061400158EU 2004 6 14 ULX2004F00013 120040301A2435N18401 BRUSHES SNIAS 350 AS350B2 8680813EU STARTER GEN WORN B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01223LA 719 3278 BRUSHES FOUND WORN ON BRUSH CHECK. 1G71 3U H9EU 20040614001592004061400159NM 2004 6 14 DLM88040514 120040609A5270BAN7024501 SWITCH DOUG MD88 MD88 3023688NM TAIL CONE UNSERVICEABLE A DALAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO27980DL 53267 ON LAYOVER CHECK FOUND TAIL CONE EMERGENCY HANDLE CABLE UNDONE WITH NO MSG IN COCKPIT SHOWING TAIL CONE UNSAFE. REPLACED SWITCH S1-538, NOW OPS NORMAL. RECONNECTED CABLE PER M/M 53-53-00-501 STEP 7 H-K. 2L72 4F RTA6WE 20040614001612004061400161NM 2004 6 14 DL73S040515 120040610A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE FOUND IN THE LOWER SKIN OF THE S19L LAP BETWEEN BS 360 AND 540. ISSUED REPAIR VIA ERA 090436-14. 2L72 4F A16WE 20040614001622004061400162NM 2004 6 14 DL73S040516 120040610A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE S10R LAP, LOWER SKIN, BETWEEN BS 540 AND 727. ISSUED REPAIR VIA 089765-14. 2L72 4F A16WE 20040614001662004061400166EA 2004 6 14 ASO2004F00011 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING C-CHECK, THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL 27 AND RBL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL27 AND RBL27 IAW EO. (ASOA04345) 2L72 4F4 FRTA21EA E15NE 20040614001692004061400169NM 2004 6 14 DL73S040519 120040610A53306545771653 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARK DAMAGE AT STR 16L FROM STA 540 - 727. REPAIRED IN ACCORDANCE WITH ER/A 090576-14. 2L72 4F A16WE 20040614001702004061400170NE 2004 6 14 MDR04049 120040412A64106516000025103 STRAP SKRSKYS64 S64E 8142604NE M/R BLADE CRACKED A JYDRK NONE O OTHER ININSP/MAINT 1 NM09CGJZK 64003 DURING ROUTINE INSP, THE STRAP WAS FOUND CRACKED ON THE OB SIDE OF THE BLADE APPROX 9.375 INCHES FROM THE TE OF THE FAIRING THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROX 1.0 INCH. THE STRAP IS CRACKED ON THE IB SIDE OF THE BLADE APPROX 9.25 INCHES FRO THE TE OF THE FAIRING. THE CRACK STARTS AT THE CUFF END OF THE BLADE AND EXTENDS TOWARD THE TIP END OF THE BLADE APPROXIMATELY 1.5 INCHES. THESE CRACKS START WHERE THE LE OF THE FAIRING SLIDES BETWEEN THE STRAP AND THE CHANNEL ASSY. PROBABLE CAUSE IS ROUGH EDGES ON SKIN. 2G72 4U H4EA 20040614001712004061400171NM 2004 6 14 DL73S040520 120040610A5330654577550 SKIN BOEING737 737247 138448DNM FUSELAGE TORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 TEAR IN THE UPPER FUSELAGE SKIN ADJACENT TO THE STR 25 R LAP JOINT. DAMAGE TO BE INCORPORATED INTO LAP SPLICE REPAIR. AREA REPAIRED IN ACCORDANCE WITH ERA 090580-14. 2L72 4F A16WE 20040614001752004061400175NM 2004 6 14 DLM88040445 120040517A5330593602161 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27993DL 53345 DAMAGE WAS NOTED JUST AFT OF THE AFT LAV SERVICE DOOR CUTOUT. DAMAGE WAS FOUND IN THE SKIN AND UNDERLYING DOUBLER. DAMAGE WAS REMOVED AND AREA REPAIRED PER ERA 090262-14. 2L72 4F RTA6WE 20040614001772004061400177NM 2004 6 14 DL76S040447 120040518A2761271002216 ACTUATOR BOEING767 767332 1382001NM NR 5 SPOILER CRACKED A DALAK NONE K FLUID LOSS TOTAKEOFF 1 SO27134DL 25123 A/C LOST CENTER HYD SYSTEM PRESSURE AND QTY. REPLACED NUMBER 5 SPOILER ACTUATOR FOR CRACKED HOUSING. 2L72 4F RTA1NM 20040614001782004061400178NM 2004 6 14 DL764040449 120040518A5753 BUSHING BOEING767 767432ER 1385134NM T/E FLAP WORN A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27832MH 29704 WHEN FLAPS DOWN LINKAGE ON THE RIGHT OUTBOARD FLAP INBOARD TRACK WAS FOUND LOOSE. SEVERAL WORN AND FLAT BUSHINGS ON THE CARRIAGE ASSY. REPAIRED OR REPLACED DAMAGED PARTS. 2L72 4F RTA1NM 20040614001812004061400181WP 2004 6 14 UPS04842371 120040505A5314 ATTACH ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 KEEL BEAM WEB ATTACH ANGLE IS CRACKED AT STATION 857 RBL 6. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5613920 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040614001822004061400182WP 2004 6 14 UPS04842373 120040506A5320 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 RINGER DOUBLER IS CORRODED BEYOND LIMITS ON LEFT MLG, WHEEL WELL UPPER PRESSURE WEB AT STATION 960-980 LBL 65. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-7-1 FIG 10 AND SRM 51-1-20D. 2L74 4F RT4A25 20040614001842004061400184WP 2004 6 14 UPS04842375 120040503A5320 STRAP DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14L. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5895045 AND SRM 51-1-21. 2L74 4F RT4A25 20040614001852004061400185NM 2004 6 14 RYN2004F00015 120040427A5312 BULKHEAD BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CORRODED E RYNAK NONE O OTHER ININSP/MAINT 1 CE078878Z 21451 AT C-CHECK, FOUND CORROSION AROUND FASTENERS, IN THE FORWARD PIT AFT BULKHEAD CENTER PANEL. 2L73 4F4 F A3WE E2EA 20040614001862004061400186NM 2004 6 14 RYN2004F00017 120040501A5320213734 WEB BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A RYNAO OTHER O OTHER NRNOT REPORTED 1 CE078878Z 21451 AT C-CHECK, FOUND 1.5 INCH CRACK IN WEB, AT STA 1181, RBL 52. 2L73 4F4 F A3WE E2EA 20040614001882004061400188NM 2004 6 14 RYN2004F00013 120040429A5320 TRANSITION PANEL BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE GOUGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE078878Z 21451 AT C-CHECK, FOUND GOUGE AND CORROSION IN LT TRANSITION PANEL, FWD PIT STA 710, LBL 20. 2L73 4F4 F A3WE E2EA 20040614001892004061400189NM 2004 6 14 RYN2004F00016 120040429A5320 WEB BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A RYNAO OTHER O OTHER NRNOT REPORTED 1 CE078878Z 21451 AT C-CHECK, FOUND CRACK AND GOUGE IN INNER WEB, FORWARD CARGO COMPARTMENT, AFT CARGO DOOR CUTOUT, STATION 620. 2L73 4F4 F A3WE E2EA 20040614001932004061400193NM 2004 6 14 RYN2004F00018 120040502A5320 TRANSITION PANEL BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE078878Z 21451 AT C-CHECK, FOUND FOUR CRACKS IN TRANSITION PANEL, IN AFT PIT STATION 850B TO 1090. 2L73 4F4 F A3WE E2EA 20040614001962004061400196EU 2004 6 14 ASO2004F00005 120040310A3350 SOCKET AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS2661 405 DURING C-CHECK, THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR WAS FOUND TO HAVE A DAMAGED AND CORRODED SOCKET. MAINTENANCE REMOVED AND REPLACED THE DAMAGED AND CORRODED EXTERNAL EMERGENCY LIGHT ASSY. (ASOA04372) 2H72 4T4 TRT E20NE 20040614002052004061400205 2004 6 14 GAIA04071 420040427A22102588880901 COUPLER BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE YAW DAMPNER MALFUNCTIONED A GAIAO OTHER O OTHER NRNOT REPORTED 1 SW07281KH 21105 DEPARTURE, FLIGHT, WITH AIRSPEED CHANGES, AIRCRAFT YAW CHANGES NOTICEABLY. AFTER RUDDER IS RETRIMMED AIRCRAFT DUTCH ROLLS A FEW TIMES IN A JERKING MANNER. WITH INCREASING SPEEDS MORE RT TRIM IS REQUIRED. CREW RETURNED TO DEPARTURE AIRPORT, WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED LOWER YAW DAMPNER COUPLER. YAW DAMPNER AND RUDDER OPS CHECK AND INDICATES NORMAL ON GROUND TEST. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20040614002062004061400206 2004 6 14 SWAA041646 420040610A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040614002132004061400213EA 2004 6 14 ASO2004F00014 120040510A5210601R3190169 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MAIN PAX BINDING A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27835AS14209 7258 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHEKS GOOD. AIRCRAFT OK FOR SERVICE. (ASOA04340) 2L72 4F4 FRTA21EA E15NE 20040614002172004061400217NE 2004 6 14 MDR04047 120040316A6210151520604000 SPAR SKRSKYS64 CH54B 8142610NE M/R BLADE CRACKED A JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09159AC1381 64084 THE BLADE WAS REMOVED FROM THE AIRCRAFT DUE TO A RED BIM INDICATION. DURING A 10 DAY LEAK CHECK, LOSS OF PRESSURE WAS NOTED. FURTHER INVESTIGATION FOUND A .6250 INCH CRACK LOCATED ON TOP OF BLADE. THE CRACK IS LOCATED 142.5 INCHES FROM TIP END, 6.75 INCH FROM LEADING EDGE, AND 19.5 INCH FROM TRAILING EDGE OF POCKET. APPEARS CRACK ORIGINATED FROM IMPACT/EROSION/CORROSION PIT. 2G72 4U H6EA 20040614002192004061400219NE 2004 6 14 MDR04045 120040310A6320643520017019 HOUSING SKRSKYS64 CH54B 8142610NE MGB CRACKED A JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09159AC 2215 64084 DURING ROUTINE FIELD MAINTENANCE INSPECTIONS, A CRACK WAS DISCOVERED UNDER NR 2 INPUT (ARM PIT) APPROXIMATELY 6 INCHES LONG FROM APPROXIMATELY THE 5 TO 8 OCLOCK POSITION. THIS WAS VERIFIED BY FPI. PROBABLE CAUSE IS UNKNOWN. 2G72 4U H6EA 20040614002232004061400223CE 2004 6 14 GUU2004F00017 120040523A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO175354518008 UE185 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040614002262004061400226EU 2004 6 14 ASO2004F00006 120040307A5315 FLOORBEAM AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27640AS 405 DURING C-CHECK INSPECTION, THE FLOORBEAMS AT FRAMES 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAMS IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21,2004. (ASOA04371) 2H72 4T4 TRT E20NE 20040614002302004061400230EA 2004 6 14 ASO2004F00016 120040506A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CENTER WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO. 2L72 4F4 FRTA21EA E15NE 20040614002312004061400231NM 2004 6 14 UIEA200400097 120040525A541465B9405326 SKIN BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 2 PYLON WRINKLED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D CHECK AT SIN. DURING MAINTENANCE INSPECTION, FOUND NR 2 PYLON RT SIDE SKIN WRINKLED. DAMAGE WAS FOUND IN FOUR BAYS OF THE RT SUBJECT SKIN ASSEMBLY AFT OF NAC STA 286. THE DAMAGES ARE JUS AFT OF THE STRUT LARGE TITANIUM DOUBLER. SUBJECT SKIN ASSEMBLY WAS REPAIRED BY TRIMMING THE AFFECTED AREA OF THE DENT DAMAGE AND INSTALLING REPAIR DOUBLERS TO RESTORE STRUCTURE TO DESIGN CAPABILITY. 2L74 4F4 F A20WE E23EA 20040614002352004061400235SO 2004 6 14 CHQA000482 120040507A3397 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11258 145768 LEFT AFT FLOOR ARROW EMERGENCY LIGHT STRIP DOES NOT WORK. REPAIRED BROKEN WIRE ON PLUG SP9114 IAW EMB145 WM 1520 CHAP 20-00-03-1. OPS CHECKS GOOD AT THIS TIME. 2L72 4T RTT00011AT 20040614002402004061400240SO 2004 6 14 CHQA000484 120040503A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11269 145293 EMERGENCY LIGHT OVERHEAD FWD CABIN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN FWD CABIN OVERHEAD POSITION. 2L72 4T RTT00011AT 20040614002412004061400241NE 2004 6 14 ALG2004F00024 120040515A3260 BRACKET SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE WOW SWITCH OUT OF ADJUST E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03860AL 760527 20601TEC WHEN RETRACTING LANDING GEAR AFTER TAKEOFF THE RED GEAR UNLOCKED LIGHT CAME ON. RECYCLED GEAR WITH SAME AFFECT. RETURNED TO GNO WITH GEAR LOCKED IN THE DOWN POSITION. MAINTENANCE INSPECTED LANDING GEAR FOUND WEIGHT ON WHEEL SWITCH BRACKET SLIGHTLY OUT OF AFJUSTMENT, ADJUSTED BRACKET AS REQUIRED. 1G72 3U3 UNCH1NE E19EU 20040614002422004061400242EA 2004 6 14 ASO2004F00015 120040510A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27867AS 7463 DURING A GROUND INSPECTION, THE FIRST FIVE SEGMENTS OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040614002442004061400244CE 2004 6 14 GUU2004F00015 120040519A324030204A BRAKE ASSY BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT MLG WORN A GUUAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO1781538 UE199 DURING TAXI, RT SIDE BRAKING ACTION NOT ADEQUATE. REMOVED AND REPLACED NR 3 BRAKE ASSEMBLY. BLED BRAKES. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040614002492004061400249EU 2004 6 14 ULX2004F00010 120040301A2435 SHAFT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE STARTER GEN SHEARED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01228LA 3316 DRIVE SHAFT FOUND SHEARED. PROBABLE CAUSE: GENERATOR BROUGHT ON LINE WITH HIGH ELECTRICAL LOAD. RECOMMENDATION: PILOT BRING ON LINE WITH LOW LOAD AND THEN ADD LOAD. 1G71 3U3 U H9EU E19EU 20040614002502004061400250CE 2004 6 14 GUU2004F00016 120040523A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO175354518008 UE185 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040614002542004061400254SO 2004 6 14 CHQA000489 120040505A3350 LIGHT EMB 135 EMB135LR 3260305SO EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11845 145551 LEFT SIDE FUSELAGE UPPER EMERGENCY LIGHT INOP. OPS CHECKED GOOD IAW E33-50-00-710-001. 2L72 4F RTT00011AT 20040610001402004061000140NM 2004 6 10 DL757040497 120040601A3350 LIGHT BOEING757 757232 1384965NM EXTERIOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27676DL 25981 4R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA2NM 20040610001662004061000166NM 2004 6 10 DL76G040475 120040528A2460BACC18X25 CIRCUIT BREAKER BOEING767 767332 1382001NM COCKPIT POPPED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO271613B 32776 A/C HAD NUMEROUS FAULTS AND WARNINGS AND THE CREW DECLARED AN EMERGENCY. AFTER EMERGENCY DECLARED THE CREW FOUND THE DC STBY C/B POPPED ON THE P-6 PANEL DOWN BY THE FLOOR. RESET THE C/B AND ALL SYSTEMS NORMAL. MTC DID A FUNCTIONAL CHECK OF THE STBY POWER SYSTEM. ALL SYSTEM CHECK OK. 2L72 4F RTA1NM 20040610001752004061000175NM 2004 6 10 DL76K040484 120040530A3350 LIGHT BOEING767 767332 1382001NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27173DZ 29692 OVERHEAD EMERGENCY LIGHTS AT FWD F/A POSITION MID GALLEY AND SEAT ROW 47 INOP. RELAMPED, ALL CHECKED GOOD PER MM33. 2L72 4F RTA1NM 20040610001972004061000197 2004 6 10 DL76L040508 420040531A31604058650931 CDU BOEING767 767332 1382001NM COCKPIT FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27199DN 28456 FIRST OFFICER FMS/CDU BLANKED IN FLIGHT. RETURNED TO JFK FOR REPAIRS. REPLACED CDU. 2L72 4F RTA1NM 20040610002112004061000211NM 2004 6 10 DL76S040452 120040520A3350387 LIGHT BOEING767 767332 1382001NM EXTERIOR INOPERATIVE A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO27136DL 23146 1L DOOR SLIDE LIGHT INOP. REPAIRED SAME. 2L72 4F RTA1NM 20040610002212004061000221NM 2004 6 10 DLM88040456 120040523A2530 OVEN DOUG MD88 MD88 3023688NM AFT GALLEY MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27990DL 53342 AFT GALLEY - FUMES (ELECTRICAL) WERE DETECTED, NO SMOKE. ALL GALLEY CB'S WERE PULLED, ODOR DISAPPEARED. FOUND FWD OVENS IN AFT GALLEY AT FAULT. REPLACED SAME. 2L72 4F RTA6WE 20040610002462004061000246WP 2004 6 10 GTIA040388 120040427A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 389 TO STATION 465 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED ON EDGES/SEVERAL INSERTS DAMAGED. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040610002632004061000263WP 2004 6 10 GTIA040368 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 1036-1309 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK RIGHT OUTBOARD STATION 1036-1309. FABRICATED SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M) 2L72 4F RTA6WE 20040610002702004061000270WP 2004 6 10 GTIA040375 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 NM01836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 256-456 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 256-456. LOCATED AND DRILLED HOLES ON SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M) 2L72 4F RTA6WE 20040614000512004061400051EA 2004 6 14 A6WA200440063 120040510A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31434AW 7322 FOUND RIGHT FS 718 FRAME FLANGE CRACKED BETWEEN STRINGERS 10R AND 12R. REMOVED DAMAGED FLANGE, PERFORMED NDT, FITTED AND INSTALLED REPAIR DOUBLER IAW BOMBARDIER REO 601R-53-61-193 REV A. (M) 2L72 4F RTA21EA 20040614000522004061400052EA 2004 6 14 A6WA200440062 120040510A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31434AW 7322 FOUND LEFT FS 718 FRAME FLANGE CRACKED BETWEEN STRINGERS 10L AND 12L. REMOVED DAMAGED FLANGE, PERFORMED NDT, FITTED AND INSTALLED DOUBLER BOMBARDIER REO NR 601R-53-61-19. (M) 2L72 4F RTA21EA 20040614000532004061400053EA 2004 6 14 A6WA200440056 120040430A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31402AW 7281 FLIGHT ATTENDANT REPORTING GASSY FUMES IN VICINITY OF GALLEY, IRRITATING TO NOSE, THROAT AND EYES. INSPECTED INTERNAL/EXTERNAL OF AIRCRAFT, NO EVIDENCE OF UNUSUAL SMELL. APU AND PASSENGER OPS NORMALLY. REVIEWED AIRCRAFT HISTORY. NO RECORD OF SMOKE. (M) 2L72 4F RTA21EA 20040614000562004061400056NM 2004 6 14 ASAA0440025 120040204A5414311A145017 SKIN BOEING737 7374Q8 138447QNM NR 2 PYLON WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - NR 2 PYLON SKIN WORN INBOARD SIDE 22-30 INCHES FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON INBOARD SKIN IAW ASA EA 5430-01128. (M) 2L72 4F RTA16WE 20040614000592004061400059NM 2004 6 14 ASAA0440019 120040204A5420S302T001219 HOUSING BOEING737 7374Q8 138447QNM NR 1 PYLON WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 NR 1 ENGINE PYLON SPHERICAL BEARING OUTER RACE IS LOOSE IN HOUSING UPPER SPAR ATTACHMENT FITTING FOR UPPER LINK. REMOVED AND REPLACED NR 1 ENGINE PYLON SPHERICAL BEARING, PYLON CROWN BEAM, IAW ASA EA 5440-01011, TYPICAL REPAIR. (M) 2L72 4F RTA16WE 20040614000632004061400063NM 2004 6 14 ASAA0440005 120040119A5414311A145018 SKIN BOEING737 7374Q8 138447QNM NR 2 PYLON WORN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, NR 2 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257 RIGHT. REPAIR IAW EA. (M) 2L72 4F RTA16WE 20040614000852004061400085NM 2004 6 14 ASAA0440009 120040119A53206517688U165 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01763AS 25100 GYR - DURING MAINTENANCE CHECK, FOUND L1 DOOR CREASE BEAM Z-CHANNEL IS CORRODED FROM BS 306 TO 342. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040614000912004061400091NM 2004 6 14 ASAA0440035 120040204A5414311A145017 SKIN BOEING737 7374Q8 138447QNM NR 2 PYLON WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - NR 2 PYLON SKIN WORN OUTBOARD SIDE 22-30 INCH FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON SKIN OUTBOARD IAW ASA EA 5430-01128. (M) 2L72 4F RTA16WE 20040614001012004061400101NM 2004 6 14 ASAA0440022 120040204A575365C348126 FLAP TRACK BOEING737 7374Q8 138447QNM T/E FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - NR 2 FLAP TRACK HAS PITTING ON LOWER SIDE OF THE UPPER TRACK. REPLACED FLAP TRACK FITTING PER AMM 27-51-49. (M) 2L72 4F RTA16WE 20040614001252004061400125NM 2004 6 14 USAA040189 120040505A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US51091 23934 CLT - FOUND SKIN CRACKED 1.8125 INCH CRACK STATION 727D, STRINGER 24R. DOUBLER INSTALLED PER SRM 53-00-01, DETAIL X1, FIG 229. (M) 2L72 4F RTA16WE 20040614001392004061400139NM 2004 6 14 USAA040182 120040503A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US50060 23930 PIT - FOUND FLOORBEAM CORRODED, STATION 986.5. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED INTERCOSTAL STRUCTURE BETWEEN STATION 986.5 AND 100.6 PER SRM 52-10-02. (M) 2L72 4F RTA16WE 20040614001512004061400151EU 2004 6 14 ULX2004F00011 120040301A2435150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE FAILED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01233LA 845 3366 NO OUTPUT, REPAIRED 3.1 HOURS EARLIER. UNKNOWN CAUSE OF FAILURE. 1G71 3U3 U H9EU E19EU 20040614001562004061400156EU 2004 6 14 ULX2004F00009 120040301A2435150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE VIBRATION B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01229LA 3317 REMOVED FOR EXCESSIVE VIBRATION. BRUSHES DESTROYED, ENDBELL BEARING LINER WORN. 1G71 3U3 U H9EU E19EU 20040614001732004061400173NM 2004 6 14 DL73S040522 120040610A533065457788 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS ON THE FUSELAGE SKIN AT STRINGER 10R BETWEEN STA 986 T0 1016. AREA REPAIRED IAW ER/A 089689-14. 2L72 4F A16WE 20040614001832004061400183WP 2004 6 14 UPS04842374 120040505A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 1580 FRAME IS CORRODED BEYOND LIMITS RIGHT SIDE AT CUSP LEVEL. REMOVED FRAME SECTION, FABRICATED FRAME SECTION AND REPAIR ANGLES AND INSTALLED IAW SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20040614001972004061400197EU 2004 6 14 ASO2004F00007 120040307A5315 FLOORBEAM AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE FLOORBEAM AT FRAME 36 NEAR THE SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM. AIRCRAFT WAS RELEASED FORM C-CHECK ON MARCH 21, 2004. (ASOA04370) 2H72 4T4 TRT E20NE 20040614002072004061400207 2004 6 14 SWAA041647 420040610A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040614002162004061400216CE 2004 6 14 GUU2004F00014 120040320A55201016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO176954916805 UE194 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BACKET. 2L72 4T3 TRTA24CE E2NE 20040614002182004061400218NM 2004 6 14 SWAA041649 120040610A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 19 DEF, INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040614002252004061400225SO 2004 6 14 CHQA000463 120040212A3350 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11287 145460 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2L72 4T RTT00011AT 20040614002332004061400233CE 2004 6 14 ZSE2004F00000 120040525A212157033 FAN CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE MOTOR BEARING BINDING E ZSEAO OTHER O OTHER NRNOT REPORTED 1 CE01555KT 1290 5500420 7115152 APPROXIMATELY 15 MILES FROM ARRIVAL AIRPORT, COCKPIT AND CABIN INDICATED SIGS OF SMOKE/FUMES WITH ELECTRICAL ODOR. ALL FANS WERE SHUTDOWN AND CHECKLISTS COMPLETED. WITHIN A COUPLE OF MINUTES, AIR BEGIN TO CLEAR AND LANDING MADE A FEW MINUTES LATER. 2210 HOURS OF AIRCRAFT FLIGHT TIME REMAINED BEFORE SCHEDULED REPLACEMENT. 1L72 4F4 F A22CE E1NE 20040614002552004061400255SO 2004 6 14 CHQA000491 120040505A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11845 145551 MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT BULB IAW 135 AMM CH 33-50-10-4. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20040614002592004061400259EU 2004 6 14 ULX2004F00014 120040301A2435 ARMATURE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE STARTER GEN SHORTED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01225LA3279 375 3308 ARMATURE SHORTED, BRUSHES RIVETS CAME LOOSE. PROBABLE CAUSE: EXCESSIVE AMPERAGE. MONITOR ELECTRICAL LOAD DURING OPERATION. 1G71 3U3 U H9EU E19EU 20040614002602004061400260NM 2004 6 14 RYN2004F00019 120040503A5320 DOUBLER BOEING737 73725A 1384481NM PWA JT8 JT8D9 52048NE FUSELAGE TORN A RYNAO OTHER O OTHER NRNOT REPORTED 1 CE078878Z 21451 AT C-CHECK, FOUND TEAR IN R-1 DOOR THRESHOLD DOUBLER, AT STATION 392. 2L72 4F4 FRTA16WE E2EA 20040614002622004061400262EU 2004 6 14 ULX2004F00016 120040301A2435 BRUSHES SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE STARTER GEN INOPERATIVE B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01221LA 8841 3220 NO OUTPUT, PROBABLE CAUSE: BRUSHES DESTROYED, BRUSH SPRINGS DAMAGED, ARMATURE GROOVED. HIGH AMPERAGE. MONITOR LOAD DURING USING. 1G71 3U3 U H9EU E19EU 20040614002672004061400267EU 2004 6 14 USA2004F00034 120040508A2120 ODOR AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19710UW 1019 ENROUTE, DURING DESCENT, THE CABIN CREW REPORTED A PUNGENT ODOR IN THE CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE CABIN, CARGO, AND AVIONICS COMPARTMENTS. NO ABNORMALITIES FOUND. OK FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20040614002682004061400268EU 2004 6 14 USA2004F00035 120040514A4990 APU AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE APU BAY SHUTDOWN A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19101UW 0936 ENROUTE, WITH THE NR 2 ENGINE INTEGRATED DRIVE GEN (IDG) ON MINIMUM EQUIPMENT LIST (MEL), THE AUXILARY POWER UNIT (APU) SHUT DOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE THE NR 2 ENGINE IDG AND REMOVED MEL. THE APU WAS THEN PLACED ON MEL. FURTHER ACTION IS PENDING. 2L72 4F4 FRTA28NM E2GL 20040614002702004061400270EA 2004 6 14 UIA9314 120040427A541485410588 SKIN DHAV DHC8 DHC8311 1386006EA LT NACELLE CRACKED Z K NONE O OTHER ININSP/MAINT 1 TW0015221 325 DURING TX CHECK FOUND LT NACELLE IB SKIN WAS CRACKED. REPAIR IAW RD-8-54-1900 RD-8-57-2830 RD-8-57-2832 TO BE DONE BY THE MFG OEM REPAIR TEAM. 2H72 4T RTA13NM 20040614002722004061400272EA 2004 6 14 COMA0460339 120040528A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 COMPLY WITH E.O. 53-027 S/B 601R-53-055 (718 FRAME). COMPLIED WITH E.O. 53-027 S/B 601R-53-055. 2L72 4F RTA21EA 20040614002742004061400274NM 2004 6 14 AWXA200400577 120040526A3350900835A BATTERY BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE EMERGENCY LIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 DEN - EEL - DURING 4-DAY CHECK THE OVERHEAD (CEILING) EMERGENCY EXIT LIGHT AT SEAT ROW 9 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK AT BS 617, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2EA 20040614002752004061400275NM 2004 6 14 AWXA200400575 120040525A5270 WARNING LIGHT BOEING737 7373U3 13844CCNM L-2 DOOR ILLUMINATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28335AW 28740 ON TAKEOFF, EN ROUTE, RECEIVED L-2 DOOR WARNING INDICATION, REJECTED TAKEOFF AT LESS THAN 60 KTS. FLIGHT CREW RE-SECURED L-2 DOOR AND WARNING LIGHT EXTINGUISHED, AIRCRAFT DEPARTED TO LAS. UPON ARRIVAL IN LAS MAINTENANCE INSPECTED THE L-2 DOOR PROXIMITY SWITCH AND DOOR OPERATION, NO DEFECTS WERE NOTED. DUE TO RECENT HISTORY OF L-2 DOOR WARNING INDICATIONS A FOLLOW UP WAS WRITTEN TO RE-INSPECT THE PROXIMITY SWITCH AND PERFORM A SOFT LATCH INSPECTION. MAINTENANCE PERFORMED L-2 DOOR RIG CHECK, OPERATION OF DOOR WAS GOOD WITH HANDLE HAVING A POSITIVE OVER CENTER. DISCOVERED JAM NUT ON SENSOR ADJUSTMENT PLATE LOOSE, READJUSTED PROXIMITY SENSOR AND SECURED AND SAFETIED JAM NUT. 2L72 4F RTA16WE 20040614002762004061400276EU 2004 6 14 AWXA200400579 120040527A2121 FAN AIRBUS320 A320231 3930325EU CABIN SEIZED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 WP28621AW 053 ON APPROACH, EN ROUTE FROM SNA AN ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT BURNING ODOR AND FOUND EXTRACT FAN SEIZED, REMOVED AND REPLACED EXTRACT FAN. CONFIRMED FAILURE OF EXTRACT FAN S/N 4091. UNIT SEIZED DUE TO CONTACT BETWEEN IMPELLER AND BELLMOUTH. FRONT FLANGE CENTER HOLE WAS WORN BEYOND TOLERANCE AND BEARING WERE BROKEN. REPLACED FRONT FLANGE & BEARINGS; BLENDED IMPELLER & BELLMOUTH, BALANCED ROTOR & MOTOR/IMPELLER, AND FUNCTIONALLY TESTED UNIT IAW CMM 21-26-42, REV. 6. 2L72 4F RTA28NM 20040614002772004061400277SO 2004 6 14 CHQA000487 120040509A3350 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11299 145532 RIGHT SIDE AFT EXTERNAL EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED RIGHT SIDE AFT EXTERNAL EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040614002782004061400278SO 2004 6 14 CHQA000438 120040228A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11273 145331 RIGHT AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT EMERGENCY LIGHT IAW EMB 145 MM 33-40. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040614002802004061400280SO 2004 6 14 CHQA000488 120040511A3350 LIGHT EMB 135 EMB135KL 3260302SO EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378 145593 LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT OVERWING EXTERNAL EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-10. OPS CHECKS GOOD. 2L72 4F RTT00011AT 20040614002822004061400282SO 2004 6 14 CHQA000441 120040217A3350 BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260 145128 RIGHT WING EMERGENCY LIGHT DOESN'T WORK. FOUND EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY POWER UNIT IAW EMB 145 AMM CH 33-50-04. 2L72 4T RTT00011AT 20040614002842004061400284EA 2004 6 14 COMA0460315 120040513A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01969CA 7141 CORROSION ON CARGO FLOOR CAP AT LBL 9. REMOVED AND REPLACED FLOORBEAM CAP AT LBL 9, IAW CRJ SRM 51-42-06, 51-42-13, 51-42-21, 51-42-34. 2L72 4F RTA21EA 20040614002852004061400285EA 2004 6 14 COMA0460316 120040509A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01959CA 7116 LEFT LOWER WING PLANK CRACKED. REPAIRED IAW REO 601R-57-21-130. 2L72 4F RTA21EA 20040614002862004061400286EA 2004 6 14 COMA0460317 120040509A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01959CA 7116 CARGO BAY FLOOR SUPPORT ANGLE STRUCTURE CRACKED. REPAIRED IAW REO 601R-53-61-004. 2L72 4F RTA21EA 20040614002872004061400287CE 2004 6 14 DXTA200400294 120040416A326065430087 UPLOCK SWITCH CESSNA560 560XL 2076702CE RT MLG FAULTY E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07603QS 5605203 AFTER TAKEOFF AND GEAR WAS SELECTED UP, HYDRAULIC PRESS LIGHT CAME ON, STAB MIS-COMPARE AND GEAR UNLOCK LIGHTS ALSO CAME ON. CORRECTED STAB MIS-COMPARE, HYD PRESS AND WAS GEAR UNLOCK LIGHT STAYED ON. RECYCLED GEAR ONE TIME, WHEN GEAR WAS SELECTED UP GOT SAME LIGHT INDICATION AGAIN. TROUBLESHOT AND FOUND HIGH RESISTANCE SPIKES ON RIGHT MLG UP-LOCK SWITCH WHEN ACTUATED. REMOVED AND REPLACED RT MAIN GEAR UP-LOCK SWITCH, OPS CHECKED GOOD IAW CITATION 560XL MM CHAPTER 32-60-00. 2L72 4F RTA22CE 20040614002882004061400288CE 2004 6 14 DXTA200400299 120040422A3411 PITOT LINE CESSNA750 750 2076810CE PITOT/STATIC SYSCONTAMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07919QS 7500224 ON TAKEOFF ROLL AT APPROX 75 KNTS, THE MACH TRIM KICKED OFF AND ON, THEN THE YAW DAMPER KICKED OFF, MASTER CAUTION CAME ON, ABORT TAKEOFF. FOUND PITOT MASTS FULL OF WATER, PURGED OUT WATER WITH NITROGEN. PERFORMED LEAK CHECK OF PITOT SYSTEM IAW CESSNA 750 MM CHAPTER 34-11-01. 2L72 4J RTT00007WI 20040614002892004061400289CE 2004 6 14 DXTA200400300 120040422A3246 NUT DUNLOP RAYTHNDH125 HAWKER800XP 7150012CE LT MLG MISSING E DXTAK NONE O OTHER ININSP/MAINT 1 GL07838QS ZK181 258338 ON PREFLIGHT DISCOVERED 10 NUTS MISSING ON THE LEFT INBOARD MAIN WHEEL, ONLY 2 NUTS HOLDING WHEEL TOGETHER. REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL ASSEMBLIES. ALL WORK DONE IAW HAWKER 800XPMM CHAPTER 32-40-12. 2L72 4F RTA3EU 20040614002922004061400292WP 2004 6 14 UPS04842376 120040503A5320 STRAP DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14R. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5895045 AND SRM 51-1-21. 2L74 4F RT4A25 20040614002932004061400293WP 2004 6 14 UPS04842377 120040504A5210 ANGLE DOUG DC8 DC871F 302199DWP L1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 L-1 DOOR LOWER AFT CORNER HAS CRACKED L-ANGLE. REMOVED, FABRICATED AND REPLACED L-ANGLE IAW SRM 52-3-1 FIG 1, AND SRM 51-1-21. 2L74 4F RT4A25 20040614002962004061400296SO 2004 6 14 C2XA04SH283 120040514A532014521725615 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV-DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040614002972004061400297SO 2004 6 14 C2XA04SH285 120040514A491014526850401 FIREWALL EMB 145 EMB145 3260210SO APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP END OF THE RIGHT HAND VERTICAL STIFFENER. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040614002982004061400298SO 2004 6 14 4013 220040514A7200 ENGINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ2Y BHCJ2YF2 GL RIGHT SHUTDOWN E BSYAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 GL0758WA TH201 823786R DZ793 EN ROUTE, THE RT ENGINE SHUTDOWN ON ITS OWN, PILOT FEATHERED THE ENGINE AND LANDED, NO PROBLEM. MAINT.CHECKED FOR WATER IN FUEL (NONE FOUND),CHECKED OIL FILTER (NOTHING FOUND),CHANGED PLUGS FOR PRECAUTIONARY MEASURES. TRIED TO RUN ENGINE COULD ONLY GET 800RPM, CHECKED UNFEATHERING ACCUMULATOR IT WAS OK, BUT DID FIND OIL IN THE AIR SIDE OF THE PROP DOME, SWAPPED PROP FROM LT ENGINE, RT ENG RAN FINE. INSTALLED OVHL PROP ON LT ENGINE. GOING TO DO A TEST FLT ON AIRCRAFT BEFORE RELEASING FOR 135 FLT. MECHANIC COULD NOT FIND ANY REASON FOR ENGINE TO COMPLETELY SHUT DOWN IN FLT, FULL POWER GROUND NORMAL. 1L72 3O3 O 3A16 E5CE 5 CP37EA 20040614003002004061400300EU 2004 6 14 RAIA00405008 120040507A2120 COOLING TURBINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP RIGHT MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03565HK 41082 RT DUCT OVER TEMP INDICATION. MAINTENANCE DEFERRED RT FLOW SYSTEM IAW MEL 21-18. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING COOLING TURBINE. 2L72 4T3 TRTA41NM E2WE 20040614003012004061400301NM 2004 6 14 ABXA040177 120040518A5250H312761 STOP BOEING767 767231 1385131NM PWA JT9 JT9D* NE COCKPIT DOOR BROKEN A ABXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL23709AX 22572 COCKPIT ENTRY DOOR CAME OPEN AND THEN JAMMED DURING TAXI AND COULD NOT BE OPENED. COCKPIT DOOR LATCH BROKEN. REPLACED BROKEN DOOR STOP IAW 767 SRM 51-40-2. 2L72 4F4 FRTA1NM E20EA 20040614003032004061400303WP 2004 6 14 ABXA040184 120040521A3230 DRAG LINK DOUG DC9 DC941 302207NWP PWA JT8 JT8D1 52044NE NLG MALFUNCTIONED A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23958AX 47760 NOSE GEAR WOULD NOT EXTEND WHEN GEAR LEVER WAS PLACED DOWN. FOLLOWED ABNORMAL AND PULLED EMERGENCY GEAR EXTENSTION LEVER. NOSE GEAR EXTENDED AND LOCKED. RESET HANDLE. REPLACED RT NOSE LANDING GEAR DOOR HINGES IAW SRM 51-30-1 AND ADJUSTED NOSE LANDING GEAR DOORS IAW MM 32-22-01-2. REPLACED NOSE GEAR OVER CENTER LINKS AND LOWER DRAG LINK IAW MM 32-21-03-04. SWUNG GEAR SEVERAL TIMES WITH NO ABNORMALITIES. 2L72 4F4 F A6WE E2EA 20040614003042004061400304EU 2004 6 14 CX7A194J0430 120040524A2611CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CARGO BAY MALFUNCTIONED A CX7AF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 GL03316CE 340B348 DISCHARGED NR 1 CARGO FIRE EXTINGUISHER FOR CARGO SMOKE WARNING. 2L72 4T4 TRTA52EU E8NE 20040614003052004061400305NM 2004 6 14 ANCF200400011 120040604A27804952287401 SWITCH DOUG MD80 MD83 3023681NM SLATS FAILED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23583AN2693323110 53183 DURING TAKE OFF WARNING FLAPS WAS PRESENTED WITH DISAGREE LIGHT ON MOMENTARILY BACK TO TAKE OFF. STALL WARNING COMPUTERS WAS CHECKED FOR FAULT CODE AND THEY SHOW FLAPS FAIL, RESET WAS ACCOMPLISHED AND TEST WAS PERFORMED IAW AMM NOT DUPLICATED FAIL. FLAP/SLAT HANDLE POSITION SWITCH AND TRANSMITTER WAS REPLACED IAW AMM 27-80-07 PAGE 201-204, TEST OF FLAP/SLAT HANDLE CAM SWITCH WAS SATISFACTORY IAW AMM 27-80-07 PAGE 205-207. PSEU WAS REPLACED IAW AMM 32-60-04 PAGE 201-2002, AUTOMATIC TEST WAS SATISFACTORY IAW AMM 32-60-04 PAGE 201 P/N OFF-ON 4952287-503 S/N OFF AV07 S/N ON AV04.AUTO SPOILER SWITCHING UNIT WAS REPLACE IAW AMM 27-60-09/109. 2L72 4F RT 20040614003062004061400306WP 2004 6 14 GTIA040452 120040512A716059304645503 NOSE COWL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 1 INLET DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23809NK 49503 NR 1 INLET COWL HAS A DENT AT 5 O`CLOCK POSITION. REMOVED AND REPLACED NOSE COWL. 2L72 4F4 FRTA6WE E2EA 20040614003082004061400308NM 2004 6 14 EIA2004036 120040513A7932 WARNING SYSTEM BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE COCKPIT ACTIVATED A EIAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM09481EV 19896 663044 NR 2 ENGINE OIL QUANTITY DECREASED TO 1/16 LOW OIL PRESS LIGHT ILLUMINATED. SHUT DOWN NR 2 ENG AT 0305Z WINDMILL OIL PRESSURE 15 PSI FOR 57 MINUTES. 2L74 4F4 F A20WE E20EA 20040614003122004061400312WP 2004 6 14 GTIA040455 120040311A5730 PANEL DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE LT WING CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 LT L/E WING PANEL NR 1165C EXFOLIATED CORROSION AROUND FASTENER HOLES. FABRICATED NEW PANEL. 2L72 4F4 F A6WE E2EA 20040614003152004061400315WP 2004 6 14 GTIA040458 120040310A5313 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 AFT PIT 1099 STR 29R CORRODED. REMOVED LONGERON 29R FROM STA 1136 TO 1003. FABRICATED NEW LONGERON SECTIONS FROM STA 1003 TO 1068.875 AND FROM STA 1068 TO STA 1136. FABRICATED LONGERON SPLICE. INSTALLED LONG 29R AND SPLICE FROM STA 1003-1136. 2L72 4F4 F A6WE E2EA 20040614003162004061400316WP 2004 6 14 GTIA040459 120040326A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 AFT CARGO FS 1022-1034, SKIN HAS CORRODED AT SKIN JOINT. REMOVED SPLICE DOUBLER FROM EXTERNAL SKIN. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN SPLICE AND DOUBLER. FABED FINGER DOUBLERS. INSTALLED NEW SKIN SPLICE AND DOUBLER AND FINGER DOUBLERS. 2L72 4F4 F A6WE E2EA 20040614003172004061400317WP 2004 6 14 GTIA040457 120040322A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 RT SIDE FUSELAGE JUST AFT OF AFT CARGO DOOR WATER WASTE DRAIN AND SURROUNDING SKIN CORRODED. CUT OUT DAMAGED AREA. FABED DOUBLER. FABRICATED INTERNAL DOUBLER. FABRICATED FILLER. INSTALLED DOUBLERS AND FILLER. 2L72 4F4 F A6WE E2EA 20040614003232004061400323WP 2004 6 14 IXXA0400024S 120040216A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL91910 46003 DURING A ROUTINE C-CHECK INSPECTION RIGHT INBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS STA XW.104.000-110.000 MAJOR REPAIR. MAINTENANCE PERFORMED MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-21A PG 1-4. FABRICATED NEW PLATING (2024T30.040") IN ACCORDANCE WITH 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF PLATING IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 57-7-1 PG 2, DC8 STRUCTURAL REPAIR MANUAL 51-1-21A PG 1-4, DC8 STRUCTURAL REPAIR MANUAL 51-3-0 PG 1. 2L74 4F RT4A25 20040614003242004061400324 2004 6 14 GTIA040454 420040314A2565 CABLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE TAILCONE SLIDE DISENGAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 EVACUATION SLIDE COVER AT TAILCONE SECURITY CABLE LT SIDE DISENGAUGED. RESECURED LT SECURITY CABLE. 2L72 4F4 F A6WE E2EA 20040614003252004061400325WP 2004 6 14 GTIA040453 120040513A3260833703 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE MLG INOPERATIVE A GTIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL23820NK 49126 LT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. DURING ARRIVAL INTO FLL. QRH C/W GEAR DOOR OPEN EXTINGUISH WITH HYDRAULIC SYSTEM HI. 3000 GEAR DOOR LIGHT ILLUMINATED AGAIN WITH HYDRAULIC SYSTEM IN 1500 PSI LOW POSITION. CLEANED AND ADJUSTED LT GEAR DOOR PROXIMITY SWITCH AND REMOVED AND REPLACED LT MLG UP AND LATCH PROXIMITY SWITCH. CHECK NORMAL ON GROUND. 2L72 4F4 F A6WE E2EA 20040614003282004061400328WP 2004 6 14 GTIA040461 120040308A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 DENT AT FS 58.75 BELOW RT CUSP LINE. REMOVED DAMAGED AREA 10.2500 X 16.5000. FABRICATED FILLER, DOUBLER, AND PLATE EA 5330-0410. INSTALLED REPAIR PARTS. 2L72 4F4 F A6WE E2EA 20040614003302004061400330WP 2004 6 14 GTIA040462 120040411A5313 LONGERON DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 AFT PIT LONGERON 29L AT STA 1193 HAS CORROSION UNDER LIP AT HI LOC ATTACH POINT. REMOVED SECTION OF LONG 29L FROM FS 1127-1202. FABRICATED NEW LONGERON. FABRICATED NEW LONGERON SPLICE. INSTALLED STRINGER SPLICE. INSTALLED LONGERON SECTION. 2L72 4F4 F A6WE E2EA 20040614003332004061400333 2004 6 14 MWEA040076 420040513A342570515V1 INDICATOR DOUG MD88 MD88 3023688NM COCKPIT INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31601ME 49762 THE POWER OFF FLAG APPEARED & STAYED IN VIEW ON THE STANDBY HORIZON GYRO. REMOVED AND REPLACED STANDBY HORIZON INDICATOR. 2L72 4F RTA6WE 20040614003342004061400334 2004 6 14 GTIA040467 420040519A2565 LANYARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE L2 DOOR SLIDE DISCONNECTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 L2 DOOR SLIDE PACK NEEDS REATTACHED. REATTACHED L2 SLIDE PACK LANYARD. 2L72 4F4 F A6WE E2EA 20040614003352004061400335WP 2004 6 14 GTIA040466 120040517A3231 DOOR DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE MLG INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23811NK 48017 ENROUTE, THE GEAR DOOR OPEN LIGHT CAME ON. TURNED ON THE HYD`S AND THE LIGHT WENT OUT. AFTER TURNING OFF THE HYD`S THE LIGHT CAME BACK ON. TURNED ON RT HYD AND LEFT IN HI. PERFORMED PROXIMITY TEST, MAIN GEAR DOORS, TEST PASSED. VERIFIED GEAR DOOR ROLLER AND HOOK MEASUREMENTS, WITHIN TOLERANCES CLEANED GEAR DOOR PROXIMITY SWITCHES. 2L72 4F4 F A6WE E2EA 20040614003362004061400336NM 2004 6 14 AWXA200400502 120040509A5270189915 PROXIMITY SENSOR BOEING737 7373U3 13844CCNM L2 DOOR OUT OF ADJUST A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28335AW 28740 SEA - ABORTED TAKEOFF - FLT 0154 - ON TAKEOFF ROLL AT SEA EN ROUTE FOR PHX L-2 DOOR WARNING LIGHT ILLUMINATED, REJECTED TAKEOFF AT 133 KTS. FLIGHT CREW CONFIRMED L-2 DOOR WAS SECURE, MAINTENANCE CONTROL ISSUED MEL 52-3, COND 1, L-2 DOOR WARNING LIGHT INOP. MAINTENANCE FOUND THE L-2 DOOR WARNING PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED PLUNGER TO PROXIMITY SENSOR TARGET IAW BMM 52-71-11, TASK 822-014-B00, OPERATIONAL CHECK OF DOOR WARNING SYSTEM WAS GOOD. 2L72 4F RTA16WE 20040614003392004061400339NM 2004 6 14 F3LA200400059 120040430A5330 SKIN AIRBUSA319 A319111 3930336NM FUSELAGE GOUGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03918FR 1943 INSPECTION REPORTED A GOUGE IN LT AFT FUSELAGE JUST FWD OF PRESSURE BULKHEAD, ZONE 261, STR 19L. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-41-11 FIG 105. REPAIRED DAMAGE PER SRM 53-00-11, 51-42-11, 51-47-00, 51-21-11, 51-23-00 AND 51-76-16. 2L72 4F RTA28NM 20040614003402004061400340 2004 6 14 MWEA040077 420040513A342570515V1 HSI DOUG DC9 DC981 3022081WP COCKPIT INOPERATIVE A MWEAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL31805ME 48031 STANDBY GYRO WILL NOT REMAIN ERECT, NO FLAG NOTED. REMOVED AND REPLACED STANDBY HORIZON INDICATOR. 2L72 4F A6WE 20040614003422004061400342NM 2004 6 14 MWEA040073 120040512A53135953050121 LONGERON BOEING717 717200 1383700NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31916ME 55179 LONGERON 25 LEFT DAMAGED AT STATION 422. SPLICED IN NEW SECTION OF LONGERON. 2L72 4F TRA6WE 20040614003442004061400344 2004 6 14 P5CA0401091 420040511A3445G551501 SPEAKER BOEING747 7472F6B 1384807NM COCKPIT FAILED A P5CAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 WP23534MC 21832 TCAS FAILED IN FLIGHT. REPLACED TCAS SPEAKER, OPS CHECK OK MM 34-45-00. 2L74 4F A20WE 20040614003452004061400345EA 2004 6 14 QXEA200400315 120040510A5210CC67038600951 DOOR CNDAIRCL600 CL6002C10 1390015EA PAX DOOR MALFUNCTIONED A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09601QX6150 10009 DEN - FLIGHT 4011 - MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE DOOR AND PERFORMED OPERATIONAL CHECKS. NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040614003482004061400348NM 2004 6 14 SWAA041655 120040610A2560P2070001 FLASHLIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29729SW 27861 DURING SPV, FOUND FWD UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20040614003492004061400349NM 2004 6 14 SWAA041651 120040610A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040614003522004061400352NM 2004 6 14 SWAA041654 120040610A335090083 BATTERY BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29713SW 27847 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS AT ROW 17 ABC AND AFT GALLEY FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040614003532004061400353NM 2004 6 14 SWAA041631 120040608A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040614003542004061400354NM 2004 6 14 SWAA041632 120040608A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040614003552004061400355NM 2004 6 14 SWAA041633 120040608A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND RIGHT CREASE BEAM WEB AT BS 467, STRINGER 17R, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20040614003562004061400356NM 2004 6 14 SWAA041656 120040609A53109078824 STRAP BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 L1 DOOR FRAME LOWER HINGE STRAP UPPER CORNER, CRACKED. REPAIRED L1 DOOR FRAME HINGE STRAP PER EA. 2L72 4F RTA16WE 20040614003572004061400357NM 2004 6 14 SWAA041657 120040610A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040614003582004061400358NM 2004 6 14 SWAA041658 120040607A531065C346701 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED UPPER AND LOWER HINGE BOX FITTINGS PER SRM. 2L72 4F RTA16WE 20040614003592004061400359NM 2004 6 14 SWAA041659 120040610A5753654782124 SPINDLE BOEING737 7372H4 138448CNM T/E FLAP BROKEN A SWAAK NONE F FLT CONT AFFECTED APAPPROACH 1 SW29083SW 22732 ON SHORT FINAL HEARD A POP FOLLOWED BY A SLIGHT ROLL TENDENCY TO THE LEFT. LANDED NORMALLY. FOUND LEFT OUTBOARD FLAP INBOARD SPINDLE BROKEN. REMOVED AND REPLACED LEFT WING INBOARD AND OUTBOARD FLAP SPINDLES PER MM. 2L72 4F A16WE 20040614003602004061400360NM 2004 6 14 SWAA041634 120040609A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 FORWARD RIGHT EMERGENCY EXIT LIGHT LENS, MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040614003612004061400361NM 2004 6 14 SWAA041635 120040609A3350101114 LENS BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LOWER LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040614003622004061400362NM 2004 6 14 SWAA041636 120040609A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040614003632004061400363 2004 6 14 SWAA041637 420040609A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040614003652004061400365NM 2004 6 14 SWAA041639 120040609A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040614003682004061400368NM 2004 6 14 SWAA041642 120040609A3350101073 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT ROW 1 DEF, MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040615000012004061500001WP 2004 6 15 GTIA040523 120040518A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 CABIN STA 522-541 STR 18R WEB CORRODED. FABBED WEB. INSTALLED WEB. 2L72 4F4 FRTA6WE E2EA 20040615000022004061500002WP 2004 6 15 GTIA040524 120040519A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 CABIN FLOOR WEB CRACKED STA 1176, LBL 18 INCHES. FABRICATED DOUBLER REPAIR AND FILLER. INSTALLED WEB DOUBLER REPAIR AND FILLER. 2L72 4F4 FRTA6WE E2EA 20040615000042004061500004WP 2004 6 15 GTIA040529 120040520A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 CABIN RT IB SEAT TRACK LT CORRODED AND WORN STA 200-1309. MATERIAL FOUND OUT OF LIMITS FROM STA 200 TO 267. REMOVED RT, IB SEAT TRACK. FABRICATED NEW SECTION SEAT TRACK. INSTALLED SEAT TRACK. 2L72 4F4 FRTA6WE E2EA 20040615000052004061500005WP 2004 6 15 GTIA040530 120040512A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 LT OB CABIN SEAT TRACK LT CORRODED AND WORN STA 200-1309. OUT OF LIMITS FROM STA 200-300 AND 1030-1206. REMOVED LT OB SEAT TRACK STA 1030 TO 1206. INSTALLED LT OB SEAT TRACK STA 200 TO 300. FABRICATED SEAT TRACK LT OB STA 1030-1206. REMOVED LT OB SEAT TRACK FROM STA 1030-1206. INSTALLED 2 EA SPLICES. INSTALLED SEAT TRACK STA 1030-1206. 2L72 4F4 FRTA6WE E2EA 20040615000062004061500006WP 2004 6 15 GTIA040528 120040520A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 FLOOR PANEL LT IB STA 200-260 DELAMINATED EDGE. FAB NEW FLOOR PANEL. 2L72 4F4 FRTA6WE E2EA 20040615000082004061500008WP 2004 6 15 GTIA040520 120040517A5320 CUSP WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 RT OB CUSP. WEB HAS A CRACK AT STA 270 AND AT STA 278. CUT OUT CRACKED SECTIONS OF CUSP WEB AT STA 270 AND 278. FABRICATED REPAIR DOUBLERS AND SPLICES. INSTALLED REPAIR DOUBLERS. 2L72 4F4 FRTA6WE E2EA 20040615000092004061500009WP 2004 6 15 GTIA040468 120040517A7120K22199SA31 MOUNT DOUG DC9 DC983 3022083WP NR 1 ENGINE INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23825NK 53012 NR 1 ENGINE FWD LOWER VIBRATION MOUNT REQUIRES CHANGE. REMOVED AND REPLACED NR ENGINE FWD/ LWR VIBRATION MOUNT. 2L72 4F RTA6WE 20040615000102004061500010WP 2004 6 15 GTIA040469 120040514A323059164605509 CONTROL VALVE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE LT MLG LOOSE A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23820NK 49126 IN CLIMB AT GEAR RETRACT LT MAIN GEAR UNSAFE LIGHT STAYED ON WITH GEAR HANDLE UP. CK QRH AND FOLLOWED PROCEDURE WITH NO CHANGE. LEAVING 10,000 FT AND PUTTING HYD. PUMPS TO LOW AND OFF THE GEAR DOOR OPEN LIGHT ALSO CAME ON. SELECTED ENGINE PUMPS TO HIGH AND GEAR DOOR OPEN LIGHT WENT OUT. WE COULD NOT NOTICE ANY ABNORMAL VIBRATIONS LIMITED SPEED TO .70M/ 300K. L/P 1338401 ON GEAR RETRACTION LT GEAR RED LIGHT STAYED ON. FOUND LT FILLET ATTACHMENT LINK LOOSE, ADJUSTED AND TIGHTENED FILLET ATTACHMENT LINK. JACKED AIRCRAFT UP PERFORMED GEAR SWING. OPS CK GOOD, NO DEFECTS NOTED. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE. OPS AND LEAK CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. 2L72 4F4 F A6WE E2EA 20040615000112004061500011WP 2004 6 15 GTIA040470 120040520A3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NLG OUT OF LIMITS A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23820NK 49126 ON CLIMBOUT CENTER GER RED LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE (CYCLED GEAR DOWN AND UP) LIGHTS WENT OUT. JACKED AC NOSE GEAR AND PERFORMED NOSE GEAR RETRACTION TEST FOR UP/DOWN POSITION LIGHTS. NO FAULTS WERE NOTED ON SEVERAL CYCLES. FOUND RT MLG DOOR PROXIMITY SWITCH OUT OF LIMITS ON GAP CHECK. ADJUSTED GEAR DOOR TARGET. MAIN GEAR DOOR INDICATION CHECK OK W/ DOORS UP. 2L72 4F4 F A6WE E2EA 20040615000132004061500013NM 2004 6 15 GTIA040546 120040514A5320 FLOOR SUPPORT DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE FUSELAGE BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 CABIN CENTER FLOOR SUPPORT STA 845 BROKEN. REMOVED BROKEN FLOOR SUPPORT. FABRICATED LOCATED AND DRILLED NEW SUPPORT. INSTALLED FLOOR SUPPORT. 2L72 4F4 FRT E2EA 20040615000162004061500016WP 2004 6 15 GTIA040531 120040501A5753 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE LT IB TE FLAP CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 LT IB FLAP T/E, PITTING CORRODED ON SKIN. REMOVED SKIN. FABED NEW SKIN, INSTALLED NEW SKIN. 2L72 4F4 FRTA6WE E2EA 20040615000182004061500018 2004 6 15 ASMF20040603 420040603A2360 STATIC WICK BOEING757 757200 1384950NM WINGS & ELEVATORLIGHTNING STRIKEW ASMFO OTHER J WARNING INDICATION DEDESCENT 1 SW23703AM 27203 DURING DESCENT, A LIGHTING STRIKE AT RANDOM AND (WXR WEAK) LIGHT TURNED ON DURING WXR OPERATION. LIGHTING STRIKE VISUAL INSPECTION WAS PERFORMED IAW MM 05-51-09 AND NO DAMAGES WERE FOUND. THE LIGHTING STRIKE WAS DISCHARGED IN 3 STATIC DISCHARGERS, ONE IN LT AND RT WING TRAILING EDGE AND THE OTHER IN LT ELEVATOR TRAILING EDGE. DURING OVERNIGHT SERVICE THE STATIC DISCHARGERS WERE REPLACED. 2L72 4F RTA2NM 20040615000212004061500021WP 2004 6 15 ASMF200406007 120040609A300032049011 SOLENOID VALVE DOUG DC9 DC987 3022087WP ANTI ICE SYS FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23216AM1958315 49586 DURING TRANSIT CHECK, WATER WAS FOUND IN THE MIDDLE OF PASSENGERS CABIN CEILING. THE WATER LEAK WAS DETECTED BETWEEN CUSHIONS AND AIR CONDITIONING DUCT IN THE CEILING, THE EMERGENCY LOCATOR ANTENNA WAS SEALED IN THE STATIONS Y937 AND Y980 IN THE UPPER FUSELAGE. DURING OVERNIGHT SERVICE, AIR CONDITIONING DUCTS WERE CHECKED BY LEAKS IAW MM 21-20-00, PRESSURIZATION TEST WAS PERFORMED IAW MM 21-00-00, LT AND RT OVERRIDE ANTI ICE VALVES WERE REPLACED IAW MM 21-20-04, WATER SEPARATORS WERE REPLACED IAW MM 21-20-02 AND OVERRIDE ANTI ICE VALVES SENSITIVE LINES WERE REPLACED IAW MM 21-20-04, ALL CORRECT. 2L72 4F RTA6WE 20040610002422004061000242NM 2004 6 10 SWAA041629 120040608A53206545833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 188 TO BS 198, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20040610002512004061000251WP 2004 6 10 GTIA040379 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT INBOARD SEAT TRACK STATION 456-656 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 456-656. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK. (M) 2L72 4F RTA6WE 20040610002542004061000254WP 2004 6 10 GTIA040390 120040324A5321FS389465 CHANNEL DOUG DC9 DC983 3022083WP FLOORBOARD CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATION 389-465 LEFT OUTBOARD HAT CHANNEL CRACKED AND STRIP DEBONDED. REMOVED DAMAGE ON HAT CHANNEL. FABRICATED SPLICE AND HAT CHANNEL. INSTALLED NEW PIECES. (M) 2L72 4F RTA6WE 20040610002732004061000273WP 2004 6 10 GTIA040371 120040414A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 836-1036 CORRODED AND GOUGED. REMOVED TRACK RIGHT INBOARD STATION 836-1036. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M) 2L72 4F RTA6WE 20040610002742004061000274WP 2004 6 10 GTIA040358 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 256 TO STATION 313 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED/DAMAGED ON EDGE. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040610002762004061000276WP 2004 6 10 GTIA040373 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 636-836 CORRODED AND GOUGED. REMOVED LEFT OUTBOARD SEAT TRACK STATION 636-836. FABRICATED SEAT TRACK, INSTALLED SEAT TRACK AND SPLICES. (M) 2L72 4F RTA6WE 20040610002792004061000279WP 2004 6 10 GTIA040367 120040314A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 836-1030 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK RIGHT OUTBOARD STATION 836-1036. FABRICATE SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M) 2L72 4F RTA6WE 20040614000752004061400075NM 2004 6 14 ASAA0440027 120040204A554265C313931 SKIN BOEING737 7374Q8 138447QNM RUDDER TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01764AS 25101 GYR - UPON RUDDER REMOVAL FOUND DAMAGE TO UPPER SKIN OF RUDDER BALANCE ARM. REPAIRED IAW ASA EA 5540-01086. (M) 2L72 4F RTA16WE 20040614001162004061400116SO 2004 6 14 SIMA200413502 120040514A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZ STAB MALFUNCTIONED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SW21808AE 145519 BOS - FLT 4546 - MOMENTARY PITCH 1 AND 2 TRIM INOPERATIVE OCCURRING ON FINAL. FLAP AT 22 DEGREE, GEAR UP. LASTED APPROX 5 SECONDS. REPLACED HSCU. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040614001242004061400124NM 2004 6 14 USAA040190 120040504A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU46468 24515 CLT - FOUND SKIN CRACKED 1.5 INCHES, BS 727 0 PLUS 12 STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040614001432004061400143 2004 6 14 UPS04142379 420040513A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU EVAC SLIDE INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01152UP 0834 INSPECTION TYPE:N/A REF M280836 & WAN 892403, EVAC SLIDE WARNING LIGHT INOP. T/S IAW TSM 52-73-00-0 & PERFORMED OPERATIONAL TEST IAW MM 52-73-00-5 & CHECKED NORMAL WITH NO FAULTS. 2L72 4F RTA35EU 20040614001442004061400144NM 2004 6 14 UIEA200400096 120040525A541065B941383 FITTING BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D-CHECK. REWORK OF STRUT NR 1 DIAGONAL BRACE LOWER SPAR FITTING, SP 747-54A2196 REV 1. DURING ACCOMPLISHMENT OF THE TERMINATING ACTION, DAMAGE WAS FOUND AT THE UPPER MOST FASTENER HOLE ON THE RIGHT SIDE OF THE FITTING AFT VERTICAL FLANGE. THE DEFECT WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO 0.434 INCHES DIAMETER PRIOR TO FURTHER OVERSIZING TO 0.4521 INCHES DIAMETER. A SAME TYPE FASTENER AS USED WAS INSTALLED AT THE DISCREPANT LOCATION. ALL OTHER FITTING REWORK AND REFINISH WAS ACCOMPLISHED IAW WITH THE TERMINATING ACTION. 2L74 4F4 F A20WE E23EA 20040614001482004061400148NM 2004 6 14 AMTA200400543 120040509A7710 INDICATOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT MALFUNCTIONED A AMTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL11554TZ 32588 31817 ON TAKEOFF ROLL DURING MAX TO. EPR N2 AND N3 INDICATED EXCEEDENCES AT AROUND 90-100 KNOTS. CONTINUED FLYING NOTED EXCEEDENCES OF N2: 104.6 PERCENT: N3 101.5 PERCENT : 6. 2L72 4F4 FRTA2NM E12EU 20040614001532004061400153NM 2004 6 14 DL73S040512 120040608A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334DL 23105 FUSELAGE SKIN, FS 767, STR 19R CRACK ALONG CHEM-MILL 3 INCH CRACK WAS FOUND ALONG A CHEM MILL LINE. A REPAIR WAS INSTALLED PER THE 737-200 SRM 53-30-3 FIG 48. A TEAR STRAP WAS ALSO DAMAGED AND REPAIRED FOLLOWING THE SRM INSTRUCTIONS ERA 091033-14 REV A. 2L72 4F RTA16WE 20040614001642004061400164NM 2004 6 14 DL73S040517 120040610A5330 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S4R LAP SPLICE, LOWER SKIN, BETWEEN BS 259.5 AND 360. ISSUED REPAIR 089821-14. 2L72 4F A16WE 20040614001652004061400165EU 2004 6 14 ASO2004F00009 120040307A5320 BRACKET AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK INSPECTION, CORROSION WAS FOUND BEYOND LIMITS ON BOTH THRESHOLD SUPPORT BRACKETS OF PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED THE CORRODED THRESHOLD SUPPORT BRACKETS IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2H72 4T4 TRT E20NE 20040614001672004061400167NM 2004 6 14 DL73S040518 120040610A53306545771654 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARKS FOUND AT S16R BETWEEN BS 540 AND 727. DAMAGE REMOVED AND REPAIRED PER ERA 090575-14. 2L72 4F A16WE 20040614001722004061400172NM 2004 6 14 DL73S040521 120040610A5310 DOOR FRAME BOEING737 737247 138448DNM FUSELAGE UNKNOWN A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 FASTENER INSTALLATION REQUIRED RADIUS BLOCKS AND OVERSIZED FASTENER WHILE PERFORMING EO 03-055852-03AD AT THE FWD SERVICE DOOR CUTOUT AFT FRAME. VA 72553AD ISSUED AND 8110-3 RECEIVED PROVIDING APPROVAL. 2L72 4F A16WE 20040614001792004061400179NM 2004 6 14 DL73S040450 120040519A53206546568551 STIFFENER BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27245WA 23519 WHILE ACCOMPLISHING S/B 737-53A1075 A CRACKED Z-STIFFENER ON THE BS 1016 AFT P-DOME AT S23R WAS NOTED. THE STIFFENER IS LOCATED IN THE INSPECTION AREA, HOWEVER, IS NOT ONE OF THE STIFFENERS DETAILED IN THE BAC DWG. DAMAGE REMOVED AND REPAIRED VIA ERA 089941-14AD. 2L72 4F A16WE 20040614001912004061400191NM 2004 6 14 MYW2004F00001 120040425A213171211997101AC CONTROLLER BOEING737 7378Q8 13844BXNM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A MYWAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO19734MA 30039 IN FLT NR 620, HSV/LAS AUTO PRESSURIZATION FAILED. AUTO SWITCHING ACCOMPLISHED. QUICK REFERENCE HANDBOOK PROCEDURES ACCOMPLISHED. ITEM TRANSFERRED TO DMI LOG NR 1994 IAW 21-15-2B. TRANSFERRED FROM DMI LOG NR 1994. TROUBLESHOT SYSTEM. REMOVED AND REPLACED NR 1 PRESSURE CONTROLLER IAW AMM 21-31-02. SYSTEM OPS CHECKED NORMAL. CLEARED DMI. AC RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20040614002102004061400210EA 2004 6 14 ASOA04338 120040430A5260601R3198067 STEP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27707EV 10057 10057 DURING C-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. 2L72 4F4 FRTA21EA E15NE 20040614002112004061400211NM 2004 6 14 SWAA041648 120040610A3350101114 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040614002222004061400222EU 2004 6 14 ULX2004F00015 120040301A2435 STATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE STARTER GEN SHORTED A ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01228LA2742 112 3316 STATOR SHORTED, BRUSHES DESTROYED, COMMUTATOR GROOVED. EXCESSIVE AMPERAGE. MONITOR ELECTRICAL LOAD DURING OPERATION. 1G71 3U3 U H9EU E19EU 20040614002272004061400227SO 2004 6 14 CHQA000447 120040125A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11841 145737 RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT LAMP IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. LAMP P/N 1317. 2L72 4F RTT00011AT 20040614002282004061400228EA 2004 6 14 ASOA4342 120040506A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CENTER WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO. 2L72 4F4 FRTA21EA E15NE 20040614002372004061400237EA 2004 6 14 ASO2004F00017 120040505A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27856AS 7404 DURING C-CHECK, THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D. OPERATIONAL CHECKS GOOD. (ASOA04343) 2L72 4F4 FRTA21EA E15NE 20040614002392004061400239SO 2004 6 14 CHQA000483 120040501A3350 SIGN EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265 145226 RIGHT EMERGENCY EXIT ROW SIGN AT SEAT 12F INOP. FOUND TERMINAL DISCONNECTED FROM SIGN. REMOVED AND REPLACED SIGN AND NR 5 INVERTER IAW EMB145 CH 33-50-13 AND 33-50-11-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040614002532004061400253SO 2004 6 14 CHQA000476 120040406A5610163500111 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A CHQAGHA O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11294 2525 45464 FLT 6471 DFW - MSY: WHILE DESCENDING INTO MSY, CREW SMELLED SMOKE AND SAW A WHITE HAZE IN THE COCKPIT. DONNED MASKS IMMEDIATELY. SUSPECTED 115 VAC BUS SINCE IT TRIPPED OFF TWICE IN FLIGHT. AFTER TURNING OFF, SMOKE CLEARED. DECLARED EMERGENCY, LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT AND FOUND THAT THE SMOKE WAS RELATED TO NR 1 WINDSHIELD HEAT SYSTEM. SYSTEM WAS DEACTIVATED AND AIRCRAFT FERRIED TO MCO FOR WINDSHIELD CHANGE. THE WINDSHIELD WAS REPLACED AND SYSTEMS OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040614002912004061400291NM 2004 6 14 HNAA0400052 120040511A531185320103 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 FRAME X220 CORRODED AT STRINGER 31S. REMOVED AND REPLACED FRAME & VERTICAL BEAM IAW EO 8-53-04-0316. 2H72 4T RTA13NM 20040614003022004061400302WP 2004 6 14 ABXA040183 120040511A5350 LINK DOUG DC9 DC941 302207NWP PWA JT8 JT8D1 52044NE RT WING DAMAGED A ABXAK NONE E VIBRATION/BUFFET CLCLIMB 1 GL23962AX 47768 AIRCRAFT VIBRATES AT 320 KTS AT LOW ALTITUDE CLIMB AND CRUISE REGARDLESS OF POWER SETTINGS. REPLACED RT WING TO STRUCTURE TRAILING LINKS AND HARDWARE DUE TO EXCESSIVE MOVEMENT IAW MM 20-10, 20-15 & 20-16. 2L72 4F4 F A6WE E2EA 20040614003092004061400309 2004 6 14 GTIA040449 420040504A2565 STRAP DOUG DC9 DC982 3022082WP SLIDE PACK FRAYED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23820NK 49126 AFT TAIL SLIDE PACK COVER HOLD DOWN STRAP FRAYED AND PRESS GAUGE NOT IN WINDOW. REMOVED AND REPLACED FRAID COVER HOLD DOWN STRAP ON AFT TAILCONE SLIDEPACK. ADJUSTED PACK COVER SO GAUGE WAS VISIBLE. 2L72 4F A6WE 20040614003102004061400310WP 2004 6 14 GTIA040450 120040511A3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RT MLG INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23801NK 48048 ON TAKEOFF, GEAR RETRACTION RT MAIN GEAR UNSAFE LIGHT, RECYCLED GEAR LIGHT WENT OUT. ON CLEANED RT MAIN PROXIMITY SWITCH. PERFORMED PROXIMITY BOX CHECK SYSTEM OPS CHECK. 2L72 4F4 F A6WE E2EA 20040614003132004061400313NM 2004 6 14 EIA2004033 120040429A2710 CONNECTOR BOEING747 747212B 1384886NM LT AILERON DIRTY A EIAAA UNSCHED LANDING FE FLT CONT AFFECTED VIBRATION/BUFFET CLCLIMB 1 NM09485EV 20712 ON CLIMBOUT WITH FLAPS UP, NOTICED IN LEFT TURN SLIGHT BUFFETING. UPON VISUAL FOUND LEFT OUTBOARD AILERON NOT LOCKED OUT. RETURNED TO PHIK. COULD NOT DUPLICATE. CLEANED AND FOUND OILY GRIME ON LEFT HAND OUTBOARD AILERON CANNON PLUG. CHECKED VOLTAGE WITH FLAPS UNRETRACTED PIN 3 28 VOLTS DC, FLAPS DEPLOYED PIN 1 28 VOLTS DC AND PIN 2 GROUND CHECKED NORMAL PER WD 27-11-21. OPERATED AILERONS PER MM 27-11-16, OPS CHECKED NORMAL. ALSO CLEANED GROUNDS. 2L74 4F A20WE 20040614003212004061400321WP 2004 6 14 IXXA0400022S 120040214A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL91910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND L/E HOLES ELONGATED ON UPPER SKIN SURFACE, STA XFS 526.000. REPAIR ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-1 PG 1, DC8 SRM 57-3-3. REMOVED UPPER SKIN SURFACE OF LT WING CTR L/E STA SXF 526.00 IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-20D PG 21. FABRICATED AND INSTALLED NEW SKIN IAW DC8 SRM 57-3-3 PG 12. CLEANED, TREATED AND PRIMED INNER FACE OF NEW SKIN IAW DC8 SRM 51-1-8B, 51-1-21 PG 1, 51-3-0 PG 1, 51-1-20D, REFER TO NR 0275 FOR REMOVAL/REINSTALLATION OF LW WING CNT L/E. 2L74 4F RT4A25 20040614003312004061400331WP 2004 6 14 GTIA040463 120040514A3260 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE MLG DOOR INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23801NK 48048 GEAR DOOR OPEN LIGHT ILLUMINATED. DURING CRUISE. EXT AFTER 30 MIN. ADJ. RT AND LT DOOR PROXIMITY SWITCHES. OPS CHECK GOOD WITH GEAR SWING. MONITIORED DOOR LIGHT WITH NO PRESSURE AND GEAR UP. ALL INDICATIONS NORMAL. 2L72 4F4 F A6WE E2EA 20040614003322004061400332WP 2004 6 14 GTIA040465 120040517A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE UPLOCK INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23801NK 48048 RT MLG UNSAFE LIGHT ON AFTER GEAR RETRACTION. RECYCLE GEAR. LIGHT OUT. REMOVED AND REPLACED MLG UPLOCK PROXIMITY SENSOR. OPS CHECK NORMAL. 2L72 4F4 F A6WE E2EA 20040614003432004061400343NM 2004 6 14 MWEA040074 120040512A53305936434193 SKIN BOEING717 717200 1383700NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31916ME 55179 LOWER SKIN SECTION AT STATION 422 BELOW LONGERON 26 LEFT IS TORN 3 INCHES. REMOVED AND REPLACED DAMAGED SECTION. 2L72 4F TRA6WE 20040614003472004061400347SO 2004 6 14 RAIA00405006 120040509A323023092900001 UPLOCK EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03815HK12988 145048 ATL - LANDING GEAR DISAGREE MESSAGE WITH NLG UNLOCK INDICATION. MAINTENANCE REMOVED AND REPLACED NLG UPLOCK BOX. OPS CHECK OK ON RETRACTION CHECK. 2L72 4T RTT00011AT 20040614003662004061400366 2004 6 14 SWAA041640 420040609A2565D31354 SLIDE BOEING737 7375H4 138449DNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040614003672004061400367NM 2004 6 14 SWAA041641 120040609A3350101114 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29425LV 29829 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER AT ROW 15 ABC, CRACKED. REMOVED AND REPLACED LIGHT COVER PER MM. 2L72 4F RTA16WE 20040615000032004061500003WP 2004 6 15 GTIA040527 120040520A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 PAX CABIN FLOOR PANEL STA 1155-1250 DELAMINATED. FAB NEW CABIN. 2L72 4F4 FRTA6WE E2EA 20040615000072004061500007NM 2004 6 15 GTIA040545 120040512A5320 WEB DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 DENT AT FS 204 BETWEEN LONGERONS 15 AND 17L. DENT IS WITHIN ONE INCH FROM STRUCTURE AND MUST BE REPAIRED. FOUND WEB AT STA 200-207 CRACKED. FABRICATED WEB DOUBLER AND REPAIR FILLER. INSTALLED WEB DOUBLER REPAIR. 2L72 4F4 FRT E2EA 20040615000322004061500032WP 2004 6 15 ASMF200406001 120040601A5313 STRINGER DOUG DC9 DC982 3022082WP FUSELAGE LEAKING W ASMFK NONE O OTHER ININSP/MAINT 1 SW231003Y 48068 DURING TRANSIT CHECK, A WATER LEAK WAS DETECTED ON UPPER CREW CABIN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE AIRCRAFT WAS PRESSURIZED AND LEAK TEST WAS PERFORMED, DETECTING LEAKS ON STRINGER 1 FS. Y-157 TO Y-157A AND 256, STRINGER 2 AND 3 AND FS. Y-1136 TO FS. Y-1380, LT STRINGER 14 TO RT STRINGER 14. AFFECTED AREAS AND TCAS UPPER ANTENNA WERE SEALED IAW SRM 51-20-0, AND AFFECTED RIVETS WERE REPLACED AT FS. Y-207 AND STRINGER NR 1 IAW SRM 51-30-2, ALL CORRECT. 2L72 4F A6WE 20040615000342004061500034NM 2004 6 15 ASAA001A 120040124A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 DURING RECON INSPECTION, FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK THEN LIGHT TESTED NORMAL. (M) 2L72 4F RTA16WE 20040615000352004061500035NM 2004 6 15 ASAA001B 120040124A3350BACC18Z2R CIRCUIT BREAKER BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 DURING INSPECTION FOUND, THE EMERGENCY FLOOR PATH LIGHTING ON WITH SWITCH IN ARMED OR OFF POSITION. RESET THE EMERGENCY FLOORPATH LIGHTING CIRCUIT BREAKER THEN LIGHT TESTED NORMAL. (M) 2L72 4F RTA16WE 20040615000372004061500037NM 2004 6 15 ASAA0410214 120040426A531069412264 CREASE BEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND CREASE BEAM DOUBLER AT STATION 1004-1012, RBL 45-46 IS CORRODED. REMOVED DOUBLER AND INSTALLED NEW IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040615000382004061500038NM 2004 6 15 ASAA0410215 120040426A53106550568503 CREASE BEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND CREASE BEAM AT STATION 980-1016, LBL 45 IS CORRODED. REMOVED CREASE BEAM AND INSTALLED NEW IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040615000402004061500040NM 2004 6 15 ASAA0410243 120040501A5313654577738 STRINGER BOEING737 737290C 138448VNM FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND LEFT STRINGER 18 AT STA 986 IS CRACKED. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW SRM 53-10-3. (M) 2L72 4F A16WE 20040615000412004061500041NM 2004 6 15 ASAA0410238 120040501A53156554909501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND C-CHECK, FOUND FLOORBEAM AT STATION 807, LBL 24-44 IS CORRODED AT AFT END UPPER T-CAP. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA5310-02353. (M) 2L72 4F A16WE 20040615000422004061500042NM 2004 6 15 ASAA0410237 120040501A5315656714034 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND C-CHECK, FOUND FLOORBEAM AT STATION 727B, RBL 25-45 IS CORRODED AT NUTPLATES. REMOVED DAMAGE AND INSTALLED RPR ANGLES IAW EA5310-02357. (M) 2L72 4F A16WE 20040615000432004061500043NM 2004 6 15 ASAA0410234 120040501A5315655490510 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM AT STATION 480 UPPER FLANGE SURFACES CORRODED. REMOVED DAMAGED AND INSTALLED RPR STRAPS IAW EA5310-02356. (M) 2L72 4F A16WE 20040615000482004061500048NM 2004 6 15 ASAA0410231 120040501A53156554909501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND FLOORBEAM AT STATION 807, RBL 44-RBL 60 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA5310-02353. (M) 2L72 4F A16WE 20040615000502004061500050NM 2004 6 15 ASAA0410227 120040501A531565498851 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM AT STATION 986, LBL 15 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR ANGLE AND STRAP IAW SRM 53-10-9. (M) 2L72 4F A16WE 20040615000522004061500052NM 2004 6 15 ASAA0410225 120040501A53156554908501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT STATION 787 IS CORRODED AROUND FASTENER HOLES. REMOVED DAMAGE AND INSTALLED RPR STRAP, ANGLES AND STIFFENERS IAW EA5310-02360. (M) 2L72 4F A16WE 20040615000542004061500054NM 2004 6 15 ASAA0410223 120040105A534765549721 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND SEAT TRACK AT STATION 887-940, BL 0 HAS SEVERE CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED REPLACEMENT SECTION IAW SRM 51-20-1. (M) 2L72 4F A16WE 20040615000562004061500056NM 2004 6 15 ASAA0410221 120040426A5320657940151 SEAL BOEING737 737290C 138448VNM LT MLG WW CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND LEFT WHEEL WELL BLADE SEAL LANDING HAS CORROSION AND BARE METAL AT TOP SURFACE. REMOVED DAMAGED LANDING AND INSTALLED NEW IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040615000572004061500057NM 2004 6 15 ASAA0410210 120040426A52456548685116 SKIN BOEING737 737290C 138448VNM A/C BAY DOOR DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND RIGHT AIR CONDITIONING BAY DOOR IS DISBONDING. REBONDED ALUMINUM FOIL PLY IAW EA 5240-01114. (M) 2L72 4F A16WE 20040615000582004061500058NM 2004 6 15 ASAA0410212 120040426A532065673931 INTERCOSTAL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK- FOUND ANGLE ON INTERCOSTAL AT STATION 980-986, LBL 45 IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND REPLACED INTERCOSTAL IAW 51-30-2. (M) 2L72 4F A16WE 20040615000592004061500059NM 2004 6 15 ASAA0410236 120040501A532065621101 THRESHOLD BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND C-CHECK MAIN CARGO DOOR THRESHOLD WEB IS CORRODED AROUND FASTENER HOLES. REMOVED DAMAGE AND INSTALLED RRR DOUBLER IAW EA 5310-02355. (M) 2L72 4F A16WE 20040615000612004061500061NM 2004 6 15 ASAA0410219 120040426A5313655162816 STRINGER BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND C-CHECK, FOUND CORROSION UNDER LIP OF STRINGER 24L AT STATION 986. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW 53-10-2. (M) 2L72 4F A16WE 20040615000652004061500065NM 2004 6 15 ASAA0410241 120040501A57536571909118 SKIN BOEING737 737290C 138448VNM TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP ASSEMBLY LOWER SURFACE HAS BARE METAL AND IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA5750-01948. (M) 2L72 4F A16WE 20040615000662004061500066NM 2004 6 15 ASAA0410240 120040501A716065ND5430010 NOSE COWL BOEING737 737290C 138448VNM NR 2 ENGINE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND NR 2 ENGINE NOSE COWL CRACK EMINATING FROM FASTENER HOLE. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW EA7110-01233. (M) 2L72 4F A16WE 20040615000672004061500067NM 2004 6 15 ASAA0410239 120040501A783065MK784216 SHROUD BOEING737 737290C 138448VNM NR 2 ENG T/R PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND NR 2 ENGINE THRUST REVERSER LWR INBOARD SIDE SKIN IS PUNCTURED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA7830-01329. (M) 2L72 4F A16WE 20040615000682004061500068NM 2004 6 15 ASAA0410228 120040501A53156546568 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM AT STATION 1016, RBL 5-40 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT UPPER CHORD IAW EA5310-02354. (M) 2L72 4F A16WE 20040615000692004061500069NM 2004 6 15 ASAA0410192 120040413A53156546811514 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND FLOORBEAM TOP SURFACE AT STATION 1006, RBL 1-LBL 12 IS CORRODED. REMOVED DAMAGED RPR, INSTALLED REPLACEMENT RPR ANGLES IAW SRM 53-10-9. (M) 2L72 4F A16WE 20040615000712004061500071NM 2004 6 15 ASAA0410194 120040413A531369353642 STRINGER CLIP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND STRINGER CLIP AT STATION 986, STRINGER 19L IS CORRODED. REMOVED DAMGAED CLIP AND INSTALLED REPLACEMENT CLIP IAW SRM 51-20-1. (M) 2L72 4F A16WE 20040615000732004061500073NM 2004 6 15 ASAA0410201 120040420A531065232562 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND SHEAR TIE AND FRAME AT STATION 986, BETWEEN STRINGER 18L AND 19L IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE AND NEW FRAME SPLICE IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040615000752004061500075NM 2004 6 15 ASAA0410196 120040420A5347655496818 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND SEAT TRACK AT STATION 370-468 IS WORN AND GOUGED. REMOVED DAMAGED SECTION AND INSTALLED RPR SEAT TRACK SECTION IAW SRM 53-10-5. (M) 2L72 4F A16WE 20040615000772004061500077NM 2004 6 15 ASAA0410198 120040420A531565671407 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STATION 540-650. OPENED UP HOLES, INSPECTION WITH HFEC, TREATED AND PRIMED AREA IAW EA 5310-02341. (M) 2L72 4F A16WE 20040615000792004061500079NM 2004 6 15 ASAA0410203 120040420A53476554968509 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK FOUND SEAT TRACK INBOARD FLANGE AT STATION 420-480, RBL 24 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040615000902004061500090NM 2004 6 15 SWAA041662 120040611A335010107451 LENS BOEING737 7373H4 1384600NM ROW 23 DEF LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT SIGN LENS AT ROW 23 DEF, LOOSE. SECURED EMERGENCY EXIT SIGN LENS PER MM. 2L72 4F RTA16WE 20040615000922004061500092NM 2004 6 15 SWAA041664 120040611A335007912 STRIP BOEING737 7375H4 138449DNM ROWS 10 - 13 ABCWORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED C2 CHECK, FOUND EEPLS FLOOR STRIP AT ROW 10 ABC TO ROW 13 ABC, WORN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20040615000962004061500096EA 2004 6 15 SWIA200413340 120040408A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DOOR SILL CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 PAX DOOR SILL BRACKETS AND CLEATS AT FS 316 AND FS 343 CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SILL BRACKETS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13. 2L72 4F4 FRTA21EA E15NE 20040615000982004061500098EA 2004 6 15 SWIA200413342 120040408A5310 FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 MAIN FUSELAGE; PRESSURE FLOOR/WING TIE BEAM FITTING IS DENTED AND CRACKED ALONG LOWER FLANGE; LBL 3.0 FS 460.00. DISCOVERED DURING C-CHECK INSPECTION. NEW TIE BEAM FIT, DRILLED AND INSTALLED IAW CRJ SRM 51-40-11. 2L72 4F4 FRTA21EA E15NE 20040615001022004061500102WP 2004 6 15 ABXA040179 120040506A53135911423103 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23948AX 47065 BULGE AT STA 889 - 1005 LONGERON 17 LEFT - 18 LEFT. REPLACED CORRODED SECTION OF LONGERON IAW DC-9 SRM 53-02. 2L72 4F A6WE 20040615001032004061500103EA 2004 6 15 SWIA200413298 120040505A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 FS 280 LT FLOORBEAM LBL 9.0 ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-21-11 2L72 4F RTA21EA 20040615001042004061500104EA 2004 6 15 SWIA200413299 120040505A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 FUSELAGE PULLEY INTERCOSTAL HAS I/B AND O/B ANGLES CRACKED AT FS 484.00 LBL 27.0 AND 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV ''A'' . 2L72 4F RTA21EA 20040615001052004061500105NM 2004 6 15 EIA2004032 120040424A2821 FILTER BOEING747 747132 1384882NM PWA JT9 JT9* 52054NE NR 1 ENGINE CONTAMINATED A EIAAA UNSCHED LANDING XRJENGINE FLAMEOUT PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 NM09481EV 19896 662327 AT FL 360 IN CRUISE NR 1 ENG SLOWLY SPUN DOWN AND THEN APPEARED TO FLAMEOUT. EPR WAS SET AT 1.41 AT THE TIME. ATTEMPTED TO RESTART BUT NR 1 ENGINE DID NOT RESTART. REPLACED NR 1 ENG FUEL FILTER PER MM 73-11-08. PERFORMED LEAK CHECK, ALL OK. INSP FRONT VISUAL AND REAR OF ENGINE. PERFORMED IDLE RUN OF ENG FOUND N1 INOP ON RT EIDS SYSTEM DISPLAY UNIT. REPORTED BITE IS FAILURE ON FUEL FLOW COMP. REMOVED & REPLACED RT EIDS DISPLAY AND GROUND RUN PER MM 77-40-09. N1 OK. NOTE: FOUND NR 1 IGN SYSTEM INOP ON NR 1 ENGINE (ENTERED ON LOG PAGE 250514 ITEM M1202). FOUND NR 1 FUEL FILTER HEAVLY CONTAMINATED. REMOVED & REPLACED FUEL FILTER. CHECKED COARSE/ FINE FILTER ON FMC, BOTH CLEAN. CLEANED ALL C/P ON EIDS S2L74 4F4 F A20WE E20EA 20040615001072004061500107SO 2004 6 15 SWIA200413331 120040414A5420 SUPPORT EMB 120 EMB120ER 3260203SO LT MLG WW DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 CRACKED VERTICAL SUPPORT ON INBOARD SIDE OF LEFT WHEEL WELL WHERE ENGINE CABLES RUN THROUGH. REPLACED VERTICAL SUPPORT AT INBOARD SIDE OF LEFT NACELLE IAW SRM 120 51-10-02 PG 2 SEC 2B. 2L72 4T RTA31SO 20040615001092004061500109SO 2004 6 15 SWIA200413333 120040414A5310 SUPPORT EMB 120 EMB120ER 3260203SO COCKPIT WIDOW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 CAPTAIN'S DV WINDOW AFT SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT BRACKET IAW 120 SRM 51-10-02 PAR 3. P/N: 120-12545-001. 2L72 4T RTA31SO 20040615001102004061500110SO 2004 6 15 SWIA200413334 120040414A5410 SUPPORT CHANNEL EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL AT INBOARD IAW EMB120 SRM 51-10-02 SEC 2 ITEM C. 2L72 4T RTA31SO 20040615001142004061500114EA 2004 6 15 SWIA200413338 120040519A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07934SW8 8 7722 RECEIVED O/B GROUND SPOILER FAULT AND FLT SPOILERS FAULT STATUS MSGS WHILE ON SHORT APPROACH TO SLC. REMOVED AND REPLACED NR 1 AND NR 2 SECU'S REF AMM 27-61-05. OPS CHECK GOOD. NR 2 SECU S/N OFF: 01715. 2L72 4F RTA21EA 20040615001152004061500115 2004 6 15 SWIA200413339 420040517A2210 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07251YV 120251 ON ROTATION RECEIVED TRIPLE CHIME WITH TRIM FAIL AND AUTO PILOT, APT AP/FD FAILURE WITH FD FLAG ON CAPT EADI. CB E33 POPPED. RERACKED CAPT AP COMPUTER, TESTED AP SYSTEM, ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA31SO 20040615001162004061500116WP 2004 6 15 ABXA040175 120040513A323039147385001 BUNGEE CYLINDER DOUG DC9 DC941 302207NWP NLG FAILED A ABXAL ABORTED APPROACH O OTHER APAPPROACH 1 GL23958AX 47760 EN ROUTE TO ILN, WHILE EXTENDING THE GEAR, THE NOSE LANDING GEAR DID NOT EXTEND. RECEIVED A GEAR UNSAFE LIGHT. CREW DID A GO-AROUND AND DECLARED AN EMERGENCY. EXTENDED THE GEAR MANUALLY AND THE NOSE GEAR CAME DOWN, ALL INDICATION NORMAL. FOUND THE NOSE GEAR BUNGEE CYLINDER TO BE FAULTY. REMOVED AND REPLACED NOSE GEAR BUNGEE CYLINDER IAW DC-9 MM 32-32-07-2-0002. OPS CHECKED GOOD. NO DEFECTS NOTED. 2L72 4F A6WE 20040615001182004061500118WP 2004 6 15 2025 120040513A7932581167 OIL FILTER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE LEAKING I U2RBE ENGINE SHUTDOWN F FLT CONT AFFECTED CLCLIMB 1 GL23921R 508 508 46145 669644 SHUTDOWN NR 2 ENGINE CLIMBING OUT OF ILG AT FL240 AT 1220Z OIL QUANTITY DROPPED TO 1 GALLON, WINDMILLING OIL PRESSURE 20 PSI. 2L74 4F4 F 4A25 1E8 20040615001222004061500122SO 2004 6 15 C2XA04BT060 120040510A3350B6245 LIGHT EMB 145 EMB145LR 3260212SO PAX DOOR FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716976 145171 DURING SERVICE ROUTINE CHECK MAINTENANCE FOUND THE MAIN PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY ON PASSENGER DOOR IAW EMB145 MM 33-50-06. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040615001252004061500125NM 2004 6 15 HNAA0400045 120040511A531385320056 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 STRINGER 31S IS CORRODED AT X252. SPLICED IN NEW SECTION OF STR 31S IAW EO 8-53-04-0318. 2H72 4T RTA13NM 20040615001282004061500128NM 2004 6 15 WRLA200417 120040429A5210CDSP11101 SOLENOID DOUG MD11 MD11F 3023600NM COCKPIT DOOR SMOKE A WRLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11275WA 48631 DURING CLIMB AFTER 3 MINUTES THE FLIGHT CREW SMELLED SMOKE IN THE COCKPIT. RETURNED BACK TO KDAY, THE CREWS HAD TO DUMP FUEL TO PERFORM A SUCCESSFUL LANDING. THE CAUSE OF THE SMOKE WAS DETECTED BY THE FIRE DEPARTMENTS USE OF INFRA RED HEAT UNIT TO BE AROUND THE COCKPIT DOOR LOCK MECHANISM. THE DOOR SOLENOID WAS REPAIRED BY MAINTENANCE PRIOR TO THE FLIGHT. WORLD AIRWAYS IS INVESTIGATING THE CAUSE OF THE SMOKE SOLENOID. 2L73 4F RTA22WE 20040615001292004061500129NM 2004 6 15 HNAA0400053 120040511A531185320937 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 FRAME X252.7 CORRODED AT STR 31S. INSTALLED NEW FRAME SECTION PER EO8-53-04-0315. 2H72 4T RTA13NM 20040615001302004061500130NM 2004 6 15 HNAA0400018 120040305A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07934HA 139 CORROSION FRAME LEG X252 AND STRINGER 31S. REMOVED STRINGER. 2H72 4T RTA13NM 20040615001312004061500131NM 2004 6 15 F3LA200400058 120040509A3240 WARNING LIGHT AIRBUSA319 A319111 3930336NM BRAKES ILLUMINATED A F3LAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03920FR 1997 ABORTED TAKEOFF. FLIGHT CREW REPORTED BRAKE CONFIGURATION WARNING (TEMP). ABORTED TAKEOFF AT 65 KTS. NO FAULTS OR FAILURES ON POST FLIGHT REPORT. PERFORMED OPERATIONAL CHECK OF NORMAL BRAKE SYSTEM PER AMM 32-42-00-710-001. PERFORMED OPERATIONAL CHECK OF ALT BRAKE SYSTEM PER AMM 32-43-00-710-001. PERFORMED BRAKE INSPECTION OF FUSE PLUGS AND WHEELS. BRAKE TEMPERATURE MAX WAS LESS THAN 660 DEG CELSIUS AND WITHIN 150 DEG CELSIUS OF EACH OTHER. PERFORMED AFS TEST PER AMM 22-96-00-710-001. FMGC 1 AND 2 PASS; FAC 1 AND 2 PASS. PERFORMED REALIGNMENT. NO DAMAGE NOTED. NO FAULTS FOUND. 2L72 4F RTA28NM 20040615001332004061500133NM 2004 6 15 200405121 120040405A5753652678676A FLAP BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE WINGS BINDING A SQ7AK NONE O OTHER ININSP/MAINT 1 SO018642653126100 21364 INBOARD FLAPS STUCK AT 2 DEGREES POSITION. 2L73 4F4 F A3WE E2EA 20040615001352004061500135NM 2004 6 15 HNAA0400017 120040305A5311 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07934HA 139 MAJOR REPAIR FRAME SPLICE AT X 240 AND STRINGER 28S. 2H72 4T RTA13NM 20040615001362004061500136WP 2004 6 15 ABXA040180 120040520A335060030451 BATTERY DOUG DC9 DC915 3022036WP EMERGNECY LIGHT DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23927AX 45717 EMERGENCY LIGHTS STAYED ON AFTER POWER SHUT DOWN. REPLACED BATTERY POWER SUPPLY WITH A SERVICEABLE UNIT IAW DC-9 MM 33-53-02-4-0001. OPS CHECKED GOOD. 2L72 4F A6WE 20040615001402004061500140SO 2004 6 15 SWIA200413303 120040428A5610 WINDSHIELD EMB 120 EMB120ER 3260203SO COCKPIT CRACKED A SWIAO OTHER O OTHER CRCRUISE 1 NM07215SW 120281 RIGHT WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. P/N ON&OFF: NP-151311-2, S/N OFF: 98099H2740. 2L72 4T RTA31SO 20040615001432004061500143EA 2004 6 15 SWIA200413306 120040505A2730276003 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07438SW6934 6934 7574 WITH SYSTEM NR 3 TURNED ON LEFT ELEVATOR STUCK IN FULL DOWN POSITION (VISUALLY VERIFIED). WITH EITHER SYSTEM NR 1 OR NR 2 TURNED ON, LEFT ELEVATOR RETURNS TO NEUTRAL POSITION AND OPERATES NORMALLY. REPLACED LT ELEVATOR NR 3 PCU AND PCU SHEAR PIN. OPS CHECK GOOD IAW RII 27-404 AND MM 27-33-01. P/N: 27600-3, S/N OFF: MAL3718. 2L72 4F RTA21EA 20040615001442004061500144EA 2004 6 15 SWIA200413307 120040507A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07416SW 7089 EXIT SIGN AT FORWARD WARDROBE INOP. REMOVED AND REPLACED EXIT SIGN AT FORWARD WARDROBE. OPS CHECKS GOOD. P/N: 6020-6. 2L72 4F RTA21EA 20040615001452004061500145EA 2004 6 15 SWIA200413308 120040511A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 12 INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07431SW 7536 AFT EMERGENCY LIGHT OVERHEAD IS INOP. REMOVED AND REPLACED EMERGENCY LIGHT AT ROW 12 AS REQUIRED. OPS CHECK GOOD. 2L72 4F RTA21EA 20040615001462004061500146EA 2004 6 15 SWIA200413309 120040509A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07454SW7 7 7749 FLIGHT SPOILER AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE CAME UP ON SHORT FINAL. REMOVED AND REPLACED NR 2 SECU PER MM 27-61-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20040615001472004061500147EA 2004 6 15 SWIA200413321 120040512A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA RT ENGINE SHORTED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07946SW 7776 RIGHT JET OVHEAT FAIL CAUTION MESSAGE ON EICAS AFTER ENGINE START UP. REPOSITION LOOP-A, NO LONGER TOUCHING AIRCRAFT BODY IAW CRJ MM 26-11-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20040615001482004061500148NM 2004 6 15 HNAA0400048 120040511A531185320638111 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE INADEQUATE A HNAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA07908HA 015 FRAME X240 HAS AN INADEQUATE SPLICE AT STR 33. REMOVED AND REPLACED FRAME AT X240 PER EO 8-53-04-0314, MAJOR REPAIR. 2H72 4T RTA13NM 20040615001502004061500150SO 2004 6 15 SWIA200413322 120040513A2497 RELAY EMB 120 EMB120ER 3260203SO COCKPIT OVERHEATED A SWIAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM0757734 120199 FIRST OFFICER'S HORIZONTAL RIGHT CONSOLE IS VERY HOT TO TOUCH AND HAS A STRONG ELECTRICAL BURNING ODOR. REPLACED APU STARTER CONTACTOR AND FEEDER PROTECTION RELAY AND MOUNTING BRACKET FOR THE FEEDER PROTECTION RELAY. APU OPS CHECK GOOD IAW EMB 120 MM 24-30-03 AND 24-52-00. 2L72 4T RTA31SO 20040615001512004061500151EA 2004 6 15 SWIA200413323 120040515A2710 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA AILERONS DAMAGED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07461SW 7811 AILERON TRIM IS INTERMITTENT WHEN TRIMMING TO THE RT (LWR TRIM IS OKAY). REPLACED AILERON TRIM PANEL WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 601R51227-13. 2L72 4F RTA21EA 20040615001522004061500152SO 2004 6 15 SWIA200413324 120040517A3150 CIRCUIT BREAKER EMB 120 EMB120ER 3260203SO TRIM WARNING TRIPPED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07565SW 120340 ON TAKEOFF ROLL AURAL TRIM SOUNDED WITH TRIM WITHIN GREEN. ABORTED TAKEOFF. RESET AURAL WARN CB (H8). OPS CHECK GOOD ON GROUND. 2L72 4T RTA31SO 20040615001562004061500156SO 2004 6 15 SWIA200413328 120040414A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 RIGHT AFT SIDEWALL SEAT TRACK CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT AFT SIDEWALL SEAT TRACK AS NEEDED. 2L72 4T RTA31SO 20040615001572004061500157SO 2004 6 15 SWIA200413329 120040414A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 LEFT AFT FLOOR SEAT TRACK CORRODED, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK AS NEEDED. 2L72 4T RTA31SO 20040615001592004061500159NM 2004 6 15 ABXA040178 120040519A5620140T24134 WINDOW BOEING767 767281 1385109NM CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23784AX 23017 DURING SERVICE CHECK WALK AROUND, FOUND MAIN DECK CARGO WINDOW AT STA 785-90 RIGHT SIDE CRACKED, PART OF OUTER PANE MISSING, THIRD WINDOW FORWARD OF THE OVERWING EXIT. REPLACED STA 785.90 OUTER WINDOW PANE, RIGHT SIDE, IAW 56-21-01-4. LEAK CHECKED GOOD IAW 05-51-24-2. 2L72 4F RTA1NM 20040615001602004061500160WP 2004 6 15 ABXA040174 120040510A335041B004AD07G3 BATTERY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW AMM 33-00-00. 2L72 4F A6WE 20040615001612004061500161NM 2004 6 15 SWAA041630 120040608A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29385SW 26600 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 867, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040615001622004061500162SO 2004 6 15 SWIA200413320 120040518A5753 RIB EMB 120 EMB120ER 3260203SO LT NACELLE FLAP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07295UX 120295 LEFT NACELLE FLAP 3RD UPPER RIB SUPPORT (FROM OUTBOARD) CRACKED. DISCOVERED DURING A-CHECK INSPECTION. REMOVED AND REPLACED LEFT NACELLE FLAP WITH SERVICEABLE UNIT. REF MM 27-50-03. 2L72 4T RTA31SO 20040615001642004061500164NM 2004 6 15 0400716718 120040504A5315 FLOORBEAM BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 420 BETWEEN LBL 8 AND RBL 58. REPAIRED PER EA 67-165119. 2L74 4F A20WE 20040614001342004061400134CE 2004 6 14 HSY2004F00000 120040430A2841C6680501108 TRANSMITTER CESSNA208 208B 2073701CE PWA PT6 PT6A11 52043NE FUEL SYS MALFUNCTIONED E HSYAK NONE O OTHER ININSP/MAINT 1 NM05730FX 208B0477 UPON REMOVAL OF RT WING NR 3 OB FUEL TRANSMITTER, PART WAS FOUND MISSING THE ROLL PIN THAT SECURES THE FLOAT ARM TO THE TRANSMITTER ASSY. FUEL TRANSMITTER INSPECTION WAS PERFORMED ON 2/19/04. THE SERIAL NR OF THIS TRANSMITTER WAS NOT APPLICABLE TO THE SERIAL NUMBERS LISTED IN CAB04-1. (THIS PART SN: 2395, CAB 04-1 LIST APPLICABLE SN`S 2410-2709) MALFUNCTION OF THIS PART IS CONGRUENT WITH PURPOSE OF CAB04-1. 1H71 3T3 T A37CE E4EA 20040614001372004061400137CE 2004 6 14 GUU2004F00018 120040519A2697 WIRE HARNESS BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA FIRE BOTTLE OUT OF POSITION A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1787555 UE234 DURING FLIGHT, RT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. REPOSITIONED AND SECURED WIRE HARNESS AT SQUIB. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E4EA 20040614001552004061400155NM 2004 6 14 DL73S040513 120040608A5313 STRINGER BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27377DL 23604 CORROSION ON STR 27L FROM STA 947.6 TO STA 1006. REPAIRED PER SRM 53-10-3 FIG 1. 2L72 4F A16WE 20040614001742004061400174NM 2004 6 14 DL757040443 120040515A3610PW2037RTC CLAMP BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALAK NONE JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 SO27622DL 22912 716587 THE FOLLOWING IRREGULARITY WAS REPORTED BY FLIGHT CREW; RT ENG HI STAGE, RT ENG BLEED OFF, RT PACK OFF EICAS MSG, RT ENG FIRE LOOP 2 STATUS MSG, RT ENG OIL PRESS MISSING FROM LOWER EICAS DISPLAY. MTC FOUND RT ENG HIGH STAGE DUCT CLAMP FAILED AT COOLER, DAMAGING 2 FIRE WALL HARNESS. REPLACED CLAMP AND OTHER DAMAGED PARTS. 2L72 4F4 FRTA2NM E17NE 20040614001762004061400176NM 2004 6 14 DL76L040446 120040517A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27185DN 27961 ON TWO OCCASIONS INFLIGHT, A BURNING SMELL (DESCRIBED AS BURNING RUBBER) WAS NOTICED BY SEVERAL CREW MEMBERS NEAR SEATS 27F AND G. DISSIPATED QUICKLY, COULD NOT BE LOCALIZED OR IDENTIFIED. HOT READING LAMPS WERE INITIALLY SUSPECTED. MAINTENANCE INSPECTED AIRCRAFT. UNABLE TO DUPLICATE SMELL. 2L72 4F RTA1NM 20040614001802004061400180WP 2004 6 14 UPS04842370 120040504A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 603. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040614001922004061400192NM 2004 6 14 RYN2004F00014 120040423A5321 FLOOR PANEL BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE FUSELAGE CRACKED E RYNAK NONE O OTHER ININSP/MAINT 1 CE078878Z 21451 AT C-CHECK, FOUND CRACK IN FORWARD PIT FLOOR PANEL, AT STA 480 TO 540. 2L73 4F4 F A3WE E2EA 20040614002042004061400204NE 2004 6 14 MDR04050 120040421A5310642062363042 SUPPORT BEAM SKRSKYS64 CH54B 8142610NE PWA JFTD12JFTD12A4A 52047NE RT MGB CRACKED A JYDRK NONE O OTHER ININSP/MAINT 1 NM09159AC6897 64084 IN THE COURSE OF A POST FLIGHT INSPECTION, THE FIELD MAINTENANCE CREW DISCOVERED A CRACK IN THE RT MGB SUPPORT BEAM APPROXIMATELY STA 333. SL 199 AND RBL 20. THIS IS ON THE FORWARD TOP SIDE OF THE BEAM. OVERALL CRACK LENGTH APPROXIMATELY 3 INCHES. PROBABLE CAUSE IS UNKNOWN. THE PART WILL BE EXAMINED. 2G72 4U4 U H6EA E15EA 20040614002082004061400208WP 2004 6 14 15HA0358005 120040518A2120 SMOKE CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL COCKPIT DETECTED A I5HAO OTHER O OTHER NRNOT REPORTED 1 GL23582P 475 CREW NOTICED SMOKE IN THE COCKPIT AND CARGO COMPARTMENT JUST AFTER RT ENG WAS STARTED IN PREP FOR THE REGULARLY SCHEDULED FLIGHT. ENG WAS SHUTDOWN AND INSPECTED. NOTHING OUT OF ORDINARY WAS DISCOVERED. MECHANIC HAD CREW DISCONNECT EDC AND ENG WAS RESTARTED. THERE WAS NO SMOKE AFTER ENGINE WAS RESTARTED WITH THE EDC DISCONNECTED. THE EDC WAS LEFT DISCONNECTED AND DEFERRED. THE AC DEPARTED 30 MIN LATE AND FLEW THE SCHEDULED FLIGHT WITH NO FURTHER PROBLEMS. FOLLOWING DAY THE EDC, ASSOCIATED DUCT INSTALLATION AND THE AC SYS WERE ALL THOROUGHLY INSPECTED AND OPERATED. THERE WAS NO EVIDENCE OF SMOKE, OIL OR EXCESSIVE OIL CONSUMPTION FROM THE EDC OR AC TURBINE. THE AC WAS RETURNED TO SERVICE. 2L72 4R4 T 6A6 E282 20040614002142004061400214EA 2004 6 14 ASO2004F00018 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM. (ASOA04334) 2L72 4F4 FRTA21EA E15NE 20040614002152004061400215NE 2004 6 14 RYN2004F00028 220040213A7230 COMPRESSOR AIRBUSA321 A321211 3930370EU IAE V2533 V2533A5 NE NR 2 ENGINE DAMAGED A RYNAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07DALAQ 1438 DURING CLIMB OUT, NR 2 ENGINE STALLED. APPROPRIATE PROCEDURES WERE FOLLOWED. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. REMOVED AND REPACED NR 2 ENGINE. 2L72 4F4 FRTA28NM E40NE 20040614002212004061400221NM 2004 6 14 SWAA041650 120040610A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 961, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040614002242004061400224EU 2004 6 14 ASO2004F00004 120040307A5310 CREASE BEAM AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK INSPECTION, THE CREASE BEAM PLATE AFT OF FRAME 39 ON THE LT SIDE WAS FOUND BENT AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED AND BENT CREASE BEAM PLATE IAW SRM. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. (ASOA04373) 2H72 4T4 TRT E20NE 20040614002342004061400234SO 2004 6 14 CHQA000472 120040402A3350 LIGHT EMB 145 EMB145LR 3260212SO EXTERIOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 EMERGENCY LIGHT OVER RIGHT WING INOPERATIVE. REMOVED AND REPLACED RIGHT EXTERNAL OVERWING EMERGENCY LAMP AND OPS CHECK GOOD IAW EMB 145 MM 33-50-10. 2L72 4T RTT00011AT 20040614002562004061400256SO 2004 6 14 CHQA000486 120040511A3350 BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11283 145424 NR 4 BATTERY PACK POWER SUPPLY FOR EMERGENCY LIGHTING DEAD. REMOVED AND REPLACED BATTERY PACK IAW EMB145 AMM 33-50-04. 2L72 4T RTT00011AT 20040614002662004061400266 2004 6 14 USA2004F00033 420040505A2565 GIRT BAR AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE DOOR SLIDE DETACHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19764US 1369 THE MAIN ENTRY DOOR SLIDE GIRT BAR WAS FOUND DETACHED. MAINTENANCE ATTACHED GIRT BAR. OK FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20040614002792004061400279SO 2004 6 14 CHQA000439 120040224A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11269 145293 EMERGENCY EXIT LIGHT AT 12A AND 12B/C FOR CEILING INOP. REMOVED AND REPLACED BULBS PER EMB 145 AMM 33-50-50. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040614002812004061400281SO 2004 6 14 CHQA000440 120040224A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11292 145488 RIGHT AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT EMERGENCY LIGHT IAW EMB 145 33-40. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040614002832004061400283SO 2004 6 14 CHQA000485 120040511A3350 BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11273 145331 NR 3 EMERGENCY BATTERY ASSY INOP. REMOVED AND REPLACED NR 3 EMERGENCY BATTERY ASSY PER EMB 145 MM 33-50-04. OPS CHECKS GOOD. 2L72 4T RTT00011AT 20040614002952004061400295SO 2004 6 14 C2XA04SH284 120040514A532014521725001 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV-DURING C-CHECK THE LEFT HAND SILL FROM FRAME 18 TO FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040614002992004061400299EU 2004 6 14 CX7A194J0423 120040513A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT & RT TAILPIPECONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03314CE 340B335 RECEIVED LT & RT TAILPIPE HOT CWP ON TAKEOFF ROLL. 2L72 4T RTA52EU 20040614003142004061400314NM 2004 6 14 EIA2004034 120040504A5350 RADOME BOEING747 747273C 1384896NM FUSELAGE BIRD STRIKE A EIAAK NONE O OTHER CLCLIMB 1 NM09471EV 20651 JUST AFTER ROTATION AIRCRAFT FLEW THROUGH A FLOCK OF SEAGULLS, IMPACTING SOUNDS HEARD. ALL INSTRUMENT AND ENGINE PARAMETERS NORMAL. NO VISIBLE DAMAGE SEEN FROM CARGO COMPARTMENT. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND RADOME DAMAGE BEYOND LIMITS ON LEFT SIDE FROM STA 100 TO 130 WL 215 TO 250. REMOVED AND REPLACED RADOME IAW MM 53-52-01. ALSO FOUND TWO BIRD STRIKES ON LEFT FUSELAGE STATION 310 WL 210 AND NOSE LANDING GEAR STRUT AT WL 95. INSPECTED BIRD STRIKE AREAS IAW SRM, NO DEFECTS NOTED. CLEANED BIRD REMAINS OFF AIRCRAFT. 2L74 4F A20WE 20040614003202004061400320NE 2004 6 14 EIA2004035 220040508A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9* 52054NE NR 4 STALLED A EIAAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 NM09482EV 20713 662412 NR 4 ENGINE STALLED AT FL 370, INFLIGHT START ACCOMPLISHED AT FL 210, ALL INDICATIONS NORMAL. 2L74 4F4 F A20WE E20EA 20040614003262004061400326WP 2004 6 14 IXXA0400025S 120040210A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL91910 46003 DURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED AT THE RIGHT FUSELAGE TAIL SECTION BETWEEN STATION 1750.00 AND 1752.00, L14R-L15R. REPAIR ACCOMPLISHED, REMOVED FASTENERS AND DAMAGE AREA IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 53-2-1 FIGURE 7. FABRICATED DOUBLER, FINGER DOUBLER AND FILLER IN ACCORDANCE WITH DC8 STRUCTURAL MANUAL 53-2-1 FIG 7, CLEANED, TREATED AND PRIMED DOUBLER, FINGER DOUBLER AND FILLER. INSTALLED ALL IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 53-2-1 FIG 7, 51-2-20D PAGE 9, AND 51-1-21 PAGE 1. 2L74 4F RT4A25 20040614003292004061400329WP 2004 6 14 IXXA0400026S 120040212A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL91910 46003 DURING C-CHECK INSPECTION FOUND LEFT OUTBOARD WING L/E INBOARD SECTION WITH CORROSION ON SEVERAL AREAS OF UPPER SKIN SURFACE (STA XW 485.000-XPS 710.000). PERFORMANCE MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 56-2-1 FIG 44. REMOVED CORROSION FOUND OUTER LIMITS, REPAIR ACCOMPLISHED, REMOVED DAMAGED SKIN IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 57-2-1 FIG 44, FABRICATED DOUBLER, CLEANED TREATED AND PRIMED THEN APPLIED SEALANT TO FRAYING SURFACE IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-15 PAGE 1. INSTALLED DOUBLER WITH NEW FASTENERS, IAW DC8 SRM 57-2-1 FIG 44, 51-1-21 PAGE 1, 51-1-20D PAGE 9. 2L74 4F RT4A25 20040614003372004061400337NM 2004 6 14 AWXA200400503 120040511A3350321454 EPSU AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE J WARNING INDICATION ININSP/MAINT 1 WP28802AW43422149 924 PHX - EEL - DURING OPERATIONAL TEST OF EMERGENCY LIGHTS RECEIVED FAILURE INDICATION, EPSU INT LOAD FWD L. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040614003462004061400346SO 2004 6 14 RAIA00404019 120040424A2697 WIRE EMB 145 EMB145 3260210SO NR 2 BRAKE SHORTED A RAIAC ABORTED TAKEOFF N FALSE WARNING TXTAXI/GRND HDL 1 CE03827HK 145021 5621 - STL - BRAKE 2 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 2 BRAKE HEAT INDICATION PER MEL 32-40-01. SUBSEQUENTLY CLEARED DMI BY REPAIRING SHORTED WIRE AT PIN A CANNON PLUG P 1090. 2L72 4F RTT00011AT 20040614003502004061400350NM 2004 6 14 SWAA041652 120040610A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 727D + 5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040614003642004061400364NM 2004 6 14 SWAA041638 120040609A53116546596 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727B, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040614003692004061400369 2004 6 14 SWAA041643 420040609A256563550 SLIDE BOEING737 7377H4 1384404NM R2 & L2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 DURING SCHEDULED HC2 CHECK, FOUND R2 & L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 & L2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040614003702004061400370NM 2004 6 14 SWAA041644 120040609A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 3, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040615000152004061500015WP 2004 6 15 GTIA040525 120040521A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 RT CUSP WEB AT 1174, 1210 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F RTA6WE 20040615000232004061500023NM 2004 6 15 ANCF200400010 120040603A2750 WARNING LIGHT DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE TE FLAPS ILLUMINATED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23583AN 53183 DURING TAKE OFF WITH TAKE OFF THRUST ADJUSTED VOCAL WARNING AND FLAPS DISAGREE LIGHT ON, RETURN TO GATE WAS PERFORMED. RESET IN BOTH STALL WARNING COMPUTERS WERE PERFORMED, ADDITIONALLY POSITION SWITCH WAS CHECK IN STATUS TEST PANEL AND NOT SHOW DIFFERENCE. FLAP TAKE OFF TEST WAS PERFORMED IAW AMM 27-00-00 AND 34-19-00, PAGE 202. 2L72 4F4 FRT E2EA 20040615000392004061500039NM 2004 6 15 ASAA0410253 120040503A531565549052 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM LOWER SURFACE OF BOTTOM FLANGE AT STATION 420 IS CORRODED. REMOVED DAMAGED RPR STRAPS AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-02346. (M) 2L72 4F A16WE 20040615000442004061500044NM 2004 6 15 ASAA0410233 120040501A53156554909501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND STATION 807 BEAM CAP AT RBL 24.75 TO LBL 24.75. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA5310-02353. (M) 2L72 4F A16WE 20040615000462004061500046NM 2004 6 15 ASAA0410213 120040426A5754 SKIN BOEING737 737290C 138448VNM SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND RT OUTBOARD SLAT CRACKED AND DELAMINATED AT UPPER TRAILING EDGE. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EA 5740-01391. (M) 2L72 4F A16WE 20040615000602004061500060NM 2004 6 15 ASAA0410211 120040426A531565465688 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM VERT WED AT STATION 1016, RBL 42 IS CORRODED. REMOVED DMG DOUBLER AND INSTALLED RPLC DOUBLER IAW 51-20-1. (M) 2L72 4F A16WE 20040615000642004061500064NM 2004 6 15 ASAA0410242 120040501A57536571909117 SKIN BOEING737 737290C 138448VNM FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND LT OUTBOARD FLAP ASSEMBLY LOWER SURFACE HAS BARE METAL AND IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA5750-01947. (M) 2L72 4F A16WE 20040615000702004061500070NM 2004 6 15 ASAA0410193 120040413A531565549061 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND FLOORBEAM LOWER FLANGE AT STATION 500, BL 0 - LBL 45 HAS LIGHT CORROSION. REMOVED DAMAGED PRP STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW SRM 51-30-2 AND EA 5310-01463. (M) 2L72 4F A16WE 20040615000722004061500072NM 2004 6 15 ASAA0410202 120040420A534765549698 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND SEAT TRACK AT STATION 827-947, RBL 25 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW SRM 51-30-2. 2L72 4F A16WE 20040615000802004061500080NM 2004 6 15 DXTA200400298 120040419A2131 CONTROLLER GULSTM200 200 4500308NM CABIN PRESSURE MALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 GL07702QS 070 COULD NOT CONTROL PRESSURIZATION IN AUTO OR MANUAL MODE WITH SEVERAL ATTEMPTS, DECLARED EMERGENCY AND DIVERTED TO ILM. COMPLIED WITH ENGINE RUN UP TO MAX CLIMB DETENT SEVERAL TIMES, UNABLE TO DUPLICATE DISCREPANCY AT THIS TIME. ALL WORK DONE PER GULFSTREAM-200 MAINTENANCE MANUAL CHAPTER 71-00-00, NO FURTHER ACTION REQUIRED AT THIS TIME. 2L72 4F RTA53NM 20040615000862004061500086WP 2004 6 15 ABXA040191 120040521A57554925721501 FITTING DOUG DC9 DC941 302207NWP RT WING L/E CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 LEFT INBOARD SPOILER TORSION BAR CAM OUTBOARD SUPPORT FITTING CRACKED AT TOP END. REPLACED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20040615000882004061500088NM 2004 6 15 SWAA041660 120040610A324426066712 TIRE BOEING737 7373H4 1384600NM RT MLG BLOWN A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW29358SW 26595 AIR TURNBACK / DECLARED EMERGENCY. NR 3 MAIN TIRE BLEW ON TAKEOFF. BLOWN TIRE DAMAGED RT WING INBOARD, GROUND SPOILER, INBOARD MID FLAP, INBOARD FORE FLAP, INBOARD T/E FLAP, INBOARD MID FLAP AND FUSELAGE SKIN AT BS 382, STRINGER 14L. REMOVED AND REPLACED NR 3 MAIN TIRE/WHEEL ASSEMBLY PER MM. REPAIRED RT WING, INBOARD MID FLAP, INBOARD T/E FLAP, INBOARD GROUND SPOILER, INBOARD FORE FLAP, AND SKIN PER MM AND SRM. 2L72 4F RTA16WE 20040615000952004061500095 2004 6 15 SWAA041667 420040612A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040615000972004061500097EA 2004 6 15 SWIA200413341 120040408A5340 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE DOOR SILL CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 SERVICE DOOR; FRAME TO SILL ANGLE IS CORRODED AT FS 349.00. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CORRODED ANGLE IAW CRJ SRM 51-42-21, 51-40-11, 51-23-00, 51-42-21, 20-21-00. 2L72 4F4 FRTA21EA E15NE 20040615000992004061500099EA 2004 6 15 SWIA200413343 120040408A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CUT A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 MAIN FUSELAGE; FLOORBEAM CUT ALONG BOTTOM FLANGES, FS 467.0; LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO-53-41-211. 2L72 4F4 FRTA21EA E15NE 20040615001132004061500113SO 2004 6 15 SWIA200413337 120040518A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07292UX568 568 120292 RECEIVED A FLAP AND ADVANCE SWS MAP IN FLIGHT WITH ASSOCIATED CONTROL FAULT ON OVERHEAD PANEL INDICATING FAULT IN OUTBOARD PAIR OF FLAPS. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW EMB 120 MM 27-50-05. ALSO REPAIRED DEFECTIVE SPLICE ON LEFT OUTBOARD FLAP ACTUATOR WIRE W502-0026-22. OPS CHECK GOOD. 2L72 4T RTA31SO 20040615001172004061500117WP 2004 6 15 ABXA040176 120040430A5311995823807 FRAME DOUG DC9 DC941 302207NWP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23973AX 47511 FRAME AT STA 1056 HAD EXFOLIATED CORROSION IN SEVERAL LOCATIONS ON AFT SIDE FROM LONGERON 8 LEFT TO 4 LEFT. REPAIRED FRAME WITH SPLICE REPAIR IAW DC-9 SRM 53-03 AND SSRM K05907. 2L72 4F A6WE 20040615001192004061500119NM 2004 6 15 AWXA200400504 120040511A3260106122615 UPLOCK SENSOR BOEING737 7373Y0 1384671NM LT MLG DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28334AW 23747 ON CLIMBOUT OF PHX EN ROUTE FOR ORD AFTER LANDING GEAR RETRACTION LT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CYCLED LANDING GEAR AND LIGHT CIRCUIT BREAKER, LIGHT REMAINED ON, TURNED BACK TO PHX FOR REPAIR. MAINTENANCE FOUND A BROKEN YELLOW WIRE INSIDE INSULATION & CONDUIT WHILE TROUBLESHOOTING LT MAIN LANDING GEAR UPLOCK SENSOR S72. REMOVED AND REPLACED LT MAIN LANDING GEAR UPLOCK SENSOR S72 IAW BMM 32-61-21, AND REPAIRED BROKEN WIRE, OPERATIONAL CHECK OF LANDING GEAR WAS GOOD. 2L72 4F RTA16WE 20040615001212004061500121NM 2004 6 15 AWXA200400506 120040504A53126573328 BULKHEAD BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 17.1, WL 230. MAINTENANCE REMOVED CRACK IN BS 178 BULKHEAD VERTICAL WEB BEAM AT RBL 17.1, WL 230; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13, FIG 1. 2L72 4F RTA16WE 20040615001232004061500123WP 2004 6 15 ARWA20040504 120040511A283034255 ACTUATOR DOUG DC8 DC863 302198AWP DUMP CHUTE INOPERATIVE A ARWAO OTHER J WARNING INDICATION CLCLIMB 1 SO19345JW 46042 DUMP CHUTE WILL NOT RETRACT ELECTRICALLY. REMOVE AND REPLACED AC MOTOR ACTUATOR IAW DC8 MM 28-30-2. OPERATIONAL CHECK ACCOMPLISHED FOUND OK IAW DC8 MM 28-30-2. 2L74 4F 4A25 20040615001242004061500124WP 2004 6 15 ARWA20040503 120040511A5101 SEAL DEPRESSOR DOUG DC8 DC863 302198AWP FUSELAGE DAMAGED A ARWAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19345JW 46042 ON CLIMB PRESSURIZATION LEAK HAPPENED AT FL 280. UNABLE TO MAINTAIN CABIN PRESSURE 10,000 FT. REMOVED AND REPLACED LOWER SEAL DEPRESSOR IAW AERONAUTICAL ENGINEERS DRAWING AE2412 & DC8 SRM 51-3-0 PAGE 1, 2 & 3. PERFORMED CABIN PRESSURIZATION OPS CHECK IAW NASI SYSTEM ST466CH & MM 21-00-00, FOUND NORMAL IAW DC8 MM 21-31-0. 2L74 4F 4A25 20040615001262004061500126NM 2004 6 15 HNAA0400047 120040511A531385320872 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 STRINGER 27S CORRODED FWD OF FRAME X220 JUST UNDER LAV SERVICE PORT. REMOVED AND REPLACED STRINGER 27S. 2H72 4T RTA13NM 20040615001492004061500149NM 2004 6 15 0400745515 120040426A5321 FLOOR PANEL BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 23203 DURING H-CHECK FOUND CORROSION ON FLOOR WEB UPPER SURFACE FROM BS 1712 TO 1716 LBL 50 TO RBL 50. REPAIRED PER EA 55-199013. 2L72 4F RTA2NM 20040615001582004061500158NM 2004 6 15 F3LA200400060 120040425A5315 FLOORBEAM BOEING737 73736E 138443ANM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03317FL 2731 25263 DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 328, RBL 15 AND 35. REMOVED DAMAGED TOP CHORD OF FLOORBEAM, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-51 AND EA B3-53R10393. 2L72 4F RTA16WE 20040615001652004061500165NM 2004 6 15 0400736718 120040430A5340 FITTING BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING H-CHECK FOUND CRACK IN NOSE CARGO DOOR FRAME CLOSURE FITTING. REPAIRED PER EA 67-165115. 2L74 4F A20WE 20040615001662004061500166NM 2004 6 15 0400726718 120040504A5315 FLOORBEAM BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING H-CHECK FOUND CRACK IN UPPER DECK FLOORBEAM CHORD AT BS 520. REPAIRED PER EA 67-165122. 2L74 4F A20WE 20040615001672004061500167WP 2004 6 15 DHL2004802005 120040512A573037702921 BRACKET DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 INBOARD SLOT, RT WING BRACKET ASSEMBLY CRACKED AT MOUNTING AREA. INSTALLED BRACKET ASSEMBLY P/N: 3770292-1 (I/B AT WING SLOT) IAW DC-8 M/M 22-80-1. 2L74 4F RT4A25 20040615001692004061500169EA 2004 6 15 SWIA200413310 120040510A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07954SW2062 2062 7815 HSTA STAB TRIM CH NR 1 CB POPS. INSTALLED SERVICEABLE HSTA AND MCU. OPS CHECKS GOOD IAW 27-42-01. MCU P/N: 7062-3, S/N OFF: 1110. 2L72 4F RTA21EA 20040615001742004061500174EA 2004 6 15 SWIA200413315 120040510A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07920SW 7660 DURING ORIGINATING CHECK, RUDDER TRIM WOULD ONLY MOVE RIGHT, NOT LT. REMOVED AND REPLACED TRIM CONTROL PANEL IAW CRJ 200 MM CHAPTER 27-12-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20040615001762004061500176EA 2004 6 15 SWIA200413317 120040512A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07405SW 7029 LOOP-B ON LT JETPIPE HAS BEEN PRODUCING FAIL MESSAGES. REMOVED AND REPLACED ALL A & B EYELET CONNECTIONS AS REQUIRED. OPS CHECKS GOOD AT THIS TIME IAW MM 26-11-0. 2L72 4F RTA21EA 20040615001772004061500177EA 2004 6 15 SWIA200413318 120040514A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07918SW4657 4657 7645 FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED POWER DRIVE UNIT FOR FLAPS IAW 27-52-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040616000012004061600001NM 2004 6 16 ASAA0410246 120040501A53126545808141 BULKHEAD BOEING737 737290C 138448VNM NLG WW CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND NOSE WHEEL WELL AFT BULKHEAD IS CHAFED. REPAIRED NOSE WHEEL WELL AFT BULKHEAD IAW SRM 51-40-2. (M) 2L72 4F A16WE 20040616000022004061600002NM 2004 6 16 ASAA0480405 120040516A532199365451 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, CABIN FLOOR PANEL AT STATION 160-200, LBL 8-44 HAS DISBONDED CORNERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000042004061600004NM 2004 6 16 ASAA0480406 120040516A532199365461 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, LBL 8 - RBL 8 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000052004061600005NM 2004 6 16 ASAA0480409 120040516A532199365471 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURNIG HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 180-200, RBL 8-44 HAS CORRODED AND BROKEN INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000112004061600011NM 2004 6 16 ASAA0480413 120040516A532199365831 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV-CHECK, FOUND OVERWING AREA FLOORBOARD IS DISBONDED ON CORNER. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000122004061600012NM 2004 6 16 ASAA0480412 120040516A532199365501 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, LBL 22-44 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000182004061600018NM 2004 6 16 ASAA0480421 120040516A5311 FRAME DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1117, LONGERON 29R TO 29L IS CORRODED. REMOVED DAMAGE AND INSTALLED NEW FRAME IAW 51-30-1. (M) 2L72 4F RT 20040616000212004061600021NM 2004 6 16 ASAA0440114 120040426A53156546811 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 FOUND FLOORBEAM UPPER CAP IS CORRODED AT CLIP FROM RBL 24-49. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS. FABRICATED REPAIR, TREATED AND PRIMED AND INSTALLED, REF 737 SRM 53-00-51. (M) 2L72 4F RTA16WE 20040616000242004061600024NM 2004 6 16 ASAA0480426 120040517A53119919603 FRAME DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND FRAME IN AFT PIT AT STATION 1231, LONGERON 29L-29R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE IAW 53-03. (M) 2L72 4F RT 20040616000262004061600026NM 2004 6 16 ASAA0480424 120040517A5310 SHEAR TIE DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1148, LONGERON 29L TO 28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE IAW 51-10-2. (M) 2L72 4F RT 20040616000272004061600027NM 2004 6 16 ASAA0480423 120040517A5310995773935 SHEAR TIE DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND SHEAR TIE IN AFT PIT AT STATION 1287, LONGERON 29L TO 29R IS CORRODED. REMOVED DAMAGE AND INSTALLED FRAME REPAIR SPLICE IAW 53-03. (M) 2L72 4F RT 20040616000292004061600029 2004 6 16 ASAA0480078 420040203A25658370024 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 OKC - DURING HV-6 CHECK, FOUND AFT EXIT TAIL EMERGENCY ESCAPE SLIDE FAILED TO DEPLOY DURING OPERATIONAL CHECK. LANYARD PULLED LOOSE FROM SLIDE PACK COVER, AND COVER REMAINED IN POSITION. S/D - INVESTIGATION SUGGESTS THAT THE PROBABLE CAUSE OF FAILURE WAS A WORN VELCRO ATTACHMENT AT THE SLIDE COVER END OF THE RELEASE LANYARD. THIS ATTACHMENT, IN CONJUNCTION WITH A METAL SNAP, IS WHAT FASTENES THE LANYARD TO THE COVER. IT WOULD APPEAR THAT NEITHER, ALONE, IS SUFFICIENT UNDER TENSION TO KEEP THE LANYARD FASTENED TO THE COVER. LUBRICATION FLUIDS FROM THE EMPENNAGE TEND TO DROP ON THE SLIDE COVER, AND THIS MAY, OVERTIME, BE WHAT DAMAGED THE VELCRO. THE LANYARD WAS REPLACED. (M) 2L72 4F RTA6WE 20040616000302004061600030NM 2004 6 16 ASAA0480431 120040517A55325912166104 PANEL DOUG MD80 MD83 3023681NM VERTICAL STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND RIGHT VERT STAB UNDER PANEL 3804A HAS CHAFED SURFACE. REMOVED DAMAGED SKIN PANEL AND INSTALLED NEW PANEL IAW 51-20-8. (M) 2L72 4F RT 20040616000312004061600031NM 2004 6 16 ASAA0480430 120040517A5311 FRAME DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND FRAME IN AFT CARGO PIT AT STATION 1287, LONGERON 29L-28R IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR FRAME SEGMENT IAW 53-03. (M) 2L72 4F RT 20040616000332004061600033NM 2004 6 16 ASAA0440117 120040407A5311655828064 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 FOUND FS 360 AT STRINGER 8L FRAME IS CRACKED AT SIDEWALL LIGHT ATTACHMENT BRACKET. REPAIRED FRAME AT STATION 360 AT STRINGER 8L. (M) 2L72 4F RTA16WE 20040616000342004061600034NM 2004 6 16 ASAA0440116 120040420A533065C377672 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 FOUND DENT IN FUSELAGE SKIN, AFT OF L1 DOOR, 8 INCHES ABOVE VERT. REPAIRED DENT IN FUSELAGE STATION 360 TO 380, STRINGER 17L AND 18L REF SRM 53-00-01 FIG 201. (M) 2L72 4F RTA16WE 20040616000352004061600035NM 2004 6 16 ASAA0480419 120040516A532099305389 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV-CHECK, FOUND CUSP WEB PANEL AT STATION 674, L18 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-10-4. (M) 2L72 4F RT 20040616000362004061600036NM 2004 6 16 ASAA0480418 120040516A532199365343 FLOOR PANEL DOUG MD80 MD83 3023681NM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV-CHECK, FOUND FLOOR WEB AT STATION 200, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M) 2L72 4F RT 20040616000392004061600039NM 2004 6 16 ASAA0480415 120040516A532099305389 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CUSP WEB BETWEEN STATION 693-712 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 51-70-4. (M) 2L72 4F RT 20040616000422004061600042NM 2004 6 16 ASAA0480432 120040517A5230 ANGLE DOUG MD80 MD83 3023681NM AFT CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND AFT CARGO DOOR BOTTOM EDGE 'L' ANGLE IS GOUGED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE IAW 51-30-5. (M) 2L72 4F RT 20040616000462004061600046 2004 6 16 0400925802 420040603A2565D31393109 SLIDE BOEING757 757351 1384991NM LEFT OFFWING WILL NOT TEST A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01582NW5870 5870 32981 LEFT AFT EMERGENCY EXIT DID NOT DEPLOY LEFT OVERWING SLIDE DURING OPERATIONAL SAMPLING TEST. SAMPLING TEST WAS PERFORMED BY FORECAST INSPECTION 55-0525-8-0225. ADJUSTED LEFT AFT AUTO FIRE SWITCH. 2L72 4F RTA2NM 20040616000472004061600047SO 2004 6 16 MASA200400199 120040414A3350602024 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07835MJ 145353 A/C OUT OF C-CHECK WENT TO CLT AND THE EMERGENCY EXIT SIGN AT THE PAX DOOR WAS FOUND TO BE INOP. MX REPLACED THE SIGN. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040616000522004061600052EA 2004 6 16 MASA200400305 120040601A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07591ML 7388 EMERGENCY EXIT LIGHT SWITCH LEFT IN THE ON POSITION. LIGHTS WERE INOPERATIVE. MX FOUND NO FAULT WITH EMERGENCY EXIT LIGHTING SYSTEM. OPS GOOD NO PARTS USED. 2L72 4F RTA21EA 20040616000542004061600054SO 2004 6 16 MASA200400191 120040409A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07837MJ 145367 ASH FLT 2674 BHM. OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE ROW 12. MX SECURED WIRING AT LIGHT ASSEMBLY WIRING HARNESS. NO PARTS USED. 2L72 4T RTT00011AT 20040616000552004061600055SO 2004 6 16 MASA200400224 120040426A33501317 BULB EMB 145 EMB145LR 3260212SO EMRGENCY LIGHT BLOWN A MASAK NONE L NO TEST ININSP/MAINT 1 SW07856MJ 145626 UPON OVERNIGHT INSPECTION THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MX REPLACED BULB, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040616000562004061600056SO 2004 6 16 MASA200400257 120040510A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07825MJ 145179 THE LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. MX COULD NOT DUPLICATE THE DISCREPANCY. A/C DEPARTED WITHOUT FURTHER DISCREPANCY. NO PARTS USED. 2L72 4T RTT00011AT 20040616000582004061600058NM 2004 6 16 MASA200400270 120040517A1420 CONNECTOR DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT CONTAMINATED A MASAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SW07446YV 446 RAP - DEN, DURING TAXI OUT THE EMERGENCY LIGHTS FLICKERED ON/OFF. MX TROUBLESHOT AND CLEANED THE CONNECTOR AND RESECURED IT ON THE F/A'S CONTROL PANEL. OPS CHECK GOOD, NO PARTS USED. 2H72 4T RTA13NM 20040616000622004061600062NM 2004 6 16 2004UALA00485 120040522A5315 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA 27114 STA 246 FLOORBEAM RBL 46 FWD SIDE STIFFENER CRACKED (BUCKLED). MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER. 2L72 4F4 FRTA1NM E24NE 20040616000642004061600064NE 2004 6 16 2004UALA00487 220040522A7261 SCAVENGE PORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 5 BEARING OBSTRUCTED A UALAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 WP29424UA 506 AFTER SHUT DOWN EXPERIENCED TAILPIPE FIRE IN NR 1 ENGINE. NR 5 BEARING COMPARTMENT FLOODED DUE TO BLOCKED OIL SCAVENGE PORT. MAINTENANCE IS INITIATING A MAINTENANCE TASK TO REPLACE SUSPECT OIL TUBES DURING C-CHECKS. 2L72 4F4 FRTA28NM E40NE 20040616000652004061600065EU 2004 6 16 2004UALA00489 120040524A3397 TERMINAL BLOCK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT CONTAMINATED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29496UA 1845 DURING EMERGENCY ESCAPE PATH LIGHT CHECK, ROWS 1, 2, 3, 6 AND 7 FAILED TO ILLUMINATE. FOUND SMALL PARTICLES IN TERMINAL BLOCK - CLEANED, INSTALLED NEW POWER SUPPLY AND OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616000662004061600066NM 2004 6 16 2004UALA00490 120040524A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 FUSELAGE FRAME DENTED AT BS 1520 STR 26L AFT PIT. MAJOR REPAIR ACCOMPLISHED. FABRICATED, INSTALLED DOUBLER & FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616000682004061600068NM 2004 6 16 2004UALA00492 120040524A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 AFT PIT FRAME INNER FLANGE DENTED AT STA 1420 ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616000702004061600070NM 2004 6 16 0400916303 120040511A5330 SKIN BOEING747 747451 1384940NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01663US 23818 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN BETWEEN BS 2638 & BS 2658 WL 310. REPAIRED PER EA 63-194964. 2L74 4F RTA20WE 20040616000712004061600071NM 2004 6 16 2004UALA00474 120040514A2930 PRESSURE SWITCH AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE GREEN HYD SYS FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29824UA 965 LANDED UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM LOW PRESSURE MESSAGE. THE SAME MESSAGE CAUSED DIVERSION OF NEXT FLIGHT DUE TO EN ROUTE WEATHER CONDITIONS AND TRADEWINDS AT PLANNED DESTINATION. HYDRAULIC PUMP PRESSURE SWITCH FAILED. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SWITCH. RAN BOTH ENGINES FOR SEVERAL MINUTES AND OPERATION OF NR 1 ENGINE HYDRAULIC PUMP WAS NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616000722004061600072EU 2004 6 16 2004UALA00475 120040516A3350321454 EPSU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGNECY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29420UA 489 EMERGENCY LIGHTS FAIL TEST INT LOADS LEFT. REPLACED POWER SUPPLY UNIT. CABIN EMERGENCY LIGHTS NOW PASS. 2L72 4F4 FRTA28NM E40NE 20040616000742004061600074NM 2004 6 16 2004UALA00477 120040516A3350362624 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE ROW 15-16B INTERMITTENT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29120UA 29166 EMERGENCY EXIT LIGHTS 15-16B, COME ON-OFF FOR NO REASON. RELAMPED AND SECURED BATTERY PACK. NO FLICKERING AT 15-16B AREA. EMERGENCY EXIT LIGHTS TEST OK. 2L74 4F4 FRTA20WE E24NE 20040616000772004061600077NM 2004 6 16 2004UALA00481 120040518A5310 SHEAR WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 STA 194 SHEAR WEB AT STR 17 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20040616000792004061600079NM 2004 6 16 MASA200400271 120040517A2910 LINE DHAV DHC8 DHC8202 2809007NM NR 2 HYD SYSTEM CRACKED A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07448YV 448 RETURNED TO FIELD DUE TO LOSS OF NR 2 HYD SYSTEM QTY. MX FOUND 2 LINES CRACKED AND REPLACED THEM WITH FLEX LINES PER THE AMM UNTIL PARTS COME. 2H72 4T RTA13NM 20040616000832004061600083EU 2004 6 16 2004UALA00514 120040528A2920 RAM AIR TURB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29416UA 479 RAT DOES NOT WORK. WOULD NOT PRESSURIZE BLUE SYSTEM OR PROVIDE ELECTRICAL POWER. TEST BOX MALFUNCTIONED CAUSING ERONOUS INDICATIONS. 2L72 4F4 FRTA28NM E40NE 20040616000852004061600085NM 2004 6 16 2004UALA00516 120040531A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29391UA 24666 STA 706 STR 4 RT, STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STR CLIP. 2L72 4F4 FRTA16WE E2GL 20040616000862004061600086NM 2004 6 16 2004UALA00517 120040601A2897 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CROSS FEED VALVEFAILED A UALAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 WP29328UA 24148 FLIGHT DIVERTED DUE TO A STUCK FUEL CROSS-FEED VALVE CAUSING A FUEL IMBALANCE. CREW REPORTED FUEL CROSSFEED LIGHT REMAINS BRIGHT (INDICATING VALVE IS IN TRANSIT) NO MATTER WHAT POSITION THE CROSSFEED SWITCH IS IN. AND FUEL CROSS FEED VALVE POSITION LIGHT DOES NOT AGREE WITH SWITCH POSITION. FOUND BROKEN WIRE AT CONNECTOR D792. REPAIRED WIRE. 2L72 4F4 FRTA16WE E2GL 20040616000872004061600087NM 2004 6 16 0400886302 120040524A3350 BATTERY PACK BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK, FOUND B-ZONE RIGHT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040616000892004061600089NM 2004 6 16 0400866309 120040518A3350 SOCKET BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C-31C. REPLACED EMERGENCY LIGHT SOCKET ASSEMBLY AT SEAT 21C. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040616000902004061600090NM 2004 6 16 0400966301 120040610A3350 POWER SUPPLY BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040616000922004061600092NM 2004 6 16 2004UALA00520 120040601A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STRINGER DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STATION 727A STRINGER SPLICE HAS ELONGATED HOLE. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040616000942004061600094NM 2004 6 16 2004UALA00522 120040601A2750 WARNING LIGHT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE TE FLAPS ILLUMINATED A UALAO OTHER J WARNING INDICATION DEDESCENT 1 WP29604UA 21865 LANDED LAX UNDER AMBER ALERT DUE TO FLAP DISAGREE INDICATION. ACCOMPLISHED FLAP POSITION TRANSMITTER SYNCHRONIZATION CHECK ON 3, 4, AND 5 FLAP POSITION TRANSMITTERS. FOUND NR 4 OUT OF LIMITS. ADJUSTED TRANSMITTER. 2L72 4F4 FRTA1NM E3NE 20040616000952004061600095WP 2004 6 16 0400811243 120040515A2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501WP CARGO BAY FALSE ACTIVATIONA NWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01243NW 48315 EN ROUTE TO AMS AT APPROXIMATELY 02:45Z, NR 3 AFT CARGO SMOKE DETECTOR LIGHT ILLUMINATED ALONG WITH MASTER WARNING AND CARGO FIRE SUMMARY LIGHT. FOLLOWED COM PROCEDURES, DISCHARGED BOTH FIRE BOTTLES, AND DIVERTED TO KEF. NO EVIDENCE OF FIRE WAS FOUND. MAINTENANCE CHECKED THE WIRING AND REPLACED THE SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20040616000972004061600097NM 2004 6 16 0400856309 120040518A3350 SOCKET BOEING747 747451 1384940NM EMERGENCY LIGHT DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C-31C. REPLACED EMERGENCY LIGHT SOCKET ASSEMBLY AT SEAT 21C. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040616000982004061600098NM 2004 6 16 UPS04442386 120040507A5414A1S130100501 DOUBLER BOEING747 747256B 1384865NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01528UP 24071 INSPECTION TYPE: C, NR 3 PYLON LOWER WEB EXTERNAL O/B FWD OF REAR ENG BHD FITTING SKIN CRACKED AS RED MARKED (NAC 212-214 WBL R470). THE CRACK STOP DRILLED PER SRM 54-14-03 FIG 2 & REPAIR DOUBLER INSTALLED PER SRM 54-14-03 FIG 2, NDT CONFIRMED NO CRACK. 2L74 4F RTA20WE 20040616000992004061600099WP 2004 6 16 UPS04842381 120040504A53203779659501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 850 LONGERON 2L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, M/M 20-14-00. 2L74 4F RT4A25 20040616001012004061600101WP 2004 6 16 UPS04842383 120040505A532097537709 INTERCOSTAL DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 160-1180 INTERCOSTAL ABOVE C-PIT DOOR IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753770 AND SRM 51-1-21, 51-1-21A. 2L74 4F RT4A25 20040616001022004061600102WP 2004 6 16 UPS04842384 120040511A5320 STRAP DOUG DC8 DC871F 302199DWP FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 360 LBL 12 STRAP IS BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633833 AND SRM 51-1-21. 2L74 4F RT4A25 20040616001042004061600104NM 2004 6 16 0400896305 120040530A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01665US 23820 DURING LINE CHECK, FOUND D-ZONE RIGHT AND E-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING AT 43J AND DOOR 4L. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040616001052004061600105NM 2004 6 16 2004UALA00523 120040601A5310 DOUBLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STRAP DOUBLERS ARE CUT AT STR 26R, BETWEEN STA 727C AND 727D. REPLACED STRAP DOUBLERS. 2L72 4F4 FRTA16WE E2GL 20040616001092004061600109NM 2004 6 16 2004UALA00527 120040602A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 AFT CARGO DOOR CUTOUT AFT EDGE BEAR STRAP REPAIR DOUBLER IS INSUFFICIENT. REPLACED BEAR STRAP DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040616001112004061600111 2004 6 16 2004UALA00530 420040528A2565 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE L1 DOOR SLIDE INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29595UA 28748 DOOR 1L SLIDE ARM LIGHT INOP. RELAMPED LIGHT, OPS CHECKED OK. 2L72 4F4 FRTA2NM E17NE 20040616001122004061600112NM 2004 6 16 2004UALA00532 120040602A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STRINGER MISINSTALLED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29399UA 24674 TWO EA STRINGER SPLICES WERE FOUND WITH INADEQUATE EDGE DISTANCE AT FASTENER LOCATIONS STA 907 STR 26R AND 25R. REPLACED STRINGER SPLICES. 2L72 4F4 FRTA16WE E2GL 20040616001132004061600113NM 2004 6 16 2004UALA00533 120040602A5310 BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 AFT PIT SILL BEAM HAD CORROSION. REPLACED LOWER SILL BEAM WEB. 2L72 4F4 FRTA16WE E2GL 20040616001152004061600115NM 2004 6 16 2004UALA00535 120040602A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 BS 580 FRAME BETWEEN STRINGERS 24L AND 25L HAS A DENT (LBL 30). MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001162004061600116NM 2004 6 16 2004UALA00536 120040602A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 CABIN FLOORBEAM UPPER CAP CORRODED AROUND FASTENER HOLES STA 365 AT RBL 26 TO 44. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001192004061600119NM 2004 6 16 2004UALA00494 120040524A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 FRAME DENTED AND CRACKED AT BS 1480 BETWEEN STR 25L AND 26L AFT PIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040614002712004061400271NE 2004 6 14 ASMF200405027 220040528A7200MA20A10011 VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23805AM17094 26272 726732 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WAS SHUTDOWN AND (FUEL CONT) AND (SPAR VALVE) LIGHTS TURNED ON. STATUS DISPLAY MESSAGES, APU PERFORMANCE AND ABNORMAL STATUS WERE CHECKED, ALL CORRECT. LT SPAR FUEL SHUTOFF VALVE WAS OPERATED MANUALLY AND IT WAS WITH FAILURE. START ENGINE WAS PERFORMED AND (SPAR VALVE) LIGHT CONTINUED ON. SPAR VALVE WAS REPLACED IAW MM 28-22-11 AND TESTED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20040614002732004061400273NM 2004 6 14 AWXA200400576 120040525A3320BV031120333 SOCKET BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE SEAT ROW 15 BURNED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP28309AW 24711 PRIOR TO DEPARTURE, FLIGHT CREW OBSERVED SMOKE IN CABIN BETWEEN SEAT ROWS 13 AND 18. MAINTENANCE DEACTIVATED THE RECIRCULATION FAN AND PLACED SYSTEM ON MEL 21-31, COND. 1 (RECIRC FAN INOP). AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE MAINTENANCE DISCOVERED TWO EACH CABIN FLORESCENT LIGHTS (SEAT ROW 15-18) BURNED AT THE CONNECTOR. REMOVED AND REPLACED LAMP HOLDER ASSEMBLY AND BULBS AT SEAT ROW 15, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040614002902004061400290NM 2004 6 14 HNAA0400046 120040511A532085300273102 FITTING DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 FUSELAGE SKIN BUBBLED AT X202 AND STRINGER 31 BELOW AND INBOARD OF LAV SERVICING DOOR, FOUND TENSION FITTING CORRODED CAUSING PRESSURE ON SKIN. REMOVED AND REPLACED TENSION FITTING, CLEANED PRIMED SKIN. 2H72 4T RTA13NM 20040614002942004061400294NE 2004 6 14 NACA20040020 220040513A8530 VALVE PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 1 ENGINE MISSING A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03993301097 1097 775755 43576 510152 NR 1 ENGINE SHUTDOWN DUE TO NR 12 CYLINDER LOW COMPRESSION. INSPECTED CYLINDER AND FOUND VALVE MISSING. REPLACED NR 1 ENGINE. 2L74 4R4 R 6A3 5E8 20040614003072004061400307NM 2004 6 14 EIA2004030 120040422A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09486EV 20888 EMERGENCY LIGHT LT SIDE STATE ROOM UPPER DECK WENT OUT IN 5 SECONDS. REMOVED & REPLACED LT SIDE STATE ROOM (UPPER DECK) EMERGENCY LIGHT PER B747 MM 33-51-00. OP'S CHECK GOOD PER MM 33-51-00. 2L74 4F A20WE 20040614003112004061400311WP 2004 6 14 GTIA040451 120040511A3260833703 SENSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE LATCH INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23827NK 49793 AFTER TAKEOFF WE GOT AN UNSAFE LIGHT (RED). WE RECYCLED AND IT WENT OUT. (RT MAIN). REMOVED AND REPLACED RT UP AND LATCH SENSOR. 2L72 4F4 FRTA6WE E2EA 20040614003192004061400319NM 2004 6 14 EIA2004031 120040424A3350 BATTERY PACK BOEING747 747212B 1384886NM CABIN DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09486EV 20888 EMERGENCY EXIT LIGHT INOP ABOVE CREW EXIT DOOR. REPLACED EMERGENCY EXIT BATTERY PACK PER MM 33-51-04. REPLACED SIGN PER 33-51-02, OPS CHECKED GOOD. ALSO REPLACED SIGN BATTERY PACK. 2L74 4F A20WE 20040614003222004061400322WP 2004 6 14 IXXA0400023S 120040214A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL91910 46003 DURING A ROUTINE C-CHECK FOUND RIGHT OUTBOARD FLAP UPPER PANEL DOUBLER HAS WEAR OUT OF LIMITS, STATION 159.00 - 213.00. MAINTENANCE REMOVED SKIN SEGMENT WITH DOUBLER ON IT. IN ACCORDANCE STRUCTURAL REPAIR MANUAL CHAPTER 57-1-0 AND 57-7-1 FIG 4 AREA WAS CLEANED, TREATED AND PRIMED. FABRICATION AND INSTALLATION ON NEW SKIN WAS DONE IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 51-1-8B AND 51-1-21. 2L74 4F RT4A25 20040614003412004061400341NM 2004 6 14 MWEA040072 120040512A53305936434193 SKIN BOEING717 717200 1383700NM FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31916ME 55179 SCRATCH ON FUSELAGE SKIN AT STATION 484 AND LONGERON 25 LEFT REQUIRES REPAIR. INSTALLED REPAIR DOUBLER. 2L72 4F TRA6WE 20040614003512004061400351NM 2004 6 14 SWAA041653 120040610A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED C2 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20040615000122004061500012WP 2004 6 15 GTIA040521 120040512A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE COCKPIT DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 COCKPIT RT FLOORBOARD, DELAMINADED AND EDGE DAMAGED. FAB RT COCKPIT FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040615000142004061500014WP 2004 6 15 GTIA040522 120040513A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE COCKPIT CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 COCKPIT STA 127 LBL 6 FLOOR WEB CRACKED. TRIMMED OUT CRACK. FABRICATED FILLER AND DOUBLER. INSTALLED DOUBLER AND FILLER. 2L72 4F4 FRTA6WE E2EA 20040615000172004061500017WP 2004 6 15 GTIA040526` 120040518A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 CABIN STA 1210-1220 STR 18R WEB CORRODED. CUT OUT DAMAGED AREAS. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA6WE E2EA 20040615000332004061500033NM 2004 6 15 ASMF200406002 120040601A32465930594547 WHEEL DOUG MD80 MD83 3023681NM MLG DAMAGED W ASMFO OTHER O OTHER LDLANDING 1 SW23831LF9861 53050 DURING LANDING, TIRE NR 3 WAS LOST AND WATER DEFLECTOR WAS DAMAGED. MAIN TIRES WERE REPLACED IAW MM 32-43-10, ANTI-SKID TEST WAS PERFORMED IAW MM 32-43-00 AND DURING OVERNIGHT SERVICE AT MEX, WATER DEFLECTOR WAS REPLACED IAW MM 32-10-01, ALL CORRECT. 2L72 4F RT 20040615000362004061500036NM 2004 6 15 ASAA001C 120040123A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01747AS 23124 DURING INSPECTION, FOUND THE EMERGENCY FLOORPATH LIGHING ON WITH SWITCH IN 'ARMED' OR 'OFF' POSITION. RESET BATTERY PACKS ON PALLETS 5-12, 6-11, 9-11, 9-5, 7-6, AND 10-11 THEN LIGHTS TESTED NORMAL. (M) 2L72 4F RTA16WE 20040615000452004061500045NM 2004 6 15 ASAA0410229 120040501A531565468243 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND HOLE IN LONGITUDINAL FLOORBEAM, OUTBOARD FLANGE AT STATION 609, RLB 46. REMOVED DAMAGE AND INSTALLED RPR AND STUD BEAM IAW EA5310-02348. (M) 2L72 4F A16WE 20040615000472004061500047NM 2004 6 15 ASAA0410232 120040501A53156554909501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND AFT AIRSTAIR COLUMN OUTBOARD FLOOR MOUNT HOLES CORRODED. REMOVED DAMAGE, REAMED HOLES AND INSTALLED REPLACEMENT BUSHINGS IAW EA5260-01142. (M) 2L72 4F A16WE 20040615000492004061500049NM 2004 6 15 ASAA0410230 120040501A53156554906501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND FLOORBEAM AT STATION 500A, LOWER FLANGE, LOWER SURFACE IS CORRODED. REMOVED DAMAGED RPR STRAP AND INSTALLED RPR STRAP IAW EA5310-02349. (M) 2L72 4F A16WE 20040615000512004061500051NM 2004 6 15 ASAA0410226 120040501A53156546811502 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM FLANGE AT STATION 1006, RBL 45 IS CORRODED. REMOVED DAMAGE AND INSTALLED UPPER T-CHORD IAW EA5310-02347. (M) 2L72 4F A16WE 20040615000532004061500053NM 2004 6 15 ASAA0410224 120040501A531565549068 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND FLOORBEAM RPR AT STATION 520 UPPER CHORD IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT PRP CHORD SECTION IAW EA5310-02358. (M) 2L72 4F A16WE 20040615000552004061500055NM 2004 6 15 ASAA0410220 120040426A532065549063 STRAP BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND LOWER SURFACE OF LOWER FLANGE AT STATION 500B, BETWEEN BL 0 AND LBL 45. REMOVED DAMAGED STRAP AND INSTALLED REPAIR STRAP IAW EA 5310-01464. (M) 2L72 4F A16WE 20040615000742004061500074NM 2004 6 15 ASAA0410195 120040413A531565549101 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND FLOORBEAM RPR STRAP AT STATION 847 IS CORRODED. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW SRM 51-10-2 AND EA 5310-01478. (M) 2L72 4F A16WE 20040615000762004061500076NM 2004 6 15 ASAA0410197 120040420A53156545818106 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND SPOT CORROSON ON BEAM CAP SUPPORT JUNCTION AT STATION 360, RBL 12. REMOVED DAMAGE AND INSTALLED RPR SECTION IAW SRM 53-10-9. (M) 2L72 4F A16WE 20040615000782004061500078NM 2004 6 15 ASAA0410199 120040420A53476554969 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 FOUND CABIN SEAT TRACK AT LBL 45, STATION 727-887 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW SRM 51-20-1. (M) 2L72 4F A16WE 20040615000822004061500082WP 2004 6 15 ABXA040185 120040513A553199118235 RIB DOUG DC9 DC941 302207NWP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 REMOVEABLE VERTICAL LEADING EDGE SECTION 6TH RIB UP ON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159. 2L72 4F A6WE 20040615000842004061500084WP 2004 6 15 ABXA040188 120040513A531139123471F FRAME DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 CORROSION ON FRAME LOWER LEG AT LONGERON 30, STA 408. REPAIRED FRAME IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040615000912004061500091 2004 6 15 SWAA041663 420040611A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040615000932004061500093 2004 6 15 SWAA041665 420040611A256565C19901 CABLE BOEING737 7375H4 138449DNM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED C2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE CABLES PER MM. 2L72 4F RTA16WE 20040615000942004061500094 2004 6 15 SWAA041666 420040611A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040615001012004061500101 2004 6 15 QXEA200400271 420040415A2210C18112AA ACTUATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 300 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09406QX4759 1833 4048 YAW DAMPER DISENGAGE MESSAGE ON BOTH PFD'S. RAN CHECKLIST AND MESSAGE REAPPEARS. REMOVED AND REPLACED YAW DAMPER ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040615001122004061500112SO 2004 6 15 SWIA200413336 120040521A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07167311280 1280 120190 EN ROUTE TO IAH RECEIVED FLAP ON MAP WITH ASYMMETRY IN OVERHEAD PANEL. LANDED FLAP 0 DEGREES IN IAH. REPLACED FLAP ANNUNCIATOR UNIT IAW AMM 27-50-00. FLAP SYSTEM OPS CHECK GOOD. 2L72 4T RTA31SO 20040615001202004061500120NM 2004 6 15 AWXA200400505 120040511A53116546539 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN MAIN CABIN FRAME AT BS 616, LBL 65, BELOW FLOOR LEVEL WL 205. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME AT BS 616, LBL 65, WL 205; FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-001. 2L72 4F RTA16WE 20040615001272004061500127NM 2004 6 15 HNAA0400049 120040511A531185320318 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 FRAME X202 CORRODED AT STRINGER 31S. 2H72 4T RTA13NM 20040615001322004061500132EU 2004 6 15 UPS04142364 120040512A2612273902 CONTROL UNIT AIRBUSA300 A300F4622R 3930360EU FIRE DETECTION FALSE INDICATIONA IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01131UP 0816 AFTER TAKEOFF FROM CAE AT 2,500 FT THE CREW RECEIVED A NR 2 FIRE INDICATION LIGHT. THE CREW MADE THE DECISION TO RETURN BACK TO CAE. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT PER MM 26-12-11-4. 2L72 4F RTA35EU 20040615001342004061500134NM 2004 6 15 HNAA0400051 120040511A531185320318 FRAME DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07908HA 015 FRAME X220 CORRODED AT STRINGER 29S. REMOVED AND REPLACED FRAME 220 IAW EO 8-53-04-0316. 2H72 4T RTA13NM 20040615001372004061500137EA 2004 6 15 SWIA200413300 120040505A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 FUSELAGE PULLEY INTERCOSTAL HAS OUTBOARD RETURN FLANGE CRACKED AT FS 484.00 RBL 36.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV ''A''. 2L72 4F RTA21EA 20040615001392004061500139EA 2004 6 15 SWIA200413302 120040505A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 ENGINE SUPPORT BEAM LOWER WEB RBL 38 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-366, REV ''D''. 2L72 4F RTA21EA 20040615001422004061500142SO 2004 6 15 SWIA200413305 120040505A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07214SW 120280 EMERGENCY LIGHT AT PAX DOOR CEILING IS INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N: 209. 2L72 4T RTA31SO 20040615001552004061500155SO 2004 6 15 SWIA200413327 120040427A5410 BRACKET EMB 120 EMB120ER 3260203SO NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07237SW 120314 RT HYDRAULIC PACK VERTICAL MOUNT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD HALF OF VERTICAL MOUNT BRACKET ASSY PER SRM 51-40-02. 2L72 4T RTA31SO 20040615001632004061500163SO 2004 6 15 CHQA000492 120040507A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INTERMITTENT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11972 145440 EMERGENCY LIGHTS IN CABIN FLASH OR PULSE INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED NR 2 POWER SUPPLY IAW EMB 145 AMM 33-50-04. 2L72 4T RTT00011AT 20040615001732004061500173SO 2004 6 15 SWIA200413314 120040510A27503069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07189SW4057 1205 120048 FLAP LIGHT ON MAP INTERMITTENTLY ILLUMINATES DURING CRUISE FLIGHT AND CLEARS ITSELF. REMOVED AND REPLACED FLAP ANNUNCIATOR ASSEMBLY IAW MM 27-50-05. OPS CHECK GOOD. 2L72 4T RTA31SO 20040615001752004061500175EA 2004 6 15 SWIA200413316 120040512A5220 HOOK CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH BROKEN A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07589SW 7072 COCKPIT OVERHEAD ESCAPE HATCH RIGHT AFT HOOK IS BROKEN AT HINGE POINT. INSTALLED RIGHT AFT HOOK IAW CRJ MM 52-22-00. OPS AND LEAK CHECK GOOD. 2L72 4F RTA21EA 20040616000062004061600006NM 2004 6 16 ASAA0480408 120040516A532199365491 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, RBL 44-54 IS CRACKED. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000072004061600007NM 2004 6 16 ASAA0410200 120040420A5347655496921 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND CABIN SEAT TRACK AT LBL 25, STATION 887 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040616000132004061600013NM 2004 6 16 ASAA0480411 120040516A53219936539503 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV-CHECK, FOUND CABIN FLOOR PANEL AT STATION 144-160, RBL 32-44 HAS DELAMINATED CORNERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000162004061600016NM 2004 6 16 ASAA0480422 120040516A53119919604501 FRAME DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV-CHECK, FOUND FRAME IN AFT PIT AT STATION 1250, LONGERON 29R TO 28L IS CORRODED. REMOVED DAMAGE AND INSTALLED FRAME REPAIR ANGLES IAW 53-03. (M) 2L72 4F RT 20040616000222004061600022NM 2004 6 16 ASAA0480428 120040517A5753 WEDGE DOUG MD80 MD83 3023681NM TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND RIG WING INBOARD FLAP, INBOARD WEDGE LOWER SURFACE IS GOUGED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 57-03. (M) 2L72 4F RT 20040616000372004061600037NM 2004 6 16 ASAA0480417 120040516A5347593054787 SEAT TRACK DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 200-237, RBL 44 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR SECTION IAW 53-05. (M) 2L72 4F RT 20040616000402004061600040NM 2004 6 16 ASAA0480414 120040516A532199365345 FLOOR PANEL DOUG MD80 MD83 3023681NM COCKPIT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND FORWARD CABIN FLOOR MEMBER AT STATION 200, RBL 8 - LBL 8 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPAIR SPLICE IAW 51-10-4. (M) 2L72 4F RT 20040616000412004061600041NM 2004 6 16 ASAA0480433 120040517A5730ARB0975517 PANEL DOUG MD80 MD83 3023681NM RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND RT WING FUEL PANEL 1462 HAS LIGHT SURFACE CORROSION. REMOVED DAMAGE AND REPLACED WITH NEW FUEL PANEL IAW 51-22-2A. (M) 2L72 4F RT 20040616000442004061600044NM 2004 6 16 ASAA0440118 120040425A53156546811 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 FOUND STATION 986 FLOORBEAM UPPER CAP IS CORRODED AT CLIPNUT HOLES FROM RBL 24 TO RBL 49. REMOVED AND RELACED UPPER CAP AT STATION 986 RBL 24 TO RBL 49. (M) 2L72 4F RTA16WE 20040616000512004061600051SO 2004 6 16 MASA200400293 120040525A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07853MJ 145464 ON THE RON AIRCRAFT SCHEDULED FOR ROUTINE. DURING THE WALK-AROUND IT WAS DISCOVERED THAT THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS INOP. REPLACED THE LIGHT BULB AND OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20040616000592004061600059NM 2004 6 16 UPS04442380 120040513A3350 BATTERY PACK BOEING747 747283B 1384867NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:N/A UPPER DECK SERVICE DOOR RT SIDE DOOR FRAME EMERGENCY LIGHTS INOP. TOP TRIM PANEL REMOVED FOR ACCESS TO BATTERY PACK. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2L74 4F A20WE 20040616000612004061600061NM 2004 6 16 2004UALA00484 120040522A5753 FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAPS CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA 27114 LEFT INBOARD T/E MAIN FLAP MIDDLE AFT FLAP HINGE FITTING CRACKED ON INBOARD SIDE NEAR FLAP AFT SPAR. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA1NM E24NE 20040616000632004061600063NM 2004 6 16 2004UALA00486 120040522A3251 SERVO AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NLG STEERING FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29838UA 1477 LANDED UNDER AMBER ALERT DUE TO A NOSE WHEEL STEERING FAULT PROBLEM. NOSE STEERING SERVO UNIT FAILED. REPLACED NOSE STEERING SERVO UNIT. OPERATIONS CHECK NORMAL WITH NO MESSAGES OR LEAKS. 2L72 4F4 FRTA28NM E40NE 20040616000732004061600073NM 2004 6 16 2004UALA00476 120040516A3350582233 POWER SUPPLY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT INTERMITTENT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29668UA 30024 EMERGENCY EXIT FLOOR LIGHTS ARE ON LAST 5 ROWS BY 4R. LIGHTS ARE INTERMITTENT. *S/D* REPLACED EMERGENCY LIGHT POWER SUPPLY. OPERATIONS CHECK OKAY. 2L72 4F4 FRTA1NM E24NE 20040616000782004061600078NM 2004 6 16 2004UALA00482 120040518A5310 SHEAR WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 STA 194 SHEAR WEB AT STR 17 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20040616000842004061600084EU 2004 6 16 2004UALA00515 120040530A2910 VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE YELLOW HYD SYS LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP29487UA 1669 ARRIVED UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM. FOUND LEAK MEASUREMENT VALVE LEAKING, REPLACED VALVE. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616000912004061600091NM 2004 6 16 2004UALA00519 120040601A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STATION 727A INBOARD OF STRINGER 27L SHEAR TIE HAD EXCESSIVE MATERIAL LOSS. REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20040616000932004061600093NM 2004 6 16 2004UALA00521 120040601A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE MISREPAIRED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29399UA 24674 STATION 787 SHEAR TIE BETWEEN STR 2L AND 27R HAS NO EDGE DISTANCE ON PREVIOUS REPAIR. REPAIRED SHEAR TIE. 2L72 4F4 FRTA16WE E2GL 20040616001202004061600120NM 2004 6 16 2004UALA00495 120040524A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 DENT ON FUSELAGE SKIN AT STA 1417, BETWEEN STRINGERS 27R & 28R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001222004061600122NM 2004 6 16 2004UALA00497 120040521A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BULKHEAD MISINSTALLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 STATION 178 LT UPPER FRAME WL 243 NO EDGE DISTANCE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED ANGLE SPLICE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040616001262004061600126NM 2004 6 16 2004UALA00501 120040521A2611CM382AS10 BULB BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE SMOKE DETECTOR INCORRECT A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29659UA 27114 E&E SMOKE DETECTOR FAILS TEST. REPLACED E&E SMOKE DETECTOR. INCORRECT BULB INSTALLED. FOUND BULB ML382 INSTALLED, SHOULD BE CM382AS10. 2L72 4F4 FRTA1NM E24NE 20040616001282004061600128WP 2004 6 16 0400859874 120040517A2780 WARNING LIGHT DOUG DC9 DC951 3022051WP SLATS ILLUMINATED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01783NC 48108 DURING SLAT EXTENSION FOR LANDING AT BUF, THE AIRCRAFT ROLLED WITH BOTH THE SLAT DISAGREEMENT AND SLAT EXTEND LIGHTS ILLUMINATED. COMPLIED WITH COM PROCEDURES AND FIRST OFFICER WENT BACK TO VISUALLY CHECK THAT BOTH SLATS WERE EXTENDED PRIOR TO LANDING. THE SLAT DISAGREEMENT LIGHT EXTINGUISHED AND THE FLIGHT EXECUTED A NORMAL APPROACH AND LANDING. MAINTENANCE AT BUF COULD NOT DUPLICATE ANY DISCREPANCIES IN THE SLAT SYSTEM BUT DID REPLACE THE LT WING SLAT EXTEND SWITCH AS A PRECAUTION. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20040616001292004061600129EU 2004 6 16 2004UALA00503 120040526A2910 YAW DAMPER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN HYD SYS LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP29402UA 439 FLT LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616001312004061600131NM 2004 6 16 2004UALA00505 120040526A2170 WATER SEPARATOR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN AIR CONTAMINATED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29919UA 25386 FLIGHT DIVERTED TO MRY DUE TO A BURNING ODOR IN COCKPIT. WATER SEPARATOR TEMPERATURE SENSOR FAILED. REPLACED TEMPERATURE SENSOR AND LH/RH COALESCER BAGS. PERFORMED OPERATIONAL TEST AND NO SMELL NOTED. 2L72 4F4 FRTA16WE E2GL 20040616001322004061600132NM 2004 6 16 2004UALA00506 120040526A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE MISINSTALLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STA 178 LT UPPER FRAME HAS SHORT EDGE DISTANCE AT SPLICE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040616001332004061600133NM 2004 6 16 2004UALA00507 120040527A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 AFT PIT FRAME CORRODED AT BS 1300 BL 0 TO RBL 3. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER & ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001342004061600134NM 2004 6 16 2004UALA00508 120040527A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 CABIN FLOORBEAM UPPER CAP CORRODED AT STA 310 RBL 42. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FILLER & CAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001352004061600135NM 2004 6 16 C1HA200494003 120040513A3230656021123 ACCESSORY UNIT BOEING727 727290 138408WNM MLG MALFUNCTIONED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15294AS 22146 ON TAKEOFF FROM STL AFTER GEAR RETRACTION, THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LDG ACC UNIT IAW 32-04-121 & NLG POS SW IAW32-61-71, PERFORMED ADJ/TEST, OP'S CHECK SATISFACTORY. 2L73 4F A3WE 20040616001362004061600136NM 2004 6 16 C1HA200492012 120040519A5313 STRINGER BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 STA 684 STR 27R STRINGER CORRODED. INSTALLED REPAIR DOUBLER. 2L73 4F A3WE 20040616001382004061600138NM 2004 6 16 C1HA200492007 120040519A5330 SKIN BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 STA 680 STR 27R CORROSION ON SKIN. 2L73 4F A3WE 20040616001392004061600139NM 2004 6 16 C1HA200492009 120040519A5620 SKIN BOEING727 727212 138407GNM WINDOW BELT CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 WINDOW 17 RIGHT CORROSION ON SKIN BEYOND LIMITS. INSTALLED DOUBLER. 2L73 4F A3WE 20040616001432004061600143NM 2004 6 16 2004UALA00509 120040527A2751 WARNING LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAPS ILLUMINATED A UALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP29656UA 25394 RETURNED TO BLOCKS TWICE DUE TO FLAP INDICATIONS. 2L72 4F4 FRTA1NM E24NE 20040616001462004061600146NM 2004 6 16 2004UALA00540 120040602A2150 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EQUIP COOLING ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29329UA 24149 EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED IN BOTH NORMAL AND ALTERNATE MODES. THE EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED. 2L72 4F4 FRTA16WE E2GL 20040616001472004061600147NE 2004 6 16 2004UALA00541 220040602A7200 FAN BLADE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 ENGINE INCORRECT A UALAA UNSCHED LANDING EJWVIBRATION/BUFFET WARNING INDICATION INADEQUATE Q C CLCLIMB 1 WP29922UA 26642 NUMBER 1 ENGINE VIBRATION AT 5.0. INCORRECT REPLACEMENT OF 2 FAN BLADE PAIRS RESULTED IN UN-BALANCED FAN SYSTEM. REPLACED FAN BLADES. 2L72 4F4 FRTA16WE E2GL 20040616001482004061600148NM 2004 6 16 2004UALA00542 120040603A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA TO CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 CABIN FLOOR CREASE BEAM WEB CORRODED ON UPPER SURFACE FROM STA 968.5 TO 969.5, RBL 70 - RBL 71. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH DOUBLER. 2L72 4F4 FRTA2NM E17NE 20040616001492004061600149 2004 6 16 2004UALA00543 420040603A2565 SPRING BOEING757 757222 1384956NM PWA 2037 PW2037 NE GIRT BAR BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29506UA 24627 GIRT BAR FORWARD SPRING BROKEN, DOOR HARD TO DISARM DOOR 4 LT. OUTBOARD ANGLE OF SPRING WAS BROKEN AND REMAINDER OF SPRING JAMMED SLIDER BLOCK IN ARMED POSITION. REASON FOR BROKEN SPRING HAS NOT BEEN DETERMINED, BUT GALLEY DEBRIS IN GIRT AREA IS AN OCCASIONAL CAUSE OF ARM/DISARM WRITE-UPS. 2L72 4F4 FRTA2NM E17NE 20040616001502004061600150NM 2004 6 16 2004UALA00448 120040508A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 HFEC INSPECTION FOUND INDICATIONS OF DEFECTS PER NDT 51-00-01 AT SEVERAL LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND EXTERNAL FUSELAGE SKIN DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040616001512004061600151NM 2004 6 16 2004UALA00450 120040507A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STRINGER SPLICE CRACKED AT STA 907 STR 4L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040616001522004061600152NM 2004 6 16 2004UALA00451 120040507A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STRINGER SPLICE CRACKED AT STA 907 STR 4R. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040616001532004061600153NM 2004 6 16 2004UALA00452 120040510A2120214N21091 DUCT BOEING757 757222 1384956NM PWA 2037 PW2037 NE AIR COND SPLIT A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29516UA 24860 RETURN TO FIELD DUE TO AIR CONDITIONING CABIN TEMPERATURE PROBLEM. OVERHEAD DISTRIBUTION DUCT AT ROWS 15 TO 18 HAD 4 FOOT SPLIT. REPLACED OVERHEAD DUCT. 2L72 4F4 FRTA2NM E17NE 20040616001552004061600155NM 2004 6 16 2004UALA00454 120040510A5310 TORQUE BOX BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 AFT PIT TORQUE BOX WEB BETWEEN STA 1840 - 1860 LBL 61 HAS 1 CRACK AND DENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW TORQUE BOX WEB. 2L74 4F4 FRTA20WE E24NE 20040616001562004061600156NM 2004 6 16 2004UALA00455 120040510A5310 TORQUE BOX BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 FWD PIT TORQUE BOX AT STA 660-680 LBL 25 TO LBL 40 WEB HAS 3 EA DENTS AROUND EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW WEB. 2L74 4F4 FRTA20WE E24NE 20040616001582004061600158NM 2004 6 16 2004UALA00457 120040510A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 FWD PIT STA 840 RBL 49 FLANGE OF UPPER TEE CHORD IS BENT RBL 8 TO RBL 65. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLES & T-EXTRUSION. 2L74 4F4 FRTA20WE E24NE 20040616001592004061600159NM 2004 6 16 2004UALA00458 120040510A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 AFT PIT FRAME AT STA 1840 LBL 61 HAS DENT AT LOWER SECTION. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW FRAME. 2L74 4F4 FRTA20WE E24NE 20040616001602004061600160NM 2004 6 16 2004UALA00459 120040510A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE BENT A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 FWD PIT STA 760 RBL 49 AFT FLANGE OF UPPER TEE CHORD IS BENT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLES AND T-EXTRUSION. 2L74 4F4 FRTA20WE E24NE 20040616001612004061600161NM 2004 6 16 2004UALA00460 120040510A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 TOP OF FLOORBEAM CORRODED AT STA 324 AT RT CUSP. MAJOR REPAIR ACCOMPLISHED. CORROSION CAUSED FROM WET AREA OF GALLEY. FLOORBEAM REPAIR ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20040616001632004061600163NM 2004 6 16 2004UALA00558 120040607A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 SKIN DAMAGED AT STA 290 BETWEEN STR 20R AND 22R. REPLACED SKIN PANEL AND STR 21R AND 22R SEGMENTS. 2L72 4F4 FRTA16WE E2GL 20040616001642004061600164EU 2004 6 16 2004UALA00472 120040512A2621 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE FALSE ACTIVATIONA UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29417UA 483 ENG 1 AGENT 1 DISCHARGE LIGHT STAYS ILLUMINATED. FLIGHT DIVERTED. CLEANED BOTTLE, RESET FDU, TESTED OK. 2L72 4F4 FRTA28NM E40NE 20040616001692004061600169 2004 6 16 2004UALA00564 420040606A2565 RELAY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE ESCAPE SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29669UA 30025 RIGHT OVERWING ESCAPE SQUIB TEST FAILS TO ILLUMINATE DURING TEST. LAMP CHECKS OKAY WITH PRESS-TO-TEST. REPLACED BATTERY PACK PER MM 33-51-07 AND MM 25-65-17, TESTED OK. TWO MONTHS LATER RELAY P/N XD4L015 AND BATTERY WERE REPLACED, SUGGESTING THAT RELAY AND BATTERY MAY HAVE BEEN RELATED IN BOTH CASES. 2L72 4F4 FRTA1NM E24NE 20040616001712004061600171NM 2004 6 16 2004UALA00566 120040610A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29519UA 24872 EXTERNAL FUSELAGE SKIN STA 615-620 AT STR 16L LT DENTED, STR 16 LT DAMAGED AT STA 618. INSTALLED SKIN DOUBLER AND FILLER REPAIR. DOUBLER REPAIR INSTALLED ON STRINGER. 2L72 4F4 FRTA2NM E17NE 20040616001732004061600173NM 2004 6 16 C1HA200483009 120040530A5315 FLOORBEAM BOEING727 7272S7 138407ZNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15683CA 22490 STA 344 LBL 18 FLOORBEAM CORRODED. REPAIRED IAW SRM 53-10-8 FIG 9. 2L73 4F A3WE 20040616001772004061600177SO 2004 6 16 MASA200400180 120040401A2720SYLC53058 ACTUATOR EMB 145 EMB145LR 3260212SO GUST LOCK LEAKING A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07860MJ696 145773 RETURNED TO GATE. RUDDER ELECTRO MECHANICAL GUST LOCK WOULD NOT DISENGAGE. MX CURRENTLY TROUBLESHOOTING 4/1/2004. MX REPLACED THE GUST LOCK ACTUATOR. OP CHECKS GOOD. 2L72 4T RTT00011AT 20040616001782004061600178SO 2004 6 16 MASA200400184 120040406A2611 CONNECTOR EMB 145 EMB145LR 3260212SO SMOKE DETECTOR CONTAMINATED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07853MJ 145464 BAGGAGE SMOKE DETECTION SYSTEM INOP. MX CLEANED THE DEBRIS AND CLEANED THE CONNECTORS. SYSTEM OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040616001792004061600179SO 2004 6 16 MASA200400198 120040414A5210 MECHANISM EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A MASAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW07857MJ 145765 CREW REPORTED UNABLE TO CLOSE AND LOCK MAIN CABIN DOOR. MX LUBED AND OPS CHECKED GOOD. NO PART USED. 2L72 4T RTT00011AT 20040616001802004061600180SO 2004 6 16 MASA200400210 120040419A5210 LATCH EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07837MJ 145367 IN CLT THE CREW WAS NOT ABLE TO OPEN THE DOOR. MX WAS CALLED. MX LUBED THE DOOR LATCH MECHANISM. OP CHECKS NORMAL. NO PARTS USED. 2L72 4T RTT00011AT 20040616001832004061600183 2004 6 16 MASA200400243 420040502A34180861DT5MOD2 SENSOR EMB 145 EMB145LR 3260212SO NR 1 AOA BROKEN A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07856MJ256 145626 ABORTED TAKEOFF AND RETURNED TO GATE. DURING TAKEOFF ROLL HAD SPS1 WARNING MESSAGE. MX REPLACED THE NR 1 AOA VANE, OPS CHECK GOOD. 2L72 4T RTT00011AT 20040616001882004061600188WP 2004 6 16 UPS04842390 120040508A57403645611 FITTING DOUG DC8 DC871F 302199DWP LEFT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, INSIDE NR 1 ALT FUEL TANK STATION XRS 440 STRINGER 58 BOOST PUMP FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D. 2L74 4F RT4A25 20040616001902004061600190NE 2004 6 16 0400936642 220040606A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7Q 52054NE NR 1 FLAMED OUT A NWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL01642NW 21942 702200 WHILE AT CRUISE, THE NR 1 ENGINE FLAMED OUT WITH OIL PRESSURE DROPPING TO ZERO. NO RESTART WAS ATTEMPTED. THE FLIGHT RETURNED TO NRT LANDING WITHOUT INCIDENT. MAINTENANCE FOUND METAL ON THE CHIP DETECTORS AND THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E3NE 20040616001912004061600191NM 2004 6 16 2004UALA00545 120040603A2520 CONTROL UNIT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE SEAT LOMBAR OVERHEATED A UALAO OTHER M OVER TEMP NRNOT REPORTED 1 WP29643UA 25093 LOMBAR CONTROL SEAT 9A IS HOT AND MELTING. REPLACED SWITCH. THE BURNED BACK CYCLER SWITCH WAS AN OLDER, ORIGINAL UNIT. THE ORIGINAL BACK CYCLER SWITCH WAS UPGRADED IN 2001 DUE TO RELIABILITY PROBLEMS. AN IMPROVED, REPLACEMENT SWITCH WAS DEVELOPED AND INTRODUCED IN DECEMBER OF 2001. 2L72 4F4 FRTA1NM E24NE 20040616001922004061600192EU 2004 6 16 2004UALA00546 120040606A2910 CHECK VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE YELLOW HYD SYS INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29441UA 751 RETURN TO FIELD UNDER AMBER ALERT DUE TO LOSS OF YELLOW HYDRAULICS. YELLOW HYDRAULIC SYSTEM PUMP CHECK VALVE FAILED. REPLACED CHECK VALVE. 2L72 4F4 FRTA28NM E40NE 20040616001942004061600194EU 2004 6 16 2004UALA00548 120040604A5521 RIB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT ELEVATOR LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29433UA 589 RIGHT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS. 2L72 4F4 FRTA28NM E40NE 20040616001952004061600195NM 2004 6 16 2004UALA00549 120040604A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ESCAPE SLIDE WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29829UA 1211 EMERGENCY LIGHT TEST FAILED AFTER SLIDE REPLACEMENT AT DOOR 2L. THE SLIDE SHOP TESTED THE SLIDE ASSEMBLY UPON RECEIPT AND THE SHOP VERIFIED THE UNIT TO HAVE FAILED THE LIGHT TEST. THE COMPLETE LAMP HARNESS WAS REPLACED AND THE 22 BLOWN LIGHTS WERE REPLACED. READING AFTER REPAIR WAS PASSING PER THE SHOP CMM. 2L72 4F4 FRTA28NM E40NE 20040616001962004061600196NM 2004 6 16 2004UALA00550 120040604A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 CABIN FLOORBEAM STA 1640 HAS CORROSION AROUND SEVERAL NUT PLATES HOLES FROM RBL 14 TO RBL 44, UPPER FLANGE, LWR AND UPPER SURFACES. FABRICATED & INSTALLED NEW TEE AND DOUBLERS. 2L72 4F4 FRTA2NM E17NE 20040616001972004061600197NM 2004 6 16 2004UALA00551 120040604A5230 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 AFT CARGO DOOR HAS SKIN DENT AFT LWR CORNER. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001982004061600198NM 2004 6 16 2004UALA00553 120040607A2782 ACTUATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LE FLAPS FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29386UA 24661 RETURNED TO FIELD DUE TO NR 3 LEADING EDGE FLAP PROBLEM. REPLACEMENT OF THE LEADING EDGE FLAP ACTUATOR CORRECTED THE DISCREPANCY. THE LEADING EDGE FLAP ACTUATOR WAS FOUND WITH A SEVERELY DETERIORATED PISTON HEAD SEAL. THE CONDITION OF THIS SEAL SUPPORTS THE REASON FOR REMOVAL OF SLOW TO RETRACT. THE DETERIORATED SEAL WOULD RESULT IN CONSIDERABLE LEAKAGE (OR BYPASSING) ACROSS THE PISTON HEAD, RENDERING THE ACTUATOR VERY INEFFICIENT AT CONVERTING HYDRAULIC PRESSURE INTO ACTUATION FORCE. THIS IS ESPECIALLY TRUE IN THE RETRACT DIRECTION, AS THE NOMINAL PRESSURE DELTA IS LESS DURING RETRACTION THAN IN EXTENSION. 2L72 4F4 FRTA16WE E2GL 20040616002002004061600200NM 2004 6 16 2004UALA00555 120040607A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 EXFOLIATION ON MAIN CABIN FLOORBEAM STA 324, RBL 62. TEE ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040616002022004061600202NM 2004 6 16 2004UALA00557 120040608A3510 OXYGEN SYSTEM AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT DISCHARGED A UALAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 WP29827UA 1022 FLIGHT CREW OXYGEN SYSTEM REPORTED AT 50 PSI. FLIGHT DIVERTED. CREW O2 MASK SET TO 100% AND IMPROPERLY STOWED. SERVICED TO FULL. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616002032004061600203WP 2004 6 16 UPS04842399 120040506A5313 LONGERON DOUG DC8 DC871F 302199DWP MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 920 LONGERON 24L IS CRACKED ABOVE GEAR UPLATCH. NDT VERIFIED CRACKS TERMINATED AT FASTENER HOLES. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 53-2-2 FIG 5. 2L74 4F RT4A25 20040616002042004061600204WP 2004 6 16 UPS04842400 120040508A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 1730 LONGERON 15L IS CRACKED. REMOVED LONGERON SECTION, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED REPAIR STRAPS AND SPLICES IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040616002052004061600205WP 2004 6 16 UPS04842401 120040504A5320 CUSP WEB DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 1265 LONGERON 21L (CUSP) IS CRACKED. REMOVED CUSP SECTION BETWEEN STATION 1280 TO 1380, FABRICATED AND INSTALLED CUSP SECTION AND SPLICES IAW SRM 53-2-5 FIG 15A. 2L74 4F RT4A25 20040616002062004061600206WP 2004 6 16 UPS04842402 120040507A574046143911 FITTING DOUG DC8 DC871F 302199DWP LEFT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, NR 2 MAIN TANK STRINGER 51 AT XRS 50 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4614391 AND SRM 51-1-20D. 2L74 4F RT4A25 20040616002072004061600207WP 2004 6 16 UPS04842403 120040507A53403758497 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 1140 LONGERON TO FRAME ATTACH FITTING IS CRACKED AT LONG 35R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D. 2L74 4F RT4A25 20040616002102004061600210NE 2004 6 16 UPS04M42406 220040524A7200 ENGINE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE NR 1,2,3 MALFUNCTIONED A IPXAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 SO01254UP ON DESCENT, 8000 FT ALL ENGS DID NOT RESPOND TO THROTTLE COMMAND. PUSHED THROTTLES FULL FWD NO RESPONSE. TURNED ON IGN OVRD END CAME BACK. BOTH MCP PNLS CONFIRMED ENG OUT THRUST LIMITS SHOWED MCT EAD. OIL PRESS ON 1&3 FELL BELOW 19 PSI, ENG 2 OIL 22 PSI. N1'S 35% W/THROTTLE FULL FWD ALL N1'S STILL DECREASING. W/ENG IDLE RUMBLE STOPPED. INCREASED THRUST ON EA ENG SEPARATELY. WHEN ADVANCED ENG 1 HAD LOUD NOISE. FLT DATA REC, PCMCIA MEDIA DISK & C/P VOICE REC DATA REVIEWED BY UPS PWR PLANT ENG & UPS FLT SAFETY. BOTH EVALS IND ALL 3 ENGS OP'D NORMAL DURING ENTIRE DESCENT PROFILE,NO LIMITS EXCEEDED, NO FLAMEOUTS, NO ENG SUB-IDLE CONDITIONS, APPROPRIATE THROTTLE RESPONSES & NO OTHER ABNORMS. 2L73 4F4 FRTA22WE E31N3 20040616002122004061600212NM 2004 6 16 0400825515 120040427A5315 FLOORBEAM BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 23203 DURING H-CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED PER EA 55-198769. 2L72 4F RTA2NM 20040616002132004061600213WP 2004 6 16 0400839996 120040504A5320 SUPPORT ANGLE DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING M-CHECK FOUND CRACK IN SLANTED PRESSURE PANEL SUPPORT ANGLE AT BS 699. REPAIRED PER EA 99-198726. 2L72 4F A6WE 20040616002152004061600215NM 2004 6 16 2004UALA00434 120040430A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA / STR 17 DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 SKIN IS DENTED AT STA 618 BELOW STR 17L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040616002192004061600219EA 2004 6 16 MASA200400286 120040523A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW077264V 7264 CREW REPORTED THAT THE ORANGE SECTION OF THE FLOOR PROXIMITY LIGHTING AT THE EMERGENCY EXIT WAS NOT ILLUMINATED DURING THE PREFLT CHECKS. CONTRACT MAINTENANCE WAS CALLED OUT AND FOUND THE CONNECTOR LOOSE BETWEEN THE SECTIONS ON THE FLOOR. RESECURED THE CONNECTOR, ACCOMPLISHED AN OPS CHECK, OPS CHECK WAS GOOD. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2L72 4F RTA21EA 20040616002212004061600221SO 2004 6 16 MASA200400241 120040502A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07828MJ 145218 THE FORWARD SECTION OF THE FLOOR EMERGENCY EXIT LIGHTS INOP. MX IS CURRENTLY TROUBLESHOOTING, OPS CHECKED LIGHTS AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040616002242004061600224NM 2004 6 16 ASAA0440109 120040420A5512655482128 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 FOUND TWO EACH DENTS ON HORIZONTAL STABILIZER LEADING EDGE, ONE AT 13 INCHES FROM INBOARD PLUS 1.25 INCHES BY .875 BY .020 DEEP, ONE AT 50 INCHES FROM INBOARD EDGE REF LOG PAGE 5755154. REPAIRED DENTES ON RIGHT HORIZONTAL STABILIZER LEADING EDGE PER SRM 55-10-01. (M) 2L72 4F RTA16WE 20040616002252004061600225NM 2004 6 16 ASAA0410252 120040503A53206545855524 INTERCOSTAL BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - FOUND DURING C-CHECK, INTERCOSTAL TOP AND BTM SIDES AT STATION 1006-1016, RBL 45-50 IS CORRODED. REMOVED DAMAGED WEB AND INSTALLED REPLACEMENT WEB IAW SRM 51-20-1. (M) 2L72 4F A16WE 20040616002312004061600231WP 2004 6 16 ASAA0480309 120040421A532199366401 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRUSHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 886-927, RBL 22-44 HAS CRUSHED EDGES. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040616002332004061600233NM 2004 6 16 ASAA0410235 120040501A531565671406 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND LONGITUDINAL FLOORBEAM AT STATION 540-727B, RBL 45 INBOARD FLANGE SURFACES CORRODED. REMOVED DAMAGED AND INSTALLED RPR STRAPS IAW EA5310-02356. (M) 2L72 4F A16WE 20040616002342004061600234NM 2004 6 16 ASAA0410249 120040503A53126546881119 BULKHEAD BOEING737 737290C 138448VNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND LOWER EXTERNAL SIDE OF AFT PRESSURE BULKHEAD AT SECTION 48, STATION 1040 IS DENTED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW SRM 53-10-4. (M) 2L72 4F A16WE 20040617000022004061700002WP 2004 6 17 ASAA0480354 120040423A533059114063 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND DENT IN FUSELAGE SKIN STATION 218 AND LONGERON 17L D = 1.5, X= .023, LESS THAN 1 INCH FROM LONGERON 17L. COLD WORKED DENT, COMPLIED WITH HFED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040617000032004061700003SO 2004 6 17 C2XA04BT063 120040601A3350 LIGHT EMB 145 EMB145ER 3260211SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714947 145054 CREW REPORTED PASSENGER DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. RESET EMERGENCY EXIT LIGHT SYSTEM, SYSTEM OPS CHECKED GOOD. AFTER ARRIVING IN EWR, DURING PREFLIGHT FOUND EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE INSPECTED SYSTEM, OPERATIONALLY TESTED EMERGENCY EXIT LIGHT SYSTEM IAW EMB145 MM 33-50-00, OPS CHECKED THE SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040617000042004061700004SO 2004 6 17 C2XA04BT065 120040611A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW2714952 145067 CREW REPORTED, DURING TAXI-OUT, EMERGENCY LIGHTS NOT ARMED, AND ELECTRICAL EMERGENCY ABNORMAL MESSAGES ON EICAS, EMERGENCY LIGHTS CAME ON IN CABIN. EVERYTHING BACK TO NORMAL AFTER 10-15 SECONDS. RETURN TO GATE IN NEWARK. MAINTENANCE FOUND PIN 62 ON CONNECTOR JO838 NOT STAYING SECURE. REMOVED AND REPLACED CANNON PLUG JO838, OPS CHECKED SYSTEM GOOD IAW EMB 145 AMM 24-61-55 (CHAPTER 20-4-0-01). AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040617000062004061700006SO 2004 6 17 C2XA04CL063 120040611A49304951680 VALVE EMB 145 EMB145LR 3260212SO APU STUCK A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2713997 145298 CLE FLIGHT 2044, THE CREW REPORTED A STRONG FUEL ODOR FROM THE APU. MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040617000072004061700007SO 2004 6 17 C2XA04CL062 120040603A3230 PROXIMITY SENSOR EMB 135 EMB135ER 3260203SO NLG DIRTY A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2717507 145215 CREW REPORTED THAT THE LANDING GEAR LEVER COULD NOT BE MOVED UP AFTER TAKEOFF. ALSO GOT LANDING GEAR AIR/GROUND FAIL MESSAGE ON ICAS. CREW DIVERTED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM. CLEANED CONNECTIONS ON NOSE LANDING GEAR PROXIMITY SENSORS, AND CYCLED GEAR SEVERAL TIMES. SYSTEM OPERATIONALLY TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040617000082004061700008SO 2004 6 17 C2XA04CL061 120040604A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712996 145296 CLE FLIGHT 2266, THE CREW REPORTED THAT THE SECOND TO AFT EMERGENCY LIGHT STRIP WAS INOP WHEN TESTED. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LIGHT STRIP. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040617000122004061700012 2004 6 17 SWAA041684 420040615A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 R2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040617000142004061700014NM 2004 6 17 SWAA041686 120040615A3350101114 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29503SW 24180 LEFT OVERWING EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS COVER PER MM. 2L72 4F RTA16WE 20040617000152004061700015 2004 6 17 SWAA041687 420040615A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 R2 DOOR EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040615000632004061500063NM 2004 6 15 ASAA0410217 120040426A5310654655830 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND SHEAR TIE AT STATION 986, BETWEEN 17L AND 19L IS CORRODED. REMOVED DAMAGED SHEAR TIE AND INSTALLED REPLACEMENT SHEAR TIE IAW 51-20-1. (M) 2L72 4F A16WE 20040615000812004061500081WP 2004 6 15 ABXA040187 120040513A5531991188218 RIB DOUG DC9 DC941 302207NWP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 2ND RIB DOWN FROM REMOVEABLE VERTICAL LEADING EDGE SECTION CRACKED ON RIGHT AFT SIDE. REPAIRED IAW ABX SSRM K05159 DRAWING. 2L72 4F A6WE 20040615000832004061500083WP 2004 6 15 ABXA040190 120040514A53125910130392N1 BULKHEAD DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 NR 2 TEE CAP WAS FOUND TO BE CRACKED AT OUTBOARD END OF RADIAL Z34. REPLACED NR 2 TEE CAP IAW EA 53120033. 2L72 4F A6WE 20040615000852004061500085WP 2004 6 15 ABXA040189 120040513A53115911448509 FRAME DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 CORROSION ON FRAME LOWER LEG AT STA 446, LONGERON 30. REPAIRED IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040615000872004061500087WP 2004 6 15 ABXA040186 120040513A553199118297 RIB DOUG DC9 DC941 302207NWP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23976AX 47596 REMOVEABLE VERTICAL LEADING EDGE SECTION 5TH RIB UPON RIGHT SIDE CRACKED AT AFT END. REPAIRED RIB IAW DC-9 SSRM K05159. 2L72 4F A6WE 20040615000892004061500089NM 2004 6 15 SWAA041661 120040611A33501000679 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 OVERHEAD EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F A16WE 20040615001002004061500100EA 2004 6 15 SWIA200413344 120040416A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07405SW 7029 FS 280 RIGHT FLOORBEAM ANGLE RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPAIRED IAW CRJ REO 601R-53-11-136 REV NC AND RII 53-401. 2L72 4F RTA21EA 20040615001062004061500106NM 2004 6 15 SWAA041645 120040609A3350OL3071BPEGL LAMP BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED A2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040615001082004061500108SO 2004 6 15 SWIA200413332 120040414A5712 RIB EMB 120 EMB120ER 3260203SO LT WING LE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 LT INBOARD LEADING EDGE RIB HAS A SMALL CRACK. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT ADDED AT AFFECTED AREA OF LT LEADING EDGE RIB IAW EMB120 SRM 51-10-02 PG 2 SEC 2B. 2L72 4T RTA31SO 20040615001112004061500111EA 2004 6 15 SWIA200413335 120040519A274184897131 MOTOR CNDAIRCL600 CL6002C10 1390015EA HOR STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07702SK 10136 STAB TRIM CH 1 INOP, DURING DESCENT. REMOVED AND REPLACED STAB TRIM ACTUATOR MOTOR NR 1 IAW AMM 27-42-03-400-801-401. OPS CHECK GOOD IAW CRJ MM 27-40-00 AND SL-27-022 REV A. S/N OFF: 488. 2L72 4F RTA21EA 20040615001382004061500138EA 2004 6 15 SWIA200413301 120040505A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 ENGINE SUPPORT BEAM UPPER WEB RBL 6.0 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED UPPER AND LOWER WEBS OF ENGINE SUPPORT BEAM IAW CRJ REO 601R-53-61-345 REV ''C''. 2L72 4F RTA21EA 20040615001412004061500141EA 2004 6 15 SWIA200413304 120040506A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07939SW3015 3015 7742 STAB TRIM CH NR 1 WILL NOT RESET MESSAGE STAB CH 1 INOP. REMOVED AND REPLACED HSTCU & MCU IAW CRJ MM 27-42-01 & 27-42-05 & FORM RII 27-415. OPS CHECKS GOOD. MCU, P/N: 7062-3, S/N OFF: 1034. 2L72 4F RTA21EA 20040615001532004061500153EA 2004 6 15 SWIA200413325 120040518A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA FLAPS MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07448SW 7678 CONTINUOUS OVERSPEED WARNING SOUNDS WITH FLAPS SELECTED GREATER THAN 20 DEGREES. REMOVED AND REPLACED FECU IAW MM 27-51-05. SYSTEM OPS CHECKS GOOD. S/N OFF: 921. 2L72 4F RTA21EA 20040615001542004061500154SO 2004 6 15 SWIA200413326 120040505A5415 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07581SW 120349 LEFT OUTBOARD NACELLE BRACKET ATTACHED TO GEAR DOOR HINGE POINT FRAME AND CRADLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER ON LEFT OUTBOARD HALF FRAME ATTACH BRACKET IAW 120 SRM 51-10-02 PG 2 SEC 2B. 2L72 4T4 TRTA31SO E20NE 20040615001712004061500171EA 2004 6 15 SWIA200413312 120040511A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07405SW1182 1182 7029 LARGE ROLLING MOMENT WHEN FLIGHT SPOILERS EXTENDED. INSTALLED SERVICEABLE PCU ON RIGHT SPOILER IAW 27-62-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040616000092004061600009NM 2004 6 16 ASAA0410209 120040426A5245 STRUCTURE BOEING737 737290C 138448VNM A/C DOOR DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - FOUND DURING C-CHECK, LEFT AIR COND BAY DOOR IS DISBONDING. REBONDED ALUMINUM FOIL PLY IAW EA 5240-01114. (M) 2L72 4F A16WE 20040616000102004061600010NM 2004 6 16 ASAA0410247 120040503A5315 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 DURING C-CHECK, FOUND AFT CARGO BAY MAIN FLOORBEAM IS CORRODED. INSTALLED PERMANENT REPAIR IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040616000142004061600014NM 2004 6 16 ASAA0480410 120040516A532199365441 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-200, LBL 44-54 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000252004061600025NM 2004 6 16 ASAA0480425 120040517A532095200089 STRAP DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND AFT PIT DOOR JAMB STRAP AT STATION 1168-1207 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT STRAP IAW 51-10-2. (M) 2L72 4F RT 20040616000322004061600032NM 2004 6 16 ASAA0480429 120040517A5730ARB0975517 PANEL DOUG MD80 MD83 3023681NM WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND FUEL PANEL NR 1478C HAS SURFACE CORROSION ON INSIDE FLANGE. REMOVED DAMAGE AND REPLACED FUEL PANEL IAW 51-22-2A. (M) 2L72 4F RT 20040616000382004061600038NM 2004 6 16 ASAA0480416 120040516A532199578241 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL BELOW FIRST OFFICERS SEAT IS PUNCTURED. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW 53-01. (M) 2L72 4F RT 20040616000482004061600048SO 2004 6 16 MASA200400250 120040506A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07829MJ 145228 CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS INOP. MX REPLACED THE BULB AND OPS CHECK GOOD. 2L72 4T RTT00011AT 20040616000502004061600050SO 2004 6 16 MASA200400239 120040401A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07834MJ 145340 CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 12 LIGHT WAS INOP. MX REPAIRED WIRING AT THE EXIT ROW SIGN, OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040616000532004061600053SO 2004 6 16 MASA200400211 120040420A1420 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SW07844MJ 145481 AT DEPARTURE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT AT ROW 12 INOP. MX FOUND LOOSE CONNECTOR. RESECURED, OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040616000602004061600060NM 2004 6 16 2004UALA00483 120040522A5753 FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAPS CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29659UA 27114 RT WING INBOARD FLAP, MIDDLE T/E HINGE FITTING IS CRACKED AT SPAR. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA1NM E24NE 20040616000822004061600082NM 2004 6 16 2004UALA00513 120040530A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 CABIN FLOORBEAM UPPER CAP CORRODED AT STA 365 RBL 9 TO 16. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS. 2L72 4F4 FRTA2NM E17NE 20040616000882004061600088NM 2004 6 16 2004UALA00518 120040601A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STATION 277 STRINGER 15R STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20040616000962004061600096WP 2004 6 16 0400959989 120040603A2923AS19593C PUMP DOUG DC9 DC931 3022065WP RT HYD SYSTEM LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL018945E 47181 RIGHT HYDRAULIC SYSTEM QUANTITY DROPPED TO LESS THAN 3 QUARTS DURING DESCENT. COM PROCEDURES COMPLIED WITH AND PRESSURE WAS NORMAL. FLIGHT LANDED WITHOUT INCIDENT AT IAH AND THEN HYDRAULIC QUANTITY DROPPED TO ZERO AFTER TOUCHDOWN. MAINTENANCE FOUND A LEAK AT THE PRESSURE OUTLET OF THE AUXILIARY HYDRAULIC PUMP. THE ELECTRIC AND THE ENGINE DRIVEN PUMPS ALONG WITH ALL FIVE OF THE RIGHT HYDRAULIC SYSTEMS FILTERS WERE REPLACED. THE AIRCRAFT HAS RETURNED TO SERVICE. 2L72 4F A6WE 20040616001062004061600106NM 2004 6 16 2004UALA00524 120040528A2421 GENERATOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LEFT INOPERATIVE A UALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 WP29644UA 25094 RETURN TO FIELD DUE TO L-GENERATOR INOP. TEARDOWN REVEALED THAT THE DIFFERENTIAL AND CLUSTER GEARS WERE SEVERELY DAMAGED BEYOND REPAIR. IT APPEARS THAT SOME KIND OF CONTAMINATION WAS INTRODUCED WHICH EITHER INTERRUPTED/DILUTED THE OIL SUPPLY TO ONE OF THE CLUSTER GEARS, OR DAMAGED THE PLATING ON THE SHAFT RESULTING IN LARGE AMOUNTS OF METAL INTRODUCED IN-BETWEEN BEARING SURFACES. THE CONTAMINATION COULD HAVE BEEN FUEL (OR SOME OTHER CONTAMINATE WHICH LOWERED THE VISCOSITY OF THE OIL), OR SOME OTHER FOREIGN PARTICLE(S) INTRODUCED EARLY IN THE UNITS LIFE. NO FUEL SMELL WAS NOTED BY TECHNICIAN DURING TEARDOWN. THE UNIT IS UNDERGOING A COMPLETE OVERHAUL. 2L72 4F4 FRTA1NM E24NE 20040616001082004061600108NM 2004 6 16 2004UALA00526 120040531A4920 APU BOEING757 757222 1384956NM PWA 2037 PW2037 NE MALFUNCTIONED A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29564UA 26666 APU ON AT GATE FOR 3 MIN. PUT BOTH PACKS ON NOTICED BLUE-OIL SMOKE IN COCKPIT & CABIN. REPLACED APU. STAT-O-SEALS FAILED IN THE DRIVEN COMPRESSOR MODULE. RUBBER WAS EXTRUDED AND TORN FROM BOLT HEAD AND SHAFT. NO LOOSE BOLTS NOTED. SEALING FUNCTION COMPROMISED ON BACKSHROUD INNER DIAMETER BOLT CIRCLE. 2L72 4F4 FRTA2NM E17NE 20040616001182004061600118NM 2004 6 16 2004UALA00493 120040524A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 AFT PIT FRAME INNER FLANGE DENTED 3 PLACES WITHIN 7.5 INCHES FROM JUST INBOARD OF STR 26L TO JUST ABOVE STR 26L AT STA 1400. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001232004061600123NM 2004 6 16 2004UALA00498 120040524A2910 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE YELLOW HYD SYS ILLUMINATED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29838UA 1477 CREW ADVISED MOMENTARY LOSS OF BLUE & YELLOW HYDRAULICS WHILE EN ROUTE. REGAINED YELLOW. AMBER ALERT DECLARED. UNABLE TO DUPLICATE DISCREPANCY. NO PARTS REPLACED. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616001272004061600127NM 2004 6 16 2004UALA00502 120040524A2497W5081300120 WIRE HARNESS BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CARGO BAY SHORTED A UALAO OTHER M OVER TEMP NRNOT REPORTED 1 WP29791UA29899 26933 FOUND WIRE BUNDLE IN PIT BURNED. ALL CB'S IN PIT POPPED. CAUSE IS UNDERSTOOD AT THIS TIME TO BE A PRODUCTION SPLICE FOR A PDU SHORTED FROM MOISTURE, RESULTING FROM DIRECT CONTACT WITH THE BILGE INSULATION. REMOVED WIRES ARE BEING ANALYZED. REPLACED THE DAMAGED WIRES IN THE BUNDLE BY SPLICING PER AMM CHAPTER 20, AND RAISING THE WIRE BUNDLE UP OFF THE INSULATION BLANKET BY INCORPORATING THE INTENT OF BOEING SERVICE BULLETIN 777-25-0171. 2L72 4F4 FRTT0001SE E46NE 20040616001302004061600130NM 2004 6 16 2004UALA00504 120040526A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 LEFT FUSE SKIN IS DENTED AT STA 610-625, STR 15L-17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW PARTIAL SKIN PNL WITH DOUBLER SPLICES. 2L72 4F4 FRTA2NM E17NE 20040616001372004061600137NM 2004 6 16 C1HA200492011 120040519A5330 SKIN BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 STA 970 STR 28L SKIN CORROSION. INSTALLED DOUBLER. 2L73 4F A3WE 20040616001412004061600141NM 2004 6 16 C1HA200492008 120040519A5310 SHEAR TIE BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 STA 1148 STR 27L SHEAR TIE CORROSION. 2L73 4F A3WE 20040616001442004061600144NM 2004 6 16 2004UALA00510 120040527A5311 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 STA 887 SHEAR TIE BETWEEN STR 24R AND 25R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SHEAR TIE WEB AND REPLACED. 2L72 4F4 FRTA16WE E2GL 20040616001542004061600154NM 2004 6 16 2004UALA00453 120040510A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 AFT PIT FRAME WEB AT STA 2120 RBL 41.33 CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB SECTION. 2L74 4F4 FRTA20WE E24NE 20040616001622004061600162NM 2004 6 16 2004UALA00461 120040510A5330 LAP JOINT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 FUSELAGE STATION 1710 STR 20L LAP SEAM SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. SERVICE TRUCK DAMAGE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR AND FILLER MATERIAL. 2L72 4F4 FRTA2NM E17NE 20040616001652004061600165NM 2004 6 16 2004UALA00560 120040428A5754 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE LE SLATS TE DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29773UA 26929 TRAILING EDGE WEDGE DELAMINATED LWR INBOARD SURFACE. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE. 2L72 4F4 FRTT0001SE E46NE 20040616001682004061600168NM 2004 6 16 2004UALA00563 120040608A2913 PUMP AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE YELLOW HYD SYS FAILED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29805UA 783 YELLOW HYDRAULIC SYSTEM FAILED. NR 2 ENGINE DRIVEN PUMP FOUND LEAKING. REPLACED ENGINE DRIVEN PUMP. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040616001722004061600172NM 2004 6 16 2004UALA00567 120040610A2821 FUEL FILTER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT ENGINE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29664UA 29236 LT ENGINE FUEL FILTER EICAS MSG DISPLAYED 10 TO 15 MINS THEN CHANGED TO STATUS MSG. THE FUEL FILTER WAS REPLACED AND NO CONTAMINATION WAS FOUND. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER EVENTS. 2L72 4F4 FRTA1NM E24NE 20040616001842004061600184SO 2004 6 16 MASA200400248 120040505A5210 GATE EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A MASAK NONE O OTHER ININSP/MAINT 1 SW07857MJ 145765 THE PAX DOOR UPPER FLAP WOULD NOT CLOSE COMPLETELY. MX LUBED THE DOOR AND THE FLAP OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2L72 4T RTT00011AT 20040616001872004061600187WP 2004 6 16 UPS04842389 120040508A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 1741 LONG 17L IS CRACKED. REMOVED LONGERON SECTION, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION AND INSTALLED SPLICE FITTINGS AND STRAPS IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040616001892004061600189WP 2004 6 16 UPS04842391 120040503A53203779659U501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE:C1 STATION 850 LONGERON 5R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, AND M/M 20-14-00. 2L74 4F RT4A25 20040616002082004061600208WP 2004 6 16 UPS04842404 120040507A534037558271N FITTING DOUG DC8 DC871F 302199DWP LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 280 BANANA FITTING IS CRACKED BETWEEN LONG 31R-32R. REMOVED AND REPLACED FITTING IAW DWG 3755827 AND SRM 51-1-20D. 2L74 4F RT4A25 20040616002092004061600209WP 2004 6 16 UPS04842405 120040510A5240 DOUBLER DOUG DC8 DC871F 302199DWP LT CENTER DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, LT CENTER SERVICE DOOR TORQUE TUBE CUTOUT DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 52-2-0 FIG 2. 2L74 4F RT4A25 20040616002112004061600211EA 2004 6 16 MASA200400290 120040524A77976015091017 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NR 1 ENGINE INOPERATIVE A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0717217153132203 7217 DURING TAKEOFF ROLL A NR 1 ENGINE N2 VIBE ICON ILLUMINATED CAUSING THE PILOT TO ABORT TAKEOFF. DURING TROUBLESHOOTING IT WAS DETERMINED TO BE AN INDICATION ONLY AND PLACED ON MEL. MX REPLACED WIRE HARNESS AND TRANSDUCER. 2L72 4F RTA21EA 20040616002272004061600227WP 2004 6 16 ASAA0480313 120040421A5347593054768 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 242-256, X=-45 IS GOUGED. REMOVED DAMAGED SECTION AND REPLACED PER SRM 53-05. (M) 2L72 4F RTA6WE 20040616002322004061600232WP 2004 6 16 ASAA0480308 120040421A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 864-886, LBL 22-44 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040617000012004061700001WP 2004 6 17 ASAA0480353 120040423A52805930503501 RUB STRIP DOUG DC9 DC983 3022083WP MLG DOOR DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND RUB STRIP DISBONDED ON DOOR LANDING FOR PANEL 1365C. REMOVED RUBSTRIP, REAMED DISCREPANT HOLES, FABRICATED AND INSTALLED REPAIR SLEEVE BUSHINGS. INSTALLED RUBSTRIP IAW ASA EA 5720-01248 AND AAR EA 10394. (M) 2L72 4F RTA6WE 20040617000112004061700011NM 2004 6 17 SWAA041696 120040615A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 930 TO BS 947, BETWEEN STRINGERS 21R & 24R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20040617000162004061700016NM 2004 6 17 SWAA041688 120040615A3350PL2230LH00 LIGHT BOEING737 7377H4 1384404NM ROW 17 WORN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29756SA 27872 EEPLS STRIP WORN AT ROW 17. REMOVED AND REPLACED EEPLS STRIP SECTION PER MM. 2L72 4F RTA16WE 20040617000172004061700017NM 2004 6 17 SWAA041689 120040615A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 19R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040617000202004061700020SO 2004 6 17 C2XA04SH342 120040604A531514529150003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715572 145636 DURING C-CHECK THE RIGHT CROSS BEAM ANGLE AT FRAME 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000212004061700021SO 2004 6 17 C2XA04SH318 120040525A531014525480003 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000242004061700024GL 2004 6 17 C2XA04IA055 220040525A7313FNKA1P3 FUEL NOZZLE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ZONE 400 FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2726549 145571 CREW REPORTED THAT THERE WERE FUMES IN THE CABIN AND COCKPIT DURING ANTI-ICE OPERATION. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL NOZZLES. THE ENGINES WERE RUN AND THE ANTI-ICE SYSTEM OPERATED WITH NO FURTHER SMELL NOTED. THE DISCREPANCY WAS THEN CLEARED. 2L72 4T4 FRTT00011ATTE6CH 20040617000272004061700027NM 2004 6 17 SWAA041691 120040615A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20040617000282004061700028SO 2004 6 17 C2XA04CL056 120040514A1420 CONNECTOR EMB 145 EMB145ER 3260211SO COCKPIT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714947 145054 CLE FLIGHT 2025, THE CREW REPORTED THE EMERGENCY LIGHT AT THE COCKPIT STEP WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET CONNECTOR ON THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040617000302004061700030SO 2004 6 17 C2XA04SH345 120040606A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715572 145636 SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED BY THE LEFT AND RIGHT UPPER SUPPORT BRACKETS. MAINTENANCE PERFORMED DOUBLER REPAIRS TO THE AFFECTED AREAS IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000312004061700031NM 2004 6 17 SWAA041692 120040615A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND STR 5L CRACKED AT FASTENER HOLE, BS 380. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040617000342004061700034SO 2004 6 17 C2XA04IA057 120040406A33502013BR BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27159853061 262 145248 DURING ROUTINE CHECK, THE FORWARD AISLE PATH LIGHTING STRIP WAS FOUND TO BE DIM WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK, OPERATIONALLY CHECKED THE LIGHTING SYSTEM, AND THE DISCREPANCY WAS CLEARED. 2L72 4T RTT00011AT 20040617000362004061700036SO 2004 6 17 C2XA04IA065 120040613A243232845001 BATTERY EMB 145 EMB145LR 3260212SO MASTER OVERTEMP A C2XAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW27169191123 1123 145393 THE CREW REPORTED A NUMBER TWO BATTERY OVERTEMP IN FLIGHT. THE AIRCRAFT DIVERTED TO EFD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH AIRCRAFT BATTERIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000372004061700037SO 2004 6 17 C2XA04IA064 120040609A33507287580501 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714923 145318 FLIGHT 3388 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING AT MID-CABIN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000382004061700038SO 2004 6 17 C2XA04SH300 120040519A532014522226003 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000402004061700040SO 2004 6 17 C2XA04IA066 120040613A3350602044 SIGN EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT AN EMERGENCY EXIT SIGN WAS INOPERATIVE. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT HAND EMERGENCY EXIT LINER SIGN TO BE INOPERATIVE. CONTRACT MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617000422004061700042SO 2004 6 17 C2XA04SH351 120040610A532014521718003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714573 145638 DURING C-CHECK THE LEFT RAMP ANGLE BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED, FABRICATED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-30-00 AND EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000432004061700043SO 2004 6 17 C2XA04SH353 120040610A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714573 145638 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 4 FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000442004061700044SO 2004 6 17 C2XA04SH354 120040610A531514521725001 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE LEFT CROSSBEAM AT FRAME 19 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000452004061700045SO 2004 6 17 C2XA04IA062 120040608A33501317 LAMP EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 IAH- FLIGHT 2673, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT, AND FLOOR PROXIMITY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE GALLEY EMERGENCY LIGHT BULB, RESET THE EMERGENCY LIGHT SYSTEM, AND OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000462004061700046SO 2004 6 17 C2XA04IA063 120040609A33502013BR BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27111213723 3723 145683 IAH - FLIGHT 2556, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT NUMEROUS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617000472004061700047SO 2004 6 17 C2XA04CL058 120040521A3350 SIGN EMB 145 EMB145ER 3260211SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714942 145037 THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20040617000482004061700048NM 2004 6 17 SWAA041668 120040613A53209078224 STRAP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND H-STRAP AT FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REPAIRED STRAP PER EA. 2L72 4F RTA16WE 20040617000502004061700050WP 2004 6 17 MWEA040081 120040525A53105934423 DOOR FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 AFT BAG PIT DOOR JAMB WEB AT STATION 1160 BETWEEN LONGERON 28 RIGHT AND 29 RIGHT HAS AREAS OF CORROSION AROUND ACCESS HOLE. FABRICATED AND INSTALLED WEB. 2L72 4F A6WE 20040617000512004061700051NM 2004 6 17 MWEA040082 120040524A2701 CONTROL COLUMN BOEING717 717200 1383700NM FLIGHT CONTROL INOPERATIVE A MWEAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31913ME 55177 CREW REPORTED COLUMN DISCONNECT. RECONNECTED CONTROL COLUMN, OPERATIONS CHECK GOOD. 2L72 4F TRA6WE 20040617000522004061700052CE 2004 6 17 ACE052804 120040528A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE MLG CONTAMINATED E YADAO OTHER S AFFECT SYSTEMS APAPPROACH 1 AL03112AX UC45 PILOT REPORTED LANDING GEAR DID NOT EXTEND WHEN HANDLE WAS SELECTED DOWN. ALTERNATE (HAND PUMP) EXTENSION PERFORMED. REPLACED HYDRAULIC MOTOR RELAY (CONTAMINATED WITH WATER). 2L72 4T RTA24CE 20040617000562004061700056NM 2004 6 17 AWXA200400568 120040515A5347D5311278220201 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD END OF SEAT TRACK Y1292 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 FROM FR 12 TO FR 24; INSTALLED NEW REPLACEMENT SEAT TRACK IAW A319 SRM 51-72-11 PG 1 & 2. 2L72 4F RTA28NM 20040617000572004061700057NM 2004 6 17 AWXA200400569 120040516A5320D5347112320200 SUPPORT AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FRAME SUPPORT JUST FORWARD OF FR 70, STR 23 LT. MAINTENANCE REMOVED CORRODED FRAME SUPPORT AT FR 70, STR 23 LT; FABRICATED A NEW REPLACEMENT FRAME SUPPORT; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 1-3, 8, 14 & 17. 2L72 4F RTA28NM 20040617000592004061700059NM 2004 6 17 AWXA200400571 120040515A5315D5347217220200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 AT FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11. 2L72 4F RTA28NM 20040617000632004061700063WP 2004 6 17 DHL2004803504 120040319A5347 SEAT TRACK DOUG DC8 DC873 302199CWP FUSLAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN STA 1580.000. CUT OUT WORN SECTION OF NR 6 FLOOR TRACK, STA 1580.000 IAW DC8 SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3-0 PG 1, DC8 SRM 53-2-3 PG 17-19. 2L74 4F RT4A25 20040617000652004061700065WP 2004 6 17 DHL2004803503 120040318A5347 SEAT TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN, STA 1493.000. CUT OUT DAMAGED SECTION OF NR 6 FLOOR TRACK STA 1493.000 IAW DC8 SRM 53-2-3 FIG 6D, PG 17. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3-0 PG 1, DC8 SRM 53-2-3 PG 17-19. 2L74 4F RT4A25 20040617000672004061700067WP 2004 6 17 DHL2004803500 120040319A534774529523 SEAT TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT NR 2 FLOOR TRACK PLUG IN POOR CONDITION, STA 774.000. REMOVED PLUG AT STA 774.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20040617000682004061700068WP 2004 6 17 DHL2004803518 120040328A5310 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 FWD CARGO COMPT SPLICE FITTING CRACKED 9.000 STA FS 440.000 TO 460.000, L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20040617000692004061700069WP 2004 6 17 DHL2004803505 120040323A5753 SKIN DOUG DC8 DC873 302199CWP RT TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RIGHT INBOARD FLAP HAS INTERIM REPAIR ON UPPER FWD PLATING, STA XW 104.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 1. REMOVED PLATING WITH INTERIM REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING 92024T3 0.040 IAW DC8 SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND PLATING INNER FACE IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040617000702004061700070WP 2004 6 17 DHL2004803509 120040319A5531 FRAME DOUG DC8 DC873 302199CWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 VERTICAL STAB L/E FRAME CRACKED 2.000 AT STA 105.000 (RT SIDE). STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040617000712004061700071WP 2004 6 17 DHL2004803552 120040519A57205643433 ANGLE DOUG DC8 DC873 302199CWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LEFT WING REAR SPAR L-ANGLE CORRODED, STA XCW 46.000. REMOVED CORRODED L-ANGLE IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1-3. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. FABRICATED NEW L-ANGLE (7075-T651) IAW EA 5730-019, DWG 5643433. HEAT TREATED IAW DC8 SRM 51-1-1 PG 1-13-17. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA AND NEW L-ANGLE IAW DC8 SRM 51-1-8B. INSTALLED NEW L-ANGLE AFTER COMPLYING WITH MSI 57100020-001-D IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040617000722004061700072NM 2004 6 17 SWAA041670 120040613A53106546529 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500, BL 0, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040617000732004061700073NM 2004 6 17 SWAA041671 120040613A53116546539 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT LT BS 616, WL 208, CRACKED. REPAIRED FRAME SECTION PER T1-153-018. 2L72 4F RTA16WE 20040617000742004061700074 2004 6 17 SWAA041672 420040613A256563550 SLIDE BOEING737 7377H4 1384404NM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29403WN 29815 DURING SCHEDULED C2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040617000752004061700075 2004 6 17 SWAA041673 420040613A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F A16WE 20040617000802004061700080NM 2004 6 17 SWAA041678 120040614A53106617365 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM ZEE CHORD AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED CREASE BEAM Z CHORD PER SRM. 2L72 4F RTA16WE 20040617000842004061700084SO 2004 6 17 C2XA04SH304 120040519A532014524131007 BRACKET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK, THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000852004061700085SO 2004 6 17 C2XA04SH356 120040610A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000862004061700086SO 2004 6 17 CX2A04RI001 120040609A3350 LIGHT EMB 145 EMB145XR 3260214SO EMERGENCY EXIT INOPERATIVE A C2XAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW2718102 145643 CREW REPORTED THE RIGHT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. MAINTENANCE RESET THE EMERGENCY EXIT LIGHT AND PERFORMED A SATISFACTORY OPERATIONAL TEST. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617000912004061700091SO 2004 6 17 C2XA04SH365 120040614A531513500222001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 DURING C-CHECK THE UPPER STRINGER ON THE CENTER FLOORBEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000922004061700092SO 2004 6 17 C2XA04SH333 120040529A532014521725013 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C-CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000932004061700093SO 2004 6 17 C2XA04SH334 120040529A532014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C-CHECK, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000942004061700094SO 2004 6 17 C2XA04SH308 120040520A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713566 145622 DURING C-CHECK, THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000952004061700095SO 2004 6 17 C2XA04TY082 120040522A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715912 145439 DURING A SERVICE ROUTINE INSPECTION OF A/C, THE LT AFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IAW EMB 135/145 AMM 33-50-07. OPS CHECK WAS GOOD AND A/C WAS PUT BACK IN SERVICE. 2L72 4T RTT00011AT 20040617000962004061700096SO 2004 6 17 C2XA04IA054 120040511A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716999 145307 THE MAIN PASSENGER DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LIGHT ASSEMBLY, OPERATIONALLY TESTED THE LIGHT AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20040617000992004061700099SO 2004 6 17 C2XA04SH358 120040611A531514532636401 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01124. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001012004061700101SO 2004 6 17 C2XA04SH347 120040609A533014520554001 SKIN EMB 145 EMB145 3260210SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE EXTERNAL FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 20 AND 21, AND BETWEEN STRINGERS 12L AND 13L. MAINTENANCE PERFORMED A PATCH REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001032004061700103SO 2004 6 17 C2XA04SH349 120040609A491014547494401 FIREWALL EMB 145 EMB145 3260210SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND MOUNTING BRACKET. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001082004061700108SO 2004 6 17 C2XA04TY090 120040612A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712569 145630 TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER RIGHT ENGINE MOUNT. MAINTENANCE FABRICATED A FILLER AND DOUBLER, AND INSTALLED IAW EC5330-01267. 2L72 4T RTT00011AT 20040617001122004061700112SO 2004 6 17 C2XA04TY086 120040530A531514522226003 FLOORBEAM EMB 145 EMB145LR 3260212SO LAV FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715574 145639 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LAVATORY CENTER FLOORBEAM CAP AT FRAME 58. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM CAP IAW EMB SRM 51-40-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040617001132004061700113SO 2004 6 17 C2XA04IA058 120040604A243232845001 BATTERY EMB 145 EMB145XR 3260214SO MASTER OVERTEMP A C2XAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW2713161282 282 14500805 AUS - FLT 3214, THE CREW REPORTED THAT THE NR 1 MAIN BATTERY OVERHEATED IN CLIMB. THE AIRCRAFT DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH MAIN BATTERIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617001142004061700114SO 2004 6 17 C2XA04IA059 120040606A3230 LANDING GEAR EMB 145 EMB145XR 3260214SO MAINS MALFUNCTIONED A C2XAO OTHER J WARNING INDICATION TOTAKEOFF 1 SW2711127 145697 DURING TAKEOFF, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE GEAR LEVER WITH SATISFACTORY RESULTS AND CONTINUED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS FOR THE EXTENSION/RETRACTION SYSTEM IAW EMB-145 AMM 32-30-00 WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617001152004061700115SO 2004 6 17 C2XA04IA060 120040529A335020131A BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27241289966 8605 145700 DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE RIGHT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS PLACED ON MEL 33-50-04 CONTROL 041499, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO MCI ON 05-30-04 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617001162004061700116SO 2004 6 17 C2XA04SH306 120040520A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER RIGHT HAND MOUNT BRACKET. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001172004061700117NE 2004 6 17 C1HA200474003 220040531A7230 COMPRESSOR BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE NR 1 ENGINE STALLED A C1HAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL15674MG 21450 COMPRESSOR STALLS NR 2 ENGINE 350 LEVEL OFF, PWR REDUCTION, NR 2 EPR DROPPED. THRUST LEVER TO IDLE INDICATIONS NORMAL. LEFT IN IDLE FOR REMAINDER OF FLIGHT. PERFORMED CENTER ENGINE COMPRESSOR STALL CHECK, GROUND CHECK FOR BLEED OPERATION AND ACEL/DECEL CHECK. MALFUNCTION NOT DUPLICATED. ENGINE OPERATED WITHIN PARAMETERS M/M 71-00-00, 73-30-00, 71-00-36. BLEED VALVE LUBRICATION MM 72-00-00 STEP 6, ENGINE RUNS OPS CHECK GOOD. 2L73 4F4 F A3WE E2EA 20040617001222004061700122SO 2004 6 17 C2XA04SH305 120040520A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAMES 20 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001232004061700123SO 2004 6 17 C2XA04SH307 120040520A532014522460013 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001242004061700124SO 2004 6 17 C2XA04SH291 120040516A531514522461011 DOUBLER EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV - DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001262004061700126SO 2004 6 17 C2XA04SH289 120040516A532014529150003 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV - DURING C-CHECK THE LOWER ANGLE ON THE CROSSBEAM BETWEEN THE SERVICE DOOR AFT SILL AND THE CENTER FLOORBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001322004061700132SO 2004 6 17 C2XA04SH368 120040615A532014521725001 SILL EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 DURING C-CHECK THE LEFT FLOOR SILL WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001332004061700133SO 2004 6 17 C2XA04CL060 120040601A3240510404EE17 COUPLING EMB 145 EMB145LR 3260212SO NR 4 BRAKE LOOSE A C2XAO OTHER O OTHER LDLANDING 1 SW2716951 145063 THE CREW REPORTED THE BRAKES WERE NOT VERY EFFECTIVE ON LANDING. THE ANTI-SKID WAS ENGAGED UNTIL 10 KNOTS. MAINTENANCE INSPECTED AND FOUND THE NR 4 BRAKE NOT WORKING ON NORMAL BRAKING. THE QUICK DISCONNECT COUPLING ON THE NR 4 BRAKE WAS RETIGHTED. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040617001342004061700134SO 2004 6 17 C2XA04SH367 120040615A532014525422001 SILL EMB 135 EMB135LR 3260305SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 DURING C-CHECK THE LEFT HAND CARGO SILL WAS FOUND TO BE CORRODED AT FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001402004061700140SO 2004 6 17 C2XA04TY083 120040521A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712567 145623 DURING A SCHEDULED 1C INSPECTION THE LT FLOORBEAM WAS FOUND CORRODED AT THE CARBON SUPPORT. MAINTENANCE REPAIRED THE LT FLOORBEAM, ALODINED AND PAINTED IAW EMB 135/145 SRM 53-21-10; AND CPM 51-21-04; 05; 06 ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040617001442004061700144NM 2004 6 17 C1HA200492002 120040518A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 SEAT TRACK CORROSION. 2L73 4F A3WE 20040617001452004061700145NM 2004 6 17 C1HA200492001 120040518A5320 INTERCOSTAL BOEING727 727212 138407GNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 INTERCOSTAL CRACKED AT UPPER FLANGE. 2L73 4F A3WE 20040617001462004061700146SO 2004 6 17 C2XA04TY084 120040521A532014529150003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712567 145623 DURING A SCHEDULED 1C INSPECTION THE AFT GALLEY STEP-UP WAS FOUND CORRODED. MAINTENANCE REMOVED THE AFT GALLEY STEP-UP. NEW STEP-UP, ALODINED, PRIMED, PAINTED AND INSTALL IAW EMB 135/145 SRM 51-40-03; 51-21-03; 04; 05 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040617001502004061700150SO 2004 6 17 C2XA04SH350 120040609A533014520556001 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714573 145638 DURING C-CHECK THE RIGHT LOWER FUSELAGE SKIN WAS FOUND TO BE DENTED IN 4 PLACES, 3 OF THE DENTS WERE WITHIN LIMITS IAW EMB 145 SRM 53-22-01 AND THE 4TH DENT WAS FOUND TO BE GOUGED IN THE BOTTOM OF THE DENT. MAINTENANCE REMOVED THE DAMAGED AREA AND RECONTOURED THE DENT AREA AND INSTALLED A RIVET/WASHER REPAIR IAW EMB 145 SRM 51-30-01 AND EMB 145 SRM 53-22-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001522004061700152SO 2004 6 17 C2XA04SH293 120040518A531014521699003 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 20 AND 21. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001542004061700154NM 2004 6 17 SWAA041680 120040614A53216545833 FLOOR PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT RIGHT BS 188 TO RIGHT BS 196, WL 208, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2L72 4F RTA16WE 20040617001572004061700157NM 2004 6 17 SWAA041683 120040614A53126546541 STIFFENER BOEING737 7377H4 1384404NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29729SW 27861 DURING SPV, FOUND BULKHEAD ANGLE STIFFENER AT BS 663, LBL 10 TO LBL 24, CRACKED. REMOVED AND REPLACED STIFFENER SRM. 2L72 4F RTA16WE 20040617001582004061700158SO 2004 6 17 C2XA04SH320 120040526A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV - DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001592004061700159SO 2004 6 17 C2XA04SH321 120040526A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 1 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 SHV - DURING C-CHECK THE NR 1 ENGINE INTAKE COWLING MOUNTING FLANGE WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001612004061700161SO 2004 6 17 C2XA04SH299 120040519A532014524131011 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713566 145622 DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001622004061700162GL 2004 6 17 C2XA04IA072 220040615A7200AE3007A1E ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL RIGHT FAILED A C2XAO OTHER RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW27211291590 850 145703 CAE312406 THE CREW REPORTED THAT ON DESCENT INTO IAH THE NUMBER TWO ENGINE FAILED (UNCOMMANDED SHUT DOWN). THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRT TE6CH 20040617001642004061700164SO 2004 6 17 C2XA04SH329 120040529A532014521721009 BUTTSTRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED ON THE LEFT HAND SIDE AT FRAME 14. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01121. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001652004061700165SO 2004 6 17 C2XA04SH337 120040531A541114576603013 RIB EMB 145 EMB145LR 3260212SO LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE LEFT HAND LOWER COWLING RIB AT STATION NX-2180.0 WAS FOUND TO HAVE A HOLE CHAFED IN IT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 54-10-07 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001692004061700169SO 2004 6 17 MASA200400218 120040422A1420 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07837MJ 145367 DCA - BTV, AT DEPARTURE TIME FLT ATT REPORTED THE OVERHEAD EMERGENCY LIGHT AT ROW 12 WAS INOP. MX FOUND LOOSE CONNECTOR. MX RESECURED CONNECTOR, OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040617001702004061700170SO 2004 6 17 MASA200400254 120040510A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07848MJ 145530 AIRCRAFT WAS ON RON AND SCHEDULED FOR A ROUTINE CHECK. DURING THE WALK-AROUND IT WAS DISCOVERED THAT THE LT FORWARD EMERGENCY LIGHT WAS INOP. MX REPLACED THE LIGHT BULB AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040617001712004061700171SO 2004 6 17 MASA200400222 120040423A3350375924 SIGN EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07837MJ7784 145367 ROW 12 FORWARD CEILNG EXIT SIGN PANEL INOP. MX REPLACED THE SIGN. 2L72 4T RTT00011AT 20040615001682004061500168EA 2004 6 15 COMA0460312 120040511A3230555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01916CA23706 7014 FLT 5872 GEAR DISAGREE WARNING WHEN SELECTED DOWN. COULD NOT DUPLICATE. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20040615001702004061500170EA 2004 6 15 SWIA200413311 120040510A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA FLT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07928SW3720 3720 7701 INBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT MESSAGES ON GROUND. REMOVED AND REPLACED NR 1 SECU IAW CRJ MM 27-61-05. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040615001722004061500172SO 2004 6 15 SWIA200413313 120040510A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07186SW1861 1861 120034 REAR HALF OF EMERGENCY FLOOR LIGHTING STRIPS ARE NOT WORKING. REMOVED AND REPLACED NR 4 POWER SUPPLY IAW 33-50-00. OPS CHECK GOOD. P/N: D366-04-001, S/N ON: 1204, S/N OFF: 1209. 2L72 4T RTA31SO 20040616000032004061600003NM 2004 6 16 ASAA0480407 120040516A53219936537503 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 144-160, RBL 8-16 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000152004061600015NM 2004 6 16 ASAA0480404 120040516A532199365531 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV-CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, RBL 22-44 HAS CORRODED INSERTS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000172004061600017NM 2004 6 16 ASAA0480403 120040516A532199365521 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 200-256, LBL 15 - RBL 22 HAS TORN FIBERS. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOOR PANEL IAW 53-05. (M) 2L72 4F RT 20040616000192004061600019NM 2004 6 16 ASAA04800420 120040516A5320993053885 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CUSP WEB AT STATION 246, RBL 44.5 IS CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW 53-01. (M) 2L72 4F RT 20040616000202004061600020NM 2004 6 16 ASAA0440119 120040404A53126516300511 BULKHEAD BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 FOUND BULKHEAD STATION 178 HAS WEB DAMAGED WL 219, LBL 18.1, PART NR 65-16300-511. REPAIR DAMAGED WEB IAW ASA EA 5310-02343 PAGE 3 STEP 3. (M) 2L72 4F RTA16WE 20040616000232004061600023NM 2004 6 16 ASAA0480427 120040517A5347593054790 SEAT TRACK DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK - FOUND SEAT TRACK AT STATION 200-237, RBL 22 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW 51-10-4. (M) 2L72 4F RT 20040616000282004061600028WP 2004 6 16 ASAA0480193 120040323A25602919845 LANYARD DOUG DC9 DC983 3022083WP TAIL CONE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - WHILE ACCOMPLISHING TAIL CONE EMERGENCY RELEASE TASK CARD STEPS THE LANYARD BROKE AT CAM. CABLE WAS REPAIRED AND REINSTALLED IN PREPARATION FOR AN EMERGENCY SLIDE DEPLOYMENT TEST PER TASK CARD 28625000, WHICH ENCOMPASSES, AS PART OF THE SEQUENCE, A TAILCONE RELEASE/DROP. (M) 2L72 4F RTA6WE 20040616000432004061600043 2004 6 16 ASAA0480190 420040316A25658370024 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND AFT TAILCONE PASSENGER EXIT EMERGENCY SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. THE LANYARD BROKE DURING TAILCONE DEPLOYMENT AND, AS A RESULT, DID NOT PULL OPEN THE SLIDE COVER, ALLOWING THE SLIDE TO DEPLOY. THE LANYARD WAS REPLACED, AND A SUCCESSFUL SLIDE DEPLOYMENT ACCOMPLISHED. THE SLIDE ASSEMBLY WAS THEN REPLACED AS WELL. (M) 2L72 4F RTA6WE 20040616000452004061600045WP 2004 6 16 0400949758 120040506A5330 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01758NW 47286 DURING L-CHECK FOUND CRACKS IN FUSELAGE LT & RT NOSE SKIN AT BS 69.5. REPAIRED PER EA 97-198147. 2L72 4F A6WE 20040616000492004061600049SO 2004 6 16 MASA200400258 120040511A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07856MJ 145626 THE AIRCRAFT WAS ON RON FOR SCHEDULED ROUTINE. DURING WALK-AROUND IT WAS DISCOVERED THAT THE LT AFT OVERWING EMERGENCY LIGHT INOP. MX REPLACED THE LIGHT BULB, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040616000572004061600057SO 2004 6 16 MASA200400296 120040526A33506636 LIGHT EMB 145 EMB145LR 3260212SO ROW 13-14 INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07842MJ 145457 ON THE RON ON SCHEDULED ROUTINE INSPECTION DURING WALK-AROUND IT WAS DISCOVERED THAT THE ROW 13 & 14 EMERGENCY LIGHT STRIP WAS INOP. MX REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKED GOOD. 2L72 4T RTT00011AT 20040616000672004061600067NM 2004 6 16 2004UALA00491 120040524A5311 FAILSAFE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FRAME CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29558UA 26654 FAILSAFE ANGLE CRACKED AT STA 1300 ABOVE STR 21L AT LWR END OF ANGLE IN RADIUS IN AFT PIT. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616000692004061600069NM 2004 6 16 0400905533 120040521A5320 FLOOR SUPPORT BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01533US 24264 DURING H-CHECK FOUND CORROSION IN FLOOR SUPPORT AT BS 365 RBL 46. REPAIRED PER EA 55-199272. 2L72 4F RTA2NM 20040616000752004061600075NM 2004 6 16 2004UALA00478 120040515A3210 LANDING GEAR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MAINS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29367UA 24536 RETURNED TO DEN, DUE TO GEAR WOULD NOT RETRACT. TARGET FOR SWITCH S106 OF GROUND TO AIR SAFETY SENSOR IS OUT OF LIMIT. ADJUSTED SWITCH AND PERFORMED GEAR SWING. NO HISTORY BEFORE OR AFTER. 2L72 4F4 FRTA16WE E2GL 20040616000762004061600076EU 2004 6 16 2004UALA00479 120040516A3397 WIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29410UA 463 DURING CHECK OF EMERGENCY LIGHTS, PTP PANEL FAULTED MESSAGE EXT LOADS FWD LEFT. FOUND WIRE 3351-5109 BROKEN AT DOOR 1-LEFT HINGE POINT UNDER CANVESS CONDUIT. THIS IS THE WIRE TO POWER DOOR 1-LEFT SLIDE LIGHTS. REPAIRED BROKEN WIRE WITH E-BUTT SPLICE, SYS OPS NORMAL IN ALL MODES. 2L72 4F4 FRTA28NM E40NE 20040616000812004061600081NM 2004 6 16 2004UALA00512 120040530A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29182UA55591 25279 FUSELAGE DAMAGE AT STA 670-700 STR 46L-44R & STA 710-740 STR 42R-45R. MAJOR REPAIRS ACCOMPLISHED. INSTALLED JOINT REPAIRS, STRINGER REPAIRS AND THREE DOUBLER REPAIRS. 2L74 4F4 FRTA20WE E24NE 20040616001002004061600100WP 2004 6 16 UPS04842382 120040504A53203779762U1 FITTING DOUG DC8 DC871F 302199DWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 685 LONGERON 2 RT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040616001032004061600103WP 2004 6 16 UPS04842385 120040504A5210561576270 INTERCOSTAL DOUG DC8 DC871F 302199DWP R-1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, R-1 DOOR INTERIOR SIDE LOWER PAN AFT INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5615762 AND SRM 52-2-0 FIG 6. 2L74 4F RT4A25 20040616001072004061600107NM 2004 6 16 2004UALA00525 120040601A3397 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29343UA 24247 EMERGENCY ESCAPE LIGHTING INOP FROM ROWS 15-21. REPLACED FEEDER CABLE ROWS 14-21. 2L72 4F4 FRTA16WE E2GL 20040616001102004061600110NM 2004 6 16 2004UALA00528 120040602A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE MISINSTALLED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29399UA 24674 BOTTOM BELLY SKIN HAS INSUFFICIENT ED ON THE LT SKIN LAP FASTENER HOLES FROM STA 727-907. REPLACED LOWER BELLY SKIN. 2L72 4F4 FRTA16WE E2GL 20040616001252004061600125 2004 6 16 2004UALA00500 420040524A3442 SCANNER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE WX RADAR SYS INOPERATIVE A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29658UA 27113 FLIGHT DIVERTED DUE TO LOSS OF WEATHER RADAR. THE WEATHER RADAR SCANNER UNIT WAS DEFECTIVE . SCANNER WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20040616001402004061600140NM 2004 6 16 C1HA200492013 120040520A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE DAMAGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 STA 1110 BL 0 FLOORBEAM UPPER TEE. REPAIR STRAPS INSTALLED. 2L73 4F A3WE 20040616001422004061600142NM 2004 6 16 C1HA200492010 120040519A5330 SKIN BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 STA 1055 STR 28L SKIN CORROSION. INSTALLED DOUBLER. 2L73 4F A3WE 20040616001572004061600157NM 2004 6 16 2004UALA00456 120040510A5320 FLOOR SUPPORT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO BAY CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA45067 26876 AFT PIT STA 1920 T-CAP CORRODED FROM RBL 58 TO LBL 58. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW T-CAP SECTION. 2L74 4F4 FRTA20WE E24NE 20040616001742004061600174NM 2004 6 16 UPS04542421 120040525A2420729825H FILTER BOEING757 75724APF 1384969NM IDG CONTAMINATED A IPXAB EMER. DESCENT H ELECT. POWER LOSS-50 PC DEDESCENT 1 SO01420UP 23907 DESCENDING THROUGH 250, LT GEN OFF LIGHT CAME ON. THEN LT & RT BUSS OFF LIGHTS ILLUMINATED WITH SUBSEQUENT LOSS OF ALL INSTRUMENTS. FOUND CONTAMINATION IN BOTH IDG FILTERS. REPLACED BOTH LEFT AND RIGHT IDG AND OPS CHECKED NORMAL. P/N OFF 729825E, S/N OFF C0607, P/N OFF 729825H, S/N OFF C0918. 2L72 4F RTA2NM 20040616001812004061600181SO 2004 6 16 MASA200400217 120040421A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07847MJ 145517 AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH NR 2 ENGINE THRUST REVERSER DISAGREE MSG. MX PLACED THRUST REV ON MEL. MX REPLACED THE LOWER DOOR OUTBOARD STOW/TRANSIT SWITCH, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040616001852004061600185SO 2004 6 16 MASA200400267 120040517A3260852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO NLG DOOR INOPERATIVE A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07844MJ 145481 CLT - YYZ, DURING TAKEOFF CLIMBOUT THE NLG DOORS WOULD NOT CLOSE DURING RETRACTION. THE A/C RETURNED TO THE FIELD, RECEIVED A VISUAL CONFORMATION FROM THE CONTROL TOWER THAT THE DOORS WERE IN FACT OPEN AND LANDED WITH OUT INCIDENT. MX REPLACED THE SELECTOR VALVE AND CONTROL LEVER BUT DID NOT FIX THE PROBLEM. OLD PARTS WERE RE-INSTALLED AND THEN MX FOUND THE UPLOCK PROX SENSOR HAD A BROKE WIRE. MX REPLACED THE PROX SENSOR AND OPS CHECKD GOOD. 2L72 4T RTT00011AT 20040616001992004061600199NM 2004 6 16 2004UALA00554 120040607A1420 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT MISWIRED A UALAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 WP29557UA 26653 EMERGENCY EXIT LIGHT L775 JUST FORWARD OF DOOR 1L INOP. FOUND CONNECTOR FOR LIGHT L775 WIRED WRONG. REWIRED CONNECTOR D6648 PER WD33-51- 21. LIGHT L775 TESTS GOOD. 2L72 4F4 FRTA2NM E17NE 20040616002172004061600217EA 2004 6 16 MASA200400294 120040525A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775992 7401 CREW REPORTED FWD SECTION OF THE FLOOR EMERGENCY TRACK LIGHTING INOPERATIVE. MX RESEATED A CONNECTOR ON THE CONTACT STRIP AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040616002222004061600222SO 2004 6 16 MASA200400303 120040531A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07827MJ 145217 THE MAIN CABIN EMERGENCY EXIT CELING LIGHT AT ROW 3 WAS INOP. MX RELAMPED AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040616002232004061600223NM 2004 6 16 ASAA0410251 120040503A534765549692 SEAT TRACK BOEING737 737290C 138448VNM FUSELAGE NICKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 DURING C-CHECK, FOUND SEAT TRACK AT STATION 604-610, RBL 45 IS NICKED AND GOUGED. REMOVED DAMAGED SECTION ANGLE AND INSTALLED REPLACEMENT SECTION IAW SRM 53-10-5. (M) 2L72 4F A16WE 20040616002262004061600226NM 2004 6 16 ASAA0410250 120040503A5320654585554 THRESHOLD BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND AFT GALLEY DOOR LOWER SILL THRESHOLD IS CORRODED. REMOVED DAMAGED SUPPORT ANGLE AND INSTALLED NEW IAW SRM 51-30-2. (M) 2L72 4F A16WE 20040616002282004061600228WP 2004 6 16 ASAA0480312 120040421A532199365471 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND CABIN FLOORBOARD AT STATION 180-200, RBL 8 - RBL 44 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040616002292004061600229WP 2004 6 16 ASAA0480311 120040421A532199365461 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD AT STATION 160-280, LBL 8 - RBL 8 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040616002302004061600230WP 2004 6 16 ASAA0480310 120040421A532199365441 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 160-200, LBL 44-54 IS PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040617000092004061700009NM 2004 6 17 SWAA041694 120040615A53106558280 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, STR 14L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040617000102004061700010NM 2004 6 17 SWAA041695 120040615A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040617000182004061700018NM 2004 6 17 SWAA041690 120040615A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 917 AND BS 924, STR 23R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040617000222004061700022SO 2004 6 17 C2XA04SH319 120040525A541114576631621 STIFFENER EMB 145 EMB145LR 3260212SO NR 1 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE NR 1 ENGINE LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000292004061700029SO 2004 6 17 C2XA04SH344 120040606A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715572 145636 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000332004061700033SO 2004 6 17 C2XA04SH355 120040610A532014522459001 ANGLE EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK, THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000412004061700041SO 2004 6 17 C2XA04IA067 120040611A2120 ODOR EMB 145 EMB145 3260210SO COCKCPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2716961 145103 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000532004061700053WP 2004 6 17 WRLA200422 120040511A324160007446 CONTROL UNIT DOUG DC10 DC1030 3023501WP ANTI SKID SYS FAILED A WRLAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 SO1114075 46922 AIRCRAFT N14075 FLIGHT 8012 FROM LIRN TO KNGU, DURING THE LANDING AT THE KNGU THE RIGHT OUTBOARD ANTI-SKID FAIL LIGHT ILLUMINATED IN FLIGHT. DUE TO THE SHORT RUNWAY AT KNGU THE CREW DECIDED TO LAND AT KNTU. AT THE KNTU MAINTENANCE REMOVED & REPLACED THE ANTI-SKID CONTROL UNIT, OP'S CHECKED NORMAL. 2L73 4F A22WE 20040617000602004061700060NM 2004 6 17 AWXA200400572 120040515A5320D5348004320500 SILL AIRBUSA319 A319132 3930340NM R-2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 DURING B-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT PROFILE SILL FORWARD OF THE R-2 DOOR AT FR 66. MAINTENANCE CUT OUT CORRODED SECTION OF PROFILE SILL AT FR 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 SRM 53-41-14 FIG 201. 2L72 4F RTA28NM 20040617000792004061700079NM 2004 6 17 SWAA041677 120040614A531165C25228 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040617000812004061700081NM 2004 6 17 SWAA041679 120040614A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT RT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040617000822004061700082SO 2004 6 17 C2XA04SH298 120040519A532014524131009 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713566 145622 DURING C-CHECK, THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000832004061700083SO 2004 6 17 C2XA04SH302 120040519A532014526436401 SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK, THE SUPPORT PLATE FORWARD OF FRAME 61 AT STRINGER 15L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000902004061700090SO 2004 6 17 C2XA04SH363 120040613A531514530633003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25 WHERE THE CARBON FIBER CROSSMEMBER ATTACHES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000982004061700098SO 2004 6 17 C2XA04IA056 120040529A33507287114507 CONTROL PANEL EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2723139 145731 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT'S LIGHTING CONTROL PANEL, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4F RT 20040617001002004061700100SO 2004 6 17 C2XA04SH359 120040611A531014525480003 BEAM EMB 145 EMB145 3260210SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001022004061700102SO 2004 6 17 C2XA04SH348 120040609A531014521721009 BUTTSTRAP EMB 145 EMB145 3260210SO FUSLEAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 SHV - DURING C-CHECK THE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001052004061700105SO 2004 6 17 C2XA04SH346 120040609A532014522178005 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714573 145638 DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001062004061700106SO 2004 6 17 C2XA04TY089 120040612A491014526850401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712569 145630 TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER LEFT ENGINE MOUNT. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED A DOUBLER AND INSTALLED IAW EMB-145/135 SRM-53-32-13. 2L72 4T RTT00011AT 20040617001092004061700109SO 2004 6 17 C2XA04SH361 120040612A531014522460013 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 SHV - DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001102004061700110SO 2004 6 17 C2XA04SH362 120040612A532014530375001 PLATE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE SHELL PLATE ON THE CENTER FLOORBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001272004061700127SO 2004 6 17 C2XA04SH290 120040516A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001292004061700129SO 2004 6 17 C2XA04SH366 120040615A491014526850401 FIREWALL EMB 135 EMB135LR 3260305SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001352004061700135SO 2004 6 17 C2XA04SH369 120040615A532014522460015 BUTTSTRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP (AFT DIGITAL) WAS FOUND TO BE CORRODED AT FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001392004061700139SO 2004 6 17 C2XA04SH312 120040522A532014522460015 BUTTSTRAP EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001412004061700141SO 2004 6 17 C2XA04SH314 120040522A531514522461011 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE RIGHT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001422004061700142NM 2004 6 17 C1HA200492003 120040518A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 SEAT TRACK CORROSION. 2L73 4F A3WE 20040617001482004061700148SO 2004 6 17 C2XA04SH316 120040523A531514522461011 GUSSET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001532004061700153SO 2004 6 17 C2XA04SH296 120040518A531014525480003 BEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001552004061700155NM 2004 6 17 SWAA041681 120040614A5312963820 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SPV, FOUND BULKHEAD SIDE FRAME AT LT AND RT BS 178, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER ACO. 2L72 4F RTA16WE 20040617001662004061700166SO 2004 6 17 C2XA04BT064 120040604A3350789241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719966 145131 DURING SERVICE CHECK MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 6 EMERGENCY EXIT SIGN LIGHT INVERTER IAW EMB145 AMM 33-50-01. OPS CHECKED SYSTEM GOOD. 2L72 4F RTT00011AT 20040617001682004061700168SO 2004 6 17 MASA200400233 120040429A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12 INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07837MJ 145367 CREW REPORTED EMERGENCY LIGHT SIGN AT ROW 12 O/H DOES NOT ILLUMINATE. MX PERFORMED EMERGENCY LIGHT TEST AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040617001722004061700172SO 2004 6 17 MASA200400279 120040520A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07825MJ 145179 LEFT OVERWING EMERGENCY EXIT INDENTIFER SIGN INOP. RESET LIGHTING SYSTEM AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040617001732004061700173SO 2004 6 17 MASA200400192 120040413A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 3D INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 CLT - ATL, EMERGENCY LIGHT AT ROW 3D WILL NOT ILLUMINATE. MX PERFORMED AN OPERATIONAL CHECK AND THE CHECK WAS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040617001742004061700174SO 2004 6 17 MASA200400221 120040423A3350 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07860MJ 145773 AFTER POWERING THE AIRCRAFT UP, THE FORWARD EMERGENCY LIGHT WOULD NOT EXTINGUISH. MX DISCONNECTED THE BATTERY CHARGER FROM THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK. THE CONNECTIONS WERE INSPECTED, CLEANED AND RECONNECTED. THE LIGHTS WORKED NORMALLY UPON RE-POWERING. NO PARTS USED. 2L72 4T RTT00011AT 20040617001762004061700176NM 2004 6 17 2004UALA00442 120040505A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29551UA 25399 LEFT FUSELAGE SKIN IS DAMAGED AT BS 760 TO BS 780, BETWEEN STR 15L AND 16L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. EXISTING DOUBLERS REMOVED AND AREA, NDT INSPECTED. NO DEFECTS NOTED. PERMANENT DOUBLER REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040617001772004061700177NM 2004 6 17 2004UALA00444 120040506A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29516UA 24860 EXTERNAL FUSELAGE SKIN DENTED IN TWO AREAS FWD OF NR 2 LT MED AT STA 610-620 STR 15LT. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. INSTALLED FILLER AND DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040617001792004061700179NM 2004 6 17 0400806637 120040515A3350 BATTERY BOEING747 747251B 1384892NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01637US 23548 DURING LINE CHECK, FOUND ZONE-A FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040617001802004061700180WP 2004 6 17 0400789874 120040515A27805919526508 DUCT DOUG DC9 DC951 3022051WP RT WING SLAT DAMAGED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01783NC 48108 DURING SLAT EXTENSION ON APPROACH, THE AIRCRAFT ROLLED RIGHT WITH THE SLAT DISAGREEMENT LIGHT ILLUMINATED. INITIATED COM PROCEDURES WHEN CREW HEARD A THUD AND THE LIGHT EXTINGUISHED. LANDING AT MSP WAS NORMAL. MAINTENANCE REPLACED THE T-DUCT, O-RINGS, SLIDERS, AND PACKINGS ON SLAT SIDE BUSHING ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20040617001812004061700181NM 2004 6 17 0400796306 120040515A1420 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK, FOUND ZONE-D LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RESEATED CONNECTOR. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040617001842004061700184SO 2004 6 17 MASA200400225 120040424A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGNECY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07843MJ 145478 THE AIRCRAFT WAS ON RON LAST NIGHT AND SCHEDULED FOR A ROUTINE. DURING THE WALK-AROUND DISCOVERED THE LT OVERWING EMERGENCY LIGHT INOP. REPLACED THE BULB, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040617001872004061700187NM 2004 6 17 2004UALA00463 120040510A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 AFT PIT LT SIDE STA 1420 BETWEEN STRS 23L AND 26L HAS 2 EACH DENTED AREA ON FRAME. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. REMOVED DAMAGED AREA AND FABRICATED FRAME REPAIR ANGLE AND INSTALLED IAW SRM. 2L72 4F4 FRTA2NM E17NE 20040617001912004061700191NM 2004 6 17 2004UALA00468 120040512A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 AFT PIT LEFT SIDE STA 1400 FRAME BETWEEN STRS 23L AND 26L HAS 2 EACH DENTS ON FRAME. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. CUT OUT DAMAGED AREA AND FABRICATED ANGLE REPAIR AND INSTALLED IAW SRM. 2L72 4F4 FRTA2NM E17NE 20040617001942004061700194NM 2004 6 17 2004UALA00471 120040512A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 STA 380 FRAME HAS CORROSION FROM STR 28L TO 28R. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040617001952004061700195NM 2004 6 17 2004UALA00473 120040513A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CROWN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 FUSELAGE CROWN SKIN AT BS 1240 AND STRINGER 3L HAS DAMAGE TO STRINGER RADIUS DUE TO LIGHTNING STRIKE. *S/D* MAJOR REPAIR ACCOMLISHED. REPAIRED STRINGER 3L WITH REPAIR ANGLE & FILLERS AND FUSELAGE SKIN WITH EXTERNAL DOUBLER. 2L72 4F4 FRTA2NM E17NE 20040617001962004061700196EA 2004 6 17 SWIA200413349 120040524A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07948SW 7789 AILERON TRIM INOP. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040617001982004061700198NM 2004 6 17 2004UALA00449 120040507A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 CABIN BELOW FLOOR LEVEL, BS 616R I/B FRAME CHORD CRACKED AT OVERWING EXIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE. 2L72 4F4 FRTA16WE E2GL 20040617001992004061700199EA 2004 6 17 SWIA200413351 120040525A2751 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07409SW 7056 RIGHT FLAP INDICATIONS FLUCTUATES BETWEEN 18 DEGREES TO 20 DEGREES WHEN FLAPS ARE SELECTED TO 20 DEGREES. REPLACED RIGHT FLAP POSITION TRANSMITTER PER AMM 29-55-01. OPS CHECK NORMAL. 2L72 4F RTA21EA 20040617002002004061700200NM 2004 6 17 CALA0400537 120040615A5320BAC1496444 ANGLE BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713248 28808 CORRODED ANGLE FROM LEFT 500 TO 500I AND HAS A HOLE IN LEFT FORWARD CARGO. INSTALLED FARBRICATED ZEE CHANNEL PER SRM 51-40-02 AND 53-00-53. 2L72 4F RTA16WE 20040617002012004061700201WP 2004 6 17 DHL2004803553 120040515A5720 SPLICE DOUG DC8 DC873 302199CWP LT WING SPAR CAPCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING LWR REAR SPAR CAP SPLICE TEE 1.000 CRACK, STA XRS 74.869 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, EA 5710-13, DWG 5640364. REMOVED CRACKED SPLICE TEE IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1. FABRICATED NEW SPLICE TEE, EXTRUSION 7075-T6511(S4911204-1200) IAW EA 5710-13, DWG 5640364. PERFORMED NDT INSP IAW NDT SPM PART 08.00.02.07. CLEANED, TREATED AND PRIMED AREA AND SPLICE TEE IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE TEE IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-3-1. 2L74 4F RT4A25 20040617002022004061700202WP 2004 6 17 DHL2004803551 120040519A57204647424 CLIP DOUG DC8 DC873 302199CWP NR 2 FUEL TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 2 MAIN TANK CLIP CRACK 2.000, STA XRS 22.750 S-1. REMOVED CRACKED CLIP IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW CLIP (7075-T651) IAW EA 5740-018, DWG 4647424. HEAT TREATED IAW DC8 SRM 51-1-1 PG 13-17. PERFORMED NDT INSP IAW NDT SPM PART 08-00.02.07. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW CLIP AFTER COMPLYING WITH MSI57100020-001-D IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040617002032004061700203WP 2004 6 17 DHL2004803550 120040515A571147708052 FITTING DOUG DC8 DC873 302199CWP SPAR CAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LOWER AUX SPAR CAP, FITTING CRACKED 2.000 P/N 4778052-1 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, EA 5320-014, DWG 4778052. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1. FABRICATED NEW FITTING (7075-T6 51) IAW EA 5320-014, DWG 4778052. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02-07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1, SRM 51-3-1. 2L74 4F RT4A25 20040617002052004061700205EU 2004 6 17 YENA200430 120040514A5210FE240004 CYLINDER AIRBUS320 A320232 3930326EU R1 DOOR LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15566JB3658 2042 R1 DOOR DAMPER CYLINDER READS 0 PSI. REMOVED AND REPLACED DOOR DAMPER CYLINDER IAW AMM 52-11-00-000-001 / 52-11-00-400-001. 2L72 4F RTA28NM 20040618000032004061800003WP 2004 6 18 ASAA0480220 120040402A53209930338 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND CORROSION ON CUSP WEB STRINGER 18 STATION 598-636 LEFT SIDE. REMOVED DAMAGED WEB, ORDERED AND INSTALLED NEW WEB IAW MD80 SRM 51-30-2. (M) 2L72 4F RTA6WE 20040618000042004061800004WP 2004 6 18 ASAA0480219 120040402A530099366521 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION LEFT 1155 TO 1250 DELAMINATED AND NUMEROUS INSERTS CORRODED, AND BROKEN WITH ELONGATED HOLES. FABRICATED REPLACEMENT FLOOR PANELS IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000062004061800006NM 2004 6 18 ASAA0480377 120040510A532199365481 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT FS 200-256 STIFFENERS ARE DISBONDED. REPAIR IAW MM. (M) 2L72 4F RT 20040618000072004061800007NM 2004 6 18 ASAA0480376 120040510A532199579212 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT FS 826-927 TRIM SEPARATED. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000082004061800008WP 2004 6 18 ASAA0480214 120040402A532199365451 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND CORROSION ON SEVERAL INSERTS ON FORWARD CABIN FLOOR PANEL NR 2. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000092004061800009WP 2004 6 18 ASAA0480213 120040402A53305936434127 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND FUSELAGE SKIN CORRODED STATION 540-579 AND STATION 598 LONGERON 30 TO 28L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SKIN, DOUBLERS, STRAPS, AND INNER DOUBLERS IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040618000102004061800010WP 2004 6 18 ASAA0480212 120040402A53219936537 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND DELAMINATION OF UPPER AND LOWER SURFACE OF CABIN FLOOR PANEL NR 6. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000132004061800013WP 2004 6 18 ASAA0480206 120040402A53219936539503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HV CHECK, PAX CABIN FLOOR PANEL IS DELAMINATED AT APPROX FS 150. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040618000142004061800014NM 2004 6 18 ASAA0480379 120040510A5320993053811 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CUSP WEB BETWEEN FUSELAGE AT STATION 503 AND 522 IS CORRODED LEFT. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000192004061800019WP 2004 6 18 ASAA0480227 120040402A532199579182 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HAT SECTION BENT AND CRACKED AT END OF RIGHT FLOOR PLANK STATION 465 TO 546. STOP DRILLED CRACKS FABRICATED AND INSTALLED DOUBLERS IAW MD80 SRM 53-01. (M) 2L72 4F RTA6WE 20040618000202004061800020WP 2004 6 18 ASAA0480228 120040402A53119958238515 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND FRAME CORRODED IN AFT PIT STATION 1322 FROM LONGERON 29L-29R. REMOVED DAMAGE, TRIMMED AND INSTALLED REPAIR ANGLES, SPLICE PLATE, AND FRAME SEGMENT IAW MD80 SRM 53-03. (M) 2L72 4F RTA6WE 20040618000222004061800022WP 2004 6 18 ASAA0480226 120040402A532059560409 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND AFT PIT INTERCOSTAL CORRODED AND CRACKED 1 INCH AT STATION 1007 LONGERON 30. STOP DRILLED CRACK, REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW MD80 SRM 51-70-5. (M) 2L72 4F RTA6WE 20040618000232004061800023WP 2004 6 18 ASAA0480225 120040402A5320993051257 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND CUSP WEB AT STATION 1231 LBL 44 CRACKED. REMVOED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-01. (M) 2L72 4F RTA6WE 20040618000242004061800024WP 2004 6 18 ASAA0480208 120040402A53135936053501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FOUND LONGERON 29 CORRODED IN SEVERAL SPOTS AT STATION 598-731. REMOVED CORRSION AND INSTALLED REPAIR STRAP PER EA 5310-02326. (M) 2L72 4F RTA6WE 20040618000262004061800026WP 2004 6 18 ASAA0480222 120040402A532199366541 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND APASSENGER COMPARTMENT, FLOOR PANEL AT STATION LEFT 1079 TO 1154 HAS THREE INSERTS WITH ELONGATED HOLES. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000272004061800027WP 2004 6 18 ASAA0480216 120040402A532199328162 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND PASSENGER COMPARTMENT FLOOR PANEL AT STATION 1117-1174 RIGHT DELAMINATED AND INSERTS CORRODED. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000282004061800028WP 2004 6 18 ASAA0480210 120040402A5730ARB0975520 PANEL DOUG DC9 DC983 3022083WP RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HV CHECK, RIGHT WING LOWER FUEL PANEL 1460C IS CORRODED. REPLACED PANEL NR 1460C PER MM 28-40-02 AND SRM 51-30-5. (M) 2L72 4F RTA6WE 20040618000302004061800030WP 2004 6 18 ASAA0480267 120040404A575359304953 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FOUND LEFT OUTBOARD FORE FLAP UPPER SKIN IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040618000352004061800035WP 2004 6 18 ASAA0480262 120040404A575359304964 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND DURING HV CHECK, LEFT OUTBOARD FORE FLAP, INBOARD END IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040618000372004061800037WP 2004 6 18 ASAA0480261 120040404A575359304964 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND DURING HV CHECK, LEFT OUTBOARD FORE FLAP, LOWER TRAIL EDGE SURFACE IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040618000382004061800038WP 2004 6 18 ASAA0480260 120040404A531359360281 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FOUND LONGERON 30 AT STATIN 1193-1212 IS CORRODED. REPAIRED PER EA 5310-02339. (M) 2L72 4F RTA6WE 20040618000412004061800041WP 2004 6 18 ASAA0480248 120040404A53305936010 SKIN DOUG DC9 DC983 3022083WP FS GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND TWO EACH GOUGED IN RIGHT TAIL EXTERIOR SKIN AFT OF CANTED FRAME 1485 STRINGER 14R AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND SKIN PLUGS IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040618000432004061800043WP 2004 6 18 ASAA0480218 120040402A5320993053885 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND FORWARD CABIN RIGHT STATION 256-275 CUSP WEB HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M) 2L72 4F RTA6WE 20040618000482004061800048WP 2004 6 18 ASAA0480358 120040423A5320993053885 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN RIGHT CUSP WEB STATION 256 RBL 44 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-10-4. (M) 2L72 4F RTA6WE 20040618000502004061800050NM 2004 6 18 ASAA0480391 120040510A531099364545 SHEAR TIE DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND AFT CARGO COMPARTMENT STATION 1060 BETWEEN LONGERON 29R AND 30 CORROSION ON SHEAR TIE. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000512004061800051NM 2004 6 18 ASAA0480385 120040510A53219936550 FLOOR PANEL DOUG MD80 MD83 3023681NM FS CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL STATION 200-256 AND LBL 15-22 CRACKED. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000522004061800052NM 2004 6 18 ASAA0480386 120040510A53219936547 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 160-180 AND RBL 8-44 DAMAGED. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000532004061800053WP 2004 6 18 ASAA0480360 120040423A533059366673 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FUSELAGE SKIN DENTED FROM INSIDE OUT AT STATION 1241 AT LONGERON 30. COLD WORKED DENT, COMPLIED WITH HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040618000542004061800054NM 2004 6 18 ASAA0480390 120040510A531059128525 DOOR FRAME DOUG MD80 MD83 3023681NM NLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND LEFT NOSE GEAR DOOR JAMB FRAME CRACKED AT FS 69. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000562004061800056NM 2004 6 18 ASAA0480389 120040510A531059128526 DOOR FRAME DOUG MD80 MD83 3023681NM NLG CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND RIGHT NOSE GEAR DOOR JAMB FRAME CRACKED AT STATION 69. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000572004061800057NM 2004 6 18 ASAA0480388 120040510A532199365831 FLOORBOARD DOUG MD80 MD83 3023681NM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND OVERWING AREA FLOORBOARD HAS A HOLE AT STATION 826. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000592004061800059NM 2004 6 18 ASAA0480384 120040510A533059114103 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND DENT IN FUSELAGE SKIN AT SIDE STATION 239 BETWEEN 18L AND 19L. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000622004061800062NM 2004 6 18 ASAA0480381 120040510A5330991183955 SKIN DOUG MD80 MD83 3023681NM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND EMP SKIN PUNCTURED BETWEEN 1474-1485. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000632004061800063WP 2004 6 18 ASAA0480343 120040421A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND AFT PIT SKIN BETWEEN STATION 1149 AND 1155, LONGERON 29L IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER EA 5330-01774. (M) 2L72 4F RTA6WE 20040618000642004061800064WP 2004 6 18 ASAA0480357 120040423A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 22-44 FIBERGLASS TORN. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000662004061800066SO 2004 6 18 CHQA000504 120040613A3350 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11263 145199 FWD PROX STRIP LIGHT AND SERVICE DOOR EXIT SIGN FOUND INOP. REMOVED AND REPLACED NR 2 INVERTER IAW EMB 145 AMM 33-50-11 AND REPLACED FWD STRIP LIGHT IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040618000682004061800068SO 2004 6 18 LR7A04056 120040512A5310 BEAM LKHEED382 382G 526414USO MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 670 4698 DURING SCHEDULED B1 INSPECTION PER JOB CARD HB3200 FOUND RT MLG WHEEL WELL FS 577 MLG BEAM CRACKED AT RBL 66, WL 199. REPAIRED IAW SRM SMP 583 53-40-19. 2H74 4T A1SO 20040618000692004061800069EA 2004 6 18 QXEA200400328 120040517A2720530113 RUDDER PEDAL CNDAIRCL600 CL6002C10 1390015EA ZONE 700 OUT OF RIG A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09607QX6572 10024 PDX - DURING GEAR RETRACTION, GOT GEAR DISAGREE MASTER WARNING. BY THE TIME CHECKLIST WAS RETRIEVED, MESSAGE WENT AWAY AND GEAR RETRACTION WAS NORMAL. RIGGED RUDDER PEDAL RVDT. C/W OPERATIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYSTEM. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040618000702004061800070WP 2004 6 18 2039 120040522A53305801531 SKIN PANEL DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED I U2RBK NONE O OTHER ININSP/MAINT 1 GL23921R 67711692 46145 DURING REPETITIVE INSPECTION OF A/D 2000-20-08 ON LEFT FRONT PAX ENTRANCE DOOR LOWER FORWARD CORNER, VISUALLY DETECTED FUSELAGE SKIN CRACK EXTENDING OUTWARD FROM DOOR RADIUS 1.5 INCH. 2L74 4F 4A25 20040618000712004061800071WP 2004 6 18 DHL2004803521 120040329A5347S2772660 SEAT TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT NR 1 SEAT TRACK LUGS WORN, STA 1120.000. CUT OUT NR 1 SEAT TRACK DAMAGED SEGMENT IAW DC8 SRM 53-2-3 PG 49-50 FIG 14. FABRICATED (3EA) SPLICES (7075-T6 0.100/ 0.125/ 0.160) IAW DC8 SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW DC8 SRM 53-2-3 PG 49-50 FIG 14, DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040618000742004061800074WP 2004 6 18 DHL2004803522 120040329A5347S2772660 SEAT TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT NR 2 FLOOR TRACK LUGS WORN (STA 1680.000-1701.000). REMOVED DAMAGED NR 2 FLOOR TRACK SEGMENT (STA 1680.000-1701.000) IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040618000762004061800076WP 2004 6 18 DHL2004803523 120040331A5753 FRAME DOUG DC8 DC873 302199CWP LT WING TE FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LEFT INBOARD FLAP LOWER FRAME 1.000 CRACK AT STA XW 127.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (7075-T6 0.040) IAW DC8 SRM 57-2-0 PG 2E-2F. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040618000782004061800078WP 2004 6 18 DHL2004803520 120040402A5720 CLIP DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING CTR L/E UPPER INTERNAL PART FORMER DOUBLER CLIP CRACKED 0.500 XFS 427.000. REMOVED CRACKED CLIP IAW SRM 51-1-21 PG 1. FABRICATED NEW CLIP (ALCLAD 2024-T3 0.063) IAW SRM 57-2-0 PG 1, 2. CLEANED, TREATED AND PRIMED AREA AND NEW CLIP IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040616001212004061600121NM 2004 6 16 2004UALA00496 120040524A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 LEFT EXTERNAL FUSELAGE AFT OF L2 DOOR IS DAMAGED. REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER. 2L72 4F4 FRTA16WE E2GL 20040616001242004061600124NM 2004 6 16 2004UALA00499 120040524A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29906UA 25006 LEFT FUSE SKIN AND SIDE FRAME DENTED AT BS 178 WL 195. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER. 2L72 4F4 FRTA16WE E2GL 20040616001452004061600145NM 2004 6 16 2004UALA00511 120040528A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN SHORTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29348UA 24252 EMERGENCY EQUIPMENT LIGHT (EEL) IS SHORTING OUT AT THE AFT SECTION OF THE EEL SYSTEM. REPLACE LIGHT ASSEMBLY. 2L72 4F4 FRTA16WE E2GL 20040616001662004061600166NM 2004 6 16 2004UALA00561 120040608A5321 FLOOR PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 FLOOR WEB APPROX 1 INCH AFT OF BS 199.9 AND HALF INCH INBOARD FROM FUSELAGE SKIN ON RIGHT SIDE CRACKS EMANATING FROM FASTENER BUCK TAIL. FABRICATED & INSTALLED WEB REPAIR. 2L72 4F4 FRTA2NM E17NE 20040616001702004061600170NM 2004 6 16 2004UALA00565 120040609A5320 ANGLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE INTERCOSTAL CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29391UA 24666 ANGLE ON AFT OF INTERCOSTAL STA 294 STR 23L CRACKED. FABRICATED AND INSTALLED ANGLE. 2L72 4F4 FRTA16WE E2GL 20040616001752004061600175SO 2004 6 16 MASA200400168 120040328A2612 FIRE DETECTOR EMB 145 EMB145LR 3260212SO NR 2 ENGINE MALFUNCTIONED A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07841MJ 145448 CREW RETURNED TO FIELD REPORTING NR 2 ENG SHOWED FIRE INDICATION ON EICAS. MX PERFORMED THE REQUIRED FIRE WARNING INSPECTION AND CHECKS COUPLED WITH THE FIRE SYSTEM TEST AND ENGINE RUNS. NO DEFECTS NOTED. NO PARTS USED. 2L72 4T RTT00011AT 20040616001762004061600176SO 2004 6 16 MASA200400176 120040401A4930 FUEL SYS EMB 145 EMB145LR 3260212SO APU LEAKING A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07834MJ 145340 STRONG ODOR OF FUEL VAPORS IN CABIN WHEN APU BLEEDS TURNED ON. ODOR STARTED TO DISSIPATE WHEN BLEEDS SWITCHED OFF BUT TAXI WAS TOO SHORT TO FULLY DISSIPATE WITH PACKS RUNNING OFF ENG BLEEDS. APU INTERNAL LEAK. MX DEFERRED THE APU 4/3/2004. MX RAN APU, NO DEFECTS NOTED. NO PARTS USED. 2L72 4T RTT00011AT 20040616001822004061600182SO 2004 6 16 MASA200400223 120040423A521014533969401 CRANK ASSY EMB 145 EMB145LR 3260212SO PAX DOOR INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 CREW REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. MX LUBED AND OPS CHECKED GOOD. MX REPLACED CRANK ROD ASSY, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040616001862004061600186NM 2004 6 16 0400756624 120040512A3397 CONNECTOR BOEING747 747251B 1384892NM EMERGENCY LIGHT LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01624US 21706 DURING LINE CHECK, FOUND ZONE E-FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RESEATED EMERGENCY LIGHT POWER SUPPLY CONNECTOR. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040616001932004061600193EU 2004 6 16 2004UALA00547 120040604A5521 RIB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT ELEVATOR LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29433UA 589 LEFT ELEVATOR RIB 10 WAS DAMAGED BY LIGHTNING. REPLACED RIB AND INSTALLED BLIND FASTENERS. 2L72 4F4 FRTA28NM E40NE 20040616002142004061600214WP 2004 6 16 0400849996 120040430A5313 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING M-CHECK FOUND CRACKS IN LONGERON 28R BS 756. REPAIRED PER EA 96-198627. 2L72 4F A6WE 20040616002182004061600218NM 2004 6 16 2004UALA00441 120040504A5510 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 FOUND DENT ON RIGHT STABILIZER LEADING EDGE. DENT IS LOCATED ELEVEN BAYS O/B OF STA 86.66 IN CENTER OF BAY. DIMENSIONS ARE 1.00 VERT LENGTH X 0.41 HORIZONTAL WIDTH X 0.047 DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL DOUBLER AND FLUSH FILLER. 2L72 4F4 FRTA16WE E2GL 20040616002202004061600220SO 2004 6 16 MASA200400227 120040427A3350 CONTROL PANEL EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07844MJ 145481 MID-CABIN CEILING EMERGENCY EXIT LIGHT PANEL INOPERATIVE. RESECURED LIGHT PANEL, OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040617000052004061700005SO 2004 6 17 C2XA04SH370 120040617A531014525480003 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000132004061700013 2004 6 17 SWAA041685 420040615A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 R2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040617000232004061700023SO 2004 6 17 C2XA04SH343 120040606A532014525840003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715572 145636 SHV - DURING C-CHECK, THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000252004061700025SO 2004 6 17 C2XA04SH335 120040529A532014528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715572 145636 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19L WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000262004061700026SO 2004 6 17 C2XA04SH336 120040529A533012020333053 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715572 145636 SHV - DURING C-CHECK THE EXTERNAL SKIN WAS FOUND TO BE DENTED AT FRAME 81 AND STRINGER 13L. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-01 FIGURE 206. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000492004061700049 2004 6 17 SWAA041669 420040613A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 L1 DOOR EVAC SLIDE FELL OUT. INSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040617000582004061700058NM 2004 6 17 AWXA200400570 120040515A5320D5347112420100 SHEAR PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE AT AFT END OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF Y1292, BETWEEN FR 69 AND FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-72-11 PG 1 & 2. 2L72 4F RTA28NM 20040617000612004061700061NM 2004 6 17 AWXA200400573 120040515A5320D5311282720100 DUMMY RAIL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28804AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 AT FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 9-18. 2L72 4F RTA28NM 20040617000622004061700062WP 2004 6 17 DHL2004803545 120040512A53204612650 FITTING DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 FWD ACCESSORY COMPT END FITTING CRACKED 2.000 AT STA 8.000, L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED END FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED END FITTING (NEW) IAW SRM 51-1-20D PG 9, SRM 51-1-14 PG 1. 2L74 4F RT4A25 20040617000642004061700064WP 2004 6 17 DHL2004803535 120040420A5755 CRANK ASSY DOUG DC8 DC873 302199CWP SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 3 LEFT FLT SPOILER OUTBOARD CRANK AND LINK CRACK. REMOVED AND REPLACED OUTBOARD CRANK, LINK AND 4EA BOLTS TO NR 3 LEFT SPOILER IAW DC8 MM 20-16-0 PG 201-202. 2L74 4F RT4A25 20040617000782004061700078NM 2004 6 17 SWAA041676 120040613A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29354SW 25219 AFT OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED WITH ALL SWITCHES IN NORMAL POSITION. RESEATED OVERHEAD LIGHT PER MM. 2L72 4F RTA16WE 20040617000892004061700089SO 2004 6 17 C2XA04SH357 120040610A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001042004061700104SO 2004 6 17 C2XA04SH322 120040526A716014575001409 INTAKE EMB 145 EMB145LR 3260212SO NR 2 ENGINE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C-CHECK THE NR 2 INTAKE WAS FOUND TO BE GOUGED AT 12 O'CLOCK. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001182004061700118SO 2004 6 17 C2XA04SH364 120040614A531013500469401 CROSSBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 SHV - DURING C-CHECK THE CROSSBEAM AT FRAME 22 FROM THE RIGHT SILL TO THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001202004061700120SO 2004 6 17 C2XA04IA061 120040609A7500P1097 FILTER HAMSTD EMB 145 EMB145XR 3260214SO NR 1 ENGINE DIRTY A C2XAO OTHER MBJOVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SW2714117 200208123 145674 ON DESCENT THE CREW REPORTED A BLEED ONE OVERTEMP AND A BURNING ODOR IN THE COCKPIT ON FINAL DESCENT. THE AIRCRAFT LANDED AT PBI WITHOUT INCIDENT WHERE DELTA MAINTENANCE CLEANED THE FAN AIR VALVE FILTER, OPERATIONALLY CHECKED THE AIRCRAFT WITH SATISFACTORY RESULTS. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040617001212004061700121SO 2004 6 17 C2XA04TY081 120040414A5210 SKIN EMB EMB 135 EMB135LR 3260305SO PAX DOOR DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714516 145323 DURING A SCHEDULED 2C INSPECTION THE PAX DOOR WAS FOUND WITH 3 DENTS IN IT. DENT 1 AND DENT TWO WERE FOUND WITHIN LIMITS. ALODINED PRIMED AND PAINTED IAW EC5210-01103. DENT NR 3 WAS OUT OF LIMITS. MAINTENANCE CUT OUT AFFECTED AREA, FAB A DOUBLER AND FILLER AND INSTALLED IAW EC 5210-01104. ALODINED AND PAINTED AREA AFFECTED IAW 135/145 CPM 51-21-04; 05; 06. PRESSURE CHECKS PERFORMED AND GOOD. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040617001312004061700131SO 2004 6 17 C2XA04IA071 120040514A1420MS27467T23F35P CONNECTOR EMB 145 EMB145LR 3260212SO FUSELAGE BURNED A C2XAO OTHER FBSFLT CONT AFFECTED SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS DEDESCENT 1 SW2714952 145067 THE CREW REPORTED A HEAVY ELECTRICAL ODOR IN THE AFT CABIN AREA WITH PITCH TRIM 2 AND RUDDER 2 INOP MESSAGES, STICK SHAKER 1 AND CABIN INTERPHONE CIRCUIT BREAKERS POPPED ON FINAL APPROACH. THE AIRCRAFT LANDED AT HRL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND CONNECTOR P0838 TO BE BURNED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CONNECTOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001372004061700137SO 2004 6 17 C2XA04SH310 120040522A533014520554001 SKIN EMB 145 EMB145LR 3260212SO FUSLAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C- CHECK THE OUTER SKIN WAS FOUND TO BE DENTED AT FRAME 20 AND JUST BELOW STRINGER 11L. MAINTENANCE BLENDED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001382004061700138SO 2004 6 17 C2XA04SH313 120040522A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001432004061700143NM 2004 6 17 C1HA200492004 120040518A5320 STRAP BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15292AS 21458 REPAIR STRAP CORRODED. 2L73 4F A3WE 20040617001512004061700151SO 2004 6 17 C2XA04BT061 120040515A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714998 145302 DURING 5A INSPECTION MAINTENANCE FOUND THE SERVICE DOOR EMERGENCY LIGHT TO NOT BE WORKING. FOUND BROKEN WIRE, RECONNECTED BUTT SPLICE CONNECTION AND OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20040617001562004061700156NM 2004 6 17 SWAA041682 120040614A53306545775 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 878, STRINGER 25L, BS 827, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM AND EA. 2L72 4F RTA16WE 20040617001602004061700160SO 2004 6 17 C2XA04SH301 120040519A335078812 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE NUMBER 5 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001672004061700167SO 2004 6 17 C2XA04IA070 120040614A33507287100507 PANEL EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT CONTAMINATED A C2XAK NONE L NO TEST NRNOT REPORTED 1 SW2713913 145438 IAH - FLIGHT 2186, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS CAME ON WHEN CALLING THE FLIGHT ATTENDANT. MAINTENANCE CLEANED THE FLIGHT ATTENDANT CALL PANEL OF MOISTURE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001822004061700182EA 2004 6 17 SWIA200413319 120040514A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07590SW 7077 STAB CH 1 STATUS MESSAGE, CANNOT RESET. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR AND MCU IAW MM 27-42-01. OPS CHECKED GOOD. MCU P/N: 7062-3, S/N OFF: 602. 2L72 4F RTA21EA 20040617001832004061700183SO 2004 6 17 MASA200400288 120040524A335066361 LIGHT EMB 145 EMB145LR 3260212SO ROW 8 & 9 BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07825MJ 145179 AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK-AROUND DISCOVERED THAT ROW 8 & 9 EMERGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040617001882004061700188NM 2004 6 17 2004UALA00464 120040509A2751 WARNING LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE TE FLAPS ILLUMINATED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29664UA 29236 RECEIVED EICAS TRAILING EDGE FLAP DISAGREE MESSAGE. OPERATED SYSTEM, UNABLE TO DUPLICATE FAULT. 2L72 4F4 FRTA1NM E24NE 20040617002042004061700204EU 2004 6 17 YENA200429 120040510A2121EVT3454H FAN AIRBUS320 A320232 3930326EU E/E BAY FAILED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15536JB8132 1784 IN CRUISE AT FL 350 A GRINDING NOISE WAS COMING FROM UNDER FORWARD LAV FOLLOWED BY A BURNING ODOR SHORTLY THEREAFTER ECAM VENT EXTRACT FAULT ILLUMINATED. BOTH THE SOUND AND ODOR WENT AWAY. CONTINUED TO OAK NO OTHER PROBLEM NOTED. ITEM WAS CONTINUED UNDER MEL 21-26-02. LATER AT LGB REMOVED AND REPLACED EXTRACT FAN PER 21-26-51. AEVC TEST CHECKS GOOD PER 21-26-51. 2L72 4F RTA28NM 20040618000212004061800021WP 2004 6 18 ASAA0480229 120040402A532059560409 VERTICAL SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND VERTICAL SUPPORT IS DENTED AT FS 1007 BL 0 JUST ABOVE FLOOR LINE IN AFT PIT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW MD80 SRM 51-70-5. (M) 2L72 4F RTA6WE 20040618000292004061800029WP 2004 6 18 ASAA0480268 120040404A575359304954 VANE DOUG DC9 DC983 3022083WP TE FLAP NICKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FOUND LEFT INBOARD FORE FLAP, OUTBOARD LOWER SURFACE LEADING EDGE HAS SEVERAL NICKS AND DINGS. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M0 2L72 4F RTA6WE 20040618000312004061800031WP 2004 6 18 ASAA0480266 120040404A5313993061223 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND DURING HV CHECK, LONGERON 18R CUSP MEMBRANE AT STATION 1136-1155 IS CORRODED. REMOVED AND REPLACED WEB. (M) 2L72 4F RTA6WE 20040618000332004061800033WP 2004 6 18 ASAA0480264 120040404A575359304963 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FOUND LEFT OUTBOARD FORE FLAP, INBOARD LEAD EDGE IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040618000362004061800036WP 2004 6 18 ASAA0480207 120040402A532199365371 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND HV CHECK, PAX CABIN ARROW HEAD FLOOR PANEL IS TORN. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040618000392004061800039WP 2004 6 18 ASAA0480259 120040404A57303070100 ACCESS PANEL DOUG DC9 DC983 3022083WP WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FUEL ACCESS PANEL NR 1410 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040618000422004061800042WP 2004 6 18 ASAA0480247 120040404A5347593056675 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND SEAT TRACK LBL 22 STATION 1168 TO 1220 HAS NUMEROUS GOUGES. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION AND SPLICE IAW MD80 SRM 51-10-4. (M) 2L72 4F RTA6WE 20040618000492004061800049WP 2004 6 18 ASAA0480359 120040423A53219932816504 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD STATION 256-294 RBL 44 HAS CORROSION AND BARE METAL NUMEROUS PLACES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000612004061800061NM 2004 6 18 ASAA0480382 120040510A5310575468827 WINDOW FRAME DOUG MD80 MD83 3023681NM COCKPIT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND CRACK ON CAPTAINS CLEAR VIEW WINDOW CUT OUT AT UPPER AFT CORNER ON INNER SURFACE. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000652004061800065SO 2004 6 18 CHQA000503 120040602A3320 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11263 145199 PROX STRIP LIGHT FOUND BROKEN AND ONE FOUND INOP. REPLACED BOTH STRIPS IAW EMB 145 AMM 33-50-12-4. 2L72 4T RTT00011AT 20040618000722004061800072WP 2004 6 18 DHL2004803531 120040412A5311 FRAME DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 FWD ACCESSORY COMPT FRAME CRACK 1.000, STA 55.000 L-24R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 2. TRIMMED OUT DAMAGED FRAME SEGMENT AND FABRICATED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT (ALCLAD 7075-0 0.071) IAW DC8 SRM 53-2-0 FIG 2. HEAT TREATED IAW DC8 SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED 2EA ANGLE DOUBLER AND NEW FRAME SEGMENT IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040618000802004061800080WP 2004 6 18 DHL2004803517 120040325A5711 FRAME DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT INNER WING CTR L/E FORMER CRACKED 0.250, XFS 427.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP HOLE ON CRACK END AND FABRICATED DOUBLER (2024-T3AL 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20040618000812004061800081WP 2004 6 18 DHL2004803532 120040414A5755 FITTING DOUG DC8 DC873 302199CWP FLT SPOILER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 3 LT FLT SPOILER (1EA) DRIVE FITTING WITH CRACK IN IT. REMOVED AND REPLACED DRIVE FITTING (NR 3 LEFT SPOILER) IAW DC8 MM 20-16-0 PG 201. 2L74 4F RT4A25 20040618000822004061800082NE 2004 6 18 TSAA0436040 220040518A75321074925 BLEED VALVE BOEING737 73776N 13844CHNM GE CFM56 CFM56* 13802NE NR 1 ENG FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13740AL 28640 NR 1 ENGINE BLEED VALVE DOES NOT CLOSE. RETURN TO HNL, NO EMERGENCY DECLARED; REQUESTED PRECAUTIONARY FOR OVERWEIGHT LANDING AND POSSIBLE HOT BRAKES. OVERWEIGHT LANDING (147,000 LBS) WITH MINIMUM SINK RATE. WITH ENGINE NR 1 AT IDLE, VERIFIED NR 1 ENGINE BLEED DOES NOT TURN OFF WITH SWITCH POSITION IN OFF. VERIFIED BLEED AIR REGULATOR INOP, REMOVED AND REPLACED IAW AMM 36-11-03-4. OPS CHECK GOOD. VERIFIED 4 EA BRAKES WARM TO TOUCH. OPS CHECK NORMAL IAW AMM 05-51-35-2. PERFORMED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 05-51-35-2, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20040618000862004061800086NM 2004 6 18 SWAA041700 120040616A335065C34691 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 11 DEF, INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040618000872004061800087 2004 6 18 SWAA041701 420040616A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040618000882004061800088NM 2004 6 18 SWAA041702 120040616A55106551524 CLEVIS BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION CLEVIS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20040618000892004061800089NM 2004 6 18 SWAA041703 120040616A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 44, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040618000902004061800090NM 2004 6 18 SWAA041704 120040616A53156545410 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 664, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040618000932004061800093SO 2004 6 18 CHQA000494 120040516A3320 LIGHT EMB 145 EMB145LR 3260212SO ROWS 1-3 INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 ROW 1, 2, & 3 FLOOR EGRESS (EMER) LIGHT STRIPS ARE INOP. REMOVED AND REPLACED FORWARD FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040618000952004061800095SO 2004 6 18 CHQA000496 120040519A3350 LIGHT EMB 145 EMB145MR 3260213SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11974 145203 RIGHT FORWARD WING EXTERNAL EMERGENCY LIGHT OUT. REMOVED AND REPLACED FORWARD RIGHT EXTERNAL EMERGENCY LIGHT PER ERJ 145 MM 33-50-10. OPERATIONAL CHECK SATISFACTORY PER ERJ 145 MM 33-50-00. 2L72 4T RTT00011AT 20040618000972004061800097SO 2004 6 18 CHQA000497 120040519A3350 LIGHT EMB 145 EMB145MR 3260213SO ROW 12 INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11974 145203 EMERGENCY LIGHT OUT IN PSU ABOVE ESCAPE HATCH AT ROW 12E/F. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT PER ERJ 145 MM 33-50-07. OPERATIONAL CHECK OF EMERGENCY LIGHTS SATISFACTORY PER ERJ MM 33-50-00. 2L72 4T RTT00011AT 20040618000992004061800099CE 2004 6 18 DXTA200400310 120040511A3260674101016 PROXIMITY SENSOR CESSNA750 750 2076810CE MLG STUCK E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07956QS 7500156 DURING GEAR RETRACTION THE RIGHT MAIN STAYED GREEN, DURING RETRACTING GEAR THE RED UNSAFE LIGHT STAYED ON FOR A FEW SECONDS WHILE THE NOSE AND LEFT MAIN RETRACTED NORMALLY. THE RIGHT MAIN STAYED GREEN WITH NO RED LIGHT, CYCLED GEAR WITH SAME RESULTS. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR RETRACTION CHECK, FOUND WHEN GEAR WAS UP AND LOCKED, ALL THREE IN VISUALLY LOCKED. RIGHT MAIN LANDING GEAR STILL HAD GREEN DOWN AND LOCKED INDICATION, TROUBLESHOT SYSTEM AND FOUND THE RT MLG DOWN AND LOCK PROX SWITCH TARGET PIN STUCK UP. CLEANED PIN AND LUBED, CYCLED GEARS SEVERAL TIMES, OPS CHECKED GOOD, ALL WORK DONE IAW CITATION X MM CHAPTER 32. 2L72 4J RTT00007WI 20040618001002004061800100CE 2004 6 18 DXTA200400311 120040511A324021641 BRAKE CESSNA560 560XL 2076702CE MLG FIRE E DXTAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 GL07622QS530 5605286 PERFORMED HIGH SPEED TAXI AFTER BRAKE MAINTENANCE, TAXIED BACK USING NORMAL BRAKING PROCEDURE. UPON RETURN TO RAMP, LEFT WHEEL/BRAKE ASSEMBLY WAS ON FIRE, RIGHT WHEEL/BRAKE ASSEMBLY SMOKING. EXTINGUISHED FIRE WITH PURPLE K, DRY CHEMICAL (B-C) EXTINGUISHER. INSPECTED LEFT AND RIGHT MAIN GEAR, NO OTHER DAMAGE NOTED. REMOVED AND REPLACED BOTH LT AND RT MAIN GEAR WHEELS AND BRAKES, BOTH BRAKES HAD BEEN SENT TO OVERHAUL SHOP TO DETERMINE CAUSE OF SMOKE/FIRE. 2L72 4F RTA22CE 20040618001042004061800104WP 2004 6 18 GTIA040477 120040505A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE COCKPIT CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 COCKPIT FLOOR PANEL CRACKED AND NON SKID MISSING. FABRICATED NEW PANEL. 2L72 4F4 FRTA6WE E2EA 20040618001052004061800105EA 2004 6 18 ASOA04383 120040526A52101170681 LEVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR RELEASE LEVER AND OPEN LOCK MECHANISM. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040618001072004061800107EU 2004 6 18 ASOA04393 120040530A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27632AS 1360 338 DURING AN (A) CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20040618001082004061800108WP 2004 6 18 GTIA040290 120040309A5330 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 AFT CARGO DOOR LATCH CUT OUT HOLE IS DEFORMED AND REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F4 F A6WE E2EA 20040618001102004061800110WP 2004 6 18 GTIA040478 120040428A5712 RIB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RT WING CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT WING L/E COMPARTMENT STA XRS267, L/E SUPPORT RIB IS CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA6WE E2EA 20040618001152004061800115EA 2004 6 18 ASOA04342 120040506A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MLG BATT RIB ASSEMBLIES AT WS 53.60 IAW EO60057039A. 2L72 4F4 FRTA21EA E15NE 20040618001162004061800116EA 2004 6 18 ASOA04350 120040514A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING C-CHECK INSPECTION, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKED FLOOR SUPPORT ANGLES IAW REO 601R5361117. 2L72 4F4 FRTA21EA E15NE 20040618001192004061800119EA 2004 6 18 ASOA04379 120040522A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27838AS 7276 DURING A C-CHECK, THE FORWARD EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK AND THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040618001202004061800120NM 2004 6 18 GTIA040543 120040509A5522 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE RT ELEVATOR DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 RT ELEVATOR LOWER SKIN IS CREASED. CUT OUT DAMAGED AREA OF LOWER SKIN AT RT ELEVATOR (9.5 X 18.5) FABRICATED FINGER DOUBLERS AND SKIN FILLER. INSTALLED REPAIR PARTS. 2L72 4F4 FRT E2EA 20040618001232004061800123WP 2004 6 18 GTIA040484 120040430A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 DENT AND GOUGE AT FS 446 TO FS 457 BETWEEN LONGERONS 25 AND 26R, DENT IS WITHIN THE CRITICAL AND SEMI CRITICAL OF THE RVSM CONTROLLED AREA AND REQUIRES REPAIR. CUT OUT DAMAGED SKIN (10.5 INCH X 33.5 INCH) FABRICATED REPAIR FILLER. REPAIR DOUBLERS (5 EA) AND FINGER DOUBLER. INSTALLED REPAIR. 2L72 4F4 FRTA6WE E2EA 20040618001242004061800124WP 2004 6 18 GTIA040488 120040430A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 AFT PIT STA 1309-1322 LBL 17 CARGO TIE DOWN TRACK INTERCOASTAL CORRODED UNDER NUT PLATES. REMOVED INTERCOASTAL. FABRICATED INTERCOASTAL. INSTALLED INTERCOASTAL. 2L72 4F4 FRTA6WE E2EA 20040621000012004062100001WP 2004 6 21 ASAA0480342 120040420A532059561573 PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 DURING C-CHECK, FOUND AFT WING FILLET PANEL 2208C BETWEEN ATTACH RUB STRIP AND FUSELAGE SKIN IS CORRODED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040621000032004062100003NM 2004 6 21 ASAA0480393 120040513A335060030451 POWER SUPPLY DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01981AS 53472 LAX - FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 31. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040621000052004062100005WP 2004 6 21 ASAA0480246 120040404A143059360481 FASTENER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND RUSTED FASTENERS ON LONGERON 29R STATION 1231-1250. REMOVED DAMAGED LONGERON, ORDERED AND INSTALLED NEW LONGERON IAW MD80 SRM 51-30-5. (M) 2L72 4F RTA6WE 20040621000082004062100008WP 2004 6 21 ASAA0480243 120040404A53133914677U507 SPLICE DOUG DC9 DC983 3022083WP LONGERON CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND LONGERON 29L CORRODED AT SPLICE JOINT STRAP STATION 1212-1193. REMOVED DAMAGED SPLICE, ORDERED AND INSTALLED NEW SPLIC IAW MD80 SRM 51-30-5. (M) 2L72 4F RTA6WE 20040621000092004062100009WP 2004 6 21 ASAA0480242 120040404A53219957918 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND CRACK AND FASTENER PULLED THROUGH TOP SIDE OF RIGHT FLOOR PLANK STATIN 546-626. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-01. (M) 2L72 4F RTA6WE 20040621000102004062100010WP 2004 6 21 ASAA0480241 120040404A53305924802509 SKIN DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND GOUGE AND DENT IN FUSELAGE SKIN STATION 237 AT LONGERON 17L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAPS, DOUBLERS, AND FILLER IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040621000112004062100011WP 2004 6 21 ASAA0480341 120040420A531199122466 FRAME DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 DURING C-CHECK, FOUND LEFT VENTRAL AFT ACCESSORY COMPARTMENT FRAME IS GOUGED AND CHAFED. REPAIRED DAMAGED AREAS PER EA 5310-02342. (M) 2L72 4F RTA6WE 20040621000132004062100013WP 2004 6 21 ASAA0480240 120040404A5320991015175 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND CORROSION ON CUSP WEB STATION 845 TO 864 LEFT FUSELAGE LBL 44 TO LBL 59. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M) 2L72 4F RTA6WE 20040621000142004062100014WP 2004 6 21 ASAA0480256 120040404A57308570030326 PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND LEFT WING PANEL 1361 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL 1361 IAW MD80 SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040621000172004062100017WP 2004 6 21 ASAA0480335 120040419A53219936537501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRUSHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL IS CRUSHED IN SEVERAL LOCATIONS AT FS 140-160. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000182004062100018WP 2004 6 21 ASAA0480336 120040419A532199365461 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS AT FS 160-120. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000192004062100019WP 2004 6 21 ASAA0480338 120040420A532199365511 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - DURING C-CHECK, FOUND PASSENGER CABIN FLOOR PANEL IS CRACKED AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000202004062100020WP 2004 6 21 ASAA0480339 120040420A532199365531 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AT FS 200-256. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000212004062100021WP 2004 6 21 ASAA0480340 120040420A57535930496025 VANE DOUG DC9 DC983 3022083WP TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 FOUND DURING C-CHECK, LEFT OUTBOARD FLAP INBOARD VANE ACCESS PANEL IS CREASED. REPLACED FLAP VANE PANEL PER SRM 51-10-4 AND 51-30-1. (M) 2L72 4F RTA6WE 20040621000242004062100024WP 2004 6 21 ASAA0480400 120040515A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE MISINSTALLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM01974AS 53450 OKC - DURING C-CHECK, FOUND MID CARGO DOOR LOWER BEAM DOUBLER INSTALLED INCORRECTLY. REMOVED DOUBLER, TRIMMED AND INSTALLED NEW DOUBLER IAW ASA TASKCARD 28553001 AND 51-30-5. (M) 2L72 4F RTA6WE 20040621000252004062100025 2004 6 21 ASAA0480237 420040404A2565220123101 GIRT BAR DOUG MD80 MD83 3023681NM L1 DOOR DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 PHX - DURING PREFLIGHT CHECK, FOUND FORWARD PAX L1 DOOR EMERGENCY SLIDE GIRT LANYARD DETACHED. RESECURED LANYARD TO GIRT BAR. (M) 2L72 4F RT 20040621000262004062100026WP 2004 6 21 ASAA0480395 120040513A5610 LINKAGE DOUG DC9 DC983 3022083WP COCKPIT WINDOW OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 ANC - DURING PREFLIGHT CHECK, FOUND LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED SLIDING MECHANISM IN TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040621000272004062100027WP 2004 6 21 ASAA0480159 120040302A532099365831 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01961AS 53075 OKC - DURING FLOOR PANEL AT FS 617 TO 655 X = 22, DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040621000312004062100031WP 2004 6 21 ASAA0480231 120040404A532199365531 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HV CHECK, PASSENGER CABIN FLOOR PANEL AT STATION 200-256 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000322004062100032WP 2004 6 21 ASAA0480232 120040404A532199365481 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HV CHECK, PASSENGER CABIN FLOOR PANEL AT STATION 200-256 IS DISBONDING. REPLACED FLOOR PANEL PER MM 20-20-01. (M) 2L72 4F RTA6WE 20040621000362004062100036WP 2004 6 21 ASAA0480329 120040419A532199365451 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AND HOLES NEAR FORWARD ENTRY AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000372004062100037WP 2004 6 21 ASAA0480330 120040419A532199365451 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS CORRODED INSERTS AND COMPOSIT DAMAGE AT CORNER AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000412004062100041WP 2004 6 21 ASAA0480334 120040419A532199365471 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS SEVERAL CRACKED INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000422004062100042WP 2004 6 21 ASAA0480337 120040419A532199365461 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - DURING C-CHECK, FOUND PASSENGER CABIN FLOOR PANEL HAS BROKEN AND CORRODED INSERTS AT FS 160-120. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000432004062100043WP 2004 6 21 ASAA0480370 120040507A5610 LINKAGE DOUG DC9 DC983 3022083WP COCKPIT WINDOW DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01969AS 53063 ANC - DURING PREFLIGHT CHECK, FOUND LEFT CAPTAINS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. RECONNECTED LINKAGE. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040621000442004062100044WP 2004 6 21 ASAA0480364 120040503A5210 STRUCTURE DOUG DC9 DC982 3022082WP L1 DOOR BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING C-CHECK, FOUND LOWER LEFT EDGE OF L1 DOOR BENT INWARD. REPAIR IAW SRM. (M) 2L72 4F A6WE 20040621000452004062100045WP 2004 6 21 ASAA0480365 120040503A532199365811 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING C-CHECK, FOUND FLOORBOARD IS DELAMINATED AT FS 693-750. REPAIR IAW SRM. (M) 2L72 4F A6WE 20040621000522004062100052 2004 6 21 VNAA0406010 420040614A34187013348937 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT STICK SHAKER FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL05425JS5713 3037 DURING CLIMBOUT, THE CREW RECEIVED A RT STICK SHAKER CAS MESSAGE AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000532004062100053NM 2004 6 21 VNAA0406009 120040614A2611SD9422A0A01 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAV FAILED A VNAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL05440JS193963839 3058 THE CREW RECEIVED A LAV SMOKE CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000552004062100055NM 2004 6 21 VNAA0406001 120040602A3234 HANDLE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG FAILED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05434JS 3051 AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO UP AND THE CREW RETURNED TO CAK. MAINTENANACE INSPECTED AND REPLACED THE GEAR RETRACT CIRCUIT BREAKER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000572004062100057EA 2004 6 21 VNAA0406003 120040602A2751601R930303 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL05202PS1175 7858 DURING FLIGHT, THE CREW RECEIVED A FLAP DEGRADE STATUS MESSAGE AND DIVERTED TO BTV. MAINTENANCE WAS SENT TO BTV. MAINTENANCE THEN INSPECTED AND REPLACED THE LEFT HAND FLAP POSITION TRANSMITTER ASSEMBLY IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040621000592004062100059EA 2004 6 21 VNAA0406006 120040610A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT INTERMITTENT A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL05250PS 7929 DURING FLT, THE CREW RECEIVED A RT EMERGENCY EXIT DOOR CAS MESSAGE, THE PRESSURE WAS NORMAL AND THE INDICATION EXTINGUISHED BY ITSELF ON DESCENT. MAINTENANCE DEFERRED WITH THE CREW USING MEL 52-70-03 CODE-C. 2L72 4F4 FRTA21EA E15NE 20040621000612004062100061 2004 6 21 VNAA0406008 420040613A3418 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AOA OUT OF POSITION A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL05438JS 3056 DURING TAKEOFF, THE ANGLE OF ATTACK VANE WAS OUT OF POSITION AND THE CREW ABORTED TAKEOFF. THE ANGLE OF ATTACK VANE WAS RESET AND FLIGHT 2572 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000622004062100062 2004 6 21 VNAA0406011 420040615A3418 WARNING LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE STICK SHAKER ILLUMINATED A VNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL05426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND STICK SHAKER PUSHER ON SIDE FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE SHAKER PUSHER RESET ITSELF AND FLIGHT 2417 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 2417 THEN DEPARTED WITH NO FURTHER INCIDENTS. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000652004062100065NM 2004 6 21 SWAA041709 120040617A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040621000672004062100067NM 2004 6 21 SWAA041711 120040617A57536546434302 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING T/E INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT WING INBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040621000682004062100068NM 2004 6 21 SWAA041712 120040617A57536546435346 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED PM CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING T/E FLAP PER MM. 2L72 4F RTA16WE 20040621000712004062100071EU 2004 6 21 AWXA200400578 120040527A76973957985205 WIRE AIRBUS320 A320231 3930325EU ZONE 120 CHAFED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28645AW22617 238 ON CLIMBOUT, RECEIVED ECAM INDICATION NR 2 ENG NACELLE TEMP VARIES BETWEEN 315 & 380 DEGREES, INDICATION INTERMITTENT, DIVERTED TO PHX FOR REPAIR. MX TROUBLESHOT WIRING FROM PIN A/10B OF ENGINE INTERFACE UNIT (EIU) TO PIN 1 OF NACELLE TEMP SENSOR, NO FAULTS WERE NOTED, BUT DID FIND NACELLE SENSOR WIRE 8G004 CHAFED/CUT, RE-TERMINATED WIRE AT GP5-4, OHMS CHECK WAS GOOD. REPLACED NR 2 ENGINE NACELLE TEMPERATURE SENSOR (HEAT DETECTOR) IAW AMM 75-41-15, AND EIU IAW AMM 73-25-34. PERFORMED HIGH POWER ASSURANCE RUN, BOTH ENGINE NACELLE TEMPERATURES WITHIN 10 DEGREES OF EACH OTHER. BENCH TEST OF EIU S/N 988 WAS NO FAULT FOUND, UNIT PASSED ALL ACCEPTANCE TESTS PER CMM 73-25-35, REV. 4. 2L72 4F RTA28NM 20040621000722004062100072CE 2004 6 21 0029 120040514A3244178K235 TIRE LEAR 35 35A 5170602CE MLG BULGED E CIEAO OTHER O OTHER NRNOT REPORTED 1 NM03244LJ132 244 DURING PREFLIGHT CHECK OF THE AIRCRAFT THE NR 3, RT INBOARD, TIRE HAD A BULGE IN THE TREAD AREA OF THE TIRE. THE WHEEL AND TIRE WERE REPLACED WITH A SERVICEABLE UNIT. THIS UNIT HAD NOT FAILED AT THIS POINT BUT FAILURE OF THE TIRE COULD RESULT IN DAMAGE TO UNDERSIDE OF WING AND TO THE FLAP AREA. 2L72 4F A10CE 20040621000732004062100073EU 2004 6 21 CX7A194J0424 120040518A33206500006 SOCKET SAAB SF340 340B 7860101EU CABIN LIGHT BURNED OUT A CX7AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL03302CE 340B193 WINDOW LIGHT AT 5A BURNED OUT, PAX NOTICED SPARKE AND SMOKE. 2L72 4T RTA52EU 20040621000752004062100075EA 2004 6 21 COMA0470042 120040514A2150 ACM CNDAIRCL600 CL6002C10 1390015EA ACM BAY SMOKE A COMAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO01625CA 10113 FLIGHT 9484 DURING CVG APPROACH ON FERRY FLIGHT, CREW REPORTED SIGNS OF SMOKE IN CABIN. PERFORMED A VISUAL INSPECTION OF CABIN AND COCKPIT LIGHTING. PERFORMED GROUND RUNS AND TAXI, PRESSURIZED AIRCRAFT. NO DEFECTS OR SIGNS OF SMOKE. 2L72 4F RTA21EA 20040621000762004062100076 2004 6 21 PCAA0405208 420040519A3442071013190010 RADAR DHAV DHC8 DHC8102 2809003NM WX SYSTEM FAILED A PCAAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 EA13981HA5101 23 378 FLIGHT 3966 DEPARTED MIDDLETOWN TO PITTSBURGH AND HAD TO RETURN TO FIELD DUE TO THE WEATHER RADAR BEING REPORTED AS INOP. DUE TO POSSIBLE SEVERE WEATHER IN PITTSBURGH THE FLIGHT ELECTED TO RETURN TO MIDDLETOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RADAR R/T AND OPERATIONAL SYSTEM CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040621000802004062100080EA 2004 6 21 COMA0460325 120040516A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01458CA 7613 FLIGHT 3733 ORANGE EMERGENCY LIGHT NEAR CABIN DOOR IS INOP. SECURED LOOSE WIRE CONNECTION. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040621000812004062100081WP 2004 6 21 IXXA0400064S 120040404A5730 PANEL DOUG DC8 DC873F 302199FWP RT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD L/E SLANT PANEL UPPER SKIN SURFACE CORRODED, STA XCW 69.000 AND XFS 207.000. REPAIR ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, FAX TIN-N 043, BOEING MESSAGE DATE 03/31/2004. REMOVED CORROSION IAW DC8 SRM 51-1-I PG 17-18, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED SLANT PANEL IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. TRIMMED OUT HOLE LOCATIONS ON NEW SLANT PANEL, FABRICATED FILLER, DOUBLER IAW BOEING MESSAGE 03-31-04, CLEANED, TREATED AND PRIMED AREA, FILLER, DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER, DOUBLER ON NEW SLANT PANEL IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1 20D PG 9, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040621000822004062100082EA 2004 6 21 COMA0460322 120040518A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01938CA 7046 FLIGHT 5316 LEFT THRUST REVERSER UNLOCK CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040621000842004062100084EA 2004 6 21 COMA0460321 120040519A323317008111 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO01916CA14286 7014 FLIGHT 5854 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE RT MLG RETRACT ACTUATOR. 2L72 4F RTA21EA 20040621000852004062100085EA 2004 6 21 COMA0460323 120040518A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01784CA 7319 FLIGHT 5229 EMERGENCY FLOOD LIGHT AT CABIN DOOR IS INOP. REPLACED THE NR 2 EMERGENCY BATTERY. 2L72 4F RTA21EA 20040621000872004062100087EA 2004 6 21 COMA0460320 120040515A323061750 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01936CA24106 7043 FLIGHT 5740 GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20040621000882004062100088GL 2004 6 21 CHQA000490 220040517A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 SMOKE A CHQAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL11291SK 145486 CAE311900 FLT 3090 CREW REPORTS, RECEIVED LAV SMOKE WARNING DURING CLIMBOUT OF DCA AND FLT ATTENDANT REPORTED SMOKE IN THE LAV AREA. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FIRE DEPT REPORTS NO VISUAL SIGNS OF SMOKE AND NO SCENT. MX REPORTS, PERFORMED PNEUMATIC RUNS AND HAD NO LAV SMOKE INDICATION, PERFORMED H/P RUNS, NO SIGNS OF OIL CONSUMPTION, PERFORMED VISUAL INSP FOR OIL LEAKS EXTERNALLY. MX REMOVED FLOORBOARDS TO CHECK FOR LEAKS, NO INDICATION. PERFORMED TEST FLIGHT, OPS CHECK GOOD. AFTER FERRYING THE AIRCRAFT TO IND FOR THOROUGH INVESTIGATION, THE CAUSE WAS ISOLATED TO NR 1 ENGINE AND WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040621000892004062100089EA 2004 6 21 COMA0460331 120040526A5210601R31881273 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR PANEL BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01470CA5718 7650 PAX DOOR PRESSURE PANEL CABLE IS BROKEN AT THE END OF THE CLEAVIS DUE TO RUBBING ON THE FLAP (P/N 601R318122-3). PAX DOOR PRESSURE PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE (P/N 601R3188127-3). 2L72 4F RTA21EA 20040621000902004062100090EA 2004 6 21 COMA0460332 120040523A261324403615 ELEMENT CNDAIRCL600 CL6002B19 1900309EA RT MLG WW MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01427CA 7460 FLIGHT 5436 MLG BAY OVERTEMP WARNING. REPLACED RT MLG BAY SENSING ELEMENT. 2L72 4F RTA21EA 20040621000912004062100091NE 2004 6 21 COMA0470043 220040521A72304114T15P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ENG COMP VIBRATION A COMAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01317CA3939 10055 FLIGHT 5249 LT ENGINE FAN AT 2.3 VIBES. REPLACED THE LT ENGINE FAN BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20040621000942004062100094NM 2004 6 21 CALA0400528 120040609A532069482836 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714662 28923 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT UPPER FLANGE FASTENER HOLE IN E&E COMPARTMENT BILGE AREA, STA 300, LBL 4. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 69-48283. 2L72 4F RTA16WE 20040621000952004062100095EU 2004 6 21 YENA200418 120040322A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT DISCHARGED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15564JB3387 2020 EMERGENCY LIGHTS FAIL OPERATIONAL TEST. REPLACED 11WL EPSU PER AMM 33-51-38-04. OPERATIONS CHECK OF EMERGENCY LIGHTS NORMAL. 2L72 4F RTA28NM 20040621000972004062100097NM 2004 6 21 TSAA0456041 120040521A5610141A48107 WINDOW BOEING737 73776N 13844CHNM COCKPIT CRACKED A TSAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP13745AL5458 1388 29904 CAPTAIN’S NR 2 OUTER WINDOW PANE CRACKED. RETURNED TO HNL. OVERWEIGHT LANDING AT 141,000 LBS. DESCENT RATE LESS THAN 100 FEET PER MINUTE AT 140 KTS. REPLACED NR 2 CAPTAIN SIDE WINDOW IAW AMM 56-12-11-4. OPS CHECK OK. PERFORMED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 5-51-35-2. NO DEFECTS NOTED. VERIFIED WINDOW HEAT SYSTEM OPERATIONAL IAW AMM 30-41-00-710-80, OPS CHECK NORMAL. AS PRECAUTION; REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-11, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040621000982004062100098SO 2004 6 21 RAIA00405013 120040521A3610AS568226 O-RING EMB 145 EMB145LR 3260212SO NR 1 BLEED SYS DETERIORATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03817HK 145058 STL - BLEED LEAK NR 1 INDICATION. MAINTENANCE REMOVED AND REPLACED NR 1 BLEED LINE SEAL UNDER CARGO BAY FLOOR. 2L72 4T RTT00011AT 20040621000992004062100099EU 2004 6 21 RAIA00405014 120040522A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU FUEL CONTROL DIRTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03564HK 41081 STL - RIGHT RED BETA LIGHT ILLUMINATED. MAINTENANCE CLEANED CONNECTOR ON RT FUEL CONTROL. 2L72 4T RTA41NM 20040617000192004061700019SO 2004 6 17 C2XA04SH288 120040516A531514522461011 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000322004061700032SO 2004 6 17 C2XA04SH295 120040518A541114576631022 STIFFENER EMB 145 EMB145 3260210SO NR 2 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 SHV - DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000352004061700035SO 2004 6 17 C2XA04SH352 120040610A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714573 145638 SHV - DURING C-CHECK, THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 201, SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000392004061700039 2004 6 17 C2XA04IA068 420040611A34177014700921 ADC EMB 145 EMB145 3260210SO COCKPIT BURNED OUT A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW27139641095410954 145123 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A SMOKE ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AIR DATA COMPUTER TO BE THE SOURCE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED COMPUTER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000542004061700054NM 2004 6 17 AWXA200400565 120040524A33501012621 LIGHT BOEING737 737277 1384570NM OVERWING EXIT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28186AW 22653 DURING 8-DAY CHECK THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040617000552004061700055NM 2004 6 17 AWXA200400567 120040429A531065479767 CREASE BEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON CREASE BEAM WEB (STR 17 RT) BETWEEN BS 827 AND BS 847. MAINTENANCE REMOVED CORRODED WEB (STR 17 RT) FROM BS 827 TO BS 847; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47976; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, 8 & 9. 2L72 4F RTA16WE 20040617000662004061700066WP 2004 6 17 DHL2004803501 120040319A5347 SEAT TRACK DOUG DC8 DC873 302199CWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT NR 6 FLOOR TRACK LUGS WORN, STA 1482.000. CUT OUT DAMAGED SECTION OF NR 6 FLOOR TRACK, STA 1482.000 IAW DC8 SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 51-3-0 PG 1, DC8 SRM 53-2-3 PG 17-19. 2L74 4F RT4A25 20040617000762004061700076NM 2004 6 17 SWAA041674 120040613A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29712SW 27846 DURING SCHEDULED RON, FOUND EXTERIOR EMERGENCY EXIT GROUND ILLUMINATION LIGHTS WEAK. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040617000772004061700077NM 2004 6 17 SWAA041675 120040613A57536546435336 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT OUTBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20040617000872004061700087SO 2004 6 17 C2XA04SH303 120040519A532014524131005 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617000882004061700088SO 2004 6 17 C2XA04IA069 120040612A3397GS85008DC WIRE EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715948 145056 IAH - DURING AIRCRAFT MODIFICATION SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND GROUND WIRE GS85008DC TO BE LOOSE. MAINTENANCE RESECURED THE GROUND WIRE, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617000972004061700097SO 2004 6 17 C2XA04IA053 120040507A3350RPS1B BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711155 145782 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHT OVER ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4F RT 20040617001072004061700107SO 2004 6 17 C2XA04TY087 120040530A532014525480003 SILL EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715574 145639 TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT SILL AT 65. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR CUTOUT SILL IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040617001112004061700111SO 2004 6 17 CX2A04TY088 120040602A532014521725001 SILL EMB 145 EMB145LR 3260212SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713979 145181 DURING A SCHEDULED MODIFICATION THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CARGO DOOR SILL AND THRESHOLD PLATE. INSTALL A NEW DOOR SILL IAW EMB 135/145 SRM 51-40-02. LEAK CHECKS GOOD IAW EMB 145 AMM 21-31-00. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040617001192004061700119SO 2004 6 17 C2XA04SH360 120040612A532014526437001 BUTTSTRAP EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 SHV - DURING C-CHECK THE RIGHT BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001252004061700125SO 2004 6 17 C2XA04SH286 120040516A532014521725013 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001282004061700128SO 2004 6 17 C2XA04CL059 120040601A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW2714925 145004 THE CREW REPORTED THE EMERGENCY EXIT SIGN WAS INOPERATIVE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040617001302004061700130SO 2004 6 17 C2XA04SH287 120040516A532014522178005 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001362004061700136SO 2004 6 17 C2XA04SH309 120040522A711014576502413 COWLING EMB 145 EMB145 3260210SO NR 1 ENGINE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 DURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040617001472004061700147SO 2004 6 17 C2XA04SH315 120040523A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001492004061700149SO 2004 6 17 C2XA04SH317 120040523A531514522461011 GUSSET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 SHV - DURING C-CHECK THE RIGHT FLOORBEAM DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001632004061700163SO 2004 6 17 C2XA04SH311 120040522A532014528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714920 145380 DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040617001852004061700185NM 2004 6 17 2004UALA00462 120040510A5247 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 FWD CORNER OF APU DOOR 315AR SKIN CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. DAMAGED FROM CONTACT WITH MAINTENANCE VEHICLE. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER SRM AND INSTALLED DOUBLER AND FILLER MATERIAL. 2L72 4F4 FRTA2NM E17NE 20040617001862004061700186SO 2004 6 17 MASA200400260 120040512A3350BR9279232 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07839MJ 145416 LT FUSELAGE EXTERIOR EMERGENCY EGRESS FLOODLIGHT INOP. REPLAMPED AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040617001902004061700190NM 2004 6 17 2004UALA00467 120040512A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 FRAME AT STA 1500 ABOVE STR 26L DENTED. MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. CUT OUT DAMAGED AREA AND FABRICATED ANGLE REPAIR AND INSTALLED IAW SRM. 2L72 4F4 FRTA2NM E17NE 20040617001932004061700193NM 2004 6 17 2004UALA00470 120040512A3350DHE1141 SENSOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29829UA 1211 CABIN EMERGENCY LIGHTS FAILED TO TEST. RESET CIDS SYSTEM AND NO SMOKING LIGHTS. ACCOMPLISHED OPERATIONAL TEST OF EMERGENCY LIGHTS PER MM 33-51-00-710-001, SYSTEM GROUND TESTED OK, NO FAULTS NOTED ON PTP. 2L72 4F4 FRTA28NM E40NE 20040617001972004061700197SO 2004 6 17 SWIA200413350 120040524A27513471001001 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07232SW 120306 ON LANDING EXTENDING FLAPS TO 25 DEGREES, GOT CONTROL FAULT ON OUTBOARD FLAPS. REPLACED FLAP ANNUNICIATOR. OPS CHECKS GOOD. S/N OFF: 0171. 2L72 4T RTA31SO 20040618000112004061800011WP 2004 6 18 ASAA0480211 120040402A5730ARB0975517 PANEL DOUG DC9 DC983 3022083WP RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND WING RIGHT LOWER FUEL PANEL NR 1454C CORRODED. ORDERED AND REPLACED WITH NEW PANEL IAW MD80 SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040618000182004061800018WP 2004 6 18 ASAA0480223 120040402A532199365411 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND PASSENGER COMPARTMENT, FLOOR PANEL AT STATION 1154 TO 1250 RBL 22 TO LBL 22 IS DELAMINATED AND HAS CORRODED/BROKEN INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000252004061800025WP 2004 6 18 ASAA0480209 120040402A533059366671 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 1287 BETWEEN LONGERONS 29L-29R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-04. (M) 2L72 4F RTA6WE 20040618000322004061800032WP 2004 6 18 ASAA0480265 120040404A575359304954 VANE DOUG DC9 DC983 3022083WP TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FUOND RIGHT INBOARD FLAP VANE, INBOARD LEAD EDGE IS GOUGED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040618000402004061800040WP 2004 6 18 ASAA0480258 120040404A5730ARB0872538 ACCESS PANEL DOUG DC9 DC983 3022083WP WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 DURING HV CHECK, FUEL ACCESS PANEL NR 1414 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040618000552004061800055NM 2004 6 18 ASAA0480392 120040510A532099305388 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND MAIN CABIN STATION 731 AT LONGERON 18R CORROSION ON UPPER AND LOWER SURFACE OF CUSP MEMBRANE. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000602004061800060NM 2004 6 18 ASAA0480383 120040510A5330991183955 SKIN DOUG MD80 MD83 3023681NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND EMP SKIN GOUGED BETWEEN STATION 1497 AND 1510. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000672004061800067NM 2004 6 18 750WL0004 120040520A3350 BULB BOEING757 757200 1384950NM EMERGENCY LIGHT BROKEN A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05750WL 23928 ONE LIGHT OUT IN FWD CABIN FLOOR PATH LIGHTING. REPLACED BROKEN BULB. OPS CHECKS GOOD. 2L72 4F RTA2NM 20040618000752004061800075WP 2004 6 18 DHL2004803524 120040405A57203645612 SUPPORT DOUG DC8 DC873 302199CWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79388 46123 AFT BOOSTER PUMP SUPPORT CRACK. REMOVED AND REPLACED AFT BOOSTER PUMP SUPPORT IAW DC8 SRM 51-1-20D PAGE 219. 2L74 4F RT4A25 20040618000792004061800079WP 2004 6 18 DHL2004803527 120040331A57203645612U BRACKET DOUG DC8 DC873 302199CWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET (NR 1 ALT TANK) IAW DC8 SRM 51-1-20D PG 9, 21. 2L74 4F RT4A25 20040618000912004061800091NM 2004 6 18 SWAA041705 120040616A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040618000922004061800092NM 2004 6 18 SWAA041706 120040616A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040618001092004061800109WP 2004 6 18 GTIA040472 120040519A3220 MONITOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RT REAR DEFLECTOINOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23832NK 49618 NOSE GEAR SPRAY DEFLECTOR MISSING RT REAR DEFLECTOR. REPLACED RT REAR DEBRIS DEFLECTOR ON NOSE GEAR SPRAY DEFLECTOR. 2L72 4F4 FRTA6WE E2EA 20040621000062004062100006WP 2004 6 21 ASAA0480245 120040404A5330591140659 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND FUSELAGE SKIN DENTED AND GOUGED AT FS 294 LONGERON 17R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-04. (M) 2L72 4F RTA6WE 20040621001012004062100101CE 2004 6 21 60926 120040428A32601293640455 CIRCUIT CARD BEECH 1900 1900D 1154162CE MLG FAILED A AMWAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 CE07162YV UE162 CREW DID NOT RECEIVED MLG INDICATION WHEN GEAR WAS DOWN AND LOCKED. RESET THE INDICATOR C/B NORMAL CONFIRM 3 GREENS. LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR INDICATOR CB. REMOVED AND REPLACED 3 PCB CARD. P/N 129-3640455, S/N 814196. 2L72 4T RTA24CE 20040621001032004062100103EA 2004 6 21 COMA0460328 120040521A3260 UPLOCK SENSOR CNDAIRCL600 CL6002B19 1900309EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01916CA 7014 FLIGHT 5319 GEAR DISAGREE WARNING DURING RETRACTION. ADJUSTED THE RT MLG UPLOCK PROXY SENSOR. 2L72 4F RTA21EA 20040621001052004062100105SO 2004 6 21 ESPA200400002 120040515A3246L610549 BEARING GOODYEAR GULSTMG159 G159 3952202SO NR 1 MAIN WHEEL SEIZED E ESPAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO11196PA 414 AUG6579 139 AFTER TAKEOFF, DISCOVERED THAT THE NR 1 MAIN WHEEL ASSEMBLY HAD DISCONNECTED FROM THE AXLE. THE AXLE NUT WAS STILL IN PLACE. IT WAS DETERMINED THAT A WHEEL BEARING FAILURE WAS PROBABLY THE CAUSE. 2L72 4T 1A17 20040621001152004062100115NM 2004 6 21 750WL0003 120040511A3350 LIGHT BOEING757 757200 1384950NM L2 DOOR INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY LIGHT AT L2 DOOR IS INOP. REPLACED EMERGENCY LIGHT AT L2 DOOR. OPS CHECKS GOOD. 2L72 4F RTA2NM 20040621001582004062100158 2004 6 21 ASMF200406013 420040615A34214608000306 GYRO DOUG DC9 DC987 3022087WP COCKPIT FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23803ML7488 7478 49726 CAPTAIN REPORTED THAT DURING FLIGHT UNTIL APPROACH, RDMI AND ND WITH DIFFERENCE BETWEEN 30-40 DEGREES. DURING TRANSIT CHECK AT CUU, AHRU NR 1 WAS REPLACED IAW MM 34-21-10, TEST CORRECT. AIRCRAFT WAS DISPATCHED AND RETURNED OF FLIGHT, DFGC AND AHRU NR 2 FAILED AND FLIGHT DIRECTOR BUSES IN BOTH PFD´S AND FMA´S WITHOUT INFORMATION. AFTER LANDING, AHRU INFORMATION WAS RECOVERED, AHRU NR 2 WAS REPLACED, TEST CORRECT. DURING OVERNIGHT SERVICE, DFGC TEST WAS PERFORMED IAW MM 22-01-05, ALL CORRECT. 2L72 4F RTA6WE 20040621001602004062100160 2004 6 21 ASMF200406015 420040615A34426225132101 RADAR DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE WX SYSTEM FAILED W ASMFA UNSCHED LANDING O OTHER CRCRUISE 1 SW231075T3335 3335 49724 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, LOW FUEL AND CAPTAIN REPORTED RADAR SYSTEM FAILED. DURING MAINTENANCE REVISION, RADAR, ANTENNA, TRANSCEIVER AND RADAR DISPLAY WERE CHECKED, ALL CORRECT. RADAR TRANSCEIVER WAS REPLACED IAW MM 34-41-04, TEST CORRECT. AIRCRAFT WAS REFUELED, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040621001632004062100163 2004 6 21 ASMF2004010 420040413A3497 CONNECTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE VOR SYSTEM DAMAGED W ASMFK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW23838AM 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT THE LT VHF SYSTEM WAS OUT OF SERVICE. TECHNICAL PERSONNEL REPLACED RX VOR ILS AND CONTROL PANEL, BUT FAIL CONTINUED. WIRING WAS CHECKED DETECTING THE LINE 1RN11A22 OF THE CONNECTOR P10-407 (PIN H) DAMAGED. IT WAS REPAIRED IAW WDM 34-32-01 AND TESTED IAW MM 34-32-00, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040621001642004062100164NM 2004 6 21 ANCF200400013 120040611A2131 CONTROLLER BOEING767 767383 1385214NM CABIN PRESSURE MALFUNCTIONED W ANCFO OTHER J WARNING INDICATION CRCRUISE 1 SO23984AN 24357 EICAS MESSAGE. LT ENGINE BLEED OFF AND BLEED LIGHT ILLUMINATED. REMOVED AND REPLACED TEMP SENSOR FAN MODULATING VALVE. IAW AMM 36-11-17 PG 401 TEST SATISFACTORY. CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUMINATE EICAS MSG CABIN ALTITUDE WAS UNABLE TO RESTORE. CABIN PRESS USING MANUAL MODE. P/N 773284-6 S/N 900210. CABIN PRESS CONTROLLER BITE PERFORMED, IAW FIM 21-30-00/101 FIG 104 IT WAS FOUND CONTROLLER FAULT. REMOVED AND REPLACED THE 2 CABIN PRESS CONTROLLER, IAW AMM 21-31-02 P 401 OPERATIONALS CHECKS SATISFACTORY.P/N 2117388-6, S/N 10-1976 AND S/N 18-1346 2L72 4F RTA1NM 20040621001652004062100165NM 2004 6 21 ANCF200400009 120040430A3251 STEERING SYS DOUG MD80 MD83 3023681NM NLG STUCK W ANCFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO23593AN 53093 DURING ALIGNMENT FOR T/O AT MDE NOSE WHEEL STEERING, STUCK. INSPECTION CHECK TO NOSE WHEEL STEERING , STRUT AND SECURITY CABLES BY CONDITION AND LEAKS WAS PERFORMED IAW 32-50-00 PAGE 103,201,202 WITH SATISFACTORY RESULTS. 2L72 4F RT 20040621001662004062100166NM 2004 6 21 ASMF200406009 120040611A2913405893 PUMP DOUG MD88 MD88 3023688NM HYD SYSTEM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23162PL8125 5 49765 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT DURING TAXING AT MEX WITH 33 DEGREES (R HYD TEMP HI) LIGHT TURNED ON AND DURING REVISION AT MTY, AUXILIARY ELECTRICAL HYDRAULIC PUMP WAS WITH HIGH TEMPERATURE AND WAS REPLACED IAW MM 29-10-06, TEST CORRECT IAW MM 29-00-00. DURING TAXING AT MTY, AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF PUMP BREAKER WAS ACTIVATED. RIGHT HYDRAULIC SYSTEM FILTERS WERE DETECTED WITH METALLIC PARTICLES; FILTERS, HYDRAULIC LIQUID, RIGHT HYDRAULIC PUMP AND PTU WERE REPLACED IAW MM 29-10-14, 29-10-06 AND 29-10-07, RESPECTIVELY, TESTS CORRECT. 2L72 4F RTA6WE 20040621001672004062100167WP 2004 6 21 ASMF200406016 120040617A27305918125501 DAMPER DOUG DC9 DC982 3022082WP LT AILERON JAMMED W ASMFD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SW23491SH330817022 49150 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AND ELEVATOR CONTROL TEST, CAPTAIN REPORTED ELEVATOR JAMMED. ELEVATOR CONTROL SYSTEM WAS CHECKED AND DAMAGE WAS DETECTED IN CONTROL COLUMN DURING MOVEMENT OF NOSE DOWN. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, ELEVATOR CABLES AND PULLEYS WERE VERIFIED IAW MM 27-30-00, TAIL CONE AND CARGO COMPARTMENTS WERE CHECKED, ALL CORRECT. LT ELEVATOR CONTROL VALVE AND HYDRAULIC MULTIPLE WERE REPLACED IAW MM 27-30-07 AND 27-33-08, RESPECTIVELY, TEST CORRECT. 2L72 4F A6WE 20040621001692004062100169 2004 6 21 ASMF200406006 420040607A22104034241974 COMPUTER DOUG DC9 DC982 3022082WP FLT GUIDANCE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23505MD4311 49149 AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF FAIL IN LT FLIGHT GUIDANCE SYSTEM INDICATION. SYSTEM WAS REACTIVATED AND ELECTRICAL BUSS TURNED OFF, AUTO TEST IN BOTH SYSTEMS WAS PERFORMED, ALL CORRECT. DURING OVERNIGHT SERVICE, FLIGHT GUIDANCE COMPUTER WAS REPLACED IAW MM 22-01-01, TEST CORRECT. 2L72 4F A6WE 20040621001732004062100173WP 2004 6 21 ASMF200406012 120040613A5242 DOOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE E/E BAY UNLOCKED W ASMFA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SW23505MD 49149 AIRCRAFT RETURNED, ELECTRIC/ELECTRONIC DOOR LIGHT TURNED ON. DURING MAINTENANCE REVISION WAS DETECTED THAT ELECTRIC/ELECTRONIC DOOR WAS NOT LOCKED. DOOR WAS CORRECTLY CLOSED AND LOCKED, ALL CORRECT. 2L72 4F4 F A6WE E2EA 20040621001752004062100175NM 2004 6 21 AWXA200400528 120040427A5330655298813 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.125 INCH CRACK WAS FOUND IN EXTERNAL FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT L-2 DOOR LOWER FORWARD CUTOUT BS 957, STR 17 LT. MAINTENANCE REAMED OUT CRACK AT FASTENER HOLE AND PERFORMED A HFEC INSPECTION. FABRICATED A FILLER, DOUBLER, AND COUNTERSUNK REPAIR WASHER, INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 203 PG 205-208. 2L72 4F RTA16WE 20040621001762004062100176NM 2004 6 21 QXEA200400361 120040524A1430 NUT PLATE BOMBDRDHC8 DHC8401 1390041NM EXTERIOR LIGHT LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - AFT LEFT AND FORWARD LEFT NUT PLATES HAS COME LOOSE FROM THE RED LOCATOR BEACON. REPAIRED IAW SRM 51-43-05. 2H72 4T RTA13NM 20040621001782004062100178NM 2004 6 21 AWXA200400529 120040503A5330654577810 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .375 INCH CRACK WAS FOUND IN EXTERNAL FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT R-2 DOOR LOWER FORWARD CORNER BS 957, STR 17 RT. MAINTENANCE REAMED OUT CRACK AT FASTENER HOLE AND PERFORMED A HFEC INSPECTION. FABRICATED A FILLER, DOUBLER, AND COUNTERSUNK REPAIR WASHER, INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 203 PG 205-208. 2L72 4F RTA16WE 20040621001812004062100181EU 2004 6 21 AWXA200400537 120040512A5753D57570087200 SKIN AIRBUS320 A320231 3930325EU TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK FOUND THE RT INBOARD FLAP DELAMINATED AT THE LOWER INBOARD SURFACE, 7 INCHES OUTBOARD OF RIB 1, WS 700 RIGHT. MAINTENANCE CUT OUT DELAMINATED AREA OF RT INBOARD FLAP LOWER SKIN AT RIB 1, WS 700 RT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211. 2L72 4F RTA28NM 20040621001822004062100182EU 2004 6 21 AWXA200400538 120040515A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU EMERGENCY LIGHT DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 MCN - EEL - DURING C-03 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT WIRING DAMAGED AT FORWARD LT PARTITION JUST INSIDE THE L-1 DOORWAY FR 20, Y765 LT. MAINTENANCE REPAIRED DAMAGED EMERGENCY ESCAPE PATH LIGHT WIRE AT FORWARD LT PARTITION, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040621001832004062100183NM 2004 6 21 AWXA200400539 120040429A531365479767 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 17 RT BETWEEN BS 827 AND BS 847. MAINTENANCE REMOVED CORRODED SECTION OF STRINGER 17 RT FROM BS 827 TO BS 847; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-47976; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 8, & 9. 2L72 4F RTA16WE 20040621001852004062100185NM 2004 6 21 QXEA200400330 120040519A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX - EMERGENCY FLOOR TRACK LIGHTING AT STATION 270.50 IS CRACKED AND HAS EXPOSED WIRES. REMOVED AND REPLACED TRACK LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040621001862004062100186NM 2004 6 21 QXEA200400331 120040518A5312 PRESSURE PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 700 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - UPPER CEILING WALL IN NOSE WHEEL WELL HAS A PROTRUDING DENT FROM ABOVE, IN THE CENTER OF TWO RIVETS, JUST ABOVE THE LEFT HAND TRUNNION PROX SENSOR. REPAIRED IAW HORIZON AIR EA 6-53-353. 2H72 4T RTA13NM 20040621001882004062100188NM 2004 6 21 QXEA200400333 120040520A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - SEAT TRACK NR 9 AT STATION X778.5 HAS SURFACE CORROSION IN CHANNEL. REPAIRED IAW HORIZON AIR EA 6-53-356. 2H72 4T RTA13NM 20040621001902004062100190NM 2004 6 21 QXEA200400335 120040520A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - SEAT TRACK NR 9 AT STATION X778.5 HAS SURFACE CORROSION IN CHANNEL. REPAIRED IAW HORIZON AIR EA 6-53-356. 2H72 4T RTA13NM 20040621001922004062100192NM 2004 6 21 QXEA200400351 120040520A7810 ATTACH BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - NR 1 EXHAUST OUTLET (FINGERNAIL) HAS SIX CRACKED BRACKETS BETWEEN INNER AND OUTER LAYERS AND THE LOWER AFT ATTACH BRACKET IS CRACKED. REPAIRED IAW -8 TASK 78-10-26-400-801. 2H72 4T RTA13NM 20040621001952004062100195NM 2004 6 21 QXEA200400344 120040522A5410 ROD DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH 513 PDX - NR 2 ENGINE RIGHT HAND LOWER STRUT IS CHAFED FROM HOLD OPEN ROD ON PANEL 424AR. REPAIRED IAW RD 8-54-038. 2H72 4T RTA13NM 20040621002022004062100202NM 2004 6 21 AWXA200400513 120040427A575465C26602218 SKIN BOEING737 7373G7 1384595NM NR 5 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .25 INCH CRACK IN NR 5 SLAT LOWER SKIN AT FASTENER HOLES BELOW INBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGE IN NR 5 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20040621002042004062100204NM 2004 6 21 AWXA200400515 120040506A5320654580733 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN INTERCOSTAL ATTACH ANGLE BS 288 JUST FORWARD OF R-1 DOOR STR 10 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL ATTACH ANGLE BS 288, STR 10 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45807; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6, 7, 8, 12, & 14. 2L72 4F RTA16WE 20040621002112004062100211EA 2004 6 21 QXEA200400329 120040516A3620 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA RT BLEED ILLUMINATED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09615QX 10065 SMF - ON FLIGHT 2494, ON CLIMBOUT, RT BLEED DUCT WARNING MESSAGE AFTER 5 SEC WARN WENT OUT AND REPLACED WITH RT BLEED DUCT CAUTION MESSAGE. C/W CHECKLIST AND MANUAL BLEED PROCEDURES. FOUND MDC TO SHOW A BLEED LEAK EVENT OCCURRED AT MT143/144 CHANNEL A & B. NO CURRENT FAULTS. SELF TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040621002132004062100213EA 2004 6 21 QXEA200400347 120040515A2730C16258AA TRANSDUCER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 INTERMITTENT A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09617QX4149 10130 DEN - ON FLIGHT NUMBER 4216, DURING CRUISE AT FL330, MACH .80, THE CREW GOT AN INTERMITTENT STICK SHAKER, STALL SIREN AND FLASHING STALL LIGHT WITH STALL FAIL CAUTION MESSAGE. MAINTENANCE INTEROGATED THE MDC AND FOUND THE LT AOA RESOLVER INTERMITTENT. MAINTENANCE THEN REMOVED AND REPLACED LEFT ANGLE OF ATTACK TRANSDUCER. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040622000032004062200003NE 2004 6 22 QXEA200400354 220040524A7200 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 600 LACK OF LUBE A QXEAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09609QX 10031 GRR965297 OKC FLIGHT 4182 ON CLIMBOUT OF DEN, NR 2 ENGINE VIBRATION AT 1.3, CLIMBING THRU 26K FT VIBRATION WENT TO 1.8 AS PER CHECKLIST, REDUCED POWER ON NR 2 ENGINE, VIBRATION BACK IN GREEN AT 1.6. MAINTENANCE COMPLIED WITH TASK 72-21-02-200-803-A01, PART 2, FAN BLADES LUBRICATION WITHIN 10 FLIGHT HOURS. 2L72 4F4 FRTA21EA EOOO63EN 20040622000042004062200004WP 2004 6 22 ASAA0480284 120040420A5347593054765 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND PASSENGER SEAT TRACK GOUGED AT FS 275-300. REMOVED DAMAGED SECTION AND INSTALLED REINFORCEMENT PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000062004062200006WP 2004 6 22 ASAA0480198 120040330A53219936639501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CORRODED, GOUGED, AND CHAFED AT FS 886-946. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000072004062200007WP 2004 6 22 ASAA0480199 120040402A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND DURING HV CHECK, PAX CABIN FLOOR PANEL IS CORRODED AT FS 886-937. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000112004062200011NM 2004 6 22 ASAA0410254 120040505A5315 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - DURING C-CHECK, FOUND UPPER CHORD DAMAGE ON FLOORBEAM WEB. REMOVED DAMAGE AND INSTALLED RPR PARTS IAW SRM 51-40-2. (M) 2L72 4F A16WE 20040622000142004062200014WP 2004 6 22 ASAA0480296 120040420A532099177013 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND DENT ON INTERCOSTAL FLANGE 1 INCH WIDTH BY 3 INCHES DEEP AT CANTED STATION 1497-1510 AT 25L. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW MD80 SRM 51-30-2 AND DRAWING 99177011. (M) 2L72 4F RTA6WE 20040622000152004062200015WP 2004 6 22 ASAA0480295 120040420A53305911401211 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE STATION 178 BETWEEN 28R AND 29R DENTED D=1.25 BY = .023. COMPLIED WITH HFEC INSPECTION, NO DEFECT NOTED. NO FURTHER ACTION REQUIRED IAW ASA EA 5530-01775. (M) 2L72 4F RTA6WE 20040622000172004062200017NM 2004 6 22 ASAA0410259 120040402A53156562175 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION AFT CARGO BAY MAIN CABIN FLOORBEAM REPAIR STRAP LOWER FLANGE. REMOVED CORRODED REPAIR STRAP ON FLOORBAM LOWER FLANGE, FABRICATED REPAIR STRAP AND INSTALLED. (M) 2L72 4F A16WE 20040622000182004062200018NM 2004 6 22 ASAA0410261 120040516A33508821004 BATTERY PACK BOEING737 737298C 1384490NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (M) 2L72 4F RTA16WE 20040622000232004062200023WP 2004 6 22 ASAA0480285 120040420A53475930565 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND DURING HV CHECK, PASSENGER SEAT TRACK GOUGED AT FS 807. REMOVED DAMAGED SECTION AND INSTALLED REINFORCEMENT PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000272004062200027WP 2004 6 22 ASAA0480289 120040420A532199365851 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND PASSENGER CABIN FLOOR PANEL TORN AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M0 2L72 4F RTA6WE 20040622000292004062200029WP 2004 6 22 ASAA0480275 120040412A532199365481 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE ELONGATED A K NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL HAS ELONGATED HOLES AT FS 200-256. FIBERGLASS REPAIR PER MM 25-00-00. (M) 2L72 4F RTA6WE 20040622000302004062200030WP 2004 6 22 ASAA0480276 120040412A53219932816503 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAT CHANNELS DISBONDED AT FS 256-294. BOND-REPAIRED PER MM 20-20-01. (M) 2L72 4F RTA6WE 20040622000322004062200032WP 2004 6 22 ASAA0480278 120040412A53009936656 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 1309-1361. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000332004062200033NM 2004 6 22 ASAA0410244 120040501A5315 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - DURING C-CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED FLOOR BEAM IAW SRM 53-10-1. (M) 2L72 4F A16WE 20040622000342004062200034WP 2004 6 22 ASAA0480230 120040402A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND FLOORBOARD STATION 100-250 RBL 22 HAS EDGE DAMAGE, DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000382004062200038WP 2004 6 22 ASAA0480203 120040402A143059644461 FASTENER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND DURING HV CHECK, CORROSION AROUND FASTENER INSIDE LONGERON 30 AT STATION 655 IN MID PIT. REMOVED CORROSION, INSTALLED U-CHANNEL REPAIR PER SRM 53-02. (M) 2L72 4F RTA6WE 20040622000402004062200040WP 2004 6 22 ASAA0480399 120040515A53209936368101 SUPPORT ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OKC - FOUND DURING C-CHECK, LEFT WHEEL WELL FORWARD INBOARD CORNER FRAME SUPPORT ANGLE IS CRACKED. REMOVED ANGLE AND INSTALLED REPLACEMENT ANGLE IAW 51-10-2. (M) 2L72 4F RTA6WE 20040622000412004062200041WP 2004 6 22 ASAA0480398 120040515A533059114003 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OKC - FOUND DURING C-CHECK, NOSE GEAR, RIGHT AFT DOOR, AFT HINGE CUT OUT SKIN IS CRACKED. STOP DRILLED CRACK, COMPLIED WITH HFEC, INSTALLED RPR DOUBLER IAW 53-05. (M) 2L72 4F RTA6WE 20040622000422004062200042WP 2004 6 22 ASAA0480397 120040515A532059327311 SPLICE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - DURING C-CHECK, FOUND L30 SPLICE AT STATION 585 IS CORRODED. REMOVED DAMAGED SPLICE AND INSTALLED NEW IAW 51-30-5. (M) 2L72 4F RTA6WE 20040622000432004062200043WP 2004 6 22 ASAA0480396 120040515A532099367183 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - FOUND DURNG C-CHECK, LEFT INTERCOSTAL IN AFT PIT AT STATION 1307-1322 IS CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW IAW 51-30-2. (M) 2L72 4F RTA6WE 20040622000442004062200044WP 2004 6 22 ASAA0480197 120040330A53219957918501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CRACKED AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000452004062200045WP 2004 6 22 ASAA0480201 120040402A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CORRODED AT FS 826-869. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000482004062200048WP 2004 6 22 ASAA0480300 120040420A532199365491 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 160-200 RBL 44 TO RBL 54 HAS MISSING MATERIAL. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000492004062200049WP 2004 6 22 DHL2004803542 120040422A5730 SKIN DOUG DC8 DC873 302199CWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RIGHT WING CTR L/E UPPER SURFACE SHOWS CORROSION AT STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDV43-7, DWG V43-R07. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-7, DWG V43-R07. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001, FABRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.071) IAW ED EDV43-7, DWG V43-R07. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER AND DOUBLER. 2L74 4F RT4A25 20040622000502004062200050WP 2004 6 22 DHL2004803543 120040422A5730 SKIN DOUG DC8 DC873 302199CWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING OUTBOARD L/E INNER SECTION CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-6, DWG V43-R06. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6 0.050) AND DOUBLER (7075-T6 0.063) IAW ED EDV43-6, DWG V43-R06. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW ED EDV43-6, DWG V43-R06, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040622000522004062200052WP 2004 6 22 DHL2004803544 120040422A5730 SKIN DOUG DC8 DC873 302199CWP LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING OUTBOARD L/E INNER SECTION CORRODED, STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-1, DWG V43-R01. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6A; 0.050) AND DOUBLER (7075-T6 0.063) IAW ED EDV43-1, DWG V43-R01. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER IAW ED EDV43-1, DWG V43-R01, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040622000532004062200053 2004 6 22 QXEA200400348 420040523A2200 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA AUTOPILOT TRIM ILLUMINATED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09611QX 10041 OKC - ON FLIGHT 4165, AFTER DEPARTING DENVER CREW RECEIVED AN AUTOPILOT TRIM INDICATOR NOSE DOWN MESSAGE ON NR 1 MFD. CREW COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST AND NO FURTHER PROBLEM WERE ENCOUNTERED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO MESSAGES POSTED. OPERATIONAL TEST OF ELEVATOR SERVO WERE PERFORMED AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040622000542004062200054EA 2004 6 22 QXEA200400349 120040522A2760D14303 PCU CNDAIRCL600 CL6002C10 1390015EA ZONE 500 JAMMED A QXEAO OTHER O OTHER APAPPROACH 1 NM09607QX6256 496 10024 PDX - ON FLIGHT NUMBER 2560, ON APPROACH INTO PDX THE OUTBOARD FLIGHT SPOILERS, OUTBOARD SPOILERONS CAUTION MESSAGE DISPLAYED ON THE SYNOPTIC PAGE. LEFT OUTBOARD WAS AMBER AND RIGHT WAS WHITE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT OUTBOARD MULTIFUNCTION SPOILER PCU WAS JAMMED. THE PCU WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040622000552004062200055NM 2004 6 22 AWXA200400541 120040505A5522 SKIN BOEING737 7373G7 1384595NM RT ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE RT ELEVATOR UPPER SURFACE SKIN DELAMINATED AT ELEV STA 52.0. MAINTENANCE PREPARED SURFACE AND BONDED REPAIR PLIES IAW B737-300 SRM 51-70-04 FIG 10 REPAIR 1. 2L72 4F RTA16WE 20040622000562004062200056WP 2004 6 22 IXXA0400027S 120040212A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK FOUND RT WING OUTBOARD L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STATION XW 485.000- XFS 710. REPAIR IS ACCOMPLISHED. REMOVED FASTENER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 57-2-1 FIG 44. REMOVED CORROSION FROM UPPER SKIN SURFACE OF RT WING OUTBD L/E INNER SECTION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED DAMAGED SKIN SECTION IAW DC8 SRM 57-2-1 FIG 44, FABRICATED DOUBLER IAW DC8 SRM 57-2-1. CLEANED, TREATED AND PRIMED AREA & INNER FACE OF DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-1 FIG 44, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622000612004062200061WP 2004 6 22 IXXA0400032S 120040303A5753 SKIN DOUG DC8 DC873F 302199FWP RT WING TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE INSPECTION RT OUTBOARD FLAP HAS INTERIM REPAIR ON UPPER PANEL (STA SF 415.000-440.000) MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-4 FIG 4. REMOVED UPPER SKIN WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-1-21 PG 1, FABRICATED NEW SKIN IAW DC8 SRM 57-7-1 FIG 4. CLEANED, TREATED AND PRIMED AREA & INNER FACE OF NEW SKIN IAW DC8 SRM 51-1-8B. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040622000622004062200062WP 2004 6 22 IXXA0400033S 120040224A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION AFT PASSENGER DOOR RT UPPER JAMB CORNER WITH .5 INCH CRACK IN IT, STA 1660.000. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 53-2-0 FIG 18, FABRICATED FILLER, DOUBLER, TRIPLER IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 11. INSTALLED FILLER, DOUBLER & TRIPLER WITH NEW FASTENERS IAW DC8 SRM 53-2-0 FIG 18, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622000632004062200063WP 2004 6 22 IXXA0400034S 120040303A5753 SKIN DOUG DC8 DC873F 302199FWP RT WING TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR BETWEEN STA XF 415.000 TO XF 440.00. REPAIR IS ACCOMPLISHED BY REPLACEMENT WAS ACCOMPLISHED IN ACCORDANCE WITH DC8 SRM CHAPTERS 57-1-0 PG 1, 57-7-1 FIG 4 TR 57-94, 51-1-21 AND N/R 3024. 2L74 4F RT4A25 20040622000672004062200067WP 2004 6 22 IXXA0400038S 120040303A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING CTR FLOORBEAM FLANGE, STA 798.000 LBL 10 IAW DC8 SRM 51-1-8 PG 17-18, IAW DC8 SRM 53-2-0 PG 2M. REMOVED DAMAGED SECTION AND FABRICATED (7075-T651 0.250) IAW DC8 SRM 51-1-21 FIG 1. PERFORMED NDT INSP, CLEANED, TREATED AND PRIMED AREA & FILLER & DOUBLER, INSTALLED FILLER & DOUBLER IAW DC8 SRM 51-2-1 FIG 1, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-D PG 1. 2L74 4F RT4A25 20040622000682004062200068WP 2004 6 22 IXXA0400039S 120040319A5753 JOINT DOUG DC8 DC873F 302199FWP RT WING TE FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD JOINT FLAP BRACE CRACKED. REPAIR IS ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED JOINT FLAP BRACE IAW DC9 SRM 51-1-21 PAGE 1. CLEANED, TREATED, PRIMED AREA IAW DC8 SRM 51-1-80 PAGE 1. INSTALLED NEW BRACE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040622000712004062200071NM 2004 6 22 AWXA200400544 120040512A5320654795711 STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND IN SEVERAL PLACES ON UPPER SURFACE OF AFT CARGO COMPARTMENT THRESHOLD STRAP BETWEEN BS 767 AND BS 857. MAINTENANCE REMOVED DAMAGED THRESHOLD STRAP FROM BS 767 TO BS 857; FABRICATED A NEW REPLACEMENT THRESHOLD STRAP PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6, 7, 8 & 12. 2L72 4F RTA16WE 20040622000752004062200075NM 2004 6 22 AWXA200400548 120040519A3350BR964411 LIGHT BOEING757 757225 1384959NM SEAT ROW 11 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28915AW 22209 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040622000762004062200076EU 2004 6 22 AWXA200400549 120040514A3397E0261CF20 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 11 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28653AW 1003 DURING P-09 CHECK FOUND A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED THE BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040622000792004062200079NM 2004 6 22 AWXA200400552 120040501A53136545767120 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2.5 INCH CRACK WAS FOUND IN STRINGER 16 RT AT BS 500C+5. MAINTENANCE TRIMMED OUT DAMAGE ON STRINGER 16 RT AT BS 500C+5 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, REPAIR CHANNEL, AND A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PARTS IAW AWA ER 03-5331-04140-RA1. 2L72 4F RTA16WE 20040622000802004062200080NM 2004 6 22 AWXA200400553 120040502A53136573746 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 988. MAINTENANCE REMOVED DAMAGE SECTION OF STRINGER 27 LT AT BS 988; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-03 FIG 201. 2L72 4F RTA16WE 20040622000812004062200081NM 2004 6 22 AWXA200400554 120040412A53206545833 FLOOR SUPPORT BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .625 INCH CRACK WAS FOUND IN MAIN CABIN FLOOR SUPPORT ANGLE (STRAP) AT BS 328, LBL 25, E & E COMPARTMENT. MAINTENANCE CUT OUT CRACKED SECTION OF MAIN CABIN FLOOR SUPPORT STRAP AT BS 328, LBL 25; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204, SHEETS 1-7. 2L72 4F RTA16WE 20040622000832004062200083NM 2004 6 22 AWXA200400525 120040430A532066142081 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2.1875 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 295, LBL 54, WL 252. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 295, LBL 54, WL 252; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 66-14208; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040622000842004062200084NM 2004 6 22 AWXA200400526 120040430A531369366002 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 277, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 154 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12, 13 & 14. 2L72 4F RTA16WE 20040622000862004062200086NM 2004 6 22 AWXA200400530 120040504A53106516301UP FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 LCQ - MAJOR REPAIR - DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN LT FRAME BS 188, AT FLOOR LEVEL WL 207. MAINTENANCE REMOVED CRACKED LT FRAME AT BS 188, WL 207; FABRICATED A NEW REPLACEMENT FRAME PER DWG 65-16301; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05 FIG 3. 2L72 4F RTA16WE 20040622000882004062200088EU 2004 6 22 AWXA200400532 120040515A1420E00528B3APNE CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 22 LT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 DURING C-03 CHECK FOUND WIRES PULLED OUT OF CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT. MAINTENANCE REMOVED AND REPLACED CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040622000892004062200089EU 2004 6 22 AWXA200400533 120040515A3397320559 SPLICE AIRBUS320 A320231 3930325EU SEAT ROW 1 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 MCN - EEL - DURING C-03 CHECK FOUND A DAMAGED WIRE AT CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 1 LT. MAINTENANCE REPAIRED DAMAGED WIRE AT CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040622000912004062200091NM 2004 6 22 SWAA041715 120040618A531465621257 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C2 CHECK, FOUND LT KEEL BEAM AT BS 500D + 7, CORRODED. REPAIRED LT KEEL BEAM PER EA. 2L72 4F RTA16WE 20040622000972004062200097NM 2004 6 22 SWAA041721 120040619A534065C360751 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C1 CHECK, FOUND LT FWD ENTRY DOOR LOWER HINGE BOX FITTING AFT EDGE, CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM. 2L72 4F RTA16WE 20040622000982004062200098EA 2004 6 22 QXEA200400350 120040522A3250 STEERING SYS CNDAIRCL600 CL6002C10 1390015EA NLG MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09607QX 10024 PDX - ON FLIGHT 2560, NOSE WHEEL STEERING INOPERABLE. THE CREW PERFORMED THE CHECKLIST AND THE FAULT WAS CLEARED. THE AIRCRAFT WAS TAXIED AND COULD NOT DUPLICATE THE FAULT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040617001752004061700175EA 2004 6 17 MASA200400283 120040522A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW0747239 7239 DEN - ABQ, THE CREW REPORTED THE SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. MX FOUND A BROKEN WIRE, REPAIRED THE WIRE, THE SYSTEM OPERATIONALY CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. 2L72 4F RTA21EA 20040617001782004061700178NM 2004 6 17 2004UALA00446 120040506A5310 STRUCTURE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 CORROSION AND MATERIAL LOSS ON STA 986.5 RBL 28 TO RBL 33. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20040617001892004061700189NM 2004 6 17 2004UALA00465 120040511A3397417U52014 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29642UA 25092 RIGHT SIDE AISLE NEXT TO MID GALLEY 1 EEL LIGHT STRIP SECTION OUT. *S/D* REPLACED CABLE AND SPLICED IN A NEW SECTION. 2L72 4F4 FRTA1NM E24NE 20040617001922004061700192NM 2004 6 17 2004UALA00469 120040513A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29556UA 26650 LEFT FUSELAGE HAS 2 DENTS FWD DOOR 2L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. SKIN REPAIR DOUBLERS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040618000012004061800001NM 2004 6 18 ASAA0480380 120040510A5330991183955 SKIN DOUG MD80 MD83 3023681NM FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND EMP SKIN PUNCTURED BETWEEN STATION 1485 AND 1497. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000022004061800002WP 2004 6 18 ASAA0480221 120040402A53219936651515 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND PASSENGER COMPARTMENT, FLOOR PANEL AT FS 1079 LBL 22 TO RBL 22 IS DELAMINATED AND HAS CORRODED/BROKEN INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000052004061800005NM 2004 6 18 ASAA0480378 120040510A5320991015176 CUSP WEB DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK FOUND MAIN CABIN RIGHT SIDE CUSP WEB CORRODED BETWEEN STATION 845 AND 864. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000122004061800012WP 2004 6 18 ASAA0480205 120040402A531059128521 DOOR FRAME DOUG DC9 DC983 3022083WP NLG DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND HV CHECK, FOUND FASTENER HOLE CRACKED ON LEFT SIDE OF FUSELAGE ABOVE NOSE WHEEL WELL DOOR CUT OUT AT STATION 47. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01. (M) 2L72 4F RTA6WE 20040618000152004061800015NM 2004 6 18 ASAA0480375 120040510A5321993663913 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND OVERWING AREA FLOOR PANEL HAS 2 CRACKS ON ATTACH STRIP. REPAIR IAW MM. (M) 2L72 4F RT 20040618000162004061800016NM 2004 6 18 ASAA0480374 120040510A53219936639501 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND OVERWING AREA FLOOR PANEL HAS CRACKED ATTACH STRIP. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000172004061800017WP 2004 6 18 ASAA0480224 120040402A5320364213501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND CAPTAINS YOKE FLOOR MOUNT COVER MISSING FASTENERS. REMOVED CAPTAINS FLOOR PANEL, ORDERED AND INSTALLED A NEW FLOOR PANEL IAW MD80 SRM 53-70-01. (M) 2L72 4F RTA6WE 20040618000342004061800034WP 2004 6 18 ASAA0480263 120040404A575359304954 VANE DOUG DC9 DC983 3022083WP TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND HV CHECK, LEFT INBOARD FORE FLAP, LOWER SURFACE IS PUNCTURED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040618000442004061800044WP 2004 6 18 ASAA0480217 120040402A532199365841 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND PASSENGER COMPARTMENT FLOOR PANELS STATION 1117 TO 1174 LEFT DELAMINATED, CORE MISSING, AND MISSING INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000452004061800045WP 2004 6 18 ASAA0480215 120040402A532199365501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND DELAMINATED AT SEVERAL PLACES AROUND INSERT HOLES AND CABIN FLOOR PANEL NR 9. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040618000462004061800046WP 2004 6 18 ASAA0480355 120040423A5320993653573 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED AND PUNCTURED STATION 218 LBL 32. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-01. (M) 2L72 4F RTA6WE 20040618000472004061800047WP 2004 6 18 ASAA0480356 120040423A5321993663913 MEMBRANE DOUG DC9 DC983 3022083WP CABIN FLOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 DURING HV CHECK, FOUND CABIN FLOOR PANEL FROM STATION 886 TO STATION 946 IS CHAFED AND CRACKED. REMOVED DAMAGED W CHANNEL, ORDERED AND INSTALLED NEW W CHANNEL IAW MD80 SRM 51-30-8. (M) 2L72 4F RTA6WE 20040618000582004061800058NM 2004 6 18 ASAA0480387 120040510A53219957918501 FLOOR PANEL DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 DURING HV CHECK, FOUND CABIN FLOOR PANEL AT STATION 927-1003 CRACKED. REPAIR IAW SRM. (M) 2L72 4F RT 20040618000772004061800077WP 2004 6 18 DHL2004803525 120040405A5720 ANGLE DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING OUTBOARD FLAP UPPER RT PART TEE ANGLE CRACKED 1.500 AT STA XF 164.000. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-0 PG 1-2. FABRICATED FILLER (AL 7075-T6 0.063) IAW SRM 57-2-0 PG 1-2. FABRICATED DOUBLER (AL 7075-T6 0.063) IAW SRM 57-2-0 PG 1-2. CLEANED, TREATED AND PRIMED FILLER, DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040618000852004061800085NM 2004 6 18 SWAA041699 120040616A3350100031 SIGN BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FWD AISLE CABIN OVERHEAD EMERGENY EXIT SIGN CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040618000942004061800094SO 2004 6 18 CHQA000495 120040519A3350 BULB EMB 145 EMB145MR 3260213SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11974 145203 MAIN DOOR EMERGENCY LIGHT OUT ON HANDRAIL. REMOVED AND REPLACED BULB PER ERJ 145 MM 33-50-10. OPERATIONAL CHECK SATISFACTORY PER ERJ 145 MM 33-50-00. 2L72 4T RTT00011AT 20040618000962004061800096NM 2004 6 18 801DM0013 120040525A335020131A BATTERY PACK BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05801DM 26240 EMERGENCY LIGHT BATTERY PACK AT STA 1681 IS BAD. REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 1681 AND OPS CHECKED PER MM 33-51-00. 2L72 4F RTA2NM 20040618001012004061800101GL 2004 6 18 CHQA000493 220040518A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ODOR A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11291SK 145486 CAE311900 DURING T/O ROLL PILOT NOTICED FUNNY ODOR IN CABIN SIMILAR TO OIL ODOR. A FEW SECONDS INTO CLIMBOUT, LAV SMOKE DETECTOR SOUNDED. A/C RETURNED TO FIELD AT PHL AND LANDED WITHOUT INCIDENT. MX INSPECTED A/C, PERFORMED GROUND RUNS AT ALL POWER SETTINGS WITH BLEEDS & PACKS ON. NO INDICATIONS OF SMOKE OR LAV SMOKE INDICATION. REMOVED AND REPLACED LAV SMOKE DETECTOR. A/C FERRIED TO IND FOR FURTHER EVALUATION. A THOROUGH INVESTIGATION AND CHECKS WERE PERFORMED ON THE A/C AND ENGINES, AND NR 1 ENGINE WAS CONFIRMED TO BE CAUSING THE ODORS. NR 1 ENGINE WAS REMOVED AND REPLACED PER TASK CARD CE720001. ENGINE RUNS ACCOMPLISHED, NO LEAKS AND NO ODORS NOTED IN CABIN. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040618001022004061800102CE 2004 6 18 61470 120040516A3297 WIRE BEECH 1900 1900D 1154162CE MLG CHAFED A AMWAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 CE07174YV UE174 ON TAXI FROM GATE THE LANDING GEAR WARNING HORN AND THE GEAR INTRANSIT LIGHT ACTIVATED. CREW STOP TAXI AND SHUT DOWN AIRCRAFT WITH NO FURTHER INCIDENT. REPAIRED CHAFED WIRE D40A22 TO A406K5. 2L72 4T RTA24CE 20040618001112004061800111EA 2004 6 18 ASOA04341 120040510A3350362624 BULB BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27867AS 7463 DURING A GROUND INSPECTION, THE FIRST FIVE SEGMENTS OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040618001132004061800113EA 2004 6 18 ASOA04340 120040510A5210601R3190169 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MAIN PAX BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27835AS 7258 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040618001172004061800117EU 2004 6 18 ASOA04358 120040429A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK, THE LT OB SEAT TRACK WAS FOUND CORRODED ON THE INNER FLANGE AROUND THE CLIP NUT HOLES BETWEEN FRAMES 14 AND 17. MAINTENANCE REPAIRED THE CORRODED SEAT TRACK IAW SRM 530000, FIG 434. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040618001182004061800118EA 2004 6 18 ASOA04361 120040515A274170744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE TRIM SYS INOPERATIVE A ASOAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO27720AS1778 1778 10115 DURING CLIMBOUT, A STABILIZER TRIM FAILURE WAS EXPERIENCED FOLLOWED BY MACH TRIM FAILURE AND AUTO PILOT TRIP FUNCTION INOPERATIVE. THE CAPTAIN REPORTED THAT THE FORCES ON THE CONTROLS WERE MANAGEABLE. CREW COMPLIED WITH THE QRH TO RESET THE SYSTEM, BUT THE ATTEMPT WAS UNSUCCESSFUL. EMERGENCY EQUIPMENT WAS REQUESTED TO STANDBY AS A PRECAUTION, AND A SAFE LANDING WAS PERFORMED. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM MOTOR CONTROL UNIT. OPERATIONAL CHECKS, GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040618001212004061800121NE 2004 6 18 GTIA040464 220040513A7200JT8D219 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 1 INOPERATIVE A GTIAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 GL23815NK 49415 AFTER START NR 1 OIL QUANTITY FELL TO ZERO. FOLLOWED QRH PROCEDURES, OIL PRESS FELL TO 35 PSI AND FLUCTUATED, SHUT DOWN NR 1 ENGINE. 2L72 4F4 FRTA6WE E2EA 20040618001222004061800122WP 2004 6 18 GTIA040483 120040502A5320 ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE INTERCOSTAL CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 AFT FUSELAGE COMPARTMENT STA 1483 CANT, LONG 21L, INTERCOASTAL IS CRACKED. FOUND SUPPORT ANGLE IB AFT SIDE OF INTERCOASTAL CRACKED ALSO. REMOVED CRACKED INTERCOASTAL (T) ANGLE. REMOVED CRACKED SUPPORT ANGLE. FORMED NEW INTERCOASTAL (T) ANGLE. DRILLED AND LOCATED NEW INTERCOASTAL SUPPORT. INSTALLED NEW (T) ANGLE AND INTERCOASTAL SUPPORT ANGLE. 2L72 4F4 FRTA6WE E2EA 20040621000022004062100002NM 2004 6 21 ASAA0480272 120040413A14200105606 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01982AS 53473 DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 3. RECONNECTED WIRE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040621000042004062100004WP 2004 6 21 ASAA0480251 120040404A532099305389 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND CORROSION ON CUSP WEB STATION 598 TO 636 STRINGER 18L. REMOVED DAMAGED CUSP WEB, ORDER AND INSTALLED NEW CUSP WEB IAW MD80 SRM 51-30-5. (M) 2L72 4F RTA6WE 20040621000072004062100007WP 2004 6 21 ASAA0480244 120040404A53475930566509 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 FOUND SEAT TRACK AT STATION 1163 LBL 44 HAS INTERGRANULAR CORROSION. REMOVED DAMAGED SEAT TRACK FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK IAW 51-10-4, 51-30-5, MD80 SRM. (M) 2L72 4F RTA6WE 20040621000162004062100016WP 2004 6 21 ASAA0480238 120040404A5320993053877 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND MID CARGO COMPARTMENT STATION 636-938 AT 18R CEILNG CUSP MEMBRANE IS CORRODED. REMOVED DAMAGED CUSP WEB, ORDERED AND INSTALLED NEW CUSP WEB IAW MD80 SRM 51-30-5. (M) 2L72 4F RTA6WE 20040621000302004062100030WP 2004 6 21 ASAA0480252 120040404A53109919605501 DOUBLER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND DOUBLER ATTACHED TO STATION 1271 CORRODED LONGERON 29R TO 29L. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-03. (M) 2L72 4F RTA6WE 20040621000332004062100033WP 2004 6 21 ASAA0480233 120040404A5347593056675 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HV CHECK, PASSENGER CABIN SEAT TRACK AT STATION 1168-1220 IS CORRODED. REMOVED CORROSION AND INSTALLED RPR SECTION AND SPLICE PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000382004062100038WP 2004 6 21 ASAA0480331 120040419A530099365471 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AND HAS CRACKED EDGE AT FS 160-180. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000402004062100040WP 2004 6 21 ASAA0480333 120040419A532199365521 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS SEVERAL CRACKED AND MISSING INSERTS. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000462004062100046WP 2004 6 21 ASAA0480367 120040503A53139912246503 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING C-CHECK, FOUND RIGHT STATION 1380 LONGERON 17-19R FRAME CHAFED UNDER TUBE CLAMP. REPAIR IAW SRM. (M) 2L72 4F A6WE 20040621000472004062100047WP 2004 6 21 ASAA0480369 120040503A533039286495 MOUNT DOUG DC9 DC982 3022082WP ANTENNA CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING C-CHECK, FOUND .5 INCH CRACK ON MOUNT AREA OF FEED ASSEMBLY RIGHT SIDE OF TAIL CONE. REPAIR IAW EA. (M) 2L72 4F A6WE 20040621000482004062100048WP 2004 6 21 ASAA0480366 120040503A531099365811 BEAM DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING C-CHECK, FOUND AFT CARGO LOWER DOOR BEAM CORRODED AROUND FORWARD DOOR STOP FITTINGS. REPAIR IAW EA. (M) 2L72 4F A6WE 20040621000512004062100051NM 2004 6 21 VNAA0406012 120040616A24301180001 GCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05426JS212042220 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND ENGINE CONTROL UNIT FAIL INDICATION AND ABORTED TAKEOFF. ON TAXI BACK, THE CREW RECEIVED A DC GENERATOR FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE GENERATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000542004062100054EA 2004 6 21 VNAA0405013 120040522A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT ILLUMINATED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL05250PS 7929 THE CREW REPORTED RECEIVING A RT EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICATION WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE C. 2L72 4F4 FRTA21EA E15NE 20040621000702004062100070NM 2004 6 21 SWAA041714 120040617A5312BAC1514 STIFFENER BOEING737 7373Q8 1384670NM BULKHEAD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REMOVED STIFFENER PER SRM. 2L72 4F RTA16WE 20040621000772004062100077WP 2004 6 21 MWEA040080 120040519A53119911838443 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 CANTED FRAME 1388 TOP WEB CRACKED OUTBOARD OF VERTICAL SPAR TANG RIGHT SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040621000782004062100078EA 2004 6 21 04115622 120040423A79327225363 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LOW OIL LEVEL INTERMITTENT A VTZABE EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 EA27622BR 7187 DURING DESCENT OF FLIGHT 7688 CREW REPORTED A LEFT HAND ENGINE FAILURE ON APPROACH. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. THE LOW LEVEL OIL SENSOR WAS FOUND TO GIVE FALSE INDICATIONS AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040621000862004062100086EA 2004 6 21 COMA0460330 120040519A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01973CA 7146 CARGO FLOORBEAM CAP AT LBL 27 CORRODED THRU AT NUT PLATE FROM FS 589 TO 609. REMOVED AND REPLACED CARGO FLOORBEAM CAP AT LBL 27 WITH NEW SERVICEABLE CAP (P/N 601R35031-1) IAW CRJ SRM 51-42-13 AND CRJ SRM 51-42-21. 2L72 4F RTA21EA 20040621000932004062100093WP 2004 6 21 CALA0400527 120040609A3350AD4002P BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2772822 49482 INSPECTION FOUND THE FLIGHT DECK AND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. THE EMERGENCY LIGHT BATTERIES IN FORWARD CEILING WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F A6WE 20040621000962004062100096NM 2004 6 21 373PA0049 120040520A2150 WARNING LIGHT BOEING737 7373Y0 1384671NM LT AC PACK ILLUMINATED A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05373PA 23749 ON TAKEOFF ROLL, LEFT PACK TRIP OFF LIGHT CAME ON. INSPECTED LEFT PACK BAY, NO DEFECTS NOTED. RAN BOTH ENGINES, PACKS ON, PACKS OPERATED NORMAL PER MM 21-40-00. 2L72 4F RTA16WE 20040621001042004062100104EA 2004 6 21 COMA0460329 120040520A27507455001 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01816CA9386 7398 FLIGHT 5578 FLAPS FAILED ON APPROACH. REPLACED THE FLAP CONTROL LEVER. 2L72 4F RTA21EA 20040621001072004062100107NM 2004 6 21 CALA0400529 120040610A3231 LINKAGE BOEING737 737524 1384721NM RT NLG DOOR BROKEN A CALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW2717619 27332 A LOUD NOISE WAS HEARD AND VIBRATION WAS FELT COMING FROM THE NOSE GEAR WHEEL WELL AREA AFTER GEAR RETRACTION LEAVING JAX. THE NOISE STOPPED WHEN THE GEAR WAS LOWERED FOR A RETURN TO JAX. MAINTENANCE FOUND RT NOSE GEAR DOOR LOWER LINKAGE BROKEN. THE LINKAGE WAS REMOVED AND REPLACED IAW MM 32-22-11. THE DOOR WAS ADJUSTED IAW MM 32-33-61 AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040621001112004062100111NM 2004 6 21 CALA0400533 120040612A5320BAC1496444 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713248 28808 INSPECTION FOUND Z-CHANNEL CORRODED AT STA 500A-500I IN RT FORWARD CARGO AREA. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040621001122004062100112NM 2004 6 21 CALA0400534 120040613A5312143A948535 ANGLE BOEING737 737824 13844BZNM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713248 28808 INSPECTION FOUND LOWER ANGLE AT AFT BULKHEAD OF FORWARD CARGO COMPARTMENT CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040621001172004062100117EA 2004 6 21 COMA0460326 120040521A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA 7027 SURFACE CORROSION FOUND ON CARGO FLOORBEAM CAP LBL 27 AT FS 600 AROUND OUTBOARD NUT PLATE. REMOVED FLOORBEAM CAP LBL 27 AT FS 600 AND INSTALL NEW FLOORBEAM CAP IAW CRJ SRM 51-40-11, 51-41-02, 51-45-00, 51-42-13, 51-42-21, 51-42-06, 51-42-34. 2L72 4F RTA21EA 20040621001572004062100157WP 2004 6 21 ASMF200406008 120040609A217017946081 WATER SEPARATOR DOUG DC9 DC987 3022087WP CABIN AIR FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23216AM107702272 49586 DURING TRANSIT CHECK, WATER WAS FOUND IN THE MIDDLE OF PASSENGERS CABIN CEILING. THE WATER LEAK WAS DETECTED BETWEEN CUSHIONS AND AIR CONDITIONING DUCT IN THE CEILING, THE EMERGENCY LOCATOR ANTENNA WAS SEALED IN THE STATIONS Y937 AND Y980 IN THE UPPER FUSELAGE. DURING OVERNIGHT SERVICE, AIR CONDITIONING DUCTS WERE CHECKED BY LEAKS IAW MM 21-20-00, PRESSURIZATION TEST WAS PERFORMED IAW MM 21-00-00, LT AND RT OVERRIDE ANTI ICE VALVES WERE REPLACED IAW MM 21-20-04, WATER SEPARATORS WERE REPLACED IAW MM 21-20-02 AND OVERRIDE ANTI ICE VALVES SENSITIVE LINES WERE REPLACED IAW MM 21-20-04, ALL CORRECT. 2L72 4F RTA6WE 20040621001942004062100194NM 2004 6 21 QXEA200400353 120040520A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - SEAT TRACK 15 NEEDS REPLACED FOR CORROSION PITS. REPLACED IAW HORIZON AIR EA 6-53-356. 2H72 4T RTA13NM 20040621001962004062100196NM 2004 6 21 QXEA200400345 120040521A5410 TRUSS DHAV DHC8 DHC8202 2809007NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - NR 1 ENGINE INBOARD LOWER TRUSS CHAFED 6 X .001 INCH ADJACENT TO FUEL FLOW TRANSMITTER. REPAIRED IAW RD 8-54-036. 2H72 4T RTA13NM 20040621001982004062100198EU 2004 6 21 AWXA200400509 120040507A5753D57571601270 SKIN AIRBUS320 A320231 3930325EU TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK FOUND A DISBOND AREA ON THE LT OUTBOARD FLAP UPPER SKIN AT INBOARD END RIB 3 + 2 INCH. MAINTENANCE CUTOUT DAMAGED SKIN ON UPPER LT OUTBOARD FLAP AT RIB 3; FABRICATED A DOUBLER AND REPAIR CORE; BONDED REPAIR PARTS TO FLAP IAW AWA ER 26-5128-02218-SS1. 2L72 4F RTA28NM 20040621002002004062100200NM 2004 6 21 AWXA200400511 120040502A532069353654 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .5 INCH CRACK IN CABIN FLOOR ATTACH ANGLE AT SHEAR WEB BS 384 TO BS 309, BL 0, WL 208. MAINTENANCE REMOVED CRACKED ATTACH ANGLE AT SHEAR WEB BS 384 TO BS 309, BL 0, WL 208; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7 & 8. 2L72 4F RTA16WE 20040621002102004062100210WP 2004 6 21 IXXA0400065S 120040328A5320 FLANGE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 C-CHECK INSP MAIN CARGO COMP WEB, BEAM LOWER FLANGE CORRODED STA 960 RBL 58 - 64. REMOVED FASTENERS, CORROSION FOUND OUT OF LIMITS. REMOVED DAMAGED CORROSION AREA & SECTION OF FLANGE. FABBED FILLER & DOUBLER. PERFORMED NDT INSP, FABBED EXTERNAL REPAIR DOUBER, 2 INTERNAL REPAIR DOUBLER, FILLER, 03 SHIMS, OTHER SHIM FROM AN INTERNAL DOUBLER & 2 Z-REINFORCEMENTS. CLEANED, TREATED AND PRIMED REPAIR PARTS EXCEPT 2 Z-REINFORCEMENT STEEL, APPLIED PRC SEALANT ON FAYING SURFACES, INSTALLED FILLER, DOUBLER FOR FLANGE AREA. INSTALLED EXTERNAL, INTERNAL REPAIR DOUBLERS, FILLER, SHIMS & 2 Z-REINFORCEMENTS. REPAIRED RT FUSELAGE FITTING P/N 3647117 AT PANEL PRIOR ACCOMPLISHING WEB & FLOORBEAM REPAIR. 2L74 4F RT4A25 20040622000022004062200002NM 2004 6 22 QXEA200400324 120040517A3230483023 SEQUENCE VALVE BOMBDRDHC8 DHC8401 1390041NM NLG FAULTY A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09408QX6451 4050 BOI - FLIGHT 2401 - ON DEPARTURE AND AFTER GEAR RETRACTION, THE AMBER NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR SOLENOID SEQUENCE VALVE. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040622000102004062200010WP 2004 6 22 ASAA0480204 120040402A53205956879501 COVER DOUG DC9 DC983 3022083WP TORQUE BOX CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND TORQUE BOX COVER TAB CRACKED AT FASTENER HOLE AT STATION 200, STRINGER 10L. REMOVED DAMAGE, INSTALLED DOUBELR PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040622000132004062200013WP 2004 6 22 ASAA0480297 120040420A532199365521 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-156 LBL 22 TO RBL 14 DELAMINATING. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000282004062200028WP 2004 6 22 ASAA0480302 120040420A532199365471 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD STATION 160-180 RBL 08 TO RBL 44 FIBERGLASS TEARING OFF. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000372004062200037WP 2004 6 22 ASAA0480202 120040402A53219957918502 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL IS CRACKED AND HAS BARE METAL AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000392004062200039NM 2004 6 22 ASAA0410266 120040516A5315BAC1505100246 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM. (M) 2L72 4F A16WE 20040622000472004062200047WP 2004 6 22 ASAA0480301 120040420A532199365531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 44 TO RBL 22 FIBERGLASS TORN OFF. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000592004062200059WP 2004 6 22 IXXA0400030S 120040303A5753 HINGE FITTING DOUG DC8 DC873F 302199FWP RT WING TE FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD FLAP HINGE SUPPORT FITTING CRACKED 4 INCHES STA XW 97-906. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REAIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B, INSTALLED NEW FITTING IAW DC8 SRM 51-3-0 PAGE 1 AND DC8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20040622000602004062200060WP 2004 6 22 IXXA0400031S 120040225A5753 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL9191029104 46003 DURING ROUTINE C-CHECK INSPECTION FOUND RT WING INBD FLAP UPPER PANEL HAS INTERM REPAIR, STA XW 28.000-XW 86.000 MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 2 PAGE 2. REMOVED INTERM REPAIR IAW DC8 SRM 51-1-21 PAGE 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B, FABRICATED NEW SKIN (202473 0.040) IAW DC8 SRM 57-7-1 PAGE 2, FIG 1. CLEANED, TREATED AND PRIMED NEW SKIN INTERIOR IAW DC8 SRM 51-1-8B, APPLIED PRC SEALANT OF FAYING SURFACE IAW DC8 SRM 51-1-15 PAGE 1. INSTALLED NEW SKIN WITH FASTENERS IAW DC8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20040622000642004062200064WP 2004 6 22 IXXA0400035S 120040212A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK FOUND FUSELAGE NOSE FWD PASSENGER DOOR UPPER FWD CORNER HAS INTERIM REPAIR STATION 25.0001-9L. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0, PAGE 2-5. TR 53-182. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. MEASURED CRACK 5.250 INCH, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 15 TR 53-182, CONTINUED REPAIR, TIN-LIT 04-00016. MARCH 05, 2004 AND TIN-LIT 04 00017H MARCH 08, 2004 WITH FORM 8110-3. REMOVED CRACKED SKIN IAW DC8 SRM 53-2-0 FIG 15 FABRICATED DOUBLER, TRIPLER AND FILLER IAW DC8 SRM 53-2-0 FIG 15. CLEANED, TREATED AND PRIMED DOUBLER AND TRIPLER AND FILLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER & DOUBLER & TRIPLER IAW DC8 SRM 53-2-0 FIG 15 SRM 51-1-20D, PAGE 9, SRM 51-1-21 PAGE 1 SRM2L74 4F RT4A25 20040622000742004062200074EU 2004 6 22 AWXA200400547 120040519A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONE 221 OUT OF TOLERANCEA AWXAK NONE L NO TEST ININSP/MAINT 1 WP28629AW4103610 076 PHX - EEL - DURING 4-DAY CHECK THE LT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040622000782004062200078NM 2004 6 22 AWXA200400551 120040421A531369412262 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND STRINGER 17 RT BETWEEN BS 887 AND BS 907. MAINTENANCE REMOVED DAMAGE ON STRINGER 17 RT FROM BS 887 TO BS 907; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11 FIG 1 PG 1-6. 2L72 4F RTA16WE 20040622000852004062200085NM 2004 6 22 AWXA200400527 120040429A531065458053 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND IN ATTACH ANGLE (SHEAR TIE) AT BS 727D, BETWEEN STR 13 AND STR 14 RT. MAINTENANCE CUT OUT DAMAGE IN SHEAR TIE AT BS 727D, BETWEEN STR 13 AND STR 14 RT; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 205. 2L72 4F RTA16WE 20040622000932004062200093NM 2004 6 22 SWAA041717 120040618A5754 SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 628 24572 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT UPPER T/E CORNER DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20040622000992004062200099NM 2004 6 22 SWAA041722 120040619A53126516300 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 6 TO RBL 10, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040622001022004062200102NM 2004 6 22 SWAA041725 120040620A5751654476116 PCU BOEING737 7372H4 138448CNM LT WHEEL WELL LEAKING A SWAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW29082SW 22731 EXCESSIVE PLAY IN THE AILERONS. REMOVED AND REPLACED A-SYSTEM AILERON PCU PER MM. 2L72 4F A16WE 20040622001042004062200104NM 2004 6 22 SWAA041727 120040620A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 500B, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040622001052004062200105EA 2004 6 22 QXEA200400355 120040525A2910AE71357812 HYDRAULIC LINE CNDAIRCL600 CL6002C10 1390015EA ZONE 700 CRACKED A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09607QX6616 10024 LAX - FLIGHT 2556 - THE FLIGHT WAS DIVERTED WHEN AFTER TAKEOFF THE CREW RECEIVED A GEAR DISAGREE LIGHT AND THE NUMBER 3 HYDRAULIC SYSTEM FAILED. THE NUMBER 3 HYDRAULIC FLUID QUANTITY WENT TO ZERO. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR RETRACT ACTUATOR LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040622001062004062200106NM 2004 6 22 AWXA200400566 120040524A30408300005602 CONTROLLER BOEING737 7373G7 1384595NM WINDOW HEAT MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28322AW5021726453 25400 PHX - AIR TURNBACK - ON CLIMBOUT OF PHX EN ROUTE FOR DEN THE CAPTAINS SLIDING WINDOW CRACKED, ELECTRICAL ARCING NOTED IN CORNER OF WINDOW, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SLIDING WINDOW IAW T/C R1B56003, AND WINDOW HEAT CONTROL UNIT M322 IAW BMM 30-41-11, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF WINDOW HEAT CONTROL UNIT S/N 2920 CONFIRMED FAILURE OF UNIT FOR OUTPUT TEST. TEARDOWN OF UNIT FOUND BAD COLD SOLDER JOINT ON PC BOARD A1, JOINT WAS RE-SOLDERED AND UNIT TESTED GOOD IAW CMM 30-40-03, REV. 6. 2L72 4F RTA16WE 20040622001072004062200107EU 2004 6 22 AWXA200400574 120040525A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONE 241 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW2021010917 053 DEN - EEL - DURING 4 DAY CHECK THE EMERGENCY LIGHT SYSTEM FAILED TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040622001082004062200108 2004 6 22 P5CA0401095 420040523A3461 CDU BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL COCKPIT INOPERATIVE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23453PA 30811 CAPTAINS FMC CDU INOPERATIVE. SWAPPED CAPTAINS CDU WITH CENTER CDU, CAPTAINS CDU OPERATIONAL CHECK OK, AS PER MM 34-61-00. CENTER CDU PLACED ON DEFERRAL PER MEL 34-62-2-1. 2L74 4F4 FRTA20WE E23EA 20040622001092004062200109SO 2004 6 22 CHQA000505 120040611A32503085701003 MANIFOLD EMB 135 EMB135LR 3260305SO NLG STEERING MALFUNCTIONED A CHQAO OTHER O OTHER LDLANDING 1 GL11843 2353 145599 UPON LANDING INTO DFW FROM FLIGHT 6490, AIRCRAFT WAS PULLING TO THE RIGHT AND THERE WAS NO LEFT RUDDER RESPONSE. THE AIRCRAFT VEERED OFF RUNWAY AND WAS STUCK IN MUD. NO APPARENT DAMAGE TO THE AIRCRAFT. AFTER RECOVERING THE AIRCRAFT AND INVESTIGATING THE PROBLEM, MAINENANCE FOUND THE STEERING MANIFOLD TO BE FAULTY. REMOVED AND REPLACED STEERING MANIFOLD PER EMB 135 AMM 32-50-04. ALL WHEELS AND BRAKES WERE REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040622001102004062200110EU 2004 6 22 CX7A194J0429 120040523A2612 WARNING LIGHT SAAB SF340 340B 7860101EU RT TAILPIPE ILLUMINATED A CX7AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL03318CE 340B358 ABORTED TAKEOFF DUE TO RT TAILPIPE HOT LIGHT. 2L72 4T RTA52EU 20040622001112004062200111CE 2004 6 22 DXTA200400315 120040519A5210 SUPPORT BRACKET CESSNA560 560XL 2076702CE PAX DOOR STEP CRACKED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07697QS 5605197 DURING INSPECTION FOUND LOWER HALF OF MAIN ENTRY DOOR STEPS SUPPORT BRACKETS AND A COVER PLATE / WEB ASSEMBLY CRACKED. REPLACED BOTH SUPPORT BRACKETS, PLATE ASSEMBLY AND WEB ASSEMBLY PER CESSNA SERVICE BULLETIN 560XL-52-12. 2L72 4F RTA22CE 20040622001132004062200113EU 2004 6 22 YENA200416 120040311A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT UNSERVICEABLE A YENAK NONE L NO TEST ININSP/MAINT 1 EA15505JB15695 1173 DURING EMERGENCY LIGHT TEST, FAULT INDICATION OF LEFT EPSU UNIT. FOUND WIRE HARNESS D9299200900200 AT SEAT 3C CHAFED CAUSING FAULT DURING TEST OF THE EMERGENCY LIGHTING SYSTEM IAW 33-51-00-710-001. ITEM PLACED ON MEL UNTIL PART CAN BE REPLACED. REMOVED AND REPLACED HARNESS & LT EPSU OVERWING EXIT. 2L72 4F RTA28NM 20040622001142004062200114NM 2004 6 22 CALA0400536 120040614A335020131A BATTERY PACK BOEING757 757224 1384958NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714115 27557 THE EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE. TWO AFT BATTERY PACKS WERE REMOVED AND REPLACED AT STA 1680 IAW MM 33-51-00. OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED. 2L72 4F RTA2NM 20040622001152004062200115EA 2004 6 22 QXEA200400325 120040516A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 BOI - FORWARD CARGO COMPARTMENT SMOKE DETECTOR PROTECTIVE COVER IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040622001182004062200118NM 2004 6 22 374PA0011 120040517A5330 SKIN BOEING737 73736M 138443BNM FUSELAGE DENTED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 DENT AT RIGHT SIDE OF AIRCRAFT AT BS 312 AND STR 20. REPAIRED PER SRM 53-00-01 AND EA 53-121. 2L72 4F RTA16WE 20040622001202004062200120EU 2004 6 22 DHL2004364515 120040311A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN DECK COURIER AREA HAVE CORROSION EVIDENCE ON FLOOR PANEL SUPPORT/SEAT TRACK FROM APPROX FR 14 TO FR 19 RBL 36 (MARKED). REMOVED CORROSION FROM TRACK FR 14 TO FR 19 RBL 36. MATERIAL LOSS .025 FOUND OUT OF LIMITS AS PER A-300 SRM 53-10-00, FIG 612 AND SRM 51-40-11. REMOVED SEAT TRACK FROM FR 14 TO FR 19 RBL 36 AS PER A-300 SRM 51-30-30. MATERIAL USED 60-22457 PO 23236312. TREATED AND PRIMED AND POLYWHITE TRACK SECTION AS PER A-300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION SECTION FROM FR 14 TO FR 19 RBL 36 IAW A-300 SRM 51-30-30. 2L72 4F RTA35EU 20040622001212004062200121WP 2004 6 22 DHL2004803534 120040417A573097510822 PANEL DOUG DC8 DC873 302199CWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RT WING L/E SLANT PANEL UPPER CAP CORRODED STA XFS 57.500 - XFS 82.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. REMOVED CORRODED SLANT PANEL UPPER CAP IAW SRM 51-1-21 PG 1. CLEANED AND APPLIED POLYURETHANE COATING ON AREA IAW SRM 51-1-12 PG 11-12. INSTALLED BUSHING IAW FAX DATED 04-12-2004, SRM 51-1-25. INSTALLED NEW SLANT PANEL UPPER CAP IAW SRM 57-2-1 FIG 37, PAGES 135-136, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, FAX DATED 04-12-2004, ROD SKETCH 04-04-08.001 DRA 03013. 2L74 4F RT4A25 20040622001222004062200122WP 2004 6 22 DHL2004803549 120040505A5320 ANGLE DOUG DC8 DC873 302199CWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 MAIN CARGO COMPT PRESSURE PANEL ATTACH ANGLE CORRODED AT STA 857.125 RBL 29 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 51-2-1 PG 8-14. REMOVED CORROSION FROM PRESSURE PANEL ATTACH ANGLE AT STA 857.125 RBL 29 IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2M. CUT OUT DAMAGED SECTION IAW DC8 SRM 51-2-1 PG 8. FABRICATED FILLER (7075-T6 0.125) AND REPAIR ANGLE (7075-T651) IAW DC8 SRM 51-2-1 PG 8-14. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED FILLER AND REPAIR ANGLE IAW DC8 SRM 51-2-1 PG 8-14, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622001272004062200127WP 2004 6 22 DHL2004803533 120040402A5730 ACCESS DOOR DOUG DC8 DC873 302199CWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RT INNER WING AFT TOP PANEL PLATING ACCESS DOOR (505F) INTERNAL DOUBLER TWO CRACKS DAMAGE (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 36. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. FABRICATED INTERNAL DOUBLER (7075-T6 0.063) IAW DC8 SRM 57-2-1 PG 133-134 FIG 36. FABRICATED EXTERNAL DOUBLER (7075-T6 0.160) IAW DC8 SRM 57-2-1 PG 133-134 FIG 36. CLEANED, TREATED AND APPLIED YELLOW TOP COATING TO INTERNAL DOUBLER IAW DC8 SRM 51-1-12 PG 7, 21. INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW DC8 SRM 57-2-1 PG 133-134 FIG 36 DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040622001282004062200128WP 2004 6 22 DHL2004803510 120040319A5531 FRAME DOUG DC8 DC873 302199CWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 VERTICAL STABILIZER L/E FRAME CRACKED 2.000 AT FS 98.000 (LT SIDE). PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622001332004062200133NM 2004 6 22 DHL2004783010 120040518A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 HOLE FOUND IN AIRCRAFT BETWEEN STATION 1050 & 1070 BETWEEN STRINGERS S-24 & S-25 LEFT SIDE AIRCRAFT. CUT OUT DAMAGE AREA, FABRICATED DOUBLER, & INSTALLED AS PER 727 SRM 57-30-01. PERFORMED PRESSURE CHECK IAW M/M 21-31-0. CHECK OK, MAJOR REPAIR. 2L73 4F A3WE 20040622001342004062200134NM 2004 6 22 DHL2004750041 120040526A3350 LENS BOEING727 7272M7 138407SNM EMERGENCY EXIT CRACKED A DHLAO OTHER L NO TEST NRNOT REPORTED 1 SO01750DH 21951 DURING FLIGHT THE EMERGENCY EXIT SIGN OVER THE FORWARD ENTRY DOOR FELL TO THE FLOOR AND CRACKED ITS LENS. REMOVED AND REPLACED ENTRY OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECKED GOOD IAW M/M 33-50-01. 2L73 4F A3WE 20040622001352004062200135EU 2004 6 22 DHL2004366002 120040520A3260BED00101 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01366DH 249 REJECTED T/O, RT MAIN GEAR UNSAFE LIGHT ON FWD PANEL ILLUMINATED & GREEN SAFE LIGHT WENT OUT. INDICATIONS NORMAL BEFORE LEAVING RUNWAY. USING SYSTEM 2 WEIGHT 343700, OAT 21C, PA 706, BRAKE TEMP 270 C. SYSTEM 2 GEAR INDICATOR DEFERRED. MEL 32-31-01-2. DMI CONTROL 16651. REMOVED AND REPLACED PROXIMITY DETECTION MODULE 54GB PER M/M 32-61-12. SYSTEM OPS CHECKED GOOD. THIS CLEARS DMI 16651 - PLACARD REMOVED. MX CONTROL NOTIFIED. 2L72 4F RTA35EU 20040622001382004062200138EU 2004 6 22 DHL2004364513 120040313A531310012599 STRINGER AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, LOWER FWD CARGO COMPT FR 37L & STR 45 HAS CORROSION ON STRINGER UNDER FLOOR AT BELLY SKIN. REMOVED CORROSION AT FWD CARGO FR 37L AND STR 45L IAW SRM 51-40-11. FOUND TO BE OUT OF LIMITS IAW A-300 SRM 53-10-10 PG 618. CUT OUT DAMAGE AREA IN LOWER FWD CARGO COMP FR 37L & STR 45 IAW A-300 SRM 53-10-10. INSPECTED NDT HFEC IAW A-300 NDT MANUAL 51-31-05, STRINGER CUT OUT AT STR 45, FR 37L, NO CRACK INDICATIONS NOTED. FABRICATED REPAIR PARTS IAW A-300 SRM 53-10-10. TREAT AND PRIMED PARTS AND AREA IAW A-300 SRM 51-40-12. OK TO INSTALL REPAIR PART IAW A-300 SRM 53-10-10. INSTALLED REPAIR LOWER FWD CARGO COMP FR 37L AND STR 45 IAW A-300 SRM 53-10-10. TOUCH UP FUS PAINT PER A-300 SRM 51-40-12. 2L72 4F RTA35EU 20040622001412004062200141NM 2004 6 22 P5CA0401093 120040516A2840 WARNING LIGHT BOEING747 74747UF 1384949NM COCKPIT ILLUMINATED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23496MC 29257 STATUS MESSAGE FUEL JET-B. DEFERRED PER MEL 28-31-4-1, PLACARDS INSTALLED. 2L74 4F RT1384945 20040622001642004062200164EA 2004 6 22 ASOA04392 120040530A3350363782 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27925EV 7831 DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHT POWER CABLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT POWER STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040622001652004062200165EA 2004 6 22 ASOA04331 120040506A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27882AS 7503 DURING A GROUND INSPECTION, THE RT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040622001662004062200166EU 2004 6 22 ASOA04390 120040528A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27634AS24280387 370 DURING AN A-CHECK, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT 73WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20040622001672004062200167EA 2004 6 22 ASOA04332 120040505A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO600530072. 2L72 4F4 FRTA21EA E15NE 20040622001682004062200168EA 2004 6 22 ASOA04335 120040506A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE LT AND RT SIDE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT SIDE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600530105. 2L72 4F4 FRTA21EA E15NE 20040622001702004062200170EA 2004 6 22 ASOA04381 120040525A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK, THE IB CLIPS AT FS280, LBL9 AND RBL 9 IN THE FORWARD AVIONICS EQUIPMENT BAY WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIPS AT FS280, LBL9 AND RBL9 IN THE FORWARD AVIONICS EQUIPMENT BAY. 2L72 4F4 FRTA21EA E15NE 20040622001732004062200173EA 2004 6 22 ASOA04343 120040505A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040622001772004062200177EA 2004 6 22 ASOA04345 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE IB CLIPS AT THE FLOOR SUPPORT, FS484, LBL27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL 27 AND RBL 27 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20040622001812004062200181EA 2004 6 22 ASOA04344 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE CLIPS AT FS280, LBL9 AND RBL9 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL9 AND RBL 9 ON THE LT AND RT SIDES IAW SRM51-00. 2L72 4F4 FRTA21EA E15NE 20040622001832004062200183NE 2004 6 22 ASOA04376 220040521A72616087T04P06 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE CLOGGED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27908EV4957 7654 873409 DURING CRUISE, AT APPROXIMATELY 35,000 FEET THE CREW RECEIVED A RED RT ENGINE OIL PRESSURE MESSAGE AND ASSOCIATED AURAL WARNING. OIL PRESSURE FLUCTUATED BETWEEN THE HIGH TEENS AND LOW TWENTIES. THE CREW REDUCED THE RT ENGINE TO IDLE THROUGH DESCENT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT DIVERTED, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT LUB AND SCAVENGER PUMP. THE (S) B-SUMP REGULATOR WAS ALSO REMOVED AND REPLACED FOR PREVENTATIVE MAINTENANCE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040622001842004062200184EA 2004 6 22 ASOA04374 120040514A5210601R3198055 STEP BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 7276 DURING C-CHECK, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. 2L72 4F4 FRTA21EA E15NE 20040622001852004062200185EU 2004 6 22 ASOA04373 120040307A5310 CREASE BEAM AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK INSPECTION, THE CREASE BEAM PLATE AFT OF FRAME 39 ON THE LT SIDE WAS FOUND BENT AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED AND BENT CREASE BEAM PLATE IAW SRM 512503. AIRCRAFT WAS RELEASED FOR C-CHECK ON MARCH 21, 2004. 2H72 4T4 TRT E20NE 20040622001862004062200186EU 2004 6 22 ASOA04367 120040307A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK, THE LT AND RT SIDE FLOOR SUPPORT WAS FOUND CORRODED BEYOND LIMITS AFT OF FRAME 39. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR SUPPORTS IAW SRM 51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2H72 4T4 TRT E20NE 20040622001872004062200187EA 2004 6 22 ASOA04386 120040526A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK, THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 IAW EO 600530098. 2L72 4F4 FRTA21EA E15NE 20040622001882004062200188EA 2004 6 22 ASOA04385 120040526A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES ON THE LT AND RT SIDES IAW EO 600-53-0105. 2L72 4F4 FRTA21EA E15NE 20040622001892004062200189EU 2004 6 22 ASOA04372 120040310A3350 SOCKET AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27640AS21853 405 DURING C-CHECK, THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR WAS FOUND TO HAVE A DAMAGED AND CORRODED SOCKET. MAINTENANCE REMOVED AND REPLACED THE DAMAGED AND CORRODED EXTERNAL EMERGENCY LIGHT ASSY. 2H72 4T4 TRT E20NE 20040622001902004062200190EU 2004 6 22 ASOA04375 120040520A33507012210 LAMP AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS 654 362 DURING AN A-CHECK, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20040622001912004062200191WP 2004 6 22 GTIA040476 120040504A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 RT OB FLOORBOARD PANEL STA 1003-1079 RIVETS PULLED AND PANEL DELAMINATED, SPACER MISSING. FABRICATED REPLACEMENT FILLER. BONDED FILLER TO RT OB FLOOR PANEL. 2L72 4F4 FRTA6WE E2EA 20040618000832004061800083NM 2004 6 18 SWAA041697 120040616A55206561751 TORQUE TUBE BOEING737 7373A4 1384585NM TAIL WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE, AFT BUSHING AND BEARING PER MM. 2L72 4F RTA16WE 20040618000842004061800084 2004 6 18 SWAA041698 420040616A2565D31354 SLIDE BOEING737 7373T5 1384608NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040618000982004061800098CE 2004 6 18 DXTA200400309 120040511A24315518119 SENSOR CESSNA500 560CESSNA 2076750CE BATTERY TEMP MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07312QS 5600312 BATTERY TEMP INDICATOR IN FLIGHT INDICATED 180ºF VARIED SLOWLY TO 160ºF, EMEGENCY DECLARED. INDICATION DURING 2 PREVIOUS LEGS WAS 120ºF PREFLIGHT COCKPIT ROTARY BATTERY CHECKED OK, NO MASTER WARNING ON BATTERY OVERTEMP ANNUNCIATOR. REMOVED AND REPLACED BATTERY TEMP SENSOR, OPERATIONAL CHECK GOOD IAW CESSNA 560 M/M CHAPTER 24-30-01. 2L72 4F RTA22CE 20040618001142004061800114EA 2004 6 18 ASOA04336 120040507A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27849AS 7347 DURING A GROUND INSPECTION, THE RT FORWARD EXTERIOR EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERIOR EMERGENCY LIGHT LAMP AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040622001942004062200194EA 2004 6 22 ASOA04388 120040526A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A C-CHECK, THE LT AND RT CLIPS BELOW THE BOX BEAM AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT CLIPS BELOW THE BOX BEAM AS FS621. 2L72 4F4 FRTA21EA E15NE 20040622001972004062200197WP 2004 6 22 GTIA040480 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 CABIN RT IB FLOORBOARD AT STA 1250-1309 DELAMINATED SEVERAL PLACES. FAB NEW CABIN FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040622001992004062200199WP 2004 6 22 GTIA040489 120040504A5742 ATTACH ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE WING CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 CRACK ON RT LOWER ATTACH ANGLE FOR PYLON ON AFT END. TRIMMED CRACKED AREA. FABRICATED REPAIR ANGLE. FABRICATED FILLER. INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA6WE E2EA 20040622002012004062200201EA 2004 6 22 ASOA04384 120040526A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27882AS 7503 DURING A C-CHECK, THE OB CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OB CLIP AT FS 280, LBL 9 IAW SRM 51-42-21. 2L72 4F4 FRTA21EA E15NE 20040622002122004062200212NM 2004 6 22 277952 120040417A5210 DOOR BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE PAX OPEN A RYNAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 CE078878Z 21451 AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE AND THE AFT ENTRY DOOR LIGHT CAME ON IN THE COCKPIT. AIRCRAFT RETURNED TO DAYTON AND LANDED WITHOUT INCIDENT. CLOSED AND LOCKED AFT ENTRY DOOR. PRESSURIZATION OPERATIONAL CHECK NORMAL. 2L73 4F4 F A3WE E2EA 20040623000072004062300007SO 2004 6 23 UC22004F00000 120040604A3710 COUPLING PIPER PA28 PA28181 7102807SO LYC O360 IO360A1A 41514EA DRY AIR PUMP SEIZED B UC2RO OTHER O OTHER NRNOT REPORTED 1 GL1941487 C05072 2843179 DRY AIR PUMP SEIZED AND SHEARED THE PUMP DRIVE COUPLING WITHIN THE FIRST 2 HOURS OF FLIGHT. THE PUMP WILL BE SENT BACK TO THE MANUFACTURE FOR FURTHER EVALUATION. CAUSE UNKNOWN AT THIS TIME. 1L71 3O3 O 2A13 1E10 20040623000212004062300021WP 2004 6 23 GTIA040501 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 G2 GALLEY FLOOR BOARD AT STA 148 TO STA 200 (H) DELAMINATED. REMOVED FLOORBOARD. FAB NEW FLOORBOARD. INSTALLED FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040623000292004062300029WP 2004 6 23 GTIA040533 120040504A7830 ACOUSTIC LINER DOUG DC9 DC983 3022083WP THRUST REVERSER CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 NR 2 ENGINE THRUST REVERSER, SN 119702, INNER ACOUSTIC LINER HAS HOLE AT 8 OCLOCK POSITION AND 2 EA CRACKS AT 3 OCLOCK POSITION. REWELDED DAMAGED AREAS. 2L72 4F RTA6WE 20040623000302004062300030WP 2004 6 23 GTIA040535 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 LT OB SEAT TRACK FS 1231 THRU FS 1309 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACKS. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED SEAT TRACK AND SPLICES. 2L72 4F4 FRTA6WE E2EA 20040623000332004062300033EU 2004 6 23 ASOA04354A1 120040428A5320S5367800820002 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE LT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 40. OUT OF LIMITS CORROSION WAS ALSO FOUND ON THE RT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 41. MAINTENANCE REMOVED AND REPLACED THE CORRODED Z-SUPPORTS ON THE LT AND RT SIDES IAW SRM 512502 AND 512501 RESPECTIVELY. AIRCRAFT WAS RELEASED FROM C-CHECK MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040623000342004062300034EA 2004 6 23 ASOA04334 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS640 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS640, BELOW THE BOX BEAM. 2L72 4F4 FRTA21EA E15NE 20040623000362004062300036EA 2004 6 23 ASOA04378 120040522A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27838AS8280 813 7276 DURING A C-CHECK, THE FORWARD EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR1 EMERGENCY BATTERY PACK AND THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040623000432004062300043EA 2004 6 23 ASOA04348 120040514A5712601R57510466 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING C-CHECK INSPECTION, THE RT MLG BATT RIB WAS FOUND CRACKED. MAINTENANCE REPAIRED THE CRACKED MLG BATT RIB IAW EO 600570039A AND 600570042. 2L72 4F4 FRTA21EA E15NE 20040623000472004062300047EA 2004 6 23 ASOA04333 120040506A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO BAY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72 TO FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72 TO FS 589.00 IAW EO600530095. 2L72 4F4 FRTA21EA E15NE 20040623000532004062300053NM 2004 6 23 GTIA040544 120040511A5347 SEAT TRACK DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE FUSELAGE WORN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 CABIN RT MIDDLE SEAT TRACK WORN AND CORRODED STA 200-1307. MATERIAL LOSS ON RT MIDDLE SEAT TRACK STA 937-1033 OUT OF LIMITS. REMOVED RT MIDDLE SEAT TRACK. LOCATED AND DRILLED RT MIDDLE REPLACEMENT SEAT TRACK STA 937-1033 AND SPLICE. INSTALLED RTMIDDLE SEAT TRACK. 2L72 4F4 FRT E2EA 20040623000572004062300057WP 2004 6 23 GTIA040532 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 LT IB SEAT TRACK FS 927 THRU 1098 CORRODED AND GOUGED. REMOVED LT IB SEAT TRACK FROM STA 896-1098. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND SPLICES. 2L72 4F4 FRTA6WE E2EA 20040623000592004062300059WP 2004 6 23 GTIA040537 120040429A7120K221995A31 ISOLATOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RT ENGINE OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 RT ENGINE PYLON, LOWER VIBRATION ISOLATOR ALIGNMENT MARK MISMATCH EXCEEDS ALLOWABLE LIMITS. REMOVED LOWER VIBRATION ISOLATOR. INSTALLED VIBRATION ISOLATOR. 2L72 4F4 FRTA6WE E2EA 20040623000632004062300063EU 2004 6 23 ASOA04371 120040307A5315 FLOORBEAM AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK INSPECTION, THE FLOORBEAMS AT FRAMES 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAMS IAW SRM51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2H72 4T4 TRT E20NE 20040623000652004062300065WP 2004 6 23 GTIA040482 120040430A5320 ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 FORWARD CARGO DOOR JAMB FS 385 LONGERON 19R L-ANGLE EXFOLIATED. REMOVED L-ANGLE. FABRICATED L-ANGLE. INSTALLED L-ANGLE. 2L72 4F4 FRTA6WE E2EA 20040623000662004062300066WP 2004 6 23 GTIA040485 120040503A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 CRACKED INTERCOASTAL STA 1022 TO STA 1041 BODY LINE. REMOVED DAMAGED INTERCOASTAL. FABRICATED NEW INTERCOASTAL. INSTALLED NEW INTERCOASTAL. 2L72 4F4 FRTA6WE E2EA 20040623000672004062300067WP 2004 6 23 GTIA040494 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 G2 GALLEY FLOORBOARD AT STA 200 TO STA 256 (P) DELAMINATED. FAB FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040623000682004062300068WP 2004 6 23 GTIA040496 120040501A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE SEPARATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 FLOOR PANEL 1251-1309 SEPARATED. FAB NEW FLOOR PANEL. 2L72 4F4 FRTA6WE E2EA 20040623000692004062300069WP 2004 6 23 GTIA040491 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 G4 GALLEY FLOORBOARD AT STA 1117 TO STA 1287 (C) DELAMINATED. FABRICATED NEW FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040623000702004062300070WP 2004 6 23 GTIA040492 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 G4 GALLEY FLOORBOARD AT STA 1155 TO STA 1287 (D) DELAMINATED. REPAIRED DELAMINATED AREAS. 2L72 4F4 FRTA6WE E2EA 20040623000712004062300071WP 2004 6 23 GTIA040497 120040501A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE COCKPIT CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 COCKPIT F/O`S FLOOR PANEL CRACKED AND DRILLED OFF SCREW. CUT OUT CRACKED PART. FABRICATED DOUBLER. INSTALLED FABED PARTS. 2L72 4F4 FRTA6WE E2EA 20040623000732004062300073EU 2004 6 23 ASOA04368 120040307A5320 SUPPORT BRACKET AEROSPATR72 ATR72 EU PWA PW120 PW127 NE THRESHOLD CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK INSPECTION, CORROSION WAS FOUND BEYOND LIMITS ON BOTH THRESHOLD SUPPORT BRACKETS OF PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED THE CORRODED THRESHOLD SUPPORT BRACKETS IAW SRM 51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21,2004. 2H72 4T4 TRT E20NE 20040623000792004062300079WP 2004 6 23 GTIA040512 120040523A3260 SENSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RT MLG INOPERATIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23820NK 49126 RT MAIN GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RAISED. GEAR WAS CYCLED AND LIGHT EXTINGUISHED. ADJUSTED RT MLG UP LATCH PROXIMITY SENSOR TO TARGET CLEARANCE. JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS. ALL INDICATIONS NORMAL. 2L72 4F4 F A6WE E2EA 20040623000812004062300081 2004 6 23 GTIA040514 420040525A2565 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE R1 DOOR UNSECURE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 48087 R1 DOOR SLIDE PACK FELL OFF DOOR. INSTALLED R1 DOOR SLIDE PACK COVER. 2L72 4F4 F A6WE E2EA 20040623000832004062300083WP 2004 6 23 GTIA040506 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 LT IB SEAT TRACK FS 1231 THRU FS 1309 GOUGED AND CORRODED. REMOVED LT IB SEAT TRACK. LOCATED AND DRILLED NEW TRACK. INSTALLED SEAT TRACK. 2L72 4F4 FRTA6WE E2EA 20040623000852004062300085WP 2004 6 23 GTIA040538 120040508A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 CORRODED, ENLONGATED HOLE, AFT PIT INTERCOASTAL STA 1174. FORMED INTERCOASTAL. FABRICATED (L) FITTING. 2L72 4F4 FRTA6WE E2EA 20040623000882004062300088WP 2004 6 23 GTIA040504 120040429A5320 ANGLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE CARGO BAY CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 AFT PIT FORWARD AND AFT DOOR LATCH SUPPORT ANGLES CRACKED. REMOVED 2 EA CRACKED SUPPORT ANGLES. FABRICATED 2 EA SUPPORT ANGLES. INSTALLED 2 EA SUPPORT ANGLES. 2L72 4F4 FRTA6WE E2EA 20040623000922004062300092EA 2004 6 23 ASOA04382 120040525A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27882AS 7503 DURING A (C) CHECK, THE OB CLIP AT FS 280, RBL 9 IN THE AVIONICS EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 280, RBL9 IN THE AVIONICS EQUIPMENT BAY. 2L72 4F4 FRTA21EA E15NE 20040623000932004062300093EA 2004 6 23 ASOA04339 120040508A5210601R3807423 ANCHOR FITTING BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PASSENGER DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27868AS 7475 7474 DURING AN A-CHECK, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040623000952004062300095WP 2004 6 23 GTIA040508 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT OB SEAT TRACK FS1022- FS 1309 CORRODED AND GOUGED. SEAT TRACK REMOVED FROM STA 1032-1309. 3 EA SEAT TRACK SPLICES LOCATED AND DRILLED AR RBL 44 ON STA 1032, 1146 AND 1222. CRACK FOUND AS FS 1022. REMOVED DAMAGED AREA ON WEB. FABRICATED FILLER AND DOUBLER FOR WEB. INSTALLED REPAIR FILLER/ DOUBLER. INSTALLED RT SEAT TRACK SPLICES. 2L72 4F4 FRTA6WE E2EA 20040623000972004062300097WP 2004 6 23 GTIA040511 120040522A3260 LIGHT DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE MLG INDICATOR INTERMITTENT A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23810NK 48015 NOSE GEAR LIGHT FLICKERS ON AND OFF IN FLIGHT. REMOVED AND CLEANED CANNON PLUG. 2L72 4F4 F A6WE E2EA 20040623000982004062300098WP 2004 6 23 GTIA040503 120040428A7830 DOUBLER DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE THRUST REVERSER CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 NR 1 ENGINE THUST REVERSER SN 11443, RT SIDE LOWER TR SHELL CRACKED AT PREVIOUS REPAIR DOUBLER. REMOVED CRACKED REPAIR DOUBLER. FORMED NEW REPAIR DOUBLER. INSTALLED NEW REPAIR DOUBLER. 2L72 4F4 FRTA6WE E2EA 20040623001002004062300100EA 2004 6 23 ASOA04360 120040515A3350 BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE EMERGENCY LIGHT DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27706EV 10054 DURING A COCKPIT CHECK TEST ON THE GROUND, THE EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. THE FLIGHT ATTENDANT FOUND THE EMERGENCY LIGHT SWITCH IN THE ON POSITION. MAINTENANCE CHARGED THE EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040623001022004062300102EU 2004 6 23 ASOA04357 120040428A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK, INTERCOSTALS BETWEEN FRAMES 36 AND 38 ON BOTH LT AND RT SIDES WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED INTERCOSTALS IAW SRM 512501. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040623001032004062300103WP 2004 6 23 GTIA040519 120040512A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23802NK 53168 CABIN RT OB SEAT TRACK LT CORRODED AND WORN. RT OB SEAT TRACK FROM STA 200 TO 300 OUT OF LIMITS. REMOVED SEAT TRACK. LOCATED AND DRILLED HOLES FOR SEAT TRACK FROM STA 200 TO 300 RT OB. INSTALLED NEW SEAT TRACK SECTION. 2L72 4F4 FRTA6WE E2EA 20040623001052004062300105EU 2004 6 23 ASOA04369 120040307A5347 SEAT TRACK AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK, THE LT SIDE SEAT TRACK AT FRAMES 36-39 AS WELL AS THE RT SIDE SEAT TRACK FROM FRAME 39-40 WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM51-25. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2H72 4T4 TRT E20NE 20040623001072004062300107NM 2004 6 23 GTIA040547 120040514A5320 FLOOR SUPPORT DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1155 LBL 22 TO LBL 44. REMOVED FLOOR SUPPORT. LOCATED AND DRILLED SUPPORT. INSTALLED MAIN CABIN FLOOR SUPPORT. 2L72 4F4 FRT E2EA 20040623001122004062300112WP 2004 6 23 ABXA040199 120040601A33505708458503 BATTERY DOUG DC8 DC863F 302198FWP EMERGENCY LIGHT INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23826AX 208 46061 DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHTS BATTERY PACK ASSEMBLY IAW DC8 MM 33-50-01. 2L74 4F 4A25 20040623001132004062300113NM 2004 6 23 QXEA200400390 120040602A521085217555005 SEAL BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX5813 4060 GEG - FLIGHT 2314 - THE FLIGHT ATTENDANT STATES THAT THE AFT PASSENGER DOOR IS DIFFICULT TO PUSH OUT AND THAT IT STICKS AFTER UNLOCKING. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR SEAL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040623001142004062300114EA 2004 6 23 COMA0460364 120040609A4990 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA APU OIL SYS ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01999CA 7230 FLIGHT 5905 APU OIL PRESSURE CAUTION. COULD NOT DUPLICATE, FOUND NO DEFECTS WITH APU. 2L72 4F RTA21EA 20040623001152004062300115EA 2004 6 23 COMA0460363 120040607A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01708CA 7235 FLIGHT 5576 EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REMOVED AND REINSTALLED TRACK LIGHT IAW AMM, OPERATION SATISFACTORY. 2L72 4F RTA21EA 20040623001182004062300118EA 2004 6 23 COMA0470048 120040607A2750 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01641CA 10122 FLIGHT 5553 CONFIG FLAPS CAUTION DURING T/O. COULD NOT DUPLICATE. NO FAULTS IN COMPUTER. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20040623001192004062300119NM 2004 6 23 QXEA200400381 120040524A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - NUMBER 8 SEAT TRACK HAS CORROSION ON INBOARD FLANGE FROM STATION X490 TO X496. REPAIRED IAW RD 8-53-1339, 8-53-4473 AND SRM 51-40-11. 2H72 4T RTA13NM 20040623001202004062300120NM 2004 6 23 QXEA200400384 120040525A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - RIGHT HAND OUTBOARD NUMBER 12 SEAT TRACK TOP FLANGE IS GOUGED AND PITTED AT STATION X518.0. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20040623001212004062300121NM 2004 6 23 QXEA200400391 120040603A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09363PH112614381 520 PSC - FLIGHT 2096 - AIRCRAFT RETURNED TO FIELD, NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. CAUTION LIGHT WOULD NOT EXTINGUISH UNTIL AUXILLARY PUMPS AND STANDBY PUMPS WERE TURNED OFF. LEFT TRU LIGHT ALSO ILLUMINATED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 1 AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040623001222004062300122NM 2004 6 23 QXEA200400380 120040527A5410 SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - LEFT HAND NACELLE LOWER INBOARD ENGINE SUPPORT STRUT IS CHAFED ON INBOARD SIDE OF STRUT. APPLIED PROTECTIVE COATING PER RD 8-54-036. 2H72 4T RTA13NM 20040623001232004062300123 2004 6 23 PCAA0405214 420040526A3442071013190010 RADAR DHAV DHC8 DHC8102 2809003NM WX SYSTEM INTERMITTENT A PCAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA13808 2362 1072 299 FLIGHT 3854 LGA TO SYR REPORTED WEATHER RADAR AS SPOKING INTERMITTANTLY AND NOT PAINTING THE WEATHER. CONDITION OCCURRED DURING CRUISE. CREW RETURNED TO LGA DUE TO SEVERE WEATHER EN ROUTE. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR R/T AND ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040623001252004062300125 2004 6 23 61779 420040526A61228210410 GOVERNOR BEECH 1900 1900D 1154162CE PROPELLER MALFUNCTIONED A AMWAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 CE07143ZV UE143 ON TAKEOFF RIGHT PROP RPM INDICATOR WENT TO 2000 RPM CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED RT PROP GOV & OVERSPEED GOV CHECKS GOOD. P/N 8210-410. 2L72 4T RTA24CE 20040623001262004062300126 2004 6 23 WRLA200423 420040526A256524D3005331 SLIDE DOUG DC10 DC1030 3023501WP R-1 DOOR FAILED A WRLAK NONE O OTHER ININSP/MAINT 1 SO1114075 46922 DURING MAINTENANCE CHECK, GYR R-1 DOOR SLIDE SCHEDULE FOR TEST DEPLOYMENT, THE TEST ACCOMPLSHED PER DC-10 MM, DURING THE TEST CHECK THE SLIDE INFLATED WHEN THE DOOR WAS APPROXIMATELY 3/4 OPEN AND DEPLOYED INSIDE THE AIRCRAFT (THE SLIDE NEVER LEFT THE DOOR WAY). REMOVED AND REPLACED THE SLIDE. 2L73 4F A22WE 20040623001272004062300127CE 2004 6 23 61743 120040525A32601013645789 CONTROL UNIT BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER APAPPROACH 1 CE07126YV UE126 ON APPROACH FOR LANDING IN PFN, THE LT MAIN GEAR WON'T INDICATE DOWN AND LOCK. EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED A125 PCB, OPS CHECK NORMAL. P/N 101-364578-9, S/N 671396. 2L72 4T RTA24CE 20040624000052004062400005WP 2004 6 24 ABXA040200 120040602A2740A074022 JACKSCREW DOUG DC8 DC863F 302198FWP STAB BINDING A ABXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL23811AX 46113 DURING APPROACH TO GUA, STABILIZER JAMMED, WOULD NOT MOVE BOTH ELECTRIC OR HYDRAULIC. INDICATOR AT 5.2 DEGREES. FOUND GEARBOX SPROCKET SHEAR PINS SHEARED AND RIGHT JACKSCREW BINDING. INSTALLED NEW SHEAR PINS IAW DC8 OVHL MM 27-10-1. REPLACED LEFT AND RIGHT LONGITUDINAL TRIM JACKSCREWS ASSEMBLIES IAW DC8 MM 27-41-01-2. ACCOMPLISHED ADJ/TEST IAW DC8 MM 27-40-00-5, PARTS 1 THROUGH AND INCLUDING 3B. NO FURTHER DEFECTS NOTED. LUBRICATED BOTH LEFT AND RIGHT JACKSCREWS AFTER INSTALLATION IAW DC8 MM 12-82-01-3. CHECKED OIL LEVEL ON STAB TRIM GEARBOX. OIL LEVEL WAS WITHIN LIMITS IAW DC8 MM 27-41-05-21 AND 12-82-01-3. 2L74 4F 4A25 20040624000092004062400009SO 2004 6 24 SWIA200413372 120040602A2730 SCREW EMB 120 EMB120ER 3260203SO INDICATOR LOOSE A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07235SW 120310 TRIM AURAL WARNING ON TAKEOFF ROLL. TIGHTENED INDICATOR GEAR ECCENTRIC SCREW. OPS CHECKS GOOD. 2L72 4T RTA31SO 20040624000102004062400010EA 2004 6 24 SWIA200413373 120040531A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07592SW 7279 SPOILERON FAULT STATUS MESSAGE WOULD NOT CLEAR. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER INBOARD PCU IAW MM 27-61-00. LEAK AND OPS CHECK GOOD. 2L72 4F RTA21EA 20040624000112004062400011NM 2004 6 24 DHL2004754008 120040511A5740 MOUNT BRACKET BOEING727 727223 1384074NM KRUEGER FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING C-CHECK, RT WING NR 6 KRUEGER FLAP ACTUATOR MOUNT IS CRACKED AT LOWER CORNERS. REMOVED ACTUATOR MOUNT, FABRICATED REPLACEMENT PART 7075-T6, .063 PO 900861 (8 X 3) IAW B727 SRM 57-20-2 RM171 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED PART IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040624000122004062400012EA 2004 6 24 COMA0460375 120040615A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANED 650BB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2L72 4F RTA21EA 20040624000142004062400014EA 2004 6 24 COMA0460369 120040615A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 CARGO BAY FLOORBEAM CAP AT LBL 9 CORRODED BETWEEN FS 589 AND FS 610. REMOVED CORRODED CAP AND INSTALLED NEW CAP P/N 601R35031-3 I/A/W CRJ SRM 51-42-13 AND CRJ SRM 51-42-06. 2L72 4F RTA21EA 20040624000152004062400015EU 2004 6 24 DHL2004364517 120040316A5320 ANGLE AIRBUS300 A300B4203 3930306EU FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 C-CHECK, REPLACE INNER & OUTER RIM ANGLES FR 80 STA 4944 STR 56L. REMOVED FASTENERS, SEALANT, PNEU DUCT FR 76-80 LT FOR ACCESS. REMOVED FORMED SECTION FR 80 & CONNECTING FITTINGS P27L-P27R, NO CORROSION. REMOVED FASTENERS AT INNER RIM ANGLE REPAIR AREA P42L-P42R, RADIAL SECTIONS & CIRCUMFERENTIAL STRAPS CONNECTING STRAPS SHIMS & RIM ANGLE (INNER). CUT CIRCULAR STRAP. PERFORMED HFEC EXPOSED OUTER ATTACH ANGLE, NO CRACKS. RE-EVALUATION OF OUTER RIM ANGLE, NO DAMAGE OR CORROSION. FOUND INNER RIM ANGLE DAMAGED. DRILLED NEW INNER RIM SECTION. INSTALL FORKED SECTION FR 80, CONNECTING FITTINGS & CIRCUMFERENTIAL STRAP SECTION STRAP SECTION. INSTALL SUPPORT SEGMENTS, LT & RT SERVO HYD LINES LOWER FR 80 BLKHD. 2L72 4F RTA35EU 20040624000162004062400016EA 2004 6 24 COMA0460376 120040615A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 FRETTING DAMAGE NOTED ON LEFT HAND WING PLANK LOWER ACCESS HOLE AT 550 CB. BLENDED FRETTING AREAS IAW 601R-57-21-030. ALODINED AND PRIMED IMW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON PANEL 550 CB AMM 51-80-00. BOND CHECK GOOD. 2L72 4F RTA21EA 20040624000172004062400017EA 2004 6 24 COMA0460371 120040615A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 LEFT LOWER WING PLANK CRACKED AT WS 148.019. COMPLIED WITH EO 57-020 REV A. MODIFICATIONS OF THE LEFT WING LOWER WING PLANK AT WS 148. 2L72 4F RTA21EA 20040624000192004062400019EA 2004 6 24 COMA0460379 120040615A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 640FB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 640FB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 640FB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2L72 4F RTA21EA 20040624000212004062400021EA 2004 6 24 COMA0460374 120040615A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 650BB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2L72 4F RTA21EA 20040624000232004062400023NM 2004 6 24 DHL2004754005 120040511A575465173103 FITTING BOEING727 727223 1384074NM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, NR 2 SLAT WS 629 AT ATT ACT HAS INBD ATTACH FRAME CRACKED. REMOVED & REPLACED DAMAGED ATTACH FITTINGS P/N 65-17310-3, PO 4175400 & P/N 65-17310-4, PO 422356 IAW 727 SRM 51-30-2. 2L73 4F A3WE 20040624000242004062400024NM 2004 6 24 DHL2004741007 120040602A3350 LIGHT BOEING727 7272Q9 138448MNM COCKPIT INOPERATIVE A DHLAO OTHER L NO TEST ININSP/MAINT 1 SO01741DH 21931 EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR WON'T ILLUMINATE WITH LIGHT SWITCH ON THE PILOTS OVERHEAD PANEL TO ON. HOWEVER, POSITION THE SWITCH ON THE LIGHT ASSEMBLY TO ON AND LIGHT WORKS. REPLACED LIGHT ASSEMBLY AND TESTED GOOD PER M/M 33-50-00 PAGE 501. 2L73 4F RTA3WE 20040624000252004062400025EU 2004 6 24 DHL2004364008 120040604A3260BED201 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU MLG FAILED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01364DH 141 LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. COMPLETED ABNORMAL PROCEDURE AND GEAR HANDLE OPERATED NORMALLY. SWITCHED TO SYSTEM 1. PERFORMED OPS CHECK OF GEAR PROXIMITY UNIT REVEALED FAULT AT B12; SLAVED IN NLG SENSOR, NO HELP. RESTORED ORIGINAL. REPLACED PROXIMITY DETECTOR UNIT IAW M/M 32-61-12. OPS CHECKED, NO FAULTS FOUND. 2L72 4F RTA35EU 20040624000262004062400026NM 2004 6 24 QXEA200400376 120040527A2797 WIRE DHAV DHC8 DHC8202 2809007NM RT WING BROKEN A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09354PH15251 498 SEA - FLIGHT 2296 - WHILE EN ROUTE TO SEA, THE FLIGHT SPOILER 1 PUSH OFF ILLUMINATED. THE NUMBER 1 HYDRAULIC PRESSURE WAS NORMAL AND THE CHECKLIST WAS RUN. THE CREW PUSHED OFF THE FLIGHT SPOILER AND THE MASTER CAUTION ROLL SPOILER INBOARD HYDRAULIC ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE ON THE RIGHT WING AILERON QUADRANT. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040624000272004062400027NM 2004 6 24 DHL2004754014 120040515A5754 BRACKET BOEING727 727223 1384074NM LE FLAP ACTUATORCRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, NR 5 L/E FLAP ACTUATOR TRUNNION BRACKET SUPPORT CRACK INDICATION INBOARD SIDE. REMOVED DAMAGED BRACKET AND FABBED NEW FROM 7075-T6.063 PO 900861 DIM 9.5 X 6.25 INCH IAW 727 SRM 57-20-2 FIG 1. BRACKET TREATED & PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-30-2. 2L73 4F A3WE 20040624000332004062400033NM 2004 6 24 UPS04M42510 120040302A5754 SLAT TRACK DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, RT WING SLAT TRACK NR 16, I/B WEB SUSPECTED CRACK. HFEC INSPECT CUTOUT FOUND TEAR AT LHW SLAT TRACK NR 16 I/B WEB. REMOVAL ACCESS AS PER AMM 27-80-32 R45. CRACKED I/B WEB AT RHW SLAT NR 16 REMOVED PER SRM 51-33-01 & 51-35-01 V2R34. PICK UP HOLES ON NEW WEB & INSTALLED NEW WEB AS PER SRM 51-33-01 & 51-35-01 V2R34. RHW SLAT TRACK NR 16 TRACK REINSTALLED AS PER AMM27-80-32 R45. 2L73 4F RTA22WE 20040624000352004062400035NM 2004 6 24 UPS04M42512 120040312A5510 BARREL NUT DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 21 FOUND CORROSION AT BOTTOM & BEARING SURFACE. CORR REMOVED PER SRM 51-21-01V2R34 MAT REMOVED 0.021 INCH. SLEEVE BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. REPAIR CUTOUT AT BARREL NUT HOLE NR 21 RT FOUND WITHIN LIMIT OF EO MD 11-5510-19409-G & EN1146-04. 2L73 4F RTA22WE 20040624000382004062400038NE 2004 6 24 DHL2004745018 220040602A7200 ENGINE BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 2 SHUTDOWN A DHLAO OTHER X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 SO01745DH 20665 NR 2 ENGINE SHUTDOWN AFTER START COMPLETED. VALVE INTRANSIT LIGHT REMAINED ILLUMINATED DURING START. RESTART NR 2 ENGINE AND MAINTAINED ENGINE PARAMETERS. NR 2 ENGINE START AND OPS CHECKED OK PER B727 M/M 80-11-0. DUE TO WRITE UP ON LOG PAGE 008250 ON FUEL SHUT-OFF VALVE STAYED ILLUMINATED. CHECK SHUT-OFF VALVE OPERATION. OPS CHECK NR 2 ENGINE FUEL SHUT-OFF VALVE VIA FUEL START LEVER, FIRE HANDLE, AND FUEL SHUT-OFF VALVE ON S/O'S PANEL. OPS CHECKED SERVICEABLE IAW B727 M/M 28-22-01. 2L73 4F4 F A3WE E2EA 20040624000392004062400039EA 2004 6 24 COMA0460385 120040619A2432 BATTERY CNDAIRCL600 CL6002B19 1900309EA APU MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01960CA 7117 FLIGHT 5721 DURING CRUISE FLIGHT APU BATTERY INDICATED 99 AMPS, AIRCRAFT DIVERTED TO CLE. DEFERRED THE APU BATTERY PER MEL 24-32-03. 2L72 4F RTA21EA 20040624000402004062400040NM 2004 6 24 UPS04M42515 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB LT BARREL NUT HOLE NR 12 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR AT BOTTOM OF HOLE REMOVED MATERIAL REMOVED 0.038 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19409-E. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040624000422004062400042NM 2004 6 24 QXEA200400385 120040601A1420 CONNECTOR DHAV DHC8 DHC8202 2809007NM ZONE 300 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09359PH14329 514 SEA - FLIGHT 2189 - THE FLIGHT RETURNED TO FIELD WHEN THE CREW RECEIVED A RUDD FULL PRESS CAUTION LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED CONNECTOR 2721-P3, 2721-P4, AND TERMINAL BLOCK 2721-TB1. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040624000442004062400044 2004 6 24 SWAA041728 420040621A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F A16WE 20040624000452004062400045 2004 6 24 SWAA041729 420040621A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040624000462004062400046 2004 6 24 SWAA041730 420040621A25651061323433 SLIDE BOEING737 7373H4 1384600NM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040624000472004062400047 2004 6 24 SWAA041731 420040621A2565D31354125 SLIDE BOEING737 7373Q8 1384670NM L2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 L2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040624000482004062400048 2004 6 24 SWAA041732 420040621A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040624000502004062400050NM 2004 6 24 SWAA041734 120040621A53106517684 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND DOOR FRAME AT BS 303, STRINGER 16L, CRACKED. REPAIRED DOOR FRAME SECTION PER SB. 2L72 4F RTA16WE 20040624000512004062400051NM 2004 6 24 SWAA041735 120040621A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20040624000522004062400052 2004 6 24 SWAA041736 420040621A2565D31354 SLIDE BOEING737 7373A4 1384585NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040624000532004062400053NM 2004 6 24 SWAA041737 120040621A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 872, RBL 60 TO RBL 67, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20040624000552004062400055NM 2004 6 24 UPS04M42516 120040316A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 10 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040624000562004062400056NM 2004 6 24 UPS04M42517 120040319A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT NR 20 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040624000602004062400060NM 2004 6 24 DHL2004754016 120040509A7160 NOSE COWL BOEING727 727223 1384074NM NR 3 ENGINE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, NR 3 ENGINE NOSE COWL INLET RING OUT EXTERIOR SURFACE AFT SKIN EDGE AREA AT 3 O'CLOCK POSITION HAS A DENT. DAMAGE OUT OF LIMITS IAW B727 SRM 54-30-1 FIG 1, CUT OUT DAMAGED AREA DIM 2.25 X 1.75 INCH AND FABRICATED NEW FILLER DIM 2.25 X 1.75 INCH AND DOUBLER DIM 6 X 2.625 INCH FROM 2024T3 .050, PO 900780 IAW B727 SRM 54-30-3 FIG 2. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER AND FILLER ON NR 3 ENG NOSE COWL INLET RING OUT EXTERIOR SURFACE AFT SKIN EDGE AREA AT 3 O'CLOCK POSITION IAW B727 SRM 51-30-2 AND 54-30-3. 2L73 4F A3WE 20040624000612004062400061NM 2004 6 24 DHL2004754017 120040509A7110 COWLING BOEING727 727223 1384074NM NR 2 ENGINE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, NR 2 ENG LT FWD UPPER SUPPORT STRUCTURE HAS (2 EA) HINGE CUTOUT PLATES FOR COWLING ARE BENT OUT & CRACKED AT RADIUS. REMOVED PREVIOUS REPAIRS 2 EA NR 2 ENG L/H FWD UPPER SUPPORT IAW B727 SRM 51-30-2 FABRICATED (2 EA) NEW DOUBLERS 301 1/2 HD .063, PO 900125 (3 X 5.75) (3 X 6) IAW B727 SRM 54-10-2 & 51-40-3. TREAT AND PRIME IAW B727 SRM 51-10-2. INSTALLED (2 EA) DOUBLERS IAW B727 SRM 51-40-3. 2L73 4F A3WE 20040921000522004092100052EA 2004 9 21 ASOA04594 120040814A2121GC670950283 FAN CNDAIRCL600 CL6002C10 1390015EA GALLEY BURNED OUT A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11709EV4288 10068 DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT NOTICED AN ODOR FROM THE AIR CONDITIONING SYSTEM. IT PERSISTED DURING THE FLIGHT FROM ATL-IAH CAUSING EYE IRRITATIONS AND DIFFICULTY BREATHING FOR THE FLIGHT ATTENDANT AND PASSENGERS. THE AIRCRAFT LANDED SAFELY IN IAH. MAINTENANCE REMOVED AND REPLACED THE LAVATORY/GALLEY EXHAUST FAN, BOTH RECIRCULATION FAN FILTERS AND CLEANED THE LAVATORY DRAIN TUBE. NO FURTHER SMELLS WERE NOTICED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000542004092100054EA 2004 9 21 ASOA04600 120040815A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11824AS 7203 DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000652004092100065WP 2004 9 21 GTIA040737 120040802A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND FORWARD CABIN FLOOR SUPPORT CORROSION FS 160-200 LBL 44. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040921000762004092100076 2004 9 21 GTIA040749 420040825A2565 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FOUND L1 DOOR LANYARD IS OFF. REINSTALLED L1 DOOR LANYARD. GTIA (M) 2L72 4F A6WE 20040921000792004092100079WP 2004 9 21 GTIA040763 120040828A2612 FIRE WARNING DOUG DC9 DC983 3022083WP LT ENGINE ACTIVATED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23831NK 49617 FIRE DETECTOR LOOP LIGHT ON DURING FLIGHT DID PROCEDURE IN QRH LEFT ENGINE LOOP B. (M) GTIA 2L72 4F RTA6WE 20040921000812004092100081EU 2004 9 21 SIMA200424302 120040828A30206068T56P01 VALVE SAAB SF340 340B 7860101EU NR 2 ENGINE MALFUNCTIONED A SIMAA UNSCHED LANDING RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW21390AE 340B390 DURING CRUISE WITH ANTI-ICE ON, CREW ENCOUNTERED MULTIPLE COMPRESSOR STALLS ON NR 2 ENGINE ACCOMPANIED BY SLIGHT CHANGES IN TORQUE AND ITT. ALSO, RECEIVED NR 2 IGNITION LIGHT. REPLACED ANTI-ICE VALVE ON NR 2 ENGINE. PERFORMED BOROSCOPE OF HOT AND COLD SECTIONS WITH NO DISCREPANCIES NOTED. OPERATIONAL CHECKS FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040921000922004092100092WP 2004 9 21 GTIA040751 120040826A3240284702 CONTROL VALVE DOUG DC9 DC982 3022082WP BRAKES MALFUNCTIONED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FLL - FLT 478 - FOUND BRAKE PEDAL DEPRESSION ON LEFT SIDE IS ALMOST TWICE THE RIGHT SIDE BEFORE BRAKE PADS MAKE CONTACT. REMOVED AND REPLACED LEFT WHEEL WELL BRAKE CONTROL VALVE. BLED ALL FOUR BRAKES FREE OF AIR. (M) 2L72 4F A6WE 20040921000972004092100097EA 2004 9 21 A6WA200340402 120040101A3250 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NLG STEERING FALSE ACTIVATIONA A6WAK NONE J WARNING INDICATION ININSP/MAINT 1 GL31406AW 7402 STEERING INOPERATIVE MESSAGE SHORTLY AFTER GEAR RETRACTION, GEAR DISAGREE MESSAGE AND NOSE DOOR OPEN MESSAGE. CYCLED GEAR SEVERAL TIMES. COULD NOT DUPLICATE. OPS CHECK GOOD IAW AMM 32-30-00. (M) 2L72 4F RTA21EA 20040921001072004092100107EA 2004 9 21 ASOA04515 120040716A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11828AS 7213 DURING A HANGAR INSPECTION IN BTR, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921001202004092100120NM 2004 9 21 04240417 120040827A3350 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27417FJ 3174 NR 3 CEILING EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT BULB IAW 33-21-31. 2H72 4T RTA55NM 20040921001232004092100123EA 2004 9 21 04240634 120040827A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS DEFECTIVE A VTZAO OTHER S AFFECT SYSTEMS DEDESCENT 1 EA27634BR 7287 FLAP FAIL 8 DEGREES. PERFORMED TEST OF FECU AND RESET. OPS CHECK GOOD IAW 27-51-00. 2L72 4F RTA21EA 20040921001332004092100133NM 2004 9 21 SWAA042713 120040918A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040921001362004092100136NM 2004 9 21 SWAA042716 120040918A335065C27095 BATTERY PACK BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED A1 CHECK, FOUND LOWER EMERGENCY EXIT LIGHTS ON AFT SERVICE AND ENTRY DOORS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040922000012004092200001NM 2004 9 22 SWAA042718 120040919A53306545774 SKIN BOEING737 7373TO 138447GNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SPV, FOUND FUSELAGE SKIN AT BS 727D, RBL 1, WL 148, CORRODED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040922000122004092200012WP 2004 9 22 GTIA040692 120040708A5755 SKIN DOUG DC9 DC982 3022082WP RT WING SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND RIGHT WING GROUND SPOILER TOP SIDE HAS DENTS AND DELAMINATED. REPAIRED TWO DELAMINATIONS. (M) 2L72 4F A6WE 20040922000162004092200016WP 2004 9 22 GTIA040695 120040729A3260833604 UPLOCK SENSOR DOUG DC9 DC982 3022082WP RT MLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL23801NK 48048 THE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN HYDRAULIC PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PLUMBING, GEAR, DOOR MECH'S. ON RIGHT GEAR NO DEFECTS NOTED. REMOVED AND REPLACED TR GEAR UPLOCK SENSOR. REMOVED AND REPLACED PROX SWITCH ELECT UNTI AS PRECAUTIONARY, GROUND CHECKS OK AT THIS TIME. (M) 2L72 4F A6WE 20040922000292004092200029WP 2004 9 22 GTIA040689 120040721A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT MISWIRED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FOUND O/H EMERGENCY LIGHT AT ROW 30 IS INOPERATIVE. FOUND LIGHT L2-633 WIRED INCORRECTLY. CORRECTED WIRING. (M) 2L72 4F A6WE 20040922000312004092200031WP 2004 9 22 GTIA040690 120040708A5755 SKIN DOUG DC9 DC982 3022082WP RT WING SPOILER DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND RIGHT WING OUTBOARD FLIGHT SPOILER BOTTOM SIDE DENTED/DELAMINATED. REPAIRED BOTTOM SIDE OF OUTBOARD FLIGHT SPOILER. (M) 2L72 4F A6WE 20040922000522004092200052NM 2004 9 22 USAA040375 120040721A5312 BULKHEAD BOEING737 7373B7 1384580NM AFT PRESSURE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND SKIN CRACKED 1.25 INCH, THROUGH FASTENER STATION 1040 BL-0 AFT PRESSURE BULKHEAD, 9 FASTENERS ABOVE CENTER OF BULKHEAD. MANUFACTURED FILLER AND DOUBLER PER 53-80-08 FIG 201. (M) 2L72 4F RTA16WE 20040922000602004092200060SO 2004 9 22 SWIA200413815 120040914A3350 LAMP EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07221SW 120290 RED EMERGENCY LAMP BELOW FLIGHT ATTENDANT JUMPSEAT IS INOPERATIVE. ADJUSTED RED LIGHT AT FA STATION. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040922000612004092200061EA 2004 9 22 SWIA200413816 120040915A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07959SW 7840 ON CLIMBOUT, (STEERING INOP) CAUTION MSG CAME ON FOLLOWED BY (STAB TRIM) (BOTH CHANNELS), THEN (MACH TRIM). OPS CHECKED NWS AFTER RESET AND OPS CHECK GOOD. REPLACED HSTCU AND PERFORMED OPERATIONAL CHECK IAW CRJ MM 27-41-01. 2L72 4F4 FRTA21EA E15NE 20040922000622004092200062NM 2004 9 22 04260416 120040916A5350 SEAL DORNERDO32 DO328300 NM PWA 306 PW306B NE NR 1 FAIRING LOOSE A VTZAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA27416FJ 3171 LOUD THUMPING SOUND ON CLIMBOUT. CAUSE WAS TOP FUSELAGE NR1 FAIRING SEAL LOOSE. REBONDED SEAL. 2H72 4T4 FRTA55NM E35NE 20040922000662004092200066EA 2004 9 22 COMA0460536 120040911A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01987CA162035536 7199 FLIGHT 5738 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F4 FRTA21EA E15NE 20040922000672004092200067NE 2004 9 22 FWTA200431601 220040718A7200CF680C2B7F ENGINE BOEING767 767300 1385204NM GE CF6 CF680C2B7 NE RIGHT SEIZED A FWTAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO19316LA 704600 FLT RF 773, LANDING, WITH RT ENG SHUT DOWN IN FLT, AFTER LOUD NOISE AND VIBRATION ENG SHUT DOWN. STATUS MSG APPEARS RT OIL FILTER, R REVERSE ISOLATION VALVE. 79 02 25 02 OIL FILTER . DISPLAY OUT OF VIEW WHEN THRUST REDUCE. OIL PRESSURE, NORMAL. 79 02 11 02 ENG OIL TEMP HIGH 139 (C) OIL PRESS 14 PSI. NOTE: EGT 898 (C) WHEN ENG SHUT DOWN. A/C OVER WEIGHT LANDING 1490.000 KG. 2L72 4F4 FRTA1NM E13NE 20040922000702004092200070 2004 9 22 TXER097330 420040826A3416150201182 ALTIMETER UROCOPEC155 EC155B 8681000EU COCKPIT INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588CF 6662 ALITIMERTER INOPERATIVE, OFF 100 FEET. 1G72 3U H10EU 20040922000722004092200072SW 2004 9 22 ALGA097279 120040907A6420B1212 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR DAMAGED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL1635 52280 TAIL ROTOR BEARING HAS FLAT SPOTS ON NEEDLE ROLLERS. REPLACED W/NEW PART BY OVERHAUL SHOP. 1G71 3U3 UNCH2SW E1GL 20040922000732004092200073SW 2004 9 22 ALGA097281 120040907A6420206011812005 TRUNNION BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL1635 52280 TAIL ROTOR TRUNNION HAS CORROSION DAMAGE ON SPLINES. REPLACED W/SERVICEABLE HOUSING BY OVERHAUL SHOP. 1G71 3U3 UNCH2SW E1GL 20040922001072004092200107NM 2004 9 22 SWAA042720 120040919A53306552988 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 942, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040922001082004092200108NM 2004 9 22 SWAA042721 120040919A57436567172 FITTING BOEING737 7373H4 1384600NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG AFT INBOARD STABILIZER FITTING CORRODED. REMOVED AND REPLACED LT MLG STABILIZER FITTING PER MM. 2L72 4F RTA16WE 20040922001092004092200109 2004 9 22 SWAA042722 420040920A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040922001152004092200115NM 2004 9 22 SWAA042728 120040920A53156546811 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM FWD FLANGE UNDERSIDE AT BS 986 LT AFT GIRT BAR MOUNT, CORRODED. REPAIRED FLOORBEAM FLANGE PER SRM. 2L72 4F RTA16WE 20040922001322004092200132NM 2004 9 22 DHL2004745522 120040706A5311 FRAME BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, AFT CARGO FRAME BS 1010 HAS A DENT INTO THE RADIUS ABOVE STR 26L TO STR 24L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED EXISTING SPLICE, CUT OUT DAMAGED FRAME, FABBED NEW FROM 7075 T-6 .063 PO 900408 DIM 13.5 X 5.25 INCHES AND 1 MORE SPLICE FROM 7075-T6 .071 PO 900489 DIM 8 X 4.125 INCHES IAW 727 SRM 51-40-3 FIG 1 & 53-10-2 FIG 3. PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 & 51-40-3 FIG 1. 2L73 4F A3WE 20040922001342004092200134NM 2004 9 22 DLM88040855 120040908A5270 PROXIMITY SENSOR DOUG MD88 MD88 3023688NM E/E BAY DOOR FAILED A DALAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO27911DE 49967 AT T/O AIRCRAFT WOULD NOT PRESSURIZE. TRIED BOTH MANUAL AND AUTO PRESS, NO HELP. LOUD NOISE HEARD THROUGHOUT A/C. ALL DOORS ON OAP SHOWED CLOSED. RESEATED E/E DOOR. REPLACED PROX SENSOR FOR DOOR. 2L72 4F RTA6WE 20040922001382004092200138NM 2004 9 22 SWAA042662 120040914A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 668, LBL 25, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040922001502004092200150NM 2004 9 22 DL73S040842 120040903A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 700. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092798-14AD. 2L72 4F RTA16WE 20040922001602004092200160EA 2004 9 22 COMA0460456 120040811A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01984CA 7171 SKIN RADIUS AT FS 235, BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT CORNER CRACKED APPROXIMATELY .25 INCH. REPAIRED IAW REO 601R-53-11-048. 2L72 4F RTA21EA 20040922001672004092200167NM 2004 9 22 SWAA042625 120040909A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040922001692004092200169NM 2004 9 22 SWAA042668 120040914A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 277, STRINGER 15R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040922001712004092200171NM 2004 9 22 SWAA042670 120040914A53206551698 SPLICE BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND E&E COMPARTMENT STRINGER SPLICE AT BS 360, STRINGER 28L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040922001732004092200173NM 2004 9 22 SWAA042672 120040914A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L, AT BS 360, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040922001752004092200175NM 2004 9 22 SWAA042640 120040911A552365C2638428A FITTING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED SERVICE CHECK, FOUND RT ELEVATOR TAB NR 1 HINGE FITTING WORN. REMOVED AND REPLACED TAB ASSEMBLY PER MM. 2L72 4F RTA16WE 20040922001772004092200177NM 2004 9 22 DLM88040859 120040909A2497 WIRE DOUG MD88 MD88 3023688NM GALLEY CHAFED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27914DL 49545 CREW REPORTED HEARING A BANG FROM BEHIND THE CB PANEL AT WHICH TIME THE COCKPIT FILLED WITH SMOKE. FLIGHT ATTENDANT REPORTED SEEING SPARKS FROM THE OVERHEAD PANEL JUST OUTSIDE ON THE FIRST CLASS GALLEY. NO SMOKE REPORTED IN CABIN AREA. SMOKE DISSIPATED AND NORMAL LANDING. FOUND GALLEY POWER CABLES CHAFED AGAINST A/C SUPPLY DUCT CLAMP. REPAIRED WIRING AND DUCT INSULATION. REPLACED DUCT CLAMPS. 2L72 4F RTA6WE 20040922001812004092200181NM 2004 9 22 DL738040863 120040910A3350 BULB BOEING737 737832 13844CFNM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27386DA 30373 EMERGENCY LIGHT ABOVE 14C INOP. RELAMPED, OPS NORMAL. 2L72 4F RTA16WE 20040922001832004092200183NM 2004 9 22 AALA20040918 120040829A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 DFW - EMERGENCY LIGHTS AT SEATS 2AB THROUGH 6AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 2AB THROUGH 6AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040922001852004092200185NM 2004 9 22 AALA20040916 120040829A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21188AN 32382 SFO - RIGHT HAND FUSELAGE OVERWING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT M10954 FOR RIGHT HAND OVERWING FORWARD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040922001862004092200186WP 2004 9 22 AALA20040907 120040828A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21939AS 49657 DFW - FORWARD CABIN EMERGENCY BYPASS LIGHTING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN EMERGENCY BYPASS LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040922001872004092200187NM 2004 9 22 DL757040865 120040912A3230257T110320 MODULE BOEING757 757232 1384965NM COCKPIT UNSERVICEABLE A DALAO OTHER J WARNING INDICATION DEDESCENT 1 SO27635DL 23762 LANDING GEAR DISAGREE MSG. REPLACED LANGING GEAR HANDLE MODULE. 2L72 4F RTA2NM 20040923000072004092300007NM 2004 9 23 AWXA200401044 120040908A5310654587545 CREASE BEAM BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK CORROSION WAS FOUND ON R-1 DOORWAY CREASE BEAM INNER CHORD BETWEEN BS 294 AND BS 356, RBL 58, WL 208. MAINTENANCE REMOVED CORRODED CREASE BEAM INNER CHORD FROM BS 294 TO BS 356, RBL 58; FABRICATED A NEW REPLACEMENT CREASE BEAM INNER CHORD IAW DWG 65-45875; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 8, AND 12. 2L72 4F4 FRTA16WE E21EU 20040923000772004092300077 2004 9 23 KBM2004F00120 420040620A342455608505N3LA INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TURN COORDINATORINOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH3251 3141 TURN COORDINATOR, INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040923000972004092300097WP 2004 9 23 Z2M2004F00000 120040703A25607260111453 CYLINDER ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA SEAT BELT FAULTY E Z2MAO OTHER O OTHER NRNOT REPORTED 1 CE037036J1118 0583 L2538140A SEAT BELT BEGAN TO HANG UP, EVERY TIME IT WAS EXTENDED (INERTIA REEL WAS ENGAGED). REPLACED SEAT BELT AND RETRACTOR UNIT WITH NEW ONE. 1G71 3O3 O H11NM E295 20040923001012004092300101NE 2004 9 23 KBM2004F00127 220040523A75320177555170 BLEED VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 BLEED VALVE STAYS ON. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040923001032004092300103 2004 9 23 KBM2004F00131 420040612A34143839999002 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE AIRSPEED DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 SPOOL TO 180 DEGREES AND THEN STOCK NEEDLE TO 98 KNOTS. REMOVED AND REPLACED INDICATOR DUE TO ROTATING CARD FACE. 1G71 3U3 UNCH9EU E19EU 20040923001042004092300104NE 2004 9 23 KBM2004F00137 220040606A73210164248810 FUEL CONTROL SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ENGINE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA2955 2143 FUEL CONTROL UNIT, UNABLE TO OBTAIN DESIRED NR. REPLACED WITH 0.0 TSO UNIT. OPS CHECK GOOD. 1G71 3U3 U H9EU E19EU 20040923001062004092300106EU 2004 9 23 KBM2004F00130 120040531A6220EIT303201A FREQ ADAPTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 1 EA MAIN ROTOR FREQUENCY ADAPTER HAS A CRACK LENGTH BLISTER OUT OF LIMITS, SN 10659. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040923001072004092300107CE 2004 9 23 UAT2004F00000 120040722A1430MS21042L5 NUT CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO WING FITTING CRACKED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL039736M19282 20700722 REMOVED WING STRUTS TO REBUILD WINGS AND FOUND TWO CRACKED NUTS ON ONE WING STRUT. 5 EA NAS464P5A27 BOLTS HOLD THE STRUT FITTINGS IN EACH END OF THE WING STRUTS AND THESE NUTS HOLD THE BOLTS IN. THERE ARE ONE THICK AND ONE THIN WASHER ON EACH BOLT IAW IPC. THIS INSTALLATION WAS CORRECT IAW THE IPC. NO INDICATION THAT THESE NUTS AND BOLTS HAD EVER BEEN REMOVED OR REPLACED DURING THE LIFE OF THE AIRCRAFT; HOWEVER, THEY COULD HAVE BEEN AT SOME POINT. THIS CONDITION CAUSED NO OPERATIONAL PROBLEM AND I HAVE NO IDEA HOW LONG THE NUTS HAD BEEN CRACKED. 1H71 3O3 O A16CE E5CE 20040923001082004092300108CE 2004 9 23 CWQ2004F00009 120040119A1430AN17413A BOLT CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP ELEVATOR CONTROLBENT B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05713QS 6507103 DURING PHASE 5 INSP, NOTICED CORROSION ON PN 62610401, IDLER ASSY(ELEVATOR CONTROL SYS), THE -1 IDLER ASSY IS MADE OF STEEL AND HAS 2 EA ARM ASSY ATTACHED TO IT WHICH ARE ALUMINUM. THE ARMS HAD TO BE REMOVED FROM THE ASSY TO GAIN ACCESS TO AREA TO BE TREATED. THERE IS A TOTAL, 5 FASTENERS WHICH HOLED THE THREE PARTS TOGETHER, PN AN174-13A BOLTS. UPON DISASSEMBLY THE FASTENERS REMOVED WERE HI-LOKS PN HL64-8. MFG TECH SAID NO CALL OUT TO DEVIATE FROM THE AN174-13A BOLTS. ALL THE HI-LOKS REMOVED WERE BENT, COULD NOT DETERMINE IF BENT ON INSTALLATION OR STRESS DURING USE. INSTALLED WHAT THE IPC CALLED OUT AND TECH VERIFIED FROM THE BUILD PRINT. NOT PROBLEM WITH HOLE ALIGNMENT. PICTURES. 2L72 4F4 F A9NM E6WE 20040923001142004092300114WP 2004 9 23 P8UF200400001 120040708A2910AJG70415533 VALVE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR 1 HYD SYS FAILED W P8UFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO23833LA 46937 DURING CLIMB, FLIGHT CREW NOTICED HYDRAULIC LOSS ON SYSTEM NR 1, CAPTAIN DECIDED FLIGHT BACK TO POINT OF DEPARTURE. 2L73 4F4 F A22WE E23EA 20040923001152004092300115NM 2004 9 23 ASMF200408002 120040802A2914AS66411LS666 PUMP DOUG MD80 MD83 3023681NM RT HYD SYSTEM FAILED W ASMFO OTHER J WARNING INDICATION APAPPROACH 1 SW23945AS226967165 49643 DURING APPROACH, RT HYDRAULIC SYSTEM PRESSURE WAS LESSENED AND ABNORMAL PROCEDURE WAS PERFORMED. AIRCRAFT LANDED WITH LANDING GEAR DOORS DOWN. SYSTEM WAS CHECKED AND NO FAILURE WAS DETECTED, IT WAS PURGED AND 2 QUARTS WERE ADDED, QUANTITY AND PRESSURE TRANSMITTERS WERE CHECKED, ALL CORRECT. AS A PREVENTIVE ACTION, HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, TEST CORRECT. MLG DOORS WERE CHECKED IAW MM 32-12-00, ALL CORRECT. 2L72 4F RT 20040923001182004092300118NM 2004 9 23 150AW0030 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001212004092300121NM 2004 9 23 150AW0034 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 CRACK IN FUSELAGE FRAME AT BS 312 AT STR 6 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001222004092300122 2004 9 23 075491 420040827A3425 DISPLAY SAAB SF340 SF340A 7850100EU EFIS MALFUNCTIONED A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL17146SD 146SD DURING TAKEOFF ALL FOUR EFIS SCREENS WENT TO INITIALIZATION MODE. AIRCRAFT RETURNED TO FIELD. 2L72 4T RTA52EU 20040923001242004092300124NM 2004 9 23 150AW0028 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STR 18 RT BS 747. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001252004092300125NM 2004 9 23 N150AW0010 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACKS PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001262004092300126EU 2004 9 23 374PA0013 220040902A7532 LINE BOEING737 73736M 138443BNM CFMINTCFM56 CFM563C1 13802EU BLEED VALVE LOOSE A PIDAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO05374PA 28333 858393 RIGHT ENGINE DOESN'T SPOOL UP. ADJUSTED GROUND IDLE PER MM. ADJUSTED SPECIFIC GRAVITY PER MM. TIGHTENED LINE AT BLEED REGULATOR. BOTH ENGINES OPERATE NORMAL PER MM. 2L72 4F4 FRTA16WE E21EU 20040923001282004092300128NM 2004 9 23 150AW0039 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 3 RT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001292004092300129NM 2004 9 23 150AW0040 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 2 RT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001302004092300130 2004 9 23 374PA0012 420040903A2210 CIRCUIT BREAKER BOEING737 73736M 138443BNM WARNING SYSTEM FAILED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05374PA 28333 AUTO PILOT DISENGAGES BY ITSELF AND AURAL WARNING CIRCUIT BREAKER KEEPS POPPING OUT AFFECTING AUTO PILOT DISCONNECT HORN. REPLACED AURAL WARNING CIRCUIT BREAKER PER MM 31-26-00 AND OPS CHECKED. PERFORMED SELF TEST OF AUTO PILOT SYSTEM PER MM 22-02-10 AND 22-03-10. NO DEFECTS NOTED. 2L72 4F RTA16WE 20040923001322004092300132NM 2004 9 23 151AW0036 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 907 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001332004092300133NM 2004 9 23 151AW0027 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 400 AT STR 9 RT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001342004092300134NM 2004 9 23 151AW0028 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 400 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001352004092300135NM 2004 9 23 151AW0007 120040702A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER TIE CLIP CRACKED AT BS 277 AT STR 16 RT. REPLACED TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001362004092300136SO 2004 9 23 C2XA04TY160 120040826A532014521700001 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 DURING A SCHEDULED 4C INSPECTION, THE LT OMEGA SHAPE WAS FOUND TO HAVE CORROSION NEAR FRAME 20. MX REMOVED THE CORRODED SECTION OF THE OMEGA SHAPE AND SPLICED IN A NEW SECTION IAW EC5320-01145. THE ACFT WILL BE RELEASED FOLLOWING THE COMPLETION OF THE 4C INSPECTION. 2L72 4F RTT00011AT 20040923001382004092300138SO 2004 9 23 C2XA04CL086 120040827A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715910 145455 CLE FLIGHT 2050, CREW REPORTED THAT THE FIRST SEGMENT OF THE EMERGENCY PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE NR 1 INVERTER. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040923001392004092300139SO 2004 9 23 C2XA04IA109 120040823A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713553 145585 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT OVER ROW THREE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040923001412004092300141SO 2004 9 23 C2XA04SH489 120040828A532014530628001 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714925 145004 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040923001422004092300142SO 2004 9 23 C2XA04SH488 120040828A532014530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714925 145004 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040923001502004092300150NM 2004 9 23 2004UALA00787 120040826A2612 FIRE DETECTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU BAY MALFUNCTIONED A UALAF ACTIVATE FIRE EXT. J WARNING INDICATION TXTAXI/GRND HDL 1 WP29307UA 23668 AT GATE APU FIRE HANDLE LIGHT ON AND BELL, PULLED HANDLE AND DISCHARGED BOTTLE. INSPECTED THE APU COMPARTMENT AND NO EVIDENCE OF FIRE DAMAGE OR OVERHEAT CONDITION WERE NOTED. RESET APU FIRE HANDLE AND ACCOMPLISHED APU FIRE TEST. SYSTEM TESTED NORMAL. REPLACED APU FIRE EXTINGUISHER BOTTLE. 2L72 4F4 FRTA16WE E2GL 20040923001522004092300152SO 2004 9 23 C2XA04SH495 120040830A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711113 145662 SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040923001532004092300153SO 2004 9 23 C2XA04SH496 120040831A532014521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711113 145662 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040923001552004092300155NM 2004 9 23 151AW0026 120040702A5313 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER 16 LT AT BS 500C HAS THREE CRACKS. REPAIRED CRACKS PER SB737-53-1145. 2L72 4F RTA16WE 20040923001562004092300156NM 2004 9 23 151AW0034 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT FS 807 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001572004092300157NM 2004 9 23 150AW0035 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 727E BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001592004092300159NM 2004 9 23 SWAA042740 120040921A53126549892 FITTING BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND SPAR FITTING AT BS 1016, LBL 1, WL 247, CRACKED. REPAIRED FITTING PER ER. 2L72 4F RTA16WE 20040923001622004092300162NM 2004 9 23 SWAA042743 120040921A52416545871523 SKIN BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN AT BOTTOM HINGE CRACKED. REPAIRED DOOR SKIN PER EA. 2L72 4F RTA16WE 20040923001632004092300163NM 2004 9 23 SWAA042744 120040921A53116516301 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND 2 FRAMES AT BS 188, LBL 32 AND BS 188, RBL 32, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040923001642004092300164NM 2004 9 23 SWAA042745 120040921A53126546568 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 9L, CRACKED. REPAIRED BULKHEAD DOME CAP PER SRM. 2L72 4F RTA16WE 20040923001652004092300165NM 2004 9 23 SWAA042746 120040921A53116546557 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 887, STRINGER 8L, CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040923001672004092300167NM 2004 9 23 150AW0032 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 8 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001692004092300169SO 2004 9 23 C2XA04IA108 120040825A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714514 145303 IAH - DURING 3A INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040923001752004092300175NM 2004 9 23 SWAA042733 120040921A3350604222 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29367SW 26578 AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT FOR ABOUT 2 MINUTES THEN WENT OUT. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040923001782004092300178NM 2004 9 23 SWAA042736 120040921A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 22R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040923001802004092300180NM 2004 9 23 SWAA042738 120040921A53216920158 FLOOR PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D-CHECK, FOUND LT FLOOR PANEL AT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR PANEL SECTION PER SRM. 2L72 4F RTA16WE 20040923001822004092300182NM 2004 9 23 372PA0050 120040909A5347 SEAT TRACK BOEING737 737306 13844BGNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 SEAT TRACK DAMAGED AT BS 470 AT RBL 24. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-00-52. 2L72 4F RTA16NE 20040923001832004092300183NM 2004 9 23 372PA0067 120040909A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 UPPER SURFACE OF FLOORBEAM AT BS 294 HAS SEVERAL AREAS OF CORROSION. REPLACED T-CAP PER SRM 53-10-51 AND SRM 51-10-2. 2L72 4F RTA16NE 20040923001842004092300184NM 2004 9 23 372PA0068 120040909A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 UPPER SURFACE OF FLOORBEAM AT BS 312 HAS SEVERAL AREAS OF CORROSION. REPLACED SECTION OF T-CAP PER SRM 53-10-51. 2L72 4F RTA16NE 20040923001852004092300185NM 2004 9 23 372PA0049 120040909A5420 ANGLE BOEING737 737306 13844BGNM LT PYLON CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 ANGLE CRACKED ON I/B SIDE OF LEFT PYLON AT THE I/B CUTOUT FOR THE MID FLAP TORQUE TUBE. REPLACED ANGLE PER SRM 51-10-02. 2L72 4F RTA16NE 20040923001872004092300187NM 2004 9 23 372PA0060 120040909A5320 STRAP BOEING737 737306 13844BGNM FLOORBEAM CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 FLOORBEAM STRAP AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES FROM RBL 7 TO LBL 7. REPLACED STRAP PER SRM 51-10-2 AND SRM 51-40-0. 2L72 4F RTA16NE 20040923001892004092300189NM 2004 9 23 372PA0063 120040909A5320 WEB BOEING737 737306 13844BGNM CARGO BIN CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 FWD CARGO BIN WEB FROM BS 460 TO BS 480 AT STR 25 LT CRACKED. REPLACED INTERCOSTAL WEB PER SRM 51-10-02 AND SRM 51-20-01. 2L72 4F RTA16NE 20040923001942004092300194NM 2004 9 23 372PA0053 120040909A5330 SKIN BOEING737 737306 13844BGNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 OUTFLOW VALVE CUTOUT DOUBLER AT BS 986 BETWEEN STR 23 RT AND STR 24 RT HAS CORROSION. REPLACED DOUBLER PER SRM 51-20-01. 2L72 4F RTA16NE 20040923001972004092300197NM 2004 9 23 372PA0058 120040909A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 AFT CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 45 TO RBL 45. REPLACED T-CAP PER EA 53-234. 2L72 4F RTA16NE 20040923001982004092300198 2004 9 23 249TR0035 420040815A2230734SUE23 COMPUTER BOEING737 7372K5 138448XNM AUTOTHROTTLES INOPERATIVE A PIDAO OTHER O OTHER CRCRUISE 1 SO05249TR 22598 AUTO THROTTLES BECAME INOP WHILE EN ROUTE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101 AND OPS CHECKED PER 22-31-01. 2L72 4F RTA16WE 20040924000032004092400003NE 2004 9 24 GTIA040735 220040817A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23803NK 48087 709816 POSSIBLE FUEL LEAK ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20040924000062004092400006WP 2004 9 24 GTIA040726 120040817A1410 B-NUT DOUG DC9 DC983 3022083WP AUX TANK LOOSE A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23832NK 49618 DTW - FOUND FORWARD CABIN HAS A HEAVY FUEL ODOR, AFT CABIN IS FINE. FOUND B-NUT LOOSE AT FORWARD AUX TANK VENT FITTING DRAIN LINE, TIGHTENED. (M) 2L72 4F RTA6WE 20040924000082004092400008NM 2004 9 24 USAA040475 120040812A5230 SKIN BOEING757 7572B7 1384964NM CARGO DOOR TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 PIT - FOUND SKIN WITH .250 INCH TEAR, STATION 1774 AFT CARGO DOOR, LOWER CORNER SKIN. INSTALLED DOUBLER PER SRM 52-30-01. (M) 2L72 4F RTA2NM 20040924000092004092400009WP 2004 9 24 GTIA040718 120040812A3260833605 PROXIMITY SWITCH DOUG DC9 DC983 3022083WP NLG FAILED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23836NK 53045 MCO - FLT 1862 - FOUND NOSE GEAR RED LIGHT ILLUMINATED SEVERAL TIMES DURING FLIGHT. DUE TO PROXIMITY SWITCH ELECTRONIC UNIT FAILURE, REMOVED AND REPLACED PSEU. (M) 2L72 4F RTA6WE 20040924000132004092400013NM 2004 9 24 USAA040445 120040722A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US 24548 PIT - FOUND FLOORBEAM CORRODED 27 INCH AREA, FLOOR SUPPORT BEAM FS 344 BETWEEN 10 INCH LBL AND 20 INCH RBL. REPLACED FLOORBEAM PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20040924000152004092400015NM 2004 9 24 USAA040443 120040810A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND SKIN GOUGED 1.60 INCH BY 3.20 INCH BY .017 INCH DEEP, FORWARD OF BS 1016 AND STRINGER 3L. INSTALLED DOUBLER PER SRM 53-00-01 AND EA 78850. (M) 2L72 4F RTA16WE 20040924000162004092400016NM 2004 9 24 USAA040444 120040723A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FRAME CRACKED .380 INCH, STATION 727D BETWEEN STRINGER 8R AND STRINGER 9R. CUT OUT CRACK AND INSTALLED 2 REPAIR DOUBLERS PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20040924000172004092400017NM 2004 9 24 USAA040446 120040713A575465C26603101 SKIN BOEING737 7374B7 1384702NM NR 3 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND LOEWR SKIN AND CORE WITH DELAMINATED AND CHAF DAMAGED 3 INCH BY 4 INCH, NR 3 SLAT T/E CORNER. REMOVED DELAMINATED SKIN AND CORE MATERIAL, INSTALLED NEW AND LOWER SKIN DOUBLER REPAIR PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924000192004092400019NM 2004 9 24 USAA040438 120040722A5350 FAIRING BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FAIRING COVER CRACKED 1 INCH, LEFT SIDE NUTTED FAIRING, NR 1 HINGE COVER. REMOVED CRACKED MATERIAL, INSTALLED DOUBLER PER EA 78848 AND SRM 51-60-00. (M) 2L72 4F RTA16WE 20040924000202004092400020NM 2004 9 24 USAA040442 120040812A5754 ATTACH BRACKET BOEING737 7374B7 1384702NM NR 2 SLAT GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND ATTACH BRACKET GOUGED .625 INCH LONG BY .625 INCH WIDE BY .035 INCH DEEP, NR 2 SLAT ACTUATOR ATTACH BRACKET OUTBOARD SIDE INBOARD FACE. BLENDED PER TYPICAL REPAIR 57-20-0-0A. (M) 2L72 4F RTA16WE 20040924000232004092400023WP 2004 9 24 GTIA040730 120040814A2131 CONTROLLER DOUG DC9 DC982 3022082WP CABIN PRESSURE MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23823NK 48020 LGA - FLT 779 - LEVEL AT FL280, FLOW LT ILLUMINATED AND CABIN ALT STARTED CLIMBING. PRESSURIZATION CONFIRMED FULL FORWARD. DESCENDED INITIATED AND CABIN PRESSURIZATED AT 17000 FLOW LIGHT OUT COMPLIED WITH QRH PROC. REMOVED AND REPLACED 7 CONTROLLER/SELECTOR WITH 5 SELECTOR. PERFORMED RATE LOGIC ALTITUDE SELECTION AND FLOW LIGHT CHECKS. (M) 2L72 4F A6WE 20040924000252004092400025WP 2004 9 24 GTIA040722 120040816A3260833605 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP LT MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23820NK 49126 LGA - FLT 779 - FOUND LEFT MAIN GEAR UNSAFE LIGHT CAME ON AND STAYED ON IN FLIGHT. FOLLOW QRH PROCEDURES CONT TO FLL AT .700 MACH. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. (M) 2L72 4F A6WE 20040924000272004092400027NM 2004 9 24 USAA040471 120040812A5320 SUPPORT ANGLE BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 1320-1340 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M) 2L72 4F RTA2NM 20040924000312004092400031WP 2004 9 24 GTIA040732 120040815A7120K22199SA31 ISOLATOR DOUG DC9 DC982 3022082WP NR 2 NACELLE SHIFTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 RSW - FOUND FORWARD LOWER ISOLATOR FOUND SHIFTED ON NR 2 PYLON. REPLACED FORWARD LOWER ISOLATOR. (M) 2L72 4F A6WE 20040924000332004092400033NM 2004 9 24 USAA040459 120040810A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU39393 27124 FOUND INTERCOSTAL CORRODED 2 SQUARE INCH AREA BY .020 INCH DEEP, BS 1161 TO 1681, BL 0. CORROSION LEVEL 1, TASK NR C53-251-03 AND 252-03. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-2 AND 51-40-2. (M) 2L72 4F RTA2NM 20040924000342004092400034WP 2004 9 24 GTIA040733 120040810A2510 HANDLE DOUG DC9 DC983 3022083WP PILOTS SEAT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 DTW - FLT 308 - FOUND CAPTAIN SEAT FORWARD AND AFT HANDLE BROKE OFF. (M) 2L72 4F RTA6WE 20040924000372004092400037WP 2004 9 24 GTIA040725 120040817A3297 CONDUIT DOUG DC9 DC982 3022082WP MLG WIRE OUT OF POSITION A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23820NK 49126 DTW - FLT 563 - AFTER TAKEOFF LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON/RED FOR ONE MINUTE AFTER ALL OTHER LANDING GEAR LIGHTS OUT. AS SLOWED TO 230 KIAS FOR QRH PROCEDURE LIGHT WENT OUT AND REMAINED OUT FOR REMAINDER OF FLIGHT. FOUND WIRE CONDUIT FROM GEAR UPLATCH SENSOR ARM IN THE PATH SLIGHTLY OF THE GEAR SWING MOTION. REPOSITIONED CONDUIT AND GEAR SWING PATH IS GOOD. (M) 2L72 4F A6WE 20040924000392004092400039NM 2004 9 24 USAA040468 120040812A5340 ATTACH ANGLE BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FASTENER HOLES AT RBL 10 ABOVE WATER TANK, STATION 1661 TO 1681. FABRICATED PART FROM .040 INCH 7075-T6 PER SRM 53-60-51. (M) 2L72 4F RTA2NM 20040924000422004092400042EU 2004 9 24 ASOA04541 120040712A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 39 AROUND THE NUT PLATES WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 39 IAW SRM 51-25-01 AND 51-25-00. (M) 2H72 4T RTA53EU 20040924000432004092400043EU 2004 9 24 ASOA04540 120040712A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040924000462004092400046NM 2004 9 24 USAA040360 120040726A5330654577566 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US 23316 PIT - FOUND SKIN CRACKED APPROXIMATELY .375 INCH CRACK, AFT CARGO DOOR FORWARD FRAME CUTOUT. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER PER EA 78434. (M) 2L72 4F RTA16WE 20040924000482004092400048NM 2004 9 24 USAA040394 120040726A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 FOUND STRINGER CRACKED 1.25 INCH, STRINGER 5A LEFT BS 1138 HORIZ STAB CUTOUT. SPLICED STRINGER PER TYPICAL REPAIR 53-80-04, SRM 53-00-01 FIG 221. (M) 2L72 4F RTA16WE 20040924000492004092400049NM 2004 9 24 AMTA200400985 120040804A5320 CHANNEL BOEING757 75723N 1384973NM LAVATORY FLOOR CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOND LEFT FORWARD LAV FLOOR CHANNEL, BS 340, LBL 20 TO LBL 30 LIGHT CORROSION. REMOVED AND REPLACED INTERCOSTAL CHANNEL IAW B757 SRM 51-40-02. (M) 2L72 4F RTA2NM 20040924000502004092400050NM 2004 9 24 ASAA0470005 120040628A5320143A750180 ANGLE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01622AS 30165 OAK - DURING C-CHECK, FOUND ZEE ANGLE CORRODED FORWARD CARGO COMPARTMENT RBL 21. REPAIR IAW SRM. (M) 2L72 4F RTA16WE 20040924000512004092400051NM 2004 9 24 ASAA0470008 120040628A53201496377 ANGLE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01622AS 30165 OAK - DURING C-CHECK, FOUND ZEE ANGLE CORRODED FROM STATION 727A TO 747 RT. REPAIRE IAW SRM. (M) 2L72 4F RTA16WE 20040924000522004092400052NM 2004 9 24 ASAA0410184 120040331A3350873100211 LIGHT BOEING737 737290C 138448VNM L1 DOOR INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE, FOUND EMERGENCY LIGHT PACK ABOVE L1 DOOR WILL NOT EXTINGUISH. REMOVED AND REPLACED LIGHT PACK ASSEMBLY. (M) 2L72 4F A16WE 20040924000532004092400053 2004 9 24 ASAA0480479 420040729A25653961896501 LANYARD DOUG DC9 DC983 3022083WP L2 DOOR SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA - DURING PREFLIGHT CHECK, FOUND AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040924000562004092400056NM 2004 9 24 USAA040396 120040729A5730 SKIN BOEING737 737301 1384611NM WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND SKIN DELAMINATED, 5 INCH BY 6 INCH AREA OF DELAMINATION, OUTBOARD END OF T/E. REMOVED DAMAGED CORE MATERIAL AND REPLACED, INSTALLED DOUBLERS PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040922000852004092200085EA 2004 9 22 SWIA200413808 120040906A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07943SW 7762 FS 280 LT FLOORBEAM LBL 9.0 IB AND OB ATTACH ANGLES CRACKED. ( ITEM FOUND AT C-CHECK INSPECTION.) REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-52-06, 51-42-13, 51-23-00, 51-21-11, 51-42-21 AND 51-25-16. 2L72 4F4 FRTA21EA E15NE 20040922000902004092200090EU 2004 9 22 04FDEA02689 120040916A5315 FLOORBEAM AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 AFT CARGO COMPARTMENT, BETWEEN FR 54 AND 54.2, FLOOR STRUCTURE RT SIDE, 3 AREAS OF CORROSION ON CLIP NUTS HOLE TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW A310 SRM 51-74-10, AND FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-15, TREATED PRIMED AND TOP COATED IAW A310 SRM 51-75-10. 2L72 4F4 FRTA35EU E13NE 20040922000922004092200092EU 2004 9 22 04FDEA02694 120040916A5347 SEAT TRACK AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 SEAT TRACK 0, SECTION BETWEEN FR73 TO FR80 HAS TWO DISCREPANT AREAS. TRACK 0 AT APPROX 12 INCHES AFT FROM FR 77 HAS 2 GOUGES INSIDE OF SCALLOPED AREA. TRACK 0 APPROX 10 INCHES AFT OF FR78 HAS CORROSION ON TOP OF TRACK AND IN SCALLOPED AREA. REMOVED CORROSION IAW SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REPAIRED TRACK BY REMOVING DAMAGED SECTION AND SPLICING IN A REPAIR SECTION IAW A310 SRM. 2L72 4F4 FRTA35EU E13NE 20040922000962004092200096EU 2004 9 22 04FDEA02698 120040916A5315 FLOORBEAM AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 FWD CARGO FLOORBEAM STRUCTURE FR33 NOTED INDICATION OF CRACK. REMOVED DAMAGED AREA IAW A310 SRM 53-10-15, AND REPAIRED BY INSTALLING A DOUBLER IAW A310 SRM 53-10-15. 2L72 4F4 FRTA35EU E13NE 20040922001162004092200116NM 2004 9 22 SWAA042729 120040920A53126546568524 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT BS 1016, 1 O'CLOCK, 2 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED BULKHEAD WEB PER EA. 2L72 4F RTA16WE 20040922001182004092200118NM 2004 9 22 SWAA042731 120040920A53106545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.5, LBL 32, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040922001422004092200142NM 2004 9 22 SWAA042665 120040914A53106547959 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME FWD FACE, CORRODED. REMOVED AND REPLACED CARGO DOOR FRAME CUTOUT PER SRM. 2L72 4F RTA16WE 20040922001432004092200143NM 2004 9 22 AALA20040912 120040828A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21642AA 24600 EMERGENCY LIGHT ON SIDE OF SEAT 21D INOPERATIVE. FOUND CONNECTOR LOOSE AT SIDEWALL. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040922001532004092200153NM 2004 9 22 DL73S040846 120040904A335020121 CHARGER BOEING737 737232 1384475NM EMERGENCY EXIT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27301DL 23073 EMERGENCY EXIT SIGN AT FWD LEFT DOOR AND OTHER LIGHTS ASSOCIATED WITH BATTERY PACK M1133 ARE INOP. FOUND THAT THIS BATTERY PACK WOULD NOT COMPLETELY SHUTOFF AND WAS DRAINING THE BATTERY. REPLACED THE RACK AND THE BATTERY. ALL NORMAL. 2L72 4F RTA16WE 20040922001592004092200159NM 2004 9 22 AALA20040904 120040827A3350 CONNECTOR BOEING757 757231 1384950NM EMERGENCY LIGHT MISSING A AALAK NONE L NO TEST ININSP/MAINT 1 SW21723TW 29378 DFW - EMERGENCY FLOOR TRACK LIGHTING END PLUG MISSING TO THE RIGHT OF SEAT 1B. INSTALLED END PLUG AT RIGHT OF SEAT 1B FOR EMERGENCY FLOOR TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040922001612004092200161NM 2004 9 22 SWAA042667 120040914A53116546532 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040922001622004092200162WP 2004 9 22 AALA20040936 120040906A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170425 49337 OVERHEAD EMERGENCY EXIT PATH LIGHTING AT ROWS 28-29 INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT PATH LIGHTING BATTERY AT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040922001652004092200165EU 2004 9 22 AALA20040940 120040903A3260 SENSOR AIRBUS300 A300B4605R 3930308EU LANDING GEAR DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2170073 516 JFK - UNABLE TO RETRACT LANDING GEAR ON TAKEOFF. RETURNED AND LANDED JFK WITHOUT INCIDENT. REPLACED RIGHT GEAR SENSORS AND TARGET BRACKET ASSEMBLY AND ACCOMPLISHED GEAR RETRACTION TEST PER M/M. SYSTEM GROUND CHECKED NORMAL. 2L72 4F RTA35EU 20040922001662004092200166NM 2004 9 22 SWAA042622 120040909A53116546532 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 480, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040922001682004092200168NM 2004 9 22 SWAA042639 120040911A52106550573 GATE BOEING737 7373H4 1384600NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR LOWER GATE CRACKED. REMOVED AND REPLACED LOWER GATE PER MM. 2L72 4F RTA16WE 20040922001702004092200170 2004 9 22 SWAA042669 420040914A25656557463 FITTING BOEING737 737301 1384611NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT FITTINGS CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20040922001722004092200172NM 2004 9 22 SWAA042671 120040914A57116546321 SPAR BOEING737 737301 1384611NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND RT WING UPPER REAR SPAR CHORD AT RSS 285, CRACKED. REMOVED AND REPLACED CHORD PER BAC DRAWING, ER, SRM. 2L72 4F RTA16WE 20040922001742004092200174NM 2004 9 22 SWAA042673 120040914A55126941313 SKIN BOEING737 737301 1384611NM RT HORZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN AT STATION 79, REAR SPAR, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040922001792004092200179NE 2004 9 22 DL76L040861 220040910A7240PW40603 COMBUST CHAMBER BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27181DN55695 25986 724178 ENGINE FAILED BORO OP 5067 COMBUSTION CHAMBER LINER CRACKED. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20040923000022004092300002SO 2004 9 23 2004F00390 120040917A6120 INDICATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE PROP TORQUE MALFUNCTIONED E A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO15267AS 120198 20001112 UPON TAKEOFF PILOT REPORTED THAT THE LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. ABORTED THE LAST LEG AND CHOSE TO LAND. A GROUND RUN UP DETERMINED THAT THE LT NP WAS READING CORRECTLY. THE CAUSE FOR THIS DESCREPANCY IS YET UNKNOWN. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20040923000032004092300003EU 2004 9 23 04FDEA02724 120040917A5347A5381312720000 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 MDCC SEAT TRACK SECTION AT R2, BETWEEN FR54 TO 8 INCHES AFT OF FR54.1 HAS DAMAGE TO THE SCALLOP LUGS. (ON EDGES AND BENEATH LUGS) REMOVED DAMAGE AND FOUND TO BE CRACKED IAW SRM 51-73-10. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040923000142004092300014NM 2004 9 23 P5CA0401207 120040914A5320 WEB BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FWD CARGO COMPARTMENT WEB CRACKED. REMOVED CRACKED WEB, FABRICATED NEW WEB AND INSTALLED. 2L74 4F4 F A20WE E20EA 20040923000252004092300025NM 2004 9 23 FWTA200431602 120040917A7997 WIRE BOEING767 767300 1385204NM GE CF6 CF680C2B7 NE LT ENGINE CHAFED A FWTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO19316LA 30842 704701 ENG OIL PRESS LGT ILLUM EICAS MSG /LT ENG OIL PRESS, OIL PRESS WAS ABOVE 15 PSI. FOUND WIRE CHAFFED AT 2 INCHES OF CANNON PLUG. OIL LOW PRESS, RELOCATION WIRE AND INSULATION IAW SWPM IAW MM 71-00-00. REJECT TAKE OFF AT 60K DUE TO LT ENG OIL PRESS LIGHT AND EICAS MESSAGE ILLUM. PERFORMED INSPECTION IAW AMM 05-51-14. NO DISCREPANCIES FOUND AT THIS TIME. 2L72 4F4 FRTA1NM E13NE 20040923000322004092300032CE 2004 9 23 GLBA20030716 120040907A5270 WARNING LIGHT BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE PAX DOOR ILLUMINATED A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03208GL UE208 CABIN DOOR ANNUN ILLUM IN FLIGHT, ADJUSTED CABIN DOOR SILL SWITCH. 2L72 4T4 TRTA24CE E26NE 20040923000372004092300037WP 2004 9 23 ASMF200409002 120040906A3411851AK PITOT TUBE DOUG DC9 DC987 3022087WP LT SIDE DAMAGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23754RA 49641 AIRCRAFT RETURNED TO PLATFORM, (PITOT STALL HEAT OFF) LIGHT TURNED ON. DURING MAINTENANCE REVISION, CAPTAIN PITOT TUBE WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 34-11-02, TEST CORRECT. 2L72 4F RTA6WE 20040923000502004092300050EU 2004 9 23 AALA20040937 120040906A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY65015 54557NE EMERGENCY LIGHT DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW211421K 11404 FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRT E25NE 20040923000522004092300052SW 2004 9 23 ALG2004F00035 120040614A6210206015001119 BLADE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL MAIN ROTOR HEAD DELAMINATED E ALGAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW03211EL2116 45251 IN CRUISE FLIGHT, AIRCRAFT COMMENCED AN APPROX 1/1 VERTICAL BEAT WITH AN UNUSUAL NOISE AND (HUM) IN THE AIRFRAME. PILOT DIVERTED TO FIELD LANDING SITE. AFTER SHUT-DOWN, PILOT FOUND BLADE SKIN DELAMINATING NEAR TIP. MAINTENANCE REMOVED AFFECTED BLADE AND INSTALLED SERVICEABLE MAIN ROTOR BLADE, BALANCED AND TRACKED IAW MM, OPS CHECK FLIGHT WAS GOOD. 1G71 3U3 U H2SW E1GL 20040923000532004092300053WP 2004 9 23 ASMF200407032 120040729A2720 PROXIMITY SENSOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE RUDDER LIMITER DIRTY W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23216AM 49586 AIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT TURNED OFF BEFORE TAKE OFF AND LT GENERATOR INOPERATIVE. PSEU TEST WAS PERFORMED, ALL CORRECT; RUDDER LIMITER PROXIMITY SWITCH WAS CLEANED AND CHECKED, RUDDER WAS ACTUATED WITH HYDRAULIC PRESSURE AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, D1-33 AND D1-34 RUDDER SENSOR TAG WAS ADJUSTED IAW MM 27-20-00 AND TESTED IAW MM 27-20-06, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040923000702004092300070EU 2004 9 23 KBM2004F00121 120040109A78100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENG EXHAUST WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2342 ENGINE EXHAUST SUPPORTS HEAT SHRINK IS WORN. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040923000722004092300072 2004 9 23 USA2004F00073 420040605A2565 SWITCH AIRBUS330 A330323 3930335EU PWA 4158 PW4158 NE SLIDE LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US AX0429 0388 EPSU (ESCAPE SLIDE LT SW EPSU R2) FAULTED DURING TEST. MAINTENANCE FOUND THE R2 SLIDE LIGHT SWITCH BAD. REMOVED AND REPLACED R2 SLIDE ASSY IAW MM. ALL TESTS OK. 2L72 4F4 FRTA46NM E24NE 20040923000732004092300073EU 2004 9 23 USA2004F00075 120040607A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19724UW14445 1122 THE AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E2GL 20040923000932004092300093EU 2004 9 23 KBM2004F00157 120040422A2150060018 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE A/C SYSTEM BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 A/C BELT BROKEN IN MID-FLIGHT. A/C SYSTEM INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040923001002004092300100WP 2004 9 23 ASMF200406030 120040626A2421 SELECTOR SWITCH DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE GENERATOR FAILED W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23583MD 49659 AIRCRAFT RETURNED TO PLATFORM, APU OUT OF SERVICE AND ENGINE GENERATORS WITHOUT INDICATION OF VOLTAGE AND FREQUENCY. CIRCUIT BREAKERS B1-204, B1-205 AND B1-206 WERE CHECKED AND SWITCH SELECTOR S1-99 WAS REPLACED IAW MM 24-21-01, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20040923001022004092300102WP 2004 9 23 ASMF200406032 120040627A3411HG280D80 CADC DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE NR 1 FAILED W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23583MD7675 49659 CAPTAIN REPORTED THAT DURING CRUISE AT 35,000 FEET, VERTICAL VELOCIMETER BAR FD TRI WAS OUT OF SERVICE AND CADC ABNORMAL PROCEDURE WAS PERFORMED. DURING TRANSIT CHECK AT TIJ, PITOTS AND STATIC PORTS WERE CHECKED BY OVERHEAT AND NO DAMAGE WAS DETECTED. PITOTS AND STATIC PORTS WERE DRAINED, CADC CONNECTOR WAS CLEANED AND STATIC CONNECTOR LINE WAS TIGHTENED, TEST CORRECT. DURING TRANSIT CHECK AT MEX, CADC NR 1 WAS REPLACED IAW MM 34-16-01, TEST CORRECT. DURING OVERNIGHT SERVICE, CADC NR 1 TEST WAS PERFORMED IAW MM 34-16-00, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040923001162004092300116NE 2004 9 23 ACO2004F00000 220040527A7261P1010 SCREEN BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE ENGINE MAKING METAL B ACORO OTHER J WARNING INDICATION APAPPROACH 1 SO05540CB12 FA135 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON FINAL. ENGINE WAS CHECKED AND FILTER HAD METAL IN IT. UPON FURTHER INSPECTION, BYPASS FILTER SCREEN APPEARED DAMAGED. AFTER CLOSURE INSPECTION, BYPASS FILTER SCREEN SEAM DETACHED. THIS WOULD ALLOW OIL TO FLOW UNFILTERED. ENGINE WAS REMOVED FOR MIO INSPECTION. 2L72 4T4 T A24CE E4EA 20040923001172004092300117GL 2004 9 23 CHQA000545 220040828A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ZONE 400 ODOR A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11265SK1172711727 145226 CAE311281 AFTER ROTATING AND ON CLIMBOUT DURING FLIGHT 3135 FROM CLT TO YYZ, THE CREW REPORTED A LAV SMOKE WARNING INDICATION ON EICAS. THE FLIGHT ATTENDANT NOTICED A LIGHT HAZE THROUGHOUT THE CABIN AND A BURNING ODOR. THE SMELL CLEARED UP DURING DESCENT. THE AIRCRAFT RETURNED TO THE FIELD AND PERFORMED AN OVERWEIGHT LANDING. AFTER TROUBLESHOOTING THE SMELL WAS ISOLATED TO THE NR 2 ENGINE. AIRCRAFT WAS FERRIED FROM CLT TO CMH. WHILE DOING ENGINE RUNS, THE E2 ITT WAS HIGH AND AN E2 LOW MARGIN MESSAGE APPEARED ON EICAS. THE SMELL WAS TROUBLESHOT DOWN TO THE NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD IAW EMB 145 JOBCARD CE720001. 2L72 4T4 FRTT00011ATTE6CH 20040923001272004092300127NM 2004 9 23 150AW0033 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 616. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001462004092300146NM 2004 9 23 2004UALA00781 120040821A2730 ELEVATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MALFUNCTIONED A UALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP29352UA 24320 RETURNED TO DEN WITH ELEVATOR PROBLEM. NO FAULT HAS BEEN IDENTIFIED WITHIN THE ELEVATOR SYSTEM. THE FOLLOWING ACTIONS WERE TAKEN IN THE COURSE OF TROUBLESHOOTING:1. PITOT LEAK CHECK OF ELEVATOR FEEL SYSTEM. ACCOMPLISHED WITH NO LEAKS FOUND. 2. HORIZONTAL STAB TRIM RIG CHECKED GOOD USING TREMMLE BAR, 3. STAB TRIM LIMIT SWITCHES CHECKED GOOD. 4. LT ELEVATOR PCU AND BOTH AUTOPILOT SERVOS WERE ADJUSTED. 5. ELEVATOR CABLE TENSION CHECKED. 2L72 4F4 FRTA16WE E2GL 20040923001492004092300149NM 2004 9 23 2004UALA00785 120040825A2612 FIRE DETECTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU MALFUNCTIONED A UALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP29202UA 24717 ON TAXI OUT, RECEIVED AN APU FIRE WARNING. MAINTENANCE INSPECTED APU COMPARTMENT AND NO EVIDENCE OF FIRE DAMAGE OR OVERHEAT CONDITION WERE NOTED. INSPECTED APU OVERHEAT DETECTION SYSTEM AND FOUND APU TAILPIPE OVERHEAT DETECTOR LOOP M717 SHORTED TO GROUND. REPLACED APU OVERHEAT DETECTOR LOOP M717. 2L72 4F4 FRTA16WE E2GL 20040923001702004092300170NM 2004 9 23 DL757040866 120040913A5330146N31111 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27620DL 22910 FUSELAGE SKIN REPAIRED AT THE SKY RADIO ANTENNA CUTOUT AT STA 1320 AND BL 0. REPAIRED IAW ERA 092512-14. 2L72 4F RTA2NM 20040923001712004092300171NM 2004 9 23 DL76S040867 120040913A2530 COFFEEMAKER BOEING767 767332 1382001NM GALLEY CONTAMINATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27131DN 24852 DIVERTED TO KJFK WITH REPORTED FUMES IN AFT GALLEY. UNKNOWN SOURCE, BUT REPORTED AS BURNING PLASTIC ODOR, WHICH DID NOT GO AWAY EVEN AFTER TURNING OFF UTILITY BUSSES AND RECIRC FANS. ATL/TMC NOTIFIED AT 1055Z. AFTER OPERATING NR 4L COFFEEMAKER FOUND DEBRIS UNDER POT. CONFIRMED SMELL WITH FLT CREW. OPERATED ALL C/MS. CHECKED E AND E COMPT, AFT CARGO. NO FURTHER FUMES. OK FOR SERVICE. 2L72 4F RTA1NM 20040923001812004092300181NM 2004 9 23 SWAA042739 120040921A55536546872 FITTING BOEING737 7373A4 1384585NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER SPAR ATTACH FITTINGS AIRCRAFT SIDE, FWD LT FITTING AFT LUG AFT FACE CORRODED. REPAIRED VERTICAL STAB FITTINGS PER ER. 2L72 4F RTA16WE 20040923001862004092300186NM 2004 9 23 372PA0052 120040909A5320 PAN BOEING737 737306 13844BGNM LAV SER PANEL CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 AFT LAV SERVICE PANEL PAN HAS CORROSION AROUND DUMP SHOOT CONNECTION. REPLACED CORRODED CHANNELS P/N 69-36677-1 AND 69-36677-2 PER SRM 51-40-02 AND DRAWING 65-45781. REMOVED MINOR CORROSION FROM PAN PER SRM 51-20-01 AND SRM 51-40-00. 2L72 4F RTA16NE 20040924000012004092400001 2004 9 24 GTIA040721 420040811A2565 LANYARD DOUG DC9 DC983 3022083WP L1/R1 DOORS MISINSTALLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 DTW - FOUND L1 AND R1 DOOR SLIDES INFLATION LANYARDS NOT CONNECTED PROPERLY. CONNECTED LANYARDS L1 AND R1 DOOR SLIDES. (M) 2L72 4F RTA6WE 20040924000042004092400004NM 2004 9 24 USAA040474 120040812A5230 SKIN BOEING757 7572B7 1384964NM CARGO DOOR TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND SKIN 2.5 INCH TEAR, STATION 1772 AFT CARGO DOOR UPPER EDGE SKIN. INSTALLED DOUBLER PER EA 95708. (M) 2L72 4F RTA2NM 20040924000052004092400005 2004 9 24 GTIA040720 420040810A2565 BOTTLE DOUG DC9 DC983 3022083WP R1 SLIDE DISCHARGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 DTW - FOUND R1 SLIDE PACK PRESS GAUGE READS IN RED. REMOVED AND REPLACED R1 EVACUATION SLIDE. (M) 2L72 4F RTA6WE 20040924000072004092400007NE 2004 9 24 GTIA040734 220040818A72205000350010 GUIDE VANE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 709816 DTW - NR 1 ENGINE IGV HAS A HAIRLINE CRACK ON THE VANE ATTACHMENT WELD AT THE 3:30 POSITION APPROX 2.750 INCH LONG. REMOVED AND REPLACED IGV. (M) 2L72 4F4 F A6WE E9NE 20040924000122004092400012NM 2004 9 24 USAA040441 120040812A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 FOUND SKIN CRACKED 1.5 INCH, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT. INSTALLED DOUBLER PER SRM 53-10-01 FIG 202. (M) 2L72 4F RTA16WE 20040924000182004092400018NM 2004 9 24 USAA040473 120040812A5340 ATTACH ANGLE BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND ATTACH ANGLE CRACKED .5 INCH, FASTENER HOLES, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M) 2L72 4F RTA2NM 20040924000212004092400021WP 2004 9 24 GTIA040728 120040811A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2L72 4F A6WE 20040924000242004092400024NE 2004 9 24 GTIA040731 220040812A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RIGHT FAILED A GTIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL23803NK 48087 48087 FOUND RIGHT ENGINE FAILED AT 800 FEET DURING CLIMB-OUT FROM RSW. REPLACED NR 2 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20040924000262004092400026NM 2004 9 24 USAA040472 120040812A5740 ATTACH ANGLE BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 FOUND ATTACH ANGLE WITH .375 INCH CRACK, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M) 2L72 4F RTA2NM 20040924000412004092400041WP 2004 9 24 GTIA040677 120040720A3320 LIGHT DOUG DC9 DC983 3022083WP CABIN ODOR A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23826NK 49391 FOUND 2 HOURS INTO FLIGHT, FLIGHT ATTENDANTS COMPLAINED OF ACRID ODOR ROWS 22 AND 23 RIGHT SIDE. TURNED OFF SIDEWALL LIGHTING THE ODOR WENT AWAY. RELAMPED CEILING LIGHTS AT ROW 22 DEF AND LOWER SIDEWALL LIGHTS AT 22 DEF. OPS CHECK OK. (M) 2L72 4F RTA6WE 20040924000452004092400045NM 2004 9 24 USAA040359 120040726A5300656571034 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55230 22956 PIT - FOUND CHANNEL CRACKED 2 INCHES AND 1.5 INCHES, BETWEEN BS 727D AND BS 727E. REPLACED PART NR 65-65710-34. (M) 2L72 4F RTA16WE 20040924000572004092400057NM 2004 9 24 USAA040397 120040801A53206546812169 SUPPORT BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 FOUND SUPPORT CORRODED 2 INCHES BY 20 INCH AREA, INTERCOSTAL AT FS 986.5-967 LBL 18. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20040924000602004092400060NM 2004 9 24 USAA040386 120040721A575465C26602108 SKIN BOEING737 7373B7 1384580NM NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US51331 23315 FOUND SKIN AND CORE BONDED 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED NEW CORE AND TOP SKIN PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924000612004092400061NM 2004 9 24 USAA040393 120040723A57536546431285 SKIN BOEING737 737301 1384611NM TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 PIT - FOUND SKIN DELAMINATED 12 INCHES BY 3 INCHES WIDE DELAMINATED, LT WING T/E FLAP, TRAILING EDGE DELAMINATED, 15 INCHES FROM INBOARD END. REMOVED SKIN AND CORE, INSTALLED NEW SECTION AND TOP DOUBLER PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924000622004092400062EU 2004 9 24 ASOA04556 120040722A5330 SKIN AEROSPATR72 ATR72212 8680945EU FUSELAGE DENTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, A DENT IN THE SKIN BETWEEN FS 38 AND FS 39, LEFT STRINGER 17 AND 18 WAS FOUND TO BE BEYOND LIMITS. MAINTENANCE REPAIRED THE SKIN BETWEEN FS 38/39, LEFT STRINGER 17 AND 18 IAW SRM 53-00-00. (M) 2H72 4T RTA53EU 20040924000632004092400063NE 2004 9 24 ASOA04505 220040705A732073664310 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUEL SYSTEM MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11820AS 7188 FLT 4124 - DURING CLIMB-OUT FROM TRI-ATL, THE CREW NOTICED A LARGE FUEL DISPARITY BETWEEN THE PEFORMANCE INITIALIZATION PAGE AND THE TOTAL FUEL ON THE EICAS AND OVER THE FOLLOWING TEN MINUTES THE FUEL QUANTITY DROPPED 2,000 LBS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETUREND TO TRI, LANDIGN SAFELY. MAINTENANCE RESET THE FUEL COMPUTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040924000652004092400065EA 2004 9 24 ASOA04557 120040801A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11886AS 7531 DURING A C-CHECK IN MCN, THE PASSENGER DOOR STRUCTURE BELOW THE TOP STEP AFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR EDGE MEMBER BELOW THE TOP STEP AFT IAW ASA EO 600-52-0043. (M) 2L72 4F RTA21EA 20040924000672004092400067NM 2004 9 24 USAA040371 120040728A5414 PANEL BOEING737 7373B7 1384580NM PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND PYLON CRACKED .5 INCH, UPPER PYLON SKIN AT ACCESS PANEL OPENING FOR PANEL 5827R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M) 2L72 4F RTA16WE 20040924000692004092400069NM 2004 9 24 USAA040378 120040728A5740695988632 FITTING BOEING737 7373B7 1384580NM RT WING GALLED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND GALLED FITTING, MLG WALKING BEAM, RIGHT WING REAR SPAR, STATION 200. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BMM 20-50-11-2-912-002 FIG 202. (M) 2L72 4F RTA16WE 20040924000702004092400070NM 2004 9 24 USAA040381 120040729A5740 FITTING BOEING737 7373B7 1384580NM RT WING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND FITTING CORRODED .25 INCH AREA, RIGHT WING AFT SPAR AND LG BEAM GEAR DOOR HINGE POINT OUTBOARD. REAMED AND COUTNERSINK NEW FITTING PER MM 20-50-11-2-912-002 FIG 202. (M) 2L72 4F RTA16WE 20040924000712004092400071NM 2004 9 24 MEX2004002 120040101A274042G1141 SWITCH DOUG MD88 MD88 3023688NM STABILIZER FAILED A ASMFO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW23160PL 49763 CAPTAIN REPORTED THAT DURING FLIGHT THE LIGHT OF 'AIRFOIL ICE PROTECT PRESS ABNORMAL' CAME ON, ALTHOUGH THE ANTI-ICE PROTECTION WAS SHUTOFF. AT MEX STATION, THE SYSTEM WAS VERIFIED AND IT WAS DETECTED THAT AFTER A SYSTEM ANTI-ICE CYCLE, THE MENTIONED LIGHT CAME ON. THE SWITCH S1-146 WAS REPLACED AND SYSTEM TESTED IAW MM 30-10-10, ALL CORRECT. (M) 2L72 4F RTA6WE 20040924000732004092400073NM 2004 9 24 UIEA200400034 120040329A261251291009 FIRE LOOP BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 2 ENGINE CHAFED A UIEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15526MC 22337 517658 AT APPROXIMATELY 10,000 FT, NR 2 ENIGNE 'A' LOOP WAS INDICATING 7 UNITS, 'B' LOOP INDICATING 2.5. COMPLETED FHB 3.26.10 PROCEDURES NACELLE TEMPERATURE INDICATION ABNORMAL. RETARDED THROTTLE NO CHANGE, 30 SECON LATER 'A' LOOP INDICATES 9 PLUS, 'B' LOOP FLUCTUATES BETWEEN 2.5 AND 7.5. ENGINE FAILURE SHUTDOWN CHECKLIST ACCOMPLISHED. NR 2 ENGINE 'B' LOOP FOUND CHAFFING WIRES. REPAIRED WIRES AS PER SWPM 20-20-00 AND OPERATION CHECK SATISFACTORY AS PER MM 26-01-00. (M) 2L74 4F4 FRTA20WE E23EA 20040924000742004092400074EA 2004 9 24 ASOA04504 120040705A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11835AS9245 7258 DURING CLIMB-OUT FROM DFW-SHV, AT APPROXIMATELY 14,000 FEET AND 290 KTS THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT RETURNED TO DFW. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT (FECU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040924000752004092400075NM 2004 9 24 TSAA0475030 120040220A7500577957 DUCT BOEING737 7372T4 1384492NM NR 1 ENG FUEL HEFAILED A TSAAO OTHER J WARNING INDICATION CLCLIMB 1 WP13808AL 23445 FLT 286 - LIH-HNL - PASSING 10,000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INSTRUMENTS IN GREEN. RETARDED NR 1 ENGINE AND THE LIGHT WENT OUT. REPLACED NR 1 ENGINE FUEL HEAT DUCT DUE TO CRACKED WELD. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040924000762004092400076EA 2004 9 24 ASOA04506 120040705A2621365000183 EXTINGUISHER CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11920EV1201144 7810 DURING CLIMB-OUT FROM DFW-ICT, THE CREW RECEIVED A CARGO BTL LOW CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH AND THE BOTTLES DID NOT TEST SUCCESSFULLY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE HARD CARGO FIRE EXTINGUISHER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040924000772004092400077EA 2004 9 24 ASOA04455 120040626A3397487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECKI N MCN, THE FORWARD EMEGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE RIGHT AND LEFT EMEGENCY EXIT LIGHTS AND THE FLOOR TRACK LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040924000782004092400078EA 2004 9 24 A6WA200440025 120040221A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SMOKE A A6WAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31408AW 7568 SMOKE FROM APU, SHUTDOWN APU AND BLEW BOTTLE. REMOVED AND REPLACED APU FIRE EXTINGUSHER IAW AMM 26-22-07. OPS CHECK GOOD. PERFORMED OPS CHECK OF APU, NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20040924000792004092400079EA 2004 9 24 ASOA04534 120040729A5210H341437 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11855AS 7395 FLT 4425 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040924000802004092400080EU 2004 9 24 ASOA04551 120040714A5753S5751203220300 RIB AEROSPATR72 ATR72212 8680945EU TE FLAP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 7 FOR THE CAM GUIDE WAS FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 7 FOR THE CAM GUIDE IAW SRM 51-25-03 AND 51-25-01. (M) 2H72 4T RTA53EU 20040924000812004092400081 2004 9 24 USAASA04076 420040804A2565 STRAP AIRBUSA321 A321211 3930370EU ESCAPE SLIDE CUT A USAAK NONE O OTHER ININSP/MAINT 1 EA19171US 1465 CLT - DURING THE SLIDE SHOP VISIT, FOUND THE SLIDE ENCLOSURE DOOR RETAINING STRAPS CUT AT THE DOOR ATTACH POINT. MAINTENANCE RETURNED THE SLIDE TO THE VENDOR FOR REPAIR. (M) 2L72 4F RTA28NM 20040924000822004092400082EU 2004 9 24 ASOA04546 120040713A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT INBOARD SEAT TRACK FROM FRAME 13 TO FRAME 17A WERE FOUND TO BE GOUGED AND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD SEAT TRACKS FROM FRAME 13 TO FRAME 18 IAW SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RTA53EU 20040924000832004092400083NM 2004 9 24 USAA040448 120040714A575465C26602223 SKIN BOEING737 7374B7 1384702NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND EXT SKIN AND CORE BOND DELAMINATED AND CHAFE WEAR 3 INCH BY 5 INCH AREA, UPPER OUTBOARD T/E AFT CORNER OF NR 2 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED FILLER AND INTERNAL AND UPPER DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924000842004092400084NM 2004 9 24 USAA040461 120040819A5210 STOP BOEING737 7373B7 1384580NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND .5 INCH CRACK , AFT DOOR STOP NR'S 4, 5 AND 6 AT PAN. INSTALLED DOUBLERS PER TYPICAL REP 52-10-16. (M) 2L72 4F RTA16WE 20040924000852004092400085NM 2004 9 24 USAA040464 120040805A5553 FITTING BOEING737 7374B7 1384702NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND LUG CORRODED .150 INCH DIAMETER SPOTS (TWO EACH), RIGHT AFT OUTBOARD VERTICAL STAB ATTACH LUG ON FUSELAGE. REAMED AND REBUSHED PER EA 78920. (M) 2L72 4F RTA16WE 20040924000872004092400087NM 2004 9 24 USAA040453 120040731A5320 CHANNEL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND Z-CHANNEL CORRODED .25 INCH AREA (6 EACH), MED ENTRANCE FLOOR AREA OUTBOARD SILL SUPPORT AROUND FASTENER HOLES. REPLACED Z-CHANNEL PER BOEING DWG 65-17688. (M) 2L72 4F RTA16WE 20040924000882004092400088NM 2004 9 24 USAA040463 120040805A5315 FLOORBEAM BOEING737 7374B7 1384702NM FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND BEAM CORRODED 20 INCHES LONG BY .035 INCH, STATION 294 LBL 10 TO RBL 10. INSTALLED SPLICE PER SRM 53-10-08. (M) 2L72 4F RTA16WE 20040924000912004092400091NM 2004 9 24 USAA040479 120040806A5542 SKIN BOEING737 737301 1384611NM RUDDER GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND RUDDER GOUGED .25 INCH BY 1 INCH BY .045 INCH DEEP, MAIN PCU ATTACH FITTING. REPLACED RUDDER PER JPC J3-65-27301. (M) 2L72 4F RTA16WE 20040924000922004092400092NM 2004 9 24 USAA040481 120040806A5320 ANGLE BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND ZEE ANGLE CORRODED 3 INCH BY 30 INCH AREA, AFT ENTRY DOOR SILL BS 947-1006. REPLACED Z-ANGLE PER SRM 51-10-2. (M) 2L72 4F RTA16WE 20040924000992004092400099NM 2004 9 24 USAA040491 120040817A5320654962156 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND INTERCOSTAL CRACKED 2 INCHES, STATION 787 FLOOR ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20040924001002004092400100NM 2004 9 24 USAA040492 120040822A5210 WEB BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - MED INNER DOOR WEB HAS .375 INCH CRACK, AFT SIDE AT NR 5 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED DOUBLER PRE TYPICAL REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20040924001012004092400101NM 2004 9 24 USAA040462 120040818A5230 SKIN BOEING737 7373B7 1384580NM AFT CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 PIT - FOUND AFT CARGO DOOR CRACKED 1.5 INCH BY 1 INCH, MIDDLE OF DOOR 6 INCH AFT OF L/E. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-01, REV A. (M) 2L72 4F RTA16WE 20040924001022004092400102NM 2004 9 24 USAA040465 120040813A57306546435238 SKIN BOEING737 7373B7 1384580NM RT WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU48131 24412 PIT - FOUND SKIN TO CORE BOND DELAMINATION 11.25 INCH BY 7.25 INCH, RIGHT WING OUTBOARD AFT FLAP TOP SKIN TO CORE BOND, CENTER. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE SECTION AND DOUBLER ASSY PER T/R 57-50-39A AND 51-70-10. (M) 2L72 4F RTA16WE 20040924001052004092400105NM 2004 9 24 USAA040496 120040822A5210 PAN BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND MED DOOR PAN CRACKED .250 INCH, AFT SIDE AT NR 4 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED A DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20040924001072004092400107NM 2004 9 24 USAA040502 120040809A5343 SUPPORT FITTING BOEING737 737301 1384611NM RT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND RIGHT MLG SUPPORT FITTING CRACKED .460 INCH, NR 2 HOLE OF RIGHT MLG SUPPORT FITTING, VERTICAL LEG OF AFT SPAR. INSTALLED BOEING MLG FITTING, OVERSIZED NR 3 HOLE, INSTALLED FREEZE PLUG PER EA 78861, EO M3-56-93810. (M) 2L72 4F RTA16WE 20040924001082004092400108NM 2004 9 24 USAA040483 120040805A5320 SHIM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND SHIM AND ANGLE CORRODED PLUS 1 INCH BY 20 INCH AREA, BL 0 FROM BS 927-947. FABRICATED NEW ANGLE AND SHIM, ASSEMBLED AND INSTALLED PER SRM 653-60-51, 51-10-1. (M) 2L72 4F RTA16WE 20040924001112004092400111NM 2004 9 24 USAA040503 120040813A5343 SUPPORT FITTING BOEING737 737301 1384611NM RT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND RIGHT MLG SUPPORT FITTING CRACKED .460 INCH, NR 2 HOLE OF RT MLG SUPPORT FITTING, VERTICAL LEG OF AFT SPAR. INSTALLED REINFORCING DOUBLER TO AFT SPAR UPPER WING SURFACE PER EA 78860, EO 5702V054. (M) USAA 2L72 4F RTA16WE 20040924001122004092400112NM 2004 9 24 USAA040486 120040805A5510 BAR BOEING737 737301 1384611NM STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND STABILIZER BAR CORRODED, 7 EACH 1.5 INCH DIAMETER AREAS, RSS 181 LT WING. REMOVED STABILIZER BAR AND REPLACED WITH NEW PER WORK CARD J332-11-01 STEP NR 17. (M) 2L72 4F RTA16WE 20040924001142004092400114NM 2004 9 24 USAA040499 120040729A5753654643099 SKIN BOEING737 737301 1384611NM FORE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND TOP SKIN DENTED WITH DELAMINATION, 1.5 INCH BY .025 INCH AREA, LEFT INBOARD FOREFLAP TOP CAMBER 58 INCHES FROM OUTBOARD END. INSTALLED TOP DOUBLER WITH FILLER MATERIAL PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924001182004092400118NM 2004 9 24 USAA040478 120040805A5320 ANGLE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND ANGLE CRACKED .5 INCH, BS 328 BETWEEN S20L AND S21L. REMOVED CRACKED ANGLE AND MFG NEW FROM EXTRUSION PER BOEING DWG 65-54892 AND SRM 51-40-03, 53-10-07. (M) 2L72 4F RTA16WE 20040924001202004092400120NM 2004 9 24 USAA040460 120040813A5210 SKIN BOEING737 7373B7 1384580NM DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND SKIN CRACKED .1875 INCH, LOWER AFT CORNER EDGE. REMOVED DAMAGED AREA, AND INSTALLED DOUBLER PER SRM 52-00-01. (M) 2L72 4F RTA16WE 20040924001212004092400121NM 2004 9 24 AMTA200400975 120040804A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND FLOOR SUPPORT AT BUTT LINE ZERO FROM FS 1661 TO 1681 HAS EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0. (M) 2L72 4F RTA2NM 20040924001222004092400122NM 2004 9 24 USAA040385 120040701A57536546486156 SKIN BOEING737 737401 1384701NM TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19423US42694 23990 PIT - FOUND FLAP T/E SECTION HAS 2 INCH AREA DELAMINATION, 25 INCHES FROM INBOARD EDGE, 3 INCHES FROM L/E. REMOVED AND REPLACED DAMAGED/DISBONDED AREA AND INSTLALED REPAIR DOUBLER PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040927000022004092700002 2004 9 27 SWAA042760 420040922A2565D31354 SLIDE BOEING737 7372T4 1384492NM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C1 CHECK, FOUND 2 EACH DOOR EVAC SLIDES OUT OF ADJUST AT THE L2 AND R2 DOORS. ADJUSTED BOTH L2 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F A16WE 20040927000032004092700003NM 2004 9 27 SWAA042761 120040922A335007912 COVER BOEING737 7372T4 1384492NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C1 CHECK, FOUND 2 EACH EEPLS COVERS AT ROW 19 DEF AND ROW 10 DEF TO ROW 12 DEF, LOOSE. SECURED EEPLS COVERS PER MM. 2L72 4F A16WE 20040927000042004092700004NM 2004 9 27 SWAA042762 120040922A335007912 COVER BOEING737 7372T4 1384492NM EMERGENCY LIGHT CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS AT ROWS 1 DEF TO 2 DEF AND 20 DEF, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F A16WE 20040927000052004092700005NM 2004 9 27 SWAA042763 120040922A53306545778556 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 914, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040927000082004092700008NM 2004 9 27 CALA0400640 120040917A5414 ACCESS PANEL BOEING737 7373T0 1384582NM NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712349 23587 INSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5724 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20040927000102004092700010NM 2004 9 27 CALA0400642 120040918A5315 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717133 29282 INSPECTION FOUND UPPER FLANGES OF FLOORBEAM CORRODED AT BS 720. THE FLOORBEAM WAS REPAIRED IAW SRM 51-40-05. 2L72 4F RTA2NM 20040927000122004092700012 2004 9 27 234TR0020 420040812A22104038891916 COMPUTER BOEING737 737228 13844AGNM FCC MALFUNCTIONED A PIDAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO05234TR 23004 BOTH A&B AUTO PILOTS DISENGAGE IN SMOOTH AIR, LEVEL FLIGHT, WITHOUT PROVOCATION. REPLACED B-SYSTEM FCC COMPUTER. OPS CHECKS NORMAL PER MM 22-11-331. 2L72 4F RTA16WE 20040927000142004092700014NM 2004 9 27 372PA0066 120040909A5320 WEB BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 CLOSE OUT WEB ON FWD FRAME AT BS 794 HAS CORROSION FROM STR 25 RT TO STR 23 RT. REPLACED WEB PER SRM 53-60-15 AND SRM 51-70-13. 2L72 4F RTA16NE 20040927000162004092700016NM 2004 9 27 0401286638 120040720A5412 BULKHEAD BOEING747 747251B 1384892NM NR 2 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01638US 23549 DURING H-CHECK FOUND CRACK IN NR 2 PYLON ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 66-165162. 2L74 4F A20WE 20040927000182004092700018NM 2004 9 27 372PA0065 120040909A5347 SEAT TRACK BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 SEAT TRACK AT RBL 45 CORRODED IN NUMEROUS PLACES FROM BS 328 TO BS 480. REPLACED SEAT TRACK PER SRM 51-10-02, SRM 53-00-52, AND DWG 65-46814. 2L72 4F RTA16NE 20040927000252004092700025SO 2004 9 27 CHQA000509 120040615A3350 POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260SK 145128 CABIN FLOOR EMERGENCY LIGHTING FROM ROW 8 TO REAR OF CABIN INOP. REMOVED AND REPLACED POWER SUPPLY NR 4 IAW EMB 145MM 33-50-04. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20040927000262004092700026NM 2004 9 27 SWAA042767 120040922A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040927000282004092700028NM 2004 9 27 SWAA042769 120040922A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT UPPER AFT RADIUS CRACKED. REPAIRED DOOR SKIN CUTOUT PER SRM. 2L72 4F RTA16WE 20040927000302004092700030NM 2004 9 27 SWAA042771 120040922A57536573731 SKIN BOEING737 7377H4 1384404NM LT WING FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29752SW 29804 DURING SCHEDULED 5Y CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED LT WING INBOARD AFT FLAP PER SRM. 2L72 4F RTA16WE 20040927000312004092700031NM 2004 9 27 SWAA042747 120040921A57436567172 FITTING BOEING737 737301 1384611NM LT & RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND BOTH RT AND LT MLG SUPPORT BEAM AFT STABILIZER FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM. 2L72 4F RTA16WE 20040927000322004092700032NM 2004 9 27 SWAA042748 120040921A53116547959 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT FWD FRAME AFT FACE AT BS 794.3, RBL 25, WL 156, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040927000332004092700033NM 2004 9 27 SWAA042749 120040921A53156545812 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 328, RBL 45, CORRODED. REPAIRED FLOORBEAM WEB PER ER. 2L72 4F RTA16WE 20040927000342004092700034NM 2004 9 27 SWAA042750 120040921A53306545890 BEAR STRAP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND 2 EACH BEAR STRAPS AT FWD ENTRY DOOR UPPER AND LOWER HINGE CUTOUTS, CRACKED. REPAIRED SKIN SECTIONS PER ER. 2L72 4F RTA16WE 20040927000352004092700035NM 2004 9 27 SWAA042751 120040921A53116546554 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS 847, RBL 30, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040927000362004092700036NM 2004 9 27 372PA0077 120040909A5311 FRAME BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 FRAME CRACKED IN RADIUS AT BS 460 AT STR 25 LT. REPAIRED PER SRM 51-70-11. 2L72 4F RTA16NE 20040927000372004092700037NM 2004 9 27 372PA0078 120040909A5311 FRAME BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 FRAME CRACKED IN RADIUS AT BS 480 AT STR 25 LT. REPAIRED PER SRM 51-70-11. 2L72 4F RTA16NE 20040927000382004092700038NM 2004 9 27 SWAA042752 120040921A53116546525 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 380, LBL 6 TO RBL 6, CORRODED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040927000392004092700039NM 2004 9 27 SWAA042753 120040921A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 370, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040927000402004092700040NM 2004 9 27 SWAA042754 120040921A53306545768 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 351 TO BS 361 STRINGER 28R, CORRODED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040927000412004092700041NM 2004 9 27 SWAA042755 120040921A53156976148 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 1010, LBL 39, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB PER SRM. 2L72 4F RTA16WE 20040927000422004092700042NM 2004 9 27 SWAA042756 120040921A53206545833 WEB BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS AT BS 188 TO BS 196, STRINGER 17L AND BS 188 TO BS 196, STRINGER 17R. REMOVED AND REPLACED FLOORBEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20040927000432004092700043NM 2004 9 27 SWAA042757 120040921A53146545866 KEELBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CHORD AT BS 500C, STRINGER 28R, CORRODED. REPAIRED CHORD PER ER. 2L72 4F RTA16WE 20040927000442004092700044NM 2004 9 27 SWAA042758 120040922A33503071BPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29764SW 27878 EEPLS AT ROW 11 ABC, INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040927000452004092700045NM 2004 9 27 372PA0051 120040909A5420 ACOUSTIC LINER BOEING737 737306 13844BGNM NR 1 NACELLE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 NR 1 ENGINE FWD ACOUSTICAL PANEL AT 6 O'CLOCK POSITION CRACKED. REPLACED PANEL PER MM 72-33-02. 2L72 4F RTA16NE 20040927000462004092700046NM 2004 9 27 372PA0057 120040909A5320 INTERCOSTAL BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 INTERCOSTAL HAS CORROSION, AFT CABIN BS 967 TO BS 986.5 AT RBL 18. REPLACED INTERCOSTAL PER SRM 51-10-01. 2L72 4F RTA16NE 20040927000472004092700047NM 2004 9 27 372PA0059 120040909A5347 GALLEY TRACK BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 GALLEY SUPPORT AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES AT BL 0. REPLACED GALLEY SUPPORT PER SRM 51-10-2 AND SRM 51-40-00. 2L72 4F RTA16NE 20040927000492004092700049SO 2004 9 27 CHQA000526 120040727A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265SK 145226 FIRST SECTION OF PASSENGER EMERGENCY FLOOR LIGHTING IS INOP. REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY. OPERATIONAL CHECK IS GOOD AT THIS TIME. 2L72 4T RTT00011AT 20040927000512004092700051SO 2004 9 27 CHQA000527 120040804A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281SK 145391 FIRST SECTION OF FLOOR EMERGENCY PROXIMITY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY LIGHT STRIP NR 1 IAW EMB 145 AMM 33-50-12. 2L72 4T RTT00011AT 20040927000542004092700054WP 2004 9 27 0401389609 120040820A2810 FUEL TANK DOUG DC9 DC932 3022066WP RT WING LEAKING A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01609NW 47234 FLIGHT CREW NOTICED A FUEL IMBALANCE OF 1200 LBS BETWEEN LEFT AND RIGHT MAIN WING FUEL TANKS WHILE AT CRUISE. CREW HAD TO MANUALLY CROSSFEED THE FUEL AND ELECTED TO DIVERT TO ALTERNATE. THE LANDING AT GRB WAS UNEVENTFUL BUT NO MENTION OF COM PROCEDURES OR IF AN EMERGENCY WAS DECLARED. MAINTENANCE AT GRB CONFIRMED A FUEL LEAK FROM THE RIGHT WING AND LATER MSP SEALED A FUEL LEAK AT THE RIGHT INBOARD FLAP HINGE. ALSO DISCOVERED, WAS AN ERRONEOUS READING FROM THE RIGHT WING FUEL QUANTITY INDICATOR WHICH WAS ALSO REPLACED LATER AT MSP. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040927000562004092700056WP 2004 9 27 0401379961 120040821A215020495055 COOLING TURBINE DOUG DC9 DC931 3022065WP RT SYSTEM ODOR A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01924RW 47185 DURING CLIMBOUT FROM MSP, THE FLIGHT CREW NOTICED THAT THE RIGHT AIR CONDITIONER SYSTEM IN OVERHEAT CONDITION. CABIN CREW REPORTED A HAZE OF SMOKE AND BURNING ODOR IN THE CABIN. WHEN THE RIGHT PACK WAS SHUT DOWN THE SMOKE AND SMELL DISSIPATED. FLIGHT CONTINUED TO DESTINATION AND LANDED UNEVENTFULLY. CONTRACT MAINTENANCE AT SDF MEL'D THE RIGHT PACK AND WHEN THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE AND WATER SEPARATOR BAG. OPERATIONAL CHECK GOOD, MEL REMOVED, AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040927000582004092700058NM 2004 9 27 252TR0026 120040919A33506104789 BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 RIGHT OVERWING EMERGENCY EXIT LIGHTS, LOW BATTERY PACK. REPLACED RIGHT WING LIGHT BATTERY PACK PER MM 33-51-31. 2L72 4F RTA16WE 20040923000312004092300031EA 2004 9 23 COMA0460531 120040910A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE GROUND POWER OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01958CA 7111 GROUND POWER SERVICE DOOR WAS LEFT OPEN. INSPECTED DOOR AREA FOR DAMAGE. NO DEFECTS FOUND. SECURED DOOR. 2L72 4F4 FRTA21EA E15NE 20040923000562004092300056 2004 9 23 5040070604B 420040706A3418600591541 VANE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE AOA SENSOR OUT OF LIMITS E S4WAK NONE L NO TEST ININSP/MAINT 1 WP07807Z 213 5040 DURING COMPLETION OF AD 2003-22-12, FOUND VANE OUT OF LIMITS. 2L72 4F4 FRTA21EA E15NE 20040923000632004092300063NM 2004 9 23 S04432029 120040703A323065B0150423 HOSE BOEING747 747400 NM PWA 4056 PW4056 NE MLG BURST W SAJFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP03 24309 AFTER LIFT-OFF, GEAR LEVER CAN NOT MOVE TO UP. MSG"GEAR TILT", "GEAR DOOR", AND "GEAR DISAGREE" APPEAR. ATB. LANDING GEAR SWING TEST FOUND LT BLG TILT ACTUATOR MALFUNCTION AND ONE HOSE ASSY HYD FLUID LEAK. REPLACE LT BLG TILT ACTUATOR AND HOSE ASSY. AC ON JACK FOR SWING TEST NORMAL. PRELIMINARY SHOP REPORTS OF TILT ACT STATE NO FAULT FOUND. A BURST MARK WAS FOUND ON HOSE NEAR ONE END OF SOCKET. 2L74 4F4 FRTA20WE E24NE 20040923000672004092300067 2004 9 23 5040070604C 420040706A34186005915221 COMPUTER CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE STALL WARNING FAULTY E S4WAK NONE L NO TEST ININSP/MAINT 1 WP28807Z 213 5040 AFTER REPLACEMENT OF OUT OF TOLERANCE AOA VANES, COMPUTER WAS DETERMINED TO BE FAULTY BECAUSE OF OUTPUT INFORMATION NOT CORRECT AND INACCURATE BASED ON INPUTS. 2L72 4F4 FRTA21EA E15NE 20040923000682004092300068 2004 9 23 5040070604A 420040706A3418 TRANSDUCER CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE AOA VANE OUT OF TOLERANCEE S4WAK NONE L NO TEST ININSP/MAINT 1 WP07807Z 213 5040 DURING COMPLETION OF AD 2003-22-12, FOUND TRANSDUCER OUT OF LIMITS 2L72 4F4 FRTA21EA E15NE 20040923000922004092300092EU 2004 9 23 KBM2004F00156 120040422A2110 CLUTCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE A/C COMPRESSOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH797 2957 A/C BELT BROKEN IN MID-FLIGHT. COMPRESSOR CLUTCH BURNING, A/C INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040923001602004092300160NM 2004 9 23 SWAA042741 120040921A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040923001722004092300172NM 2004 9 23 DL757040868 120040910A5330141N333112 SKIN BOEING757 757232 1384965NM L1 DOOR CORNER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27689DL 27172 A DRILL START WAS ERRONEOUSLY MADE TO THE FUSELAGE SKIN NEAR THE LOWER FORWARD CORNER OF THE L1 DOOR CUTOUT. THE AREA OF SKIN WITH THE DAMAGE WAS TRIMMED OUT. THE TRIM OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 093358-14, REV A. 2L72 4F RTA2NM 20040923001762004092300176 2004 9 23 SWAA042734 420040921A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040923001772004092300177 2004 9 23 SWAA042735 420040921A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040923001882004092300188 2004 9 23 251TR0010 420040826A2230655153412 TRANSDUCER BOEING737 737228 13844AGNM AUTOTHROTTLES FAILED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05251TR 23792 AUTO THROTTLES INTERMITTENT. AUTO THROTTLES PLACED ON MEL 22-1. 08/28/2004: REPLACED LINEAR VELOCITY DISPLACEMENT TRANSDUCER ON THE NR 1 ENGINE. OPS CHECKS OK PER MM 22-30-00. 2L72 4F RTA16WE 20040923001912004092300191NM 2004 9 23 372PA0073 120040909A5320 INTERCOSTAL BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 INTERCOSTAL FROM BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2L72 4F RTA16NE 20040923001922004092300192NM 2004 9 23 372PA0074 120040909A5311 FRAME BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 AFT CARGO AFT FRAME AT BS 847 AT STR 23 RT DOOR STOP ATTACH FITTING CRACKED. REPLACED FITTING PER SRM 51-10-2. 2L72 4F RTA16NE 20040923001962004092300196NM 2004 9 23 372PA0061 120040909A5313 STRINGER BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 LOWER LOBE STR 26 RT CORRODED FROM BS 1006 TO BS 1016. REPLACED SECTION OF STRINGER PER DRAWING 65-45776-8 AND SRM 51-10-2. 2L72 4F RTA16NE 20040924000112004092400011NM 2004 9 24 USAA040440 120040812A5313 STRINGER BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41533 24548 PIT - FOUND STRINGER CRACKED .5 INCH, STATION 277, STRINGER 11R. INSTALLED REPAIR SPLICE PER SRM 53-00-03, FIG 201 AND EA 78897. (M) 2L72 4F RTA16WE 20040924000142004092400014NM 2004 9 24 USAA040458 120040810A5753 WEDGE BOEING757 7572B7 1384964NM LT WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU39393 27124 CLT - FOUND TRAILING EDGE WEDGE DELAMINATED .5 SQUARE FT AREA, LT WING, INBOARD MAIN FLAP, 48 INCHES IN FROM OUTBOARD END. REMOVED AND REPLACED T/E WEDGE PER SRM 51-72-11 AND BOEING DWG 113N2600. (M) 2L72 4F RTA2NM 20040924000222004092400022 2004 9 24 GTIA040729 420040817A2565 LANYARD DOUG DC9 DC982 3022082WP L2 DOOR SLIDE MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND L2 SLIDE PACK NOT INSTALLED CORRECTLY PULL CABLE NOT INSTALLED. INSTALLED MANUAL PULL CABLE. (M) 2L72 4F A6WE 20040924000322004092400032NM 2004 9 24 USAA040476 120040812A5753 SKIN BOEING757 7572B7 1384964NM RT WING AFT FLAPDEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND AFT FLAP RIGHT WING DISBONDED 12 SQUARE INCHES, APPROXIMATELY 3 FEET FROM .125 END. REMOVED AND REPLACED FLAP IAW AMM 27-51-12. (M) 2L72 4F RTA2NM 20040924000352004092400035 2004 9 24 GTIA040736 420040818A2565D29985103 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR MISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23803NK 48087 DTW - FOUND CHECK L2 SLIDE FOR CORRECT INSTALLATION. REMOVED AND REPLACED L2 SLIDE PACK. ESCAPE SLIDE REMOVAL AND INSTALLATION. (M) 2L72 4F A6WE 20040924000362004092400036NM 2004 9 24 USAA040514 120040818A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU63100 22198 FOUND SKIN CORRODED 3 INCHES, STATOIN 660-668, STRINGER 27L-29L. INSTALLED DOUBLER PER EA 87501 AND 87502A. (M) 2L72 4F RTA2NM 20040924000402004092400040WP 2004 9 24 GTIA040719 120040810A5210 MECHANISM DOUG DC9 DC982 3022082WP DOOR INTERLOCK STICKING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DTW - FLT 417 - FOUND MAIN CABIN DOOR WILL NOT CLOSE. INSPECTED AND FOUND INTERLOCK MECH STICKING, LUBED AND ADJUSTED INTERLOCK ARM. OPS CHECK GOOD. INSPECTED L1 DOOR. (M) 2L72 4F A6WE 20040924000472004092400047NM 2004 9 24 AMTA200400980 120040804A5320 WEB BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND CABIN STATION 1720, LBL 52 TO RBL 52, EXFOLIATION CORROSION ON WEB. CUT OUT DAMAGED SECTION, FABRICATED DOUBLER REPAIR AND INSTALLED IAW B757 SRM 53-60-51-1. (M) 2L72 4F RTA2NM 20040924000542004092400054NM 2004 9 24 ASAA0440102 120040409A3350 SOCKET BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01772AS 25105 JNU - FOUND FLOOR TRACK LIGHTS INOPERATIVE AT SECTION FIRST CLASS ROWS 2-6. RECONNECTED LAMP SOCKET AT ROW 2. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040924000552004092400055NM 2004 9 24 USAA040395 120040729A5320 ANGLE BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND ZEE ANGLE CORRODED 3 INCH BY 20 INCH AREA, BS 727B-727C LEFT ZEE ANGLE IN AFT CARGO. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-60-53, FIG 204 AND TYPICAL REPAIR 53-40-1. (M) 2L72 4F RTA16WE 20040924000592004092400059NM 2004 9 24 USAA040398 120040801A53106546812185 BEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 FOUND BEAM CRACKED 8 INCHES, INTERCOSTAL BETWEEN STATION 986 AND 1006 LBL 20. DEFECTIVE PART REPLACED WITH IDENT PART. (M) 2L72 4F RTA16WE 20040924000642004092400064NM 2004 9 24 USAA040376 120040721A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND STRINGER CRACKED .5 INCH, FS 1120, STRINGER 5A, LEFT SIDE. INSTALLED REPAIR ANGLE PE TYPICAL REPAIR 53-80-04. (M) 2L72 4F RTA16WE 20040924000682004092400068NM 2004 9 24 USAA040372 120040727A5740 FITTING BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND FITTING CRACKED .75 INCH, RIGHT WING REAR SPAR STATION 224. INSTALLED NEW SUPPORT FITTING PER EA 78781. (M) 2L72 4F RTA16WE 20040924000862004092400086NM 2004 9 24 USAA040489 120040822A5320 PAN BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND FLOOR PAN CORRODED, 4 EACH 1 INCH BY .5 INCH AREAS, SUBFLOOR AFT OF STATION 1016 TO AFT PRESSURE BULK FROM BL 0 TO RBL 37.5. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE PER SRM 51-70-13. (M) 2L72 4F RTA16WE 20040924000902004092400090NM 2004 9 24 USAA040484 120040806A5320 WEB BOEING737 737301 1384611NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND WEB WITH OVERSIZED FASTENER HOLES, 20 EACH, .0625 INCH DIAMETER OVERSIZE, WEB BS 986.5 TO 1006 AT LBBL 33. REMOVED AND MANUFACTURED NEW WEB AND INSTALLED PER BOEING DWG NR 65C32677 AND SRM 51-40-00. (M) USAA 2L72 4F RTA16WE 20040924000972004092400097NM 2004 9 24 USAA040467 120040819A5754 SKIN BOEING737 7373B7 1384580NM NR 6 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19529AU48045 24411 PIT - FOUND SKIN CRACKED .5 INCH, NR 6 SLAT LOWER SKIN AT O/B AUX ATTACH AREA. DOUBLER INSTALLED PER SRM 57-43-01. (M) 2L72 4F RTA16WE 20040924001132004092400113NM 2004 9 24 USAA040498 120040730A5754 SKIN BOEING737 737301 1384611NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 FOUND TOP SKIN/CORE BOND WITH 2 INCHES OF DELAMINATION, NR 2 SLAT TOP OUTBOARD T/E SURFACE. INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924001152004092400115NM 2004 9 24 USAA040485 120040806A5320 INTERCOSTAL BOEING737 737301 1384611NM BS DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND INTERCOSTAL WITH OVERSIZED FASTENER HOLES, 10 EACH AT .0625 INCH, BS 986.5 TO 1006 AT LBBL 33. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-2. (M) 2L72 4F RTA16WE 20040927000062004092700006NM 2004 9 27 SWAA042764 120040922A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 784, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040927000502004092700050 2004 9 27 373PA0051 420040902A2210408404042911 COUPLER BOEING737 7373Y0 1384671NM YAW DAMPER DAMAGED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05373PA 23749 YAW DAMPER POPS DC CIRCUIT BREAKER. REPLACED YAW DAMPER COUPLER AND OPS CHECKED PER MM 22-12-31 AND 22-12-01. 2L72 4F RTA16WE 20040927000592004092700059EU 2004 9 27 0401333270 120040813A5320 SILL AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01370NW 1037 DURING SPECIAL VISIT FOUND CORROSION ON AFT RT DOOR SILL AT FR 66. REPAIRED PER EA 32-200296. 2L72 4F RTA28NM 20040927000612004092700061 2004 9 27 A6WA200460032 420040827A2300 WIRE BAC 146 146300A 1500267EU MICROPHONE JACK SHORTED A A6WAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL31616AW E3145 SHORTLY AFTER TAKEOFF, LOST ALL RADIO COMMUNICATION. RETURNED TO RDU, LANDED UNDER LANDING WEIGHT. MAINTENANCE REPAIRED SHORTED KEY WIRE TO YOKE MIC JACK SYSTEM. OPS CHECK GOOD. (M) 2H74 4F RTA49EU 20040927000622004092700062NE 2004 9 27 AMTA200401084 220040827A7261 ENGINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE NR 2 OVERSERVICED A AMTAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 GL11163AT 1229 IN FLIGHT TURN BACK, NR 2 ENGINE VIB 2.6 A/B CHANNELS AND LOW BAND DURING CLIMB EPR .580 VIBS ON TAKEOFF 2.1 EPR .430. FOUND ENGINE OIL OVERSERVICED. DRAINED 2 QUARTS, PERFORMED OIL IN DRUM TEST AND AVM SURVEY PER M11-71-16 AND MM 71-00-00. ALL CHECKS GOOD, OK FOR SERVICE. (M) 2L73 4F4 F A23WE E12EU 20040927000632004092700063EU 2004 9 27 USAASA04081 120040826A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19116US 1210 CLT - EMERGENCY LIGHT TEST FAILED. MAINTENANCE REPLACED THE MID RIGHT EPSU. (M) 2L72 4F RTA28NM 20040927000672004092700067EA 2004 9 27 A6WA200440121 120040826A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA MACH TRIM FAILED A A6WAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31404AW 7294 MACH AND STAB TRIM FAIL. REMOVED AND REPLACED HST ACTUATOR IAW AMM 27-42-01. (M) 2L72 4F RTA21EA 20040927000682004092700068EA 2004 9 27 A6WA200440122 120040829A3000 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA AOA HEAT FALSE INDICATIONA A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31416AW 7603 IN FLIGHT RIGHT AOA HEAT CAUTION, COMPLIED WITH QRH. COMPLIED WITH OPS CHECK OF RIGHT AOA HEAT CONFIRMED THAT VANE IS HEATING AND CHECKED WIRING TO HEAT CONTROLLER. COULD NOT DUPLICATE IAW AMM 30-30-00. (M) 2L72 4F RTA21EA 20040927000692004092700069CE 2004 9 27 2004F00394 120040821A55201016200111 BRACKET BEECH 1900 1900D 1154162CE RT STAB ELEVATORCORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1717541 UE203 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20040927000702004092700070CE 2004 9 27 2004F00395 120040821A55201016200111 BRACKET BEECH 1900 1900D 1154162CE LT STAB ELEVATORCORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1717541 UE203 AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20040927000712004092700071CE 2004 9 27 2004F00396 120040821A55201016200131 BRACKET BEECH 1900 1900D 1154162CE RT STAB ELEVATORCORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO171754117715 UE203 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20040927000722004092700072NM 2004 9 27 USAA040512 120040824A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FLOOR SUPPORT WITH CORROSION .75 INCH IN DIAMETER, AROUND FASTENER HOLE ON FLOOR BOARD SUPPORT 3, AFT SPAR 312, LBL 11. REPLACED FLOOR SUPPORT PER SRM 51-10-00. (M) 2L72 4F RTA16WE 20040927000732004092700073EA 2004 9 27 A6WA200440123 120040830A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH STUCK A A6WAK NONE O OTHER ININSP/MAINT 1 GL31403AW 7288 CREW ESCAPE HATCH OUTER HANDLE IS STUCK. LUBRICATED OUTER HANDLE SHAFT, WORKED HANDLE FREE AND LUBED SHAFT WITH DC 33. (M) 2L72 4F RTA21EA 20040927000742004092700074NM 2004 9 27 USAA040511 120040824A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND INTERCOSTAL CRACKED 1.5 INCH AND 1 INCH TWO PLACES, AT BL 46 BETWEEN STATION 312 AND 328. REPLACED INTERCOSTAL PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20040927000752004092700075NM 2004 9 27 UIEA200400153 120040828A2612233U3214300 CONTROL PANEL BOEING747 74747UF 1384949NM FIRE DETECTION DIRTY A UIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15409MC 30558 HKG/ICN - AFTER TAKEOFF CLIMBING THROUGH 13,000 FEET, HAD INDICATION OF MAIN DECK CARGO FIRE. NO EICAS, NO WARNING BELL, JUST OVERHEAD SWITCH. IT WAS RAINING VERY HARD AND HIGH MOISTURE CONTENT IN AIRCRAFT. DEEP CLEANED MAIN DECK CARGO FIRE SWITCH. PERFORMED CMC GROUND TEST PASS PER MM 26-16-00. (M) 2L74 4F RT1384945 20040927000762004092700076EU 2004 9 27 USAASA04080 120040822A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19702UW 0896 DCA - THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT IN THE FORWARD POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040927000772004092700077CE 2004 9 27 RU3A0412 120040831A5330 SKIN LEAR 60 60LEAR 5170707CE FUSELAGE CRACKED A RU3AK NONE O OTHER ININSP/MAINT 1 SW1558 647 057 DURING INSPECTION, LEFT DELTA FIN WAS FOUND TO HAVE EXCESSIVE MOVEMENT ON THE LOWER SKIN. REMOVED FIN AND FOUND CRACK IN LOWER FIN ATTACHMENT, ADJACENT TO THE SCREW HOLES, UNDER FIN TO FUSELAGE ATTACH ANGLE. CRACK WAS THIRTEEN INCHES LONG. LOWER SKIN WAS ALSO DELAMINATED. THE INBOARD RIB HAD A CRACK SIX INCHES LONG JUST AFT OF THE LEADING EDGE. (M) 2L72 4F RTA10CE 20040927000782004092700078EA 2004 9 27 RU3A0411 120040826A291060075123107 HOSE CNDAIRCL600 CL6002B16 1900305EA NR 3 HYD SYS RUPTURED A RU3ABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW1585 3416 5138 LOST ALL HYDRAULIC PRESSURE ON NR 3 HYDRAULIC SYSTEM, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED HYDRAULIC PRESSURE HOSE, P/N 600-75123-107 RUPTURED. RU3A (M) 2L72 4F RTA21EA 20040927000792004092700079NM 2004 9 27 USAA040504 120040803A5711 SPAR BOEING737 737301 1384611NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 PIT - FOUND LEFT WING SPAR CRACKED .09375, AFT SPAR LEFT MAIN GEAR AREA. REWORKED HOLE PER EA 78859, REAMING HOLE AND INST BUSHING. (M) 2L72 4F RTA16WE 20040927000802004092700080NM 2004 9 27 USAA040505 120040824A5320 THRESHOLD BOEING737 737401 1384701NM FWD CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US43294 23987 PIT - FOUND CARGO DOOR THRESHOLD 1.5 INCH CRACK, FORWARD CARGO DOOR THRESHOLD. WELDED PER TR 53-30-04. (M) 2L72 4F RTA16WE 20040927000812004092700081NM 2004 9 27 USAA040506 120040824A5310 BEAM BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US53788 22958 PIT - FOUND VERTICAL BEAM CRACKED, VERT CHORD 5.7 LEFT WL 184 STATION 178 FPBH. REMOVED DEFECTIVE PARTS, INSTALLED REPAIR ANGLE PER EO 5300V155. (M) 2L72 4F RTA16WE 20040927000822004092700082NM 2004 9 27 USAA040507 120040812A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US52018 23316 PIT - FOUND SKIN CRACKED 1.250 INCH, STATION 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040927000832004092700083NM 2004 9 27 USAA040515 120040819A53119V53261485 BELTFRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU56643 23700 PIT - FOUND BELTFRAME CRACKED .125 INCH, AT FS 807, RIGHT OVERHEAD BIN LOWER ATTACH POINT. INSTALLED 1 AND 2 DOUBLER PER TR 53-10-20A. (M) 2L72 4F RTA16WE 20040927000842004092700084NM 2004 9 27 USAA040513 120040820A53106545871523 DOOR FRAME BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FRAME CRACKED .25 INCH, NR 4 DOOR STOP CUT OUT AFT SIDE OF DOOR. CUT OUT DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M) 2L72 4F RTA16WE 20040927000852004092700085NM 2004 9 27 USAA040516 120040820A5311 BELTFRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU56643 23700 PIT - FOUND BELTFRAME CRACKED .125 INCH, FS 787 LEFT OVERHEAD BIND LOWER ATTACH POINT. REMOVED CRACK AND INSTALLED REPAIR ANGLES PER TYP REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20040927000862004092700086NM 2004 9 27 USAA040509 120040825A5210 PAN BOEING737 7374B7 1384702NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND AFT DOOR PAN CRACKED .25 INCH, IN AFT PAN AT NR 5 STOP CUTOUT AND NR 6 STOP CUTOUT, FORWARD ENTRY DOOR. CUT OUT DAMAGE, INSTALLED DOUBLERS PER TYP REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20040927000882004092700088EA 2004 9 27 A6WA200440120 120040826A2420 GENERATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 FAILED A A6WAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 GL31404AW 7294 NR 2 GENERATOR FAILED DURNG TAKEOFF. SERVICED NR 2 IDG IAW AMM 12-13-24. RAN ENGINE TO POWER. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040927000902004092700090EU 2004 9 27 ASOA04568 120040806A33503011160 LIGHT AEROSPATR72 ATR72212 8680945EU GALLEY DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11533AS 460 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040927000912004092700091EA 2004 9 27 ASOA04559 120040802A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11886AS 7531 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 582.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040927000932004092700093NM 2004 9 27 USAA040450 120040724A5230 PLATE BOEING737 7374B7 1384702NM CARGO DOOR FRAMECORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND PLATE CORRODED 20 INCH LONG AREA, AFT CARGO DOOR FRAME INNER PLATE. NEW PLATE WAS FABRICATED AND INSTALLED PER SRM 51-70-13. CORROSION LEVEL 1, TASK NR C53-202-01. (M) 2L72 4F RTA16WE 20040927000952004092700095WP 2004 9 27 ASAA0480480 120040801A52403705141503 HANDLE DOUG DC9 DC983 3022083WP SERVICE DOOR MALFUNCTIONED A ASAAO OTHER O OTHER TXTAXI/GRND HDL 1 NM01969AS 53063 LAS - POST FLIGHT INSPECTION, FOUND AFT SERVICE L2 DOOR COULD NOT BE OPENED FROM INSIDE. REPLACED DOOR HANDLE AND RETAINING PIN, BOLT P/N 2705574. DOOR THEN OPENED PROPERLY. (M) 2L72 4F RTA6WE 20040927000962004092700096EA 2004 9 27 ASOA04507 120040710A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP CLIP AT FS 625 AFT EQUIPMENT BAY. (M) 2L72 4F RTA21EA 20040927000982004092700098NM 2004 9 27 UIEA200400014 120040211A5414 SKIN BOEING747 747243B 1384830NM NR 2 PYLON WRINKLED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, FOUND NR 2 PYLON HAS A WRINKLE CONDITION ON RIGHT SIDE. SKIN ASSY WAS TRIMMED TO REMOVED THE WRINKLED AREA. NDT INSPECTION OF THE REPAIR AREA, INCLUDING HFEC INSPECTION OF SKIN TRIMMED EDGES AND REPAIR FASTENERS HOLES WAS PERFORMED TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. A NEW SKIN REPAIR DOUBLER ASSEMBLY WAS INSTALLED FROM STATION 286-300. THE NEW SKIN REPAIR DOUBLER ASSY WAS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED IMMEDIATELY AFT OF THE TITANIUM SKIN DOUBLER EXTENSION. THE NEW SKIN REPAIR DOUBLER ASSEMBLY FORWARD END WAS ATTACHED TO THE EXISTING TITANIUM DOUBLER EXTENSION WITH A NEW TRIPLER MADE FROM TITANIUM SHEET. (M) 2L74 4F A20WE 20040927001002004092700100EA 2004 9 27 ASOA04458 120040628A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GALLEY CRACKED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT COVER IN THE GALLEY BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR. (M) 2L72 4F RTA21EA 20040927001022004092700102EA 2004 9 27 ASOA04457 120040628A3350 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT COVER AT THE CABIN ENTRANCE WAS FOUND MISSING. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE CABIN ENTRANCE. (M) 2L72 4F RTA21EA 20040927001032004092700103EU 2004 9 27 ASOA04456 120040627A33503011162 COVER AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 FLT 4285 - DURING A GROUND INSPECTION IN ATL, THE FLOOR EMERGENCY EXIT SIGN AT ROW 1D WAS FOUND MISSING AND THE WIRE EXPOSED. MAINTENANCE REPLACED FLOOR EMERGENCY EXIT SIGN COVER AT ROW 1D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040927001062004092700106EA 2004 9 27 ASOA04447 120040620A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN MCN, THE LEFT LOWER ENGINE SUPPORT BEAM PANEL AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT LOWER ENGINE SUPPORT BEAM PANEL AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20040927001082004092700108NM 2004 9 27 USAA040451 120040805A5340 FITTING BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND T-FITTING AND LUG FITTING CORRODED 1.5 INCH DIAMETER AND MOUNT HOLE, LEFT AFT OUTBOARD ATTACH FITTING AT MATING AREA OF FWD T-FITTING AND FUSELAGE LUG FITTING. REAMED AND REBUSHED PER EA 78920. (M) 2L72 4F RTA16WE 20040927001102004092700110NM 2004 9 27 USAA040447 120040714A575465C26602223 SKIN BOEING737 7374B7 1384702NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US 24548 PIT - FOUND SKIN AND CORE BOND DELAMINATION WITH CHAF DAMAGE 1 INCH BY 2 INCH AREA, UPPER INBOARD T/E AFT CORNER OF NR 2 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED FILLER, INTERNAL AND TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040927001112004092700111NM 2004 9 27 USAA040454 120040816A5753 BRACKET BOEING737 7373B7 1384580NM NR 2 FLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU48131 24412 PIT - FOUND BRACKET GOUGED 1.75 INCH BY .125 INCH WIDE BY .020 INCH DEEP, LEFT OUTBOARD AFT FLAP BRACKET NR 2. BLENDED PER EA 78975. (M) 2L72 4F RTA16WE 20040927001122004092700112NM 2004 9 27 USAA040455 120040818A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU49423 23705 PIT - FOUND SKIN GOUGED 1 INCH LONG BY .5 INCH WIDE BY .020 INCH DEEP, STATION 959 STRINGER 20L 2 INCH ABOVE LAP SEAM. INSTALLED TEMPORARY REPAIR PER EA 78993. (M) 2L72 4F RTA16WE 20040927001132004092700113NM 2004 9 27 USAA040456 120040816A5240 STRUCTURE BOEING737 7374B7 1384702NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19447US38174 24874 PIT - FOUND FORWARD SERVICE DOOR CRACKED .5 INCH, TWO EACH, FORWARD MOST RIVET HOLE IN ROW DIRECTLY UNDER UPPER HINGE ARM. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBELR PER SRM 52-00-01 FIG 202. (M) 2L72 4F RTA16WE 20040927001152004092700115EA 2004 9 27 ASOA04462 120040628A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040927001162004092700116EA 2004 9 27 ASOA04461 120040628A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040927001182004092700118EA 2004 9 27 ASOA04450 120040624A1420487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11847AS 7335 FLT 4420 - DURING A GROUND INSPECTION IN DFW, THE FIRST FIVE ROWS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTION TO THE FIRST FIVE ROWS OF EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040927001242004092700124 2004 9 27 SWAA042773 420040923A2565D31354 SLIDE BOEING737 7373G7 1384595NM L2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 L2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040927001252004092700125 2004 9 27 SWAA042774 420040923A2565D71702001 BATTERY BOEING737 7377H4 1384404NM ESCAPE SLIDE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR ESCAPE SLIDE LIGHT AND AFT CENTER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040927001262004092700126NM 2004 9 27 SWAA042775 120040923A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29437WN 29832 DURING SCHEDULED MV2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXTERIOR LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040927001302004092700130SO 2004 9 27 SWIA200413746 120040825A2913PV302229 PUMP EMB 120 EMB120ER 3260203SO HYD SYSTEM LEAKING A SWIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM07189SW 120048 DURING CRUISE AT FL200, HYDRAULIC RESERVOIR LOW LEVEL LIGHT ILLUMINATED FOLLOWED BY RESERVOIR LOW PRESS, MAIN PUMP LOW PRESS, AND ELECTRIC PUMP LIGHTS. DIVERTED TO SFO. SWAGGED NR 6 HYDRAULIC RETURN LINE AT RIGHT ENGINE NACELLE. REPLACED RIGHT ENGINE DRIVEN HYDRUALIC PUMP AND SYSTEM RETURN FILTERS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040927001312004092700131NE 2004 9 27 SWIA200413747 220040824A7261PV302229 CARBON SEAL EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE RT ENGINE LEAKING A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 NM07564SW 120339 OIL PRESSURE 50 PSID IN RIGHT ENGINE. PERFORMED QRH FOR LOW OIL PRESSURE 40-55 PSID. OIL PRESSURE WENT UP TO 60 PSID. INSTALLED NEW CARBON SEAL AND CENTRIFUGAL BREATHER GEAR SHAFT IAW P&W MM 3034622 72-20-00 PARA (2) (D) AND (10) (F). OPERATIONAL CHECK GOOD. P/N 3121371-01, 3037223. 2L72 4T4 TRTA31SO E20NE 20040927001332004092700133EA 2004 9 27 SWIA200413749 120040821A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07938SW 7741 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED FS 280.00 LBL 9.0 O/B CLIP. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-01, 51-42-13, 51-21-11, 51-25-16. 2L72 4F RTA21EA 20040927001342004092700134EA 2004 9 27 SWIA200413750 120040821A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07938SW FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 RBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. LOWER FLANGE REPAIRED IAW CRJ REO #601R-53-11-171 REV A. 2L72 4F RTA21EA 20040927001352004092700135EA 2004 9 27 SWIA200413751 120040821A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA APU BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07938SW APU COMPARTMENT FS 625.00 STR 14L HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2L72 4F RTA21EA 20040927001362004092700136EA 2004 9 27 SWIA200413752 120040821A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA APU BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07938SW APU COMPARTMENT FS 625.00 STR 14R HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-25-16. 2L72 4F RTA21EA 20040927001382004092700138SW 2004 9 27 AC2A094950 120040410A21505861653 TURBINE BELL 430 430 1182150SW CABIN COOLING SEIZED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SW03430CV 49072 TURBINE IS SEIZED. 1G72 3U RTH9SW 20040927001392004092700139SW 2004 9 27 AC2A094951 120040404A2424222375060119 VOLT REGULATOR BELL 430 430 1182150SW MAIN INTERMITTENT B AC2AO OTHER O OTHER NRNOT REPORTED 1 SW03430CH6712 49037 VOLTAGE REGULATOR INTERMITTENT. REPLACED VOLTAGE REGULATOR AND WILL SEND IN FOR WARRANTY REPAIR. 1G72 3U RTH9SW 20040927001402004092700140SW 2004 9 27 ALGA094925 120040531A6310406040542107 FLANGE BELL 407 407 1182206SW FREEWHEEL UNIT ELONGATED B ALGAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW03437AL A4722 53141 ELONGATION FOUND ON BOLT HOLES OF ADAPTER P/N: 406-040-542-107. REPLACED WITH NEW PART. 1G71 3U O H2SW 20040927001412004092700141EU 2004 9 27 BAQA094424 120040524A243523081057 STARTER GEN UROCOPEC135 EC135T1 5620026EU ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135MH1866 0131 GENERATOR WILL NOT START ENGINE. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 06/02/2004 1G72 3U H88EU 20040927001432004092700143SW 2004 9 27 ALGA094801 120040525A6220406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03408AL435 53491 EXCESSIVE AXIAL WEAR AND BINDING. REPLACED WITH NEW PART, BY FIELD MAINT. 1G71 3U O H2SW 20040927001462004092700146EA 2004 9 27 SWIA200413735 120040612A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW 7028 ANGLE AT STRINGER 3L APPROXIMATELY 2 INCHES AFT OF FS 280 BULKHEAD IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE AT STRINGER 3L STA FS 280 IAW CRJ SRM REF 52-42-06. 2L72 4F RTA21EA 20040928000042004092800004WP 2004 9 28 UPS04843142 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, WING LT L/E AT STA XFS 578 RIB IS CRACKED. NDT VERIFIED CRACK .5 INCH LONG. STOP DRILLED CRACK. NDT VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2. 2L74 4F4 FRT4A25 E2GL 20040928000052004092800005WP 2004 9 28 UPS04843143 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 WING LT L/E RIB IS CRACKED AT STA XFS 816.250. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2 2L74 4F4 FRT4A25 E2GL 20040928000062004092800006WP 2004 9 28 UPS04843144 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 LT WING L/E AT STA. XFS 716.250 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0 FIG 2. 2L74 4F4 FRT4A25 E2GL 20040928000072004092800007WP 2004 9 28 UPS04843145 120040909A571257695892 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 WING RT L/E AT APPROX. STA XFS 465 HAS CRACKED RIB. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLER AND INSTALLED IAW SRM 57-2-0 FIG 2. 2L74 4F4 FRT4A25 E2GL 20040928000082004092800008WP 2004 9 28 UPS04843146 120040908A571257695892 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 RT WING MID L/E XFS 335 UPPER RIB IS CRACKED AT AFT END. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLERS AND INSTALLED IAW SRM 57-2-0 FIG 2. 2L74 4F4 FRT4A25 E2GL 20040928000092004092800009WP 2004 9 28 UPS04843147 120040909A571257695892 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 WING RT L/E AT STA XFS 335.250 DRAIN HOLE DOUBLER IS CRACKED. NDT VERIFIED CRACK IS APPROX. .3750 INCH LONG. REMOVED INTERNAL DOUBLER ON RT WING L/E, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769589-27. INSTALLED REPLACEMENT DOUBLER ON RT L/E AT STA XFS 335.250 IAW SRM 51-1-21 AND 51-1-21D. 2L74 4F4 FRT4A25 E2GL 20040928000102004092800010WP 2004 9 28 UPS04843148 120040909A57129890103502 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 4 STUB WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 RT WING NR 4 STUB WING HAS TWO RIBS CRACKED ABOVE NR 4 PYLON FOOT STOOL. STOP DRILLED ONE CRACK AND CUT OUT ONE CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK AND NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2. 2L74 4F4 FRT4A25 E2GL 20040928000112004092800011NE 2004 9 28 IXXA0400106O 220040822A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE NR 1 FAILED A IXXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW11823BX* 712 46064 DURING TAKE OFF NR 1 GEN HAD NO FREQ AND LOW VOLT ON ENGINE DISCONNECTED GENERATOR. ON TAKE OFF TOWER WAS TOLD THAT NR 1 ENGINE HAD A TAIL PIPE FIRE. ENGINE SHUT DOWN, AIRCRAFT RETURNED TO BLOCKS AND TRIED TO ROTATE N1 FAN NO ROTATION, TRIED TO MOTOR ENGINE N2 INDICATION BUT NO N1 ROTATION, NO FIRE WARNING OR OTHER INDICATION IN COCKPIT. WORK IN PROGRESS AS ADDITIONAL INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2L74 4F4 FRT4A25 E2GL 20040928000122004092800012NM 2004 9 28 BB04085 120040922A2721 TRIM SYSTEM BOEING767 767201 1385125NM GE CF6 CF680C2B2 30025NE RUDDER INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19648US 23900 AFTER TAKE-OFF, CREW NOTED THAT THE RUDDER TRIM WAS INOPERATIVE. CREW ALSO REPORTED THAT THE ANTI-SKID WAS INOPERATIVE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A RUDDER TRIM CHECK IAW THE FIM AND A VISUAL INSPECTION OF THE TRIM ACTUATOR AND ASSOCIATED WIRING. NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA1NM E13NE 20040928000132004092800013NM 2004 9 28 NACA20040039 120040921A5270602EN6026 SWITCH BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE CARGO DOOR OUT OF ADJUST A NACAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AL03992AJ 19428 MAIN CARGO DOOR UNLOCKED LIGHT CAME ON IN FLIGHT. VERIFIED MAIN CARGO DOOR CLOSED AND LOCKED. DEFERRED LIGHT ASSEMBLY. REPLACED LATCH PIN ROD ACTUATOR CHECK VALVE, INSPECTED ALL WARNING SWITCHES AND WIRING WITH NO DEFECTS FOUND. TESTED PER FED-EX MM 52-70-09 WITH ALL CHECKS NORMAL. 2L73 4F4 F A3WE E2EA 20040928000142004092800014CE 2004 9 28 DXTA200400400 120040919A275099143742 CONVERTER CESSNA650 650 2076802CE GARRTTTFE731TFE7314R 01518WP TE FLAPS DEFECTIVE E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07789QS4886 6507089 FLAPS INOPERATIVE ANNUNCIATOR ILLUMINATED AFTER TAKEOFF WITH FLAPS INDICATING UP, FLAP WOULD NOT RESET. DURING LANDING APPROACH FLAPS WOULD RESET AND OPERATE BUT FLAPS INOP ANNUNCIATOR REMAINS ILLUMINATED ON THE GROUND. TROUBLESHOT SYSTEM TO DEFECTIVE FLAP RESOLVER CONVERTER, REMOVED AND REPLACED CONVERTER, RIGGED FLAPS IAW MM CHAPTER 27-54-00, OPS CHECKS GOOD. 2L72 4F4 F A9NM E6WE 20040928000162004092800016CE 2004 9 28 DXTA200400398 120040917A3240215672 FRICTION BRAKE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL MLG DAMAGED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07907QS 7500201 RT BRAKE VERY SPONGY AND DOES NOT GRAB UNTIL EXCESSIVE PRESSURE IS APPLIED THEN GRABS VERY ABRUPTLY. INSPECTED THE LT AND RT BRAKES, FOUND NO LEAKS AND .2 LEFT ON BRAKES LT AND RT. BLED RT BRAKES AND FOUND NO AIR IN SYSTEM, BRAKES OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW MM CHAPTER 32-42-00-721. 2L72 4J4 FRTT00007WITE6CH 20040928000172004092800017CE 2004 9 28 DXTA200400397 120040916A32406633622039 CABLE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL PARKING BRAKE STIFF E DXTAO OTHER O OTHER LDLANDING 1 GL07909QS 7500009 EXCESSIVE BRAKE PRESSURE IS REQUIRED TO STOP THE AIRCRAFT FROM THE PILOTS SIDE. CO-PILOTS BRAKES APPEAR NORMAL. TROUBLESHOT TO LT AND RT PARKING BRAKE CABLES STIFF, REMOVED AND REPLACED CABLES, OPS CHECKS GOOD IAW MM CHAPTER 32-42-00. 2L72 4J4 FRTT00007WITE6CH 20040928000182004092800018 2004 9 28 DXTA200400393 420040915A34257014300901 DISPLAY CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL COCKPIT FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07971QS4920 7500071 NR 1 MFD ON PILOTS BURNED OUT IS COMPLETLY DARK WITH NO RED X COULD SMELL ELECTRICAL FUMES. REMOVED PILOTS NR 1 MFD AND INSTALLED SERVICEABLE UNIT. 2L72 4J4 FRTT00007WITE6CH 20040928000222004092800022CE 2004 9 28 DXTA200400401 120040920A3230 WARNING LIGHT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07314QS 5600441 AFTER TAKEOFF, RT MAIN GEAR WOULD NOT RETRACT, FLYING AT APPROX. 200 KTS. THE RT MAIN GEAR LIGHT WAS ON ALONG WITH THE GEAR UNSAFE LIGHT, THE HYDRAULIC LIGHT DID GO OUT. RAN THE EMERGENCY GEAR EXTENSION CHECK LIST AND BLEW THE GEAR DOWN, GOT THREE GREEN LIGHTS AND LANDING WAS NORMAL. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20040928000242004092800024CE 2004 9 28 DXTA200400404 120040921A2130 WARNING LIGHT CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE CABIN PRESSURE ILLUMINATED E DXTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL07806QS 5600614 AT ROTATION GOT LOUD NOISE AND EXCESSIVE HEAT AND A NOTICEABLE ODOR WAS PRESENT. ANNUNCIATOR PANEL WAS CLEAR, PRESSURE SOURCE WAS NORMAL, ANNUNCIATOR PANEL EMERGENCY PRESSURE LIGHT CAME ON WHEN CYCLED KNOB TO RIGHT. EMERGENCY PRESSURE THEN BACK TO NORMAL -1400 ON CABIN ALTITUDE PANEL. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E00053EN 20040928000252004092800025SO 2004 9 28 CHQA000559 120040917A781023075866 DIFFUSER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EXHAUST SEPARATED A CHQAK NONE O OTHER ININSP/MAINT 1 GL11565RP 145679 ON WALK AROUND AFTER FLIGHT 6357, THE FLIGHT CREW NOTICED .3333 TO .5000 OF THE NR 2 ENGINE EXHAUST MIXER ASSEMBLY WAS MISSING. MAINTENANCE DISCOVERED .3333 OF THE DIFFUSER IS MISSING ALONG WITH INTERNAL DAMAGE TO THE THRUST REVERSER AND EXHAUST CONE. MAINTENACE REMOVED AND REPLACED THE DIFFUSER, DUCT SHROUD, AND EXHAUST CONE. THE THRUST REVERSER WAS PUT ON A 50 HOUR FLY BY. ON 9/21/04 THE THRUST REVERSER WAS REMOVED AND REPLACED. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040928000262004092800026NM 2004 9 28 04FDEA02775 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 SNRM NR N0484 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, OB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000272004092800027NM 2004 9 28 04FDEA02776 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 SNRM NR N0483 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000282004092800028NM 2004 9 28 04FDEA02777 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, IB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000292004092800029NM 2004 9 28 04FDEA02778 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, OB FLAP, IB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000312004092800031NM 2004 9 28 04FDEA02780 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 SNRM NR N0488- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA1-5750-79749. 2L73 4F4 FRTA22WE E31N3 20040928000322004092800032NM 2004 9 28 04FDEA02781 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000332004092800033NM 2004 9 28 04FDEA02782 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 SNRM NR N0486- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA#1-5750-79749. 2L73 4F4 FRTA22WE E31N3 20040928000352004092800035NM 2004 9 28 04FDEA02784 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OB FLAP, OB AFT HINGE, IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000362004092800036EU 2004 9 28 AWXA200401058 120040911A5347D53112729202 SEAT TRACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON SEAT TRACK RAIL Y254 LT AT FR 16. MAINTENANCE CUTOUT THE DAMAGE ON SEAT TRACK RAIL Y254 LT AT FR 16; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW SRM 53-00-14, FIG. 206. 2L72 4F4 FRTA28NM E40NE 20040928000372004092800037NM 2004 9 28 AWXA200401059 120040826A5330659187911 SKIN BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING C-18 CHECK RIVETS WERE FOUND PULLING THROUGH KEEL BEAM SKIN BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGED KEEL BEAM SKIN FROM BS 663 TO BS 727, LBL 6.3 TO RBL 6.3; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL; INSTALLED REPAIR PARTS IAW AWA ER 03-5310-02085-JS1. 2L72 4F4 FRTA16WE E2GL 20040928000382004092800038NM 2004 9 28 AWXA200401061 120040825A53106517688 CREASE BEAM BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-1 DOOR CREASE BEAM AT FASTENER HOLES BETWEEN BS 318 AND BS 335. MAINTENANCE REMOVED CORRODED U-CHANNEL AT L-1 DOOR FROM BS 318 TO BS 335; FABRICATED A NEW REPLACEMENT U-CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-30-01, FIG. 7. 2L72 4F4 FRTA16WE E2GL 20040928000402004092800040NM 2004 9 28 04FDEA02802 120040922A5414 SKIN DOUG DC10 DC10 N/A-SDRNM GE CF6 CF650C2 30018NE ZONE 400 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 NR 1 ENGINE IB COE COWL IS DAMAGED AT LEADING EDGE. REMOVED CORE COWL, CUT OUT DAMAGE, REMOVED FRAME AND RUBSTRIP, FABRICATED DOUBLER AND FILLER, DRILLED AND FITTED NEW FRAME AND RUBSTRIP, INSTALLED DOUBLER AND FILLER, FRAME AND RUBSTRIP IAW DC10 SRM 54-00-01 VOL I, 51-21-01 VOL II, 51-35-01 VOL II AND EA 8-7110-81479. APPLIED ANTI-CHAFFE IAW SRM 51-23-01 VOL II. INSTALLED CORE COWL IAW MM 71-13-01. READJUSTED AFT LATCH AND REISTALLED IAW MM 71-13-01-2. REFERENCE N/R N01383 2L73 4F4 FRTA22WE E23EA 20040928000432004092800043NM 2004 9 28 04FDEA02805 120040923A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03 PAGES 442 TO 443. 2L73 4F4 FRTA22WE E31N3 20040928000442004092800044NM 2004 9 28 04FDEA02806 120040923A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, IB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER = 1.249, FINAL DIAMETER = 1.257. COMPLIED WITH FEDEX EA 1-5750-79749, 2L73 4F4 FRTA22WE E31N3 20040928000452004092800045NM 2004 9 28 04FDEA02807 120040923A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, IB FLAP, OB AFT HINGE PIVOT HOLE OB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03. 2L73 4F4 FRTA22WE E31N3 20040928000462004092800046NM 2004 9 28 04FDEA02808 120040923A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.289, FINAL DIAMETER= 1.291. COMPLIED WITH FEDEX EA 1-5750-79749 2L73 4F4 FRTA22WE E31N3 20040923001052004092300105SO 2004 9 23 FFK2004F00005 220040708A7314649368261A1 PUMP PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO LT ENGINE FAULTY B FFKRA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO0586BW 419 347770340 826849R PILOT REPORTED THAT THE LT ENGINE SURGED ON TAKE OFF. AFTER INVESTIGATING LT ENGINE, FOUND THAT THE ENGINE DRIVE FUEL PUMP FUEL FLOW WOULD DROP OFF AT HIGH RPMS. SUSPECT BAD FUEL PUMP, REPLACED AS NEEDED. 1L72 3O3 O A7SO E9CE 20040923001102004092300110EU 2004 9 23 M7F2004F00000 120040610A6710 COLLECTIVE STICK BOLKMS105 BO105S 5626006EU COCKPIT MISINSTALLED B M7FRO OTHER W INADEQUATE Q C NRNOT REPORTED 1 EA2340EG 4070 S347 UPON REMOVAL OF THE MIXING LEVER ASSY DURING M/R KMSN REMOVAL, THE COLLECTIVE FORK WAS FOUND TO BE INCORRECTLY INSTALLED ONTO THE BEARING BLOCK (105-42124.01). THE B0105 MM MANDATES PROPER SHIMMING OF THE FORK/BEARING BLOCK DURING ASSY. THERE WERE NO SHIMS INSTALLED IN THIS INSTANCE, THUS PRELOADING THE EARS OF THE CAST ALUMINUM ALLOY BEARING BLOCK. FAILURE OF THIS PART COULD CAUSE LOSS OF CONTROL OF THE HELICOPTER, PART DISPOSITION, SCRAPPED. 1G72 3U H3EU 20040923001192004092300119NM 2004 9 23 150AW0031 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 7 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001202004092300120NM 2004 9 23 150AW0027 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 13 RT BS 867. REPLACED STRINGER TIE CLIP PER SRM 51-10-002. 2L72 4F RTA16WE 20040923001312004092300131NM 2004 9 23 150AW0042 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001372004092300137SO 2004 9 23 C2XA04TY159 120040822A532014525800009 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FLOOR SILL AT FRAME 28. THE SILL WAS REMOVED AND REPLACED IAW THE EMB SRM. ACFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION. 2L72 4F RTT00011AT 20040923001402004092300140SO 2004 9 23 C2XA04IA105 120040820A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713969 145141 DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT LOCATED ON THE COCKPIT STEP INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040923001432004092300143SO 2004 9 23 C2XA04TY158 120040822A532014521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 DURING A SCHEDULED 4C INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW THE EMB SRM. ACFT PENDING RELEASE UPON COMPLETION OF 4C INSPECTION. 2L72 4F RTT00011AT 20040923001442004092300144 2004 9 23 2004UALA00778 420040820A3420 CAPACITOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EHSI FAILED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29668UA 30024 RETURNED TO FIELD DUE TO SMOKE IN COCKPIT. FLT CREW REPORTED THAT CAPTAIN'S ELECTRONIC HORIZONTAL SITUATION INDICATOR (EHSI) WENT BLANK DURING THE INCIDENT. CAPTAIN'S EHSI WAS REPLACED. SHOP DETERMINED THAT THE REMOVED EHSI HAD A FAILED CAPACITOR C116 ON CARD A5A1. THE CAPACITOR HAS SIGNS OF OVERHEATING AND LIKELY CAUSED THE SMOKE IN THE COCKPIT. 2L72 4F4 FRTA1NM E24NE 20040923001452004092300145NE 2004 9 23 2004UALA00780 220040821A7200 ENGINE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 FLUCTUATES A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29929UA 26652 RETURNED TO ORD WITH NR 1 ENGINE EGT FLUCTUATING. REPLACED LOWER AND UPPER LEFT HAND EGT HARNESS DUE TO FAILURE OF RESISTANCE CHECKS. SHOP CHECK CONFIRMS FAILURE OF RESISTANCE CHECK. 2L72 4F4 FRTA16WE E2GL 20040923001472004092300147NM 2004 9 23 2004UALA00782 120040808A2420 GENERATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29362UA 24455 APU GEN ON LINE, FOUND VOLTAGE TO INDICATE 127VAC, WITH COCKPIT PANEL LIGHTS DIM, E&E LIGHTS VERY DIM AND FLUCTUATING, EXHAUST FAN NORMAL CB POPS. APU POWER IS NO GOOD. APU GEN C-B (C899) CONTACT B2 TERMINAL LUG & 3EA WIRES INSULATION BURNT 8 INCHES FROM B2 LUG. SUSPECT TERMINAL LUG LOOSE, REPLACED B2 LUG & WIRE, CLEANED B3 LUG & REPLACED NR 1 APU GEN BREAKER C889. 2L72 4F4 FRTA16WE E2GL 20040923001512004092300151SO 2004 9 23 C2XA04SH485 120040810A532014521713003 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714925 145004 SHV - DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040923001542004092300154NE 2004 9 23 04232678 220040819A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT SHUTDOWN A VTZAEA ENGINE SHUTDOWN UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27678BR 7653 LT ENG SHUTDOWN FOR LOW OIL PRESSURE. R&R LT OIL PRESS TRANSDUCER. LK & OP'S CK GOOD. PERFORMED FDR DOWNLOAD. REMOVED SCREENS FROM LT ENGINE C-SUMP FITTINGS. R&R LT ENG OIL LUBE & SCAVANGE PUMP. R&R LT ENG OIL VENT LINE & B-SUMP VENT REGULATOR VALVE. PERFORMED LT ENG PERFORMANCE RUNS. NORMAL OIL PRESSURE & NO OTHER DEFECTS. R&R ENG OIL. LEAK CK GOOD. CLEANED DEBRIS FROM SCAVANGE SCREENS & REINSTALLED. PERFORMED LT ENG INSPECTION FOR OIL LEAKAGE, NO LEAKS. PERFORMED LT ENG OIL CONSUMPTION RUNS BAGGED GANG DRAIN LINES, NO LEAKS. PERFORMED LEAK TEST OF LT ENG, NO LEAKS. RAN ENG & PERFORMED OIL LVL QTY CK, CK OK. PERFORMED ENG LOW OIL LVL OPS TEST. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20040923001582004092300158NM 2004 9 23 150AW0041 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 500C BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001612004092300161NM 2004 9 23 SWAA042742 120040830A3350OL3071BPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29740SW 29276 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 18 DEF, INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040923001662004092300166NM 2004 9 23 150AW0026 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 16 RT BS 727E. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. 2L72 4F RTA16WE 20040923001682004092300168NM 2004 9 23 151AW0006 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAMES CRACKED AT BS 380 STR 9 RT. CRACK REPAIRED PER SRM 53-00-07. 2L72 4F RTA16WE 20040923001732004092300173NM 2004 9 23 CALA0400639 120040915A53136545774 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND STRINGER 25L CORRODED AT STA 867-907 IN AFT BAGGAGE BIN. THE CORROSION WAS REMOVED AND A REPAIR SECTION OF STRINGER WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20040923001742004092300174 2004 9 23 SWAA042732 420040921A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040923001792004092300179NM 2004 9 23 SWAA042737 120040921A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040923001902004092300190NM 2004 9 23 372PA0070 120040909A5320 ATTACH ANGLE BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 INTERCOSTAL ATTACH ANGLE CRACKED AFT SIDE OF BS 344 FLOORBEAM AT LBL 12. REPLACED ANGLE PER SRM 53-10-51, SRM 51-20-01 AND SRM 51-40-00. 2L72 4F RTA16NE 20040923001932004092300193NM 2004 9 23 372PA0056 120040909A5320 INTERCOSTAL BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 INTERCOSTAL HAS CORROSION, AFT CABIN FROM BS 967 TO BS 986.5 AT LBL18. REPLACED INTERCOSTAL PER SRM 51-10-01. 2L72 4F RTA16NE 20040923001952004092300195NM 2004 9 23 372PA0054 120040909A5320 ATTACH ANGLE BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 SIDEWALL ATTACH ANGLE CRACKED AT BS 767 LBL 54. REPLACED ANGLE PER SRM 51-10-02. 2L72 4F RTA16NE 20040924000022004092400002WP 2004 9 24 GTIA040727 120040808A5210 HANDLE DOUG DC9 DC983 3022083WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 LGA - FLT 703 - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2L72 4F RTA6WE 20040924000102004092400010NM 2004 9 24 USAA040439 120040723A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FRAME CRACKED .5 INCH AT RIVET HOLE, STATION 787 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20040924000282004092400028NM 2004 9 24 USAA040470 120040812A5320 SUPPORT ANGLE BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH, STATION 1520-1540 BL 0. REPLACED WITH FABRICATED LIKE PART PER SRM 53-00-51. (M) 2L72 4F RTA2NM 20040924000292004092400029NM 2004 9 24 USAA040469 120040812A5320 SUPPORT ANGLE BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36221 27244 CLT - FOUND SUPPORT ANGLE CRACKED .5 INCH STATION 1200-1220 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 51-40-02. (M) 2L72 4F RTA2NM 20040924000302004092400030WP 2004 9 24 GTIA040723 120040814A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP LT MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23820NK 49126 ORD - FLT 1525 - LEFT MAIN LANDING GEAR INDICATOR STAYED RED AFTER GEAR RETRACTION FOLLOWED QRH AND HAD NORMAL INDICATIONS AFTER. REMOVED AND REPLACED LEFT MLG UPLOCK PROX SENSOR. PERFORMED OPS CHECK OF SENSOR THROUGH PROX SWITCH ELECT. (M) 2L72 4F A6WE 20040924000382004092400038 2004 9 24 GTIA040724 420040814A2565 LANYARD DOUG DC9 DC983 3022083WP TAILCONE SLIDE MISINSTALLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FLL - TAILCONE ESCAPE SLIDE LANYARD ROUTED INCORRECTLY. ROUTED LANYARDS CORRECTLY. (M) 2L72 4F RTA6WE 20040924000442004092400044EA 2004 9 24 ASOA04538 120040802A5210601R3190169 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX LACK OF LUBE A ASOAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11846AS13106 7328 FLT 4243 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND HARD TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040924000932004092400093NM 2004 9 24 USAA040482 120040806A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND FLOORBEAM UPPER CAP CORRODED 2 FT BY 70 INCH AREA, BS 986.5 CABIN FLOORBEAM UPPER CAP. REMOVED CORRODED T-CAP AND REPLACED WITH NEW PER TYPICAL REPAIR 53-10-05B. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20040924001062004092400106NM 2004 9 24 USAA040497 120040729A575465C2660297 SKIN BOEING737 737301 1384611NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND TOP SKIN/CORE BOND WITH DELAMINATION, 3 INCH BY 3.5 INCH AREA, NR 2 SLAT TOP SURFACE INBOARD END. REMOVED DAMAGE, INSTALLED NEW CORE SECTION, TOP DOUBLER, SEAL END PER BOEIGN SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924001092004092400109NM 2004 9 24 USAA040487 120040803A5551 FITTING BOEING737 737301 1384611NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND RIGHT HORIZ STAB LUGS CORRODED 1 INCH BY 2 INCH, R-9, 11, 12, 13, 14, 15, 17, 18, 19. CLEANED FACES AND BORE IAW SRM 55-10-10, NEW BUSHINGS. (M) 2L72 4F RTA16WE 20040924001102004092400110NM 2004 9 24 USAA040500 120040726A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND STRINGER CRACKED 1.25 INCH, STRINGER 5A LEFT BS 1138 HORIZ STABILIZER CUTOUT. SPLICED STRINGER PER TYPICAL REPAIR 53-80-04, SRM 53-00-01 FIG 221. (M) 2L72 4F RTA16WE 20040924001162004092400116NM 2004 9 24 USAA040501 120040818A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US53332 23311 PIT - FOUND SKIN CRACKED 2 INCHES, BETWEEN 747 AND 767 STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040924001172004092400117NM 2004 9 24 USAA040495 120040822A5210 PAN BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND DOOR PAN WITH .187 INCH LONG CRACK, MED DOOR PAN, AFT SIDE AT NR 5 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20040924001192004092400119NM 2004 9 24 USAA040457 120040812A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19525AU48388 23860 PIT - FOUND FORWARD PRESSURE BULKHEAD CENTER CRACKED .5 INCH, STATION 178 FPBH RBL 6 WL 215. INSTALLED DOUBLER REPAIR PER EO 5300V153 REV A. (M) 2L72 4F RTA16WE 20040927000522004092700052SO 2004 9 27 C2XA04CL087 120040831A335082311 LIGHT EMB 145 EMB145XR 3260214SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 CLE FLIGHT 3290, CREW REPORTED THAT THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE MID CABIN EMERGENCY EXIT LIGHT ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040927000552004092700055NM 2004 9 27 0401416303 120040821A3040 CONTROLLER BOEING747 747451 1384940NM WINDOW HEAT ODOR A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01663US 23818 DURING CLIMB, RECEIVED A HEAT WINDOW R EICAS MESSAGE. AFTER COMPLYING WITH COM PROCEDURE, AN ELECTRICAL FUME ODOR EMITTED. PLACED THE WINDOW HEAT SWITCH TO OFF AND PULLED THE CIRCUIT BREAKER AND THE FUME ODOR DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE 1R RIGHT WINDSHIELD AND WINDOW 1R HEAT CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040927000572004092700057 2004 9 27 2004UALA00775 420040818A2565 SQUIB BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE ESCAPE SLIDE WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29669UA 30025 RIGHT EMERGENCY ESCAPE SLIDE SQUIB WILL NOT TEST. REPLACED RIGHT ESCAPE SYSTEM RELAY ASSY M1136. SQUIB TESTS OK. 2L72 4F4 FRTA1NM E24NE 20040927000642004092700064NM 2004 9 27 USAABB04080 120040825A2422100201021000 STATIC INVERTER BOEING757 7572B7 1384964NM E/E BAY OVERHEATED A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA19633AU 27811 PIT - FLT 123 - DURING PASSENGER LOADING, CREW SWITCHED FROM GROUND POEWR TO APU AND INITIATED AIR CONDITIONING OPERATIONS. SHORTLY THEREAFTER, AN ELECTRICAL ODOR WAS NOTED IN BOTH THE COCKPIT AND CABIN. AIR CONDITIONING WAS SECURED, BUT THE ODOR PERSISTED. MAINTENANCE WAS CALLED TO INVESTIGATE. WHEN THE E/E COMPARTMENT WAS OPENED, IT COULD NOT BE ENTERED DUE TO THE AMOUNT OF SMOKE. THE AIRCRAFT WAS DEPLANED AND THE FLIGHT CANCELLED. IT WAS REPORTED THAT ONCE THE STATIC INVERTER WAS REMOVED, AND IT THEN CAUGHT FIRE. (M) 2L72 4F RTA2NM 20040927001202004092700120NM 2004 9 27 C7WA200400027 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND E/E COMPARTMENT STRINGER 20 RIGHT STATION 460 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2L73 4F A3WE 20040927001222004092700122NM 2004 9 27 C7WA200400025 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND E/E COMPARTMENT STRINGER 28 LEFT STATION 720C CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-4 FIGURE 13. (M) 2L73 4F A3WE 20040927001282004092700128NM 2004 9 27 SWAA042777 120040923A5330655298874 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040927001292004092700129NM 2004 9 27 SWAA042778 120040923A53306518420 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT COCKPIT C-D WINDOW POST, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040927001322004092700132 2004 9 27 SWIA200413748 420040823A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM0758733 120197 DURING FINAL APPROACH, SELECTED FLAPS 25 AND GOT CONTROL FAULT ON FLAP PANEL WITH FLAP AND ADV SWS ON MAP. STALL WARNING COMPUTERS 1 & 2 WERE REPLACED. OPERATIONAL CHECK GOOD. REFERENCING 27-34-00 & 27-50-00. P/N C-8106-1, S/N OFF 472. 2L72 4T RTA31SO 20040927001372004092700137SW 2004 9 27 AC2A094949 120040410A3040222325001028 GUIDE BELL 430 430 1182150SW WINDSHIELD WIPERCORRODED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SW03430CV 49072 PIVOT POINT OF GUIDE ARM CORRODED SWELD AND BROKE. 1G72 3U RTH9SW 20040927001442004092700144EU 2004 9 27 BAQA094804 120040427A249745033500 BUSS TIE UROCOPEC135 EC135P1 8680990EU CDS OPEN B BAQAO OTHER O OTHER APAPPROACH 1 EA03601FH1997 0069 CDS HAS BUSS TIE OPEN, UNIT WILL NOT TEST. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 05/25/2004 1G72 3U O H88EU 20040928000022004092800002NM 2004 9 28 UPS04643149 120040922A2560 SEAL BOEING767 76734AF 1385212NM GE CF6 CF680C2B7 NE FIRST AID KIT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01303UP 27241 SEAL BROKEN ON FIRST AID KIT. REMOVED AND REPLACED FIRST AID KIT IAW MM 25-60-00. 2L72 4F4 FRTA1NM E13NE 20040928000152004092800015CE 2004 9 28 DXTA200400399 120040919A2750 FLAP CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL WING TE STUCK E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07931QS 7500064 DURING APPROACH THE (FLAP FAIL) CAS AND FLAPS STUCK AT APPROX. 4 DEGREES, SLAT NORMAL. REMOVED AND REPLACED THE LEFT HAND NR 4 ACTUATOR & GEARBOX WITH OVERHAULED UNIT, OPERATIONAL CHECKS WERE SATISFACTORY. ALL WORK WAS PERFORMED IAW CESSNA CITATION 750 MAINTENANCE MANUAL CHAPTER 27-52-00. 2L72 4J4 FRTT00007WITE6CH 20040928000472004092800047CE 2004 9 28 GLBA20030724 120040920A29101013880167 LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HYDRAULIC SYS INOPERATIVE A GLBAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM03169GL UE169 LANDING GEAR WILL NOT EXTEND. MANUALLY EXTENDED, REMOVED AND REPLACED HYDRAULIC LINE, PN 101-388016-7. 2L72 4T4 TRTA24CE E26NE 20040928000482004092800048NE 2004 9 28 04264677 220040920A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT INOPERATIVE A VTZAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA27677BR 7652 WO DESC: APR COMMAND SET CAUTION DURING RT ENG START. CLOSED DM. PERFORMED APR TEST IN REF AMM CH 76-13-00. OPS CHECK GOOD. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20040928000492004092800049SO 2004 9 28 2004F00386 120040920A6120 PROPELLER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE LEFT MALFUNCTIONED E GNOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15267AS 120198 20001112 UPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. CHOSE TO LAND THE AIRCRAFT SGF FOR FUTHER INVESTIGATION FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIP WAS CANCELLED, IT WAS A REPOSITIONING FLIGHT. THE CAUSE IS STILL UNKNOWN AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20040928000502004092800050NM 2004 9 28 04261421 120040917A7601 WARNING LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE ENGINES FALSE INDICATIONA VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27421FJ 3179 SLOW SPEED ABORT DUE TO ENGINE MISCOMPARE MESSAGE. MECHANIC PERFORMED ENGINE RUNS AT MULTIPLE POWER SETTINGS. NO DEFECT NOTED. COULD NOT DUPLICATE 2H72 4T4 FRTA55NM E35NE 20040928000582004092800058EU 2004 9 28 I7LA0002739 120040819A6520109044001115 GEARBOX AGUSTAA109 A109K2 0260502EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR DAMAGED E I7LAO OTHER O OTHER NRNOT REPORTED 1 NM07901HC3479 10033 REMOVAL OF TAIL ROTOR HUB AND BLADE ASSY. FOUND TAIL ROTOR GEARBOX OUTPUT SHAFT TO HAVE METAL TRANSFER TYPE DAMAGE TO SPLINE AREA. HEAT GENERATED FROM THE TAIL ROTOR TRUNION WAS ALSO EVIDENT. 1G72 3U3 URTH7EU E19EU 20040928000612004092800061 2004 9 28 CUC2004F00000 420040927A8300 BEARING BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE REDUCTION G/B INOPERATIVE E CUCAO OTHER O OTHER NRNOT REPORTED 1 WP17911KW4037 2316 30592 63039 NR 1 POWER SECTION, NR 6 BEARING KEY WASHER WAS FOUND DISTORTED WITH OPEN FRACTURE AT THE STAKING LOCATIONS OF THE WASHER. MISSING WASHER PARTS FOUND ON CHIP PLUG. TIME SINCE LAST GEARBOX REPAIR 767.3 HOURS. 1G71 4U4 U H4SW E22EA 20040928000662004092800066GL 2004 9 28 UAB2004F00000 120040527A792128010413 FLEX PACK ENSTRMF28 ENSTROM480 GL ALLSN 250C 250C20 03013GL COOLER DRSHFT FAILED B UABRO OTHER O OTHER NRNOT REPORTED 1 NM11480EH 5046 DURING INSPECTION AFTER ENGINE OIL COOLER DRIVE SHAFT FLEX PACK FAILURE. THE AIRFRAME WAS FOUND TO BE CRACKED APPROXIMATELY 90 PERCENT AROUND THE CIRCUMFERENCE OF THE TUBE. THIS WAS BELOW THE WELD, RT SIDE, AFT OF RT AFT TRANSMISSION MOUNT AREA. RECOMMEND A ONE TIME INSPECTION (VISUAL) OF THIS AREA. AFTER LANDING FOR HIGH OIL TEMP. THE OIL COOLER DRIVESHAFT WAS FOUND LAYING ON THE ENGINE. EXAMINATION FOUND THAT BOTH FLEX PLATES HAD SEPARATED. ONE BOLT WAS FOUND TO HAVE 2 BEVELED WASHERS ON ONE SIDE OF FLEX PLATE INSTEAD OF 1. ONE WAS FOUND TO HAVE FLAT SIDE OF WASHER NEXT TO FLEX PLATE. RECOMMEND ONE TIME INSPECTION, FOR PROPER INSTALLATION. 1G71 3O3 UNCH1CE E4CE 20040928000692004092800069SW 2004 9 28 ALG2004F00046 120040820A6397 WIRE BELL 407 407 1182206SW ALLSN 250C 250C47B GL CHIP DETECTOR SHORTED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03937AL 53383 ON TAKE OFF. WHILE TAKING OFF THE MAIN TRANSMISSION CHIP LIGHT CAME ON, RETURNED TO GI 59 AND LANDED. MAINTENANCE CHECKED CHIP DETECTOR SYSTEM FOUND NO MENTAL, DID FIND UPPER CHIP DETECTOR HAD BROKEN WIRES SHORTING OUT, REPAIRED BROKEN WIRES TESTED GOOD. 1G71 3U3 UO H2SW E1GL 20040928000722004092800072NM 2004 9 28 DLM90040921 120040926A3222 STRUT DOUG MD90 MD9030 3023690NM NOSE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27905DA 53385 AFTER LIFT OFF NOSE GEAR FAILED TO RETRACT WITH RED NOSE LIGHT REMAINING ILLUMINATED. AFTER FOLLOWING CORRECTIVE PROCEDURES THE NOSE GEAR OPERATED CORRECTLY. FOUND NOSE STRUT FLAT AND VALVE LEAKING. REPLACED O-RING AND RESERVICED STRUT WITH OIL AND AIR. OPERATED NOSE GEAR PER AMM 32-30-00-720-801 AND WAS NORMAL. 2L72 4F RTA6WE 20040928000732004092800073NM 2004 9 28 DLM88040922 120040927A2432 BATTERY DOUG MD88 MD88 3023688NM E/E COMPT. OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27991DL 53343 DURING MAINTENANCE TAXI, SHIP'S BATTERIES OVERCHARGED, CAUSING SMOKE EMISSION FROM E/E COMPARTMENT. REPLACED BATTERIES AND CHARGER. 2L72 4F RTA6WE 20040928000752004092800075NM 2004 9 28 DL73S040924 120040927A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 FUSELAGE SKIN CRACKED AT NUMEROUS LOCATIONS ALONG STRINGER 4L FROM STATION 540 - 727. REPAIRED IAW ERA 093294-14AD. 2L72 4F RTA16WE 20040928000762004092800076NM 2004 9 28 DL73S040925 120040927A5330654577644 SKIN BOEING737 737232 1384475NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 FUSELAGE SKIN GOUGED AT STATION 827 AND STR 26R. REPAIRED IAW ERA 093263-14. 2L72 4F RTA16WE 20040928000782004092800078NM 2004 9 28 DL76L040927 120040927A2710 ACTUATOR BOEING767 767332 1382001NM LT O/B AILERON MALFUNCTIONED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO27193DN 28450 AILERON LOCKOUT IN FLIGHT AND C/B POPPED. A/C DIVERTED DUE TO WEATHER AND LT O/B AILERON LOCKED OUT. CLEANED LT O/B AILERON LOCKOUT ACT CONNECTOR AND SWAPPED LEFT AND RIGHT SAMS. ALL AILERONS OPERATIONAL. AS PRECAUTION PUT THE AILERON LOCKOUT SYS TO MCO 27-11-02A. 2L72 4F RTA1NM 20040928000802004092800080 2004 9 28 SWAA042786 420040924A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040928000822004092800082 2004 9 28 SWAA042788 420040925A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SW29388SW 26591 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040928000842004092800084 2004 9 28 SWAA042790 420040925A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29727SW 27859 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040928000882004092800088NM 2004 9 28 DL73S040888 120040917A2897 RELAY BOEING737 737232 1384475NM FUEL PUMP INOPERATIVE A DALAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO27307DL 23079 BOTH AFT FUEL PUMP CBS POPPED. REPLACED R-19 RELAY. 2L72 4F RTA16WE 20040928000902004092800090NM 2004 9 28 DLM88040890 120040917A5320 RETAINER DOUG MD88 MD88 3023688NM WINDOW BELT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CRACK IN WINDOW BELT RETAINER BETWEEN STA Y= 886 AND Y=905 RT SIDE. REPAIRED WINDOW BELT RETAINER PER ERA 398163-14MA AEROMEXICO NRC T0024621. 2L72 4F RTA6WE 20040928000912004092800091NM 2004 9 28 DLM90040891 120040917A2120 ODOR DOUG MD90 MD9030 3023690NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27908DA 53388 WHILE AT GATE FLIGHT ATTENDANTS REPORT SMELL AND FUMES IN CABIN. SUSPECT LEFT PACK OVERHEAT. REPLACED COALESCER BAGS AND CHECKED ENGINES AND APU FOR LEAKS. NONE FOUND. RAN PACKS FOR 30 MINUTES, NO MORE ODOR. PACK TEMP CONTROLS ARE BOTH GOOD IN AUTO MANUAL. CHECKS ARE GOOD PER MD90 TROUBLESHOOTING MANUAL. 2L72 4F RTA6WE 20040928000932004092800093NM 2004 9 28 DLM88040893 120040917A53209911579 FITTING DOUG MD88 MD88 3023688NM FWD RT FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CRACK ON FWD AND AFT CLIP OF R1 DOOR BEAM NR 1. REPLACED CLIPS AEROMEXICO NRC T0024531. CRACK ON FWD EDGE OF R1 DOOR BEAM NR 1. REPLACED BEAM AEROMEXICO NRC T0024532. CRACK ON FWD EDGE OF R1 DOOR BEAM NR 4. REPLACED BEAM AEROMEXICO NRC T0024533. CRACK ON FWD FITTING OF R1 DOOR BEAM NR 1. REPLACED FITTING AEROMEXICO NRC T0024605. 2L72 4F RTA6WE 20040928000962004092800096NM 2004 9 28 SWAA042793 120040926A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040928001002004092800100EA 2004 9 28 COMA0460533 120040911A3241428853 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01988CA19936 7204 FLIGHT 5819 ANTI SKID CAUTION DURING LANDING. REPLACED THE ANTI SKID CONTROL UNIT. 2L72 4F RTA21EA 20040928001012004092800101EA 2004 9 28 COMA0460538 120040919A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01987CA 7199 FLIGHT 9469 RECEIVED A GEAR DISAGREE CAUTION DURING TAKEOFF, CREW DECLARED AN EMERGENCY AND RETURNED TO THE GATE SAFELY. ADJUSTED THE NLG PROXIMITY SENSOR. 2L72 4F RTA21EA 20040928001022004092800102EA 2004 9 28 COMA0460539 120040916A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01739CA 7273 FLIGHT 5808 RECEIVED A FLIGHT SPOILER CAUTION MESSAGE DURING TAKEOFF, ABORTED T/O AND RETURNED TO THE GATE. REPLACED SECU NR 1 AND 2. 2L72 4F RTA21EA 20040928001032004092800103NM 2004 9 28 CALA0400645 120040926A5311BAC1517706 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND A 1 INCH CRACK IN THE LT AND RT FRAME AT STA 616. THE FRAME WAS REPAIRED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20040928001052004092800105EA 2004 9 28 SWIA200413737 120040612A5320 THRESHOLD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW DOUBLER AT FS 312 FORWARD OF FRONT SERVICE DOOR LOWER THRESHOLD IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW DOUBLER P/N 601R38669-49. ALL WORK IAW CRJ 200 SRM 51-23-00, 51-25-21, 51-42-06, 51-25-16. 2L72 4F RTA21EA 20040928001062004092800106EA 2004 9 28 SWIA200413738 120040612A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW FS 280.00 FWD AND O/B OF RBL 9 VERTICAL J-ANGLE CRACKED P/N 600-34017-514. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW FABRICATED J-ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-13. 2L72 4F RTA21EA 20040928001072004092800107EA 2004 9 28 SWIA200413739 120040612A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW LEFTHAND 621.00 ANGLE CRACKED OUTBOARD END. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-004. 2L72 4F RTA21EA 20040928001092004092800109EA 2004 9 28 SWIA200413741 120040612A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW FS 484.00 ANGLE CRACKED AT RBL 27 OUTBOARD SIDE. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED FS 484 RBL 27 OUTBOARD INTERCOSTAL ANGLE IAW BOMBARDIER INC REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20040928001112004092800111EA 2004 9 28 QXEA200400642 120040826A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX LACK OF LUBE A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09601QX6990 10009 DEN - FLIGHT 4436 - THE FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR IS DIFFICULT TO PUSH OPEN AFTER IT HAS BEEN UNLATCHED. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBRICATED THE DOOR BOLTS AND HINGE POINTS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040928001122004092800112NM 2004 9 28 C1HA200478003 120040622A5714 SKIN BOEING727 727225 1384077NM CENTER WING CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15678MG 22555 CENTER WING LOWER SKIN IS CORRODED ON RT SIDE AT STA 535. REPAIRED IAW EO-727-57-10-01. 2L73 4F A3WE 20040928001152004092800115CE 2004 9 28 DXTA200400361 120040816A3260 POSITION SWITCH CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07330QS 5600329 AFTER POSITIVE RATE OF CLIMB DURING TAKEOFF THE GEAR WOULD NOT FULLY RETRACT, WHEN THE GEAR SELECTOR WAS MOVED TO THE UP POSITION THE MAIN GEARS WOULD NOT STOW AND THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. TROUBLESHOT LANDING GEAR SYSTEM, FOUND GEAR HANDLE WAS NOT ACTIVATING THE MICRO SWITCHES (LEVER HANGING UP). ACCESS GEAR HANDLE, LUBED MICRO SWITCH RAMP AND LEVER. CYCLED GEAR APPROX 12 TIMES, ALL OPS CHECKS GOOD REF THE CESSNA 560 MM CHAPTER 32-31-01 & 32-30-00. 2L72 4F RTA22CE 20040928001162004092800116EA 2004 9 28 COMA0460517 120040804A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01821CA 7420 CARGO DOOR ENTRY FLOOR SIDE CORRODED. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21 AND 51-25-01. 2L72 4F RTA21EA 20040928001172004092800117EU 2004 9 28 MALA040568 120040907A2560 CHARGER SAAB SF340 340B 7860101EU FLASHLIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15416XJ 340B416 CABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED HOLDER. 2L72 4T RTA52EU 20040928001202004092800120EU 2004 9 28 MALA040565 120040903A3260 SWITCH BAC 146 AVRO146RJ85A1500097EU LT MLG DIRTY A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15535XJ E2371 LEFT MLG INDICATION STAYED RED AFTER GEAR RETRACTION. MAINTENANCE PERFORMED FAULT ISOLATION FIG 108 MM CHAP 32, ALL CHECKS GOOD. CLEANED ALL SWITCHES ON LT GEAR, PERFORMED SEVERAL GEAR SWINGS, ALL CHECKS GOOD. 2H74 4F RTA49EU 20040928001212004092800121NM 2004 9 28 QXEA200400634 120040822A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM AFT CARGO BAY FAILED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09379PH11579 530 SEA - FLIGHT 2107 - DURING THE CLIMB, THE SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY FOLLOWED BY AN ASSOCIATED MASTER WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED BOTH CARGO COMPARTMENT SMOKE DETECTORS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040928001232004092800123NM 2004 9 28 DL75A040871 120040903A5320141N63221 BRACKET BOEING757 757212 1384951NM L-1 DOORWAY DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 STA 333.45 STR 7L PULLEY EMERGENCY POWER ASSIST PASSENGER DOOR L-1. PULLEY BRACKET DAMAGED. REMOVED DAMAGED PULLEY BRACKET. REMOVED FASTENER, DRILLED MOUNT HOLES. REPLACED PULLEY BRACKET PER BAC 141N6322. EMERGENCY POWER ASSIST SYSTEM RIGGED ON OPN 7899. 2L72 4F RTA2NM 20040928001252004092800125NM 2004 9 28 DL75A040873 120040819A5270284N15081 SWITCH BOEING757 757212 1384951NM AFT RH OVERWING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 RIGHT AFT OVERWING EXIT CUTOUT AUTOFIRE SWITCH CAM CORRODED. REMOVED CORROSION PER SRM 53-00-00D FIG 1. OK TO CHECK LIMITS. RIGGED SWITCH PER AMM. FOUND CAM OUT OF LIMITS PER BAC DWG 284N1508 AND REPLACED SWITCH ASSY. 2L72 4F RTA2NM 20040928001262004092800126NM 2004 9 28 DL75A040874 120040831A5270284N15081 CAM BOEING757 757212 1384951NM RT FWD OVERWING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 CAM CORRODED RIGHT OVERWING EXIT HATCH CUTOUT AUTO FIRE SWITCH CAM FWD POSITION. CLEANED CAM AND HAND BURNISHED PAINT AND DIRT RESIDUE. NO CORROSION FOUND PER SRM 51-10-02. CW VISUAL PER SRM 51-10-02, NO CORROSION FOUND. OK TO TREAT AND PAINT. RESTORED FINISH PER SRM 51-10-02. 2L72 4F RTA2NM 20040928001272004092800127NM 2004 9 28 DL757040875 120040914A5415311N31811 FITTING BOEING757 757232 1384965NM NR 2 PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27620DL 22910 NR 2 PYLON LOWER SPAR FITTING HAD FOUR OVERSIZED FASTENERS. REPAIRED IAW ERA 092712-14AD. 2L72 4F RTA2NM 20040928001282004092800128NM 2004 9 28 DL757040876 120040914A5330143N34714 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27620DL 22910 FUSELAGE SKIN AT STATION 500 - 520 AND STR 27R - 28R SUFFERED MULTIPLE DAMAGE AREAS DUE TO GROUND DAMAGE. REPAIRED IAW ERA 092585-14. 2L72 4F RTA2NM 20040928001292004092800129 2004 9 28 YENA200436 420040621A23301713310 CONNECTOR AIRBUS320 A320232 3930326EU LIVE TV OVERHEATED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15583JB 2150 LIVE TV SYS INOP. DUE TO BURNING ODOR AT 7D, PERFORMED LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR & INFORMATION NOTICE 2003-T050TR A. FOUND DISCOLORATION AT RJM (REMOTE JACK MARDULE) AT 7D. REMOVED AND REPLACED RJM IAW LTV MM 23-39-00. ALSO REMOVED SEB AT 7E AS PRECAUTIONARY IAW INFO NOTICE 2003-T050TR A AND IAW LTV MM 23-39-00. LTV SYS REACTIVATED. OPS CHECK NORMAL. 2L72 4F RTA28NM 20040928001302004092800130NM 2004 9 28 DL757040877 120040914A5330146N37505 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27620DL 22910 FUSELAGE SKIN FROM STA 1701 - 1711 ABOVE STR 17L DENTED. REPAIRED IAW ERA 092423-14. 2L72 4F RTA2NM 20040928001312004092800131NM 2004 9 28 DL75A040878 120040914A5330146N35318 SKIN BOEING757 757212 1384951NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 FUSELAGE SKIN AT STATION 1510 BETWEEN STR 28L - 29L CORRODED. REPAIRED IAW ERA 092820-14. 2L72 4F RTA2NM 20040928001332004092800133 2004 9 28 YENA200445 420040821A256560592103 BOTTLE AIRBUS320 A320232 3930326EU OVERWING SLIDE LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15591JB63 2246 LT OVERWING SLIDE RESERVOIR BOTTLE PRESSURE LOW. REMOVED AND REPLACED BOTTLE IAW 25-62-00. 2L72 4F RTA28NM 20040928001342004092800134WP 2004 9 28 IXXA0400076S 120040504A5710 VANE DOUG DC8 DC871F 302199DWP RT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING VANE SLOT HOLES ELONGNATED AT SX 515.720. REPAIR WAS ACCOMPLISHED. REMOVED ALL FASTENERS WITH THE REPAIR AREA AND REMOVED DAMAGED AREA PER APPLICABLE MANUALS, PERFORMED NDT INSPECTION PER NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED IAW EC8 SRM 51-1-8R. FABRICATED ON EXTERNAL DOUBLER, A FILLER & INTERNAL DOUBLER IAW DWG V82-R04. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER (EXTERNAL) INTERIOR SURFACE, FILLER & INTERNAL DOUBLER, APPLIED PRC SEALANT ON FAYING SURFACES PER ALL APPLICABLE MANUALS. INSTALLED EXTERNAL DOUBLER, FILLER & INTERNAL DOUBLER ON RT WING SLOT VANE IAW DWG V82-R04, DC8SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040928001352004092800135NM 2004 9 28 DL76K040881 120040914A2121211002542 FAN BOEING767 767332 1382001NM CABIN FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27174DZ 29693 DURING CRUISE AT FL410 FLIGHT ATTENDANTS NOTIFIED OF ODOR, BUT NO SMOKE. STARTED IN FIRST CLASS GALLEY, THEN WENT BACKWARDS IN AIRCRAFT, FIVE MINUTES LATER STARTED TO SMELL ODOR IN COCKPIT. F/A'S REPORT NO SMELL AFT OF FIRST CLASS. STRONG ODOR IN E/E COMPARTMENT. INSPECTED ALL F/C GALLEY, COCKPIT, FWD CARGO, AND E/E COMP. FOUND EQUIP COOLING SUPPLY FAN NOT OPERATING CORRECTLY. FAN THEN SEIZED WITH EQUIP COOLING OVERHEAT. SMELL DISSIPATED AND DID NOT RETURN. REPLACED FAN P/N 211002542. 2L72 4F RTA1NM 20040928001372004092800137EU 2004 9 28 MALA040573 120040915A2930 MANIFOLD SAAB SF340 340B 7860101EU HYD PRESSURE MALFUNCTIONED A MALAK NONE J WARNING INDICATION DEDESCENT 1 GL15451XJ 340B451 HYDRAULIC CAUTION LIGHT ILLUMINATED AND PRESSURE INDICATED LOW AFTER EXTENDING LANDING GEAR. HYDRAULIC QUANTITY READS GOOD. FOLLOWING QRH PUMPING FLAPS DOWN. HAND PUMP WOULD NOT WORK, CAME IN WITH NO FLAPS. ON THE GROUND WENT TO OVERRIDE AND THE PRESSURE CAME UP AND STAYED. MAINTENANCE REPLACED MAIN HYDRAULIC RESEVOIR AND HYD PRESS MANIFOLD. EMERGENCY HAND PUMP OPERATES NORMALLY. EMERGENCY PRESSURE HOLDS NORMALLY. 2L72 4T RTA52EU 20040928001392004092800139NM 2004 9 28 DL76P040882 120040915A2611 SMOKE DETECTOR BOEING767 767332 1382001NM MID GALLEY MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27144DA 27584 MID CABIN SMOKE ALARM WENT OFF ON T/O. F/A NOTIFIED CREW SHORTLY AFTER T/O. THOROUGHLY INSPECTED AIRCRAFT, RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE. 2L72 4F RTA1NM 20040928001402004092800140NM 2004 9 28 DL73S040883 120040915A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK INDICATION IN A FASTENER HOLE AT FS 690. THE CRACKED AREA WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 093308-14AD. 2L72 4F RTA16WE 20040928001412004092800141NM 2004 9 28 DL75A040884 120040916A5330141N83305 BEAR STRAP BOEING757 757212 1384951NM L1 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27757AT 23127 FUSELAGE BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR. REPAIRED IAW ERA 093001-14AD. 2L72 4F RTA2NM 20040928001452004092800145WP 2004 9 28 IXXA0400078S 120040503A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSP CRACK WAS FOUND IN LT FUSE NOSE SECTION HOLD OPEN HOOK COMPT BETWN STA FS 8.00 TO FS 17.0, L-15L TO L-16L. REPAIR WAS ACCOMPLISHED. FASTENERS WITHIN REPAIR AREA, INCLUDING DAMAGED SKIN WERE REMOVED. PERFORMED A NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, TWO FINGER DOUBLERS AND A FILLER IAW DRAWING V82-R03. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER, FILLER AND FINGER DOUBLERS IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG 1. INSTALLED THE REPAIR DOUBLER, FINGER DOUBLERS AND FILLERS ON FWD PASSENGER DOOR BUMPER SKIN AREA USING NEW FASTENERS IAW DWG V82-R03, DC8 SRM 51-1-21 AND 51-3-0 PG 1. 2L74 4F RT4A25 20040929000022004092900002NM 2004 9 29 04FDEA02263 120040728A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON UPPER SURFACE OF STRINGER 7L STA 876. CORROSION DAMAGE ON UPPER SURFACE OF STRINGER 7L, STA 876 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED DAMAGED STRINGER SECTION BS 870 - 890+10, STR 7L PER SRM 51-10-5 AND 51-30-2. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED, INSTALLED NEW STRINGER SECTION BS 870 - 890+10 AND REPAIR PLATES PER SRM 53-10-3 FIG 3 STEPS 4-8. 2L73 4F RTA3WE 20040929000042004092900004NM 2004 9 29 04FDEA02265 120040728A5330651862216 SKIN BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON INNER SKIN AT AFT CARGO DOOR AFT CUTOUT LOWER CORNER. REPAIRED INNER SKIN AT AFT CARGO DOOR AFT CUT OUT LOWER CORNER PER FED EX E.A. 7-5310-55341. 2L73 4F RTA3WE 20040929000052004092900005NM 2004 9 29 AWXA200400789 120040720A2933EA933376 SEAL BOEING BOEING737 737277 1384570NM HYD INDICATOR DAMAGED A AWXAO OTHER N FALSE WARNING CRCRUISE 1 WP28189AW B01114 22656 PHX - EMERGENCY LANDING - FLT 0628 - EN ROUTE FROM OAK TO PHX AT 33,000 FT A-SYSTEM HYDRAULIC QUANTITY INDICATOR WAS ERRATIC INDICATING BETWEEN A HALF QT AND FULL. DECLARED EMERGENCY INTO PHX. AFTER LANDING HYDRAULIC QUANTITY INDICATION RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED A-SYSTEM HYDRAULIC QUANTITY TRANSMITTER IAW T/C R4R29001, INDICATOR STILL READING INCORRECT, REPLACED QUANTITY INDICATOR AND SYSTEM CHECKED GOOD. VENDORS FUNCTIONAL TEST OF INDICATOR S/N B01114 CONFIRMED FAILURE OF UNIT. TEARDOWN OF UNIT FOUND HEAVY CONTAMINATION, LAMPS INOPERATIVE CAUSING UNEVEN ILLUMINATION, AND A DAMAGED FILL TUBE. REPLACED LAMPS (P/N 328) AND FILL TUBE, UNIT WAS CLEANED, CALIBRATED AND TESTED IAW CMM 292L72 4F RTA16WE 20040929000062004092900006NM 2004 9 29 04FDEA02180 120040726A5330 SKIN BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 DENT IN FUSELAGE SKIN BS 320-330 AND 2 INCHES ABOVE STR 21R. REPAIRED THE FUSELAGE SKIN AT BS 320 TO 330 2 INCHES ABOVE STR 21R PER EA 7-5330- 70671 2L73 4F RTA3WE 20040929000092004092900009NM 2004 9 29 04FDEA02088 120040715A5315 FLOORBEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION FLOORBEAM FASTENER HOLES BS 1110 LBL 21 WL 208. REMOVED AND REPLACED FLOORBEAM UPPER CHORD SECTION AT BS 1110 LBL 20-22.5 WL 208 PER SRM 53-10-8 2L73 4F RTA3WE 20040929000172004092900017NM 2004 9 29 04FDEA01978 120040706A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093", FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000182004092900018NM 2004 9 29 04FDEA01979 120040706A5720ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040929000212004092900021NM 2004 9 29 04FDEA01982 120040706A5753ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.407; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.405 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000222004092900022NM 2004 9 29 04FDEA01983 120040706A5753ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.399; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.395 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000232004092900023NM 2004 9 29 04FDEA01984 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.196. COMPLIED WITH FEDEX EA# 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040929000242004092900024NM 2004 9 29 04FDEA01985 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.195. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040929000252004092900025NM 2004 9 29 04FDEA02007 120040707A5710ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000272004092900027NM 2004 9 29 04FDEA02009 120040707A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.406; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000282004092900028NM 2004 9 29 04FDEA02010 120040707A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.408; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000292004092900029NM 2004 9 29 04FDEA02011 120040707A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.020; REMAINING THICKNESS: 0.486 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000302004092900030NE 2004 9 29 AALA20040984 220040902A7261 GASKET DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE OIL CAP WORN A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW2173444 49470 INFLIGHT BLUE HAZE AND FAINT SMOKE IN CABIN ON TAKEOFF. HAZE SOON DISSIPATED. AFTER LANDING DURING TAXI IN, SMOKE AND ODOR APPEARED AGAIN. PACKS SHUT DOWN AND SMELL AND HAZE DISSIPATED AGAIN. FOUND APU OIL SERVICE CAP WITH WORN GASKET. REPLACED APU OIL SERVICE CAP AND PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20040929000312004092900031WP 2004 9 29 AALA20040985 120040923A7830 ACCOUSTIC LINER DOUG DC9 DC982 3022082WP THRUST REVERSER DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21578AA 53155 BNA - FOUND HOLE IN LEFT THRUST REVERSER ACCOUSTIC LINING 1.5 INCHES LONG BY .5 INCHES WIDE BY .5 INCH DEEP AT 1.00 POSITION 7.5 INCHES IN FROM TRAILING EDGE LOOKING UP AT TAIL PIPE. AIRCRAFT FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM BNA TO DFW FOR FURTHER EVALUATION OF DAMAGE. 2L72 4F A6WE 20040929000322004092900032WP 2004 9 29 AALA20040986 120040923A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21245AA 49257 MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT POSITION AB51 AND AB52 FOR MID CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000332004092900033WP 2004 9 29 AALA20040987 120040923A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 AFT TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000342004092900034NM 2004 9 29 AT0400016 120040829A2120 ODOR BOEING717 717200 1383700NM CABIN DETECTED A ZZDAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO15952AT 55014 RETURNED TO ATL AFTER TAKEOFF BECAUSE OF REPORTED SMELL OF SMOKE OR ELECTRICITY EMITTING FROM THE GALLEY 2 AREA. RAN LEFT AND RIGHT ENGINE AND BOTH PACKS, NO DEFECTS NOTED. CHECKED E & E AND CARGO COMPARTMENT REF M/M 49-10, 21-00, 71-00 AND 05-52. 2L72 4F TRA6WE 20040929000352004092900035 2004 9 29 P5CA0401189 420040909A221637572021 COMPUTER BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE COCKPIT MALFUNCTIONED A P5CABA EMER. DESCENT UNSCHED LANDING O OTHER CLCLIMB 1 WP23920FT 22237 AFTER T/O AFTER GEAR UP, FELT A/COLL TO THE LEFT, GOT CONTROL OF A/C THAN IT HAPPENED AGAIN. FLIGHT CONTROL SHOWING UPPER RUDDER MOVING TO THE LEFT, THEN SLOWLY GOING BACK TO CENTER. DECLARED EMERGENCY & SHUTOFF UPPER YAW DAMPER COMPUTER, PROBLEM SEEMED TO GO AWAY. REPLACED UPPER YAW DAMPER COMPUTER, ALL OPERATIONS NORMAL. 2L74 4F4 F A20WE E3NE 20040929000362004092900036NM 2004 9 29 P5CA0401190 120040907A291027204100113 LINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL HYD SYSTEM DENTED A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23454PA 30812 AFTER T/O NOSE GEAR WOULD NOT RETRACT. STATUS MESSAGE -GEAR DISAGREE-, -GEAR MONITOR-, -GEAR DOOR-. REPLACED DENTED HYDRAULIC LINE & BROKEN STOP BRACKET IN NOSE WHEEL WELL, PERFORMED INSPECTION OF NOSE WHEEL WELL & NO FURTHER DAMAGE. GEAR SWING ACCOMPLISHED PER AMM 12-15-05, ALL OPS NORMAL. 2L74 4F4 FRTA20WE E23EA 20040929000372004092900037NM 2004 9 29 P5CA0401216 120040914A5320 FITTING BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LEFT NOSE WELL BULKHEAD O/B SIDE OF NLG LWR STR FITTING IS CORRODED. REMOVED CORROSION, PRIMED & TREATED. 2L74 4F4 F A20WE E20EA 20040929000382004092900038NM 2004 9 29 P5CA041224 120040914A5330 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 EXTERNAL SKIN AT STA 255 STR 32L AT LAP JOINT DELAMINATION. REMOVED BULGE, NO CORROSION FOUND, REMOVED FASTENER, INSTALLED NEW FASTENER, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040924000582004092400058EA 2004 9 24 ASOA04562 120040803A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11827AS 7212 DURING AN OVERNIGHT CHECK IN SHV, THE EXTERIOR LEFT OVERWING AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR LEFT OVERWING AFT EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040924000892004092400089NM 2004 9 24 USAA040466 120040818A5330 SKIN BOEING737 7373B7 1384580NM KEELBEAM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19529AU48045 2441 PIT - FOUND KEEL BEAM SKIN CRACKED .5 INCH, KEEL BEAM SKIN STATION 684 RBL 6. DOUBLER INSTALLED PER SRM 53-60-12 FIG 202. (M) 2L72 4F RTA16WE 20040924000942004092400094NM 2004 9 24 USAA040493 120040822A5210 PAN BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND MED DOOR PAN CRACKED .187 INCH, AFT SIDE AT NR 6 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M) 2L72 4F RTA16WE 20040924000952004092400095NM 2004 9 24 USAA040480 120040806A5343 FITTING BOEING737 737301 1384611NM MLG BEAM CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND FITTING CORRODED 1 INCH IN DIAMETER, TWO EACH, RSS 202 ON MAIN LANDING GEAR BEAM. REMOVED AND REPLACED FITTING, DRILLED AND REAMED AS REQUIRED PER AMM 57-15-00. (M) 2L72 4F RTA16WE 20040924000962004092400096NM 2004 9 24 USAA040449 120040721A5754 SKIN BOEING737 7374B7 1384702NM NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND SKIN TO CORE BOND DELAMINATION 2 INCH BY 3 INCH AREA, NR 5 SLAT TOP SURFACE OUTBOARD END. REMOVED DAMAGED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040924000982004092400098NM 2004 9 24 USAA040490 120040822A5311 FRAME BOEING737 737301 1384611NM FS DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - REPLACED INCORRECT FRAME REPAIR, STATION 727B AND 727C STRINGERS S-19R TO S23R. REMOVED OLD REPAIR AND FABRICATED NEW REPAIR PARTS AND INSTALLED PER EA 68376. (M) 2L72 4F RTA16WE 20040924001032004092400103NM 2004 9 24 USAA040477 120040823A5743 SPAR BOEING737 737301 1384611NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND SPAR CRACKED .015625 INCH CRACK, LEFT REAR SPAR MLG MOUNT HOLE 6 O'CLOCK POS. REAM HOLE AND PIT WITH MACHINED BUSHING PER EO 5702V054. (M) 2L72 4F RTA16WE 20040924001042004092400104NM 2004 9 24 USAA040494 120040822A5210 WEB BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 PIT - FOUND WEB CRACKED .750 INCH LONG, MED INNER DOOR WEB, AFT SIDE AT NR 4 DOOR STOP. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER TYP REPAIR 52-10-16. (M) USAA 2L72 4F RTA16WE 20040927000012004092700001NM 2004 9 27 SWAA042759 120040922A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29764SW 27878 EEPLS COVER AT ROW 11 ABC, MISSING. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040927000072004092700007NM 2004 9 27 SWAA042765 120040922A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 827, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040927000092004092700009NM 2004 9 27 CALA0400641 120040917A3350D71701100 BATTERY BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2724202 30429 THE EMERGENCY BATTERY PACK AT LT SEAT ROW 20 & 21 (STA 1250) FAILED TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00. 2L72 4F RTA16WE 20040927000112004092700011NM 2004 9 27 CALA0400643 120040919A3320F40D41 SOCKET BOEING737 7373T0 1384582NM ROW 18 ABC SHORTED A CALAFH ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2760312 23363 SMOKE BEGAN COMING FROM THE FLOURESCENT SIDEWALL LIGHTING AT ROWS 18-19 ABC WHILE EN ROUTE FROM TUS TO IAH. THE HALON FIRE EXTINGUISHER WAS USED, LIGHTS WERE TURNED OFF, AND CIRCUIT BREAKERS WERE PULLED. THE SMOKE SUBSEQUENTLY CLEARED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND THE LIGHT SOCKET AT ROW 18 ABC SHORTED. THE LIGHT SOCKET WAS REMOVED AND REPLACED. IN ADDITION, THE FIRE EXTINGUISHER WAS REPLACED. 2L72 4F RTA16WE 20040927000132004092700013NM 2004 9 27 372PA0062 120040909A5310 FAILSAFE BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 FAILSAFE LINK BETWEEN BS 967 AND BS 986.5 AT LBL 46 CORRODED. REPLACED FAILSAFE LINK PER SRM 51-10-2. 2L72 4F RTA16NE 20040927000152004092700015NM 2004 9 27 372PA0064 120040909A5320 SUPPORT ANGLE BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 AFT CARGO BIN BS 767 AT STR 19 LT UPPER SIDE WALL PANEL SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-02. 2L72 4F RTA16NE 20040927000172004092700017NM 2004 9 27 0401306309 120040810A3350 BATTERY PACK BOEING747 747451 1384940NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND C-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040927000202004092700020SO 2004 9 27 CHQA000534 120040812A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286SK 145443 FORWARD EMERGENCY LIGHTS STAY ON WHEN TESTING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT THE SERVICE DOOR IAW EMB 145 AMM 33-50-11. OPS CHECKS GOOD AT THIS TIME AND DATE. 2L72 4T RTT00011AT 20040927000212004092700021SO 2004 9 27 CHQA000517 120040709A3350 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT MALFUNCTIONED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265SK 145226 SERVICE DOOR EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED DC/AC INVERTER NR 2 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040927000222004092700022SO 2004 9 27 CHQA000518 120040709A3350 LIGHT EMB 145 EMB145LR 3260212SO SEAT 8A INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265SK 145226 FLOOR LEVEL EMERGENCY LIGHTING AT SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING STRIP AT SEAT 8A IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040927000232004092700023NM 2004 9 27 372PA0076 120040909A5320 ANGLE BOEING737 737306 13844BGNM RAD INLET CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 DRAG ANGLE CRACKED ABOVE RIGHT RAM AIR INLET. REPLACED ANGLE PER EA 53-235. 2L72 4F RTA16NE 20040927000242004092700024NM 2004 9 27 SWAA042766 120040922A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040927000272004092700027NM 2004 9 27 SWAA042768 120040922A3350612825 BATTERY BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED A1 CHECK, FOUND RT FWD SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040927000292004092700029NM 2004 9 27 SWAA042770 120040922A53206546568 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER WEB AT BS 1016, STRINGER 7R, CRACKED. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040927000532004092700053NM 2004 9 27 0401406313 120040822A3397 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHT LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01673US 30268 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51ABC-61ABC. SECURED ELECTRICAL CONNECTION ON AFT LIGHT SOCKET. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040927000652004092700065CE 2004 9 27 2004F00392 120040821A55201016200131 BRACKET BEECH 1900 1900D 1154162CE LT STAB ELEVATORCORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 SO1717541 UE203 AT SCHEDULED ROUTINE MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT CENTER ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20040927000662004092700066CE 2004 9 27 2004F00393 120040823A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE LT ENGINE BROKEN A GUUAO OTHER N FALSE WARNING CRCRUISE 1 SO1787554 UE227 FLT 9307 - EYW/TPA - DUIRNG FLIGHT, LEFT FIRE LOOP AND LEFT FIRE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20040927001232004092700123 2004 9 27 SWAA042772 420040923A256565C16820 HOOK BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 R2 DOOR EVAC SLIDE HOOK ATTACH SCREW, MISSING. REMOVED AND REPLACED ATTACH SCREW PER MM. 2L72 4F RTA16WE 20040927001272004092700127NM 2004 9 27 SWAA042776 120040923A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND 5 EACH EEPLS COVERS AT ROWS 1 ABC, 2 ABC, 5 ABC, 17 ABC, 23 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040927001452004092700145EU 2004 9 27 ALGA094840 120040527A6230C622A1003102 SCISSORS UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03516AL1057 1157 SCISSORS DEBONDED. REPLACED WITH NEW OR SERVICEABLE PART BY FIELD MAINT. 1G72 3U NCR0001RD 20040928000232004092800023CE 2004 9 28 DXTA200400402 120040920A2120 ODOR CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE GALLEY DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07316QS 5600516 DURING CLIMB BETWEEN FL180-FL190, NOTICED A STRONG FUEL SMELL IN THE COCKPIT AND AT THE REFRESHMENT CENTER, DURING DECENT AND LANDING THE SMELL FADED AWAY. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20040928000302004092800030NM 2004 9 28 04FDEA02779 120040920A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040928000412004092800041NM 2004 9 28 04FDEA02803 120040922A5320 FLOOR SUPPORT BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 AFT CARGO COMPT FLOOR SUPPORT BEAM CORRODED UNDER NUTPLATE STA. 1110, RBL 6. REMOVED CORROSION, MATERIAL OUT OF LIMITS IAW SRM 53-10-5 FIG.6,PG.16 AND SRM 51-10-6. REMOVED DAMAGED AREA FROM STA 1105 TO 1115 RBL, FABRICATED 4 EA ANGLES (SPLICES). REPAIR AND 1EA U-CHANNEL IAW SR27-53-039 FIG.27, PG.52 AND 53-10-5 FIG.4, PG.9, MATERIAL USED 10133-0702/18, BAC 1509-100146/18,AND 60-27570/18 IAW SRM 53-10-5 FIG.4,PG.9. INSTALLED NEW REPAIR IAW SR27-53-039 FIG.27, PG.52. 2L73 4F4 FRTA3WE E2EA 20040928000422004092800042NM 2004 9 28 04FDEA02804 120040923A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.251, FINAL DIAMETER= 1.314. COMPLIED WITH FEDEX EA 1-5750-79749, 2L73 4F4 FRTA22WE E31N3 20040928000512004092800051NE 2004 9 28 COMA0460526 220040831A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO01819CA 7415 LT ENGINE N1 DROPPED 5 PERCENT DURING T/O. COULD NOT DUPLICATE. FOUND NO DEFECTS, OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA21EA E15NE 20040928000652004092800065NM 2004 9 28 ANCF200400031 120040918A2750 WARNING SYSTEM DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE TE FLAP FALSE ACTIVATIONW ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23593AN 53093 DURING TAKE OFF ROLL WITH FLAP AT 24 DEG, TAKE OFF WARNING WAS PRESENTED (FLAP ALARM) FLAP ALARM SWITCH WAS CHECKED AND FLAP OPERATIONAL TEST WAS PERFORMED AND FAIL DOES NOT DUPLICATE IAW AMM 27-53-01. MAINTENANCE PRACTICES FLAPS TAKE OFF WARNING, SWITCH WAS PERFORMED IAW AMM 27-53-01 PAGE 201. FLAP CONTROL VALVE WAS ADJUSTED IAW AMM 27-52-01 PAGE 204. 2L72 4F4 FRT E9NE 20040928000742004092800074NM 2004 9 28 DLM88040923 120040925A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27955DL 49886 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED IN THE BELLY AT STRINGER 30 NEAR AN ANTENNA CUTOUT AT FS 725. THE DAMAGED AREA OF SKIN AND DOUBLER WERE CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 093801-14, REV A. 2L72 4F RTA6WE 20040928000772004092800077NM 2004 9 28 DL76G040926 120040927A3610460500 SEAL BOEING767 7673P6 1385105NM LT BLEED DUCT BLOWN A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27153DL 24985 LEFT BLEED DUCT LIGHT AND MESSAGE. FOUND SEALS BLOWN IN LEFT WING ROOT DUCT AREA. REPLACED SEALS. 2L72 4F RTA1NM 20040928000812004092800081NM 2004 9 28 SWAA042787 120040924A57536546435333 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040928000852004092800085NM 2004 9 28 SWAA042791 120040925A5340907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED UPPER AND LOWER HINGE BOX FITTINGS PER SRM. 2L72 4F RTA16WE 20040928000862004092800086NM 2004 9 28 SWAA042792 120040926A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040928000872004092800087NM 2004 9 28 DL75K040887 120040916A275018196917 TRANSMITTER BOEING757 757232 1384965NM TE FLAP SYS INTERMITTENT A DALAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO27648DL 24372 DURING DESCENT INTO EWR FLAPS LOCKED OUT AT LESS THAN 1 UNIT WITH STATUS MSG T/E FLAP DISAGREE AND T/E FLAP ASYMMETRY. FLAP UP LANDING AT EWR. REPLACED LT FLAP TRANSDUCER. 2L72 4F RTA2NM 20040928000892004092800089NM 2004 9 28 DLM88040889 120040917A2120 ODOR DOUG MD88 MD88 3023688NM COCKPIT DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27952DL 49883 DURING NORMAL T/O POWER APPLICATION AT APPROX 130 KNOTS BOTH PILOTS NOTICED A STRONG ELEC ODOR. FLT ATTENDANT CALLED AT 3000 FT WITH SAME IN CABIN. RETURNED TO ATL. PERFORMED OPN 5088 - UNABLE TO DUPLICATE CONDITION. 2L72 4F RTA6WE 20040928000952004092800095NM 2004 9 28 DLM88040895 120040917A53119915562 FRAME DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CRACK ON FORMER WEB AT X=0 OF AFT P-DOME FWD FACE STRUCTURE AEROMEXICO NRC T0024606. REPLACED FORMER WEB. 2L72 4F RTA6WE 20040928000972004092800097NM 2004 9 28 SWAA042794 120040926A534065C27314 STRINGER CLIP BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP AT BS 706, STRINGER 1L, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040928000982004092800098EA 2004 9 28 COMA0460519 120040916A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01965CA 7131 FS 574 LEFT HAND SIDE HAS TWO CORRODED FASTENERS AT 8 POSITION ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1135. 2L72 4F RTA21EA 20040928001042004092800104EA 2004 9 28 SWIA200413736 120040612A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA DOOR SILL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW JOINT BRACKET LOWER SILL AT FS 319.70 P/N 601R38335-1 FWD OF RVC DOOR LOWER THRESHOLD IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CORRODED BRACKET WITH NEW, P/N 601R38-335-1 IAW CRJ SRM 51-42-21. 2L72 4F RTA21EA 20040928001102004092800110EA 2004 9 28 SWIA200413742 120040612A5320 THRESHOLD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW SERVICE DOOR THRESHOLD (SILL) CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SERVICEABLE SERVICE DOOR THRESHOLD IAW CRJ SRM 51-41-02. 2L72 4F RTA21EA 20040928001142004092800114CE 2004 9 28 DXTA200400362 120040817A28218975131 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 2 ENGINE OBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07886QS 258486 P107226 NUMBER 2 ENGINE FUEL LIGHT ILLUMINATED ON TAKEOFF ROLL AT FULL POWER GOING 30 KTS. REPLACED NR 2 ENGINE FUEL FILTER IAW HONEYWELL TFE731-5BR LMM CHAPTER 73-00-00, LEAK CHECK, OPS CHECK SATISFACTORY. 2L72 4F4 FRTA3EU E6WE 20040928001192004092800119EU 2004 9 28 MALA040570 120040910A3230HP848430721 CONTROL VALVE SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15406XJ 340B406 LANDING GEAR CONTROL C/B POPPED WHEN GEAR SELECTED DOWN, RESET C/B AND GEAR EXTENDED. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE P/N HP848430-721, S/N OFF 0019, S/N ON 2108, IAW SAAB AMM 32-31-15 OPS CHECKED GOOD. ALSO REMOVED AND REPLACED LANDING CONTROL C/B P/N MS3320-5. OPS CHECK GOOD. 2L72 4T RTA52EU 20040928001222004092800122NM 2004 9 28 DL76K040870 120040913A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27172DZ 29691 F/A REPORTED BURNING ODOR IN MID CABIN, NO COCKPIT IND WERE NOTED. SMELL DISSIPATED WHEN UTILITY BUSES WERE TURNED OFF. ONE PAX SMELLED OIL SMELL AT 42A, AFT F/A REPORTED BURNING SMELL ON FINAL APPROACH, IT TO DISSIPATED. CHECKED OVERHEAD LIGHTING, SIDEWALL LIGHTING, READING LIGHTS. CHECKED GALLEY AREAS, LAVS, RAN ENGS AND RAN PACKS WITH ENG AIR SOURCE. RECYCLED TRIM AIR VLVS, RECIRC FANS, GASPER FAN, EQUIP COOLING & NO ODOR. OK FOR SERVICE. 2L72 4F RTA1NM 20040928001322004092800132NM 2004 9 28 DL73S040880 120040914A2780655280726 CONTROL UNIT BOEING737 737232 1384475NM LE FLAPS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27322DL 23094 UPON FLAP RETRACTION AFTER TAKEOFF L/E FLAPS TRANSIT LIGHT FLICKERED, NR 1 L/E SLAT ANNUNCIATOR INDICATED FULL EXT, L/E FLAPS TRANSIT LIGHT EVENTUALLY REMAINED ILLUMINATED. REPLACED FLAP/SLAT POSITION SWITCH UNIT MODULE AND PERFORMED A TEST WITH L/E FLAP/SLAT BREAK OUT BOX -10M8546. OPS CHECKED OK PER MM27-88-000-101. 2L72 4F RTA16WE 20040929000082004092900008NM 2004 9 29 04FDEA02087 120040715A5310 CREASE BEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON CREASE BEAM BS 1080 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1080, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED CREASE BEAM. INSTALLED NEW CREASE BEAM IAW 51-30-2, 51- 20-4. 2L73 4F RTA3WE 20040929000132004092900013SO 2004 9 29 CHQA000535 120040818A801135059105 STARTER EMB 145 EMB145LR 3260212SO ENGINE FAILED A CHQAA UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 GL11375 7033 145569 AT APPROX 100-200 FT AFT T/O, ENG NR 1 FIRE INDICATION. ENG IDENTIFIED, THRUST LEVER REDUCED INDICATION WENT OUT. EMERGENCY DECLARED, RETURNED TO FIELD. ON THE GROUND THE EMERGENCY FIRE EQUIPMENT INSPECTED THE AIRCRAFT FOR FIRE INDICATIONS. NO FIRE PRESENT UPON STOPPING AND PARKING THE AIRCRAFT, BUT FOUND INDICATIONS OF A FIRE WITH A THERMAL SCOPE. MX FOUND AIR TURBINE STARTER HAD FAILED. EXHAUST DUCT AND AIR TURBINE STARTER EXHAUST SCREEN ARE BOTH DAMAGED DUE TO EXCESSIVE HEAT. REMOVED & REPLACED AIR TURBINE STARTER, AIR TURBINE STARTER GARLOCK SEAL, EXHAUST SCREEN & DUCT, ALSO AIR TURBINE STARTER SHUT OFF VALVE. A/C LEAK CHECKED & OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040929000152004092900015NM 2004 9 29 AWXA200400841 120040801A7711LG80A6 TRANSMITTER BOEING737 737277 1384570NM NR 1 ENGINE FAULTY A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28178AW3103347 22645 ON TAKEOFF ROLL AT LAS EN ROUTE FOR LAX NR 1 ENGINE TAKEOFF EPR ONLY REACHED 1.57, NR 2 ENGINE WAS NORMAL, REJECTED TAKEOFF AT 75 KTS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER IAW BMM 77-011-21-4. ENGINE RUN OPERATIONAL TEST WAS GOOD. VENDORS FUNCTIONAL CHECK OF EPR TRANSMITTER S/N N0103 COULD NOT CONFIRM REASON FOR REMOVAL. UNIT WAS FOUND TO HAVE TWO LEAKING HOSES, HOSES WERE REPLACED AND THE UNIT WAS RE-CERTIFIED. 2L72 4F RTA16WE 20040929000192004092900019NM 2004 9 29 04FDEA01980 120040706A5753ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25606FE 48602 LEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.495; MATERIAL REMOVED 0.032"; REMAINING THICKNESS: 0.463 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000202004092900020NM 2004 9 29 04FDEA01981 120040706A5753ARC199113 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.504 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76784, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000262004092900026NM 2004 9 29 04FDEA02008 120040707A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062"; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040929000392004092900039NM 2004 9 29 P5CA0401218 120040914A5230 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FWD CARGO DOOR/LWR AFT SKIN HAS CORROSION. REMOVED CORROSION, FABRICATED DOUBLER & FILLER. 2L74 4F4 F A20WE E20EA 20040929000402004092900040NM 2004 9 29 P5CA0401211 120040914A5330 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FUSELAGE SKIN JOINT HAS SURFACE CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000412004092900041NM 2004 9 29 P5CA0401213 120040914A5347 SEAT TRACK BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LEFT CENTER SEAT TRACK DIRTY & CORRODED. REMOVED MINOR CORROSION FROM TRACK, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000422004092900042NM 2004 9 29 P5CA0401223 120040914A5321 PANEL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CARGO BAY CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 AFT CARGO COMPT WALKWAY PANEL STA 1775-1795 LBL 22-45 HAS CRACKS, & CORROSION. REMOVED CORROSION, BLENDED & CUTOUT CRACK, FABRICATED DOUBLER, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000432004092900043NM 2004 9 29 P5CA0401225 120040914A5414 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LEFT WING UPPER SURFACE O/B NR 2 PYLON L/E AREA 3 PLACES OF CRACKED SKIN. REMOVED SPLICE PLATE CRACK, FABRICATED SPLICE PLATE, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000442004092900044NM 2004 9 29 P5CA0401221 120040914A5313 STRINGER BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 AFT CARGO COMPT STRINGER 50L B/W STA 1680-1700 CORRODED. REMOVED LIGHT CORROSION, PRIMED & TREATED. 2L74 4F4 F A20WE E20EA 20040929000452004092900045NM 2004 9 29 P5CA0401222 120040914A5330 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LEFT MAIN LANDING GEAR FWD CUTOUT EXTERNAL PANEL SKIN FROM LBL 21 - LBL 10 HAS CORROSION. REMOVED CORROSION, CORROSION WITHIN LIMITS, PRIMED & TREATED. 2L74 4F4 F A20WE E20EA 20040929000462004092900046NM 2004 9 29 P5CA0401214 120040914A5312 BULKHEAD BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULKHEAD EXIT SIDE UNDER RADOME LT SIDE 3RD BEAM DOWN FROM TOP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000472004092900047NM 2004 9 29 P5CA0401210 120040914A5314 KEELBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 KEEL BEAM FROM STA 1075-1095 HAS CORROSION LEFT & RIGHT SIDE. REMOVED CORROSION & TREATED PER SRM 53-10-01. 2L74 4F4 F A20WE E20EA 20040929000482004092900048NM 2004 9 29 P5CA0401215 120040914A5314 KEELBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 KEEL BEAM BOX BOTTOM SURFACE HAS CORROSION LEFT & RIGHT SIDE. REMOVED FASTENER, REMOVED CORROSION & REINSTALLED FASTENER, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000492004092900049NM 2004 9 29 P5CA0401205 120040914A5350 FAIRING BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE WING TO BODY DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 WING TO BODY FAIRING 1916L HAS DELAMINATION. CLEANED AREA & REBONDED. 2L74 4F4 F A20WE E20EA 20040929000502004092900050NM 2004 9 29 P5CA0401217 120040914A5314 KEELBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 KEEL BEAM BOX, PANEL SUPPORT STRUCTURE INNER LIP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000512004092900051NM 2004 9 29 P5CA0401227 120040927A5230 SKIN BOEING747 747249F 1384849NM PWA JT9 JT9D7A 52054NE CARGO DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 PRIOR TO DEPARTURE FOUND DAMAGE ON FWD CARGO DOOR LWR SKIN. REPAIRED DAMAGE AT LWR CORNER SKIN PER SRM 52-30-06, FIGURE 1 SHEET 7. 2L74 4F4 F A20WE E20EA 20040929000522004092900052NM 2004 9 29 P5CA0401226 120040914A5311 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 CTR CARGO COMPT FRAME TOP OF UPPER CHORD AT STA 1740 RBL 40 IS CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALLED NEW CHORD. 2L74 4F4 F A20WE E20EA 20040929000532004092900053NM 2004 9 29 P5CA0401219 120040914A5321 FLOOR PANEL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CARGO BAY CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO LEFT SIDE FLOOR PANEL BS 2040-2160 DENTED & CRACKED. CUT OUT DAMAGE AREA, FABRICATED & INSTALLED DOUBLER, PRIME & TREATED. 2L74 4F4 F A20WE E20EA 20040929000552004092900055NM 2004 9 29 P5CA0401220 120040914A2750 JACKSCREW BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE TE FLAPS CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LEFT WING NR 2 TRACK JACKSCREW HAS PITTED CORROSION. REMOVED AND REPLACED LEFT WING JACKSCREW AS PER MM 27-51-41. 2L74 4F4 F A20WE E20EA 20040929000572004092900057NM 2004 9 29 P5CA0401194 120040914A5313 STRINGER BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CARGO BAY CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 AFT CARGO COMPT STRINGER 51R HAS CORROSION. REMOVED LITE CORROSION MATERIAL, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000612004092900061NM 2004 9 29 P5CA0401198 120040914A5312 BULKHEAD BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 AFT BULKHEAD UNDER FLOOR & WEB CORRODED. REMOVED STIFFENER & WEB FROM FLOORBEAM, INSTALLED NEW ONE. 2L74 4F4 F A20WE E20EA 20040929000622004092900062NM 2004 9 29 P5CA0401199 120040914A5330 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 AFT FUSELAGE HAS SKIN CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000632004092900063WP 2004 9 29 AALA20040975 120040922A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21955U 49427 DFW - TWO EACH AFT TAIL CONE EMERGENCY LIGHTS AND AFT CATWALK OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR TWO EACH AFT TAIL CONE EMERGENCY LIGHTS AND AFT CATWALK OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000642004092900064NM 2004 9 29 AALA20040983 120040902A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21901AN 29503 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 566 FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 566 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000662004092900066WP 2004 9 29 AALA20040966 120040918A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213507A 49801 DTW - AFT AISLE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED MODULE AT ROW 20 FOR AFT AISLE PATH EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000692004092900069NM 2004 9 29 AALA20040977 120040902A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGNECY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT 952R FAILED CHECK PER CARD 2904. REPLACED BATTERY PACK AT STATION 952R FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000732004092900073NM 2004 9 29 AALA20040988 120040923A3260 SENSOR BOEING757 757231 1384950NM ZONE 700 OUT OF ADJUST A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21716TW 28484 INFLIGHT AFTER TAKEOFF RIGHT HALF OF LEFT GREEN INDICATOR GEAR LIGHT REMAINED ILLUMINATED WITH ACCOMPANING STATUS MESSAGE LANDING GEAR MONITOR. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. NOT OVERWEIGHT. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE LANDING GEAR UP LOCK/DOWN LOCK SENSOR NUMBER 2 OUT OF LIMITS. ADJUSTED NUMBER 2 UPLOCK/DOWNLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040929000762004092900076NE 2004 9 29 AALA20040990 220040921A7314 PUMP DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE ZONE 600 INOPERATIVE A AALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW219407R 49400 726804 DEN - INFLIGHT ON INITIAL CLIMBOUT SHORTLY AFTER AIRFOIL ANTI ICE TURNED ON, RIGHT ENGINE FAILED OR WENT TO IDLE POWER. RIGHT ENGINE STARTED TO PROVIDE NORMAL POWER AFTER 1 AND ONE HALF TO TWO MINUTES. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. REPLACED RIGHT ENGINE FUEL PUMP AND FUEL CONTROL. TRIMMED ENGINES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E2EA 20040929000792004092900079WP 2004 9 29 0031 220040617A753210969641 BLEED VALVE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP LT ENGINE CONTAMINATED E CIEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM03553V 5 35A141 P74430C AFTER T/O IFR CONDITIONS PILOT NOTICED LT ENG UNABLE TO MAINTAIN N1 POWER & ITT CLOSE TO MAX. RETURNED TO BASE. MX PERFORMED GROUND RUN, WAS ABLE TO VERIFY CONDITION ON GROUND. ENG SURGE VALVE SOLENOID PACK FOUND TO HAVE WATER CONTAMINATION. ENG REMOVED ENOUGH TO GAIN ACCESS TO SURGE VALVE, VALVE FOUND STUCK IN OPEN POSITION. REASON FOR MOISTURE IN SURGE VALVE SOLENOID PACK NOT DETERMINED. SURGE VALVE & SURGE VALVE SOLENOID PACK REPLACED WITH SERVICEABLE OVERHAULED UNITS. INNER CONNECT TUBING INSPECTED FOR CONDITION, SECURITY & CONTAMINATION AND WERE CLEANED. ENG REINSTALLED, RUN AND CHECKED ON THE GROUND AND FOUND TO PERFORM NORMAL. 2L72 4F4 F A10CE E6WE 20040929000832004092900083CE 2004 9 29 173041 120040618A2612 CLAMP BEECH 1900 1900C 1154161CE RT FIRE LOOP LOOSE A NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27210CJ UC110 RIGHT FIRE HANDLE FLICKERING INTERMITTENTLY IN FLIGHT. REMOVED TOP AND SIDE COWLS, INSPECTED FIRE LOOP ASSY AND CLAMPS REPOSITIONED AND SECURED LOOP ASSY PER MM 26-10-01, PERFORMED LAMP TEST, OP CHECKED GOOD. 2L72 4T RTA24CE 20040929000862004092900086CE 2004 9 29 DXTA200400353 120040803A3240387072 PRESSURE VALVE CESSNA500 560CESSNA 2076750CE BRAKE SYS FAILED E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07373QS7709 5600373 DURING TAXIING THE F/O'S BRAKES FELT SOFT, CAPTAIN'S SIDE WAS GOOD. AFTER TAKEOFF CONTINUED TO OBSERVE BRAKE PRESSURE, ALL NORMAL. AT CRUISE NOTICED A VIBRATION AND HUMMING SOUND, DIVERTED AIRCRAFT INTO MEM AND DECLARED EMERGENCY FOR LANDING. BRAKES OPS CHECK GOOD ON GROUND, JACKED AIRCRAFT FOUND BRAKE PUMP CYCLED PROPERLY. SWUNG GEAR AND PUMP STOPPED, PRESSURE BLEEDS OFF, WHILE BRAKE WAS BEING BLEED LOUD BANG FROM POWER BRAKE VALVE. REPLACED BRAKE VALVE, LEAK CHECKED AND OPS CHECKED GOOD, ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-05. 2L72 4F RTA22CE 20040929000912004092900091WP 2004 9 29 AALA20040973 120040919A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21589AA 53252 DFW - CEILING EMERGENCY LIGHTS AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040929000932004092900093NM 2004 9 29 AALA20040981 120040902A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21901AN 29503 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 500 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000952004092900095NM 2004 9 29 AALA20040979 120040901A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 LEFT FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 500 LEFT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000972004092900097NE 2004 9 29 04FDEA01815 220040620A7200 ENGINE AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4D 52054NE NR 2 FAILED A FDEAC ABORTED TAKEOFF AJ FLAME/FIRE WARNING INDICATION TOTAKEOFF 1 SO25454FE 278 UNRECOVERABLE STALL ENG NR 2 DURING T/O AT 500 FT ATB. EGT WAS RAISING TO 670 DEG C, EGT LIGHT ON, PULLED BACK THE THROTTLE TO PREVENT FURTHER EGT INCREASE. FLAME NOTED BY ATC. AS PER MTSI 72-00/3790 REMOVED AND REPLACED NR 2 ENG VANE AND BLEED CONTROL PER MM 75-31-04-4A, FOR LEAK CHECK AND ENG TRIM RUN. PREMATURE REMOVAL/INSTALLATION OFF MFG 776555-7, ON MFG 776555-5. 2L72 4F4 FRTA35EU E3NE 20040929000992004092900099WP 2004 9 29 04FDEA01734 120040615A3260806124 PROXIMITY SENSOR DOUG DC10 DC1030 3023501WP MLG MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25317FE 46835 AFTER T/O OF BOSTON GEAR HANDLE WOULD NOT RAISE. AFTER TWO ATTEMPTS GEAR HANDLE WAS RAISED. HOWEVER BOTH MAINS INDICATE UNSAT (RED LIGHTS AT S/O AND PILOTS INDICATORS ILLUMINATED). FOLLOWED QRH DIRECTION, WITH SAME RESULTS. FLEW REMAINING FLIGHT AT < 260 KIAS. T/S AS PER TAFI MANUAL REF 32-30 FAULT CODE -AC-, PERFORMED BITE TEST OF PROXIMITY BOX WITH NO FAULTS NOTED. REMOVED AND REPLACED PROX BOX AS PRECAUTIONS ALL TEST PASS NO FAULTS NOTED REF DC-10 MM REF 32-61-01-2. A/C OK FOR SERVICE. ALL INDICATIONS NORMAL. 2L73 4F A22WE 20040929001002004092900100NM 2004 9 29 QXEA200400641 120040825A1420 CONNECTOR DHAV DHC8 DHC8202 2809007NM SMOKE DETECTOR DIRTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09355PH15839 500 PDX - FLIGHT 2082 - DURING CRUISE FLIGHT, THE CREW REPORTED AN INTERMITTENT BAGGAGE SMOKE WARNING. NO SMOKE WAS NOTED. MAINTENANCE INSPECTED THE SYSTEM AND AIRCRAFT, THEN CLEANED AND RE-SEATED THE CONNECTORS ON BOTH BAGGAGE BAY SMOKE DETECTORS. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040929001012004092900101EA 2004 9 29 HNAA0400074 120040822A3244314802 TIRE DHAV DHC8 DHC8311 1386006EA NLG FAILED A HNAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA07329EN 290 AFTER LANDING A/C VEERED TO THE RIGHT. NOSEWHEEL STEERING AND LEFT RUDDER WOULD NOT RECOVER A/C TO CENTERLINE APPLIED LEFT BRAKE A/C RECOVERED TO CENTERLINE. LEFT MAIN TIRE BLOWN. REMOVED AND REPLACED LEFT MAIN TIRE, RIGHT MAIN TIRE AND NR 3 & 4 BRAKE ASSY. 2H72 4T RTA13NM 20040929001022004092900102NM 2004 9 29 AT0400018 120040917A3397 WIRE BOEING717 717200 1383700NM EMERGENCY LIGHT LOOSE A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15953AT 55015 EMERGENCY EXIT SIGN ABOVE FORWARD FLIGHT ATTENDANT SEAT COMES ON DIM WHEN ENTRY LIGHT SWITCH TURNED ON. SIGN OPS CHECK AS REQUIRED WITH EMERGENCY LIGHTS ON. ALSO LIGHT ABOVE L-1 DOOR AND 3 LIGHTS NEXT TO ENTRY LIGHTS. SECURED GROUND WIRE AT FORWARD ENTRY LIGHT ASSEMBLY, OPS CHECK FORWARD LIGHT AND EMERGENCY LIGHT NORMAL. 2L72 4F TRA6WE 20040929001042004092900104EA 2004 9 29 COMA0460541 120040921A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01458CA 7613 FLGIHT 5707 DURING TAXI OUT RECEIVED A FLAPS FAIL CAUTION MESSAGE. AIRCRAFT RETURNED TO GATE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT-. MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20040929001062004092900106NM 2004 9 29 CALA0400644 120040923A5230146A611028 SKIN BOEING737 737824 13844BZNM AFT CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2754241 28953 INSPECTION FOUND A DENT IN THE AFT CARGO DOOR SKIN. THE DENT WAS LOCATED IN THE SKIN BAY BETWEEN BEAMS B, C, AND D JUST FORWARD OF BS 809.35. THE DOOR SKIN WAS REPAIRED IAW ECRA 5231-01058. 2L72 4F RTA16WE 20040929001072004092900107EA 2004 9 29 COMA0460540 120040922A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01814CA6551 7387 FLIGHT 5442 DURING CRUISE FLIGHT RECEIVED A FLAPS FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT CVG. REPLACED THE BRAKE POSITION SENSING UNIT. 2L72 4F RTA21EA 20040929001092004092900109EU 2004 9 29 MALA040563 120040908A2913 SEAL BAC 146 AVRO146RJ85A1500097EU EDP SHAFT LEAKING A MALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 ON CLIMBOUT NOTICED OIL QUANTITY 0 AND OIL PRESSURE FLUCUATION ON RETURN TO MSP OIL PRESSURE DROPPED BELOW 50 PSI , ENGINE WAS SHUTDOWN AND SECURED PER QRH. MAINTENANCE FOUND NR 2 ENGINE EDP SHAFT SEAL BAD. REPLACED SEAL IAW 29-10-17 201, ALL CHECKS, OPS AND LEAK GOOD. NOTE 8.75 QTS OIL ADDED. 2H74 4F RTA49EU 20040929001102004092900110NM 2004 9 29 HNAA0400077 120040824A5330 SKIN DHAV DHC8 DHC8102 2809003NM FUSELAGE LIGHTNING STRIKEA HNAAK NONE O OTHER ININSP/MAINT 1 EA07935HA 142 DURING C-CHECK FOUND LIGHTNING BURNS ON FUSELAGE SKIN BETWEEN STA X123 & X136 AND STR 31S/32S. REPAIRED IAW EO8-53-04-0572. WORK SCOPE REQUIRED WAS A MAJOR REPAIR. 2H72 4T RTA13NM 20040929001112004092900111NM 2004 9 29 DLM88040914 120040923A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27917DL 49573 THE FUSELAGE SKIN WAS FOUND CORRODED NEAR AN ANTENNA CUTOUT IN THE BELLY SKIN AT FS 725 AND STRINGER 30. THE CORROSION DAMAGE WAS REMOVED WITH A 12 X 7.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 093726-14, REV A. 2L72 4F RTA6WE 20040929001122004092900112NM 2004 9 29 DL73S040915 120040923A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27317DL 23089 A 1.5 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 20L AND FS 765. THE CRACK WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE B737 SRM AND ER/A 093792-14. 2L72 4F RTA16WE 20040929001132004092900113NM 2004 9 29 DL73S040916 120040924A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08 -15 REVEALED A CRACKED FASTENER HOLE AT FS 807. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093396-14AD. 2L72 4F RTA16WE 20040929001142004092900114NM 2004 9 29 DL73S040917 120040922A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 787. THE CRACK WAS REMOVED WITH A SKIN CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093400-14AD. 2L72 4F RTA16WE 20040929001152004092900115NM 2004 9 29 DL73S040918 120040923A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 390. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED PER THE B737 SRM AND PER ER/A 093394-14AD. 2L72 4F RTA16WE 20040929001162004092900116NM 2004 9 29 DL76L040919 120040925A4940BA0601 BATTERY BOEING767 767332 1382001NM AFT CARGO OVERHEATED A DALAK NONE MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27187DN 27582 APU BATTERY OVERHEATED ON GROUND. SMELL IN CABIN OCCURRED DURING TRANSIT. REPLACED BATTERY. 2L72 4F RTA1NM 20040929001172004092900117NM 2004 9 29 DL738040920 120040925A33501317 BULB BOEING737 737832 13844CFNM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27380DA 30266 EMERGENCY LIGHT AT 15D BULLNOSE INOP. RELAMPED, CHECK GOOD. 2L72 4F RTA16WE 20040929001192004092900119CE 2004 9 29 DXTA200400350 120040801A3220 LANDING GEAR CESSNA500 560CESSNA 2076750CE NOSE MALFUNCTIONED E DXTAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL07825QS 5600655 DURING APPROACH NOSE GEAR WOULD GO TO DOWN AND LOCK ON TWO TRIES. BLEW GEAR DOWN AND PROCEEDED TO LAND. JACKED AIRPLANE, CYCLED GEAR 15 TIMES TO BLEED SYSTEM RESET AND RE-SERVICED NITROGEN BOTTLE. COULD NOT DUPLICATE GEAR PROBLEM IN ANY OF THE OPERATIONS. ALL WORK DONE IAW CESSNA 560 M/M CHAPTER 32-30-00. 2L72 4F RTA22CE 20040929001212004092900121CE 2004 9 29 DXTA200400351 120040801A1420 CONNECTOR CESSNA500 560CESSNA 2076750CE MLG DAMAGED E DXTAO OTHER N FALSE WARNING CLCLIMB 1 GL07367QS 5600367 GEAR WOULD NOT RETRACT, GEAR INTRANSIT LIGHT STAYED ON AS WELL AS THE HYDRAULIC PRESSURE LIGHT. THE GEAR WAS CYCLED SEVERAL TIMES AND NO CHANGE. JACKED AIRCRAFT AND RAN GEAR SEVERAL TIMES COULD NOT DUPLICATE. PERFORMED SLOW STROKE, OPS CHECK GOOD. FROZE UPLOCK SWITCHES AND RAN GEAR, OPS CHECK GOOD. REMOVED LT AND RT GEAR WELL CONNECTORS, TESTED RESISTANCE ON UPLOCK SWITCHES, FOUND LT MLG UPLOCK SWITCH RESISTIVE. TROUBLESHOT RESISTANCE TO LT UPLOCK SPLICES, REPAIRED WIRING IAW CHAPTER 32-60-01 OF THE CESSNA 560 WIRING DIAGRAM MANUAL, OPS CHECK GOOD. 2L72 4F RTA22CE 20040929001232004092900123CE 2004 9 29 DXTA200400338 120040715A772010644D02M03 INDICATOR CESSNA560 560XL 2076702CE ITT FAILED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07677QS7 5605367 ON TAKEOFF ROLL THE LEFT ITT IND FAILED MESSAGE CAME ON, ABORTED TAKEOFF. VERIFIED INDICATOR FAILED. REMOVED FAILED INDICATOR AND REPLACED WITH AN INSPECTED INDICATOR. OPS CHECKED GOOD DURING LEFT/RIGHT ENGINE RUNS, ALL INDICATIONS NORMAL IAW THE CESSNA 560XL MM CHAPTER 77-40-00. 2L72 4F RTA22CE 20040929001242004092900124NM 2004 9 29 DLM88040896 120040917A521099557521 BEAM DOUG MD88 MD88 3023688NM L1 DOORWAY CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CRACK ON AFT EDGE OF L1 DOOR BEAM NR 1 NRC T0024535. REPAIRED AFT EDGE OF L1 DOOR BEAM NR 1. 2L72 4F RTA6WE 20040929001252004092900125NM 2004 9 29 0401266638 120040717A5415 FRAME BOEING747 747251B 1384892NM PYLON BULKHEAD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01638US 23549 DURING H-CHECK FOUND CRACK IN NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 66-165160. 2L74 4F A20WE 20040929001262004092900126NM 2004 9 29 DLM88040897 120040917A53105936038501 BEAM DOUG MD88 MD88 3023688NM CARGO DOORWAY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CORROSION ON C3 CARGO BIN DOOR JAMB BEAM NRC T0024527. REPLACED C3 CARGO BIN DOOR JAMB BEAM. 2L72 4F RTA6WE 20040929001272004092900127NM 2004 9 29 DLM88040898 120040918A531059364421 DOOR FRAME DOUG MD88 MD88 3023688NM C3 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CORROSION ON AFT LOWER WEB OF C3 CARGO BIN DOOR JAMB CLOSE TO STA Y= 1212 AEROMEXICO NRC T0024551. REPLACED WEB OF LOWER C3 CARGO BIN DOOR JAMB. 2L72 4F RTA6WE 20040929001282004092900128NM 2004 9 29 DLM88040899 120040918A531059360381 BEAM DOUG MD88 MD88 3023688NM DOORWAY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CORROSION ON C2 CARGO BIN DOOR JAMB BEAM AEROMEXICO NRC T0024526. REPLACED CORRODED AREA OF C2 CARGO BIN DOOR JAMB BEAM. 2L72 4F RTA6WE 20040929001292004092900129CE 2004 9 29 DXTA200400344 120040722A5310 MOUNT CESSNA560 560XL 2076702CE PAX DOOR FRAME FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07635QS 5605358 AFTER TAKEOFF DOOR SEAL & CABIN DOOR ANNUNCIATOR ILLUMINATED, LOUD WIND NOISE FROM AROUND DOOR. ACCOMPLISHED AIR TURNBACK AND UPON LANDING THE MAIN ENTRANCE DOOR FELL OPEN. REPLACED AFT DOOR STRUT MOUNTING FRAMES IAW CESSNA 560XL B/P 6611267, BOTH DOOR CABLES IAW CESSNA 560 XL MM 52-10-03. PERFORMED CABIN LEAK RATE PRIMARY AND SECONDARY SEALS CHECKED GOOD IAW CESSNA 560 XL MM 21-30-00. VERIFIED DOOR OPERATION AND DOOR SEAL LEAK DOWN RATE GOOD IAW CESSNA 560 XL MM 52-10-04. 2L72 4F RTA22CE 20040929001312004092900131NM 2004 9 29 DL764040900 120040918A3233273T41124 ACTUATOR BOEING767 767432ER 1385134NM NLG CRACKED A DALAK NONE K FLUID LOSS ININSP/MAINT 1 SO27825MH 00822 29696 ON PREFLIGHT FOUND NOSE GEAR RETRACT CYLINDER RAM CRACKED AT ROD END ATTACH POINT. REPLACED NOSE GEAR RETRACT CYCLINDER BORROWED FROM AA, S/N ON 00196, S/N OFF 00822, ASSY NR 273T4112-4. 2L72 4F RTA1NM 20040929001322004092900132NM 2004 9 29 DL733040901 120040919A2611473925 CONTROLLER BOEING737 7373B7 1384580NM FIRE DETECTION FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27947WP 23376 PASSING FL280 DEPARTING SFO HAD INERMITTENT FWD CARGO FIRE WARNING (BELL & LIGHT). BOTTLES FIRED. VERIFIED NO FIRE. REPLACED FIRE DETECTION CONTROLLER. 2L72 4F RTA16WE 20040929001342004092900134NM 2004 9 29 DL73S040902 120040919A2823MA11A1062B SHUTOFF VALVE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENG FUEL MALFUNCTIONED A DALAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO27326DL 23098 709153 AFTER PUSHBACK ENGINE START, NR 2 ENGINE HAD A FLAME OUT OCCUR. DISCOVERED THAT THE NR 2 ENGINE FUEL SHUTOFF VALVE WAS AT FAULT. PART REPLACED BY TPA MTC AND ENGINE RUN NORMAL. 2L72 4F4 FRTA16WE E2EA 20040929001362004092900136NM 2004 9 29 DLM88040903 120040919A2497D233920 CABLE DOUG MD88 MD88 3023688NM BATTERY CHAFED A DALAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27951DL 49882 A/C CAME IN WITH A BATTERY CHARGER C/B POPPING. WHILE REPLACING THE BATTERY CHARGER FOUND THAT THE BATTERY CABLE HAD CHAFED AND BURNT A .25 X .75 INCH AREA IN THE REMOTE BATTERY C/B STAND. REPLACED CABLE AND CHARGER. 2L72 4F RTA6WE 20040929001382004092900138NM 2004 9 29 DL738040905 120040920A3340 BULB BOEING737 737832 13844CFNM OVERWING BURNED OUT A DALAK NONE L NO TEST ININSP/MAINT 1 SO273768 29630 LEFT OVERWING AFT EMERGENCY LIGHT INOP. RELAMPED SAME, OPS NORMAL. 2L72 4F RTA16WE 20040929001402004092900140NM 2004 9 29 DL76L040907 120040922A21503209953 VALVE BOEING767 767332 1382001NM CABIN PRESSURE INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27175DN 627 24803 CLIMBING THROUGH 7000 FT HEARD THUMP FROM RT SIDE OF CABIN. CABIN RATE OF CLIMB WENT TO 2000 FT/MIN UP. COULD NOT CONTROL PRESSURIZATION. REPLACED EQUIPMENT COOLING EXHAUST VALVE. 2L72 4F RTA1NM 20040929001422004092900142NM 2004 9 29 DL73S040909 120040923A3320 BALLAST BOEING737 737247 138448DNM CABIN LIGHTS ODOR A DALAO OTHER M OVER TEMP TXTAXI/GRND HDL 1 SO27382DL 23609 FLT ATTENDANT IN AFT GALLEY REPORTED ELECTRIC SMELL JUST PRIOR TO PUSHBACK. FOUND BALLAST IN AFT CABIN HOT. REPLACED SAME. 2L72 4F A16WE 20040929001442004092900144CE 2004 9 29 DXTA200400358 120040814A2821 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL FILTER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07842QS 258542 P107627 NUMBER 2 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF ROLL AT 100 KNTS, REJECTED TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FUEL FILTER ELEMENTS WITH NEW ELEMENTS, BOTH FILTERS CLEAN. RAN BOTH ENGINES AT 5 PERCENT BELOW TAKEOFF POWER FOR 5 MINUTES, COULD NOT DUPLICATE DISCREPANCY. ALL WORK DONE IAW HONEYWELL TFE731-5BR MM CHAPTER 73-21-02, LEAK CHECK SATISFACTORY. 2L72 4F4 FRTA3EU E6WE 20040929001472004092900147NM 2004 9 29 2004UALA00767 120040813A2913 PUMP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE HYD SYSTEM LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29642UA 25092 LOST RIGHT HYDRAULIC SYSTEM EN ROUTE, CONTINUING TO DESTINATION. LOSS OF PRESSURE DUE TO FAILED NR 2 ENGINE DRIVEN PUMP. PUMP HAS INDICATION OF OVERHEAT CONDITION. NO ADDITIONAL DETAILS FROM OSV REPORTED. 2L72 4F4 FRTA1NM E24NE 20040929001482004092900148CE 2004 9 29 DXTA200400356 120040808A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07399QS 5600510 DURING BRAKE CHECK ON TAXI OUT FOUND BOTH PEDALS ON RIGHT SIDE SPONGY. BLED BRAKE SYSTEM PER BRAKE BLEEDING PROCEDURES IAW CESSNA560 MM CHAPTER 32-42-00, BRAKES OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA22CE 20040929001502004092900150NM 2004 9 29 DL73S040911 120040923A5330 SKIN BOEING737 737232 1384475NM FUSLEAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 FUSELAGE SKIN CRACKED AT STRINGER 4L AND STATION 727A +10. REPAIRED IAW ERA 093401-14AD. 2L72 4F RTA16WE 20040929001522004092900152NM 2004 9 29 DL73S040912 120040923A5330 SKIN BOEING737 737232 1384475NM FUSLEAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27306DL 23078 FUSELAGE SKIN CRACKED AT STRINGER 4R AND STATION 390 & 400. REPAIRED IAW ERA 093395-14AD. 2L72 4F RTA16WE 20040930000012004093000001WP 2004 9 30 ABXA040332 120040831A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23814AX 46041 INSPECTION DEVIATION PER ABX REA D853-50097MR, REPAIR TRIPLER, FUSELAGE SKIN, FS 273-280, LONGERON 19 LEFT - 20 LEFT. REPAIRED AREA IAW ABX REA D853-50097MR. COI GENERATED FOR MAINTENANCE TRACKING. 2L74 4F 4A25 20040930000032004093000003WP 2004 9 30 ABXA040306 120040816A531199196182 FRAME DOUG DC9 DC931 3022065WP RT WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CRACK IN THE FORWARD POCKET EXTENDED FROM THE MAIN ATTACH HOLE TO THE FIRST REPAIR ATTACH HOLE. RIGHT MAIN FRAME REPLACED IAW EA 53400324-001-2 AND WORK ACCOMPLISHED ON NR 0271. 2L72 4F A6WE 20040930000042004093000004WP 2004 9 30 ABXA040309 120040819A53205956034363 FLOOR SUPPORT DOUG DC9 DC931 3022065WP AFT CARGO BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 LEFT INBOARD FLOOR SUPPORT FITTING CRACKED AT STA 945. REPLACED FITTING AT LEFT FLOOR TRACK, AFT LOWER CARGO, STA 945 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040930000052004093000005WP 2004 9 30 ABXA040308 120040819A5347S4755395 SEAT TRACK DOUG DC9 DC931 3022065WP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DOUBLE SEAT TRACK CORRODED AT FS 996, RIGHT BUTT LINE 6. REPLACED TRACK AT RIGHT BUTT LINE 6 AT STA 965 - 1019 IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20040930000062004093000006WP 2004 9 30 ABXA040305 120040818A531199196181 FRAME DOUG DC9 DC931 3022065WP LT WHEEL WELL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CRACK IN THE MAIN FRAME AFT POCKET, EXTENDED TO THE MAIN ATTACH BOLT. CRACK LENGTH 1.625 AND 2.170. REPAIRED IAW SERVICE REWORK DRAWING 5934375-505 IAW ABX REA D953-50391. INITIATED WATCH ITEM 924-035 FOR REPETITIVE INSPECTION INTERVALS OF 1600 FLIGHT HOURS FOR CRACK GROWTH PROGRESSION. 2L72 4F A6WE 20040930000072004093000007WP 2004 9 30 ABXA040307 120040819A5347S4755395 SEAT TRACK DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CENTER SEAT TRACK CRACKED AND CORRODED AT FS 996. SPLICED IN NEW SECTION OF TRACK STA 926 - 1019 IAW DC-9 SRM K05406 AND SRM 51-30-1. 2L72 4F A6WE 20040930000082004093000008WP 2004 9 30 ABXA040310 120040819A532099576664 INTERCOSTAL DOUG DC9 DC931 3022065WP AFT CARGO BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 CENTER INTERCOSTAL AT LOWER EDGE OF AFT LOWER CARGO DOOR HAD CRACKED ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20040930000092004093000009NM 2004 9 30 USAA040518 120040826A52301036541 HOUSING BOEING737 7373B7 1384580NM DOOR LATCH WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND HOUSING WITH EXCESSIVE WEAR CAUSING GOUGES, LATCH HANDLE SHAFT HOUSING, AFT CARGO DOOR. BLENDED OUT GOUGES AND REPLACED WORK HOUSING ASSEMBLY PER SRM 52-30-01, FIG 101, DETAIL V. (M) 2L72 4F RTA16WE 20040930000102004093000010EU 2004 9 30 ASOA04614 120040818A33503011052 LENS AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT DAMAGED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11536AS 465 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS AT ROW 1 WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT ROW 1. (M) 2H72 4T RTA53EU 20040927000602004092700060EU 2004 9 27 0401343270 120040810A5315 FLOORBEAM AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01370NW 1037 DURING SPECIAL VISIT FOUND CORROSION ON FLOORBEAM Y1162.5 FRAME 68. REPAIRED PER EA 32-200295. 2L72 4F RTA28NM 20040927000872004092700087NM 2004 9 27 USAA040517 120040819A532069365569 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 PIT - FOUND FLOOR SUPPORT INTERCOSTAL CRACKED THREE PLACES, 3 INCH EACH, BETWEEN 927 AND 947 AT 0 INCH LBL. REMOVED AND REPLACED PER SRM 53-60-51. (M) 2L72 4F RTA16WE 20040927000892004092700089EA 2004 9 27 ASOA04536 120040802A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11886AS 7531 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14 L/R WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14 L/R IAW ASA EO 600-53-0174. (M) 2L72 4F RTA21EA 20040927000922004092700092EU 2004 9 27 ASOA04554 120040715A5753S5751204920500 GUIDE AEROSPATR72 ATR72212 8680945EU NR 1 TE FLAP CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP CAM GUIDE NR 1 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP CAM GUIDE NR 1 IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040927000942004092700094NM 2004 9 27 AMTA200400986 120040804A5320 INTERCOSTAL BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND CORRODED INTERCOSTAL FROM STATION 333 TO STATION 343, LBL 12. INSTALLED NEW INTERCOSTAL CHANNEL IAW B757 SRM 51-40-02. (M) 2L72 4F RTA2NM 20040927001012004092700101EA 2004 9 27 ASOA04459 120040628A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280. (M) 2L72 4F RTA21EA 20040927001042004092700104EA 2004 9 27 ASOA04454 120040626A783022850741115 SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF ADJUST A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11849AS 7347 FLT 4242 - DURING CLIMB-OUT FROM ATL-BTR, THE CREW RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE ON EICAS AT APPROXIMATELY 18,000 FEET. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE CLEANED AND ADJUSTED THE LEFT ENGINE THRUST REVERSER STOW SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040927001052004092700105EA 2004 9 27 ASOA04453 120040623A339764645 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11913EV 7731 DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY FLOOR TRACK LIGHT AT ROW 9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR TRACK LIGHT CABLE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040927001072004092700107EA 2004 9 27 ASOA04448 120040620A5210601R3807423 MOUNT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN MCN, THE AFT ANCHOR MOUNT ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR MOUNT ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040927001092004092700109NM 2004 9 27 USAA040452 120040726A5347 SEAT TRACK BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND SEAT TRACK CORRODED 16 INCHES LONG BY .027 INCH DEEP, LEFT INBOARD SEAT TRACK STATION 44-360. SEAT TRACK EXTRUSION MACHINED, SPLICED IN SET TRACK PER SRM 53-00-52. (M) 2L72 4F RTA16WE 20040927001142004092700114NM 2004 9 27 USAA040488 120040822A5320 WEB BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND FLOOR PAN CORRODED, 3 EACH 1 INCH BY .5 INCH AREA, SUBFLOOR AFT OF STATION 1016 TO APB BL 0 TO RBL 37.5. CORROSION LEVEL 1, TASK NR C53-107-02. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01 AND 05, 51-21, 51-31 AND 51-40. (M) 2L72 4F RTA16WE 20040927001172004092700117EA 2004 9 27 ASOA04460 120040628A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE LEFT FRAME FS 718, STRINGER 10-11 AND DOUBLER WEAR FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT FRAME FS 718, STRINGER 10-11 AND DOUBLER IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20040927001192004092700119EA 2004 9 27 ASOA04449 120040623A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN MCN, THE RIGHT SIDE CLIP AT FS 484, RBL 27 AND 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT SIDE CLIP AT FS 484, RBL 27 AND 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040927001212004092700121NM 2004 9 27 C7WA200400026 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND E/E COMPARTMENT STRINGER 27 LEFT STATION 450 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2L73 4F A3WE 20040927001422004092700142EU 2004 9 27 BAQA094291 120040429A243523032022 STARTER GEN BOLKMS117 BK117A3 5626015EU ENGINE FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117LG 7032 EXCHANGE. BATTERY DISCHARGE LIGHT ON AUD MOTOR ARCHING ON ARMATURE WITH POWER ON. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 06/02/2004 1G72 3U H13EU 20040928000012004092800001NM 2004 9 28 UPS04543151 120040923A5610141T480014 WINDOW BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01461UP 28265 WINDOW CRACKED. WINDOW HEAT ARCED AND THEN OUTER WINDOW SHATTERED. F/O'S (R1) WINDSHIELD ASSY REPLACED IAW AMM 56-11-01. WINDSHIELD PROCURED FROM MFG COMPANY. AUTHORIZED RELEASE CERT FORM 8130-3. 2L72 4F4 FRTA2NM E12EU 20040928000032004092800003WP 2004 9 28 UPS04843139 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 C3 WING LT L/E AT STA. XFS 591.250 RIB IS CRACKED. REPAIRED LT WING L/E RIB AT STA. XFS 591.250 IAW SRM 57-2-0 FIG 2. 2L74 4F4 FRT4A25 E2GL 20040928000192004092800019CE 2004 9 28 DXTA200400394 120040915A3260327 BULB CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL MLG INDICATOR BURNED OUT E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07964QS2844 7500164 NOSE LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT COME ON WHEN LANDING GEAR EXTENDED. WENT OUT AND TROUBLESHOT THE PROBLEM CHECKLIST FOLLOWED AND LANDING GEAR WERE PNEUMATICALLY BLOWN DOWN AND D RING FOR NLG WAS PULLED NO RED UNSAFE LIGHT EVER ILLUMINATED. NO GEAR HORN WITH FLAPS AT 35 DEGREE, NO GREEN NLG LIGHT WHEN ROTARY TEST SELECTED TO LDG GEAR POSITION. PLACED AIRCRAFT ON JACKS AND PERFORMED RETRACTION TEST, FOUND NLG LIGHT BURNED OUT. REPLACED LIGHT BULBS, PERFORMED LANDING GEAR OPS CHECK IAW MM CHAPTERS 32-20-06 AND 12-10-36, NO DEFECTS NOTED. 2L72 4J4 FRTT00007WITE6CH 20040928000202004092800020CE 2004 9 28 DXTA200400396 120040916A323067421801 BARREL CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL MLG CORRODED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07953QS3351 7500153 AT FL 390 AIRPLANE EXPERIENCE A JOLT AND THE GEAR UNLOCK LIGHT ILLUMINATED WE SLOWED AND DESCENDED BELOW FL180, EXTENDED GEAR NORMALLY AND WITH EMERGENCY BLOW DOWN. REMOVED THE NOSE LANDING GEAR UPPER AND LOWER BARREL ASSEMBLIES, INSPECTED AND FOUND UPPER BARREL TO BE PITTED AND CORRODED. INSTALLED NEW UPPER BARREL IAW SRM CHAPTER 32-20-02. 2L72 4J4 FRTT00007WITE6CH 20040928000212004092800021CE 2004 9 28 DXTA200400392 120040913A3234 SELECTOR PANEL CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07342QS 5600324 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 3 GREEN LIGHTS. HYD PRESS ON LIGHT ILLUMINATED, NOSE GEAR HANDLE IN UP POSITION. RETURNED GEAR HANDLE TO DOWN POSITION. ALL INDICATIONS NORMAL. TROUBLESHOT AND FOUND PROBLEM TO BE WITH GEAR SELECTOR ASSEMBLY, FOUND CONNECTOR P160 TO BE LOOSE, RE-SECURED CONNECTOR. PERFORMED OPERATIONAL CHECKS, NO DEFECTS NOTED. WORK DONE IAW MM CHAPTER 32-30-01. 2L72 4F4 FRTA22CE E25EA 20040928000532004092800053SO 2004 9 28 GW12004F00001 120040408A323042042002 ARM PIPER PA42 PA42720 7104212SO PWA PT6 PT6* 52043EA LT MLG FRACTURED B GW1RO OTHER O OTHER NRNOT REPORTED 1 EA03950TA2684 425501050 LEFT MLG RETRACT ARM, PN 42042002, WHICH ATTACHES THE ACTUATOR TO THE FORWARD SIDE BRACE FAILED DURING RETRACTION OF THE LANDING GEAR AFTER TAKE OFF. PILOT STATED THAT AFTER A NORMAL TAKE OFF HE ATTEMPTED TO RETRACT THE LANDING GEAR THE LEFT MAIN FAILED TO RETRACT. THE PILOT THAT STATED THE LEFT GEAR DOWN LIGHT REMAINED ILLUMINATED. THE PILOT THEN EXTENDED THE NLG AND RT MLG AND CONTINUED, WHERE THE RETRACT ARM WAS REPLACED, THE GEAR WAS INSPECTED AND RETRACTION TEST ACCOMPLISHED. 1L72 4T3 T A23SO E2NE 20040928000642004092800064NE 2004 9 28 ASMF200409003 220040910A732176960615 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23162PL14870152 49765 725568 AIRCRAFT RETURNED TO PLATFORM, DURING TAKE OFF RT GENERATOR FAILED. RT ENGINE WAS INDICATED 530 DEGREE C, WITH OUT EPR AND FUEL FLOW INDICATION. FCU, PT7 TEST POINT WERE CHECKED, ACCELERATION CAMERA WAS LUBRICATED AND ENGINE WAS RUNNING WITH N1 24 PERCENT, N2 53 PERCENT EGT 435 DEGREES C, EPR 1.03, F/F 900 AND FAIL CONTINUE. FCU WAS REPLACED IAW MM 73-12-02, BOROSCOPE INSPECTION WAS PERFORMED IAW MM 72-00-00, ALL CORRECT AND TRIMMING WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040928000682004092800068SW 2004 9 28 ALG2004F00047 120040825A6220 ROTOR BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL MAIN OVERTORQUED E ALGAA UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 SW03174AL 52067 IN A HOVER, WAS AT A HOVER ABOUT TO TAKE OFF WHEN EVERYTHING STARTED SPEEDING UP, LOOKED AT THE TORQUE GAUGE AND SAW 120 PERCENT TORQUE, IMMEDIATELY LOWERED THE COLLECTIVE AND LANDED, AS LOWERED THE COLLECTIVE AND EVERYTHING RETURNED TO NORMAL. MAINTENANCE IS COMPLYING WITH A OVERTORQUE INSPECTION IAW MM. 1G71 3U3 UNCH2SW E1GL 20040928000942004092800094NM 2004 9 28 DLM88040894 120040917A531099577359 BEAM DOUG MD88 MD88 3023688NM RT OVERWING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CRACK ON FWD ANGLE OF AFT RIGHT OVERWING EXIT DOOR BEAM NR 1 AEROMEXICO NRC T0024557. REPLACED FWD ANGLE OF RIGHT OVERWING EXIT DOOR BEAM NR 1. 2L72 4F RTA6WE 20040928001182004092800118EU 2004 9 28 MALA040569 120040909A2560 BATTERY PACK SAAB SF340 340B 7860101EU FLASHLIGHT INOPERATIVE A MALAO OTHER L NO TEST LDLANDING 1 GL15454XJ 340B454 UPON LANDING IN DTW, F/A REPORTS EMERGENCY FLASHLIGHT IS NOT BLINKING. MAINTENANCE INSTALLED SERVICABLE BATTERY PACK, ALL CHECKS GOOD. 2L72 4T RTA52EU 20040928001362004092800136NM 2004 9 28 QXEA200400633 120040821A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM AFT CARGO DOOR DAMAGED A QXEAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 NM09411QX6608 4055 BOI - FLIGHT 2341 - WHILE AT FL250, THE FLIGHT EXPERIENCED A RAPID DEPRESSURIZATION. THE CREW PERFORMED AN EMERGENCY DESCENT TO 15,000 FT AND DONNED THE 02 MASKS. THE FLIGHT WAS DIVERTED TO BOI AND MADE A NORMAL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR SEAL DAMAGED. THE SEAL WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040929000032004092900003NM 2004 9 29 04FDEA02264 120040728A531065207291 DOOR FRAME BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD CONTINUING UNDER FILLER. REPAIRED AFT CARGO DOORWAY AFT FRAME AT CORNER THRESHOLD PER FED EX E.A. 7-5310- 55341. 2L73 4F RTA3WE 20040929000072004092900007NM 2004 9 29 04FDEA02085 120040715A5310 CREASE BEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON CREASE BEAM BS 1010 - 1050 LBL 65 WL 208. CORROSION ON CREASE BEAM BS 1010 TO BS 1050, LBL 65, WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVE DAMAGED CREASE BEAM, INSTALLED NEW CREASE BEAM IAW SRM 51-30- 2, 51-20-4. 2L73 4F RTA3WE 20040929000102004092900010NM 2004 9 29 04FDEA02089 120040715A5315 FLOORBEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION FLOORBEAM LWR FWD AT BS 1050 LBL 1 TO 22 WL 201. REMOVED DAMAGE ON FLOORBEAM LWR FWD AT BS 1050, LBL 1-22. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-8, 51-10-1. 2L73 4F RTA3WE 20040929000112004092900011NM 2004 9 29 04FDEA02032 120040708A5740ARC4125501 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP ATTACHING RIB STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20040929000122004092900012NM 2004 9 29 04FDEA02033 120040709A5320A5A71241 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 CENTER CARGO BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. LONGERON SPLICE 48R REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PART MARKED FX A5A7124-1 PER GMM 7-0-1001. 2L73 4F RTA22WE 20040929000142004092900014NM 2004 9 29 VNAA0408007 120040815A219736HB RELAY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE RECIRC FAN FAILED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07440JS 3058 IN FLIGHT, THE CREW REPORTED SMOKE IN THE CABIN AND DIVERTED TO TRI. MAINTENANCE CONTROL DISPATCHED MECHANICS FROM PIT. MAINTENANCE FOUND THAT THE RECIRC FAN WOULD NOT TURN OFF AND OVERHEATED CAUSING SMOKE DUE TO A FAILED 36HB RELAY. THE RECIRC FAN WAS MEL'D WITH 21-1-2 CODE-C. THE MEL WAS CLEARED IN PIT WHEN MAINTENANCE REPLACED THE 36HB RELAY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040929000562004092900056NM 2004 9 29 P5CA0401193 120040904A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RIGHT WING UPPER SKIN HAS SURFACE CORROSION. REMOVED LITE CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000582004092900058NM 2004 9 29 P5CA0401195 120040914A5315 FLOORBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT FLOORBEAM CRACKED. REMOVED & REPLACED DAMAGED AREA. 2L74 4F4 F A20WE E20EA 20040929000602004092900060NM 2004 9 29 P5CA0401197 120040914A5320 FLOOR SUPPORT BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT LONGITUDINAL FLOOR SUPPORT CRACKED. REMOVED AND REPLACED DAMAGE AREA. 2L74 4F4 F A20WE E20EA 20040929000822004092900082NM 2004 9 29 PCAA0406224 120040621A275144281508010 GAUGE DHAV DHC8 DHC8102 2809003NM TE FLAPS MALFUNCTIONED A PCAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA13807EX32161 292 FLIGHT 3730 HAD TO ABORT TAKEOFF FROM BWI TO LGA DUE TO RECEIVING THE TAKEOFF WARNING HORN DURING TAKEOFF AT 20 KNOTS. THIS CONDITION WAS A REPEAT. ASSOCIATED POWER LEVER SWITCHES HAD ALREADY BEEN CLEANED AND CHECKED. MAINTENANCE REMOVED AND REPLACED THE FLAP GAUGE AND OPERATIONAL CHECKED THE SYSTEM. ALL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040929000842004092900084NM 2004 9 29 AALA20040968 120040913A3350 END PLUG BOEING757 7572Q8 1384972NM EMERGENCY LIGHT MISSING A AALAK NONE L NO TEST ININSP/MAINT 1 SW21701TW 28160 END PLUG MISSING FOR EMERGENCY ESCAPE PATH LIGHTING TO THE RIGHT OF SEAT 1B AND BEHIND SEAT 24D. INSTALLED END PLUGS FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 1B AND BEHIND SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040929000872004092900087NM 2004 9 29 AALA20040978 120040901A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 322 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000892004092900089NM 2004 9 29 AALA20040970 120040921A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 DFW - EXTERIOR EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACK AT GALLEY 1L FOR EXTERIOR EMERGENCY LIGHT AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040929000942004092900094WP 2004 9 29 AALA20040974 120040922A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21555AN 53085 DFW - FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RE-RACKED BATTERY PACK IN ASSEMBLY FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000962004092900096NM 2004 9 29 AALA20040969 120040921A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 DFW - WALL MOUNTED EMERGENCY LIGHTS IN FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK AT 1L FOR WALL MOUNTED EMERGENCY LIGHTS IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040929001432004092900143CE 2004 9 29 DXTA200400357 120040811A28218975131 FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL SYSTEM OBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07861QS 258361 P107507 NUMBER ONE ENGINE FUEL LIGHT CAME ON DURING TAKEOFF ROLL, EXTINGUISHED AFTER REJECTED TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FUEL FILTER ELEMENTS WITH NEW ELEMENTS PER HONEYWELL TECH SUPPORT REQUEST, NOTED SMALL AMOUNTS OF LINT ON EACH FILTER. RAN BOTH ENGINES AT 5 PERCENT BELOW TAKEOFF POWER FOR 5 MINUTES, COULD NOT DUPLICATE DISCREPANCY. ALL WORK DONE IAW HONEYWELL TFE731-5BR MM CHAPTER 73-21-02. 2L72 4F4 FRTA3EU E6WE 20040929001462004092900146CE 2004 9 29 DXTA200400360 120040813A2821 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL FILTER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07875QS 258375 P107650 AS THROTTLES WERE ADVANCED TO TAKEOFF POWER, THE FUEL LOOK UP ANNUNCIATOR LIGHT CAME ON, ACCOMPANIED BY THE ENGINE FUEL NR 1 ANNUNCIATOR. REMOVED AND REPLACED LEFT AND RIGHT ENGINE FUEL FILTER ELEMENTS IAW HONEYWELL TFE-731-5BR LIGHT MAINTENANCE MANUAL CHAPTER 73-21-02. RAN ENGINES, OPS CHECK NORMAL, LEAK CHECK GOOD. 2L72 4F4 FRTA3EU E6WE 20040929001492004092900149NM 2004 9 29 DLM88040910 120040923A55305911384505 SPAR CAP DOUG MD88 MD88 3023688NM VERTICAL STAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27902DE 53379 VERTICAL STABILIZER HORIZONTAL STABILIZER HINGE PLATES HAD THREE HOLES WITH DAMAGE. REPAIRED IAW ERA 093177-14AD. 2L72 4F RTA6WE 20040929001532004092900153NM 2004 9 29 DL73S040913 120040923A2410 GENERATOR BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE INOPERATIVE A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27245WA 23519 709223 ON TAKEOFF ROLL APPROX 100 KIAS EXPERIENCED RT GENERATOR BUSS OFF LIGHT. ABORTED TAKEOFF. REPLACED NR 2 CSD & GEN. 2L72 4F4 F A16WE E2EA 20040930000112004093000011EA 2004 9 30 ASOA04605 120040817A5210601R389643 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11833AS 7246 FLT 4226 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930000122004093000012NM 2004 9 30 AMTA200401120 120040905A2612710127 FIRE DETECTOR BOEING757 75723N 1384973NM RT ENGINE MALFUNCTIONED A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL31514AT 27971 INTERMITTENT 'R ENG FIRE LOOP 2' STATUS MESSAGE. REMOVED AND REPLACED NR 2 ENGINE NR 2 FIRE LOOP NR 4 DETECTOR IAW MM 26-11-01-4. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040930000132004093000013NM 2004 9 30 GAIA04090OP 120040824A5210 ARM BOEING727 727223 1384074NM L1 DOOR OUT OF ADJUST A GAIAK NONE O OTHER ININSP/MAINT 1 SW076809 19484 L1 DOOR HARD TO CLOSE. ADJUSTED PROGRAMMING ARM. CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040930000152004093000015EA 2004 9 30 ASOA04607 120040817A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9. (M) 2L72 4F RTA21EA 20040930000162004093000016EU 2004 9 30 A6WA200460033 120040831A2910200877943 LINE BAC 146 146300A 1500267EU HYD SYSTEM RUPTURED A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31612AW E3122 FOUND RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF, REV UNSAFE LIGHT ILLUMINATED, CYCLED MLG DOWN, RETUREND TO RDU FOR FERRY FLIGHT BACK TO ATW. INSPECTED AND FOUND RT MLG FLEX LINE FOR RETRACTOR BRAKES RUPTURED WITH HYDRAULIC FUSE BLOWN, REPLACED LINE. RESET HYDRAULIC FUSE, SERVICED HYDRAULICS, SWUNG MLG AND NLG ASSEMBLY. OPS CHECK GOOD. (M) 2H74 4F RTA49EU 20040930000182004093000018EA 2004 9 30 A6WA200440124 120040831A4930 FUEL LINE CNDAIRCL600 CL6002B19 1900309EA APU CHAFED A A6WAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31467AW 7900 STRONG FUEL SMELL IN CABIN AND COCKPIT WITH APU AIR SUPPLYING PACKS. OK ENGINE AIR. FOUND FUEL LEAK INSIDE APU ENCLOSURE, NO LEAKS WITH APU DEACTIVATED. FOUND APU FUEL LINE CHAFED BY CLAMP. REMOVED AND REPLACED APU FUEL LINE. OPS CHECK GOOD, REF AMM 49-31-00. (M) 2L72 4F RTA21EA 20040930000192004093000019NE 2004 9 30 Y2PA04021 220040828A726156675N1 GARLOCK SEAL AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE NR 2 ENGINE LEAKING A Y2PAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23822AA 195 299G043 NR 2 ENGNE OIL PRESSURE BECAME ERRATIC ALL OTHER GAUGED INDICATED NORMAL. OIL PRESSURE GAUGE THEN DROPPED FOLLOWED BY 'OIL P' LIGHT. SHUTDOWN NR 2 ENGINE IMMEDIATELY, REFERRED TO EMERGENCY CHECKLIST PG E2. DECLARED EMERGENCY AND DIVERTED TO RDU. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE SENT TO RDU AND REMOVED AND REPLACED NR 2 ENGINE GARLOCK SEAL AND O-RING WITH NEW SEAL AND O-RING IAW SEI MM CHP 72. OPS AND LEAK CHECK GOOD IAW SEI 189. DURING ENGINE, RUN UP NO OTHER DEFECTS OTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 F A7EU E7EA 20040930000232004093000023EA 2004 9 30 ASOA04611 120040817A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040930000252004093000025EU 2004 9 30 SIMA200425312 120040904A5330AL2027T3 SKIN SAAB SF340 340B 7860101EU FS DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21347SB 340B347 DURING AN HMBV INSPECTION, A DENT WAS FOUND ON THE RIGHT FUSELAGE AT STATION 390 AND BETWEEN SL 1615 AND 1616. PERFORMED CUTOUT OF THE DAMAGED AREA AND PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER AND TRIPLER. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 44, CHAPTERS 53-70-10. (M) 2L72 4T RTA52EU 20040930000272004093000027SO 2004 9 30 SIMA200425602 120040911A27403621005009MO CONTROL UNIT EMB 145 EMB145LR 3260212SO AVIONICS BAY INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21633AE4783 2456 145148 FWA - FLT 3794 - AFTER TAKEOFF, CREW RECEIVED PITCH TRIM MAIN AND PITCH TRIM BACKUP INOPERATIVE MESSAGE. PERFORMED AOM PROCEDURES AND PITCH TRIM WAS NOT REESTABLISHED. CREW ELECTED TO RETURN TO FWA. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040930000282004093000028GL 2004 9 30 SIMA200426501 220040918A7200 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 2 FIRE A SIMAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SW21807AE 145506 ORD - FLT 4161 - NR 2 ENGINE FIRE REPORTED FROM RAMP. FLAMES SHOT OUT OF THE EXHAUST. NO INDICATION WAS PRESENT IN COCKPIT. CREW DISCHARGED BOTH FIRE BOTTLES. PERFORMED GENERAL VISUAL INSPECTION OF THE NR 2 ENGINE WITH NO DISCREPANCIES NOTED. PERFORMED GROUND RUN WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20040930000292004093000029NM 2004 9 30 BJNA040810 120040812A5330 SKIN BOEING737 7372K9 1384494NM FS DENTED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11222TM 23404 DURING C-CHECK INSPECTION AT TIMCO, LAKE CITY, FL, FOUND SKIN DENTED AT BS 1009 AND BS 1013 BETWEEN STRINGER 12L AND 15L BETWEEN ADJACENT BOYS. REMOVED FUSELAGE SKIN FROM BS 1009-1013, FABRICATED AND INSTALLED NEW SKIN SECTOIN IAW TIMCO REPAIR ENGINEERING ORDER REO-LOO795 REV IR MATERIAL 2024-T3 .071 26 BY 30. (M) 2L72 4F A16WE 20040930000302004093000030EU 2004 9 30 ASOA04622 120040802A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DUIRNG A C-CHECK IN YUL, THE LEFT AND RIGHT INTERCOSTALS AT FS 38/39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INTERCOSTALS AT FS 38/39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040930000312004093000031EA 2004 9 30 ASOA04618 120040822A5210601R3807423 BRACKET CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DURING A C-CHECK IN MCN, THE FORWARD AND AFT CABLE ANCHOR MOUNTING BRACKETS ON THE PASSENGER DOOR WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD AND AFT CABLE ANCHOR MOUNTING BRACKETS ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040930000332004093000033EA 2004 9 30 ASOA04609 120040817A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040930000352004093000035EA 2004 9 30 ASOA04616 120040822A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A ASOAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO11847AS 7335 FLT 4414 - DURING CRUISE FROM MEM-DFW, AT APPROXIMATELY 28,000 FEET WITH THE AUTOPILOT ENGAGED, STABILIZER TRIM CHANNELS 1 AND 2 DISENGAGED. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED RE-ENGAGEMENT OF CHANNELS 1 AND 2, WHICH RE-ENGAGED AND DISENGAGED AGAIN. AN EMERGENCY WAS DECLARED. FLAPS WERE SELECTED TO TWENTY DEGREES WITH THE AIRCRAFT LANDING SAFELY IN DFW. THE MAINTENANCE DIAGNOSTIC COMPUTER WAS INTERROGATED AND NO FAULTS WERE FOUND. MAINTENANCE ALSO ENGAGED THE STABILIZER TRIM SEVERAL TIMES AND PERFORMED A HORIZONTAL STABILIZER TRIM CONTROL UNIT SELF-TEST. AGAIN NO FAULTS WERE FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930000362004093000036EA 2004 9 30 ASOA04610 120040817A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040930000432004093000043EU 2004 9 30 ASOA04625 120040802A5310 CREASE BEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE LEFT CREASE BEAM AT FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT CREASE BEAM AT FS 39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040930000452004093000045EA 2004 9 30 ASOA04621 120040822A5320601R950159 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DURING A C-CHECK IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY. (M) 2L72 4F RTA21EA 20040930000462004093000046EU 2004 9 30 ASOA04627 120040802A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD SEAT TRACK AT FS 36 TO 39, AND THE LEFT SEAT TRACK AT FS 36/38 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SEAT TRACK AT FRAME 36 TO FRAME 39, AND THE LEFT SEAT TRACK AT FS 36/38 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20040930000482004093000048NM 2004 9 30 USAASB04114 120040830A335020121 POWER SUPPLY BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19563AU 23551 BOS - PILOT REPORTED THE COCKPIT EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY LIGHT IN COCKPIT AND REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040930000492004093000049EU 2004 9 30 USAABA04021 120040830A335032146210 POWER SUPPLY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19670UW 0315 PIT - DOOR 3R EPSU FAULTED. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA46NM 20040930000512004093000051EU 2004 9 30 ASOA04635 120040803A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 3 CAM GUIDE AT RIB 16 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 3 CAM GUIDE AT RIB 16 IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000542004093000054NM 2004 9 30 USAASB04113 120040823A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US 23991 BDL - FOUND COCKPIT AND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD BATTERY CHARGER AND BATTERY. (M) 2L72 4F RTA16WE 20040930000582004093000058SO 2004 9 30 SIMA200425308 120040901A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 ABI - DURNG AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4061B DATED AUGUST 31, 2004. (M) 2L72 4F RTT00011AT 20040930000592004093000059SO 2004 9 30 SIMA200425601 120040911A49204504113 APU EMB 135 EMB135KL 3260302SO APU BAY SMOKE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21815AE1206 163 145545 DURING GROUND OPERATIONS WITH APU POWER AND BLEEDS ON CREW NOTED SMOKE IN CABIN. CREW PERFORMED APU SHUTDOWN AND UNLOADED PASSENGERS SAFELY. NO FURTHER INCIDENTS WRE REPORTED. SMOKE AND ISOLATED TO THE AUP AND AN MEL WAS ISSUED. REPLACED APU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040930000602004093000060SO 2004 9 30 SIMA200425309 120040904A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 ABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL BETWEEN FRAMES 14 AND 16 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 16.25 INCH SECTION OF THE FORWARD DIGITAL. FABRICATED A 16.25 INCH REPAIR PLATE. FABRICATED A RIGHT DOUBLER AND LEFT DOUBLER SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10. (M) 2L72 4F RTT00011AT 20040930000622004093000062EU 2004 9 30 SIMA200425306 120040829A5414 SKIN SAAB SF340 340B 7860101EU RT NACELLE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21347SB 340B347 ABI - DURING AN HMBV INSPECTION, THE RIGHT NACELLE INBOARD SKIN ABOVE THE INTAKE SEAL WAS FOUND TO BE GOUGED. REMOVED DAMAGED SKIN BY MAKING A .75 INCH DIAMETER CUTOUT. FABRICATED A DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS3079 REV 44, 54-10-10. (M) 2L72 4T RTA52EU 20040930000642004093000064SO 2004 9 30 SIMA200425307 120040831A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER, SHIM AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 27, 53-21-10. (M) 2L72 4F RTT00011AT 20040930000652004093000065SO 2004 9 30 SIMA200425310 120040901A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FS 25 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 27, 53-22-10. (M) 2L72 4F RTT00011AT 20040930000662004093000066EU 2004 9 30 2004F00399 120040718A5610NP1588011 WINDSHIELD AEROSPATR42 ATR42300 8680920EU COCKPIT CRACKED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21271AT6517 273 DURING THE CLIMB PORTION OF FLIGHT FROM SANTO DOMING TO SAN JUAN, SPARKS WERE COMING OUT OF THE CAPTAINS WINDSHIELD AND THEN CRACKED. FLIGHT DIVERTED TO LA ROMANA. REPLACED CAPTAIN WINDSHIELD. (M) TRBA 2H72 4T RTA53EU 20040930000692004093000069EU 2004 9 30 ASOA04561 120040803A5210 DOOR AEROSPATR72 ATR72212 8680945EU PAX MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 FLT 4374 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE CYCLED THE DOOR BUT COULD NOT DUPLICATE THE DISCREPANCY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040930000702004093000070EU 2004 9 30 ASOA04634 120040803A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 2 CAM GUIDE AT RIB 15 WAS FOUND TO BE CORRODED LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 2 CAM GUIDE AT RIB 15 IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000722004093000072EA 2004 9 30 ASOA04646 120040825A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040930000732004093000073EU 2004 9 30 ASOA04637 120040804A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE LEFT OUTBOARD FLAP NR 6 CAM GUIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP NR 6 CAM GUIDE IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000742004093000074EU 2004 9 30 ASOA04636 120040803A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP NR 4 CAM GUIDE AT RIB 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP NR 4 CAM GUIDE AT RIB 17 IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000772004093000077EA 2004 9 30 ASOA04650 120040827A5210601R3196041 HINGE CNDAIRCL600 CL6002B19 1900309EA DOOR STEP BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 FLT 4573 - DURING A GROUND INSPECTION IN DFW, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930000792004093000079EU 2004 9 30 ASOA04652 120040827A33503012000 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11534AS 463 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR. (M) 2H72 4T RTA53EU 20040930000812004093000081EU 2004 9 30 ASOA04631 120040803A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FS 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 39 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040930000822004093000082EU 2004 9 30 ASOA04638 120040805A5320 SUPPORT BEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURNG A C-CHECK IN YUL, THE LEFT Z-SUPPORT BEAM BETWEEN FS 39 AND FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT Z-SUPPORT BEAM BETWEEN FS 39 AND FS 40 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040930000832004093000083NM 2004 9 30 USAASB04095 120040721A33501012623 LIGHT BOEING737 737301 1384611NM SEAT ROW 10 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19584US 23743 PIT - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 10, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 10, LEFT SIDE. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040930000862004093000086NM 2004 9 30 C7WA200400022 120040609A5313 STRINGER BOEING727 727232 1384082NM CARGO BAY CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND AFT CARGO COMPARTMENT STRINGER 27 RIGHT STATION 950E HAS LIGHT CORROSION. INSTALLED STRINGER REPAIR IAW 727 SRM 51-40-4 FIGURE 3. (M) 2L73 4F A3WE 20040930000902004093000090NM 2004 9 30 C7WA200400018 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND STRINGER 28 RIGHT STATION 1050 EVIDENCE OF CORROSION. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 53-30-3 FIGURE 3. (M) 2L73 4F A3WE 20040930000912004093000091NM 2004 9 30 C7WA200400017 120040609A5230MS200116 HINGE BOEING727 727232 1384082NM MAIN CARGO DOOR CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND MAIN CARGO DOOR UPPER AFT HINGE SECITON CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AE MM CHAPTER 52 PAGE 15. (M) 2L73 4F A3WE 20040930000922004093000092NM 2004 9 30 USAA040336 120040617A5420 BRACKET BOEING757 757225 1384959NM PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU60209 22192 CLT - FOUND BRACKET CRACKED .1875 INCH, CENTER LINE OF PYLON ON FORWARD SIDE OF STATION 174.30, JUST AFT OF PRECOOLER. REMOVED CRACKED BRACKET, FABRIATED REPLACEMENT, HEAT TREATED PER SRM 51-10-2. (M) 2L72 4F RTA2NM 20040930000932004093000093NM 2004 9 30 C7WA200400020 120040609A5730 SKIN BOEING727 727232 1384082NM CENTER WING CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND WING CENTER SECTION UPPER SKIN CORRODED LBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M) 2L73 4F A3WE 20040930000982004093000098EU 2004 9 30 USAASA04082 120040314A5240 DAMPER AIRBUSA321 A321211 3930370EU L2 DOOR LEAKING A USAAK NONE K FLUID LOSS ININSP/MAINT 1 EA19172US 1472 LAX - THE L2 DOOR DAMPER WAS FOUND TO BE LEAKING. MAINTENANCE FOUND A PUNCTURED DIAPHRAM AND A LOOSE SCHARADER VALVE. REPLACED THE DIAPHRAM, AND TIGHTENED AND SAFETIED THE SCHRADER VALVE. OPS CHECKED OK. (M) 2L72 4F RTA28NM 20040930000992004093000099EA 2004 9 30 ASOA04644 120040825A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 INBOARD AND AT RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 INBOARD AND AT RBL 9 INBOARD AND OUTBOARD IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040930001002004093000100EA 2004 9 30 ASOA04642 120040824A25101C30941AJF STEP CNDAIRCL600 CL6002C10 1390015EA COCKPIT SEAT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11716EV 10084 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY STEP ON THE CO-PILOT'S SEAT BACK WAS FOUND MISSING. MAINTENANCE REPLACED THE EMERGENCY STEP ON THE CO-PILOTS SEAT BACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930001072004093000107EA 2004 9 30 ASOA04648 120040826A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE INBOARD CLIP AT FS 484, LBL 27 AND OUTBOARD CLIP T FS 484, LBL 36 WERE FOUND TO BE CRAKCED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD CLIP AT FS 484, LBL 27 AND REPAIRING THE OUTBOARD CLIP AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040930001082004093000108 2004 9 30 USAASA04083 420040511A2565 SLIDE AIRBUSA319 A319112 3930323EU CABIN DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW 0904 BFM - THE ESCAPE SLIDE WAS REMOVED FOR TIME. MAINTENANCE FOUND THE JUNCTION SEAM BRIDGING IS COMING APART AT RUNWAY END UPPER TUBE. SLIDE WAS RETURNED TO VENDOR FOR REPAIR. THE SLIDE WAS REPAIRED AT THE VENDOR AND RETURNED TO THE SLIDE SHOP. THE SLIDE OVERHAUL WAS COMPLETED AND THE SLIDE WAS RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 20040930001092004093000109EU 2004 9 30 USAASA04077 120040802A5210 DIAPHRAGM AIRBUSA319 A319112 3930323EU R 1 DOOR ASSIST RUPTURED A USAAK NONE O OTHER ININSP/MAINT 1 EA19763US 1360 UPON ATTEMPT TO ENTER THE AIRCRAFT, THE MAINTENANCE CREW FOUND THAT THE R1 DOOR WOULD NOT OPEN FROM THE OUTSIDE. PRESSURE WAS FELT AGAINST THE DOOR AS THE ATTEMPT TO OPEN WAS MADE. MAINTENANCE FOUND THE DOOR ASSIST BOTTLE DIAPHRAM DISK PUNCTURED. SUSPECT PRESSURE FROM THE DOOR ASSIST BOTTLE WAS PUSHING DOOR AGAINST THE STOPS, PREVENTING DOOR FROM OPENING. ALSO, SUSPECT THAT DOOR MAY HAVE PREVIOUSLY BEEN ATTEMPTED TO OPEN WITH THE ESCAPE SLIDE ARMED, BUT HELD SHUT AS DOOR ASSIST BOTTLE RELEASED PRESSURE, FORCING DOOR TO THE CLOSED POSITION. REPLACED THE DIAPHRAM DISK AND SERVICED THE DOOR ASSIST BOTTLE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040930001152004093000115NM 2004 9 30 USAABB04081 120040830A3397 WIRE BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19653US 24894 CLT - FOUND CEILING MOUNTED EMERGENCY LIGHT AT ROW 11 BC INOPERATIVE. MAINTENANCE RESECURED LOOSE TERMINALS ON THE LIGHT. (M) 2L72 4F RTA1NM 20040930001172004093000117EU 2004 9 30 USAABA04018 120040819A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19677UW 0380 PHL - EPSU 17WL AND 18WL FAULTED DURING TEST. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20040930001192004093000119WP 2004 9 30 ASAA0480478 120040727A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 LAX - DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY OVERHEAD FLOOR LIGHTS INOPERATIVE UPON TEST. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040930001202004093000120NM 2004 9 30 ASAA0410258 120040507A2597 WIRE BOEING737 737298C 1384490NM INTERIOR PALLET INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 DURING MAINTENANCE CHECK, FOUND TWO AFT PEEPLES LIGHT ON PALLET 5-2 BLINK ON TEST. REPLACED WIRING ON PALLET. (M) 2L72 4F RTA16WE 20040930001212004093000121EA 2004 9 30 ASOA04647 120040825A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE CARGO DOOR SILL FLOOR LANDING PLATE AT FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE IS REPAIRING THE CARGO DOOR SILL FLOOR LANDING PLAT AT FS 605 IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20040930001222004093000122NM 2004 9 30 AMTA200400982 120040804A5310 SHEAR WEB BOEING757 75723N 1384973NM FUSELAGE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND CABIN BS 1661 TO 1681, RBL 10, SHEAR WEB UPPER CHORD CRACKED, BROKEN. REMOVED AND REPLACED UPPER SHEAR WEB UPPER CHORD FROM BS 1661 TO BS 1681, RBL 10 IAW B757 SRM 53-60-51-2, FIG 202. (M) 2L72 4F RTA2NM 20040930001232004093000123NM 2004 9 30 AMTA200400983 120040804A5320 ANGLE BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 NR 1 RIGHT PASSENGER DOOR LOWER SILL Z-ANGLE BS 333 TO BS 365 CORROSION. REMOVED AND REPLACED Z-ANGLE AND Z-ANGLE SHIM IAW B757 SRM 51-40-2. (M) 2L72 4F RTA2NM 20040930001312004093000131NM 2004 9 30 2004F00382 120040105A323069353703 SENSOR BOEING737 737231 1384079NM NLG MALFUNCTIONED A FX7AA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO1954348 21967 UNABLE TO RAISE THE GEAR AFTER TAKEOFF. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG SAFETY SENSOR PER MM 32-09 AND THE LANDING GEAR ACCESSORY UNIT FOR PRECAUTIONARY. PERFORMED OPS CHECK OF LANDING GEAR PER PER MM 32-32. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (M) 2L72 4F RTA16WE 20040930001342004093000134NE 2004 9 30 2004F00385 120040722A6320643520035102 CAM SKRSKYS64 S64E 8142604NE GEARBOX FAILED B E8KLK NONE O OTHER ININSP/MAINT 1 NM09172AC 64061 MAIN GEARBOX S/N A6-168 WAS REMOVED FOR OVERHAUL FROM THE AIRCRAFT. THE 2ND STAGE ASSY WAS DISASSEMBLED AND CAM ASSY WAS REMOVED AND CLEANED FOR NDT INSPECTION. UPON INSPECTION FROM NDT, 2 CRACKS WERE FOUND TO BE LOCATED ON GEAR TOOTH AREA. EACH CRACK APPROXIMATELY 2 INCHES APART AND TRAVELING .125 INCH UP IN LENGTH, FROM THE BOTTOM OF GEAR TOOTH AREA ON CAM ASSY. E8KL (M) TONY CHECK THIS 2G72 4U H4EA 20040930001362004093000136NM 2004 9 30 SWAA042803 120040926A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED GROUND WIRE TO AIRFRAME AND RELAMPED PER MM. 2L72 4F RTA16WE 20040930001382004093000138NM 2004 9 30 SWAA042806 120040927A53116558280 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 27L AND STRINGER 27R, CORRODED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040930001412004093000141NM 2004 9 30 SWAA042795 120040927A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040930001422004093000142NM 2004 9 30 SWAA042796 120040927A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040930001432004093000143NM 2004 9 30 SWAA042797 120040927A551265C25727 SKIN BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED C4 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN AT STATION 146, REAR SPAR, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040930001452004093000145NM 2004 9 30 SWAA042799 120040927A53306545866 SKIN BOEING737 737301 1384611NM KEELBEAM CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C3 CHECK, FOUND KEELBEAM SKIN AT BS 660, LBL 6.3, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040930001472004093000147NM 2004 9 30 SWAA042801 120040927A3350OL307IBPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29706SW 27840 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROWS 9 ADC AND 11 ABC, INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20040930001492004093000149EA 2004 9 30 HNAA0400080 120040826A6100 ENGINE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 2 OUT OF RIG A HNAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 EA07337EN 284 AFTER TAKEOFF NR 2 ENGINE SURGED, POSSIBLE BETA LOCKOUT FAILURE. OPERATED PROP AT 900 RPM AND SURGE DISSIPATED. DEACTIVATED BETA LOCKOUT SYSTEM. RIGGED NR 2 ENGINE PER W/C 76-00-02Q REACTIVATED BETA LOCK OUT C/W W/C 61-20-10Q BETA LOGIC OPS CHECK BETA LOCKOUT AND PROP GOVERNOR OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20040930001522004093000152WP 2004 9 30 ABXA040330 120040810A57305708334362 SKIN DOUG DC8 DC863F 302198FWP RT WING GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23814AX 46041 RIGHT WHEEL INBOARD AILERON, 3 RIVETS MISSING HEADS OR PART OF HEAD AND OPEN HOLE AT APPROXIMATELY XA 562, LOWER LEADING EDGE. REMOVED AND REPLACED DAMAGED SKIN SECTION AND DOUBLER IAW REA D857-49983MR. 2L74 4F 4A25 20040930001532004093000153WP 2004 9 30 ABXA040328 120040917A21105614845517 COMPRESSOR DOUG DC8 DC861 3021952WP CABIN AIR DAMAGED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL23847AX7779 46031 AFTER TURNING ON THE NR 4 CTC, THE AIRCRAFT FILLED WITH A BURNING OIL SMELL. TURNED NR 4 CTC OFF AND SMELL DISSIPATED. NOTE: DID NOT GET AN OVERHEAT LIGHT, RPM'S NORMAL. FOUND NR 4 CTC FAN BLADE DAMAGED. REMOVED AND REPLACED NR 4 CTC. OPS CHECKED GOOD IAW DC-8 MM CHAPTER 21. ADDITIONAL INFO: THE CREW HAD THE PROBLEM WITH THE NR 4 CTC ON TAKEOFF OUT OF ILN EN ROUTE TO SAT, FLIGHT 392. DID NOT DO AN AIR TURNBACK, NOR ABORT TAKEOFF. MAINTENANCE ALSO FOUND THE NR 3 CTCS DAMAGED. BOTH THE NR 3 AND NR 4 CTCS WERE CHANGED OUT. A BIRD STRIKE INSPECTION WAS ALSO PERFORMED WITH NO ADDITIONAL FINDINGS. 2L74 4F 4A25 20040930001552004093000155NM 2004 9 30 HNAA0400121 120040910A792128E997 OIL COOLER DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE LEAKING A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07810EX31835 308 FLIGHT 3796 HAD TO ABORT TAKEOFF DUE TO RECEIVING THE NR 2 ENGINE OIL PRESSURE LIGHT. MAINTENANCE FOUND THE NR 2 OIL COOLER TO BE LEAKING. UNIT WAS REMOVED AND REPLACED. AIRCRAFT RUN COMPLIED WITH, LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040930001562004093000156WP 2004 9 30 ABXA040322 120040901A5210591412143 ANGLE DOUG DC9 DC931 3022065WP DOOR PAN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 MAIN ENTRY DOOR BOTTOM ANGLE OF DOOR CRACKED AT BOTH FORWARD AND AFT SIDES. REMOVED AND REPLACED LOWER ANGLES OF MAIN ENTRY DOOR IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 20040930001572004093000157WP 2004 9 30 ABXA040323 120040902A5320991050311 CUSP WEB DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 RIGHT CUSP WEB CRACKED SEVERAL PLACES FORWARD OF FS 965. REPAIRED RIGHT CUSP WEB FORWARD OF STA 965 IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040930001592004093000159WP 2004 9 30 ABXA040325 120040903A5511591800011 SPAR CAP DOUG DC9 DC931 3022065WP LT HORZ STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 LEFT HORIZONTAL STABILIZER LOWER AFT SPAR CAP CRACKED OUTBOARD TIP. REPAIRED AREA IAW REA D955-50434MR. 2L72 4F A6WE 20040930001612004093000161 2004 9 30 ABXA040320 420040831A2210 COMPUTER DOUG DC9 DC941 302207NWP EMPENNAGE MALFUNCTIONED A ABXAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL23955AX 47619 AIRCRAFT INITITATED DUTCH ROLL DURING CLIMBOUT AND PROGRESSIVELY GOT WORSE WITH THE HIGHER CLIMB. ROLL TOOK PLACE WITH OR WITHOUT AUTO PILOT ON AND OFF, WITH YAW DAMPER SWITCH ON OR OFF. ACCOMPLISHED RUDDER CONTROL TAB INSP/TEST IAW DC9 MM 27-20-02-04. NO DEFECTS NOTED. LUBRICATED RUDDER PACKAGE. 2L72 4F A6WE 20040930001622004093000162NM 2004 9 30 HNAA0400085 120040920A3220 LOCK DHAV DHC8 DHC8201 2809001NM NLG WHEEL ENGAGED A HNAAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 EA07997HA 507 NOSE WHEELS WOULD NOT RETRACT AFTER UP SELECTION. ON GROUND FOUND NOSE WHEEL LOCK ENGAGED. RESET NOSE GAUGE WHEEL LOCK AND INSPECTED GEAR. NO DEFECTS NOTED. 2H72 4T RTA13NM 20040930001632004093000163NM 2004 9 30 HNAA0400122 120040922A2422DH103024600C2B INVERTER DHAV DHC8 DHC8102 2809003NM CABIN FAULTY A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07846EX13164 326 FLIGHT 3893 REPORTED AUXILLARY INVERTER CAUTION LIGHT ILLUMINATED ALONG WITH A STRONG FISH ODOR AND CIRCUIT BREAKER D-8 POPPING. MAINTENANCE REPLACED THE AUXILLARY INVERTER AND ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040930001652004093000165WP 2004 9 30 ABXA040314 120040817A5313577991211 LONGERON DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23817AX 45928 FORWARD CARGO STA 600, LONGERON 31 LEFT, CORRODED. REPAIRED AREA IAW REA D853-50003-MR. 2L74 4F 4A25 20040930001692004093000169NM 2004 9 30 P5CA0401201 120040914A5320 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CARGO BAY CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 CENTER CARGO COMPT FRAME UPPER CHORD HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040930001712004093000171NM 2004 9 30 P5CA0401191 120040909A760363030006 ACTUATOR BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE FUEL CONDITION MALFUNCTIONED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23921FT 21575 689169 AFTER PUSHBACK, ON ENGINE START NR 1 ENGINE FUEL CONDITION ACTUATOR CIRCUIT BREAKER OPENED. REMOVED AND REPLACED NR 1 FUEL CONDITION ACTUATOR, ALL OPS NORMAL. 2L74 4F4 F A20WE E3NE 20040930001722004093000172NM 2004 9 30 P5CA0401192 120040909A7830 WARNING LIGHT BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE THRUST REVERSER ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23921FT 21575 689184 NR 2 ENG THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON FORWARD ANNUNCIATOR PANEL ON POWER UP FOR TAKEOFF. REPEATED THRUST REVERSER LIGHT ON FLIGHT ENGINEER PANEL. LOCKED OUT REVERSER PER AMM 78-00-00, OPENED MEL 78-12A. 2L74 4F4 F A20WE E3NE 20040930001752004093000175NE 2004 9 30 HNAA0400120 320040902A611087110047001 MOUNT DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF* NE ZONE 400 BROKEN A HNAAO OTHER E VIBRATION/BUFFET CLCLIMB 1 EA07828EX 392 930405 FLIGHT 4079 REPORTED A PROP VIBRATION DURING CLIMB, CRUISE, DESCENT WITH PROPS AT 900 RPM. MAINTENANCE FOUND THE RIGHT HAND INBOARD REAR MOUNT STRUT TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20040621000122004062100012WP 2004 6 21 ASAA0480394 120040513A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS 53079 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 32. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040621000282004062100028WP 2004 6 21 ASAA0480249 120040404A531159128524 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND CRACK IN LOWER FRAME AT FASTENER JUST FORWARD OF STATION 47 ON RIGHT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MD80 SRM 53-01. (M) 2L72 4F RTA6WE 20040621000342004062100034WP 2004 6 21 ASAA0480234 120040404A53209930538U12 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND HV CHECK, RIGHT CUSP WEB AT STATIN 505-518, STRINGER 18R, FORWARD PIT IS CORRODED. REMOVED AND REPLACED CUSP WEB PER SRM 51-30-1. (M) 2L72 4F RTA6WE 20040621000352004062100035WP 2004 6 21 ASAA0480328 120040419A5311990224619 WEB DOUG DC9 DC983 3022083WP ACCESSORY BAY GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 FOUND C-CHECK, LEFT VENTRAL AFT ACCESSORY COMPARTMENT FRAME, WEB, GOUGED AT FS 1380. REPLACED WEB PER SRM 51-70-4. (M) 2L72 4F RTA6WE 20040621000392004062100039WP 2004 6 21 ASAA0480332 120040419A532199365441 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 OKC - FOUND DURING C-CHECK, PASSENGER CABIN FLOOR PANEL HAS DISBONDED AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040621000582004062100058EA 2004 6 21 VNAA0406004 120040602A5220 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT FAILED A VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL05247JS 7922 THE CREW REPORTED THAT AT THE RT EMERGENCY EXIT, THERE WAS SOME OF THE SEAL MISSING AROUND THE WINDOW. MAINTENANCE INSPECTED AND PLACED THE SEAL ON THE CDL LIST, CDL 51-23. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040621000642004062100064 2004 6 21 SWAA041708 420040617A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040621000662004062100066 2004 6 21 SWAA041710 420040617A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040621000742004062100074EA 2004 6 21 COMA0460319 120040517A5311601R3600123 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01984CA 7171 CRACK ON LEFT HAND FS 718 BETWEEN STRINGER 11 AND 12. REPAIRED FRAME BETWEEN STRINGER 11 AND 12 ON CT FS 718.00 IAW REO 601R-53-61-193. 2L72 4F RTA21EA 20040621001002004062100100EU 2004 6 21 RAIA00405015 120040524A3260AIR035670 SQUAT SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG DEFECTIVE A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03553HK 41066 STL - STALL WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NLG WEIGHT ON WHEEL SWITCH. 2L72 4T RTA41NM 20040621001022004062100102EU 2004 6 21 YENA200428 120040510A5210 SHRADER VALVE AIRBUS320 A320232 3930326EU ASSIST BOTTLE LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15558JB 1915 L1 DOOR ASSIST BOTTLE READS 0 PSI, SHRADER VALVE LEAKS. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE SHRADER VALVE, SERVICED PER MM 52-11-00, LEAK CHECK OK. 2L72 4F RTA28NM 20040621001062004062100106 2004 6 21 WRLA200421 420040507A34204006584901 INDICATOR DOUG DC10 DC1030 3023501WP ATTITUDE FAILED A WRLAJA DUMP FUEL UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO1114075 46922 THE AIRCRAFT NR 1 VERTICAL GYRO WAS INOPERATIVE, ON CLIMBOUT OF BAHRAIN N2 (FIRST OFFICER) FAILED, THE CREW UNABLE TO RESET OR RESTORE IT AND DECIDED TO RETURN BACK TO BAHRAIN. AT BAHRAIN MAINTENANCE REPLACED THE F/O ATTITUDE DIRECTOR INDICATOR PER MM 34-23-02 OP'S CHECK GOOD, AIRCRAFT RETURN TO SERVICE. 2L73 4F A22WE 20040621001102004062100110NM 2004 6 21 CALA0400532 120040612A5320BAC1446777 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713248 28808 INSPECTION FOUND Z-CHANNEL CORRODED AT STA 747-767, RT SIDE OF AFT CARGO PIT. A NEW Z-CHANNEL WAS INSTALLED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040621001162004062100116EA 2004 6 21 COMA0460327 120040521A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR ILLUMINATED A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01917CA 7017 FLIGHT 5326 GEAR DISAGREE WARNING DURING EXTENSION. COULD NOT DUPLICATE. RETRACTION CHECKS WERE NORMAL. 2L72 4F RTA21EA 20040621001612004062100161WP 2004 6 21 ASMF200406010 120040612A7930 WARNING LIGHT DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RT ENGINE ILLUMINATED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23491SH 49150 718106 AIRCRAFT REJECTED TAKE OFF AT 110 KNOTS AND RETURNED TO PLATFORM, (RT STRAINER CLOGGING) LIGHT TURNED ON. RT FILTER WAS REMOVED, CHECKED, CLEANED AND ENGINE OIL WAS REPLACED IAW MM 79-20-06, WHEELS WERE CHECKED BY REJECTED TAKE OFF, ALL CORRECT. DURING TRANSIT CHECK, MAIN OIL FILTER WAS REPLACED, TEST CORRECT. 2L72 4F4 F A6WE E9NE 20040621001702004062100170NM 2004 6 21 ANCF200400012 120040609A36107732888 SHUTOFF VALVE BOEING767 767383 1385214NM LT ENGINE FAILED W ANCFO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO23984AN 504 24357 DURING WING AND ENGINE ANTI-ICING USE CABIN CONTROL WITH AUTO 1 SELECTED, WITH 7.0 UNITS OF DIFFERENT TO LAND, 9500 OF ALTITUDE WITH STRONG PRESSURIZATION SURGE. THIS CONDITION WAS PRESENTED AT 35.000 FT WITH CABIN 2 SELECTED INDICATIONS WERE NORMAL. WAS REMOVED AND REPLACED PRSOV IN THE RT ENGINE IAW AMM 36-11-09 PAGE 401, THE SENSE LINE OF VALVE WAS ADJUSTED AND THE LEAK WAS ELIMINATE. IN THE LT ENGINE THE PRSOV WAS REMOVED AND REPLACED IAW AMM 36-11-09 PAGE 401. ENGINE RUN UP TEST WAS PERFORMED WITH SATISFACTORY RESULTS, BLEED AND ANTI-ICE SYSTEM NORMAL IAW AMM 71-00-00 PAGE 201-273 RT PRSOV P/N ON AND OFF:773288-8 S/N OFF: 890815 LT PRSOV P/N ON AND OFF: 773288-8 S/N OFF:900415 2L72 4F RTA1NM 20040621002012004062100201NM 2004 6 21 AWXA200400512 120040430A5320500794648 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .5 INCH CRACK IN INTERCOSTAL AT BS 295, LBL 54, WL 244. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 295, LBL 54, WL 244; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 50-07946; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2L72 4F RTA16WE 20040621002032004062100203NM 2004 6 21 AWXA200400514 120040430A531065458053 SHEAR TIE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND IN SHEAR TIE AT BS 277, LBL 58, WL 253. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 277, LBL 58, WL 253; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-45805; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-07 FIG 205. 2L72 4F RTA16WE 20040621002052004062100205NM 2004 6 21 AWXA200400516 120040430A532050826162 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.0625 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 294, STR 4 LT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 4 LT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 50-8261; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7 & 8. 2L72 4F RTA16WE 20040622000012004062200001NM 2004 6 22 AWXA200400540 120040426A53206545402581 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.1 INCH CRACK WAS FOUND IN ANGLE AT AFT END OF RT AIR CONDITIONING BAY ABOVE TURBO FAN BS 639, RBL 20, WL 178. MAINTENANCE REMOVED CRACKED ANGLE AT AFT END OF RT AIR CONDITIONING BAY BS 639, RBL 20, WL 178; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45402; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7 & 8. 2L72 4F RTA16WE 20040622000092004062200009WP 2004 6 22 ASAA04800294 120040420A53305911401211 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE FROM STATION 193 TO 204 BETWEEN LONGERON 27R AND 28R IS DENTED WITHIN TWO FRAME BAYS D= 6.00 BY =.060. COLD WORKED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND SHIMS IAW ASA EA 5330-01775 AND AAR EA 10890. (M) 2L72 4F RTA6WE 20040622000242004062200024WP 2004 6 22 ASAA0480286 120040420A53403934011503 FITTING DOUG DC9 DC983 3022083WP DOOR FRAME CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND DURING HV CHECK, AFT CARGO DOOR FRAME TEE- FITTING ON UPPER INNER STRUCTURE IS CRACKED. REPLACED TEE PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040622000252004062200025WP 2004 6 22 ASAA0480287 120040420A5720993751735 ANGLE DOUG DC9 DC983 3022083WP LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND DURING HV CHECK, FOUND LEFT WING LEADING EDGE ATTACH ANGLE IS CRACKED AT STATION XRS 164. REPLACED ANGLE PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20040622000312004062200031WP 2004 6 22 ASAA0480277 120040412A531199581881 FRAME DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FRAME FASTENER HOLE ELONGATED ON UPPER SURFACE AT FS 1322. REPAIRED HOLE WITH FILLER, SHIM, AND ANGLE PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000652004062200065WP 2004 6 22 IXXA0400036S 120040223A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION FOUND TEMPORARY REPAIR OF FUSELAGE EXTERIOR SKIN STATION 1459.000-1512.000 L-31L TO L-34L. REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA IAW DC8 SRM 53-2-1 PG 107-108 FIG 7. FABRICATED FILLER & DOUBLER & FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7. CLEANED, TREATED AND PRIMED AREA PLUS FILLER, DOUBLER AND FINGER DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 107-108 FIG 7, SRM 51-1-20D PG 9, AND DC8 SRM 51-1-21. 2L74 4F RT4A25 20040622000662004062200066WP 2004 6 22 IXXA0400037S 120040309A5753 SKIN DOUG DC8 DC873F 302199FWP RT WING TE FLAP WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT OUTBD FLAP UPPER PLATING DOUBLER WORN OUT OF LIMITS (STA 226.000-333.000) MAJOR REPAIRS. REPAIR IS ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 4. REMOVED WORN PLATING IAW DC8 SRM 51-1-21 PG 1, FABRICATED NEW PAINTING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 FIG 4, CLEANED TREATED AND PRIMED PLATING INNER SIDE & INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-8B. 2L74 4F RT4A25 20040622000722004062200072NM 2004 6 22 AWXA200400545 120040501A532065479573 SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND IN THREE PLACES ON AFT CARGO COMPARTMENT THRESHOLD SUPPORT WEB BETWEEN BS 796 AND BS 847, RBL 23 AND RBL 27. MAINTENANCE REMOVED DAMAGED THRESHOLD SUPPORT WEB FROM BS 796 TO BS 847, RBL 23 TO RBL 27; FABRICATED A NEW REPLACEMENT THRESHOLD SUPPORT WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9-10. 2L72 4F RTA16WE 20040622000772004062200077EU 2004 6 22 AWXA200400550 120040520A332032507010 BALLAST AIRBUS320 A320231 3930325EU SEAT ROW 1 LT DEFECTIVE A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP28636AW 098 LAS - BURNING ODOR - FLT 0747 - EN ROUTE FROM CHM TO LAS AT 10,000 FT A BURNING ELECTRICAL ODOR WAS OBSERVED IN THE COCKPIT AND FORWARD CABIN, SMELL DISSIPATED AFTER APPROXIMATELY 1 MINUTE. MAINTENANCE FOUND A DEFECTIVE CEILING LIGHT BALLAST AT SEAT ROW 1 LT, REPLACED LIGHT BALLAST SEAT ROW 1 LT, OPERATIONAL CHECK OF CABIN LIGHTING WAS GOOD. 2L72 4F RTA28NM 20040622000942004062200094 2004 6 22 SWAA041718 420040618A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040622000952004062200095NM 2004 6 22 SWAA041719 120040618A33506114789 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR OVERWING FWD AND AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040622001002004062200100 2004 6 22 SWAA041723 420040619A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED L1 DOOR EVAC SLIDE HOOKS PER MM. 2L72 4F RTA16WE 20040622001192004062200119EU 2004 6 22 DHL2004364516 120040316A5320A2577105120000 ANGLE AIRBUS300 A300B4203 3930306EU FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, REPLACE INNER & OUTER RIM ANGLES FR 80 STA 4944 STR 56L. REMOVED FASTENERS, SEALANT & PNEU DUCT FR 76-FR 80 LT, FORMED SECTION FR 80 & CONNECTING FITTINGS P27L - P27R. NO CORROSION. REMOVED FASTENERS INNER RIM ANGLE REPAIR AREA P42L - P42R, RADIAL SECTIONS & CIRCUM STRAPS CONNECTING STRAPS SHIMS & RIM ANGLE (INNER), CUT CIRCULAR STRAP, PERFORMED HFEC OF EXPOSED OUTER ATTACH ANGLE, NO CRACKS. RE-EVALUATION OF OUTER RIM ANGLE, NO DAMAGE OR CORROSION. FOUND INNER RIM ANGLE DAMAGED. DRILLED NEW INNER RIM SECTION, INSTALL FORKED SECTION FR 80, CONNECTING FITTINGS & CIRCUM STRAP SECTION, SUPPORT SEGMENTS STR 27L-27R AFT FACE OF FRAME 80. REINSTALLED LT & RT SERVO HYD LINES LOWER FR 80 BLKHD. 2L72 4F RTA35EU 20040622001262004062200126WP 2004 6 22 DHL2004803546 120040512A57305611014453 PANEL DOUG DC8 DC873 302199CWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING T/E LWR HONEYCOMB PANEL INTERIOR AND EXTERIOR SKIN DELAMINATED (STA XF 219.000-339.000). REMOVED AND REPLACED HONEYCOMB PANEL TO LT WING INBD T/E (STA XF 219.000-339.000) IAW DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040622001742004062200174EU 2004 6 22 ASOA04353 120040428A5320 SUPPORT BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK, CORROSION WAS FOUND OUT OF LIMITS ON THE BRACKET SUPPORT ON THE LT SIDE THRESHOLD AT STRINGER 14 LT AT FRAME 37 AND BETWEEN FRAMES 38 AND 39. MAINTENANCE REPLACED THE CORRODED BRACKETS IAW SRM 512500. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040622001792004062200179EA 2004 6 22 ASOA04349 120040514A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING C-CHECK INSPECTION, THE CLIPS AT FS 280 WERE FOUND CRACKED ON BOTH IB AND OB SIDES OF RBL AND LBL 9. MAINTENANCE REMOVE AND REPLACED CRACKED CLIPS IAW SRM 5100. 2L72 4F4 FRTA21EA E15NE 20040622001802004062200180WP 2004 6 22 GTIA040475 120040308A575499375012 BRACKET DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE RT WING SLAT DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 TEMPORARY BLEND OUT REPAIR TO SLAT BRACKET (PN 9937501-2) RT WING STA 199. REMOVED TEMPORARY DOUBLER. FABRICATED -3 FILLER AND -5 DOUBLER IAW EA 2780-0405. INSTALLED -3 FILLER AND -5 DOUBLER. 2L72 4F4 F A6WE E2EA 20040622002022004062200202NM 2004 6 22 277847 120040508A2923323636 PUMP BOEING727 727200 138407ENM HYD SYS LEAKING A RYNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE077635U 19908 DURING CRUISE FLIGHT, EXPERIENCED A LOSS OF HYDRAULIC FLUID ON (B) SYSTEM. AN EMERGENCY LANDING WAS INITIATED AND THE AIRCRAFT LANDED, WITHOUT INCIDENT. REMOVED AND REPLACED B SYSTEM HYDRAULIC PUMP. 2L73 4F RTA3WE 20040623000182004062300018WP 2004 6 23 GTIA040487 120040429A57539957576502 SKIN PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE RT FLAP DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT FLAP TE NR 1 DENTED, RIVETS PULLING THROUGH. REMOVED DAMAGED SKIN. LOCATED, DRILLED NEW PANEL. INSTALLED NEW PANEL. 2L72 4F4 FRTA6WE E2EA 20040623000462004062300046EA 2004 6 23 ASOA04391 120040528A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27842AS 7304 DURING HANGER MAINTENANCE, THE NR 3 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040623000512004062300051WP 2004 6 23 GTIA040479 120040504A5315 FLOORBEAM DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 FLOORBEAM AT STA 1309 FROM RBL 22 TO LBL 22 CORROSION. REMOVED FLOORBEAM. FABED FLOORBEAM. INSTALLED FLOOR SUPPORT. 2L72 4F4 FRTA6WE E2EA 20040623000522004062300052WP 2004 6 23 GTIA040490 120040427A5310 FITTING DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE CARGO BAY CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 MID PIT DOOR FORWARD DOOR UPLATCH BRACKET BENT, FITTING CRACKED AND GUIDE WORN. REMOVED FITTING. INSTALLED FITTING. 2L72 4F4 FRTA6WE E2EA 20040623000542004062300054WP 2004 6 23 GTIA040541 120040430A5310 BEAM DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 AFT PIT DOOR JAM BEAM STA 1155-1212 REPAIRED STRAP AND LOWER OB FLANGE CORRODED. REMOVED JAM BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. 2L72 4F4 FRTA6WE E2EA 20040623000562004062300056WP 2004 6 23 GTIA040493 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE CABIN DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 G2 GALLEY FLOORBOARD AT STA 200 TO STA 256 (N) DELAMINATED. FAB NEW FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040623000602004062300060WP 2004 6 23 GTIA040539 120040501A5330 DOUBLER DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE SKIN CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 AFT PIT CARGO DOOR CUT OUT INTERNAL SKIN DOUBLER CORRODED STA 1157-1211, L26R-28R. CUT OUT DAMAGED PORTION OF INTERNAL DOUBLER. FABRICATED REPAIR DOUBLERS AND FILLER. INSTALLED 2 EA REPAIR DOUBLERS AND FILLER. 2L72 4F4 FRTA6WE E2EA 20040623001082004062300108NM 2004 6 23 GTIA040548 120040518A5321 FLOOR PANEL DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 LT FLOORBOARD STA 927-1003 CORNERS CRACKED. FABED NEW FLOOR PANEL. 2L72 4F4 FRT E2EA 20040623001092004062300109NM 2004 6 23 PCAA0406215 120040602A532083231031103 FAILSAFE DHAV DHC8 DHC8102 2809003NM LT MLG WW BROKEN A PCAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA13839EX 226 FLIGHT 3806 LGA TO BURLINGTON EXPERIENCED A PROBLEM WITH THE LEFT MAIN GEAR DOOR FAILING TO RETRACT. THE AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO MIDDLETOWN FOR MAINTENANCE. IT WAS DISCOVERED THAT THE ATTACH POINT FOR THE PRE MOD GEAR DOOR ACTUATOR HAD BACKED OUT DUE TO THE FAILSAFE RETAINING TAB BEING BROKEN OFF, WHICH ALLOWED THE ACTUATOR PIVOT PIN TO MISALIGN AND PREVENT PROPER UPLOCK. FAILSAFE WAS REPLACED AND THE GEAR OPERATIONAL CHECKED. ALL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040624000022004062400002NM 2004 6 24 QXEA200400383 120040525A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - RIGHT HAND OUTBOARD NUMBER 11 SEAT TRACK AT STATION X438.0, TOP FLANGE IS SCRATCHED AND GOUGED. CHANNEL IS SCRATCHED. REPAIRED IAW DHC-8 SRM 51-40-00 AND 51-40-11. 2H72 4T RTA13NM 20040624000032004062400003EA 2004 6 24 COMA0470051 120040614A2760 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01369CA 10079 FLIGHT 5078 SPOILER, STAB AND RUDDER LIMIT FAULT MESSAGE DURING T/O. COULD NOT DUPLICATE. RESET SSCU 1 AND 2, SYSTEM CHECK SATISFACTORY. 2L72 4F RTA21EA 20040624000182004062400018EA 2004 6 24 COMA0460370 120040615A53116003603023 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 FRAME RADIUS CRACKED ABOVE STRINGER 10 AT LEFT HAND FS 718. FRAME RADIUS CRACKED BELOW STRINGER 11 AT LEFT HAND FS 718. PREVIOUS REPAIR HOLE PATTERN BETWEEN STRINGER 10 AND 11 WILL NOT ALLOW FOR EO 53-027. REMOVED AND REPLACED SECTION OF FS 718.00. COMPLIED WITH FRAME SPLICE IAW CRJ SRM 53-11-15. 2L72 4F RTA21EA 20040624000292004062400029NM 2004 6 24 UPS04542532 120040517A5347 SEAT TRACK BOEING757 75724APF 1384969NM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01411UP 23851 INSPECTION TYPE: C3, CORROSION SEAT TRACK BS 880-895 LBL 46 HAS MECHANICAL DAMAGE AND CORROSION. REMOVED CORRODED AND DAMAGED SEAT TRACK, AND REPLACED WITH FABRICATED SEAT TRACK. 2L72 4F RTA2NM 20040624000302004062400030NM 2004 6 24 UPS04542533 120040517A5311 FRAME BOEING757 75724APF 1384969NM FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01411UP 23851 INSPECTION TYPE:C3 FWD CARGO COMPARTMENT BS 680, BETWEEN STR 23 RT AND STR 24 RT, FRAME IS DENTED. REMOVED DAMAGE FROM FRAME, FABRICATED DOUBLER AND INSTALLED PER SRM 51-70-11 FIG 1. 2L72 4F RTA2NM 20040624000412004062400041EA 2004 6 24 COMA0470047 120040606A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01368CA 10075 FLIGHT 5249 RT THRUST REVERSER UNSAFE CAUTION DURING T/O. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040624000432004062400043WP 2004 6 24 ABXA040212 120040619A32607000010101ABX DOWNLOCK SWITCH DOUG DC9 DC932 3022066WP NLG MALADJUSTMENT A ABXAO OTHER O OTHER NRNOT REPORTED 1 GL23988AX915 47084 NOSE GEAR RED UNSAFE INDICATOR WOULD NOT ILLUMINATE WITH THROTTLES AT IDLE. PRESS TO TEST OK, HAD TO RECYCLE GEAR TO OBTAIN NOSE GEAR GREEN SAFE LIGHT. TESTED NOSE GEAR DOWNLOCK SWITCH. COULD NOT DUPLICATE. REPLACED THE NOSE GEAR DOWNLOCK SWITCH AS A PRECAUTION IAW DC9 MM 32-60-01-2-0101. OPS CHECK GOOD ON GEAR SWING. 2L72 4F A6WE 20040624000492004062400049NM 2004 6 24 SWAA041733 120040621A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS AT ROW 20 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040624000632004062400063EA 2004 6 24 COMA0470052 120040619A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01391CA 10108 FLIGHT 5048 RECEIVED A RIGHT THRUST REVERSER UNSAFE CAUTION DURING TAKEOFF ROLL, ABORTED AND RETURNED TO THE GATE. DEFERRED THE RIGHT THRUST REVERSER SYSTEM PER MEL 78-30-01. 2L72 4F RTA21EA 20040624000642004062400064NE 2004 6 24 COMA060384 220040616A7320 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO01981CA 7163 FLIGHT 5402 LT ENGINE SURGED 15 PERCENT DURING T/O. DEFERRED ENGINE SPEED CONTROL PER MEL. 2L72 4F4 FRTA21EA E15NE 20040624000662004062400066EA 2004 6 24 COMA0460335 120040528A5280 SKIN CNDAIRCL600 CL6002B19 1900309EA MLG DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 SKIN CRACKED BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT HAND SIDE APPROX .500 IN LENGTH. COMPLIED WITH REO 601R-52-11-048 AS INSTRUCTED. 2L72 4F RTA21EA 20040624000692004062400069EU 2004 6 24 DHL2004364004 120040529A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 2 ENGINE INTERMITTENT A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01364DH 141 ENGINE NR 2 LOOP-A LIGHT ON INTERMITTENTLY WITH MASTER WARNING PANEL (MWP) LOOPS LIGHT AND CHIME. ABNORMAL PROCEDURE COMPLETE. LOOP-B TESTS GOOD. INSPECTED NR 2 ENGINE LOOPS FOR DEFECTS, NONE NOTED. SYSTEM OPS CHECKED OK PER M/M 26-12-12. 2L72 4F RTA35EU 20040624000702004062400070EU 2004 6 24 DHL2004364005 120040530A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 2 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01364DH 141 LOOPS-A ON ENGINE NR 2 ILLUMINATED ON S/O'S PANEL WITH LOOPS LIGHT ON MASTER WARNING PANEL (MWP) ILLUMINATED WITH A CHIME. COMPLETED ABNORMAL PROCEDURES. LOOP-B TESTS OK. DEFERRED A-LOOP ON NR 2 ENGINE IAW MEL 26-12-01, CAT-B, DMI 16753. PLACARDS INSTALLED. TROUBLESHOT PER FIM 26-13-00. REPLACED HOT SECTION AFT LOOP PER A/B M/M 26-12-12 AND OPS CHECKED SERVICEABLE PER A/B M/M 26-12-12. DMI 16753 CLEARED. PLACARD REMOVED. 2L72 4F RTA35EU 20040624000732004062400073WP 2004 6 24 ABXA040211 120040616A561029190701 SPRING DOUG DC8 DC861 3021952WP COCKPIT WINDOW BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23843AX 46017 DURING MAINTENANCE INSPECTION, FOUND THE FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND SPRING BROKEN ON AFT LOWER HOOK. REPLACED SPRING. WINDOW CHECKED GOOD PER DC8 MM 56-10-03. 2L74 4F 4A25 20040624000742004062400074NE 2004 6 24 ABXA040210 220040617A7200 ENGINE DOUG DC8 DC861 3021952WP PWA JT3D JT3D3B 52039NE NR 3 VIBRATION A ABXAO OTHER E VIBRATION/BUFFET APAPPROACH 1 GL23847AX598633191 46031 644651 AT 2000 FEET AND LEVELING OFF, POWER ADVANCED TO MAINTAIN AIRSPEED, HAD SEVERE NR 3 ENGINE VIBRATION. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IAD TO ILN. UPON ARRIVAL AT ILN, THE NR 3 ENGINE WAS REPLACED. 2L74 4F4 F 4A25 1E8 20040624000772004062400077EA 2004 6 24 COMA0460350 120040604A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01917CA 7017 PAX DOOR FORWARD LOWER ANGLE DAMAGED AT FS 310.00 AT FORWARD PULL-IN LEVER. REPAIRED DAMAGED ANGLE IAW BOMBARDIER REO 601R-52-11-509. 2L72 4F RTA21EA 20040624000782004062400078EA 2004 6 24 COMA0460340 120040527A2613601R31039162 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01936CA19582 7043 FLIGHT 5530 MLG OVERHEAT WARNING. REPLACED THE RT MLG WHEEL BIN ASSY. 2L72 4F RTA21EA 20040624000792004062400079EA 2004 6 24 COMA0460341 120040527A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01960CA 7117 FLIGHT 5399 LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL. 2L72 4F RTA21EA 20040624000802004062400080EA 2004 6 24 QXEA200400386 120040530A5240CC670382641 UPLOCK CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DISENGAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09600QX6203 10005 PDX - FLIGHT 2553 - UNABLE TO OPEN FORWARD GALLEY SERVICE DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE DOOR UPLOCK ACTUATOR INNER AND OUTER ASSEMBLIES DISENGAGED. THE ASSEMBLIES WERE RE-ENGAGED AND OPERATIONAL CHECKS WERE PERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040624000812004062400081EA 2004 6 24 COMA0460360 120040607A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYSTEM UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA17256 7017 FLIGHT 5056 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20040624000832004062400083NE 2004 6 24 COMA0460381 220040614A72615018T49P01 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01716CA 7250 FLIGHT 5835 RT ENGINE LOW OIL PRESSURE WARNING. REPLACED ACCESSORY GEARBOX DRIVE OIL SEALS. 2L72 4F4 FRTA21EA E15NE 20040624000852004062400085WP 2004 6 24 ABXA040206 120040604A533099155871 PANEL DOUG DC9 DC932 3022066WP WINDOW BELT DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23984AX 47258 COMPLY WITH COI 42381-001. REMOVED AND REPLACED WINDOW BELT RIGHT FUSELAGE EMERGENCY EXIT AREA. COMPLIED WITH COI 42381-001. 2L72 4F A6WE 20040624000862004062400086WP 2004 6 24 ABXA040205 120040527A534049191472 FITTING DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23984AX 47258 FITTING CRACKED AFT SIDE FS 1038, LONGERON 15 RIGHT. REPLACED FITTING AT AFT SIDE OF FRAME FS 1038, LONGERON 15 RIGHT IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 20040624000872004062400087NE 2004 6 24 ARWA20040505 220040513A7250758701 BLADE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7A 52039NE NR 2 ENGINE DAMAGED A ARWAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO19906R 590655498 46087 671275 NR 2 ENGINE EGT (EXHAUST GAS TEMPERATURE) IS 40 DEGREES HIGHER THAN OTHER ENGINES IN CRUISE. ALL OTHER PARAMETERS NORMAL. ON POST-FLIGHT INSPECTION, NR 2 ENGINE APPEARS TO HAVE T4 BLADES DAMAGED. UPON INSPECTION, NR 2 ENGINE TURBINE 1ST STAGE (T-1) VANE BLADE BROKEN (50 PERCENT) AND L/E WITH NICKS. REMOVED AND REPLACED NR 2 ENGINE IAW ARROW AIR J/C DC8MM 007 & DC8MM 71-00. ACCOMPLISHED ENGINE RUN-UP IAW ARROW AIR J/C DC8MM 003 & DC8MM 71-00, FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20040624000892004062400089EA 2004 6 24 COMA0460357 120040608A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01916CA220 7014 FLIGHT 5805 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040624000902004062400090EA 2004 6 24 COMA0460356 120040608A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01709CA15073 7238 FLIGHT 5156 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040624000922004062400092EA 2004 6 24 COMA0460359 120040608A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01716CA 7250 FLIGHT 5143 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040624000932004062400093EA 2004 6 24 COMA0460362 120040609A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 RIGHT HAND FS 718.00 BETWEEN STRINGERS 10-12 CRACKED. REMOVED ACCESS PANEL 423CB FROM RIGHT HAND PYLON. REMOVED HI-LOKS AND RIVETS FROM 718 FRAME IN AREA OF REPAIR. CUT THE FRAME FLANGE AND FRAME DOUBLER BETWEEN STRINGERS 10 & 11. COMPLIED WITH NDT CUT OUT IAW EO 53-027. DRILLED DOUBLERS, INSTALLED RIVETS AND HI-LOKS IAW S/B 601R-53-055. COMPLETED PARTS A AND C OF S/B 601R-53-055. INSTALLED ACCESS PANEL 423 CB IAW S/B 601R-53-055. 2L72 4F RTA21EA 20040624000942004062400094NE 2004 6 24 COMA0470046 220040527A72304114T16P02 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE VIBRATES A COMAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01367CA1180 10069 965772 FLIGHT 5672 NR 2 ENGINE FAN VIBE INDICATES 2.4. REPLACED THE RT ENGINE FAN BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20040624000982004062400098NM 2004 6 24 PCAA0405213 120040524A2710DSC65 ROD END DHAV DHC8 DHC8102 2809003NM AILERON WORN A PCAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA13812EX 312 FLIGHT 4099 REPORTED A VIBRATION DURING CRUISE FLIGHT. THE VIBRATION DID NOT APPEAR TO BE ASSOCIATED WITH THE PROPELLERS. THE CREW DECIDED TO DIVERT TO MIDDLETOWN. MAINTENANCE FOUND THE INPUT CONTROL ROD AT THE RIGHT HAND AILERON WORN. BUSHING WAS INSTALLED PER RD 8-57-087 AND ROD END FOR CONTROL ROD WAS REPLACED. AIRCRAFT WAS TEST FLOWN, TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040624001022004062400102NM 2004 6 24 QXEA200400387 120040526A5330 PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - PANEL 122AR HAS A STRIPPED NUT PLATE. MAINTENANCE REMOVED AND REPLACED NUT PLATE IAW Q400 SRM. 2H72 4T RTA13NM 20040624001032004062400103NM 2004 6 24 F3LA200400063 120040523A5730 PANEL BOEING737 7373L9 1384470NM RT WING CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03312FL 2843 24569 DURING C-6 CHECK, INSPECTION REPORTED RT WING UPPER SURFACE AFT PYLON PANEL CRACKED AT AFT I/B CORNER AT FASTENER COMMON TO FUEL CELL. REPLACED PANEL PER SRM 51-40-02 AND 51-40-65. 2L72 4F RTA16WE 20040624001052004062400105EA 2004 6 24 COMA0460348 120040601A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01914CA629 7012 FLIGHT 5483 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040624001062004062400106NM 2004 6 24 QXEA200400389 120040528A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 526 PDX - A NUT PLATE ON PANEL 121BL SPINS, BOTTOM ROW, MIDDLE NUT PLATE. MAINTENANCE REMOVED AND REPLACED THE NU00177T PLATE IAW-200 SRM. 2H72 4T RTA13NM 20040624001082004062400108WP 2004 6 24 ABXA040203 120040607A5330591970731 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND CORRODED AT STA 917 AND LONGERON 28 RIGHT. REPAIRED SKIN IAW REA D953-49934MR. 2L72 4F A6WE 20040624001102004062400110WP 2004 6 24 ABXA040202 120040607A5330591142125 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND BULGED AT STA 759, LONGERON 29 RIGHT. REPAIRED SKIN IAW DC-9 SRM 53-04, FIG 12B. 2L72 4F A6WE 20040624001122004062400112EA 2004 6 24 COMA0460383 120040616A2420 STATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE ALTENATOR MALFUNCTIONED A COMAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO01495CA GJA19638 7774 FLIGHT 5242 RT ENGINE N2 FLUCTUATIONS. REPLACED THE ALTERNATOR STATOR. 2L72 4F4 FRTA21EA E15NE 20040624001132004062400113NE 2004 6 24 ABXA040208 220040610A7200 ENGINE DOUG DC9 DC932F 3022067WP PWA JT8 JT8D9A 52048NE LEFT STALLED A ABXAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23909AX1778 47148 665904 LEFT ENGINE COMP STALLED AND STARTED TO VIBRATE. PULLED THROTTLE BACK TO IDLE AND DIVERTED TO BDL. REMOVED AND REPLACED NR 1 ENGINE IAW DC-9 AMM 72 AND ABX JOB CARDS. OPS CHECKED GOOD. 2L72 4F4 F A6WE E2EA 20040624001162004062400116EA 2004 6 24 SWIA200413360 120040418A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 U-CHANNELS ON FUSELAGE, PAX DOOR SILL CORRODED (UNDER PANEL 231CLF). DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL P/N 601R31527-217 AT FOWARD AND AFT LOCATIONS IAW CRJ SRM 51-42-06 AND 51-42-11. 2L72 4F4 FRTA21EA E15NE 20040624001182004062400118EA 2004 6 24 SWIA200413362 120040528A2701 NUT CNDAIRCL600 CL6002B19 1900309EA YOKE LOOSE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07448SW 7678 AUDIBLE AND TACTILE CLICK/RUDDER AT 30 DEGREES YOKE INPUT; BOTH DIRECTIONS. FERRIED TO SLC. TORQUED THE PILOT'S CONTROL YOKE CENTER SHAFT NUTS IAW CRJ MM 27-11-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040624001202004062400120NM 2004 6 24 XNOA1188 120040602A3220 LANDING GEAR BOEING727 727227 1384078NM NOSE MALFUNCTIONED A XN0AO OTHER J WARNING INDICATION APAPPROACH 1 GL2376753 21249 ON FINAL, NOSE GEAR WOULD NOT EXTEND, RECYCLED PER CHECKLIST AND LANDED. PERFORMED NORMAL LANDING GEAR CONTROL SYSTEM TEST IAW B727MM 32-31-0. TEST GOOD. 2L73 4F A3WE 20040624001212004062400121NM 2004 6 24 DHL2004754015 120040520A5320 ANGLE BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING C-CHECK, AFT LWR COMPART INTERCOSTAL WEB CORRODED WHERE ATTACHED TO TRANSITION PANEL BS 1050 THRU BS 1070 BY STR 26R. CORROSION FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. REMOVED WEB & ANGLE AND FABBED NEW ANGLE FROM 2024-T3 .050, PO 900931 DIM 19 X 2 INCHES IAW 727 SRM 51-40-3 FIG 1. ANGLE TREATED & PRIMED IAW 727 SRM 51-10-2, NEW ANGLE & WEB INSTALLED IAW 727 SRM 51-30-2. 2L73 4F A3WE 20040624001222004062400122EA 2004 6 24 COMA0460367 120040613A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01806CA 7359 FLIGHT 5054 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040624001242004062400124EA 2004 6 24 COMA0460354 120040609A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 AIRCRAFT DAMAGED BELOW APU EXHAUST. AIRCRAFT HAS GASH 5.50 INCHES LONG AT FS 682 AND GOUGED SKIN FROM FS 672.00 TO 700. REMOVED EXISITNG FASTENERS AROUND DAMAGED AREA. CUT OUT AREAS OF DAMAGE AND PERFORMED CPI PER NDTM 51-20-08. ALODINED AND PRIMED AFFECTED AREA. DUPLICATED DOUBLER FROM 2024 T3 .063 AND BACK DRILLED ALL HOLES. READY TO SEAL AND SHOOT ON. SEALED DOUBLER AND INSTALLED FASTENERS IAW BOMBARDIER REO 601R-53-61-1045. 2L72 4F RTA21EA 20040624001252004062400125EA 2004 6 24 COMA0460355 120040609A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 DENT IN FUSELAGE SKIN, JUST AFT OF FS 700 AND ABOVE STRINGER. CUT OUT DAMAGED AREA. FABRICATED DOUBLER (2024T-3. 063), INSTALLED DOUBLER. COMPLETED REPAIR IAW REO 601R-53-61-1045. 2L72 4F RTA21EA 20040625000012004062500001WP 2004 6 25 AALA20040626 120040608A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21479AA 49654 DFW - AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING AT SEAT 27D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHTING ASSEMBLY AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040625000022004062500002WP 2004 6 25 AALA20040627 120040608A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21293AA 49305 DFW - EMERGENCY EXIT CEILING LIGHTS AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040625000032004062500003WP 2004 6 25 AALA20040628 120040609A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21585AA 53248 TPA - EMERGENCY EXIT LIGHT AT SEAT 11D INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT SOCKET AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040625000042004062500004NM 2004 6 25 AALA20040629 120040606A2910 LINE BOEING767 767323 1385205NM HYD SYSTEM LEAKING A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21374AA 25201 JFK - LEFT HYDRAULIC FLUID LOW AND DROPPING, SYSTEM WAS SHUT DOWN. LANDED JFK WITHOUT INCIDENT. SECURED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040625000052004062500005 2004 6 25 AALA20040630 420040520A34206227999003 HSI BOEING767 767323 1385205NM COCKPIT DEFECTIVE A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21355AA 24036 OGG - FIRST OFFICERS HSI BLANKED OUT. REPLACED FIRST OFFICERS HSI. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040625000062004062500006NM 2004 6 25 AALA20040631 120040522A3610 WARNING LIGHT BOEING767 767300 1385204NM RT ENGINE ILLUMINATED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21398AN 29605 GRU - RIGHT PACK OFF LIGHT ILLUMINATED AND RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED. ACCOMPLISHED BYTE CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040625000072004062500007NM 2004 6 25 AALA20040632 120040523A2410 IDG BOEING767 767323 1385205NM LT ENGINE MALFUNCTIONED A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21370AA 25197 FCO - LEFT GENERATOR DRIVE EICAS MESSAGE APPEARED, FLICKERED AND THEN EXTINGUISHED. SERVICED LEFT HAND IDG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040625000092004062500009NM 2004 6 25 AALA20040635 120040604A2420756603E GENERATOR BOEING777 777223 1385213NM RT ENGINE DEFECTIVE A AALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW21771AN 29579 RIGHT GENERATOR FAILED. REPLACED RIGHT GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040625000102004062500010WP 2004 6 25 AALA20040662 120040619A335040030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21438AA 49456 DFW - CEILING EMERGENCY LIGHTS AT ROWS 2 THROUGH 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 2 THROUGH 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040625000112004062500011NM 2004 6 25 AALA20040663 120040619A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21969AN 29546 RNO - INSEAT EMERGENCY LIGHTS AT ROWS 12, 13 AND 14DEF INOPERATIVE. REPLACED BATTERY PACK AT RIGHT HAND OVERWING EMERGENCY EXIT FOR ROWS 12, 13, AND 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040625000122004062500012NM 2004 6 25 UPS04M42519 120040322A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 35 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.015 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-4 (REF UPS ENGINEERING FILE NR MD11-55-20042. 2L73 4F RTA22WE 20040625000132004062500013NM 2004 6 25 UPS04M42520 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 30 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.041 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040625000142004062500014NM 2004 6 25 UPS04M42521 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 21 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000152004062500015NM 2004 6 25 UPS04M42522 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 05 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000162004062500016NM 2004 6 25 UPS04M42523 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 06 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.018 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-194094-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040625000172004062500017NM 2004 6 25 UPS04M42524 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 02 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.022 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040625000182004062500018NM 2004 6 25 UPS04M42525 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 27 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED EN 1157-04 (REF UPS ENGINEERING FILE NR MD 11-55-20040). 2L73 4F RTA22WE 20040625000192004062500019NM 2004 6 25 UPS04M42526 120040326A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 08 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED BOTTOM BORED DOWN 0.018 INCH PER EN 1124-04. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-55 10-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040625000202004062500020NM 2004 6 25 UPS04M42527 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 30 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-04 (REF UPS ENGINEERING FILE NR MD11-55-20042). 2L73 4F RTA22WE 20040625000212004062500021NM 2004 6 25 UPS04M42528 120040324A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 16 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.058 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERNG FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000242004062500024NM 2004 6 25 UPS04M42535 120040603A5610NBA604721 WINDOW DOUG MD11 MD11F 3023600NM COCKPIT LEAKING A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01271UP 57 MINUTES INTO FLIGHT AT FL320, FLIGHT AIR NOISE EMANATING FROM UPPER LEFT CORNER OF R2 WINDOW. AT 66 MINUTES INTO FLIGHT NOISE BECOMES A WHISTLE SOUND. SOUND BECAME INTERMITTENT FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RT SLIDING WINDOW AS PER MM 56-12-01. PERFORMED ADJ/TEST IAW MM 56-12-01 PG 501. FOUND SATISFACTORY. THIS CLEARS D281995. 2L73 4F RTA22WE 20040625000252004062500025NM 2004 6 25 UPS04M42456 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 01 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.055 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1109-04 (REF UPS ENGINEERING FILE NR MD11-55-20037). 2L73 4F RTA22WE 20040625000352004062500035NM 2004 6 25 UPS04M42466 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE RT NR 02 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 43 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000362004062500036NM 2004 6 25 UPS04M42467 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 33 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.009 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5110-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-04 (UPS ENGINEERING FILE NR M D11-55-20042). 2L73 4F RTA22WE 20040625000372004062500037NM 2004 6 25 UPS04M42468 120040401A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 05 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040625000402004062500040NM 2004 6 25 UPS04M42471 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 15 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.007 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000412004062500041NM 2004 6 25 UPS04M42472 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 33 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040625000432004062500043NM 2004 6 25 UPS04M42474 120040324A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 35 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040621000152004062100015WP 2004 6 21 ASAA0480257 120040404A5730ABB0975522 PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND LEFT WING PANEL 1472C CORRODED. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040621000222004062100022WP 2004 6 21 ASAA0480239 120040404A5320991015193 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND CORROSION ON CUSP WEB STATION 826 TO 845 LEFT FUSELAGE LBL 44 TO LBL 59. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-70-4. (M) 2L72 4F RTA6WE 20040621000232004062100023WP 2004 6 21 ASAA0480402 120040515A532199363051 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OKC - DURING C-CHECK, FOUND LEFT EXIT ROW 22 FLOOR PANEL IS BROKEN AND DELAMINATED. REMOVED FLOOR PANEL AND INSTALLED REPLACEMENT FLOORBOARD IAW 53-05. (M) 2L72 4F RTA6WE 20040621000292004062100029WP 2004 6 21 ASAA0480253 120040404A5313593666713 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - FOUND LONGERON 30 IS CORRODED AT STATION 1231 TO 1250. REMOVED DAMAGE, ORDERED TRIMMED AND INSTALLED NEW LONGERON SECTIN AND SPLICE IAW MD80 SRM 53-02. (M) 2L72 4F RTA6WE 20040621000492004062100049WP 2004 6 21 ASAA0480368 120040503A531159305846124 FRAME DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS 49236 OKC - DURING C-CHECK, FOUND TEMP REPAIR INSTALLED ON FORWARD FRAME AT FS 811. REPAIR IAW SRM. (M) 2L72 4F A6WE 20040621000502004062100050WP 2004 6 21 ASAA0480401 120040515A53115930584123 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OKC - DURING C-CHECK, FOUND LEFT WHEEL WELL FAIRING FRAME CRACKED AT FASTENER. REMOVED DAMAGED FRAME AND INSTALLED NEW IAW 51-30-2. (M) 2L72 4F RTA6WE 20040621000562004062100056NM 2004 6 21 VNAA0406002 120040602A3350501122803 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL05429JS19038788 3043 THE CREW REPORTED THAT DURING THE EMERGENCY POWER SUPPLY TEST, ONLY THE TOP LIGHT CAME ON. MAINTENANCE INSPECTED AND REPLACED THE FORWARD EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENACE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000602004062100060NM 2004 6 21 VNAA0406007 120040613A3350 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL05441JS 3059 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLIES FAILED TO TEST. MAINTENANCE HAD THE CREW RUN THE ENGINES FOR 10 MINUTES AND PERFORM AN OPERATIONAL CHECK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040621000632004062100063NM 2004 6 21 SWAA041707 120040617A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040621000692004062100069NM 2004 6 21 SWAA041713 120040617A57536546435273 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED PM CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E FLAP PER MM. 2L72 4F RTA16WE 20040621000792004062100079EA 2004 6 21 VNAA0404018 120040424A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT ILLUMINATED A VNAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL07245PS37 7919 DURING TAXI RT OVERWING EMERGENCY EXIT CAS MESSAGE ILLUMINATED. FLIGHT 2303 RETURNED TO GATE. MAINTENANCE INSPECTED AND DEFERRED THE DOOR INDICATION 52-70-03 CODE C. 2L72 4F RTA21EA 20040621000832004062100083CE 2004 6 21 GLBA20030627 120040519A61235038912121 PRESSURE SWITCH BEECH 1900 1900D 1154162CE AUTO FEATHER MALFUNCTIONED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 NM03179GL6637 UE179 LEFT AUTO FEATHER EXTINGUISHES AFX DISABLES WITH POWER AT 3250 FT. REMOVED AND REPLACED RT AUTO FEATHER HIGH PRESS SWITCH P/N 50-389121-21. 2L72 4T RTA24CE 20040621000922004062100092NM 2004 6 21 CALA0400526 120040526A3213161W11521 STRUT BOEING777 777224 1385225NM RT MLG CRACKED A CALAK NONE K FLUID LOSS ININSP/MAINT 1 SW277800824216 29478 INSPECTION FOUND THE RT MLG SHOCK STRUT LEAKING FLUID FROM TOP OF THE OUTER CYLINDER. THE INNER AND OUTER CYLINDERS WERE REMOVED. THE ORIFICE SUPPORT TUBE WAS REMOVED FROM THE OUTER CYLINDER AND FOUND TO BE CRACKED THROUGH. THE INSIDE DIAMETER OF THE OUTER CYLINDER WAS INSPECTED AND NO DAMAGE WAS FOUND. A NEW ORIFICE SUPPORT TUBE WAS INSTALLED ON THE EXISTING OUTER CYLINDER WHICH WAS REINSTALLED. THE SHOCK STRUT WAS FULLY SERVICED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. THE ORIFICE SUPPORT TUBE WAS SENT TO BOEING FOR INVESTIGATION AND ANALYSIS. 2L72 4F RTT00001SE 20040621001092004062100109NM 2004 6 21 CALA0400531 120040612A3350D71702001 POWER SUPPLY BOEING767 767424ER 1385270NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2776055 29450 THE EMERGENCY LIGHTS IN CEILING AT 17L, 38L, AND 40L AND AFT GALLEY CENTER SECTION FLOOR WERE FOUND INOPERATIVE. THE M738 EMERGENCY LIGHT POWER SUPPLY WAS REMOVED AND REPLACED IAW 33-51-07, PAGE 201-211. 2L72 4F RTA1NM 20040621001192004062100119NE 2004 6 21 P5CA0401094 220040523A7261 B-NUT BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE ENGINE OIL LINE LOOSE A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP23920FT 22237 702238 NR 2 ENGINE IN FLIGHT SHUTDOWN DUE TO OIL PRESSURE LOSS AND OIL QTY=0. ON ENGINE INSPECTION FOUND MAIN SUPPLY OIL LINE B-NUT LOOSE AT OIL TANK, SECURED B-NUT SERVICED OIL, PERFORMED ENGINE RUN. 2L74 4F4 F A20WE E3NE 20040621001592004062100159 2004 6 21 ASMF200406014 420040615A34212587794 AHRS DOUG DC9 DC987 3022087WP NR 1 FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23803ML 49726 AIRCRAFT RETURNED, AHRU NR 1 FAILED. AIRCRAFT WAS DISPATCHED IAW ABNORMAL PROCEDURES MANUAL 10-4. DURING OVERNIGHT SERVICE, MAGNETIC FLOW VALVE WAS REPLACED IAW MM 34-21-06, TEST CORRECT. 2L72 4F RTA6WE 20040621001622004062100162NE 2004 6 21 ASMF200406011 220040613A7412103538754 EXCITER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23216AM 49586 718083 AIRCRAFT RETURNED TO PLATFORM, ENGINE NR 2 WITHOUT IGNITION. CAPTAIN PERFORMED ENGINE START IN OVERRIDE POSITION AND FAIL CONTINUED. EXCITER IGNITION BOX WAS REPLACED IAW MM 74-10-01, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040621001712004062100171 2004 6 21 ASMF200406004 420040604A3432VS534 RELAY DOUG DC9 DC987 3022087WP GLIDE SLOPE FAILED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23754RA 49641 AIRCRAFT RETURNED TO PLATFORM DURING ENGINE START, VHF NAV NR 1 FAILED. VHF NR 1 CONTROL PANEL, DFGC AND VOR RECEPTOR WERE REPLACED AND FAIL CONTINUE. ENGINE WAS SHUTDOWN AND HIGH FREQUENCY ON LT GENERATOR WAS DETECTED. LT GENERATOR WAS INOPERATIVE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIGHT SERVICE, RELAY R2-47 WAS REPLACED IAW WDM 24-23-00 AND TEST WAS PERFORMED IAW MM 34-32-00, ALL CORRECT. 2L72 4F RTA6WE 20040621001842004062100184NM 2004 6 21 QXEA200400359 120040521A3060 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM PROP DE-ICE SYS FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09539DS 4016 PDX - PROP DEICE CAUTION LIGHT CAM ON. RESET PROP DEICE PER CHECLIST, NO HELP ON CAUTION LIGHT. PROPS APPEARED TO WORK VIA GREEN LIGHTS. MAINTENANCE CHECKED CDS FAULT-ARONC RECEIVE BUS 2 ON TMCU 1 & 2. CLEARED FAULTS. PERFORMED FIM TASK. FUNCTION TEST AND CAL OF PROP DEICE SYSTEM. NO FAULTS REOCCURED. NO PARTS REPLACED, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040621001872004062100187NM 2004 6 21 QXEA200400332 120040518A5320 THRESHOLD BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - FORWARD RIGHT EMERGENCY EXIT THRESHHOLD CORROSION AROUND DOOR STOPS AND UNDER SILL PLATE. REPAIRED IAW HORIZON AIR EA 6-53-352. 2H72 4T RTA13NM 20040621001892004062100189NM 2004 6 21 QXEA200400334 120040520A1430 RIVET BOMBDRDHC8 DHC8401 1390041NM ZONE 200 BURNED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - ABOVE PILOT AND CO-PILOT WINDSHIELD HAS RIVET HEAD BURNED. REPAIRED IAW HORIZON AIR EA 6-53-354. 2H72 4T RTA13NM 20040621001912004062100191NM 2004 6 21 QXEA200400336 120040520A5320 CHANNEL BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - SEAT TRACK NR 15 , CORROSION PITS IN CHANNEL, IMPACT DAMAGE TO BOTH TOP FLANGES, STATION X705 TO X708. REPAIRED IAW DHC-8-400 SRM TASK 51-21-00-350-901. 2H72 4T RTA13NM 20040621001932004062100193NM 2004 6 21 QXEA200400352 120040520A1430 RIVET BOMBDRDHC8 DHC8401 1390041NM ZONE 200 BURNED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09401QX 4031 PDX - ABOVE PILOT AND CO-PILOT WINDSHIELD HAS RIVET HEADS BURNED APPROXIMATELY X-74 AND Z173.000. ALSO HAS SKIN DAMAGE. REPAIRED IAW HORIZON AIR EA 6-53-354 -A-. 2H72 4T RTA13NM 20040621001972004062100197EU 2004 6 21 AWXA200400508 120040515A2611 CONTROL UNIT AIRBUS320 A320231 3930325EU ZONE 120 MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28624AW 55 PHL - DIVERSION - FLT 0419 - DURING CLIMBOUT FROM BDL EN ROUTE FOR PHX RECEIVED CLASS 1 ECAM MESSAGE FOR FORWARD AND AFT CARGO SMOKE FOLLOWED BY FORWARD & AFT SMOKE DETECTOR FAULTS, ALSO RECEIVED LAVATORY SMOKE DETECTOR FAULT, DIVERTED TO PHL. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR CONTROL UNIT (10WQ) IAW AMM 26-17-34-04, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF SMOKE DETECTOR CONTROL UNIT COULD NOT DUPLICATE REASON FOR REMOVAL. UNIT WAS TESTED IAW CMM 26-17-34 AND RETURNED TO SERVICE. 2L72 4F RTA28NM 20040621001992004062100199NM 2004 6 21 AWXA200400510 120040429A531369451562 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND A .5 INCH CRACK IN STRINGER TIE CLIP AT BS 767, STR 1 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 767, STR 1 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-45156; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 6 & 8. 2L72 4F RTA16WE 20040621002072004062100207NM 2004 6 21 AWXA200400518 120040505A552265C25746132SP SKIN BOEING737 7373G7 1384595NM ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR RMCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR BETWEEN ELEV STA 159.0 AND ELEV STA 169.0. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-04 FIG 10. 2L72 4F RTA16WE 20040621002092004062100209NM 2004 6 21 AWXA200400520 120040511A552265C25746132SP SKIN BOEING737 7373G7 1384595NM ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR AT ELEV STA 212. MAINTENANCE PREPARED SURFACE AND PERFORMED BOND REPAIR TO RT ELEVATOR UPPER HONEYCOMB SURFACE PANEL AT ELEV STA 212 IAW B737-300 SRM 51-70-04 FIG 10. 2L72 4F RTA16WE 20040621002122004062100212NM 2004 6 21 QXEA200400346 120040521A3397 WIRE DHAV DHC8 DHC8202 2809007NM ZONE 200 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH 514 EMERGENCY LIGHTS WILL NOT TURN ON FROM FLIGHT ATTENDANTS SWITCH. REPAIRED BROKEN WIRE ON FLIGHT ATTENDANTS CONTROL PANEL SWITCH HARNESS AT THE CAPACITOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20040622000122004062200012WP 2004 6 22 ASAA0480298 120040420A53219936537501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURNG C-CHECK, FOUND CABIN FLOORBOARD STATION 168-160 LBL 8 TO RBL 17 FIBERGLASS TORN. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000202004062200020NM 2004 6 22 ASAA0410265 120040514A53126545808141 BULKHEAD BOEING737 737290C 138448VNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND BULKHEAD WEB CHAFED. REPAIRED NOSE WHEEL WELL AFT BULKHEAD PER SRM 51-40-2 FIG 1. (M) 2L72 4F A16WE 20040622000262004062200026WP 2004 6 22 ASAA0480288 120040420A5320593639517 ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND RIGHT MLG DOOR CUT OUT AFT OUTBOARD ANGLE CRACKED. REPLACED ANGLE PER SRM 53-05. (M0 2L72 4F RTA6WE 20040622000362004062200036NM 2004 6 22 ASAA0410263 120040515A5310654795910 FAILSAFE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON BS 794 FRAME FAIL/SAFE CHORD RBL 8-20 WL 155. INSTALLED NEW FAIL/SAFE CHORD. (M) 2L72 4F A16WE 20040622000462004062200046WP 2004 6 22 ASAA0480283 120040420A532199365441 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000732004062200073NM 2004 6 22 AWXA200400546 120040504A532065807351 CREASE BEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE UPPER AND LOWER SURFACE CREASE BEAM BETWEEN BS 967 AND BS 991, RBL 47, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED CREASE BEAM INNER CHORD SILL FROM BS 910 TO BS 1006, RBL 47; FABRICATED A NEW REPLACEMENT CREASE BEAM INNER CHORD PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1, 8 & 12. 2L72 4F RTA16WE 20040622000822004062200082NM 2004 6 22 AWXA200400555 120040428A5320146N874817 FITTING BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 LCQ - MAJOR REPAIR - DURING C-07 CHECK A 2 INCH CRACK WAS FOUND IN AFT CABIN INTERCOSTAL FITTING AFT OF THE L-4 DOOR CUTOUT, AT DOOR STOP FITTING BS 1681, WL 248. MAINTENANCE REMOVED CRACKED INTERCOSTAL FITTING AFT OF L-4 DOOR CUTOUT BS 1681, WL 248; FABRICATED A NEW REPLACEMENT INTERCOSTAL FITTING PER DWG 146N8748; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20040622000922004062200092NM 2004 6 22 SWAA041716 120040618A53116554892 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 340, STRINGER 23L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040622000962004062200096NM 2004 6 22 SWAA041720 120040619A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 960, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040622001012004062200101NM 2004 6 22 SWAA041724 120040620A56105893543140 WINDOW BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAO OTHER O OTHER CRCRUISE 1 SW29309SW 22948 RIGHT R1 COCKPIT WINDOW ARCHED AT CRUISE AND DEVELOPED A CRACK, WINDOW HEAT SELECTED OFF, QRH PROCEDURE COMPLETED, WINDOW DEVELOPED MORE SMALL CRACKS ON OUTER PANE. REMOVED AND REPLACED R1 COCKPIT WINDOW PER MM. 2L72 4F RTA16WE 20040622001122004062200112NE 2004 6 22 GLBA20030632 320040526A6197 PROPELLER EMB 120 EMB120ER 3260203SO HAMSTD14RF 14RF9 NE RIGHT MALFUNCTIONED A GLBAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM03299UX 120299 RT PROP FEATHERED WHEN CONDITION LEVERS PUSHED FWD ON 5 MILE FINAL. RAN A/C, INSPECTED SYSTEMS, COULD NOT DUPLICATE. NTSB REPORT: MX REPAIRED CHAFED WIRE ON RT ENGINE TORQUE SIGNAL CONDITIONER. 2L72 4T RTA31SO 6 CP11NE 20040622001162004062200116NM 2004 6 22 374PA0009 120040517A5320 THRESHOLD BOEING737 73736M 138443BNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 AFT CARGO DOOR CENTER SECTION OF THRESHOLD CRACKED. WELDED PER BAC 5975. 2L72 4F RTA16WE 20040622001252004062200125WP 2004 6 22 DHL2004803547 120040516A57203755028504 CLIP DOUG DC8 DC873 302199CWP NR 2 MAIN TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 NR 2 MAIN TANK LWR SPAR CLIP CRACKED 1.500 AT STA XW -6.000. REMOVED AND REPLACED CRACKED CLIP ON NR 2 MAIN TANK LWR SPAR, XW -6.000 IAW DC8 SRM 51-1-20D PG 9-21. 2L74 4F RT4A25 20040622001302004062200130WP 2004 6 22 DHL2004803514 120040325A5730 DOUBLER DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT WING CTR L/E LWR PART INTERNAL DOUBLER CRACKED 0.500 AT XFS 335.250. REMOVED CRACKED DOUBLER IAW DC8 SRM 57-1-0 PG 1, SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075-T6AL 0.090) IAW SRM 57-3-3 PG 14. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622001312004062200131WP 2004 6 22 DHL2004803515 120040324A5712 RIB DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LT OUTER WING OTBD L/E RIB CRACKED 0.250 AT XFS 741.250 (UPPER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (2024-T3AL 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622001402004062200140NM 2004 6 22 P5CA0401092 120040515A3240 LINE BOEING747 747230B 1384889NM NR 3 BRAKE LOOSE A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23508MC 21644 NR 3 BRAKE LEAK, FOUND ON PRE-FLIGHT. TIGHTENED NR 3 BRAKE LINES AS PER MM 32-41-03, LEAK CHECK OK. 2L74 4F A20WE 20040622001422004062200142NM 2004 6 22 P5CA0401097 120040525A2121 FAN BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL E/E BAY MALFUNCTIONED A P5CAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 WP23451PA 30809 MULTIPLE CMC STATUS MESSAGES PRIOR TO DEPARTURE, ZONE TEMPRATURE, E/E COOLING & GEAR MONITORING. GEAR MONITORING MESSAGE CLEARED, DEFERRED ZONE TEMPERATURE MEL 21-61-8A, DEFERRED E/E COOLING FAN PER MEL 21-58-6. 2L74 4F4 FRTA20WE E23EA 20040622001472004062200147CE 2004 6 22 60947 120040429A3297M8182411 WIRE BEECH 1900 1900D 1154162CE MLG DAMAGED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07162YV UE162 WHEN GEAR SELECTED DOWN GEAR INDICATOR C/B POPPED. NOTIFIED DISPATCH AND DIVERTED TO DUJ. LANDED WITH 3 GREENS DOWN. NO FURTHER INCIDENT. REMOVED, REPLACED AND REPAIRED DAMAGED WIRES, CHECKS GOOD. 2L72 4T RTA24CE 20040622001782004062200178EA 2004 6 22 ASOA04347 120040514A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27824AS 7203 DURING A GROUND INSPECTION, THE RT CENTER OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED THE EXTERNAL OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040622001982004062200198WP 2004 6 22 GTIA040486 120040501A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 MAIN CABIN STA 470 CENTER FLOORBOARD IS SPONGY UNDER FOOT. FAB FLOORBOARD. INSTALLED NEW FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040622002042004062200204WP 2004 6 22 GTIA040474 120040308A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE DENTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 DENT AT FS 1212 BETWEEN LONGERONS 26R-28R. REMOVED LOWER FUSELAGE SKIN FROM STA 1202 TO 1279, L26L TO L26R. FABRICATED 33 DOUBLER. FABRICATED 5 DOUBLER. FABRICATED 9 EA LONGERON STRAPS. FABRICATED 79-81 DOUBLERS. INSTALLED NEW SKIN AFT CARGO DOOR AFT CORNER REPAIR DOUBLERS 79, 81, 9 EA LONGERON STRAPS, 9 AND 5 DOUBLERS IAW EA 5330-0406. 2L72 4F4 F A6WE E2EA 20040622002142004062200214WP 2004 6 22 GTIA040481 120040504A3350 LENS DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE EMERGENCY LIGHT BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 CABIN SIDEWALL PANEL LT NR 18 EMERGENCY LIGHT LENSE IS MISSING. EMERGENCY LIGHT ASSY IS BROKEN AT THE BOTTOM. REPLACED LT NR 18 SIDEWALL PANEL EMERGENCY LIGHT ASSY. 2L72 4F4 FRTA6WE E2EA 20040623000192004062300019WP 2004 6 23 GTIA040495 120040505A5321 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT OB FLOORBOARD PANEL STA 1079-1117 PANEL DELAMINATED. BONDED FLOORBOARD. 2L72 4F4 FRTA6WE E2EA 20040623000722004062300072EU 2004 6 23 ASOA04370 120040307A5315 FLOORBEAM AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE FLOORBEAM AT FRAME 36 NEAR THE SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01. AIRCRAFT WAS RELEASED FROM C-CHECK ON MARCH 21, 2004. 2H72 4T4 TRT E20NE 20040623000782004062300078 2004 6 23 GTIA040510 420040521A2565 COVER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE ESCAPE SLIDE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23803NK 1774 48087 R1 DOOR SLIDE PACK FELL TO THE GROUND AND HOUSING IS CRACKED. REMOVED AND REPLACED R1 DOOR SLIDE PACK. 2L72 4F4 F A6WE E2EA 20040623000802004062300080 2004 6 23 GTIA040513 420040521A2565 SLIDE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE R1 DOOR UNSECURE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23815NK 49415 R1 SLIDE PACK LANYARD NEEDS TO BE SECURED. RE-ATTACHED R1 SLIDE PACK LANYARD. 2L72 4F4 FRTA6WE E2EA 20040623000822004062300082WP 2004 6 23 GTIA040499 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 LT IB SEAT TRACK FS 1098 THRU 1231 CORRODED AND GOUGED. REMOVED LT IB SEAT TRACK. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND SPLICE. 2L72 4F4 FRTA6WE E2EA 20040623000842004062300084WP 2004 6 23 GTIA040536 120040501A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 AFT PIT STA 1150 L29R INTERNAL SKIN DOUBLER CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED DOUBLER. 2L72 4F4 FRTA6WE E2EA 20040623000862004062300086WP 2004 6 23 GTIA040509 120040430A5320 CUSP WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 AFT CARGO STA 1287-1309 RT LOWER CUSP WEB CORRODED. UPON FURTHER EVALUATION, FOUND A CRACK IN CUSP WEB AT STA 1280. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA6WE E2EA 20040623000872004062300087WP 2004 6 23 GTIA040502 120040430A5751 WEDGE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE AILERON CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT WING AILERON BETWEEN TRIM TAB AND CONTROL TAB CRACKED AT WEDGE TRAILING EDGE. REPAIRED CRACK USING 181 GLASS CLOTH. 2L72 4F4 FRTA6WE E2EA 20040623000992004062300099EU 2004 6 23 ASOA04356 120040428A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK, THE INTERCOSTALS BETWEEN FRAMES 38 AND 39 ON BOTH LEFT AND RT SIDES WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED INTERCOSTALS IAW SRM 512501 AND 512500. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040623001012004062300101EU 2004 6 23 ASOA04354A2 120040428A5320S5367800821602 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27532AS 458 DURING C-CHECK, CORROSION BEYOND LIMITS WAS FOUND ON THE LT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 40. OUT OF LIMITS CORROSION WAS ALSO FOUND ON THE RT SIDE FLOOR SUPPORT BETWEEN FRAMES 39 AND 41. MAINTENANCE REMOVED AND REPLACED THE CORRODED SUPPORTS ON THE LT AND RT SIDES IAW SRM 512502 AND 512501 RESPECTIVELY. AIRCRAFT WAS RELEASED FROM C-CHECK MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040623001062004062300106EU 2004 6 23 ASOA04359 120040429A5321 FLOOR PANEL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK INSPECTION, THE FLOOR WEB AT THE FORWARD CARGO DOOR ENTRANCE AT FRAME 13 TO 17 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR WEB IAW SRM 533780 AND 512500. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040623001112004062300111CE 2004 6 23 61638 120040522A32601013841377 UPLOCK SWITCH BEECH 1900 1900D 1154162CE LT MLG MALFUNCTIONED A AMWAO OTHER J WARNING INDICATION CLCLIMB 1 CE07133YV UE133 AFTER TAKEOFF FROM CLT TO LWB, GEAR WAS SELECTED UP, GEAR HANDLE INTRANSIT LIGHT REMAINED ILLUM. AIRCRAFT THEN RETURNED TO CLT. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR UPLOCK SWITCH. P/N 101-384137-7, S/N 1170. 2L72 4T RTA24CE 20040623001162004062300116NM 2004 6 23 PCAA0406216 120040603A554072760059101 BRACKET DHAV DHC8 DHC8102 2809003NM RUDDER ACTUATOR CRACKED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13837EX35078 217 WHILE AIRCRAFT WAS REMOVED FROM OPERATION SITTING AT MAINTENANCE BASE THE RUDDER ACTUATOR WAS NEEDED FOR USE ON ANOTHER AIRCRAFT. DURING REMOVAL OF ACTUATOR IT WAS NOTICED THAT THE ACTUATOR ADAPTER MOUNT BRACKET WAS CRACKED TWO THIRDS THE WAY AROUND THE MOUNT ITSELF. MOUNT WILL BE REPLACED. 2H72 4T RTA13NM 20040623001172004062300117EA 2004 6 23 COMA0470049 120040608A32514480000501 ECU CNDAIRCL600 CL6002C10 1390015EA NLG STEERING MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01390CA2684 10106 FLIGHT 5665 NLG STEERING INOP CAUTION MESSAGE. REPLACED THE NWS ECU. 2L72 4F RTA21EA 20040623001242004062300124EA 2004 6 23 SWIA200413371 120040531A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07463SW 7820 GEAR/FLAP EICAS INDICATIONS CAME ON INTERMITTANTLY FROM TAKEOFF THROUGH CLIMBOUT. REMOVED AND REPLACED FECU IAW 27-51-05. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20040624000062004062400006EA 2004 6 24 COMA0460347 120040602A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYS MALFUNCTIONED A COMAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 SO01710CA14976 7241 FLIGHT 5556 LANDING GEAR DISAGREE WARNING. REPLACED THE NR 3 SYSTEM HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20040624000322004062400032WP 2004 6 24 UPS04842534 120040504A53405641007501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, LT STATION 781 FITTING IS CRACKED AT LONG 17L. REMOVED, FABRICATED AND REPLACED FITTING IAW UPS ENGINEERING FILE NUMBER DC8-53-20416A, AND SAA SK 730-108-A AND DWG 5641007. 2L74 4F RT4A25 20040624000342004062400034NM 2004 6 24 UPS04M42511 120040302A5754 SLAT TRACK DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, LT WING SLAT TRACK NR 16, 11B WEB SUSPECTED CRACK. HFEC INSPECT FOUND CRACK APPROX .375 INCH LENGTH. REMOVAL CUTOUT FOR ACCESS AS PER 27-80-32 R45. CRACK I/B WEB RIB AT LT WING SLAT TRACK NR 16 REMOVED AS PER SRM 51-33-01 & 51-35-01 V2R34. PICKED UP HOLES & REINSTALLATION CUTOUT AS SRM 51-33-01 & 51-35-01 V2R34. LT WING NR 16 SLAT TRACK REINSTALLED AS PER MM 27-80-32 R45. 2L73 4F RTA22WE 20040624000362004062400036NM 2004 6 24 UPS04M42513 120040312A5510 BARREL NUT DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE:C, HORIZONTAL STAB RT BARREL NUT HOLE NR 06 FOUND CORROSION AT BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 V2R34, MAT REMOVED 0.018. SLEEVE & BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. SLEEVE & BUSHING HOLE REWORKED PER EN-1153-04. BARREL NUT REPAIR PER EN-1153-04 (UPS ENGR) & EO MD11-5510-19409-G. 2L73 4F RTA22WE 20040624000542004062400054NM 2004 6 24 SWAA041738 120040621A5320BAC15171489 STRUCTURE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND ZEE AT BS 270, BBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED ZEE PER SRM. 2L72 4F RTA16WE 20040624000572004062400057NM 2004 6 24 UPS04M42518 120040328A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 28 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.048 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040624000582004062400058CE 2004 6 24 61334 120040512A1430 SCREW BEECH 1900 1900D 1154162CE AIRSTAIR DOOR LOOSE A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07142ZV UE142 AT DFW AIRSTAIR DOOR WILL NOT CLOSE SECURE. NO FURTHER INCIDENT. RESECURED LOOSE SCREWS ON COVER PLATES. 2L72 4T RTA24CE 20040624000622004062400062EA 2004 6 24 COMA0460386 120040620A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD SYSTEM FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01934CA12421 7042 FLIGHT 5252 DURING CLIMBOUT OF CVG RECEIVED A GEAR DISAGREE CAUTION, CREW DECLARED AN EMERGECY AND RETURNED TO THE FIELD. REPLACED THE NR 3 RESERVOIR. 2L72 4F RTA21EA 20040624000652004062400065EA 2004 6 24 COMA0470053 120040621A32416007302 CONTROL BOX CNDAIRCL600 CL6002C10 1390015EA BRAKE SYS FAULTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01378CA3461 10097 FLIGHT 5661 DURING TAKEOFF ROLL RECEIVED A BRAKE OVERTEMP WARNING ON ED1, ABORTED AND RETURNED TO THE GATE. REPLACED THE ANTI SKID CONTROL UNIT. 2L72 4F RTA21EA 20040624000672004062400067EA 2004 6 24 COMA0460336 120040528A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 WORK IN PROGRESS ON DMI 800602, LOWER LT WING PLANK HAS .625 INCH CRACK ALONG WS 148. REPAIRED LOWER LEFT WING PLANK WS 148.019L PER REO 601R-57-21-130. 2L72 4F RTA21EA 20040624000912004062400091EA 2004 6 24 COMA0460358 120040608A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01957CA 7109 FLIGHT 5301 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED MAINT ON DOOR WARNING SYSTEM PER MEL. 2L72 4F RTA21EA 20040624000952004062400095EA 2004 6 24 COMA0460342 120040525A323317008113 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA LT MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01818CA10424 7408 FLIGHT 5506 GEAR DISAGREE WARNING, LT MLG INDICATES DOWN WHEN LANDING GEAR IS UP. REPLACED THE LT MLG SIDE STAY ACTUATOR. 2L72 4F RTA21EA 20040624000962004062400096EU 2004 6 24 CX7A194J0431 120040530A26131734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE SATURATED A CX7AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03302CE 340B193 RIGHT TAILPIPE HOT LIGHT CAME ON MULTIPLE TIMES BETWEEN 3-10 MINUTES AFTER TAKEOFF. 2L72 4T RTA52EU 20040624001002004062400100NM 2004 6 24 MWEA040083 120040601A2760 WARNING LIGHT BOEING717 717200 1383700NM SPOILER FALSE INDICATIONA MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31907ME 00177 55171 SPOILER INBOARD FAIL ALERT. PERFORMED FIM 27-60-805/807 SPOILER ELECTRONIC CONTROL UNIT RETURN TO SERVICE, PASSED TEST AND NO FAULTS NOTED. CLEARED SYSTEM, OPERATION CHECKED GOOD. 2L72 4F TRA6WE 20040624001012004062400101NM 2004 6 24 F3LA200400064 120040523A5414 PANEL BOEING737 7373L9 1384470NM NR 1 PYLON DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03312FL 2843 24569 DURING C-6 CHECK, INSPECTION REPORTED SCREW BROKEN ON NR 1 PYLON TOP AFT FAIRING PANEL ATTACHED TO THE WING AND A CRACK FROM THE HOLE. REPLACED PANEL PER SRM 51-40-02, SRM 51-40-08 AND MM 28-11-00. PERFORMED LEAK CHECK. NO LEAKS NOTED. 2L72 4F RTA16WE 20040624001112004062400111NM 2004 6 24 QXEA200400388 120040528A5542 SKIN BOMBDRDHC8 DHC8401 1390041NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - A THREE INCH CRACK WAS NOTED IN THE TRAILING RUDDER SKIN AT APPROXIMATELY STA 35. 202.276 AT RIB 30. MAINTENANCE REPAIRED THE TRAILING RUDDER IAW RD 8/4-55-075. 2H72 4T RTA13NM 20040624001152004062400115EA 2004 6 24 SWIA200413359 120040418A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FORWARD BULKHEAD TO STRINGER 21 LT, ATTACH CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED CLIP IAW CRJ 200 SRM CH 51-42-06. 2L72 4F RTA21EA 20040624001172004062400117EA 2004 6 24 SWIA200413361 120040527A3320 BALLAST CNDAIRCL600 CL6002B19 1900309EA GALLEY LIGHT MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07591SW 7079 STRONG ELECTRICAL ODOR IN COCKPIT DURING AND RIGHT BEFORE ENGINE START. ODOR GOT STRONGER AFTER TAKEOFF, THEN ALMOST WENT AWAY, THEN ON TAXI-IN THE ODOR WAS STRONGEST. REMOVED AND REPLACED GALLEY LIGHT BALLAST AND GALLEY EXHAUST FAN. 2L72 4F RTA21EA 20040624001232004062400123EA 2004 6 24 COMA0460368 120040611A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01988CA24407 7204 FLIGHT 5282 EMERGENCY LIGHTS WILL NOT TEST. REPLACED THE EMERGENCY BATTERIES. 2L72 4F RTA21EA 20040624001262004062400126NM 2004 6 24 TSAA0434043 120040601A3411 PITOT TUBE BOEING737 7372X6C 1384552NM AIRSPEED CONTAMINATED A TSAAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 WP13817AL 23292 CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS READ 20 KTS DIFFERENCE. RETURNED TO HNL. REMOVED FOD FROM PITOT TUBE, SYS OPS & LEAK CHECK GOOD IAW AMM 34-11-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040625000232004062500023NM 2004 6 25 UPS04M42531 120040603A5610 WINDOW DOUG MD11 MD11F 3023600NM COCKPIT LEAKING A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01271UP INSPECTION TYPE:N/A 57 MIN INTO FLIGHT, FELT EARS POP AND LOUND NOISE IN COCKPIT FROM F/O WINDOW. F/O WINDOW RE-RIGGED IAW FIM 56-12-01. CLEARANCES SPECIFIED ARE WITHIN LIMITS. LOADS SPECIFIED ARE WITHIN LIMITS. CANNON PLUG ON F/O CLEAR VIEW DEFOG RESEATED. 2L73 4F RTA22WE 20040625000332004062500033NM 2004 6 25 UPS04M42464 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 27 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1160-04 (UPS ENGINEERING FILE NR MD 11-55-20042). 2L73 4F RTA22WE 20040625000382004062500038NM 2004 6 25 UPS04M42469 120040401A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 25 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000452004062500045WP 2004 6 25 UPS04842479 120040512A531051242520 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, CORROSION ON FUSELAGE SKIN AND AROUND FASTENER HOLES FS 300-320 L29L. REMOVED CORROSION AND FOUND OUT OF LIMITS ORIG THICKNESS .063 THINNEST SPOT .034 720 IAW DC8 SRM 51-1-8 AND 53-2-0. FAB, ALODINED, PRIMED AND INSTALLED 31 REPAIR ANGLE IAW DC8 SRM 53-2-2 FIG 10, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20040625000462004062500046WP 2004 6 25 UPS04842480 120040523A53109754913 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, FWD BAG PIT, L28L CORROSION BETWEEN FS 320 & 340. REMOVED CORR FROM L28L SIDE OF VERTICAL LEG AT FS 325, 330 & 335. ORIG THICKNESS VERTICAL LEG .063 IAW DAC DWG 9754913 MAT'L REMOVED .015, AMT REMAINING .048. OUT OF LIMITS. FAB -31 REPAIR ANGLE AND SHIM. ALODINED AND PRIMED. INSTALLED IAW DC8-SRM 51-1-20D. 2L74 4F RT4A25 20040625000482004062500048WP 2004 6 25 UPS04842482 120040510A53105616666185 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, MAIN CABIN L-2 DOOR TORQUE BOX AFT EDGE INT STRUCTURE SHEAR TIE GOUGED. BLENDED GOUGED AREA. ORIG MAT THICKNESS .080 DAC DWG 5616606. REMOVED INTERCOSTAL 8 & 9. REC'D PART FROM HEAT TREAT IN T6 CONDITION IAW DAC DWG 5616666 AND FAB NEW PART. ALODINED AND PRIMED IAW 51-1-8. OPEN WEB TORQUE BOX FOM. INSTALLED NEW PART ON L-2 TORQUE BOX IAW DC8 SRM 51-1-20-D AND 51-1-21. 2L74 4F RT4A25 20040625000492004062500049WP 2004 6 25 UPS04842483 120040507A534097540226503 FITTING DOUG DC8 DC873F 302199FWP FLOORBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, FLOORBEAM END FITTING AT STA 260 RT CUSP EXFOLIATED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-21, 51-1- 24. 2L74 4F RT4A25 20040625000502004062500050WP 2004 6 25 UPS04842484 120040507A534752772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, FWD PIT STA 260-280, RBL, WL 0, CORROSION EMINATING, FROM BENEATH NUT PLATES AND NUT PLATES CORRODED FLOOR PLK B6014. REMOVED CORROSION FROM SEAT TRACK. FOUND TO BE OUT OF LIMITS MAT ID FOR SEAT TRACK IS 52772660 7075-T6 EXT PO SP0916641. MAT ID FOR SEAT TRACK SPLICE IS 7075-T6 (A&B PLATES) C PLATE IS 7075-T6 100 PO 4412585 FAB SPLICE A, B, C, 2 EACH, D 2 EACH, E 2 EACH, LOCATED & DRILLED HOLES REC'D UPS SPLICE PER EO DC853B003. ALODINED A-E SPLICES & PRIMED. 2L74 4F RT4A25 20040625000522004062500052NM 2004 6 25 UPS04M42486 120040401A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 13 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000532004062500053NM 2004 6 25 UPS04M42487 120040319A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 36 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.070 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1094-04 (REF UPS ENGINEERING FILE NR 55-20019). 2L73 4F RTA22WE 20040625000542004062500054NM 2004 6 25 UPS04M42488 120040326A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 11 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.048 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040625000562004062500056NM 2004 6 25 UPS04M42490 120040401A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 34 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (REF UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040625000572004062500057NM 2004 6 25 UPS04M42491 120040325A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, BARREL NUT HOLE NR 10 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.035 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000582004062500058NM 2004 6 25 UPS04M42492 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 01 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.030 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1072-04 (REF UPS ENGINEERING FILE NR MD11-55-20024). 2L73 4F RTA22WE 20040625000612004062500061NM 2004 6 25 UPS04M42495 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 17 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MATERIAL REMOVED 0.050 INCH FOUND WITHIN LIMITS PER EO MD11-5510-19409-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR CARRIED OUT WITHIN LIMIT PER EN1091-04 (REFER UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000622004062500062NM 2004 6 25 UPS04M42496 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 24 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.006 INCH FOUND WITHIN LIMIT PER EO MD11-5510-194 09E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1082-04 (REFER UPS ENGINEERING FILE NUMBER MD11-55-20041). 2L73 4F RTA22WE 20040625000672004062500067NM 2004 6 25 UPS04M42501 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 20 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19 409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1092-04 (REFER UPS ENGINEERING FILE NUMBER MD11-55-20039). 2L73 4F RTA22WE 20040625000682004062500068NM 2004 6 25 UPS04M42502 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 09 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH WITHIN LIMIT PER EO MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1073-04 (REFER UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000702004062500070NM 2004 6 25 UPS04M42504 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 23 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE BLENDED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.006 INCH FOUND WITHIN LIMITS PER EO MD11-5510-1 9409-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1093-04 (REFER UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000712004062500071NM 2004 6 25 UPS04M42505 120040328A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 25 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMTS PER EO MD11-5510-194 09-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1123-04 (REFER UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000742004062500074NM 2004 6 25 UPS04M42508 120040328A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 34 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.085 INCH DEEP FOUND WITHIN LIMITS PER EN1120-04. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1120-04 (REFER UPS ENGINEERING FILE NR MD11-55-20042). 2L73 4F RTA22WE 20040625000762004062500076NM 2004 6 25 AWXA200400586 120040527A531369353509 STRINGER CLIP BOEING737 7373G7 1384595NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 500, STR 28 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500, STR 28 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35350-9; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12, PG 1, 38, & 45. 2L72 4F RTA16WE 20040625000772004062500077EU 2004 6 25 AWXA200400587 120040522A5210FE240004 CYLINDER AIRBUS320 A320231 3930325EU R2 DOOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW14792 099 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE R-2 DOOR DAMPER CYLINDER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE R-2 DOOR DAMPER CYLINDER IAW AMM TASK 52-13-14-000-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040625000782004062500078EU 2004 6 25 AWXA200400588 120040522A5210FE174004 CYLINDER AIRBUS320 A320231 3930325EU L1 DOOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW14792 099 MCN - EMERGENCY EVACUATION - DURING C-03 CHECK THE L-1 DOOR DAMPER CYLINDER WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER CYLINDER IAW AMM TASK 52-11-14-000-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040625000812004062500081EA 2004 6 25 SWIA200413383 120040528A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 LEFT WING LWR WING PLANK IS CRACKED WS 148.019. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-57-21-130 REV. E AND REO 601R-57-21-131 REV. NC. 2L72 4F RTA21EA 20040628000012004062800001NM 2004 6 28 04134452 120040514A3350363674 LAMP DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27452FJ 3214 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE FLEX LAMP WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040628000022004062800002EA 2004 6 28 04135652 120040514A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27652BR 7429 DURING INSPECTION THE LEFT HAND NR 4 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000032004062800003EA 2004 6 28 04145708 120040524A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000042004062800004NM 2004 6 28 041334101 120040512A3350 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27410FJ 3165 DURING INSPECTION THE LEFT REAR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE BATTERY WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA55NM 20040628000062004062800006EA 2004 6 28 04129630 120040508A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27630BR 7255 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000072004062800007EA 2004 6 28 04129653 120040508A3350OL3071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27653BR 7438 DURING INSPECTION TWO LAMPS IN THE EMERGENCY ESCAPE PATH LIGHTING WERE FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000082004062800008EA 2004 6 28 SWIA200413463 120040615A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07452SW 7716 CRACKED INTERCOSTAL AT STA 484.00 LBL 36. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. A. 2L72 4F4 FRTA21EA E15NE 20040628000092004062800009EA 2004 6 28 SWIA200413464 120040615A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07452SW 7716 FS 625 RIGHT ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20040628000102004062800010EA 2004 6 28 SWIA200413465 120040615A5315 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07452SW 7716 FS 621 RIGHT FLOOR SUPPORT ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV. B. 2L72 4F RTA21EA 20040628000112004062800011EA 2004 6 28 SWIA200413466 120040519A5310 ANGLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR FR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 FS 700 AFT EQUIPMENT COMPARTMENT DOOR CUTOUT RIGHT ANGLE CRACKED. REPAIRED ANGLE IAW CRJ SRM 51-31-00 PAGE 3 TO PAGE 5, 51-40-11, 51-42-06, 51-23-00. 2L72 4F RTA21EA 20040628000122004062800012EA 2004 6 28 SWIA200413467 120040521A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ANGLES (2) REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00, AND RII 53-401. 2L72 4F RTA21EA 20040621001082004062100108NM 2004 6 21 CALA0400530 120040612A335020131A BATTERY PACK BOEING737 7373T0 1384582NM SEATS 14-20 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2777303 23354 INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE ON SEATS 14-20. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040621001132004062100113NM 2004 6 21 CALA0400535 120040613A533055C30802 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769348 23586 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 747, STRINGER 23L. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 229. 2L72 4F RTA16WE 20040621001142004062100114NE 2004 6 21 NAFA200400004 220040326A7421AUBURN283 SPARK PLUG DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 11 CYLINDER SHORTED I N32BEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL017780B410 410 45372 P35317 NR 1 ENGINE FEATHERED DUE TO NR 11 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED BOTH FRONT AND REAR SPARK PLUGS ON NR 11 CYLINDER. CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20040621001182004062100118 2004 6 21 HNAA0400055 420040519A3442071131900 RADAR DHAV DHC8 DHC8102 2809003NM WX SYSTEM INOPERATIVE A HNAAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 EA07940HA 156 WX RADAR INOP, AIR TURNBACK FROM 20 MILES OUT, DISPATCH DETERMINED MUST HAVE FOR CVG FLT. REMOVED AND REPLACED RT, OPS GOOD. 2H72 4T RTA13NM 20040621001722004062100172NM 2004 6 21 ASMF200406005 120040605A27814952287503 SWITCH DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE TE FLAPS FAILED W ASMFK NONE N FALSE WARNING ININSP/MAINT 1 SW23158PL2771 49761 DURING TRANSIT CHECK, CAPTAIN REPORTED (AUTO SLAT FAIL) LIGHT TURNED ON IN FLIGHT. DURING MAINTENANCE REVISION LIGHT TURNED ON AT 11 AND 15 FLAPS DEGREES. TEST IN STALL COMPUTER WAS PERFORMED AND (AUTO SLAT FAIL) LIGHT TURNED ON IN STALL COMPUTER NR 2, STALL COMPUTER WAS REPLACED AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR AND SWITCH S1-467 AND TX FLAP HANDLE T20-10 WERE REPLACED AND ADJUSTED IAW MM 27-80-07, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20040621001772004062100177NM 2004 6 21 QXEA200400362 120040524A5541 RIB BOMBDRDHC8 DHC8401 1390041NM RUDDER DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 PDX - RIGHT HAND UPPER PORTION OF THE RUDDER HAS A SMALL CREASE BETWEEN RIB. REPAIRED IAW HORIZON AIR EA 6-27-161. 2H72 4T RTA13NM 20040621001792004062100179NM 2004 6 21 AWXA200400535 120040518A3350BR9660105 LIGHT BOEING737 73733A 1384673NM EMERGENCY EXIT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY EXIT LIGHT JUST FORWARD OF THE L-2 DOOR IN THE LT AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT AFT GALLEY EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040621001802004062100180EU 2004 6 21 AWXA200400536 120040507A5753D57570087201 SKIN AIRBUS320 A320231 3930325EU TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK FOUND THE LT INBOARD FLAP DELAMINATED AT THE UPPER INBOARD END BETWEEN WS 700 AND WS 707 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF LT INBOARD FLAP UPPER SKIN BETWEEN WS 700 AND WS 707 LT; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211. 2L72 4F RTA28NM 20040621002062004062100206NM 2004 6 21 AWXA200400517 120040427A5320652072344 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A .3125 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT INTERCOSTAL AT BS 494, STR 24 RT. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 494, STR 24 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-20723; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20040621002082004062100208NM 2004 6 21 AWXA200400519 120040430A53136561777503 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND 2.1875 INCH CRACK IN STRINGER 14 LT AT BS 359. MAINTENANCE REMOVED CRACKED STRINGER 14 LT AT BS 359; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER PER DWG 65-61777; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20040622000052004062200005WP 2004 6 22 ASAA0480299 120040420A532199365511 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 15 TO RBL 22 FIBERGLASS TORN OFF. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M) 2L72 4F RTA6WE 20040622000082004062200008WP 2004 6 22 ASAA0480200 120040402A532199366391 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING HV CHECK, FOUND PAX CABIN FLOOR PANEL HAS TORN FIBERS AT FS 826-886. REPLACED PANEL PER SRM 53-05. (M) 2L72 4F RTA6WE 20040622000162004062200016WP 2004 6 22 ASAA0480293 120040420A53305911410531 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING C-CHECK, FOUND DENT LEFT SIDE FUSELAGE SKIN AT FS 313 AND LONGERON 22L D= 3 INCHES BY =.100 DENT IS LESS THAN 1 INCH FROM LONGERON 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-04 AND 51-30-5. (M) 2L72 4F RTA6WE 20040622000192004062200019NM 2004 6 22 ASAA0410264 120040514A531065671406 BEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON LONGITUDINAL BEAM OUT OF LIMITS. REPLACED WITH NEW LONGITUDINAL BEAM. (M) 2L72 4F A16WE 20040622000212004062200021WP 2004 6 22 ASAA0480273 120040412A531099360737 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND DURING HV CHECK, SHEAR TIE CORRODED AT FS 636. REPLACED SHEAR TIE PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040622000222004062200022WP 2004 6 22 ASAA0480274 120040412A53219936548501 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DISBONDING AT SUPPORTS AT FS 200-256. BOND-REPAIRED PER MM 25-00-00. (M) 2L72 4F RTA6WE 20040622000352004062200035NM 2004 6 22 ASAA0410262 120040515A531065465507 FAILSAFE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON BS 787 FRAME FAIL/SAFE CHORD RBL 20 WL 155. REPAIRED FAIL/SAFE CHORD. (M) 2L72 4F A16WE 20040622000512004062200051WP 2004 6 22 DHL2004803540 120040422A5730 SKIN DOUG DC8 DC873 302199CWP RT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 OUTER PLATING CORROSION DAMAGE TO RT INNER WING CENTER L/E SLOT UPPER SIDE AROUND STA XFS 422.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-8 DWG V43-R08. PERFORMED NDT INSP IAW DC8 NDT SPM PART 6-10-01.001. FABRICATED FILLER (7075-T6 0.063) AND DOUBLER (7075-T6 0.071) IAW ED EDV43-8, DWG V43-R08. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER, DOUBLER AND NEW FASTENERS. 2L74 4F RT4A25 20040622000572004062200057WP 2004 6 22 IXXA0400028S 120040225A5730 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE INSPECTION RIGHT WING CTR L/E UPPER SKIN SURFACE CORRODED (STA XFS 341.500-416.500) MAJOR REPAIR. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D, REMOVED CORROSION FROM UPPER SKIN SURFACE OF LT WING CIR L/E IAW DC8 SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW DC8 SRM 51-2-1 PG 11-12, REMOVED DAMAGED SKIN SEGMENT IAW DC8 SRM 57-2-1 PG 44, FABRICATED DOUBLER IAW DC8 SRM 57-2-1 PG 44, CLEANED, TREATED AND PRIMED AREA AND DOUBLER INNER SIDE IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622000582004062200058WP 2004 6 22 IXXA0400029S 120040306A5730 SKIN PANEL DOUG DC8 DC873F 302199FWP RT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION RT WING INBD VANE SLOT UPPER SKIN HAS ELONGATED HOLES AT STA XS 247.000 (MAJOR REPAIR). REPAIR IS ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-3-3 FIG 10 PAGE 22. REMOVED DETERIORATED SKIN IAW DC8 SRM 51-3-0 PAGE 1, SRM 51-1-21 PAGE 1. FABRICATED NEW SKIN IAW DC8 SRM 57-3-3 PAGE 22 FIG 10, CLEANED TREATED AND PRIMED AREA & SKIN INTERIOR IAW DC8 SRM 51-1-83. INSTALLED NEW SKIN IAW DC8 SRM 51-3-0, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20040622000692004062200069NM 2004 6 22 AWXA200400542 120040501A53136545774 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER 20 LT AT BS 817. MAINTENANCE CUTOUT CORRODED SECTION OF STRINGER 20 LT AT BS 817 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A HAT SECTION, CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 201, PG 201-207. 2L72 4F RTA16WE 20040622000702004062200070NM 2004 6 22 AWXA200400543 120040505A532065524576 PAN BOEING737 7373G7 1384595NM CABIN FLOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON MAIN CABIN FLOOR WEB (DRIP PAN) BETWEEN BS 1016 AND BS 1029, RBL 45 AND RBL 55. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR WEB FROM BS 1016 TO BS 1029, RBL 45 TO RBL 55; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13 FIG 1. 2L72 4F RTA16WE 20040622000872004062200087EU 2004 6 22 AWXA200400531 120040507A5753D57570087200 SKIN AIRBUS320 A320231 3930325EU TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28636AW 098 MCN - MAJOR REPAIR - DURING C-03 CHECK RT INBOARD FLAP LOWER INBOARD REPAIR WAS FOUND DELAMINATED IN 3 PLACES. MAINTENANCE REMOVED EXISTING REPAIR AND CUT OUT DAMAGE IN RT INBOARD FLAP AT RIB 3 + 5 INCH; FABRICATED A CORE FILLER AND A DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211. 2L72 4F RTA28NM 20040622000902004062200090EU 2004 6 22 AWXA200400534 120040514A3397E0261CF20 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 11 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28653AW 1003 DURING P-09 CHECK FOUND A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED THE BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040622001032004062200103 2004 6 22 SWAA041726 420040620A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040622001172004062200117NM 2004 6 22 374PA0010 120040517A5330 SKIN BOEING737 73736M 138443BNM FUSELAGE DENTED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05374PA 28333 DENT IN FUSELAGE SKIN AFT OF L1 DOOR AT STA 400 BETWEEN STR 17 LT AND STR 18 LT. REPAIRED AREA PER SRM 53-00-01 AND EA 53-120. 2L72 4F RTA16WE 20040622001232004062200123WP 2004 6 22 DHL2004803548 120040516A57115615058505 SPAR CAP DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 BOLT HOLE OUTBD END OF LT WING INBD LWR AUX SPAR CAP WITH 1.000 AND 2.250 LENGTH CRACKS IN IT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED CRACKED LT INBD LWR AUX SPAR CAP IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW INBD AUX SPAR CAP IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1, SRM 51-3-1 (TORQUE). 2L74 4F RT4A25 20040622001242004062200124WP 2004 6 22 DHL2004803526 120040403A5751 SKIN DOUG DC8 DC873 302199CWP RT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RT WING AILERON INBD L/E FASTENER HOLE, SKIN CRACKED 0.500, STA XA 500.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-8-1 PAGE 2 SRM 57-1-0 PAGE 1. REMOVED CRACKED PLATE IAW SRM 51-1-21, SRM 51-3-0 PAGE 1. FABRICATED NEW PLATE (7075 T6 AL 0.040) IAW SRM 57-8-1 PAGE 1. CLEANED, TREATED AND PRIMED AREA AND NEW INNER PLATE IAW SRM 51-1-8B, INSTALLED NEW PLATING IAW SRM 51-1-21 PAGE 1, SRM 51-3-0 PAGE 1. 2L74 4F RT4A25 20040622001292004062200129WP 2004 6 22 DHL2004803513 120040323A5751 STRUCTURE DOUG DC8 DC873 302199CWP RT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 RT WING OTBD AILERON L/E PLATING CRACKED 0.250 AROUND STA XA 646.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-8-01 FIG 4 PG 9. REMOVED CRACKED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NOSE PLATING (2024-T3 0.032) IAW DC8 SRM 57-8-01 FIG 4 PG 09. CLEANED, TREATED AND PRIMED NOSE PLATING INTERNAL PART IAW DC8 SRM 51-1-8B. INSTALLED NOSE PLATING IAW DC8 SRM 51-1-21 PG 1, SRM 57-8-01 PG 9. REBALANCE MOMENT 3324 LBS/IN FOUND WITHIN ALLOWABLE LIMITS IAW SRM 51-4-3 PG 1-2-3. 2L74 4F RT4A25 20040622001322004062200132WP 2004 6 22 DHL2004803516 120040319A5531 FRAME DOUG DC8 DC873 302199CWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 VERTICAL STABILIZER L/E FORMER CRACKED 0.500 (LT SIDE) AT ZFS 86.000. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3AL 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 55-2-0 PG 7-8, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040622001362004062200136NE 2004 6 22 DHL2004809006 220040515A7200 SENSOR DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE CDP CLOGGED A DHLAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01809DH 46047 693498 NR 4 ENG ROLLED BACK AT 0300Z; WINDMILL N2 = 12 PERCENT, N1 = 28 PERCENT, OIL PRESSURE = 3 PSI, OIL QTY = 16 QTS. FOUND RT CDP SENSOR CLOGGED. CLEARED BLOCKAGE, PERFORMED POWER RUN, OPS CHECKED SERVICEABLE. TROUBLESHOT NR 4 ENG, ENG LOSES POWER OR FLAMES OUT. PERFORMED INLET/EXHAUST VISUAL INSPECTION, CHECKED FLIGHT IDLE, CHECKED N1 ROTOR, SPECIFIC GRAVITY, CHIP DETECTORS, INSPECTED & REPLACED FUEL FILTER, & INSPECTED ENG FUEL PUMP IMPELLER ROTATION. NO DEFECTS. FUEL FILTER P/N: CH0697101552N00 REMOVED & REPLACED. LEAK CHECK REQUIRED FOR NR 4 ENG DUE TO FUEL FILTER REPLACED AND FUEL PUMP INSPECTION. GROUND RAN NR 4 ENG. FILTER AND FUEL PUMP LEAK CHECKED OK. 2L74 4F4 FRT4A25 E2GL 20040622001372004062200137NM 2004 6 22 DHL2004752003 120040515A2610 BATTERY BOEING727 727223 1384074NM SMOKE DETECTOR DISCHARGED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01752DH 22466 AFTER T/O FORWARD FIRE LOWER CARGO INDICATION, AFTER SEVERAL MINUTES LIGHT EXTINGUISHED. DEFERRED FORWARD LOWER CARGO COMPARTMENT FIRE DETECTION PER MEL 26-19, COMPLIED WITH SPECIAL PROCEDURES (FORWARD PIT EMPTY). PLACARDS INSTALLED DMI 16604. WORKING DMI 16604 AFTER T/O FORWARD FIRE LOWER CARGO INDICATION, AFTER SEVERAL MINUTES LIGHT EXTINGUISHED. REPLACED BATTERIES ON ALL FORWARD LOWER CARGO SMOKE DETECTORS NR 1 THRU 5 IAW M/M 26-16-02. DMI 16604 CLEARED. 2L73 4F A3WE 20040622001392004062200139NM 2004 6 22 DHL2004755012 120040508A2612 FIRE LOOP BOEING727 727225 1384077NM APU BAY LOOSE A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01755DH 21857 APU FIRE BELL DURING T/O. TRANSFERRED TO DMI LOG 16554 CAT-C REF MEL 49-1. PLACARD INSTALLED. RTO 40 KIAS 11 DEG C, 155,900 LBS 1000FT PA NORMAL ZONE DUE TO APU FIRE WARNING. PER BRAKING CHART NO FURTHER INSPECTION REQUIRED. DURING ROLL OUT. APU FIRE BELL ON. APU FIRE HANDLE STILL PULLED FROM PREVIOUS WRITE UP. T/S FOUND LEFT SIDE 2ND CLIP ON BEAM UNSECURE. RESECURED CLIP. FIRE LOOP NOW NOT TOUCHING OIL PSI LINE. OPS CHECKED APU & FIRE TEST C/O IAW M/M 26-15-00 NO FAULTS. REMOVED AND REPLACED APU FIRE BOTTLE & SQUIB. THIS CLEARS DMI 16554. PLACARDS REMOVED. 2L73 4F A3WE 20040622001482004062200148EU 2004 6 22 CX7A194J0425 120040520A26131734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101EU LT ENGINE CONTAMINATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03302CE 340B193 LEFT TAILPIPE HOT INDICATION CAME ON WHEN AIRCRAFT ELECTRICAL SYSTEMS WERE POWERED UP. ENGINES WERE NOT RUNNING. 2L72 4T RTA52EU 20040622001712004062200171EA 2004 6 22 ASOA04380 120040524A5610NP13932112 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT BROKEN A ASOAO OTHER O OTHER DEDESCENT 1 SO27926EV 7843 DURING DESCENT, OUT OF 25,000 FT, THE F/O`S WINDSHIELD SHATTERED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT LANDED SAFELY. 2L72 4F4 FRTA21EA E15NE 20040622001722004062200172EA 2004 6 22 ASOA04334S 120040506A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING A C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM. 2L72 4F4 FRTA21EA E15NE 20040622001822004062200182EU 2004 6 22 ASOA04377 120040521A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 1168 372 DURING A GROUND INSPECTION, THE EMERGENCY LIGHT ON THE PASENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20040622002002004062200200WP 2004 6 22 GTIA040498 120040501A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE COCKPIT DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 F/O STEERING COLUMN FLOOR PANEL DELAMINATED. REBONDED DELAMINATED AREA. 2L72 4F4 FRTA6WE E2EA 20040622002052004062200205NE 2004 6 22 ASOA04387 220040527A72615018T49P01 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE LEAKING A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27856AS AGBGEE8727087404 872708 DURING CLIMB OUT, WHEN PASSING THROUGH 14,500 FEET THE CREW NOTICED A DROP IN THE LT ENGINE OIL PRESSURE TO 27 PSI, IT THEN BEGAN FLUCTUATING BETWEEN 27 PSI AND 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE AIR TURBINE STARTER CARBON SEAL ASSEMBLY. OPERATIONAL AND OIL CONSUMPTION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. THE AIRCRAFT WAS PUT ON DAILY CHECK FOR LT ENGINE HIGH OIL CONSUMPTION DURING NEXT FIVE DAYS. 2L72 4F4 FRTA21EA E15NE 20040623000202004062300020WP 2004 6 23 GTIA040500 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 LT OB SEAT TRACK FS 1098 THRU 1231 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACK. LOCATED AND DRILLED SEAT TRACK. LOCATED ADN DRILLED SPLICE. INSSTALLED SEAT TRACK AND SPLICE. 2L72 4F4 FRTA6WE E2EA 20040623000272004062300027EA 2004 6 23 ASOA04351 120040514A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING C-CHECK INSPECTION, THE CARGO COMPARTMENT SILL PLATE BETWEEN FS 562.72 AND FS 589.00 WAS FOUND TO HAVE CORROSION IN SEVERAL AREAS, AND WAS ALSO CRACKED. MAINTENANCE IS REPAIRING THE SILL PLATE IN THE CARGO COMPARTMENT IAW REO 601R5361690 AND EO 600530095. 2L72 4F4 FRTA21EA E15NE 20040623000322004062300032 2004 6 23 ASOA04346 420040513A34526226523207 CONTROL HEAD AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE ATC INOPERATIVE A ASOAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27632AS4393 338 ENROUTE, DURING CRUISE FLIGHT, CREW NOTICED AN OILY/WATERY SUBSTANCE ON THE TRANSPONDER RADIO HEAD. SHORTLY FOLLOWING THE DIGITS DISAPPEARED AND ATC REPORTED TO THE CREW THAT THEY HAD LOST BOTH NR 1 AND NR 2 TRANSPONDERS. THEN SMOKE WAS NOTICED IN COCKPIT BETWEEN THE CONDITION LEVERS FOR APPROXIMATELY 15-20 SECONDS. ALL NON-ESSENTIAL EQUIPMENT WAS TURNED OFF, AND THE SMOKE DISSIPATED. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED, WHERE A SAFE LANDING WAS ACCOMPLISHED. MAINTENANCE REMOVED AND REPLACED THE ATC CONTROL HEAD AND RESET THE TCAS CIRCUIT BREAKER. OPERATIONAL CHECKS FOR BOTH ATC NR 1 AND NR 2 TRANSPONDERS GOOD. AC RETURNED TO SERVICE. 2H72 4T4 TRTA53EU E20NE 20040623001102004062300110EA 2004 6 23 COMA0460352 120040607A5210 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01457CA 7612 FLIGHT 5097 CABIN DOOR SQUEAL AFTER T/O. REPAIRED DAMAGED DOOR SEAL NIBS. 2L72 4F RTA21EA 20040624000012004062400001CE 2004 6 24 61517 120040518A77121143800653 INDICATOR BEECH 1900 1900D 1154162CE ENGINE TORQUE MALFUNCTIONED A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE0710675 UE10675 ON POWER UP FOR TAKEOFF LEFT HAND TORQUE GAUGE DROPPED TO ZERO. THE TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE AND MAINTENANCE CALLED. REMOVED AND REPLACED NR 1 TORQUE METER, OPS CHECK GOOD. P/N 114-380065-3, S/N 630. 2L72 4T RTA24CE 20040624000072004062400007EA 2004 6 24 COMA0460346 120040531A3411 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA CONTAMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01958CA 7111 FLIGHT 5229 IAS CAUTION DURING T/O. REMOVED WATER FROM PITOT LINES, SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20040624000082004062400008EA 2004 6 24 COMA0460372 120040615A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 CRACK FOUND RIGHT SIDE CABIN ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT BETWEEN 409 AND 128 TO 559 PRESSURE FLOOR SKIN. REPAIRED DAMAGE ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT IAW REO 601R-53-41-223. 2L72 4F RTA21EA 20040624000132004062400013EA 2004 6 24 COMA0460373 120040615A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650CB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650CB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 650CB IAW CRJ AMM 51-80-00. BOND CHECK GOOD. 2L72 4F RTA21EA 20040624000202004062400020EA 2004 6 24 COMA0460378 120040615A5315601R350313 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 CARGO BAY FLOORBEAM CAP AT LBL 27 HAS SURFACE CORROSION. REMOVED CORRODED CAP AND INSTALL NEW (P/N 601R35031) IAW CRJ SRM 51-42-06 AND 51-42-13. LOCATED AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1049 AND REO 601R-53-61-1046. 2L72 4F RTA21EA 20040624000222004062400022NM 2004 6 24 QXEA200400382 120040524A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - NR 4 SEAT TRACK HAS CORROSION ON OUTBOARD EDGE OF TRACK FLANGE AT STATION X226. REPAIRED IAW RD 8-53-1139, 8-53-1102, 8-53-4473 AND SRM 51-30-26 AND 51-40-11. 2H72 4T RTA13NM 20040624000282004062400028NM 2004 6 24 DHL2004754012 120040513A5754 ACTUATOR BOEING727 727223 1384074NM NR 4 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, NR 4 SLAT WS 405 INTERIOR RIBS AT ACTUATOR ATTACH INBOARD & OUTBOARD CRACKED RIBS. REMOVED NR 4 L/E SLAT IAW B727 M/M 27-81-11. REMOVED DAMAGE RIBS FROM NR 4 SLAT WS 405 INBOARD & OUTBOARD RIBS AT ACTUATOR ATTACH POINT IAW B727 SRM 51-30-2, LOCATED AND DRILLED NEW RIBS INBOARD & OUTBOARD NR 4 SLAT WS 405 P/N 65-17276-9, PO 4175400 AND 65-17276-11, PO 4175400 IAW B727 SRM 51-30-5. TREATED, PRIMED AREA WHERE RIBS ARE TO BE REPLACED IAW B727 SRM 51-10-2. INSTALLED NEW RIBS IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040624000312004062400031WP 2004 6 24 UPS04842530 120040503A534037799782 FITTING DOUG DC8 DC871F 302199DWP FRAME TO LONG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1, STATION 781 LONGERON TO FRAME ATTACH FITTING IS CRACKED AT LONG 18L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D. 2L74 4F RT4A25 20040624000372004062400037NM 2004 6 24 UPS04M42514 120040327A5510 BARREL NUT DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE:C, HORIZONTAL STAB LT BARREL NUT HOLE NR 03 FOUND CORROSION AT BOTTOM SIDEWALL & BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 V2R34, MAT REMOVED 0.030. SLEEVE BUSHING FAB & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE (LT NR 03) REPAIR CUTOUT PER EN-1148-04 (UPS ENGR) & MD11-5510-19409-G. 2L73 4F RTA22WE 20040624000592004062400059NM 2004 6 24 DHL2004754018 120040512A5260 AIRSTAIR BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, AFT AIRSTAIRS DENTED AT BS 1273 LBL 15. CUT OUT DAMAGED AREA AND FABBED DOUBLER FROM 2024 T3.050, PO 900980 DIM 6 X 5.25 INCH & FILLER FROM 2024-T3.040, PO 900825 DIM 2.5 X 2 INCH IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 52-10-2 FIG 4. 2L73 4F A3WE 20040624000682004062400068NM 2004 6 24 ABXA040182 120040520A79308D1467 PRESSURE SWITCH BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE LT ENGINE OIL DEFECTIVE A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23702AX 2716 22566 709644 LT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED & ENG SHUTDOWN. NR 1 ENG OIL PRESSURE LIGHT DID NOT COME ON. C/W FIM 79A-35-00-90, OIL FILTER EICAS MESSAGE WAS NOT DISPLAYED AT AIRCRAFT ARRIVAL THOUGH ENGINE WAS STILL WINDMILLING IN HEADWIND. EXAMINED NR 1 ENGINE OIL STRAINER, NO CONTAMINATION. REPLACED NR 1 ENGINE MAIN OIL SCREEN. EXAMINED THE FULL FLOW MASTER CHIP DETECTOR FOR CONTAMINATION, NONE NOTED. INSPECTED ALL ENGINE AND GEARBOX CHIP DETECTORS WITH NO CONTAMINATION NOTED IAW AMM. C/W ENGINE RUN, NO DEFECTS ON ENGINE RUN AFTER NR 1 FILTER CHANGE. REPLACED DIFFERENTIAL OIL PRESSURE SWITCH ON NR 1 ENGINE. PERFORMED ADJ TEST OF OIL BYPASS WARNING SYSTEM. CHECKED GOOD.2L72 4F4 FRTA1NM E3NE 20040624000762004062400076EA 2004 6 24 COMA0460349 120040604A5210 SKIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR GOUGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01917CA 7017 PAX DOOR SKIN GOUGED AT FS 310.00 NEAR PULL-IN LEVER. COMPLIED WITH BOMBARDIER REO 601R-52-11-507 REPAIR TO PAX DOOR AT FS 310.00. 2L72 4F RTA21EA 20040624000822004062400082EA 2004 6 24 COMA0460361 120040609A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 RIGHT HAND FS 718.00 BETWEEN STRINGERS 10-12 CRACKED. REMOVED ACCESS PANEL 423CB FROM RIGHT HAND PYLON. REMOVED HI-LOKS AND RIVETS FROM 718 FRAME IN AREA OF REPAIR. CUT THE FRAME FLANGE AND FRAME DOUBLER BETWEEN STRINGERS 10 & 11. COMPLIED WITH NDT CUTOUT IAW EO 53-027. DRILLED DOUBLERS, INSTALLED RIVETS AND HI-LOKS IAW S/B 601R-53-055. COMPLETED PARTS A AND C OF S/B 601R-53-055. INSTALLED ACCESS PANEL 423CB IAW S/B 601R-53-055. 2L72 4F RTA21EA 20040624000842004062400084WP 2004 6 24 ABXA040204 120040609A335060030451 POWER SUPPLY DOUG DC9 DC915 3022036WP CABIN INOPERATIVE A ABXAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL23927AX15 45717 ON POWER SHUT DOWN, EMERGENCY LIGHTS STAYED ON. REPLACED EMERGENCY LIGHT POWER SUPPLY WITH A SERVICEABLE UNIT IAW DC-9 MM 33-53-02-4-0001. OPS CHECKED GOOD. 2L72 4F A6WE 20040624000882004062400088EA 2004 6 24 COMA0460382 120040615A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A COMAK NONE L NO TEST ININSP/MAINT 1 SO01940CA 7048 FLIGHT 5141 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. CLEANED WIRE CONNECTION, SYSTEM TEST NORMAL. 2L72 4F RTA21EA 20040624001092004062400109WP 2004 6 24 ABXA040201 120040603A56105912290506 WINDSHIELD DOUG DC9 DC931 3022065WP RIGHT CRACKED A ABXAA UNSCHED LANDING O OTHER CRCRUISE 1 GL23906AX 47072 FIRST OFFICER'S WINDSHIELD STARTED TO ARC AT THE LOWER RIGHT CORNER, THEN CRACKED SHORTLY THEREAFTER. AIRCRAFT MADE A DIVERSION TO STL AND MADE AN EMERGENCY LANDING. REPLACED RIGHT WINDSHIELD IAW DC-9 MM 56-10-02-2-0004. REPLACED TEMP CONTROLLER IAW DC-9 MM 30-41-00-2-001. 2L72 4F A6WE 20040624001142004062400114 2004 6 24 SWIA200413358 420040527A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NR 1 YAW DAMPER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07448SW 7678 YAW DAMPER NR 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW CRJ MM 22-22-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040624001192004062400119NE 2004 6 24 SWIA200413363 220040531A7320 HMU EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A SWIAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 NM07212SW 120276 DURING CRUISE, PARTIAL POWER LOSS ON LEFT ENG. FUEL FLOW AROUND 70, TORQUE SHOWING 0 AND REDUCED T6, NP NH AND NL VALUES. NO MAP LIGHTS. REMOVED LEFT HMU AND INSTALLED A SERVICEABLE UNIT, IAW MM 73-21-00 AND RII CARD 73-301. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040625000082004062500008NM 2004 6 25 AALA20040633 120040527A2410 WARNING LIGHT BOEING767 767323 1385205NM COCKPIT ILLUMINATED A AALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21370AA 25197 CDG - LEFT GENERATOR DRIVE LIGHT WARNING ILLUMINATED. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040625000262004062500026NM 2004 6 25 UPS04M42457 120040322A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 04 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1108-4 & EN1158-04 (REF UPS ENGINEERING FILE NR MD11-55-20025). 2L73 4F RTA22WE 20040625000302004062500030NM 2004 6 25 UPS04M42461 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 08 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000312004062500031NM 2004 6 25 UPS04M42462 120040319A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 23 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000342004062500034NM 2004 6 25 UPS04M42465 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 18 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000422004062500042NM 2004 6 25 UPS04M42473 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 24 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.015 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000632004062500063NM 2004 6 25 UPS04M42497 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 29 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.030 INCH DEEP FOUND WITHIN LIMITS PER EO MD11-5 510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1089-04 (REFER UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040625000642004062500064NM 2004 6 25 UPS04M42498 120040316A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 11 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED FOR SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH DEEP FOUND WITHIN LIMITS PER EO MD11-5 510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1090-04 (REFER UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000662004062500066NM 2004 6 25 UPS04M42500 120040319A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 14 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.010 INCH FOUND WITHIN LIMITS PER EO MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1099-04 (REFER UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000692004062500069NM 2004 6 25 UPS04M42503 120040319A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 17 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMIT PER EO MD11-5510-194 09-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1097-04 (REFER UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000802004062500080EU 2004 6 25 AWXA200400590 120040522A5320D5348002069601 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK A 2 INCH CRACK WAS FOUND IN SHEAR PLATE (TRAY) BETWEEN FR 68 AND FR 69, OUTBOARD OF BEAM Y1732, AFT OF L-2 DOOR LOWER SILL. MAINTENANCE REMOVED CRACKED SHEAR PLATE FROM FR 68 TO FR 69, BEAM Y1732 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 8, 12, & 18. 2L72 4F RTA28NM 20040628000052004062800005EA 2004 6 28 04127672 120040506A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27672BR 7594 DURING INSPECTION THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000132004062800013EA 2004 6 28 SWIA200413468 120040521A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 FS 484 AT RBL 36 INTERCOSTAL IS CRACKED. ACCOMPLISHED REPAIR IAW CRJ REO 601R-53-41-059 REV A; RII 53-401. 2L72 4F RTA21EA 20040628000152004062800015NM 2004 6 28 AALA20040666 120040622A30406240664 CONTROLLER BOEING757 757223 1384957NM WINDSHIELD HEAT ARCED A AALAO OTHER A FLAME/FIRE CRCRUISE 1 SW21671AA 25336 LIM - INFLIGHT T0947 RIGHT FORWARD WINDSHIELD ARCHED AND SMALL FIRE OCURRED AT BASE OF WINDSHIELD. TURNED RIGHT WINDOW HEAT SWITCH OFF TO STOP ARCING. REPLACED WINDOW AND WINDOW HEAT CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040628000162004062800016EU 2004 6 28 AALA20040667 120040621A2822 PUMP FOKKERF28 F28MK0100 4990807EU FUEL BOOST INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW211414D 11377 STL - INFLIGHT T2041 ON CLIMBOUT L1 AND L2 FUEL PUMP LIGHTS CAME ON AND WENT OFF. LATER MAIN LEVELS BECAME INBALANCED. REPLACED L1 AND L2 BOOST PUMPS AND LEFT FILTER BYPASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040628000172004062800017NM 2004 6 28 AALA20040669 120040622A3397 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT PINCHED A AALAK NONE O OTHER ININSP/MAINT 1 SW21324AA 22325 LAX - EMERGENCY LIGHTS AT SEATS 10, 11 AND 17HJ WILL NOT EXTINGUISH AT END OF LIGHT TEST. FOUND MID GALLEY FLOOD LIGHT WIRES PINCHED BENEATH GALLEY FLOOR. REPLACED MID GALLEY FLOOD LIGHT ASSEMBLY WIRES FOR EMERGENCY LIGHTS AT SEATS 10, 11 AND 17HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628000182004062800018NM 2004 6 28 AALA20040670 120040621A3350 LIGHT BOEING777 777223 1385213NM GALLEY DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21757AN 32636 DFW - EMERGENCY LIGHT DAMAGED LEFT AND RIGHT HAND SIDE OF FORWARD GALLEY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT LEFT AND RIGHT HAND SIDE OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040628000192004062800019WP 2004 6 28 04152324 220040531A732031024766 TORQUE BRIDGE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33143 01514WP ENGINE CONTROL OUT OF BALANCE A VTZAO OTHER FR FLT CONT AFFECTED PARTIAL RPM/PWR LOSS DEDESCENT 1 EA27324UE 41017 76074 DURING DESCENT CREW REPORTED ENGINE SPEED GOING TO -3 PERCENT WITH AN ASSOCIATED AIRCRAFT YAW. THE TORQUE BRIDGES WERE SWAPPED AND UNDERSPEED FUEL CONTROL ADJUSTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA41NM E2WE 20040628000212004062800021SO 2004 6 28 SWIA200413401 120040515A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07288SW 120316 RIGHT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO RIGHT INBOARD NACELLE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B. 2L72 4T4 TRTA31SO E20NE 20040628000222004062800022SO 2004 6 28 SWIA200413402 120040515A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07288SW 120316 LEFT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO LEFT OUTBOARD NACELLE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B. 2L72 4T4 TRTA31SO E20NE 20040628000272004062800027EU 2004 6 28 AALA20040671 120040603A5320 ROLLER TRAY AIRBUS300 A300B4605R 3930308EU CARGO BAY CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2125071 514 TUL - FOUND CORROSION ON SIX INCH BY FIVE INCH SECTION OF UNDERSIDE OF ROLLER TRAY NUMBER 6 BETWEEN FRAME 57.3 AND 58 AT STATION NUMBER 3885. CORROSION HAD A DEPTH OF 0.100 INCH. REMOVED CORRODED SECTION OF NUMBER 6 ROLLER TRAY AND SPLICED IN NEW SECTION PER SRM 53-10-15-2. 2L72 4F RTA35EU 20040628000292004062800029 2004 6 28 SWIA200413471 420040618A2220 INDICATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MACH TRIM CONTAMINATED A SWIAO OTHER J WARNING INDICATION DEDESCENT 1 NM07432SW 7548 RECEIVED IAS EI MACH TRIM CAUTION MESSAGE ON DESCENT. DRAINED WATER FROM MACH SYSTEM NR 1. RESET CIRCUIT BREAKERS. OPERATIONAL CHECK OK. 2L72 4F4 FRTA21EA E15NE 20040628000322004062800032SO 2004 6 28 SWIA200413474 120040612A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07227SW1924 1924 120304 FLAP DISAGREEMENT AT FLAPS 25 DEGREES. REPLACED FLAP HANDLE WITH SERVICEABLE. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040628000372004062800037EA 2004 6 28 SWIA200413479 120040616A2760 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07407SW 7034 FLIGHT SPOILER FAULT (AMBER MESS) CAME ON AT SHORT FINAL. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW 27-61-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040628000412004062800041NM 2004 6 28 SWAA041762 120040623A2121215201 FAN BOEING737 7373T5 1384608NM E&E BAY OVERHEATED A SWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW29667SW 23063 DURING LAST 15 MINUTES OF FLIGHT, REPORTS OF SMOKE ODOR IN CABIN. TURNED OFF GASPER FAN AND RECIRCULATION FAN ODOR CONTINUED. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20040628000452004062800045SO 2004 6 28 SWIA200413435 120040611A2710 CONTROL HANDLE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AILERONS MISLOCATED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM0715732 120195 AILERON CONTROL DISENGAGE HANDLE WAS STICKING UP ABOUT .5 INCH WITH NO MAP LIGHTS ILLUMINATED. WHEN THE HANDLE WAS PUSHED IN, THE AILERON DISCONNECTED. RECONNECTED AILERON DISCONNECT PER MM 27-00-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040628000472004062800047SO 2004 6 28 SWIA200413437 120040613A27503203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07268UE6304 5847 120207 REPEATEDLY RECEIVE FLAP DISAGREEMENT WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW EMB 120 MM 27-50-09. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040628000492004062800049 2004 6 28 SWIA200413439 420040613A3418 PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07564SW 120339 STALL WARNING TEST, RED LIGHTS REMAIN ILLUMINATED AFTER TEST. REPLACED STALL WARN TEST PANEL PER MM 27-34-08, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040628000512004062800051SO 2004 6 28 SWIA200413412 120040529A5711 SPAR CAP EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07188SW 120039 LEFT WING LOWER SURFACE OUTBOARD OF LEFT NACELLE FUEL LEAKING NEAR SKIN JOINT. FOUND WING LOWER FORWARD SPAR CRACK CRACKED. REPAIRED SPAR CAP IAW EMB SRM 57-20-05. 2L72 4T4 TRTA31SO E20NE 20040628000522004062800052EA 2004 6 28 SWIA200413413 120040609A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07961SW1256 1256 7857 STAB CHANNEL 1 INOP AFTER T/O. REMOVED AND REPLACED HSTCU, OPERATIONAL CHECK GOOD IAW 27-40-00. 2L72 4F RTA21EA 20040628000542004062800054EA 2004 6 28 SWIA200413415 120040608A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM DIRTY A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07433SW 7550 RUDDER TRIM WILL NOT RE-CENTER; ONLY MOVES NR, WILL NOT RETURN NL. CLEANED CONNECTOR AND PINS. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040628000572004062800057EA 2004 6 28 04149645 120040528A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27645BR 7383 DURING INSPECTION THE MIDDLE SECTION OF EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE WIRING WAS REPAIRED AND BATTERY CHARGER REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000582004062800058EA 2004 6 28 04149644 120040528A335064641 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27644BR 7379 DURING INSPECTION THE FORWARD ORANGE SECTION OF ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE LIGHT SECTION WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000602004062800060EU 2004 6 28 AALA20040665 120040617A5310 BUTT JOINT AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 CIRCUMFERENTIAL JOINT SPLICE STRAP CORRODED AT FRAME 65 BETWEEN STRINGERS 54 AND 55L. AREA IS 2 INCHES BY 5 INCHES IN THE AFT CARGO AREA. INSTALLED NEW BUTTSTRAP AND BUTTSTRAP EXTERNAL DOUBLER PER ESO 30595 DATED 6/16/04. 2L72 4F RTA35EU 20040628000662004062800066WP 2004 6 28 AALA20040659 120040616A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219402W 53138 DFW - CEILING EMERGENCY LIGHTS AT ROW 14 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040628000672004062800067NM 2004 6 28 AALA20040660 120040616A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21198AA 32392 SEAT MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040628000682004062800068NM 2004 6 28 AALA20040661 120040617A34124040800912 COMPUTER BOEING757 757223 1384957NM ADCS LOOSE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21623AA 24581 SFO - INFLIGHT T044 JUST PRIOR TO A/C ROTATION LOST BOTH AIRSPEED INDICATORS, BOTH ALTIMETERS, BOTH VSI, BOTH FDS, AUTOTHROTTLES, AUTO PRESS 1&2, BOTH EEC, RUDDER RATIO, MACH TRIM, TCAS, ALT REPORTING, AUDIO ALTS. UNABLE TO RESTORE ANY SYSTEM. AFTER LANDING ON ROLLOUT SYSTEMS RETURNED TO NORMAL. FOUND BOTH CADCS, SERIAL NUMBERS LEFT HAND 82080237 AND RIGHT HAND 01056148, NOT SECURED IN RESPECTIVE RACKS. REPLACED BOTH ADCS AS PRECAUTIONARY AND PERFORMED REQUIRED PITOT/STATIC CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040628000692004062800069WP 2004 6 28 AALA20040655 120040615A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21565AA 49347 DEN - EMERGENCY LIGHTS AT B5-27 INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040628000742004062800074EA 2004 6 28 04181668 120040609A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27668BR 7544 DURING INSPECTION THE NR 3 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000752004062800075EA 2004 6 28 04180620 120040608A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27620BR 7179 DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000762004062800076EA 2004 6 28 04127644 120040506A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27644BR 7379 DURING INSPECTION THE LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000772004062800077EA 2004 6 28 04131649 120040510A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27649BR 7414 DURING INSPECTION THE RIGHT HAND EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000792004062800079EA 2004 6 28 04129637 120040508A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27637BR 7308 DURING INSPECTION THE LEFT HAND EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000822004062800082NM 2004 6 28 04151415 120040530A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27415FJ 3170 DURING INSPECTION THE LAVATORY EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040628000842004062800084EA 2004 6 28 04129664 120040508A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000862004062800086EA 2004 6 28 04146708 120040525A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION THE AFT CABIN EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000882004062800088NM 2004 6 28 AALA20040651 120040614A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21358AA 24039 SFO - EMERGENCY EXIT LIGHTS AND EMERGENCY LIGHTS AT SEATS 20 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AND EMERGENCY LIGHTS AT SEATS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628000902004062800090NM 2004 6 28 AALA20040643 120040612A3350 CONTACTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISPLACED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21183AN 29593 SFO - OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27 INOPERATIVE. ADJUSTED LAMP CONTACTS AT OVERHEAD STORAGE BIN 27ABC FOR OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 23 AND 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040628000912004062800091WP 2004 6 28 AALA20040644 120040612A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21297AA 49309 LGA - AFT FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT FLOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000922004062800092WP 2004 6 28 AALA20040642 120040611A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217506 49800 DFW - EMERGENCY LIGHTS IN TAIL CONE ARE INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000942004062800094WP 2004 6 28 AALA20040647 120040613A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21410AA 49321 TPA - LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000952004062800095WP 2004 6 28 AALA20040648 120040611A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21467AA 49597 DTW - EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000992004062800099WP 2004 6 28 AALA20040636 120040610A33508039001 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21279AA 49295 AUS - AFT RT AND LT UPPER EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT RT AND LT UPPER EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628001002004062800100WP 2004 6 28 AALA20040637 120040610A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21279AA 49295 AUS - OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628001012004062800101NM 2004 6 28 AALA20040638 120040610A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21353AA 24034 DFW - EMERGENCY LIGHT A SEAT 40B INOPERATIVE. REPLACED CONNECTOR ON SEAT HARNESS AT SEAT 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628001022004062800102NM 2004 6 28 AALA20040639 120040610A3350 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21353AA 24034 DFW - EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628001032004062800103NM 2004 6 28 AALA20040640 120040610A3350 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21353AA 24034 DFW - EMERGENCY LIGHT AT SEAT 11B IS INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628001042004062800104NM 2004 6 28 AALA20040641 120040610A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21791AN 30254 MIA - EMERGENCY LIGHTS ON COACH SEATS INOPERATIVE. REPLACED FAULTY BATTERY PACK M33401 FOR EMERGENCY LIGHTS ON COACH SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040628001052004062800105EU 2004 6 28 AWXA200400591 120040522A5320D5347112470100 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR RT AFT SHEAR PLATE FR 69 TO FR 70, AFT END OF BEAM Y1292. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FR 69 TO FR 70, BEAM Y1292; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3, & 8. 2L72 4F RTA28NM 20040628001072004062800107NM 2004 6 28 DHL2004754011 120040513A5754 MOUNT BRACKET BOEING727 727223 1384074NM SLAT ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, NR 2 SLAT ACT ATTACH OUTBOARD BRACKET INSIDE PLATE HAS NEW CRACK. REMOVED CRACKED STIFFENER AND FABBED NEW FROM BAC 1503-100145, PO 3111123 DIM 9.2 X 3.5 INCHES IAW S/B 727-57-0130 REV 3 FIG 1. PART TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 S/B 727-57-0130 REV 3 FIG 1. 2L73 4F A3WE 20040628001102004062800110NM 2004 6 28 DHL2004754002 120040509A5330 SKIN BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, RT FUSE SKIN IS PILLOWING, AFT BS 1050, AT STR 28R. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-01 FIG 1. CUT OUT DAMAGE OF SKIN SIDE 23 X 3 INCHES ON RT FUSE SKIN BS 1050-1073, STR 28R IAW B727 SRM 53-30-03 FIG 3, FABRICATED REPAIR DOUBLER FROM 2024-T3, .063 SIZE 23 X 3 INCH PO 900759 AND FILLER FROM 2024-T3 .050 SIZE 23 X 3 INCH PO 900780 IAW B727 SRM 53-30-03 FIG 3. TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-02, INSTALLED DOUBLER REPAIR IAW B727 SRM 53-30-03 FIG 3. 2L73 4F A3WE 20040624000712004062400071EA 2004 6 24 COMA0460380 120040615A7110 SKIN CNDAIRCL600 CL6002B19 1900309EA COWL PUNCTURED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 RIGHT LOWER TRANS COWL HAS PUNCTURE THRU OUTER SKIN. REPAIRED RIGHT HAND LOWER TRANS COWL IAW AERODESIGN REPORT 5170-1. 2L72 4F RTA21EA 20040624000722004062400072EA 2004 6 24 COMA0460377 120040615A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01962CA 7123 CRACK FOUND ON LEFT SIDE CABIN ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT BETWEEN 409 AND 28 AND 559 PRESSURE FLOOR SKIN. REPAIRED DAMAGE ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT IAW REO 601R53-41-223. 2L72 4F RTA21EA 20040624000752004062400075EA 2004 6 24 COMA0460343 120040528A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01933CA 7040 FLIGHT 5463 FLAPS FAIL CAUTION MESSAGE. RESET FLAPS AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040624000972004062400097EA 2004 6 24 COMA0460351 120040604A71602285240801 INLET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE ERODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01975CA 7150 RT HAND ENGINE HEATED IN-LIT LIP ERRODED OUT OF LIMITS. REPAIRED RIGHT HAND ENGINE LIP-SKIN USING SERVICEABLE SKIN, 12.5 SECTION IAW SHORTS CMM 71-61-01. 2L72 4F4 FRTA21EA E15NE 20040624000992004062400099EA 2004 6 24 COMA0470045 120040531A2780 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01371CA 10082 FLIGHT 2780 SLATS FAIL CAUTION MESSAGE. RESET THE SECUS, SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20040624001042004062400104WP 2004 6 24 DHL2004804003 120040602A3260313 BULB DOUG DC8 DC873F 302199FWP MLG DOOR IND FAULTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01804DH 46124 AFTER T/O DOOR NOT LATCHED LIGHT ILLUMINATED, RAN ABNORMAL PROCEDURE, LIGHT REMAINED LIT. PROCEEDED AT .65 M - 230 KTS PER PROCEDURE. TROUBLESHOT AND FOUND FAULTY BULB ON DOORS NOT LATCHED LAMP. REMOVED AND REPLACED BULB. PERFORMED LANDING GEAR DOOR OPS CHECK. OPS CHECKED SERVICEABLE IAW M/M 32-60-0. P/N: 313. 2L74 4F RT4A25 20040624001072004062400107CE 2004 6 24 ACE060204 120040602A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE MLG CONTAMINATED E YADAO OTHER J WARNING INDICATION APAPPROACH 1 AL03112AX25 UC45 PILOT REPORTED LANDING GEAR DID NOT EXTEND WHEN HANDLE WAS SELECTED DOWN. ALTERNATE HAND PUMP EXTENSION PERFORMED, FERRY WITH GEAR DOWN FOR REPLACEMENT OF MS24171D1 POWER PACK RELAY (CONTAMINATED WITH WATER). 2L72 4T RTA24CE 20040625000222004062500022NM 2004 6 25 UPS04M42529 120040322A5310 DOOR FRAME DOUG MD11 MD11F 3023600NM ZONE 450 CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, NR 2 ENGINE LEFT FAN COWL DOOR JAMB (FUSELAGE) FOUND LWR SURFACE CHAFE MARK AS MARKED. MEASURED CHAFE AREA FOUND (0.058 INCH), OUT OF LIMIT ORIG THK 0.100 INCH. NR 2 ENG LEFT FAN COWL DOOR JAMB LWR SURFACE SKIN TRIM PER EN1162-04. DOUBLERS FAB & INSTALLED PER EN1162-04. 2L73 4F RTA22WE 20040625000282004062500028NM 2004 6 25 UPS04M42459 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 12 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.020 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000292004062500029NM 2004 6 25 UPS04M42460 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LEFT BARREL NUT HOLE NR 09 FOUND CORROSION AT BOTTOM, SIDEWALL BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.050 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1158-04 (UPS ENGINEERING FILE NR M D11-55-20025). 2L73 4F RTA22WE 20040625000322004062500032NM 2004 6 25 UPS04M42463 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 32 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.006 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1157-04 (UPS ENGINEERING FILE NR MD 11-55-20040). 2L73 4F RTA22WE 20040625000392004062500039NM 2004 6 25 UPS04M42470 120040325A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 19 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.080 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156-04 (UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000442004062500044NM 2004 6 25 UPS04M42475 120040322A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 04 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.015 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1155-04 (REF UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000472004062500047WP 2004 6 25 UPS04842481 120040510A5310570465021 DOUBLER DOUG DC8 DC873F 302199FWP TAIL CONE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, AREA AROUND LOWER TAIL NAV LIGHT CORROSION & NUT PLATES BAD. REMOVED DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-21. LOCATED AND DRILLED NEW DOUBLER P/N 5704650-21 IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040625000512004062500051NM 2004 6 25 UPS04M42485 120040316A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 14 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.005 INCH. SPLICE FITTING FABRICATED & INSTALLED PER EN 1156-04. BARREL NUT HOLE REPAIRED PER EN 1156-04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000592004062500059NM 2004 6 25 UPS04M42493 120040312A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE:C HORIZONTAL STAB, LT BARREL NUT HOLE NR 36 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.082 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED EN 1078-04 (REF UPS ENGINEERING FILE NR MD 11-55-20020). 2L73 4F RTA22WE 20040625000602004062500060NM 2004 6 25 UPS04M42494 120040313A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 15 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED 0.040 INCH. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1159-04 (REF UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040625000732004062500073NM 2004 6 25 UPS04M42507 120040328A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 31 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BOTTOM OF BARREL NUT HOLE PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.025 INCH FOUND WITHIN LIMITS PER EO MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN 1119-04 (REFER UPS ENGINEERING FILE NR MD11-55-20042). 2L73 4F RTA22WE 20040625000752004062500075NM 2004 6 25 UPS04M42509 120040326A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, LT BARREL NUT HOLE NR 19 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR CORROSION AT BOTTOM OF BARREL NUT HOLE REMOVED PER SRM 51-21- 01 VOL 2 REV 34 MAT'L REMOVED 0.005 INCH WITHIN LIMIT PER EO MD11-5510-19 409-E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1118-04 (REFER UPS ENGINEERING FILE NR MD11-55-20041). 2L73 4F RTA22WE 20040628000232004062800023SO 2004 6 28 SWIA200413403 120040515A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07288SW 120316 LEFT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW EMB120 SRM 51-10-02 PG 2 SEC 2B. 2L72 4T4 TRTA31SO E20NE 20040628000242004062800024SO 2004 6 28 SWIA200413404 120040515A5420 CHANNEL EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07288SW 120316 RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED. DISCOVERED AT C-CHECK. REPLACED RIGHT HYDRAULIC RESERVOIR LOW SUPPORT CHANNEL IAW SRM 120 51-10-02 PG 3 SEC 3A. 2L72 4T4 TRTA31SO E20NE 20040628000282004062800028SO 2004 6 28 SWIA200413470 120040617A1420 CONNECTOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE STICK SHAKER DAMAGED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07578SW 120346 CAPTAIN'S STICK SHAKER INOPERATIVE. REPAIRED WIRE AT STICK SHAKER CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040628000302004062800030SO 2004 6 28 SWIA200413472 120040618A3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE MLG OUT OF ADJUST A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07560SW 120334 AFTER TAKEOFF LEFT MAIN GEAR WOULD NOT RETRACT. RE-ADJUSTED BOTH MAIN GEAR DOOR SEQUENCE VALVES PER MM 32-32-04 PG 503. OPERATIONAL CHECK OK. 2L72 4T4 TRTA31SO E20NE 20040628000332004062800033EA 2004 6 28 SWIA200413475 120040618A5240 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SERVICE DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07956SW 7825 GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED DOOR HANDLE SHAFT OF DEBRIS AND LUBRICATED AS NEEDED. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040628000342004062800034 2004 6 28 SWIA200413476 420040616A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AUTO PILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07213SW1018810188 120277 AUTOPILOT ON CAPTAIN'S SIDE INFLIGHT WILL GET THE AUTOPILOT WARNING WITH NO DISCONNECT OF THE AUTO PILOT AP LIGHT ON FCP. REMOVED AND REPLACED CAPTAIN'S AUTO PILOT COMPUTER IAW MM 22-10-02 AND AUTO PILOT PANEL IAW MM 22-10-04. OPERATIONAL CHECK GOOD IAW MM 22-10-00. P/N: 622-6684-006, S/N OFF: 1728. 2L72 4T4 TRTA31SO E20NE 20040628000352004062800035EA 2004 6 28 SWIA200413477 120040617A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07955SW 7817 STAB TRIM CHANNEL 1 INOP STATUS MESSAGE DISPLAYED. REPLACED HSTA AND MOTOR CONTROL UNIT (MCU). OPERATIONAL CHECK GOOD. P/N: 8396-3, S/N OFF: 1087. 2L72 4F4 FRTA21EA E15NE 20040628000402004062800040NM 2004 6 28 SWAA041761 120040623A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040628000462004062800046 2004 6 28 SWIA200413436 420040612A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIAL ABORTED APPROACH L NO TEST NRNOT REPORTED 1 NM07923SW 7664 DURING FFOD STALL TEST, STICK SHAKER DID NOT ACTUATE. REPAIRED WIRING TO FIRST OFFICER'S STICK SHAKER IAW MM 27-35-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040628000562004062800056EA 2004 6 28 SWIA200413417 120040610A2730 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA LT ELEVATOR MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07442SW 7609 LEFT ELEVATOR EICAS INDICATION SURFACE POSITION NOT AT CENTER POSITION AND IS NOT IN LINE WITH RIGHT SIDE. REMOVED AND REPLACED ELEVATOR POSITION TRANSMITTER IAW MM 27-34-10. 2L72 4F RTA21EA 20040628000612004062800061NM 2004 6 28 AALA20040664 120040620A33500202365001 LIGHT BOEING777 777223 1385213NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21799AN 30258 JFK - EMERGENCY LIGHT AT CORNER OF 1L CLOSET DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT CORNER OF 1L CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040628000652004062800065WP 2004 6 28 AALA20040657 120040616A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21233AA 49180 PHL - EMERGENCY LIGHTS WILL NOT TEST PROPERLY. REPLACED SWITCH AT FLIGHT ATTENDANT POSITION AND REPLACED BATTERY PACK AT B5-49 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000732004062800073EA 2004 6 28 04160675 120040608A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 DURING INSPECTION THE PASSENGER DOOR EXTERIOR EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000872004062800087NM 2004 6 28 AALA20040650 120040614A33500201720002 LIGHT BOEING737 737823 13844BZNM SEAT 14D DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21932AN 29530 SFO - FLOOR PROXIMITY LIGHT ASSEMBLY AT SEAT 14D DAMAGED. REPLACED FLOOR PROXIMITY LIGHT ASSEMBLY AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040628001082004062800108EU 2004 6 28 DHL2004364006 120040602A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 2 ENGINE FAULTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01364DH 141 ON CLIMBOUT ENGINE NR 2 LOOP-A LIGHT ILLUMINATED WITH SINGLE STROKE CHIME (SSC) ON MASTER WARNING PANEL (MWP). RAN ABNORMAL PROCEDURE AND TEST WAS SUCCESSFUL. DEFERRED NR 2 ENGINE A-LOOP AS PER MEL 26-12-01-1 CAT-B. ASSIGNED DMI 16774 PLACARD PANEL. REMOVED AND REPLACED FAULTY A-LOOP SENSOR, (FORWARD PYLON DETECTOR ASSEMBLY), AS PER M/M 26-12-12. OPS CHECKED GOOD. THIS CLEARS DMI 16774. 2L72 4F RTA35EU 20040628001132004062800113EA 2004 6 28 QXEA200400357 120040524A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 DEN - FORWARD CARGO BAY CHIMNEY AT DOOR OPENING IS BROKEN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001142004062800114CE 2004 6 28 DXTA200400318 120040527A7830 POSITION SWITCH CESSNA500 560CESSNA 2076750CE THRUST REVERSER MALFUNCTIONED E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07367QS 5600367 CLIMBING 13,000 FT 265 KTS, LT THROTTLE SNATHER ENGAGED, BRINGING ENG BACK 1 INCH FROM STOPS. A LOUD RUSHING NOISE HEARD CONSISTENCE WITH T/R DEPLOYMENT. NO T/R LIGHTS ILLUMINATED, SLOWING DOWN 185 KTS, NOISE WENT AWAY & ABLE TO MOVE THROTTLE SLIGHTLY, DIVERTED TO SMF. INSPECTED, DAMAGE LT T/R OUTBOARD AFT ENG FAIRING, NO DAMAGE ON INBOARD SIDE. RT T/R DEPLOYED BOTH T/R'S, FOUND MULTIPLE CRACKS IN LT T/R BUCKET UPPER & LOWER HALVES, ONE SMALL CRACK RT LOWER HALF T/R BUCKET. REMOVED CRACKED ANGLES & FITTINGS, TRIMMED & DRILLED NEW ANGLES, INSTALLED RIVETS LT UPPER & LOWER T/R DOORS. FOUND BAD T/R STOW SWITCH, INSTALLED NEW SWITCH, RIGGED & OPS CHECKED GOOD. SERVICED RESERVIOR. 2L72 4F RTA22CE 20040628001152004062800115SO 2004 6 28 SWIA200413364 120040530A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07566SW 120341 FLOOR EMERGENCY LAMP OUT AT 8A. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT AT SEAT 8A. CHECKS GOOD IAW 33-50-00. 2L72 4T RTA31SO 20040628001162004062800116EA 2004 6 28 SWIA200413365 120040528A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A SWIAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07437SW7246 7246 7564 SMELL OF SMOKE AND LEFT PACK HI TEMP ON TAKEOFF ROLL. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE AS NEEDED PER CRJ MM 21-51-10. OPS CHECK GOOD. NO LEAKS FOUND. 2L72 4F RTA21EA 20040628001192004062800119EA 2004 6 28 SWIA200413368 120040529A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07440SW 7589 UPON INITIAL POWER UP OF AIRCRAFT, THE CARGO FIREX PANEL INDICATED SMOKE CARGO. BOTH RED LIGHTS ILLUMINATED WITHOUT BOTTLE ARMED LIGHTS ILLUMINATING. REPLACED BOTH NR 1 AND NR 2 SMOKE DETECTORS IN THE CARGO COMP. SYSTEM OPS CHECKS GOOD. P/N: 473597-19, S/N OFF: 1917, S/N OFF: 0857. 2L72 4F RTA21EA 20040628001202004062800120EA 2004 6 28 SWIA200413369 120040530A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07943SW 7762 MAIN CABIN DOOR OUTER HANDLE BROKEN. REMOVED AND REPLACED MAIN CABIN DOOR OUTER HANDLE WITH SERVICEABLE UNIT. OPS CHECKS GOOD IAW CRJ MM CHAPTER 52. 2L72 4F RTA21EA 20040628001212004062800121EA 2004 6 28 SWIA200413370 120040531A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07454SW3801 3801 7749 FLAPS FAIL MESSAGE APPEARED AFTER SELECTING FLAPS 30 DEGREES. REMOVED AND REPLACED R3 AND R4 FLAP ACTUATOR IAW 27-53-05. OPS CHECK GOOD. REF RII 27-412. P/N: 854D100-20, S/N 2274. 2L72 4F RTA21EA 20040628001222004062800122NM 2004 6 28 HNAA0400056 120040519A1400 PIN DHAV DHC8 DHC8102 2809003NM STORAGE BOX LOOSE A HNAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 EA07942HA 163 NOISE NOTED AT AIRSTAIR DOOR EXTERIOR AFTER T/O AIR TURNBACK, FOUND PROP TIE STREAMER HANGING FROM AIRSTAIR DOOR PROP TIE STORAGE AREA. INSPECTION OF ACFT FOUND NO DAMAGE. 2H72 4T RTA13NM 20040628001232004062800123WP 2004 6 28 ABXA040207 120040613A2560A051491 ESCAPE ROPE DOUG DC8 DC863F 302198FWP CABIN DOOR MISMANUFACTURED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23811AX 46113 CHECK EMERGENCY ROPE AT MAIN CABIN DOOR FOR PROPER LENGTH. ROBBED EMERGENCY ROPE FROM 826AX, CHECKED FOR PROPER LENGTH AND INSTALLED ON 811AX IAW DC-8 MM 25-60-02-0002. CANNIBALIZATION FORM WAS FILLED OUT. 2L74 4F 4A25 20040628001242004062800124EU 2004 6 28 RAIA00405012 120040519A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03550HK 41039 STL - ESCAPE PATH LIGHTS INOP ROWS 3A TO 5A. MAINTENANCE RE-SECURED LOOSE CONNECTOR AT EMERGENCY ESCAPE PATH LIGHTS. 2L72 4T RTA41NM 20040628001262004062800126NM 2004 6 28 AWXA200400593 120040602A3260841602 DOWNLOCK SENSOR BOEING757 7572S7 1384962NM ZONE 100 FAILED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28904AW2722221 23566 ON CLIMBOUT RECEIVED EICAS MESSAGE MLG MONITOR DISPLAYED MLG UP & LOCKED. MLG HANDLE IN UP/OFF POSITION & LT HALF OF NLG INDICATOR GREEN. TURNED OFF PAX ENTERTAIN EQUIP, LIGHT REMAINED ILLUM. TURNED BACK & LANDED W/O EVENT. MX ERASED EICAS MESSAGE. MESSAGE DID NOT RETURN. NO IN-FLT FAULTS DETECTED ON PSEU, BITE CHECK SYSTEM 2, MLG DID HAVE 006 CARD FAULT, SYS 1 OK. R & R NLG DOWNLOCK SENSOR, NO HELP. R & R PSEU IAW BMM & SWUNG MLG SEVERAL TIMES, OPS CK GOOD. CONFIRMED FAILURE OF UNIT. PBC CARD 006 FAILED TEST FOR DRIVER 106 (L6GA), RESEATED BOARDS & FAULT CLEARED. CARD 007 ALSO FAILED, PERFORMED CONTINUITY TEST & FOUND HIGH RESISTANCE AT PINS J7-B11, J11-C40, J12-B9 C4, AND J13-A11 C39. 2L72 4F RTA2NM 20040628001282004062800128NM 2004 6 28 QXEA200400338 120040520A243023088002B GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09364PH7904 966 524 MFR - ON FLIGHT 2080- NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED JUST PRIOR TO LANDING. RAN CHECKLIST, GENERATOR WOULD NOT RESET. REMOVED AND REPLACED DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040628001312004062800131WP 2004 6 28 ABXA040197 120040521A5711591486529 SPAR CAP DOUG DC9 DC941 302207NWP WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 WING FRONT SPAR LOWER T-CAP CORRODED BETWEEN LONGERON 30 AND LONGERON 29 LEFT UNDER THE ANTI-ICE DUCT. REPLACED T-CAP IAW DWG 5914865. 2L72 4F A6WE 20040628001342004062800134WP 2004 6 28 ABXA040195 120040520A53305910228187 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 FUSELAGE EXTERIOR SKIN CRACKED STA 1208 9:00 POSITION LOOKING FORWARD. REPAIRED IAW DC-9 SRM 53-01 AND 51-60-0. 2L72 4F A6WE 20040628001352004062800135WP 2004 6 28 ABXA040196 120040520A5330592032339 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 FUSELAGE SKIN CRACKED AT FORWARD LOWER CARGO DOOR CUTOUT FORWARD UPPER CORNER. REPAIRED DOOR UPPER CORNER IAW DWG SR0953117. 2L72 4F A6WE 20040628001432004062800143EU 2004 6 28 150721 120040502A2613 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ROTOL R389 R3894123F26 NE RT TAILPIPE ILLUMINATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL1740SZ 40 E367503 DRG153688 ON 05-02-04, APPROX 1605 (UTC), FLT 8960 LEX-PIT ABORTED TAKEOFF WHEN THE LT TAIL PIPE HOT LIGHT ILLUMINATED. 2L72 4T4 TRTA52EU E8NE6 6 CP30NE 20040628001462004062800146NM 2004 6 28 AWXA200400521 120040505A5522 SKIN BOEING737 7373G7 1384595NM ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR AT ELEV STA 65. MAINTENANCE PREPARED SURFACE AND BONDED REPAIR PLIES TO RT ELEVATOR UPPER HONEYCOMB SURFACE PANEL ELEV STA 65 TO ELEV STA 73 IAW B737-300 SRM 51-70-04 FIG 10. 2L72 4F RTA16WE 20040628001482004062800148NM 2004 6 28 SWAA041741 120040621A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040628001492004062800149NM 2004 6 28 SWAA041742 120040621A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040628001522004062800152NM 2004 6 28 AWXA200400522 120040505A5522 SKIN BOEING737 7373G7 1384595NM ELEVATOR DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND GRAPHITE FIBER DELAMINATED OFF THE UPPER HONEYCOMB SURFACE PANEL OF THE RT ELEVATOR AT ELEV STA 142.0. MAINTENANCE PREPARED SURFACE AND BONDED REPAIR PLIES TO RT ELEVATOR UPPER HONEYCOMB SURFACE PANEL AT ELEV STA 142.0 IAW B737-300 SRM 51-70-04 FIG 10. 2L72 4F RTA16WE 20040628001532004062800153NM 2004 6 28 AWXA200400523 120040427A57536546435239 SKIN BOEING737 7373G7 1384595NM LT WING TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND LT WING OUTBOARD FLAP; OUTBOARD END TRAILING EDGE DELAMINATED AT WBL 410.38. MAINTENANCE CUT OUT DAMAGED SECTION OF LT WING OUTBOARD FLAP AT WBL 410.38; FABRICATED 2 EACH DOUBLERS, A FILLER, AND A CORE REPAIR; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 21. 2L72 4F RTA16WE 20040628001552004062800155WP 2004 6 28 ABXA040209 120040615A3230 LANDING GEAR DOUG DC9 DC941 302207NWP LT & RT MALFUNCTIONED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23953AX 47608 OVERSHOT UPLATCH CHECK DETENT. RIGHT & LEFT RED GEAR UNSAFE & YELLOW GEAR DOOR OPEN LIGHT ILLUMINATED. PER ABNORMAL, RECYCLED GEAR & NORMAL OPERATION FOLLOWED. NOTED BY MAINTENANCE, PERFORMED VISUAL INSPECTION OF GEAR UPLOCKS. NO DEFECTS NOTED. 2L72 4F A6WE 20040628001572004062800157EA 2004 6 28 COMA0460387 120040619A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01936CA 7043 DURING PREFLIGHT DISCOVERED EMERGENCY LIGHTING INOPERATIVE. REPLACED 8 EMERGENCY BATTERIES. 2L72 4F RTA21EA 20040628001592004062800159EU 2004 6 28 NACA20040021 120040515A3230E0217XUU001A RELAY AEROSPATR42 ATR42* 8680900EU MLG INOPERATIVE A NACAO OTHER O OTHER LDLANDING 1 AL0342NC 067 LANDING GEAR WOULD NOT EXTEND WITH LEVER IN THE DOWN POSITION. GRAVITY EXTENSION PROCEDURE WAS USED. FOUND 14GA RELAY DEFECTIVE AND POOR WIRE RETENTION AT RELAY BASE. REPLACED 14GA RELAY AND RESET PINS. GEAR RETRACTION TEST GOOD MULTIPLE TIMES. 2H72 4T RTA53EU 20040628001622004062800162EA 2004 6 28 SWIA200413352 120040526A2613 ELEMENT CNDAIRCL600 CL6002B19 1900309EA MLG WW BROKEN A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07429SW 7518 RECEIVED MULTIPLE NUISANCE AMBER MLG OVERHEAT FAIL MESSAGES. UPON TOUCHDOWN, RECEIVED MASTER WARNING MLG BAY OVERHEAT WITH AURAL GEAR BAY OVERHEAT. REMOVED AND REPLACED BROKEN LT WHEEL BIN ELEMENT PER CRJ MM 26-14-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20040628001632004062800163 2004 6 28 SWIA200413353 420040526A2210 DAMPER CNDAIRCL600 CL6002B19 1900309EA NR 2 INOPERATIVE A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07945SW 7770 YAW DAMPER NR 2 INOPERATIVE, STATUS MESSAGE DURING TURBULENT FLIGHT. UNABLE TO RE-ENGAGE. COULD NOT DUPLICATE DISCREPANCY. SWAPPED FCC CARDS IN THE IAPS CARD CAGE FROM NR 1 TO NR 2 SIDE. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040628001682004062800168EA 2004 6 28 04131620 120040510A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27620BR 7179 DURING INSPECTION THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001712004062800171WP 2004 6 28 0400981221 120040608A261130231R17 FIRE DETECTOR DOUG DC10 DC1030 3023501WP CARGO BAY MALFUNCTIONED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01211NW4658812733 46868 DURING CRUISE, THE FORWARD CARGO COMPARTMENT NR 2 AND NR 4 SMOKE DETECTOR LIGHTS AND FORWARD CARGO FIRE LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE AND PROCEEDED TO NEAREST AIRPORT (BIL) FOR AN UNEVENTFUL LANDING. BOTH FIRE BOTTLES RELEASED. REPLACED NR 2, 3 AND 4 SMOKE DETECTORS AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20040628001792004062800179NM 2004 6 28 SWAA041751 120040622A335090083 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 DURING SCHEDULED C4 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040628001802004062800180NM 2004 6 28 SWAA041752 120040622A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 787, STRINGER 22L TO STRINGER 25L, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040628001812004062800181NM 2004 6 28 SWAA041753 120040622A53106546812 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 967 TO BS 986.5, RBL 49, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20040628001832004062800183NM 2004 6 28 SWAA041755 120040622A55236959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR TRIMWORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW296021W 27953 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1HINGE BUSHINGS PER MM. 2L72 4F RTA16WE 20040628001842004062800184NM 2004 6 28 SWAA041756 120040622A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D + 4, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040628001852004062800185NM 2004 6 28 SWAA041757 120040622A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 807, STRINGER 19L, BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM AND EA. 2L72 4F RTA16WE 20040628001862004062800186NM 2004 6 28 SWAA041758 120040622A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040628001872004062800187NM 2004 6 28 SWAA041743 120040621A5310907822 DOOR FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT LOWER RADIUS, CRACKED. REPAIRED FRAME HINGE CUTOUT PER EA. 2L72 4F RTA16WE 20040628001902004062800190NM 2004 6 28 SWAA041745 120040621A5743656717223 FITTING BOEING737 7373H4 1384600NM LT W/W CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND LEFT W/W AFT STABILIZER FITTING, CORRODED. REPAIRED PER EA. 2L72 4F RTA16WE 20040628001912004062800191NM 2004 6 28 SWAA041746 120040622A5755 SKIN BOEING737 7373H4 1384600NM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW MA2042 23960 DURING SCHEDULED A1 CHECK, FOUND RT WING NR 5 SPOILER DELAMINATED. REMOVED AND REPLACED RT WING NR 5 SPOILER PER MM. 2L72 4F RTA16WE 20040628001932004062800193EA 2004 6 28 COMA0460313 120040511A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A COMAK NONE O OTHER ININSP/MAINT 1 SO01966CA 7132 FLIGHT 5423 EMERGENCY FLOOR PATH LIGHTING ROWS 1 THRU 5 IS INOP. CLEANED CONNECTIONS ON FLOOR LIGHTING, OPERATION CHECKS NORMAL. 2L72 4F RTA21EA 20040628001952004062800195 2004 6 28 SWAA041749 420040622A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040628002042004062800204SO 2004 6 28 SWIA200413419 120040609A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07237SW9698 9698 120314 RECEIVED FLAP CONTROL FAULT ON GROUND AFTER START UP WITH ASSOCIATED FLAP MAP AND OUTBOARD PAIR SECOND ROW (10 DEGREES) LIGHT FLASHING ON OVERHEAD PANEL. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECKS GOOD IAW EMB 120 MM 27-50-00. 2L72 4T RTA31SO 20040628002062004062800206EA 2004 6 28 SWIA200413422 120040609A3620 LOOP CNDAIRCL600 CL6002B19 1900309EA LT NACELLE MALFUNCTIONED A SWIAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 NM07410SW 7066 INFLIGHT FROM OAK TO SLC LEFT 14TH DUCT MSG POSTED, SHUTDOWN LEFT ENGINE. REMOVED AND REPLACED LEFT 14TH STAGE PYLON LOOP WITH SERVICEABLE UNIT IAW MM 36-21-04. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629000012004062900001WP 2004 6 29 04FDEA01622 120040604A5753ARC01822 HINGE BRACKET DOUG DC10 DC1010 3022110WP RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5750-78220A WINGS RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET SIDE BRACE REPAIR. COMPLIED WITH EA 8-5750-78220 A WINGS RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET SIDE BRACE REPAIR. 2L73 4F A22WE 20040629000022004062900002WP 2004 6 29 04FDEA01623 120040605A5530AMC72652 CHANNEL DOUG DC10 DC1010 3022110WP VERTICAL STAB ELONGATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5530-78221 STABILIZERS VERTICAL. RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC7265-2. COMPLIED WITH EA 8-5530-78221 STABILIZERS VERTICAL RIGHT FWD ACCESS PANEL JAMB ELONGATED HOLES REPAIR, P/N AMC 7265-2. 2L73 4F A22WE 20040629000032004062900003WP 2004 6 29 04FDEA01624 120040605A5754ARB1189 RIB DOUG DC10 DC1010 3022110WP NR 1 SLAT TRACK GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189. COMPLIED WITH EA 8-5710-77421 WINGS REWORK OF GOUGES IN NR 1 SLAT TRACK SUPPORT RIB ARB1189. 2L73 4F A22WE 20040629000052004062900005NM 2004 6 29 04FDEA01626 120040606A5754 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT WING, SLAT TRACK NR 16 INBOARD RIB SUSPECT CRACKED. 2L73 4F RTA22WE 20040629000062004062900006NM 2004 6 29 04FDEA01627 120040607A5753 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT WING O/B FLAP STOP FITTINGS FOUND CRACKED. RT WING O/B FLAP REMOVED AND REPLACED, REFER TO SNRM 1134. 2L73 4F RTA22WE 20040629000092004062900009NM 2004 6 29 04FDEA01630 120040607A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION ON FLOORBEAM STRAP AT BS 950, LBL 9, WL 138. 2L73 4F RTA3WE 20040629000102004062900010NM 2004 6 29 04FDEA01631 120040607A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FWD CARGO BAY STA 680 FRAME DENTED STR 25 LT. 2L73 4F RTA3WE 20040629000122004062900012WP 2004 6 29 04FDEA01634 120040608A5753ARC2761 BRACKET DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 LEFT I/B FLAP IDLER ARM ATTACH FITTING IS CORRODED. REMOVED BUSHINGS FOR ACCESS IAW M/M 20-20-07, REMOVED CORROSION BY REAMING TO 1.079, OUT OF LIMITS IAW DWG ARC2761. REMOVED AND REPLACED FITTING IAW SRM 51-35-01 AND 51-31-01. LOCATED AND DRILLED 4EA MOUNT HOLES IAW DWG ARC2761. REAMED TO 378. PAINTED FITTING IAW SRM 51-21-02. 2L73 4F A22WE 20040629000132004062900013WP 2004 6 29 04FDEA01620 120040604A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT STA 791-808 RBL 45. REMOVED SEAT TRACK SECT AT STA 766-815. FABBED NEW TRACK AND SPLICES ON MAE TRAVELERS, T4/434382, T4/434383, T4/434384. LOCATED AND DRILLED IAW SRM 53-70-00. TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED NEW TRACK & SPLICE IAW SRM 53-70-00. 2L73 4F A22WE 20040629000142004062900014WP 2004 6 29 04FDEA01621 120040604A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT STA 791-808 RBL 27. SEAT TRACK OUT OF LIMITS IAW SRM 53-70-00. REMOVED DAMAGED SECTION OF SEAT TRACK, FABBED NEW SECTION OF SEAT TRACK AND SPLICES ON MAE TRAVELERS T4/434273, T4/434274, T4/434272. LOCATED AND DRILLED NEW TRACK IAW SRM 53-70-00. TREATED AND PRIMED IAW SRM 51-21-01. INSTALLED NEW TRACK AND SPLICES IAW SRM 53-70-01. 2L73 4F A22WE 20040629000152004062900015WP 2004 6 29 04FDEA01642 120040608A5320NFA603633 RETAINER DOUG DC10 DC1010 3022110WP AFT CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 AFT CARGO COMPT DOOR SILL DOOR SEAL RETAINER AFT LWR CORNER AFT SIDE CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-35-01, SRM 51-41-01, SRM 51-33-01. 2L73 4F A22WE 20040629000162004062900016WP 2004 6 29 04FDEA01643 120040609A5753ARC27612 SUPPORT BRACKET DOUG DC10 DC1010 3022110WP RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 COMPLY WITH EA 8-5750-78222 WINGS RIGHT INBOARD FLAP TRACK MOUNTING/DRIVE SUPPORT BRACKET, P/N ARC2761-2. COMPLIED WITH EA 8-5750-78222 WINGS RIGHT INBOARD FLAP TRACK MOUNTING/DRIVE SUPPORT BRACKET, P/N ARC 2761-2. 2L73 4F A22WE 20040629000172004062900017WP 2004 6 29 04FDEA01644 120040609A5320S2929841 FLOOR SUPPORT DOUG DC10 DC1010 3022110WP FWD CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 FLOOR PANEL SUPPORT CORRODED LWR FWD PIT FS 819 RIGHT SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 AND SRM 51-35-01. 2L73 4F A22WE 20040629000192004062900019NM 2004 6 29 04FDEA01646 120040609A5311AFA0018 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN CABIN LEFT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1741 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I. 2L73 4F RTA22WE 20040629000202004062900020NM 2004 6 29 04FDEA01647 120040609A5311AFA0020 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1701 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I. 2L73 4F RTA22WE 20040629000222004062900022NM 2004 6 29 04FDEA01637 120040608A5753ARC74903 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - I/B FLAP VANE I/B TEE FITTING BORE FOUND CORRODED. LEFT WING - I/B FLAP VANE I/B TEE FITTING BORES CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.8765 INCH, CENTER=0.877 INCH, AFT=0.880 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA 1-5750-76737. WINGS LEFT AND RIGHT INBOARD FLAP VANE NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040629000232004062900023NM 2004 6 29 04FDEA01638 120040608A5753ARC74903 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING - I/B FLAP VANE I/B TEE FITTING BORE FOUND CORRODED. RIGHT WING - I/B FLAP VANE I/B TEE FITTING BORES CORROSION REMOVED PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.879 INCH, CENTER=0.880 INCH, AFT=0.880 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA 1-5750-76737 WINGS LEFT AND RIGHT INBOARD FLAP VANE NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040629000242004062900024NM 2004 6 29 04FDEA01639 120040608A5753ARC74903 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RIGHT WING - I/B FLAP VANE O/B TEE FITTING BORE FOUND CORRODED. RIGHT WING - I/B FLAP VANE O/B TEE FITTING BORES CORROSION REMOVED PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.8795 INCH, CENTER=0.8775 INCH, AFT=0.8790 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA NR 1-5750-76737 - WINGS LEFT AND RIGHT INBOARD FLAP VANE NR 1 & 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040629000252004062900025NE 2004 6 29 SWIA200413410 220040613A7320 PUMP EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE HMU MALFUNCTIONED A SWIAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM07217SW 120286 DURING CLIMB RIGHT ENGINE LOST POWER INDICATING ABOUT 15 PERCENT TQ, T6 450, DECREASING FUEL FLOW 250, DECREASING NP 100 PERCENT. REMOVED AND REPLACED HMU FUEL PUMP. OPERATIONAL CHECK GOOD. P/N: 786390-10, S/N OFF: F10376, P/N: 5006488G, S/N OFF: 2178. 2L72 4T4 TRTA31SO E20NE 20040629000262004062900026 2004 6 29 SWIA200413411 420040611A3418C12851AA03 COMPUTER CNDAIRCL600 CL6002C10 1390015EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07702SK 10136 AT CRUISE (FL350), STALL FAIL CAUTION MESSAGE CAME ON, FOLLOWED BY R-FACED FAULT 2 AND L-FADEC FAULT 2 STATUS MESSAGES. REMOVED AND REPLACED SPC IAW MM 27-30-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629000272004062900027NM 2004 6 29 SWAA041768 120040623A53306545835 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST DUCT CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040629000282004062900028NM 2004 6 29 SWAA041769 120040624A29101U1234 VALVE BOEING737 7373Y0 1384671NM MLG WW LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29308SA 23498 AIR TURNBACK, A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED FWD MLG MODULE VALVE, AND REMOVED AND REPLACED CASE DRAIN FILTERS, PER MM. 2L72 4F RTA16WE 20040629000292004062900029NM 2004 6 29 SWAA041770 120040624A278265445519 ACTUATOR BOEING737 7373H4 1384600NM LT WING LE FLAP FAULTY A SWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW29640SW 27713 AIR TURNBACK, LT WING NR 3 L/E FLAP ANNUNCIATOR ILLUMINATED AMBER AFTER FLAP RETRACTION ON TAKEOFF. CYCLED FLAPS, NO HELP. NORMAL INDICATIONS ON DESCENT. REMOVED AND REPLACED NR 3 L/E KRUEGER FLAP ACTUATOR PER MM. 2L72 4F RTA16WE 20040629000322004062900032EU 2004 6 29 AWXA200400596 120040606A2913MX635336 PUMP AIRBUS320 A320232 3930326EU NR 2 ENGINE MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28642AW1124710265 584 EN ROUTE, RECEIVED ECAM MESSAGE YELLOW HYDRAULIC PUMP LOW PRESSURE, DIVERTED TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE NR 2 (YELLOW) ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-13-51-04, OPERATIONAL CHECK AND LEAK CHECK WAS GOOD. CONFIRMED FAILURE OF ENGINE DRIVEN HYDRAULIC PUMP S/N MX635336. UNIT WAS DISASSEMBLED AND NUMEROUS SEALS WERE FOUND WORN BEYOND LIMITS. REPLACED 32 SEALS/PACKINGS AND TESTED UNIT IAW CMM 29-11-34, REV. 4. 2L72 4F RTA28NM 20040629000332004062900033NM 2004 6 29 AWXA200400597 120040526A5320DHM42377C03602 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER SPLICE CHANNEL AT BS 500C+4, STR 16 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL AT BS 500C+4, STR 16 LT; FABRICATED A NEW REPLACEMENT SPLICE CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-03-2, FIG 201 PG 201-207. 2L72 4F RTA16WE 20040629000352004062900035NM 2004 6 29 AWXA200400599 120040526A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 706, STRINGER 1. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 706, STRINGER 1; FABRICATED A NEW REPLACEMENT CLIP PER DWG 65-49902; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIGS 8 & 12. 2L72 4F RTA16WE 20040629000392004062900039NM 2004 6 29 04FDEA01640 120040608A5753ARC74903 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 LEFT WING - I/B FLAP VANE O/B TEE FITTING BORE FOUND CORRODED. LEFT WING - I/B FLAP VANE O/B TEE FITTING BORES CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.877 INCH, CENTER=0.878 INCH, AFT=0.8785 INCH. FPI CARRIED OUT, RESULT: NO CORROSION AND NO CRACK EVIDENT. BUSHING FABRICATED & INSTALLED AS PER EA 1-5750-76737. WINGS LEFT AND RIGHT INBOARD FLAP VANE NR 1 & NR 3 TEE FITTING WEAR REPAIR. 2L73 4F RTA22WE 20040629000402004062900040NM 2004 6 29 04FDEA01641 120040608A3260859803 PSEU DOUG MD11 MD11 3023602NM ZONE 700 DEFECTIVE A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25597FE 48596 GEAR UNSAFE ON PRIMARY AND SECONDARY INDICATIONS WITH LANDING GEAR UP. RIGHT MAIN LANDING GEAR DOOR LINK AND BRACKET ASSEMBLY ADJUSTMENT/TEST CARRIED OUT AS PER AMM 32-34-05-5. PROXIMITY SWITCH ELECTRONICS UNIT REMOVED & REPLACED, OPERATIONAL TEST CARRIED OUT AS PER AMM 31-71-01-2. FOUND SATISFACTORY. LANDING GEAR RETRACTION CARRIED OUT AS PER AMM 32-31-00-5. FOUND SATISFACTORY. PREMATURE REMOVAL/INSTALLATION OFF MFG 8-598-03, POS ONL SRL 42, TAG 578968, ON MFG 8-598-03, SRL C269, TAG 542239. 2L73 4F RTA22WE 20040629000412004062900041NM 2004 6 29 04FDEA01649 120040609A5311AFA0027 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1661 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I. 2L73 4F RTA22WE 20040629000442004062900044NM 2004 6 29 AWXA200400612 120040609A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 13 LT SHORTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT CAME LOOSE FROM SEAT ROW 13 LT AND SHORTED OUT WHEN TRYING TO FEED WIRES BACK THROUGH SEAT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040629000452004062900045NM 2004 6 29 AWXA200400613 120040607A53306545774 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3.125 INCH CRACK WAS FOUND IN EXTERNAL FUSELAGE SKIN ABOVE UPPER RIVET ROW BS 847, STR 25 LT, CONFIRMED BY HFEC INSPECTION. MAINTENANCE TRIMMED OUT CRACK IN FUSELAGE SKIN BS 847, STR 25 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20040629000472004062900047NM 2004 6 29 04FDEA01654 120040609A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CABIN SEAT TRACK DAMAGED AT STA 635 LBL 47.5. EXISTING SPLICE REPAIR SEAT TRACK REMOVED AS PER SRM 51-31-01 VOL II. NEW SEAT FABRICATED AS PER DWG ACA7399 AND INSTALLED AS PER SRM 51-33-01 VOL II. NEW SEAT TRACK FABRICATED AS PER DWG ACA7399 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040629000512004062900051NM 2004 6 29 SWAA041775 120040624A53106546544 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 787, BETWEEN STRINGER 26R AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040629000522004062900052NM 2004 6 29 04FDEA01652 120040609A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CABIN STA 6-30 LBL 55 SEAT TRACK FOUND DAMAGED. CUT & REMOVED AT STA 1109 & STA 6-40 LBL 47.5 AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II RESPECTIVELY. REPAIR SEAT TRACK FABRICATED & ISNTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-33-01 VOL II. FOR WORK ACCOMPLISHMENT, REFER TO SNRM N0541. 2L73 4F RTA22WE 20040629000552004062900055WP 2004 6 29 04FDEA01657 120040610A5730ARB71571 PANEL DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25388FE 46622 LEFT MAIN LANDING GEAR, WING SUPPORT FITTING CORROSION IN THREE TAPER LOCK HOLES. CORROSION REMOVAL AND OVERSIZED TAPER LOKS INSTALLATION IAW FEDEX EA 8-5710-70153. 2L73 4F A22WE 20040629000592004062900059NM 2004 6 29 SWAA041776 120040624A53306545890 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 303.9, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040629000602004062900060NM 2004 6 29 04FDEA01660 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG DIA 1.063, FINAL DIA 1.189. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000612004062900061NM 2004 6 29 04FDEA01661 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.402, REMAINING THICKNESS=0.400, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000622004062900062NM 2004 6 29 04FDEA01662 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG DIA 1.063, FINAL DIA 1.189. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000632004062900063NM 2004 6 29 04FDEA01663 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.404, REMAINING THICKNESS=0.402, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000682004062900068 2004 6 29 SWAA041778 420040624A256563550 SLIDE BOEING737 7377H4 1384404NM R1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED HC1 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040629000702004062900070 2004 6 29 SWIA200413441 420040612A3418C818171 TRANSDUCER EMB 120 EMB120ER 3260203SO AOA MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07565SW6893 5084 120340 LEFT AOA C/B POPS. REPLACED LEFT AOA TRANSDUCER WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N C-81817-1, S/N ON 733, S/N OFF 898. 2L72 4T RTA31SO 20040629000732004062900073NE 2004 6 29 SWAA041780 220040624A7200CFM56 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 OVERTEMP A SWAAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW29366SW 26577 858617 NR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20040629000742004062900074NM 2004 6 29 04FDEA01668 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000762004062900076EA 2004 6 29 SWIA200413454 120040615A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07925SW 7682 SPOILERON FAULT ON RUNWAY. REMOVED AND REPLACED NR 1 SECU AND LEFT OUTBOARD PCU IN REF TO AMM 27-61-00 AND 27-62-1. OPS CHECK GOOD. SECU S/N OFF: 03059, PCU P/N: 27000-7, S/N OFF: MAL-5776. 2L72 4F RTA21EA 20040629000772004062900077SO 2004 6 29 SWIA200413455 120040617A5412 BULKHEAD EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW 120151 RIGHT NACELLE OUTBOARD BULKHEAD CRACKED OUT AT OUTBOARD TAILPIPE SUPPORT IN NUT PLATE AREA. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-70-05. 2L72 4T RTA31SO 20040629000792004062900079SO 2004 6 29 SWIA200413457 120040620A7712 PICKUP EMB 120 EMB120ER 3260203SO TORQUE METER MALFUNCTIONED A SWIAC ABORTED TAKEOFF RS PARTIAL RPM/PWR LOSS AFFECT SYSTEMS TOTAKEOFF 1 NM07188SW 120039 RIGHT TORQUE GAUGE WOULD ONLY RESPOND TO 20 PERCENT. RIGHT ENGINE FEATHERED. ABORTED TAKEOFF. REPLACED THE TORQUE METER PICK-UP PROBE IAW 77-11-02. OPERATIONAL CHECK GOOD. P/N: 4002-0000-02. 2L72 4T RTA31SO 20040629000802004062900080NM 2004 6 29 04FDEA01669 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.404, REMAINING THICKNESS=0.402, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000832004062900083NM 2004 6 29 04FDEA01672 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.128. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000852004062900085NM 2004 6 29 04FDEA01674 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG DIA 1.063, FINAL DIA 1.095. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000862004062900086NM 2004 6 29 04FDEA01675 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.508, REMAINING THICKNESS=0.506, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000872004062900087NM 2004 6 29 04FDEA01676 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000892004062900089NM 2004 6 29 04FDEA01678 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.189. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000932004062900093NM 2004 6 29 04FDEA01682 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.092. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000972004062900097NM 2004 6 29 AWXA200400614 120040609A3397BMS13311122 WIRE BOEING737 7373Y0 1384671NM SEAT ROW 13 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28331AW 23747 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040629000982004062900098NM 2004 6 29 AWXA200400615 120040530A533065C33756 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 LCQ - MAJOR REPAIR - DURING C-17 CHECK A .625 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTOUT JUST ABOVE SCUFF PLATE, EMANATING FROM EDGE OF CUTOUT EXTENDING THROUGH FASTENER HOLE, BS 294, RBL 65, WL 210. MAINTENANCE CUTOUT DAMAGE AT LOWER AFT CORNER OF R-1 DOOR CUTOUT; FABRICATED 2 EACH DOUBLERS (PLATES NR 2 & NR 5); INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01 FIG 202. 2L72 4F RTA16WE 20040625000552004062500055NM 2004 6 25 UPS04M42489 120040325A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB RT BARREL NUT HOLE NR 22 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. CORR REMOVED PER SRM 51-21-01 VOL 2 REV 34 MATERIAL REMOVED FOUND WITHIN LIMIT PER EO MD11-5510-19409-E. SLEEVE BUSHING FABRICATED & INSTALLED PER EO MD11-5510-19409-E. BARREL NUT HOLE REPAIRED PER EN 1156- 04 (REF UPS ENGINEERING FILE NR MD11-55-20039). 2L73 4F RTA22WE 20040625000652004062500065NM 2004 6 25 UPS04M42499 120040318A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 26 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L REMOVED 0.006 INCH FOUND WITHIN LIMIT PER EO MD11-5510-19409E. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1095-04 (REFER UPS ENGINEERING FILE NR MD11-55-20040). 2L73 4F RTA22WE 20040625000722004062500072NM 2004 6 25 UPS04M42506 120040327A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE: C, HORIZONTAL STAB, RT BARREL NUT HOLE NR 03 FOUND CORROSION AT BOTTOM, SIDEWALL AND BEARING SURFACE. MINOR SURFACE CORROSION AT BOTTOM OF HOLE REMOVED PER SRM 51-21-01 VOL 2 REV 34, MAT'L REMOVED 0.005 INCH FOUND WITHIN LIMITS PER EO MD11-551 0-19409-4. SLEEVE BUSHING FABRICATED PER EO MD11-5510-19409E. BARREL NUT HOLE REPAIR CARRIED OUT PER EN1121-04 (REFER UPS ENGINEERING FILE NR MD11-55-20026). 2L73 4F RTA22WE 20040625000792004062500079EU 2004 6 25 AWXA200400589 120040522A5320D5348002034300 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK A 7 INCH CRACK WAS FOUND IN SHEAR PLATE (TRAY) BETWEEN FR 68 AND FR 69, OUTBOARD OF BEAM Y1732, AFT OF R-2 DOOR LOWER SILL. MAINTENANCE REMOVED CRACKED SHEAR PLATE FROM FR 68 TO FR 69, BEAM Y1732 TO BEAM Y1736; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 8, 12, & 18. 2L72 4F RTA28NM 20040628000142004062800014EA 2004 6 28 SWIA200413469 120040521A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07449SW 7699 CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH CLIP FOR STOP FITTING IS CRACKED FS 589.00 LBL 43.0. REPAIRED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16. 2L72 4F RTA21EA 20040628000362004062800036EA 2004 6 28 SWIA200413478 120040615A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07702SK 10136 SSCU 1 FAULT STATUS MSG. REPLACED NR 1 SSCU IAW CRJ MM 27-61-05-401. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040628000382004062800038NM 2004 6 28 SWAA041766 120040623A531565C33940 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 45 TO RBL 51, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040628000392004062800039 2004 6 28 SWAA041767 420040623A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040628000432004062800043NM 2004 6 28 SWAA041764 120040623A2560P4010021 BATTERY BOEING737 7377H4 1384404NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29731SA 27863 DURING SPV, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040628000592004062800059EA 2004 6 28 04143654 120040522A3350110049 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27654BR 7454 DURING INSPECTION THE FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB AND BATTERY WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000712004062800071NM 2004 6 28 04161405 120040609A3350321473 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27405FJ 3155 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE POWER SUPPLIES WERE FOUND DISCHARGED AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040628000722004062800072NM 2004 6 28 04158409 120040606A712002ND714011 MOUNT DORNERDO32 DO328300 NM ENGINE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27409FJ 264386 DURING INSPECTION THE RIGHT HAND FORWARD ENGINE MOUNT WAS FOUND WITH LEVEL 2 CORROSION AND WAS REPLACED. AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2H72 4T RTA55NM 20040628000812004062800081EA 2004 6 28 04154653 120040602A2701 NUT CNDAIRCL600 CL6002B19 1900309EA CONTROL COLUMN LOOSE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27653BR 7438 DURING AIRCRAFT OPERATION THE CREW REPORTED THE FIRST OFFICERS YOKE BINDING. THE YOKE NUT WAS FOUND LOOSE AND RETORQUED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000832004062800083EA 2004 6 28 04127652 120040506A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27652BR 7429 DURING INSPECTION THE NR 4 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000852004062800085EA 2004 6 28 04127628 120040506A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27628BR 7240 DURING INSPECTION THE NR 3 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000892004062800089WP 2004 6 28 AALA20040645 120040613A3350 LIGHT DOUG DC9 DC982 3022082WP SEATS 15D & 19D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21259AA 49289 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 15D AND 19D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 15D AND 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000932004062800093NM 2004 6 28 AALA20040646 120040613A3397 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21328AA 22328 LAX - MID GALLEY EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRING UNDER MID GALLEY CABIN FLOOR FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628000962004062800096WP 2004 6 28 AALA20040649 120040614A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21469AA 49599 ATL - EMERGENCY LIGHT AT ROWS 20 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROWS 20 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000972004062800097NE 2004 6 28 AALA20040653 220040613A7320J219P05A GASKET BOEING767 767323 1385205NM GE CF6 CF680C2B6 30025NE FUEL FLOW METER LEAKING A AALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW21387AM 27184 695621 GRU - INFLIGHT T0907 ON DESCENT THROUGH 22000 FEET RT ENGINE FLAMED OUT. ACCOMPLISHED AN INFLIGHT START WITHIN 2 MINUTES. DESCENDING THROUGH 6000 FT, RT ENGINE HAD UNCOMMANDED SHUTDOWN. ACCOMPLISHED SINGLE ENGINE LANDING. LANDED WITHOUT INCIDENT. FOUND FUEL LEAK FROM FLOWMETER FUEL TUBE SEAL GASKET. REPLACED THE SEAL GASKET AND FOUR BOLTS FOR RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20040628001112004062800111EA 2004 6 28 COMA0460365 120040610A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01912CA 7011 FLIGHT 5909 EMERGENCY FLOOR LIGHTS AT ROWS 2, 3 AND 4 ARE INOP. REPLACED STRIP LIGHT. 2L72 4F RTA21EA 20040628001302004062800130WP 2004 6 28 ABXA040194 120040520A52205912995503 PAN DOUG DC9 DC941 302207NWP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 LEFT FORWARD EMERGENCY EXIT DOOR PAN CRACKED FORWARD SIDE AT SECOND BEAM FROM THE BOTTOM. REPAIRED DOOR PAN IAW DC-9 SRM 52-05. 2L72 4F A6WE 20040628001322004062800132WP 2004 6 28 ABXA040198 120040525A534039240281 FITTING DOUG DC9 DC941 302207NWP FWD CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 LONGERON 30 END CAP CRACKED AT STA 644. REMOVED LONGERON 30 END CAP. DRILLED NEW END CAP IAW DC-9 SRM 51-10-4. INSTALLED NEW END CAP IAW DC-9 MM. 2L72 4F A6WE 20040628001382004062800138EA 2004 6 28 SWIA200413357 120040531A2752853D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07454SW3801 3801 7749 FLAPS FAIL MESSAGE APPEARED AFTER SELECTING FLAPS 30 DEGREES. REMOVED AND REPLACED R3 AND R4 FLAP ACTUATOR IAW 27-53-05. OPS CHECK GOOD. REF RII 27-412. P/N: 854D100-20, S/N 2274. 2L72 4F RTA21EA 20040628001412004062800141 2004 6 28 YENA200427 420040510A2565 PANEL AIRCRUISERS AIRBUS320 A320232 3930326EU ESCAPE SLIDE LOOSE A YENAO OTHER E VIBRATION/BUFFET CLCLIMB 1 EA15508JB147644140 A7348 1257 AIRFRAME VIBRATION NOTED IN FLIGHT, GW-138,000 LBS / AUTO THRUST ON/OFF, AIRSPEED - MACH .78 THRU .81 (IAS 250 KTS), ENGINE VIB 1 - 1.5 / 0.1, ENGINE VIB 2 - 1.6 / 0.3, PHASE OF FLIGHT - CLIMB & CRUISE, TURB / NO, NO ECAM OSCILLATION, AP 1 - ON SWITCHED TO AP 2 SAME RESULTS, VIBRATION SEEMS MORE PRONOUNCED IN THE AFT. INSPECTED ACFT FOR VIBRATION. AS A RESULT OF THIS TASK THE RT OFFWING EXIT SLIDE PANEL WAS LOOSE AND OUT OF LIMIT IAW AIR CRUISER CMM 25-60-58 FIG 505. A PORTION OF THE OFF WING SLIDE WAS FOUND TO BE PROTRUDING THROUGH THE FORWARD EDGE OF THE PANEL. OFF-WING SLIDE WAS REPLACED IN LOG PG 60154. A VIBRATION REPORTING SHEET HAS BEEN IN LOG BOOK TO TRACK FUTURE OCCURANCES. 2L72 4F RTA28NM 20040628001452004062800145EA 2004 6 28 COMA0470050 120040611A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX NOISY A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01625CA 10113 FLIGHT 5794 FLIGHT CREW HEARD THUD/BANG NOISE FROM CABIN DOOR AREA. INSPECTED CABIN DOOR AREA, PRESSURIZED AIRCRAFT, NO DEFECTS FOUND. 2L72 4F RTA21EA 20040628001472004062800147NM 2004 6 28 SWAA041740 120040621A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 747, STRINGER 8R AND STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040628001672004062800167EA 2004 6 28 04130695 120040509A335060205 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27695BR 7772 DURING INSPECTION THE GALLEY DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001722004062800172 2004 6 28 04139633 420040518A22136229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FLT CONTROL INTERMITTENT A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27633BR 7274 DURING AIRCRAFT OPERATION THE CREW REPORTED AN INTERMITTENT UNCOMMANDED YAW MOVEMENT. THE FLIGHT LANDED UNEVENTFULLY. THE FLIGHT CONTROL COMPUTER WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001822004062800182NM 2004 6 28 SWAA041754 120040622A53156545815 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, RBL 55 TO LBL 51, BS 344, LBL 55 TO BL 0, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORDS PER SRM. 2L72 4F RTA16WE 20040628001922004062800192 2004 6 28 SWAA041747 420040622A256565C34691 GIRT BAR BOEING737 7373Y0 1384671NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 R1 DOOR EVAC SLIDE GIRT BAR FELL OUT. INSTALLED R1 DOOR EVAC SLIDE GIRT BAR PER MM. 2L72 4F RTA16WE 20040628001972004062800197 2004 6 28 SWAA041760 420040622A25656557463 FITTING BOEING737 7373H4 1384600NM L1 DOOR GIRT BARCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT MOUNT FITTINGS, CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE GIRT BAR MOUNT FITTINGS PER SRM. 2L72 4F RTA16WE 20040628001992004062800199WP 2004 6 28 IXXA0400066O 120040609A3230 UPLOCK DOUG DC8 DC873F 302199FWP MLG LACK OF LUBE A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11602AL937752455 45991 ON DEPATURE FROM KBDL TO KTOL GEAR UPLATCH CHECK FAILED. THE GEAR NOT LATCHED LIGHT CAME ON AND NOSE GEAR CAME OUT OF THE WHEEL WELL. CREW COMPLETED FLIGHT TO KTOL AND LANDED WITH OUT INCIDENT. MAINTENANCE JACKED AIRCRAFT, INSPECTED, CLEANED AND LUBED UPLATCH MECHANISM. NO DEFECTS WERE NOTED. SWUNG GEAR AND PERFORMED UPLATCH CHECK AND OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040628002012004062800201EU 2004 6 28 AWXA200400507 120040512A3397ABS0374A24 TERMINAL AIRBUS320 A320231 3930325EU SEAT ROW 5 LT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28645AW 238 PHX - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE TERMINALS AT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040629000072004062900007NM 2004 6 29 04FDEA01628 120040607A5753 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING O/B FLAP STOP FITTINGS FOUND CRACKED. LT WING O/B FLAP STOP FITTING REMOVED AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040629000082004062900008NM 2004 6 29 04FDEA01629 120040607A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION ON FLOORBEAM AT BS 950, RBL 27.5, WL 208 UPPER FLANGE. 2L73 4F RTA3WE 20040629000302004062900030 2004 6 29 SWAA041771 420040624A2565D31354 SLIDE BOEING737 7372T4 1384492NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040629000372004062900037NM 2004 6 29 AWXA200400601 120040527A534069387902 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING C-15 CHECK A .5625 INCH CRACK WAS FOUND IN STRINGER TIE CLIP ON AFT SIDE OF BS 597, STR 11 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 597, STR 11 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-38790; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040629000382004062900038NM 2004 6 29 AWXA200400602 120040518A5340693535214 STRINGER CLIP BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 727B, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 4 RT FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PARA 4B. 2L72 4F RTA16WE 20040629000422004062900042NM 2004 6 29 04FDEA01650 120040609A5311AFA0016 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1621 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I. 2L73 4F RTA22WE 20040629000532004062900053WP 2004 6 29 04FDEA01655 120040609A5350ALC71081 PANEL DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 AFT FUSE LEFT SIDE BANANA PANEL HAS CORROSION. REMOVED AND REPLACED PANEL IAW SRM 51-31-01. 2L73 4F A22WE 20040629000642004062900064NM 2004 6 29 04FDEA01664 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000992004062900099NM 2004 6 29 AWXA200400616 120040531A532069165003 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT STIFFENER WEB (INTERCOSTAL) ABOVE STR 25 RT, BETWEEN BS 747 AND BS 767. MAINTENANCE REMOVED DAMAGED INTERCOSTAL FROM BS 747 TO BS 767, STR 25 RT; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-16500; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040629001002004062900100NM 2004 6 29 AWXA200400617 120040526A5320146N5318 SHEAR PLATE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON MAIN CABIN AFT SHEAR DECK UNDER G4B GALLEY AT BS 1715, BL 0 TO RBL 48. MAINTENANCE CUTOUT DAMAGE ON AFT SHEAR DECK BS 1715, BL 0 TO RBL 48; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-51, FIG 203 PG 204-208. 2L72 4F RTA2NM 20040629001022004062900102NM 2004 6 29 AWXA200400619 120040526A5320146N5318 SHEAR PLATE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK UNDER G4B GALLEY BETWEEN BS 1681 AND BS 1725, RBL 50. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK FROM BS 1681 TO BS 1725, RBL 50; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2L72 4F RTA2NM 20040629001032004062900103EA 2004 6 29 SWIA200413375 120040528A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE PULLEY INTERCOSTAL CLIP ANGLE CRACKED FS 484.00 RBL 27 O/B. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL CLIP REPLACED IAW CRJ REO 601R-53-41-059. 2L72 4F RTA21EA 20040629001042004062900104EA 2004 6 29 SWIA200413376 120040528A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE PULLEY INTERCOSTAL CLIP ANGLE CRACKED FS 484.00 LBL 27 O/B. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059. 2L72 4F RTA21EA 20040629001052004062900105EA 2004 6 29 SWIA200413377 120040528A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE INTERCOSTAL FITTING CRACKED AT FS 461 RBL 9 O/B. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21. 2L72 4F RTA21EA 20040629001072004062900107EA 2004 6 29 SWIA200413379 120040528A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE VERTICAL BEAM LWR I/B AND O/B FLANGE CRACKED AT FS 559 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV. NC. 2L72 4F RTA21EA 20040629001112004062900111NM 2004 6 29 04FDEA01688 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001172004062900117NM 2004 6 29 AWXA200400620 120040526A5320146N5318 SHEAR PLATE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK AT BS 1681 FROM BL 0 TO RBL 48. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK AT BS 1681 FROM BL 0 TO RBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2L72 4F RTA2NM 20040629001202004062900120NM 2004 6 29 AWXA200400623 120040526A5320146N5318 SHEAR PLATE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK AT BS 1715 FROM BL 0 TO LBL 48. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK AT BS 1715 FROM BL 0 TO LBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2L72 4F RTA2NM 20040629001212004062900121EU 2004 6 29 AWXA200400603 120040522A5320D5347112420000 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 MCN - MAJOR REPAIR - DURING C-03 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR AFT SHEAR PLATE BETWEEN FR 69 AND FR 70 AT AFT END OF BEAM Y1292 LT. MAINTENANCE REMOVED CORRODED CABIN FLOOR AFT SHEAR PLATE FROM FR 69 TO FR 70 AT BEAM Y1292 LT; FABRICATED A NEW REPLACEMENT SECTION OF AFT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3 & 8. 2L72 4F RTA28NM 20040629001222004062900122SO 2004 6 29 SWIA200413426 120040611A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07582SW8208 2043 120350 WHEN EMERGENCY LIGHT TESTED, MIDDLE ROW DOES NOT TURN ON. WHEN EMERGENCY LIGHT TURNED OFF AND AC POWER OFF, MIDDLE ROW LIGHTS TURN ON. REPLACED AND SECURED FORWARD CABIN EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040629001242004062900124EA 2004 6 29 SWIA200413428 120040611A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07906SW 7536 ONE CEILING EMERGENCY LIGHT INOP. REPLACED MAIN DOOR CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629001272004062900127EA 2004 6 29 SWIA200413432 120040411A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07449SW 7701 AP PITCH TRIM CAUTION MESSAGE ILLUMINATED DURING CRUISE FLIGHT. STAB TRIM CHANNEL 1 MESSAGE ILLUMINATED DURING FLIGHT WITH AUTOPILOT OFF. REMOVED AND REPLACED CO-PILOT'S PITCH TRIM DISCONNECT SWITCH PER AMM 27-41-03. OPERATIONAL CHECK GOOD PER AMM 27-40-00. 2L72 4F RTA21EA 20040629001282004062900128EA 2004 6 29 SWIA200413433 120040611A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07418SW 7446 CAPTAINS WINDSHIELD CRACKED ON TAXI IN. REMOVED AND REPLACED THE PILOT'S WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. P/N OFF NP-139321-1, S/N OFF 97007H5138. 2L72 4F4 FRTA21EA E15NE 20040629001292004062900129 2004 6 29 SWAA041781 420040618A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR WILL NOT TEST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29714CB 27848 DURING SPECIAL VISIT, R1 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE ASSEMBLY PER MM. 2L72 4F RTA16WE 20040629001312004062900131 2004 6 29 SWAA041783 420040627A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040629001332004062900133NM 2004 6 29 SWAA041785 120040625A3350100031 SIGN BOEING737 7373H4 1384600NM EMERGENCY EXIT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 FWD RT OVERHEAD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20040629001352004062900135NM 2004 6 29 SWAA041787 120040625A575465C26686 WEDGE BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER EA. 2L72 4F RTA16WE 20040629001362004062900136 2004 6 29 SWAA041788 420040625A25656557463 FITTING BOEING737 7373H4 1384600NM R2 DOOR SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTING ADAPTERS CORRODED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR ADAPTERS PER MM. 2L72 4F RTA16WE 20040629001402004062900140SO 2004 6 29 SWIA200413387 120040515A5320 BRACKET EMB 120 EMB120ER 3260203SO WINDOW FRAME CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07578SW 120346 FRAME 12 PILOT SIDE DV WINDOW FRAME CENTER AFT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FRAME 12 CENTER AFT BRACKET PILOT'S SIDE DV WINDOW. 2L72 4T RTA31SO 20040629001412004062900141EA 2004 6 29 SWIA200413388 120040602A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07452SW 7716 CARGO SMOKE MESSAGE ON TAXI. REMOVED AND REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS REF AMM 26-15-01. CARGO SMOKE TEST FUNCTIONS GOOD. P/N: 473597-19, S/N OFF: 2086, S/N OFF: 1315. 2L72 4F RTA21EA 20040629001432004062900143NM 2004 6 29 SWAA041789 120040625A534365C10300 FITTING BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND BOTH NLG ACTUATOR ROD FITTINGS, CORRODED. REPAIRED NLG FITTINGS PER ER. 2L72 4F RTA16WE 20040629001452004062900145NM 2004 6 29 SWAA041791 120040626A57536546435236 SKIN BOEING737 7372H4 138448CNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT FLAP PER MM. 2L72 4F A16WE 20040629001462004062900146NM 2004 6 29 SWAA041792 120040626A33501012624 BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED PM CHECK, FOUND LOW LEVEL EMERGENCY EXIT LIGHTS AT FWD ENTRY AND FWD SERVICE DOORS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040629001492004062900149NE 2004 6 29 SWIA200413396 220040606A7261 O-RING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 IDG LEAKING A SWIAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07944SW 7764 CREW HAD TO SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PSI. REMOVED AND REPLACED O-RINGS FOR IDG, STARTER, HYDRAULIC PUMP IAW CRJ MM CHAPTERS 80-11-01, 24-11-01, 29-11-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040629001502004062900150NM 2004 6 29 AWXA200400604 120040526A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 706, STRINGER 3 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 706, STRINGER 3 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20040629001522004062900152NM 2004 6 29 AWXA200400606 120040519A531365516989 SPLICE BOEING737 73733A 1384673NM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 3 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 907, STR 3 LT, WL 302; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040629001532004062900153NM 2004 6 29 AWXA200400607 120040517A533065C35777 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK 10 EACH CRACKS WERE FOUND ON UPPER AND LOWER FASTENER ROWS OF FUSELAGE SKIN LAP SEAM BETWEEN BS 950 AND BS 960, STR 20 LT, WL 192. MAINTENANCE REMOVED EXISTING DOUBLER & FILLER AND ENLARGED CUTOUT TO REMOVE CRACKED SECTION OF SKIN FROM BS 950 TO BS 960, STR 20 LT, WL 192; PERFORMED HFEC OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 129. 2L72 4F RTA16WE 20040629001542004062900154SO 2004 6 29 SWIA200413397 120040607A2710 ARM EMB 120 EMB120ER 3260203SO CONTROL WHEEL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07293SW 120320 DURING PREFLIGHT NOTICE A SIGNIFICANT BINDING IN THE CONTROL WHEEL WHEN AILERONS ARE USED RIGHT AND LEFT AND IN ALL POSITIONS OF THE ELEVATOR. REMOVED AND REPLACED RIGHT AILERON RVDT AND ARM IAW EMB MM 31-30-11. OPERATIONAL CHECK GOOD. P/N: D370519, S/N OFF: 00D00131. 2L72 4T RTA31SO 20040629001552004062900155EA 2004 6 29 SWIA200413398 120040606A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM07403SW 7028 RIGHT WINDOW CRACKED DURING PUSHBACK. REPLACED RIGHT WINDOW IAW 56-00-00, 56-12-01 AND RII56-402. P/N OFF NP-139322-6, S/N OFF 03169H6693. 2L72 4F RTA21EA 20040629001562004062900156SO 2004 6 29 SWIA200413399 120040609A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07288SW 120316 RIGHT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW 120 SRM 51-10-02 P2 SEC 2B. 2L72 4T4 TRTA31SO E20NE 20040629001572004062900157EA 2004 6 29 SWIA200413406 120040603A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07948SW1652 1652 7789 MACH TRIM DISENGAGED WOULD NOT RESET. REMOVED AND REPLACED HSTCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD PER MM 27-41-01. 2L72 4F4 FRTA21EA E15NE 20040629001582004062900158SO 2004 6 29 SWIA200413407 120040605A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 NM07157321369 1369 120195 AMBER ADVANCED SWS AND FLAP ON LANDING AND ALL 3 FLAP WARNING INDICATIONS. REMOVED AND REPLACED FLAP ANNUNCIATOR WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040629001592004062900159EA 2004 6 29 SWIA200413408 120040605A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07919SW 7657 RIGHT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EXTERIOR EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629001602004062900160EA 2004 6 29 SWIA200413443 120040613A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA MACH TRIM STUCK A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07967SW 7872 STAB TRIM 1 AND 2 AND MACH TRIM FAILED ON TAKEOFF. RETURNED TO FIELD, FOUND CO-PILOT TRIM DISCONNECT SWITCH JAMMED. RESET, OPS CHECKS GOOD. 2L72 4F RTA21EA 20040629001612004062900161EA 2004 6 29 SWIA200413444 120040520A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 FS 621 LEFT FLOOR SUPPORT ANGLE LBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV A AND RII53-401. 2L72 4F4 FRTA21EA E15NE 20040629001622004062900162EA 2004 6 29 SWIA200413445 120040520A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601RR-53-61-117 REV A AND RII53-401. 2L72 4F4 FRTA21EA E15NE 20040629001642004062900164EA 2004 6 29 SWIA200413447 120040604A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07928SW 7701 FUSELAGE FLOORBEAM ATTACH CLIPS ARE CRACKED; INBOARD AND OUTBOARD FS 280.0 RBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-42-13, 51-25-16, 51-42-13. 2L72 4F RTA21EA 20040629001662004062900166EA 2004 6 29 SWIA200413449 120040604A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07928SW 7701 AFT EQUIPMENT COMPARTMENT ENTRY HAS CRACKED ATTACH ANGLE; FS 700.00 LBL 13.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ SRM 53-61-23, 51-24-36, 51-24-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06. 2L72 4F RTA21EA 20040629001682004062900168EA 2004 6 29 SWIA200413424 120040611A2780 COMPUTER CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07702SK 10136 SLATS HALF SPEED MSG (STATUS) INFLIGHT. CLEANED MDC INHIBITS FOR SLATS SYSTEM. OPERATIONAL CHECK GOOD IAW FIM 27-81-00. 2L72 4F RTA21EA 20040629001702004062900170SO 2004 6 29 SWIA200413391 120040604A2460 RELAY EMB 120 EMB120ER 3260203SO APU BURNED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07233SW 120307 PILOT'S COMPLAIN OF BURNED ODOR IN COCKPIT. REMOVED AND REPLACED APU FEEDER PROTECTION RELAY IAW SRM 20-40-00 AND MM 24-52-00 FIG 7. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040629001712004062900171EA 2004 6 29 SWIA200413392 120040602A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07594SW 7285 STAB TRIM DISENGAGES AFTER TAKEOFF. REMOVED AND REPLACED THE CAPTAINS STAB TRIM DISCONNECT SWITCH IAW AMM 27-41-30. 2L72 4F RTA21EA 20040629001722004062900172EA 2004 6 29 SWIA200413393 120040604A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07440SW2924 2924 7589 SPOILERON FAULT STATUS MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED INBOARD SPOILERON PCU IAW 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629001762004062900176SO 2004 6 29 SWIA200413452 120040611A2120 ODOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE GALLEY DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07566SW 120341 ELECTRIC BURNING ODOR COMING FROM GALLEY. INSPECTED COFFEE POT PLUGS. SERVICED AND INSTALLED JUGS COULD NOT DUPLICATE. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20040629001792004062900179EA 2004 6 29 SWIA200413460 120040604A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV. B. 2L72 4F4 FRTA21EA E15NE 20040629001842004062900184EA 2004 6 29 SWIA200413382 120040528A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA BEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE VERTICAL BEAM LWR I/B FLANGE CRACKED AT FS 409+128 LBL 27. DISCOVERED DURING C-CHECK INSPECTION. CARRIED OUT REPAIR IAW CRJ REO 601R-53-41-056 REV. C. 2L72 4F RTA21EA 20040630000022004063000002NM 2004 6 30 USAA040231 120040516A5320 STIFFENER BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 STIFFENER (1 INCH X 1 INCH AREA) CORROSION; NO LEVEL/TASK NO LEVEL/TASK STA 1016 AT BL 0. CLEANED CORROSION AND TREATED AND PRIMED IAW SRM 53-00-01 FIG 101. 2L72 4F4 FRTA16WE E2GL 20040630000032004063000003NM 2004 6 30 USAA040205 120040506A5711 SPAR CAP BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US 24555 SPAR CAP CRACKED (.2187 INCH CRACK) WBL 157 LT WING UPPER SKIN AT AFT SPAR. 2L72 4F4 FRTA16WE E2GL 20040630000042004063000004NM 2004 6 30 USAA040206 120040506A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US51418 23316 SERVICE DOOR CUTOUT (.2500 INCH CRACK) AFT CORNER AT STA 332.101 FWD TO DOOR CUTOUT. REPAIRED IAW 53-10-01 FIG 202, PAGE 207. 2L72 4F RTA16WE 20040715000532004071500053 2004 7 15 SWIA200413515 420040617A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07290SW8842 8842 120317 TRIM FAIL LIGHT ILLUMINATED TWICE ON CLIMBOUT. DISCONNECTED THE AUTOPILOT TO FIND HEAVY NOSE DOWN CONTROL PRESSURE ON FLIGHT CONTROLS. REMOVED AND REPLACED THE ELEVATOR TRIM SERVO IAW MM 27-32-00 AND REMOVED AND REPLACED NR 1 APC 65B. OPS CHECKS GOOD. APC P/N: 622-8315-402, S/N OFF: 3788. 2L72 4T RTA31SO 20040715000552004071500055SO 2004 7 15 SWIA200413517 120040624A2612365000183 DETECTOR EMB 120 EMB120ER 3260203SO APU FIRE MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM0757734 120199 APU INOP FIRE DETECTION LIGHT ILLUMINATED ON TAXI. REMOVED AND REPLACED APU FIRE/OVERHEAT DETECTOR. OPS CHECK GOOD REF 26-12-01. P/N: 3601-90-4501180C, S/N OFF: 80388. 2L72 4T RTA31SO 20040630000082004063000008NM 2004 6 30 R342004F00000 120040427A7312320115 VALVE BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE ENG FUEL HEATER INOPERATIVE B R34RO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP23289MT 22467 666121 NR 1 OIL TEMP CLIMBED INTO CAUTION RANGE DURING CLIMBOUT AND WOULD NOT RETURN BACK TO NORMAL OPERATING TEMP. SHUTDOWN NR 1 ENGINE AS PRECAUTIONARY MEASURE AND RETURNED TO BASE. REMOVED MAIN OIL FILTER AND INSPECTED NO CONTAMINATION ON FILTER. TROUBLESHOOT ENG OIL SYS. FOUND FUEL HEAT BUTTERFLY VALVE OPEN AND LIGHT FOR OPEN POSITION DOES NOT INDICATE OPERATION. REMOVED AND REPLACED FUEL HEAT VALVE PN 320115, SYS OPERATES NORMAL NO FURTHER DISCREPANCIES ON FOLLOWING FLIGHTS. 2L73 4F4 F A3WE E2EA 20040630000112004063000011CE 2004 6 30 DEL2004F00000 120040504A143026520023 BOLT LEAR 35 31A 5170531CE GARRTTTFE731TFE7312B WP RT ENG AFT MOUNTCRACKED B DELRO OTHER O OTHER NRNOT REPORTED 1 CE03129FX3637 171 DURING ENGINE REMOVAL, FOUND RT ENGINE AFT MOUNT BOLT CRACKED (PN26520023). 2L72 4F4 FRTA10CE E6WE 20040630000122004063000012CE 2004 6 30 CED2004F00003 120040521A2810 FUEL SYS LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE LT WING TIP LEAKING E CEDAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 SW05140CA 140 ON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS RELEASED FOR TEST FLIGHT, NO DEFECTS WERE NOTED. 2L72 4J4 J A10CE 1E16 20040630000132004063000013CE 2004 6 30 BTA2004F00002 120040516A3240 BRAKE ASSY CESSNA500 550 2076604CE PWA JD15 JT15D1A NE MLG MALFUNCTIONED E BTAAO OTHER O OTHER NRNOT REPORTED 1 GL23223J 5500412 LOSS OF BRAKE ACTUATING FORCE, NO PRIOR BRAKE PROBLEMS INDICATED. UTILIZED EMERGENCY HAND BRAKE TO STOP AIRCRAFT. BLED BRAKES PERFORMED OPS CHECKS NUMEROUS TIMES. PERFORMED ANTI-SKID CHECK AND TAXI CHECKED. COULD NOT DUPLICATE. 1L72 4F4 F A22CE E25EA 20040630000152004063000015EU 2004 6 30 UO22004F00006 120040601A324025CX1225A LEVER BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE731* 01518WP FWD PRESS BKHD MISINSTALLED B UO2RO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL1946WC NA0334 PARKING BRAKE HANDLE WOULD NOT GO INTO THE FIRST DETENT WHICH ALLOWS USE OF THE EMERGENCY BRAKE SYSTEM AND USE OF THE PARKING BRAKE. ACCESSED PARKING BRAKE SYSTEM IN COCKPIT AND DETERMINED THAT THE SPLINED LEVER ASSEMBLY HAD COME OFF THE SPLINED SHAFT THAT GOES THROUGH THE PRESSURE VESSEL. DETERMINED THAT THE LEVER ASSEMBLY COULD NOT HAVE BEEN COMPLETELY INSTALLED AT BUILD DUE TO IT BEING PHYSICAL IMPOSSIBLE FOR THE LEVER ASSEMBLY TO COME OFF THE SPLINE WITH THE BOLT THROUGH THE LEVER ASSEMBLY. INSTALLED SHAFT INTO THE PROPER POSITION, REINSTALLED LEVER AND SAFETIED. 2L72 4F4 F A3EU E6WE 20040630000162004063000016NM 2004 6 30 USAA040243 120040601A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US51985 23314 SKIN CRACKED (1 INCH X Q.22 INCH) LOWER AFT CORNER FORWARD SERV CUTOUT STA 322, 4 INCH/ 14 INCH. INSTALLED DOUBLERS IAW SRM. 2L72 4F4 FRTA16WE E2GL 20040630000172004063000017EU 2004 6 30 USAA040248 120040526A5315D5347209001000 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 FLOORBEAM, 2.0 INCH X 2.0 INCH X .035 INCH D, CORROSION BETWEEN FR 64 &66, +Y 1270, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000182004063000018EU 2004 6 30 USAA040264 120040601A5320D5347219220 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 FLOOR SUPPORT/ RAIL, 2.25 INCH X 1.0 INCH X .088 INCH D, CORROSION; LEVEL 2; MAIN DECK, FRAME 68 AT +765. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM. 2L72 4F RTA28NM 20040630000192004063000019EU 2004 6 30 USAA040284 120040608A5321D5367179900000 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 FLOOR PANEL, GREATER THAN 10 PERCENT OF AREA, DELAMINATION, MAIN DELAMINATION, MAIN DECK FLOOR PANEL, 221PF. FABRICATED NEW PANEL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000222004063000022EU 2004 6 30 USAA040317 120040604A5320D5311278220201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW 0997 FLOOR SUPPORT, 2.0 INCH X 1.0 INCH X .026 INCH D, CORROSION; LEVEL 2 BETWEEN FR 21-22, Y1292, Z240. REMOVED AND REPLACED PART IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000252004063000025EA 2004 6 30 A6WA200440065 120040521A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 CLIP ANGLE AT FS 280.0 IB SIDE OF RBL 9 IS CRACKED. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PN 601R31113-58 IAW CRJ SRM 51-42-06 AND 51-42-21. 2L72 4F4 FRTA21EA E15NE 20040630000262004063000026EA 2004 6 30 A6WA200440068 120040527A3230 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG TRUNNION WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW10717 7257 MUC 44 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .020. REMOVED AND REPLACED LT MAIN LANDING GEAR AFT TRUNNION BUSHING IAW MFG REO 601R5721003 REV B. 2L72 4F4 FRTA21EA E15NE 20040630000282004063000028CE 2004 6 30 CED2004F00001 120040517A78106023T09G02 CASE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR 2 ENG EXHAUSTCRACKED E CEDAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW05239CA 25B149 WHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED WITH NO FURTHER INCIDENT. 2L72 4J4 J A10CE 1E16 20040630000292004063000029NM 2004 6 30 MYW2004F00002 120040521A2120 DUCT BOEING737 737800* NM GE CFM56 CFM56* 13802NE APU CONTAMINATED A C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO19733MA 30619 ON TAKEOFF THRUST, SMOKE IN COCKPIT AND CABIN. ABORTED TAKEOFF AND RETURNED TO HANGER. TROUBLE SHOT SYSTEM. ACCOMPLISHED AIR CONDITIONING PACK BITE CHECK. CHECK WAS NORMAL. REMOVED APU SUPPLY DUCT CONNECTOR TO CHECK FOR CONTAMINATION IAW 49-11-02. NONE FOUND. ACCOMPLISHED AC SYSTEM OIL CONTAMINATION REMOVAL IAW MM. ALL CHECKS NORMAL. RETURNED AIRCRAFT TO SERVICE. (SDR040011) 2L72 4F4 FRTA16WE E2GL 20040630000302004063000030SO 2004 6 30 SIMA200414203 120040520A27313621005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL PITCH TRIM FAILED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SW21620AE 145102 CREW HAD A DUAL PITCH TRIM FAILURE DURING DESCENT AT 210 KTS AND ALT OF 6,000 FT. FLAPS WERE AT 9 AND SPEED BRAKES WERE BEING DISENGAGED. REPLACED HSCU IAW MFG AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406970) 2L72 4T4 FRTT00011ATTE6CH 20040630000312004063000031NM 2004 6 30 MYW2004F00004 120040523A2611473925 CONTROL UNIT BOEING737 7378Q8 13844BXNM SMOKE DETECTORS SHORTED A MYWAK NONE L NO TEST ININSP/MAINT 1 SO19739MA 30670 DURING PREFLIGHT CHECK, FOUND AFT CARGO FIRE DETECTOR CIRCUIT BREAKER POPPED AND WOULD OT RESET. TROUBLESHOT SYSTEM. FOUND AFT CARGO SMOKE DETECTOR ELECTRONIC UNIT AT FAULT. REMOVED AND REPLACED ELECTRONIC UNIT. SYSTEM CHECKED NORMAL IAW 26-16-02. AIRCRAFT RETURNED TO SERVICE. (SDR040012) 2L72 4F RTA16WE 20040630000342004063000034EA 2004 6 30 A6WA200440064 120040521A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31432AW 7257 RT 718 FRAME FLANGE BETWEEN STRINGERS 11 AND 12 IS CRACKED. REPAIRED RT 718 LOWER FRAME FLANGE AT STRINGERS 11 AND 12 IAW MFG REO 601R-53-61-193 REV A. 2L72 4F4 FRTA21EA E15NE 20040630000352004063000035EA 2004 6 30 A6WA200440066 120040510A53206013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31434AW9049 7322 LT FS 625 OBLIQUE ANGLE ON INTERCOSTAL CRACKED. REMOVED AND REPLACED NEW INTERCOSTAL AT FS 625. 2L72 4F4 FRTA21EA E15NE 20040630000372004063000037EU 2004 6 30 A6WA200460017 120040528A5753 FLAP TRACK BAC 146 146300A 1500267EU LYC ALF502ALF502* 41580EA NR 2 FLAPS WORN A K NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 RT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908003. MAINTENANCE MAPPED AND SUBMITTED TO BE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6762/04-04-MK. NO CRACKS NOTED. DV INSPECTION DONE IAW BAE FAX BARA/AVR/6762/04-MK, NO DISCREPANCIES NOTED. (M) 2H74 4F4 FRTA49EU E6NE 20040630000392004063000039NM 2004 6 30 USA2004F00037 120040508A335020131A BATTERY PACK BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19300AU 23228 MAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040630000402004063000040SW 2004 6 30 ALG2004F00029 120040601A28222C271 PUMP BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL FUEL BOOST INOPERATIVE E ALGAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW03359AL 51461 DURING FLIGHT TO EL309 THE RIGHT BOOST PUMP CAUTION LIGHT ILLUMINATED AND RETURNED TO DEPARTURE. MAINTENANCE REMOVED BOOST PUMP AND INSTALLED SERVICEABLE BOOST PUMP, ALL WORK DONE IAW MM. 1G71 3U3 U H2SW E1GL 20040630000452004063000045GL 2004 6 30 ALG2004F00026 220040520A753223073353 BLEED VALVE CESSNASTC STC206C 1182107CE ALLSN 250C 250C30P 03013GL ENGINE INOPERATIVE E ALGAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW032611 6381 419 45417 WHILE TAKING OFF, HEARD POP AND AIRCRAFT YAWED, SYMPTOMS OF A COMPRESSOR STALL. LANDED STRAIGHT AHEAD AND HAD TOWER CALL AIRLOG OPS. MAINTENANCE REMOVED BLEED VALVE AND INSTALLED SERVICEABLE BLEED VALVE (PN 23073353)(SN FF44236). ALL WORK DONE IAW 206L-1MM AND RR MM. 1H71 3O3 UNTA4CE E1GL 20040630000462004063000046SO 2004 6 30 SIMA200412107 120040429A2120 ODOR EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW21840AE 145656 DURING LANDING, CREW REPORTED SMOKE AND ELECTRICAL ODOR IN COCKPIT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RAN ON GROUND WITH PACKS ON AND NO SMOKE REPORTED. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406986) 2L72 4F4 FRTT00011ATTE6CH 20040630000482004063000048EU 2004 6 30 DAT2004F00002 120040416A3242AC67750 CONTROL VALVE STBROSSD3 SD330 8100602EU PWA PT6 PT6* 52043EA BRAKE FAILED E DATAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL13334AC3647 SH3029 THE BRAKES WENT OUT ON THE GROUND. THE FLIGHT CREW LOST CONTROL AND HIT ANOTHER AIRCRAFT. THE RIGHT WING TIP HIT THE RT VERTICAL STABILIZER ON OTHER AC. MECHANICS WERE DISPATCHED, THE RT WING TIP WAS REMOVED AND REPLACED. THE BRAKE CONTROL VALVE WAS ALSO REMOVED AND REPLACED AND OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T3 T A41EU E2NE 20040630000492004063000049CE 2004 6 30 W322004F00001 120040519A32409550273C BRAKE ASSY LEAR 24 24 5170302CE MLG CRACKED E W32AO OTHER O OTHER NRNOT REPORTED 1 WP0739EL 24251 AIRCRAFT REPORTED LOSS OF HYDRAULIC PRESSURE AFTER FAILURE OF FLAPS TO DEPLOY. UPON INITIAL INSPECTION, HYDRAULIC FLUID WAS FOUND FLOWING FROM LT BRAKE ASSEMBLY. UPON REMOVAL FROM AIRCRAFT, BOTH BRAKE ASSEMBLIES WERE FOUND TO BE CRACKED IN IDENTICAL LOCATIONS, RADIATING FROM TRUNION BLOCKS TOWARD THE OUTER EDGES. CAUSE OF CRACKS AT THIS TIME ARE UNKNOWN, CAUSE COULD BE ATTRIBUTED TO POSSIBLE INSTALLATION ERROR. 2L72 4J A10CE 20040630000512004063000051NM 2004 6 30 FX72004F00001 120040523A3220 WARNING LIGHT BOEING737 737231 1384079NM PWA JT8 JT8D15 52051NE NLG ILLUMINATED G FX7AO OTHER J WARNING INDICATION CLCLIMB 1 SO1964346 21633 NOSE GEAR UNSAFE LIGHTS ON FRONT AND F/E PANELS STAYED ON RETURNED WITHOUT INCIDENT. JACKED A/C AND PERFORMED GEAR SWING IAW MM. NLG SWING PERFORMES NORMALLY. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENTS. 2L72 4F4 FRTA16WE E2EA 20040630000522004063000052SO 2004 6 30 SIMA200412001 120040426A335020131A BATTERY PACK EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21735TS 145386 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY THE FIRST FOUR ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406977) 2L72 4F4 FRTT00011ATTE6CH 20040630000572004063000057SO 2004 6 30 H2U2004F00001 120040513A1430AN723A BOLT MAULE MX7 MXT7160 5470204SO LYC O320 O320* 41508EA LT MLG STRUT BROKEN D H2USO OTHER O OTHER NRNOT REPORTED 1 SW11103HS2146 17007C LT IB MLG BOLT AND NUT THAT ATTACHES IB MLG TO AIRCRAFT FRAME CAME LOOSE AND FELL OUT. NUT IS (LOCKNUT PN AN365-720) (BOLT PN AN7-23A). WHEN BOLT CAME OUT IB MLG BROKE BOTTOM SKIN AND MLG PLASTIC FARRING. LOWER SKIN PANEL $80, FARRING $70 NO OTHER DAMAGE OCCURED. NEW IMPROVED ATTACH HARDWARE HAS BEEN ORDERED FROM MFG FOR ALL OUR AIRCRAFT. (SW11200406346) 1H71 3O3 O 3A23 E274 20040630000582004063000058NM 2004 6 30 UIEA200400100 120040528A575465B151803 CHANNEL BOEING747 747271C 1384869NM GE CF6 CF650* 30018NE NR 7 LE FLAP CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15537MC 22403 CENTER CHANNEL CRACKED BEYOND PRIVOUS REPAIR IB HINGE ON NR 7 LE FLAP. FOUND DURING VISUAL INSPECTION. CAUSE IS UNKNOWN. LOCATION IS WING STA 944.5. CORRECTIVE ACTION REPLACED LE FLAP ASSY IAW MM. 2L74 4F4 F A20WE E23EA 20040630000612004063000061CE 2004 6 30 UG8AGM0412 120040507A2730991444012 CONTROL UNIT CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL LT ELEVATOR SYS INOPERATIVE E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235115 3767 7500018 PITCH CONTROL PRESSURE IS EXCESSIVELY HIGH. THE LEFT ELEVATOR (A) SYSTEM PITCH CONTROL UNIT SHUTOFF SOLINOID HAD AN INTERNAL SHORT TO GROUND WHICH CAUSED HYDRAULIC PRESSURE TO BE SHUT OFF TO THE (A) SYSTEM PCU. THE HYDRAULIC DEACTIVATION OF THE (A) PCU, BY DESIGN, CAUSED THE SYSTEMS SINGLE HYDRAULIC SHUTOFF VALVE TO ALSO CUTOFF HYDRAULIC PRESSURE TO THE (B) SYSTEM PCU. REPLACED THE LT ELEVATOR (A) SYSTEM PITCH CONTROL UNIT. LT ELEVATOR OPERATION NOW NORMAL. 2L72 4J4 FRTT00007WITE6CH 20040630000642004063000064 2004 6 30 SIMA200414402 420040522A3140701700082407 COMPUTER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EICAS FAILED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21707EB 145195 IN CRUISE AT FL 290 CAPTAIN MULITFUNCTIONAL DISPLAY AND EICAS FAILED WITH BURNING ODOR. DIVERTED, OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200407047) 2L72 4F4 FRTT00011ATTE6CH 20040630000672004063000067SO 2004 6 30 SIMA200414401 120040521A27503632001003 DRIVE UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL TE FLAPS INOPERATIVE A SIMAO OTHER O OTHER LDLANDING 1 SW21845AE 145685 DURING LANDING, CREW DECLARED AN EMERGENCY DUE TO FLAP FAIL. FLAPS WERE AT 9 DEGREES AND NO INDICATION WAS SEEN IN COCKPIT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT FOR FLAPS. OPERATIONAL CHECK WAS GOOD IAW MM AND AIRCRAFT WAS RETURNED TO SERVICE. (SW212004046965) 2L72 4F4 FRTT00011ATTE6CH 20040630000682004063000068NM 2004 6 30 FX72004F00002 120040524A3230656021123 ACCESSORY UNIT BOEING727 727200 138407ENM PWA JT8 JT8D17 52049NE LT MLG MALFUNCTIONED A FX7AO OTHER J WARNING INDICATION CLCLIMB 1 SO19211DB 20766 AFTER T/O AND AFTER GEAR RETRACTION, LT MAIN GEAR RED LIGHT STAYED ON, RECYCLED GEAR DID NOT SOLVE PROBLEM AC RETURNED WITHOUT INCIDENT. T/S SYSTEM REPLACED LANDING GEAR ACCY. PERFORMED GEAR SWING IAW MM AND LANDING GEAR ACCY UNIT IAW MM. SYSTEM CHECKS GOOD, AC RETURNED TO SERVICE WITHOUT INCIDENT. 2L73 4F4 FRTA3WE E2EA 20040630000692004063000069NM 2004 6 30 RJE2004F00000 120040603A3246315301 WHEEL AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE LT MLG DAMAGED W RJEFK NONE O OTHER ININSP/MAINT 1 SO23477TA 1952 V11571 DURING TRANSIT CHECK OF FLIGHT 390 AT TGU STATION, IT WAS FOUND ONE TIRED WITHOUT PRESSURE AND ANOTHER ONE WITH A CUT IN THE SHOULDER. AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE AT TGU STATION. TECHS PERFORMED INSPECTION IAW AMM 05-51-15, AND FOUND MAIN WHEEL NR 3 DEFLATED AND MAIN WHEEL NR 1 WITH A CUT OUT OF LIMITS. NO OTHER DAMAGES WERE FOUND TO THE AIRCRAFT. WHEELS NR 1, NR 2, NR 3, AND NR 4 WERE REPLACED IAW MM. AIRCRAFT RETURNED TO NORMAL OPERATION. 2L72 4F4 FRTA28NM E40NE 20040628000202004062800020NM 2004 6 28 04147426 120040526A3350321430 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27426FJ 3190 DURING INSPECTION THE EMERGENCY LIGHTS IN THE CENTER OF CABIN WERE FOUND INOPERATIVE. THE BATTERY PACK WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA55NM 20040628000252004062800025SO 2004 6 28 SWIA200413405 120040515A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07288SW 120316 RIGHT ENGINE FRAME NR 1 IS CRACKED ON OUTBOARD SIDE. DISCOVERED AT C-CHECK. INSTALLED NEW RIGHT ENGINE FRAME NR 1 IAW SB 120-54-0036 AND RII CARD RII54-301. 2L72 4T4 TRTA31SO E20NE 20040628000262004062800026NM 2004 6 28 AALA20040688 120040622A3397 WIRE HARNESS BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21379AA 25448 DFW - EMERGENCY LIGHT AT SEAT 13HJ INOPERATIVE. INSTALLED SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040628000422004062800042 2004 6 28 SWAA041763 420040623A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29785SW 30602 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040628000442004062800044EA 2004 6 28 SWIA200413434 120040611A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07958SW 7833 SPOILER FAULT CAUTION MESSAGE ON TAXI. REMOVED AND REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD PER CRJ MM 27-61-05. 2L72 4F RTA21EA 20040628000552004062800055SO 2004 6 28 SWIA200413416 120040610A5610 WINDSHIELD EMB 120 EMB120ER 3260203SO COCKPIT FAILED A SWIAO OTHER O OTHER TXTAXI/GRND HDL 1 NM07581SW 120349 CAPTAIN'S WINDSHIELD SHATTERED DURING TAXI. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-01. P/N: NP151311-1, S/N OFF: 98183H1103. 2L72 4T RTA31SO 20040628000622004062800062NM 2004 6 28 04133410 120040512A3350 BATTERY DORNERDO32 DO328300 NM EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27410FJ 3165 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHTING WAS FOUND WORKING INTERMITTENTLY. THE BATTERY WAS REPLACED AND A SATISAFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040628000632004062800063NM 2004 6 28 AALA20040654 120040614A3350 LIGHT BOEING757 757223 1384957NM L2 DOOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21697AN 26977 MIA - EMERGENCY LIGHT AT L2 DOOR INOPERATIVE. REPOSITIONED EMERGENCY LIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040628000642004062800064WP 2004 6 28 AALA20040656 120040615A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217521A 49898 FORWARD EMERGENCY LIGHT AT COCKPIT OVERHEAD INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR FORWARD EMERGENCY LIGHT AT COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040628000702004062800070EU 2004 6 28 AALA20040658 120040618A33506040681 POWER UNIT FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211421K 11404 EWR - EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK UNIT FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040628000782004062800078EA 2004 6 28 04129646 120040508A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INOPERATIVE A VTZAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 EA27646BR 7392 DURING AIRCRAFT OPERATION THE CREW REPORTED A FLAP CONTROL FAILURE MESSAGE AT 0 DEGREES. THE FECU AND BPSU WERE REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000802004062800080EA 2004 6 28 04152664 120040531A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 DURING INSPECTION THE RIGHT AFT OVERWING EMERGENCY EXIT LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628000982004062800098WP 2004 6 28 AALA20040652 120040613A2170 COALESCER BAG DOUG DC9 DC983 3022083WP RT PACK CONTAMINATED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21438AA 49456 SFO - INFLIGHT T1907 SMOKE IN CABIN REPORTED SOON AFTER TAKEOFF. TURNED RECIRCULATION FAN OFF AND NO SMOKE VISIBLE. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. FOUND RT PACK LEAKING OIL. REPLACED RIGHT HAND COALESCER BAG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040628001062004062800106NM 2004 6 28 DHL2004754003 120040510A5754 MOUNT BOEING727 727223 1384074NM K-FLAP ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01754DH 22008 DURING A C-CHECK, RT WING NR 6 KRUEGER FLAP ACTUATOR MOUNT IS CRACKED AT LOWER CORNERS. REMOVED ACTUATOR MOUNT, FABRICATED REPLACEMENT PART 7075-T6, .063, PO 900861 (8 X 3 INCH) IAW B727 SRM 57-20-02 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-02 AND INSTALLED PART IAW B727 SRM 51-30-02. 2L73 4F A3WE 20040628001092004062800109NM 2004 6 28 TSAA0427042 120040529A2750 CONTROL CABLE BOEING737 7372M6C 1384708NM TE FLAPS OUT OF ADJUST A TSAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP13805AL 21809 AT 34,000 FT DURING CRUISE THE L/E FLAP TRANSIT LIGHT CAME ON, AUTO-PILOT KICKED OFF AND ON DESCENT THE CONFIGURATION HORN CAME ON. RETURNED TO HNL. ADJUST FLAP CABLE WFA & WFB TENSION IAW AMM 27-51-01 AS ADDRESSED BY BOEING SERVICE LETTER 27-040. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040628001172004062800117 2004 6 28 SWIA200413366 420040528A22166225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07227SW9538 9538 120304 AUTOPILOT DRIFTS OFF COURSE. REPLACED AILERON SERVO WITH SERVICEABLE UNIT. ALL FUNCTIONAL CHECKS GOOD. 2L72 4T RTA31SO 20040628001252004062800125NM 2004 6 28 AWXA200400592 120040602A3397BR963180 WIRE HARNESS BOEING737 7373G7 1384595NM SEAT ROW 18 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - EEL - DURING 4-DAY CHECK FOUND A WIRE PULLED OUT OF CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT. MAINTENANCE REMOVED AND REPLACED THE WIRE HARNESS FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040628001272004062800127NM 2004 6 28 DHL2004752004 120040519A2611100064901 SMOKE DETECTOR BOEING727 727223 1384074NM CARGO BAY MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01752DH 22466 IN FLIGHT LOWER CARGO FIRE DETECTION. FOUND SMOKE DETECTOR S/N: 8650, TO BE GIVING FALSE WARNING. REMOVED AND REPLACED ALL 5 FORWARD SMOKE DETECTORS IAW B727 M/M 26-16-01, REMOVED AND REPLACED CENTRAL CONTROL UNIT (CCU) IAW B727 M/M 26-16-20, OPS CHECKED SERVICEABLE IAW B727 M/M 26-16-01. 2L73 4F A3WE 20040628001372004062800137EA 2004 6 28 SWIA200413356 120040525A2741 PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07916SW 7634 STAB CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED STAB TRIM ENGAGE PANEL. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040628001392004062800139EU 2004 6 28 DHL2004364514 120040311A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN DECK COURIER AREA HAS CORROSION EVIDENCE ON FLOOR PANEL SUPPORT/SEAT TRACK FROM APPROX FR 14 TO FR 19 LBL 36 (MARKED). REMOVED CORROSION FROM FLOOR PANEL SUPPORT (SEAT TRACK) BETWEEN FR 14 TO FR 19, LBL 36 IAW A-300 SRM 51-40-11. MAT LOSS APPROXIMATELY 0.030, FOUND TO BE OUT OF LIMITS IAW A-300 SRM 53-10-00 FIG 612 (NOMINAL THICKNESS 0.090). REMOVED DAMAGED SEAT TRACK SECTION FROM FRAME 14 TO FRAME 19 LBL 36, IAW A-300 SRM 51-30-30. TRIM NEW SEAT TRACK EXTRUSION TO FIT, MATERIAL USED P/N 60-22457, PO 23236312 IAW A-300 SRM 51-27-00 AND 51-30-40. TREATED AND PRIMED AND POLIWHITE SEAT TRACK IAW A-300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION IAW A-300 SRM 51-30-30 AND 51-10-40. 2L72 4F RTA35EU 20040628001512004062800151NM 2004 6 28 PCAA0405207 120040517A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY INOPERATIVE A PCAAO OTHER L NO TEST ININSP/MAINT 1 EA13810EX20967563 308 DURING TEST BY MAINTENANCE IT WAS REPORTED THAT THE NR 1 BAGGAGE SMOKE DETECTOR DID NOT TEST. MAINTENANCE REMOVED AND REPLACED THE UNIT, ALL SYSTEMS TEST NORMAL. 2H72 4T RTA13NM 20040628001562004062800156CE 2004 6 28 DXTA200400316 120040531A323062420107 FRICTION BRAKE CESSNA650 650 2076802CE LANDING GEAR OVERTORQUED E DXTAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL07791QS4547 6507091 AFTER TAKEOFF COULD NOT RETRACT LANDING GEAR, GEAR HANDLE WOULD NOT MOVE. FOUND NOSE GEAR FRICTION BRAKE TOO TIGHT, NOT ALLOWING NOSE STEERING TO CENTER WHEN STRUT IS EXTENDED. ADJUSTED NOSE GEAR FRICTION BRAKE IAW CESSNA 560 MM CHAPTER 32-20-00, PERFORMED SEVERAL GEAR SWING, OPS CHECKED GOOD AT THIS TIME. 2L72 4F A9NM 20040628001692004062800169EA 2004 6 28 04132638 120040511A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27638BR 7311 DURING INSPECTION AN OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001702004062800170EA 2004 6 28 04132675 120040511A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 DURING INSPECTION THE LEFT HAND FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001732004062800173NE 2004 6 28 04150324 220040529A7200310349016 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RIGHT INOPERATIVE A VTZAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA27324UE 41017 76099 DURING CLIMB OF FLIGHT 7459 CREW REPORTED A RT ENGINE FAILURE. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO FIELD UNEVENTFULLY. THE RT ENGINE WAS CHANGED AND A SATISFACTORY FUNCTIONAL CHECK WAS ACCOMPLISHED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA41NM E18NE 20040628001742004062800174EA 2004 6 28 04151671 120040530A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27671BR 7572 DURING INSPECTION THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001752004062800175EA 2004 6 28 04153645 120040601A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27645BR 7383 DURING INSPECTION THE LT NR 1 AND NR 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001762004062800176WP 2004 6 28 0400979959 120040611A2170 DUCT DOUG DC9 DC931 3022065WP WATER SEPARATOR DISCONNECTED A NWAAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 GL01919RW 47162 WHILE CRUISING AT FL330, THE CABIN ALTITUDE CLIMBED TO 11,000 FT. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO BNA. CABIN STOPPED CLIMBING AND MAINTAINED 11,000 FEET UNTIL AIRCRAFT PASSED 15,000 FEET THEN CABIN STARTED DESCENDING AND OPERATED NORMALLY UNTIL JUST PRIOR TO LANDING. AFTER LANDING, THE CABIN PRESSURE AUTO FAIL LIGHT ILLUMINATED AND REMAINED ON UNTIL ENGINE WAS SHUT DOWN. LANDING AT BNA WAS UNEVENTFUL. MAINTENANCE FOUND THE LT DUCT OFF AND AFT END OF THE WATER SEPARATOR AND RESECURED IT. CHECKED SECURITY OF THE RIGHT DUCT. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO MENTION OF COM OR BITE IN LOGPAGE. 2L72 4F A6WE 20040628001882004062800188NM 2004 6 28 SWAA041744 120040621A53126546547599 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED PM CHECK, FOUND BULKHEAD AT LEFT BS 727, LEFT MLG W/W FLAP MOTOR ATTACH, CRACKED. REPAIRED BULKHEAD PER EA. 2L72 4F A16WE 20040628001892004062800189EA 2004 6 28 04149672 120040528A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27672BR 7594 DURING INSPECTION THE LEFT HAND FUSELAGE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001942004062800194 2004 6 28 SWAA041748 420040622A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29089SW 22904 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040629000112004062900011WP 2004 6 29 04FDEA01632 120040607A5754 RIB DOUG DC10 DC1010 3022110WP SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN LEADING EDGE SLAT RIB ARB1092-1. COMPLIED WITH EA 8-5710-77417 WINGS REWORK OF GOUGE IN WING LEADING EDGE SLAT RIB ARB1092-1. 2L73 4F A22WE 20040629000312004062900031EU 2004 6 29 AWXA200400595 120040603A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU SEAT ROW 15 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28605AW 543 PHX - EEL - DURING 4-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT FAILED FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT SEAT TO WALL HARNESS AT SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040629000362004062900036NM 2004 6 29 AWXA200400600 120040526A534069414372 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 DURING C-15 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 663.75, STRINGER 10 RT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 663.75, STRINGER 10 RT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIGS 8 & 12. 2L72 4F RTA16WE 20040629000432004062900043WP 2004 6 29 04FDEA01651 120040609A5753ARC25172 HINGE DOUG DC10 DC1010 3022110WP ZONE 600 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 COMPLY WITH EA 8-5750-78223, WINGS INBOARD FLAP, AFT HINGE ASSY, REWORK OF GOUGED ARC2517-2 STRAP. COMPLIED BY EA 8-5750-78223, WINGS INBOARD FLAP, AFT HINGE ASSY. 2L73 4F A22WE 20040629000482004062900048NM 2004 6 29 SWAA041772 120040624A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND PHOTOLUMINESCENT STRIPS AT BS 336 AND BS 948, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER ACO. 2L72 4F RTA16WE 20040629000502004062900050NM 2004 6 29 SWAA041774 120040624A53116550568 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 986 TO BS 992, RBL 46, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2L72 4F RTA16WE 20040629000652004062900065NM 2004 6 29 04FDEA01666 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.096. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000672004062900067NM 2004 6 29 SWAA041777 120040624A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED HC1 CHECK, BATTERY AT RIGHT CENTER EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY AND CHARGER PER MM. 2L72 4F RTA16WE 20040629000752004062900075EA 2004 6 29 SWIA200413453 120040619A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07915SW5264 5264 7615 STAB TRIM CH 1 DISENGAGED IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT, IAW CRJ MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040629000812004062900081NM 2004 6 29 04FDEA01670 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000842004062900084NM 2004 6 29 04FDEA01673 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.490, REMAINING THICKNESS=0.488, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000922004062900092NM 2004 6 29 04FDEA01681 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.497, REMAINING THICKNESS = 0.495, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000942004062900094NM 2004 6 29 04FDEA01683 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.513, REMAINING = THICKNESS = 0.511, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000952004062900095NM 2004 6 29 04FDEA01684 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001102004062900110NM 2004 6 29 04FDEA01687 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.399, REMAINING = THICKNESS = 0.397, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001252004062900125SO 2004 6 29 SWIA200413430 120040610A5610 WINDOW EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT CRACKED A SWIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM07214SW 120280 LEFT CAPTIANS SIDE WINDOW CRACKED ON GROUND. REMOVED AND REPLACED LEFT SIDE WINDSHIELD IAW MM 56-10-01. PN: NP151311-1, S/N OFF: 00108. 2L72 4T4 TRTA31SO E20NE 20040629001262004062900126EA 2004 6 29 SWIA200413431 120040609A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07923SW 7664 PASSENGER DOOR EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629001322004062900132 2004 6 29 SWAA041784 420040625A2565D31591478 SLIDE BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 L1 DOOR EVAC SLIDE GIRT BAR LOOSE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040629001372004062900137EA 2004 6 29 SWIA200413384 120040528A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 INTERCOSTAL BETWEEN FS 621 AND 625 ADJACENT STR 14 RIGHT IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW CRJ SRM 51-40-11, 51-40-06. 2L72 4F RTA21EA 20040629001672004062900167EA 2004 6 29 SWIA200413423 120040608A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS ILLUMINATED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07918SW 7645 FLT SPOILERS FAULT STATUS MSG CYCLES ON AND OFF, TAXIED BACK TO GATE. PERFORMED FAULT ISOLATION PROCEDURES OF FLIGHT SPOILERS SYSTEM. NO DEFECTS NOTED. 2L72 4F RTA21EA 20040629001742004062900174EA 2004 6 29 SWIA200413450 120040505A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 CARGO PIT STEP PLATE ASSEMBLY SUPPORT IS BROKEN OUT ALONG INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. SUPPORT REPLACED IAW CRJ SRM 51-41-02. 2L72 4F RTA21EA 20040629001832004062900183EA 2004 6 29 SWIA200413381 120040528A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA BEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE VERTICAL BEAM LWR O/B FLANGE CRACKED AT FS 409+128 LBL 9. DISCOVERED DURING C-CHECK INSPECTION. CARRIED OUT REPAIR IAW CRJ REO 601R-53-41-056 REV. C. 2L72 4F RTA21EA 20040630000012004063000001NM 2004 6 30 USAA040199 120040426A531065C3760727 VERTICAL SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US 23318 SUPPORT (1.5 INCH CRACKED) CRACKED. VERTICAL SUPPORT AT LBL 5.7. 2L72 4F RTA16WE 20040630000062004063000006CE 2004 6 30 J0U2004F00001 120040524A2510 CABLE BEECH MU300 400A 1155402CE LUMBAR SUPPORT BROKEN B J0URO OTHER O OTHER NRNOT REPORTED 1 SO0925CU 224 RK361 PILOT REPORTED NO LUMBAR SUPPORT FOR CREW SEAT. ADJUSTMENT USING CONTROL KNOB MADE NO DIFFERENCE IN SUPPORT. REMOVED AFT UPHOLSTERY FROM SEAT AND FOUND CONTROL CABLE BROKEN. SUGGEST USING HEAVIER CABLE. 2H72 4F RTA16SW 20040630000092004063000009NM 2004 6 30 USAA040230 120040516A5310 LAP JOINT BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 .2500 INCH DIA. AREA OF CORROSION ON LAP JOINT AT STA 1016 BL 0. REMOVED RIVET AND CLEANED CORROSION AROUND RIVET HOLE AND REINSTALLED RIVET IAW SRM, FIG 1. 2L72 4F4 FRTA16WE E2GL 20040630000272004063000027NM 2004 6 30 MYW2004F00003 120040521A3350RPS1B POWER SUPPLY BOEING727 727212 138407GNM PWA JT8 JT8D17 52049NE L2 DOOR WEAK A MYWAK NONE L NO TEST ININSP/MAINT 1 SO19727NK 21945 DURING PREFLIGHT TRANSIT FOUND WHITE EMERGENCY DOOR LIGHTS AT L-2 AFT DOOR VERY WEAK. REMOVED AND REPLACED POWER SUPPLY BATTERY CHARGER ASSY. OPS CHECK OK IAW MM 33-50-02. (SDR040010) 2L73 4F4 F A3WE E2EA 20040630000442004063000044SO 2004 6 30 SIMA200411201 120040419A1420 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A SIMAO OTHER L NO TEST NRNOT REPORTED 1 SW21635AE 145158 DISC - FWD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406984) 2L72 4T4 FRTT00011ATTE6CH 20040630000552004063000055SO 2004 6 30 SIMA200414201 120040517A27503632001003 CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL TE FLAPS FAILED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21639AE 145182 ON APPROACH, CREW SELECTED FLAPS TO 9 DEGREES AT WHICH POINT THEY RECEIVED FLAPS FAIL MSG AND FLAPS FAILED TO MOVE. DECLARED EMERGENCY AND LANDED SAFELY WITH 0 FLAPS. FPDU OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200406985) 2L72 4T4 FRTT00011ATTE6CH 20040630000622004063000062SW 2004 6 30 ALG2004F00028 120040513A712023069751 MOUNT BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE WORN E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03527AL669 53211 DURING TIME CHANGE OF ENGINE ASSEMBLY. REAR ENGINE MOUNT BEARING ON THE SUPPORT HAS EXCESSIVE WEAR, ALSO THE BEARING HOUSING HAS EXCESSIVE PLAY WHICH IS BEYOND LIMITS. 1G71 3U3 UO H2SW E1GL 20040630000662004063000066SO 2004 6 30 SIMA200414601 120040523A335020131A POWER SUPPLY EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21735TS 145386 TOP AND LOWER LT EXIT LIGHTS ON SERVICE DOOR WILL NOT REMAIN ILLUMINATED. REPLACED NR 2 BATTERY POWER SUPPLY. AC RETURNED TO SERVICE. (SW21200407048) 2L72 4F4 FRTT00011ATTE6CH 20040630000702004063000070NM 2004 6 30 UIEA200400102 120040604A541265B941091 BULKHEAD BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 1 NACELLE CRACKED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D-CHECK, DURING MAINTENANCE INSPECTION. NR 1 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND W.L. 146.5, ALSO THE STRUT SKIN ASSEMBLY AT THE AFT LOWER ACCESS CUT OUT EDGE ADJACENT TO THE STRAP CRACK LOCATION WAS FOUND WITH CHAFING DAMAGE. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. THE SKIN ACCESS CUT OUT EDGE CHAFING DAMAGE WAS REMOVED BY BLENDING. REPAIR DOUBLERS WAS FABRICATED FROM 0.063 INCH THICK TITANIUM SHEET WERE INSTALLED COMMON TO THE STRUT OUTER SKIN ASSEMBLY USING MECHANICAL FASTENERS. 2L74 4F4 F A20WE E23EA 20040630000752004063000075 2004 6 30 USAA040260 420040524A2565D5311201600100 PAD AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE GIRT BAR FITTINGCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW13221 0844 ADAPTER PAD, 11 INCH X 2 INCH X 0.050 INCH, CORROSION; LEVEL 2; AFT GIRT BAR FITTING, R1 DOOR, FR 19-20, Z240, Y1293. REPLACED PORT GIRT BAR FITTING ADAPTER IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000782004063000078NM 2004 6 30 USAA040200 120040503A5313 STRINGER BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US 23930 STRINGER (.2500 INCH X .1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02. 2L72 4F4 FRTA16WE E2GL 20040630000852004063000085NE 2004 6 30 A6WA200440069 220040529A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 2 MALFUNCTIONED A A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31403AW 7288 NR 2 ENGINE N2 OVERSPEED BEYOND 100 PERCENT INDICATION ERRATIC AND UNCONTROLABLE EVEN WHEN SELECTED TO FLIGHT IDLE. COMPLIED WITH QRH, ENGINE SHUTDOWN. TAT -41C ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 ENGINE STATOR, GROUND RAN. ALL ENGINE INDICATIONS WITHIN LIMITS. IAW FIM 72-00-00, PG 1305. 2L72 4F4 FRTA21EA E15NE 20040630000862004063000086EU 2004 6 30 USAA040234 120040520A5320D5347112420100 SHEAR WEB AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW 0890 SHEAR WEB, 8 INCHES X 3 INCHES X .040 INCH DEEP. CORROSION THRU WEB FR 69-70, Y200, Z240. REMOVED AND REPLACED SHEAR WEB IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000872004063000087EU 2004 6 30 USAA040237 120040521A5320D5361019900100 SUPPORT ANGLE AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW 0890 SUPPORT ANGLE ASSY, .95 INCH X .50 INCH AREA, CORROSION; LEVEL 2 Z240,Y1732, X=843. REMOVED AND REPLACED SUPPORT ANGLE ASSY IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000892004063000089 2004 6 30 USAA040233 420040521A2565D5348015900500 GIRT BAR AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE ESCAPE SLIDE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW 0890 PLATE (GIRT BAR) 1.30 INCHES X .50 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-26053500, FR 68, Z240, Y1230. EXFOLIATED ON OB EDGE, REMOVED AND REPLACED PLATE IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000912004063000091EU 2004 6 30 USAA040238 120040521A5315D5347217220290 FLOORBEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW 0890 FLOORBEAM, 1.3 INCH X 1.9 INCH X .35 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA26053500, FR68, Y1300MM, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000942004063000094CE 2004 6 30 H8A2004F00000 120040521A3233353800943 MOTOR BEECH 35 V35 1151538CE CONT O520 IO520* 17032SO MLG INOPERATIVE B H8ARO OTHER O OTHER NRNOT REPORTED 1 EA052082W D8008 PILOT REPORTED, COULD NOT LOWER GEAR ELECTRICALLY, PILOT PERFORMED EMERGENCY EXTENSION SUCESSIVELY. UPON INSPECTION OF LANDING GEAR FOUND MOTOR INOPERATIVE. BRUSHES WERE COMPLETELY WORN OUT, REPLACED MOTOR. 1L71 3O3 O 3A15 E5CE 20040630001022004063000102EU 2004 6 30 USAA040235 120040520A5315D5347217220390 FLOORBEAM AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW 0890 FLOORBEAM, 1.0 INCH X 0.950 INCH X 0.055 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA260535, FR 66-68, Y1200, Z240. REPLACED WITH NEW FRAME IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001032004063000103 2004 6 30 A6WA200440070 420040601A3497601R57729IPE1 COAX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RADAR ALTIMETER FAILED A O OTHER O OTHER NRNOT REPORTED 1 GL31402AW 7281 RADAR ALT ERRONEOUS INDICATIONS ON CLIMB TOO LOW TERRAIN AND PULL-UP SOUNDED INTERMITTENT. GLD UNSAFE AMBER CASS, COMPLIED WITH QRH. REPLACED RAD ALT TRANSMIT AND RECEIVE COAX CABLES. SYSTEM CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20040630001052004063000105NM 2004 6 30 GAIA04077OP 120040427A3230656021136 ACCESSORY UNIT BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE E/E BAY MALFUNCTIONED A GAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL116833 20186 RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN UP POSITION. RECYCLED GEAR AND NO CHANGE. MADE OVERWEIGHT LANDING WITH LOW SINK RATE. LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. UNIT OPS CHECKS GOOD. RT MLG UNSAFE LIGHT EXTINGUISHED. PERFORMED OVERWEIGH LANDING INSPECTION. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040630001082004063000108NE 2004 6 30 OEJ2004F00000 220040524A732032447593 FUEL CONTROL CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE RT ENGINE FAILED G OEJAO OTHER O OTHER NRNOT REPORTED 1 SW1553FT 3360 5500276 FUEL CONTROL FAILED, FUEL CONTROL REPLACED. ENGINE OPERATIONS NORMAL. (SW15200410518) 1L72 4F4 F A22CE E1NE 20040630001102004063000110EU 2004 6 30 USAA040249 120040526A5315D5347218820200 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 FLOORBEAM, 2.0 INCH X 2.0 INCH X .025 INCH D, BETWEEN FR 68-69, Y1270, Z240, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001112004063000111EU 2004 6 30 USAA040254 120040528A5315D53472172203 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW13221 0844 FLOORBEAM, 2.5 INCH X 1.5 INCH X .030 INCH DEEP, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001232004063000123NM 2004 6 30 USAA040201 120040504A5312 INTERCOSTAL BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE AFT PRESS BLKHD CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19375US 22954 BULKHEAD, INTERCOSTAL (5 INCH WIDE X 7 INCHES TALL) CORROSION; NO LEVEL OR TASK NR STA 1016 AFT PRESS BULKHEAD AT LOWER AREA, BL 0 . REPAIRED IAW EO5302V112A, DOUBLER INSTALLATION. 2L72 4F4 FRTA16WE E2GL 20040630001262004063000126EU 2004 6 30 USAA040257 120040521A5315D5347209200000 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 FLOORBEAM, 1.0 INCH X 1.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FRAME 64 & 66, +Y787, Z240. 2L72 4F4 FRTA28NM E2GL 20040630001272004063000127EU 2004 6 30 USAA040259 120040522A5315D5347219320000 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 FLOORBEAM, 1.5 INCH X 1.0 INCH X .02 INCH DEEP, CORROSION; LEVEL 2; FR 66-68, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001282004063000128EU 2004 6 30 USAA040319 120040609A5311D5311283020200 FRAME AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FRAME, .090 INCH X .090 INCH X .026 INCH AREA, CORROSION; LEVEL 2; FR16, Y81, Z240. NEW FRAME ASSY INSTALLED IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001302004063000130EU 2004 6 30 USAA040258 120040521A5315D53472090000200 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW13221 0844 FLOORBEAM, 3.0 INCH X 2.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FR66-68, +Y762,Z240. REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001322004063000132EU 2004 6 30 USAA040318 120040610A5311D5347209001000 FRAME AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW 0997 FRAME , 3.0 INCH X 1.5 INCH X .040 INCH AREA, CORROSION, LEVEL 2; FR66, Y1292, Z240. INSTALLED NEW FRAME IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001352004063000135NM 2004 6 30 USA2004F00046 120040505A2131 CONTROLLER BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE CABIN PRESSURE MALFUNCTIONED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19518AU 23704 ENROUTE, CREW REPORTED VIA ACARS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CONTROL PRESSURIZATION. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA16WE E2GL 20040630001362004063000136EU 2004 6 30 USA2004F00044 120040514A3350321430 BATTERY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19707UW 0949 THE RT SIDE EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE MID CABIN RT SIDE EMERGENCY POWER SUPPLY UNIT BATTERY. OPS CHECKED OK. 2L72 4F4 FRTA28NM E2GL 20040630001372004063000137NM 2004 6 30 USA2004F00045 120040520A2121 FAN BOEING757 7572B7 1384964NM RECIRCULATION FAILED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19614AU 27145 ON CLIMB-OUT, CREW RECEIVED THE (E/M`R ENG EEC) AND LIGHT. AS THE CREW TROUBLESHOT THE PROBLEM, AND ELECTRICAL ODOR WAS NOTED IN THE COCKPIT. CREW DONNED OXYGEN MASKS, AND BEGAN A RETURN. THE SMOKE DISSIPATED, AND THEN RETURNED PRIOR TO LANDING. THE CABIN CREW ALSO NOTED A LIGHT HAZE AND SMELL NEAR THE L2 DOOR. MAINTENANCE PERFORMED NUMEROUS CHECKS IN THE CABIN AND COCKPIT, INCLUDING INSPECTING CIRCUIT BREAKER PANELS AND AVIONICS COMPARTMENTS, RUNNING THE PACKS AND PNEUMATIC SYSTEM. THE RT RECIRCULATION FAN WAS FOUND TO BE OPERATING INTERMITTENTLY. FURTHER ACTION PENDING. 2L72 4F RTA2NM 20040630001392004063000139CE 2004 6 30 BAQR361C 120040602A324611580014 WHEEL BEECH 100 A100 1152915CE PWA PT6 PT6A60A 52043NE MLG DAMAGED B BAQRO OTHER O OTHER NRNOT REPORTED 1 EA03777GS 64 B241 WHEEL HAD 64.9 HOURS, 106 LANDINGS SINCE OVERHAULED. 1L72 3T4 T A14CE E4EA 20040630001422004063000142NM 2004 6 30 USA2004F00050 120040517A2780 FLAP BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE LE MALFUNCTIONED A USAAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 EA19385US 22958 ON APPROACH, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ASSOCIATED WITH A YELLOW TRANSIT LIGHT ON THE NR 3 LEADING EDGE SLAT. CAPTAIN REPORTED THE FLAPS WOULD NOT EXTEND PAST 15 UNITS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AN EMERGENCY WAS DECLARED. MAINTENANCE CHECKED WIRING AND FOUND NO DEFECTS. OPERATED LEADING EDGE AND TRAILING EDGE DEVICES NUMEROUS TIMES. NORMAL OPERATION NOTED. 2L72 4F4 FRTA16WE E2GL 20040630001432004063000143NM 2004 6 30 USA2004F00051 120040505A2133322684003 OUTFLOW VALVE BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19518AU52758 23704 ENROUTE, CREW REPORTED CABIN ALTITUDE WARNING HORN SOUNDED AS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CNTRL PRESS. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT FOUND FWD OUTFLOW VALVE FAILED IN OPEN POSITION. REPLACED VALVE IAW MM. ALSO FOUND AND REPAIRED LEAKS AT RT PACK MIX VALVE (HOT SIDE) AT FUSELAGE PEN IN PACK BAY, AFT DRAIN MAST, ALL (4) CABIN DOORS, REPLACED LEAKING PRESS REG VALVE FOR AVIONICS EQUIP COOLING AND REPLACED LT A/C MIX VALVE FOR INTERMITTENT OPS. ACCOMPLISHED SATISFACTORY OPS CK OF PRESSURE CNTRL SYS IAW MM AND SINGLE PACK. AC OK FOR SERVICE.2L72 4F4 FRTA16WE E2GL 20040630001442004063000144NM 2004 6 30 AMTA200400570 120040518A2420 IDG BOEING757 75733N 1384931NM RROYCERB211 RB211* 54555NE GENERATOR DISCONNECTED A AMTAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 GL11554TZ11595 A1250 32588 GEN DRIVE AND DRIVE WARNING LIGHT FLICKERS. IDG WAS DISCONNECTED. REMOVED AND REPLACED NR 1 ENG IDG IAW M57-24-01. 2L72 4F4 FRTA2NM A12EU 20040630001462004063000146CE 2004 6 30 MV52004F00000 120040519A2750S229440 LINK CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE FLAP CABLE SHEARED B MV5RO OTHER O OTHER NRNOT REPORTED 1 GL11848D 3915 5500039 WHILE PERFORMING FLAP RIGGING CHECK FOR AC, THE LT DOWN CABLE TO CHAIN MASTER LINK WAS FOUND TO BE SHEARED AT THE OB AFT PIN. AFTER CAREFUL INSPECTION CORROSION WAS FOUND ACROSS THE PIN INDICATING THE PIN HAD BEEN CRACKED FOR SOME TIME. FURTHER INVESTIGATION FOUND THE FWD LINK ON THE LT FLAP ALSO WAS SHEARED. THE DAMAGE WAS NOT NOTICEABLE UNTIL THE CHAIN AND CABLE WERE MOVED FOR CABLE TENSION CHECK REVEALING ONLY A SLIGHT INDICATION OF A PROBLEM. IT IS SUSPECTED THE CABLES WERE NOT TENSIONED TIGHT ENOUGH, ALLOWING THE CABLE TO CHAIN MASTER LINK TO RIDE UP INTO THE SPROCKET CAUSING THE DAMAGE. (GL11200410769) 1L72 4F4 F A22CE E1NE 20040630001472004063000147EU 2004 6 30 USAA040309 120040608A5321D5367175900300 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, PANEL 262EF. FABRICATED NEW FLOOR PANEL 262 EF. 2L72 4F4 FRTA28NM E2GL 20040630001512004063000151CE 2004 6 30 CED2004F00002 120040519A2612872281 FIRE DETECTOR LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE NR 1 ENGINE MALFUNCTIONED E CEDAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05273CA 039 AFTER TAKEOFF AT FLIGHT LEVEL 220 THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STARNDARD EMERGENCY PROCEDURES AND RETURNED WITHOUT FURTHER INCIDENT. ONCE BACK IN MAINTENANCE FOUND THE FIRELOOP ELEMENT TOUCHING THE COWLING GIVING A FALSE FIRE INDICATION. 2L72 4J4 J A10CE 1E16 20040630001542004063000154NM 2004 6 30 QXEA200400406 120040606A27207G7921 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 300 INOPERATIVE A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09360PH 515 PDX - ON FLIGHT NUMBER 2092, ON TAKEOFF ROLL AFTER POWER WAS APPLIED AT ABOUT 50 KIAS, THE RUD FULL PRESSURE CAUTION LIGHT ILLUMINATED. THE LIGHT HAD EXTINGUISHED WHEN THE TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 2 RUD FULL PRESSURE SWITCH ON THE RUDDER DUAL PRESSURE REGULATOR. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630001552004063000155EA 2004 6 30 QXEA200400408 120040608A2613 LOOP CNDAIRCL600 CL6002C10 1390015EA ZONE 300 OUT OF POSITION A QXEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM09611QX 10041 GEG - ON FLIGHT NUMBER 4216, ON TAKEOFF ROLL THE RIGHT BLEED DUCT MASTER WARNING LIGHT CAME ON. ABORTED TAKEOFF AND THE MASTER WARNING LIGHT WENT AWAY AND THEN RECEIVED RIGHT BLEED DUCT MASTER CAUTION LIGHT. THE EVENT HISTORY SHOWS THE MT146R WITH NO PRESENT FAULTS. RE-POSITIONED LOOPS AWAY FROM DUCT COVERS. GROUND RAN AIRCRAFT WITH NO WARNING OR CAUTION MESSAGES. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040630001592004063000159NM 2004 6 30 AALA20040634 120040520A2930019012001 TRANSMITTER BOEING767 767323 1385205NM LT ENGINE DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21355AA 24036 DFW - LEFT HAND HYDRAULIC MESSAGE SHOWED QUAINTY FLUCUATING. REPLACED LEFT HAND QUAINTY TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040630001612004063000161CE 2004 6 30 HAEA00146 120040609A2130 PRESSURE SWITCH LEAR 24 24D 5170311CE CABIN PRESSURE FAULTY E HAEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW05295TW1029210292 24D266 AIRCRAFT DEPARTED SDF AND THE CABIN WOULD NOT PRESSURIZE. AIRCRAFT RETURNED SDF. LANDING NORMAL. 2L72 4J A10CE 20040630001622004063000162NM 2004 6 30 QXEA200400394 120040605A2420 CONNECTOR DHAV DHC8 DHC8202 2809007NM ZONE 100 DIRTY A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09368PH 512 SEA - FLIGHT 2168 - NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT. RESET SWITCH AS PER CHECKLIST. LIGHT THEN WENT OUT FOR REMAINDER OF FLIGHT. CLEANED CONNECTORS ON NR 1 AC GENERATOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630001632004063000163NM 2004 6 30 QXEA200400393 120040604A335061047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09348PH5393 440 484 PDX - AFT CEILING EMERGENCY LIGHT AND AFT RIGHT HAND OUTSIDE EMERGENCY LIGHT ARE INOPERATIVE. REMOVED AND REPLACED PS4 BATTERY POWER SUPPLY. 2H72 4T RTA13NM 20040630001652004063000165NM 2004 6 30 WRLA200424 120040321A335060441105 BATTERY DOUG MD11 MD11 3023602NM ZONE 100 DISCHARGED A WRLAK NONE L NO TEST ININSP/MAINT 1 SO11277WA 48743 DURING REGULAR LINE MAINTENANCE CHECK ON AIRCRAFT N272WA AT LAX, MAINTENANCE FOUND THE EMERGENCY LIGHT TEST BATTERY NR 1 WAS LOW. MAINTENANCE AT LAX REMOVED AND REPLACED THE BATTERY & THE CONTROLLER PER MD-11 MM 33-51-00 & 31-42-00, OP'S CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA22WE 20040630001662004063000166NM 2004 6 30 C8GA20040005 120040609A2612MS280341 SENSOR BOEING727 727223 1384074NM NR 2 ENGINE FAILED A C8GAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO15899AA 22015 FLT 2161 FROM KDFW TO KMCI. AFTER TAKEOFF FROM DFW, THE LOWER AFT CARGO FIRE WARNING CAME ON. ALSO, THE NR 2 ENGINE DUCT OVERHEAT LIGHT ON IN FLIGHT. FOLLOW ALL CCIA AOM ABNORMAL PROCEDURES AND AIR TURNBACK TO DFW. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS THEN INSPECTED AND DEFERRED THE AFT CARGO COMPARTMENT FIRE DETECTION UNDER MEL 26-19 AND DEFERRED THE NR 2 ENGINE BLEED SYSTEM UNDER MEL 36-6-2. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 26-19 BY FUNCTIONALLY TESTING THE LOWER CARGO SMOKE DETECTION SYSTEM PER SECURAPLANE ST3000 MANUAL WITH NO MALFUNCTION FOUND. CHECKED ALL DETECTORS DB LEVELS IN SSV MODE, ALL DETECTORS LEVELS WERE ABOVE MINIMUM LEVELS. CLEARED MEL 36-6-2 BY REPLACING THE TEMPERA2L73 4F A3WE 20040630001672004063000167NM 2004 6 30 PCAA0406217 120040609A323282970018013 ACTUATOR DHAV DHC8 DHC8102 2809003NM RT MLG DOOR FAULTY A PCAAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA13806EX3198511702 263 FLIGHT 3555 REPORTED THE RIGHT MAIN GEAR DOOR REMAINING OPEN AFTER TAKEOFF. GEAR WAS CYCLED ONCE AND THE DOOR CLOSED. MAINTENANCE FOUND THE RIGHT HAND FORWARD GEAR DOOR ACTUATOR TO BE AT FAULT. ACTUATOR WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630001682004063000168NM 2004 6 30 TSAA045204506 120040608A3350BACR13CT2AB RELAY BOEING737 73773A 1384606NM EMERGENCY LIGHT FAILED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13739AL 28500 FLIGHT 442, HNL-OAK: RIGHT OVERWING EXIT DOOR OPEN LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF REJECTED. PSEU SELF-TEST INDICATES MSG 52-76018. DEFER RIGHT OVERWING EXIT FLIGHT-LOCK PER MEL 52-15, PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE. PERFORM FIM TASK 52-20-00-810, ALL BITES AND OPS CHECKS PASS WITH NO VISIBLE FAULT. OK FOR CONTINUED SERVICE, PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE. PSEU SELF-TEST INDICATES FAULT 52-76018. PERFORMED FIM 52-20 TASK 807, REPLACED RELAY R743, REPAIR CONFIRMATION OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040630001692004063000169NM 2004 6 30 TSAA0452045 120040608A5270BACR13CT2AB RELAY BOEING737 73773A 1384606NM EMERGENCY EXIT FAILED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13739AL 28500 FLIGHT 442, HNL-OAK: RIGHT OVERWING EXIT DOOR OPEN LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF REJECTED. PSEU SELF-TEST INDICATES MSG 52-76018. DEFER RIGHT OVERWING EXIT FLIGHT-LOCK PER MEL 52-15, PLACARDS INSTALLED. AIRCRAFT RETURNED TO SERVICE. PERFORM FIM TASK 52-20-00-810, ALL BITES AND OPS CHECKS PASS WITH NO VISIBLE FAULT. OK FOR CONTINUED SERVICE, PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE. PSEU SELF-TEST INDICATES FAULT 52-76018. PERFORMED FIM 52-20 TASK 807, REPLACED RELAY R743, REPAIR CONFIRMATION OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040630001712004063000171NM 2004 6 30 PCAA0406220 120040609A3297 WIRE DHAV DHC8 DHC8102 2809003NM RT MLG CHAFED A PCAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA13846EX 326 FLIGHT 4096 REPORTED THE RIGHT MAIN GEAR DOOR LIGHT ILLUMINATING DURING TAXI. MAINTENANCE IN PITTSBURGH WAS UNABLE TO REPAIR, AND A FERRY PERMIT ISSUED TO MIDDLETOWN. MAINTENANCE FOUND A CHAFED WIRE BETWEEN PROXIMITY SENSOR CONTROL UNIT CANNON PLUG PIN 36 AND THE ADVISORY LIGHT CONTROL BOX CANNON PLUG PIN 22. WIRE WAS REPAIRED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630001732004063000173EA 2004 6 30 QXEA200400409 120040608A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - MAIN CABIN DOOR OUTER SKIN HAS SEVERAL SCRATCHES WITH METAL SHOWING. REPAIRED IAW CRJ SRM 51-25-01, SRM 52-11-01, AND SRM 53-00-01. 2L72 4F RTA21EA 20040630001742004063000174NM 2004 6 30 P5CA0401101 120040609A361020109ZJ6 LINE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE BLEED AIR LOOSE A P5CAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP23355MC 23395 530389 DURING CLIMBOUT NR 4 ENGINE FIRE LIGHT ILLUMINATION AND FIRE BELL SOUNDED. ENGINE SHUT DOWN, BOTTLES NOT FIRED. FOUND SENSE LINE OFF PRV. SECURED LINE & CHANGED UNION PER MM 36-11-19. OPERATIONAL CHECK OK. 2L74 4F4 FRTA20WE E23EA 20040630001752004063000175EU 2004 6 30 U30A200400007 120040605A2120 ODOR AIRBUS320 A320214 3930316EU CABIN DETECTED A U30AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA17263AV 1860 AFTER T/O, F/A NOTICED ODOR & HAZE VIEWED FROM FWD CREW SEATS IN AFT PORTION OF A/C. VERIFIED SAME CONDITIONS AFT. ADJUSTED AIR CONDITIONING SYS TO INCREASE AIRFLOW AND ELIMINATE ODOR & HAZE. HAZE & ODOR BEGAN TO CLEAR, TEN MINS LATER HAZE & ODORS RETURNED. DIVERT INTO PHL. PERFORMED FUMES REMOVAL CHECKLIST, HAZE/FUMES CLEARING, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT, ALL PAX DEPLANED. TROUBLESHOT SYS & COULD NOT DUPLICATE. ENGS RAN 1 HR AT DIFFERENT POWER SETTINGS, COULD NOT DUPLICATE. INSPECTED APU FOR LEAKS & OIL SERVICE WITH NO DEFECTS. INSPECTED ENG FOR EXTERNAL LEAKS & OIL SERVICE WITH NO DEFECTS. INSPECTED AIR CONDITIONING PACK BAYS FOR DEFECTS, NO DEFECTS. A/C RETURNED TO SERVICE. 2L72 4F RTA28NM 20040630001762004063000176WP 2004 6 30 P9RA20040018 120040610A2910NAS16128 O-RING DOUG DC9 DC982 3022082WP HYD SYSTEM LEAKING A P9RAO OTHER K FLUID LOSS CRCRUISE 1 SO11135NJ 49440 EN ROUTE IAH-CUN, LOST RIGHT HYDRAULIC PRESSURE IN FLIGHT. QRH FOLLOWED, NO EMERGENCY DECLARED. REMOVED AND REPLACED O-RINGS IN THE TUBES OF THE SPOILER BYPASS VALVE IAW MM 29-10-26 AND SERVICED HYDRAULIC SYSTEM, WHICH WAS LOW, TO NORMAL LEVELS. AIRCRAFT REPOSITION CUN-IAH AS A MAINTENANCE PRECAUTIONARY. CHECK AND REPLACE RETURN AND CASE DRAIN FILTERS IN RIGHT HYDRAULIC SYSTEM. REMOVED AND REPLACED RETURN AND CASE DRAIN FILTERS IN RIGHT HYDRAULIC SYSTEM. NO DISCREPANCIES NOTED. 2L72 4F A6WE 20040630001772004063000177NM 2004 6 30 PCAA0406221 120040604A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY INTERMITTENT A PCAAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING NRNOT REPORTED 1 EA13840EX 327 FLIGHT 3909 REPORTED THE BAGGAGE BAY SMOKE WARNING AS BEING INTERMITTANTLY ACTIVATED. MAINTENANCE TROUBLESHOT AND DISABLED THE FAULTY DETECTOR IN THE BAGGAGE BAY. ITEM WAS MEL'D UNTIL PARTS COULD BE OBTAINED. ALL OTHER ASSOCIATED SYSTEMS WERE TESTED AND IN WORKING ORDER. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630001782004063000178NM 2004 6 30 P5CA0401102 120040609A36108988061 RELIEF VALVE BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 4 ENGINE LEAKING A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23355MC 23395 530389 DURING A/C CLIMBOUT AT 23,000 FT, NR 4 ENGINE NACELLE TEMPERATURE WAS INDICATING 8 UNITS. ACCOMPLISHED PROCEDURE FOR ABNORMAL NACELLE TEMPERATURE RETURNED TO NORMAL. NACELLE TEMPERATURE FLUCTUATED WITH THROTTLE MOVEMENT. REMOVED AND REPLACED PRESSURE REGULATING VALVE, HIGH STAGE VALVE AND PRESSURE RELIEF VALVE PRECAUTIONARY. 2L74 4F4 FRTA20WE E23EA 20040630001812004063000181NM 2004 6 30 PCAA0406219 120040609A3350 WIRE DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHTSBROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13824EX 387 WHILE IN MAINTENANCE DURING THE TEST PROCEDURE IT WAS FOUND THAT TWO FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE LEADING TO THE POWER SUPPLY. WIRE WAS REPAIRED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS WERE GOOD. 2H72 4T RTA13NM 20040630001852004063000185NM 2004 6 30 TSAA0427044 120040602A278238180010011003 ACTUATOR BOEING737 73773A 1384606NM LE SLAT FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13738AL15232 28499 FLIGHT 482, HNL-SNA: L/E FLAP TRANSIT LIGHT REMAINED ON AFTER TAKEOFF, QRH COMPLETED AND RETURN TO HNL. WEIGHT ON LANDING APPROXIMATELY 150,000 LBS, LOW SINK RATE AT TOUCHDOWN. FOUND THE NR 2 AND NR 5 SLAT ACTUATORS INTERNALLY BYPASSING, REPLACED NR 2 AND NR 5 SLAT ACTUATORS IAW AMM 27-81-41-4. LEAK AND OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING PHASE I INSPECTION IAW AMM 05-51-35-2, NO DEFECTS NOTED. AIRCRAFT RETURNED SERVICE. 2L72 4F RTA16WE 20040630001862004063000186NM 2004 6 30 N150AW0008 120040525A5312 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 DRILL MARK ON AFT PRESSURE BULKHEAD AT RBL 37.5 AT THE MOISTURE BARRIER RETAINER. REPAIRED PER SRM 53-80-08. 2L72 4F RTA16WE 20040630001892004063000189NM 2004 6 30 F3LA200400067 120040603A2780 CONTROL MODULE BOEING737 7373L9 1384470NM FLAP/SLATS INOPERATIVE A F3LAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03313FL 2625 26442 ABORTED TAKEOFF. FLIGHT CREW REPORTED L/E FLAPS TRANSIT LIGHT ILLUMINATED WITH NR 2 SLAT ON OVERHEAD PANEL SHOWING INTRANSIT. TAKEOFF ABORTED AT 111 KIAS. REPLACED FLAP/SLAT MODULE PER MM 27-88-41. CHECKED TARGET TO EXTEND SENSORS ON NR 2, 3 AND 5 SLATS PER MM 27-88-11. CHECKED NORMAL. COMPLIED WITH HIGH ENERGY INSPECTION PER MM 05-51-07, PAGES 201-203 (5). COMPLIED WITH RTO INSPECTION PER MM 05-51-07 AND 22-88-41. OPERATIONAL TEST WAS NORMAL ON FLAP/SLAT SYSTEM. 2L72 4F RTA16WE 20040630001902004063000190NM 2004 6 30 N150AW00170 120040525A5320 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 L-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2. 2L72 4F RTA16WE 20040630001912004063000191NM 2004 6 30 N150AW0017 120040525A5320 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 L-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2. 2L72 4F RTA16WE 20040630001932004063000193NM 2004 6 30 UPS04242555 120040527A5740 TEE FITTING BOEING727 72725C 138400HNM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, TEE FITTING CRACKED ON UPPER I/B T-EDGE PANEL FOR APU EXHAUST 70.5 WBL. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-10-2. 2L73 4F A3WE 20040630001952004063000195NM 2004 6 30 UPS04242557 120040531A5751 WEB BOEING727 72725C 138400HNM LT I/B AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, LEFT I/B AILERON, O/B WEB CRACKED AT AFT UPPER FASTENER, AND FASTENER MISSING FROM WEB. REPAIR CARRIED OUT IAW 51-30-02. 2L73 4F A3WE 20040701000012004070100001NM 2004 7 1 SWAA041816 120040628A5315BAC150910046 FLOORBEAM BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727D + 6', LBL 2 TO RBL 7, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040701000022004070100002NM 2004 7 1 SWAA041817 120040628A53116546546 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 847, RBL 14, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040701000042004070100004NM 2004 7 1 SWAA041819 120040628A53156546808 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53.52, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F RTA16WE 20040701000052004070100005NM 2004 7 1 SWAA041820 120040628A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT RIGHT BS 616, WL 208, CRACKED. REPAIRED FRAME CHORD PER ER. 2L72 4F RTA16WE 20040701000102004070100010NM 2004 7 1 SWAA041825 120040629A53306552988 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 946, STRINGER 24L. REPAIRED SKIN PER SWS EA. 2L72 4F RTA16WE 20040701000112004070100011NM 2004 7 1 UPS04442552 120040610A3510 COUPLER BOEING747 747121 1384871NM 02 BOTTLE LEAKING A IPXAO OTHER O OTHER CRCRUISE 1 SO01683UP 20353 INSPECTION TYPE:N/A CREW 02 INDICATOR F/E PANEL SLOWLY DECREASED FROM 1200 TO 0 AFTER 3.5 HOURS OF FLIGHT. SYSTEM PRESS GAUGE SIDE WALL WENT TO 0 PSI. REMOVED AND REPLACED LOWER & UPPER 02 BOTTLES AS PER MM 35-10-00, FOUND UPPER BOTTLES COUPING LEAKING. PART ON ORDER, REMOVED AND REPLACED UPPER CYLINDER 02 REGULATOR, LEAK CHECK C/W NORMAL. 2L74 4F A20WE 20040701000122004070100012NM 2004 7 1 QXEA200400410 120040609A335082520975109 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09353PH 496 BOI - ON FLIGHT NUMBER 2202, THE EMERGENCY STRIP LIGHTING IN THE CABIN BY ROW 1 HAS TWO WIRES STICKING OUT. REMOVED AND REPLACED EMERGENCY LIGHT STRIP ASSEMBLY AT ROW 1 TO ROW 2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040701000132004070100013NM 2004 7 1 QXEA200400392 120040604A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09355PH 500 PDX - EMERGENCY TRACK LIGHTING FORWARD SIX INCH RED SECTION IS BROKEN. REMOVED AND REPLACED EMERGENCY TRACK LIGHTING. 2H72 4T RTA13NM 20040701000162004070100016 2004 7 1 513NA0007 420040607A2210 INDICATOR BOEING757 7572T7 1384914NM AUTO LAND MALFUNCTIONED A PIDAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO05513NA 23895 ON DESCENT INTO KSFB, NO AUTO LAND DISPLAYED ON AUTO LAND STATUS INDICATOR. RESET RIGHT FCC AND RAN MCDP TEST PER MM 22-10-00. ALL AUTO PILOT ENGAGE AND FCC CHECKS GOOD. 2L72 4F RTA2NM 20040628001122004062800112EA 2004 6 28 COMA0460366 120040607A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA MAIN LACK OF LUBE A COMAO OTHER WJ INADEQUATE Q C WARNING INDICATION APAPPROACH 1 SO01709CA 7238 FLIGHT 5334 GEAR DISAGREE WARNING, WHEN SELECTED DOWN. CLEAN AND LUBED LANDING GEAR. 2L72 4F RTA21EA 20040628001182004062800118SO 2004 6 28 SWIA200413367 120040525A2120 SMOKE EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07298SW 120328 DURING CRUISE, AFTER SETTING CRUISE POWER AND PACKS TO NORM CABIN FILLED WITH SMOKE. LAV SMOKE ALARM ACTIVATED. RAN RIGHT PACK ON GROUND FOR SEVERAL MINUTES, PACK OPERATES NORMAL. COULD NOT DUPLICATE DISCREPANCY. 2L72 4T RTA31SO 20040628001292004062800129WP 2004 6 28 ABXA040192 120040519A5330591141265 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 FUSELAGE SKIN EXFOLIATED/BULGING FROM FS 636 - 664, LONGERON 29 LEFT - 29 RIGHT. REMOVED CORROSION IAW DC-9 SRM 51-10-3. REPAIRED IAW DC-9 SRM 53-04. 2L72 4F A6WE 20040628001332004062800133WP 2004 6 28 ABXA040193 120040520A52205912995504 PAN DOUG DC9 DC941 302207NWP EMERGENCY EXIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 RIGHT AFT EMERGENCY EXIT DOOR PAN CRACKED FORWARD SIDE TOP BEAM. REPAIRED DOOR PAN IAW DC-9 SRM 52-05. 2L72 4F A6WE 20040628001362004062800136EA 2004 6 28 SWIA200413355 120040525A2720 RUDDER PEDAL CNDAIRCL600 CL6002B19 1900309EA COCKPIT OUT OF ADJUST A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07951SW 7795 WHEN MOVING RUDDER PEDALS FOR TAXI CHECK, CLICKING NOISE HEARD AND FELT ON CAPTAIN'S SIDE ONLY. REMOVED AND REPLACED RUDDER PEDAL ADJUSTMENT ROD AND SCREW ACTUATOR IAW MM 27-21-01. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040628001402004062800140NM 2004 6 28 DHL2004783009 120040516A5330 SKIN BOEING727 727227 1384078NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 DENT FOUND IN LEFT AFT SIDE OF AIRCRAFT AT STATION 1110 & 1130 AT STRINGER S24 & S25. REMOVED DAMAGE AREA, FABRICATED DOUBLER, & INSTALLED AS PER 727 SRM 53-30-01. PERFORMED PRESSURE CHECK IAW 21-31-0. CHECK OK. 2L73 4F A3WE 20040628001422004062800142NM 2004 6 28 QXEA200400337 120040520A521085217003001 DOOR BOMBDRDHC8 DHC8401 1390041NM PAX JAMMED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX5705 4060 BOI - FLIGHT 2404 - CREW REPORTS THAT THE AFT PASSENGER DOOR IS JAMMED. MAINTENANCE INSPECTED THE AIRCRAFT DOOR AND SECURED THE LOOSE TRIM ON THE ARTICULATING ARM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040628001502004062800150NM 2004 6 28 PCAA0405206 120040515A79308SC0062 TRANSMITTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 OIL PRESS FAULTY A PCAAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA13811AW 201 120827 FLIGHT 3778 NOTICED A/C WAS LOSING OIL PRESSURE IN THE NR 1 ENGINE DURING CLIMB AT 1000 FEET. CREW SHUTDOWN THAT ENGINE AND DECLARED AN EMERGENCY AND DIVERTED TO ROCHESTER. FLIGHT WAS HEADING FROM BUFFALO TO LGA. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE SWAPPED NR 1 AND NR 2 OIL PRESSURE INDICATORS AND TRANSMITTERS FOR TROUBLESHOOTING PURPOSES, THEN REPLACED THE AFFECTED NR 1 OIL PRESSURE TRANSMITTER. ALL OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040628001542004062800154NM 2004 6 28 AWXA200400524 120040430A5313693660011 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.0625 INCH CRACK FOUND IN STRINGER TIE CLIP AT BS 277, STR 10 LT. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 277, STR 10 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040628001602004062800160SO 2004 6 28 CHQA000502 120040608A2820 VALVE EMB 145 EMB145LR 3260212SO RT WING LEAKING A CHQAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL11292 145488 DURING CLIMBOUT OF MCO, LIQUID WAS SEEN LEAKING FROM THE TRAILING EDGE OF THE RIGHT WING. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT TANK VENT VALVE. FURTHER INVESTIGATION REVEALED THAT THE FLAPPER VALVE TO RIGHT DRY BAY OR PRESSURE TANK TO BE DETACHED CAUSING THE LEAK. REPLACED FLAPPER VALVE PER MM 28-10-00 AND 28-23-00. 2L72 4T RTT00011AT 20040628001612004062800161EA 2004 6 28 COMA0460353 120040607A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01471CA 7655 FLIGHT 5615 FLAPS FAIL MESSAGE DURING TAXI. C/W RIGGING OF THE BPSU'S, SYSTEM CHECK SATISFACTORY. 2L72 4F RTA21EA 20040628001642004062800164SO 2004 6 28 SWIA200413354 120040525A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07584SW372 372 120352 DURING FLAP RETRACTION, RECEIVED CONTROL FAULT MESSAGE NUMEROUS TIMES. WOULD NOT RESET. REMOVED AND REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE. OPS CHECK GOOD. 2L72 4T RTA31SO 20040628001652004062800165SO 2004 6 28 C2XA04SH324 120040527A491014547494401 FIREWALL EMB 145 EMB145LR 3260212SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711565 145621 DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13 SECTION 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040628001662004062800166EA 2004 6 28 04130680 120040509A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27680BR 7679 DURING INSPECTION THE AFT EMERGENCY DOOR LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040628001772004062800177GL 2004 6 28 C2XA04BT062 220040520A7200 ENGINE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 1 FAILED A C2XAEA ENGINE SHUTDOWN UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW27149431313113131 145040 CAE310066 CREW REPORTED, NR 1 ENGINE FAILED INFLIGHT. N1 STABILIZED AT ABOUT 14 PERCENT AND 100 DEGREES. FAILURE OCCURRED DURING CLIMBOUT IN SHALLOW LEFT BANK WITH CLIMB THRUST SET. PERFORMED AIR RETURN TO NEWARK. LANDED UNEVENTFULLY. MAINTENANCE FOUND UNACCEPTABLE DEBRIS ON INDICATING CHIP DETECTOR, ALSO NOTED RAPID N2 RISE DURING ATTEMPTED START (APPROXIMATELY 50 PERCENT N2 WITHIN 3 SECONDS). SUSPECTED DAMAGE TO ACCESSORY DRIVE UNIT. REMOVED AND REPLACED NR 1 ENGINE IAW EXPRESS JET EMB145 TASKCARD 627001. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040628001782004062800178NM 2004 6 28 SWAA041750 120040622A3350101114 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F A16WE 20040628001962004062800196NM 2004 6 28 SWAA041759 120040622A53306545767 SKIN BOEING737 7377H4 1384404NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN AT BS 500A + 5, BOTTOM CENTERLINE, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040628001982004062800198NM 2004 6 28 C1HA200474004 120040531A3610 RETAINER BOEING727 727225 1384077NM DUCT LOOSE A C1HAO OTHER J WARNING INDICATION CRCRUISE 1 GL15674MG 21450 NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AT 26.0. FOLLOWED COM PROCEDURE, LIGHT WENT OUT. PERFORMED DUCT INSPECTION AND LOOP INSPECTION DID 2 HIGH POWER ENGINE RUNS. OVERHEAT NOT DUPLICATED HOWEVER AIR LEAK WAS FOUND IN 8TH STAGE DUCT. NR 3 ENG 8TH STAGE SUPPLY DUCT PARTIALLY REMOVED TO FACILATE OTHER MAINTENANCE. DUCT SHIMS VERY LOOSE. REPLACED AND TIGHTENED RETAINER DAMAGED. REPLACED, DUCT COUPLING CRACKED ON ONE SIDE AND WARPED DURING DISASSEMBLY. DUCT REPLACED, LEAK CHECKED GOOD AFTER INSTALLATION MM 36-11-00. 2L73 4F A3WE 20040628002032004062800203SO 2004 6 28 SWIA200413418 120040610A2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO RT ELEVATOR TRIMMALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07568SW 120343 TAKEOFF TRIM AURAL WARNINGS CAME ON WITH TRIM IN GREEN BAND. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM PROXIMITY SENSORS IAW EMB MM 27-32-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040628002052004062800205EA 2004 6 28 SWIA200413420 120040608A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07955SW2228 2228 7817 STAB TRIM CHANNEL 1 FAIL OFFLINE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629000042004062900004NM 2004 6 29 04FDEA01625 120040606A3260ARG7531502 TARGET DOUG MD11 MD11 3023602NM ZONE 700 BROKEN A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25597FE 48596 RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED PRIMARY AND SECONDARY WITH GEAR UP. PERFORMED QRH PROCEDURE AND RESTRICTED SPEED TO 230 KTS. ON POSTFLIGHT FOUND TARGET BROKEN. REMOVED AND REPLACED RT MLG TARGET AS PER AMM 32-34-05-4. PROXIMITY SENSOR & THE TARGET ASSY ADJUSTMENT CARRIED OUT AS PER AMM 32-61-15-820-001. CARRIED OUT RIGHT MLG DOOR LINK AND BRACKET ASSEMBLY ADJUSTMENT/TEST AS PER AMM 32-34-05-5, FOUND SATISFACTORY. CARRIED OUT LANDING GEAR EXTENSION/RETRACTION ADJUSTMENT/TEST AS PER AMM 34-31-00-5 AND FOUND SATISFACTORY. 2L73 4F RTA22WE 20040629000182004062900018NM 2004 6 29 04FDEA01645 120040609A5311AFA0028 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN CABIN LT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76734, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR: 1-2520-7-3308) PART I. 2L73 4F RTA22WE 20040629000212004062900021NM 2004 6 29 04FDEA01648 120040609A5311AFA0020 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 MAIN CABIN RIGHT SIDE, TRANSVERSE FRAME DAMAGED AT FS Y= 1681 ALONG LONGERON 12L. COMPLIED WITH FEDEX EA 1-5310-76735, FUSELAGE MAINFRAME REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO NR: 1-2520-7-3308 PART I. 2L73 4F RTA22WE 20040629000342004062900034NM 2004 6 29 AWXA200400598 120040527A532069414937 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND ON UPPER FORWARD CORNER OF STRINGER 26 LT INTERCOSTAL, AFT SIDE OF BS 500A. MAINTENANCE REMOVED CRACKED STRINGER 26 LT INTERCOSTAL, BS 500A; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 69-41473; INSTALLED REPAIR PART IAW B737-300 SRM 51-42-02 FIGS 8 & 12. 2L72 4F RTA16WE 20040629000462004062900046NM 2004 6 29 04FDEA01653 120040609A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CABIN STA 1119 LBL 55 SEAT TRACK FOUND DAMAGED. CUT & REMOVED AT STA 1109 & STA 6-40 LBL 47.5 AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II RESPECTIVELY. REPAIR SEAT TRACK FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040629000492004062900049NM 2004 6 29 SWAA041773 120040624A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040629000662004062900066NM 2004 6 29 04FDEA01667 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.500, REMAINING THICKNESS=0.498, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000692004062900069SO 2004 6 29 SWIA200413440 120040613A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07214SW 120280 FORWARD EMERGENCY RED LIGHT STRIP ON FLOOR INOP. REPLACED FORWARD EMERGENCY LIGHT STRIP ON FLOOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2L72 4T RTA31SO 20040629000712004062900071SO 2004 6 29 SWIA200413442 120040614A2121AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07587335424 2190 120197 SMOKEY ODOR IN COCKPIT FROM LEFT PACK WHILE ON THE GROUND. REPLACED LEFT GROUND COOLING FAN IAW EMB 120 21-20-00. P/N AE1711AA0, S/N ON 136, S/N OFF 112. 2L72 4T RTA31SO 20040629000722004062900072NE 2004 6 29 SWAA041779 220040623A7250CFM533 TURBINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A SWAAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW29346SW 24153 856245 IN FLIGHT SHUTDOWN / AIR TURNBACK, DURING CLIMB NR 1 ENGINE MADE A LOUD BANG. EGT INDICATION INCREASED TO 1060 DEGS. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20040629000782004062900078EA 2004 6 29 SWIA200413456 120040619A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY DOOR OUT OF ADJUST A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07416SW 7089 LEFT EMERGENCY DOOR (OVERWING) MESSAGE CAME ON AFTER LANDING. ADJUSTED PROX SENSOR TARGET. OPS CHECK GOOD. 2L72 4F RTA21EA 20040629000822004062900082NM 2004 6 29 04FDEA01671 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.408, REMAINING THICKNESS=0.406, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000882004062900088NM 2004 6 29 04FDEA01677 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.402, REMAINING THICKNESS = 0.402, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000902004062900090NM 2004 6 29 04FDEA01679 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.0417, REMAINING = THICKNESS = 0.415, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20040629000912004062900091NM 2004 6 29 04FDEA01680 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.128. COMPLIED WITH FEDEX EA #1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629000962004062900096EA 2004 6 29 SWIA200413374 120040528A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 BRACKET CRACKED AT FS 202.75, 8:00 POSITION IN NOSE HYDRAULIC BAY COMPARTMENT. DISCOVERED DURING C-CHECK INSPECTION. CLIP REPAIRED IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-24-16, 51-24-36, 51-25-06, AND 51-25-16. 2L72 4F RTA21EA 20040629001012004062900101NM 2004 6 29 AWXA200400618 120040530A5315BAC1518827 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER FORWARD FLANGE OF FLOORBEAM AT BS 1681, RBL 32. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 1681, RBL 32; FABRICATED 2 EACH ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51 FIG 202. 2L72 4F RTA2NM 20040629001062004062900106EA 2004 6 29 SWIA200413378 120040528A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE FS 280 RBL 9 LWR FLANGE CRACKED ON TRANSVERSE. DISCOVERED DURING C-CHECK INSPECTION. REPAIR BEAM IAW CRJ REO 601R-53-11-171 REV. NC. 2L72 4F RTA21EA 20040629001082004062900108NM 2004 6 29 04FDEA01685 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.412, REMAINING = THICKNESS = 0.410, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001092004062900109NM 2004 6 29 04FDEA01686 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED. 2L73 4F RTA22WE 20040629001122004062900112NM 2004 6 29 04FDEA01689 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.500, REMAINING = THICKNESS = 0.472, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001142004062900114NM 2004 6 29 04FDEA01691 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.502, REMAINING THICKNESS = 0.500, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001152004062900115NE 2004 6 29 04FDEA01692 220040624A7200CFM56 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM56* 13802NE NR 1 OVERTEMP A SWAAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW29366SW 26577 858617 NR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20040629001182004062900118NM 2004 6 29 AWXA200400621 120040531A5320146N524023 ANGLE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, RBL 40. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, RBL 40; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5240-23. 2L72 4F RTA2NM 20040629001232004062900123 2004 6 29 SWIA200413427 420040607A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07569SW 120344 STALL WARNING SYSTEM TEST NR 2 BUTTON LIGHT OUT, AFTER TEST BUTTONS PUSHED, BOTH SIDES STMI WARN RED LIGHT ON MAP STAYS ON. REPLACED STALL WARNING CONTROL PANEL. STALL WARNING 1 AND 2 OPERATIONAL CHECK GOOD. PN: 120-34428-505, S/N OFF: 120473. 2L72 4T RTA31SO 20040629001392004062900139SO 2004 6 29 SWIA200413386 120040515A5420 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07578SW 120346 RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET APPEARS TO BE CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT HYDRAULIC PACK LOWER SUPPORT BRACKET WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00. 2L72 4T RTA31SO 20040629001422004062900142SO 2004 6 29 SWIA200413389 120040531A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07237SW7915 7324 120314 FLAP CONTROL FAULT ON OUTBOARD PAIR FLAPS IN CRUISE FLIGHT. REPLACED FCU. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20040629001482004062900148 2004 6 29 SWIA200413395 420040605A3418501125904 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA STICK PUSHER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07959SW2326 2326 7840 EXPERIENCED STALL FAIL CAUTION MESSAGE DURING FLIGHT. REPLACED STALL PROTECTION STICK PUSHER ACTUATOR IAW CRJ MM 27-35-15. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040629001632004062900163EA 2004 6 29 SWIA200413446 120040520A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH ANGLE IS CRACKED FOR DOOR STOP FITTING FS 589.00 LBL 43.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-02, AND RII53-401. 2L72 4F4 FRTA21EA E15NE 20040629001692004062900169EA 2004 6 29 SWIA200413390 120040604A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07445SW5210 5210 7651 SPOILERON FAULT MESSAGE. REPLACED HYDRAULIC NR 1 PRESSURE SWITCH, LEFT SPOILERON PCU AND NR 2 SECU. OPS CHECK GOOD IAW MM CH 27-62-01. P/N 49-164-06, S/N OFF 01598. 2L72 4F4 FRTA21EA E15NE 20040629001732004062900173SO 2004 6 29 SWIA200413425 120040605A1420 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAPS DIRTY A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07584SW 120352 AT 500 FT, FLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED. CLEANED AND RE-SAFETIED FLAP CONNECTORS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040629001852004062900185NM 2004 6 29 QXEA200400407 120040606A323082450203503 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM ZONE 700 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09401QX 4031 GTF - ON FLIGHT NUMBER 2324, DURING CRUISE FLIGHT BOTH MAIN GEAR DOORS OPENED FOR 2 SECONDS. THE AIRSPEED WAS 245 KIAS AT 25,000 FEET. THE EVENT MARKER WAS PUSHED 20 SECONDS AFTER OCCURRENCE. GEAR OPERATED NORMAL. ADJUSTED LEFT AND RIGHT MAIN GEAR UPLOCK PROX SENSORS. VERIFIED INDUCTANCE VALUES FOR BOTH UPLOCK SENSORS. EXTENSION/RETRACTION TEST WAS PERFORMED. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630000202004063000020EU 2004 6 30 USAA040308 120040608A5321D5387175505200 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, FLOOR PANEL 261DF. FABRICATED NEW FLOOR PANEL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000362004063000036 2004 6 30 GUU2004F00020 420040525A34006226521016 CONTROLLER BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA NAVAGATION SHORTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO1787557 586 UE246 DURING APPROACH, ODOR OF ELECTRICAL SMOKE WAS PRESENT IN THE COCKPIT, AND NR 1 NAVIGATION CONTROLLER WAS INOPERATIVE. REMOVED AND REPLACED NR 1 NAVIGATION CONTROLLER. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040630000382004063000038NE 2004 6 30 ALG2004F00031 120040505A53127620123008122 BULKHEAD SKRSKYS76 S76C 8143008NE FUSELAGE CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03861AL302 760529 BULKHEAD CRACKED FROM RT STIFFENER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FROM RIVET HOLE TO EDGE. DOOR ASSY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS. 1G72 3U NCH1NE 20040630000592004063000059NM 2004 6 30 UIEA200400101 120040604A575365B159592 BEARING BOEING747 747212B 1384886NM GE CF6 CF650E 30018GL FLAP TRACK MIGRATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D-CHECK, DURING MAINTENANCE INSPECTION, ELONGATION DAMAGE WAS FOUND AT OB TRAILING EDGE FLAP TRACK NR 8 MOVABLE FAIRING ASSEMBLY HINGE FITTING LUGS. OVERSIZED THE BORES. DYE PENETRANT THE BORES TO ENSURE DEFECT FREE CONDITION. REFINISHED, INSTALLED ONE PIECE REPAIR SLEEVE AND A NEW DESIGN TYPE BEARING. 2L74 4F4 F A20WE E23EA 20040630000652004063000065SO 2004 6 30 SIMA200414202 120040519A27313621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL PITCH TRIM INOPERATIVE A SIMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 SW21807AE6093 3564 145506 MAINTENANCE REPORTED A DUAL PITCH TRIM FAIL ON LANDING AND TWICE ENROUTE PITCH TRIM 1 AND 2 INOPERATIVE. MESSAGE APPEARED FOR 5 SECONDS EACH TIME, THEN WENT OUT. REPLACED HSCU IAW MFG MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406973) 2L72 4F4 FRTT00011ATTE6CH 20040630000742004063000074EU 2004 6 30 USAA040256 120040522A5315D5347209200000 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW13221 0844 FLOORBEAM, 1.0 INCH X 1.0 INCH X .03 INCH D, CORROSION; LEVEL 2; FR64-66, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000792004063000079NM 2004 6 30 USA2004F00036 120040513A335020121 CHARGER BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19300AU 23228 MAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY. ALSO, REPLACED THE BATTERY PACK. OPS CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040630000832004063000083EU 2004 6 30 SDR2004029 120040513A3222D56797 AXLE AEROSPATR72 ATR72212A 8680902EU NLG CRACKED A TRBAO OTHER W INADEQUATE Q C LDLANDING 1 SO21548AT A050 548 AFTER LANDING THE NOSE GEAR AXLE CRACKED ALLOWING THE LT NOSE WHEEL TO CAME LOOSE FROM THE NOSE GEAR ASSY. NOSE WEEL AND BROKEN AXLE FOUND ON RUNWAY. REPLACED THE NOSE LANDING GEAR SHOCK ABSORBER ASSEMBLY. 2H72 4T RTA53EU 20040630000922004063000092EU 2004 6 30 USAA040239 120040521A5320D5347218820200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW15935 0890 FLOOR SUPPORT, 1.5 INCH X 1.2 INCH X .055 INCH DEEP, CORROSION; LEVEL 2. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000952004063000095NM 2004 6 30 USA2004F00052 120040508A215032194211 SHUTOFF VALVE BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE LT PACK BAY FAILED A USAABG EMER. DESCENT O2 MASK DEPLOYED O OTHER CRCRUISE 1 EA19376US28091 22955 RT PACK TRIP OFF LIGHT ILLUMINATED, WOULD NOT RESET. LT PACK TRIP OFF LIGHT ILLUMINATED DURING TEMP ADJMT. IMMEDIATE DESCENT WAS INITIATED TO 10,000 FT BUT CABIN ALTITUDE CLIMBED ABOVE 14,000 FT DEPLOYING OXYGEN MASKS. LT PACK RESET, PRESS WAS REGAINED. FLIGHT CONTINUED, LANDED W/O FURTHER INCIDENT. MAINT FOUND LT PACK 35 DEGREE SHUT OFF VALVE STUCK IN OPEN POSITION. REPLACED VALVE IAW MM. OPS CHECK, LEAK CHECK GOOD. REPACKED OXY MASKS AND REPLACED OXY GEN. PERFORMED HULL LEAK RATE CHECK AND FOUND AC FAILED TO REACH 100 SECOND LIMIT. FOUND FWD OUTFLOW VALVE CYCLING IN AC MODE. REPLACED AFT OUTFLOW VALVE. OPS CHECK, NORMAL. CLEARED RT PACK PROBLEM BY REPLACING INOPERATIVE RT TURBO FAN VALVE IAW MM.2L72 4F4 FRTA16WE E2GL 20040630000972004063000097EU 2004 6 30 USA2004F00042 120040514A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGNECY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19707UW4873 0949 THE AFT EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECKED OK. 2L72 4F4 FRTA28NM E2GL 20040630001042004063000104NE 2004 6 30 ALG2004F00032 120040505A53127620123008122 BULKHEAD SKRSKYS76 S76C 8143008NE FUSELAGE CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03860AL302 760527 BULKHEAD CRACKED FRO RT STIFFENER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FORM RIVET HOLE TO EDGE. DOOR ASSY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS. 1G72 3U NCH1NE 20040630001092004063000109NM 2004 6 30 GAIA04074OP 120040514A27821U1110 ACTUATOR BOEING727 727224 1384076NM PWA JT8 JT8D9 52048NE NR 5 KRUGER LEAKING A GAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0769739 20667 NOTED ELEVATOR LOW PRESSURE LIGHT CAME ON, HYDRAULIC SYSTEM (A) QUANTITY INDICATED ZERO, SYSTEM (A) ENGINE PUMP LOW PRESSURE LIGHTS BLINKING. FLIGHT DIVERTED MAINTENANCE BASE WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN INSERT IB TRUNNION FITTING ON NR 5 KRUGER FLAP ACTUATOR. REMOVED AND REPLACED NR 5 KRUGER FLAP ACTUATOR. INSPECTED NR 1 AND NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN AND (A) SYSTEM PRESSURE FILTERS. NO EVIDENCE OF PUMP FAILURE. FILTERS AND LEAK CHECKS GOOD. AC WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040630001122004063000112SO 2004 6 30 H2U2004F00000 120040513A1430AN365720 NUT MAULE MAULE MX7 MXT7160 5470204SO LYC O320 O320* 41508EA LT IB MLG BROKEN D H2USO OTHER O OTHER NRNOT REPORTED 1 SW11103HS2146 17007C LT IB MLG BOLT AND NUT THAT ATTACHES IB MLG TO AIRCRAFT FRAME CAME LOOSE AND FELL OUT. NUT IS LOCKNUT (PN AN365-720) (BOLT PN AN7-23A). WHEN BOLT CAME OUT IB MLG BROKE BOTTOM SKIN AND MLG PLASTIC FARRING. LOWER SKIN PANEL $80 , FARRING $70 NO OTHER DAMAGE OCCURED. NEW IMPROVED ATTACH HARDWARE HAS BEEN ORDERED FROM MFG FOR ALL OUR AIRCRAFT. (SW11200406346) 1H71 3O3 O 3A23 E274 20040630001172004063000117SW 2004 6 30 FTU2004F00003 120040607A5751250000375 SPAR GULSTM690TP 690B 7630516SW GARRTTTPE331TPE331* 01514WP RT AILERON CRACKED B FTURK NONE O OTHER ININSP/MAINT 1 NE0520MA 5936 11514 WHILE COMPLYING WITH SB 236. AILERON SPAR IB HINGE INSPECTION AND REINFORECMENT DATED MARCH 9, 2004 PART 1, BOTH AILERON IB SPAR WEBS AT IB HINGE AREA WERE FOUND CRACKED, THE AFT AND FORWARD END RIBS ALSO SHOWED CRACKS. WHILE COMPLYING WITH THE NEEDED REPAIRS IAW PART III, A CRACK WAS FOUND ON THE CENTER SPAR JUST OB OF THE CENTER HINGE UPPER ATTACH BOLT AREA. AFTER REMOVING THE CENTER SPAR WEB IT WAS FOUND TO HAVE A CRACK GENERATING AT EACH BOLT HOLE. MFG WAS NOTIFIED OF OUR FINDINGS. (PROBABLE CAUSE SEEMS TO BE AGE RELATED.) 1H72 3T3 T 2A4 E2WE 20040630001212004063000121EU 2004 6 30 USAA040250 120040525A5347D5311278220201 SEAT TRACK AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW 0844 SEAT TRACK, 5.45 INCH X 0.813 INCH X .047 INCH D, CORROSION, FR17 AT Y 1270, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001222004063000122EU 2004 6 30 USAA040251 120040604A5320D5348004320401 SILL AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW13221 0844 SILL, 2.0 INCH X 1.0 INCH X 0.06 INCH AREA, CORRODED. BETWEEN FR 66 & 68, BL Y11371, WL Z240. INSTALLED NEW SILL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001312004063000131EU 2004 6 30 USAA040311 120040608A5321D5367179900000 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW 0997 FLOOR PANEL, EXCEEDS 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK PANEL 221 PF. FABRICATED NEW FLOOR PANEL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001332004063000133NM 2004 6 30 USA2004F00040 120040516A335020131A BATTERY PACK BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19784AU 25023 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 21DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK ABOVE SEAT ROW 21DEF. OPS CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040630001452004063000145NM 2004 6 30 USA2004F00049 120040516A5414311A10659597 PANEL BOEING737 7373B7 1384580NM NR 1 PYLON LOOSE A USAAO OTHER C F.O.D. APAPPROACH 1 EA19396US 23318 (2) SECONDS PRIOR TO TOUCHDOWN, A PASSENGER REPORTED THAT TWO PANELS DEPARTED THE NR 1 ENGINE PYLON. ONE PANEL WAS REPORTED THO HAVE STRUCK THE LT HORIZONTAL STABILIZER LEADING EDGE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE PYLON PANELS AND CHECKED SECURITY OF NR 2 ENGINE PYLON PANELS. REPAIRED DAMAGE TO THE LT HORIZONTAL STABILIZER LEADING EDGE, FOUR FEET FROM ROOT THAT MEASURED 1 INCH X 1 INCH X .0625 INCH DEEP, IAW SRM. PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK VISIT. 2L72 4F RTA16WE 20040630001532004063000153CE 2004 6 30 UG8AGM0413 120040514A2701 YOKE CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL FLIGHT CONTROL SINCORRECT A UG8AO OTHER O OTHER NRNOT REPORTED 1 GL235115 3767 7500018 CONTROL YOKES SHOW 25 DEGREE RT BANK DURING STRAIGHT AND LEVEL. RT AILERON IS UP AND LT ELEVATOR IS UP. PITCH CONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. TROUBLESHOOTING FLIGHT CONTROL SYSTEMS IN PROGRESS. AIRCRAFT HAS NOT FLOWN. 2L72 4J4 FRTT00007WITE6CH 20040630001572004063000157NM 2004 6 30 F3LA200400066 120040606A2612 FIRE LOOP BOEING737 7373L9 1384470NM NR 2 ENGINE FAULTY A F3LAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03312FL 86 24569 AIR RETURN, NR 2 ENG OVERHEAT CAUTION LIGHT ILLUM TWICE. DECLARED EMERGENCY, LANDED W/O INCIDENT. ON DESCENT, MASTER CAUTION SYS ILLUM 4 TIMES, NO SIX PACK INDICATION. MX TESTED CAUTION SYS THRU SIMULATION OF CONDITIONS CAUSING ILLUMIN ANNUNCIATORS, ALL SYS OPERATED NORM. COULD NOT DUPLICATE. REPLACED NR 2 ENG PRSOV, LEAK CHECKED OK. PERFORMED LEAK CHECK NR 2 ENG AIR DUCTS, NO LEAKS FOUND. RAN NR 2 ENG AT T/O POWER APPROX 2 MIN & ENG OVERHEAT LIGHT ILLUM. SWITCHED OVER TO A-LOOP, FAULT REMAINED. SWITCHED TO B-LOOP, FAULT WENT AWAY. PROBLEM COULD ONLY BE DUPLICATED WITH ENGINE HOT. PLACARD NR 2 ENG A-LOOP, COMPLIED WITH SPECIAL PROCEDURES. PERFORMED OVERWEIGHT LANDING INSPECTION, NO DEFECTS FOUND. 2L72 4F RTA16WE 20040630001602004063000160NM 2004 6 30 QXEA200400395 120040605A3150 WARNING HORN DHAV DHC8 DHC8202 2809007NM ZONE 300 ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09353PH 496 RDM - FLIGHT 2035- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. RESET FLAPS TO 5 DEGREES. PERFORMED TAKEOFF CHECK. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040630001642004063000164CE 2004 6 30 61901 120040531A32601143800419 DOWNLOCK SWITCH BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07126YV UE126 WITH MAIN LANDING GEAR SELECTED DOWN THE LEFT MAIN LANDING GEAR WON'T INDICATE DOWN AND LOCKED. AIRCRAFT DIVERTED TO DUJ. EMERGENCY DECLARED, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LT MLG ACTUATOR/DOWNLOCK SWITCH CK GOOD. P/N 114-380041-9, S/N 193A. 2L72 4T RTA24CE 20040630001722004063000172EU 2004 6 30 WRNA200400005 120040610A292040157 PUMP AIRBUS300 A300B4203 3930306EU HYD SYSTEM LEAKING A WRNAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO05820SC 154 DURING DESCENT GREEN SYSTEM LEVEL LOW LIGHT ILLUMINATED, PERFORMED CHECK LIST AND PERFORMED ABNORMAL CHECK LIST DUE TO LOSS OF SYSTEM HYDRAULICS. BOTH HYDRAULIC PUMPS WERE PLACED TO DUMP PRIOR TO TOTAL FLUID LOSS. AIRCRAFT LANDED NORMAL. AFTER LANDING NOSE STEERING WOULD NOT RESPOND DUE TO HYDRAULIC LOSS. DETERMINED FLUID LOSE DUE TO NR 1 GREEN ELECTRIC PUMP CASE LEAK. REMOVED AND REPLACED PUMP. LEAK AND OP'S CHECK NORMAL IAW MM 29-21-11. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20040630001872004063000187NM 2004 6 30 N150AW0011 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 BS 747 FRAME CRACKED AT STR 13 LT. REPAIRED PER SRM 51-70-11. 2L72 4F RTA16WE 20040630001922004063000192NM 2004 6 30 N150AW0018 120040525A5315 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 BS 1016 AT RBBL 14 CORROSION AT FLOORBOARD ATTACH HOLE. REPLACED FLOORBEAM T-CAP PER SRM 51-10-2. 2L72 4F RTA16WE 20040630001942004063000194NM 2004 6 30 UPS04242556 120040527A7120 SUPPORT BOEING727 72725C 138400HNM CENTER ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, CENTER ENGINE LEFT AND RIGHT SUPPORT WEBS AT BS 1387 ARE CRACKED. WEBS REMOVED IAW SRM 51-30-02. NEW WEBS FABRICATED IAW BOEING DRAWING 65-17553, NEW WEBS INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20040701000152004070100015WP 2004 7 1 UPS04842551 120040610A2121500702 FAN DOUG DC8 DC873F 302199FWP E&E BAY FAILED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01852UP 46052 SMOKE IN COCKPIT PASSING 25,000 BEGAN TO FILL THE COCKPIT WITH STRONG ELECTRICAL FIRE SMELL. DECLARED EMERGENCY AND LANDED ASAP. FOUND RECIRC FAN INTERNAL FAILURE. REMOVED RECIRC FAN 67302. INSTALLED NEW FAN IAW 21-01-2, OPS CHECK NORMAL. OK FOR CONTINUED SERVICE. 2L74 4F RT4A25 20040701000182004070100018 2004 7 1 249TR0029 420040604A2230 COMPUTER BOEING737 7372K5 138448XNM AUTO THROTTLES MALFUNCTIONED A PIDAO OTHER O OTHER TXTAXI/GRND HDL 1 SO05249TR 22598 AUTO THROTTLES WILL NOT ENGAGE ON GROUND BEFORE TAKEOFF. PDC MUST BE RELOADED. RE-SEATED PDC AND AUTO THROTTLE COMPUTERS. PERFORMED BITE TEST. OPS NORMAL PER MM 22-31-01. 2L72 4F RTA16WE 20040701000192004070100019NM 2004 7 1 801DM0014 120040602A335020131A BATTERY PACK BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05801DM 26240 ALL EMERGENCY EXIT LIGHTS POWERED BY M731 ARE INOP. REPLACED BATTERY PACK PER MM 33-51-07. LIGHTS CHECK GOOD. 2L72 4F RTA2NM 20040701000202004070100020NE 2004 7 1 160041 320040606A6110 CONNECTOR SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE PROP OIL TEMP INDAMAGED A NSVAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27277MJ 340B277 NR 2 LEFT PROP OIL TEMP GAUGE INDICATES EXCESSIVE TEMP IN FLT, AIRCRAFT DIVERTED FROM DCA TO HEF. FOUND BROKEN WIRE ON TEMP SENSOR CONNECTOR. REPLACED PIN IN CONNECTOR IAW SAAB WM 20-30-25, OP CHECKED GOOD. 2L72 4T RTA52EU 6 CP61GL 20040701000212004070100021NM 2004 7 1 DHL2004751002 120040605A3350 BATTERY BOEING727 727264 138408MNM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 GALLEY EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY, OPS CHECKED GOOD IAW 33-50-71. 2L73 4F A3WE 20040701000222004070100022EU 2004 7 1 NACA20040023 120040606A3230MS27370G0125 HOSE AEROSPATR42 ATR42* 8680900EU LT MLG RUPTURED A NACAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 AL0342NC 067 GREEN HYDRAULIC SYSTEM LOW LEVEL INDICATION UPON GEAR RETRACTION AFTER TAKEOFF. REPLACED LEFT MAIN LANDING GEAR UP LINE AT ACTUATOR FOR BEING RUPTURED. CHECKED GOOD. 2H72 4T RTA53EU 20040701000232004070100023NM 2004 7 1 MWEA040087 120040605A33203355088501 BALLAST DOUG MD88 MD88 3023688NM CABIN LIGHT BURNED OUT A MWEAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31701ME 49760 FLIGHT ATTENDANT REPORTED BURNING SMELL IN AFT CABIN. VERIFIED BURNED BALLAST FOR SIDEWALL LIGHTS AT ROW 13/14F. REMOVED AND REPLACED BALLAST FOR SIDEWALL LIGHTS ROW 13/14F. 2L72 4F RTA6WE 20040701000242004070100024NM 2004 7 1 N150AW0002 120040525A5754 SKIN BOEING737 7373G7 1384595NM NR 5 SLAT DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 LEADING EDGE OF WING DAMAGED OUTBOARD END OF THE NUMBER 5 SLAT. REPAIRED PER SRM 51-70-17. 2L72 4F RTA16WE 20040701000262004070100026WP 2004 7 1 MWEA040091 120040608A534039363611 SUPPORT DOUG DC9 DC981 3022081WP MLG ACTUATOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 LEFT MAIN LANDING GEAR DOOR RETRACT ACTUATOR UPPER FORWARD SUPPORT IS CRACKED. STOP DRILLED CRACK. 2L72 4F A6WE 20040701000272004070100027WP 2004 7 1 MWEA040092 120040608A528039364031 SUPPORT DOUG DC9 DC981 3022081WP RT MLG DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31805ME 48031 RT MAIN LANDING GEAR DOOR RETRACT ACTUATOR UPPER FORWARD SUPPORT CRACKED. STOP DRILLED CRACK. 2L72 4F A6WE 20040701000282004070100028NM 2004 7 1 N150AW0009 120040525A5510 SKATE ANGLE BOEING737 7373G7 1384595NM DORSAL FIN WORN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 FORWARD END OF LEFT SKATE ANGLE FOR VERTICAL DORSAL FIN IS WORN AT BS 1016. REPLACED SKATE ANGLE PER SRM 51-10-02. 2L72 4F RTA16WE 20040701000292004070100029EA 2004 7 1 QXEA200400411 120040606A5240 ROD CNDAIRCL600 CL6002C10 1390015EA SERVICE DOOR OUT OF ADJUST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09612QX5421 10042 SEA - FLIGHT 2455 - CREW REPORTED THAT THE SERVICE DOOR WILL NOT OPEN. MAINTENANCE INSPECTED THE DOOR AND REPOSITIONED THE ROD ASSEMBLY FOR VERTICAL MOVEMENT. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040701000302004070100030NM 2004 7 1 QXEA200400399 120040602A27207G7921 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 300 INOPERATIVE A QXEAC ABORTED TAKEOFF J WARNING INDICATION CRCRUISE 1 NM09374PH 528 SEA - ON FLIGHT NUMBER 2248, ABORTED TAKEOFF, RUDDER FULL PRESSURE CAUTION LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. THERE WAS NO OTHER CAUTION LIGHT OBSERVED. REMOVED AND REPLACED PRESSURE SWITCH. RUDDER FULL PRESSURE CAUTION LIGHT STAYED OFF. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040701000332004070100033NE 2004 7 1 QXEA200400396 220040603A7420312241503 IGNITER BOMBDRDHC8 DHC8401 1390041NM PWA PW121 PW121 52124NE ZONE 400 INOPERATIVE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09402QX 4032 GEE965210 PDX - ON FLIGHT NUMBER 2308, NR 1 ENGINE HAD NO LIGHT OFF DURING ENGINE START. THERE WAS GOOD FUEL FLOW AND ROTATION, BUT THERE WAS NO ITT RISE. EMERGENCY CHECKLIST PERFORMED. THE 2ND ATTEMPT WAS THE SAME RESULT. REMOVED AND REPLACED BOTH IGNITORS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040701000362004070100036EA 2004 7 1 QXEA200400402 120040605A2611 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09600QX 10005 PDX - AFT CARGO SMOKE DETECTOR CAUTION MESSAGE DISPLAYED, THEN WENT OUT. INSPECTED BOTH AFT CARGO SMOKE DETECTORS WITH NO DEFECTS FOUND. NO CAUTION MESSAGES DISPLAYED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040701000372004070100037EA 2004 7 1 QXEA200400404 120040607A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09614QX6352 10049 PDX - ON FLIGHT NUMBER 2507, 10 MINUTES INTO FLIGHT, RECEIVED A GEAR DISAGREE WARNING MESSAGE WHEN GEAR WAS SELECTED UP. AN EMERGENCY CHEKLIST WAS PERFORMED. EMERGENCY GEAR EXTENSION WAS PERFORMED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR SELECT VALVE. OPERATIONAL CHECK GOOD. NO DAMAGE OR DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040701000382004070100038EA 2004 7 1 QXEA200400397 120040604A31108221310101 DCU CNDAIRCL600 CL6002C10 1390015EA ZONE 600 INOPERATIVE A QXEAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM09614QX1326 1326 10049 SBA - FLIGHT 2455 - AILERON TRIM MOVING RIGHT WING DOWN SIMULTANEOUSLY WITH RUDDER TRIM MOVING NOSE RIGHT, WITHOUT PILOT INPUT. ON GROUND, CANNOT MOVE AILERON TRIM TO FULL LEFT WING DOWN OR RUDDER TRIM TO FULL NOSE LEFT. AFTER SHUTDOWN AILERON TRIM CONTINUES TO MOVE AT A VERY SLOW RATE. RIGHT WING DOWN AND RUDDER TRIM CONTINUES TO MOVE AT A VERY SLOW RATE, NOSE RIGHT. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 DCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040701000422004070100042NM 2004 7 1 N150AW0015 120040525A5312 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 VERTICAL STIFFENER ON THE AFT SIDE OF BS 178 BULKHEAD IS CRACKED AT LBBL 5.7 AND WL 184. REPAIRED AREA PER SRM 53-10-8. 2L72 4F RTA16WE 20040701000442004070100044NM 2004 7 1 N150AW0004 120040525A5347 SEAT TRACK BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STATION 727B SEAT TRACK AT RBBL 24.82 OUTBOARD FLANGE AND SEAT TRACK AT RBBL 45.57 INBOARD AND OUTBOARD FLANGES HAVE A CRACK ON THE UPPER CHORD ON THE HORIZONTAL FREE FLANGE AT THE TRANSVERSE BEAM CONNECTION POINT. REPAIRED AREAS PER EA NR 53-085. 2L72 4F RTA16WE 20040701000492004070100049NM 2004 7 1 AWXA200400626 120040525A53156545808179 FLOORBEAM BOEING737 7373G7 1384595NM CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON UPPER T-CAP OF MAIN CABIN FLOORBEAM AT BS 294.5, FROM LBL 11 TO RBL 55. MAINTENANCE REMOVED CORRODED UPPER T-CAP AND PREVIOUSLY INSTALLED REPAIR ANGLES ON MAIN CABIN FLOORBEAM AT BS 294.5, FROM LBL 11 TO RBL 55. FABRICATED A NEW REPLACEMENT UPPER T-CAP PER DWG 65-45808; INSTALLED REPAIR PART USING EXISTING REPAIR ANGLES IAW B737-300 SRM 51-40-02 FIG 12-14. 2L72 4F RTA16WE 20040701000502004070100050NM 2004 7 1 AWXA200400627 120040527A532069366564 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH PIECE OF SHEAR WEB ANGLE (TOP LEG) WAS FOUND CRACKED AND BROKEN OFF AT BS 935, BL 0. MAINTENANCE REMOVED CRACKED SHEAR WEB ANGLE AT BS 935, BL 0; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-36656; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 6-8. 2L72 4F RTA16WE 20040701000532004070100053NM 2004 7 1 AWXA200400630 120040531A5320146N530022 ANGLE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, LBL 45. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, LBL 45; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5300-22. 2L72 4F RTA2NM 20040701000542004070100054 2004 7 1 UPS04142543 420040604A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU COCKPIT WILL NOT ARM A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 INSPECTION TYPE:N/A DIFFICULTY IN ARMING MAIN ENTRANCE DOOR SLIDE. COULD NOT GET SLIDE ARMED INDICATION UNTIL AFTER REPEATED ATTEMPTS. PERFORMED DOOR EMERGENCY SLIDE ARMING ADJUSTMENT AND TEST PER MM 52-73-00-5, OPS CHECK GOOD. 2L72 4F RTA35EU 20040701000552004070100055WP 2004 7 1 UPS04842536 120040505A5753 STRUCTURE DOUG DC8 DC873F 302199FWP RT TE FLAP BENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2, RIGHT WING I/B FLAP I/B END (LIP) BENT AT AFT AREA, CHAFING FILLET PANEL 192 U. FABBED NEW WEB AND DOUBLER REPAIR IAW REO G09806. 2L74 4F RT4A25 20040701000562004070100056WP 2004 7 1 UPS04842537 120040507A531197558583 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 AFT PIT LOWER BILGE FWD WALL AREA FRAME STA 1000 BETWEEN L27R AND 27L EXFOLIATED ON FWD SIDE IN NUMEROUS AREAS. REMOVED CORROSION OUT OF LIMITS. CUT OFF DAMAGED SECTION FROM L34L-L34R IAW DC8 SRM 53-2-0. LOCATED AND DRILLED FRAME SECTION AND REPAIRED SPLICES. LOCATED AND UP ANGLE. ALODINED AND PRIMED FRAME SECTION, SPLICES AND ANGLE. INSTALLED FRAME SECTION, ANGLE, REPAIR SPLICES, FRAME CAP, GASKETS AND BRACKETS IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040701000582004070100058WP 2004 7 1 UPS04842539 120040509A5711 SPAR DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2, RIGHT WING FWD SPAR AT XFS 520.00 HAS 500 HOLE WITH CRACK INDICATED. REPAIRED RIGHT WING FWD IAW DWG J060232-532 CONF AND REO GO9802 2L74 4F RT4A25 20040701000592004070100059WP 2004 7 1 UPS04842540 120040509A5330561537871 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2, FS 1400 D PIT EXTERIOR CUTOUT SKIN CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB REPAIRED DOUBLER IAW REO GO9822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC8 SRM 51-1-20D AND REO GO988. 2L74 4F RT4A25 20040701000602004070100060WP 2004 7 1 UPS04842541 120040513A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2, MAIN CABIN FS AT 995 SEAT TRACK -E- HAS CORROSION BETWEEN LUGS. REMOVED CORROSON FOUND TO BE OUT OF LIMITS. REMOVED FLOORBOARD 1000 TO 1060. CUT SEAT TRACK FROM STA 830 TO 1100 IAW EO DC8 5320517C DWG DC8 53B 003. MAT ID SEAT TRACK 2772660 PO SPO905314, & 2 SPLICE FITTING SEAT TRACK. ALODINED AND PRIMED. INSTALLED SEAT TRACK & 2 SPLICE FITTING, INSTALLED FLOORBOARD FROM STA 1000-1060 IAW DC8 SRM 51-3-0, 51-3-1. 2L74 4F RT4A25 20040701000612004070100061WP 2004 7 1 UPS04842542 120040514A533057549423 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, MARKER BEACON MOUNT AREA HAS HEAVY CORROSION (SKIN). BLEND CORROSION FOUND OUT OF LIMITS. REMOVED LT LOWER STRESS PANEL MAT ID 7075-T6, -.071, PO 434977.6 FOR DOUBLER IAW REO GO 9816. FAB REPAIR DOUBLERS IAW REO GO9816. ALODINED & PRIMED. INSTALLED DOUBLER IAW REO GO9816. RE-INSTALLED STRESS PANEL IAW DC8 SRM 51-3-1. 2L74 4F RT4A25 20040701000622004070100062 2004 7 1 373PA0050 420040603A2220HG1050AD04 IRU BOEING737 7373Y0 1384671NM LEFT FAILED A PIDAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO05373PA 23749 LEFT ADI ROLLED 20 DEGREES PITCH UP AND 45 DEGREES LEFT BANK AT 33,000 FT. AUTO THROTTLES REDUCED TO IDLE. LATER IN LANDING PATTERN THE LEFT IRU FAULTED AND FLAGGED. REPLACED LEFT IRU PER MM 34-28-31. CHECKED IRU AFFECTED SYSTEMS PER WDM 34-26-13 AND RAN BITE CHECK. IRU OPS NORMAL. 2L72 4F RTA16WE 20040701000632004070100063NM 2004 7 1 371PA0044 120040606A3350 LIGHT BOEING737 737306 13844BGNM CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. CLEANED WATER FROM TRACK AND LIGHT RECEPTICALS. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20040701000642004070100064NM 2004 7 1 P9RA20040016 120040606A5260 WARNING LIGHT BOEING737 737231 1384079NM AIRSTAIR ILLUMINATED A P9RAO OTHER J WARNING INDICATION DEDESCENT 1 SO1154344 21631 IN DESCENT, AMBER AFT AIRSTAIR LIGHT ILLUMINATED ON FLIGHT ENGINEERS PANEL. CLEANED AND LUBRICATED SWITCHES, INSPECTED WIRING AND CYCLED STAIRS SEVERAL TIMES. ALL INDICATIONS WERE NORMAL PER BMM 52-62. 2L72 4F RTA16WE 20040701000652004070100065NE 2004 7 1 GLBA20030635 320040602A6197 WIRE EMB 120 EMB120ER 3260203SO HAMSTD14RF 14RF9 NE RT PROP CHAFED A GLBAO OTHER O OTHER APAPPROACH 1 NM03299UX 120299 RIGHT PROP AUTOFEATHERED WHEN CONTROL LEVERS MOVED TO MAX DURING APPROACH AROUND 40 PERCENT TQ. REPAIRED CHAFED WIRING ON TSU, RIGGED RIGHT AIR FROM RIGGING ON POWER LEVER AND TRIMMED RT ENGINE. 2L72 4T RTA31SO 6 CP11NE 20040701000692004070100069NM 2004 7 1 SWAA041793 120040627A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP DURING TEST. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040701000702004070100070NM 2004 7 1 SWAA041794 120040627A53116545815 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 344, STRINGER 17L, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040701000722004070100072NM 2004 7 1 SWAA041796 120040627A33501619 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F A16WE 20040701000732004070100073NM 2004 7 1 SWAA041797 120040627A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 500C + 16, BETWEEN STRINGER 15R AND STRINGER 14R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040701000762004070100076NM 2004 7 1 SWAA041800 120040627A53146545866 PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED C4 CHECK FOUND RT KEEL BEAM PANEL, CRACKED. REPAIRED KEEL BEAM PANEL PER EA. 2L72 4F RTA16WE 20040701000792004070100079NM 2004 7 1 SWAA041803 120040627A3350610478 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040701000802004070100080NM 2004 7 1 SWAA041804 120040628A5754BACB30LJ45U7 BOLT BOEING737 7373H4 1384600NM RT WING SLAT SHEARED A SWAAO OTHER O OTHER LDLANDING 1 SW29332SW 23696 ON APPROACH NR 4 L/E SLAT INDICATED INTRANSIT, RECYCLED PER QRH WITH NORMAL DEPLOYMENT. UPON LANDING CYCLE FLAPS/SLATS AND NOTED A LOUD BANG AND ASYMMETRICAL RATE OF DEPLOYMENT ON NR 4 L/E SLAT, NR 4 L/E SLAT OUTBOARD SIDE STICKS. REMOVED AND REPLACED NR 4 L/E SLAT DETENT BOLT PER MM. 2L72 4F RTA16WE 20040701000842004070100084 2004 7 1 SWAA041808 420040628A2565D31354 SLIDE BOEING737 7373A4 1384585NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040701000862004070100086WP 2004 7 1 MWEA040084 120040607A531099581561 WINDOW FRAME DOUG DC9 DC981 3022081WP FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW NR 29 FRAME ON LOWER FORWARD CORNER. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES. 2L72 4F A6WE 20040701000872004070100087WP 2004 7 1 MWEA040085 120040607A531099581561 WINDOW FRAME DOUG DC9 DC981 3022081WP FUSELAGE LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 LIGHTNING STRIKE ON CABIN WINDOW FRAME 29 AFT LOWER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE AS TEMPORARY REPAIR TO BE PERMANENTLY REPAIRED ON OR BEFORE 7,000 CYCLES. 2L72 4F A6WE 20040701000882004070100088NM 2004 7 1 N150AW0012 120040525A531365516982 SPLICE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER SPLICE CRACKED AT BS 907 AT STR 4 LT AND AT STR 4 RT. REPLACED STRINGER SPLICE AT STR 4 LT AND STR 4 RT PER SRM 51-10-02. 2L72 4F RTA16WE 20040701000902004070100090EU 2004 7 1 DXTA200400319 120040605A2150 A/C PACK BRAERO1000 BAE1251000 1500287EU MALFUNCTIONED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07514QS NA1005 NOTICED FUMES AND SLIGHT SMOKE COMING FROM THE CO-PILOTS AIR CONDITIONING VENT DURING DEPARTURE, ODOR WAS STRONGEST WHEN MAIN AIR VALVES WERE FIRST OPENED AND WENT AWAY AFTER THE VALVES WERE PLACED TO LOW PRESSURE. RAN BOTH ENGINES AND APU WITH BLEED AIR ON FOR 45 MINUTES, NOTICED SLIGHT SMELL FOR FEW SECONDS. WENT FULL HOT ON CABIN HEAT ODOR DID NOT RETURN, SYSTEM OPS CHECKED GOOD IAW HAWKER 1000 MM CHAPTER 21-30-00. 2L72 4F RTA3EU 20040701000922004070100092NM 2004 7 1 SWAA041810 120040628A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 986, RBL 0 TO RBL 50, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040701000932004070100093NM 2004 7 1 SWAA041811 120040628A53106546546 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, BETWEEN STRINGER 25R AND STRINGER 26R, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040701000942004070100094NM 2004 7 1 SWAA041812 120040628A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27L AT BS 500D, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040701000952004070100095NM 2004 7 1 SWAA041813 120040628A53106546529 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 480, LBL 18, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040629001132004062900113NM 2004 6 29 04FDEA01690 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040629001162004062900116WP 2004 6 29 04FDEA01693 120040611A3230806125 PSEU DOUG DC10 DC1010 3022110WP MLG MALFUNCTIONED A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25373FE 46611 ON FIRST GEAR EXTENSION RIGHT MAIN GEAR INDICATED UNSAFE. ANTI-SKID WOULD NOT TEST EITHER. RECYCLED GEAR AND RIGHT MAIN GEAR ON F/O PANEL STILL INDICATED UNSAFE. S/O PANEL INDICATED ALL THREE GEAR DOWN AND LOCKED. ANTI-SKID TESTED OK. F/O RESEATED RIGHT MAIN GEAR LIGHT AND GOT POSITIVE GEAR DOWN INDICATION (GREEN LIGHT). LANDED WITH NO FURTHER PROBLEMS. INSPECTED RIGHT MAIN GEAR PROX SWITCHES AND LINKAGES, NO FAULTS FOUND. TESTED PROX BOX, BOX INDICATED FAULT IN 31 RIGHT POSITION. REPLACED PROX BOX AND TESTED OK PER TAFI 32-30-00. ANTI-SKID TESTED OK PER M/M 32-44-00. 2L73 4F A22WE 20040629001192004062900119NM 2004 6 29 AWXA200400622 120040531A5320146N530021 ANGLE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, RBL 45. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, RBL 45; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5300. 2L72 4F RTA2NM 20040629001302004062900130NM 2004 6 29 SWAA041782 120040627A71103142200 COWLING BOEING737 7377H4 1384404NM NR 1 ENGINE DEPARTED A SWAAO OTHER D INFLIGHT SEPARATION LDLANDING 1 SW29748SW 29800 ON TOUCHDOWN AND REVERSER DEPLOYMENT LOST BOTH SIDES OF NR 1 ENGINE COWLING, WITH DAMAGE TO LT FUSELAGE, LT UPPER WING AND LT HORIZONTAL STAB L/E. ACCOMPLISHED CONDITIONAL INSP OF FUSELAGE, HORIZONTAL STAB, AND PYLON. INSP DUE TO FAN COWLING DEPARTING FROM AIRCRAFT PER EA. 2L72 4F RTA16WE 20040629001342004062900134NM 2004 6 29 SWAA041786 120040625A335090083 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29103SW 23109 DURING SCHEDULED PM CHECK, FOUND AFT CABIN OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK PER MM. 2L72 4F A16WE 20040629001382004062900138EA 2004 6 29 SWIA200413385 120040528A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 CARGO PIT FS 621 FLOOR SUPPORT ANGLE REPAIR CRACKED AT LBL 42. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401. 2L72 4F RTA21EA 20040629001442004062900144NM 2004 6 29 SWAA041790 120040626A3350101114 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM. 2L72 4F A16WE 20040629001472004062900147EA 2004 6 29 SWIA200413394 120040604A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07592SW8851 8851 7279 SPOILERON FAULT MESSAGE ON TAXI OUT WITH BOTH ENGINES RUNNING. REMOVED AND REPLACED LT NR 1 SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040629001512004062900151NM 2004 6 29 AWXA200400605 120040518A5313BAC1498157 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .6875 INCH CRACK WAS FOUND IN STRINGER AT BS 495C, STR 16 RT, WL 188. MAINTENANCE CUT OUT CRACKED SECTION OF STRINGER AT BS 495C, STR 16 RT, WL 188; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, HAT SECTION, CHANNEL, AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 201. 2L72 4F RTA16WE 20040629001652004062900165EA 2004 6 29 SWIA200413448 120040604A5315 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07928SW 7701 FUSELAGE FLOORBEAM ATTACH CLIP IS CRACKED; OUTBOARD LOCATION FS 280.0 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-42-13, 51-25-16. 2L72 4F RTA21EA 20040629001752004062900175EA 2004 6 29 SWIA200413451 120040505A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07720SW 7297 CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH CLIP FOR STOP FITTING IS CRACKED, FS 605.00, LBL 43.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-41-02, 51-41-04, 51-21-11 & 51-25-16. 2L72 4F RTA21EA 20040629001772004062900177EA 2004 6 29 SWIA200413458 120040604A5315 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 FUSELAGE FLOORBEAM ATTACH CLIPS ARE CRACKED (2) INBOARD AND OUTBOARD FS 280.00 RBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11. 2L72 4F4 FRTA21EA E15NE 20040629001782004062900178EA 2004 6 29 SWIA200413459 120040604A5315 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 FUSELAGE FLOORBEAM ATTACH CLIP IS CRACKED INBOARD LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11 2L72 4F4 FRTA21EA E15NE 20040629001802004062900180EA 2004 6 29 SWIA200413461 120040604A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07932SW 7714 AFT EQUIPMENT BAY CLIP CRACKED AT FS 621.00 - 625.00 STR 14R. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-41-06, AND 51-25-16. 2L72 4F4 FRTA21EA E15NE 20040629001822004062900182EA 2004 6 29 SWIA200413380 120040528A5320 FLANGE CNDAIRCL600 CL6002B19 1900309EA BEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW 7089 FUSELAGE VERTICAL BEAM LWR I/B FLANGE CRACKED AT FS 559 RBL 9. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-057 REV. NC. 2L72 4F RTA21EA 20040714000092004071400009WP 2004 7 14 UPS04842596 120040614A534037552221 ATTACH FITTING DOUG DC8 DC873F 302199FWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, FLOORBEAM ATTACH FITTING IS CRACKED AT STA 781 LBL 24. REMOVED AND REPLACED FITTING IAW DWG 3755222 AND SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040630000072004063000007SO 2004 6 30 FO72004F00000 120040521A29103195100 RELIEF VALVE PIPER PA23 PA23250 7102308SO HYD PWR PACK LEAKING D FO7RO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO13545044695 2924 273369 UPON GEAR RETRACTION PILOT NOTICED GEAR UNSAFE LIGHT, GEAR WOULD NOT EXTEND, HAND PUMP TRIED, NO PRESSURE, CO2 BOTTLE PULLED, HYDRAULIC POWER PACK COVER LIFTED AND CAUSED FLUID TO LEAK OVER INTO COCKPIT FLOOR, AIRCRAFT LANDED GEAR UP WITH MINOR DAMAGE, HYDRAULIC POWER PACK DISASSEMBLED AND FOUND HOLD DOWN PLATES (PN 31886-02, 03) CRACKED, ALLOWING RELIEF VALVE BODY TO UNSEAT SO NO HYDRAULIC PRESSURE COULD BE ROUTED TO SYSTEM, A POWERPACK REBUILD SHOP SAID THIS IS A COMMON PROBLEM. 1L72 3O 1A10 20040630000142004063000014SO 2004 6 30 SIMA200414602 120040523A531312022656034 STRINGER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FWD FUSELAGE CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21711PH 145235 AIRCRAFT STRUCK BY GPU ON RT SIDE JUST AFT OF RADOME. REPLACED 2 SKIN PANELS, 1 STRINGER, AND 1 FRAME. IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406972) 2L72 4F4 FRTT00011ATTE6CH 20040630000322004063000032CE 2004 6 30 FPI2004F00003 120040505A214045C40 COMBUST CHAMBER BEECH 58 58 1152740CE CONT O520 IO520* 17032SO HEATER CRACKED E FPIAK NONE L NO TEST ININSP/MAINT 1 SO1593DF 80 TH61 DURING ANNUAL INSPECTION A HEATER DECAY TEST WAS PERFORMED. THE HEATER FAILED THE TEST AND WAS REMOVED FROM THE AIRCRAFT. A SUBSEQUENT PRESSURE TEST WAS DONE ON THE BENCH. TWO LARGE CRACKS WERE FOUND AT THE WELD JOINTS BETWEEN THE INNER COMBUSTION TUBE AND TWO OF THE CROSS OVER PORTS. THIS HEATER WAS INSTALLED AS OVERHAULED AND HAS LESS THAN 100 HOURS OF OPERATION. A FAULTY WELD MAY BE A CONTRIBUTING FACTOR. RECOMMEND REGULAR DECAY TESTING. 1L72 3O3 O 3A16 E5CE 20040630000332004063000033EU 2004 6 30 A6WA200460018 120040528A5753 FLAP TRACK BAC 146 146300A 1500267EU LYC ALF502ALF502* 41580EA NR 2 FLAP WORN A O OTHER O OTHER NRNOT REPORTED 1 GL31611AW E3120 LT NR 2 FLAP TRACK HAS WEAR BEYOND THE SRM LIMITS MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS REF AVMAX FAX 611-1908004. DAMAGED AREA MAPPED AND SUBMITTED TO BAE FOR REPAIR CRITERIA. NDT HFEC CARRIED OUT IAW BAE FAX BARA/AVR/6761/04-MK, NO CRACKS NOTED. DV INSPECTION DONE IAW FAX BARA/AVR/6761/04-MK. NO DISCREPANCIES NOTED. (M) 2H74 4F4 FRTA49EU E6NE 20040630000432004063000043EU 2004 6 30 QU22004F00000 120040520A7160F50B58110163 INLET AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE731* 01518WP ENGINE CRACKED B QU2RK NONE O OTHER ININSP/MAINT 1 EA17888ME 41 (REGISTRATION NR CHANGE FROM 888MF). DURING INSPECTION, A FLUSH PATCH APPROXIMATELY .5 INCH BY 2 INCHES WAS NOTED IN THE ENGINE INLET. THIS IS NOT AN APPROVED REPAIR. MFG REQUIREMENTS ARE TO RESKIN THE INNER INLET. 2L73 4F4 F A46EU E6WE 20040630000502004063000050SO 2004 6 30 SIMA200414403 120040523A5610NP15131111 WINDOW EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT FAILED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21647AE 145222 DURING CRUISE FLIGHT, CREW REPORTED THE CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT WAS DIVERTED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406966) 2L72 4T4 FRTT00011ATTE6CH 20040630000532004063000053NM 2004 6 30 USA2004F00038 120040514A3350110049 POWER SUPPLY BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE FWD CABIN FAULTY A USAAO OTHER L NO TEST NRNOT REPORTED 1 EA19506AU 23381 PILOT REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INDEPENDENT OF SWITCH POSITION. MAINTENANCE REMOVED AND REPLACED THE M1136 POWER SUPPLY AND BATTERY PACK IAW MM. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040630000562004063000056NM 2004 6 30 UIEA200400103 120040604A541265B941091 BULKHEAD BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE FUSELAGE CRACKED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D-CHECK, DURING MAINTENANCE INSPECTION. NR 4 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND WL 146.5. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. THE SKIN ACCESS CUT OUT EDGE CHAFING DAMAGE WAS REMOVED BY BLENDING. REPAIR DOUBLERS WAS FABRICATED FROM 0.063 INCH THICK TITANIUM SHEET WERE INSTALLED COMMON TO THE STRUT OUTER SKIN ASSY USING MECHANICAL FASTENERS. 2L74 4F4 F A20WE E23EA 20040630000602004063000060CE 2004 6 30 GUU2004F00022 120040518A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153617881 UE152 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040630000632004063000063SO 2004 6 30 SIMA200405502 120040223A3350 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCONNECTED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21639AE 145182 EMERGENCY EXIT SIGN ABOVE GALLEY SERVICE DOOR INOPERATIVE AND EMERGENCY EXIT SIGN ON RT FW BULKHEAD IN FRONT OF SEATS 2 B,C INOPERATIVE. FOUND CONNECTOR P8530 OFF, RECONNECTED P8530. AC GOOD IAW MFG AMM. (SW21200406975) 2L72 4T4 FRTT00011ATTE6CH 20040630000712004063000071CE 2004 6 30 GUU2004F00021 120040518A55201016200131 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT STAB ELEVATORCORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178153617881 UE152 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040630000732004063000073CE 2004 6 30 ALG2004F00027 120040603A32977655200904045 CABLE CESSNA750 750 2076810CE ALLSN 250C 250C30S 03013GL MLG FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03971QS 7500071 CAE890809S LT MAIN GEAR GREEN LIGHT WOULD NOT COME ON FOR LANDING AT EC335, LANDING GEAR WAS RECYCLED AND GOT THREE GREEN LIGHTS. AFTER TAKE OFF LANDING GEAR WAS RECYCLED TO SEE IF WE WOULD HAVE ANY MORE PROBLEMS, LT MAIN GEAR LIGHT WOULD NOT COME ON, GEAR WAS RECYCLED SEVERAL TIMES, EMERGENCY CHECKLIST WAS COMPLIED WITH, AC WAS DIVERTED FOR MAINTENANCE. MAINTENANCE CHECKED ON JACKS AND FOUND LT MLG DOWN LIMIT CABLE SEGMENT AT FAULT. REMOVED AND REPLACED CABLE SEGMENT. FUNCTIONED CHECK WITH AIRCRAFT ON JACKS MANY TIMES, CHECKED GOOD. 2L72 4J3 URTT00007WIE1GL 20040630000772004063000077EU 2004 6 30 A6WA200460016 120040526A5315 FLOORBEAM BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502* 41580EA FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL23611AW E3120 CRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS REF AVMAX FAX 611-1908002. REPAIRED IAW BAE FAX BARA/AVR/6759/04-DC AND BARA/AVR/6752/04-02. PRIMED IAW BAE 146 AMM 20-10-11. (M) 2H74 4F4 FRTA49EU E6NE 20040630000802004063000080NM 2004 6 30 USA2004F00039 120040516A335020121 CHARGER BOEING777 777222 1385219NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19784UA 26951 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSY IN THE AFT GALLEY CEILING. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTT0001SE E2GL 20040630000962004063000096NM 2004 6 30 USAA040211 120040509A5347 SEAT TRACK BOEING767 767201 1385125NM GE CF6 CF680 30025NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19646US68850 23898 SEAT TRACK, CORROSION, NO LEVEL, BS1087-1469, RBL 88.5 CABIN FLOOR. 2L72 4F4 FRTA1NM E13NE 20040630001162004063000116 2004 6 30 Z5F2004F00002 420040526A2312 RADIO CESSNA500 550 2076604CE PWA 530 PW530A NE COCKPIT SMOKE E Z5FAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NE03306CS 5500881 DURING CRUISE, CREW REPORTED A BURNING SMELL AND SLIGHT AMOUNT OF SMOKE COMING FROM UNDER THE GLARE SHIELD. PROBLEM OCCURRED WHILE USING NR 2 COMM., CREW DETERMINED SMELL AND SMOKE COMING FROM RADIO. THE NR 2 COMM. CIRCUIT BREAKER WAS PULLED; SMELL AND SMOKE CLEARED. CREW DETERMINED IT WOULD BE BEST TO LAND AIRCRAFT AND DETERMINE CAUSE. AIRCRAFT DIVERTED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT IS BEING INSPECTED BY MAINTENANCE. 1L72 4F4 F A22CE E00053EN 20040630001482004063000148EU 2004 6 30 USAA040320 120040616A5347D5311282600101 SEAT TRACK AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 SEAT TRACK, 27 INCHES X .85 INCH X .047 INCH AREA, CORROSION; LEVEL 2; MAIN DECK FLOOR SUPPORT, FRAME 14-16, Y+503. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001492004063000149NM 2004 6 30 USA2004F00047 120040511A2530 ODOR BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE GALLEY DETECTED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19446US 24873 CREW ADVISED OF A BURNING RUBBER ODOR IN THE AFT GALLEY. THE MAIN GALLEY POWER SWITCH WAS SECURED AND THE ODOR DISSIPATED. MAINTENANCE INSPECTED THE AREA AND OPERATED THE GALLEY EQUIPEMENT. NOT PROBLEM WAS FOUND. 2L72 4F4 FRTA16WE E2GL 20040630001502004063000150NM 2004 6 30 USA2004F00048 120040513A32606558225029 CIRCUIT CARD BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE MLG MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19591US 23936 AFTER TAKEOFF, THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED OPERATION OF NOSE LANDING GEAR DOWN LOCK SENSOR AND GEAR POSITION SENSOR. OPERATIONAL CHECK GOOD. SWUNG GEAR SEVERAL TIMES. OPERATIONAL CHECK GOOD WITH NO FAULTS FOUND. CLEANED SENSORS IAW MM AND REPLACED CIRCUIT CARD M983, AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040630001522004063000152NM 2004 6 30 AMTA200400583 120040522A3350 CONNECTOR BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11516AT 27972 EMERGENCY EGRESS LIGHT, ROW 35 AFT GALLEY INOPERATIVE. RECONNECTED EGRESS LIGHT AT ROW 35, OPS CHECK OK. 2L72 4F4 FRTA2NM A12EU 20040630001562004063000156 2004 6 30 F3LA200400065 420040606A2200C12850AC02 CONTROL UNIT AIRBUSA318 A318111 3940019EU COCKPIT ODOR A F3LAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03803FR2518 2017 IN CRUISE CREW REPORTED SMOKE COMING FROM FLIGHT CONTROL UNIT. NO ECAMS NOTED, SMOKE/AVNCS SMOKE. QRH PROCEDURE APPLIED, EMERGENCY DECLARED. DIVERTED TO OKC & LANDED WITHOUT INCIDENT. PERFORMED INSPECTION OF FWD E&E BAY, MID & AFT E&E BAY, MID LT E&E BAY AND NO DAMAGE FOUND. FOUND FCU HAD SMELL OF BURNED WIRE INSULATION. REMOVED FCU, INSPECTED WIRING FWD TO LT & RT BEHIND LCD'S AND GLARESHIELD, NO DAMAGE FOUND. INSTALLED NEW FLIGHT CONTROL UNIT. PERFORMED LIGHT OPS TEST, TESTED GOOD. PERFORMED OPS TEST OF FLIGHT CONTROL UNIT AND TESTED GOOD. PERFORMED AFS TEST, TEST PASS. PERFORMED OPS LAND, TEST PASS. CLEANED AND STOWED CREW O2 MASKS. 2L72 4F RT 20040630001582004063000158NM 2004 6 30 N150AW0001 120040525A5320 WEB BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 WEB DAMAGED AFT OF R-2 DOOR. REPLACED WEB PER SRM 51-10-02. 2L72 4F RTA16WE 20040630001802004063000180 2004 6 30 372PA0045 420040605A2230735SUE912 COMPUTER BOEING737 737306 13844BGNM AUTO THROTTLE MALFUNCTIONED A PIDAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO05372PA 23546 AUTO THROTTLE DISENGAGES IN LEVEL FLIGHT. WILL NOT RE-ENGAGE. REPLACED AUTO THROTTLE COMPUTER. OPS CHECK AND BITE TEST OK. REF ATA 22-30. 2L72 4F RTA16NE 20040630001822004063000182CE 2004 6 30 GLBA20030637 120040610A3210 LANDING GEAR BEECH 1900 1900D 1154162CE LEFT MALFUNCTIONED A GLBAO OTHER J WARNING INDICATION CRCRUISE 1 NM03253GL UE253 LEFT MLG WILL NOT STAY RETRACTED, NFF OPS CHECK GOOD. 2L72 4T RTA24CE 20040630001882004063000188NM 2004 6 30 N150AW0016 120040525A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 IMPROPER REPAIR INSTALLED AT BS 887 AT STR 20 RT AND AT BS 500A AT STR 10 LT ACCORDING TO AD2002-07-10 AND SB737-53A1177. REPLACED EXISTING REPAIRS PER SRM 53-00-014 FIG 229. 2L72 4F RTA16WE 20040701000032004070100003NM 2004 7 1 SWAA041818 120040628A53306555074 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT NR 1 COCKPIT WINDOW OUTBOARD UPPER CORNER, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040701000062004070100006NM 2004 7 1 SWAA041821 120040628A53116554892 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 348, LBL 60, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040701000142004070100014NM 2004 7 1 UPS04542554 120040610A2120 INSULATION BOEING757 75724APF 1384969NM AIR DUCT DETERIORATED A IPXAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01424UP 25369 CREW NOTICED ELECTRICAL SMOKE SMELL DURING TAXI. DID BTB FOR FURTHER INSPECTION. CREW COULD NOT DETERMINE SOURCE. FOUND AIR DISTRIBUTION DUCT INSULATION DETERIORATED AND HAD FALLEN ACROSS WIRING & C/B'S IN THE UPPER PORTION OF THE OVERHEAD P-11 PANEL. REMOVED DETERIORATED INSULATION & CLEANED BACK OF P-11 PANELS, NO OTHER FAULTS NOTED. 2L72 4F RTA2NM 20040701000402004070100040NM 2004 7 1 N150AW0013 120040525A5312 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 HFEC REVEALED CRACK INDICATIONS ON THE I/B SIDE OF VERTICAL STRAP ON THE BS 178 BULKHEAD AT RBBL 5.7 AND WL 201 AND THE I/B SIDE OF THE VERTICAL STRAP AT LBBL 5.7 AND WL 198.5. REPAIRED CRACKED AREAS PER SRM 53-10-8. 2L72 4F RTA16WE 20040701000452004070100045NM 2004 7 1 N150AW0005 120040525A5320 THRESHOLD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 FORWARD CORNER OF THE FORWARD CARGO DOOR THRESHOLD IS CRACKED. REPAIRED PER BAC 5975. 2L72 4F RTA16WE 20040701000462004070100046NM 2004 7 1 N150AW0021 120040525A5330651635227 BEAR STRAP BOEING737 7373G7 1384595NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 CORROSION BETWEEN STRAP AND SKIN AT BS 490 AT STR 28 RT AND IMPROPER REPAIR AT STR 27 RT AT BS 476 PER AD 2002-07-10 AND SB737-53A1177. REPAIRED PER EA NR 53-090. 2L72 4F RTA16WE 20040701000742004070100074NM 2004 7 1 SWAA041798 120040627A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS AT L2 DOOR LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040701000752004070100075NM 2004 7 1 SWAA041799 120040627A57436567172 FITTING BOEING737 7373H4 1384600NM MLG WW WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT MLG FWD AND AFT STAB FITTINGS WORN. REPAIRED LT AND RT MLG STAB FITTINGS PER EA AND OHM. 2L72 4F RTA16WE 20040701000812004070100081 2004 7 1 SWAA041805 420040628A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040701000832004070100083 2004 7 1 SWAA041807 420040628A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040701000892004070100089NM 2004 7 1 N150AW0022 120040525A5314 KEELBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 CORROSION ON THE HORIZONTAL FLANGE OF THE KEEL BEAM AT STR 28 RT SPLICE AT BS 500C + 9.0. REPAIRED PER EA NR 53-087. 2L72 4F RTA16WE 20040701000962004070100096 2004 7 1 SWAA041814 420040628A2565D31354 SLIDE BOEING737 7373T5 1384608NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040701000972004070100097NM 2004 7 1 SWAA041815 120040628A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R, BS 500B AND STRINGER 25L, BS 956, CORRODED. REPAIRED STRINGER SECTIONS PER SRM. 2L72 4F RTA16WE 20040701000982004070100098NM 2004 7 1 UPS04242550 120040609A3350 LIGHT BOEING727 72731C 1384011NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 EMERGENCY EXIT LIGHTS NOT OPERATING. RESEATED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL. 2L73 4F A3WE 20040701001002004070100100WP 2004 7 1 UPS04842545 120040508A534047723981 FITTING DOUG DC8 DC873F 302199FWP L1766 30R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE: C-2, FWD OF AFT PRESSURE BULKHEAD AT BS 1766 LONGERON 30 SPLICE FITTING HAS CORROSION (DOT E 2880). REMOVED CRACKED FITTING. FOUND OUT OF LIMITS. REC'D LONGERON END FITTING P/N 4772398-1 PO 446277.2 IAW DWGS 4772398. LOCATED, DRILLED & DEBURRED FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-21. ALODINED & PRIMED IAW DC8 SRM 51-1-8. 2L74 4F RT4A25 20040701001012004070100101WP 2004 7 1 UPS04842549 120040605A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHILE PERFORMING EMERGENCY LIGHT CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK. LIGHTS OPS CHECKED NORMAL REFERENCE MM 33-50-01-2. 2L74 4F RT4A25 20040701001022004070100102NM 2004 7 1 AWXA200400608 120040525A575465C26793 SKIN BOEING737 7373G7 1384595NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW THE ACTUATOR AT SS 68.26. MAINTENANCE CUT OUT CRACKED SLAT SKIN AT SS 68.26 AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 PG 216-219. 2L72 4F RTA16WE 20040701001042004070100104NM 2004 7 1 AWXA200400610 120040604A575465C267933 SKIN BOEING737 7373G7 1384595NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND EMANATING FROM STOP DRILL HOLES IN NR 4 SLAT LOWER OUTBOARD SKIN AT SS 116.75. MAINTENANCE CUT OUT CRACKED SLAT SKIN AT SS 116.75; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20040701001052004070100105NM 2004 7 1 AWXA200400611 120040526A532065468225 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION FOUND ON CABIN FLOOR LT OUTBOARD SHEAR WEB BETWEEN BS 727D AND BS 727D+10, LBL 69, WL 208. MAINTENANCE REMOVED CORRODED SECTION OF LT OUTBOARD SHEAR WEB FROM BS 727D TO BS 727D+10, LBL 69, WL 208; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-46822; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040701001062004070100106EU 2004 7 1 161041 120040608A1420 CONNECTOR SAAB SF340 340B 7860101EU EMERGENCY LIGHT DAMAGED A NSVAK NONE O OTHER ININSP/MAINT 1 EA27242CJ 340B242 LEFT OVERWING EMERGENCY EXIT SIGN INOP. FOUND WIRES IN CONNECTOR SEVERED, RE-INSTALLED IAW SAAB 33-50-00, OP CHECKED GOOD. 2L72 4T RTA52EU 20040701001082004070100108NM 2004 7 1 P5CA0401099 120040412A7810314U210070 NOZZLE BOEING747 74746NF 13848BTNM GE CF6 CF680 30025NE ENGINE EXHAUST DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23450PA 30808 706123 NR 1 ENGINE EXHAUST NOZZLE HAS A DENT AT 7 O`CLOCK 5.125 LONG .5 INCH WIDE AND .001 INCH DEEP, BEYOND .80 LIMIT. REMOVED AND REPLACED EXHAUST NOZZLE. 2L74 4F4 FRTA20WE E13NE 20040701001092004070100109NM 2004 7 1 USA2004F00055 120040525A335020121 CHARGER BOEING737 737401 1384701NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19425US 23992 MAINTENANCE REPORTED NUMEROUS EMERGENCY LIGHTS, THROUGHOUT THE INTERIOR CABIN, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040706000042004070600004NM 2004 7 6 04FDEA01755 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187", FINAL DIAMETER=1.255 AND REPAIRED AS PER FEDEX EA 1-5750- 76775, TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP - PIVOT BORE - REPAIR. 2L73 4F RTA22WE 20040706000062004070600006NM 2004 7 6 04FDEA01757 120040616A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK FOUND WORN AT STA 492 RIGHT 63. 2L73 4F RTA22WE 20040706000092004070600009NM 2004 7 6 04FDEA01711 120040614A5744ARC0502 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.495 INCH, MATERIAL REMOVED = 0.015 INCH, REMAINING THICKNESS = 0.480 INCH. FOUND WITHIN LIMITS AS PER DWG: ARC0502. 2L73 4F RTA22WE 20040706000122004070600012NM 2004 7 6 04FDEA01714 120040614A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. 2L73 4F RTA22WE 20040706000132004070600013EU 2004 7 6 04FDEA01746 120040615A2910 WARNING LIGHT AIRBUS300 A300F4605R 3930327EU GREEN HYD SYS ILLUMINATED A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25680FE 794 T/O PLUS 1 HR, DURING DESCENT TO FL240, GOT ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY. GAGE AND ECAM SCHEMATIC SHOWED QUANTITY AT THE RED DOT LEVEL. TURNED OFF GREEN PUMPS, MANUALLY EXTENDED THE GEAR, UTILIZED THE ALTERNATE BRAKE SYSTEM AND LANDED AT MSY. AFTER GEAR WAS MANUALLY LOWERED, QUANTITY SHOWED JUST BELOW TOP HAT. PERFORMED A VISUAL INSPECTION OF THE A/C TO DETERMINE IF ANY EVIDENCE OF HYDRAULIC FLUID LEAKAGE IS PRESENT, NONE FOUND. SERVICED GREEN SYSTEM RESERVOIR PER MM 12-12-29-0. RESTORED LANDING GEAR SYSTEM TO NORMAL CONDITION AFTER LANDING GEAR FREEFALL PER MM 32-33-00-2. RAN ENGINES 1 & 2 PER JRH AND OPERATED ALL FLIGHT CONTROLS THROUGH THE FULL RANGE OF MOTION. 2L72 4F RTA35EU 20040706000142004070600014NM 2004 7 6 04FDEA01747 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040706000172004070600017NM 2004 7 6 04FDEA01750 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040706000182004070600018NM 2004 7 6 04FDEA01751 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040706000202004070600020NM 2004 7 6 04FDEA01715 120040614A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. 2L73 4F RTA22WE 20040706000212004070600021NM 2004 7 6 04FDEA01716 120040614A5744ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402 - 407. ORIGINAL THICKNESS = 0.452 INCH, MATERIAL REMOVED = 0.002 INCH, REMAINING THICKNESS = 04.50. COMPLIED WITH FEDEX EA 15740-76741, WINGS - LEFT AND RIGHT - OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY. 2L73 4F RTA22WE 20040706000222004070600022WP 2004 7 6 04FDEA01717 120040203A5512 SKIN DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25569FE 47828 HORIZONTAL STABILIZER - UPPER COSTANT SECTION AND OUTBOARD SKINS CRACKS WITHIN FLYABLE LIMITS. PANELS INVOLVED: ALC7436-1, ALC7437-1, ALC7207-1 AND ALC7208-1. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73235. 2L73 4F A22WE 20040706000232004070600023WP 2004 7 6 04FDEA01718 120040302A5710 ANGLE DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25569FE 47828 EXISTING REPAIR SPLICE ON LEFT WING STRINGER 4 CRACKED AT XORS 930. CRACKED REPAIR ANGLE REPLACED BY A NEW REPAIR ANGLE MADE FROM 7075-73511 THAT ARE MORE FATIGUE RESISTANT IAW FEDEX EA 8-5710-73240. 2L73 4F A22WE 20040706000242004070600024WP 2004 7 6 04FDEA01719 120040204A5720ARB07601 CAP DOUG DC10 DC1010 3022110WP RT & LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25569FE 47828 RIGHT AND LEFT WING UPPER CAP CRACKED AT XORS 372. THE CRACKS ARE AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED. REPAIR ANGLE AND DOUBLERS HAVE BEEN INSTALLED IAW FEDEX EA 8-5710-73236. 2L73 4F A22WE 20040706000252004070600025NM 2004 7 6 04FDEA01760 120040616A5320 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, LEFT HAND LONGERON 51 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 SUSPECT CRACKED. 2L73 4F RTA22WE 20040706000272004070600027NM 2004 7 6 04FDEA01762 120040616A5320 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 45 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED. 2L73 4F RTA22WE 20040706000282004070600028NM 2004 7 6 04FDEA01763 120040616A5320 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 49 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED. 2L73 4F RTA22WE 20040706000292004070600029 2004 7 6 04FDEA01764 420040616A3432 HOUSING DOUG MD11 MD11 3023602NM GLIDE SLOPE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 GLIDE SLOPE HOUSING MOUNTING BRACKET FOUND CRACKED. GLIDESLOPE HOUSING MOUNTING BRACKET REMOVED AND REPLACED AS PER AMM 32-21-34-4 AND GLIDESLOPE FUNCTIONAL TEST CARRIED OUT AS PER AMM 34-32-02-2, FOUND SATIS. 2L73 4F RTA22WE 20040706000302004070600030NM 2004 7 6 04FDEA01765 120040616A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CABIN FLOOR PANEL SUPPORT CORRODED AT STA 1741 RBL 63. 2L73 4F RTA22WE 20040706000312004070600031NM 2004 7 6 04FDEA01766 120040616A5320 ANGLE DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CENTER LANDING GEAR WHEEL WELL LOWER RIGHT HAND SIDE FOUND ANGLE PLATE CRACKED AT STATION 1381. 2L73 4F RTA22WE 20040706000322004070600032NM 2004 7 6 04FDEA01767 120040616A5320 ANGLE DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 CENTER LANDING GEAR WHEEL WELL LOWER LEFT HAND SIDE FOUND ANGLE PLATE CRACKED AT STATION 1381. 2L73 4F RTA22WE 20040706000332004070600033NM 2004 7 6 04FDEA01768 120040616A5740 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE INTERNAL RIB FITTING (FORWARD OUTBOARD SIDE) FOR HINGE ATTACHMENT CRACKED APPROXIMATELY 2 INCHES IN LENGTH. RIGHT HAND WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27- 50-30-4 AND FLAPS RIGGING AND OPERATIONAL CHECK CARRIED OUT AS PER MM 27-50-00-5, FOUND SATIS. 2L73 4F RTA22WE 20040706000362004070600036NM 2004 7 6 SWAA041828 120040629A53306545776 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 959, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040706000382004070600038NM 2004 7 6 SWAA041832 120040629A53106545803 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND BULKHEAD STIFFENER AT BS 291.5, RT WL 240 TO RT WL 253, CRACKED. REMOVED AND REPLACED STIFFENER PER SRM. 2L72 4F RTA16WE 20040706000402004070600040NM 2004 7 6 SWAA041835 120040629A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR LOWER FWD HINGE CUTOUT, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040706000412004070600041NM 2004 7 6 SWAA041836 120040630A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040706000422004070600042 2004 7 6 SWAA041837 420040630A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040706000442004070600044NM 2004 7 6 04FDEA01772 120040617A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK RT STA 1741 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS CORROSION. REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR PANEL SUPPORT FABRICATED AS PER DRAWING AFA3853 AND INSTALLED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040706000462004070600046NM 2004 7 6 SWAA041840 120040630A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 773, RBL 3 TO LBL 17, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040706000472004070600047NM 2004 7 6 SWAA041841 120040630A53106547957 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FWD FRAME CUTOUT, CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040706000482004070600048NM 2004 7 6 SWAA041842 120040630A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040706000492004070600049NM 2004 7 6 SWAA041843 120040630A33501619 LAMP BOEING737 7373H4 1384600NM FUSELAGE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND RT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040706000502004070600050 2004 7 6 SWAA041844 420040630A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR WILL NOT TEST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29714CB 27848 DURING SPV, R1 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040706000512004070600051NM 2004 7 6 SWAA041845 120040630A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040706000532004070600053NM 2004 7 6 SWAA041847 120040630A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 868 TO BS 886, STRINGER 1L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040706000542004070600054NM 2004 7 6 SWAA041848 120040630A5534 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FWD AND AFT BODY LUG FACE CORRODED. REPAIRED VERTICAL STAB PER ER. 2L72 4F RTA16WE 20040706000572004070600057NM 2004 7 6 04FDEA01774 120040617A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK RIGHT HAND STA 1851 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. FLOOR SUPPORT REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814 & INSTALLED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040706000582004070600058 2004 7 6 YENA200432 420040606A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU SEAT SHORTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15553JB68 1896 FLIGHT CREW REPORTED ODOR AT RIGHT MID CABIN. PERFORMED TSM TASK 24-00-00-810-823. FOUND PROBABLE CAUSE LTV SEAT ELECTRONIC BOX AT ROW 12 DEF. REMOVED AND REPLACED SEAT ELECTRONIC BOX DUE TO EVIDENCE OF ELECTRONIC ODOR IAW ATA 23-39 LIVE TV SYSTEM INTEGRETY CHECK CONCERNING ELECTRONIC ODOR. 2L72 4F RTA28NM 20040706000602004070600060WP 2004 7 6 MWEA040086 120040607A531099360791 WINDOW FRAME DOUG DC9 DC981 3022081WP NR 34 AFT UPPER LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 LIGHTNING STRIKE ON LEFT SIDE CABIN WINDOW FRAME NR 34 ON AFT UPPER SIDE. BLENDED OUT DAMAGE, ACCEPTABLE FOR STRENGTH AS IS. 2L72 4F A6WE 20040706000612004070600061NM 2004 7 6 04FDEA01775 120040617A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK STA 1890 TO STA 2007 RIGHT HAND LONGITUDINAL FLOOR SUPPORT X=59 HAS CORROSION. CORROSION REMOVED AS PER SRM 51-35-01 VOL II. FABRICATED NEW FLOOR SUPPORT AS PER DRAWING AGA7551 AND FPI CARRIED OUT AS PER DPS 4-707 AND FOUND NO CRACK AND INSTALLED AS PER AMM 20-50-02. 2L73 4F RTA22WE 20040706000632004070600063NM 2004 7 6 04FDEA01777 120040617A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK FOUND CRACKED AT STA 905 RT 28. REMOVED AND REPAIRED IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040706000642004070600064NM 2004 7 6 04FDEA01696 120040611A2612473925 CONTROL UNIT BOEING727 727200 138407ENM FIRE DETECTION MALFUNCTIONED A FDEAFD ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO25270FE277 277 22035 FORWARD LOWER CARGO COMPARTMENT FIRE INDICATION ON TAXI OUT. NO ACTUAL FIRE REPORTED BY FIRE DEPARTMENT AFTER FIRE BOTTLES DISCHARGED INTO FWD LOWER CARGO COMPARTMENT. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES AND THE CARTRIDGES PER MM 26-17-014-2. SYSTEM STILL GIVING THE SMOKE INDICATION, BELL, AND FAULT LIGHT ON A, B AND BOTH, WITH ALL DETECTORS DISCONNECTED NO CHANGE. SUSPECT CEU AND (1) IN STOCK INDY. REMOVED AND REPLACED CONTROL ELECTRONIC UNIT IN FWD LWR CARGO COMPT PER MM 26-17-012-2. OPS CHECK NORMAL, A/C OK FOR SERVICE. 2L73 4F RTA3WE 20040706000662004070600066NM 2004 7 6 SWAA041854 120040701A3350101114 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 EMERGENCY EXIT LIGHT LENS MISSING AT RT OVERWING EXIT. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040706000672004070600067 2004 7 6 SWAA041855 420040701A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040706000682004070600068NM 2004 7 6 SWAA041856 120040701A335007912 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29412WN 29818 EEPLS LIGHT COVER MISSING AT LT ROW 1. REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040706000702004070600070NM 2004 7 6 SWAA041858 120040701A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 380, STRINGER 16R, BS 400, STRINGER 17R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040706000722004070600072NM 2004 7 6 SWAA041860 120040701A57536546434370 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29618WN 28034 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040706000742004070600074NM 2004 7 6 04FDEA01783 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR. 2L73 4F RTA22WE 20040706000772004070600077NM 2004 7 6 04FDEA01786 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040706000802004070600080NM 2004 7 6 04FDEA01789 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIG THK 0.52 MATERIAL REMOVED 0.033 REMAINING THICKNESS 0.487 & FOUND WITHIN LIMITS AS PER DWG TOLERANCE OF ARC0502. 2L73 4F RTA22WE 20040706000822004070600082NM 2004 7 6 04FDEA01791 120040618A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK FOUND WORN AT STA 699 LBL 47 INCHES. 2L73 4F RTA22WE 20040706000842004070600084WP 2004 7 6 04FDEA01695 120040611A5414 PANEL DOUG DC10 DC1010 3022110WP ZONE 400 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568051 47805 COMPLY WITH EA 8-5410-78219, PYLON HORIZONTAL ENGINE PYLON LT ACCESS PANEL REPAIR. COMPLIED WITH EA 8-5410-78219. 2L73 4F A22WE 20040706000852004070600085NM 2004 7 6 04FDEA01733 120040614A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK RT STA 1741 TO STA 2007 SEAT TRACK REF X=102.5 SEAT TRACK HAS CORROSION. SEAT TRACK REMOVED AS PER SRM 51-21-01 VOL II, FOUND EXCEEDED LIMIT: ORIG. THICKNESS =0.080, MATERIAL REMAINED=0.043, MATERIAL REMOVED =0.037 AS PER SRM 53-70-00 FIG 3 PAGE 7 VOL I. SEAT TRACK SPLICED AND REPAIRED AS PRE SRM53-70-00 FIG7 VOL I AND SRM 53-70-00 FIG1 VOL I. 2L73 4F RTA22WE 20040706000862004070600086NM 2004 7 6 04FDEA01736 120040615A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK FOUND CORROSION AT STA 5-113 LEFT HAND 8 INCHES. 2L73 4F RTA22WE 20040706000882004070600088NM 2004 7 6 04FDEA01738 120040615A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT WING O/B FLAP VANE - OVAL SHAPE HOLE ON NR 1 TEE FITTING (FIRST FROM I/B SIDE) FOUND CORRODED. LT WING OUTBOARD FLAP VANE REMOVED AS PER CMM 20-10-02; ORIGINAL HOLE OVAL SIZE=0.860 X 0.560, REWORKED TO SIZE=0.870 X 0.600; FPI CARRIED OUT IAW CMM20-30-02 REV 42, FOUND NO CORROSION AND NO CRACK EVIDENT; SLIP FIT BUSHING MACHINED AS PER SRM57-20-00 FIG18 PAGE47 VOL I & INSTALLED AS PER MM27-50-34-4. INSTALLATION OF LT WING FLAP VANE MOST INBOARD TEE FITTING AS PER CMM57-52-04. 2L73 4F RTA22WE 20040706000892004070600089NM 2004 7 6 04FDEA01792 120040618A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK FRAME FOUND DENT AT STA 535 LONGERON L19-24. 2L73 4F RTA22WE 20040706000922004070600092NM 2004 7 6 SWAA041862 120040701A53306545890 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 349, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040706000932004070600093NM 2004 7 6 SWAA041850 120040701A2910BACH8B04EE0207 HOSE BOEING737 7372H4 138448CNM NLG WW LEAKING A SWAAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW29091SW 22963 AIR TURNBACK/DECLARED EMERGENCY. AFTER TAKEOFF NLG WOULD NOT RETRACT AND A-SYSTEM HYDRAULIC QTY WAS DECREASING. REMOVED AND REPLACED NLG ACTUATOR UPLOCK HOSE. 2L72 4F A16WE 20040706000942004070600094 2004 7 6 SWAA041851 420040701A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040706000972004070600097NM 2004 7 6 SWAA041863 120040701A5312BAC1514 STIFFENER BOEING737 7373T5 1384608NM BULKHEAD CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND RADIAL STIFFENER AT BS 1016, BL 0, CORRODED. REPAIRED STIFFENER PER SRM. 2L72 4F RTA16WE 20040706001002004070600100WP 2004 7 6 04FDEA01744 120040615A5247 DRAIN PAN DOUG DC10 DC1010 3022110WP APU DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 APU DOOR EXTERIOR DRAIN PAN CRACKED. REMOVED DRAIN PAN IAW TRAVELER T4/436545. INSTALLED NEW DRAIN PAN IAW SRM 51-31-01. 2L73 4F A22WE 20040706001022004070600102NM 2004 7 6 SWAA041865 120040701A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 DURING SPV, FOUND PHOTOLUMINESCENT STRIP OUT OF POSITION. PLACED PHOTOLUMINESCENT STRIP IN PROPER POSITION PER ACO. 2L72 4F RTA16WE 20040706001042004070600104NM 2004 7 6 SWAA041867 120040701A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29706SW 27840 DURING SPV, FOUND PHOTOLUMINSCENT STRIP OUT OF POSITION. PLACED PHOTOLUMINESCENT STRIP IN PROPER POSITION PER ACO. 2L72 4F RTA16WE 20040706001052004070600105NM 2004 7 6 04FDEA01778 120040617A5710 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING LOWER WINGLET WING SIDE - AFT INTERNAL MOUNT BOLT HOLE AREAS HAVE MINOR SURFACE CORROSION. 2L73 4F RTA22WE 20040706001072004070600107WP 2004 7 6 04FDEA01780 120040121A5512ALC72041 SKIN DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 DURING ACCOMPLISHMENT -F- TO -ACF- AT OAN, INSPECTION FOUND CRACKS IN 2 LWR CONSTANT SECTION SKINS OF THE HORIZONTAL STAB. THE CRACKS WHERE WITHIN FLYLABLE LIMITS. HOWEVER, DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PLANKS AND CONTINUE INSPECTION OF THE SKINS PER EO 8-5510-7-2307 PART 1 AT 24 MONTH INTERVALS. THE WORK IS BEING ACCOMPLISHED PER SB 55-16 FOR GROUP 1 A/C. 2L73 4F A22WE 20040706001102004070600110EU 2004 7 6 04FDEA01721 120040614A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25652FE 735 INSIDE COURIER AREA AT FLOOR LEVEL NR 3 RIGHT SEAT TRACK HAS AN AREA OF CORROSION ABOUT 6 INCHES LONG AT FRAME 18. REMOVED AND REPLACED NR 3 RIGHT SEAT TRACK PER A300 SRM 51-40-21. 2L72 4F RTA35EU 20040706001112004070600111EU 2004 7 6 04FDEA01722 120040614A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25652FE 735 INSIDE COURIER AREA AT FLOOR LEVEL AND FRAME 18 THE NR 1 LEFT SEAT TRACK HAS CORROSION. REMOVED AND REPLACED NR 1 LEFT SEAT TRACK AT FR18 IAW A300 SRM 51-40-21. 2L72 4F RTA35EU 20040706001132004070600113NM 2004 7 6 04FDEA01769 120040616A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK FOUND WORN AT STA 792 RIGHT 48 INCHES. 2L73 4F RTA22WE 20040706001152004070600115NM 2004 7 6 04FDEA01702 120040612A5315 FLOORBEAM BOEING727 727200 138407ENM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25244FE 21647 FLOORBEAM AND SHEAR WEB STA 1130, RBL 19 (TOP CHORD) EXFOLIATED. INSTALLED SEAT TRACK, 2 STRAPS AND T-CHORD IAW SRM 51-30-2. INSTALLED REPAIR IAW SRM 53-10-8. 2L73 4F RTA3WE 20040706001162004070600116WP 2004 7 6 04FDEA01703 120040612A5753 ANGLE DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 LEFT I/B FLAP, AFT END OF I/B FAIRING, ANGLE IS GOUGED. REMOVED ANGLE IAW SRM 51-31-01. FAB ANGLE ON TRAVLER T4/436154 IAW SRM 57-52-01. INSTALLED ANGLE IAW SRM 51-31-01. 2L73 4F A22WE 20040706001172004070600117NM 2004 7 6 04FDEA01704 120040612A5310 SHEAR TIE BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25244FE 21647 FWD CARGO COMPT BILGE AREA HAS A CORRODED SHEAR TIE FS 520, STR 26L - 27L. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. 2L73 4F RTA3WE 20040630000822004063000082NM 2004 6 30 GAIA04075OP 120040506A33501000677 LIGHT BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE COCKPIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW076827 20180 L-1 EMERGENCY EXIT LIGHT DIM, COCKPIT EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED (L-1 AND COCKPIT) EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040630000842004063000084EA 2004 6 30 A6WA200440067 120040527A76032100140007 GEARBOX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT ENG THROTTLE DAMAGED A A6WAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL31421ZW13146 7346 LT THRUST LEVER WHEN MOVED TO IDLE STOP SHUT OFF FUEL TO ENGINE. 2 INCH PLAY IN THRUST LEVER WITH NO ENGINE RESPONSE. REMOVED AND REPLACED THROTTLE CONTROL GEARBOX. OPS CHECK GOOD. IWA ENG SHOP MANAGER, REMOVED AND REPLACED NR 1 ENGINE THROTTLE GEARBOX IAW 76-11-17-400-801 C/W RIGGING AND SAFETIED T/R CABLE RIGGING REF 118912 NR 2. 2L72 4F4 FRTA21EA E15NE 20040630000882004063000088EU 2004 6 30 USA2004F00043 120040514A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19707UW14805 0949 THE LT SIDE EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE MID CABIN LT SIDE EMERGENCY POWER SUPPLY UNIT. OPS CHECKED, OK. 2L72 4F4 FRTA28NM E2GL 20040630000902004063000090EU 2004 6 30 USAA040236 120040518A5311D5347218920200 FRAME AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19701UW15935 0890 FRAME, 1.100 INCH X 1.00 INCH X 0.62 INCH, CORROSION. REPLACED NEW FRAME IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000932004063000093EU 2004 6 30 USAA040316 120040610A5311D5347218820400 FRAME AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FR68,Y1292,Z240 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FRAME, 4.5 INCH X 1.75 INCH X .064 INCH AREA, CORROSION; LEVEL 2; FR68, Y1292, Z240. INSTALLED NEW FRAME IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001062004063000106 2004 6 30 GAIA04076OP 420040525A3442 INDICATOR BOEING727 727224 1384076NM PWA JT8 JT8D9 52048NE COCKPIT MALFUNCTIONED A GAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0769735 20664 AFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. INSPECTED RADAR SYSTEM, FOUND BAD RADAR INDICATOR, TRANSFERRED TO DMI NR 1855 IAW MEL 34-21, CAT (C) DUE. 2L73 4F4 F A3WE E2EA 20040630001142004063000114EU 2004 6 30 USAA040252 120040527A5320D5348015800300 PLATE AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19102UW13221 0844 PLATE CORROSION, 4 INCH X 4 INCH X .70 INCH DEEP. REMOVED AND REPLACED PORT IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001152004063000115EU 2004 6 30 USAA040253 120040527A5320D5367010900700 ANGLE AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19102UW 0844 ANGLE CORROSION, 2.0 INCH X 2.0 INCH X .02 INCH DEEP. REMOVED AND REPLACED PART IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001192004063000119EU 2004 6 30 USAA040240 120040522A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19701UW15935 0890 DOOR SILL, 1.0 INCH L X 1.2 INCH W X .08 INCH D. REMOVED AND REPLACED DOOR SILL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001202004063000120EU 2004 6 30 USAA040247 120040526A5315D5347217220290 FLOORBEAM AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FR66,68,Y1270 CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19102UW13221 0844 FLOORBEAM, 3.0 INCH X 1.5 INCH X .03 INCH AREA. CORROSION; LEVEL 2. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001292004063000129EU 2004 6 30 USAA040269 120040608A5320 PLATE AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19710UW16211 1019 PLATE ASSY, 6 INCHES X 4 INCHES X 0.060 INCH DEEP, CORROSION; LEVEL 2; FR68, Y1732, Z240. REPLACED WITH NEW PART IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001382004063000138CE 2004 6 30 UNI2004F00000 120040517A575326220753 FLAP TRACK CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA WINGS CORRODED E UNIAO OTHER O OTHER NRNOT REPORTED 1 WP25127HA17308 208B0148 UPON PERFORMANCE OF INSPECTION OPERATION MD OF MFG MM, SEVERE EXFOLIATION, CORROSION WAS FOUND ON BOTH OB FLAP TRACKS. AREAS ON FLAP TRACK WHERE CORROSION WAS DISCOVERED INCLUDE: AFT RECESSED WEB AREA AND ADJACENT UPPER AND LOWER PORTIONS OF TRACK. CONTRIBUTING FACTORS TO THIS INCLUDE; AIRCRAFT EXPOSED TO SALT AIR ENVIRONMENT FIRST YEARS OF LIFE AND HAS CONTINUED TO LIVE OUTSIDE. RECOMMEND INITIAL INSPECTION INTERVAL OF 15,000 LANDINGS BE REDUCED. (17308 LANDINGS) 1H71 3T3 T A37CE E2NE 20040630001402004063000140SO 2004 6 30 FO72004F00001 120040521A29103188602 PLATE PIPER PA23 PA23250 7102308SO HYD POWERPACK CRACKED B FO7RO OTHER O OTHER NRNOT REPORTED 1 SO13545044695 273369 UPON GEAR RETRACTION, PILOT NOTICED GEAR UNSAFE LIGHT, GEAR WOULD NOT EXTEND, HAND PUMP TRIED, NO PRESSURE, CO2 BOTTLE PULLED, HYDRAULIC POWER PACK COVER LIFTED AND CAUSED FLUID TO LEAK OVER INTO COCKPIT FLOOR, AIRCRAFT LANDED GEAR UP WITH MINOR DAMAGE, HYDRAULIC POWER PACK DISASSEMBLED AND FOUND HOLD DOWN PLATES (PN 31886-02, 03) CRACKED ALLOWING RELIEF VALVE BODY TO UNSEAT SO NO HYDRAULIC PRESSURE COULD BE ROUTED TO SYSTEM, A POWER PACK REBUILD SHOP SAID THIS IS A COMMON PROBLEM. 1L72 3O 1A10 20040630001702004063000170NM 2004 6 30 PCAA0406218 120040608A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM CARGO BAY FALSE ACTIVATIONA PCAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA13815EX3006014010 321 FLIGHT 3921 REPORTED CARGO SMOKE LIGHT ILLUMINATING FOR 3 TO 4 SECONDS THEN EXTINGUISHING. FLIGHT ATTENDANT INSPECTED THE AREA AND FOUND NO SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SMOKE DETECTOR AND OPERATIONAL CHECKED THE SYSTEM, ALL CHECKS GOOD. 2H72 4T RTA13NM 20040630001792004063000179 2004 6 30 P9RA20040017 420040610A2565D31041147 SLIDE BOEING757 757236 1384971NM R3 DOOR ACTIVATED A P9RAK NONE O OTHER ININSP/MAINT 1 SO11962PG 24119 WHILE THE AIRCRAFT WAS IN MAINTENANCE, THE R3 DOOR SLIDE WAS DEPLOYED BY ACCIDENT. REMOVED AND REPLACED R3 DOOR SLIDE IAW BMM 25-66. 2L72 4F RTA2NM 20040630001842004063000184 2004 6 30 GLBA20030553 420040203A3414 INDICATOR BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM03247GL UE247 FAILURE OF FIRST OFFICER'S A/S INDICATOR. PERFORMED GROUND CHECK, FOUND NO DEFECTS. 2L72 4T RTA24CE 20040701000072004070100007NM 2004 7 1 SWAA041822 120040628A53106547977 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 580, RBL 65, CRACKED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040701000082004070100008 2004 7 1 SWAA041823 420040624A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29715SW 27849 DURING SCHEDULED HC1 CHECK, R1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040701000092004070100009NM 2004 7 1 SWAA041824 120040629A534065C360751 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR LOWER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SAM FORM. 2L72 4F RTA16WE 20040701000342004070100034NM 2004 7 1 QXEA200400398 120040607A1430 RIVET DHAV DHC8 DHC8202 2809007NM ZONE 300 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - THERE ARE THREE SMOKING RIVETS ON AFT RUDDER LOWER LEFT SIDE. REPAIRED IAW DHC8 SRM 51-40-00. 2H72 4T RTA13NM 20040701000352004070100035NM 2004 7 1 QXEA200400400 120040604A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LOOSE A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09412QX 4059 SEA - ON FLIGHT NUMBER 2312, ON TAKEOFF ROLL AT 60 KIAS, RECEIVED FUSELAGE DOOR WARNING. ABORTED TAKEOFF. FOUND AFT BAGGAGE DOOR UN-LATCHED. DOOR HANDLE POPPED OUT. CLEANED AND INSPECTED DOOR HANDLE STOWAGE LATCH. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040701000432004070100043NM 2004 7 1 N150AW0019 120040525A5312 PRESSURE PANEL BOEING737 7373G7 1384595NM FUSLEAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 CORROSION AT BS 1016 AT LOWER DRAIN HOLE ON FORWARD SIDE OF THE PRESSURE PANEL. REPAIRED PER SRM 53-80-08. 2L72 4F RTA16WE 20040701000512004070100051NM 2004 7 1 AWXA200400628 120040526A5320146N5318 SHEAR PLATE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK BETWEEN BS 1681 AND BS 1720 LBL 50. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK FROM BS 1681 AND BS 1720 LBL 50; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2L72 4F RTA2NM 20040701000662004070100066NM 2004 7 1 DHL2004751001 120040605A3350MISC062 BATTERY BOEING727 727264 138408MNM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 COCKPIT EMERGENCY EXIT LIGHT BATTERY LOW. REMOVED AND REPLACED BATTERIES IAW 33-50-71. OPS CHECKED GOOD. P/N: MISC062. 2L73 4F A3WE 20040701000672004070100067NE 2004 7 1 P9RA20040015 220040531A753239271611 BLEED VALVE BOEING737 737231 1384079NM PWA JT8 JT8D217C 52053NE NR 3 ENGINE ODOR A P9RAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO1154344 21631 SMOKE ODOR IN CABIN AFTER TAKEOFF FROM IAH. RETURNED TO IAH, NOT OVERWEIGHT. REMOVED AND REPLACED NR 3 ENGINE HIGH PRESSURE BLEED VALVE IAW BMM 36-12. ENGINE RUN UP AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E9NE 20040701000682004070100068NM 2004 7 1 N150AW0006 120040525A5340 ATTACH ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 FRAME SHELF ATTACH ANGLES CRACKED AT BS 294.5 AT STR 12 RT, STR 11 RT, AND AT STR 10 RT. REPLACED ANGLES PER SRM 51-10-02. 2L72 4F RTA16WE 20040701000712004070100071NM 2004 7 1 SWAA041795 120040627A53116936642 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SPV, FOUND BULKHEAD LOWER LT SIDE FRAME AT BS 178, CRACKED. REMOVED AND REPLACED SIDE FRAME PER ACO. 2L72 4F RTA16WE 20040701000782004070100078 2004 7 1 SWAA041802 420040627A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040701000852004070100085NM 2004 7 1 SWAA041809 120040628A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED A2 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040701000992004070100099WP 2004 7 1 UPS04842544 120040510A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2 ALC, CORROSION AROUND FASTENERS, HOLE ON CABIN, FLOORBOARD PANEL FS 1040 RBL 45. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FLOORBOARD FROM 840 TO 1060 RT RBL 45, CUT SEAT TRACK FROM 870-1050 IAW EO DC853205167C, MAT ID SEAT TRACK AND 1 SPLICE FITTING P/N DC8-003-501 PO SPO94445 SEAT TRACK P/N 2772660 PO -O-. LOCATED, DRILLED, DEBURR & 2 SPLICES. ALODINED & PRIMED. INSTALLED SEAT TRACK. INSTALLED FLOORBOARD FROM 840-1060. 2L74 4F RT4A25 20040701001032004070100103NM 2004 7 1 AWXA200400609 120040526A531369414372 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A .625 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 663.75, STR 10 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 663.75, STR 10 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20040701001072004070100107NE 2004 7 1 P5CA0401100 220040603A7321WVG21246 MEC BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 1 ENGINE FAILED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23509MC 21221 530388 AFTER ENGINE START, NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT, IDLE PARAMETERS NORMAL. REPLACED MEC PER AMM 73-21-01. 2L74 4F4 F A20WE E23EA 20040706000022004070600002NM 2004 7 6 04FDEA01753 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040706000032004070600003NM 2004 7 6 04FDEA01754 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040706000072004070600007NM 2004 7 6 04FDEA01758 120040616A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK - SEAT TRACK FOUND WORN AT STA 492 RT 63. 2L73 4F RTA22WE 20040706000082004070600008NM 2004 7 6 04FDEA01633 120040607A5315AFA0043 FLOORBEAM DOUG MD11 MD11 3023602NM LWR CTR CARGO CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25578FE 48458 FOUND LWR FLOORBEAM IN CENTER CARGO COMP AT APPROX FRAME STA 1701 AT APPROX 30 INCHES FROM CENTER LINE ON RT SIDE. NOTE: THERE IS ALSO DAMAGE TO LT SIDE. 2L73 4F RTA22WE 20040706000112004070600011NM 2004 7 6 04FDEA01713 120040614A5744ARC0502 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.224 INCH. COMPLIED WITH FEDEX EA 1-5740-76742, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040706000192004070600019NM 2004 7 6 04FDEA01759 120040616A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK AT R1 DOOR WAY FOUND CORRODED. 2L73 4F RTA22WE 20040706000262004070600026NM 2004 7 6 04FDEA01761 120040616A5320 FITTING DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 CENTER CARGO COMPARTMENT BILGE AREA, RIGHT HAND LONGERON 44 SPLICE FITTING BETWEEN STA 5-113 AND STA 1541 FOUND CRACKED. 2L73 4F RTA22WE 20040706000352004070600035NM 2004 7 6 SWAA041827 120040629A53206545409 WEB BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 30.5, CRACKED. REMOVED AND REPLACED BEADED PRESSURE WEB SECTION PER SRM. 2L72 4F RTA16WE 20040706000372004070600037NM 2004 7 6 SWAA041831 120040629A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040706000432004070600043 2004 7 6 SWAA041838 420040630A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040706000562004070600056NM 2004 7 6 04FDEA01773 120040617A5321 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK RT STA 1821 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040706000592004070600059WP 2004 7 6 ROSA060704 120040607A335060030431 BATTERY PACK DOUG DC9 DC915F 3022037WP EMERGENCY LIGHT INOPERATIVE A ROSAO OTHER L NO TEST NRNOT REPORTED 1 SW01166DE 47152 CABIN EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK 60-0304-31 SN 4094, SENT TO SHOP FOR INSPECTION AND DEEP CYCLE. INSTALLED SAME, SYSTEM FUNCTION CHECKS SATISFACTORY. 2L72 4F A6WE 20040706000712004070600071NM 2004 7 6 SWAA041859 120040701A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE AT BS 380, STRINGER 15R, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040706000812004070600081NM 2004 7 6 04FDEA01790 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040706000902004070600090NM 2004 7 6 04FDEA01793 120040618A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 FRAME FOUND CHAFED MARK AT STA 535 LONGERON R19-24. 2L73 4F RTA22WE 20040706001012004070600101WP 2004 7 6 04FDEA01745 120040615A5744 BRACKET DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 LEFT OUTBOARD FLAP MOUNTED HINGE FAIRING ATTACH BRACKET CRACKED AT NUT PLATE. REMOVED AND REPLACED BRACKET AT LEFT O/B FLAP MOUNTED HINGE FAIRING IAW SRM 51-31-01. 2L73 4F A22WE 20040706001202004070600120 2004 7 6 DLM90040551 420040614A34402041270416 TRANSCEIVER DOUG MD90 MD9030 3023690NM WX RADAR INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27913DN 53393 RADAR RT FAIL. REPLACED WXR RADAR RT PER M/M. 2L72 4F RTA6WE 20040706001222004070600122NM 2004 7 6 DL757040553 120040614A5697 TERMINAL BOEING757 757232 1384965NM WINDOW HEAT LOOSE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27690DL 27585 BURNING ODOR NOTICED WHEN THROTTLES ADVANCED DURING CLIMB AND DESCENT. ODOR WAS NOTICED IN FLIGHT DECK ONLY. CHECKED BOTH EQUIP COOLING FANS. LT AND RT RECIRC FANS. FWD AND MID E/E FOR SIGNS OF HEAT OR SMOKE. NO PROBLEMS FOUND. REMOVED FWD GALLEY OVEN AND COFFEEMAKER AND CHECKED WIRING. NO SIGNS OF OVERHEAT. REMOVED OVERHEAD PANELS IN COCKPIT AND INSPECTED. ALL CHECKS GOOD. CHECKED ALL WINDOW HEAT CONNECTIONS, FOUND PILOT'S LOOSE. SECURED CONNECTOR. PERFORMED ENGINE RUN WITH PACKS ON. NO ODOR NOTICED. NO ODOR NOTICED DURING THROTTLE ADVANCEMENTS. A/C OK FOR SERVICE. 2L72 4F RTA2NM 20040706001252004070600125NM 2004 7 6 DL738040556 120040515A2782275040007 ACTUATOR BOEING737 737832 13844CFNM NR 5 SLAT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27384DA 30347 AFTER TAKEOFF UPON FLAP RETRACTION FROM FLAPS 1 TO UP L/E FLAPS TRANSIT LIGHT REMAINED ILLUMINATED WITH T/E FLAPS RETRACTED. PERFORMED LEADING EDGE FLAP TRANSIT CHECKLIST BUT NO CHANGE OCCURRED. T/E FLAPS OPERATED NORMALLY L/E DEVICES LOCKED OUT. REPLACED NR 5 SLAT ACTUATOR. 2L72 4F RTA16WE 20040706001262004070600126NM 2004 7 6 DL73S040557 120040615A53156546800508 FLOORBEAM BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 FUSELAGE CABIN FLOORBEAM AT STATION 520 FOUND WITH A CRACK AT THE UPPER CHORD. AREA REPAIRED IAW ERA 090614-14. 2L72 4F A16WE 20040706001302004070600130EU 2004 7 6 SOKF2341AA 120040610A28215UL0048 ELEMENT AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE FUEL FILTER CONTAMINATED W SOKFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23482TA 1482 V10964 DURING TAKEOFF RUN, ENGINE NR 2 DID NOT SPOOL UP BEFORE 80 KNOTS. AIRCRAFT RETURNED TO GATE. TECHS PERFORMED ANALYSIS IAW TSM AND AMM., REPLACED MAIN ELEMENT OF FUEL FILTER IAW AMM 73-1242, INSPECTED VSV MECHANISM IAW 73-32-42. CLEANED P 4.9, P2/T2 TUBES SYSTEM AIR IAW AMM 73-22-49. PERFORMED TEST NR 11 HIGH POWER ASSURANCE TEST IAW AMM. GROUND FUNCTIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT RETURNED TO NORMAL OPERATION. 2L72 4F4 FRTA28NM E40NE 20040707000032004070700003NM 2004 7 7 SWAA041887 120040703A53156519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 375, RBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040707000052004070700005EU 2004 7 7 MALA040439 120040605A3150 SOCKET SAAB SF340 340B 7860101EU INDICATOR LOOSE A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15370PX 340B300 WHEN L/P BLEED IS CLOSED RIGHT BLEED CLOSED LIGHT DOES NOT ILLUMINATE, THOUGH MASTER CAUTION LIGHT AND CWP A/C LIGHT DO ILLUMINATE. LAMPS CHECK GOOD ON RIGHT BLEED CLOSED LIGHT. MAINTENANCE FOUND LIGHT SOCKET (LAMPHOLDER) TO NOT BE FULLY SETTED IN SLOT. AFTER CYCLING POWER AND RESETTING LAMPHOLDER ON OVERHEAD PANEL, OPS CHECK GOOD OFF BLEED CLOSED LIGHT AT THIS TIME. PILOT RELAMPED BUT DID NOT FULLY SET HOLDER. 2L72 4T RTA52EU 20040707000072004070700007EU 2004 7 7 MALA040441 120040603A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4Y/2Y INSPECTION IN LCQ, FS 294 TO FS 319 RIGHT O/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/7/04. 2L72 4T RTA52EU 20040707000082004070700008EU 2004 7 7 MALA040442 120040604A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15407XJ 340B407 DURING 4K INSPECTION IN LCQ, FS 723 RT FUSELAGE HAS A DENT PWI 203077. CUT OUT DAMAGED AREA, ACCOMPLISHED HFEC, FABRICATED AND INSTALLED A DOUBLER REPAIR IAW MESABA EO S53229. 2L72 4T RTA52EU 20040707000122004070700012EU 2004 7 7 AWXA200400653 120040615A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 26 L/H BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOR THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040707000142004070700014NE 2004 7 7 MALA040443 220040608A7261 SEAL SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE LEAKING A MALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15457XJ 340B457 IN CRUISE FLIGHT LT ENGINE OIL PRESSURE FLUCTUATES AND CWP LIGHT ILLUMINATED. PRESSURE GAUGE FLUCTUATES +/- 10 PSI ALL OTHER PARAMETERS NORMAL. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE BB AXIS SEAL. 2L72 4T4 TRTA52EU E8NE 20040707000162004070700016EU 2004 7 7 MALA040445 120040530A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15366PX 340B267 BATTERY PACK P/N 61-0478-9, S/N ELB109 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 55-2198-1. UNIT PASSED CMM CHECK AND WAS RETURNED TO SERVICE 6/4/04. 2L72 4T RTA52EU 20040707000172004070700017EU 2004 7 7 MALA040446 120040420A33505502202251 RESISTOR BAC 146 AVRO146RJ85A1500097EU POWER SUPPLY BURNED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15533XJ E2367 EMERGENCY POWER SUPPLY INOP P/N 60-3550-1, S/N OFF 2703. REPLACED BURNT RESISTOR R6, P/N 55-022=225-1000F. UNIT TESTS GOOD IAW CMM. RETURNED TO SERVICE 6/4/04. 2H74 4F RTA49EU 20040707000182004070700018NM 2004 7 7 DL73S040560 120040615A5311654653122 FRAME BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 INNER FLANGE OF FRAME AT STATION 500 DENTED BETWEEN STRINGERS 24R AND 25R. AREA REPAIRED IAW 090636-14. 2L72 4F A16WE 20040707000222004070700022SO 2004 7 7 RAIA00405019 120040530A5270 WARNING LIGHT EMB 145 EMB145 3260210SO PAX DOOR ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03809HK 145187 PIT - MAIN DOOR OPEN MESSAGE ON TAKEOFF ROLL. MAINTENANCE PLACED DOOR INDICATING ON DEFERRAL PER MEL. 2L72 4F RTT00011AT 20040707000232004070700023SO 2004 7 7 RAIA00405020 120040530A5270 WARNING LIGHT EMB 145 EMB145 3260210SO SERVICE DOOR ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03801HK 145053 SERVICE DOOR WARNING ON TAKEOFF ROLL. MAINTENANCE DEFERRED DOOR WARNING PER MEL. 2L72 4F RTT00011AT 20040707000252004070700025SO 2004 7 7 RAIA00405022 120040531A3610 DUCT EMB 145 EMB145 3260210SO NR 1 ENGINE LOOSE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03809HK 145187 ERI - BLEED AIR LEAK INDICATION NR 1 ENGINE. MAINTENANCE RE-SECURED BLEED AIR DUCT. 2L72 4F RTT00011AT 20040707000262004070700026SO 2004 7 7 RAIA00406001 120040601A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03817HK 145058 STL - EMERGENCY LIGHT AT BACK CEILING INOP. MAINTENANCE RE-SECURED LOOSE BULB. 2L72 4T RTT00011AT 20040707000282004070700028CE 2004 7 7 DXTA200400323 120040614A32600327 BULB CESSNA750 750 2076810CE MLG INDICATOR BURNED OUT E DXTAA UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 GL07966QS 7500166 LEFT MAIN GEAR DOWN INDICATOR LIGHT DOES NOT ILLUMINATE WITH GEAR DOWN AND LOCKED. GEAR EMERGENCY EXTENSION KNOB PULLED AS PRECAUTION. FOUND GEAR INDICATION LIGHT BURNED, REPLACED LIGHT BULB, PERFORMED OPERATIONAL CHECK GOOD. RESET BLOW DOWN BOTTLE AND PNEUMATIC OVERRIDE VALVE, JACKED AIRCRAFT AND BLED HYDRAULIC GEAR SYSTEM, PERFORMED GEAR SWINGS ALL CHECKED GOOD. WORK DONE IAW CESSNA 750 CHAPTER 32-00-01 AND 32-60-00. 2L72 4J RTT00007WI 20040707000292004070700029SO 2004 7 7 RAIA00406002 120040601A5270 WARNING LIGHT EMB 145 EMB145LR 3260212SO CARGO DOOR ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03832HK 145771 ORD - BAGGAGE DOOR WARNING CAME ON AT 35,600 FT. MAINTENANCE PLACED DOOR WARNING SYSTEM ON DEFERRAL PER MEL. 2L72 4T RTT00011AT 20040707000312004070700031SO 2004 7 7 RAIA00406004 120040603A27403621001007 CONTROL UNIT EMB 145 EMB145LR 3260212SO PITCH TRIM INOPERATIVE A RAIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE03831HK9771 145232 PITCH TRIM MAIN AND BACK-UP FAILED. MAINTENANCE REMOVED AND REPLACED PITCH TRIM CONTROL UNIT. 2L72 4T RTT00011AT 20040707000352004070700035 2004 7 7 DLM88040561 420040615A3440066500080406 TRANSCEIVER DOUG MD88 MD88 3023688NM WX RADAR SYS DEFECTIVE A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO27947DL 12250 49878 AFTER TAKEOFF WEATHER RADAR FAILED. REPLACED RADAR INDICATOR, NO HELP. REPLACED RADAR TRANSCEIVER AND CLEANED COOLING FAN SCREEN. NOW TESTS GOOD. 2L72 4F RTA6WE 20040707000372004070700037NM 2004 7 7 DL73S040563 120040615A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27323DL 23095 A 2.5 INCH CRACK ON SKIN AT STA 870 BELOW STR 24R. REPAIRED PER SRM 53-30-3 FIG 48. 2L72 4F RTA16WE 20040707000392004070700039NM 2004 7 7 DLM90040565 120040616A2612 FIRE LOOP DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27911DA 53391 020026 PASSING 3000 FT RT ENGINE FIRE DETECTOR FAULT MESSAGE ILLUM IT STAYED ON FOR APPROX 1 MIN AND THEN WENT OUT. FIRE DET FAULT MESSAGE CAME ON WITH RT ENG B-LOOP LIGHT. LIGHT INTERMITTENT CAME ON AND OFF WITH WITH -B- LOOP. PERFORM FAULT TEST PER T/S MANUAL. NO FAULTS. SELECTED -A- LOOP AND PERFORM FIRE DETECTOR TEST. TEST GOOD. FWD THE RT ENGINE -B- LOOP TO MCO AND PLAC INOP PER MEL 26-11-01. 2L72 4F4 FRTA6WE E40NE 20040707000402004070700040NM 2004 7 7 DL73S040566 120040616A53206546877143 WEB BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 FUSELAGE SHEAR BEAM WEB CRACKED AT STRINGER 18A AND STA 727. AREA REPAIRED IAW ERA 090776-14. 2L72 4F A16WE 20040707000422004070700042NM 2004 7 7 DLM88040568 120040616A3260329001000 PSEU DOUG MD88 MD88 3023688NM MLG INTERMITTENT A DALAO OTHER N FALSE WARNING APAPPROACH 1 SO27997DL 53364 INTERMITTENT UNSAFE GEAR INDICATION (LEFT MAIN). REPLACED PSEU. 2L72 4F RTA6WE 20040707000432004070700043NM 2004 7 7 DLM88040569 120040616A2150321417611 REGULATOR DOUG MD88 MD88 3023688NM RT A/C PACK INOPERATIVE A DALAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO27903DE 53380 ON CLIMBOUT SAT RIGHT PACK FAILED. COOL OFF AND RESET, PROCEDURE DID NOT REGAIN PACK INITIALLY. PACK REGAINED APPROX 10 MINUTES LATER. ON CLIMBOUT SAT BOTH AUTO 1 AND AUTO 2 CONTROLLERS FAILED AFTER RT PACK FAILED. RAN BOTH ENGINES TO TAKEOFF POWER. FOUND RIGHT ENGINE AUG VALVE NOT WORKING CORRECTLY. REPLACED ANTICIPATOR. 2L72 4F RTA6WE 20040707000442004070700044NM 2004 7 7 DL73S040570 120040615A5551654759522 ATTACH FITTING BOEING737 737247 138448DNM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 HORIZONTAL STABILIZER FRONT AND REAR SPAR ATTACH LUGS CORRODED. AREA REPAIRED IAW ERA 090805-14AD. 2L72 4F A16WE 20040707000462004070700046NM 2004 7 7 UPS04242558 120040531A5420 FITTING BOEING727 72725C 138400HNM NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, AREA ABOVE NR 2 HORIZONTAL FIREWALL, UPPER LEFT FITTING AT STA 1470. 5 AND WL 300.15 IS CRACKED. FITTING REMOVED IAW SRM 51-30-02, NEW FITTING INSTALLED IAW SRM 51-30-02 AND BOEING DRAWING 65-17553. 2L73 4F A3WE 20040707000472004070700047NM 2004 7 7 UPS04242559 120040528A5512 PANEL BOEING727 72725C 138400HNM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, NR 5 LEFT BALANCE BAY PANEL HAS VERY LITE SURFACE CORROSION. UPON INVESTIGATION, CORROSION FOUND TO BE BEYOND LIMITS. BALANCE PANEL PLATE REPLACED IAW MM 27-30-27. 2L73 4F A3WE 20040707000482004070700048NM 2004 7 7 UPS04242564 120040522A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, FASTENERS POPPED AT S25R BETWEEN BS 290 & BS 300 SUSPECT CORROSION BETWEEN SKIN & STRINGER. REPAIR CARRIED OUT IAW SRM 51-20-01, 51-30-02, 51-10-1, 53-30-01, 51-20-04 & 51-80-01. 2L73 4F A3WE 20040707000492004070700049NM 2004 7 7 UPS04242565 120040528A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 CRACK IN SKIN AT FWD ENTRY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT IAW UPS EO B727-5330-1460 & SRM 51-30-02. 2L73 4F A3WE 20040707000502004070700050NM 2004 7 7 UPS04242566 120040602A5347 SEAT TRACK BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE:N/A ON INSPECTION SEAT TRACK SECTION FOUND CORRODED AT BS 730 AT RBBL 625 APPROX. NEW SEAT TRACK SECTION FABRICATED IAW SRM 51-20-1 AND ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW EO B727-5310-7477 STEP 28. 2L73 4F A3WE 20040707000522004070700052NM 2004 7 7 UPS04242570 120040529A5730 SKIN BOEING727 72725C 138400HNM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE:C SUSPECT CRACK IN SKIN AT LT WING ICE LIGHT CUTOUT (UPPER FWD). REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING 2004-054-004 & SRM 51-30-02 & 51-00-00. 2L73 4F A3WE 20040707000532004070700053NM 2004 7 7 UPS04542567 120040611A3350 LAMP BOEING757 75724APF 1384969NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01429UP 25460 HALF OF EMERGENCY LIGHT ARMED ANNUNCIATOR IS INOP. RELAMPED & REPLACED DRAWER ASSY PER MM 33-16-02-2. 2L72 4F RTA2NM 20040707000542004070700054NM 2004 7 7 DHL2004743005 120040616A783065378316 VALVE BOEING727 7272B7 138407LNM THRUST REVERSER LEAKING D DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01760AT 21954 NR 1 THRUST LEVER WOULD NOT COME OUT OF REVERSE THRUST AFTER LANDING. T/R LOCK OUT BOLT INSTALLED, O/B SIDE, PLUG & CAP ALSO INSTALLED. DEFER NR 1 T/R PER MEL REF 78-1, PLACARD INSTALLED. FOUND T/R DIRECTIONAL VALVE LEAKING. REMOVED AND REPLACED VALVE PER IPC 76-10-00-54, RAN ENG PER JRH 5.2, T/R OPS CHECKS NORMAL PER 6.6. THIS CLEARS DMI 16923. 2L73 4F A3WE 20040707000552004070700055NM 2004 7 7 UPS04242571 120040527A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, SKIN CORRODED AT BS 1263 S9R. CORROSION REMOVED IAW SRM 53-30-3 FIG 4. HFEC CARRIED OUT AROUND CUTOUT, NO DEFECTS FOUND. COMPLETED REPAIR IAW AAAE EO 2004-054-003. 2L73 4F A3WE 20040707000562004070700056NM 2004 7 7 UPS04242577 120040530A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, FASTENER HEAD POPPED & BULGE IN SKIN. SUSPECT CORROSION BETWEEN SKIN & STR AT BS 1065 S29L. SKIN CUTOUT BETWEEN BS 1061 AND BS 1072 AT S29L, CORROSION REMOVED IAW SRM 51-10-6. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR COMPLETED IAW AAAE EO 2004-054-001 AND UPS EO 727-53-20148. 2L73 4F A3WE 20040707000572004070700057NM 2004 7 7 UPS04242581 120040529A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, BULGING IN SKIN AT BS 1183 BETWEEN S6R AND S10R. CUT OUT INTERNAL BONDED DOUBLER BETWEEN S6R TO S10R BS 1183 TO BS 1177 REFERENCE SRM 53-30-3. HFEC CARRIED OUT, NO DEFECTS FOUND. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3. REPAIR DOUBLER AND FILLER INSTALLED WITH SEALANT IAW SRM 53-30-3 FIG 1 AND 5. 2L73 4F A3WE 20040707000582004070700058NM 2004 7 7 UPS04242590 120040531A5312 BULKHEAD BOEING727 72725C 138400HNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, SUSPECT CRACK IN NLG WHEEL WELL WALL AT LBL 24, BS 285 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2, 51-40-07 & MM 32-33-51. 2L73 4F A3WE 20040707000592004070700059EU 2004 7 7 218651 120040620A7500 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT BLEED SYS ILLUMINATED A UHLAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 GL17140CQ 140 APPROXIMATELY 1220 (UTC), FLT 7993 HPN-IAD, AIRCRAFT WAS EN ROUTE TO IAD WHEN THE RT BLEED LIGHT ILLUMINATED. CREW FOLLOWED QRH, LIGHT REMAINED ON. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. 2L72 4T4 TRTA52EU E8NE6 20040707000602004070700060NM 2004 7 7 AWXA200400643 120040516A5320654957323 ATTACH ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN RIGHT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE ON AFT OUTBOARD SIDE BS 665, RBL 64. MAINTENANCE REMOVED CRACKED RIGHT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-49573; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040707000612004070700061NM 2004 7 7 DHL2004760005 120040616A2612 FIRE DETECTOR BOEING727 7272B7 138407LNM CARGO BAY INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01760AT 21954 FWD FIRE DETECTOR WON'T ILLUMINATE. C/F TO DMI LOG IAW MEL 26-19 ASSIGNED 16934 PLACARD INSTALLED. CYCLED LOWER CARGO DETECTOR CIRCUIT BREAKERS IAW MM 26-16-01, SYSTEM OPS CKS NORMAL. TEST FUNCTIONS CHECK GOOD THIS CLEARS DMI 16934, PLACARD REMOVED. NO PARTS REPLACED. 2L73 4F A3WE 20040707000632004070700063NM 2004 7 7 UPS04542553 120040610A2120 INSULATION BOEING757 75724APF 1384969NM P-11 PANEL DETERIORATED A IPXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01424UP 25369 INSPECTION TYPE:N/A CREW NOTICED ELECTRICAL SMOKE ODOR DURING TAXI. DID BLOCK TURNBACK FOR FURTHER INSPECTION. CREW COULD NOT DETERMINE SOURCE. FOUND AIR DISTRIBUTION DUCT INSULATION DETERIOATED AND HAD FALLEN DOWN ACROSS WIRING AND C/BS IN THE UPPER PORTION OF HTE OVERHEAD P-11 PANEL. REMOVED DETEROIATED INSULATION AND CLEANED P-11 PANEL. NO OTHER FAULTS FOUND. EO 757-5310-20596-A ISSUED FOR REMOVAL OF INSULATION. 2L72 4F RTA2NM 20040707000652004070700065 2004 7 7 213483 420040701A3400 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE AVIONICS TRIPPED A UHLAB EMER. DESCENT GS MULTIPLE FAILURE AFFECT SYSTEMS CRCRUISE 1 GL17150CN 150 FLIGHT 4574 LEX-PIT. DURING CRUISE CLOSE TO APPROACH INTO PIT THE RIGHT AVIONICS CIRCUIT BREAKER AHC-2 POPPED CAUSING THE FIRST OFFICER'S AVIONICS SYSTEM TO COMPLETELY BLANK OUT. THE CAPTAIN'S BOTTOM EFIS SCREEN WAS STARTING TO ALSO FADE. THE CREW ASKED ATC FOR PRIORITY INTO PIT. ATC DECLARED AN EMERGENCY FOR THE LANDING. THE A/C LANDED SAFELY AND WAS TAKEN OUT OF SERVICE IN PIT AT 2230 (LT). 2L72 4T4 TRTA52EU E8NE6 20040707000682004070700068NE 2004 7 7 RAIA00405023 220040506A753232149582 BLEED VALVE AEROSPATR72 ATR72202 8680940EU PWA PW120 PW124B NE NR 1 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03723TE19838 283 STL - NR 1 BLEED LEAK INDICATION. MAINTENANCE DEFERRED BLEED PER MEL. SUBSEQUENTLY CLEARED DMI REMOVING AND REPLACING NR 1 HP BLEED VALVE. 2H72 4T4 TRTA53EU E2ONE 20040707000702004070700070EU 2004 7 7 RAIA00405025 120040512A3260AIR135690 DOWNLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG INOPERATIVE A RAIAO OTHER J WARNING INDICATION DEDESCENT 1 CE03561HK 41077 UPON DESCENT INTO SLT RT STAND BY GEAR INDICATION INOP. MAINTENANCE REMOVED AND REPLACED RT MLG DOWNLOCK SWITCH. 2L72 4T RTA41NM 20040707000712004070700071EU 2004 7 7 RAIA00405026 120040513A3260 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG CONTAMINATED A RAIAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 CE03558HK 41071 CHO - LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AND CLEANED MLG UPLOCK SWITCHES AND CPS, OPS OK. 2L72 4T RTA41NM 20040707000722004070700072EU 2004 7 7 RAIA00405029 120040514A261251228532 FIRE LOOP JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE SHORTED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03560HK 41076 SSGT - RIGHT ENGINE FIRE WARNING. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE ZONE 1 FIRE LOOP. 2L72 4T RTA41NM 20040707000752004070700075EU 2004 7 7 RAIA00405032 120040523A32401SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU PARKING BRAKE DEFECTIVE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03551HK 41040 MEM - TOCWS WARNING ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE SWITCH. 2L72 4T RTA41NM 20040707000772004070700077NM 2004 7 7 AWXA200400632 120040611A3397BR964411 WIRE BOEING737 73733A 1384673NM SEAT ROW 21 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 DEN - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040707000812004070700081NM 2004 7 7 AWXA200400636 120040613A33501001841 SOCKET BOEING737 737277 1384570NM SEAT ROW 10 LT SHORTED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP28182AW 22649 PHX - EMERGENCY LANDING - FLT 0628 - ON DESCENT INTO PHX EN ROUTE FROM OAK AT FL 120 EXPERIENCED AN ELECTRICAL BURNING ODOR FOLLOWED BY SMOKE IN COCKPIT, DONNED O2 MASKS AND DECLARED AN EMERGENCY. AT FL 030 FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN COMING FROM OVERHEAD BIN NEAR LT OVERWING EXIT, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE VISUALLY INSPECTED INSTRUMENT AND CIRCUIT BREAKER PANELS IN COCKPIT FOR EVIDENCE OF FIRE, NO DAMAGE NOTED. FOUND A BURNT SOCKET, LENS COVER, AND ELECTRICAL BRACKET ON PASSENGER SERVICE UNIT PANEL ABOVE SEATS AT ROW 10 LT. REPLACED ALL THREE DEFECTIVE PARTS IAW BMM 33-021-051-2, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040707000842004070700084NM 2004 7 7 AWXA200400639 120040525A5320654587545 SILL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND IN INNER STRUCTURE ON R-1 DOOR SILL AT BS 294.5 AND BS 328, RBL 58. MAINTENANCE REMOVED CORRODED INNER STRUCTURE ON R-1 DOOR SILL FROM BS 294.5 TO BS 328, RBL 58; FABRICATED A NEW REPLACEMENT INNER STRUCTURE PER DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040707000852004070700085NM 2004 7 7 AWXA200400640 120040603A33971703661 WIRE BOEING737 7373G7 1384595NM EMERGENCY LIGHT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW1 1 24009 MCN - EEL - DURING C-15 CHECK FOUND NUMEROUS DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS BETWEEN BS 360 AND BS 927. MAINTENANCE REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES ON SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT HARNESS IAW SWPM 20-42-01, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040707000862004070700086NM 2004 7 7 AWXA200400641 120040603A5311654580764 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN FRAME AT BS 294.5, STR 17 RT. MAINTENANCE TRIMMED OUT CRACK IN FRAME AT BS 294.5, STR 17 RT; FABRICATED A FILLER, ANGLE, SHIM, WASHER, AND GUSSET; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-04163-RC1. 2L72 4F RTA16WE 20040707000912004070700091EU 2004 7 7 RAIA00405034 120040527A30204D209222 VALVE JETAIRJETSTMJETSTM4101 1500501EU DE ICE SYSTEM DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03569HK15966 41088 STL - AIRFRAME DEICE LOW PRESSURE INDICATION. MAINTENANCE DEFERRED AIRFRAME DEICE PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING DEICE PRESSURE REGULATOR VALVE. 2L72 4T RTA41NM 20040707000942004070700094SO 2004 7 7 RAIA00406007 120040602A3030 HEATER EMB 145 EMB145 3260210SO PITOT TUBE DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03820HK12904 152458 145064 DEN - PITOT ONE HEAT INOP INDICATION. MAINTENANCE DEFERRED NR 1 PITOT HEAT PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE NR 1 PITOT TUBE. 2L72 4F RTT00011AT 20040707000962004070700096EU 2004 7 7 MALA040434 120040601A3350743301 LIGHT SAAB SF340 340B 7860101EU ROW 4C INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15404XJ 340B404 ONE FLOOR TRACK LT LAMP AT 4C INOP. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP AT 9A P/N-7433-1, OPS CHECKS GOOD. 2L72 4T RTA52EU 20040708000012004070800001WP 2004 7 8 2004000005 120040531A1420 CONNECTOR DOUG DC10 DC1030 3023501WP BRAKE SENSOR DAMAGED A CNMAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LDLANDING 1 SW0749082 47927 DURING LANDING ROLLOUT, F/A NOTED SMOKE BRIEFLY EMITTING FROM VENTILATION SYSTEM OVERHEAD ROW 4 - 7 ON RT. F/E NOTED A HIGH BRAKE TEMP ON NR 5 WHEEL. PASSENGERS WERE CONCURRENTLY RELOCATED TO ZONES B & C. THE APPARENT SMOKE WAS LATER DISCRIBED AS FOGGY HAZE WHICH QUICKLY DISSIPATED. POST FLIGHT, MECHANICS FOUND NR 5 BRAKE TEMPERATURE SENSOR INDICATING ERRONEOUSLY HIGH DUE TO BENT PINS / SHORT CIRCUIT IN AN ELECTRICAL CONNECTOR WITH NO EVIDENCE OF OVERHEATING OR MALFUNCTION OF THE BRAKE SYSTEM. THE PRESUMPTIVE CAUSE OF THE SMOKE WAS CONDENSATION OF WATER VAPOR. 2L73 4F A22WE 20040708000022004070800002EU 2004 7 8 CX7A194J0433 120040611A26131734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE LOOSE A CX7AEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03304CE 340B198 TAILPIPE HOY CWP LIGHT ILLUMINATED, SHUT DOWN RIGHT ENGINE. 2L72 4T RTA52EU 20040708000032004070800003NE 2004 7 8 HAEA00147 220040615A72614003T54P01 PUMP AMD FALC20FALCONE 2720305EU GE CF700 CF7002D2 30010NE LT ENGINE FAILED E HAEAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SW05285TW15760 285 304412 ON DESCENT INTO CHS, AIRCRAFT LOST OIL PRESSURE IN NR 1 ENGINE. CREW INITIATED ENGINE SHUTDOWN PROCEDURES. DECLARED EMERGENCY, LANDED AT CHS UNEVENTFUL. 2L72 4F4 F A7EU E7EA 20040708000042004070800004WP 2004 7 8 NACA20040024 120040615A542079095 STUD DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE XMTER BRACKET BROKEN A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL0399330 43576 31613 NR 1 ENGINE FEATHERED DUE TO OIL LOSS. FOUND BROKEN STUD AT FUEL FLOW TRANSMITTER BRACKET. REPLACED STUD, LEAK CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20040708000072004070800007EU 2004 7 8 CX7A194J0435 120040616A26131734362450 DETECTOR SAAB SF340 340B 7860101EU RT TAILPIPE LOOSE A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03318CE 340B358 RIGHT TAILPIPE HOT LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. 2L72 4T RTA52EU 20040708000082004070800008NE 2004 7 8 2004000007 220040613A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 1 FAILED A CNMAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW0759083 47926 ON T/O ROLL, NR 1 ENGINE MADE LOUD BANG, ENGINE FAIL LIGHT ILLUMINATED AND EGT PEGGED. N1 WAS 130 PERCENT AND SPEED WAS 125 KIAS. T/O ABORTED. TOWER NOTED FIRE FROM INTAKE. 2L73 4F4 F A22WE E23EA 20040708000092004070800009NE 2004 7 8 00140 220040514A7200 ENGINE LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW05147TW8221 8221 023 251385A PILOT REPORTED LT ENGINE FLAMED OUT AT FL430 IN SEVERE TURBULANCE ON TRIP FROM HKS TO LRD. ENGINE RELET NORMALLY AT FL 250. CONTINUED TRIP TO LRD. MAINTENANCE PERFORMED INSPECTION IN ACCORDANCE WITH GE M/M 77-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4J4 J A10CE 1E16 20040708000122004070800012CE 2004 7 8 HAEA0019 120040616A3230 SAFETY SWITCH LEAR 24 24D 5170311CE MLG FAULTY E HAEAO OTHER J WARNING INDICATION DEDESCENT 1 SW05299TW1175611756 299 ON DESCENT, LANDING GEAR WOULD NOT EXTEND, 2 REDS. PERFORMED MANUAL EXTENSION. LANDING UNEVENTFUL. 2L72 4J A10CE 20040708000132004070800013EU 2004 7 8 00143 120040602A3260A23870101 SQUAT SWITCH AMD FALCONFALCON20 2730103EU LT MLG FAILED E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05295TW5000 5000 005 AIRCRAFT DEPARTED STL, ON CLIMBOUT GEAR RETRACTED BUT RED DOOR LIGHTS STAYED ON. WHEN GEAR DOWN, DOOR LIGHTS EXTINGUISH. AIRCRAFT RETURNED STL. LANDING UNEVENTFUL. 2L72 4F RTA7EU 20040708000182004070800018NM 2004 7 8 AWXA200400654 120040616A335032145410 BATTERY PACK AIRBUSA319 A319132 3930340NM ZONE 241 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28805AW18244 1049 PHX - EEL - DURING 4-DAY CHECK THE LT OVERWING EMERGENCY BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL) FAILS PUSH BUTTON TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040708000202004070800020EU 2004 7 8 AWXA200400656 120040602A5753D57571005007A WEDGE AIRBUS320 A320231 3930325EU RT WING TE FLAPSDEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - C-04 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF RT OUTBOARD FLAP AT OUTBOARD END OF NR 3 SPOILER. MAINTENANCE CUT OUT DISBONDED AREA OF LOWER SURFACE OF RT OUTBOARD FLAP; FABRICATED A CORE FILLER AND REPAIR DOUBLER; BONDED REPAIR TO FLAP IAW A320 SRM 57-53-00 FIG 211 PG 247-257. 2L72 4F RTA28NM 20040708000222004070800022NM 2004 7 8 AWXA200400658 120040606A575465C26603 SKIN BOEING737 7373S3 1384711NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 LCQ - MAJOR REPAIR - DURING C-17 CHECK SEVERAL CRACKS WERE FOUND AT RIVET HOLES ON NR 4 LEADING EDGE SLAT FROM SS 28 RT TO SS 84 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF NR 4 SLAT SKIN FROM SS 28 RT TO SS 84 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206 SHEETS 3 & 4. 2L72 4F RTA16WE 20040708000242004070800024SO 2004 7 8 RAIA00406009 120040611A315080069424 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03814HK8702 145046 STL - TAKEOFF CONFIG GAVE TRIM WARNING WITH TRIM IN THE GREEN. MAINTENANCE REMOVED AND REPLACED AURAL WARNING UNIT. 2L72 4T RTT00011AT 20040708000252004070800025NM 2004 7 8 DL73S040530 120040608A5330654577644 SKIN BOEING737 737232 1384475NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334DL 23105 FUSELAGE SKIN WAS FOUND CORRODED AROUND THE AFT LAV SERVICE PANEL NEAR STA 986 AND STR 27R. AREA REPAIRIED IAW ERA 091035-14. 2L72 4F RTA16WE 20040708000272004070800027NM 2004 7 8 DL767040532 120040610A5551182T13101 FITTING BOEING767 767232 1385132NM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27112DL 22224 LEFT HORIZONTAL STAB CENTER SECTION PIVOT FITTING WAS FOUND WITH A ROTATED BUSHING RETAINER AND SUBSEQUENTLY CORROSION IN THE BORE. REPAIRED PER ERA 090340-14. 2L72 4F RTA1NM 20040708000282004070800028 2004 7 8 DL75K040533 420040611A2330 DISPLAY BOEING757 757232 1384965NM SEAT 23B DEACTIVATED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO276715C 30486 DURING TAXI OUT, F/A REPORTED AN ACRID ODOR COMING FROM TV IN SEAT 23B. TV WAS SHUT OFF, STILL SMELLED. RETURNED TO GATE. TESTED IFE SYSTEM, UNABLE TO DUPLICATE. 2L72 4F RTA2NM 20040708000302004070800030NM 2004 7 8 DL73S040535 120040609A533065458001141 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRIBE MARK DAMAGE WAS FOUND DUE TO METAL PAINT SCRAPER USE ON THE LOWER SKIN AT THE STRINGER 14L LAP SPLICE, LOCATED BETWEEN FUSELAGE STA 259 AND 312. REPAIRED PER ERA 089672-14. 2L72 4F A16WE 20040708000322004070800032WP 2004 7 8 DHL2004807008 120040612A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH 45990 THE D-PIT DOOR CUTOUT LWR FWD CORNER 8 INCHES LONG X 2.5 INCHES WIDE X .50 INCH DENT ON EDGE OF DOOR. REPAIRED DENT IAW SRM 51-1-9, TREATED & PRIMED IAW SRM 51-1-8. 2L74 4F RT4A25 20040708000332004070800033NE 2004 7 8 DHL2004801006 220040612A72613050125090 LINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 500 LEAKING A DHLAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01801DH 46033 IN FLIGHT NR 2 ENGINE OIL QUANTITY INDICATED LESS THAN 2 QUARTS, PERFORMED OIL QUANTITY LOW ABNORMAL PROCEDURE AND INFLT ENGINE SHUTDOWN ABNORMAL PROCEDURE, WIND MILLING STARTED AT 0818 ZULU OIL PRESSURE 3 PSI OIL PRESSURE WAS 20 PSI WHEN ENGINE WAS SHUTDOWN. FOUND OIL LEAKING AT STARTER. FOUND STARTER SHAFT SHEARED. REMOVED AND REPLACED STARTER AND STARTER SHUTOFF VALVE IAW 80-10-1 AND 80-10-3. PERFORMED IDLE ENG RUN ON NR 2 ENG PER JRH. STARTER AND STARTER SHUTOFF OPS AND LEAKS CHECKS GOOD. FOUND OIL LEAKING AT B-NUT, AT ACCESSORY GEARBOX LINE CRACK. REMOVED AND REPLACED LINE IAW 20-13-0, PERFORMED ENG RUN NR 2 ENG IAW JRH, OPS AND LEAKS CHECKS GOOD. LINE P/N 305-012-509-0. 2L74 4F4 FRT4A25 E2GL 20040708000362004070800036 2004 7 8 00144 420040601A3414B070410046 LIMITER AMD FALCONFALCON20 2730103EU AIRSPEED IND FAILED E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05977TW5000 5000 013 ON TAKEOFF FROM ADS, CO-PILOTS AIRSPEED INDICATOR FAILED TO INDICATE. CREW RETURNED TO ADS, AIRCRAFT INPUT FOR MAINTENANCE. 2L72 4F RTA7EU 20040708000372004070800037NM 2004 7 8 DHL2004764005 120040611A2611 SMOKE DETECTOR BOEING727 727264 138408MNM CARGO BAY WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01764AT 22984 CARGO FIRE DETECTOR WILL NOT TEST. FOUND FAULT LIGHT ON RESET SYSTEM CB'S, SYSTEM CHECKS NORMAL REF MM 26-11-0. NO COMPONENTS REPLACED. 2L73 4F A3WE 20040708000382004070800038NM 2004 7 8 DL73S040537 120040609A5330654577872 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 FUSELAGE SKIN FS 908 - FS 1016 S4R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE AT S4R BETWEEN FS 908 AND FS 1016. REPAIR DOUBLERS INSTALLED ER/A 090115-14, REV A. 2L72 4F A16WE 20040708000392004070800039NM 2004 7 8 DL73S040538 120040609A533065458001205 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 FUSELAGE SKIN FS 259-360 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW THE LAP SPLICE ALONG S19R BETWEEN FS 259 AND FS 360. REPAIR DOUBLERS INSTALLED ER/A 089739-14, REVISION INITIAL. 2L72 4F A16WE 20040708000452004070800045NM 2004 7 8 AWXA200400644 120040614A2560P2070001214 FLASHLIGHT BOEING737 7373G7 1384595NM ZONE 900 - LAVATINOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 PHX - EEL - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT RED INDICATOR WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040708000462004070800046NM 2004 7 8 AWXA200400645 120040518A5313BAC1498157 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 495D, AFT OF LT WING INSPECTION LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGE IN STRINGER 16 LT AT BS 495D; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, A FILLER AND DOUBLER; INSTALLED SPLICE REPAIR IAW B737-300 SRM 53-00-03 FIG 201. 2L72 4F RTA16WE 20040708000472004070800047NM 2004 7 8 AWXA200400646 120040519A53206517683125 CREASE BEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-1 DOOR CREASE BEAM AT TOP OF FLOOR STRUCTURE AROUND FASTENER HOLES FROM BS 300 TO BS 344. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 300 TO BS 344; FABRICATED A NEW REPLACEMENT CREASE BEAM PER DWG 65-17683; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4-B. 2L72 4F RTA16WE 20040701000172004070100017NM 2004 7 1 DHL2004782007 120040609A3230 LANDING GEAR BOEING727 727227 1384078NM MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01782DH 21998 LANDING GEAR HANDLE WOULD NOT GO PAST OFF DURING GEAR RETRACTION. ABNORMAL PROCEDURE COMPLETED, AND THE GEAR RETRACTED NORMALLY. TESTED LANDING GEAR HANDLE IN GROUND AND FLIGHT MODE, OPS CHECKED NORMAL IAW 32-31-0. 2L73 4F A3WE 20040701000252004070100025WP 2004 7 1 MWEA040090 120040608A534039364031 ATTACH FITTING DOUG DC9 DC981 3022081WP RT MLG WW CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 RIGHT MAIN LANDING GEAR DOOR ACTUATOR BULKHEAD ATTACH FITTING IS CRACKED. REMOVED AND REPLACED SUPPORT. 2L72 4F A6WE 20040701000312004070100031NM 2004 7 1 QXEA200400401 120040531A3250481505 MANIFOLD BOMBDRDHC8 DHC8401 1390041NM ZONE 700 INOPERATIVE A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09414QX5088 4061 PDX - ON FLIGHT NUMBER 2354, NOSE WHEEL STEERING CAUTION CAME ON 8 SECONDS AFTER NOSE WHEEL STEERING SELECTED ON. CONDUCTED ABNORMAL CHECKLIST PROCEDURES AND CAUTION RE-ILLUMINATED. INTERROGATED SCU CODES. CLEANED SCU AND FOUND SQVC TO BE HARD FAULTED. REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040701000322004070100032EA 2004 7 1 QXEA200400403 120040603A2611 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 200 ILLUMINATED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09603QX 10011 EUG - ON FLIGHT NUMBER 2545, AFT CARGO SMOKE DETECTOR CAUTION MESSAGE. C/W CRJ 700 FIM TASK 26-15-01-810-801-A01. NO CAUTION MESSAGES DISPLAYED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040701000392004070100039NM 2004 7 1 N150AW0007 120040525A5320 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 CRACK AT CUTOUT IN WEB, 4 INCHES FOWRARD OF L-2 DOOR AT STR 11 LT. REPAIRED PER SRM 51-70-13. 2L72 4F RTA16WE 20040701000412004070100041NM 2004 7 1 N150AW0014 120040525A5312 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 HFEC REVEALED A CRACK INDICATION AT FASTENER AT RBBL 10.5 AND WL 234 ON THE BS 178 BULKHEAD. REPAIRED AREA PER SRM 53-10-8. 2L72 4F RTA16WE 20040701000472004070100047NM 2004 7 1 AWXA200400624 120040526A5320146N5318 SHEAR PLATE BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT SHEAR DECK AT BS 1681 FROM BL 0 TO LBL 48. MAINTENANCE CUTOUT DAMAGE ON AFT SHEAR DECK AT BS 1681 FROM BL 0 TO LBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208. 2L72 4F RTA2NM 20040701000482004070100048EU 2004 7 1 AWXA200400625 120040604A5321D53670049000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK FOUND THE AFT GALLEY FLOOR PANEL 261EF DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 261EF FROM FR 66 TO FR 68, Y1292 LT TO Y1732 LT. FABRICATED AND INSTALLED NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670049. 2L72 4F RTA28NM 20040701000522004070100052NM 2004 7 1 AWXA200400629 120040531A5320146N52407 ANGLE BOEING757 7572S7 1384962NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, LBL 48. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, LBL 48; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5240-7. 2L72 4F RTA2NM 20040701000572004070100057WP 2004 7 1 UPS04842538 120040508A53403750545501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:C-2, AFT PIT LOWER BILGE BETWEEN STA 1040-1080 L35L HAS CORROSION INSIDE CHANNEL. REMOVED CORROSION FOUND TO BE WITHIN LIMITS. REMOVED LONGERON SPLICE CLIP AND INTERCOSTAL STA 1040-1060. LONGERON SPLICE FOUND TO BE CRACKED, REC'D LOCATED AND DRILLED NEW SPLICE. ALODINED AND PRIMED. INSTALLED NEW SPLICE FITTING AND REINSTALLED INTERCOSTAL AND CLIP STA 1040-1060 IAW DC8 SRM 51-3-0 AND 51-1-20D. 2L74 4F RT4A25 20040701000772004070100077NM 2004 7 1 SWAA041801 120040627A53156545833149 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29514SW 25153 DURING OTS, FOUND FLOORBEAM AT BS 270, LBL 4, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040701000822004070100082 2004 7 1 SWAA041806 420040628A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040701000912004070100091CE 2004 7 1 DXTA200400320 120040605A2730 INDICATOR CESSNA500 560CESSNA 2076750CE TRIM MALFUNCTIONED E DXTAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL07390QS 5600490 DURING TAKEOFF ROLL PILOT EXPERIENCED EXCESSIVE BACK PRESSURE ON THE CONTROL COLUMN, TOOK APPROX 60 LBS OF FORCE TO NEUTRALIZE CONTROL COLUMN, TRIM INDICATOR WAS IN T/O RANGE, TAKEOFF ABORTED. INSPECTED ELEVATOR AND ELEVATOR TRIM SYSTEM, FOUND ELEVATOR TRIM WHEEL INDICATOR AT TAKEOFF POSITION BUT ELEVATOR TRIM AT FULL NOSE-UP POSITION. RE-INSTALLED TRIM INDICATOR AND WHEEL TO ONE CORRECT READINGS. CHECK ELEVATOR AND TRIM UP / DOWN DEGREES OF TRAVEL, NO DEFECTS NOTED, TRIM WHEEL OP'S CHECK GOOD. WORK PERFORMED IAW CESSNA CE-560 MAINTENANCE MANUAL CHAPTER 27-31-05. 2L72 4F RTA22CE 20040706000012004070600001NM 2004 7 6 04FDEA01752 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040706000052004070600005NM 2004 7 6 04FDEA01756 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.328 AND REPAIRED AS PER FEDEX EA 1-5750- 76775, TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP - PIVOT BORE - REPAIR. 2L73 4F RTA22WE 20040706000102004070600010NM 2004 7 6 04FDEA01712 120040614A5744ARC0502 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.224 INCH. COMPLIED WITH FEDEX EA 1-5740-76742, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040706000152004070600015NM 2004 7 6 04FDEA01748 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED. 2L73 4F RTA22WE 20040706000162004070600016NM 2004 7 6 04FDEA01749 120040616A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040706000452004070600045NM 2004 7 6 SWAA041839 120040630A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED RT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040706000552004070600055NM 2004 7 6 SWAA041849 120040630A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29466WN 30677 DURING SCHEDULED MV1 CHECK, FOUND AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040706000652004070600065NM 2004 7 6 04FDEA01701 120040612A5320 INTERCOSTAL BOEING727 727200 138407ENM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25244FE 21647 AFT LWR CARGO COMPT INTERCOSTAL INBOARD OF STR 26L, BETWEEN FS 1140 TO 1166, UPPER AND LWR FLANGES CORRODED. INSTALLED FABRICATED FLANGES OF INTERCOSTAL IAW SRM 51-30-2. INSTALLED FABRICATED DOUBLER AT STA 1140 -1166, STR 26L IAW SRM 51-30-2. 2L73 4F RTA3WE 20040706000692004070600069NM 2004 7 6 SWAA041857 120040701A33506114781 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS AT RT AND LT OVERWING EXITS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F A16WE 20040706000732004070600073NM 2004 7 6 04FDEA01782 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.225 AND REPAIRED AS PER FEDEX EA 1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR. 2L73 4F RTA22WE 20040706000782004070600078NM 2004 7 6 04FDEA01787 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78010, OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040706000792004070600079NM 2004 7 6 04FDEA01788 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER =1.187, FINAL DIAMETER=1.221 AND REPAIRED AS PER FEDEX EA 1-5750-78010, OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040706000832004070600083WP 2004 7 6 04FDEA01694 120040611A2612355194310 FIRE LOOP DOUG DC10 DC1030 3023501WP NR 2 PYLON DAMAGED A FDEAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 SO25302FE 46801 NR 2 MANIFOLD FAIL LIGHT ILLUMINATED DURING CLIMB, CHECKLIST COMPLETE, LIGHT WENT OUT. DUMPED FUEL AND RETURNED TO MEM. LANDED UNEVENTFULLY. *S/D* PERFORMED DECAY CHECK OF NR 2 SYSTEM REF DC10-30 JRH. DECAY TEST FAILED FOUND THE CENTER CARGO JET PUMP SHUTOFF VALVE STUCK IN THE OPEN. REMOVED AND REPLACED THE CARGO JET PUMP SHUTOFF VALVE REF DC-10MM 21-41-03-2. FOUND LOOPS IN NR 2 PYLON BAD. REMOVED AND REPLACED LOOPS D1-29, D1-28B, D1-28CREF: DC-10-30 MM 36-23-02-4. PERFORMED MANIFOLD FAILURE SYSTEM TEST PER DC10-30 MM 36-23-00-2, WITH NO DEFECTS NOTED. OPS AND LEAK CHECK OF CARGO JET PUMP SHUTOFF VALVE PER DC-10-30 MM 21-41-03-2, CHECKS GOOD. PRESS DECAY CHECK PER THE JRH CHECKS GOOD. RETURNED TO SE2L73 4F A22WE 20040706000952004070600095 2004 7 6 SWAA041852 420040701A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DEPLOYED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29791SW 27886 L1 DOOR EVAC SLIDE DEPLOYED AT GATE. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040706000982004070600098NM 2004 7 6 SWAA041864 120040701A53106546529 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, STRINGER 27L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040706001082004070600108WP 2004 7 6 04FDEA01781 120040121A5512ALC72051 SKIN DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 DURING ACCOMPLISHMENT -F- TO -ACF- AT OAN, INSPECTION FOUND CRACKS IN 2 LWR CONSTANT SECTION SKINS OF THE HORIZONTAL STAB. THE CRACKS WHERE WITHIN FLYLABLE LIMITS. HOWEVER, DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PLANKS AND CONTINUE INSPECTION OF THE SKINS PER EO 8-5510-7-2307 PART 1 AT 24 MONTH INTERVALS. THE WORK IS BEING ACCOMPLISHED PER SB 55-16 FOR GROUP 1 A/C. 2L73 4F A22WE 20040706001092004070600109EU 2004 7 6 04FDEA01720 120040614A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25652FE 735 INSIDE COURIER AREA 2ND SEAT TRACK ON RIGHT SIDE AT FRAME 18 HAS CORROSION ON IT. REMOVED AND REPLACED SEAT TRACK AT COURIER AREA 2ND SEAT TRACK RIGHT SIDE AT FRAME 18 IAW A300 SRM 51-40-21. 2L72 4F RTA35EU 20040707000012004070700001WP 2004 7 7 DBCA122D3 220040514A7200 ENGINE CESSNA650 650 2076802CE GARRTTTPE731TFE7313C WP NR 1 FOD E DBCAA UNSCHED LANDING CJ F.O.D. WARNING INDICATION CLCLIMB 1 GL13260VP 6500190 87506 AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGRADE WITH OVERTEMP LIGHT. FLIGHT CREW SECURED NR 1 ENGINE AND RETURNED TO OMA. LANDING WAS UNEVENTFUL. INITIAL VISUAL INSPECTION SHOWED NO SIGN OF FOD DAMAGE TO COMPRESSOR OR HIGH PRESSURE TURBINE. ENGINE REMOVED BY MFG, SPI FOR TEARDOWN AND INSPECTION. FOLLOW-UP WILL BE SUBMITTED WHEN CAUSE OF SHUT-DOWN IS DETERMINED TO INCLUDE PN AND TIME/CYCLES ON FAILED PART. 2L72 4F4 F A9NM E6WE 20040707000132004070700013CE 2004 7 7 62060 120040607A27511293800021 INDICATOR BEECH 1900 1900D 1154162CE TE FLAPS MALFUNCTIONED A AMWAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE07133YV UE133 UPON APPROACH, FLAP POSITION INDICATOR WOULD NOT INDICATE BEYOND 10 DEGREES DOWN. PILOT ACCOMPLISHED TOWER FLYBY FOR FLAP POSITION VERIFICATION. AIRCRAFT LANDED WITH FLAPS DOWN FULL WITH NO FURTHER INCIDENT. REMOVED AND REPLACED FLAP INDICATOR, OPS CHECK NORMAL. P/N 129-380002-1, S/N 542. 2L72 4T RTA24CE 20040707000242004070700024EU 2004 7 7 RAIA00405021 120040531A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU DISCONNECTED A RAIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE03560HK 41076 STL - LANDING GEAR HANDLE WILL NOT GO TO THE UP POSITION. MAINTENANCE FOUND CONNECTOR 1MUFP BACK-SHELL DISCONNECTED. CLEANED WIRES AND RE-CONNECTED BACK-SHELL. 2L72 4T RTA41NM 20040707000382004070700038NM 2004 7 7 DL73S040564 120040615A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 FUSELAGE SKIN AND STRINGER CRACKED AT STA 525 AND STR 16L. ERA 091121-14 COMPLIED WITH FOR REPAIR. 2L72 4F A16WE 20040707000412004070700041NM 2004 7 7 DL73S040567 120040616A3350333101582 BATTERY PACK BOEING737 737232 1384475NM EMERGENCY LIGHT MALFUNCTIONED A DALAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO27320DL 23092 CABIN EMERGENCY LIGHTS REMAIN ILLUMINATED IN DIM MODE. REPLACED BATTERY PACK IN AFT OVERHEAD. 2L72 4F RTA16WE 20040707000452004070700045 2004 7 7 UPS04142572 420040611A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01134UP 0818 EVAC SLIDE WARNING LIGHT INOP. DEFERRED PER MEL 52-73-01-4, REF M282572. RELAMPED EVAC SLIDE WARNING LIGHT, OPS CHECKED GOOD PER MM. THIS CLEARS ITEM M282572. REFERENCE LP 166569. 2L72 4F RTA35EU 20040707000662004070700066EU 2004 7 7 120631 120040702A2910 WARNING LIGHT SAAB SF340 SF340A 7850100EU HYD SYSTEM ILLUMINATED A UHLAO OTHER J WARNING INDICATION DEDESCENT 1 GL1743SZ 340A043 FLIGHT 7982 FROM TYS TO IAD, ON FINAL WITH GEAR UP HYD LIGHT ILLUMINATED ON CWP. AIRCRAFT HAD LOW MAIN AND EMERGENCY INDICATIONS. AIRCREW FOLLOWED QRH. WHEN GEAR WAS SELECTED DOWN ONLY NOSE GEAR CAME DOWN. WHILE DOING A GO-AROUND THE RIGHT GEAR CAME DOWN. PULLED T-HANDLE FOR LT GEAR. AIRCRAFT LANDED SAFELY. 2L72 4T RTA52EU 20040707000692004070700069SO 2004 7 7 RAIA00405024 120040512A33977287501658 WIRE HARNESS EMB 145 EMB145ER 3260211SO OVERHEAD PANEL BURNED A RAIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE03827HK 145021 ATL - ELECTRIC SMOKE COMING FROM 14A OVERHEAD AREA. MAINTENANCE DEFERRED 14A WASH LIGHT PER MEL. SUBSEQUENTLY CLEARED DMI REPLACING BURNT CONNECTOR. 2L72 4F RTT00011AT 20040707000732004070700073SO 2004 7 7 RAIA00405030 120040516A7830 ACTUATOR EMB 145 EMB145 3260210SO THRUST REVERSER MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03801HK 145053 BOS - ENGINE NR 1 T/R DISAGREE. MAINTENANCE DEFERRED NR 1 T/R PER MEL. SUBSEQUENTLY CLEARED DMI BY ADJUSTING NR 1 T/R BOTTOM ACTUATOR. 2L72 4F RTT00011AT 20040707000742004070700074SO 2004 7 7 RAIA00405031 120040517A21508152403 ACM EMB 145 EMB145ER 3260211SO NR 1 OVERHEATED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03826HK707 145016 SMOKE IN CABIN WHILE PARKED AT GATE. MAINTENANCE DEFERRED NR 1 PACK PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 AIR CYCLE MACHINE. 2L72 4F RTT00011AT 20040707000792004070700079EU 2004 7 7 AWXA200400634 120040612A3110C19266AA01 DISPLAY AIRBUS320 A320232 3930326EU COCKPIT SHORTED A AWXAH DEACTIVATE SYST/CIRCUITS BS SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS CLCLIMB 1 WP28665AW19 19 1644 CLIMBING OUT, AT FL 250 NR 2 MULTIPURPOSE CONTROL & DISPLAY UNIT (MCDU) FAILED SENDING SMOKE & A STRONG BURNING ODOR THROUGHOUT COCKPIT. PULLED NR 2 FMGC & NR 2 MCDU CIRCUIT BREAKERS & DONNED 02 MASKS. SMOKE DISSIPATED, REMOVED 02 MASKS, & CONTINUED FLT UNDER NORMAL OPERATING CONDITIONS. MX R & R NR 2 MCDU IAW AMM 22-82-12-04. ACCEPTANCE TEST CONFIRMED FAILURE OF MCDU. FOUND POWER SUPPLY MODULE BURNED AND FUSE BLOWN, REPLACED POWER SUPPLY MODULE AND FUSE. UNIT REPAIRED AND RETESTED IAW CMM 22-82-03A, REV. 00, AND CMM 22-82-03, REV. 02. 2L72 4F RTA28NM 20040707000872004070700087NM 2004 7 7 AWXA200400642 120040516A5320654957323 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A 1 INCH CRACK WAS FOUND IN LT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE ON AFT OUTBOARD SIDE BS 665, LBL 64. MAINTENANCE REMOVED CRACKED LT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-49573; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040707000892004070700089CE 2004 7 7 DXTA200400321 120040607A52305060001 ISOLATION VALVE CESSNA750 750 2076810CE CARGO DOOR SEAL FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07929QS1499 7500129 DURING FLIGHT BAGGAGE SEAL LIGHT CAME ON THEN CABIN ALTITUDE STARTED TO CLIMB. CLOSED BAGGAGE ISOLATION VALVE, CABIN ALTITUDE CONTINUED TO CLIMB. COULD NOT CONTROL CABIN ALTITUDE IN AUTO OR MANUAL MODE. DECLARED EMERGENCY AND DIVERTED AIRCRAFT TO MTJ. AIRCRAFT LANDED SAFELY. PURGED BAGGAGE DOOR SEAL IAW CESSNA 750 MM CHAPTER 52-30-04. REPLACED ISOLATION VALVE SOLENOID IAW CESSNA 750 MM CHAPTER. OPS CHECK SYSTEM IAW CESSNA 750 M/M CHAPTER 21-51-00, SYSTEM OPS CHECKED GOOD. 2L72 4J RTT00007WI 20040707000972004070700097EU 2004 7 7 MALA040440 120040603A5320 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4Y/2Y INSPECTION IN LCQ, FS 294 TO FS 319 RIGHT I/B SEAT TRACK CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/7/04. 2L72 4T RTA52EU 20040708000102004070800010EU 2004 7 8 CX7A194J0434 120040615A26131734362450 DETECTOR SAAB SF340 340B 7860101EU TAILPIPE SATURATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03300CE 340B184 ABORTED TAKEOFF DUE TO TAILPIPE HOT (4X) PRIOR TO V1. 2L72 4T RTA52EU 20040708000172004070800017EU 2004 7 8 MALA040438 120040608A5101 STRUCTURE SAAB SF340 340B 7860101EU FUSELAGE VIBRATION A MALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL15402XJ 340B402 A/C HAS A LATERAL VIBRATION SIMILAR TO LIGHT TURBULENCE, SEEMS TO BE MORE PRONOUNCED AT SPEEDS ABOVE 210. AIRCRAFT IS SHOWING SIMILAR VIBRATION AT ALL ALTITUDES. MAINTENANCE INSPECTED AIRCRAFT RUDDER DAMPNER, ALL PANELS SWING GEAR RAN ENGINE, TESTED FLT CONTROLS FOR SECURITY, OPS CHECKED. DE-ICE BOOTS, AND LANDING GEAR DOORS UP AND DOWN POSITIONS, ALL INSPECTIONS CHECKED GOOD. 2L72 4T RTA52EU 20040708000212004070800021NM 2004 7 8 AWXA200400657 120040603A5330655298874 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 LCQ - MAJOR REPAIR - DURING C-17 CHECK A 5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 940, STR 20 LT. MAINTENANCE REMOVED EXISTING REPAIR DOUBLERS AND CUT OUT DAMAGED AREA OF SKIN AT BS 940, STR 20 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 3 EACH FILLERS, A REPAIR DOUBLER, AND A TRIPLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5361-04166-RC1. 2L72 4F RTA16WE 20040708000292004070800029NM 2004 7 8 DL757040534 120040611A2820BACC63CB2041 CONNECTOR BOEING757 757232 1384965NM FUEL PUMP FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27634DL 23615 WORKING MCO RT AFT MAIN FUEL PUMP INOPERATIVE. FOUND RT AFT SPAR MOUNTED CONNECTOR D40930P BURNED AND ARCING. REPLACED CONNECTOR D40930P, OPS CHECK OK. 2L72 4F RTA2NM 20040708000412004070800041NM 2004 7 8 DL73S040540 120040609A5753654642744 FLAP TRACK BOEING737 737247 138448DNM RT WING STRIPPED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 RIGHT WING O/B FLAP I/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 BOLT HOLES THAT ATTACH MAIN CARRIAGE STOP TO O/B FLAP I/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090835-14, REVISION INITIAL. 2L72 4F A16WE 20040708000422004070800042NM 2004 7 8 DL73S040541 120040609A5753654642742 FLAP TRACK BOEING737 737247 138448DNM RT WING STRIPPED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 RIGHT WING O/B FLAP O/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 HOLES THAT ATTACH MAIN FLAP CARRIAGE STOP TO O/B FLAP O/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090836-14, REVISION INITIAL. 2L72 4F A16WE 20040708000432004070800043NM 2004 7 8 DL73S040542 120040608A5551654759522 FITTING BOEING737 737247 138448DNM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 HORIZONTAL STABILIZERS ATTACH FITTINGS LUGS AND CLEVIS LUGS CORROSION: CORROSION BLENDED AND O/S BUSHINGS INSTALLED ER/A 090581-14AD, REVISION INITIAL. 2L72 4F A16WE 20040708000482004070800048NM 2004 7 8 AWXA200400647 120040519A53106935350 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .875 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE BS 500A, STR 16 RT. MAINTENANCE REMOVED DAMAGED STRINGER SHEAR TIE CLIP AT BS 500A, STR 16 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040708000492004070800049NM 2004 7 8 AWXA200400648 120040524A53206546812 SHEAR WEB BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .875 INCH CRACK WAS FOUND IN AFT CABIN SHEAR WEB, JUST BELOW FLOOR LEVEL AT BS 967, LBL 36. MAINTENANCE REMOVED DAMAGED AFT CABIN SHEAR WEB AT BS 967, LBL 36; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PART IAW B737-300 SRM 53-60-51 FIG 1. 2L72 4F RTA16WE 20040708000502004070800050NM 2004 7 8 AWXA200400649 120040521A5313BAC1498157 STRINGER BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON STRINGER 15 LT AT BS 1006. MAINTENANCE CUT OUT DAMAGE IN STRINGER 15 LT AT BS 1006; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, FILLER AND DOUBLER; INSTALLED SPLICE REPAIR IAW B737-300 SRM 53-00-03 FIG 201. 2L72 4F RTA16WE 20040708000512004070800051NM 2004 7 8 AWXA200400650 120040525A53206546811 WEB BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LCQ - MAJOR REPAIR - DURING C-19 CHECK A .75 INCH CRACK AND CORROSION WERE FOUND ON AFT CABIN FLOOR WEB WHERE FLANGE ATTACHED TO SEAL AND RETAINER AT BS 1006, RBL 38. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR WEB AT BS 1006, RBL 38; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-13 FIG 1. 2L72 4F RTA16WE 20040708000522004070800052EU 2004 7 8 AWXA200400651 120040611A5210FE1740011 DAMPENER AIRBUS320 A320231 3930325EU L-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW46634 082 MCN - EES - DURING C-04 CHECK THE L-1 DOOR ASSIST CYLINDER WAS FOUND TO HAVE NO DAMPENING ACTION. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR ASSIST CYLINDER IAW AMM 52-11-14-000-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040708000542004070800054NM 2004 7 8 DHL2004748003 120040611A2612 FIRE LOOP BOEING727 727225 1384077NM NR 1 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01748DH 22440 NR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ON C/B PANEL ILLUMINATED IN FLIGHT. DOES NOT ILLUMINATE ON GROUND. DEFERRED NR 1 FIRE WARNING GROUND FAULT DETECTOR SYS. PER MEL 26-9-1 DMI 16886 PLACARD INSTALLED. REPOSITIONED NR 1 ENG FIRE LOOP PER DHL B727 MM 26-11-012. OPS CHECKS GOOD PER MM 26-11-001. THIS CLEARS DMI 16886. PLACARD REMOVED. NO PARTS REMOVED. 2L73 4F A3WE 20040708000552004070800055NM 2004 7 8 DL73S040543 120040610A533065458001205 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRATCH WAS FOUND ON THE LOWER SKIN AT THE S14 SKIN LAP FROM STA 259-312. REPAIRED PER ERA 089694-14. 2L72 4F A16WE 20040708000562004070800056NM 2004 7 8 DL73S040544 120040610A53306545800 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRATCHES WERE FOUND ON THE LOWER FUSELAGE SKIN AT THE STR 14L LAP SPLICE BETWEEN STA 345 AND 360. REPAIRED PER ERA 090265-14. 2L72 4F A16WE 20040708000582004070800058NM 2004 7 8 DL73S040546 120040612A261365528087 DETECTOR BOEING737 737232 1384475NM NR 1 ENGINE MALFUNCTIONED A DALAB EMER. DESCENT N FALSE WARNING CRCRUISE 1 SO27323DL 23095 RECEIVED LT WING BODY OVERHEAT AT 31,000 NORM CRUISE. TURNED LT BLEED OFF, LIGHT CONTINUED. DESCENDED AND PULLED LT ENG TO IDLE, LIGHT EVENTUALLY WENT OUT. REPLACED OVERHEAT DETECT CONT UNIT. TIGHTENED SEVERAL CLAMPS IN LT A/C BAY AND LT LEADING EDGE. CLEANED LOOP CONNECTORS. 2L72 4F RTA16WE 20040708000592004070800059NM 2004 7 8 DL73S040547 120040612A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27379DL 23606 ER/A 091163-14 - FUSELAGE SKIN FS 727B & STR 18L REPAIR OF CRACK. A 3.75 INCH LONG CRACK DUE TO FATIGUE WAS FOUND ALONG THE CHEM MILL LINE JUST BELOW STRINGER 18L JUST AFT OF FS 727B. 2L72 4F A16WE 20040708000602004070800060NM 2004 7 8 DL73S040548 120040612A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27379DL 23606 ER/A 091164-14 - FUSELAGE SKIN FS 747, STR 18R REPAIR OF CRACK. A 2.0 INCH LONG FATIGUE CRACK WAS FOUND ALONG THE CHEM MILL LINE JUST BELOW STRINGER 18R AFT OF FS 747. 2L72 4F A16WE 20040708000622004070800062NM 2004 7 8 DL76S040525 120040609A5330143T31112 SKIN BOEING767 767332 1382001NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27132DN 24981 LIGHTNING STRIKE ON THE FUSELAGE SKIN AT STATION 564 AND STRINGER 3L. REPAIRED IAW ER/A 090627-14. 2L72 4F RTA1NM 20040708000632004070800063NM 2004 7 8 DL73S040526 120040609A5330654580026 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRATCHES ON THE FUSELAGE SKIN AT STRINGER 19L FROM STATIONS 259 - 360. AREA REPAIRED IN ACCORDANCE WITH ERA 090232-14. 2L72 4F A16WE 20040708000642004070800064NM 2004 7 8 DL73S040527 120040609A53126546568524 BULKHEAD BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 STATION 1016 BULKHEAD WEB, STIFFENERS AND CHORDS CORRODED AT BL 0. CHORD SUFFERED DAMAGE AT BL 0 DURING COURSE OF REPAIR. AREA REPAIRED IAW ERA 089856-14AD. 2L72 4F A16WE 20040708000652004070800065NM 2004 7 8 DL73S040528 120040609A53306545800709 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SKIN AT STATION 178 AND WL 195 SUFFERED DAMAGE AND REQUIRED OVERSIZE FASTENERS THRU THE STATION 178 BULKHEAD CHORD AND AN EDGE TRIM. REPAIRED IAW ERA 089942-14AD. 2L72 4F A16WE 20040708000672004070800067NM 2004 7 8 DL73S040549 120040613A21337110035 OUTFLOW VALVE BOEING737 737247 138448DNM CABIN PRESSURE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27375DL 106613 23602 PASSING FL 220 CABIN UNABLE TO MAINTAIN PRESSURIZATION. DESCENT INITIATED QRH PROCEDURES ACCOMPLISHED. NO INJURIES OR AIRCRAFT DAMAGE. REPLACED AIRCRAFT OUTFLOW VALVE ASSEMBLY PER M/M. SYSTEM CHECKS NORMAL. 2L72 4F A16WE 20040708000682004070800068NM 2004 7 8 DL73S040550 120040613A53306545765726 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27379DL 23606 DURING ACCOMPLISHMENT OF ME-09 OF EO 03-071327-03, IT WAS NECESSARY TO OVERSIZE SEVERAL FUSELAGE SKIN FASTENER HOLES WHICH HAD BEEN INSTALLED THROUGHT THE REMOVED EGPWS DOUBLER. REPAIR PER ERA 091173-14. 2L72 4F A16WE 20040708000722004070800072NM 2004 7 8 UPS04242574 120040531A5340 ATTACH FITTING BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, ATTACH FITTING AT THE BASE OF THE BS 950 STRUCTURAL FITTING HAS EVIDENCE OF INTERGRANULAR CORROSION. FITTING REPLACED IAW SRM 51-30-02 & DRAWING 65-16338. 2L73 4F A3WE 20040708000742004070800074NM 2004 7 8 UPS04242576 120040531A5730 PANEL BOEING727 72725C 138400HNM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, CRACK ON LT WING T/E PANEL UPPER SURFACE FWD OF NR 5 SPOILER. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-30-02 & 51-10-02. 2L73 4F A3WE 20040708000752004070800075NM 2004 7 8 UPS04242580 120040529A53206518415 ANGLE BOEING727 72725C 138400HNM NLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, CORROSION AT BS 312L VIEW IN 3RD LIGHTENING HOLE FROM FRONT OM INBOARD ANGLE MIDWAY BETWEEN UPPER AND LOWER NWW CHORDS. CORRODED ANGLE FABRICATED AND INSTALLED IAW DWG 65-18415. 2L73 4F A3WE 20040708000782004070800078NM 2004 7 8 UPS04242588 120040531A5320 WEB BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, NOSE WHEEL WELL STRUCTURE HAS EVIDENCE OF CRACK AT BSTA 240 LBL. REPAIR CARRIED IAW SRM 51-40-02. LEAK CHECKED SATISFACTORY. 2L73 4F A3WE 20040708000822004070800082NM 2004 7 8 SWAA041870 120040702A335010126211 LIGHT BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29631SW 27706 FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040708000832004070800083NM 2004 7 8 SWAA041871 120040702A57546546421200 SKIN BOEING737 7372H4 138448CNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 RIGHT WING NR 6 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 6 L/E SLAT PER MM. 2L72 4F A16WE 20040708000862004070800086NM 2004 7 8 SWAA041874 120040702A3350101073 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW296231W 27933 FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20040708000892004070800089NM 2004 7 8 SWAA041877 120040702A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING OTS, FOUND FUSELAGE SKIN AT BS 942, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040708000902004070800090 2004 7 8 SWAA041878 420040702A256561621469 SLIDE BOEING737 7373G7 1384595NM R2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040708000922004070800092NM 2004 7 8 UPS04M42585 120040511A5330 SKIN DOUG MD11 MD11F 3023600NM AFT FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP INSPECTION TYPE: C2, FUSELAGE SKIN IS GOUGED BEYOND LIMITS AFT OF STATION 1946.75 AFT OF AFT BULK CARGO DOOR. BLENDED OUT GOUGES, TRIMMED EXISTING DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5330-20608-A, SAA SK 251-690. 2L73 4F RTA22WE 20040708000932004070800093NM 2004 7 8 UPS04M42586 120040511A7160 INLET DOUG MD11 MD11F 3023600NM NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP INSPECTION TYPE: C2, NR 2 ENGINE INLET EXTERIOR SKIN IS CRACKED AROUND FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED FILLERS AND DOUBLERS IAW SRM 54-10-00 FIG 1 AND SERVICE BULLETIN MD11-54-065. 2L73 4F RTA22WE 20040708000982004070800098 2004 7 8 SWAA041883 420040703A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040708000992004070800099NM 2004 7 8 SWAA041884 120040703A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040708001002004070800100NM 2004 7 8 04FDEA01707 120040613A3243 SENSOR DOUG MD11 MD11 3023602NM MLG BRAKE MALFUNCTIONED A FDEAO OTHER N FALSE WARNING LDLANDING 1 SO25580FE 48471 AFTER T/O & GEAR RETRACTION, PASSING 6000 FT, BRAKE DIFF TEMP ALERT APPEARED. TEMP ON BRAKE NR 6 WAS 400 & RISING. ALL OTHER BRAKE TEMPS WERE LESS THAN 50. LANDING GEAR WAS EXTENDED TO COOL & STOP THE RISING TEMP ON BRAKE NR 6. BRAKE DIFF TEMP ALERT WENT AWAY AFTER TEMP DECREASE BELOW 300. AFTER LANDING BRAKE TEMP IS AT 656 DEG. REMOVED AND REPLACED BRAKE TEMP SENSOR PER MM 32-46-01-4. 2L73 4F RTA22WE 20040708001022004070800102NM 2004 7 8 SWAA041885 120040703A53156546810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947, LBL 53, CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040708001032004070800103NM 2004 7 8 SWAA041886 120040703A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 26L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040708001042004070800104NM 2004 7 8 SWAA041868 120040702A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 16, STRINGER 16R AND STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040708001052004070800105SO 2004 7 8 C2XA04SH377 120040620A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 14. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 55320-01125. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001062004070800106SO 2004 7 8 C2XA04IA075 120040620A335072875775 LIGHT EMB 145 EMB145ER 3260211SO GALLEY LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714943 145553 IAH - FLIGHT 2551, DURING PREFLIGHT INSPECTION THE LOWER FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE LOOSE. MAINTENANCE RESECURED THE AFFECTED EMERGENCY LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001072004070800107SO 2004 7 8 C2XA04IA074 120040617A4930 ODOR EMB 145 EMB145 3260210SO APU DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2713964 145123 IAH - FLIGHT 2197, THE CREW REPORTED A STRONG FUEL ODOR WHEN THE APU WAS STARTED AFTER LANDING. MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DISCREPANCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001082004070800108SO 2004 7 8 C2XA04TY094 120040623A531014522461003 GUSSET EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION FR 22 GUSSET CAP WAS FOUND CORRODED AROUND THE RIVETS. REMOVED FR 22 GUSSET CAP, FAB A NEW CAP, ALODINED, PRIMED AND PAINTED. THEN INSTALL FAB PART IAW EMB 135/145 SRM 51-30-03; SRM 51-40-02; 03; 04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040708001092004070800109NM 2004 7 8 SWAA041894 120040704A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 513, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040708001112004070800111 2004 7 8 SWAA041896 420040706A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040708001122004070800112 2004 7 8 SWAA041897 420040706A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29407WN 29817 R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R2 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2L72 4F RTA16WE 20040708001132004070800113NM 2004 7 8 SWAA041898 120040706A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND SEVERAL PHOTOLUMINESCENT STRIPS THROUGHOUT CABIN, DAMAGED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20040708001142004070800114NM 2004 7 8 SWAA041899 120040706A57546546431279 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040708001172004070800117EU 2004 7 8 169041 120040611A2150 A/C PACK SAAB SF340 340B 7860101EU CABIN COOLING MALFUNCTIONED A NSVAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27346CJ 346 SMOKE FILLED COCKPIT AND CABIN IN FLIGHT LAV SMOKE ANNUNCIATOR ILLUMINATED. AIRCRAFT MADE UNSCHEDULED LANDING, FOUND RIGHT ACM TURBINE SIEZED. RAN AIRCRAFT TO VERIFY NO FURTHER TRACES OF SMOKE, DEFERRED PER MEL RIGHT AIR CONDITIONING PACK 21-50-1 CAT C. 2L72 4T RTA52EU 20040708001182004070800118NE 2004 7 8 200410 220040614A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA PW121 PW121 52124NE NR 2 MALFUNCTIONED A KPVAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP13813SN 032 LOW TORQUE (LESS THAN 20) ON APPLYING TAKEOFF POWER. ABORTED TAKEOFF. INSPECTED NR 2 ENGINE RIGGING, POWER AND CONDITION LEVERS. PERFORMED GROUND MAINTENANCE TEST RUN-UP IAW DHC -8 PSM 1-8-2, 71-00-00 PG 551-552. OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20040708001212004070800121SO 2004 7 8 C2XA04IA076 120040607A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713124 145689 MCI - FLIGHT 2669, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT RT AFT EXTERIOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040708001222004070800122NM 2004 7 8 234TR0018 120040610A33506104789 BATTERY PACK BOEING737 737228 13844AGNM EMERGNECY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05234TR 23004 EMERGENCY LIGHTS OUTSIDE OF L1 AND R1 DOORS INOP. REPLACED BATTERY PACK IN FORWARD CARGO BIN. LIGHTS OPERATE NORMAL PER MM 33-51-01. 2L72 4F RTA16WE 20040708001232004070800123 2004 7 8 HNAA0400058 420040612A3442MI5853512 DISPLAY DHAV DHC8 DHC8311 1386006EA WX RADAR SYS INOPERATIVE A HNAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA07326EN 234 WITH WEATHER RADAR ON, GRAPHICS AND WEATHER COMPRESS'S TOWARD CENTER OF RADAR SCREEN. RETURNED TO FIELD. REMOVED AND REPLACED INDICATOR, OPS CHECKED GOOD. 2H72 4T RTA13NM 20040708001252004070800125SO 2004 7 8 C2XA04SH380 120040622A532014529495003 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001272004070800127NM 2004 7 8 SWAA041901 120040706A53116546566 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 994, RBL 47, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2L72 4F RTA16WE 20040708001282004070800128NM 2004 7 8 SWAA041902 120040706A53116546949 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 987 RBL 43, CORRODED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2L72 4F RTA16WE 20040708001292004070800129 2004 7 8 SWAA041889 420040705A2565D31354 SLIDE BOEING737 7372H4 138448CNM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED RON, R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2L72 4F A16WE 20040708001312004070800131NM 2004 7 8 SWAA041891 120040704A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500B + 4, STRINGER 16R, BS 500B + 14, STRINGER 16R, BS 500B + 10, STRINGER 6R, BS 500D + 6, STRINGER 15R, CRACKED. REPAIRED FUSELAGE SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040708001332004070800133NM 2004 7 8 SWAA041893 120040704A57436937877 FITTING BOEING737 7373A4 1384585NM RT & LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED PM CHECK, FOUND LT AND RT MLG WALKING BEAM HANGER FITTINGS CORRODED. REPAIRED RT AND LT FITTINGS PER EA. 2L72 4F RTA16WE 20040708001352004070800135 2004 7 8 SWAA041904 420040706A256565C161216 GIRT BAR BOEING737 7373H4 1384600NM L1 DOOR SLIDE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED L1 DOOR EVAC DOOR SLIDE FITTING PER SRM. 2L72 4F RTA16WE 20040708001362004070800136NM 2004 7 8 SWAA041905 120040706A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 188 STRINGER 15R, BS 188 STRINGER 16L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040708001382004070800138NM 2004 7 8 SWAA041907 120040706A53116517685 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT BS 348, LBL 50, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040708001392004070800139NM 2004 7 8 SWAA041908 120040706A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040708001402004070800140SO 2004 7 8 C2XA04BT067 120040622A1420 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE GALLEY EMERGENCY LIGHT, OPS CHECKED LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040708001412004070800141SO 2004 7 8 C2XA04SH383 120040622A532014525991003 DOUBLER EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE LEFT HAND SIDE WALL DOUBLER AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001422004070800142NM 2004 7 8 SWAA041909 120040706A55306546872 CLEVIS BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR CLEVIS, FWD AND AFT LUG, CORRODED. REPAIRED VERTICAL STAB PER ER. 2L72 4F RTA16WE 20040708001432004070800143NM 2004 7 8 SWAA041910 120040706A55106551524 CLEVIS BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND LT AND RT HORIZONTAL STAB CENTER SECTION CLEVIS, FWD AND AFT LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20040708001462004070800146SO 2004 7 8 C2XA04SH389 120040626A532014521725015 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001482004070800148NM 2004 7 8 MWEA040099 120040615A5270 WARNING LIGHT BOEING717 717200 1383700NM GALLEY ILLUMINATED A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31916ME 55179 FORWARD GALLEY DOOR LIGHT ILLUMINATED. PERFORMED FIM PROCEDURE 52-40 TASK 806, ADJUSTED AIR GAP. OPERATION CHECKED GOOD. 2L72 4F TRA6WE 20040708001512004070800151EU 2004 7 8 U30A200400006 120040525A3230114079017 SELECTOR VALVE AIRBUS320 A320214 3930316EU ZONE 744 FAULTY A U30AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA17266AV 1152 ON FLT 280 EWR-PIE AFTER TAKEOFF, THE CREW HAD ECAM INDICATIONS THAT THE LANDING GEAR DOORS WERE NOT CLOSED AND THE LANDING GEAR WAS NOT UPLOCKED. THE CREW ATTEMPTED A GEAR RE-CYCLE WITH NO SUCCESS. AFTER PLACING THE GEAR HANDLE DOWN & CONFIRMING 3 GREEN (DOWN & LOCKED), THE CREW RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE IAW AMM 32-31-00-720-002 AND CYCLED THE GEAR 5 TIMES WITH NO DEFECTS NOTED. A MAINTENANCE ACCEPTANCE FLIGHT WAS ALSO CONDUCTED WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040708001522004070800152NM 2004 7 8 C1HA200497001 120040610A5260 STRIKER BOEING727 727270 138408PNM MLG OUT OF ADJUST A C1HAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15697CA 23052 AFT AIRSTAIR AMBER LIGHT CAME ON IN FLIGHT. RAN COM 2.25.2. RETURNED TO LAS. DAYLIGHT WAS VISABLE FROM INSIDE THE AIRCRAFT. INSPECTED & RESCHEDULED PER MEL 52-6-C CAT -C- CONTROL C06208. PLACARDS INSTALLED & MX CONTROL NOTIFIED. NO DDG REQUIRED. STAIRS VERIFIED UP & LOCKED ON DEPARTURE. ITEM RESOLVE UNDER MDDR: C06208. ADJUSTED AFT LEFT UPLOCK SWITCH STRIKER PLATE IAW MM 57-67-01. 2L73 4F RTA3WE 20040708001542004070800154SO 2004 7 8 C2XA04BT069 120040624A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 DURING ROUTINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS NOT WORKING WHEN IN ARMED AND IN AUTO ESSENTIAL ELECTRICAL MODE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECKED GOOD IAW EMB 145 MM 33-50-00. 2L72 4T RTT00011AT 20040708001552004070800155NM 2004 7 8 QXEA200400429 120040610A6120D44044 POTENTIOMETER DHAV DHC8 DHC8202 2809007NM ZONE 400 INOPERATIVE A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09379PH 530 PDX - ON FLIGHT NUMBER 2294, AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL, TESTED OK DURING DEPARTURES. TORQUE WAS AT 96 PERCENT. THE AIRSPEED WAS AT 70 KIAS. ADJUSTED AUTOFEATHER ARMING POTENTIOMETER ON THE NR 1 AND NR 2 POWER LEVERS. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001562004070800156NE 2004 7 8 QXEA200400427 220040612A72303038060 IMPELLER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 VIBRATION A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09600QX 10005 965221 PDX - ON FLIGHT NUMBER 2555, ON CLIMBOUT, NR 1 FAN VIBRATION ROSE ABOVE 1.7. AFTER LERCHING AT 29,000 FT, AIRCRAFT COULD NOT MAINTAIN CRUISE SPEED WITH POWER SET TO KEEP FAN ON THE GREEN ARC. FOUND ONE BLADE TIGHT. LOOSENED AS REQUIRED. GROUND RAN AIRCRAFT WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040708001572004070800157NM 2004 7 8 QXEA200400428 120040610A6120954215B653323 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 400 INOPERATIVE A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09379PH 530 PDX - ON FLIGHT NUMBER 2149, DURING TAKEOFF ROLL, THE AUTOFEATHER FAILED TO ARM. THE TORQUE WAS AT 95 PERCENT. THE AIRSPEED WAS AT 70 KIAS. AUTOFEATHER SELECT HAD ILLUMINATED AND AUTOFEATHER TEST NORMAL. CLEANED, INSPECTED AND SECURED CANNON PLUGS ON 1 & 2 ENGINE TORQUE SIGNAL CONDITIONER. NO DEFECTS WERE NOTED. INSPECTED AND CLEANED POWER AND CONDITIONER LEVER PEDESTAL SWITCHES. THERE WERE NO DEFECTS NOTED. GROUND RAN AIRCRAFT AND ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001582004070800158EA 2004 7 8 QXEA200400430 120040612A75404157T43P01 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 400 INOPERATIVE A QXEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09607QX251 10024 9655313 PDX - ON FLIGHT NUMBER 2555, AFTER DEPARTURE THE AFT LAVATORY SMOKE DETECTOR WARNING MESSAGE APPEARED. FLIGHT ATTENDANT REPORTED SEEING SMOKE NEAR THE CEILING OF CABIN. SMOKE HAD AN ACRID SMELL TO IT. REPLACED THE 4TH STAGE SHUT OFF VALVE ON NR 2 ENGINE, FOR PRECAUTIONARY MEASURES. GROUND RAN ENGINES AND APU WITH NO SMOKE/SMELL NOTICED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040708001602004070800160SO 2004 7 8 C2XA04BT070 120040623A33505113WW BULB EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2713936 145025 CREW REPORTED, STRONG ODOR OF BURNED ELECTRICAL COMPONENTS IN CABIN ROW 7 AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY AT ROW 5 AND 6 AREA IAW EMB 145 MM 33-21-06, OPS CHECKED LIGHTS GOOD. 2L72 4F RTT00011AT 20040708001622004070800162NE 2004 7 8 GLBA20030638 220040611A75321098129 BLEED VALVE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03299UX1272 1272 120299 LT PACK PRODUCED SMOKE IN THE CABIN. REMOVED AND REPLACED RIGHT ENGINE BLEED VALVE. 2L72 4T4 TRTA31SO E20NE 20040708001662004070800166SO 2004 7 8 ENHA2004P3102 120040522A5730 SKIN PIPER PA31 PA31350 7103110SO RT WING DAMAGED E ENHAK NONE O OTHER ININSP/MAINT 1 AL034105D 318252027 PILOT REPORTED INSPECTION OF AIRCRAFT REQUIRED AFTER LANDING. PILOT REPORTED THAT AIRCRAFT ENCOUNTERED EXTREME SEVERE TURBULANCE UPON DEPATURE FROM GOOD NEWS BAY, ALASKA. VISUAL INSPECTION DETERMINED THAT THE LEFT WING ENCOUNTERED SEVERE STRESS FORMING WRINKLES AND RIPPLED SKIN OF THE WING TOP SURFACE OUTBOARD OF THE ENGINE NACELLE. THE RIGHT WING ALSO SHOWS STRESS WRINKLES AND RIPPLES ON THE WING UPPER SURFACE IN THE SAME LOCATION AS LEFT WING. INSPECTION OF THE ELEVATORS SHOWS STRESS BUCKLING AT THE SAME LOCATIONS BOTH LEFT AND RIGHT JUST INBD OF THE OUTBD HINGE. THE RIGHT ELEVATOR HORN SHOWS STRESS WRINKLING ON THE TOP SURFACE. AIRCRAFT REMOVED FROM SERVICE PENDING EVALUATION. 1L72 3O A20SO 20040708001712004070800171NM 2004 7 8 250TR0033 120040614A33506013211 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 AFT DOORS EXTERIOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY BATTERY CHARGER FOR L2 AND R2 EXTERIOR EMERGENCY LIGHTS. OPS CHECKS GOOD PER MM 33-51-8P. 2L72 4F RTA16WE 20040708001722004070800172NM 2004 7 8 304AW0008 120040617A3350 BATTERY PACK BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05304AW 24011 ROWS 1-4 OF EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED FUSES IN BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-51. 2L72 4F RTA16WE 20040708001742004070800174NM 2004 7 8 QXEA200400432 120040612A526085217758105 TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 800 CLOGGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09415QX1129 4081 PDX - ON FLIGHT NUMBER 2310, FLIGHT ATTENDANT UNABLE TO OPEN AFT AIRSTAIR DOOR. UPON INSPECTION FOUND THE AIRSTAIR TRACKS GUMMED AND CLOTTED WITH DEBRIS. CLEANED AND LUBED TRACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001762004070800176EA 2004 7 8 QXEA200400447 120040615A24303502 TRU CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09608QX6149 6149 10026 DEN - FLIGHT 4093 - BURNED WIRE ODOR COMING FROM NR 2 RIGHT OUTBOARD TRU. REMOVED AND REPLACED NR 2 RIGHT HAND TRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040708001772004070800177 2004 7 8 TSAA0479046 420040609A8300207K BEARING BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 2 ENG GBOX FAILED A TSAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 WP13807AL55673 23443 666682 NON-ETOPS FLIGHT 206, HNL-OGG: ON DESCENT ONTO OGG THE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, THE OIL PRESSURE DECREASED TOWARD ZERO AND THE OIL QUANTITY BEGAN DROPPING WITH THE OIL TEMPERATURE IN THE NORMAL RANGE. FOLLOWED QRH AND SHUT DOWN THE NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE IAW FORM M-211, 212, 213, 214 AND 215. LEAK AND OPS CHECK GOOD. INSPECTION OF GEARBOX INDICATED REAR LUBE OIL PUMP DRIVE SHAFT BEARING FAILURE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A16WE E2EA 20040708001802004070800180SO 2004 7 8 C2XA04SH379 120040622A532014525422001 SILL EMB 145 EMB145 3260210SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE LEFT HAND CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 60 AND FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001812004070800181SO 2004 7 8 C2XA04SH378 120040622A532014522226003 BUTTSTRAP EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 DURING C-CHECK THE CENTER BUTTSTRAP FROM FRAME 59 TO FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001822004070800182 2004 7 8 BHA07RS 420040603A6122DCFS290D9AT3 GOVERNOR CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C505 GL LT ENGINE MALFUNCTIONED E EA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM04115BH 958 340A1531 290378 860907 DURING CRUISE, AT AN ALTITUDE OF 10,000 FEET, THE PILOT NOTICED A REDUCTION IN MANIFOLD PRESSURE AND POWER FOR THE LEFT ENGINE. THE LEFT PROPELLER STARTED TO FEATHER. THE PILOT SHUT DOWN THE LEFT ENGINE AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. POST FLIGHT INSPECTION FOUND THE LEFT PROPELLER GOVERNOR HAD FAILED INTERNALLY. SUBMITTED TO CORRECT PREVIOUSLY SUBMITTED SDR, OPERATOR CONTROL #BHA06RS 1L72 3O3 O 3A25 E8CE 5 CP22EA 20040708001832004070800183NM 2004 7 8 20049 120040611A2611 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005NM CARGO BAY MALFUNCTIONED A KPVAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP13808WP 026 SMOKE WARNING LIGHT ILLUMINATED ON TAXI OUT. INSPECTED SMOKE DETECTORS IN BAGGAGE COMPARTMENT AND PERFORMED OPS CHECK IAW DHC 8 MM 26-12-00 PG 201 PAR 1A. OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 20040708001842004070800184SO 2004 7 8 CHQA000500 120040602A3320 BALLAST EMB 145 EMB145LR 3260212SO GALLEY OVERHEATED A CHQAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11284 145427 FLT 3101 SDF - CLT: PASSING THROUGH 10,000 FT F/A REPORTED ODOR LIKE BURNING PLASTIC COMING FROM THE GALLEY AREA. NO VISIBLE SMOKE OR VAPOR. ELECTED TO RETURN TO SDF. DONNED 02 AND ACCOMPLISHED EMERGENCY CHECKLISTS. DECLARED EMERGENCY WITH SDF APPROACH. DEPRESSURIZED CABIN AND ODOR WENT AWAY. SDF FIRE/RESCUE SCANNED AIRCRAFT AT GATE WITH IR IMAGING CAMERA AND FOUND NO HOTSPOTS. MX PRESSURIZED ACFT, RAN PACKS, AND FOUND SMELL COMING FROM OVERHEAD PANEL ABOVE GALLEY. FOUND BALLAST OVERHEATED. REMOVED AND REPLACED BALLAST. INSPECTED WIRING AND SURROUNDING AREA, NO DEFECTS. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040706000342004070600034NM 2004 7 6 SWAA041826 120040629A5313BAC1498 STRINGER BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 25L, BS 969, CORRODED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040706000392004070600039 2004 7 6 SWAA041834 420040629A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND L2 AND R2 DOOR EVAC DOOR SLIDES GIRT BAR DOOR HOOKS CORRODED. REMOVED AND REPLACED L2 AND R2 DOOR EVAC SLIDE GIRT BAR DOOR HOOKS PER MM. 2L72 4F RTA16WE 20040706000522004070600052NM 2004 7 6 SWAA041846 120040630A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 370, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040706000622004070600062NM 2004 7 6 04FDEA01776 120040617A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK RIGHT HAND STA 1891 FLOOR SUPPORT HAS CORROSION BETWEEN SEAT TRACK REF X=75.25 AND X=102.5. REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814 & INSTALLED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040706000752004070600075NM 2004 7 6 04FDEA01784 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING INBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FEDEX EA #1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR. 2L73 4F RTA22WE 20040706000762004070600076NM 2004 7 6 04FDEA01785 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER MOUNTING OUTBOARD BOLT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=0.516, FINAL DIAMETER=0.596 AND REPAIRED AS PER FEDEX EA #1-5750-78009, OUTBOARD TRAILING EDGE FLAPS - OUTBOARD FORWARD HINGE BRACKET (WING SIDE) - CORROSION REMOVAL - REPAIR. 2L73 4F RTA22WE 20040706000872004070600087NM 2004 7 6 04FDEA01737 120040615A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT WING O/B FLAP VANE, OVAL SHAPE HOLE ON NR 2 TEE FITTING SECOND FROM I/B SIDE FOUND CORRODED. REMOVED AS PER CMM 20-10-02; ORIGINAL OVAL HOLE=0.860 X 0.566; REWORKED OVAL HOLE=0.870 X 0.610; FPI CARRIED OUT IAW CMM 20-30-02 REV 42 FOUND NO CORROSION AND NO CRACK EVIDENT; SLIP FIT BUSHING MACHINED AS PER SRM 57-20-00 FIG 18 PAGE 47 VOL 1; INSTALLED AS PER MM 27-50-34-4; RT WING O/B FLAP VANE NR 2 TEE FITTING INSTALLED AS PER CMM 57-52-04. 2L73 4F RTA22WE 20040706000912004070600091NM 2004 7 6 SWAA041861 120040701A5310571769 WINDOW FRAME BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND BOTH LT AND RT NR 1 COCKPIT WINDOW POSTS CRACKED AT UPPER CORNERS. REPAIRED RT AND LT WINDOW POSTS PER EA. 2L72 4F RTA16WE 20040706000962004070600096NM 2004 7 6 SWAA041853 120040701A3350311500 LENS BOEING737 7373H4 1384600NM ROW 6C MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 BULLNOSE EMERGENCY EXIT LIGHT AT ROW 6C, MISSING. REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040706000992004070600099WP 2004 7 6 04FDEA01743 120040615A5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110WP ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 FWD CARGO COMPT BILGE STA 879 BL 6R FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 53-00-01, FIG 1 VOL 2. ORIGINAL MATERIAL .063, AFTER BLEND OUT, .038 OUT OF LIMITS EXCEEDING 20 PERCENT. INSTALLED NEW PART, FABRICATED ON MAE TRAVELER T4/ 436359 IAW SRM 51-31-01. 2L73 4F A22WE 20040706001032004070600103NM 2004 7 6 SWAA041866 120040701A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29706SW 27840 DURING SPV, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040706001062004070600106WP 2004 7 6 04FDEA01779 120040610A5711ARB0007501 SPAR CAP DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 DURING C-CHECK AT OAN, INSPECTION FOUND A CRACK IN THE REAR SPAR LOWER CAP AT XORS 412. THE CRACK EXTEND INTO THE VERTICAL LAG AND FWD HORIZONTAL LAG, AND IS CONSISTENT WITH CRACKING DESCRIBED IN S/B DC10-57A137. 2L73 4F A22WE 20040706001122004070600112EU 2004 7 6 04FDEA01723 120040614A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25652FE 735 INSIDE COURIER AREA AT FLOOR LEVEL NR 2 LEFT SEAT TRACK HAS AN AREA OF CORROSION ABOUT 8 INCHES LONG AT FRAME 18. REMOVED AND INSTALLED 1 NEW SEAT TRACK NR 2 LEFT P/N A5361251820002 IAW SRM 51-40-21. 2L72 4F RTA35EU 20040706001142004070600114NM 2004 7 6 04FDEA01771 120040617A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 MAIN CARGO DECK RIGHT HAND STA 1741 TO STA 2007 SEAT TRACK REF X=102.5 SEAT TRACK HAS CORROSION. SEAT TRACK REMOVED AS PER SRM 51-21-01 VOL II, FOUND EXCEEDED LIMIT: ORIG. THICKNESS =0.080, MATERIAL REMAINED=0.043", MATERIAL REMOVED =0.037 AS PER SRM 53-70-00 FIG 3 PAGE 7 VOL I. SEAT TRACK SPLICED AND REPAIRED AS PRE SRM53-70-00 FIG7 VOL I AND SRM 53-70-00 FIG1 VOL I. 2L73 4F RTA22WE 20040706001192004070600119NM 2004 7 6 04FDEA01706 120040613A2612473925 CONTROL UNIT BOEING727 727200 138407ENM FIRE DETECTION FAILED A FDEAFB ACTIVATE FIRE EXT. EMER. DESCENT N FALSE WARNING DEDESCENT 1 SO25270FE 22035 DISCHARGED BOTH LOWER CARGO COMPT FIRE BOTTLES, INDICATION OF FWD LOWER CARGO FIRE. AFTER CHECKING COMPARTMENT AND WHILE BEING TOWED HAD ANOTHER ACTIVATION OF LOWER CARGO FIRE WARNING. REMOVED AND REPLACED LWR FWD CARGO COMPT FIRE SUPP/SMOKE DET CONTROL ELEC UNIT AND CONTROL PANEL PER MM 26-17-012-2 AND MM 26-17-001-5. ALSO, REMOVED AND REPLACED BOTH CARGO COMPT FIRE BOTTLES. 2L73 4F RTA3WE 20040706001282004070600128NM 2004 7 6 DL73S040559 120040615A5210 SKIN BOEING737 737247 138448DNM R1 DOOR CORNER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 FUSELAGE SKIN AT THE R1 DOOR LOWER AFT CORNER WAS FOUND WITH A FATIGUE CRACK. AREA HAD BLIND FASTENER REPAIR INSTALLED AND PERMANENT REPAIR INSTALLED PER ER/A 363957-14. 2L72 4F A16WE 20040707000042004070700004NM 2004 7 7 SWAA041888 120040703A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040707000112004070700011CE 2004 7 7 62188 120040612A5210 COVER BEECH 1900 1900D 1154162CE PAX DOOR DISLODGED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07171YV UE171 PAX DOOR CAM COVER FOUND HANGING INTO CAM AREA, INHIBITING DOOR OPERATION, PAX WERE NOT BOARDED. TIGHTENED HARDWARE, OPS CHECK NORMAL. 2L72 4T RTA24CE 20040707000152004070700015EU 2004 7 7 MALA040444 120040530A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15445XJ 340B445 EMERGENCY LIGHT POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK P/N 3301-51, S/N 2140, JC 33-50-03, UNIT ALSO FAILED ON BENCH. REPLACED BATTERY ASSEMBLY P/N 3301-31 AND PASSED CMM TESTS. RETURN TO SERVICE 6/4/04. 2L72 4T RTA52EU 20040707000192004070700019EU 2004 7 7 RAIA00405016 120040526A275126V10TT4B01 TRANSMITTER AEROSPATR72 ATR72202 8680940EU TE FLAPS INTERMITTENT A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03723TE 283 FLAP EXTENSION FLAG APPEARED AND FLAPS CYCLED WITH FLAP LEVER STILL AT FLAT 15. MAINTENANCE REMOVED AND REPLACED FLAP TRANSMITTER. 2H72 4T RTA53EU 20040707000202004070700020 2004 7 7 RAIA00405017 420040526A23127012100811 RMU JETAIRJETSTMJETSTM4101 1500501EU NR 1 INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03566HK141264190 41084 STL - NR 1 RMU FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 RMU. 2L72 4T RTA41NM 20040707000272004070700027NE 2004 7 7 DHL2004807009 220040615A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 & 3 OVERTEMP P DHLAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO01807DH 45990 NR 1 AND NR 3 WENT ABOVE 905 DEGREES CELSIUS ON T/O, NR 1 TO 917 DEGREES CELSIUS AND NR 3 TO 910 DEGREES CELSIUS N1 WAS SET TO MAX POWER FOR T/O TEMPS WERE EXCEEDED DURING THE INITIAL CLIMB PHASE OF FLIGHT. REF L/P 374627 ITEM 5M AND 6M FOR TROUBLESHOOTING FINDINGS. BOTH ENGINE`S POWER ASSURANCE RUN CHECKED PER JRH 13.3 AND CFM M/M 71-00-00. BOTH ENGINE'S CHECK SERVICEABLE. 2L74 4F4 FRT4A25 E2GL 20040707000362004070700036NM 2004 7 7 DL73S040562 120040524A5315 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 FLOORBEAM TEE CAP UPPER FLANGE CRACKED STA 328 AT LBL 12. INSTALLED REPAIR PER SRM 53-10-9D. 2L72 4F RTA16WE 20040707000512004070700051NM 2004 7 7 UPS04242569 120040530A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, DUE TO BELOW MIN EDGE DISTANCE & CORROSION ON SKIN DURING RT 740 FITTING REPLACEMENT, SKIN REPAIR REQUIRED BETWEEN S17 & S18 RT TO BETWEEN S24 & 25 RT. REPAIR CARRIED OUT IAW AIR ATLANTA AERO ENGINEERING EO 2004-054-005 & SRM 51-30-2 7 51-20-04 UPS ENGINEERING FILE 727-53-20144. 2L73 4F A3WE 20040707000622004070700062EU 2004 7 7 071152 120040623A2612 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE ILLUMINATED A UHLAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL1735SZ 35 APPROXIMATELY 1430 (UTC), FLT 7926 IAD-ABE. THE AIRCRAFT WAS EN ROUTE TO ABE WHEN THE CREW OBSERVED THE RIGHT FIRE DETECT FAIL INDICATION, FOLLOWED BY THE RIGHT FIRE WARNING. CREW FOLLOWED QRH PROCEDURES. BOTH EXTINGUISHERS WERE USED. THE ENGINE WAS SHUTDOWN IN FLIGHT. 2L72 4T4 TRTA52EU E8NE6 20040707000642004070700064EU 2004 7 7 217671 120040625A7710 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENG TORQUE INOPERATIVE A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL17148SD 340A148 APPROXIMATELY 1610 (UTC), FLT 4524 LEX-PIT, THE CREW HAD REJECTED TAKEOFF WHEN THE LT TORQUE GAUGE INDICATED ZERO WITH CONDITION LEVER MAX AND POWER LEVER ADVANCED. 2L72 4T4 TRTA52EU E8NE6 20040707000672004070700067 2004 7 7 UPS04M42478 420040601A2565MN1400 LIGHT DOUG MD11 MD11F 3023600NM L1 DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP LT SLIDE REMOTE PRESS TO TEST LIGHT FOR THE SLIDE NOT WORKING (L1 DOOR). DEFERRED PER MEL 25-61-2. REPLACED BATTERIES, EVAC SLIDE PRESSURE PRESS TO TEST LIGHT CHECKS GOOD. THIS CLEARS M281932. 2L73 4F RTA22WE 20040707000782004070700078NM 2004 7 7 AWXA200400633 120040612A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 8 LT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 LAS - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040707000882004070700088NE 2004 7 7 210061 220040618A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT BIRD INGESTION A UHLAA UNSCHED LANDING C F.O.D. CLCLIMB 1 GL17152CQ 152 217 FLIGHT 4556 PIT-FWA, DURING CLIMBOUT A DEADHEADING CREW MEMBER SAW A BIRD STRIKE THE LT NACELLE. FLIGHT ATTENDANT NOTIFIED THE CREW. THE LT TORQUE STARTED TO DROP WITH AN ASSOCIATED RISE IN TEMPERATURE. THE CREW WITH ADVICE FROM MOC TURNED BACK TO PIT. THE A/C LANDED OVERWEIGHT. A/C TAKEN OUT OF SERVICE. 2L72 4T4 TRTA52EU E8NE6 20040707000902004070700090WP 2004 7 7 DHL2004802006 120040616A33505708458505 BATTERY PACK DOUG DC8 DC873 302199CWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH 46076 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSY WITH SERVICABLE UNIT IAW MM 33-50-1. OPS CHECK, P/N OFF 5708458-505, S/N ID6303, P/N ON 5708458-505, S/N 117J. 2L74 4F RT4A25 20040707000922004070700092SO 2004 7 7 RAIA00405035 120040530A3020C1460092 VALVE EMB 145 EMB145 3260210SO LT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03805HK11895 145096 EVV - LEFT ENGINE ANTI ICE FAIL MESSAGE. MAINTENANCE DEFERRED NR 1 ENGINE ANTI ICE PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING NR 1 ENGINE ANTI ICE VALVE. 2L72 4F RTT00011AT 20040707000952004070700095EU 2004 7 7 RAIA00406008 120040607A7712 TORQUE BRIDGE JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03558HK 41071 PIT - ERRATIC INDICATION ON RT ENGINE. MAINTENANCE CLEARED IEC FAULTS AND SWAPPED TORQUE BRIDGE FROM NR 2 TO NR 1 POSITION AND OPS CHECK GOOD. 2L72 4T RTA41NM 20040708000142004070800014EU 2004 7 8 MALA040436 120040603A2730 ELEVATOR BAC 146 AVRO146RJ85A1500097EU MALFUNCTIONED A MALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 GL15533XJ E2367 DURING LANDING FLARE, FELT CATCH IN ELEVATOR. MAINTENANCE INSPECTED G-WEIGHT DAMPNER IAW 27-31-34, ALL CHECKS GOOD. INSPECTED LT & RT RIGGING AND CABLE CIRCUITS IAW 27-31-00. INSPECTED LAYSHAFT & G-WEIGHT CIRCUIT IAW 27031-00, ALL CHECKS GOOD. PERFORMED RTS OF ELEVATOR AND ELEVATOR TRIM SYSTEM, ALL CHECKS GOOD. SUSPECT DAMPNER MOD, OPS CHECKS GOOD. 2H74 4F RTA49EU 20040708000152004070800015 2004 7 8 MALA040435 420040601A3421H341ADM2 INDICATOR SAAB SF340 340B 7860101EU STBY ATTITUDE MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15412XJ 340B412 IN ROUTE TO SUX STANDBY HORIZON FLAGGED. PILOT RESET C/B. C/B POPPED AGAIN. AIRCRAFT CONTINUED ON TO SUX WHERE A/C WAS GROUNDED UNTIL REPAIRS WERE MADE. MAINTENANCE REPLACED STANDBY ATTITUDE INDICATOR P/N H341ADM2, S/N ON 5106, S/N OFF 6254. STANDBY ATT INDICATOR OPS CHECKS GOOD IAW SF 340 MM CHAP 34. 2L72 4T RTA52EU 20040708000262004070800026NM 2004 7 8 DL73S040531 120040609A5330654577518 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 DAMAGE ON FUSELAGE SKIN ALONG THE TRAILING EDGE WING-TO-BODY FAIRING. REPAIRED IAW ERA 090712-14. 2L72 4F A16WE 20040708000442004070800044 2004 7 8 DHL2004364009 420040611A2565 GIRT BAR AIRBUS300 A300B4203 3930306EU R-1 DOOR DIRTY A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 UNABLE TO DISARM R-1 DOOR. REMOVED DIRT FROM GIRT BAR. OPS CHECK GOOD IAW 52-10-00. NO PARTS REPLACED. 2L72 4F RTA35EU 20040708000532004070800053EU 2004 7 8 AWXA200400652 120040602A5753D5757008720100 SKIN AIRBUS320 A320231 3930325EU FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK A DISBOND AREA WAS FOUND ON THE LOWER SURFACE OF THE RT INBOARD FLAP 13.5 INCH FROM THE INBOARD END. MAINTENANCE CUT OUT DAMAGE ON LOWER SURFACE OF THE RT INBOARD FLAP; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-52-00 FIG 211 PG 247-257. 2L72 4F RTA28NM 20040708000572004070800057 2004 7 8 DL764040545 420040611A23108220990001 TRANSCEIVER BOEING767 767432ER 1385134NM E & E BAY SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27833MH 29706 DETECTED BURNING ELECTRICAL ODOR IN COCPIT. LEFT HF COMM G8 C/B POPPED, ODOR WENT AWAY. REPLACED LEFT HF TRANSCEIVER. 2L72 4F RTA1NM 20040708000662004070800066NM 2004 7 8 DL73S040529 120040609A533065458001178 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 SCRATCHES IN THE FUSELAGE SKIN AT STRINGER 10L BETWEEN STATION 345 AND 360. REPAIR IAW ERA 090206-14. 2L72 4F A16WE 20040708000712004070800071NM 2004 7 8 UPS04242573 120040520A5340 FITTING BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, RIGHT BS 740 FITTING CRACKED BEYOND LIMITS OUTBOARD FLANGE. FITTING REPLACEMENT & REPAIR CARRIED OUT IAW AAAE EO 2004-054-005 UPS ENG FILE 727-53-20144 & UPS EO B727-5310-7477, DRG 65C13724 & SRM 51-30-2. 2L73 4F A3WE 20040708000762004070800076NM 2004 7 8 UPS04242582 120040601A5312 BULKHEAD BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, SUSPECT CRACK IN NLG WW LOCATED ON PRESSURE WEB B STA 240 RBL 24. AREA REPAIRED IAW SRM 51-40-02. 2L73 4F A3WE 20040708000792004070800079NM 2004 7 8 UPS04542587 120040615A2150 A/C PACK BOEING757 75724APF 1384969NM RIGHT SEIZED A IPXAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01419UP 23906 AT 1150Z FL390, SMOKE WAS DETECTED IN THE COCKPIT. APPEARED TO BE LOW IN COCKPIT. DEFERRED RIGHT PACK PER MEL 21-51-1. FOUND RIGHT PACK SEIZED UP. REMOVED AND REPLACED RT ACM IAW M/M 21-51-03-4, RT PACK OPS CHECKS NORMAL. THIS CLEARS M 282798. 2L72 4F RTA2NM 20040708000842004070800084NM 2004 7 8 SWAA041872 120040702A53306518420 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C2 CHECK, FOUND COCKPIT WINDOW POST SKIN BETWEEN L1 AND L2 WINDOWS UPPER CORNER CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040708000852004070800085NM 2004 7 8 SWAA041873 120040702A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 513, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040708000882004070800088NM 2004 7 8 SWAA041876 120040702A53156546803 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 500C + 16, RBL 13.8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040708001102004070800110NM 2004 7 8 SWAA041895 120040704A53306545768 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 316, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040708001152004070800115SO 2004 7 8 C2XA04CL064 120040619A3350375911 LIGHT EMB 145 EMB145LR 3260212SO ROW 12A INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714920 145380 CLE FLIGHT 2314 THE CREW REPORTED THE EMERGENCY LIGHT WAS INOPERATIVE AT 12A ON CEILING. MAINTENANCE REPLACED THE EMERGENCY LIGHT ON THE CEILING AT ROW 12A. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040708001162004070800116SO 2004 7 8 C2XA04SH375 120040618A541214526850401 FIREWALL EMB 145 EMB145 3260210SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV-DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, STEP 4 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001202004070800120WP 2004 7 8 MWEA040103 120040615A528039363611 SUPPORT DOUG DC9 DC981 3022081WP LEFT MLG CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 LEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTINGS IS CRACKED. REMOVED AND REPLACED SUPPORT FITTING. 2L72 4F A6WE 20040708001302004070800130NM 2004 7 8 SWAA041890 120040704A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040708001442004070800144SO 2004 7 8 C2XA04TY093 120040623A531514521700007 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713970 145146 DURING A SCHEDULED 3C INSPECTION, FR 23 LT OMEGA BEAM SPLICE, THE RIVETS ALONG THE AISLE SUPPORT FRAMING SHOWED EVIDENCE OF CORROSION. REMOVED AND REPLACED THE OMEGA BEAM BY SPLICE METHOD FROM FR 19 TO FR 20 IAW EC 5320-01126 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040708001502004070800150SO 2004 7 8 C2XA04BT068 120040622A32347455503 LEVER EMB 145 EMB145 3260210SO COCKPIT FAULTY A C2XAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW2713956 145078 CREW REPORTED, LANDING GEAR WOULD NOT RETRACT. AIR RETURNED TO NEWARK. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, SWUNG LANDING GEAR SEVERAL TIMES, SERVICED NOSE STRUT, CHECKED ALL LANDING GEAR PROXIMITY SWITCHES AND ALL ITEMS OPS CHECKED GOOD. RELIABILITY ENGINEERING RECOMMENDED CHANGING LANDING GEAR SELECTOR LEVER, PERFORMED GEAR RETRACTION TEST, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040708001652004070800165SO 2004 7 8 C2XA04SH382 120040622A532013500322002 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 60. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001682004070800168SO 2004 7 8 C2XA04SH374 120040618A532014524131011 BRACKET EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 SHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001782004070800178SO 2004 7 8 C2XA04SH372 120040618A532014521699003 BUTTSTRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 SHV - DURING C-CHECK THE LEFT FORWARD BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 20 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001862004070800186CE 2004 7 8 EOXA200400001 120040427A5330 SKIN LEAR 60 60LEAR 5170707CE ZONE 100 CORRODED E E0XAK NONE O OTHER ININSP/MAINT 1 SO35460BG 90 LITE TO MODERATE TO SEVERE CORROSION ON FUSELAGE WHERE ANTENNAS ARE MOUNTED. CORROSION UNDER AND AROUND SIX DIFFERENT ANTENNAS ON LOWER FUSELAGE FROM FRAME 9 AFT TO FRAME 20.DME 1, FLITEPHONE, TCAS, DME 2, ATC 1, AND ATC 2. ANTENNAS REMOVED, CLEANED & EVALUATED. SURFACES OF FUSELAGE UNDER ANTENNAS WERE BLENDED & CLEANED FREE OF CORROSION. MINIMUM THICKNESS OF BLENDED AREAS WERE MEASURED BY AN ULTRASONIC THICKNESS TESTER AND MEASUREMENTS WERE FOUND TO BE AS FOLLOWS; .037 INCH AT FS 137.79, .037 INCH AT FS 151.19, .032 INCH AT 184.99, .032 INCH AT FS 222.19, .036 INCH AT FS 280.00, AND .017 INCH AT FS 302.59. THE MINIMUM ALLOWABLE THICKNESS IN ACCORDANCE WITH THE LEAR 60 SRM CH 53-10-00 PG 102 IS .037 INCH. 2L72 4F RTA10CE 20040708001872004070800187SO 2004 7 8 C2XA04TY095 120040623A531514521721005 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713970 145146 DURING A SCHEDULED 3C INSPECTION THE FWD DIGITAL HAD SMALL AREAS OF CORROSION IN THE GALLEY. PERFORMED THE REPAIR IAW EC 5320-01074. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040708001882004070800188NM 2004 7 8 WRLA200425 120040608A2611 SCREEN DOUG MD11 MD11F 3023600NM SMOKE DETECTOR DIRTY A WRLAO OTHER N FALSE WARNING LDLANDING 1 SO11276WA 48632 FLIGHT 615 FROM PANC TO RCTP DURING THE LANDING AT RCTP A LEVEL 3 CABIN SMOKE ALERT WAS RECEIVED. THE CREW FOLLOWED THE VOL 1 CHECKLIST STANDARD EMERGENCY PROCEDURE, AFTER MORE INVESTIGATION CREW VERIFIED THAT THE ALERT WAS FALSE. AT RCTP MAINTENANCE CLEANED THE SMOKE DETECTOR SCREEN, OP'S CHECK GOOD, NO DEFECTS FOUND. 2L73 4F RTA22WE 20040708001912004070800191SO 2004 7 8 C2XA04BT066 120040616A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714991 145278 CREW REPORTED, ROW 12A EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040708001942004070800194NM 2004 7 8 QXEA200400433 120040613A521085210170101 BUSHING DHAV DHC8 DHC8202 2809007NM ZONE 800 DRY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09369PH13078 513 PSC - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. LUBED FORWARD BUSHING. CABIN DOOR FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001952004070800195NM 2004 7 8 QXEA200400435 120040612A30804100S00501 VALVE BOMBDRDHC8 DHC8401 1390041NM ZONE 300 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09411QX719 4055 SEA - ON FLIGHT NUMBER 2340, DE-ICE CAUTION LIGHT ILLUMINATED WHEN DE-ICE BOOT MODE SELECTED IN AUTO (FAST OR SLOW). RIGHT HAND INBOARD GREEN BOOT ON TAIL FAILS TO ILLUMINATE. RAN CHECKLIST AND NO DROP IN ISO WHEN USING A MANUAL SELECTION OF THE BOOTS, THE GREEN TAIL LIGHT STILL DOES NOT ILLUMINATE, BUT THERE IS NO DE-ICE PRESS CAUTION LIGHT. THE NR 5 DUAL DISTRIBUTION VALVE OPERATED INTERMITTENTLY. REMOVED AND REPLACED NR 5 DUAL DISTRIBUTION VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001962004070800196EA 2004 7 8 QXEA200400436 120040613A4920WE38007703 APU CNDAIRCL600 CL6002C10 1390015EA ZONE 300 INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09607QX5994 10024 PDX - WHILE ON THE GROUND AFTER ENGINE SHUTDOWN WITH APU ON, NOTICED ACRID SMELL IN CABIN. REMOVED AND REPLACED APU. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040708001972004070800197NM 2004 7 8 PCAA0406223 120040615A323183232013003 BELLCRANK DHAV DHC8 DHC8102 2809003NM NLG DOOR BROKEN A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13981HA 378 FLIGHT 4061 REPORTED DURING TAKEOFF AND UPON GEAR RETRACTION THE NOSE GEAR DOOR REMAINED OPEN. CREW ELECTED TO RETURN TO BUFFALO. AIRCRAFT WAS FERRIED FOR REPAIRS TO MIDDLETOWN. MAINTENANCE FOUND THE NOSE LANDING GEAR DOOR BELLCRANK TO BE BROKEN AT THE ATTACH POINT OF THE OVERCENTER LOCK. BELLCRANK WAS REPLACED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD, AIRCRAFT RETUNRED TO SERVICE. 2H72 4T RTA13NM 20040708001982004070800198NM 2004 7 8 WRLD200426 120040608A5522 SKIN DOUG MD11 MD11 3023602NM ELEVATOR DELAMINATED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING POSTFLIGHT INSPECTION FOR AIRCRAFT N278WA AT FNLU (LUANDA) MAINTENANCE FOUND THE RT OUTBOARD ELEVATOR DELAMINATED. MAINTENANCE CREW AT FNLU REMOVED AND REPLACED THE RT OUTBOARD ELEVATOR PER MD-11 MM 27-30-30. 2L73 4F RTA22WE 20040708002002004070800200SO 2004 7 8 4014 220040615A8520 CASE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO HARTZLHCJ3Y PHCJ3YR2 GL ENGINE DAMAGED E BSYAA UNSCHED LANDING RKJPARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07525GW TH557 823798R WHILE IN CRUISE FROM BHM TO PFN PILOT NOTICED OIL PRESSURE DROPPING, DECLARED AN EMERGENCY AND LANDED AT DHN. ON THE GROUND MAINT FOUND A HOLE IN CASE, LEFT SIDE CASE NR 3 ROD, CAUSE UNKNOWN AT THIS TIME. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20040708002032004070800203WP 2004 7 8 MWEA040096 120040615A55229937804501 DOUBLER DOUG DC9 DC982 3022082WP LT ELEVATOR LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LEFT ELEVATOR LOWER SKIN OUTBOARD AFT SKIN HAS AN AREA OF LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040708002042004070800204WP 2004 7 8 MWEA040095 120040615A5522591041279 DOUBLER DOUG DC9 DC982 3022082WP LT ELEVATOR LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LEFT ELEVATOR OUTBOARD CLOSEOUT COVER HAS LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040708002072004070800207NM 2004 7 8 QXEA200400444 120040613A33506138001 BATTERY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09539DS3768 4016 BLI - THE EMERGENCY LIGHTS WERE LEFT ON. ALL EIGHT EMERGENCY LIGHT POWER SUPPLY BATTERIES WERE DEAD. REPLACED ALL EIGHT EMERGENCY LIGHT POWER SUPPLY BATTERIES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708002092004070800209 2004 7 8 YENA200434 420040611A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ODOR A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15543JB2641 1823 PILOT CALLED MAINTENANCE CONTROL CENTER 25 MINUTES PRIOR TO ARRIVAL AT JFK WITH AN ELECTRIC SMELL IN THE CABIN AND WHEN LTV WAS SHUTOFF SMELL DISSIPATED. LOGBOOK ITEM STATES ELECTRICAL SMELL COMING FROM ROW NR 4. PERFORMED OPERATIONAL CHECK AS PER INFO NOTICE 2003-T050TR A, REMOVED AND REPLACED SEB AS PRECAUTIONARY AT 4B. PERFORMED OPERATIONAL CHECK IAW LTV MM 23-39-00. ALL OPS CHECK NORMAL. NO SMELL OF ELECTRICAL NOTED. ALL SCREENS SHOW NORMAL. 2L72 4F RTA28NM 20040709000082004070900008SO 2004 7 9 C2XA04SH376 120040619A33507287580503 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 SHV-DURINC CHECK THE NR 6 AISLE PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-08, THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000092004070900009SO 2004 7 9 C2XA04SH417 120040701A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729917 145414 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040709000102004070900010SO 2004 7 9 C2XA04SH418 120040702A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729917 145414 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCEMENT ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040709000112004070900011SO 2004 7 9 C2XA04SH420 120040703A531514522226003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 59-61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000122004070900012NM 2004 7 9 AALA20040703 120040703A3350S283T0143 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21682AA 25339 DFW - MID CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR MID CABIN OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040709000132004070900013NM 2004 7 9 AALA20040704 120040703A3350 CHARGER BOEING757 7572Q8 1384972NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21703TW 27620 DFW - EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS INOPERATVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS ON RIGHT HAND FIRST CLASS BAGGAGE BINS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040709000152004070900015EU 2004 7 9 AALA20040706 120040702A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217082A 643 MIA - ECONOMY CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR ECONOMY CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040709000162004070900016WP 2004 7 9 AALA20040707 120040704A3350 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21433AA 49451 SEA - EMERGENCY SEAT MOUNTED LIGHT FROM 20 AFT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLIES AT MID CABIN STATION 833R AND CONTROL MODULE AT 833R. REPLACED EMERGENCY LIGHT POWER SUPPLY AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040709000172004070900017WP 2004 7 9 AALA20040708 120040705A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170404 49315 ORD - CEILING EMERGENCY LIGHTS AT ROW 8-9 INOPERATIVE. REPLACED BATTERY PACK B1-505 FOR CEILING EMERGENCY LIGHTS AT ROW 8-9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000192004070900019WP 2004 7 9 AALA20040710 120040705A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21279AA 49295 PHX - EXIT SIGNS ABOVE AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY FOR EXIT SIGNS ABOVE OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000212004070900021NM 2004 7 9 AALA20040685 120040630A3350 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHTSDISLODGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21650AA 24608 DFW - EMERGENCY ESCAPE PATH LIGHT AT SEAT 32D INOPERATIVE. FOUND CONNECTOR PINS UNDER SEAT 32D DISLODGED. REINSTALLED CONNECTORS AT SEAT 32D FOR EMERGENCY ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040709000222004070900022NM 2004 7 9 AALA20040687 120040629A3350P4010049 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219413T 53188 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT IN AFT HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD AND AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040709000232004070900023WP 2004 7 9 AALA20040684 120040628A3246 SHIMMY DAMPENER DOUG DC9 DC982 3022082WP RT MLG FAILED A AALAO OTHER E VIBRATION/BUFFET LDLANDING 1 SW21251AA 49270 ORD - IMMEDIATELY AFTER TOUCHDOWN AIRCRAFT BEGAN SHAKING VIOLENTLY. DURING TAXI SHAKING CONTINUED AT ALL SPEEDS ABOVE A WALK. FOUND RIGHT HAND MAIN LANDING GEAR SHIMMY DAMPENER FAILED WITH DAMAGE TO TIRES AND MAIN LANDING GEAR. REPLACED UPPER AND LOWER TORQUE LINKS APEX BOLT AND SHIMMY DAMPENER BRAKE ROD BEAM LINK AND ROD. REPLACED FOUR HYDRAULIC LINES AND COUPLINGS. INSPECTED UPPER TRUNNION AREA AND SIDE BRACE WORK ACCOMPLISHED PER ESO 3221 CHAPTER 32-17-0-0 AND 32-17-01. INSTALLED BRAKES, WHEELS AND SPRAY DEFLECTOR. AIRCRAFT BEING EVALUATED FOR FURTHER STRUCTURAL DAMAGE. 2L72 4F A6WE 20040709000242004070900024NM 2004 7 9 AALA20040689 120040628A3350DD71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 RNO - RIGHT HAND AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND AFT EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040709000262004070900026WP 2004 7 9 AALA20040686 120040630A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21980TW 53630 SFO - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040709000302004070900030EU 2004 7 9 AALA20040698 120040625A5310 BEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW217076A 610 TUL - NUMBER FOUR GANTRY BEAM AT FRAME 52 IS CRACKED APPROXIMATELY .50 INCH LONG. AREA WAS MODIFIED PER ECO E1273AD TO ACCOMPLISH NDT INSPECTION. STOP DRILLED CRACK. HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACK TERMINATED IN STOP DRILL HOLE AREA. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH ESO 90595 DATED JUNE 25, 2004 REPAIR NUMBER 40 531500 3477. 2L72 4F RTA35EU 20040709000312004070900031EU 2004 7 9 AALA20040692 120040623A5330 SKIN AIRBUS300 A300B4605R 3930308EU RT WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 CORROSION ON LOWER RIGHT WING SKIN INSIDE SLAT TRACK SEVEN TRACK WELL. AREA OF CORROSION IS SEVEN INCHES BY FIVE INCHES AND LOCATED A STATION NUMBER 1260. REPAIRED CORROSION PER ESO 30595 DATED JUNE 22, 2004. 2L72 4F RTA35EU 20040709000332004070900033EU 2004 7 9 AALA20040691 120040621A5313 STRINGER AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 STRINGER 56L IS CORRODED JUST AFT OF FRAME 54. CORRODED AREA WAS 2 INCH BY 2 INCH. REPAIRED STRINGER 56L PER 51-71-10-0. 2L72 4F RTA35EU 20040709000362004070900036NM 2004 7 9 AALA20040701 120040610A5311 FAILSAFE BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 AFW - SECTION 43 FORWARD CARGO, INNER CHORD ANGLE OF FAILSAFE CHORD FORWARD CARGO DOOR HAS CORROSION REMOVAL BLENDOUTS ON THE LOWER SURFACE IN 2 LOCATIONS AT FASTENERS. STA 591 IS 1.5 INCH DIAGONAL WITH DEPTH OF .030 INCHES & STA 527.65 IS 1.2 INCHES DIAGONAL WITH DEPTH OF .021 INCH DEEP. CORROSION REMOVED, PERFORM EDDY CURRENT, & ROTOPEEN BLENDED AREA. REFINISH BLENDED AREA WITH ALODINE & 2 COATS OF PRIMER. INSTALLED FAILSAFE STRAP, FABRICATE REPAIR STRAPS. STRAP MUST EXTEND A MINIMUM OF .5 INCH BEYOND CENTER OF EACH FASTENER HOLE. FINISH STRAP WITH ALODINE & 2 COATS OF BMS1011 PRIMER. INSTALL A STRAP AT EACH BLENDED LOCATION. ADJUST GRIP LENGTH OF BOLTS TO ACCOMODATE REPAIR STRAP. 2L72 4F RTA1NM 20040709000372004070900037NM 2004 7 9 AALA20040702 120040617A5311 FRAME BOEING767 767323 1385205NM FUSELAGE CUT A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 AFW - WHILE ACCOMPLISHING C1945CB STEP E3 FRAME WAS CUT AT .30 INCH FROM UPPER FASTENER OF REMAINING FRAME, NOT .46 INCH AS ECO STATES. AREA WAS ONE INCH BY ONE INCH AT A DEPTH OF 1.3 INCHES. FILLED GAP WITH BMS595 SEALANT AND COMPLETE REPAIR PER ECO C1945 INSTRUCTIONS. 2L72 4F RTA1NM 20040709000382004070900038EU 2004 7 9 AALA20040694 120040623A5753 FLAP TRACK AIRBUS300 A300B4605R 3930308EU WING GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 TUL - FLAP TRACK NUMBER ONE LIFT GOUGED INSIDE AFT ATTACH POINT BARREL NUT HOLE. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH AND LOCATED AT STATION 3300. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004. 2L72 4F RTA35EU 20040709000412004070900041NM 2004 7 9 AALA20040676 120040624A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21952AA 30088 LAX - SEAT MOUNTED EMERGENCY LIGHT AT ROW 7D THROUGH 11D INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHT AT ROW 7D THROUGH 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040709000422004070900042WP 2004 7 9 AALA20040672 120040623A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21974TW 53624 DEN - FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040709000432004070900043NM 2004 7 9 AALA20040674 120040622A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21397AN 29604 DFW - SLIDE EMERGENCY LIGHTS AT LEFT FORWARD AND AFT WING AND LEFT AFT DOOR INOPERATIVE. REPLACED BATTERY PACK M738 FOR SLIDE EMERGENCY LIGHTS AT LEFT FORWARD AND AFT WING AND LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040709000442004070900044WP 2004 7 9 AALA20040675 120040624A3350 LIGHT DOUG DC9 DC982 3022082WP ROW 22D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 22D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000452004070900045EU 2004 7 9 AALA20040673 120040623A1420 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHTSDISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170054 461 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. RECONNECTED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040709000472004070900047NM 2004 7 9 SWAA041918 120040707A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 986.5, BL 0 TO RBL 18, CORRODED. REPAIRED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040709000492004070900049SO 2004 7 9 C2XA04SH421 120040705A532014529495003 SILL EMB 145 EMB145ER 3260211SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR CLEAT AT FRAME 73 STR 9R-11R WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR CLEAT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000502004070900050SO 2004 7 9 C2XA04SH422 120040703A532014525800015 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AT FRAME 48 TO 52. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000542004070900054SO 2004 7 9 C2XA04SH425 120040628A531514530635001 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 53-58. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000562004070900056SO 2004 7 9 C2XA04SH427 120040628A531514530643403 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000582004070900058SO 2004 7 9 C2XA04SH428 120040628A531514530633005 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 29-37. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000602004070900060SO 2004 7 9 C2XA04SH430 120040626A532014524131007 BRACKET EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000612004070900061SO 2004 7 9 C2XA04SH431 120040626A532014524131005 BRACKET EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000622004070900062SO 2004 7 9 C2XA04SH432 120040705A532014522226003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000632004070900063SO 2004 7 9 C2XA04SH405 120040702A531014525800010 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO FRAME 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000642004070900064SO 2004 7 9 C2XA04SH403 120040702A531514526437001 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 61 IN THE LAV. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000652004070900065SO 2004 7 9 C2XA04SH407 120040702A531014525181017 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED AT FRAME 68 AND STRINGERS 6R-7R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000662004070900066SO 2004 7 9 C2XA04SH404 120040702A532014520609005 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SVH - DURING C-CHECK THE RIGHT HAND FLOOR SILL WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000682004070900068SO 2004 7 9 C2XA04BT071 120040628A335020131A BATTERY PACK EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2712934 145019 CREW REPORTED, ODOR OF WIRE INSULATION BURNING IN COCKPIT AND FLIGHT ATTENDANT JUMPSEAT, ALONG WITH CABIN AND CABIN EMERGENCY PUSHBUTTONS ILLUMINATING. MAINTENANCE FOUND EMERGENCY BATTERY NR 2 NOT INSTALLED CORRECTLY. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY, POWER SUPPLY IAW EMB145 MM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040709000692004070900069SO 2004 7 9 C2XA04BT072 120040629A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 CREW REPORTED EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 5 EMERGENCY EXIT SIGN LIGHT INVERTER IAW EMB145XR AMM 33-50-11. OPS CHECKED GOOD. 2L72 4F RT 20040709000722004070900072SO 2004 7 9 C2XA04SH394 120040626A531514524188003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000742004070900074SO 2004 7 9 C2XA04SH391 120040626A531514530628001 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000752004070900075SO 2004 7 9 C2XA04SH396 120040627A531514522460015 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE AFT DIGITAL WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000772004070900077SO 2004 7 9 C2XA04SH395 120040626A531114522461011 DOUBLER EMB 145 EMB145ER 3260211SO FRAME CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE DOUBLER AT FRAME 20 WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000782004070900078SO 2004 7 9 C2XA04CL067 120040624A33507277120501 CIRCUIT BOARD EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED A C2XAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2713955 145075 BUF FLIGHT 2167, THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR NEAR THE GALLEY AND ALONG ROW 3 SEAT B&C. MAINTENANCE FOUND THE ELECTRICAL ODOR COMING FROM THE PSU AT ROW 3 B&C. THE CIRCUIT BOARD WAS REMOVED AND THE AIRCRAFT WAS RELEASED IAW MEL 25-60-02/4 AND 25-60-02/11. ON 6/25/04 THE CIRCUIT BOARD WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040709000802004070900080SO 2004 7 9 C2XA04SH397 120040627A541114576010001 RIB EMB 145 EMB145ER 3260211SO ENGINE COWL CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE NR 1 UPPER ENGINE COWLING FT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000812004070900081SO 2004 7 9 C2XA04IA077 120040626A3397W198820120 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2722909 145459 MKE - FLIGHT 2843, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT AN OVERHEAD BIN EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AFFECTED LIGHT ASSEMBLY, AND RESECURED WIRE W198-8201-20, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040709000822004070900082SO 2004 7 9 C2XA04IA078 120040626A32608005701 PROXIMITY SENSOR EMB 145 EMB145ER 3260211SO NLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27179281584 1584 145007 IAH - FLIGHT 2891 DURING CLIMBOUT OF LCH THE CREW REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040706001182004070600118NM 2004 7 6 04FDEA01705 120040612A5311 FRAME BOEING727 727200 138407ENM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25244FE 21647 AFT LWR CARGO COMPT FRAME 1010 UPPER FLANGE DENTED AT STR 26L. REPLACED FRAME IAW B727 SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20040706001212004070600121NM 2004 7 6 DLM90040552 120040614A291060060911 PRESSURE SWITCH DOUG MD90 MD9030 3023690NM LT WW INOPERATIVE A DALAH DEACTIVATE SYST/CIRCUITS O OTHER TXTAXI/GRND HDL 1 SO27911DA 53391 WHILE TAXIING SLOWLY ARMED T/O MODE OF AUTOBRAKES A/C IMMEDIATELY AND ABRUPTLY STOPPED. RECEIVED AUTOBRAKE FAIL MESSAGE ON EOAP. NORMAL BRAKING OPERATES FINE. FAULTS IBCV1 SOV. REPLACED SAME. 2L72 4F RTA6WE 20040706001232004070600123NM 2004 7 6 DL75K040554 120040614A21313964801 CONTROLLER BOEING757 757232 1384965NM LT A/C PACK MALFUNCTIONED A DALAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 SO27645DL 24216 RT CRUISE FL350 GOT CABIN ALT WARNING. CABIN CONTINUED TO CLIMB TO 12,500 FT BEFORE REVERSING. INITIATED DESCENT TO FL240. CABIN WILL NOT HOLD WITH LEFT THROTTLE AT OR NEAR IDLE BOTH DUCT PRESSURES APPEAR NORMAL (40-42 PSI) AT CRUISE FL280 CABIN ALT AT 280 = 4000 FT, NO RATE NOTED IE PRESS STEADY. FOUND LT PAC BITE MSG WOULD NOT ERASE. FOUND LT PAC CONTROLLER FAULTING LT PAC CONTROL VALVE. REMOVED AND REPLACED SAME PER MM, RAN PAC NOW CHECKS GOOD. RAN ENGINES PER PFHB PRESS CABIN TO 5 PSI DIFF PRESS, ALL CHECKS GOOD, NO MESSAGES. 2L72 4F RTA2NM 20040706001242004070600124NM 2004 7 6 DL73S040555 120040615A534365468305 FITTING BOEING737 737247 138448DNM MLG SIDE STRUT CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 CORROSION ON THE MLG SIDE STRUT ATTACH AT FUSELAGE STA 685 MLG FITTING. AREA REPAIRED IN ACCORDANCE WITH ERA 090842-14. 2L72 4F A16WE 20040706001272004070600127NM 2004 7 6 DL73S040558 120040615A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 CRACKS IN FUSELAGE SKIN AT STATION 380 BETWEEN S-17L AND 18L. AREA REPAIRED IAW ERA 090754-14. 2L72 4F A16WE 20040707000062004070700006NE 2004 7 7 235791 220040605A7261 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A1 30030NE LT ENG CHIP DET ILLUMINATED A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL17340SZ 340A004 504 ON TAKEOFF FLT 7944 CRW-IAD JUST AFTER WHEELS UP THE LEFT CHIP DETECTOR LIGHT ILLUMINATED. THE CAPTAIN FOLLOWED THE QRH AND RETURNED TO THE FIELD. 2L72 4T4 TRTA52EU E8NE 20040707000092004070700009CE 2004 7 7 DXTA200400322 120040612A326065430087 POSITION SWITCH CESSNA560 560XL 2076702CE NLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07699QS 5605199 AFTER TAKEOFF NOSE WHEEL LANDING GEAR GREEN LIGHT REMAIN ILLUMINATED, DID NOT EXTINGUISH AFTER GEAR WAS RECYCLED. REMAINED ON FOR THE DURATION OF FLIGHT, UPON LANDING GEAR CYCLED DOWN, ALL 3 GREEN LIGHTS CAME ON. JACKED AIRCRAFT, COMPLIED WITH GEAR SWING AND CONFIRMED SQUAWK, FOUND UPLOCK SWITCH INOP. REMOVED AND REPLACED NOSE GEAR SWITCH. ACCOMPLISHED GEAR SWING AND OPS CHECK GOOD. BLED HYDRAULIC SYSTEM AND DOWN JACKED AIRCRAFT, WORK DONE IAW CESSNA MM CHAPTER 32-31-14. 2L72 4F RTA22CE 20040707000102004070700010CE 2004 7 7 62040 120040606A5260 CABLE BEECH 1900 1900D 1154162CE AIRSTAIR DOOR OUT OF ADJUST A AMWAK NONE O OTHER ININSP/MAINT 1 CE07139ZV UE139 UPON FIRST FLIGHT OF THE DAY INITIAL WALK AROUND INSPECTION, CAPTAIN NOTICED PAX MAIN DOOR SLIGHTLY LOOSE WHEN FULLY CLOSED WITH INDICATOR FULLY IN VIEW. PAX NEVER BOARDED. AIRCRAFT DID NOT LEAVE GATE. RE-ADJUSTED UPPER, FWD AIRSTAIR DOOR CABLE, OPS CHECK NORMAL. 2L72 4T RTA24CE 20040707000212004070700021SO 2004 7 7 RAIA00405018 120040529A801232153580 START VALVE EMB 145 EMB145 3260210SO RT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03820HK5060 1309 145064 STL - RIGHT ENGINE NO ROTATION ON START. MAINTENANCE REMOVED AND REPLACED NR 2 AIR START VALVE. 2L72 4F RTT00011AT 20040707000302004070700030SO 2004 7 7 RAIA00406003 120040603A7714 WARNING SYSTEM EMB 145 EMB145LR 3260212SO RT ENGINE ACTIVATED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03819HK 145062 RT ENGINE INDICATED HIGH N2 SPEED. MAINTENANCE OPS CHECKED OK WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20040707000322004070700032SO 2004 7 7 RAIA00406005 120040603A2797 WIRE EMB 145 EMB145LR 3260212SO PITCH TRIM BROKEN A RAIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE03831HK 145232 MAIN PITCH TRIM INOP. MAINTENANCE REPAIRED BROKEN WIRE TO CAPTAIN'S TRIM SWITCH. 2L72 4T RTT00011AT 20040707000762004070700076EU 2004 7 7 RAIA00405033 120040525A79308582 PRESSURE SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE OIL DEFECTIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03566HK533 41084 XNA - LEFT ENGINE OIL PRESSURE WARNING INDICATION WITH OIL PRESSURE AT 50 PSI. MAINTENANCE DEFERRED LEFT ENGINE OIL PRESSURE WARNING SYSTEM. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING OIL PRESSURE SWITCH. 2L72 4T RTA41NM 20040707000802004070700080NM 2004 7 7 AWXA200400635 120040613A2560P4010021 BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040707000822004070700082NM 2004 7 7 AWXA200400637 120040606A5320654587547 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN WEB AT R-1 DOOR THRESHOLD BS 295.5, STR 17 RT. MAINTENANCE REMOVED CRACKED THRESHOLD WEB AT R-1 DOOR FROM BS 295.5 TO BS 342, STR 17 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2L72 4F RTA16WE 20040707000832004070700083NM 2004 7 7 AWXA200400638 120040603A53206937402 SUPPORT ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND IN SUPPORT ANGLE AT BS 294.5, STR 17 RT. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AT BS 294.5, STR 17 RT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-37402; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 5 & 8. 2L72 4F RTA16WE 20040707000932004070700093EU 2004 7 7 RAIA00406006 120040602A2910 LINE JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03550HK 41039 STL - HYD PRESSURE AND QUANTITY ZERO. MAINTENANCE REPAIRED CHAFED HYDRAULIC PRESSURE LINE. 2L72 4T RTA41NM 20040708000052004070800005NM 2004 7 8 C8GA20040006 120040613A143066129681 BOLT BOEING727 7272A1 138407FNM DOWNLOCK MISLOCATED A C8GAO OTHER W INADEQUATE Q C ININSP/MAINT 1 SO15286SC13318 21601 ON WALK AROUND IN KDEN, FOUND THE LT MAIN GEAR BOLT DOWNLOCK LINK PIVOT IMPROPERLY INSTALLED AS PER BOEING IPC 32-10-01-04. A SPECIAL MAINTENANCE FERRY FLIGHT WAS ISSUED ON 6-14-2004 FROM KDEN TO KTOL. PRIOR TO FLIGHT, A VISUAL INSPECTION WAS PERFORMED IN THE LEFT HAND MAIN LANDING GEAR DOWNLOCK LINK ASSEMBLY. ON JUNE 15, 2004 THE AIRCRAFT WAS FERRIED FROM KDEN TO KTOL AND LANDED WITHOUT INCIDENT. UPON ARRIVAL IN KTOL, THE AIRCRAFT WAS INSPECTED AND CLEARED BY REPOSITIONING THE LT MAIN GEAR DOWN LOCK BOLT TO ITS ORIGINAL CONFIGURATION IAW BOEING IPC 32-10-01-04 AND B727 MM 32-13-01 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20040708000062004070800006EU 2004 7 8 HAEA00148 120040616A3260 SQUAT SWITCH AMD FALC20FALCON 2720302EU MLG STICKING E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05240TW1472814728 40 AIRCRAFT DEPARTED FWA, LANDING GEAR WOULD NOT RETRACT. GEAR DOWN 3 GREENS. RETURNED FWA, LANDING UNEVENTFUL. 2L72 4F A7EU 20040708000112004070800011EU 2004 7 8 CX7A194J0432 120040611A33206500006 SOCKET SAAB SF340 340B 7860101EU CABIN LIGHTS BURNED A CX7AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL03301CE 340B191 CREW SMELLED SMOKE UPON BOARDING AIRCRAFT IN MDW. 2L72 4T RTA52EU 20040708000162004070800016EU 2004 7 8 MALA040437 120040604A21507769106 ACM SAAB SF340 340B 7860101EU CABIN COOLING ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL15364PX 340B262 BURING WIRE ODOR WAS PRESENT DURING DESCENT. SUPP A/C ON, BOTH BLEEDS WERE ON, NO CAUTION OR WARNING INDICATIONS PRESENT. ODOR WAS STRONGEST IN COCKPIT AND DISSIPATED AFT OF F/A JUMPSEAT. MAINTENANCE DETERMINED ODOR TO BE DUE TO RT ACM BEING CEASED. REMOVED AND REPLACED ACM P/N 776910-6, S/N OFF 880342, S/N ON 8614121, IAW JOB CARD 215181, OPS CHECK GOOD. 2L72 4T RTA52EU 20040708000192004070800019NM 2004 7 8 AWXA200400655 120040524A57536546435275 WEDGE BOEING737 7373G7 1384595NM LT WING TE FLAPSDEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28302AW 24009 MCN - MAJOR REPAIR - DURING C-15 CHECK FOUND A DISBOND AREA ON THE LT WING OUTBOARD AFT FLAP AT LOWER INBOARD END WBL 230.68 TO WBL 235.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING OUTBOARD AFT FLAP AT LOWER INBOARD END; FABRICATED A CORE FILLER AND REPAIR DOUBLERS; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 21 PG 84D-84F. 2L72 4F RTA16WE 20040708000232004070800023 2004 7 8 AWXA200400659 420040616A34426225132120 RADAR BOEING757 7572G7 1384963NM ZONE 113 FROZEN A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28908AW46210274 24233 ON CLIMBOUT OF PHX EN ROUTE FOR LAS BOTH THE CAPTAINS AND FIRST OFFICERS WEATHER RADAR LOCKED IN TEST MODE, SWITCHING SYMBOL GENERATORS AND CYCLING TERRAIN SWITCHES, NO HELP. DUE TO WEATHER EN ROUTE, TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR RECEIVER TRANSMITTER IAW BMM 34-43-01, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF WEATHER RADAR RECEIVER TRANSMITTER S/N 3652 WAS NO FAULT FOUND, PERFORMED A VISUAL INSPECTION OF UNIT, RETESTED, RETURNED TO SERVICE IAW CMM 34-45-21, REV. 009. 2L72 4F RTA2NM 20040708000312004070800031NM 2004 7 8 DL73S040536 120040609A5330654577644 SKIN BOEING737 737247 138448DNM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 FUSELAGE SKIN FS 727, S16L - BL 0 FILLET PANEL PERIMETER + FS 770-908, S20L LAP SPLICE REPAIR OF SCRIBE MARKS, TOOLING DAMAGE BELOW THE LAP SPLICE ALONG S20L BETWEEN FS 727 AND FS 908 AND ALONG THE EDGE OF THE FILLET PANEL AFT OF THE WING. REPAIR DOUBLERS WERE INSTALLED ERA 090669-14, REV INITIAL. 2L72 4F A16WE 20040708000342004070800034WP 2004 7 8 DHL2004806001 120040612A3242 LINE DOUG DC8 DC873F 302199FWP ANTI SKID SYS LOOSE A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01806DH 46002 PARKING BRAKE WILL NOT HOLD PRESSURE WHEN BRAKES ARE SET. FOUND LINE SEEPING ON OUTBOARD ANTI SKID CONTROL VALVE. TIGHTENED LINE, LEAK CHECK GOOD PER 20-13-0, BRAKES OPS CHECK GOOD PER MM 32-40-0. NO COMPONENT REMOVAL. 2L74 4F RT4A25 20040708000352004070800035WP 2004 7 8 DHL2004807007 120040612A5210 HANDLE DOUG DC8 DC873F 302199FWP PAX DOOR LOOSE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01807DH 45990 LEFT FWD ENTRY DOOR INTERIOR DOOR HANDLE HAS PLAY. REMOVED HANDLE & TIGHTENED HARDWARE, REINSTALLED HANDLE, OPS CHECK NORMAL MM 52-14-1. NO PARTS REPLACED. 2L74 4F RT4A25 20040708000402004070800040NM 2004 7 8 DL73S040539 120040609A53306545768295 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27244WA 23518 FUSELAGE SKIN FS 360 - FS 440 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE. REPAIR DOUBLERS INSTALLED ER/A 090445-14, REVISION INITIAL. 2L72 4F A16WE 20040708000612004070800061NM 2004 7 8 DL75K040524 120040610A2121731376 FAN BOEING757 757232 1384965NM EQUIP COOLING FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27685DA 0543 27588 A/C DIVERTED DUE TO SMOKE IN CABIN. REPLACED EQUIPMENT COOLING FAN. 2L72 4F RTA2NM 20040708000732004070800073NM 2004 7 8 UPS04242575 120040601A7830 FAIRING BOEING727 72725C 138400HNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER O/B FAIRING IS CRACKED AT MID AFT END. REPLACED FAIRING IAW MM 78-30-43. 2L73 4F A3WE 20040708000772004070800077NM 2004 7 8 UPS04242584 120040531A5754651622718A SKIN BOEING727 72725C 138400HNM NR 6 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 INSPECTION TYPE: C, NR 6 L/E FLAP CRACKED I/B OF LANDING LIGHT & JUST ABOVE BULLNOSE. FLAP REPLACED IAW MM 27-81-01. 2L73 4F A3WE 20040708000802004070800080CE 2004 7 8 00137 120040506A1420 CONNECTOR LEAR 24 24 5170302CE THRUST REVERSER FAULTY E HAEAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SW05333TW1571015710 168 PILOT REPORTED RIGHT THRUST REVERSER UNSAFE LIGHT ILLUMINATED DURING DESCENT. PER CHECKLIST ENGINE SHUT DOWN AND EXECUTED AN UNEVENTFUL LANDING IN LRD. REPLACED CONNECTOR, OPS CHECKED GOOD. 2L72 4J A10CE 20040708000872004070800087NM 2004 7 8 SWAA041875 120040702A335007912 COVER BOEING737 7377H4 1384404NM ROW 1 ABC MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29412WN 29818 EEPLS LIGHT COVER MISSING AT ROW 1 ABC. REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040708000942004070800094NM 2004 7 8 SWAA041879 120040702A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040708001242004070800124SO 2004 7 8 C2XA04TY091 120040617A33501317 BULB EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714508 145220 DURING A SEVICE/ROUTINE OF A/C THE EMERGENCY LIGHT BULB WAS FOUND BLOWN OVERHEAD LEFT EMERGENCY DOOR. REPLACED BULB AND OPS CHECK WAS GOOD. A/C WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20040708001262004070800126NM 2004 7 8 SWAA041900 120040706A335065C273672 BRACKET BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND ALL FOUR OVERWING EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY MOUNTING BRACKETS, CRACKED. REMOVED AND REPLACED ALL FOUR MOUNTING BRACKETS PER MM. 2L72 4F RTA16WE 20040708001342004070800134NM 2004 7 8 SWAA041903 120040706A53156545810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 328 AND BS 344, RBL 10 TO RBL 59, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTIONS PER SRM. 2L72 4F RTA16WE 20040708001452004070800145NM 2004 7 8 SCNA04009 120040612A335011583315 LIGHT BOEING737 7378Q8 13844BXNM EMERGENCY EXIT INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15801SY 30332 FWD RIGHT EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM 33-21-00, OPS CHECKS GOOD. 2L72 4F RTA16WE 20040708001492004070800149WP 2004 7 8 MWEA040100 120040616A7711LG80E1 TRANSMITTER DOUG DC9 DC982 3022082WP LEFT ENGINE INOPERATIVE A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31809ME 48071 LEFT EMERGENCY POWER RELAY INDICATOR LOW FLAGGED. REMOVED AND REPLACED EMERGENCY TRANSMITTER. 2L72 4F A6WE 20040708001692004070800169SO 2004 7 8 C2XA04SH373 120040618A532014524131009 BRACKET EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 SHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001792004070800179EU 2004 7 8 U30A200400005 120040521A1420EO390DD01S2A12B CONNECTOR AIRBUS320 A320214 3930316EU ELEVATOR CONTROLLOOSE A U30AO OTHER E VIBRATION/BUFFET CRCRUISE 1 EA17268AV19 19 2175 AFTER FERRY FLIGHT (LFBO-BIKF-KPHL), THE FLIGHT CREW REPORTED THAT THE AIRCRAFT EXPERIENCED MINOR PITCH CHANGES & VIBRATION DURING THE FLIGHT. MAINTENANCE REPLACED THE NR 2 ELAC (ELEVATOR AILERON COMPUTER) AND STILL RECEIVED A F/CTL ELAC 2 PITCH FAULT. MAINTENANCE ALSO REPLACED THE ELEVATOR SERVO CONTROL ACTUATOR VALVE AND FAULT WAS STILL INTERMITTANT. FURTHER TROUBLESHOOTING IDENTIFIED THE SOURCE OF THE DIFFICULTY, WHICH WAS A LOOSE SCREW (IMPROPERLY SECURED) ON CONNECTOR 24VC, LOCATED IN 80 VU. AFTER INSPECTING & RESECURING THE CONNECTOR AND OPERATIONAL CHECKS, NO FURTHER FAULTS WERE DETECTED. A MAINTENANCE ACCEPTANCE FLIGHT WAS ACCOMPLISHED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA28NM 20040708001932004070800193NM 2004 7 8 QXEA200400434 120040609A521085217002003 MECHANISM BOMBDRDHC8 DHC8401 1390041NM AFT PAX DOOR DIRTY A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX5868 4060 BOI - ON FLIGHT NUMBER 2302, REAR AIRSTAIR DOOR WILL NOT OPEN OR CLOSE. REMOVED OBSTRUCTION, CLEANED AND LUBED AIRSTAIR DOOR. DOOR FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708002012004070800201SO 2004 7 8 C2XA04SH384 120040622A531514525381003 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000182004070900018NM 2004 7 9 AALA20040709 120040705A3350S283W6032 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21902AN 29504 BOS - SEAT MOUNTED EMERGENCY LIGHTS FROM 7D THROUGH 11D INOPERATIVE. REPLACED FLOOR MOUNTED BATTERY PACK FORWARD OF SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040709000282004070900028EU 2004 7 9 AALA20040690 120040701A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW211409B 11367 ORD - EMERGENCY LIGHTS AT EXTERIOR RIGHT AND LEFT HAND OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT EXTERIOR RIGHT AND LEFT HAND OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040709000462004070900046WP 2004 7 9 AALA20040677 120040624A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 9D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21224AA 49174 DFW - EMERGENCY ESCAPE PATH LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000572004070900057SO 2004 7 9 C2XA04SH419 120040701A335020131A BATTERY EMB 145 EMB145 3260210SO EMERGENCY LIGHTSDISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW271396911165743 145141 SHV - DURING ROUTINE MAINTENANCE THE AISLE PATH LIGHTS 1 THRU 3 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY IAW EMB 145 SRM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000732004070900073SO 2004 7 9 C2XA04SH392 120040626A531514530628001 FLOORBEAM EMB 145 EMB145 3260210SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24 TO 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000762004070900076SO 2004 7 9 C2XA04SH390 120040626A531514525480003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000792004070900079SO 2004 7 9 CX2A04RI003 120040618A2560PR18 LAMP EMB 145 EMB145LR 3260212SO FLASHLIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716976 145171 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND CAPTAINS EMERGENCY FLASHLIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BULB. OPERATIONALLY CHECKED SUCCESSFULLY. 2L72 4T RTT00011AT 20040709000832004070900083SO 2004 7 9 C2XA04CL021 120040312A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716541 145542 CLE FLIGHT 2846, THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT ARM. THE CREW RESET THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040709001062004070900106SO 2004 7 9 C2XA04TY106 120040701A531514521700003 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION THE LEFT INBD FLOOR SUPPORT WAS FOUND CORRODED AT BOTTOM OF RAMP IN GALLEY. MAINT CUT OUT DAMAGE AND FAB A NEW REPAIR FOR THE EFFECTED AREA AND INSTALL NEW REPAIR PART IAW EMB 135/145 SRM 53-21-10; 53-21-03 AND 51-40-06 ALSO CPM 51-21-04; 05; 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040709001072004070900107SO 2004 7 9 C2XA04TY107 120040701A532014526435401 BRACKET EMB 145 EMB145 3260210SO SINK DRAIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE SINK DRAIN BRACKETS. MAINT REMOVED THE SINK BRACKETS, FAB A NEW PART, ALODINED, PRIMED AND PAINTED AND INSTALL THE NEW BRACKET IAW EMB 13/145 SRM 51-40-02; 51-30-03; 51-21-03; 04; 05 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040712000012004071200001SO 2004 7 12 C2XA04TY102 120040701A532014524131009 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION THE PAX DOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE DOOR SILL IAW EMB 135/145 SRM 51-40-02; 03 AND EMB CPM51-21-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040712000022004071200002SO 2004 7 12 C2XA04TY104 120040701A531514526437001 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION, CORROSION WAS FOUND ON THE RIGHT LAV FLOORBEAM TOP CAP IN SEVERAL PLACES. MAINT REMOVED AND REPLACED THE RIGHT TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040712000032004071200003SO 2004 7 12 C2XA04TY103 120040701A532014524945003 FLOOR SUPPORT EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON LEFT SIDE LAV FLANGE. MAINT REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040712000042004071200004SO 2004 7 12 C2XA04TY108 120040701A2722PE64042H401603 BUSHING EMB 145 EMB145 3260210SO RUDDER CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION MAINT FOUND CORRODED BUSHING ON ALL RUDDER 2 HINGE POINTS. MAINT REMOVED AND REPLACED ALL OF THE HINGE POINT BUSHINGS IAW EMB 20-10-08. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040712000052004071200005SO 2004 7 12 C2XA04CL018 120040307A2711 TRIM SYSTEM EMB 145 EMB145LR 3260212SO ROLL TRIM MALFUNCTIONED A C2XAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW2712996 145296 IAH FLIGHT 2390 CREW REPORTED, ROLL TRIM RUN-AWAY AFTER TAKEOFF FROM IAH. CREW FOLLOWED QRH AND RESET CIRCUIT BREAKER FOR AILERON TRIM. SYSTEM OPS CHECKED GOOD. CREW CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM WITH NO DEFECTS FOUND. 2L72 4T RTT00011AT 20040712000072004071200007SO 2004 7 12 C2XA04TY105 120040701A491012010732001 FRAME EMB 145 EMB145 3260210SO APU FIREWALL GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED 3C INSPECTION THE BOTTOM OF THE APU FIREWALL HAD A GOUGE. MAINT FOUND THE GOUGES TO BE ON FR 81, BLENDED DYE PEEN GOUGE AREA, REMOVED RIVETS, FAB DOUBLER AND INSTALL IAW EC 5330-01352. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040712000082004071200008NM 2004 7 12 SWAA041920 120040707A57536546434369 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040712000092004071200009NM 2004 7 12 SWAA041921 120040707A57536546431279 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FORE FLAP DELAMINATED. R & R LT OUTBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20040712000102004071200010NE 2004 7 12 USA2004F00057 220040531A7261 ENGINE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RIGHT LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19677UW 0380 THIS FLIGHT WAS A VERIFICATIONS FLIGHT FOR RT ENGINE OIL LOSS. CREW NOTED THAT THE RT ENGINE WAS AGAIN LOOSING OIL. FLIGHT DIVERTED. AFTER THE PREVIOUS FLIGHT, EIGHT QUARTS OF OIL HAD BEEN ADDED TO THE ENGINE. MAINTENANCE PERFORMED TSM TASK 79-00-00-810-813 AND COMPLETED THE NR BEARING COMPARTMENT BREATHER CHECK. NO DISCREPANCIES WERE FOUND. THE ENGINE WAS OPERATED FOR APPROXIMATELY FORTH-FIVE MINUTES WITH NO OIL LOSS. THE AIRCRAFT WAS RELEASED FOR THIS FLIGHT. MAINTENANCE REPLACED THE DEOILER DRIVE SEAL. ENGINE CONTINUED TO LOSE OIL. THE RT ENGINE WAS REPLACED. 2L72 4F4 FRTA46NM 20040712000112004071200011EU 2004 7 12 USA2004F00058 120040529A3350 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHTSINOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19757UW 1342 THE EMERGENCY LIGHTS FAILED THE TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. SYSTEM CHECKS OK. 2L72 4F4 FRTA28NM E2GL 20040712000122004071200012CE 2004 7 12 AJZ2004F00000 120040410A3297 WIRE BEECH 99 C99 1154006CE PWA PT6 PT6A36 52043NE MOTOR LOOSE E AJZAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP19206AV U206 PILOT REPORTED WHEN LANDING GEAR SELECTED TO EXTEND THE CIRCUIT BREAKER POPPED. PERFORMED FLYBY AND CONFIRMED GEAR NOT DOWN. EXTENDED GEAR MANUALLY AND LANDED WITHOUT FURTHER INCIDENT. REPAIRED WIRING ON THE GEAR MOTOR. GEAR SWING CHECK GOOD. AIRCRAFT WAS TEST FLOWN AND APPROBED FOR RETURN TO SERVICE. 1L72 3T4 T A14CE E4EA 20040712000132004071200013NM 2004 7 12 UIEA200400108 120040602A3610 PRECOOLER BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 (D) CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 3 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE, EXPOSED WINDOW STRAP SURFACE, ALONG WITH FASTENER HOLES, WERE HFEC INSPECTED TO ENSURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO 254. RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON NR 3 STIFFENER. ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2L74 4F4 F A20WE E23EA 20040712000152004071200015GL 2004 7 12 PNR2004F00002 120040519A5302281123011CS DOUBLER ENSTRMF28 280C 3300505GL LYC O360 HIO360* 41514EA TAILBOOM CRACKED D PNRGO OTHER O OTHER NRNOT REPORTED 1 NM09646H 2053 1099 BULKHEAD DOUBLER UNDER NR 3 TAILROTOR DRIVESHAFT PILLOW BLOCK FOUND CRACKED. CRACKS WERE PROPAGATING FROM THE RADIUS AREA ON BOTH UPPER TABS WERE THE NUT PLATES ARE RIVETED ON. BOTH NUT PLATES HAD PREVIOUSLY BEEN ROUNDED IN THE RADIUS AREA TO REDUCE THE CHANCES OF CRACKING. IT IS POSSIBLE THAT THE OUTSIDE RADIUS ON THE DOUBLER IS TOO LARGE TO FIT IN THE INSIDE RADIUS OF THE BULKHEAD, CREATING AN AREA BETWEEN THE TWO PIECES THAT IS COMPRESSED WHEN THE BOLT IS TIGHTENED INTO THE NUT PLATE AND THERE BY CAUSING THE DOUBLER TO CRACK. 1G71 3O3 O H1CE 1E10 20040712000212004071200021EU 2004 7 12 USA2004F00059 120040603A335032142410 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAULTY A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19721UW3895 1095 THE AFT LEFT EMERGENCY POWER SUPPLY UNIT FAILED TESTING. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E2GL 20040712000242004071200024CE 2004 7 12 ML22004F00000 120040615A2400 DIODE BEECH 300 300BEECH 1152930CE POWER RELAY WRONG PART B ML2RO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL11455SC FL384 DURING THE FIRST PHASE 1 INSPECTION BEING CONDUCTED, NO EXTERNAL POWER WAS ABLE TO BE APPLIED TO THE AIRCRAFT. TROUBLESHOOTING THE EXTERNAL POWER SYSTEM REVEALED THAT A ZENER DIODE HAD BEEN INSTALLED ON THE A124 EXTERNAL POWER RELAY AT THE FACTORY. THIS CREATED AN OVERCURRENT CONDITION, WHICH WAS BLOWING THE A260 POWER CONTROL CIRCUIT BOARD 3 OF THESE BOARDS HAD BEEN BLOWN BEFORE THIS DIODE WAS FOUND. NO REFERENCE TO THIS DIODE WAS FOUND IN THE WIRING DIAGRAMS. RAC TECHNICAL SUPPORT WAS NOTIFIED AND THY CONFIRMED THAT THE DIODE WAS NOT SUPPOSED TO BE INSTALLED ON THIS RELAY. THE AIRCRAFT WAS RETURNED TO THE ORIGINAL PRINT CONDITION AND RETURNED TO SERVICE. 2L72 4T A24CE 20040712000252004071200025NE 2004 7 12 ALG2004F00033 120040610A261130231R7B SMOKE DETECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL CARGO BAY WILL NOT TEST E ALGAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW03522AL 760236 CAE890100S DURING RUN UP, FIRE DETECTOR IN AFT BAGGAGE COMPARTMENT LIGHT FAILED TO COME ON DURING TEST. MAINTENANCE CARRIED FORWARD TO MCOD, PART IS ON ORDER AND IT IS A 10 MEL ITEM. A FOLLOW UP REPORT WILL BE TURNED IN WHEN THE PART IS CHANGED AND OPERATIONAL CHECK IS COMPLETE. 1G72 3U3 U H1NE E1GL 20040712000342004071200034SW 2004 7 12 FTU2004F00004 120040616A53133107765 LONGERON GULSTM690TP 690C 7630517SW GARRTTTPE331TPE3315 01514WP FUSELAGE CRACKED B FTURK NONE O OTHER ININSP/MAINT 1 NE05840JC7744 11643 WHILE COMPLYING WITH SB 187, ANTENNA INSPECTION AND MODIFICATION PART 1, THE LT FS 223.98 UPPER FUSELAGE FRAME CHANNEL RETURN FLANGE AT THE LT NR 1 LONGERON INTERSECTION WAS FOUND CRACKED. THE DAMAGED FRAME SECTION IS COMMON TO THE NR 1 LONGERON AND IS SHIMMED AND ATTACHED AT THAT POINT BY ONE AN4704 RIVET. THE UPPER FLANGE ON THE FRAME HAD COMPLETELY BROKEN AWAY. IN ADDITION, THE NR 1 LONGERON HAD CRACKED ALONG THE LOWER BEND DIAGONALLY 2 INCHES FORE AND AFT OF THE ATTACHMENT POINT TO THE FRAME AT FU. ST 223.98. WITH AN ANTENNA BEING MOUNTED TO FUSELAGE IN THAT AREA APPARENTLY IT WAS APPLYING STRESS ON THE STRUCTURE. COMPLETION OF SB MOD PROVIDED THE ADDITIONAL SUPPORT FOR ANTENNA INSTALLATION. 1H72 3T4 T 2A4 E4WE 20040712000352004071200035NE 2004 7 12 ALG2004F00034 120040615A1420 CONNECTOR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 2 SERVO DIRTY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03917QS 760217 AFTER TAKEOFF AND ENTERING CRUISE FLIGHT THE NR 2 SERVO SYSTEM CAUTION LIGHT ILLUMINATED, AFTER UTILIZING EMERGENCY CHECKLIST WAS UNABLE TO EXTINGUISH LIGHT, LANDED AND REFERRED TO MAINTENANCE. MAINTENANCE CLEANED CONNECTORS ON THE NR 2 HYDRAULIC MODULE NO FURTHER DEFECTS. 1G72 3U3 U H1NE E1GL 20040712000372004071200037 2004 7 12 USA2004F00065 420040604A2565 STRAP AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19124US 1314 THE EMERGENCY ESCAPE SLIDE/RAFT GIRT BAR RELEASE STRAP ON THE LT REAR ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2L72 4F4 FRTA28NM E2GL 20040712000382004071200038EA 2004 7 12 XGK2004F00000 220040708A7414 SHAFT PIPER PA28 PA28181 7102807SO LYC O360 O360A4A 41514EA LT ROTOR SHEARED E XGKAO OTHER O OTHER NRNOT REPORTED 1 WP2538850 00100373 287790599 L2738436A COMPLAINT OF EXCESSIVE MAG DROP. FIELD REPAIR FOUND TIMING 5 DEGREES LATE, RESET MAG TIMING AND FERRY AIRCRAFT TO BASE FOR INSPECTION. REMOVED MAGNETO AND FOUND NO PROBLEMS WITH INTERNAL TIMING. REINSTALLED, TIMED MAGNETO AND MARKED POSITION WITH TORQUE SEAL. TEN HOURS LATER AFTER COMPLETION OF FLIGHT , FOUND 200 RPM MAG DROP ON RT MAG. FIELD REPAIR FOUND MAG TIMING TEN DEGREES LATE, RE ADJUSTED AND FERRIED AIRCRAFT TO BASE. REMOVED MAG AND DISASSEMBLED. FOUND ROTOR SHAFT SHEARED BELOW MAGNET. REPLACED MAGNETO. 388 HOURS PRIOR TO THIS FAILURE THE LT MAGNETO WAS REPLACED AFTER FAILING 45 MINUTES AFTER 500 HOUR INSPECTION. NO CAUSE WAS FOUND, TT ON MAG WAS 1000 HOURS. (WP25200406593) 1L71 3O3 O 2A13 E286 20040712000392004071200039CE 2004 7 12 RSH2004F00000 120040708A321051411035 BARREL CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO TRUNNION CRACKED E RSHAK NONE O OTHER ININSP/MAINT 1 SO21220RS 402C0220 DURING ROUTINE INSPECTION OF LANDING GEAR A CRACK WAS FOUND ON LT LANDING GEAR ANCHOR LUG UPPER TORQUE LINK AND TRUNION ASSY. 1L72 3O3 O A7CE E8CE 20040712000482004071200048 2004 7 12 USA2004F00069 420040524A23106225272001 TRANSCEIVER BOEING767 7672B7 1385107NM GE CF6 CF680 30025NE HF SYSTEM OVERHEATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19653US30637 24894 HF NR 2 RADIO TAKES EXCESSIVELY LONG TO CHANNELIZE AND WILL NOT TRANSMIT. ELECTRICAL SMELL NOTED DURING CHANELIZATION PROCESS, BUT DISIPATED AFTER HF WAS TUNED. MAINTENANCE INSPECTED HF RELATED WIRING AND CONNECTION AND COULD NOT FIND A FAULT. THE HF NR 2 TRANSCEIVER AND BOTH CONTROL PANELS WERE REPLACED AS A PRECAUTION. 2L72 4F4 FRTA1NM E13NE 20040712000492004071200049SO 2004 7 12 SIMA200417209 120040617A532014522178005 CHANNEL EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL FUSELAGE WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21622AE 145108 DURING MBV INSPECTION THE SERVICE DOOR SILL BETWEEN FRAMES 20 AND 22 RT SIDE WAS FOUND CORRODED. REMOVED AND REPLACED THE CHANNEL IAW MFG SRM. 2L72 4T4 FRTT00011ATTE6CH 20040712000522004071200052NM 2004 7 12 USA2004F00078 120040605A2730 CONTROL SYSTEM BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE ELEVATOR MALFUNCTIONED A USAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA19563AU 23551 ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING, NOT AS MUCH EFFORT WAS REQUIRED. AIRCRAFT WAS FOUND IN SAFE CONDITION FOR MAINTENANCE FERRY FLIGHT. FERRY FLIGHT CREW REPORTED FLIGHT WAS NOT BAD ON TAKEOFF BUT THAT THERE WAS A DEFINITE PROBLEM ON LANDING. JUST AFTER FLARE, WENT TO PUSH OVER NOSE, FELT LIKE MECHANICAL BINDING. PUSHED HARDER AND IT RELEASED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA16WE E2GL 20040712000542004071200054SO 2004 7 12 SIMA200417002 120040617A27503631601 FCU EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL AVIONICS BAY INOPERATIVE A SIMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW21639AE 145182 CREW A FLAP FAIL MESSAGE WHEN FLAPS WERE RETRACTED AFTER TAKEOFF. FLAPS REMAINED AT 9 DEGREES. FOLLOWED AOM PROCEDURES AND LANDED WITH FLAPS AT 9 DEGREES AND OVERWEIGHT AT 42,800 AND 300 FPM. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040712000562004071200056SO 2004 7 12 SIMA200415803 120040603A27303621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO RROYCEDART DART* NE HORIZONTAL STAB INOPERATIVE A SIMAO OTHER O OTHER DEDESCENT 1 SW21833AE 145629 DURING DESCENT CREW REPORTED PITCH .5 INOP MESSAGE. MESSAGE WENT OUT AFTER 10 SECONDS. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW MFG MM. OPERATIONAL CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. ETN EB WAS COMPLIED WITH. (SW21200407369) 2L72 4F4 TRTT00011AT 20040712000572004071200057SO 2004 7 12 SIMA200416202 120040608A2750 CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL TE FLAPS MALFUNCTIONED A SIMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW21657AE 145744 DURING APPROACH CREW REPORTED FLAP FAIL AND SPS ADVANCE CAUTION MESSAGES ON EICAS. RESETING BREAKERS DID NOT HELP. MAINTENANCE RESET FLAP ELECTRIC CONTROL UNIT IAW MM. INDICATION RETURNED TO NORMAL AND ALL EICAS MESSAGES WERE CLEARED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040712000612004071200061NM 2004 7 12 BJNA040601A 120040605A33506104789 BATTERY BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 DURING A MAINTENANCE WALK AROUND CHECK, THE RT SIDE OVER-WING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT HAND OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. 2L72 4F4 FRTA16WE E2EA 20040712000652004071200065NM 2004 7 12 USA2004F00071 120040608A3397 WIRE BOEING737 737301 1384611NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19563AU 23551 MAINTNANCE REPORTED THE EMERGENCY LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPLACED A BROKEN WIRE. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E17NE 20040712000662004071200066EA 2004 7 12 REX2004F00000 120040620A2612 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO FIRE ILLUMINATED A REXAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW218598B5423 7598 FALSE CARGO SMOKE WARNING ON FINAL. EMERGENCY DECLARED QRH FOLLOWED EXTINGUISHERS DISCHARGED, UNEVENTFUL LANDING. CARGO FIRE EXTINGUISHERS REPLACED, OPERATIONAL TEST PERFORMED IAW AMM OF CARGO DETECTION SYSTEM WITH NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20040712000672004071200067EU 2004 7 12 MALA040470 120040620A2150 MOTOR SAAB SF340 340B 7860101EU COMPRESSOR SMOKE A MALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15450XJ 340B450 UPON BOARDING A/C CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED A/C, SUSPECTS SMOKE CAME FROM THE SUPPLEMENTAL AIR CONDITIONING. MAINTENANCE REMOVED AND REPLACED COMPRESSOR MOTOR. 2L72 4T RTA52EU 20040712000682004071200068 2004 7 12 SWAA041925 420040708A2565D31354 SLIDE BOEING737 7373Q8 1384670NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE INTO CONTAINER PER MM. 2L72 4F RTA16WE 20040712000692004071200069NE 2004 7 12 MALA040450 220040620A7200200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 SHUTDOWN A MALAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL15533XJ E2367 NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE, 1304240-1,1304240-2 & 1304241-3 FROM PREVIOUS LOG PAGES. AC TO BE 3 ENG. FERRIED FROM MEM TO MSP FOR NR 2 ENG REPLACEMENT. NR 2 ENG LOCK DOWN 3 FWD GALLEY CARTS REMOVED & POTABLE WATER DRAINED. MAINTENANCE REMOVED & REPLACED NR 2 ENG P/N 2-003-040-15, S/N ON LF07608, OFF P07892 IAW JOB CARD 7100-502 REF WORK PACKAGE ISSUED BY PLANNING DATED 6-21-04. 2H74 4F4 FRTA49EU E6NE 20040712000702004071200070 2004 7 12 MALA040468 420040617A3450 RECEIVER SAAB SF340 340B 7860101EU NR 1 NAVAGATION ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15429XJ 340B429 ELECTRICAL BURNING ODOR IN COCKPIT GOES AWAY WHEN NAV 1 IS TURNED OFF. MAINTENANCE INSPECTED COCKPIT AND AVIONICS RACK FOUND ONLY SLIGHT ODOR IN AVIONICS RACK, SUSPECT ODOR IS FROM NR 1 NAV RECEIVER CHANGED ON 6/16/04 AND ODOR IS RESIDUAL. 2L72 4T RTA52EU 20040712000712004071200071 2004 7 12 MALA040469 420040618A2565 INDICATOR BAC 146 AVRO146RJ85A1500097EU GIRT BAR MISSING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15513XJ E2329 RED DISARMED GIRT BAR INDICATOR IS MISSING ON FWD AND LEFT BOARDING DOOR. MAINTENANCE REPLACED INDICATOR STRIP AS REQUIRED. 2H74 4F RTA49EU 20040712000722004071200072EU 2004 7 12 MALA040465 120040628A243023080031 GCU SAAB SF340 340B 7860101EU DC GENERATOR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15449XJ 340B449 LEFT DC GEN FAILED IN FLIGHT WOULD NOT RESET. REMOVED AND REPLACED DC GENERATOR P/N 23080-031, S/N 6926 ON, S/N OFF 3974, GCU, P/N 51539-007B, S/N ON 99700, S/N OFF 97131, ALL CHECKS GOOD. 2L72 4T RTA52EU 20040712000732004071200073EU 2004 7 12 MALA040466 120040614A3240 BRAKE ASSY SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAO OTHER O OTHER LDLANDING 1 GL15423XJ 340B423 UPON LANDING IN MEM, PILOT REPORTED MUSHY BRAKES, AIRCRAFT PULLED TO THE RIGHT. BRAKE PRESSURE NORMAL. MAINTENANCE TAXIED AIRCRAFT, BRAKES WORK FINE, OK FOR SERVICE. DID NOT NOTICE PULLING TO RIGHT. 2L72 4T RTA52EU 20040712000772004071200077NM 2004 7 12 SWAA041927 120040708A53106545409 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20040712000782004071200078NM 2004 7 12 SWAA041928 120040708A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND RT KEELBEAM AT BS 500C, RBL 12, CORRODED. REMOVED AND REPLACED KEEL BEAM CHORD SECTION PER EA. 2L72 4F RTA16WE 20040712000792004071200079NM 2004 7 12 SWAA041929 120040708A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD VERTICAL BEAM WEB AT BS 178, RBL 17, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040712000802004071200080NM 2004 7 12 SWAA041930 120040708A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND BUTTSTRAPS AT BS 360, STRINGER 10R, BS 360 STRINGER 14R, CRACKED. REPAIRED BUTTSTRAPS PER SRM. 2L72 4F RTA16WE 20040712000812004071200081NM 2004 7 12 SWAA041931 120040708A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND STRINGER SPLICES AT BS 540, STRINGER 14R, BS 540, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20040712000822004071200082NM 2004 7 12 SWAA041932 120040708A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040712000842004071200084NM 2004 7 12 SWAA041935 120040708A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29470WN 33860 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040712000862004071200086EU 2004 7 12 MALA040472 120040624A3350 LIGHT SAAB SF340 340B 7860101EU CABIN BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15421XJ 340B421 EMERGENCY FLOOR TRACK LIGHTING BROKEN AT SEAT 16A. MAINTENANCE REMOVED SEGMENT AND DEFERRED FLOOR PROX EMERGENCY LIGHTING IAW MEL 3-53-2-2, ENTERED INTO DMR, MXC NOTIFIED 1376. 2L72 4T RTA52EU 20040712000872004071200087EU 2004 7 12 MALA040474 120040628A3350 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15402XJ 340B402 DURING LC1 & LC2 CHECKED EMERGENCY LIGHTING SYSTEM. NOTED SECTION OF FLOOR PROX INOP. UPON REMOVAL NOTED WIRES WERE PULLED FROM THE STRIP. MAINTENANCE REMOVED AND REPLACED 46LN PN 6636-3, OPS CHECK GOOD. 2L72 4T RTA52EU 20040712000892004071200089NM 2004 7 12 SWAA041937 120040708A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29786SW 29811 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT MODULE PER MM. 2L72 4F RTA16WE 20040712000902004071200090EU 2004 7 12 MALA040449 120040610A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15445XJ 340B445 EMERGENCY POWER SUPPLY P/N 3301-51, S/N OFF 2149 FAILED ON WING CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 6/11/04. 2L72 4T RTA52EU 20040712000922004071200092EU 2004 7 12 MALA040448 120040604A3350 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15518XJ E2337 BATTERY PACK P/N 61-2275-1, S/N OFF 97080028, WAS REMOVED FOR SCHEDULED CAPACITY TEST, FAILED TEST. MAINTENANCE REMOVED AND REPLACED CELL PACK P/N 61-2275-1, ALL CMM CHECKS GOOD. A/C RETURNED TO SERVICE 6/11/04. 2H74 4F RTA49EU 20040712000942004071200094EU 2004 7 12 MALA040457 120040613A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING 4K INSPECTION IN LCQ, FWD PAX CABIN FLOORBOARD SUPPORT UPPER SIDE HAS CORROSION AT PNL 121AZ FWD SIDE. MAINTENANCE REMOVED CORROSION FOUND OUT OF LIMITS IAW SAAB 340 SRM 51-10-10. CUT OUT CORROSION AND FABRICATED REPAIR AND INSTALLED REPAIR IAW SAAB 340 SRM 51-40-21 AND EO 53108. A/C RELEASE DATE 6/24/04. 2L72 4T RTA52EU 20040712000952004071200095EU 2004 7 12 MALA040451 120040608A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 294 LEFT I/B SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SECTION OF LEFT I/B SEAT TRACK AT FS 294 IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/23/04. 2L72 4T RTA52EU 20040712000992004071200099 2004 7 12 MALA040456 420040617A3445 ANTENNA SAAB SF340 340B 7860101EU TCAS CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING 4K INSPECTION IN LCQ, EVIDENCE OF HEAVY CORROSION UNDER EXTERNAL DOUBLER STA 248 SL1527-SL1627. DURING 4K CHECK, CORROSION WAS FOUND OF THE TCAS ANTENNA DOUBLER AND LOWER FUSELAGE SKIN. REPAIRED IN IAW MESABA EO S53232. A/C RELEASE DATE 6/24/04. 2L72 4T RTA52EU 20040712001002004071200100 2004 7 12 MALA040476 420040702A3425 COMPUTER SAAB SF340 340B 7860101EU NR 2 AHRS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15418XJ 340B418 AVIONICS COMPARITOR INFLIGHT F/O'S SIDE APPEARS TO BE 10-20 DEG OFF CAPTAINS SIDE. CAPTAINS SIDE APPEARS TO AGREE WITH STBY COMP. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER, OP CHECKS GOOD. 2L72 4T RTA52EU 20040712001012004071200101NE 2004 7 12 MALA040475 220040630A7200200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL15512XJ E2326 WHILE IN CRUISE, CREW REPORTED NR 2 ENGINE TEMP LIMITED AND LOW N1. AIR RETURN TO MEM. MAINTENANCE REPLACED BLOWN OUT COMBUSTER BLEED SEAL ON NR 1 ENG. REMOVED AND REPLACED NR 2 ENG P/N ON/OFF 2-003-040-15, S/N ON PO7801, S/N OFF P07793 IAW MAL JC 7100-502, COMPLETED WORK PACKAGE DATED 6-30-04 OK FOR SERVICE. TROUBLESHOOTING FOUND CUSTOMER BLEED AIR PIPE GASKET BLOWN OUT. REPLACED GASKET P/N RS6263. COMPLETED FOUR POINT ENGINE RUN MARGIN ROW AT +5.5 POWER ASSURANCE/TAKEOFF MARGIN WITHIN LIMITS, REF HONEYWELL AMM 72-00-00 TESTING. 2H74 4F4 FRTA49EU E6NE 20040712001052004071200105EU 2004 7 12 MALA040458 120040606A3520 LATCH BAC 146 AVRO146RJ85A1500097EU O2 DOOR DAMAGED A MALAG O2 MASK DEPLOYED P NO WARNING INDICATION NRNOT REPORTED 1 GL15531XJ E2365 DURING FLIGHT SEAT 14A & 14B ARE INOP, O2 MASKS OVER SEATS 14 A/B DEPLOYED. VERIFIED O2 GENERATOR NOT DEPLOYED. REPACKED AND RESET MASKS AND DOOR WON'T STAY SET, DEFERRED SEATS 14 A/B PER MEL 25-00-2-1 ENTERED INTO DMR. MXC NOTIFIED, SECURED DOOR WITH TAPE. MAINTENANCE RESECURED DOOR LATCH PIN PER PURITIAN BENNETT CMM 35-21-66, SECURITY CHECKS GOOD. REMOVED FROM DMR MXC NOTIFIED. 2H74 4F RTA49EU 20040712001062004071200106EU 2004 7 12 MALA040463 120040609A3350549117001 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15420XJ 340B420 DURING SCHEDULED CAPACITY CHECK, IN HOUSE WO 369067, EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N 2056, FAILED CAPACITY CHECK. MAINTENANCE REPLACED 12 EA P/N 549-1170-01 CELLS, UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 6/12/04. 2L72 4T RTA52EU 20040712001072004071200107EU 2004 7 12 MALA040464 120040628A335066363 RELAY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15402XJ 340B402 DURING LC1 & LC2, CHECKED EMERGENCY LIGHTING SYSTEM. NOTED SECTION OF FLOOR PROX INOP. UPON REMOVAL NOTED WIRES WERE PULLED FROM THE STRIP. MAINTENANCE REMOVED AND REPLACED 46LN, P/N 6636-3. OPS CHECK GOOD. 2L72 4T RTA52EU 20040712001092004071200109EU 2004 7 12 MALA040462 120040609A33506121981 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15510XJ E2323 DURING CAPACITY CHECK IN HOUSE WO 369315, BATTERY PACK P/N 61-2275-1, S/N 0011447, FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 61-2198-1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 6/13/04. 2H74 4F RTA49EU 20040712001102004071200110NM 2004 7 12 SWAA041922 120040707A57536546430129 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20040712001112004071200111NM 2004 7 12 SWAA041923 120040707A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS TRACK COVERS CRACKED. REMOVED AND REPLACED EEPLS TRACK COVERS PER MM. 2L72 4F RTA16WE 20040712001132004071200113NM 2004 7 12 SWAA041912 120040707A55526959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE BUSHING AND HARDWARE PER MM. 2L72 4F RTA16WE 20040712001142004071200114NM 2004 7 12 SWAA041913 120040707A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727, STRINGER 27L, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040712001152004071200115NM 2004 7 12 SWAA041914 120040707A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND SHEAR TIE AT BS 520, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040712001162004071200116NM 2004 7 12 SWAA041916 120040707A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND STRINGER 6L AT BS 374, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040712001172004071200117 2004 7 12 SWAA041917 420040707A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED R1 AND L1 DOOR EVAC SLIDES GIRT BAR FITTINGS PER MM. 2L72 4F RTA16WE 20040712001182004071200118SO 2004 7 12 C2XA04SH398 120040628A532014525800009 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001202004071200120SO 2004 7 12 C2XA04TY100 120040629A532014521725613 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713970 145146 DURING A SCHEDULED C-CHECK INSPECTION, THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. THE SILL WAS REMOVED AND REPLACED IAW EMB SRM. THE ACFT WAS SUBSEQUENTLY RELEASED FOLLOWING C-CHECK INSPECTION. 2L72 4F RTT00011AT 20040712001222004071200122SO 2004 7 12 C2XA04IA026 120040307A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714940 145033 DURING SCHEDULED MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE LIGHTING SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY. 2L72 4F RTT00011AT 20040712001232004071200123WP 2004 7 12 AALA20040678 120040628A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21596AA 53286 SEA - EMERGENCY LIGHTS NEAR B5-23 INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040712001252004071200125WP 2004 7 12 AALA20040680 120040625A2170 COALESCER BAG DOUG DC9 DC983 3022083WP CONTAMINATED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21592AA 53255 ABQ INFLIGHT T1114/25 - AFTER TAKEOFF FLIGHT ATTENDANT REPORTED GREYISH SMOKE THROUGHOUT ENTIRE CABIN. SMELL WAS A HOT SMELL. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. FOUND APU INLET SOAKED WITH OIL. REMOVED AND REPLACED WATER SEPARATOR COALESCER. CLEANED AND REPLACED BAGS AND ACCOMPLISHED A PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040712001312004071200131SO 2004 7 12 C2XA04SH401 120040630A532014525422003 SILL EMB 145 EMB145ER 3260211SO CARGO CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT HAND FORWARD CARGO FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 61 AND 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001362004071200136SO 2004 7 12 C2XA04TY096 120040621A532014522460013 ANGLE EMB 145 EMB145 3260210SO GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AND AFT NUT PLATE OF THE CENTER TOP CAP UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE CENTER TOP CAP IAW EMB SRM 51-40-02 AND 57-20-03. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040708000692004070800069EU 2004 7 8 UPS04142579 120040611A3350 LAMP AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01137UP 0810 INSPECTION TYPE:AS TOILET EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT. 2L72 4F RTA35EU 20040708000702004070800070EU 2004 7 8 UPS04142589 120040601A5321B5327053100000 FLOORBOARD AIRBUSA300 A300F4622R 3930360EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 INSPECTION TYPE: C2, AFT PIT FLOOR PNL 151CF CRACKED IN 3 PLACES. FABRICATE NEW FLOORBOARD IAW EO A300-5320-16407-A. 2L72 4F RTA35EU 20040708000812004070800081 2004 7 8 SWAA041869 420040702A25656567380 LENS BOEING737 7373H4 1384600NM R1 DOOR SLIDE MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVAC SLIDE CONTAINER MISSING GAUGE LENS. REPLACED LENS PER MM. 2L72 4F RTA16WE 20040708000912004070800091WP 2004 7 8 UPS04842578 120040611A3350 LAMP DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: AS, EMERGENCY LIGHT IN COURIER AREA INOP. RELAMPED EMERGENCY LIGHT. 2L74 4F RT4A25 20040708000952004070800095NM 2004 7 8 SWAA041880 120040702A335007912 COVER BOEING737 7377H4 1384404NM ROW 8 - 12 CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT COVERS AT ROW 8 ABC, ROW 12 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040708000962004070800096NM 2004 7 8 SWAA041881 120040703A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727 + 15, STRINGER 27L, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040708000972004070800097NM 2004 7 8 SWAA041882 120040703A335007912 COVER BOEING737 7373H4 1384600NM ROW 8 ABC DAMAGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C2 CHECK, FOUND EEPLS LIGHT COVER AT ROW 8 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040708001012004070800101NM 2004 7 8 04FDEA01708 120040614A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 SEAT TRACK FOUND CRACKED AT STA 792 RIGHT 28 INCHES. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL 1 AND CRACK FREE ON CUT OUT AREA BY NDT INAPECTION. 2L73 4F RTA22WE 20040708001192004070800119WP 2004 7 8 MWEA040102 120040615A528039364031 SUPPORT DOUG DC9 DC981 3022081WP MLG DOOR ACT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 RIGHT MAIN LANDING GEAR DOOR ACTUATOR FITTING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT RIGHT SIDE. 2L72 4F A6WE 20040708001322004070800132NM 2004 7 8 SWAA041892 120040704A53436545819 WEB BOEING737 7373H4 1384600NM NLG SUPPORT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C2 CHECK, FOUND FWD NLG SUPPORT WEB, CRACKED. REMOVED AND REPLACED NLG FWD SUPPORT WEB PER SRM. 2L72 4F RTA16WE 20040708001372004070800137NM 2004 7 8 SWAA041906 120040706A53206445833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT LT AND RT BS 188 TO BS 496, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER BAC DRAWING AND SRM. 2L72 4F RTA16WE 20040708001472004070800147NM 2004 7 8 MWEA040098 120040615A52471911703113 CONTROLLER BOEING717 717200 1383700NM APU DOOR INOPERATIVE A MWEAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 GL31909ME 55173 AUXILIARY POWER UNIT QUIT DURING ENGINE START. REMOVED AND REPLACED AUXILIARY DOOR CONTROLLER. 2L72 4F TRA6WE 20040708001532004070800153NM 2004 7 8 PCAA0406222 120040614A3260841005 PSEU DHAV DHC8 DHC8102 2809003NM MLG INTERMITTENT A PCAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA13824EX280649842 387 FLIGHT 3952 REPORTED NOSE GEAR INTRANSIT LIGHT FLICKERED ON AND OFF AS THE NOSE GEAR WENT OUT OF THE UPLOCK POSITION AND BACK TO UPLOCK DURING CLIMB. CREW ELECTED TO RETURN TO LGA, AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS THEN FERRIED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SWITCHING ELECTRONICS UNIT (PSEU) AND INSPECTED AND CLEANED THE ASSOCIATED PROXIMITY SWITCHES AND CANNON PLUGS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001592004070800159NM 2004 7 8 QXEA200400431 120040611A2612 FIRE LOOP DHAV DHC8 DHC8202 2809007NM ZONE 200 MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09353PH 496 SEA - THERE WAS A LOOP -A- FAULT LIGHT ILLUMINATED ON NR 1 ENGINE FIRE DETECTION SYSTEM. FOUND NR 1 ENGINE FIRE LOOP -A- CIRCUIT BREAKER NOT SET. RESET CIRCUIT BREAKER. C/W FIRE/OVERHEAT DETECTION SYSTEM ADJUST/TEST. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040708001612004070800161GL 2004 7 8 CX2A04RI004 220040618A7200 ENGINE EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL NR 1 FIRE A C2XAF ACTIVATE FIRE EXT. BA SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TXTAXI/GRND HDL 1 SW27275068517 1838 145206 CAE311212 CREW RETURNED ACFT TO THE GATE AFTER ENG NR 1 HUNG START AND AN ABORTED ENG NR 1 HOT START. PASSENGERS WERE DEPLANED. MAINTENANCE DISCOVERED NR 1 ENG SMOKING AND SUSPECTED ENGINE CORE FIRE. MAINTENANCE PROCEEDED WITH NR 1 ENG DRY MOTORING TO EXPEL RESIDUAL FUEL. GROUND CREW REPORTED FLAMES COMING FROM INSIDE THE ENGINE. MAINTENANCE NOTICED SMOKE BECAME PROGRESSIVELY WORSE BUT THERE WAS NO FIRE WARNING INDICATION IN THE COCKPIT. MAINTENANCE DISCHARGED BOTH ENGINE FIRE BOTTLES AND NOTIFIED FIRE DEPARTMENT. FIRE WAS EXTINGUISHED. ENGINE NR 1 WAS REMOVED AND REPLACED. ENGINE LEAK AND OPERATIONAL CHECK WAS PERFORMED AND ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040708001632004070800163 2004 7 8 150AW0023 420040614A2230 SENSOR BOEING737 7373G7 1384595NM AUTO THROTTLES OUT OF ADJUST A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05150AW 23218 AUTO THROTTLE WILL KICK OFF ON TAKEOFF PRIOR TO REACHING TAKE OFF THRUST. WILL NOT RE-ENGAGE UNTIL FLAPS ARE RETRACTED AND ALL LIGHTS OUT. ADJUSTED PLA SYNCHRO PER MM 22-31-11. AUTO THROTTLE BITE TEST PERFORMS NORMAL. 2L72 4F RTA16WE 20040708001642004070800164SO 2004 7 8 CX2A04RI002 120040616A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714977 145175 RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-09. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. 2L72 4T RTT00011AT 20040708001702004070800170SO 2004 7 8 C2XA04SH371 120040618A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2728518 145334 SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-21-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001732004070800173SO 2004 7 8 C2XA04TY092 120040623A5510KSC270720 BEARING EMB 145 EMB145 3260210SO HORIZONTAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713970 145146 DURING A SCHEDULED 3C INSPECTION THE RT HORIZONTAL SPHERICAL BEARING WAS FOUND WORN. REMOVED AND REPLACED THE RT SPHERICAL BEARING IAW EC 5510-01083. ALL WORK WAS ACCOMPLISHED AND THE DIEHEDRAL AND INCIDENCE CHECKS WERE ALL GOOD. A/C WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20040708001752004070800175SO 2004 7 8 C2XA04CL065 120040620A4920 APU EMB 145 EMB145XR 3260214SO ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2713123 145688 DAY FLIGHT 2286 THE CREW REPORTED AFTER STARTING THE APU A MINOR BURNING ODOR WAS NOTED. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00. 2L72 4F RT 20040708001852004070800185WP 2004 7 8 MWEA040101 120040617A57545930495504 VANE DOUG DC9 DC981 3022081WP LE FLAP CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 RIGHT FLAP NR 2 FIXED VANE LEADING EDGE IS CHAFED. FABRICATED AND INSTALLED PATCH FOR REPAIR. 2L72 4F A6WE 20040708001902004070800190GL 2004 7 8 C2XA04IA073 220040618A7261 ENGINE EMB 135 EMB135ER 3260203SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A C2XAE ENGINE SHUTDOWN JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27145057068 136 145192 CAE311394 IAH - FLIGHT 2376 THE CREW REPORTED THAT THE NUMBER ONE ENGINE SHOWED LOW OIL PRESSURE, AND HIGH OIL TEMPERATURE WITH A SMELL OF SMOKE DURING CRUISE. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ENGINE, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040708001922004070800192SO 2004 7 8 C2XA04SH387 120040623A531014526436401 CROSSBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE CROSSMEMBER BETWEEN THE LEFT HAND SILL AND THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 59 AND 60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040708001992004070800199NM 2004 7 8 0400996623 120040608A2432401767 BATTERY BOEING747 747251B 1384892NM MASTER SMOKE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01623US 21705 DURING CRUISE, SMOKE EMITTED IN THE FLIGHT DECK. FOLLOWED COM PROCEDURE AND THE SMOKE DISSIPATED AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE MAIN BATTERY AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040708002022004070800202NM 2004 7 8 MWEA040093 120040612A55225912148506 DOUBLER BOEING717 717200 1383700NM LT ELEVATOR LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31905ME 55169 LEFT ELEVATOR UPPER SKIN OUTBOARD AFT SKIN HAS AN AREA OF LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F TRA6WE 20040708002082004070800208EU 2004 7 8 YENA200433 120040608A25304110001137 COFFEEMAKER AIRBUS320 A320232 3930326EU GALLEY SMOKE A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15520JB4638 1446 F/A REPORTED NR 2 COFFEEMAKER WAS SMOKING. TURNED OFF COFFEEMAKER AND SMOKE DISSIPATED. PULLED C/B FOR NR 2 COFFEEMAKER. REMOVED COFFEEMAKER AFTER OPS CHECK. FOUND NO FAULT OR LOOSE CONNECTIONS BEHIND COFFEEMAKER. REPLACED COFFEEMAKER FOR PRECAUTIONARY REASONS. OPS CHECK NORMAL PER AMM 25-35-15. OPERATION CHECKED NEW POT AND NO SMOKE OR BURNING SMELL. 2L72 4F RTA28NM 20040709000042004070900004NM 2004 7 9 200414S 120040605A3297 TERMINAL DHAV DHC8 DHC8102 2809003NM MLG SWITCH LOOSE A KPVAO OTHER N FALSE WARNING LDLANDING 1 WP13813SN 032 GEAR REMAINED UP & LOCKED WITH GEAR HANDLE DOWN (3 RED LIGHTS ONLY). RECYCLED GEAR HANDLE TWICE. GEAR EXTENDED N THIRD ATTEMPT. COMPLIED WITH A WALK AROUND INSPECTION AND HAVE DETERMINED THIS AIRCRAFT TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT FROM MKK TO HNL ONLY. RETIGHTENED TERMINAL IN BACK OF INHIBIT SWITCH. OPS CHECK GOOD IAW DHC 8 MM CH. 32-35-00 PG. 201-203 PARA. 1A. SWING GEAR, OPS CHECK GOOD IAW DHC 8 MM 32-30-00 PG. 204-205 PARA. 2A. 2H72 4T RTA13NM 20040709000202004070900020WP 2004 7 9 AALA20040711 120040707A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21558AA 53088 PHX - THREE AFT ACCESSORY CEILING LIGHTS AND TWO SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER B5-28 IN RIGHT AFT LAV FOR AFT ACCESSORY CEILING LIGHTS AND TWO SLIDE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000342004070900034EU 2004 7 9 AALA20040699 120040625A5310 BEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW217076A 610 TUL - NUMBER THREE GANTRY BEAM AT FRAME 49 IS CRACKED APPROXIMATELY .50 INCH LONG. AREA WAS MODIFIED PER ECO 1273AD TO ACCOMPLISH NDT INSPECTION. STOP DRILLED CRACK. HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACK TERMINATION IN HOLE. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ESO 30595 DATED JUNE 25, 2004 REPAIR NUMBER 40 51300 3477. 2L72 4F RTA35EU 20040709000352004070900035EU 2004 7 9 AALA20040700 120040625A5310 BEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW217076A 610 TUL - NUMBER THREE GANTRY BEAM AT FRAME 49 1 IS CRACKED APPROXIMATELY THREE EIGHTS OF AN INCH LONG. AREA WAS MODIFIED PER ECO 1273AD TO ACCOMPLISH NDT INSPECTION. STOP DRILLED CRACK AND HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACK TERMINATED IN STOP DRILL HOLE. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH ESO 30595 DATED JUNE 25, 2004 REPAIR NUMBER 40 531500 3477. 2L72 4F RTA35EU 20040709000392004070900039EU 2004 7 9 AALA20040693 120040623A5330 SKIN AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 TUL - SKIN CORRODED BETWEEN STRINGERS 53L AND 54L AT FRAME 65 IN AFT CARGO AT STATION NUMBER 4256. AREA OF CORROSION IS 3.75 INCHES BY 4.88 INCHES. INSTALLED SKIN FILLER AND STACK DOUBLER PER ESO 30595 DATED JUNE 22, 2004. 2L72 4F RTA35EU 20040709000482004070900048 2004 7 9 SWAA041919 420040707A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED C2 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 AND L2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040709000592004070900059SO 2004 7 9 C2XA04SH429 120040706A532014524765615 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 DURING C-CHECK THE SHEAR CLIP AT FRAME 67, BETWEEN STRINGER 6L AND 7L WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000672004070900067SO 2004 7 9 C2XA04SH406 120040702A531514530633001 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO FRAME 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000702004070900070SO 2004 7 9 C2XA04SH393 120040626A532014520609001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 TO 29. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712000172004071200017GL 2004 7 12 PNR2004F00001 120040519A5540281432015 BEARING ENSTRMF28 280C 3300505GL LYC O360 HIO360* 41514EA RUBBER DELAMINATED D PNRGO OTHER O OTHER NRNOT REPORTED 1 NM09646H 1085 1099 PILOTS COMPLAINED ABOUT HEAVY COLLECTIVE AND EXCESSIVE AMOUNT OF RT COLLECTIVE INPUT TO FLY. UPON INSPECTION OF THE LAMIFLEX BEARINGS, IT WAS DISCOVERED THAT THE RUBBER AND BRASS MATERIAL WAS EXTRUDING AND DELAMINATING. UNABLE TO DETERMINE CAUSE. USEFUL LIFE IS RATED AT FIVE YEARS, AND THESE HAD 25 MONTHS TIME IN SERVICE WHEN REMOVED. 1G71 3O3 O H1CE 1E10 20040712000222004071200022 2004 7 12 USA2004F00060 420040525A2565 LANYARD AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE ESCAPE SLIDE MISSING A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19710UW13285 1019 THE ESCAPE SLIDE RELEASE LANYARD WAS FOUND NOT INSTALLED WHEN SLIDE WAS REMOVED FOR ACESS DURING THE HEAVY MAINTENANCE VISIT. MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA28NM E2GL 20040712000232004071200023GL 2004 7 12 ALG2004F00036 220040612A753223073353 BLEED VALVE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03194H 11235 45660 WHILE HOVERING FOR TAKEOFF, IN A RT PEDAL TURN TO ALIGN THE AIRCRAFT WITH THE FLY AWAY WHEN A NOTICEABLE BANG CAME FROM THE ENGINE COMPARTMENT AND RT YAW OCCURRED. IMMEDIATELY LANDED, CHECK ALL SYSTEMS IN THE GREEN AND HOVERED TO THE MAINTENANCE PAD. MAINTENANCE INSPECTED COMPRESSOR INLET AREA FOUND NO EVIDENCE OF FOD, INSPECTED COMPRESSOR SECTIONS FOR CRACKS AND LEAKS NONE FOUND AND AIRLINES CHECKED GOOD. REMOVED AND REPLACED BLEED VALVE, OPS CHECK WAS GOOD. 1G71 3U3 U H2SW E1GL 20040712000292004071200029 2004 7 12 USA2004F00068 420040520A23106225272001 TRANSCEIVER BOEING767 7672B7 1385107NM GE CF6 CF680 30025NE HF SYSTEM OVERHEATED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19653US30123 24894 AFTER UNSUCCESSFUL ATTEMPT TO TUNE OR TRANSMIT ON HF NR 1, AND ELECTRICAL SMELL WAS NOTED IN THE COCKPIT. THE HF NR 1 CIRCUIT BREAKER WAS PULLED AND THE SMELL DISSIPATED. MAINTENANCE REPLACED THE NR 1 HF TRANSCEIVER. 2L72 4F4 FRTA1NM E13NE 20040712000322004071200032NE 2004 7 12 FXT2004F00000 220040608A72503032151 VANE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL HOT SECTION WORN E FXTAO OTHER O OTHER NRNOT REPORTED 1 AL011263Y231 208B0731 PCO630 983925 CT-VANE SEGMENTS SLIPPED AND RUBBED INTO THE CT-DISK, CAUSING ABNORMALLY HOT OPERATION OF THE ENGINE. A NEW HOT SECTION WAS IN STALLED AND THE PROBLEM WAS FIXED ALL OPERATING TEMPERATURES WERE NORMAL. THE FIRST TIME THIS HAPPENED WAS IN NOV OF 2003. AT THAT TIME WE THOUGHT IT WAS JUST A FLUKE BECAUSE WE HAVE BEEN OPERATING THESE ENGINES A LONG TIME AND NEVER HAD THIS PROBLEM BEFORE. MAY OF 2004, SAME THING HAPPENED, THE CT-VANE SEGMENTS SLIPPED AND RUBBED INTO THE CT-DISK CAUSING ABNORMALLY HOT OPERATION OF THE ENGINE. ENGINE OVERHAUL FACILITY HAS TOLD US THE PROBLEM IS IN THE DESIGN OF THE RETAINING RING THAT HOLDS THE SEGMENTS IN PLACE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20040712000502004071200050SO 2004 7 12 SIMA200415805 120040605A3230852701 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT MLG INOPERATIVE A SIMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW21631AE 145139 DURING TAKEOFF CREW REPORTED THE LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. CREW NOTED A LDG AIR/GRD MESSAGE ON EICAS. CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE DOWNLOADED CMC AND FOUND MULTIPLE FAILURES ON THE LT PROXIMITY SWITCH. THE LT WOW PROXIMITY SWITCHES 1 AND 2 WERE REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040712000592004071200059SO 2004 7 12 SIMA200417207 120040617A551014524979001 BUSHING EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL HORIZONTAL STAB WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21622AE 145108 DURING MBV INSPECTION THE LT HORIZONTAL STABILIZER OB BUSHING WAS FOUND TO BE MIGRATING. REPLACED BUSHINGS IAW MFG SRM. 2L72 4T4 FRTT00011ATTE6CH 20040714000102004071400010WP 2004 7 14 UPS04842597 120040614A53305645332117 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STATION 960-980 LBL 63. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5645332 AND SRM 53-7-3 FIG 4, 51-1-20D. 2L74 4F RT4A25 20040712000752004071200075EU 2004 7 12 MALA040471 120040622A2620 TUBE SAAB SF340 340B 7860101EU EXTINGUISHER BENT A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15417XJ 0105558 340B417 LAV & FIRE BOTTLE EXTINGUISHING TUBE BENT AND UNABLE TO EXTINGUISH. MAINTENANCE REMOVED AND REPLACED LAV WASTE BIN FIRE EXTINGISHER P/N ON/OFF A8001002, S/N OFF 0105558, S/N ON 0334 WT CHECK DUE 3-22-05. 2L72 4T RTA52EU 20040712000912004071200091EU 2004 7 12 MALA040447 120040613A3260 PROXIMITY SENSOR BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15512XJ E2326 RT SOLID GEAR UNSAFE LIGHT AND LIGHT IN GEAR HANDLE ON AFTER T/O AND REST OF GEAR UP LIGHT ON CONTINUOUS UNTIL GEAR DOWN. REMOVED AND REPLACED RIGHT MLG DOOR UPLOCK PROX SENSOR, ALL CHECKS GOOD AT THIS TIME. 2H74 4F RTA49EU 20040712000962004071200096EU 2004 7 12 MALA040452 120040608A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 294 RIGHT I/B SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SECTION OF RIGHT I/B SEAT TRACK AT FS 294 IAW MESABA EO S53060. AIRCRAFT RELEASE DATE 6/23/04. 2L72 4T RTA52EU 20040712000972004071200097EU 2004 7 12 MALA040453 120040607A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 686.38 AFT CARGO FRAME CHAFED. FABRICATED AND INSTALLED REPAIR ANGLE ON AFT CARGO FRAME AT FS 686.38 IAW MESABA EO S53152. AIRCRAFT RELEASE DATE 6/23/04. 2L72 4T RTA52EU 20040712000982004071200098EU 2004 7 12 MALA040454 120040607A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 DURING 4K INSPECTION IN LCQ, FS 630.112 AFT CARGO FRAME CHAFED. MAINTENANCE FABRICATED AND INSTALLED FRAME ANGLE ON AFT CARGO FRAME AT FS 630.112 IAW MESABA EO S53152. AIRCRAFT RELEASE DATE 6/23/04. 2L72 4T RTA52EU 20040712001022004071200102EU 2004 7 12 MALA040459 120040623A3350501171202 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15407XJ 340B407 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N/1488 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. FAILED CAPACITY CHECK. REPLACED 2 EACH P/N 549-1324-06 CELL PACKS AND CAP CHECKS GOOD. A/C RETURNED TO SERVICE 6/28/04. 2L72 4T RTA52EU 20040712001192004071200119SO 2004 7 12 C2XA04SH399 120040628A532014529495001 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001242004071200124WP 2004 7 12 AALA20040679 120040628A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21573AA 53092 RDU - EMERGENCY EXIT LIGHTS ABOVE VENTRAL STAIRS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS ABOVE VENTRAL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040712001272004071200127EU 2004 7 12 AALA20040682 120040603A5321 ROLLER TRAY AIRBUS300 A300B4605R 3930308EU CARGO BAY CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2125071 514 TUL - CORROSION ON LEFT FLOORBOARD FLANGE OF NUMBER 4 ROLLER TRAY BETWEEN FRAME 60 AND 61. AREA OF CORROSION IS 1 INCH BY 2 INCHES WITH A DEPTH OF .050. BLENDED OUT CORROSION PER SRM 51-74-0 AND INSTALLED REPAIR STRAP PER 53-30-00-1. 2L72 4F RTA35EU 20040712001302004071200130SO 2004 7 12 C2XA04TY101 120040629A531514529150007 FLOORBEAM EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713970 145146 DURING A SCHEDULED C-CHECK INSPECTION, CORROSION WAS FOUND THE FLOOR CROSSBEAM ANGLE AT FRAME 23. THE CROSSBEAM ASSEMBLY WAS REMOVED AND REPLACED IAW EMB SRM AND THE ACFT WAS SUBSEQUENTLY RELEASE FOLLOWING THE COMPLETION OF THE C- CHECK INSPECTION. 2L72 4F RTT00011AT 20040712001402004071200140SO 2004 7 12 C2XA04SH388 120040623A532014521725001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT HAND FLOOR SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 19 AND 24. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001412004071200141SO 2004 7 12 C2XA04TY099 120040623A532014524119007 THRESHOLD EMB 135 EMB135LR 3260305SO ENTRY DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715527 145413 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER ENTRY DOOR THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD PLATE IAW EMB SRM 51-21-00. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040712001422004071200142SO 2004 7 12 C2XA04386 120040623A531514521721009 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001442004071200144SO 2004 7 12 C2XA04IA080 120040618A521014525311403 SEAL EMB 145 EMB145ER 3260211SO MAIN PAX DOOR DRY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 EWR - FLIGHT 2311, THE CREW REPORTED THAT THE MAIN CABIN DOOR JAMS WHEN OPENING, AND IS VERY DIFFICULT TO OPEN. MAINTENANCE LUBED THE PASSENGER DOOR, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001452004071200145SO 2004 7 12 C2XA04SH408 120040702A531514521721005 STRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAO OTHER O OTHER LDLANDING 1 SW2714930 145011 SHV - DURING C-CHECK THE FORWARD DIGITAL A FRAME 14 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001472004071200147SO 2004 7 12 C2XA04SH409 120040702A531514522460011 STRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE FORWARD DIGITAL WAS FOUND TO BE CORRODED FROM FRAME 17 TO 18. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 4, FIG 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001502004071200150SO 2004 7 12 C2XA04SH412 120040702A532014525800016 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 48 TO 52. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001512004071200151SO 2004 7 12 C2XA04SH413 120040702A531514530633003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 24 TO 36. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001522004071200152SO 2004 7 12 C2XA04SH414 120040702A532014521699003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001542004071200154SO 2004 7 12 C2XA04SH416 120040629A541114576057622 RIB EMB 145 EMB145ER 3260211SO NR 2 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001692004071200169WP 2004 7 12 ASMF200406026 120040622A2620898150 EXTINGUISHER DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE NR 2 ACTIVATED W ASMFF ACTIVATE FIRE EXT. J WARNING INDICATION NRNOT REPORTED 1 SW23205AM3865 49405 DURING TRANSIT CHECK, FIRE EXTINGUISHER NR 2 WAS ACTIVATED WITHOUT APPARENT CAUSE. AIR CONDITIONING SYSTEM WAS CHECKED BY LEAKS AND COOLING TURBINE CLAMP AND DUCT WERE DETECTED LOOSEN. CLAMP AND DUCT WERE ADJUSTED AND FIRE EXTINGUISHER WAS REPLACED IAW MM 26-20-01, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040712001702004071200170NE 2004 7 12 ASMF200406018 220040618A7314384300 PUMP DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUEL SYSTEM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS703 49643 718221 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE LOW POWER. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE FUEL PUMP AND FUEL CONTROL UNIT WERE REPLACED IAW MM 73-12-01 AND 73-20-01, RESPECTIVELY, TEST WAS PERFORMED IAW MPCM 71-00-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20040712001742004071200174NM 2004 7 12 ASMF200406028 120040623A2913 CIRCUIT BREAKER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE HYD PUMP TRIPPED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM 26273 AIRCRAFT RETURNED TO PLATFORM, "CTL HYDRAULIC PUMP" LIGHT TURNED ON AND EICAS MESSAGE, ENGINES WERE SHUTDOWN. DURING MAINTENANCE CHECK, HYDRAULIC PUMP BREAKER K24 WAS ACTIVATED AND REESTABLISHED, FIM PROCEDURE 29-11-00 WAS PERFORMED, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20040712001762004071200176WP 2004 7 12 ASMF200406019 120040619A3260 WARNING LIGHT DOUG DC9 DC987 3022087WP MLG ILLUMINATED W ASMFO OTHER N FALSE WARNING APAPPROACH 1 SW23204AM 49404 CAPTAIN REPORTED NOSE LANDING GEAR RED LIGHT TURNED ON DURING APPROACH AND WHEN LANDING GEAR WAS DOWN, AUDIBLE WARNING ACTIVATED AND LIGHT CONTINUED TURNED ON. LANDING GEAR WAS OPERATED MANUALLY. AIRCRAFT WAS SENT TO THE HANGAR AND SENSORS D1-31Y AND D1-32 WERE CHECKED BY CONDUCTIVITY AND THEY WERE REPLACED IAW MM 32-60-05, TEST CORRECT. 2L72 4F RTA6WE 20040712001812004071200181SW 2004 7 12 M0516 120040702A5302407530014101 TAIL BOOM BELL 407 407 1182206SW FUSELAGE CRACKED B BXORK NONE O OTHER ININSP/MAINT 1 EA09555BH 53201 CRACK DETECTED FROM RIVET ATTACHING LT DOUBLER REQUIRED BY ASB 407-01-48 / AD 2003-05-03. CRACK EXTENDED FROM FIRST RIVET ABOVE HI-LOK RIVET ON FORWARD EDGE OF DOUBLER. VISIBLE CRACK APPROX .6250 INCH LONG DISAPPEARED UNDER DOUBLER. TOTAL LENGTH UNKNOWN. TAIL BOOM FORWARDED TO MFG FOR INVESTIGATION. 1G71 3U O H2SW 20040712001972004071200197WP 2004 7 12 ASMF200406023 120040621A55235910413507 TAB DOUG DC9 DC987 3022087WP ELEVATOR DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23214AM 49585 DURING OVERNIGHT SERVICE LIGHTING STRIKE DAMAGE WAS DETECTED IN LT ELEVATOR TAB, WITH 1 INCH OF DIAMETER. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00 AND ELEVATOR TAB WAS REPLACED IAW MM 27-30-03, TEST CORRECT. 2L72 4F RTA6WE 20040713000032004071300003EU 2004 7 13 USAA040137 120040418A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 FOUND SILL CORRODED 2 INCHES BY 1.5 INCHE BY .070 INCH AREA, R2 DOOR SILL, FRAME 66, -Y1732. REMOVED AND REPLACED SILL PER SRM 51-42-11, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000052004071300005EU 2004 7 13 USAA040127 120040426A5310D5347219021000 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 FOUND BEAM CORRODED TWO PLACES 1.5 INCH LONG BY 1 INCH WIDE BY .02 INCH DEEP, FRAME Y1292 AND CROSSBEAM C66-Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040713000072004071300007EU 2004 7 13 USAA040138 120040410A5347D5347209000300 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND SEAT TRACK BEAM CORRODED 2 INCHES IN DIAMETER BY .030 INCH DEEP AREA, BETWEEN FRAME 64 AND 65, -Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11, 51-44-00, 51-23-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000122004071300012EU 2004 7 13 USAA040132 120040418A5330D5367180500400 PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND PANEL CORRODED 2.2 INCH BY .95 INCH COMPLETELY THROUGH METAL, PANEL 262FF, -Z340, FRAME 67, Y-1763. REMOVED AND REPLACED PANEL PER SRM 51-42-11, 51-74-00. CORROSION LEVEL 2, TASK NR JA-260-53100. (M) 2L72 4F RTA28NM 20040713000162004071300016WP 2004 7 13 ASAA0480322 120040421A57109936314503 SPLICE PLATE DOUG DC9 DC983 3022083WP LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND LEFT WING LEADING EDGE SPLICE PLATE IS CRACKED AT STATION XRS164. REMOVED DAMAGED SPLICE PLATE AND INSTALLED NEW PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040713000172004071300017WP 2004 7 13 ASAA0480321 120040421A523059101413 SKIN DOUG DC9 DC983 3022083WP AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND AFT PIT DOOR SKIN DENTED AT STATIN 1186, APPROX 15 INCHES FROM TOP, D=2 INCHES X=.040. REMOVED DAMAGED AREA OF SKIN AND INSTALLED RPR DOUBLERS PER SRM 53-04. (M) 2L72 4F RTA6WE 20040713000192004071300019EU 2004 7 13 USAA040145 120040421A5310D5311281520200 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND BEAM CORRODED 1 INCH BY .65 INCH BY .045 INCH DEEP AREA, FRAME 20, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-11-14, 51-23-11. CORROSION LEVEL 2. TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040713000222004071300022EU 2004 7 13 USAA040142 120040416A5310D5347209200000 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01704US16409 0922 BFM - FOUND BEAM CORRODED 1 INCH BY .75 INCH BY .024 INCH DEEP, FRAME 68, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 53-00-14. CORRODED LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000252004071300025WP 2004 7 13 ASAA0480255 120040404A57308570030326 PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING LEFT WING PANEL 1367 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040713000262004071300026WP 2004 7 13 GTIA040341 120040406A5321 FLOORBOARD DOUG DC9 DC983 3022083WP COCKPIT CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND COCKPIT FLOORBOARD CRACKED, SPLIT, CUT, BROKEN, GOUGED AND BENT. FABRICATED NEW COCKPIT FLOORBOARD. (M) 2L72 4F RTA6WE 20040713000272004071300027WP 2004 7 13 GTIA040342 120040406A5321 FLOORBOARD DOUG DC9 DC983 3022083WP COCKPIT CUT A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND COCKPIT FLOORBOARD SECTION CUT OUT AND HONEY COMB EXPOSED. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040713000282004071300028EU 2004 7 13 USAA040148 120040428A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND DOOR SILL BEAM CORRODED 1.2 INCHES LONG BY .080 INCH WIDE BY .052 INCH DEEP, BETWEEN FRAME 66-68, Y1970, -Z240. REMOVED AND REPLACED PART PER SRM 51-74-00, 53-41-14, 53-42-11, 51-77-11, 51-42-11. (M) 2L72 4F RTA28NM 20040713000312004071300031EU 2004 7 13 USAA040151 120040423A5310D5347218820200 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND BEAM CORRODED 1.2 INCH BY 1 INCH BY .047 INCH DEEP AREA, BETWEEN FRAME 68 AND 69, Y1292,-Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M) 2L72 4F RTA28NM 20040713000322004071300032EU 2004 7 13 USAA040150 120040423A5310JA16053500 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23704US16409 0922 BFM - FOUND BEAM ASSEMBLY CORRODED 1 INCH BY 1.2 INCH BY .035 INCH DEEP AREA, BETWEEN FRAME 64/65, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15, 51-42-11, 53-00-14. (M) 2L72 4F RTA28NM 20040713000352004071300035WP 2004 7 13 GTIA040350 120040406A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND CABIN FLOORBOARD STATON 826-864 RIGHT CENTER AFT INBOARD CORNER IS CRACKED ON LOWER SURFACE. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040713000372004071300037WP 2004 7 13 GTIA040353 120040317A5321 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT MID SEAT TRACK STATION 1136-1309 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK FROM FS 1126-1309. FABRICATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F RTA6WE 20040713000382004071300038EU 2004 7 13 USAASA04040 120040428A3260 CONNECTOR AIRBUSA319 A319112 3930323EU MLG DIRTY A USAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA19743UW 1277 CLT - FLT 83 - EN ROUTE CLT-SAN - DURING FLIGHT, THE CREW HEARD A NOISE COMING FROM THE NOSE LANDING GEAR AREA. A CHECK OF THE LANDING GEAR POSITION INDICATION REVEALED THAT THE NOSE LANDING DOORS WERE INDICATING AS AN AMBER 'X'. THE CREW RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A BITE CHECK OF THE SYSTEM AND FOUND NO FAULTS. THE NOSE LANDING GEAR DOOR SENSORS, TARGETS, AND CONNECTORS WERE CLEANED. A GEAR SWING WAS PERFORMED. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040713000392004071300039WP 2004 7 13 GTIA040347 120040409A5320 STIFFENER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - AFT PIT DOOR BEAM WEB STIFFENER STATION 1174 HAS CORROSION. FABRICATED STIFFENER. (M) 2L72 4F RTA6WE 20040713000452004071300045WP 2004 7 13 GTIA040343 120040406A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND COCKPIT FLOORBOARD POTTING COMPOUND AND DISBONDING. FABRICATE NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040713000472004071300047NM 2004 7 13 USAASB04049 120040503A77976131508551 WIRE HARNESS BOEING737 7373B7 1384580NM NR 2 ENGINE EGT FAULTY A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19376US 22955 PIT - FLT 991 - EN ROUTE FROM PHL TO DFW, SOUTH OF PIT, CREW REPORTED THE NR 2 ENGINE EGT SPIKED TO 1,000 DEGREES WITH THE RED OVERHEAT LIGHT ILLUMINATING. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW REDUCED POWER ON THE NR 2 ENGINE AND THE LIGHT EXTINGUISHED. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVD AND REPLACED THE NR 2 ENGINE EGT CORE HARNESS DUE TO MEGGER TEST IRREGULARITIES. RAN NR 2 ENGINE AT TAKEOFF POWER FOR SIX TO EIGHT MINUTES, THEN TAXIED AIRCRAFT AT HIGH POWER SETTING. ALL CHECKED NORMAL PER MM 77-21-00. (M) 2L72 4F RTA16WE 20040713000482004071300048 2004 7 13 USAASA04039 420040428A2565D30664109 SLIDE AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US 0922 CLT - THE MAIN CABIN ENTRY DOOR WOULD NOT ARM. THE SLIDE ARMED LIGHT WOULD FLASH ON AND OFF ON ECAM DOOR DISPLAY. ALSO, THE HANDLE WAS SPONGY. MAINTENANCE REPLACED THE MAIN CABIN ENTRY DOOR SLIDE/RAFT. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040713000492004071300049EU 2004 7 13 USAASA04042 120040503A2810D2821024300060 DISC AIRBUSA321 A321211 3930370EU CNTR FUEL CELL RUPTURED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19161UW 1403 ONT - FLT 46 - LAX-PHL, AFTER TAKEOFF, A FUEL IMBALANCE DEVELOPED, ACCOMPANIED BY A 'FUEL AUTO TRANSFER FAULT' MESSAGE. BY ABOUT FL180, THE IMBALANCE HAD REACHED 3,000 LBS, WITH THE LEFT WING LOSING FUEL. MANUAL FEED WAS SELECTED, BUT DID NTO HAVE ANY AFFECT. BY FL230, FLIGHT DECLARED AN EMERGENCY AND BEGAN TO RETURN TO FIELD AT LAX. THE FUEL IMBALANCE CONTINUED TO WORSEN, SO CREW OPTED TO LAND AT A CLOSER ALTERNATE AIRPORT. FLIGHT DIVERTED TO ONT. DURING APPROACH, RECEIVED A 'RIGHT WING TANK OVER FULL' OVER FULL MESSAGE. BY THE TIME THE AIRCRAFT REACHED THE GATE, THERE WAS A 9,000 POUND IMBALANCE AND FUEL WAS SPILLING OUT OF THE RIGHT WING VENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO LAX, WHERE THE CE2L72 4F RTA28NM 20040713000502004071300050NM 2004 7 13 USAASB04048 120040430A2150 FAN BLADE BOEING737 7373B7 1384580NM ACM ERODED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19518AU 23704 IAH - FLT 775 - EN ROUTE FROM PHL-IAH, AT FL310, THE CABIN ALTITUDE CLIMBED VERY SLOWLY TO 9,500 FEET. AT THIS TIME, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN IMMEDIATE DESCENT OT FL240. CABIN ALTITUDE BEGAN TO DESCEND AND STABILIZE AT 3,500 FEET. FLGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT IAH. NO OXYGEN MASKS WERE DEPLOYED. S/D MAINTENANCE INSPECTED AIRCRAFT AND FOUND IT IN SAFE CONDITION FOR MAINTENACNE FERRY FLIGHT FROM IAH TO PIT. MAINTENANCE IN PIT FOUND THE RIGHT TURBO FAN BLADES SEVERELY ERODED. REMOVED AND REPLACED RIGHT TURBO FAN ALONG WITH THE LEFT TURBO FAN. ALSO, REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND MIX VALVE, RIGHT PACK FLOW CONTROL VALVE, FORWA2L72 4F RTA16WE 20040713000532004071300053WP 2004 7 13 GTIA040346 120040402A5340 STRINGER CLIP DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND STATION 237 STRINGER 28 LEFT CLIP CRACKED. REMOVED CLIP. FABRICATED AND LOCATED HOLES. INSTALLED NEW CLIP. (M) 2L72 4F RTA6WE 20040713000542004071300054WP 2004 7 13 GTIA040354 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FUOND MAIN C/B CENTER FLOOR PANEL STATOIN 886-946 TWO RIVETS PULL THROUGH, CRACKED AT EXPANSION CHANNEL BOTH SIDES AND PUNCTURE HOLE. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040713000552004071300055WP 2004 7 13 GTIA040356 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL HAS DISBONDED AT HAT CHANNELS/RUB STRIPS, BARE METAL AT HAT CHANNEL, STATION 256-313, 313-398, 826-923, 923-1003, 1003-1079. REBONDED HAT CHANNEL. (M) 2L72 4F RTA6WE 20040713000572004071300057EU 2004 7 13 USAA040154 120040423A5310D5348015900500 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US 0922 BFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH BY 1.4 INCH BY .025 INCH, FRAME 69, -Y1732, -Z240. REMOVED AND REPLACED PLATE ASSEMBLY PER SRM 53-02-00, 51-77-10, 51-11-00, 51-72-11. CORROSION LEVEL 2, TASK NR JA-260-53500.(M) 2L72 4F RTA28NM 20040713000582004071300058EU 2004 7 13 USAA040153 120040423A5310D5347219020400 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US 0922 FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .023 INCHE DEEP, FRAME 66, -Y1292, -Z240. REMOVED AND REPLACED BEAM PE SRM 53-41-15, 51-74-00, 51-42-11. (M) 2L72 4F RTA28NM 20040713000602004071300060EU 2004 7 13 ASOA04305 120040323A5320S536780082162 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORT ON THE RIGHT SIDE BETWEEN FRAME 39 AND FRAME 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT ON THE RIGHT SIDE BETWEEN FRAME 39 AND FRAME 41 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040713000622004071300062EU 2004 7 13 ASOA04301 120040323A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FRAME 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOORBEAMS AT FRAME 38/39 IAW SRM 53-00-00. (M) 2H72 4T RTA53EU 20040713000632004071300063EU 2004 7 13 ASOA04300 120040323A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURNG A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040708002052004070800205WP 2004 7 8 MWEA040097 120040613A2420976J2526 GENERATOR DOUG DC9 DC981 3022081WP LEFT INOPERATIVE A MWEAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 GL31804ME 48030 AIRCRAFT CROSSTIE LOCKOUT ILLUMINATED WITH LEFT GENERATOR OFF LIGHT. REMOVED AND REPLACED LEFT ENGINE GENERATOR. 2L72 4F A6WE 20040708002062004070800206WP 2004 7 8 MWEA040094 120040615A552299378041 DOUBLER DOUG DC9 DC982 3022082WP LT ELEVATOR LIGHTNING STRIKEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LEFT ELEVATOR UPPER SKIN OUTBOARD AFT SKIN HAS AN AREA OF LIGHTNING STRIKE DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040709000142004070900014WP 2004 7 9 AALA20040705 120040702A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 12D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21450AA 49476 DFW - SEAT MOUNTED EMERGENCY LIGHT AT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000252004070900025WP 2004 7 9 AALA20040683 120040629A5248 RELEASE MECH DOUG DC9 DC982 3022082WP TAIL CONE INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21232AA 49179 LAX - TAIL CONE FAILED TO RELEASE. ADJUSTED TAIL CONE RELEASE SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000272004070900027WP 2004 7 9 AALA20040668 120040629A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21262AA 49290 SAT - FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040709000292004070900029 2004 7 9 AALA20040696 420040624A256570150970031 CYLINDER AIRBUS300 A300B4605R 3930308EU ESCAPE SLIDE FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 DURING SLIDE RAFT DEPLOYMENT TEST LEFT 4 DOOR FAILED TO FULLY OPEN. REPLACED EMERGENCY OPERATION CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040709000322004070900032EU 2004 7 9 AALA20040697 120040625A5310 BEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW217076A 610 TUL - NUMBER THREE GANGRY BEAM AT FRAME 52 IS CRACKED APPROXIMATELY .25 INCH LONG. AREA WAS MODIFIED PER ECO 1273AD TO ACCOMODATE NDT INSPECTION. ACCOMPLISHED ESO 30595 DATED JUNE 25, 2004 REPAIR NUMBER 40 531500 3477. CRACK STOP DRILLED AND HIGH FREQUENCY EDDY CURRENT CONFIRMED CRACKS TERMINATED IN STOP DRILL HOLE. REPAIR DOUBLER INSTALLED. 2L72 4F RTA35EU 20040709000402004070900040EU 2004 7 9 AALA20040695 120040623A5753 FLAP TRACK AIRBUS300 A300B4605R 3930308EU LEFT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2191050 423 TUL - NUMBER ONE LEFT HAND FLAP TRACK HAS LIGHT CORROSION INSIDE RADIUS AFT END OF NUMBER ONE FLAP TRACK ATTACH POINT BARREL NUT. CORRODED AREA IS ONE INCH BY ONE INCH. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004. 2L72 4F RTA35EU 20040709000512004070900051SO 2004 7 9 C2XA04SH423 120040705A532014529495005 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 53 TO 59. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000522004070900052SO 2004 7 9 C2XA04IA082 120040703A3350 LIGHT EMB 145 EMB145LR 3260212SO ROW 12 MALFUNCTIONED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040709000532004070900053SO 2004 7 9 C2XA04SH424 120040630A541114576631622 RIB EMB 145 EMB145ER 3260211SO NR 2 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE NR 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040709000552004070900055SO 2004 7 9 C2XA04SH4426 120040628A531514530634007 BUTTSTRAP EMB 145 EMB145ER 3260211SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 39-45. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712000162004071200016CE 2004 7 12 LX52004F00001 120040621A2910624833 PRESSURE SWITCH BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE HARTZLHCB4M HCB4MP3 GL HYD PWR PACK LEAKING E LX5AO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL19961LL2298 MX552250A FL264 PCEPK0268 FWA2851 DURING A SCHEDULED FLIGHT, THE PILOT NOTICED THE LOW HYDRAULIC FLUID LIGHT HAD COME ON. UPON APPROACH, THE GEAR WAS SELECTED DOWN AND THE POWER PACK RAN FOR 14 SECONDS THEN TRIPPED THE BREAKER. THE GEAR WAS THEN MANUALLY PUMPED DOWN AND PLANE LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUN THAT THE GEAR UP PRESSURE SWITCH WAS LEAKING INTRENALLY AND ALLOWING HYDRAULIC FLUID TO LEAK OUT OF THE VENT HOLE IN THE SWITCH. THIS IS WHAT CAUSED THE LOW HYDRAULIC FLUID LEVEL. UPON REPLACING THIS SWITCH THE SYSTEM OPERATED NORMAL. UNKNOWN WHAT CAUSED SWITCH TO GO BAD. 2L72 4T4 T A24CE E4EA 6 CP56GL 20040712000272004071200027 2004 7 12 USA2004F00062 420040603A2565 RELEASE MECH AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19711UW 1033 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT FORWARD SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2L72 4F4 FRTA28NM E2GL 20040712000282004071200028 2004 7 12 USA2004F00063 420040602A2565 RELEASE MECH AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19121UW 1294 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT FORWARD SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2L72 4F4 FRTA28NM E2GL 20040712000302004071200030EU 2004 7 12 SIMA200416201 120040607A3350MS274601 SWITCH SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21398AM 340B398 FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT ARMING BUTTON TO BE INOPERATIVE. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHT SWITCH IAW MFG MM. OPS CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (SW21200407466) 2L72 4T4 TRTA52EU E8NE 20040712000362004071200036CE 2004 7 12 BEM2004F00000 120040708A2430 BEARING BEECH 65 65 1152802CE LYC O720 IO720A1B 41546EA HARTZLHCM2Y HCM2YK GL ALTERNATOR FAILED E BEMAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 GL155078N134 90513C4 LF16 L149554A BJ1432 NR 1 ALTERNATOR WENT INOPERATIVE IN FLIGHT INVESTIGATION FOUND REAR ROTOR BEARING OF ALTERNATOR HAD NO GREASE AND FAILED. 1L72 3O3 O 3A20 1E15 5 CP43GL 20040712000402004071200040NM 2004 7 12 GAIA04084SD 120040611A24332299 TRU BOEING727 727243 138408DNM NR 1 OVERHEATED A GAIAO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 GL231269Y 21269 FIRE WAS REPORTED FROM NR 1 TRANSFORMER RECTIFIER UNIT (TRU), LOCATED IN FORWARD EE BAY. PWR HAD BEEN ON AC APPROX 1HOUR AND 30 MINUTES. FIRE WAS EXTINGUISHED AND TRU WAS REMOVED FROM AC. FIRE WAS CONTAINED WITHIN TRU WITH HEAT DAMAGE TO DRIP SHIELD LOCATED ABOVE TRU. REPLACED NR 1 TRU, REPLACED DAMAGED DRIP SHIELD, SEPARATED-CLEANED, INSPECTED WIRE BUNDLE ABOVE TRU, REMOVED DEBRIS AND CLEANED ALL SHELVES AND EE COMPARTMENT. INSPECTED EE COMPARTMENT FOR FIRE, HEAT OR SMOKE DAMAGE, ALL OK. MONITORED NR 1 TRU FOR 4 HOURS, ALL OK. AC WAS RETURNED TO SERVICE. (SW07200406999) DISASSEMBLED TO INSPECT AND REPAIR. FOUND CAUSE OF SHORT TO BE CAPACITOR, C1-C6 WHICH EXPLODED CAUSING EXTENSIVE DAMAGE. 2L73 4F RTA3WE 20040712000442004071200044 2004 7 12 USA2004F00066 420040602A31407024401901 MODULE EMB ERJ170ERJ170100 EU GE CF34 CF34* NE AVIONICS SYS SHORTED A USAAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19802MD496 17000013 AT APPROXIMATELY FORTY MILES OUTSIDE THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO AN ELECTRICAL BURNING ODOR IN THE COCKPIT. THE FLIGHT CREW DONED THEIR OXYGEN MASKS AND LANDED THE AIRCRAFT WITHOUT AN INCIDENT. FOUND MODULAR AVIONICS UNIT CIRCUIT BREAKER POPPED AND DC POWER SUPPLY 3 BURNT. REPLACED MODULAR AVIONICS UNIT ONE POWER SUPPLY 3 MODULE AND SERVICE OXYGEN. 2L74 4F4 FRTA56NM E15NE 20040712000472004071200047CE 2004 7 12 NZZ2004F00000 120040427A2820MS2874180184 HOSE BEECH 58 58 1152740CE CONT O520 IO520* 17032SO FUEL SYSTEM LOOSE E NZZAO OTHER KA FLUID LOSS FLAME/FIRE NRNOT REPORTED 1 GL0358MH 772 TH609 EXPERIENCED AN ENGINE FIRE DUE TO LOOSE FIREWALL TO FUEL PUMP INLET HOSE. HOSE LEAKED WHEN PRESSURIZED BY FUEL BOOST PUMP. ON TAXI OUR, ENGINE RAN ROUGH (AIR LEAKING). PILOT HIT BOOST PUMP, MOMENTAIRLY ENGINE SMOOTHED OUT AND CAUGHT FIRE. DAMAGE MOSTLY TO WIRE BUNDLE BEHIND ENGINE. (GL03200402723) 1L72 3O3 O 3A16 E5CE 20040712000552004071200055NM 2004 7 12 UIEA200400106 120040601A521065B0431128 DOOR BOEING747 7472D7B 1384803NM GE CF6 CF650* 30018NE R-4 CRACKED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 R-4 DOOR LOWER AFT CORNER HAS 2 CRACKS, ONE CRACK IS 4 INCHES AND THE OTHER CRACK IS 3 INCHES, STA 1715, W/L 199.8. CAUSE OF DAMAGE UNKNOWN. CRACKS FOUND DURING VISUAL INSPECTION. INSTALLED DOUBLER REPAIR IAW SRM. 2L74 4F4 FRTA20WE E23EA 20040712000642004071200064 2004 7 12 Y292004F00000 420040610A2562 ELT AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE CABIN ACTIVATED E Y29EO OTHER O OTHER NRNOT REPORTED 1 NM0388MX 183 ON GOING PROBLEMS WITH OUR ELT COMING ON IN FLIGHT FOR NO APPARENT REASON. THE PILOTS ARE USUALLY ABLE TO RESET FROM COCKPIT. REPLACED THE ELT UNIT 3 TIMES. TROUBLESHOT AND INSPECTED REST OF SYSTEM WITH NO FAULTS FOUND. WOULD LIKE TO KNOW IF THIS IS A PROBLEM ON OTHER MAKES AND MODELS. 2K73 4F4 FRTA50NM E44NE 20040712000932004071200093EU 2004 7 12 MALA040455 120040619A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15364PX 340B262 DURING 4K INSPECTION IN LCQ, FUSELAGE SKIN RIGHT SIDE HAS A GROUP OF DENTS FROM BS 307.5 TO 319.0 UNDER PAX WINDOW 1.5 FT TO FLOOR LEVEL APPROXIMATELY. MAINTENANCE REMOVED AND REPLACED NR 8 ICE GUARD, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SAAB SRM 51-10-10 & 53-70-10-2 AND IAW MESABA EO S53005. A/C RELEASE DATE 6/24/04. 2L72 4T RTA52EU 20040712001042004071200104EU 2004 7 12 MALA040460 120040609A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15367PX 340B271 BATTERY PACK P/N 61-0478-9, S/N ELB052 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1, PASSES CMM CHECKS. A/C RETURNED TO SERVICE 6/13/04. 2L72 4T RTA52EU 20040712001212004071200121SO 2004 7 12 C2XA04IA079 120040605A33507287100507 CONTROL PANEL EMB 145 EMB145ER 3260211SO EMERGENCY LIGHTSCONTAMINATED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MIDDLE EMERGENCY LIGHTS ON THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTION AT THE FLIGHT ATTENDANTS LIGHTING CONTROL PANEL, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20040712001282004071200128SO 2004 7 12 C2XA04SH400 120040630A531514522461011 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001322004071200132SO 2004 7 12 C2XA04CL066 120040627A1420 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714947 145054 CLE FLIGHT 3352, CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND FOUND A LOOSE CONNECTOR ON THE EMERGENCY LIGHT INVERTER. MAINTENANCE RESECURED THE CONNECTOR. SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4F RTT00011AT 20040712001332004071200133SO 2004 7 12 C2XA04SH385 120040622A531514522461011 DOUBLER EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP DOUBLERS AT FRAMES 20 AND 23 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001372004071200137SO 2004 7 12 C2XA04TY097 120040621A532014522459003 ANGLE EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE UNDER THE CARBON FIBER BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040712001392004071200139SO 2004 7 12 C2XA04SH386 120040623A532014521721009 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE CENTER FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AROUND A NUT PLATE HOLE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5320-01127. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001432004071200143 2004 7 12 SWAA041924 420040708A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040712001732004071200173NM 2004 7 12 ASMF2004027 120040622A2720 SENSOR DOUG MD80 MD83 3023681NM RUDDER OUT OF ADJUST W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23861LF 49826 DURING TRANSIT CHECK, CAPTAIN REPORTED "RUDDER TRAVEL UNRESTRICTED" LIGHT TURNED ON OCCASIONALLY IN FLIGHT. ELECTRICAL SYSTEM, INDICATION AND MECHANISM WERE CHECKED, ALL CORRECT. AIRCRAFT WAS DISPATCHED AND RETURNED TO PLATFORM, "RUDDER TRAVEL UNRESTRICTED" LIGHT TURNED OFF WHEN PEDALS WERE OPERATED. D1-33 AND D1-34 SENSORS WERE ADJUSTED IAW MM 27-20-06, TEST CORRECT. 2L72 4F RT 20040727000082004072700008WP 2004 7 27 04FDEA02151 120040722A5712ARB2440501 RIB DOUG DC10 DC1030 3023501WP ZONE 500 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25326FE 47813 LEFT WING I/B LEADING EDGE ACCESS PANEL 516FE RIB WITH CRACK. REMOVED AND REPLACED STIFFENER IAW SRM 51-35-01. 2L73 4F A22WE 20040713000062004071300006EU 2004 7 13 USAA040126 120040413A5310D5347218920200 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND BEAM CORRODED 2 INCHES LONG BY 1.5 INCHES WIDE BY .040 INCHE DEEP AREA, FRAME -Y1292 BETWEEN CROSSBEAM C68 AND C69. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000082004071300008EU 2004 7 13 USAA040139 120040412A5310D5347217320100 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND BEAM CORRODED 2 INCHES BY 1.5 INCHES BY .025 INCH AREA, Y-254, FR 66-68, -Z240. REMOVED AND REPLACED BEAM PE SRM 51-42-11, 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000092004071300009EU 2004 7 13 USAA040129 120040413A5310D5347218820400 CROSSBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND BEAM CORRODED 2.5 INCHES LONG BY 1.5 INCHES WIDE BY .03 INCH DEEP AREA, FRAME Y1732 BETWEEN CROSSBEAM C68 AND C69 -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M0 2L72 4F RTA28NM 20040713000142004071300014EU 2004 7 13 USAA040130 120040412A5310D5347112420100 SHEAR PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND SHEAR PLATE CORRODED 3.5 INCH IN DIAMETER AND .010 INCH DEEP AREA, FRAME 71292 BETWEEN CROSSBEAM C89 AND C70 -Z40. REMOVED AND REPLACED SHEAR PLATE PER SRM 51-74-00, 53-41-17 AND 51-42-11. (M) 2L72 4F RTA28NM 20040713000152004071300015WP 2004 7 13 ASAA0480323 120040421A575359367813 SUPPORT FITTING DOUG DC9 DC983 3022083WP LT TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FORWARD HINGE ARM OF LEFT INBOARD FLAP, OUTBOARD HINGE IS DINGED. REMOVED DAMAGE THEN PEENED, TREATED AND PRIMED AREA PER EA 5740-01389. (M) 2L72 4F RTA6WE 20040713000212004071300021EU 2004 7 13 USAA040143 120040416A5310D5347209300000 CROSSBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND CROSSBEAM CORRODED 1.3 INCHES BY 1.9 INCH BY .033 INCH AREA, C68, Y-765, AND -Z240. REMOVED AND REPLACED CROSSBEAM PER SRM 51-74-00, 53-00-15, 53-00-14. (M) 2L72 4F RTA28NM 20040713000232004071300023EU 2004 7 13 USAA040155 120040427A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND SILL PLATE ASSEMBLY CORRODED 5 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP, L2 DOOR SILL PLATE ASSEMBLY, Y1732 FORWARD OF FRAME 66. REMOVED AND REPLACED PER SRM 53-41-14, 53-41-11. (M) 2L72 4F RTA28NM 20040713000292004071300029EU 2004 7 13 USAA040159 120040423A5321D5367180500200 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND FLOOR PANEL CORRODED 1.5 INCH BY 2.5 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, Y1732, -Z240. REMOVED AND REPLACED FLOOR PANEL PER SRM 51-42-11, 51-74-00. (M) 2L72 4F RTA28NM 20040713000302004071300030EU 2004 7 13 USAA040152 120040423A5310D5347218920200 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND BEAM CORRODED 2 INCHES BY 1.6 INCHES BY .058 INCH DEEP AREA, FRAME 68, -Y1732, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040713000362004071300036EU 2004 7 13 USAA040156 120040423A5321D5367180500300 FLOORBOARD AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND FLOORBOARD CORRODED 1.3 INCHES BY 1.125 INCH BY .10 INCH DEEP, BETWEEN FRAME 66-68, -Y1732, -Z240. REMOVED AND REPLACED FLOORBOARD PER SRM 51-42-11, 51-74-00. (M) 2L72 4F RTA28NM 20040713000402004071300040WP 2004 7 13 GTIA040348 120040322A5320 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND LEFT MAIN CABIN CUSP WEB STATION 780, STATION 800, STATION 836, STATION 874, STATION 894 IS CORRODED. WEB AT STATOIN 836 TO 894 IS OUT OF LIMITS. REMOVED WEB. FABRICATED TWO SECTION CUSPS FROM STATION 807-845 AND 845-905. INSTALLED LEFT MAIN CABIN CUSP WEB. (M) 2L72 4F RTA6WE 20040713000462004071300046EU 2004 7 13 USAA040157 120040424A5321D5361060500100 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND FLOOR PANEL CORRODED 2 INCHES BY 38.5 INCHES BY 13 INCHES AND .5 INCH BY 10 INCH AREA, PANEL NR 222FF, FRAME 16-20, Y=-1732, Z=-240. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-02-00. CORROSION LEVEL 2, TASK NR JA-220-53300. (M) 2L72 4F RTA28NM 20040713000512004071300051WP 2004 7 13 GTIA040344 120040329A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP COCKPIT DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND COCKPIT FLOOR PANEL NR 4411A TOP METAL LAYER DISBONDING. CLEANED PANEL AND RESEALED. (M) 2L72 4F RTA6WE 20040713000802004071300080NM 2004 7 13 BJNA040201 120040221A2560ACREM1A MEGAPHONE BOEING737 7372K9 1384494NM AFT CLOSET INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11222TM 23404 AFT MEGAPHONE INOPERATIVE WOULD NOT TEST. REPLACED AFT MEGAPHONE IAW AMM 25-69-0. (M) 2L72 4F A16WE 20040713000812004071300081EU 2004 7 13 USAA040125 120040413A5347D5347217220390 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - OFUND SEAT TRACK CORRODED 2 INCHES BY 1.5 INCH BY .025 INCHE DEEP, FRAME 66-68, -Y1292, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-41-14, 53-00-14, 51-42-11, 51-74-00. (M) 2L72 4F RTA28NM 20040713000822004071300082EU 2004 7 13 USAA040140 120040410A5310D5347209000200 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND BEAM CORRODED 2 INCHES BY 2 INCHES BY .020 INCH DEEP, BETWEEN FRAME 64 AND 65, Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14, 51-74-00, 51-42-11. (M) 2L72 4F RTA28NM 20040713000832004071300083EU 2004 7 13 USAASA04041 120040430A21332079002AC OUTFLOW VALVE AIRBUSA319 A319112 3930323EU CABIN PRESSURE FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19753US 1326 CLT - FLT 9215 - FERRY FLIGHT FROM MHT-CLT, EN ROUTE, WHILE AT FL390, THE AIRCRAFT EXPERIENCED A NR 1 CABIN PRESSURIZATION FAILURE, FOLLOWED TEN SECONDS LATER BY A NR 2 CABIN PRESSURIZATION FAILURE. A RAPID DESCENT WAS MADE TO 10,000 FEET. AFTERWARDS, THE FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OUTFLOW VALVE. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040713000842004071300084NM 2004 7 13 USAABB04041 120040428A335020131A BATTERY PACK BOEING757 7572B7 1384964NM PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19627AU 27805 CLT - THE EMERGENCY LIGHT OVE THE R1 AND FORWARD LAVATORY WERE FOUND INOPERATIVE. MAINTENANCE INSTALLED A NEW BATTERY PACK. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA2NM 20040713000852004071300085NM 2004 7 13 USAA040161 120040429A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US40473 24555 PIT - FOUND BEAM CAP CORRODED 1 INCH AREA, BS 986 RBBL 10. CUT OUT CORRODED SECTION OF BEAM UPPER CAP AND SPLICED IN NEW PER TYPICAL REPAIR 53-60-01 REV A. (M) 2L72 4F RTA16WE 20040713000942004071300094WP 2004 7 13 AMTA200400018 120040106A5210 CONTROL ROD LKHEED1011 10113853 5265020WP PAX DOOR OUT OF ADJUST A AMTAK NONE O OTHER ININSP/MAINT 1 GL11163AT 1229 L1 PASSENGER DOOR WILL NOT OPEN IN EMERGENCY MODE FROM EXTERNAL HANDLE. FOUND ACTUATOR CONTROL ROD OUT OF AJDUST. RIGGED PER MM 52-12-24. DOOR NOW OPS CHECKS GOOD FROM INSIDE AND OUT. OK FOR SERVICE. (M) 2L73 4F A23WE 20040713000952004071300095NM 2004 7 13 USAABB04005 120040112A33509221009 BATTERY BOEING757 7572B7 1384964NM R4 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19623AU 27244 PHL - FOUND R4 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA2NM 20040713001012004071300101SO 2004 7 13 SIMA200412704 120040501A2120 ODOR EMB 135 EMB135LR 3260305SO COCKPIT DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21720AE 145279 JFK - FLT 4754 - DURING CLIMB, CREW REPORTED A STRONG BURNING ODOR IN COCKPIT. AIRCRAFT WAS RETURNED TO JFK AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK OF THE PACKS WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040713001022004071300102SO 2004 7 13 SIMA200412002 120040426A2120 ODOR EMB 145 EMB145 3260210SO CABIN DETECTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21612AE 145079 GSO - FLT 3625 - CREW REPORTED A MILD IRRITANT ODOR IN CABIN. SMELLS LIKE EUCALYPTUS OIL OR VICKS VAPOR RUB. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. GROUND RAN AIRCRAFT WITH CREW TO ISOLATE ANY ODORS. NO ODORS NOTED FROM EITHER PACK OR BLEED SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040713001032004071300103SO 2004 7 13 SIMA200413002 120040509A27403621005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZONTAL STAB MALFUNCTIONED A SIMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW21642AE 145193 ORD - FLT 4142 - DURING APPROACH CREW REPORTED A DUAL PITCH TRIM FAILURE WITH AUTO PILOT ON AFTER SELECTING FLAPS TO 9 DEGREES. IAS WAS 210 KNOTS IN SMOOTH AIR IN VMC CONDITIONS LEVELING OFF AT 5000 FEET. NO CONTROL COLUMN FORCE WAS FELT DUE TO AUTO PILOT BEING ON. REPLACED HSCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040713001072004071300107SO 2004 7 13 SIMA200412702 120040503A49204504113 APU EMB 135 EMB135LR 3260305SO APU BAY FAILED A SIMAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21734EK 145371 RIC - FLT 4507 - DURING TAXI CREW RECEIVED APU GEN OFF BUSS MESSAGE. RESET GENERATOR WHILE PARKING AIRCRAFT. DC BUSS FAILED CAUSING NUMEROUS ELECTRICAL WARNINGS AND NOTICED SMOKE FROM RIGHT SIDE OF AIRCRAFT. APU SHUTDOWN AND FIRE BOTTLE EXTINGUISHED. SMOKE IN CABIN WAS EVIDENT. NO FIRE EVIDENCE WAS NOTED. AIRCRAFT WAS INSPECTED AND FERRIED TO BGR FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB MM. OPS AND LEAK CHECKS WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. APU FIRE BOTTLE WAS ALSO REPLACED. (M) 2L72 4F RTT00011AT 20040713001082004071300108SO 2004 7 13 SIMA200412003 120040426A21508152403 ACM EMB 145 EMB145LR 3260212SO CABIN COOLING SEIZED A SIMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21652RS 145432 ORD - FLT 4023 - AFTER RETURNING TO THE GATE, THE CREW REPORTED THE CABIN FILLING WITH SMOKE. MAINTENANCE FOUND AN AIR CYCLE MACHINE SEIZED. THE AIR CYCLE MACHINE WAS REMOVED AND REPLACED IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040713001092004071300109SO 2004 7 13 SIMA200412108 120040429A779723062387 WIRE HARNESS EMB 145 EMB145LR 3260212SO NR 2 ENGINE CHAFED A SIMAO OTHER O OTHER CRCRUISE 1 SW21625AE 145115 ORD - FLT 4136 - CREW REPORTED A FLAME OUT IN SMOOTH AIR LEVEL AT FL280 JUST AFTER LEVEL OFF. THRUST LEVERS HAD NOT BEEN MOVED FROM THRUST SET POSITION IN CLIMB MODE. LOSS N1, N2, AND ITT. IGNITION A/B CAME ON ABOUT 30 SECONDS BETWEEN EVENTS. NO PRECIPATATION REPORTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE EXTERNAL CONTROL B HARNESS IAW EMB MM. AN FCF WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040713001112004071300111EU 2004 7 13 SIMA200413205 120040422A3260CM328 BULB SAAB SF340 340B 7860101EU MLG INDICATOR INOPERATIVE A SIMAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW21284AE 340B284 LAX - FLT 3080 - ON APPROACH, WHEN SELECTED LANDING GEAR DOWN, LEFT WOULD NOT INDICATE WITH GREEN LIGHT. FOLLOWED AOM PROCEDURES, PERFORMED EMERGENCY GEAR EXTENSION, STILL NO GREEN LIGHT. RELAMPED BULB, NO FIX. DID A FLYBY AND GEAR APPEARED DOWN AND LOCKED. RAI LIGHT BULB IN LEFT MLG INDICATOR. OPS CHECK GOOD. (M) 2L72 4T RTA52EU 20040713001132004071300113NM 2004 7 13 GAIA04073OP 120040515A33501000677 LIGHT BOEING727 727214 138407RNM EMERGENCY EXIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07750US 21512 FOUND EMERGENCY EXIT LIGHT OVER COCKPIT DOOR, BATTERY LOW. REMOVED COCKPIT EMERGENCY LIGHT FOR RECHARGING. INSTALLED NEW EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040713001162004071300116NM 2004 7 13 USAA040162 120040429A5711 SPAR BOEING737 7374B7 1384702NM WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US49473 24555 PIT - FOUND UPPER SPAR CRACKED .21875 INCH, RSS 222.5 REAR SPAR UPPER CHORD FITTING AT MLB BEAM. OVERSIZED FASTENER HOLE TO REMOVE CRACK AND INSTALLED FREEZE PLUG PER EA 78361. (M) 2L72 4F RTA16WE 20040713001182004071300118NM 2004 7 13 USAABB04018 120040206A335086210066 BATTERY BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19630AU 27808 PHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 9, 13, 18, 29 AND 33 FAILED BATTERY CHECK. MAINTENANCE REPLACED THE BATTERIES IN LOW LEVEL EMERGENCY LIGHTS FOR SEAT ROWS 9, 13, 29 AND 33. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040713001192004071300119NM 2004 7 13 USAABB04040 120040426A2120 ODOR BOEING757 757225 1384959NM CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA19605AU 22201 PIT - FLT 1275 - ON TAKEOFF OUT OF PHL, CREW REPORTED A FAINT ELECTRICAL ODOR AROUND THE L2 DOOR. AFTER TAKEOFF, ODOR DISSIPATED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT PIT. MAINTENANCE CHECKED ELECTRICAL SYSTEM AROUND THE L2 DOOR, INCLUDING THE CIRCUIT BREAKERS. CHECKED ABOVE CEILING PANELS AND COULD NOT FIND OR DUPLICATE SOURCE. MAINTENANCE SUSPECTS RUNWAY ODOR. (M) 2L72 4F RTA2NM 20040713001212004071300121EU 2004 7 13 USAABA04011 120040404A3350321430 BATTERY AIRBUS330 A330323 3930335EU R3 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19670UW 0315 PHL - FOUND R3 DOOR EPSU FAILED. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA46NM 20040713001252004071300125EU 2004 7 13 USAA040123 120040410A5320D53471124201 WEB AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND WEB CORRODED 1.5 INCHES BY 1.5 INCH BY .005 INCH AREA, BETWEEN FRAME 69 AND FRAME 70 BL Y1292. REMOVED AND REPLACED WEB PER SRM 53-41-17, 51-74-00, 51-42-11, 51-72-11. (M) 2L72 4F RTA28NM 20040713001302004071300130EU 2004 7 13 ASOA04303 120040323A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A C-CHECK IN YUL, THE SEAT TRACKS AT FRAME 36-39 AND FRAME 39-40 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS AT FRAME 36 TO 39 AND FRAME 39 TO 40 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20040713001312004071300131EA 2004 7 13 ASOA04296 120040426A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040713001322004071300132EA 2004 7 13 ASOA04294 120040426A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP AS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR BOTTOM STEP IAW SRM 51-74-00. (M) 2L72 4F RTA21EA 20040713001342004071300134WP 2004 7 13 WX0400008 120040430A3397 CIRCUIT BREAKER DOUG DC9 DC987 3022087WP GRD SRVC BUSS TRIPPED A WXOAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 WP17945MA 49725 TEN TO FIFTEEN MINUTES INTO THE FLIGHT FROM IFP TO EUG, THE LEAD FLIGHT ATTENDANT INFORMED THE CAPTAIN THAT ALL THE OVERHEAD CABIN LIGHTS WERE OUT. THE FLIGHT WAS DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE L5 CIRCUIT BREAKER ON THE GROUND SERVICE BUSS POPPED. THE CIRCUIT BREAKER WAS RESET AND THE SYSTEM FOUND TO OPERATE NORMALLY. THE WORK WAS DONE IAW AMM 33-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20040713001352004071300135EU 2004 7 13 ASOA04299 120040323A5320 BRACKET AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A C-CHECK IN YUL, THE BRACKET AT FS 39, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT FRAME 39, STRINGER 14R IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040713001362004071300136EA 2004 7 13 ASOA04298 120040426A7830M835362028M RELAY CNDAIRCL600 CL6002B19 1900309EA LT ENGINE MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO11908EV 764 DURING DESCENT INTO DFW FROM LBB, AT APPROXIMATELY 27,000 FEET A LEFT ENGINE REVERSER UNLOCK MESSAGE WAS RECEIVED. THE QRH WAS COMPLIED WITH AND AN EMERGENYC WAS DECLARED. NO UNUSUAL DESCENTS OR APPROACH SPEEDS WERE NECESSARY. THE AIRCRAFT LANDED SAFELY IN DFW. AFTER ENGIEN INSPECTION BY FIRE SERVICE PERSONNEL, THE AIRCRAFT TAXIED SAFELY TO THE GATE. MAINTENANCE REMOVED AND REPLACED A RELAY INSIDE JUNCTION BOX THREE AND THE POWER DRIVE UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040713001372004071300137EA 2004 7 13 ASOA04297 120040426A5300 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING AN A-CHECK IN BTR, THE LEFT DOUBLER AT FS 640, STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT DOUBLER AT FS 640, STRINGER 9. (M) 2L72 4F RTA21EA 20040713001412004071300141EU 2004 7 13 USAA040124 120040413A5310D5347219021100 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND BEAM TRACK ASSEMBLY CORRODED 1.5 INCHES IN DIAMETER BY .03 INCH DEEP AREA, FRAME 1292 AND CROSSBEAM C66 -Z240. REMOVED AND REPLACED TRACK BEAM ASSEMBLY PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040713001432004071300143NM 2004 7 13 USAABB04016 120040206A335020121 CHARGER BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19622AU 27201 TPA - FOUND THE R3 AND R4 DOOR EXTERIOR EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040713001492004071300149NM 2004 7 13 BJNA040102 120040128A1420 CONNECTOR BOEING737 737282 13844ATNM BATTERY CHARGER INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A MAINTENANCE WALKAROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTORS ON THE FORWARD BATTERY CHARGER AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKED NORMAL. WORK IAW MANUFACTURES MM 33-51-11. (M) 2L72 4F RTA16WE 20040713001502004071300150EU 2004 7 13 ASOA04313 120040413A5320 INTERCOSTAL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE INTERCOSTAL FROM FS 38 TO FS 39 ON THE LEFT SIDE UNDER THE THRESHOLD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL FROM FS 38 TO FS 39 ON THE LEFT SIDE UNDER THE THRESHOLD IAW SRM 51-25-01. (M) 2H72 4T RT 20040713001512004071300151NM 2004 7 13 USAASB04047 120040427A2133322684007 OUTFLOW VALVE BOEING737 737401 1384701NM E/E COMPT MALFUNCTIONED A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19423US 23990 AFTER CLIMB EN ROUTE, CABIN ALTITUDE WARNING HORN SOUNDED. CREW STATED THEY LOST CABIN PRESSURE & WERE UNABLE TO CONTROL IN ANY MODE. PERFORMED EMERGENCY DESCENT. FLT DIVERTED & LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINT FOUND FWD OUTFLOW VALVE WOULDN`T CLOSE. R & R FWD OUTFLOW VALVE & OPS CK PER MM. AFT OUTFLOW VALVE LEAKING AT VALVE DOOR EDGE. R & R AFT OUTFLOW VALVE & OPS CK & LEAK CK PER MM. 26 BELLY DRAINS LEAKING, FWD CARGO DOOR THRESHOLD CRACKED & FWD GALLEY DOOR LEAKING. REPAIRED BELLY DRAINS, THRESHOLD & GALLEY DOOR. PERFORMED SINGLE PACK CONFIDENCE CK. ALL CHECKS GOOD. HULL LEAK RATE IS NOW 4 PSI TO 2.5 PSI IN 100 SECONDS. SUCCESSFUL TEST FLT TO FL350. CABIN PRESSURE OPS NORMAL. 2L72 4F RTA16WE 20040713001532004071300153NE 2004 7 13 GTIA040011 220040115A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RIGHT FLAMED OUT A GTIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL23812NK 48021 708450 RT ENG FLAMED-OUT, AIR RETURN AT 800 TO 1000 MLS RT ENG EPR DROPPED BELOW 1.2 EPR, ARTS FIRED BASES X-TERED TO LT GENERATORS ACCOMPLISHED QRH ITEMS PULLED CVR C/B. PERFORMED ENG HI-POWER TRIM CHECKRUN ENG OPS CK NORM. R & R NR 2 ENG FUEL CONT, OPS CK GOOD. R & R FUEL PUMP ON N2 2 ENG, OPS CK GOOD. BORESCOPED PER 72-00-04, NO DEFECTS FOUND. PERFORMED INSP, ON NR 2 ENG INLET & EXHAUST AREAS FOR DAMAGED INSP FCU REAR TUBE FOR DAMAGE AND MOISTURE, ENG FUEL PUMP AND CTRL FILTER FOR MOISTURE, SUMP TANKS FOR WATER CONTAM. A FILTER INSP FOR DEBRIS PLUS SAMPLE OF FUEL, FUEL PUMP A FCA FILTER NO CONTAM, NO DEFECTS FOUND. PERFORMED BORESCOPE INSP, NO DEBRIS FOUND, ENG START, ENG FLAME OUT INSPECTION, OPS CK GOOD. 2L72 4F4 F A6WE E9NE 20040713001542004071300154GL 2004 7 13 2004F00157 220040131A731499144251 PUMP CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LEFT ENGINE FAILED A UG8AO OTHER O OTHER TXTAXI/GRND HDL 1 GL235115 7500018 'FUEL BOOST ON' AMBER CAS MESSAGE CAME ON IMMEDIATELY AFTER LANDING. LEFT ENGINE FUEL BOOST PUMP FAILURE. REMOVED FAULTY PUMP AND INSTALLED NEW SERVICEABLE UNIT. PERFORMED RUN-UP LEAK CHECK PER CESSNA MM. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J4 FRTT00007WITE6CH 20040713001552004071300155 2004 7 13 2004F00158 420040126A34426226523208 CONTROLLER BEECH 1900 1900D 1154162CE TRANSPONDER SHORTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO1987550 UE205 FLT 9194 - FLL/FPO, AFTER TAKEOFF, ELECTICAL SMOKE APPEARED FROM THE DASHBOARD. RETURNED TO FLL. LANDED WITHOUT INCIDENT. FOUND TRANSPONDER CONTROL HEAD SHORTED INTERNALLY. REMOVED AND REPLACED TRANSPONDER CONTROL HEAD. OPS CHECK NORMAL. NO DEFECTS NOTED. (M) 2L72 4T RTA24CE 20040713001562004071300156CE 2004 7 13 2004F00159 120040126A3240 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A GUUAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO1987551 UE206 FLT 9281 - MIA/MCO - WHEN LEFT BRAKE APPLIED, AIRCRAFT WILL NOT STOP. RETURNED TO GATE. PERFORMED BRAKE SYSTEM BLEEDING. OPS CHECK NORMAL. (M) 2L72 4T RTA24CE 20040713001602004071300160WP 2004 7 13 ASAA0480250 120040404A531359360501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING LONGERON 30 CORRODED STATION 1231 TO 1212. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP IAW MD80 SRM 53-02. (M) 2L72 4F RTA6WE 20040713001662004071300166NM 2004 7 13 2004F00161 120040210A33506038443 POWER SUPPLY DHAV DHC8 DHC8103 1386005NM EMERGENCY LIGHT INOPERATIVE A GULCK NONE L NO TEST ININSP/MAINT 1 WP13808WP 026 HNL - FOUND FORWARD EMERGENCY EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT POSITION 3351 PS1. OPS CHECK GOOD IAW DHC-8 MM 33-51-00 PAGES 201-202. (M) 2H72 4T RTA13NM 20040713001712004071300171EA 2004 7 13 ASOA04322 120040429A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO11862AS 7476 FLT 4522 - DURING APPROACH FROM ATL-GTR, A FLAPS FAIL MESSAGE WAS RECEIVED AFTER SELECTING THE FLAPS TO THIRTY DEGREES. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. DUE TO A DEFERRED RIGHT THRUST REVERSER AND A SHORTER RUNWAY AT GTR, THE AIRCRAFT DIVERTED TO CMB, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNTI (FECU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040713001752004071300175NE 2004 7 13 UIEA200400090 220040504A753273836222 BLEED VALVE BOEING747 747228F 1384895NM GE CF6 CF650C2 30018NE NR 2 ENGINE MALFUNCTIONED A UIEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15536MC 21576 DURING CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. NR 2 ENGINE SUSTAINED 6 OR MORE HARD COMPRESSOR STALLS WHILE CLIMBING THROUGH 18,000 FT TO 24,000 FT. INSPECTED INTAKE/EXHAUST AREAS, NIL DISCREPANCIES. CHIP DETECTORS CLEAN REMOVED AND REPLACED SAME 8TH STAGE CHECK VALVE AFTTER INSPECTION. ALL OK. CHECKED ALL DUCTS ENGINE AREA FOR LEAKS/CHECKED DUCTS ETC. NIL DISCREPANCIES NOTED. STALL INSPECTIONS COMPLETED PER L/P 522816 NR 1. AIRCRAFT WAS DIVERTED TO FCO/PIK. (M) 2L74 4F4 F A20WE E23EA 20040713001802004071300180EA 2004 7 13 A6WA200460014 220040509A7321216381031 FUEL CONTROL BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502* 41580EA NR 3 ENGINE FLUCTUATES A A6WAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL31611AW E3120 LF05575AC WHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 8 PERCENT, N1 26, 10 PSI, OIL QUANT 3/4 FULL. MAINTENANCE REMOVED AND REPLACED NR 3 FUEL CONTROL UNIT IAW AMM. (M) 2H74 4F4 FRTA49EU E6NE 20040713001812004071300181EA 2004 7 13 A6WA200440013 120040505A27507455001 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31460AW 7867 ON DEPARTURE OUT OF IND, FLAP FAIL CAS MESSAGE, ED1 AND FLIGHT CONTROL PAGE SHOWS FLAP FAIL AT 8 DEGREES, RAN QRH DIVERTED TO MKE. REPLACED FLAP CONTROL LEVER AND RIGGED LEFT PBSU PER AMM 27. OPS CHECK NORMAL. (M) 2L72 4F RTA21EA 20040713001832004071300183EA 2004 7 13 ASOA04321 120040428A5210601R386493 CONTROL ROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11850AS 7355 FLT 4708 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO CLISE AND THE DOOR HANDLE DIFFICULT TO STOW. MAINTENANCE ADJUSTED THE PASSENGER DOOR FLAPPER CONTROL ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040713001862004071300186EA 2004 7 13 ASOA04307 120040427A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11846AS 7328 DURING HANGAR MAINTENANCE IN BTR, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. (M) 2L72 4F RTA21EA 20040713001872004071300187EU 2004 7 13 2004F00162 120040213A2910 FITTING AIRBUS320 A320233 3930329EU HYD SYSTEM LEAKING A RJEFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO23453TA 747 CREW REPORTED HYD G+Y LOW PRESSURE. A/C RETURNED TO STATION FOR INSP. A/C LANDED WITHOUT INCIDENT. MAINT TECHS VERIFIED HYD SYS & PERFORMED INSP ON AFT BLKHD AREA PER AMM & FOUND LEAD SOURCE ON YELLOW SYS FITTING AT REAR BULKHEAD, PART CRACKED. ELBOW FITTING REPLACED PER AMM & EO A320RP29-005/03 R1. PTU REPLACED PER AMM. HYD SYS TESTED PER AMM, DURING TESTS ECAM WARNING SYS SHOWED HYD LOW PRESS IND OF ENG PUMP NR 1. R & R LOW PRESS SWITCH ON ENG NR 1 PER AMM & PERFORMED A NEW TEST PER AMM. ALL SYSTEMS NORMAL. OVERWEIGHT LANDING REPORTED, DMU CARD VERIFIED & ALSO AIDS SYS REPORT 15. AIRCRAFT RETURNED TO NORMAL OPERATION. 2L72 4F RTA28NM 20040713001892004071300189EU 2004 7 13 ASOA04312 120040413A5320 INTERCOSTAL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE INTERCOSTALS FROM FS 36 TO FS 38 UNDER THE LEFT AND RIGHT THRESHOLDS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS FROM FS 36 TO FS 38 UNDER THE LEFT AND RIGHT THRESHOLDS IAW SRM 51-25-01. (M) 2H72 4T RT 20040713001912004071300191EU 2004 7 13 ASOA04309 120040413A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE AFT CARGO SEAT TRACK ON THE RIGHT SIDE BETWEEN FS 41 AND FS 42 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT CARGO SEAT TRACK ON THE RIGHT SIDE BETWEEN FS 41-42 IAW SRM 51-25-04. (M) 2H72 4T RT 20040713001922004071300192EA 2004 7 13 A6WA200440060 120040422A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31433AW 7289 FOUND RIGHT FS 718 BETWEEN STRINGERS 11 AND 12 HAS A CRACK ON FRAME FLANGE. TRIMMED OUT SECITON OF FRAME FLANGE, PERFORMED LPI OF CUT LINES TO VERIFY ALL DAMAGE WAS REMOVED AND NO CRACKS EXIST. FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED REPAIR PARTS IAW BOMBARDIER 601R-53-61-193. REV A. (M) 2L72 4F RTA21EA 20040713001932004071300193WP 2004 7 13 ASAA0480316 120040421A53219957918524 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND METAL FLOORBOARD AT STATION 1003-1079 IS CRACKED. REMOVED DAMAGE AND INSTALLED PRP DOUBLER PER SRM 51-10-3. (M) 2L72 4F RTA6WE 20040713001942004071300194WP 2004 7 13 ASAA0480324 120040421A5730ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP WING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND FUEL ACCESS PANEL 1355C HAS ONE ELONGATED HOLE. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040713001962004071300196EU 2004 7 13 SIMA200412106 120040421A53117253813485 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21341SB 340B341 ABI - DURING AN MBV INSPECTION FRAME 677 WAS FOUND TO BE DENTED 3.5 INCHS AND 14 INCH ABOVE THE FLOOR. REMOVED FRAME 677 AND INSTALLED NEW FRAME IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 51-40-40, 51-40-22, 51-40-23 AND 51-40-40. (M) 2L72 4T RTA52EU 20040713001982004071300198NE 2004 7 13 AMTA200400526 220040505A7200 ENGINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B NE NR 2 VIBRATION A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11188AT 193C1078 NR 2 ENGINE EXPERIENCED A SUDDEN INCREASE IN VIBRATION FROM .8 TO 2.5 WITH A SELECTED. WARNING LIGHT WAS ON. SELECTED B DID NOT HELP SHUTDOWN ENGINE AT 1350Z ENGIEN CONTINUED TO WINDMILL AT APPROX 14 PERCENT N1 PLUS MADE OIL PRESS B2 + C2 ATM'S RUN CONTINUOUS REF DISC 7230/689 AND 7230-689 FAN COMPRESSOR DISC CHNGE PER M11-72-34. ENG OK FOR SERVICE. OPS AND LEAK CHECK PER M11-71-02. NO DEFECTS. (M) 2L73 4F4 F A23WE E12EU 20040713002002004071300200WP 2004 7 13 ASAA0480320 120040421A53209915554416 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK FOUND INTERCOSTAL AT STATOIN 769-788, LONGERON 28R IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW PER SRM 51-30. (M) 2L72 4F RTA6WE 20040713002022004071300202WP 2004 7 13 ASAA0480319 120040421A53209910151100 CUSP WEB DOUG DC9 DC983 3022083WP FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND RIGHT CUSP WEB CORRODED AT STATION 984-1003. REMOVED DAMAGED WEB AND INSTALLED NEW PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040713002042004071300204WP 2004 7 13 ASAA0480317 120040421A53159957918524 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DRING HV CHECK, FOUND METAL FLOORBOARD CHANNEL SUPPORT AT STATION 1003-1079 IS CRACKED. REMOVED DAMAGE AND INSTALLED RPR SPLICES AND ANGLES PER SRM 53-01. (M) 2L72 4F RTA6WE 20040713002062004071300206WP 2004 7 13 ASAA0480314 120040421A531359360501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND UNDERSIDE OF LONGERON 30 AT STATION 1200 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 53-2. (M) 2L72 4F RTA6WE 20040713002082004071300208EA 2004 7 13 ASOA04308 120040427A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11875AS 7559 DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M) 2L72 4F RTA21EA 20040709001052004070900105SO 2004 7 9 C2XA04IA028 120040309A3230 WARNING LIGHT EMB 145 EMB145ER 3260211SO MLG ILLUMINATED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714940 145033 DURING CLIMB THE CREW REPORTED THAT THE LANDING GEAR DISAGREE WARNING ILLUMINATED WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LANDING GEAR OPERATIONAL TESTS AND COULD NOT DUPLICATE THE DISCREPANCY. THE DISCREPANCY WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040712000142004071200014 2004 7 12 USA2004F00061 420040603A2565 RELEASE MECH AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE GIRT BAR MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19711UW 1033 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT REAR SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2L72 4F4 FRTA28NM E2GL 20040712000182004071200018EU 2004 7 12 ALG2004F00037 120040614A1420 CONNECTOR UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE GENERATOR DIRTY E ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW03523AL 1262 34281 ON TAKE OFF, THE GENERATOR LIGHT ILLUMINATED, RESETTING THE GENERATOR AND ELECTRICAL SWITCHES HAD NO EFFECT. MAINTENANCE CLEANED CONNECTOR AND OPS CHECK WAS GOOD. 1G72 3U3 UNCR0001RD E34NE 20040712000332004071200033 2004 7 12 USA2004F00064 420040603A2565 STRAP AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19704US 0922 THE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE LT FORWARD ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP. 2L72 4F4 FRTA28NM E2GL 20040712000412004071200041NM 2004 7 12 UIEA200400098 120040525A324026056623 BRAKE BOEING747 7472D7B 1384803NM GE CF6 CF650* 30018NE LT MLG DAMAGED G UIEAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 EA15524MC 21784 GT9813/24 RME/JFK BRAKE TEMPERATURE OVERHEAT LIGHT: BRAKE TEMPERATURE OVERHEAT LIGHT ILLUMINATED DURING TAXI-IN. LEFT BODY, LEFT REAR BRAKE TEMPERATURE APPROXIMATELY INDICATING 7.40. FOUND NR 7 BRAKE DAMAGED, REMOVED AND REPLACED SAME IAW MM, LEAK CHECKS GOOD. ACCOMPLISHED INSPECTION , ALL NORMAL. 2L74 4F4 FRTA20WE E23EA 20040712000422004071200042 2004 7 12 USA2004F00070 420040526A23304976500001 VIDEO MONITOR BOEING767 767201 1385125NM GE CF6 CF680 30025NE AFT CABIN FAULTY A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19648US45911 23900 PASSENGER REPORTED THAT THE AFT VIDEO MONITOR EMITTED A MOMENTARY PUFF OF SMOKE AND THEN BLANKED OUT. THE CREW SECURED THE VIDEO SYSTEM. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE VIDEO SYSTEM AND MONITOR WERE OPERATED FOR APPROXIMATELY FORTY-FIVE MINUTES WITH NO DISCREPANCIES NOTED. THE MONITOR WAS REPLACED AS A PRECAUTION. 2L72 4F4 FRTA1NM E13NE 20040712000582004071200058SO 2004 7 12 SIMA200417201 120040619A2701 YOKE EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL COCKPIT VIBRATION A O OTHER E VIBRATION/BUFFET CRCRUISE 1 SW21624AE 145111 DURING CLIMB AND MOST OF FLIGHT INTO MQT, CREW NOTED A SLIGHT VIBRATION ON BOTH YOKES. NOTE: VIBRATION WAS AT AIRSPEEDS OF 230-310. AUTO PILOT ON/OR OFF HAD NO AFFECT. REPLACED LEFT AILERON BUSHING AND HARDWARE. PASSED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 FRTT00011ATTE6CH 20040713001882004071300188EA 2004 7 13 ASOA04283 120040413A3260 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA MLG ILLUMINATED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11724EV 10138 DURING TAKEOFF FROM SAT-DFW, THE CREW RECEIVED A GEAR DISAGREE WARNING AFTER SELECTING THE GEAR UP POSITION. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO SAT, LANDING SAFELY. MAINTENANCE FOUND MAINTENANCE DIAGNOSTIC COMPUTER (MDC)FAULTS FOR ALL THREE GEAR UPLOCK FAR. MAINTENANCE PERFORMED TWENTY GEAR SWINGS AND ALSO INPECTED THE DOWN AND UPLOCKS, GEAR SELECTOR VAVLE, ELECTRICAL AND HYDRAULIC CONNECTIONS FOR SECURITY. NO DEFECTS WERE NOTED. THE MDC SHOWED NO FURTHER FAULTS IN OPERATION. AIRCRAFT OK FOR SERVCE. (M) 2L72 4F RTA21EA 20040712000602004071200060SO 2004 7 12 SIMA200417205 120040617A5510KSC357620V BEARING EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL HORIZONTAL STAB WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21622AE 145108 DURING MBV INSPECTION, THE RT AND LT HORIZONTAL STABILIZER HINGE BEARINGS WERE FOUND TO HAVE PLAY. REMOVED AND REPLACED RT AND LT HORIZONTAL TO VERTICAL SPHERICAL BEARINGS IAW MFG AMM AND SB. 2L72 4T4 FRTT00011ATTE6CH 20040712000622004071200062CE 2004 7 12 GUU2004F00023 120040610A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT STAB ELEVATORCORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178755016609 UE205 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVTOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040712000742004071200074 2004 7 12 MALA040467 420040616A34506226137001 RECEIVER SAAB SF340 340B 7860101EU NR 1 NAVAGATION ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15429XJ 340B429 AFTER STARTING RT ENGINE ODOR OF SMOKE NOTED IN COCKPIT AND FWD SECTION OF CABIN, NO VISUAL SMOKE NOTED, ODOR WAS MORE INTENSE WITH BLEED AIR OFF AND RECIRC ON. MAINTENANCE FOUND BURNED ODOR COMING FROM 31 NAV RX. REPLACED NR 1 NAV RX P/N 622-6137-001, S/N ON 18273, S/N OFF 1652 31, NAV RX OPS CHECKS GOOD IAW SF340 MM CH34. 2L72 4T RTA52EU 20040712000762004071200076NM 2004 7 12 SWAA041926 120040708A3350610478 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED OVERWING BATTERY PER MM. 2L72 4F A16WE 20040712000832004071200083NM 2004 7 12 SWAA041933 120040708A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040712000882004071200088NM 2004 7 12 SWAA041936 120040708A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 64 WL 200, CRACKED. REMOVED AND REPLACED FRAME CHORD PER SB. 2L72 4F RTA16WE 20040712001082004071200108EU 2004 7 12 MALA040461 120040609A33506122741 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL1598XJ 340A098 DURING CAPACITY CHECK IN HOUSE, BATTERY PACK 61-0478-0, S/N /1824 WILL NOT TURN ON LIGHTS. UNIT FAILED CAPACITY CHECK. REPLACED BATTERY ASSY 61-2274-1, BATTERY ASSEMBLY UNIT PASS CMM CHECKS. A/C RETURNED TO SERVICE 6/13/2004. 2L72 4T RTA52EU 20040712001122004071200112NM 2004 7 12 SWAA041911 120040707A3350100031 SIGN BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 LEFT OVERWING EXIT OVERHEAD SIGN LOOSE. SECURED OVERHEAD SIGN PER MM. 2L72 4F RTA16WE 20040712001262004071200126NM 2004 7 12 AALA20040681 120040610A5330 SKIN BOEING757 757223 1384957NM FUSELAGE DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21681AA 25338 TUL - SMALL DENT IN UPPER FUSELAGE SKIN BETWEEN STATION 1370 AND 1380 ADJACENT TO STRINGER 2L. AREA IS 0.312 BY 0.312 WITH A DEPTH OF 0.018, CRACK LENGTH IS 0.250. INSTALLED DOUBLER PER ESO 90309 DATED 06/03/2004. 2L72 4F RTA2NM 20040712001292004071200129SO 2004 7 12 C2XA04SH402 120040630A531114525991003 DOUBLER EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CARGO FORWARD PARTITION FRAME DOUBLER WAS FOUND TO BE CORRODED AT FRAME 61 BETWEEN STRINGERS 16L AND 17L. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001342004071200134SO 2004 7 12 C2XA04SH381 120040622A531514526437001 BUTTSTRAP EMB 145 EMB145 3260210SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713969 145141 SHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001352004071200135SO 2004 7 12 CX2A04RI005 120040620A335066368 LAMP EMB 145 EMB145 3260210SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719966 145131 IAH - DURING ROUTINE INSPECTION, MAINTENANCE FOUND AFT EMERGENCY LIGHT STRIP NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP. OPERATIONAL TESTS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001482004071200148SO 2004 7 12 C2XA04SH410 120040702A532014525800014 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE RIGHT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001592004071200159 2004 7 12 ASMF200406017 420040618A34254608000307 COMPUTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE AHRU FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML753 49726 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AHRU NR 2 FAILED. AHRU WAS REPLACED IAW MM 34-21-10, TEST CORRECT. DURING OVERNIGHT SERVICE SYSTEM WAS CHECKED, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040712001722004071200172WP 2004 7 12 ASMF200406025 120040622A322039567851 LINK DOUG DC9 DC982 3022082WP MLG FAILED W ASMFA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW231003Y10764 48068 AIRCRAFT RETURNED OF FLIGHT, STRONG VIBRATION IN NOSE LANDING GEAR. DURING MAINTENANCE CHECK WAS DETECTED LT NOSE LANDING GEAR DOOR OPENED, DOOR AND ACTUATOR WERE CHECKED AND ACTUATOR WAS REPLACED IAW MM 32-22-01, TEST FLIGHT WAS PERFORMED AND THREE CYCLES OF LANDING GEAR WERE ACCOMPLISHED, ALL CORRECT. 2L72 4F A6WE 20040713000042004071300004EU 2004 7 13 USAA040128 120040413A5310D53472172204 CROSSBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND 1.5 INCH LONG BY 1 INCH WIDE BY .02 INCH DEEP 4 PLACES, FR 1732 BETWEEN CROSSBEAM C66 AND C68. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040713000102004071300010EU 2004 7 13 USAA040136 120040418A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND SILL 2 INCHES BY 1.5 INCH BY .070 INCH AREA, L2 DOOR SILL, FRAME 66, Y1732. REMOVED AND REPLACED SILL PER SRM 51-42-11, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000202004071300020EU 2004 7 13 USAA040144 120040420A5310D5347217320100 CROSSBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND CORSSBEAM CORRODED, 1 INCH BY .7 INCH BY .55 INCH DEEP, FRAME -Y254, CROSSBEAM C68 -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040713000242004071300024NM 2004 7 13 BJNA040503 120040512A3350362624 LIGHT BOEING737 737282 13844ATNM CABIN BURNED OUT A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A MAINTENANCE WALK AROUND CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP OF THE AFT SECTION OF EMERGENCY FLOOR TRACK IAW EEL COMPONENT MAINTENANCE MANUAL 33-50-01. SYSTEM NOW CHECKS NORMAL. (M) 2L72 4F RTA16WE 20040713000412004071300041WP 2004 7 13 GTIA040351 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATON 1079 TO STATOIN 1155 LEFT SIDE O/B METALLIC PANEL HAS CRACKED/DISBONDED AT HAT CHANNEL. REPAIRED MAIN CABIN FLOORBOARD. (M) 2L72 4F RTA6WE 20040713000432004071300043WP 2004 7 13 GTIA040355 120040329A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B METALLIC PANEL RIGHT SIDE OUTBOARD HAS DISBONDED AT HATS CHANNEL, RUB STRIP, BARE METAL AT HAT SECTON STATON 1079-1117, 541-617, 826-927. BONDED RIGHT SIDE OUTBOARD AT HAT CHANNEL. (M) 2L72 4F RTA6WE 20040713000442004071300044EU 2004 7 13 USAA040158 120040424A5321D5361060500000 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND FLOOR PANEL CORRODED 1 INCH BY 36 INCHES, 1 INCH BY 12 INCHES, 1 INCH BY 10 INCHES, PANEL NR 221FF, FRAME 16-20, Y=1732, Z=-240. REMOVED AND INSTALLED NEW PANEL. CORROSION LEVEL 2, TASK NR JA-220-53300-001. (M) 2L72 4F RTA28NM 20040713000872004071300087EU 2004 7 13 2004F00152 120040518A2430N04063 ALTERNATOR FOKKERF27 F27MK600 4990706EU LT ENGINE INOPERATIVE A COEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NM13742FE 10349 LEFT AC ALTERNATOR FAILED ON CLIMB-OUT FROM KTN. AIRCRAFT RETURNED TO KTN WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE ALTERNATOR WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20040713001172004071300117NM 2004 7 13 USAABB04017 120040206A335020131A BATTERY PACK BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19622AU 27201 TPA - MAINTENANCE FOUND THE R3 DOOR EXTERIOR EVACUATION LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040713001202004071300120NM 2004 7 13 USAABB04042 120040503A335020121 CHARGER BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 SNN - FOUND EMERGENCY LIGHTS WHICH OPERATE FROM THE M730 POWER SUPPLY INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) 2L72 4F RTA1NM 20040713001332004071300133 2004 7 13 WX0400009 420040430A34142594466906 INDICATOR DOUG DC9 DC982 3022082WP CAPT. AIRSPEED FAILED A WXOAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP17890GA 49371 DURING THE TAKEOFF ROLL FROM LAS TO EUG, THE CREW REPORTED THAT THE CAPTAINS AIRSPEED INDICATOR WAS STUCK ON 70-75 KNOTS. THE CAPTAIN CROSS CHECKED THE F/O INDICATOR AND IT WAS SHOWING 90-95 KTS. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. MANTENANCE REMOVED AND REPLACED THE CAPTAINS AIRSPEED INDICATOR AND PERFORMED A FUNCTIONAL CHECK. THE SYSTEM CHECKED OK. WORK WAS DONE IAW AMM 34-13-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A6WE 20040713001822004071300182EA 2004 7 13 A6WA200440059 120040426A5312 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31433AW 7289 FOUND Z MEMBER CHAFED IN AFT EQUIPMENT BAY AT FS 625, BL0, WL 136, ON AFT SIDE OF AFT PRESSURE BULKHEAD. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION. FABRICATED AND INSTALLED A REPAIR ANGLE IAW BRAS EO 601R-53-4884A. (M) 2L72 4F RTA21EA 20040713001852004071300185EU 2004 7 13 ASOA04317 120040413A5315 FLOORBEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE FLOORBEAM PLATE AT FRAME 40, LBL 20, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM PLATE AT FRAME 40, LBL 20 IAW SRM 51-25-01. (M) 2H72 4T RT 20040713001902004071300190EU 2004 7 13 ASOA04311 120040413A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE SEAT TRACKS FROM FS 36 TO FS 39 ON THE LEFT AND RGHT SIDES WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS FROM FS 36 TO FS 39 ON THE LEFT AND RIGHT SIDES IAW SRM 51-25-04. (M) 2H72 4T RT 20040713001952004071300195EU 2004 7 13 SIMA200412104 120040414A53117253813007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21391AE 340B391 ABI - DURING AN MBV INSPECTION A PREVIOUS REPAIR ON GALLEY FLOOR FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED PREVIOUS REPAIR PARTS, CLEANED AND TREATED AREA. FABRICATED A REPAIR DOUBLER, TRIPLER AND SHIMS. REPAIR DONE IAW SAAB SRM LKS 3079 REV 43, CHAPTERS 53-70-30 PARA 6. (M) 2L72 4T RTA52EU 20040713001972004071300197EU 2004 7 13 SIMA200412103 120040422A53302024T3 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21341SB 340B341 ABI - DURING AN HMBV INSPECTION, TWO DENTS WERE FOUND AFT OF THE LEFT ICESHIELD THAT FAILED SAAB SRM PROXIMITY LIMITS. REMOVED DENTS BY CREATING A CUTOUT. PERFORMED AN EDDY CURRENT INSPECTOIN OF CUTOUT WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS006933. (M) 2L72 4T RTA52EU 20040713001992004071300199EU 2004 7 13 SIMA200412105 120040418A53117253813485 FRAME SAAB SF340 340B 7860101EU FUSELAGE BENT A SIMAK NONE O OTHER ININSP/MAINT 1 SW21391AE 340B391 ABI - DURING AN MBV INSPECTION, FOUND CARGO FRAME AT STATION 677 WAS FOUND BENT. RECONTOURED THE CARGO FRAME AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR L ANGLE DOUBLER. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS006945 PARA 7 DATED APRIL 15, 2004. (M) 2L72 4T RTA52EU 20040713002012004071300201WP 2004 7 13 ASAA0480325 120040421A5730ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND LOEWR SRFC OF FUEL ACCESS PANEL 1454 IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040713002032004071300203WP 2004 7 13 ASAA0480318 120040421A5320993053886 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HV CHECK, FOUND CABIN CUSP WEB AT STATION 256, RBL 44 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-10-4. (M) 2L72 4F RTA6WE 20040713002052004071300205WP 2004 7 13 ASAA0480315 120040421A5310993607319 SHEAR TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURING HC CHECK, FOUND SHEAR TIE AT STATOIN 1193, BETWEEN 29R AND 28L IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20040713002072004071300207WP 2004 7 13 ASAA0480254 120040404A57303912757503 ACCESS PANEL DOUG DC9 DC983 3022083WP WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 OKC - DURING FUEL ACCESS PANEL UPPER WING NR 1409 MATTING FLANGE PITTED AND CORRODED. REMOVED AND REPLACED PANEL NR 1409 IAW MD80 SRM 51-22-2A. (M) 2L72 4F RTA6WE 20040714000042004071400004NM 2004 7 14 QXEA200400450 120040616A5210 HANDLE DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR STICKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09347PH16290 480 SEA - FLIGHT 2202 - FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR HANDLE IS DIFFICULT TO OPERATE. MAINTENANCE INSPECTED THE DOOR HANDLE AND CLEANED AND LUBED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000052004071400005NM 2004 7 14 QXEA200400451 120040617A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM MAIN CABIN STICKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09402QX7226 4032 SEA - AFT PASSENGER DOOR IS STICKING. MAINTENANCE INSPECTED THE DOOR AND OPENED AND CLOSED IT 10 TIMES. THE DOOR OPERATED NORMALLY. NO DISCREPANCIES WERE NOTED WITH THE OPERATION. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000062004071400006WP 2004 7 14 UPS04842598 120040611A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 STA 1756, LONG 14 LT CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1746 TO STA 1766. INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040714000072004071400007WP 2004 7 14 UPS04842599 120040611A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, LONG 12 LT CRACKED AT STA 1746. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONG SECTION FROM STA 1740 TO 1766 & INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 11. 2L74 4F RT4A25 20040714000112004071400011NM 2004 7 14 QXEA200400489 120040630A2711 TRIM TAB DHAV DHC8 DHC8202 2809007NM ZONE 300 OUT OF RIG A QXEAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM09351PH 490 OTH - FLIGHT 2208 - WHEN AUTOPILOT SELECTED OFF DURING DESCENT AIRCRAFT IMMEDIATELY ROLLED RIGHT. TOOK 1/2 AILERON TRIM TO LEVEL. ROLL CONTROL FEELS SLUGGISH AND STIFF. AIRCRAFT LANDED SAFELY. RIGGED ADJUSTABLE TAB PER DHC-8 MM 27-13-00-830-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000122004071400012NM 2004 7 14 UPS04242664 120040624A5320 INTERCOSTAL BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C SUPPORT INTERCOSTAL FOR LWR CENTER LINE FAIRING CORRODED AT BS 740 BETWEEN S28L AND S28R. INTERCOSTAL REPLACED WITH FABRICATED INTERCOSTAL IAW SRM 51-30-02 AND 51-20-2. 2L73 4F A3WE 20040714000132004071400013NM 2004 7 14 UPS04242666 120040709A5753 CARRIAGE BOEING727 727173C 1384059NM TE FLAPS WORN A IPXAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01938UP 19506 AIRFRAME HAS A VIBRATION - ATB. TE FLAP CARRIER HAS EXCESS PLAY. 2L73 4F A3WE 20040714000152004071400015NM 2004 7 14 UPS04242669 120040623A5753 ANGLE BOEING727 72725C 138400HNM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, ANGLE CRACKED AT RT ELEPHANTS EAR. FABRICATED ANGLE IAW SRM 51-30-2, INSTALLED NEW ANGLE IAW SRM 51-20-01 FIG 7 AND BOEING DRG 65-26786. 2L73 4F A3WE 20040714000162004071400016NM 2004 7 14 UPS04442656 120040707A3350M334 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 EMERGENCY LIGHT AFT OF LAV DOOR INOP. DEF M283794. REPLACED BATTERY PACK LIGHT, OPS CHECK NORMAL. THIS CLEARS M238794. 2L74 4F A20WE 20040714000182004071400018WP 2004 7 14 UPS04842637 120040614A534097540242 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, STATION 1220 VERTICLE FRAME FITTING AT LONG 27R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 20040714000202004071400020EA 2004 7 14 QXEA200400504 120040702A2840L92B13602 CARTRIDGE CNDAIRCL600 CL6002C10 1390015EA RT WING FAULTY A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09612QX5651 10042 SJC - FLIGHT 2572 - THE CREW REPORTED A RIGHT TRANSFER SHUT OFF VALVE CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT FUEL TRANSFER SHUT OFF VALVE CARTRIDGE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040714000252004071400025NM 2004 7 14 UPS04442643 120040706A3350 COVER BOEING747 747212B 1384886NM EMERGENCY LIGHT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 EMERGENCY LIGHT JUST AFT OF LAV DOOR ON CEILING IS INOP. FOUND LIGHT COVER ASSEMBLY BROKEN. ORDERED LIGHT COVER ASSEMBLY EMERGENCY LIGHT DEFERRED PER MEL 33013. PLACARD INSTALLED. 2L74 4F A20WE 20040714000302004071400030NM 2004 7 14 QXEA200400500 120040703A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - A DENT AND A SCRATCH WAS DISCOVERED BETWEEN PANELS 121AL AND 121BL. THE DAMAGE IS BETWEEN FRAMES 69.4 AND 89.2. THE DENT IS APPROXIMATELY 3 X .052 INCH DEEP AFTER BLENDING. MAINTENANCE PERFORMED A REPAIR IAW EA 6-53-368. 2H72 4T RTA13NM 20040714000312004071400031EU 2004 7 14 UPS04142689 120040709A3242 BRAKE AIRBUSA300 A300F4622R 3930360EU MLG INOPERATIVE A IPXAO OTHER O OTHER LDLANDING 1 SO01120UP 0805 INSPECTION TYPE:N/A ON LANDING & TAXI IN NO LEFT BRAKE ON EITHER SIDE OF COCKPIT. REMOVED AND REPLACED NORMAL BRAKE MASTER VALVE LT PER MM 32-42-19-4 R/R 774905 PERFORM FUNCTIONAL TEST OR MAXIMUM PRESS DELIVERED TO BRACES IAW MM 32-42-00-5 PARA 3 (3), SYS CKS OK. TAXI CHECK OF BRAKES OK FROM BOTH SIDES OF COCKPIT. 2L72 4F RTA35EU 20040714000332004071400033NM 2004 7 14 UPS04242672 120040618A5753 ATTACH FITTING BOEING727 72725C 138400HNM RT IB FLAP G/B CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C SUSPECT CRACK ON OFFSET GEARBOX AT ATTACHMENT LUG ON RIGHT I/B FLAPS. HFEC CONFIRMED CRACK ON LUG. OFFSET GEARBOX REPLACED IAW MM 27-51-60 PARA 1-3. 2L73 4F A3WE 20040714000342004071400034NM 2004 7 14 UPS04242674 120040617A5754 SKIN BOEING727 72725C 138400HNM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C NR 6 L/E SLAT UPPER SKIN HAS SCRATCHES 2 OF WHICH ARE SUSPECT CRACKS NR 1 IS 3 INCHES O/B OF ACTUATOR, NR 2 IS 4 INCHES I/B OF ACTUATOR AND FROM PREVIOUS REPAIR CUTOUT. HFEC INSP CARRIED OUT ON THE ABOVE AREAS IAW B727 NDTM PT6 51-00-00 FIG 4. TWO CRACKS CONFIRMED AND ENDS MARKED. SLAT REPLACED IAW MM 27-81-11, 27-81-32 & SRM 51-30-02. 2L73 4F A3WE 20040714000372004071400037NM 2004 7 14 UPS04242677 120040621A5754 BRACKET BOEING727 72725C 138400HNM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C, NR 7 SLAT O/B TRACK TO SKIN ATTACH BRACKETS ARE CRACKED. NEW BRACKETS INSTALLED IAW SRM 51-30-02, OHM 57-51-61. 2L73 4F A3WE 20040714000402004071400040NM 2004 7 14 UPS04242681 120040617A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, CRACK IN SKIN FOUND AT WING SCANNING LIGHT CUTOUT LT BS 675. REPAIR CARRIED OUT IAW AAAE EO 2004-061-001, UPS ENGINEERING FILE NR 727-53-20149 & SRM 53-30-3 & MM 33-41-02. 2L73 4F A3WE 20040714000412004071400041NM 2004 7 14 UPS04242682 120040621A5313 STRINGER BOEING727 72725C 138400HNM FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, STR WORN ON BS 1183 AFT SIDE AT WL 208 I/B OF SYS-A PRESSURE MODULE. REPAIR CARRIED OUT IAW AAAE EO 2004-061-004, UPS ENGINEERING FILE NR 727-53-20150 & SRM 51-30-02. 2L73 4F A3WE 20040714000432004071400043NM 2004 7 14 QXEA200400459 120040624A6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS OUT OF ADJUST A QXEAC ABORTED TAKEOFF P NO WARNING INDICATION CLCLIMB 1 NM09357PH 504 PDX - AUTO FEATHER FAILED TO ARM. MAINTENANCE ADJUSTED AUTO FEATHER ARMING POTENTIOMETER. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000472004071400047NM 2004 7 14 QXEA200400463 120040623A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - NR 11 SEAT TRACK HAS SUSPECTED PITTING CORROSION AT STATION X484.5 TO 499.0. REPAIRED IAW DHC-82 SRM 51-40-11. 2H72 4T RTA13NM 20040714000512004071400051NM 2004 7 14 QXEA200400467 120040623A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 400 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - LEFT HAND NR 5 SEAT TRACK INBOARD UPPER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989. 2H72 4T RTA13NM 20040714000532004071400053NM 2004 7 14 QXEA200400469 120040623A5711 SPAR DHAV DHC8 DHC8202 2809007NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - CORROSION ON FRONT SPAR LOWER AFT FLANGE UNDER PANEL 625 AT ONE INCH AFT OF FRONT SPAR VERTICAL PANEL AT RIGHT HAND WING STATION 423.00. REPAIRED IAW DHC-8-200 MM 57-20-00, TASK 57-20-00-400-801. 2H72 4T RTA13NM 20040714000542004071400054NM 2004 7 14 QXEA200400470 120040622A5752 HINGE DHAV DHC8 DHC8202 2809007NM ZONE 500 CUT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - LEFT AILERON SPRING TAB HINGE AT YW435.30 LEFT HAND DAMAGED, HINGE TAB UNDERCUT BY HINGE BUSHING. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040714000552004071400055NM 2004 7 14 QXEA200400482 120040629A5320 THRESHOLD DHAV DHC8 DHC8201 2809001NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH 514 PDX - LITE CORROSION AT MAIN CABIN DOOR THRESHOLD AT NUT PLATES UNDERSIDE. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20040714000562004071400056WP 2004 7 14 UPS04842690 120040610A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, MID ACC COMPT CORRODED LONG 31 RT STA 640-668. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED SECTION LONGERON STA 610 TO 710 IAW DC8 SRM 51-1-20D. RECEIVED, LOCATED & DRILLED UP LONGERON NR 2646610, IAW DC8 SRM 51-1-24, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED LONGERON IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040714000582004071400058NM 2004 7 14 QXEA200400503 120040706A5414 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 400 BUCKLED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH 506 PDX - LOWER LEFT HAND NACELLE IS BUCKLED JUST AFT OF NR 1 ENGINE LOWER COWL ASSEMBLY. REPAIRED IAW RD 8-54-063. 2H72 4T RTA13NM 20040714000602004071400060NM 2004 7 14 QXEA200400412 120040610A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 10 HAS SPOT OF CORROSION IN CENTER OF TRACK AT STATION X308. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20040714000612004071400061NM 2004 7 14 QXEA200400417 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 12 HAS GOURGES ON LUGS AT STATION X531. REPAIRED IAW RD 8-53-3644 AND DHC-8-200 SRM 51-20-36. 2H72 4T RTA13NM 20040714000622004071400062NM 2004 7 14 QXEA200400415 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 11 HAS AREA OF CORROSION INSIDE AT STATION X496. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20040714000632004071400063NM 2004 7 14 QXEA200400416 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 12 HAS CORROSION ON TOP OF TRACK AT STATION X521. REPAIRED IAW DHC-8-200 SRM 51-20-36 AND RD 8-53-3644. 2H72 4T RTA13NM 20040714000642004071400064NM 2004 7 14 QXEA200400418 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEVERAL FLOOR FLANGE RECEPTICLE HOLES SCRATCHED/GOUGED OUTBOARD SIDE OF RIGHT HAND SEAT RAIL NR 8 AT APPROXIMATELY STATION X469.0 TO X487.0. REPAIRED BY LIGHTLY SANDING RECEPTICLE. 2H72 4T RTA13NM 20040714000652004071400065NM 2004 7 14 QXEA200400425 120040609A5751 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - RIGHT HAND WING UPPER LEADING EDGE ATTACH BRACKET CRACKED AT YW138, AT UPPER SPAR CAP. REPAIRED IAW DHC-8 SRM 51-40-00. 2H72 4T RTA13NM 20040714000662004071400066NM 2004 7 14 QXEA200400438 120040611A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 6 HAS CORROSION ON INBOARD FLANGE FROM STATION X580 TO X586. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20040714000682004071400068NM 2004 7 14 QXEA200400440 120040611A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - MULTIPLE SPOTS OF DEEP CORROSION ON RIGHT HAND INBOARD SEAT RAIL NR 7 BETWEEN APPROXIMATELY STATION X215.500 AND X252.70. REPAIRED IAW RD 8-57-102 AND RD 8-53-4473. 2H72 4T RTA13NM 20040714000692004071400069NM 2004 7 14 QXEA200400483 120040625A5751 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 300 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - RIGHT HAND AILERON HAS IMPACT DAMAGE FROM OUTBOARD EDGE, 9 INCHES FROM TRAILING EDGE ON TOP PANEL. REPAIRED IAW RD 8-57-2861 AND HORIZON AIR EA 2-57-261. 2H72 4T RTA13NM 20040714000702004071400070NM 2004 7 14 QXEA200400484 120040629A7810 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 PDX - NR 2 EXHAUST SHROUD DECK CHANNEL AT AFT EXHAUST EJECTOR SHROUD ATTACH BOLTS CRACKED. REPAIRED IAW RD 8/4-54-033. 2H72 4T RTA13NM 20040714000722004071400072NM 2004 7 14 QXEA200400486 120040629A7810 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 PDX - NR 2 ENGINE AFT RIGHT EXHAUST PANEL 424AR HAS DAMAGE ON AFT EDGE FROM INTERFERENCE WITH AFT EXHAUST COLLECTOR SHROUD. REPAIRED IAW RD 8/4-54-012. 2H72 4T RTA13NM 20040714000752004071400075EU 2004 7 14 UPS04142607 120040618A5313F5347524420000 STRINGER AIRBUSA300 A300F4622R 3930360EU FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01157UP 0005 STRINGER 44R DAMAGED AT FRAME 57 TO 58. REPLACED STRINGER IAW A300 SRM 51-40-21. 2L72 4F RTA35EU 20040714000762004071400076EU 2004 7 14 UPS04142608 120040618A5330 SKIN AIRBUSA300 A300F4622R 3930360EU FUSELAGE PUNCTURED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01157UP 0005 A/C SKIN DAMAGED BY GSE APPROX AT STRINGER 42R-54R AT FRAME 58. REPLACED STRINGERS 44R & 45R INTERCOSTAL 43R AND REPAIRED SKIN DAMAGED IAW REO-GO9854. 2L72 4F RTA35EU 20040714000782004071400078WP 2004 7 14 UPS04842602 120040613A531337585931 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C3, STATION 1260-1280 LONG 34L IS CRACKED. REMOVED AND REPLACED LONGERON SECTION BETWEEN STATION 1270 TO 1350 IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040714000792004071400079WP 2004 7 14 UPS04842603 120040612A531037549301 FITTING DOUG DC8 DC873F 302199FWP CARGO DOOR FRAMECRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2, C-PIT DOOR FRAME LOWER FWD LATCH BACKUP FITTING AT STATION 1168 LONG 34R APPROX IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754930, AND SRM 51-1-20D. 2L74 4F RT4A25 20040714000822004071400082WP 2004 7 14 UPS04842693 120040614A5313577991211 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3 FWD PIT STA 460-480 L31L GOUGED. REMOVED GOUGES, FOUND OUT OF LIMITS, GEN RFTS, REC'D RFTS W/ REO GO98956, FAB LONGERON SPLICES IAW REO-G098956, ALODINED & PRIMED, FAB NEW LONGERON SEC & REPAIRED. REC'D HEAT TREAT, LOCATED, DRILLED & PRIMED. INSTALLED STA 460 & 480, INSTALLED LONGERON SEC STA 450-470 IAW REO GO9895 6 & DC8 SRM 51-1-20D, 51-1-21, 51-1-24, 53-2-0, & 53-4-1. 2L74 4F RT4A25 20040714000832004071400083WP 2004 7 14 UPS04842694 120040615A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3, CABIN SEAT TRACK LBL 25 STA 850- 870 CORROSION MARKED DOT C 6580. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK MAT ID FOR NEW SEAT TRACK 2772660/60-15176 PO SPO771694 IAW DC8 SRM 53-7-3 & UPS EO DC8-5320-5167C. MAT ID FOR SEAT TRACK SPLICE FITTING PO DC8-53B-003-501, PO SPO990445. FAB SEAT TRACK & FITTINGS. LOCATED, DRILLED & DEBURRED. ALODINED & PRIMED. INSTALLED SEAT TRACK & FITTINGS. 2L74 4F RT4A25 20040714000842004071400084WP 2004 7 14 UPS04842696 120040701A57125769589 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3, RIGHT WING CTR L/E RIB CRACKED AT APPROX STA XFS 304 VERIFIED BY NDT. PERFORMED AFEC IAW DAC SPM NDT 06-10-001-01 TO VERIFY CRACK END AT FASTENER HOLE. MAT THICKNESS FOR RIB AT STA XFS 304 .063 7075-T6, MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. FAB REPAIR ANGLE IAW DC8 SRM 57-2-0, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0. 2L74 4F RT4A25 20040714000882004071400088WP 2004 7 14 UPS04842632 120040614A53403643110 ATTACH ANGLE DOUG DC8 DC873F 302199FWP WING TO BODY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 FUSELAGE FWD CENTER SPAR FRAME TO WING ATTACH ANGLE CRACKED AT STA 759 RBL 50. REMOVED CRACKED ANGLE REF SRM 51-1-20D. FABRICATED REPLACEMENT ANGLE REF DAC DWG 3643110. INSTALLED ANGLE PER SRM 51-1-20D. 2L74 4F RT4A25 20040714000912004071400091WP 2004 7 14 UPS04842604 120040610A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB LEADING EDGE UPPER SKIN IS CORRODED XFS 272.5. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20040714000922004071400092WP 2004 7 14 UPS04842698 120040702A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, RT CENTER 4E HAS CRACKED RIB AT APPROX STA 448.00. REMOVED FASTENERS IN REPAIR AREA RT CENTER L/E AT STA 448.00 & STOP DRILL CRACK. MAT ID FOR REPAIR ANGLE 9751065-33 EXTRUSION 7075-T6 PO 387706. PERFORMED HFEC IAW MD NDT SPM 06-10-01.001, NO CRACKS INDICATED BEYOND STOP DRILL. CUTOUT, FAB, LOCATED, DRILLED & DEBURRED REPAIR ANGLE. ALODINED & PRIMED ANGLE. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040714000942004071400094WP 2004 7 14 UPS04842699 120040702A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, RT CENTER L/E HAS CRACKED RIB AT APPROX STA 304.600. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-211. MAT ID FOR REPAIR ANGLE BAC 1503-100147 EXTRUSION 7075-T6 PO 437138. STOP DRILLED CRACKED. LOCATED, DRILLED & DEBURRED REPAIR ANGLE. ALODINED & PRIMED. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040714000952004071400095NM 2004 7 14 QXEA200400460 120040617A7600312306401 TSCU DHAV DHC8 DHC8202 2809007NM NR 1 ENGINE MALFUNCTIONED A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09358PH12931 506 OTH - FLIGHT 2121, NR 1 ENGINE AUTOFEATHERED AFTER TAKEOFF, OVERTORQUE AT 138 PERCENT NOTED. PEAK OVERTORQUE NOT NOTED. DURATION OF OVERTORQUE NOT NOTED. REPLACED TSCU, ENGINE HARNESS AND NR 1 PROPELLER ASSEMBLY. HARNESS S/N AA8411 HAD 13087.8 HOURS AND 18778 CYCLES. PROPELLLER S/N 97122 HAD 1563.4 HOURS AND 2350 CYCLES. C/W OVERTORQUE INSPECTION AND MTC. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000962004071400096NM 2004 7 14 QXEA200400471 120040624A2910829700091 LINE DHAV DHC8 DHC8202 2809007NM NR 2 HYD SYS CRACKED A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM09356PH15354 502 SEA - FLIGHT 2029 - CREW REPORTED LOSS OF BOTH THE NR 2 HYDRAULIC PRESSURE AND QUANTITY WHILE ON APPROACH. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 AFT MAIN LANDING GEAR DOOR HYDRAULIC LINE CRACKED AND LEAKING. THE LINE WAS REPLACED, LEAK CHECKS AND OPERATIONAL CHECKS WERE PERFORMED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714001002004071400100NM 2004 7 14 151AW00220 120040702A5754 STRUCTURE BOEING737 7373G7 1384595NM NR 2 SLAT CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 NR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01. 2L72 4F RTA16WE 20040714001012004071400101NM 2004 7 14 151AW0023 120040702A1430 BOLT BOEING737 7373G7 1384595NM RUDDER LOOSE A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FOUND 7 RUDDER FLANGE BOLTS LOOSE. TORQUED AND REPLACED BOLTS AS REQUIRED PER SB 737-55A1087. 2L72 4F RTA16WE 20040714001022004071400102NM 2004 7 14 151AW0024 120040702A5320 ANGLE BOEING737 7373G7 1384595NM DOOR FRAME CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 CRACK IN ANGLE ON AFT SIDE OF AFT DOOR FRAME OF L1 DOOR AT THE NR 2 STOP FITTING. REPLACED ANGLE. 2L72 4F RTA16WE 20040714001032004071400103NM 2004 7 14 151AW0020 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 INCORRECT REPAIR AT BS 360 STR 24 RT AT INTERSECTION OF SKIN LAP AND BUTT JOINT. REPLACED EXISTING REPAIR PER EA 53-148A. 2L72 4F RTA16WE 20040714001052004071400105NM 2004 7 14 151AW0003 120040702A5320 SPLICE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER SPLICE CRACKED AT STRINGER 4 RT AT BS 907 AND AT STRINGER 4 LT AT BS 907. REPLACED STRINGER SPLICE AT 4 RT AND 4 LT PER SRM 51-40-02. 2L72 4F RTA16WE 20040714001072004071400107WP 2004 7 14 CALA0400542 120040622A532059364692N ANGLE DOUG DC9 DC981 3022081WP DOOR FRAME CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714871 48022 INSPECTION FOUND AFT CARGO DOOR FORWARD DOOR JAMB ANGLE CORRODED AT STA 1155, LONGERON 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. 2L72 4F A6WE 20040714001082004071400108NM 2004 7 14 CALA0400543 120040621A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 277 AND 294.5 UNDER RIGHT GALLEY. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040714001092004071400109NM 2004 7 14 750WL0005 120040709A3350 LAMP BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 3. RELAMPED AND OPS CHECKED OK. 2L72 4F RTA2NM 20040714001122004071400112WP 2004 7 14 CALA0400540 120040618A53202167365 STAND OFF DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714871 48022 INSPECTION FOUND FLOOR STANDOFF CORRODED AT STA 200 CENTER OF FLOOR. THE FLOOR STANDOFF WAS REMOVED AND REPLACED IAW SRM 51-30-5-001. 2L72 4F A6WE 20040714001142004071400114NM 2004 7 14 CALA0400568 120040707A53106515303 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND SHEAR TIE CORRODED IN E&E COMPARTMENT AT STA 360, LBL 5 BETWEEN S28L AND S29L. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND REPAIRED IAW SRM 53-00-07, FIGURE 207, REPAIR 1. 2L72 4F RTA16WE 20040714001182004071400118SO 2004 7 14 MASA200400165 120040325A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07844MJ 145481 MID CABIN CEILING EMERGENCY EXIT PANEL BACKSIDE LIGHTING INOP. MX REPAIRED CONNECTION. OP CHECKS GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040714001202004071400120SO 2004 7 14 MASA200400373 120040627A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 CENTER CABIN EMERGENCY EXIT SIGN INOP. AOG FOR INVERTER, MX REPLACED INVERTER. 2L72 4T RTT00011AT 20040714001212004071400121EA 2004 7 14 MASA200400375 120040627A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07759844571 7489 DURING PRE-FLIGHT THE EXIT SERVICE DOOR EMERGENCY LIGHTS WERE INOP. PLACED ON MEL. MX REPLACED CHARGER. 2L72 4F RTA21EA 20040714001222004071400122SO 2004 7 14 MASA200400376 120040627A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07834MJ 145340 CREW REPORTED THE OVERHEAD EMERGENCY EXIT SIGN AT ROW 12 LIGHT INOP. MX RESET AIRCRAFT ELECTRICAL POWER, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040714001242004071400124EA 2004 7 14 MASA200400384 120040702A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775999 7471 THE SECOND FROM FORWARD EMERGENCY CABIN CEILING LIGHT WAS INOP. CONTRACT MAINTENANCE RELAMPED THE LIGHT AND PERFORMED THE OPERATIONAL CHECKS. 2L72 4F RTA21EA 20040714001272004071400127NM 2004 7 14 151AW0009 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 BS 639 RT FRAME I/B WEB, AND O/B CRACKED. REPLACED PER SRM 51-10-2, REPAIRED WEB PER SRM 51-70-13, AND REPAIRED PER EA 53-148-1. 2L72 4F RTA16WE 20040714001282004071400128 2004 7 14 150AW0024 420040703A2230 TRANSDUCER BOEING737 7373G7 1384595NM AUTOTHROTTLES INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05150AW 23218 AUTO THROTTLE WILL DISENGAGE AND NOT RE-ENGAGE UNTIL FLAPS RETRACTED AND ALL LIGHTS OUT. SEEMS NR 1 THROTTLE LAGS BEHIND NR 2 AFTER TOGA IS PUSHED. PLACED AUTO THROTTLE SYSTEM ON MEL 22-4. ADJUSTED NR 2 ENGINE PLA TRANSDUCER PER MM 22-31-11. OPS CHECK OK. 2L72 4F RTA16WE 20040714001292004071400129 2004 7 14 249TR0031 420040705A2230 TRANSMITTER BOEING737 7372K5 138448XNM AUTOTHROTTLE OUT OF ADJUST A PIDAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO05249TR 22598 AUTO THROTTLE SHUTS OFF ON TAKEOFF. ADJUSTED THROTTLE POSITION TRANSMITTERS PER MM 22-31-81. 2L72 4F RTA16WE 20040714001312004071400131NM 2004 7 14 151AW0008 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 BS 639 LT FRAME I/B CHORD, WEB, AND O/B CHORD CRACKED. REPLACED I/B AND O/B CHORDS PER SRM 51-40-02 AND REPAIRED WEB PER SRM 51-70-13. 2L72 4F RTA16WE 20040714001332004071400133SO 2004 7 14 MASA200400298 120040528A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07834MJ 145340 CENTER CABIN CEILNG EMERGENCY EXIT SIGN INOP. SYSTEM OPS CHECKED GOOD, NO DEFECTS NOTED. NO PARTS USED. 2L72 4T RTT00011AT 20040714001342004071400134EA 2004 7 14 MASA200400307 120040602A335064645 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775998 7336 DURING A PLANNED SIT TIME MX DISCOVERED THE AFT EMERGENCY FLOOR TRACK LIGHTS WERE INOP. MX REPLACED THE PWR STRIP AND CONNECTOR CABLE. OPS CHECK GOOD. 2L72 4F RTA21EA 20040714001362004071400136SO 2004 7 14 MASA200400311 120040604A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07827MJ 145217 ON THE RON ON A SCHEDULED ROUTINE DURING THE WALK AROUND IT WAS DISCOVERED THAT THE LEFT OVERWING EMERGENCY LIGHT WAS INOP. REPLACED THE LIGHT BULB, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040714001402004071400140EA 2004 7 14 MASA200400322 120040607A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 THE CREW REPORTED THE EMERGENCY ESCAPE FLOOR PROXIMITY LIGHT STRIP AT THE SERVICE DOOR INOPERATIVE. MAINTENANCE FOUND THE STRIP DISCONNECTED FROM THE POWER CIRCUIT, RECONNECTED THE STRIP AND SYSTEM OPERATIONALLY CHECKED NORMAL. NO PARTS USED. 2L72 4F RTA21EA 20040714001412004071400141EA 2004 7 14 MASA200400329 120040611A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0717275 7275 BOTH FWD ENTRY DOOR EXTERNAL EMERGENCY LIGHTS INOP. MX REPLACED BATTERY PACK, OPS CHECKED GOOD. 2L72 4F RTA21EA 20040714001432004071400143SO 2004 7 14 MASA200400333 120040614A1420 CONNECTOR EMB 145 EMB145LR 3260212SO BATTERY PACK LOOSE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07841MJ 145448 FLOOR PROX LIGHTS INOP BETWEEN ROWS 8-12. MX RECONNECTED BATTERY PACK CONNECTORS. NO PARTS USED. 2L72 4T RTT00011AT 20040714001442004071400144EA 2004 7 14 MASA200400338 120040615A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0737178 7178 THE PILOT REPORTED A CABIN EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20040714001452004071400145EA 2004 7 14 MASA200400345 120040617A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW077305V 7305 DURING PREFLIGHT THE FWD AND AFT CABIN EMERGENCY FLOOD LIGHTS WERE INOP. THESE WERE PLACED ON MEL WITH THE CREW. MX RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20040712001382004071200138SO 2004 7 12 C2XA04TY098 120040622A531514521713005 FLOORBEAM EMB 145 EMB145 3260210SO GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713968 145138 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040712001462004071200146SO 2004 7 12 C2XA04SH433 120040705A532014529495003 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 59-61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001492004071200149SO 2004 7 12 C2XA04SH411 120040702A532014525800013 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT SILL WAS FOUND TO BE CORRODED FROM FRAME 42 TO 47. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001532004071200153SO 2004 7 12 C2XA04SH415 120040703A531514522215407 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM JUST FORWARD OF FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01129. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040712001562004071200156NM 2004 7 12 ASMF200406021 120040621A3230 PIN DOUG MD80 MD83 3023681NM MLG INSTALLED W ASMFA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW23945AS 49643 AIRCRAFT RETURNED OF FLIGHT, MAIN LANDING GEAR UNLOCK INDICATION AND STRONG VIBRATION. DURING MAINTENANCE REVISION, RT AND LT LOCK PINS WERE DETECTED INSTALLED IN MAIN LANDING GEAR. LOCK PINS WERE REMOVED AND MAIN LANDING GEAR AND OVERWEIGHT INSPECTION WERE PERFORMED IAW MM 32-30-00 AND 05-51-04, RESPECTIVELY, ALL CORRECT. 2L72 4F RT 20040712001982004071200198 2004 7 12 ASMF200406022 420040621A3420HG280D80 COMPUTER DOUG DC9 DC982 3022082WP CADC FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW231003Y41030 48068 DURING TRANSIT CHECK, CAPTAIN REPORTED SPEED FLAG IN BOTH ADI´S AND FLAG IN EPR LIMIT INDICATOR. CADC´S AND DFGC´S RESEAT WERE PERFORMED AND FAIL CONTINUED. DIFFERENCE OF 150 FEET BETWEEN BOTH ALTIMETERS WAS REPORTED AND CADC´S WERE REPLACED IAW MM 34-16-01, TESTS CORRECT. 2L72 4F A6WE 20040713000132004071300013EU 2004 7 13 USAA040131 120040413A5320D5361018300200 STIFFENER AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19708UW15683 0972 BFM - FOUND STIFFENER ASSEMBLY CORRODED 3.5 INCH BY 1.0 INCH BY .015 INCH DEEP, FRAME 12, BETWEEN Y-81 AND Y-1379.5, Z-240. REMOVED AND REPLACED STIFFENER ASSEMBLY PER SRM 53-11-14, 51-42-11, 51-74-00. CORRODED LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040713000182004071300018NM 2004 7 13 UIEA200400092 120040511A304029155 CONTROLLER BOEING747 74747UF 1384949NM WINDOW HEAT MALFUNCTIONED A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15418MC 32840 HKG/ICN - ON GROUND, ODOR IN FLIGHT DECK. FOUND WINDOW HEAT SWITCH 'ON' POSTION, BUT IT WAS GONE AFTER SWITCH 'OFF' POSTION. REPLACED HEAT CONTROLLER SEE LOG PAGE 511683 ITEM NR 1. (M) 2L74 4F RT1384945 20040713000332004071300033EU 2004 7 13 USAA040149 120040423A5310D5347217220290 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US 0922 BFM - FOUND BEAM CORRODED 1 INCH BY .20 INCH BY .27 INCH DEEP AREA, FRAME 67, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-15 51-42-11, 53-00-14, 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713000342004071300034WP 2004 7 13 GTIA040349 120040407A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN CABIN FLOOR PANEL LEFT OUTBOARD FS 1250-1309 HAT CHANNEL ON BOTTOM IS DISBONDED ON FORWARD END AND CRACKED AT BOTH ENDS. REPAIRED DAMAGED HAT CHANNEL. BONDED FORWARD END OF HAT CHANNEL. (M) 2L72 4F RTA6WE 20040713000422004071300042WP 2004 7 13 GTIA040352 120040324A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 1309 TO STATION 1250 RIGHT SIDE OUTBOARD METALLIC PANEL HAS CRACKED AT HAT CHANNEL. REPAIRED DAMAGE. (M) 2L72 4F RTA6WE 20040713000522004071300052WP 2004 7 13 GTIA040345 120040401A5420 ANGLE DOUG DC9 DC983 3022083WP LT PYLON CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 FTW - FOUND LEFT SIDE PYLON UPPER ATTACHED ANGLE IS CRACKED, FORWARD L/E 12 INCHES. REMOVED LEFT SIDE PYLON UPPER ANGLE. FABRICATED UPPER ANGLE. INSTALLED UPPER ANGLE. (M) 2L72 4F RTA6WE 20040713000562004071300056WP 2004 7 13 GTIA040357 120040324A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DETERIORATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 FTW - FOUND MAIN C/B STATION 674 TO 693 MID RIGHT SIDE HAS DETERIORTATED ON TOP PANEL EDGE FILLER. FABRICATED FLOORBOARD. (M0 2L72 4F RTA6WE 20040713000612004071300061EU 2004 7 13 ASOA04302 120040323A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A C-CHECK IN YUL, THE SEAT TRACK AT FS 35 AND 36 LEFT INBOARD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AT FRAME 35 AND FRAME 36 LEFT INBOARD IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20040713000642004071300064NM 2004 7 13 2004F00150 120040419A494038880585 IGNITION UNIT BOEING737 7378Q8 13844BXNM APU SHORTED A MYWAK NONE O OTHER ININSP/MAINT 1 SO19733MA 30619 PRIOR TO DEPARTURE SNN APU DID NOT START, FAULT LIGHT COMES ON DURING CYCLE. TRANSFERRED ITEM TO DMI LOG ITEM NR 4360. AIRCRAFT CONTINUED TO SREVIE ONE LEG TO STN. PERFORMED APU BITE CHECK IAW FIM 49-40 TASK 801-802. REPLACED IGNITION UNIT IAW MM 49-41-31. OPERATION CHECK NORMAL. CLEARED DMI 4360, PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. ACCOMPLISHED ETOPS VERIFICATION. APU STARTED SUCCESSFULLY AT CRUISE ALTITUDE. ALL PARAMETERS NORMAL. (M) 2L72 4F RTA16WE 20040713000772004071300077NM 2004 7 13 UIEA200400024 120040223A3240 SMOKE BOEING747 74747UF 1384949NM RT MLG WW DETECTED A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15498MC 29259 ANC/BNA - ONCE THE AIRCRAFT LANDED, GROUND CREW NOTICED WHITE SMOKE COMING FROM THE RIGHT WING GEAR AREA. A FIRE EXTINGUISHER WAS USED TO PUT OUT WHAT IT WAS THOUGHT TO BE A FIRE BY THE GROUND CREW. VISUALLY INSPECTED THE RIGHT WING GEAR AREA FOR EVIDENCE OF FIRE, NIL FOUND. INSPECTED NR 13 MOUNTING WHEEL AND BRAKE ASSEMBLY IAW MM 32-45-01 AND WASHED THE GEAR DOWN WITH WATER IN ORDER TO REMOVED THE FIRE EXTINGUISHING AGENT RESIDUE. NO DEFECTS NOTED. REMOVED AND REPLACED NR 13 WHEEL AND BRAKE ASSEMBLY AS PRECAUTIONARY. (M) 2L74 4F RT1384945 20040713000782004071300078NM 2004 7 13 2004F00151 120040102A771230005000055 TSCU DHAV DHC8 DHC8103 1386005NM NR 1 ENGINE MALFUNCTIONED A IZZAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 WP13808WP 026 FLT 1126 - HNL - NR 2 ENGINE AUTO FEATHERED ON TAKEOFF ROLL, FIRST APPLICATION OF POWER. REMOVED AND REPLACED NR 1 TORQUE SIGNAL CONDITION UNIT (TSCU) IAW PW MM CHAPTER 72-01-10 PAGE 414-419/420, OPS CHECK GOOD. (M) 2H72 4T RTA13NM 20040713000792004071300079NM 2004 7 13 USAABB04019 120040206A3350767 BULB BOEING757 7572B7 1384964NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19630AU 27808 PHL - MAINTENANCE FOUND THE R3 AND R4 DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TIGHTENED THE BULB ASSEMBLY IN BOTH THE R3 AND R4 DOOR EXTERIOR EMERGENCY LIGHTS. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040713000862004071300086NM 2004 7 13 USAASB04045 120040425A32606301001033 BULB BOEING737 7373B7 1384580NM INSTUMENT PANEL INOPERATIVE A USAAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA19383US 22956 BUF - FLT 962 - ON FINAL APPROACH INTO BUF, CREW LOWERED GEAR AND DID NOT RECEIVE ANY INDICATION FOR THE RIGHT MLG. A TOWER FLY-BY WAS ACCOMPLISHED WITH THE TOWER CONFIRMING THE GEAR WAS DOWN. CREW REPLACED LIGHT BULBS AND RECEIVED GREEN LIGHTS. THE EMERGENCY EQUIPMENT WAS CALLED OUT AND AN EMERGENCY WAS DECLARED BUT BOTH WERE CANCELLED ONCE THE GREEN LIGHTS FOR THE GEAR WERE RECEIVED. FLIGHT LANDED WITHOUT INCIDENT AND CONTINUED ON ITS LINE OF FLYING. CREW RELAMPED RIGHT MAIN LANDING GEAR INDICATION LIGHTS ON THE P2-2 CENTER INSTRUMENT PANEL. NO FURTHER MAINTENANCE ACTION ACCOMPLISHED. (M) 2L72 4F RTA16WE 20040713001102004071300110SO 2004 7 13 SIMA200412502 120040501A533014520556001 SKIN PANEL EMB 145 EMB145LR 3260212SO FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21670AE 145790 SAW - FOUND LIGHTNING STRIKE DAMAGE ON RIGHT SIDE OF FUSELAGE BETWEEN FRAMES 25 AND 26 AT STRINGER 18A. REPAIRED LIGHTNING STRIKE DAMAGE AREA WITH A CUT OUT AND DOUBLER PATCH IAW SRM 53-22-01 FIG 304 SHEET 3. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040713001152004071300115EA 2004 7 13 A6WA200440024 120040222A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31406AW 7402 PASSENGER DOOR OUTER HANDLE CAS MESSAGE IN FLIGHT. COMPLIED WITH QRH. CABIN PRESSURE NORMAL ALL SIX CAMS INDICATE LOCKED, MEL'D. (M) 2L72 4F RTA21EA 20040713001222004071300122EU 2004 7 13 USAA040115 120040419A5320D5347112420100 SHEAR PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19704US16409 0922 BFM - FOUND SHEAR PLATE CORRODED 1.2 INCH BY 1.3 INCH BY .012 INCH AREA, BETWEEN C69-C70, Y-1292. REMOVED AND REPLACED WITH NEW PART PER SRM 51-74-00, 51-42-11, 53-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040713001232004071300123NM 2004 7 13 USAASB04052 120040506A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19776AU 24934 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS INOPERATIVE AT THE RIGHT OVERWING EXIT, THE LEFT OVERHEAD AT EMERGENCY EXIT AND THE LEFT EXTERIOR OVERWING. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT THE RIGHT OVERHEAD EMERGENCY EXIT. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040713001282004071300128EU 2004 7 13 ASOA04304 120040323A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11531AS 454 DURING A C-CHECK IN YUL, THE INTERCOSTALS BETWEEN FRAME 38 TO FRAME 39 STRINGERS 16L AND 16R WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS BETWEEN FRAME 38 TO 39 AT STRINGERS 16L AND 16R IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040713001292004071300129EA 2004 7 13 ASOA04295 120040426A3397M2275934229 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11823AS 7196 DURING A GROUND INSPECTION IN DFW, THE LOWER EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPINNED AND RESECURED A BROKEN WIRE ON THE LOWER EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040713001392004071300139NM 2004 7 13 USAA040160 120040409A532065516988 STRINGER SPLICE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US50060 23930 PIT - FOUND STRINGER SPLICE WITH TWO .125 INCH CRACKS, FS 907, S4R STRINGER SPLICE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20040713001442004071300144NM 2004 7 13 BJNA040203 120040223A33505822514 POWER SUPPLY BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND THE EMERGENCY BATTERY PACK IAW BOEING MM 33-51-0, SYSTEM NOW CHECKS NORMAL. (M) 2L72 4F RTA16WE 20040713001482004071300148NM 2004 7 13 UIEA200400016 120040213A541565B41383 ATTACH FITTING BOEING747 747243B 1384830NM NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURNG D-CHECK AT SIN ON NR 1 PYLON DIAGONAL BRACE ATTACH FITTING, HFEC INSPECTOIN FOUND CRACK IN HOLE LOCATION REF 'A'. HOLE OVERSIZED TO .0405, BUT CRACK REMAINS. THE DEFECT WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO .434 INCHES PRIOR TO FURTHER OVERSIZING TO .4521-0 .4541 INCHES. A SAME TYPE FASTENER WAS INSTALLED AT THE DISCREPANT LOCATION. ALL OTHER FITTING REWORK AND REFINISH WAS ACCOMPLISHED IAW TERMINATING ACTION. (M) 2L74 4F A20WE 20040714000012004071400001NM 2004 7 14 QXEA200400477 120040628A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM ZONE 100 STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH13691 520 PDX - FUSELAGE PANEL 121AL HAS 3 STRIPPED OUT NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES IAW DHC-8 SRM. 2H72 4T RTA13NM 20040714000082004071400008WP 2004 7 14 UPS04842595 120040610A55115654549501 RIB DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB UPPER RIB IS CRACKED AT XFS 47.5. REMOVED AND REPLACED ANGLE IAW DWG 5654549 AND SRM 51-1-20D. 2L74 4F RT4A25 20040714000142004071400014NM 2004 7 14 UPS04242668 120040623A5320 CLIP BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, SUPPORT CLIP FOUND CRACKED AT BS 580 BETWEEN S2L AND S3L. SUPPORT CLIP FABRICATED AND INSTALLED IAW 51-20-01 AND 51-30-2. 2L73 4F A3WE 20040714000172004071400017WP 2004 7 14 UPS04842636 120040614A531536431102 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, LOWER FLOORBEAM ANGLE IS CRACKED AT STATION 759 AT RBL 50. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 3643110, AND SRM 51-1-20D. 2L74 4F RT4A25 20040714000192004071400019WP 2004 7 14 UPS04842638 120040612A53404758514505N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT 1240 AFT SIDE AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D. 2L74 4F RT4A25 20040714000212004071400021NM 2004 7 14 QXEA200400505 120040706A2820AV24B1319D3 VALVE DHAV DHC8 DHC8202 2809007NM ZONE 400 LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09365PH* 3631 526 PDX - MAINTENANCE DISCOVERED A FUEL LEAK ON THE NR 2 NACELLE. THE LEAK WAS NOTED TO BE COMING FROM THE REFUEL - DEFUEL VALVE. THE VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000222004071400022NM 2004 7 14 QXEA200400495 120040608A3010 BOOT PATCH BOMBDRDHC8 DHC8401 1390041NM DE ICE SYSTEM LOOSE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09408QX 4050 PDX - FLIGHT 2357, DEICE PRESSURE CAUTION LIGHT ILLUMINATED. LIGHT WENT OUT AFTER CHECKLIST PROCEDURE, CAME ON AGAIN AFTER 10 MINUTES AND WENT OUT AGAIN AFTER CHECKLIST PROCEDURE. FLIGHT LANDED AFTER 15 MINUTES. VISUALLY INSPECTED ALL DEICE BOOTS WHILE INFLATED. MAINTENANCE FOUND TWO LOOSE DEICE BOOT PATCHES. RE-SECURED, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000242004071400024NM 2004 7 14 QXEA200400457 120040619A2611473082 SMOKE DETECTOR BOMBDRDHC8 DHC8401 1390041NM LAVATORY INTERMITTENT A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09401QX7146 4031 SEA - THE FORWARD LAVATORY SMOKE DETECTOR ALARM GOES OFF INTERMITTENTLY. MAINTENANCE INSPECTED THE DETECTOR AND THEN REPLACED SAME. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000362004071400036NM 2004 7 14 UPS04242676 120040621A5754 BRACKET BOEING727 72725C 138400HNM NR 5 SLAT STOP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C, NR 5 SLAT, O/B UPSTOP BOLT RETAINING BRACKET IS CRACKED. BRACKET REMOVED IAW SRM 51-30-02, BRACKET FABRICATED IAW SRM 51-30-01, BRACKET INSTALLED IAW SRM 51-30-1 & MM 20-80-01. STOP ADJUSTED TO WITHIN LIMITS IAW MM 27-81-11. 2L73 4F A3WE 20040714000452004071400045NM 2004 7 14 QXEA200400455 120040621A5420 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - CRACKED L-BRACKET TOP FORWARD RIGHT HAND ENGINE NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283 AND RD 8/471-032. 2H72 4T RTA13NM 20040714000502004071400050NM 2004 7 14 QXEA200400466 120040623A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - LEFT HAND NR 5 FLAP TRACK INBOARD LOWER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989. 2H72 4T RTA13NM 20040714000522004071400052NM 2004 7 14 QXEA200400468 120040623A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - LEFT HAND NR 5 SEAT TRACK INBOARD CENTER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989. 2H72 4T RTA13NM 20040714000672004071400067NM 2004 7 14 QXEA200400424 120040609A5710 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - LEFT HAND WING LEADING EDGE UPPER ATTACH BRACKET CRACKED YW384.5, YW137. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20040714000742004071400074EU 2004 7 14 UPS04142606 120040618A5313F5347524520000 STRINGER AIRBUSA300 A300F4622R 3930360EU FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01157UP 0005 STRINGER 45R DAMAGE AT FRAME 57 TO 58. REPLACED STRINGER IAW A300 SRM 51-40-21. 2L72 4F RTA35EU 20040714000972004071400097NM 2004 7 14 QXEA20400512 120040710A335061047811 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09345PH9126 127 476 PDX - THE FORWARD EMERGENCY LIGHT STRIP (RED PORTION) WILL NOT ILLUMINATE. REPLACED POWER SUPPLY NR 5. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000982004071400098NM 2004 7 14 QXEA200400449 120040618A5210 BUSHING DHAV DHC8 DHC8202 2809007NM PAX DOOR UNSECURE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09345PH16627 476 SEA - PASSENGER DOOR INTERMITTENTLY HANGS UP WHEN OPENING DOOR. MAINTENANCE INSPECTED THE DOOR AND RESECURED THE THREADED BUSHING ON MAIN CABIN DOOR AFT RAIL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000992004071400099NM 2004 7 14 QXEA200400461 120040621A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09364PH1158 524 PDX - EMERGENCY FLOOR PATH LIGHTING AT ROWS 1 AND 7 ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT PS6. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714001062004071400106NM 2004 7 14 151AW0021 120040702A5414 SKIN BOEING737 7373G7 1384595NM RT PYLON CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 RIGHT PYLON UPPER SKIN AT NAC STA 213 LBL 10 CRACKED AT PANEL CUTOUT. REPAIRED PER SB 737-54-1035. 2L72 4F RTA16WE 20040714001112004071400111WP 2004 7 14 CALA0400539 120040618A5320S2929169 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714871 48022 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 200-230, LBL 15. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-3. 2L72 4F A6WE 20040714001172004071400117NM 2004 7 14 151AW0002 120040702A5315 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 EXISTING DOUBLER AT RIGHT FWD SIDE OF BS 540 FLOORBEAM AT BL 0 CRACKED AND UNDERSIDE OF BS 540 LINK BEAM AT BL 0 CRACKED. REPLACED LINK BEAM AND LEFT AND RIGHT CHANNELS ON FLOORBEAM PER SRM 53-60-51 AND SRM 51-40-02. 2L72 4F RTA16WE 20040714001192004071400119SO 2004 7 14 MASA200400197 120040413A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07844MJ 145481 CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 12 LIGHT WAS INOP AFT SIDE. MX REPLACED A FAULTY ELECTRICAL SPLICE. OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040714001252004071400125EA 2004 7 14 MASA200400387 120040704A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777331 7331 FWD EMERGENCY FLOOR STRIP LIGHT INOP. CONTRACT MAINTENANCE RESECURED THE CONNECTION AND PERFORMED THE OPERATIONAL CHECKS. 2L72 4F RTA21EA 20040714001302004071400130NM 2004 7 14 151AW0005 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 O/B SIDE OF FLOOR FRAME CRACKED AT BS 639. REPAIRED FLOOR CHORD ANGLE PER SRM 51-70-12 AND SRM 51-40-02. 2L72 4F RTA16WE 20040714001352004071400135EA 2004 7 14 MASA200400310 120040603A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717217 7217 AFT CABIN SECTION EMERGENCY TRACK LIGHTING INOP. MX TROUBLESHOOTING. MX REPLACED THE NR 4 INVERTER. 2L72 4F RTA21EA 20040714001392004071400139SO 2004 7 14 MASA200400320 120040606A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07826MJ 145214 FLOOR EMERGENCY PROX LIGHTING INOP. MAINTENANCE RESET SYSTEM AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4T RTT00011AT 20040714001472004071400147EA 2004 7 14 MASA200400348 120040617A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0787353 7353 ONE SERVICE DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. PLACED ON MEL. MX RELAMPED. 2L72 4F RTA21EA 20040714001482004071400148EA 2004 7 14 MASA200400349 120040617A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW077305V6563 7305 SERVICE DOOR EMERGENCY FLOOD LIGHTS INOP. MX REPLACED NR 1 EMERGENCY BATTERY PACK, OPS CHECK GOOD. 2L72 4F RTA21EA 20040714001492004071400149EA 2004 7 14 MASA200400355 120040619A1420487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07652ML 7036 FLOOR PROXIMITY LIGHTING BETWEEN ROWS 1-5 INOP. MX REPLACED STRIP LIGHTING CONNECTOR. 2L72 4F RTA21EA 20040714001502004071400150SO 2004 7 14 MASA200400356 120040619A3350375914 SIGN EMB 145 EMB145LR 3260212SO ROW 12 BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW07831MJ 145273 CABIN EMERGENCY FLOOD LIGHT OVER ROW 12 INOP. AOG FOR PARTS, MX REPLACED THE EXIT SIGN ASSY, OPS CHECK GOOD. 2L72 4T RTT00011AT 20040714001552004071400155NM 2004 7 14 MASA200400368 120040623A3397 WIRE DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07445YV 445 THE CREW REPORTED THE RED EMERGENCY LIGHT AT ROW 1 INOP. MX RECONNECTED THE LOOSE WIRE TO THE LIGHT, NO PARTS USED. 2H72 4T RTA13NM 20040714001572004071400157NM 2004 7 14 DL73S040580 120040621A2120 ODOR BOEING737 737247 138448DNM COCKPIT DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27244WA 23518 EN ROUTE AT 33,000 FT STRONG ELEC ODOR IN THE VICINITY OF THE COPILOTS CIRCUIT PANEL. NO SMOKE. INSPECTED AREA AND RAN ENGINES/PACKS. UNABLE TO DUPLICATE. 2L72 4F A16WE 20040714001582004071400158NM 2004 7 14 DL76G040589 120040622A5522 SKIN BOEING767 767332 1382001NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO271608 000815 30573 THE RIGHT AND LEFT INBOARD ELEVATORS WERE FOUND WITH DAMAGE ON THE LOWER SKIN PANELS. THE DAMAGE EXTENDS THROUGH THE OUTER SKIN, INNER SKIN, AND HONEYCOMB CORE. REPAIRED PER ER/A 417308-14. 2L72 4F RTA1NM 20040714001592004071400159NM 2004 7 14 DL76G040590 120040622A5522 SKIN BOEING767 767332 1382001NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO271609 000816 30574 THE RIGHT AND LEFT INBOARD ELEVATORS WERE FOUND WITH DAMAGE ON THE LOWER SKIN PANELS. THE DAMAGE EXTENDS THROUGH THE OUTER SKIN, INNER SKIN, AND HONEYCOMB CORE. REPAIRED PER ER/A 417308-14. 2L72 4F RTA1NM 20040714001602004071400160 2004 7 14 DL76L040591 420040622A344020412220407 DISPLAY BOEING767 767332 1382001NM RADAR INOPERATIVE A DALAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO27179DN 25144 WX RADAR NOT WORKING. REPLACED TRANSCEIVER. 2L72 4F RTA1NM 20040714001622004071400162NM 2004 7 14 DL73S040622 120040630A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27322DL 23094 THE FUSELAGE SKIN WAS FOUND WITH A TYPICAL 3.5 INCH LONG CRACK ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 18L NEAR FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 091605-14. 2L72 4F RTA16WE 20040714001662004071400166NM 2004 7 14 CALA0400570 120040710A3350D71701100 BATTERY PACK BOEING737 737824 13844BZNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2712218 28778 THE EMERGENCY LIGHTS IN THE FIRST FIVE ROWS OF COACH SECTION WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06-960-80P. 2L72 4F RTA16WE 20040714001682004071400168WP 2004 7 14 CALA0400572 120040624A53135936034 LONGERON DOUG DC9 DC981 3022081WP STA CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714871 48022 INSPECTION FOUND A SMALL CRACK IN LOWER EDGE OF THE VERTICAL LEG OF LONGERON 20L AT APPROXIMATELY STA 995. THE CRACK RAN FROM THE BOTTOM EDGE OF THE VERTICAL FLANGE TO THE FIRST FASTENER HOLE LOCATION WHERE IT TERMINATED. THE LONGERON WAS REPAIRED IAW ECRA 5311-01198. 2L72 4F A6WE 20040714001692004071400169NM 2004 7 14 SWAA041966 120040712A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040714001702004071400170NM 2004 7 14 SWAA041967 120040712A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 188, STRINGER 17R, BS 188, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040714001712004071400171NM 2004 7 14 SWAA041969 120040712A53306545765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 516, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040714001722004071400172 2004 7 14 SWAA041959 420040712A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040714001752004071400175NM 2004 7 14 SWAA041962 120040712A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR LWR HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040714001762004071400176 2004 7 14 SWAA041963 420040712A256565C16820 GIRT BAR BOEING737 7373H4 1384600NM R1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOK RIVETS PER MM. 2L72 4F RTA16WE 20040714001772004071400177NM 2004 7 14 372PA0046 120040706A335020131A BATTERY PACK BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT INOP. REPLACED RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-00. 2L72 4F RTA16NE 20040714001792004071400179NM 2004 7 14 237TR0006 120040710A33501000679 LIGHT BOEING737 737228 13844AGNM PAX DOOR INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05237TR 23007 LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD. 2L72 4F RTA16WE 20040714001812004071400181NM 2004 7 14 CALA0400557 120040629A531565C339503 FLOORBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714601 27314 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 42. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW ECRA 5321-01196. 2L72 4F RTA16WE 20040714001832004071400183NM 2004 7 14 513NA0008 120040628A1430 BOLT BOEING757 7572T7 1384914NM MLG WHEEL MISSING A PIDAK NONE O OTHER ININSP/MAINT 1 SO05513NA 23895 DURING WALK-AROUND, FOUND NR 7 MAIN WHEEL ASSEMBLY TIE BOLT MISSING. REPLACED NR 7 MAIN WHEEL ASSEMBLY PER MM 32-45-01. 2L72 4F RTA2NM 20040714001842004071400184 2004 7 14 151AW0025 420040709A22104084042911 COUPLER BOEING737 7373G7 1384595NM YAW DAMPER MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05151AW 23219 YAW DAMPER DISENGAGES INTERMITTENTLY. REPLACED YAW DAMPER COUPLER PER MM 27-12-31. SYSTEM TEST NORMAL. 2L72 4F RTA16WE 20040714001852004071400185 2004 7 14 371PA0045 420040624A2220 SENSOR BOEING737 737306 13844BGNM ELEVATOR OUT OF ADJUST A PIDAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO05371PA 23543 AIRCRAFT CLIMBS ON AUTO PILOT DURING CRUISE FLIGHT AT .780 AND ABOVE. STAB OUT OF TRIM ILLUMINATES. PLACED MACH TRIM ON MEL 22-5. 6/26/2004: ADJUSTED BOTH STAB (ELEVATOR) POSITION SENSOR RODS. CHECKED GOOD PER FMC ELEVATOR RIG, AUTO PILOT AND AUTO LAND TESTS. 2L72 4F RTA16NE 20040714001862004071400186 2004 7 14 371PA0046 420040624A2210 AUTOPILOT SYS BOEING737 737306 13844BGNM MALFUNCTIONED A PIDAO OTHER O OTHER DEDESCENT 1 SO05371PA 23543 DURING DESCENT ON -B- AUTO PILOT -AP- WARNING LIGHT FLASHES WITH -CWSP & CWSR- ANNUNCIATIONS AT SAME TIME. PLACED AUTO PILOT -B- CHANNEL ON MEL 22-1. 6/29/04: BITE CHECKED NORMAL. SWAPPED DAA'S FOR FURTHER EVALUATION. BOTH AUTO PILOTS BITE PASSED. CLEARED MEL 22-1. 2L72 4F RTA16NE 20040714001872004071400187NM 2004 7 14 QXEA200400487 120040622A3620 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09412QX 4059 SEA FLIGHT 2381, DESCENDING OUT OT 10,000 FT WHEN POWER WAS REDUCED TO APPROXIMATLEY 10 PERCENT TORQUE, NR 1 BLEED HOT CAUTION LIGHT CAME ON. AFTER FOLLOWING CHECKLIST, CAUTION LIGHT WENT OUT. MAINTENANCE INTERROGATED CDS. NO FAULTS FOUND. GROUND RAN NR 1 BLEED SYSTEM FULL HOT THEN FULL COLD, NO CAUTION LIGHT. PERFORMED OPS TEST OF ECS TEMPERATURE CONTROL SYSTEM, TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714001912004071400191NM 2004 7 14 371PA0047 120040703A3350 LIGHT BOEING737 737306 13844BGNM CABIN CONTAMINATED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05371PA 23543 AFT EMERGENCY PATH LIGHTING WILL NOT COME ON. DRIED WATER FROM TRACK. OPS CHECKS OK PER MM 25-60-00. 2L72 4F RTA16NE 20040714001922004071400192NM 2004 7 14 UPS04542629 120040701A2750 ADC BOEING757 75724APF 1384969NM TE FLAPS MALFUNCTIONED A IPXAO OTHER O OTHER APAPPROACH 1 SO01448UP 27737 INSPECTION TYPE:N/A AT 1500 FT FLAPS 30 WERE SELECTED AT 155 KTS FLAPS DID NOT MOVE BEYOND 20 WITH NO OTHER INDICATION. GO AROUND INITIATED AND T/E DISAGREE ILLUMINATED. T/E FLAP DISAGREE COMPLETED AND LANDING ACCOMPLISHED WITH LT FLAP PROCEDURE. ACCOMPLISHED FSEU BITE IAW FIM 27-51-00 NR 1 FSEU FLIGHT FAULT FLAP FAIL DISPLAYED. ACCOMPLISHED FIM 27-51-00 FIG 107. REPLACED LT ADC PER BLT NR 2. REF MM 34-12-01-4. LT ADC, OPS CHECKS GOOD. 2L72 4F RTA2NM 20040714001942004071400194WP 2004 7 14 UPS04842621 120040615A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C, GOUGE ON SEAT TRACK AT FS 1310 45 LBL. BLEND GOUGE AREAS IAW DC8 SRM 53-2-0, OUT OF LIMITS. LOCATED & DRILLED SEAT TRACK PLUG DC8-53B-007-002 & DC8-53B-007-006, CHANNEL IAW DC8 UPS EO DC8-5340-7779. ALODINED & PRIMED IAW SRM 51-1-8, INSTALLED PLUG & CHANNEL IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040714001972004071400197WP 2004 7 14 UPS04842624 120040621A53305613862 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C, NOSE EXT PWR RECEPTICAL DOOR PNL CUTOUT HAS BROKEN SECTION. REMOVED INNER DOUBLER IAW DC8 SRM 51-1-21. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 428102.3 IAW DC8 DWG 5613862 & DC8 SRM 51-9-0 FIG 68A. FAB NEW DOUBLER, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-1-21 & 51-1-21A. 2L74 4F RT4A25 20040714001982004071400198WP 2004 7 14 UPS04842625 120040621A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C, EXISTING REPAIR DOUBLER AT EXT PWR RECEPTICAL FOUND TO HAVE PREVIOUS DAMAGE ON FAYING SURFACE (GOUGE). REMOVED DOUBLER. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 442690.4 IAW DC8 SRM 53-2-0 & 51-9-0 FIG 68A. FAB DOUBLER IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-2 & 51-1-21A. 2L74 4F RT4A25 20040714002012004071400201NM 2004 7 14 UPS04M42628 120040702A5210 BOTTLE DOUG MD11 MD11F 3023600NM L1 DOOR DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP L1 PRESS LOW FOUND ON PREFLIGHT SERVICED L1 DOOR EMERGENCY OPEN NITROGEN BOTTLE IAW AMM 12-25-04, PRESSURE CHECKED GOOD. 2L73 4F RTA22WE 20040714002032004071400203SO 2004 7 14 MASA200400337 120040614A32608005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212SO NLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07843MJ 145478 RETURNED TO THE FIELD DUE TO LANDING GEAR WILL NOT RETRACT AND LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. A/C FERRIED TO CLT FOR REPAIR. MX REPLACED THE NLG DOOR PROXIMITY SENSOR SWITCH AND THE SYSTEM OPS CHECKS GOOD. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20040714002042004071400204SO 2004 7 14 MASA200400344 120040616A5310 STRUCTURE EMB 145 EMB145LR 3260212SO FUSELAGE BIRD STRIKE A MASAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07858MJ 145767 RETURNED TO FIELD DUE TO A BIRD STRIKE DURING TAKEOFF ROLL. DAMAGE AT FWD FUSELAGE 1 CLOSE TO FRAME 5 AND STRINGER 6R INFORMATION WAS FORWARDED TO EMB. INITIALLY A/C WAS GOING TO FERRY TO BNA FOR REPAIR BUT EMBRAER STRUCTURAL ENGINEERING GRANTED A 500 FLT CYCLE FLY ON. COMPLETED RO WITH CONTRACT MX AND A/C REPOSITIONED TO PHL. MX COMPLIED WITH RO EMB145-53-1160. 2L72 4T RTT00011AT 20040714002052004071400205NM 2004 7 14 SWAA041942 120040709A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927, STRINGER 27L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040714002062004071400206NM 2004 7 14 SWAA041943 120040709A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040714002072004071400207 2004 7 14 SWAA041944 420040710A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040714002092004071400209 2004 7 14 SWAA041946 420040710A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C4 CHECK, FOUND L1 & L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 & L2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040715000012004071500001NM 2004 7 15 DL76G040626 120040702A2780851801 SENSOR BOEING767 767332 1382001NM NR 1 SLAT MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO271612T 30575 LEADING EDGE SLAT ASYM ON TAKEOFF OUT OF EHAM. LIGHT CAME ON GOING FROM FLAPS 1 WITH FLAP HANDLE UP. PSEU LEFT SLAT 1 INBD SENSOR 282 PER AMM REPLACED SENSOR PER AMM. OPS OK PSEU NO FAULTS ALL NEAR/FAR INDICATIONS GOOD FOR DIFFERENT SLAT POSITIONS. OK FOR SERVICE. SLATS CHECKED, NO ACTUAL ASYMMETRY. 2L72 4F RTA1NM 20040715000022004071500002NM 2004 7 15 DL76L040627 120040628A2530251009133 OVEN BOEING767 767332 1382001NM AFT GALLEY WORN A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27180DN 25985 AFT GALLEY UPPER OVENS ON F/O SIDE IS BURNING THE WALL. FOUND DOOR SEAL ON OVEN WORN. REPLACED OVEN. 2L72 4F RTA1NM 20040715000062004071500006NM 2004 7 15 DL757040631 120040706A5330143N34719 SKIN BOEING757 757232 1384965NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27663DN 24992 FUSELAGE SKIN DENTED AT STR 27L AND STATION 450. AREA REPAIRED IAW ERA 091136-14. 2L72 4F RTA2NM 20040715000092004071500009NM 2004 7 15 DL757040634 120040707A5330143N34719 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27663DN 24992 FUSELAGE SKIN SUFFERED LIGHTNING STRIKE DAMAGE BETWEEN STA 480 AND STR 27R. AREA REPAIRED IAW ERA 091141-14. 2L72 4F RTA2NM 20040715000102004071500010NM 2004 7 15 SWAA041949 120040710A52306547955 DOUBLER BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR DOUBLER AT BS 793, RBL 9, CRACKED. REPAIRED DOUBLER PER EA. 2L72 4F RTA16WE 20040715000112004071500011NM 2004 7 15 QXEA200400488 120040630A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09364PH16987324 524 PSC - EMERGENCY FLOOR STRIP LIGHTING, SECOND STRIP, FORWARD 2 RED LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PS6. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040715000122004071500012SO 2004 7 15 MASA200400289 120040524A30403801D2MODA CONTROLLER EMB 145 EMB145LR 3260212SO WINDSHIELD HEAT BURNED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07835MJ 145353 CAPTAIN REPORTED THAT WHEN THE NR 1 WINDSHIELD HEAT IS TURNED ON THAT A ELECTRICAL BURNING ODOR IS PRESENT IN THE COCKPIT. MAINTENANCE TROUBLESHOT TO WINDSHIELD CONTROLLER. REPLACED NR 1 WINDSHIELD HEAT TEMPERATURE CONTROLLER. 2L72 4T RTT00011AT 20040715000162004071500016SO 2004 7 15 MASA200400319 120040606A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07827MJ 145217 RETURNED TO FIELD MAIN LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. LANDING LEVER DISAGREE MESSAGE. AIRCRAFT FERRIED GEAR DOWN TO CLT FOR REPAIRS. MX REPLACED 2 PROXIMITY SWITCHES, WIRING HARNESS AND LANDING GEAR CONTROL LEVER. PERFORMED GEAR SWING AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040715000172004071500017SO 2004 7 15 MASA200400321 120040607A2731 PITCH CONTROL EMB 145 EMB145LR 3260212SO TRIM SYS MALFUNCTIONED A MASAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW07838MJ 145384 ABE-PIT HAD THE MAIN AND BACKUP PITCH TRIM INOP DURING APPROACH INTO PIT AFTER AUTO PILOT WAS DISENGAGED. MAINTENANCE INSPECTED SYSTEM AND PERFORMED OPERATIONAL CHECK AND FOUND NO DEFECTS. A/C DEPARTED WITHOUT FURTHER INCIDENT. NO PARTS USED. 2L72 4T RTT00011AT 20040715000192004071500019 2004 7 15 SWAA041939 420040709A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29074SW 22674 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040715000202004071500020NM 2004 7 15 SWAA041940 120040709A57546573714 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED RT WING NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20040715000212004071500021NM 2004 7 15 SWAA041941 120040709A575365C30462 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD FORE FLAP PER MM. 2L72 4F RTA16WE 20040715000222004071500022NM 2004 7 15 SWAA041950 120040710A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 794, RBL 7 TO RBL 11, CORRODED. REPAIRED SHEAR TIE PER EA. 2L72 4F RTA16WE 20040715000232004071500023NM 2004 7 15 SWAA041951 120040710A57536541475274 SKIN BOEING737 7373A4 1384585NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040715000272004071500027 2004 7 15 SWIA200413551 420040703A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO INTEGRATED ALARMMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07579SW 120347 COULD NOT CLEAR STALL LIGHT ON SYS 1, IT TOOK NUMEROUS ATTEMPTS TO CLEAR SYS 2. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N 120-34428-505. 2L72 4T RTA31SO 20040715000282004071500028EA 2004 7 15 SWIA200413552 120040705A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07429SW LEFT OUTBOARD SPOILERON FAULT, WILL NOT CLEAR. INSTALLED SERVICEABLE PCU ON LEFT SPOILERON OUTBOARD POSITION. OPERATIONAL CHECK GOOD IAW 27-62-01. P/N: 27000-7, S/N OFF: 4403. 2L72 4F RTA21EA 20040715000302004071500030SO 2004 7 15 SWIA200413554 120040708A27523430001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAP LEAKING A SWIAO OTHER KF FLUID LOSS FLT CONT AFFECTED NRNOT REPORTED 1 NM07227SW9756 9756 120304 LOST GREEN SYSTEM HYDRAULIC FLUID QUANTITY AND PRESSURE. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR AS PER MM 27-50-09. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040715000322004071500032NM 2004 7 15 SWAA041971 120040713A33506114789 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND AFT SERVICE EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PER MM. 2L72 4F A16WE 20040715000332004071500033NM 2004 7 15 SWAA041972 120040713A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE AT AFT ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040715000342004071500034NM 2004 7 15 SWAA041973 120040713A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT FWD ENTRY DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040715000352004071500035NM 2004 7 15 SWAA041974 120040713A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT FWD SERVICE DOOR LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040715000362004071500036NM 2004 7 15 SWAA041975 120040713A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 907, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040715000372004071500037NM 2004 7 15 SWAA041976 120040713A531165C37762 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB. 2L72 4F RTA16WE 20040715000392004071500039NM 2004 7 15 SWAA041978 120040713A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 706, STRINGER 11R AND STRINGER 11L CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040715000402004071500040NM 2004 7 15 SWAA041979 120040713A53106546958 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT RIGHT BS 460 TO RIGHT BS 480, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040715000412004071500041NM 2004 7 15 SWAA041980 120040713A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 947, LBL 8, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040715000452004071500045NM 2004 7 15 SWAA041984 120040713A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS AT ROW 2 DEF, ROW 14 DEF, ROW 16 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040715000462004071500046 2004 7 15 SWAA041985 420040713A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040715000482004071500048SO 2004 7 15 SWIA200413510 120040623A2797 WIRE EMB 120 EMB120ER 3260203SO TRIM SWITCH BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW 120039 FIRST OFFICER'S ELECTRIC TRIM WHEN PUSHED FORWARD, SETS OFF THE TRIM FAIL WARNING. REPAIRED WIRE AT TRIM SWITCH. 2L72 4T RTA31SO 20040715000492004071500049EA 2004 7 15 SWIA200413511 120040622A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07906SW 7510 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11. 2L72 4F4 FRTA21EA E15NE 20040713001042004071300104SO 2004 7 13 SIMA200413001 120040505A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZONTAL STAB INOPERATIVE A SIMAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 SW21814AE 145541 ORD - FLT 4303 - DURING DESCENT, CREW REPORTED PITCH TRIM ONE AND TWO TO BE INOPERATIVE WITH NO EICAS MESSAGE. MAINTENANCE COMPLIED WITH ETN EB 27-022 AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND HSCU SHOCK MOUNTS. OPERAITONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040713001052004071300105 2004 7 13 GTIA040328 420040418A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FLL - FLT 433 - L2 DOOR SLIDE FELL OFF. INSTALLED SLIDE ASSEMBLY. (M) 2L72 4F A6WE 20040713001062004071300106 2004 7 13 GTIA040329 420040415A2565 BRACKET DOUG DC9 DC983 3022083WP GIRT BAR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 DTW - FOUND GIRT BAR BRACKET ON FLOOR, DOOR L2 IS LOOSE. INSTALLED PROPER LENGTH SCREWS. (M) 2L72 4F RTA6WE 20040713001122004071300112SO 2004 7 13 SIMA200412701 120040504A274036721005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO E/E BAY INOPERATIVE A SIMAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW21628AE 145124 GSP - FLT 3758 - DURING MAIN TRIM SWITCH ACTIVATION CREW REPORTED AN EICAS WARNING PITCH TRIM MAIN INOPERATIVE AND PITCH TRIM BACKUP INOPERATIVE. COMPLIED WITH CHECKLIST AND PITCH TRIM C/B RESET PROCEDURE WAS PERFORMED. MAIN AND BACKUP TRIM SYSTEMS BOTH RECOVERED. MAINTENANCE COMPLIED WITH ETN EM 27-028R1 AND REMOVED AND REPLCED THE HSCU IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040713001382004071300138NM 2004 7 13 USAASB04050 120040503A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19439US 24781 PIT - PILOT REPORTED THE RIGHT FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD BATTERY CHARGER ASSEMBLY. OPERAITONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20040713001672004071300167EA 2004 7 13 ASOA04324 120040430A3240158863 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA PARKING BRAKE MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11823AS 7196 FLT 4615 - DURING APPROACH INTO DFW FROM VPS, A PARKING BRAKE SHUTOFF VALVE AND ANTI-SKID INBOARD CAUTION MESSAGES WERE RECEIVED SHORTLY AFTER GEAR EXTENSION. QRH PROCEDURES WERE COMPLIED WITH AND AFTER GEAR RETRACTION, BOTH MESSAGES EXTINGUISHED. DUE TO THE POSSIBLITY OF UNCOMMANDED HYDRUALIC PRESSURE IN THE BRAKE LINES, THE CREW REQUESTED EMERGENCY VEHICLES BE ON STANDBY AS A PRECAUTION. UPON GER REEXTENSION, THE MESSAGES DID NOT REOCCUR AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE PARKIGN BRAKE SHUTOFF VALVE. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040713001682004071300168EU 2004 7 13 ASOA04315 120040413A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE Z-FLOOR SUPPORT ON THE LEFT SIDE FROM FS 39 TO FS 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT ON THE LEFT SIDE FROM FS 39 TO FS 40 IAW SRM 51-25-03. (M) 2H72 4T RT 20040713001692004071300169EU 2004 7 13 ASOA04310 120040413A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE SEAT TRACKS FROM FS 39 TO FS 40 ON THE RIGHT SIDE AND FROM FS 39 TO FS 41 ON THE LEFT SIDE WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS FROM FS 39 TO FS 40 ON THE RIGHT SIDE AND FROM FS 39 TO FS 41 ON THE LEFT SIDE IAW SRM 51-25-04. (M) 2H72 4T RT 20040713001722004071300172EU 2004 7 13 SIMA200412101 120040423A54147075T6 SKIN SAAB SF340 340B 7860101EU LEFT NACELLE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21391AE 340B391 ABI - DURING AN MBV INSPECTION, THE LEFT NACELLES INBOARD SKIN AT THE WING TO NACELLE FAIRING WAS FOUND TO BE CHAFED. BLENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTION, NO DEFECTS NOTED FABRICATED A DOUBLER AND TRIPLER. ALSO FABRICATED SHIMS. REPAIR DONE IAW SAAB 340 SRM, (72LKS 3079 REV 43) 54-10-10, PAGE 205-210 FIG 208. (M) 2L72 4T RTA52EU 20040713001732004071300173EU 2004 7 13 SIMA200412102 120040421A53117253814437 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21341SB 340B341 ABI - DURING AN MBV INSPECTION, FOUND FRAME 640 TO BE DENTED 12.5 INCHES ABOVE THE FLOOR. REMOVED FRAME AND INSTALLED NEW FRAME IAW SAAB 340 SRM 72LKS 3079 REV 43, 51-40-21, 51-40-40, 51-40-22, AND 51-40-40. (M) 2L72 4T RTA52EU 20040713001742004071300174EU 2004 7 13 SIMA200412703 120040505A2120QB0443 FILTER SAAB SF340 340B 7860101EU CABIN CONTAMINATED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21373AE 340B373 DFW - FLT 3364 - CREW REPORTED A STRONG SMELL LIKE BURNING RUBBER COMING FROM BOTH PACK BLEED AIR SYSTEMS INTO COCKPIT AND GALLEY AREAS. MOST NOTICEABLE AT LOW ALTITUDE AND LOW POWER SETTING. SEEMS TO BE MORE FROM RIGHT SIDE PACK THAN FROM THE LEFT PACK. MAINTENANCE REPLACED THE COCKPIT AND CABIN AIR FILTERS IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040713001762004071300176NM 2004 7 13 UIEA200400093 120040512A2612 WARNING LIGHT BOEING747 7472D3B 1384805NM CARGO FIRE FALSE ACTIVATIONA UIEAABG UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 EA15506MC 21252 AFT CARGO FIRE WARNING LIGHT ILLUMINATED, CAUSING FIRE WARNING. CARRIED OUT PROCEDURE IAW QRH. RETURNED FOR LANDING. CARRIED OUT INSPECTION OF AFT CARGO IAW MM 26-16-00. NO EVIDENCE OF SMOKE OR FIRE DAMAGE. OFF LOADED CARGO FOR INSPECTION. ALL SYSTEM NORMAL, FIRE TEST CARRIED OUT. OPS CHECKED SATISFACTORY. CARRIED OUT CONDITIONL IAW MM 5-51-39, SEE LOG PAGE 82077 ITEM NR 1/2. (M) 2L74 4F RTA20WE 20040713001772004071300177EA 2004 7 13 A6WA200440058 120040508A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31434AW 7322 LEFT AND RIGHT VERICAL SUPPORT ANGLES ARE CRACKED AT FS 280. REMOVED CRACKED ANGLES P/N 601R31113-58 AND P/N 601R31113-57 AND INSTALLED NEW ANGLES P/N 601R31113-58 AND P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2L72 4F RTA21EA 20040713001782004071300178WP 2004 7 13 ASAA0480327 120040421A5320ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURNG HV CHECK, FOUND LOWWR RING SRFC OF FUEL ACCESS PANEL 1470C IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PANEL PER 51-22-2A. (M) 2L72 4F RTA6WE 20040713001792004071300179WP 2004 7 13 ASAA0480326 120040421A5730ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - DURNG HV CHECK, FOUND FRETTING CORROSION ON FUEL ACCESS PANEL 1456C. REMOVED AND REPLACD FUEL ACCESS PANEL PER 51-22-2A. (M) 2L72 4F RTA6WE 20040713001842004071300184 2004 7 13 AMTA200400532 420040506A2565 LANYARD BOEING757 75723N 1384973NM R1 DOOR SLIDE MISINSTALLED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11523AT 30232 UNABLE TO DISARM DOOR 1R. FOUND ROPE/LANYARD TO BE INPROPERLY STOWED ON SLIDE AND WAS INTERFERING WITH THE GIRT BAR. STOWED ROPE/LANYARD PROPERLY, AND OPS CHECKED PER AMM 52-11-25. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20040714000022004071400002NM 2004 7 14 QXEA200400479 120040624A5420 TUBE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX5990 4060 PDX - THE FORWARD LOWER TRUSS TUBE IS CHAFED. MAINTENANCE REPAIRED THE TRUSS IAW EA 6-54-302. 2H72 4T RTA13NM 20040714000032004071400003NM 2004 7 14 QXEA200400491 120040702A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM ZONE 200 FALSE INDICATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09352PH15943 494 SEA - FLIGHT 2002 - WHILE ON APPROACH, THE CREW RECEIVED A SMOKE WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000272004071400027EA 2004 7 14 QXEA200400510 120040709A3620 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09612QX 10042 SFO FLIGHT 2475, LEFT ENGINE BLEED CAUTION MESSAGE CAME ON AFTER LANDING AND STAYED ON FOR 3-5 MINUTES. MESSAGE WENT AWAY BEFORE ABNORMAL CHECKLIST WAS ACCOMPLISHED. MAINTENANCE INTERROGATED MDC. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040714000292004071400029EA 2004 7 14 QXEA200400498 120040703A2611 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA SMOKE DETECTOR DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 FORWARD BAGGAGE BAY CHIMNEY ASSEMBLY ABOVE DOOR IS DAMAGED. THE CARGO BAY CHIMNEY WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040714000322004071400032EU 2004 7 14 UPS04142695 120040711A2560 COVER AIRBUSA300 A300F4622R 3930360EU ESCAPE ROPE UNSECURE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01133UP 0817 F/O'S EMERGENCY ESCAPE ROPE COVER NEEDS SECURED. INSTALLED NEW VELCRO AND SECURED COVER. 2L72 4F RTA35EU 20040714000442004071400044NM 2004 7 14 QXEA200400454 120040621A7110 COLLAR BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09414QX 4061 PDX - CHAFING AROUND OUTSIDE OF HORSE COLLAR. REPAIRED IAW HORIZON AIR EA 6-54-301. 2H72 4T RTA13NM 20040714000462004071400046NM 2004 7 14 QXEA200400462 120040623A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - SEAT TRACK NR 10 HAS SUSPECTED PITTING CORROSION AT STATION X277. REPAIRED IAW SRM 51-40-11. 2H72 4T RTA13NM 20040714000492004071400049NM 2004 7 14 QXEA200400465 120040623A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - LEFT HAND NR 4 FLAP TRACK OUTBOARD UPPER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20040714000572004071400057WP 2004 7 14 UPS04842691 120040630A5347S2772660 SEAT TRACK DOUG DC8 DC873F 302199FWP 600 RBL 60 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, FWD PIT FS 600 MIDDLE ROW OF FASTENERS IN SEAT TRACK SPLICE (AS SEEN FROM BELOW) LOCATED AT BC 60 R- CORROSION AROUND FASTENERS & SPACER. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. MAT ID FOR SEAT TRACK SPLICES A & B 7075-T6 .160 PO 333834.1 IAW DC8 SRM 53-2-3. FABBED CENTER SEAT TRACK SPLICES A & B, OB & I/B C, D & E SPLICES IAW DC8 SRM 51-1-8, INSTALLED CENTER SEAT TRACK & SPLICES A & B, I/B & O/B & C, D & E. INSTALLED FLOOR PANEL STA 580-608 RBL 60, AIR GRILL STA 513-702. 2L74 4F RT4A25 20040714000712004071400071NM 2004 7 14 QXEA200400485 120040629A7810 SHROUD BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 PDX - NR 2 EXHAUST SHROUD DECK CRACKED ABOVE CHANNEL AT AFT EXHAUST EJECTOR SHROUD AFT ATTACH BOLTS. REPAIRED IAW RD 8/4-54-044. 2H72 4T RTA13NM 20040714000802004071400080NM 2004 7 14 QXEA200400481 120040629A33506138001 BATTERY PACK BOMBDRDHC8 DHC8401 1390041NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09539DS103 4016 PDX - FORWARD LEFT EGRESS LIGHT, FORWARD CENTER OVERHEAD EXIT SIGN, MAIN CABIN DOOR EXIT SIGN AND FORWARD CEILING AISLE EMERGENCY LIGHTS FAIL TO ILLUMINATE WHEN SELECTED ON. CHECKED CHARGING VOLTAGE TO EMERGENCY BATTERIES LEFT HAND AND RIGHT HAND. VOLTAGE CHECKS GOOD. REPLACED EMERGENCY BATTERIES LEFT HAND (S/N 0202081) AND RIGHT HAND (S/N 0303184). OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000812004071400081WP 2004 7 14 UPS04842692 120040614A5347S2772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3, FS 1580, RBL 24 FLOOR TRACK GOUGED (DOT B7269). BLENDED GOUGED AREA, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. MAT ID FOR SEAT TRACK 60-15176/2772660 PO SP0916641. LOCATED & DRILLED HOLES. ALODINED & PRIMED, TRANSFERRED SPACERS 2 EACH FROM OLD TO NEW SEAT TRACK, INSTALLED SEAT TRACK TO WEB & FLOORBEAMS. DRILLED HOLES FROM FLOORBOARD. REINSTALLED FLOORBOARDS STA 1520-1600, RBL 20, 1600-1680 RBL 24. 2L74 4F RT4A25 20040714000852004071400085WP 2004 7 14 UPS04842697 120040701A57125769589 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3, RIGHT CENTER L/E RIB CRACKED AT APPROX STA 379.000 VERIFIED BY NDT. STOP DRILL CRACK. MAT ID FOR RIB AT XFS 379 .063 7075-T6. MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. ACCOMPLISHED HFEC INSP OF STOP DRILL IAW DAC NTSPM 06 10-01.001. FAB REPAIR ANGLE, ALODINED & PRIMED REPAIR ANGLE IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0. 2L74 4F RT4A25 20040714000902004071400090WP 2004 7 14 UPS04842634 120040613A53203773479514 FITTING DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, LOWER CUSP FITTING CRACKED IN B-PIT TUNNEL, RIGHT SIDE, STA 560 (FRAME TO BEAM ATTACH FITTING). REMOVED CRACKED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DAC DWG 3773479. INSTALLED FITTING PER SRM 51-1-20D, 51-3-0, 51-1-8. 2L74 4F RT4A25 20040714001042004071400104NM 2004 7 14 151AW0022 120040702A5754 SKIN BOEING737 7373G7 1384595NM NR 2 SLAT CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 NR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01. 2L72 4F RTA16WE 20040714001152004071400115NM 2004 7 14 CALA0400569 120040708A323365446104 ACTUATOR BOEING737 7373T0 1384582NM NLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW271232728591 23457 THE NOSE LANDING GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. THE RED UNSAFE LIGHT WAS ILLUMINATED. THE GEAR WAS CYCLED AND THE NLG EXTENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG RETRACT ACTUATOR AT FAULT. THE RETRACT ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-11. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040714001232004071400123SO 2004 7 14 MASA200400379 120040630A335066368 LIGHT EMB 145 EMB145LR 3260212SO ROW 15 & 16 INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 FLOOR PROXIMITY LIGHT STRIP BETWEEN SEAT ROWS 15 AND 16 INOP. REPLACED LIGHT STRIP. 2L72 4T RTT00011AT 20040714001262004071400126NM 2004 7 14 151AW00030 120040702A5320 SPLICE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER SPLICE CRACKED AT STRINGER 4 RT AT BS 907 AND AT STRINGER 4 LT AT BS 907. REPLACED STRINGER SPLICE AT 4 RT AND 4 LT PER SRM 51-40-02. 2L72 4F RTA16WE 20040714001372004071400137EA 2004 7 14 MASA200400312 120040604A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 11 INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0727173 7173 CREW REPORTED THE FLOOR PROXIMITY ESCAPE PATH EMERGENCY LIGHT STRIP AT ROW 11 NOT ILLUMINATING. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. NO PARTS USED. 2L72 4F RTA21EA 20040714001382004071400138EA 2004 7 14 MASA200400315 120040605A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0717358 7358 THE CAPTAIN REPORTED A FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB, OPS CHECK GOOD. 2L72 4F RTA21EA 20040714001512004071400151EA 2004 7 14 MASA200400359 120040620A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CONTAMINATED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0775987 7405 FLOOR EMERGENCY PROXIMITY LIGHTING BETWEEN ROWS 3-8 INOP. MX CLEANED MOISTURE SOAKED STRIPS AND CONNECTORS. OPS CHECKED GOOD, NO PARTS REPLACED. 2L72 4F RTA21EA 20040714001522004071400152EA 2004 7 14 MASA200400360 120040620A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0777331 7331 ONE FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. PLACED ON MEL. MX RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20040714001532004071400153SO 2004 7 14 MASA200400363 120040621A335082324 LIGHT EMB 145 EMB145LR 3260212SO PAX CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07834MJ 145340 THE AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THAT THE ROW 12 CEILING EMERGENCY EXIT SIGN LIGHT INOP. REPLACED THE LIGHT STRIP, OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20040714001542004071400154EA 2004 7 14 MASA200400367 120040622A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0775991 7422 THE PILOT REPORTED THE MAIN CABIN FWD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20040714001642004071400164NM 2004 7 14 DLM88040624 120040704A2622892480 EXTINGUISHER DOUG MD88 MD88 3023688NM CABIN LEAKING A DALAK NONE K FLUID LOSS ININSP/MAINT 1 SO27905DE 53410 AFT WATER FIRE EXTINGUISHER LEAKING. REPLACED SAME. 2L72 4F RTA6WE 20040714001802004071400180WP 2004 7 14 CALA0400556 120040629A3350AD4002P BATTERY DOUG DC9 DC982 3022082WP STA INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2772822 49482 THE CABIN OVERHEAD EMERGENCY LIGHTS WOULD NOT ILLUMINATE BETWEEN ROWS 10-18. THE POWER PACK BATTERIES AT STA 500 WERE REMOVED AND REPLACED IAW MM 33-53-00. 2L72 4F A6WE 20040714001882004071400188NM 2004 7 14 CALA0400558 120040630A53206545805 SHEAR WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND A .75 INCH CRACK IN SHEAR WEB AT LEFT SIDE OF FLOORBEAM WEB, STA 277, S18L. THE CRACKED AREA WAS CUT OUT AND A SHEAR TIE WAS INSTALLED IAW SRM 53-00-07. 2L72 4F RTA16WE 20040714001892004071400189NM 2004 7 14 CALA0400559 120040701A5347655384426 CARGO TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND CARGO TRACK TIE DOWN RAIL IN AFT BAGGAGE BIN CORRODED AT STA 787-847, RBL 30, JUST ABOVE S27R. THE CARGO TRACK TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040714002082004071400208NM 2004 7 14 SWAA041945 120040710A3350BCREF4146 LIGHT BOEING737 7372H4 138448CNM COCKPIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040715000052004071500005NM 2004 7 15 DLM88040630 120040706A2120 VENT DOUG MD88 MD88 3023688NM TAIL STUCK A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27917DL 49573 TAIL COMPT HIGH LIGHT. ABORTED T/O 115 - 120 KTS. FOUND LEFT TAIL COMPARTMENT EXHAUST VENT FLAPPER STUCK CLOSED. FREED SAME. 2L72 4F RTA6WE 20040715000182004071500018 2004 7 15 SWAA041938 420040706A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR WILL NOT TEST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29374SW 26582 DURING SPV, R2 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040715000262004071500026NM 2004 7 15 SWAA041954 120040711A253064769001 COFFEEMAKER BOEING737 7377H4 1384404NM AFT GALLEY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29724SW 27856 ELECTRICAL ODOR IN AFT GALLEY REPORTED. REMOVED AND REPLACED BOTH AFT COFFEEMAKERS PER MM. 2L72 4F RTA16WE 20040715000522004071500052EA 2004 7 15 SWIA200413514 120040622A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07906SW 7510 CARGO PIT FLOORBEAM ANGLE IS CRACKED FS 621.00 LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-52-11-213. FLOOR SUPPORT ANGLE AT FS 621.00 LBL 42.0 REPAIRED IAW CRJ REO 601R-53-61-117 REV. B. 2L72 4F RTA21EA 20040715000562004071500056NM 2004 7 15 DL757040635 120040707A5315141N2930115 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27663DN 24992 FUSELAGE FLOORBEAM AT STA 324 AND RBL 63 TO LBL 10 UPPER WEB AND CAP SUFFERED TOOLING DAMAGE AND OVERSIZED FASTENER HOLES. REPAIR IAW ERA 091387-14. 2L72 4F RTA2NM 20040715000572004071500057SO 2004 7 15 SWIA200413520 120040627A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN MALFUNCTIONED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07560SW 120334 SOME LIGHTS INOP ON FLOOR LEVEL EMERGENCY LIGHTS IN CABIN. REMOVED AND REPLACED 1ST WHITE EMERGENCY LIGHT AS NEEDED ON EMERGENCY STRIP. OPS CHECK GOOD. 2L72 4T RTA31SO 20040715000592004071500059NM 2004 7 15 DL757040639 120040709A2497 WIRE BOEING757 75726D 1384907NM CABIN SHORTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27900PC 28446 SPARKS OBSERVED BY FLIGHT ATTENDANT AND PAX OVER 2R DOOR, CAT PAX REPORTED 4 FT SPARKS FROM 2R DOOR AREA. OPENING UP CEILING PANELS FOUND AND REPAIRED WIRE W3662-003-08 AT STA 686 BY PERFORMING BUTT SPLICE PER BOEING STANDARD WIRING PRACTICE MANUAL. WIRE WAS FOUND CHAFING AGAINST STEEL BRAIDED POTABLE WATER LINE TO 2L LAV. 2L72 4F RTA2NM 20040715000602004071500060NM 2004 7 15 DLM90040640 120040709A4940 STARTER DOUG MD90 MD9030 3023690NM APU BURNED A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO27909DA13416 P1004 53389 P1004 FIVE MINUTES AFTER FAILED START ATTEMPT SMOKE COMING FROM APU AREA. SMALL FIRE AT APU STARTER EXTINGUISHED WITH DRY CHEM EXT. APU REPLACEMENT IN PROGRESS. REPLACED APU ASSY AND APU START RELAY. 2L72 4F RTA6WE 20040715000612004071500061NM 2004 7 15 DLM88040641 120040709A2120 ODOR DOUG MD88 MD88 3023688NM GALLEY DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27971DL 53214 ELECTRICAL ODOR REPORTED IN COCKPIT/CABIN DIDN'T DISPERSE BY SHUTTING OFF GALLEY POWER OR CABIN LIGHTS. ODOR DISSIPATED AFTER 10 MIN, ACFT DIVERTED TO IND. PERFORMED DUCT BURNOUT PROCEDURE AND INSPECTED/RAN AIRCRAFT SYSTEMS. UNABLE TO DUPLICATE. 2L72 4F RTA6WE 20040715000622004071500062NE 2004 7 15 DL76L040642 220040710A7200 ENGINE BOEING767 767332 1382001NM PWA 4090 PW4090 52119NE NR 1 FAILED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27175DN10297 24803 071503 T/O ROLL 70 KNTS FELT STALL AND LOST OIL PRESS. EXAMINED TAILPIPE FOUND METAL N1 WON`T TURN. REPLACED ENGINE. 2L72 4F4 FRTA1NM E46NE 20040715000632004071500063NM 2004 7 15 DL757040643 120040710A275018196917 TRANSMITTER BOEING757 757232 1384965NM LT WING T/E FLAPINTERMITTENT A DALAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO27606DL 22813 DECLARED EMERGENCY LANDING WITH FLAPS FULL UP, T/E FLAPS ASYMMETRY STATUS MSG AND ASSOCIATED LIGHT. FOUND ASYMMETRY TROUBLES INTERMITTANT. REPLACED FSEU WHICH FAULTED LT FLAP POS XMTR / WIRING. RAN WIRING FROM FSEU-1 TO LT FLAP POSITION XMTR, CHECKED GOOD. REPLACED LT FLAP POSITION XMTR PER AMM. ALL FLAP ANGLE VALUES WITHIN TOLERANCE. CYCLED FLAPS THROUGH FULL TRAVEL SEVERAL TIMES. ALL OPS NORMAL. AFCT RETURNED TO SERVICE. 2L72 4F RTA2NM 20040715000642004071500064SO 2004 7 15 SWIA200413521 120040611A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07223SW 120291 LEFT FORWARD FLOOR SEAT TRACK SMALL 3 HOLE PIECE IS CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD SEAT TRACK IAW 53-01-05. 2L72 4T4 TRTA31SO E20NE 20040715000652004071500065SO 2004 7 15 SWIA200413522 120040611A5410 STRUCTURE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07223SW 120291 LEFT HYDRAULIC BAY SHEET METAL CRACKED AT BULKHEAD. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED BULKHEAD IAW 120 SRM 51-10-02 PAGE 2, PAR 2B. 2L72 4T4 TRTA31SO E20NE 20040715000672004071500067SO 2004 7 15 SWIA200413524 120040506A5720 BRACKET EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT WING UPPER 2ND FROM LAST SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. SKIN SUPPORT REMOVED AND REPLACED IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2L72 4T4 TRTA31SO E20NE 20040715000682004071500068EA 2004 7 15 SWIA200413525 120040626A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AILERONS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07936SW 7726 AILERON TRIM SWITCH STICKS, WILL NOT ALLOW RIGHT TRIM INPUT. REMOVED AND REPLACED TRIM PANEL IAW CRJ AMM 27-12-00. OP CHECKS GOOD. P/N: 601R51226-23SW. 2L72 4F RTA21EA 20040715000712004071500071NM 2004 7 15 DL738040593 120040623A30300851HT1 PITOT TUBE BOEING737 737832 13844CFNM RIGHT INOPERATIVE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO273768 29630 RIGHT ELEVATOR PITOT HEAT INOP. REPLACED THE RIGHT ELEVATOR PITOT PROBE PER M/M 27-31-94-000-801. 2L72 4F RTA16WE 20040715000722004071500072NM 2004 7 15 DLM88040644 120040711A2560P4010021 BATTERY DOUG MD88 MD88 3023688NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27903DE 53380 MID CABIN FLIGHT ATTENDANT FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED LIGHT ASSY. 2L72 4F RTA6WE 20040715000732004071500073NM 2004 7 15 DL757040594 120040623A1430705072 BOLT BOEING757 757232 1384965NM BRAKE SHEARED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27611DL 22818 AFTER DEPARTURE RECEVED LT HYDRAULIC QTY MESSAGE, QTY INDICATED ZERO, LT ENGINE HYDRAULIC PRESSURE 60 PSI. ELECTRIC / HYDRAULIC USED ALT FLAPS ALT GEAR EXT O/W, LANDING LAX NO NOSE STEERING. COOLED BRAKE TEMP SHOWED ALL O,S. FOUND DUAL BRAKE METERING VALVE FAILURE. REPLACED SAME. 2L72 4F RTA2NM 20040715000742004071500074NM 2004 7 15 DL76G040595 120040623A2780 SWITCH BOEING767 767332 1382001NM NR 3 SLAT OUT OF RIG A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO271610D 30594 L/E ASSYM ON T/O AT 1000 AGL RETURNING TO LGW. FOUND SLAT ASSYM SWITCH 284 OUT OF ADJUSTMENT. RESHIMMED PROX SWITCH 284 ON NR 3 SLAT. 2L72 4F RTA1NM 20040715000762004071500076NM 2004 7 15 DL76L040597 120040624A335020121 POWER SUPPLY BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27183DN 27110 EMERGENCY SEAT LIGHTING ROWS 1-5 WILL NOT TEST. FOUND M90003 POWER SUPPLY AND BATTERY BAD. REPLACED BOTH, OPS CHECKS NORMAL. 2L72 4F RTA1NM 20040715000782004071500078SO 2004 7 15 SWIA200413555 120040703A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07190SW 120050 EMERGENCY LIGHT ON OVERHEAD BIN ROW 9 DOESN'T ILLUMINATE. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040715000802004071500080SO 2004 7 15 SWIA200413557 120040708A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07284YV8289 8289 FLOOR LEVEL TRACK LIGHTS INOPERATIVE AT GALLEY. REPLACED MIDDLE POSITION EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040715000812004071500081EA 2004 7 15 SWIA200413558 120040706A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07979SW 7954 LEFT EMERGENCY DOOR CAUTION EICAS MESSAGE AT 31,000 FT. ADJUSTED TARGET ON LEFT DOOR PROXIMITY SENSOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040715000822004071500082EA 2004 7 15 SWIA200413559 120040711A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07435SW DURING CRUISE AT 33,000 RIGHT SIDE FRONT WINDSHIELD CRACKED. REPLACED RT WINDSHIELD PER MM 56-11-01. OPERATIONAL CHECK GOOD. P/N OFF: 601R33033-14, S/N OFF: 01123H7078. 2L72 4F RTA21EA 20040715000832004071500083 2004 7 15 SWIA200413560 420040711A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING WILL NOT TEST A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07561SW 120335 STALL WARNING SYSTEM WILL NOT TEST. REPLACED NR 1 AND NR 2 STALL WARNING COMPUTERS. OPERATIONAL CHECK GOOD. P/N: C-81806-1, S/N OFF: 724. 2L72 4T RTA31SO 20040715000852004071500085NM 2004 7 15 DLM88040612 120040630A3510359001020 CONTROL BOX DOUG MD88 MD88 3023688NM OXY SYSTEM LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27987DL 53338 CREW LOSS O2 IN FLIGHT. FOUND F/O MASK STUCK IN TEST. REPLACED F/O MASK BOX. 2L72 4F RTA6WE 20040715000862004071500086NM 2004 7 15 DL73S040613 120040630A1420MS24266R16T2 CONNECTOR BOEING737 737247 138448DNM FLAP TRANSMITTERWORN A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27243WA 23517 DURING TAKEOFF FLAPS LOCKED UP BETWEEN 1 AND 2 DEG, THE LEFT FLAP STAYED AT 1.5 AND RIGHT AT 2.0. CHECK OF SYSTEM SHOWED LEFT FLAP SYSTEM FLUCUATING. REPLACED LEFT FLAP TRANSMITTER CONNECTOR D275, OP CHECKS NORMAL. 2L72 4F A16WE 20040715000872004071500087NM 2004 7 15 DL767040614 120040701A5753113T122625 STRUCTURE BOEING767 767232 1385132NM WING FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27114DL 22226 WHILE ACCOMPLISHING THE I/B TRAILING EDGE MAIN FLAP ATTACH BOLT REPLACEMENT PER EA 01-085672-12AD, CORROSION WAS FOUND IN THE BORES OF THE FWD TWO AND AFT ATTACH FOUR HOLES OF THE 9-10 BEAM AND THE ASSOCIATED MATING HOLES ON THE FLAP AND THE FOUR HOLES COMMON TO THE I/B ATTACH SUPPORT BEAM AND THE ASSOCIATED HOLES IN THE FLAP COLLAR FITTING. THIS ERA PROVIDES REPAIRS FOR THE SUBJECT HOLES. 2L72 4F RTA1NM 20040715000902004071500090EA 2004 7 15 SWIA200413528 120040701A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07915SW 7615 DURING LEVEL FLIGHT AP PITCH TRIM MESSAGE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040715000922004071500092EA 2004 7 15 SWIA200413530 120040625A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07587SW1091010910 7062 FLAPS HALF-SPEED STATUS MESSAGE ON INTERMITTENTLY. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040715000952004071500095NM 2004 7 15 CALA0400545 120040626A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FORWARD ENTRY LEFT I/B SEAT TRACK CORRODED AT STA 360-380. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040715000962004071500096NM 2004 7 15 CALA0400546 120040626A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FORWARD ENRTY RIGHT O/B SEAT TRACK CORRODED BETWEEN STA 344 AND 360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040715000972004071500097NM 2004 7 15 CALA0400547 120040626A53116546539 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 616, S17L. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158. 2L72 4F RTA16WE 20040715000992004071500099NM 2004 7 15 CALA0400549 120040626A53156545812 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 20. THE CORRODED AREA OF FLOORBEAM WAS REMOVED AND A NEW UPPER CHORD AND REPAIR SPLICE WERE INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20040715001002004071500100SO 2004 7 15 SWIA200413480 120040506A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 FRAME 15 IN BELLY CRACKED FRAME AT AFT AIR STAIR ACTUATOR. DISCOVERED DURING C-CHECK INSPECTION. FRAME REPAIRED IAW EMB 120 SRM 53-00-04 PG 201-204. 2L72 4T RTA31SO 20040715001022004071500102SO 2004 7 15 SWIA200413482 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02. 2L72 4T RTA31SO 20040715001042004071500104SO 2004 7 15 SWIA200413484 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW SRM 57-20-07, 51-40-05, 52-25-00, 51-40-02. 2L72 4T RTA31SO 20040715001052004071500105SO 2004 7 15 SWIA200413485 120040506A5741 STRUCTURE EMB 120 EMB120ER 3260203SO WING TO BODY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202. 2L72 4T RTA31SO 20040715001062004071500106NM 2004 7 15 151AW0016 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 SKIN REPAIR FORWARD OF WATER SERVICE DOOR AT STR 24 LT BS 927 IS TOO CLOSE TO SKIN LAP. REPLACED REPAIR PER EA 53-135. 2L72 4F RTA16WE 20040715001072004071500107NM 2004 7 15 CALA0400550 120040626A53206545834256 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312-328, RBL 10.8. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040715001112004071500111NM 2004 7 15 SWAA041958 120040711A53116547957 WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME UPPER CLOSE OUT WEB LOWER AREA, CORRODED. REMOVED AND REPLACED DOOR CUTOUT FRAME WEB PER SRM. 2L72 4F RTA16WE 20040715001142004071500114NM 2004 7 15 CALA0400553 120040627A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 907-927. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040716000012004071600001SO 2004 7 16 SWIA200413486 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2L72 4T RTA31SO 20040716000042004071600004SO 2004 7 16 SWIA200413562 120040708A2750 CONTROL UNIT EMB 120 EMB120ER 3260203SO HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07583SW 120351 INFLIGHT AND ON APPROACH RECEIVED FLAP CONTROL FAULT. REPLACED HSTCU AS REQUIRED PER CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040716000052004071600005NM 2004 7 16 QXEA200400458 120040621A27303994001011 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 300 PITCH INOPERATIVE A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09401QX3401 4031 SEA - ON FLIGHT NUMBER 2317, PITCH TRIM CAUTION LIGHT ILLUMINATED ON SHORT FINAL. NO OTHER CAUTION LIGHTS ILLUMINATED. PITCH TRIM INDICATED FULL NOSE UP. RAN CHECKLIST AFTER LANDING. PITCH TRIM DID NOT MOVE. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000072004071600007NM 2004 7 16 QXEA200400420 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - RIGHT HAND INBOARD SEAT RAIL NR 8 TOP FLANGE HAS SMALL SCRATCH/CORROSION AT APPROXIMATELY STATION X487.0. REPAIRED IAW DHC8 200 SRM 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20040716000082004071600008NM 2004 7 16 QXEA200400413 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 11 HAS GOUGE AND CORROSION IN TOP AND CENTER OF TRACK AT STATION X438 TO X445. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20040716000102004071600010NM 2004 7 16 QXEA200400426 120040612A5410 FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 PDX - FORWARD LEFT CLEAT FOR NR 1 ENGINE SPLINE COWL CRACKED. REPAIRED IAE RD 8/4-71-032. 2H72 4T RTA13NM 20040716000112004071600011NM 2004 7 16 QXEA200400437 120040611A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 6 HAS A GOUGE IN CENTER OF TRACK AT STATION X547. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20040716000122004071600012NM 2004 7 16 QXEA200400419 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - TOP FLANGE HAS LITE PITTING ON RIGHT HAND INBOARD SEAT RAIL NR 8 AT APPROXIMATELY STATION X515.0. REPAIRED IAW SRM 51-20-36 AND RD 8-53-1339. 2H72 4T RTA13NM 20040716000152004071600015NM 2004 7 16 QXEA200400439 120040611A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - LEFT HAND INBOARD SEAT RAIL NR 6 TOP FLANGE SMALL GOUGE AT APPROXIMATELY STATION X531.0. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20040716000162004071600016NM 2004 7 16 QXEA200400441 120040610A5320 CLIP DHAV DHC8 DHC8202 2809007NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - CLIP CRACKED AT FRAME 4 STRINGER 4 LEFT. REPAIRED IAW RD 8-55-199. 2H72 4T RTA13NM 20040716000172004071600017NM 2004 7 16 QXEA200400442 120040610A5320 CLIP DHAV DHC8 DHC8202 2809007NM ZONE 300 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - CLIP CRACKED AT FRAME 4 STRINGER 4 RIGHT. REPAIRED IAW RD 8-55-199. 2H72 4T RTA13NM 20040716000182004071600018SO 2004 7 16 SWIA200413487 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02. 2L72 4T RTA31SO 20040716000222004071600022SO 2004 7 16 SWIA200413491 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET AT RIB 20 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, 51-40-02. 2L72 4T RTA31SO 20040716000232004071600023SO 2004 7 16 SWIA200413492 120040506A5712 RIB EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING FORWARD RIB 20 CRACKED AT TOP TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 20 REPLACED IAW 51-25-00, 51-40-05, 51-40-02, 51-22-00. 2L72 4T RTA31SO 20040716000262004071600026SO 2004 7 16 SWIA200413495 120040506A5712 RIB EMB 120 EMB120ER 3260203SO RT WING WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING LEADING EDGE INBOARD OF NACELLE, OUTBOARD ATTACH POINT RIB WORN THROUGH. DISCOVERED DURING C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1. 2L72 4T RTA31SO 20040716000302004071600030NM 2004 7 16 QXEA200400511 120040705A2730 CONTROL CIRCUIT DHAV DHC8 DHC8202 2809007NM ZONE 100 OUT OF RIG A QXEAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM09352PH15965 494 SEA - FLIGHT 2089 - ELEVATOR CONTROL IS UNUSUALLY HEAVY AND JERKY, ESPECIALLY NOTICEABLE DURING FLARE. MAINTENANCE INSPECTED THE AIRCRAFT AND RIGGED THE PILOTS AND COPILOTS ELEVATOR CONTROL CABLE CIRCUITS IAW AMM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000342004071600034EA 2004 7 16 SWIA200413534 120040703A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07924SW6965 6965 7681 STAB TRIM CH 1 INOP 1500 FT AFTER TAKEOFF. REMOVED AND REPLACED HSTA AND MCU PER AMM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 109. 2L72 4F RTA21EA 20040716000352004071600035 2004 7 16 SWIA200413535 420040704A22156225734002 SERVO EMB 120 EMB120ER 3260203SO RT RUDDER PEDAL WORN A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07288SW9753 9753 120316 RIGHT RUDDER PEDAL RUBBING AND GRINDING AND CATCHING ON SOMETHING DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO AND SERVO CLUTCH IAW MM 22-10-05 AND 27-00-03. OPERATIONAL CHECK GOOD. P/N 622-5734-004, S/N OFF 7268. 2L72 4T RTA31SO 20040716000372004071600037EA 2004 7 16 SWIA200413537 120040702A5240 HANDLE CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR JAMMED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07464SW 7827 SERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE. REMOVED AND REPLACED SERVICE DOOR OUTER HANDLE ASSY IAW CRJ SRM 51-42-21 AND 51-10-06. 2L72 4F RTA21EA 20040716000392004071600039EA 2004 7 16 SWIA200413539 120040701A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07920SW4746 4746 7660 AUTO-PILOT PITCH TRIM CAUTION MESSAGE WHEN FLAPS EXTENDED TO 30 DEGREES. REMOVED AND REPLACED MOTOR CONTROL UNIT AND HSTA IAW CRJ MM 27-42-05 AND 27-42-01. OPERATIONAL CHECK GOOD IAW CRJ MM 27-40-00. P/N (HSTA): 8396-3, S/N OFF: 908. 2L72 4F RTA21EA 20040716000412004071600041NM 2004 7 16 QXEA200400478 120040628A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM ZONE 100 STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH13691 520 PDX - FUSELAGE PANEL 122AR HAS 2 STRIPPED OUT NUT PLATES. MAINTENANCE REPLACED THE NUT PLATES IAW THE DHC-8 SRM. 2H72 4T RTA13NM 20040716000422004071600042NM 2004 7 16 QXEA200400480 120040629A2810AV24B1319D3 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007NM ZONE 400 DEFUEL LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09348PH16245149 484 PDX - FUEL DRIPPING FROM RIGHT NACELLE, BETWEEN FUEL DOOR AND GEAR DOOR. REMOVED AND REPLACED REFUEL/DEFUEL SHUTOFF VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000462004071600046EA 2004 7 16 SWIA200413541 120040622A27507455001 LEVER CNDAIRCL600 CL6002B19 1900309EA FLAP CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07948SW 7789 FLAP SELECTOR IS HARD TO SELECT FROM 20 TO 30. REMOVED AND REPLACED FLAP CONTROL HANDLE IAW CRJ MM 27-51-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040716000482004071600048NE 2004 7 16 DL76L040572 220040614A7230PW40603 BLADE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27180DN41377 25985 724166 DURING REPLACEMENT OF NR 1 BEARING CARBON SEAL, FOUND DAMAGE TO 5TH STAGE HPC BLADES. FAILED BOROSCOPE INSPECTION. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20040716000492004071600049NM 2004 7 16 DLM88040573 120040616A3260329001000 PSEU DOUG MD88 MD88 3023688NM MLG FAILED A DALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO27997DL 53364 ON APPROACH HAD LT MLG UNSAFE INDICATION. A/C LANDED WITH GEAR DOORS DOWN DUE TO ALT GEAR EXTENSION. A/C WAS FERRIED TO BOS FOR GEAR MTC. IN BOS CHECKED OUT ALL 3 LT GEAR PROX SWITCHES WITH ELEC TEST KIT. ALL CHECKS OK. SHOOK DOWN WIRING HARNESS FOR ALL 3 PROX SWITCH CHECKS. JACKED AND CYCLED GEAR. ALL CHECKS OK. REPLACED PSEU PER MM. 2L72 4F RTA6WE 20040716000512004071600051NM 2004 7 16 DL76S040576 120040618A3244BLADE TIRE BOEING767 767332 1382001NM RT MLG DAMAGED A DALAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 SO27127DL 24077 FOUND ON ARRIVAL NR 3 MAIN TIRE WITHOUT TREAD. PERFORMED TIRE TREAD CONDITIONAL INSPECTION AND REPLACED TIRE PER AMM. 2L72 4F RTA1NM 20040716000522004071600052NM 2004 7 16 UPS04542614 120040626A2780 BYPASS VALVE BOEING757 75724APF 1384969NM SLATS FAILED A IPXAO OTHER J WARNING INDICATION LDLANDING 1 SO01460UP 25481 AFTER SELECTING FLAPS 1, FLAP POSITION INDICATOR STOPPED BETWEEN 0 AND 1, LEADING EDGE SLAT DISAGREE MSG APPEARED. COMPLETED APPROPRIATE CHECKLIST AND LANDED FLAPS 20 W/O FURTHER PROBLEM. REMOVED AND REPLACED L/E SLAT BY-PASS VALVE, OPS CHECKS GOOD PER MM 27-81-09-4. LEAK CHECK GOOD FSEU-3 MSG, SLAT PDU XTR, FAULT. REMOVED AND REPLACED PDU XTR (SLATS) CHECKS GOOD PER MM 27-81-08-2. 2L72 4F RTA2NM 20040716000542004071600054NM 2004 7 16 DL73S040579 120040617A1430BACB BOLT BOEING737 737232 1384475NM ELEVATOR DAMAGED A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO27324DL 23096 YOKE FAILED TO RETURN TO NEUTRAL AFTER DEFLECTION. REPLACED BOLT IN ELEVATOR FEEL AND CENTERING OUTPUT ROD. 2L72 4F RTA16WE 20040716000552004071600055NM 2004 7 16 DL76S040581 120040620A3233 ROD BOEING767 767332 1382001NM LT MLG ACTUATOR BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27120DL 00049 23279 ON TAKEOFF HAD GEAR DISAGREE LIGHT ON EICAS WITH WARNING, GEAR HANDLE UP. LEFT MAIN GEAR INDICATED DOWN WITH DOORS LIGHT ON AND GEAR LIGHT ON. PUT GEAR DOWN AND ALL GEAR INDICATED SAFE. RETURNED TO ATLANTA. FOUND SIDE BRACE ACTUATOR RETRACT ROD BROKEN. REPLACED SIDE BRACE ACTUATOR PER M/M. JACKED A/C AND PERFORMED GEAR SWING FOR PRECAUTION. GEAR SWING CHECKS GOOD. 2L72 4F RTA1NM 20040716000592004071600059NM 2004 7 16 DL73S040585 120040618A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 4R SKIN LAP JOINT AT FS 695. THE CRACK WAS REMOVED WITH A 4.25 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND DOCUMENTED PER ER/A 090771-14AD. 2L72 4F RTA16WE 20040716000622004071600062NM 2004 7 16 DL73S040588 120040618A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 10R SKIN LAP JOINT AT FS 439. THE CRACK WAS REMOVED WITH A 4.25 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND DOCUMENTED PER ER/A 090887-14AD. 2L72 4F RTA16WE 20040716000632004071600063 2004 7 16 249TR0030 420040616A2297 WIRE BOEING737 7372K5 138448XNM AUTOPILOT DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 BOTH TOGA SWITCHES INOP AND A-SYSTEM AUTO PILOT INOP. PLACED BOTH SYSTEMS ON MEL. REPAIRED GROUND WIRE ON T215. PERFORMED LAND VERIFY TEST AND OPERATIONAL TEST SATISFACTORY PER MM 22-11-01. CLEARED MEL. 2L72 4F RTA16WE 20040716000642004071600064NM 2004 7 16 QXEA200400472 120040624A5410 STIFFENER BOMBDRDHC8 DHC8401 1390041NM NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09413QX 4060 PDX - CRACK IN WEB STIFFENER FOR AFT CONE. STIFFENER IS AT 12 O'CLOCK POSITION ON CONE NR 1 LOWER ENGINE COWL. COMPLETED INSTALLATION OF FASTENER AS PER Q400 SRM 51-42-03. 2H72 4T RTA13NM 20040716000652004071600065NM 2004 7 16 QXEA200400473 120040624A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09353PH15747 496 PSC - EMERGENCY LIGHTS FLOOR STRIP NR 2 HAS 2 RED LIGHTS INOP. MAINTENANCE FOUND NO VOLTAGE AT 3352-J4/P4 PIN NR 2. REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000662004071600066NM 2004 7 16 DL764040600 120040625A2432BA3501 BATTERY BOEING767 767432ER 1385134NM E/E BAY DISCHARGED A DALAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SO27835MH 29708 DURING TRANSIT CHECK PAT WENT OFFLINE - ON P6 PANEL APU FIELD GEN LIGHT ILLUM NUMEROUS COCKPIT LIGHTS WERE OUT. CORR T/S TO MAIN BATTERY, BATTERY AT 20VDC WITH NO LOAD ON IT. REMOVED AND REPLACED BATTERY PER MM, EVERYTHING RESET AND CHECKS GOOD. 2L72 4F RTA1NM 20040716000682004071600068NM 2004 7 16 DLM88040602 120040624A5330593600419 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27936DL 49723 FUSELAGE SKIN FOUND BULGED/CORRODED AT STA 625 BETWEEN LONGERONS 29R AND 30. DAMAGE CUT OUT AND EXTERNAL DOUBLER/TRIPLER INSTALLED PER ERA 091432-14 REV A. 2L72 4F RTA6WE 20040716000692004071600069NM 2004 7 16 DL767040603 120040623A5320146T80482 SILL BOEING767 767232 1385132NM FS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27107DL 22219 ER/A 091340-14, C2 DOOR LOWER SILL WAS FOUND WITH CORROSION LOCATED ON THE INNER CHORD UPPER FLANGE AT FS 1270-1279. ADDITIONAL CORROSION WAS FOUND ON THE WEB AT FS 1279. 2L72 4F RTA1NM 20040716000702004071600070NM 2004 7 16 DL733040604 120040626A2530 ODOR BOEING737 737347 1384647NM GALLEY DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27302WA 23182 FLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL PRESENT. APPLIANCES AND LIGHTS ALL CHECK NORMAL. OK FOR SERVICE. 2L72 4F RTA16WE 20040716000752004071600075WP 2004 7 16 CALA0400561 120040702A57309936822506 PANEL DOUG DC9 DC981 3022081WP RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714871 48022 INSPECTION FOUND A 6 INCH CRACK IN RIGHT WING PANEL AT WING STA XFS 70-196. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2L72 4F A6WE 20040714000232004071400023NM 2004 7 14 QXEA200400456 120040619A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM BAGGAGE COMP WILL NOT TEST A QXEAO OTHER L NO TEST NRNOT REPORTED 1 NM09364PH2796 2796 524 SEA - FLIGHT 2283 - BAGGAGE SMOKE DETECTOR NUMBER 1 WILL NOT TEST. MAINTENANCE INSPECTED THE DETECTOR AND REPLACED SAME. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040714000262004071400026EA 2004 7 14 QXEA200400509 120040710A3620 DUCT CNDAIRCL600 CL6002C10 1390015EA BLEED AIR LEAKING A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09600QX 10005 BOI FLIGHT 2522 RETURN TO FIELD FOR RIGHT BLEED DUCT WARNING LIGHT - LIGHT EXTINGUISHED AT COMPLETION OF EMERGENCY CHECKLIST WHEN AIRCRAFT WAS DEPRESSURIZED. MAINTENANCE REMOVED BLEED AIR CROSSOVER DUCT IAW RT 36-0078. NO ABNORMAL INDICATIONS OR LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040714000282004071400028EA 2004 7 14 QXEA200400497 120040702A2741AL00102 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA ZONE 300 MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09611QX5602 5602 10041 DEN - FLIGHT 4011- ABORTED TAKEOFF AT 115-120 KTS, MASTER WARNING, RUDDER MISCONFIGURATION. WARNING WENT AWAY WHILE CLEARING RUNWAY. RUDDER AND AILERON INDICATED GREEN. REMOVED AND REPLACED RUDDER TRIM ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040714000352004071400035NM 2004 7 14 UPS04242675 120040622A5754 SKIN BOEING727 72725C 138400HNM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C, NR 6 L/E SLAT O/B UPSTOP HAS CRACK ON SURROUNDING SKIN. REPAIR CARRIED OUT IAW MM 27-81-11 & SRM 57-30-4 FIG 4. 2L73 4F A3WE 20040714000382004071400038NM 2004 7 14 UPS04242678 120040623A5320 FLOOR SUPPORT BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, AFT CARGO FLOOR SUPPORT RAIL AT BS 1035 RBL 4 APPROX, CORRODED. SECTION OF FLOOR SUPPORT RAIL REPLACED IAW SRM 53-10-5 & DRAWING 65-19 388. 2L73 4F A3WE 20040714000392004071400039NM 2004 7 14 UPS04242680 120040616A5512 SKIN BOEING727 72725C 138400HNM DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C PULLED RIVETS & BULGE ON RT STAB LWR SKIN APPROX 4 INCHES FROM REAR SPAR AND AT STAB STA 66 APPROX. REPAIR CARRIED OUT IAW SRM 51-30-02, 55-10-3 FIG 3, 51-10-1 & MM 51-20 -01 & 27-30-51. 2L73 4F A3WE 20040714000422004071400042NM 2004 7 14 UPS04242683 120040618A5754 STRUCTURE BOEING727 72725C 138400HNM NR 3 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C, NR 3 LEADING EDGE FLAP, O/B BONDING WIRE ATTACH SCREW HOLE IS CRACKED. REPAIR CARRIED OUT IAW AAAE EO 2004-061-002, UPS ENGINEERING FILE NR 727-57-20113. 2L73 4F A3WE 20040714000482004071400048NM 2004 7 14 QXEA200400464 120040623A5753 FLAP TRACK DHAV DHC8 DHC8202 2809007NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09351PH 490 PDX - NR 4 FLAP TRACK HAS PITTING CORROSION ON LOWER OUTBOARD TRACK UPPER SURFACE. REPAIRED IAW RD 8-57-988. 2H72 4T RTA13NM 20040714000592004071400059NM 2004 7 14 QXEA200400443 120040610A5320 CAMLOCK DHAV DHC8 DHC8202 2809007NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - PANEL 261DT HAS MULTIPLE CAMLOCKS CORRODED. REPAIRED IAW RD 53-3366. 2H72 4T RTA13NM 20040714000732004071400073EU 2004 7 14 UPS04142605 120040618A5320A53978102 INTERCOSTAL AIRBUS300 A300B4622R 3930312EU FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01157UP 0005 43R INTERCOSTAL DAMAGED AT FRAME 57-58 RT. FABRICATED NEW INTERCOSTAL & INSTALLED IAW A300 SRM 51-26-00 AND PER SAMPLE IAW UPS GMM 5-9-2. 2L72 4F RTA35EU 20040714000772004071400077NM 2004 7 14 UPS04442609 120040623A2910 LINE BOEING747 747200 1384847NM NR 3 HYD SYSTEM CHAFED A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO01522UP 21936 NR 3 HYD SYS LOST FLUID TO 0.5 GAL EDP ZERO WITH LOW PRESSURE LIGHT. ADP PRESSURE NORMAL. CHECKLIST COMPLETE FOR SYSTEM LEAK. FOUND PRESSURE LINE CHAFED ON PNEU DUCT IN UPPER SECTION OF NR 3 PYLON (MARKED WITH RED TAPE) BB 09326 INSTALLED NEW LINE, LEAK CHECK OK. 2L74 4F RTA20WE 20040714000862004071400086WP 2004 7 14 UPS04842630 120040612A53403755847U2 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2, C-PIT FWD DOOR JAMB FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-21 AND 51-3-2. 2L74 4F RT4A25 20040714000872004071400087WP 2004 7 14 UPS04842631 120040615A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, FUSELAGE SKIN CRACKED AT RIGHT AFT HEAT EXCHANGER CUTOUT STA -12, L27R. REPAIRED PER UPS EO 5330-4732D. 2L74 4F RT4A25 20040714000892004071400089WP 2004 7 14 UPS04842633 120040615A53204772397U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, LONG 17 AND END FITTING CRACKED AT STA 1766 LT. REMOVED L17L AND END FITTING AT STA 1766-1790 (APPROX) REF SRM 51-1-21 & 51-1-20D. FABRICATED L17 FROM S1616757 EXTRUSION REF DWG 5649327. INSTALLED REPLACEMENT L17 AND NEW 4772397U1 FITTING REF SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20040714000932004071400093WP 2004 7 14 UPS04842610 120040625A2510 SEAT DOUG DC8 DC873F 302199FWP CAPTAIN'S MALFUNCTIONED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01802UP 46100 INSPECTION TYPE:N/A CAPTAINS SEAT WILL NOT LOCK IN PLACE, IT SLID OUT OF POSITION AT BEGINNING OF T/O ROLL AND SETTING THE BRAKES AT ENGINE SHUTDOWN. SEAT WAS IN FALSE LOCK POSITION. REPLACED CAPTAIN'S SEAT ASSY IAW 25-11-01-2. OPS CHECK GOOD. 2L74 4F RT4A25 20040714001102004071400110WP 2004 7 14 CALA0400538 120040618A53209936534139 FLOOR SUPPORT DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714871 48022 INSPECTION FOUND FLOOR SUPPORT TRACK CORRODED AT STA 160-200, RBL 7. THE FLOOR SUPPORT TRACK WAS REPLACED IAW SRM 51-30-3. 2L72 4F A6WE 20040714001132004071400113WP 2004 7 14 CALA0400541 120040621A3350BR9279106 LIGHT DOUG DC9 DC982 3022082WP EMERGENCY EXIT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2716806 49260 INSPECTION FOUND EMERGENCY LIGHTS BY LEFT FORWARD EMERGENCY OVERWING EXIT AT FLOOR LEVEL INOPERATIVE. THE LIGHT FIXTURE WAS REMOVED AND REPLACED. 2L72 4F A6WE 20040714001162004071400116NM 2004 7 14 151AW0001 120040702A5320 SCUFF PLATE BOEING737 7373G7 1384595NM L1 DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FWD CORNER SCUFF PLATE AND AFT CORNER SCUFF PLATE OF L1 DOOR HAVE SMALL CRACKS. WELDED CRACKS PER BAC 5975. 2L72 4F RTA16WE 20040714001322004071400132EA 2004 7 14 MASA200400281 120040522A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW0775992 7401 CAPTAIN REPORTED ONE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AND THE LEFT EMERGENCY EXIT SIGN AT ROW 8 INOP. MX FOUND EXTERIOR EMERGENCY LIGHTS OUT AS WELL AND REPLACED AN EMERGENCY BATTERY PACK WITH NO EFFECT. STILL TROUBLESHOOTING. MX REPLACED INVERTER, OPS CHECK GOOD. 2L72 4F RTA21EA 20040714001422004071400142SO 2004 7 14 MASA200400331 120040613A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07851MJ5610 145572 FWD FLOOR PROX LIGHTS INOP. MX REPLACED BATTERY PACK. 2L72 4T RTT00011AT 20040714001632004071400163NM 2004 7 14 DLM88040623 120040703A7711779001001 TRANSMITTER DOUG MD88 MD88 3023688NM NR 1 ENGINE FAILED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27992DL 53344 UPON T/O LEFT EPR HUNG AT 1.6 WITH RAPIDLY RISING EGT, ABORTED AT 30 KNOTS. REPLACED EPR TRANSMITTER. 2L72 4F RTA6WE 20040714001732004071400173NM 2004 7 14 SWAA041960 120040712A3350311500 LENS BOEING737 737317 138447PNM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29661SW 23173 BULL NOSE EMERGENCY EXIT LENS AT ROW 6 ABC, MISSING. INSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040714001742004071400174NM 2004 7 14 SWAA041961 120040712A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 907, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040714001822004071400182NM 2004 7 14 250TR0034 120040625A33506013211 BATTERY PACK BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 EMERGENCY EXIT LIGHTS ON RIGHT EXTERIOR BELOW HATCH AND AFT OF WING INOP. REPLACED BATTERY PACK AND OPS CHECKED OK PER MM 33-51-81. 2L72 4F RTA16WE 20040714001952004071400195WP 2004 7 14 UPS04842622 120040615A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C, SEAT TRACK GOUGED AT FS 860 45 RBL. BLEND GOUGE IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. LOCATED & DRILLED DC8-53B-007-006 CHANNEL & DC8 53B-007-002 PLUG. OK TO INSTALL, REMOVED DAMAGED IAW DC8 SRM 53-2-3, INSTALLED PLUG & U-CHANNEL IAW DC8 SRM 51-3-0 AND 51-3-1. 2L74 4F RT4A25 20040714002002004071400200 2004 7 14 UPS04M42627 420040630A2565 SLIDE DOUG MD11 MD11F 3023600NM ENTRY DOOR WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01272UP 48571 LEFT CREW ENTRY DOOR SLIDE LIGHT WILL NOT TEST. DEFERRED PER MEL 25-61-2 M283588. INSTALLED CORRECT P/N BULBS IN REMOTE TEST SW PER WDM 25-61-01. OPS CHECKS GOOD. THIS CLEARS M283588. 2L73 4F RTA22WE 20040714002022004071400202EA 2004 7 14 QXEA200400445 120040616A2130GG670980023 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 FAULTY A QXEABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09604QX4968 4968 10019 DEN - FLIGHT 4104 - THE FLIGHT RETURNED TO FIELD WHEN DURING THE CLIMB THRU FL230, THE CABIN ALTITUDE CAUTION LIGHT CHANGED TO A CABIN PRESSURE WARNING LIGHT. THE CREW PERFORMED AN EMERGENCY DESCENT. THE FLIGHT CREW NOTED NO CONTROL OF CABIN PRESSURE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT PACK FLOW CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040714002102004071400210NM 2004 7 14 SWAA041947 120040710A3350OL3071BPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 23 DEF, INOP. RELAMPED BULL NOSE LIGHT PER MM. 2L72 4F RTA16WE 20040714002112004071400211NM 2004 7 14 SWAA041948 120040710A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 964, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040715000042004071500004NE 2004 7 15 DL757040629 220040705A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 FAILED A DALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27611DL39508 22818 716568 HEARD POP ON TAKEOFF, 30 KNOTS, VEERED LEFT. ABORTED TAKEOFF. PILOT IN ANOTHER PLANE SAW FLAMES SHOOT OUT BACK OF LEFT ENGINE. T/S PER FIM. BORO 6TH AND 16TH STAGE COMPRESSOR. FOUND SEVERAL BLADES DAMAGED. ALSO FOUND METAL IN TAILPIPE. ENGINE CHANGE IN PROGRESS. 2L72 4F4 FRTA2NM E17NE 20040715000132004071500013SO 2004 7 15 MASA200400295 120040526A783083990168 SWITCH EMB EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07830MJ TR0382 145259 ABORTED TAKEOFF, RETURNED TO GATE WITH A E1 T/R DISAGREE MESSAGE. CONTRACT MX DEFERRED T/R PER MEL 78-34-00 AND CONTINUED OPS. MX REPLACED LOWER STOW/TRANSIT SWITCH. 2L72 4T RTT00011AT 20040715000242004071500024NM 2004 7 15 SWAA041952 120040710A3350101114 LAMP BOEING737 7373Q8 1384670NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED A2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040715000252004071500025NM 2004 7 15 SWAA041953 120040710A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29714CB 27848 DURING SCHEDULED C1 CHECK, ALL OVERHEAD EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040715000312004071500031NM 2004 7 15 SWAA041970 120040713A3350100031 SIGN BOEING737 7377H4 1384404NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29797MX 27890 AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN, MISSING. REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20040715000442004071500044 2004 7 15 SWAA041983 420040713A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29777QC 30592 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040715000472004071500047NM 2004 7 15 SWAA041986 120040713A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 867, STRINGER 23L, BS 727B + 10, STRINGER 23L, BS 777, STRINGER 23L, CRACKED. REPAIRED SKIN SECTIONS PER EA. 2L72 4F A16WE 20040715000582004071500058NM 2004 7 15 DL767040637 120040707A21203209954 VALVE BOEING767 767232 1385132NM E/E BAY INOPERATIVE A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27103DA 22215 ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REPLACED FWD EQUIPMENT COOLING OVERBOARD EXHAUST VALVE. 2L72 4F RTA1NM 20040715000702004071500070EA 2004 7 15 SWIA200413527 120040630A5610 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07701SK 10133 FIRST OFFICER'S WINDSHIELD CRACKED INFLIGHT. REPLACED FIRST OFFICER'S WINDSHIELD IAW 56-11-01 PER RII 56-202. LEAK CHECK GOOD. 2L72 4F RTA21EA 20040715000752004071500075NM 2004 7 15 DLM88040596 120040624A3240329001469 BRAKE DOUG MD88 MD88 3023688NM NR 4 FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27995DL 53362 NR 4 BRAKE SEIZED CAUSING NR 4 TIRE TO WEAR THROUGH AND DEFLATE. REPLACED WHEELS AND BRAKE ASSY. 2L72 4F RTA6WE 20040715000792004071500079SO 2004 7 15 SWIA200413556 120040702A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07284YV8795 8795 120284 SEVERAL EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040715000842004071500084EA 2004 7 15 SWIA200413561 120040706A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07935SW STAB TRIM NR 1 CAME OFF ON DESCENT AND ON LEVEL OFF. REPLACED HSTCU AS REQUIRED PER CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040715000912004071500091SO 2004 7 15 SWIA200413529 120040629A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAP MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07167313288 1397 120190 ON TAKEOFF ROLL EXPERIENCED FLAP CONTROL FAULT ON NACELLE FLAPS. REPLACED FLAPS CONTROL ELECTRICAL UNIT. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040715001012004071500101SO 2004 7 15 SWIA200413481 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2L72 4T RTA31SO 20040716000092004071600009NM 2004 7 16 QXEA200400423 120040609A5720 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - LEADING EDGE ATTACH BRACKET CRACKED IN TWO PLACES ON LEFT HAND WING X384.5 YS137. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20040716000212004071600021SO 2004 7 16 SWIA200413490 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2L72 4T RTA31SO 20040716000252004071600025SO 2004 7 16 SWIA200413494 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING UPPER 4TH FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-40, 51-40-05, AND 51-40-02. 2L72 4T RTA31SO 20040716000332004071600033SO 2004 7 16 SWIA200413533 120040703A275012064207615 LEVER EMB 120 EMB120ER 3260203SO FLAP SELECTOR MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07583SW5394 5394 120351 FLAP CONTROL FAULT DURING FLIGHT. REPLACED FLAP CONTROL HANDLE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040716000382004071600038SO 2004 7 16 SWIA200413538 120040630A2731 SWITCH EMB 120 EMB120ER 3260203SO STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07213SW 120277 WHEN AUTOPILOT IS TRANSFERRED TO FIRST OFFICER'S SIDE, TRIM FAIL ON MAP AND AUTOPILOT CONTROL PANEL. REPLACED FIRST OFFICER'S TRIM SWITCH IAW MM 22-10-10. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040716000502004071600050NM 2004 7 16 DL73S040574 120040617A3350 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHTSFAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27327DL 23099 EMERGENCY LIGHTS INOP ROW 11 THRU 15. REPLACED PWR SUPPLY FUSE. REPAIRED CHAFED WIRE. 2L72 4F RTA16WE 20040716000532004071600053NM 2004 7 16 DL764040578 120040620A3350 LAMP BOEING767 767432ER 1385134NM EMERGENC LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27840MH NA 29717 AT 23GF MID GALLEY AND AFT GALLEY HAS ONE EACH EMERGENCY CEILING LIGHT INOP. RELAMPED, OPS CHECK OK. 2L72 4F RTA1NM 20040716000572004071600057NM 2004 7 16 DL73S040583 120040618A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 INSPECTION OF THE FUSELAGE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 4R SKIN LAP JOINT AT FS 847. THE CRACKED AREA WAS REMOVED WITH A 4.25 INCH CUTOUT IN THE SKIN. THE AREA WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND DOCUMENTED PER ER/A 090881-14AD. 2L72 4F RTA16WE 20040716000612004071600061NM 2004 7 16 DL73S040587 120040618A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED A CRACK IN THE STRINGER 4R SKIN LAP JOINT AT FS 439. THE CRACK WAS REMOVED WITH A 4.25 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND DOCUMENTED PER ER/A 090880-14AD. 2L72 4F RTA16WE 20040716000722004071600072NM 2004 7 16 DL76S040606 120040627A335020121 CHARGER BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27128DL 24078 EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP ON RIGHT SIDE. REMOVED AND REPLACED BATTERY SUPPLY. 2L72 4F RTA1NM 20040716000742004071600074NM 2004 7 16 DL78K040608 120040628A3350D71702001 BATTERY PACK BOEING737 737832 13844CFNM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO273735D 30381 AFT OVERWING RIGHT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2L72 4F RTA16WE 20040716000772004071600077NM 2004 7 16 CALA0400563 120040703A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 907-927. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040716000792004071600079NM 2004 7 16 CALA0400565 120040704A3350UNK FUSE BOEING737 737524 1384721NM BATTERY PACK BLOWN A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714654 28915 THE EMERGENCY EXIT LIGHTS ABOVE L-2 DOOR AND FLOOR PATH LIGHTS ON ROWS 18-21 WERE FOUND INOPERATIVE. THE BATTERY PACK FUSE WAS REMOVED AND REPLACED IAW MM 33-51-02-101. 2L72 4F RTA16WE 20040716000802004071600080NM 2004 7 16 CALA0400566 120040614A5230 SKIN BOEING737 737824 13844BZNM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713248 28808 INSPECTION FOUND A DENT WITH GOUGE IN THE AFT CARGO DOOR AT STA 809.35. THE DENT WAS LOCATED IN THE SKIN BAY BETWEEN BEAMS B AND C JUST FORWARD OF BS 809.35. HFEC INSPECTION OF THE AREA DISCOVERED THAT THE GOUGE CONTAINED A CRACK. THE AFT CARGO DOOR WAS REPAIRED IAW ECRA 5231-01053. 2L72 4F RTA16WE 20040716000822004071600082NE 2004 7 16 QXEA200400474 220040623A7310AV24B1319D3 VALVE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE NR 2 ENG FUEL LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09367PH109423708 511 SEA - FLIGHT 2065 - FUEL WAS NOTED DRIPPING FROM THE FORWARD FUEL DOOR AT A RATE OF 11 DRIPS PER MINUTE. MAINTENANCE INSPECTED THE AREA AND FOUND THE REFUEL / DEFUEL VALVE LEAKING. THE VALVE WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040716000832004071600083NM 2004 7 16 CALA0400555 120040628A3233651781914 ACTUATOR BOEING737 7373T0 1384582NM NLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW271232736686 23457 THE NOSE GEAR DID NOT EXTEND INITIALLY WHEN THE GEAR WAS SELECTED DOWN ON APPROACH INTO IAH. THE GEAR WAS CYCLED RESULTING IN NORMAL EXTENSION AND INDICATIONS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. THE LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21. THE GEAR WAS SWUNG SEVERAL TIMES AND ALL OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20040716000862004071600086WP 2004 7 16 UPS04842640 120040615A53403750257U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 STATION 600-620 LONG 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2L74 4F RT4A25 20040716000872004071600087WP 2004 7 16 UPS04842641 120040609A5311 FRAME DOUG DC8 DC873F 302199FWP AC COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND SPLICES IAW SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20040716000892004071600089WP 2004 7 16 UPS04842644 120040613A5313 LONGERON DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 STATION 1260-1280 LONGERON 35R IS CRACKED. REMOVED LONGERON SECTION BETWEEN STATION 1270-1290, FABRICATED AND INSTALLED REPAIR DOUBLERS, CHANNELS, STRAP AND LONGERON SEGMENT IAW UPS ENGINEERING FILE NUMBER DC8-53-20422 AND SAA SK 894-477. 2L74 4F RT4A25 20040716000902004071600090WP 2004 7 16 UPS04842645 120040609A5311 FRAME DOUG DC8 DC873F 302199FWP AC COMPARTMENT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, STATION 55 FRAME IS CRACKED AT LONG 24R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND REPAIR SPLICES IAW SRM 53-2-0 FIG 2. 2L74 4F RT4A25 20040716000912004071600091WP 2004 7 16 UPS04842646 120040612A53403755847U1 FITTING DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 STATION 1220 BANANA FITTING IS CRACKED AT LONG 34R. REMOVED AND REPLACED FITTING IAW DWG 3755847, SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040716000942004071600094WP 2004 7 16 UPS04842649 120040615A5313 LONGERON DOUG DC8 DC873F 302199FWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 STATION 1766 LONG 17R AND END FITTING ARE CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON AND END FITTING IAW DWG 5649327, 4772397 AND SRM 51-1-20D, 520D, 51-1-21. 2L74 4F RT4A25 20040716000962004071600096WP 2004 7 16 UPS04842651 120040615A53405894282501502 FITTING DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, STATION 1210 AFT T-BOLT BACKUP FITTINGS FWD AND AFT SIDES ARE CRACKED AT LONG 33R. REMOVED AND REPLACED FITTINGS IAW DWG 5894282 AND SRM 51-1-20D. 2L74 4F RT4A25 20040716000982004071600098WP 2004 7 16 UPS04842653 120040615A57405614372503 FITTING DOUG DC8 DC873F 302199FWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 LEFT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5614372 AND M/M 27-51-12. 2L74 4F RT4A25 20040716000992004071600099WP 2004 7 16 UPS04842654 120040610A5510 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E IS CORRODED AT XFS 178.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS OR CORROSION AT CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20040716001002004071600100WP 2004 7 16 UPS04842655 120040707A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT STIFF A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:N/A CAPTAINS CLEARVIEW WINDOW HARD TO OPEN. OPENED AND CLOSED CAPTAIN'S SLIDING WINDOW THROUGH CYCLES. WINDOW OPENS AND CLOSES NORMALLY. NO DEFECTS NOTED. OK FOR CONTINUOUS SERVICE. 2L74 4F RT4A25 20040716001012004071600101WP 2004 7 16 UPS04842657 120040614A53403755841501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3 AFT PIT STATION 1200 FITTING IN TORQUE BOX 1 FT INBD OF DOOR CUTOUT IS CORRODED. REMOVED CRACKED Z-FITTING IAW DC8 SRM 51-1-20D. REC'D, LOCATED, & DRILL NEW Z-FITTING AND -3, -5 REPAIR ANGLES IAW DC8 SRM 51-1-24. FAB -7 & -9 IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040716001022004071600102WP 2004 7 16 UPS04842659 120040615A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3 CABIN SEAT TRACK BL 0 AT STA 850 TO 870 WORN & GOUGED SCALLOPS. BLENDED GOUGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS, CUT OUT DAMAGE IN TRACK IAW DC8 SRM 53-2-3 & EO DC8 5340-7779B. ALODINED & PRIMED SEAT TRACK, MAT ID SEAT TRACK P/N DC8-53B-007-002, PO SP0906208, CHANNEL SEAT TRACK, LOCATED AND DRILLED, PLUG AND CHANNEL ON SEAT TRACK. INSTALLED PLUG SEAT TRACK CHANNEL SEAT TRACK ON SEAT TRACK. 2L74 4F RT4A25 20040716001032004071600103WP 2004 7 16 UPS04842660 120040615A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, RIGHT WING LEADING EDGE INTERIOR RIB CHAFED ABOVE PNEUMATIC SHUT OFF VALVE. INSTALLED REPAIR DOUBLER IAW 57-2-0. 2L74 4F RT4A25 20040719000012004071900001 2004 7 19 ASMF200407011 420040707A34426225132106 TRANSCEIVER DOUG MD80 MD83 3023681NM RADAR DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23945AS10037 49643 CAPTAIN REPORTED LIGHTING STRIKE AND RADAR DISPLAY FAILED. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00, ALL CORRECT, BUT RADAR ANTENNA WAS INOPERATIVE. ANTENNA AND RADAR TRANSCEIVER WERE REPLACED IAW MM 31-41-01 AND 34-41-02, TESTS CORRECT. 2L72 4F RT 20040719000032004071900003NE 2004 7 19 ASMF200407010 220040705A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT FAILED W ASMFA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW23946AS225369940 49658 728049 AIRCRAFT RETURNED, RT ENGINE FAILED. CAPTAIN REPORTED DURING TAKE OFF AT 111 KNOTS, RT ENGINE EXPERIMENTED AN EXPLOSION WITH DROPPED OF PARAMETERS AND LOW FUEL FLOW, REACHED 770 DEGREES (F). DURING MAINTENANCE REVISION, RT ENGINE WAS DETECTED WITH FAN JAMMED BY HIGH TEMPERATURE, T3 AND T4 SECTION WITH BLADES DAMAGED IN 90 PERCENT AND NGV´S DAMAGED. RT ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. FURTHER INFORMATION ABOUT ENGINE FAILURE ANALYSIS WILL BE SENT AS SUPPLEMENT. 2L72 4F4 FRT E9NE 20040719000072004071900007NM 2004 7 19 ANCF200400016 120040706A26136002701 SENSOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE BRAKE TEMP MALFUNCTIONED W ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23583AN 53183 DURING TAKE OFF ROLL, WHEN RELEASING BRAKES IT FELT LIKE ONE BRAKE WAS STUCK, BRAKE TEMPERATURE WENT UP TO 320 DEGREES (C) GIVING OVERHEAT LIGHT ON. TAKE OFF WAS DISCONTINUED. SENSOR PROBE WAS REMOVED AND REPLACED IN BRAKE NR 3 IAW AMM 32-42-07 PAGE. 201/203 2L72 4F4 FRT E2EA 20040719000232004071900023NE 2004 7 19 ASMF200407015 220040711A75325840207104 BLEED VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE FAILED W ASMFO OTHER J WARNING INDICATION CLCLIMB 1 SW23803AM147775348 26268 1727138 CAPTAIN REPORTED WHEN STARTING CLIMB FROM FL350 TO FL390 THE RT ENGINE EPR'S INDICATION FLUCTUATE SEVERALLY AND ENGINE PANCAKING AND NOT CLIMBING. AIRCRAFT WAS SENT TO THE HANGAR AND BOROSCOPE INSPECTION AND FIM TESTS WAS PERFORMED TO RT ENGINE IAW MM 72-00-00 AND 71-05-00 NO DAMAGES WERE FOUND. 14TH AND 17TH STAGES BLEED CONVERTER VALVES WERE REPLACED IAW MM 75-32-03 AND 75-32-02, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20040719000572004071900057EA 2004 7 19 FFS2004F00001 220040622A8530LW16740 EXHAUST VALVE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NR 3 CYLINDER CRACKED E FFSAK NONE O OTHER ININSP/MAINT 1 AL013536B1339 317952205 L820561A COMPRESSION CHECK REVEALED ZERO COMPRESSION IN THE NR 3 CYLINDER. INVESTIGATION FOUND A HOLE BURNED THROUGH THE HEAD OF THE EXHAUST VALVE. THE FAILURE SEEMED UNUSUAL BECAUSE THERE WERE MULTIPLE CRACKS IN THE HEAD OF THE VALVE IN A CIRCUMFERENTIAL ORIENTATION AROUND THE STEM BUT THE EDGE OF THE VALVE AND THE SEATING AREA APPEARED IN REASONABLY GOOD CONDITION FOR THE TIME IN SERVICE. (AL01200404049) 1L72 3O3 O A20SO E14EA 20040719000732004071900073NM 2004 7 19 USA2004F00091 120040629A793121SN04334 PRESSURE SWITCH BOEING767 767201 1385125NM GE CF6 CF680C2B2 30025NE RT ENGINE FAULTY A USAAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 EA19650US 23902 695423 INBOUND, THE CREW RECEIVED THE EICAS MESSAGE (R ENG OIL FILTER). THE MESSAGE REMAINED ILLUMINATED WHEN THE ENGINE THRUST WAS REDUCED. CREW SECURED THE ENGINE. FLIGHT LANDED, WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH. 2L72 4F4 FRTA1NM E13NE 20040719000762004071900076EU 2004 7 19 A6WA200460019 120040602A5230 SKIN BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502* 41580EA CARGO DOOR SCRATCHED A K NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 AFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CUT DAMAGED AREA OUT IAW BAE SRM 52-32-11 FIG 201 PARA 3B PER BAE FAX BARA/AVR/6767/04-DC. HFEC INSPECTION C/O ON CUT OUT REPAIR, NO CRACKS NOTED. REPAIR PARTS FABRICATED AND INSTALLED IAW BARA/AVR/6767/04-DC. (M) 2H74 4F4 FRTA49EU E6NE 20040719000912004071900091NM 2004 7 19 USAA040025 120040114A5315 FLOORBEAM BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US55490 24894 CLT - FOUND FLOORBEAM CORRODED 1 INCH BY .5 INCH AREA, STATION 283, RBL 88 TOP OF FLOORBEAM. CUT T-CAP OUT AND FABRICATED NEW CAP PER SRM 53-00-51. (M) 2L72 4F RTA1NM 20040719000942004071900094EA 2004 7 19 A6WA200440020 120040206A2750 DRIVE ASSY CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 GL31403AW 7288 FOUND FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. REMOVED AND REPLACED 1 FLEX DRIVE CABLE AND 2 BPSU IAW MM 27-51-10. PERFORMED RIGGING AND OPS CHECK. OPS CHECK GOOD, S/N 5310, 0857. 2L72 4F RTA21EA 20040719000982004071900098EA 2004 7 19 A6WA200440080 120040613A4930 ELBOW CNDAIRCL600 CL6002B19 1900309EA APU FUEL SOV LEAKING A A6WAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL31450AW 7823 AIR VENT IN COCKPIT AND CABIN EMITTING A OIL LIKE ODOR, SMELLS LIKE KEROSENE, STRONGER AT TIMES THAN OTHERS WITH NO RELATION TO POWER SETTINGS. FOUND APU FUEL SOV SOLENOID LEAKING FROM LOWER ELBOW FITTING INSTALLED NEW PACKING ON ELBOW FITTING, OPS CHECK GOOD IAW 49-31-05. (M) 2L72 4F RTA21EA 20040719000992004071900099EA 2004 7 19 ASOA04243 120040327A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11846AS 7328 DURING A GROUND INSPECTION IN DFW, THE RT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040719001002004071900100NM 2004 7 19 2004F00163 120040217A5753 SKIN BOEING727 727222 1384073NM MID FLAP DELAMINATED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077638U 19911 AT C-CHECK, FOUND LEFT WING INBOARD MID FLAP LOWER SURFACE TRAILING EDGE WITH DELAMINATION. FABRICATED FILLER AND DOUBLER. CUT NEW CORE. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED AND SEALED. (M) 2L73 4F A3WE 20040719001012004071900101 2004 7 19 2004F00164 420040326A2210C13042BA01 COMPUTER AIRBUS320 A320233 3930329EU FLT MANAGE MALFUNCTIONED A SOKFA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO23486TA 1730 SJO - FLT 641 - DURING APPROACH DUAL FMGC MESSAGE CAME ON, DUE TO THIS CONDITION AIRCRAFT RETURNED TO SAN JOSE AIRPORT. ON GROUND MAINTENANCE, RESET BOTH FMGC SYSTEMS PER AMM 22-83-00, AND FOUND NORMAL, THEM RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4F RTA28NM 20040719001022004071900102NM 2004 7 19 USAABB04028 120040304A324071404 VALVE BOEING757 7572B7 1384964NM RT MLG WW INOPERATIVE A USAAO OTHER J WARNING INDICATION LDLANDING 1 EA19631AU 27809 PHL - FLT 738 - CREW REPORTED THAT THE RIGHT SIDE BRAKES WERE INOPERATIVE ON LANDING ROLLOUT. MAINTENANCE REPLACED THE RIGHT BRAKE METERING VALVE ASSEMBLY. (M) 2L72 4F RTA2NM 20040719001042004071900104EA 2004 7 19 ASOA04245 120040328A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A C-CHECK IN MCN, THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 27 AFT CLIP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 27 AFT CLIP BRACKET IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040719001072004071900107NM 2004 7 19 USAA040057 120040308A5320 SUPPORT BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU61617 22196 CLT - FOUND SUPPORT CORRODED .5 INCH BY 2 INCHES, THRESHOLD SUPPORT, R4 DOOR, STATION S1640 TO STATION 1680 RIGHT. REPLACED SUPPORT BRACKETS PER SRM 53-00-04, 51-20-05, 51-40-02. (M) 2L72 4F RTA2NM 20040719001082004071900108NM 2004 7 19 USAA040059 120040307A5313 STRINGER BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU61617 22196 CLT - FOUND STRINGER 14R CRACKED 1.5 INCH, AT BS 800. INSTALLED STRINGER AND SPLICES PER SRM 53-00-03 FIG 201 AND SRM 51-10-02. (M) 2L72 4F RTA2NM 20040719001132004071900113EA 2004 7 19 A6WA200440091 120040604A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31431AW 7256 FOUND FLOORBEAM ANGLES CRACKED AT FS 280, WL 73.50, LBL 9 AND RBL 9, FLOOR LEVEL. REMOVED OLD FLOOR SUPPORT ANGLES AT FS 280 WL 73.50 INBOARD SIDE OF LBL 9 AND RBL 9. INSTALLED NEW ANGLES PART NR RH 601R31113-58, LH 601R31113-57. ALL WORK IAW CRJ200 SRM 51-23-00, 51-25-21, 51-40-11, 51-42-21, 51-21-11, 51-25-16, AND 51-42-06. (M) 2L72 4F RTA21EA 20040719001182004071900118SO 2004 7 19 SWIA200413564 120040709A2797 WIRE EMB 120 EMB120ER 3260203SO ELEVATOR BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07576SW 120345 NO LIGHTS OR ALARMS SOUNDED DURING AILERON/ELEVATOR DISCONNECT OPERATION. REPAIRED TWO BROKEN WIRES WERE NEAR THE CONNECTOR AT THE ELEVATOR DISCONNECT. OPERATIONAL CHECK GOOD REFERENCING MM 27-13-01. 2L72 4T RTA31SO 20040719001192004071900119SO 2004 7 19 SWIA200413565 120040708A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07563SW7923 7923 120338 MIDDLE SECTION EMERGENCY LIGHTS IN CABIN INOP. REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040714001462004071400146EA 2004 7 14 MASA200400347 120040617A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0787353 7353 TWO SERVICE DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHTS INOP. PLACED ON MEL. MX RELAMPED. 2L72 4F RTA21EA 20040714001562004071400156NM 2004 7 14 DL73S040621 120040701A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27320DL 23092 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH TYPICAL CRACK ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 18R NEAR FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 091644-14. 2L72 4F RTA16WE 20040714001612004071400161NM 2004 7 14 DL757040592 120040623A5410 PIN BOEING757 757232 1384965NM NR 1 DIAG BRACE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27632DL 23613 CRACKS WERE NOTED IN THE FUSE PINS ON THE NR 1 PYLON DIAGONAL BRACE. COMPLIED WITH ERA 091408-14AD. 2L72 4F RTA2NM 20040714001652004071400165NM 2004 7 14 DL757040625 120040703A3350 BULB BOEING757 757232 1384965NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27625DL 22915 ON LAYOVER, FOUND TRACK LIGHTS INOP AT 3D AND 12D. RELAMPED, OPN OK. 2L72 4F RTA2NM 20040714001672004071400167NM 2004 7 14 CALA0400571 120040710A5347 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 910-927. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040714001782004071400178NM 2004 7 14 250TR0035 120040705A3397 WIRE BOEING737 7372K5 138448XNM EMERGENCY LIGHT DAMAGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 L-2 LOW LEVEL LIGHT DOOR IDENTIFIER INOP. REPAIRED WIRING AT LIGHT ASSY. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20040714001902004071400190NM 2004 7 14 CALA0400560 120040702A3350 FUSE BOEING757 757224 1384958NM BATTERY PACK BLOWN A CALAK NONE O OTHER ININSP/MAINT 1 SW2767134 29283 INSPECTION FOUND EMERGENCY LIGHTS AT AIRCRAFT CABIN LEFT MID SECTION INOPERATIVE. INSPECTION FOUND BATTERY PACK M10954 HAD FUSE BLOWN. THE FUSE WAS REPLACED AND THE EMERGENCY LIGHT OPERATION WAS RESTORED IAW MM 33-51-13. 2L72 4F RTA2NM 20040714001932004071400193WP 2004 7 14 UPS04842620 120040607A5347S4889036 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C, LUG BROKEN POS 3 LEFT O/B SEAT TRACK PLANK NEXT TO LOCK. REMOVED AND REPLACED SEAT TRACK PLANK SECTION FS-200 TO FS-265-00. 2L74 4F RT4A25 20040714001962004071400196WP 2004 7 14 UPS04842623 120040615A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C, LBL 25 SEAT TRACK SCALLOPS GOUGED AT BS 1138 & 1144 APPROX MAIN CARGO. BLENDED GOUGE IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. CUT OUT SEAT TRACK FROM STA 1115 TO 1215 LBL 25. MAT ID P/N 60-15176 PO SPO 980402 ID FITTING SPLICE P/N DC8-53B-003-501 IAW EO DC8-5320-5167-C. LOCATED, DRILLED & DEBURRED SEAT TRACK & FITTING SPLICE. ALODINED SEAT TRACK, INSTALLED SEAT TRACK & FITTING SPLICE IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040714001992004071400199WP 2004 7 14 UPS04842626 120040615A53472772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C, CABIN SEAT TRACK LBL 50 FROM STA 740 TO STA 770 WW & GOUGED AREAS. REMOVED GOUGE AND WORN SPOTS, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE ON TRACK. LOCATED & DRILLED 745295-3 PLUGS & DC8-53B-007-006 CHANNEL IAW DC8 SRM 53-2-3 & UPS EO DC8-5340-7779B, ALODINED & PRIMED, INSTALLED 2 PLUGS AND 2 CHANNELS IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040715000032004071500003NM 2004 7 15 DL764040628 120040705A3350 BULB BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27836MH 29709 ON LAYOVER FOUND EMERGENCY EXIT LIGHT AT 33 CDE INOP. RELAMPED, OPERATION OK. 2L72 4F RTA1NM 20040715000072004071500007NM 2004 7 15 DL757040632 120040706A5330141N32416 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO27663DN 24992 FUSELAGE SKIN SUFFERED LIGHTNING STRIKE DAMAGE AT STA 436 AND STR 27R. REPAIRED IAW ERA 091144-14. 2L72 4F RTA2NM 20040715000082004071500008NM 2004 7 15 DL764040633 120040706A2910N012000000 TURBINE BOEING767 767432ER 1385134NM HYD SYSTEM FAILED A DALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO27832MH 29704 SHIP 1808 EXPERIENCED A ADP TURBINE FAILURE WHICH CAUSED SUPPORT ROD TO BREAK OFF AND BEND, ALSO 1 INCH HOLES IN ADP DOOR AND FAIRING WEB. REPAIRED AND REPLACED DAMAGED COMPONENTS. 2L72 4F RTA1NM 20040715000142004071500014SO 2004 7 15 MASA200400309 120040604A25604566M37B042NM PBE EMB 145 EMB145LR 3260212SO COCKPIT BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW07829MJ7781 145228 COCKPIT PBE SEAL BROKEN. REPLACED PBE. 2L72 4T RTT00011AT 20040715000152004071500015SO 2004 7 15 MASA200400317 120040605A2731 SWITCH EMB 145 EMB145LR 3260212SO PITCH TRIM DIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 PITCH TRIM RUNAWAY FULL NOSE DOWN AFTER WEIGHT ON WHEELS. MX CLEANED PITCH TRIM SWITCHES, SYSTEM OPS CHECKED OK. NO PARTS USED. 2L72 4T RTT00011AT 20040715000292004071500029SO 2004 7 15 SWIA200413553 120040707A5610 WINDSHIELD EMB 120 EMB120ER 3260203SO COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW 120281 RIGHT WINDSHIELD SHATTERED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040715000382004071500038NM 2004 7 15 SWAA041977 120040713A53116546593 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040715000422004071500042NM 2004 7 15 SWAA041981 120040713A52106969854 DOOR BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AT AFT FRAME LOWER CORNER, CRACKED. REPAIRED DOOR PER BAC DRAWING. 2L72 4F RTA16WE 20040715000432004071500043NM 2004 7 15 SWAA041982 120040713A335007912 COVER BOEING737 7375H4 138449DNM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER AT ROW 7 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040715000542004071500054SO 2004 7 15 SWIA200413516 120040627A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER P NO WARNING INDICATION TXTAXI/GRND HDL 1 NM07197SW496 496 120186 UPON SELECTING FLAPS 15 DEGREES ON TAXI, WITH THE FLAP SELECTOR IN THE 15 DETENT, NO MOVEMENT ON FLAP COMMAND OR ON INDICATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR ASSEMBLY IAW 27-50-05. OPS CHECKED GOOD. 2L72 4T RTA31SO 20040715000982004071500098NM 2004 7 15 CALA0400548 120040626A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FORWARD ENTRY RIGHT I/B SEAT TRACK CORRODED BETWEEN STA 328 AND 344. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-00-52. 2L72 4F RTA16WE 20040715001152004071500115NM 2004 7 15 CALA0400554 120040628A532065C3397210 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 340-360, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040716000062004071600006NM 2004 7 16 QXEA200400414 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - SEAT TRACK NR 11 HAS CORROSION ON TOP OF TRACK AT STATION X455. REPAIRED IAW RD 8-53-1342. 2H72 4T RTA13NM 20040716000132004071600013NM 2004 7 16 QXEA200400421 120040609A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - RIGHT HAND INBOARD SEAT RAIL NR 8 CHANNEL SCRATCHED AT APPROXIMATELY STATION X500.0 TO 518.0. REPAIRED IAW RD 8-53-1339, SRM 51-20-16 AND SRM 51-20-36. 2H72 4T RTA13NM 20040716000202004071600020SO 2004 7 16 SWIA200413489 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING UPPER FORWARD SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2L72 4T RTA31SO 20040716000292004071600029 2004 7 16 QXEA200400499 420040706A342042000332501 COMPUTER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 AHRS FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09415QX1304 1304 4081 SUN TO LAX - FLIGHT 2342 - AIRCRAFT DIVERTED TO BOI. WHILE CLIMBING THROUGH 18,000 AT - 200 KTS, HAD ELEVATOR FEEL CAUTION LIGHT. YAW DAMPER AND NR 2 ATT/HDG FAILURE. FOLLOWED ELEVATOR FEEL CHECKLIST. AIRCRAFT LANDED IN BOI SAFELY. REMOVED AND REPLACED NR 2 AHRS COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000442004071600044 2004 7 16 SWIA200413518 420040623A341845150340 VANE CNDAIRCL600 CL6002B19 1900309EA AOA MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM07412SW 7101 WIND SHEAR FAIL STATUS MESSAGE ON TAKEOFF AND DESCENT ONLY. REMOVED AND REPLACED LEFT AOA VANE IAW CRJ 200 MM CHAPTER 27-35-05. S/N OFF: 138. 2L72 4F RTA21EA 20040716000452004071600045SO 2004 7 16 SWIA200413519 120040627A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07188SW 120039 LIGHT BULB OUT ON ESCAPE PATH LIGHTING. RELAMPED AND REPLACED SOCKET IAW 33-51-01. OPS CHECK GOOD. 2L72 4T RTA31SO 20040716000472004071600047NM 2004 7 16 DL73S040571 120040615A555365474506 ATTACH FITTING BOEING737 737247 138448DNM VERTICAL STAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27373DL 23520 VERTICAL STABILIZER ATTACH LUG FOUND TO HAVE A THINNER FLANGE THAN BLUEPRINT. AREA REPAIRED IAW ERA 090968-14AD. 2L72 4F A16WE 20040716000582004071600058NM 2004 7 16 DL73S040584 120040618A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 INSPECTION OF THE FUSELAGE SKIN LAP JOINTS PER AD 2003-08 -15 REVEALED CRACKS IN THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 560 & 590. THE CRACKS WERE REMOVED WITH A 32.5 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND DOCUMENTED PER ER/A 090759-14AD. 2L72 4F RTA16WE 20040716000602004071600060NM 2004 7 16 DL73S040586 120040618A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27303DL 23075 INSPECTION OF THE SKIN LAP JOINTS PER AD 2003-08-15, REVEALED CRACKS IN THE STRINGER 4L LAP JOINT BETWEEN FS 430 & 450. THE CRACKS WERE REMOVED WITH A 25 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND DOCUMENTED PER ER/A 090993-14AD. 2L72 4F RTA16WE 20040716000672004071600067NM 2004 7 16 DL767040601 120040624A5330 SKIN BOEING767 767232 1385132NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27107DL 22219 CORROSION FOUND ON THE FUSELAGE SKIN AT APPROX FS 1323 BETWEEN S-39R AND 39L. DAMAGE REPAIRED WITH DOUBLER/TRIPLER ARRANGEMENT VIA ERA 091295-14 REV B. 2L72 4F RTA1NM 20040716000712004071600071NM 2004 7 16 DL73S040605 120040626A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27382DL 23609 ER/A 091431-14, CRACK FOUND IN FUSELAGE SKIN AT APPROX FS 520 JUST ABOVE STRINGER 16L. CRACK IS APPROX .5 INCH LONG. 2L72 4F A16WE 20040716000732004071600073NE 2004 7 16 DLM88040607 220040624A7314 PUMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FUELFAILED A DALAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SO27908DL40581 49539 718069 ON TAKEOFF ROLL AT 50 KTS RT ENGINE ROLLED BACK AND SHUTDOWN. REPLACED FUEL PUMP AND FUEL CONTROL UNIT PER MM. RAN ENGINE PER PFHB. 2L72 4F4 FRTA6WE E9NE 20040716000852004071600085WP 2004 7 16 UPS04842639 120040612A534037536451 FITTING DOUG DC8 DC873F 302199FWP BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, STATION 1766 AFT SIDE OF BULKHEAD, FITTING TO THE LEFT OF UPPER TAIL SKID FITTING IS CRACKED AT BOTTOM J FRAME AND BULKHEAD. REMOVED AND REPLACED FITTING IAW DWG 3753645 AND SRM 51-1-20D. 2L74 4F RT4A25 20040716000882004071600088WP 2004 7 16 UPS04842642 120040615A53403755841501N FITTING DOUG DC8 DC873F 302199FWP AFT LOWER CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE: C2, STATION 1200 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20040719000922004071900092NM 2004 7 19 USAA040026 120040106A5330 SKIN BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US55490 24894 PIT - FOUND SKIN CORRODED 1 INCH BY 1 INCH AREA, STATION 106, LBL 13 AFT CARGO INTERIOR BELLY SKIN. BLENDED CORROSION AREA TO INSURE CONTAINMENT OF CORROSION PER EA 95089. (M) 2L72 4F RTA1NM 20040719000952004071900095EA 2004 7 19 A6WA200440071 120040604A5300601R3111357 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31431AW 7256 FLOOR SUPPORT ANGLES CRACKED AT FS 280, WL 73.5 LBL 9 AND RBL 9, BOTH INBOARD ANGLES. REMOVED LEFT ANGLE, P/N 601R31113-57 AND RT ANGLE P/N 601R31113-58 AND INSTALLED NEW SAME P/N ANGLES LEFT AND RT AND TREATED AND PAINTED. ALL WORK PERFORMED IAW SRM 51-23-00, 51-25-21, 51-40-11, 51-42-21, 51-21-11, 51-25-16 AND 51-42-06. (M) 2L72 4F4 FRTA21EA E15NE 20040719000962004071900096EA 2004 7 19 A6WA200440086 120040616A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 FLOOR SUPPORT ANGLE AT FS 484 RBL 36 IS CRACKED. REMOVED CRACKED ATTACHMENT FLANGE, FABRICATED NEW REPAIR ANGLE,P/N 2 FROM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M) 2L72 4F RTA21EA 20040719001032004071900103EU 2004 7 19 USAASA04027 120040318A521061639103 BOTTLE AIRBUSA321 A321211 3930370EU ESCAPE SLIDE DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19173US10643 1481 CLT - THE L2 DOOR ESCAPE SLIDE INFLATION RESERVOIR PRESSURE WAS FOUND TO BE LOW. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE RESERVOIR. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040719001112004071900111EA 2004 7 19 A6WA200440072 120040604A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31431AW 7256 FLOOR ANGLE AT FS 484, RBL 27 RIGHT INBOARD IS CRACKED. REMOVED CRACKED RT INBOARD FLOOR ANGLE AT FS 484 WL 73.5 AND FABRICATED NEW ANGLE FROM S6144-14 AND INSTALLED IAW REPAIR NUMBER 601R-53-0029. (M) 2L72 4F4 FRTA21EA E15NE 20040719001202004071900120SO 2004 7 19 SWIA200413566 120040709A2612 FIRE LOOP EMB 120 EMB120ER 3260203SO LT NACELLE FALSE INDICATIONA SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07227SW LEFT ENGINE WHEEL WELL FIRE DETECTION LIGHT INDICATION ON. REMOVED AND REPLACED LEFT HAND ENGINE FIRE DETECTION LOOP IAW MM 26-11-01. OPERATIONAL CHECK GOOD. P/N: 3601-75-450/160C-5-817, S/N OFF: 7071. 2L72 4T RTA31SO 20040719001222004071900122EA 2004 7 19 SWIA200413569 120040519A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07595SW RIGHT SIDE 625 OBLIQUE ANGLE CRACKED RBL 14. REMOVED AND INSTALLED A NEW OBLIQUE ANGLE P/N 600-35012-52 IAW CRJ 200 SRM 51-42-21. 2L72 4F RTA21EA 20040719001252004071900125SO 2004 7 19 SWIA200413572 120040713A5230 SEAL EMB 120 EMB120ER 3260203SO CARGO DOOR DAMAGED A SWIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM07288SW 120316 LEVELING AT 22,000 CABIN PRESSURIZATION DUMPED. REPLACED CARGO DOOR SEAL AT 3 LOWER SEAL RETAINERS IAW EMB MM 52-30-01. LEAK CHECK GOOD. 2L72 4T RTA31SO 20040719001272004071900127 2004 7 19 SWAA041998 420040715A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040719001282004071900128NM 2004 7 19 SWAA041999 120040715A33506114789 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED A1 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20040719001292004071900129NM 2004 7 19 SWAA042000 120040715A531365C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 685, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040719001332004071900133NM 2004 7 19 SWAA042005 120040715A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29700GS 27835 DURING SCHEDULED C3 CHECK, FWD AND MID-AFT EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERIES PER MM. 2L72 4F RTA16WE 20040719001352004071900135 2004 7 19 SWAA042007 420040715A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040719001362004071900136NM 2004 7 19 SWAA042008 120040715A3350207377 LENS BOEING737 7377H4 1384404NM ROW 1 ABC MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 DURING SCHEDULED RON, FOUND EEPLS LENS AT ROW 1 ABC, MISSING. INSTALLED EEPLS LENS PER MM. 2L72 4F RTA16WE 20040719001382004071900138NM 2004 7 19 SWAA041990 120040714A3350101114 LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT FWD ENTRY, FWD SERVICE, RT OVERWING, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM. 2L72 4F A16WE 20040719001392004071900139 2004 7 19 SWAA041991 420040714A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040719001402004071900140NM 2004 7 19 SWAA041992 120040714A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND R1 DOOR CUTOUT STUB FRAME AT BS 296, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040719001432004071900143NM 2004 7 19 SWAA041995 120040714A3350604222 BATTERY BOEING737 7373Q8 1384670NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SPV, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040719001472004071900147 2004 7 19 SWIA200413542 420040629A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07224SW RIGHT STALL WARNING SYSTEM DOES NOT TEST. REMOVED AND REPLACED STALL WARNING PANEL, OPERATIONAL CHECK GOOD IAW EMB MM 27-36-00. 2L72 4T RTA31SO 20040719001502004071900150SO 2004 7 19 SWIA200413573 120040713A2797 WIRE EMB 120 EMB120ER 3260203SO AILERONS BROKEN A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07561SW 120335 CONTROLS DISENGAGE LIGHT ON MAP COMES ON INTERMITTENTLY. REPAIRED BROKEN WIRE NEAR AILERON DISCONNECT IAW 20-00-00, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040719001512004071900151SO 2004 7 19 SWIA200413574 120040702A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0716731 120190 FORWARD MOST EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED BLOWN FUSE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040719001532004071900153EA 2004 7 19 SWIA200413576 120040713A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07953SW 7813 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MCU AND HSTA. OPERATIONAL CHECK GOOD IAW CRJ MM CH 27-41-01. HSTA P/N: 9386-3, S/N OFF: 1080. 2L72 4F RTA21EA 20040719001542004071900154EA 2004 7 19 SWIA200413577 120040608A53206013701413 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW 7497 FS 625 RIGHT OBLIQUE ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. REMOVED 625 OBLIQUE ANGLE RIGHT SIDE, INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20040719001552004071900155EA 2004 7 19 SWIA200413578 120040608A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW LEFT 484 OUTBOARD VERTICAL SUPPORT ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. REMOVED AND INSTALLED SERVICEABLE REPAIR ANGLE IAW SRM 601R-53-0030 AND REO 601R-53-41-059. 2L72 4F RTA21EA 20040719001562004071900156EA 2004 7 19 SWIA200413579 120040608A5420 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW RIGHTHAND 484 OUTBOARD VERTICAL SUPPORT ANGLE IS CRACKED. ITEM FOUND AT C-CHECK. INSTALLED SERVICEABLE REPAIR ANGLE IAW SRM 601R-53-0030 AND REO 601R-53-41-059. 2L72 4F RTA21EA 20040719001582004071900158NM 2004 7 19 QXEA200400452 120040622A5210 MECHANISM BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX7070 4046 SEA - AFT PASSENGER DOOR IS HARD TO OPEN AND CLOSE. UPON INSPECTION FOUND DOOR SURROUND DIRTY. MAINTENANCE CLEANED THE AREA. NO PARTS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040719001592004071900159NM 2004 7 19 QXEA200400453 120040621A5210 MECHANISM BOMBDRDHC8 DHC8401 1390041NM ZONE 800 DIRTY A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX1144 4083 BOI - FLIGHT 2303 - THE CREW REPORTS THE AFT PASSENGER DOOR IS STICKY. MAINTENANCE INSPECTED THE DOOR AND REMOVED OBSTRUCTION AND THEN LUBED THE DOOR AS NEEDED. NO PARTS WERE REPLACED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040719001602004071900160NM 2004 7 19 DL73S040609 120040629A53206546877143 WEB BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 SHEAR BEAM WEB AT STRINGER 18A AND STA 727 FOUND CRACKED AT TYPICAL LOCATION. REPAIR IAW ERA 091442-14. 2L72 4F A16WE 20040719001612004071900161NM 2004 7 19 DL733040617 120040630A5330654577572 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 FUSELAGE SKIN CRACKED AT STA 767 AND STR 22R AT A CHEM MILL LOCATION. REPAIRED IN ACCORDANCE WITH ERA 091533-14. 2L72 4F RTA16WE 20040719001642004071900164NM 2004 7 19 DL73S040620 120040701A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27320DL 23092 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH LONG TYPICAL CRACK ALONG THE BONDED DOUBLER MILL LINE AT STRINGER 18R AT FS 747. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 091645-14. 2L72 4F RTA16WE 20040719001662004071900166NM 2004 7 19 QXEA200400507 120040701A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH 514 PDX - NR 4 SEAT TRACK HAS PITTING CORROSION ON FLANGE AND OUTBOARD SIDE OF LUGS. REPAIRED IAW SRM 51-40-11 AND RD 8-53-1102. 2H72 4T RTA13NM 20040719001672004071900167NM 2004 7 19 QXEA200400506 120040706A5311 FRAME DHAV DHC8 DHC8202 2809007NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH 514 PDX - THE FUSELAGE TO RADOME MOUNTING FLANGE FRAME AT THE 10:30 POSITION HAS A GOUGE THAT RUNS THE LENGTH OF IT AND IS APPROXIMATELY .012/.013 DEEP AT ONE POINT. REPAIRED IAW HORIZON AIR EA 2-53-563 AND RD 8-53-7981. 2H72 4T RTA13NM 20040719001682004071900168NM 2004 7 19 QXEA200400508 120040706A242031708001A GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09367PH3136 3136 511 SEA - ON FLIGHT NUMBER 2102, THE NR 2 AC GENERATOR LIGHT ILLUMINATED AFTER DEPARTURE. FOLLOWED CHECKLIST PROCEDURES AND WAS UNABLE TO RESET. REMOVED AND REPLACED NR 2 AC GENERATOR. PERFORMED FUNCTIONAL TEST OF AC GENERATOR SYSTEM. NO LEAKS OR FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040719001702004071900170EU 2004 7 19 UPS04142618 120040629A5210 DOOR AIRBUS300 A300B4622R 3930312EU CABIN UNLOCKED A IPXAO OTHER J WARNING INDICATION CRCRUISE 1 SO01148UP 831 ECAM L FWD CABIN NOT CLOSED. CHECK DOOR INDICATIONS BOTH UNLOCKED. DESCENDED 10,000 ECAM MESG CLEARED CABIN DIFF 4.5 CABIN ALTITUDE 6000 FT AT 10,000 CHECKED DOOR CLOSED INDICATORS UNSAFE. TROUBLESHOT TO DOOR LOCKING OUT OF RIG. RIGGED PER MM 52-10-21-05 AND CKS GOOD PER SAME. INSTALLED DOOR LINING PER MM 52-10-13-4, ALL DOOR INDICATION NORMAL. CHECKED DOOR WARNING PER MM 52-71-00 AND CKS OK. PRESSURIZED A/C TO 4P520 AND NO DOOR WARNING MESSAGES OCCURRED. 2L72 4F RTA35EU 20040719001712004071900171NM 2004 7 19 UPS04242616 120040621A5320 WEB BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, SUPPORT WEB BENEATH STAND-BY PUMP CRACKED AT ACCESS HOLE FOR DRAIN PLUG. STOP DRILLED CRACK AND SUPPORT WEB REPAIRED IAW SRM 51-40-2. 2L73 4F A3WE 20040719001722004071900172NM 2004 7 19 UPS04242617 120040623A5320 WEB BOEING727 72725C 138400HNM FUSELAGE PUNCTURED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, VENTRAL STAIRS TORQUE BOX HORIZONTAL WEB PUNCTURED AFT OF BS 1243 RIGHT O/B END. REPAIRED AREA IAW SRM 51-40-02. 2L73 4F A3WE 20040719001732004071900173NM 2004 7 19 UPS04542615 120040628A5330 SKIN BOEING757 75724APF 1384969NM FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01403UP 23725 DENT STA 450 JUST ABOVE STR 19L. REPAIR DOUBLER INSTALLED PER EO B757-5330-19636-C. 2L72 4F RTA2NM 20040719001742004071900174NM 2004 7 19 SWAA041964 120040712A53116546560 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 947, STRINGER 25R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040719001752004071900175NM 2004 7 19 SWAA041965 120040712A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040719001762004071900176NM 2004 7 19 QXEA200400493 120040510A2120 ODOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09539DS 4016 SEA FLIGHT 2339, BLEED FLOW IN CABIN AND COCKPIT VERY WEAK. FLIGHT ATTENDANTS REPORTS STUFFY AIR IN CABIN WITH ASSOCIATED DIRTY SOCK SMELL. ALL GASPER VENTS OPEN. OPERATEE NR 1 AND NR 2 ENGINES BLEED FLOW RESPONDED NORM AND MAN, NORM AND MAX TEMPERATURE CONTROL ALSO NORM. FLOW AND FLIGHT DECK AND CABIN POS APPEARED NORMAL. 2H72 4T RTA13NM 20040719001772004071900177NM 2004 7 19 QXEA200400494 120040520A3060 STRAP BOMBDRDHC8 DHC8401 1390041NM PROP BUSS BROKEN A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09403QX 4037 YYC FLIGHT 2331, PROP DE-ICE CAUTION LIGHT ILLUMINATED IN FLIGHT. UPON RESET VIA CHECKLIST, LIGHT CAME BACK ON WITH NR 2 AC GENERATOR CAUTION LIGHT. AC GENERATOR CAUTION RESET NORMALLY. MAINTENANCE FOUND NR 3 BUSS STRAP ON NR 2 PROP BROKEN. REPLACED BUS STRAP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040719001782004071900178NM 2004 7 19 QXEA200400496 120040702A5412 FIREWALL DHAV DHC8 DHC8202 2809007NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH 514 PDX - NR 2 NACELLE FIREWALL HAS A CRACK .300 INCH LONG AT STATION XN125.00 AND ZN-7.00, LEFT HAND SIDE BY EXHAUST OPENING. REPAIRED IAW RD 8-54-104. 2H72 4T RTA13NM 20040719001802004071900180NM 2004 7 19 QXEA200400502 120040707A2750 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS ILLUMINATED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09410QX 4053 FLAP POWER CAUTION LIGHT ILLUMINATED WHEN SELECTING FLAPS AT 5 DEGREES FOR LANDING. CYCLED FLAPS, CIRCUIT BREAKER AS PER CHECKLIST. FLAPS OPERATED NORMALLY. COMPLIED WITH OPERATIONAL TEST OF FLAPS. NO DEFECTS NOTED. CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040719001812004071900181NM 2004 7 19 151AW0014 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE SKIN CRACKED AT STR 25 RT BETWEEN BS 927 AND BS 947. REPAIRED PER SRM 53-00-01. 2L72 4F RTA16WE 20040719001822004071900182NM 2004 7 19 151AW0015 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO05151AW 23219 THREE CRACKS UNDER AN IMPROPER REPAIR AT STR 20 LT BS 727D, REPAIR TOO CLOSE TO SKIN LAP AT STR 20 LT BS 967, AND REPAIR INSTALLED WITH BLIND FASTENERS AT STR 24 LT BS 727E. REPAIRED AREAS PER SRM 53-00-01. 2L72 4F RTA16WE 20040719001832004071900183 2004 7 19 QXEA200400448 420040617A3418C16258AA TRANSDUCER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 AOA FAULTY A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09617QX5297 274 10130 THE FLIGHT RETURNED TO FIELD AFTER RECEIVING A STALL FAIL CAUTION DURING THE CLIMBOUT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LEFT ANGLE OF ATTACK TRANSDUCER. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040719001842004071900184NM 2004 7 19 151AW0018 120040702A5320 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 INTERCOSTAL CRACKED AT BS 360 LT STR 13. FABRICATED INTERCOSTAL AND INSTALLED PER EA 53-145. 2L72 4F RTA16WE 20040719001852004071900185NM 2004 7 19 QXEA200400475 120040624A5210 HANDLE DHAV DHC8 DHC8202 2809007NM ZONE 800 STIFF A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09369PH 513 MAIN CABIN DOOR OPEN/LOCK HANDLE IS GETTING VERY STIFF TO OPEN FROM BOTH INSIDE AND OUTSIDE. CLEANED AND LUBED DOOR STOP PADS. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040719001862004071900186NM 2004 7 19 151AW0011 120040702A5313 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 CRACK IN STR 7 LT AT BS 344. REPLACED STRINGER SECTION PER SRM 51-10-03. 2L72 4F RTA16WE 20040719001872004071900187NM 2004 7 19 151AW0013 120040702A5340 ATTACH ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FLOOR TO FRAME TRANSITION ANGLE CRACKED AT BS 639 LT. REPAIRED PER SRM 51-70-12. 2L72 4F RTA16WE 20040719001882004071900188NM 2004 7 19 151AW0017 120040702A5314 KEELBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 CORROSION ON KEEL BEAM AT BS 500D STR 28 RT. REPAIRED PER EA 53-144. 2L72 4F RTA16WE 20040719001892004071900189NM 2004 7 19 151AW0019 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE SKIN CRACKING AT SEVERAL LOCATIONS UNDER EXISTING REPAIR INSTALLED WITH BLIND FASTENERS FROM BS 727E TO BS 767 STR 18 LT TO STR 20 LT. REPAIRED PER EA 53-147. 2L72 4F RTA16WE 20040719001912004071900191EA 2004 7 19 QXEA200400492 120040703A2130GG670980051 SAFETY VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 FAULTY A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09604QX6163 10019 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A CABIN ALTITUDE WARNING WHILE PASSING THROUGH 17,000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 SAFETY VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040719001942004071900194EA 2004 7 19 A6WA200440092 120040622A5512 SKIN CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 DENT IN LEFT HORIZONTAL STABILIZER BOTTOM SKIN APPROXIMATELY 74 INCHES FROM VISOR AND 9 INCHES FROM 4E. PERFORMED A MAJOR REPAIR IAW BRAS EO 601R-55-5102 BY DRILLING NR 30 HOLE IN DAMAGE AREA AND PULLING DENT TO ORIGINAL CONTOUR. PERFORMED EDDY CURRENT INSPECTION TO ENSURE NO CRACKS EXIST AND INSPECTED FOR OIL CANNING. FILLED HOLE WITH CR3214 RIVET. (M) 2L72 4F RTA21EA 20040719001962004071900196EA 2004 7 19 A6WA200440081 120040616A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 FOUND RIGHT SIDE FS 621/FS 625 OBLIQUE ANGLE AT STRINGER 14R IS CRACKED IN RADIUS APPROXIMATELY 1 INCH. REPLACED CRACKED ANGLE WITH NE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M) 2L72 4F RTA21EA 20040719001972004071900197EA 2004 7 19 A6WA200440079 120040613A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31411ZW 7569 FLAPS FAIL MASTER CAUTION DURING FLAP RETRACTION DURING TAKEOFF 17 DEGREE SETTING. REMOVED AND REPLACED LEFT BPSU REF AMM 27-51-10. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040719001992004071900199EA 2004 7 19 A6WA200440089 120040616A5730 ACCESS DOOR CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OT AT WS 54.897 HAS FRETTING DAMAGE IN TWO AREAS, INBOARD AND FORWARD .004 IN CHES DEEP AT WORST AREA. REMOVED FRETTING CORROSION ON LOWER WING PLANK FUEL ACCESS DOOR IN THREE PLACES (.004 DEEP) WS 54.897 PANEL 640BB IAW BOMBARDIER REO 601R-57-21-030 REV C. (M) 2L72 4F RTA21EA 20040719002022004071900202EU 2004 7 19 A6WA200460023 120040614A5730 SKIN BAC 146 146300A 1500267EU LT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 FOUND LEFT INBOARD LEADING EDGE HAS WEAR DAMAGE OT THE INBOARD LEADING EDGE WHERE THE STALL BAR ATTACHES. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 612-190-006. (M) 2H74 4F RTA49EU 20040719002032004071900203EU 2004 7 19 A6WA200460021 120040607A3260 WARNING LIGHT BAC 146 146200A 1500266EU MLG DOOR ILLUMINATED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31606AW E2033 AFTER GEAR UP SELECTED LEFT MLG RED INDICATION STAYED ILLUMINATED WITH GEAR INTRANSIT IN GEAR HANDLE ILLUMINATED GEAR SELECTED DOWN ALL NORMAL INDICATIONS. MAINTENANCE FOUND LEFT GEAR DOOR IN THE OPEN FOR MAINTENANCE POSITION. CLOSED DOOR FOR FLIGHT. (M) 2H74 4F A49EU 20040719002042004071900204NE 2004 7 19 GAIA04083OP 220040619A7200 ENGINE BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 3 MALFUNCTIONED A GAIAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW07279US 21158 696499 FLT 2878 - DURING CLIMB, SFO-FWA - SHUTDOWN NR 3 DUE TO HIGH OIL PRESSURE AND RISING OIL TEMP. OIL PRESSURE WAS 53 PSI, OIL TEMP WAS 130 UNTIL POWER REDUCED, THEN OIL TEMP SPIKED OFF SCALE. DUMPED 20,000 LBS FUEL. OIL TEMP GAUGE REMAINED OFF SCALE. AN EMERGENCY WAS DECLARED AND THE CREW RETURNED TO SFO WHERE AN UNEVENTFUL LANDING WAS MADE. (M) 2L73 4F4 F A3WE E2EA 20040719002052004071900205NM 2004 7 19 USAA040244 120040601A5315 FLOOR SUPPORT BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU60500 22203 CLT - FOUND FLOORBEAM CORRODED 6 INCH TOTAL AREA, LOWER DOOR SILL OF AFT CARGO DOOR FUSE STATION 1380-1440. REMOVED VERY LIGHT SURFACE CORROSIONPER SRM 53-60-15 FIG 101, SH 6. (M) 2L72 4F RTA2NM 20040719002062004071900206EU 2004 7 19 USAA040272 120040602A5320D5347112420000 WEB AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW 1019 BFM - FOUND WEB CORRODED 2.2 INCHES BY 1.7 INCHES BY .45 INCH AND 1.4 INCH BY 1.65 INCH BY .04 INCH, MAIN DECK FLOOR WEB AFT LEFT CORNER FRAME 69-70, Y1192-Y1292. REMOVED AND REPLACED WEB PER SRM 53-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002072004071900207EU 2004 7 19 USAA040275 120040603A5320D5347218920200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND FLOOR SUPPORT RAIL CORRODED 1.60 INCH BY .900 INCH WIDE BY .023 INCH DEEP, FRAME 68-69, -Y1192, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002082004071900208NM 2004 7 19 USAABB04044 120040520A21216067723 FAN BOEING757 7572B7 1384964NM FWD CARGO COMPT INTERMITTENT A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19614AU 27145 AUA - ON CLIMB-OUT, CREW RECEIVED THE E/M 'R ENG EEC' AND LIGHT. AS THE CREW TROUBLESHOT THE PROBLEM, AND ELECTRICAL SMELL WAS NOTED IN THE COCKPIT. CREW DONNED OXYGEN MASKS, AND BEGAN A RETURN TO AUA. THE SMOKE DISIPATED AND THEN RETURNED PRIOR TO LANDING. THE CABIN CREW ALSO NOTED A LIGHT HAZE AND SMELL NEAR THE L2 DOOR. MAINTENANCE PERFORMED NUMEROUS CHECKS IN THE CABIN AND COCKPIT, INCLUDING INSPECTING CIRCUIT BREAKER PANELS AND AVIONICS COMPARTMENTS, RUNNING THE PACKS AND PNEUMATIC SYSTEM. THE RIGHT RECIRCULATION FAN WAS FOUND TO BE OPERATING INTERMITTENTLY. MAINTENANCE REPLACED THE RIGHT EEC AND THE RIGHT RECIRCULATION FAN. (M) 2L72 4F RTA2NM 20040719002092004071900209NM 2004 7 19 USAABB04055 120040619A33201010181 HOUSING BOEING757 7572B7 1384964NM LIGHT SHORTED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19614AU 27145 MCI - FLT 625 - EN ROUTE, CREW REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LIGHT ASSEMBLY FOR THE NS/FSB SIGN SHOWED SIGNS OF ARCING. THE LIGHT HOUSING WAS REPLACED. (M) 2L72 4F RTA2NM 20040719002112004071900211EU 2004 7 19 USAA040267 120040602A5320D5348001921600 WEB AIRBUSA319 A319112 3930323EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND WEB CRACKED 5 INCHES BY .0003 INCH BY .063 INCH, FS 68-59, Y 1192, -Z240. REPLACED WITH NEW PART PER SRM 51-72-11, PAGE 1, 51-42-11, 51-44-11. (M) 2L72 4F RTA28NM 20040719002122004071900212NM 2004 7 19 USAABB04054 120040619A4900 FILTER BOEING767 7672B7 1385107NM APU IDG BYPASSING A USAAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 EA19652US 24765 ON TAXI OUT, THE RIGHT IDG ON MEL AND THE APU OPERATING, THE APU PERFORMED AN AUTO SHUTDOWN. THE FLIGHT RETURNED TO THE GATE. MAINTENANCE FOUND IDG FILTER BYPASS BUTTON POPPED AND REPLACED THE IDG. FURTHER ACTION ON THE APU PENDING. (M) 2L72 4F RTA1NM 20040719002142004071900214EU 2004 7 19 USAA040270 120040601A5320D5347217220290 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 1.5 INCH BY .060 INCH DEEP, FRAME 68-69, Y1192, -Z240. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-535. (M) 2L72 4F RTA28NM 20040719002152004071900215EU 2004 7 19 USAA040273 120040601A5320D5347112420100 WEB AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND WEB CRACKED 2.5 INCHES BY 1.35 INCH BY .040 INCH, AFT OF FRME 69, -Y1192, -Y1292. REPLACED WEB PER SRM 51-41-17. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002172004071900217EU 2004 7 19 USAA040265 120040530A5310D5347209001000 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND BEAM CORRODED 2 INCHES BY 1 INCH BY .068 INCH AREA, FLOOR SUPPORT, FRAME 64-66, Y1292, -Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-15. (M) 2L72 4F RTA28NM 20040719002182004071900218EU 2004 7 19 USAA040268 120040608A5347D5311278720201 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND TRACK CORRODED .150 INCH BY .045 INCH BY .025 INCH AREA, SEAT TRACK, FRAME 23,Y-1292. REMOVED AND REPLACED TRACK PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040719002192004071900219EU 2004 7 19 USAA040277 120040603A5320D5347209001100 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND FLOOR SUPPORT RAIL CORRODED 1.4 INCH LONG BY .098 INCH WIDE BY .023 INCH DEEP, FRAME 64-66, -Y1292. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-74-00, 53-00-14, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-74-00, 53-00-14, 51-42-11. (M) 2L72 4F RTA28NM 20040719002202004071900220NM 2004 7 19 USAA040279 120040604A5312 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US51120 23934 PIT - FOUND WEB CORRODED .25 INCH AREA, STATION 1016, AFT PRESSURE BULKHEAD WEB AT BL 0 UNDER STIFFENER. REMOVED FASTENERS BURNISHED AREA, TREATED, PRIMED, RE-INSTALLED FASTENERS PER EO 5302V112A. (M) 2L72 4F RTA16WE 20040719002212004071900221NM 2004 7 19 USAA040245 120040601A5330 SKIN PANEL BOEING757 7572B7 1384964NM HORIZONTAL STAB CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19630AU32420 27808 CLT - FOUND SKIN PANEL CHAFED/GOUGED, 6 INCHES BY .040 AREA, UNDR RIGHT HORIZONTAL STABILIER SLIDING SEAL. FABRICATED SMALL SKIN PANEL AND INSTALLED PER SRM 53-80-01 FIG 101 DWG 148N3611. (M) 2L72 4F RTA2NM 20040719002222004071900222EU 2004 7 19 USAA040263 120040601A5315D5347218820200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1 INCH BY .075 INCH AREA, FS 66-68M Y1192 TO Y1292, -Z240. REPLACED FLOORBEAM PER SRM 53-00-14. CORRODED LEVEL 2, TASK NR JA-160-53500. (M) 2L72 4F RTA28NM 20040719002232004071900223EU 2004 7 19 USAA040276 120040602A5347D5347209000300 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND BEAM ASSEMBLY SEAT TRACK 2 INCHES BY 1.6 INCH BY .070 IND DEEP AREA, FRAME 64-66, -Y765, -Z240. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11, 51-21-11, 51-23-11. (M) 2L72 4F RTA28NM 20040719002282004071900228EU 2004 7 19 USAA040327 120040612A5320D538004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND DOOR SILL CORRODED 1 INCH BY 1 INCH BY .068 INCH AREA, R2 DOOR SILL, -Y1732, FRAME 66-68, -Z240. REPLACED DOOR SILL PER SRM 53-41-14. (M) 2L72 4F RTA28NM 20040719002292004071900229EU 2004 7 19 USAA040261 120040604A5315D5347209000200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .032 INCH DEEP, FS 66, Y765, Z240. REMOVED AND REPLACED BEAM PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA 260 53500. (M) 2L72 4F RTA28NM 20040719002312004071900231EU 2004 7 19 USAA040283 120040604A5321D536106Z100000 FLOOR PANEL AIRBUSA319 A319112 3930323EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND FLOOR PANEL DELAMINATED MORE THAN 10 PERCENT MAIN DECK FLOOR PANEL, 231 CF. FABRICATED NEW PANEL PER SRM 53-02-00, FIG 209. (M) 2L72 4F RTA28NM 20040719002322004071900232NM 2004 7 19 USAA040280 120040529A532065516989 SPLICE BOEING737 737301 1384611NM STRINGER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US51120 23934 PIT - FOUND STRINGER SPLICE CRACKED 1 INCH, STRINGER 4 LEFT, FRAME STATION 907 IN CENTER FLANGE OF STRINGER SPLICE. REMOVED AND REPLACED PART PER OM-26 AND J3-58-53513-C-001. (M) 2L72 4F RTA16WE 20040719002332004071900233NM 2004 7 19 USAA040281 120040608A5312 STIFFENER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US50306 23740 PIT - FOUND BULKHEAD STIFFENER 1 INCH BY 2 INCH AREA, STATION 1016 LBL 0. REMOVED CORROSION AND INSTALLED REPAIR PER BOEING DWG 65C28106. (M) 2L72 4F RTA16WE 20040719002342004071900234NM 2004 7 19 USAASB04063 120040521A3397 WIRE BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 5, 6, 7, 8 AND 10 INOPERATIVE. MAINTENANCE FOUND WIRES SHORTED AT SEAT ROW 9, LEFT SIDE. REPAIRED WIRES. ALSO, REPLACED BATTERY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040719002352004071900235EU 2004 7 19 USAA040241 120040601A5315D5347219021000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW15935 0890 FOUND BEAM CORRODED 1.5 INCHES LONG BY 2 INCHES WIDE BY .029 INCH DEEP, FRAME 64-66, Y1375, Z240. REMOVED AND REPLACED BEAM ASSEMBLY PER SRM 53-41-14, 51-42-11, 51-23-11 AND EA 95512. (M) 2L72 4F RTA28NM 20040719002382004071900238EU 2004 7 19 USAA040242 120040601A5315D5347209001100 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19701UW15935 0890 PIT- FOUND BEAM ASSEMBLY CORRODED 1.5 INCHES LONG BY 1.3 INCH BY .65 INCH AREA, FRAME 64-66, -Y1300, Z240. REMOVED AND REPLACED BEAM ASSEMBLY PER SRM 51-42-11, 53-00-14, EA 95512. (M) 2L72 4F RTA28NM 20040719002412004071900241EU 2004 7 19 USAA040313 120040607A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND SILL ASSEMBLY CORRODED 1 INCH BY .8 INCH BY .061 INCH AREA, FRAME 66, -Y1732, -Z240. INSTALLED NEW ILL ASSEMLBY PER SRM 53-41-14, PAGE 103 FIG 101. (M0 2L72 4F RTA28NM 20040719002432004071900243EU 2004 7 19 USAA040330 120040610A5320D5311146020201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND FLOOR SUPPORT CORRODED 1 INCH BY .90 INCH BY .040 INCH AREA, FRAME 20, -Y254, Z-240. INSTALLED NEW FLOOR SUPPORT PER SRM 53-11-14, FIG 102. (M) 2L72 4F RTA28NM 20040719002442004071900244EU 2004 7 19 USAA040329 120040609A5347R53070089202 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND SEAT TRACK CORRODED 1 INCH BY 5 INCH BY .032 INCH AREA, FRAME 24 BL Y-1292. INSTALLED NEW SEAT TRACK SEGMENT AND SPLICES. (M) 2L72 4F RTA28NM 20040719002462004071900246EU 2004 7 19 USAA040333 120040609A5320D5348015900400 SUPPORT AIRBUSA319 A319112 3930323EU FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND SUPPORT PLATE CORRODED 6 INCHES BY .5 INCH BY .020 INCH AREA, FRAME 66, -Y1975, -Z240. REMOVED AND REPLACED R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE PER SRM 51-74-00, SRM 53-12-00. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002472004071900247EU 2004 7 19 USAA040326 120040610A5315D5347219021100 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND BEAM CORRODED 1 INCH BY 1 INCH BY .20 INCH AREA, FS 66, BL -Y1292, -Z240. REPLACED WITH NEW PART PER SRM 53-00-14 FIG 102. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002482004071900248EU 2004 7 19 USAA040325 120040610A5315D5347218920200 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND BEAM CORROED 1.5 INCHES BY 1 INCH BY .25 INCH CORRODED, BETWEEN FRAME 68 AND 69, BL -Y1292, -Z240. REPLACED WITH NEW PART PER SRM 53-00-14, FIG 102. (M) 2L72 4F RTA28NM 20040719002492004071900249EU 2004 7 19 USAA040314 120040603A5330D5311253400000 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW 1019 BFM - FOUND PLATE ASSEMBLY CORRODED 1 INCH LONG BY .075 INCH WIDE BY .040 INCH DEEP AREA, L7 DOOR 9R, -Z240, FRAME 68. REMOVED AND REPLACED PARTS PER SRM 51-72-11. (M) 2L72 4F RTA28NM 20040719002512004071900251EA 2004 7 19 A6WA200440009 120040118A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31448AW 7814 CAPTAINS FORWARD WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD. (M) 2L72 4F RTA21EA 20040720000012004072000001EU 2004 7 20 HXS2004F00099 120040419A6210355A11002011 BLADE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR CRACKED B HXSDO OTHER O OTHER NRNOT REPORTED 1 AL0557954 1127 MAIN ROTOR BLADE WAS FOUND TO HAVE A CRACK ON THE LOWER SURFACE OF THE BLADE, 172.72 CM FROM PIN ROOT. CRACK IS 5.08 CM LONG. (AL05200400824) 1G71 3U3 UNCH9EU E19EU 20040720000042004072000004WP 2004 7 20 UPS04842661 120040707A3242 LINK DOUG DC8 DC871F 302199DWP NR 4 BRAKE BROKEN A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01706UP 46056 NR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK TO BRAKE IAW M/M 32-42-01-4 AND 32-33-002 2L74 4F RT4A25 20040720000062004072000006EU 2004 7 20 2004F00175 120040620A5330D5331034900200 PANEL AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A SOKFK NONE O OTHER ININSP/MAINT 1 SO23463TA 1339 MIA-SJO - DURING GROUND INSPECTION OF FLIGHT LR627, IT WAS FOUND PANEL 191DT DAMAGED, WITH MATERIAL LOST AND DELAMINATED. AT MIA STATION, REPLACEMENT OF THE PANEL 191DT WAS PERFORMED, PER AMM 53-35-11. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040715000512004071500051EA 2004 7 15 SWIA200413513 120040622A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07906SW 7510 FUSELAGE TRANSVERSE BEAM HAS A CRACK BY LOWER FLANGE FS 280.00 RBL 12.0. DISCOVERED DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-11-171. REV. "NC" 2L72 4F RTA21EA 20040715000662004071500066SO 2004 7 15 SWIA200413523 120040506A5720 BRACKET EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET IS CRACKED AT RIB 22. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW SRM 57-20-07, 51-40-05, 51-25-00, 51-40-02. 2L72 4T4 TRTA31SO E20NE 20040715000692004071500069SO 2004 7 15 SWIA200413526 120040629A3350 LIGHT EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE CABIN INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07223SW 120291 FIRST 2 EMERGENCY OVERHEAD LIGHT PODS ARE INOP. REPLACED 1ST EMERGENCY OVERHEAD LIGHT POD WITH A SERVICEABLE UNIT. SECOND OVERHEAD EMERGENCY LIGHT OPERATES NORMALLY. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040715000772004071500077NM 2004 7 15 DLM88040598 120040624A3244 CAP DOUG MD88 MD88 3023688NM NR 3 TIRE FAILED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO27958DL 49977 NR 3 MAIN TIRE CAP FAILED AFTER TAKEOFF FROM PVD, A/C DIVERTED TO BOSTON. REPLACED SAME AND REPAIRED SECONDARY DAMAGE. 2L72 4F RTA6WE 20040715000882004071500088NM 2004 7 15 DLM88040615 120040701A3320D77311001 BALLAST DOUG MD88 MD88 3023688NM 27 ABC UNSERVICEABLE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27995DL 53362 REPORTED BY OVERNIGHT CLEANING CREW, SMOKE COMING FROM OVERHEAD BIN 27. FOUND BALLAST BURNED. REPLACED SAME, ALL OPS NOW NORMAL. 2L72 4F RTA6WE 20040715000892004071500089NM 2004 7 15 DL733040616 120040630A53306545775575 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 FUSELAGE SKIN CRACKED AT CHEM MILL LINE AT STA 727E BETWEEN STR 23L AND 25L. REPAIRED IAW 091565-14. 2L72 4F RTA16WE 20040715000932004071500093SO 2004 7 15 SWIA200413531 120040702A2460 RELAY EMB 120 EMB120ER 3260203SO APU FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM0758733 ELECTRICAL BURNING ODOR EMINATING FROM F/O'S WALL PANEL AREA, VERY HOT TO THE TOUCH. REMOVED AND REPLACED APU FEEDER PROTECTION RELAY K0152 AND APU START CONTACTOR K0089, APU FEEDER PROTECTION RELAY PHENOLIC SEAT AND ASSOCIATED BUS BARS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040715000942004071500094NM 2004 7 15 CALA0400544 120040625A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND FORWARD ENTRY FLOORBEAM UPPER CHORD CORRODED AT STA 312, LBL 30 TO RBL 48. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2L72 4F RTA16WE 20040715001032004071500103SO 2004 7 15 SWIA200413483 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02. 2L72 4T RTA31SO 20040715001082004071500108NM 2004 7 15 SWAA041955 120040711A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040715001092004071500109NM 2004 7 15 SWAA041956 120040711A53156545804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 45, CORRODED. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20040715001102004071500110NM 2004 7 15 SWAA041957 120040711A53116547957 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME LOWER CLOSE OUT WEB AFT EDGE CRACKED. REMOVED AND REPLACED DOOR CUTOUT FRAME WEB PER SRM. 2L72 4F RTA16WE 20040715001122004071500112NM 2004 7 15 CALA0400551 120040626A5320AND101362404 FLOOR SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED BETWEEN STA 312 AND 344, LBL 15. THE FLOOR SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW ECRA 5310-03585 AND SRM 51-10-02. 2L72 4F RTA16WE 20040715001132004071500113NM 2004 7 15 CALA0400552 120040626A3350 CHARGER BOEING737 7373T0 1384582NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2712349 23587 THE EMERGENCY EXIT SIGN AT L-2 DOOR WAS FOUND FLICKERING ON AND OFF. THE BATTERY CHARGER AND BATTERY PACK AT L-2 DOOR WERE REMOVED AND REPLACED IAW MM 33-51-51, PAGES 201-207. AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT WAS GOOD. 2L72 4F RTA16WE 20040716000022004071600002EA 2004 7 16 QXEA200400490 120040614A2150GG670950083 HEAT EXCHANGER CNDAIRCL600 CL6002C10 1390015EA ZONE 100 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09607QX6760 10024 PDX - FLIGHT 2506 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE FLIGHT ATTENDANT REPORTED A STRONG BURNING/HOT SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RT DUAL HEAT EXCHANGER. OPERATIONAL CHECKS WERE GOOD AND THE A/C WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040716000032004071600003EA 2004 7 16 SWIA200413532 120040704A5350 RADOME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07464SW 7827 THE F/O SIDE WINDSHIELD CRACKED. REMOVED AND REPLACED F/O'S SIDE WINDSHIELD IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R33033-12, S/N OFF 03099H1509. 2L72 4F RTA21EA 20040716000142004071600014NM 2004 7 16 QXEA200400422 120040609A5740 ATTACH BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09358PH 506 PDX - RIGHT HAND WING AT BOTTOM LEADING EDGE 611E ATTACH BRACKET CRACKED, YW138, BOTTOM SPAR CAP. REPAIRED IAW SRM 51-40-00. 2H72 4T RTA13NM 20040716000192004071600019SO 2004 7 16 SWIA200413488 120040506A5720 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02. 2L72 4T RTA31SO 20040716000242004071600024SO 2004 7 16 SWIA200413493 120040506A5712 RIB EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RIGHT WING FORWARD RIB 19 CRACKED AT TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 19 REPLACED IAW EMB 120 SRM 51-40-07, 51-40-04, 51-40-05, 51-22-00, AND 51-40-07, AND CONTINUATION SHEET 1 AND 2. 2L72 4T RTA31SO 20040716000272004071600027SO 2004 7 16 SWIA200413496 120040530A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07284YV 120284 RIGHT FRAME 13 FLOOR PROP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10. 2L72 4T RTA31SO 20040716000312004071600031SO 2004 7 16 SWIA200413498 120040530A5320 SUPPORT BRACKET EMB 120 EMB120ER 3260203SO COCKPIT WINDOW CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07284YV 120284 FRAME 12 SUPPORT BRACKET AT PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL AFT OF PILOT'S DV WINDOW AT FS 3900 (BETWEEN FRAME 12, 13) PER EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20040716000322004071600032SO 2004 7 16 SWIA200413499 120040530A5420 BRACKET EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07284YV 120284 RIGHT HYDRAULIC PACK RESERVOIR, RIGHT LOWER MOUNTING BOLT BRACKET CRACKED INSIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SIDE OF RIGHT HYDRAULIC PACK VERTICAL MOUNT BRACKET PER SRM 51-40-02. 2L72 4T4 TRTA31SO E20NE 20040716000362004071600036EA 2004 7 16 SWIA200413536 120040703A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA LT MLG WW MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07965SW 7871 MAIN LANDING GEAR OVERHEAT MESSAGE INFLIGHT. REPLACED LEFT MAIN LANDING GEAR BAY HARNESS OVERHEAT SENSOR LOOP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040716000402004071600040NM 2004 7 16 QXEA200400501 120040514A33506104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09346PH159 477 SEA - RIGHT HAND FORWARD EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000432004071600043 2004 7 16 SWIA200413540 420040701A2340509612 HANDSET EMB 120 EMB120ER 3260203SO CABIN SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07583SW9057 9057 120351 SMOKE FROM FLIGHT ATTENDANT`S HANDSET. REMOVED AND REPLACED FLIGHT ATTENDANT'S HANDSET. 2L72 4T RTA31SO 20040716000562004071600056NM 2004 7 16 DLM88040582 120040621A5330595305077 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27994DL 53346 SKIN DENTED AT STATION 389 BELOW LONGERON 23L. AREA REPAIRED IAW ERA 090912-14. 2L72 4F RTA6WE 20040716000812004071600081 2004 7 16 CALA0400567 420040702A25655A32951 SLIDE BOEING767 767424ER 1385270NM R-4 DOOR DEPLOYED A CALAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SW276905910528 29454 THE R-4 DOOR ESCAPE SLIDE WAS INADVERTENTLY DEPLOYED BY CATERING WHILE AT AMS. THE SLIDE DEPLOYED TO THE GROUND, BUT DID NOT INFLATE. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-66-01-404-036. INVESTIGATION BY ENGINEERING CONCLUDED THAT WHEN THE SLIDE DEPLOYED IT STRUCK A CATERING VEHICLE RESULTING IN A 38 INCH TEAR IN THE SLIDE WHICH PREVENTED IT FROM INFLATING. 2L72 4F RTA1NM 20040716000842004071600084NM 2004 7 16 QXEA200400476 120040626A5210 LINKAGE DHAV DHC8 DHC8202 2809007NM PAX DOOR LACK OF LUBE A QXEAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 NM09347PH 480 SEA - FLIGHT 2215 - FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. CLEANED AND LUBED MAIN CABIN DOOR STOPS AND LINKAGE. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040716000922004071600092WP 2004 7 16 UPS04842647 120040614A57403645611U FITTING DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2, NR 1 ALT TANK BOOST PUMP FITTING IS CRACKED AT STRINGER 58 BETWEEN XRS 463-XRS428. REMOVED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D. 2L74 4F RT4A25 20040716000932004071600093WP 2004 7 16 UPS04842648 120040614A57403645611U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 BOOST PUMP BRACKET IS CRACKED IN NR 4 ALT BETWEEN XRS 463-XRS 428, ON STRINGER 58 AND 59. REMOVED AND REPLACED BRACKET IAW DWG 3645611 AND SRM 51-1-20D AND DWG 3645612. 2L74 4F RT4A25 20040719000022004071900002WP 2004 7 19 ASMF200407012 120040707A2910 LINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE HYD SYSTEM LEAKING W ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW23751RA 49779 CAPTAIN REPORTED REVERSE INOPERATIVE DUE TO -LT REVERSE ACCUMULATOR LOW- LIGHT ILLUMINATED. DURING CHECK HYDRAULIC LEAK WAS DETECTED IN ACCUMULATOR LINE. HYDRAULIC LINE WAS REPLACED IAW MM 78-31-04, ALL CORRECT. DURING REVERSE TEST, ACCUMULATOR PRESSURE INDICATED 3000 PSI AND DURING RETRACTED PRESSURE DROPPED TO INITIAL PRESSURE. REVERSE WAS DEFERRED IAW MEL 78-1. 2L72 4F4 FRTA6WE E2EA 20040719000772004071900077WP 2004 7 19 ASMF200406031 120040627A2760 LEVER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE SPOILERS DEFECTIVE W ASMFK NONE O OTHER ININSP/MAINT 1 SW23505MD 49149 CAPTAIN REPORTED, SPEED BRAKES AND GROUND SPOILERS SYSTEM OUT OF SERVICE DURING FLIGHT. SYSTEM WAS CHECKED AND LEVER WAS DETECTED VERY HARD AND OCCASIONALLY JAMMED. SPOILER MECHANISM WAS CHECKED AND SPOILER ACTUATOR CONNECTOR WAS DISCONNECTED. CONNECTOR WAS RECONNECTED AND TESTED IAW MM 27-62-05, ALL CORRECT. 2L72 4F4 F A6WE E2EA 20040719000932004071900093EA 2004 7 19 A6WA200440090 120040620A5743 BUSHING CNDAIRCL600 CL6002B19 1900309EA RT MLG LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 RIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .062 INCH. PERFORMED A MAJOR REPAIR TO MIGRATED RIGHT MLG AFT TRUNNION BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20040719001052004071900105NM 2004 7 19 UIEA200400004 120040111A3610 CLAMP BOEING747 747228F 1384895NM RN 2 BLEED VALVEBROKEN A UIEAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA15536MC 21576 LEFT WING OVERHEATED TWICE ON CLIMB-OUT AND THEN IN CRUISE. COMPLETED CHECKLIST TO ISOLATE LEFT WING WITH ONLY NR 2 ENGINE PYLON VALVES OFF, AND ISOLATION VALVE OPEN. FOLLOWING CLIMB FL320 TO FL350 WITH NR 1 AND NR 2 ENGINES BLEED VALVES CLOSED AND LEFT AND RIGHT ISOLATION VALVES OPEN WITH BOTH AIRCRAFT PACKS VALVES OPEN, LEFT WING OVERHEAT REOCCURRED. AS PER CHECKLIST COMPLETELY ISOLATED LEFT BLEED MANIFOLD FOR REMAINDER OF FLIGHT. FOUND NR 2 PYLON BLEED AIR VALVE AFT CLAMP BROKEN, BLEED AIR LEAKING. REMOVED AND REPLACED CLAMP IAW MM 36-11-04. LEAK CHECK GOOD. NO OVERHEAT INDICATION NOTED AND NO OVERHEAT DAMAGE NOTED. OVERHEAT TESTED IAW MM 36-22-01, OPERATION CHECK GOOD. (M) 2L74 4F A20WE 20040719001092004071900109NM 2004 7 19 USAA040058 120040308A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19602AU61617 22196 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 1 INCH AREA, TOP OF INTERCOSTAL BS 324-345 LBL 18, WL 208. REMOVED CORROSION AND FABRICATED FILLER STRAP PER SRM 51-40-02 AND BOEING DWG 141N5170. (M) 2L72 4F RTA2NM 20040719001122004071900112EA 2004 7 19 A6WA200440087 120040616A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 ATTACHMENT ANGLES AT FS 621 CRACKED AT LEFT/RIGHT SIDES. PERFORMED A MAJOR REPAIR TO CRACKED UNDER FLOOR SUPPORT ANGLE AT FS 621 LEFT SIDE AND RT SIDE BY REMOVING CRACKED SECTION OF ANGLE AND INSTALLING REPAIR IAW BOMBARDIER REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20040719001142004071900114EA 2004 7 19 A6WA200440085 120040616A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 FOUND FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 27. (M) 2L72 4F RTA21EA 20040719001162004071900116 2004 7 19 A6WA20440032 420040316A23006229851001 TUNING UNIT CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL31445AW 7804 STRONG ELECTRICAL ODOR ON FLIGHT DECK ON DESCENT INTO SAVE BACKUP RTU BACKLIGHTING AND RTU INOPERATIVE. REMOVED AND REPLACED BACKUP TUNING UNIT. TEST GOOD IAW AMM. REMOVED OFF MEL. NO FURTHR OCCURRENCES. (M) 2L72 4F RTA21EA 20040719001312004071900131NM 2004 7 19 SWAA042002 120040715A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040719001342004071900134NM 2004 7 19 SWAA042006 120040715A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29705SW 27839 DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 6 ABC, INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040719001452004071900145NM 2004 7 19 SWAA041987 120040713A21216454051 FAN BOEING737 7373H4 1384600NM E/E BAY OVERHEATED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW29604SW 27955 THIRTY MINUTES PRIOR TO LANDING, ELECTRICAL ODOR IN FWD PART OF CABIN. TURNED OFF GALLEY POWER, RECIRC FAN, GASPER FAN, SMELL SUBSIDED. REMOVED AND REPLACED RECIRC FAN PER MM. 2L72 4F RTA16WE 20040719001482004071900148EA 2004 7 19 SWIA200413543 120040704A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA E/E BAY LOOSE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07918SW 7645 FLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED ON ED2. RESECURED NR 1 SECU IN RACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040719001522004071900152EA 2004 7 19 SWIA200413575 120040714A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07932SW2319 2319 7714 STAB TRIM/MACH TRIM AUTO DISCONNECT INTERMITTENTLY. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD, REF CRJ MM CHAP 27-42-00. 2L72 4F RTA21EA 20040719001572004071900157EA 2004 7 19 SWIA200413580 120040608A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07427SW FLOOR SUPPORT ANGLE CRACKED AT FS 621.0, RBL 45, WS 73.5. ITEM FOUND AT C-CHECK. INSTALLED NEW ANGLES AT FS 621 RBL 45 WL 73 IAW BOMBARDIER REO 601R-53-61-117. 2L72 4F RTA21EA 20040719001622004071900162NM 2004 7 19 DL76S040618 120040702A5330146T32621 SKIN BOEING767 767332 1382001NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27133DN 24982 FUSELAGE SKIN CRACKED AT STA 1197+100 AND BL 0 AT LOWER VHF ANTENNA. AREA REPAIR IAW ERA 091394-14. 2L72 4F RTA1NM 20040719001982004071900198EA 2004 7 19 A6WA200440083 120040616A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 FOUND FLOOR SUPPORT ANGLE BRACKET IS CRACKED AT FS 484, LEFT SIDE, LBL 36. REMOVED CRACKED ATTACHMENT FLANGE AND FABRICATED NEW REPAIR ANGLE, P/N 1 FORM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M) 2L72 4F RTA21EA 20040719002272004071900227EU 2004 7 19 USAA040328 120040612A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND SILL CORRODED 1 INCH BY 1 INCH BY .080 INCH AREA, L2 DOOR SILL, FRAME 66 TO 68 PLUS Y1732, -Z240. REPLACED DOOR SILL PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002362004071900236EU 2004 7 19 USAA040332 120040608A5330D5348015800400 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND PLATE ASSEMBLY CORRODED 4 INCHES BY .50 INCH BY .020 INCH AREA, Y1732, -Z240, FRAME 66. INSTALLED NEW PLATE ASSEMBLY PER SRM 53-12-00. (M) 2L72 4F RTA28NM 20040719002372004071900237EU 2004 7 19 USAA040331 120040608A5330D5348015900400 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND PLATE ASSEMBLY CORRODED 2 INCHES BY 2 INCHES BY .40 INCH AREA, Y1732, -Z240, FRAME 68. INSTALLED NEW PLATE ASSEMBLY PER SRM 53-12-00. (M) 2L72 4F RTA28NM 20040719002402004071900240EU 2004 7 19 USAA040312 120040602A5347D53112782200 SEAT TRACK AIRBUSA319 A319112 3930323EU CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND SEAT TRACK CORRODED .135 INCH LONG BY .060 INCH WIDE BY .017 INCH DEEP AREA, BETWEEN FRAME 21 AND 23, BL Y-965, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15 FIG 101. (M) 2L72 4F RTA28NM 20040720000032004072000003CE 2004 7 20 WVB2004F02004 120040526A7820C1560200101 MUFFLER CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL LEFT INOPERATIVE E WVBAO OTHER O OTHER NRNOT REPORTED 1 AL01756DJ U20604005 826663 EC1485A DURING DEPARTURE CLIMB OUT OF NONESSENTIAL ELECTRICAL ITEMS. HE INSREASED VENTILATION AS THE CO INDICATOR GOT DARKER INDICATING CO INCREASE. HE RETURNED AND LANDED WITHOUT FURTHER PROBLEMS ALTHOUGH HE DID EXPERIENCE A HEADACHE AND NAUSEA. MAINTENANCE REPLACED THE MUFFLER AND HEATER SHROUD ON THE LT SIDE. OPS CHECK FLIGHT WAS NORMAL. 1H71 3O3 O A4CE E5CE 5 CP25EA 20040720000052004072000005NM 2004 7 20 2004F00174 120040615A29106517844314 LINE BOEING727 727224 1384076NM HYD SYSTEM CRACKED A FX7AO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO1979750 22452 DURING FINAL APPROACH HYDRAULIC SYSTEM A QUANTITY DROPPED TO ZERO LANDED SAFELY WITHOUT INCIDENT. FOUND NR 2 ENGINE SUPPLY LINE CRACKED REPLACED SAME PER MM 29-00. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVIEC WITHOUT FURTHER INCIDENT. (M) 2L73 4F A3WE 20040720000072004072000007EU 2004 7 20 SIMA200416004 120040531A53117252813117 FRAME SAAB SF340 340B 7860101EU FUSELAGE BENT A SIMAK NONE O OTHER ININSP/MAINT 1 SW21350CF20967 340B350 DURING A MBV INSPECTION, FOUND CARGO FRAME AT STATION 677 WAS FOUND BENT. RECONTOURED CARGO FRAME AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER AND HEAT TREATED DOUBLER TO T42, REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007172 PARA 7 DATED APRIL 28, 2004. (M) 2L72 4T RTA52EU 20040720000082004072000008EU 2004 7 20 SIMA200416003 120040602A53117252814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21350CF 340B350 ABI - DURING AN MBV INSPECTION, THE AFT FLANGE OF FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED THE CORRODED AREA BY CREATING A 2 INCH BY .75 INCH CUTOUT. FABRICATED A REPAIR ANGLE AND A FILLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 53-70-30 PARA 5 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040720000092004072000009EU 2004 7 20 SIMA200416002 120040601A53302024T3 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21350CF 340B350 DURING AN MBV INSPECTION OF THE FUSELAGE A DENT AFT OF FRAME 363 ON THE LEFT SIDE, WAS FOUND TO BE BEYOND SRM LIMITS. COMPLETELY REMOVED THE DAMAGED BY CREATING A 2.7 INCH BY 1.1 INCH CUTOUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE CUTOUT. NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 53-70-10 PARA 4 FIG 209 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040720000102004072000010EU 2004 7 20 USAA040322 120040610A5311 FRAME AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW 0997 FOUND FRAME CORRODED 4.5 INCHES BY 2 INCHES BY .053 INCH AREA, FRAME 66-68, Y1292, Z-240. INSTALLED NEW FRAME PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040720000112004072000011 2004 7 20 GAIA04076AOP 420040525A3442 INDICATOR BOEING727 727224 1384076NM RADAR SMOKE A GAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0769735 20664 BOS - AFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. REMOVED AND REPLACED RADAR INDICATOR. OPS CHECK AND SELF TEST GOOD ON GROUND. THIS CLEARS DMI NR 1855. PLACARD REMOVED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040720000132004072000013EU 2004 7 20 SIMA200415415 120040509A55127255150522 SKIN SAAB SF340 340B 7860101EU RT HORIZ STAB DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21400BR 340B400 ABI - AIRCRAFT SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZONTAL STAB UPPER SKIN. REMOVED DAMGAED UPPER SKIN. I NSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS3079, REV 43, 51-40-21, 22, 23, 25, 40, 51-20-50, 56, AND SAAB REPAIR STATEMENT 340SDSS007026. (M) 2L72 4T RTA52EU 20040720000142004072000014EU 2004 7 20 2004F00176 120040620A5270 WARNING LIGHT AIRBUS320 A320233 3930329EU E/E DOOR FALSE ACTIVATIONA RJEFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23470TA 1400 DURING CLIMB, AN ECAM MESSAGE OF DOOR AVIONIC OPEN CAME ON. CREW DIVERTED THE FLIGHT TO SAP STATION FOR MAINTENANCE. AFTER LANDING, INSPECTION OF THE AVIONICS DOOR WAS PERFORMED, WHICH IT WAS FOUND CLOSED. THE ECAM MESSAGE OF THE DOOR OPEN INDICATION WAS ENTER AS DEFERRED DEFECT PER MEL 52-70-01. AIRCRAFT RETURNED TO NORMAL OPERATION, BACK TO MAIN BASE. (M) 2L72 4F RTA28NM 20040720000152004072000015EU 2004 7 20 SIMA200415413 120040526A55327075T6 SKIN SAAB SF340 340B 7860101EU VERTICAL STAB DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 ABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON THE RIGHT SIDE OF THE VERTICAL STAB AND MBV INSPECTION. CUTOUT TWO DISBOND DENTS. THIRTEEN ABOVE VOR ANTENNA 6.0 AND 9.0 FORWARD OF TRAILING EDGE. FABRICATED TWO FILLERS, FILLER CUT OUT CORES WITH LY/HY 5052 MICROSPHERES AND AL FILLERS AND CURED. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SAAB REPAIR STATEMENT 340 SDS 006859 PARA 6.3.2 DATED 03-24-2004. PERFORMED SONIC BOND CHECK, NO DEFECTS NOTED. (M) 2L72 4T RTA52EU 20040720000162004072000016EU 2004 7 20 SIMA200415412 120040526A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 DURING AN MBV INSPECTION FRAME 677 WAS FOUND TO BE DENTED JUST ABOVE THE FLOOR ON THE RIGHT SIDE OF THE FUSELAGE. RECONTOURED THE DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION OF THE REWORKED AREA, NO DEFECTS NOTED. FABRICATED A ANGLED REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007144 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040720000172004072000017EU 2004 7 20 SIMA200415411 120040519A55127255150522 SKIN SAAB SF340 340B 7860101EU RT HORIZ STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 ABI - AIRCRAFT SUSTAINED HAL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZ STAB UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 22, 25, 40, 51-20-50, 51-40-60 AND SAAB REPAIR STATEMENT 72SDS1514. (M) 2L72 4T RTA52EU 20040720000182004072000018EU 2004 7 20 04FDEA02052 120040712A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 MAIN CARGO COMPT RIGHT SEAT TRACK NR 3 BETWEEN FRAMES 44.5 AND 54 HAS CORROSION AT FR 52, 48.5 AS MARKED. REMOVED SEAT TRACK DAMAGE AREA, FAB AND INSTALLED NEW SEAT TRACK SECTION REPAIR IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040720000192004072000019NM 2004 7 20 SWAA042014 120040716A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040720000202004072000020EA 2004 7 20 VNAA0406017 120040630A2910 B-NUT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE HYD SYSTEM FAILED A VNAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07705PS 10144 ON CLIMBOUT, THE CREW RECEIVED A NR 2 LOW PRESSURE AMBER CAS MESSAGE. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED THE B-NUT ON THE LEFT HAND SIDE OF THE NOSE GEAR AND INSPECTED THE NR 2 SYSTEM HYDRAULIC LINE PRESSURE IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040720000222004072000022EU 2004 7 20 RAIA00406011 120040614A3250AIR135670 SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG STEERING MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03564HK 41081 5473 - XNA - NOSE WHEEL STEERING INOP AND STICK SHAKER GOES OFF CONTINUALLY. MAINTENANCE REMOVED AND REPLACED WOW SWITCH. 2L72 4T RTA41NM 20040720000252004072000025 2004 7 20 RAIA00406014 420040615A34207003360948 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03568HK170694771 41086 3641 - PIT - AHRS NR 1 FAILED. MAINTENANCE REMOVED AND REPLACED AHRS COMPUTER. 2L72 4T RTA41NM 20040720000282004072000028SO 2004 7 20 RAIA00406017 120040616A3610S2U2226 O-RING EMB 145 EMB145 3260210SO CABIN AIR LEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03809HK 145187 3515 - PIT- DURING TAXI NR 2 LEAD LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED DUCT O-RING IN DISTRIBUTION DUCT AFT AVIONICS BAY. 2L72 4F RTT00011AT 20040720000302004072000030 2004 7 20 VNAA0407001 420040704A3418 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LT AOA FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL05426JS 3038 DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND AOA AND PUSHER FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE VISUALLY INSPECTED THE SYSTEM AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. THE SYSTEM WAS RESET AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040720000522004072000052SO 2004 7 20 C2XA04SH452 120040630A571114567215001 SPAR EMB 145 EMB145ER 3260211SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 DURING C-CHECK EDDY CURRENT INSPECTION USING EDDY CURRENT PROBE TEST BLOCK TB-M030B AS A STANDARD, LT WING SPAR 3 UPPER O/B HOLE FOR TORQUE BOX 1 ATTACH REVEALED A CRACK. MX REAMED HOLE TO 8.382MM(.330) AND REINSPECTED. CRACK WAS NOT REMOVED. HOLE WAS REAMED TO 8.763MM (.345) AND REINSPECTED. CRACK FOUND TO BE REMOVED. SINCE 2ND OVERSIZE CORRESPONDING FASTENER TO REAMED HOLE SIZE, P/N AIC791-05011Y, IS NOT AVAILABLE. MX REAMED HOLE TO .377 - .378 (V-SIZE REAMER) AND INSTALLED MS21134-06011 USING TORQUE VALUES OF 175 IN-LB, (19.8 N-M). MX INSTALLED A WASHER (MS21299-C6) UNDER THE HEAD OF THE BOLT, AND WASHER (MS21299-6) AND NUT (MS21133-06). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000542004072000054SO 2004 7 20 C2XA04IA083 120040703A3350SG9632 LIGHT EMB 145 EMB145XR 3260214SO GALLEY CRACKED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713123 145688 IAH - DURING ROUTINE INSPECTION THE GALLEY EMERGENCY LIGHT STRIP WAS FOUND TO HAVE A CRACKED COVER. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040720000562004072000056NM 2004 7 20 DL76L040652 120040713A2750 FITTING BOEING767 767332 1382001NM LT IB FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO271201P 28458 LEFT I/B FLAP I/B SUPPORT COLLAR FITTING ATTACHMENT FASTENER HOLE (O/B FWD HOLE) CORRODED REF NR 394 7-11-04. REPAIRED PER ERA 089397-14MA REV B. 2L72 4F RTA1NM 20040720000602004072000060NM 2004 7 20 DLM88040657 120040714A29107952170529 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM CRACKED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27988DL 53339 FL230 LOST RIGHT HYD QTY QTY DOWN TO 4 QTS. SHUT OFF RT HYD ENG PUMP PER CKLIST. QTY REMAINED CONSTANT AT 4 QTS UNTIL PUMP WAS TURNED ON IN PREP FOR LANDING. QTY THEN DECREASED TO 1 QT. MAINTENANCE NOTED HYD FLUID UNDER AIRCRAFT. APU NOT STARTED PER CREW CKLIST. ALSO NO LOW PRESSURE INDICATION FOR HYD. INSTALLED TEMP LINE ON RT SYS PRESS TRANS. LEAK CK'D GOOD. OK FOR 350 HRS PER M/M 20/12/09. INSP AFTER 175 FLT HOURS. 2L72 4F RTA6WE 20040720000612004072000061NM 2004 7 20 SWAA042013 120040716A53116546559 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE FRAME AT BS 927, STRINGER 24L, CORRODED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040720000632004072000063NM 2004 7 20 VNAA0406016 120040514A5350001A537A0120000 TAIL CONE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE AFT FAILED A VNAAO OTHER O OTHER CRCRUISE 1 GL05430JS23038 3044 UPON LANDING AT GSO, IT WAS FOUND THAT THE APU ACCESS DOOR HAD OPENED IN FLIGHT. MAINTENANCE WAS SENT TO GSO AND REPLACED THE APU TAIL CONE ASSMEBLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 53-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040720000852004072000085NM 2004 7 20 AALA20040722 120040713A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21913AN 29514 MIA - EMERGENCY LIGHT AT FORWARD CENTER CEILING AISLE AT ROW 3 IS INOPERATIVE. REPLACED BATTERY PACK M1674 FOR EMERGENCY LIGHT AT FORWARD CENTER CEILING AISLE AT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040720000912004072000091SO 2004 7 20 C2XA04SH439 120040707A531014522557617 SHEAR TIE EMB 145 EMB145ER 3260211SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000932004072000093SO 2004 7 20 C2XA04SH441 120040706A531014525181015 SHEAR TIE EMB 145 EMB145ER 3260211SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000952004072000095SO 2004 7 20 C2XA04SH442 120040706A491014536850601 FIREWALL EMB 145 EMB145ER 3260211SO APU BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13, SECTION 3, FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000972004072000097SO 2004 7 20 C2XA04SH445 120040622A531014522460009 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 19 TO 23. MAINTENANCE REMOVED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. MAINTENANCE WILL REPLACE THE AFFECTED BUTTSTRAP WHEN PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720000982004072000098SO 2004 7 20 C2XA04SH446 120040622A532014522459001 ANGLE EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED RAMP ANGLE IAW EMB 145 SRM 51-40-02 AND WILL REPLACE THE AFFECTED ANGLE WHEN THE PART BECOMES AVAILABLE. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720000992004072000099SO 2004 7 20 C2XA04SH447 120040628A531014530634009 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720001002004072000100SO 2004 7 20 C2XA04SH448 120040628A531014530634001 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720001012004072000101SO 2004 7 20 C2XA04SH449 120040703A531014523521002 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720001022004072000102SO 2004 7 20 C2XA04SH450 120040703A531014524765012 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720001032004072000103SO 2004 7 20 C2XA04CL068 120040707A323023092900001 UPLOCK EMB 135 EMB135ER 3260203SO ZONE 700 BROKEN A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2717507 145215 CLE FLT 2885 THE CREW REPORTED THE RIGHT MAIN LANDING GEAR DID NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE RT MLG UPLOCK BOX. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040720001042004072000104SO 2004 7 20 C2XA04SH454 120040630A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729917 145414 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10, STEP 2, FIG 201, SHEET 1. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4T RTT00011AT 20040720001052004072000105SO 2004 7 20 C2XA04SH455 120040710A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716918 145397 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040720001062004072000106SO 2004 7 20 C2XA04SH456 120040710A531014529150003 CROSSBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2729917 145414 SHV - DURING C-CHECK THE CROSSBEAM AT FRAME 23 FROM THE SERVICE DOOR AFT SILL TO THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040720001072004072000107SO 2004 7 20 C2XA04TY110 120040712A531514532636401 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2710575 145640 TYS - DURING A SCHEDULED 1C INSPECTION THE RT OMEGA BEAM FOR THE AISLE CROSS BEAM WAS FOUND CORRODED AT FR 25. MAINTENANCE REMOVED THE CORRODED AREA, FORMED, BENT A DOUBLER AND FILLER, PLUS SHIMS, ALODINED, PRIMED AND PAINTED. FAB PARTS WERE INSTALL IAW EMB 135/145 SRM 51-21-10; EMB 135/145 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040720001082004072000108SO 2004 7 20 C2XA04TY111 120040712A531514502851001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2710575 145640 TYS - DURING A SCHEDULED 1C INSPECTION THE CENTER FLOORBEAM AT FR 25 WAS FOUND CORRODED. MAINT BLENDED AREAS OF CORROSION FORWARD OF CROSSBEAM AT FR 25. ALODINED BLENDED AREA. PRIMED AND PAINTED AREA IAW EMB 135/145 CPM 51-21-04, 05, 06 AND SRM 51-10-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20040720001092004072000109SO 2004 7 20 C2XA04IA084 120040708A521014540853407 DOOR EMB 145 EMB145XR 3260214SO MAIN PAX OUT OF ADJUST A C2XAK NONE O OTHER ININSP/MAINT 1 SW27311313504 3504 145705 IAH - FLIGHT 2568, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE PASSENGER DOOR WAS EXTREMELY HARD TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR IN ACCORDANCE WITH EMB-145 AMM 52-18-06, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040720001102004072000110SO 2004 7 20 RAIA00406021 120040623A3610S2U226 SEAL EMB 145 EMB145 3260210SO BLEED LINE DETERIORATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK 145068 5766 - OKC - LEFT BLEED LEAK INDICATION. MAINTENANCE REMOVED AND REPLACED BLEED LINE COUPLING SEAL. 2L72 4F RTT00011AT 20040720001112004072000111SO 2004 7 20 RAIA00406022 120040624A2621 WARNING SYSTEM EMB 145 EMB145LR 3260212SO FIRE BOTTLE FALSE INDICATIONA RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03815HK9977 30480D1 145048 5616 - STL - ENG 1/2 BOTTLE EXT INOP WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 1 FIRE BOTTLE. 2L72 4T RTT00011AT 20040720001122004072000112SO 2004 7 20 RAIA00406023 120040624A3610S2U226 SEAL EMB 145 EMB145 3260210SO BLEED SYSTEM DETERIORATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03821HK 145068 5747 - STL - BLEED 2 LEAK WARNING MESSAGE. MAINTENANCE REMOVED AND REPLACED COUPLING SEAL. 2L72 4F RTT00011AT 20040720001132004072000113SO 2004 7 20 RAIA00406025 120040625A21328152915 SWITCH EMB 145 EMB145LR 3260212SO NR 2 A/C PACK FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK 145256 3572 - PIT - PACK 2 OVERLOAD WARNING MESSAGE. MAINTENANCE SWAPPED NR 1 AND NR 2 OVERTEMP SWITCHES. 2L72 4T RTT00011AT 20040720001142004072000114NM 2004 7 20 AALA20040724 120040624A5320 FLOOR SUPPORT BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 AFW - FLOOR SUPPORT TEE AT LEFT 4 DOOR HAS CORROSION REMOVAL ON H3 HINGE. VERIFIED CORROSION WAS COMPLETELY REMOVED. DYE CHECKED AREA FOR CRACKS AND REFINISHED THE BLENDED AREA WITH ALODINE AND TWO COATS OF BMS10-11 PRIMER. APPLIED CORROSION INHIBITING COMPOUND TO FLOOR SUPPORT TEE. FILLED BLEND WITH BMS5-99 SEALENT. 2L72 4F RTA1NM 20040720001192004072000119SO 2004 7 20 C2XA04SH460 120040716A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716918 145397 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040720001212004072000121SO 2004 7 20 C2XA04SH462 120040716A541014576057621 STIFFENER EMB 145 EMB145LR 3260212SO NR 1 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716918 145397 SHV - DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040720001232004072000123NM 2004 7 20 DL76L040646 120040711A2750113T11671 LINK BOEING767 767332 1382001NM LT IB FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO271201P 28458 DURING PSV7 ACCOMPLISHMENT OF EO 1-85672-12 REVEALED CORROSION IN THE LEFT I/B FLAP I/B SUPPORT IN THE O/B FWD HOLE. HOLE WAS REWORKED PER ERA 089397-14MA. 2L72 4F RTA1NM 20040720001252004072000125NM 2004 7 20 DLM88040648 120040712A3397487191 SPLICE DOUG MD88 MD88 3023688NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27990DL 53342 ON INSPECTION FOUND EMERGENCY PATH LIGHTS INOP FROM ROW 18-23. FOUND BAD SPLICE IN WIRES AT ROW 17 AND 18. REPAIRED WIRING AND LIGHTS NOW OPERATE NORMALLY. 2L72 4F RTA6WE 20040720001272004072000127 2004 7 20 RAIA00407007 420040711A34207003360948 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS MALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03558HK 41071 FIRST OFFICERS EFIS TUMBLED. REMOVED AND REPLACED NR 2 AHARS IAW J41 MM 34-25-05, OPS OK. 2L72 4T RTA41NM 20040720001292004072000129SO 2004 7 20 C2XA04CL070 120040710A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN AISLE AT ROW 12 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 12 EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040720001302004072000130SO 2004 7 20 SWIA200413500 120040530A5330 SKIN EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07284YV 120284 AT RIB 15A IN PAX DOOR ENTRANCE AFT OF PAX DOOR AFT ACTUATOR RIB CLIP IS CORRODED THROUGH TO SKIN. P/N 120-09800-001. DISCOVERED DURING C-CHECK INSPECTION. REMOVED FRAME SHEAR AT FRAME 15A. INSTALLED FRAME 15A SHEAR TIE BETWEEN STRINGER 18L - 19L. 2L72 4T4 TRTA31SO E20NE 20040720001312004072000131SO 2004 7 20 SWIA200413501 120040530A5313 STRINGER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07284YV 120284 STRINGER 18L AT FS 482(5) APPROX CORRODED OUT OF LIMITS PER EMB 120 SRM 53-00-03; APPROX 3 INCH AREA. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPLACEMENT STRINGER SECTION 18L AND SPLICE DOUBLERS 2 EA PER EMB 120 SRM 53-00-00. 2L72 4T4 TRTA31SO E20NE 20040720001322004072000132 2004 7 20 SWIA200413502 420040613A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07250YV 120250 RIGHT STALL WARNING ACTIVATES ON MAP AND AURAL WARNING INTERMITTENTLY IN FLIGHT. REPLACED STALL WARN COMPUTER WITH SERVICEABLE UNIT. ALSO REPLACED STALL WARN PANEL WITH SERVICEABLE UNIT. ALL CHECKS GOOD. PANEL P/N: 120-34428-505, S/N OFF 120127. 2L72 4T RTA31SO 20040720001352004072000135EA 2004 7 20 SWIA200413506 120040625A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07952SW2564 2564 7805 STAB TRIM CHANNEL NR 1 FAILED. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT PER RII 27-415 CARD. OPS CHECK GOOD IAW CRJ MM 27-40-00. MCU P/N: 7062-3, S/N OFF: 1105. 2L72 4F RTA21EA 20040721000022004072100002EU 2004 7 21 04FDEA02054 120040712A5310 CROSSBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 ZONE 152, AFT CARGO FLOOR CROSS MEMBER BEAM, RT CENTER AT FR 58 CORRODED. REMOVED CORRODED BAD SECTION IAW A310-200 SRM 53-10-15 FIG 207. FABBED REPAIR ANGLE AND FILLER IAW A310-200 SRM 53-10-15. LOCATED, DRILLED, DEBURRED, AND COUNTERSUNK IAW A310-200 SRM 51-40-44. INSTALLED ANGLE AND FILLER IAW A310-200 SRM 53-16-10. 2L72 4F RTA35EU 20040721000032004072100003NM 2004 7 21 04FDEA02055 120040712A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT OUTBOARD FLAP, OUTBOARD HINGE (FLAP SIDE) AFT MOUNTING AREA FORWARD HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.610. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED. 2L73 4F RTA22WE 20040721000062004072100006NE 2004 7 21 GAIA04079OP 220040609A7200500706301 TUBE BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE BROKEN A GAIAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW0769735 20664 FLT 6007 - SEA-KTN - DURING DEPARTURE, ENGINE NR 2 N2 AT 102 PERCENT AND EGT AT RED LINE ON CLIMB-OUT, EPR AT 1.89. AIRCRAFT RETURNED. LANDING WEIGHT 142000, NORMAL LANDING AND BRAKING. LANDING WAS MADE WITHOUT INCIDENT. INSPECTED NR 2 ENGINE AND FOND BROKEN PRBC LINE. REMOVED AND REPLACED PRESSURE LINE. RUN NR 2 PER KHA JET RUN HANDBOOK. OPS CHECK GOOD. ENGINE NR 2 TAKEOFF POWER AT 2.01 EPR, N1-95 PERCENT, EGT 560, N2 93 PERCENT. SYSTEM OPS CHECK GOOD. NO DEFECT NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20040721000072004072100007GL 2004 7 21 SIMA200415801 220040603A7200 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 1 FAILED A EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW21814AE 145541 DURING CLIMB AT FL290, CREW REPORTED A NR 1 ENGINE VIBRATION FOLLOWED BY A PUFF OF SMOKE IN THE COCKPIT. POWER WAS REDUCED AND A/C WAS DIVERTED TO CLT. DURING APPROACH WHEN NR 1 WAS BROUGH OUT OF IDLE CREW REPORTED MAX VIBRATION AND LOSS OF OIL PRESSURE. ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS LANDED SAFELY. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20040721000132004072100013EU 2004 7 21 SIMA200415406 120040519A53117252813485 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 ABI - DURING AN MBV INSPECTION, THE UPPER FLANGE OF FRAME 225 WAS FOUND TO CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED THE CORROSION BY CREATING A 3.0 CUTOUT OF THE UPPER FLANGE. FABRICATED A REPAIR ANGLE, SPACER AND FILLER PIECE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007122 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040721000162004072100016NM 2004 7 21 AMTA200400608 120040527A5210 DOOR BOEING757 757200 1384950NM MAIN PAX DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11512TZ 26635 UNABLE TO DISARM L2 DOOR. INSPECTED DOOR, FOUND TO BE FULLY DISARMED BY FLIGHT CREW, ARMED /DISARMED DOOR SEVERAL TIMES, NO DEFECTS NOTED, DOOR CHECKS OK. (M) 2L72 4F RTA2NM 20040721000182004072100018 2004 7 21 UIEA200400087 420040427A341737571835 CADC BOEING747 747243B 1384830NM NR 1 INOPERATIVE A UIEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 EA15540MC 22508 MIA-JFK - APPROXIMATELY 45 MINUTES DURING CRUISE, NR 1 CADC POWER C/B OPENED. C/B RESET PER FHB PROCEDURES. C/B OPENED AGAIN AND WAS LEFT OPENED FOR DURATIONOF FLIGHT. NY MAINTENANCE CONTROL DIVERT A/C TO MIA. REMOVED AND REPLACED NR 1 CADC OPERATION CHECKED FOUND TO BE SATISFACTORY IAW B747 MM 34-12-01. (M) 2L74 4F A20WE 20040721000192004072100019EU 2004 7 21 SIMA200415405 120040507A53117252813117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21359SB 340B359 DURING AN MRB 4000 HOUR INSPECTION, TWO DENTS WERE FOUND NEAR FLOOR LEVEL ON CARGO FRAME 658.5 THAT WERE BEYOND SRM LIMITS. RECONTOURED THE FRAME AND PERFORMED AN EDDY CURRENT INSPECTION NO CRACK INDICATED. FABRICATED A REINFORCEMENT DOUBLER. INSTALLED, REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007060, PARA 5. (M) 2L72 4T RTA52EU 20040721000232004072100023SO 2004 7 21 SIMA200409902 120040407A272015793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO RUDDER FAILED A SIMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 SW21625AE 145115 DFW - FLT 3764 - AUTOPILOT FAIL RUDDER SYSTEM 1-2 INOPERATIVE. ALSO, RAI NR 2 RUDDER PRESSURE SWITCH PERFORMED OPERATIONAL CHECK ON RUDDER SYSTEM AND AUTO PILOT SYSTEM IAW EMB 145 AMM 27-22-00 AND 22-11-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040721000242004072100024SO 2004 7 21 SIMA200410001 120040328A324431590 TIRE EMB 135 EMB135LR 3260305SO NR 3 MLG FAILED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21723AE 145288 NR 3 TIRE THREW TREAD CAUSING FLAP DAMAGE. REPLACED NR 3 WHEEL ASSEMBLY AND RIGHT FLAP, IAW EMB AMM. (M) 2L72 4F RTT00011AT 20040721000272004072100027 2004 7 21 SIMA200415402 420040530A34427014300901 DISPLAY EMB 135 EMB135LR 3260305SO RADAR INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW21704PG 145174 DCA - FLT 4753 - CREW REPORTED SMOKE SMELL AND NR 2 PFD WENT BLANK. REPLACED NR 2 MFD IAW EMB AMM 34-22-00-700-801-A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M0 2L72 4F RTT00011AT 20040721000282004072100028EU 2004 7 21 SIMA200415409 120040519A55127255150521 SKIN SAAB SF340 340B 7860101EU LT HORIZ STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 AIRCRAFT SUSTAINED HAIL DAMATE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZ, STAB UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED AND INSTALLED NEW SKIN. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, 51-40-21, 22,23, 25, 40, 60, 51-20-50 AND SAAB REPAIR STATEMENT. (M) 2L72 4T RTA52EU 20040721000302004072100030NM 2004 7 21 AMTA200400500 120040428A3350 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11526AT 30735 EGRESS TRACK LIGHTING INOPERATIVE FROM ROW 6 TO ROW 9. RECONNECTED WIRES TO LIGHT AT ROW 6. OPERATIONA NORMAL AT THIS TIME. (M) 2L72 4F RTA2NM 20040721000392004072100039NM 2004 7 21 2004F00182 120040424A25308101210000B OVEN BOEING737 73733A 1384673NM FWD GALLEY BURNED A FX7AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO19371FA 23631 SMOKE COMING FROM LOWER P6 PANEL, ACCOMPLISHED NNC 8.4-8.5 SMOKE DISSIPATED LANDED IN KMIA WITHOUT INCIDENT. FOUND FORWARD GALLEY OVEN SHORTED OUT. REMOVED OVEN FOR REPAIRS AND A/C RETURNED TO SERVICE WITHOUT INCIDENT. (M) 2L72 4F RTA16WE 20040721000402004072100040NM 2004 7 21 BJNA040501 120040503A3350900835A BATTERY PACK BOEING737 737282 13844ATNM EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, AN AISLE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE PER BOEING MM 33-51-81, SYSTEM NOW CHECKS NORMAL. (M) 2L72 4F RTA16WE 20040716000782004071600078NM 2004 7 16 CALA0400564 120040703A335020131A BATTERY PACK BOEING737 7373T0 1384582NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2770352 23590 INSPECTION FOUND THE EMERGENCY LIGHTS INOPERATIVE NEAR L-1 DOOR. THE OVERHEAD BATTERY PACK IN FORWARD GALLEY WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20040716000952004071600095WP 2004 7 16 UPS04842650 120040615A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2, LEFT AFT HEAT EXCHANGER LOUVER OPENING LOWER AFT CORNER SKIN IS CRACKED AT STATION -12 AT LONG 27L. CUT OUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO DC8-5330-4732-D. 2L74 4F RT4A25 20040716000972004071600097WP 2004 7 16 UPS04842652 120040610A5512 DOUBLER DOUG DC8 DC873F 302199FWP HORIZONTAL STAB DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 INSPECTION TYPE:C2 RIGHT UPPER HORIZONTAL STAB LEADING EDGE HAS ELONGATED HOLES BETWEEN XFS 47.5 TO XFS 110.0. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG 5644330 AND SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20040719000312004071900031NE 2004 7 19 ASMF200407003 220040702A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT OVERTEMP W ASMFO OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SW23946AS3507611369 49658 725561 CAPTAIN REPORTED THAT DURING TAKE OFF AT HMO, LT ENGINE EGT INDICATION REACHED 610 DEGREES (C) DURING 40 SECONDS AND DURING CLIMB (TAIL COMP HIGH) LIGHT TURNED ON. HIGH TEMPERATURE PROCEDURE WAS PERFORMED IAW MM 72-00-00 AND (TAIL COMP HIGH) LIGHT TURNED OFF. DURING OVERNIGHT SERVICE, PNEUMATIC LEAKS CHECK WAS PERFORMED IAW MM 72-00-00 AND 36-10-00, NO LEAKS WERE DETECTED AND EGT WAS WITHIN LIMITS. 2L72 4F4 FRT E9NE 20040719000592004071900059NM 2004 7 19 ASMF200407008 120040705A24219762J2528 GENERATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT SIDE FAILED W ASMFA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SW23861LF365086366 49826 716778 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, RT GENERATOR AND BATTERY CHARGER BREAKER FAILED AND (STALL INDICATION FAILURE) LIGHT TURNED ON. BATTERY CHARGER BREAKER WAS REESTABLISHED, STALL COMPUTERS TEST AND RT ENGINE START WAS PERFORMED TO VERIFY RT GENERATOR CONDITION AND GENERATOR WAS DETECTED WITHOUT VOLTAGE AND FREQUENCY. GENERATOR AND CSD WERE REPLACED IAW MM 24-10-01 AND 24-10-00, RESPECTIVELY, TESTS CORRECT. DURING OVERNIGHT SERVICE, GENERATOR AND CSD TESTS WERE PERFORMED IAW MM 24-10-02, ALL CORRECT. 2L72 4F4 FRT E9NE 20040719000972004071900097EA 2004 7 19 A6WA200440082 120040615A53206013501252 ANGLE CNDAIRCL600 CL6002B19 1900309EA LT FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 FOUND LEFT SIDE FS 621/FS 625, OBLIQUE ANGLE AT STRINGER 14L IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG, 1.1 INCHES. REPLACED CRACKED ANGLE WITH NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M) 2L72 4F RTA21EA 20040719001102004071900110NM 2004 7 19 USAA040048 120040312A5310 BEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19619AU36419 27198 PIT- FOUND BEAM CORRODED 2 INCH BY 20 INCH AREA, BL 0 BS 345-365. CORROSION LEVEL 1. REMOVED CORROSION AND INSTALLED DOUBLERS AND SHIMS PER SRM 51-70-12. (M) 2L72 4F RTA2NM 20040719001152004071900115EA 2004 7 19 A6WA200440035 120040310A3210601R572100321 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG TRUNNION LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31424AW 7656 THE LEFT MLG AFT TRUNNION BUSHING IS MIGRATED .058. REMOVED MIGRATED BUSHING. REAMED TRUNNION BORE TO 1ST OVERSIZE AND INSTALLED 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW SERVICE BULLETIN 601R-32-054 REV B PART B STEP 3A THROUGH 3E. (M) 2L72 4F RTA21EA 20040719001172004071900117SO 2004 7 19 SWIA200413563 120040709A2120 SMOKE EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07217SW 120286 SMELLED SMOKE IN COCKPIT ON GROUND. RAN BOTH PACKS. NO DEFECTS NOTED. 2L72 4T RTA31SO 20040719001232004071900123EA 2004 7 19 SWIA200413570 120040519A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07595SW INTERCOSTAL CLIP ON LEFT HAND SIDE AT FS 484 LBL 27 CRACKED. LOCATED UNDER FLOOR PANEL 261DLF. REMOVED CRACKED CLIP. INSTALLED NEW CLIP 601R31171-17 IAW CRJ 200 REO 601R-53-41-059. 2L72 4F RTA21EA 20040719001262004071900126NM 2004 7 19 SWAA041997 120040715A53306545768 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 315, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040719001322004071900132NM 2004 7 19 SWAA042004 120040715A57536546437 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD END, DELAMINATED. REMOVED AND REPLACED LT OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20040719001412004071900141NM 2004 7 19 SWAA041993 120040714A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO BAY FLOORBEAM AT BS 771, RBL 3 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040719001442004071900144NM 2004 7 19 SWAA041996 120040714A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29737JW 27869 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVERS AT ROW 2 ABC, ROW 8 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040719001462004071900146NM 2004 7 19 SWAA041988 120040714A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 FWD EEPLS COVER LOOSE, WIRE DISCONNECTED. SECURED COVER AND RECONNECTED WIRE PER MM. 2L72 4F RTA16WE 20040719001652004071900165WP 2004 7 19 UPS04842662 120040617A5712 RIB DOUG DC8 DC873F 302199FWP RT WING GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, RT WING OUT BOUND L/E INBOARD END RIB HAS DEEP GOUGE. BLENDED GOUGE AREA, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB DOUBLER REPAIR IAW DC8 SRM 57-2-0 AND 51-1-4. LOCATED & DRILLED DOUBLER IAW DC8 SRM 51-1-24 & 51-2-0. ALODINED & PRIMED DOUBLER IAW DC 8 SRM 51-1-8. INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-20D AND 51-2-0 FIG 2. 2L74 4F RT4A25 20040719001692004071900169EU 2004 7 19 UPS04142613 120040615A5753A57960032200 SKIN AIRBUSA300 A300F4622R 3930360EU LT INBD FLAP CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01120UP 0805 INSPECTION TYPE: C, LEFT WING INBOARD DAMAGED INTERIM REPAIR MADE IAW EO A300-5750-19043-A 1500 FLT CYCLE LIMIT (D263708). REPAIRED I/B FLAP WITH PERMANENT REPAIR IAW A300-600 SRM 57-50-00. 2L72 4F RTA35EU 20041227000422004122700042NM 2004 12 27 2004UALA01153 120041124A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT BETWEEN STA 1180L AND STA 1200L AT STRINGER 17L, CREASE BEAM WEB HAS CORROSION. REPLACED CREASE BEAM WEB. 2L72 4F4 FRTA2NM E17NE 20040719001902004071900190NM 2004 7 19 151AW00200 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE MISREPAIRED A PIDAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO05151AW 23219 INCORRECT REPAIR AT BS 360 STR 24 RT AT INTERSECTION OF SKIN LAP AND BUTT JOINT. REPLACED EXISTING REPAIR PER EA 53-148A. 2L72 4F RTA16WE 20040719001922004071900192EA 2004 7 19 A6WA200440078 120040608A2130601R9521171 DUCT CNDAIRCL600 CL6002B19 1900309EA CABIN AIR DAMAGED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31404AW 7294 PASSING THROUGH 10K FEET NOTICED LACK OF AIRFLOW. SWITCHED TO APU AIR. NO HELP PASSING THROUGH 22K FEET. RECEIVED 'CABIN HI ALT' MESSAGE. PERFORMED EMERGENCY DESCENT. DECLARED EMERGENCY AND RETURNED TO ORD. REMOVED AND REPLACED DUCT. REMOVED AND REPLACED CHECK VALVE (P/N 92E20-3) AND WATER SEPARATOR, P/N 601R95251-15. (M) 2L72 4F RTA21EA 20040719001952004071900195EA 2004 7 19 A6WA200440084 120040615A2910MS2190806 ELBOW CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A A6WAB EMER. DESCENT J WARNING INDICATION LDLANDING 1 GL31467AW 7900 HYDRAULIC NR 3 LOW PRESSURE CAS MESSAGE INFLGHT NR 3 HYDRAULIC SYSTEM QUANTITY AT ZERO PERCENT COMPLIED WITH QRH, PERFORMED MANUAL GEAR EXTENSION. FOUND FORWARD GROUND PRESSURE LINE FITTING LEAKING. REPLACED ELBOW FITTING. LEAK CHECK GOOD. SERVICED NR 3 SYSTEM. (M) 2L72 4F RTA21EA 20040719002002004071900200EU 2004 7 19 A6WA20046002 120040613A2750 ECU BAG BAE146BAE146200A 1500266EU TE FLAPS MALFUNCTIONED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL31610AW E2082 WHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREES AIRCRAFT RETURNED TO DEN. MAINTENANCE FOUND CODE 4 ON FLAP ECU, RESET ECU, NO FAULTS. NOTED. (M) 2H74 4F RTA49EU 20040719002012004071900201EU 2004 7 19 A6WA200460024 120040614A5512 SKIN BAC 146 146300A 1500267EU HORIZONTAL STAB GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 FOUND RIGHT HORIZONTAL STABILIZER TOP SKIN SMALL GOUGE IN THE UPPER SKIN OF THE RIGHT HORIZONTAL STABILIZER BETWEEN RIBS 9 AND 10. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 612-1909007. (M) 2H74 4F RTA49EU 20040719002102004071900210EU 2004 7 19 USAA040266 120040529A5347D5311281520200 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND SEAT TRACK CORRODED .750 INCH LONG BY .600 INCH WIDE BY .077 INCH DEEP, SEAT TRACK FRAME 16 AT Y + 765, -Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11, SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040719002132004071900213EU 2004 7 19 USAA040262 120040528A5310D5311282600201 BEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW 1019 BFM - FOUND BEAM CORRODED 4.8 INCH LONG BY 1.8 INCH WIDE BY .051 INCH DEEP, Z240 BETWEEN FS 13 AND FS 18 BL +Y503.2. INSTALLED NEW BEAM PER SRM 53-11-14, FIG 103. (M) 2L72 4F RTA28NM 20040719002242004071900224NM 2004 7 19 USAA040278 120040604A532051120 STIFFENER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US 23934 FOUND RADIAL STIFFENER CORRODED 1 INCH, STATION 1016, AFT PRESS BULKHEAD CENTER RADIAL AT BL 0 . MANUFACTURED AND INSTALLED REPAIR ANGLES TO REPLACED SECTION PER EO 5302V112A. (M) 2L72 4F RTA16WE 20040719002252004071900225EA 2004 7 19 A6WA200440088 120040617A5260 ANGLE CNDAIRCL600 CL6002B19 1900309EA AIRSTAIR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 PASSENGER DOOR STAIR STRUCTURE AFT ANGLE, P/N 601R31907-303 IS CRACKED .8 INCH LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. (M) 2L72 4F RTA21EA 20040719002262004071900226NE 2004 7 19 USAAEM04008 220040622A7320 COMPUTER EMB ERJ170ERJ170100 EU GE CF34 CF34* NE FADAC FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807MD177 17000020 PIT - ENGINE NR 1 FADEC REMOVED FOR TROUBLESHOOTING FOR ENGINE NR 1 FADEC FAULT. MAINTENANCE REPLACED NR 1 ENGINE FADAC. (M) 2L74 4F4 FRTA56NM E15NE 20040719002392004071900239EU 2004 7 19 USAA040324 120040610A5315D534721720390 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND BEAM CORRODED 1 INCH BY .50 I NCH BY .20 INCH AREA, BETWEEN FRAME 66 AND 68 BL -Y1292. REPLACED WITH NEW PART PER SRM 53-00-10 FIG 102. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040719002502004071900250EU 2004 7 19 USAA040323 120040608A5320D5347112420100 WEB AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND WEB CORRODED 5 INCHES BY 3 INCHES BY .040 INCH DEEP AREA, C69 TO C70 -Y1292. REMOVED AND REPLACED WEB PER SRM 53-14-00, 51-42-11. CORROSION LEVEL 2, TASK NR JA-260-53500. (M) 2L72 4F RTA28NM 20040720000272004072000027EU 2004 7 20 RAIA00406016 120040615A3260 SQUAT SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG OUT OF ADJUST A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03560HK 41076 5476 - STL- LANDING GEAR HANDLE WILL NOT MOVE TO UP POSITION. MAINTENANCE ADJUSTED LEFT MAIN LANDING GEAR WOW SWITCH. 2L72 4T RTA41NM 20040720000332004072000033 2004 7 20 SWAA042016 420040716A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29756SA 27872 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040720000342004072000034NM 2004 7 20 SWAA042017 120040717A3350207377 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 DURING SCHEDULED RON, FOUND EEPLS LIGHT LENSES AT RT ROW 3, RT ROW 11, BROKEN. REMOVED AND REPLACED EEPLS LENSES PER MM. 2L72 4F RTA16WE 20040720000352004072000035NM 2004 7 20 SWAA042018 120040717A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29637SW 27710 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040720000362004072000036NM 2004 7 20 SWAA042019 120040717A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29707SA 27841 AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT OVERHEAD LIGHT PER MM. 2L72 4F RTA16WE 20040720000372004072000037NM 2004 7 20 SWAA042020 120040717A57536546435303 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040720000382004072000038NM 2004 7 20 SWAA042021 120040717A33501010174 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C4 CHECK, FOUND CENTER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040720000392004072000039NM 2004 7 20 SWAA042022 120040717A3350BR9293 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040720000642004072000064NM 2004 7 20 VNAA0407002 120040713A3350 LIGHT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE CABIN FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07430JS 3044 THE CREW REPORTED THAT A EMERGENCY FLOOR LIGHT STRIP WAS NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY FLOOR LIGHTING STRIP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040720000662004072000066SO 2004 7 20 C2XA04SH457 120040703A554012034100005 BRACKET EMB 145 EMB145LR 3260212SO RUDDER GROOVED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27299177606 145414 SHV - DURING C-CHECK THE RUDDER LOWER ACTUATOR FITTING WAS FOUND TO BE GROOVED. MAINTENANCE REMOVED THE UNDERSIZED BUSHING, OVERSIZED THE HOLE ON THE FITTING TO ACCEPT AN OVERSIZED BUSHING AND INSTALLED THE OVERSIZED BUSHING IAW EC5540-01029. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040720000682004072000068SO 2004 7 20 C2XA04SH458 120040705A531014524790629 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 66 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR CLIP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720000762004072000076 2004 7 20 RAIA00406026 420040625A3425 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03558HK 41071 3657 - BWI - RIGHT AHRS FAILED. MAINTENANCE RERACKED AHRS COMPUTER AND OPS CHECK OK. 2L72 4T RTA41NM 20040720000792004072000079 2004 7 20 RAIA00407005 420040711A34207003360948 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU AHRS MALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03558HK 41071 FIRST OFFICERS EFIS TUBES TUMBLED. SWAPPED NR 1 AND NR 2 SYMBOL GENERATORS FOR TROUBLESHOOTING. REMOVED AND REPLACED NR 2 AHARS IAW J41 MM 34-25-05, OPS CHECKED GOOD. SHOOK WIRES AT AHARS UNIT AND SYMBOL GEN NR 2 OPS OK. 2L72 4T RTA41NM 20040720000812004072000081EU 2004 7 20 RAIA00406018 120040620A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU LEFT MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03558HK255 41071 3637 - PIT - LEFT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED LEFT STARTER GENERATOR. 2L72 4T RTA41NM 20040720000832004072000083WP 2004 7 20 AALA20040723 120040713A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21296AA 49308 ORD - EMERGENCY CEILING LIGHTS BETWEEN ROWS 18 AND 21 INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR EMERGENCY CEILING LIGHTS BETWEEN ROWS 18 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000872004072000087SO 2004 7 20 C2XA04SH435 120040703A531014525376003 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000892004072000089SO 2004 7 20 C2XA04SH437 120040702A531014525376007 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000922004072000092SO 2004 7 20 C2XA04SH440 120040628A531014530634003 BUTTSTRAP EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000942004072000094SO 2004 7 20 C2XA04SH434 120040630A531514521700005 FLOORBEAM EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 2, FIG 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000962004072000096SO 2004 7 20 C2XA04SH444 120040708A532014522178005 SILL EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SERVICE DOOR LOWER THRESHOLD WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE RETURNED TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720001372004072000137SO 2004 7 20 C2XA04CL074 120040717A3397SP9220 WIRE EMB 145 EMB145ER 3260211SO EXIT LIGHT DAMAGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713935 145022 CLE FLIGHT 2150 THE CREW REPORTED THE RIGHT FORWARD PARTITION EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED SPLICE SP9220. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040720001392004072000139NM 2004 7 20 AALA20040712 120040707A3350 LIGHT BOEING737 737823 13844BZNM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21918AN 29519 BOS - EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040721000012004072100001EU 2004 7 21 04FDEA02053 120040712A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 MAIN CARGO COMPT RIGHT NR 5 SEAT TRACK BETWEEN FR 45 AND FR 54 HAS CORROSION AT FR 48.7, 50.8, 53, 53.6 AS MARKED. REPAIRED SEAT TRACK IAW A300-600 SRM 53-10-16 PARA 5.0 FIG 205. 2L72 4F RTA35EU 20040721000102004072100010EU 2004 7 21 SIMA200415414 120040519A57307075T6 SKIN SAAB SF340 340B 7860101EU RT WING CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 DURING A MBV INSPECTION OF THE RIGHT WING TO NACELLE FILLET AREA THE INBOARD SIDE WAS FOUND TO BE CHAFED. BLENDED CHAFED AREA. PERFORMED AND EDDY CURRENT INSPECTION OF BLENDED AREA. NO CRACKS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. WORK DONE IAW SAAB 340 SRM, (72LKS 3079, REV 43) 54-10-10 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040721000122004072100012EU 2004 7 21 SIMA200415408 120040520A53117252814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE13560 340B388 DURING AN MBV INSPECTION, THE UPPER FLANGE OF FRAME 272 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE EMERGENCY BATTERY PACK MOUNTING BRACKET TO ACCESS THE REPAIR AREA. COMLETELY REMOVED THE CORROSION BY CREATING A 2.5 INCH CUTOUT OF THE UPPER FLANGE. FABRICATD A REPAIR ANGLE AND FILLER AND SHIMS. REPAIR DONE IAW SAAB SRM, 72LKS 3079 REV 43, 53-70-30 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040721000142004072100014EA 2004 7 21 2004F00179 120040604A2420 IDG CNDAIRCL600 CL6002B16 1900305EA NR 1 ENGINE FAILED A O2GAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 NE03601BE 5103 IN FLIGHT AT CRUISE ALTITUDE GENERATOR NR 1 TRIPPED OFF LINE. GENERATOR NR 2 ABSORBED ELECTRICAL LOAD AND REMAINED WITHING NORMAL PARAMETERS. AIRCRAFT WAS DIVERTED TO CYUL FOR MAINTENANCE. NR 1 IDG WAS REPLACED WITH A REPAIRED UNIT. (M) 2L72 4F RTA21EA 20040721000202004072100020WP 2004 7 21 AMTA200400580 120040521A2731 CONTROL CABLE LKHEED1011 1011385115 5265015WP PITCH TRIM ICED A AMTAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL11194AT 193B1230 AT CRUISE FL340, AUTOPILOT LIMIT ANNUNCIATED. UNABLE TO PITCH TRIM WITH ELECTRIC OR MANUAL. AP COUPLED NO OTHER INOPERATIVE/FAIL OR PUSH INDICATIONS. UNABLE TO PITCH TRIM DURING DESCENT THROUGH LANDING. FOUND PITCH TRIM CABLES AND PULLEYS, RIGHT SIDE HAD ICE JUST AFT OF PRESSURE BULKHAD. ICE HAD FORMED FROM LEAK AT AFT NR 4 LAV SINK ONTO CABLES IN C3 PIT AFT BULKHEAD. TRIM OPERATES NORMAL, NORMAL WHEN ICE REMOVED. REPAIRED DRAIN LEAK. LUBED CABLES. (M) 2L73 4F A23WE 20040721000382004072100038NM 2004 7 21 USAASB04027 120040310A29101U1234 VALVE BOEING737 7373B7 1384580NM TAIL COMPT CRACKED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19374US 22953 CREW REPORTED LOSING SYSTEM A-HYDRAULICS ON TAKEOFF AS LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY INDICATED ZERO. FLT LEVELED OFF AT 5,000 FEET TO COMPLETE QUICK REFERENCE HANDBOOK PROCEDURES, THEN THE FLIGHT RETURNED TO FIELD AT BNA. UPON LANDING, THE LANDING GEAR WAS PINNED AND THE AIRCRAFT WAS TOWED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 FEEL ACTUATOR ISOLATION VALVE IN THE TAIL COMPARTMENT CRACKED AND LEAKING. REMOVED AND REPLACED VALVE PER MM 27-31-87. ALSO, REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP (P/N 65075-06) FOR LEAKING PER MM 29-15-12. REPLACED ASSOCIATED FILTERS AND SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. (M) 2L72 4F RTA16WE 20040721000432004072100043EU 2004 7 21 2004F00185 120040511A5310 STRUCTURE AIRBUS320 A320233 3930329EU FUSELAGE VIBRATION A RJEFA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO23477TA 1113 DURING CRUISE, AIRCRAFT DIVERTED TO MIAMI, DUE PILOT REPORTED MODERATED STRUCTURAL VIBRATION. THE AIRCRAFT LANDED WITHOUT ANY OTHER DISCREPANCY, AND STILL ON GROUND FOR MAINTENANCE. (M) 2L72 4F RTA28NM 20040721000462004072100046EA 2004 7 21 A6WA200440077 120040610A32465010598 WHEEL CNDAIRCL600 CL6002B19 1900309EA NLG DAMAGED A A6WAO OTHER E VIBRATION/BUFFET LDLANDING 1 GL31468AW 7916 UPON LANDING, NOSEWHEEL MADE STRANGE NOISE, STOP ON TAXI WAY AND LEFT NOSEWHEEL MISSING BEARING AND ABOUT TO FALL OFF. REMOVED AND REPLACED NLG SLIDING MEMBER, PER AIRCRAFT AMM 32-21-30. ALL OPS CHECK NORMAL. REMOVED AND REPLACED BOTH NLG WHEEL ASSEMBLIES. (M) 2L72 4F RTA21EA 20040721000522004072100052NM 2004 7 21 2004F00186 120040513A1420 CONNECTOR BOEING727 727225 1384077NM RT WING DAMAGED A RYNAO OTHER N FALSE WARNING CLCLIMB 1 CE078878Z 21451 DURING CLIMB-OUT, THE NR 8 LEADING EDGE SLAT LIGHT ON THE FORWARD PANEL STAYED ILLUMINATED WHEN THE SLATS WERE RETRACTED. AIRCRAFT RETURNED TO SEATTLE AND LANDED WITHOUT INCIDENT. REPAIRED RECESSED PIN IN CONNECTOR AT NR 8 LEADING EDGE SLAT. (M) 2L73 4F A3WE 20040721000542004072100054SO 2004 7 21 SIMA200415301 120040529A335020131A CHARGER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21735TS 145386 DCA - FLT 4606 - EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT 9A. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY AND CHARGER IAW EMB 135 AMM CH 33-50-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040721000552004072100055NM 2004 7 21 AMTA200400052 120040116A7700 TUBE BOEING757 75733N 1384931NM LT ENGINE MISSING A AMTAO OTHER O OTHER CLCLIMB 1 GL11558TZ 32592 DURING CLIMB ABOVE FL180 ALL LT ENGINE INSTRUMENT INDICATORS BEGAN TO FLUCTUATE EPR FLUCTUATING BETWEEN 1.65 AND 1.5 EPR FOR APPROXIMATELY THREE MINUTES 94335. INSTALLED MISSING PROBE HEAD PER MM 77-11-04-8. PERFORMED ENGINE HIGH POWER TAKEOFF. ALL PARAMETERS NORMAL. (M) 2L72 4F RTA2NM 20040721000592004072100059 2004 7 21 P8UF200400002 420040713A221337570827 COMPUTER DOUG DC10 DC1030 3023501WP YAW DAMPER FAILED W P8UFA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO23831LA 46936 DURING CLIMB LOWER YAW DAMPER B-CHANNEL BECOMES INOPERATIVE. 2L73 4F A22WE 20040721000732004072100073WP 2004 7 21 04FDEA02057 120040712A7160AJC7415 SHROUD DOUG MD10 MD1010F 3022112WP NR 2 ENGINE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 AT C-CHECK AT BFM N/R N00504 WAS WRITTEN FOR THE NR 2 ENGINE LT SHROUD FAN COWL LAND BEING GOUGED. REMOVE AND REPLACE THE SHROUD IAW SRM 51-31-01. THE SHROUD PANEL WAS FABBED ON MAE TRAVELER T/4-442977. 2L73 4F RTA22WE 20040721000752004072100075WP 2004 7 21 04FDEA02015 120040707A5710ARC31024 BEAM DOUG MD10 MD1010F 3022112WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 RIGHT WING INBOARD AILERON LOWER BEAM CRACKED AT END. REMOVE TEE-CAP IAW DC10 SRM 51-35-01 VOL I, FABRICATED -4 TEE CAP IAW DCA DWG ARC 3012 AND DC10 SRM 51-10-01 FIG 13 VOL 3. TRIMMED, LOCATED, DRILLED AND DEBURRED -4 TEE CAP IAW DC10 SRM 57-31-01 VOL 2 AND DAC DWG ARC 3102. RE-ASSEMBLED TEE CAP IAW DAC DWG ARC 3102 AND DC10 SRM 51-31-01 VOL 2. INSTALLATION TO BE ACCOMPLISHED ON NR N00307. 2L73 4F RTA22WE 20040721000762004072100076WP 2004 7 21 04FDEA02016 120040707A5751 SKIN DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 RIGHT HAND WING INBOARD AILERON LOWER SKIN BULGED/CORRODED AND I EACH FASTENER POPPED. REMOVED AND REPLACED INBOARD AILERON LOWER SKIN PER FEDEX EA 8-5750-77595. REMOVE AND REPLACE LEADING EDGE SKIN PER FEDEX DC10-10 SRM 51-35-01 VOL 2. 2L73 4F RTA22WE 20040721000772004072100077WP 2004 7 21 04FDEA02071 120040714A5347 FLOORBEAM DOUG MD10 MD1010F 3022112WP ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 FLOORBEAM AT FUSELAGE STATION 1921, LBL 50, FOUND DAMAGED ON EDGE OF CUTOUT, AT CABLE LOCATION. COMPLIED WITH FEDEX EA 8-5310-77598, FUSELAGE STATION 1921, X=-50, FLOORBEAM LIGHTENING HOLE REPAIR. 2L73 4F RTA22WE 20040721000792004072100079EU 2004 7 21 04FDEA02074 120040714A5315 FLOORBEAM AIRBUS300 A300F4605R 3930327EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 FWD CARGO COMPT UPPER FLOORBEAM AT FR29 O/B OF 1ST SEAT TRACK FROM CENTER IS CRACKED. REF SNRM N00276. REMOVED DAMAGE, NO CRACK NOTED. INSTALLED REPAIR ANGLES, AND SHIM AND TREATED AND PRIMED, AND TOP COATED IAW A33/600 SRM 53-10-15 AND 51-75-10. 2L72 4F RTA35EU 20040721000802004072100080EU 2004 7 21 04FDEA02075 120040714A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 COMPT RT NR 2 SEAT TRACK BETWEEN FR45 AND 54 HAS CORROSION AT FR45, 46.2, 49, 53.8, 52. REF SNRM N00454. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW A 300/600 SRM 51-72-10. 2L72 4F RTA35EU 20040721000812004072100081EU 2004 7 21 04FDEA02076 120040714A5311A305300101 FRAME AIRBUS300 A300B4605R 3930308EU ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE FRAME 20A AT FWD CARGO PIT DOOR, FWD SIDE DENTED 4 X 2 X .125 INCH. CUT OUT DAMAGE AND REPAIRED IAW A300600 SRM 51-40-21 AND FED EX SRM 30-53-001. 2L72 4F RTA35EU 20040721000822004072100082NM 2004 7 21 04FDEA02077 120040714A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON STR 23R BS 740. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION OF STRINGER PER SRM 53-10-3. FABRICATED REPAIR PER SRM 53-10-3 FIG. 1. INSTALLED REPAIR ONS TR 23R BS 740 PER SRM 53-10-3 AND SRM 53-30-2. 2L73 4F RTA3WE 20040721000842004072100084EU 2004 7 21 04FDEA02073 120040714A5310 CROSSBEAM AIRBUS300 A300F4605R 3930327EU FUSELOAGE DEFORMED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 AFTER REMOVAL OF CLS ADAPTER AT FR65 BETWEEN LT SEAT TRACK 3 & 4. DEFORMATION OF CROSS BEAM FLANGE WAS FOUND TO BE AT .250 INCH, REF A300/600 SRM 53-10-15 FIG 205, MAX DEFORMATION IS .197 INCH, REF SNRM N00405. REPAIRED IAW FED EX EA 6-5310-80084. 2L72 4F RTA35EU 20040721000862004072100086WP 2004 7 21 04FDEA01888 120040630A5310 TEAR STRIP DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING P TO F MODIFICATION TRANSITION CHECK, AFTER REMOVAL SKIN IS NOTED 2EA TEAR STRIP WITH CRACK .50 INCH LONG STA 879 AND 899 BETWEEN L46 TO L48 RIGHT SIDE. FABRICATE A NEW TEAR STRIP (INCREASE LENGTH .10 INCH TO ENSURE 2DE MARGINE) IAW SRM 51-35-01. 2L73 4F A22WE 20040721000882004072100088WP 2004 7 21 04FDEA01890 120040630A5311 FRAME DOUG DC10 DC1030 3023501WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-01 VOL 2 AND DC10 SRM 51-35-01. 2L73 4F A22WE 20040721000892004072100089WP 2004 7 21 04FDEA01891 120040630A5330 SKIN DOUG DC10 DC1030 3023501WP ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER IS DENTED AT FS 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL I PAGE 6116 NR 2. FABRICATED REPAIR COMPONENTS IAW DC10 SRM 53-20-00 FIG 6 VOL 2 AND DC10 SRM 53-33-01 VOL 3 FIG 2 AND DC10 SRM 51-20-01 VOL 2, INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-41-01 VOL 2 AND DC10 SRM 51-33-01 VOL 2. 2L73 4F A22WE 20040721000902004072100090WP 2004 7 21 04FDEA01892 120040630A5797 WIRE HARNESS DOUG DC10 DC1030 3023501WP ZONE 600 ARCED A FDEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO25323FE 47811 RT WING INSIDE NR 3 FUEL TANK THRU ACCESS PANEL NR 634 AT FUEL PROBE WIRE HARNESS HAS CUT WIRE WITH EVIDENCE OF ARCING, LOCATED JUST BELOW ACCESS PANEL. REMOVED AND REPLACED WIRE BUNDLE IAW DC10 MM 20-30-01-2. 2L73 4F A22WE 20040721000912004072100091WP 2004 7 21 04FDEA01893 120040630A5720 RUB STRIP DOUG DC10 DC1030 3023501WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 LEFT WING FUEL PANEL 536DD LANDING RUB STRIP HAS CORROSION AND PITTING LOWER WING. REMOVED CORRODED RUB STRIP IAW DC10 SRM 51-35-01 VOL 2. FOUND LANDING CORRODED, TRIMMED OUT CORRODED AREA AND FABRICATED EXTERNAL DOUBLER, INTERNAL DOUBLER, 2 EACH SHIMS AND FILLERS IAW DC10 SRM 57-10-00 VOL I. INSTALLED REPAIR COMPONENTS IAW DC10 SRM 57-10-00 VOL I. INSTALLED RUB STRIP AND GANG CHANNEL IAW DC10 SRM 51-35-01 VOL 2 AND 51-42-04 VOL 2. 2L73 4F A22WE 20040721000922004072100092WP 2004 7 21 04FDEA01894 120040630A5753ARC142925 BRACKET DOUG DC10 DC1030 3023501WP ZONE 600 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND OUTBOARD FLAP INBOARD HINGE HAS A BROKEN BRACKET PART NUMBER ARC 2149-25. DISASSEMBLED HINGE PANEL STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. REMOVED BROKEN BRACKET IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW BRACKET IAW DAC DWG ARC 2149. INSTALLED BRACKET IAW DC10 SRM 51-35-01 VOL 2, RE-ASSEMBLED STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. 2L73 4F A22WE 20040721000932004072100093SO 2004 7 21 C2XA04IA081 120040702A4900792254 ROTARY SWITCH EMB 135 EMB135LR 3260305SO COCKPIT INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2714516 145323 IAH - FLIGHT 3407, DURING CLIMBOUT OF IAH THE CREW REPORTED AN EMERGENCY ELECTRICAL ABNORMAL TRANSFER CAUTION INDICATION, APU AUTO-SHUTDOWN IN FLIGHT, AND EMERGENCY LIGHTS ON. THE CREW RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY SWITCH, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040721000942004072100094WP 2004 7 21 04FDEA02101 120040717A5730ANB71702 PLATE DOUG DC10 DC1030 3023501WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 FUSELAGE RT BASE PLATE INBOARD FLAP SUPPORT SURFACE CORROSION REPAIR P/N ANB7170-2. COMPLIED WITH EA 8-5310-80573. 2L73 4F A22WE 20040721000952004072100095WP 2004 7 21 04FDEA02102 120040717A5753 SUPPORT DOUG MD10 MD1010F 3022112WP TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 COMPLY WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT OUTBOARD FLAP. COMPLIED WITH EA 8-5750-80574 WINGS FLAP VANE SUPPORT CORROSION REWORK ON RIGHT O/B FLAP. 2L73 4F RTA22WE 20040721000962004072100096GL 2004 7 21 04FDEA02103 220040718A7200 ENGINE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 3 STALLED A FDEAE ENGINE SHUTDOWN JRYWARNING INDICATION PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CRCRUISE 1 SO25560FE68025 46938 451184 AT FL330, SELECTED ENGINE AND WING ANTI-ICE ON, ENGINE 3 ANTI-ICE DISAGREE AND COMPRESSOR STALL AT SAME TIME. N1 ROLLED BACK TO 67 PERCENT. RAN COMPRESSOR STALL CHECKLIST. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN APPROXIMATELY 1+05 FLIGHT TIME REMAINING (WINDMILLING). 2L73 4F4 FRTA22WE E23EA 20040721000972004072100097NM 2004 7 21 04FDEA02104 120040718A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040721000992004072100099NM 2004 7 21 04FDEA02092 120040716A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 MECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442, STR 6L. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER 6L BS 442 I.A.W. BOEING 727 SRM 53-10-3 FIG 3. 2L73 4F RTA3WE 20040721001002004072100100NM 2004 7 21 04FDEA02093 120040716A5321 FLOOR PANEL BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON FLOOR WEB BS 620, LBL 48-55, WL 208, AND ELONGATED FASTENER HOLES. COMPLIED WITH FED EX E.A. 7-5310-70670 ON THE 620 FLOORBEAM LBL 48-55 WL 208. 2L73 4F RTA3WE 20040721001022004072100102NM 2004 7 21 04FDEA02095 120040716A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 FWD CARGO COMPARTMENT, STR 21 LT BS 488 IS CRACKED. REMOVED DAMAGE PORTION OF STR 21 LT, BS 488. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20040721001042004072100104WP 2004 7 21 04FDEA02097 120040717A5740ARC0318502 FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25359FE 46635 C/W EA 8-5740-79557 WINGS RIGHT AILERON SUPPORT ASSY CORROSION REPAIR P/N ARC0317- 502. COMPLIED WITH EA 8-5740-79557. 2L73 4F RTA22WE 20040721001052004072100105WP 2004 7 21 04FDEA2099 120040717A5740NRC6041503 FITTING DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 C/W EA 8-5750-79553 WINGS OUTBOARD AILERON, ACTUATOR ATTACH FITTING REWORK. COMPLIED WITH EA 8-5750-79553. 2L73 4F RTA22WE 20040721001072004072100107NM 2004 7 21 04FDEA01905 120040701A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.628. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED. 2L73 4F RTA22WE 20040721001092004072100109NM 2004 7 21 04FDEA01906 120040701A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.620. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RT OUTBOARD FLAP - SUPPORTS CORRODED 2L73 4F RTA22WE 20040721001102004072100110NM 2004 7 21 04FDEA01907 120040701A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.458, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED 2L73 4F RTA22WE 20040721001132004072100113EU 2004 7 21 04FDEA02060 120040713A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 AFT CARGO LEFT SIDE FLOORBOARD SUPPORT CROSS MEMBER HAS EXFOLIATION CORROSION AT FRAME 60. CUT DAMAGED SECTION IAW A310-200 SRM 53-10-15, VERIFIED MAT'L TO FAB, FABBED REPAIR ANGLE AND FILLER, LOCATED, DRILLED DEBURRED AND COUNTERSUNK IAW A310 SRM 51-40-44. TREATED, PRIMED AND TOP COATED IAW A310 SRM 51-23-22. INSTALLED REPAIR ANGLE IAW SRM 53-10-15. 2L72 4F RTA35EU 20040721001152004072100115EU 2004 7 21 04FDEA02062 120040713A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 ZONE 252, SEAT TRACK 2 RIGHT 4 INCHES AFT OF FR 72 HAS CORROSION ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK SECTION PER A310 SRM 53-10-16. 2L72 4F RTA35EU 20040721001172004072100117EU 2004 7 21 04FDEA02064 120040713A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MDC, SEAT TRACK L3 AT FRAME 16 AND GOING FWD 16 INCHES HAS MODERATE LEVEL 2 SURFACE CORROSION. SEAT TRACK FR 16 L3 OUT OF LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-21. SEAT TRACK FABRICATION WAS ACCOMPLISHED ON N00428. 2L72 4F RTA35EU 20040721001192004072100119EU 2004 7 21 04FDEA02066 120040713A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 UPPER MAIN CABIN ZONE 220 AT Y1959, FR14 TO 15A TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-40-20. 2L72 4F RTA35EU 20040721001202004072100120EU 2004 7 21 04FDEA02067 120040713A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MDC, LATERAL SEAT RACK AT FR 45 BETWEEN SEAT TRACKS R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20040721001232004072100123NM 2004 7 21 SWAA042032 120040718A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29732SW 27864 DURING SCHEDULED C1 CHECK, EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PER MM. 2L72 4F RTA16WE 20040721001262004072100126NM 2004 7 21 SWAA042035 120040717A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 797, STRINGER 18L, BS 767, 18L, BS 797, STRINGER 19L, CRACKED. REPAIRED SKIN PER EA & SRM. 2L72 4F RTA16WE 20040721001272004072100127NM 2004 7 21 SWAA042036 120040717A53306516352 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 475, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040721001282004072100128NM 2004 7 21 SWAA042038 120040719A335010107451 SIGN BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 FWD ENTRY DOOR EMERGENCY EXIT SIGN COVER BROKE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSEMBLY PER MM. 2L72 4F RTA16WE 20040721001292004072100129NM 2004 7 21 SWAA042023 120040718A5230BAC1505100022 STRUCTURE BOEING737 7375H4 138449DNM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR LOWER T-CHORD, CRACKED. REMOVED AND REPLACED T-CHORD PER SRM. 2L72 4F RTA16WE 20040721001302004072100130 2004 7 21 SWAA042024 420040718A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040721001312004072100131NM 2004 7 21 SWAA042025 120040718A57536573732 SKIN BOEING737 7372T4 1384492NM RT WING TE FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 RIGHT WING OUTBOARD T/E FLAP CRACKED. REPAIRED RIGHT OUTBOARD T/E FLAP PER EA. 2L72 4F A16WE 20040719001212004071900121EA 2004 7 19 SWIA200413568 120040519A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07595SW 7292 INTERCOSTAL CLIP ON RT SIDE AT FS 484 RBL 29 CRACKED. LOCATED UNDER FLOOR PANEL 262DRF. REMOVED CRACKED CLIP, INSTALLED NEW CLIP 601R31171-9 IAW CRJ 200 REO 6501R-53-41-059. 2L72 4F RTA21EA 20040719001242004071900124EA 2004 7 19 SWIA200413571 120040712A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AILERONS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07590SW 7077 AILERON TRIM WILL SOMETIMES NOT MOVE TO THE RIGHT. REMOVED AND REPLACED AILERON/RUDDER TRIM PANEL IAW MM 27-12-10, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040719001302004071900130NM 2004 7 19 SWAA042001 120040715A575465C26603 SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND LT WING NR 3 L/E SLAT WEDGE OUTBOARD UPPER END, DELAMINATED. REPAIRED LT WING NR 3 L/E SLAT PER SRM. 2L72 4F RTA16WE 20040719001372004071900137NM 2004 7 19 SWAA041989 120040714A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 730, STRINGER 14L, CRACKED. REPAIRED SKIN SECTION PER SRM. 2L72 4F A16WE 20040719001422004071900142 2004 7 19 SWAA041994 420040714A25656949956 CABLE BOEING737 7373L9 1384470NM L2 DOOR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM. 2L72 4F RTA16WE 20040719001492004071900149SO 2004 7 19 SWIA200413544 120040626A2710 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO ELEVATOR OUT OF ADJUST A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07271YV ON FFOD CHECKS NO TRIM AURAL WARNING. REPAIRED WIRING AT ELEVATOR TRIM PROX SENSORS AND ADJUSTED PER MM. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040719001632004071900163NM 2004 7 19 DL757040619 120040701A5330141N33131 SKIN BOEING757 757232 1384965NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27605DL 22812 INSPECTION OF THE FWD UPPER CORNER OF THE L1 DOOR CUTOUT PER AD 2004-09-32, REVEALED A SMALL CRACK IN THE SKIN. THE CRACK WAS REMOVED WITH A 1 INCH CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 091537-14AD, REV A. 2L72 4F RTA2NM 20040719001792004071900179NM 2004 7 19 151AW0010 120040702A5320 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 SUPPORT ANGLE CRACKED AT BS 807 FRAME RIGHT BUTTOCK LINE 22. REPLACED SUPPORT ANGLE PER SRM 51-10-2. 2L72 4F RTA16WE 20040719002162004071900216EU 2004 7 19 USAA040274 120040603A5320D5347217220390 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND FLOOR SUPPORT FRAME CORRODED, 2 INCHES LONG BY .900 INCH WIDE BY.032 INCH DEEP, FRAME 66-68, -Y1192 TO -Y1292, -Z240. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-14. CORROSION LEVEL 2, TASK NR JA-260-5300. (M) 2L72 4F RTA28NM 20040719002302004071900230EU 2004 7 19 USAA040271 120040602A5347D5311281520200 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND TRACK CORRODED .85 INCH BY .75 INCH BY .36 INCH DEEP, MAIN DECK FLOOR SUPPORT, FRAME 16, Y 1292. REMOVED AND REPLACED TRACKS PER SRM 53-11-14. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040719002422004071900242EU 2004 7 19 USAA040334 120040610A5347D5311278220201 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY 1 INCH BY .026 INCH AREA, FS 24, BL -Y1292, -Z-240. REPLACED WITH NEW PART PER SRM 53-00-15. CORROSION LEVEL 2, TASK NR JA-220-53500. (M) 2L72 4F RTA28NM 20040719002452004071900245EU 2004 7 19 USAA040315 120040608A5330D5311254700600 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19710UW16211 1019 BFM - FOUND PLATE CORRODED .075 INCH BY .050 INCH BY .040 INCH DEEP, FS 16, Y1970, -Z40. REMOVED AND REPLACED PLATE ASSEMBLY. (M) 2L72 4F RTA28NM 20040721001332004072100133NM 2004 7 21 SWAA042027 120040718A335007912 COVER BOEING737 7375H4 138449DNM CABIN DAMAGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29506SW 24183 EEPLS COVER AT ROW 1 ABC, DISCOLORED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040721001342004072100134 2004 7 21 SWAA042028 420040718A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C3 CHECK, FOUND L2 & R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 & R1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040721001352004072100135NM 2004 7 21 SWAA042029 120040718A534065C346701 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM. 2L72 4F RTA16WE 20040721001372004072100137NM 2004 7 21 SWAA042040 120040718A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED C3 CHECK, FOUND BEAR STRAP AT BS 294.5, STRINGER 10L, CRACKED. REPAIRED BEAR STRAP PER EA. 2L72 4F RTA16WE 20040721001402004072100140NM 2004 7 21 SWAA042042 120040719A53306545778 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT LOWER FWD CORNER, CRACKED. REPAIRED AFT ENTRY DOOR CUTOUT PER EA. 2L72 4F RTA16WE 20040721001412004072100141NM 2004 7 21 SWAA042043 120040719A53126545409 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20040721001442004072100144NM 2004 7 21 SWAA042046 120040717A53146562125 KEELBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED C2 CHECK, FOUND LT AND RT KEEL BEAM AT RT BS 540, GROUND A/C DUCT CENTERLINE, CORRODED. REPAIRED RT & LT KEEL BEAM CHORDS PER EA. 2L72 4F RTA16WE 20040721001452004072100145NM 2004 7 21 SWAA042047 120040717A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040721001462004072100146 2004 7 21 SWAA042048 420040719A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040721001512004072100151 2004 7 21 AALA20040725 420040621A25655A33073 SLIDE BOEING737 737823 13844BZNM SERVICE DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21916AN 29517 FORWARD SERVICE ENTRANCE SLIDE DID NOT INFLATE WHEN DROPPED. MANUALLY PULLED FOR INFLATION. REPLACED SLIDE FOR FORWARD SERVICE ENTRANCE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040721001532004072100153SO 2004 7 21 SWIA200413546 120040702A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 AFT OVERHEAD POD LIGHT INOP IN MAIN CABIN. REPLACED BULB IN AFT EMERGENCY LIGHT IN MAIN CABIN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040721001562004072100156EA 2004 7 21 SWIA200413549 120040706A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07912SW 7595 UPON TAXI TO RUNWAY SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. REMOVED AND REPLACED THE LEFT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF MAL-5805. 2L72 4F RTA21EA 20040721001582004072100158SO 2004 7 21 RAIA00407009 120040709A5270 WARNING LIGHT EMB 145 EMB145 3260210SO SERVICE DOOR ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03821HK 145068 SERVICE DOOR OPEN WARNING MSG ILLUMINATION. DEFERRED SERVICE DOOR 52-70-00-1. SUBSEQUENTLY CLEARED DMI BY CLEANING DOOR WARNING SWITCHES. 2L72 4F RTT00011AT 20040721001672004072100167EU 2004 7 21 USAASA04013 120040208A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU PAX CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19727UW 1147 DCA- THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT LATCHED FOR AN INTERNAL LIGHT FAULT. MAINTENANCE REPLACED THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040721001702004072100170 2004 7 21 WRLA200403 420040106A256524D3005331 SLIDE DOUG DC10 DC1030 3023501WP LEFT FWD DOOR FAILED A WRLAK NONE O OTHER ININSP/MAINT 1 EA27526MD 46998 DURING ROUTINE DEPLOYMENT CHECK OF L1 DOOR SLIDERAFT PER WORLD TASK CARD 101C-022, TIMCO W/O 107021, THE SLIDE RAFT DEPLOYED INWARD AS THE DOOR WAS APPROXIMATELY HALF OPEN. THE SLIDE DID NOT FALL OUT OF THE DOOR OPENING AS DURING NORMAL DEPLOYMENT. REMOVED AND REPLACED SLIDE/RAFT ASSEMBLY. (M) 2L73 4F A22WE 20040721001752004072100175NM 2004 7 21 UIEA200400020 120040219A5410 STRUT BOEING747 747243B 1384830NM NR 4 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING ZONAL INSPECTION IT WAS DISCOVERED THE NR 4 ENGINE PYLON STRUT PRECOOLER EXHAUST VENT WITH CRACKS ON THE RIGHT SIDE OF THE STRUT. THE REPAIRS WERE MADE ON THE RIGHT SIDE OF THE STRUCT STRUCTURE ASSEMBLY. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO STATION 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F A20WE 20040721001762004072100176NM 2004 7 21 HALA0400211 120040209A5311991183915 FRAME BOEING717 717200 1383700NM FUSELAGE CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13485HA 55130 HNL - DURING A 1A/1C4 CHECK, A 1.75 INCH CIRCUMFERENTIAL CRACK WAS FOUND ON THE CANTED FRAME REAR SPAR BULKHEAD STATION 1178.225 BELOW LONGERON 17L, IN THE CAP'S FORWARD FLANGE P/N 9911839-15. ACCOMPLISHED REPAIR PER HAL M105 FILE 485031. REMOVED AND INSTALLED UPPER LEG OF DOUBLER, SINGLE ROW 5. (M) 2L72 4F TRA6WE 20040721001782004072100178NM 2004 7 21 TSAA0452026 120040204A53106520722 DOOR FRAME BOEING737 73725A 1384481NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13819AL 23791 FOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 46, DETAIL II. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040721001802004072100180NM 2004 7 21 TSAA0433024 120040116A3350100679 BATTERY PACK BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 REPLACED FORWARD SERVICE DOOR IDENT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 20040721001812004072100181NM 2004 7 21 TSAA0433027 120040209A335086210151 BATTERY PACK BOEING737 737209 13844AENM PAX CABIN INOPERATIVE A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 REPLACED FORWARD SERVICE DOOR IDENT EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040721001922004072100192EA 2004 7 21 A6WA20044006 120040113A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31404UW 7294 RIVET ON RIGHT FUSELAGE SKIN AT FS 265 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSKINK HOLE IN SKIN. REMOVED FASTENER, ENLARGED FASTENE HOLE TO A NOMINAL .1875 INCH DIAMETER, PERFORMED EDDY CURRENT TO ENSURE NO CRACKS EXISTED AND DAMAGED WS REMOVED. INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578. (M) 2L72 4F RTA21EA 20040721001932004072100193EA 2004 7 21 A6WA200440007 120040113A5610NP1393225 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31432AW 7257 AT 33,000 FEET, LEFT SIDE WINDOW SHATTERED 'PRESSURIZATION SPIKED DOWN 500 FEET THEN STABILIZED. AIRCRAFT EN ROUTE FROM ICT TO ATL. REMOVED AND REPLACED LEFT SIDE WINDOW PER AMM 56-12-01. (M) 2L72 4F RTA21EA 20040721001952004072100195WP 2004 7 21 MEX2004049 120040206A3213592060211 STRUT DOUG DC9 DC987 3022087WP NLG DISCHARGED A ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW231075T 49724 FLT 253 - GDL-MEX - DURING TRANSIT CHECK, THE NOSE LANDING GEAR STRUT WAS FOUND COMPRESSED WITHOUT NITROGEN PRESSURE. THE NLG STRUT SEALS WERE REPLACED IAW MM 32-31-02 AND AN AJUSTMENT TO THE GROUND SENSING CONTROL MECHANISM WAS PERFORMED IAW MM 32-23-01, TESTS CORRECT. AT MEX, THE NLG STRUT CONTINUE WITH HYDRAULIC LEAKAGE. DURING OVERNIGHT SERVICE, THE NLG STRUT SEALS WERE REPLACED IAW MM 32-21-02, GROUND SENSING CONTROL MECHANISM AS VERIFIED IAW 32-23-01, EXTENSION AND RETRACTION TESTS AND LUBRICATION WERE PERFORMED IAW MM 32-30-00 AND 12-21-04, ALL CORRECT. THE NLG STRUT WAS REPLACED AND SYSTEM TESTED IAW MM 32-21-02, ALL CORRECT. (M) 2L72 4F RTA6WE 20040722000042004072200004NM 2004 7 22 USAABB04003 120040102A33508731002511REV15 LIGHT BOEING757 7572B7 1384964NM R1 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19619AU 27198 CLT - FOUND EXIT IDENTIFIER AT R1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2L72 4F RTA2NM 20040722000052004072200005NE 2004 7 22 2004F00189 220040617A7200 LINE LEAR 25 25B 5170511CE GE CJ610 CJ610* 30006NE JET PUMP LOOSE A CEDAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW058005Y 121 WHILE EN ROUTE FROM MFE-LIT, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PERIMETERS. THE FLIGHT CREW DECIDED TO DIVERT TO ADS AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION MAINTENANCE CREW FOUND A LINE LOOSE ON THE PRESSURIZATION JET PUMP. (M) 2L72 4J4 J A10CE 1E16 20040722000092004072200009CE 2004 7 22 2004F00190 120040604A291399146142 MOTOR CESSNA750 750 2076810CE RUDDER SYSTEM FAILED A UG8AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL235113 7500013 AFTER THE MAIN ENGINES WERE STARTED, THE 'RSS SYSTEM FAIL' MESSAGE WAS DISPLAYED. AN ALTERNATE AIRCRAFT WAS UTILIZED FOR THAT TRIP. THE RUDDER STANDBY SYSTEM PUMP/MOTOR WAS NOTICED TO BE SLOW AND NOISY. SMOKE WAS ALSO COMING FROM THE MOTOR. THE RSS PUMP/MOTOR WAS REPLACED WITH A SERVICEABLE UNIT. OPERATION OF THE SYSTEM WAS NORMAL. (M) 2L72 4J RTT00007WI 20040722000102004072200010NM 2004 7 22 GAIA04080OP 120040616A278226900273 ACTUATOR BOEING727 7272J0 138407ENM NR 2 SLAT INOPERATIVE A GAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07281KH 21105 FLT 716 - FWA-PHX - ON DEPARTURE AFTER RETRACTING FLAPS NOTED NR 2 LED DID NOT RETRACT, PROCEEDED TO CHECK LIST. RETURNED TO FWA WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND NR 2 L/E SLAT ACTUATOR INOPERATIVE. REMOVED AND REPLACED ACTUATOR. OPS CHECK GOOD. NO LEAKS NOTED PER MM CH 24-81. PERFORMED OVERWEIGHT LANDING INSPECTION WORK CARD NR BH-059615. NO DEFECTS NOTED. AIRCRAFT IS SAFE FOR FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040722000192004072200019NM 2004 7 22 USAASB04007 120040109A2130189929 SENSOR BOEING737 7374B7 1384702NM CABIN PRESSURE OUT OF TOLERANCEA USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19443US 24842 CLT - FLT 1244 - ON CLIMB-OUT FROM CLT, EN ROUTE TO MCO, AT FL200, THE CABIN ALTITUDE WARNING HORN SOUNDED AS CABIN ALTITUDE INDICATED 10,000 FT. AUTO AND STANDBY PRESSURIZATION MODES DID NOT IMPROVE THE SITUATION. CREW SWITCHED TO MANUAL PRESSURIZATIO MODE AND WAS ABLE TO GAIN CONTROL OF CABIN PRESSURE AS AIRCRAFT DESCENDED TO 10,000 FT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THAT THE AIRCRAFT REMAINED IN THE GROUND MODE WHILE IN FLIGHT. FOUND THE S105 AIR/GROUND SENSOR RESISTANCE OUT OF TOLERANCE. REMOVED AND REPLACED S105 SENSOR PER MM 32-09-01. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040722000232004072200023EU 2004 7 22 2004F00200 120040321A3234A23870101 SELECTOR SWITCH AMD FALC20FALCON 2720302EU LT MLG OUT OF ADJUST A CEDAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05207CA 153 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. FLIGHT CREW NOTIFIED TOWER AND LANDED WITHOUT INCIDENT. (M) 2L72 4F A7EU 20040722000292004072200029EU 2004 7 22 USA2004F00087 120040617A5330 SKIN AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FOUND DENT IN FUSELAGE SKIN, 2.5 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040722000312004072200031CE 2004 7 22 JEM2004F00000 120040622A5511 RIB BEECH MU300 400A 1155402CE PWA JT15 JT15D4 52112NE HORIZONTAL STAB CRACKED B JEMRK NONE O OTHER ININSP/MAINT 1 CE018167Y RK67 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB ON THE RT SIDE AND THE RIBS WERE CRACKED. THE INITIAL INSPECTION WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE ADJACENT THE SIDE ROLLERS. THE FOLLOWING PARTS WERE CHANGED PN45A21046-6 RIB, 45A21086-4, AND 45A21085-4 BRACKETS. 2H72 4F4 FRTA16SW E1NE 20040722000362004072200036NM 2004 7 22 USAA040202 120040420A7120 FAIRING BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE ENGINE STRUT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19375US 22954 PIT, ENGINE STRUT FAIRING, 1 INCH CRACK, FWD LT MOUNT HOLE NAC STA 279.50. REMOVED DEFECTIVE PART, WELDED AND REINSTALLED. 2L72 4F4 FRTA16WE E2GL 20040722000372004072200037GL 2004 7 22 UIEA200400118 220040628A73209378M27PO1 GASKET BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 4 ENGINE DAMAGED G UIEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15412MC 30559 706125 DURING CRUISE ENGINE SHUT DOWN DUE TO FUEL IMBALANCE. POSSIBILITY OF A FUEL LEAK NR 4 ENGINE. FUEL IMBALANCE BETWEEN MAIN NR 1 TANK, AND MAIN NR 4 TANKS. FUEL ENROUTE WAS 1.3 TO 1.4 TOTALIZER 22.6 WHILE CALCULATED 25.6, LEAK COULD BE DOWN STREAM OF FUEL CONTROL UNIT NR 4. LEAK CONFIRMED VISUALLY. ACCOMPLISHED ENGINE SHUT DOWN. REMOVED NR 4 ENGINE HMU CHECK FOUND GASKET SEAL BROKEN; REPLACED GASKET AND INSTALLED HMU IAW MM. PERFORMED ENGINE WET MOTOR TEST ECU ACTUATOR GROUND TEST 12. IDLE AND ENGINE RUNUP LEAK CHECK NORMAL. 2L74 4F4 FRT1384945 E23EA 20040722000412004072200041CE 2004 7 22 JEM2004F00002 120040617A551045A211465 BRACKET BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2H72 4F4 FRTA16SW E1NE 20040722000432004072200043NM 2004 7 22 USA2004F00092 120040609A2424915F2125 GCU BOEING737 7373B7 1384580NM NR 2 ENG GEN FAILED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19504AU477807966 23379 ENROUTE, CREW REPORTED THE G-3 PANEL CIRCUIT BREAKER OPENED IN FLIGHT. AN ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT PRIOR TO THE OPENING OF THE CIRCUIT BREAKER. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE GENERATOR CONTROL UNIT. ENGINE RUN AND OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20040722000442004072200044NM 2004 7 22 USA2004F00095 120040524A3230BACV10BT1 CHECK VALVE BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE RT MLG WW CONTAMINATED A USAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA19352US 23555 ON APPROACH, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED AND THAT THE RT MLG WOULD NOT EXTEND. TOWER CONFIRMED THAT THE RT MLG WAS NOT DOWN. CAPTAIN EXTENDED THE RT MLG MANUALLY USING THE ALTERNATE GEAR EXTENSION PROCEDURES. GEAR FELL AND LOCKED INTO PLACE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND DEBRIS IN CHECK VALVE UPSTREAM OF UNLOCK PORT OF RT MLG UPLOCK ACTUATOR. REPLACED CHECK VALVE. ALSO, REMOVED AND REPLACED RT MLG HYDRAULIC MODULE AND LOCK ACTUATOR FOR TROUBLESHOOTING PURPOSES. REMOVED AND REPLACED HYDRAULIC SYSTEM A AND B RETURN FILTERS. NO CONTAMINATION NOTED. PERFORMED SATISFACTORY GEAR SWING. OPS CHECK AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040722000502004072200050EU 2004 7 22 SDR2004038 120040601A3240215493 BRAKE ASSY AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RT MLG WORN A TRBAO OTHER O OTHER TXTAXI/GRND HDL 1 SO21141AE 141 WHEN APPLYING BRAKING ACTION AN UNUSUAL NOISE COMES FROM RT BRAKES. REPLACED IB AND OB BRAKES ASSEMBLIES. 2H72 4T4 TRTA53EU E20NE 20040722000542004072200054CE 2004 7 22 JEM2004F00001 120040617A551045A211466 BRACKET BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2H72 4F4 FRTA16SW E1NE 20040722000562004072200056CE 2004 7 22 JEM2004F00004 120040617A551145A210864 RIB BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE HORIZONTAL STAB CRACKED B JEMRK NONE O OTHER ININSP/MAINT 1 CE01250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2H72 4F4 FRTA16SW E1NE 20040722000572004072200057NM 2004 7 22 35505 120040518A5315146737414 FLOORBEAM BOEING767 76733AER 1385230NM FUSELAGE CORRODED B T48RK NONE O OTHER ININSP/MAINT 1 GL09637TW 25403 CABIN FLOORBEAM AT STA 1480 LBL 70 CORROSION OUT OF LIMITS B767 SRM 53-00-51. REPAIR REQUIRED. FLOORBEAM CORRODED BECAUSE OF LAY AREA LEAKS. LAY AREA NEEDS TO BE PROPERLY SEALED. 2L72 4F RTA1NM 20040722000582004072200058NE 2004 7 22 RU32004F00000 220040625A7200 ENGINE BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE LEFT BIRD INGESTION E RU3AA UNSCHED LANDING C F.O.D. NRNOT REPORTED 1 SW1566 FF1 WHILE CONDUCTING CLEARANCE BELOW PATH RUN, A PAIR OF PIGEONS DIVED AND STRUCK LEFT ENGINE AREA. HEARD A THUMP AND ALL CREW MEMBERS STARTED NOTICING A BURNING SMELL. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. CREW REQUESTED IMMEDIATE LANDING AND WAS GIVEN A LANDING CLEARANCE. AIRCRAFT LANDED WITHOUT INCIDENT, TAXIED CLEAR OF RUNWAY AND SHUTDOWN. FIRE DEPARTMENT CHECKED AC AND RELEASED IT TO BE TOWED. PIGEON REMAINS WERE FOUND ON THE LEFT ENGINE INTAKE, INSIDE THE ENGINE IN THE SCREEN, ON THE LEFT WING LEADING EDGE, AND ON THE RT SIDE OF THE RUDDER. 2L72 4T4 T A24CE E4EA 20040722000592004072200059EA 2004 7 22 A6WA200440073 120040605A53116003603023 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31431AW 7256 FRAME FLANGE BETWEEN STRINGER 11-12 HAS A CRACK COMING FROM A RIVET HOLE. TRIMMED OUT CRACKED PORTION OF FRAME FLANGE. PERFORMED LPI OF CUTLINE TO ENSURE NO CRACKS EXIST. FABRICATING REPAIR FLANGE FROM FRAME SECTOR PN 600-36030-23 INSTALLED IAW REO 601R-53-61-193 REV. A. 2L72 4F4 FRTA21EA E15NE 20040722000602004072200060NM 2004 7 22 USAA040246 120040521A5220 WEB BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US40473 24555 PIT, Q5, WEB .5000 INCH CRACK, 2ND LIGHTENING HOLE FROM FWD EDGE OF DOOR 12 INCHES UP FROM LOWER EDGE OF DOOR. CUT OUT DAMAGE AND INSTALLED REPAIR PLATE IAW SRM. 2L72 4F4 FRTA16WE E2GL 20040722000652004072200065CE 2004 7 22 GUU2004F00024 120040608A2612 FIRE LOOP BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RIGHT INTERMITTENT A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1781556 UE239 DURING FLIGHT, RT FIRE LOOP ANNUNCIATOR ILLUMINATED INTERMITTNETLY. CONTINUED, LANDED WITHOUT INCIDENT. INSPECTED FORWARD AND AFT FIRE LOOP ASSEMBLY. CLEANED RT FIRE LOOP CONNECTORS. OPS CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040722000672004072200067CE 2004 7 22 UG8APA04001 120040608A32222341171 AXLE LEAR 60 60LEAR 5170707CE NLG CORRODED E UG8AO OTHER O OTHER NRNOT REPORTED 1 GL23699DA1083 237 DURING NOSE WHEEL TIRE CHANGE THE INNER BORE OF THE NOSE AXLE WAS FOUND TO BE CORRODED. PART HAD TO BE ORDERED TRIP WAS CANCELLED. REMOVED CORRODED AXLE (PN 2342117002) SN R274 AND INSTALLED NEW AXLE IAW MFG MM. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA10CE 20040727000112004072700011EU 2004 7 27 04FDEA02154 120040722A5340 MOUNT AIRBUS310 A310203 3930313EU LAVATORY DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MAIN CARGO COMPT LAV I/B AFT MOUNTING HOLE IS GOUGED. REPLACED DAMAGED SECTION OF TEE CAP IAW A310 SRM 51-40-21, 51-27-00, 51-23-10, AND 51-21-10. 2L72 4F RTA35EU 20040727000132004072700013EU 2004 7 27 04FDEA02156 120040722A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MAIN CABIN DUMMY TRACK 2R FR38.2 TO FR40/41 HAS 3 EA AREAS OF EXFOLIATED CORROSION LEVEL 3. REMOVED AND REPLACED SEAT TRACK IAW 51-40-20 AND 51-40-21. 2L72 4F RTA35EU 20040727000142004072700014EU 2004 7 27 04FDEA02157 120040722A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MAIN CABIN SEAT TRACK 1L 3 INCHES AFT OF FR 38.2 HAS CORROSION ON SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-20, 51-40-21, AND 51-72-10. 2L72 4F RTA35EU 20040727000152004072700015EU 2004 7 27 04FDEA02159 120040722A5310 CROSSBEAM AIRBUS310 A310203 3930313EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 ZONE 232 FRAME IS CRACKED UNDER CLS ADAPTER PLATE AT FR 23 BETWEEN SEAT TRACKS 1R & 2R. REPAIRED CRACKED FRAME 23 IAW A310-200 SRM 53-10-15 WITH REPAIR ANGLES AND FILLERS. WORK DOCUMENTED ON NRC N00411. 2L72 4F RTA35EU 20040727000182004072700018NM 2004 7 27 SWAA042079 120040722A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 FWD ENTRY AREA EMERGENCY EXIT LIGHT LENS LOOSE NEXT TO F/A'S SEAT. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040727000192004072700019 2004 7 27 SWAA042080 420040722A2565D31354 SLIDE BOEING737 7373Y0 1384671NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040727000222004072700022NM 2004 7 27 SWAA042084 120040722A53116546548 FRAME BOEING737 7373H4 1384600NM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED AT BS 747, LBL 7 TO LBL 11. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040727000242004072700024NM 2004 7 27 SWAA042086 120040722A55206959227 BUSHING BOEING737 7373Q8 1384670NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE ATTACH BUSHINGS PER MM. 2L72 4F RTA16WE 20040727000252004072700025NM 2004 7 27 04FDEA02161 120040722A5350 FRAME DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 EMP - FORWARD TAIL CONE FRAME CRACKED. 2L73 4F RTA22WE 20040727000272004072700027NM 2004 7 27 04FDEA02163 120040723A5710 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED 2 PLACES. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01, VOLUME II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040727000282004072700028NM 2004 7 27 04FDEA02164 120040723A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25626FE 48445 DURING PASSENGER TO FREIGHTER CONVERSION, FOUND CORROSION IN LT HORIZONTAL STABILIZER NR 1 BARREL NUT HOLE. FOUND EXISTING OVALITY HOLE 1.706 X 1.441 INCH REPORT ATTACHED. PERFORM REWORK/REPAIR X EA 1-5510-77038. 2L73 4F RTA22WE 20040727000322004072700032WP 2004 7 27 04FDEA02070 120040713A5753NRC6053 VANE DOUG DC10 DC1030 3023501WP LT OB FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 COMPLY WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB1860-3. COMPLIED WITH EA 8-5710-79550 WINGS REWORK OF GOUGE IN OUTBD FLAP VANE SUPPORT RIB ARB 1860-3 AT MAE. 2L73 4F A22WE 20040727000332004072700033GL 2004 7 27 04FDEA01853 220040625A7210 MOUNT BRACKET DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ACCESSORY GB WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 COMPLY WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET WEAR REPAIR. COMPLIED WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET AT MAE. 2L73 4F4 FRTA22WE E23EA 20040727000342004072700034WP 2004 7 27 04FDEA01854 120040625A78309019M14G05 GUIDE DOUG MD10 MD1010F 3022112WP THRUST REVERSER BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 NR 3 ENGINE LEFT T/R UPPER GUIDE IS BROKEN. REMOVED AND REPLACED NR 3 ENGINE LEFT T/R UPPER GUIDE IAW SRM 51-33-01 AT MAE. 2L73 4F RTA22WE 20040727000362004072700036NM 2004 7 27 04FDEA02107 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.096 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT HAND OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000382004072700038NM 2004 7 27 04FDEA02109 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000392004072700039NM 2004 7 27 04FDEA02110 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040727000412004072700041NM 2004 7 27 04FDEA02129 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040727000422004072700042NM 2004 7 27 04FDEA02130 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.503, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.499 AND REPAIRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000442004072700044NM 2004 7 27 04FDEA02132 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040727000472004072700047NM 2004 7 27 04FDEA02135 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.403, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000502004072700050WP 2004 7 27 04FDEA01858 120040320A5712ARB07601 RIB DOUG DC10 DC1010 3022110WP ZONE 500/600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25385FE 46619 RIGHT AND LEFT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. CRACKS HAVE BEEN TRIMMED AND ROUTED, REPAIR ANGLE AND DOUBLER INSTALLED TO RESTORE STRENGTH IAW FEDEX EA 8-5710-75729 (REF FEDEX NRC N0732, N0626). 2L73 4F A22WE 20040727000522004072700052NM 2004 7 27 04FDEA01860 120040625A2810 FUEL TANK BOEING727 727200 138407ENM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25209FE 22931 CORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821 RBL 13. *S/D* CORROSION ON UPPER SURFACE OF CENTER WING TANK AT BS 821, RBL 13 REPAIRED PER EA NR 7-5730-55326. 2L73 4F RTA3WE 20040727000562004072700056WP 2004 7 27 04FDEA02036 120040710A3220TA4075M0814 BRACKET DOUG MD10 MD1010F 3022112WP NLG BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 HYD CLAMP SUPPORT BRACKET IS BROKEN AT LOWER MOUNT OF THE MAINT PLATFORM ON THE NOSE GEAR STRUT. REMOVED AND REPLACED BRACKET IAW MM 20-50-02-2 AT MAE. 2L73 4F RTA22WE 20040727000642004072700064WP 2004 7 27 04FDEA01879 120040629A5247AJC7237 FITTING DOUG MD10 MD1010F 3022112WP APU DOOR DAMAGED A FDEAK NONE O OOTHER OTHER ININSP/MAINT 1 SO25398FE 46634 APU COMPT ACCESS DOOR SNUBBER ROD ATTACH POINT ANGLE HOLE IS ELONGATED. REMOVED AND REPLACED FITTING IAW SRM 51-31-01 AT MAE. 2L73 4F RTA22WE 20040728000012004072800001WP 2004 7 28 04FDEA01880 120040629A5414AUB7108 DOUBLER DOUG DC10 DC1010 3022110WP NR 3 ENG PYLON GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 NR 3 ENG PYLON AFT UPPER FAIRING ANGLES LT AND RT GOUGED AND CHAFED AT AFT FASTENER HOLES. REMOVED AND REPLACED WORN ANGLES LT AND RT IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040728000022004072800002WP 2004 7 28 04FDEA01881 120040630A5754ARB147468 SUPPORT ANGLE DOUG MD10 MD1010F 3022112WP RT WING SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 RIGHT WING SLAT TRACK NR 16 LOWER FAIRING PANEL INBOARD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-31-01 AT MAE. 2L73 4F RTA22WE 20040728000032004072800003WP 2004 7 28 04FDEA01882 120040630A5420ASL006725 ANGLE DOUG DC10 DC1010 3022110WP NR 1 ENGINE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 NR 1 ENG I/B FAN COWL LWR EDGE ANGLE BENT. REMOVED AND REPLACED IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040728000042004072800004WP 2004 7 28 04FDEA01883 120040630A5350AKC7251 BRACKET DOUG DC10 DC1010 3022110WP TAIL CONE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 BOTH LEFT AND RIGHT FWD SUPPORT PIN BRACKETS HAVE ELONGATED HOLES ON TAIL CONE WORK PLATFORM. REMOVED AND REPLACED BRACKETS IAW SRM 51-35-01 AT MAE. 2L73 4F A22WE 20040728000072004072800007WP 2004 7 28 04FDEA01886 120040630A5313AGA7810505 LONGERON DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING P TO F MODIFICATION AND TRANSITION CHECK, AFT FUSELAGE COMPT FOUND STA 1877-1951 STR 51 RT WITH CORROSION. REPLACED LONG 51 RT IAW SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34-47. 2L73 4F A22WE 20040728000102004072800010NM 2004 7 28 04FDEA02111 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIA.=1.062, FINAL DIAMETER = 1.218 AND REPAIRED AS PER EA NR 1-5750-77943. TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000112004072800011NM 2004 7 28 04FDEA02112 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.502 AND REPAIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000132004072800013NM 2004 7 28 04FDEA02114 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.501 AND REPAIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000142004072800014NM 2004 7 28 04FDEA02115 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.196 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000152004072800015NM 2004 7 28 04FDEA02116 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.404, MATERIAL REMOVED=0.007, REMAINING THICKNESS=0.397 AND REPAIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000172004072800017NM 2004 7 28 04FDEA02118 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.406, MATERIAL REMOVED=0.008, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEX EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000192004072800019NM 2004 7 28 04FDEA02120 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.510, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.507, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000202004072800020NM 2004 7 28 04FDEA02121 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040728000212004072800021NM 2004 7 28 04FDEA02136 120040719A5753 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040728000222004072800022NM 2004 7 28 04FDEA02137 120040719A5753 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040728000242004072800024WP 2004 7 28 04FDEA02041 120040710A7830580210002 LATCH DOUG DC10 DC1030 3023501WP THRUST REVERSER BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 NR 3 ENG LEFT T/R UPPER LATCH ROD IS BENT. REMOVED AND REPLACED UPPER LATCH ROD IAW MM 78-32-19 AND 20-50-02 AT MAE. 2L73 4F A22WE 20040728000252004072800025NM 2004 7 28 04FDEA02042 120040710A5714 SUPPORT FITTING BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25245FE 22016 CENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT BS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1. 2L73 4F RTA3WE 20040728000292004072800029NM 2004 7 28 04FDEA02046 120040712A5744ARC050213 BRACKET DOUG MD11 MD11 3023602NM TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 COMPLY EA 1-5750-78010 OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR. OUTBOARD TRAILING EDGE FLAPS INBOARD HINGE BRACKET (WING SIDE) CORROSION REPAIR HAS BEEN COMPLIED. 2L73 4F RTA22WE 20040728000312004072800031EU 2004 7 28 04FDEA02049 120040712A5315 FLOORBEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 FWD CARGO COMPT UPPER FLOORBEAM AT FRAME 30 O/B OF NR 1 SEAT TRACK FROM CENTER IS CRACKED AS MARKED (RT SIDE). REMOVED DAMAGE, NO CRACK NOTED, FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, 1 EA SHIM IAW A300-600 SRM 53-10-15 FIG 311/312, TREATED, PRIMED, AND TOPCOATED ALL AREAS IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20040728000322004072800032EU 2004 7 28 04FDEA02050 120040712A5315 FLOORBEAM AIRBUS300 A300F4605R 3930327EU FUSLEAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 FWD CARGO COMPT UPPER FLOORBEAM AT FRAME 30 O/B OF NR 1 SEAT TRACK FROM CENTER IS CRACKED AS MARKED (RT SIDE). REMOVED DAMAGE, NO CRACK NOTED, FABRICATED AND INSTALLED 2 EA REPAIR ANGLES, 1 EA SHIM IAW A300-600 SRM 53-10-15 FIG 311/312, TREATED, PRIMED, AND TOPCOATED ALL AREAS IAW A300-600 SRM 51-75-10. 2L72 4F RTA35EU 20040728000342004072800034NM 2004 7 28 SWAA042069 120040721A3350311500 LENS BOEING737 7373K2 13844BANM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29345SA 23786 BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 3 ABC, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040728000362004072800036NM 2004 7 28 SWAA042071 120040721A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 793, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040728000412004072800041NM 2004 7 28 SWAA042076 120040721A276165448517 ACTUATOR BOEING737 7373H4 1384600NM GROUND SPOILER BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD GROUND SPOILER, OUTBOARD ACTUATOR FWD ATTACH POINT BROKEN. REMOVED AND REPLACED LT WING GROUND SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20040728000442004072800044NM 2004 7 28 SWAA042068 120040721A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 AFT EMERGENCY FLASHLIGHT WEAK. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040728000512004072800051WP 2004 7 28 04FDEA02082 120040715A3240 FITTING DOUG DC10 DC1030 3023501WP ZONE 700 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 NOSE WHEEL WELL LT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC-10-30 M/M 32-42-02-7. 2L73 4F A22WE 20040728000522004072800052WP 2004 7 28 04FDEA02083 120040715A3240 FITTING DOUG DC10 DC1030 3023501WP ZONE 700 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 NOSE WHEEL WELL RT OVERHEAD FLIGHT BRAKE FITTING HAS GOUGED AREAS. REMOVED AND REPLACED FITTING IAW DC10-30 M/M 32-42-02-7. 2L73 4F A22WE 20040728000572004072800057NM 2004 7 28 04FDEA01794 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000582004072800058NM 2004 7 28 04FDEA01795 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000592004072800059NM 2004 7 28 04FDEA01796 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000602004072800060NM 2004 7 28 04FDEA01797 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000612004072800061NM 2004 7 28 04FDEA01800 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000622004072800062NM 2004 7 28 04FDEA01848 120040624A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING FORWARD AND AFT BOLT HOLES CORRODED. 2L73 4F RTA22WE 20040728000652004072800065WP 2004 7 28 04FDEA01803 120040619A5753ANB7254502 FITTING DOUG DC10 DC1010 3022110WP RT IB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 RIGHT I/B FLAP SIDE LOAD ROLLER FITTING 3 EA ROLLER BORES AND FACES CORRODED. SIDE LOAD FITTING REMOVED AND REPLACED WITH NEW FITTING IAW CMM 57-55-22 AT MAE. 2L73 4F A22WE 20040728000682004072800068NM 2004 7 28 04FDEA01806 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000692004072800069NM 2004 7 28 04FDEA01807 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000712004072800071NM 2004 7 28 04FDEA01809 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000772004072800077WP 2004 7 28 04FDEA01870 120040628A5712ARB10861 RIB DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 ACCOMPLISH EA 8-5710-78226, WINGS REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1086-1. COMPLIED WITH EA 8-5710-78226. 2L73 4F A22WE 20040728000782004072800078NM 2004 7 28 04FDEA01816 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000792004072800079NM 2004 7 28 04FDEA01817 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000802004072800080NM 2004 7 28 04FDEA01818 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000812004072800081NM 2004 7 28 04FDEA01819 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000832004072800083NM 2004 7 28 04FDEA01821 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000882004072800088EU 2004 7 28 04FDEA01914 120040702A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 MAIN CABIN SEAT TRACK 4L HAS 2EA AREAS OF CORROSION INCLUDING ON AND UNDER SCALLOPS BETWEEN FR 75 & 76 AND BETWEEN FR 74 & 75. REMOVED CORRODED SECTION AND REPAIRED IAW A300-600 SRM 53-10-16, INSTALLED 1EA TRACK 4 FT 9 INCHES AND 2 EA SPLICES. 2L72 4F RTA35EU 20040728000912004072800091NM 2004 7 28 04FDEA01814 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000962004072800096NM 2004 7 28 04FDEA02139 120040720A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 538AB. REPAIR SPLICE ANGLE FABRICATED AS PER SRM 57-20-00, VOLUME I; NEW STRINGER AND SPLICE ANGLES INSTALLED AS PER SRM 57-20-00, VOLUME I. 2L73 4F RTA22WE 20040728000982004072800098NM 2004 7 28 04FDEA01740 120040615A5744ARC0154 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORRODED. LEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORROSION. REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS = 0.483 INCH, REMAINING THICKNESS = 0.446 INCH, MATERIAL REMOVED = 0.037 INCH. REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-76744, TITLE: WINGS - LEFT AND RIGHT INBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040728000992004072800099NM 2004 7 28 SWAA042101 120040724A33506556633 LIGHT BOEING737 7372T4 1384492NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040728001002004072800100NM 2004 7 28 04FDEA01741 120040615A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 FOUND FRAME BS 783 RT FASTENER HOLE CRACKED. REPAIR PER EO 7-5310-7-3367 PART 9. REPAIRED FRAME BS 783 RT PER EO 7-5310-7-3367 PART 9. 2L73 4F RTA3WE 20040728001012004072800101NM 2004 7 28 04FDEA01742 120040615A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION ON FLOORBEAM, STA 760, LBL 66, WL 206. *S/D* CORROSION OUT OF LIMITS. REMOVED STUB FLOORBEAM BS 760 LT SIDE. DRILLED UP & INSTALLED NEW STUB FLOORBEAM WL 200 PER SRM 51-30-2, 51-30-5, 53-10-1. 2L73 4F RTA3WE 20040928000572004092800057SW 2004 9 28 ALG2004F00048 120040819A2497MS24171D1 RELAY BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL BATTERY OVERHEATED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03167H 2968 IN FLIGHT CREW AND PASSENGERS SMELLED SMOKE, LANDED AT FIRST AVAILABLE PLATFORM (WC 620) AND AFTER LANDING AIRCRAFT EXPERIENCED TOTAL ELECTRICAL FAILURE. REMOVED AND REPLACED AIRCRAFT BATTERY AND BATTERY RELAY, SET GENERATOR VOLTAGE AND INSPECTED WIRES IN AIRCRAFT NO DEFECTS NOTED. BATTERY RELAY GOT HOT. AIRCRAFT GROUND RAN NO DEFECTS NOTED ALL WORK DONE IAW MM. 1G71 3U3 U H2SW E4CE 20040928000632004092800063SW 2004 9 28 2004F00397 120040923A3213 CROSSTUBE BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL SKID BROKEN I O OTHER O OTHER TXTAXI/GRND HDL 1 CE035001N3000 2410 BOTH SKID TUBES FAILED AT FWD EDGE OF SKID SHOE JUST AFT OF AFT CROSS TUBE. THIS HAPPENED IN HANGAR WHEN PERSONNEL PULLED DOWN ON THE T/R GEARBOX. FAILURE WAS DUE TO CORROSION/STRESS CRACK, AND INPROPER POSITIONING, AT DESIGN, OF THE SKID SHOE. SKID SHOE SHOULD BE BELOW END OF AFT CROSS TUBE. MFG PLACED IT JUST AFT OF CROSS TUBE. ON EVERY LANDING, SKID TUBE IS FLEXED AT THIS POINT DUE TO AC WEIGHT. PART ALSO ALLOWS WATER INTO SKID TUBE WITH NO WAY FOR IT TO EXIT, CAUSING CORROSION WITHIN TUBE. NEW PART HAS THIS DEFECT REMEDIED. PLACEMENT OF SKID SHOE IS STILL IN WRONG PLACE ON NEW PART. MFG ADVISED ME THIS IS NOT A NEW PROBLEM. I HAVE OPERATED THESE AIRCRAFT FOR 25 YEARS, AND HAVE NEVER HEARD OF THIS DEFECT.1G71 3U3 U H2SW E4CE 20040928000672004092800067WP 2004 9 28 ASMF200409008 120040921A2913AS66411LS666 PUMP DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE HYD SYSTEM FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML405165800 49726 AIRCRAFT RETURNED TO PLATFORM, LT HYDRAULIC PUMP FAILED. HYDRAULIC PUMP SOLENOID WAS CHECKED AND CIRCUIT BREAKERS WERE RESEATED AND FAIL CONTINUED. LT HYDRAULIC PUMP WAS REPLACED IAW MM 29-01-02, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040928000792004092800079NM 2004 9 28 SWAA042785 120040924A335065C27093 LIGHT BOEING737 7372T4 1384492NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040928000832004092800083 2004 9 28 SWAA042789 420040925A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29457WN 33856 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040928000992004092800099EA 2004 9 28 COMA0460516 120040916A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01427CA 7460 LEFT HAND INTERCOSTAL CORRODED IN CABIN AT LBL 36 AND LBL 27 AT FS 484. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20040928001132004092800113NM 2004 9 28 DL738040869 120040912A2913887477 PUMP BOEING737 737832 13844CFNM HYD SYSTEM FAILED A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO273750D 32375 LOW PRESS LIGHT ON SYS-A ELECT HYD PUMP CAME ON AND A-SYS HYD QTY STEADILY DECREASED TO 21 PERCENT THEN SYS PRESS BEGAN FLUCTUATING. COMPLIED WITH QRH NNC 13.2. REPLACED FAILED AND LEAKING A SYS ELECT HYD PUMP AND FILTERS. 2L72 4F RTA16WE 20040928001242004092800124NM 2004 9 28 DL75A040872 120040905A5270284N10581 SWITCH BOEING757 757212 1384951NM EMERGENCY EXIT INCORRECT A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27757AT 23127 GAP INCORRECT. GAP BETWEEN AUTOFIRE SWITCH ROLLER AND CAM INCORRECT IN RIGHT AFT OVERWING EXIT CUTOUT. REPLACED ADJUSTED GAP BETWEEN AUTO FIRE SWITCH ROLLER AND CAM IN RIGHT AFT OVERWING EXIT PER AMM 25-26-11-404-010. TEST NOW CORRECT PER AMM. 2L72 4F RTA2NM 20040928001382004092800138EU 2004 9 28 BAQA094843 120040528A771454487099111 INDICATOR BOLKMSBK117 BK117C1 5626025EU ENGINE RPM FAILED B BAQAK NONE O OTHER APAPPROACH 1 EA03911TG 7506 NR 2 ENG N1 IND LED DIGITAL DISPLAY DIM/BRITE BULB BURNED OUT. REPLACED WITH SERVICABLE UNIT. 06/04/2004 1G72 3U NCH13EU 20040928001422004092800142NM 2004 9 28 DL738040885 120040916A2120 ODOR BOEING737 737832 13844CFNM CABIN DETECTED A DALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO273753 29671 FLIGHT ATTENDANT REPORTED A STRANGE INTERMITTENT SMELL AFT OF LAST SECTION OF SEATS ON CAPTS SIDE. TURNED OFF LIGHTS AND SMELL DID NOT RETURN. TURNED LIGHTS ON, NO SMELLS NOTED. RAN PACKS NO ODORS NOTED PER CREW COMMENT SMELL COULD HAVE BEEN EMITTED FROM A PASSENGER. A/C OK FOR SERVICE. 2L72 4F RTA16WE 20040928001432004092800143NM 2004 9 28 DL76G040886 120040916A3610361001795 CONTROLLER BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 1 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271607B 30388 704233 LEFT ENG BLEED LIGHT, LT ENG COWL OPEN 605396. REACTIVATED LEFT ENG HPSOV AND REMOVED AND REPLACED LT ENG HP CONTROLLER AS PER AMM. REPLACED RELAY K650 IN PANEL P36. FOUND LOOSE LINE AT PRV VALVE TIGHTENED SAME. COWL CLOSED AND SECURED. BLEED OPS NORMAL ON HIGH PWR RUN UP. 2L72 4F4 FRTA1NM E13NE 20040928001442004092800144WP 2004 9 28 IXXA0400077S 120040501A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION A CRACK (1 INCH) WAS FOUND ON FUSELAGE EXTERIOR STA 174.000-1745.000, L-16R TO L-17R. REPAIR WAS ACCOMPLISHED. FASTENERS AND EXISTING EXTERNAL DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN IAW DC8 SRM 53-2-1 PG 105-106 FIG 7 VIEW 6. FABRICATED DOUBLER, FILLERS AND FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 SHEET 1. CLEANED, TREATED AND PRIMED IAW 51-1-8B AND INSTALLED FILLERS, DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 SHEET 1, DC8 SRM 51-1-21 PG 1 AND DC8 SRM 51-1-15 PG 1. 2L74 4F RT4A25 20040928001462004092800146WP 2004 9 28 IXXA0400079S 120040501A5210 DOOR DOUG DC8 DC871F 302199DWP PAX DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION FOUND AN INTERIM REPAIR ON THE UPPER AFT CORNER OF AFT PASSENGER DOOR STA 1660.000 L-9L TO L-11L. REPAIR WAS ACCOMPLISHED. THE INTERIM REPAIR WAS REMOVED IAW DC8 SRM 51-1-21 PG 1, FABRICATED A NEW DOUBLER, TRIPLER AND FILLER IAW DC8 SRM 53-2-0 FIG 18. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-15 PG 1. INSTALLED FILLER, DOUBELR AND TRIPLER IAW DC8 SRM 53-2-0 FIG 18, DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040929000012004092900001NE 2004 9 29 DL777040854 220040827A7200 ENGINE BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 2 BIRD INGESTION A DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO27866DA20068 29738 51149 BIRD INGESTION AT TAKEOFF. SURGE AND ENGINE EXCEEDENCE. ENGINE CHANGED. 2L72 4F4 FRTT00001SEE00050EN 20040929000162004092900016NM 2004 9 29 04FDEA02142 120040720A5340 FITTING BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CRACKED STR FITTING AT BS 874 STR 9R. REMOVED AND REPLACED STRINGER 9R FITTING AT BS 874 IAW BOEING 727 SRM 51-30-5, BOEING 727 SRM 51-30-2. 2L73 4F RTA3WE 20040929000542004092900054NM 2004 9 29 P5CA0401212 120040914A5311 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT FUSELAGE FRAME WEB BELOW THE UPPER CHORD IS PUNCTURED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER & FILLER, REINSTALLED, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040929000652004092900065NM 2004 9 29 AALA20040982 120040902A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21901AN 29503 TUL - CABIN EMERGENCY LIGHT BATTERY PACK FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000672004092900067WP 2004 9 29 AALA20040976 120040922A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217533A 49987 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT ROW 22 INOPERATIVE. REPLACED SOCKET FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000702004092900070WP 2004 9 29 AALA20040967 120040914A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21581AA 53158 EMERGENCY LIGHTS IN CEILING AT ROW 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING AT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000752004092900075 2004 9 29 AALA20040991 420040923A3460 COMPUTER BOEING757 757223 1384957NM FLT MANAGE INOPERATIVE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21188AN 32382 INFLIGHT RIGHT FLIGHT MANAGEMENT COMPUTER FAIL LIGHT ILLUMINATED. LEFT FLIGHT MANAGEMENT COMPUTER KEYS FROZEN. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT FLIGHT MANAGEMENT COMPUTER AND PLACARD LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. *S/D* REPLACED LEFT FLIGHT MANAGEMENT COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040929000772004092900077EA 2004 9 29 COMA0470070 120040919A2760 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA SPOILERS ACTIVATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01355CA 10067 FLIGHT 5852 DURING DESCENT RECEIVED AN OUTBOARD SPOILERON CAUTION. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. PERFORMED SYSTEM RESET. 2L72 4F RTA21EA 20040929000812004092900081NM 2004 9 29 HNAA0400111 120040812A335061047811 BATTERY PACK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHT INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07807EX 292 WHILE IN MAINTENANCE IT WAS DISCOVERED DURING ROUTINE OPERATIONAL CHECK THAT THE LEFT HAND FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED EMERGENCY BATTERY. OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 20040929001182004092900118NM 2004 9 29 HNAA0400117 120040830A2721682015 SWITCH DHAV DHC8 DHC8102 2809003NM RUDDER TRIM STUCK A HNAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA07815EX 321 FLIGHT 4039 NORFOLK TO LGA REPORTED HAVING A RUDDER TRIM ACTUATOR RUNAWAY CONDITION. CREW FOLLOWED THE ABNORMAL PROCEDURES CHECKLIST AND CONTINUED THE FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE IN LGA TROUBLESHOT SYSTEM AND FERRIED AIRCRAFT TO MIDDLETOWN FOR MAINTENANCE. MAINTENANCE FOUND THE RUDDER TRIM SWITCH TO BE HANGING UP WHEN SELECTED TOWARDS THE LEFT HAND POSITION. SWITCH WAS REMOVED AND REPLACED. SYSTEM WAS OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040929001202004092900120CE 2004 9 29 DXTA200400349 120040801A3230 SQUAT SWITCH CESSNA560 560XL 2076702CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07671QS 5605071 AFTER TAKEOFF, FOUND LANDING GEAR WOULD NOT RETRACT, DIVERTED AIRCRAFT TO GTF AND LANDED SAFELY. JACKED UP AIRCRAFT AND ADJUSTED LT MLG SQUAT SWITCH IAW CESSNA 560XL MAINTENANCE MANUAL CHAPTER 32-61-00. SERVICED LT & RT MLG OLEO'S IAW CESSNA 560XL MM CHAPTER 12-14-00, INSPECTED WIRING IN LT WHEEL WELL, LANDING GEAR CONTROL UNIT AND LANDING GEAR CONTROL VALVE IAW CESSNA-560XL M/M CHAPTER 32-32-02. SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20040929001222004092900122EU 2004 9 29 120411 120040813A7930 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE ENGINE OIL INTERFERENCE A UHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1719XS 340A019 122 DURING CRUISE THE CREW NOTICED THE RT ENGINE OIL PRESSURE DROPPING TO THE LOW SIDE OF THE GREEN ARC. CREW FOLLOWED QRH AND CONTACTED MOC AND SOC. MOC ADVISED THE CREW TO MONITOR AND CONTINUE TO HPN. SHORTLY AFTER HANGING UP INDICATION CONTINUED TO DROP INTO THE YELLOW WITH THE ASSOCIATED WARNING LIGHT ON THE CWP. THE LIGHT IMMEDIATELY WENT OUT. THE CREW DIVERTED TO ABE THE CWP WARNING LIGHT BRIEFLY ILLUMINATED AFTER LANDING WHEN THE ENGINE WAS PUT INTO REVERSE. 2L72 4T4 TRTA52EU E8NE6 20040929001302004092900130CE 2004 9 29 DXTA200400343 120040720A1420 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE BEACON FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07833QS 258433 BEACON LIGHT INOP, CIRCUIT BREAKER POPPED INFLIGHT, PRIOR TO C/B POPPING CREW NOTICED A SLIGHT ELECTRICAL BURNING ODOR IN THE COCKPIT. FOUND THE UPPER BEACON OVERHEATED, CAUSING A SHORT IN THE PARALLEL CIRCUIT, THE WIRING CHECKED OUT GOOD. REPAIRED THE PIN IN THE CONNECTOR AND REPLACED THE UPPER BEACON, SYSTEM OPS CHECKED GOOD IAW CESSNA MM CHAPTER 33-40-32. 2L72 4F RTA3EU 20040929001332004092900133WP 2004 9 29 0401279997 120040805A5342 ANGLE DOUG DC9 DC931 3022065WP VERTICAL STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING M-CHECK FOUND CRACK IN VERTICAL STABILIZER ATTACH ANGLE AT BS 1095. REPAIRED PER EA 99-195833. 2L72 4F A6WE 20040929001352004092900135 2004 9 29 YENA200443 420040812A2350ACP2788AB04 AUDIO PANEL AIRBUS320 A320232 3930326EU COCKPIT INOPERATIVE A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15564JB5147 2020 F/O ACP NOT WORKING, C/B G7 POPPED AND THERE WAS A BRIEF BURNING SMELL. REMOVED AND REPLACED F/O'S ACP IAW AMM 23-51-12, ALL OPS CHECKS GOOD AT THIS TIME. INSPECTED CENTER PEDESTAL, NO SIGNS OF BURNING OR ODOR. 2L72 4F RTA28NM 20040929001392004092900139NM 2004 9 29 DL76P040906 120040921A3350P4010021SM BATTERY BOEING767 767332 1382001NM 1L DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO271402A 25989 NR 1 LEFT DOOR EMERGENCY FLASHLIGHT BATTERY LOW. REPLACED BATTERY AND BULB. 2L72 4F RTA1NM 20040929001412004092900141NM 2004 9 29 DL73S040908 120040922A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27317DL 23089 TWO INCH CRACK IN FUSELAGE SKIN STA 930 STR 24 RIGHT. REPAIRED PER SRM. 2L72 4F RTA16WE 20040929001452004092900145CE 2004 9 29 DXTA200400359 120040815A2170 WATER SEPARATOR CESSNA650 650 2076802CE CABIN CONTROL CONTAMINATED E DXTAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07797QS 6507097 WHILE ON GROUND, MASTER WARNING AND SMOKE LIGHT CAME ON, ENGINE WERE AT IDLE, APU ON. NOTICED SMOKE AND FAINT ODOR COMING OUT FROM BETWEEN THE LAV DOOR POCKET AND RIGHT REAR OVERHEAD LIGHT. PERFORMED ENGINE RUNS, WITH APU ON, COULD NOT SMELL SMOKE IN CABIN BUT HEAVY CONDENSATION COMING OUT OF WEMACS FLOOR VENTS AND SIDEWALL VENTS, CAUSING THE MASTER WARNING & SMOKE LIGHT TO COME ON FOR A SPLIT SECOND. PLACED CLIMATE CONTROL IN FULL COLD POSITION TO FULL HOT, NO CONDENSATION, NO MASTER WARNING. REMOVED COALESCER SOCKS FROM BOTH WATER SEPARATORS, CLEANED AND AIR DRIED THEN REINSTALLED. PERFORMED A FUNCTIONAL CHECK OF CLIMATE CONTROL OPS CHECK GOOD, WORK PERFORMED IAW CESSNA650 MM CHAPTER 12-10-01. 2L72 4F A9NM 20040929001512004092900151 2004 9 29 HNAA0400110 420040811A3442071131930 TRANSCEIVER DHAV DHC8 DHC8102 2809003NM WX RADAR INOPERATIVE A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07805EX22734651 228 FLIGHT 3920 ELECTED TO RETURN TO FIELD DUE TO WEATHER RADAR GOING INOPERATIVE DURING CLIMB WITH WEATHER POSSIBLE IN THE AREA. THE AIRCRAFT DID NOT ENCOUNTER ANY SEVERE WEATHER AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RADAR R/T. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040930000202004093000020EA 2004 9 30 ASOA04608 120040817A5320601R53611002 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE RIGHT INTERCOSTAL AT FS 625 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INTERCOSTAL AT FS 625 IAW BOMBARDIER REO 601R-53-61-100 AND SRM 51-40-00. (M) 2L72 4F RTA21EA 20040930000222004093000022EU 2004 9 30 ASOA04612 120040818A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11534AS18400 463 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040930000382004093000038EA 2004 9 30 ASOA04620 120040822A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DUIRNG A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE ON THE RIGHT SIDE AT FS 621 WAS FOUND TO BE CRACKED AT THE CORNER BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE ON THE RIGHT SIDE AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040930000402004093000040EU 2004 9 30 ASOA04629 120040802A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A CHECK IN YUL, THE NR 2 CAM GUIDE OUTBOARD ON THE LEFT OUTBOARD FLAP WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 2 CAM GUIDE OUTBOARD ON THE LEFT OUTBOARD FLAP IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000472004093000047EU 2004 9 30 2004F00398 120040918A5610NP1588513 WINDSHIELD AEROSPATR72 ATR72212 8680945EU COCKPIT CRACKED A SIMAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21425MJ 425 DURING CRUISE AT FL 240, CAPTAIN WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO SANTO DOMINGO. REMOVED AND REPLACED CAPTAINS WINDSHIELD ASSY. (M) 2H72 4T RTA53EU 20040930000572004093000057SO 2004 9 30 SIMA200425302 120040907A2150815243 ACM EMB 135 EMB135LR 3260305SO NR 1 SEIZED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21707EB 145195 DURING CRUISE FLIGHT, THE CREW REPORTED VISABLE SMOKE AND BLACK SOOT COMING FROM AIR VENTS IN FLIGHT DECK ALSO, FLIGHT ATTENDANT ALSO NOTED SMOKE IN CABIN AND CRACKLING NOISE FROM UNDER CABIN FLOOR. CREW DIVERTED TO ROA, EMERGENCY WAS DECLARED AND CFR FOLLOWED A/C TO GATE WITH NO FURTHER INCIDENT REPORTED. REPLACED NR 1 ACM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040930000612004093000061SO 2004 9 30 SIMA200423910 120040821A552214532237405 SKIN EMB 145 EMB145LR 3260212SO LT ELEVATOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21618AE 145097 ABI - DURING AN MBV INSPECTION, TORN SKIN WAS DISCOVERED ON THE LEFT ELEVATOR AT THE SERVO TAB ROD CUTOUT. PERFORMED A CUTOUT OF THE DAMAGED MATERIAL AND TREATED THE EDGES. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 55-20-01. (M) 2L72 4T RTT00011AT 20040930000712004093000071EU 2004 9 30 ASOA04633 120040803A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP NR 2 CAM GUIDE AT RIB 5, AND THE RIGHT INBOARD FLAP NR 3 CAM GUIDE AT RIB 6 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP NR 2 CAM GUIDE AT RIB 5, AND THE RIGHT INBOARD FLAP NR 3 CAM GUIDE AT RIB 6 IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000842004093000084NM 2004 9 30 C7WA200400024 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 700 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE. (M) 2L73 4F A3WE 20040930000872004093000087NM 2004 9 30 C7WA200400021 120040609A5311 FRAME BOEING727 727232 1384082NM CARGO BAY CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED STAITON 1148 STRINGER 25 RIGHT. INSTALLED INTERNAL FRAME REPAIR IAW 727 SRM 51-20-1 AND 51-30-2. (M) 2L73 4F A3WE 20040930000892004093000089NE 2004 9 30 2004F00364 120040713A5320642066341101 SPLICE SKRSKYS64 S64E 8142604NE FUSELAGE CRACKED B E8KLK NONE O OTHER ININSP/MAINT 1 NM09CGJZK 64003 IN THE COURSE OF PERFORMING POST FLIGHT INSPECTION THE FIELD MAINTENANCE CREW DISCOVERED A CRACKED IN THE LEFT SPLICE FITTING. THE CRACK ORIGINATED AT THE FORWARD HI-LOCK FASTENER ON THE PYLON SIDE FUSELAGE 770 INCH WL 178 LBL 14. THIS CRACK MEASURES .400 INCH IN LENGTH. (M) 2G72 4U H4EA 20040930001022004093000102 2004 9 30 GTIA040684 420040728A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 DTW - FOUND SLIDE PACK FELL OFF. REINSTALLED L1 DOOR SLIDE PACK. (M) 2L72 4F A6WE 20040930001132004093000113NM 2004 9 30 USAASB04115 120040830A3350 SOCKET BOEING737 7373B7 1384580NM EMERGENCY LIGHT SHORTED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19391US 23313 PIT - MAINTENANCE REPORTED THE OVERHEAD MOUNTED AISLE ILLUMINATION EMERGENCY LIGHTS AT SEAT ROWS 5 AND 9, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND SEAT ROW 5 LIGHT SOCKET SHORTED AND THE BATTERY CHARGER FUSE BLOWN. REPLACED SEAT ROW 5 LIGHT/SOCKET ASSEMBLY, LEFT SIDE, PER MM 33-51-21 AND BATTERY CHARGER, P/N 2012-1 PER MM 33-51-51. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040930001162004093000116 2004 9 30 USAAEM04014 420040817A25654A40302 SLIDE EMB ERJ170ERJ170100 EU LEFT FWD DOOR DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19816MA 17000037 FLT 1611, ROC-PHL - DOOR 1L WOULD NOT DISARM FROM INSIDE OF AIRCRAFT. GIRT BARS WERE MANUALLY RELEASED BY MAINTENANCE AFTER DOOR WAS ASSISTED OPEN BY EXTERIOR HANDLE. THE DOOR ASSIST BOTTLE DISCHARGED, MAINTENACNE FOUND THE DOOR SLIDE LANYARD NOT ATTACHED AND TORN. REATTACHED LANYARD AND FERRIED TO PIT FOR SLIDE REPLACEMENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY SLIDE. (M) 2L74 4F RTA56NM 20040930001182004093000118EA 2004 9 30 ASOA04653 120040827A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11882AS 7503 DURING AN A-CHECK IN MCN, THE BOTTOM STEP AT THE ATTACH LINK ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930001262004093000126EA 2004 9 30 A6WA200440097 120040704A2120 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA COCKPIT FUMES A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31423AW 7636 FUMES ENTERING COCKPIT AND CABIN WHEN ADJUSTING THE TEMP. PERFORMED OPS CHECK OF NR 1 AND NR 2 PACK NO FUMES NOTED. OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930001302004093000130NM 2004 9 30 C7WA200400032 120040609A5330 SKIN BOEING727 727232 1384082NM FUSELAGE DENTED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND LEFT FUSELAGE SKIN DENTED FS 380 STRINGER 26 RT. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M) 2L73 4F A3WE 20040930001402004093000140NM 2004 9 30 SWAA042808 120040927A53106578062 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT FWD NR 5 STOP, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040930001442004093000144NM 2004 9 30 SWAA042798 120040927A53206551698 SPLICE BOEING737 737301 1384611NM STRINGER CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 26L, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040930001482004093000148WP 2004 9 30 ABXA040311 120040819A5230593410443AX INTERCOSTAL DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 FORWARD LOWER CARGO DOOR INTERCOSTAL ANGLE WAS CRACKED AT THE FORWARD LOWER STOP AREA. REPLACED ANGLE FORWARD LOWER STOP DOOR IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040930001642004093000164WP 2004 9 30 ABXA040313 120040826A57115597832501 SPAR CAP DOUG DC8 DC863 302198AWP LT WING DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23817AX 45928 FRONT SPAR CAP AT NR 3 PYLON, INSIDE NR 4 MAIN TANK, HAD 3 EACH OVERSIZE HOLES. REPAIRED IAW REA D857-50013MR. 2L74 4F 4A25 20040930001662004093000166WP 2004 9 30 ABXA040315 120040809A57305643130 SKIN DOUG DC8 DC863 302198AWP CENTER WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23817AX 45928 MAIN CABIN FS 759, RIGHT BUTT LINE 8, WING CENTER SECTION, CORRODED. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW REA D857-49995-MR. 2L74 4F 4A25 20040930001732004093000173NM 2004 9 30 HNAA0400084 120040920A261130326E7 AMPLIFIER DHAV DHC8 DHC8102 2809003NM SMOKE DETECTORS INOPERATIVE A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07941HA 161 AT ABOUT 1500 FEET SMOKE WARNING ILLUMINATED ALONG WITH MASTER WARNING LIGHT. REMOVED AND REPLACED FWD AFT SMOKE DETECTORS P/N OFF 473054, S/N OFF 0772, FWD P/N ON 473054, S/N ON 1568. AFT SMOKE DETECTOR P/N ON AND OFF 30-231-3. S/N ON 31572, S/N OFF 31820. REMOVED AND REPLACED AMPLIFIER GROUND, OPS CHECK GOOD. 2H72 4T RTA13NM 20040930001762004093000176NM 2004 9 30 P5CA0401203 120040914A5311 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT FUSELAGE FRAME, UPPER CHORD TOP & BOTTOM HAS SURFACE CORROSION. REMOVE CORROSION, ORIGINAL MATERIAL IS 0.085, AFTER REWORK 0.083 WITHIN LIMITS. 2L74 4F4 F A20WE E20EA 20040930001792004093000179EA 2004 9 30 HNAA0400081 120040831A3350 BULB DHAV DHC8 DHC8311 1386006EA EMERGENCY LIGHT BURNED OUT A HNAAH DEACTIVATE SYST/CIRCUITS L NO TEST NRNOT REPORTED 1 EA07848EN 331 AT ROW NR 1 RED EMERGENCY FLOOR EXIT LIGHT IS OUT. REMOVED AND REPLACED BULB, OPS CHECK GOOD. 2H72 4T RTA13NM 20040930001812004093000181WP 2004 9 30 ABXA040316 120040817A5313577991211 LONGERON DOUG DC9 DC9 3022002WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23817AX 45928 FORWARD CARGO STA 480, LONGERON 31 LEFT CORRODED. FABRICATED REPAIR AND REPAIRED AREA IAW REA D853-49998-MR. 2L72 4F A6WE 20040930001822004093000182 2004 9 30 ABXA040326 420040915A2565 GIRT BAR BOEING767 767281 1385109NM ESCAPE SLIDE CONTAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23795AX 23145 DOOR SLIDING ARMING HANDLE DIFFICULT TO ARM. REMOVED DEBRIS AND DIRT FROM GIRT BAR CAM ENGAGEMENT PINS AND MECHANISM. CLEANED AREA AND OPERATED DOOR THROUGH SEVERAL CYCLES. OPS CHECKED GOOD IAW B767 AMM 52. 2L72 4F RTA1NM 20040930001892004093000189 2004 9 30 SWAA042779 420040924A256565C16280 HOOK BOEING737 7373H4 1384600NM R1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR STOW HOOK PER MM. 2L72 4F RTA16WE 20040930001952004093000195NM 2004 9 30 UPS04M43190 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 33 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE CORROSION REMOVED, BLEND AND REAMED TO 1.162 INCH AT B/N HOLE NR 33 RT, FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 33 RT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 33 RT IAW EO MD11 -5510-19409-H, EN:1253-04, FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20040930001962004093000196SO 2004 9 30 W1X2004F00000 120040607A52804752932 HINGE PIPER PA31 PA31 7103102SO LYC O540 TIO540A1A 41532EA MLG DOOR BROKEN G W1XAO OTHER O OTHER NRNOT REPORTED 1 GL13405PA 31424 STEEL HINGE (PW 4752932) FAILED PRIOR TO AD 2000-25-01 INTERVAL. (GL13200409283) 1L72 3O3 O A20SO E14EA 20040930001972004093000197NM 2004 9 30 DHL2004760007 120040928A3260757 BULB BOEING727 7272B7 138407LNM PWA JT8 JT8D17 52049NE WARNING LIGHT BURNED OUT A DHLAK NONE P NO WARNING INDICATION TXTAXI/GRND HDL 1 SO01760AT 21954 MAIN GEAR ANTI-SKID LIGHTS FAILED TO ILLUMINATE WHEN ANTI-SKID WAS SWITCHED OFF. REMOVED AND REPLACED LIGHT BULBS. SYS CK GOOD. P/N 757 2L73 4F4 F A3WE E2EA 20040930001992004093000199NM 2004 9 30 EIA2004084 120040903A5310 SKIN BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE WINDOW BELT CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 MAIN CABIN WINDOW BELT CORRODED BETWEEN B.S. 680-700 LT. REMOVED CORROSION FOUND OUT OF LIMITS INSTALLED REPAIR IAW ECRA 480-53-171-2. 2L74 4F4 F A20WE E20EA 20041001000012004100100001NM 2004 10 1 EIA2004078 120040904A5710 STRUCTURE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE LT MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 LT WING GEAR W/W STA. 1241 LBL 40-80 CORROSION BETWEEN CANTED WEB AND LWR CHORD. REMOVED CORROSION AND REPAIRED IAW ECRA 480-53-167-2 2L74 4F4 F A20WE E20EA 20041001000022004100100002NM 2004 10 1 EIA2004079 120040906A5311 FRAME BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 STA 1840 FRAME CRACKED AT STR 12R. FABBED AND INSTALLED REPAIR IAW SRM 51-40-03 FIG 2 1-6. 2L74 4F4 F A20WE E20EA 20041001000042004100100004NM 2004 10 1 EIA2004083 120040902A5313 STRINGER BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 MAIN CABIN INTERIOR RT STRINGER 22 BS 160-220 CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, REPLACED STRINGER 22R BS 140-220 IAW SRM 51-30-02 AND 53-10-01. 2L74 4F4 F A20WE E20EA 20041001000062004100100006 2004 10 1 SA04092 420040929A2565D30664105 SLIDE AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE CABIN SEPARATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US155388917 861 THE SLIDE SHOP FOUND THAT THE BRIDGING ON UPPER TUBE AT RUNWAY END HAD A SEAM SEPARATION. THE REPAIR SHOP SENT THE SLIDE BACK TO THE VENDOR FOR REPAIR. 2L72 4F4 FRTA28NM E38NE 20041001000092004100100009NM 2004 10 1 UPS04M43193 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 15 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLENDED AND REAMED TO 1.067 INCHES AT B/N HOLE NR 15 LT, FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 15 LT IAW EO MD11-5510-19409-H. REPAIR C/OUT AT B/N HOLE NR 15 LT IAW EO MD11-5510-19409-H AND EN:1272-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041001000112004100100011NM 2004 10 1 UPS04M43195 120040726A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 22 LT BARREL NUT HOLE FOUND CORRODED ON BEARING SURFACE. CORROSION AT B/N HOLE NR 22 LT REMOVED, BLENDED AND REAMED TO 1.067 INCHES FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOL E NR 22 LT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 22 LT IAW EO MD11-5510-19409-H AND EN:1271-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041001000122004100100012NM 2004 10 1 UPS04M43197 120040812A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 13 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AMD BEARING SURFACE CORROSION AT B/N HOLE NR 13 RT REMOVED, BLENDED AND REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 13 RT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 13 RT IAW EO MD 11-5510-19409-H AND EN:1297-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041001000132004100100013 2004 10 1 UPS04M43215 420040928A2565 BULB DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE DISARM LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 R1 ENTRY DOOR SLIDE DISARM LIGHT NEEDS REPLACEMENT LIGHT BULB. REMOVED AND REPLACED, OPS CHECK GOOD. 2L73 4F4 FRTA22WE E24NE 20041001000162004100100016CE 2004 10 1 64696 120040908A2497 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE DEFROST HANDLE CHAFED A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE07231YV UE231 WHILE TAXING FOR TAKEOFF CREW NOTED ARCING BY F/O'S DEFROST HANDLE AND RETURNED TO GATE. REPAIRED CHAFED WIRES AND REPOSITIONED AS NEEDED. 2L72 4T4 TRTA24CE E26NE 20041001000172004100100017NM 2004 10 1 DXTA200400407 120040927A2120 ODOR AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE COCKPIT DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL07226QS 126 ELECTRICAL SMOKE SMELL IN COCKPIT WITH ELECTRICAL POWER ON, WHEN CIRCUIT BREAKER PANEL PUSH TO LIGHT BUTTON WAS USED THE OVERHEAD CIRCUIT BREAKER ON ESSENTIAL BUSS POPPED, STRONGEST SMELL ON LT SIDE. ITEM IS UNDER INVESTIGATION. 2K73 4F4 FRTA50NM E44NE 20041001000182004100100018CE 2004 10 1 65141 120040921A61201143800653 TORQUEMETER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 2 ENGINE INOPERATIVE A AMWAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 CE0710675 UE10675 ON TAKEOFF ROLL CREW OBSERVED NR 2 ENGINE VERY SLOW TO MAKE POWER. TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO THE GATE, MAINTENANCE CALLED. CORRECTIVE ACTION TAKEN: REMOVED AND REPLACED RT ENGINE TORQUE IND. OPS CK NORMAL. P/N 1143800653 S/N 461 2L72 4T4 TRTA24CE E26NE 20041001000192004100100019CE 2004 10 1 65355 120040927A2750 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE TE FLAPS DIRTY A AMWAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE07131YV UE131 AFTER TAKEOFF FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD, MAINTENANCE WAS CALLED. CLEANED FLAP SAFETY SWITCHES. 2L72 4T4 TRTA24CE E26NE 20041001000242004100100024WP 2004 10 1 WX0400030 120040915A3350 CONNECTOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE EMERGENCY LIGHT LOOSE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19890GA 49371 MAINTENANCE REPORTED SEAT EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. MAINTENANCE SECURED LOOSE CONNECTOR, EMERGENCY EXIT LIGHT OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20041001000282004100100028NE 2004 10 1 GJR2004F00002 220040901A7314TF9005 PUMP DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985* 52008NE FUEL SYSTEM INOPERATIVE B GJRRO OTHER O OTHER NRNOT REPORTED 1 NM01900KA 1676 LOSS OF FUEL PRESSURE. 1H71 3R3 R A806 5E1 20041001000292004100100029EA 2004 10 1 QXEA200400691 120040922A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 UPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CORRODED FROM LBL 22.0 TO RBL 22.00. REPAIRED IAW EA R-53-203. 2L72 4F4 FRTA21EA EOOO63EN 20041001000302004100100030EA 2004 10 1 QXEA200400685 120040916A5321 FLOOR PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 AFT SUPPORT BEAM FOR COCKPIT FLOOR PANEL 221 ALF IS CORRODED ON UPPER SURFACE. REPAIRED IAW CRJ-700 SRM 51-40-11 AND SRM 51-25-06. 2L72 4F4 FRTA21EA EOOO63EN 20041001000362004100100036EU 2004 10 1 04FDEA02834 120040928A5730 PANEL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE LT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 PANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998. 2L72 4F4 FRTA35EU E13NE 20041001000372004100100037EU 2004 10 1 04FDEA02835 120040928A5730 PANEL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 PANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1. 2L72 4F4 FRTA35EU E13NE 20041001000402004100100040SO 2004 10 1 D942004F00000 220040802A8520652130 ROCKER BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO NR 5 CYLINDER BROKEN B D94RC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW136037W110 TC2238 ON TAKEOFF ROLL PILOT LOST POWER TO THE LT ENGINE. INVESTIGATION REVEALED THAT THE NR 5 CYLINDER EXHAUST VALVE ROCKER ARM WAS BROKEN. ADDITIONAL INSPECTION REVEALED DAMAGE TO THE NR 5 PUSH ROD AND HOUSING, AND THE HYDRAULIC LIFTER ASSY. ENGINE WAS MANUFACTURED 7-23-01 AND HAS A TT OF 110.6 HRS. INSPECTION AND REPAIR WAS COMPLETED IAW INSTRUCTIONS FROM A TECH REP. THE BROKEN ROCKER ARM WAS SENT TO MFG WARRANTY, IAW THEIR REQUEST AND THE OWNERS APPROVAL. (SW13200404842) 1L72 3O3 ORT3A16 3E1 20041001000412004100100041NM 2004 10 1 CALA0400646 120040927A53206545875U70 ANGLE BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND R-1 DOOR THRESHOLD Z-ANGLE CORRODED AT STA 277-360, S17R. THE Z-ANGLE WAS REPLACED IAW SRM 51-10-2, FIGURE 101. 2L72 4F4 FRTA16WE E2GL 20041001000462004100100046EA 2004 10 1 SWIA200413864 120040926A2711 PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON TRIM INTERMITTENT A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07446SW 7666 AILERON TRIM SWITCH DOES NOT TRIM PROPERLY (INTERMITTENT). REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000472004100100047EA 2004 10 1 SWIA200413865 120040927A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY EXIT SIGNBURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07913SW 7597 FA REPORTS, EXIT LIGHTS ON GALLEY EXIT SIGN BURNED OUT. REPLACED LAMPS AT GALLEY EXIT SIGN, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000512004100100051NE 2004 10 1 2004UALA00846 220040918A7210 HOUSING BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 2 GEARBOX LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29791UA 26933 NR 2 ENGINE LOSS OF OIL PRESS/QUANTITY, TEMP INCRG/PRESS DCRSG. AMBER ALERT DECLARED FOR EMERGENCY EQUIPMENT, AFCT LANDED NORMALLY. FOUND MEATL ON THE MAIN & ANGLE GEARBOX (AGB) CHIP DETECTOR. THE ENGINE WAS REPLACED IN SEA. (NOTE: THE MASTER MCD HAD CHECKED CLEAN AT ORD, IMMEDIATELY PRIOR TO THIS FLIGHT.) AT TEARDOWN, THE AGB HOUSING WAS FOUND LEAKING FROM A CRACK. ADDITIONALLY, THE AGB SHOWED HEAVY SIGNS OF COKING AND HEAT DISTRESS. THE AGB HAD ONLY BEEN INSTALLED FOR 214 HOURS (32 CYCLES). THE PRIOR AGB ON THIS ENGINE HAD SUFFERED SIMILAR COKING AND HEAT DISTRESS. IN SPITE OF ALL ENGINE MODULES HAVING BEEN DISASSEMBLED, NO ROOT CAUSE WAS FOUND. 2L72 4F4 FRTT0001SE E46NE 20041001000522004100100052NM 2004 10 1 2004UALA00847 120040816A2530 OVEN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY CONTAMINATED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29937UA 26668 GALLEY OVEN INOPERATIVE AT FWD CAB, FWD RT GAL HAD ISOLATED SMOKE OVERHEAT IN OVEN, CB PULLED. NO ADDITONAL PROBLEM. PLASTIC MATERIAL WAS INGESTED INTO THE FAN AREA THAT MIGRATED TO THE OVEN HEATER ELEMENTS, POSSIBLY CAUSING MINOR IGNITION OF THE FLAMMABLE PLASTIC MATE 2L72 4F4 FRTA16WE E2GL 20041001000552004100100055EA 2004 10 1 04265652 120040921A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR INOPERATIVE A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27652BR 7429 PASSENGER DOOR WILL NOT OPEN. CLEANED AND LUBED PASSENGER DOOR INNER HANDLE. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000672004100100067NM 2004 10 1 0401745813 120040925A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING CHAFED A NWAAK NONE K FLUID LOSS ININSP/MAINT 1 GL01593NW4102 32993 THE FUEL SUPPLY TUBE IN THE RT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED IAW EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041001000712004100100071 2004 10 1 DHL2004742007 420040928A3418 CONTROLLER BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE STALL WARNING MALFUNCTIONED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01742DH 21290 ON GROUND STALL WARNING, STICK SHACKER AND AUTOPILOT DISCONNECT WARNING CAME ON AND COULD SMELL ELECTRICAL SMOKE IN COCKPIT. ADJUSTED AOA IAW 34-18-01, INSPECTED WIRING IN EE BAY NO SIGN OF SMOKE DETECTED SUSPECTED SMOKE FROM APU, INSPECTED APU IAW 21-20-01. OPS CHECK NORMAL. 2L73 4F4 F A3WE E2EA 20041001000722004100100072NE 2004 10 1 GLBA20030728 220040925A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT MAKING METAL A GLBAED ENGINE SHUTDOWN RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 NM0394GL 23562 UE94 114224 RT POWER SECTION MADE METAL, REMOVED AND REPLACED ENGINE. 2L72 4T4 TRTA24CE E26NE 20041001000742004100100074WP 2004 10 1 COOSDR040022 120040823A573057695822 SKIN DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE RT WING CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 RT WING LEADING EDGE SLOT SKIN CORRODED, BETWEEN XW 329.25 AND XW 359.0. 2L74 4F4 F 4A25 1E8 20041001000812004100100081WP 2004 10 1 MWEA040172 120040923A573059304941 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT WING DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LT WING FIXED VANE HAS MANY SMALL DENTS ON LOWER SURFACE IN A 6 IN X 6 IN AREA. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20041001000832004100100083WP 2004 10 1 MWEA040174 120040923A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 A DENT ON FUSELAGE SKIN IS 1.2500 INCH LONG BY 1 INCH WIDE LOCATED 1INCH BELOW 4 LT AND 1.6250 INCH AFT OF FRAME STATION 218 MAXIMUM DEPTH .007. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20041001000852004100100085NM 2004 10 1 COOSDR040012 120040817A5730 SKIN BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE CENTER WING SEC CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 WING CENTER SECTION FROM STA 740 TO STA 745 BETWEEN LBL 67.000 INCHES AND LBL 61.000 INCHES, UPPER SKIN PANEL WITH CORROSION ON OUTER SURFACE. 2L73 4F4 FRTA3WE E2EA 20041001000882004100100088EU 2004 10 1 04FDEA02810 120040923A5347A538129342000 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 MAIN CABIN FR52 SEAT DUMMY TRACK (CLS ADAPTOR) AT TRACK 2R, 24 INCHES TO RT OF CTRIS, CRACKED UNDERNEATH AT BEND RADIUS APPROX 4 IN LONG. REMOVED AND REPLACED CLS ADAPTOR FR52 2R IN MAIN CABIN IAW SRM A310/200 51-40-21. 2L72 4F4 FRTA35EU E13NE 20041001000932004100100093EA 2004 10 1 SWIA200413836 120040921A2752854D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07430SW 7523 FLAP FAIL DURING LANDING. INSTALLED NEW SERVICEABLE FLEX DRIVE SHAFT AND HOUSING BETWEEN ACTUATORS 3 AND 4 ON RT SIDE IAW MM 27-53-10. REMOVED AND REPLACED RT ACTUATOR IAW CRJ MM 27-53-05. OPERATIONAL CHECK GOOD. PN 601R93105-405 SN OFF 5453. 2L72 4F4 FRTA21EA E15NE 20041001000952004100100095 2004 10 1 SWIA200413838 420040920A22166225734002 SERVO EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RUDDER PEDALS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07586SW1064310643 120354 LT RUDDER IS HANGING UP OR CATCHING (BINDING). INSTALLED SERVICEABLE SERVO FOR RUDDER PEDALS AS REQUIRED. REF 22-10-05, OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041001000972004100100097EA 2004 10 1 SWIA200413840 120040919A27507805013 LEVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07416SW 7089 (FLAPS FAIL) CAUTION MSG ON APPROACH TO SLC. REMOVED AND REPLACED FLAP HANDLE IAW MM 27-51-01, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000992004100100099NM 2004 10 1 2004UALA00848 120040921A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP29588UA 26717 LANDED UNDER AMBER DUE TO BURNING ODOR IN CABIN. CAUSE UNKNOWN. NO PRIOR HISTORY BEFORE OR SINCE THIS INCIDENT IN ATA 21 OR 36. ENGINE RUNS, PACK RUNS AND OTHER ELECTRICAL INSPECTIONS FAILED TO PRODUCE ANY DISCREPANCIES. NO PARTS REPLACED. 2L72 4F4 FRTA2NM E17NE 20041001001002004100100100NM 2004 10 1 04FDEA02786 120040921A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20041001001012004100100101NM 2004 10 1 04FDEA02787 120040921A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20041001001022004100100102NM 2004 10 1 04FDEA02788 120040921A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20041001001032004100100103NM 2004 10 1 04FDEA02789 120040921A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20041001001052004100100105WP 2004 10 1 P9RA20040043 120040928A33501001191 LIGHT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE EMERGENCY EXIT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1110801 49127 AIRCRAFT IN MAINTENANCE SYR. LT FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE.REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY IAW MM. 2L72 4F4 F A6WE E9NE 20041001001072004100100107SO 2004 10 1 VA12004F00000 220040802A8520653020 CRANKSHAFT CESSNA421 421C 2076016CE CONT O520 GTSIO520N 17032SO ENGINE BROKEN B VA1RO OTHER O OTHER NRNOT REPORTED 1 SW19421GF1317 141 421C1110 292296R CRANKSHAFT HAD BEEN ULTRASONIC INSPECTED IAW APPLICABLE CSB 99-6A DURING OVERHAUL. RETURNED TO SERVICE AND AFTER 141.1 HOURS, FAILED IN SAME GENERAL OF REQUIRE INSPECTIONS. BROKEN AT NR 3 MAIN JOURNAL TO NR 5 ROD THROW. 1L72 3O3 O A7CE E7CE 20041001001162004100100116 2004 10 1 AP1718879 420040812A2562 ANTENNA PIPER PA28 PA28R180 7102809SO LYC O360 IO360A1A 41514EA ELT BROKEN B GGURO OTHER O OTHER NRNOT REPORTED 1 NM137579J 28R30969 ELT ANTENNA SHAFT IS BREAKING OFF AT BASE AND ANTENNA BEING LOST IN FLIGHT. BASE THAT CONNECTS TO COAX IS STILL ON PLANE. CENTER SHAFT IS ACTUAL ANTENNA IS HELD IN PLACE WITH A JAM TYPE-LOCKING FEATURE. ANTENNA ROD IS CRIMPED TO A PIN THAT MAKES CONTACT WITH COAX LEAD. THEY ARE BREAKING, REPLACED SIX ANTENNAS THAT LOSE CONTINUITY OR COMPLETELY GONE WHEN AC ARRIVES. ANTENNA SHAFT IS NOT RIGGED TO PUT ON AN AC THAT FLIES OVER 100 KNOTS. INCASE OF AN ACCIDENT ELT WOULD ONLY BE A DEAD WEIGHT. MAYBE AT MOST A VERY WEEK SIGNAL WOULD BE TRANSMITTED IF ANY. SUGGEST THAT YOU PUT OUT A LETTER TO CHECK THE CONTINUITY BETWEEN THE ANTENNA AND THE CONNECTION ON THE ELT UNIT MADE. 1L71 3O3 O 2A13 1E10 20041004000012004100400001NM 2004 10 4 USAA040549 120040806A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 PIT - FOUND FLOORBEAM CORROSION EMINATING FROM FASTENER HOLES, STATION 377 AT LBL 6 TO RBL 30. REMOVED UPPER T-CAP AND REPLACED WITH FABRICATED PART PER SRM 53-00-01 FIG 203, EA 95751. (M) 2L72 4F RTA2NM 20041004000042004100400004EA 2004 10 4 ASOA04671 120040901A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW THE CRJ-200 MM. (M) 2L72 4F RTA21EA 20041004000062004100400006NM 2004 10 4 USAA040553 120040812A5751 SKIN BOEING757 7572B7 1384964NM LT AILERON DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND SKIN DELAMINATED 3 INCH AREA, 48 INCHES FROM OUTBOARD END, TOP SURFACE, LEFT AILERON. COMPOSITE REPAIR AND BALANCED PER SRM 51-70-17, 51-60-01. (M) 2L72 4F RTA2NM 20041004000072004100400007NM 2004 10 4 USAA040546 120040812A5320 SUPPORT ANGLE BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND SUPPORT ANGLE CORRODED .75 INCH BY .75 INCH AREA, STATION 1663 RBL 56.5. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-10-2. CORROSION LEVEL 1, TASK NR C53-251-03, C53-252-03. (M) 2L72 4F RTA2NM 20041013001122004101300112EA 2004 10 13 SWIA200413866 120040805A5312 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07430SW 7523 LT FS 625 OBLIQUE ANGLE IS CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD IN ECS BAY. ( ITEM FOUND AT C-CHECK INSPECTION.) REMOVED AND REPLACED DAMAGED BRACKET IAW SRM 51-42-06. N 601R-35012-51. 2L72 4F4 FRTA21EA E15NE 20041013001152004101300115EA 2004 10 13 SWIA200413869 120040926A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FO'S YOKE INOPERATIVE A SWIAL ABORTED APPROACH F FLT CONT AFFECTED NRNOT REPORTED 1 NM07951SW 7795 FO STAB TRIM INOPERATIVE IN NOSE UP DIRECTION. REPLACED FO'S YOKE TRIM SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041013001192004101300119EA 2004 10 13 SWIA200413873 120040920A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07944SW INTERCOSTAL HAS A CRACKED RETURN FLANGE, FS 484.00 RBL 36.0. ( ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-53-41-059 REV "A" . 2L72 4F4 FRTA21EA E15NE 20041014000162004101400016SO 2004 10 14 MASA200400444 120040810A49204501968D SEAL EMB 145 EMB145LR 3260212SO APU BLOWN A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07838MJ129718059 145384 RECEIVED A LAV SMOKE WARNING DURING TAXI. ON CALL MX INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE AND COMPLIED WITH MEL PROCEDURES. MAINTENANCE FOUND APU COMBUSTION SEAL BLOWN AND PLACED THE APU ON MEL 10/17/04. MAINTENANCE REMOVED AND REPLACED THE APU. 2L72 4T RTT00011AT 20041014000222004101400022WP 2004 10 14 CALA0400665 120041007A52109955752 BEAM DOUG DC9 DC982 3022082WP L1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772824 49484 L1 DOOR UPPER CORNER BEAM CRACKED. STOP DRILLED CRACK, INSTALLED NEW DOUBLER PER SRM 52-05, FIG 31. 2L72 4F A6WE 20041014000282004101400028EA 2004 10 14 MASA200400502 120040907A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727314 7314 DURING POST FLIGHT IN PHX, THE LEFT EXTERNAL EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB AND OPS WERE NORMAL. 2L72 4F RTA21EA 20041014000292004101400029EA 2004 10 14 MASA200400503 120040907A3350CM6839 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW077291Z 7291 EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT. 2L72 4F RTA21EA 20041014000372004101400037NM 2004 10 14 MASA200400418 120040723A3234574205A SELECTOR VALVE DHAV DHC8 DHC8202 2809007NM MLG INOPERATIVE A MASAO OTHER J WARNING INDICATION LDLANDING 1 SW07446YV1472 446 DURING LANDING SET-UP WHEN LANDING GEAR HANDLE PUT IN DOWN POSITION, NONE OF THE LANDING GEAR EXTENDED AND HAD 3 RED UNSAFE LIGHTS. CREW USED ALTERNATE EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. CURRENTLY TROUBLESHOOTING PROBLEM 7/24. MX REPLACED THE SELECTOR VALVE AND GEAR HANDLE. 2H72 4T RTA13NM 20041014000532004101400053SO 2004 10 14 MASA200400480 120040828A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07841MJ TR0776 145448 ABORTED TAKEOFF DUE TO AN E2 REVERSE DISAGREE MESSAGE. MX PLACED NR 2 THRUST REVERSER ON MEL. A/C DEPARTED WITHOUT FURTHER INCIDENT. 8/30/04 MAINTENANCE REPLACED STOW/TRANSIT SWITCHES. S/N'S OFF 0037, 0040, 0041, 0039. 2L72 4T RTT00011AT 20041014000652004101400065EA 2004 10 14 MASA200400518 120040910A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775992 7401 DURING OVERNIGHT MX, FOUND NR 4 BATTERY PACK LOW VOLTAGE. MX REPLACED THE BATTERY PACK, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041014000812004101400081WP 2004 10 14 ARWA20040702 120040714A283034255 ACTUATOR DOUG DC8 DC862 3021970WP FUEL DUMP SYS INOPERATIVE A ARWAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 SO19810BN 45905 FUEL DUMPED PER ABNORMAL CHECKLIST AT MAXIMUM LANDING WEIGHT SWITCH PUT IN DRAIN POSITION, BUT CONTINUED DUMPING MANUALLY PUT IN DRAIN POSITION FOR 5 MINUTES, REMAINDER OF ELECTRICAL CYCLE OK. TRANSFERRED TO DMI 18610 IN ACCORDANCE WITH MEL 28-9-1. MANUAL FUEL DUMP SYSTEM IS OPERATIVE. REMOVED AND REPLACED ACTUATOR MOTOR IN ACCORDANCE WITH MM 28-30-2. OPERATIONAL CHECK NORMAL, NO LEAKS NOTED, THIS CLEARS DMI 18610. 2L74 4F 4A25 20041014000842004101400084WP 2004 10 14 ARWA20040805 120040824A7400H676 SWITCH DOUG DC8 DC862 3021970WP NR 4 ENGINE FAILED A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19810BN 45905 ON ENGINE START, NR 4 ENGINE WOULD NOT LIGHT UP WITH A & B AND BOTH IGNITERS. T/S DOWN TO FUEL SHUT-OFF LEVER SWITCH TRANSFERRED TO DMI 18678 IN ACCORDANCE WITH MEL 74-1 CATEGORY-C, PLACARD INSTALLED. REPLACED START LEVER SWITCH PER MM 74-00; OPERATIONAL NORMAL. THIS CLEARS DMI 18678. PLACARD REMOVED. 2L74 4F 4A25 20041014000872004101400087NM 2004 10 14 DL76G040955 120041009A2611261780107 CIRCUIT CARD BOEING767 767332 1382001NM E/E BAY FAILED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO271602 29694 ON TAKEOFF SEVERAL LIGHTS FLICKERED AND REMAINED ON FOR UP TO 1 MINUTE, FIRE ON ANNUNCIATOR PANEL ILLUMINATED. REPLACED AFOLTS CARD. 2L72 4F RTA1NM 20041014001122004101400112NE 2004 10 14 04FDEA02262 220040728A7230 FAN AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 ENGINE OUT OF BALANCE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25684FE 802 705281 EN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9 VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 80 - 60 PERCENT. PERFORMED FAN TRIM BALANCE ON NR 2 ENG IAW A300-600 MM REF 72-21-00-2. ENGINE VIB INDICATED 0.2 UNITS AFTER FAN TRIM BALANCE. OK FOR SERVICE. 2L72 4F4 FRTA35EU E13NE 20041014001272004101400127EU 2004 10 14 A6WA200460037 120040903A5553 ANGLE BAC 146 146200A 1500266EU FUSE TO STAB CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31156TR E2156 FOUND CRACK ON THE VERTICAL STAB TO FUSELAGE CLOSING ANGLE LEFT SIDE, AT APPROX FRAME 45. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015003. (M) 2H74 4F A49EU 20041014001332004101400133NM 2004 10 14 USAA040647 120040914A53201137986 WEB BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND WEB CORRODED BETWEEN STATION 794 TO 847, BETWEEN STATION 794 TO 847. WEB AND STRAP REPLACEMENT ON AIR CARGO DOOR SILL PER DWG 65-47957. (M) 2L72 4F RTA16WE 20041014001382004101400138CE 2004 10 14 2004F00402 120040909A1420MS349E2241 CONNECTOR BEECH 1900 1900D 1154162CE DISPLAY CORRODED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO1781536 UE152 FLT 9225 - MIA/NAS - DURING FLIGHT, PILOTS DISPLAY PROCESSOR CIRCUIT BREAKER POPPED ACCOMPANIED BY SMELL OF SMOKE MOMENTARILY. MAINTENANCE FERRY TO FLL. FOUND BULKHEAD CONNECTOR J368 PINS SHORTED. REMOVED AND REPLACED J368 CONNECTOR AND RECEPTACLE P/N MS3476W2241S. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20041014001412004101400141CE 2004 10 14 2004F00404 120040901A55201016200111 BRACKET BEECH 1900 1900D 1154162CE LT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1769549 UE194 AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20041014001442004101400144NM 2004 10 14 2004F00407 120040911A291265179897 HOUSING BOEING727 7272J0 138407ENM HYD FILTER CRACKED A RIVAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NE05364PA 21107 DURING CHARGER FLT FROM CANCUN-BOS, B HYDRAULIC SYSTEM PRESSURE WENT TO ZERO, BOTH NR 1 AND NR 2 PUMP LOW PRESSURE LIGHTS ON. DUMPED 20,000 LBS OF FUEL AND DIVERTED TO MCO. FOUND B HYDRAULIC SYSTEM CASE DRAIN FILTER HOUSING CRACKED. REPLACED FILTER AND HOUSING. OPS CHECK AND LEAK CHECK GOOD. (M) 2L73 4F RTA3WE 20041014001452004101400145 2004 10 14 2004F00408 420040920A34426225132622 RADAR AIRBUS320 A320233 3930329EU WX SYS FAILED A SOKFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23482TA 1482 SJO - FLT 631 - DURING CLIMB, THE WX RADAR WAS INOPERATIVE AND AIRCRAFT WAS RETURNED TO SAN JOSE STATION FOR MAINTENANCE. AFTER LANDING, IT WAS FOUND UNSERVICEABLE THE TRANSCEIVER WEATHER RADAR, IT WAS REPLACED PER AMM 34-41-33 AND GROUND FUNCTIONAL CHECKS WERE PERFORMED AND FOUND SATISFACTORY. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20041014001462004101400146CE 2004 10 14 2004F00409 120040907A55201016200111 BRACKET BEECH 1900 1900D 1154162CE LT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1738537 UE158 AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20041015000122004101500012NM 2004 10 15 USAA040630 120040908A5320 SUPPORT BOEING737 7374B7 1384702NM FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SUPPORT ZEE ANGLE CORRODED .5 INCH BY 10 INCH AREA, STATION 727E PLUS 8 INCHES TO STATION 787, LEFT SIDE. REMOVED AND REPLACED ZEE ANGLE PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20041015000142004101500014NM 2004 10 15 USAA040626 120040905A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FLOOR SUPPORT WEB CORRODED .5 INCH BY .75 INCH AREA, STATION 847-867 RBL 21 AFT CARGO. INSTALLED NEW WEB PER SRM 53-60-53. (M) 2L72 4F RTA16WE 20041015000202004101500020NM 2004 10 15 USAA040619 120040917A5320 SUPPORT ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, BETWEEN STATION 500 AND 500A MOUNTED TO STRINGER 28L AND 28R. REMOVED AND REPLACED ANGLE PER DWG 65-45783. (M) 2L72 4F RTA16WE 20041015000232004101500023NM 2004 10 15 USAA040595 120040826A5347 MOUNT BOEING737 7374B7 1384702NM LAVATORY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND LAVATORY MOUNT WITH CORROSION 2 SQUARE INCH, RT OUTBOARD LAVATORY MOUNT STATION 947. REPLACED LAVATORY MOUNT PER SRM 51-10-00. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20041015000312004101500031EA 2004 10 15 ASOA04663 120040830A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR LANDING PLATE AT FS 589 AND FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 589 TO FS 605 IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20041015000362004101500036NM 2004 10 15 USAA040658 120040918A5711654532421 SPAR BOEING737 7373B7 1384580NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND UPPER CHORD CRACKED MORE THAN .343, BUT LESS THAN .6285, NR 2 HOLE, LEFT REAR SPAR UPPER CHORD AT RSS 224.14. OVERSIZED HOLE, INSTALLED FILLER, INSTALLED WING SKIN DOUBLER PER EA 78987. (M) 2L72 4F RTA16WE 20041015000432004101500043NM 2004 10 15 USAA040605 120040917A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND FLOORBEAM ANGLE CORRODED 2 INCHES, STATON 397 RBL 26-28. REPLACED ANGLE IAW SRM 51-10-02. (M) 2L72 4F RTA2NM 20041015000472004101500047NM 2004 10 15 USAA040572 120040902A5710 BEAM BOEING757 757225 1384959NM WING WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU63100 22198 CLT - FOUND BEAM WITH APPROXIMATELY 5 INCHES OF WEAR, LOWER FLANGE OF LEAD BEAM, AFT END OF BEAM. BLENDED AND TREATED PER EA 95815. (M) 2L72 4F RTA2NM 20041015000492004101500049NM 2004 10 15 BJNA040902 120040806A5330 SKIN BOEING737 737282 13844ATNM FUSELAGE CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BOTTOM OF L1 DOOR CUT OUT BS 336. INSTALLED DOUBLER AND STRAP AT L1 DOOR LOWER CUTOUT IAW SB 737-53-1083 REV 3. (M) 2L72 4F RTA16WE 20041015000512004101500051NM 2004 10 15 UIEA200400165 120040921A541065B941004 PYLON BOEING747 747230B 1384889NM NR 4 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, NR 4 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-FS 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION WAS ACCOMPLISHED AT EACH REPAIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DEFECT FREE CONDITION. (M) 2L74 4F A20WE 20041015000592004101500059WP 2004 10 15 DHL2004801537 120040917A282058924272 CONTROL BOX DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUEL LEVER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 1349: RT WING NR 4 ALT TANK FUEL LEVEL CONTROL BOX CRACKED. REMOVED AND REPLACED FUEL LEVEL CONTROL BOX ASSY ON RT WING NR 4 ALT TANK IAW MM 28-21-15 PG. 201-203. 2L74 4F4 FRT4A25 E2GL 20041015000722004101500072WP 2004 10 15 DHL2004801510 120040902A5511 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 2045: RT HORIZONTAL STABILIZER IB. L/E LWR FORMER CRACKED 1.000 AT XFS 53.750. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20041015000772004101500077 2004 10 15 ASMF200410004 420041006A2562100503121 SLIDE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE TAILCONE DEPLOYED W ASMFK NONE W INADEQUATE Q C ININSP/MAINT 1 SW23204AM2724311905 49404 DURING TRANSIT CHECK GROUND PERSONNEL ACTIVATED THE TAILCONE AND THE SLIDE. SLIDE WAS REPLACED IAW MM 25-62-01 AND TAILCONE WAS REINSTALLED IAW MM 53-53-00. DURING OVERNIGHT SERVICE TAIL CONE WAS CHECKED, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20041018000012004101800001SO 2004 10 18 SWIA200413931 120041011A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07292SW1010910109 120319 FLAP DISAGREEMENT ON RETRACTION. REMOVED AND REPLACED NACELLE FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20041018000022004101800002EA 2004 10 18 SWIA200413922 120040816A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 INTERCOSTAL FLOATING ANGLE AT FS 484 RBL 27 OB CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLE IAW REO 601R-53-41-059. 2L72 4F4 FRTA21EA E15NE 20041018000142004101800014NM 2004 10 18 UPS04443321 120040930A5710 SPLICE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C, LT WING UPPER BS 1241 WL 180 REAR SPAR SPLICE PLATE FASTENER HOLE NR 7 FOUND CRACKED AT SPAR CHORD UPPER LAYER RUNNING AFT APPROX .0625 INCH LONG. HOLE REWORKED AND OVERSIZED IAW EO B747-5740-17032. 2L74 4F4 F A20WE E20EA 20041018000152004101800015WP 2004 10 18 DHL2004801507 120040902A5511 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 2046: RT IB L/E LWR FORMER CRACKED 1.000, XFS 60.000 (RT HORZ STAB). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20041018000342004101800034EU 2004 10 18 MALA040584 120040923A2612 FIRE LOOP SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15424XJ 340B424 CLIMBING THRU 11.8K FT LT ENG FIRE INDICATION OCCURED WHILE PERFORMING MEMORY ITEMS FIRE INDICATION WENT OUT. WO PULLING FIRE HANDLE OR BLOWING BOTTLE AS STARTED THE QRH FIRE INDICATION REOCCURED. FIRE HANDLE PULLED AND BOTTLE BLOWN ALL INDICATIONS WENT OUT AT THAT TIME. FEW MINUTES LATER GOT ANOTHER INDICATION SO BLEW THE BOTTLES. MAINTENANCE REMOVED AND REPLACED SHORTED FIRE LOOP SEGMENT ON IB SIDE OF LT NACELLE. REMOVED AND REPLACED FIRE BOTTLES SEE TASK CARD 262107 FOR DETAILS. ALL WORK IAW 340 AMM CHAP 26 AND 72 SEE MM409 NR 093909 FOR DETAILS. 2L72 4T4 TRTA52EU E8NE 20041018000932004101800093NM 2004 10 18 04FDEA02448 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 STRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **. 2L73 4F4 FRTA3WE E2EA 20041018001712004101800171NM 2004 10 18 ASMF200409011 120040927A3340702242 LIGHT DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE STROBE DAMAGED W ASMFO OTHER O OTHER APAPPROACH 1 SW23881LF 53051 CAPTAIN REPORTED THAT DURING FINAL APPROACH LIGHTING IMPACT ON THE AIRCRAFT RADOME. LIGHTING IMPACT INSPECTION WAS PERFORMED IAW MM 05-53-00, NO MAJOR DAMAGES WERE DETECTED. THREE STATIC DISCHARGERS ON LT AND RT STROBE LIGHTS AND UPPER ANTI-COLLISION LAMP WERE REPLACED IAW MM 33-42-01 AND 33-43-01, TESTS WERE CORRECT. 2L72 4F4 FRT E9NE 20041018001782004101800178NE 2004 10 18 ASMF200409010 220040926A7230815431 BLADE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT SIDE DAMAGED W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23501AM 49150 725614 DURING TRANSIT CHECK WAS DETECTED LT ENGINE BLADES DAMAGED BY FOD. BLADES WERE REWORKED AND CHECKED, THEY WERE WITHIN LIMITS IAW MM 72-33-21. ENGINE RUN TEST WAS PERFORMED ALL CORRECT. DURING OVERNIGHT SERVICE 6TH AND 7TH COMPRESSOR STAGES WERE CHECKED, ALL CORRECT. C DISK PAIR OF BLADES WERE REPLACED IAW MM 72-33-21, OPERATIONAL TESTS WERE PERFORMED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20041018001802004101800180NM 2004 10 18 ANCF200400033 120041010A3220 LANDING GEAR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NOSE OUT OF RIG W ANCFC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO23632CT 49632 TAKE-OFF WAS ABORTED DUE TO STRONG VIBRATION OA THE NOSE GEAR, IT HAPPENED ABOVE 100 KTS. IAW AMM 32-21-03 PAGE 403. IN NLG WAS PERFORMED CHECK AND RIGGING IN NOSE GEAR UPPER LINKAGE TORQUE TUBE. 2L72 4F4 FRT E9NE 20041018001932004101800193NE 2004 10 18 ASMF200410003 220041006A7200 TURBINE BLADES DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE DAMAGED W ASMFC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SW23755RA 49727 725382 AIRCRAFT RETURNED OF FLIGHT, LT ENGINE FLAME OUT AFTER TAKEOFF AT 400 FT EGT'S WERE 590 DEGREE C. DURING REVISION, TECHNICAL PERSONNEL DETECTED THE LOW TURBINE BLADES WERE DAMAGED. AIRCRAFT WAS SENT TO THE HANGAR AND LT ENGINE WAS REPLACED IAW MM 71-00-00 AND 71-00-02, TESTS WERE CORRECT. FURTHER INFORMATION WILL BE SENT AS A SUPPLEMENT. 2L72 4F4 FRTA6WE E9NE 20041018001942004101800194NM 2004 10 18 SWAA042976 120041013A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041018001952004101800195 2004 10 18 SWAA042977 420041013A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29768SW 30587 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041018001962004101800196NM 2004 10 18 SWAA042964 120041013A3210654611316 PIN BOEING737 7373H4 1384600NM RT MLG SHEARED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29351SW 24572 DIVERSION, RT MLG UNSAFE LIGHT ILLUMINATED, AFTER LANDING GEAR RETRACTION ON TAKEOFF. CYCLED GEAR DOWN NORMAL INDICATION, LANDING GEAR TO UP POSITION RT MLG UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED RT MLG TRUNNION ANTI ROTATION PIN PER MM. 2L72 4F RTA16WE 20041018001972004101800197NM 2004 10 18 SWAA042965 120041013A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 470, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041018001982004101800198NM 2004 10 18 SWAA042966 120041013A27616544561 ACTUATOR BOEING737 7373H4 1384600NM LT WING SPOILER LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29316SW 23338 AIR TURNBACK, B-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED CAP AND O-RING ON NR 2 SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20041018001992004101800199NM 2004 10 18 SWAA042967 120041013A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29361SW 26572 AFT OUTBOARD EMERGENCY FLASHLIGHT LOW CHARGE. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041020000022004102000002EU 2004 10 20 A6WA200460042 120040921A5320 FITTING BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 ZEE MEMBER LT SIDE OF FUSELAGE AFT OF REAR SERVICE DOOR CORRODED BETWEEN FRAME 43 AND 44, REPAIR IN PROGRESS. (M) 2H74 4F4 F A49EU E6NE 20041020000032004102000003NM 2004 10 20 ASAA0440149 120040816A5320BAC1496377 ANGLE BOEING737 7374S3 1384711NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE LT ZEE ANGLE FROM 727-750 SPLICE IS CORRODED. REMOVED AND REPLACED ZEE ANGLE LT STATION 727-750 IN REF TO SRM 53-60-53 FIG 204 PGS 208-209. (M) 2L72 4F4 FRTA16WE E21EU 20041020000052004102000005NM 2004 10 20 ASAA0410361 120040805A3350883200312 RECEIVER BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14 INOPERATIVE. REPLACED LIGHT RECEIVER, OPS CHECK GOOD. (M) 2L72 4F4 F A16WE E2EA 20040720000122004072000012EU 2004 7 20 SIMA200415416 120040508A53117252813485 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21359SB 340B359 ABI - DURING A 400 HOUR INSPECTION, THE UPPER FLANGE OF FRAME 225 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED THE CORROSION BY CREATING A CUTOUT OF THE UPPER FLANGE. FABRICATED REPAIR ANGLE, SPACER AND FILLER PIECE. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 53-70-03 PARA 4 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040720000212004072000021 2004 7 20 RAIA00406010 420040614A34207003110901 DISPLAY JETAIRJETSTMJETSTM4101 1500501EU EFIS INOPERATIVE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03573HK1467411758 41092 5508 - STL - RIGHT EFIS SCREEN WENT BLANK. MAINTENANCE REMOVED AND REPLACED COPILOTS TOP EFIS TUBE. 2L72 4T RTA41NM 20040720000232004072000023EU 2004 7 20 RAIA00406012 120040614A612031057165 GOVERNOR JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03563HK2909 41079 3644- CVG - RED BETA CAP ELIMINATED PLUS VIBRATION ON RT ENGINE. ENGINE SHUT DOWN. MAINTENANCE REMOVED AND REPLACED RT PROPELLER GOVERNOR. 2L72 4T RTA41NM 20040720000242004072000024 2004 7 20 RAIA00406013 420040615A34180020BN4 COMPUTER EMB 145 EMB145LR 3260212SO STALL WARNING MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03812HK109 145373 3572 - GRR - SPS 1 INOP AND SPS ADVANCE INDICATIONS. MAINTENANCE REMOVED AND REPLACED STALL WARNING COMPUTER. 2L72 4T RTT00011AT 20040720000312004072000031SO 2004 7 20 C2XA04SH443 120040706A531014529744001 RIB EMB 145 EMB145ER 3260211SO BATTERY BAY CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE BATTERY COMPARTMENT CENTER RIB WAS FOUND TO BE CRACKED AND BENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000402004072000040NM 2004 7 20 SWAA042009 120040716A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 FWD LT EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040720000412004072000041NM 2004 7 20 SWAA042010 120040716A3350OL3071BPEGPL BULB BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C1 CHECK, FOUND EEPLS RED LIGHT INOP AT AFT GALLEY. REMOVED AND REPLACED EEPLS BULB PER MM. 2L72 4F A16WE 20040720000422004072000042NM 2004 7 20 SWAA042011 120040716A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED C1 CHECK, FOUND AFT GALLEY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT PER MM. 2L72 4F RTA16WE 20040720000432004072000043 2004 7 20 SWAA042012 420040716A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040720000442004072000044NM 2004 7 20 VNAA0406013 120040617A26115165351 FIRE LOOP DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RIGHT FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05430JS23261 3044 ON CLIMBOUT, THE CREW RECEIVED A RIGHT HAND FIRE LOOP FAIL MESSAGE. FLIGHT 2490 RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRE DETECTION BOX IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040720000452004072000045EA 2004 7 20 VNAA0407003 120040716A2612 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT FAILED A VNAAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07245PS 7919 THE CREW REPORTED RECEIVING A LEFT HAND JET OVERHEAT FAIL INTERMITTENTLY. MAINTENANCE INSPECTED AND FOUND THAT WITH THE LOOP-B SELECTED, THE INDICATION EXTINGUISHES AND WITH LOOP-A, SELECTED, THE INDICATION STAYS ON. MAINTENANCE CONTROL THEN DEFERRED LOOP-A IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 26-11-02-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040720000462004072000046WP 2004 7 20 AALA20040714 120040709A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21487AA 49680 LGA - EMERGENCY LIGHTS BATTERY PACK B5-105 INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK B5-105 PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000472004072000047WP 2004 7 20 AALA20040715 120040708A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217521A 49898 DEN - OVERHEAD EMERGENCY LIGHTS AT SEATS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY OVERHEAD LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000482004072000048WP 2004 7 20 AALA20040716 120040708A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21576AA 53153 DEN - EMERGENCY CEILING LIGHTS AT ROWS 28 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN 29 FOR ROWS 28 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000492004072000049WP 2004 7 20 AALA20040717 120040708A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21485AA 49678 AFT SEAT MOUNTED EMERGENCY EPL AT 7D IS INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EPL ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000502004072000050WP 2004 7 20 AALA20040718 120040708A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21485AA 49678 DFW - AFT TAIL CONE SLIDE EMERGENCY LIGHT AND AFT OVERHEAD EMERGENCY LIGHT FOR LAV AREA INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK B5-23 FOR TAIL CONE SLIDE EMERGENCY LIGHT AND OVERHEAD EMERGENCY LIGHT FOR LAV AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000532004072000053SO 2004 7 20 C2XA04BT074 120040704A335066364 LIGHT EMB 145 EMB145 3260210SO CABIN FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714972 145151 CREW REPORTED, EMERGENCY LIGHT (AFT) STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY PATH LIGHT STRIP, OPS CHECKED GOOD IAW EMB145 AMM 33-50-12. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040720000552004072000055NM 2004 7 20 DLM88040651 120040712A2910 B-NUT DOUG MD88 MD88 3023688NM HYD SYSTEM LOOSE A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27921DL 49645 AFTER CONFIGURING FOR LANDING LEFT HYD QTY DROPPED TO 2 QUARTS WITH THE LOW LEVEL LIGHT. ACCOMPLISHED PROCEDURE, PRESSURE REMAINED NORMAL UNTIL TAXI WHEN LEFT PRESSURE DROPPED TO 0 PSI. FOUND LOOSE B-NUT FITTING AT TOP END AND BOTTOM END OF LEFT THRUST REVERSER CONTROL VALVE LINE. TIGHTENED NUTS, RAN ALL HYD PUMPS FOR LEAK CHECK WITH NO LEAKS. HYDRAULIC QUANTITY AND PRESSURE ALL GOOD. 2L72 4F RTA6WE 20040720000582004072000058NM 2004 7 20 DL76L040654 120040711A3240767300ERM WHEEL BOEING767 767332 1382001NM MLG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27192DN 28449 ON W/A NR 3 WHEEL ASSY OUTBOARD DISC HAS SEVERAL CRACKS. REPLACED WHEEL PER MM, SPACER INSTALLED. CONTROL NUMBER 692579001, WHEEL ASSY DPN 321002928, S/N DL1291. 2L72 4F RTA1NM 20040720000622004072000062NM 2004 7 20 VNAA0406015 120040621A2497 TERMINAL BLOCK DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE COCKPIT FAILED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL05429JS 3043 THE CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND REPLACED FUSES AND A TERMINAL BLOCK UNDER THE CAPTAIN'S SEAT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040720000692004072000069SO 2004 7 20 C2XA04SH459 120040709A324039807 CONTROL VALVE EMB 145 EMB145ER 3260211SO BRAKE INOPERATIVE A C2XAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW27159411984 1984 145035 SHV - DURING TAXI TO THE GATE BRK OUTBD INOP WAS OBSERVED ON THE EICAS. CREW RESET THE CIRCUIT BREAKERS AND THE MESSAGE WENT AWAY. DURING TAXI TO THE HANGER THE MESSAGE REAPPEARED AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE IAW EMB 145 AMM 32-41-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000702004072000070SO 2004 7 20 C2XA04CL071 120040709A49504952281 DUCT EMB 145 EMB145LR 3260212SO APU LEAKING A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW2718556 145595 CLE FLIGHT 2899 THE CREW REPORTED A APU FIRE WARNING ON DESCENT AFTER APU START UP. WARNING WENT AWAY AFTER A FEW SECONDS AND APU STARTED NORMALLY. MAINTENANCE INSPECTED AND FOUND A BLEED LEAK OF THE APU BLEED DUCT AT THE FLEX JOINT. THE BLEED DUCT WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040720000712004072000071 2004 7 20 RAIA00407004 420040711A34207011672112 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU FAILED A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03558HK 41071 LEFT EFIS FAILED IN FLIGHT. REMOVED AND REPLACED LT SYMBOL GENERATOR IAW J41 MM 34-36-25. 2L72 4T RTA41NM 20040720000722004072000072SO 2004 7 20 C2XA04SD002 120040701A256072875561180D GLOWSTRIP EMB 145 EMB145XR 3260214SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2725134 145714 SDF - DURING 3A CHECK INSPECTION FOUND CABIN FLOOR FWD EMERGENCY PHOTOLUMINESCENT PATH LIGHTING STRIP COVER CRACKED. 2L72 4F RT 20040720000732004072000073SO 2004 7 20 C2XA04BT075 120040708A335066364 LIGHT EMB 145 EMB145ER 3260211SO CABIN DEACTIVATED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714945 145049 CREW REPORTED, NR 2 EMERGENCY LIGHT STRIP IN CABIN INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00, OPS CHECKED EMERGENCY LIGHTS GOOD. 2L72 4F RTT00011AT 20040720000742004072000074SO 2004 7 20 C2XA04TY109 120040712A335020131A BATTERY EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714505 145192 TYS - DURING A OVERNIGHT SERVICE/ROUTINE INSPECTION THE EMERGENCY LIGHT STRIP AT SEAT ROWS 7, 8 AND 9 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AT THE NR 3 LOCATION. OPS CHECK WAS GOOD AND A/C PUT BACK IN SERVICE. 2L72 4F RTT00011AT 20040720000752004072000075SO 2004 7 20 C2XA04CL069 120040710A335066364 LIGHT EMB 145 EMB145LR 3260212SO ROW 15-17 INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 DURING ROUTINE MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP WAS INTERMITTENT AT ROW 15-17. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP AT ROW 15-17. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040720000772004072000077EU 2004 7 20 RAIA00406027 120040627A2913384925 PUMP JETAIRJETSTMJETSTM4101 1500501EU HYD SYSTEM MALFUNCTIONED A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03572HK16050257 41091 3633 - TRI - AT GEAR RETRACTION HYDRAULIC LOW PRESSURE WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 HYDRAULIC PUMP. 2L72 4T RTA41NM 20040720000782004072000078SO 2004 7 20 RAIA00406028 120040627A27203603001001 PCU EMB 145 EMB145LR 3260212SO RUDDER CONTROL MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03819HK13310 145062 5752 - STL - RUDDER OVERBOOST WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED RUDDER PCU. 2L72 4T RTT00011AT 20040720000802004072000080 2004 7 20 RAIA00407008 420040711A3442700549822 TRANSMITTER JETAIRJETSTMJETSTM4101 1500501EU WX RADAR SYS FAILED A RAIAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 CE03551HK 41040 WEATHER RADAR FAILED IN FLIGHT. REMOVED AND REPLACED WEATHER RADAR TRANSMITTER OPS GOOD IAW MM 34-41-05. 2L72 4T RTA41NM 20040720000822004072000082NM 2004 7 20 AALA20040720 120040709A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21779AN 29955 DFW - EMERGENCY LIGHTS AT BOTH SIDES OF COACH ROWS 30 THROUGH 42 INOPERATIVE. REPLACED 3R EMERGENCY LIGHT BATTERY PACK FOR BOTH SIDES OF COACH ROWS 30 THROUGH 42. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040720001152004072000115SO 2004 7 20 RAIA00406029 120040607A335066368 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03808HK 145157 3548 - PIT - LAST FLOOR EMERGENCY STRIP LIGHT PARTIALLY INOPERATIVE. MAINTENANCE DEFERRED STRIP LIGHT PER MEL 33-50-00-2. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING STRIP LIGHT. 2L72 4F RTT00011AT 20040720001162004072000116EU 2004 7 20 RAIA00406030 120040609A5297 WIRE JETAIRJETSTMJETSTM4101 1500501EU PAX DOOR DEFECTIVE A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03558HK 41071 3645 - PIT - PAX DOOR WARNING INDICATION. MAINTENANCE DEFERRED PAX DOOR WARNING PER MEL 52-2. SUBSEQUENTLY CLEARED DMI BY RE-WIRING PAX DOOR WARNING SWITCH. 2L72 4T RTA41NM 20040720001172004072000117EU 2004 7 20 RAIA00406031 120040628A3230 HYDRAULIC SYSTEM JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03572HK 41091 3626 - TRI - LANDING GEAR WILL NOT RETRACT. MAINTENANCE BLEED HYDRAULIC SYSTEM AND OPS CHECKED OK. 2L72 4T RTA41NM 20040720001182004072000118SO 2004 7 20 RAIA00407001 120040703A5610 WINDOW EMB 145 EMB145LR 3260212SO COCKPIT LEAKING A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03829HK 145281 3578 - RIC - LOUD SQUEAL COMING FROM CAPTAINS WINDSHIELD AREA. MAINTENANCE RE-TORQUED CAPTAINS WINDSHIELD AND PRESSURIZED AIRCRAFT TO 5.0 PSI WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20040720001202004072000120SO 2004 7 20 C2XA04SH461 120040716A541014576631621 STIFFENER EMB 145 EMB145LR 3260212SO NR 1 NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716918 145397 SHV - DURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040720001222004072000122NM 2004 7 20 DLM90040645 120040712A4997 TERMINAL DOUG MD90 MD9030 3023690NM APU BURNED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27909DA 53389 AFTER PUSHBACK STRONG SMELL OF ELECTRICAL FIRE, NO VISIBLE SMOKE. RAN ELECTRICAL FIRE CKLIST, STRONG SMELL NEAR F/C FLIGHT ATTENDANT JUMPSEAT. FOUND APU POWER RELAY PHASE A1 TERMINALS BURNT. REPLACED RELAY BASE AND CONTROL. FWD TO MCO/PLAC 49-10-01. APU INOP DUE TO TERMINALS BURNT. 2L72 4F RTA6WE 20040720001332004072000133EA 2004 7 20 SWIA200413503 120040624A2740 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07953SW 7813 STAB TRIM CH NR 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM CONTROL PANEL. OPS CHECK GOOD IAW MM 27-00-00. P/N 601R51706-3. 2L72 4F RTA21EA 20040720001342004072000134EA 2004 7 20 SWIA200413504 120040520A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 FS 484 ANGLE JUST OUTBOARD OF LBL 9 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW BRAS EO 601R-53-4997 ON FS 484 LBL 9 STEPS 6-9. 2L72 4F RTA21EA 20040720001362004072000136EA 2004 7 20 SWIA200413507 120040626A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07423SW 7456 STAB TRIM AND MACH TRIM CAUTION MESSAGES APPEARED ON CLIMBOUT. RETURNED TO FIELD. REMOVED AND REPLACED NR 1 STAB TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. P/N: 966-0013, S/N OFF: 341. 2L72 4F RTA21EA 20040720001382004072000138SO 2004 7 20 SWIA200413508 120040626A27203211001003 CONTROL UNIT EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CLCLIMB 1 NM07580SW1031310313 120348 COULD NOT PUSH RIGHT RUDDER PEDAL AFTER TAKEOFF. REPLACED RUDDER PCU PER MM 27-27-01. OP AND LEAK CHECK OK PER RII 27-312. 2L72 4T RTA31SO 20040720001402004072000140WP 2004 7 20 AALA20040713 120040707A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21203AA 49145 MSP - ENTRY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR ENTRY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720001412004072000141 2004 7 20 SWIA200413509 420040625A2210 AUTOPILOT SYS CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07907SW 7511 SHORTLY AFTER DISCONNECTING THE AUTOPILOT THE ELEVATOR JAMS. COULD NOT DUPLICATE PROBLEM WITH AUTOPILOT SYSTEM. OPS CHECKS GOOD IAW MM 32-11-00. 2L72 4F RTA21EA 20040721000052004072100005EU 2004 7 21 2004F00178 120040619A3260848401 PROXIMITY SENSOR AIRBUS320 A320233 3930329EU NLG MALFUNCTIONED A RJEFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO23451TA 733 DURING CLIMB, NLG REMAINED UNLOCKED & A/C RETURNED TO STATION FOR MX. AFTER LANDING, INSPECTION OF NLG PERFORMED PER AMM, & REMOVED TWO NLG PROXIMITY SENSORS PER AMM. PERFORMED BITE TEST PER AMM, & FOUND NORMAL. A VERIFICATION OF NLG HINGE BEARING CLEARANCES PERFORMED PER AMM & FOUND WITHIN LIMITS. A DETAILED VISUAL INSPECTION OF LANDING GEAR UPLOCK, DOOR UPLOCK UNITS & PINS WERE PERFORMED PER AMM 32-31-00-2000. ALSO, THE LGCIU (P/N 6647000500A4D)NR 1 WAS REPLACED AND TESTED PER AMM 32-31-71-000-001. A FUNCTIONAL AND OPERATIONAL TEST OF THE NORMAL EXTENSION RETRACTION WAS PERFORMED PER AMM 32-31-00-720-003. SATISFACTORY RESULTS WERE NOTED ON ALL THE SYSTEM. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M)2L72 4F RTA28NM 20040721000082004072100008EU 2004 7 21 SIMA200416001 120040602A53477253725191 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21384AE 340B384 ABI - DURING AN MBV INSPECTION, THE CABIN SEAT TRACK AT BL 0.0 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT THE WING BOX. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW TRACK IAW SAAB 340 SRM, 72LKS3079, REV 43, 53-70-60 PARA 8 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040721000152004072100015NM 2004 7 21 AMTA200400619 120040531A7100430101 CONTROL UNIT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT ENGINE FAILED A AMTAO OTHER J WARNING INDICATION DEDESCENT 1 GL11522AT 29330 31604 L ENGINE AND ENGINE LIMITER INOPERATIVE LIGHT ILLUMINATED. EICAS MSG L ENG EEC, L ENG LIMITER DISPLAYED. REMOVED AND REPLACED BOTH DGCU PER AMM 71-00-00-5 TEST NR 3. ALL CONDITIONS NORMAL. OK FOR SERVICE. (M) 2L72 4F4 FRTA2NM E12EU 20040721000212004072100021NE 2004 7 21 SIMA200415302 220040529A7261 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT LEAKING A SIMAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21222NE 340B222 GEE785504 DFW - FLT 3357 - ON CLIMB-OUT, RIGHT ENGINE LOST ALL OIL PRESSURE. CREW SHUTDOWN RIGHT ENGINE, DECLARED EMERGENCY AND RETURNED TO DFW LANDED SAFELY WITH NO OTHER PROBLEMS NOTED. REPLACED RIGHT ENGINE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20040721000252004072100025EU 2004 7 21 SIMA200415410 120040522A55117253707014 SPAR SAAB SF340 340B 7860101EU RT HORIZ STAB ELONGATED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 DURING A MBV INSPECTION OF AIRCRAFT, FOUR RIGHT HORIZONTAL STAB FORWARD UPPE SPAR CAP FASTENERS HOLES AT THE INBOARD END WERE FOUND TO BE ELONGATED. REAMED ALL FOUR HOLES TO .286 OVERSIZE CONDITION AND ACCOMPLISHED COULD WORKING. PERFORMED EDDY CURRENT INSPECTION INSPECTION OF REAMED HOLES, NO DEFECTS NOTED. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007138, SAAB SERVICE BULLETIN 340-55-034 AND STANDARD SAAB SRM, 72LKS 3079 REV 43, PRACTICES. (M) 2L72 4T RTA52EU 20040721000262004072100026EU 2004 7 21 SIMA200415404 120040509A53477253725191 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21400BR 340B400 DURING A MBV INSPECTION ONE AREA OF CORROSION WAS FOUND ON THE WEB OF SEAT TRACK BL 0.0 AT STATION 298.8. BLENDED THE CORRODED AREA. ONE CORROSION PIT REMAINED. COMPLETELY REMOVED CORROSION PIT BY DRILLING A NR 21 HOLE IN THE WEB. WET INSTALLED ONE MS20470ADS5-4 RIVET IN THE HOLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007059. (M) 2L72 4T RTA52EU 20040721000372004072100037EU 2004 7 21 USAASA04026 120040316A3350321430 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT WEAK A USAAK NONE L NO TEST ININSP/MAINT 1 EA19184US 1651 BDL - FOUND THE EMERGENCY POWER SUPPLY UNIT BATTERY WEAK AT THE L3 DOOR LOCATIONS. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POEWR SUPPLY UNIT AT THE L3 DOOR LOCATION. (M) 2L72 4F RTA28NM 20040721000412004072100041 2004 7 21 2004F00183 420040413A3418 WARNING LIGHT AIRBUS320 A320233 3930329EU AOA SYS FALSE INDICATIONA RYNAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE07941LF 461 DURING CRUISE FLIGHT WHILE FLYING THROUGH MODERATE RAIN, THERE WAS AN AOA DISCREPANCY. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO DFW. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. INSPECTED AOA VANES AND TESTED AUTOMATIC FLIGHT SYSTEM AFS. RAN BITE CHECKS OF AIR DATA REFERENCE SYSTEMS NR 1, NR 2 AND NR 3. NO FAULTS OR DISCREPANCIES NOTED. (M) 2L72 4F RTA28NM 20040721000422004072100042NM 2004 7 21 2004F00184 120040601A561069B10028101 WINDSHIELD BOEING747 747228F 1384895NM COCKPIT CRACKED A Q2SAH DEACTIVATE SYST/CIRCUITS M OVER TEMP CRCRUISE 1 NE03751SA 22678 CAPTAINS NR 1 WINDOW STARTED ARCING FIVE HOURS INTO FLIGHT THEN CRACKED SHORTLY AFTER. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST IAW QUICK REF QRH. REMOVED AND REPLACED CAPTAINS NR 1 L-1 WINDOW IAW AMM 56-11-01. (M) 2L74 4F A20WE 20040721000452004072100045EU 2004 7 21 SIMA200415407 120040522A53117253813007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21388AE 340B388 DURING AN MBV INSPECTION, FRAME 258 WAS FOUND TO HAVE CORROSION BENEATH A PREVIOUS DOUBLER REPAIR. REMOVED THE PREVIOUS DOUBLER, SHIMS, AND FILLER. DOUBLER AND SHIMS INSPECTION AND FOUND TO BE SERVICEABLE. COMPLETELY REMOVED CORROSION BY CUT OUT. PERFORMED EDDY CURRENT OF THE CUTOUT NO DEFECTS NOTED. FABRICATED A FILLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007122 AMDT 1 AND STANDARD SRM, 72LKS 3079 REV 43, PRACTICES. (M) 2L72 4T RTA52EU 20040721000472004072100047 2004 7 21 A6WA200440076 420040610A3414 INDICATOR CNDAIRCL600 CL6002B19 1900309EA STANDBY AIRSPEEDINOPERATIVE A A6WAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL31426AW 7669 STANDBY AIRSPEED INOPERATIVE DURING TAKEOFF ROLL AT 80-90 KNOTS. ABORTED TAKEOFF. COMPLIED WITH ABORTED TAKEOFF INSPECTION, NO DEFECTS. PERFORMED P3 CONTAMINATION REMOVAL PER TASK 34-11-00-100-806, AND LEAK TESTED. NO LEAKS DETECTED. (M) 2L72 4F RTA21EA 20040721000482004072100048WP 2004 7 21 AMTA200400681 120040607A3350516574 CHARGER LKHEED1011 10113853 5265020WP EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11163AT 1229 EGRESS LIGHT FOR R-1 DOOR INSIDE AND OUT DO NOT ILLUMINAT. REMOVED AND REPLACED EMERGENCY POWER PACK AT R1 DOOR IAW MM 33-51-03. OPS CHECK NORMAL. (M) 2L73 4F A23WE 20040721000492004072100049SO 2004 7 21 SIMA200415401 120040529A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21800AE 145425 DLH - FLT 4465 - OPERATIONS REPORTED THE EMERGENCY LGIHTS ON THE AIRCRAFT ARE IN THE ON POSITION AND COULD NOT ACCESS THE COCKPIT. EMERGENCY BATTERY PACKS ARE LOW. REPLACED 4 BATTERY PACKS P/N 2013-1A S/N 73055, P/N 2013-1A S/N 69967, P/N 2013-1A S/N 73159, P/N 2013-1A S/N 70931. (M) 2L72 4F RTT00011AT 20040721000512004072100051NM 2004 7 21 AMTA200400678 120040603A760344111115 CONTROL BOX BOEING757 75723N 1384973NM NR 1 ENGINE MALFUNCTIONED A AMTAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL11520AT22435 27976 SEVERAL TIMES DURING DESCENT LEFT THROTTLE LEVER WOULD JAM AND WAS NOT ABLE TO BE POSITIONED TO IDLE. FORCING T-LEVER FORWARD FREED MOVEMENT. REMOVED AND REPLACED NR 1 ENGINE LOWER CONTROL BOX ASSEMBLY PER 76-11-10-4. NO BINDING NOTED AT THIS TIME AT THIS TIME. PERFORMED EEC TEST PER 76-11-10-4. NO FAULTS NOTED. PERFORMED TEST 10 PER 22-32-01-714-017-A/T TEST PASSED AT THIS TIME. (M) 2L72 4F RTA2NM 20040721000602004072100060NM 2004 7 21 ANCF200400017 120040711A2741 MODULE BOEING767 767284 1385184NM STAB TRIM FAILED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23988AN 24742 UNSCHEDULE STAB TRIM DISPLAYED DURING TAKE OFF ROLL. CHECKED SAMS NO FAULTS BALLS SET-CARRIED OUT FIM 27-09-00 FIG 106A BLOCKS 1+2 STAB TRIM TRIED WITH C/C SWS STAB TRIM ALT SWS MOVEMENT CORRECT-CUT OUT SWS TRIED AND FUNCTION ON (NO MOVEMENT). IAW AMM 27-41-11 /401 THE LT STCM WAS REPLACED, TEST ON GROUND SATISFACTORY 2L72 4F RTA1NM 20040721000722004072100072NM 2004 7 21 04FDEA02056 120040712A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FORWARD CABIN SEAT TRACK AT STA 495 APRROXIMATELY 27.5 CORRODED. REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SET TRACK TRIMMED, REWORKED AND REPAIR PARTS INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20040721000742004072100074NM 2004 7 21 04FDEA02014 120040707A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040721000782004072100078EU 2004 7 21 04FDEA02072 120040714A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE SEAT TRACK NR 2 RT BETWEEN FR26 AND FR38.2 HAS CORROSION ON FR 26.8, FR 28.5, FR30.2, AND 32.7. REF SNRM N00401. REMOVED AND REPLACED SEAT TRACK IAW A300/600 SRM 53-10-16. 2L72 4F RTA35EU 20040721000852004072100085WP 2004 7 21 04FDEA01887 120040630A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP FUSLEAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING P TO F MODIFICATION AND TRANSITION CHECK, FOUND DRILLED ADA3203-33 FLOOR PANEL STA 879-824 AT X /- 75.25 PROCURE DAMAGED HOLES .440 INCH Q/TA 5 HOLE ON EXISTING SEAT TRACK. PERFORM REPAIR IAW SRM 57-70-00 FIG 1A VOL I. INSTALL P/N WSP0414-7, ACA7414-3. 2L73 4F A22WE 20040721000872004072100087WP 2004 7 21 04FDEA01889 120040630A5311 FRAME DOUG DC10 DC1030 3023501WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 AREA AFT OF AFT CARGO COMPARTMENT BILGE HAS AREA OF CORROSION, FS 1971, RBL 8 TO LBL 4. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC10 SRM 53-00-01, FIG 7 VOL I AND DC10 SRM 51-33-01 VOL 2 AND DC10 SRM 51-35-01. 2L73 4F A22WE 20040721001012004072100101NM 2004 7 21 04FDEA02094 120040716A5315 FLOORBEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION 870 FLOORBEAM UPPER SECTION RBL 20 & RBL 26 WL 208. REMOVED CORROSION ON 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208. FOUND 870 BEAM UPPER CHORD, RBL 20 TO RBL 26, WL 208 TO BE IN LIMITS IAW SRM 53-10-1, FIG 8. 2L73 4F RTA3WE 20040721001032004072100103NM 2004 7 21 04FDEA02096 120040716A5330 SKIN BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 (C54-451-01, 2) EXTERNAL FUSELAGE SKIN PILLOWED & EMINATING POWDER AT BUTT JOINTS BS 1363-1379, 6 INCHES OVER NR 2 ENGINE CUTOUT, RT SIDE. REMOVED DAMAGE SKIN PANEL AT BS 1363 TO 1379 AND FABRICATED NEW PANEL. ALODINE, PRIMED AND PAINTED NEW PANEL. INSTALL PANEL IAW SRM 51-30-2, 53-30-1 AND FED EX MM 51-21-151. 2L73 4F RTA3WE 20040721001062004072100106NM 2004 7 21 04FDEA01904 120040701A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.656. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED. 2L73 4F RTA22WE 20040721001082004072100108WP 2004 7 21 04FDEA02100 120040717A5740ANB7434 FITTING DOUG DC10 DC1030 3023501WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 C/W EA 8-5720-79541 WINGS INBOARD FLAP SIDE LOAD SUPPORT FITTING CORROSION REPAIR P/N ANB7434. COMPLIED WITH EA 8-5720-79541. 2L73 4F A22WE 20040721001112004072100111NM 2004 7 21 04FDEA01908 120040701A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.443, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RIGHT OUTBOARD FLAP - SUPPORTS CORRODED 2L73 4F RTA22WE 20040721001122004072100112EU 2004 7 21 04FDEA02059 120040713A2410 GENERATOR AIRBUS310 A310324 3930206EU NR 1 FAILED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25801FD 539 ON TAKEOFF CDG NR 1 GEN FAULTED ECAM ALERT AT 60 KTS. REJECTED T/O NR 1 GEN WOULD NOT RESET. SEE PREVIOUS MEL 13JUL04 09:42 RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 16JUL04 MEL 24-11-01: GEN 1 IDG INOP. 2L72 4F RTA35EU 20040721001182004072100118EU 2004 7 21 04FDEA02065 120040713A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 UPPER MAIN CABIN ZONE 220 AT Y1456 FR 15A - FR 14 TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-72-10, ZONE 220 AT Y1456 FR15A-FR14. 2L72 4F RTA35EU 20040721001212004072100121NM 2004 7 21 SWAA042030 120040718A57536546435274 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RIGHT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040721001222004072100122NM 2004 7 21 SWAA042031 120040718A53106517684 DOOR FRAME BOEING737 7375H4 138449DNM R1 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME, LOWER AFT CORNER CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040721001242004072100124 2004 7 21 SWAA042033 420040718A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29732SW 27864 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040721001252004072100125NM 2004 7 21 SWAA042034 120040717A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 793.5, STRINGER 18L, BS 840, STRINGER 15L, CRACKED. REPAIRED SKIN PER EA & SRM. 2L72 4F RTA16WE 20040721001362004072100136NM 2004 7 21 SWAA042039 120040719A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED RON, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD ENTRY EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040721001422004072100142NM 2004 7 21 SWAA042044 120040719A3350OL3071BPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 3 ABC, INOP. RELAMPED PER BULL NOSE LIGHT PER MM. 2L72 4F RTA16WE 20040721001432004072100143NM 2004 7 21 SWAA042045 120040719A3350OL3071BNPEGPL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED C1 CHECK, FOUND FWD RIGHT EEPLS INOP. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20040721001502004072100150SO 2004 7 21 RAIA00407006 120040714A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO SMOKE DETECTOR FALSE ACTIVATIONA RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03837HK 145255 LAV SMOKE ON EICAS THROUGH 13,000 FT, ICE PROTECT CAME ON ABOUT THE SAME TIME. INSPECTED ELECTRICAL SYSTEM AND LAV COULD NOT DETECT ANY SMOKE. 2L72 4T RTT00011AT 20040721001522004072100152 2004 7 21 SWIA200413545 420040617A34446222937004 INDICATOR EMB 120 EMB120ER 3260203SO RADO ALTIMETER FAILED A SWIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07236SW6231 6231 120312 BUZZING SOUND AND SMOKE FROM LEFT SIDE INSTRUMENT PANEL. PULLED CIRCUIT BREAKER ON RADIO ALTIMETER, NOISE STOPPED. REPLACED RADIO ALTIMETER WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040721001542004072100154EA 2004 7 21 SWIA200413547 120040704A2721 KNOB CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07409SW 7056 RUDDER TRIM STICKS TO LEFT. CLEANED AND RE-ADJUSTED RUDDER TRIM KNOB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040721001592004072100159 2004 7 21 RAIA00407002 420040705A3421 COMPUTER EMB 145 EMB145LR 3260212SO NR 2 AHRS MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03813HK 145044 5752 - STL - AHRS NR 2 FAIL. MAINTENANCE RE-RACKED NR 2 AHRS AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040721001622004072100162NM 2004 7 21 MEX2004059 120040214A30101059842 VALVE DOUG MD88 MD88 3023688NM ANTI ICE SYS FAILED A ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23169PL 53175 FLT 610 - CUN-MEX - FLIGHT RETURNED, 'AIR FOIL ICE PROTECT' OUT OF SERVICE AT 31,000 FEET WITH ICING CONDITIONS. DURING REVISION THE WINGS AND TAIL ANTI-ICE VALVES WERE TESTED AND RELAY R2-189 WAS ADJUSTED. DURING OVERNIGHT SERVICE THE H3766020 AND 2H378C20 ELECTRIC LINES WERE CHECKED AND RELAY R5-1203 WAS FOUND WITH PINS DAMAGED. IT WAS REPAIRED IAW WDM 30-11-01 AND ANTI-ICE VALVES WERE REPLACED IAW MM 30-10-02 AND 30-10-03, TEST CORRECT IAW MM 36-10-00. (M) 2L72 4F RTA6WE 20040721001652004072100165GL 2004 7 21 UIEA200400003 220040110A72611978M64G01 LINE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 4 ENGINE CRACKED A UIEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15412MC 30559 706125 PRECAUTIONARY NR 4 ENGINE SHUTDOWN DUE TO OIL QUANTITY FALLING TO 3 QUARTS AT 1825Z, FL300, MACH .835. FOUND OIL LINE TO LUBE AND SCAVENGE PUMP CRACKED IPC 79-21-03-01 ITEM 303. REPLACED LINE IAW MM 79-21-00, SERVIED ENGINE OIL IAW MM 12-13-03. PERFORMED MPA RUN UP IAW MM 72-00-00, FOUND ALL SATISFACTORY. (M) 2L74 4F4 FRT1384945 E23EA 20040721001662004072100166NM 2004 7 21 USAA040021 120040119A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU60654 22205 CLT - FOUND INTERCOSTAL CRACKED 1 INCH N LENGTH, STATION 660, S-16R WING SCANLIGHT INERCOSTAL. DAMAGE REMOVED, FILLER ANGLE AND REPAIR ANGLE INSTALLED PER EA 94837. (M) 2L72 4F RTA2NM 20040721001692004072100169NM 2004 7 21 TSAA0453023 120040120A53106520722 DOOR FRAME BOEING737 7372M6C 1384708NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 FOUND CRACK ON LOWER INBOARD CORNER OF FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. VERIFIED CRACK REMOVED USING HFEC INSPECTION. FABRICATED A REPAIR ANGLE, ALODINED, AND PRIMED. INSTLALED REPAIR PARTS. REPAIR COMPLETED IAW ECO 1763. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040721001722004072100172 2004 7 21 P9RA20040021 420040718A2565D30654122 SLIDE BOEING757 757236 1384971NM L1 DOOR DEPLOYED A P9RAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11521NA 25592 AIRCRAFT IN MAINTENANCE. L1 DOOR SLIDE INADVERTENTLY DEPLOYED BY MAINTENANCE. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 256601 2L72 4F RTA2NM 20040721001772004072100177NM 2004 7 21 TSAA0453025 120040201A533065465485 SKIN BOEING737 737230 1384401NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13818AL 22117 TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL X. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040721001792004072100179NM 2004 7 21 TSAA0453028 120040202A53306552879 SKIN BOEING737 737209 13844AENM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13827AL 23913 TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED IAW ECO 2840R2, DEVIATION C. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040721001822004072100182EA 2004 7 21 REXA04001 120040117A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE INDICATIONA REXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO258847A 7847 UPON CLIMB-OUT AT 3000 AGL, RECEIVED LAVATORY SMOKE MESSAGE. INSPECTED LAVATORY SMOKE SYSTEM AND PERFORMED OPERATIONAL TEST ALONG WITH ENGINE RUNS COULD NOT DUPLICATE, FOUND TO BE FALSE WARNING. (M) 2L72 4F RTA21EA 20040721001832004072100183NE 2004 7 21 WRLA200404 220040111A7230S6A621 FAN BLADE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 2 ENGINE DAMAGED A WRLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO11274WA 48633 ON TAKEOFF ROLL, ENGINE 2 EVM COMP READ 5.0 UNITS WITH STRONG VIBRATION. TAKEOFF ABORTED BELOW 80 KNOTS. REMOVED AND REPLACED FOUR EACH FAN BLADES ON NR 2 ENGINE PER MM 72-31-02 PERFORMED ENGINE RUN AT 95 PERCENT N1 EVM COMP 7 READING, OPS CHECK GOOD. REPLACED DAMGAED FAN BLADES. (M) 2L73 4F4 FRTA22WE E24NE 20040721001842004072100184NM 2004 7 21 AMTA200400032 120040109A7500430101 CONTROL UNIT BOEING757 75723N 1384973NM LT ENGINE MALFUNCTIONED A AMTAO OTHER O OTHER DEDESCENT 1 GL11518AT 27974 ON DESCENT PASSING THROUGH 16,000 FEET SUSPECTED ENGINE SURGE. AT 11,000 FEET, NOTICED RIGHT ENGINE FUEL FLOW AND EGT HIGHER. FUEL FLOW ABOUT 1000 LBS HIGHER THAN LEFT ENGNE AND EGT ABOUT 100 DEGREES HIGHER THAN LEFT ENGINE. ON POST RIGHT ENGINE SURGE BITE EICAS MSG. REMOVED AND REPLACED DGCU IAW MM 73-21-10-4, LOWER RIGHT ENGINE. (M) 2L72 4F RTA2NM 20040721001852004072100185NE 2004 7 21 MEX2004044 220040203A7230821501 DISC DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED A ASMFK NONE O OTHER ININSP/MAINT 1 SW23XATWT 49706 718240 DURING TRANSIT CHECK, MAINTENANCE FOUND DAMAGE OUT OF LIMITS, CAUSED BY FOD IN THE RT ENGINE FAN BLADES. TECHNICAL PERSONNEL WAS SENT TO HMO TO ATTEND THE DAMAGES. THE C1 DISK WS REPLACED AND ENGINE TESTED IAW MM 72-00-3, ALL CORRECT. (M) 2L72 4F4 FRTA6WE E9NE 20040721001862004072100186NM 2004 7 21 MEX2004045 120040204A3213 SEAL DOUG MD88 MD88 3023688NM NLG FAILED A ASMFA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW23169PL 53175 FLT 118 - GDL-TIJ - AIRCRAFT RETURNED DUE TO NLG DID NOT GO AND AND NLG RED LIGHT CAME ON, THE HORIZONTAL STABILIZER AND PRESSURIZATION WERE OUT OF CONTROL, SEVERAL ALARMS WERE ACTIVATED, TCAS WAS OUT OF SERVICE AND STALL INDICATOR FAILURE AND AUTO BRAKE FAIL LIGHTS CAME ON. AIRCRAFT LANDED WITH MAXIMUM LANDING WEIGHT. THE NLG WAS FOUND WITHOUT NITROGEN PRESSURE. THE NLG'S PACKINGS WERE REPLACED AND SYSTEM TESTED IAW MM 32-21-02, THE HORIZONTAL STABILIZER WAS TESTED, OVERWEIGHT INSPECTION WAS PERFORMED IAW MM 05-51-04 AND THE FLIGHT DATA RECORDER WAS REPLACED IAW MM 31-31-01. AIRCRAFT FLIGHT FERRY TO MEX. (M) 2L72 4F RTA6WE 20040721001872004072100187NM 2004 7 21 MEX2004046 120040204A3213 SEAL DOUG MD88 MD88 3023688NM NLG FAILED A ASMFA UNSCHED LANDING FG FLT CONT AFFECTED MULTIPLE FAILURE CLCLIMB 1 SW23169PL 53175 FLT 118 - GDL-TIJ - DURING OVERNIGHT SERVICE, NLG SEALS WERE REPLACED IAW MM 32-21-02. GROUND SENSING CONTROL MECHANISM WAS VERIFIED IAW MM 32-23-01, STEERING SYSTEM TEST ACCOMPLISHED IAW MM 32-50-00. LUBRICATION WAS PERFORMED IAW MM 12-21-04 AND NLG EXTENSION AND RETRACTION WAS ACCOMPLISHED IAW MM 32-30-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20040721001882004072100188NM 2004 7 21 MEX2004069 120040220A24209008D093 RELAY DOUG MD80 MD83 3023681NM RT GENERATOR FAILED A ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23881LF 53051 AIRCRAFT RETURNED TO GATE, RIGHT GENERATOR FAILED. WHEN GENERATOR WAS SHUTDOWN THE FREQUENCY AND VOLTAGE WERE CORRECT, BUT WHEN SWITCH WAS IN 'ON' POSITION THE GENERATOR FAILED. THE GENERATOR WAS DEFERRED IAW MEL 24-1. CAPTAIN REQUEST RIGHT CSD INOPERATIVE AND AIRCRAFT WAS REFUELED FOR DISPATCH. DURING OVERNIGHT SERVICE, THE RELAYS R2-34 AND R2-42 WERE REPLACED IAW MM 24-20-06, TESTS CORRECT. (M) 2L72 4F RT 20040721001902004072100190CE 2004 7 21 2004F00166 120040209A2740EM407011 ACTUATOR CESSNA750 750 2076810CE VERTICAL STAB INOPERATIVE A UG8AO OTHER O OTHER CRCRUISE 1 GL235113 7500013 'RUDDER LIMIT FAIL B' CAS MESSAGE ILLUMINATED IN FLIGHT. AIRCRAFT LANDED WITH NO FURTHER DISCREPANCIES. LINEAR ACTUATOR OF LOWER RUDDER LIMITER 'B' FAILED AT 16 PERCENT. REPLACED LOEWR RUDDER LIMITER ACTUATOR ASSEMBLY AND PERFORMED APPROPRIATE RIGGING PROCEDURES FROM CESSNA MM. OPERATION WAS NORMAL. (M) 2L72 4J RTT00007WI 20040721001912004072100191EA 2004 7 21 A6WA200440010 120040113A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 RIVET ON RIGHT FUSELAGE SKIN AT FS 265 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 INCH DIAMETER, PERFORMED EDDY CURRENT TO ENSURE NO CRACKS EXISTED AND DAMAGE WAS REMOVED. INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578. (M) 2L72 4F RTA21EA 20040721001942004072100194NE 2004 7 21 A6WA200440008 220040117A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 VIBRATION A A6WAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL31422AW 7341 872581 NR 1 ENGINE INDICATES VIB YELLOW CAUTION ON TAKEOFF ROLL BELOW 60 KNOTS. ABORTED TAKEOFF, NO VIBRATION FELT. REVIEWED HISTORY, PERFORMED TWO SEPARATE ENGINE POWER RUNS, NO VIBRATION NOTED. FAN BLADE INSPECTED, NO DISCREPANCIES. TAKEOFF WAS PERFORMED IN SEVERE ICING CONDITIONS. SUSPECT ICE BUILD-UP ON FAN. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040722000012004072200001EU 2004 7 22 2004F00188 120040619A79311047PGSB SWITCH FOKKERF27 F27MK600 4990706EU RT ENGINE MALFUNCTIONED A COEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM13730FE 10386 DURING CLIMB-OUT FROM RAP AT 11,000 FEET, THE RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATD. THE CREW SHUT DOWN THE RIGHT ENGINE AS A PRECAUTION. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO RAP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE OIL PRESSURE WARNING SWITCH. OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20040722000022004072200002NM 2004 7 22 GAIA04081OP 120040616A27511812993 INDICATOR BOEING727 727251 138408HNM TE FLAPS INOPERATIVE A GAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07279US 21158 ON CLIMB-OUT INBOARD FLAPS WOULD NOT RETRACT PAS 2 DEGREES. CREW RETURNED TO FWA WHERE A LANDING WAS MADE WITHOUT INCIDENT, LANDED AT 167600 LBS. REMOVED AND REPLACED INBOARD FLAP POSITION INDICATOR AND LUBED FLAP QUADRANT ASSEMBLIES. RAN FLAPS SEVERAL TIMES ON GROUND, OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW 5-51-271, NO DEFECTS FOUND. AIRCRAFT IS SAFE FOR FLIGHT AND WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040722000062004072200006NM 2004 7 22 C7WA200400008 120040309A5311 FRAME BOEING727 727231 1384079NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO1754354 21986 FOUND LOWER FUSELAGE FRAME AND SKIN CORRODED FS 1140 STRINGER 29 RT. REMOVED CORROSION, SKIN CORROSION REMOVED WITHIN ALLOWABLE DAMAGE LIMITS PER 727 SRM 53-30-1 FIG 2. REPAIRED FRAME IAW 727 SRM 53-10-4 FIG 12. (M) 2L73 4F A3WE 20040722000162004072200016SO 2004 7 22 2004F00195 120040528A3231 STRIKER GULSTMGV GULFSTREAMGV3980116SO MLG DOOR SWITCH LOOSE A UG8AO OTHER J WARNING INDICATION CRCRUISE 1 GL23661GA 561 2 HOURS & 25 MIN INTO FLT, BOTH ENG WENT TO FLT IDLE WITH AUTO-THROTTLES ENGAGED. AUTO-THROTTLES DISENGAGED & THROTTLES PUSHED BACK TO CRUISE. AUTO-THROTTLES REENGAGED WITH NO PROBLEMS. A/C MANUFACTURER REVEALED THIS CONDITION OCCURRED BEFORE WITH A G-V A/C. INTERMITTENT MLG DOOR OPEN SIGNAL WILL CAUSE AFCS SYS LOGIC TO RETARD THROTTLES SO A/C WONT EXCEED V(LE). CAN BE CAUSED BY MLG DOOR SWITCH MISRIGGING. DUPLICATED ON GROUND AT GAC. DETAILED MLG SYS INSP ACCOMPLISHED. RT MLG, OUTER DOOR SWITCH NOT CONTACTING STRIKER PLATE WHICH COULD HAVE CAUSED MISRIGGING CONDITION AT CRUISE. PLATE REPOSITIONED & SWITCH RIGGED PER THE G-V MM, AN FDR DOWNLOAD SHOWED NO IN-FLT FAULTS. A/C WAS RETURNED TO SERVICE. (M) 2L72 4F RTA12EA 20040722000202004072200020NM 2004 7 22 GAIA04082OP 120040616A2150656022936 DUCT BOEING727 727251 138408HNM ACM BLOWN A GAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07278US 21157 DURING CRUISE,UNABLE TO MAINTAIN CABIN ALTITUDE AT FLIGHT LEVEL 310, DIVERTED TO MSP. LANDED AIRCRAFT AT 169000 LBS, LANDING WAS UNEVENTFUL. FOUND BLOWN DUCT ON RIGHT PACK FROM FORWARD HEAT EXCHANGER TO COMPRESSOR DISCHARGE PORT OF ACM. REMOVED AND REPLACED RIGHT 35 DEGREE VALVE AND RIGHT COALESCER BAG PRECAUTIONARY. REMOVED AND REPLACED DUCT ASSEMBLY OP CHECKS AND LEAK CHECKS GOOD. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION, NO DAMAGE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040722000222004072200022 2004 7 22 2004F00198 420040330A3460B546CCM0104 COMPUTER AIRBUS320 A320233 3930329EU FMGC MALFUNCTIONED A RJEFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23991LR 561 SAL-TGU-SAP - FLT TA390 - DURING CLIMB, MULTIPLE ECAM WARNING MESSAGES ON SCREEN CAME ON, CABIN PRESSURE, LANDING ELEVATION, NAV ILS R FAULT, AUTO FLT, NAV GPWS, UNABLE CAPTAIN SIDE TO SELECT VOR ON RMP NR 1 AND THEN ON NR 2 ALSO ND NR 1 INOP, FIRST OFFICER AND CAPTAIN PROBE. AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING AT SAL STATION, MAINTENANCE TECHS BITE TESTED THE AUTO FLIGHT SYSTEM PER AMM 22-96-00 AND FOUND THAT THE FMGC NR 1 FAULTY. THE UNIT WAS REPLACED AND TESTED PER AMM 22-83-34. ALL WAS FOUND NORMAL AFTER THE REPLACEMENT AND TEST OF THE FMGC. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040722000242004072200024GL 2004 7 22 15HA0358008 220040107A7200 ENGINE CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL LEFT MALFUNCTIONED A I5HAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL23584E 24 500726 DURING THE DESCENT INTO MEM, THE PILOT OBSERVED THE 'LOW OIL PRESSLURE' LIGHT ILLUMINATE FOR THE LT ENGINE AND AN ASSOCIATED LOSS OF OIL QUANTITY TO ZERO GALLONS. THE CREW PERFORMED AN INFLIGHT EMERGENCY SHUTDOWN USING THE 'E' HANDLE. THE AIRCRAFT MADE AN UNEVENTFUL SINGLE ENGINE LANDING IN MEM. THE LEFT QEC WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4R4 T 6A6 E282 20040722000262004072200026WP 2004 7 22 2004F00202 220040106A7250 BEARING LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP LP TURBINE FAILED A EXOAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 SO1732HJ 463 P74855 RT ENGINE TEMP (ITT) RISE FOLLOWED BY OIL PRESSURE FLUCTUATIN, O/P DROPPED TO YELLOW. ENGINE SHUT DOWN, EMERGENCY DECLARED, UNEVENTFUL LANDING SUSPECT LPT MODULE BEARING FAILURE. ENGINE SENT TO GARRETT FOR EXAMINATION. (M) 2L72 4F4 F A10CE E6WE 20040722000342004072200034NM 2004 7 22 USA2004F00093 120040626A3200 CIRCUIT BREAKER BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE MLG TRIPPED A USAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 EA19522AU 23857 ON APPROACH, CREW DID NOT RECEIVE ANY LANDING GEAR INDICATION LIGHTS AFTER GEAR EXTENSION. A MISSED APPROACH WAS EXECUTED. CREW TESTED THE LIGHTS BUT HAD NO ILLUMINATION OF THE GEAR LIGHTS. BULBS CHECKED OK ALONG WITH CIRCUIT BREAKERS. MAINTENANCE FOUND THE SECTION 5, MASTER CAUTION CB TRIPPED. RESET BREAKER. OPERATIONAL CHECK GOOD. NO FURTHER REPORTS AS OF 7/2/2004. 2L72 4F4 FRTA16WE E2GL 20040722000382004072200038NM 2004 7 22 USA2004F00083 120040626A2150 WARNING LIGHT BOEING767 767201 1385125NM GE CF6 CF680 30025NE E/E BAY ILLUMINATED A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19645US 23897 ENROUTE, THE FORWARD EQUIPMENT COOLING LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH IN THE STANDBY MODE. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND AND FLIGHT MODE TESTS OF THE EQUIPMENT COOLING SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA1NM E13NE 20040722000392004072200039EA 2004 7 22 REX2004F00003 120040629A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE APU BAY LEAKING A REXAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO258505Q8938 4567 7505 AT APPROX 1000 FEET AGL ON INITIAL CLIMB OUT, THE FLIGHT CREW OBSERVED A LIGHT BLUE SMOKE COMING FROM THE AIR VENTS. THIS WAS FOLLOWED BY A REPORT OF SMOKE IN THE CABIN AND A TOILET SMOKE WARNING. FLT CREW DONNED THEIR OXYGEN MASKS AND DECLARED AN EMERGENCY. ON REDUCTION OF THRUST, THE SMOKE STARTED TO CLEAR. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS PERFORMED. NO EVACUATION OF THE PASSENGERS WAS ORDERED DUE TO THE FACT THAT THE SMOKE HAD DISSIPATED. MAINTENANCE FOUND THE SOURCE OF THE SMOKE TO BE OIL COMING FROM THE APU BLEED INTO THE ACM`S. THE APU WAS REPLACED AND THE ACM PIPING AND FILTERS CLEANED. SUBSEQUENT GROUND RUN OF THE APU AND MAIN ENGINES WERE NORMAL. 2L72 4F4 FRTA21EA E15NE 20040722000422004072200042EU 2004 7 22 USA2004F00088 120040609A5347R53070089202 SEAT TRACK AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FOUND CORROSION ON SEAT TRACK, 1 INCH X 5 INCHES X .032 INCH. INSTALLED NEW SEAT TRACK SEGMENT AND SPLICES IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040722000452004072200045NM 2004 7 22 USA2004F00094 120040630A335020121 CHARGER BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19512AU 23595 FOUND SEVERAL AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANE REPLACED THE AFT BATTERY AND CHARGER. 2L72 4F4 FRTA16WE E2GL 20040722000492004072200049 2004 7 22 SDR2004035 420040528A83003037223 SEAL AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE ACC GEARBOX WORN A TRBAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO21246AE 243 121032 RT ENGINE OIL PRESSUE FLUCTUATED. EVIDENCE OF OIL LEAK NOTED. REPLACED ENGINE ACCESSORY GEAR BOX BREATHER TUBE SEALS. 2H72 4T4 TRTA53EU E20NE 20040722000532004072200053EA 2004 7 22 ASO2004F00019 120040603A3220521153 TORQUE LINK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG DISCONNECTED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27716EV3466 SP0101 10084 DURING CLIMB OUT, THE CREW SELECTED GEAR UP AND THE GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. SEVERAL SECONDS LATER THEY RECEIVED A WEIGHT ON WHEELS INPUT CAUTION MESSAGE FOLLOWED BY A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT RETURNED TO PHF. NORFOLK APPROACH DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY BACK IN PHF. MAINTENANCE FOUND THE (NLG) UPPER AND LOWER TORQUE LINK ASSEMBLIES DISCONNECTED AND RECONNECTED THEM. OPERATIONAL CHECKS GOOD DURING GROUND TAXI CHECK. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040722000642004072200064EA 2004 7 22 REX2004F00001 120040601A490038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE ODOR A REXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO258444F3570 7444 ELECTRICAL/AC SMOKE IN CABIN. EVACUATED AIRCRAFT-MECHANIC NOTIFIED. PERFORMED ENG RUNS/BLEED AIR CHECKS IAW. NO SMOKE NOTED. OK FOR SERVICE. SMOKE IN CABIN ON APU START WITH PACKS ON APU. DEFERRED APU IAW MEL, CAT C AUTHORIZATION NR 48877. DM48877 IS DUE BY 6/12/04, WITH MAINTENANCE COMMENTS OF (6/02 STRONG OIL SMELL IN CABIN WHEN PACKS RUN OFF APU. NO SMELL REPORTED WHEN SUPPLIED BY ENGINES IN FLIGHT. EVACUATED THE AIRCRAFT. CAPTAIN DID NOT DECLARE AN EMERGENCY. 2L72 4F4 FRTA21EA E15NE 20040722000682004072200068SO 2004 7 22 SIMA200417206 120040617A783014577751407 THRUST REVERSER EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL RT ENGINE CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21622AE 145108 DURING MBV INSPECTION THE RT THRUST REVERSER HAS APPROXIMATE 3 INCH CRACK AT THE FORWARD LOWER OB SECTION. REPAIRED CRACK IAW MFG SRM. 2L72 4T4 FRTT00011ATTE6CH 20040722000712004072200071CE 2004 7 22 JEM2004F00006 120040617A551145A210854 RIB BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS, THE FOLLOWING PARTS WERE CHANGED: 1) 45A21146-6, 2) 45A21146-5, RIBS: 3) 45A21086-3, 4) 45A21086-4, 5) 45A21085-3, 6) 45A21085-4. 2H72 4F4 FRTA16SW E1NE 20040727000012004072700001NM 2004 7 27 04FDEA02143 120040720A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 MECHANICAL DAMAGE IN MAIN CARGO ON STRINGER AT BS 442 STR 5L. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-10-3, 51-30-2, 51-10-2 AND 51-10-6. INSTALLED REPAIR PARTS PER SRM 51-10-6 AND 51-30-2. 2L73 4F RTA3WE 20040727000032004072700003NM 2004 7 27 04FDEA02145 120040721A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 MAIN DECK, SEAT TRACK LBL 47 FOUND WITH DEEP SCRATCHES AT STA 1100. NEW TRACK AND SPLICE REWORKED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I. 2L73 4F RTA22WE 20040727000042004072700004NM 2004 7 27 04FDEA02147 120040721A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 MAIN DECK, LEFT HAND MOST OUTBOARD SEAT TRACK CORRODED AT L1 DOORWAY. CORRODED SEAT TRACK AT MAIN DECK, LEFT HAND MOST OUTBOARD AT L1 DOORWAY REMOVED AS PER SRM 51-31-01, VOLUME II AND REPLACED AS PER SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040727000212004072700021NM 2004 7 27 SWAA042083 120040722A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED AT BS 727A TO BS 727B, RT SIDE. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040727000232004072700023 2004 7 27 SWAA042085 420040722A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040727000292004072700029WP 2004 7 27 04FDEA02165 120040723A5330ALC7205501 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING PASSENGER TO FREIGHTER CONVERSION FOUND ON PANEL 7205 -1 LT SIDE FOUND BY ULTRASONIC INSPECTION NR 1 HOLE WITH CRACK L= 1.25 - 1.65 INCH ON BOTTOM NR 6 POSITION. COSTANT SKIN SECTION REPLACEMENT PER EA 8-5510-70126. 2L73 4F A22WE 20040727000302004072700030EU 2004 7 27 04FDEA02068 120040713A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MDC, LATERAL SEAT RACK AT FRAME 44 BETWEEN SEAT TRACK R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OF TRACK ON OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW SRM 51-72-10. 2L72 4F RTA35EU 20040727000372004072700037NM 2004 7 27 04FDEA02108 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.395 AND REPAIRED AS PER EA NR 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000432004072700043NM 2004 7 27 04FDEA02131 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.002, REMAINING THICKNESS=0.504, AND REPAIRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000482004072700048NM 2004 7 27 04FDEA01855 120040625A5511ALC8131501 SPAR CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND HORIZONTAL STABILIZER NR 36L FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT AS PER SB MD11 55-023. HORIZONTAL STABILIZER NR 36L BARREL NUT BORE REPAIR CARRIED OUT AS PER FEDEX EA 1-5510-78026. HORIZONTAL STABILIZER BARREL NUT BORE NR 36L CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040727000492004072700049NM 2004 7 27 04FDEA01856 120040625A5510ALC8103 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 EMPENNAGE HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 35R SIDEWALL CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPENNAGE HORIZONTAL STABILIZER RIGHT HAND NR 35R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78027. HORIZONTAL STABILIZER BARREL NUT BORE NR 35R. BLEND OUT EXCEEDING MAX, LIMITS AFTER BORING THROUGH THE BOTTOM (MD-11 S/B 55-023 REV 1). 2L73 4F RTA22WE 20040727000532004072700053NM 2004 7 27 04FDEA01861 120040625A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25209FE 22931 STA 1037 ABOVE STR 23R SKIN IS DENTED. DENT AT BS 1037 STR 23 FOUND TO BE OUT OF LIMITS. REPAIRED DENT PER SRM 53-30-3 FIGURE 1. 2L73 4F RTA3WE 20040720000262004072000026 2004 7 20 RAIA00406015 420040615A3418C850176 VANE JETAIRJETSTMJETSTM4101 1500501EU NR 1 AOA INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03567HK2275 41085 5522 - STL - LEFT STALL CAP ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 1 AOA VANE. 2L72 4T RTA41NM 20040720000292004072000029 2004 7 20 VNAA0406014 420040621A34187013348937 DAU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05425JS7841 3037 ON CLIMBOUT, THE CREW RECEIVED AN ON SIDE BLUE STICK SHAKER CAS MESSAGE. THE AIRCRAFT THEN RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED, AND REPLACED THE NR 2 DATA ACQUISITION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040720000512004072000051SO 2004 7 20 C2XA04SH451 120040629A531114564145001 DOUBLER EMB 145 EMB145ER 3260211SO FRAME CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE DOUBLER ON FRAME 61 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000572004072000057 2004 7 20 DL76L040653 420040713A3410 COMPUTER BOEING767 767332 1382001NM ADC MALFUNCTIONED A DALAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SO27199DN 28456 AFTER TAKEOFF CAPT'S AIRSPEED BECAME UNRELIABLE. SWITCHING TO ALTERNATE ADC PRODUCED RELIABLE INDICATIONS. PERFORMED LT ADC BITE CHECK NO FAULTS SHOWN ON MDC. NO EXTERNAL FAULT SHOWN. PERFORMED ADC FUNCTIONAL TEST, ALL OK. AS PRECAUTION REPLACED LT ADC COMPUTER PER 34-12-01, ADC TEST OK. PERFORMED MDCP GROUND TEST 30, ALSO OK. 2L72 4F RTA1NM 20040720000592004072000059NM 2004 7 20 DL76G040655 120040713A3320BV03203N40 SOCKET BOEING767 767332 1382001NM LIGHT FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27169DZ 29689 ELECTRICAL SMELL IN AFT GALLEY FOUND BAD LIGHT SOCKET. FLUORESCENT TUBE LIGHT COPILOTS SIDE ACROSS FROM LAV AT R4 DOOR. FWD TO MCO AND PLACARD PER MEL 25-20-01K. BULB REMOVED. 2L72 4F RTA1NM 20040720000652004072000065SO 2004 7 20 C2XA04BT077 120040712A21214611028900 FAN EMB 145 EMB145LR 3260212SO CABIN SEIZED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2726545 145558 CREW REPORTED, CABIN SMOKE ONCE AIRBORNE WITH ENGINE BLEED SELECTED ON. AIRCRAFT RETURNED TO NEWARK, LANDED UNEVENTFULLY. MAINTENANCE FOUND CABIN RECIRCULATING FAN INOPERATIVE. REMOVED AND REPLACED CABIN RECIRCULATING FAN IAW EMB145 MM 21-24-01, OPS CHECKED GOOD. ALSO, PERFORMED EMB145 FIM TASK 21-20-00-810-801-A, NO SMELL IS NOTICED IN CABIN, RAN ENGINES TO VERIFY SMELL, NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040720000672004072000067SO 2004 7 20 C2XA04SH453 120040713A531514521713005 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK. 2L72 4F RTT00011AT 20040720000842004072000084NM 2004 7 20 AALA20040721 120040711A3350P4010051112 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21177AN 32396 JFK - FORWARD CABIN FLOOR PROXIMITY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD CABIN FLOOR PROXIMITY EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040720000862004072000086WP 2004 7 20 AALA20040719 120040709A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21287AA 49299 PHX - AFT RIGHT HAND BATTERY PACK INOPERATIVE. REPLACED AFT RIGHT HAND BATTERY PACK IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040720000882004072000088SO 2004 7 20 C2XA04SH436 120040703A531014522368004 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720000902004072000090SO 2004 7 20 C2XA04SH438 120040707A531014522369003 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714930 145011 SHV - DURING C-CHECK THE SHEAR TIE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHEAR TIE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040720001242004072000124NM 2004 7 20 DLM88040647 120040712A7330766342 VALVE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE LEAKING A DALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO27921DL 49645 726088 NR 1 ENG SHUTDOWN ON ROLLOUT. FOUND P&D VLV LEAKING. REPLACED VLV PER M/M. 2L72 4F4 FRTA6WE E9NE 20040720001262004072000126NM 2004 7 20 DLM88040649 120040713A3610 OIL SYSTEM DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE APU LEAKING A DALAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27934DL15536 49721 P80331 FIRST FLIGHT ATB SMOKE IN CABIN WITH LAV DETECTORS SOUNDING FLIGHT CXLD. MTC WORKING OPN'S 5088 AND 5089 SMOKE T/S AND DUCT BURN OUT. 2L72 4F4 FRTA6WE E9NE 20040721000042004072100004EU 2004 7 21 2004F00177 120040620A5330 SKIN AIRBUS320 A320233 3930329EU FUSELAGE DELAMINATED A K NONE O OTHER ININSP/MAINT 1 SO23463TA 1339 DURING GROUND INSPECTION, FOUND PANEL 191DT DAMAGED, WITH MATERIAL LOST AND DELAMINATED. AIRCRAFT REMAINS AT MIA STATION FOR REPAIR. (M) 2L72 4F RTA28NM 20040721000092004072100009SO 2004 7 21 SIMA200415802 120040603A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN MALFUNCTIONED A SIMAO OTHER O OTHER CRCRUISE 1 SW21709GB 145211 RDU - FLT 4634 - DURING CRUISE FLIGHT, CREW REPORTED THE EMERGENCY LIGHT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. NO MESSAGES WERE FOUND ON THE CMC. AN OPERATIONAL CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040721000112004072100011NM 2004 7 21 GAIA04078OP 120040604A2797W32520528R WIRE BOEING727 7272J0 138407ENM VERTICAL STAB BROKEN A GAIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW07281KH 21105 FLT 2715 - ELP-DFW-FWA - DURING CLIMB, THE UPPER RUDDER INDICATOR WAS SWINGING BETWEEN MINOR INDICIES. AT 10,000 AGL THE LOWER RUDDER SWUNG HARD LEFT AND THEN ANOTHER LEFT NOT AS HARD. CREW FOLLOWED FLIGHT CONTROL EMERGENCY PROCEDURE AND RETURNED TO ELP. AN UNEVENTFUL LANDING WAS MADE. REPAIRED BROKEN WIRE AT SPLICE 2 OF LOWER RUDDER PCU AND LOWER RUDDER POSITION SENSOR WIRE. SYSTEM OPS CHECKED GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040721000222004072100022EU 2004 7 21 A6WA200460020 120040607A5320 SILL BAC 146 146300A 1500267EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 L1 SILL PLATE CORRODED BEYOND LIMITS. SIL PLATE L1 REPAIRED IAW BAE SRM 51-43-00, 51-42-00 AND 51-23-00. (M) 2H74 4F RTA49EU 20040721000312004072100031 2004 7 21 A6WA200440054 420040430A3460 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA FMS BURNED A A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31412AW 7582 FMS PAGE STUCK ON PERFORMANCE SCREEN, AFTER DETECTING ELECTRICAL BURNING ODOR IN COCKPIT AND IN FROM CABIN. PULLED CIRCUIT BREAKER H12. REMOVED AND REPLACED FMS CONTROL PANEL FOR BURNING ODOR AFTER FROZEN SCREEN. NO FURTHER ODOR NOTED WITH REPLACEMENT. OPS CHECK GOOD IAW 34-61-01. (M) 2L72 4F RTA21EA 20040721000502004072100050NM 2004 7 21 AMTA200400655 120040602A1420 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 FOUND ROW 27 EMERGENCY EGRESS FLOOR TRACK LIGHT INOPERATIVE. FOUND CONNECTOR DISCONNECTED, RECONNECTED SAME, OPS SATISFACTORY. (M) 2L72 4F RTA2NM 20040721000532004072100053NM 2004 7 21 2004F00187 120040324A7160 SKIN BOEING727 727222 1384073NM RT ENG INTAKE DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077643U 20037 DURNG WALK AROUND INSPECTION FOUND, SKIN DAMAGE WITH SKIN PEELED AND MISSING ON LOWER FORWARD RIGHT SIDE CENTER ENGINE AIR INLET DUCT HOUSING, BETWEEN FUSELAGE STATION 1183 AND 1233. REMOVED SKIN DAMAGE AS NECESSARY. INSTALLED EXTERNAL DOUBLER REPAIR AT LOWER FORWARD RIGHT SIDE CENTER ENGINE AIR INLET DUCT HOUSING BETWEEN FUSELAGE STATION 1183 AND 1233. (M) 2L73 4F A3WE 20040721000982004072100098NM 2004 7 21 04FDEA02105 120040718A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.511, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.508 AND REPAIRED AS PER EA 1-5750-77943. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040721001142004072100114EU 2004 7 21 04FDEA02061 120040713A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 ZONE 252, SEAT TRACK 2 RIGHT HAS THREE AREAS OF CORROSION BETWEEN FRAMES 69 TO 10 INCHES AFT OF FRAME 71, 12 INCHES AFT OF FR 69, 12 INCHES AFT OF FR 70, 8 INCHES AFT OF FR 71, ALL ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10, NEW SEAT TRACK FABBED ON N00420. 2L72 4F RTA35EU 20040721001162004072100116EU 2004 7 21 04FDEA02063 120040713A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 UPPER TRACK BREAK TO BREAK FR 69 TO 59.5, 6 EA PLACES AS MARKED FLOOR TRACKS HAVE LITE SURFACE CORROSION EACH APPROX 1 X 1 X 0.003 INCH DEPTH WITHOUT BLENDOUT, AND 1 EA GOUGE TOP SIDE OF TRACK AS MARKED (FR 60) 0.500 X 0.500 X 0.010 INCH DEPTH WITHOUT BLENDOUT, TRACK 2R. REMOVED OLD SEAT TRACK AND RE-INSTALLED NEW SEAT TRACK IAW A310 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20040721001322004072100132 2004 7 21 SWAA042026 420040718A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040721001472004072100147NM 2004 7 21 SWAA042037 120040719A52406523464 SNUBBER BOEING737 7375H4 138449DNM L2 DOOR INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 L2 DOOR WILL NOT OPEN. REMOVED AND REPLACED L2 DOOR SNUBBER PER MM. 2L72 4F RTA16WE 20040721001552004072100155EA 2004 7 21 SWIA200413548 120040703A2750855D1009 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07408SW4779 4779 7055 ON APPROACH, SELECTED FLAPS TO 20 DEGREES AND RECEIVED FLAPS FAIL. REMOVED AND REPLACED LEFT HAND BPSU, RIGGED LEFT HAND AND RIGHT HAND BPSU. OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20040721001632004072100163WP 2004 7 21 MEX2004060 120040215A2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082WP LEFT LEAKING A ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23505MD 49149 DURING TRANSIT CHECK, THE LEFT HYDRAULIC SYSTEM WAS EMPTY. DURING REVISION AT THE TAIL AREA IN THE VENTRAL STAIR WAS DETECTED A HYDRAULIC LIQUID LEAK. THE AREA WAS CLEANED AND LEAK WAS REPAIRED. (M) 2L72 4F A6WE 20040721001642004072100164EA 2004 7 21 REXA04002 120040119A4900 ODOR CNDAIRCL600 CL6002B19 1900309EA APU DETECTED A REXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO258525B 7525 APU AUTO SHUTDOWN DURING CLIMB-OUT. PILOT ATTEMPTED TO RESTART APU. THIS START ATTEMPT RESULTED IN A STRONG FUEL SMELL IN THE CABIN AND COCKPIT. CREW REQUESTED AND WAS GRANTED PERMISSION TO RETURN TO DAYTON. AN OTHERWISE UNEVENTFUL LANDING WAS PERFRMED AT DAY. MAINTENANCE RAN AIRCRAFT TO POWRE WITH BOTH ECS SYSTEMS SET TO FULL HOT. NO FURTHER RESIDUAL ODOR OR FUMES WERE DETECTED. THE APU WAS DEFERRED PER THE MEL. (M) 2L72 4F RTA21EA 20040721001732004072100173 2004 7 21 WRLA200401 420040103A256531002200C ASPIRATOR DOUG DC10 DC10 N/A-SDRNM ESCAPE SLIDE SEPARATED A WRLAK NONE O OTHER ININSP/MAINT 1 EA27541SA 46541 DURING MAINTENANCE CHECK, AT GSO, THE REQUIRED TEST DEPLOYMENT OF THE R1 DOOR EVACUATION SLIDE WAS ACCOMPLISHED. DURING TEST THE AFT ASPIRATOR OF THE SLIDE CAME APART. FOUND THE RETAINING RING THAT HOLDS THE ASPIRATOR IN PLACE ON THE SLIDE CAME OUT WHEN THE SLIDE BLEW, CAUSING THE SLIDE NOT TO FULLY INFLATE. THE FORWARD ASPIRATOR WORKED GOOD NO PROBLEMS. THE O-RING THAT FITS UNDERNEATH THE TOP OF ASPIRATOR ALSO CAME OUT AND WAS FOUND ON GROUND WITH THE METAL RETAINER RING. REMOVED AND REPLACD R-1 SLIDE ASSEMBLY. 2L73 4F RTA22WE 20040721001742004072100174NM 2004 7 21 TSAA0449022 120040209A49202118966222 ECU BOEING737 73776N 13844CHNM APU FAILED A TSAAO OTHER O OTHER LDLANDING 1 WP13744AL 32582 FLT 441 - OAK-HNL - APU FAULT LIGHT ILLUMINATED ON FINAL APPROACH, AUTO SHUTDOWN. REPLACED APU ECU. SYSTEM OPS CHECK GOOD IAW MM 49-61-12-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040722000132004072200013CE 2004 7 22 2004F00192 120040614A3244301345870 TIRE LEAR 25 25B 5170511CE LT MLG FAILED A CEDAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW05236CA 161 ON TAKEOFF ROLL, THE AIRCRAFT BLEW THE LEFT MAIN GEAR TIRES IN ELP. (M) 2L72 4J A10CE 20040722000212004072200021NM 2004 7 22 UIEA200400033 120040322A3040 CONTROL UNIT BOEING747 74747UF 1384949NM COCKPIT WINDOW MALFUNCTIONED A UIEAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA15408MC 29261 EICAS MESSAGE -HEAT WINDOW LT- DISPLAYED AFTER 1 HOUR CRUISE FLT AT FL330 AND SIMULTANEOUSLY L1 WINDOW CRACKED. PRESSURIZATION WAS NORMAL. REPLACED L1 WINDOW HEAT CONTROL UNIT IAW MM 30-41-00 OPERATION CHECK NORMAL. REMOVED AND REPLACED L1 WINDSHIELD IAW MM 56-11-01 AND OPERATION CHECK NORMAL. (M) 2L74 4F RT1384945 20040722000272004072200027CE 2004 7 22 2004F00203 120040402A21001143641407 CIRCUIT BOARD BEECH 1900 1900D 1154162CE ENVIRO CONTROL SHORTED A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO1917541 UE203 DURING FLIGHT, ELECTRICAL SMOKE IN FLIGHT DECK. LEFT ENVIRONMENTAL WHITE OFF LIGHT ILLUMINATED. PULLED CIRCUIT BREAKER. CONTINUED TO FLL. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENVIRONMENTAL CONTROL PC BOARD. (M) 2L72 4T RTA24CE 20040722000302004072200030EU 2004 7 22 USA2004F00090 120040608A5321D536106500000 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW 0997 FOUND CORROSION THROUGH MAIN FLOOR DECK PANEL, 2 INCH X 2 INCH X .040 INCH. REPLACED PANEL. 2L72 4F4 FRTA28NM E2GL 20040722000322004072200032NM 2004 7 22 USA2004F00084 120040618A2613285N002836 OVERHEAT LOOP BOEING767 767201 1385125NM GE CF6 CF680 30025NE E/E BAY FAULTY A USAAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19650US 23902 CLIMBING THROUGH 12,000 FT, CREW RECEIVED EICAS MESSAGE (R ENG OVHT) AND ASSOCIATED LIGHT. AFTER PERFORMING QRH PROCEDURE, LIGHT AND MESSAGE REMAINED. ENGINE WAS SECURED AND THE FLT RETURNED TO DEPARTURE AIRPORT. (SET APPROX 15 MIN) MAINTENANCE REPLACED BOTH OVERHEAT DETECTION CARDS (M689 AND M690) AND THE RT ENGINE OVERHEAT LOOPS 1 AND 2. SUBSEQUENTLY, ON 20JUN04, FLIGHT 230, THE CREW AGAIN RECEIVED THE RT OVERHEAT INDICATIONS. QRH PROCEDURE WAS AGAIN FOLLOWED AND THE ENGINE SHUTDOWN. THE OVERHEAT INDICATIONS REMAINED ON UNTIL POWER TRANSFER AT THE GATE. (SET 15 MINUTES) MAINTENANCE WAS ABLE TO DUPLICATE THE OVERHEAT LIGHT BY MANIPULATING THE M10274 AFOLTS CARD. THE CARD WAS REPLACED. 2L72 4F4 FRTA1NM E13NE 20040722000332004072200033NM 2004 7 22 USAA040203 120040513A5230 SKIN PANEL BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US 24555 PIT, Q5, INNER SKIN PANEL, .2500 INCH CRACKS, LIGHTENING HOLE NR 22. ROUTED OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER IAW EA 78419. 2L72 4F4 FRTA16WE E2GL 20040722000512004072200051NE 2004 7 22 GAIA04083AOP 220040623A7200 ENGINE BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 3 MALFUNCTIONED A GAIAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW07279US 21158 696499 SHUTDOWN NR 3 DUE TO HIGH OIL PRESSURE AND RISING OIL TEMP. OIL PRESSURE WAS 53 PSI, OIL TEMP WAS 130 UNTIL POWER REDUCED, THEN OIL TEMP SPIKED OFF SCALE. DUMPED 20,000 POUNDS FUEL. OIL TEMP GAUGE REMAINED OFF SCALE. (AN EMERGENCY WAS DECLARED AND THE CREW RETURNED, WHERE AN UNEVENTFUL LANDING WAS MADE). REMOVED AND REPLACED NR 3 ENGINE IAW WC BH719401. OPERATION CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040722000522004072200052NM 2004 7 22 USAA040204 120040505A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE 7LBBL12.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19433US40473 24555 PIT, Q5, FLOOR SUPPORT, 1 INCH DIA CORROSION; LEVEL 1 TASK NR C53-208-01, BS 727F PLUS 7 LBBL 12.50. REMOVED DAMAGED SECTION AND INSTALLED NESTED IAW TYPE REP 53-10-06B. 2L72 4F4 FRTA16WE E2GL 20040722000612004072200061NE 2004 7 22 REX2004F00002 220040610A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT MALFUNCTIONED A REXAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO258577D 7577 AT LEVEL CRUISE AT FL310 AND MACH .74, THE FIRST OFFICER NOTICED A FLUXUATION IN THE RT ENGINE OIL PRESSURE. WITHIN FIVE MINUTES THE FLUXUATION BEGAN TO INCREASE. THE CAPTAIN ALSO NOTICED AN ASSOCIATED INCREASE IN OIL TEMPERATURE. THE FLIGHT CREW PERFORMED THE QRH CHECKLIST AND SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT WAS DIVERTED. DESCENT AND LANDING WERE WITHOUT FURTHER INCIDENT. CAUSE OF THIS INCIDENT IS STILL UNDER INVESTIGATION. 2L72 4F4 FRTA21EA E15NE 20040722000622004072200062NM 2004 7 22 278229 120040518A3230656021132 ACCESSORY UNIT BOEING727 727222 1384073NM PWA JT8 JT8D1 52044NE RT MLG INOPERATIVE A RYNAO OTHER J WARNING INDICATION TOTAKEOFF 1 CE077638U 19911 DURING CLIMB, EXPERIENCED MULTIPLE WARNINGS FOR UNSAFE RT MAIN GEAR. ALTITUDE WARNING HORN SOUNDED AT 2000 FT, INADDITION TO WINDSHEAR LIGHT AND STICK SHAKER (NO SHEAR NOTED). AIRCRAFT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR ACCY UNIT. 2L73 4F4 F A3WE E2EA 20040722000692004072200069NM 2004 7 22 TIP2004F00001 120040429A5315141T5114160 FLOORBEAM BOEING767 76733AER 1385230NM FUSELAGE CORRODED B TIPRO OTHER O OTHER NRNOT REPORTED 1 SO05637TW 25403 CABIN FLOORBEAM AT STA 347, LBL 20 THUR LBL28. CORROSION OUT OF LIMITS B767 SRM, REPAIR REQUIRED. FLOORBEAM HAS CORROSION FROM GALLEY AREA LEAKS, HAVE CORRODED THE BEAM. 2L72 4F RTA1NM 20040722000702004072200070EA 2004 7 22 ASO2004F00020 120040530A326017300221 SQUAT SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG OUT OF ADJUST A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27847AS 7335 DURING CLIMB OUT, UPON GEAR RETRACTION, THE CREW HEARD A STRANGE NOISE FROM THE GEAR WITH ALL INDICATIONS SHOWING NORMAL. WHEN PASSING THROUGH 2,000 FEET THE CREW RECEIVED A GEAR DISAGREE EICAS WARNING MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW ELECTED TO SELECT THE GEAR DOWN AT WHICH TIME ALL INDICATIONS WERE NORMAL AND ALL AURAL MESSAGES DISCONTINUED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE ADJUSTED THE WEIGHT ON WHEELS (WOW) SENSOR UPON DISCOVERING THE GAP WAS OUT OF LIMITS. MAINTENANCE ALSO NOSE JACKED THE AIRCRAFT AND OPERATED THE GEAR FIFTEEN TIMES. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040727000072004072700007WP 2004 7 27 04FDEA02150 120040722A5712ARB24406 RIB DOUG DC10 DC1030 3023501WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 RIGHT WING I/B LEADING EDGE ACCESS PANEL 616ET SEVERAL RIBS CRACKED. REMOVED CRACKED RIBS AND REPLACED WITH NEW RIBS IAW SRM 51-31-01. PAINTED IAW SRM 51-23-01. 2L73 4F A22WE 20040727000122004072700012EU 2004 7 27 04FDEA02155 120040722A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25407FE 254 MAIN CABIN SEAT TRACK 2R FR45 TO FR54 HAS 6 EA AREAS OF EXFOLIATED CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20040727000162004072700016NM 2004 7 27 04FDEA02160 120040722A5340 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 AFT FUSELAGE COMPT STA 2007 RIGHT HAND X=-10 VERTICAL SUPPORT FITTING MOST END SUSPECT CRACKED. CUT AND REMOVED AS PER SRM 53-00-01, FIGURE 8, VOLUME I. REPAIR ANGLES FABRICATED AS PER SRM 53-00-01, FIGURE 8, VOLUME I, T-SECTION MACHINED AS PER FEDEX E.A. NO. 1-5310-80363, TITLE: MAIN FRAME - AFT PRESSURE BULKHEAD STA 2007.000 - EXTRUDED CAP SUBSTITUTION, AND INSTALLED AS PER SRM 53-00-01, FIGURE 8, VOLUME I. 2L73 4F RTA22WE 20040727000262004072700026NM 2004 7 27 04FDEA02162 120040723A5740 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP STOP FITTING CRACKED 2 PLACES. REPLACED AS PER MM 27-50-30- 4. ON P/N: NRC6753-503 AND ON S/N: 047. OFF P/N: NRC6753-503 AND OFF S/N: 006. FUNCTIONAL CHECK REFER TO SNRM N0508 FOR WORK DETAILS. 2L73 4F RTA22WE 20040727000512004072700051WP 2004 7 27 04FDEA01859 120040320A5711ARB22161 SPAR CAP DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25385FE 46619 CRACK FOUND IN THE LT WING UPPER CAP AT RIB STATION XORS 402. THE CRACK IS ALL WAY THRU THE CAP AND IS LOCATED IMMEDIATELY FORWARD OF STRINGER 15. CRACKS ROUTED AND EXTRUDED REPAIR ANGLE INSTALLED IAW FEDEX EA 8-5710-75730 (REF FEDEX NRC N0625). 2L73 4F A22WE 20040727000542004072700054WP 2004 7 27 04FDEA02034 120040710A5350AKC700522 BRACKET DOUG MD10 MD1010F 3022112WP TAIL CONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 TAIL CONE RIGHT FWD FRAME MIDDLE GUIDE PIN BRACKET IS CRACKED. REMOVED AND REPLACED GUIDE PIN BRACKET IAW SRM 51-31-01 & SRM 51-35-01 AT MAE. 2L73 4F RTA22WE 20040727000552004072700055WP 2004 7 27 04FDEA02035 120040710A5753ARC2801504 FITTING DOUG MD10 MD1010F 3022112WP RT WING IB FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 RIGHT WING I/B FLAP I/B TRACK FAIRING AFT MOUNT WORN. REMOVED AND REPLACED MOUNT IAW SRM 51-33-01 AT MAE. 2L73 4F RTA22WE 20040727000572004072700057NM 2004 7 27 04FDEA02037 120040710A3600 DUCT DOUG MD11 MD11 3023602NM NR 1 ENGINE FAILED A FDEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25595FE 48553 FIVE MINUTES AFTER T/O RECEIVED HYD PUMP 1R OFF ALERT. HYD SYS SNOPSIS SHOWED -T- OVER 1R PUMP, 1 MINUTE LATER HYD SYSTEM FAILED, PRESSURE WENT TO -0-. ALSO NOTED AMBER -T- OVER LEFT PUMP PRIOR TO HYD 1 SYS OFF. REPLACED NR 1 ENG LOW PRESS TURBINE SUPPLY AIR DUCT AT THE 11 O`CLOCK POSITION. REMOVED AND REPLACED LT EDP NR 1 ENGINE IAW MD-11AMM 29-11-20-41. LEAK CHECKS GOOD. 2L73 4F RTA22WE 20040727000602004072700060WP 2004 7 27 04FDEA02040 120040710A5753ARC2177 FITTING DOUG MD10 MD1010F 3022112WP RT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 COMPLY WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79545 WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. 2L73 4F RTA22WE 20040727000612004072700061WP 2004 7 27 04FDEA01862 120040518A5500ALC74412 SKIN PANEL DOUG DC10 DC1010 3022110WP ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25385FE 46619 PERFORMING REPAIR PROVIDED BY SB 55-16, INTERESTED PANEL HAS BEEN CUT OVER THE LAYOUT TRIM LINE REQUIRED. DAMAGED SKIN PANEL PORTION REPLACED AND SPLICED TO EXISTING SKINS IAW FEDEX EA 8-2740-75698 (REF FEDEX NRC N0747, N0940). 2L73 4F A22WE 20040727000622004072700062WP 2004 7 27 04FDEA01863 120040610A5711ARB0007501 SPAR CAP DOUG DC10 DC1010 3022110WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 WING LEFT REAR SPAR AFT LOWER CAP CRACK AT XORS 412. THE CRACK EXTENDS INTO THE VERTICAL LEG AND FWD HORIZONTAL LEG. PERFORM PERMANENT REPAIR SIMILAR IN CONCEPT TO DWG SR10570019 WITH DIFFERENT FASTENER CALL OUTS TO COMPENSATE FOR PREVIOUS REWORK IAW EA 8-5710-78175. 2L73 4F A22WE 20040727000632004072700063WP 2004 7 27 04FDEA01878 120040629A5753ARC1455502 VANE DOUG DC10 DC1010 3022110WP RT O/B FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 COMPLY WITH EA 8-5750-78235 WINGS OUTBOARD FLAP ARC 1537 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-78235 WINGS O/B FLAP ARC1537 FLAP VANE SUPPORT CORROSION REWORK AT MAE. 2L73 4F A22WE 20040728000052004072800005WP 2004 7 28 04FDEA01884 120040630A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 N-12476 DURING PASSENGER TO FREIGHTER MODIFICATION AND TRANSITION CHECK LT OUTBOARD FLAP, FWD HINGE SECTION STA XW 486 WITH CORROSION IN THE BORES OF BUSHINGS ACTUATOR ATTACH POINTS. REMOVED CORROSION AND CHECK LIMITS IAW CMM 57-44-08 AND INSTALLED BUSHING REPAIR HOLE BORE (5A), (5B). 2L73 4F A22WE 20040728000062004072800006WP 2004 7 28 04FDEA01885 120040630A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING PAX TO FREIGHTER MODIFICATION AND TRANSITION CHECK, FOUND LT OUTBOARD FLAP FWD HINGE SECTION STA XW 486 WITH CORROSION AT THE FACE OF BORE FOR BEARING. CORROSION REWORK FWD INNER HINGE NR 4 LUG FACE IAW CMM 57-44-08 IN LIMIT REF FIG 401 SH 1 CMM 57-44-08, INSTALL SHIM IAW CMM 57-44-08. 2L73 4F A22WE 20040728000082004072800008WP 2004 7 28 04FDEA01895 120040630A5753ARC1953 WEDGE DOUG DC10 DC1030 3023501WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RT OUTBOARD FLAP NR 2 TRAILING EDGE WEDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN ASSEMBLY IAW DC10 SRM 57-21-01 VOL 2 AND DC10 SRM 51-40-01 VOL 2. 2L73 4F A22WE 20040728000122004072800012NM 2004 7 28 04FDEA02113 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.193 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000232004072800023NM 2004 7 28 04FDEA02138 120040719A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 DAMAGE AT REPAIR DOUBLER AT BS 930, 3 INCHES ABOVE STR 14 LT, AFT SIDE OF FRAME. REMOVED AND REPLACED REPAIR DOUBLER AT BS 930, 3 ABOVE STR 14 LT PER SRM 51-30-2, 53-10-3. 2L73 4F RTA3WE 20040728000262004072800026NM 2004 7 28 04FDEA02043 120040710A5714 SUPPORT FITTING BOEING727 727200 138407ENM CENTER WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25245FE 22016 CENTER WING BOX FWD SUPPORT FITTING IS CORRODED AT FS 740 RBL 14.5. REMOVED AND REPLACED BRACKET AND FITTING ASSY IAW SRM 51-10-1. 2L73 4F RTA3WE 20040728000282004072800028NM 2004 7 28 04FDEA02045 120040712A2710 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 COMPLY WITH EA 1-5510-76669 HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. HORIZONTAL STABILIZER BARREL NUTS REWORK PER SB MD11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000' HAS BEEN COMPLIED. 2L73 4F RTA22WE 20040728000302004072800030EU 2004 7 28 04FDEA02048 120040712A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 MAIN CABIN SEAT TRACK NR 5 LEFT OF CENTER LINE AT FR 20 HAS 2 EA BROKEN LUGS. REPAIRED MAIN CABIN SEAT TRACK 35 LT OF CENTERLINE AT FR 20 IAW A300-600F SRM 53-10-16 FIG 201. 2L72 4F RTA35EU 20040728000332004072800033EU 2004 7 28 04FDEA02051 120040712A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25665FE 769 MAIN CARGO COMPT RT SEAT TRACK NR 3 BETWEEN FRAMES 44.5 AND 54 HAS CORROSION AT FR 52, 48.5 AS MARKED. REMOVED SEAT TRACK DAMAGE AREA, FAB AND INSTALLED NEW SEAT TRACK SECTION REPAIR IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20040728000352004072800035 2004 7 28 SWAA042070 420040721A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728000372004072800037 2004 7 28 SWAA042072 420040721A2565D31354 SLIDE BOEING737 7372T4 1384492NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040728000382004072800038NM 2004 7 28 SWAA042073 120040721A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 53, CRACKED. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20040728000402004072800040NM 2004 7 28 SWAA042075 120040721A57536546430122 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM. 2L72 4F RTA16WE 20040728000432004072800043NM 2004 7 28 SWAA042067 120040720A291065C268413138 LINE BOEING737 7373H4 1384600NM B-HYD SYSTEM LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29346SW 24153 DECLARED EMERGENCY, HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH QUANTITY GOING DOWN. REMOVED AND REPLACED HYDRAULIC B-SYSTEM PUMP PRESSURE LINE PER MM. 2L72 4F RTA16WE 20040728000462004072800046NM 2004 7 28 04FDEA02123 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000472004072800047NM 2004 7 28 04FDEA02124 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040728000482004072800048NM 2004 7 28 04FDEA02125 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED ASPER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER 1.062, FINAL DIAMETER 1.207, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000492004072800049NM 2004 7 28 04FDEA02126 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.405", MATERIAL REMOVED = 0.005, REMAINING THICKNESS=0.400, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000532004072800053WP 2004 7 28 04FDEA02084 120040715A5280ARC28132 FITTING DOUG DC10 DC1030 3023501WP ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 RIGHT MAIN GEAR DOOR FWD UPPER H-11 BOLT POSITION NR 1 PER DWG ARC2859 HAS GOUGES AND CORROSION. REMOVED FITTING AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW FITTING IAW EO 8-5710-7-5005 AND DWG ARC2859 AND SRM 51-31-01. 2L73 4F A22WE 20040728000562004072800056NM 2004 7 28 04FDEA02090 120040715A5315 FLOORBEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON LOWER FLOORBEAM FASTENERS BS 1110 RBL 1-12 WL 201. REMOVED CORROSION ON FLOORBEAM LWR CHORD BS 1110 RBL 6 WL 201, 2 X 1 MAXIUMUN MATERIAL LOSS .036 ORIGINAL THICKNESS .125 OUT OF LIMMITS PER SRM 51-10-6, 53-10-2 CUT OUT DAMAGE LWR FLANGE BS 1110 AND REPAIRED LWR CHORD BS 1110 LBL 23.5-RBL 9.3 IAW SRM 53-10-8 FIG 2. 2L73 4F RTA3WE 20040728000632004072800063NM 2004 7 28 04FDEA01700 120040612A5753ARC2517U501 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP P/N ARC2517U501 REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040728000642004072800064NM 2004 7 28 04FDEA01801 120040618A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK UPPER BOLT HOLE FOUND CORRODED. 2L73 4F RTA22WE 20040728000662004072800066NM 2004 7 28 04FDEA01804 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000672004072800067NM 2004 7 28 04FDEA01805 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000702004072800070NM 2004 7 28 04FDEA01808 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000722004072800072NM 2004 7 28 04FDEA01810 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000752004072800075NM 2004 7 28 04FDEA01836 120040621A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP VANE NR 2 TEE FITTING FWD BOLT HOLE CORRODED. CORROSION REMOVED AS PER SRM 51-21-01. 2L73 4F RTA22WE 20040728000762004072800076NM 2004 7 28 04FDEA01837 120040621A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP VANE NR 4 TEE FITTING AFT BOLT HOLE CORRODED. 2L73 4F RTA22WE 20040728000822004072800082NM 2004 7 28 04FDEA01820 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000852004072800085NM 2004 7 28 04FDEA01823 120040620A5753 HINGE DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000872004072800087WP 2004 7 28 04FDEA01913 120040702A5530AJC77055 BULKHEAD DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED AND PRIMED IAW SRM 51-21-01. 2L73 4F A22WE 20040728000892004072800089NM 2004 7 28 04FDEA01812 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 . 2L73 4F RTA22WE 20040728000932004072800093WP 2004 7 28 04FDEA01910 120040701A5350ARC715017 ANGLE DOUG DC10 DC1010 3022110WP TAICONE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 FUSE TAIL CONE CENTER PLATFORM LT ANGLE SUPPORT WORN. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE. 2L73 4F A22WE 20040728000952004072800095NM 2004 7 28 04FDEA01824 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000972004072800097NM 2004 7 28 04FDEA02140 120040720A5713 STRINGER DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 638AB. REPAIR ANGLES FABRICATED AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED AS PER SRM 57-20-00, FIGURE 10, SHEET 6, VOLUME I. 2L73 4F RTA22WE 20040728001022004072800102NM 2004 7 28 04FDEA01825 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728001032004072800103NM 2004 7 28 04FDEA01827 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728001042004072800104NM 2004 7 28 04FDEA01828 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728001062004072800106 2004 7 28 GTIA040550 420040519A8300777188A GEARBOX DOUG DC9 DC981 3022081WP NR 2 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 ACY - FOUND FRONT ACCESSORY DRIVE GROUP COVER CRACKED AT 7 O'CLOCK POSITION. REMOVED AND REPLACED FRONT ACCESSORY, N-1 TACH, GEAR BOX. (M) 2L72 4F A6WE 20040728001082004072800108 2004 7 28 GTIA040556 420040531A2565 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FLT 503 - DTW - L2 SLIDE PACK FELL OFF. FOUND SLIDE PACK COVER LANYARD DISCONNECTED, REINSTALLED LANYARD. (M) 2L72 4F A6WE 20040728001092004072800109 2004 7 28 GTIA040557 420040530A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 DTW - FLT 599 - FOUND L1 SLIDE PACK NEEDS TO BE SECURED. RESECURED L1 SLIDE PACK. (M) 2L72 4F A6WE 20040728001122004072800112 2004 7 28 GTIA040582 420040620A2565 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 RSW - FLT 1504 - SLIDE PACK L-1 DOOR CAME OFF AS THE DOOR WAS OPENED IN ORD. REINSTALLED L-1 DOOR SLIDE PACK AND COVER. (M) 2L72 4F RT 20040728001162004072800116WP 2004 7 28 GTIA040602 120040614A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 617-693 MISSING INSERTS. FABRICATED NEW CENTER CABIN FLOOR PANEL. (M) 2L72 4F RTA6WE 20040728001172004072800117WP 2004 7 28 GTIA040597 120040511A5230 STOP FITTING DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND FORWARD CARGO PIT ALL SET SCREWS RUSTY AND CORRODED. LOCATED AND DRILLED TWO NEW DOOR STOPS STATION 427 AT L26R AND L21R. INSTALLED NEW TWO DOOR STOPS STATION 427 AND L26R-L21R. INSTALLED NEW TWO DOOR STOPS AT STATION 428/389, L20R. INSTALLED NEW DOOR STOPS AT STATION 370 L26R. (M) 2L72 4F RTA6WE 20040728001182004072800118WP 2004 7 28 GTIA040600 120040606A5310 DOUBLER DOUG DC9 DC983 3022083WP MLG DOOR FRAME CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND LEFT MLG INBOARD DOOR AFT DOOR JAMB HAS CRACK AR PREVIOUS REPAIR CRACK BEYOND STOP DRILL STATION 1003. REMOVED PREVIOUS REPAIR DOUBLER. STOPPED DRILL AT THE END OF CRACK. FABRICATED NEW REPAIR DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040728001202004072800120WP 2004 7 28 GTIA040599 120040606A3350 SIGN DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND NUMEROUS EMERGENCY LIGHTS IN CABIN INOPERATIVE. EXIT IDENTIFIER MISSING. INSTALLED NEW R1 DOOR EXIT SIGN. (M) 2L72 4F RTA6WE 20040728001222004072800122WP 2004 7 28 GTIA040608 120040607A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND RIGHT OUTBOARD SEAT TRACKS STATION 700-798 GOUGED AND CORRODED. SEAT TRACK 790-798 OUT OF LIMITS. REMOVED RIGHT OUTBOARD SEAT TRACK STATION 778-798. DRILLED AND LOCATED RIGHT OUTBOARD REPAIR SEAT TRACK STATION 778-798. INSTALLED SEAT TRACK STATION 778-798. (M) 2L72 4F RTA6WE 20040728001232004072800123WP 2004 7 28 GTIA040614 120040609A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CABIN FLOOR PANEL STATION 168-200 MISSING INSERT AND DELAMINATED. FABRICATED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040728001242004072800124WP 2004 7 28 GTIA040603 120040614A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 693-769 MISSING INSERTS. FABRICATED NEW FLOOR BOARD PANEL. (M) 2L72 4F RTA6WE 20040728001252004072800125 2004 7 28 GTIA040585 420040619A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 RSW - FLT 670 - FOUND FORWARD CABIN SLIDE PACK FELL OUT. REINSTLALED L1 SLIDE PACK ASSEMBLY. (M) 2L72 4F A6WE 20040728001262004072800126WP 2004 7 28 GTIA040609 120040614A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND CABIN STATION 541-617 STRINGER 18L AND STATION 636-712 STRINGER 18L FLOOR WEB CORRODED IN NUMEROUS AREAS. MATERIAL LOSS IS OUT OF LIMITS STATION 636-655 AT STATION 642-647. CUT OUT AREA. FORMED FILLER AND REPAIR DOUBLER. INSTALLED FILLER AND DOUBLER STATION 633-655. (M) 2L72 4F RTA6WE 20040728001272004072800127WP 2004 7 28 GTIA040615 120040614A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND LEFT CABIN FLOOR PANEL STATION 1174-1287 MISSING INSERTS BROKEN EDGES. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040728001282004072800128WP 2004 7 28 GTIA040611 120040607A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND LEFT OUTBOARD SEAT TRACKS STATION 798-1309 GOUGED AND CORRODED. OUT OF LIMITS FROM STATION 1032-1309. REMOVED SEAT TRACK STATIN 1032-1309. FABRICATED THREE NEW SEAT TRACKS FROM STATION 1032 TO 1136, 1136 TO 1250 AND 1250 TO 1309. FABICATED TWO SPLICES. INSTALLED SEAT TRACKS. (M) 2L72 4F RTA6WE 20040728001292004072800129WP 2004 7 28 GTIA040610 120040614A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CABIN STATION 332-503 STRINGER 18L FLOOR WEB CORRODED IN NUMEROUS AREAS. WEB AT STATION 366 IS OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040728001302004072800130EU 2004 7 28 USAA04342 120040608A5320D5348015900400 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FOUND CORROSION ON PLATE ASSEMBLY, 2 INCHES PLUS 2 INCHES BY .040 INCH. REPLACED PLATE. (M) 2L72 4F RTA28NM 20040728001332004072800133WP 2004 7 28 GTIA040578 120040621A2612 CONNECTOR DOUG DC9 DC982 3022082WP FIRE LOOP SHORTED A GTIAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23823NK 48020 ORD - FLT 1103 - RIGHT ENGINE LOOP B AND FIRE DETECTOR LOOP CAUTION LIGHTS CAME ON WITH NO OTHER ABNORMALITIES. LOOP A SELECTED AND LOOP A TESTED GOOD. FOUND CONNECTOR P1-863 SHORTED REMOVED AND REPLACED CONNECTOR P1-863 ON RIGHT ENGINE FIRE LOOP 'B'. SYSTEM OPS CHECK GOOD. (M) 2L72 4F A6WE 20040728001372004072800137WP 2004 7 28 GTIA040586 120040531A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND FLIGHT COMPARTMENT CENTER FLOOR PANEL STATION 148 TO STATION 160 HAS SEVERAL CRACKS ON EDGES AND CORRODED AT INSERTS. FABRICATED NEW FLOORBOARD. (M) 2L72 4F RTA6WE 20040728001392004072800139NM 2004 7 28 ASAA0440081 120040316A53206935362 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01783AS 25114 OAK - FOUND AFT CARGO COMPARTMENT BILGE HAD CRACKED INTERCOSTAL. REPLACED INTERCOSTAL. (M) 2L72 4F RTA16WE 20040728001402004072800140NM 2004 7 28 ASAA0410271 120040523A5315BAC1505100246 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F A16WE 20040728001412004072800141NM 2004 7 28 ASAA0410260 120040514A5315BAC1505100246 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON UNDERSIDE OF UPPER CHORD AFT SIDE OF FLOORBEAM. REMOVED DAMAGE AND REPAIRED PER SRM. (M) 2L72 4F A16WE 20040728001442004072800144 2004 7 28 SWAA042088 420040723A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728001482004072800148NM 2004 7 28 SWAA042092 120040723A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM AT BS 727B +2 TO BS 727B + 12, CORRODED. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040728001492004072800149WP 2004 7 28 04FDEA02079 120040714A5420AUB70153 WEB DOUG MD10 MD1010F 3022112WP ZONE 400 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 COMPLY WITH EA 8-5450-79556 NACELLES / PYLONS NR 3 ENGINE PYLON WEB DAMAGE. COMPLIED WITH EA 8-5450-79556 NACELLES / PYLONS NR 3 ENGINE PYLON WEB DAMAGE. 2L73 4F RTA22WE 20040728001502004072800150EU 2004 7 28 04FDEA02080 120040715A5730 PANEL AIRBUS310 A310222 3930315EU WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25449FE 217 PANEL LAND 650 KB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5730-55328A PT1. 2L72 4F RTA35EU 20040728001522004072800152NM 2004 7 28 04FDEA01838 120040621A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP VANE NR 1 TEE FITTING AFT BOLT HOLE CORRODED. 2L73 4F RTA22WE 20040728001532004072800153NM 2004 7 28 04FDEA01839 120040621A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE BRACKET (FLAP SIDE), AFT ATTACHMENT POINT FORWARD BOLT HOLE FOUND CORRODED. 2L73 4F RTA22WE 20040728001552004072800155WP 2004 7 28 04FDEA01841 120040621A2150ACM7019 DUCT DOUG DC10 DC1010 3022110WP AIR COND BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 COMPLY WITH EA 8-2150-78236, AIR CONDITIONING NR 2 AC PACK EXHAUST DUCT STIFFENER REPAIR P/N-ACM7019. COMPLIED WITH EA 8-2150-78236 FOR STIFFENER REPAIR. 2L73 4F A22WE 20040728001582004072800158 2004 7 28 SWAA042105 420040724A256563551101 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EVAC SLIDE PRESSURE IND OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728001602004072800160NM 2004 7 28 04FDEA01995 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1801, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1801, RBL 27.5 SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040728001612004072800161NM 2004 7 28 04FDEA01996 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1795 - 1815, RBL 27.5 FOUND DAMAGED. MAIN DECK AT STA 1795 - 1815, RBL 27.5, SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040728001622004072800162NM 2004 7 28 04FDEA01997 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1251, LBL 47.5 FOUND WITH GOUGED MARK. MAIN DECK - DAMAGED SEAT TRACK CROWN AT STA 1251, LBL 47.5 REMOVED FROM STA 1268 TO 7 - 0 LBL 47.5 PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME 2. REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-30-00 VOLUME 2. 2L73 4F RTA22WE 20040728001632004072800163NM 2004 7 28 04FDEA01972 120040706A5320A5A7112 SPLICE DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 CRACKED. MAIN DECK - SPLICE FITTING AT RT STA 1531 LONGERON 14 REMOVED AS PER SRM 51-31-01 VOLUME 2. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7112 AND INSTALLED AS PER SRM 51-31-01 VOLUME 2. 2L73 4F RTA22WE 20040728001642004072800164NM 2004 7 28 04FDEA02098 120040717A5712ARC2966 RIB DOUG MD11 MD11 3023602NM ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 C/W EA 8-5750-80579 WINGS RT INBOARD FLAP VANE TRACK OVERSIZE HOLE REPAIR AT XIFH 216.3 (P/N ARC2966). COMPLIED WITH EA 8-5750-80579. 2L73 4F RTA22WE 20040728001672004072800167WP 2004 7 28 04FDEA01917 120040703A5753NRC6062520 VANE DOUG DC10 DC1030 3023501WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND INBOARD FLAP VANE, UPPER SKIN HAS MULTIPLE AREA OF DENTS AND DELAMINATION. REMOVED AND REPLACED WITH OVERHAULED VANE RIGHT HAND INBOARD FLAP VANE IAW FEDEX WORKCARD E-8- 5750-7-5002 C PT4. 2L73 4F A22WE 20040728001682004072800168WP 2004 7 28 04FDEA01918 120040703A5753NRC6062509 VANE DOUG DC10 DC1030 3023501WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 LEFT HAND INBOARD FLAP VANE, LOWER SKIN DAMAGED AT OUTBOARD STOP. REMOVED AND INSTALLED OVERHAULED VANE AT LEFT HAND INBOARD FLAP IAW FEDEX WORKCARD E-8-5750-7-5002 C PT3. 2L73 4F A22WE 20040728001692004072800169NM 2004 7 28 04FDEA01987 120040706A5753ARC2512 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.326 INCH, AND REPAIRED AS PER EA 1-5750-76787, TITLE: WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. 2L73 4F RTA22WE 20040728001702004072800170NM 2004 7 28 04FDEA01991 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1090, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47.5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2. 2L73 4F RTA22WE 20040721001382004072100138NM 2004 7 21 SWAA042041 120040719A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727D, STRINGER 8L & STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040721001392004072100139EA 2004 7 21 SWIA200413505 120040625A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY FAILED A SWIAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07408SW4579 4579 7055 APU AUTO SHUTDOWN ON GROUND. STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT PRIOR TO APU SHUTDOWN. RECEIVED APU FIRE WARNING. COMPLIED WITH QRC AND QRH PROCEDURES. FERRIED TO SLC. REMOVED AND REPLACED APU ASSEMBLY IAW MM 49-10-00 AND RII 49-401. OPS CHECK GOOD. 2L72 4F RTA21EA 20040721001482004072100148SO 2004 7 21 RAIA00406020 120040621A2750 LINKAGE EMB 145 EMB145 3260210SO TE FLAPS OUT OF ADJUST A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03806HK 145112 FLAP FAIL MESSAGE AT FLAP RETRACTION. MAINTENANCE ADJUSTED FLAP MECHANICAL LINKAGE. 2L72 4F RTT00011AT 20040721001492004072100149EU 2004 7 21 RAIA00406019 120040617A3230AIR235692 SWITCH JETAIRJETSTMJETSTM4101 1500501EU MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03555HK 41072 LANDING GEAR HANDLE WOULD NOT GO TO THE UP POSITION. MAINTENANCE REMOVED AND REPLACED THE LEFT AOG SWITCH. 2L72 4T RTA41NM 20040721001572004072100157SO 2004 7 21 SWIA200413550 120040706A27523430001003 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07214SW7466 7466 120280 AFTER LANDING SELECTED FLAPS UP, RECEIVED A CONTROL FAULT ON OUTBOARD FLAPS. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. REPAIRED PIN 4 AT CONNECTOR P1867. REMOVED AND REPLACED FCU IAW 27-50-00 AND OPERATIONAL CHECKED GOOD IAW 27-50-00. 2L72 4T RTA31SO 20040721001602004072100160 2004 7 21 RAIA00407003 420040708A3425 DISPLAY EMB 145 EMB145ER 3260211SO COCKPIT FAILED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03826HK 145016 CAPTAIN PRIMARY FLIGHT DISPLAY WENT BLANK. MAINTENANCE SWAPPED CAPTAINS MFD AND PFD AND DEFERRED CAPTAIN’S MFD PER MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING CAPT'S MFD. 2L72 4F RTT00011AT 20040721001682004072100168EU 2004 7 21 USAASA04012 120040207A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19738US 1254 DCA - THE EMERGENCY LIGHTS DO NOT TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MID RIGHT CABIN POSITION. (M) 2L72 4F RTA28NM 20040721001712004072100171NE 2004 7 21 WRLA200402 220040102A7200 ENGINE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 2 LEAKING A WRLAO OTHER J WARNING INDICATION CLCLIMB 1 EA27278WA 48746 733792 TAKEOFF PLUS 30 LEVEL OFF FL310 NR 2 ENGINE OIL TEMP HIGH 165 DEGREES FOR 15 MINUTES 170 DEGREES MOMENTARY OIL QUANITY DROPPED TO 7 QUARTS DESCEND TO FL230 STABILIZED 234 PSI, 142 DEGREES, 7 QUARTS. AIRCRAFT DIVERTED TO LAWANDA. REMOVED AND REPLACED ENGINE. (M) 2L73 4F4 FRTA22WE E24NE 20040721001892004072100189CE 2004 7 21 2004F00165 120040210A2720991455811 LIMITER CESSNA750 750 2076810CE RUDDER DAMAGED A UG8AO OTHER O OTHER CRCRUISE 1 GL235112 7500010 CREW REPORTED A 'FAILED RUDDER LIMITER B' MESSAGE ON THE CAS. THE LOWER RUDDER LIMITER LINEAR ACTUATOR B-CHANNEL, FAILED AT 25 PERCENT. REPLACED RUDDER LIMITER ACTUATOR 'B' IAW CHAPTER 27-23-00 OF CESSNA MM, OPERAITON CHECK GOOD OK FOR SERVICE. (M) 2L72 4J RTT00007WI 20040722000072004072200007NM 2004 7 22 C7WA200400005 120040309A5313 STRINGER BOEING737 737231 1384079NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO1754354 21986 FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED STRINGER 28 LEFT BETWEEN FS 1052 AND 1064. CUTOUT DAMAGED SKIN. REPAIRED SKIN IAW 727 SRM 53-30-3, FIG 3. STRINGER REPAIRED IAW 727 SRM 53-10-3 FIG 1. (M) 2L72 4F RTA16WE 20040722000122004072200012EU 2004 7 22 2004F00191 120040616A3260GE83 BULB AMD FALC20FALCON 2720302EU MLG INDICATOR BURNED OUT A CEDAO OTHER P NO WARNING INDICATION DEDESCENT 1 SW05217CA 75 ON DESCENT INTO TVF, THE FLIGHT CREW DID NOT GET INDICATION THAT THE RIGHT MAIN GEAR WAS DOWN AND LOCKED. THE FIGHT CREW THEN DECLARED AN EMERGENCY AND DIVERTED TO GFK. THE TOWER CONFIRMED THE GEAR WAS DOWN, THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW INSPECTED AIRCRAFT AND FOUND THE LIGHT FOR THE RIGHT MAIN GEAR HAD BURNED OUT. REPLACED THE BULB AND THE SYSTEM OPERATIONAL CHECKED NORMAL. (M) 2L72 4F A7EU 20040722000172004072200017NM 2004 7 22 C7WA200400007 120040309A5330 SKIN BOEING727 727231 1384079NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO1754354 21986 FOUND LOWER FUSELAGE SKIN CORROSION AT STRINGER 28 RIGHT BETWEEN FS 1046 AND 1072, AFT EDGE OF EXISTING REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGE, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M) 2L73 4F A3WE 20040722000252004072200025NM 2004 7 22 2004F00201 120040429A2740AJH73781 PIN DOUG DC10 DC1040F 3023507NM HS DRIVE UNIT SHEARED A CLCAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO19140WE 46920 HORIZONTAL STABILIZER JAMMED AT APPROXIMATELY 1.5 ANU DURING CRUISE. ABNORMAL PROCEDURES COMPLIED WITH FOR LANDING. LANDING AT DESTINATION UNEVENTFL. FOUND SHEAR PIN SHEARED ON HORIZ STAB DRIVE UNIT. REPLACED HORIZ STAB CHAIN DRIVE UNIT, OPERATIONAL CHECKS NORMAL IAW AMM 27-44-05. AIRCRAFT RETURNED TO REVENUE SERVICE. (M) 2L73 4F RTA22WE 20040722000282004072200028CE 2004 7 22 2004F00204 120040331A55201016200111 BRACKET BEECH 1900 1900D 1154162CE RT STAB CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1947542 UE198 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20040722000462004072200046 2004 7 22 USA2004F00086 420040609A2565D5348015900400 SUPPORT AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE GIRT BAR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FOUND CORROSION ON SUPPORT PLATE, 6 INCH X 0.5 INCH X .020 INCH. INSTALLED NEW R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE. 2L72 4F4 FRTA28NM E2GL 20040722000482004072200048NM 2004 7 22 UIEA200400115 120040617A5230411U40802 SKIN BOEING747 747400 NM GE CF6 CF680 30025NE CARGO DOOR DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15492MC 29253 FOUND NOSE CARGO DOOR DENTED. AREA APPROX 8 INCHES IN LENGTH 6 INCHES WIDE AND .1875 INCH DEEP ON THE BOTTOM OF THE DOOR, 4 INCHES FROM THE AFT EDGE. EXTERNAL PATCH REPAIR CARRIED OUT IAW SRM. 2L74 4F4 FRTA20WE E13NE 20040722000552004072200055CE 2004 7 22 JEM2004F00003 120040617A551145A210863 RIB BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS. 2H72 4F4 FRTA16SW E1NE 20040722000632004072200063NM 2004 7 22 BJNA040601 120040605A33506013211 POWER SUPPLY BOEING737 737282 13844ATNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK FOR THE RT OVER-WING EMERGENCY EXIT LIGHT IAW MFG MM. EMERGENCY EXIT LIGHTS NOW OPERATE NORMALLY. 2L72 4F4 FRTA16WE E2EA 20040722000662004072200066SO 2004 7 22 SIMA200417204 120040617A533014530203003 SKIN PANEL EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL FUSELAGE BIRD STRIKE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21622AE 145108 DURING MBV INSPECTION THE LT FORWARD FUSELAGE SKIN DAMAGED FROM BIRD STRIKE. REPLACED DAMAGED SKIN IAW SRM. 2L72 4T4 FRTT00011ATTE6CH 20040727000022004072700002WP 2004 7 27 04FDEA02144 120040721A5753ARC21771 FITTING DOUG DC10 DC1030 3023501WP LT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 COMPLY WITH EA 8-5750-79540; WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177. COMPLIED WITH EA 8-5750-79540, WINGS OUTBOARD FLAP, FLAP SPINDLE CARRIAGE SUPPORT FITTING CORROSION REPAIR, P/N ARC2177 AT MAE. 2L73 4F A22WE 20040727000052004072700005NM 2004 7 27 04FDEA02146 120040721A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 MAIN DECK, RIGHT HAND MOST OUTBOARD SEAT TRACK CORRODED AT R1 DOORWAY. REMOVED LAVATORY ON MAIN DECK AS PER AMM 25-41-06-4. REMOVED AND REPLACED RIGHT HAND MOST OUTBOARD SEAT TRACK AT R1 DOORWAY AS PER SRM 51-35-01, VOLUME II. REINSTALLED LAVATORY MODULE AS PER AMM 25-41-06-4. CARRIED OUT LEAK CHECK ON LAVATORY MODULE FOUND SATISFACTORY. 2L73 4F RTA22WE 20040727000062004072700006WP 2004 7 27 04FDEA02149 120040722A5411 FRAME DOUG DC10 DC1030 3023501WP ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 NR 2 ENGINE RIGHT CORE COWL FORTH RIB AFT CRACKED JUST ABOVE ACCESS DOOR. REMOVED DOUBLER IAW SRM 51-31-01. RECEIVED FROM WELD SHOP CORE COWLING FRAME WELDED BY TRAVLER T4/445038 AND DPS10-301. INSTALLED DOUBLER STIFFENER AND CLIP IAW SRM 51-33-01 AND SRM 51-31-01. 2L73 4F A22WE 20040727000172004072700017NM 2004 7 27 SWAA042078 120040722A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 CABIN OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. SECURED LENS PER MM. 2L72 4F RTA16WE 20040727000202004072700020 2004 7 27 SWAA042081 420040722A256565C16820 HOOK BOEING737 7373Q8 1384670NM GIRT BAR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 R2 DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO STOW AND REMOVE FROM CONTAINER. ADJUSTED GIRT BAR STOW CLIP HOOKS AT CONTAINER PER MM. 2L72 4F RTA16WE 20040727000312004072700031EU 2004 7 27 04FDEA02069 120040713A3243 CONTROL UNIT AIRBUS310 A310222 3930315EU AUTO BRAKES FAILED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25455FE 331 BRAKES BINDING ON TAKEOFF CLEARANCE. A/C WOULD NOT ROLL EVEN AT 45 PERC. FLASHING AUTO BRAKE FAIL, TRIED TO BITE TEST ON BSCU AND SHOWED FAULT CODE 223 & 222. REMOVED AND REPLACED NR 6 BRAKE ASSY PER MM 32-42-27-4. REMOVED AND INSTALLED BRAKE SYS CONTROL UNIT AND TESTED OK AS PER AMM 32-42-72-4. REMOVED AND INSTALLED FROM FACT PREMATURE REMOVAL/INSTALLATION. OFF MFG C20101304-201. 2L72 4F RTA35EU 20040727000352004072700035NM 2004 7 27 04FDEA02106 120040719A5753 HINGE DOUG MD11 MD11 3023602NM CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.507, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EA NR 1-5750-77943. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000402004072700040NM 2004 7 27 04FDEA02128 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.095 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000452004072700045NM 2004 7 27 04FDEA02133 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040727000582004072700058WP 2004 7 27 04FDEA02038 120040710A5753NRC6068513 VANE DOUG MD10 MD1010F 3022112WP LT O/B FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 COMPLY WITH EA 8-5750-79551 WINGS FLAP VANE SUPPORT CORROSION REWORK (LT OUTBD FLAP). COMPLIED WITH EA 8-5750-79551 WINGS FLAP VANE SUPPORT CORROSION REWORK (LT OUTBD FLAP) AT MAE. 2L73 4F RTA22WE 20040727000592004072700059WP 2004 7 27 04FDEA02039 120040710A5753ARC1984 FITTING DOUG MD10 MD1010F 3022112WP RT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 COMPLY WITH EA 8-5750-79549 WINGS RIGHT O/B FLAP I/B HINGE LUG CORROSION REPAIR (P/N ARC1984). COMPLIED WITH EA 8-5750-79549 WINGS RIGHT OUTBD FLAP INBD HINGE LUG CORROSION REPAIR (P/N ARC1984). 2L73 4F RTA22WE 20040728000092004072800009WP 2004 7 28 04FDEA01896 120040630A5753 WEDGE DOUG DC10 DC1030 3023501WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 437811 RIGHT HAND OUTBOARD FLAP HAS DENT OUT OF LIMITS AT STATION 478 INBOARD END. REMOVE WEDGE IAW DC10 SRM 51-40-2 VOL 2. REMOVE WEDGE SKIN IAW DC10 SRM 51-40-2 VOL 2, FABRICATED NEW SKIN IAW FED-EX EA 8-57-50-77573 AND DC10 DAC DWG ARC 1949. INSTALLED NEW SKIN IAW DC10 SRM 51-40-2 VOL 2. REINSTALLED WEDGE IAW DC10 SRM 51-40-2 VOL 2. 2L73 4F A22WE 20040728000162004072800016NM 2004 7 28 04FDEA02117 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000182004072800018NM 2004 7 28 04FDEA02119 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NO. 1-5750-77941. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000272004072800027WP 2004 7 28 04FDEA02044 120040711A5753NRC6068510 VANE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 COMPLY WITH EA 8-5750-79552 WINGS FLAP VANE SUPPORT CORROSION REWORK (RT OUTBOARD FLAP). COMPLIED WITH EA 8-5750-79552 WINGS FLAP VANE SUPPORT CORROSION REWORK, RIGHT O/B FLAP. 2L73 4F RTA22WE 20040728000392004072800039NM 2004 7 28 SWAA042074 120040721A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040728000422004072800042NM 2004 7 28 SWAA042077 120040721A53306545857 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR CUTOUT FWD LOWER CORNER, CRACKED. REPAIRED DOOR CUTOUT PER EA. 2L72 4F RTA16WE 20040728000452004072800045NM 2004 7 28 04FDEA02122 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.505, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000502004072800050NM 2004 7 28 04FDEA02127 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040728000542004072800054WP 2004 7 28 04FDEA02086 120040715A5744ARC01542 HINGE DOUG DC10 DC1030 3023501WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 C/W EA 8-5740-80575 WINGS RT INBD FLAP OUTBD HINGE UPPER HOLE LUG CORROSION REPAIR P/N ARC0154-2. COMPLIED WITH EA 8-5740-80575. 2L73 4F A22WE 20040728000552004072800055WP 2004 7 28 04FDEA02091 120040716A5720ARC0391504 SUPPORT DOUG MD10 MD1010F 3022112WP RH WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 COMPLY WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR. COMPLIED WITH EA 8-5740-80572 WINGS RT SUPPORT ASSY ACTUATOR AND HOLD DOWN NR 1 SPOILER CORROSION REPAIR AT MAE. 2L73 4F RTA22WE 20040728000732004072800073NM 2004 7 28 04FDEA01811 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 AND REPAIRED AS PER EA 1-5750-78012. 2L73 4F RTA22WE 20040728000742004072800074NM 2004 7 28 04FDEA01826 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED. 2L73 4F RTA22WE 20040728000842004072800084NM 2004 7 28 04FDEA01822 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED. 2L73 4F RTA22WE 20040728000862004072800086WP 2004 7 28 04FDEA01912 120040702A5530AJC77055 BULKHEAD DOUG DC10 DC1010 3022110WP ZONE 300 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479 IAW SRM 51-31-01. BLENDED GOUGES IAW SRM 55-00-01. NDT CRACK CHECK, FOUND NO CRACKS, TREATED AND PRIMED IAW SRM 51-21-01. 2L73 4F A22WE 20040728000902004072800090NM 2004 7 28 04FDEA01813 120040620A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD HOLE SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040728000922004072800092WP 2004 7 28 04FDEA01909 120040701A5350AKC70802 GUIDE DOUG DC10 DC1010 3022110WP TAILCONE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 RIGHT TAIL CONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW 51-33-01 AT MAE. 2L73 4F A22WE 20040728000942004072800094WP 2004 7 28 04FDEA01911 120040702A5712 RIB DOUG MD10 MD1010F 3022112WP ZONE 600 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 COMPLY WITH EA 8-5750-79543 WINGS RT FIXED LEADING EDGE SLAT RIB TRACK RIB GOUGE REPAIR XOS 427.4. COMPLIED WITH EA 8-5740-79543. 2L73 4F RTA22WE 20040728001102004072800110WP 2004 7 28 GTIA040558 120040602A2560 GLOWSTRIP DOUG DC9 DC983 3022083WP L1 GALLEY BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FLL - FLT 367 - SAFE T GLO AT L1 GALLEY BROKEN. INSTALLED NEW SAFE T GLO AT L1 GALLEY. (M) 2L72 4F RTA6WE 20040728001142004072800114WP 2004 7 28 GTIA040596 120040510A5310 BEAM DOUG DC9 DC983 3022083WP CARGO DOOR FRAMECORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND AFT CARGO LOWER DOOR JAMB BEAM HAS CORROSION. REMOVED AFT PIT JAMB BEAM. LOCATED AND DRILLED NEW BEAM. INSTALLED NEW BEAM. UPON FURTHER INSPECTION INTERCOSTAL FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTAL. INSTALLED NEW INTERCOSTAL. (M) 2L72 4F RTA6WE 20040728001152004072800115 2004 7 28 GTIA040601 420040512A2565D29984211 SLIDE DOUG MD80 MD83 3023681NM TAILCONE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23822NK 49392 FTW - FOUND TAILCONE EVAC SLIDE UNPACKED AND MISSING O/H DATE. REMOVED TAILCONE EVAC SLIDE. INSTALLED TAILCONE EVAC SLIDE. (M) 2L72 4F RT 20040728001192004072800119 2004 7 28 GTIA040584 420040619A2565 GIRT BAR DOUG DC9 DC982 3022082WP GALLEY DOOR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 ACY - FLT 341 - FORWARD GALLEY DOOR GIRT BAR CAN NOT BE REMOVED FROM ARMED POSITION. CLEANED DEBRIS FROM GIRT BAR RECEIVING LATCH AND LUBRICATED. (M) 2L72 4F A6WE 20040728001342004072800134WP 2004 7 28 GTIA040579 120040619A3260 WARNING LIGHT DOUG DC9 DC982 3022082WP MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23820NK 49126 FOUND LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. (M) 2L72 4F A6WE 20040728001352004072800135WP 2004 7 28 GTIA040590 120040518A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND CABIN STATION 799 STRINGER 18R WEB CORRODED. FABRICATED DOUBLER. ROUTED OUT CRACK. INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20040728001462004072800146NM 2004 7 28 SWAA042090 120040723A3350311500 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 17 ABC, LOOSE. SECURED BULL NOSE EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040728001512004072800151EU 2004 7 28 04FDEA02081 120040715A5730 PANEL AIRBUS310 A310222 3930315EU WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25449FE 217 PANEL 550HB HAS 2 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310/200 SRM 51-40-44 FIG 1 CHAMBER CODE-J, COMPLIED WITH EA 6-5730-55328A PT 1 ON 1EA HOLE. 2L72 4F RTA35EU 20040728001592004072800159NM 2004 7 28 04FDEA01994 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1129, RBL 28 FOUND WITH GOUGED MARK. MAIN DECK - SEAT TRACK FROM STA 1129 TO 7 - 0, RBL 28 REMOVED AS PER SRM 51-31-01 VOLUME 2. SEAT TRACK REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REWORKED TRACK INSTALLED AS PER 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME 2. 2L73 4F RTA22WE 20040728001652004072800165WP 2004 7 28 04FDEA01915 120040702A5320S29227811 SUPPORT DOUG DC10 DC1010 3022110WP CNTR CARGO CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 CENTER CARGO CEILING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT S2922781-1 AT MAE. 2L73 4F A22WE 20040728001712004072800171NM 2004 7 28 04FDEA01992 120040706A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 6-20, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 6-20, RBL 47.5 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2. 2L73 4F RTA22WE 20040728001722004072800172NM 2004 7 28 04FDEA01993 120040706A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 6-80, RBL 47.5 FOUND DAMAGED. MAIN DECK - DAMAGED SEAT TRACK AT STA 6-80, RBL 47.5 REMOVED FROM STA 1129 TO STA 7-0 RBL 4.75 AND REPLACED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-31-01 VOLUME 2. 2L73 4F RTA22WE 20040728001732004072800173NM 2004 7 28 04FDEA01842 120040622A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 MAIN DECK SEAT TRACK FOUND CRACKED AT STA 635 RT 8 INCHES. 2L73 4F RTA22WE 20040728001742004072800174WP 2004 7 28 04FDEA01845 120040623A3260 WARNING LIGHT DOUG DC10 DC1010 3022110WP MLG MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO2568056 47810 ON GEAR RETRACTION LT MAIN GEAR LIGHT STAYED RED ON FORWARD AND F/E'S GEAR INDICATION. RAN RED TABS, GEAR EXTEND NORMALLY. REPEAT WRITE UP, RETURNED TO MEM. 2L73 4F A22WE 20040728001752004072800175EU 2004 7 28 04FDEA01846 120040623A5410A5461004200200 SHACKLE AIRBUS300 A300B4605R 3930308EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25652FE 735 NR 2 ENGINE O/B NR 4 SHACKLE HAS PITTING CORROSION NEAR BOTH UPPER AND LOWER BUSHES AT THREE PLACES. (OFF AIRCRAFT PART) PROCURED NEW FOR NR 2 PYLON OUTBOARD SHACKLE PYLON WING ATTACH POINTS, STA 539/RIB 8. 2L72 4F RTA35EU 20040728001762004072800176EU 2004 7 28 04FDEA01847 120040623A5410A5461004200200 SHACKLE AIRBUS300 A300F4605R 3930327EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25652FE 735 NR 2 ENGINE NR 1 SHACKLE HAS TWO AREAS OF PITTING CORROSION NEAR BUSHES. OFF AIRCRAFT PART. PROCURED NEW SHACKLE FOR NR 2 PYLON WING ATTACH POINTS. INSTALLED ON WC 64S0506, STA 485/RIB 7. 2L72 4F RTA35EU 20040728001792004072800179NM 2004 7 28 SWAA042095 120040723A57536546435278 SKIN BOEING737 737301 1384611NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040728001802004072800180NM 2004 7 28 SWAA042096 120040723A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM WEB AT BS 663, RBL 39, CRACKED. REPAIRED FLOORBEAM WEB PER SRM. 2L72 4F RTA16WE 20040728001812004072800181NM 2004 7 28 SWAA042097 120040723A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND RT AND LT FWD OVERHEAD DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040728001822004072800182 2004 7 28 SWAA042098 420040724A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728001832004072800183NM 2004 7 28 SWAA042099 120040724A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT ENTRY EMERGENCY LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040728001842004072800184 2004 7 28 SWAA042100 420040724A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728001852004072800185NM 2004 7 28 SWAA042054 120040720A33506114789 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29093SW 22965 DURING SCHEDULED A1 CHECK, FOUND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY PER MM. 2L72 4F A16WE 20040728001872004072800187NM 2004 7 28 SWAA042056 120040720A53156546810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 1016, RBL 14 TO RBL 25, CORRODED. REMOVED AND REPLACED FLOORBEAM PER ER. 2L72 4F RTA16WE 20040728001882004072800188NM 2004 7 28 SWAA042057 120040720A53306545765 SKIN BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT RIGHT KEEL BEAM BS 500C TO RT KEELBEAM BS 500D, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040728001892004072800189NM 2004 7 28 SWAA042058 120040720A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 25L, BS 747, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040728001902004072800190NM 2004 7 28 SWAA042059 120040720A57536546435278 SKIN BOEING737 737301 1384611NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20040728001922004072800192NM 2004 7 28 SWAA042062 120040720A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040728001932004072800193NM 2004 7 28 SWAA042063 120040720A53116545808 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294, STRINGER 7R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040728001942004072800194NM 2004 7 28 SWAA042065 120040720A53116546533 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040728001972004072800197NM 2004 7 28 SWAA042050 120040719A5310BAC15061653 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME WEB AT FWD ENTRY DOOR CUTOUT BS 303.9, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SB AND SRM. 2L72 4F RTA16WE 20040728001982004072800198NM 2004 7 28 SWAA042051 120040719A5510183A8410 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STAB NR 6 ELEVATOR HINGE FITTING, CORRODED. REMOVED AND REPLACED HINGE FITTING PER ACO. 2L72 4F RTA16WE 20040728001992004072800199NM 2004 7 28 SWAA042052 120040720A2910AS152G0340CCN HOSE BOEING737 7372H4 138448CNM LT MLG HYD SYS LEAKING A SWAAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 SW29090SW 22905 AIRTURN BACK, ON TAKEOFF NR 2 HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH DROP IN QUANTITY. NR 1 HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH LOSS OF PRESSURE. REMOVED AND REPLACED NR 1 BRAKE HOSE PER MM. 2L72 4F A16WE 20040728001052004072800105NM 2004 7 28 SWAA042102 120040724A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040728001072004072800107 2004 7 28 GTIA040554 420040531A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DISLODGED A GTIAO OTHER O OTHER TOTAKEOFF 1 GL23817NK 49141 DTW - FLT 1408 - R1 DOOR SLIDE PACK FELL OFF DURING TAKEOFF. REINSTALL AND SECURED SLIDE PACK. OK FOR SERVICE. (M) 2L72 4F A6WE 20040728001112004072800111WP 2004 7 28 GTIA040559 120040501A5313 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FTW - FOUND AFT PIT STATOIN 1079-1117 L28L CORRODED AT FASTENERS AND SPOT CORROSION AT STATION 1114. REMOVED LONGERON AFT PIT L28L STATION 1050-1127. FABRICATED LONGEORN REPAIR. FABRICATED 2 LONGERON SPLICES. INSTALLED NEW SECTION LONGERON. INSTALLED TWO LONGERON SPLICES. (M) 2L72 4F RTA6WE 20040728001132004072800113WP 2004 7 28 GTIA040613 120040607A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND LEFT INBOARD SEAT TRACKS STATION 798-1309 GOUGED AND CORRODED. CUT OUT SEAT TRACK SECTION FROM STATION 936.5-1309. LOCATED AND DRILLED 4 EACH SECTION SEAT TRACKS AT STATION 936-1051, 1051-1146, 1146-1222 AND 1222-1309. LOCATED AND DRILLED 4 SPLICES. INSTALLED LEFT INBOARD SEAT TRACKS. REMOVED LEFT INBOARD SEAT TRACK STATION 797-836. LOCATED AND DRILLED LEFT INBOARD SEAT TRACK STATION 797-836 LOCATED AND DRILLED SPLICE. INSTALLED LEFT INBOARD SEAT TRACK STATION 797-836 AND SPLICE AT STATION 836. (M) 2L72 4F RTA6WE 20040728001212004072800121WP 2004 7 28 GTIA040607 120040615A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 1174-1287 CORRODED INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040728001312004072800131EU 2004 7 28 USAA04343 120040608A5320D5348015900400 PLATE AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 FOUND CORROSION ON PLATE ASSEMBLY, 2 INCHES BY 2 INCHES BY .040 INCHES. REPLACED PLATE. (M) 2L72 4F RTA28NM 20040728001362004072800136WP 2004 7 28 GTIA040592 120040604A52304934916507 LATCH DOUG DC9 DC983 3022083WP CARGO DOOR WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND MID PIT DOOR LATCH WORN AND RUSTED AFT SIDE OF JAMB. REMOVED DOOR LATCH PIN. INSTALLED NEW DOOR LATCH. (M) 2L72 4F RTA6WE 20040728001382004072800138WP 2004 7 28 GTIA040587 120040520A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND FLOOR PANEL LEFT OUTBOARD STATION 1097-1155 CRACKED. REPAIRED FLOOR PANEL. (M) 2L72 4F RTA6WE 20040728001432004072800143NM 2004 7 28 SWAA042087 120040722A2121215201 FAN BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAD RETURN TO BLOCK O OTHER NRNOT REPORTED 1 SW29653SW 28398 AIR TURNBACK, GASPER FAN CAUSED A BURNING SMELL THROUGHOUT CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20040728001452004072800145 2004 7 28 SWAA042089 420040723A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29751SW 29803 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728001472004072800147 2004 7 28 SWAA042091 420040723A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040728001542004072800154NM 2004 7 28 04FDEA01840 120040621A5510ALC8102501 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 EMPENNAGE - HORIZONTAL STABILIZER LEFT HAND BARREL NUT 24L SURFACE CORROSION BLENDED OUT FOUND EXCEEDED LIMIT. EMPENNAGE - HORIZONTAL STABILIZER LEFT HAND 24L BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78030, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE 24L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7- 5000. 2L73 4F RTA22WE 20040728001562004072800156NM 2004 7 28 SWAA042103 120040724A53156546803 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 500D, RBL 13, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040728001572004072800157NM 2004 7 28 SWAA042104 120040724A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29787SA 29812 DURING SCHEDULED MV1 CHECK, FOUND AFT EEPLS AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040728001662004072800166WP 2004 7 28 04FDEA01916 120040703A5410AUB7000501 FITTING DOUG MD10 MD1010F 3022112WP ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 COMPLY WITH EA8 -5420-79546 NR 1 PYLON FWD TRUSS FITTING CORROSION. COMPLIED WITH EA 8-5410-79546. 2L73 4F RTA22WE 20040728001772004072800177WP 2004 7 28 04FDEA01920 120040703A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 FWD CARGO PIT FLOORBEAM AT BS 652 IS CRACKED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS LOCATED AND DRILLED IAW DC10 SRM 53-00-01 VOL 1. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL 2, INSTALLED REPAIR PARTS IAW DC10 SRM 53-00-01 VOL 1. 2L73 4F A22WE 20040728001782004072800178NM 2004 7 28 SWAA042094 120040723A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY EXIT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED RON, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040728001862004072800186NM 2004 7 28 SWAA042055 120040720A55116551524 SPAR BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND RT & LT HORIZONTAL STAB, CENTER SECTION FWD & AFT SPAR LUGS, CORRODED. REPAIRED HORIZONTAL STAB CENTER SECTION LUGS PER SRM. 2L72 4F RTA16WE 20040728001912004072800191NM 2004 7 28 SWAA042061 120040720A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040728001962004072800196NM 2004 7 28 SWAA042049 120040719A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040728002002004072800200 2004 7 28 SWAA042053 420040720A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040730000012004073000001NM 2004 7 30 04FDEA02227 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RIGHT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.877. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80311, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000052004073000005NM 2004 7 30 SWAA042138 120040727A53116546525 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND FRAME AT BS 380, STRINGER 15R, STRINGER 16R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040730000062004073000006NM 2004 7 30 SWAA042139 120040727A53116546534 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND FRAME AT BS 520, STRINGER 12L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040730000072004073000007NM 2004 7 30 SWAA042140 120040727A53306545770 SKIN BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 621, STRINGER 4L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040730000082004073000008NM 2004 7 30 SWAA042141 120040727A575465C26602311A SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20040730000092004073000009NM 2004 7 30 SWAA042142 120040727A53156545805 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 270, RBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM. 2L72 4F RTA16WE 20040730000112004073000011 2004 7 30 SWAA042144 420040727A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29667SW 23063 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040730000122004073000012NM 2004 7 30 04FDEA02228 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.124 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000142004073000014NM 2004 7 30 04FDEA02230 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RIGHT HAND WING INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8982. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80311, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000162004073000016NM 2004 7 30 04FDEA02232 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8806. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80313, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000172004073000017NM 2004 7 30 04FDEA02233 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8772. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80313, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000182004073000018NM 2004 7 30 04FDEA02234 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.402 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000192004073000019NM 2004 7 30 04FDEA02235 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE INBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.882. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80313, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000212004073000021NM 2004 7 30 04FDEA02237 120040728A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8784. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80310, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000232004073000023NM 2004 7 30 04FDEA02239 120040728A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER=0.876, FINAL DIAMETER=0.8932. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80310, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES. CORROSION REPAIR. 2L73 4F RTA22WE 20040730000242004073000024NM 2004 7 30 04FDEA02240 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.009, REMAINING THICKNESS = 0.491 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000252004073000025WP 2004 7 30 04FDEA02166 120040723A5320ACA37777 INTERCOSTAL DOUG DC10 DC1030 3023501WP NLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 NOSE GEAR WHEEL WELL FWD PRESSURE BULKHEAD ACCESS DOOR 115AZ INSIDE BOTTOM CORRODED. REMOVED AND REPLACED INTERCOSTALS IAW SRM 51-31-01 AND SRM 51-35-01 ON N/R N00743 AT MAE. 2L73 4F A22WE 20040730000292004073000029NM 2004 7 30 04FDEA02242 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.125 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000302004073000030NM 2004 7 30 04FDEA02243 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.407 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000352004073000035NM 2004 7 30 04FDEA02248 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.401 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000362004073000036NM 2004 7 30 04FDEA02249 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.499, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.494 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000382004073000038NM 2004 7 30 04FDEA02251 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.105 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000402004073000040NM 2004 7 30 04FDEA02179 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 910 LBL 48. AREA REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70- 00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040730000412004073000041NM 2004 7 30 04FDEA02252 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.510, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.505 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000422004073000042NM 2004 7 30 04FDEA02253 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.504, MATERIAL REMOVED = 0.024, REMAINING THICKNESS = 0.480 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000452004073000045NM 2004 7 30 04FDEA02256 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.415, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.408 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000462004073000046NM 2004 7 30 SWAA042145 120040727A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29402WN 29814 DURING SCHEDULED C3 CHECK, FWD EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040730000472004073000047NM 2004 7 30 SWAA042146 120040727A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVERS AT ROW 13 ABC, ROW 18 ABC, BROKEN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040730000512004073000051NM 2004 7 30 SWAA042132 120040727A30402315 CONTROLLER BOEING737 7377H4 1384404NM COCKPIT WINDOW ARCED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29400WN 27891 ON DESCENT AT 12,000 FT AND 250 KIAS, COCKPIT R1 WINDOW OUTER PANE SHATTERED. ELECTRICAL ARCHING FROM HEATING ELEMENTS. REMOVED AND REPLACED COCKPIT R1 WINDOW AND RH WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20040730000522004073000052NM 2004 7 30 04FDEA02173 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1089 RBL 48. DAMAGED SEAT TRACK AT CABIN STA 1089 RBL 48 REMOVED AS PER SRM 53-70- 00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040730000552004073000055NM 2004 7 30 04FDEA02176 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1169 LBL 48. REMOVED AS PER SRM 53-70- 00, FIGURE 1, VOLUME I AND 51-31-01, VOLUME II. REPAIR TRACK AND SPLICE FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040730000572004073000057NM 2004 7 30 04FDEA02170 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1089 RBL 28. REMOVED AS PER SRM 51-31- 01, VOLUME II AND SRM 53-70-00, FIGURE 1, VOLUME I. REPAIR TRACK AND PARTS FABRICATED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040730000602004073000060NM 2004 7 30 SWAA042109 120040725A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040730000612004073000061NM 2004 7 30 SWAA042110 120040725A534365C10300 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING RON, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG FITTING PER SRM. 2L72 4F RTA16WE 20040730000622004073000062NM 2004 7 30 SWAA042111 120040725A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040730000632004073000063NM 2004 7 30 SWAA042112 120040725A57536546481 SPINDLE BOEING737 7373H4 1384600NM RT WING TE FLAP FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 INBOUND CREW REPORTED A HEAVY THUMP WHEN FLAPS 30 SELECTED. UPON INSPECTION, MX REPORTED RT OUTBOARD FLAP SPINDLE FAILURE. REMOVED AND REPLACED RT OUTBOARD FLAP SPINDLES PER MM. 2L72 4F RTA16WE 20040730000652004073000065NM 2004 7 30 SWAA042114 120040725A53206920158 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT RT AND LT BS 188 TO BS 196, CRACKED. REMOVED AND REPLACED FLOOR WEB PER SRM. 2L72 4F RTA16WE 20040730000672004073000067NM 2004 7 30 04FDEA02177 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 800 RBL 6. REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040802000012004080200001NM 2004 8 2 04FDEA02266 120040728A533065183868 SKIN BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CRACK IN SKIN AT EDGE OF LAP JOINT BS 1064 RBL 26 STR 26R. 2L73 4F RTA3WE 20040802000022004080200002NM 2004 8 2 AMTA200400318 120040318A2910 LINE BOEING757 75723N 1384973NM HYD PUMP DRAIN LEAKING A AMTAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11518AT 27974 LEFT HYDRAULIC QUANTITY EICAS MESSAGE FOLLOWED BY 'RSVR' ON OVERHEAD PANEL. REPLACED LEFT ENGINE HYD PUMP CASE DRAIN LINE WITH SERVICEABLE PREFABRICATED HIGH PRESSURE HOSE PER GMM CH 3, P46. NO LEAKS NOTED. (M) 2L72 4F RTA2NM 20040802000042004080200004EU 2004 8 2 SIMA200408803 120040327A335066902 LIGHT SAAB SF340 340B 7860101EU ROW 6A-8A INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21387AE 340B387 ILE - FLT 3394 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTING AT ROWS 6A AND 8A TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIPS IAW SAAB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040802000062004080200006EU 2004 8 2 2004F00218 120040128A2460 CIRCUIT BREAKER FOKKERF27 F27MK600 4990706EU DC SYSTEM TRIPPED A COEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NM13702FE 10350 AFTER DEPARTURE FROM FSD, THE AIRCRAFT EXPERIENCED A DC ELECTRICAL SYSTEM FAILURE. CREW SELECTED EMERGENCY POWER AND RETURNED TO FSD, NO EMERGENCY WAS DECLARED. TROUBLESHOT DC POWER SYSTEM, FOUND REVERSE CURRENT RELAY CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. OPS CHECKED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20040802000072004080200007EA 2004 8 2 A6WA200440036 120040322A32465010598 WHEEL CNDAIRCL600 CL6002B19 1900309EA NLG BENT A A6WAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL31422AW200 7341 STRUCK SOMETHING ON RUNWAY ON TAKEOFF ROLL. NOSE WHEEL BENT, LESS THAN 60 KNOTS, MIN BRAKE USED. INSPECTED NOSE TIRES, NR 2 WHEEL HALF DAMAGED, VISUALLY INSPECTED NOSE STRUT AND SPINDLE. ALSO INSPECTED FUSELAGE, LEADING EDGE AND BOTH ENGINE INTAKES. NO DAMAGE NOTED AT THIS TIME. REMOVED AND REPLACED NOSE WHEEL TIRE ASSEMBLY IAW AMM 32-42-01. (M) 2L72 4F RTA21EA 20040802000082004080200008NM 2004 8 2 AMTA200400338 120040323A2613 OVERHEAT SENSOR BOEING757 75733N 1384931NM LT STRUT MALFUNCTIONED A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11557TZ 32591 EICAS MESSAGE LT STRUT OH DET 2 INTERMITTENT. PERFORMED FIM 26-12-00 FIG 104 SYSTEM OPS CORRECTLY. PERFORMED STRUT OH DET SYSTEM, BITE PROCEDURE, COMPONENTS AND WIRE INTERFACE OPERATED CORRECTLY PER FIM 26-12-00 FIG 103. (M) 2L72 4F RTA2NM 20040802000092004080200009NM 2004 8 2 2004F00219 120040128A3250 STEERING SYS BOEING727 727224 1384076NM NWS OUT OF ADJUST A FX7AD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO1979750 22452 DISCONTINUED TAKEOFF ROLL, DUE TO LACK OF STEERING CONTROL TO THE RIGHT. RETURNED TO RAMP WITHOUT INCIDENT. ADJUSTED RUDDER PEDAL STEERING MECHANISM PER MM 32-51-0. OPS CHECK GOOD. (M) 2L73 4F A3WE 20040802000142004080200014NM 2004 8 2 GAIA04054OP 120040317A275140174 SWITCH BOEING727 727243 138408DNM RT WING LE FLAP INOPERATIVE A GAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07579PE 21662 FLT 753 - CLT-FWA - DURING TAXI, THE FLIGHT CREW NOTICED THAT THE NR 5 LEADING EDGE DEVICE WOULD NOT EXTEND. REMOVED AND REPLACED THE NR 5 LEADING EDGE FLAP POSTION SWITCH. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040802000152004080200015WP 2004 8 2 2004F00220 120040303A5313609458 STRINGER DOUG DC3 DC3C 3021457WP FUSELAGE CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11376AS 27047 DURING PERIODIC CHECK INSPECTION MAINTENANCE, FOUND CORROSION ON THE RIGHT SIDE OF FUSELAGE STRINGER BELOW FLOOR LEVEL AT STATION 312.5 TO 450.5. THE STRINGER WAS REMOVED FOR REPLACMENT. (M) 2L72 4R A669 20040802000162004080200016NM 2004 8 2 AMTA200400381 120040331A3397 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11520AT 27976 FOUND TWO EGRESS TRACK LIGHTS INOPERATIVE AT SEAT 8 DEF. RESECURED CONNECTOR ON EGRESS TRACK LIGHT AT 8DEF REF AMM 33-51-11, OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20040802000172004080200017EU 2004 8 2 2004F00221 120040406A5610 WINDSHIELD AIRBUS320 A320233 3930329EU COCKPIT BIRD STRIKE A RJEFA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO23981LR 558 DURING CLIMB, A BIRD STRUCK THE LEFT WINDSHIELD, CRACKING THE OUTER PLY OF THE WINDSHIELD. THE AIRCRAFT DIVERTED ITS NORMAL FLIGHT TO EL SALVADOR STATION. AFTER LANDING AT SAL STATION, TECHNICIANS PERFORMED INSPECTION DUE BIRD STRIKE PER AMM 05-51-14. THE LEFT WINDSHIELD WAS FOUND DAMAGED. IT WAS REPLACED PER AMM 56-11-11. IT WAS PERFORMED INSPECTION OF BOTH ENGINES PER AMM 72-00-00-200-010. THE INSPECTION REVEALED NO EXTERNAL OR INTERNAL DAMAGE ON BOTH ENGINES. NO OTHER DAMAGES WERE FOUND ON THE FUSELAGE. ALSO AN IMPACT ON THE NOSE RADOME WAS FOUND. THE RADOME WAS INSPECTED, PER NTM 51-10-06, NO DAMAGE WAS FOUND. THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040802000202004080200020 2004 8 2 GTIA040568 420040612A2565D29982113 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 LGA - OFUND R1 DOOR EVAC SLIDE ON RAMP BACK SHELL DAMAGED. REMOVED AND REPLACED R1 DOOR SLIDE, OK FOR SERVICE. (M) 2L72 4F A6WE 20040802000222004080200022CE 2004 8 2 2004F00223 120040108A7810235510026 NOZZLE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE EXHAUST DAMAGED A CEDABA EMER. DESCENT UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05233CA 133 251414A BRO - ON CLIMB-OUT, THE NR 1 ENGINE FLAMED OUT AT 39,600 FEET. THE AIRCRAFT DESCENDED TO FLIGHT LEVEL 25,000 FEET AND RESTARTED THE ENGINE. THE AIRCRAFT THEN DIVERTED TO ADS, AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS INSPECTED AND THE EXHAUST NOZZLE WAS CHANGED PER GE SB 72-140 AND LEARJET SSK 959. THE AIRCRAFT WAS TEST FLOW AND CHECKED GOOD. (M) 2L72 4J4 J A10CE 1E16 20040802000232004080200023EU 2004 8 2 2004F00224 120040116A3350 SWITCH BAG JETSTMJETSTM3101 1500215EU EMERGENCY LIGHT INOPERATIVE A B16AK NONE L NO TEST ININSP/MAINT 1 NE05538PA 751 PILOT REPORTED, EMERGENCY LIGHT CIRCUIT BREAKER POPPED WITH LIGHT SWITCH IN ARM AND OFF POSITION, BATTERY MASTER ON. ISOLATED FAULT USING J-31 WIRING MANUAL PG 33-50-01 AND 33-20-01. SHORT CIRCUIT FOUND AT MAIN DOOR EXIT SIGN. REPAIRED SHORT BY REPOSITIONING 28 VOLT LAMP CONTACT. FUNCTIONAL TEST OF EMERGENCY LIGHTING GOOD IAW J-31 AMM 33-50-00. (M) 2L72 4T RTA21EU 20040802000262004080200026NM 2004 8 2 ASAA0410267 120040517A5311BAC14702807 FRAME BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 FOUND CRACKED FRAME. REPLACED FRAME. (M) 2L72 4F A16WE 20040802000272004080200027NM 2004 8 2 ASAA0440085 120040316A5320BAC1509100146 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01783AS 25114 OAK -FOUND AFT CARGO COMPARTMENT BILGE AREA LBL 3 LONGITUDINAL FLOOR SUPPORT CHANNEL IS CORRODED AT FLOOR PANEL SPLICE STRAP ATTACH HOLES BETWEEN STATOIN 767 AND 787. REPLACED LONGITUDINAL FLOOR SUPPORT CHANNEL FROM STATION 727G AND STATION 787 USING EXISTING SPLICES. (M) 2L72 4F RTA16WE 20040802000282004080200028WP 2004 8 2 GTIA040589 120040524A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FOUND FLOOR SUPPORT AT STATION 200 TO 260 LBL 15 HAS CORROSION. REMOVED FLOOR SUPPORT. FLOOR SUPPORT FABRICATED. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040802000332004080200033WP 2004 8 2 GTIA040598 120040512A5320 ANGLE DOUG DC9 DC983 3022083WP FS CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND TEE ANGLE EXFOLIATED IN AFT ACCY COMP AT FS 1474 15 INCHES LBL, NEAR LONGERON 3L. REMOVED 'T' ANGLE. FABRICATE 'T' ANGLE. INSTALLED 'T' ANGLE. (M) 2L72 4F RTA6WE 20040802000342004080200034WP 2004 8 2 GTIA040604 120040615A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND LEFT CABIN FLOOR PANEL STATION 200-257 BROKEN INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040802000382004080200038WP 2004 8 2 GTIA050616 120040612A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND COCKPIT FLOOR PANEL CENTER FS 120-148 IS DAMAGED SEVERAL PLACES. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040802000392004080200039WP 2004 8 2 GTIA040617 120040605A5310 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND AFT AIRSTAIR DOOR JAMBS AFT WEB CORRODED. CUT OUT PORTION OF CRACKED WEB. FABRICATED WEB. INSTALLED WEB. (M)WEB 2L72 4F RTA6WE 20040802000402004080200040WP 2004 8 2 GTIA040619 120040610A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND CENTER CABIN FLOOR PANEL STATION 552-560 BROKEN EDGES. FABRICATED NEW PANEL. (M) 2L72 4F RTA6WE 20040802000432004080200043WP 2004 8 2 GTIA040588 120040524A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND CENTER CABIN FLOORBOARD STATION FS 200-256 INSERTS PULLED THROUGH. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040802000442004080200044WP 2004 8 2 GTIA040591 120040608A7120K22199SA32 ISOLATOR DOUG DC9 DC983 3022083WP RT ENGINE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND RIGHT ENGINE PYLON AFT VIBRATION ISOLATOR CONCEAL SURFACE PITTED. REMOVED AFT VIBRATION ISOLATOR. INSTALLED SERVICEABLE AFT ISOLATOR. (M) 2L72 4F RTA6WE 20040802000452004080200045EU 2004 8 2 USAA04345 120040610A5347D5311278220201 SEAT TRACK AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND CORROSION ON SEAT TRACK, 2 INCHES BY 1 INCH BY .026 INCH. REPLACED SEAT TRACK. (M) 2L72 4F RTA28NM 20040802000462004080200046 2004 8 2 USAASB04082 420040628A2565D17978113 RESERVOIR BOEING737 7373B7 1384580NM AFT DOOR SLIDE DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US11503 22957 MCO - FOUND THE AFT RIGHT SLIDE BOTTLE PRESSURE READING 'ZERO'. MAINTENANCE REPLACED THE SLIDE. (M) 2L72 4F RTA16WE 20040802000472004080200047NM 2004 8 2 GTIA040581 120040618A3610 AUGMENT VALVE DOUG MD80 MD83 3023681NM LEFT DAMAGED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23822NK 49392 MCO - FLT 940 - DURING THE USE OF ENGINE ANTI-ICE ON, PASSENGER COMPLAINED OF A BAKEOLITE OR OTHER SUBSTANCE, BURNING/OVER HEAT ODOR. REMOVED AND REPLACED LEFT AUG VALVE. (M) 2L72 4F RT 20040802000512004080200051NM 2004 8 2 GAIA04055OP 120040318A3260656021136 ACCESSORY UNIT BOEING727 727224 1384076NM E/E BAY MLG MALFUNCTIONED A GAIAO OTHER N FALSE WARNING CLCLIMB 1 SW0769739 20667 FLT 772 - DTW-FWA - NOSE GEAR RED LIGHT ON GEAR ANNUNCIATOR PANEL CAME ON AFTER GEAR RETRACTION. RERACKED LANDING GEAR ACCESSORY UNIT. CYCLED GEAR NUMEROUS TIMES. NO DEFECTS NOTED. OPS CHECK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040802000532004080200053NM 2004 8 2 ASAA0440106 120040417A53116547959501 FRAME BOEING737 737490 1384715NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01703AS 28893 OAK - AFT CARGO FRAME AT BS 794.3 HAS DAMAGE FROM STOP DRILLING, PER EA 5310-02274, PERMANENT REPAIR TO BE ACCOMPLISHED AT C-CHECK. REMOVED STOP DRILL DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER REPAIR REF SRM 51-70-11 PAGES 1-5. (M) 2L72 4F RTA16WE 20040802000542004080200054NM 2004 8 2 ASAA0440130 120040514A53306545767193 SKIN BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01774AS 25107 SEA - ON WALK AROUND, FOUND DENT/CRACK IN FUSELAGE SKIN ON BS 363 S17L. REPAIRED PER EA 5330-01779. (M) 2L72 4F RTA16WE 20040802000592004080200059NM 2004 8 2 ASAA0440082 120040316A5320655384422 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01783AS 25114 OAK - FOUND CORROSION BETWEEN RIGHT STATION 787-793 FLOOR SUPPORT BEAM. REMOVED AND REPLACED FLOOR SUPPORT BEAM. (M) 2L72 4F RTA16WE 20040802000612004080200061NM 2004 8 2 USAASB04076 120040625A3230655825029 CIRCUIT CARD BOEING737 737301 1384611NM MLG MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19558AU 23512 ON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, CREW RECEIVED A RIGHT MLG UNSAFE INDICATION WITH GEAR UP AND LOCKED. FLIGHT RETURNED TO FIEDL AT BOS AND LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED RECEIVING A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS WHEN EXTENDING THE GEAR. NO EMERGENCY WAS DECLARED. MAINTENANCE SWUNG THE GEAR AND WAS UNABLE TO DUPLICATE THE PROBLEM. REMOVED AND REPLACED THE M982 ANDM986 PRINTED CIRCUIT CARDS, AS PRECAUTIONARY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040802000662004080200066NM 2004 8 2 USAA040300 120040526A57536546435273 SKIN BOEING737 7374B7 1384702NM LT TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US38197 24893 FOUND SKIN DELAMINATED WITH CORROSION 13 INCHES LONG BY 8 INCHES WIDE, LT OUTBOARD AFT FLAP INBOARD T/E TOP SURFACE HEAVY CORE CORROSION. INSTALLED NEW CORE PER T/R 57-50-39A. LEVEL 1, TASK NR C57-306-01. (M) 2L72 4F RTA16WE 20040802000672004080200067NM 2004 8 2 USAA040297 120040527A575465C26602218 SKIN BOEING737 737301 1384611NM NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US 23934 PIT - FOUND SKIN AND CORE DELAMINATED 4 INCHES BY 4 INCHES, NR 5 SLAT OUTBOARD END TRAILING EDGE SECTION. INSTALLED NEW CORE PER SRM 51-20-10. (M) 2L72 4F RTA16WE 20040802000682004080200068NM 2004 8 2 USAA040296 120040607A57540032794 SKIN BOEING737 737401 1384701NM NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US 23991 PIT - FOUND SKIN TO CORE DELAMINATED 1 INCH BY 5 INCH AREA, RT WING NR 4 SLAT OUTBOARD TRAILING EDGE. INSTALLED REPAIR CORE AND TOP DOUBLER, SEALED DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040802000692004080200069NM 2004 8 2 USAA040295 120040607A5754 SKIN BOEING737 737401 1384701NM NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 PIT - FOUND SKIN TO CORE DELAMINATED AND KNIFE EDGE WEAR, RT WING NR 4 SLAT INBOARD TRAILING EDGE. INSTALLED FILLER AND INTERNAL DOUBLER REPAIR COREW, TOP REPAIR DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040802000702004080200070NM 2004 8 2 USAA040292 120040526A57536546435273 SKIN BOEING737 7374B7 1384702NM LT TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19449US38197 24893 PIT - FOUND SKIN AND CORE DELAMINATED 13 INCHES LONG BY 8 INCHES WIDE, LT OUTBOARD AFT FLAP, INBOARD T/E TOP SURFACE, HEAVY CORE CORROSION. INSTALLED NEW CORE, SKIN PANEL AND DOUBLER PER T/R 57-50-39A. (M) 2L72 4F RTA16WE 20040802000712004080200071NM 2004 8 2 USAA040291 120040609A5311 FRAME BOEING737 7373B7 1384580NM BULKHEAD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU 23702 PIT - FOUND LOWER LEG OF CHORD CORRODED .5 INCH BY 1 INCH AREA, AFT SIDE OF PRESSURE BULKHEAD FROM STRINGER 27L TO 26L. CLEANED CORROSION, TREATED AND PRIMED PER SRM 51-10-02 AND 51-20-01. (M) 2L72 4F RTA16WE 20040802000722004080200072NM 2004 8 2 USAA040290 120040608A5340 LUG BOEING737 737301 1384611NM BEARING WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US50842 23231 PIT - FOUND BEAR LUG WORN, BEARING LUG BORE WORN INSIDE DIAMETER SURFACE .75 INCH. ROTO PEENED BORE ID PER TYPE REPAIR 54-50-09 REV C. (M) 2L72 4F RTA16WE 20040802000742004080200074 2004 8 2 GTIA040625 420040623A2565 SLIDE DOUG DC9 DC983 3022083WP TAIL CONE MISINSTALLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 DTW - AFT TAILCONE SLIDE PACK COVER FORWARD HOLD DOWN STRAPS FOUND INSTALLED INCORRECTLY. INSTALLED AFT TAILCONE SLIDE PACK COVER. NO OTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040802000752004080200075NM 2004 8 2 AMTA200400801 120040625A5711 PLATE BOEING757 75723N 1384973NM RT WING SPAR CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 FOUND RIGHT WING T/E LOWER SPAR WIGGLE PLATE CRACKED AND PULLED FASTENERS BETWEEN WS 328 TO WS 336. FOUND CRACK TO BE OUT OF LIMITS. REMOVED AND REPLACED THE RT WING T/E LOWER SPAR WIGGLE PLATES FROM WS 328 TO WS 336 IAW SRM 51-40-02 AND SRM 51-40-05. (M) 2L72 4F RTA2NM 20040802000782004080200078NM 2004 8 2 C7WA200400012 120040412A5230MS2000116 HINGE BOEING727 7272Q6 138407VNM CARGO DOOR CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO171279E 21971 FOUND MAIN CARGO DOOR FORWARD HINGE HAS A CRACKED LOBE. REPLACED FORWARD HING HALF IAW AERONAUTICAL ENGINEERS INC SERVICE BULLETIN AE101-01. (M) 2L73 4F RTA3WE 20040802000792004080200079NE 2004 8 2 GTIA040627 220040621A7250 TURBINE WHEEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 1 ENGINE DAMAGED A GTIAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 GL23824NK 53015 718229 NR 1 ENGINE FAILED DURING TAKEOFF, 10K AND 1.50 EPR. FOUND NR 1 TURBINE SECTION DAMAGED BEYOND LIMITS. REMOVED AND REPLACED NR 1 ENGINE, OPS AND LEAK CHECKED GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20040802000802004080200080WP 2004 8 2 GTIA040630 120040625A2530 COFFEEMAKER DOUG DC9 DC983 3022083WP GALLEY ODOR A GTIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23815NK 49415 FLT 931 - ORD - LEAD F/A OBSERVED A BURNING SMELL FROM FORWARD GALLEY COFFEE MAKER. THE LIGHT THEN WENT OUT CAPTAIN TURNED OFF GALLEY POWER, SMELL STOPPED. RESET C/B ON BACK OF COFFEE MAKER AND RALAMPED POWER LAMP, PERF BREWING OPS CHECK GOOD. NO LEAKS NOTED FOUND OK TO CONT. (M) 2L72 4F RTA6WE 20040728001952004072800195NM 2004 7 28 SWAA042066 120040720A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040730000042004073000004NM 2004 7 30 SWAA042137 120040727A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 420, STRINGER 10R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040730000152004073000015NM 2004 7 30 04FDEA02231 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.506, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.502 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000262004073000026NM 2004 7 30 04FDEA02167 120040726A5350 FRAME DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD TAIL CONE FORWARD FRAME CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040730000332004073000033NM 2004 7 30 04FDEA02246 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 1 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER=1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000342004073000034NM 2004 7 30 04FDEA02247 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.192 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000372004073000037NM 2004 7 30 04FDEA02250 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER=1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RIGHT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000392004073000039NM 2004 7 30 04FDEA02178 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 894-910 RBL 48. DAMAGED AREA REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040730000482004073000048NM 2004 7 30 SWAA042147 120040727A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 21 ABC INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 21 ABC. REMOVED AND REPLACED EEPLS LIGHT PER MM. 2L72 4F RTA16WE 20040730000492004073000049NM 2004 7 30 SWAA042148 120040727A53306545775594 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040730000502004073000050NM 2004 7 30 SWAA042131 120040727A335020131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29387SW 26602 AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040730000532004073000053NM 2004 7 30 04FDEA02174 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1059 RBL 48. DAMAGED SEAT TRACK AT CABIN STA 1059 RBL 48 REMOVED AS PER SRM 51-31- 01 VOL II & SRM 53-70-00 FIG 1 VOL I. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040730000562004073000056NM 2004 7 30 04FDEA02169 120040726A5350 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD TAIL CONE RIGHT HAND FORWARD LOWER SKIN CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040730000592004073000059NM 2004 7 30 04FDEA02172 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACKS FOUND DAMAGED AT STA 1301 RBL 47. DAMAGED SEAT TRACK AT CABIN STA 1301 RBL 47 REMOVED AS PER SRM 53-70- 00 FIG 1 VOL I. REPAIR PARTS FABRICATED & ISNTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31- 01 VOL II. 2L73 4F RTA22WE 20040802000052004080200005NM 2004 8 2 UIEA200400036 120040326A245065B6220613 PDU BOEING747 7472D3B 1384805NM SMOKE A UIEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA15506MC 21252 ANC/DFW - PDU MAIN DECK POSITION 18R INOPERATIVE STARTED SMOKING. REMOVED PDU FOUND MOTOR INOPERATIVE. REMOVED CONNECTOR AND DEACTIVATED PDU. TRANSFERRED TO DI PAGE 55833 DMI C-4-003. (M) 2L74 4F RTA20WE 20040802000822004080200082WP 2004 8 2 GTIA040628 120040624A3310 RHEOSTAT DOUG DC9 DC983 3022083WP MAP LIGHT BURNED OUT A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23836NK 53045 ORD - FLT 1108 - AFTER LEVELING OFF AT 330, SMELLED SMOKE. NOTICED IT IN THE OVERHEAD MAP LIGHT. I WENT TO TURN THE LIGHT UP AND THE REOSTAT WAS VERY HOT TO THE TOUCH, PULLED THE C/B. REMOVED AND REPLACED CAPTAINS OVERHEAD LIGHT RHEOSTAT. (M) 2L72 4F RTA6WE 20040802000832004080200083WP 2004 8 2 GTIA040629 120040626A2910 LINE DOUG DC9 DC982 3022082WP MLG HYD SYS LEAKING A GTIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL23820NK 49126 LGA - FLT 779 - JUST AFTER TAKEOFF LGA, STRANGE ODOR CAME THROUGH VENTS. BRAKE TEMP INDICATOR LIGHT WAS FLASHING AND TEMP NEEDLE MOVING, LEFT LANDING GEAR DOWN TO MAKE SURE NO BRAKE HEAT, LIGHT WENT OUT, ODOR WENT AWAY. FOUND NR 2 BRAKE AFT HYD LINE LOOSE AND LEAKING, RE-INSTALLED, TIGHTEN AND SAFETY WIRED NR 2 BRAKE AFT HYDRAULIC LINE LEAK AND OPS CHECK OK BRAKE SYSTEM OPERATED LEFT AND RIGHT A/C PACKS, NO ODOR NOTICED IN A/C SYSTEM. (M) 2L72 4F A6WE 20040802000842004080200084WP 2004 8 2 GTIA040631 120040626A3230 BUNGEE CYLINDER DOUG DC9 DC983 3022083WP MLG DAMAGED A GTIAO OTHER J WARNING INDICATION APAPPROACH 1 GL23827NK 49793 ON FINAL APPROACH, 3 GREEN LANDNG GEAR, THEN AT 500 FEET RT MLG FLICKERED RED, THEN WENT STEADY RED ACCOMPANED BY LANDING GEAR WARNING HORN. FOLLOWED QRH PULLED THEN STOWED EMERGENCY LANDING GEAR HANDLE AFTER GETTING 3 GREEN LIGHT, LANDING UNEVENTFUL. LUBED OVER CENTER LINKS AND REMOVED AND REPLACED MLG BUNGEE CYLINDER, OPS AND LEAK CHECK GOOD ON GEAR SWING. (M) 2L72 4F RTA6WE 20040802000862004080200086NM 2004 8 2 C7WA200400013 120040412A5311 FRAME BOEING727 7272Q6 138407VNM FUSELAGE CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO171279E 21971 FOUND FUSELAGE FRAME CRACKED FS 680 WL 208. REPAIRED FUSELAGE FRAME IAW B727 MM 51-40-3. (M) 2L73 4F RTA3WE 20040802000902004080200090NM 2004 8 2 USAA040298 120040526A575465C26603100 SKIN BOEING737 737301 1384611NM NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US51120 23934 PIT - FOUND SURFACE TO CORE DELAMINATION 3 INCHES BY 2.5 INCH AREA, NR 4 SLAT TOP SURFACE INBOARD TRAILING EDGE. INSTALLED NEW CORE AND EXT DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040802000972004080200097EU 2004 8 2 2004F00211 120040118A2910NAS16128 PACKING AIRBUS320 A320233 3930329EU MLG HYD SYSTEM LEAKING A RJEFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO23451TA 733 SAP - FLT TAI390, DURING GROUND INSPECTION, FOUND A HYDRAULIC LEAK IN THE RIGHT WHEEL WELL. TECHS PERFORMED AN INSPECTION OF THE WHEEL WELL AREA AND FOUND THAT THE LEAK SOURCE WAS ON A FITTING ON THE AUTOMATIC BRAKE SELECTOR VALVE AND TWO SEALS WERE REPLACED AT THE VALVE PER AMM 32-42-13. THE SYSTEM WAS TESTED PER AMM 32-42-13 AND NO LEAKS WERE FOUND. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040802001002004080200100CE 2004 8 2 2004F00212 120040116A2130238015611 FLOW VALVE LEAR 25 25B 5170511CE CABIN PRESSURE INOPERATIVE A CEDAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05140CA 140 DEPARTED DTW, EN ROUTE TO ADS, AFTER ABOUT 5 MINUTES AT FLIGHT LEVEL 390 THE ALTITUDE ALERTER CAME ON. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES AND LANDED AT SUS WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND FLOW CONTROL VALVE HAD GONE BAD. REPLACED FLOW CONTROL VALVE ALL OPERATIONAL CHECKS AND TEST FLIGHT CHECK GOOD. (M) 2L72 4J A10CE 20040802001062004080200106NM 2004 8 2 USAASB04013 120040129A3297BR20AXH5V3 RELAY BOEING737 7373B7 1384580NM MLG MALFUNCTIONED A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19387US 22959 BOS - FLT 2046 - AFTER TAKEOFF FROM DCA, EN ROUTE TO BOS, THE NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WHEN GEAR HANDLE WAS PLACED TO THE UP POSITION. CREW CONTACTED MAINTENANCE AND IT WAS AGREED UPON TO CONTINUE TO BOS. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND RECYCLED THE GEAR BUT RECEIVED THE SAME GEAR INDICATIONS. AT BOS, A TOWER FLYBY CONFIRMED THAT GEAR WAS DOWN. UPON LANDING, THE NOSE LANDING GEAR RED LIGHT EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. CREW DID DECLARE AN EMERGENCY. MAINTEANCE REMOVED AND REPLACED THR R374 NOSE LANDING GEAR LATCHING RELAY. OPERATIONAL CHECK AND INDICATION CHECK OF NOSE LANDING GEAR NORMAL. (M) 2L72 4F RTA16WE 20040802001082004080200108NM 2004 8 2 AMTA200400806 120040628A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM FORWARD GALLEY TO ROW 2. RECONNECTED WIRING INTO ROW 2. EGRESS LIGHTS CHECK GOOD FROM FORWARD GALLEY TO ROW 2. (M) 2L72 4F RTA2NM 20040802001142004080200114NE 2004 8 2 REXA04003 220040131A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE LT ENGINE LOW A REXAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO258444F 7444 FLIGHT CREW RECEIVED AN AURAL OIL PRESSURE WARNING FOR THE LEFT ENGINE. OIL PRESSURE WAS OBSERVED TO BE FLUCTUATING BETWEEN 25-30 PSI. FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN, DECLARED AN EMERGENCY AND WAS DIVERTED TO TULSA. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT TUL. MAINTENANCE FOUND THE LEFT ENGINE TO BE LOW ON OIL. THE ENGINE WAS SERVICED AND A GROUND RUN LEAK CHECK WAS PERFORMED. THE LEAK CHECK WAS SATISFACTORY. HOWEVER, THIS ENGINE HAS BEEN PLACED ON OIL WATCH TO PRECLUDE A REPEAT OIL LOSS EVENT. (M) 2L72 4F4 FRTA21EA E15NE 20040802001172004080200117EA 2004 8 2 ASOA04411 120040605A5210 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A GROUND INSPECTION IN DFW, THE FLT ATTENDANT REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HINGE POINTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001222004080200122WP 2004 8 2 GTIA040622 120040607A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND LEFT OUTBOARD SEAT TRACKS STATION 200-798 GOUGED AND CORRODED. FOUND STATION 790-798 OUT OF LIMITS. REMOVED SEAT TRACK STATION 760-837. LOCATED AND DRILLED NEW TRACK SECTION AND SPLICE. INSTALLED SEAT TRACK. (M) 2L72 4F RTA6WE 20040802001252004080200125WP 2004 8 2 GTIA040621 120040625A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND RIGHT INBOARD SEAT TRACKS STATION 798-1309 GOUGED AND CORRODED. FOUND TRACK OUT OF LIMITS FROM STATION 798 TO 817 AND 1260-1309. REMOVED TRACK SECTION FROM STATION 798 TO 817. FABRICATED SECTION OF TRACK. INSTALLED SECTION SEAT TRACK AND SPLICES AT STATION 798-817. REMOVED SEAT TRACK SECTION 1224-1309. LOCATED AND DRILLED SEAT TRACK. LOCATED NEW SPLICE. INSTALLED ONE SPLICE AT STATION 1222 AND SEAT TRACK FROM STATION 1222-1309. (M) 2L72 4F RTA6WE 20040802001302004080200130WP 2004 8 2 GTIA040569 120040608A2560 GLOWSTRIP DOUG DC9 DC982 3022082WP CABIN CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DTW - FOUND SAFETY GLOW COVER CRACKED, FORWARD LAV AREA ALSO NEEDS CLEANED. REPLACED SAFETY GLOW. (M) 2L72 4F A6WE 20040802001342004080200134EU 2004 8 2 BMAC040001 120040107A3350AD3128 BATTERY PACK BAG JETSTMJETSTM3101 1500215EU EMERGENCY LIGHTSINOPERATIVE A B16AK NONE L NO TEST ININSP/MAINT 1 NE05508PA DURING PREFLIGHT, EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL FOUR EMERGENCY LIGHT POWER PACKS. SUSPECT SWITCH WAS INADVERTENTLY LEFT ON. (M) 2L72 4T RTA21EU 20040802001352004080200135 2004 8 2 GTIA040551 420040622A2565 COVER DOUG DC9 DC983 3022083WP SLIDE MISINSTALLED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 DTW - FOUD TAILCONE EVACUATION SLIDE COVER IS NOT INSTALLED PROPERLY. REINSTALLED TAILCONE EVACUATION SLIDE COVER. NO DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040802001362004080200136 2004 8 2 GTIA040570 420040607A2565 RELEASE CABLE DOUG MD80 MD83 3023681NM SLIDE PACK MISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23828NK 49823 DTW - FOUND TAIL SLIDE COVER RELEASE CABLES NOT INSTALLED CORRECTLY. INSTALLED TAIL SLIDE COVER RELEASE CABLES PROPERLY. (M) 2L72 4F RT 20040802001422004080200142EU 2004 8 2 ASOA04401 120040602A33503011052 COVER AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11536AS 465 FLT 4297 - DUIRNG A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT COVER AT ROW 1-A/B WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER/LENS ASSEMBLY AT ROW 1-A/B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040802001452004080200145WP 2004 8 2 GTIA040575 120040616A2530 LANYARD DOUG DC9 DC982 3022082WP SLIDE PACK LOOSE A GTIAO OTHER O OTHER APAPPROACH 1 GL23817NK 49141 LGA - FLT 1581 - UPON ARRIVAL R1 SLIDE COVER LANYARD CAME LOOSE. REATTACHED LANYARD. NO DEFECTS NOTED. (M) 2L72 4F A6WE 20040802001462004080200146EA 2004 8 2 ASOA04406 120040602A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M) 2L72 4F RTA21EA 20040802001512004080200151EA 2004 8 2 ASOA04398 120040602A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES IN THE LOWER LEFT AND RIGHT CORNERS AT FS 621 OF THE CARGO COMPARTMENT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES IN THE LOWER LEFT AND RIGHT CORNERS AT FS 621 OF THE CARGO COMPARTMENT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040802001542004080200154EA 2004 8 2 ASOA04397 120040602A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625 BELOW THE BOX BEAM. (M) 2L72 4F RTA21EA 20040802001592004080200159 2004 8 2 GTIA040561 420040604A2565 SLIDE DOUG DC9 DC983 3022083WP L2 DOOR DEPLOYED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23836NK 53045 L2 DOOR SLIDE PACK CABLE FOR AUTO/MANUAL DEPLOY NOT HOOKED UP. REMOVED COVER AND REINSTALLED CABLE OT LANYARD AND REINSTALLED COVER. (M) 2L72 4F RTA6WE 20040802001602004080200160NM 2004 8 2 MEX2004051 120040208A32225920602507 LANDING GEAR DOUG MD88 MD88 3023688NM NOSE FAILED A ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23169PL 53175 FLT 296 - CUN-GDL - AIRCRAFT RETURNED, NLG DID NOT RETRACT. CAPTAIN REPORTED THE PERFORMED 3 CYCLES BUT FAIL REMAIN. AT PLATFORM, A MAINTENANCE SERVICE WAS PERFORMED TO THE NLG IAW MM 32-21-02 AND A TEST FLIGHT WAS REQUESTED TO VERIFY THE PERFORMANCE OF THE NLG, ALL CORRECT. DURING OVERNIGHT SERVICE, THE NLG ASSY WAS REPLACED IAW MM 32-21-02, MAINTENANCE SERVICE WAS PERFORMED TO THE NLG IAW MM 32-21-02, GROUND SENSING CONTROL MECHANISM WS VERIFIED IAW MM 32-23-01, RETRACTION AND EXTENSION TESTS WERE PERFORMED IAW MM 32-30-00, THE STEERING SYSTEM WAS TESTED IAW MM 32-52-00 AND THE NLG ACTUATOR WAS REPLACED IAW MM 32-32-06, ALL CORRECT. (M) 2L72 4F RTA6WE 20040802001632004080200163NE 2004 8 2 TSAA0479019 220040116A7261 ENGINE BOEING737 7372Y5 1384554NM PWA JT8 JT8D9A 52048NE NR 1 LEAKING A TSAAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13810AL 24031 FLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AND SHUTDOWN THE NR 1 ENGINE. DECLARED EMERGENCY AND HAD UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 1 ENGINE PER FORMS M-211 THROUGH M-215. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4U4 FRTA16WE E2EA 20040802001642004080200164NM 2004 8 2 C7WA200400004 120040309A5313 STRINGER BOEING737 737231 1384079NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO1754354 21986 FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED AT STRINGER 28 RIGHT FS 1030. CUT OUT DAMAGED SKIN AND STRINGER, STRINGER REPAIRED IAW 727 SRM 53-10-3, FIG 1, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M) 2L72 4F RTA16WE 20040802001652004080200165NM 2004 8 2 C7WA200400006 120040309A5330 SKIN BOEING727 727231 1384079NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO1754354 21986 FOUND LOWER FUSELAGE SKIN CORRODED AT STRINGER 30 RT BETWEEN FS 1050 AND 1062. CUT OUT DAMAGE, SKIN REPAIRED IAW 727 SRM 53-30-3, FIG 3. (M) 2L73 4F A3WE 20040802001662004080200166 2004 8 2 USAABB04004 420040106A2565140N27669 ATTACH FITTING BOEING757 757225 1384959NM R4 DOOR GIRT BARMISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 CLT - FOUND R4 DOOR SLIDE FORWARD GIRT BAR ATTACH FITTING MISSING. MAINTENANCE REPLACED THE GIRT BAR FITTING. (M) 2L72 4F RTA2NM 20040802001672004080200167GL 2004 8 2 15HA0358007 220040106A73106000F1A20 QUICK DISCONNECT CVAC 580 580 2422806WP ALLSN 501D 501D13D 03004GL RT ENGINE WORN A I5HAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL23582P 475 501090 IMMEDIATELY AFTER TAKEOFF FROM CLE, EN ROUTE TO CVG, RIGHT ENGINE AUTO-FEATHERED. THE CREW RETURNED TO CLE WHERE THEY MADE AN UNEVENTFUL SINGLE ENGINE LANDING. INSPECTION REVEALED THE RIGHT ENGINE MAIN FUEL FEED LINE 'QUICK DISCONNECT' FITTING AT THE FIRE WALL WAS PARTIALLY DISCONNECTED RESULTING IN FUEL STARVATION. AFTER FURTHER INVESTIGATION, THE DETERMINATION WAS MADE THAT THE QD WAS SUFFICIENTLY WORN TO HAVE ALLOWED IT TO WORK ITS WAY OFF DURING NORMAL ENGINE OPERATION. REMOVED AND REPLACED THE 'QUICK DISCONENCT' FITTING FOR THE MAIN FUEL FEED LINE AT THE FIRE WALL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 TRT E282 20040802001712004080200171EA 2004 8 2 ASOA04426 120040609A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M) 2L72 4F RTA21EA 20040802001722004080200172SO 2004 8 2 SIMA200417004 120040618A2121 FAN EMB 135 EMB135KL 3260302SO AVIONICS BAY OVERHEATED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21803AE 145483 SJC - FLT 3183 - DURING CRUISE FLIGHT CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. NO EMERGENCY DECLARED. LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE FOUND INSULATION IN FORWARD AVIONICS FAN CAUSING OVERHEAT CONDTION. INSULATION WAS REMOVED AND OPERATIONAL CHECK OF FAN WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040802001732004080200173NM 2004 8 2 AMTA200400732 120040613A2613579601 DETECTOR BOEING757 75733N 1384931NM OVERHEAT SYS INTERMITTENT A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 STATUS MSG 'LT ENG OH LP2' DISPLAYS INTERMITTENTLY. UNABLE TO DUPLICATE FAULT, REMOVED AND REPLACED LEFT ENG NACELLE OVERHEAT LOOP 1 AND 2 ASSY PER AMM 26-11-01-4 AS PRECAUTIONARY. LOOPS 1 AND 2 OPERATIONALLY CHECK NORMAL. (M) 2L72 4F RTA2NM 20040802001742004080200174NM 2004 8 2 USAA04336 120040622A5511 SPAR BOEING737 737301 1384611NM HORIZONTAL STAB DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 PIT - FOUND PROBLEM WITH PREVIOUS REPAIR ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB AT REAR SPAR LOWER SURFACE. REPAIRED PER SRM FIUTE 204 DETAIL NR 1. (M) 2L72 4F RTA16WE 20040802001752004080200175NM 2004 8 2 AMTA200400767 120040618A2613 WARNING LIGHT BOEING757 75733N 1384931NM LT ENGINE ILLUMINATED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11559TZ 32593 L ENG OVERHEAT EICAS MESSAGE DISPLAYED. SHUT OFF L ENG BLEED AIR SWITCH AND RETARDED THROTTLE PER QRH, MESSAGE CLEARED. COULD NOT DUPLICATE T/S PER FIM 26-11-00, NO LEAKS NOTED. (M) 2L72 4F RTA2NM 20040802001762004080200176EA 2004 8 2 ASOA04425 120040612A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11839AS 7284 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5-8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 5-8. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001772004080200177EA 2004 8 2 ASOA04417 120040609A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING A C-CHECK IN MCN, THE SCREW HOLES ON THE CARGO COMPARTMENT FLOOR SILL PLATE AT FS 562.72-589 WERE FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR SILL PLATE AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040802001782004080200178EA 2004 8 2 ASOA04415 120040609A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING A C-CHECK IN MCN, THE AVIONICS DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS DOOR HANDLE ASSEMBLY. (M) 2L72 4F RTA21EA 20040802001792004080200179EA 2004 8 2 ASOA04424 120040611A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING A C-CHECK IN MCN, THE INTERCOSTAL ANGLE AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTAL ANGLE AT FS 484, LBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040802001802004080200180 2004 8 2 GTIA040564 420040608A2565 SLIDE DOUG DC9 DC983 3022083WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 LAS - FLT 711 - FOUND L1 SLIDE PACK COVER LOOSE. RESECURED SLIDE PACK CABLE LANYARD. (M) 2L72 4F RTA6WE 20040802001822004080200182EA 2004 8 2 ASOA04414 120040607A1420487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 FLT 4402 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 2/4 WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTORS TO THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 2 AND 4 LOOSE AND RECONNECTED THEM. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001832004080200183EA 2004 8 2 ASOA04421 120040610A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11843AS 7310 FLT 4512 - DURING HANGAR MAINTENANCE IN BTR, THE LOWER LEFT EMERGENCY FLOOD LIGHT NEAR THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT EMERGENCY FLOOR LIGHT LAMP NEAR THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001852004080200185 2004 8 2 AMTA200400710 420040610A2565 SLIDE BOEING757 75723N 1384973NM R4 DOOR OUT OF ADJUST A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 FOUND R4 DOOR SLIDE WOULD NOT ENGAGE PROPERLY. ADJUSTED AND LUBED IAW MM, OPS CHECK NORMAL PER 52-11-04-822-056. (M) 2L72 4F RTA2NM 20040802001862004080200186NM 2004 8 2 AMTA200400711 120040610A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT EXPOSED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11527AT 30886 FOUND AFT RED EMERGENCY FLOOR LIGHT HAS WIRES STICKING OUT AND DOESN'T LIGHT UP. SECURED AS REQUIRED, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040802001872004080200187EA 2004 8 2 ASOA04428 120040614A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11909EV 7658 FLT 4486 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001882004080200188NM 2004 8 2 USAA04337 120040622A5330 SKIN BOEING737 737301 1384611NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 FOUND PROBLEM WITH PREVIOUS REPAIR AT BS 470, STRINGER 8L TO 9L. REPAIRED PER SRM 53-00-01 FIGURE 201. (M) 2L72 4F RTA16WE 20040802001912004080200191EU 2004 8 2 SIMA200416205 120040529A53117252814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21384AE 340B384 ABI - DURING AN MBV INSPECTION, THE BOTTOM FRAME UPPER FLANGE AT STATION 258, 17 INCHES FROM OUTBOARD HAS SINGLE ISOLATED CORROSION PIT. REMOVED CORROSION BY DRILLING A .215 DIAMETER HOLE. WET INSTALLED A NAS1241AD6 RIVET CUT TO LENGTH. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007185 PARA 2 DATED MAY 28, 2004. (M) 2L72 4T RTA52EU 20040802001922004080200192EU 2004 8 2 ASOA04427 120040613A3230C24295350 SOLENOID VALVE AEROSPATR72 ATR72212 8680945EU FUSELAGE LEAKING A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11632AS 338 FLT 4133 - DURING FINAL APPROACH INTO VPS FROM ATL, THE CREW RECEIVED A FLAPS UNLOCK ALERT AT APPROXIMATELY 900 FT WITH AN APPROXIMATE AIRSPEED OF 130 KNOTS. THE QRH WAS COMPLIED WITH AND AN EMEGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN VPS. MAINTENANCE REMOVED AND REPLCED THE NOSE WHEEL STEERING SOLENOID VALVE. OPS AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040802001932004080200193NM 2004 8 2 AMTA200400740 120040614A2610285N0028136 LOGIC CARD BOEING757 75733N 1384931NM LT ENGINE MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 EICAS STATUS MSG L ENG OH LP2 DISPLAYED. TROUBLESHOT DISC PER FIM 26-11-11. REMOVED AND REPLACED AFOLTS CARD. SYSTEM OP NORMAL. NO OTHER DISC FOUND. (M) 2L72 4F RTA2NM 20040802001982004080200198EA 2004 8 2 ASOA04422 120040610A3350467190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11843AS 7310 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR LIGHTING AT ROW 7-C/D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTOR ON THE EMERGENCY FLOOR LIGHT TRACK AT ROW 7-C/D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802002002004080200200EU 2004 8 2 USAAEM04010 120040625A3200 PIN EMB ERJ170ERJ170100 EU MLG INSTALLED A USAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 EA19803MD 17000015 AFTER TAKEOFF, THE RIGHT MAIN GEAR DID NOT RETRACT. THE CAPTAIN RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED, CLEANED AND REINSTALLED LOCK STAY PIN. (M) 2L74 4F RTA56NM 20040802002012004080200201EU 2004 8 2 SIMA200416204 120040529A53117252813117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21384AE 340B384 ABI - DURING AN MBV INSPECTOIN, CARGO FRAME AT STATION 677 WAS FOUND DENTED 5.5 INCH ABOVE FLOOR. PERFORMED A CUTOUT OF FRAME 677 FLANGE WITH A MIN RADIUS OF .040 INCH AND RECONTOURED THE WEB. PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE FOR REPAIR. WORK DONE IAW SAAB REPAIR STATEMENT 340SDS007185 PARA 3 DATED MAY 28, 2004. (M) 2L72 4T RTA52EU 20040802002022004080200202EA 2004 8 2 ASOA04413 120040607A5210600314457 HINGE PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11920EV 7819 FLT 4730 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT CLOSE FROM THE INSIDE. MAINTENANCE LUBRICATED THE HINGE ROD ENDS ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802002032004080200203NM 2004 8 2 USAA04335 120040422A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19427US41294 24549 PIT - FOUND .036 INCH DEEP BY .75 INCH LONG BY .5 INCH WIDE DENT. INSTALLED DOUBLERS PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040803000022004080300002NM 2004 8 3 RJEF598HAA 120040715A5270 WARNING LIGHT AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE E/E BAY DOOR ILLUMINATED A RJEFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW99477TA 1952 V1157172 DURING CRUISE, PILOT REPORTED INDICATION OF AFT AVIONICS DOOR. THE AC WAS DIVERTED. AFTER LANDING, INSPECTION OF THE DOOR WAS PERFORMED AND FOUND IT PROPERLY CLOSED AND INDICATIONS WERE NORMAL. ALSO PERFORMED PROXIMITY SENSORS CLEANING AND INSTALLATION OF THE TARGET AT CONTROL LEVER IAW MM 52-35-13; OPERATIONALLY TESTED SEVERAL TIMES, NORMAL IAW MM. ADDITIONALLY, THE DOOR HAS BEEN CONFIRMED CLOSED AND LOCKED. THE AIRCRAFT RETURNED TO NORMAL OPERATIONS. 2L72 4F4 FRTA28NM E40NE 20040818001492004081800149SW 2004 8 18 KBM2004F00135 120040608A2121 MOTOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL A/C BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV10770 2704 REMOVED BLOWER MOTOR, AIR CONDITIONER BLOWS WARM, FOUND FAN AND BEARINGS DEFECTIVE. INSTALLED SERVICEABLE MOTOR ASSY. OPS CHECKED GOOD. 1G71 3U3 U H2SW E4CE 20040803000042004080300004NM 2004 8 3 151AW0019A 120040702A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE SKIN CRACKING AT SEVERAL LOCATIONS UNDER EXISTING REPAIR INSTALLED WITH BLIND FASTENERS FROM BS727E TO BS767 STR18 RT TO STR20 RT. REPAIRED PER EA 53-147. 2L72 4F RTA16WE 20040803000072004080300007NM 2004 8 3 SWAA042167 120040729A57146545329 FITTING BOEING737 7373H4 1384600NM RT & LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND LT AND RT CENTER SECTION FITTINGS ABOVE CENTER TANK RT AND LT BS 616, CRACKED. REPAIRED FITTINGS PER T1-153-018. 2L72 4F RTA16WE 20040803000092004080300009NM 2004 8 3 SWAA042170 120040729A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040803000142004080300014 2004 8 3 SWAA042165 420040729A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 R1 DOOR EVAC SLIDE FELL OUT. REINSTALLED AND SECURED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040803000172004080300017EU 2004 8 3 MALA040496 120040712A3350501122804 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL15421XJ 340B421 AFTER START UP NOTICED EMERGENCY POWER LIGHT ILLUMINATED. VOLTAGED 28 VOLTS BUT LIGHT REMAINED ON. RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY 24-35-10-ND RELAY AT 9PD (P/N M83536-2) IAW AMM 24-35-00. EPS S/N ON OFF 502142, P/N 501-1228-04. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040803000182004080300018 2004 8 3 MALA040498 420040715A2565D31050105 SLIDE BAC 146 AVRO146RJ85A1500097EU L1 DOOR DISLODGED A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15502XJ E2307 LEFT DOOR 1L SLIDE WAS ON FLOOR AFTER PUSHBACK. MAINTENANCE REPLACED PAX DOOR 1L ESCAPE SLIDE REF MAL TASK 2560-501-14-00. ESCAPE SLIDE DEPLOYED. A/C OKAY FOR SERVICE P/N D31050-105, S/N OFF 1708, S/N ON 1422. 2H74 4F RTA49EU 20040803000192004080300019EU 2004 8 3 MALA040500 120040723A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 LEFT SEAT TRACK HAS SMALL SPOTS OF CORROSION AT STA 305 & 310. NEW SEAT TRACK SECTION WAS FABRICATED AND INSTALLED IAW MESABA EO 53060. 2L72 4T RTA52EU 20040803000212004080300021 2004 8 3 MALA040502 420040726A2565 CLIP BAC 146 AVRO146RJ85A1500097EU GIRT BAR BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15519XJ E2344 AFT LEFT DOOR 2L GIRT BAR SPRING CLIP IS BROKEN OFF AND MISSING. MAINTENANCE REPLACED DOOR 2L GIRT BAR FWD END PN ON/OFF HC521H0242-208 EMERGENCY SLIDE GIRT BAR CHECK GOOD. A/C GOOD FOR CONTINUED SERVICE. 2H74 4F RTA49EU 20040803000222004080300022EU 2004 8 3 MALA040497 120040718A3350M835362024M RELAY SAAB SF340 340B 7860101EU EMERGENCY LIGHTSFAILED A MALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15421XJ 340B421 AFTER START, EMERGENCY POWER LIGHT AND POWER REMAINED ON. MAINTENANCE REPLACED RELAY AT 9PD P/N M83536-2-024M. ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20040803000232004080300023WP 2004 8 3 AALA20040728 120040715A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217538A 49992 EMERGENCY LIGHTS AT FIRST EMERGENCY EXIT ROW LT AND RT INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT FIRST EMERGENCY EXIT ROW LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000262004080300026WP 2004 8 3 AALA20040726 120040714A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219622A 53593 EMERGENCY LIGHT ABOVE CAT WALK IN TAIL COMPARTMENT INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ABOVE CAT WALK IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040803000292004080300029NM 2004 8 3 04FDEA02267 120040728A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79820, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000302004080300030NM 2004 8 3 04FDEA02268 120040728A1430 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 29 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79809, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000312004080300031NM 2004 8 3 04FDEA02269 120040728A1430 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 27 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79810, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000322004080300032NM 2004 8 3 04FDEA02270 120040728A5730 SKIN PANEL DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND WING UPPER SURFACE TRAILING EDGE PANEL FORWARD EDGE FOUND BULGING AT OUTBOARD OF NR 5 SPOILER XORS 827. REMOVED AS PER SRM 51-21-01, VOLUME II, MATERIAL THICKNESS=0.270, MATERIAL REMAINED=0.231, MATERIAL REMOVED=0.039 FOUND WITHIN LIMIT (0.054) AS PER SRM 57-20-00, FIGURE 16, VOLUME I, AREA REPROTECTED AS PER SRM 51-21-01, VOLUME II. ALSO FOUND WITHIN LIMIT AS PER FEDEX EA NR 1-5710-79802, LT REAR SPAR UPPER TEE CHORD AT XORS 795 - AFT FLANGE CORROSION REPAIR. 2L73 4F RTA22WE 20040803000332004080300033NM 2004 8 3 04FDEA02271 120040728A1430 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 10 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79818, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING S/B MD-11, 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000372004080300037EU 2004 8 3 MALA040495 120040711A3610 PIPE BAC 146 AVRO146RJ85A1500097EU NR 4 ENGINE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15501XJ E2208 NR 4 ENG AIR BLEED SYSTEM, CLIMBING OUT OF MEM AROUND 14,000 FT, THE NR 4 PYLON OVERHEAT LIGHT ILLUMINATED. TURNED NR 4 BLEED AIR OFF AS PER QRH & THE LIGHT WENT OUT. RETURNED TO MEM LANDING WT 79,000 LBS. MAINTENANCE REPLACED PIPE, TEMP SENSOR AND GASKET. 2H74 4F RTA49EU 20040803000382004080300038EU 2004 8 3 MALA040493 120040710A3240 BRAKE ASSY BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAO OTHER O OTHER LDLANDING 1 GL15501XJ E2208 DURING LANDING ROLLOUT, PILOT REPORTED THAT IT TOOK MORE BRAKING PRESSURE THAN NORMAL TO GET RESPONSE. BRAKES FELT STIFF. MAINTENANCE FOUND EXCESSIVE AIR IN YELLOW BRAKE SYS. BLED YELLOW BRAKE SYS IAW AMM CH 12, ALL CHECKS GOOD AT THIS TIME, OKAY FOR SERVICE. 2H74 4F RTA49EU 20040803000442004080300044WP 2004 8 3 AALA20040769 120040722A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21475AA 49650 LAX - ALL FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5100 FOR ALL FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000452004080300045NM 2004 8 3 AALA20040761 120040724A3350 LIGHT BOEING757 757223 1384957NM ROW 16 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21691AA 25697 DFW - AFT EMERGENCY PATH LIGHT AT ROW 16 INOPERATIVE. REPLACED AFT EMERGENCY PATH LIGHT ASSEMBLY AT SEAT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040803000462004080300046WP 2004 8 3 AALA20040766 120040722A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21279AA 49295 OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000472004080300047WP 2004 8 3 AALA20040784 120040728A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21287AA 49299 EWR - EMERGENCY SEAT LIGHTS INOPERATIVE. REPLACED TWO EACH POWER MODULES FOR EMERGENCY SEAT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000502004080300050WP 2004 8 3 AALA20040771 120040723A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21292AA 49304 BDL - COCKPIT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 211 FOR COCKPIT CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000512004080300051WP 2004 8 3 AALA20040780 120040727A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217544A 53026 SAT - EMERGENCY CEILING LIGHTS AT ROWS 19, 20 AND 22 INOPERATIVE. REPLACED BATTERY PACK ON OVERHEAD BIN ON SEAT ROW 20 FOR EMERGENCY CEILING LIGHTS AT ROWS 19, 20, AND 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000522004080300052WP 2004 8 3 AALA20040774 120040726A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219681B 53631 DFW - EMERGENCY ESCAPE PATH LIGHTING AT FORWARD GALLEY FLOOR INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY CONNECTOR FOR AT FORWARD GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040804000052004080400005NM 2004 8 4 04FDEA02181 120040726A5315 FLOORBEAM BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION FLOORBEAM BS 344, BS LBL 60 - RBL 12, WL 208. *S/D* REMOVED AND REPLACED FLOORBEAM SECTION AT BS 344 LBL 7 TO LBL 65 WL 208 PER SRM 53-10-8. 2L73 4F RTA3WE 20040804000072004080400007NM 2004 8 4 04FDEA02183 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 LBL 25 WL 205. *S/D* REMOVED AND REPLACED SEAT TRACK LINK BS 740 TO BS 760, LBL 25, IWL 205 IAW SRM 51-30-2. 2L73 4F RTA3WE 20040804000082004080400008NM 2004 8 4 04FDEA02184 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION AROUND SEAT TRACK LINK FWD ATTACH BOLT BS 742 RBL 48 WL 205. *S/D* CORROSION ON LINK AT BS 742 WAS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK LINK AND FWD ATTACH BOLT AT BS 742 RBL 48 WL 205 PER SRM 51-30-2, 53-10-1 & 53-10-5 & AT BS 740-760 RBL 45 WL 208. 2L73 4F RTA3WE 20040804000092004080400009NM 2004 8 4 04FDEA02185 120040726A5320 ANGLE BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 FWD CARGO COMPARTMENT J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. *S/D* FOUND J-ANGLE DENTED OUT OF LIMITS AT BS 500 LBL 28 WL 155. REMOVED, FABRICATED AND INSTALLED NEW J-ANGLE IAW SRM 53-10-1 PG 2 FIG 1 SHEET 2, SRM 51-30-2. 2L73 4F RTA3WE 20040804000172004080400017NM 2004 8 4 04FDEA02278 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 20R BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED MD11 S/B LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79822, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 20R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000192004080400019NM 2004 8 4 AALA20040747 120040717A2420 BEARING BOEING767 767323 1385205NM GE CF6 CF680C2B6 30025NE ALTERNATOR FAILED A AALAA UNSCHED LANDING YHJENGINE STOPPAGE ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW21347AN 33086 690402 SJC - INFLIGHT T0073/17 LEFT ENGINE N2 ALTERNATOR DRIVE BEARINGS FAILED ON CLIMBOUT. REPLACED NUMBER 1 ENGINE PER SPECIAL ITEM CARDS 71-93-01 AND 71-95-22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20040804000212004080400021WP 2004 8 4 AALA20040749 120040720A56205951584501 WINDOW DOUG DC9 DC982 3022082WP PAX CABIN DEBONDED A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW217517A 49894 PHX - INFLIGHT T517/20 DFW TO LAX PASSENGER WINGOW AT SEAT 19A OUTER PANE DISBONDED. LANDED PHX WITHOUT INCIDENT. EVALUATION IN PROGRESS. 2L72 4F A6WE 20040804000322004080400032NM 2004 8 4 04FDEA02279 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 7L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79815, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 7L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000332004080400033NM 2004 8 4 04FDEA02280 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 11L BARREL NUT BORE FOUND WITH CORROSION. REPAIRED AS PER FEDEX EA NR 1-5510-79804, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 11L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000352004080400035NM 2004 8 4 04FDEA02282 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 28R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79814, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 28R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000392004080400039NM 2004 8 4 AALA20040755 120040701A2932705073 VALVE BOEING757 757223 1384957NM HYD SYSTEM INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21634AA 24592 SJU - INFLIGHT T790/01 TWO MINUTES AFTER TAKEOFF LOST LEFT HYDRAULIC SYSTEM QUANTITY. MANUALLY EXTENDED GEAR AND FLAPS AND TURNED LEFT HYDRAULIC PUMPS OFF WHEN PRESSURE LIGHT ILLUMINATED. LANDED SJU WITHOUT INCIDENT. FOUND BRAKE METERING VALVE DAMPED. REPLACED RIGHT BRAKE METERING VALVE ASSEMBLY AND CHECKED LEFT SYSTEM HYDRAULIC FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804000462004080400046NM 2004 8 4 04FDEA02284 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 22 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79811, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000472004080400047NM 2004 8 4 AALA20040786 120040729A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21960AN 29542 TUL - BATTERY PACK AT STATION 727 LEFT FAILED 15 MINUTE TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT STATION 727 LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040804000482004080400048NM 2004 8 4 AALA20040785 120040728A5315 FLOORBEAM BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21603AA 27054 TUL - CORROSION ON TOP OF FLOORBEAM AT STATION 1640 LEFT BUTTLINE 15 TO LEFT BUTTLINE 53. CORRODED AREA IS 2 INCHES BY 40 INCHES. REPAIRED CORROSION ON TOP OF FLOORBEAM AT STATION 1640 LET BUTTLINE 15 TO LEFT BUTTLINE 53 IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 53 00 51. 2L72 4F RTA2NM 20040804000492004080400049NM 2004 8 4 AALA20040787 120040729A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM FUSELAGE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21960AN 29542 TUL - BATTERY PACK FOR EMERGENCY LIGHTS AT STATION 565 RIGHT AND LEFT FAILED 15 MINUTE TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT STATION 565 RIGHT AND LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040804000572004080400057NM 2004 8 4 04FDEA02292 120040729A2730 SKIN DOUG MD11 MD11 3023602NM ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND ELEVATOR LOWER SURFACE AT STA XE 356 TO XE 370 FOUND WITH DELAMINATION APPROXIMATELY 14 INCHES IN DIAMETER. REMOVED AND REPLACED AS PER MM 27-30-30. ELEVATOR OPERATIONAL CHECK CARRIED OUT AS PER MM 27-30-00, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040804000582004080400058EU 2004 8 4 MALA040482 120040709A3510 BOTTLE SAAB SF340 SF340A 7850100EU OXYGEN SYSTEM LEAKING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL1599XJ 340A099 CREW O2 LEAKED DOWN INFLIGHT. MAINTENANCE TIGHTENED NUT ON BOTTLE. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040804000602004080400060EU 2004 8 4 MALA040483 120040709A79301125997 TRANSDUCER BAC 146 AVRO146RJ85A1500097EU NR 2 ENG OIL MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15512XJ E2326 NR 2 OIL LOW PRESSURE LIGHT ILLUMINATED SEVERAL TIMES ON CLIMBOUT. OIL QUANTITY 3/4 OIL TEMPS AROUND 110 DEG AND OIL PSI BETWEEN 80-100 PSI LIGHT WAS OUT FOR LAST 10-15 MINUTES OF FLIGHT. AIR RETURN TO MSP. MAINTENANCE CND, FOR PRECAUTIONARY PURPOSES REPLACED NR 2 TRANSDUCER P/N 2-303-869-01, S/N OFF 1125997, S/N ON 888486. SWAPPED PCB 2QL1 AND 3QL1, RAN AC AT TAKEOFF POWER, OP CHECK GOOD. 2H74 4F RTA49EU 20040804000612004080400061EU 2004 8 4 MALA040481 120040705A261353183111 DETECTOR BAC 146 AVRO146RJ85A1500097EU OVERHEAT SYS MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15501XJ E2208 EN ROUTE NR 4 ENGINE PYLON OVERHEAT CAPTION ILLUMINATED. PERFORMED QRH, LIGHT WENT OUT ALMOST IMMEDIATELY. LIGHT REMAINED OUT FOR DURATION OF FLT. MAINTENANCE REMOVED AND REPLACED NR 4 PYLON OVERHEAT DECK P/N 53183-111 IAW 26-14-17, OPS CHECKS GOOD. 2H74 4F RTA49EU 20040804000622004080400062EU 2004 8 4 MALA040484 120040714A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, CORROSION FOUND ON LT CARGO BAY SEAT TRACKS FROM FS 621-686. NEW SEAT TRACK SECTION INSTALLED IAW MESABA AIR EO S53063. A/C RELEASE DATE 7/15/04. 2L72 4T RTA52EU 20040804000632004080400063EU 2004 8 4 MALA040487 120040714A5315 FLOORBEAM SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, CORROSION ON STA 225 FLOORBOARD ANGLE. REMOVED CORROSION WITH 100 PERCENT MAT LOSS. FABRICATED ANGLE DOUBLER FROM 2024T3.040 TREATED, PRIMED AND INSTALLED IAW EO S53108. A/C RELEASE DATE 7/15/04. 2L72 4T RTA52EU 20040730000022004073000002 2004 7 30 SWAA042133 420040727A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040730000032004073000003NM 2004 7 30 SWAA042134 120040727A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT FLOOR PATH PHOTOLUMINESCENT STRIPS AT ROW 9 DEF TO ROW 11 DEF, CRACKED. REMOVED & REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20040730000132004073000013NM 2004 7 30 04FDEA02229 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RIGHT HAND WING INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8794. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80311, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000202004073000020NM 2004 7 30 04FDEA02236 120040728A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - INBOARD FLAP - FLAP VANE OUTBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8794. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA 1-5750-80310, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE - OUTBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040730000272004073000027NM 2004 7 30 04FDEA02168 120040726A5310 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD TAIL CONE RIGHT HAND DOOR CUTOUT JAMB CRACKED. FORWARD TAILCONE RIGHT HAND DOOR CUT OUT CRACKED FRAMES AND DOUBLER REMOVED AS PER SRM 51-31-01 VOL II, AND NEW FRAMES AND DOUBLER INSTALLED AS PER SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040730000282004073000028NM 2004 7 30 04FDEA02241 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.510, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.505 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000312004073000031NM 2004 7 30 04FDEA02244 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAPSIDE) ACTUATOR HOLE NR 1 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.220 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000432004073000043NM 2004 7 30 04FDEA02254 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.074 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000642004073000064NM 2004 7 30 SWAA042113 120040725A27826954550 ROD END BOEING737 7372H4 138448CNM LT WING SLAT OUT OF ADJUST A SWAAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW29082SW 22731 DURING TAKEOFF UNTIL APPROX 10 TO 15 SECONDS AFTER GEAR RETRACTION ABNORMAL RIGHT ROLLING TENDENCY, REQUIRING APPROX 30 DEGREES YOKE DEFLECTION. DURING FLAP EXTENSION ON GROUND TOOK SEVERAL CYCLES OF FLAPS TO EXTINGUISH, SLAT NR 3 AND 4 AMBER LIGHTS ON OVERHEAD PANEL, AMBER LIGHT ON FWD PANEL. ADJUSTED NR 3 L/E SLAT ACTUATOR ROD END PER MM. 2L72 4F A16WE 20040730000662004073000066NM 2004 7 30 SWAA042115 120040725A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FRAME CHORDS AT RT AND LT BS 188, CRACKED. REPAIRED FRAME CHORDS PER SRM. 2L72 4F RTA16WE 20040802000032004080200003EA 2004 8 2 A6WA200440037 120040328A2100 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA A/C PACKS FALSE ACTIVATIONA A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31418AW 7618 AFTER TAKEOFF CAS MESSAGE 'LT PACK HI PRESS' MESSAGE. OVERHEAD PANEL INDICATION 'LT PACK FAIL'. SYNOPTIC PAGE INDICATED NEITHER PACK OPERATING. LANDED AT 50,600 LBS - VI 0 LIGHT BRAKING. HOTTEST TEMP 2, SPEED 135 KNOTS. INSPECTED AND OPERATED BOTH AC PACKS IAW AMM 21-51-00. BOTH PACKS OPERATE NORMALLY. NO FAULTS NOTED. OVERWEIGHT LANDING INSPECTION NOT REQUIRED PER AMM 5-51-01. (M) 2L72 4F RTA21EA 20040802000102004080200010EA 2004 8 2 ASOA04062 120040124A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A HANGAR INSPECTION IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802000182004080200018EA 2004 8 2 ASOA04063 120040124A3350100865 PSU CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11845AS 7324 DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802000242004080200024NM 2004 8 2 ASAA0410270 120040521A5315BAC1503100246 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR. (M) 2L72 4F A16WE 20040802000292004080200029 2004 8 2 GTIA040580 420040620A2565 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR DISLODGED A GTIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23822NK 49392 FLT 223 - ORD - ON TAXI OUT, FOUND L1 SLIDE PACK FELL OUT OF COVER. REINSTALLED SLIDE PACK ADJUSTED LOWER LATCH AND CLIP MECH. (M) 2L72 4F RT 20040802000352004080200035WP 2004 8 2 GTIA040605 120040615A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 1309-1338 RUSTED INSERTS. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040802000372004080200037WP 2004 8 2 GTIA040612 120040607A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOND LEFT INBOARD SEAT TRACKS STATION 200-798 GOUGED AND CORRODED. MATERIAL OUT OF LIMITS STATION 200-270. REMOVED SEAT TRACK. FABRICATED RIGHT INBOARD SEAT TRACK. LOCATED AND DRILLED SEAT TRACK AND SPLICE. INSTALLED SEAT TRACK. INSTALLED SPLICE. (M) 2L72 4F RTA6WE 20040802000482004080200048WP 2004 8 2 GTIA040618 120040612A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND FORWARD EMERGENCY LIGHT ASSEMBLY ON FORWARD DROP CEILING PANEL BROKEN. REMOVED LIGHT ASSEMBLY. INSTALLED NEW LIGHT ASSEMBLY. (M) 2L72 4F RTA6WE 20040802000652004080200065NM 2004 8 2 USAA040294 120040607A575465C26603101 SKIN BOEING737 737401 1384701NM LT NR 3 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 FOUND SKIN TO CORE DELAMINATION 1.5 SQUARE INCH AREA, LT WING NR 3 SLAT INBOARD END TRAILING EDGE CORNER. INSTALLED NEW CORE MATERIAL, TOP REPAIR DOUBLER, SEALED EDGE AND TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040802001092004080200109 2004 8 2 2004F00214 420040106A2200101351198125 CONTROL CABLE STBROSSD3 SD330 8100602EU POWER LEVER FROZEN A DATAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL13390GA SH3077 ON DESCENT INTO IKK, THE POWER LEVER STUCK, FROZE. THE CREW COULD NOT UN-STICK, THEREFORE HAD TO CONDUCT A PRECAUTIONARY ENGIEN SHUTDOWN PRIOR TO LANDING. THE LANDIG WAS UNEVENTFUL AND THE FLIGHT TERMINATED UNTIL REPAIRS COULD BE MADE. A MECHANIC WAS SENT TO IKK. THE LEFT TELEFLEX POWER CABLE WAS REMOVED, CLEANED, REGREASED, AND REINSTALLED IAW THE SHORTS SD3-30 MM. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A41EU 20040802001112004080200111CE 2004 8 2 2004F00226 120040115A5542114630000121 SKIN BEECH 1900 1900C 1154161CE RUDDER TE CRACKED A FFSAK NONE O OTHER ININSP/MAINT 1 AL01575X UC149 DURING A SCHEDULED INSPECTION, A CRAC WAS DISCOVERD IN THE RUDDER SKIN. THE CRACK LOCATION WAS ABOUT 4 INCHES DOWN FROM THE TOP OF THE RUDDER. THE CRACK SPLIT THE TRAILING EDGE FOR ABOUT 1.5 INCHES THEN CRACKED TO OPPOSITE SIDES OF THE RUDDER FROM EITHER END FOR A TOTAL CRACK LENGTH OF ABOUT 3.5 INCHES. (M) 2L72 4T RTA24CE 20040802001292004080200129EA 2004 8 2 ASOA04402 120040602A2560268 BATTERY CNDAIRCL600 CL6002C10 1390015EA MEGAPHONE INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11723EV 10132 FLT 4696 - DURING A GROUND INSPECTION IN DFW, THE REAR PORTABLE MEGAPHONE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE REAR PORTABLE MEGAPHONE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001312004080200131 2004 8 2 GTIA040571 420040615A2565 COVER DOUG DC9 DC982 3022082WP R1 DOOR SLIDE DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 ACY - R1 SLIDE PACK COVER FELL OFF. REPOSITIONED AND RESECURED R1 SLIDE PACK COVER. (M) 2L72 4F A6WE 20040802001322004080200132NM 2004 8 2 BJNA040101 120040107A33506013211 BATTERY PACK BOEING737 737282 13844ATNM RT OVERWING WILL NOT TEST A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 RIGHT OVERWING EXTERNAL EMERGENCY EXIT LIGHTS WILL NOT TEST. REPLACED BATTERY PACK PER AMM 33-51-31. (M) 2L72 4F RTA16WE 20040802001332004080200133 2004 8 2 GTIA040572 420040617A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DISCHARGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 LGA - FOUND SLIDE FROM R1 HAS LOW PRESSURE. REMOVED AND REPLACED R1 SLIDE. (M) 2L72 4F A6WE 20040802001382004080200138EA 2004 8 2 ASOA04396 120040601A52104442440105 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 FLT 4442 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001402004080200140EA 2004 8 2 A6WA200440011 120040124A29152590 RELIEF VALVE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM INOPERATIVE A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31428AW2840 7695 NOSE GEAR DISAGREE INFLIGHT AFTER TAKEOFF, COMPLIED WITH QRH. HYDRAULIC 3 HIGH TEMP ON GROUND. COMPLIED WITH QRH. REMOVED AND REPLACED PRESSURE MANIFOLD RELIEF VALVE PER AMM 29-12-07. LEAK CHECK GOOD. PERFORMED MULTIPLE GEAR SWINGS IAW 32-30-00. REMOVED AND REPLACED 3B PUMP IAW AMM 29-12-03. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040802001622004080200162NM 2004 8 2 UIEA200400002 120040109A2120 ODOR BOEING747 747243B 1384830NM COCKPIT DETECTED A UIEAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 EA15518MC 23476 AFTER LANDING, STRONG FUEL ODOR IN THE COCKPIT, BALLAST FUEL 5000 AND TWO PACKS RUNNING. PERFORMED THOROUGH VISUAL CHECK OF AIR CONDITIONING BAY AND WING BODY FAIRING AREA PER MM 28-11-00. NO FUEL LEAKS NOTED. RAN PACK, NO FUEL ODOR NOTED. (M) 2L74 4F A20WE 20040802001812004080200181EA 2004 8 2 ASOA04416 120040609A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7500 DURING A C-CHECK IN MCN, THE RIGHT OUTBOARD AND LEFT INBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT OUTBOARD AND LEFT INBOARD CLIPS AT FS 280. (M) 2L72 4F RTA21EA 20040802001842004080200184EA 2004 8 2 ASOA04420 120040610A3350 POWER SUPPLY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11706EV 10054 FLT 4712 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY LIGHTS IN THE 'ON' POSITION AND CHARGED THE EMERGENCY BATTERY IN THE POWER SUPPLY UNITS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001942004080200194EA 2004 8 2 ASOA04419 120040609A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS IN THE AFT EQUIPMENT BAY AT FS 625 BELOW THE ENGINE SUPPORT BEAM WERE OFUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS IN THE AFT EQUIPMENT BAY AT FS 625 BELOW THE ENGINE SUPPORT BEAM. (M) 2L72 4F RTA21EA 20040802001962004080200196NM 2004 8 2 USAA04340 120040620A5534 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US 23991 FOUND .25 INCH BY .25 INCH CORROSION ON THE FORWARD TEE FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. REMOVED CORROSION AND INSTALLED NEW BUSHINGS PER EA 78608. (M) 2L72 4F RTA16WE 20040802001992004080200199SO 2004 8 2 SIMA200417203 120040619A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21646AE 145213 CLT - FLT 3807 - CREW REPORTED TWO OVERHEAD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY UNIT P/N 110049, AND BATTERY IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040803000062004080300006NM 2004 8 3 SWAA042166 120040729A335090083 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED A2 CHECK, FOUND FWD & AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2L72 4F A16WE 20040803000112004080300011NM 2004 8 3 SWAA042172 120040729A57546573714 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND RT WING NR 6 L/E SLAT SKIN, CRACKED. REPAIRED NR 6 L/E SLAT SKIN PER SRM. 2L72 4F RTA16WE 20040803000202004080300020EU 2004 8 3 MALA040501 120040723A7997230391903 WIRE HARNESS BAC 146 AVRO146RJ85A1500097EU ENGINE OIL IND DAMAGED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15517XJ E2335 NR 2 OIL LOW PRESSURE BLINKING EVERY FEW SECONDS. ILLUMINATION OCCURRED JUST AFTER TAKEOFF AND CONTINUED ALL THE WAY TO THE GATE. AIR RETURN TO MSP. MAINTENANCE REPLACED PRESS WARNING PROCESSOR, NO FIX. REINSTALLED ORIG. REPLACED OIL PRESS X-DUCER, OPS CHECK NO GOOD. LEAK GOOD. P/N ON 2-303-869-01. S/N ON 892321, OFF/02153380021. PIGGY BACKED HARNESS P/N 2-303-919-03 ON TO NR 2 ENGINE. OPS CHECK GOOD. INITIATED PLANNING WATCH ITEM TO PERMANENTLY INSTALL HARNESS AT NEXT ENGINE REMOVAL. 2H74 4F RTA49EU 20040803000242004080300024NM 2004 8 3 AALA20040730 120040716A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21929AN 30078 EMERGENCY LIGHTS ABOVE SEATS 8A AND 7D ON OVERHEAD BIN INOPERATIVE. REPLACED BATTERY PACK M01676 FOR EMERGENCY LIGHTS ABOVE SEATS 8A AND 7D ON OVERHEAD BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040803000282004080300028EU 2004 8 3 AALA20040727 120040715A3350321441 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2141063 506 JFK - EMERGENCY LIGHT AT RT NR 2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040803000412004080300041 2004 8 3 SWAA042175 420040729A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED SLIDE PER MM. 2L72 4F RTA16WE 20040803000432004080300043WP 2004 8 3 AALA20040765 120040722A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969TW 53619 DFW - EMERGENCY CEILING LIGHT AT ROW 28 AND AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHT AT ROW 28 AND AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040803000532004080300053WP 2004 8 3 AALA20040775 120040725A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2177421 49333 DFW - TAIL COMPARTMENT WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL WALKWAY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000542004080300054WP 2004 8 3 AALA20040744 120040714A3230 CABLE DOUG DC9 DC982 3022082WP MLG BROKEN A AALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW21498AA 49736 TUL - INFLIGHT T1215/14 COULD NOT RETRACT MAIN LANDING GEARS AFTER TAKEOFF. AIRCRAFT RETURNED TO TUL GATE. FOUND BROKEN ANTI RETRACTION CABLE SEGMENT 118A. INSTALLED AND ADJUSTED A SERVICEABLE CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000022004080400002WP 2004 8 4 AALA20040741 120040719A3350P4010051111 CONTROL PANEL DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217508 49802 TPA - EMERGENCY LIGHT AT AFT LEFT HAND EXIT INOPERATIVE. REPLACED AISLE PATH LIGHT CONTROL FOR EMERGENCY LIGHT AT AFT LEFT HAND EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000062004080400006NM 2004 8 4 04FDEA02182 120040726A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION WHILE WORKING CARD N00233 FOUND CORROSION ON STRINGER 26 LEFT LBL 20 BS 1135. CORROSION ON STA 26 LEFT BS 1135 WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED STR 26 LEFT BS 1120-1140 AND INSTALLED NEW STRINGER & REPAIR SPLICE PER SRM 53-10-3. 2L73 4F RTA3WE 20040804000112004080400011NM 2004 8 4 04FDEA02188 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION SEAT TRACK BS 760-840 RBL 22 WL 208. REMOVED AND REPLACED LONGITUDAL BEAM STA 760-848 RBL 22, WL 208 IAW SRM 51-30-02, 51-30-5. 2L73 4F RTA3WE 20040804000122004080400012NM 2004 8 4 04FDEA02189 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION SEAT TRACK BS 870-950, RBL 45, WL 208. CORROSION ON SEAT TRACK AT BS 870-950 RBL 45 WL 208 WAS FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED SEAT TRACK PER SRM 53-10-5. 2L73 4F RTA3WE 20040804000262004080400026WP 2004 8 4 AALA20040773 120040723A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21553AA 53083 DFW - EMERGENCY CEILING LIGHTS AT SERVICE DOOR AND STATIONS 1100 THROUGH 1200 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190R FOR EMERGENCY CEILING LIGHTS AT SERVICE DOOR AND STATIONS 1100 THROUGH 1200. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000442004080400044WP 2004 8 4 AALA20040782 120040727A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21471AA 49601 DEN - EXTERIOR EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK B549 FOR EXTERIOR EMERGENCY EXIT SIGN LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000452004080400045NM 2004 8 4 04FDEA02283 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 30 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79808, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 30R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000522004080400052NM 2004 8 4 04FDEA02287 120040729A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING INBOARD FLAP FLAP VANE NR 1 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLES DIAMETER FORWARD=0.688, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80305, TITLE: WINGS - TRAILING EDGE FLAPS - LT INBOARD FLAP VANE, NR 3 VANE TO TRACK SUPPORT ASSEMBLY CORRODED. 2L73 4F RTA22WE 20040804000532004080400053NM 2004 8 4 04FDEA02288 120040729A5753 VANE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING INBOARD FLAP FLAP VANE NR 3 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLES DIAMETER FORWARD=0.688, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80306, TITLE: WINGS - TE FLAPS - LT INBOARD FLAP VANE, NR 3 VANE TO TRACK SUPPORT ASSEMBLY CORRODED. 2L73 4F RTA22WE 20040804000642004080400064EU 2004 8 4 MALA040485 120040714A5321 FLOOR PANEL SAAB SF340 340B 7860101EU FUSLEAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, FLOOR WEB CORRODED AT STA 225 BELOW COCKPIT DOOR. ACCOMPLISHED WEB REPAIR IAW MESABA EO S53236. A/C RELEASE DATE 7/15/04. 2L72 4T RTA52EU 20040804000652004080400065EU 2004 8 4 MALA040486 120040714A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, LEFT I/B SEAT TRACK HAS CORROSION AT STA 294. NEW SEAT TRACK SECTION WAS INSTALLED IAW MESABA EO S53060. A/C RELEASE DATE 7/15/04. 2L72 4T RTA52EU 20040804000682004080400068NM 2004 8 4 SWAA042117 120040726A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 923, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040804000692004080400069NM 2004 8 4 SWAA042118 120040726A3350101114 LENS BOEING737 7373Q8 1384670NM EMERGENCY EXIT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 CENTER AISLE OVERWING EMERGENCY EXIT LIGHT MISSING 2 EACH LENSES. INSTALLED 2 EACH LIGHT LENSES PER MM. 2L72 4F RTA16WE 20040804000702004080400070NM 2004 8 4 SWAA042119 120040726A52106951337 GUIDE ARM BOEING737 7377H4 1384404NM L1 DOOR MIGRATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 UPON ARRIVAL AT LAS, COULD NOT OPEN FWD ENTRY DOOR MORE THAN A FEW INCHES. REINSTALLED UPPER ARM GUST LOCK PIN PER MM. 2L72 4F RTA16WE 20040804000712004080400071NM 2004 8 4 SWAA042120 120040726A53156545416 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040804000722004080400072 2004 8 4 SWAA042121 420040726A25656557463 FITTING BOEING737 7373H4 1384600NM L2 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED L2 DOOR EVAC SLIDE FITTING PER MM. 2L72 4F RTA16WE 20040804000732004080400073NM 2004 8 4 SWAA042122 120040726A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040804000742004080400074NM 2004 8 4 SWAA042123 120040726A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040804000752004080400075NM 2004 8 4 SWAA042124 120040726A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SPV, FOUND PHOTOLUMINESCENT STRIPS OUT OF ADJUST. ADJUSTED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20040804000762004080400076NM 2004 8 4 SWAA042125 120040726A3350612825 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29633SW 27936 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 15 ABC TO ROW 20 ABC, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040804000772004080400077NM 2004 8 4 SWAA042126 120040726A2560P40021 BATTERY BOEING737 7375H4 138449DNM FLASHLIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED A2 CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040804000782004080400078NM 2004 8 4 SWAA042106 120040725A53146562125 KEELBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM OUTER FLANGE AT BS 718 TO BS 726, LBL 11, CORRODED. REPAIRED KEEL BEAM FLANGE PER EA. 2L72 4F RTA16WE 20040804000802004080400080NM 2004 8 4 SWAA042108 120040725A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND STRINGER SPLICE AT BS 908, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040804000812004080400081NM 2004 8 4 SWAA042127 120040726A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29470WN 33860 DURING SPV, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040804000822004080400082NM 2004 8 4 SWAA042128 120040726A5320BAC15171489 CHANNEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND FLOOR ZEE CHANNEL AT BS 270, RBL 10, CORRODED. REMOVED AND REPLACED FLOOR ZEE CHANNEL PER SRM. 2L72 4F RTA16WE 20040804000832004080400083 2004 8 4 SWAA042182 420040731A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED RON, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804000842004080400084NM 2004 8 4 SWAA042183 120040731A33506104789 BATTERY BOEING737 737317 138447PNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND L1 & L2 & OVERWING EXIT LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PER MM. 2L72 4F RTA16WE 20040804000862004080400086 2004 8 4 SWAA042185 420040731A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29718SW 27852 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804000872004080400087NM 2004 8 4 SWAA042186 120040731A3260189915 SENSOR BOEING737 7373H4 1384600NM NLG OUT OF TOLERANCEA SWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW29323SW 23344 AIR TURNBACK, AFTER TAKEOFF AND GEAR HANDLE UP, RED NOSE GEAR LIGHT REMAINED ILLUMINATED, CYCLED GEAR HANDLE DOWN AND UP. INDICATION NORMAL, APPROX 5 MINUTES LATER IN CLIMB, RED AND GREEN NOSE GEAR LIGHTS ILLUMINATED. REMOVED AND REPLACED SENSOR S845 PER MM. 2L72 4F RTA16WE 20040804000882004080400088 2004 8 4 SWAA042177 420040731A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804000942004080400094NM 2004 8 4 SWAA042150 120040728A57536546435277 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040804000982004080400098NM 2004 8 4 SWAA042154 120040728A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 727B TO BS 942, RBL 68 TO RBL 57, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20040804000992004080400099NM 2004 8 4 SWAA042156 120040728A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 460 TO BS 466, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20040804001022004080400102NM 2004 8 4 SWAA042181 120040731A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED A1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040804001032004080400103WP 2004 8 4 AALA20040738 120040718A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219307R 49663 DFW - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 26 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 26 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040804001052004080400105WP 2004 8 4 AALA20040734 120040717A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217549A 53031 ORD - AFT OVERHEAD EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERHEAD EMERGENCY LIGHTS BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804001062004080400106WP 2004 8 4 AALA20040732 120040717A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 EMERGENCY LIGHTS AT SEAT 14D OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 14D OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804001072004080400107WP 2004 8 4 AALA20040735 120040717A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217549A 53031 ORD - BOTTOM EMERGENCY LIGHTS AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR BOTTOM EMERGENCY LIGHTS AT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804001092004080400109NM 2004 8 4 AALA20040736 120040718A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 DFW - OUTSIDE OVERWING RIGHT HAND EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER EQUIPMENT NUMBER M731 FOR OUTSIDE OVERWING RIGHT HAND EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040804001112004080400111EU 2004 8 4 MALA040489 120040714A3030 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU ALPHA LIGHT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15110XJ 340A110 DURING FLIGHT L ALPHA LIGHT CAME ON, RAN QRH LIGHT STAYED ON. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED CIRCUIT BREAKER 13 XA, ALL CHECKS GOOD IAW SF-340MM CH 24. 2L72 4T RTA52EU 20040804001122004080400112WP 2004 8 4 04FDEA02021 120040707A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 SEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL 1 AND 51-21-01 VOL 2. 2L73 4F RTA22WE 20040804001132004080400113WP 2004 8 4 04FDEA02022 120040707A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 SEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20-00 VOL 1 AND 51-21-01 VOL 2. 2L73 4F RTA22WE 20040804001152004080400115WP 2004 8 4 04FDEA02024 120040707A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25385FE 46620 FORWARD LOWER CARGO COMPARTMENT, AFT LOWER END OF DOOR CUTOUT SKIN IS GOUGED. REMOVED DAMAGED IAW DC10/MD10 SRM 53-50-00 VOL 1, FABRICATED REPAIR IAW DC10/MD10 SRM 53-50-00 VOL 1, INSTALLED REPAIR IAW DC10/MD10 SRM 53-50-00 VOL 1. 2L73 4F RTA22WE 20040804001162004080400116WP 2004 8 4 04FDEA01874 120040629A5313AGA3104506 LONGERON DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING PAX TO FREIGHTER CONVERSION, AFT CARGO AREA, STA 1877 TO STA 1951, STRINGER 51 LT, FOUND CORRISION INNER EXTRUSION LONGERON. REPLACED LONGERON 51 IAW SRM 51-33-01 FIG 34, 47 AND SRM 51-35-01. 2L73 4F A22WE 20040804001172004080400117 2004 8 4 SWAA042158 420040728A2565D31354 SLIDE BOEING737 7373L9 1384470NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804001182004080400118NM 2004 8 4 SWAA042159 120040728A53306545765 SKIN BOEING737 7373L9 1384470NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040804001202004080400120NM 2004 8 4 SWAA042161 120040728A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM ROW 13 ABC MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29441WN 29837 DURING SCHEDULED MV2 CHECK, FOUND PHOTOLUMINSCENT STRIP AT ROW 13 ABC, MISSING. REPLACED STRIP PER MM. 2L72 4F RTA16WE 20040804001222004080400122 2004 8 4 SWAA042163 420040728A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE LOOSE. SECURED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804001242004080400124WP 2004 8 4 04FDEA02017 120040707A5753 WEDGE DOUG DC10 DC1030 3023501WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND OUTBOARD FLAP NR 2 TRAILING EDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN IAW DC10 SRM 51-40-02 VOL 2. 2L73 4F A22WE 20040804001252004080400125NM 2004 8 4 04FDEA01966 120040706A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT WING - OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. 2L73 4F RTA22WE 20040804001262004080400126WP 2004 8 4 04FDEA01876 120040629A5311ABA72213 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING PAX TO FREIGHTER MODIFICATION AND TRANSITION CHECK, FOUND FWD AVIONICS COMPARTMENT AT STA 421, FRAME CORRODED. REMOVED AND REPLACED FRAME IAW SRM 51-31-01 PAGE 1-12 AND SRM 51-33-01. 2L73 4F A22WE 20040804001272004080400127WP 2004 8 4 04FDEA02030 120040708A5410AUB7000501 TRUSS FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 COMPLY WITH EA 8-5420-7-79546B NACELLE/PYLON NR 1 ENGINE FWD TRUSS FITTING CORROSION REPAIR P/N AUB7000-501. COMPLIED WITH EA 8-5420-7-79546B. 2L73 4F RTA22WE 20040804001292004080400129WP 2004 8 4 04FDEA01898 120040630A5350AKC70801 GUIDE DOUG DC10 DC1010 3022110WP TAILCONE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 LEFT TAILCONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW SRM 51-33-01 AT MAE. 2L73 4F A22WE 20040804001312004080400131NM 2004 8 4 04FDEA01900 120040701A5320 INTERCOSTAL BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25190FE 19083 FWD CARGO COMPARTMENT INTERCOSTAL IS CRACKED AT STRINGER 22R BS 572 THRU BS 580. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1. 2L73 4F RTA3WE 20040804001322004080400132WP 2004 8 4 AALA20040753 120040727A30202028TP DUCT DOUG DC9 DC982 3022082WP LT ENGINE BROKEN A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21234AA 49181 INFLIGHT T630/27 ON CLIMBOUT LEFT ENGINE LOOP-A ILLUMINATED WITH A FIRE WARNING. LEFT ENGINE AURAL REDUCED POWER AND FIRE WARNING EXTINGUISHED. RETURNED TO SJC AND LANDED WITHOUT INCIDENT. FOUND BLOWN DUCT AT LEFT HAND ENGINE UPPER INBOARD NOSE COWL ANTI ICE. PERFORMED OPERATIONS CHECK OF FIRE LOOP WITH NO DISCREPANCY NOTED. REPLACED BROKEN DUCT AT LEFT HAND ENGINE UPPER INBOARD NOSE COWL ANTI ICE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804001342004080400134EU 2004 8 4 AALA20040752 120040701A5310 BEAM AIRBUS300 A300B4605R 3930308EU FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW2150051 459 TUL - FRAME 51 LEFT HAND GANTRY BEAM NUMBER 4 CRACKED AT LOWER OUTBOARD FLANGE AT STATION 3195. CRACK IS 2 INCHES IN LENGTH. REPAIRED PER ESO 30595 DATED 2004 JULY 01 REPAIR NUMBER 40 531500 3505. 2L72 4F RTA35EU 20040804001362004080400136NM 2004 8 4 CALA0400583 120040721A5330148N3204401 SKIN BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717139 30352 INSPECTION FOUND SKIN UNDER RT AIRPHONE ANTENNA CORRODED AT STA 1440, S29R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 204. 2L72 4F RTA2NM 20040804001372004080400137NM 2004 8 4 CALA0400584 120040723A533065458001120 SKIN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769348 23586 INSPECTION FOUND FUSELAGE SKIN CORRODED AND CRACKED AT STA 259.5-360, S24L TO S29L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5310-04421. 2L72 4F RTA16WE 20040804001412004080400141NM 2004 8 4 CALA0400577 120040719A3350D71701100 BATTERY BOEING737 737724 13844BYNM L1 DOOR LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2739728 28944 INSPECTION FOUND THE L-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY CHARGER AND BATTERY PACK WERE REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD PER WDG 33-51-12. 2L72 4F RTA16WE 20040804001422004080400142NM 2004 8 4 CALA0400578 120040716A5520BACB30NM3K4 BOLT BOEING737 7373T0 1384582NM ELEVATOR SHEARED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714346 23584 THE LEFT O/B ELEVATOR HINGE BOLT WAS FOUND MISSING AND SHEARED OFF DURING A WALKAROUND INSPECTION. THE BOLT OR HINGE HARDWARE WAS JAMMED BETWEEN THE STABILIZER AND ELEVATOR RESULTING IN ADDITIONAL DAMAGE. THE LEFT HORIZONTAL STABILIZER, LEFT ELEVATOR, AND ELEVATOR TAB WERE REPLACED IAW MM 27-31-34, 27-41-11, AND 27-31-11. 2L72 4F RTA16WE 20040804001482004080400148SO 2004 8 4 SWIA200413608 120040720A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT FAILED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07284YV 120284 ONE RED LIGHT ON EMERGENCY LIGHT STRIP IS BURNED OUT. REPAIRED WIRES TO RED LIGHT AT FORWARD FLOOR EMERGENCY LIGHTS, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040804001492004080400149EA 2004 8 4 COMA0460403 120040702A3213 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01931CA 7037 FLIGHT 5759 GEAR DISAGREE WARNING WOW AND STEERING INOP MESSAGE. SERVICED THE NLG SHOCK STRUT. RETRACTION CHECKS NORMAL. 2L72 4F RTA21EA 20040804001502004080400150EA 2004 8 4 COMA0460412 120040712A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 DAMAGED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01917CA25909 7017 FLIGHT 5553 GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20040804001512004080400151EA 2004 8 4 COMA0460409 120040719A5311 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01427CA 7460 RIGHT HAND 640 FRAME DOUBLERS CRACKED. REPAIRED IAW REO 601R-53-61-1089. 2L72 4F RTA21EA 20040804001522004080400152NM 2004 8 4 CALA0400587 120040727A2120UNK SCREEN BOEING777 777224 1385225NM IFE COOLING CLOGGED A CALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW2778008 29478 THE FLIGHT CREW REPORTED THAT THE IFE (INFLIGHT ENTERTAINMENT) CMT UNIT WAS OVERHEATING WHILE EN ROUTE FROM TLV TO EWR. THE AIRCRAFT WAS DIVERTED TO MXP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE FORWARD IFE AIR VENT SCREEN OVER IFE CONTROL STATION WAS PLUGGED WITH LINT AND DIRT IN THE OVERHEAD AREA. THIS PREVENTED THE IFE CMT UNIT FROM GETTING COOLING AIR. THERE WERE NO SIGNS OF ELECTRICAL BURNING AND BOTH IFE FANS WERE WORKING. THE CMT WAS REPLACED. THE AIR VENT SCREEN WAS CLEANED. OPERATION OF THE IFE COOLING SYSTEM CHECKED GOOD IAW MM 21-27-700-803. AN FCD WAS ISSUED TO INSPECT THE REST OF THE FLEET. 2L72 4F RTT00001SE 20040804001532004080400153NM 2004 8 4 CALA0400588 120040708A5230146A611013 DOOR BOEING737 737724 13844BYNM AFT CARGO DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2739728 28944 INSPECTION FOUND A DENT IN THE AFT CARGO DOOR. THE DENT WAS LOCATED IN THE SKIN BAY BETWEEN BEAMS B AND C JUST AFT OF BS 809.35. THE DOOR WAS REPAIRED IAW ECRA 5231-01055. 2L72 4F RTA16WE 20040804001542004080400154SO 2004 8 4 SWIA200413638 120040729A5713 STRINGER EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 LEFT HAND WING STRINGER 10 CRACKED BY RIB 5. ITEM FOUND AT C-CHECK. 2L72 4T RTA31SO 20040804001572004080400157NM 2004 8 4 SWAA042201 120040802A3350604222 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED RON, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS RANDOMLY ILLUMINATE. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040804001592004080400159NM 2004 8 4 SWAA042203 120040801A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT EXTERNAL AIR CONDITION HOOK UP CUTOUT FWD RT CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040804001622004080400162NM 2004 8 4 CALA0400590 120040723A5210141A160417 FITTING BOEING737 737524 1384721NM PAX DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713665 28926 INSPECTION FOUND A CRACK IN THE FORWARD ENTRY DOOR UPPER AFT CORNER DOOR STOP. THE DOOR STOP FITTING WAS REMOVED AND REPLACED IAW ECRA 5210-01783. 2L72 4F RTA16WE 20040804001632004080400163NM 2004 8 4 CALA0400581 120040721A532065C8073533 INTERCOSTAL BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714668 28928 INSPECTION FOUND A 24 INCH CRACK IN INTERCOSTAL AT TOP FASTENER HOLES AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20040804001652004080400165SO 2004 8 4 SWIA200413634 120040618A5413 STRINGER EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07236SW 120312 LEFT NACELLE EXHAUST CRADLE STRINGER CRACKED INBOARD SIDE. ITEM FOUND AT C-CHECK. REPLACED LEFT HAND NACELLE EXHAUST CRADLE STRINGER INBOARD SIDE PER SRM 51-40-00. 2L72 4T RTA31SO 20040804001682004080400168SO 2004 8 4 SWIA200413599 120040718A7712 SIGNAL COND UNIT EMB 120 EMB120ER 3260203SO RT ENGINE MALFUNCTIONED A SWIAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM07190SW 120050 ON T/O ROLL, RIGHT ENGINE AUTO-FEATHERED DURING POWER LEVER ADVANCEMENT. REMOVED AND REPLACED RIGHT HAND ENGINE TORQUE SIGNAL CONDITIONER IAW MM 77-11-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040804001702004080400170SO 2004 8 4 SWIA200413602 120040721A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07234SW LEFT SIDE FLOOR REAR ROW EMERGENCY LIGHT DOES NOT ILLUMINATE. REPAIRED WIRING TO AFT FLOOR EMERGENCY LIGHT. EMERGENCY LIGHTS OPERATE NORMALLY. 2L72 4T RTA31SO 20040804001712004080400171NM 2004 8 4 CALA0400573 120040714A575465C26601 SKIN BOEING737 7373T0 1384582NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND A 2 INCH CRACK IN NR 3 SLAT SKIN LOWER EDGE AT RIVET HOLES ADJACENT TO ACTUATOR. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 57-43-01, FIGURE 206. 2L72 4F RTA16WE 20040804001732004080400173NM 2004 8 4 CALA0400575 120040715A53206546568520 STIFFENER BOEING737 7373T0 1384582NM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND APB VERTICAL STIFFENER CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200. 2L72 4F RTA16WE 20040804001752004080400175EA 2004 8 4 SWIA200413614 120040715A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW LEFT HAND WHEEL WELL HAT ANGLE AT FS 530.00 ON UNDERSIDE OF PRESSURE FLOOR IS CRACKED. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ SRM 51-31-00, 51-24-21, 51-24-36, 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-06, AND 51-23-00. 2L72 4F RTA21EA 20040804001762004080400176EA 2004 8 4 SWIA200413615 120040715A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW RIGHT HAND WHEEL WELL HAT ANGLE AT FS 530.00 ON UNDERSIDE OF PRESSURE FLOOR IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED HAT ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-25-16, 51-21-11. 2L72 4F RTA21EA 20040804001772004080400177EA 2004 8 4 SWIA200413616 120040715A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED O/B LOCATION FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-25-16, AND 51-21-11. 2L72 4F RTA21EA 20040804001792004080400179EA 2004 8 4 SWIA200413618 120040715A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED I/B LOCATION. ITEM FOUND AT C-CHECK. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, AND 51-23-00. 2L72 4F RTA21EA 20040804001832004080400183EA 2004 8 4 SWIA200413622 120040630A5320 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07929SW 7703 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.0 RBL 9.0 I/B. ITEM FOUND AT C-CHECK. 2L72 4F RTA21EA 20040804001882004080400188EA 2004 8 4 SWIA200413627 120040722A5270 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA EMERGENCY DOOR DIRTY A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07971SW 7947 RIGHT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. CLEANED DEBRIS FROM RIGHT EMERGENCY DOOR PROXIMITY SWITCH. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20040804001912004080400191SO 2004 8 4 SWIA200413630 120040725A5230 SEAL EMB 120 EMB120ER 3260203SO CARGO DOOR DAMAGED A SWIAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 NM07295SW 120322 LOST PRESSURIZATION IN AUTO AND MANUAL MODES. REINSTALLED CARGO DOOR SEAL AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040804001932004080400193 2004 8 4 SWAA042187 420040731A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804001942004080400194NM 2004 8 4 SWAA042188 120040731A3350110049 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND AFT CENTER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED AFT LIGHT BATTERY PER MM. 2L72 4F A16WE 20040804001952004080400195 2004 8 4 SWAA042189 420040731A256565C16820 HOOK BOEING737 7373H4 1384600NM R1 DOOR GIRT BARCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS, CORRODED. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20040804001962004080400196 2004 8 4 SWAA042190 420040801A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804001972004080400197NM 2004 8 4 SWAA042192 120040801A3350300432 LIGHT BOEING737 7373H4 1384600NM L2 DOOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND BATTERY PER MM. 2L72 4F RTA16WE 20040804001982004080400198NM 2004 8 4 SWAA042193 120040801A53116547684 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303.9, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB. 2L72 4F RTA16WE 20040730000102004073000010NM 2004 7 30 SWAA042143 120040727A531565C33940 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294, RBL 53, CORRODED. REPAIRED CHORD PER SRM. 2L72 4F RTA16WE 20040730000222004073000022NM 2004 7 30 04FDEA02238 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.394, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.390 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LEFT HAND OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000322004073000032NM 2004 7 30 04FDEA02245 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) ACTUATOR HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.405, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.398 AND REPAIRED AS PER FEDEX EA 1-5750-80280, TITLE: WINGS - RT OUTBOARD FLAP - OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000442004073000044NM 2004 7 30 04FDEA02255 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.129 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040730000542004073000054NM 2004 7 30 04FDEA02175 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1209 LBL 48. REMOVED AT STA 1266 TO LBL48 AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME II. REPAIR TRACK AND SPLICE FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040730000582004073000058NM 2004 7 30 04FDEA02171 120040726A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK FOUND DAMAGED AT STA 1259 RBL 48 AT 3 LOCATIONS. DAMAGED SEAT TRACK AT CABIN STA 1259 RBL 48 AT 3 LOCATIONS REMOVED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & PARTS FABRICATED & INSTALLED AS PER SRM 51-31-01 VOL II & SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20040804001992004080400199NM 2004 8 4 SWAA042194 120040801A533065C35772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN UNDER DORSAL FIN AT BS 860, WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040804002012004080400201NM 2004 8 4 SWAA042196 120040801A5310907822 HINGE BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER HINGE INTERIOR H-DOUBLER CRACKED. REPAIRED FWD ENTRY DOOR HINGE PER EA. 2L72 4F RTA16WE 20040804002032004080400203 2004 8 4 MALA040491 420040716A3420PC251123C INVERTER SAAB SF340 340B 7860101EU NR 1 INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15437XJ 340B437 AFTER DEPARTURE FROM MQT INTO IMC, THE EADI'S BEGAN TO DRIFT TO THE LEFT TO APPROX 20 DEGREES OFF RUNWAY HEADING. DURING TURNOUT THE HDG FLAGGED ON BOTH EADI'S. AFTER LEVELING OFF CONFIRMED THE EADI'S WERE OFF COMPASS HEADING BY 50 DEGREES. RECEIVED RMI FLAGS ON BOTH RMI'S. TRIED THE NR 1 INVERTER, NO CHANGE. A/C DIVERTED TO ESC. MAINTENANCE REPLACED NR 1 INVERTER P/N PC251-123C, S/N OFF 9123, S/N ON 8198. NR 1 INVERTER CHECKS GOOD IAW SF340 MM CH 24. RESET NR 1 AND NR 2 AHRS COMPUTERS. NR 1 AND NR 2 AHRS CHECK GOOD IAW SF340 MM CH 34. 2L72 4T RTA52EU 20040804002062004080400206EA 2004 8 4 SWIA200413586 120040719A274170744 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA HORIZONTAL STAB INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07702SK 10136 STAB CH 1 INOPERATIVE. REMOVED AND REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW CRJ 700 MM 27-42-07. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040804002072004080400207EA 2004 8 4 SWIA200413587 120040716A1420 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA SMOKE DETECTOR DIRTY A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07702SK CARGO SMOKE DETECTOR CAUTION MESSAGE. CLEANED CONNECTORS TO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040805001092004080500109WP 2004 8 5 ASAA0480438 120040517A532059360717 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - DURING C-CHECK, FOUND INTERCOSTAL IS CORRODED AT FS 1211-1231 AT LONGERON 29L. REPLACED INTERCOSTAL PER SRM 51-30-5. (M) 2L72 4F RTA6WE 20040805001112004080500111WP 2004 8 5 ASAA0480456 120040529A532199365811 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - FOUND DURING C-CHECK, FLOOR PANEL DELAMINATED AT CABIN ROW 11. REBONDED PANEL PER MM 25-00-00. (M) 2L72 4F A6WE 20040805001142004080500114WP 2004 8 5 ASAA0480473 120040605A561059644202 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS2820816596 53020 SEA - DURING PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REINSTALLED LOCK/UNLOCK PIN IN LINK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040805001152004080500115WP 2004 8 5 ASAA0480474 120040607A561059644202 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS2823316621 53020 DURING PREFLIGHT CHECK, FOUND RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPOSITION FORWARD UPPER ALIGNMENT PIN IN TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040805001172004080500117WP 2004 8 5 ASAA0480470 120040604A57535910042 VANE DOUG DC9 DC983 3022083WP TE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01977AS 53453 FOUND DURING C-CHECK, RIGHT OUTBOARD FLAP T/E INBOARD FOREFLAP IS PUNCTURED ON L/E. REMOVED DAMAGED EDGES. ADDED DOUBLER AND FILLER PER SRM 53-03. (M) 2L72 4F RTA6WE 20040805001202004080500120WP 2004 8 5 ASAA0480472 120040604A561059644202 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS2820816596 53020 SEA - DURING PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED GUIDE PIN IN UPPER LEFT CORNER. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040805001212004080500121NM 2004 8 5 ASAA0410293 120040617A53306522216 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND LOWER NOSE COMPARTMENT ACCESS DOOR OUTER SKIN CRACKED 4.5 INCHES FROM FORWARD EDGE 3.5 INCHES FROM RT EDGE. REPAIRED LOWER NOSE COMPARTMENT ACCESS DOOR OUTER SKIN WITH DOUBLER AND FILLER. (M) 2L72 4F RTA16WE 20040805001232004080500123NM 2004 8 5 ASAA04010282 120040603A531165549183 FRAME BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR LOWER AFT STUB FRAME HAS ELONGATED HOLES. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-20-01. (M) 2L72 4F A16WE 20040805001242004080500124NM 2004 8 5 ASAA0410285 120040603A53116554919 FRAME BOEING737 737290C 138448VNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR STUB FRAME IS GOUGED. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-30-2. (M) 2L72 4F A16WE 20040805001252004080500125NM 2004 8 5 ASA04010307 120040701A532065458953 SPLICE BOEING737 737298C 1384490NM STRINGER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 27L SPLICE CAP AT BS 908 HAS OVERSIZE HOLES. REMOVED AND REPLACED STRINGER 27L SPLICE CAP. (M) 2L72 4F RTA16WE 20040805001262004080500126NM 2004 8 5 ASAA0410295 120040619A53306573742 SKIN BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE SKIN BLEND OUT IS OUT OF LIMITS FROM CHAFE. ACCOMPLISHED EXTERNAL SKIN REPAIR. (M) 2L72 4F RTA16WE 20040805001292004080500129NM 2004 8 5 ASAA0410272 120040527A53106546537 BEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED CORROSION AND REPAIRED LONGITUDINAL BEAM. (M) 2L72 4F A16WE 20040805001302004080500130NM 2004 8 5 ASAA0410281 120040603A523065622302 FITTING BOEING737 737290C 138448VNM CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR FORWARD LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPAIRED IAW GOODRICH EO 04-2573. (M) 2L72 4F A16WE 20040805001312004080500131NM 2004 8 5 ASAA0410273 120040527A5310656210042 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION AND REPAIRED WEB. (M) 2L72 4F A16WE 20040805001332004080500133NM 2004 8 5 ASAA0410328 120040709A5310654655116 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON FRAME SHEAR TIE REPAIR. REMOVED AND REPLACED FRAME SECTION. (M) 2L72 4F RTA16WE 20040805001342004080500134NM 2004 8 5 ASAA0410347 120040712A53136545778554 STRINGER BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CRACK IN STRINGER 15R BS 1003 WL 226. REPAIRED STRINGER. (M) 2L72 4F RTA16WE 20040805001352004080500135NM 2004 8 5 ASAA0410322 120040712A53146547693502 KEELBEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON KEEL BEAM AFT CARGO BAY RT BEAM. REMOVED AND REPLACED KEEL BEAM. (M) 2L72 4F RTA16WE 20040805001372004080500137NM 2004 8 5 ASAA0410316 120040708A531065465505002 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSON ON FRAME SHEAR TIE REPAIR. REMOVED CORRODED SHEAR TIE, FABRICATED REPLACEMENT PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001402004080500140 2004 8 5 ASAA0480464 420040529A25653961896501 LANYARD DOUG DC9 DC983 3022083WP L2 DOOR SLIDE DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01947AS 53020 SEA - AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20040805001412004080500141WP 2004 8 5 ASAA0480459 120040529A532199365811 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT CLASS DIVIDERS. REBONDED PANELS PER MM 25-00-00. (M) 2L72 4F A6WE 20040805001422004080500142WP 2004 8 5 ASAA0480460 120040529A57545930580 SKIN DOUG DC9 DC982 3022082WP LT NR 5 SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING C-CHECK, FOUND LEFT WING NR 5 SLAT IS DENTED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER SRM 57-03. (M) 2L72 4F A6WE 20040805001442004080500144WP 2004 8 5 ASAA0480440 120040517A5330593442561 PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - DURING C-CHECK, FOUND LEFT LOWER VOR ANTENNA PANEL IS DELAMINATED. REMOVED AND REPLACED DAMAGED SECTION PER EA 3450-01028. (M) 2L72 4F RTA6WE 20040805001462004080500146NM 2004 8 5 ASAA0440123 120040507A5320BAC1496377 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 OAK - AFT CARGO COMP RIGHT 'Z' ANGLE CORRODED STATION 727D TO 727G. REMOVED AND REPLACED Z-ANGLE RT STATION 727D TO 727G. (M) 2L72 4F RTA16WE 20040805001472004080500147NM 2004 8 5 ASAA0410275 120040528A53156554906501 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM LOWER SURFACE. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F A16WE 20040805001482004080500148NM 2004 8 5 ASAA0410276 120040528A533065621091 BEAR STRAP BOEING737 737290C 138448VNM PWA JT8 JT8D* NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 FOUND FUSELAGE SKIN CRACKED AT MAIN CARGO DOOR CUTOUT UPPER FORWARD CORNER. REMOVED DAMAGE/CRACKED AREA, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F4 F A16WE E2EA 20040805001552004080500155WP 2004 8 5 ASAA0480469 120040604A55205930557501 COVER DOUG DC9 DC983 3022083WP ELEVATOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01977AS 53453 OKC - DURING C-CHECK,FOUND LEFT ELEVATOR INBOARD FAIRING COVER UPPER OUTBOARD FASTENER HOLE IS CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 5520-01193. (M) 2L72 4F RTA6WE 20040805001572004080500157NM 2004 8 5 ASAA0410274 120040528A5315655491317 FLOORBEAM BOEING737 737290C 138448VNM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON FLOORBEAM UPPER CHORD. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F A16WE 20040805001602004080500160NM 2004 8 5 ASAA0410306 120040701A53306545771 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON FUSELAGE OUTER SKIN FORWARD OF BUTT SPLICE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, DAMAGED AREA TO INCORPORTATE INTO REPAIR. (M) 2L72 4F RTA16WE 20040805001622004080500162NM 2004 8 5 ASAA0410296 120040621A5310BAC14902807 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON SHEAR TIE. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE REPAIR. (M) 2L72 4F RTA16WE 20040805001632004080500163NM 2004 8 5 ASAA0410290 120040605A523065622314 FITTING BOEING737 737290C 138448VNM CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR NR 2 FORWARD LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPLACED FITTING. (M) 2L72 4F A16WE 20040805001642004080500164NM 2004 8 5 ASAA0410288 120040605A531165C352433 FRAME BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION AFT PIT BAY FRAME. ACCOMPLISHED REPAIR OF THE AFT CARGO DOOR CUTOUT FORWARD FRAME. (M) 2L72 4F A16WE 20040805001652004080500165NM 2004 8 5 ASAA0410291 120040605A5230656622301 FITTING BOEING737 737290C 138448VNM CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR NR 1 AFT LATCH FITTING HAS FASTENER HOLES ARE ELONGATED. REMOVED AND REPAIRED ON MIG 5 4841772 AND GOODRICH ER 04-2573. (M) 2L72 4F A16WE 20040805001662004080500166NM 2004 8 5 ASAA0410308 120040701A532065458953 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 26L SPLICE CAP AT BS 908 HAS OVERSIZE HOLES. REMOVED AND REPLACED STRINGER 26L SPLICE CAP. (M) 2L72 4F RTA16WE 20040805001682004080500168NM 2004 8 5 ASAA0410299 120040628A53116546595517 FRAME BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON FRAME, AFT CARGO BAY. REMOVED DAMAGE AND REPAIRED FRAME. (M) 2L72 4F RTA16WE 20040805001692004080500169NM 2004 8 5 ASAA0410301 120040629A5330 SKIN BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND GOUGE IN FUSELAGE SKIN. INSTALLED DOUBLER, TRIPLER. (M) 2L72 4F RTA16WE 20040805001712004080500171NM 2004 8 5 ASAA0410297 120040621A53306573741 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED CRACK AT CAPTAIN'S C-D WINDOW LOWER FORWARD CORNER BS 204.5. (M) 2L72 4F RTA16WE 20040805001742004080500174NM 2004 8 5 ASAA0410321 120040709A5310BAC14902807 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND DAMAGED SHEAR TIE. REMOVED DAMAGE, FABRICATED AND INSTALLED SHEAR TIE REPAIR. (M) 2L72 4F RTA16WE 20040805001812004080500181NM 2004 8 5 ASAA0410324 120040711A5310BAC14902807 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND AFT CARGO SHEAR TIE IS CORRODED. REMOVED AND REPLACED SHEAR TIE. (M) 2L72 4F RTA16WE 20040805001822004080500182NM 2004 8 5 ASAA0410303 120040701A53306545771 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON FUSELAGE SKIN FORWARD OF BUTT SPLICE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. DAMAGED AREA TO BE INCORPORATED INTO REPAIR. (M) 2L72 4F RTA16WE 20040805001842004080500184NM 2004 8 5 ASAA0410298 120040627A5310656217319 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND SHEAR TIE CORRODED BETWEEN STRINGER 27R AND 28R BS 520 PREVIOUS FRAME SHEAR TIE REPAIR. REMOVED AND REPLACED SHEAR TIE. (M) 2L72 4F RTA16WE 20040805001862004080500186NM 2004 8 5 ASAA0410344 120040712A53206545435501 ANGLE BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON SKIN TO BULKHEAD ANGLE STATION 535 RBL 16 WL 146. REPAIRED BULKHEAD ANGLE. (M) 2L72 4F RTA16WE 20040805001962004080500196WP 2004 8 5 ASAA0480435 120040517A53135936027501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - DURING C-CHECK, FOUND LONGERON 28R IS CORRODED AROUND FASTENERS AT FS 1039-1046. REMOVED DAMAGE AND INSTALLED DOUBLER AND TRIPLER PER EA 5310-02369. (M) 2L72 4F RTA6WE 20040805002022004080500202NM 2004 8 5 ASAA0410310 120040704A5313BAC1498161 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON STRINGER 23L. SPLICE IN NEW STRINGER SECTION. (M) 2L72 4F RTA16WE 20041124000632004112400063EA 2004 11 24 ASOA04825 120041021A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7198 7203 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND CRACKED AROUND THE BASE. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE. 2L72 4F4 FRTA21EA E15NE 20041124000732004112400073NM 2004 11 24 GAIA04141 120040910A5730 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE LT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND LT WING UPPER L/E SKIN NR 3 SLAT HOOK CUT OUT CRACKED. REF FASI N/R ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4. 2L73 4F4 F A3WE E2EA 20041124000762004112400076NM 2004 11 24 ASAA0410398 120040917A335020131A BATTERY BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 DURING MAINTENANCE CHECK, SMOKE BARRIER (EXIT TO REAR) LIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECKED GOOD. 2L72 4F4 F A16WE E2EA 20041124000942004112400094EA 2004 11 24 ASOA04826 120041024A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27824AS 7203 DURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, LBL 27 AND LBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, LBL 36 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041124000952004112400095 2004 11 24 A6WA200440168 420041025A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AHRS UNRELIABLE A A6WAO OTHER S AFFECT SYSTEMS CRCRUISE 1 GL31437AW2355 1003 7744 PITCH AND ROLL ANNUNCIATOR ILLUMINATED ON CAPTS EFIS IN FLIGHT. PITCH UNRELIABLE, MORE THAN 6 DEGREES THAN F/O EFIS ATTITUDE. PITCH ILLUMINATED ON GROUND DEPOWERED AND REPOWERED. TAXI TEST OK. PROBLEM REOCCURRED IN FLIGHT. REMOVED AND REPLACED NR 1 AHRS COMPUTER IAW 34-21-01, OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041124001032004112400103NM 2004 11 24 GAIA04154 120040910A5754 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 5 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND RT WING L/E AT NR 5 SLAT GUIDE CUTOUT CRACKED. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4. 2L73 4F4 F A3WE E2EA 20041124001042004112400104SW 2004 11 24 ALG2004F00064 120040908A2560 SHOULDER BELT BELL 407 407 1182206SW ALLSN 250C 250C47B GL PAX CABIN ODOR E ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW03537AL 53230 CAE847018 AFTER DEPARTING LFT WITH MMS DIRECT TO SM58 PASSENGER IN BACK RT SEAT FORWARD FACING COMPLAINED OF (STRONG FUEL ODOR) TO THE POINT OF ASKING FOR AIR SICK BAG. DIVERTED AIRCRAFT FOR MAINTENANCE. MAINTENANCE INSPECTED ENGINE COMPARTMENT AT 100 PERCENT, NO LEAKS NOTED, REMOVED HAT RACK BIN, FUEL VALVE ACCESS PANEL, ENGINE MOUNT ACCESS PANELS AND ROLL OVER PANELS, NO LEAKS NOTED. REPLACED RT AFT PASSENGER SHOULDER HARNESS DUE TO A SLIGHT SMELL OF FUEL ODOR. REINSTALLED SAME AS REMOVED PANELS AND RELEASED THE AIRCRAFT TO SERVICE. 1G71 3U3 UO H2SW E1GL 20041124001092004112400109NM 2004 11 24 USAA040816 120040902A53206546812161 STRAP BOEING737 7374B7 1384702NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19783AU55352 25022 PIT, Q5, STRAP 1 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 1016 BL 0. REPLACED STRAP IAW MFG DRAWING 65-46812. 2L72 4F4 FRTA16WE E2GL 20041124001402004112400140EA 2004 11 24 ASOA04801 120041015A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A C-CHECK, RT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO 600-53-0105. 2L72 4F4 FRTA21EA E15NE 20041124001422004112400142EA 2004 11 24 ASOA04725S 120040923A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE POWER SUPPLY DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27820AS148891210 7188 DURING ROUTINE SERVICE INSPECTION, THE PASSENGER DOOR EMERGENCY FLOODLIGHT AND THE FORWARD OVERWING EMERGENCY EXIT LIGHTS ON THE LT AND RT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041124001572004112400157CE 2004 11 24 GUU2004F00033 120041003A55201016200131 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178755117763 UE206 AT SCHEDULED ROUTINE MAINTENANCE, RT CTR ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CTR ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20041129000192004112900019NM 2004 11 29 UIEA200400195 120041115A542065B907072 FAIRING BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 4 PYLON DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 4 PYLON FAIRING ASSY. AT THE AFFECTED AREA, SKIN AND CORE WERE TRIMMED FROM BOTH IB AND OB SIDES WITH REPLACEMENT CORE, SKIN AND DOUBLERS BONDED IAW SRM 51-40-06. PERFORM DETAILED VISUAL INSPECTION INCLUDING COIN TAP OF THE FAIRINGS AT THE SUBJECT REPAIR AREAS, EVERY C-CHECK OR 18 MONTHS WHICHEVER COMES FIRST FOR DELAMINATION, CRACKING OR LOOSE FASTENERS. EO TO BE ISSUED TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2L74 4F4 F A20WE E23EA 20041129000282004112900028EA 2004 11 29 ASOA04836 120041025A5330 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A C-CHECK, THE RT DOUBLER AT FS 640 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT DOUBLER AT FS 640. 2L72 4F4 FRTA21EA E15NE 20041129000322004112900032EU 2004 11 29 ASOA04806 120041018A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27530AS 1359 453 DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041129000422004112900042NM 2004 11 29 USAA040805 120040913A5310 DOOR FRAME BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, WEB FRAME, 3 INCH CRACK AT FWD ENTRY DOOR LOWER WEB FRAME FORWARD CORNER. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-02 FIG 1, SRM 51-70-11 FIG 1. 2L72 4F4 FRTA16WE E2GL 20041129000552004112900055CE 2004 11 29 FFS2004F00003 120040923A561010138402522 WINDSHIELD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL COCKPIT FAILED E FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575Y UC162 COPILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED AFTER THE AIRCRAFT LEVELED OFF AT FL240, OUTSIDE AIR TEMPERATURE OF -37 DEGREES C WITH THE WINDSHIELD HEAT OFF. THE CRACKS APPEARED SUDDENLY ALL OVER, WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE, UNKNOWN. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20041129000602004112900060NM 2004 11 29 AMTA200401345 120041101A5310 SHEAR WEB BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11520AT 27976 CORROSION ON DECK PLATE, BS 1681, LBL 30 AT FASTENER HOLE. SHEAR WEB BS 1681 TO 1720 WILL BE REPLACED ON EO 757-53SW-25 91, REVC. 2L72 4F4 FRTA2NM E12EU 20041129000642004112900064NM 2004 11 29 USAA040817 120040825A5753 STRUCTURE BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE LT OB FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, MIDFLAP 1 INCH X 1 INCH, WORN. LT OB MIDFLAP LOWER SIDE AFT OF OB JACKSCREW ATTACH BRACKET. INSTALLED DOUBLER IAW TR 57-50-17. 2L72 4F4 FRTA16WE E2GL 20041129000752004112900075NM 2004 11 29 C7WA200400042 120040922A5311 DOOR FRAME BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 ELECTRONIC COMPARTMENT DOOR CUTOUT AFT FRAME CORRODED STA 450 BETWEEN STRINGER 27 RT AND 27 LT. REMOVED AND REPLACED FRAME SECTION. FABRICATED NEW FRAME SECTION IAW SAMPLE. MATER USED 7075-0, .050, HEAT TREATMENT TO 7075-T6 IAW BAC 5602. 2L73 4F4 F A3WE E2EA 20041129000822004112900082EU 2004 11 29 DAT2004F00005 120041020A7714WL3301KTD6 INDICATOR STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA LT TACHOMETER FAILED E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13167RC SH3038 RETURNED AFTER TAKEOFF DUE TO LOW PROP RPM ON LT ENGINE. MECHANIC DETERMINED A BAD PROP GAUGE. REMOVED AND REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2H72 4T4 T A41EU E4EA 20041129000892004112900089EA 2004 11 29 SIMA200429815 120041023A3350GE1317 BULB CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21502AE 10018 CREW REPORTED THE OVERHEAD REAR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041129000972004112900097NM 2004 11 29 GAIA04173OP 120041113A33501000677 LIGHT BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE L-1 DOOR INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07751US 21513 NO FLIGHT FWA: DURING POST FLIGHT, FOUND FORWARD ENTRY EMERGENCY EXIT LIGHT NOT TAKING A CHARGE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041129001242004112900124EU 2004 11 29 A6WA200460049 120041021A5730 SKIN BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE LT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 CHAFE DAMAGE TO THE LT WING UPPER SKIN MAX DEPTH OF DAMAGE IS .028 INCH. MAINTENANCE REQUESTED REPAIR FROM AVMAX FAX 608-2049001. 2H74 4F4 F A49EU E6NE 20041129001262004112900126EA 2004 11 29 ASOA04772 120040929A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN AIR CONTAMINATED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27823AS 7196 DURING CRUISE, CREW NOTICED RESIDUAL FUEL/OIL ODOR FROM PREVIOUS FLIGHT IN THE COCKPIT. ODOR DID NOT PROGRESS BUT PILOT AND F/O PUT ON THEIR OXYGEN MASKS AS A PRECAUTION FOR REMAINDER OF FLIGHT. THERE WERE NO SIGNS OF HYPOXIA OR ANY OTHER DETRIMENTAL SIDE EFFECTS. THE AIRCRAFT LANDED SAFELY. UPON INSP MAINTENANCE FOUND RESIDUAL FUEL IN THE AFT EQUIPMENT BAY BELOW THE BLEED AIR SUPPLY DUCTS AND CLEANED AREA. MAINT ALSO REMOVED AND REPLACED COALESCER SOCKS ON LT AND RT PACKS FOR PREVENTATIVE MAINT. MAINT GROUND THE ENGINES, AUXILIARY POWER UNIT AND BOTH PACKS. NO LEAKS OR ODORS WERE NOTED. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001382004112900138NM 2004 11 29 GAIA04110 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CANNING A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN OIL CANNED AT STA250 BELOW STR24R. REF FASI NR 86514 INSTALL DOUBLER REPAIR IAW SRM 53-30-3, FIG 24. 2L73 4F4 F A3WE E2EA 20041129001452004112900145NM 2004 11 29 GAIA04161 120040910A5314 KEELBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW13180AX 20041 DURING C-CHECK INSPECTION FOUND RT WHEEL WELL KEELBEAM WEB AT BS 870, CRACKED. REF FASI NR 86980 INSTALLED WEB REPAIR DOUBLER IAW SRM51-40-3. 2L73 4F4 F A3WE E2EA 20041129001482004112900148NM 2004 11 29 M562004F00002 120040704A5347 SEAT TRACK BOEING737 737400 138449ANM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED I M56BO OTHER O OTHER NRNOT REPORTED 1 EA0537NY 17852 23976 MAIN CABIN STA 903-927, WL 208, LBL 44, SEAT TRACK HAS CORROSION TO SURFACE. REMOVED AND REPLACED SEAT TRACK. C1, C2, C3 INSP 8/4/04. 2L72 4F4 FRTA16WE E21EU 20041129001562004112900156EA 2004 11 29 ASOA04773 120040930A5210601R3189103 ROD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE OR OUTSIDE. MAINTENANCE ADJUSTED THE LOCK MECHANISM ROD ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001772004112900177NM 2004 11 29 ASAA0410417 120041002A533065458001183 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE AT SKIN LAP. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2EA 20041129001802004112900180EA 2004 11 29 A6WA200440163 120041025A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 RT WS 53.60 BATT RIB ASSY IS CRACKED, 1 INCH LONG IN AFT UPPER RADIUS. REPAIRED BATT RIB ASSY BY CUTTING OUT DAMAGED SECTION. FABBED REPAIR ANGLE FROM S6144-0 AND FILLER FROM 7075T62 P.O. NR 35850, INSTALLED REPAIR PARTS WET USING SOLID RIVETS AND HI-LIGHT FASTENERS. ALL WORK DONE IAW REO 601R-57-51-046, REV B AND EO 601R-57-5541. 2L72 4F4 FRTA21EA E15NE 20041129001942004112900194EU 2004 11 29 ASOA04489S 120040706A2752FE231002 ACTUATOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT WING TE FLAP LEAKING A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27643AS8127 5656 413 DURING CLIMB-OUT, AT APPROXIMATELY 6,000 TO 7,000 FEET, THE CREW RECEIVED A LOW LEVEL MESSAGE ON THE BLUE HYDRAULIC SYSTEM. THE CREW FOLLOWED THE QRH AND SHUTOFF THE BLUE PUMPS. APPROXIMATELY FORTY MILES FROM AIRPORT, A LOW LEVEL MESSAGE ON THE GREEN HYDRAULIC SYSTEM WAS RECEIVED. THE CREW FOLLOWED THE QRH AND SHUT OFF THE GREEN PUMP EXPERIENCING A TOTAL HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND AC LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED LT IB FLAP ACTUATOR. ALSO, CYCLED THE FLAPS FIFTEEN TIMES WITHOUT ANY DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041129002082004112900208NM 2004 11 29 USAA040700 120040907A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 ANGLE SUPPORT, .1250 INCH X .1250 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 794, S-25R. REPLACED ANGLE IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20041130000032004113000003EA 2004 11 30 COMA0460634 120041118A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RT WING FAULTY A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01981CA5924 7163 FLIGHT 5304 RECEIVED A FLAP FAIL CAUTION MESSGE DURING TAXI OUT. AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT BPSU. 2L72 4F RTA21EA 20041130000202004113000020EA 2004 11 30 SWIA200414101 120041115A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER CRCRUISE 1 NM07907SW 7511 WHILE LEVEL AT FL350 LEFT WINDSHIELD SHATTERED. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01. P/N OFF 601R33033-13, S/N OFF 61030H8727. 2L72 4F RTA21EA 20041130000242004113000024NM 2004 11 30 AWXA200401290 120041101A521065458715 DOOR FRAME BOEING737 7373Y0 1384671NM R-1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT. MAINTENANCE TRIMMED OUT CRACK IN AFT EDGE OF R-1 DOOR AT 4TH DOOR STOP FROM BOTTOM BS 312, STR 12 RT. PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY CRACK CONTAINED, TREATED REPAIR AREA. 2L72 4F RTA16WE 20041130000302004113000030EA 2004 11 30 COMA0460643 120041122A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01973CA 7146 LEFT HAND FS 484 CRACKED AT INTERCOSTAL, INBOARD AND OUTBOARD UNDERNEATH FLOORBOARD 261 DLF. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20041130000552004113000055WP 2004 11 30 ABXA040370 120041027A53119919617502 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 FORWARD RIGHT MAIN FRAME, STA 699, REQUIRED REPLACEMENT. CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED RIGHT MAIN FRAME, STA 699 IAW JOB CARD EA 53400322-001-4. 2L72 4F A6WE 20041130000642004113000064EU 2004 11 30 AWXA200401273 120041023A5320D53112087200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK LONGITUDINAL FLOORBEAM (FLOOR SUPPORT) Y254 LT WAS FOUND WITH WORN HOLES BETWEEN FR 12 AND FR 14. MAINTENANCE REMOVED WORN FLOOR SUPPORT Y254 LT FROM FR 12 TO FR 14. FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND 4 EACH ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14 FIG 202. 2L72 4F RTA28NM 20041130000692004113000069NE 2004 11 30 CX7A194J0458 320041118A611469992A16 BEARING RACE HAMSTD 14RF19 SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE PROP HUB SPLIT A CX7AK NONE O OTHER ININSP/MAINT 1 GL03315CE6987 20011012 340B343 871080 RIGHT PROP HUB NR 2 BLADE BEARING RACE DAMAGED AND SPLIT BALL BEARINGS. 2L72 4T RTA52EU 6 CP11NE 20041130000842004113000084EU 2004 11 30 AWXA200401265 120041025A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 43 AND FR 44. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 43 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000932004113000093NM 2004 11 30 CALA0400724 120041121A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20041130000992004113000099EA 2004 11 30 SWIA200414111 120041118A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07441SW 7602 CARGO SMOKE WARNING ILLUMINATED IN FLIGHT FOR 2 SECONDS, THEN EXTINGUISHED. FIVE MINUTES LATER SAME WARNING ILLUMINATED FOR 2 SECONDS THEN WENT AWAY. OPERATIONALLY TESTED CARGO SMOKE DETECTION SYSTEM IAW CRJ AMM 26-15-00. NO DEFECTS NOTED AT THIS TIME. 2L72 4F RTA21EA 20041130001002004113000100EA 2004 11 30 COMA0460640 120041123A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A COMAK NONE O OTHER ININSP/MAINT 1 SO01442CA 7483 CABIN EMERGENCY CEILING LIGHT INOPERATIVE. REPLACED LIGHT BULB. 2L72 4F RTA21EA 20041130001012004113000101NM 2004 11 30 AALA20041160 120041123A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21603AA 27054 SFO - EMERGENCY AISLE LIGHTS FROM ROW 26 AFT OF CABIN INOPERATIVE. REPLACED MODULE M1801 AND BATTERY PACK FOR EMERGENCY AISLE LIGHTS FROM ROW 26 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041130001022004113000102NM 2004 11 30 AALA20041156 120041122A33506011779 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219630A 53561 BNA - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20041130001042004113000104EA 2004 11 30 COMA0460639 120041123A490038004883 APU CNDAIRCL600 CL6002B19 1900309EA AFT BAY ODOR A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01989CA5829 7215 FLIGHT 5397 AFTER TAKEOFF FROM CVG NOTICED OIL ODOR IN COCKPIT. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE APU. 2L72 4F RTA21EA 20041130001082004113000108NM 2004 11 30 DL738041032 120041112A2910S332A21019 FITTING BOEING737 737832 13844CFNM CFMINTCFM567CFM567B2US 13802NE A-HYD LINE BROKEN A DALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27380DA 30266 876561 ON TAXI OUT ENG NR 1 A-HYD PUMP FAILED. REPLACED SUPPLY HOSE. 2L72 4F4 FRTA16WE E2GL 20041130001112004113000111NM 2004 11 30 DL76L041035 120041115A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27191DN 28448 ON TAKEOFF NOTICED AN ELECTRICAL ODOR INSIDE THE CABIN AROUND THE WING AREA. SHORTLY AFTER THE ODOR DISSIPATED AND WAS FINE THE REST OF THE FLIGHT. INSPECTED AIRCRAFT AND SYSTEMS. UNABLE TO DUPLICATE. 2L72 4F RTA1NM 20041130001132004113000113SO 2004 11 30 RAIA00411017 120041116A34110856NF PITOT TUBE EMB 145 EMB145 3260210SO NR 3 INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03826HK7131 145016 STL - PITOT 3 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 3 PITOT PROBE. 2L72 4F RTT00011AT 20041130001162004113000116EA 2004 11 30 SWIA200414073 120041106A2750 CONTROL LEVER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07961SW 7857 AFTER LANDING CHECK FLAPS FAIL CAUTION AFTER RETRACTING TO 30 DEGREES. REPLACED FLAP CONTROL LEVER, OPERATIONAL CHECKED GOOD. P/N OFF 292-65253-1, S/N OFF 592. 2L72 4F RTA21EA 20041130001172004113000117EA 2004 11 30 SWIA200414074 120041108A27515913164 DETECTOR CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07713SK 10174 FLAPS HALF SPEED MESSAGE WITH FLAPS AT 0. REMOVED AND REPLACED RIGHT HAND OUTBOARD FLAP SKEW DETECTOR IAW 27-52-45. OPERATIONAL CHECK GOOD. P/N: 5913164, S/N OFF: A1172. 2L72 4F RTA21EA 20041130001182004113000118EU 2004 11 30 AWXA200401295 120041023A5315D5347217220390 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 67+11 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT AT FR 67+11 INCHES; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130001212004113000121NM 2004 11 30 F3LA200400115 120041122A5315 FLOORBEAM BOEING737 7373M8 1384615NM FUSELAGE DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 1637 25039 DURING C-6 CHECK, INSPECTION REPORTED FLOORBEAM WEB AT STA 294 DAMAGED FROM ELEVATOR CABLE. INSTALLED REPAIR PER EA B3-53R-10584 ON WEB OF FLOORBEAM AT STA 294. 2L72 4F RTA16WE 20041130001222004113000122SO 2004 11 30 RAIA00411009 120041110A7603 SWITCH EMB 145 EMB145LR 3260212SO THRUST LEVER DIRTY A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03829HK 145281 PIT- SPEED BRAKE DISAGREE MESSAGE. MAINTENANCE CLEANED THRUST LEVER SWITCHES, PERFORMED HIGH SPEED TAXI AND FUNCTIONAL TEST OF SPOILER/SPEED BRAKE SYSTEM. 2L72 4T RTT00011AT 20041130001232004113000123 2004 11 30 RAIA00411010 420041110A3418C850176 SENSOR JETAIRJETSTMJETSTM4101 1500501EU AOA FAILED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03572HK15202 41091 BWI- RIGHT STALL LIGHT ILLUMINATED DURING TAXI. MAINTENANCE REMOVED AND REPLACED AOA SENSOR. 2L72 4T RTA41NM 20041130001252004113000125EU 2004 11 30 RAIA00411012 120041111A6120 BETA SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT BETA SYSTEM FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03562HK 41078 PIT- LEFT BETA LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE CLEANED AND SWAPPED BETA SWITCHES. 2L72 4T RTA41NM 20041130001262004113000126EA 2004 11 30 QXEA200400783 120041119A5280 DOOR CNDAIRCL600 CL6002C10 1390015EA NR 2 DEPARTED A QXEAO OTHER D INFLIGHT SEPARATION CLCLIMB 1 NM09612QX 10042 THE NR 2 INBOARD GEAR DOOR BROKE OFF DURING CLIMBOUT OF MFR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE INBOARD DOOR MISSING, AND THE CONNECTING ROD BROKEN OFF AT THE MOUNT BOLT. DAMAGE TO THE INBOARD FLAP WAS ALSO FOUND. MAINTENANCE REMOVED THE REMAINDER OF THE INBOARD DOOR AND PLACED ON RSI. 2L72 4F RTA21EA 20041130001302004113000130SO 2004 11 30 SWIA200414064 120041105A5210 ROLLER EMB 120 EMB120ER 3260203SO PAX DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07197SW 120186 MAIN CABIN DOOR IS HARD TO OPEN/CLOSE. CLEANED MAIN CABIN DOOR ROLLERS AND ACTUATORS. RELUBED ROLLERS AND LOCKING MECHANISM. OPERATIONAL CHECK GOOD IAW 52-00-00. 2L72 4T RTA31SO 20041130001332004113000133EA 2004 11 30 COMA0460627 120041116A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01962CA6789 7123 FLT 5497 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20041130001362004113000136EA 2004 11 30 COMA0460628 120041121A339764643 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA CABIN FAULTY A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01735CA 7267 FLIGHT 5906 FLOOR EMERGENCY LIGHTING FROM ROW 2 THROUGH 5 INOPERATIVE. REPLACED DEFECTIVE EMERGENCY LIGHTING STRIP. 2L72 4F RTA21EA 20041130001402004113000140EA 2004 11 30 COMA0460629 120041117A3297 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA ANTI-SKID SYSTEMDAMAGED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01975CA 7150 FLIGHT 5806 RECEIVED AN ANTI-SKID CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT OUTBOARD ANTI-SKID DETECTOR WIRING HARNESS. 2L72 4F RTA21EA 20041130001412004113000141EA 2004 11 30 COMA0460630 120041119A3030 SENSOR CNDAIRCL600 CL6002B19 1900309EA AOA HEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01924CA 7026 FLIGHT 5092 RECEIVED A RIGHT AOA HEAT CAUTION MESSAGE DURING CLIMBOUT OF CVG. AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. PERFORMED SYSTEM RESET. 2L72 4F RTA21EA 20041130001442004113000144EA 2004 11 30 MASA200400442 120040808A3411 PITOT LINE CNDAIRCL600 CL6002D24 1390016EA PITOT/STATIC SYSOBSTRUCTED A MASAO OTHER P NO WARNING INDICATION TOTAKEOFF 1 SW07911FJ 15011 CREW REPORTED THE COPILOT AIRSPEED INOP ON TAKEOFF ROLL. MX CYCLED THE SYSTEM AND CLEARED DEBRIS FROM THE PITOT STATIC SYSTEM AND DID A BITE CHECK THE ADC. OPS CHECKED GOOD. 2L72 4F RTA21EA 20041130001452004113000145EA 2004 11 30 MASA200400555 120041001A3350110049 CHARGER CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07514MJ 10116 CAPTAIN REPORTED EMERGENCY EXIT LIGHTS INOPERATIVE AT FORWARD CLOSET DOORS. THE AIRCRAFT WAS FERRIED TO DEN WHEN MX IS CURRENTLY TROUBLESHOOTING THE MALFUNCTION. 10/3/04 MAINTENANCE REMOVED AND REPLACED BATTERY PACK P/N 2013-1A AND BATTERY CHARGER P/N 11-0049 AND REMOVED DEBRIS FROM SERVICE DOOR FLOOD LIGHT. 2L72 4F RTA21EA 20041130001462004113000146 2004 11 30 MASA200400575 420041010A3420HG2010AC02 AHRS EMB 145 EMB145LR 3260212SO NR 1 MALFUNCTIONED A MASAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 SW07831MJ8959 145273 RETURNED TO THE FIELD DUE TO AN AHRS 1 FAIL IN FLIGHT. MAINTENANCE IS TROUBLESHOOTING AT THIS TIME. 10/10 MAINTENANCE REPLACED THE NR 1 ATTITUDE AND HEADING COMPUTER, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041130001472004113000147 2004 11 30 MASA200400583 420041016A3417 ADC CNDAIRCL600 CL6002B19 1900309EA NR 1 FAILED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07571ML 7209 ADC 1 FAILURE IN FLIGHT WITH ASSOCIATED WINDSHEAR. THE CAPTAIN DECLARED AN EMERGENCY DUE TO REPORTED WINDSHEAR IN STL. RESET SYSTEM IAW FIM. OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20041130001482004113000148EA 2004 11 30 MASA200400630 120041109A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777195 7195 REPORTED THE FORWARD FLOOR PATH LIGHTING INOP. MAINTENANCE IN PHL SECURED A LOOSE CONNECTOR ON THE PATH LIGHT STRIP. OPS CHECKED GOOD. 2L72 4F RTA21EA 20041130001492004113000149EA 2004 11 30 MASA200400634 120041112A335020131A BATTERY PACK CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07921FJ 15021 THE PRIOR CREW LEFT THE EMERGENCY LIGHTS ON. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD. 2L72 4F RTA21EA 20041130001542004113000154NM 2004 11 30 2004UALA01049 120041112A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME INBOARD FLANGE DENTED AT STA 1520 ABOVE STR 26L. TYPICAL CARGO PIT DENT DAMAGE DUE TO CARGO LOADING. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001552004113000155NM 2004 11 30 2004UALA01136 120041117A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETERIORATED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29571UA 26681 EMERGENCY EVACUATION LIGHT STRIP AT LAV AREA DETERIORATED. REPLACED LIGHT STRIP. 2L72 4F4 FRTA2NM E17NE 20041130001562004113000156NM 2004 11 30 2004UALA01145 120041118A5310 TEAR STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 AFT PIT TEAR STRAP EXFOLIATED FWD AND AFT SIDE OF STA 1400 BETWEEN STR 27L AND 28L. SPLICE STRAP REPLACED. 2L72 4F4 FRTA2NM E17NE 20041130001572004113000157NM 2004 11 30 2004UALA01134 120041112A5312 BULKHEAD BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29912UA 25290 STATION 178 FWD BULKHEAD IS DAMAGED. ACCOMPLISHED ULTRASONIC INSPECTION ALONG THE STIFFENER AT WATER LINE 195 FROM THE AFT SIDE OF THE WEB. REPLACED BS 178 BULKHEAD WEB. 2L72 4F4 FRTA16WE E2GL 20041130001582004113000158 2004 11 30 SWIA200414124 420041119A34183995100208 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07437SW8621 8621 7564 STALL FAIL MESSAGE ON TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT, OPERATIONAL CHECK GOOD IAW CRJ 27-34-00. 2L72 4F RTA21EA 20041130001592004113000159SO 2004 11 30 SWIA200414146 120041005A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 INTERCOSTAL CORRODED AT FRAME 38 ON RIGHT SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW SRM 51-25-00, 51-40-02, AND 51-40-05. 2L72 4T RTA31SO 20041130001632004113000163EU 2004 11 30 MALA040683 120040929A3350 LIGHT SAAB SF340 340B 7860101EU EMERGENCY EXIT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY EXIT LIGHT AFT OF OVERWING EXIT INOP. MAINTENANCE REPAIRED WIRE IAW SAAB WM 33-50-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041130001652004113000165EU 2004 11 30 MALA040682 120040929A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, SEVERAL DENTS AFT OF RT ICE SHIELD BETWEEN SL 1536 & SL 1534. REPAIRED IAW MESABA EO S530005. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041130001662004113000166NM 2004 11 30 AALA20041158 120041123A3350 LIGHT BOEING767 767323 1385205NM COCKPIT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21397AN 29604 ORD - COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR COCKPIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041130001682004113000168NM 2004 11 30 2004UALA01050 120041112A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME INNER FLANGE DENTED AT BS 1440 INBOARD OF STR 26L. TYPICAL CARGO PIT DENT DAMAGE. INSTALLED J ANGLE REPAIRS. 2L72 4F4 FRTA2NM E17NE 20041130001702004113000170NM 2004 11 30 2004UALA01052 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME DENTED AT STA 1540 BETWEEN STRINGERS 25L & 26L. INSTALLED NESTED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001712004113000171NM 2004 11 30 2004UALA01053 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME DENTED AT STA 1600 ABOVE STR S25L. INSTALLED NESTED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001732004113000173NM 2004 11 30 2004UALA01055 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME INNER FLANGE DENTED AT BS 1400 ABOVE STR 26L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001742004113000174NM 2004 11 30 2004UALA01056 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME INNER FLANGE DENTED AT BS 1320 ABOVE STR 26R. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001762004113000176NM 2004 11 30 2004UALA01123 120041114A5310 BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR SILL CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29903UA 25003 AFT CARGO DOOR LWR SILL BEAM UPPER WEB HAS CORROSION. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED WEB. 2L72 4F4 FRTA16WE E2GL 20041130001772004113000177NM 2004 11 30 2004UALA01124 120041115A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29903UA 25003 STA 986 FRAME I/B FLANGE HAS AN ELONGATED FASTENER HOLE AT WL 206. INSTALLED ANGLE DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20041130001812004113000181NM 2004 11 30 2004UALA01128 120041116A3397 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHTSFAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29342UA 24246 EEL LIGHTS INOPERATIVE FROM SEATS 17 TO AFT GALLEY. REPLACED FLOOR FEEDER CABLE FOR EEL LTS FROM ROW 17 BACK. 2L72 4F4 FRTA16WE E2GL 20041130001842004113000184NM 2004 11 30 2004UALA01135 120041117A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FRAME CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 BS 1400 AFT PIT FRAME SHEAR TIE CORRODED BETWEEN STR 27L & 28L. DAMAGE CAUSED BY CORROSION. REPLACED FRAME SECTION AND CORRODED SHEAR TIES. 2L72 4F4 FRTA2NM E17NE 20041130001852004113000185NM 2004 11 30 2004UALA01058 120041114A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT STA 1400 BETWEEN STR 29L AND 30L SHEAR TIE CRACKED. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20041130001872004113000187NM 2004 11 30 2004UALA01059 120041114A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 AFT PIT STA 1440 FRAME DENTED AT STR 25L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001902004113000190NM 2004 11 30 2004UALA01062 120041115A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 STA 365 RBL 58 TO 63 FLOORBEAM CORRODED. REMOVED CORROSION AND INSTALLED REPAIR TO FLOORBEAM. 2L72 4F4 FRTA2NM E17NE 20041130001912004113000191NM 2004 11 30 2004UALA01063 120041115A5320 INTERCOSTAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 AFT CARGO PIT STA 1620 RBL 3 INTERCOSTAL WEB HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED NEW INTERCOSTAL WEB. 2L72 4F4 FRTA2NM E17NE 20041130001922004113000192NM 2004 11 30 2004UALA01064 120041115A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 MAIN CABIN STA 365 FLOORBEAM CORRODED FROM RBL 26 TO RBL 0. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM. 2L72 4F4 FRTA2NM E17NE 20041130001932004113000193NM 2004 11 30 2004UALA01065 120041115A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 MAIN CABIN STA 324 RS FLOORBEAM CORRODED FROM RBL 40 TO CUSP. REMOVED CORROSION DAMAGE AND INSTALLED FLOORBEAM REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001942004113000194NM 2004 11 30 2004UALA01129 120041116A2781 WARNING LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLATS ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29676UA 30028 RETURNED TO ORD DUE TO LEADING EDGE SLAT INDICATION. REPLACED THE S282, AND S297 SWITCHES. SYSTEM OPS CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20041130001952004113000195NM 2004 11 30 2004UALA01066 120041114A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 EXTERIOR FUSELAGE SKIN AT STA 620 ABOVE STR 16L HAS 2 EACH DENTS. REMOVED EXISTING SKIN REPAIRS. REMOVED PORTION OF DAMAGED SKIN PANEL. ACCOMPLISHED A PARTIAL SKIN PANEL REPLACEMENT. SKIN PANEL SPLICED BY DOUBLER STRAPS AND TRIPLERS. 2L72 4F4 FRTA2NM E17NE 20041130001972004113000197NM 2004 11 30 2004UALA01108 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME DENTED AT RT SIDE BETWEEN STRINGERS S25R & S26R. REMOVED DAMAGED FRAME CAP AND INSTALLED NESTED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001982004113000198NM 2004 11 30 2004UALA01109 120041112A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME DENTED AT STA 1420 BETWEEN STRINGERS 25L & 26L. TYPICAL CARGO PIT DENT DAMAGE DUE TO CARGO LOADING. REMOVED DAMAGED FRAME CAP AND INSTALLED NESTED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130002002004113000200NM 2004 11 30 2004UALA01111 120041114A5315 FLOORBEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29903UA 25003 STA 986 FLOOR BEAM UPR CAP HAS CORROSION AT RBL 16 . SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. SPLICED UPR T-CAP SECTION AT STA 986 FROM RBL 24 TO LBL 65. 2L72 4F4 FRTA16WE E2GL 20041130002032004113000203EU 2004 11 30 YENA200456 120041124A27519028A000401 POSITION SENSOR AIRBUS320 A320232 3930326EU TE FLAPS FAILED A YENAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 EA15556JB 1904 FLIGHT CONTROL FLAPS FAULT AT FLAPS 2 190 KNOTS. FLAPS DID NOT EXTEND TO POS 2. SLATS EXTENDED NORMALLY. FOLLOWED ECAM AND RECYCLED FLAPS, EXTENDED NORMAL. REMOVED AND REPLACED RT (PPU) POSITION PICK OFF UNIT IAW 27-51-18. 2L72 4F RTA28NM 20041130002052004113000205EA 2004 11 30 SWIA200414128 120041120A2780766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07705SK 10145 SLATS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED NR 1 SFECU IAW CRJ700 MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130002072004113000207EA 2004 11 30 SWIA200414130 120041121A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MOTOR MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07928SW 7701 STAB CHANNEL 2 STATUS MESSAGE WILL NOT CLEAR. INSTALLED SERVICEABLE MOTOR CONTROL UNIT IAW CRJ 200 MM 27-42-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130002092004113000209SO 2004 11 30 SWIA200414132 120041122A2750 FCU EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM0758733 120197 RECEIVED FLAP CONTROL FAULT MESSAGE WHEN SELECTING FLAPS 15. REMOVED AND REPLACED FCU AND LEFT NACELLE ACTUATOR. REFERENCES A/C MM (27-50-08) (27-50-06) OPERATIONAL CHECK GOOD. P/N 347200-1001, S/N OFF 3039, P/N 308200-1007, S/N OFF 016. 2L72 4T RTA31SO 20041130002172004113000217NM 2004 11 30 AWXA200401276 120041112A3350321454 POWER SUPPLY AIRBUSA319 A319132 3930340NM ZONE 242 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28829AW4968538025 1563 ATL - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041130002192004113000219EU 2004 11 30 AWXA200401278 120041112A2421766219 IDG AIRBUS320 A320231 3930325EU NR 1 ENGINE FAILED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 WP28631AW223185047 077 3 SHARP JOLTS OCCURRED IN YAW APPROX 45 SEC TO 1 MIN APART. AFTER 2ND JOLT RECEIVED ECAM INDICATION NR 1 GEN FAULT, AFTER 3RD JOLT ECAM INDICATED AUTO/FLT YAW DAMP NR 1 INOP, DIVERTED, LANDED W/O EVENT. MX ISSUED MELS. YAW DAMP NR 1 INOP. NR 1 IDG INOP. MX INSPECTED NR 1 GEN FEEDER CABLES FOR POSSIBLE ARCING, NO DEFECTS NOTED. R & R NR 1 ENG IDG. FOUND APU GEN SWITCH NOT LATCHING, REPLACED PUSH BUTTON SWITCH PER ESPM, OPS CK GOOD. IDG CONFIRMED REASON FOR REMOVAL. TEARDOWN OF UNIT FOUND GENERATOR MAIN STATOR WINDING SHORTED WITH A HOLE BLOWN THROUGH IT, THIS CONDITION WOULD CERTAINLY RESULT IN AN OFF LINE TRIP, REMOVED AN REPLACED GENERATOR MAIN STATOR. 2L72 4F RTA28NM 20041130002202004113000220EU 2004 11 30 AWXA200401279 120041113A2133VFT300A1 OUTFLOW VALVE AIRBUS320 A320231 3930325EU ZONE 126 INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28631AW44263180 077 ON TAKEOFF, WHEN APPROACHING V1 UPPER ECAM INDICATED VENT SKIN VALVE FAULT. FOLLOWED ECAM INSTRUCTIONS, AIRCRAFT WOULD NOT PRESSURIZE, TURNED BACK TO STL AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED SKIN AIR VALVE IAW T/C R2A21301, OPERATIONAL CHECK WAS GOOD. TEST OF OUTFLOW VALVE INITIALLY TESTED GOOD, ACTUATOR REMOVED OFF VALVE AND ALSO TESTED GOOD. UNIT RE-ASSEMBLED & CYCLED APPROXIMATELY 30 TIMES WHEN VALVE FINALLY FAILED TO CLOSE. ACTUATOR MOTOR DISASSEMBLED & ARMATURE CHECKED, 1 WINDING OPEN AND ALL OTHER ON DRIVE END MEASURED 4.7 OHMS INSTEAD OF 5.6 OHMS. REPLACED ACTUATOR & OVERHAULED VALVE IAW CMM. 2L72 4F RTA28NM 20041130002212004113000221EU 2004 11 30 AWXA200401280 120041023A5321D5348015900500 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON GIRT BAR FLOOR PLATE AT R-2 DOOR ENTRY WAY FR 68. MAINTENANCE REMOVED CORRODED GIRT BAR FLOOR PLATE AT FR 68; INSTALLED NEW REPLACEMENT FLOOR PLATE IAW T/C C1D25310. 2L72 4F RTA28NM 20041130002222004113000222EA 2004 11 30 SWIA200414054 120041030A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 280 LT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-00, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041130002232004113000223EA 2004 11 30 SWIA200414055 120041030A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INBOARD AND OUTBOARD ANGLES REMOVED IAW CRJ SRM 51-40-11, ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041130002242004113000224EA 2004 11 30 SWIA200414056 120041030A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAJ DUMP FUEL O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 484.0 LEFT HAND INTERCOSTAL OUTBOARD FLANGE LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A" . 2L72 4F RTA21EA 20041130002492004113000249WP 2004 11 30 AALA20041131 120041113A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21407AA 49318 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 18D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041130002512004113000251EA 2004 11 30 MASA200400619 120041101A5101 UNKNOWN CNDAIRCL600 CL6002D24 1390016EA BIRD STRIKE A MASAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW07914FJ 15014 REJECTED TAKEOFF DUE TO BIRD STRIKE. MAINTENANCE C/W INSPECTION AND FOUND NO DAMAGE. 2L72 4F RTA21EA 20041130002522004113000252NM 2004 11 30 AWXA200401301 120041116A213340631997201AA OUTFLOW VALVE BOEING737 7373U3 13844CCNM CABIN PRESSURE FLUCTUATES A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28335AW4239 28740 CABIN PRESSURE FLUCTUATED AT ALL ALTITUDES, CABIN CLIMBS & DESCENDS 4000 PSI, DIVERTED FOR REPAIR. MX TROUBLESHOT CABIN PRESSURE SYS & REPLACED AFT OUTFLOW VALVE. AFTER INSTALL OF NEW OUTFLOW VALVE A NEW FAULT OCCURRED, CABIN PRESSURE CONTROL INOP IN AUTO. MX ISSUED MEL 21-14. AUTO CABIN PRESSURE SYS INOP & MX FERRIED ACRFT. MX REPLACED AFT OUTFLOW VALVE IAW BMM, OPS CHK GOOD. CONFIRMED REASON FOR REMOVAL, UNIT FAILED PARA 7 BONDING RESISTANCE CHK. CLEANED MATING SURFACE FOR EBOX 2 & REACCOMPLISHED TEST, UNIT PASSED PER CMM. FUNCTIONAL TEST OF OUTFLOW VALVE ALSO FAILED EBOX TESTING. EBOX 1, C2 (CAPACITOR) FOUND LEAKING ON POWER SUPPLY BOARD, CAPACITOR REPLACED & BOARD CLEANED. 2L72 4F RTA16WE 20041201000012004120100001NM 2004 12 1 DL73S041055 120041120A5330 SKIN BOEING737 737232 1384475NM S-18L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27326DL 23098 A 1.5 INCH CRACK WAS FOUND IN THE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18L AT FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 095229-14AD. 2L72 4F RTA16WE 20041201000022004120100002NM 2004 12 1 DLM88041049 120041120A5330591140659 SKIN DOUG MD88 MD88 3023688NM FUSLEAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27908DE 53417 FUSELAGE SKIN PREVIOUSLY DAMAGED AT STA 228 BETWEEN L-17L AND 18L. PERMANENT REPAIR INSTALLED PER ERA 382691-14 REV B. 2L72 4F RTA6WE 20041201000032004120100003EU 2004 12 1 AWXA200401302 120041117A3397ABS0374A24 TERMINAL AIRBUS320 A320231 3930325EU SEAT ROW 11 RT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28626AW 65 PHX - EEL - DURING 4-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 11 RT. MAINTENANCE REPLACED TERMINAL 10N EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041201000062004120100006NM 2004 12 1 DL73S041039 120041117A53306545768307 SKIN BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 FUSELAGE SKIN DAMAGED AT THE C1 DOOR CUTOUT AT STATION 440 AND STR 23R - 24R. REPAIRED IAW ERA 257313-14 REV E. 2L72 4F A16WE 20041201000072004120100007 2004 12 1 DL75K041040 420041118A2565D31393107 SLIDE BOEING757 757232 1384965NM LEFT WING LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO27698DL 29911 THE LEFT HAND WING SLIDE WAS FOUND TO BE PARTIALLY UNPACKED WHEN THE SLIDE ACCESS DOOR WAS OPENED FOR R/R OF THE SLIDE. REPLACED SAME. 2L72 4F RTA2NM 20041201000092004120100009EA 2004 12 1 SWIA200414116 120041116A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA FLT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07442SW 7609 TRIED TO DEPLOY FLIGHT SPOILERS IN FLIGHT. ONLY THE LEFT SIDE DEPLOYED. RIGHT SIDE CAUTION MESSAGE APPEARED. THE AIRCRAFT TURNED HARD TO THE LEFT. RETRACTED THE SPOILERS AND THE AIRCRAFT THEN TURNED NORMAL. REMOVED AND REPLACED INBOARD (RIGHT) FLIGHT SPOILER IAW AMM 27-62-01. REMOVED AND REPLACED SECU NR 2 IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF MAL 5175, P/N OFF 49-164-05, S/N OFF 01466. 2L72 4F RTA21EA 20041201000112004120100011EU 2004 12 1 AWXA200401322 120041106A5755D5755103920051 BOLT AIRBUS320 A320232 3930326EU SPOILER HINGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - FLIGHT CONTROL - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON NR 4 SPOILER HINGE BOLTS WS 924 AND WS 970 LT. MAINTENANCE REMOVED AND REPLACED NR 4 SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-44-020-050-B, AND SUBTASK 27-64-44-420-050-B. 2L72 4F RTA28NM 20041201000122004120100012EU 2004 12 1 AWXA200401323 120041116A5755D5755103920051 BOLT AIRBUS320 A320232 3930326EU SPOILER HINGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - FLIGHT CONTROL - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON NR 4 SPOILER HINGE BOLTS WS 924 AND WS 970 RT. MAINTENANCE REMOVED AND REPLACED NR 4 RT SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-44-020-050-B, AND SUBTASK 27-64-44-420-050-B. 2L72 4F RTA28NM 20041201000142004120100014SO 2004 12 1 MASA200400622 120041103A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07841MJ 145448 EMERGENCY OVERWING EXIT SIGN INOP. MAINTENANCE RESEATED THE CONNECTOR AND THE LIGHT WORKED. 2L72 4T RTT00011AT 20041201000152004120100015SO 2004 12 1 MASA200400623 120041103A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 EMERGENCY EXIT FLOOR LIGHTING AFT HALF INOP. MAINTENANCE RESET THE LIGHT. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041201000162004120100016NE 2004 12 1 ARWA20041004 220041022A7230 COMPRESSOR DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 3 ENGINE STALLED A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19791AL 46150 671299 REJECTED TAKEOFF AT 60 KTS DUE COMPRESSOR STALL NR 3 ENGINE. INSPECTED ENGINE INLET AND EXAUST, NO DEFECTS FOUND. ENGINE RUN UP C/W IN ACCORDANCE WITH MM 71-00. UNABLE TO DUPLICATE PROBLEM. OK FOR SERVICE. 2L74 4F4 F 4A25 1E8 20041201000172004120100017NM 2004 12 1 2004UALA01146 120041118A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 AFT PIT STA 1340 FRAME DENTED AT STR 25R. TYPICAL AFT PIT FRAME DENT DAMAGE DUE TO CARGO LOADING. FRAME CAP REPAIRED USING "J" ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041201000192004120100019SO 2004 12 1 SWIA200414125 120041120A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07585SW1080310803 120353 NACELLES ARE VERY SLOW TO RETRACT CAUSING A DISAGREEMENT ON THE COMPUTER. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-03. OPS CHECK GOOD. 2L72 4T RTA31SO 20041201000202004120100020 2004 12 1 SWIA200414126 420041118A22166225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER STUCK A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07565SW1062510625 120340 DISENGAGED AP WITH BALL CENTERED DURING A DESCENT AND RUDDER WAS JAMMED. SHORTLY AFTER SOMETHING LET LOOSE AND PROBLEM WAS CORRECTED. REPLACED RUDDER SERVO IAW AMM 27-11-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041201000212004120100021EA 2004 12 1 SWIA200414127 120041115A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07946SW2038 2038 7776 STAB TRIM CH 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU WITH SERVICEABLE UNIT PER CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD. P/N 7060-9, S/N ON 1407, S/N OFF 846. 2L72 4F RTA21EA 20041201000222004120100022SO 2004 12 1 MASA200400585 120041018A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07843MJ 145478 EMERGENCY LIGHT ABOVE THE FLIGHT DECK WAS INOP. MAINTENANCE RELAMPED AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20041201000232004120100023EA 2004 12 1 MASA200400586 120041018A3397 CONNECTOR CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07905J 15005 CREW REPORTED THE CEILING LIGHT 3RD ROW FLOODLIGHT INOP. MAINTENANCE PLACED THE ITEM ON MEL. 10/18/04 MAINTENANCE RE-INSTALLED CONNECTOR AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20041201000242004120100024SO 2004 12 1 MASA200400591 120041020A3350 LIGHT EMB 145 EMB145LR 3260212SO SEAT 12A INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 EMERGENCY LIGHT 12A INOP. MX CYCLED POWER TO THE LIGHT AND IT OPERATED NORMALLY. 2L72 4T RTT00011AT 20041201000252004120100025SO 2004 12 1 MASA200400594 120041020A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 EMERGENCY EXIT SIGN AT ROW 12 WOULD NOT ILLUMINATE. MAINTENANCE SECURED THE ELECTRICAL CONNECTION, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041201000262004120100026EA 2004 12 1 MASA200400596 120041023A3350 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSTRIPPED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717175 7175 EMERGENCY LIGHTS CAME ON IN FLIGHT WITH SWITCH IN ARMED POSITION. MX FOUND CIRCUIT BREAKER POPPED AND RESET. OPS CHECKED GOOD. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20040802000112004080200011EA 2004 8 2 ASOA04061 120040124A5210601R3176541 LATCH CNDAIRCL600 CL6002C10 1390015EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27705EV 10051 FLT 4195 - DURING A GROUND INSPECTION IN DFW, THE INSIDE PASSENGER DOOR HANDLE WAS FOUND STUCK WHEN ATTEMPTING TO UNLOCK THE DOOR FROM THE INSIDE. MAINTENANCE CLEANED, ADJUSTED AND LUBRICATED THE PASSENGER DOOR LATCH ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802000122004080200012EA 2004 8 2 ASOA04060 120040122A5210601R3198075 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27702EV 10035 DURING A C-CHECK IN MCN, THE TOP PASSENGER DOOR STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP PASSENGER DOOR STEP. (M) 2L72 4F RTA21EA 20040802000312004080200031WP 2004 8 2 GTIA040595 120040530A5313 LONGERON DOUG DC9 DC983 3022083WP CHAFED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FTW - FOUND LONGERON 8R AT FS 1280-1401 IN AFT ACC COMP CHAFED. REMOVED SECTION OF LONGERON FROM STATION 1391-1427. LOCATED AND DRILLED NEW SECTION AND ONE SPLICE. INSTALLED NEW SECTION LONGERON AND SPLICE. (M) 2L72 4F RTA6WE 20040802000362004080200036WP 2004 8 2 GTIA040606 120040614A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 1287-1309 BROKEN EDGES. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040802000412004080200041EU 2004 8 2 USAA04344 120040610A5320D5311146020201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19709UW16153 0997 BFM - FOUND CORROSION ON FLOOR SUPPORT, 1 INCH BY .90 INCH BY .040 INCH. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA28NM 20040802000502004080200050NM 2004 8 2 USAASB04035 120040323A2170V1211 COALESCER BAG BOEING737 737301 1384611NM PACK BAY CONTAMINATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19584US 23743 PHL - FLT 1483 - EN ROUTE FROM BTV TO PHL, CREW REPORTED STRONG FUMES THROUGH OUT THE CABIN. MAINTENANCE CHECKED FOR LEAKS AT BOTH THE APU AND THE PACK AREA. NO LEAKS WERE NOTED. RAN ENGINES WITH BOTH PACKS ON FROM IDLE TO TAKEOFF POWER. NO FUMES NOTED. RAN APU AND CHECKED INTAKE, EXHAUST AND BLEED. NO ODOR OR SMELL NOTED IN CABIN OR COCKPIT. CONDITION COULD NOT BE DUPLICATED. THE PACK WATER SEPARATOR BAGS WERE REPLACED AS A PRECAUTION. (M) 2L72 4F RTA16WE 20040802000522004080200052 2004 8 2 2004F00225 420040316A25655WP230100201 SLIDE DOUG DC10 DC1030 3023501WP R1 DOOR FAILED A CLCAK NONE L NO TEST ININSP/MAINT 1 SO19279AX 47816 DURING C-CHECK AT VARIG, THE R1 DOOR SLIDE FAILED TO DEPLOY DURING ACCOMPLISHMENT OF TASK CARD 101C-002. UPON INVESTIGATION FOUND, 'TRANSPORTATION SAFETY PIN' INSTALLED WITH NO WARNING FLAG ATTACHED. REMOVED PIN, REPACKED SLIDE AND SLIDE DEPLOYMENT WAS ACCOMPLISHED NORMALLY WITHOUT INCIDENT. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M) 2L73 4F A22WE 20040802000602004080200060NM 2004 8 2 ASAA047003 120040514A3350 WIRE BOEING737 737790 13844CNNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01627AS 30794 OAK - FOUND EMERGENCY TRACK LIGHTING INOPERATIVE, FIRST 3 ROWS. RECONNECTED EMERGENCY TRACK LIGHTING, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040802000622004080200062NM 2004 8 2 USAASB04077 120040625A3260189929 UPLOCK SENSOR BOEING737 7373B7 1384580NM RT MLG MALFUNCTIONED A USAAO OTHER N FALSE WARNING CLCLIMB 1 EA19385US 22958 AFTER TAKEOFF FROM GSO, CREW RECEIVED A RIGHT MLG RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW LOWERED GEAR PER QUICK REF HANDBOOK PROCEDURES AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS AND NO RED LIGHTS. FLIGHT LANDED WITHOUT INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE S74 RIGHT MLG UPLOCK SENSOR PER MM 32-61-21. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040802000642004080200064NM 2004 8 2 USAASB04079 120040623A274169732013 SPROCKET BOEING737 737301 1384611NM STAB TRIM FAILED A USAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA19574US 23739 CLT - FLT 895 - ON 10 MILE FINAL INTO CLT FROM SAV, AT 190 KNOTS, CREW REPORTED THE STABILIZER JAMMED. BOTH PILOTS' MANUALLY TRIMMED AIRCRAFT BUT COULD NOT BREAK THE JAM. AIRCRAFT LANDED AT CLT WITH FLAPS 15 PER QUICK REFERENCE HANDBOOK. MAINTENANCE REMOVED AND REPLACED THE STABILIZER TRIM MECHANISM SPROCKET PER MM 27-41-41. ALSO, REMOVED AND REPLACED THE STABILIZER TRIM CONTROL BEARINGS AND SHAFT PER EO 2700V225. OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 20040802000732004080200073NM 2004 8 2 USAA040289 120040609A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US43568 23885 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 727D STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 231. (M) 2L72 4F RTA16WE 20040802000772004080200077NM 2004 8 2 2004F00209 120040109A3350 LIGHT BOEING737 7378Q8 13844BXNM RT OVERWING DOORFAILED A MYWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO19734MA 30039 ON DEPARTURE OUT OF OAK ABORTED TAKEOFF AT 40 KNTS. RIGHT OVERWING DOOR LIGHT ILLUMINATED WHEN TAKEOFF POWER WAS APPLIED. TROUBLESHOT SYSTEM PERFORMED VISUAL INSPECTION OF BOTH OVERWING EXIT DOORS AND FOUND NO DISCREPANCIES. RESET BOTH FORWARD AND AFT RIGHT OVERWING EXIT DOORS. PERFORMED BITE TEST OF PSEU IAW 52-20. RESET PSEU. SYSTEM OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040802000852004080200085 2004 8 2 GTIA040632 420040628A2565 SLIDE DOUG DC9 DC983 3022083WP GIRT BAR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23832NK 49618 FORWARD L1 DOOR SLIDE PACK LANYARD CAME OFF GIRT BAR. REINSTALLED FORWARD L1 SLIDE PACK LANYARD. (M) 2L72 4F RTA6WE 20040802000882004080200088NM 2004 8 2 USAA040307 120040609A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU60209 22192 CLT - FOUND SKIN CORRODED 8 INCHES BY 10 INCHES, STATION 610 BETWEEN S29L-S28L. SURFACE CORROSION REMOVED, ALODINED AND ANTENNA REINSTALLED PER SRM 53-30-01 AND 53-10-02-01. (M) 2L72 4F RTA2NM 20040802000932004080200093NM 2004 8 2 USAA040306 120040609A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU60209 22192 CLT - FOUND SKIN CORRODED 6 INCH BY 6 INCH AREA, STATION 610 AND S30 NR 2 CENTER AFT RADIO ANTENNA. LIGHT SURFACE CORROSION REMOVED, ALODINED, RE-INSTALLED PER SRM 53-30-01 AND 51-10-02-01. (M) 2L72 4F RTA2NM 20040802000992004080200099EA 2004 8 2 REXA04006 120040321A2913 O-RING CNDAIRCL600 CL6002B19 1900309EA HYD EDP LEAKING A REXAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO258390F 7390 FLT CREW RECEIVED AN AURAL OIL PRESSURE WARNING FOR THE LT ENGINE. OIL PRESSURE WAS OBSERVED TO BE FLUTUATING BETWEEN 25 TO 30 PSI. FLT CREW PERFORMED AN IN-FLT SHUTDOWN, DECLARED AN EMERGENCY AND WAS CLEARED INTO MSP. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT MSP. MX FOUND THE LT ENGINE TO BE LOW ON OIL. THE ENGINE WAS SERVICED AND A GROUND RUN LEAK CHECK WAS PERFORMED. GROUND RUN REVEALED OIL LEAK AT ENGINE DRIVEN HYDRAULIC PUMP TO ACCESSORY GEARBOX MATING FLANGE DUE TO A BROKEN O-RING. O-RING REPLACED, ENGINE TOPPED OFF WITH OIL AND ANOTHER GROUND RUN PERFORMED, WITH SATISFACTORY RESULTS. ENGINE HAS BEEN PLACED ON DAILY OIL WATCH AND CHIP DETECTOR MONITORING FOR NEXT 50 FLT HRS. (M) 2L72 4F RTA21EA 20040802001052004080200105NM 2004 8 2 C7WA200400009 120040412A5210 STRAP BOEING727 7272Q6 138407VNM FWD ENTRY DOOR CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO171279E 21971 FOUND FORWARD ENTRANCE DOOR AFT LOWER STRAP CRACKED. REPAIRED STRAP IAW B727 SRM 51-40-4. (M) 2L73 4F RTA3WE 20040802001102004080200110NM 2004 8 2 AMTA200400803 120040625A5210 STRUCTURE BOEING757 75723N 1384973NM L2 DOOR CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11517AT 27973 LIGHTING HOLE CRACKED AT L2 DOOR JUST FORWARD OF TORQUE TUBE, BEHIND DOOR ESCAPE SLIDE INDICATOR. REMOVED CRACKED WEB FOUND TO BE OUT OF LIMITS ON L2 DOOR FORWARD OF TORQUE TUBE BEHIND ESCAPE SLIDE INDICATOR. FABRICATED AND INSTALLED NEW WEB IAW SRM 51-40-2, 51-20-01 AND MM 51-21-00-7. (M) 2L72 4F RTA2NM 20040802001232004080200123WP 2004 8 2 GTIA040623 120040607A5320 ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND RIGHT MLG WW FORWARD OUTBOARD UPPER CORNER EXTRUSION ANGLE CORRODED. LOCATED AND DRILELD NEW L ANGLE. INSTALLED L ANGLE. (M) 2L72 4F RTA6WE 20040802001392004080200139EA 2004 8 2 ASOA04395 120040531A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 FLT 4123 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER FOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001432004080200143WP 2004 8 2 GTIA040566 120040610A2611 SMOKE DETECTOR DOUG DC9 DC982 3022082WP CARGO BAY MALFUNCTIONED A GTIAA UNSCHED LANDING BL SMOKE/FUMES/ODORS/SPARKS NO TEST CLCLIMB 1 GL23803NK 48087 FLL - FLT 1174 - BURNING SMELL IN CABIN TWICE ONCE AT TAKEOFF AGAIN AT 18000 FT CARGO SMOKE DETECTOR FAILED TEST FAILURE LIGHTS AND FIRE DETECTOR LOOP LGHT REMAINED ON FOR DURATION OF FLIGHT TEST OK AT GATE ON GROUND POWER. PERFORMED INSPECTION OF CARGO AREA BAYS AND CABIN AREA FOR SMOKE WITH ENG RUNNING AND PACKS ON, NO SMOKE OR SMELLS NTOED ALSO PERFORMED, OPS CHECK OF CARGO SMOKE DETECTOR SYSTEM, TEST FUNCTION OK. (M) 2L72 4F A6WE 20040802001442004080200144WP 2004 8 2 GTIA040567 120040610A3233 ACTUATOR DOUG DC9 DC983 3022083WP MLG MALFUNCTIONED A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23827NK 49793 LGA - FLT 706 - AFTER TAKEOFF, RIGHT MAIN GEAR DOOR LIGHT WOULD NOT GO OUT WITH GEAR UP. JACKED AIRCRAFT FOR THE TROUBLE SHOOTING FOUND MLG ACTUATOR SLOW TO RETRACT ON RIGHT SIDE. REMOVED AND REPLACED RT MLG ACTUATOR. PERFORMED GEAR SWING ALL LIGHTS OUT. OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20040802001492004080200149EA 2004 8 2 ASOA04409 120040604A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11867AS 7463 DURING HANGAR MAINTENANCE IN BTR, THE RIGHT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001522004080200152EU 2004 8 2 ASOA04412 120040607A3350LP1670 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11640AS 405 DURING HANGAR MAINTENANCE IN MCN, THE LAST BULB IN THE AFT END OF THE EMERGENCY FLOOR LIGHT TRACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040802001532004080200153EA 2004 8 2 ASOA04405 120040602A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR HANDLE STRUCTURE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE ASSEMBLY. (M) 2L72 4F RTA21EA 20040802001902004080200190SO 2004 8 2 SIMA200417001 120040615A33201010861 LIGHT EMB 135 EMB135KL 3260302SO PAX DOOR ODOR A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21821AE 145577 CREW REPORTED A BURNING ODOR IN AIRCRAFT. MAINTENANCE FOUND THE ODOR COMING FROM THE PASSENGER DOOR ENTRY LIGHT. LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040802001972004080200197NM 2004 8 2 AMTA200400762 120040619A2697 WIRE BOEING757 75723N 1384973NM OVERHEAT LOOP CHAFED A AMTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11515AT 27598 ON TAKEOFF ROLL, STATUS MSG LEFT ENGINE OH LP2 ILLUMINATED DISAPPEARED ON THRUST REDUCTION AND REAPPEARED DURING INITIAL CLIMB. APPROXIMATELY 9,000 AGL WITH CLIMB THRUST SET DISAPPEARED FOR REMAINDER OF CLIMB. FOUND WIRE CHAFED IN NACELLE GOING TO OVERHEAT LOOP, REPLACED WIRE 'D' BETWEEN CONNECTORS D41072P AND D2 402, OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040803000012004080300001NE 2004 8 3 HXS2004F2004A 220040705A72300292005060 COMPRESSOR SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1 60030NE ENGINE FOD A HXSAO OTHER O OTHER NRNOT REPORTED 1 AL05579583952 1512 4815TEC ENGINE WAS FOUND TO HAVE INGESTED A ROCK THROUGH THE INTAKE AND DAMAGED TO INLET COMPRESSOR. FOD DAMAGE. THIS ENGINE IS TO BE SENT FOR EVALUATION AND REPAIR. 1G71 3U3 U H9EU E19EU 20040803000152004080300015EU 2004 8 3 MALA040492 120040719A33206500111 SOCKET SAAB SF340 340B 7860101EU WINDOW LIGHT BURNED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL15361PX 340B249 PRIOR TO EXTENDING GEAR ON FINAL APPROACH INTO BGM, A SMELL OF ELECTRICAL BURNING. JUST PRIOR THE F/O HAD TURNED CABIN AND FLIGHT DECK TEMP SELECTOR TO MID RANGE. MAINTENANCE FOUND WINDOW LIGHT SOCKET AT 3A BURNED. CLIPPED AND STOWED WIRES TO BURNED SOCKET. REPLACED THE SOCKETS AT 3A REPLACED HALOS P/N-6500111 AND 6500110. ALL CHECKS GOOD. REMOVED FROM DMR, MXC NOTIFIED. 2L72 4T RTA52EU 20040803000252004080300025EU 2004 8 3 AALA20040729 120040716A3350321441 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2180057 465 EMERGENCY EXIT LIGHT DID NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK FOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040803000392004080300039EU 2004 8 3 MALA040494 120040712A3230AIR124792 ATTACH BOLT SAAB SF340 340B 7860101EU RABAB BROKEN A MALAK NONE O OTHER ININSP/MAINT 1 GL15415XJ 340B415 ON WALKAROUND FOUND RABAB BOLT BROKEN OFF. MAINTENANCE REMOVED AND REPLACED RABAB BOLT P/N AIR 124792, ALL CHECKS GOOD. 2L72 4T RTA52EU 20040803000552004080300055WP 2004 8 3 AALA20040743 120040715A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 24D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21575AM 53152 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 24D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000142004080400014NM 2004 8 4 04FDEA02191 120040726A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 WHILE WORKING CARD N00533, FOUND CRACKED STRINGER AT BS 1114 STR 25 RT. *S/D* REPAIRED STRINGER 25 RT AT BS 1107-1115 PER SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20040804000242004080400024 2004 8 4 AALA20040779 420040726A2565 GIRT BAR BOEING757 757223 1384957NM L1 DOOR MISINSTALLED A AALAK NONE O OTHER ININSP/MAINT 1 SW21627AA 24585 MEX - L1 DOOR SLIDE LIGHT INOPERATIVE. REINSTALLED GIRT BAR AT L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804000302004080400030EU 2004 8 4 AALA20040763 120040725A3397 WIRE AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW2125071 514 BOS - LEFT HAND MID CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN WIRES AT FORWARD FLOOD LIGHT AT L3 DOOR. REPAIRED WIRE PER MM CHAPTER 20 FOR LEFT HAND MID CABIN EMERGENCY LIGHTS AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040804000312004080400031WP 2004 8 4 AALA20040767 120040722A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21408AA 49319 EMERGENCY LIGHT AT L2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000342004080400034NM 2004 8 4 04FDEA02281 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 32 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79806, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 32R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000402004080400040NM 2004 8 4 AALA20040756 120040720A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21956AN 30090 TUL - EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040804000432004080400043NM 2004 8 4 AALA20040777 120040726A3350 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21641AA 24599 EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. FOUND LOOSE WIRE. RESECURED LOOSE WIRE FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804000542004080400054NM 2004 8 4 04FDEA02289 120040729A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING INBOARD FLAP FLAP VANE NR 1 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLE DIAMETER FORWARD=0.748, MIDDLE=0.748, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80307, TITLE: WINGS - TE RT INBOARD FLAP VANE, NR 1 VANE TO TRACK SUPPORT CORRODED REPAIR. 2L73 4F RTA22WE 20040804000552004080400055NM 2004 8 4 04FDEA02290 120040729A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING INBOARD FLAP FLAP VANE NR 3 VANE TO TRACK SUPPORT ASSEMBLY HOLES FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. FINAL HOLE DIAMETER FORWARD=0.688, MIDDLE=0.688, AND AFT=0.748. BUSHINGS FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80308, TITLE: WINGS - TE FLAPS - RT INBOARD FLAP VANE, NR 3 VANE TO TRACK SUPPORT ASSEMBLY CORRODED. 2L73 4F RTA22WE 20040804000562004080400056NM 2004 8 4 04FDEA02291 120040729A2730 SKIN DOUG MD11 MD11 3023602NM ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT OUTBOARD ELEVATOR LOWER SURFACE STA XE 353 TO XE 372 FOUND WITH DELAMINATION APPROXIMATELY 18 INCHES IN DIAMETER. REMOVED AND REPLACED AS PER MM 27-30-30. ELEVATOR OPERATIONAL CHECK CARRIED OUT AS PER MM 27-30-00, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040804000792004080400079NM 2004 8 4 SWAA042107 120040725A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND BUTT STRAP AT BS 908, STRINGER 4R, CRACKED. REPAIRED STRAP PER SRM. 2L72 4F RTA16WE 20040804000902004080400090NM 2004 8 4 SWAA042129 120040726A555365C25879 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN BODY FITTING LUGS CORRODED. REPAIRED VERTICAL FIN PER ER. 2L72 4F RTA16WE 20040804000932004080400093NM 2004 8 4 SWAA042149 120040728A2560P4010021 BATTERY BOEING737 7377H4 1384404NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29749SW 29801 FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040804001082004080400108NM 2004 8 4 AALA20040737 120040719A3350 LIGHT BOEING757 757223 1384957NM SEAT 16D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21182AN 29592 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 16D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804001192004080400119NM 2004 8 4 SWAA042160 120040728A52306546921528 TEE FITTING BOEING737 7373L9 1384470NM FWD CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR LOWER TEE CRACKED. REMOVED AND REPLACED FWD CARGO DOOR PER MM. 2L72 4F RTA16WE 20040804001232004080400123NM 2004 8 4 04FDEA02005 120040707A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 FOUND CRACKED AT THE BOTTOM SIDE. FWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1. 2L73 4F RTA22WE 20040804001302004080400130NM 2004 8 4 04FDEA01899 120040701A5330 SKIN BOEING727 727100 1384036NM FUSELAGE BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25190FE 19083 SKIN BULGE AT BS 1180 STRINGER 26L THRU STRINGER 23L. REPAIRED AREA IAW EA 7-5330-79539. 2L73 4F RTA3WE 20040804001332004080400133NM 2004 8 4 AALA20040751 120040623A5711 SPAR BOEING767 767323 1385205NM RT WING PUNCTURED A AALAK NONE O OTHER ININSP/MAINT 1 SW21351AA 24032 AFW - RIGHT WING FORWARD SPAR PUNCTURED AT STATION 1028. AREA IS 1 INCH BY 0.125 INCH. TRIMMED OUT THE DAMAGED PORTIONS OF SPAR WEB BETWEEN FSS 1022 AND 1032 AND SPLICED IN A NEW WEB SEGMENT FABRICATED FROM 0.140 INCH THINK 2024T3 ALUMINUM. TWO 0.080 INCH THICK 2024T3 SPLICE PLATES ARE INSTALLED AT EACH SPLICE LOCATION. BOTH SPLICE PLATES PICK UP A MINIMUM OF TWO ROWS OF FASTENERS ON EACH SIDE OF THE WEB CUT LINES AND THE SPLICE PLATE ADJACENT TO THE WEB PICKS UP 1 ADDITIONAL ROW OF FASTENERS ON EACH SIDE OF WEB CUT LINES. ALL REPAIR STRAPS AND WEB SECTIONS WERE ALODINED AND PRIMED WITH A MINIMUM OF 2 COATS OF BMS1020 AND INSTALLED WET WITH BMS526. 2L72 4F RTA1NM 20040804001392004080400139 2004 8 4 CALA0400586 420040724A8300 DRIVE SHAFT BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE GEARBOX SHEARED A CALAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SW2770352 23590 720269 THE NR 2 ENGINE STOPPED RUNNING AT TOP OF CLIMB AT FL 270 AFTER DEPARTING DFW BOUND FOR IAH. THE ENGINE FAILURE CHECKLIST WAS PERFORMED. A RESTART WAS NOT ATTEMPTED BECAUSE NO OIL PRESSURE AND NO N2 WAS PRESENT. THE FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HORIZONTAL DRIVESHAFT FOR NR 2 ENGINE TRANSFER GEARBOX SHEARED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. ENGINEERING INVESTIGATION CONCLUDED THAT THE ENGINE FAILURE WAS THE RESULT OF THE RADIAL DRIVESHAFT BEARING SPALLING THAT SUBSEQUENTLY LEAD TO FAILURE OF THE RADIAL DRIVESHAFT. THE SDR IS CONSIDERED CLOSED WITH THE ADDITION OF THESE FINDINGS AND PART INFORMATION. 2L72 4F4 FRTA16WE E2GL 20040804001402004080400140NM 2004 8 4 CALA0400576 120040716A53306545776107 SKIN BOEING737 737524 1384721NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714667 28927 INSPECTION FOUND A DEEP CREASE IN FUSELAGE SKIN AT STA 986.5, S26L TO S26R. A REPAIR WAS INSTALLED IAW ECRA 5331-01131. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR ON OR BEFORE JULY 14, 2006 OR THE ACCUMULATION OF 14,390 TOTAL FLIGHT CYCLES. 2L72 4F RTA16WE 20040804001432004080400143NM 2004 8 4 CALA0400579 120040718A2421761574B SEAL BOEING737 737924 13848A1NM NR 2 ENGINE IDG LEAKING A CALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW273141212644 30129 A BURNING ODOR WAS NOTED IN THE CABIN AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DETERMINE THE SOURCE OF THE SMELL. IT WAS NOTED THAT THE NR 1 ENGINE UNDERWENT A FAN LUBE WHILE ON RON THE PREVIOUS NIGHT. THE NR 2 ENGINE HAD OIL IN THE EXHAUST WHICH WAS ATTRIBUTED TO LEAKAGE OF THE NR 2 ENGINE IDG DRIVE SEAL. THE IDG AND DRIVE SEAL WERE REMOVED AND REPLACED. BOTH ENGINES WERE BOROSCOPED AND THERE WERE NO ANOMALIES FOUND RELATED TO THE BURNING ODOR. A PNEUMATIC DUCT CLEAN OUT WAS PERFORMED AND RECIRCULATION FILTERS WERE REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L74 4F RTA16WE 20040804001552004080400155NM 2004 8 4 SWAA042198 120040802A3350OL3071BPEGPL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED A1 CHECK, FOUND FWD LT EEPLS INOP. RELAMPED FWD EEPLS PER MM. 2L72 4F RTA16WE 20040804001582004080400158NM 2004 8 4 SWAA042202 120040801A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 953, STRINGER 24L, BS 967, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040804001602004080400160NM 2004 8 4 SWAA042204 120040801A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 735, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040804001782004080400178EA 2004 8 4 SWIA200413617 120040715A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED ANGLE FS 484.00 RBL 27.0 O/B LOCATION. ITEM FOUND AT C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, AND 51-25-16. 2L72 4F RTA21EA 20040804001812004080400181EA 2004 8 4 SWIA200413620 120040715A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW FUSELAGE PULLEY INTERCOSTAL FLANGE CRACKED FS 484 LBL 36 PREVIOUS REPAIR ANGLE. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ REO 601R-53-41-059 REV. A 2L72 4F RTA21EA 20040804001822004080400182EA 2004 8 4 SWIA200413621 120040715A5320 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW FUSELAGE FITTING CRACKED AT FS 461 RBL 9 O/B. ITEM FOUND AT C-CHECK. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11. 2L72 4F RTA21EA 20040804001852004080400185EA 2004 8 4 SWIA200413624 120040630A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07929SW CARGO PIT FLOORBOARD SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 40. ITEM FOUND AT C-CHECK. 2L72 4F RTA21EA 20040804001862004080400186EA 2004 8 4 SWIA200413625 120040709A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07934SW 7722 FS 280 RIGHT HAND FLOORBEAM RBL 9.0 O/B ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK. 2L72 4F RTA21EA 20040804001892004080400189EA 2004 8 4 SWIA200413628 120040722A2751 POTENTIOMETER CNDAIRCL600 CL6002B19 1900309EA FLAP INDICATOR INACCURATE A SWIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM07405SW 7029 DURING TAXI-OUT, RIGHT FLAP INDICATES 2 DEGREES MORE THAN LEFT FLAP. TAXI BACK TO GATE. ADJUSTED THE RIGHT FLAP INDICATOR POTENTIOMETER IAW AMM 27-55-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040804001902004080400190EA 2004 8 4 SWIA200413629 120040724A3597 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07980SW 7955 EMERGENCY LIGHTS WILL NOT ACTIVATE FROM FLIGHT ATTENDANT SWITCH IN ARM POSITION. SPLICED WIRE LY46B22 IN REFERENCE TO STANDARD PRACTICES. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040804001922004080400192EA 2004 8 4 SWIA200413631 120040726A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07588SW6932 6932 STAB TRIM CHANNEL NR 2 FAILED TEST. REMOVED AND REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW MM 27-42-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040804002042004080400204EA 2004 8 4 SWIA200413584 120040711A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILER INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07442SW 7609 PRIOR TO DEPARTURE, RECEIVED FLT SPOILERS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT HAND OUTBOARD FLIGHT SPOILER PCU PER AMM 27-62-01. OPERATIONAL CHECK GOOD. S/N OFF: MAL-5178. 2L72 4F RTA21EA 20040804002052004080400205SO 2004 8 4 SWIA200413585 120040715A275012064207615 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07565SW5408 5408 120340 CREW REPORTED WHILE SELECTING FLAPS 45 DEGREES, FLAPS DID NOT MOVE, NO FAULTS SHOWN AND COMMAND BAR AT 45 DEGREES. REMOVED FLAP SELECTOR HANDLE AND INSTALLED SERVICEABLE HANDLE, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040805001102004080500110WP 2004 8 5 ASAA0480439 120040517A532099364881 TIE DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - DURING C-CHECK, FOUND FRAME TIE CORRODED AT FS 1098 BETWEEN LONGERON 27L-28L. REMOVED DAMAGED AREA. INSTALLED FILLER AND REPAIR ANGLES PER SRM 51-70-5. (M) 2L72 4F RTA6WE 20040805001182004080500118WP 2004 8 5 ASAA0480471 120040604A57535910043 VANE DOUG DC9 DC983 3022083WP TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01977AS 53453 OKC - DURING C-CHECK, FOUND LEFT WING OUTBOARD T/E FLAP VANE IS GOUGED ON INBOARD L/E. REMOVED DAMAGE. ADDED DOUBLER AND FILLER PER SRM 51-70-2. (M) 2L72 4F RTA6WE 20040805001542004080500154WP 2004 8 5 ASAA0480468 120040604A5320593607112 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM01977AS 53453 OKC - DRING C-CHECK, FOUND AFT CARGO BAY INTERCOSTAL IS BENT AND BUCKLED. REPLACED DAMAGED INTERCOSTAL PER SRM 51-10-2. (M) 2L72 4F RTA6WE 20040805001562004080500156WP 2004 8 5 ASAA0480454 120040529A53115930584120 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - FOUND DURING C-CHECK, RIGHT MLG FORWARD INBOARD CORNER FRAME CHANNEL CRACKED. REPLACED FRAME PER SRM 51-10-4. (M) 2L72 4F A6WE 20040805001582004080500158NM 2004 8 5 ASAA0410294 120040617A53306522216 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND LOWER NOSE COMPARTMENT ACCESS DOOR OUTER SKIN CRACKED 1 INCH FROM AFT EDGE 2.5 INCHES FROM RT EDGE. REMOVED DAMAGED FASTENER HOLE, FABRICATED FILLER AND OUTER SKIN REPAIR DOUBLER WILL BE ACCOMPLISHED ON CARD NR 4844002. (M) 2L72 4F RTA16WE 20040805001612004080500161NM 2004 8 5 ASAA04100309 120040701A532065458953 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 26R SPLICE CAP AT BS 908 HAS OVERSIZE FASTENER HOLES. REMOVED AND REPLACED STRINGER 26R SPLICE CAP. (M) 2L72 4F RTA16WE 20040805001802004080500180NM 2004 8 5 ASAA0410323 120040712A5314654769327 KEELBEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON KEEL BEAM AFT CARGO BAY LEFT BEAM. REMOVED AND REPLACED KEEL BEAM. (M) 2L72 4F RTA16WE 20040805001832004080500183NM 2004 8 5 ASAA0410304 120040701A53306545768565 SKIN BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND DENT IN SKIN BS 428 3 INCHES ABOVE STRINGER 23R. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001872004080500187NM 2004 8 5 ASAA0410327 120040709A53306545774545 SKIN BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STATION 727B PLUS 12, 3 INCHES ABOVE STRINGER 18L. REPAIRED SKIN BLENDOUT ER 04-3115, REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001892004080500189NM 2004 8 5 ASAA0410333 120040709A532065458953 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 26R SPLICE CAP AT BS 908 HAS OVERSIZED HOLES. REMOVED AND REPLACED STRINGER 26R SPLICE CAP. (M) 2L72 4F RTA16WE 20040805001922004080500192NM 2004 8 5 ASAA0410338 120040712A53306545774548 SKIN BOEING737 737298C 1384490NM CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE SKIN PILLOWING. REPAIRED PILLOWING SKIN AT FS 727A-727B STRINGER 23L IAW ER-04-31-32 AND EA 5330-01801. (M) 2L72 4F RTA16WE 20040809000012004080900001NM 2004 8 9 ASAA0410331 120040709A532065458953 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 27L SPLICE CAP AT BS 908 HAS OVERSIZED HOLES. REMOVED AND REPLACED STRINGER 27L SPLICE CAP. (M) 2L72 4F RTA16WE 20040802000132004080200013EU 2004 8 2 USAASA04020 120040304A3200 LANDING GEAR AIRBUSA321 A321211 3930370EU MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19163US 1417 PIT - FLT 45 - EN ROUTE PIT-LAX, AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE CREW CYCLED THE GEAR, BUT THE CONDITION REMAINED THE SAME. FLIGHT RETURNED TO FIELD IN PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS NOT DECLARED, HOWEVER, THE EQUIPMENT WAS CALLED OUT BY ATC. (M) 2L72 4F RTA28NM 20040802000192004080200019EA 2004 8 2 ASOA04404 120040602A1420487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11917EV 7769 FLT 4157 - DUIRNG A GROUND INSPECTION IN HOU, THE EMERGENCY FLOOR LIGHTS FROM ROW 8 TO THE LAVATORY WERE FOUND INOPERATIVE. MAINTENANCE RESECURED A LOOSE CONNECTOR ON THE EMERGENCY FLOOR LIGHTS NEAR THE LAVATORY. OPS CHECKES GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802000252004080200025NM 2004 8 2 ASAA0410268 120040517A5310BAC14702807 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 FOUND DAMAGED FASTENER HOLES ON SHEAR TIE. REPAIRED SHEAR TIE. (M) 2L72 4F A16WE 20040802000302004080200030WP 2004 8 2 GTIA040593 120040609A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND LEFT CABIN FLOOR PANEL STATION 200-256 MISSING INSERTS AND DELAMINATED. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F RTA6WE 20040802000322004080200032WP 2004 8 2 GTIA040594 120040610A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND CABIN FLOOR PANEL STATOIN 256-313 HAT CHANNEL DISBONDED. REPAIRED DISBONDING HAT CHANNELS. (M) 2L72 4F RTA6WE 20040802000422004080200042WP 2004 8 2 GTIA040583 120040618A3350 LIGHT DOUG DC9 DC981 3022081WP AFT AIRSTAIR INOPERATIVE A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23810NK 48015 MCO - AFT AIRSTAIRS EMERGENCY LIGHT OUT, CENTER. REINSTALLED MISSING SCREW FROM LIGHT. OPS CHECK NORMAL. (M) 2L72 4F A6WE 20040802000492004080200049NM 2004 8 2 UIEA200400035 120040325A1420BACC63BR14B75NL CONNECTOR BOEING747 74747UF 1384949NM GE CF6 CF680C GL NR 1 HMU DIRTY A UIEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA15492MC 29253 704890 LAX/ICN - DURING ATTEMPTED TAKEOFF, NR 1 ENGNE FAILED TO ACCELERATE BEYOND IDLE. CLEANED CONNECTOR ON NR 1 ENGINE HMU A/B CHANNELS. GROUND OPERAITON CHECKED GOOD IAW MM 73-21. (M) 2L74 4F4 FRT1384945 E23EA 20040802000572004080200057NM 2004 8 2 ASAA0440083 120040316A53206935362 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01783AS 25114 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT. BILGE RIGHT SIDE BETWEEN STATION 747-767 INTERCOSTAL CRACKED. REMOVED AND REPLACED WITH NEW INTERCOSTAL AY RT SIDE AT AFT PIT STATION 747-767. (M) 2L72 4F RTA16WE 20040802000632004080200063NM 2004 8 2 USAASB04078 120040625A5240 ROD BOEING737 737301 1384611NM DOOR HINGE DAMAGED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19587US 23932 PHL - FLT 301 - ON CLIMB-OUT FROM PHL, EN ROUTE TO MCO, THE AIRCRAFT WOULD NOT PRESSURIZE. CREW SWITCHED ON THE ENGINE BLEEDS WITH NO HELP. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED BUT THE AIRCRAFT STILL WOLD NOT PRESSURIZE. SWITCHED TO STANDBY, MANUAL AC AND DC PRESSURIZATION MODES AND CLOSED THE OUTFLOW VALVE WITH NO HELP. FLIGHT ATTENDANT NOTICED A LOUD NOISE AT THE AFT RGHT SERVICE DOOR. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. (M) 2L72 4F RTA16WE 20040802000762004080200076EU 2004 8 2 2004F00208 120040123A3244 TIRE AMD FALCONFALCON20 2730103EU MLG FAILED A CEDAO OTHER O OTHER LDLANDING 1 SW05216CA 11 WHILE AIRCRAFT WAS LANDING AT MSP, THE AIRCRAFT BLEW TWO MAIN TIRES. REMOVED AND REPLACED THE NR 1 AND NR 2 MAIN TIRE ASSEMBLIES, FUNCTIONAL TESTED ANTI-SKID SYSTEM AND FOUND NO DEFECTS. PERFORMED HIGH SPEED TAXI OF AIRCRAFT TO TEST ANTI-SKID SYSTEM AND FOUND NO DEFECTS. (M) 2L72 4F RTA7EU 20040802000892004080200089NM 2004 8 2 USAA040299 120040602A575465C26602223 SKIN BOEING737 737401 1384701NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 PIT - FOUND SKIN AND CORE BOND HAS DELAMINATION AND KNIFE EDGE CHAFE WEAR, 5 INCHES BY 5 INCHES, LT WING NR 2 SLAT INBOARD T/E CORNER. REPLACED CORE MATERIAL, INSTALLED TOP SKIN REPLACEMENTS, SEALED AND PAINTED PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040802000942004080200094NM 2004 8 2 USAA040293 120040607A5753654635278 SKIN BOEING737 7374B7 1384702NM RT TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 PIT - FOUND SKIN AND CORE DELAMINATION 2.5 INCH BY 3 INCH AREA, RT OUTBOARD T/E FLAP, INBOARD END TRAILING EDGE. INSTALLED NEW CORE MATERIAL AND TOP DOUBLER, SEAL END, PER TYP REP 57-50-39A. (M) 2L72 4F RTA16WE 20040802000952004080200095NM 2004 8 2 USAA040288 120040611A5530 BEAM BOEING737 737301 1384611NM VERTICAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US44758 23558 PIT - FOUND BEAM CRACKED 2 INCHES, 3 INCHES FROM LOWER END OF VERT STAB LT T/E BEAM. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-30-13 FIG 1. (M) 2L72 4F RTA16WE 20040802001012004080200101NM 2004 8 2 AMTA200400822 120040701A2760 WARNING LIGHT BOEING757 75733N 1384931NM SPOILERS FALSE INDICATIONA AMTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL11554TZ 32588 ATTEMPTED ROLLING TAKEOFF RIGHT AT KPIE CONFIG WAS NORMAL FOR TAKEOFF. AFTER EPR SELECTED, WARNING HORN SOUNDED. SPOILER MSG DISPLAYED. PERFORMED FIM 27-09-00, NO DEFECTS NOTED. A/C OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040802001032004080200103NM 2004 8 2 C7WA200400011 120040412A5310 DOOR FRAME BOEING727 7272Q6 138407VNM FUSELAGE CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO171279E 21971 FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M) 2L73 4F RTA3WE 20040802001042004080200104NM 2004 8 2 C7WA200400010 120040412A5230 DOOR FRAME BOEING727 7272Q6 138407VNM MAIN CARGO DOOR CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO171279E 21971 FOUND MAIN CARGO DOOR FORWARD UPPER FRAME CRACKED. REPAIRED FRAME IAW AERONAUTICAL ENGINEERS INC EO NR 1434. (M) 2L73 4F RTA3WE 20040802001122004080200112SO 2004 8 2 2004F00215 220040112A8520 CONNECTING ROD CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE BROKEN A OIKAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP135403M 402B0003 2060179E ENGINE FAILED IN FLIGHT FROM HNL TO MKK, NR 1 CYL CONNECTING ROD BROKE OFF AT FLT ALT. 1,500 FEET 27 INCHES OF MANIFOLD, 2300 RPM. AIRCRAFT RETURNED TO HNL. (M) 1L72 3O3 O A7CE E8CE 20040802001132004080200113 2004 8 2 HALA0400131 420040121A8300 GEARBOX BOEING717 717200 1383700NM ACCESSORY G/B MAKING METAL A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13487HA 55132 FLT 360 - HNL - DURING CLIMB, ENGINE ANNUNCIATOR LIGHT CAME ON. ENGINE PAGE SHOWED ENGINE RT SYSTEM FAIL AND ENG RT OIL FILTER. INSPECTION REVEALED METAL IN GEARBOX SCREEN. REPLACED ENGINE GEAR BOX. TOWER SHAFT BEARING CAGE FAILED. (M) 2L72 4F TRA6WE 20040802001192004080200119EA 2004 8 2 ASOA04403 120040602A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11875AS 7559 FLT 4612 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY EXIT SIGN AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN LAMP AT THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001242004080200124WP 2004 8 2 GTIA040624 120040514A5753 VANE DOUG DC9 DC983 3022083WP TE FLAP CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 FOUND INBOARD FLAP VANE OF OUTBOARD FLAP HAS CORROSION AND MISSING SCREW. REMOVED DAMAGED AREA. SKIN ALTERNATE ID 2024T81 SUBSTITUATION FOR 2075T6- .016 HOT BONDED REPAIR. (M) 2L72 4F RTA6WE 20040802001412004080200141EA 2004 8 2 ASOA04407 120040602A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M) 2L72 4F RTA21EA 20040802001482004080200148EA 2004 8 2 2004F00230 120040118A7830MS244236 ISOLATION VALVE CNDAIRCL600 CL6002D24 1390016EA THRUST REVERSER FAILED A FDKAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07905FJ1554 15005 FRL 6643 - PHX-DFW - ABORTED TAKEOFF, DUE TO RIGHT REVERSER UNSAFE CAUTION LIGHT ON. ITEM DEFERRED PER MEL 78-30-01. MAINTENANCE REPLACED THE ISOLATION VALVE ON THE RT THRUST REVERSER. ALL LEAK AND OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20040802001582004080200158 2004 8 2 GTIA040560 420040603A2565 SLIDE DOUG DC9 DC983 3022083WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 SJU - FLT 912 - L1 SLIDE PACK BRACKETS LOOSE. SECURED BRACKETS. (M) 2L72 4F RTA6WE 20040802001612004080200161NM 2004 8 2 UIEA200400001 120040108A7931 MANIFOLD BOEING747 74747UF 1384949NM OIL PRESSURE MALFUNCTIONED A UIEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15412MC 30559 HKB-DXB - NR 4 ENGINE OIL CONSUMPTION HIGH, QUANITY AT ZERO APPROXIMATELY 3 HOURS INTO FLIGHT. OIL PRESSURE LOW APPROXIMATELY 2 HOURS LATER. NR 4 ENGINE SHUTDOWN AT 1758Z, FL330, MACH .813. REPLACED OIL PRESSURE TRANSMITTER MANIFOLD. CARRIED OUT LEAK CHECK PER MM 71-00-00 NIL LEAKS EVIDENT. CARRIED OUT WINDMILL INSPECTION PER MM 72-00-00, NO DAMAGE FOUND. (M) 2L74 4F RT1384945 20040802001682004080200168EA 2004 8 2 ASOA04418 120040609A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11870AS 7530 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040802001692004080200169SO 2004 8 2 SIMA200416701 120040613A1420 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT LOOSE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21738NR 145401 BGR - FLT 4655 - EMERGENCY EXIT LIGHT ON AFT GALLEY BULKHEAD INOPERATIVE. RESECURED LOOSE CONECTOR OVER GALLEY CEILING LIGHT. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040802001892004080200189NM 2004 8 2 USAA04338 120040620A5534 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 FOUND .25 INCH BY .25 INCH CORROSION ON THE FORWARD TEE FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. CORROSOIN LEVEL 1, TASK JK-64-55200-C-001. REMOVED CORROSION AND INSTALLED NEW BUSHINGS PER EA 78608. (M) 2L72 4F RTA16WE 20040803000102004080300010NM 2004 8 3 SWAA042171 120040729A53116546526 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 400, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040803000132004080300013NM 2004 8 3 SWAA042164 120040728A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT MISSING PLASTIC LENS. INSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040803000162004080300016EU 2004 8 3 MALA040499 120040719A3350 COVER SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISLODGED A MALAO OTHER O OTHER LDLANDING 1 GL15454XJ 340B454 THE RIGHT EMERGENCY EXIT HANDLE COVER FELL OFF DURING LANDING. MAINTENANCE RESECURED COVER. 2L72 4T RTA52EU 20040803000342004080300034NM 2004 8 3 04FDEA02272 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 25L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79812, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 25L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000352004080300035NM 2004 8 3 04FDEA02273 120040728A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 6 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79821, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 6R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000362004080300036NM 2004 8 3 04FDEA02274 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 21L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79805, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 21L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040803000402004080300040NM 2004 8 3 SWAA042174 120040729A3350604222 BATTERY BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR OVERHEAD EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040803000482004080300048EU 2004 8 3 AALA20040781 120040727A3350 WIRE AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW2119059 469 BOS - EMERGENCY LIGHT ASSEMBLY AT SEAT 20G INOPERATIVE. FOUND BROKEN WIRES AT SEAT 20G. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040804000032004080400003WP 2004 8 4 AALA20040742 120040721A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21296AA 49308 PHX - EMERGENCY EXIT SIGNS ABOVE AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY B5105 FOR EMERGENCY EXIT SIGNS ABOVE AFT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000102004080400010NM 2004 8 4 04FDEA02275 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 19L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79817, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 19L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000162004080400016NM 2004 8 4 04FDEA02277 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 15L BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79816, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 15L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000182004080400018NM 2004 8 4 AALA20040750 120040606A3350D71701100 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21773AN 29583 AFW - BATTERY PACK LIGHTS WENT OUT AFTER SIX MINUTE BURN IN FIRST CLASS. DID NOT LAST 10 MINUTES PER WORK CARD 0357. REPLACED BATTERY PACK FOR FIRST CLASS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040804000202004080400020WP 2004 8 4 AALA20040748 120040721A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217541A 49995 DFW - FORWARD CABIN SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT SOCKETS AT SEATS 18D THROUGH 10D FOR FORWARD CABIN SEAT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000362004080400036WP 2004 8 4 AALA20040759 120040723A3260 INDICATOR DOUG DC9 DC982 3022082WP MLG MALFUNCTIONED A AALAO OTHER N FALSE WARNING DEDESCENT 1 SW21408AA 49319 DFW - INFLIGHT T369/23 INBOUND TO DFW NOSE GEAR UNSAFE INDICATION EXTENSION FAULT. NOSE GEAR FAILED TO EXTEND ON FIRST ATTEMPT. EXTENDED AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. CYCLED NOSE GEAR SEVERAL TIME WITH NO FAULTS FOUND. ALL INDICATIONS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000412004080400041NM 2004 8 4 AALA20040762 120040725A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21685AA 25342 DFW - AFT EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804000422004080400042WP 2004 8 4 AALA20040768 120040722A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21475AA 49650 LAX - LEFT AND RIGHT AFT OVERWING EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK B5105 FOR LEFT AND RIGHT AFT OVERWING EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000502004080400050NM 2004 8 4 04FDEA02285 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 36 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79825, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000512004080400051WP 2004 8 4 04FDEA02286 120040729A5210ABA85642 SUPPORT DOUG DC10 DC1030 3023501WP R1 DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 R-1 AFT UPPER CHAIN GUARD BRACKET CRACKED. REMOVED AND REPLACED CHAIN GUARD BRACKET AND CHAIN GUARD IAW MM 52-11-09 AT MAE. 2L73 4F A22WE 20040804000592004080400059EU 2004 8 4 MALA040480 120040704A3350330151 SWITCH SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15424XJ 340B424 EMERGENCY LIGHTS INOP, WILL WORK WITH BATTERY POWER AND EXTERNAL BUT NOT INDEPENDENT. FOUND COCKPIT SWITCH BAD. REPLACED SWITCH ASSY. DURING COMPLETION OF OPS CHECK CARD 335003, FOUND 24LN FAILED. REPLACED P/N 3301-51, S/N ON 2148. ALL CHECKS GOOD. 2L72 4T RTA52EU 20040804000662004080400066EU 2004 8 4 MALA040488 120040714A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 DURING 4Y/2Y INSPECTION IN LCQ, CORROSION ON SEAT TRACK (MIDDLE) IN CARGO BAY AT FS 686. REMOVED AND REPLACED WITH NEW SEAT TRACK SECTION IAW MESABA EO S53060. A/C RELEASE DATE 7/15/04. 2L72 4T RTA52EU 20040804000672004080400067NM 2004 8 4 SWAA042116 120040725A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB FITTING LUGS, CORRODED. REPAIRED HORIZONTAL STAB PER ER AND SRM. 2L72 4F RTA16WE 20040804000892004080400089 2004 8 4 SWAA042178 420040731A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804000922004080400092NM 2004 8 4 SWAA042130 120040726A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB PER ER. 2L72 4F RTA16WE 20040804000962004080400096 2004 8 4 SWAA042152 420040728A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR GIRT BARDISCONNECTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE DISCONNECTED. SECURED CABLE PER MM. 2L72 4F RTA16WE 20040804000972004080400097NM 2004 8 4 SWAA042153 120040728A5210507945299 DOOR FRAME BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR, AFT DOOR FRAME, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR PER MM. 2L72 4F RTA16WE 20040804001002004080400100NM 2004 8 4 SWAA042157 120040728A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS CORRODED. REPAIRED VERTICAL STAB FITTING PER ER. 2L72 4F RTA16WE 20040804001012004080400101 2004 8 4 SWAA042180 420040731A25656949956 CABLE BOEING737 7372H4 138448CNM R1 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29090SW 22905 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R1 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F A16WE 20040804001102004080400110EU 2004 8 4 MALA040490 120040714A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15535XJ E2371 CREW REPORTED OUTBOUND TO DFW, THE GREEN SYSTEM HIGH TEMP LIGHT ILLUMINATED, TURNED OFF PUMP AND RETURNED TO MEM. MAINTENANCE REPLACED NR 3 EDP P/N ON OFF 521449, S/N ON F9717007, S/N OFF F9840492, RAN AND LEAK CHECK GOOD IAW AMM CH 29. 2H74 4F RTA49EU 20040804001142004080400114WP 2004 8 4 04FDEA02023 120040707A5330 SKIN DOUG DC10 DC1030 3023501WP ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND LOWER FUSELAGE SKIN EXTERNAL REPAIR DOUBLER DENTED AT STA 1019 BETWEEN L-36R AND L-37R. DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-20-00 VOL 2. FABRICATED REPAIR PARTS IAW DC10 SRM 53-20-00 FIG 6 VOL 1 AND DC10 SRM 53-33-01 VOL 2 FIG 2. INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-41-01 VOL 2 AND DC10 SRM 51-33-01 VOL 2. 2L73 4F A22WE 20040804001212004080400121NM 2004 8 4 SWAA042162 120040728A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS STRIP COVERS PER MM. 2L72 4F RTA16WE 20040804001352004080400135WP 2004 8 4 AALA20040754 120040714A292341003106 PUMP DOUG DC9 DC982 3022082WP HYD SYSTEM INOPERATIVE A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21486AA 49679 INFLIGHT T1622/14 AFTER TWO HOURS OF FLIGHT LEFT HYDRAULIC PRESSURE DECREASED TO CA 500 PSI WITH LEFT ENGINE PUMP IN LOW. PERFORMED QRH PROCEDURE FOR RIGHT SYSTEM ENGINE PUMP HI TRANSFER PUMP ON. OPERATED NORMALLY FOR APPROXIMATELY 10 MINUTES AND RIGHT SYSTEM FAILED. RESTORED RIGHT SYSTEM LATER IN FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED HYDRAULIC TRANSFER PUMP. ALSO REPLACED LEFT HYDRAULIC PRESSURE TRANSMITTER AND RETURN FILTERS. SERVICED HYDRAULIC SYSTEM AS REQUIRED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804001442004080400144NM 2004 8 4 CALA0400580 120040719A32304105DA VALVE BOEING737 7373T0 1384582NM NLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW271232727305 23457 THE NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. A MANUAL EXTENSION WAS PERFORMED AND THE NOSE GEAR SHOWED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LANDING GEAR SELECTOR VALVE WAS REMOVED AND REPLACED IAW MM 32-31-51. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20040804001562004080400156NM 2004 8 4 SWAA042199 120040802A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040804001612004080400161 2004 8 4 SWAA042205 420040802A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804001662004080400166SO 2004 8 4 SWIA200413635 120040725A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07563SW 120338 FORWARD EMERGENCY LIGHT WON`T TEST. REMOVED AND REPLACED FORWARD BATTERY PACK FOR EMERGENCY LIGHTS PER EMB 120 MM 24-33-01. OPERATIONAL CHECK GOOD. P/N D366-04-001, S/N OFF 893/03-91. 2L72 4T RTA31SO 20040804001742004080400174EA 2004 8 4 SWIA200413613 120040715A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 PASSENGER DOOR; STAIRS AFT DRAG ANGLE IS CRACKED BY DOOR ASSIST PULLEY BRACKET. ITEM FOUND AT C-CHECK. PASSENGER DOOR DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513 REV. NC. 2L72 4F RTA21EA 20040804001802004080400180EA 2004 8 4 SWIA200413619 120040715A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW FUSELAGE VERTICAL BEAM LOWER FLANGE CRACKED FS 559 LBL 9 O/B. ITEM FOUND AT C-CHECK. REPAIRED IAW CRJ REO 601R-53-41-057 REV. NC. 2L72 4F RTA21EA 20040804001842004080400184EA 2004 8 4 SWIA200413623 120040630A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07929SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.0 LBL 9.0 O/B. ITEM FOUND AT C-CHECK. 2L72 4F RTA21EA 20040804002002004080400200NM 2004 8 4 SWAA042195 120040801A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040805001192004080500119NM 2004 8 5 ASAA0480444 120040522A575499194441 SKIN DOUG MD80 MD83 3023681NM NR 2 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND LEFT NR 2 SLAT LOWER SURFACE SKIN IS CRACKED. REPLACED SKIN PER SRM 51-30-8. (M) 2L72 4F RT 20040805001282004080500128NM 2004 8 5 ASAA0410283 120040603A53116554919 FRAME BOEING737 737290C 138448VNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - MAIN CARGO DOOR LOWER AFT STUB FRAME HAS ELONGATED HOLES. REMOVED, FABRICATED AND INSTALLED STUB FRAME IAW 51-20-01. (M) 2L72 4F A16WE 20040805001382004080500138NM 2004 8 5 ASAA0410292 120040506A531065671406 BEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON LONGITUDINAL BEAM OUT OF LIMITS. REPLACED WITH NEW LONGITUDINAL BEAM. (M) 2L72 4F A16WE 20040805001702004080500170NM 2004 8 5 ASAA0410286 120040605A523065549172 ANGLE BOEING737 737290C 138448VNM CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR LATCH FITTING ANGLE CRACKED. REPAIRED MAIN CARGO DOOR LOEWR BEAM AND LATCH FITTING. (M) 2L72 4F A16WE 20040805001782004080500178NM 2004 8 5 ASAA0410350 120040711A53306545775558 SKIN BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUD 3 SKIN BLENDOUTS AT STATION 768 1 INCH ABOVE STRINGER 23R AND BS 771 3 INCHES BELOW STRINGER 21R EXCEED LIMITS. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001792004080500179NM 2004 8 5 ASAA0410348 120040712A53306545800691 SKIN BOEING737 737298C 1384490NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUEL ENTRY DOOR CUTOUT SKIN UNDER THRESHOLD IS GOUGED. REPAIRED SKIN GOUGE UNDER THRESHOLD, FOUND ADDITIONAL DAMAGED FASTENER HOLES, INCORPORATED THEM INTO THIS REPAIR, FABRICATED DOUBLER AND TRIPLER AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001902004080500190NM 2004 8 5 ASAA0410305 120040701A53306545775558 SKIN BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 FOUND DENT IN FUSELAGE SKIN. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001912004080500191NM 2004 8 5 ASAA0410336 120040712A53306545778558 SKIN BOEING737 737298C 1384490NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND DENT ON FUSELAGE OUTER SKIN STATION 998 3 INCH BELOW STRINGER 14R. REPAIRED DENT IN SKIN. (M) 2L72 4F RTA16WE 20040805001982004080500198NM 2004 8 5 ASAA0480450 120040522A53113936607513 FRAME DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV-CHECK, FOUND FRAME IS CORRODED IN AFT CARGO BAY AT FS 1079 AT LONGERON 29R. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02365. (M) 2L72 4F RT 20040805002032004080500203NM 2004 8 5 ASAA0410318 120040707A522050797897 DOOR BOEING737 737298C 1384490NM OVERWING EXIT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND LEFT OVERWING EXIT REPLACED DUE TO MULTIPLE CORROSION AND STRUCTURE DEFECTS. REMOVED AND REPLACED LEFT OVERWING EXIT. (M) 2L72 4F RTA16WE 20040809000032004080900003NM 2004 8 9 ASAA0410313 120040706A532065516985 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 25L SPLICE CAP HAS OVERSIZED HOLES. REMOVED AND REPLACED SPLICE CAP. (M) 2L72 4F RTA16WE 20040809000062004080900006NM 2004 8 9 ASAA0440140 120040627A5320BAC1469377 FLOOR SUPPORT BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01792AS 28887 OAK - FOUND AFT CARGO COMPARTMENT, FLOOR SUPPORT ZEE ANGLE CORRODED BEYOND SERVICABLE LIMITS, STATION 727 TO 767 RT. REPLACED ZEE ANGLE SUPPORT AND SUPPORT SPLICES. (M) 2L72 4F RTA16WE 20040809000072004080900007NM 2004 8 9 ASAA0440139 120040623A5420 BRACKET BOEING737 737490 1384715NM RT PYLON CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01792AS 28887 OAK - FOUND RIGHT ENGINE PYLON ANGLE BRACKET IS CRACKED. REMOVED CRACKED BRACKET AND INSTALLED NEW ANGLE BRACKET ON RIGHT ENGINE PYLON. (M) 2L72 4F RTA16WE 20040809000082004080900008 2004 8 9 ASAA0440141 420040615A25652560010384A PAD BOEING737 737490 1384715NM L2 DOOR DISLODGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01799AS 29270 SEA - DURNG A ROUTINE FLIGHT ATTENDANT TRAINING CAMP, THE L2 DOOR SLIDE FAILED TO COMPLETELY INFLATE. UPON INVESTIGATION IW WAS NOTED THAT THE AIRCRAFT DOOR PAD WAS TAPED TO THE SIDE OF THE AIRCRAFT, THE TAPE ITSELF WAS OF POOR QUALITY AND INSUFFICIENT SIZE TO HOLD THE PAD IN PLACE. THIS ALLOWED THE PAD TO BE SUCKED INTO THE ASPIRATOR, BLOCKING THE AIR FROM ENTERING THE SLIDE. USE BAG PIT TAPE WHICH IS WIDER AND MORE ADHESIVE TO ATTACH PAD TO AIRCRAFT. (M) 2L72 4F RTA16WE 20040809000112004080900011SO 2004 8 9 SIMA200417003 120040618A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21649PP 145234 OMA - FLT 4079 - DURING PREFLIGHT, CREW REPORTED THAT SOME CABIN FLOOR PROXIMITY EMERGENCY LIGHTS AFT OF OVERWING EXITS DID NOT ILLUMINATE. AIRCRAFT WAS FERRIED TO ORD FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY AND INVERTER ASSEMBLY P/N 67343 IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040809000122004080900012 2004 8 9 SIMA200416703 420040613A22103621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZONTAL STAB MALFUNCTIONED A SIMAO OTHER J WARNING INDICATION LDLANDING 1 SW21854AE 145743 DFW - FLT 3582 - DUAL PITCH TRIM FAILURE ON LANDING WITH AUTO PILOT ON. DECLARED EMERGENCY AND LANDED WTHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040809000132004080900013EU 2004 8 9 USAAEM04009 120040624A3230 ARM EMB ERJ170ERJ170100 EU MLG BINDING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19804MD 17000016 FLT 1621 - PIT-SYR - AFTER TAKEOFF, THE LEFT MAIN GEAR AND NOSE GEAR FAILED TO RETRACT. THE CAPTAIN RETURNED TO PIT AND LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MAIN LANDING GEAR LOWER LOCK STAY ARM BINDING. REMOVED, CLEANED AND REINSTALLED. (M) 2L74 4F RTA56NM 20040809000142004080900014 2004 8 9 GTIA040565 420040609A2565 CABLE DOUG DC9 DC982 3022082WP GIRT BAR MISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23817NK 49141 FLL - L1 DOOR SLIDE GIRT BAR CABLE IMPROPERLY ROUTED. REROUTED GIRT BAR CABLE. (M) 2L72 4F A6WE 20040809000152004080900015NM 2004 8 9 USAA040305 120040615A573065C2660399 SKIN BOEING737 737301 1384611NM WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US50306 23740 PIT - FOUND WING DELAMINATED 1.5 SQUARE INCH, TOP SURFACE AT OUTBOARD TRACK AREA TRAILING EDGE OF NR 3 SLAT. REMOVED DAMAGE. INSTALLED FILLER/CORE MATERIAL, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040809000162004080900016WP 2004 8 9 GTIA040563 120040607A5220 LATCH DOUG DC9 DC982 3022082WP TAIL CONE STUCK A GTIAK NONE O OTHER ININSP/MAINT 1 GL23820NK 49126 LGA - FLT 1174 - FLIGHT ATTENDANT SAYS THAT AFT CABIN DOOR IS VERY HARD TO CLOSE. AFT FLIGHT ATTENDANT REPORTED SAFETY DOOR FOR TAIL CONE HANDLE ABOVE FLIGHT ATTENDANT SEAT WOULD NOT LATCH. FREED LATCH, OPS CHECK NORMAL. NO FAULT REPORTED OR FOUND WITH AFT CABIN DOOR. (M) 2L72 4F A6WE 20040809000192004080900019NM 2004 8 9 USAA040301 120040526A575465C26602217 SKIN BOEING737 737301 1384611NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19589US51120 23934 PIT - FOUND SKIN TO CORE BOND WITH 1 INCH DIAMETER AND .75 INCH DIAMETER, LEFT WING NR 2 SLAT TOP SURFACE INBOARD AND OUTBOARD T/E CORNERS. REMOVED EXT SKIN AND DAMAGED CORE, INSTALLED NEW PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040809000202004080900020NM 2004 8 9 USAA040302 120040526A575465C26602223 SKIN BOEING737 737401 1384701NM NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 PIT - FOUND SKIN AND CORE 7.5 INCH BY 4.25 INCH, DELAMINATION WITH LOWER SKIN KNIFE EDGE WEAR, LT WING NR 2 SLAT OUTBOARD T/E CORNER. REMOVED DAMAGED SKIN AND CORE, REPLACED CORE AND TOP SKIN PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040809000212004080900021WP 2004 8 9 GTIA040517 120040527A2560 GLOWSTRIP DOUG DC9 DC982 3022082WP L2 DOOR AREA LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FOUND SAFE T GLO STRIP MISSING L-2 DOOR AREA IN FRONT OF GALLEY. RESECURED SAFE T GLO STRIP L-2 DOOR AREA. OK FOR SERVICE. (M) 2L72 4F A6WE 20040809000222004080900022WP 2004 8 9 GTIA040552 120040528A2560 GLOWSTRIP DOUG DC9 DC983 3022083WP CABIN DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 DTW - FOUND FLT 1678 - AFT GALLEY EMERGENCY TRACK GLOW STRIP CAME OFF. REINSTALLED STRIP. (M) 2L72 4F RTA6WE 20040809000232004080900023WP 2004 8 9 GTIA040553 120040531A3350 LIGHT DOUG DC9 DC983 3022083WP AFT GALLEY MISSING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 RSW - FLT 936 - AFT GALLEY FLOOR PATH EXIT MARKER MISSING. REINSTALLED AFT GALLEY FLOOR PATH EXIT MARKER. NO OTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20040809000242004080900024WP 2004 8 9 GTIA040555 120040531A57555910055526 SKIN DOUG DC9 DC981 3022081WP SPOILER DEBONDED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 DTW - FOUND RIGHT INBOARD FLIGHT SPOILER HAS PREVIOUS REPAIR DISBONDED. REMOVED AND REPLACED RIGHT INBOARD FLIGHT SPOILER. OPS CHECK GOOD. (M) 2L72 4F A6WE 20040809000282004080900028WP 2004 8 9 ASAA0480441 120040517A5330593442573 PANEL DOUG DC9 DC983 3022083WP VOR ANTENNA DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OKC - DURING C-CHECK, FOUND RIGHT LOWER VOR ANTENNA PANEL IS DELAMINATED. REMOVED AND REPLACED DAMAGED SECTION PER EA 3450-01029. (M) 2L72 4F RTA6WE 20040809000292004080900029NM 2004 8 9 ASAA0440126 120040412A53306547952358 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 GYR - AFT CARGO DOOR OUTER SKIN DENTED AND GOUGED IN NUMEROUS PLACES. REPLACED THE AFT CARGO DOOR OUTER SKIN. (M) 2L72 4F RTA16WE 20040809000302004080900030NM 2004 8 9 ASAA0480445 120040522A521059114069 RIVET DOUG MD80 MD83 3023681NM R1 DOOR SHEARED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, REAR SERVICE R1 DOOR HAS SHEARED RIVET IN LOWER FORWARD SECTION. INSTALLED DOUBLER AND BUSHING PER EA 5200-01017. (M) 2L72 4F RT 20040809000332004080900033NM 2004 8 9 UIEA200400006 120040119A326065B4750552 LOGIC CARD BOEING747 747230B 1384889NM MLG DAMAGED A UIEAO OTHER J WARNING INDICATION LDLANDING 1 EA15508MC 21644 TLV/AMS - ON CALL BEFORE LANDING CHECK, GEAR INDICAT DOWN, INTERMITTENT BEEPING WAS HEARD. GEAR LIGHT WENT RED. PRIMARY AND ALTERNATE CHECK SHOWED RIGHT BODY AND RIGHT WING GEAR NO DOWN. CREW INITIATED GO AROUND, LEFT GEAR DOWN AND LEVEL OFF GEAR LIGHT WENT GREEN AND CHECKED IN BOTH ALTERNATE AND PRIMARY. CONFIGURED FLAPS FOR LANDING 2ND TIME AND HAD ALL GREEN. GEAR WENT RED AGAIN BUT INDICATED GEAR DOWN IN PRIMARY. ALTERNATE SHOWED RIGHT BODY GEAR AND RIGHT WING GEAR NOT DOWN. INDICATION FINALLY SETTLED WITH RIGHT WING NO DOWN IN ALTERNATE POSITION. REMOVED AND REPLCED BOTH PRIMARY AND ALTERNATE LOGIC (P/N 65B4750867) BOXES IAW AMM 31-61-14. OPERATION CHECK ALL NORMAL. (M) 2L74 4F A20WE 20040809000372004080900037EU 2004 8 9 USAASA04001 120040111A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT WILL NOT TEST A USAAK NONE L NO TEST ININSP/MAINT 1 EA19725UW 1135 DCA - ESPU FAILED SELF-TEST. MAINTENANCE REPLACED THE LEFT (11LWA) EMREGENCY LIGHT EPSU. (M) 2L72 4F RTA28NM 20040809000422004080900042NM 2004 8 9 2004F00167 120040202A75006522454143 DUCT BOEING727 727222 1384073NM NR 3 ENGINE CRACKED A RYNAEC ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE077640U 19913 ON TAKEOFF ROLL OUT OF ICT, NR 3 ENGINE FIRE WARNING CAME ON. SHUTDOWN NR 3 ENGINE IAW RYAN PROCEDURES AND RETURNED ICT. AIRCRAFT LANDED ICT WITHOUT INCIDENT. REMOVED AND REPLCED NR 3 ENGINE 13 STAGE SADDLE DUCT. GROUND OPERATIONAL CHECK NORMAL. (M) 2L73 4F A3WE 20040809000452004080900045EA 2004 8 9 ASOA04242 120040326A3230601R751451 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11884AS 7513 FLT 4783 - DUIRNG TAKEOFF FROM DFW-AMA, THE LEFT MAIN GEAR FAIL TO RETRAC AND SHOWED INTRANSITION. THE QRH WAS COMPLIED WITH. THE CREW RECYCLED THE GEAR, IT CAME DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE AND PERFORMED GEAR SWINGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040809000472004080900047NM 2004 8 9 USAASB04037 120040326A3260189929 SENSOR BOEING737 737301 1384611NM RT MLG WW FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19352US 23555 CLT - FLT 401 - DURING CRUISE, EN ROUTE FROM CLT-IND, THE AIRCRAFT EXPERIENCED MULTIPLE AVIONICS AND SYSTEM FAILURES. AIRCRAFT LOST THE FLIGHT DIRECTOR, L NAV, TRANSPONDER, CABIN PRESSURIZATION AND LOW IDLE ON ENGINE. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. CREW ALSO NOTED THAT THE SPEED BRAKE WOULD NOT ARM FOR LANDING, THE INFORMATION ON THE FMC WAS NOT ACCURATE AND THE CAPTAINS AUDIO PANEL WOULD NOT TRANSMIT. UPON ARRIVAL AT THE GATE, THE AIRCRAFT WOULD NOT ACCEPT GROUND POWER. MX FOUND THE RED LEG OF THE S105 SENSOR RESISTANCE OUT OF TOLERANCE. SENSOR READ INFINITY TO GROUND. AIRCRAFT WAS IN THE AIR MODE THROUGH THE S106 SENSOR, BUT IN THE GROUND MODE THROUGH THE S105 SENSOR. REMOVED2L72 4F RTA16WE 20040802000812004080200081NM 2004 8 2 USAA040287 120040610A5315 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US44758 23558 PIT - FOUND BEAM CORRODED THREE 1 INCH DIAMETER AREAS, BS 947 LBL 30 TO LBL 46. REMOVED CORROSION, TREATED AND PRIMED, PERFORMED TYP REPAIR 53-15-01B, SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20040802000912004080200091NM 2004 8 2 USAASB04073 120040618A3350210310005 FUSE BOEING737 7373B7 1384580NM POWER SUPPLY INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19521AU 23856 PHL - PILOT REPORTED THE SEAT ROW EMERGENCY LIGHTS, FROM ROWS 17 THROUGH 22, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 5 AMP FUSE IN THE POWER SUPPLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040802000922004080200092NM 2004 8 2 USAASA04074 120040620A335020121 POWER SUPPLY BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19433US 24555 MAINTENANCE REPORTED THE RIGHT BULLNOSE EMERGENCY LIGHT, AT SEAT ROW 20, INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND THE M1137 POWER SUPPLY FUSES BURNED. REMOVED AND REPLACED THE M1137 POWER SUPPLY. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040802001022004080200102 2004 8 2 GTIA040633 420040629A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FLL - FLT 478 - DOOR R1 SLIDE PACK FELL OFF OF DOOR WHEN OPENED FOR CATERING ACCESS. REINSTALLED R-1 SLIDE. (M) 2L72 4F A6WE 20040802001202004080200120EA 2004 8 2 ASOA04410 120040604A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11923EV 7828 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEOP ON THE PASSENGER DOOR WAS FOUND TO BE BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040802001212004080200121WP 2004 8 2 GTIA040620 120040607A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND RIGHT INBOARD SEAT TRACKS STATION 200-798 GOUGED AND CORRODED. FOUND STATION 200 TO 370 IS OUT OF LIMITS. REMOVED SEAT TRACK. LOCATED AND DRILL NEW RIGHT INBOARD SEAT TRACK. LOCATED AND DRILLED THREE EACH SPLICES. INSTALLED THEE SPLICE. INSTALLED RIGHT INBOARD SEAT TRACK. (M) 2L72 4F RTA6WE 20040802001262004080200126NM 2004 8 2 AMTA200400807 120040628A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM ROW 33 TO 35. RECONNECTED CONTACT AT ROW 33 EGRESS STRIP. OPS CHECK NORMAL AT THIS TIME IAW MM PER 33-51-11. (M) 2L72 4F RTA2NM 20040802001372004080200137EA 2004 8 2 ASOA04400 120040602A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL UNDER THE FORWARD LATCH AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO BAY FLOOR SILL AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040802001472004080200147WP 2004 8 2 GTIA040574 120040617A2612 CONNECTOR DOUG DC9 DC982 3022082WP FIRE LOOP DIRTY A GTIAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23823NK 48020 RIGHT LOOP B LIGHT CAME ON DURING FLIGHT. PERFORMED QRH PROCEURE, LOOP A OK. T/S CLEANED CONNECTORS ON B LOOP ENGINE CONNECTORS UNABLE TO FIND CONCLUSIVE FAULT, OPS CHECK OK. (M) 2L72 4F A6WE 20040802001502004080200150EA 2004 8 2 ASOA04399 120040602A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11884AS 7513 DURING A C-CHECK IN MCN, THE LEFT INTERCOSTAL CLIP AT FS 484, BL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT INTERCOSTAL CLIP AT FS 484, BL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040802001552004080200155 2004 8 2 GTIA040573 420040615A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 CUN - FLT 278 - R1 SLIDE PACK CAME LOOSE FROM DOOR MOUNT. RESECURED R1 SLIDE PACK DOOR COVER. (M) 2L72 4F A6WE 20040802001702004080200170SO 2004 8 2 SIMA200417005 120040618A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21675AE 14500806 DURING PREFLIGHT, THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. AIRCRAFT WAS FERRIED TO ORD FOR REPAIRS. MAINTENANCE REPLACED THE FORWARD FLOOR STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040802001952004080200195NM 2004 8 2 USAA04339 120040620A5534 FITTING BOEING737 737401 1384701NM VERTICAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 FOUND .25 INCH BY .25I NCH CORROSION ON THE FORWARD T-FITTING OF THE OUTBOARD ATTACH FITTING ON THE LEFT AFT SIDE OF THE VERTICAL STAB. REMOVED CORROSION AND INSTALLED NEW BUSHING PER EA 78608. (M) 2L72 4F RTA16WE 20040803000082004080300008NM 2004 8 3 SWAA042169 120040729A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEBS AT BS 360 TO BS 380, BS 500A TO BS 500B, CORRODED. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20040803000122004080300012NM 2004 8 3 SWAA042173 120040729A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040803000272004080300027WP 2004 8 3 AALA20040731 120040717A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21479AA 49654 MIA - FLOOR LEVEL EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPAIRED BROKEN WIRE FOR FLOOR LEVEL EMERGENCY EXIT LIGHT AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040803000422004080300042NM 2004 8 3 SWAA042176 120040729A5313BAC1498 STRINGER BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 26R, BS 500A, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040803000492004080300049WP 2004 8 3 AALA20040770 120040722A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219404V 53140 FORWARD RIGHT HAND EMERGENCY EXIT LIGHT IDENTIFIER INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR FORWARD RIGHT HAND EMERGENCY EXIT LIGHT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040803000562004080300056WP 2004 8 3 AALA20040746 120040717A2120 A/C PACK DOUG DC9 DC983 3022083WP SMOKE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW219628W 53598 SFO - INFLIGHT T0698/17 SMOKE IN CABIN AND COCKPIT ON ROTATION. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN PER MCM 21-92-12 WITH NO DEFECTS NOTED. FUNCTIONAL CHECK FLIGHT OPERATED NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040803000572004080300057NM 2004 8 3 AALA20040739 120040719A335024003 SWITCH BOEING767 767323 1385205NM CABIN SHORTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21351AN 24032 CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND SWITCH AT RIGHT HAND AFT FLIGHT ATTENDANT PANEL SHORTED. REPLACED SWITCH AT RIGHT HAND AFT FLIGHT ATTENDANT PANEL FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040804000012004080400001WP 2004 8 4 AALA20040740 120040719A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21223AA 49173 DTW - OVERHEAD EMERGENCY LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000042004080400004WP 2004 8 4 AALA20040745 120040715A2170 COALESCER BAG DOUG DC9 DC983 3022083WP AIR CON SYS INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW219628W 53598 SFO - INFLIGHT T1436/15 BEFORE V1 ENGINE VALVE LIGHT ILLUMINATED AFTER ROTATION. BURNING SMELL ALONG WITH SMOKE IN CABIN WAS NOTED. EMERGENCY WAS DECLARED. LANDED SFO WITHOUT INCIDENT. INSPECTED ENGINE APU AND AIR CONDITIONING DUCTING. INSPECTED BOTH ENGINES WITH NO DISCREPANCIES NOTED. REPLACED COALESCER BAGS AND ACCOMPLISHED CARD 21-92-12 BURN OUT HIGH PRESSURE PNEUMATIC DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040804000152004080400015NM 2004 8 4 04FDEA02276 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 16R BARREL NUT BORE FOUND WITH CORROSION. CLEAN UP CORROSION AND FOUND EXCEEDED MD11 S/B LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79836, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 16R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040804000222004080400022WP 2004 8 4 AALA20040778 120040726A7997 WIRE DOUG DC9 DC982 3022082WP SENSOR LOOSE A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21293AA 49305 DFW - INFLIGHT T402/26 RIGHT ENGINE OIL TEMPERATURE WENT OFF SCALE. HIGH DURING CLIMBOUT THROUGH 27,000 FEET AT CRUISE. GAUGE WAS ERRATIC DURING DESCENT. ALL OTHER ENGINE INDICATIONS WERE NORMAL. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND GROUND WIRE TO ENGINE OIL TEMPERATURE SENSOR WAS LOOSE. SECURED LOOSE GROUND WIRE AND REPLACED TEMPERATURE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000232004080400023NM 2004 8 4 AALA20040783 120040727A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21369AA 25196 DFW - EMERGENCY LIGHT AT SEAT 30H INOPERATIVE. RESEATED LIGHT FIXTURE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040804000252004080400025NM 2004 8 4 AALA20040772 120040723A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21654A 24612 DFW - EMERGENCY LIGHTS AT L561 AND L562 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L561 AND L562. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804000272004080400027WP 2004 8 4 AALA20040776 120040725A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21513AA 49890 DFW - FORWARD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804000282004080400028NM 2004 8 4 AALA20040757 120040707A2620 EXTINGUISHER BOEING767 767323 1385205NM CARGO BAY CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21347AN 33086 AFW - AFT CARGO FIRE EXTINGUISHING SYSTEM LINES AND FILTER DRYER AND REGULATOR CLOGGED WITH CORROSION BUILD-UP. REPLACED AFT CARGO FIRE EXTINGUISHING SYSTEM LINES AND FILTER DRYER AND REGULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040804000292004080400029NM 2004 8 4 AALA20040764 120040726A21216067727 FAN BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21654A 24612 LAS - INFLIGHT T392/26 AIRCRAFT AIR INTERRUPT INTO LAS WITH BURNING SMELL AND LITE HAZE IN CABIN. LANDED WITHOUT INCIDENT. FOUND RIGHT RECIRCULATON FAN CIRCUIT BREAKER POPPED. FOUND BAD BEARINGS IN FAN. REPLACED RIGHT RECIRCULATION FAN. OPERATED BOTH ENGINES AND PACKS WITH NO SMELL FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040804000372004080400037NM 2004 8 4 AALA20040758 120040726A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21926AN 29527 TUL - BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS FAILED 15 MINUTE LOAD CHECK. REPLACED BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040804000382004080400038NM 2004 8 4 AALA20040760 120040723A2822 PUMP BOEING737 737823 13844BZNM GE CFM56 CFM567B24 NE ZONE 500 INOPERATIVE A AALAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 SW21959AN 30828 ORD - INFLIGHT T818/23 NUMBER ONE ENGINE FAILED ON LANDING ROLL OUT OR SHORT FINAL BEFORE TOUCHDOWN. REPLACED LEFT HAND ENGING HMU AND FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA16WE E00055EN 20040804000852004080400085NM 2004 8 4 SWAA042184 120040731A33501619 LAMP BOEING737 737317 138447PNM R2 DOOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040804000912004080400091 2004 8 4 SWAA042179 420040731A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29441WN 29837 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040804000952004080400095NM 2004 8 4 SWAA042151 120040728A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 484, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040804001042004080400104WP 2004 8 4 AALA20040733 120040718A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21424AA 49336 PHX - EMERGENCY LIGHTS IN COCKPIT, FORWARD ENTRY, FORWARD SERVICE DOOR AND AISLE CEILING INOPERATIVE. REPLACED BATTERY PACK B523 FOR EMERGENCY LIGHTS IN COCKPIT, FORWARD ENTRY, FORWARD SERVICE DOOR AND AISLE CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040804001282004080400128NM 2004 8 4 04FDEA01897 120040630A5712ARC4102502 RIB DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING CRACKED. RIGHT WING, FOUND OUTBOARD FLAP, ATTACHING RIB STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040804001382004080400138NM 2004 8 4 CALA0400585 120040724A53300322024T3 SKIN BOEING737 737524 1384721NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714668 28928 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT PRODUCTION LAP JOINT APPROXIMATELY FIVE FEET BELOW R-1 DOOR, STA 294, S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 229, SHEET 41. 2L72 4F RTA16WE 20040804001452004080400145EA 2004 8 4 COMA0460389 120040622A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01416CA 7450 FORWARD SIDE FS 621.00 BULKHEAD LEFT AND RIGHT FLOOR ANGLES CRACKED. REPAIRED IAW REO 601R-53-61-004. 2L72 4F RTA21EA 20040804001462004080400146NM 2004 8 4 CALA0400589 120040730A3397 WIRE BOEING737 7373T0 1384582NM EMERGENCY LIGHTSBROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2777303 23354 INSPECTION FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5-10. A BROKEN WIRE WAS FOUND AT ROW 5. REPAIRED WIRE PER WDM 33-51-01 AND AN OPERATIONAL CHECK OF THE LIGHTS WERE GOOD. 2L72 4F RTA16WE 20040804001472004080400147EA 2004 8 4 COMA0460390 120040622A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01416CA 7450 CARGO BAY LANDING CRACKED AT TWO LOCATIONS. REPAIRED IAW REO 601R-53-61-433. 2L72 4F RTA21EA 20040804001642004080400164NM 2004 8 4 CALA0400582 120040721A575165C2591117A SKIN BOEING737 7373T0 1384582NM LT WING AILERON DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND THE LT AILERON DAMAGED ON THE LOWER BONDED SKIN PANEL. THE DAMAGE WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5751-01058. 2L72 4F RTA16WE 20040804001672004080400167 2004 8 4 SWIA200413636 420040724A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07295UX 120295 AUTOPILOT WANDERS IN PITCH AXIS EXCEEDING COMMAND BARS ABOVE AND THEN BELOW. REMOVED AND REPLACED ELEVATOR SERVO. AUTOPILOT OPERATIONAL CHECK GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20040804001692004080400169 2004 8 4 SWIA200413601 420040720A22156225734002 SERVO EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07234SW9313 9313 120308 AUTOPILOT DOESN'T CAPTURE ALTITUDES. REPLACED AUTOPILOT ELEVATOR SERVO PER MM 22-10-05. OPERATIONAL CHECK GOOD PER MM 22-11-00. 2L72 4T RTA31SO 20040804001722004080400172NM 2004 8 4 CALA0400574 120040715A5312654656841 BULKHEAD BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND APB WEB CORRODED ON BOTTOM SIDE AT STA 1016, BBL 0. REPAIRED IAW ECRA 5311-01200. 2L72 4F RTA16WE 20040804001872004080400187SO 2004 8 4 SWIA200413626 120040726A4900 RELAY EMB 120 EMB120ER 3260203SO APU FEEDER BURNED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07293SW 120320 BURNING ODOR COMING FROM F/O RELAY SIDE PANEL. REPLACED APU FEEDER PROTECTOR RELAY AND BRACKET. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040804002022004080400202NM 2004 8 4 SWAA042197 120040801A533065C35764 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 510, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040805001162004080500116WP 2004 8 5 ASAA0480475 120040613A561059644202 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS2830216690 53020 YVR - PREFLIGHT CHECK, FOUND RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW COULD NOT OPEN. RESECURED UPPER CAM FOLLOWER IN TRACK. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040805001322004080500132NM 2004 8 5 ASAA0410278 120040601A531565549067 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON LOWER CHORD FLOORBEAM. REMOVED CORROSION. FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F A16WE 20040805001362004080500136NM 2004 8 5 ASAA0410315 120040708A53200507075T6 STRAP BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON STRAP, AFT CARGO BAY. REMOVED CORRODED STRAP, FABRICATED NEW STRAP AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001452004080500145NM 2004 8 5 ASAA0440124 120040507A53306540881 SKIN BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 OAK - DURING MAINTENANCE IN SEA, A GOUGE WAS NOTED ON FUSELAGE SKIN BS 1029 S-16L. GOUGE WAS BLENDED SMOOTH. MEASUREMENT 1 INCH BY 1 INCH BY .021 INCH DEEP. INSTALLED NEW REPAIR DOUBLER AND FILLER RED SRM 53-80-01 PAGE 206-211. (M) 2L72 4F RTA16WE 20040805001512004080500151NM 2004 8 5 ASAA0480447 120040522A53209911839 ANGLE DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV CHECK, FOUND SUPPORT ANGLE IS CRACKED AT FS 1463 AT LONGERON 6R. REPLACED DAMAGED ANGLE PER SRM 51-10-4. (M) 2L72 4F RT 20040805001522004080500152NM 2004 8 5 ASAA0480448 120040522A53209911839179 CLIP DOUG MD80 MD83 3023681NM FUSLEAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV-CHECK, FOUND LOWER ATTACHMENT CLIP IS CRACKED AT FS 1463 AT RIGHT SIDE OF LONGERON 3. REPLACED CLIP PER SRM 51-10-2. (M) 2L72 4F RT 20040805001532004080500153WP 2004 8 5 ASAA0480467 120040604A53105936038501 BEAM DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01977AS 53453 OKC - FOUND DURNG C-CHECK, AFT CARGO BAY DOOR JAMB FORWARD BEAM IS CORRODED ON THE INBOARD SLIDE AROUND NUMEROUS RIVETS AT FS 1155 TO 1211. REMOVED DAMAGE AND SPOT FACED AROUND FIVE FASTENERS PER EA 5310-02379. (M) 2L72 4F RTA6WE 20040805001722004080500172NM 2004 8 5 ASAA0410287 120040605A53306545778 SKIN BOEING737 737290C 138448VNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND FUSELAGE SKIN CRACKED. REPAIRED PER EA 5330-01787. (M) 2L72 4F A16WE 20040805001752004080500175NM 2004 8 5 ASAA0410335 120040712A53306545775 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE SKIN PILLOWING AND FASTENERS PULLING THROUGH. TO BE REPAIRED ON MIG-5 4843713. (M) 2L72 4F RTA16WE 20040805001762004080500176NM 2004 8 5 ASAA0410351 120040711A53306545775 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN PILLOWING STATION 727A-727B STATION 23L. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001942004080500194WP 2004 8 5 ASAA0480465 120040530A561056644202 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS2816216550 53020 LAX - PREFLIGHT CHECK, RIGHT FIRST OFFICERS SLIDING CLEARVIEW WINDOW WOULD NT OPEN. REALIGNED WINDOW. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040805001992004080500199NM 2004 8 5 ASAA0480451 120040522A57535910043 VANE DOUG MD80 MD83 3023681NM TE FLAP NICKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD VANE IS NICKED AT LEADING EDGE. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2. (M) 2L72 4F RT 20040805002002004080500200NM 2004 8 5 ASAA0480461 120040529A531099578571 DOOR FRAME DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 OKC - DURING C-CHECK, FOUND NLG CUTOUT LONGITUDINAL FRAME IS CRACKED ON LEFT SIDE AT TOP FASTENER HOLE. STOP DRILLED AND INSTALLED REPAIR ANGLE AND SHIM PER SRM 53-05. (M) 2L72 4F RT 20040805002012004080500201NM 2004 8 5 ASAA0410341 120040712A53136552928518 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORRODED STRINGER. REPAIRED STRINGER. (M) 2L72 4F RTA16WE 20040805002062004080500206NM 2004 8 5 ASAA0410312 120040706A5313655162812 STRINGER BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND DAMAGE ON STRINGER 27RT BS 915. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040809000052004080900005NM 2004 8 9 ASAA0410314 120040707A5330 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED WINDOW POST. INSTALLED DOUBLER AFTER STOP DRILLING. (M) 2L72 4F RTA16WE 20040809000262004080900026 2004 8 9 ASAA0480442 420040517A3454593442573 ELEMENT DOUG DC9 DC983 3022083WP VOR ANTENNA DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS 53450 OKC -DURING C-CHECK, FOUND VOR ANTENNA NR 6303 ELEMENT IS DELAMINATED. REMOVED AND REPLACED DAMAGED ELEMENT PER EA 3450-01030. (M) 2L72 4F RTA6WE 20040809000272004080900027NM 2004 8 9 ASAA0480463 120040529A5330591022813 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 OKC - DURING C-CHECK, FUSELAGE SKIN IS DENTED ON LEFT SIDE NEAR VERTICAL STABILIZER. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 53-01. (M) 2L72 4F RT 20040809000352004080900035NM 2004 8 9 USAASB04002 120040101A3234 SELECTOR BOEING737 737301 1384611NM MLG MALFUNCTIONED A USAAL ABORTED APPROACH O OTHER APAPPROACH 1 EA19574US 23739 CLT - FLT 229 - ON APPROACH TO CLT FROM RDU, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS DURING GEAR EXTENSION. CREW RECYCLED THE GEAR AND RAN GEAR LIGHTS DISAGREE QUICK REFERENCE HANDBOOK PROCEDURE. RECEIVED THREEE GREEN LIGHTS WITH NO RED LIGHTS AND ACCOMPLISHED A TOWER FLYBY TO DOUBLE CHECK GEAR. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE WITH NO PROBLEMS. MAINTENANCE FOUND THE GEAR SELECTOR HANDLE STICKING. CLEANED AND LUBED GEAR SELECTOR HANDLE. JACKED AIRCRAFT AND ACCOMPLISHED NUMEROUS GEAR SWINGS. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040809000362004080900036NM 2004 8 9 USAASB04006 120040108A32602732511 CABLE BOEING737 737401 1384701NM RT MLG WW OUT OF ADJUST A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19417US 23984 CLT - FLT 1191 - AFTER TAKEOFF FROM CLT, EN ROUTE TO MIA, CREW WS UNABLE OT RAISE THE LANDING GEAR SELECTOR HANDLE. CONTINUED CLIMB AND TROUBLESHOT PROBLEM. CREW PLACED GEAR SELECTOR HANDLE DOWN AND RECEIVED THREE GREEN INDICATION LIGHTS FOR THE GEAR. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING, THE AIRCRAFT STOPPED ON THE TAXIWAY TO HAVE THE GEAR PINNED. AIRCRAFT LANDING, THE AIRCRAFT STOPPED ON THE TAXIWAY TO HAVE THE GEAR PINNED. AIRCRAFT THEN TAXIED TO THE GATE. MAINTENANCE FOUND THE GROUND SPOILER TELEFLEX CABLE OUT OF ADJUSTMENT. READJUSTED CABLE PER MM 27-62-51 AND PERFORMED GEAR SWING. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040809000402004080900040EA 2004 8 9 ASOA04241 120040326A5311 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FRAME CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11849AS 7347 DURING AN A-CHECK IN BTR, THE LEFT SIDE FS 640 FRAME DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE FS 640 FRAME DOUBLER. (M) 2L72 4F RTA21EA 20040809000412004080900041WP 2004 8 9 GTIA040549 120040528A3260 UPLOCK SENSOR DOUG DC9 DC982 3022082WP MLG OUT OF ADJUST A GTIAK NONE N FALSE WARNING ININSP/MAINT 1 GL23820NK 49126 ORD - FLT 1525 - FOUND LEFT MAIN GEAR INDICATES UNSAFE, RED LIGHT, WITH GEAR HANDLE UP DURING CLIMB AND CRUISE ONLY. T/S LEFT INDICATING SYSTEM CHECKED AIR GAPS ON MAIN GEAR LEFT UPLOCK, DOOR OPEN, AND DOWNLOCK PROX SENSORS. FOUND LEFT UPLOCK SENSOR OUT OF ADJUST TO WIDE ADJ PROX SENSOR. PERF PROX BITE CHECK OF EFFECTIVE SENSOR, NO FAULTS NEAR FAR PASS. (M) 2L72 4F A6WE 20040809000442004080900044EU 2004 8 9 TRBA2004023 120040319A612030048000018 AUTOFEATHER SYS AEROSPATR72 ATR72 EU LT ENGINE FAILED A TRBAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO21438AT 438AT ON CLIMB, AROUND 6000 FEET, LEFT ENGINE LOST TORQUE (POWER) AND ITT DROPPED TO 480 DEGREE. ENGINE WAS SHUTDOWN AND CREW PROCEEDED WITH EMERGENCY PROCEDURES. REMOVED AND REPLACED AUTO-FEATHER UNIT. (M) 2H72 4T RT 20040809000482004080900048EA 2004 8 9 A6WA200440034 120040325A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31425AW 7663 MAINTENANCE WORK CARD NR 14, FOUND THE RIGHT OBLIQUE ANGLE IS CRACKED AT FS 625.3 ADJACENT TO STRINGER 14R AT WATERLINE 95. (M) 2L72 4F RTA21EA 20040809000492004080900049CE 2004 8 9 2004F00169 120040326A2612 WARNING LIGHT CESSNA208 208B 2073701CE ENGINE FIRE DET INTERFERENCE A COEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM13880FE 208B0215 ENGINE FIRE LIGHT BLINKED ON TWICE FOR ONE SECOND AND EACH TIME THAT HAPPENED THE HORN CHIRPED. PILOT RETURNED TO MFR WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS INSPECTED WITH NO DEFECTS FOUND. FIRE WARNING SYSTEM TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1H71 3T A37CE 20040809000502004080900050EU 2004 8 9 ASOA04306 120040427A3350LP1670 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11637AS 383 FLT 4135 - DUIRNG A GROUND INSPECTION IN VPS, THE AFT SECOND TO LAST EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT SECOND TO LAST EMERGENCY FLOOR LIGHT LAMPS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040809000542004080900054EU 2004 8 9 ASOA04318 120040413A5315 FLOORBEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURNG A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 40 IAW SRM 51-25-01. (M) 2H72 4T RT 20040809000582004080900058NM 2004 8 9 2004F00170 120040314A2910 LINE BOEING737 737201 1384454NM A-HYD SYSTEM LEAKING A RYNAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE07240AU 22355 DURING CRUISE FROM GSO-ACY, EXPERIENCED A LOSS OF THE A-SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT ACY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC FEED LINE. CONDUCTED 'A' SYSTEM TROUBLESHOOTING PROCEDURES FOR PUMP STARVATION. OPS LEAK CHECKED NORMAL. (M) 2L72 4F A16WE 20040809000612004080900061NM 2004 8 9 2004F00173 120040205A5754 DOUBLER BOEING727 727222 1384073NM NR 8 SLAT CRACKED A RYNAK NONE O OTHER ININSP/MAINT 1 CE077638U 19911 AT C-CHECK, FOUND RIGHT WING NR 8 SLAT ACTUATOR ATTACH OUTER OUTBOARD FRAME LAYER IS CRACKED WING LEADING EDGE CAVITY. FABRICATE, PRIMED AND INSTALL NEW DUOBLER REPAIR AT RIGHT WING NR 8 SLAT ACTUATOR. (M) 2L73 4F A3WE 20040809000622004080900062EU 2004 8 9 USAASA04024 120040312A259765757101 CABLE AIRBUS320 A320214 3930316EU AFT CARGO BAY BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19113UW 1141 THE LEFT OVERWING SLIDE BOTTLE CABLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE LT OVERWING SLIDE BOTTLE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040809000632004080900063NM 2004 8 9 USAA040023 120040112A5347 SEAT TRACK BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 2 INCHES BY .090 INCHES, STATION 337, WL 200, RBL 98 ON TRANSITION ANGLE JUST AFT OF FORWARD SVC DOOR OPENING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER DWG 141T5121. (M) 2L72 4F RTA1NM 20040809000642004080900064NM 2004 8 9 DL76L040685 120040722A3350GE767 LAMP BOEING767 767332 1382001NM EMERGENCY SLIDE INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27178DN 25143 OVERWING EMERGENCY SLIDE LIGHT ON AFT RT SIDE INOPERATIVE RELAMPED LIGHT. 2L72 4F RTA1NM 20040809000652004080900065NM 2004 8 9 DL738040686 120040721A5330141A372124 SKIN BOEING737 737832 13844CFNM FUSELAGE PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO273752 29670 THE FUSELAGE SKIN WAS PUNCTURED JUST AFT OF THE FS 178 BULKHEAD BELOW WL 234 FROM CONTACT WITH A JETWAY. THE DAMAGE WAS REMOVED WITH A 8.25 X 4.5 INCH CUTOUT AND REPAIRED WITH AN INTERNAL REPAIR DOUBLER PER ER/A 091962-14, REV A. 2L72 4F RTA16WE 20040809000662004080900066NM 2004 8 9 DL738040687 120040721A5312141A21728 BULKHEAD BOEING737 737832 13844CFNM FUSELAGE PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO273752 29670 THE FS 178 BULKHEAD ASSY WAS DAMAGED BY CONTACT WITH A JETWAY AT WL 230 NEAR RBL 30. THE RBL 17 BEAM, THE UPPER BULKHEAD AND RT SIDE CHORD WERE DAMAGED AND REPLACED. THE BULKHEAD WEB DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO ALUMINUM REPAIR DOUBLERS PER ER/A 091837 -14, REV A. 2L72 4F RTA16WE 20040809000682004080900068NM 2004 8 9 DL76L040689 120040723A324026124121A BRAKE BOEING767 767332 1382001NM NR 7 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 BRAKE DELAMINATED. REPLACED BRAKE. 2L72 4F RTA1NM 20040809000692004080900069NM 2004 8 9 DL757040690 120040724A2530 ODOR BOEING757 757232 1384965NM AFT CABIN DETECTED A DALAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SO27607DL 22814 ON TAXI OUT UNIDENTIFIED ODOR POSSIBLY ELECTRICAL NOTED IN AFT PART OF A/C NEAR AFT F/A. UNABLE TO CONFIRM, IDENTIFY, OR LOCATE SOURCE. CHECKED FOR ODOR IN AFT CABIN AREA, NONE FOUND. CHECKED AFT CARGO COMPT AND AFT E/E RACK, NO ODOR DETECTED. 2L72 4F RTA2NM 20040809000712004080900071EA 2004 8 9 COMA0470055 120040629A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01354CA 10064 FLIGHT 5086 LEFT THRUST REVERSER UNSAFE MESSAGE DURING T/O. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040809000722004080900072NM 2004 8 9 DL76G040708 120040729A1430 BOLT BOEING767 7673P6 1385105NM MLG WHEEL SHEARED A DALAO OTHER O OTHER LDLANDING 1 SO27154DL DL1566 25241 NR 3 MLG WHEEL MISSING TIE BOLT. REPLACED WHEEL ASSY. 2L72 4F RTA1NM 20040809000762004080900076EA 2004 8 9 COMA0460422 120040720A801035051889 STARTER CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01729CA191584395 7265 FLIGHT 5782 RIGHT STARTER CUTOUT CAUTION. REPLACED THE ATS. 2L72 4F RTA21EA 20040809000772004080900077EA 2004 8 9 COMA0460413 120040713A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01989CA 7215 FLIGHT 5518 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040809000782004080900078EA 2004 8 9 COMA0460414 120040713A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01989CA16307683 7215 FLIGHT 5890 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040809000792004080900079EA 2004 8 9 COMA0460416 120040714A531160034017 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01713CA14920 7245 DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW COMAIR EA 10-5310-00389. 2L72 4F RTA21EA 20040809000802004080900080EA 2004 8 9 COMA0460417 120040717A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01708CA 7235 FLIGHT 4938 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040809000822004080900082EA 2004 8 9 COMA0460395 120040627A2613601R31039162 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG WW MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01816CA5538 7398 MLG OVERHEAT MESSAGE. REPLACED THE RT MLG WHEEL BIN. 2L72 4F RTA21EA 20040809000832004080900083EA 2004 8 9 COMA0470054 120040625A7830 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01369CA 10079 LEFT THRUST REVERSER UNSAFE CAUTION MESSAGE. DEFERRED MAINT ON THRUST REVERSER PER MEL. 2L72 4F RTA21EA 20040809000842004080900084NM 2004 8 9 DL757040709 120040730A5330143N31212 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27664DN 25012 MULTIPLE FUSELAGE SKIN REPAIRS BETWEEN STATION 672 AND 692 AT STR 2R COMBINED INTO ONE REPAIR. REPAIR IAW ERA 091861-14. 2L72 4F RTA2NM 20040809000852004080900085 2004 8 9 COMA0460423 420040718A34406229302004 RADAR CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01491CA4187 7756 FLIGHT 5325 RADAR FAULT MESSAGE. REPLACED THE RADAR UNIT. 2L72 4F RTA21EA 20040809000862004080900086NM 2004 8 9 SWAA042227 120040805A335065C27093 LIGHT BOEING737 7372T4 1384492NM CABIN LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT, LOOSE. SECURED EMERGENCY EXIT LIGHT PER MM. 2L72 4F A16WE 20040809000882004080900088NM 2004 8 9 SWAA042229 120040805A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, RBL 24 TO RBL 26, WL 158, CORRODED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040809000892004080900089NM 2004 8 9 SWAA042230 120040805A53116545808 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 294, RBL 54, CORRODED. REMOVED AND REPLACED STUB FRAME PER SRM. 2L72 4F RTA16WE 20040809000902004080900090 2004 8 9 SWAA042231 420040805A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED GIRT BAR CABLE PER MM. 2L72 4F RTA16WE 20040809000912004080900091NM 2004 8 9 SWAA042232 120040805A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040809000932004080900093NM 2004 8 9 SWAA042234 120040805A52106969854 DOOR FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR AFT LOWER FRAME AT LOWER STOP, CRACKED. REMOVED AND REPLACED LOWER FRAME PER BAC DRAWING. 2L72 4F RTA16WE 20040805001082004080500108WP 2004 8 5 ASAA0480437 120040517A5320993658045 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 DURING C-CHECK, FOUND INTERCOSTAL IS CRACKED ON UPPER FLANGE AT FS 1287-1307. REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2L72 4F RTA6WE 20040805001122004080500112WP 2004 8 5 ASAA0480457 120040529A53219936639501 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT G-3 AND G-4 GALLEYS. REBONDED PANELS PER MM 25-00-00. (M) 2L72 4F A6WE 20040805001132004080500113WP 2004 8 5 ASAA0480458 120040529A532199365811 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC - DURING C-CHECK, FOUND FLOOR PANEL DELAMINATED AT ROWS 20 AND 21. REBONDED PANELS PER MM 25-00-00. (M) 2L72 4F A6WE 20040805001222004080500122NM 2004 8 5 ASAA0410280 120040630A531565549067 FLOORBEAM BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND CORROSION ON LOWR CHORD FLOORBEAM. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EA5310-02377. (M) 2L72 4F A16WE 20040805001272004080500127NM 2004 8 5 ASAA04100284 120040603A52306554918 STIFFENER BOEING737 737290C 138448VNM CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 FOUND MAIN CARGO DOOR STIFFENER COMMON TO TORQUE TUBE MOUNT IS GOUGED. REMOVED, FABRICATED AND INSTALLED STIFFENER IAW 51-30-2. (M) 2L72 4F A16WE 20040805001392004080500139WP 2004 8 5 ASAA0480466 120040602A561059644202 WINDOW DOUG DC9 DC983 3022083WP COCKPIT STUCK A ASAAK NONE O OTHER ININSP/MAINT 1 NM01974AS2816216550 53450 SEA - RIGHT SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. TIGHTENED NUT ON UPPER GUIDE RAIL. WINDOW THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040805001432004080500143NM 2004 8 5 ASAA0440122 120040507A5320BAC1496377 ANGLE BOEING737 7374Q8 138447QNM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01775AS 25108 OAK - FOUND AFT CARGO COMPARTMENT RIGHT Z-ANGLE CORRODED STATION 727D TO 747. REMOVED AND REPLACED Z-ANGLE RT STATION 727D TO 747. (M) 2L72 4F RTA16WE 20040805001492004080500149WP 2004 8 5 ASAA0480194 120040325A53505961568 CAM DOUG DC9 DC983 3022083WP TAILCONE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 OKC - FOUND TAILCONE EMERGENCY SLIDE FAILED TO DEPLOY DURING SLIDE DEPLOYMENT TEST PER WORK CARD 28625000. THE FAILURE WAS ATTRIBUTED NOT TO THE SLIDE ASSEMBLY, BUT TO A BROKEN TAILCONE JETTISON AND HOISTING CONTROL CAM. THE CAM WAS REPLACED, BUT THE DEPLOYMENT TEST WAS DEFERRED TO THE NEXT MD-80 AIRCRAFT IN CHECK. (M) 2L72 4F RTA6WE 20040805001502004080500150NM 2004 8 5 ASAA0480446 120040522A57545937422501 SKIN DOUG MD80 MD83 3023681NM SLAT GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV-CHECK, FOUND LEFT NR 0 SLAT INBOARD UPPER SKIN IS GOUGED AT AFT CORNER. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 57-09. (M) 2L72 4F RT 20040805001592004080500159NM 2004 8 5 ASAA0410289 120040605A523065622311 FITTING BOEING737 737290C 138448VNM CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01742AS 23136 PAE - FOUND MAIN CARGO DOOR NR 2 AFT LATCH FITTING HAS ELONGATED HOLES. REMOVED AND REPLACED FITTING. (M) 2L72 4F A16WE 20040805001672004080500167NM 2004 8 5 ASAA0410300 120040627A53206545413111 FLANGE BOEING737 737298C 1384490NM FUSELAGE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 FOUND RIGHT A/C BAY LOWER TEE CHORD INBOARD FLANGE WORN FROM A/C BAY DOOR LATCH STATION 570, LOWER T-CHORD FOR WING CENTER SECTION BEAM RBL 41. REMOVED, FABRICATED, AND INSTALLED NEW LOWER T-CHORD. (M) 2L72 4F RTA16WE 20040805001732004080500173NM 2004 8 5 ASAA0410317 120040707A523050797897 DOOR BOEING737 737298C 1384490NM OVERWING EXIT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND RIGHT OVERNIGHT EXIT REPLACED DUE OT MULTIPLE CORROSION AND STRUCTURE DEFECTS. REMOVED AND REPLACED RIGHT OVERWING EXIT. (M) 2L72 4F RTA16WE 20040805001852004080500185NM 2004 8 5 ASAA0410326 120040709A53306545774552 SKIN BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STATION 764 4 INCHES BELOW STRINGER 19L. REPAIRED SKIN. (M) 2L72 4F RTA16WE 20040805001882004080500188NM 2004 8 5 ASAA0410325 120040709A53136582928 STRINGER BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION ON STRINGER 22L AFT CARGO BAY. REMOVED DAMAGED STRINGER, FABRICATED NEW STRINGER AND REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040805001932004080500193NM 2004 8 5 ASAA0410337 120040712A53306545775561 SKIN BOEING737 737298C 1384490NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND THREE SKIN BLEND OUTS OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER. (M) 2L72 4F RTA16WE 20040805001952004080500195WP 2004 8 5 ASAA0480455 120040529A5311593639517 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 OKC- DURING C-CHECK, FOUND RIGHT MLG AFT OUTBOARD CORNER FRAME CHANNEL REPAIR T-CRACKED. REPLACED PREVIOUS REPAIR PER SRM 53-05. (M) 2L72 4F A6WE 20040805001972004080500197NM 2004 8 5 ASAA0480449 120040522A53135936432507 LONGERON DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01979AS 53471 OKC - DURING HV-CHECK, FOUND LONGERON 28R CORRODED AROUND FASTENERS IN AFT CARGO BAY AT FS 1079. REMOVED CORROSION AND APPLIED PROTECTIVE TREATMENT PER EA 5310-02364. (M) 2L72 4F RT 20040805002042004080500204NM 2004 8 5 ASAA0410329 120040709A531065465952 SHEAR TIE BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CRACK ON FRAME SHEAR TIE REPAIR. REPLACED SHEAR TIE. (M) 2L72 4F RTA16WE 20040805002052004080500205NM 2004 8 5 ASAA0410330 120040709A5314656212528 KEELBEAM BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND KEEL BEAM IS CORRODED FROM BS 500B TO 520 RT. REMOVED AND REPLACED KEEL BEAM. (M) 2L72 4F RTA16WE 20040809000022004080900002NM 2004 8 9 ASAA0410311 120040706A532065458953 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 FOUND STRINGER 27R BS 908 SPLICE CAP HAS OVERSIZED HOLES. REMOVED AND REPLACED SPLICE CAP. (M) 2L72 4F RTA16WE 20040809000042004080900004NM 2004 8 9 ASAA0410343 120040712A53306573742 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND CORROSION, FUSELAGE OUTER SKIN AFT OF BUTT SPLICE STATION 907 STRINGR 25L TO 25R. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040809000102004080900010NM 2004 8 9 AMTA200400741 120040614A2613 LOGIC CARD BOEING757 75733N 1384931NM OVERHEAT SYS MALFUNCTIONED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11557TZ 32591 EICAS STATUS MSG R ENG OH LP2 DISPLAYED. TROUBLESHOT DISC PER FIM 26-11-11. REMOVED AND REPLACED AFLOTS CARD. SYSTEM OPS NORMAL. NO OTHER DISCREPANCIES FOUND. (M) 2L72 4F RTA2NM 20040809000172004080900017NM 2004 8 9 USAA040304 120040615A573065C2660399 SKIN BOEING737 737301 1384611NM WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 PIT - FOUND WING DELAMINATION 1 SQUARE INCH, NR 3 SLAT INBOARD END TRAILING EDGE. REMOVED DAMAGE, INSTALLED FILLER INTERNAL DOUBLER AND NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20040809000182004080900018NM 2004 8 9 USAA040303 120040603A552265C2574613A SKIN BOEING737 737301 1384611NM LT ELEVATOR DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US 23740 PIT - FOUND SKIN DENTED WITH DELAMINATION TWO AREAS 2 INCHES BY 1.5 INCH AND 1 INCH BY 1.375 INCH AREA, LEFT ELEVATOR LOWER SURFACE BETWEEN 176/200. REMOVED DISBONDED SKIN AND CORE, REPLACED CORE MATERIAL AND NEW DOUBLERS PER SRM 55-20-01 AND EA 78563. (M) 2L72 4F RTA16WE 20040809000252004080900025NM 2004 8 9 ASAA0480462 120040529A531099578572 DOOR FRAME DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01981AS 53472 OKC - DURING C-CHECK, FOUND NLG CUTOUT LONGITUDINAL FRAME IS CRACKED ON RIGHT SIDE AT TOP FASTENER HOLE. STOP DRILLED AND INSTALLED REPAIR ANGLE AND SHIM PER SRM 53-05. (M) 2L72 4F RT 20040809000342004080900034NM 2004 8 9 USAASB04003 120040101A4930655280131 CONTROL UNIT BOEING737 737401 1384701NM APU MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19405US 23885 CLT - FLT 684 - FLIGHT DEPARTED CLT WITH THE NR 2 ENGINE CSD ON MEL 24-1 FOR LEAKING OIL. DURING CLIMB, AT FL220, THE APU AUTO SHUT-DOWN DUE TO AN OVERSPEED CONDITION. THE FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE CSD (P/N 735511A) AND REMOVED MEL 24-1. ACCOMPLISHED APU PERFORMANCE CHECK PER JOB CARD JK-049. ALL READINGS NORMAL. HOWEVER, APU FAILED IN FLIGHT START CHECK. APU SHUTDOWN FOR OVERSPEED AFTER ONE MINUTE OPERATION WHILE DESCENDING TO FL290. MAINTENANCE REMOVED AND REPLACED THE M280 APU CONTROL UNIT. OPS CHECK GOOD PER MM. NO FAULTS NOTED. (M)(M) 2L72 4F RTA16WE 20040809000522004080900052EU 2004 8 9 ASOA04320 120040413A5315 FLOORBEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURNG A C-CHECK IN YUL, THE FLOORBEAM AT FS 36 FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 36 IAW SRM 51-25-01. (M) 2H72 4T RT 20040809000602004080900060NM 2004 8 9 2004F00172 120040204A3230656021132 ACCESSORY UNIT BOEING727 727222 1384073NM E/E BAY FAULTY A RYNAO OTHER J WARNING INDICATION APAPPROACH 1 CE077640U 19913 ON APPROACH INTO DAY, UNSAFE RIGHT MAIN LANDING GEAR INDICATION. RED LIGHT WAS ILLUMINATED. GEAR WS VISUALLY VERIFIED DOWN BY THE TOWER. ACCOMPLISHED APPROPRIATE CHECKLIST FOR UNSAFE GEAR. RECYCLED GEAR SECOND TIME AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED DAY WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX. (M) 2L73 4F A3WE 20040809000872004080900087NM 2004 8 9 SWAA042228 120040805A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040809000942004080900094NM 2004 8 9 SWAA042235 120040805A53306545857 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT R2 DOOR CUTOUT AFT LOWER CORNER, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040809000952004080900095NM 2004 8 9 SWAA042236 120040805A3350101114 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040809000992004080900099NM 2004 8 9 DL757040710 120040730A5330146N31111 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27665DN 25013 FUSELAGE SKIN REPAIR AT SKY RADIO ANTENNA CUTOUT AT BL 0 AND STA 1360. REPAIR IAW ERA 091886-14. 2L72 4F RTA2NM 20040809001022004080900102NM 2004 8 9 DLM88040713 120040801A26128762963 CARTRIDGE DOUG MD88 MD88 3023688NM CARGO WILL NOT TEST A DALAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO27956DL 49887 GREEN LIGHT ON SQUIB 2 AFT CARGO FIRE WILL NOT TEST, LIGHT CHECKS GOOD. T/S PER M/M AND FOUND NR 2 BOTTLE AFT SQUIB BAD. REPLACED SQUIB PER M/M. 2L72 4F RTA6WE 20040809001032004080900103 2004 8 9 DL76G040714 420040802A256560231002 INFLATOR BOEING767 7673P6 1385105NM OVERWING SLIDE UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27152DL14850 24984 WORKING C/N C07234480 REPLACE LEFT SIDE OVERWING SLIDE INFLATOR S/N DL257. DISARMED LEFT SIDE OVERWING SLIDE PER M/M 25-65-02-004-001. REPLACED SLIDE INFLATOR. ARMED LEFT SIDE OVERWING SLIDE PER M/M 25-65-00-442-010 STEP 6 OF THE M/M, C/W SQUIB TEST, NR 2 EMG DID NOT TEST. FOUND ACTUATOR EXTENDED AND SQUIB FIRED. NOTE SPOILER WAS IN THE STOWED POSITION. REPLACED SPOILER ACTUATOR OVERRIDE OFF WING ESCAPE SLIDE. 2L72 4F RTA1NM 20040809001052004080900105NM 2004 8 9 DL764040716 120040803A2410 GENERATOR BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 1 ENGINE INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27829MH 29700 706163 LEFT GEN DRIVE LIGHT CAME ON AFTER TAKEOFF AND IDG WAS SUBSEQUENTLY DISCONNECTED ACCORDING TO THE QRH. BPCU FAULTED LEFT GEN OVER FREQ CODE 24-355-01 AND 24-314-11 OVER FREQ. REPLACED LEFT GCU. RAN ENGINE, LEFT ENG GEN SYS CHECK NORMAL. 2L72 4F4 FRTA1NM E13NE 20040809001082004080900108EA 2004 8 9 COMA0460391 120040623A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01436CA 7482 DURING FLIGHT RECEIVED A FLAP CAUTION MESSAGE. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES. 2L72 4F RTA21EA 20040809001092004080900109NM 2004 8 9 DL73S040658 120040715A555365468747 FITTING BOEING737 737247 138448DNM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 VERTICAL STABILIZER NR 5 FIN LUG AFT FACE CORRODED. REPAIRED IAW ERA 091628-14. 2L72 4F A16WE 20040809001112004080900111NM 2004 8 9 DL777040660 120040714A21214100943C FAN BOEING777 777232 1385232NM LWR BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27860DA 29951 FOUR HRS INTO FLT F/A SMELLED ELEC ODOR IN CABIN MID GALLEY AREA SMELL DISSIPATED, 30 MIN LATER SMELL RETURNED AND THERE WAS A RECIRC FAN STATUS MSG IN COCKPIT. TURNED BOTH RECIRC FANS OFF AND ODOR DISSIPATED. MTC MSG 21-24700 RECORDED FOUND RT LWR REC FAN INOP. NOTED BURNING ODOR UPON REMOVAL. INSTALLED NEW FAN PER M/M, OPS NORMAL MAT SYS TEST PASS OK FOR SERVICE. 2L72 4F RTT00001SE 20040809001122004080900112NM 2004 8 9 DL75A040662 120040715A5330 SKIN BOEING757 757212 1384951NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27750AT 23126 FUSELAGE, SKIN L1 DOOR CUTOUT, UPPER FWD CORNER REPAIR OF CRACK FATIGUE CRACK FOUND DURING INSPECTION OF THE L1 DOOR CUTOUT. ERA WAS GENERATED INSTALLING A REPAIR DOUBLER, TRIPLER AND QUADRUPLER TO REPAIR THE DAMAGE. ERA 097855-14AD REVISION ORIGINAL 2L72 4F RTA2NM 20040809001132004080900113NM 2004 8 9 DL767040663 120040715A5711112T20011 FITTING BOEING767 767232 1385132NM LT WING SPAR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27114DL 22226 LEFT WING FRONT SPAR OUTBOARD PITCH LOAD FITTING HAS TWO DAMAGED HOLES DUE TO TOOLING WHILE ACCOMPLISHING EO 01-074906-03AD. REPAIR IAW ERA 091345-14AD. 2L72 4F RTA1NM 20040809001162004080900116EA 2004 8 9 COMA0460407 120040709A2613 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01798CA264528308 7348 FLIGHT 5017 GEAR BAY OVERHEAT WARNING. REPLACED THE RIGHT WHEEL WELL BIN ASSY. 2L72 4F RTA21EA 20040809001182004080900118EA 2004 8 9 COMA0460408 120040711A3240158863 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA MLG BRAKE MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01712CA27 7244 FLIGHT 5724 PARKING BRAKE SOV CAUTION MESSAGE. REPLACED THE PARKING BRAKE SOV. 2L72 4F RTA21EA 20040809001212004080900121NM 2004 8 9 DL777040721 120040803A7330 FILTER BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 1 ENGINE CONTAMINATED A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27877DA 29739 051360 EICAS MSG ENGINE FUEL FILTER LT OCCURRED INTERMITT, EICAS MSG ENGINE FUEL FILTER LT OCCURRED MOMENTARILY DURING CLIMBOUT. T/S PER FIM 73-11 TASK 801. REPLACED LT ENGINE FUEL FILTER PER MM. RAN ENGINE, LEAK CHECK GOOD. 2L72 4F4 FRTT00001SEE00050EN 20040809001222004080900122NM 2004 8 9 DL764040722 120040804A7330 PRESSURE SWITCH BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27828MH 29699 706193 RT ENGINE FUEL FILTER MSG ON T/O CLIMB. T/S PER FIM. NO CONTAMINATION FUEL FILTER. REPLACED FUEL DIFF PRESS SW BORROWED FROM CAL. OPERATED ENG PER PFHB, NO DISCREPANCIES. 2L72 4F4 FRTA1NM E13NE 20040809001242004080900124NM 2004 8 9 DL76G040666 120040717A5330143T35622 SKIN BOEING767 767332 1382001NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO271602 29694 ER/A 092012-14 REV A: FUSELAGE SKIN STA 698 S-35R REPAIR OF GOUGES. DUE TO SERVICE DAMAGE, THE FUSELAGE SKIN WAS FOUND GOUGED AND SCRATCHED AT FS 698 ADJACENT TO STRINGER 35R. AN APPROX 8.25 INCHES WIDE X 6 INCHES TALL SKIN CUTOUT WAS REQUIRED TO REMOVE THE DAMAGE. ER/A ACCOMPLISHES A REPAIR CONSISTING OF INSTALLATION OF AN EXTERNAL REPAIR DOUBLER. 2L72 4F RTA1NM 20040809001252004080900125NM 2004 8 9 DL767040723 120040804A335020131 BATTERY BOEING767 767232 1385132NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27112DL 22224 ON SERVICE CHECK FOUND LT SIDE AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER M/M, CHECKS GOOD. 2L72 4F RTA1NM 20040809001272004080900127NM 2004 8 9 DL767040725 120040804A335020131 BATTERY BOEING767 767232 1385132NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27112DL 22224 ON SERVICE CHECK FOUND RT AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER PER M/M. CHECKS GOOD. 2L72 4F RTA1NM 20040809001282004080900128NM 2004 8 9 DL767040726 120040804A335020121 CHARGER BOEING767 767232 1385132NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27112DL 22224 ON SERVICE CHECK FOUND RT AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND BATTERY CHARGER PER M/M. CHECKS GOOD. 2L72 4F RTA1NM 20040809001302004080900130NM 2004 8 9 DL757040728 120040805A5330146N35318 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27665DN 25013 FUSELAGE SKIN CORRODED AT STATION 1510 AND STR 28R - 29R. REPAIRED IAW ERA 091976-14. 2L72 4F RTA2NM 20040809001322004080900132NM 2004 8 9 DL757040730 120040805A5330146N31111 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE L NO TEST ININSP/MAINT 1 SO27665DN 25013 FUSELAGE SKIN SUFFERED LIGHTNING STRIKE DAMAGE AT STATION 1208 AND STR 2R. REPAIRED IAW ERA 091963-14. 2L72 4F RTA2NM 20040809001362004080900136NM 2004 8 9 DL76G040667 120040718A4900BA0601 BATTERY BOEING767 7673P6 1385105NM APU FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27154DL 25241 CATERING REPORTED SMOKE TO F/A WENT BACK AND SMELLED SMOKE ABOUT 4 ROWS PRIOR TO THE AFT BULKHEAD. OTHER CREW MEMBERS ALSO NOTICED THE ODOR. FIRST F/A ALSO REPORTED SEEING SMOKE IN THE AFT PART OF THE AIRCRAFT. ISOLATED MAIN ODOR TO APU BATTERY OVERHEATING. REPLACED APU BATTERY AND APU BATTERY CHARGER PER MM. 2L72 4F RTA1NM 20040810000012004081000001WP 2004 8 10 ASAA0480282 120040418A335060030451 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 PDX - FOUND DURING LINE CHECK, EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 1 TO 8. REPLACED ASSOCIATED BATTERY PACK, POWER SUPPLY. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040810000022004081000002WP 2004 8 10 ASAA0480281 120040418A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 PDX - FOUND ON LINE CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE AT ROW 22. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040810000052004081000005NM 2004 8 10 GAIA04086OP 120040710A3350 BULB BOEING727 727251 138408HNM EMERGENCY LIGHTINOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07278US 21157 EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED AND CLEANED BATTERY CONTACTS, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040810000062004081000006NM 2004 8 10 ASAA0440128 120040510A533065C329541 SKIN BOEING737 737490 1384715NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND LOWER FUSELAGE BELLY SKIN HAS DENT AFT OF FRAME AT FS 767 BETWEEN STRINGER 27L AND 27R. TRIMMED OUT DAMAGED AREA AND REINSTALLED REPAIR DOUBLER PER SRM 53-00-01 DETAIL 11 PAGE 368 AT STATION 767 BETWEEN STRINGER 27L AND 27R LOWER FUSELAGE. (M) 2L72 4F RTA16WE 20040810000072004081000007WP 2004 8 10 ASAA0480236 120040405A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE UP TO ROW 7. REPAIRED SHORTED CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040810000102004081000010NM 2004 8 10 ASAA0440129 120040514A533065C329541 SKIN BOEING737 737490 1384715NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND LWER FUSELAGE BELLY SKIN HAS DENT AFT OF FRAME AT STATION 807 BETWEEN STRINGER 27L AND 27R. REMOVED DAMAGED AREA AND REINSTALLED DOUBLER PER SRM 53-00-01, DETAIL XI PG 368 AT STATION 807 BETWEEN STRINGER 27L AND 27R. LOWER FUSELAGE BELLY SKIN. (M) 2L72 4F RTA16WE 20040810000122004081000012EU 2004 8 10 ASAA0440137 220040613A7250 NOZZLE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU NR 1 TURBINE SECDAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01706AS 28894 7195 FOUND LEFT NR 1 ENGINE EXHAUST NOZZLE AND PLUG ROTOR AND STATOR HAVE SUSTAINED SEVERE DAMAGE, RIPPED AND TORN BLADE SEGMENTS WITH MISSING MATERIAL. REMOVED AND REPLACED ENGINE PER T/C'S 4855400 AND 48571016. (M) 2L72 4F4 FRTA16WE E21EU 20040810000132004081000013NM 2004 8 10 ASAA0440131 120040514A531165465502 FRAME BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND AFT PIT STAITON 787 LEFT SIDE FRAME ZEE ANGLE ATTACHMENT HOLES ARE DAMAGED. REMOVED DAMGAED AREA AT FS 787 LEFT FRAME. FABRICATED REPAIR REF SRM 51-70-11. TREATED, PRIMED AND APPLIED TOPCOAT, REF 51-20-01, AND INSTALLED REPAIR REF 51-40-02. (M) 2L72 4F RTA16WE 20040810000142004081000014NM 2004 8 10 ASAA0440121 120040509A531565C339504 FLOORBEAM BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND BS 986.5 FLOORBEAM IS CORRODED RBL 8 TO RBL 44. SPLICED IN NEW UPPER CAP OF TEE CHORD FLOORBEAM FROM RBL 8 TO RBL 53. (M) 2L72 4F RTA16WE 20040810000152004081000015NM 2004 8 10 ASAA0440120 120040509A531565C339482 FLOORBEAM BOEING737 737490 1384715NM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND BS 947.5 FLOORBEAM IS CORRODED LBL 20 TO RBL 20. REPAIRED FLOORBEAM IAW REO A00224. (M) 2L72 4F RTA16WE 20040810000172004081000017NM 2004 8 10 ASAA0440135 120040606A533065326031 SKIN BOEING737 737490 1384715NM FUSLAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01791AS 28886 SEA - FOUND BAGGAGE CART STRUCK AIRCRAFT AFT DRAIN MAST AND FUSELAGE SKIN. THREE SCRATCHES JUST ABOVE POTABLE WATER SERVICE DOOR. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA .004 DEEP, 1 INCH LONG. BLENDED DAMAGED AREA AND ALODINED PER EA 5330-10789. (M) 2L72 4F RTA16WE 20040810000182004081000018NM 2004 8 10 ASAA0440132 120040523A52466545778 ACCESS PANEL BOEING737 737490 1384715NM FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 PAE - FOUND SCRATCH DAMAGE JUST AFT OF AFT LAVATORY SERVICE PANEL, SCRATCHES WERE BLENDED AND FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-00-01. REPAIRED SCRATCH/GOUGE AT STAITON 1006/STRINER 25R. (M) 2L72 4F RTA16WE 20040810000192004081000019EA 2004 8 10 A6WA200440106 120040717A5753 VANE CNDAIRCL600 CL6002B19 1900309EA TE FLAP CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31429AW 7711 RIGHT INBOARD FLAP VANE AT FLAP STATION 60.005 IS CHAFED .012 INCH DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP VANE BY REMOVING INBOARD END LEADING EDGE SKIN AND INSTALLING NEW LEADING EDGE SKIN, P/N 601R14303-54 IAW CRJ SRM 51-42-13. (M) 2L72 4F RTA21EA 20040810000212004081000021EA 2004 8 10 6WA200440101 120040711A2150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK ILLUMINATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31470ZW 7927 FOUND LEFT PACK HIGH PRESSURE CAS MESSAGE. (M) 2L72 4F RTA21EA 20040810000232004081000023NE 2004 8 10 USAABB04063 220040703A753232143043 BLEED VALVE BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE RT ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 EA19600AU 22192 MIA - FLT 1463 - WITH THE LEFT PACK ON MEL, DESCENDING FROM FL350, THE RIGHT BLEED SYSTEM BLEED LIGHT ILLUMINATED. THE BLEED SYSTEM WAS RESET, BUT TRIPPED OFF AGAIN. THE CABIN ALTITUDE BEGAN TO CLIMB. THE AIRCRAFT DESCENDED TO 10,000 FEET AND DIVERTED TO MIA. MAINTENANCE REPLACED THE PRSOV. (M) 2L72 4F4 FRTA2NM A12EU 20040810000242004081000024NM 2004 8 10 GAIA04087OP 120040715A33501000677 LIGHT BOEING727 727214 138407RNM COCKPIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07751US 21513 FLT 713 - MIA-FWA - FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040810000272004081000027 2004 8 10 USAASA04064 420040603A2565 LANYARD AIRBUSA319 A319112 3930323EU GIRT BAR MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19711UW 1033 BOS - DURING AN INSPECTION OF THE GIRT BAR LANYARD ROUTING, THE FORWARD LEFT, AND THE REAR LEFT ESCAPE SLIDE SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK DOR SERVICE. (M) 2L72 4F RTA28NM 20040810000282004081000028 2004 8 10 USAASA04060 420040525A2565 LANYARD AIRBUSA319 A319112 3930323EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19710UW 1019 BFM - THE FORWARD RIGHT SERVICE DOOR, AFT LEFT ENTRY DOOR, AND THE AFT RIGHT SERVICE DOOR ESCAPE SLIDES SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY WHEN THE SLIDES WERE REMOVED FROM THE AIRCRAFT FOR HEAVY MAINTENANCE. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040810000302004081000030 2004 8 10 USAASA04063 420040603A2565 LANYARD AIRBUS320 A320214 3930316EU GIRT BAR MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19115US 1171 PHL - FOUND DURING AN INSPECTION OF THE GIRT BAR LANYARD ROUTING, THE FORWARD LEFT ESCAPE SLIDE ELECTRICAL HARNESS, AND THE REAR RIGHT, ESCAPE LSIDE SURVIVAL KIT LANYARD WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARD AND THE ELECTRICAL HARNESS. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040810000312004081000031 2004 8 10 USAASA04062 420040602A2565 LANYARD AIRBUS320 A320214 3930316EU GIRT BAR MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19121UW 1294 BOS - FOUND DURING AN INSPECTION OF THE GIRT BAR ROUTING, THE FORWARD LEFT AND THE RIGHT, ESCAPE SLIDE SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040810000352004081000035NM 2004 8 10 ASAA0440138 120040623A5311BAC14902807 FRAME BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01792AS 28887 OAK - FOUND AFT CARGO COMPARTMENT, FRAME AT STATION 767 CORRODED ON FORWARD SIDE FROM STRINGER 25R TO BL 0. REPAIRED FRAME IAW SRM 53-00-07 PAGE 210-212. (M) 2L72 4F RTA16WE 20040810000372004081000037WP 2004 8 10 ASAA0480280 120040417A335060030431 POWER SUPPLY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING LINE CHECK, FOUND EMERGENCY OVERHEAD LIGHTS INOPERATIVE AT BOTH LEFT AND RIGHT OVERWING EXITS. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F A6WE 20040810000382004081000038WP 2004 8 10 ASAA0480373 120040510A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040810000392004081000039WP 2004 8 10 ASAA0480371 120040507A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SAN - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS AND AT ROWS 13-15. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040810000402004081000040NM 2004 8 10 ASAA0440108 120040420A5512655482128 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 GYR - FOUND DEN ON HORIZ STAB LEADING EDGE APPROX 50 INCHES FROM INBOARD EDGE MEASURED 1 INCH DIAMETER .040 DEEP. REPAIRED DENT IAW SRM 55-10-01 AND REPAIRED RIB PER SRM 55-10-09. (M) 2L72 4F RTA16WE 20040810000422004081000042NM 2004 8 10 ASAA0440133 120040525A57516525914 SPAR BOEING737 737490 1384715NM LT AILERON DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 PAE - FOUND LEFT AILERON, OUTBOARD HINGE ACCESS PANEL ATTACH POINT DAMAGED. REPLACED LEFT AILERON LOWER FRONT SPAR. (M) 2L72 4F RTA16WE 20040810000452004081000045NM 2004 8 10 SWAA042247 120040806A57536546431285 SKIN BOEING737 7373H4 1384600NM FORE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED LEFT OUTBOARD T/E FORE FLAP PER MM. 2L72 4F RTA16WE 20040810000462004081000046NM 2004 8 10 SWAA042248 120040806A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29417WN 29822 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED EXTERIOR LIGHT PER MM. 2L72 4F RTA16WE 20040810000472004081000047NM 2004 8 10 SWAA042249 120040807A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 EEPLS FWD COVER MISSING. REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040810000492004081000049NM 2004 8 10 SWAA042251 120040807A3350101073 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040810000542004081000054 2004 8 10 SWAA042241 420040806A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040810000562004081000056NM 2004 8 10 SWAA042243 120040806A53306552880 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 1004, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040810000572004081000057NM 2004 8 10 SWAA042244 120040806A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 1 DEF, LOOSE. SECURED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040810000582004081000058NM 2004 8 10 SWAA042245 120040806A53126517583 BEAM BOEING737 7373H4 1384600NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM AT BS 178, RBL 17.1, WL 226, CRACKED. REMOVED AND REPLACED VERTICAL BEAM PER SRM. 2L72 4F RTA16WE 20040810000592004081000059WP 2004 8 10 ABXA040234 120040629A2760 ARM DOUG DC8 DC863F 302198FWP CONTROL VALVE LOOSE A ABXAO OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED DEDESCENT 1 GL23826AX 46061 DURING DESCENT THRU 10,000, AIRCRAFT BEGAN A ROLL TO LEFT, AUTOPILOT DISCONNECTED AND AIRCRAFT CONTINUED TO ROLL UNTIL RIGHT AILERON WAS APPLIED. DURING ROLL EVENT, AIRCRAFT HAD A MILD SHAKING. MAINTENANCE FOUND LATERAL CONTROL SPOILER POWER CONTROL VALVE ARM LOOSE. SECURED ARM IAW DC-8 AMM 27-62-09. LUBED AILERON CONTROL CABLES ON LEFT WHEEL WELL IAW DC-8 AMM 20-17-00. OPS CHECKED AILERON. SYSTEMS WORKING NORMAL IAW DC-8 AMM 27-11-00. 2L74 4F 4A25 20040810000602004081000060WP 2004 8 10 ABXA040254 120040705A57119919474501 CAP DOUG DC9 DC931 3022065WP LT TE REAR SPAR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23937AX 47074 TRAILING EDGE FITTING CRACKED AT INBOARD SPOILER INBOARD END STOP PAD. REPLACED FITTING IAW DC-9 MM. 2L72 4F A6WE 20040810000612004081000061WP 2004 8 10 ABXA040256 120040702A531199196432 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23937AX 47074 FRAME CRACKED AT LOWER END, STA 639 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03. 2L72 4F A6WE 20040810000622004081000062WP 2004 8 10 ABXA040255 120040705A532039203422 BRACKET DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23937AX 47074 ATTACH ANGLE CRACKED FORWARD SIDE FLOORBEAM STA 639, RBL 54. REPLACED ANGLE IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20040810000632004081000063WP 2004 8 10 ABXA040250 120040625A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23828AX 45999 AFT CARGO LONGERON 35 RIGHT, BLEEDING CORROSION BETWEEN TOP OF LONGERON AND INTERCOSTAL, STA 1080. REPAIRED AREA IAW REA D853-49160MR. 2L74 4F 4A25 20040810000642004081000064WP 2004 8 10 ABXA040253 120040705A78305958782503 DRIVE LINK DOUG DC9 DC931 3022065WP THRUST REVERSER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23937AX 47074 WHILE ACCOMPLISHING NEA7800001-001, THE LOWER RIGHT THRUST REVERSER LINK WAS FOUND CRACKED AROUND CENTER PIVOT FLANGE AND BOSS. LINK REPLACED ON J/C NEA78300001-001. 2L72 4F A6WE 20040810000662004081000066WP 2004 8 10 ABXA040252 120040702A5310995823911 SHEAR TIE DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23937AX 47074 SHEAR TIE CRACKED FS 1019 JUST ABOVE LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159. 2L72 4F A6WE 20040810000672004081000067NM 2004 8 10 ABXA040249 120040617A1430BACB30MT16K48 BOLT BOEING767 767281 1385109NM VERTICAL STAB SHEARED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23767AX 22785 WHILE ACCOMPLISHING INSPECTION OF AD2001-19-04, FOUND 1 VERTICAL STAB ATTACH BOLT SHEARED AT FS 1654 LEFT SIDE. REMOVED AND REPLACED ALL 16 VERTICAL ATTACH BOLTS AND NUTS IAW ABX EA 53420014-001. 2L72 4F RTA1NM 20040810000692004081000069WP 2004 8 10 ABXA040257 120040626A5420408447905 ATTACH ANGLE DOUG DC9 DC932 3022066WP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23880DP 47635 PYLON LEADING EDGE LOWER ATTACH ANGLE ON FUSELAGE CRACKED. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 20040810000712004081000071WP 2004 8 10 ABXA040258 120040628A52105060213 DOOR FRAME DOUG DC9 DC932 3022066WP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23880DP 47635 INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REMOVED FITTING AND STOP FOR REPLACEMENT AND REPAIR, FABRICATED PART IAW REA D952-50078. PRIMED AND PAINTED REINSTALLED IAW DC-9 SRM 52-05. 2L72 4F A6WE 20040810000742004081000074EA 2004 8 10 SWIA200413647 120040623A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07930SW 7713 FLOOR SUPPORT STRUCTURE, RIGHT SIDE 621 ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON RIGHT SIDE 621 ANGLE IAW BOMBARDIER REO 601R-53-61-117. 2L72 4F RTA21EA 20040810000752004081000075NE 2004 8 10 ABXA040235 220040630A732171128726 FUEL CONTROL DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 1 ENGINE DEFECTIVE A ABXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL23820AX 5804 46155 671316 PASSING FL 200 ON DESCENT 320 KTS, AS THROTTLE ADVANCED NR 1 ENG FLAMED OUT. IMMEDIATE ACTION ITEM COMPLETED & ENG RESTARTED NORMALLY. MX INSPECTED FUEL TANK BOOST PUMP AND OUTPUT PRESSURE, NO EVIDENCE OF FOD, NO DEFECTS. CHECKED FORWARD PUMP OUTPUT, 190 PSI, WITHIN LIMITS. REPLACED NR 1 FCU, LEAK CHECKED GOOD. REPLACED NR 1 FUEL FILTER, NO CONTAMINATION FOUND, LEAK CHECKED GOOD. REPLACED FUEL CONTROL GARLOCK SEAL, LEAK CHECKED GOOD ON ENG RUN. TRIMMED NR 1 ENG PER DC8 MM 71-00-00 DUE TO FCU CHANGE. CHECKED FUEL FEED LINE INTEGRITY FOR NR 1 ENG COMMON TO NR 1 MAIN FUEL CELL, CHECKED NORMAL. REPLACED NR 1 ENG FUEL FLEX LINE, LEAK CHECKED GOOD. 2L74 4F4 F 4A25 1E8 20040810000762004081000076WP 2004 8 10 ABXA040214 120040604A53305920323513 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 A .5 INCH CRACK COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR UPPER CORNER FUSELAGE SKIN. INSTALLED REPAIR IAW EA 53100110-001. 2L72 4F A6WE 20040810000782004081000078WP 2004 8 10 ABXA040216 120040604A533059114331 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 SKIN CRACKED ABOVE LEFT PYLON AT RIVET, STA 1038, LONGERON 12 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-31-0. 2L72 4F A6WE 20040810000812004081000081WP 2004 8 10 ABXA040219 120040604A5330 FINGER DOUBLER DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 AFT CARGO STA 1480, LONGERON 31 LEFT, FINGER DOUBLER, CORRODED. REPAIRED FUSELAGE SKIN IAW DC-8 SRM 53-2-1 AND REPAIRED FRAME SECTION IAW DWG K04888 AND REA D853-49146, SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-3-1. 2L74 4F 4A25 20040810000822004081000082WP 2004 8 10 ABXA040220 120040608A5340 MOUNT DOUG DC8 DC863F 302198FWP CARGO DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 MAIN CARGO DOOR LOWER LATCH MOUNT HOLES WORN. REPAIRED AREA IAW REA D852-49174MR. 2L74 4F 4A25 20040810000832004081000083WP 2004 8 10 ABXA040221 120040608A5230 HINGE DOUG DC8 DC863F 302198FWP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 MAIN CARGO DOOR AFT HINGE HAD AFT ATTACHMENT FASTENER HOLE SHOWING CRACK INDICATION. REPAIRED AREA IAW REA D852-49168MR. 2L74 4F 4A25 20040810000842004081000084WP 2004 8 10 ABXA040222 120040604A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 FLOORBEAM WEB AT BS 240 HAD 4 CRACK INDICATIONS AT SPLICE PLATE ATTACH FASTENERS LEFT BUTTLINE 57. REPAIRED AREA IAW REA D853-49184MR. 2L74 4F 4A25 20040810000862004081000086WP 2004 8 10 ABXA040233 120040629A32607000010101ABX DOWNLOCK SWITCH DOUG DC9 DC932 3022066WP MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING LDLANDING 1 GL23902AX7074 47426 NOSE LANDING GEAR DOWN (GREEN LIGHTS) DID NOT ILLUMINATE AFTER SELECTING LANDING GEAR DOWN. RECYCLED LANDING GEAR NOSE DOWN INDICATOR (GREEN LIGHT) INDICATED NORMAL DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC-9 MM 32-60-01-2-0101. OPS CHECKED GOOD. 2L72 4F A6WE 20040810000912004081000091WP 2004 8 10 ABXA040265 120040712A5610 SPRING DOUG DC8 DC861 3021952WP COCKPIT WINDOW BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23842AX 46015 DURING MAINTENANCE, FOUND FIRST OFFICER'S WINDOW WAS STUCK. REPLACED SPRING, OPS CHECKED WINDOW. WINDOW DID NOT STICK. PRESSURIZED AIRCRAFT TO 5 PSI DIFF. CHECKED WINDOW AFTER DEPRESSURIZATION. OPENED AND CLOSED NORMALLY. 2L74 4F 4A25 20040809000092004080900009EU 2004 8 9 SIMA200416203 120040606A55127255150521 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21396AE 340B396 ABI - DURING MBV INSPECTION, AIRCRAFT PREVIOUSLY HAD SUSTAINED HAIL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZONTAL STABILIZER UPPER SKIN. REMOVED DAMAGED UPPER SKIN AND INSTALLED NEW SKIN IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 22, 23 AND 40 AND SAAB REPAIR STATEMENT 72SDS1514. (M) 2L72 4T RTA52EU 20040809000312004080900031WP 2004 8 9 ASAA0480436 120040517A53113936607539 FRAME DOUG DC9 DC983 3022083WP FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 OKC - FOUND DURING C-CHECK, FRAME IS CORRODED AT NUMBER LOCATIONS BETWEEN LONGERON 28L AND 28R AT FS 1079. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-03. (M) 2L72 4F RTA6WE 20040809000322004080900032NM 2004 8 9 UIEA200400005 120040111A1420 CONNECTOR BOEING747 747228F 1384895NM NR 3 ENGINE DAMAGED A UIEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15809MC 20887 OKO/SUU - NR 3 ENGINE FILTER BYPASS LIGHT CAME ON DURING CLIMB. RETARDING THROTTLE DID NOT OUT IT OUT. ENGINE SHUTDOWN PER FHB AT 0633Z. LIGHT REMAINED ON. REMOVED AND REPLACED OIL FILTER AND INSPECTED, NO CONTAMINATION FOUND. INSTALLED NEW FILTER, LEAK AND OPERATION CHECK NORMAL PER MM 79-21-07. CONFIRMED INDICATOIN PROBLEM, ITEM TRANSFERRED TO DMI M04-004 PER MEL 79-03 D1 PAGE 50807. TROUBLESHOT FOUND CONNECTOR BACK SHELL LOOSE, SECURED BACK SHEELL PER CHAP 20 MAINTENANCE PRACTICES MANUAL. OPERATION CHECK NORMAL. DMI CLEARED AND PLACARD REMOVED. (M) 2L74 4F A20WE 20040809000432004080900043EU 2004 8 9 TRBA2004022 120040317A610011S76180650008 SWITCH AEROSPATR72 ATR72212 8680945EU CENTER PEDESTAL FAULTY A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO21288AM 288 ON TAKEOFF ROLL, THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM DID NOT ARM. TAKEOFF ABORTED. REMOVED AND REPLACED MICROSWITCH. (M) 2H72 4T RTA53EU 20040809000462004080900046CE 2004 8 9 2004F00168 120040405A55241016200111 BRACKET BEECH 1900 1900D 1154162CE RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO198755116716 UE206 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATORY HINGE BRACKET. (M) 2L72 4T RTA24CE 20040809000512004080900051EU 2004 8 9 ASOA04323 120040429A275126V10TT4B01 TRANSMITTER AEROSPATR72 ATR72 EU TE FLAPS MALFUNCTIONED A ASOAO OTHER N FALSE WARNING APAPPROACH 1 SO11641AS 387 FLT 4724 - DURING APPROACH FROM ATL-MGM, THE CREW RECEIVED A FLIGHT CONTROL MASTER CAUTION MESSAGE ACCOMPANIED BY A FLAPS ASYMMETRY INDICATION. THE FLAPS WERE OBSERVED STUCK BETWEEN FIFTEEN TO THIRTY DEGREES ON THE FLAP INDICTOR THE CRW WAS UNABLE TO RAISE OR LOWER THE FLAPS AND COULD NOT DETERMINE IF THERE WAS ANY ASYMMETRY BY AIRCRAFT HANDLING OR USUAL MEANS. QRH PROCEDURES WERE COMPLIED AND AN EMERGENCY WAS DECLARED. THE CREW PERFORMED A FIFTEEN DEGREE LANDING PROCEDURE AND THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER AND THE FLAP CONTROL SWITCH UNIT (P/N 7048-1). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040809000532004080900053EU 2004 8 9 ASOA04319 120040413A5315 FLOORBEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FS 38 IAW WITH SRM 51-25-00. (M) 2H72 4T RT 20040809000562004080900056EU 2004 8 9 ASOA04314 120040413A5320 INTERCOSTAL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE INTERCOSTALS BETWEEN FS 39 TO FS 40 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENACNE REMOVED AND REPLACED THE INTERCOSTALS BETWEEN FS 39 TO FS 40 ON THE LEFT AND RIGHT SIDES IAW SRM 51-25-01. (M) 2H72 4T RT 20040809000572004080900057NM 2004 8 9 USAA040022 120040213A5347 SEAT TRACK BOEING767 7672B7 1385107NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US55490 24894 FOUND SEAT TRACK CORRODED 3 INCHES, BS 1087 AT LBL 88. FABRICATED AND INSTALLED SEAT TRACK AND REPAIR SPLICE PE SRM 53-00-52. (M) 2L72 4F RTA1NM 20040809000672004080900067NM 2004 8 9 DL76L040688 120040723A324026124121A BRAKE BOEING767 767332 1382001NM NR 3 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 NR 3 BRAKE DELAMINATED. REPLACED NR 3 BRAKE. 2L72 4F RTA1NM 20040809000702004080900070EA 2004 8 9 COMA0460418 120040716A3610355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA R/H CHAFED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01912CA 7011 FLIGHT 5215 RIGHT 14TH STAGE BLEED AIR DUCT WARNING DURING T/O. REPLACED THE 14TH STAGE BLEED LEAK SENSING ELEMENTS. 2L72 4F RTA21EA 20040809000732004080900073EA 2004 8 9 COMA0460431 120040727A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01938CA 7046 FLT 5987 EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED FLEXIBLE LIGHT STRIP. 2L72 4F RTA21EA 20040809000742004080900074EA 2004 8 9 COMA0460432 120040727A491038760016 SWITCH CNDAIRCL600 CL6002B19 1900309EA APU MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01798CA 7348 FLT 5888 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL PRESSURE SWITCH. 2L72 4F RTA21EA 20040809000922004080900092 2004 8 9 SWAA042233 420040805A2565D31354 SLIDE BOEING737 737317 138447PNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040809001002004080900100NM 2004 8 9 DL764040711 120040731A3350 BULB BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27842MH 29715 ON TRANSIT CHECK FOUND EMERGENCY LIGHTS INOP AT 31 AND 36 ABOVE HEAD. RELAMPED, CHECKED OK. 2L72 4F RTA1NM 20040809001012004080900101NM 2004 8 9 DL767040712 120040801A2920291001891 VALVE BOEING767 767232 1385132NM RAT FAILED A DALAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO27115DA 22227 AFTER TOUCHDOWN LOST CENTER HYDRAULIC SYSTEM C HYD QTY. FOUND CHECK VALVE ON RAT BROKEN. REPLACED SAME. 2L72 4F RTA1NM 20040809001062004080900106EA 2004 8 9 COMA0460415 120040715A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA NR 3 HYD MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01917CA1273212 7017 FLIGHT 5605 LANDING GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20040809001072004080900107NM 2004 8 9 DLM88040717 120040804A2910 LINE DOUG MD88 MD88 3023688NM NR 2 ENGINE FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27987DL 53338 LOST COMPLETE RIGHT HYD SYS. PERFORMED EMERGENCY PROC AND RET TO ATL. FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE BLOWN. REPLACED SAME. 2L72 4F RTA6WE 20040809001102004080900110NM 2004 8 9 DLM88040659 120040715A3260833703 SENSOR DOUG MD88 MD88 3023688NM NLG MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27926DL 49713 NOSE GEAR UNSAFE INDICATION AFTER T/O, CHECKLIST WAS C/W NON NORMAL CHECKLIST INITIATED FOR UNSAFE GEAR. INDICATION SHOWED SAFE AFTER ALL HYD PUMPS ON. REPLACED NOSE GEAR UP PROX SENSOR AND CENTER PROX SENSOR. 2L72 4F RTA6WE 20040809001192004080900119NM 2004 8 9 DL757040719 120040804A2120 ODOR BOEING757 757232 1384965NM MID GALLEY DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27653DL 24393 DURING FLIGHT TO DAY, BURNING PLASTIC SMELL IN MID GALLEY, THIS PER FLT ATTENDANT REPORT. CALLED CONTRACT MTC TO INVESTIGATE. CONTRACT MTC TURNED ON ALL MID GALLEY OVENS AND COFFEEMAKERS AND LIGHT. COULD NOT FIND ANY EVIDENCE OF A BURNING PLASTIC SMELL FROM MID GALLEY. 2L72 4F RTA2NM 20040809001202004080900120NM 2004 8 9 DL777040720 120040804A2821TRENT892 FILTER BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 2 ENGINE CONTAMINATED A DALAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO27877DA 29739 051361 ON TAKEOFF EICAS ENGINE FUEL FILTER RT, WHEN PWR REDUCED LIGHT WENT OUT AND REMAINED OUT. ALL OTHER ENG IND NORMAL. FOUND MAINT MSG 73-90122 LP FUEL FILTER ELEMENT RT ENGINE IS BLOCKED. REPLACED RT ENGINE LP FUEL FILTER AS PER MM. PERFORMED FUEL AND OIL LEAK TEST, TEST NR 2 AND ALL CHECKS NORMAL. 2L72 4F4 FRTT00001SEE00050EN 20040809001232004080900123EA 2004 8 9 COMA0460388 120040622A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01416CA 7450 CABLE GUIDE SUPPORT ANGLE UNDER FLOOR PANEL 261 CLF, FS 484 CRACKED. REPAIRED IAW REO 601R-53-41-225. 2L72 4F RTA21EA 20040809001262004080900126NM 2004 8 9 DL767040724 120040804A335020121 CHARGER BOEING767 767232 1385132NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27112DL 22224 ON SERVICE CHECK FOUND LT SIDE AFT EXT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER M/M, CHECKS GOOD. 2L72 4F RTA1NM 20040809001372004080900137NM 2004 8 9 DL764040668 120040717A3350 BULB BOEING767 767432ER 1385134NM SEAT 28AB MISSING A DALAK NONE L NO TEST ININSP/MAINT 1 SO27835MH 29708 EMERGENCY LIGHT AT SEAT 28AB INOP. FOUND NO BULBS INSTALLED. INSTALLED 2 BULBS, OPS CHECK GOOD. 2L72 4F RTA1NM 20040810000112004081000011NM 2004 8 10 ASAA0440136 120040610A5340693535214 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A K NONE O OTHER ININSP/MAINT 1 NM02778AS 25110 FOUND FUSELAGE INTERNAL STATION 400 CLIP ATTACHED TO STRINGER NR 2 LEFT HAS A GOUGE. REMOVED AND REPLACED STRINGER TIE CLIP ON STRINGER NR 2 LEFT. (M) 2L72 4F RTA16WE 20040810000222004081000022EU 2004 8 10 USAASA04067 120040705A33501012887 LIGHT AIRBUS320 A320214 3930316EU ROW 8 ABC INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19101UW 0936 PHL - DURING WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 8ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040810000292004081000029EU 2004 8 10 USAASA04068 120040705A3397 WIRE AIRBUS320 A320214 3930316EU EMERGENCY LIGHT BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19101UW 0936 PHL - DURING THE WEEKLY CHECK, FOUND THE EMERGENCY LIGHT AT ROW 19ABC INOPERATIVE. MAINTENANCE REPAIRED THE BROKEN PIN/WIRE UNDER THE SEAT. OPS CHECKS GOOD. (M) 2L72 4F RTA28NM 20040810000362004081000036WP 2004 8 10 ASAA0480453 120040526A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 OKC - FOUND DURING HV CHECK, PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M) 2L72 4F A6WE 20040810000442004081000044NM 2004 8 10 SWAA042246 120040806A575465C26603192 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20040810000482004081000048 2004 8 10 SWAA042250 420040807A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040810000512004081000051NM 2004 8 10 SWAA042253 120040807A335057771 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29405WN 27893 FWD EEPLS END CAP BROKEN. REMOVED AND REPLACED EEPLS END CAP PER MM. 2L72 4F RTA16WE 20040810000522004081000052 2004 8 10 SWAA042239 420040806A2565D31354 SLIDE BOEING737 7372H4 138448CNM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040810000722004081000072WP 2004 8 10 ABXA040260 120040628A521099557523 FRAME DOUG DC9 DC932 3022066WP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23880DP 47635 INTERCOSTAL FRAME CRACKED IN RADIUS FORWARD END OF FORWARD PASSENGER DOOR VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REPAIRED INTERCOSTAL IAW DC-9 SRM 52-05. REINSTALLED DOOR STOP IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20040810000852004081000085NM 2004 8 10 SCNA04010 120040616A3350 COVER BOEING737 7378Q8 13844BXNM EXIT SIGN LOOSE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15805SY 30032 EXIT SIGN COVER LEFT AFT GALLEY CAME LOOSE. MAINTENANCE REINSTALLED EXIT SIGN AS REQUIRED, OK FOR SERVICE. 2L72 4F RTA16WE 20040810000872004081000087WP 2004 8 10 ABXA040223 120040604A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 FLOORBEAM WEB AT BS 180 WAS CORRODED AT 3 ATTACH FASTENERS FOR SPLICE PLATE LEFT BUTTLINE 57. REPAIRED AREA IAW REA D853-49182MR. 2L74 4F 4A25 20040810000942004081000094WP 2004 8 10 ABXA040240 120040621A5330591142689 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 SKIN CRACKED STA 980 BETWEEN LONGERON 13 LEFT AND 14 LEFT. REPAIRED SKIN IAW DC-9 SRM 53-04. 2L72 4F A6WE 20040810000962004081000096WP 2004 8 10 ABXA040271 120040719A533099234343 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23957AX 47759 FUSELAGE SKIN BULGED AND FASTENER POPPED AT FS 617, LONGERON 29 RIGHT. REPAIRED FUSELAGE SKIN AND INTERNAL DOUBLER AT STA 617 IAW DC-9 SRM 53-04. 2L72 4F A6WE 20040810000972004081000097NE 2004 8 10 ABXA040270 220040725A7200JT8D15 ENGINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE LEFT DEFECTIVE A ABXAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL23951AX7799 47616 686296 LEFT ENGINE LOW OIL QUANTITY 0, LOW OIL PRESSURE 35 PSI, OIL PRESSURE LIGHT ON, SHUT DOWN LEFT ENGINE. FROM PDX, MADE DIVERSION TO YAK. REMOVED AND REPLACED LEFT ENGINE IAW DC-9 JOB CARD 9090010 ON WP 600204098. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F4 F A6WE E2EA 20040810000982004081000098WP 2004 8 10 ABXA040268 120040729A531199196172 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 RIGHT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS H - I. REPLACED FRAME IAW ABX EA 53400322-001-4, WO 600204273. 2L72 4F A6WE 20040810001062004081000106NM 2004 8 10 DL73S040674 120040720A5511654751310 STIFFENER BOEING737 737247 138448DNM HORIZONTAL STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 LEFT HORIZOINTAL STABILIZER INTERNAL RIB WEB STIFFENER CRACKED AT STA 175. REPAIR IAW ERA 091677-14. 2L72 4F A16WE 20040810001082004081000108NM 2004 8 10 ABXA040245 120040713A3230284T042511 BRACKET BOEING767 767281 1385109NM MLG MISINSTALLED A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23767AX 22785 GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. CAPTAIN'S DISCRETION TO NOT USE LOCK OVERRIDE SWITCH. MAINTENANCE TROUBLESHOT AIR/GROUND RELAY SYSTEM PER B767 WDM 32-09 AND FOUND RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET INCORRECTLY INSTALLED. REPOSITIONED THE RIGHT MAIN LANDING GEAR TILT SENSOR BRACKET PER B767 MM 32-09-09 AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST PER B767 MM 32-32-10 AND SYSTEM CHECKED GOOD. 2L72 4F RTA1NM 20040810001092004081000109EA 2004 8 10 COMA0460426 120040722A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01969CA 7141 FLIGHT 5495 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. C/W EO 27-046 OPERATION NORMAL. 2L72 4F RTA21EA 20040810001122004081000112EA 2004 8 10 COMA0460400 120040629A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 LEFT LOWER CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A. 2L72 4F RTA21EA 20040810001132004081000113EA 2004 8 10 COMA0460397 120040629A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 CARGO FLOOR SUPPORT STRUCTURE LBL 9 HAS CORROSION AROUND NUT PLATE HOLES. REPAIRED IAW CRJ SRM 51-42-06, 51-42-13 AND 51-42-21. 2L72 4F RTA21EA 20040811000022004081100002SO 2004 8 11 C2XA04TY124 120040726A531514521700007 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOORBEAM AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB SRM 51-40-02, 53-21-10,51-40-06, 51-20-03, AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000032004081100003SO 2004 8 11 C2XA04SH468 120040727A531514521713003 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713975 145163 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040811000052004081100005SO 2004 8 11 C2XA04TY127 120040726A531514530633006 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM TOP CAP AT FRAME 29. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000072004081100007SO 2004 8 11 C2XA04CL075 120040719A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714950 145061 CLE FLIGHT 2249, THE CREW REPORTED THE EMERGENCY LIGHT IN THE CABIN AT SEAT 3B WAS NOT WORKING. MAINTENANCE INSPECTED AND CONNECTED EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040811000102004081100010SO 2004 8 11 C2XA04TY141 120040723A27503631101007 SELECTOR EMB 135 EMB135LR 3260305SO TE FLAPS DEFECTIVE A C2XAO OTHER N FALSE WARNING CLCLIMB 1 SW2727512 145274 CLE - UPON GEAR RETRACTION OF FLIGHT 2127 THE LANDING GEAR AURAL WARNING INDICATION CAME ON. REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB 135/145 AMM 27-51-03. OPS CHECKS WERE GOOD OF THE FLAPS AND LANDING WARNING SYSTEM IAW EMB AMM 27-50-00 AND 32-60-00. A/C WAS RELEASED TO SERVICE. 2L72 4F RTT00011AT 20040811000112004081100011NM 2004 8 11 04FDEA02384 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH PIVOT HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.508 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.506 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040811000122004081100012NM 2004 8 11 04FDEA02385 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.189 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040811000132004081100013NM 2004 8 11 04FDEA02386 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH PIVOT HOLE INBOARD FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 MATERIAL REMOVED = 0.012 REMAINING THICKNESS = 0.485 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040811000142004081100014NM 2004 8 11 04FDEA02387 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.223 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040811000152004081100015NM 2004 8 11 04FDEA02388 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.221 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040811000162004081100016NM 2004 8 11 04FDEA02389 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OUTBOARD FLAP - INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE INBOARD FLANGED CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.411 MATERIAL REMOVED = 0.005 REMAINING THICKNESS = 0.406 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040811000182004081100018SO 2004 8 11 C2XA04BT082 120040731A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716919 145393 NON-ROUTINE WORK CARD WRITE UP, NR 2 OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 OVERWING EMERGENCY LIGHT IAW EMB 145 MM 33-50-07. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040811000242004081100024SO 2004 8 11 C2XA04IA090 120040724A49304504205D FADEC EMB 145 EMB145XR 3260214SO APU INOPERATIVE A C2XAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27181204165 4165 145681 THE CREW REPORTED THAT THE APU FAILED TO START DURING FLIGHT AND CAUSED A FUEL ODOR IN THE CABIN. THE APU WAS PLACED ON MEL 49-00-00 CTL 044579, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 07/24/04 FLIGHT 2222 THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE APU FADEC, OPERATIONALLY CHECKED GOOD IAW EMB-145 AMM 49-64-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040811000252004081100025SO 2004 8 11 C2XA04BT080 120040727A49504951680 BLEED VALVE EMB 145 EMB145XR 3260214SO APU FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27181202098 2098 145681 CREW REPORTED, FUEL ODOR IN COCKPIT/CABIN FOLLOWING APU START INFLIGHT. MAINTENANCE REMOVED AND REPLACED APU BLEED VALVE IAW EMB 145XR MM 36-12-01, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20040811000262004081100026SO 2004 8 11 C2XA04BT081 120040727A1420 CONNECTOR EMB 135 EMB135LR 3260305SO ENGINE NACELLE CONTAMINATED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2712530 145533 CREW REPORTED, STRONG FUEL ODOR WITH APU START. MAINTENANCE FOUND WATER IN NR 1 ENGINE BLEED VALVE CONNECTOR, REMOVED WATER FROM CONNECTOR AND RESECURED NR 1 ENGINE BLEED VALVE CONNECTOR IAW EMB135 AMM 36-12-01, OPS CHECKED GOOD. NO ODOR NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040811000272004081100027SO 2004 8 11 C2XA04BT083 120040731A26123601133500 FIRE LOOP EMB 145 EMB145LR 3260212SO NR 2 ENGINE DEFECTIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2715986 145254 NR 2 FIRE DET FAIL. REMOVED AND REPLACED ENG NR 2 FIRE LOOP, OPS CHECK GOOD. 2L72 4T RTT00011AT 20040811000282004081100028SO 2004 8 11 C2XA04TY133 120040802A531514521713003 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER AREA OF THE FLOORBEAM AT FR 20>23. REMOVED AND REPLACED THE FLOORBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 4C INSPECTION. 2L72 4F RTT00011AT 20040811000292004081100029SO 2004 8 11 C2XA04SH469 120040728A531514530628001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716976 145171 SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 24, GREATER THAN 30 PERCENT OF ORIGINAL THICKNESS OF .070 INCH (OUT OF LIMITS) BUT WITHIN REPAIRABLE LIMITS. 2L72 4T RTT00011AT 20040811000302004081100030SO 2004 8 11 C2XA04SH471 120040721A531514530644407 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2724517 145332 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 35 AND 39. MAINTENANCE REMOVED THE DAMAGED AREA AND FOUND IT TO BE GREATER THAN 30 PERCENT OF ORIGINAL MATERIAL THICKNESS, BUT WITHIN REPAIRABLE LIMITS. A DYE PENETRANT INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED. THE AREA WAS THEN RESTORED IAW EMB 135 CPM 51-21-04, CPM 51-21-05 AND CPM 51-21-06. ALL WORK WAS PERFORMED PER EC5310-01280 REV A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040811000312004081100031SO 2004 8 11 C2XA04SH472 120040730A531514530627001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713975 145163 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040811000322004081100032SO 2004 8 11 C2XA04TY138 120040731A532014525422001 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 61 TO FRAME 65. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000332004081100033SO 2004 8 11 C2XA04TY139 120040731A532014550906001 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 23 TO 30. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000352004081100035NM 2004 8 11 DL76L040735 120040807A2121 FAN BOEING767 767332 1382001NM COCKPIT FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27190DN 28447 CREW REPORTED BURNT SMELL FROM COCKPIT VENTS MOMENTARILY AND EICAS MESSAGE LEFT RCIRC FAN WITH ASSOCIATED OFF LIGHT. REPLACED RECIRC FAN. 2L72 4F RTA1NM 20040811000372004081100037 2004 8 11 DL76G040737 420040807A34174040800912 ADC BOEING767 767332 1382001NM COCKPIT MALFUNCTIONED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO271611B 30595 CAPT FLIGHT INSTRUMENTS FAILED AND BOTH EECS WENT TO ALT MODE. SWITCHED CAPT AIR DATA TO ALT AND RECOVERED FLIGHT INSTRUMENTS. STATUS MESSAGE WARNING. REPLACED LEFT AIR DATA COMPUTER, OPS CHECKS OK. 2L72 4F RTA1NM 20040811000382004081100038NM 2004 8 11 DL764040738 120040806A3350 LIGHT BOEING767 767432ER 1385134NM FWD GALLEY INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27834MH 29707 EMERGENCY LIGHT INOP FWD GALLEY MIDDLE LIGHT IN FRONT OF FLT ATTENDANT SEATS. RELAMPED SAME. 2L72 4F RTA1NM 20040811000432004081100043EA 2004 8 11 COMA0460410 120040719A5311 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FRAME CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01427CA 7460 LEFT HAND 640 FRAME DOUBLERS CRACKED. REPAIRED IAW REO 601R-53-61-1089. 2L72 4F RTA21EA 20040811000442004081100044EA 2004 8 11 COMA0460419 120040716A77971697M50G04 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA RT ENGINE DEFECTIVE A COMAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO01484CA 7702 FLIGHT 5541 RIGHT ENGINE N1, ITT, AND N2 SURGING. REPLACED THE ENGINE BLUE WIRE HARNESS. 2L72 4F RTA21EA 20040811000452004081100045EA 2004 8 11 COMA0460420 120040720A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01472CA 7667 RIGHT HAND FS 621.00 FLOOR SUPPORT ANGLE CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20040811000462004081100046NM 2004 8 11 DLM88040695 120040726A2133 HANDLE DOUG MD88 MD88 3023688NM COCKPIT STUCK A DALAB EMER. DESCENT P NO WARNING INDICATION CRCRUISE 1 SO27915DE 53420 CABIN PRESSURE CONTROL WENT INOPERATIVE IN CRUISE. CREW REPORTED OUTFLOW VALVE HANDLE STUCK. REMOVED FALLEN AUTOPILOT SELECTOR KNOB FROM OUTFLOW VALVE CONTROL WHEEL. 2L72 4F RTA6WE 20040811000472004081100047WP 2004 8 11 ABXA040246 120040715A5610 LOCK PIN DOUG DC9 DC932 3022066WP COCKPIT WINDOW OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT GLIDE BACK TO FULL OPER POSITION. ADJUSTED CLEARVIEW WINDOW ECCENTRIC LOCK PIN. WINDOW OPENS AND CLOSES SMOOTHLY. 2L72 4F A6WE 20040811000482004081100048NM 2004 8 11 DLM88040696 120040706A531059360381 BEAM DOUG MD88 MD88 3023688NM CARGO DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27919DL 49584 CORROSION ON C2 CARGO BIN DOOR JAMB BEAM FOUND DURING MTC VISIT. REMOVED CORROSION FROM C2 BIN DOOR JAMB BEAM AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-05D FIG 63 SECTION E-E SHEET 2 AND WAS REPAIRED IAW SRM 53-05D FIG 63. 2L72 4F RTA6WE 20040811000502004081100050NM 2004 8 11 DL73S040698 120040726A7930 TRANSMITTER BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27303DL 23075 687675 NUMBER 1 OIL PRESSURE WENT TO 6 PSI AFTER LEVEL OFF. REPLACED NR 1 OIL PRESSURE TRANSMITTER. 2L72 4F4 FRTA16WE E2EA 20040811000512004081100051NM 2004 8 11 DLM88040700 120040518A531059360381 BEAM DOUG MD88 MD88 3023688NM CARGO DOORWAY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27914DE 49957 CORROSION ON C3 CARGO BIN LOWER DOOR JAMB BEAM. REMOVED CORROSION FROM C3 CARGO DOOR JAMB BEAM AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-05D FIG 63 SHEET 2. DOOR JAMB BEAM WAS REPAIRED IAW SRM 53-05D FIG 63. 2L72 4F RTA6WE 20040811000522004081100052NM 2004 8 11 DLM88040744 120040808A3350RPS1 POWER SUPPLY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27915DE 53420 DURING LAYOVER INSPECTION FOUND FIRST CLASS SECTION EMERGENCY PATH LIGHTING INOP. T/S AND REPLACED PWR SUPPLY FOR SECTION PER AMM, OPS CHECKS NORMAL. 2L72 4F RTA6WE 20040811000532004081100053NM 2004 8 11 VNAA0407006 120040724A5220 DOOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY EXIT FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL07438JS 3056 THE CREW REPORTED THAT THE EMERGENCY DOOR AT ROW 9A WAS NOT OPENING PROPERLY. MAINTENANCE INSPECTED AND REPOSITIONED SEATS 2A THROUGH 8A IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25-00-00. OPERATION CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040811000542004081100054NE 2004 8 11 VNAA0407004 220040717A7200PW119B ENGINE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LEFT BIRD INGESTION A VNAAO OTHER C F.O.D. LDLANDING 1 GL07440JS210665092 3058 DURING LANDING, FLIGHT 2576 HAD A BIRD STRIKE. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-57-04. FURTHER INSPECTION FOUND FOD DAMAGE TO THE LEFT HAND ENGINE IMPELLER BLADES. THE DAMAGE REQUIRED REMOVAL OF THE LEFT HAND ENGINE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-02-02. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040811000562004081100056NM 2004 8 11 VNAA0407007 120040726A3240S4340200001 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG BRAKE FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07429JS2377413071 3043 DURING CLIMBOUT, THE CREW RECEIVED A EMERGENCY PARKING BRAKE ACCUMULATOR LOW CAS MESSAGE AND RETURNED TO PHL. MAINTENANCE CONTROL FERRIED THE AIRCRAFT TO PIT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040811000582004081100058NM 2004 8 11 VNAA0407009 120040731A2611SD9422AOAO01 SMOKE DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE LAVATORY FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07441JS2005110383 3059 THE CREW REPORTED RECEIVING A LAV SMOKE MESSAGE. MAINTENANCE CONTROL DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH MEL 26-3 CODE-C. THE MEL WAS CLEARED BY REPLACING THE LAV SMOKE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040811000602004081100060EA 2004 8 11 VNAA0408001 120040802A5220 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07220PS 7887 THE CREW REPORTED RECEIVING A RIGHT HAND EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL MEL'D THE EMERGENCY DOOR IN ACCORDANCE WITH MEL 52-70-3 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040811000632004081100063SO 2004 8 11 C2XA04SH475 120040802A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716976 145171 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040811000642004081100064SO 2004 8 11 C2XA04SH474 120040801A531514530633003 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713975 145163 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT THE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040811000652004081100065SO 2004 8 11 C2XA04TY128 120040802A532014526465001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FLOORBOARD SILL ON THE LT SIDE AT FR 53-58. REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE COMPLETION OF THE 4C INSPECTION. 2L72 4F RTT00011AT 20040811000682004081100068EA 2004 8 11 COMA0470058 120040722A3297 WIRE HARNESS CNDAIRCL600 CL6002C10 1390015EA BRAKE OVERHEAT DAMAGED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01374CA 10090 FLIGHT 5666 BRAKE OVERHEAT WARNING DURING T/O. REPAIRED WIRE CONNECTION ON BTMS HARNESS. 2L72 4F RTA21EA 20040811000702004081100070NM 2004 8 11 SWAA042224 120040804A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040811000722004081100072NM 2004 8 11 SWAA042226 120040804A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040811000752004081100075NM 2004 8 11 SWAA042214 120040803A3350OL3071BPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29792SW 27887 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 DEF, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040811000762004081100076NM 2004 8 11 SWAA042215 120040803A57536546434369 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040811000772004081100077 2004 8 11 SWAA042216 420040803A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811000812004081100081NM 2004 8 11 DLM88040701 120040518A531059360381 BEAM DOUG MD88 MD88 3023688NM DOOR FRAME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27914DE 49957 CORROSION ON C2 CARGO DOOR JAMB BEAM. REMOVED CORROSION FROM C2 CARGO BIN LOWER DOOR JAMB BEAM AND WAS FOUND OUT OF LIMITS IAW SRM 53-05D FIG 63 SHEET 2. REPAIRED DAMAGED AREA PER SRM 53-05D FIG 63. 2L72 4F RTA6WE 20040811000822004081100082NM 2004 8 11 SWAA042207 120040801A533065C35764 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 12R, BS 520, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040811000832004081100083 2004 8 11 SWAA042208 420040801A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 R2 DOOR EVAC SLIDE LOOSE. SECURED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811000842004081100084 2004 8 11 SWAA042209 420040803A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811000852004081100085 2004 8 11 SWAA042210 420040803A2565D31354 SLIDE BOEING737 7373T5 1384608NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811000872004081100087NM 2004 8 11 SWAA042212 120040803A551265C25727 SKIN BOEING737 7373A4 1384585NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C4 CHECK, FOUND LEFT AND RIGHT HORIZONTAL STAB LOWER SKIN AT REAR SPAR STATION 107, CRACKED. REPAIRED HORIZONTAL STAB SKIN PER SRM. 2L72 4F RTA16WE 20040811000882004081100088NM 2004 8 11 SWAA042213 120040803A1430183A80101 BOLT BOEING737 7373A4 1384585NM ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB CONTROL ROD END BOLTS PER MM. 2L72 4F RTA16WE 20040811000892004081100089EA 2004 8 11 COMA0460424 120040722A339759465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNRELIABLE A COMAK NONE O OTHER ININSP/MAINT 1 SO01436CA 7482 FLIGHT 5912 EMERGENCY FLOOR PATH LIGHTING IS INOP ROWS 5 THRU 8. REPLACED CONNECTOR WIRE AT ROW 8. 2L72 4F RTA21EA 20040811000912004081100091EA 2004 8 11 COMA0460428 120040717A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAO OTHER JS WARNING INDICATION AFFECT SYSTEMS APAPPROACH 1 SO01937CA8608 4214 7044 FLIGHT 5475 GEAR DISAGREE WARNING ON APPROACH. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20040811000942004081100094NM 2004 8 11 DLM88040704 120040728A3222 LANDING GEAR DOUG MD88 MD88 3023688NM NOSE UNDERSERVICED A DALAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO27919DL 49584 CREW REPORTS NOSE GEAR UNSAFE LIGHT ON AFTER TAKEOFF. SERVICED NOSE STRUT, SWUNG GEAR. 2L72 4F RTA6WE 20040811000972004081100097WP 2004 8 11 ABXA040279 120040723A5320D0489833 CUSP WEB DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 LEFT CUSP CRACKED AT STA 880. REPLACED LEFT CUSP BETWEEN FS 832 TO 899 IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 20040811000982004081100098SO 2004 8 11 C2XA04SH476 120040802A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716976 145171 SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 22 1/2. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, FIG 208. MAINTENANCE IS AWAITING ENGINEERING APPROVAL FOR REPAIR. 2L72 4T RTT00011AT 20040811000992004081100099EA 2004 8 11 COMA0460401 120040705A3350363782 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01938CA 7046 FLIGHT 5378 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. REPLACED FLOOR LIGHTING BETWEEN ROWS 2 TO 5. 2L72 4F RTA21EA 20040811001012004081100101EA 2004 8 11 SWIA200413588 120040715A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TRIM MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07935SW3681 3681 7725 STAB CHANNEL 1 INOP MESSAGE DISPLAYED ON STATUS PAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-42-05. STAB TRIM ACTUATOR P/N: 8396-2, S/N OFF: 949. 2L72 4F RTA21EA 20040811001022004081100102EA 2004 8 11 SWIA200413589 120040716A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07915SW3218 3218 7615 STAB TRIM AND MACH TRIM CAUTION MESSAGES JUST AFTER T/O AND REPEATED IN FLIGHT. REMOVED AND REPLACED HSTC ACTUATOR AND HRTCU MOTOR IAW CRJ MM 27-42-01 AND 27-42-05 RESPECTIVELY. OPERATIONAL CHECK GOOD. P/N: 7062-3, S/N ON: 602, S/N OFF: 138. 2L72 4F RTA21EA 20040811001042004081100104EA 2004 8 11 SWIA200413591 120040716A2741 TRIM MOTOR CNDAIRCL600 CL6002B19 1900309EA STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07591SW 7079 STABILIZER TRIM FAILED IN FLIGHT, WOULD NOT RESET. STABILIZER TRIM AND MACH TRIM CAUTION MSGS. POWERED DOWN AIRCRAFT. PERFORMED SELF-TEST OF HSTCU. MOTORED STABILIZER TRIM BOTH CHANNELS AND SINGLE CHANNEL FULL TRAVEL 4 TIMES IAW MM 27-40-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040811001052004081100105SO 2004 8 11 SWIA200413592 120040715A2150 A/C PACK EMB 120 EMB120ER 3260203SO LEFT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07568SW 120343 LEFT PACK BLOWING SMOKE INTO THE AIR CONDITIONING SYSTEM. PERFORMED AIR CONDITIONING SYSTEM OPERATIONAL CHECK PER MM 21-50-00. SYSTEM OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040811001092004081100109NE 2004 8 11 COMA0460393 220040623A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RIGHT FAILED A COMAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO01912CA199004869 7011 807354 FLIGHT 5364 RIGHT ENGINE FAILED AFTER T/O. REPLACED THE RIGHT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040811001122004081100112SO 2004 8 11 SWIA200413596 120040718A301038E966A REGULATOR VALVE EMB 120 EMB120ER 3260203SO LT ENGINE LEAKING A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07293SW554 9 IMMEDIATELY AFTER T/O AS RETRACTING WHEELS, MASTER WARNING, MAP DUCT LEAK, AIR CONDITIONING PANEL DUCT LEAK. RETURNED TO LAX. SHUT DOWN LEFT ENGINE ON TAXI WAY. LIGHT OUT ON ENGINE SHUTDOWN. REPLACED LEFT ENGINE PRESSURE REGULATOR IAW MM EMB 30-10-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040811001172004081100117WP 2004 8 11 ABXA040226 120040612A5310991183851 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23959AX 47761 SPOT OF EXFOLIATION ON SHEAR TIE, AFT SIDE OF FS 1123 CANTED AT LONGERON 3 LEFT. INSTALLED NEW CLIP, AFT SIDE FS 1123, LONGERON 3 LEFT IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040811001182004081100118WP 2004 8 11 ABXA040227 120040614A5310991558236 STIFFENER DOUG DC9 DC941 302207NWP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558. 2L72 4F A6WE 20040811001202004081100120WP 2004 8 11 ABXA040230 120040614A53129925558231 STIFFENER DOUG DC9 DC941 302207NWP BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 LEFT. REPAIRED IAW DC-9 SERVICE BULLETIN 53-166. 2L72 4F A6WE 20040811001222004081100122WP 2004 8 11 ABXA040228 120040614A5312991558234 STIFFENER DOUG DC9 DC941 302207NWP BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED IN RADIUS AT LONGERON 12 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558. 2L72 4F A6WE 20040811001232004081100123EA 2004 8 11 COMA0460406 120040708A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01959CA232088286 7116 FLIGHT 5120 FLAPS FAILED DURING APPROACH. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20040811001262004081100126EA 2004 8 11 COMA0470057 120040707A2150GG43620041 SENSOR CNDAIRCL600 CL6002C10 1390015EA LT A/C PACK MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01378CA 10097 FLIGHT 5582 LEFT ENGINE BLEED CAUTION MESSAGE. REPLACED THE LEFT PACK INLET PRESSURE SENSOR. 2L72 4F RTA21EA 20040811001282004081100128NM 2004 8 11 SCNA0412 120040802A3350 LIGHT BOEING737 7378Q8 13844BXNM R1 DOOR BROKEN A SCNAK NONE O OTHER ININSP/MAINT 1 GL15804SY 30689 EMERGENCY EXIT LIGHT FOUND BROKEN ABOVE DOOR R1. REPLACED LIGHT ASSEMBLY. 2L72 4F RTA16WE 20040811001292004081100129EA 2004 8 11 SWIA200413658 120040801A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07937SW CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 LBL 39.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20040811001302004081100130EA 2004 8 11 SWIA200413659 120040801A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07937SW CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 39.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20040811001322004081100132EA 2004 8 11 SWIA200413661 120040801A2750 DRIVE UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07959SW 7840 FLAPS FAIL CAUTION MESSAGE ON TAXI OUT. REPLACED SDU, FLAP SLOW DETECTION, OPERATIONAL CHECK GOOD IAW 27-31-10. 2L72 4F RTA21EA 20040811001352004081100135EA 2004 8 11 COMA0470056 120040708A5610NP13932111 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01391CA2778 10108 FLIGHT 5832 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20040811001362004081100136EA 2004 8 11 COMA0460394 120040625A2150 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01786CA 7333 FLIGHT 5769 LEFT PACK HIGH PRESSURE CAUTION DURING T/O. DEFERRED MAINT ON LEFT PACK PER MEL. 2L72 4F RTA21EA 20040811001372004081100137SO 2004 8 11 SWIA200413663 120040804A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07296SW1212612126 120325 DURING CRUISE, FLAP AND ADVANCED SWS LIGHTS ILLUMINATED. REMOVED AND REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-06. 2L72 4T RTA31SO 20040811001382004081100138EA 2004 8 11 SWIA200413664 120040803A5240 BEARING CNDAIRCL600 CL6002B19 1900309EA SERVICE DOOR ROUGH A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07920SW 7660 GALLEY SERVICE DOOR DIFFICULT TO CLOSE. LUBRICATED/SERVICED SERVICE DOOR CORNER SLIDE BEARINGS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040811001402004081100140WP 2004 8 11 ABXA040278 120040723A5320489833 CUSP WEB DOUG DC9 DC931 3022065WP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 NUMEROUS CRACKS IN LEFT CUSP WEB, FS 945 TO 965. REPLACED LEFT CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 20040811001412004081100141WP 2004 8 11 ABXA040272 120040720A533059114065 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 SKIN WAS CRACKED AT MAIN ENTRY DOOR CUTOUT, UPPER AFT STOP. REPAIRED MAIN ENTRY DOOR CORNER IAW DC-9 SRM 53-05. 2L72 4F A6WE 20040811001422004081100142WP 2004 8 11 ABXA040274 120040721A531359114269 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 LONGERON 12 RIGHT CRACKED AT FRAME STA 944. REPAIRED LONGERON 12 RIGHT, FS FRAME 944 IAW DC-9 SRM 53-02. 2L72 4F A6WE 20040811001432004081100143WP 2004 8 11 ABXA040275 120040722A531199196181 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 LEFT MAIN FRAME STA 718 WAS CRACKED BEYOND LIMITS. REPLACED MAIN FRAME IAW JOB CARD EA 53400323-001-2. 2L72 4F A6WE 20040811001442004081100144WP 2004 8 11 ABXA040276 120040722A53159922397501 FLOORBEAM DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 FLOORBEAM CORRODED AT STA 937, RIGHT BUTTLINE 18. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05. 2L72 4F A6WE 20040811001462004081100146WP 2004 8 11 ABXA040273 120040721A5313591140911 LONGERON DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 LONGERON 17 RIGHT CRACKED AT FRAME STA 560. REPLACED DAMAGED SECTION OF LONGERON IAW DC-9 SRM 53-02. 2L72 4F A6WE 20040811001472004081100147NM 2004 8 11 SWAA042254 120040807A575465C26602312 SKIN BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT WEDGE, DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT WEDGE PER MM. 2L72 4F RTA16WE 20040811001502004081100150NM 2004 8 11 SWAA042257 120040808A3350BR2013 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND AFT CABIN EEPLS INOP. REMOVED AND REPLACED AFT EEPLS ASSEMBLY PER MM. 2L72 4F A16WE 20040809000812004080900081EA 2004 8 9 COMA0460411 120040714A2750857D100401 COUPLING CNDAIRCL600 CL6002B19 1900309EA TE FLAPS BROKEN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01989CA 7215 FLIGHT 9494 FLAPS FAIL CAUTION MESSAGE. REPLACED BROKEN FLEX SHAFT, RIGHT NR 4 POSITION. 2L72 4F RTA21EA 20040809000962004080900096NM 2004 8 9 SWAA042237 120040805A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29718SW 27852 DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 19 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040809000982004080900098 2004 8 9 SWAA042221 420040804A256565C16820 HOOK BOEING737 7373H4 1384600NM R1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20040809001172004080900117NM 2004 8 9 DLM88040718 120040803A5313 STRINGER DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27921DL 49645 CRACK IN STRINGER 1 AT JOINT WITH STA Y=160, CRACK IN NR 2 LT STRINGER AT JOINT WITH STA Y=160, CRACK IN NR 4 LT STRINGER AT JOINT WITH STA Y=160 AND Y=180. REPLACED NR 1 STRINGER, SPLICED IN NEW SECTION FOR STRINGERS NR 2 & 4. 2L72 4F RTA6WE 20040809001292004080900129NM 2004 8 9 DL777040727 120040805A2560P4010021 BATTERY BOEING777 777232 1385232NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27864DA 29736 REPLACED FLASHLIGHT AT POS 2L FOR LOW BATTERY LIGHT. 2L72 4F RTT00001SE 20040809001352004080900135NM 2004 8 9 DL73G040733 120040807A243260B400177 BATTERY BOEING737 73735B 13844BMNM MASTER ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27222DZ 23971 AIR TURNBACK, ODOR OF ELECTRICAL IN CABIN. REPLACED BATTERIES AND CHARGER. 2L72 4F RTA16WE 20040810000042004081000004NM 2004 8 10 ASAA0410279 120040601A335007912 LENS BOEING737 7372X6C 1384552NM EMERGENCY LIGHT MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM01747AS 23124 ANC - FOUND ROW 18 EMERGENCY FLOOR TRACK LIGHT MISSING LAMP IN GALLEY AREA. REPLACED MISSING CLEAR LENS COVER. (M) 2L72 4F RTA16WE 20040810000082004081000008NM 2004 8 10 ASAA0440100 120040407A5311655828064 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 GYR - FOUND STATION 360 AT 8L FRAME IS CRACKED AT SIDEWALL ATTACHMENT BRACKET. REPAIRED FRAME AT STATION 360 AT 8L. (M) 2L72 4F RTA16WE 20040810000342004081000034NM 2004 8 10 ASAA0440127 120040510A533065C329541 SKIN BOEING737 737490 1384715NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 GYR - FOUND LOWER FUSELAGE BELLY SKIN IS CREASED ALONG THE FRAME AT FS 827 BETWEEN STRINGER 27L AND 27R. TRIMMED OUT DAMAGED AREA AND REINSTALLED REPAIR DOUBELR PER SRM 53-00-01 DETAIL 11 PAGE 368 AT STATION 827 BETWEEN STRINGER 27L AND 27R LOWER FUSELAGE. (M) 2L72 4F RTA16WE 20040810000412004081000041NM 2004 8 10 ASAA0440113 120040405A53136545778 STRINGER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 GYR - FOUND AFT PIT STRINGER 25R IS EXFOLIATED AT STATION 940. CUTOUT DAMAGED SECTION OF STRINGER, FABRICATED REPAIR PART AND INSTALLED REPAIR IAW SRM 53-00-03 FIG 201. (M) 2L72 4F RTA16WE 20040810000502004081000050NM 2004 8 10 SWAA042252 120040807A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29405WN 27893 FWD EEPLS COVER LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040810000552004081000055NM 2004 8 10 SWAA042242 120040806A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29405WN 27893 EEPLS AT ROW 1 ABC WIRES EXPOSED AND COVER LOOSE. STOWED WIRES AND SECURED COVER PER MM. 2L72 4F RTA16WE 20040810000652004081000065WP 2004 8 10 ABXA040251 120040625A5313 LONGERON DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23828AX 45999 AFT LOWER CARGO COMPARTMENT, STA 1380, AT LONGERON 36, THE FORWARD SIDE OF FRAME 1380 HAD CORROSION. BLENDED AND REMOVED ALL CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR PARTS IAW REA D853-49155MR. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-20B. 2L74 4F 4A25 20040810000682004081000068SO 2004 8 10 SWIA200413646 120040720A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07584SW 120352 RIGHT HAND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM 33-52-01, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040810000702004081000070WP 2004 8 10 ABXA040259 120040628A521099557533 FRAME DOUG DC9 DC932 3022066WP PAX DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23880DP 47635 INTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM THIRD LIGHTENING HOLE FROM TOP. STOP DRILLED CRACK AND REPAIRED PASSENGER DOOR NR 2 BEAM AFT END IAW DC-9 MM. 2L72 4F A6WE 20040810000732004081000073WP 2004 8 10 ABXA040261 120040628A575499193987 SUPPORT DOUG DC9 DC932 3022066WP RT WING SLAT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23880DP 47635 LEFT SLAT DRIVE LOWER INBOARD BOLT ATTACHMENT SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 20040810000892004081000089WP 2004 8 10 ABXA040247 120040720A32607000010101ABX DOWNLOCK SWITCH DOUG DC9 DC931 3022065WP MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23924AX 47403 DURING GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE WHILE THE NOSE GEAR UNSAFE LIGHT STAYED LIT. THE GEAR WAS RECYCLED. AFTER ONE MINUTE, THE NOSE GEAR CAME DOWN AND LOCKED. REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC-9 MM 32-60-10. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 20040810000922004081000092WP 2004 8 10 ABXA040241 120040623A5420591326218 ATTACH ANGLE DOUG DC9 DC932 3022066WP LT ENG PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 NR 2 PYLON UPPER ATTACH ANGLE CRACKED STA 980 LONGERON 14. REPAIRED NR 2 PYLON UPPER ATTACH ANGLE STA 930 LONGERON 14 IAW DC-9 SRM 54-04-10. INSTALLED FASTENERS IAW DC-9 SRM 51-30-5 AND PROTECTED AREA AGAINST CORROSION IAW DC-9 SRM 51-30-3. 2L72 4F A6WE 20040810000992004081000099WP 2004 8 10 ABXA040267 120040729A531199196171 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 LEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273. 2L72 4F A6WE 20040810001032004081000103NM 2004 8 10 DL767040671 120040720A5753113T12265 SUPPORT BEAM BOEING767 767232 1385132NM TE FLAPS CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27114DL 22226 LEFT AND RIGHT INBOARD FLAP INBOARD AND OUTBOARD SUPPORTS CORRODED. REPAIRED IAW ERA 091244-14. 2L72 4F RTA1NM 20040810001042004081000104NM 2004 8 10 DL73S040672 120040720A555165505817 ATTACH FITTING BOEING737 737247 138448DNM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 HORIZONTAL STABILIZER ATTACH LUGS CORRODED. REPAIRED IAW ERA 091571-14AD. 2L72 4F A16WE 20040810001142004081000114NE 2004 8 10 DLM88040734 220040807A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 MALFUNCTIONED A DALAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO27972DL31684 53215 726047 NR 2 ENGINE N1/EGT EXCEEDANCE. ABORTED TAKEOFF AT 100 KIAS. REPLACED FAN. 2L72 4F4 FRTA6WE E9NE 20040810001192004081000119EA 2004 8 10 SWIA200413643 120040726A33503472001001 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7701 AFT EMERGENCY FLOODLIGHT INOP. RE-ENGAGED BULB IN AFT EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040811000172004081100017SO 2004 8 11 C2XA04TY142 120040803A532014525800006 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000222004081100022SO 2004 8 11 C2XA04SD005 120040801A33501127641 COVER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT CRACKED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2721144 145741 SDF - DURING 2A CHECK FOUND PAX DOOR PHOTOLUMINESCENT LIGHT STRIP COVER CRACKED. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP COVER. AIRCRAFT APPROVED AND RETURNED TO SERVICE. 2L72 4F RT 20040811000342004081100034SO 2004 8 11 SWIA200413645 120040730A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07289YV5992 5992 120289 FORWARD EMERGENCY EXIT 3 LIGHTS IN FLOOR STRIP INOPERATIVE. REPLACED FORWARD EMERGENCY BATTERY IAW MM 33-50-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040811000392004081100039NM 2004 8 11 DL73G040739 120040806A3350 CONNECTOR BOEING737 73735B 13844BMNM EMERGENCY LIGHT DISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27225DL 25069 ON PRE-DEPARTURE FOUND ROWS 1 AND 2 DEF EMERGENCY LIGHTS INOP ON SEATS. PINS WERE FOUND OUT OF THE CONNECTOR AND RE-INSERTED INCORRECTLY RESULTING IN THE FUSABLE LINK AT THE BATTERY CHARGER M1132 FAILING. REPLACEMENT OF FUSABLE LINK CORRECTED THE SITUATION. 2L72 4F RTA16WE 20040811000592004081100059EA 2004 8 11 VNAA0407010 120040731A5220 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT ILLUMINATED A VNAAO OTHER J WARNING INDICATION DEDESCENT 1 GL07256PS 7937 DURING DESCENT, THE CREW RECEIVED A LEFT HAND EMERGENCY EXIT DOOR AMBER CAS MESSAGE WHICH EXTINGUISHED AT 8,000 FEET. MAINTENANCE THEN MEL'D THE EXIT DOOR IN ACCORDANCE WITH 52-70-03 CODE-C. 2L72 4F4 FRTA21EA E15NE 20040811000622004081100062WP 2004 8 11 ABXA040266 120040729A56105613217520 WINDOW DOUG DC8 DC861 3021952WP COCKPIT STICKING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23842AX 46015 FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REPLACED FIRST OFFICER'S SLIDING WINDOW IAW DC8 56-10-0. 2L74 4F 4A25 20040811000662004081100066SO 2004 8 11 C2XA04TY131 120040802A532014530628001 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FR 25. REMOVED AND REPLACED THE OMEGA BEAM BETWEEN FR 22 AND FR 25. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-40-02 AND WILL BE RELEASED UPON COMPLETION OF ALL 4C WORK. 2L72 4F RTT00011AT 20040811000792004081100079NM 2004 8 11 SWAA042218 120040803A55536547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB FITTING LUGS, CORRODED. REPAIRED VERTICAL STAB FITTING LUGS PER SRM AND ER. 2L72 4F RTA16WE 20040811000802004081100080NM 2004 8 11 SWAA042206 120040801A335007912 COVER BOEING737 7372T4 1384492NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29702ML 22054 EEPLS COVER AT RIGHT OVERWING EXIT LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F A16WE 20040811000932004081100093NM 2004 8 11 DL76L040703 120040727A7830 PROXIMITY SWITCH BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENG T/R MALFUNCTIONED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27192DN27635 28449 727754 AMBER REV ANNUNCIATION OCCURRED ON TAKE/OFF, UPON PUSHING LEVER UP TOWARD TAKEOFF POWER. ANNUNCIATION OCCURRED LESS THAN 40 KNOTS. REPLACED PROX SWITCH. 2L72 4F4 FRTA1NM E24NE 20040811001112004081100111SO 2004 8 11 SWIA200413595 120040717A3010 DUCT EMB 120 EMB120ER 3260203SO ENGINE BLEED LEAKING A SWIAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 NM07293SW ON TAKEOFF OUT OF LAX AT ABOUT 300 FT, RECEIVED A DUCT LEAK ON LEFT ENGINE. SHUTDOWN LEFT ENGINE AND LIGHT EXTINGUISHED AFTER 2-3 MINUTES. RETURNED TO LAX. REINSTALLED COVER OVER REGULATING VALVE. RAN ENGINE WITH BLEEDS IN LOW AND AUTO FOR 1/2 HOUR. NO DEFECTS NOTED. 2L72 4T RTA31SO 20040811001152004081100115SO 2004 8 11 SWIA200413583 120040710A2701 SPRING EMB 120 EMB120ER 3260203SO CONTROL COLUMN BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM0757734 120199 ELEVATOR FEELS HEAVY. INSTALLED SERVICEABLE SPRING ON CAPTAINS CONTROL COLUMN. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040811001212004081100121WP 2004 8 11 ABXA040231 120040614A5312991558239 STIFFENER DOUG DC9 DC941 302207NWP BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 15 LEFT. REPAIRED STIFFENER IAW DC-9 DWG J060110. 2L72 4F A6WE 20040811001242004081100124EA 2004 8 11 COMA0460399 120040629A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 FUSELAGE SKIN CRACK BEHIND NOSE LANDING GEAR AFT DOOR ON RIGHT SIDE. REPAIRED IAW REO 601R-53-11-048 AND REO 601R-53-11-781. 2L72 4F RTA21EA 20040811001252004081100125EA 2004 8 11 SWIA200413657 120040801A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07937SW FUSELAGE PULLEY INTERCOSTAL IS CRACKED ON OUTBOARD FLANGE; FS 484.00 RBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SERVICEABLE ANGLE IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20040811001512004081100151NM 2004 8 11 SWAA042258 120040808A33506556633 LIGHT BOEING737 7372T4 1384492NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REPAIRED WIRE SPLICE PER MM. 2L72 4F A16WE 20040811001542004081100154NM 2004 8 11 SWAA042261 120040808A521065C346701 FITTING BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE FITTING, CRACKED. REMOVED AND REPLACED UPPER HINGE FITTING PER SRM. 2L72 4F RTA16WE 20040811001562004081100156EA 2004 8 11 COMA0460448 120040809A2913601R751547 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01916CA176293036 7014 FLIGHT 5090 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2L72 4F RTA21EA 20040811001582004081100158EA 2004 8 11 COMA0460450 120040808A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01981CA10631 7163 FLIGHT 5748 GEAR DISAGREE WARNING. REPLACED HYDRAULIC PUMP 3A. 2L72 4F RTA21EA 20040811001592004081100159EA 2004 8 11 COMA0470061 120040808A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA HYD SYSTEM UNRELIABLE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01354CA898 10064 FLIGHT 5020 NR 2 HYDRAULIC SYSTEM HIGH TEMP WARNING. REPLACED THE RIGHT ENGINE HYDRAULIC PUMP. 2L72 4F RTA21EA 20040811001612004081100161EA 2004 8 11 COMA0460434 120040730A3810 WATER HEATER CNDAIRCL600 CL6002B19 1900309EA GALLEY ODOR A COMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01804CA 7352 FLIGHT 5126 F/A REPORTS ELECTRIC SMELL IN GALLEY AREA. SMELL DISPATCHED WITH POWER OFF. DEACTIVATED AND DEFERRED GALLEY PER MEL. 2L72 4F RTA21EA 20040811001622004081100162NM 2004 8 11 HNAA00064 120040707A532085320686101 THRESHOLD DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07933HA 134 AIRSTAIR DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED THRESHOLD. 2H72 4T RTA13NM 20040811001652004081100165NM 2004 8 11 MWEA040105 120040618A2420762904D PCDU BOEING717 717200 1383700NM APU INOPERATIVE A MWEAD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 GL31917ME 55180 RECEIVED ELECTRICAL FAULT, CENTER TRANSMITTER SHOWS 29 VOLTS AND ZERO LOAD. REMOVED AND REPLACED POWER CONVERSION AND DISTRIBUTION UNIT. 2L72 4F TRA6WE 20040811001682004081100168NM 2004 8 11 P5CA0401112 120040703A5230P20702 ACTUATOR BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE CARGO DOOR INOPERATIVE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23355MC 23395 BEFORE DEPARTURE COULD NOT LOCK LATCHES ON MAIN CARGO DOOR. REPLACED LATCH ACTUATOR, OPS CHECK OK AS PER MM 52-32-09. 2L74 4F4 FRTA20WE E23EA 20040811001692004081100169NM 2004 8 11 750WL0007 120040801A3350 LAMP BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY TRACK LIGHT OPPOSITE ROW 3 INOP. RELAMPED TRACK LIGHTING AT ROW 3. OPS CHECKS GOOD. 2L72 4F RTA2NM 20040811001712004081100171WP 2004 8 11 MWEA040110 120040624A2420976J2544 GENERATOR DOUG DC9 DC981 3022081WP LEFT INOPERATIVE A MWEAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 GL31804ME 48030 LEFT GENERATOR FAILED. REMOVED AND REPLACED LEFT GENERATOR. 2L72 4F A6WE 20040811001742004081100174EA 2004 8 11 COMA0460436 120040727A5610NP13932111 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAB EMER. DESCENT O OTHER CRCRUISE 1 SO01868CA3608 1991 7427 FLIGHT 5005 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20040811001752004081100175WP 2004 8 11 0401239760 120040716A217017946081 SEPARATOR DOUG DC9 DC941 302207NWP A/C PACK ODOR A NWAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL01760NW 47288 JUST AS AIRCRAFT LEVELED OFF AT FL220, A STRONG ELECTRICAL SMELL AND LIGHT SMOKE APPEARED IN THE CABIN. BOTH THE FORWARD AND AFT LAVATORY SMOKE DETECTORS ACTIVATED. NO MENTION OF COM COMPLIANCE OR PACK CONFIGURATION. CREW DECLARED AN EMERGENCY AND RETURNED TO AN OVERWEIGHT LANDING AT DTW. MAINTENANCE DID NOT FIND ANY OBVIOUS FAULT OR ANY EVIDENCE OF FIRE. POSSIBLE INGESTION OF INSULATION BY PACK COOLING FAN MAY HAVE CAUSED BURNING SMELL. MAINTENANCE CLEANED THE HEAT EXCHANGER AND REPLACED THE WATER SEPARATORS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040811001772004081100177NM 2004 8 11 HNAA0407102 120040720A491078279010 APU DHAV DHC8 DHC8102 2809003NM APU BAY VIBRATES A HNAAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 EA07828EX22371453 392 FLIGHT 4097 REPORTED THE APU VIBRATING THE WHOLE AIRCRAFT WITH AN ASSOCIATED BURNING SMELL IN THE AFT CABIN AREA. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE AIR CYCLE MACHINE GRINDING. THE UNIT WAS REMOVED AND REPLACED AND THE SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040811001792004081100179NM 2004 8 11 AT0400014 120040704A3350 LIGHT BOEING717 717200 1383700NM CABIN SMOKE A ZZDAK NONE BL SMOKE/FUMES/ODORS/SPARKS NO TEST ININSP/MAINT 1 SO15933AT 55071 WHEN TESTING EMERGENCY LIGHTS, AISLE PATH LIGHTS STARTED TO SMOKE. TURNED OFF LIGHTS AND SMOKE STOPPED. RELAMPED EMERGENCY EXIT LIGHTS AT 20D, OPS CHECKED GOOD IAW 33-51. 2L72 4F TRA6WE 20040811001802004081100180 2004 8 11 249TR0032 420040801A2230106198246 COMPUTER BOEING737 7372K5 138448XNM AUTO THROTTLES MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO THROTTLES WILL ONLY ARM EVERY OTHER FLIGHT AND WHEN DISENGAGED TO DO TREND, AUTO THROTTLES WILL NOT RE-ARM. REPLACED AUTO THROTTLE COMPUTER AND OPS CHECKED PER MM 22-31-01. 2L72 4F RTA16WE 20040811001832004081100183NM 2004 8 11 MWAE040126 120040730A2931 BYPASS VALVE BOEING717 717200 1383700NM ELEVATOR OPEN A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31913ME 55176 LEFT HYDRAULIC TEMPERATURE HIGH CAME ON. FOUND ELEVATOR BYPASS VALVE OPEN. CLOSED VALVE, OPERATED BOTH HYDRAULIC SYSTEMS WITHOUT DISCREPANCY. 2L72 4F TRA6WE 20040811001852004081100185NM 2004 8 11 HNAA0407104 120040723A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM BAGGAGE BAY INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07984HA215451952 377 WHILE IN MAINTENANCE IT WAS REPORTED AS THE NR 1 BAGGAGE BAY SMOKE DETECTOR AS BEING INOPERATIVE UPON TEST. MAINTENANCE REMOVED AND REPLACED THE NR 1 SMOKE DETECTOR. SYSTEM OPERATIONAL CHECKS GOOD. 2H72 4T RTA13NM 20040811001862004081100186 2004 8 11 372PA0047 420040716A22104051600913 COMPUTER BOEING737 737306 13844BGNM FLT DIRECTOR FAILED A PIDAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION NRNOT REPORTED 1 SO05372PA 23546 FIRST OFFICER'S FLIGHT DIRECTOR INOPERATIVE AND SPEED TRIM FAIL AND MACH TRIM LIGHTS ILLUMINATED ON RECALL DURING LANDING CHECKS (SINGLE CHANNEL FAILURE). REPLACED B-CHANNEL FCC. BITE TEST AND OPS CHECKS NORMAL PER MM 22-10. 2L72 4F RTA16NE 20040811001892004081100189NM 2004 8 11 0401126301 120040625A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21 ABC - 31 ABC. RECONNECTED WIRE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040811001902004081100190NM 2004 8 11 SWAA042262 120040808A534065C360751 FITTING BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29376SW 26584 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED LOWER HINGE FITTING PER SRM. 2L72 4F RTA16WE 20040811001922004081100192NM 2004 8 11 SWAA042263 120040808A3350OL3071BPEGL LAMP BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 6 ABC, 8 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20040811001942004081100194NM 2004 8 11 SWAA042265 120040808A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS FADED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040811001952004081100195NM 2004 8 11 SWAA042266 120040808A53116545808 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 294, STRINGER 16R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040811001962004081100196NM 2004 8 11 SWAA042267 120040808A53116545806 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FRAME WEB AT BS 294, STRINGER 11R, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2L72 4F RTA16WE 20040811001992004081100199NE 2004 8 11 MWEA040120 220040712A7321ARG10250 THERMOCOUPLE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE ENGINE ILLUMINATED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31904ME 55168 LEFT ENGINE SYSTEM FAIL ALERT CAME ON. REMOVED AND REPLACED LEFT ENGINE CHANNEL A AND B T-30 THERMOCOUPLES. 2L72 4F4 FTRA6WE E00061EN 20040811002002004081100200NM 2004 8 11 HNAA0407103 120040723A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM BAGGAGE BAY INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07808EX113051930 299 FLIGHT 3807 PILOT REPORTED THE NR 1 SMOKE WARNING TEST FOR THE BAGGAGE COMPARTMENT UNIT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE NR 1 SMOKE DETECTOR AND OPERATIONAL CHECKED THE SYSTEM. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040811002012004081100201NM 2004 8 11 252TR0022 120040715A33506013211 BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 LEFT WING OVERWING EMERGENCY EXIT LIGHT OUT AND LEFT FORWARD ENTRANCE DOOR EMERGENCY SLIDE LIGHT OUT. REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK AND LEFT FORWARD ENTRANCE DOOR EMERGENCY SLIDE BATTERY PACK. 2L72 4F RTA16WE 20040811002062004081100206NM 2004 8 11 SWAA042278 120040808A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040811002072004081100207NM 2004 8 11 SWAA042279 120040808A53116546546 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 807, STR 27L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040811002082004081100208NM 2004 8 11 SWAA042280 120040809A7830315A1500533 SLEEVE BOEING737 7375H4 138449DNM THRUST REVERSER MISSING A SWAAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW29526SW 26568 DURING FLIGHT, NR 1 ENGINE THRUST REVERSER UNLOCKED LIGHT, ENGINE LIGHT AND REVERSER LIGHT ILLUMINATED. UPON LANDING FOUND NR 1 THRUST REVERSER SLEEVE DEPARTED. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER OUTBOARD SLEEVE PER MM. 2L72 4F RTA16WE 20040811002092004081100209 2004 8 11 SWAA042281 420040809A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29073SW 22673 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040812000032004081200003NM 2004 8 12 UPS04442811 120040714A5313 LONGERON BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING NR 17 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. ( BS 1241 BULKHEAD SPLICE STRAP AFT HOLE) NR 17 MOUNT BOLT HOLE CORRODED, CLEANED BY OVERSIZE BOLT HOLE .0156 INCH IAW SRM51-30-05 BUT FOUND SPLICE STRAP CRACKED RUNNING FWD AND AFT BY HFEC INSP. IAW NTM PART 6.51-00-00 FIG 1 FURTHER REFER UPS RECORD SPLICE STRA WERE PREVIOUSLY INSPECTED AND CRACK DOCUMENTED RE-INSP. NOT DUE FOR ANOTHER 1600 CYC AND SCHEDULED SPLICE STRAP REPLACEMENT. 2L74 4F RTA20WE 20040812000052004081200005NM 2004 8 12 UPS04442813 120040714A5320 FITTING BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 5 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. LT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 5 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 INCH IAW SRM 51-30-05 PAGE 13 AND MOUNT BOLT ALSO REPLACED IAW MM 20-51-01. 2L74 4F RTA20WE 20040812000062004081200006SO 2004 8 12 LR7A04066 120040717A27203773041 BOOT LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL RUDDER DISLODGED A LR7AA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 AL03403LC4 4590 HEARD A LOUD NOISE IN THE CARGO COMP, PRESSURIZATION WENT TO ZERO, AT 5000 FT IAW MINUTE NOTICE LIGHT COMING IN ON BOTH SIDE OF AFT DOOR. DECENDED TO 11,000 FT DUMPED APPROX 7000 LBS ALTITUDE AT TIME OF INCIDENT 20,000 FT, DID NOT GET A DOOR WARNING LIGHT. PRESSURE OF 13IN. TROUBLESHOOTING CARRIED OUT FOUND RUDDER BOOT ASSY DISLODGED FROM HOUSING ON A/C STRUCTURE SIDE. BOOT ASSY. REMOVED AND REPLACED IAW SMP 581-27-20 PG 210B. P/N 377304-1 (1 EA). PRESS LEAK CHECK C/OUT IAW SMP 581-21-30 PG 217/218 FIG 21-30-07 FOUND SATISFACTORY. 2H74 4T4 T A1SO E282 20040812000152004081200015WP 2004 8 12 IXXA0400067S 120040501A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING OB LE LOWER SKIN CRACKED .5000 INCH. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 AND 51-1-20D PG1. REMOVED DAMAGED AREA IAW DWG V82-R01. PERFORMED NDT INSPECTION IAW NDT SPM PART 06-10-01.001. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER AND A FILLER IAW DWGV82-R01. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLERS INTERIOR SURFACE AND FILLER IAW SRM 51-1-8B. APPLIED PAC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG1. INSTALLED THE REPAIR DOUBLER AND FILLER ONLY WING OB LE LOWER SKIN USING NEW FASTENER IAW DWG V82-R01, SRM 51-1-21 AND 51-1-20D PAGES 1 AND 9. 2L74 4F4 FRT4A25 E2GL 20040812000162004081200016WP 2004 8 12 IXXA0400080S 120040518A5240 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE SERVICE DOOR DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE A-CHECK INSPECTION, FOUND AFT SERVICE DOOR HAS INTERIM REPAIR ON UPPER AFT CORNER, STA 1660.000 L-11R TD L-98. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW SRM 53-2-0, FIG 76, TR NR 53-197 MAR 26/04 REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG. 1, REMOVED DAMAGED SECTION IAW SRM 53-2-0, FIG. 16 PG. 109-110 FABRICATED FILLER & DOUBLER TREATED AND PRIMED AREA, FILLER, DOUBLER & TRIPLER IAW SRM 51-1-8B INSTALLED CONICAL WASHER IAW DC8 SRM 51-1-26 PG. 1 APPLIED (PRC) SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9 INSTALLED FILLER DOUBLER & TRIPLER IAW SRM 53-2-0 PG. 108-110, SRM 51-1-21 PG. SRM 51-1-20D PG. 9 ALL ENTERED ON LP NR 094771 ITEM 5M. 2L74 4F4 FRT4A25 E2GL 20040812000212004081200021NM 2004 8 12 2004UALA00697 120040726A5320 CHANNEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29563UA 26665 AFT CABIN PRESS DECK HAT CHANNEL STA 1715 TO 1730 IS CORRODED. FABRICATED & INSTALLED NEW HAT CHANNEL. 2L72 4F4 FRTA2NM E17NE 20040812000222004081200022WP 2004 8 12 IXXA0400072S 120040503A5753 VANE DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE RT WING FLAP ELONGATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 ROUTINE C-CHECK INSP FOUND RT IB VANE SLOT ELONGATED HOLES AT STA XS. 250.089. REPAIR WAS ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREAS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DWG V82-R07. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL DOUBLER AND FILLER AND INTERNAL DOUBLER IAW DWG VR2-R07. CLEANED, TREATED AND PRIMED REPAIR DOUBLER INTERIOR SURFACE, FILLER AND INTERNAL DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG1. INSTALLED EXTERNAL DOUBLER, FILLER AND INTERNAL DOUBLER ON RT IB VANE SLOT USING NEW FASTENERS IAW DWG V82-R07, SRM 51-1-21 PG.1, SRM 51-1-20D PG7. 2L74 4F4 FRT4A25 E2GL 20040812000232004081200023WP 2004 8 12 IXXA0400073S 120040503A5512 SKIN PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE HORIZONTAL STAB DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION FOUND RT HORIZONTAL STABILIZER LE HAS AND INTERIM REPAIR. STA XFS 210.000. REPAIR WAS ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER AND FILLER IAW SRM 55-2-1 PG 17 FIG 4. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INTERIOR IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS IAW SRM 51-1-21 PG 1. 2L74 4F4 FRT4A25 E2GL 20040812000242004081200024WP 2004 8 12 IXXA0400084S 120040603A5320 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE A-CHECK INSPECTION, FOUND ALT. CARGO COMPT FITTING CRACKED AT STA 1260.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW SRM 53-1-0 PAGE, PAIR SPECIFICATION NR 2003-05M DWG NR 3350223, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, TRIMMED FOR CRACKED FITTING REMOVAL IAW SRM 53-2-2 FIG 10, REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED STANDARD LONGERON SPLICE, (TR NR 53-193 MARCH 15/04) DWG SR08530009, FABRICATED FITTING, IAW SRM REPAIR SPECIFICATION PART 08-00-02102, SRM 53-2-2 FIG 10M CLEANED, TREATED AND PRIMED STANDARD LONGERON SPLICES & FITTING WITH FASTENERS IAW DC8 SRM 51-1-20D PAGE 9. 2L74 4F4 FRT4A25 E2GL 20040812000252004081200025WP 2004 8 12 IXXA0400074S 120040503A5512 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE HORIZONTAL STAB DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND RT HORIZONTAL STAB LE HAS AN INTERIM REPAIR. STA XFS. 109.750. REPAIR WAS ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG1. FABRICATED DOUBLER. CLEANED, TREATED AND PRIMED AREA AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PAGE 1. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 55-2-1 PG 17. FIG 4, SRM 51-1-21 PG1, SRM 51-1-21A PAGES 1-4. 2L74 4F4 FRT4A25 E2GL 20040812000262004081200026WP 2004 8 12 IXXA0400075S 120040503A5532 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE VERTICAL STAB DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND VERTICAL STAB LE HAS AN INTERM REPAIR STA ZFS 179.750. REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1, FABRICATED FILLER AND DOUBLER IAW SRM 55-2-1 PG 17 FIG 4. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER & DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-15 PG 1. INSTALLED FILLER & DOUBLER IAW SRM 55-2-1 PG 17 FIG.4 SRM 51-1-21 PG 1. 2L74 4F4 FRT4A25 E2GL 20040812000272004081200027NM 2004 8 12 04FDEA02293 120040729A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING, IB FLAP OB HINGE (FLAP SIDE) PIVOT HOLE NR 1, OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 PAGES 442 TO 443. ORIGINAL DIAMETER= 1.187, FINAL DIAMTER= 1.257" AND REPAIRED AS PER FEDEX EA 1-5750-80283, TITLE: WINGS - TRAILING EDGE FLAPS - LT INBOARD FLAP (FLAP SIDE) - PIVOT BORE REPAIR. 2L73 4F RTA22WE 20040812000282004081200028NM 2004 8 12 04FDEA02296 120040730A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT NR 29 BARREL NUT CORRODED REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80301, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040812000302004081200030WP 2004 8 12 IXXA0400082S 120040602A5230 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE CARGO DOOR DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE A-CHECK INSPECTION FOUND B-CARGO DOOR HAS REPAIRS & DENTS ON EXTERIOR SKIN AND .2500 INCH BROKEN AT RT SIDE EDGE. REPAIRS WERE ACCOMPLISHED BY PERFORMING REPAIR IAW SRM 52-10 PG. 1, SRM 52-4-1 PG. 2 FIG. 1, REMOVED DAMAGED EXTERIOR SKIN IAW SRM 51-1-21 PG. 1-2, FABRICATED NEW EXTERIOR SKIN, DOUBLER PLATE & EXTERNAL DOUBLERS, IAW SRM 52-4-1 PG. 2 FIG. 1 CLEANED, TREATED AND PRIMED AREA OF EXTERIOR SKIN, DOUBLER PLATE & EXTERNAL DOUBLERS IAW SRM 51-1-11 PG. 9 INSTALLED DOUBLER PLATE, EXTERIOR SKIN & EXTERNAL DOUBLER IAW SRM 51-1-21 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20040812000312004081200031NM 2004 8 12 04FDEA02298 120040730A1430 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT NR 33 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80290, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 33R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040812000332004081200033NM 2004 8 12 04FDEA02300 120040730A1430 BARREL NUT DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT NR 32 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79832, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 32L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F4 FRTA22WE E13NE 20040812000342004081200034WP 2004 8 12 0401001225 120040617A2612 FIRE LOOP DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01225NW 46582 ON CLIMBOUT AT 31,000 FT, RECEIVED NR 2 ENGINE FIRE WARNING INDICATION. NR 2 ENGINE B-LOOP WAS PUT ON MEL. SHUT DOWN NR 2 ENGINE IAW COM PROCEDURE. DUMPED 90,000 LBS OF FUEL AND RETURNED TO NRT FOR AN UNEVENTFUL LANDING. WORK IN PROGRESS-SUPPLEMENTAL INFORMATION TO FOLLOW. 2L73 4F4 F A22WE E23EA 20040812000352004081200035NM 2004 8 12 AALA20040819 120040810A33501000679 LIGHT BOEING767 767223 1385123NM GE CF6 CF680 30025NE CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21325AA 22326 EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA1NM E13NE 20040812000362004081200036NM 2004 8 12 AWXA200400747 120040707A1420ZZLRC12147S CONNECTOR BOEING757 757225 1384959NM RROYCERB211 RB211* 54555NE NR 2 ENGINE WORN A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28907AW 22691 ON TAKEOFF ROLL NR 2 ENG WOULD NOT REACH TAKEOFF EPR WITH THRUST LEVER FULL FORWARD & ENGINE LIMITER OFF, ENGINE PARAMETERS NORMAL FOR LOW EPR, REJECTED TAKEOFF 90 KTS. MX RAN ENGINES TO TAKEOFF POWER 3 TIMES, ALL INDICATIONS NORMAL. ISSUED MEL 73-21-09 COND. 1, (RT ENG LIMITER INOP). MAINTENANCE T/S/S, BITE CHECK OF ELECTRONIC ENGINE CONTROLS (EEC) FOUND FAULT CODES F2 B3 35 & F0 B3 35. IAW FAULT ISOLATION MANUAL SWAPPED NR 2 ENGINE EEC'S 1 AND 2. VISUAL INSP OF WIRING FOUND PINS 1, 2 OF DEDICATED GENERATOR CONNECTOR PLUG D1384 WITH BAD PIN RETENTION. REPLACED CONNECTOR PLUG D1384 AND RE-TERMINATED ALL 7 WIRES IAW WDM 71-51-11, PG. 1 SHEET 6. PERFORMED ENG RUN OPS CHECK, SYSTEM OPERATED NORMALLY. 2L72 4F4 FRTA2NM A12EU 20040812000372004081200037NM 2004 8 12 AWXA200400755 120040708A2560P2070001214 FLASHLIGHT BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE ZONE 900 - LAVATINOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 EMERGENCY EQUIPMENT, DURING 4-DAY CHECK THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040812000392004081200039NM 2004 8 12 AWXA200400757 120040620A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MAJOR REPAIR, DURING C-15 CHECK, A .5000 INCH CRACK WAS FOUND IN FLOORBEAM AT FASTENER HEAD IN WEB BS 700, LBL 24.5, WL 204. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR BEAM WEB AT BS 700, LBL 24.5, WL 204; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A REINFORCING DOUBLER; INSTALLED REPAIR PARTS IAW AWA E R 03-5702-04184-ES2A. 2L72 4F4 FRTA16WE E2GL 20040812000422004081200042 2004 8 12 RAIA00407013 420040706A22117010680938 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP TRIM WARNING MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03574HK14053 41093 5534 - STL - TRIM WARNING LIGHT CAME ON. MAINTENANCE DEFERRED ELECTRIC TRIM IAW MEL. SUBSEQUENTLY REMOVED AND REPLACED AUTO PILOT COMPUTER. 2L72 4T3 TRTA41NM E2WE 20040812000452004081200045GL 2004 8 12 RAIA00407016 220040726A732023076627 FADEC EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 1 ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03808HK11267 145157 NO DISPATCH MESSAGE, NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FADECS. 2L72 4F4 FRTT00011ATTE6CH 20040812000462004081200046NE 2004 8 12 RAIA00407017 220040726A732031035016 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LT ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03562HK 41078 76086 LT ENGINE IEC FAULT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE P2 SENSOR. 2L72 4T4 TRTA41NM E18NE 20040812000472004081200047EU 2004 8 12 RAIA00407018 120040726A3320BR90001 BALLAST JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE CABIN OVERHEATED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE03570HK 41089 5493 - PIA - BURNING SMELL IN CABIN. MAINTENANCE FOUND BALLAST AT 8BC VERY HOT, DEACTIVATED AND DEFERRED CEILING LIGHTS AT 6BC-8BC. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING BALLAST. 2L72 4T4 TRTA41NM E18NE 20040812000542004081200054EU 2004 8 12 2004UALA00699 120040727A5270 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY EXIT ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29445UA 826 RT EMERGENCY OVERWING EXIT WARNING LIGHT ILLUMINATED. RETURN TO FIELD. DEBRIS IN DOOR SEAL CAUSED LEAK. NO OTHER FINDINGS, CLEANED DOOR SEAL, REINSTALLED COVER. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040812000572004081200057NM 2004 8 12 2004UALA00703 120040729A5740 FITTING BOEING737 737322 1384676NM GE CFM56 CFM563US 13802NE ACTUATOR BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 NR 5 GROUND SPOILER OB ACTUATOR ATTACH LUG BROKEN. NR 5 GROUND SPOILER ACTUATOR WAS FOUND FRACTURED AT THE BEARING END DURING ROUTINE HMV MAINTENANCE INSPECTION. THE ACTUATOR WAS SENT TO THE SHOP FOR INITIAL EVALUATION BEFORE BEING SENT TO BOEING FOR A FULL FAILURE ANALYSIS. 2L72 4F4 FRTA16WE E2GL 20040812000592004081200059NM 2004 8 12 DHL2004755014 120040703A27821U109592 ACTUATOR BOEING727 727225 1384077NM PWA JT8 JT8D* NE NR 7 SLAT MALFUNCTIONED A DHLAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO01755DH 21857 NR 6 SLAT FAILED TO RETRACT AFTER TAKEOFF. ABNORMAL PROCEDURES COMPLIED WITH, WOULD NOT RETRACT. UPON CHECK AT ARRIVAL FOUND NR 7 SLAT AMBER LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED NR 7 SLAT ACTUATOR IAW MM 27-81-32. CHECKED OPERATION OF NR 6 CLEANED CONNECTOR, ALL CHECK OK IAW MM 27-81-00. 2L73 4F4 F A3WE E2EA 20040812000612004081200061NM 2004 8 12 AWXA200400803 120040721A3397BR963180 WIRE HARNESS BOEING737 7373S3 1384711NM SEAT ROW 19 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 DURING 8-DAY CHECK, FOUND WIRES PULLED OUT FROM EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040812000622004081200062EU 2004 8 12 MALA040478 120040630A3260 WARNING SYSTEM BAC 146 AVRO146RJ85A1500097EU MLG ACTIVATED A MALAO OTHER J WARNING INDICATION LDLANDING 1 GL15526XJ E2351 GEAR HORN KEEPS GOING ON IN DECENT AND ON APPROACH UNTIL GEAR IS DOWN. SPEED WAS 290 AND SLOW AND RED LIGHT IN GEAR HANDLE CAME ON ALSO FROM L/P 1094114. AIRCRAFT TO BE FERRIED TO REPAIR GEAR HANDLE UNSAFE LIGHT AND GEAR UNSAFE HORN DISCREPANCY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND SAFE FOR FERRY FLIGHT WITH GREEN HANDLE UNSAFE LIGHT AND HORN GOING OFF WITH GEAR SELECTED UP. AIRCRAFT TO BE FLOWN GEAR DOWN BELOW 210 KNOTS NO ICING CONDITIONS AND BELOW 20000 FT ALTITUDE. FROM L/P NR 1094114 REMOVED AND REPLACED ADAU ALL CHECKS GOOD IN FJ-85 MM CH 34. 2H74 4F RTA49EU 20040812000652004081200065EU 2004 8 12 MALA040477 120040701A29134018502 PUMP SAAB SF340 340B 7860101EU HYD SYSTEM FAILED A MALAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 GL15436XJ 340B436 AIRCRAFT LOST ALL HYDRAULIC PRESSURE ON TAXI OUT. MAINTENANCE REPLACED HYDRAULIC PUMP P/N ON OFF 40185-02 S/N ON AH-93358, S/N OFF NO71. SERVICED IAW 12-10-29. OPS CHECK GOOD. 2L72 4T RTA52EU 20040812000672004081200067NM 2004 8 12 AWXA200400805 120040621A532069372542 SUPPORT ANGLE BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND IN SUPPORT ANGLE UNDER KEELBEAM PANEL 3402 AT BS 616. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE UNDER KEEL BEAM PANEL 3402 AT BS 616; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 69-37254. 2L72 4F4 FRTA16WE E2GL 20040812000682004081200068NM 2004 8 12 AWXA200400806 120040714A5320D5347209000200 BEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN LAVATORY MOUNT HOLE ON BEAM Y765 LT, FORWARD OF FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 64 TO FR 66; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 18. 2L72 4F4 FRTA28NM E311NE 20040812000692004081200069NM 2004 8 12 AWXA200400807 120040714A5315D5347217220200 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN NUT PLATE HOLE ON FLOORBEAM Y1292 LT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 12 AND 18. 2L72 4F4 FRTA28NM E311NE 20040812000712004081200071NM 2004 8 12 AWXA200400809 120040714A5320D5347112420000 SHEAR PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MAINTENANCE REMOVED CORRODED SECTION OF RT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHEAR PLATE, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 8 AND 10. 2L72 4F RTA28NM 20040812000772004081200077WP 2004 8 12 DHL2004805006 120040627A3260 WARNING LIGHT DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE MLG FALSE INDICATIONA DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01805DH 46125 DURING UPLATCH CHECK RT GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE CYCLED GEAR TWICE UPLATCH CHECKED, OK. DEFER IAW MEL32-16-1 CAT A ITEM DMI NR 17038, COMPLIED WITH S/P 32-16,MAIN LANDING GEAR UPLATCH SYS. PLACARD INSTALLED. 2L74 4F4 FRT4A25 E2GL 20040812000782004081200078SO 2004 8 12 SWIA200413605 120040726A5610 WINDOW EMB 120 EMB120 3260201SO PWA 118 PW118 NE COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW 120151 2 CRACKS APPROXIMATELY 3 INCHES IN LENGTH AT LT DIRECT VISION WINDOW AT LOWER FORWARD CORNER. ITEM FOUND AT C CHECK INSPECTION. 2L72 4T4 TRTA31SO E20NE 20040812000792004081200079CE 2004 8 12 CWQ2004F00005 120040723A2510 VAPOR BARRIER CESSNA560 560XL 2076702CE PWA 545 PW545A NE FUSELAGE CRACKED B CWQRK NONE O OTHER ININSP/MAINT 1 GL05694QS 5605194 DURING ROUTINE PHASE INSP. 1-4 HAD TO REMOVE RT IB LE FOR ANOTHER PROBLEM (REF SCR NR 156504) BEFORE REINSTALLATION OF REPAIRED LE INSPECTED AREA AND FOUND THE HEAT SHIELD/ VAPOR BARRIER PN 6621281-30 CRACKED ON LOWER ATTACH FLANGE 4 FT 2 IN LONG. A CAUSE DUE TO MFG/ASSY ISSUES. FIRST BEING HEAT SHIELD ATTACH FLANGE NOT BEING BENT ENOUGH OR TOO MUCH. WHICH PUTS SHIELD IN A BIND WHEN SANDWICHED BY LE AND WING SKIN ATTACH FLANGE. THE SECOND ISSUE BEING THAT THE WING SKIN ATTACH FLANGE EDGE IS CUT SQUARE AND NOT RADIUSED ON THE CONTACT EDGE. THE CRACK IS NOT ON THE HEAT SHIELD/VAPOR BARRIER FLANGE BEND RADIUS BUT BACK ABOUT .5000 INCH. 2L72 4F4 FRTA22CE E00059EN 20040812000802004081200080CE 2004 8 12 CWQ2004F00007 120040630A2897 WIRE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE FUEL BOOST PUMP MISINSTALLED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05336QS 5600336 WHEN COMPLYING WITH SB ON AC, THE RT WING FUEL BOOST PUMP WIRING WAS FOUND TO BE UNACCEPTABLE IAW SB OUTER JACKET, WIRE BRAID AND WIRE INSULATION CHAFED THRU, ALSO ABOUT HALF OF WIRE WAS ALSO CHAFED. THE WIRING WAS CHAFED ON A FUEL SUPPLY TUBE PN 652635548 WHICH IS ALSO BEING REPLACED DUE TO THE STATED ALLOWABLE LIMITS BEING EXCEEDED. BOTH THE PUMP AND THE TUBE WERE REPLACED THIS MAINT VISIT. THE AC WAS IN SCHEDULED MAINT WHEN THIS ISSUE WAS FOUND. 2L72 4F4 FRTA22CE E25EA 20040812000822004081200082NM 2004 8 12 HNAA0400060 120040629A534085320980105 ADAPTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE LAVATORY CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07933HA 134 FOUND LEVEL 2 CORROSION ON LAV ADAPTER MOUNTING FLANGE. 2H72 4T4 TRTA13NM E20NE 20040812000852004081200085NM 2004 8 12 DHL2004749005 120040714A2613 OVERHEAT LOOP BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE AFT BODY MALFUNCTIONED A DHLAO OTHER L NO TEST NRNOT REPORTED 1 SO01749DH 22013 LOWER AFT BODY OVERHEAT DOES NOT TEST. RESEATED AND CYCLED SYSTEM POWER ON OVERHEAT DETECTION SYSTEM BOX. REF B727 M/M 26-14-000. TESTED LOWER AFT BODY OVERHEAT, OPS CHECKS NORMAL. 2L73 4F4 FRTA3WE E2EA 20040812000862004081200086SO 2004 8 12 C2XA04SH467 120040725A531014525480003 BEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL DOOR FRAME CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2724517 145332 DURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040812000872004081200087SO 2004 8 12 C2XA04TY116 120040726A532014521725613 SILL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE FWD SERVICE DOOR SILL. MAINT. REMOVED AND REPLACED THE FWD DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL, BE REL. UPON COMPLETION OF ALL 4C WORK. 2L72 4F4 FRTT00011ATTE6CH 20040812000882004081200088SO 2004 8 12 C2XA04TY117 120040726A532014521725615 SILL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION,CORROSION WAS FOUND ON THE AFT SERVICE DOOR SILL. MAINT REMOVED AND REPLACED THE AFT DOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C WORK. 2L72 4F4 FRTT00011ATTE6CH 20040812000902004081200090WP 2004 8 12 UPS04842796 120040719A5320DWG5645332 FINGER DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE SUBFLOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 CORROSION ON/AROUND MAIN CABIN SUBFLOOR FINGER DOUBLER STA 880 TO 900 RBL60-64 FINGER DOUBLER CORRODED BEYOND LIMITS. UNDERLYING STRUCTURE OK. FABBED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, SRM 53-2-0 FIG1F, 51-1-8, 51-1-21, 51-1-20D, 51-1-11. 2L74 4F4 FRT4A25 E2GL 20040812000912004081200091NM 2004 8 12 04216408 120040803A7930 TRANSDUCER DORNERDO32 DO328300 NM OIL SYSTEM FALSE INDICATIONA VTZAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 EA27408FJ 3160 ABORTED TAKE OFF DUE TO LT ENGINE LOW OIL PRESSURE MESSAGE. REMOVED AND REPLACED OIL PRESSURE DIFFERENTIAL TRANSDUCER. 2H72 4T RTA55NM 20040812000922004081200092SO 2004 8 12 C2XA04TY118 120040726A532014524131009 THRESHOLD EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON PAX DOOR THRESHOLD. MAINT REMOVED AND REPLACED PAX DOOR FWD AND AFT SILLS IAW EMB 135/145 SRM 51-40-02.ALL WORK WAS ACCOMPLISHED AND WILL BE REL. AT THE COMPLETION OF THE 4C INSPECTION. 2L72 4F RTT00011AT 20040812000932004081200093SO 2004 8 12 C2XA04TY119 120040726A532014522226003 CAP EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL LAVATORY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RIVETS AT THE CENTER LAV TOP CAP. MAINT REMOVED AND REPLACED THE LAV TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL 4C INSPECTION. 2L72 4F4 FRTT00011ATTE6CH 20040812000942004081200094EA 2004 8 12 COMA0460430 120040727A2420 IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 1 LACK OF LUBE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01934CA 7042 FLIGHT 5829 NR 1 IDG CAUTION AND GENERATOR CAUTION. SERVICE IDG OIL TO PROPER LEVEL. 2L72 4F4 FRTA21EA E15NE 20040812000952004081200095NM 2004 8 12 P5CA0401118 120040709A2781 SWITCH BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE TE FLAPS DIRTY A P5CAK NONE N FALSE WARNING ININSP/MAINT 1 WP23355MC 23395 AFTER START AND TAXI, LE FLAPS NR 4L WOULD NOT EXTEND FROM AMBER, ALT SYSTEM ATTEMPTED, STILL REMAINED AMBER. NR 4L LE FLAP IND GREEN UNTIL TAKEOFF POWER SETTING APPLIED, IND WENT AMBER, ALSO TAKEOFF WARNING HORN SOUNDED. INSPECTED CLEANED IND SWITCH ASSEMBLY CYCLED, LE FLAPS OPS CHECK NORMAL. FOUND CARD A-5 IN LE FLAP POSITION MODULE LOOSE, RESEAT CARD, OPS CHECKS GOOD, ALL IAW MM 27-81-01 AND 27-88-01. 2L74 4F4 FRTA20WE E23EA 20040812000962004081200096NM 2004 8 12 P5CA0401119 120040710A2781 PDU BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE LE FLAPS INOPERATIVE A P5CAD RETURN TO BLOCK S AFFECT SYSTEMS ININSP/MAINT 1 WP23355MC 23395 NR 4 LEADING EDGE (AMBER) TRANSIT LIGHT ON WITH FLAPS EXTENDED. REMOVED AND REPLACED NR 4 EDGE PDU IAW MM 27-81-01, OPS CHECK NORMAL, ALSO REPLACED PDU ELECTRICAL CONNECTOR. 2L74 4F4 FRTA20WE E23EA 20040812000972004081200097NE 2004 8 12 0401256745 220040728A7250 ENGINE BOEING747 747222B 1384904NM PWA JT9 JT9D7R4D 52054NE NR 1 FAILED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING MRTOVER TEMP PARTIAL RPM/PWR LOSS ENGINE CASE PENETRATION CLCLIMB 1 GL01645NW 23736 715257 DURING INITIAL CLIMB AT APPROXIMATELY 300 FT AGL, A LOUD BANG WAS HEARD FROM THE NR 1 ENGINE ALONG WITH LOSS OF THRUST AND RISING EGT. THE CREW PERFORMED THE COM PROCEDURE FOR AN ENGINE FAILURE AND SHUT DOWN THE NR 1 ENGINE. THE FLIGHT RETURNED TO KIX AND LANDED WITHOUT INCIDENT. INSPECTION FOUND THE ENGINE HAD FAILED WITH APPARENT ENGINE CASE PENETRATION IN THE AREA OF THE HIGH PRESSURE TURBINE. THE ENGINE WILL BE REPLACED. 2L74 4F4 FRTA20WE E3NE 20040812000982004081200098NM 2004 8 12 DHL2004745508 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT BS 1010 ABOVE STR 21L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024 T3 .063 PO NR 900732 DIM 2.5 INCHES X 2.5 INCHES AND DOUBLER FROM 2024-T3 .071 PO NR 900790 DIM 9 INCHES X 8.5 INCHES IAW 727 SRM 53-30-3 FIG 3A. REPAIR PARTS TREATED, PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 53-30-3 FIG 3A 2L73 4F4 F A3WE E2EA 20040812000992004081200099NM 2004 8 12 DHL2004745509 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS 580 ABOVE STR 27 LT. CORRECTIVE ACTION; DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 2.8750 INCH X 1.7500 INCH AND FABBED FILLER FROM 2024 T3 .040 PO NR 900130 DIM 2.8750 INCH X 1 INCH AND DOUBLER FROM 20424 T3 .063 PO NR 9001061 DIM 28.2500 INCHES X 9.2500 INCHES IAW 727 SRM 53-30-3 FIG 3. PARTS TREATED, PRIMED IAW 727 SRM 51-10-2, INSTALLED IAW 727 SRM 53-30-3 FIG 3. 2L73 4F4 F A3WE E2EA 20040812001002004081200100NE 2004 8 12 ASMF200407033 220040729A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RIGHT FOD W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23160PL367629536 49763 725418 DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED TO RT ENGINE IAW MM 72-00-00. BLADES OF 1ST HIGH TURBINE STAGE WAS DETECTED WITH DAMAGES OUT OF LIMITS. FOREIGN MATERIAL WAS DETECTED ON 1ST HIGH TURBINE STAGE AND RT ENGINE WAS REPLACED IAW MM 71-00-02 AND TESTED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040812001022004081200102WP 2004 8 12 04FDEA02346 120040802A5320 FITTING DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 CORROSION AT THE INTERIOR OF AFT CARGO DOOR UPPER BOX AT LONGERON 27L FITTING AND SEVERAL HARDWARE, STA 1787 TO STA 1841, LONGERON 27L, LBL 101.0 TO LBL 106.0. REMOVED CORROSION, EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL I, REMOVED AND REPLACED HEADER BEAM, REMOVED AND REINSTALLED SHROUD, TORQUE BOX WEBS, AFT TORQUE BOX, BATHTUB FITTING, ATTACH ANGLES, TEE FITTING, STUB FRAMES, INTERCOSTALS, END FITTING, SCUFF FITTING, STIFFNER, RACK, STOP PAD, CONTROL ARM FITTING, SEAL RETAINER, GILL LINER AND CLOSEOUT PANELS REMOVED TO FOM IAW DC10 SRM 51-31-01 VOL II, 51-33-01 VOL II, 53-00-01 AND 51-35-01 VOL II. 2L73 4F4 F A22WE E23EA 20040812001032004081200103WP 2004 8 12 04FDEA02347 120040802A5714 FITTING DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 CRACKED FITTING, CENTER WING SECTION TO FUSELAGE SPLICE, STATION 1157, LEFT HAND SIDE AT LONGERON 37L, EXTERNAL FITTING. REMOVED DAMAGED FITTING IAW DC10 SRM 51-33-01 VOL II. NEW FITTING FABBED ON FEDEX CARD N00880. LOCATED AND DRILLED FITTING IAW DC10 SRM 51-33-01 VOL II. INSTALLED FITTING IAW DC10 SRM 51-33-01 VOL. II. 2L73 4F4 F A22WE E23EA 20040812001072004081200107NM 2004 8 12 TSAA0477057 120040726A7711LG80A6 TRANSMITTER BOEING737 737282C 13844AUNM NR 1 ENG EPR FAILED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13826AL 23051 ABORTED TAKE-OFF DUE TO LOW POWER INDICATION ON NR 1 ENGINE EPR. (NR 1 EPR=1.78, NR 2 EPR=2.01) RETURNED TO FREIGHT RAMP. LEAK CHECK NR 1 ENGINE PT7 SYSTEM, SYSTEM CHECKS GOOD. REPLACED NR 1 EPR. PERFORM POWER ASSURANCE CHECK IAW FORM M-215, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040812001092004081200109WP 2004 8 12 UPS04842797 120040720A53403758498U2 FITTING DOUG DC8 DC873F 302199FWP INTERCOSTAL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, INTERCOSTAL ATTACH FITTING CRACKED AT STA 1240 LONG 35R REMOVED AND REPLACED FITTING IAW SRM 51-3-2, 51-1-20D. 2L74 4F RT4A25 20040812001102004081200110WP 2004 8 12 UPS04842798 120040718A53203750257U1 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, LONGERON 31 LT SPLICE FITTING CRACKED AT STA 450. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-11, 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040812001112004081200111WP 2004 8 12 UPS04842800 120040717A5330 FINGER DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, FINGER DOUBLER CORRODED IN COCKPIT SUBFLOOR. STA.-75 AT LT CUSP REMOVED, FABRICATED, AND REPLACED CORRODED EDGE DOUBLER IAW SRM 53-3-3 FIG.6, 51-1-8, 51-1-21, AND DWG5612298. 2L74 4F4 FRT4A25 E2GL 20040812001162004081200116EA 2004 8 12 04216660 120040803A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SPOILER ILLUMINATED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27660BR 7519 SPOILER FAULT. ABORTED TAKE OFF. 2L72 4F4 FRTA21EA E15NE 20040812001172004081200117NE 2004 8 12 P5CA0401131 220040727A7320 VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE PYLON MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23505MC 21251 689169 AFTER ENGINE START NR 1 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT. ALL INSTRUMENTS INDICATED ENGINE AT IDLE POWER. CLEANED CDP LINE, NO HELP, REPLACED CIT SENSOR, ENGINE NOW RUNS HIGH EGT, FOUND PYLON VALVE AT FAULT, OPENED DMI NR 36-5-2. 2L74 4F4 FRTA20WE E23EA 20040812001202004081200120CE 2004 8 12 63383 120040726A3242 BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA HYD FLUID LOW A AMWAO OTHER J WARNING INDICATION NRNOT REPORTED 1 CE07165YV UE165 RECEIVED CALL FROM CREW ABOUT BRAKES FEELING SPONGY. CALLED PIT MAINTENANCE. BLEED LT AND RT BRAKES. SERVICED BRAKE HYDRAULIC RESERVIOR LEAK CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040812001212004081200121CE 2004 8 12 63379 120040726A2910 HYDRAULIC SYSTEM BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA BRAKE SYSTEM LOW A AMWAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 CE07165YV UE165 RECEIVED CALL FROM CAPTAIN HIS LT BRAKE WAS BLEEDING OFF. THEN CALLED MAINTENANCE IN PIT. BLEED LT BRAKE AND SERVICED HYDRAULIC BRAKE GROUND CK GOOD. LEAK CK GOOD 2L72 4T3 TRTA24CE E2NE 20040809000972004080900097NM 2004 8 9 SWAA042238 120040805A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHTS FAILED LONG TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040809001142004080900114NM 2004 8 9 DL764040664 120040716A25301105011 COFFEEMAKER BOEING767 767432ER 1385134NM AFT GALLEY SPARKS A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27843MH 29716 CREW REPORTED RIGHT AFT GALLEY COFFEEMAKER HAD SPARKS AT TOD CREW PULLED COFFEEMAKER CIRCUIT BREAKER. SPARKS STOPPED. INSPECTED WIRE HARNESS FOR RT COFFEEMAKERS. NO EVIDENCE OF ARCING OR FAILURE ON NR 3 COFFEEMAKER. ALSO FOUND A ELECTRICAL PLUG FOR NR 3 COFFEEMAKER NIS. ISOLATED NR 3 RT COFFEEMAKER SECURING C/BS. FWD NR 3 COFFEEMAKER TO MCO PLACARD PER MEL 25-20-01. 2L72 4F RTA1NM 20040809001152004080900115 2004 8 9 DL76G040665 420040717A2565101651303 BOTTLE BOEING767 767324 1385203NM L1 SLIDE DISCHARGED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO27394DL 27394 1L DOOR SLIDE BOTTLE READING 0 PSI. REMOVED AND REPLACED 1L DOOR SLIDE PER AMM 25-66-01. 2L72 4F RTA1NM 20040809001312004080900131NM 2004 8 9 DL757040729 120040805A5330146N37506 SKIN BOEING757 757232 1384965NM FUSELAGE GOUGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27665DN 25013 FUSELAGE SKIN SUFFERED GROUND DAMAGE AT STATION 1627 ABOVE STR 20L. REPAIRED IAW ERA 092009-14. 2L72 4F RTA2NM 20040809001332004080900133NM 2004 8 9 DLM88040731 120040805A3350D31BAA RELAY DOUG MD88 MD88 3023688NM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO27905DL 49536 A/C DID NOT PASS EMERGENCY POWER TEST. REPLACED BATTERY CHARGER AND TRANSFER RELAY. 2L72 4F RTA6WE 20040809001342004080900134NM 2004 8 9 DL73S040732 120040806A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27308DL 23080 FUSELAGE SKIN STR-14R LAP JOINT FS 380 REPAIR OF CRACK. INSPECTION PER SI 03-086337-12AD DISCOVERED A CRACK AT A FASTENER HOLE IN THE LOWER ROW OF THE STRINGER S-14R LAP SPLICE AT STA 380. THE DAMAGE IS REPAIRED BY ER/A 092107-14 WHICH IS PER B737-200 SRM 53-30-3 FIG 42. AD 2003-08-15 MANDATES REPAIR PER SB 737-53A1177 WHICH CALLS FOR THE SRM REPAIR. THE REPAIR CONSISTS OF EXTERNAL ALUMINUM DOUBLERS AND FILLERS INSTALLED WITH ALUMINUM RIVETS. 2L72 4F RTA16WE 20040810000032004081000003NM 2004 8 10 ASAA0410277 120040601A33506013211 BATTERY BOEING737 737210C 1384459NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 FOUND AFT STAIRS AND SERVICE DOOR EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY. (M) 2L72 4F A16WE 20040810000092004081000009NM 2004 8 10 ASAA0440104 120040413A53156546811 FLOORBEAM BOEING737 7374Q8 138447QNM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 GYR - FOUND STATION 986 FLOORBEAM UPPER CAP IS CORRODED AT CLIP NUT HOLES FROM RBL 24 TO RBL 49. REMOVED AND REPLACED UPPER CAP AT STATION 986 RBL 24 TO RBL 49. (M) 2L72 4F RTA16WE 20040810000162004081000016NM 2004 8 10 ASAA0440134 120040525A5755 SKIN BOEING737 737490 1384715NM SPOILER ASSEMBLYDENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01768AS 27082 PAE - FOUND DENT ON LOWER SURFACE OF RIGHT GROUND SPOILER 3 INCHES OUTBOARD OF INBOARD END. REPAIRED RIGHT GROUND SPOILER NR 5. (M) 2L72 4F RTA16WE 20040810000202004081000020EA 2004 8 10 A6WA200440100 120040712A3230 BUSHING CNDAIRCL600 CL6002B19 1900309EA MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31428AW 7695 FOUND LEFT MLG AFT TRUNNION BUSHING IS MIGRATED .003 INCH. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20040810000252004081000025EA 2004 8 10 A6WA200440098 120040706A5230 SKIN CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31435AW 7724 FOUND SCRATCH AND DENT ON LOWER SECTION OF CARGO DOOR 10 INCHES LONG VERTICALLY AND 2 INCHES FROM FORWARD EDGE. REPAIRED DAMAGE TO CARGO DOOR BY INSTALLING REPAIR PER BOMBARDIER REO 601R-52-31-050. (M) 2L72 4F RTA21EA 20040810000262004081000026 2004 8 10 USAASA04061 420040602A2565 LANYARD AIRBUSA319 A319112 3930323EU GIRT BAR MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19712US 1038 BOS - DURING AN INSPECTION OF THE GIRT BAR ROUTING, THE FORWARD LEFT AND RIGHT, AND THE REAR LEFT AND RIGHT, ESCAPE SLIDE SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040810000322004081000032EA 2004 8 10 A6WA200440105 120040718A3230 BUSHING CNDAIRCL600 CL6002B19 1900309EA MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31429AW 7711 AFT RIGHT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .015, WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED RIGHT MLG AFT TRUNNION BUSHING AND INSTALLING FIRST OVERSIZE BUSHING. (M) 2L72 4F RTA21EA 20040810000332004081000033EA 2004 8 10 A6WA200440099 120040712A3230 BUSHING CNDAIRCL600 CL6002B19 1900309EA MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31428AW 7695 FOUND RIGHT MLG TRUNNION BUSHING IS MIGRATING .032 INCH. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20040810000432004081000043NM 2004 8 10 ASAA0440115 120040415A5712654544555 RIB BOEING737 7374Q8 138447QNM LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01785AS 27628 GYR - FOUND LEFT WING INTERNAL RIB AT WING STATION 135.50 CRACKED FORWARD OF REAR SPAR. REPAIRED THE RIB LOEWR CHORD PER THE BOEING 737-57-1186 SERVICE BULLETIN. (M) 2L72 4F RTA16WE 20040810000532004081000053 2004 8 10 SWAA042240 420040806A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040810000772004081000077WP 2004 8 10 ABXA040215 120040604A5320991073415 CUSP WEB DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 CUSP WEB CRACKED IN TWO AREAS FS 237 TO FS 254, RIGHT BUTTLINE 45 TO RIGHT BUTTLINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01. 2L72 4F A6WE 20040810000792004081000079WP 2004 8 10 ABXA040217 120040604A533059114332 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 SKIN CRACKED ABOVE RIGHT PYLON AT RIVET, STA 1038, LONGERON 12 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-31-0. 2L72 4F A6WE 20040810000802004081000080WP 2004 8 10 ABXA040218 120040607A523059101573 SKIN DOUG DC9 DC931 3022065WP AFT CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 AFT LOWER CARGO DOOR SKIN WAS CRACKED AT THE DOOR HANDLE CUTOUT. REMOVED CRACKS, INSTALLED SCUFF PLATE IAW DC-9 SRM 52-05. 2L72 4F A6WE 20040810000882004081000088WP 2004 8 10 ABXA040224 120040604A5330 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 STA 1440, LONGERON 29 RIGHT REQUIRED PERMANENT REPAIR. PERMANENT REPAIR ACCOMPLISHED IAW REA D853-49148MR. 2L74 4F 4A25 20040810000902004081000090NM 2004 8 10 SCNA04008 120040611A3320 LIGHT BOEING737 737800* NM ROW 14F INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15PHHZJ 30389 FLUORESCENT LIGHT AT 14F INOPERATIVE, EMERGENCY EXIT ROW. ITEM PLACED ON MEL 33-2-1 CATEGORY C. 2L72 4F RTA16WE 20040810001022004081000102NM 2004 8 10 DLM88040669 120040719A32225920629519 AXLE DOUG MD88 MD88 3023688NM NLG DAMAGED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27903DE 53380 CREW REPORTED NOSE SCRAPPING SOUND FROM NOSE GEAR AFTER 90 DEGREE TURN ON RAMP. ON NOSE GEAR FOUND LEFT WHEEL BOTH INNER AND OUTER BEARINGS DAMAGED AND ROLLERS MISSING. LEFT AXLE REQUIRES REPLACING. 2L72 4F RTA6WE 20040810001112004081000111EA 2004 8 10 COMA0460396 120040629A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE GOUGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 GOUGE IN SKIN ON RIGHT SIDE. REPAIRED IAW CRJ SRM 51-42-05, 51-25-00 ADN 53-00-31. 2L72 4F RTA21EA 20040810001152004081000115EA 2004 8 10 SWIA200413639 120040725A27518004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07982SW58 58 7956 FLAP FAILED ON TAXI. REMOVED AND REPLACED SKEW DETECTOR IAW 27-51-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040811000042004081100004SO 2004 8 11 C2XA04TY126 120040726A531514530627001 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOORBEAM AT FRAME 25. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB SRM 61-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000062004081100006SO 2004 8 11 C2XA04CL073 120040715A3350 LIGHT EMB 145 EMB145ER 3260211SO ROW 3 INOPERATIVE A C2XAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW2713935 145022 CLE FLIGHT 3411 - THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON ROW 3 BULKHEAD WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTT00011AT 20040811000192004081100019SO 2004 8 11 C2XA04BT073 120040701A33507287124503 CONTROL PANEL EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2721144 145741 CREW REPORTED, EMERGENCY LIGHTS ILLUMINATE WHEN SIDE LIGHTS SELECTED ON FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED FLIGHT ATTENDANTS CONTROL PANEL IAW EMB145 MM 33-26-01 AND RESECURED PIN 10 ON CONNECTOR P8905 IAW EMB 145XR AMM 20-21-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20040811000232004081100023SO 2004 8 11 C2XA04IA086 120040714A2750 CONTROL SYSTEM EMB 145 EMB145LR 3260212SO TE FLAPS MALFUNCTIONED A C2XAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW2715574 145639 ON APPROACH THE CREW REPORTED THAT THE FLAPS WERE STUCK AT 22 DEGREES. THE CREW ABORTED THE APPROACH, AND LANDED AT LIT WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040811000412004081100041NE 2004 8 11 DL76G040741 220040808A7230CF680C2B8F ENGINE BOEING767 767332 1382001NM GE CF6 CF680 30025NE NR 1 FAILED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO271604R 30180 706206 DIVERSION INTO PHX, NR 1 ENGINE COMPRESSOR STALL AT CRUISE. PHX MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20040811000422004081100042 2004 8 11 DLM90040742 420040808A2397 WIRE HARNESS DOUG MD90 MD9030 3023690NM CABIN ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27911DA 53391 PAX NOTICED ARCING AND SMOKE FROM FLOOR NEAR 26C. INSPECTED AREA COULD NOT FIND DAMAGE BUT RT SIDE OF A/C AUDIO ENTERTAINMENT SYSTEM DEAD. REPLACED HARNESS AT ROWS 25-26 FOR ARCING DAMAGE. 2L72 4F RTA6WE 20040811000492004081100049NM 2004 8 11 DLM88040697 120040706A531059360381 BEAM DOUG MD88 MD88 3023688NM CARGO DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27919DL 49584 CORROSION ON C3 CARGO BIN DOOR JAMB BEAM FOUND DURING MTC VISIT. REPLACED C3 CARGO BIN DOOR JAMB BEAM PER DOUGLAS DRAWING 5936038. 2L72 4F RTA6WE 20040811000552004081100055EA 2004 8 11 VNAA0407005 120040720A2612 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE FAILED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07202PS 7858 THE CREW REPORTED THAT THE LEFT HAND ENGINE FIRE LOOP-A WAS INOP. MAINTENANCE CONTROL DEFERRED THE LEFT HAND FIRE LOOP-A WITH THE CREW PER MEL 26-11-01 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040811000692004081100069 2004 8 11 SWAA042223 420040804A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040811000862004081100086NM 2004 8 11 SWAA042211 120040803A3350311500 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. SECURED EMERGENCY EXIT LIGHT LENS PER MM. 2L72 4F RTA16WE 20040811000952004081100095NM 2004 8 11 DLM88040705 120040728A4920947F9453 APU DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE APU BAY FAILED A DALAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO27933DL 49720 P80515 APU GEN KICKED OFF INFLIGHT WITH A/C XTIE LOCKOUT RESULTING IN RT A/C BUS UNPOWERED. REPLACED GCU. 2L72 4F4 FRTA6WE E2EA 20040811001032004081100103 2004 8 11 SWIA200413590 420040715A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07187SW STALL WARNING ON MAP WILL NOT CLEAR. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N: 120-84428-505, S/N OFF: 1200034R. 2L72 4T RTA31SO 20040811001072004081100107SO 2004 8 11 SWIA200413594 120040627A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07290SW9708 9708 120317 FLAP DISAGREEMENT WHEN SELECTION FROM 45 DEGREES FLAPS TO 0 DEGREES. FOUND AT C-CHECK. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08. OPERATIONAL CHECKED GOOD. 2L72 4T RTA31SO 20040811001082004081100108EA 2004 8 11 COMA0460392 120040628A2760 COMPUTER CNDAIRCL600 CL6002B19 1900309EA MACH TRIM MALFUNCTIONED A COMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 SO01949CA 7080 FLIGHT 5546 STAB TRIM AND MACH TRIM CAUTION. RESET HSTCU, COULD NOT DUPLICATE, OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040811001102004081100110EA 2004 8 11 COMA0460398 120040629A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01978CA 7158 CARGO FLOOR SUPPORT STRUCTURE LBL 27 HAS CORROSION AROUND NUT PLATE HOLES. REPAIRED IAW CRJ SRM 51-40-11, 51-45-00, 51-42-10, 51-25-16 AND 51-41-02. 2L72 4F RTA21EA 20040811001132004081100113EA 2004 8 11 SWIA200413581 120040718A2751855D10011 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07929SW3874 3874 7703 DURING FINAL OPERATIONAL CHECK, FLAPS FAULTED AT 6 DEGREES. REMOVED, REPLACED AND RIGGED LEFT HAND FLAP BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040811001162004081100116NE 2004 8 11 ABXA040225 220040624A7230JT8D11 ENGINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE LEFT STALLED A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL23974AX115 47623 676222 LEFT ENGINE SHUT DOWN IN FLIGHT DUE TO SEVERE COMPRESSOR STALLS. ENGINE WINDMILLED APPROX 20 MINUTES. OIL PRESSURE WAS NOT NOTED. REPLACED NR 1 ENGINE IAW ABX JOBCARD 9090010. OPS CHECK GOOD ON ENGINE RUN. 2L72 4F4 F A6WE E2EA 20040811001192004081100119WP 2004 8 11 ABXA040229 120040614A5312SB09530166289 STIFFENER DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23959AX 47761 P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 12 LEFT, TOP AND BOTTOM. REPAIRED LOWER STIFFENER. REPLACED UPPER CLIP IAW DC-9 DWG J060110. 2L72 4F A6WE 20040811001272004081100127EA 2004 8 11 COMA0460405 120040702A7930601509199 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA RT ENGINE OIL MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01712CA 7244 FLIGHT 5282 RIGHT ENGINE OIL PRESSURE WARNING DURING T/O. REPLACED THE OIL PRESSURE TRANSDUCER. 2L72 4F RTA21EA 20040811001312004081100131 2004 8 11 SWIA200413660 420040805A22156225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER YAW MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07224SW1062210622 120294 WITH THE RUDDER YAW ENGAGED DURING APPROACH, THERE WERE SEVERAL MODERATE VIBRATIONS FELT ON THE RUDDER PEDALS (BOTH SIDES). REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040811001522004081100152NM 2004 8 11 SWAA042259 120040808A3350604222 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29328SW 23692 R2 & L2 DOOR EMERGENCY EXIT LIGHTS STAY ON IN ARMED POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040811001662004081100166WP 2004 8 11 MWEA040107 120040618A534039363611 SUPPORT FITTING DOUG DC9 DC982 3022082WP MLG ACTUATOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LEFT MAIN LANDING GEAR ACTUATOR SUPPORT FITTINGS CRACKED INBOARD AFT RADIUS OF VERTICAL LEG. REMOVED AND REPLACED SUPPORT FITTINGS. 2L72 4F A6WE 20040811001722004081100172NE 2004 8 11 MWEA040109 220040623A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE RIGHT OVERTEMP A MWEAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 GL31812ME 48006 725406 RIGHT ENGINE REPORTED RUNNING HOT AT IDLE, RIGHT EXHAUST GAS TEMPERATURE AT 480C WITH PACK OFF 495C WITH PACK ON. PERFORMED TAKEOFF POWER ASSURANCE CHECK, ALL PARAMETERS WITHIN LIMITS. OK FOR SERVICE. 2L72 4F4 F A6WE E9NE 20040811001732004081100173NM 2004 8 11 P5CA0401135 120040808A3610NH420021010 CLAMP BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE HI STAGE VALVE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 689185 NR 3 ENGINE HIGH STAGE VALVE WILL NOT OPEN AT ALTITUDE WITH THRUST LEVER CLOSED. REPLACED CLAMP ON HIGH STAGE VALVE, OPERATIONAL CHECK & LEAK CHECK OK PER MM 36-11-00. 2L74 4F4 F A20WE E3NE 20040811001932004081100193NM 2004 8 11 SWAA042264 120040808A3350OL3071BPEGL LAMP BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29519SW 25318 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 11 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040812000042004081200004NM 2004 8 12 UPS04442812 120040714A5320 FITTING BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, LT BS 1241 AREA EXTERNAL LONGERON FITTING NR 10 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. LT BS1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 10 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 IAW SRM 51-30-05 PAGE 13 AND MOUNT BOLT ALSO REPLACED IAW MM 20-51-01. 2L74 4F RTA20WE 20040812000072004081200007NM 2004 8 12 UPS04442815 120040713A5310A1S13010050IN DOOR FRAME BOEING747 747200 1384847NM PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, L1 DOOR AFT LOWER CORNER FRAME FOUND CRACKED. LWR CORNER FRAME REPAIRED IAW SRM 52-10-02 2L74 4F RTA20WE 20040812000092004081200009NM 2004 8 12 UPS04542789 120040717A5315 FLOORBEAM BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01412UP 23852 INSPECTION TYPE: C3, CORROSION MAIN CABIN FLOORBEAM BS 780, RBL 51, WL 208. REPAIRED FLOORBEAM IAW ER 04-3426. 2L72 4F RTA2NM 20040812000102004081200010WP 2004 8 12 UPS04842792 120040715A5553SRO85380053 ATTACH ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1750 RT SIDE. STRIPPED PAINT IAW MM51-20-00. NDT VERIFIED CRACK. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG.16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-11, 51-1-26. 2L74 4F RT4A25 20040812000122004081200012WP 2004 8 12 UPS04842794 120040719A532056453325 WEB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE SUBFLOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, CORROSION ON SUBFLOOR BETWEEN WEB AND CHANNEL, MAIN CABIN STA 857 AT FUEL DUMP TORQUE TUBE. REMOVED UPPER CHANNEL IAW SRM 51-1-21. CUT OUT DAMAGED AREA. FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM53-2-0 FIG23, DWG 5645332, 51-1-21, 51-1-8. REINSTALLED UPPER CHANNEL IAW SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20040812000132004081200013WP 2004 8 12 UPS04842795 120040722A53404758514520N FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, HFEC INSPECTION DETECTED A CRACK IN FITTING AT STA 1150, FWD SIDE AT LONGERON 33 RT. REMOVED AND REPLACED FITTING AT STA 1150, LONGERON 33 RT IAW SRM 51-3-2, 51-1-8, 51-1-21, 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040812000202004081200020WP 2004 8 12 IXXA0400071S 120040501A5730 SKIN PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CTR LE UPPER SURFACE CORRODED AT STA XFS 341.500. REPAIR WAS ACCOMPLISHED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-8 PG 17-18 AND 57-2-1 PG 11. TOOK OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 38, TR NR 57-85 NOV 22/00. FABRICATED DOUBLER AND FILLER IAW SRM 57-2-1 FIG 38 TR NR 57-85 NOV 22/00. CLEANED, TREATED AND PRIMED AREA & INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG. 38 TR NR 57-85 NOV 22/00, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-1-15. PG 1. 2L74 4F4 FRT4A25 E2GL 20040812000322004081200032NM 2004 8 12 04FDEA02299 120040730A1430 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT NR 36 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80292, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040812000382004081200038NM 2004 8 12 AWXA200400756 120040708A3260893301 PROXIMITY SENSOR AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE NLG DEFECTIVE A AWXAO OTHER J WARNING INDICATION APAPPROACH 1 WP28802AW 924 LANDING GEAR, ON FINAL APPROACH, ENROUTE, AT APPROXIMATELY 170 KTS WITH LANDING GEAR HANDLE PLACED IN DOWN POSITION GEAR DOORS APPEARED TO COME OPEN BUT LANDING GEAR DID NOT EXTEND, RECYCLED LANDING GEAR UP THEN DOWN IAW ECAM INSTRUCTIONS AND GEAR CAME DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR PROXIMITY SWITCH (37GA) IAW AMM 32-31-73-000-001, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20040812000522004081200052NE 2004 8 12 CX7A194JU0439 220040714A72615078T36P01 SEAL SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE BENT A CX7AE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL03315CE 340B343 GEE785528 LT ENG OIL PRESS CWP, ENG OIL PRESSURE FLUCTUATING AND BELOW 30PSI. APPLIED ENGINE SHUTDOWN PROCEDURE. BB AXIS SEAL WAS LEAKING. 2L72 4T4 TRTA52EU E8NE 20040812000562004081200056 2004 8 12 2004UALA00701 420040728A3442 CONTROL PANEL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE WX RADAR SYS FAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29649UA 25286 FLIGHT DIVERTED DUE TO WX RADAR FAILURE. CREW REPORTED WX RADAR INOP. DOES NOT PAINT AND GREEN ARC ON DISPLAY. ALSO, NO GROUND RETURNS. ( THE GREEN ARC IS A FLAT PLATE ANTENNA ANOMALY THAT DOES NOT AFFECT WX RADAR PERFORMANCE.) MAINTENANCE REPLACED THE WX RADAR CONTROL PANEL AND THE WX RADAR SCANNER. THERE HAVE BEEN NO RECURRING PROBLEMS INVOLVING WX RADAR PERFORMANCE. 2L72 4F4 FRTA1NM E24NE 20040812000602004081200060NM 2004 8 12 AWXA200400802 120040720A2612 WARNING LIGHT BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE CARGO DETECTORS FALSE INDICATIONA AWXAO OTHER N FALSE WARNING CRCRUISE 1 WP28182AW 22649 FALSE FIRE WARNING ON CLIMB OUT, AFTER SELECTING FLAPS UP RECEIVED FWD CARGO FIRE LIGHT AND FIRE BELL, DISCHARGED NR 1 CARGO FIRE BOTTLE AND LIGHT EXTINGUISHED, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINT MET AC AND PERFORMED A MAINT BITE TEST OF CARGO SMOKE DETECTION SYSTEM IAW TR 26-0003AW, ONLY FAULTS INDICATED WERE FOR SQUIB AND FIRE BOTTLE THAT WERE DISCHARGED. PERFORMED A CARGO COMPARTMENT SMOKE DETECTION SYS TEST IAW T/C F1B26004, AND CARGO FIRE BOTTLE SQUIB CIRCUIT TEST IAW T/C A2B26001, NO FAULTS FOUND ON EITHER TEST. REPLACED NR 1 CARGO FIRE EXTINGUISHING BOTTLE IAW T/C R2B26002, AND REPLACED FIRE SUPPRESSION DIVERTER VALVE IAW T/C R2B26001, PRESSURE AND OPS TESTS WERE GOOD. 2L72 4F4 FRTA16WE E2EA 20040812000632004081200063NM 2004 8 12 P5CA0401113 120040703A2840 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C2B6F 30025NE TRANSFER VALVE ILLUMINATED A P5CAK NONE J WARNING INDICATION ININSP/MAINT 1 WP23453PA 30811 LOWER FUEL INDICATION OF RESERVE TANK TRANSFER VALVE 2 AND 3 OPEN LIGHT ON. ITEM TRANFERED TO DMI NR 32738 IAW MEL NR 28-16-1. 2L74 4F4 FRTA20WE E13NE 20040812000642004081200064NE 2004 8 12 MALA040479 220040705A7200 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 VIBRATION A MALAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL15530XJ E2364 AFTER DEPARTING, EXPERIENCED ENG VIBRATION OF UP TO 1.9, QRH WAS FOLLOWED, POWER REDUCED, ENG VIB FEL TO .8, THEN WENT BACK TO 1.3, AND PERFORMED A PRECAUTIONARY SHUTDOWN. OIL QTY PRIOR TO START AND TAKEOFF .7500 - .5000. AFTER SHUTDOWN .2500. OIL PRESSURE 10 PSI IN FLIGHT. MAINTENANCE 1 CHECK NR 3 OIL BYPASS PIN AND CHIP DETECTORS. 1 FOUND BYPASS PIN POPPED. ALL CHIP DETECTORS FOUND TO BE CLEAN 2 CHECK NR 3 ENG OIL LEVEL 2 NR 3 ENG 3.5 QTS LOW. SERVICED ENG W/ OIL (NOTED INSIDE OF TAILPIPE AND AFT TURBINE TO BE SOAKED W/ OIL.) 3 REPLACE NR 3 ENG OIL FILTER 3 REPLACED NR 3 ENG OIL FILTER IAW AVRO AMM 79-20-01. 4 REPLACED NR 3 ENGINE 4 REPLACED NR 3 ENGINE REF WORK PACKAGE DATED 7/7/04. 2H74 4F4 FRTA49EU E6NE 20040812000722004081200072NM 2004 8 12 DHL2004745515 120040705A5330 PANEL BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT. WING IB LOWER MLG BEAM PANEL WBL114 OB SURF IS DELAMINATED SEVERAL PL. CUT OUT 2EA DELAMINATED AREAS DIM 3 INCH DIA & 4 INCH DIA FABBED FILLERS DIA 3 INCH DIA & 4 INCH DIA, DOUBLERS 2EA 6.5 INCH DIA FROM 2024 T3 .020 PO NR 900573, APPLIED ADHESIVE PRIMER, BONDED FILLERS AND DOUBLERS, CURED, SEALED AND PROMER IAW 727 SRM 51-40-20 FIG 30 REINSTALL MLG LWR PANEL WBL 114 IAW B727 SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20040812000742004081200074NM 2004 8 12 P5CA0401130 120040801A2931 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL COCKPIT ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23450PA 30808 NR EICAS STATUS MESSAGE; HYDRAULIC PRESSURE 4. TRANSFERED TO DMI NR 32889 IAW MEL NR 29-11-0. 2L74 4F4 FRTA20WE E23EA 20040812000752004081200075NM 2004 8 12 DHL2004745539 120040730A5522 SKIN BOEING727 727224 1384076NM RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT ELEVATOR UPPER SKIN DENTED BETWEEN ELEV STA 173-209. DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA 1 INCH X .7500 INCH AND FABBED DOUBLER FROM 2024-T3 .032 DIM 4 INCHES X 4 INCHES. PO NR 9001030 IAW SRM 55-20-3 FIG 5 DOUBLER TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2 & 55-20-3 FIG 5. 2L73 4F A3WE 20040812000762004081200076NM 2004 8 12 WLDA200440 120040802A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 33.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 33 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040812000832004081200083 2004 8 12 04FDEA02148 420040626A2565D31023101 SLIDE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE PAX DOOR DEPLOYED A FDEAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 SO25673FE6610 780 UNINTENTIONAL CAPTIVE. RAMP PERSON OPENED DOOR AFTER PUSHBACK. (R.FWD DOOR) SLIDE DEPLOYED, BUT FAILED TO DEPLOY. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-11-01-02 ATTN: MX; FLT SAFETY HAS REQUESTED THE SLIDE THAT FA ILED TO DEPLOY BE SENT TO MATT DUKE/FLT SAFETY EMP NR 397304 FOR INSPECTION BEFORE BEING SENT TO THE VENDO R. FACT 29JUN04 01:02 RDU R REP'D R-1 ENTRY DOOR ESCAPE SLIDEIAW MM 25-61-21-4. RII:099091 BY: 278128 RPT BY: 278128 R/I 29JUN04 01:03 RDU R R/I FROM FACT OFF MFG D31023-101, POS R1 SRL 0461, TAG 593630 ON MFG D31023-101 SRL 0391, TAG 517304. 2L72 4F4 FRTA35EU E13NE 20040812000842004081200084 2004 8 12 SCNA04011 420040713A25655A33073 SLIDE BOEING737 7378Q8 13844BXNM GE CFM56 CFM56* 13802NE R1 DOOR MALFUNCTIONED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15804SY9207 30689 R-1 DOOR SLIDE DID NOT INFLATE AUTOMATICALLY DURING OPS CHECK SUN COUNTRY TASK CARD 25-220-00-02. ESCAPE SLIDE INFLATED MANUALLY AFTER PULLING THE MANUAL INFLATION HANDLE. 2L72 4F4 FRTA16WE E2GL 20040812001062004081200106 2004 8 12 TSAA0425056 420040725A256561621469 SLIDE BOEING737 737230 1384401NM L2 DOOR DEPLOYED A TSAAH DEACTIVATE SYST/CIRCUITS W INADEQUATE Q C TXTAXI/GRND HDL 1 WP13823AL 23154 AFT PASSENGER ESCAPE SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED AFT PASSENGER ESCAPE SLIDE IAW AMM 25-61-311. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040812001082004081200108NM 2004 8 12 TSAA0452055 120040722A5210BACR13CG2AB RELAY BOEING737 73773A 1384606NM GE CFM56 CFM56* 13802NE FLT LOCK FAILED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13739AL 28500 THE LT OVER-WING EXIT LIGHT ILLUMINATED DURING TAKE-OFF AT 15 KTS. REJECTED TAKE-OFF AND RETURNED TO GATE. VERIFIED THAT THE LT OVER-WING EXIT DOOR WAS CLOSED AND LOCKED. CONFORMED WITH PSEU BITE CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. ETOPS FLIGHT 475, OAK-LIH CONTINUED: LT OVER-WING EXIT DOOR LIGHT ILLUMINATED ENROUTE. REMOVED AND REPLACED FLIGHT LOCK RELAY R742 IAW FIM 52-20-00-810-807. VERIFICATION FLIGHT CHECKS OK. AIRCRAFT OK FOR CONTINUED SERVICE. 2L72 4F4 FRTA16WE E2GL 20040812001122004081200112WP 2004 8 12 UPS04842801 120040720A5320575503289 INTERCOSTAL DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, INTERCOSTAL CRACKED IN MAIN CABIN SUBFLOOR, STA 1726, LBL 35. REMOVED, FABBED, AND REPLACED INTERCOSTAL IAW DWG 5755032, SRM 51-1-21, 51-1-8, 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20040812001142004081200114WP 2004 8 12 UPS04842805 120040720A5313 LONGERON DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, LONGERON 28L CRACKED AT FRAME INTERSECTION STA 1400, CUT OUT DAMAGED LONGERON SECTION FROM 1390 TO 1410. FABRICATED REPLACEMENT LONGERON. SECTION SRM53-2-2 FIG10 AND SRO853009 AND 53-4-1 FIG44. INSTALLED 2 SPLICE FITTINGS AND LONGERON SECTION IAW SRM 51-1-20D, 51-1-21, 51-1-8 2L74 4F4 FRT4A25 E2GL 20040812001182004081200118EA 2004 8 12 COMA0470060 120040726A3240 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE ASCU MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01354CA 10064 FLIGHT 5524 BRAKE OVERHEAT MASTER WARNING. COULD NOT DUPLICATE. RESET THE ASCU. 2L72 4F4 FRTA21EA E15NE 20040812001232004081200123NM 2004 8 12 P5CA0401132 120040731A7830 STRUCTURE BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE THRUST REVERSER DAMAGED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23921FT 21575 NR 3 THRUST REVERSER DAMAGED. PERFORMED INTEAM REPAIR IAW SRM 54-07-00. THRUST REVERSER REPAIR PLACARD ON COI NR 162. TRANSFERED TO DMI NR 32887 T/R DEACTIVATED IAW MEL 78-1-2. 2L74 4F4 F A20WE E3NE 20040812001242004081200124EU 2004 8 12 04FDEA02158 120040722A2916 RESERVOIR AIRBUS300 A300F4605R 3930327EU GE CF6 CF680 30025NE HYD SYSTEM LOW A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25686FE 804 DURING CRUISE FLIGHT AT FL 330 .80 MACH ECAM ALERTED-INDICATING LOSS OF BLUE HYD SYSTEM (HYD RSVR LO LEVEL) - ECAM SYSTEM PAGE SHOWED BLUE HYD SYSTEM RESEVIOR WAS LOW. ECAM PROCEDURE FOR HYD RSVR LO LEVEL ACCOMPLISHED. REMAINING HYD SYSTEMS NORMAL. FOUND BLUE HYD SYS PSI TRANS CRACKED. REMOVED AND REPLACED BLUE HYD SYS PSI TRANS. OPS AND LK CK OK. REF A300MM 29-32-13-4. ENT BY: 446285 RPT BY: 446285 R/I 22JUL04 11:26 MEM R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 64250-005-2, POS P1, SRL 12051, TAG 611495 ON MFG 64250-005-2 SRL 11564, TAG 609018. 2L72 4F4 FRTA35EU E13NE 20040812001252004081200125WP 2004 8 12 ASMF200408003 120040803A783041000740104 CONTROL VALVE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE THRUST REVERSER DAMAGED W ASMFO OTHER JK WARNING INDICATION FLUID LOSS CLCLIMB 1 SW231003Y129709294 48068 708437 CAPTAIN REPORTED, DURING CLIMB "LT REVERSE ACCUMULATOR" LIGHT TURNED ON AND LT HYDRAULIC QUANTITY DOWN AT 4 QUARTERS. LT REVERSE VALVE WAS CHECKED AND LEAK ON PRESSURE LINE WAS DETECTED, NIPPLE WAS TIGHTENED AND HYDRAULIC PRESSURE WAS APPLIED AND LEAK CONTINUED. WHEN VALVE WAS REMOVED, DAMAGE WAS DETECTED IN THE HOUSING VALVE. VALVE WAS REPLACED IAW MM 78-31-04, TEST CORRECT. 2L72 4F4 F A6WE E9NE 20040812001262004081200126NM 2004 8 12 DHL2004742008 120040703A3241 BRAKE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE LT MLG LOCKED A DHLAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01742DH 21290 LT BRAKE REMAINS LOCKED AFTER PARKING BRAKE RELEASED. REF. ITEM 4M L/P 003102. NR 2 BRAKE CHANGED. ALSO REPLACED NR 1 BRAKE IAW B-727 M/M 32-41-32. OPS AND LEAK CHECKS SERVICEABLE. TAXI CHECK IAW JRH 9.1. OPS SERVICEABLE. 2L73 4F4 F A3WE E2EA 20040812001272004081200127 2004 8 12 DHL2004780005 420040622A344220412323110 INDICATOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE RADAR INTERMITTENT A DHLAO OTHER O OTHER CLCLIMB 1 SO01780DH 22006 RADAR PAINTS INTERMITTENT PICTURE IN ALL MODES. REMOVED AND REPLACED RADAR DISPLAY IAW B727 M/M 34-41-01. OPS CK GOOD ON GROUND. 2L73 4F4 F A3WE E2EA 20040812001282004081200128 2004 8 12 F3LA200400072 420040723A3417PG1152BC02 ADC AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE INOPERATIVE A F3LAC ABORTED TAKEOFF G MULTIPLE FAILURE TOTAKEOFF 1 NM03906FR 358 1684 ABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FIRST OFFICER'S AIRSPEED WAS 110 KIAS. BRAKE TEMP ACHIEVED 550 DEG. TROUBLESHOT LACK OF AIRSPEED INDICATION. PERFORMED EFCS GND SCAN IAW AMM 27-96-00-740-001 AND IRU-1 GND SCAN IAW 34-13-00-740-003, INCLUDING BITE TESTS/DYNAMIC SLEW OF ADIRU-1. REPLACED ADC 19FP1 IAW AMM 34-11-17, PAGE 401. ADM LEAK CHECK GOOD. INSPECTED BRAKES IAW AMM 05-51-16-PB601. NO DEFECTS NOTED. 2L72 4F4 FRTA28NM E2GL 20040812001292004081200129NE 2004 8 12 CWQ2004F00006 220040722A7230662128132 DIFFUSER CESSNA560 560XL 2076702CE PWA 545 PW545A NE ENGINE CRACKED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05694QS 5605194 FOUND LT AND RT IB LE SKIN WHERE IT JOINS CUFF SKIN RIVETS FOUND COCKED IN HOLES WITH HEAD COCKED ABOVE SURFACE. TO REPLACE RIVETS THE LE HAD TO BE REMOVED, UPON REMOVAL, NOTICED DIFFUSER WAS CRACKED 2 PLACES AND KRINKLED IN 2 PLACES WITH A LITTLE BROWNING ON PRIMER. CRACKS WENT VERTICAL AND WERE 1.0 INCH LONG. SINCE AC WAS IN FOR AN INSP, THE PART WAS REPLACED WITH NEW. . 2L72 4F4 FRTA22CE E00059EN 20040812001312004081200131EU 2004 8 12 DHL2004362009 120040802A2613 OVERHEAT LOOP AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE LT WING INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 LT WING MANIFOLD OVERHEAT DETECT INOPERATIVE IN B-LOOP. DEFERRED IAW MEL 36-12-03. CONTROL NR 17394 ASSIGNED. SP C/W. 21864 2L72 4F4 FRTA35EU E23EA 20040812001322004081200132CE 2004 8 12 4017 120040803A32332327100 ACTUATOR LEAR 35 35A 5170602CE GARRTTTFE731TFE7312 01518WP RT MLG SLOW E BSYAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL0727BL 11844 163 P74333 GOING INTO STP RT MAIN GEAR LIGHT FAILED TO COME ON, PILOT DID A GO AROUND, CYCLED THE GEAR LIGHT CAME ON LANDED NO PROBLEM. REMOVED AND REPLACED RT GEAR ACTUATOR FOR BEING SLOW. 2L72 4F4 F A10CE E6WE 20040812001332004081200133NM 2004 8 12 DHL2004745520 120040706A5720 STIFFENER BOEING727 727224 1384076NM PWA JT8 JT8D* NE LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-PICCOLO TUBE CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT WING IB L/E INT STIFFENER IB SIDE OF WBL 92 FRAME 12 INCHES FROM FWD SPAR IS CRACKED ON TOP. REMOVED DAMAGED ANGLE AND FABBED NEW FROM 7075-T6 .040 PO NR 900920 DIM 3.1250 INCH X2 INCHES X3 INCHES X .5 INCHES IAW SRM 51-30-2, 57-20-2 FIG 1. ANGLE TREATED AND PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2. LEAK CHECK GOOD IAW MM 29-11-00, MM 30-13-0. 2L73 4F4 F A3WE E2EA 20040813000022004081300002NM 2004 8 13 DHL2004745538 120040730A5730 SKIN BOEING727 727224 1384076NM RT WING LE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT WING LE SKIN DENT 4 INCHES OB OF IB LANDING LIGHT LE STA 120. CUT OUT 2EA DAMAGED AREAS, FABBED FILLERS FROM 2024-T3 .050 PO NR 900920 DIM 1INCH X 1INCH EA, 1EA DOUBLER FROM 2024-T3 .063 PO NR 900781 DIM 7.5 INCH X 6 INCH IAW SRM 57-30-4 FIG 5 REPAIR PARTS TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED IAW SRM 57-30-4 FIG 5 2L73 4F A3WE 20040813000052004081300005WP 2004 8 13 ABXA040236 120040618A531099577395 SHEAR TIE DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 CRACKED SHEAR TIE AT FS 945 LONGERON 14 RIGHT. REPLACED SHEAR TIE ON EA 53110008-202. REPLACED SHEAR TIE ON E.A. 53110008-202. 2L72 4F4 F A6WE E2EA 20040813000072004081300007WP 2004 8 13 ABXA040238 120040618A5320591006891 TEE FITTING DOUG DC9 DC932 3022066WP PWA JT8 JT8D* NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 CRACKED AND CORRODED TEE ANGLE, AFT OF LT KIDNEY PANEL AT STA 606. REPLACED ANGLE IAW SRM 51-30-2. 2L72 4F4 F A6WE E2EA 20040813000082004081300008 2004 8 13 HAEA200400158 420040720A2210 AUTOPILOT SYS LEAR 24 24E 5170316CE COCKPIT MALFUNCTIONED E HAEAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 SW05330TW1167011670 330 AIRCRAFT PITCHES DOWN WHEN AUTOPILOT IS ENGAGED (ALT HOLD). THE FLIGHT DIRECTOR DOES THE SAME THING , EVEN WITH THE AUTOPILOT TURNED OFF. REPAIRED SHOULDER PORT DRAIN CAN SYSTEM AND REMOVED FLIGHT DIRECTOR FOR REPAIR. INSTALLED FLIGHT DIRECTOR AFTER REPAIR. OPERATIONAL CHECK GOOD. (CLOSED) 2L72 4J A10CE 20040813000092004081300009EA 2004 8 13 COMA0460421 120040717A2130 MODULE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN PRESSURE FAILED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01491CA 7756 FLIGHT 9460 CPAM FAIL MESSAGE DURING TAKEOFF. COULD NOT DUPLICATE. NO FAULTS FOUND. 2L72 4F4 FRTA21EA E15NE 20040813000102004081300010NM 2004 8 13 2004UALA00678 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FRAME AT STA 1540 DENTED ABOVE STR 25R AND 25L. INSTALLED FILLER AND REPAIR J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20040813000152004081300015NM 2004 8 13 2004UALA00683 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FRAME STATION 1440 ABOVE STR 25L IS DENTED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000222004081300022EU 2004 8 13 AWXA200400681 120040604A5320D5348004820000 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SHAPE SILL BETWEEN FR 65 AND FR 68. MAINTENANCE REMOVED L-2 DOOR SHAPE SILL FROM FR 66 TO FR 68, Y1700; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2-8. 2L72 4F RTA28NM 20040813000232004081300023EU 2004 8 13 AWXA200400682 120040602A3350BR8164002 MODULE AIRBUS320 A320231 3930325EU ZONE 900 - LAVATBROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK FOUND THE G-5 GALLEY LOWER COMPARTMENT CENTER DIVIDER WALL EMERGENCY EXIT LIGHT DAMAGED. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT G-5 GALLEY LOWER COMPARTMENT CENTER DIVIDER WALL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040813000252004081300025EU 2004 8 13 AWXA200400684 120040604A5320D5347556521000 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK CORROSION WAS FOUND IN 9 PLACES ON AFT CARGO DOOR SILL WEB BETWEEN FR 52A AND FR 54. MAINTENANCE REMOVED AFT CARGO DOOR SILL WEB FROM FR 52A TO FR 54; FABRICATED A NEW REPLACEMENT WEB SILL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2-8, 12-13, & 18. 2L72 4F RTA28NM 20040813000262004081300026EU 2004 8 13 AWXA200400685 120040605A5347D5337111000200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 LT IB SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 LT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11, FIG. 4 AND 18. 2L72 4F RTA28NM 20040813000282004081300028EU 2004 8 13 AWXA200400687 120040604A5320D53230771200 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO DOOR SILL PLATE BETWEEN FR 52A AND FR 56. MAINTENANCE REMOVED AFT CARGO DOOR SILL PLATE FROM FR 52A TO FR 56; FABRICATED A NEW REPLACEMENT SILL PLATE IAW DWG D53230771; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2-8, 12-13, AND 18. 2L72 4F RTA28NM 20040813000292004081300029NE 2004 8 13 YENA200435 220040616A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 FAILED A YENAEA ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15533JB6243 4302 1652 V11363 AT FLT 250 EXPERIENCED A POP SHUTTER, ENGINE 2 ECAM STALL, F/A CALLED UP REPORTED SMOKE IN CABIN. ENGINE REIGNITED THEN SHUTDOWN 2 OIL FILTER CLOG. THEN ENG 2 FAULT SHUTDOWN ECAM. REPLACED NR 2 ENGINE IAW WORK CARD 710020-J1-2 DUE METAL IN OIL CHIP DETECTORS. 2L72 4F4 FRTA28NM E40NE 20040813000302004081300030SO 2004 8 13 4016 220040623A7414 MAGNETO CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C505 GL LT ENGINE FAILED E BSYAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL075238J 310R0810 826067R 920868 IN ROUTE, PILOT NOTICED HI EGT AND ROUGH LT ENGINE, PILOT DID MAG CHECK RT MAGNETO DEAD, CONTINUED APPROACH, LT ENGINE QUIT, LANDED NO PROBLEM. CAUSE UNKNOWN AT THIS TIME. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20040813000312004081300031NM 2004 8 13 HNAA0407100 120040709A612078249050 PCU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE HAMSTD14SF 14SF* NE NR 2 PROPELLER FAULTY A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA07808EX266612031 299 900838 FLIGHT HAD TO SHUTDOWN THE NR 2 ENGINE DUE TO THE NR 2 PROP OVERSPEEDING THEN AUTOFEATHERING ON TAKEOFF CLIMB. IT WAS REPORTED AS THE TORQUE BEING 120 FOR 5 SECONDS AND THE PROP RPM WAS 1234 FOR 3 TO 4 SECONDS. PROP ASSEMBLY WAS REMOVED FOR AN OVERTORQUE INSPECTION. MAINTENANCE TROUBLESHOT SYSTEMS AND REMOVED AND REPLACED THE NR 2 PCU (PROPELLER CONTROL UNIT). ALL REQUIRED SYSTEM CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20040813000332004081300033NM 2004 8 13 04212452 120040730A7732 METER DORNERDO32 DO328300 NM VIBRATION SHORTED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27452FJ 3214 RT ENGINE VIBRATION INDICATION IN THE CLIMBING PHASE. RTF AND PASSENGERS DEPLANED AT THE GATE. CHECKED SHIELDED WIRES AT VIBROMETER FOR SHORTS. NO DEFECT NOTED. SUSPECT INTERMITTENT SHORT TO SHIELD AT VIVE TEST SWITCH. 2H72 4T RTA55NM 20040813000352004081300035NM 2004 8 13 ASMF200407035 120040730A7603 LEVER DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE SPRING LOCK LEVEBROKEN W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23162PL 49765 AIRCRAFT RETURNED TO PLATFORM, FUEL LEVER UNLOCKED. DURING MAINTENANCE REVISION, SPRING LOCK LEVER WAS DETECTED BROKEN. AIRCRAFT WAS SENT TO THE HANGAR AND SPRING WAS REPLACED IAW MM 76-12-00, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20040813000372004081300037NM 2004 8 13 04FDEA02339 120040801A5713 STRINGER DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING FUEL TANK ACCESS CUT-OUT 538AB, INTERIOR, UPPER STRINGER 9, STRINGER END FOUND WITH ABOUT 10 INCH LONG CRACK. REPAIR CARRIED OUT AT LEFT WING, FUEL TANK ACCESS CUT-OUT 538AB, INTERIOR, UPPER STRINGER 9, AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II AT LEFT HAND WING STRINGER NR 9. 2L73 4F4 FRTA22WE E13NE 20040813000402004081300040NM 2004 8 13 04FDEA02341 120040801A5713 STRINGER DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING, THRU FUEL TANK ACCESS PANEL CUT-OUT 636AB, UPPER STRINGER NR 11 STRINGER END FOUND WITH CRACK OF ABOUT 8 INCHES LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT WING FUEL TANK ACCESS PANEL CUT OUT NR 636AB AT STRINGER NR 11. 2L73 4F4 FRTA22WE E13NE 20040813000412004081300041NM 2004 8 13 04FDEA02342 120040801A5713 STRINGER DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING, THRU FUEL ACCESS PANEL CUT-OUT 636CB MOST FORWARD, UPPER STRINGER NR 10, STRINGER END FOUND CRACK OF ABOUT 10 INCHES LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT WING FUEL TANK ACCESS PANEL CUT OUT NR 636CB AS PER SRM 51-33-01, VOLUME II AT STRINGER NR 10. 2L73 4F4 FRTA22WE E13NE 20040813000442004081300044WP 2004 8 13 ARWA20040601 120040609A2612390D AMPLIFIER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE NR 2 FIRE LOOP MALFUNCTIONED A ARWADE RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 SO19906R 46087 DURING TAXI, NR 2 ENGINE FIRE WARNING INTERMITENTLY ILLUMINATED FIRE WARNING TEST INOPERATIVE, SHUT DOWN ENGINE; RETURNED TO RAMP. NO FIRE NOTED. CHECK FIRE WARNING SYSTEM AT RUNUP CONDITION. CHECK WIRING FOR CONDITION, ELEMENTS FOR CONDITION AT NR 2 ENGINE FIRE WARNING SYSTEM IAW MM 26-10-1. REMOVED AND REPLACED NR 2 FIRE DETECTOR AMPLIFIER IAW MM 26-10-2; FOUND SYSTEM NORMAL. CHECKED NR 2 ENGINE AT BLAST FENCE FOR FIRE WARNING SYSTEM IAW MM 71-0 AND MM 26-10-0, FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20040813000462004081300046WP 2004 8 13 ABXA040213 120040623A3260 CONNECTOR DOUG DC9 DC933F 302207AWP PWA JT8 JT8D9 52048NE MLG DIRTY A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23930AX 47363 ON INITIAL GEAR EXTENSION, RED NOSE LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION WITH NO GREEN LIGHT. RECYCLED GEAR WITH ONLY MOMENTARY FLICKER OF RED NOSE LIGHT. GREEN NOSE LIGHT EVENTUALLY ILLUMINATED AND WAS VERIFIED. ALL OTHER INDICATIONS NORMAL. INSPECTED SYSTEM IN NOSE GEAR WHEEL WELL, FOUND CORROSION P1-133 NOT SECURED, RESECURED, VERIFIED SWITCH SECURITY, CLEANED CONNECTOR AT SWITCH SW-1-9. SYSTEM WORKS WITH GOOD INDICATION ON GROUND IAW MFG AMM 32-51-00 AND 32-00. 2L72 4F4 F A6WE E2EA 20040813000502004081300050EA 2004 8 13 COMA0460441 120040804A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01821CA 7420 LT FLOOR FS 621.00 CRACKED. IAW REO 601R-53-61-117. 2L72 4F4 FRTA21EA E15NE 20040813000512004081300051NM 2004 8 13 P9RA20040026 120040731A52406556974501 GATE BOEING BOEING727 727231 1384079NM PWA JT8 JT8D9 52048NE R1 DOOR OPEN A P9RAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO115434458036 21631 UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKE OFF. FUEL DUMPED. NO EMERGENCY DECLARED. FOUND R1 DOOR PARTIALLY OPEN. PROPERLY SECURED DOOR AND GROUND PRESSURIZED THE AIRCRAFT. NO FURTHER DISCREPANCIES NOTED.NOTE. MAINTENANCE REPORTED GATE ASSEMBLY PARTIALLY OPENED. ADDITIONAL INFORMATION TO FOLLOW. 2L73 4F4 F A3WE E2EA 20040813000532004081300053NM 2004 8 13 AWXA200400810 120040714A5320D5347112420000 SHEAR PLATE AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MAINTENANCE REMOVED CORRODED SECTION OF LT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHEAR PLATE, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 8 & 10. 2L72 4F4 FRTA28NM E311NE 20040813000562004081300056SO 2004 8 13 MASA200400369 120040624A783000502710002 RESISTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07830MJ 145259 SUP/CLOSED - ASH 2681 CLT-BHM. ENG NR 1 REVERSER DISAGREE ON TAKE OFF. ABORTED TAKEOFF MX PLACED ON MEL. MAINTENANCE REPLACED RESISTOR. 2L72 4T4 FRTT00011ATTE6CH 20040813000572004081300057SO 2004 8 13 MASA200400370 120040625A7830TY204103A CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07830MJ7451 145259 CAE311323 SUP/CLOSED - ASH 2818 CAE-DCA. ENG NR 1 TR DISAGREE ON T/O, ABORTED TAKEOFF. MX PLACED ON MEL MAINTENANCE REPLACED THE ICU. 2L72 4T4 FRTT00011ATTE6CH 20040813000592004081300059NM 2004 8 13 SWAA042286 120040810A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20040813000602004081300060NM 2004 8 13 SWAA042287 120040810A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 16L CRACKED AT BS 500C+4. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040813000612004081300061NM 2004 8 13 SWAA042288 120040810A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND RT CREASE BEAM WEB CRACKED AT BS 616 TO BS 639. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040813000642004081300064NM 2004 8 13 SWAA042291 120040810A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER 4R CRACKED AT BS 500. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040813000682004081300068NM 2004 8 13 2004UALA00707 120040801A2910 HYDRAULIC SYSTEM AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE YELLOW LOW A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29810UA 843 RETURN TO FIELD WITH YELLOW HYDRAULIC SYSTEM LEVEL LOW. FOUND GREEN SYSTEM CHECK VALVE AT MANIFOLD LEAKING, REPLACED O-RING. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813000732004081300073NE 2004 8 13 2004UALA00712 220040802A7200 ENGINE BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 2 BIRD INGESTION A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29105UA 26473 ABORTED TAKEOFF AT 160 KTS DUE TO SURGE IN NR 2 ENGINE. DETERMINED SURGE DUE TO A BIRD INGESTION. ALL SURGE CHECKS PER AMM ACCOMPLISHED AND NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 FRTA20WE E24NE 20040813000742004081300074NM 2004 8 13 SWAA042295 120040810A57536546434370 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED T/E FLAP ASSY PER MM. 2L72 4F RTA16WE 20040813000762004081300076NM 2004 8 13 2004UALA00714 120040731A5751 ATTACH FITTING BOEING747 747422 1384935NM PWA 4056 PW4056 NE WING TO AILERON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29187UA 26876 FOUND APPROX 7.5 INCH VERTICAL CRACK ON THE 2ND FROM OUTBOARD FWD WING TO AILERON HINGE ATTACH FITTING SUPPORT STRUCTURE FOR RIGHT. THE NR 2 RIGHT OUTBOARD AILERON HINGE FITTING HAD BEEN REPLACED DUE TO PRIOR CRACKING. DURING REPLACEMENT A SLIGHT MIS-ALIGNMENT OF THE FITTING WITH THE AILERON INDUCED A SIDE PRELOAD. THIS SIDELOAD CAUSED A CRACK IN THE REPLACED FITTING. 2L74 4F4 FRTA20WE E24NE 20040813000782004081300078NE 2004 8 13 2004UALA00716 220040802A7200 SEAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE MISINSTALLED A UALAC ABORTED TAKEOFF WAJINADEQUATE Q C FLAME/FIRE WARNING INDICATION TOTAKEOFF 1 WP29393UA 24668 ABORTED TAKEOFF AT VERY LOW SPEED DUE TO A REPORT OF FLAMES COMING FROM THE TAILPIPE OF THE NR 2 ENGINE. FLT RETURNED TO THE GATE UNDER IT'S OWN POWER. TEARDOWN OF THE ENGINE REVEALED THAT AN HPC STAGE 6 HONEYCOMB HAD FAILED. THIS FAILURE MODE IS AN INDUSTRY KNOWN FAILURE MODE AND IT INVOLVES SHOP TECHNIQUES AND PRACTICES DUE TO THE CRITICALITY OF THE SEAL INSTALLATION. OVER THE YEARS ENGINEERING HAS REVIEWED THE INSTALLATION PROCEDURE AND HAS IMPLEMENTED BEST SHOP PRACTICES TO ENSURE PROPER INSTALLATION OF THE SEAL. 2L72 4F4 FRTA16WE E2GL 20040813000812004081300081NM 2004 8 13 2004UALA00719 120040803A3260 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 WP29350UA 24301 DIVERTED TO JFK DUE TO NOSE GEAR RED LIGHT INDICATION. PERFORMED GEAR SWING AND NOTED NOSE GEAR LOCK ACTUATOR WOULD NOT LOCK IN RETRACT POSITION WITH GEAR LEVER IN OFF POSITION. REPLACED NOSE GEAR LOCK ACTUATOR AND ACCOMPLISHED SEVERAL GEAR SWING AND MANUAL EXTENSION. NO SYSTEM FAULT NOTED. ALL INDICATIONS FOUND NORMAL. 2L72 4F4 FRTA16WE E2GL 20040813000882004081300088NM 2004 8 13 SWAA042299 120040810A335065C27093 LIGHT BOEING737 7377H4 1384404NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29789SW 29816 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 3 DEF. RELAMPED PER MM. 2L72 4F RTA16WE 20040813000892004081300089NM 2004 8 13 SWAA042300 120040810A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, FOUND 2 FUSELAGE SKIN CRACKS, BS 927, STR 23L AND BS 932, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040813000902004081300090NM 2004 8 13 SWAA042301 120040810A534065C34670 STRUCTURE BOEING737 7373H4 1384600NM HINGE BOX CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM. 2L72 4F RTA16WE 20040813000932004081300093 2004 8 13 2004UALA00724 420040101A2565 VALVE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29524UA 24977 LOW BOTTLE PRESSURE. PRESSURE RELIEF VALVE DEFECTIVE. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PRESSURE RELIEF VALVE. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. 2L72 4F4 FRTA2NM E17NE 20040813000952004081300095 2004 8 13 2004UALA00726 420040420A2565 O-RING AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE SLIDE BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29841UA 1545 LOW BOTTLE PRESSURE. SLOW LEAK DETECTED IN VALVE SHAFT THROUGH THE PLATE AND COVER HOUSING. VALVE WAS OVERHAULED AND NEW O-RINGS AND BACKUP RINGS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040813000972004081300097 2004 8 13 2004UALA00728 420040330A2565 SLIDE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FOD A UALAK NONE C F.O.D. ININSP/MAINT 1 WP29203UA 24718 SCREWDRIVER IN SLIDE PACK. CAUSE WAS PROCEDURAL (HUMAN) ERROR BY DEFUNCT SLIDE SHOP. CORRECTIVE ACTION WAS REMOVAL OF SCREWDRIVER AND OVERHAULED SLIDE. 2L72 4F4 FRTA16WE E2GL 20040813000982004081300098 2004 8 13 2004UALA00729 420040130A2565 BOTTLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29547UA 25368 LOW BOTTLE PRESSURE. CAUSE NOT FOUND. BOTTLE TOPPED OFF AND CHECKED FOR LEAKS. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. THERE WAS NO FAULT FOUND. 2L72 4F4 FRTA2NM E17NE 20040813000992004081300099 2004 8 13 2004UALA00689 420040723A3400 INDICATOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NAVIGATIONAL SYSINOPERATIVE A UALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP29808UA 804 DIVERTED DUE TO LOSS OF NAVIGATIONAL INSTRUMENTS & IFR CONDITIONS AT PLANNED DESTINATION. NAV ACCURACY LOW AND MCDU RAD/NAV PAGE UNAVAILABLE. IRU'S REALIGNED AND NAV SWITCHES ON RADIO MANAGEMENT PANEL CYCLED. INDICATIONS RETURNED TO NORMAL. FMGC BITE READOUT ACCOMPLISHED WITH NO FMGC FAULTS INDICATED. SYSTEM OPERATION HAS BEEN NORMAL TO DATE. 2L72 4F4 FRTA28NM E40NE 20040810000932004081000093WP 2004 8 10 ABXA040239 120040618A53135920319 LONGERON DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 LONGERON 29 LEFT CRACKED AT STA 579 THROUGH KIDNEY PANELS. INSTALLED NEW SECTION OF LONGERON 29 FS 579 TO 600 IAW REA D953-50039, DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20040810000952004081000095WP 2004 8 10 ABXA040232 120040625A29137927176624 LINE DOUG DC9 DC941 302207NWP HYD SYS FAILED A ABXAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL23972AX 47631 LEFT HYDRAULIC FLUID QUANTITY DECREASE BELOW RED ARC AFTER TAKEOFF ASSOCIATED WITH A DETECTABLE ODOR IN COCKPIT. REPLACED HYDRAULIC LINE TO THE LEFT BRAKE PRESSURE TRANSMITTER IAW DC9 MM. 2L72 4F A6WE 20040810001002004081000100WP 2004 8 10 ABXA040269 120040727A3340 SWITCH DOUG DC9 DC931 3022065WP TAXI LIGHT FAILED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL23944AX 47550 ON FINAL, COCKPIT SMELLED LIKE ELECTRICAL BURNING. TURNED RADAR OFF, HELPED SOMEWHAT. VERIFIED ELECTRICAL BURNING SMELL CAME FROM NOSE TAXI LIGHT SWITCH. REPLACED SWITCH IAW DC-9 WDM 33-41-01, FOR PRECAUTIONARY. CHECKED TRANSFORMER RECTIFIERS, WINDOW HEAT, FLUORESCENT LIGHT BALLAST, ANNUNCIATOR PANEL ASSEMBLY, OVERHEAD PANEL, AND E & E COMPARTMENT. NO DISCREPANCIES NOTED. NO BURNING ODOR NOTED. 2L72 4F A6WE 20040810001012004081000101EA 2004 8 10 SWIA200413656 120040801A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07937SW FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; INBOARD SIDE FS 280.0 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CLIP IAW CRJ SRM. 2L72 4F RTA21EA 20040810001052004081000105NM 2004 8 10 DL73S040673 120040720A5330654580026 SKIN BOEING737 737247 138448DNM L1 DOOR CUTOUT GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 FUSELAGE SKIN AT THE LOWER EDGE OF THE L1 DOOR CUTOUT FOUND GOUGED. REPAIR IAW ERA 091667-14. 2L72 4F A16WE 20040810001072004081000107NM 2004 8 10 DL73S040675 120040720A5330654577886 SKIN BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 FUSELAGE SKIN DAMAGED AT MULTIPLE LOCATIONS FROM STA 915 - 970, STR 18R - 23R DUE TO SERVICE DAMAGE. REPAIR IAW ERA 091443-14. 2L72 4F A16WE 20040810001102004081000110EA 2004 8 10 COMA0460425 120040724A325016900107 ECU CNDAIRCL600 CL6002B19 1900309EA NLG STEERING MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01975CA2289 1519 7150 FLIGHT 5801 NW STEERING INOP MESSAGE. REPLACED THE NWS ECU. 2L72 4F RTA21EA 20040810001162004081000116EA 2004 8 10 SWIA200413640 120040727A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07442SW2707 2707 7609 IN FLIGHT AP PITCH TRIM MSG DISPLAYED. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW 27-41-00. 2L72 4F RTA21EA 20040810001172004081000117EA 2004 8 10 SWIA200413641 120040730A3397 PIN CNDAIRCL600 CL6002C10 1390015EA LIGHT CONNECTOR LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07705SK 10145 FORWARD EMERGENCY FLOODLIGHT ON THE CEILING IS INOPERATIVE. RE-LOCKED LOOSE PIN BACK INTO PLUG P355. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040810001182004081000118SO 2004 8 10 SWIA200413642 120040724A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07234SW9952 9952 120308 ON TAXI OUT RECEIVED FLAP & ADVANCE SWS LIGHT ON MAP. REMOVED AND REPLACED FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4T RTA31SO 20040810001202004081000120SO 2004 8 10 SWIA200413644 120040726A2731 TRIM SYSTEM EMB 120 EMB120ER 3260203SO ELEVATOR OUT OF RIG A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM0757734 120199 AIRCRAFT VERY NOSE HEAVY. RE-RIGGED ELEVATOR TRIM TAB PER 27-32-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040811000012004081100001SO 2004 8 11 C2XA04TY123 120040723A532014521725001 SILL EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SILL AT FRAME 18. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB SRM 51-60-02, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000082004081100008SO 2004 8 11 C2XA04CL076 120040720A1420 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 CLE FLIGHT 3473 - THE CREW REPORTED THE RIGHT EMERGENCY EXIT LIGHT SIGN WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESEATED CONNECTOR AT THE SIGN ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20040811000092004081100009SO 2004 8 11 C2XA04TY125 120040728A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712528 145504 TYS - DURING A SCHEDULED INSPECTION THE OVERHEAD EMERGENCY LIGHT ASSEMBLE AT AISLE 9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB IAW EMB MM 33-50-08, THE OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040811000212004081100021SO 2004 8 11 C2XA04SD004 120040730A335072875566958 COVER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT CRACKED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714148 145751 SDF - DURING 1A CHECK FOUND GALLEY PHOTOLUMINESCENT LIGHT STRIP COVER CRACKED. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP COVER. AIRCRAFT WAS APPROVED AND RETURNED TO SERVICE. 2L72 4F RT 20040811000362004081100036NM 2004 8 11 DL764040736 120040806A3350 LENS BOEING767 767432ER 1385134NM MID GALLEY MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27834MH 29707 MID GALLEY BOTTOM EMERGENCY LIGHT ON RT MISSING LENS. REPLACED SAME. 2L72 4F RTA1NM 20040811000402004081100040NM 2004 8 11 DLM88040740 120040808A3510359001066 MASK DOUG MD88 MD88 3023688NM COCKPIT OXYGEN MALFUNCTIONED A DALAO OTHER L NO TEST CRCRUISE 1 SO27931DL27615 49718 CAPTS 02 MASK ALLOWS TO FLOW IN BUT NOT TO EXHALE. REPLACED MASK ASSY. 2L72 4F RTA6WE 20040811000572004081100057NM 2004 8 11 VNAA0407008 120040729A3350321430 BATTERY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL07439JS19504468 3057 THE CREW REPORTED THAT THE EMERGENCY LIGHTING WAS OUT. MAINTENANCE INSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040811000672004081100067 2004 8 11 SWAA042222 420040804A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811000712004081100071NM 2004 8 11 SWAA042225 120040804A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING OTS, FOUND FUSELAGE SKIN AT BS 530, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040811000732004081100073NM 2004 8 11 SWAA042219 120040803A533065C35772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 884, LBL 9, BS 888 RBL 9, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040811000742004081100074NM 2004 8 11 SWAA042220 120040804A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 BOTH AFT EMERGENCY FLASHLIGHTS INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040811000782004081100078 2004 8 11 SWAA042217 420040803A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM. 2L72 4F RTA16WE 20040811000902004081100090EA 2004 8 11 COMA0460427 120040719A2150 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01712CA 7244 FLIGHT 5888 RT AC PACK HIGH PRESSURE CAUTION. COULD NOT DUPLICATE. AIR CONDITION SYSTEM OPERATES NORMAL. 2L72 4F RTA21EA 20040811000962004081100096NM 2004 8 11 DL757040707 120040729A5330146N37505 SKIN BOEING757 757232 1384965NM STA STR 18L DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27664DN 25012 FUSLEAGE SKIN DENTED AND GOUGED AT STATION 1630 - 1640 BETWEEN STR 18L AND 19L. REPAIRED IAW ERA 091875-14. 2L72 4F RTA2NM 20040811001002004081100100EA 2004 8 11 COMA0460402 120040701A323046193 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA13209 7017 FLIGHT 5711 GEAR DISAGREE WARNING DURING RETRACTION. REPLACED THE MLG PRIORITY VALVE. 2L72 4F RTA21EA 20040811001062004081100106EA 2004 8 11 SWIA200413593 120040714A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MOTOR INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07943SW3309 3309 7762 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MCU IAW 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040811001142004081100114 2004 8 11 SWIA200413582 420040712A341439948E2903 INDICATOR EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07578SW816 816 120346 RUDDER SPEED SWITCH LIGHT ILLUMINATED ON MAP PANEL. REPLACED F/O'S AIRSPEED INDICATOR IAW 34-11-00 AND 34-12-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040811001332004081100133SO 2004 8 11 SWIA200413662 120040805A27513069991007 INDICATOR EMB 120 EMB120ER 3260203SO FLAP POSITION MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM0716731 120190 ON TAKEOFF ROLL AT APPROXIMATELY 90 KNOTS, EXPERIENCED A FLAP CONTROL FAULT LIGHT. PROVIDED CHAFE PROTECTION FOR ANNUNCIATOR CANNON PLUG AND REPLACED INDICATOR. OPERATIONAL CHECKS GOOD. P/N 306999-1007, S/N OFF 249. 2L72 4T RTA31SO 20040811001342004081100134EA 2004 8 11 COMA0460404 120040708A3260172825 TARGET CNDAIRCL600 CL6002B19 1900309EA LT MLG PROX SENSLOOSE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01934CA 7042 FLIGHT 5209 GEAR DISAGREE WARNING TIGHTENED LOOSE PROX SENSOR TARGET ON THE LEFT MLG UPLOCK. 2L72 4F RTA21EA 20040811001392004081100139EA 2004 8 11 SWIA200413665 120040801A2797 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA HSSCU DAMAGED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07915SW TRIM RUNAWAY ALARM AND TRIM INDICATOR ERRATIC, MACH TRIM MESSAGE. REMOVED AND REPLACED CHANNEL 1 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. REMOVED AND REPLACED CHANNEL 2 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. OPERATIONAL CHECK GOOD IAW 27-40-00 AND IAW 27-41-00. 2L72 4F RTA21EA 20040811001452004081100145WP 2004 8 11 ABXA040277 120040722A533059114015 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 EXTERIOR FUSELGAE SKIN AT STA 180, LONGERON 30 CORRODED. REPAIRED FUSELAGE SKIN AT STA 180, LONGERON 30. 2L72 4F A6WE 20040811001482004081100148 2004 8 11 SWAA042255 420040808A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811001492004081100149 2004 8 11 SWAA042256 420040808A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040811001532004081100153NM 2004 8 11 SWAA042260 120040808A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 FWD EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040811001572004081100157EA 2004 8 11 COMA0460449 120040806A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF POSITION A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA 7017 FLIGHT 5402 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DOOR HANDLE NOT CLOSED PROPERLY. OPERATED DOOR WITH NO DEFECTS. 2L72 4F RTA21EA 20040811001602004081100160NM 2004 8 11 HNAA0400063 120040707A534085320980105 ATTACH FITTING DHAV DHC8 DHC8102 2809003NM LAVATORY CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07933HA 134 LAV ADAPTER IS CORRODED. REPLACED LAV ADAPTER MOUNTING FLANGE. 2H72 4T RTA13NM 20040811001642004081100164NM 2004 8 11 MWEA040104 120040617A21339401C010101 OUTFLOW VALVE BOEING717 717200 1383700NM CABIN PRESSURE INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31918ME 5518 CABIN PRESSURE MANUAL FAIL. REMOVED AND REPLACED THE CABIN AIR OUTFLOW VALVE ACTUATOR. 2L72 4F TRA6WE 20040811001702004081100170NM 2004 8 11 513NA0009 120040730A33501317 BULB BOEING757 7572T7 1384914NM EMERGENCY LIGHT BURNED OUT A PIDAK NONE L NO TEST NRNOT REPORTED 1 SO05513NA 23895 EMERGENCY LIGHT OVER 11 DEF INOP. PLACED ON MEL 33-51-1. RELAMPED AND OPS CHECKED OK PER MM 33-50. 2L72 4F RTA2NM 20040811001762004081100176NM 2004 8 11 0401243150 120040717A2530351000 COFFEEMAKER AIRBUSA319 A319114 3930350NM GALLEY ODOR A NWAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01350NB 01819 DURING CRUISE, FLIGHT ATTENDANT REPORTED A BURN SMELL/SMOKE IN THE FRONT GALLEY. TURNED OFF GALLEY POWER AND COMMERCIAL POWER. DIVERTED TO BUF AND LANDED UNEVENTFULLY. FOUND THE COFFEEMAKER HEATING ELEMENT MELTED AND LEAKING. DEACTIVATED THE COFFEEMAKER AND APPLIED MEL PROVISIONS PENDING FURTHER TROUBLESHOOTING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040811001842004081100184 2004 8 11 MWEA040127 420040730A3418GM10242 TRANSDUCER BOEING717 717200 1383700NM COCKPIT MALFUNCTIONED A MWEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31905ME 55169 DURING FLIGHT CONTROL CHECK, CIRCUIT BREAKER POPPED AND STICK PUSHER FAIL ANNUNCIATED. REMOVED AND REPLACED FORCE TRANSDUCER. 2L72 4F TRA6WE 20040811001872004081100187NM 2004 8 11 750WL0006 120040717A3350 BULB BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST NRNOT REPORTED 1 SO05750WL 23928 TRACK LIGHT BULB INOP OPPOSITE SEAT ROW 3. RELAMPED TRACK LIGHT AT 2 ABC. OPS CHECKS OK. 2L72 4F RTA2NM 20040811001972004081100197NM 2004 8 11 SWAA042268 120040808A55516551524 FITTING BOEING737 7373Y0 1384671NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STAB FITTINGS FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20040811001982004081100198NM 2004 8 11 SWAA042271 120040808A53106546529 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 400, STR 14L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040811002042004081100204NM 2004 8 11 SWAA042276 120040808A53126969854 GUSSET BOEING737 7375H4 138449DNM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND BS 178, BULKHEAD LOWER GUSSET AFT CORNER CRACKED. REMOVED AND REPLACED GUSSET PER BAC DRAWING. 2L72 4F RTA16WE 20040811002052004081100205NM 2004 8 11 SWAA042277 120040808A5315BAC1509100146 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, RBL 8 TO LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040811002112004081100211WP 2004 8 11 MWEA040121 120040719A53119953015210 DOUBLER DOUG DC9 DC982 3022082WP AFT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 AFT ACCESSORY, CANTED FRAME 1463 HAS A 5 INCH CRACK NEAR LONGERON 9 RIGHT. FABRICATED AND INSTALLED WEB AND DOUBLER. 2L72 4F A6WE 20040812000012004081200001NM 2004 8 12 04FDEA02187 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION SEAT TRACK BS 760-840 LBL 25 WL 208 AT FASTENER HOLES. REMOVED CORROSION ON SEAT TRACK FROM BS 760-840 LBL 25 WL 208 FOUND SEAT TRACK TO BE OUT OF LIMITS. LOCATED AND DRILLED HOLES ON NEW LONGITUDAL BEAM AND INSTALLED IAW SRM 51-30-2. 2L73 4F RTA3WE 20040812000022004081200002WP 2004 8 12 P9RA20040019 120040706A3260368188117 INDICATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE MLG INOPERATIVE A P9RAO OTHER N FALSE WARNING APAPPROACH 1 SO1110801 49127 ON APPROACH IN TO RFD. RT MAIN GEAR LIGHT ASSY, INOPERATIVE. ALL GEAR INDICATIONS INOPERATIVE ON RT GEAR. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED LANDING GEAR INDICATION PANEL ASSY, ALL GEAR INDICATIONS GOOD. LANDING GEAR POSITION INDICATOR SUBSEQUENTLY REPLACED ON JULY 06 2004 BY TOL MTX. 2L72 4F4 F A6WE E2EA 20040812000172004081200017WP 2004 8 12 IXXA0400068S 120040501A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT OB WING LE OB SECTION CORRODED AT STA XFS 710.000. THIS REPAIR WAS ACCOMPLISHED IAW DWG V82-R02 AND N/R 0652. REMOVED FASTENERS IAW SRM 51-1-21 PG1. REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18. FOUND OUT OF LIMITS. REMOVED THE DAMAGED AREA AND PERFORMED NDT INSPECTION IAW NDT SPH 06-10-01-001. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES. INSTALLED REPAIR DOUBLER AND FILLER ON LT OB WING LE OB SECTION USING NEW FASTNERS IAW DWG V82-R02 AND SRM 51-1-21 PG. 1 SRM 51-1-20D PG 9. 2L74 4F4 FRT4A25 E2GL 20040812000182004081200018WP 2004 8 12 IXXA0400069S 120040501A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CENTER LE HAS REPAIR ON UPPER SURFACE, STATION XFS 304.000. THIS REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIG 38 TR NR 57-85, 51-1-21, 51-1-20D. REMOVED DOUBLER AND FABRICATED FILLER AND DOUBLER. CLEANED TREATED AND PRIMED AREA PLUS FILLER AND DOUBLER INNER FACE IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 FG. 9, INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FG. 38, TR 57-85 NOV 22100, SRM 51-1-21 PG. 1, SRM 51-1-20D PG 9. 2L74 4F4 FRT4A25 E2GL 20040812000402004081200040NM 2004 8 12 AWXA200400758 120040620A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MAJOR REPAIR, DURING C-15 CHECK A .6250 INCH CRACK WAS FOUND IN FLOORBEAM AT FASTENER HEAD IN WEB BS 705, LBL 24.5, WL 204. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM WEB AT BS 705, LBL 24.5, WL 204; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A REINFORCING DOUBLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5702-04184-ES2A. 2L72 4F RTA16WE 20040812000492004081200049NM 2004 8 12 HNAA0400071 120040729A573085711094003 PANEL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE LT WING CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07982HA 380 DURING C-CHECK INSPECTION FOUND STRESS PANELS 523 AND 623 AT WITH CORROSION IN COUNTERSINKS. REMOVED AND REPLACED PANELS. 2H72 4T4 TRTA13NM E20NE 20040812000532004081200053NM 2004 8 12 2004UALA00698 120040726A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29563UA 26665 CABIN FLOORBEAM AT FS 365 RBL 10 TO RBL 15 CORRODED. FABRICATED & INSTALLED NEW WEB AND ANGLE REPAIRS. 2L72 4F4 FRTA2NM E17NE 20040812000582004081200058NM 2004 8 12 2004UALA00704 120040717A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29394UA 24669 PREVIOUS BEAR STRAP REPAIR NEEDED TO BE REPLACED DUE TO SIDE SKIN REPLACEMENT FOR AFT CARGO. THE PREVIOUS REPAIR IS LOCATED ON THE AFT PIT DOOR CUT OUT ON THE AFT SIDE. INSTALLED QUADRUPLER. 2L72 4F4 FRTA16WE E2GL 20040812000662004081200066NM 2004 8 12 AWXA200400804 120040630A53306545427504 SKIN BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MAJOR REPAIR, DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON EXTERIOR FUSELAGE SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57. MAINTENANCE BLENDED OUT CORROSION ON SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57, MATERIAL LOSS OUT OF LIMITS; FABRICATED WASHERS AND A REPAIR STRAP; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5715-04194-RC2. 2L72 4F4 FRTA16WE E2GL 20040812000702004081200070NM 2004 8 12 AWXA200400808 120040714A5315D5347218820200 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 12 AND 18. 2L72 4F4 FRTA28NM E311NE 20040812000892004081200089EA 2004 8 12 QXEA200400569 120040726A5610NP1849036 WINDOW CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE ZONE 200 FAILED A QXEAO OTHER O OTHER CRCRUISE 1 NM09606QX7086 10023 LAX-ON FLIGHT NR 2547, AT FLIGHT LEVEL 390 WITH WINDOW HEAT ON THE LT SIDE COCKPIT WINDOW SHATTERED. THE CRACK RADIATED FROM FORWARD LOWER CORNER AND INVOLED THE OUTER LAYER. AFTER THE LT WINDOW SHATTERED THERE WAS A HEAT CAUTION MESSAGE. REMOVED AND REPLACED LT SIDE COCKIT WINDOW. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040812001042004081200104WP 2004 8 12 04FDEA02348 120040802A5340 FITTING DOUG DC10 DC10* WP GE CF6 CF6* 30020GL ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LOWER SFT WING TO CENTER BOX ATTACH SKI FITTING IS EXFOILATED. RIGHT WHEEL WELL STATION 1341 TO 1360 AT XCW 118. REMOVED ATTACHED STRUCTURE IAW DC10 SRM 51-33-01, 51-35-01 VOL II, REMOVED FITTING P/N ANB7015-2. INSTALLED NEW P/N ANB7015-2 IAW DAC DWG ANB7014, REMOVED AND REINSTALLED 2 EACH CENTER WING PANELS IAW DC10 SRM 51-31-01 VOL II, REMOVED AND REINSTALLED CROSSFEED TUBE IAW DC10 MM 28-00-01-2. REINSTALLED ATTACH STRUCTURE IAW DC10 SRM 51-33-01 AND 51- 35-01. 2L73 4F4 F A22WE E23EA 20040812001052004081200105NM 2004 8 12 TSAA0456058 120040727A56105893543130 WINDSHIELD BOEING737 737209 13844AENM COCKPIT FAILED A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13827AL 23913 NON-ETOPS FLIGHT 46, HNL-ITO: OUTER PANE OF WINDOW R1 CRACKED. RETURN TO HNL. REMOVE AND REPLACE WINDOW R1 IAW AMM 56-11-11. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20040812001192004081200119NM 2004 8 12 DHL2004745511 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS 380 BELOW STR 17L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 2 INCH X 1 INCH AND FABBED DOUBLER FROM 2024 T3 .071 PO NR 9007903 DIM 10.2500 INCHES X 9.5 INCHES IAW 727 SRM 53-30-3 FIG 3. DOUBLER TREATED, PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 53-30-3 FIG 3. 2L73 4F4 F A3WE E2EA 20040813000122004081300012NM 2004 8 13 2004UALA00680 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 AFT PIT FRAME 1420, DENTED BETWEEN STR 24L AND 25L. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000242004081300024EU 2004 8 13 AWXA200400683 120040603A5320D53231322200 SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO DOOR SILL SUPPORT BETWEEN FR 24A AND FR 28. MAINTENANCE REMOVED FORWARD CARGO DOOR SILL SUPPORT FROM FR 24A TO FR 28; FABRICATED A NEW REPLACEMENT SILL SUPPORT IAW DWG D53231322; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 12. 2L72 4F RTA28NM 20040813000392004081300039CE 2004 8 13 180041 120040625A2612 CLAMP BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA FIRE LOOP BROKEN A NSVAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27171CJ UE71 CAPT REPORTED LT T HANDLE ILLUMINATED, SECURED ENGINE, BLEW FIRE BOTTLE, T HANDLE STILL ILLUMINATED, CONDUCTED A HIGH SPEED DECENT, T HANDLE EXTINGUISHED AIRCRAFT DIVERTED. FOUND BROKEN FIRE LOOP CLAMP BELOW EXHAUST STACK, REPOSITIONED CLAMP, OPS CHECKED GOOD, REMOVED AND REPLACED BROKEN CLAMP AND FIRE BOTTLE IAW MM26-20-01 OP CHECKED GOOD. 2L72 4T3 TRTA24CE E4EA 20040813000422004081300042NM 2004 8 13 04FDEA02343 120040802A5713 STRINGER DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING, THRU FUEL TANK ACCESS PANEL CUT-OUT 536 CB, UPPER STRINGER NR 10, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES LONG. REPAIR CARRIED OUT AT LEFT HAND WING FUEL TANK ACCESS PANEL CUTOUT 536CB, UPPER STRINGER NR 10 AS PER SRM 57-20-00 FIG 10, VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10, VOL I AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II AT LT STRINGER NR 10. 2L73 4F4 FRTA22WE E13NE 20040813000472004081300047NM 2004 8 13 DHL2004745528 120040712A5313 STRINGER BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; STR 23 RT IS CORRODED AT 740 STA BULKHEAD M/R. CUTOUT SECTION OF STR 23R FROM STA 725-STA740 SIZE 15 INCHES IAW B727 SRM 51-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1496-131 SIZE 15 INCHES PO NR 3323107 AND SPLICE FROM BAC 1498-142 SIZE 14 INCHES PO NR 900878 IAW B727 SRM 53-10-3 FIG 1 TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2 INSTALLED STRINGER REPAIR IAW B727 SRM 53-10-3 FIG1 2L73 4F4 F A3WE E2EA 20040813000582004081300058NM 2004 8 13 SWAA042285 120040810A3350101114 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 R2 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20040813000632004081300063NM 2004 8 13 SWAA042290 120040810A53216545819 FLOOR PANEL BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 188 TO BS 196, LT & RT SIDES. REPAIRED FLOOR WEBS PER SRM. 2L72 4F RTA16WE 20040813000712004081300071NM 2004 8 13 2004UALA00710 120040731A3350 SQUIB BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29671UA 30026 NO LIGHT TEST ONE OR TEST TWO RIGHT SQUIB. REPLACED RIGHT OVERWING SLIDE BATTERY AND POWER SUPPLY . 2L72 4F4 FRTA1NM E24NE 20040813000912004081300091NM 2004 8 13 SWAA042302 120040810A3210M981 CIRCUIT CARD BOEING737 7373Y0 1384671NM E&E BAY FAULTY A SWAAO OTHER J WARNING INDICATION LDLANDING 1 SW29682SW 23496 RIGHT MLG UNSAFE LIGHT INDICATION. AFTER CYCLING LANDING GEARS AND USING MANUAL EXTENSION WARNING INDICATION PERSISTED. REMOVED AND REPLACED M981 CIRCUIT CARD PER MM. 2L72 4F RTA16WE 20040813001032004081300103NM 2004 8 13 2004UALA00693 120040726A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 FWD EMERGENCY LIGHT STRIP FALLS OFF OF SEAT 5E. FOUND CABLE AT THE CONNECTION OF AFT LIGHT BROKEN. CABLE SECURED. AFT LIGHT OPN OK. 2L74 4F4 FRTA20WE E24NE 20040813001042004081300104EU 2004 8 13 04FDEA02393 120040806A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25409FE 273 FLOOR SUPPORT CORRODED FWD PIT LEFT OF CTR AND AFT OF FR 38.2 (LEVEL 2). REMOVED AND REPLACED FLOOR SUPPORT (ANGLE) IAW A310/200 SRM 51-40-21. 2L72 4F RTA35EU 20040813001052004081300105 2004 8 13 2004UALA00552 420040607A2565 BOTTLE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29415UA 475 DOOR 1R ASSIST BOTTLE PRESSURE AT 1500 PSI. SERVICED DOOR BOTTLE TO 1800 PSI. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813001062004081300106NM 2004 8 13 04FDEA02390 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING OUTBOARD FLAP INBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.395 MATERIAL REMOVED = 0.002 REMAINING THICKNESS = 0.393 COMPLIED WITH FEDEX EA 1-5750-76807, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040813001072004081300107EU 2004 8 13 04FDEA02392 120040806A2550 ROLLER TRAY AIRBUS310 A310203 3930313EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25409FE 273 FWD PIT CTR ROLLER TRAY AT JUST FWD OF FR 38.1 BOTTOM SIDE IS CORRODED (LEVEL 2). REMOVED DAMAGED SECTION AND INSTALLED SPLICE SECTION IAW A310/200 SRM 53-10-15. 2L72 4F RTA35EU 20040813001082004081300108NM 2004 8 13 04FDEA02355 120040803A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO LT LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 37 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040813001092004081300109NM 2004 8 13 2004UALA00650 120040711A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 EXIT PATH LIGHT DAMAGED. REPLACED EEL. 2L74 4F4 FRTA20WE E24NE 20040813001102004081300110NM 2004 8 13 2004UALA00651 120040711A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 CABIN FLOORBEAM IS CORRODED AT STA 1640, RBL 62 TO CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND STRAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813001122004081300112NM 2004 8 13 2004UALA00653 120040711A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 CABIN FLOORBEAM CORRODED AT STA 365 RBL 42 TO RBL 49. *S/D* MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT AND ANGLE AND STRAP REPAIR ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20040813001142004081300114NM 2004 8 13 2004UALA00655 120040712A5320 INTERCOSTAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 CABIN INTERCOSTAL CORRODED AT STA 1638 TO 1640, RBL 12. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED INTERCOSTAL. 2L72 4F4 FRTA2NM E17NE 20040813001162004081300116NM 2004 8 13 2004UALA00657 120040712A7930 OIL SYSTEM BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 2 ENGINE MALFUNCTIONED A UALAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29776UA 26937 ACARS'D AIRCRAFT HAD LOST NR 2 OIL PRESSURE. NR 2 ENGINE WAS REPLACED AT LAX. TEARDOWN REVEALED THAT THE LUBRICATION & SCAVENGE OIL PUMP HAD SEIZED AS A RESULT OF METAL CHIPS JAMMING THE GEARS. CHIPS WERE FROM A KEYWASHER IN THE ANGLE GEARBOX. HOWEVER, THESE CHIPS WERE NOT FROM THE CURRENTLY INSTALLED ANGLE GEARBOX, BUT FROM ONE WHICH HAD BEEN ON-WING REPLACED BACK IN JANUARY. APPARENTLY, SOME DEBRIS FROM THE JANUARY REMOVAL WAS NOT RETRIEVED, AND EVENTUALLY MIGRATED INTO THE PUMP, RESULTING IN ITS SEIZURE. MIS CLEANUP REQUIREMENTS ARE BEING REVISED TO REQUIRE A MAIN GEARBOX SCAVENGE SCREEN CHECK FOLLOWING ANGLE GEARBOX REPLACEMENT. 2L72 4F4 FRTT0001SE E46NE 20040813001172004081300117EU 2004 8 13 2004UALA00661 120040708A5311 FRAME AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29495UA 1842 FOUND 3 DENTS AT FRAME 74 AREA, 2 DENTS WERE AT STR 32L, 1 DENT AT STR 32R. FRAME 73 SURROUNDING THE JACKING STABILIZATION POINT ON THE AFT FUSELAGE. INSTALLED SKIN DOUBLER AND FRAME DOUBLER. INSTALLED NEW SHEAR CLIPS. 2L72 4F4 FRTA28NM E40NE 20040813001192004081300119NM 2004 8 13 04FDEA02356 120040803A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO LT HAND LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 39 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040813001202004081300120NM 2004 8 13 04FDEA02357 120040803A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO LT LONGERON SPLICE AT STATION 5-113 TO 1541 LONGERON 41 CRACKED. REMOVED PER SRM 51-33-01 VOLUME II. NEW SPLICE A5A7114-553 FABRICATED PER DWG A5A7114 AND PART MARKED PER GMM 7-0-1001. FABRICATED SPLICE FX A5A7114-553 INSTALLED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040813001232004081300123 2004 8 13 SWAA042283 420040809A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040813001292004081300129EU 2004 8 13 0401053247 120040622A2132769B000001 CHECK VALVE AIRBUS320 A320212 3930322EU RT PACK BAY INOPERATIVE A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL01347NW 408 WITH NR 1 PACK ON MEL, PASSING ABOUT 15,000 FT MSL, CREW NOTED A RUMBLE IN THE AC DUCT SYSTEM. CABIN CLIMB RATE WAS ABOUT 650-700 FPM. AT FL240, CREW NOTED A STRONG RUMBLE AND VIBRATION AND INCREASE IN CABIN CLIMB RATE. THE 10,000 FT CABIN ALTITUDE WARNING SOUNDED AND THE CREW DONNED OXYGEN MASKS AND BEGAN EMERGENCY DESCENT UNTIL CABIN ALTITUDE STABILIZED BELOW 10,000 FT. CONTINUED TO DTW AND LANDED UNEVENTFULLY. REPLACED NR 2 PACK DOWNSTREAM CHECK VALVE AND SLEEVE/SEALS BETWEEN THE NR 2 PACK HEAT EXCHANGER AND ACM. BOTH PACKS LEAK AND OPERATIONAL CHECK GOOD. CLEARED NR 1 PACK MEL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20040813001302004081300130NM 2004 8 13 737DX0004 120040722A5347 SEAT TRACK BOEING737 737400 138449ANM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05737DX 24804 SEAT TRACK CORRODED FROM BS 328 TO BS 345 RBL 22. REPLACED SECTION OF SEAT TRACK INTERCOSTAL PER BOEING DRAWING 65C34624 AND SRM 53-20-01. 2L72 4F RTA16WE 20040813001312004081300131NM 2004 8 13 HNAA0408106 120040801A3320BV033001248 SOCKET DHAV DHC8 DHC8102 2809003NM CABIN LIGHT BURNED A HNAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07835EX 289 FLIGHT 3980 REPORTED A HOT ELECTRICAL SMELL IN THE CABIN WITH OVERHEAD LIGHTS ON. MAINTENANCE FOUND THE OVERHEAD LIGHT SOCKET BAD. THEN REMOVED AFFECTED BULB AND PULLED AND BANDED ASSOCIATED S1 CIRCUIT BREAKER, AND SCHEDULED TO HAVE THE SOCKET REPLACED. 2H72 4T RTA13NM 20040813001322004081300132 2004 8 13 SWAA042303 420040811A256563550101 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 FWD SERVICE DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040813001332004081300133NM 2004 8 13 SWAA042304 120040811A5310BAC1505 BEAM BOEING737 7373H4 1384600NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR BEAM CORRODED FROM BS 616 TO BS 639, STR 17R. REPAIRED BEAM PER ERO. 2L72 4F RTA16WE 20040813001342004081300134NM 2004 8 13 SWAA042305 120040811A53156545804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CHANNEL CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED CHANNEL SECTION PER SRM. 2L72 4F RTA16WE 20040813001352004081300135NM 2004 8 13 SWAA042306 120040809A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 13R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040813001372004081300137 2004 8 13 SWAA042308 420040811A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED C1 CHECK, FOUND BOTH AFT ENTRY & SERVICE DOOR EVACUATION SLIDES RELEASE CABLES MISROUTED. REROUTED CABLES PER MM. 2L72 4F RTA16WE 20040813001382004081300138NM 2004 8 13 SWAA042309 120040811A3350207330 CAP BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29412WN 29818 DURING SCHEDULED MV3 CHECK, FOUND EEPLS FWD END CAP MISSING. INSTALLED FWD EEPLS END CAP PER MM. 2L72 4F RTA16WE 20040813001392004081300139 2004 8 13 SWAA042310 420040811A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29794SW 30605 DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040813001422004081300142NM 2004 8 13 2004UALA00638 120040702A2420729825G IDG BOEING757 757222 1384956NM PWA 2037 PW2037 NE LEFT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29582UA 9792 26702 LEFT GENERATOR DRIVE LIGHT ILLUMINATED. LEFT AC INTEGRATED DRIVE GENERATOR (IDG) FAILED. REPLACED LEFT IDG. SHOP FINDINGS: HYDRAULIC MOTOR/PUMP GEAR FAILURE. 2L72 4F4 FRTA2NM E17NE 20040813001462004081300146NM 2004 8 13 2004UALA00620 120040626A5754114N4003178A SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 9 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29540UA 25252 DURING WALK AROUND, FOUND SLAT NUMBER 9 DELAMINATED AT TRAILING EDGE WEDGE. *S/D* REPLACED NUMBER 9 SLAT. DURING DISASSEMBLY OF THE SLAT WEDGE FOR REPAIR, THE SHOP FOUND THAT INADEQUATE FILM ADHESIVE (RESIN) WAS USED DURING THE PERVIOUS REPAIR WHICH LEAD TO POROSITY AND VOIDS IN THE BOND LINE BETWEEN THE UPPER SKIN AND CORE MATERIAL. IN ADDITION, HAIL DAMAGE WAS FOUND ON THE REPLACED SKIN WHICH MAY HAVE CAUSED OR ACCELERATED THE DISBOND PROCESS. 2L72 4F4 FRTA2NM E17NE 20040813001472004081300147NM 2004 8 13 2004UALA00621 120040628A2721 WARNING LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RUDDER TRIM ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29650UA 25287 RETURN TO FIELD DUE TO RUDDER TRIM PROBLEM. REPLACED RUDDER TRIM ACTUATOR. 2L72 4F4 FRTA1NM E24NE 20040813001482004081300148NM 2004 8 13 2004UALA00624 120040629A2910 LINE AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29822UA 948 RETURN TO FIELD UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM FAILURE. FOUND CUT SEAL ON HYDRAULIC LINE. REPLACED SEAL, FOUND GREEN RESERVOIR WITH THREE GALLONS OF HYD FLUID. RESET MANUAL GEAR EXTENSION. SERVICED SYSTEM TO FULL. RAN ALL HYDRAULIC PUMPS, NO LEAKS FOUND. 2L72 4F4 FRTA28NM E40NE 20040813001492004081300149NE 2004 8 13 2004UALA00625 220040629A7230 BLADE BOEING757 757222 1384956NM PWA 2037 PW2037 NE COMPRESSOR FAILED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29533UA 25073 LEFT ENGINE COMPRESSOR STALL AND SURGE WHILE IN STEADY CLIMB CONFIGURATION. SHOP TEARDOWN CONFIRMED A HPT STAGE 2 BLADE FAILURE. BLADES OF THIS PART NUMBER HAVE BEEN BEING REMOVED FROM ENGINES DURING ENGINE SHOP VISITS SINCE MAY 2003. THE REMOVAL OF THE REMAINDER OF THESE BLADES IS EXPECTED TO BE COMPLETED IN 2005. 2L72 4F4 FRTA2NM E17NE 20040813001502004081300150NM 2004 8 13 2004UALA00639 120040703A2150123CH1A SENSOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EQUIP COOLING FAILED A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29311UA 23672 RETURNED TO DEN DUE TO OVERHEATED EXHAUST COOLING FAN. THE EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED. 2L72 4F4 FRTA16WE E2GL 20040813001542004081300154NM 2004 8 13 2004UALA00644 120040706A2440 POWER UNIT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EXTERNAL POWER MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29218UA 30222 PRIM EXT POWER ACCEPT NORMALLY, BUT SEC EXT POWER WON'T ACCEPT. WHENEVER PROVIDE TO SEC EXT POWER, GROUND POWER WILL TRIP BY OVER OR UNDER VOLTAGE. SEC EXT PWR CABLE TERMINALS SHORTED BETWEEN PHASES A & B, LOCATED ON INTERNAL SIDE OF PWR RECEPTACLE. MAY HAVE BEEN FROM FOREIGN MATTER LODGED BETWEEN THE TWO TERMINALS. TERMINAL HARDWARE INSTALLATION ON STUDS OF CONTACT PINS ARE CORRECT & REFLECTS A SECURE CONDITION. SUBSEQ RPLMT OF RECEPTACLE, POWER CABLES, & RELATED HARDWARE RETURNED ACFT TO SERVICE WITH NO RESPECTIVE FAULTS. UPDATE 9/15: METALLURGICAL ANALYSIS FOUND NO FOREIGN MATERIAL AT SHORT CONTACT AREA. ONGOING INSPECTIONS HAVE FOUND LOOSE & WORN CONTACT RECEPTACLE PINS. 2L72 4F4 FRTT0001SE E46NE 20040813001572004081300157NM 2004 8 13 0401216638 120040717A5313 STRINGER BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01638US 23549 DURING H-CHECK FOUND CRACK IN STRINGER 24L AT BS 1241. REPAIRED PER EA 66-165165. 2L74 4F A20WE 20040813001582004081300158EA 2004 8 13 HNAA0400059 120040621A361082110124015 PIPE DHAV DHC8 DHC8311 1386006EA BLEED AIR CRACKED A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA07336EN 336 AFTER TAKEOFF F/A REPORTED STRONG BURNING ODOR IN CABIN, THIS HAPPENED RIGHT AFTER BLEED WAS SELECTED. MX ISOLATED ENG BLEED LEAK AT FRONT SPAR BLEED PIPE. REMOVED AND REPLACED BLEED PIPE UNDER PANELS 261JT, NT LEAK CHECK GOOD. GROUND RAN A/C, NO SMELL NOTED. 2H72 4T RTA13NM 20040813001592004081300159NE 2004 8 13 P5CA0401105 220040620A73109120M43G03 MANIFOLD BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 3 ENG FUEL LEAKING A P5CAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23505MC 21251 517365 FUEL DRAINING FROM DRAIN MAST NR 3 ENGINE PORT ON ENGINE START. REPLACED NR 3 ENGINE VBR FUEL MANIFOLD ASSY AS PER MM 75-32-00. OPS & LEAK CHECK OK AS PER MM 71-00-00 TEST NR 3. 2L74 4F4 FRTA20WE E23EA 20040813001602004081300160NM 2004 8 13 2004UALA00626 120040628A3150 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE SIX PACK ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29365UA 24534 ABORTED TAKEOFF AT 80 KNOTS DUE TO ELECTRICAL SIX PACK ALERT. COULD NOT DUPLICATE. REPLACED WORN LAMPS IN SIX PACK, CHECKS NORMAL. 2L72 4F4 FRTA16WE E2GL 20040813001632004081300163NM 2004 8 13 2004UALA00648 120040708A5310 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FLOOR SHEAR WEB FROM BS 1680 TO 1720 AFT OF DOOR 4 RIGHT IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040813001642004081300164 2004 8 13 2004UALA00649 420040708A2565 RESTRAINT BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29549UA 25397 DOOR 1R WILL NOT ARM. SURVIVAL KIT RESTRAINT STRAP WAS DISPLACED FROM ITS CORRECT POSITION AT DOOR LINER AND INTERFERRED WITH GIRT BAR. IT IS POSSIBLE STRAP CAN BE DISLODGED FROM ITS VELCRO ATTACHMENT ON DOOR LINER. CORRECT POSITION OF STRAP IS CHECKED BEFORE EVERY FLIGHT BY FLIGHT ATTENDANT. 2L72 4F4 FRTA2NM E17NE 20040813001652004081300165NM 2004 8 13 252TR0024 120040801A5313 STRINGER BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 CORROSION AT ATTACH FASTENER ON STR 25 LT AT BS 967. REPAIRED AREA PER SRM 53-10-3. 2L72 4F RTA16WE 20040813001662004081300166NM 2004 8 13 252TR0025 120040802A5320 CHANNEL BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05252TR 23001 CORROSION ON DRAIN MAST SUPPORT CHANNEL AT BS 987+8 AND STR 25LT. REPLACED SUPPORT CHANNEL PER SRM 51-10-2. 2L72 4F RTA16WE 20040813001682004081300168NM 2004 8 13 737DX0005 120040720A5320 INTERCOSTAL BOEING737 737400 138449ANM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05737DX 24804 INTERCOSTAL AT BS 336.5 RBL 34 IS CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C34625 AND SRM 51-10-2. 2L72 4F RTA16WE 20040813001692004081300169NM 2004 8 13 2004UALA00627 120040629A2130 WARNING LIGHT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN PRESSURE ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29620UA 21880 CABIN ALT WARNING & EXCESSIVE HOT AIR CAUSED DIVERSION OF FLIGHT. AT FLIGHT LEVEL 330 THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURE. THE CARGO DOOR DEPRESSOR SEAL WAS FOUND DAMAGED CAUSING A LARGE AIR LEAK. 2L72 4F4 FRTA1NM E3NE 20040813001712004081300171NM 2004 8 13 2004UALA00629 120040629A2750 DRIVE UNIT BOEING747 747422 1384935NM PWA 4056 PW4056 NE TE FLAPS INOPERATIVE A UALAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29174UA 24381 FLIGHT RETURNED TO NARITA DUE TO FLAP PROBLEM.CREW HAD EICAS MESSAGE FLAPS PRIMARY, AND RT MIDSPAN INDICATION WENT TO RED, EACH SPEED INCREASE. THE CREW SENSED NO CONTROL PROBLEMS. NRTMM REPLACED THE NR 3 RT LE SLAT DRIVE UNIT. NO FURTHER HITS HAVE BEEN REPORTED. 2L74 4F4 FRTA20WE E24NE 20040813001732004081300173NM 2004 8 13 2004UALA00631 120040701A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 FUSELAGE SKIN SPLICE STRAP BODY STATION 1400 BETWEEN STR 27L & STR 30L WAS FOUND CORRODED. FRAME AT BS 1460 AND RBL 5.6 TO LBL 14.5 WAS FOUND CORRODED. *S/D* MAJOR REPAIRS ACCOMPLISHED. J-CHANNELS INSTALLED ON THE FRAME. EXTERNAL DOUBLER INSTALLED ON SKIN SPLICE STRAP. INTERCOSTALS AND SHEAR TIES REPLACED. 2L72 4F4 FRTA2NM E17NE 20040813001762004081300176NM 2004 8 13 P5CA0401103 120040613A3040 HEATER BOEING747 747230B 1384889NM GE CF6 CF650* 30018NE WINDSHIELD ODOR A P5CAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP23509MC 21221 F/O NR 1 WINDOW LOWER RIGHT CORNER OVERHEATING AND CAUSING BURNT WIRE SMELL. TURNED OFF AND C/B PULLED. DEFERRED R-1 WINDOW HEAT PER MEL 30-11-1. 2L74 4F4 F A20WE E23EA 20040813001772004081300177NM 2004 8 13 2004UALA00634 120040701A5270 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE CARGO DOOR ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29832UA 1321 FLIGHT DIVERTED DUE TO FWD CARGO DOOR UPPER ECAM WARNING. CARGO DOOR PROXIMITY SWITCH FAILED. REPLACED CARGO DOOR PROXIMITY SWITCH . OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813001782004081300178WP 2004 8 13 MWEA040111 120040702A533059530507 SKIN DOUG DC9 DC982 3022082WP FUSELAGE OUT OF TOLERANCEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 LEFT PRIMARY STATIC PORT AREA FUSELAGE SKIN CONTOUR CHANGE IS OUT OF TOLERANCE AT STATION 579 IN BETWEEN LONGERON 25 LEFT AND 26 LEFT. FABRICATED AND INSTALLED REPAIR PARTS. 2L72 4F A6WE 20040813001812004081300181WP 2004 8 13 MWEA040117 120040706A53115912494501 ANGLE DOUG DC9 DC982 3022082WP CARGO DOORWAY OUT OF TOLERANCEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FORWARD CARGO DOOR JAMB PAN REPAIR AFT END HAS TWO FASTENERS WITH EDGE DISTANCE BELOW TOLERANCE AND GAP IS EXCESSIVE BETWEEN REPAIR PAN AND WHERE ORIGINAL PAN WAS CUT. FABRICATED AND INSTALLED 2 EACH REPAIR ANGLES. 2L72 4F A6WE 20040813001862004081300186EU 2004 8 13 2004UALA00635 120040701A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29480UA 1555 UPON CLIMBOUT, F/A'S REPORTED ODOR AND BECAME NAUSEOUS. CREW RETURNED TO FIELD. RECIRCULATION FILTERS BLOCKED. REPLACED RECIRCULATION FILTERS - NO FURTHER DISCREPANCIES REPORTED. 2L72 4F4 FRTA28NM E40NE 20040813001872004081300187NM 2004 8 13 2004UALA00636 120040630A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE SEAT 12D INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29782UA 26948 EMERGENCY LIGHTS INOP AT SEATS 3F, 12D AND 34D. REPLACED LIGHT ASSY'S. 2L72 4F4 FRTT0001SE E46NE 20040813001882004081300188NM 2004 8 13 2004UALA00637 120040701A2913NAS161212 O-RING BOEING757 757222 1384956NM PWA 2037 PW2037 NE HYD PUMP LEAKING A UALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29514UA 24839 HYDRAULIC QUANTITY DROPPED TO .47. TURNED OFF BOTH LEFT HYDRAULIC PUMPS TILL DESCENT AND LANDING. *S/D* CASE DRAIN MODULE O-RING FAILED. REPLACED O-RING. 2L72 4F4 FRTA2NM E17NE 20040813001892004081300189NM 2004 8 13 04FDEA02415 120040810A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION AT FLOORBEAM BS 950D, LBL 10 DAMAGED, WL 208 (C53-224-01, 3). BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 3. 2L73 4F RTA3WE 20040813001902004081300190NM 2004 8 13 04FDEA02416 120040810A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION ON SKIN, AFT CARGO BAY BILGE NEXT TO O/B SIDE OF STR 28L BS 994 LBL 22 WL 136. REMOVED DAMAGED AREA OF SKINA T BS 994. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F RTA3WE 20040813001912004081300191NM 2004 8 13 04FDEA02417 120040810A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION BS 1090, STR 29 LT- 29 RT. CUTOUT SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. 2L73 4F RTA3WE 20040813001922004081300192NM 2004 8 13 04FDEA02418 120040810A5313ADA3011505 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK CORROSION FOUND BETWEEN STA 6-10 AND STA 6-30 AT LONGERON 15R. CORRODED LONGERON REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. LONGERON FABRICATED AS PER DWG NR.: ADA3011. FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2L73 4F RTA22WE 20040813001952004081300195NM 2004 8 13 04FDEA02421 120040810A5313ADA3011505 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CORROSION FOUND BETWEEN STA 6-70 AND STA 6-90 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2L73 4F RTA22WE 20040813001962004081300196NM 2004 8 13 04FDEA02422 120040810A5320AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 INTERCOSTAL BETWEEN STA 1421 AND STA 1441 AT LONGERON 15L FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040813001972004081300197NM 2004 8 13 04FDEA02423 120040810A5320AEA0142509 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK - INTERCOSTAL BETWEEN STA 1175 AND STA 1199 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20040813001992004081300199NM 2004 8 13 04FDEA02401 120040809A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20040813002002004081300200NE 2004 8 13 2004UALA00670 220040718A7230 BLADE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENG COMPRESWORN A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29459UA 1192 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO NR 1 ENGINE COMPRESSOR STALL. C6 ABRADABLE SEPERATED AND ERODED THE TIPS OF THE BLADES. 2L72 4F4 FRTA28NM E40NE 20040816000012004081600001NM 2004 8 16 2004UALA00672 120040718A5310 BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA TO CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 R4 DOOR LWR SILL BEAMS CORRODED FROM STA 1640 TO 1681. MAJOR REPAIRS ACCOMPLISHED. INSTALLED NEW SILL BEAMS. 2L72 4F4 FRTA2NM E17NE 20040816000022004081600002NM 2004 8 16 2004UALA00674 120040718A335060243 LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29323UA 23955 AFT GALLEY EEL STRIP INOPERATIVE. REPLACED EEL STRIP. 2L72 4F4 FRTA16WE E2GL 20040811001552004081100155EA 2004 8 11 COMA0460447 120040804A142059465 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT CORRODED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01466CA 7627 FLIGHT 5460 EMERGENCY FLOOR PATH LIGHTS INOP AT ROWS 6 TO 8. REPLACED CORRODED CONNECTOR WIRE. 2L72 4F RTA21EA 20040811001632004081100163NM 2004 8 11 AT0400013 120040621A33508039251 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15929AT 55075 FOUND DURING SERVICE CHECK BUSINESS CLASS SEAT ROWS 1, 2 AND 3 EMERGENCY PATH LIGHTS FAILED TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY B5-118 IAW AMM 33-51-03, OPS CHECK GOOD. BLOWN FUSE INTERNAL. 2L72 4F TRA6WE 20040811001672004081100167WP 2004 8 11 MWEA040108 120040618A534039364031 SUPPORT FITTING DOUG DC9 DC982 3022082WP MLG ACTUATOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT FITTING IS CRACKED IN RADIUS ONE INCH FROM OUTBOARD INBOARD VERTICAL LEG OF AFT EDGE. REMOVED AND REPLACED SUPPORT FITTINGS. 2L72 4F A6WE 20040811001782004081100178NM 2004 8 11 0401166729 120040709A5315 FLOORBEAM BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01629US 22388 DURING L-CHECK AND ARMAR FOUND CRACK IN FLOORBEAM WEB AT BS 380 BETWEEN S12L & S13L. REPAIRED PER EA 67-165144. 2L74 4F A20WE 20040811001812004081100181NM 2004 8 11 0401045508 120040623A3350 POWER SUPPLY BOEING757 757251 1384970NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01508US 23197 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. REPLACED POWER SUPPLY M9004. OPERATIONAL CHECK GOOD. 2L72 4F RTA2NM 20040811001822004081100182WP 2004 8 11 0401039756 120040622A27805919526507 DUCT DOUG DC9 DC941 302207NWP LT WING LE DAMAGED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL01756NW 47180 DURING SLAT RETRACTION AFTER TAKEOFF, THE AIRCRAFT ROLLED TO THE LEFT ACCOMPANIED BY THE SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PROCEDURES WHICH REQUIRED THE SLATS TO BE EXTENDED AND THAT NEUTRALIZED THE UNCOMMANDED ROLLING TENDENCY. FLIGHT RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT -T- DUCT AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040811001882004081100188NM 2004 8 11 HNAA0400067 120040715A5753 SKIN DHAV DHC8 DHC8102 2809003NM TE FLAPS GOUGED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07906HA 9 DURING 20,000 HOUR INSPECTION RIGHT OUTBOARD FLAP - UPPER INBOARD SURFACE CHAFED AND GOUGED. REPAIRED PER EO 8-57-04-0476 AS A MAJOR REPAIR. DUE TO PRIOR BLENDING REPAIRS AND INABILITY TO DETERMINE REMAINING THICKNESS OF SKIN, THIS EO TRIMS OUT DAMAGE AND INSTALLS AN EXTERNAL REPAIR DOUBLER. ADDITIONALLY, THE YW 171 FLAP SHROUD FRAME IS TRIMMED OUT PER RD8-57-1549 REV A ADDRESSES DAMAGE TO STR 2 INCURRED DURING INCORPORATION OF ORIGINAL ISSUE OF THIS REPAIR. CUTOUTS ENLARGED TO ALLOW ACCESS FOR STR REWORK AND LARGER DOUBLER INSTALLED. 2H72 4T RTA13NM 20040811001912004081100191NM 2004 8 11 HNAA0400068 120040718A5270864202 SENSOR DHAV DHC8 DHC8102 2809003NM CARGO DOOR INOPERATIVE A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07942HA 163 DURING CLIMBOUT BAG BAY DOOR WARNING LIGHT ILLUMINATED. CREW INSPECTED DOOR, NO DEFECTS NOTED. CREW IS C/W APPENDIX 5 TO MEL WARNING LIGHT. REMOVED AND REPLACED FWD BAG DOOR SENSOR, OPS CHECK GOOD. 2H72 4T RTA13NM 20040811002022004081100202NM 2004 8 11 SWAA042273 120040808A53156545815 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 344, LBL 28 TO RBL 1, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040811002032004081100203NM 2004 8 11 SWAA042274 120040808A53206551698 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 908, STR 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040811002102004081100210NM 2004 8 11 SWAA042282 120040809A335065C27093 LIGHT BOEING737 7372H4 138448CNM EMERGENCY EXIT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29073SW 22673 FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040812000112004081200011WP 2004 8 12 UPS04842793 120040715A5553SRO85380053 ATTACH ANGLE DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, VERTICAL FIN TO FUSELAGE ATTACH ANGLE HAS POPPED RIVET, LT SIDE, STA 1766. REMOVED PAINT IAW SRM 51-20-00. FOUND CRACK, NDT VERIFIED. FABBED REPAIR ANGLE IAW SRM 53-2-5 FIG16A. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D, 51-1-26, 51-1-11. 2L74 4F4 FRT4A25 E2GL 20040812000142004081200014WP 2004 8 12 IXXA0400066S 120040429A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE RT WING DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND DENTS ON RT WING STATION 660. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 ALSO REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 57-2-1 FIG 24 PG 15. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-15 PG. 1. INSTALLED DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21. 2L74 4F4 FRT4A25 E2GL 20040812000192004081200019WP 2004 8 12 IXXA0400070S 120040501A5730 PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT WIND IB LE SLANT PANEL UPPER CAP CORRODED AT SEVERAL AREAS. STA XW.0 - XFS 164.000. REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 135-136. REMOVED CORRODED SLANT PANEL UPPER CAP IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW SLANT PANEL UPPER CAP IAW SRM 51-1-21 PG. 1 2L74 4F4 FRT4A25 E2GL 20040812000292004081200029NM 2004 8 12 04FDEA02297 120040730A1430 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT NR 31 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80291, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 31R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040812000412004081200041NM 2004 8 12 AWXA200400759 120040619A5330659187911 SKIN PANEL BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE KEELBEAM DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 MAJOR REPAIR, DURING C-17 CHECK FOUND 103 LOOSE RIVETS ON BOTH SIDES OF LOWER KEEL BEAM SKIN PANEL BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGED LOWER KEEL BEAM SKIN PANEL FROM BS 661.75 TO BS 727; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL; INSTALLED REPAIR PART IAW AWA E.R. 03-5310-02085-JS1. 2L72 4F4 FRTA16WE E2GL 20040812000432004081200043EU 2004 8 12 RAIA00407014 120040716A3260AIR135670 SQUAT SWITCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP MLG MALFUNCTIONED A RAIAO OTHER F FLT CONT AFFECTED LDLANDING 1 CE03557HK 41074 3657 - BWI - POWER LEVER WILL NOT GO BEHIND FLIGHT IDLE. MAINTENANCE REMOVED AND REPLACED NLG AND LT MLG WOW SWITCHES. 2L72 4T3 TRTA41NM E2WE 20040812000442004081200044EU 2004 8 12 RAIA00407015 120040725A3320BC10072002 LIGHT JETAIRJETSTMJETSTM4101 1500501EU SEAT 9BC OVERHEATED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03570HK 41089 5543 - STL - ODOR OF ELECTRICAL BURNING. MAINTENANCE FOUND BAD CEILING LIGHT FIXTURE AT SEAT 9BC, REMOVED BULB AND DEFERRED LIGHT IAW MEL. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING LIGHT FIXTURE. 2L72 4T RTA41NM 20040812000482004081200048EU 2004 8 12 RAIA00407019 120040727A2432402817 BATTERY JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP NR 1 OVERHEATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03568HK 41086 3660 - GSO - HIGH BATTERY TEMP INDICATION, NR 1 BATTERY. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY. 2L72 4T3 TRTA41NM E2WE 20040812000502004081200050CE 2004 8 12 DXTA200400325 120040617A3230651814123 CIRCUIT BOARD CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07391QS 5600493 LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF, GEAR HANDLE WOULD NOT GO OUT OF DOWN POSITION. CHECKED SQUAT SWITCH RIGGING IAW MM CHAPTER 32-61-00 NO DEFECTS FOUND. INSTALLED NEW CIRCUIT BOARD PCB103 IAW MM 24-51-01, PERFORMED NUMEROUS GEAR SWINGS AND TRIED DEPLOYMENT OF TR'S IN AIR MODE, FOUND NO DEFECTS, ALL CHECKS GOOD. 2L72 4F4 FRTA22CE E25EA 20040812000512004081200051NM 2004 8 12 QXEA200400515 120040710A2750 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA TE FLAPS ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09410QX6203 4053 FLAP POWER CAUTION LIGHT ILLUMINATED. CHECKLIST WAS RUN AND THE FLAP CONTROL CIRCUIT BREAKER WAS RESET IAW THE CHECKLIST. THE CAUTION MESSAGE CLEARED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040812000732004081200073NM 2004 8 12 P5CA0401129 120040728A3150 WARNING LIGHT BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL APU DUCT ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23496MC 29257 AFTER PUSHBACK APU DUCT LEAIL STATUS MESSAGE DISPLAYED. OPENED MEL 49-11-1-1. 2L74 4F4 FRT1384945 E23EA 20040812000812004081200081 2004 8 12 YENA200437 420040623A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE ENTERTAIN SYS MALFUNCTIONED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15503JB2400 1123 3O MINS INTO FLIGHT FA NR 1 REPORTED AN ODOR EMITTING FROM ROW 1-4, TURNED LIVE TV MASTER SWITCH TO OFF, SMELL WAS GONE AFTER 3 MIN. TV'S WERE WORKING PRIOR TO TURNING THE MASTER SWITCH OFF. COMPLIED WITH INFO NOTICE 2003-T050TR A. NO ABNORMALITIES WERE FOUND. REMOVED AND REPLACED SEB'S AT 2B & 2E FOR PRECAUTIONARY MEASURE IAW CMM 23-39-00. SYSTEM OPERATION SATISFACTORY. SEB S/N 5460 & 2017. 2L72 4F4 FRTA28NM E311NE 20040812001012004081200101WP 2004 8 12 04FDEA02345 120040802A5330 SKIN DOUG DC10 DC10* WP GE CF6 CF6* 30020GL ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO2568058 46705 LOWER FUSELAGE UNDER WING BARREL SKIN IS CORRODED FROM STATION 1368 TO 1288 FROM LONGERON 47R TO 52R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS IS .090 IAW DWG AYB7030. AFTER BLENDOUT MATERIAL IS AT .080, WITHIN LIMITS IAW DC10 SRM 51-21-01 VOL II. (OPEN) 2L73 4F4 F A22WE E23EA 20040812001132004081200113WP 2004 8 12 UPS04842804 120040722A5730 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, RT WING INTERIOR DOUBLER CORRODED AT STALL WARNING VANE, STA XFS371- 376. REMOVED CORRODED INTERNAL DOUBLERS SRM51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG5769589, AND SRM 51-1-21, & 51-1-8. 2L74 4F4 FRT4A25 E2GL 20040812001152004081200115NM 2004 8 12 SPAA0400070 120040705A33501000679 BATTERY PACK BOEING737 7372Y5 1384554NM PWA JT8 JT8D15 52051NE EMERGENCY LIGHT INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28712S 23038 R2 DOOR EMERGENCY BATTERY PACK DOES NOT OPERATE. REPLACED R2 DOOR EMERGENCY BATTERY PACK IAW BMM 33-51-101, OPERATIONAL CHECK GOOD. 2L72 4U4 FRTA16WE E2EA 20040812001302004081200130CE 2004 8 12 CWQ2004F00010 120040216A301065525024 PICCOLO TUBE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE WING BROKEN B CWQRK NONE O OTHER ININSP/MAINT 1 GL05376QS 5600276 DURING PHASE 1-4 INSP. MECH GRABBED THE TIP BLEED AIR FEED TUBE AND APPLIED PRESSURE BACK AND FORTH, A NOISE WAS HEARD BANGING AT EACH STROKE. AFTER DISASSEMBLY (REMOVAL OF LIP) FOUND THE 6552502-4, PICCOLO ASSY ATTACH LEGS (3 EA) .8750 CRACKED, ALMOST BROKEN. ALSO THE LIP NOSE CAP PN 65525051 WAS CHAFFED PAST 50 PERCENT OF MATERIAL THICKNESS. BOTH THE PICCOLO ASSY AND THE NOSE CAP (LIP) WERE REPLACED, USING SAME TYPE FASTENERS REMOVED. ATTACHED PICTURES. 2L72 4F4 FRTA22CE E25EA 20040813000032004081300003EU 2004 8 13 WRNA200400008 120040803A3260 WARNING LIGHT AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE MLG ILLUMINATED A WRNAJA DUMP FUEL UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO05821SC 211 AFTER TAKE OFF, GEAR HANDLE UP, LT GEAR DOOR AMBER AND LT GEAR UNLOCK RED LIGHT STAYED ON, ON BOTH FWD AND F/E'S PANEL. AIRPLANE START TO VIBRATE ABOVE 230 KTS. FUEL JETTISON PROCEDURE WAS ACCOMPLISHED TO MAX. LANDING WEIGHT. AIRCRAFT LANDED NORMAL. 2L72 4F4 FRTA35EU E23EA 20040813000112004081300011NM 2004 8 13 2004UALA00679 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 AFT FUSELAGE FRAME IS CORRODED AT STA 1681.8 AT STR 17R JUST AFT OF DOOR R-4 DOOR CUT OUT. INSTALLED REPAIR ANGLE FILLER AND STRAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000162004081300016NM 2004 8 13 2004UALA00684 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FRAME AT STA 1580 ABOVE STR. 25R IS DENTED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000172004081300017NM 2004 8 13 2004UALA00685 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FWD PIT STA. 640 FRAME HAS DENT BETWEEN STR 24R AND 25R. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000182004081300018NM 2004 8 13 2004UALA00686 120040723A5410 FITTING BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 PYLON GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 NR 1 PYLON AT NAC WL 160, AFT UPR DRAG FITTING IS GOUGED INSIDE BORE. OVERSIZED BORE AND INSTALLED OVERSIZE BUSHING. 2L72 4F4 FRTA2NM E17NE 20040813000192004081300019EU 2004 8 13 2004UALA00688 120040722A3210 LANDING GEAR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MAINS MALFUNCTIONED A UALAO OTHER O OTHER APAPPROACH 1 WP29459UA 1192 MANUAL GEAR EXTENSION ON APPROACH. UNABLE TO OBTAIN THREE DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. LANDING GEAR SAFETY VALVE FAILED. REPLACED THE SAFETY VALVE. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813000202004081300020EU 2004 8 13 04FDEA02337 120040801A5347 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680 30025NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25409FE 273 REF. SNRM N00381, MDC BETWEEN FR15A AND FR19 SEAT TRACK 4L HAS (LEVEL 2) CORROSION 12 INCHES FWD OF FR17. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-12-16 AND DWG A53610798 2L72 4F4 FRTA35EU E13NE 20040813000212004081300021EU 2004 8 13 AWXA200400680 120040603A5311D53112751200 FRAME AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FRAME AFT SIDE OF FR 16 AT Y1700 (FORWARD FRAME, L-1 DOORWAY). MAINTENANCE PERFORMED TEMPORARY REPAIR IAW ER 26-5320-04170-ES1 ENLARGING HOLE DIAMETER OF DAMAGED FRAME TO 15MM, PERFORMED HFEC OF REWORK, NO DAMAGE NOTED, FRAME SEGMENT WILL BE INSPECTED PRIOR TO 1500 FLIGHT CYCLES, AND REPLACED WITHIN 15 MONTHS, NOT TO EXCEED 3000 FLIGHT CYCLES. **SUPP** A REPAIR REFERENCE AND TIME REQUIREMENTS HAVE BEEN ADDED TO THIS SDR. 2L72 4F RTA28NM 20040813000452004081300045WP 2004 8 13 PNSA040702 220040709A7261 SCAVENGE PUMP SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP TURBINE SECTION LEAKING A PNSAE ENGINE SHUTDOWN J WARNING INDICATION LDLANDING 1 AL0341NE AC741B LOW OIL PRESSURE ON DESCENT. AFTER LANDING LOW OIL PRESSURE LIGHT CAME ON WITH LOW OIL PRESSURE ON GAUGE. ENGINE WAS SHUT DOWN. MAINTENANCE FOUND OIL LEVEL LOW AND SERVICED OIL. ENGINE WAS CHECKED FOR EXTERNAL AND INTERNAL LEAKS WITH NONE FOUND AND RELEASED FOR SERVICE. NEXT DAY MAINTENANCE REQUESTED PILOT TO CHECK OIL LEVEL AFTER FIRST FLIGHT AND OIL WAS FOUND LOW. AIRCRAFT WAS FERRIED BACK TO MAIN MAINTENANCE BASE AND ENGINE TURBINE SCAV PUMP WAS FOUND LEAKING INTO TURBINE SECTION. 2L72 4T3 TRTA8SW E2WE 20040813000522004081300052 2004 8 13 DHL2004364011 420040709A2565 LEVER AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE R1 DOOR SLIDE MALFUNCTIONED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 EXIT DOOR 1R ESCAPE SLIDE DISARM LEVER DOES NOT REACH FULL DISARM POSITION. DEFERRED IAW MEL 52-61-01-2 DMI NR 17140 CAT (C) PLACARD INSTALLED. 2L72 4F4 FRTA35EU E23EA 20040813000542004081300054 2004 8 13 ALGA096401 420040720A83006893672 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03417AL567 53054 CAE847532 FOUND SPALLED GEAR TEETH ON GEAR. REPLACED W/NEW PART. 1G71 3U3 UO H2SW E1GL 20040813000662004081300066NM 2004 8 13 SWAA042294 120040810A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN STRAPS CORRODED AT BS 793 AND BS 847, STR 24R. REPAIRED SKIN STRAPS PER SRM. 2L72 4F RTA16WE 20040813000672004081300067NM 2004 8 13 2004UALA00706 120040731A2930 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE HYD SYSTEM ILLUMINATED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29546UA 25367 CENTER HYDRAULIC SYSTEM EICAS QUANTITY LIGHT ILLUMINATED. QUANTITY INDICATES .40. EXCESSIVE LEAKING (CENTER SYSTEM HYDRAULIC FLUID) FROM LEFT AILERON INBOARD POWER CONTROL ACTUATOR (PCA). REMOVED AND REPLACED SUBJECT ACTUATOR WITH NEW SERVICEABLE ACTUATOR AND OPERATIONALLY CHECKED PER MM 27-11-20. ALL CHECKS NORMAL. 2L72 4F4 FRTA2NM E17NE 20040813000692004081300069EU 2004 8 13 2004UALA00708 120040801A2910 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN HYD SYS ILLUMINATED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29405UA 452 GREEN RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. LOST NOSE WHEEL STEERING. TOWED TO GATE. FOUND GREEN SYSTEM YAW DAMPER SERVO ACTUATOR LEAKING. YAW DAMPER SERVO ACTUATOR WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040813000702004081300070EU 2004 8 13 2004UALA00709 120040801A3260 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NLG ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29432UA 587 RETURN TO FIELD DUE TO NOSE GEAR NOT LOCKED INDICATION. THE SENSOR FAILED. REPLACED NLG UP LOCK ACTUATING SENSOR 12GA AND PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE NOSE LANDING GEAR. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813000772004081300077NM 2004 8 13 2004UALA00715 120040801A339758781 CABLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29351UA 24319 LAST 18 FEET OF EEL LIGHTING INOP. REPLACED FEEDER CABLE. 2L72 4F4 FRTA16WE E2GL 20040813000872004081300087NM 2004 8 13 SWAA042298 120040810A335065C27095 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29459WN 32497 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040813001222004081300122EU 2004 8 13 04FDEA02360 120040804A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25655FE 742 FWD MAIN DECK BETWEEN FR 12-13 FWD OF RT SEAT TRACK 2 AND 3 T-CAP IS CORRODED. REMOVED AND REPLACED TRACK (T-CAP) AT MAIN DECK BETWEEN FR 12-13 FWD OF SEAT TRACK NR 2 AND 3 IAW A300-600 SRM 51-40-21. 2L72 4F RTA35EU 20040813001262004081300126NE 2004 8 13 2004UALA00358 220040415A7200 NOSE COWL AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 ENGINE DAMAGED A UALAA UNSCHED LANDING CE F.O.D. VIBRATION/BUFFET CLCLIMB 1 WP29817UA 873 V10556 RETURN TO FIELD DUE TO A BIRD STRIKE TO THE NR 2 ENGINE. A BIRD STRIKE CAUSED ENGINE VIBRATION AND REDUCED POWER. REPLACED NR 2 ENGINE AND NOSE COWL. 2L72 4F4 FRTA28NM E40NE 20040813001272004081300127NM 2004 8 13 252TR0023 120040717A33506104789 BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 RIGHT WING OVERWING EMERGENCY EXIT OUTSIDE LIGHT INOP. REPLACED RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK PER MM 33-51. 2L72 4F RTA16WE 20040813001402004081300140NM 2004 8 13 SWAA042311 120040811A3350300432 LIGHT BOEING737 7373Q8 1384670NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 2. SECURED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20040813001432004081300143 2004 8 13 0401086315 420040619A3460 COMPUTER BOEING747 747451 1384940NM FLT MANAGE ODOR A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01675NW 33001 DURING CRUISE, AN ELECTRICAL BURNING ODOR EMITTED FOLLOWED BY AN AUTO THROTTLE DISCONNECT CAUTION AND EICAS MESSAGE. THE SMELL DISSIPATED AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE AUTO THROTTLE TACHOMETER AND FLIGHT MANAGEMENT COMPUTER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040813001452004081300145NM 2004 8 13 0401106308 120040621A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01668US 24223 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21C - 31C AND FROM 51C-66C. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040813001612004081300161NM 2004 8 13 2004UALA00646 120040707A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 FLOORBEAM CAP AT BS 1681 RBL 45-60 CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR ANGLE SPLICE. 2L72 4F4 FRTA2NM E17NE 20040813001672004081300167NM 2004 8 13 2004UALA00641 120040703A1420 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29525UA 24978 EEL STRIP IN FRONT OF LAV 108 INOP. SECURED LOOSE CONNECTOR. 2L72 4F4 FRTA2NM E17NE 20040813001722004081300172NM 2004 8 13 2004UALA00630 120040701A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 CABIN FLOORBEAM CORRODED BEYOND LIMITS AT BS 1640, RBL 12R-14R. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH ANGLE AND STRAP. 2L72 4F4 FRTA2NM E17NE 20040813001752004081300175NM 2004 8 13 2004UALA00633 120040701A5610 WINDSHIELD AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COCKPIT FAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29818UA 882 F/O'S WINDSHIELD SHATTERED FL370. FLIGHT DIVERTED. MOISTURE INGRESS IN THE BUSBAR AND SENSOR AREA CAUSED THE ARCING, WHICH CAUSED THE WINDOW TO SHATTER. WINDSHIELD WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20040813001792004081300179WP 2004 8 13 MWEA040112 120040702A53105912494501 DOOR FRAME DOUG DC9 DC982 3022082WP CARGO BAY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FORWARD CARGO DOOR JAMB PAN, LOWER EDGE HAS AREAS OF SEVERE CORROSION. FABRICATED AND INSTALLED REPAIR PARTS. 2L72 4F A6WE 20040813001802004081300180WP 2004 8 13 MWEA040113 120040706A533059360033 FINGER DOUBLER DOUG DC9 DC982 3022082WP FUSLEAGE OUT OF TOLERANCEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 RIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN HAS A CONTOUR CHANGE OUT OF TOLERANCE WHERE REPAIR IS INSTALLED, STATION 607 IN BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. FABRICATED AND INSTALLED FINGER DOUBLER AND FILLER. 2L72 4F A6WE 20040813001842004081300184WP 2004 8 13 0401189953 120040715A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN PRESSURE INTERMITTENT A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL01918RW 47158 FLIGHT CREW WAS NOT ABLE TO CONTROL THE PRESSURIZATION WITH AUTOMATIC CONTROL AFTER TAKEOFF, UTILIZED MANUAL CONTROL. MANUAL CONTROL FAILED AND THE OUTFLOW VALVE WENT FULL OPEN AT FL230. EMERGENCY DESCENT TO 10,000 FT AND THEN NORMAL DESCENT TO 6,000 FT. CABIN ALTITUDE REACHED A MAXIMUM ALTITUDE OF 11,000 FT DURING THE DESCENT AND THE MASKS DID NOT DEPLOY. FLIGHT RETURNED TO A NORMAL NON-EMERGENCY LANDING BACK TO DTW. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER AND THE CABIN PRESSURE RESET REGULATOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20040816000032004081600003NM 2004 8 16 2004UALA00675 120040719A55126554821 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT HORIZ STAB LEDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29394UA39586 24669 RIGHT HORIZONTAL STABILIZER DENTED ON THE FIXED LEADING EDGE TWELVE INCHES FROM INBOARD EDGE. *S/D* DURING AIRCRAFT MAINTENANCE VISIT, AN INTERIM REPAIR WAS FOUND ON THE RIGHT HORIZONTAL STABILIZER LEADING EDGE AT STA 75. THE INTERIM REPAIR WAS CHANGED TO A PERMANENT REPAIR BY INSTALLING AN INTERNAL REPAIR DOUBLER WITH PERMANENT TYPE FASTENERS. 2L72 4F4 FRTA16WE E2GL 20040816000042004081600004NM 2004 8 16 2004UALA00676 120040719A5340 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29394UA 24669 STRINGER 23R CLIP AT STA 727C CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED CLIP. 2L72 4F4 FRTA16WE E2GL 20040816000052004081600005NM 2004 8 16 2004UALA00677 120040721A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 SHEAR TIE BETWEEN STR 27L AND 28L AT BS 1400 IS CRACKED AND CORRODED. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20040816000102004081600010NM 2004 8 16 04FDEA02406 120040809A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03. 2L73 4F RTA22WE 20040816000112004081600011NM 2004 8 16 04FDEA02407 120040809A5320A5A7114515 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, LT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 50 CRACKED. LONGERON 50 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME III. 2L73 4F RTA22WE 20040816000152004081600015NM 2004 8 16 HNAA0408108 120040708A291082970009231 LINE DHAV DHC8 DHC8102 2809003NM HYD SYSTEM CHAFED A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA07808EX 299 FLIGHT 3847 REPORTED HAVING NR 1 HYDRAULIC CAUTION LIGHT FLICKERING DURING DESCENT INTO SYR. ISOLATION VALVE ACTIVATED. THERE WAS NO DISRUPTION TO HYDRAULIC SYSTEMS REMAINDER OF THE FLIGHT. MAINTENANCE FOUND A NR 6 HYDRAULIC LINE CHAFED THROUGH UNDER PANEL 419AT. DAMAGED LINE WAS REMOVED AND A TEMPORARY FLEX LINE WAS INSTALLED. AIRCRAFT WAS GROUND RUN, ALL SYSTEMS AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040816000162004081600016NM 2004 8 16 2004UALA00538 120040602A5310 SHEAR TIE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29399UA 24674 SHEAR TIES WERE FOUND DAMAGED OR HAD EXCESSIVE GAP BETWEEN SKIN AND SHEAR TIE AT STA 727 S24L-S25L, 727D S24L-S25L, 727C S25R-S26R, 727D S25R-S26R, 727E S24L-S25L AND 767 S24L-S25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIES. 2L72 4F4 FRTA16WE E2GL 20040816000182004081600018NM 2004 8 16 2004UALA00569 120040612A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 BS 600 FRAME BETWEEN STR 24L AND 25L DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816000272004081600027WP 2004 8 16 04FDEA01919 120040703A5414 SKIN DOUG DC10 DC1030 3023501WP RT WING PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 NR 3 ENG PYLON CRACK RIGHT SIDE STA YN 320 ABOVE CORE COWL. TRIMMED OUT CRACK IAW DC10 SRM 54-00-01VOL 2, FABBED DOUBLER & FILLER IAW DC10 SRM 54-00-01 VOL 1, INSTALLED REPAIR IAW DC10 SRM 54-00-01 VOL 1. 2L73 4F A22WE 20040816000292004081600029NM 2004 8 16 2004UALA00574 120040612A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 AFT PIT FRAME CORRODED AT UPPER FLANGE STA 1500, LBL 4 - 8. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816000322004081600032NM 2004 8 16 2004UALA00577 120040611A1420 CONNECTOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE EMERGENCY LIGHT LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29771UA 26932 SEAT EMERGENCY LIGHTS INOP AT 3F BOTH LIGHTS. SECURED CONNECTOR UNDER STORAGE COMPARTMENT BETWEEN SEATS. 2L72 4F4 FRTT0001SE E46NE 20040816000342004081600034NM 2004 8 16 2004UALA00579 120040514A5754114W41609 WEDGE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29785UA 26954 TRAILING EDGE WEDGE DELAMINATED AT LWR INBOARD END FROM RUBBING ON LEADING EDGE WING SKIN. MAJOR REPAIR ACCOMPLISHED. REPAIRED WEDGE. 2L72 4F4 FRTT0001SE E46NE 20040816000362004081600036NM 2004 8 16 2004UALA00581 120040604A5751 FITTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE AILERON ACTUATORCRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29774UA 26936 ACTUATOR FITTINGS CRACKED. REPLACED FITTINGS. 2L72 4F4 FRTT0001SE E46NE 20040816000382004081600038NM 2004 8 16 HNAA0408105 120040802A3230574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM MLG INTERMITTENT A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07812EX3192612262 312 FLIGHT 3983 OUT OF LGA, HAD TO RETURN TO FIELD, REPORTING THE GEAR DID NOT COME UP WHEN SELECTED UP. AIRCRAFT WAS FERRIED TO MIDDLETOWN FOR REPAIRS. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE LANDING GEAR SELCTOR VALVE INTERMITTENT. VALVE WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040816000402004081600040NM 2004 8 16 MWEA040106 120040619A5230591014167 DOUBLER BOEING717 717200 1383700NM CARGO DOOR PAN DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31904ME 55168 FORWARD CARGO DOOR PAN IS DAMAGED AT LOWER AFT CORNER. INSTALLED DOUBLER. 2L72 4F TRA6WE 20040816000452004081600045NM 2004 8 16 04FDEA02305 120040730A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 536CB, UPPER STRINGER NR 10, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES LONG. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 536CB, UPPER STRINGER NR 10 AS PER SRM 57-20-00 FIG 10, VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10, VOL I AND INSTALLED REPAIR ANGLES AS PER SRM 51-33-01 VOL II AT LT STRINGER NR 10. 2L73 4F RTA22WE 20040816000512004081600051NM 2004 8 16 04FDEA02430 120040810A5320AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 INTERCOSTAL BETWEEN STA 1481 AND STA 1501 AT LONGERON 19R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040816000522004081600052WP 2004 8 16 04FDEA02431 120040811A5320ADA01407 PANEL DOUG MD10 MD1010F 3022112WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 FWD CARGO SUMP PNL STA 900-920 IS CRACKED AND CORRODED RT SIDE. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE. 2L73 4F RTA22WE 20040816000542004081600054NM 2004 8 16 04FDEA02308 120040730A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STATION 6-30 TO 6-50 LONGERON 43L FOUND CRACKED AT AFT EDGE AREA. REMOVED AND REPLACED WITH NEW INTERCOSTAL AS PER SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040816000572004081600057NM 2004 8 16 0401156303 120040704A3350 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHT LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 23HK-31HK. RESEATED LIGHT ASSEMBLY CONNECTORS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040816000612004081600061NM 2004 8 16 04FDEA02219 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.497, MATERIAL REMOVED = 0.026, REMAINING THICKNESS = 0.471 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816000622004081600062NM 2004 8 16 04FDEA02220 120040728A5315 FLOORBEAM DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RIGHT HAND CAC COMPARTMENT AT STA 6-90 AT APPROX 64 INCHES FROM CENTER FOUND CRACK AT FLOORBEAM LOWER CHORD. CRACK AT CAC, RT COMPARTMENT AT STA 6-90 AT APPROX. 64 INCHES FROM CENTER AT FLOORBEAM LOWER CHORD CARRIED OUT REPAIR AS PER FEDEX EA NR 1-5310-79813, TITLE: FUSELAGE - MAINFRAME - FLOORBEAM ASSEMBLY - CRACK REPAIR. 2L73 4F RTA22WE 20040816000642004081600064NM 2004 8 16 04FDEA02222 120040728A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 MAIN DECK CARGO COMPARTMENT - AT STA 755 AXIS X = 47.58 SEAT TRACK LOWER SURFACE FOUND CRACKED. DAMAGED SEAT TRACK AT MAIN DECK CARGO COMPARTMENT, STA 755 AXIS X = 47.58 REMOVED AS PER SRM 51-31-01, VOLUME 2. REPAIR TRACK FABRICATED, REWORKED AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND SRM 51-31-01, VOLUME 2. 2L73 4F RTA22WE 20040816000652004081600065NM 2004 8 16 04FDEA02223 120040728A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING INBOARD FLAP VANE INBOARD TEE FITTING FORWARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.878. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, TITLE: WINGS - TRAILING EDGE FLAPS - RT INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040816000662004081600066NM 2004 8 16 04FDEA02224 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 3 PIVOT INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093, FINAL DIAMTER= 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816000672004081600067NM 2004 8 16 04FDEA02225 120040728A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING INBOARD FLAP VANE INBOARD TEE FITTING MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER = 0.881. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, TITLE: WINGS - TRAILING EDGE FLAPS - RT INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040816000682004081600068NM 2004 8 16 04FDEA02309 120040730A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STATION 6-30 TO 6-50 LONGERON 43R FOUND CRACKED AT AFT EDGE AREA. REMOVED AND REPLACED WITH NEW INTERCOSTAL AS PER SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040816000712004081600071WP 2004 8 16 0401019882 120040617A5320 FLOOR SUPPORT DOUG DC9 DC951 3022051WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01670MC 47659 DURING H-CHECK FOUND CORROSION ON Z-ANGLE FLOOR SUPPORT FROM BS 160 TO BS 200 LBL 55. REPAIRED PER EA 98-199572. 2L72 4F RTA6WE 20040816000732004081600073EU 2004 8 16 AWXA200400874 120040811A1420E0052R8B3APNE CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 26 DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 PHX - EEL - DURING E-01 CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 LT INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 26 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040816000762004081600076NM 2004 8 16 AWXA200400877 120040728A5315654580863 FLOORBEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON LOWER SURFACE UPPER AFT LEG OF FLOORBEAM UPPER CHORD AT BS 294, RBL 13, WL 208. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM UPPER CHORD AT BS 294, FROM LBL 22 TO RBL 23; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH REPAIR ANGLES, AND A STIFFENER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20040816000792004081600079NM 2004 8 16 SWAA042321 120040812A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040816000802004081600080NM 2004 8 16 SWAA042322 120040812A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29737JW 27869 DURING SCHEDULED 5Y CHECK, AFT LEFT AND RIGHT EMERGENCY EXIT LIGHTS FAILED OP CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040816000822004081600082EU 2004 8 16 AWXA200400860 120040809A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 11 BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28651AW 866 PHX - EEL - DURING 4-DAY CHECK FOUND THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CABLE HARNESS UNDER SEAT ROW 11 RT, OPERATIONAL CHECK OF LIGHT WAS GOOD. 2L72 4F RTA28NM 20040816000852004081600085NM 2004 8 16 2004UALA00619 120040628A3230 LANDING GEAR BOEING747 747422 1384935NM PWA 4056 PW4056 NE MALFUNCTIONED A UALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 WP29173UA 24380 AFTER T/O GEAR DOOR OPEN LIGHT INDICATION. CREW FELT VIBRATION FROM OPEN DOORS. PROBABLE CAUSE IS A DOOR OUT OF SEQUENCE CONDITION DUE TO ALTERNATE EXTEND MOTOR NOT RESETTING. THIS IS KNOWN CONDITION AND IS SOMETIMES CAUSED BY DEPRESSING ALTERNATE EXTEND SWITCH FOR A PERIOD LESS THAN 90 SECONDS. WHEN ACTUATED SWITCH MUST BE ENERGIZED FOR AT LEAST 90 SECONDS TO ENSURE THAT MOTOR WILL RESET. PREVIOUS INCIDENTS WERE KNOWN TO OCCUR WHEN MAINTENANCE CREWS USED SWITCH FOR WHEEL WELL ACCESS AND DID NOT RUN FOR THE REQUIRED 90 SECONDS. BOEING ISSUED SERVICE TIP 32-007 ADDRESSING THIS, AND IT HAS BEEN INCORPORATED INTO APPLICABLE SECTIONS OF THE AMM. 2L74 4F4 FRTA20WE E24NE 20040816000862004081600086 2004 8 16 SWAA042313 420040812A2565 BOTTLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29619SW 28035 L2 DOOR EVAC SLIDE LOW PRESSURE INDICATOR. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040816000872004081600087 2004 8 16 SWAA042314 420040812A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040816000902004081600090NM 2004 8 16 SWAA042317 120040812A53106545833 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM AT BS 298, AT BS 328, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040816000952004081600095NE 2004 8 16 2004UALA00585 220040615A72009325M85G04 ENGINE BOEING737 737322 1384676NM GE CFM56 CFM563US 13802NE NR 2 FLUCTUATES A UALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29375UA32639 24640 856186 ABORTED TAKEOFF AT 110 KNOTS DUE TO FUEL FLOW FLUCTUATION ON NUMBER 2 ENGINE. *S/D* ACCOMPLISHED POWER ASSURANCE CHECK, PMC CHECK, AND ACCELERATION CHECK. ALL CHECKS OK. NO FAULTS FOUND. 2L72 4F4 FRTA16WE E2GL 20040816000962004081600096NM 2004 8 16 2004UALA00586 120040616A2920NAS161210 PACKING BOEING757 757222 1384956NM HYD PACK LEAKING A UALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29589UA 28707 LEFT HYDRAULIC QUANTITY STARTED DROPPING IN CRUISE. QUANTITY STABILIZED AT .25 PERCENT AFTER PUMPS SELECTED OFF. PACKING AT HYDRAULIC MOTOR GENERATOR SHUTOFF VALVE WAS LEAKING. REPLACED PACKING. 2L72 4F RTA2NM 20040816000972004081600097NM 2004 8 16 2004UALA00587 120040330A1420BACC63CC1814S9 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE BOOST PUMP DAMAGED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29573UA 26685 IN CRUISE AT FL 370 WITH 7.8 IN CENTER TANK RIGHT CENTER BOOST PUMP LOW PRESS EICAS CAME ON. THE CTR PMP LOW PRESS INDICATION OCCURED DUE TO LOSS OF PUMP POWER AS A RESULT OF A TRIPPED RT FUEL OVRD CIRCUIT BREAKER (C370). THE CAUSE OF THE TRIPPED BREAKER WAS TRACED TO AN ELECTRICAL SHORT OF CONNECTOR D40358J. FURTHER ANALYSIS OF THE CONNECTOR INDICATES THAT THE SHORT CIRCUIT CONDITION WAS A RESULT OF A DAMAGED CONTACT LOCKING MECHANISM WHICH CUT INTO THE CONNECTOR INSULATION & CONTACTED THE ADJACENT WIRE. REPLACED THE CONNECTOR AND SPLICED IN NEW WIRES PER STANDARD PRACTICES. 2L72 4F4 FRTA2NM E17NE 20040816001012004081600101NM 2004 8 16 2004UALA00591 120040617A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29776UA 26937 SEAT 18G EEL LIGHT DOES NOT STAY IN PLACE. REPLACED EEL PROX LIGHT ASSY. 2L72 4F4 FRTT0001SE E46NE 20040816001042004081600104WP 2004 8 16 04FDEA01931 120040703A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 652 IS CRACKED. FABRICATED AND INSTALLED REPAIR PARTS IAW DC10 SRM 53-12-01 VOL 3, 53-00-01 VOL I AND 51-21-01 VOL 2. 2L73 4F A22WE 20040816001082004081600108WP 2004 8 16 04FDEA01927 120040703A5754 SKIN DOUG DC10 DC1030 3023501WP NR 8 SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND WING LOWER SURFACE, LEADING EDGE ADJACENT TO NR 8 SLAT IS GOUGED. BLENDED GOUGE IAW DC10 SRM 57-00-01 VOL I, FABRICATED AND INSTALLED DOUBLER IAW DC10 SRM 57-10-00 VOL I, 51-21-01 VOL 2, AND 51-33-01 VOL 2. 2L73 4F A22WE 20040816001112004081600111EU 2004 8 16 2004UALA00466 120040511A2897D9295750208 WIRE HARNESS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT WING TANK FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29448UA 842 FLIGHT DIVERTED DUE TO A POSSIBLE FUEL LEAK. UNWANTED FUEL TRANSFER AND DEGRADED FUEL INDICATIONS CAUSED BY LEFT HAND WING INNER FUEL QUANTITY HARNESSES FAILURE. REPLACED LEFT HAND WING INNER FUEL QUANTITY HARNESSES. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040816001122004081600112 2004 8 16 2004UALA00488 420040520A3417HG2030AD09 COMPUTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE AIR DATA MALFUNCTIONED A UALAO OTHER G MULTIPLE FAILURE DEDESCENT 1 WP29462UA 1272 DURING DESCENT ACFT LOST FACS & EXPERIENCED DOWNGRADED NAVIGATION. EMERGENCY DECLARED. AIRSPEED DISAGREE OCCURRED BETWEEN ADR 1 AND ADR 2. ADIRU NR 1 WAS REPLACED AND NR 2 AIRSPEED FAULT WAS PRESENT. SHOP FINDINGS FOUND THE UNIT REMOVED FROM POSITION 2 RECORDED AN INVALID LEFT STATIC PRESSURE INPUT. ADIRU NR 2 WAS REPLACED. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040816001132004081600113WP 2004 8 16 0401119929 120040516A5311 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018923E 45838 DURING M-CHECK FOUND CRACK IN FRAME AT BS 598 L24L. REPAIRED PER EA 99-199088. 2L72 4F A6WE 20040816001142004081600114WP 2004 8 16 04FDEA01938 120040705A5753ARC2512 HINGE DOUG DC10 DC1030 3023501WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 COMPLY WITH EA 8-5750-79542, WINGS RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COMPLIED WITH EA 8-5750-79542. 2L73 4F A22WE 20040816001182004081600118NM 2004 8 16 MWEA040125 120040728A5522591041281 SKIN BOEING717 717200 1383700NM ELEVATOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31906ME 55170 LIGHTNING STRIKE DAMAGE LEFT ELEVATOR LOWER OUTBOARD TRAILING EDGE. FABRICATED AND INSTALLED ELEVATOR STRUCTURAL ASSEMBLY. 2L72 4F TRA6WE 20040816001202004081600120WP 2004 8 16 04FDEA01923 120040703A5753 SKIN DOUG DC10 DC1030 3023501WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND INBOARD FLAP, INBOARD, AFT HOIST POINT, SKIN CRACKED/DAMAGED. REMOVED TRAILING EDGE WEDGE, FABRICATED REPAIR DOUBLER IAW DC10 SRM 51-21-01 VOLUME 2. REINSTALLED TRAILING EDGE WEDGE IAW DC10 SRM 51-31-01 VOLUME 1. 2L73 4F A22WE 20040816001212004081600121WP 2004 8 16 04FDEA01922 120040703A5753ARC2340 RIB DOUG DC10 DC1030 3023501WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND INBOARD FLAP, INBOARD TRACK UPPER FAIRING, FORWARD RIB CRACKED. REMOVED CRACKED RIB IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW RIB IAW DAC DWG ARC 2340. INSTALLED RIB IAW DC10 SRM 51-35-01 VOL 2 AND DC10 SRM 51-35-02 VOL 2. 2L73 4F A22WE 20040816001222004081600122NM 2004 8 16 04FDEA02257 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.494 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001242004081600124NM 2004 8 16 04FDEA02259 120040728A5410 STRIP BOEING727 727200 138407ENM NR 3 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25207FE 22929 COMPY WITH EA 7-7110-80586 POWERPLANT - COWL NR 3 ENG COWL RUB STRIP REPAIR P/N 259-0175-135. COMPLIED WITH EA 7-7110-80586. 2L73 4F RTA3WE 20040816001272004081600127NM 2004 8 16 04FDEA02196 120040727A5320 DOUBLER DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CENTER LANDING GEAR ZONE 146 RIGHT HAND SIDE WALL STA 1380 DOUBLER CRACKED. REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040816001302004081600130NM 2004 8 16 04FDEA02199 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT HORIZONTAL STABILIZER NR 13R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-79830, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 13R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001322004081600132NM 2004 8 16 04FDEA02201 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 2 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001372004081600137NM 2004 8 16 04FDEA02203 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 16 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79823, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 16L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001392004081600139NM 2004 8 16 04FDEA02205 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 20 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79833, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 20L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001412004081600141NM 2004 8 16 04FDEA02207 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 24L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80303, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 24L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001432004081600143NM 2004 8 16 04FDEA02209 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 1 INBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.413, MATERIAL REMOVED = 0.007, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001462004081600146NM 2004 8 16 04FDEA02212 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001522004081600152EU 2004 8 16 2004UALA00599 120040622A5310 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29461UA 1266 FUSELAGE DAMAGE IN NOSE AREA AFT OF THE E&E DOOR. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER & SUPPLATE REPAIRS. 2L72 4F4 FRTA28NM E40NE 20040816001562004081600156EU 2004 8 16 04FDEA02335 120040801A5320 TEE FITTING AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25409FE 273 MDC FR 10 TO FR 14A, 20 INCHES OUTBOARD FROM LEFT OF CTR T-CAP HAS CORROSION (LEVEL 2) INCLUDING IN AND AROUND ALL FASTENER HOLES. REMOVED AND REPLACED T-CAP IAW A310/200 SRM 51-40-21. 2L72 4F RTA35EU 20040816001572004081600157WP 2004 8 16 MWEA040116 120040706A533059360033 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE OUT OF TOLERANCEA MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 RIGHT PRIMARY STATIC PORT AREA FUSELAGE SKIN BUTT JOINT SKIN TO SKIN FLUSHNESS IS OUT OF TOLERANCE LOCATED AT STATION 589 LONGERON 26 RIGHT, UPPER SKINS ARE OUT AT .022, LOWER SKINS ARE OUT AT .015. FABRICATED AND INSTALLED LONGERON. 2L72 4F A6WE 20040816001582004081600158WP 2004 8 16 MWEA040114 120040706A523049123171 TORQUE TUBE DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 CENTER CARGO DOOR AFT TORQUE TUBE IS CORRODED. REMOVED AND REPLACED AFT TORQUE TUBE. 2L72 4F A6WE 20040816001592004081600159 2004 8 16 249TR0034 420040802A221010618165 FORCE LIMITER BOEING737 7372K5 138448XNM AILERON MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO PILOT -B- WILL NOT ENGAGE IN FLIGHT. REPLACED AILERON FORCE LIMITER AND OPS CHECKED PER MM 22-11-132. 2L72 4F RTA16WE 20040816001602004081600160NM 2004 8 16 2004UALA00696 120040721A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29926UA 26648 STRINGER 21R DAMAGED BETWEEN STA 867 AND 887. MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGED STRINGER 21R. 2L72 4F4 FRTA16WE E2GL 20040816001612004081600161NM 2004 8 16 2004UALA00702 120040725A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE ROW 10 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29938UA 26671 FOUND EMERGENCY LIGHTS FROM ROW 10 UP TO LAST ROW, INOP. SPLICED HARNESS AT ROW 10 AND REPLACED WIRE FEED HARNESS FROM ROW 12 AFT. 2L72 4F4 FRTA16WE E2GL 20040816001632004081600163NM 2004 8 16 04FDEA02213 120040728A5755 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING UPPER WING SKIN FORWARD OF NUMBER 5 SPOILER CENTER HINGE FOUND CORRODED. BLENDED OUT CORROSION AS PER SRM 51-21-01, VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 2L73 4F RTA22WE 20040816001692004081600169 2004 8 16 2004UALA00608 420040616A2565 BOLT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE VALVE MISINSTALLED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29193UA 26890 DOOR 4 RIGHT SLIDE, AT OVERHAUL A BOLT WAS FOUND INSERTED IN THE SAFETY PIN LOCATION OF THE VALVE. THE FIRING LANYARD WAS WRAPPED AROUND A INFLATION HOSE. THE SURVIVAL KIT ATTACHMENT CORD WAS LOCATED ON THE SIDE RATE COVER INSTEAD OF THE GIRT AREA. ONE OF THE SHEAR PIN RESTRAINTS WAS FOUND TO BE SHEARED. INSTALLATION OF A BOLT INSTEAD OF MANUFACTURER'S SAFETY PIN IS ACCEPTABLE PER UA AMM. OTHER DEFECTS CAUSED BY IMPROPER PACKING. AS SHOP AND PERSONNEL THAT PREVIOUSLY PACKED SLIDE ARE NO LONGER BEING USED, NO FOLLOW UP ACTION REQUIRED. 2L74 4F4 FRTA20WE E24NE 20040816001712004081600171 2004 8 16 2004UALA00610 420040623A3421 BEARING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE ATTITUDE IND BURNED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29645UA 25280 ELECTRICAL BURNING ODOR IN COCKPIT, FIRST AND BUSINESS. BURNING SMELL WAS CAUSED BY FAILED ROTOR SPIN BEARING IN COCKPIT STANDBY ATTITUDE INDICATOR (SAI). SHOP CONFIRMED SAI HAD OVERHEATED ROTOR BEARING. STATIC INVERTER (ON E1-4 SHELF) ALSO WAS FAILED. UNCERTAIN WHICH FAILURE OCCURED FIRST, BUT IT IS LIKELY THAT OVERHEATED SAI RESULTED IN FAILED INVERTER. SHOP HAS ONGOING PROJECT (BY ATTRITION) TO UPGRADE SAI'S BY REPLACING SPIN BEARING AND REDUCTION GEAR ASSY WITH MORE DURABLE CERAMIC MATERIAL. OVERHEATED SAI WAS NOT UPGRADED BEFORE FAILURE. 2L72 4F4 FRTA1NM E24NE 20040816001722004081600172NM 2004 8 16 HNAA0400065 120040710A2437 MONITOR DHAV DHC8 DHC8102 2809003NM BATTERY TEMP INOPERATIVE A HNAAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 EA07938HA 152 RETURN TO FIELD, DUE TO MAIN AND AUX BATTERIES INDICATING 65 DEGREES. REMOVED AND REPLACED BATTERY TEMP MONITOR. 2H72 4T RTA13NM 20040816001842004081600184NM 2004 8 16 2004UALA00618 120040626A5315 STIFFENER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 CRACK IN U-STIFFENER BS 246, APPROX RBL 75, FWD SIDE OF FLOORBEAM. FABRICATED & INSTALLED STIFFENER. 2L72 4F4 FRTA1NM E24NE 20040816001852004081600185NM 2004 8 16 2004UALA00612 120040624A5753 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT WING TE FLAP CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 RT WING, INBOARD FLAP, UPPER SKIN CHAFED ON OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH .032 INCH BONDED DOUBLER. 2L72 4F4 FRTA2NM E17NE 20040816001872004081600187EU 2004 8 16 04FDEA01635 120040608A5551A5557011120051 FITTING AIRBUS310 A310222 3930315EU ZONE 300 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25420FE 339 A/C 420 WAS IN FOR B-CHECK, FOUND VERT STAB FITTING HAD CORROSION. REMOVED AND REPLACED VERT STAB FITTING. 2L72 4F RTA35EU 20040816001882004081600188WP 2004 8 16 04FDEA01857 120040305A5512 SKIN DOUG MD10 MD1010F 3022112WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25385FE 46619 HORIZONTAL STABILIZER CONSTANT SECTION UPPER AND LOWER SKIN CRACKED WITHIN FLYABLE LIMITS. CRACKED PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510- 73244. PARTS AFFECTED: ALC7204-1, ALC7205-1, ALC7441-2. 2L73 4F RTA22WE 20040812001222004081200122NM 2004 8 12 DHL2004754020 120040623A3240 FUSIBLE PLUG BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NR 3 WHEEL MELTED A DHLAO OTHER E VIBRATION/BUFFET LDLANDING 1 SO01754DH 22008 NR 3 MAIN TIRE FUSE PLUG MELTDOWN AT PARKING RAMP. NR 4 MAIN TIRE FUSE PLUG MELT DOWN AT PARKING RAMP. REPLACED NR 3 MAIN TIRE ASSY IAW MM 32-45-1. REPLACED NR 4 MAIN TIRE ASSY IAW MM 32-45-1. 2L73 4F4 F A3WE E2EA 20040813000012004081300001NM 2004 8 13 C8GA20040014 120040804A2611100064901 SMOKE DETECTOR BOEING727 7272A1 138407FNM PWA JT8 JT8D* NE CARGO BAY DEFECTIVE A C8GAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO15287SC5520 21345 FLT 707 FROM KPHX TO KMCI. DURING CRUISE, THE LOWER AFT CARGO FIRE WARNING CAME ON. FOLLOW ALL CCIA AOM ABNORMAL PROCEDURES, CONTACTED ATC AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED TO KGCK AND LANDED WITHOUT INCIDENT. UPON LANDING, THE AIRCRAFT WAS THEN INSPECTED AND DEFERRED THE AFT CARGO COMPARTMENT FIRE DETECTION UNDER MEL 26-19. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 26-19 BY REPLACING THE LOWER AFT CARGO SMOKE DETECTOR IAW SECURAPLANE ST3000 MANUAL WITH NO MALFUNCTION FOUND. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040813000062004081300006WP 2004 8 13 ABXA040237 120040618A531099577395 SHEAR TIE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23981AX 47273 CRACKED SHEAR TIE AT FS 945 LONGERON 15 RT. REPLACED SHEAR TIE ON EA 53110008-202. 2L72 4F A6WE 20040813000132004081300013NM 2004 8 13 2004UALA00681 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 AFT PIT FRAME AT STA 1400 ABOVE STR 25L IS DENTED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000142004081300014NM 2004 8 13 2004UALA00682 120040723A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FRAME AT STA 1500 ABOVE STR 25L IS DENTED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040813000272004081300027EU 2004 8 13 AWXA200400686 120040623A5320D53475521200100 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR SILL FORWARD SEALING CORNER BETWEEN FR 52A AND FR 52A+10. MAINTENANCE REMOVED AND REPLACED AFT CARGO DOOR SILL FORWARD SEALING CORNER IAW A320 SRM 51-42-11, FIG. 2-8, 12-13, AND 18. 2L72 4F RTA28NM 20040813000322004081300032GL 2004 8 13 ALG2004F00042 220040625A7510 LINE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL BLEED VALVE LOOSE E ALGAAE UNSCHED LANDING ENGINE SHUTDOWN EFJVIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION HOHOVERING 1 SW032619 51375 CAE890098 WHILE HOVERING FOR TAKE OFF, A NOTICEABLE BANG CAME FROM THE ENGINE COMPARTMENT AND A RIGHT YAW OCCURRED. AIRCRAFT CONTROL WAS MAINTAINED AND SYSTEMS INSTRUMENTS WERE IN THE GREEN. AIRCRAFT WAS THEN HOVERED TO THE MAINTENANCE PAD AND SHUT DOWN. MAINTENANCE FOUND COMPRESSOR BLEED VALVE AIR LINE LOOSE, TIGHTEN AIR LINE AND COMPLIED WITH MFG PNEUMATIC AIR LINE CHECK. INSPECTED COMPRESSOR AREA FOR FOD DAMAGE FOUND NONE, AIRCRAFT WAS GROUND RUN AND LEAK CHECKED AND OPS CHECK FLOWN GOOD. 1G71 3U3 U H2SW E1GL 20040813000342004081300034NM 2004 8 13 ASMF200407034 120040730A7722766342 VALVE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LT SIDE FAILED W ASMFO OTHER MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW23158PL659 49761 725857 CAPTAIN REPORTED HIGH TEMPERATURE ON LT ENGINE. LT ENGINE REACHED 488 DEGREE (C) DURING START AND DURING TAKE OFF REACHED 605 DEGREE (C) AT 1.88 OF EPR'S, REDUCING THRUST LEVER REACHING 595 DEGREE (C) OF EGT FOR A MINUTE AND DURING CLIMB N1 AND N2 WERE ADJUSTED TO 97 AND 98.8 RESPECTIVELY, REACHING 605 DEGREE (C) DURING 10 SECONDS. LT ENGINE WAS INSPECTED IAW MM 72-00-00 AND 71-00-00, ALL CORRECT. PARAMETERS WERE CHECKED VERSUS THE MM BEING WITHIN LIMITS. DURING OVERNIGHT SERVICE, P AND D VALVE AND TEST TUBES NR. 4, 5 AND 8 WERE REPLACED IAW MM 73-13-05 AND 77-21-03 AND ENGINE TESTS WAS PERFORMED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040813000382004081300038NM 2004 8 13 04FDEA02340 120040801A5713 STRINGER DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING THRU FUEL TANK ACCESS PANEL 635 BT CUT-OUT AT MOST UPPER STRINGER NR 12 FOUND STRINGER END WITH CRACK OF ABOUT 10 INCH LONG. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED REPAIR ANGLES AT RT FUEL TANK PANEL NR 635BT AT STRINGER NR 12 AS PER SRM 51-33- 01, VOLUME II. 2L73 4F4 FRTA22WE E13NE 20040813000432004081300043EU 2004 8 13 04FDEA02344 120040802A3230D226550003 DAMPER AIRBUS330 A300* EU GE CF6 CF680 30025NE MLG FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25661FE12881700 760 AFTER TAKEOFF, GEAR WOULD NOT RETRACT, RETURNED. REMOVED AND REPLACED LT LANDING GEAR PITCH DAMPER REF MM 32-11-15-4 RII:233985, ENT BY: 274911 RPT BY: 274911, R/I 02AUG04 04:39 IAH R, FACT 02AUG04 10:38 IAH U GEAR SWING REQUIRED, JACKED A/C FOR GEAR SWING IAW MM 07-11-00-0 AT HANGER, GEAR SWING CHECKED OK IAW MM. 2L72 4F4 FRTA26NM E13NE 20040813000482004081300048EA 2004 8 13 COMA0460439 120040804A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT IB FLAP GOUGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01821CA 7420 RT IB FLAP LOWER SKIN GOUGE JUST AFT OF MAIN TIRE. IAW REO 601R-57-51-058. 2L72 4F4 FRTA21EA E15NE 20040813000492004081300049EA 2004 8 13 COMA0460440 120040804A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01821CA 7420 RT FLOOR ANGLE FS 621.00 CRACKED. IAW REO 601R-53-61-117. 2L72 4F4 FRTA21EA E15NE 20040813000622004081300062NM 2004 8 13 SWAA042289 120040810A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND BS 188, WL 208, LT & RT STUB FRAMES CRACKED. REMOVED AND REPLACED BOTH FRAMES PER SRM. 2L72 4F RTA16WE 20040813000652004081300065NM 2004 8 13 SWAA042292 120040810A53106546595 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727A, BETWEEN STRINGERS 21R & 22R. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM. 2L72 4F RTA16WE 20040813000752004081300075NM 2004 8 13 2004UALA00713 120040726A5754 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 5 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29512UA 24809 T/E WEDGE DELAMINATED, SLAT NR 5. REPLACED TRAILING EDGE WEDGE. 2L72 4F4 FRTA2NM E17NE 20040813000792004081300079NM 2004 8 13 2004UALA00717 120040802A2613 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE OVERHEAT SYS ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29329UA 24149 ABORTED TAKEOFF AT 110 KNOTS DUE TO A WING BODY OVERHEAT MESSAGE. LEFT WING BODY OVERHEAT LIGHT COME ON AT TAKE-OFF ROLL. MAINTENACE CHECKED LEFT PACK AREA FOR PNEUMATIC LEAK. NO LEAKS WERE FOUND. REPOSITIONED OVERHEAT SENSING ELEMENT GROMMETS. RAN LEFT PACK FOR AN EXTENDED TIME WITH APU AIR AND OVERHEAT LIGHT DID NOT ILLUMINATE. 2L72 4F4 FRTA16WE E2GL 20040813000802004081300080 2004 8 13 2004UALA00718 420040804A2565 COVER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29446UA 834 EVAC SLIDE ON DR2L COVER WILL NOT STAY ON. THE FWD RETAINING HOLE IN THE IN THE SLIDE FIBERGLASS PACKBOARD WAS DAMAGED. THE PROBABLE CAUSE FOR THE PACKBOARD HOLE GETTING DAMAGED IS IN-SERVICE IMPACT BY FOREIGN OBJECTS, SUCH AS SERVICE CARTS OR PERSONNEL/PASSENGERS AGAINST THE DECORATIVE COVER. REPLACED RETAINING HOLE. 2L72 4F4 FRTA28NM E40NE 20040813000822004081300082 2004 8 13 2004UALA00720 420040430A2565 BOTTLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29532UA 25072 ZERO BOTTLE PRESSURE. PRESSURE RELEASE VALVE ON GAUGE INOP. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PRESSURE RELIEF VALVE. 2L72 4F4 FRTA2NM E17NE 20040813000842004081300084 2004 8 13 2004UALA00722 420040422A2565 DISK BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BOTTLE RUPTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29519UA 24872 LOW BOTTLE PRESSURE. LEAK DETECTED AT THE RUPTURED DISK AT RELIEF HOLES. REPLACED DISK. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. 2L72 4F4 FRTA2NM E17NE 20040813000852004081300085NM 2004 8 13 SWAA042296 120040810A53126546568 BULKHEAD BOEING737 7373A4 1384585NM AFT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C4 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 6L. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20040813000862004081300086NM 2004 8 13 SWAA042297 120040810A5310141A880 WINDOW POST BOEING737 7375H4 138449DNM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT UPPER WINDOW POST CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20040813000922004081300092 2004 8 13 2004UALA00723 420040413A2565 SCHRADER VALVE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29513UA 24810 LOW BOTTLE PRESSURE. LEAK DETECTED. REPLACED SCHRADER VALVE. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS. 2L72 4F4 FRTA2NM E17NE 20040813001112004081300111NM 2004 8 13 2004UALA00652 120040711A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 CABIN FLOORBEAM AT AFT GALLEY STA 1681 LBL 36 CORRODED AROUND SCREW HOLES. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND FABRICATED FLOORBEAM CAP AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040813001152004081300115NM 2004 8 13 2004UALA00656 120040712A3350 INVERTER BOEING757 757222 1384956NM PWA 2037 PW2037 NE OVERWING EXIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29532UA 25072 EMERGENCY EXIT PATH LIGHT INOPERATIVE NEAR OVERWING EXIT. REPLACED INVERTER. 2L72 4F4 FRTA2NM E17NE 20040813001242004081300124NM 2004 8 13 SWAA042284 120040809A53126546568 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29686SW 23175 DURING SPV, FOUND BS 1016, BULKHEAD WEB AT STR 7R AND STR 8R, CRACKED. REPAIRED BULKHEAD WEB PER EA. 2L72 4F RTA16WE 20040813001252004081300125 2004 8 13 COMA0460435 420040728A34406229302004 RADAR CNDAIRCL600 CL6002B19 1900309EA AVIONICS INOPERATIVE A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01479CA1214 179 7675 FLIGHT 5352 RADAR IS INOP. COULD NOT DUPLICATE. REPLACED RADAR ASSY. 2L72 4F RTA21EA 20040813001282004081300128NM 2004 8 13 P5CA0401120 120040717A2421 SEAL BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 1 GENERATOR LEAKING A P5CAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP23534MC 21832 517200 NR 1 ENGINE OIL QTY DROPPED FROM 5.3 GALLONS AFTER TAKEOFF, QTY DROPPED TO 1.25 GALLONS, OIL PRESSURE CLIMBED FROM 50 PSI TO 75 PSI & TEMP 110C. REMOVED AND REPLACED NR 1 ENGINE GENERATOR & GENERATOR SEAL, ALSO REPLACED NR 1 ENGINE CSD SEAL. OPS CHECK OK IAW AMM 24-11-01. 2L74 4F4 F A20WE E23EA 20040813001362004081300136NM 2004 8 13 SWAA042307 120040809A575365464277 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C2 CHECK, FOUND LT WING T/E AFT FLAP DISBONDED. REMOVED AND REPLACED T/E FLAP ASSY PER MM. 2L72 4F RTA16WE 20040813001442004081300144NM 2004 8 13 0401096624 120040618A3350 BATTERY PACK BOEING747 747251B 1384892NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING LINE CHECK, FOUND D-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040813001512004081300151NM 2004 8 13 2004UALA00640 120040617A5754114N300264U1 WEDGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29525UA 24978 LEADING EDGE DELAMINATED NR 6 SLAT WEDGE. MAJOR REPAIR. REPLACED WEDGE. 2L72 4F4 FRTA2NM E17NE 20040813001522004081300152EU 2004 8 13 2004UALA00642 120040702A3230 LANDING GEAR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MAINS INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29486UA 1620 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. NOSE GEAR WOULD NOT CENTER BECAUSE THE LGCIU FAILED. REASSEMBLED NOSE GEAR, OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813001532004081300153EU 2004 8 13 2004UALA00643 120040705A3230 LANDING GEAR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MAINS INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29478UA 1533 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. NLG STRUT SEALS WERE TORN. REPL ACED THE NLG STRUT SEALS. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813001742004081300174NE 2004 8 13 2004UALA00632 220040701A7230 BLADES BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT COMPRESSOR DAMAGED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29660UA 27115 COMPRESSOR STALL AT ROTATION ON RIGHT ENGINE. RETURN TO FIELD. BOROSCOPE OF ENGINE FOUND COMPRESSOR BLADE DAMAGE AND ENGINE WAS REMOVED FROM THE AIRCRAFT. FINDINGS AT SHOP VISIT FOUND C-5 BLADE WITH A PIECE MISSING FROM THE T/E TIP (APPROX. 0.750 X 0.750 INCH). THIS IS A TEXTBOOK EXAMPLE OF ONE OF THE FAILURE MODES ASSOCIATED WITH THE "HPC FRONT END DURABILITY" ISSUES BEING ADDRESSED BY PWA. 2L72 4F4 FRTA1NM E24NE 20040813001832004081300183WP 2004 8 13 MWEA040119 120040706A5310591014211 DOUBLER DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 AT STATION 370 ON THE FORWARD CARGO DOOR WEB THERE IS A CRACK ON THE WEB UNDER THE FLOOR RAIL. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20040813001932004081300193NM 2004 8 13 04FDEA02419 120040810A5313ADA3011505 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CORROSION FOUND BETWEEN STA 6-30 AND STA 6-50 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2L73 4F RTA22WE 20040813001942004081300194NM 2004 8 13 04FDEA02420 120040810A5313ADA3011505 LONGERON DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CORROSION FOUND BETWEEN STA 6-50 AND STA 6-70 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I. 2L73 4F RTA22WE 20040813001982004081300198NM 2004 8 13 04FDEA02424 120040810A5320AEA7530521 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK INTERCOSTAL BETWEEN STA 1341 AND STA 1361 AT LONGERON 19L FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II PAGE 27. MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.095, ORIGINAL THICKNESS = 0.100 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1 FIGURE 3. 2L73 4F RTA22WE 20040816000132004081600013NM 2004 8 16 04FDEA02425 120040810A5320AEA7530521 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 INTERCOSTAL BETWEEN STA 1159 AND STA 1175 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED AS PER MD-11 SRM 53-33-01. 2L73 4F RTA22WE 20040816000172004081600017NM 2004 8 16 2004UALA00559 120040410A5610141W74002 WINDOW BOEING777 777222 1385219NM PWA PW4077PW4077 NE COCKPIT CRACKED A UALAO OTHER O OTHER CRCRUISE 1 WP29775UA 26947 AT FLIGHT LEVEL 330, THE EXTERIOR PANE OF THE WINDSHIELD CRACKED. REPLACED WINDSHIELD. FAILED WINDOW WAS INSTALLED IN AMS ON 1/10/2004. INSTALLED PART HAD BEEN BORROWED FROM KLM AND CAME WITH AN 8130 INDICATING IT WAS A SERVICEABLE PART THAT HAD BEEN OVERHAULED ON 3/25/2003. FAILURE APPEARS TO BE RESULT OF A DAMAGED BUSBAR FROM A HOLE DRILLED INTO THE INNER PLY AT SOME TIME IN THE PAST DURING A SHOP VISIT. WINDOW WAS ON AIRCRAFT FROM 1/10/04 TO 4/10/04. 2L72 4F4 FRTT0001SE E46NE 20040816000192004081600019NM 2004 8 16 2004UALA00570 120040612A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 STA 580, STR 24L-25L FRAME HAS DAMAGE INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816000212004081600021NM 2004 8 16 2004UALA00572 120040612A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 FUSELAGE FRAME STA 1400, STR 25L-27L IS DENTED 3 AREAS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816000232004081600023NM 2004 8 16 04FDEA02411 120040809A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 46R BETWEEN STA 1741 AND 1761. LONGERON 46R REMOVED AND NEW LONGERON P/N AFA7098-501 INSTALLED PER DWG AFA7098, SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20040816000242004081600024NM 2004 8 16 04FDEA02412 120040809A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT FUSELAGE SKIN AT STA Y= 1847, LONGERON 34R FOUND WIND DENT MARK. SKIN TRIMMED-OFF AND REPAIRED PER MD-11 SRM 53-20-00 VOLUME I FIGURE 2. 2L73 4F RTA22WE 20040816000252004081600025NM 2004 8 16 04FDEA02413 120040809A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, WING UNDER SURFACE JUST ABOVE NR 3 PYLON FWD INBOARD OF THRUST LINK CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME I. COMPLIED WITH FEDEX EA 1-5750-76815, WINGS RT WING - LOWER FORWARD PANEL ASSEMBLY - CORRODED. 2L73 4F RTA22WE 20040816000442004081600044NM 2004 8 16 04FDEA02304 120040730A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING, THRU FUEL TANK ACCESS PANEL CUTOUT 535BT, UPPER STRINGER NR 12, STRINGER END FOUND WITH CRACK OF ABOUT 10 INCHES IN LENGTH. REPAIR CARRIED OUT AT LT WING FUEL TANK ACCESS PANEL CUT-OUT 535BT, UPPER STRINGER NR 12 AS PER SRM 57-20-00 FIG 10, VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10, VOL I AND INSTALLED REPAIR ANGLES AT LEFT HAND WING STRINGER NR 12 AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040816000492004081600049NM 2004 8 16 04FDEA02428 120040810A5320AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48470 INTERCOSTAL BETWEEN STA 1361 AND STA 1381 AT LONGERON 15R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040816000532004081600053WP 2004 8 16 04FDEA02432 120040811A5320ADA014015 PANEL DOUG MD10 MD1010F 3022112WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 FWD CARGO SUMP PNL STA 940-960 CRACKED LT SIDE. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE. 2L73 4F RTA22WE 20040816000562004081600056NM 2004 8 16 0401146309 120040705A2530 COFFEEMAKER BOEING747 747451 1384940NM NR 1 GALLEY SMOKE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01669US 24224 DURING FLIGHT, THE NR 2 COFFEEMAKER IN THE NR 1 GALLEY STARTED SMOKING. PULLED CIRCUIT BREAKER AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED COFFEEMAKER. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040816000632004081600063NM 2004 8 16 04FDEA02221 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 3 INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.187 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816000782004081600078NM 2004 8 16 SWAA042320 120040812A3350700366 BALLAST BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 DURING SCHEDULED HC1 CHECK, FOUND RIGHT OVERWING EMERGENGY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20040816000812004081600081 2004 8 16 SWAA042323 420040812A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29763SW 27877 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040816000842004081600084NM 2004 8 16 AWXA200400862 120040728A5320654583471 STRAP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN STRAP ON BOTTOM OF BEAM AT BS 312, RBL 33, WL 200. CRACK IS ENTIRE WIDTH OF STRAP; STOP DRILL IS NOT REQUIRED. FABRICATED A REPAIR PLATE AND INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204 PG 214 - 219. 2L72 4F RTA16WE 20040816000922004081600092NM 2004 8 16 SWAA042319 120040812A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 791, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040816001032004081600103NM 2004 8 16 2004UALA00593 120040617A2841 INDICATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUEL QTY INACCURATE A UALAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 WP29399UA 24674 DIVERTED TO COS DUE TO INOP FUEL GAUGE. CREW REPORTED UNEVEN FUEL LOAD WITH EQUAL FUEL FLOW. FOUND 340 LBS DIFFERENCE BETWEEN THE DRIP STICK VALUE AND THE LEFT MAIN FUEL QUANTITY INDICATION SYSTEM. CALIBRATED NR 1 AND NR 2 FUEL QUANTITY INDICATION SYSTEMS. 2L72 4F4 FRTA16WE E2GL 20040816001092004081600109WP 2004 8 16 04FDEA01926 120040703A5754 TRACK DOUG DC10 DC1030 3023501WP NR 9 SLAT CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT WING LOWER SURFACE, LEADING EDGE DIRECTLY INBOARD OF NR 9 SLAT DRIVE TRACK IS CHAFED. BLENDED AREA, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 57-55-01 FIGURE 1 PARAGRAPH 2 VOL 3 AND 57-00-01 VOL I FIG 1A, PARAGRAPH 5. FABRICATED AND INSTALLED OUTER SLAT SKIN REPAIR IAW DC10 SRM 57-10-00 VOL I FIGURE 30 PARAGRAPH 1-5 AND 107. 2L73 4F A22WE 20040816001282004081600128NM 2004 8 16 04FDEA02197 120040727A5320 DOUBLER DOUG MD11 MD11 3023602NM ZONE 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CENTER LANDING GEAR ZONE 146 LEFT HAND SIDE WALL STA 1380 DOUBLER CRACKED.REMOVED AND REPLACED WITH NEW DOUBLER AS PER SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040816001312004081600131NM 2004 8 16 04FDEA02200 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7- 5000. 2L73 4F RTA22WE 20040816001382004081600138NM 2004 8 16 04FDEA02204 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 18 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79803, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 18L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001452004081600145NM 2004 8 16 04FDEA02211 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 1 ACTUATOR INBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001472004081600147EU 2004 8 16 2004UALA00594 120040620A3297 WIRE HARNESS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 BRAKE FAILED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29466UA 1343 DURING FLIGHT RECEIVED LOST NR 1 BRAKE SYSTEM ECAM MSG. PRECAUTIONARY LANDING. AIRCRAFT TOWED TO GATE & THE PROBLEM WAS ADDRESSED. ON SUBSEQUENT FLIGHT THE SAME SCENARIO OCCURRED. WIRING HARNESS FAILED DUE TO SHORT TO GROUND FROM FRETTING. REPLACED WIRING HARNESS. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040816001532004081600153NE 2004 8 16 2004UALA00601 220040621A7261 ENGINE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 1 LEAKING A UALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29791UA 26933 NR 1 ENGINE SHUT DOWN DUE TO LOSS OF OIL QUANTITY/PRESSURE. NR 2 BEARING FAILED. THIS IS THE MAIN THRUST BEARING SUPPORTING THE N2 ROTOR. BEARING CAGE IS FRACTURED. ALL BALLS ARE HEAVILY SPALLED AND "SQUARED OFF". OUTER RACE RIVET PIN STILL INSTALLED. OUTER RACE HAS NOT SPUN. CRACK IN THE SUPPORT THROUGH ONE OF THE RIVET PIN HOLES, ADJACENT TO THE RIVET PIN. INNER RACE HALVES ARE FRICTION WELDED TOGETHER. NR 2 REAR CARBON SEAL (C/S) DISTRESSED. PINS BENT. OIL RESIDUE ON REAR SIDE OF SUPPORT. NR 2 FRONT C/S, NR 1 C/S, AND NR 1 & 1.5 BEARINGS IN FAIRLY GOOD CONDITION. 2L72 4F4 FRTT0001SE E46NE 20040816001682004081600168NM 2004 8 16 2004UALA00607 120040622A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 FRAME DENTED STA 1580 ABOVE STR 25L ON INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH A NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20040816001702004081600170NM 2004 8 16 2004UALA00609 120040623A29201211233005 ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE RAT FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 RAT FAILED MANUAL DEPLOY OPS CHECK. RAT ACTUATOR FAILED AND WAS POPPING THE CIRCUIT BREAKER. REPLACED ACTUATOR. DURING ACTUATOR REPLACEMENT, FOUND BENT BLADE. REPLACED HUB ASSY. 2L72 4F4 FRTA2NM E17NE 20040816001782004081600178EA 2004 8 16 HNAA0400061 120040625A3260858601 PSEU DHAV DHC8 DHC8311 1386006EA MLG INDICATOR DAMAGED A HNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA07327EN 261 NOSE GEAR AND NOSE GEAR DOOR ADVISORY LIGHT & GEAR UNSAFE LIGHT CYCLED 4 TIMES WHILE AIRBORNE WITH GEAR HANDLE CYCLED UP. INSPECTED NOSE GEAR SENSORS AND PERFORMED NEAR, FAR TEST, NO DEFECTS NOTED. REMOVED AND REPLACED PSEU, SYSTEM TEST. EVALUATION FLIGHT CHECK GOOD. 2H72 4T RTA13NM 20040816001802004081600180NM 2004 8 16 2004UALA00615 120040627A7722 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 EGT ILLUMINATED A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29834UA 1420 FLIGHT DIVERTED DUE TO NR 2 EGT OVERTEMP MESSAGE. BLEED VALVE CHECK FOUND 4 LOOSE SCREWS AT BASE OF 10TH STG BLEED VALVE SOLENOID . INTERMITTENT BLEED VALVE OPEN WOULD GIVE OVERTEMP INDICATION. TIGHTENED SCREWS. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040816001902004081600190NM 2004 8 16 04FDEA01867 120040628A5753ARC4125502 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL I. 2L73 4F RTA22WE 20040816001932004081600193 2004 8 16 P5CA0401109 420040626A342325912011911 COUPLER BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE COMPASS DAMAGED A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23355MC 23395 CAPTAIN COMPASS SYSTEM WOULD NOT SYNC. REPLACED COMPASS COUPLER, OPS CHECK NORMAL AS PER AMM 34-21-00. 2L74 4F4 FRTA20WE E23EA 20040816001952004081600195NM 2004 8 16 04FDEA02226 120040728A5753 VANE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RIGHT HAND WING INBOARD FLAP. FLAP VANE INBOARD TEE FITTING AFT HOLE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOLUME II. ORIGINAL DIAMETER= 0.876, FINAL DIAMETER= 0.8784. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER FEDEX EA NR 1-5750-80312, WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP VANE - INBOARD TEE FITTING BORES - CORROSION REPAIR. 2L73 4F RTA22WE 20040816001962004081600196WP 2004 8 16 GTIA040663 120040619A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FOUND LEFT INBOARD SEAT TRACK STATION 200-1309 IS CORRODED AND GOUGED ALONG ENTIRE LENGTH. REMOVED CORROSION STATION 200-236 IS OUT OF LIMITS. MATERIAL LOSS AT STATION 948-1231 IS OUT OF LIMITS. REMOVED SEAT TRACKS FROM STATION 200-250. REMOVED LEFT INBOARD SEAT TRACK STATION 937-1231. INSTALLED SEAT TRACK LEFT INBOARD FS 200 TO 245. INSTALLED SEAT TRACK LEFT INBOARD STATION 937-1231. (M) 2L72 4F A6WE 20040816001972004081600197WP 2004 8 16 GTIA040664 120040620A5711 FRAME DOUG DC9 DC982 3022082WP WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND LOWER FIXED LEADING EDGE COMPARTMENT XFS 330 LEADING EDGE FRAME CRACK. STOP DRILL CRACK AT FORMER. FABRICATED 3 AND DRILLED REPAIR FORMER. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20040816001982004081600198WP 2004 8 16 GTIA040665 120040623A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND 20 INCH CREASE AT FS 617 BETWEEN LONGEORN 22 AND 23R, CREASE IS IN THE CONTROLLED RVSM AREA AND MUST BE REPAIRED. CUT OUT DAMAGED SKIN BETWEEN L22R-L26R STATION 586-636 SIZE, 25 INCH BY 50 INCH. FABRICATED NEW SECTION OF SKIN. DOUBLERS AND FINGER DOUBLER. INSTALLED SKIN SEC, FINGER DOUBLER, DOUBLERS. (M) 2L72 4F A6WE 20040816001992004081600199WP 2004 8 16 GTIA040666 120040625A5320 BRACKET DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND FORWARD PIT DOOR AFT LOWER INTERNAL EDGE BRACKET CRACKED. REMOVED CRACKED BRACKET. FABRICATED BRACKET. INSTALLED NEW BRACKET. (M) 2L72 4F A6WE 20040816002012004081600201WP 2004 8 16 GTIA040668 120040715A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FLL - FOUNF L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F A6WE 20040816002022004081600202EU 2004 8 16 SIMA200418803 120040609A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21396AE 340B396 ABI - AIRCRAFT ARRIVED FOR MBV INSPECTION AND REPAIR OF HAIL DAMAGE. DENT FOUND AT FS 339 SL 1501 WAS BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 34SDS007205 PARA 1.3.2 DATED 6-7-2004. (M) 2L72 4T RTA52EU 20040816002032004081600203EU 2004 8 16 SIMA200418810 120040610A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21396AE 340B396 ABI - AIRCRAFT ARRIVED FOR MBV INSPECTION AND REPAIR ON HAIL DAMAGE. DENT ON TOP SKIN FS 439.5 SL 1603 WAS FOUND BEYOND SRM LIMITS. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007205 PARA 1 DATED JUNE 7, 2004. (M) 2L72 4T RTA52EU 20040816002042004081600204EU 2004 8 16 SIMA200418814 120040604A53117252814117 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21384AE 340B384 DURING AN MBV INSPECTION A PREVIOUS REPAIR TO FRAME 258 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE CORRODED PREVIOUS REPAIR AND EXTENDED THE EXISTING CUTOUT TO COMPLETELY REMOVED THE CORROSION. FABRICATED A DOUBLER AND TWO TRIPLERS AND FILLER. REPAIR DONE IAW SAAB SRM, 72LKS 3079, REV 43, 53-70-30 AND STANDARD SRM PRACTICES. (M) 2L72 4T RTA52EU 20040816002052004081600205WP 2004 8 16 GTIA040672 120040715A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F A6WE 20040816002072004081600207WP 2004 8 16 GTIA040660 120040621A5711 FRAME DOUG DC9 DC982 3022082WP LT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND LT WING FIXED LEADING EDGE COMPARTMENT XFS 267 TWO EACH, FRAME CRACKED. STOP DRILLED CRACKS. FABRICATED TWO REPAIR DOUBLER. INSTALLED TWO FORMER REPAIR DOUBLER AND L-ANGLE. (M) 2L72 4F A6WE 20040816002092004081600209 2004 8 16 GTIA040671 420040718A2565 LANYARD DOUG DC9 DC981 3022081WP L1 DOOR SLIDE INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FLL - FOUND L1 DOOR LANYARD EVAC SLIDE BROKEN. REMOVED AND REPLACED LANYARD EVAC SLIDE AT L1 DOOR. (M) 2L72 4F A6WE 20040816002102004081600210WP 2004 8 16 GTIA040661 120040702A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE SHEARED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND G1 FORWARD INBOARD MOUNT NUT PLATE SHEAREDON INSTALLATION. REMOVED FLOORBOARD AT OUTBOARD STATION 160-200. FLOORBOARD HAS EXTENSIVE DELAMINATION. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M) 2L72 4F A6WE 20040816002112004081600211WP 2004 8 16 GTIA040662 120040623A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND EXISTING REPAIR AT FS 427 BETWEEN LONGERONS 18 AND 20R REQUIRES TO BE REPLACED WITH DC9/MD80 SRM 53-05 FIG 105 REPAIR. INSTALLED REPAIR NO LONER MEETS REQUIREMENTS FOR REPAIR AREA. REMOVED EXISTING REPAIR DOUBLER. FABRICATED DOUBLER AND TRIPLER. INSTALLED DOUBLER AND TRIPLER. (M) 2L72 4F A6WE 20040816002122004081600212SO 2004 8 16 SIMA200418602 120040703A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21650AE 145417 ORD - FLT 4431 - CREW REPORTED A HEAVY OZONE ODOR IN COCKPIT AFTER LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION IAW WORK CARD 05-200-00. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040816002142004081600214SO 2004 8 16 SIMA200417701 120040622A573014567011 SKIN EMB 145 EMB145LR 3260212SO LT WING CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21624AE 145111 DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND IN THE LEFT WING LOWER TRAILING EDGE SKIN. A DOUBLER REPAIR WAS COMPLETED IAW ENGINEERING ORDER EM 57MR-123R6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040816002152004081600215WP 2004 8 16 GTIA040669 120040714A261259585701 FIRE LOOP DOUG DC9 DC983 3022083WP RT ENGINE MALFUNCTIONED A GTIAK NONE N FALSE WARNING ININSP/MAINT 1 GL23834NK 49847 RT ENGINE B-LOOP ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE FIRE LOOP. (M) 2L72 4F RTA6WE 20040816002172004081600217EU 2004 8 16 SIMA200418812 120040613A53117253819007 FRAME SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21396AE 340B396 ABI - DURING A MBV INSPECTION, A HOLE WAS FOUND ON GALLEY FRAME 225 KICKPLATE. PERFORMED CUTOUT OF THE DAMAGE AREA. FABRICATED A FILLER TWO SHIMS AND TWO DOUBLERS. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 53-60-50, 51-40-40, 53-70-30 AND 51-40-21. (M) 2L72 4T RTA52EU 20040816002192004081600219EU 2004 8 16 SIMA200418101 120040628A21106071T20P16 CONTROL UNIT SAAB SF340 340B 7860101EU NR 2 ENGINE FAILED A SIMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW21261AE 340B261 DFW - FLT 3307 - ABORTED TAKEOFF, DUE TO NR 2 ENGINE AUTO FEATHERED ON TAKEOFF ROLL. TORQUE GAUGE WENT TO ZERO AND PROP GAUGE WENT TO 400 RPM. REPLACED NR 2 DIGITAL ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040816002202004081600220WP 2004 8 16 GTIA040635 120040601A2420 CSD DOUG DC9 DC983 3022083WP NR 2 OVERTEMP A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 NR 2 CSD WENT TO YELLOW STARTED APU DISCONNECTED CSD IN FLT. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F RTA6WE 20040816002212004081600221NE 2004 8 16 SIMA200417702 220040624A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 FAILED A SIMAA UNSCHED LANDING JYJWARNING INDICATION ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SW21901AE 340B401 GEE785623 LAX - FLT 3100 - DURING CRUISE FILGHT, RIGHT CHIP DETECTOR LIGHT ILLUMINATED AND WENT OUT SEVERAL TIMES. FORTY MINUTES INTO THE FLIGHT LIGHT ILLUMINATED AND STAYED ON. TEN MINUTES LATER A LOUD BANG WAS HEARD TOGETHER WITH OVER TEMP LIGHT COMING ON. CHECKLIST WAS COMPLIED WITH AND AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20040816002222004081600222SO 2004 8 16 SIMA200417202 120040619A276014533022409 CONTROL UNIT EMB 135 EMB135LR 3260305SO SPOILERS INOPERATIVE A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21738NR 145401 NAS - FLT 4739 - DURING TAKEOFF ROLL THRUST LEVERS AT THRUST SETTING, SPOILER DEPLOYED UNCOMMANDED. CREW REPORTED A TAKEOFF MISCONFIG MESSAGE AND WHLE TAXIING BACK TO GATE RECEIVED DAU 1 MISCOMPARE. MAINTNENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT IAW EMB MM. OPS CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040816002232004081600223WP 2004 8 16 GTIA040634 120040622A7120K22199SA31 ISOLATOR DOUG DC9 DC983 3022083WP NR 1 OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 MCO - FOUND FORWARD LOWER VIBRATION ISOLATOR OUT OF LIMITS, NR 1 ENGINE. INSTALLED FORWARD LOWER VIBRATION ISOLATOR. (M) 2L72 4F RTA6WE 20040818000012004081800001EU 2004 8 18 ASOA04485 120040706A33500341519 FUSE AEROSPATR72 ATR72 EU EMERGENCY LIGHT BLOWN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11643AS 413 DURING A GROUND INSPECTION IN VPS, THE AFT EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE EMERGENCY BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040818000042004081800004NM 2004 8 18 UIEA200400132 120040728A541465B904511 SKIN BOEING747 7472D7B 1384803NM NR NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 DURING SCHEDULE MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248, NR 2 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVE THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235 TO NACELLE STATION 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20040818000052004081800005EU 2004 8 18 A6WA200460027 120040717A5320HC537H0551000 ANGLE BAC 146 146200A 1500266EU INTERCOSTAL CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND CORROSION ON INTERCOSTAL AT CETNER JOINT PLATE 80 INCHES FROM DOOR 1L. REPLACED ANGLE, IAW BAE SRM 51-42-00 AND 51-23-00. (M) 2H74 4F A49EU 20040818000062004081800006NM 2004 8 18 USAASB04094 120040717A3350 SIGN BOEING737 737401 1384701NM SEAT 11C MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US 23885 THE EMERGENCY EXIT SIGN WAS MISSING AT SEAT 11C. MAINTENANCE REPLACED THE SIGN, CHECKS OK. (M) 2L72 4F RTA16WE 20040818000072004081800007NM 2004 8 18 USAASB04088 120040707A3350110049 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19528AU 24410 CLT - MAINTENANCE REPORTED THE LOWER EMERGENCY EXIT SIGNS AT THE L1 AND R1 DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040818000092004081800009NM 2004 8 18 USAA040346 120040715A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US49270 23237 CLT - FOUND SKIN CRACKED 2.75 INCH, STATION 727E, STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040818000102004081800010NM 2004 8 18 UIEA200400131 120040728A541465B941004 SKIN BOEING747 7472D7B 1384803NM NR 1 NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 DURING SCHEDULE MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STATION 248, NR 1 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVE THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STATION 235 TO NAC STATION 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20040818000112004081800011NM 2004 8 18 USAABB04053 120040618A4920GTCP331200ER APU BOEING757 7572B7 1384964NM APU BAY INOPERATIVE A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19610AU 27122 PIT - FLT 642 - EN ROUTE, RIGHT IDG WAS DISCONNECTED AND THE APU WAS OPERATING. CREW RECEIVED THE E/M 'APU OIL QTY.' FLIGHT DIVERTED TO PIT AND LANDED. UPON LANDING, THE APU PERFORMED AN AUTO SHUTDOWN. MAINTENANCE REPLACED SEVERAL PARTS, HOWEVER THE APU CONTINUED TO FAULT DUE TO LOW OIL QUANTITY. THE APU WAS REPLACED. (M) 2L72 4F RTA2NM 20040818000132004081800013NM 2004 8 18 USAA040347 120040714A5330 SKIN BOEING737 737301 1384611NM FS 727D CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US 23237 CLT - FOUND SKIN CRACKED .625 INCH, FS 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040818000142004081800014EU 2004 8 18 A6WA200460026 120040727A3520 BOTTLE BAC 146 146200A 1500266EU PAX OXYGEN SYS DISCHARGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 FOUND FORWARD CABIN BULKHEAD PASSENGER OXYGEN BOTTLE EMPTY. REMOVED AND REPLACED BOTTLE. (M) 2H74 4F A49EU 20040818000152004081800015SO 2004 8 18 SIMA200419406 120040710A3150 WARNING LIGHT EMB 145 EMB145LR 3260212SO COCKPIT WINDOW FALSE ACTIVATIONA SIMAK NONE N FALSE WARNING ININSP/MAINT 1 SW21620AE 145102 ON CLIMB-OUT CREW NOTICED YELLOW TAB INDICATING CAPTAINS DV WINDOW OPENED. CREW RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF WINDOW WITH NO DEFECTS NOTED. LOCKED WINDOW AND RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4T RTT00011AT 20040818000162004081800016NM 2004 8 18 USAA040343 120040711A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19409US 23879 PIT - FOUND SKIN CRACKED 3 INCHES, BETWEEN STATION 727E AND 727F AT S22L ON FUSELAGE SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040818000202004081800020NM 2004 8 18 USAA040351 120040721A5320 STIFFENER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US50302 23935 PIT - FOUND CHANNEL STIFFENER CORRODED 1 INCH BY 2 INCH AREA, BS 1016 ABOVE AND BETWEEN STRINGER 27R AND 27L. (M) 2L72 4F RTA16WE 20040818000212004081800021NM 2004 8 18 USAA040348 120040327A5313 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US44758 23558 FOUND STRINGER CORRODED TWO AREAS, 1 INCH BY 6 INCHES AND 1 INCH BY 4 INCHES, FS 1016-1022 FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED STIFFENERS AND INSTALLED DOUBLERS AND SPLICES PER SRM 53-80-08 AND BOEING DWG PL 65C28106. (M) 2L72 4F RTA16WE 20040818000242004081800024NM 2004 8 18 USAA040341 120040707A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT FOUND WEB CRACKED 2 INCHES, STATION 1040, BL 0, 9 RIVETS UP FROM CENTER OF AFT PRESSURE DOME. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-80-08. (M) 2L72 4F RTA16WE 20040818000252004081800025NM 2004 8 18 USAA040352 120040720A5330 SKIN BOEING737 7373B7 1384580NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US50417 23319 FOUND SKIN CRACKED 2.5 INCHES, 5 INCHES FORWARD OF BS 500 RT AND 1 INCH ABOVE S-15R. (M) 2L72 4F RTA16WE 20040818000262004081800026EA 2004 8 18 A6WA200440047 120040419A5246 DOOR CNDAIRCL600 CL6002B19 1900309EA GROUND SERVICE OPEN A A6WAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 GL31465AW 7893 DURING CLIMB-OUT, EXPERIENCED EXTREMELY LOUD NOISE FROM NOSE OF AIRCRAFT. RETURN TO FIELD. FOUND GROUND SERVICE DOOR OPEN. INSPECTED AND NO DAMAGE NOTED. CLOSED AND SECURED DOOR. NO FURTHER OCCURRENCES OR DEFECTS. (M) 2L72 4F RTA21EA 20040818000272004081800027EA 2004 8 18 A6WA200440095 120040626A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 FOUND FLOOR SILL PLATE AT CARGO DOOR ENTRANCE IS CRACKED. CUT OUT DAMAGED SECTION OF FLOOR SILL SECTION AND INSTALLED FABRICATED REPAIR SECTION OF FLOOR SILL AND INSTALLED FABRICATED SPLICE DOUBLER IAW BRAS EO 601R-53-5095. (M) 2L72 4F RTA21EA 20040818000312004081800031EU 2004 8 18 A6WA200460025 120040717A1430HC551B008600 BOLT BAC 146 146200A 1500266EU ELEVATOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND CORROSION ELEVATOR HINGE A-FRAME ATTACHMENT BOLTS TWO EACH. REPLACED NEW. (M) 2H74 4F A49EU 20040818000322004081800032EU 2004 8 18 A6WA200460029 120040510A5313 STRINGER BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND CORROSION ON CENTER LINE STRINGER IN FORWARD CARGO PIT BETWEEN FORWARD AND AFT RADIO ALT ANTENNAS. MAINTENANCE REPLACED STRINGER WITH MANUFACTURED REPAIR PART IAW SRM. 2H74 4F A49EU 20040818000332004081800033EU 2004 8 18 A6WA200460028 120040510A5320 FLOOR SUPPORT BAC 146 146200A 1500266EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND CORROSION ON FLOOR SUPPORT MEMBER ADJACENT TO FLOORBEAM 15.52 INCHES FROM DOOR 1L. MAINTENANCE REPLACED JOINT PLATE WITH MANUFACTURED REPAIR PART IAW BAE SRM 51-20 2H74 4F A49EU 20040818000342004081800034EU 2004 8 18 A6WA200460030 120040511A5320 INTERCOSTAL BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 22/23 AT STRINGER 21 RIGHT IN FORWRAD CARGO COMPARTMENT. MAINTENANCE REPLACED INTERCOSTAL IAW BAE SRM 51-23-00, 51-42-00 AND 51-43-00. (M) 2H74 4F A49EU 20040818000352004081800035NM 2004 8 18 AMTA200400089 120040123A5321 FLOOR PANEL BOEING737 73783N 13844HINM CARGO BAY CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11304TZ 30675 FOUND C2 CARGO FLOOR PANEL UNDER LOADING SYSTEM CORRODED FROM DOOR FORWARD. REMOVED AND REPLACED CARGO FLOOR PANEL. REINSTALLED ON A/C IAW 737 AMM 25-52-10-4. SEALED FITTINGS IAW 737 AMM 20-30-1 1-2. COATED PANEL WITH ABRASION PROTECTIVE COATING. (M) 2L72 4F RTA16WE 20040818000362004081800036NM 2004 8 18 AMTA200400127 120040204A5321 FLOOR PANEL BOEING737 73783N 13844HINM CARGO BAY CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11303TZ 28648 FOUND C2 CARGO PIT, AREA UNDER CARGO LOADING SYSTEM, PARTICALLY BY DOOR HAS CORROSION ON FLOOR STATION 727J TO 787. REMOVED AND REPLCED C-2 PIT FLOOR PANEL REF 737 AMM 25-51-1 0-4. (M) 2L72 4F RTA16WE 20040818000392004081800039SO 2004 8 18 SIMA200419706 120040706A532014522461011 PLATE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE 145328 DURING A CPCP INSPECTION, MAINTENANCE FOUND THE CABIN INTERIOR STRUCTURE FORWARD RIGHT SERVICE DOOR SIDE JUNCTION PLATE FOR FLOORBEAM CONNECTION HAS CORROSION. INSTALLED NEW JUNCTION PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818000422004081800042EU 2004 8 18 USAASA04069 120040705A21501303A000003 FLOW VALVE AIRBUS320 A320214 3930316EU NR 2 PACK FAILED A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19102UW11936 0844 GJT - FLT 82 - EN ROUTE SFO-PHL, WITH THE NR 2 PACK ON MEL, A NR 1 PACK FAULT OCCURRED. PRESSURIZATION WAS LOST AS A RESULT. FLIGHT MADE A RAPID DESCENT TO 10,000 FEET THE DIVERTED TO GJT DUE TO TERRAIN CONTRAINTS. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 PACK FLOW CONTROL VALVE. OPS CHECKED BOTH THE NR 1 AND NR 2 PACK SYSTEMS. OPS CHECKS OK. (M) 2L72 4F RTA28NM 20040818000442004081800044EU 2004 8 18 USAASA04066 120040703A3350321431 BATTERY AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19161UW 1403 DURING THE EMERGENCY LIGHTS TEST, A MESSAGE DISPLAYED INDICATING THAT THE LEFT EXIT EMERGENCY POWER SUPPLY UNIT BATTERY HAD FAILED. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN THE LEFT EXIT POSITION. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040818000452004081800045NM 2004 8 18 USAASB04085 120040701A3260BR20AXH5V3 RELAY BOEING737 7373B7 1384580NM NLG STUCK A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19532AU 24479 ON CLIMB-OUT FROM CLT, EN ROUTE TO DCA, CREW RECEIVED A RED NOSE GEAR LIGHT THA WOULD NOT EXTINGUISH WHEN THE GEAR WAS RETRACTED. AFTER SEVERAL ATTEMPTS TO EXTINGUISH THE RED LIGHT, CREW FOLLOWED PROCEDURES AND LOWERED THE GEAR, RECEIVING NORMAL GEAR INDICATIONS. FLIGHT RETURNED TO FILED AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE R374 NOSE GEAR LATCHING RELAY STUCK IN THE GEAR DOWN CONFIGURATION. REMOVED & REPLACED RELAY. PERFORMED GEAR SWING. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20040818000462004081800046NM 2004 8 18 USAASB04086 120040705A3260655825029 CIRCUIT CARD BOEING737 737301 1384611NM NLG INOPERATIVE A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19558AU 23512 DCA - FLT 2046 - AFTER TAKEOFF FROM DCA, EN ROUTE TO BOS, CREW RECEIVED BOTH THE GREEN AND RED NOSE LANDING GEAR INDICATION LIGHTS WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION. IN ASSOCIATION WITH QUICK REF HANDBOOK, CREW EXTENDED GEAR AND RECEIVED A NORMAL GEAR INDICATOIN OF ALL GREEN LIGHTS. FLIGHT RETURNED TO FIELD DCA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED LANDING GEAR POSITION AND WARNING CHECK PER MM 32-61-00 AND NOSE LANDING EXTENSION AND RETRACTION CHECK PER MM 32-33-00. ALSO, ACCOMPLISHED NOSE LANDING GEAR INDICATION SYSTEM TROUBLESHOOTING PER MM CHAPTER 32. REMOVED AND REPLACED NOSE GEAR RED LIGHT CIRCUIT CARD M983. PERFORMED GEAR SWING. 2L72 4F RTA16WE 20040818000472004081800047NM 2004 8 18 USAASB04030 120040315A291065C268101027 TUBE BOEING737 7373B7 1384580NM A-HYD SYSTEM LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19393US 23315 AFTER TAKEOFF FROM CLT, THE RIGHT MLG WOULD NOT RETRACT. THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESURE LIGHT WAS ALSO ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES, SELECTED THE HYDRAULIC PUMP TO OFF AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GATE ON OWN POWER. MAINTENANCE FOUND THE RT MAIN LANDING GEAR 'UP' TUBE ASSEMBLY SPLIT OPEN. REPLACED TUBE ASSEMBLY. CHECKED A-SYSTEM ENGINE DRIVEN PUMP CASE DRAIN AND PRESSURE FILTERS. BOTH CHECKED CLEAN. SERVICED HYDRAULIC SYSTEM. OPS CHECK AND LEAK CHECK GOOD. (M) 2L72 4F RTA16WE 20040818000492004081800049EU 2004 8 18 SIMA200419604 120040625A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21344SB 340B344 ABI - DURING AN HMBV INSPECTION, A DENT WAS DISCOVERED ON CARGO AREA FRAME 658.5. RECONTOURED THE DAMAGE AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED AN ANGLE DOUBLER AND INSTALLED. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007303 PARA 1 DATED JUNE 24, 2004. (M) 2L72 4T RTA52EU 20040818000512004081800051EU 2004 8 18 SIMA200419608 120040704A55127255150522 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21386AE 340B386 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. THE RIGHT HORIZONTAL STABILIZER TOP SKIN PANEL, HAIL DAMAGE WAS BEYOND SRM LIMITS. REMOVED EXISTING TOP SKIN PANEL. PREPARED NEW RIGHT HORIZONTAL TOP SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-40-21, 22, 23, 24, 51-20-50 AND 51-20-56. (M) 2L72 4T RTA52EU 20040818000522004081800052NM 2004 8 18 USAASB04089 120040711A26976131508551 WIRE HARNESS BOEING737 737301 1384611NM NR 2 ENGINE INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19574US 23739 BOS - FLT 1249 - FLIGHT DEPARTED PVD, EN ROUTE TO DCA, WITH THE NR 2 ENGINE 'A' FIRE LOOP ON MEL 26-2A. DURING CLIMB-OUT, THE NR 2 ENGINE 'B' FIRE LOOP FAULT LIGHT ILLUMINATED AND REMAINED ON. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE SOFT CORE HARNESS. OPERATIONAL CHECK GOOD. CLEARED MEL 26-2A. (M) 2L72 4F RTA16WE 20040818000542004081800054SO 2004 8 18 SIMA200419404 120040709A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21622AE 145108 DFW - FLT 3533 - FOUND EMERGENCY EXIT LIGHT ABOVE GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT LOCATOR IAW EMB MM 33-50-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040818000562004081800056WP 2004 8 18 GTIA040644 120040622A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FOUND CABIN FLOOR STATION 769-788 BL 0 INTERCOSTAL UPPER FLANGE IS CRACKED AROUND FASTENER HOLES WITH MATERIAL MISSING AT 2 LOCATIONS. REMOVED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL. INSTALLED INTERCOSTAL. (M) 2L72 4F A6WE 20040818000572004081800057NM 2004 8 18 USAASB04090 120040712A2781189929 SENSOR BOEING737 7373B7 1384580NM NR 4 LE FLAP MALFUNCTIONED A USAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA19515AU 23701 PIT - FLT 1058 - AFTER TAKEOFF FROM PIT, EN ROUTE TO PVD, CREW REPORTED THE NR 4 LEADING EDGE FLAP WOULD NOT RETRACT AND THE LEADING EDGE FLAP TRANSIT AMBER LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND CORROSION ON TARGET FOR NR 4 LEADING EDGE FLAP FOR RETRACTED POSITION. CLEANED CORROSION AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF FLAP SYSTEM. NO FAULTS NOTED. HOWEVER, THE PROBLEM REOCCURRED ON THE NEXT FLIGHT FROM PIT TO PVD. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP DOWN SENSOR PER MM 27-88-11. OPS CHECK OF SYSTEM GOOD. (M) 2L72 4F RTA16WE 20040818000592004081800059NE 2004 8 18 SIMA200419407 220040710A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED A SIMAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SW21392AE 340B392 GEE785527 SAN - FLT 3088 - ON TAKEOFF ROLL, CREW HEARD LOUD BAND FROM RIGHT ENGINE AND THEN EXPERIENCED YAW. TAKEOFF WAS ABORTED AND RIGHT ENGINE EXPERIENCED UNCOMMANDED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW WORK CARD 4903. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 20040818000612004081800061EU 2004 8 18 SIMA200419606 120040705A53117252813485 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21386AE 340B386 ABI - DUIRNG AN MBV INSPECTION, THE CARGO FRAME AT STATION 677 WAS FOUND DENTED. PERFORMED A CUTOUT OF THE DAMAGE AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007323 PARA 1, DATED JUNE 29, 2004. (M) 2L72 4T RTA52EU 20040818000642004081800064EU 2004 8 18 SIMA200419612 120040708A53117252813007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21394AE 340B394 ABI - DUIRNG AN MBV INSPECTION, GALLEY AREA FRAME AT FS 231 FOUND TO BE CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE CORRODED AREA. FABRICATED A FILLER, DOUBLER AND SHIMS. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079, REV 43, CHAPTER 53-70-30 FIGURE 207. (M) 2L72 4T RTA52EU 20040818000652004081800065EU 2004 8 18 SIMA200419613 120040706A531172253813007 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21394AE 340B394 DURING AN MBV INSPECTION, FOUND GALLEY ARE FRAME AT STATION 258 CORRODED ON PREVIOUS REPAIR. REMOVED EXISTING SHIM AND BLENDED THE FRAME. PERFORMED AN EDDY CURRENT AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A NEW FILLER FOR REPAIR. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-7040 AND 53-70-30. (M) 2L72 4T RTA52EU 20040818000662004081800066EU 2004 8 18 SIMA200419614 120040705A53117252814485 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21394AE 340B394 ABI - DUIRNG AN MBV INSPECTION, FOUND CARGO FRAME AT FS 677 HAD TWO DENTS. RECONTOURED THE TWO DENTS AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS007339, PARA 3, DATED JULY 2, 2004. (M) 2L72 4T RTA52EU 20040818000702004081800070SO 2004 8 18 SIMA200418604 120040704A335066368 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21633AE 145148 SDF - FLT 4087 - DURING PREFLIGHT CREW NOTED EMERGENCY LIGHTS WILL NOT TURN ON AND ILLUMINATE. AIRCRAFT WAS INSPECTED AND FERRIED TO ORD FOR REPAIR. MAINTENANCE PERFORMED OPS CHECK OF EMERGENCY LIGHTS. ALL WERE OPERATING EXCEPT FOR THE THIRD FLOOR LIGHT STRP. THE LIGHT WAS DEFERRED AND AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040818000712004081800071SO 2004 8 18 SIMA200420101 120040716A3411 PITOT SYSTEM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL BOTH CONTAMINATED A SIMAO OTHER RXJPARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW21702AE 145164 145164 DUIRNG CRUISE FLIGHT, NR 1 ENGINE LOST POWER, REGAINED POWER TWO TIMES, THEN RAN NORMALLY. AFTER LANDING NR 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FAULT ISOLATION MANUAL AND FOUND WATER IN BOTH PITOT SYSTEMS. DRAINED PITOT STATIC SYSTEM. ENGINE OPERATIONAL CHECKS GOOD. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20040818000732004081800073NM 2004 8 18 GTIA040657 120040709A3350 CONTACTOR DOUG MD80 MD83 3023681NM BATTERY LOOSE A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23822NK 49392 DTW - FOUND LEFT AND RIGHT FORWARD PLUG DOOR EMERGENCY LIGHT INOPERATIVE. CLEANED BATTERY CONTACTS. (M) 2L72 4F RT 20040813001002004081300100EU 2004 8 13 2004UALA00690 120040724A2910 HYDRAULIC SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYSTEM FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29445UA 826 RETURN TO FIELD DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. LEAKING BYPASS VALVE, LOSS OF HYDRAULIC FLUID. REPLACED THE NOSE LANDING GEAR DOOR OPENING BYPASS VALVE. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813001012004081300101EU 2004 8 13 2004UALA00691 120040716A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29428UA 523 EMERGENCY LIGHT TEST FAULTED EXT LOADS FWD L. THE EPSU FAULTED. REPLACED POWER SUPPLY. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813001182004081300118NM 2004 8 13 2004UALA00662 120040714A3350362624 LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29936UA 26667 EMERGENCY EXIT PATH LIGHTING IS INOP ON THE AFT SECTION. REPLACED DEFECTIVE RIBBON. 2L72 4F4 FRTA16WE E2GL 20040813001212004081300121NM 2004 8 13 04FDEA02358 120040803A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 SEAT TRACK CROWN DAMAGED AT APPROXIMATE STA 839 RBL 8.5. TRIMMED OFF AS PER SRM 55-70-00 FIGURE 1 VOLUME I. NEW SEAT TRACK AND FABRICATED REPAIR SPLICE INSTALLED SRM 55-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20040813001412004081300141 2004 8 13 SWAA042312 420040811A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 AFT ENTRY DOOR EVACUATION SLIDE PRESS IND BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040813001552004081300155NM 2004 8 13 2004UALA00645 120040707A5610MR56194404 WINDOW BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29908UA9594 25008 RETURNED TO DEN WITH CRACKED WINDSHIELD. CAUSE UNKNOWN. WINDOW REPLACED. 2L72 4F4 FRTA16WE E2GL 20040813001562004081300156NM 2004 8 13 0401226717 120040531A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING H-CHECK FOUND CRACK IN FRAME WEB AT BS 360 S24L. REPAIRED PER EA 67-165134. 2L74 4F A20WE 20040813001822004081300182WP 2004 8 13 MWEA040118 120040706A53119911526 FRAME DOUG DC9 DC982 3022082WP FUSELAGE WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 FRAME STATION 579 FRAME FORMER FROM LONGERON 22 LEFT THROUGH 23 LEFT REQUIRES FLANGE REPAIR. FABRICATED AND INSTALLED REPAIR FORMER. 2L72 4F A6WE 20040813001852004081300185NM 2004 8 13 04FDEA01990 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK - SEAT TRACK CROWN AT STA 1020, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47.5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2. 2L73 4F RTA22WE 20040818000742004081800074 2004 8 18 GTIA040659 420040713A2565 LATCH DOUG DC9 DC982 3022082WP R1 DOOR SLIDE DIRTY A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK 48048 R1 GIRT BAR SPRING LOADED LATCHES HAVE TO BE MANUALLY MANIPULATED TO LOCK GIRT BAR IN PLACE. CLEANED AND LUBED R1 DOOR GIRT BAR LATCHES. OPS CHECK GOOD. (M) 2L72 4F A6WE 20040818000752004081800075SO 2004 8 18 SIMA200419703 120040630A532014521713005 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE 145328 DURING A CPCP INSPECTON, MAINTENANCE FOUND CORROSION ON CENTER HAT BEAM AT FRAME 20. REMOVED AND REPLACED HAT BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818000762004081800076SO 2004 8 18 SIMA200419705 120040630A532014522178005 THRESHOLD EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE 145328 SAW - DURING AN IMBV INSPECTION, MAINTENANCE FOUND THE INTERIORS STRUCTURE RIGHT SERVICE DOOR ENTRANCE THRESHOLD TO HAVE CORROSION. INSTALLED NEW RIGHT SERVICE DOOR THRESHOLD IAW EMB SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818000772004081800077WP 2004 8 18 GTIA040658 120040706A5210 HANDLE DOUG DC9 DC981 3022081WP PAX DOOR LACK OF LUBE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23818NK 48018 MAIN ENTRANCE DOORS OUTSIDE HANDLE STAYED EXTENDED WITH DOOR LOCKED, HAD IT PUSHED IN. LUBRICATED DOOR HANDLE ASSEMBLY OPS CHECK NORMAL AT THIS TIME. (M) 2L72 4F A6WE 20040818000792004081800079 2004 8 18 GTIA040640 420040704A2565 CLIP DOUG DC9 DC982 3022082WP L2 DOOR SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 RSW - FLT 689 - L2 DOOR PAX ESCAPE SLIDE 'CLIP' DISCONNECTED. RECONNECTED 'CLIP' ON SLIDE. (M) 2L72 4F A6WE 20040818000802004081800080 2004 8 18 GTIA040641 420040706A2565 LANYARD DOUG DC9 DC983 3022083WP R1 DOOR SLIDE FRAYED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 FOUND R1 SERVCE DOOR EVACUATION SLIDE COVER LANYARD ASSEMBLY CABLE FRAYED. REMOVED AND REPLACED R-1 DOOR SLIDE LANYARD ASSEMBLY. (M) 2L72 4F RTA6WE 20040818000822004081800082WP 2004 8 18 GTIA040643 120040629A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND MAIN CABIN STATION 1250 TO STATION 1155 LEFT SIDE INBOARD FLOOR PANEL HAS SEVERAL INSERTS CORROSION SOFT/MUSHEY EDGE FILLER IS MISSING. FABRICATED NEW PANEL. (M) 2L72 4F A6WE 20040818000852004081800085EU 2004 8 18 A6WA200460010 120040322A4990 SHAFT SEAL BAG BAE146BAE146200A 1500266EU APU GENERATOR LEAKING A A6WAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 GL31156TR E2156 STRONG ODOR IN COCKPIT, EYES BURNING WITH AC PACKS ON. MAINTENANCE PERFORMED PACK BURN OUT PROCEDURE. REMOVED AND REPLACED APU ASSEMBLY. (M) 2H74 4F RTA49EU 20040818000872004081800087EA 2004 8 18 ASOA04503 120040704A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY FAILED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11881AS7149 7496 DURING APPROACH INTO ATL FROM MYR, THE CREW RECEIVED AND AUXILIARY POWER UNIT FAULT, SHUTDOWN, MESSAGE WITH THE NR 1 GENERATOR DEFERRED. AN EMEGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040818000892004081800089EA 2004 8 18 ASOA04501 120040712A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT PRESSURE WALL CLIP AT FS 625 AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT PRESSURE WALL CLIP AT FS 625 AFT EQUIPMENT BAY. (M) 2L72 4F RTA21EA 20040818000912004081800091NM 2004 8 18 AMTA200400126 120040204A5321 FLOORBOARD BOEING737 73783N 13844HINM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11303TZ 28648 FOUND FLOORBOARD INBOARD OF C2 DOOR HAS CORROSION AT FORWARD END, STATION 887 TO 740 LBL 20 TO RBL 20. REMOVED AND REPLACED C-2 PIT FLOOR PANEL REF 737 AMM 25-52-10-4. (M) 2L72 4F RTA16WE 20040818000922004081800092NM 2004 8 18 AMTA200400078 120040125A2560ACREM1A MEGAPHONE BOEING737 73783N 13844HINM CABIN INOPERATIVE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11306TZ 32348 FOUND AFT CABIN MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT CABIN MEGAPHONE. (M) 2L72 4F RTA16WE 20040818001002004081800100EU 2004 8 18 SIMA200419605 120040708A53117252814417 FRAME SAAB SF340 340B 7860101EU FUSELAGE BENT A SIMAK NONE O OTHER ININSP/MAINT 1 SW21394AE 340B394 DURING AN MBV INSPECTION, FOUND CARGO AREA FRAME AT STATION 710 WAS FOUND BENT. RECONTOURED DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTON WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER. ATTACHED REPAIR IAW SAAB REPAIR STATEMENT 340SDS007364 PARA 1 DATED JULY 7, 2004. (M) 2L72 4T RTA52EU 20040818001022004081800102NM 2004 8 18 AMTA200400160 120040212A5321 FLOOR PANEL BOEING737 73783N 13844HINM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11304TZ 30675 FOUND C-2 CARGO PIT FLOOR PANEL HAS CORROSION STATION 727E TO 727J. CORROSION OUT OF LIMITS PER SRM 53-00-53-01. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW PANEL IAW AMM 51-40-02-0. (M) 2L72 4F RTA16WE 20040818001052004081800105WP 2004 8 18 GTIA040649 120040613A53209936639UI3 CHANNEL DOUG DC9 DC983 3022083WP FLOOR PANEL CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND CENTER CABIN FLOOR PANEL STATION 826-886 W CHANNELS CRACKED. REMOVED TWO CRACKED CHANNELS. INSTLALED TWO NEW CHANNELS. (M) 2L72 4F RTA6WE 20040818001102004081800110WP 2004 8 18 GTIA040645 120040702A2612G718503 CONTROL PANEL DOUG DC9 DC983 3022083WP CARGO FIRE INTERMITTENT A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FLL - FOUND CARGO FIRE AND CARGO DET LOOP LIGHT ON IN FLIGHT INTERMITTENTLY. REMOVED AND REPLACED DETECTION CONTROL PANEL. SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20040818001122004081800112WP 2004 8 18 GTIA040653 120040622A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND MAIN CABIN STATION 806 TO STATION 826, FLOOR PANEL ONE INSERT DAMAGE/CRACKS ON EDGES. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040818001132004081800113NM 2004 8 18 AMTA200400925 120040724A3350 LIGHT BOEING757 75723N 1384973NM EMERGENCY EXIT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 NM01526AT 30735 FOUND SEAT 16C EMERGENCY EXIT LIGHT IS INOPERATIVE. RECONNECTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 16. OPS CHECKS NORMAL. (M) 2L72 4F RTA2NM 20040818001142004081800114NM 2004 8 18 AMTA200400962 120040728A2613 WARNING LIGHT BOEING757 75733N 1384931NM LT ENGINE FALSE INDICATIONA AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11559TZ 32593 EICAS MSG 'ENGINE OVERHEAT' LIGHT ON INFLIGHT. RAN ENGINE AT 70 PERCENT N3, 80 PERCENT N3, 85 PERCENT N3, AND T/O POWER SETTINGS. NO FAULTS NOTED. ISOLTATED BLEED AIR SOURCE TO LEFT ENGINE ONLY, NO DEFECTS NOTED. CYCLED ANTI-ICE, NO FAULTS COULD NOT DUPLICATE AT THIS TIME. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040818001162004081800116SW 2004 8 18 HEEA096023 120040512A2822205060606003 PUMP BELL 412 412 1182202SW PWA PT6 PT6* 52043EA FUEL BOOST FAILED B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03108X 33115 DURING FLIGHT THE NR 1 BOOST PUMP FAILED. MAINTENANCE REPLACED THE NR 1 BOOST PUMP. 1G72 4U3 T H4SW E2NE 20040818001182004081800118EU 2004 8 18 TXER096035 120040417A6220704A3363321151 SPHERICAL STOP AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR WORN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09118TA 3110 MAIN ROTOR SPHERICAL STOPS WORN. 1G72 3U3 U H11EU E19EU 20040818001212004081800121NE 2004 8 18 ALGA096404 120040707A6320SB2559101 BEARING SKRSKYS76 S76C 8143008NE M/R GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03864AL69 760557 TRANSMISSION DISASSEMBLED FOR METAL CONTAMINATION, FOUND ROLLER BEARING BREAKING DOWN. REMOVED AND REPLACED BEARING. 1G72 3U NCH1NE 20040818001232004081800123SW 2004 8 18 ALGA096465 120040718A6510407340340103 DISC PACK BELL 407 407 1182206SW ALLSN 250C 250C47B GL TAIL ROTOR CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03587AL 53248 FOUND CRACKED DISC. REPLACED W/NEW PART BY FIELD MAINT. 1G71 3U3 UO H2SW E1GL 20040818001272004081800127SW 2004 8 18 ALGA096394 120040720A6510407340340103 DISC PACK BELL 407 407 1182206SW ALLSN 250B 250B* GL TAIL ROTOR CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03436AL533 53069 FOUND ONE CRACKED DISC REPLACED ASSY BY FIELD MAINT. 1G71 3U3 TO H2SW E10CE 20040818001292004081800129EU 2004 8 18 ALGA096003 120040707A6220C622A1003102 DRIVE LINK UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03514AL245 1266 FOUND WEAR PLATE DEBONDED. ASSY. REPLACED BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001302004081800130EU 2004 8 18 ALGA096028 120040708A1430C622A2006601 BOLT UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001342004081800134EU 2004 8 18 ALGA096033 120040708A1430C622A2006601 BOLT UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001382004081800138EU 2004 8 18 CX7A194J0448 120040811A2611CGAB120101 SMOKE DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CARGO BAY FALSE INDICATIONA CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03300CE81 340B184 WHEN NR 2 ENGINE STARTER WAS ENGAGED CARGO SMOKE CWP ILLUMINATED. IMMEDIATE INSPECTION OF CARGO HOLD REVEALED NO SMOKE OR FIRE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR. 2L72 4T4 TRTA52EU E8NE 20040818001402004081800140NE 2004 8 18 DHL2004804 220040812A7261 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 2 LEAKING A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO01804DH 46124 AIRCRAFT EXPERIENCED A SUDDEN LOSS OF OIL QUANTITY AND PRESSURE THAT CAUSED THE FLIGHT CREW TO PERFORM ENROUTE ENGINE SHUTDOWN OF THE NR 2 ENGINE. 2L74 4F4 FRT4A25 E2GL 20040818001412004081800141EU 2004 8 18 KBM2004F00144 120040601A21210500847 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 BLOWER MOTOR WILL NOT TURN FAN. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001422004081800142EU 2004 8 18 KBM2004F00145 120040601A2121050037 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 BLOWER MOTOR, A/C BLOWING HOT AIR. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001432004081800143EU 2004 8 18 KBM2004F00146 120040624A5340064105430 FITTING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE VHF RADIO BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 VHF RADIO, RETAINING LUG BROKEN. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001462004081800146 2004 8 18 KBM2004F00126 420040520A2312064105430 RADIO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE VHF SYS SHORTED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P729 2347 VHF RADIO SHORTS OUT. DISPLAY GOES CLEAR AND 2 NUMBERS APPEAR IN DISPLAY. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001522004081800152NE 2004 8 18 C8GA20040017 220040810A7313 O-RING BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE FUEL PUMP LEAKING A C8GAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO15801EA44568 22432 700729 IN CRUISE, NR 1 ENGINE LOST 2 QTS OF OIL EVERY 10 MINUTES. THE NR 1 ENGINE WAS SHUTDOWN AS A PRECAUTION. AN EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO AND LANDED WITHOUT INCIDENT. FOUND INLET PRESSURE LINE LEAKING. TIGHTENED LINE, OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. OIL QUANTITY DROPPED SIGNIFICANTLY AFTER TAKE OFF. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND THE NR 1 ENGINE FUEL PUMP SHAFT O-RING MISSING. INSTALLED O-RING. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040818001582004081800158EA 2004 8 18 SWIA200413688 120040811A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07410SW786 786 7066 ON SHORT FINAL WHILE RUNNING STAB TRIM, STAB AND MACH TRIM CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040818001592004081800159EA 2004 8 18 SWIA200413689 120040812A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TRIM MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW7998 7998 7279 STAB TRIM CHANEL 1 INOPERATIVE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N: 8396-3 S/N OFF: 682 2L72 4F4 FRTA21EA E15NE 20040818001612004081800161SO 2004 8 18 SWIA200413691 120040810A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07587338319 4575 120197 FLAPS INDICATE CONTROL FAULT ON OB FLAPS. REPLACED LT OB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040818001642004081800164WP 2004 8 18 0401319919 120040810A2910 LINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D15 52051NE HYD SYSTEM RUPTURED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01941N 47450 FLIGHT CREW NOTICED THE LOSS OF HYDRAULIC FLUID FROM THE RT SYSTEM WHEN THE (RUDDER CONTROL MANUAL) LIGHT ILLUMINATED. COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT MSP WAS UNEVENTFUL. MAINTENANCE FOUND A RUPTURED RETURN LINE TO THE AUXILIARY HYDRAULIC PUMP AND REPLACED IT ALONG WITH THE PUMP. TWO OTHER LEAKS WERE FOUND AND CORRECTED DURING THE AFTER ACTION LEAK CHECK. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20040818001682004081800168SO 2004 8 18 C2XA04TY144 120040810A32402164 BRAKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG ERRATIC A C2XAO OTHER F FLT CONT AFFECTED LDLANDING 1 SW2715983 145239 REPORT TAKEN FROM LOGPAGE 958380. THE PILOT REPORTED THAT ON LANDING, THAT ON THE ROLL ON A DRY RUNWAY, THE BRAKES FELT AS IF THE ANTI-SKID WAS ACTIVATING OR THE BRAKES WERE GRABBING WITH NORMAL BRAKE PRESSURE. MAINTENANCE BLED THE BRAKES AND PERFORMED OPS CHECKS AMM 32-40-00. OPS CHECKS WERE GOOD AND A/C WAS RELEASED. 2L72 4T4 FRTT00011ATTE6CH 20040818001692004081800169SO 2004 8 18 C2XA04RI005 120040806A3350 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711536 145520 DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE RESECURED EXIT SIGN CONNECTORS AND PERFORMED A SATISFACTORY OPERATIONAL TEST. 2L72 4T4 FRTT00011ATTE6CH 20040818001742004081800174NM 2004 8 18 WLDA200449 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 19.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 19 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001752004081800175NM 2004 8 18 WLDA200450 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 18.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 18 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001772004081800177EU 2004 8 18 KBM2004F00136 120040320A54100292808740 STRAP SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE HEAT SHIELD WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 EXHAUST HEAT SHIELD STRAP. HEAT SHRINK WORN REGS REPLACEMENT. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040818001782004081800178EU 2004 8 18 KBM2004F00139 120040721A215042080001 MOTOR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE CONDENSOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA89 2143 A/C BLOWER WARM. RT CONDENSOR BLOWER INOPERATIVE. REMOVED AND REPLACED. RT CONDENSOR BLOWER. 1G71 3U3 U H9EU E19EU 20040818001802004081800180NM 2004 8 18 P5CA0401134 120040804A3110 LIGHT BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE INSTRUMENT PANELINOPERATIVE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23921FT 21575 TAT, SAT, IB FLAPS AND P-10 PANEL LIGHTS OUT, ALSO BACKGROUND HSI, CLOCK AND AIR SPEED IND. TRANSFERED TO DMI NR 32904 IAW MEL 33-1. 2L74 4F4 F A20WE E3NE 20040818001822004081800182NM 2004 8 18 P5CA0401137 120040810A1420 CONNECTOR BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE RUDDER CONTROL LOOSE A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23508MC 21644 RUDDER RATIO LIGHT CAME ON DURING CLIMBOUT, 220KTS, FLAPS 1 DEGREE. RESEATED CONNECTOR TO RUDDER RATIO CONTROLLER AND SERVO ACTUATOR IAW AMM 27-21-00.. 2L74 4F4 F A20WE E23EA 20040818001832004081800183NM 2004 8 18 WLDA200448 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 20.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 20 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001842004081800184EU 2004 8 18 KBM2004F00154 120040524A6420SL100153B PIN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 T/R EXPANDABLE PIN WORN. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040818001872004081800187NM 2004 8 18 WLDA200457 120040802A5512ALC8101504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 4.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 4 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001882004081800188WP 2004 8 18 MWEA040142 120040812A53475952421503 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE GALLEY TRACK CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD IB GALLEY 1 SUPPORT FITTING CORRODED AT FRAME STA 160, 6 INCHES LT OF CENTER LINE. FABRICATED AND INSTALLED SUPPORT FITTING. 2L72 4F4 F A6WE E9NE 20040818001892004081800189NM 2004 8 18 WLDA200447 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 ITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 21. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 21 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001902004081800190EU 2004 8 18 KBM2004F00150 120040726A2150060018 BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE A/C BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV59 3296 BELT BROKEN IN FLIGHT. REPLACED BELT WITH NEW UNIT. 1G71 3U3 U H9EU E19EU 20040818001912004081800191EU 2004 8 18 KBM2004F00155 120040224A3150350A67674403 RELAY SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HORN MALFUNCTIONED E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP19350SH 2957 HORN SOUNDED IN FLIGHT FOR LESS THAN 1 SECOND. ROTOR RPM REMAINED STEADY AND NO WARNING LIGHTS ILLUMINATED. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001922004081800192EU 2004 8 18 KBM2004F00158 120040610A77129580113120 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TORQUE IND ERRATIC E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 TORQUE GAUGE REPORTED ERRATIC. REPLACED TORQUE TRANSMITTER WITH SERVICEABLE UNIT. OPS CHECK GOOD. 1G71 3U3 UNCH9EU E19EU 20040818001932004081800193 2004 8 18 KBM2004F00179 420040527A3422200DC GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL SPINNING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH912 2884 DIRECTIONAL GYRO SPINNS IN FLIGHT. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040818001952004081800195EU 2004 8 18 CX7A194J0449 120040816A77126071T20P17 CONTROL UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE TORQUE FLUCTUATES A CX7AO OTHER N FALSE WARNING CRCRUISE 1 GL03315CE 340B343 HAD TORQUE AND PROP FLUCTUATIONS AFTER DEPARTURE APPROX 1210-1280PROP/85-90 TRQ, WITH AIRPLANE YAWING TO THE RT ENGINE. LOCKED OUT TRQ MOTOR AND LANDED WITHOUT PROBLEMS. REMOVED AND REPLACED DECU. 2L72 4T4 TRTA52EU E8NE 20040818001962004081800196EU 2004 8 18 KBM2004F00148 120040610A2560AFG0326556 INERTIA REEL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE SEAT BELT MISMANUFACTURED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV15 3296 INERTIA REEL, HARD TO BUCKLE BELT. MANUFACTURED WITH WEBBING TOO SHORT. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040818001972004081800197EU 2004 8 18 KBM2004F00149 120040623A2150 BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE A/C BAY FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 A/C BLOWS HOT AIR. COIL, PULLEY, BELT (KIT) PULLEY/ NR 3003552, COIL/ NR 652233. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040819000012004081900001EU 2004 8 19 KBM2004F00142 120040523A6230704A63320851 SPHERICAL STOP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR OUT OF LIMITS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH5729 2337 SPHERICAL THRUST BEARING LAMINATED SHIMS HAVE GAPS BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040819000032004081900003NM 2004 8 19 WLDA200452 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 16.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 16 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000062004081900006NM 2004 8 19 WLDA200439 120040802A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 34.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 34 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000072004081900007EU 2004 8 19 KBM2004F00125 120040308A78100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE EXHAUST TORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 EXHAUST STACK STRAP BRACKET HEAT SHRINK IS RIPPED. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040819000092004081900009NM 2004 8 19 WLDA200453 120040802A5512ALC8101504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 14.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 14 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000202004081900020EU 2004 8 19 KBM2004F00182 120040707A2150 BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE AIR CONDITIONER MISSING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 FOUND BELT MISSING AND SOME SHREADED MATERIAL IN GIMBEL AREA. REPLACED BELT WITH NEW. 1G71 3U3 U H9EU E19EU 20040819000212004081900021NM 2004 8 19 P5CA0401142 120040812A5320 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 MAIN CARGO RT SIDE STA 1790 FRAME PROTECTION PANEL DENTED, REMOVED AND REPLACED PANEL AND INSP FRAME FOR ANY DAMAGE. DAMAGED INSULATION MOUNT BRACKET , SEVERAL AREA OF COVERS , BLENDED AREA OUT , REPAIR IAW SRM 51-10-04, SRM 51-30-02, SRM 51-40-03. 2L74 4F4 F A20WE E3NE 20040819000242004081900024NM 2004 8 19 WLDA200473 120040802A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 22.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 22 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000252004081900025NM 2004 8 19 WLDA200474 120040802A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 20.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 20 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000272004081900027NE 2004 8 19 04227678 220040815A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT OVERSERVICED A VTZABA EMER. DESCENT UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 EA27678BR 7653 LT ENGINE OIL PRESSURE WARNING INFLIGHT. DECLARED EMERGENCY. DIVERT TO CAE. LANDED UNEVENTFULLY.WO PERFORMED GVI OF LT OIL SYSTEM AND ENGINE AND FOUND NO EXCEEDANCES OF OIL PRESSURE. DESERVICED AND SERVICED LT ENGINE OIL SYSTEM. PERFORMED SEVERAL ENGINE GROUND POWER RUNS. NO DEFECTS NOTED AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20040819000332004081900033EU 2004 8 19 RAIA00408005 120040805A32348777701 CONTROL HANDLE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE MLG INOPERATIVE A RAIAO OTHER O OTHER DEDESCENT 1 CE03574HK 41093 LANDING GEAR WOULD NOT EXTEND NORMALLY. MANUALLY EXTENDED GEAR. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. 2L72 4T4 TRTA41NM E18NE 20040819000352004081900035SO 2004 8 19 RAIA00408010 120040809A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL THRUST REVERSER ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03816HK 145055 RT ENGINE THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED RT THRUST REVERSER IAW MEL. 2L72 4T4 FRTT00011ATTE6CH 20040819000362004081900036SO 2004 8 19 RAIA00408011 120040812A801135059106 STARTER EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03827HK 145021 LT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR TURBINE STARTER. 2L72 4F4 FRTT00011ATTE6CH 20040819000392004081900039EU 2004 8 19 RAIA00408002 120040804A28401173T0623 SWITCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE FUEL LOW TEMP MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03566HK 41084 LOW FUEL TEMP WARNING INDICATION. MAINTENANCE REMOVED AND REPLACED FUEL LOW TEMP SWITCH. 2L72 4T4 TRTA41NM E18NE 20040819000402004081900040SO 2004 8 19 RAIA00408012 120040812A2913100FU01080 FUSE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL HYD PUMP BLOWN A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03815HK 145048 LT ELECTRICAL HYDRAULIC PUMP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PUMP FUSE. 2L72 4T4 FRTT00011ATTE6CH 20040819000412004081900041SO 2004 8 19 RAIA00408008 120040805A801135059105 STARTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03829HK8018 3438 145281 RT ENGINE WOULD NOT START. MAINTENANCE REMOVED AND REPLACED RT ENGINE STARTER. 2L72 4T4 FRTT00011ATTE6CH 20040819000422004081900042SO 2004 8 19 RAIA00408013 120040812A32511170A180001 POTENTIOMETER EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NLW STEERING MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03803HK13960 145077 NOSE WHEEL STEERING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POTENTIOMETER. 2L72 4F4 FRTT00011ATTE6CH 20040819000492004081900049EU 2004 8 19 066641 120040802A7712 INDICATOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE TORQUE INOPERATIVE A UHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL17148SD 340A148 ON TAKEOFF ROLL, TQ INDICATOR REMAINED AT ZERO ON THE LT SIDE. AIRCREW RETURNED TO THE GATE. 2L72 4T4 TRTA52EU E8NE6 20040819000562004081900056NM 2004 8 19 UPS04M42915 120040621A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 C RT HORIZONTAL STAB BARREL NUT HOLE NR 25 FOUND CORRODED. CORROSION ON S/W AND BEARING REMOVED AND HOLE REAMED TO 1.067 INCHES AND BLENDED OUT TO 0.008 INCH DEEP FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB IAW EN 1232-04. APPLIED SEALANT PR1422 B2 AT BARREL NUT HOLE NR 25 RT. REPAIR SLEEVE BUSHING INSTALLED AT BARREL NUT NR 25 RT IAW EN 1232-04 AND EO MD11 -5510-19409-G, FOUND SATIS. 2L73 4F RTA22WE 20040819000582004081900058NM 2004 8 19 UPS04M42917 120040610A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, RT HORIZONTAL STAB NR 23 BARREL NUT HOLE FOUND CORRODED. BARREL HOLE NR 23 RT,REAMED TO 1.067 INCH IAW EO MD11-5510-19409-G. S/W SUR FACE FOUND CORROSION BLENDED OUT 0.050 INCH DEEP EXCEEDED LIMIT. FAB AND REP AIR SLEEVE BUSHING C/OUT IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN-1207-04.REPAIR SLEEVE AND INSTALLED IAW EN1207-04 AND EO MD11- 5510-19409-G AND FOUND REPAIR ACCOMPLISHED WITHIN LIMIT, SATIS. 2L73 4F RTA22WE 20040819000632004081900063SO 2004 8 19 CHQA000533 120040808A2497 RELAY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT BURNED A CHQAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL11565RP 145679 THE PILOTS REPORTED THE COCKPIT FILLED UP WITH SMOKE AS THEY WERE SITTING AT THE GATE. THE CAPTAIN SAID THE APU WAS RUNNING AND THEY NOTICED SMOKE COMING OUT FROM THE AREA AROUND THE RELAYS SUPPORT. THE CAPTAIN REPORTED, SHUT DOWN THE AIRCRAFT POWER BUT THE SMOKE WAS STILL PRESENT. THEN SHOT THE PORTABLE COCKPIT FIRE EXTINGUISHER INTO THE HOLES AROUND THE RELAY SUPPORT. PILOT REPORTS AFTER SHOOTING THE FIRE EXTINGUISHER THE SMOKE CLEARED. REMOVED AND REPLACED FIVE DAMAGED RELAYS AND WIRES IN THE RELAY SUPPORT AND REPLACED THE PORTABLE COCKPIT FIRE EXTINGUISHER. 2L72 4T4 FRTT00011ATTE6CH 20040819000692004081900069EA 2004 8 19 COMA0460429 120040724A4990 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE APU OIL SYS ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01976CA 7151 FLIGHT 5711 APU OIL TEMP CAUTION MESSAGE. COULD NOT DUPLICATE APU OPERATIONAL CHECK SATISFACTORY. 2L72 4F4 FRTA21EA E15NE 20040819000712004081900071 2004 8 19 ARWA20040603 420040621A34202588533901 AMPLIFIER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE INDICATOR FAILED A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19661AV 45969 LOG PAGE NR 107128. CAPTAIN'S HEADING FLAG DISPLAYED INTERMITTENTLY; RETURNED TO RAMP. REMOVED AND REPLACED INSTRUMENT AMP IAW M/M 34-21-0; HORIZON SYSTEM OPERATIONAL NORMAL IAW M/M 34-25-0. 2L74 4F4 F 4A25 1E8 20040819000722004081900072EU 2004 8 19 WRNA200400007 120040721A323098A32301012000 SEQUENCE VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE NLG MISALIGNED A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05505TA 271 NOSE GEAR DID NOT RETRACT AFTER T/O RETURN TO AIRPORT. INSTALLED RIG PIN ON SEQUENCE VALVE AND RIGGED TO ZERO POSITION FOR REMOVED NLG DOOR. DOOR DEACTIVATED IAW CDL. FUNCTIONAL CHECK PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20040819000742004081900074NM 2004 8 19 DL73S040676 120040720A53156546800508 FLOORBEAM BOEING737 737247 138448DNM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27374DL 23521 STA 520 FLOORBEAM CRACKED IN RADIS. REPAIR IAW ERA 091543-14. 2L72 4F4 F A16WE E2EA 20040819000782004081900078 2004 8 19 DL76L040680 420040721A34206227999003 INDICATOR BOEING767 767332 1382001NM COCKPIT BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27180DN 25985 EHSI INDICATOR FAILED AND PUT SMOKE IN THE FLIGHT DECK. REPLACED INDICATOR. 2L72 4F RTA1NM 20040819000792004081900079 2004 8 19 DL76L040681 420040721A34206227999003 INDICATOR BOEING767 767332 1382001NM COCKPIT BURNED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27180DN 25985 IR: .AT FL 290 CAPT HSI DISPLAY WENT BLANK AND ELECTRICAL. FUMES WERE SMELLED BY CREW. REPLACED CAPTS HSI. CHECKED AIRFLOW AND WIRING ALL OK. ETOPS CATEGORY (B): DIVERSION OR TURNBACK. 2L72 4F RTA1NM 20040819000802004081900080NM 2004 8 19 DLM88040683 120040722A3244 TIRE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE LT MLG DAMAGED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO27985DL 53312 NR 2 MAIN TIRE LOST RECAP ON TAKEOFF. DAMAGE TO LT IB FLAP AND BUTE DOOR. ALSO DAMAGE TO LOWER LT ENGINE INLET COWL AT 6 O'CLOCK POSITION LOWER SIDE. NO DAMAGE TO ENGINE FAN BLADES. REPAIRED/REPLACED DAMAGED PARTS. 2L72 4F4 FRTA6WE E2EA 20040819000812004081900081NE 2004 8 19 DL76L040684 220040721A7261PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 LEAKING A DALAK NONE KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27194DN44795 28451 724691 SMOKE OIL ODOR IN CABIN FOUND OIL LEAK AT THE CARBON SEAL ON THE NR 1 BEARING, REPLACED SEAL. 2L72 4F4 FRTA1NM E24NE 20040819000822004081900082EU 2004 8 19 AWXA200400692 120040612A5320D5347112420000 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE TOP SURFACE OF THE RT AFT SHEAR WEB END OF THE Y-1292 BEAM BETWEEN FR69-FR70. REMOVED AND REPLACED SHEAR PLATE (WEB) FR 69-70- Y1292 IAW A320 SRM 51-42-11 PG 8,10,12,22 FIGS 2,3,8,. 2L72 4F RTA28NM 20040819000832004081900083EU 2004 8 19 AWXA200400693 120040612A5320D5348004320500 SILL AIRBUS320 A320231 3930325EU FUSLAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (GALVANIC) WAS FOUND ON THE R2 SILL IB OF THE AFT SLIDE ATTACH FITTING AT FR68. MAINTENANCE REPAIRED R2 SILL IB OF THE AFT SLIDE ATTACH FITTING IAW A320 SRM 53-41-14 FIG 201 2L72 4F RTA28NM 20040819000842004081900084EU 2004 8 19 AWXA200400694 120040612A5310D5347220924500 BEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE Y-1292 BEAM AT FR66. MAINTENANCE REMOVED AND REPLACED Y-1292 BEAM SECTION FR 64-67 IAW A320 SRM 51-42-11 PG 5,6,7. 2L72 4F RTA28NM 20040819000852004081900085EU 2004 8 19 AWXA200400695 120040612A5320D5347112420000 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (GALVANIC) WAS FOUND ON TOP AND BOTTOM SURFACE OF THE LT AFT SHEAR WEB END OF Y1292 BEAM FWD OF FR70. MAINTENANCE REMOVED AND REPLACED SHEAR WEB Y1292 FR 69-70 IAW A320 SRM 51-42-11 PGS 8,10,12,22,A27 FIGURES 2,3,8,62. 2L72 4F RTA28NM 20040819000862004081900086EU 2004 8 19 AWXA200400696 120040613A5347D5713014720000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (LITE TO MODERATE PITTING) WAS FOUND ON THE LT IB Y765 SEAT TRACK FR35-FR41. MAINTENANCE REPAIRED AFFECTED AREA IAW SRM 53-31-15 FIG 102. 2L72 4F RTA28NM 20040819000872004081900087EU 2004 8 19 AWXA200400697 120040613A5347D5337111000000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION WAS FOUND ON THE LT Y765 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT Y765, FR 41-47, IAW A320 SRM 51-42-11 FIGURES 9,10,12,18. 2L72 4F RTA28NM 20040819000882004081900088EU 2004 8 19 AWXA200400698 120040613A5347D5337111200100 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE RT OB Y-1292 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT Y1292, FR 41-47 IAW A320 SRM 51-42-11 PAGES 6,7,41 FIGURE 18. 2L72 4F RTA28NM 20040819000892004081900089 2004 8 19 P5CA0401114 420040707A3414A432171016 INDICATOR BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE AIRSPEED INOPERATIVE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23508MC 21644 FLIGHT OFFICER AIRSPEED INDICATOR INOPERATIVE, NO MOVEMENT. REPLACED INDICATOR OPS CHECK OK, IAW MM 34-17-03. 2L74 4F4 F A20WE E23EA 20040819000902004081900090NM 2004 8 19 AWXA200400811 120040714A5321D5361060500100 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 DURING B-04 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CABIN FLOOR PANEL 222FF IAW T/C C1D25306. 2L72 4F RTA28NM 20040819000912004081900091WP 2004 8 19 DHL2004807013 120040711A3350CM1864 BULB DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT BURNED OUT A DHLAO OTHER P NO WARNING INDICATION CRCRUISE 1 SO01807DH 45990 EMERGENCY LIGHTS DISARMED, LIGHT BULB BURNED OUT. RELAMPED EMERGENCY LIGHTS DISARMED. OPS CHECKED IAW MM CH 33-50-2,CHECKED GOOD.(P/N CM1864) 2L74 4F RT4A25 20040819000922004081900092 2004 8 19 ANCF200400021 420040722A34426225136003 ANTENNA BOEING767 767259 1385136NM PWA 4056 PW4056 NE WX RADAR DEFECTIVE W ANCFO OTHER J WARNING INDICATION CRCRUISE 1 SO23985AN21305118 24618 WXR FAIL DISPLAYED ON HSI WITH BOTH SYSTEMS SELECTED. WXR FAIL ANTENNA ON HSI. IT WAS REPLACED WXR ANTENNA IAW AMM34-43-03/401. 2L72 4F4 FRTA1NM E24NE 20040819000932004081900093WP 2004 8 19 ABXA040244 120040713A335041B004AD07G3 BATTERY DOUG DC9 DC941 302207NWP PWA JT8 JT8D* NE EMERGENCY LIGHT WILL NOT TEST A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23968AX 47499 COCKPIT OVERHEAD PANEL EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-001. 2L72 4F4 F A6WE E2EA 20040819000942004081900094WP 2004 8 19 04FDEA02349 120040802A5240ADA37521 BEAM DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25396FE 46630 ORIGINAL NON-ROUTINE N00905 LOST. L3 DOOR HAS 2 EA FWD STOP FITTINGS CRACKED. GENERATED RFTS NR 396FE-2931081, REMOVED 1 EA CRACKED BEAM PN ADA 3752-1 REMOVED 10 EA STIFFENERS, DRILLED NEW BEAM PN 3752-1, INSTALLED NEW BEAM PN ADA3752-1, INSTALLED 10 EA STIFFENERS IAW SRM 51-35-01 VOL LL,D-DWG ADA 3752, VERIFIED CRACK ON 2ND BEAM, DYE PENETRATE: NO CRACK FOUND, ALODINED AND PRIMED IAW ASTME 1417-99 AND SRM 51-21-01 VOL LL. 2L73 4F4 FRTA22WE E23EA 20040819000952004081900095NM 2004 8 19 04FDEA02350 120040802A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT HORIZONTAL STABILIZER NR 34R BARREL NUT BORE FOUND WITH CORROSION, CLEANED UP CORROSION AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80285, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 34R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040819000962004081900096NM 2004 8 19 04FDEA02351 120040802A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP IB HINGE FORWARD FITTING FORWARD. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.567, FINAL DIAMETER = 0.627. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2L73 4F RTA22WE 20040819000972004081900097NM 2004 8 19 04FDEA02352 120040802A5753 FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP OB HINGE FORWARD FITTING. FORWARD IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502. COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2L73 4F RTA22WE 20040819000982004081900098NM 2004 8 19 04FDEA02353 120040802A5753 FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP OB HINGE FORWARD FITTING MIDDLE. OB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.457, FINAL DIAMETER = 0.517 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2L73 4F RTA22WE 20040819000992004081900099NM 2004 8 19 04FDEA02354 120040802A5753 FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP OB HINGE FORWARD FITTING AFT. IB HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.442, FINAL DIAMETER = 0.502 COMPLIED WITH FEDEX EA 1-5750-80364, WINGS - TRAILING EDGE FLAPS - LEFT OUTBOARD FLAP - HINGE BRACKET SUPPORTS CORRODED. 2L73 4F RTA22WE 20040819001002004081900100EU 2004 8 19 CX7A194J0444 120040729A33206500006 BALLAST SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN LIGHT CONTAMINATED A CX7AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL03312CE 340B334 WINDOW LIGHTS OVER 12B/D STARTED SPARKING AND SMELLED ELECTRICAL SMOKE. LIGHTING BALLAST CONTAMINATED WITH WATER. 2L72 4T4 TRTA52EU E8NE 20040819001012004081900101EU 2004 8 19 AWXA200400826 120040711A5347D5337111000000 SEAT TRACK AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT IB SEAT TRACK AT Y765, FR 47. MAINTENANCE REMOVED CORRODED LT IB SEAT TRACK AT Y765, FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 13, 14, AND 18. 2L72 4F4 FRTA28NM E311NE 20040819001032004081900103EU 2004 8 19 UPS04142924 120040810A1420 CONNECTOR AIRBUSA300 A300F4622R 3930360EU LIGHT DAMAGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01121UP 0806 ON MAIN ENTRY DOOR RED LIGHT WILL NOT TEST. FOUND PIN -C- AT CONNECTOR 1587 PUSHED BACK. SEATED PIN, CHECKS NORMAL AMM 52-73-00-5. PLACARD REMOVED. 2L72 4F RTA35EU 20040819001052004081900105NM 2004 8 19 UPS04442925 120040816A5230 SKIN BOEING747 747212B 1384886NM CARGO DOOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01526UP 21937 LOWER FWD CARGO DOOR HAS DAMAGE TO SKIN ON LOWER AFT CORNER OF DOOR. INSTALLED TEMPORARY REPAIR DOUBLER. REPAIR HAS A ONE YEAR LIMIT. FWD ITEM TO DMI LOG D286216. 2L74 4F A20WE 20040819001062004081900106WP 2004 8 19 UPS04842913 120040710A57405642342U2 SUPPORT DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 RIGHT WING FLAP HINGE 3 SUPPORT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040819001072004081900107WP 2004 8 19 UPS04842914 120040728A5711 SPAR CAP DOUG DC8 DC873F 302199FWP CENTER WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 WING CENTER SPAR LOWER CAP AT WING STATION XCW 36 IS CRACKED. STOP DRILLED CRACK NDT VERIFIED STOPDRILLS TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND REPAIR ANGLE IAW SAA SK 802-190 AND UPS EO DC8-5710-20888-A. 2L74 4F RT4A25 20040819001092004081900109NE 2004 8 19 DLM88040757 220040812A7320739001000 VALVE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE FAILED A DALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO27920DL 49644 725820 LEFT ENGINE WOULD NOT ACCELERATE ABOVE 60 PERCENT N2 ON TAKEOFF ROLL. REPLACED PD VALVE. 2L72 4F4 FRTA6WE E9NE 20040819001112004081900111 2004 8 19 DLM88040761 420040813A2565D29985103 SLIDE DOUG MD88 MD88 3023688NM L2 UNSERVICEABLE A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27971DL 53214 L2 DOOR SLIDE FELL OUT OF DOOR PACK AND LANYARD PULLED FROM BUSSLE PACK. REPLACED SLIDE PACK L2 DOOR. 2L72 4F RTA6WE 20040819001132004081900113NM 2004 8 19 DLM88040763 120040814A2560P20700030 FLASHLIGHT DOUG MD88 MD88 3023688NM L-1 DOOR INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27910DL 49541 L-1 UPPER EMERGENCY FLASHLIGHT INOP. REPLACED AND TESTED PER MM. 2L72 4F RTA6WE 20040819001152004081900115NM 2004 8 19 DL73S040766 120040813A53146547693 KEELBEAM BOEING737 737232 1384475NM FS S- CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 THE KEEL CHORDS AT STRINGERS 27L & 27R WERE FOUND CORRODED NEAR THE SPLICE END AT FS 727A. THE CHORDS WERE CUT AT FS 727B+10 AND THE CORRODED ENDS REMOVED. NEW SECTIONS OF CHORD WERE SPLICE IN WITH ALUMINUM REPAIR ANGLES PER ER/A 092557-14 AND ER/A 092126-14. 2L72 4F RTA16WE 20040819001172004081900117NM 2004 8 19 DLM88040768 120040817A25408921460G5 WATER HEATER DOUG MD88 MD88 3023688NM AFT LEFT LAV FAILED A DALAO OTHER M OVER TEMP CRCRUISE 1 SO27912DL 49543 AFT LT LAV SMOKE DET BEEPING IN FLT. WATER HEATER WAS VERY HOT INITIALLY OPENED DETECTOR AND DISCONNECTED BATTERY NO ODOR DETECTED. PULLED CB'S FOR AFT LT LAV MIRROR, FLUSH MOTOR AND WATER HEATER. RAN HOT WATER UNTIL COOL. AFT F/A INTERPHONE PANEL WAS WARM BUT BECAME COOL. RE-ATTACHED SMOKE DET BATTERY RED LIGHT OUT, NO BEEPING. RESET ALL CB'S, INSPECTED AFT LT LAV FOUND WATER HEATER OVERHEATING. PULLED AND COLLARED C/B FOR WATER HEATER. FWD TO MCO AND PLAC PER MEL 25-00-12D. ALSO FOUND WATER IN SMOKE DETECTOR. REPLACED SMOKE DETECTOR, NO WATER LEAKS FOUND. 2L72 4F RTA6WE 20040819001192004081900119NM 2004 8 19 DL757040770 120040817A2121731379 FAN BOEING757 757232 1384965NM NR1 SUPPLY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27676DL 25981 DURING CRUISE HAD SLIGHT ELEC ODOR IN COCKPIT. NO ABNORMAL INDICATIONS. REPLACED FWD EQUIPMENT SUPPLY FAN. 2L72 4F RTA2NM 20040819001202004081900120NM 2004 8 19 AWXA200400893 120040816A2560EF1 FLASHLIGHT BOEING737 737277 1384570NM ZONE 900 - LAVATINOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28186AW 22653 DFW - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040819001212004081900121NM 2004 8 19 AWXA200400894 120040725A14201703661 CONNECTOR BOEING737 7373S3 1384711NM ZONE 200 DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 MCN - EEL - DURING C-19 CHECK MAINTENANCE DISCOVERED NUMEROUS DAMAGED CONNECTORS AND SPLICES ON EMERGENCY ESCAPE PATH LIGHT HARNESS LT SIDE OF CABIN. REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES LT SIDE OF CABIN, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040819001232004081900123EU 2004 8 19 AWXA200400896 120040805A5347D53112092206 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 RT AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041129000522004112900052EA 2004 11 29 ASOA04783 120041007A33501317 LAMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27706EV 10054 DURING AN A-CHECK, THE RT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041129000622004112900062CE 2004 11 29 W322004F00002 120040519A32409550273C BRAKE LEAR 24 24D 5170311CE LT MLG CRACKED D W32AO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP0739EL 251 AIRCRAFT REPORTED LOSS OF HYDRAULIC PRESSURE AFTER FAILURE OF FLAPS TO DEPLOY. UPON INITIAL INSPECTION, HYDRAULIC FLUID WAS FOUND FLOWING FROM LT BRAKE ASSEMBLY. UPON REMOVAL FROM AC, BOTH BRAKE ASSEMBLIES WERE FOUND TO BE CRACKED IN IDENTICAL LOCATIONS, RADIATING FROM TRUNNION BLOCKS TOWARDS THE OUTER EDGES. CAUSE OF CRACKS AT THIS TIME ARE UNKNOWN, CAUSE COULD BE ATTRIBUTED TO POSSIBLE INSTALLATION ERROR. 2L72 4J A10CE 20041129000632004112900063NE 2004 11 29 HJB2004F00001 220040913A7320660526AS TRANSDUCER DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE FUEL FLOW MALFUNCTIONED B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL055160G361 236 JP204945 REMOVED FUEL FLOW TRANSDUCER INSTALLED UNDER STC NR 809GL. UNIT PROVIDING ERRONEOUS FUEL FLOW READINGS AND CAUSING THE AIR DATA COMPUTER (ADC) ALSO INSTALLED IN THE AIRCRAFT TO FUNCTION IMPROPERLY. AIR DATA COMPUTER INSTALLED UNDER EFS-SV SYSTEM IAW STC NR SA02203AK. 1H71 3R3 R A806 5E1 20041129000652004112900065WP 2004 11 29 COOSDR040039 120040909A573056434111 PANEL DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE LT WING CORRODED A EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 LT WING, INNER WING T/E UPPER PANEL WITH HEAVY CORROSION. 2L74 4F4 F 4A25 1E8 20041129000692004112900069 2004 11 29 HXR2004F00000 420040921A3417962830A1S8 ADC CESSNA310 T310Q 2074244CE CONT O520 TSIO520* 17040SO COCKPIT MALFUNCTIONED E HXRAO OTHER O OTHER NRNOT REPORTED 1 AL05767RR29 310Q0455 ADC AND ALTIMETER READING 2000 FT DIFFERENCE. 1L72 3O3 O 3A10 E8CE 20041129000832004112900083NM 2004 11 29 USAA040792 120040914A5314 ANGLE BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE KEELBEAM CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, KEEP REPAIR ANGLE, 20 INCH AREA, CORROSION; LEVEL 1; TASK NR C 53-208-01 R KEEL STA 520-540. INSTALLED NEW REPAIR ANGLE/ DOUBLER IAW SRM 51-70-11. 2L72 4F4 FRTA16WE E2GL 20041129000882004112900088EA 2004 11 29 ASOA04809 120041020A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT & RIGHT ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27863AS 7487 DURING DESCENT, AN OILY ODOR FILLED THE CABIN AND COCKPIT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AND RT AIR CYCLE MACHINES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129000912004112900091EA 2004 11 29 REXA04025 120041029A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG DOOR OUT OF POSITION A REXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO258515F8173 7515 ON CLIMB-OUT FROM TAKEOFF, GOT (NOSE DOOR) MESSAGE AND (GEAR DISAGREE) MESSAGE. ORH FOLLOWED, EMERGENCY DECLARED RETURNED TO AIRPORT, UNEVENTFUL LANDING. FOUND PROXIMITY SENSOR ON NOSE GEAR OUT OF POSITION. RIGGED SENSOR IAW AMM, PERFORMED GEAR SWINGS. 2L72 4F4 FRTA21EA E15NE 20041129000922004112900092EA 2004 11 29 REXA04027 120041105A2751 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO258971A 7971 FLAP FAIL MESSAGE ON TAXI WHILE RAISING FLAPS. REMOVED AND REPLACED SKEW DETECTION UNIT. 2L72 4F RTA21EA 20041129000962004112900096EU 2004 11 29 A6WA200460051 120041025A5330 SKIN BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE SCRATCHED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 SKIN SCRATCH LT FUSELAGE BELOW CABIN WINDOW BETWEEN FRAMES 30 AND 31 JUST ABOVE STR 14L. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 608-2049005. 2H74 4F4 F A49EU E6NE 20041129000992004112900099NE 2004 11 29 Y2PA04030 220041112A72615002T29P01 LINE AMD FALC20FALCON 2720302EU GE CF700 CF7002C 30010NE NR 1 ENG OIL LEAKING E Y2PAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23816AA 290 304508B AFTER DEPARTING, ON CLIMB OUT, PASSING 12,500 FT, NR 1 OIL PRESSURE LIGHT CAME ON AND NR 1 OIL PRESSURE INDICATED ZERO. REDUCED NR 1 ENGINE TO IDLE AND FOLLOWED ENGINE SHUTDOWN PROCEDURES IN MFG OPERATING HANDBOOK. DECLARED EMERGENCY AND RETURNED TO DEPARTURE WITH NR 1 ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINT SENT, REMOVED AND REPLACED OIL TUBE LOCATED AT 3 OCLOCK POSITION AFT WITH SERVICEABLE TUBE IAW MM. OPS AND LEAKED CHECK GOOD, DURING ENGINE RUN UP IAW SEI-189. NO OTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 F A7EU E7EA 20041129001032004112900103NM 2004 11 29 LLM2004F00000 120040921A2750NAS561P38 ROLL PIN BOEING727 727200 138407ENM DRIVE GEAR MISSING B LLMYO OTHER O OTHER NRNOT REPORTED 1 EA35117JB 20993 WHEN REMOVING NR 2 T/E TRANSMISSION IT WAS DISCOVERED THAT THE IB TORQUE TUBE DRIVE GEAR WAS NOT POSITIVELY ATTACHED TO THE FLAP TRANSMISSION SPLINES. THE TRANSMISSION WAS REMOVED AND INSPECTED. THE INSPECTION REVEALED THAT GEAR/SPLINE ATTACHMENT ROLL PIN NAS 561P38 WAS MISSING (IPC 27500025A90). WHILE CARRYING OUT RIGGING PROCEDURE FOR T/E FLAPS, NR 4 TRANSMISSION IB DRIVE GEAR BECAME DETACHED FROM ITS ASSOCIATED TORQUE TUBE. CLOSE INSP REVEALED ROLL PIN HAD SHEARED, REMOVED AND REPLACED (IPC 27-50-0-27-34). ALL DEFECT RECTIFICATION HAS BEEN CARRIED OUT AND DOCUMENTED. 2L73 4F RTA3WE 20041129001112004112900111EU 2004 11 29 SIMA200416702 120040614A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT INOPERATIVE A O OTHER O OTHER NRNOT REPORTED 1 SW21345SB 340B345 EMERGENCY LIGHT ROW 8A INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY NR 22 LN IAW MFG MM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 20041129001172004112900117NM 2004 11 29 USAA040743 120041011A5312 PRESSURE BLKHD BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US38934 24863 PIT, FPBH, WEB, .1250 INCH CRACK AT RIVET. FWD PRESSURE BULKHEAD, WEB WL 234/RBL 12. WEB REPAIR, FILLER AND DOUBLER IAW SRM 53-10-08, FIG 209 AND EO 5300V153. 2L72 4F4 FRTA16WE E21EU 20041129001232004112900123NM 2004 11 29 ASAA0410415 120041001A3320 BATTERY BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02744AS 21822 DURING RECONFIGURATION DISCOVERED SMOKE BARRIER (EXIT TO REAR) LIGHT INOPERATIVE. REPLACED BATTERY. 2L72 4F4 F A16WE E2EA 20041129001312004112900131NM 2004 11 29 ASAA0410412 120040929A53306545777523 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON EXTERNAL SKIN. REPAIRED DAMAGE ON SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20041129001412004112900141NM 2004 11 29 ASAA0470012 120040827A5320BAC1496377 ANGLE BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02624AS 30778 FWD CARGO COMPARTMENT, RT ZEE ANGLE CORRODED AT STA 500C. REMOVED AND REPLACED FWD CARGO COMPARTMENT ZEE ANGLE AT STA 500C-500D. 2L72 4F4 FRTA16WE E00055EN 20041129001442004112900144 2004 11 29 KBM2004F00234 420040921A34215040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ATTITUDE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 ATTITUDE GYRO WILL NOT HOLD ATTITUDE IN FLIGHT. INSTALLED GYRO FROM 350SH SERVICEABLE. 1G71 3U3 U H9EU E19EU 20041129001502004112900150NM 2004 11 29 GAIA04117 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSE SKIN CRACKED BS 360, STR 5, LT. REF FASI NR 86545, CUT OUT DAMAGE AREA DIM 2.50 X 1.0 INSTALL DOUBLER REPAIR IAW SRM 53-30-3, FIG 3A. 2L73 4F4 F A3WE E2EA 20041129001542004112900154NM 2004 11 29 GAIA04156 120040910A5210 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE L-1 DOOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND L-1 DOOR EXTERIOR SKIN AFT UPPER CORNER BENT. REF FASI NR 86903 REWORKED SKIN TO ORIGINAL CONTOUR, FOUND SKIN CRACKED, INSTALLED DOUBLER REPAIR IAW SRM 52-10-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041129001552004112900155NM 2004 11 29 M562004F00001 120040726A5315 FLOORBEAM BOEING737 737400 138449ANM CFMINTCFM56 CFM563C1 13802EU FUSLAGE CORRODED I M56BO OTHER O OTHER NRNOT REPORTED 1 EA0537NY 23976 MAIN CABIN AFT LBL46 HAS CORROSION ON TOP OF FLOORBEAM AT STA 980. REMOVED CORROSION, PERFORMED EDDY CURRENT. RETURNED TO SERVICE. C1,C2 AND C3 INSP 8/4/04. 2L72 4F4 FRTA16WE E21EU 20041129001622004112900162NM 2004 11 29 GAIA04123 120040910A5754 RIB BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 6 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86614, REMOVED AND REPLACED NR 6 SLAT INTERIOR RIB IAW SRM 57-50-2. 2L73 4F4 F A3WE E2EA 20041129001742004112900174EA 2004 11 29 A6WA200440174 120041028A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FS 280, LBL9 OB ANGLE PN 601R31113-57 IS CRACKED IN RADIUS AT WL 73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE IAW REO 601R-53-11-171 REV A AND BRAS EO 601R-53-5547. 2L72 4F4 FRTA21EA E15NE 20041129001792004112900179EA 2004 11 29 A6WA200440162 120041025A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING CRACKED A K NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 BATT RIB ASSY IS CRACKED 1.2500 INCH LONG IN AFT UPPER RADIUS. CORRECTIVE ACTION IN PROGRESS. 2L72 4F4 FRTA21EA E15NE 20041129001842004112900184EA 2004 11 29 A6WA200440161 120041022A3260 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG SENSOR DAMAGED A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31416AW 7603 NOSE GEAR DOOR/ DISAGREE ON WITH GEAR HANDLE UP. NOSE GEAR DOWN, MAINS UP. REPLACED NOSE GEAR BRACKET WITH NOSE GEAR EXT AND PROXIMITY SENSOR IAW CMM 32-61-05 PERFORMED NOSE GEAR SWING. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041129001892004112900189SO 2004 11 29 IV42004F00000 120040831A2430 BEARING GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU GENERATOR FAILED B IV4RO OTHER O OTHER NRNOT REPORTED 1 SO09949NA 183 452EH 221 DURING CLIMBOUT, 2 HIGH TVI INDICATION ON NR 1 END AFT WAS OBSERVED (APPROX 2.5). AFTER POWER WAS REDUCED, TVI INDICATION REDUCED TO APPROX (.7), SOME FLUCTUATION ON TVI INDICATOR. GEN VOLTAGE WAS NORMAL BUT HAD SPLIT IN GEN AMPERAGE WITH NR 1 GEN SHOWING APPROX 15 AMPS. ALL OTHER INDICATIONS WERE NORMAL, NO WARNING LIGHTS. AFTER LANDING NR 1 COWLING WAS OPENED, SOME OIL WAS OBSERVED COMING FROM AROUND NR 1 GEN. SOME DAMAGE TO NR 1 GEN EXHAUST DUCT. GEN AND EXHAUST DUCT WAS REMOVED WHICH REVEALED A FAILED AFT GEN BRG. FAILED BRG PIECES CAUSED SOME ARCING IN BRUSH AREA, FIELD AREA. NEW GENERATOR WAS INSTALLED IAW MM. GEN WAS OPERATIONAL CHECKED ON AC AND WAS GOOD. AC WAS RETURNED TO SERVICE. 2L72 4F4 FRTA12EA E2EU 20041129001932004112900193WP 2004 11 29 MJ12004F00000 220040930A726130756392 CARBON SEAL BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE7313R1H 29001WP NR 2 ENGINE FAILED E MJ1RO OTHER O OTHER NRNOT REPORTED 1 EA11298BP NA0298 OPERATOR NOTED NR 2 ENGINE LOW OIL PRESSURE IN FLIGHT. ENGINE POWER SETTING WAS REDUCED TO IDLE AND CREW ELECTED TO RETURN TO ORIGIN. POST FLIGHT ATTEMPTS TO START NR 2 ENGINE WERE ABORTED DUE TO INABILITY TO OBTAIN PROPER ENGINE ROTATION. ENGINE SN P84313 WAS REMOVED FROM THE AC, A LOANER ENGINE WAS INSTALLED IN ITS PLACE. ENGINE SN P84313 WAS SENT TO MFG FOR FURTHER INVESTIGATION AND REPAIR. TEARDOWN/INVEST OF ENGINE REVEALED FAILURE CAUSED BY NR 4 CARBON SEAL CERAMIC RUNNER, WHICH WAS NOTED TO BE SHATTERED. NR 4 CARBON SEAL CERAMIC RUNNER FAILURE. 2L72 4F4 F A3EU E6WE 20041129002022004112900202CE 2004 11 29 AXS2004F00000 120040907A32461388911 BEARING BEECH 99 B99 1154004CE PWA PT6 PT6A27 52043EA MAIN WHEEL FAILED E AXSAC ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 NE05119WA 63 U154 ON THE TAKEOFF ROLL, 2 MAIN WHEEL ASSEMBLY DEPARTED THE AXLE. PRELIMINARY INVESTIGATION REVEALED THE OUTER WHEEL BEARING RACE HEAVILY DAMAGED AND THE OUTER BEARING DAMAGED BEYOND RECOGNITION. THE MAIN WHEEL AXLE NIT AND HARDWARE WAS FOUND STILL INTACT ON THE AXLE. IT APPEARS THE BEARING FAILED ALLOWING THE HUB TO DEPART THE AXLE. (NE05200408832) 1L72 3T4 T A14CE E4EA 20041129002112004112900211GL 2004 11 29 ALG2004F00058 220041011A7200250C30P ENGINE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ANIMAL INGESTIONE ALGAC ABORTED TAKEOFF CJ F.O.D. WARNING INDICATION TOTAKEOFF 1 SW032619 13076 51375 CAE890734S ON TAKEOFF THE ENGINE INGESTED A FROG, RETURNED TO BASE. MECHANIC INSPECTED THE ENGINE INLET, REMOVED FROG REMAINS, WASHED THE ENGINE. AND COMPLIED WITH POWER CHECK. FOUND SERVICEABLE. AC WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E1GL 20041129002132004112900213NM 2004 11 29 USAA040733 120041011A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU63825 22193 STRINGER, 1 INCH BY 40 INCHES, CORROSION STA 660 TO 620 STRINGER 29L. REMOVED AND INSTALLED NEW STRINGER SEC IAW SRM 53-00-03. 2L72 4F4 FRTA2NM E12EU 20041130000042004113000004EU 2004 11 30 AWXA200401320 120041025A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 46 AND FR 47. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 46 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000052004113000005NM 2004 11 30 ABXA040383 120041118A3233273T62013 ACTUATOR BOEING767 767281 1385109NM MLG DEFECTIVE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23767AX 12186 22785 ON DEPARTURE FROM ILN, LANDING GEAR DISAGREE AND GEAR DOORS EICAS MSG WITH GEAR HANDLE UP. REPLACED LEFT MAIN LANDING GEAR SIDE STRUT ACTUATOR IAW B767 MM 32-32-02-4. PERFORMED GEAR SWING, GEAR SWINGS OK. 2L72 4F RTA1NM 20041130000132004113000013EU 2004 11 30 AWXA200401270 120041022A5313D53231206200 STRINGER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON STRINGER 39 LT IN FORWARD CARGO COMPARTMENT AT FR 34. MAINTENANCE CUT OUT DAMAGED AREA OF STRINGER 39 LT AT FR 34; FABRICATED A COUPLING; INSTALLED REPAIR PART IAW A320 SRM 53-00-13 FIG 201. 2L72 4F RTA28NM 20041130000262004113000026SO 2004 11 30 MASA200400096 120040221A3097S5009140 SOCKET EMB 145 EMB145LR 3260212SO PITOT HEAT BURNED A MASAA UNSCHED LANDING JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07830MJ 145259 AIRCRAFT DIVERTED TO CLT ORIGINALLY EN ROUTE TO DHM. THE CREW REPORTED A NR 3 PITOT HEAT MESSAGE AND AN ELECTRICAL ODOR IN THE COCKPIT. MX ISOLATED THE PROBLEM TO THE CURRENT SENSOR AND SOCKET BEING BURNED. MX REPLACED THE SENSOR, SOCKET AND REPAIRED ANY DAMAGED WIRING. 2L72 4T RTT00011AT 20041130000282004113000028SO 2004 11 30 MASA200400624 120041105A3350 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 EMERGENCY EXIT INTERIOR LIGHT INOP. MAINTENANCE RESECURED LAMP. 2L72 4T RTT00011AT 20041130000292004113000029SO 2004 11 30 MASA200400626 120041105A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07835MJ 145353 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE SECURED THE CONNECTION TO THE LIGHT ASSEMBLY. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041130000412004113000041NM 2004 11 30 SWAA043409 120041120A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041130000432004113000043NM 2004 11 30 SWAA043411 120041120A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20041130000462004113000046NM 2004 11 30 SWAA043414 120041121A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED RON, FOUND 2EA FUSELAGE SKIN CRACKS AT BS 500A TO BS 520, STR 9L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041130000492004113000049EA 2004 11 30 SWIA200414086 120041104A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS LACK OF LUBE A SWIAO OTHER WFJINADEQUATE Q C FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07955SW 7817 FLAPS DEGRADED STATUS MESSAGE IN FLIGHT. LUBRICATED FLAP ACTUATORS IAW AMM 12-20-27. OPERATIONAL TEST OF SKEW DETECTION SYSTEM GOOD IAW AMM 27-51-15. 2L72 4F RTA21EA 20041130000622004113000062EA 2004 11 30 COMA0460621 120041113A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB UNRELIABLE A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01916CA4739 2189 7014 FLIGHT 9474 STAB TRIM AND MACH TRIM CAUTION MESSAGE. REPLACED THE HSTA AND MCU. 2L72 4F RTA21EA 20041130000632004113000063EA 2004 11 30 COMA0460622 120041114A5610NP1393226 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER DEDESCENT 1 SO01958CA13813 7111 FLIGHT 5905 CO-PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2L72 4F RTA21EA 20041130000662004113000066NM 2004 11 30 AWXA200401292 120041116A3397BMS13311122 WIRE BOEING737 7373Y0 1384671NM SEAT ROW 19 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28331AW 23747 PHX - EEL - DURING THRU-FLIGHT INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041130000682004113000068EU 2004 11 30 AWXA200401294 120041023A5315D5347218920000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 68. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT AT FR 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000732004113000073EA 2004 11 30 COMA0460617 120041113A2752854D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01977CA5251 7157 FLIGHT 4939 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT OUTBOARD FLAP ACTUATOR. 2L72 4F RTA21EA 20041130000922004113000092NM 2004 11 30 CALA0400723 120041121A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 328, LBL 29 TO RBL 58. THE FLOORBEAM UPPER CHORD WAS REPLACED IAW SRM 53-10-51. 2L72 4F RTA16WE 20041130001122004113000112SO 2004 11 30 RAIA00411016 120041113A2120 ODOR EMB 145 EMB145LR 3260212SO LAVATORY DETECTED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03846HK 14500855 ORB - LAV SMOKE WARNING WITH STRONG SMOKE ODOR. MAINTENANCE TROUBLESHOT WITH FAULT ISOLATION MANUAL WITH NO DEFECTS NOTED. LAV SMOKE DETECTOR OPS CHECKS GOOD, NO DEFECTS NOTED. 2L72 4T RTT00011AT 20041130001142004113000114SO 2004 11 30 SWIA200414071 120041109A3340 LIGHT EMB 120 EMB120ER 3260203SO CABIN SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07236SW 120312 MIDDLE STORM LIGHT SMOKES AT THE LEADS WHEN OPERATED. REPLACED MIDDLE STORM LIGHT IAW 33-21-02, OPERATIONAL CHECK GOOD. P/N 10-21C22-513, S/N OFF 151. 2L72 4T RTA31SO 20041130001192004113000119EA 2004 11 30 SWIA200414075 120041102A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07712SK 10172 AFTER STAB TRIM TEST SSCU 1 FAULT MESSAGE STATUS ILLUMINATED. REMOVED AND REPLACED SSCU NR 1 IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130001342004113000134NM 2004 11 30 MASA200400276 120040518A2910DSC4871 CHECK VALVE DHAV DHC8 DHC8201 2809001NM NR 2 HYD SYSTEM INOPERATIVE A MASAO OTHER J WARNING INDICATION LDLANDING 1 SW07989HA 427 THE AIRCRAFT LANDED IN PHX WITH NO HYDRAULICS IN THE NR 2 SYSTEM. MX MOVED THE AIRCRAFT TO THE HANGER AND FOUND THE AFT EQUIPMENT BAY COVERED IN HYD FLUID. IN THE PROCESS OF TROUBLESHOOTING THE PROBLEM. MX REPLACED THE NR 2 SPU PRESSURE MON CHECK VALVE AND REPLACED NR 2 HYD SYSTEM PIPE ASSY AT RT WING ROOT. 2H72 4T RTA13NM 20041130001392004113000139EU 2004 11 30 RAIA00411015 120041113A3097C40648 WIRE HARNESS JETAIRJETSTMJETSTM4101 1500501EU PROP HEAT FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK 41079 RIC - RIGHT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED PROP BOOT HARNESS NR 4 BLADE RIGHT PROP. 2L72 4T RTA41NM 20041130001432004113000143EA 2004 11 30 MASA200400361 120040620A3110 DISPLAY CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A MASAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 SW07507MJ 10077 THE CREW ABORTED TAKEOFF AND RETURNED TO GATE DUE TO THE CAPTAINS PRIMARY FLIGHT DISPLAY FAILING TO DISPLAY MULTIPLE PRIMARY FLIGHT INSTRUMENT DATA MOMENTARILY. MAINTENANCE WAS CALLED TO THE AIRCRAFT AND INSPECTED THE GENERAL SECURITY OF COMPONENTS IN THE EQUIPMENT BAY, THE SECURITY OF THE CAPTAINS PRIMARY FLIGHT DISPLAY AND PERFORMED A CHECK OF THE SYSTEM PER FIM WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041130001622004113000162EU 2004 11 30 MALA040686 120040929A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, LBL 18.5 SEAT TRACK CORRODED FROM STA 291 TO STA 339. MAINTENANCE REPAIRED IAW MESABA EO 53060. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041130001642004113000164EU 2004 11 30 MALA040684 120040929A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, SUPPORT ANGLE BETWEEN FRAMES 236.5 AND 252.0 CORRODED REPLACED IAW SAAB SRM 51-40-21. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041130001692004113000169NM 2004 11 30 2004UALA01051 120041112A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME INBOARD FLANGE DENTED AT BS 1320 BETWEEN STR 25L AND 27L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001722004113000172NM 2004 11 30 2004UALA01054 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME DENTED AT STA 1580 ABOVE STRINGER S26L. INSTALLED NESTED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041130001792004113000179NM 2004 11 30 2004UALA01126 120041110A3397 WIRE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29319UA 23951 EMERGENCY EEL LIGHTS ROWS 15ABC TO 21ABC ARE INOPERATIVE. REPLACED LOWER FEEDER WIRE. 2L72 4F4 FRTA16WE E2GL 20041130001882004113000188NM 2004 11 30 2004UALA01060 120041115A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 EXTERNAL FUSELAGE STA 736.5 BETWEEN STR 27L AND 28L INTERCOSTAL FASTENER HAS STATIC DISCHARGE HOLE OUT OF LIMITS. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER FOR SKIN. 2L72 4F4 FRTA2NM E17NE 20041130002262004113000226EU 2004 11 30 AWXA200401331 120041121A5610 WINDSHIELD AIRBUS320 A320232 3930326EU FUSLEAGE CRACKED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28602AW 565 EN ROUTE, AT FL 370 THE FO`S WINDSHIELD CRACKED WHEN HEATING ELEMENT BURNED THROUGH, DIVERTED INTO ABQ & LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW AMM, & WINDOW HEAT COMPUTER, OPERATIONAL TEST GOOD. FAILURE ANALYSIS OF WINDSHIELD, OUTBOARD GLASS PLY FRACTURED WITH ORIGIN OF FRACTURE 4.9 INCHES FROM AFT EDGE & 9.8 INCHES FROM BOTTOM EDGE OF WINDSHIELD. AN ELECTRICAL ARC PATH ORIGINATED AT BOTTOM CONDUCTIVE BUSS BAR & TRAVELED ACROSS HEATING FILM VISION AREA OF WINDSHIELD TO ORIGIN OF FRACTURE. IN AREA SURROUNDING BOTTOM CONDUCTIVE BUSS BAR EVIDENCE OF MOISTURE INGRESSION NOTED. MOISTURE INGRESSION ALSO NOTED IN SEVERAL OTHER LOCATIONS AROUND WINDOW. 2L72 4F RTA28NM 20041130002272004113000227EU 2004 11 30 AWXA200401332 120041124A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 221 FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW373233540 091 ORD - EEL - DURING 8-DAY CHECK TEST OF EMERGENCY LIGHT SYSTEM FOUND THE LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL) INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (10WL) AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041130002282004113000228EU 2004 11 30 AWXA200401333 120041116A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 251RF BETWEEN FR 58 AND FR 62. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 251RF IAW A320 SRM 53-02-00. 2L72 4F RTA28NM 20041130002292004113000229EU 2004 11 30 AWXA200401334 120041115A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK A 16 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL 231QF BETWEEN FR 28 AND FR 32. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 231QF IAW A320 SRM 53-02-00. 2L72 4F RTA28NM 20041130002302004113000230EU 2004 11 30 AWXA200401335 120041112A5320D53112821200 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM -Y254 BETWEEN FR 17 AND FR 19. MAINTENANCE CUT OUT DAMAGE IN FLOOR SUPPORT BEAM -Y254 FROM FR 17 TO FR 19; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, FIG 201. 2L72 4F RTA28NM 20041130002312004113000231EU 2004 11 30 AWXA200401336 120041116A5321D5367175000000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CABIN FLOOR PANEL 251YF WAS FOUND DELAMINATED BETWEEN FR 62 AND FR 64. MAINTENANCE CUT OUT DAMAGE IN CABIN FLOOR PANEL 251YF AND PERFORMED BOND REPAIR IAW A320 SRM 53-12-00 FIG 204. 2L72 4F RTA28NM 20041130002322004113000232EU 2004 11 30 AWXA200401337 120041112A5320D5347209000300 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BEAM -Y765 ON FORWARD SIDE OF FR 66. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM -Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130002332004113000233NM 2004 11 30 AWXA200401282 120041102A5320146N872263 WEB BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK 2 EACH CRACKS WERE FOUND IN CABIN FLOOR STRUCTURE WEB BETWEEN BS 1620 AND BS 1640, STR 17 R/T, WL 208. MAINTENANCE REMOVED CRACKED WEB FROM BS 1620 TO BS 1640; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 146N8722; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041130002342004113000234NM 2004 11 30 AWXA200401283 120041031A532065566551 WEB BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND IN AFT CARGO DOOR CUTOUT AFT TORQUE BOX LOWER WEB AT BS 842. MAINTENANCE REMOVED CRACKED WEB AT BS 842; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-56655; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 10. 2L72 4F RTA16WE 20041130002362004113000236SO 2004 11 30 SWIA200414148 120041005A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FUSELAGE; CORROSION FOUND ON SEAT TRACK (BROWN LINE) AND AROUND SCREW HEADS MARKED AT FR 17 - FR 32, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT TRACK IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, AMM 20-00-00. 2L72 4T RTA31SO 20041130002382004113000238SO 2004 11 30 SWIA200414149 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 AFT FUSELAGE BAGGAGE PIT, FRAME 44, FLOOR CROSSBEAM CORRODED. REPLACED CROSSBEAM IAW SRM 51-40-02 AND 51-25-00. 2L72 4T RTA31SO 20041130002392004113000239NM 2004 11 30 2004UALA01112 120041114A5241 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GALLEY DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 FWD GALLEY DOOR EXT SKIN IS CRACKED AT THE LWR HINGE CUTOUT. TRIMMED OUT DAMAGE AND INSTALL REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20041130002402004113000240NM 2004 11 30 AWXA200401313 120041014A5320146N5318 SHEAR PLATE BOEING757 757225 1384959NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SHEAR DECK BETWEEN BS 1680 AND BS 1720, LBL 0 AND LBL 54. MAINTENANCE REMOVED CORRODED SHEAR DECK FROM BS 1680 TO BS 1720, LBL 74 TO RBL 74; FABRICATED A NEW REPLACEMENT SHEAR DECK; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041130002412004113000241NM 2004 11 30 AWXA200401314 120041014A5320146N5318 SHEAR PLATE BOEING757 757225 1384959NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SHEAR DECK BETWEEN BS 1680 AND BS 1720, RBL 0 AND RBL 54. MAINTENANCE REMOVED CORRODED SHEAR DECK FROM BS 1680 TO BS 1720, LBL 74 TO RBL 74; FABRICATED A NEW REPLACEMENT SHEAR DECK; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041130002422004113000242NM 2004 11 30 AWXA200401315 120041014A5320146N5300 CHANNEL BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL BETWEEN BS 1697 AND BS 1716, AT RBL 7. MAINTENANCE REMOVED CORRODED HAT CHANNEL FROM BS 1697 TO BS 1716, RBL 7; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041130002432004113000243NM 2004 11 30 AWXA200401316 120041014A5320146N530012 CHANNEL BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL AT BS 1682, LBL 4. MAINTENANCE REMOVED CORRODED HAT CHANNEL FROM BS 1690 TO BS 1716, LBL 4; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041130002442004113000244NM 2004 11 30 AWXA200401317 120041112A532069353654 ATTACH ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN UPPER ATTACH ANGLE OF FLOOR INTERCOSTAL BETWEEN BS 380 AND BS 400, BL 0. MAINTENANCE REMOVED CORRODED UPPER ATTACH ANGLE ON FLOOR INTERCOSTAL FROM BS 380 TO BS 400, BL 0; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-35365-4; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20041130002462004113000246EA 2004 11 30 COMA0470079 120041114A2780 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLATS ILLUMINATED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01371CA 10082 FLIGHT 5500 SLAT FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041201000052004120100005NM 2004 12 1 DL73S041038 120041116A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 A 1 INCH CRACK WAS FOUND IN THE CORNER OF THE LOWER HINGE CUTOUT OF THE L2 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND THE UNDERLYING BEARSTRAP INSPECTED TO ENSURE IT WAS CRACK FREE. THE SKIN CRACK CUTOUT WAS REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER B737 SRM AND PER ER/A 095094-14. 2L72 4F RTA16WE 20041201000132004120100013SO 2004 12 1 MASA200400620 120041101A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 THE CREW REPORTED THE EMERGENCY EXIT SIGN ON THE GALLEY BULKHEAD NOT ILLUMINATING DURING TEST. MX REMOVED AND REPLACED AC/DC INVERTER AND THE SYSTEM TESTED NORMALLY. 2L72 4T RTT00011AT 20041201000182004120100018NM 2004 12 1 2004UALA01147 120041117A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 5E LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29196UA 28715 EMERGENCY EXIT PATH LIGHTING IS FALLING OFF AT SEAT 5E. RESECURED EEL LIGHT. 2L74 4F4 FRTA20WE E24NE 20041201000302004120100030NM 2004 12 1 2004UALA01137 120041116A5330 SKIN BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29128UA17475 30023 FOUND DENT ON RIGHT SIDE OF FUSELAGE APPROXIMATELY 4 FT FORWARD AND 4 FT BELOW DOOR 5R. DENT IS APPROXIMATELY 2.5" WIDE BY 3" HIGH BY .1875" DEEP. *S/D* SKIN REPAIR APPLIED TO CUT OUT DENT. MAJOR REPAIR ACCOMPLISHED WITH SKIN DOUBLER PER SRM. 2L74 4F4 FRTA20WE E24NE 20041201000312004120100031EA 2004 12 1 MASA200400513 120040909A26214739172 FIRE BOTTLE CNDAIRCL600 CL6002D24 1390016EA APU DISCHARGED A MASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07924FJ394 15024 RETURNED TO GATE DUE TO SMOKE IN THE COCKPIT AND CABIN CAUSED BY DE-ICE FLUID BEING SPRAYED INTO THE APU INTAKE DURING DE-ICE OPERATIONS. THE CABIN WAS EVACUATED THROUGH THE MAIN CABIN DOOR AT THE DE-ICE PAD. MAINTENANCE PERFORMED A GVI OF THE APU AND AIR DUCTS AND RAN THE ENGINES TO OPERATE THE PACKS AND CLEAR THE SYSTEM OF FUMES. THE APU FIRE BOTTLE WAS FOUND DISCHARGED AND THE APU WAS INOP AFTER THIS EVENT. 9/9 THE SMOKE WAS FOUND TO BE GLYCOL MIST, OPS CHECKED AT AIR CONDITION SYSTEM, NO FURTHER ACTION. APU FIREX BOTTLE WAS REPLACED. 2L72 4F RTA21EA 20041201000322004120100032NM 2004 12 1 2004UALA01138 120041117A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29333UA 24228 LAST 6 ROWS OF EMERGENCY FLOOR LIGHTING INOP. REPLACED POWER STRIP FOR AFT SET OF FLOOR LIGHTS. CHECKS GOOD. 2L72 4F4 FRTA16WE E2GL 20041201000342004120100034EU 2004 12 1 AWXA200401296 120041023A5320D5311206720001 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LONGITUDINAL FLOOR SUPPORT WEB Y1584 LT BETWEEN FR 20 AND FR 21. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOOR SUPPORT WEB Y1584 LT FROM FR 20 TO FR 21; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 7. 2L72 4F RTA28NM 20041201000362004120100036EU 2004 12 1 AWXA200401298 120041025A5320D5347219020590 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 65+23 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201000402004120100040NM 2004 12 1 2004UALA01115 120041110A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 RIGHT FWD FUSELAGE DENTED AND SCRATCHED APPROX 1 FT AFT OF JACKING POINT. REMOVED EXISTING TIME-LIMITED SKIN DOUBLER AND REPLACED WITH NEW DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041201000412004120100041NM 2004 12 1 2004UALA01116 120041113A3350 SOCKET BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE FAULTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 R-1 EXTERNAL EMERGENCY SLIDE ILLUMINATION LIGHT HAS A FAULTY SOCKET ASSEMBLY. REPLACED FAULTY SOCKET. PERFORMED SUCCESSFUL OPERATION CHECK OF LIGHT. 2L72 4F4 FRTA2NM E17NE 20041201000422004120100042NE 2004 12 1 ARWA20041001 220041007A7200 ENGINE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 2 VIBRATION A ARWAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO19791AL520082295 46150 671360 NR 2 ENGINE HUMMING NOISE CHANGING IN PITCH DIRECTLY PROPORTIONAL TO VIBRATION IN THROTTLE, ALL OTHER PARAMETERS NORMAL, POWER RETARDED TO IDLE, HUMMING & VIBRATION STOPPED. REMOVED AND REPLACED NR 2 ENGINE PER JOB CARD DC8-UM-003. OPERATIONAL CHECK ON ENGINE RUN NORMAL. 2L74 4F4 F 4A25 1E8 20041201000462004120100046EA 2004 12 1 SWIA200414133 120041024A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 FS 484 RIGHT SIDE, OUTBOARD INTERCOSTAL, INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER REO 601R-53-0029. 2L72 4F RTA21EA 20041201000482004120100048SO 2004 12 1 MASA200400602 120041026A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAK NONE O OTHER ININSP/MAINT 1 SW07853MJ 145464 EMERGENCY LIGHT ON THE SIDEWALL IS INOPERATIVE. MX RECONNECTED A LOOSE CONNECTION AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20041201000492004120100049EU 2004 12 1 AWXA200401299 120041023A5320D53472133200 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM -Y48 RT AT FR 66. MAINTENANCE REMOVED CORRODED FLOORBEAM -Y48 RT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201000502004120100050EA 2004 12 1 MASA200400244 120040503A2420 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775983 7481 CREW REJECTED THE TAKEOFF DUE TO AN IDG 1 CAUTION DURING TAKEOFF. CONTRACT MX WAS CONTACTED AND PERFORMED THE REQUIRED MAINTENANCE ACTION TO DEFER THE IDG AND AIRCRAFT TIME OF DISCONNECT WAS ENTERED INTO THE IDG LOG. MX SERVICED & RESET IDG. OPS CHECKED GOOD. 2L72 4F RTA21EA 20041201000512004120100051NM 2004 12 1 2004UALA01117 120041113A3350 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 R-2 DOOR EEL EXIT MARKER WIRE IS BROKEN. REPAIRED WIRE REF GNMM 2-0-15-001 AND OPS CHECKED. 2L72 4F4 FRTA2NM E17NE 20041201000522004120100052NM 2004 12 1 AWXA200401303 120041102A575465C2679312 SKIN BOEING737 7373Y0 1384671NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK 3 EACH .125 INCH CRACKS WERE FOUND IN NR 6 SLAT LOWER SKIN AT AFT ROW RIVET HOLES INBOARD OF ACTUATOR ATTACH FITTINGS SLAT STA 291 RT THRU SLAT STA 294 RT. MAINTENANCE CUT OUT DAMAGE IN NR 6 SLAT LOWER SKIN FROM SS 291 RT TO SS 294 RT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PART IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20041201000542004120100054EU 2004 12 1 MALA040677 120040929A3350 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY LIGHTS AT 46LN, 47LN INOP. REPLACED IAW SAAB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041201000562004120100056EU 2004 12 1 AWXA200401324 120041116A5755D5755103920051 BOLT AIRBUS320 A320232 3930326EU SPOILER HINGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - FLIGHT CONTROL - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON NR 2 SPOILER HINGE BOLTS WS 613 LT AND WS 670 LT. MAINTENANCE REMOVED AND REPLACED NR 2 LT SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-44-020-050-B, AND SUBTASK 27-64-44-420-050-B. 2L72 4F RTA28NM 20041201000602004120100060SO 2004 12 1 MASA200400601 120041026A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07828MJ 145218 EMERGENCY EXIT SIGN AT ROW 12 INOPERATIVE. MX REPLACED THE LAMPS IN THE SIGN. AWAITING PART INFO. 10/27/04 MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041201000612004120100061EA 2004 12 1 SWIA200414057 120041030A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 484.0 RIGHT HAND INTERCOSTAL INBOARD AND OUTBOARD FLANGE RBL 27 AND RBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20041201000632004120100063WP 2004 12 1 AALA20041141 120041118A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21279AA 49295 DEN - EMERGENCY CEILING LIGHTS AT SEATS 9 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEATS 9 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041201000642004120100064EA 2004 12 1 SWIA200414065 120041107A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07918SW 7645 BACK EMERGENCY LIGHTS INOPERATIVE. REMOVED BATTERY AND CLEANED CONTACTS. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041201000682004120100068EA 2004 12 1 SWIA200414081 120041111A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07459SW 7782 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041201000702004120100070EA 2004 12 1 MASA200400397 120040709A3350110049 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0775984 7489 LEFT AND RIGHT EXTERIOR FWD EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED POWER SUPPLY. 2L72 4F RTA21EA 20041201000712004120100071SO 2004 12 1 MASA200400451 120040813A3350 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 EMERGENCY EXIT SIGN INOP AT RIGHT ROW 3. MX COULD NOT DUPLICATE FAULT. 2L72 4T RTT00011AT 20041201000732004120100073NM 2004 12 1 MASA200400527 120040914A3320 BALLAST DHAV DHC8 DHC8201 2809001NM CABIN LIGHTS BURNED OUT A MASAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07991HA 431 AT GATE, EVACUATED PASSENGERS AND CREW DUE TO SMOKE IN THE CABIN COMING FROM TWO CEILING LIGHT BALASTS AT ROW 3 AND 4 LEFT SIDE ARCHING. PULLED CIRCUIT BREAKERS S-1 AND S-2. REMOVED BULBS. PLACED ON MEL AND RELEASED AIRCRAFT. 9/23/04 MAINTENANCE REPLACED BALLAST RECEPTACLE. 2H72 4T RTA13NM 20041201000742004120100074EU 2004 12 1 AWXA200401266 120041025A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201000752004120100075WP 2004 12 1 MWEA040209 120041117A53125910130394 STRAP DOUG DC9 DC982 3022082WP BULKHEAD DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 AFT PRESSURE BULKHEAD TEE HAS FOUR HOLES WITH TOO SHORT OF EDGE DISTANCE IN FORWARD UPPER FLANGE OF TEE BETWEEN LONGERON 18 RIGHT AND 17 RIGHT. SUBMITTED TO BOEING FOR DISPOSITION. FABRICATED AND INSTALLED NEW STRAPS AND FASTENERS. 2L72 4F A6WE 20041201000762004120100076WP 2004 12 1 MWEA040206 120041101A53305920323555 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 SKIN DENT AT STATION 294 LONGERON 24 RIGHT. FOUND TO BE OUT OF LIMITS. REMOVED DOUBLER, COLD WORK SKIN AND INSTALLED DOUBLER. 2L72 4F A6WE 20041201000772004120100077EU 2004 12 1 MALA040696 120041013A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N 9812869 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/6/04. 2L72 4T RTA52EU 20041201000792004120100079EU 2004 12 1 MALA040687 120040915A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15434XJ 340B434 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1464 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BOTH CELL PACKS P/N 549-1324-06 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04. 2L72 4T RTA52EU 20041201000832004120100083NM 2004 12 1 DL73S041044 120041120A534265495997 ATTACH FITTING BOEING737 737247 138448DNM VERT STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 BODY CLEVIS LUGS FOR VERTICAL STABILIZER ATTACH FITTINGS CORRODED. REPAIRIED IAW ERA 095009-14. 2L72 4F A16WE 20041201000842004120100084NM 2004 12 1 DL76L041045 120041120A2133211001812 OUTFLOW VALVE BOEING767 767332 1382001NM CABIN PRESSURE INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27183DN 27110 DID NOT PRESSURIZE DURING CLIMBOUT WITH EQUIP COOLING OVERHEAT MESSAGE. QRH PROCEDURE PERFORMED. CABIN OUTFLOW VALVE FULLY CLOSED. DIFF PRESS .08 MAX. C.A.T HAD FWD DK SUP FLOW AND FWD EQU SUP FLOW EICAS MSG. FOUND OVERBOARD EXHAUST VALVE NOT LOCKED CLOSED OVERCENTER AFTER EXTENSIVE T/S PER FIM 21-58-00. PRESSURIZED AIRCRAFT WITH APU AIR 3 LBS POSITIVE. NO LEAKS FOUND. OUTFLOW VALVE OPN NORMAL IN STDBY AND AUTO 1 AND AUTO 2. EXHAUST VALVE IS ON MCO/PLACARD PER MEL 21-58-01. 2L72 4F RTA1NM 20041201000852004120100085NM 2004 12 1 DLM88041046 120041120A33201565 BALLAST DOUG MD88 MD88 3023688NM GALLEY OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27919DE 53422 FIRST CLASS GALLEY COUNTER WORK LIGHT BALLAST OVERHEATED CAUSING HOT ODOR. REPLACED SAME. 2L72 4F RTA6WE 20041201000872004120100087EU 2004 12 1 MALA040693 120041004A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15453XJ 340B453 DURING CAPACITY INSPECTION IN MSP, BATTERY POWER SUPPLY P/N 3301-41, S/N 2222 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/5/04. 2L72 4T RTA52EU 20041201000892004120100089EU 2004 12 1 YENA200449 120041007A5270 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU EMERGENCY EXIT OUT OF ADJUST A YENAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15585JB 2159 AFTER TAKEOFF GOT ECAM BOTH RT SIDE OVERWING EMERGENCY EXITS SHOWING DEPLOYED OR OPEN. ITEM WAS DEFERRED PER MEL 52-70-01. LATER PROX SWITCHES 19WV2 & 21WV2 WAS ADJUSTED IAW 52-71-13. 2L72 4F RTA28NM 20041201000912004120100091NM 2004 12 1 F3LA200400111 120041005A5270 WARNING LIGHT BOEING737 73736Q 1384409NM PAX DOOR FALSE INDICATIONA F3LAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03307FL 28760 REJECTED TAKEOFF. FLIGHT CREW REPORTED FWD ENTRY DOOR LIGHT ILLUMINATED. CHECKED DOOR PROXIMITY SENSOR PER MM 52-71-11 AND CHECKED NORMAL. 2L72 4F RTA16WE 20041201000922004120100092EU 2004 12 1 MALA040699 120041013A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15512XJ E2326 DURING CAPACITY INSPECTION IN MSP, EMERGENCY BATTERY PACK P/N 61-2275-1, S/N 9803379 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE DEEP CYCLED & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/16/04. 2H74 4F RTA49EU 20041201000942004120100094EU 2004 12 1 MALA040700 120041013A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15511XJ E2325 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 61-2275-1, S/N 9908128 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/16/04. 2H74 4F RTA49EU 20041201000952004120100095EU 2004 12 1 MALA040701 120041013A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15444XJ 340B444 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2085 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/13/04. 2L72 4T RTA52EU 20041201000962004120100096EU 2004 12 1 MALA040702 120041019A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15417XJ 340B417 DURING CAPACITY INSPECTION IN MSP, EMERGENCY BATTERY SUPPLY P/N 3301-51, S/N 2056 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31, S/N 2056 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/13/04. 2L72 4T RTA52EU 20041201000972004120100097EU 2004 12 1 MALA040690 120040928A3350 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15503XJ E2310 DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-2275-1, S/N 9801237 WAS REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE DEEP CYCLED UNIT & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04. 2H74 4F RTA49EU 20041201000982004120100098EU 2004 12 1 MALA040691 120040927A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15511XJ E2325 DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-2275-1, S/N 9804487, WAS REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BOTH CELL PACKS P/N 61-2274-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04. 2H74 4F RTA49EU 20041201000992004120100099EU 2004 12 1 MALA040692 120041004A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15453XJ 340B453 DURING CAPACITY INSPECTION IN MSP, BATTERY POWER SUPPLY P/N 3301-51, S/N OFF 2170 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/5/04. 2L72 4T RTA52EU 20041201001002004120100100WP 2004 12 1 AALA20041152 120041122A1420 PIN DOUG DC9 DC983 3022083WP CONNECTOR LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219620D 53591 MSP - EMERGENCY LIGHT ON INBOARD EDGE OF SEAT 18D HAS LOOSE WIRE PIN AT PLUG. REINSERTED PIN INTO RECEPTICAL FOR EMERGENCY LIGHT ON INBOARD EDGE OF SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041201001012004120100101EA 2004 12 1 COMA0460612 120041111A3230555406 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926CA 7027 FLIGHT 5330 GEAR DISAGREE WARNING. REPLACED THE NLG DOORS SELECTOR VALVE. 2L72 4F RTA21EA 20041201001032004120100103EA 2004 12 1 COMA0460614 120041112A3297601R572221PE WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926CA 7027 FLIGHT 5165 GEAR DISAGREE WARNING. REPLACED THE NLG DOORS MICRO SWITCH HARNESS. 2L72 4F RTA21EA 20041201001042004120100104 2004 12 1 MWEA040194 420041022A2565100502119 SLIDE DOUG DC9 DC981 3022081WP AFT GALLEY DISCHARGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 AFT GALLEY SLIDE PRESSURE INDICATOR IS INDICATING IN THE RED (READS 2000 PSI). REMOVED AND REPLACED AFT GALLEY DOOR SLIDE. 2L72 4F A6WE 20041201001082004120100108 2004 12 1 SWIA200414094 420041114A3418501125801 CAPSTAN CNDAIRCL600 CL6002B19 1900309EA STICK PUSHER INOPERATIVE A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07932SW 7714 FIRST FLIGHT STALL TEST PRODUCED BINDING NOISES. REPLACED CAPTAINS STICK PUSHER ASSY IAW AMM 27-35-20. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041201001112004120100111 2004 12 1 YENA200451 420041023A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU SEAT 20E UNKNOWN A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15587JB2430 2177 NR 1 F/A REPORTED ELECTRICAL SMOKE SMELL IN MIDDLE OF CABIN UPON ACTIVATING LTV SYSTEM. PERFORMED INFO NOTICE 2004-T023TR AND TSM 24-00-00-810-823. NOTICED FAINT ODOR AT ROW 20. NO OTHER DISCREPANCIES NOTED. DEFERRED LTV SYSTEM PER MEL 25-22-03. ON 10/24/04 FOR PRECAUTIONARY REASONS REPLACED SEB AT ROW 20E. PERFORMED TASK CARD 233900-J1-17 AND NO EVIDENCE OF ELECTRICAL ODOR. CLEARED MEL AND A/C RELEASED FOR SERVICE. 2L72 4F RTA28NM 20041201001132004120100113NM 2004 12 1 F3LA200400105 120040930A532065C807351 SILL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED R2 MOP SILL CORRODED. REPLACED R2 MOP SILL PER SRM 51-10-2 AND 51-40-02. 2L72 4F RTA16WE 20041201001172004120100117NM 2004 12 1 F3LA200400110 120041004A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING A-4 CHECK, INSPECTION REPORTED PARTITION SUPPORT CORRODED AT FLOORBEAM, STA 986.5 - 1006, RBL 16. REPLACED PARTITION SUPPORT AT FLOORBEAM PER SRM 51-40-06 AND DRAWING 65C32675. 2L72 4F RTA16WE 20041201001182004120100118EA 2004 12 1 SWIA200414083 120041111A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07459SW 7782 FS 621 FLOOR SUPPORT ANGLE RIGHT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PIECES IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20041201001212004120100121EA 2004 12 1 SWIA200414117 120041120A2760 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07975SW 7951 AFTER LANDING, O/B GROUND SPOILER CAUTION MESSAGE DISPLAYED. REMOVED AND REPLACED OUTBOARD GROUND SPOILER MANIFOLD IAW 27-63-05, OPERATIONAL CHECK GOOD IAW 27-65-00. 2L72 4F RTA21EA 20041207001712004120700171WP 2004 12 7 DHL2004801503 120040901A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT WING CTR L/E UPPER FORMER CRACKED 0.500, STA XFS 360.250. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20041208000012004120800001 2004 12 8 SWAA043471 420041130A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208000152004120800015NM 2004 12 8 SWAA043458 120041128A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29373SW 26581 DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED LT T/E AFT FLAP PER SRM. 2L72 4F RTA16WE 20041208000302004120800030NM 2004 12 8 04FDEA03165 120041118A5754 HINGE BOEING727 727100 1384036NM KRUGER FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25166FE BN267 18863 CORROSION ON LT WING NR 1 K-FLAP O/B BULLNOSE HINGE LUG AROUND FASTENERS UPPER SURFACE. 2L73 4F RTA3WE 20041208000372004120800037CE 2004 12 8 DXTA200400463 120041130A5610 WINDOW CESSNA750 750 2076810CE COCKPIT FAILED E DXTAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL07967QS 7500067 DURING CRUISE FLIGHT AT FL 410, WINDSHIELD HEAT INOP R CAS MESSAGE ILLUMINATED. TEN SECONDS LATER, LEFT WING SHIELD OUTER PANE SHATTERED, ELECTIRICAL ARCING WAS OBSERVED BETWEEN PANE. PERFORMED EMERGENCY DESCENT AND DIVERSION TO KFLO. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20041208000562004120800056WP 2004 12 8 04FDEA03269 120041130A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 330 BETWEEN LONGERONS 37 RIGHT TO 38 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE REQUIREMENTS. CUT OUT DAMAGED AREA OF SKIN, FABRICATED AND INSTALLED FILLER SHIMS, INNER AND OUTER DOUBLERS AND INTERNAL FINGER DOUBLERS IAW DC10 SRM 53-20-00 VOL 1 FIGURE 6, SHEET 5 AND 51-21-01 VOL 2. 2L73 4F RTA22WE 20041208000582004120800058WP 2004 12 8 04FDEA03253 120041129A5710ARC0340504 PANEL DOUG MD10 MD1010F 3022112WP ZONE 200 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 RIGHT WING INBOARD FLAP AREA LEFT HAND FALSE SPAR CEILING PANEL INBOARD OF MAIN LANDING GEAR STRUT DELAMINATED/DENTED. REMOVED FILLET PANELS 152FT, 152ET AND SMALL PANEL OUTBOARD OF DAMAGED PANEL IAW DC10 SRM 51-31-01 VOL 2, TO FOM. REMOVED DELAMINATED PANEL IAW DC10 SRM 51-31-01 VOL 2. REPAIRED DELAMINATED PANEL IAW FEDEX EA 8-5710-81524, WING- RIGHT HAND UPPER WING PANEL ASSEMBLY MAIN LANDING GEAR FITTING TO FUSELAGE CENTER UPPER- REPAIR. REINSTALLED REPAIRED PANEL IAW DC10 SRM 51-31-01 VOL 2. REINSTALLED FILLET PANELS 152FT, 152ET AND SMALL PANEL OUTBOARD OF REPAIRED PANEL IAW DC10 SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20041208000652004120800065NM 2004 12 8 04FDEA03169 120041119A5347 SEAT TRACK BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25208FE 22930 MAIN DECK - SEAT TRACK STA 1150 - 1170, BL 0 - LUGS GOUGED. BLENDED GOUGED AREA IAW SRM 53-10-1, FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-30-2, FABBED NEW SEAT TRACK FROM 60-5017/7178-T6511 BATCH 746883 AND INSTALLED IAW SRM 51-30-2. 2L73 4F RTA3WE 20041208000832004120800083NM 2004 12 8 SWAA043510 120041201A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT EQUIPMENT COOLING EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041208000872004120800087NM 2004 12 8 SWAA043524 120041204A143018A80101 BOLT BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT NR 1 HINGE TAB BOLT PER MM. 2L72 4F RTA16WE 20041208001042004120800104EU 2004 12 8 MALA040724 120040909A5414 COWLING BAC 146 AVRO146RJ85A1500097EU NR 4 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, NR 4 ENGINE LEFT ZONE 2 COWL CHAFED IN PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041208001152004120800115NM 2004 12 8 DLM90041056 120041123A24101B1893 ELECTRICAL SYS DOUG MD90 MD9030 3023690NM IAE V2528 V2528D5 NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27914DN 53394 020101 LEFT ELEC SYSTEM FAILED EN ROUTE. REPLACED LEFT ECU. 2L72 4F4 FRTA6WE E40NE 20041208001182004120800118EA 2004 12 8 MASA200400650 120041122A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 ASH 6428 PHX-DSM. ESCAPE PATH LIGHTING INOP FROM ROW 9 AFT. MAINTENANCE SECURED THE CONNECTION AND THE LIGHTS, OPS CHECKED GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20041208001212004120800121NM 2004 12 8 DL73S041057 120041124A5730 SKIN BOEING737 737247 138448DNM LT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 LT LOWER WING SKIN WORN AT FUEL TANK ACCESS DOOR CUTOUT. REPAIRED IAW ERA 094867-14. 2L72 4F A16WE 20041208001252004120800125NM 2004 12 8 SWAA043466 120041130A335065C34691 LIGHT BOEING737 7373H4 1384600NM ROW 19 DEF LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 19 DEF, LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041208001292004120800129NM 2004 12 8 DL764041065 120041127A3350 LAMP BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27832MH 29704 RT AISLE OVERHEAD EMERGENCY ESCAPE PATH LIGHTING 1 EA INOP AT MID GALLEY. RELAMPED SAME. 2L72 4F RTA1NM 20041208001382004120800138EU 2004 12 8 MALA040712 120040910A5230 SKIN BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, AFT CARGO DOOR INNER SKIN HAS SEVERAL PATCHES OF CORROSION. MAINTENANCE REPAIRED IAW EO A57061. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208001612004120800161NM 2004 12 8 SWAA043503 120041202A53206545765 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20041208001652004120800165 2004 12 8 SWAA043516 420041203A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD HOOK LOOSE. REMOVED AND REPLACED L1 DOOR FWD HOOK PER SRM. 2L72 4F RTA16WE 20041208001682004120800168NE 2004 12 8 RAIA00411020 220041120A7261 OIL FILTER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE CONTAMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03572HK 41091 PIT - RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE CLEANED CHIP DETECTOR. REMOVED AND REPLACED OIL FILTER, THEN GROUND RAN ENGINE. 2L72 4T4 TRTA41NM E18NE 20041208001702004120800170 2004 12 8 RAIA00411023 420041121A34257003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU NR 1 INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03571HK167751180 41090 STL - NR 1 EADI AND EHSI INOP. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2L72 4T RTA41NM 20041208001712004120800171 2004 12 8 RAIA00411022 420041121A3425700360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU NR 1 MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03552HK15214 41057 STL - CAPTAINS EADI COMPARATOR ERROR PITCH. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2L72 4T RTA41NM 20041208001882004120800188NM 2004 12 8 SWAA043484 120041130A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29766SW 29806 DURING SCHEDULED HC2 CHECK, FWD AND MID CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20041208001922004120800192SO 2004 12 8 SWIA200414156 120041128A2752 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07563SW 120338 ON APPROACH, RECEIVED CONTROL FAULT, ADVANCED SWS FLAP LIGHT ON THE MAP. REMOVED AND REPLACED LT NACELLE ACTUATOR AND FLAP CONTROL COMPUTER IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001962004120800196EA 2004 12 8 SWIA200414160 120041129A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07411SW 7067 ON POST FLIGHT INSPECTION, FIRST OFFICERS FORWARD WINDOW CRACKED ON OUTER PANE. REMOVED AND REPLACED RIGHT WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. P/N: NP-139321-12, S/N OFF: 94259H4059. 2L72 4F RTA21EA 20041209000292004120900029SO 2004 12 9 MASA200400631 120041110A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07837MJ 145367 ASH 2696 CLT-SAV, ABORTED TAKEOFF DUE TO THE E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 11/20/2004 MAINTENANCE REPLACED 2 EACH STOW TRANSIT SWITCH P/N 83-990-168 WITH S/N 1468 AND 0861. 2L72 4T RTT00011AT 20041209000602004120900060 2004 12 9 SWAA043547 420041206A256565C16280 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EVAC SLIDE FWD AND AFT GIRT BAR FLOOR FITTINGS BRACKETS, CORRODED. REMOVED AND REPLACED FWD AND AFT GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20041209000612004120900061NM 2004 12 9 SWAA043555 120041206A57126545445 RIB BOEING737 7375H4 138449DNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO. 2L72 4F RTA16WE 20041209000742004120900074NM 2004 12 9 SWAA043408 120041120A33506104781 CHARGER BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND BOTH L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY PACK CHARGERS PER MM. 2L72 4F RTA16WE 20041209000762004120900076NM 2004 12 9 F3LA200400068 120040626A2700422081100 TRANSDUCER AIRBUSA319 A319111 3930336NM FLT CONTROL INOPERATIVE A F3LAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM03921FR 2662 2010 FLIGHT CREW REPORTED FLIGHT CONTROL ELAC 2 FAULT AFTER NR 2 ENGINE START. PERFORMED AFS TEST PER TASK 22-66-00-810-851. NO FAULTS FOUND. SWAPPED ELAC NR 1 AND NR 2. PERFORMED ELECTRONIC FLIGHT CONTROL SYSTEM TEST. LT AND RT ELEVATOR AND LT AND RT AILERON TESTED OKAY. REPLACED ELAC 2 POSITION TRANSDUCER ON THE ACTUATOR (9CE). OPS CHECK OK PER AMM 27-44-56 AND 27-96-00. 2L72 4F RTA28NM 20041209000852004120900085EA 2004 12 9 MASA200400487 120040829A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX JAMMED A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0737178 7178 MAIN CABIN DOOR JAMMED WHILE OPENING. MAINTENANCE OPS CHECKED AND IT OPERATED NORMAL. 2L72 4F RTA21EA 20041209001082004120900108WP 2004 12 9 GTIA040795 120041001A5210 LATCH DOUG DC9 DC983 3022083WP PWA JT8 JT8D217A 52053NE L1 DOOR OUT OF RIG A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 MAIN ENTRANCE DOOR WILL NOT LOCK. FOUND L1 DOOR INTERLOCK MECHANISM HANGING UP. LUBED SAME. ADJUSTED/RIGGED DOOR, HOLD OPEN LATCH WAS OUT OF RIG/ADJ. 2L72 4F4 FRTA6WE E9NE 20041209001102004120900110EU 2004 12 9 KBM2004F00239 120041008A6520350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR SPLIT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P931 2347 LAMINATED BEARINGS ARE SPLIT. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20041210000352004121000035NM 2004 12 10 QXEA200400811 120041122A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - NR 1 SEAT TRACK HAS CORROSION IN BOTTOM OF TRACK AT X309 AND X424. REPAIRED IAW RD 8-53-1342 AND SRM 51-40-00. 2H72 4T RTA13NM 20041210000382004121000038EA 2004 12 10 QXEA200400816 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AT STATION X650-X652, X658-X661 AND X676-X677. REPAIRED IAW HORIZON AIR EA R-53-239 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20041210000522004121000052NE 2004 12 10 NACA20040056 220041104A8530356993 CYLINDER PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 12 FAILED A NACAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AL0399330818 818 43576 P34459 ABORTED TAKEOFF DUE TO NR 2 ENGINE NR 12 CYLINDER DOUBLE SHORTED SECONDARY AND BACKFIRING. REPLACED NR 2 ENGINE NR 12 CYLINDER. OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20041210000532004121000053GL 2004 12 10 CHQA000588 220041120A7200AE3007A13 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 2 UNSERVICEABLE A CHQAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL11376 1110965 145578 CAE311280 ON ADVANCING THRUST LEVERS, CREW FELT A VIBRATION COMING FROM NR 2 ENGINE, AT THE SAME TIME A TRIPLE CHIME OF "E2 LOW N1". TAKEOFF ABORTED JUST BEFORE 80 KNOTS & TAXIED A SHORT DISTANCE TO J INTERSECTION. AFTER TAKEOFF ABORTED TRIPLE CHIME MESSAGE WENT AWAY & "E2 NO DISP" REMAINED ON. AFTER EXITING RUNWAY NR 2 ENGINE SHUTDOWN. WHEN MZ ARRIVED THEY SAW THE ATS ACCESS DOOR BLOWN OPEN & FOUND METAL SHAVINGS IN THE TAIL PIPE. MAINTENANCE STARTED THE NR 2 ENGINE & NOTICED THERE WAS NO N1 IND & SHUT IT DOWN. MX INSPECTED ENGINE & FOUND IT WAS SEVERELY DAMAGED. R/R NR 2 ENGINE. LEAKS AND OPS CHECKS GOOD. 2L72 4F4 FRTT00011ATTE6CH 20041210000552004121000055NM 2004 12 10 200420 120041104A3230 DOOR DHAV DHC8 DHC8201 2809001NM ALT EXTENSION OBSTRUCTED A KPVAO OTHER J WARNING INDICATION CLCLIMB 1 WP13544BC 547 (PIREP) AFTER DEPARTURE, UNSAFE GEAR LIGHT AND GEAR GEAR RETRACTED NORMAL BY ITSELF SHORTLY AFTER WHILE CREW DOING CHECKLIST. NORMAL GEAR EXTENSION ACCOMPLISHED. RETURN FOR LANDING. PUSHED ALL DOORS TO RESET GEAR. MX INSPECTED LANDING GEAR SYSTEM, FOUND INTERIOR PANEL OBSTRUCTING ALTERNATE EXTENSION DOOR. RESECURED PANEL AND CLOSED ALTERNATE EXTENSION DOOR. POST MAINTENANCE CHECK FLIGHT SATISFACTORY. 2H72 4T RTA13NM 20050414000822005041400082 2005 4 14 CHQA000580 420041104A25654A40302 SLIDE EMB ERJ170ERJ170100LR EU PAX DOOR DISLODGED A CHQAK NONE O OTHER TXTAXI/GRND HDL 1 GL11633 59 59 17000054 AFTER ARRIVING AT THE GATE ON FLIGHT 7702 FROM IAH TO IAD, THE FLIGHT ATTENDANT COULD NOT OPEN THE EXIT DOOR. THE GIRT BAR WOULD NOT FULLY DISENGAGE FROM THE ACTIVATED POSITION. WHEN THE DOOR WAS OPENED FROM THE OUTSIDE, THE SLIDE DID NOT DISCONNECT FROM THE AIRCRAFT AND THE SLIDE PULLED OUT OF THE CONTAINER AT THE BASE OF THE DOOR. THE DOOR SLIDE ASSEMBLY DEPLOYED UPON ARRIVAL AT THE GATE BY THE MECHANICS. MAINTENANCE PERFORMED AND INSPECTION OF THE FORWARD PASSENGER DOOR EMERGENCY MECHANISM IAW EMB 170 AMM 52-11-40. REMOVED AND REPLACED EMERGENCY SLIDE ON FORWARD PASSENGER DOOR IAW WMB 170 AMM 52-11-40. 2L74 4F RTA56NM 20041210000612004121000061CE 2004 12 10 111004 120041109A2910AE366316360320 LINE CESSNA501 501 2076603CE HYDRAULIC SYS BROKEN E ESUAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 CE03501AT 5010017 THE AIRCRAFT DEPARTED MRY AND WHEN THE GEAR WAS SELECTED "RETRACT", THE HYDRAULIC LOW PRESS AND QUANTITY ANNUNCIATOR LIGHTS ILLUMINATED. THE FLIGHT CREW RETURNED TO MRY AND SELECTED THE GEAR "DOWN" AND HAD TO "BLOW" THE GEAR DOWN AND LANDED UNEVENTFULLY. IT WAS DETERMINED THAT THE PRESSURE LINE OFF THE HYDRAULIC PUMP ON THE LEFT ENGINE HAD RUPTURED AND PUMPED THE HYDRAULIC FLUID OVERBOARD. 1L72 4F A27CE 20041210000642004121000064NM 2004 12 10 ASAA0410489 120041105A53116546551 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FRAME BENT AND DEFORMED AT LOWER FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND REPLACEMENT STRINGER CLIP IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041210000652004121000065NM 2004 12 10 ASA0440182 120041016A5310654656334 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CRACK IN FRAME SHEAR TIE. REMOVED AND REPLACED SHEAR TIE. 2L72 4F4 FRTA16WE E21EU 20041210000672004121000067NM 2004 12 10 ASA0440188 120041021A531565498854 FLOORBEAM BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 PAE - CORROSION ON FLOORBEAM. REPLACED EXISTING REPAIR STRAP. 2L72 4F4 FRTA16WE E21EU 20041210000702004121000070WP 2004 12 10 ASAA0480502 120040924A53504165X RADOME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE OUT OF ALIGNMENTA ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, RADOME FAILED GAP CHECK BETWEEN AFT EDGE OF RADOME AND FUSELAGE SKIN, STEP 17 OF T/C 244530001. RADOME TO FUSELAGE GAP ACCEPTABLE IAW EA 5350-01156. 2L72 4F4 FRTA6WE E9NE 20041210000722004121000072EA 2004 12 10 REXA04032 120041115A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258505Q8437 7505 FLAPS FAILED AT ZERO ON APPROACH WHEN SELECTED TO THIRTY. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20041210000832004121000083EA 2004 12 10 ACE110104 220041101A72003023912 SPACER BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA ENGINE IMPROPER PART E YADAO OTHER W INADEQUATE Q C APAPPROACH 1 AL03112AX UC45 PW0003 ON OPERATION CHECK FLIGHT AFTER OVERHAULED ENGINE INSTALLATION, PILOT REPORTED THAT THE POWER LEVER GOT HUNG UP ON POWER REDUCTION. AN UNEVENTFUL LANDING WAS COMPLETED AND MAINTENANCE LOCATED AND CORRECTED INCORRECT (FOR THIS MODEL ENGINE) PROPELLER REVERSING HARDWARE INSTALLATION. A BOLT & SPACER (PWC PT6A-65 IPC 76-10-00, ITEMS 261 BOLT & 265 SPACER) WERE INSTALLED DURING OVERHAUL AND MIGHT HAVE CAUSED AN ISSUE IN FLIGHT. 2L72 4T4 TRTA24CE E4EA 20041213000032004121300003NM 2004 12 13 SWAA043586 120041209A33506556633 LIGHT BOEING737 7373G7 1384595NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 LT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041213000092004121300009NM 2004 12 13 SWAA043570 120041207A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041213000102004121300010NM 2004 12 13 SWAA043571 120041207A521065C36231 SKIN BOEING737 7375H4 138449DNM AFT PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR, UPPER HINGE CUTOUT LOWER CORNER SKIN, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041213000112004121300011NM 2004 12 13 SWAA043572 120041207A534065CD27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041213000132004121300013NM 2004 12 13 SWAA043574 120041207A531565C34537 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 665, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041213000142004121300014EA 2004 12 13 04324648 120041119A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 EA27648BR 7406 EVENT SUMMARY ON 11/19 STATED FLAP FAIL AT 0 DEGREES, EMERGENCY DECLARED, LANDED WITHOUT COMPLICATIONS. INTEROGATED FECU FAULTS 1 JAM, 2 PDU DIFF, 3 UNSPECIFIED. CLEARED FAULTS. OPS CHECK GOOD AT THIS TIME REF 27-51-00. 2L72 4F RTA21EA 20041213000152004121300015NM 2004 12 13 AALA20041205 120041207A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21973AN 29548 ORD - EMERGENCY LIGHT IN CABIN FAILED TEST. REPLACED FIVE BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20041213000162004121300016NE 2004 12 13 AALA20041196 220041205A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RIGHT STOPPED A AALAO OTHER Y ENGINE STOPPAGE APAPPROACH 1 SW21237AA 49253 709942 DFW - INFLIGHT RIGHT ENGINE STOPPED RUNNING ON FINAL. THERE WAS A BANG AND ENGINE QUIT. ENGINE WAS AT NEAR IDLE. LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20041213000172004121300017NM 2004 12 13 AALA20041201 120041208A3350 WIRE DOUG MD80 MD83 3023681NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21951TW 53470 ATL - EMERGENCY LIGHT AT SEATS 13DEF INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20041213000212004121300021NM 2004 12 13 SWAA043588 120041209A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 375, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041213000232004121300023NM 2004 12 13 SWAA043590 120041209A53116546547 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND FRAME ANGLE AT BS 727 + 4, BETWEEN RBL 14 AND RBL 15, CRACKED. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20041213000242004121300024WP 2004 12 13 AALA20041200 120041205A323339567851 ACTUATOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21956U 49701 STL - INFLIGHT NOSE GEAR FAILED TO CLOSE AFTER TAKEOFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED LEFT HAND NOSE GEAR DOOR ACTUATOR. ADJUSTED AND RIGGED DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000262004121300026EU 2004 12 13 XNOA1209 120041112A3242 BRAKE ASSY AIRBUS300 A300B4203 3930306EU NR 3 DAMAGED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23224KW 073 NR 3 BRAKE DRAGING. FOUND BRAKE WITH INTERNAL DAMAGE. REMOVED AND REPLACED NR 3 BRAKE ASSY IAW AMM 32-42-27, OPS GOOD. 2L72 4F RTA35EU 20041213000272004121300027 2004 12 13 XNOA1211 420041120A2311 MICROPHONE AIRBUS300 A300B4203 3930306EU NR 1 UHF COMMS FAILED A XN0AA UNSCHED LANDING O OTHER CLCLIMB 1 GL23307FV 235 NR 1 UHF COMM F/O, F/E SIDE CARRIER ONLY - NO VOICE CAPT, ONLY CAN TRANSMIT ON NR 1 COMM. REMOVED AND REPLACED CAPT'S SIDE HAND MIC UHF SYS, OPS CHECK GOOD IAW A300MM 23-21-00. 2L72 4F RTA35EU 20041213000292004121300029NM 2004 12 13 DHL2004755501 120041018A5754 STRUCTURE BOEING727 727225 1384077NM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, NR 2 SLAT AT I/B TRACK ATTACH WBL 592 HAS OTBD FRAME WITH CRACK IN FWD LOWER RADIUS. STOP DRILLED CRACK NR 2 SLAT I/B TRACK WBL 592 IAW B727 SRM 51-10-1. FABRICATED DOUBLER P/N CRESS AISI 321.032 PO 900878, 5 X 3 INCH IAW B727 SRM 57-50-3, NDT ACCOMPLISHED HFEC INSPECTION 51-00-00 FIG 4 END OF CRACK FOUND. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. RE-INSTALLED NR 2 SLAT I/B TRACK IAW B727 MM 27-81-11, OPS CHECK OK IAW B727 MM CH 27-81-11. 2L73 4F A3WE 20041213000302004121300030CE 2004 12 13 DXTA200400467 120041205A324099123053 CLIP CESSNA500 560CESSNA 2076750CE MLG BRAKE DAMAGED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07314QS 5600441 ON LANDING PILOT APPLIED BRAKES WITH NO RESPONSE (HARD PEDAL) COPILOT APPLIED BRAKES WITH SAME RESULT. SEVERAL APPLICATIONS WERE MADE. AT 70KIAS BRAKES LOCKED MONENTARILY, ANTI SKID LIGHT ILLUMINATED AND REMAINED ON UNTIL SHUTDOWN. AFTER ILLUMINATION THE BRAKES FUNCTIONED NORMALLY. APPLIED POWER TO A/C. ANTI-SKID ANNUNCIATOR/TEST, OPS CKS GOOD. REMOVED LT & RT HUB CAPS. FOUND LT TRANSDUCER CLIP BROKEN & HUBCAP FULL OF WATER. REMOVED TRANSDUCER & CLEANED ALL WATER. NO DEFECTS NOTED. INSTALLED TRANSDUCER. ANTI-SKID FUNCTION OK, CKS GOOD. FOUND RT CLIP GAP OUT OF TOLERANCE. REMOVED & REPLACED LT & RT CLIPS. RECONFIGURED A/C. BRAKE OP CK GOOD ON ENGINE RUN. 2L72 4F RTA22CE 20041213000312004121300031EU 2004 12 13 DXTA200400468 120041207A7330 WARNING SYSTEM BRAERO1000 HAWKER1000 7450005EU FUEL/ENGINE ACTIVATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07551QS 259051 ON TAKEOFF ROLL AT APPROX 65-70 KTS FUEL/ENG LOOK UP LIGHT WITH ASSOCIATED AUX TRANSFER FAULT ILLUMINATED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20041213000342004121300034WP 2004 12 13 MWEA040216 120041130A5310 BEAM DOUG DC9 DC981 3022081WP EMERGENCY EXIT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 CORROSION AROUND LIGHTENING HOLE ON TOP OF NR 3 RIGHT FORWARD EMERGENCY EXIT DOOR BEAM. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041213000352004121300035WP 2004 12 13 MWEA040217 120041206A53305920323187 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 FUSELAGE SKIN HAS A DENT AT FRAME STATION 322.5 TO 329 ONE INCH BELOW LONGERON 23 RIGHT TO 24 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041213000392004121300039NM 2004 12 13 MWEA040218 120041206A5310595305069 FRAME DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 FRAME STATION 313 LONGERON 21 LEFT HAS A DENT WITH IN 1 INCH OF LONGERON. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041213000402004121300040EU 2004 12 13 RAIA00412008 120041207A3010 EJECTOR VALVE JETAIRJETSTMJETSTM4101 1500501EU ANTI ICE SYSTEM LACK OF LUBE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03568HK 41086 CRW - AUTO AND MANUAL ICE PROTECTION SYSTEM FAULT, CCT2 LIGHT NOT GOING OUT. MAINTENANCE LUBED EJECTOR VALVE, RAN ENGINES AND PERFORMED DE-ICE TEST. 2L72 4T RTA41NM 20041213000412004121300041EU 2004 12 13 RAIA00412009 120041203A3230A1424D SOLENOID VALVE JETAIRJETSTMJETSTM4101 1500501EU NLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03566HK17589 41084 STL - NOSE GEAR WOULDN'T RETRACT. MAINTENANCE REMOVED AND REPLACED ISOLATION VALVE. 2L72 4T RTA41NM 20041213000422004121300042NM 2004 12 13 WLDA2004103 120041103A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 DURING C2 CHECK INSPECTION, FOUND CRACK IN TWO FLOOR PANEL SUPPORT ABOVE 1 INCH AND 1.5 INCH AT STA 1541 RBL 0 TO RBL 30, LBL 0 TO LBL 30. REPAIRED CRACKED AREA USING REPAIR DOUBLERS PER MD11 SRM53-00-01 FIG 5,VOL1 REV 36. 2L73 4F4 FRTA22WE E24NE 20041213000432004121300043NM 2004 12 13 QXEA200400848 120041208A3411 LINE BOMBDRDHC8 DHC8401 1390041NM PITOT/STATIC SYSOBSTRUCTED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09412QX 4059 ON FLT NR 2414, AT FL250 TEMP 30 DEGREES RECEIVED ELEVATOR FEEL, PITCH TRIM, SPOILER O/B, RUD CONTROL CAUTION LIGHTS AND IAS MISMATCH MESSAGES. SLOW TO 200 KTS. COMPLETED CHECKLIST FOR -IAS- MISMATCH (PDF), UNAFFECTED SIDE WAS NR 2. SEA - BIL FLIGHT DIVERTED TO GEG. MAINTENANCE COMPLIED WITH CLEANING OF THE PITOT AND STATIC LINES. COMPLIED WITH OPERATIONAL TEST OF AIR DATA SYSTEM. COMPLIED WITH PITOT/STATIC LEAK CHECK. SYSTEM OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20041213000442004121300044NM 2004 12 13 WLDA2004108 120041206A5270 WARNING LIGHT DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE DOOR LOCK OVRHT ILLUMINATED A WRLAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11271 48518 AED/ODN COCKPIT DOOR LOCK OVERHEATED INFLIGHT. CABIN CREW SMELLED SMOKE, PULLED DOOR C/B, HEAT AND SMELL DISSIPATED. ENTERED IN DMI M52DE0604-35 CAT-A PER MEL 52-54-2. 2L73 4F4 FRTA22WE E24NE 20041213000462004121300046WP 2004 12 13 0402139759 120041103A5741 ANGLE DOUG DC9 DC941 302207NWP WING TO BODY CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01759NW 47287 DURING H-CHECK FOUND CRACKED RT WING TO FUSELAGE ATTACH ANGLE AT BS 644. REPAIRED PER EA 97-201426. 2L72 4F A6WE 20041213000492004121300049NM 2004 12 13 SWAA043579 120041207A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727 + 10, BELOW STRINGER 22L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041213000532004121300053NM 2004 12 13 SWAA043580 120041207A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041213000542004121300054CE 2004 12 13 DXTA200400455 120041120A3230 LANDING GEAR CESSNA560 560XL 2076702CE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07616QS 5605345 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, BLEW GEAR DOWN AND LANDED SAFELY. RESECURED EMERGENCY GEAR HANDLE CABLE CLEVIS ASSY AND REAFFIXED EMERGENCY GEAR BOTTLE SAFETY WIRE, EMERGENCY GEAR BOTTLE FOUND PROPERLY SERVICED. PERFORMED LANDING GEAR HYDRAULIC SYSTEM BLEED AND OPERATION CHECKS IAW CHAPTER 32-30-01, OPERATIONAL AND LEAK CHECKS WERE NORMAL. 2L72 4F RTA22CE 20041213000552004121300055SO 2004 12 13 RAIA00412007 120041207A3040 HEATER EMB 145 EMB145LR 3260212SO WINDSHIELD FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK 145059 STL - WINDSHIELD HEAT 2 FAIL. MAINTENANCE PERFORMED SUCCESSFUL TEST. NO FAULTS NOTED. 2L72 4T RTT00011AT 20041213000602004121300060EU 2004 12 13 341014 120041203A2613 WARNING LIGHT SAAB SF340 340B 7860101EU TAIL PIPE ILLUMINATED A NSVAO OTHER J WARNING INDICATION CRCRUISE 1 EA27346CJ 340B346 RIGHT TAILPIPE HOT LIGHT ILLUMINATED. 2L72 4T RTA52EU 20041213000612004121300061NE 2004 12 13 341024 220041203A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A11 52043NE RIGHT FAILED A NSVABA EMER. DESCENT UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 EA27124CJ UE24 RIGHT ENGINE FAILURE INFLIGHT. 2L72 4T3 TRTA24CE E4EA 20041213000632004121300063NM 2004 12 13 WLDA2004105 120041125A3241 SENSOR DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 2 TIRE PRESS SEIZED A WRLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11271 48518 FRA/KWI ABORTED TAKEOFF AT 130 KTS DUE TO LEVEL II TIRE FAILURE AURAL & VISUAL ALERT. FOUND NR 2 TIRE PRESS SENSING UNIT SEIZED. DEACTIVATED SENSING UNIT AND ENTERED IN DMI M32NO2504-138 PER MEL 32-46-3 CAT-C. PERFORMED RTO INSPECTION AS PER WO CARD 0259 NIL DAMAGE FOUND ON BRAKES OR TIRES. MONITORED TIRE PRESSURE FOR 90 MIN, NO LEAKS NOTED. 2L73 4F4 FRTA22WE E24NE 20041213000642004121300064EU 2004 12 13 XNOA1214 120041201A2780 SLAT AIRBUS300 A300B4203 3930306EU WINGS FAILED A XN0AO OTHER O OTHER TXTAXI/GRND HDL 1 GL23474AS 219 SLATS WOULD NOT EXTEND ON TAXI OUT. RETURNED TO BLOCKS. 2L72 4F RTA35EU 20041213000652004121300065EU 2004 12 13 XNOA1212 120041124A1420 CONNECTOR AIRBUS300 A300B4203 3930306EU HYD SENSOR DIRTY A XN0AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL23371PC 157 RETURN TO THE RAMP, DUE HYD BLUE SYSTEM TEMP HI, ON TAXI OUT. CLEANED INSPECTED RESECURED CONNECTOR AT TEMP BULB AT RES GROUND OP'S CHECK NORMAL PER A300 MM 29-33-00. 2L72 4F RTA35EU 20041213000662004121300066EA 2004 12 13 04338658 120041203A2701 YOKE CNDAIRCL600 CL6002B19 1900309EA COCKPIT VIBRATION A VTZAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 EA27658BR 7500 HIGH FREQ VIBE FELT THRU YOKES & GOT WORSE AS SPEED INCREASED. INTERROGATED MDC FOR ANY APPLICABLE FAULTS, NONE FOUND. PERFORMED CRJ SERVO SPIN TEST. AILERON & ELEVATOR SERVOS OK FOR SVC. PERFORMED OPS CHK OF HORIZONTAL STAB TRIM SYSTEM, NO DEFECTS NOTED. PERFORMED DETAILED INSPECTION OF ELEVATOR FLUTTER DAMPNERS, NO DEFECTS NOTED. PERFORMED OPS CHK OF ELEVATOR CONTROL SYSTEM, NO DEFECTS NOTED, PERFORMED CABLE TENSION CHK OF ELEVATOR CONTROL CABLES, FOUND TO BE WITHIN SPEC AT THIS TIME; PERFORMED OPS CHK OF AILERON CONTROL SYSTEM, NO DEFECTS NOTED AT THIS TIME; PERFORMED OPS CHK OF PITCH DISCONNECT SYSTEM, OPS CHK GOOD AT THIS TIME. INSPECTED ALL FLAP HINGE FAIRINGS FOR SECURED NESS, FOUND ALL SECURE. 2L72 4F RTA21EA 20041213000672004121300067CE 2004 12 13 DXTA200400437 120041104A3241MS2416602 RELAY CESSNA500 560CESSNA 2076750CE BRAKE ASSY FAILED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07361QS 5600361 NORMAL BRAKE SYSTEM FAILED ON LANDING, INITIATED EMERGENCY PNEUMATIC STOP. FOUND SKID CONTROL MOTOR RELAY CONTACTOR WELDED CLOSED & PUMP OPERATES CONTINUOUSLY. REPLACED RELAY WITH A NEW RELAY PER CE 560 MM 32-42-08. REPLACED SKID CONTROL MOTOR / PUMP ASSY WITH A REPAIRED UNIT DUE TO CONTINUOUS OPERATION IN FLIGHT PER CE560 MM 32-42-06. SERVICED EMERGENCY BRAKE / GEAR BOTTLE PER CE560 MM 12-13-01. BLED BRAKE SYSTEM PER CE560 MM 32-42-00. OPS CHECK BRAKE SYSTEM NORMAL. 2L72 4F RTA22CE 20041213000682004121300068CE 2004 12 13 DXTA200400466 120041203A5320 ATTACH BRACKET CESSNA650 650 2076802CE FUSELAGE OUT OF ALIGNMENTE DXTAO OTHER S AFFECT SYSTEMS CRCRUISE 1 GL07797QS 6507097 AUTOPILOT WILL CLIMB BY ITSELF WHILE IN ALTITUDE HOLD MODE ABOUT 200 FT. WHEN DESCENDING IN ANY MODE AUTOPILOT INITIATES A CLIMB AS IF YOU ARE OVERSPEEDING EVERY 500 FEET. PERFORMED OPERATIONAL CHECK OF VS AND FLC MODES USING DRUCK AIR DATA TEST. OP'S CHECKED FOUND TO BE NORMAL LEVELED AIRCRAFT AND CHECKED LEVELING OF AHRU UNITS. FOUND NR 1 ATTRS RACK SLIGHTLY OUT OF ALIGNMENT. SHIMMED RACK AS NECESSARY PER HONEYWELL SP2 8000 SYS MANUAL LEVEL CHECKED GOOD. OP'S CHECKED GOOD ON AUTOPILOT FLIGHT DIRECTION. 2L72 4F A9NM 20041213000692004121300069WP 2004 12 13 AALA20041191 120041204A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21955U 49427 DFW - CEILING EMERGENCY LIGHTS AT ROWS 27 AND 28 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 27 AND 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000712004121300071NE 2004 12 13 AALA20041185 220041122A7200 ENGINE BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE RIGHT SHUTDOWN A AALAO OTHER Y ENGINE STOPPAGE LDLANDING 1 SW21791AN 30254 51244 LGW - TWO MINUTES AFTER LANDING RIGHT ENGINE AUTO SHUTDOWN. FOUND FOD DAMAGE. FLIGHT DATA RECORDER DOWNLOADED PER WORK CARD 31 92 11. DATA SENT TO TULSA TECH. ENGINEERING ORDERED HPC BOROSCOPED CONCENTRATING ON STAGES ONE AND SIX. REPLACED RIGHT ENGINE PER MAINTENANCE CHECK MANUAL 71 94 01. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTT00001SEE00050EN 20041213000722004121300072NE 2004 12 13 AALA20041186 220041126A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ZONE 500 FOD A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21592AA 53255 725975 ORD - INFLIGHT LEFT ENGINE COMPRESSOR STALLS DURING CLIMBOUT AT 11,000 FT. ENGINE ACCELERATED FOR CLIMB NORMALLY BUT STARTED STALL WHILE AT FULL CLIMB THRUST. ENGINE ANTI-ICE ON. ENGINE FAIL CHECKLIST ACCOMPLISHED. ENGINE LEFT AT IDLE. FOUND INLET FOD. REPLACED NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20041213000732004121300073WP 2004 12 13 AALA20041187 120041124A3260 SENSOR DOUG DC9 DC983 3022083WP MLG INOPERATIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21973TW 53623 DFW - INFLIGHT RED LIGHT ON NOSE GEAR RETRACTION. THREE GREEN LIGHTS ON EXTENSION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR UP DOWN LOCK SENSOR D1 32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041213000742004121300074NE 2004 12 13 WLDA2004109 220041207A7200 ENGINE DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 2 FIRE A WRLAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN A FLAME/FIRE LDLANDING 1 SO11304 47928 517820 BBR/BGR ON LANDING TOWER ADVISED THAT NR 2 ENGINE IS ON FIRE, ACCOMPLISHED ENGINE FIRE CHECKLIST AND FIRED BOTH BOTTLES. ALL FIRE INDICATIONS REMAINED ILLUMINATED, ACCOMPLISHED EVACUATION CHECKLIST AND EXITED L1 DOOR VIA THE ESCAPE SLIDE. REMOVED AND REPLACED NR 2 ENGINE PER JOB CARD WM-280 AND DC10 MAINTENANCE MANUAL PROCEDURES. PERFORMED ENGINE RUN UP AND CHECKED ALL PARAMETERS, FOUND NORMAL. 2L73 4F4 FRTA22WE E23EA 20041213000752004121300075EU 2004 12 13 CX7A194J0459 120041207A26131734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL03300CE 340B184 SHORTLY AFTER ROTATION GOT A LEFT HAND TAILPIPE HOT INDICATION. 2L72 4T RTA52EU 20041213000762004121300076EA 2004 12 13 04340649 120041205A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY ACTIVATED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27649BR 7414 EVENT SUMMARY ON 12/5 STATED RTF FOR SMOKE IN THE LAV INDICATION. PERFORMED OPS CHK OF LAV SMOKE SYSTEM. NO DEFECTS NOTED. NO SMELL OF SMOKE NOTED. 2L72 4F RTA21EA 20041213000772004121300077NM 2004 12 13 SWAA043577 120041207A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20041213000802004121300080EU 2004 12 13 XNOA1206 120041101A2760 INDICATOR AIRBUS300 A300B4203 3930306EU SPOILERS FAILED A XN0AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL23372PC 196 FLIGHT CONTROL POSITION INDICATOR RIGHT -SP- SPOILER INDICATION FAILED. REMOVED AND REPLACED FCPI IAW A300 AMM 27-15-00, SYSTEM OPS CHECK GOOD. 2L72 4F RTA35EU 20041213000842004121300084EU 2004 12 13 U30A200400012 120041102A5610NP1653115 WINDSCREEN AIRBUS320 A320214 3930316EU ZONE 211 CRACKED A U30ABA EMER. DESCENT UNSCHED LANDING O OTHER DEDESCENT 1 EA17267AV 1198 DURING DESCENT TO 370, CAPT NOTICED SMALL CRACK ON CAPT'S FRONT WINDSCREEN. FLT CREW REQUESTED LOWER ALTITUDE & ATC COULD NOT COMPLY & TOLD FLT TO MAINTAIN 370. CRACK STARTED TO WIDEN & SPREAD RAPIDLY, FLT CREW REQUESTED AN EMERGENCY DESCENT. FLT CREW SEAT HARNESSES WERE ON & O2 MASKS DONNED. OUTER LAYERS OF WINDSCREEN DAMAGED, NO LOSS OF PRESSURIZATION. AIRCRAFT DIVERTED INTO TPA. F/O TOOK OVER PF DUTIES, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CAPT'S FRONT WINDSCREEN PER AMM 56-11-11-PB400 AND OPS CK'D OK. AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT COMPUTER PER AMM 30-42-34-401, FOR PRECAUTIONARY REASONS AND OPS CK'D OK ON 11/4/04. 2L72 4F RTA28NM 20041213000862004121300086EA 2004 12 13 04326662 120041121A3260 SQUAT SWITCH CNDAIRCL600 CL6002B19 1900309EA LT MLG FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27662BR 7526 WOW INPUT CAUTION MESSAGE AFTER RETRACT. RTF. MX REMOVED AND REPLACED LT MLG WOW NR 2 PS16GA. OPS CHECK GOOD, NO CAUTION LIGHT NOTED. 2L72 4F RTA21EA 20041213000882004121300088NE 2004 12 13 PNSA041102 220041105A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 FAILED A PNSAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 AL03665PA 340B181 785121 FLT WAS EN ROUTE FROM DUT TO ANC WHEN FLIGHT CREW PULLED TORQUE BACK TO 60 PERCENT FOR DESCENT THE NR 2 ENGINE WENT TO 20 PERCENT CREW HEARD A LOUD BANG, ITT RISING, AUTO IGNITION CAME ON OVERTEMP LIGHT CAME ON FOR 1 SEC. MEMORY ITEMS FOR COMPRESSOR STALL STARTED ENGINE RECOVERED. MX FOUND FIRST STAGE INLET GUIDE VANES VERY STIFF AND A BENT IGV ACTUATING ARM GOING TO THE ACTUATING RING OF THE IGV'S. ENGINE WAS REMOVED AND REPLACED. 2L72 4T4 TRTA52EU E8NE 20041213000912004121300091EU 2004 12 13 0402103304 120041129A324626122012 WHEEL AIRBUS330 A330323 3930335EU NR 7 FIRE A NWAAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 GL01804NW3989 15 00549 UPON ARRIVAL AT THE GATE, FIRE WAS COMING FROM THE NR 7 WHEEL/BRAKE ASSEMBLY. BRAKE COOLED AND THE FIRE EXTINGUISHED. INSPECTED GEAR AND REPLACED THE WHEEL AND BRAKE ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA46NM 20041213000922004121300092WP 2004 12 13 AALA20041190 120041130A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21581AA 53158 LAX - COCKPIT, FORWARD ENTRANCE, AND SERVICE ENTRANCE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B523 FOR COCKPIT, FORWARD ENTRANCE AND SERVICE ENTRANCE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000932004121300093WP 2004 12 13 AALA20041193 120041203A3260 SENSOR DOUG DC9 DC983 3022083WP MLG OUT OF ADJUST A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21572AA 49458 ORD - INFLIGHT ON GEAR RETRACTION NOSE GEAR INDICATOR REMAINED RED. DOORS REMAINED OPEN (AIR NOISE). NOSE LANDING GEAR INDICATED RETRACTED. STALL INDICATED FAILURE AND AUTO SPOILER DO NOT USE ILLUMINATED. PERFORMED FULL STRUT SERVICE. JACKED NOSE GEAR AND SWUNG NOSE GEAR SEVERAL CYCLES. ADJUSTED NOSE GEAR LOCK SENSOR GAP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041213000942004121300094NM 2004 12 13 QXEA200400847 120041207A5312 BULKHEAD DHAV DHC8 DHC8202 2809007NM FUSELAGE OUT OF ADJUST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09368PH14693 512 PDX - FLIGHT 2236 - THE MAIN CABIN DOOR IS DIFFICULT TO OPERATE. MAINTENANCE INSPECTED THE DOOR AND DETERMINED THAT THE DOOR WAS RUBBING AGAINST THE FORWARD BULKHEAD. THE BULKHEAD WAS ADJUSTED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041213000952004121300095WP 2004 12 13 ARWA20041201 120041202A2720 PUMP DOUG DC8 DC863F 302198FWP RUDDER INOPERATIVE A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19661AV 45969 PRIOR TO TAKEOFF STANDBY RUDDER PUMP INOPERATIVE. FOUND CURRENT LIMITER FUSE BLOWOUT. REPLACED IN ACCORDANCE WITH MM 27-24-2. 2L74 4F 4A25 20041213000962004121300096NM 2004 12 13 SWAA043592 120041209A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA. 2L72 4F RTA16WE 20041213000972004121300097NM 2004 12 13 SWAA043582 120041208A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, BETWEEN LBL 7 AND LBL 18, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041213000982004121300098NM 2004 12 13 DHL2004755502 120041012A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, LT FUSELAGE SKIN HAS A DENT AFT BS 1050 BELOW STR 22L. CUT OUT DAMAGED SKIN, 3 X 1 INCH AT STA BELOW STR 22L IAW B727 SRM 53-30-3, FABRICATED DOUBLER FROM 2024 T3.071, 10 X 7 INCH PO 9001189 IAW B727 SRM 53-30-3, TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER IAW B727 SRM 53-30-3. 2L73 4F A3WE 20041213000992004121300099NM 2004 12 13 DHL2004755503 120041015A5312 WEB BOEING727 727225 1384077NM MLG WW CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, LT W/W, WEB AT STA 950 IS CRACKED, FWD OF HYD PUMPS AND AFT OF LT MAIN GEAR DOOR AFT UP STOP SUPPORT. CUT OUT CRACK WEB, 1 X .75 INCH IAW B727 SRM 51-10-1, FABRICATED WED REPAIR P/N 2024T3.050 PO 9001425, 6.5 X 5.5 INCH IAW B727 SRM 51-40-2 FIG 1. TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED WEB REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041213001002004121300100 2004 12 13 AT0400024 420041127A3160 DISPLAY BOEING717 717200 1383700NM COCKPIT LOCKED A ZZDAO OTHER O OTHER CRCRUISE 1 SO15933AT 55071 MCDU NR 1 AND NR 2 LOCKED UP IN FLIGHT. NO FLIGHT PLAN INFO, NO AUTOPILOT RESET. RESET ITSELF AFTER 30 MINUTES. PERFORMED RTS OF BOTH VIA'S AND AUTOPILOT SYSTEM PERFORMED AUTOLAND RTS. REINSTALLED VIA SOFTWARE AND PERFORMED RTS. SYSTEMS OPS CHECK GOOD. CLEANED COOLING HOLES ON MCDU'S. 2L72 4F TRA6WE 20041213001032004121300103CE 2004 12 13 DXTA200400458 120041122A301012850511 DUCT BEECH MU300 400A 1155402CE ANTI ICE SYSTEM RUPTURED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07115QS RK383 SMOKE AND EXHAUST APPEARED IN LAV WHEN ENG AND WING ANTI-ICE WAS PLACED ON. EXHAUST SMELLED LIKE OIL AND WAS VERY VISIBLE. IT LEFT A FILM ON LAV MIRROR. FOUND THE SMOKE AND ODOR CAUSED BY A RUPTURE IN THE WING ANTI-ICE BLEED AIR LINE. INSTALLED NEW BLEED AIR LINE BY INCORPORATION OF KIT 128-5051-1 PER RAC DRAWING. CLEARED INSULATION BAGS FROM WING ANTI-ICE DUCTS IN LAV AREA. 2H72 4F RTA16SW 20041213001052004121300105CE 2004 12 13 DXTA200400459 120041122A281099144751 CHECK VALVE CESSNA750 750 2076810CE RT WING FUEL FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07997QS 7500208 WING TANK OVERFILL RT CAS MESSAGE FOLLOWED BY FUEL VENTING OUT OF RIGHT WING TIP, 6000 LBS OF FUEL TOTAL IN AIRCRAFT. FOUND RT WING SURGE TANK CHECK VALVE TO EXCESSIVE SIDE PLAY. REMOVED AND REPLACED CHECK VALVE WITH NEW. CLOSED ACCESS PANELS AND FUELED A/C. C/W OPS CHECK AND FUEL TRANSFER CHECK. ALL CK'S GOOD AT THIS TIME. LEAK CHECK GOOD IAW CESSNA 750 MM 28-10-05. 2L72 4J RTT00007WI 20041213001062004121300106NM 2004 12 13 DHL2004755506 120041019A5753 DOUBLER BOEING727 727225 1384077NM LT WING TE FLAP CHAFED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, LEFT I/B FORE FLAP O/B L/E WBL 240 HAS REPAIR DOUBLER CHAFED THRU. REMOVED PREVIOUS REPAIR AT LEFT, I/B FORE FLAP L/E IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR 2024T3.063 PO 9001276, 6 X 5 INCH IAW B727 SRM 57-50-4 FIG 1, TREATED & PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041213001072004121300107EA 2004 12 13 REXA04031 120041115A2750 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258718E4523 7718 FLAP FAILS AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED EMERGENCY DECLARED, UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20041213001092004121300109NM 2004 12 13 AT0400025 120041207A215022065201 ACM BOEING717 717200 1383700NM ACM BAY SEIZED A ZZDAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO15919AT 55084 ACM SEIZED AND SENT SMOKE INTO THE CABIN, CAPTAIN'S RESPONSE WAS TO SHUT OFF BOTH PACKS, SMOKE DISSIPATED. RETURNED TO BWI AFTER DECLARING AN EMERGENCY. CONFIRMED ACM WAS CAUSE OF SMOKE AND PLACED ITEM ON MEL 80007. PACK NOT USABLE. REMOVED AND REPLACED ACM. 2L72 4F TRA6WE 20041213001102004121300110NM 2004 12 13 0402095529 120041201A5315 FLOOR SUPPORT BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01529US 23844 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 365 RBL 45.5. REPAIRED PER EA 55-201141. 2L72 4F RTA2NM 20041213001132004121300113NM 2004 12 13 SWAA043562 120041207A3350604222 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT AND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20041213001152004121300115SO 2004 12 13 SWIA200414067 120041101A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07299SW 120329 BOTH FORWARD EXIT FLOOR LIGHTS (RED) INOPERATIVE. REPAIRED WIRES TO FLOOR TRACK LIGHTS (2 RED FWD). OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041213001162004121300116CE 2004 12 13 DXTA200400452 120041119A7332 WARNING LIGHT CESSNA500 560CESSNA 2076750CE FUEL SYSTEM ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07348QS 5600348 DURING THE TAKEOFF ROLL, THE LEFT FUEL LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED BY BOTH THE LEFT AND RIGHT FUEL BOOST PUMPS ON ILLUMINATING. CHECKED FUEL TANKS FOR FUEL CONTAMINATION, NONE FOUND. INSPECTED FUEL FILTERS PER CE560 MM 28-00-02, FOUND CLEAN & FREE OF CONTAMINATION. RAN BOTH ENGINES AT TAKEOFF POWER FOR SEVERAL MINUTES. COULD NOT DUPLICATE PROBLEM, ALL CHECKS NORMAL. 2L72 4F RTA22CE 20041213001172004121300117CE 2004 12 13 DXTA200400449 120041117A3411 PITOT SYSTEM CESSNA750 750 2076810CE PITOT STATIC OBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07904QS1630 7500210 AT APPROX 80 KTS ON TAKEOFF ROLL THE MACH TRIM CAS MESSAGE ILLUMINATED, FOLLOWED BY THE LOWER RUDDER FAIL CAS MESSAGE. FOLLOWED CHECKLIST FOR LOWER RUDDER FAIL, CAS MESSAGE WERE NORMAL. FOUND BUGS IN PITOT LINES FROM ADC. CLEANED LINES. C/W PITOT SYTEM LEAK CHECK IAW FAR 91-411 11-17-04. CHECKS NORMAL. 2L72 4J RTT00007WI 20041213001192004121300119NM 2004 12 13 AALA20041099 120041007A3397 CONNECTOR BOEING757 7572Q8 1384972NM EMERGENCY LIGHT UNSECURE A AALAK NONE O OTHER ININSP/MAINT 1 SW21709TW 28168 DFW - EMEREGNCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041213001202004121300120EU 2004 12 13 MALA040656 120041019A5210 GUARD SAAB SF340 340B 7860101EU PAX DOOR LOOSE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15443XJ 340B443 BOARDING DOOR WOULD NOT CLOSE, WHEN TRYING TO OPEN IT, THE DOOR WAS JAMMED AND WOULD NOT OPEN. RAIN GUARD JAMMED DOOR. MAINTENANCE FOUND RAIN GUARD MISSING SCREWS, GOT JAMMED BETWEEN DOOR AND FUSELAGE. RESECURED, CHECKS GOOD. 2L72 4T RTA52EU 20041213001212004121300121NM 2004 12 13 SWAA043264 120041108A55306547450 FITTING BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL FIN FITTING PER ER. 2L72 4F RTA16WE 20041213001222004121300122EU 2004 12 13 MALA040695 120041005A33505521981 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15367PX 340B271 DURING CAPACITY INSPECTION IN MSP, POWER SUPPLY P/N 61-0478-9, S/N 9903018 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/11/04. 2L72 4T RTA52EU 20041221000712004122100071NM 2004 12 21 ASA0440217 120041029A53406562208 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 STRINGER CLIP CRACKED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041221000732004122100073SO 2004 12 21 SIMA200429802 120041215A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21626AE 145117 DURING AN MBV INSPECTION A CRACK WAS DISCOVERED ON THE FORWARD DIGITAL AT FRAME 13. PERFORMED EDDY CURRENT INSPECTION TO DETERMINED THE LENGTH OF THE CRACK AND STOP DRILLED THE CARCK. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW STATEMENT IC2004/145-4832. (SW21200501190) 2L72 4T4 FRTT00011ATTE6CH 20041221000842004122100084WP 2004 12 21 GTIA040855 120041129A3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT MLG OUT OF ADJUST A GTIAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23826NK 49391 LP NR 281139-1; AIR RETURN; AT 12,000 FT HYDRAULIC PUMP PRESS REDUCTION GEAR DOOR OPEN LIGHT AND LT MAIN GEAR DOOR UNSAFE LIGHT CAME ON, COMPLIED WITH QRH. CYCLED GEAR LT MAIN GEAR UNSAFE LIGHT REMAINED ON. INSEPECTED LT MAIN GEAR UPLOCK, FOUND PROX SWITCH SENSOR WITH NO AIR GAP, ADJUSTED AIR GAP TO WITHIN LIMITS. OPS CHECK GOOD. 2L72 4F4 FRTA6WE E9NE 20041221000852004122100085WP 2004 12 21 GTIA040849 120041115A5347 SEAT TRACK DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23810NK 48015 NR B00182-05N-00119, 00121, 00124; CABIN SEAT TRACK CORRODED, STA 807-984 RBL 24 IB AND LBL 24 AND LBL 43 IB, STA 905 RBL 43 OB. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK, TREATED, PRIMED AND TOP COATED NEW SEAT TRACK. 2L72 4F4 F A6WE E9NE 20041221000912004122100091NM 2004 12 21 AMTA200401252 120041004A5313 STRINGER BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11553TZ 32587 STR 20L HAS (2) EA ELONGATED HOLES AT STA 509.5 AND STA 523.5. INSTALLED (2) EA FREEZE PLUGS IAW ERA 757-53R-5717. 2L72 4F4 FRTA2NM E12EU 20041221001052004122100105EU 2004 12 21 A6WA200460054 120041110A3520K390282 OXYGEN MASK BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE ROWS 14,16 DEF MISSING A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31612AW E3122 ROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45. 2H74 4F4 FRTA49EU E6NE 20041221001062004122100106NM 2004 12 21 ASAA0410410 120040927A261247400602 CONTROL PANEL BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE FIRE DETECTION MALFUNCTIONED A ASAAFD ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM02741AS9938 1543 21959 MULTIPLE FIRE WARNINGS, CARGO FIRE SUPPRESSION ACTIVATED IN THE AFT CARGO PIT. NO EVIDENCE OF FIRE OR SMOKE FOUND. REMOVED AND REPLACED FIRE SUPPRESSION AND SMOKE DETECTION CONTROL PANEL AS A PRECAUTIONARY MEASURE, AND REMOVED AND REPLACED THE LT CARGO PIT FIRE SUPPRESSION BOTTLE AND DRIER UNIT. SDR BEING SENT AS OPEN PENDING THE SHOP FINDINGS ON THE CONTROL PANEL. THE LINE TECH ON SITE IAW THE AMM DETERMINED THE PRELIMINARY CONDITION AS GOOD. (K) 2L72 4F4 F A16WE E2EA 20041221001142004122100114EU 2004 12 21 ASOA04920 120041102A5310 DOUBLER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE HANDRAIL FITTINGCORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE UPPER DOUBLER OF THE HANDRAIL FITTING ON THE LT THRESHOLD BETWEEN FS 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED DOUBLER IAW WITH SRM 51-21-42 AND 51-25-04. 2H72 4T4 TRTA53EU E20NE 20041221001152004122100115NE 2004 12 21 KBM2004F00241 220041004A72619560137528 MAGNETIC SEAL SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE ENGINE LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19215LA471 2143 MAGNETIC SEAL LEAKING, REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20041221001182004122100118EA 2004 12 21 ASOA04884 120041105A2721601R5122623 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RUDDER TRIM MALFUNCTIONED A ASOAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27862AS 7476 DURING CLIMB-OUT, AT APPROXIMATELY 10,000 FEET THE CREW EXPERIENCED A FULL SCALE NOSE LT RUDDER TRIM DEFLECTION. THE CAPTAIN CORRECTED FOR THE TRIM PROBLEM USING RUDDER AND AILERON INPUTS. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED TO VPS AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE AILERON/ RUDDER TRIM CONTROL PANEL. MAINTENANCE VERIFIED FULL TRAVEL ON THE AILERON AND RUDDER TRIM SWITCHES ON EICAS AND ON THE FLIGHT CONTROLS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221001252004122100125SO 2004 12 21 SIMA200429813 120041014A532014524461003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED EXISTING AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS AND PLATE. REPAIR DONE IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001502004122100150SO 2004 12 21 SIMA200431005 120040823A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21736DT 145388 DURING AN IMBV INSPECTION, THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED, CUT OUT FLANGE SECTION OF THE DAMAGED LT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501158) 2L72 4F4 FRTT00011ATTE6CH 20041221001722004122100172NM 2004 12 21 USAA040908 120041020A53201133482 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - CLIP, .5 INCH CRACK, BS 578, S8R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40. 2L72 4F4 FRTA16WE E21EU 20041221001732004122100173NM 2004 12 21 USAA040855 120041030A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - FRAME, .1250 INCH CRACK, STA 787 AND STR 9L. INSTALLED DOUBLERS IAE TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041221001742004122100174WP 2004 12 21 GTIA040824 120041018A2721 ACTUATOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE YAW DAMPER MALFUNCTIONED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23833NK 49449 RUDDER TRIM HAS 6 UNITS RT TO MAINTAIN STRAIGHT AND LEVEL. FOUND YAW DAMPER ACTUATOR OUT OF MOUNTS. REMOVED AND REPLACED YAW DAMPER ACTUATOR, OPS CHECK NORMAL. 2L72 4F4 FRTA6WE E2EA 20041221001762004122100176EU 2004 12 21 KBM2004F00242 120041004A80110174078030 DRAIN VALVE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE STARTER LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA565 2143 START DRAIN VALVE, UNIT LEAKING, REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20041221001792004122100179NM 2004 12 21 USAA040911 120041021A5340653535214 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - STRINGER TIE CLIP, .2500 INCH CRACK, STA 380, STR 2 LT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03. 2L72 4F4 FRTA16WE E21EU 20041221001802004122100180NM 2004 12 21 USAA040905 120041104A55101132329 ATTACH ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU THRUST BEAM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - ANGLE, 6 INCH LONG CRACK, HORIZ STAB CTR SECTION THRUST BEAM ATTACH ANGLE LT SIDE. REMOVED AND REPLACED ANGLE, REPLACED IAW TYP REP SRM 51-00-30. REMOVED AND REPLACED IAW TYP REP SRM 51-00-30. 2L72 4F4 FRTA16WE E21EU 20041221001882004122100188EU 2004 12 21 A6WA200460052 120041111A3520K390282 OXYGEN MASK BAC 146 146300A 1500267EU LYC ALF502ALF502R5 41580NE CABIN MISINSTALLED A A6WAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31616AW E3145 DURING INSPECTION, ALL PASSENGER O2 DROP DOWN MASKS WERE FOUND STOWED INCORRECTLY. MAINTENANCE RESTOWED ALL PASSENGER O2 DROP DOWN MASKS, CORRECTLY IAW AMM 35-20-45. 2H74 4F4 FRTA49EU E6NE 20041221002012004122100201NM 2004 12 21 USAA040920 120041104A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE INCORRECT A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1- SKIN, 12 INCH BY 6 INCH INCORRECT DOUBLER REPAIR, FRAME ST 344 S19R. OLD DOUBLER REMOVED AND NEW DOUBLER INSTALLED TO COMPLY WITH NEW SRM DIRECTIONS IAW SRM 53-00-01, FIG 231. 2L72 4F4 FRTA16WE E21EU 20041222000042004122200004NM 2004 12 22 SWAA043653 120041216A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20041222000072004122200007EU 2004 12 22 SA04116 120041219A3260ABS012110 PROXIMITY SENSOR AIRBUSA319 A319112 3930323EU ZONE 100 FAULTY A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19702UW 896 PIT FLT 132 EN ROUTE DEN - PIT. ON APPROACH TO PIT, WHEN THE LANDING GEAR WAS EXTENDED, CREW RECEIVED A L/G SYS DISAGREE MESSAGE WITH THE NOSE LANDING GEAR INDICATING UNSAFE. THE CREW FOLLOWED THE QRH PROCEDURES, AND THEN PERFORMED A FLY BY OF THE TOWER. AFTER TEN MINUTES OF OPERATION WITH THE UNSAFE INDICATION, THE NOSE LANDING GEAR BEGAN INDICATING DOWN AND LOCKED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR 18GA. BITE TESTS OK. 2L72 4F RTA28NM 20041222000122004122200012EA 2004 12 22 SWIA200414281 120041215A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA NR 1 MALFUNCTIONED A SWIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM07432SW 7548 RECEIVED CARGO SMOKE WARNING DURING BAGGAGE LOADING. REMOVED AND REPLACED NR 1 SMOKE DETECTOR IAW MM 26-15-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222000262004122200026WP 2004 12 22 04FDEA03422 120041216A5330AGA3102501 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT AFT FUSELAGE - LATERAL SKIN B/T LONG 36-48 STA 1754-1997 WITH SEVERAL EXISTING REPAIR: DENTS, NICK, CORROSION, AND MISSING MATERIAL AROUND JAMB CTR DOOR CARGO. REPLACE SKIN PER SRM 51-35-01 PAGE 1-12 SRM 51-35-02 PAGE 3- 9, SRM 51-33-01 PAGE 34-47. P/N AGA3102-504, AGA3071-505. 2L73 4F A22WE 20041222000322004122200032NM 2004 12 22 CALS093100 120041121A5330 SKIN BOEING747 747400 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED W SAJFK NONE O OTHER ININSP/MAINT 1 WP03 24309 DURING 3D CHECK, SCRIBE MARKS WERE FOUND ON THE FUSELAGE SKINS ALONG LAP JOINTS, BUTT JOINTS, AND EXTERNAL DOUBLERS. MOST OF SCRIBE MARKS WERE BLENDED OUT. MEASURED THE DEPTH OF BLENDED AREAS. QC RECHECKED THE EXISTING SCRIBE MARKS. HFEC INSPECTED TO DETECT THE CRACK. COLLECTED DATA WAS SENT TO BOEING FOR EVALUATION. 2L74 4F4 FRTA20WE E24NE 20041222000552004122200055NM 2004 12 22 QXEA200400900 120041219A6123 SWITCH DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS DIRTY A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09351PH 490 EUG FLIGHT 2062 AUTOFEATHER DID NOT ARM ON TAKEOFF. TAKEOFF WAS ABORTED AT 70 KIAS. PLACED ON RSI 348686. ON 12/20/04 MAINTENANCE REPLACED 6121-K6 AND 6121-K7 (AUTO ARM RELAYS). CLEANED AND LUBED AUTOFEATHER SWITCHES ON QUADRANT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222000622004122200062SO 2004 12 22 CHQA000595 120041219A3350744424 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11285 145435 RIGHT HAND SIDE WALL EMERGENCY EXIT SIGN IS INOP. REMOVED AND REPLACED RIGHT HAND SIDE WALL EMERGENCY EXIT SIGN IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041222000682004122200068NM 2004 12 22 DLM90041120 120041219A4940110519001 RELAY DOUG MD90 MD9030 3023690NM IAE V2500 V2500A1 NE APU STARTER FAILED A DALAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TXTAXI/GRND HDL 1 SO27903DA 53383 P1006 APU SMOKED THE CABIN CAUSING AN EMERGENCY EVACUATION. REPLACED BAD APU STARTER AND START RELAY. 2L72 4F4 FRTA6WE E311NE 20041222000792004122200079EA 2004 12 22 VNAA0412001 120041208A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A VNAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL05254PS 7935 DURING CLIMBOUT AFTER TAKEOFF FROM DCA THE CREW OF FLIGHT 2326 RECEIVED A FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 20 DEGREES. THE CREW RETURNED TO DCA AND MADE AN UNEVENTFUL LANDING. MAINTENANCE PULLED THE FAULT CODES FROM THE FLAP ELECTRONIC CONTROL UNIT. FAULT DETERMINED TO BE CAUSED BY THE FLAP HANDLE. CIRCUIT BREAKERS WERE CYCLED AND THE CAUTION MESSAGE CLEARED. THE FLAP SYSTEM WAS INSPECTED WITH NO FAULTS FOUND AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041222000802004122200080EA 2004 12 22 MASA200400704 120041217A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07504MJ 10066 ASH 7249 DSM-DEN. THE CREW REPORTED THE CEILING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE INSTALLED NEW LAMP AND THE SYSTEM TESTED NORMALLY. 2L72 4F RTA21EA 20041222000982004122200098SO 2004 12 22 RAIA00412023 120041215A2760 RELAY EMB 145 EMB145LR 3260212SO SPOILERS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03823HK 145475 SPOILER FAILED MESSAGE. MAINTENANCE REPLACED RELAY K0010 SYSTEM. 2L72 4T RTT00011AT 20041222001182004122200118NM 2004 12 22 04FDEA03387 120041207A3233 ACTUATOR BOEING727 727233 138408ANM MLG LEAKING A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO25278FE 22345 TOTAL LOSS OF SYS A QUANTITY WITH LANDING GEAR DOWN AND FLAPS AT 30 DEGREE QTY WENT TO 1.0 GALLONS FOR TEN SECONDS THEN WENT IMMEDIATELY TO 0 GALLONS SYS A PRESSURE WENT TO ZERO WITH LOW PRESSURE LIGHTS IMMEDIATELY FOLLOWING QUANTITY LOSS. TROUBLESHOT LEAK TO LEFT LANDING GEAR DOOR ACTUATOR. REMOVED AND REPLACED LEFT LANDING DOOR ACTUATOR I/A/W M/M 32-32-081-4. CHANGED 'A' SYS HYD RETURN FILTERS I/A/W M/M 29-11-062- 3. NO CONTAMINATION NOTED. SERVICED 'A' SYS HYD RESERVOIR I/A/W 12-12-000-2. OK FOR SERVICE. 2L73 4F RTA3WE 20041222001392004122200139WP 2004 12 22 A4JA12100402 120041127A2611 SMOKE DETECTOR DOUG DC9 DC981 3022081WP RT LAVATORY WILL NOT TEST A A4JAK NONE L NO TEST ININSP/MAINT 1 SO35805US 48053 ON PRE-FLIGHT CHECK, FOUND AFT RIGHT HAND LAV SMOKE DETECTOR NOT TESTING. DEFERRED IAW MEL 26-7 DMI M-805-373, DUE DATE 12-07-04, CAT C, PLACARD INSTALLED, LAV BLOCKED. 2L72 4F A6WE 20041222001672004122200167NE 2004 12 22 MALA040815 320041019A6110 BLADE SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE PROPELLER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 0208 340B408 0208 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED ALL BLADES HAVE DISBANDS IN NICKEL LEADING EDGE LT PROPELLER. MAINTENANCE REPLACED PROPELLER IAW MESABA JOB CARD 6110-B03. REFER TO NRC NR 196539 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2L72 4T RTA52EU 6 CP31NE 20041222001702004122200170CE 2004 12 22 DJFA2004040 120041208A3260 SWITCH BEECH MU300 400A 1155402CE MLG OUT OF ADJUST E DJFAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA23478LX RK387 CREW REPORTED THAT WHILE ON APPROACH THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. AN ALT EXTENSION WAS PERFORMED AND GEAR EXTENDED. THREE GREEN LIGHTS WERE RECEIVED AFTER THE ALT EXTENSION WAS PERFORMED. AN EMERG WAS DECLARED AND A/C LANDED W/O FURTHER INCIDENT. MX T/S THE SYS AND FOUND A CHAFFED WIRE IN LT WHEEL WELL. THE WIRE WAS REPAIRED BY USING A SPLICE. WHILE PERFORMING WIRING TROUBLESHOOTING THE RT GEAR DOOR OPEN SWITCH WAS FOUND TO BE OUT OF ADJUSTMENT. THE SWITCH WAS ADJUSTED AND A GEAR SWING CHECK WAS PERFORMED SEVERAL TIMES WITH NO FAULTS NOTED. THE EMERGENCY NITROGEN BOTTLE IN LEFT NOSE WAS SERVICED. A FLT CHECK WAS COMPLETED WITH NO NOTED DISCREPANCIES. A/C WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20041222001742004122200174WP 2004 12 22 IXXA0400118O 120041105A2910AE246010150134 HOSE DOUG DC8 DC862F 3021972WP HYD SYSTEM WORN A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW1141CX 7648121 46129 DURING TAKEOFF FROM KMCC, AIRCRAFT LOST HYDRAULIC PRESSURE. HYDRAULIC QUANTITY DROPPED TO AUX LEVEL. CREW RETURNED AIRCRAFT TO KMCC AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED AND REPLACED NR 2 PRESS LINE TO PUMP, SERVICED HYDRAULIC SYSTEM BLEED AIRCRAFT FLIGHT CONTROLS DURING ENGINE RUN. THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. 2L74 4F 4A25 20041222001752004122200175NM 2004 12 22 HNAA0400166 120041130A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 MAJOR REPAIR, DURING C CHECK, FOUND CORROSION ON STR 31S. LOCALLY BLENDED OUT CORROSION. INSTALLED TRIMMED REPAIR ANGLES. 2H72 4T RTA13NM 20041223000092004122300009 2004 12 23 BB04093 420041208A2565140N276218 GIRT BAR BOEING757 7572B7 1384964NM L4 DOOR UNSERVICEABLE A USAAK NONE O OTHER ININSP/MAINT 1 EA19625VJ 27246 PHL, THE L4 DOOR WOULD NOT ARM. MAINTENANCE REPLACED THE GIRT BAR. 2L72 4F RTA2NM 20041223000172004122300017EU 2004 12 23 7201 120041105A6520105304022 FITTING BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE TAIL ROTOR G/B CRACKED E A1UAK NONE O OTHER ININSP/MAINT 1 CE03211SL12635 7201 4584945884 WHILE PERFORMING A LIFENET AAIP INSPECTION, THE MECHANIC FOUND A .7500 INCH (APPROX) CRACK EXTENDING FROM THE UPPER LEFT HAND T/R GEARBOX MOUNT HOLE INBOARD THROUGH AN ADJACENT RIVET HOLE TERMINATING AT A CORNER FILLET, ON THE MOUNT FITTING FOR THE TAIL ROTOR GEARBOX. THE AIRCRAFT WAS REMOVED FROM SERVICE AND TRUCKED BACK TO SAINT LOUIS, MO. FROM JOPLIN, MO. FOR TAILBOOM REPLACEMENT. THE AFFECTED TAILBOOM WILL BE SENT TO EUROCOPTER CANADA FOR MOUNT FITTING REPLACEMENT. THE CRACK WAS FOUND VISUALLY AND VERIFIED WITH DYE PENETRANT. THIS AREA OF THE TAILBOOM HAS BEEN KNOWN TO CRACK, IT IS IMPERATIVE THAT THOROUGH INSPECTIONS ARE PREFORMED AT SCHEDULED INSPECTION INTERVALS. 1G72 3U3 U H13EU E5NE10 20041223000212004122300021EU 2004 12 23 MHIA097927 120041102A6510350A34015100 DRIVE SHAFT UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE TAIL ROTOR BENT B MHIAK NONE O OTHER ININSP/MAINT 1 EA25453AE3802 3487 23010 SHAFT WOULD NOT BALANCE BELOW 3IPS, CHECKED ON FLAT PLATE, CENTER TUBE BENT. REPLACED SHAFT. 1G72 3U3 U H9EU E00054EN 20041223000472004122300047 2004 12 23 SWIA200414271 420041212A2216 SERVO CNDAIRCL600 CL6002B19 1900309EA ELEVATOR CONTROLSTUCK A SWIAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM07915SW 7615 ON SHORT APPROACH TO DEN AT 300 FT AGL, ON AUTO PILOT DISCONNECT THE ELEVATOR FROZE. AFTER PULLING HARD ON THE YOKE, CONTROL WAS RESTORED. REMOVED AND REPLACED ELEVATOR SERVO IAW 22-11-24-00. OPERATIONAL TEST GOOD OF ELEVATOR SERVO PER AMM 22-11-24-710-801. 2L72 4F RTA21EA 20041227000062004122700006NE 2004 12 27 DXTA200400483 220041218A720030500005 ENGINE AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE RIGHT MALFUNCTIONED E DXTAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL07215QS478 214 P105568 IN FLIGHT AT FL370- NOTICABLE VIBRATION (INTERMITTENTLY), NO WARNING LIGHTS OR INDICATIONS. RIGHT ENGINE ROLLED BACK, NO ABNORMAL INDICATION, IGNITION LIGHT MOMENTARY ILLUMINATION ONLY RIGHT THROTTLE NOT RESPONSIVE DISCENDING THRU APPROX 29000 FT. ITT EXCEEDED 900 DEG, SHUT DOWN THE RIGHT ENGINE. UNABLE TO DETERMINE CAUSE OF ENGINE VIBRATION, REMOVE AND REPLACE THE RT ENGINE. 2K73 4F4 FRTA50NM E44NE 20041227000082004122700008CE 2004 12 27 DXTA200400479 120041215A315062184033 CIRCUIT CARD CESSNA650 650 2076802CE WARNING HORN FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07791QS 6507091 ON TAKEOFF ROLL THE SPEED BRAKE & NO T/O ANNC LIGHTS CAME ON. THE NO TAKEOFF HORN ALSO WENT OFF. REMOVED AND REPLACED P.C. BOARD B3 IAW CESSNA 650 M.M. CHAPTER 24-50-03. 2L72 4F A9NM 20041227000432004122700043NM 2004 12 27 2004UALA01154 120041124A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT FRAME DENTED ON UPPER FLANGE AT STA 1520 AND STR 26L. INSTALLED NESTED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041227000442004122700044NM 2004 12 27 2004UALA01155 120041124A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT FRAME DENTED AT UPPER FLANGE AT STA 1440, STR 26L. REPAIRED FRAME WITH J ANGLE REPAIR SECTION. 2L72 4F4 FRTA2NM E17NE 20041227000452004122700045NM 2004 12 27 04FDEA03032 120041108A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 AFT CARGO FRAME DENTED AT BS. 1010 STR 26R. REPAIRED PER SRM 51-40-3 2L73 4F RTA3WE 20041227000462004122700046NM 2004 12 27 2004UALA01160 120041124A5320146N38108200 STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT AFT STA 1400L BETWEEN STR 28L AND 29L, PRODUCTION SPLICE PLATE CORRODED. SPLICE STRAP REMOVED AND REPLACED. 2L72 4F4 FRTA2NM E17NE 20041227000482004122700048NM 2004 12 27 HNAA0400171 120041203A2121834280020 COOLING FAN DHAV DHC8 DHC8201 2809001NM E/E BAY BURNED A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07983HA 478 COCKPIT FILLED WITH ELECTRICAL SMOKE IN FLIGHT DECLARED EMERGENCY AND LANDED LGA. INSP'D COAT CLOSET RELAYS, ALSO AVIONICS COMP. INVERTERS, BEHIND INST PANEL, GROUND RAN BOTH ENG'S OPERATED SYSTEMS, ACCOMPLISHED AVIONICS SELF TEST OF ADC. RAN BOTH ENGINES FOR 30 MINUTES, FOUND DSPLY COOLING FAN IS SEIZED UP. NO DAMAGE FOUND IN IMMEDIATE AREA MEL COOLING FAN. 2H72 4T RTA13NM 20041227000492004122700049NM 2004 12 27 2004UALA01183 120041203A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 AFT PIT FRAME INNER FLANGE IS DENTED AT BS 1440 STR 26L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041227000502004122700050 2004 12 27 2004UALA01188 420041203A2565 O-RING BOEING747 747422 1384935NM PWA 4056 PW4056 NE REGULATOR VAVLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29122UA 29168 90 DEGREE ELBOW TUBE ASSEMBLY LEADING WHERE FITTING GOES ON TO THE REGULATOR VALVE AS O-RING. DATA THE SDR DESCRIBES AN AIR LEAK AT THE INTERFACE BETWEEN THE SLIDE BOTTLE REGULATOR ASSEMBLY AND THE 90 DEGREE ELBOW TUBE LEADING TO THE PRESSURE GUAGE. REPLACED O-RING TO STOP LEAK. 2L74 4F4 FRTA20WE E24NE 20041227000532004122700053EU 2004 12 27 EGRA20041227 120041105A5414365A21008216 COWLING AEROSPSA365 SA365N 8680669EU ENGINE DEPARTED E EGRAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 EA17365SJ 269 6018 PILOT NOTICED COWLING WAS MISSING FROM AIRCRAFT AFTER HE LANDED AT HIS HOME BASE. HE REPORTED SEVERE TURBULENCE ENROUTE FROM HIS LAST STOP. HINGE ATTACHED TO COWLING WAS STILL ATTACHED TO AIRCRAFT BUT REMAINDER OF COWLING WAS GONE. PILOT AND CREW WERE UNAWARE OF COWLING DEPARTURE UNTIL LANDING AT BASE. NO OTHER DAMAGE CAUSED BY FAILURE. LATCHES WERE NOT FOUND TO BE WORN. COWLING HAD NOT BEEN OPENED FOR SEVERAL DAYS DURING WHICH MULTIPLE FLIGHTS WERE MADE. COWLING REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1G72 3U H10EU 20041227000542004122700054NM 2004 12 27 2004UALA01192 120041208A5311141N841535 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 MAIN CABIN STA 330 BETWEEN STR 10R & STR 11R, FRAME INBD FLANGE CRACKED. FABRICATED & INSTALLED NEW SECTION OF FRAME. 2L72 4F4 FRTA2NM E17NE 20041228000022004122800002NM 2004 12 28 UPS04643615 120041221A2120 UNKNOWN BOEING767 76734AF 1385212NM COCKPIT FUMES A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01329UP 27755 FUMES IN COCKPIT, NO SMOKE, NO EMERGENCY DECLARED. RAN BOTH ENGS FOR 35 MINS WITH BOTH DUCTS OPERATING WENT TO FULL HOT AND COLD. INSPECTED ENG INLETS RAN AIR INLETS & EXHAUSTS INSPECTED BOTH ACM'S ALSO USED APU AIR WENT FULL HOT & COLD. RAN ENG ABOVE IDLE AND AT IDLE USING PACK OPERATION. UNABLE TO DUP PROBLEM. USED THE FOLLOWING MM REF 21-53-01-6, 21-45-11-4, 21-45-12-4, 21-22-00-0. 2L72 4F RTA1NM 20041228000052004122800005NM 2004 12 28 SWAA043687 120041220A53116546541 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 663, STRINGER 2R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041228000062004122800006EU 2004 12 28 MALA040840 120041123A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD CABIN FLOORBEAM AT FRAME 18 CRACKED AT RBL 20 & RBL 40. REFER TO 409, 226105 FOR ADDITIONAL DETAIL. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228000072004122800007NM 2004 12 28 SWAA043703 120041221A53306545766 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041228000092004122800009NM 2004 12 28 AWXA200401421 120041203A532066142081 WEB BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING C-18 CHECK A .3125 INCH CRACK WAS FOUND IN WEB FORWARD OF L-1 DOOR ENTRANCE AT BS 294.5, STR 11 LT. MAINTENANCE REMOVED CRACKED WEB AT BS 294.5, STR 11 LT; FABRICATED A NEW REPLACEMENT WEB PER DWG 66-14208; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20041228000112004122800011SO 2004 12 28 RAIA00412026 120041220A326023092900001 UPLOCK EMB 145 EMB145LR 3260212SO NLG INTERMITTENT A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK14715 145059 BDL - NOSE GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK BOX. 2L72 4T RTT00011AT 20041228000122004122800012EU 2004 12 28 MALA040836 120041123A5755 STRUCTURE BAC 146 AVRO146RJ85A1500097EU LE SPOILER WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, RIGHT I/B LEADING EDGE SPOILER SCREW HOLES WORN. MAINTENANCE REPAIRED IAW EO A57084. REFER TO 409, 226186 FOR ADDITIONAL DETAIL. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228000132004122800013EA 2004 12 28 04355651 120041220A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA CONTAMINATED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27651BR 7426 LAV SMOKE INDICATION AT 200FT. NO SMOKE OR FUMES BUT ODOR. SUSPECT GLYCOL IN AIR CONDITIONING. MX PERFORMED HIGH POWER RUNS. NO DEFECT NOTED. 2L72 4F RTA21EA 20041228000142004122800014NM 2004 12 28 C1HA200493004 120041122A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 RBL-45 SEAT TRACK FLANGES ARE EXFOLIATED FROM FS 1070 TO 1130, SRM REPAIR. 2L73 4F A3WE 20041228000152004122800015EU 2004 12 28 MALA040834 120041123A5230 SKIN BAC 146 AVRO146RJ85A1500097EU CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, AFT CARGO DOOR INNER SKIN AND INTERNAL TOP DOOR FRAME CRACKED AT TWO LOCATIONS 5 INCHES FROM TOP EDGE OF DOOR. MAINTENANCE REPAIRED IAW EO A52040. REFER TO 409, 226175 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228000162004122800016NM 2004 12 28 C1HA200493010 120041119A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 FLOORBEAM FS 380 BETWEEN RBL 24.75 AND LBL 24.75 UPPER CAP IS CORRODED, SRM REPAIR MINOR. 2L73 4F A3WE 20041228000182004122800018NM 2004 12 28 C1HA200493022 120041201A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1130 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED. INSTALLED REPAIR STRAP, EA-10703, MAJOR. 2L73 4F A3WE 20041228000192004122800019NM 2004 12 28 C1HA200493024 120041201A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1090 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED. INSTALLED FRAME REPAIR, EA-05-53, MINOR. 2L73 4F A3WE 20041228000202004122800020NM 2004 12 28 2004UALA01167 120041130A3220 LANDING GEAR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NOSE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29206UA 30212 NOSE GEAR DID NOT RETRACT FOR SEVERAL MINUTES ON CLIMBOUT AFTER UP SELECTED THEN NOSE GEAR FINALLY RETRACTED. CAPT DECIDED TO CYCLE THE GEAR AND NOSE GEAR SEEMS TO EXTEND OK BUT AGAIN TO ABOUT 30 SECS BEFORE NOSE GEAR STARTED TO RETRACT PER CREW. ACFT JACKED AND THE NOSE LANDING GEAR WAS OPERATIONALLY CHECKED. AFTER SEVERAL GEAR CYCLES ALL INDICATIONS WERE NORMAL WITH NO DEFECTS NOTED. MAXIMUM RETRACT TIME WAS 22 SECONDS. THE LANDING GEAR WAS LUBRICATED AS A PRECAUTIONARY MEASURE. ACFT HAS FLOWN THREE SUBSEQUENT LEGS TO DATE WITHOUT INCIDENT. 2L72 4F4 FRTT0001SE E46NE 20041228000222004122800022SO 2004 12 28 C2XA04TY181 120041221A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BLOWN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714991 145278 TYS, DURING A SCHEDULED INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041228000242004122800024NM 2004 12 28 C1HA200493008 120041118A5320 TRIM PANEL BOEING727 727212 138407GNM FUSELAGE MISSING A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 FWD LAV I/B WALL, DOOR CUTOUT BOTTOM END TRIM PIECE MISSING. SRM REPAIR MINOR. 2L73 4F A3WE 20041228000252004122800025NE 2004 12 28 MALA040857 220041215A7200340B429 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT MAKING METAL A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15429XJ 340B429 RIGHT ENGINE CHIP DETECTOR CAME ON AND STAYED ON IN FLIGHT, RIGHT CHIP DETECT LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT PERSISTED. IN FLIGHT ALL OTHER PARAMETERS WERE NORMAL. DELTA T SPLIT AT 9.00 AND 50 PERCENT TORQUE IS 40 FT HOTTER TO THE RIGHT. AIR RETURN TO DTW. MAINTENANCE ACFT 429 RIGHT ENGINE, S/N GE-E785664, S/N OFF/785747. COMPLETED TASK CARD 7910-303 & 791107 FOUND NON ALLOWABLE DEBRIS AND NO DEBRIS, AFTER RUNS INITIATED SFWI TO REVIEW LAB ANALYSIS WITHIN 40 FLT HOURS. 2L72 4T4 TRTA52EU E8NE 20041228000262004122800026EU 2004 12 28 MALA040855 120041213A2730D97439 ACTUATOR SAAB SF340 340B 7860101EU PITCH TRIM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15421XJ 340B421 BOTH CA AND F/O PITCH TRIM WILL NOT GO BELOW 1/2 UNIT BELOW NEUTRAL. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED MAIN PITCH TRIM ACTUATOR P/N D97439, S/N ON 98G18850, S/N OFF 97B3391, IAW AMM CHAPTER 27-30. ALL OPERATIONAL AND RIG CHECKS GOOD. 2L72 4T RTA52EU 20041228000272004122800027EU 2004 12 28 MALA040856 120041214A2130 A/C PACK BAC 146 AVRO146RJ85A1500097EU NOISY A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15515XJ E2333 RETURN TO DTW LOUD CABIN AIR NOISE SEE PREVIOUS WRITE UP ON LP 1346480 DESCRIP. DETAILS EXACTLY AS PREVIOUS WRITE UP NOISE BEGAN AT 7.0 PSI WENT AWAY AT 6.0 PSI A/C SPEED MOSTLY UNCHANGED STILL SUSPECT PRESSURE LEAK SUGGEST A/C BE PRESSURIZED ON GROUND TO TRY TO DUPLICATE. NOT SURE IF THE NOISE IS HIGH OR LOW IN CABIN. MAINTENANCE PRESSURIZED A/C TO 7.4 PSI, CHECKED ALL DOOR SEALS WHILE PRESSURIZED, NO DEFECTS NOTED. INSPECTED ENTIRE A/C FOR DAMAGE OR LOOSE PANELS, NONE NOTED. INSPECTED OVERHEAD PANELS ROWS 5-8, NO DEFECTS NOTED. INSPECTED ALL DOOR SEALS AFT CARGO FWD CARGO HYD BAY, E&E BAY, ALL SEALS, CHECK GOOD. INSPECTED ENTIRE A/C, NO DEFECTS NOTED. MX REQUESTS TEST FLIGHT. 2H74 4F RTA49EU 20041228000332004122800033NM 2004 12 28 SWAA043677 120041220A53306518420 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND PILOT'S NR 1 WINDOW POST UPPER AFT CORNER SKIN, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041228000342004122800034NM 2004 12 28 SWAA043678 120041220A53116546552 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 827, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041228000352004122800035NM 2004 12 28 SWAA043679 120041220A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN BS 857 AND BS 907, BL 0, WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041228000362004122800036NM 2004 12 28 SWAA043680 120041220A33506104789 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041228000412004122800041NM 2004 12 28 SWAA043684 120041220A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 870, STRINGER 1R, CHAFING. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041228000422004122800042NM 2004 12 28 SWAA043688 120041220A53116520723 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20041228000442004122800044NM 2004 12 28 SWAA043690 120041220A531165C25230 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041228000462004122800046NM 2004 12 28 C1HA200493005 120041119A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 SEAT TRACK AT RBL 22 STA 344-480 IS CORRODED AT SEVERAL AREAS. REPLACED SEAT TRACK. 2L73 4F A3WE 20041228000492004122800049EA 2004 12 28 SWIA200414285 120041005A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 AFT EQUIPMENT COMP; FIREWALL SHUT-OFF SUPPORT INTERCOSTAL HAS A CRACKED ATTACH ANGLE; FS 662.00; STR-9L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2L72 4F RTA21EA 20041228000502004122800050SO 2004 12 28 SWIA200414289 120041218A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 EMERGENCY LIGHT NEXT TO GALLEY, ONE LIGHT IN STRIP INOPERATIVE. REPAIR BROKEN WIRE AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041228000542004122800054SO 2004 12 28 C2XA04TY183 120041222A532014524131009 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 TYS, DURING A SCHEDULED INSPECTION THE FLOORBOARD SUPPORT UNDER THE PAX DOOR SILL CORRODED AROUND NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL SUPPORT UNDER THE PAX DOOR IAW EMB-145 SRM 51-40-02. 2L72 4F RTT00011AT 20041228000562004122800056NM 2004 12 28 C1HA200493012 120041122A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 RBL-25 SEAT TRACK FLANGES ARE EXFOLIATED FROM FS 1070 TO 1130. SRM REPAIR. 2L73 4F A3WE 20041228000582004122800058NM 2004 12 28 AWXA200401420 120041203A534069366001 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 277, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 10 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2L72 4F RTA16WE 20041228000602004122800060 2004 12 28 P9RA20040057 420041220A256561571127 SLIDE BOEING757 757231 1384950NM L4 DOOR UNLATCHED A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO11720TW 30319 CCS GATE, L4 DOOR INADVERTANTLY OPENED IN THE ARMED POSITION. SLIDE DID NOT INFLATE AS CREW MEMBER REACTED AND HELD DOOR TOWARDS THE CLOSED POSITION. THE SLIDE DID SEPARATE FROM THE DOOR. POWER ASSIST BOTTLE DISCHARGED. MAINTENANCE REINSTALLED L4 DOOR SLIDE IAW MM. OPS CHECK OF SYSTEM NORMAL. REMOVED AND REPLACED POWER ASSIST BOTTLE. 2L72 4F RTA2NM 20041228000622004122800062NM 2004 12 28 AWXA200401426 120041202A575465C267933 SKIN BOEING737 7373G7 1384595NM NR 4 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND IN RIVET HOLES OF NR 4 SLAT LOWER SKIN AT TEE CHORD AFT RIVET ROW SLAT STA 94.00. MAINTENANCE CUT OUT DAMAGED AREA OF NR 4 SLAT LOWER SKIN AT SS 94.00; FABRICATED A REPAIR FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20041228000652004122800065EU 2004 12 28 AWXA200401407 120041216A2821QA07301 FILTER ELEMENT AIRBUS320 A320231 3930325EU NR 1 ENGINE CONTAMINATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28621AW 053 AT TAKEOFF, RECEIVED ECAM MESSAGE FOR NR 1 ENG FUEL FILTER CLOGGED, REJECTED TAKEOFF AT 60 KTS, MESSAGE DISAPPEARED AFTER A FEW SECONDS. MADE SEVERAL ATTEMPTS TO TRY & DUPLICATE MESSAGE WITH NO SUCCESS, TAXIED BACK TO RUNWAY & TOOK OFF. AFTER TAKEOFF AT APPROX 1000 FT, NR 1 ENG FUEL FILTER CLOG MESSAGE REAPPEARED & STAYED ON FOR APPROX 5 MINS THEN DISAPPEARED FOR REMAINDER OF FLT. WHEN ACRFT LANDED, MX REPLACED NR 1 ENG FUEL FILTER ELEMENT, LEAK CHK GOOD.MX R/R NR 1 ENGINE FUEL DIFFERENTIAL PRESSURE SWITCH IAW AMM, LEAK & OPS CHECK GOOD. FUNCTIONAL TEST OF FUEL DIFFERENTIAL PRESSURE SWITCH S/N N101 COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT PASSED ALL TESTS PER CMM 73-34-15, REV. 2. 2L72 4F RTA28NM 20041228000692004122800069NM 2004 12 28 C1HA200476004 120040804A5315 FLOORBEAM BOEING727 727* NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15676MG 22554 CORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEAN, TREAT & INSTALLED REPAIR DOUBLER. 2L73 4F RTA3WE 20041228000702004122800070NM 2004 12 28 C1HA200497015 120040925A5754 SKIN BOEING727 727270 138408PNM NR 4 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 (EA) PLACES AT AERODYNAMIC FENCE MOUNTING AREA, (MARKED). REPAIRED 2 (EA) CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1 TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED. 2L73 4F RTA3WE 20041228000712004122800071NM 2004 12 28 C1HA200493007 120041119A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 SEAT TRACK AT RBL 42 STA 344-480 IS CORRODED AT SEVERAL AREAS. SRM REPAIR MINOR. 2L73 4F A3WE 20041228000722004122800072NM 2004 12 28 C1HA200493011 120041120A5320 FLOOR SUPPORT BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 CABIN FLOOR SUPPORT ANGLE AT STA 1183 BETWEEN LT AND RT LAV HAS CORROSION, EA 10696, MINOR. 2L73 4F A3WE 20041228000732004122800073NM 2004 12 28 QXEA200400903 120041221A33506138001 BATTERY BOMBDRDHC8 DHC8401 1390041NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX868 4030 WHILE COMPLING WITH OPERATIONAL CHECK OF EMERGENCY LIGHTS, FOUND LIGHTS INOPERATIONAL TO POWER SUPPLY. MAINTENANCE REPLACED POWER SUPPLY BATTERIES FOR NR 2 POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041228000742004122800074EU 2004 12 28 MALA040863 120041210A7930 PRESSURE SWITCH SAAB SF340 340B 7860101EU OIL PRESSURE FAILED A MALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15414XJ 340B414 JUST AFTER STARTING TAXI, THE RIGHT ENGINE LOW OIL PRESSURE WARNING LIGHT CAME ON, ALL INDICATIONS SEEM TO BE NORMAL. MAINTENANCE CND AS A PRECAUTION, REPLACED PGB LOW OIL PRESSURE WARNING SWITCH, AND ENG LOW OIL PRESSURE WARNING SWITCH. OPS AND LEAK CHECK GOOD. 2L72 4T RTA52EU 20041228000752004122800075EU 2004 12 28 MALA040864 120041213A3213 STRUT BAC 146 AVRO146RJ85A1500097EU MLG DISCHARGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15505XJ E2313 AFTER TAKEOFF THE GEAR WOULD NOT RETRACT, THE AUTO SPOILER AND AUTO THROTTLES DISCONNECTED. AIR RETURN TO DTW. MAINTENANCE UPON INSPECTION NOTED RT MLG STRUT FLAT. REPLACED RT SHOCK ABSORBER IAW TASK CARD 3210-503. PERFORMED LANDING GEAR FUNCTIONAL CHECKS IAW RJ-85 M/M 32-30-00 501. ALL CHECKS GOOD. 2H74 4F RTA49EU 20041228000762004122800076EU 2004 12 28 MALA040865 120041216A3234643500300 HANDLE BAC 146 AVRO146RJ85A1500097EU MLG FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15527XJ E2352 GEAR HANDLE WOULD NOT COME UP WITHOUT GEAR SELECTED TO OVERRIDE. AIR RETURN TO DTW. MAINTENANCE REPLACED GEAR HANDLE WITH SERVICABLE UNIT IAW RJ85MM 32-40-14 201. P/N 6435-003-00, S/N ON 100-99, S/N OFF 070-98. 2H74 4F RTA49EU 20041228000772004122800077EU 2004 12 28 MALA040861 120041204A3233HTE210014 ACTUATOR BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15529XJ E2363 AFTER SELECTING GEAR UP THE IN-HANDLE IN TRANSIT LIGHT ILLUMINATED BUT ALL THREE GREEN LANDING GEAR LIGHTS REMAINED LIT. THE GEAR RETRACTED NORMAL AFTER CYCLING THE GEAR HANDLE. MAINTENANCE CND, REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE ACTUATOR P/N HTE 210014, AS A PRECAUTION S/N OFF M250GB699, S/N ON M253GB799, OPS CHECKS GOOD IAW AMM 32-30-17. 2H74 4F RTA49EU 20041228000782004122800078EU 2004 12 28 MALA040862 120041209A3060 LEAD SAAB SF340 340B 7860101EU NR 3 PROP BLADE BROKEN A MALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15421XJ 340B421 DURING FIRST FLT ICE CHECK RT PROP DEICE FAILS AFTER 1:20-1:30 IN BOTH NORM AND MAX. MAINTENANCE REPAIRED BROKEN LEAD ON NR 3 BLADE, ALL CHECKS GOOD, ALL IAW SF340AMM AND DOWTY MM. 2L72 4T RTA52EU 20041228000792004122800079NM 2004 12 28 C1HA200493014 120041126A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 SEAT TRACK CORROSION AND B/M FS 852-868 LBL 24. REPLACED SEAT TRACK, MINOR. 2L73 4F A3WE 20041228000802004122800080NM 2004 12 28 C1HA200493015 120041122A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 SEAT TRACK CORROSION AND B/M FS 852-868 LBL 24. REPAIRED STRINGER, MINOR EA 10713. 2L73 4F A3WE 20041228000822004122800082GL 2004 12 28 P5CA0401286 220041220A7310 LINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL FMU LEAKING A P5CAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 EA15452PA 30810 706221 RETURNED TO BLOCKS DUE TO NR 3 ENGINE FUEL LEAK FROM DRAIN MASK. FOUND NR 3 ENG FUEL LINE FROM PYLON TO FMU LEAKING AT FMU. RETIGHTENED LINE AT FMU, RUN UP AND LEAK CHECK PER 73-11-10. 2L74 4F4 FRTA20WE E23EA 20041228000842004122800084EU 2004 12 28 AALA20041235 120041220A3350 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2119059 469 JFK - EMERGENCY LIGHT AT SEAT 3G MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 3G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041228000862004122800086 2004 12 28 XNOA1217 420041219A3497 CONNECTOR AIRBUS300 A300B4203 3930306EU DIRECTIONAL GYRODAMAGED A XN0AD RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL23473AS 203 CAPT'S DG FAILED IN FLIGHT. REMOVED, CONNECTOR & REINSTALLED NR 1 DG OPS, CHECKED GOOD. SWAPPED NR 1 DG & NR 3 DG PENDING FURTHER TROUBLESHOOTING, OPS CHECKED NR 1, NR 2, & NR 3 SYSTEMS OPS CHECKED GOOD IAW A300AMM 34-25-34 & 34-25-00. 2L72 4F RTA35EU 20041228000872004122800087NE 2004 12 28 XNO1218 220041221A7200 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE NR 1 MALFUNCTIONED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2379754 21363 NR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME. 2L73 4F4 FRTA3WE E2EA 20041228000882004122800088EU 2004 12 28 DHL2004365007 120041217A3240355511011 CONTROL UNIT AIRBUS300 A300B4203 3930306EU BRAKES MALFUNCTIONED A DHLAO OTHER M OVER TEMP LDLANDING 1 SO01365DH 149 ON LANDING AUTOBRAKE DISARMED AND RE-ARMED BY ITSELF. NR 6 BRAKE LIGHT TEMP REACHED 400 DEG CELSIUS. ALL OTHER BRAKES TEMP REMAINED COLD. DEFERRED AUTO BRAKE SYSTEM TO DMI 18867 IAW MEL 32-42-07, CAT-C. MX NOTIFIED, PLACARD. INSPECTED NR 6 BRAKE IAW MM 32-40-00, NO DEFECTS NOTED. RESET LT INNER BRAKES FAN C/B AND OPS CHECKED GOOD. REFER TO DMI 18867: ON LANDING AUTOBRAKE DISARMED AND RE-ARMED BY ITSELF. NR 6 BRAKE LIGHT TEMP REACHED 400 DEGREES CELSIUS. ALL OTHER BRAKES TEMP REMAINED COLD. REMOVED AND REPLACED AUTO BRAKE UNIT IAW MM 32-42-57, THAT CLEAR DMI 18867 PLACARD REMOVED. 2L72 4F RTA35EU 20041228000902004122800090EA 2004 12 28 SWIA200414283 120041005A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSLAGE CORRODED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07588SW 7069 LEFT SIDE SEAT RAILS CORRODED FROM FS 364 - FS 559+79. ITEM FOUND AT C-CHECK INSPECTION. SEAT RAILS REPLACED IAW CRJ SRM 51-41-02, 51-41-04, 51-23-00, REO 601R-53-00-055 REV NC. 2L72 4F RTA21EA 20041228000922004122800092NM 2004 12 28 C1HA200493020 120041201A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1110 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED, EA-10705, MAJOR. 2L73 4F A3WE 20041228000942004122800094GL 2004 12 28 P5CA0401291 220041214A7200 ENGINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 1 BIRD INGESTION A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CLCLIMB 1 EA15451PA 30809 706363 BIRD INGESTION INTO NR 1 ENG AT ROTATION. ENG SHUT DOWN. PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-14. REPLACED ENG PER PAC: P71-00-00-1A AND P71-00-00-2A. 2L74 4F4 FRTA20WE E23EA 20041228000962004122800096NM 2004 12 28 AWXA200401422 120041209A5753 SKIN BOEING737 7373G7 1384595NM FORE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING C-18 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF RT OUTBOARD FORE FLAP AT WBL 220.00. MAINTENANCE REMOVED DISBONDED SKIN ON LOWER SURFACE OF RT OUTBOARD FORE FLAP FROM WBL 216 TO WBL 224; FABRICATED A NEW SECTION OF SKIN AND A DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 30. 2L72 4F RTA16WE 20041228000982004122800098NM 2004 12 28 AWXA200401424 120041203A5752 SKIN BOEING737 7373G7 1384595NM AILERON TAB DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK THE RT AILERON TAB WAS FOUND SEPARATING AT THE TRAILING EDGE 22.5 INCHES FROM THE OUTBOARD END, WBL 456.25 - WBL 458.75. MAINTENANCE PERFORMED BOND REPAIR ON RT AILERON TAB TRAILING EDGE IAW B737-300 SRM 51-70-06 FIG 13. 2L72 4F RTA16WE 20041228001002004122800100NM 2004 12 28 SWAA043686 120041220A53306545800 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 294.5 + 16, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041228001022004122800102NM 2004 12 28 C1HA200493023 120041201A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1148 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX WAS REMOVED. INSTALLED REPAIR STRAP, EA-10720, MAJOR. 2L73 4F A3WE 20041228001032004122800103NM 2004 12 28 C1HA200493025 120041201A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1070 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED. INSTALLED REPAIR STRAP PER EA 10700, MAJOR. 2L73 4F A3WE 20041228001052004122800105NM 2004 12 28 SWAA043691 120041221A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 787, STRINGER 9R AND BS 827, STRINGER 9. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041228001072004122800107NM 2004 12 28 SWAA043693 120041221A531165353656 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 3 EACH SHEAR TIES CRACKED FROM BS 360, STRINGER 13L AND BS 400, STRINGER 14L. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20041228001082004122800108 2004 12 28 MALA040848 420041123A2565 GIRT BAR BAC 146 AVRO146RJ85A1500097EU SERVICE DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD SERVICE DOOR GIRT BAR FITTINGS & FLOOR SUPPORT PLATE FROM FRAME 15-18 IS CORRODED. MAINTENANCE REPLACED FITTINGS & SILL PLATES IAW SRM 51-42-00, 51-43-00, 51-23-00. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001092004122800109NM 2004 12 28 SWAA043694 120041221A531065353656 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041228001102004122800110NM 2004 12 28 SWAA043695 120041221A53306545772 SKIN BOEING737 7373Y0 1384671NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN FROM BS 862 TO BS 887, BL 0 TO RBL 5, WORN. REPAIRED SKIN SECTION PER SRM. 2L72 4F RTA16WE 20041228001112004122800111NM 2004 12 28 SWAA043696 120041221A53156546546 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 5 EACH CRACKS ON LONGITUDINAL FLOORBEAM AT BS 727B, FROM LBL 43 TO RBL 47. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20041228001132004122800113NM 2004 12 28 SWAA043697 120041221A53156545410 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND LOGITUDINAL FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED CHORD PER ER. 2L72 4F RTA16WE 20041228001152004122800115EU 2004 12 28 MALA040841 120041123A5320 ANGLE BAC 146 AVRO146RJ85A1500097EU MLG WW CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, MLG BAY BAFFLE TOP ATTACHMENT ANGLE IS CRACKED. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001162004122800116EU 2004 12 28 MALA040846 120041123A5330 LONGERON BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, REAR CARGO BAY LOWER COMPARTMENT LONGERON I/B SIDE BETWEEN FRAMES 35 & 36 DAMAGED. MAINTENANCE REPAIRED IAW EO A53228. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001182004122800118EU 2004 12 28 MALA040850 120041107A2520 FRAME BAC 146 AVRO146RJ85A1500097EU PAX SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FROM 409, 224360, 10 EA SEAT TRACK CRACKED. MAINTENANCE REPAIRED IAW EO A25031. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001192004122800119NM 2004 12 28 P5CA0401288 120041220A7830 LINK BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE BLOCKER DOOR MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 EA15508MC 21644 517969 NR 4 ENGINE T/R BLOCKER DOOR LINK MISSING AT 4 O'CLOCK POSITION. REMOVED BLOCKER DOOR AND BROKEN LINK PER CDL 78-31-1. T/R LOCKED OUT PER DDPG 78-1. 2L74 4F4 F A20WE E23EA 20041228001202004122800120EU 2004 12 28 RAIA00412027 120041220A33506134031 POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03558HK 41071 BWI - PART OF EMERGENCY ESCAPE PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 2 AND NR 3 EMERGENCY POWER SUPPLIES. 2L72 4T RTA41NM 20041228001222004122800122EA 2004 12 28 QXEA200400891 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION AT FUSELAGE STATION 415.00 AND 476.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041228001242004122800124WP 2004 12 28 UPS04843617 120041221A351080130700 REGULATOR DOUG DC8 DC871F 302199DWP COCKPIT O2 INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 CREW O2 LOW, POSSIBLE LEAK. ROBBED KNOWN GOOD O2 REGULATOR FROM FWD COURIER POSITION AND INSTALLED AT F/E'S POSITION, OPS AND LEAK CHECK GOOD. 2L74 4F RT4A25 20041228001262004122800126NM 2004 12 28 P5CA0401287 120041219A36108988061 REGULATOR VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 2 ENGINE FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15508MC 21644 517772 ON TAXI OUT DUCT LOW PRESS LIGHT CAME ON WITH DROP IN DUCT PRESSURE ON GAGE. ISOLATED LEFT WING PRESS LESS THAN 15 PSI. REPLACED PRESSURE REGULATOR VALVE ON ENGINE NR 2 PER MM 36-1114. PERFORMED ENGINE RUN PER MM 71-00-00. OPS CHECK OK. 2L74 4F4 F A20WE E23EA 20050104000512005010400051NM 2005 1 4 04FDEA03335 120041202A2841 DISPLAY DOUG MD11 MD11 3023602NM COCKPIT MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25608FE 48548 1 HOUR INTO FLIGHT, THE LEVEL 2 ALERT FUEL QTY/USED CHK CAME ON. CHECKED FUEL ON BOARD, SHOWED 4,300 NR DIFFERENCE. SHORTLY AFTER, THE ALERT WENT AWAY. PRIOR THE LAT FUEL UNBAL LEVEL TWO ALERT HAD COME ON TWICE DURING FIRST HOUR OF FLIGHT. CALCULATED FOB AND COMPARED TO INDICATED FUEL ON BOARD AND DURING FLIGHT. UNRELIABLE QTY AND POSSIBLE FUEL LEAK. DIVERTED TO EWR. ON POST FLIGHT INSPECTION, FOUND NO VISIBLE EVIDENCE OF FUEL LEAK. INTERROGATED FQBU FOR FAULTS NR 3 TANK SHOWING NR 15 T/U SHOWING "CAP OUT" AND "OPEN PROBE" FAULTS. R-T-S OF FSC, ALL PASSED. RELEASED FOR SERVICE PER MEL: TANK NR 3 FUEL TANK SYNOPTIC QTY DISPLAY, INOP. 2L73 4F RTA22WE 20050104000542005010400054NM 2005 1 4 04FDEA03302 120041201A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08. 2L73 4F RTA22WE 20050104000592005010400059NM 2005 1 4 04FDEA03382 120041207A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK LBL 107 CORRODED AT STA 425 TO STA 450. CORROSION REMOVED AS PER SRM 51-21-01. FOUND OUT OF LIMIT AS PER SRM 53-70-00. REPLACED AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050104000692005010400069NM 2005 1 4 04FDEA03337 120041202A5320AEA0526U2 DOUBLER DOUG MD11 MD11 3023602NM LANDING GEAR WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CENTER LANDING GEAR WHEEL WELL RT STA Y= 1381, DOUBLER FOUND CRACKED AT LOCATION ADJACENT TO RT SPOILER MIXER. DOUBLER FABRICATED PER DOUGLAS DRAWING NR AEA0526 AND PART MARKED PER GMM 7-0-1001. CRACKED DOUBLER AT CENTER LANDING GEAR WHEEL WELL RT STA Y= 1381 ADJACENT TO RT SPOILER MIXER. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050104000772005010400077EU 2005 1 4 04FDEA03378 120041206A5245 FITTING AIRBUS310 A310 EU A/C ACCESS DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND SEVERAL HOLES OF FITTINGS AT ACCESS DOORS (147 CZ) TO AIR COND COMPT DAMAGED. REPAIRED IAW EA 6-5315-82534. 2L72 4F RTA35EU 20050104000852005010400085NM 2005 1 4 04FDEA03397 120041209A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057. 2L73 4F RTA22WE 20050104000992005010400099 2005 1 4 04FDEA03182 420041122A2230 COMPUTER AIRBUS310 A310 EU AUTOTHROTTLE SYSMALFUNCTIONED A FDEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO25456FE 318 USING TOGA FOR T/O ON A WET SLIPPERY RWY. THROTTLE 2 RACED TO TRP THRUST LIMIT BUT THROTTLE 1 REMAINED AT 40 PERCENT N1, DISCONTINUED T/O ATTEMPT. REMOVED AND REPLACED THRUST CONTROL COMPUTER AS PER AMM 22-36-34-4-02. PERFORMED AFS TEST/LAND TEST AS PER AMM ADJ/TEST REF.22-40-00-5. ALL TEST SATISFACTORY. DMI CLEARED. PLACARD REMOVED. PLS CHECKED CAT 3. 2L72 4F RTA35EU 20050104001032005010400103WP 2005 1 4 04FDEA03229 120041126A5753ARC15604 SKIN DOUG DC10 DC1010 3022110WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF, FOUND RT WING OUTBD FLAP UPPER SIDE. LEADING EDGE B/T STA XOF 775-759 HAVE SKIN WITH WEAR DEEP. REPLACED SKIN PANEL X SRM 51-33-01 PG 34-47 DWG ARC1560. 2L73 4F A22WE 20050104001202005010400120EU 2005 1 4 04FDEA03458 120041221A7830 THRUST REVERSER AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C GL NR 1 ENGINE MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25653FE 736 705270 ON TAKEOFF RWY 6 KBDL- NR 1 ENGINE REV PRESSURIZED LIGHT CAME ON AT 70 KNOTS, ENGINE N1 APPROX 75 PERCENT. REJECTED TAKEOFF AT 72 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 31DEC04 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND REPLACED DIRECTIONAL PILOT VALVE AND PRESSURE SWITCH ASSY ACCORDING TO AMM78-31-06-2-F. T 29DEC04 05:38 SEAR WITH REF TO: A300-600 AMM 78-30-00-5 (GE-CF680C2A5F) NR 1 ENGINE THRUST-REVERSER RETURNED TO SERVICE. COMPLIED WITH AMM INSPECTION & OPERATING OUTLINE. NO REPEAT OF DISCREPANCY. CHECKS OK. MEL PLACARD REMOVED. 2L72 4F4 FRTA35EU E23EA 20050104001212005010400121NM 2005 1 4 04FDEA03489 120041227A5350 FRAME DOUG MD11 MD11 3023602NM TAIL CONE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 FWD TAIL CONE AFT MOST FRAME CRACKED AT 2 PLACES ABOVE & BELOW THE RIGHT TOP LATCH KEEPER ASSY CUTOUT AREA. REPAIRED AS PER SRM 53-00-01 FIG 9 VOL 2. 2L73 4F RTA22WE 20050104001302005010400130WP 2005 1 4 AALA20041230 120041218A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21559AA 53089 DEN - OVERHEAD EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR OVERHEAD EMERGENCY LIGHT BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001452005010400145NM 2005 1 4 AALA20041216 120041213A33501722331 CONNECTOR BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21373AA 25200 ORD - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26B INOPERATIVE. REPLACED CONNECTOR AND CONTACT SOCKET (1703663 MID STATE AEROSPACE) FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050104001542005010400154NM 2005 1 4 SWAA043716 120041224A5320BAC1517 STIFFENER BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29522SW 26564 DURING SCHEDULED RON CHECK, FOUND FLOOR SUPPORT STIFFENER CORRODED AT BS 270, LBL 4, WL 207.5. REPAIRED STIFFENER PER SWA EA. 2L72 4F RTA16WE 20050104001602005010400160NM 2005 1 4 SWAA043632 120041214A2612100064901 FIRE DETECTOR BOEING737 7373H4 1384600NM AFT CARGO BAY FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW29602SW 27953 DIVERSION/DECLARED EMERGENCY, AFT CARGO COMPARTMENT FIRE INDICATION IN FLIGHT, QRH PROCEDURES FOLLWED. REMOVED AND REPLACED CARGO FIRE DETECTORS, METERING VALVE, DIVERTER VALVE, CARGO FIRE CONTROL PANEL PER MM. 2L72 4F RTA16WE 20050104001622005010400162NM 2005 1 4 SWAA043603 120041212A3350101331 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050104001722005010400172 2005 1 4 SWAA043634 420041215A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20050105000012005010500001NM 2005 1 5 DL757041128 120041222A3350 CONTACTOR BOEING757 757232 1384965NM EXTERIOR LIGHT CORRODED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27622DL 22912 ON LAYOVER FOUND 3L EXTERIOR EMERGENGY LIGHT INOP. RELAMPED, NO HELP. FOUND CONTACTS CORRODED. CLEANED SAME, OPERATION OK. 2L72 4F RTA2NM 20050105000072005010500007 2005 1 5 DL73S041136 420041224A3417HG480B42 ADC BOEING737 737232 1384475NM E/E BAY CONTAMINATED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27304DL 23076 AFTER DE-ICING AUTOTHROTTLES DISARMED DURING T/O, NO RE-ENGAGE AT ACCEL PDC CADC FAIL MSG, MACH TRIM FAIL LIGHT. DURING CLIMB CAPTS A/S AND ALTM OFF MSG AFTER LVL OFF. AT FL 290 APPROX 5 MIN CABIN ALT WARN HORN DIFF PRESS 6 PSI, CABIN ALT 10K. FOLLOWED QRH AND RTB CVG. FOUND CAPTS ALT OFF FLAG / PDC INPUT FAIL LIGHT ON, FOUND BOTTOM OF CADC NR 1 WET W/GYLCOL. INSPECTED MOISTURE TRAPS BOTH SYS DRY. DRIED AREA RPLCD NR 1 CADC PER M/M. PERFORMED CADC TEST PER MM, ALL IND OF SUSPECT GYLCOL ENTERED/ STAIRWAY DOOR. 2L72 4F RTA16WE 20050105000092005010500009NM 2005 1 5 DLM88041138 120041225A33970201875003 WIRE HARNESS DOUG MD88 MD88 3023688NM CABIN DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27987DL 53338 PASSENGER SEAT 13D EMERGENCY TRACK LIGHTING INOP. REPLACED DAMAGED HARNESS. 2L72 4F RTA6WE 20050105000152005010500015NM 2005 1 5 DL733041124 120041219A53306545768229 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27312WA 23598 INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVEALED A 3 INCH CRACK ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 15R AT FS 500D+7. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND PER ER/A 095736-14AD. 2L72 4F RTA16WE 20050105000212005010500021NM 2005 1 5 DL76S041148 120041228A2560BPS73 POWER SUPPLY BOEING767 767332 1382001NM RT EMERG EXIT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27127DL 24077 FOUND ON TRANSIT CHECK, EMERGENCY ESCAPE SQUIB TEST INOP IN BOTH TEST 1 AND 2. REPLACED POWER SUPPLY. 2L72 4F RTA1NM 20050105000302005010500030EU 2005 1 5 DXTA200400478 120041212A3230 SEQUENCE VALVE BRAERO1000 BAE1251000A 1500104EU RT MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07542QS 259042 IMMEDIATELY AFTER TAKEOFF AND GEAR RETRACTION, THE RT GEAR IN TRANSIT LIGHT (RED LIGHT) REMAINED ILLUMINATED. PRIOR TO LOWERING GEAR REQUESTED (2) LOW FLIGHT PASSES WITH LIT TOWER FOR VISUAL VERIFICATION, TOWER ADVISED THE RIGHT MAIN GEAR DOOR WAS SLIGHTLY OPEN. LOWERED THE GEAR AND STBY INDICATORS INDICATED ALL GEAR DOWN AND LOCKED WITH NO RED LIGHTS. LANDED UNEVENTFULLY. ADJUSTED RT MLG REVERSING VALVE IAW HAWKER 1000 AMM 32-30-25. ADJUSTED RT MLG SIDE STAY IAW HAWKER 1000 AMM 32-10-10. PERFORMED 25 GEAR RETRACTIONS/EXTENSIONS IAW HAWKER 1000 AMM 32-10-10 & 32-30-25. OPS CHECK GOOD. 2L72 4F RTA3EU 20050105000412005010500041WP 2005 1 5 UPS04843606 120041111A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 INSPECTION TYPE:C3 LONGERON 16R AT FS 1728 IS CRACKED AT FRAME ATTACHMENTS, LENGTH OF CRACKS IS APPROX 1.5 INCH. REPAIRED LONGERON AT 16R STA1728 IAW DWG 5644130, DC-8 53-2-2 FIG 10, SRM 53-02-02-0, SRM 51-1-20D. 2L74 4F RT4A25 20050105000422005010500042NM 2005 1 5 UPS04443604 120041213A3350 BATTERY PACK BOEING747 747212B 1384886NM CABIN FAULTY A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE INTERMITTENT REQ A829506. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER 747 MM 33-51-04. 2L74 4F A20WE 20050105000552005010500055NM 2005 1 5 UPS04243174 120040831A5280 SKIN BOEING727 727173C 1384059NM RT MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, RIGHT WING DOOR LOWER SKIN HAS TWO SUSPECT CRACKS IN SKIN AT FWD END MID WAY ON DOOR. WING DOOR REPLACED ON NRC 733172. 2L73 4F A3WE 20050105000602005010500060NM 2005 1 5 UPS04443319 120040930A5730 PLATE BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, RIGHT BS 1241 WL 180 UPPER WING SPLICE PLATE NR 5 FASTENER HOLE CORROSION CRACK REVEALED AT WING UPPER SKIN LAYER. RIGHT BS 1241 UPPER WING SPLICE PLATE NR 5 FASTENER HOLE AT UPPER SKIN LAYER REWORKED AS PER EO B747-5740-17032. 2L74 4F A20WE 20050105000632005010500063NM 2005 1 5 UPS04543414 120041026A3350 LIGHT BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01455UP 25476 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS, WARNING LIGHT INOP BULBS TEST BAD. RELAMPED PER MM 33-50-00, OPS CHECK SATISFACTORY. 2L72 4F RTA2NM 20050106000012005010600001EU 2005 1 6 MALA040889 120041124A5320 FITTING SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, COCKPIT WALL AT LBL 10.5, T-SECTION IS CORRODED. DAMAGE WAS REPAIRED IAW MESABA EO S53264. AIRCRAFT RETURNED TO SERVICE 11/28/04. 2L72 4T RTA52EU 20050106000132005010600013NM 2005 1 6 MWEA040227 120041227A5270 SENSOR BOEING717 717200 1383700NM GALLEY DOOR OUT OF ADJUST A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31913ME 55176 GALLEY DOOR ILLUMINATED. FORWARD GALLEY DOOR SHOWS MARGINAL READING FOR PROXIMITY SENSOR, REQUIRES ADJUSTMENT OF SENSOR. 2L72 4F TRA6WE 20050106000212005010600021NM 2005 1 6 P5CAO401283 120041207A8011 SEAL BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 2 STARTER NICKED A P5CAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA15451PA 30809 706214 SECONDARY ENGINE EXCEEDANCE DUE WITH LOW NR 2 ENG OIL QTY DOWN TO 4 GALS. A/C RETURNED TO SHJ. INSPECTED ENG NR 2, FOUND STARTER MOTOR SHAFT SEAL NICKED AND OIL LEAK. REPLACED SEALS & ENG RUN/LEAK CHECKED PER MM 80-11-02. 2L74 4F4 FRTA20WE E23EA 20050106000262005010600026NM 2005 1 6 P5CA0401294 120041223A2910 DRAIN MAST BOEING747 747283B 1384867NM NR 3 ENGINE LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 EA15921FT 21575 NR 3 ENGINE HYD LEAK AT DRAIN MAST. FOUND HYD LEAK WITHIN LIMITS PER MM 29-11-00 FIG 601. 2L74 4F A20WE 20050106000312005010600031NM 2005 1 6 PCAA0406226 120040622A3260864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAULTY A PCAAO OTHER J WARNING INDICATION CRCRUISE 1 EA13824EX 387 FLIGHT 3875 REPORTED THE YELLOW GEAR SELECTOR LEVER ILLUMINATING ALONG WITH THE RED NOSE GEAR LIGHT AND THEN BOTH GOING OUT. ALSO A THUMPING NOISE WAS HEARD FROM THE NOSEWELL AREA. THIS HAPPENED APPROXIMATELY FOUR TIMES. THIS CONDITION HAD A HISTORY 14JUN04, REF SDR 222, PSEU WAS REMOVED AND REPLACED. CURRENT DISCREPANCY DATED 22JUNE04 WAS REMEDIED WITH THE REMOVAL AND REPLACEMENT OF THE NOSE GEAR DRAG STRUT PROXIMITY SENSOR. SYSTEMS WERE OPERATIONAL CHECKED AND A TEST FLIGHT COMPLIED WITH, ALL CHECKS GOOD. 2H72 4T RTA13NM 20050106000342005010600034NM 2005 1 6 249TR0040 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BS 270 FLOORBEAM HAS CORROSION BETWEEN RBL 10 AND LBL 10. REPAIRED PER EA 53-345. 2L72 4F RTA16WE 20050106000352005010600035NM 2005 1 6 249TR0044 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON BS 312 FLOORBEAM. REPAIRED PER SRM 53-10-9. 2L72 4F RTA16WE 20050106000492005010600049NM 2005 1 6 QXEA200400887 120041213A5260 TRACK BOMBDRDHC8 DHC8401 1390041NM AFT STAIRS WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - AFT ENTRY STAIR CARRIAGE ASSEMBLY TRACK IS WORN THIN ON THE INBOARD UPPER FLANGE NEAR AFT EDGE OF AFT ENTRY DOOR. REPAIRED IAW Q400 SRM 51-41-00 AND SRM 52-12-31-400-803. 2H72 4T RTA13NM 20050106000582005010600058NM 2005 1 6 QXEA200400865 120041130A5420 STIFFENER BOMBDRDHC8 DHC8401 1390041NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - LEFT HAND NACELLE STATION XN269, ZN10, YN-3 SHEET METAL DECK BELOW EXHAUST DUCT HAS CRACKED STIFFENER. REPAIRED IAW Q400 SRM TASK 51-42-05-330-001. 2H72 4T RTA13NM 20050106000702005010600070NM 2005 1 6 SWAA043662 120041217A57536546435277 STRUCTURE BOEING737 7373Y0 1384671NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20050106000802005010600080 2005 1 6 2004UALA01185 420041203A256562774414 SLIDE BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN DEPLOYED A UALAK NONE O OTHER ININSP/MAINT 1 WP29780UA 26944 SLIDE RECEIVED DEPLOYED. LWR LT SIDE INFLATION CHAMBER BLOWN OUT GREATER THAN 36 INCHES LONG. SLIDE RECEIVED IN SHIPPING CRATE W/O PACKBOARD OR VALISE COVER. SLIDE WAS INADVERTANTLY DEPLOYED. FINDINGS METER INDICATED SLIDE DEPLOYMENT WAS NORMAL AND SLIDE WAS NOT DAMAGED. IT IS ASSUMED DAMAGE OCCURRED SUBSEQUENT TO DEPLOYMENT DURING REMOVAL FROM AIRCRAFT OR DURING HANDLING AND SHIPPING. 2L72 4F4 FRTT0001SE E46NE 20050106001012005010600101NM 2005 1 6 2004UALA01253 120041227A2121 FAN BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT RECIRC FAILED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29198UA 28716 ELEC UTIL BUS R EICAS ADVISORY MESSAGE DISPLAYED. UTILITY BUSS 3 (OR 4) OR GALLEY BUSS 3 (OR 4) DOES NOT HAVE ELECTRICAL POWER ON IT. AIRPLANE IS NOT IN LOAD SHED CONDITION. THE LOWER LEFT RECIRCULATION FAN BEARINGS FAILED. THE FAN WAS REPLACED AND THE AIRCRAFT HAS NO FURTHER PROBLEMS. 2L74 4F4 FRTA20WE E24NE 20050106001132005010600113NE 2005 1 6 2004UALA01240 220041219A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 SPARKS A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29561UA 26661 RETURN TO BLOCKS DUE TO NR 1 ENGINE SPARKS. 2L72 4F4 FRTA2NM E17NE 20050106001202005010600120NM 2005 1 6 2004UALA01248 120041223A5311 FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 DENT WAS FOUND ON THE UPPER I/B T-CHORD ON FRAME AT STA 900 APPROX LBL 20 IN THE FWD HORIZONTAL FLANGE OF THE CHORD. REPAIR ACCOMPLISHED. 2L74 4F4 FRTA20WE E24NE 20050106001212005010600121NM 2005 1 6 2004UALA01249 120041222A2530 SMOKE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GALLEY DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29395UA 24670 FLIGHT ATTENDANT SAW SMOKE COMING FROM AFT GALLEY TRASH COMPACTOR AREA. LINE MAINTENANCE ACCOMPLISHED A DETAILED INSPECTION AND OPERATIONAL CHECK ON THE SUSPECT TRASH COMPACTOR. NO EVIDENCE OF SMOKE WAS FOUND ON THE DETAILED INSPECTION, AND A SUBSEQUENT OPERATIONAL CHECK FOUND THE UNIT TO BE WORKING NORMAL. NO OTHER EVENTS REPORTED AFTER THIS CHECK WAS DONE.POSSIBLE CAUSE FOR THE SOURCE OF THE SMOKE WAS LOCATED IN THE TRASH ITSELF AND NOT PART OF THE TRASH COMPACTOR. 2L72 4F4 FRTA16WE E2GL 20050106001222005010600122NM 2005 1 6 2004UALA01250 120041222A3830 TOILET BOEING757 757222 1384956NM PWA 2037 PW2037 NE LAVATORY INOPERATIVE A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29538UA 25222 DIVERTED DUE TO LAVATORY FLUSH SYSTEM INOPERATIVE. CAUSED BY CLOG / BLOCKAGE IN PLUMBING. SERVICED LAVATORIES, ALL OPS NORMAL. NO FLUID SPILLAGE NOTED. 2L72 4F4 FRTA2NM E17NE 20050106001342005010600134SO 2005 1 6 SWIA200414288 120041217A5210 SPLICE EMB 120 EMB120ER 3260203SO PAX DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07224SW 120294 MAIN CABIN DOOR HANDLE WILL NOT ACTUATE DOOR LOCKS. INSTALLED NEW BOLT ON MAIN CABIN DOOR INSIDE LOCKING HANDLE AND CLEANED OUT SPLICES ON HANDLE AND DOOR HANDLE SHAFT IAW MM 52-11-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050106001502005010600150NM 2005 1 6 AALA20041161 120041123A3350 SOCKET BOEING777 777223 1385213NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21799AN 30258 EXTERIOR EMERGENCY EXIT LIGHTING AT R3 INOPERATIVE. REPLACED SOCKET ASSEMBLY FOR EMERGENCY EXIT LIGHT AT R3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050106001562005010600156NM 2005 1 6 AALA20041164 120041124A3350BPS73 BATTERY PACK BOEING767 767223 1385123NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21339AA 22336 EMERGENCY LIGHTS FROM SEATS 31A TO 37A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS FROM SEATS 31A TO 37A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050106001572005010600157WP 2005 1 6 WX0400056 120041123A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19865GA 49998 LAS-MAINTENANCE REPORTED EMERGENCY OVERHEAD LAMPS BURNED OUT (3 EACH). MAINTENANCE RELAMPED OVERHEAD LAMPS (3 EACH), OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001682005010600168WP 2005 1 6 WX0400052 120041109A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19861GA 49557 LAS - MAINTENANCE REPORTED AFT EMERGENCY LIGHTS AND STANDBY POWER EMERGENCY LIGHT ROW 8 INOPERATIVE. MAINTENANCE RE-LAMPED AFT EMERGENCY LIGHTS AND STANDBY POWER EMERGENCY LIGHT AT ROW 8 IAW MM 33-50-00. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001702005010600170WP 2005 1 6 WX0400044 120041025A3397 WIRE DOUG DC9 DC987 3022087WP CABIN SHORTED A WX0AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP19945MA 49725 IFP - DURING PUSHBACK FLIGHT ATTENDANTS REPORTED ELECTRICAL SPARKS EMANATING FROM THE OVERHEAD BIN NEXT TO THE FORWARD LAVATORY. THE COCKPIT FILLED WITH DENSE WHITE ELECTRICAL SMOKE AFTER THE SPARKS WERE REPORTED. MAINTENANCE FOUND WIRES 1L1651E18, 2L1651E18, 1L1701E18 AND 2L1701E18 SHORTED AGAINST GALLEY AISLE LIGHT SHROUD. MAINTENANCE REPAIRED WIRING IAW AMM/SWPM 20-50-01 AND INSPECTED ALL WIRING IN AREA IAW SWPM 20-00-06. NO FURTHER DAMAGE FOUND. SIDEWALL LIGHTING OPERATIONALLY TESTED GOOD IAW AMM 33-20-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001712005010600171WP 2005 1 6 WX0400038 120040928A3350 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19862GA 49556 DEN - MAINTENANCE REPORTED AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE ARMED LIGHTS TO CHARGE THE EMERGENCY LIGHT BATTERIES. SYSTEM OPERATIONALLY CHECKED GOOD IAW 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001722005010600172WP 2005 1 6 WX0400039 120040928A33501315 LIGHT DOUG DC9 DC983 3022083WP CATWALK INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19862GA 49556 DEN - MAINTENANCE REPORTED TAIL EMERGENCY LIGHT AND CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-LAMPED TAIL EMERGENCY LIGHT, RE-SEATED RIGHT SIDE CATWALK LIGHT AND RE-LAMPED LEFT SIDE CATWALK LIGHT. TAIL AND CATWALK EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001732005010600173WP 2005 1 6 UPS04843571 120041122A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 EXTERNAL FUSELAGE SKIN CRACKED AT RT AFT HEAT EXCHANGER CUT OUT LOWER AFT CORNER. REPAIRED PER EO DC8-5330-4732-D. 2L74 4F RT4A25 20050106001742005010600174WP 2005 1 6 UPS04843579 120041119A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING CENTER L/E RIB CRACKED AT XW429 UPPER RIB. STOP DRILLED CRACK, NDT VERIFIED TERMINATION PER SPM 06-10-01.001. FABRICATED STACKED ANGLE REPAIR DOUBLERS FROM SHT7075T6/.040 AND .050 THICK REF SRM 57-3-1 FIG 4 ITEM C, 57-2-0 FIG2. INSTALLED PARTS REF SRM 51-1-20D, 51-1-8, 57-2-0. 2L74 4F RT4A25 20050106001752005010600175NM 2005 1 6 UPS04643600 120041212A256080230014 PBE BOEING767 76734AF 1385212NM CABIN UNSERVICEABLE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01316UP 27744 EMERGENCY PBE SMOKE MASK IS IN QUESTIONABLE CONDITION. BAG VACUUM IS MISSING. REPLACED PBE. 2L72 4F RTA1NM 20050106001772005010600177WP 2005 1 6 UPS04843586 120041129A53203755843502N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 BATHTUB FITTING CRACKED AT STA 1200 L34R-L35R. FITTING HAD BEEN PREVIOUSLY REPLACED. REMOVED AND RETAINED SPLICE PLATES FROM CRACKED FITTINGS REF SRM 51-1-20D. CUT REPLACEMENT FITTING, DRILLED, TREATED, AND PRIMED PER SRM 53-2-0 FIG2D. REMOVED AND REPLACED FITTING REF SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20050106001782005010600178WP 2005 1 6 UPS04843572 120041114A532037584962 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 INTERCOSTAL TO FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050106001822005010600182 2005 1 6 UPS04143553 420041126A2565 WARNING SYSTEM AIRBUSA300 A300F4622R 3930360EU EVAC SLIDE FALSE ACTIVATIONA IPXAK NONE O OTHER ININSP/MAINT 1 SO01156UP 0845 EVACUATION SLIDE WARNINIG SYSTEM RED LIGHT INOP ASSOCIATED WARNING BUZZER. RESET C/B (SLIDE ARM AND WARNING) LIGHT, OPS CK GOOD THIS CLEARS M292019 PLACARD REMOVED. 2L72 4F RTA35EU 20050106001842005010600184NM 2005 1 6 UPS04443554 120041129A5280 DOOR FRAME BOEING747 747121 1384871NM RT GEAR DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 RT AFT BODY GEAR DOOR ATTACH FRAME CRACKED. REMOVED CRACKED CHANNEL; OK TO INSTALL REPLACEMENT FRAME; BEGAN INSTALLATION; OF NEW FRAME 8EA FASTENERS AT AFT BULKHEAD REQUIRE INSTALLATION; FINISHED INSTALLATION AS PER SRM 51-30-02. 2L74 4F A20WE 20050106001862005010600186WP 2005 1 6 UPS04843556 120041130A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01729UP 46029 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK. OPS CK NORMAL. 2L74 4F RT4A25 20050106001872005010600187WP 2005 1 6 UPS04843513 120041029A5311DWGS2750825 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 CORROSION ON FRAME AT STA 1080 ABOVE L36. REMOVAL EXCEEDED ALLOWABLE LIMITS. NDT VERIFIED MAT`L THICKNESS FROM 0.111- 0.154 REMOVED FRAME CAP AND 3 GUSSETS FROM L33R TO L35L REF SRM 51-1-21, 51-1-20D. FABRICATED AND INSTALLED REPAIR STRAP FROM 7075T7-.080 PER UPS RA NR DC8-53-20444, SAA SK798-748. RE-INSTALLED CAP AND GUSSETS REF SRM 51-1-21, 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050106001882005010600188WP 2005 1 6 UPS04843515 120041027A5313DWG5644130 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 LONGERON 15L CRACKED AT STA 1750. REMOVED CRACKED LONGERON SECTION FROM 1740-1760, 2 SHEAR TIES AT STA 1750 END FITTING AT STA 1760 REF SRM 51-1-21 AND 53-2-3. FABRICATED REPLACEMENT LONG SECTION FROM S1616757 EXT AND STRAPS FROM 7075T6-.080 PER SRM 53-2-3. INSTALLED ALL PARTS AND NEW SPLICE FITTING PER SRM 53-2-3, 51-1-20D, AND 51-1-8. 2L74 4F RT4A25 20050106001902005010600190WP 2005 1 6 UPS04843517 120041025A532047516252N FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 LONGERON 11R END FITTING CRACKED AT STA 680. REMOVED AND REPLACED CRACKED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 20050106001932005010600193WP 2005 1 6 UPS04843522 120041027A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 LONGERON 15R CRACKED AT STA 1750. REMOVED DAMAGED LONG SECTION FROM STA 1740-1766, SHEARTIE AT STA 1750, AND END FITTING AT STA 1766 PER SRM 53-2-2 FIG10, 51-1-20D, 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION FROM S1616757 EXT AND 2 STRAPS FROM SHT7075T6-.080 PER SRM 53-2-2 FIG10, REINSTALLED END FITTING, SHEAR TIE, AND REPAIR SPILCE REF SRM 51-1-20D. 2L74 4F RT4A25 20050106001942005010600194WP 2005 1 6 UPS04843523 120041030A5315DWG2772345 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 FLOORBEAM AT STA 55 RBL40 CORRODED BEYOND LIMITS. CUT OUT CORRODED AREA, NDT VERIFIED REF NDT SPM06-10-01.001 FABRICATED 2 FILLERS FROM 7075T6-.071. REPAIR ANGLE FROM AND 10136-2403, SPACER FROM 2024T3-.032. INSTALLED ALL REPAIR PARTS REF SRM 53-2-0 FIG1 F, 53-2-0 FIG 1B, 51-1-8. 2L74 4F RT4A25 20050106001962005010600196WP 2005 1 6 UPS04843526 120041025A53115642083 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 CORROSION ON FRAME AT STA -99 AT DOOR 90A NEAR L23L. REMOVED LIGHT CORROSION AT SITE. REMOVED .003 MAT FROM .088 THICK RIB, WITH IN LIMITS PER SRM53-2-0 FIG 1F, TREATED PER SRM 51-1-8. FOUND RIB CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER (7075T6-.080) AND REPAIR ANGLE (7075O-.100 H.T. TO T6) REF SAA SK798-255, DPS 7.00-1, SRM51-1-26, 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050106001972005010600197WP 2005 1 6 UPS04843527 120041027A53204750419U1 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 FITTING CRACKED ON FRAME AT STA 1180, LONG 19R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050106001992005010600199WP 2005 1 6 UPS04843529 120041117A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING L/E RIB CRACKED AT LOWER AFT END, STA860. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FAB REPAIR ANGLE FROM S25972423 EXTRUSION. INSTALLED REPAIR PER SRM 57-2-0, 51-1-8, 51-1-21D, 51-1-20D. 2L74 4F RT4A25 20050106002002005010600200WP 2005 1 6 UPS04843530 120041118A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 RT WING L/E RIB CRACKED AT XFS828.75. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 PER SRM 57-2-0 FIG 2. INSTALLED REPAIR PER SRM 57-2-0 FIG 2, 51-1-8, 57-3-1, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20050106002032005010600203WP 2005 1 6 UPS04843543 120041119A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 CRACKED RIB IN LT CENTER L/E NEAR STA XW322. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR FROM SHT7075T6, .040 AND .032 THICK, AND INSTALLED SAME REF SRM 51-1-8, 57-2-0, 57-3-1. 2L74 4F RT4A25 20050106002072005010600207NM 2005 1 6 ASA0440192 120041027A53306546881115 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CANNING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 EXTERNAL SKIN OIL CANNING/DENTED. REMOVED OIL CANNING/DENTED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050106002102005010600210NM 2005 1 6 ASA0440187 120041021A53106546551 SHEAR TIE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 PAE - CORROSION ON SHEAR TIE. REPAIRED SHEAR TIE. 2L72 4F4 FRTA16WE E21EU 20050106002112005010600211NM 2005 1 6 ASA0440189 120041021A532065458550103 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CORROSION ON MOP SILL. REPLACED MOP SILL. 2L72 4F4 FRTA16WE E21EU 20050106002122005010600212NM 2005 1 6 ASA0440178 120041007A575565464525 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU NR 4 SPOILER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02708AS 28895 OKC - FOUND HOLE IN THE NR 4 SPOILER 12 INCHES FORWARD OF THE T/E, 19 INCHES OB OF IB EDGE ON THE LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER. 2L72 4F4 FRTA16WE E21EU 20050106002132005010600213NM 2005 1 6 ASA0440180 120041011A523065C362311 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02708AS 28895 OKC - AFT CARGO DOOR HAS A DENT WITH A GOUGE. REMOVED DAMAGE IN SIX LOCATIONS, HFEC FOR CRACKS, NONE FOUND, INSURANCE CUT ALL CUTOUTS, FABRICATED AND INSTALLED REPAIR FILLERS. 2L72 4F4 FRTA16WE E21EU 20050106002142005010600214NM 2005 1 6 ASA0440183 120041016A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CORROSION AFT CARGO BAY ON FRAME SHEAR TIE. REPAIRED SHEAR TIE. 2L72 4F4 FRTA16WE E21EU 20050106002162005010600216NM 2005 1 6 ASA0440170 120041002A53156546810 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CORROSION ON FLOORBEAM AT PREVIOUS REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLE. 2L72 4F4 FRTA16WE E21EU 20050106002172005010600217NM 2005 1 6 ASA0440228 120041109A5311BAC15171470 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 CRACKED FRAME. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050106002192005010600219NM 2005 1 6 ASAA0410424 120041006A5310ABC14902738 SHEAR TIE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND 8 EACH, BACC HOLE IN SHEAR TIE. REMOVED AND REPLACED SHEAR TIE IAW SRM. 2L72 4F4 FRTA16WE E2EA 20050106002202005010600220NM 2005 1 6 ASA0440193 120041022A335020131A BATTERY PACK BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02794AS 28889 LT AFT OUTSIDE OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2L72 4F4 FRTA16WE E21EU 20050107000012005010700001NM 2005 1 7 WLDA2004102 120041103A5320 FITTING DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 DURING "C2" CHECK INSPECTION, FOUND CORROSION IN LONGERONS FITTING AT STA 1970 BETWEEN L52L, L51L AND L51R. 2L73 4F RTA22WE 20050107000022005010700002NM 2005 1 7 RYNA200500001 120041230A2612 MODULE BOEING757 757236 1384971NM FIRE DETECTION FOD A RYNAK NONE N FALSE WARNING DEDESCENT 1 CE07526NA 24794 LEFT ENGINE FIRE LOOP NR 2 STATUS MESSAGE ILLUMINATED ON DESCENT. CLEANED FOD FROM AFOLTS CARD FILE MODULE. OPERATIONAL CHECK NORMAL. 2L72 4F RTA2NM 20050107000032005010700003NM 2005 1 7 QXEA200400929 120041228A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09374PH24217576 528 SEA - UPON INSPECTION MAINTENANCE, FOUND FORWARD AIRSTAIR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107000042005010700004NM 2005 1 7 QXEA200400925 120041225A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - A GOUGE WAS FOUND ON THE RIGHT FUSELAGE AT APPROXIMATELY STATIONS X350 AND 2100.300 2 INCHES BEHIND THE ICE SHIELD. DAMAGED AREA WAS REPAIRED, AN HFEC WAS PERFORMED WITH NO CRACKS NOTED, AND A HI-LOC FASTENER WAS INSTALLED. THE AREA WAS PRIMED AND PAINTED. 2H72 4T RTA13NM 20050107000062005010700006EU 2005 1 7 MALA040905 120041124A3020NH24668169 DUCT SAAB SF340 340B 7860101EU LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15449XJ 340B449 DURING FLIGHT, LT INTAKE HEAT INOP. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED LT FWD INLET IAW 71-60-05-4, P/N ON/OFF NH24668-169, S/N OFF L198028,ON L291011. RAN A/C FOR 20MIN. RE-INSTALLED SHOEBOXES BACK TO ORIGINAL POSITIONS. OPS CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20050107000092005010700009NM 2005 1 7 2004UALA01172 120041119A2620 CYLINDER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EXTINGUISH SYS DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29318UA 23950 SQUIB FIRED A HOLE STRAIGHT THROUGH THE CYLINDER. FIRE EXTINGUISHER BOTTLE AND CARTRIDGE WERE SUBJECTED TO AN ABNORMALLY HIGH AMBIENT TEMP, NOT CONSISTENT WITH THE DESIGN PARAMETERS OF BOTH UNITS, AND THEY FUNCTIONED AS EXPECTED. THE ELEVATED AMBIENT TEMPERATURE WAS DUE TO A RUPTURED DUCT WHICH CAUSED THE SAFETY RELIEF DISCHARGE OF THE BOTTLE. THIS ALSO CAUSED THE CARTRIDGE TO AUTO-FIRE INTO AN ALREADY DISCHARGED BOTTLE. INFORMATION FROM THE OEM INDICATED THAT AN EMPTY BOTTLE HAD NO MEDIUM TO DAMPEN THE TRAVEL OF DEBRIS MATERIAL; HENCE THE DEBRIS "PROJECTILE" PIERCED THE BOTTLE WALL DIRECTLY OPPOSITE TO THE CARTRIDGE LOCATION. REPLACED DUCT AND BOTTLE ASSEMBLY. 2L72 4F4 FRTA16WE E2GL 20050107000102005010700010EU 2005 1 7 MALA040903 120041214A5320 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, LT FWD CABIN CLOSEOUT WEB AT FS 294 BETWEEN LBL 18.3 AND LBL 36 IS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED IAW SRM 51-40-21 REFER TO EAMS WO NR 211236/TASK 1515 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000132005010700013EU 2005 1 7 MALA040904 120041214A53477253721495 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, GALLEY SEAT TRACK PROFILE PN 7253721-495 IS CORRODED OUT OF LIMITS AT AFT OB END. PART HAS BEEN REPLACED IAW SRM 51-40-21. REFER TO EAMS WO NR 211236/TASK 1509 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000152005010700015EU 2005 1 7 MALA040902 120041214A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, GALLEY SEAT TRACK PN 7253721-459 IS CORRODED OUT OF LIMITS. TRACK HAS BEEN REPLACED IAW SRM 51-40-27. REFER TO EAMS WO NR 211236/TASK 1517 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000172005010700017EU 2005 1 7 MALA040899 120041214A5330 DOUBLER SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, GPU DOOR DOUBLER HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-23 AND SRM 51-40-21. REFER EAMS WORK ORDER NR 211236/TASK 1527 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000182005010700018EU 2005 1 7 MALA040901 120041214A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BLO, BETWEEN FS 294 AND 339 IS CORRODED. DAMAGED SEAT TRACK HAS BEEN REMOVED AND REPLACED AS REQUIRED BETWEEN FS 294 AND FS 329. REFER EAMS WORK ORDER NR 211236/TASK 1525 AND MESABA EO NR S53060 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000202005010700020NM 2005 1 7 QXEA200400931 120041228A2842 SWITCH DHAV DHC8 DHC8202 2809007NM RT FUEL TANK FAILED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09348PH17353 484 PDX - FLIGHT 9800 - THE NR 2 TANK FUEL LOW MASTER CAUTION ILLUMINATED. THE NR 1 AND 2 FUEL GAUGE INDICATES EQUAL. THE CHECKLIST WAS COMPLIED WITH. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 FUEL TANK LOW LEVEL SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107000232005010700023NM 2005 1 7 AWXA200401352 120041111A533065C35178 DOUBLER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3/8 INCH CRACK WAS FOUND IN TCAS EXTERNAL DOUBLER SKIN LOCATED BETWEEN BS 380 AND BS 390, STR 1 RT AND STR 2 RT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED AN HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED. FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5331-04328-RC1. 2L72 4F RTA16WE 20050107000242005010700024EU 2005 1 7 AWXA200401375 120041112A5347D53112815200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BEAM Y765 (SEAT TRACK), BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765, FROM FS 18 TO FS 20; FABRICATED A NEW REPLACEMENT SEAT TRACK AND 2 EACH REPAIR SPLICES; INSTALLED REPAIR PARTS IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050107000252005010700025EU 2005 1 7 AWXA200401346 120041116A5321D5367005700000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK, CABIN FLOOR PANEL 241EF WAS FOUND DELAMINATED BETWEEN FS 30 AND FS 42. MAINTENANCE PERFORMED BOND REPAIR ON FLOOR PANEL 241EF IAW A320 SRM 53-02-00, FIG 201 AND 202. 2L72 4F RTA28NM 20050107000262005010700026EU 2005 1 7 AWXA200401376 120041112A5320D5311209020300 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM -Y1292, BETWEEN FS 17 AND FS 19. MAINTENANCE REMOVED CORRODED SECTION OF FLOOR SUPPORT BEAM -Y1292, FROM FS 17 TO FS 19; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT AND 2 EACH REPAIR SPLICES; INSTALLED REPAIR PARTS IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050107000272005010700027EU 2005 1 7 AWXA200401377 120041111A5321D53672027000100 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK CORROSION WAS FOUND ON AFT SIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 152BF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 152BF, FROM -Y765 TO -Y1292, FS 46 TO FS 49; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR PANEL IAW A320 SRM 53-02-00. 2L72 4F RTA28NM 20050107000282005010700028NM 2005 1 7 AWXA200401343 120041128A33502100100 SWITCH BOEING757 7572S7 1384962NM CABIN FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28906AW 23568 JFK - EEL - DURING 8-DAY CHECK, THE L-4 AND R-4 DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT TEST SWITCH AT AFT FLIGHT ATTENDANT PANEL BS 1640 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050107000322005010700032EU 2005 1 7 AWXA200401355 120041112A5321D536104500000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK, CABIN FLOOR PANEL 232DF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 232DF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53610405; FLOOR PANEL REPLACED IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000362005010700036NM 2005 1 7 AWXA200401367 120041112A53306545772193 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 860 AND BS 908, STR 2 LT AND STR 2 RT. MAINTENANCE REMOVED DAMAGED FUSELAGE SKIN FROM BS 863 TO BS 907, STR 2 LT TO STR 2 RT; FABRICATED 3 EACH FILLERS, A DOUBLER, TRIPLER AND 4 EACH SPLICE STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5361-04326-SS2. 2L72 4F RTA16WE 20050107000372005010700037EU 2005 1 7 AWXA200401371 120041112A5320D53480048202 SCUFF PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE (SHAPE SILL) Y1800, BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SHAPE SILL AT Y1800 FROM FS 66 TO FS 68 AND FOUND LOWER SURFACE CORRODED AS WELL; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050107000392005010700039EU 2005 1 7 AWXA200401230 120041029A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, FOUND BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LEFT. MAINTENANCE REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRES AT SEAT ROWS 5, 7, 13, AND 24 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050107000402005010700040EU 2005 1 7 AWXA200401231 120041103A5321D5367202100600 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, CORROSION WAS FOUND ON AFT SIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 151AF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000412005010700041EU 2005 1 7 AWXA200401232 120041018A5320D53231322200 PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, CORROSION WAS FOUND IN 7 PLACES ON FORWARD CARGO COMPARTMENT DOOR SILL PLATE BETWEEN FS 25 AND FS 28. MAINTENANCE REMOVED CORRODED FORWARD CARGO COMPARTMENT DOOR SILL PLATE FROM FS 25 TO FS 28; FABRICATED A NEW REPLACEMENT PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050107000442005010700044NM 2005 1 7 AWXA200401381 120041129A52106545871554 DOOR FRAME BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-15 CHECK, A 1/8 INCH CRACK WAS FOUND IN R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM THE BOTTOM BS 328, STR 14 RT. MAINTENANCE BLENDED OUT CRACK, MATERIAL LOSS WITHIN LIMITS IAW B737-300 SRM 52-10-02, FIG 101. PERFORMED HFEC INSPECTION OF BLEND OUT TO ENSURE NO CRACKS EXIST, TREATED AREA. 2L72 4F RTA16WE 20050107000462005010700046NM 2005 1 7 AWXA200401103 120041005A3350900835A BATTERY BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 DURING INSPECTION MAINTENANCE, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY IN EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050107000482005010700048EU 2005 1 7 AWXA200401105 120040925A5321D5367202200000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151DF WAS FOUND DELAMINATED BETWEEN FS 49 AND FS 53. MAINTENANCE REMOVED FLOOR PANEL 151DF; CUTOUT DELAMINATED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000492005010700049EU 2005 1 7 AWXA200401106 120040925A5321D5367200500000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF WAS FOUND DELAMINATED AND CRACKED BETWEEN FS 28 AND FS 30. MAINTENANCE REMOVED FLOOR PANEL 131EF; CUTOUT DELAMINATED AND CRACKED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000512005010700051EU 2005 1 7 AWXA200401108 120040925A5321D5367202300000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151GF WAS FOUND DELAMINATED AT FS 53. MAINTENANCE REMOVED FLOOR PANEL 151GF; CUTOUT DELAMINATED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000532005010700053NM 2005 1 7 AWXA200401147 120041011A5743656717218 FITTING BOEING737 73733A 1384673NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON RT MAIN LANDING GEAR (MLG) BEAM INBOARD STABILIZING AFT FITTING AT WBL 71.24. MAINTENANCE REMOVED AND REPLACED RT MLG BEAM INBOARD STABILIZING AFT FITTING IAW AMM 57-15-00, FIG 401-402. 2L72 4F RTA16WE 20050107000552005010700055NM 2005 1 7 AWXA200401369 120041112A53306545772213 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 947 AND BS 1000, STR 2 RT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN FROM BS 947 TO BS 987, STR 2 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, TEAR STRAP DOUBLERS AND FILLERS, AND 2 EACH WEAR STRAP LEVELING SHIMS; INSTALLED REPAIR PARTS IAW ER 03-5361-04326-SS3. 2L72 4F RTA16WE 20050107000562005010700056NM 2005 1 7 AWXA200401370 120041112A53306545772213 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 908 AND BS 1002, STR 2 LT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN FROM BS 908 TO BS 987, STR 2 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, TEAR STRAP DOUBLERS, AND FILLERS; INSTALLED REPAIR PARTS IAW E.R. 03-5361-04326-SS4. 2L72 4F RTA16WE 20050107000572005010700057NM 2005 1 7 AWXA200401360 120041129A57536546430130 STRUCTURE BOEING737 7373G7 1384595NM RT FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK, THE LOWER RT INBOARD FORE FLAP WAS FOUND DISBONDED JUST OUTBOARD OF THE CENTER MID FLAP TRACK BETWEEN WBL 120.5 AND WBL 121.5. MAINTENANCE CUTOUT DAMAGE IN LOWER RT INBOARD FORE FLAP OUTBOARD OF CENTER MID FLAP TRACK; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20050107000582005010700058EU 2005 1 7 AWXA200401237 120041107A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28633AW 082 DURING 8-DAY CHECK, OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 11 LT. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050107000592005010700059CE 2005 1 7 66331 120041031A3240MS2874140226 HOSE BEECH 1900 1900D 1154162CE RT BRAKE DEFECTIVE A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07133YV UE133 UPON TAXI IN TO MSS, CREW EXPERIENCED WEAK BRAKING ACTION ON RT BRAKE, CONTIUED TO GATE W/ NO FURTHER INCIDENT. REMOVED AND REPLACED BRAKE HOSE AT BRAKE ASSY. OPS CK GOOD. 2L72 4T RTA24CE 20050107000602005010700060CE 2005 1 7 66764 120041114A3340 LIGHT BEECH 1900 1900D 1154162CE NLG LOOSE A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07126YV UE126 DURING TAXI, CREW NOTED TAXI LIGHT JUMPING BACK AND FORTH. RETURNED TO GATE AND NOTED TAXI LIGHT HAD COME LOOSE AT MOUNTING POINT. NO FURTHER INCIDENT. REMOVED AND REPLACED LIGHT ASSY BULB AND HARDWARE, P/N A715-1, 130909B124, 130909B45, 130909N32. 2L72 4T RTA24CE 20050107000612005010700061 2005 1 7 63601 420040803A3418360129 COMPUTER BEECH 1900 1900D 1154162CE STALL WARNING MALFUNCTIONED A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07162ZV UE162 DURING TAKEOFF ROLL OUT AT APPROX 80 KNOTS, THE STALL WARNING HORN STARTED SOUNDING. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LEFT COMPUTER AND GROUND CALIBRATION OF STALL WARNING SYSTEM, P/N 3601-29 S/N 312. 2L72 4T RTA24CE 20050107000642005010700064 2005 1 7 62639 420040629A2297 WIRE BEECH 1900 1900D 1154162CE AUTOPILOT SYS LOOSE A AMWAA UNSCHED LANDING O OTHER CLCLIMB 1 CE0710675 N10675 AFTER TAKEOFF, CAPTAIN NOTICED AUTO PILOT DISCONNECT CHIME RUN CONTINUOUSLY. RETURNED TO FIELD WITH NO FURTHER INCIDENT. RESECURED WIRE AT CANNON PLUG, OPS CHECK NORMAL. 2L72 4T RTA24CE 20050107000652005010700065CE 2005 1 7 66317 120041031A3243 MASTER CYLINDER BEECH 1900 1900D 1154162CE RT BRAKE CONTAMINATED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07133YV UE133 UPON TAXI IN, CREW EXPERIENCED WEAK BRAKING ACTION ON THE RT BRAKE, CONTINUED TO GATE WITH NO FURTHER INCIDENT. BLED MASTER CYLINDER. 2L72 4T RTA24CE 20050107000662005010700066CE 2005 1 7 66280 120041030A32421143880241 BRAKE BEECH 1900 1900D 1154162CE RIGHT WEAK A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07133YV UE133 CREW REPORTED F/O AND CAPT RIGHT BRAKES WEAK. REMOVED AND REPLACED BOTH RT BRAKES P/N 114-388024-1 (ON) S/N SEP92-1204 (ON). P/N 114-388024-1 (OFF) S/N AUG94-1598 (OFF). P/N 114-388024-1 (ON) S/N OCT90-978 (ON). P/N 114-388024-1 (OFF) S/N JUN90-793 (OFF) 2L72 4T RTA24CE 20050107000672005010700067CE 2005 1 7 66417 120041103A32439038000133 MASTER CYLINDER BEECH 1900 1900D 1154162CE RIGHT DEFECTIVE A AMWAO OTHER O OTHER UKUNKNOWN 1 CE07133YV UE133 ON PREFLIGHT, CREW FOUND RIGHT BRAKE SPONGING FIRST FLIGHT OF THE DAY. REMOVED AND REPLACED FO'S RIGHT HAND MASTER CYLINDER, P/N 90-380001-33 S/N 6675 P/N MS27039-1-21 S/N 2931 (OFF), P/N MS20392-2C23 P/N NA815-4D. 2L72 4T RTA24CE 20050107000682005010700068CE 2005 1 7 66391 120041102A2910 HYDRAULIC LINE BEECH 1900 1900D 1154162CE RT BRAKE LOOSE A AMWAO OTHER O OTHER UKUNKNOWN 1 CE07242YV UE242 RIGHT BRAKES ARE WEAK. TIGHTENED LINE ON THE HYDRAULIC LINE AFT ON LANDING GEAR AND BLED BRAKES. 2L72 4T RTA24CE 20050107000722005010700072CE 2005 1 7 64751 120040909A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE LT ENGINE MALFUNCTIONED A AMWAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TOTAKEOFF 1 CE0710675 UE10675 WHILE WAITING TO TAKEOFF, LT ENGINE GOT MASTER CAUTION AND A FIRE WARNING CREW FOLLOWED EMERGENCY CHECKLIST AND SHUTDOWN ENGINE AND FIRED EXTINGISHER PAX WERE DEPLANNED AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. REPLACED LOOP P/N 244-12886. 2L72 4T RTA24CE 20050107000732005010700073SO 2005 1 7 C2XA04SH566 120041120A532014530645401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EC5320-0117. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050107000742005010700074SO 2005 1 7 C2XA04SH568 120041203A532014530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED AT FRAME 38. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5320-01177. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050107000752005010700075SO 2005 1 7 C2XA04SH569 120041203A532014532636401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C CHECK, THE LEFT OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED AT FRAME 29. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050107000762005010700076SO 2005 1 7 C2XA04SH564 120041202A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 AND 23. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050107000772005010700077SO 2005 1 7 C2XA04TY168 120041019A532014521725613 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714977 145175 DURING C CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. REPLACED SILL IAW EMB SRM 51-40-02. 2L72 4T RTT00011AT 20050107000782005010700078SO 2005 1 7 C2XA04IA18 120041124A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716559 145603 IAH - FLIGHT 2018, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT ONE CEILING LIGHT AND THREE LOWER LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050107000812005010700081SO 2005 1 7 C2XA04RI015 120041113A3350110049 CHARGER EMB 145 EMB145XR 3260214SO CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2741104 145646 RIC - MX, DURING PRE FLIGHT CHECK, MAINTENANCE FOUND EXTERNAL LT FWD EMERGENCY LIGHT INOP. MAINTENANCE MELED AIRCRAFT. AIRCRAFT WAS RELEASED IAW MEL PROCEDURE 33-50-00/1 CAT "C" CONTROL NR 051445. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. IAH-MX, HOUSTON MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050107000822005010700082SO 2005 1 7 C2XA04IA150 120041125A33507281000501 CONTROL MODULE EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 IAH- FLIGHT 2463, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050107000832005010700083SO 2005 1 7 C2XA04IA151 120041124A335078241 INVERTER EMB 145 EMB145ER 3260211SO CABIN DISCONNECTED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714930 145011 IAH- FLIGHT 2729, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE LAST THREE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER SIX INVERTER TO BE DISCONNECTED. MAINTENANCE RECONNECTED THE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050107000842005010700084SO 2005 1 7 C2XA04IA145 120041120A3397375901 WIRE EMB 145 EMB145LR 3260212SO CABIN BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713975 145163 IAH - FLIGHT 2890, DURING THE PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050107000852005010700085SO 2005 1 7 C2XA04IA146 120041120A3350RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716911 145446 IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050107000872005010700087SO 2005 1 7 C2XA04TY178 120041205A575114569000613 SKIN EMB 145 EMB145ER 3260211SO LT AILERON DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714939 145030 DURING 4C INSPECTION, FOUND THE LEFT AILERON LEADING EDGE DENTED BEYOND LIMITS. REPAIRED IAW EC5750-01233. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050324000832005032400083NE 2005 3 24 2005UALA00243 220040314A7200 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29656UA 25394 FLIGHT ABORTED TAKEOFF DUE TO A COMPRESSOR STALL IN THE NR 1 ENGINE. ABORTED TAKEOFF AT 100 KIAS DUE TO COMPRESSOR SURGE. ENGINE REPLACED AT EZE. UA TURBINE SHOP FINDINGS: N2 WILL NOT ROTATE. ALSO, BORESCOPE INSPECTION REVEALED HEAVY HPC 5TH STAGE BLADE DAMAGE. ENGINE RETURNED TO LESSOR ON 06/06/05 WITHOUT BEING DISASSEMBLED. 2L72 4F4 FRTA1NM E24NE 20050328000612005032800061EU 2005 3 28 KBM2005F00018 120040211A6720704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR BINDING E KBMAK NONE O OTHER ININSP/MAINT 1 WP19884SH 2884 T/R CONTROL CABLE, CABLE IS BINDING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050328000742005032800074EU 2005 3 28 KBM2005F00025 120040222A6510350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM 2167 T/R HINGE LAMS CRACKED .6666 THE WAY AROUND ON SIDE OF FORK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050328000762005032800076EU 2005 3 28 KBM2005F00022 120040202A6710ASNA013735E2 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE CYCLIC CONTROL WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19215LA 2143 BEARINGS ARE WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050328000772005032800077CE 2005 3 28 FPI2005F00003 120041118A3240RA16402706 ROTOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO BRAKE SYSTEM CRACKED E FPIAK NONE O OTHER ININSP/MAINT 1 SO156BW 368 TH292 RADIAL CRACK FOUND. LOCATED INSIDE WEAR SURFACE OF ROTOR. THIS WAS REPLACEMENT PART (PN RA-164-02706). SUSPECT MFG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETETED. (RIGHT ROTOR) 1L72 3O3 O 3A16 E5CE 20050328000872005032800087EA 2005 3 28 R7S2005F00000 220041102A7322AN3153R NUT ROBSIN ROBSINR44 R44 7640120WP LYC O540 O540* 41532EA CONTROL TUBE WORN D R7SLK NONE O OTHER ININSP/MAINT 1 SW17748BP 0676 DURING A 100 HOUR INSPECTION, THE ROD END BEARING JAM NUT ON CONTROL TUBE (C336-1) AT THE CARBURETOR ATTACHMENT ARM WAS FOUND TO BE ONLY HAND TIGHT. THE ORIGINAL SAFETY WIRE INSTALLED BY THE FACTORY WAS STILL IN PLACE, BUT THE ROD END BEARING WAS ALLOWED TO MOVE WITHIN THE CONTROL TUBE. THIS MOVEMENT OVER TIME WORE DOWN THE THREADS ON THE ROD END BEARING AND OBLONG THE HOLE WITHIN THE CONTROL TUBE. ONCE THE JAM NUT WAS BACKED OFF A FEW THREADS (BY HAND) THE ROD END BEARING WAS ABLE TO MOVE CONSIDERABLY FROM SIDE TO SIDE WITHIN THE TUBE. 1G71 3O3 O H11NM E295 20050328000962005032800096SO 2005 3 28 LX52005F00000 220041209A8530 CYLINDER CESSNA182 182Q 2072732CE CONT O470 O470* 17026SO ENGINE CRACKED B LX5RO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 GL19831LL 18266533 ON NORMAL APPROACH TO THE AIRPORT A DISTINCT TICKING SOUND WAS OBSERVED FROM THE ENGINE AREA. THE PILOT REPORTED THAT THE ENGINE HAD GOOD OIL PRESSURE AND POWER AND CONTINUED TO MAKE A NORMAL LANDING AND SHUTDOWN WITHOUT INCIDENT. MAINTENANCE WAS CONTACTED. UPON ARRIVAL THE MECHANIC FOUND A SMALL HOLE IN THE AREA OR THE NR2 EXHAUST VALVE. A REPLACEMENT OVERHAULED CYLINDER WAS INSTALLED, AN EXTENSIVE GROUND RUN AND CHECK FLIGHT WERE PERFORMED. AFTER REMOVAL, VIEW FROM THE INSIDE OF THE CYLINDER, SEVERAL CRACKS WERE NOTED COMING FROM THE EXHAUST VALVE AND EXTENDING OUT TO BOTH SPARK PLUG HOLES. THE DAMAGED CYL WAS O/H. 1H71 3O3 ONT3A13 E273 20050328001012005032800101CE 2005 3 28 DFJ2005F00000 120041203A323008411065 BELLCRANK CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL LT MLG BROKEN E DFJAK NONE O OTHER ININSP/MAINT 1 CE034264J8957 310R0201 801106 BELLCRANK BROKE DURING GEAR RETRACTION. PROBABLE CAUSE IS DUE TO FATIGUE AND STRESS. SUGGEST REMOVAL OF BELLCRANK AFTER 5,000 HOURS OF OPERATION, DYE CHECK, REINSTALL AND RIG GEAR DOOR SYSTEM IAW SRM. (K) 1L72 3O3 O 3A10 E5CE 5 CP22EA 20050328001062005032800106CE 2005 3 28 FPI2005F00000 120041126A3240RA16402706 ROTOR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO BRAKE CRACKED E FPIAK NONE O OTHER ININSP/MAINT 1 SO15752P TH422 RADIAL CRACK FOUND ON WEAR SURFACE ON INSIDE OF ROTOR. THIS WAS A REPLACEMENT PART PN RA-164-02706. SUSPECT MFG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETECTED. RT ROTOR. TT370 HOURS. (K) 1L72 3O3 O 3A16 E5CE 20050328001132005032800113CE 2005 3 28 KCQ2005F00000 120041105A32331153800025 MOTOR BEECH 99 99 1154002CE PWA PT6 PT6A28 EA MLG BURNED E KCQABA EMER. DESCENT UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL13299CZ U74 PILOT REPORTED SMOKE IN COCKPIT DURING FLIGHT AND MADE EMERGENCY LANDING. FOUND GEAR MOTOR TO BE BURNED UP, HAVING CYCLED EXCESSIVELY. MATTER STILL UNDER INVESTIGATION, APPROX 3900 HOURS SINC REPAIR OF GEAR MOTOR. (GL13200503454) (K) 1L72 3T4 T A14CE E4EA 20040816000062004081600006NM 2004 8 16 04FDEA02402 120040809A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RIGHT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD ACTUATOR ROD END ATTACHING HOLE FLANGE CORRODED. 2L73 4F RTA22WE 20040816000072004081600007NM 2004 8 16 04FDEA02403 120040809A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.187 FINAL DIAMETER = 1.327 COMPLIED WITH FEDEX EA 1-5750-76810, WINGS - LT AND RT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20040816000082004081600008NM 2004 8 16 04FDEA02404 120040809A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 57-52-03. FOUND EXCEEDED LIMITS ORIGINAL THICKNESS = 0.562, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.560 COMPLIED WITH FEDEX EA 1-5750-76810, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS BORE CORRODED. 2L73 4F RTA22WE 20040816000122004081600012NM 2004 8 16 04FDEA02408 120040809A5320A5A7114523 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, RIGHT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 51 CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME III. 2L73 4F RTA22WE 20040816000142004081600014NM 2004 8 16 372PA0048 120040719A2781 SWITCH BOEING737 737306 13844BGNM FLAP INDICATOR OUT OF ADJUST A PIDAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO05372PA 23546 LEADING EDGE FLAPS TRANSIT LIGHT AND CONFIGURATION HORN ON DURING TAKEOFF, BELOW 80 KTS. REJECTED TAKEOFF. CHECKED FLAP INDICATION SYSTEM AND ADJUSTED NR 1 LEADING EDGE FLAP SWITCH. SYSTEM OPERATES NORMAL. 2L72 4F RTA16NE 20040816000222004081600022NM 2004 8 16 04FDEA02409 120040809A5320A5A7116517 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, RIGHT LONGERON SPLICE AT STA 5-113 TO 1541 LONGERON 47 CRACKED. REMOVED AND REPALCED PER SRM 51-33-01 VOLUME II 2L73 4F RTA22WE 20040816000302004081600030NM 2004 8 16 2004UALA00575 120040611A3350 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE SEAT 1E INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29771UA 26932 EMERGENCY LIGHT INOP AT SEAT 1E AFT LIGHT AND 11D AFT LIGHT. RELAMPED LIGHT. 2L72 4F4 FRTT0001SE E46NE 20040816000312004081600031NM 2004 8 16 2004UALA00576 120040611A2931VF6184C60AA0062 SWITCH AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE HYD SYS FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29809UA 825 FLIGHT DIVERTED DUE TO GREEN HYDRAULIC RESERVOIR LOW LEVEL WARNING ON ECAM. *S/D* GREEN HYDRAULIC PUMP SWITCH FAILED. REPLACED SWITCH, OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040816000332004081600033NM 2004 8 16 2004UALA00578 120040613A2613896373 SENSING ELEMENT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29368UA 24537 722174 DIVERTED TO DENVER WITH NR 1 ENGINE OVERHEAT LIGHT ON. LANDED ON AMBER ALERT WITH ENGINE SHUTDOWN. CREW REPORTED CRUISING AT FL350, NR 1 ENGINE OVERHEAT LIGHT FLICKERED TWICE AND THEN CAME ON STEADY. ACCOMPLISHED ENGINE OVERHEAT CHECK LIST, LIGHT STAYED ON. PERFORMED TROUBLESHOOTING OF NR 1 ENGINE OVERHEAT DETECTION SYSTEM. FOUND NR 1 ENGINE M1122 CORE LOOP-A BREAKING DOWN UNDER LOAD. REMOVED AND REPLACED CORE LOOP-A. ALSO REPLACED NR 1 ENGINE CORE LOOP-B FOR GETTING FAULT LIGHT WHEN TESTING OVERHEAT DETECTION SYSTEM. NR 1 ENGINE OVERHEAT SYSTEM CHECKED GOOD PER AMM. 2L72 4F4 FRTA16WE E2GL 20040816000352004081600035NM 2004 8 16 2004UALA00580 120040520A5754114W421011 WEDGE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 3 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29785UA 26954 LWR SURFACE OF TRAILING EDGE WEDGE DELAMINATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED TRAILING EDGE WEDGE. 2L72 4F4 FRTT0001SE E46NE 20040816000372004081600037NM 2004 8 16 2004UALA00582 120040613A5511657378338 RIB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZONTAL STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29391UA40343 24666 RT HORIZONTAL O/B LEADING EDGE SKIN IS DENTED AT THE 7TH RIB. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED INTERNAL DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20040816000432004081600043NM 2004 8 16 04FDEA02303 120040730A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT HORIZONTAL STABILIZER 27R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80300, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816000462004081600046NM 2004 8 16 04FDEA02307 120040730A5320 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD CARGO COMPARTMENT INTERCOSTAL AT STA 6-10 TO 6-30 LONGERON 43L FOUND CRACKED AT AFT EDGE AREA. REMOVED AND REPLACED WITH NEW INTERCOSTAL AS PER SRM 51-31-01, VOLUME II. 2L73 4F RTA22WE 20040816000482004081600048NM 2004 8 16 04FDEA02427 120040810A5320AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 INTERCOSTAL BETWEEN STA 1341 AND STA 1361 AT LONGERON 15R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040816000502004081600050NM 2004 8 16 04FDEA02429 120040810A5320AEA0222571 INTERCOSTAL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK INTERCOSTAL BETWEEN STA 1481 AND STA 1501 AT LONGERON 19R FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II PAGE 27. MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.096, ORIGINAL THICKNESS = 0.100 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1 FIGURE 3. 2L73 4F RTA22WE 20040816000552004081600055NM 2004 8 16 P5CA0401111 120040630A278169B415309 LOGIC CARD BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE LE FLAPS INOPERATIVE A P5CAD RETURN TO BLOCK PG NO WARNING INDICATION MULTIPLE FAILURE TXTAXI/GRND HDL 1 WP23920FT 22237 PILOTS LEADING EDGE FLAP LIGHTS INOPERATIVE. FLIGHT ENGINEERS LEADING EDGE FLAP INTRANSIT LIGHT INOP. REPLACED A-4 CARD IN LEADING EDGE LOGIC CONTROL BOX AS PER 27-31-00. 2L74 4F4 F A20WE E3NE 20040816000582004081600058EA 2004 8 16 COMA0460442 120040804A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA 7043 CRACK FOUND ON RIGHT WING PLANK, I/A/W CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20040816000722004081600072WP 2004 8 16 0401029882 120040526A5320 INTERCOSTAL DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01670MC 47659 DURING H-CHECK FOUND CRACK IN INTERCOSTAL AT BS 148 L10R. REPAIRED PER EA 98-199166. 2L72 4F RTA6WE 20040816000752004081600075NM 2004 8 16 AWXA200400876 120040730A53136545767 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 RT AT BS 500C+15. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 16 RT AT BS 500C+15, FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A STRINGER SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03-2 FIG 201. 2L72 4F RTA16WE 20040816000772004081600077NM 2004 8 16 AWXA200400878 120040727A531565498852 FLOORBEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 986, BETWEEN LBL 25 AND LBL 31, WL 208. MAINTENANCE REMOVED UPPER CHORD OF FLOORBEAM AT BS 294, FROM LBL 51 TO RBL 10; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-51 FIG 202. 2L72 4F RTA16WE 20040816000882004081600088NM 2004 8 16 SWAA042315 120040812A335065C34691 LIGHT BOEING737 7373Q8 1384670NM ROW 2 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 ABC, LOOSE. SECURED BULL NOSE EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20040816000892004081600089NM 2004 8 16 SWAA042316 120040812A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L AT BS 832, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040816000912004081600091NM 2004 8 16 SWAA042318 120040812A3350OL3071BPEGL LAMP BOEING737 7373G7 1384595NM ROW 21ABC INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C3 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 21 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040816000932004081600093NM 2004 8 16 2004UALA00583 120040614A5330 LAP JOINT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29391UA 24666 REPLACEMENT OF REPAIRS AT STA 887 STR 20R LAP JOINT AND AT STA 907 SKIN SPLICE DURING THE REPLACEMENT OF RIGHT AFT LOWER SKIN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND QUADRUPLER RUNNING FROM STA 874 TO STA 921, AND FROM STR 19R TO 21R. 2L72 4F4 FRTA16WE E2GL 20040816000942004081600094NM 2004 8 16 2004UALA00584 120040615A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ROW 15 CONTAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 EMERGENCY EXIT PATH LIGHTS ARE INOP FROM ROW 15 AFT. REMOVED COFFEE AND CLEANED EEL TRACKS. OPS CHECKED NORMAL. 2L72 4F4 FRTA16WE E2GL 20040816000982004081600098NM 2004 8 16 2004UALA00588 120040616A2440 CIRCUIT BREAKER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GROUND SERVICE TRIPPED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29306UA 23667 DIVERTED TO IAD DUE TO CIRCUIT BREAKER PROBLEMS. GROUND SERVICE CB P6-11 D8 POPPED 2 TIMES ON TAXI. CYCLED BATTERY CHARGER C-B'S AFTER 20 MINUTES. RESET GROUND C-B WITH NORMAL FAN SELECTED FOR 5 MINUTES AND ALT EXHAUST FOR 20 MINUTES, GROUND C-B HELD AND STAYED IN. SYSTEM WORKING. NO SPECIFIC PART FAILURE IDENTIFIED. 2L72 4F4 FRTA16WE E2GL 20040816001002004081600100EU 2004 8 16 2004UALA00590 120040617A5246D5744383000160 DOOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RT WING OPEN A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29419UA33260 487 DURING CLIMB CREW WAS UNABLE TO RETRACT FLAPS/SLATS. FUEL DOOR WAS FOUND OPEN AND BENT AROUND WING FIXED L/E PREVENTING SLAT FROM RETRACTING FULLY. FUEL DOOR REPLACED. LEADING EDGE REPAIRED. SLAT REPLACED. 2L72 4F4 FRTA28NM E40NE 20040816001062004081600106WP 2004 8 16 04FDEA01929 120040703A5522 SKIN DOUG DC10 DC1030 3023501WP ZONE 300 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND OUTBOARD ELEVATOR HAS NUMEROUS DENTS ON UPPER SURFACE. CHECKED DENTS HIGHEST READING 97887.111, DENT FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-80-01. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 55-10-00 VOL I AND 51-21-01 VOL 2. RECORDED NEW WEIGHT 836.87 ON WEIGHT DATA TAG, WITHIN LIMITS, (ELEVATOR DOES NOT REQUIRE REMOVAL) IAW DC10 SRM 55-20-00 VOL 2. REPLACED TAG IAW DC 10 SRM 55-20-00 VOL 2. 2L73 4F A22WE 20040816001072004081600107WP 2004 8 16 04FDEA01928 120040703A5753ARC2227 ANGLE DOUG DC10 DC1030 3023501WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 LEFT HAND OUTBOARD FLAP, OUTBOARD SUPPORT FITTING, FAIRING ATTACH STRUCTURE LOWER, INBOARD L-ANGLE BRACKET IS CRACKED. REMOVED L-ANGLE BRACKET IAW DC10 SRM 51-35-01 VOL 2, 51-33-01 VOL 2. FABRICATED ANGLE AND INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL 2 AND DAC DWG ARC 2227. 2L73 4F A22WE 20040816001162004081600116NM 2004 8 16 HNAA0400066 120040713A575385750350059 FITTING DHAV DHC8 DHC8102 2809003NM FLAP TRACK CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07906HA 9 OUTBOARD FLAP NR 3 FLAP TRACK ROLLER FITTING (AFT) IS BROKEN/CRACKED. UPPER ROLLER BROKEN OFF. REMOVED AND REPLACED FLAP TRACK ROLLER ASSEMBLY. 2H72 4T RTA13NM 20040816001192004081600119WP 2004 8 16 04FDEA01924 120040703A5751 SKIN DOUG DC10 DC1030 3023501WP AILERON DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND WING INBOARD AILERON - INBOARD EDGE OF LOWER SKIN SURFACE DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW DC10 SRM 57-00-01 VOLUME 1. INSTALLED REPAIR DOUBLER IAW DC10 SRM 51-35-01 VOLUME 2. 2L73 4F A22WE 20040816001232004081600123WP 2004 8 16 04FDEA02258 120040728A5753 HINGE DOUG DC10 DC1030 3023501WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) PIVOT HOLE NR 4 OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.062, FINAL DIAMTER= 1.075 AND REPAIRED AS PER FEDEX EA 1-5750-80281, TITLE: WINGS - RT OUTBOARD FLAP - INBOARD (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F A22WE 20040816001252004081600125NM 2004 8 16 04FDEA02194 120040727A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER 26L BARREL NUT BORE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040816001262004081600126NM 2004 8 16 04FDEA02195 120040727A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 14L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040816001292004081600129NM 2004 8 16 04FDEA02198 120040727A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) MIDDLE FITTING FOUND CRACKED. ASSEMBLY REMOVED AND REPLACED AS PER MM 27-50-30-4 AND FLAP STRUCTURAL ADJUSTMENT/TEST CARRIED OUT AS PER MM 27-50-30-5, FOUND SATISFACTORY AND FLAP ADJUSTMENT/TEST CARRIED OUT AS PER MM 27-50-00-5, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040816001352004081600135NM 2004 8 16 P5CA0401110 120040626A272060130005 ACTUATOR BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE RUDDER INOPERATIVE A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23920FT 22237 RUDDER RATIO LIGHT ON DURING TAXI OUT, LOWER RUDDER INDICATOR INOP. REPLACED LOWER RUDDER RATIO ACTUATOR AS PER AMM 27-21-12 PAGE 201. OPS CHECK OK. 2L74 4F4 F A20WE E3NE 20040816001402004081600140NM 2004 8 16 04FDEA02206 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79824, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001422004081600142NM 2004 8 16 04FDEA02208 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND HORIZONTAL STABILIZER NR 28L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80302, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 28L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001442004081600144NM 2004 8 16 04FDEA02210 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001482004081600148NM 2004 8 16 2004UALA00595 120040620A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 BS 365, RBL 10-RBL 72, FLOORBEAM CAP CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP WITH ANGLES AND SHIMS. 2L72 4F4 FRTA2NM E17NE 20040816001492004081600149 2004 8 16 2004UALA00596 420040620A2565 SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE 4R DOOR SLIDE DIRTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29524UA 24977 DOOR 4R SLIDE ARMED LIGHT INOP. ANOMALIE WAS CAUSED BY DIRT OR DEBRIS ON PROXIMITY SENSORS WHICH AFFECTED THE POSITION AND THEREFORE INDUCTANCE NECESSARY FOR SYSTEM OPERATION. CORRECTIVE ACTION CONSISTED OF CLEANING AND ADJUSTMENT OF THE GIRT BAR PROXIMITY SWITCHES/SENSORS. 2L72 4F4 FRTA2NM E17NE 20040816001502004081600150NM 2004 8 16 2004UALA00597 120040621A5753 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29644UA 25094 RIGHT INBOARD FLAP-CENTER EXTERNAL HINGE FITTING IS CRACKED ON INBOARD AND OUTBOARD FLANGES AT THE TOP. REPAIRED HINGE WITH REPAIR ANGLES AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20040816001512004081600151NE 2004 8 16 2004UALA00598 220040619A7250 TURBINE BLADES BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE LT ENGINE FAILED A UALAL ABORTED APPROACH RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 WP29670UA 29240 LEFT ENGINE COMPRESSOR STALL DURING APPROACH. ENGINE OPERATED NORMAL AT IDLE BUT CONTINUED TO COMPRESSOR STALL IF POWER GREATER THAN IDLE. NORMAL LANDING AFTER GO AROUND. ENGINE SURGED ON APPROACH. SURGE CHECKS FOUND METAL IN THE TAILPIPE AND ENGINE WAS REMOVED. DURING SHOP VISIT FOUND ONE 8TH STAGE BLADE BROKEN IN THE ROOT. ALSO FOUND 2 CRACKS IN THE 6TH STAGE DISK AND 1 CRACK IN THE 7TH STAGE DISK AT THE DOVETAIL SLOTS. THIS IS ASSOCIATED WITH THE FRONT END DURABILITY ISSUE BEING ADDRESSED BY THE OEM. 2L72 4F4 FRTA1NM E24NE 20040816001622004081600162NM 2004 8 16 2004UALA00603 120040622A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 AFT PIT FUSELAGE FRAME IS DENTED AT STA 1440 LT AT FLOOR TRANSITION PANEL. DAMAGE IS ON INBOARD FLANGE IN TWO PLACES. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816001652004081600165NM 2004 8 16 2004UALA00604 120040622A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 FRAME DENTED ON INBD FLANGE, BS 1400 STR 25L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED A NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816001672004081600167NM 2004 8 16 2004UALA00606 120040622A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 FRAME IS DENTED STA 1500, STR 25L ON INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20040816001732004081600173NM 2004 8 16 04FDEA02214 120040728A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING UPPER SKIN FORWARD OF NR 4 SPOILER OUTBOARD HINGE FOUND CORRODED. BLENDED OUT CORROSION IAW SRM 51-21-01, VOLUME II AND FOUND OUT OF LIMIT AS IAW SRM 57-10-00, FIGURE 32, VOLUME I. ORIGINAL THICKNESS=0.180, MATERIAL REMOVED=0.020 AND REMAINING MATERIAL=0.160 AT LT UPPER SKIN FORWARD OF NR 4 SPOILER OUTBOARD HINGE. REFER TO FEDEX EA NR 1-5720-80314, TITLE: WINGS - UPPER PLATING - LT AFT PLANK - XORS 738 CORROSION REPAIR. 2L73 4F RTA22WE 20040816001742004081600174NM 2004 8 16 04FDEA02215 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) HOLE NR 2 OUTBOARD SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS = 0.411, MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.406 AND REPAIRED AS PER FEDEX EA 1-5750-80287, TITLE: WINGS - LT OUTBOARD FLAP - INBOARD FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001752004081600175NM 2004 8 16 04FDEA02216 120040728A5343 BEAM DOUG MD11 MD11 3023602NM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT MAIN LANDING GEAR TRUCK BEAM FOUND HEAVY PITTING AND CORROSION. REMOVED AND REPLACED AS PER MM 32-12-20-4. OPERATIONAL CHECK OF RT MAIN LANDING GEAR CARRIED OUT DURING RETRACTION AS PER MM 32-31-00-5, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040816001762004081600176NM 2004 8 16 04FDEA02217 120040728A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE) HOLE NR 2 ACTUATOR OUTBOARD HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER= 1.062, FINAL DIAMTER= 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-80282, TITLE: WINGS - LT OUTBOARD FLAP - OUTBOARD (FLAP SIDE) HINGE BRACKET PIVOT AND ACTUATOR BORES - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040816001772004081600177 2004 8 16 234TR0019 420040726A2230 COMPUTER BOEING737 737228 13844AGNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05234TR 23004 NR 1 AUTO THROTTLE WILL NOT ARM. RESEATED AUTO THROTTLE COMPUTER AND PERFORMED BITE TEST. OPERATION NORMAL PER MM 22-31-01. 2L72 4F RTA16WE 20040816001792004081600179WP 2004 8 16 04FDEA02311 120040730A5753 ROLLER DOUG DC10 DC1030 3023501WP TE FLAP TRACK WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 RIGHT HAND INBOARD FLAP MID TRACK ROLLER WORN. REMOVED AND REPLACED MID TRACK ROLLER ON RIGHT HAND INBOARD TRACK. INSTALLED AND TORQUED IAW FEDEX EA 8-5750-80957 TW 8381H DUE 12-08-04. 2L73 4F A22WE 20040816001812004081600181NM 2004 8 16 2004UALA00611 120040624A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 FRAME DENTED ON INBD FLANGE STA 1480, STR 25L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20040816001822004081600182EU 2004 8 16 2004UALA00616 120040625A2934 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYD SYSTEM ILLUMINATED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29407UA 456 FLIGHT DIVERTED DUE TO HYDRAULIC (G RSVR LO LVL) ECAM MESSAGE. LOW LEVEL SWITCH FAILED. REPLACED THE LOW LEVEL SWITCH ON THE GREEN HYDRAULIC SYSTEM . OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040816001832004081600183EU 2004 8 16 2004UALA00617 120040626A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29419UA 487 AFT PIT STR 43L EXFOLIATED FROM FR 53 TO 59. SPLICED IN NEW STRINGER SECTION. 2L72 4F4 FRTA28NM E40NE 20040816001892004081600189WP 2004 8 16 04FDEA01864 120040625A5280NNB608621 CHANNEL DOUG MD10 MD1010F 3022112WP LT MLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 LEFT MLG DOOR AFT Z-CHANNEL APPEARS CRACKED. REMOVED AND REPLACED PAN IAW SRM 51-31-01 AT MAE. 2L73 4F RTA22WE 20040816001912004081600191NM 2004 8 16 04FDEA01868 120040628A5753ARC4125501 STOP FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. LEFT HAND WING - OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30 AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040816001922004081600192NM 2004 8 16 P5CA0401107 120040625A275118158511 TRANSMITTER BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FLAP INDICATOR INOPERATIVE A P5CAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 WP23920FT 22237 RIGHT INBOARD TRAILING EDGE FLAP WILL NOT EXTEND BEYOND 12 UNITS. LEADING EDGE BANK 1 & 2 FLAP INDICATION INOP ON BOTH PILOT & F/E PANEL. REMOVED & REPLACED RIGHT HAND INBOARD FLAP TRANSMITTER. RE-RACKED A4 & A8 LOGIC CARDS. OP CHECK OK ON BOTH, AS PER AMM 27-81-00. 2L74 4F4 F A20WE E3NE 20040816001942004081600194NM 2004 8 16 2004UALA00695 120040618A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29330UA 24191 DENT IN FUSELAGE JUST FWD AND ABOVE AFT LAV SERVICE PANEL. DENT MEASURES 6 INCH LONG X 5 INCH VERTICAL AT 0.250 INCH DEEP. FRAME HAS DISTORTION. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040816002002004081600200WP 2004 8 16 GTIA040667 120040624A5210 SKIN DOUG DC9 DC982 3022082WP R1 DOOR WORN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND R1 DOOR LOCK TO HAVE EXCESSIVE MATERIAL LOSS ON LOWER SKIN. (M) 2L72 4F A6WE 20040816002132004081600213SO 2004 8 16 SIMA200418402 120040701A335066903 LIGHT EMB 145 EMB145LR 3260212SO FWD CABIN INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21649PP 145234 ORF - FLT 4524 - AMBER FLOOR PROXIMITY LIGHT AT SERVICE DOOR FAILS TO ILLUMINATE. REPLACED SERVICE DOOR FLOOR EMERGENCY LIGHT STRIP ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040816002162004081600216SO 2004 8 16 SIMA200418401 120040629A1420 CONNECTOR EMB 145 EMB145LR 3260212SO NR 2 TE FLAP LOOSE A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21674RJ 14500801 FSM - FLT 3695 - FLAPS FAILED AT 9 DEGREES ON FINAL. FOUND NR 2 FLAP VELOCITY SENSOR CONNECTOR LOOSE AND TIGHTENED. PERFORMED OPERATIONAL CHECK OF FLAP ELECTRICAL/ELECTRONIC COMPONENT ADJUSTMENT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040818000032004081800003EU 2004 8 18 USAAEM04011 120040716A2750 DRIVE SYSTEM EMB ERJ170ERJ170100 EU TE FLAPS LOOSE A USAAO OTHER W INADEQUATE Q C APAPPROACH 1 EA19810MD 17000026 ON FINAL APPROACH THE CAPTAIN REPORTED THE FLAPS WOULD NOT DEPLOY. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT ANY FURTHER INCIDENTS. MAINTENANCE FOUND RIGHT OUTBOARD FLAP DRIVE LINE LOOSE AT OUTBOARD OF INBOARD JACKSCREW. RECONNECTED AND VERIFIED FLAP CONNECTION ON FLAP DRIVE. (M) 2L74 4F RTA56NM 20040818000082004081800008NM 2004 8 18 USAASB04087 120040705A1420FRF6E2822S08 CONNECTOR BOEING737 7374B7 1384702NM FIREWALL DAMAGED A USAAO OTHER H ELECT. POWER LOSS-50 PC APAPPROACH 1 EA19785AU 25024 CLT - FLT 495 - FLIGHT DEPARTED EWR, WITH THE NR 1 GENERATOR ON MEL 24-1. ON APPROACH TO CLT, CREW REPORTED THE NR 2 GENERATOR TRIPPED OFF LINE. CREW RESET THE GENERATOR, THEN HEARD A POP WHICH RESULTED IN THE LOSS OF THE NR 2 SYSTEM-A ELECTRICL HYDRAULIC PUMP, AUTO BRAKES, FUEL BOOST PUMPS, AUTO SPOILERS AND CAPTAINS RADIO'S. CREW NOTEICED THE NR 2 AND NR 3 TRANSFORMER/RECTIFIER CIRCUIT BREAKERS POPPED. UPON LANDING, ALL SYSTEMS CAME BACK ON BY THEMSELVES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 GENERATOR ENGINE FIREWALL CONNECTOR D410 AND HARNESS CONNECTOR PER BOEING STANDARD PRACTICES CHAPTER 20-60-06. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS PER MM 24-21-2L72 4F RTA16WE 20040818000122004081800012NM 2004 8 18 USAA040350 120040721A5312 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US50302 23935 PIT - FOUND AFT WEB PRESSURE BULKHEAD CORRODED .5 INCH BY .5 INCH AREA, BS 1016 ABOVE AND BETWEEN. (M) 2L72 4F RTA16WE 20040818000182004081800018NM 2004 8 18 USAASB04093 120040717A335020131A BATTERY BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19783AU 25022 BWI - THE AFT CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS NORMAL. (M) 2L72 4F RTA16WE 20040818000192004081800019NM 2004 8 18 USAA040349 120040721A5312 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 PIT - FOUND PRESSURE FRAME CORRODED .25 INCH BY 8 INCH AREA, AFT PRESSURE BULKHEAD BS 1016 BETWEEN STRINGER 27L AND 26R. (M) 2L72 4F RTA16WE 20040818000222004081800022NM 2004 8 18 USAA040339 120040707A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19573US51164 23560 CLT - FOUND SKIN CRACKED 1.5 INCHES LONG, STATION 727D PLUS 3 AT STRINGER 23 LEFT. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040818000372004081800037NE 2004 8 18 USAABB04061 220040629A7261 ENGINE BOEING767 767201 1385125NM GE CF6 CF680C2B2 30025NE RIGHT MAKING METAL A USAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 EA19650US 23902 PHL - FLT 71 - INBOARD TO PHL, THE CREW RECEIVED THE EICAS MESSAGE 'R ENGINE OIL FILTER.' THE MESSAGE REMAINED ILLUMINATED WHTN THE ENGINE THRUST WAS REDUCED. CREW SECURED THE ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH. OIL ANALYSIS FOUND ROLLER BEARING MATERIAL. THE RIGHT ENGINE WAS REPLACED. THE ENGINE TEARDOWN SHOWED THAT THE 4B BEARING WAS DAMAGED DUE TO DEBRIS INTRODUCED DURING THE PREVIOUS SHOP VISIT. (M) 2L72 4F4 FRTA1NM E13NE 20040818000382004081800038NM 2004 8 18 USAASB04084 120040701A3230405FW504B CIRCUIT CARD BOEING737 7373B7 1384580NM MLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19532AU 24479 CLT - FLT 194 - ON CLIMB-OUT FROM CLT, EN ROUTE TO ALB, CREW RECEIVED A RED NOSE GEAR LIGHT THAT WOULD NOT EXTINGUISH WHEN THE GEAR WAS RAISED. WHEN GEAR WAS LOWERED, ALL GEAR INDICATOINS WERE NORMAL. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM TO A FAULTY NOSE GEAR LOCK CIRCUIT CARD M1215. REMOVED AND REPLACED CIRCUIT CARD AND PERFORMED LANDING GEAR POSITION AND WARNING SYSTEM TEST PER MM 32-61-00. OPS TEST NORMAL. (M) 2L72 4F RTA16WE 20040818000402004081800040SO 2004 8 18 SIMA200417703 120040624A801135059105 STARTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE BROKEN A SIMAA UNSCHED LANDING FJSFLT CONT AFFECTED WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SW21623AE1061955 145109 CAE311287 FLT 3712 - CVG - DURING TAKEOFF, 500 FT AIR CREW REPORTED E1 FIRE INDICATION FOLLOWED BY FIRE WARNING BELL ABOUT 1.5 MINUTES LATER. FOUND NR 1 ENGINE AIR TURBINE STARTER BROKEN OFF THE MOUNTING PAD SEVERING FLUID LINES IN THE AREA WHICH CAUSED FIRE. NR 1 ENGINE WAS CHANGED DUE OT FIRE DAMAGE TO THE OUTER BYPASS DUCT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 FRTT00011ATTE6CH 20040818000412004081800041 2004 8 18 USAASA04065 420040604A2565 LANYARD AIRBUS320 A320214 3930316EU ESCAPE SLIDE MISROUTED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19124US 1314 DURING AN INSPECTION OF THE GIRT BAR ROUTING, THE FORWARD LT AND RT, AND THE REAR RIGHT, ESCAPE SLIDE SURVIVAL KIT LANYARDS WERE FOUND ROUTED INCORRECTLY. MAINTENANCE CORRECTLY ROUTED THE SURVIVAL KIT LANYARDS. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040818000432004081800043EU 2004 8 18 SIMA200419602 120040624A53117252813117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21344SB 340B344 ABI - DURING AN HMBV INSPECTION, CARGO AREA FRAME 677 WAS FOUND TO HAVE THREE SMALL DENTS. RECONTOURED THE THREE DENTS ON FRAME 677 AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED ANGLE REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007303, PARA 2 DATED JUNE 24, 2004. (M) 2L72 4T RTA52EU 20040818000482004081800048NM 2004 8 18 AMTA200400173 120040215A3030 HEATER BOEING737 73783N 13844HINM PITOT HEAD MALFUNCTIONED A AMTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL11314TZ 209085 30640 RIGHT ELEVATOR PITOT HEAT LIGHT CAME ON ON RECALL BEFORE TAXI CHECK. REMOVED AND REPLACED RIGHT ELEVATOR PITOT PROBE PER MM 27-31-94-4. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040818000532004081800053EU 2004 8 18 SIMA200419615 120040704A53117252814117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21386AE 340B386 ABI - DURING AN MBV INSPECTION, THE UNDER FLOOR CARGO FRAME AT FS 658.5 FOUND DENTED. PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS007323 PARA 1 DATED JUNE 29, 2004. (M) 2L72 4T RTA52EU 20040818000602004081800060EU 2004 8 18 SIMA200418601 120040702A3297AIR130902 WIRE HARNESS SAAB SF340 340B 7860101EU RT MLG DAMAGED A SIMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW21374AE 340B374 DURING APPROACH INTO DFW RIGHT MAIN GEAR DOWN AND LOCK LIGHT DID NOT COME ON. APPROACH WAS ABORTED AND CREW COMPLIED WITH AOM PROCEDURES. RECYCLED GEAR AND DOWN AND LOCKED LIGHT CAME ON. CONTINUED INTO DFW WITH NO OTHER PROBLEMS. REMOVED AND REPLACED HARNESS. (M) 2L72 4T RTA52EU 20040818000632004081800063EU 2004 8 18 SIMA200419611 120040708A53477253799381 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21394AE 340B394 DURING AN MBV INSPECTION, FOUND PREVIOUS REPAIR ON SET TRACK BL 18.3L BETWEEN STATION 297 AND 329 FOUND TO BE CORRODED BEYOND SRM LIMITS. CUT OUT A 31.9375 SECTION OF EXISTING SEAT TRACK. PREPARED A NEW SECTION FOR REPAIR. INSTALLED NEW SEAT TRACK AND U-BEAM P/N 7253799-379. REPAIR DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTER 53-70-60 FIGURES 201, 202, 204. (M) 2L72 4T RTA52EU 20040818000672004081800067SO 2004 8 18 SIMA200419704 120040630A532014522460015 SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE 145328 SAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR FORWARD STRUCTURE CENTER SUPPORT AT FRAME 17 CORRODED. REMOVED AND REPLACED CABIN INTERIOR FORWARD STRUCTURE SUPPORT TEE FRAME 17 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818000682004081800068SO 2004 8 18 SIMA200420102 120040718A276014533022405 CONTROL UNIT EMB 145 EMB145LR 3260212SO SPOILERS INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21635AE 145158 CREW NOTED AFTER ROTATION SPOILER OPEN INDICATION ACCOMPANIED WITH EICAS MESSAGE SPOILER FAIL AND TAKEOFF CONFIGURATION WARNING. REPLACED SPOILER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040818000692004081800069GL 2004 8 18 SIMA200419401 220040708A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FAILED A SIMAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW21674RJ 14500801 CAE312576 ON CLIMB-OUT CREW REPORTED A LOUD BANG. ENGINE NR 2 ROLL BACK AND UNCOMMANDED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW EMB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T4 FRTT00011ATTE6CH 20040818000782004081800078SO 2004 8 18 SIMA200419403 120040709A3350110049 POWER SUPPLY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21837AE 145647 FOUND FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 POWER SUPPLY. OPS CHECK GOOD. AIRCAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818000812004081800081WP 2004 8 18 GTIA040642 120040611A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FOUND FUSELAGE SKIN CRACKED AROUND L1 HOLD OPEN LATCH AND REQUIRES TO BE REPAIRED. TRIMMED CRACK. FABRICATED OUTSIDE DOUBLER, INSIDE DOUBLERS. INSTALLED REPAIR. (M) 2L72 4F RTA6WE 20040818000832004081800083NM 2004 8 18 AMTA200400333 120040321A3610 CLAMP BOEING757 75733N 1384931NM BLEED AIR DUCT LOOSE A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11557TZ 32591 LT ENGINE OVERHEAT EICAS MESSAGE AT FL420, OVERHEAT INDICATION REMAINED WITH THROTTLE CLOSED, BAV CLOSED FOR APPROX 2 MINUTES EXTINGUISHED AND DID NOT REOCCUR AT ANY POWER SETTING. TROUBLESHOT PER FIM 26-11-00 FIG 103. FOUND CLAMPS LOOSE ON IP AND HP BLEED DUCTS AND VALVE 11/2 TURNS. HP SENSE LINE AT HP DUCT AND HI STAGE PILOT LOOSE. NOTING GREY FLASH AT ALL POINTS OF TIGHTENING. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040818000842004081800084EU 2004 8 18 A6WA200460009 120040318A5210 HOOK BAC 146 146200A 1500266EU PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31179US E2041 DAMAGE TO DOOR HOLD OPEN HOOK AREA ON THE DOOR, AND ASSOCIATED RECEPTICLE ON THE FUSELAGE, FORWARD PASSENGER DOOR. MAINTENANCE REPLACED UPPER HINGE AND HOLD OPEN LATCH HOUSING. REPAIRED DAMAGE TO THE FORWARD PASSENGER DOOR IAW BAE FAX REF NR BARA/AVR/6690/04DC. (M) 2H74 4F A49EU 20040818000932004081800093NM 2004 8 18 AMTA200400180 120040218A2120 ODOR BOEING737 73783N 13844HINM GALLEY DETECTED A AMTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11321TZ 28249 HOT PLASTIC ODOR IN AFT GALLEY AREA. ODOR SUBSIDED AND DIDN'T RETURN AFTER GALLEY POWER AND OVENS TURNED OFF, ALTHOUGH FLIGHT ATTENDANTS COULDN'T ISOLATE ODOR TO OVENS. NO SMOKE OR FIRE. OPS CHECKED AFT GALLEY OVENS COULD NOT DUPLICATE PROBLEM. NOTIFIED OPS AND CATERERS TO REPLACE OVEN TRAYS. (M) 2L72 4F RTA16WE 20040818000942004081800094NM 2004 8 18 TSAA0477018 120040109A7711 CIRCUIT BREAKER BOEING737 73725A 1384481NM EPR INDICATOR TRIPPED A TSAAC ABORTED TAKEOFF PG NO WARNING INDICATION MULTIPLE FAILURE TOTAKEOFF 1 WP13819AL 23791 FLT 280 - HNL-KOA - ABORTED TAKEOFF DUE TO BOTH EPR GAUGES INOPERATIVE. C/B'S RESET, NO FLAGS. RAN BOTH NR 1 AND NR 2 ENGINE AFTER EPR C/B RESET. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20040818000952004081800095NM 2004 8 18 AMTA200400161 120040212A5320 PANEL BOEING737 73783N 13844HINM CARGO BAY CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23304TZ 30675 FOUND C2 CARGO PANEL CORROSION AT STATION 767 TO 727J. FOUND CORROSION OUT OF LIMITS PER SRM 53-00-53-1. FABRICATED NEW PANEL PER SRM 53-60-53-01 AND INSTALLED PANEL. (M) 2L72 4F RTA16WE 20040818000962004081800096SO 2004 8 18 SIMA200419405 120040709A33502013BR POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21638AE 145172 ORD - FLT 4065 - FOUND EMERGENCY EXIT LIGHTS ON BOTH WALLS NEAR OVERWING EMERGENCY EXITS ARE INOPERATIVE. REPLACED EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040818000982004081800098SO 2004 8 18 SIMA200419702 120040630A532014522460013 GUSSET EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE 145328 SAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR CENTER SUPPORT BEAM AT FRAME 19 CORRODED. REMOVED AND REPLACED GUSSETT IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818001032004081800103 2004 8 18 GTIA040637 420040704A2565 LATCH DOUG DC9 DC983 3022083WP L1 DOOR SLIDE STICKING A GTIAK NONE O OTHER ININSP/MAINT 1 GL23815NK 49415 RSW - F/A'S COMPLAINED THAT L1 SLIDE PACK GIRT BAR HARD TO ARM AND UNARM. FOUND ARMING LATCH STICKING, CLEANED AND LUBED LATCH ASSEMBLY. OPS CHECKS GOOD. (M) 2L72 4F RTA6WE 20040818001042004081800104WP 2004 8 18 GTIA040638 120040705A3150H05A00354 COMPUTER DOUG DC9 DC983 3022083WP AURAL WARNING MALFUNCTIONED A GTIAK NONE N FALSE WARNING ININSP/MAINT 1 GL23825NK 53012 STABILIZER, AUTO BRAKES, FLAPS, SLATS ANNUNCIATION IN FLIGHT UNABLE TO SILENCE. REMOVED AND REPLACED CENTRAL AURAL WARNING COMPUTER SYSTEMS, OPS CHECK GOOD. PERFORMED TAKEOFF WEARING TEST AND OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20040818001072004081800107EA 2004 8 18 ASOA04476 120040701A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11885AS 7521 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040818001112004081800111WP 2004 8 18 GTIA040651 120040622A5321 FLOOR PANEL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND MAIN CABIN RIGHT INBOARD FLOOR PANEL STATION 1250-1309 HAVE CRACKS, DAMAGE ON EDGES/SEVERAL INSERTS HAVE PULLED THROUGH. FABRICATED NEW FLOOR PANEL. (M) 2L72 4F A6WE 20040818001152004081800115SW 2004 8 18 HEEA096022 120040512A3110212075962001 POWER SUPPLY BELL 412 412 1182202SW PWA PT6 PT6* 52043EA INSTRU LIGHT BURNED A HEEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0321498 36003 DURING FLIGHT THERE WAS A BURNING ODOR IN COCKPIT AND CIRCUIT BREAKER POPPED. MAINTENANCE FOUND THE INSTRUMENT LIGHTS POWER SUPPLY HAD BURNED. REPLACED BURNED INSTRUMENT LIGHTS POWER SUPPLY. 1G72 4U3 T H4SW E2NE 20040818001172004081800117EU 2004 8 18 ALGA096029 120040708A1430C622A2006601 BOLT UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIUS2B1 NE FUSELAGE CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1G72 3U3 UNCR0001RD E34NE 20040818001242004081800124SW 2004 8 18 ALGA096466 120040612A6230412010407105 RING BELL 412 412 1182202SW SWASHPLATE CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XASBZ5694 RE333 33213 FOUND OUTER RING CRACKED. REPLACED WITH SERVICEABLE PART. 1G72 4U H4SW 20040818001262004081800126SW 2004 8 18 HEEA096491 120040625A5630205032669277 WINDOW BELL 412 412 1182202SW PWA PT6 PT6* 52043EA SLIDING DOOR SEPARATED E HEEAA UNSCHED LANDING D INFLIGHT SEPARATION APAPPROACH 1 SW03108X 33115 DURING APPROACH TO LAND, A PASSENGER LEANED AGAINST THE WINDOW ON THE RT SIDE SLIDING DOOR AND THE WINDOW RELEASED AND WAS LOST. AIRCRAFT LANDED WITH NO FURTHER OR OTHER DAMAGE AND NO INJURIES. 1G72 4U3 T H4SW E2NE 20040818001312004081800131EU 2004 8 18 ALGA096030 120040708A1430C622A2006601 BOLT UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001322004081800132EU 2004 8 18 ALGA096031 120040708A1430C622A2006601 BOLT UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED D ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001372004081800137 2004 8 18 KBM2004F00129 420040526A2312A21815869808 SWITCH SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TRANSMITTER STICKS E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P1208 2347 TRIGGER SWITCH STICKS ON TRANSMITTER. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001442004081800144EU 2004 8 18 RAIA00408003 120040804A2897 WIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE FUEL TEMP DAMAGED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03566HK 41084 LOW FUEL TEMP WARNING INDICATION. AIRCRAFT FERRIED TO STL. MAINTENANCE REPAIRED WIRE AT LOW TEMP SWITCH. 2L72 4T4 TRTA41NM E18NE 20040818001512004081800151EA 2004 8 18 MW22004F00001 220040616A8530 STUD PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA NR 3 CYLINDER FAILED B MW2RO OTHER O OTHER NRNOT REPORTED 1 GL174818T 186 347250152 L226351A NR 3 CLYINDER DECK STUDS FAILED AND CYLINDER LT ENGINE. CONNECTING ROD AND PISTON ALSO NOT FOUND. 1L72 3O3 O A7SO 1E10 20040818001602004081800160SO 2004 8 18 SWIA200413690 120040808A3397 WIRE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EMERGENCY LIGHT DAMAGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07584SW 120352 EMERGENCY EXIT ROW LIGHTING IN ROW 6 INTERMITTENT, BOTH SIDES. REPAIRED WIRING BEHIND (EXIT) SIGN AT ROW 6A. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040818001652004081800165NM 2004 8 18 WLDA200454 120040802A5512ALC8101504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 10.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 10 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001662004081800166SO 2004 8 18 C2XA04SH470 120040728A531514530627001 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716976 145171 DURING C-CHECK THE LT FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01283. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040818001672004081800167SO 2004 8 18 C2XA04SH480 120040810A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716919 145393 SHV-DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED OUT OF LIMITS IAW SRM 53-21-10. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040818001762004081800176EU 2004 8 18 KBM2004F00124 120040209A7931704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE OIL PRESSURE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 OIL PRESSURE READS ZERO. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. 1G71 3U3 UNCH9EU E19EU 20040818001982004081800198EU 2004 8 18 KBM2004F00153 120040524A6510350A33215300 SPHERICAL BEARIN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/R SPHERICAL BRSEPARATED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 T/R SPHERICAL BEARINGS HAVE SEPARATION BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040818001992004081800199NM 2004 8 18 750WL0008 120040812A335020131A BATTERY PACK BOEING757 757200 1384950NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY LIGHTS AT 2LT ARE INOPERATIVE. REPLACED BATTERY PACK IAW MM. OPS CHECKS OK. 2L72 4F4 FRTA2NM A12EU 20040819000022004081900002EA 2004 8 19 04224629 120040811A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX STUCK A VTZAO OTHER O OTHER TXTAXI/GRND HDL 1 EA27629BR 7251 PAX DOOR WILL NOT OPEN. MX NO DEFECTS WERE NOTED. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040819000052004081900005CE 2004 8 19 DELA20040001 120040701A2435400SG138Q STARTER GEN LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE ENGINE ODOR E DELAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE03188TG5 5 078 DURING NORMAL START SEQUENCE, THE NR 2 ENGINE DID NOT ROTATE. CREW REPORTED BURNED ELECTRICAL ODOR FROM NR 2 NACELLE AFTER DEPLANING. NR 2 STARTER/GENERATOR REPLACED WITH OVERHAULED UNIT AND START ACCOMPLISHED WITHOUT FAULT. 2L72 4F4 FRTA10CE E35NE 20040819000082004081900008NE 2004 8 19 C8GA20040016 220040807A7261 ENGINE BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE ZONE 400 LEAKING A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15715AA594211253 22470 685546 DURING CLIMB, NR 1 ENGINE LOST 1.5 GALLONS OF OIL IN THE FIRST 10 MINUTES. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT FURTHER INCIDENT. FOUND EXCESSIVE AMOUNT OF OIL LEAKING FROM THE NR 4.5 TO NR 6 BEARING DRAIN. REPLACED THE NR 1 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040819000102004081900010WP 2004 8 19 MWEA040141 120040812A5321 FLOORBOARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE GALLEY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD GALLEY SERVICE DOOR FLOORBOARD CORRODED ALL OVER. FABRICATED AND INSTALLED SHIM. 2L72 4F4 F A6WE E9NE 20040819000122004081900012WP 2004 8 19 MWEA040144 120040812A53209961689501 PAN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD WATER SERVICE PAN LIP CORRODED AT FRAME STA 155. FABRICATED AND INSTALLED SUPPORT. 2L72 4F4 F A6WE E9NE 20040819000132004081900013WP 2004 8 19 MWEA040146 120040812A53209936534 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD AND AFT PLUGS FOR THE FLOOR SUPPORT BETWEEN STA 148-200 RT OF FUSELAGE CENTER LINE ARE CORRODED. FABRICATED AND INSTALLED PLUGS. 2L72 4F4 F A6WE E9NE 20040819000152004081900015NM 2004 8 19 WLDA200456 120040802A5512ALC8101504 PANEL DOUG MD11 MD11 3023602NM PWA JT8 JT8D217C 52053NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 5. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 5 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E9NE 20040819000222004081900022CE 2004 8 19 BAQ2004F00002 120040617A21507608061 HEAT EXCHANGER LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE7313A 01518WP CABIN COOLING CLOGGED B BAQRO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 11895 92 THE COOLING FINS WERE COMPLETELY OBSTRUCTED WITH OIL, DUST, FILM. YOU CAN NOT GAIN ACCESS OF THE COMPONENT, SHORT OF REMOVING IT FROM THE SYSTEM. 2L72 4F4 F A10CE E6WE 20040819000262004081900026NM 2004 8 19 WLDA200484 120040802A5754ARB1688502 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT NR 3 SLAT PUNCTURED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, WHILE PERFORMING J/C NR WA5740 FOUND A PUNCH HOLE ON RT WING LEADING EDGE SLAT NR 3 AT STA XOS435. PERFORMED REPAIR OF RT WING LEADING EDGE SLAT NR 3 IAW EGAT EI NR W2004A53B. CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000282004081900028NM 2004 8 19 F3LA200400078 120040812A2700 MODULE AIRBUSA319 A319111 3930336NM GE CFM56 CFM565A 13802NE MALFUNCTIONED A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03921FR 2010 AIR TURN BACK. FLIGHT CREW REPORTED ELAC2 PITCH FAULT AFTER TAKEOFF. SWAPPED ELAC2 ELECTRONIC MODULE OF THE PITCH FROM ACTUATOR WITH ELAC1/SEC1 ELECTRONIC MODULE IAW MM 27-44-57-000-002 AND MM 27-44-57-400-002. PERFORMED SYSTEM TEST OF THE THS ACTUATOR ELEC. CONTROL FOR BOTH ELAC2 AND ELAC1/SEC1 ELEC. MODULES IAW MM 27-41-00-730-001. OPS CHECK GOOD. ALSO PERFORMED TASK 27-96-00-710-002. OPS CHECK GOOD. 2L72 4F4 FRTA28NM E29NE 20040819000302004081900030NM 2004 8 19 0401325803 120040812A2910271N64441168 LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE HYDRAULIC SYS CRACKED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01583NW 32983 IN CRUISE AT FL 37,000 FT RECEIVED R HYD SYS PRESS AND R HYD SYS QTY MESSAGES. QUANTITY SHOWED ZERO IN RT SYSTEM. DECISION WAS MADE TO DIVERT TO DTW. LANDING UNEVENTFUL, MAINTENANCE FOUND THE RETURN LINE FROM THE RT (ALTERNATING CURRENT MOTOR PUMP (ACMP) CRACKED AT B-NUT. VERIFIED SYSTEM WAS EMPTY AND INSTALLED TEMPORARY FLEX LINE (P/N 00255030499). AFTER SERVICING SYSTEM FOUND RT ACMP WITH CAVITATIONS AT 1230 PSI. REMOVED AND REPLACED AC HYDRAULIC PUMP 55-2911-9-0013 S/N OFF 56289 AND ENGINE DRIVEN PUMP 55-2911-9-0016 S/N OFF 58288. 2L72 4F4 FRTA2NM E17NE 20040819000372004081900037EU 2004 8 19 RAIA00408007 120040805A7997 WIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE OIL PRESS TRANDUBROKEN A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03570HK 41089 LT ENGINE OIL PRESSURE FLUCTUATES. MAINTENANCE REPAIRED BROKEN WIRE AT OIL PRESSURE TRANSDUCER. 2L72 4T4 TRTA41NM E18NE 20040819000382004081900038EU 2004 8 19 RAIA00408009 120040809A3244AHA1837 TIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE MLG BLOWN A RAIAO OTHER O OTHER LDLANDING 1 CE03574HK 41093 NR 3 TIRE BLOWN ON LANDING. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 TIRE/WHEEL ASSEMBLY. 2L72 4T4 TRTA41NM E18NE 20040819000432004081900043EU 2004 8 19 UPS04142899 120040810A3242 BRAKE AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE MAIN BRAKE SYS FIRE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 DURING BLOCK IN NR 4 BRAKE WAS SEEN TO BE ON FIRE. SMALL AREA OFF BRAKE ONLY. WHEEL ASSY AND GEAR AREA NOT AFFECTED. REMOVED AND REPLACED NR 4 BRAKE UNIT IAW MM 32-42-27-4. 2L72 4F4 FRTA35EU E24NE 20040819000442004081900044NM 2004 8 19 UPS04242900 120040813A3350 SWITCH BOEING727 72731C 1384011NM RROYCETAY TAY65154 EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01926UP 19233 EMERGENCY EXIT LIGHTS INOPERATIVE, COCKPIT DOOR. TURNED BATTERY SWITCH ON PLACED EMERGENCY LIGHT SWITCH TO ARMED, LIGHT CHECKS GOOD. 2L73 4F4 F A3WE E25NE 20040819000452004081900045NM 2004 8 19 UPS04442897 120040812A3350 BATTERY PACK BOEING747 747212B 1384886NM PWA JT9 JT9D7Q 52054NE EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01526UP 21937 EMERGENCY LIGHT INOPERATIVE UPPER DECK R-1 DOOR REPLACE BATTERY PACK IAW MM 33-51-00. 2L74 4F4 F A20WE E3NE 20040819000462004081900046NM 2004 8 19 WLDA200466 120040802A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 31.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 31 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000502004081900050WP 2004 8 19 2004F00236 120040814A2780ARH1669 FUSE LINK DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE SLATS SHEARED B K NONE O OTHER ININSP/MAINT 1 SO25322FE 47908 RT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546. 2L73 4F4 FRTA22WE E23EA 20040819000522004081900052EA 2004 8 19 04225677 120040812A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DEFECTIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27677BR 7652 PAX DOOR CABLE KEEPS GETTING STUCK WHILE OPENING AND CLOSING DOOR. UPON INSPECTION FOUND PAX DOOR POWER ASSIST CABLE OFF PULLEY. ROUTED CABLE ONTO PULLEY. PAX DOOR POWER ASSIST FUNCTION OPERATES NORMAL IAW AMM 52-11-08. 2L72 4F4 FRTA21EA E15NE 20040816000092004081600009NM 2004 8 16 04FDEA02405 120040809A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03. CORROSION REMOVED AND FOUND EXCEEDED LIMITS PER CMM 57-52-03 2L73 4F RTA22WE 20040816000202004081600020NM 2004 8 16 2004UALA00571 120040612A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 FUSELAGE FRAME AT STA 600 BETWEEN STR 24L AND 25L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR PARTS. 2L72 4F4 FRTA2NM E17NE 20040816000262004081600026NM 2004 8 16 04FDEA02414 120040809A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 52 SPLICE BETWEEN STA 1701 AND STA 1721. CORROSION REMOVED PER SRM 53-00-01 FIGURE 3 VOLUME 1. MATERIAL THICKNESS= 0.125, MATERIAL REMOVED= 0.020, MATERIAL REMAINING= 0.105. WITHIN LIMITS PER SRM 53-00-01 FIGURE 3 VOLUME I 2L73 4F RTA22WE 20040816000392004081600039EA 2004 8 16 COMA0460444 120040802A531160034017595 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01716CA15122 7250 DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW COMAIR EA 10-5310-00389 AND REO 601R-53-11-136. 2L72 4F RTA21EA 20040816000412004081600041NM 2004 8 16 04FDEA02301 120040730A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT NR 15 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79834, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 15R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816000422004081600042NM 2004 8 16 04FDEA02302 120040730A5510 BARREL NUT DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT NR 17 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79835, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 17R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816000472004081600047NM 2004 8 16 04FDEA02426 120040810A5320AEA0142510 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48470 INTERCOSTAL BETWEEN STA 1175 AND STA 1199 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED AS PER 51-33-01 VOLUME II. 2L73 4F RTA22WE 20040816000592004081600059EA 2004 8 16 COMA0460443 120040804A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA 7043 CRACK FOUND ON LEFT WING PLANK, IAW CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20040816000602004081600060NM 2004 8 16 04FDEA02218 120040728A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 FORWARD CARGO COMPARTMENT AT STA 1119 TO 6-10 LONGERON 51R FOUND CRACKED AT SPLICE JOINT AREA. REPAIRED AS PER SRM 53-10-00 FIG 2 VOL I. NDT INSPECTION CARRIED OUT, FOUND NO CRACK EVIDENT. 2L73 4F RTA22WE 20040816000692004081600069NM 2004 8 16 04FDEA02310 120040730A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 MAIN DECK CARGO COMPARTMENT AT STATION 695 AXIS X = -47.58 SEAT TRACK LOWER SURFACE FOUND CRACKED. DAMAGED SEAT TRACK AT MAIN DECK STA 695 AXIS X = -47.58 REMOVED AS PER SRM 51-31-01 VOL 2. REPAIR TRACK FABRICATED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20040816000742004081600074NM 2004 8 16 AWXA200400875 120040730A53136545767 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 500C+5. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 LT AT BS 500C+5, FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A STRINGER SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03-2 FIG 201. 2L72 4F RTA16WE 20040816000832004081600083EU 2004 8 16 AWXA200400861 120040805A5320D53112600200 STRUCTURE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF DUMMY RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040816001022004081600102NE 2004 8 16 2004UALA00592 220040618A7230 COMPRESSOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 ENGINE BIRD INGESTION A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29195UA 26899 ABORTED TAKEOFF AT 108 KTS DUE TO NR 2 ENG COMP STALL AT 100 KTS. DETERMINED STALL DUE TO A BIRD STRIKE. 2L74 4F4 FRTA20WE E24NE 20040816001052004081600105WP 2004 8 16 04FDEA01930 120040703A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 FLOORBEAM CRACKED UNDER CENTER ROLLER TRAY AT ATTACH POINT STATION 840 LBL 2. FABRICATED AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 53-00-01 VOL I, 53-00-01 VOL I, AND 51-21-01 VOL 2. 2L73 4F A22WE 20040816001102004081600110NM 2004 8 16 04FDEA02434 120040811A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 CABIN SEAT TRACK AT STA 1855 LBL 8 FOUND CORRODED. DAMAGED SEAT TRACK REMOVED AT STA 1831 TO 1858 AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. REPAIR TRACK & SPLICE FABRICATED, REWORKED & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-35-01 VOL II. 2L73 4F RTA22WE 20040816001152004081600115WP 2004 8 16 04FDEA01932 120040703A5310 SHEAR TIE DOUG DC10 DC1030 3023501WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 CORROSION AND FLAKING PAINT AND PRIMER AT STATION 1821, LONGERON 51L-51R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 58-00-01 VOL I. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC10 SRM 53-30-00 VOL I, 51-21-01 VOL 2 AND 53-30-00 VOL I. 2L73 4F A22WE 20040816001172004081600117NM 2004 8 16 HNAA0400064 120040707A532085320686101 THRESHOLD DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07933HA 134 AIRSTAIR DOOR THRESHOLD IS CORRODED. REMOVED AND REPLACED THRESHOLD. 2H72 4T RTA13NM 20040816001332004081600133NM 2004 8 16 04FDEA02202 120040728A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LEFT HAND NR 6 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79827, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 6L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040816001342004081600134NM 2004 8 16 P5CA0401108 120040625A75002155M39G01 MANIFOLD BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 4 ENGINE RUPTURED A P5CAO OTHER J WARNING INDICATION TOTAKEOFF 1 WP23534MC 21832 517577 NR 4 ENGINE 14TH STAGE MANIFOLD RUPTURE AT LEFT HAND SIDE CDP AIR SWIVEL JOINT. REPLACED 14TH STAGE MANIFOLD & CLAMP AS PER AMM 75-23-00. OPS CHECK & LEAK CHECK ACCOMPLISH AS PER AMM 71-00-00. 2L74 4F4 F A20WE E23EA 20040816001362004081600136NM 2004 8 16 2004UALA00600 120040621A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29391UA 24666 STA 663 FRAME HAS 4 CRACKS, 2 EACH AT THE STR 3 RT LIGHTENING HOLE, AND 1 EACH AT THE STR 1 AND 2 RT LIGHTENING HOLE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND REMOVED STRINGER SPLICES FOR ACCESS, INSTALLED REPAIR ANGLE DOUBLER AND STRINGER SPLICES. 2L72 4F4 FRTA16WE E2GL 20040816001642004081600164NM 2004 8 16 2004UALA00694 120040718A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29367UA 24536 ON SKIN DAMAGE AT STA 360, A DENT IN STRINGER 20R SKIN FLANGE. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED. REPLACED STRINGER SPLICE FITTING. 2L72 4F4 FRTA16WE E2GL 20040816001662004081600166NM 2004 8 16 2004UALA00605 120040622A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 FRAME AT STA 1540 ABOVE STR 25L IS DENTED, INBD FLANGE. *S/D* MAJOR REPAIR ACCOMPLISHED. NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816002062004081600206 2004 8 16 GTIA040673 420040718A2565 GIRT BAR DOUG DC9 DC983 3022083WP L1 DOOR CONTAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 LGA - FLT 1865 - FOUND L1 GIRT BAR, RIGHT SIDE, WILL NOT STAY IN POSITION. REMOVED CHEWING GUM FROM GIRT BAR RECEPTACLE AND LUBED. (M) 2L72 4F RTA6WE 20040816002082004081600208WP 2004 8 16 GTIA040670 120040715A5711 FRAME DOUG DC9 DC982 3022082WP RT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 DTW - FOUND 2 RIGHT WING LEADING EDGE FORMERS AT APPROX STATION 351 CRACKED. (M) 2L72 4F A6WE 20040816002182004081600218SO 2004 8 16 SIMA200419402 120040707A27503635001001 BRAKE EMB 145 EMB145LR 3260212SO LT FLAP XMSN FAILED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21669MB 145788 IAH - FLT 3837 - FLAP FAIL MESSAGE ON EICAS. FLAPS SELECTED TO 9 DEGREES, NO MOVEMENT. ALSO, FLAPS WILL NOT MOVE ON GROUND. REPLACED LEFT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040816002242004081600224EU 2004 8 16 SIMA200418805 120040610A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21396AE 340B396 ABI - AIRCRAFT ARRIVED FOR MBV INSPECTION AND REPAIR ON HAIL DAMAGE. DENT ON TOP SKIN FS 439.5 SL 1603 WAS FOUND BEYOND SRM LIMITS. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007205 PARA 1 DATED, JUN 7, 2004. (M) 2L72 4T RTA52EU 20040818000022004081800002NM 2004 8 18 UIEA200400130 120040728A575365B084105 HOUSING BOEING747 7472D7B 1384803NM TE FLAPS CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 DUIRNG SCHEDULED MAINTENANCE, FOUND CORROSION DAMAGE AT THE MAIN BEARING HOUSING BORE OF THE LEFT WING INBOARD TRAILING EDGE MID-FLAP CARRIAGE BEARING HOUSINGS ASSEMBY. REAMED BORE TO 6.100 INCHES DIAMETER AND REMOVED LOCAL SURFACE DAMAGE FROM AFFECTED AREA OF HOUSING. SMOOTH BLENDED AND REFINISHED HOUSING TO DESIGN CONDITION. DYE PENETRANT INSPECTED TO ENSURE MACHINED BORE IS DAMAGE AND CRACK FREE. VISUAL AND HFEC INSPECTED SATELLITE HOLES TO ENSURE HOLES ARE ROUND AND CRACK FREE. REFINISHED AND INSTALLED OVERSIZE REPAIR SLEEVE PER THE REQUIREMENTS OF OHM 57-52-35. SHOT PEENED MAIN BORE AND RESTORE FINISH. (M) 2L74 4F RTA20WE 20040818000172004081800017NM 2004 8 18 USAA040345 120040715A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19447US37956 24874 CLT - FOUND SKIN CRACKED .8 INCH, EXTERIOR FUSELAGE SKIN BELOW S23L AT STATION 727D. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20040818000232004081800023NM 2004 8 18 USAA040340 120040708A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19355US44758 23558 PIT - FOUND FRAME CRACKED .125 INCH, STATION 480, S8L-S9L. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20040818000282004081800028EU 2004 8 18 A6WA200460031 120040511A5320HC536H0555000 INTERCOSTAL BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31607AW E2052 FOUND INTERCOSTAL CRACKED BETWEEN FRAMES 21/22 AT STRINGER 21 RT IN FORWARD CARGO BAY. MAINTENANCE REPLACED INTERCOSTAL IAW SRM 51-23-00, 51-42-00, AND 51-43-00. (M) 2H74 4F A49EU 20040818000292004081800029EA 2004 8 18 A6WA200440093 120040617A5260 AIRSTAIR CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 PASSENGER DOOR STAIR STRUCTURE AFT ANGLE IS CRACKED .80 INCH LONG IN AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. CUT AWAY DAMAGED SECTION OF DRAG ANGLE, FABRICATED REPLACEMENT DRAG ANGLE FROM 5773 EXTRUSION AND SPLICE ANGLES FROM $6144-14 ANGLE. INSTALLED ANGLES IAW BRAS EO 601R-52-5101A AND CRJ SRM 51-23-00. (M) 2L72 4F RTA21EA 20040818000502004081800050EU 2004 8 18 SIMA200419607 120040704A55127255150521 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21386AE 340B386 ABI - DURING MBV INSPECTION AND REPAIR OF HAIL DAMAGE. THE LEFT HORIZONTAL STABILIZER TOP SKIN PANEL HAIL DAMAGE WAS BEYOND SRM LIMITS. REMOVED EXISTING TOP SKIN. PREPARED NEW SKIN AND INSTALLED SKIN. WORK DONE IAW SAAB 340 SRM, SRM 72LKS 3079 REV 43, CHAPTERS 51-40-21, 22-23, 24, 51-20-50 AND 51-20-56. (M) 2L72 4T RTA52EU 20040818000552004081800055EU 2004 8 18 USAASA04070 120040704A2120 ODOR AIRBUSA319 A319112 3930323EU CABIN DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19715UW 1051 A STRONG ODOR WAS NOTED BY CREW AT CRUISE AND DESCENT. THE ODOR WAS NOTED TO BE STRONGER IN AFT GALLEY. FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED LEFT AND RIGHT ENGINES FOR OIL LEAKS AND OIL RESIDUE IN PLUMBING. NONE WAS FOUND. REMOVED, INSPECTED AND EPLACED RECIRCULATION FILTERS. INSPECTED THE APU FOR EXTERNAL LEAKAGE AND OIL RESIDUE IN PLUMBING. NOTED SOME ODOR WITH THE APU BLEED SYSTEM. PLACED THE APU BLEED AIR ON MEL. INSPECTED APU DUCT. PRV DUCT, FORWARD PACK DUCTS, AND BOTH RECIRCULATION FILTER REPLACEMETS AND FOUND NO CONTAMINATION. OPERATED THE APU WITH AIR CONDITIONING PACKS ON FOR FOUR HOURS ON GROUND. NO LEAKS OR OIL ODOR NOTED. REMOVED THE MEL. 2L72 4F RTA28NM 20040818000582004081800058EU 2004 8 18 SIMA200418605 120040704A52207252200041 SEAL SAAB SF340 340B 7860101EU EMERGENCY EXIT TORN A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21305AE 340B305 LAX - FLT 3101 - DURNG TAKEOFF, CREW DID AN AIR TURN BACK, DUE TO AN EXIT BEING OPEN. RIGHT FORWARD EMERGENCY DOOR LATCH POPPED OPEN ON TAKEOFF ROLL. REPLACED DOOR SEAL AND PERFORMED ADJUSTMENT OF DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040818000622004081800062EU 2004 8 18 SIMA200419610 120040704A53117252814117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21386AE 340B386 ABI - DURING AN MBV INSPECTION, THE CARGO FRAME AT FS 649 WAS FOUND DENTED. PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 REPAIR STATEMENT 340SDS007323, PARA 1 DATED JUNE 29, 2004. (M) 2L72 4T RTA52EU 20040818000722004081800072NM 2004 8 18 GTIA040656 120040709A2910 B-NUT DOUG MD80 MD83 3023681NM HYD SYSTEM LEAKING A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23822NK 49392 FLT 1153 - VERTY STRONG ODOR OF OIL OR SKYDROL THROUGHOUT THE CABIN AND COCKPIT DURING CRUISE. FOUND HYDRAULIC FLUID LEAKING FROM LINE IN AFT PIT LEFT WALL. FLUID DRAINED ON BOTTOM OF FUSELAGE AND WENT INTO APU INLET AND FUMES FROM FLUID WENT INTO RECIRC FAN IN AFT PIT. TIGHTENED B-NUT ON LINE. LEAK CHECK GOOD. THIS CLEARED ODOR IN CABIN. NO FURTHER DEFECTS NOTED. (M) 2L72 4F RT 20040818000882004081800088EA 2004 8 18 ASOA04502 120040704A329717300253 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG DAMAGED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11847AS 7335 DURING CLIMB-OUT FROM ATL-MKE, THE CREW RECEIVED A GEAR DISAGREE MESSAGE AND COMPLIED WITH THE QRH. THE AIRCRAFT RETURNED WITH EMERGENCY VEHICLES BEING REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG BRACE ELECTRICAL HARNESS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040818000992004081800099EU 2004 8 18 SIMA200419609 120040704A53117252814117 FRAME SAAB SF340 340B 7860101EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01386AE 340B386 DURING AN MBV INSPECTION, THE CARGO FRAME AT STATION 640 WAS FOUND DENTED. PERFORMED A CUT OUT OF THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR ANGLE. REPAIR DONE IAW SAAB 340 STATEMENT 340SDS007323, PARA 1 DATED JNE 29, 2004. (M0 2L72 4T RTA52EU 20040818001062004081800106EA 2004 8 18 ASOA04477 120040701A5730 PANEL CNDAIRCL600 CL6002B19 1900309EA LEFT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE LEFT WING LOWER AFT PANEL AT WS 148.019 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT WING LOWER AFT PANEL AT WS 148.019 IAW ASA EO 600-57-0134. (M) 2L72 4F RTA21EA 20040818001092004081800109EU 2004 8 18 ASOA04472 120040630A33503011160 LIGHT AEROSPATR72 ATR72212 8680945EU GALLEY BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 DURING AN A-CHECK IN MCN, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. (M) 2H72 4T RTA53EU 20040818001192004081800119SW 2004 8 18 ALGA096402 120040720A6210206015001119 BLADE BELL 206 206L3 1182108SW ALLSN 250C 250C30 03013GL MAIN ROTOR SEPARATED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03361AL2320 51212 FOUND CORROSION AND SEPARATION AT SKIN/SPAR INTERFACE NEAR LOWER OB GRIP FINGER DOUBLER. REMOVED AND REPLACED DEFECTIVE BLADE WITH NEW BLADE. SCRAPPED DEFECTIVE BLADE. 1G71 3U3 U H2SW E1GL 20040818001332004081800133EU 2004 8 18 ALGA096032 120040708A1430C622A2006601 BOLT UROCOPEC120 EC120B 8680987EU MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03513AL859 1261 BOLT PITTED. REPLACED BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001362004081800136WP 2004 8 18 DHL2004801008 120040812A2121 BLOWER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE E/E BAY FAILED A DHLAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01801DH 46033 RADIO RACK OVERHEAT LIGHT ILLUMINATED IN FLIGHT ABNORMAL PROCEDURE PERFORMED HOT ELECTRICAL ODOR NOTICEABLE IN COCKPIT RADIO RACK OVERHEAT LIGHT EXTINGUISHED AND ODOR WENT AWAY AFTER VENTURI VALVE OPENED. DEFERRED RADIO RACK BLOWER IWA MEL 21-27 PLACARD INSTALLED DMI 17499. 2L74 4F4 FRT4A25 E2GL 20040818001482004081800148SW 2004 8 18 KBM2004F00134 120040206A5302206031004115B STRUCTURE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TAIL BOOM CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 TAILBOOM FOUND CRACK AT AFT LT TAIL ROTOR GEAR BOX MOUNT HOLE. REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20040818001702004081800170SW 2004 8 18 KBM2004F00170 120040601A2910206076390001 LINE BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL HYD PRESS LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 HYDRAULIC LINE CHAFED AND LEAKING. REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20040818001792004081800179NM 2004 8 18 P5CA0401133 120040803A36103206254 PRESSURE VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 3 ENGINE INOPERATIVE A P5CAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23508MC 21644 530349 DURING ENGINE START NR 3 ENGINE ROTATION WAS SLOW, LIGHT OFF NORMAL BUT WOULD NOT ACCELERATE PAST 30 PERCENT. REPLACED NR 3 ENGINE PRESSURE RELIEF VALVE, OPERATIONAL CHECK GOOD IAW MM 36-11-00. 2L74 4F4 F A20WE E23EA 20040818001852004081800185EU 2004 8 18 KBM2004F00159 120040622A7712305731366 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TORQUE DEFECTIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 TORQUE GAUGE UNRELIABLE. REMOVED DEFECTIVE UNIT AND INSTALLED REPAIRED UNIT. 1G71 3U3 UNCH9EU E19EU 20040819000162004081900016EU 2004 8 19 KBM2004F00162 120040516A624039951213 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE M/R TACH FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2258 2300 GAUGE FLUCTUATES. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040819000232004081900023CE 2004 8 19 E812004F00008 120040722A29101285801011 LINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE HYD SYSTEM CHAFED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL0375RL 990 RK312 WHILE INSPECTING FORWARD FUSELAGE BRAKE HYDRAULIC LINE TUBING DURING COMPLIANCE WITH RECOMMENDED SB, FOUND TUBING DAMAGED EXTERNALLY BY FLOOR PANEL 151BTC AND FLOOR PANEL 151DTC ATTACHMENT SCREWS. REPAIRED TUBING ASSY BY SPLICING IN REPAIR TUBE WITH PERM SWAG FITTINGS IAW SB. RECOMMEND THAT TECHNICIANS INSPECT THIS ARE AND REPAIR AS REQUIRED DURING NEXT SCHEDULED INSPECTION. POSSIBILITY EXISTS THAT LOSS OF BRAKES MAY EVENTUALLY OCCUR IF DAMAGED AREA NOT NOTED OR ADDRESSED DUE TO SB COMPLIANCE BE RECOMMENDED ONLY. 2H72 4F4 FRTA16SW E25EA 20040819000312004081900031EU 2004 8 19 RAIA00408004 120040805A7603 SWITCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE CONDITION LEVER OUT OF ADJUST A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03567HK 41085 CONFIG WARNING ON TAKEOFF ROLL. MAINTENANCE ADJUSTED CONDITION LEVER SWITCH. 2L72 4T4 TRTA41NM E18NE 20040819000472004081900047WP 2004 8 19 ASMF200408011 120040812A213339271411 REGULATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE LT SIDE OPEN W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23505MD339963431 49149 CAPTAIN REPORTED THAT AT FL 330 FLOWS LIGHT TURNED ON DUE TO PRESSURIZATION FAILURE PERFORMING AN ABNORMAL AND EMERGENCY PROCEDURE. ANTI-ICE WAS APPLIED TO ENGINES AND WINGS BUT LIGHT CONTINUE AND CABIN ALTITUDE LIGHT TURNED ON, PRESSURIZATION WAS CONTROLLED AT FL 200, BUT CABIN GOT 13000 FT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING CHECK WAS DETECTED A LOOSEN LINE FROM THE RADIATOR TO THE LT CLEANING VALVE. ADDITIONALLY, PRESSURE REGULATOR VALVE WAS REPLACED IAW MM 21-31-01, TESTS WERE PERFORMED IAW MM 36-10-00 AND 21-32-00, ALL CORRECT. 2L72 4F4 F A6WE E9NE 20040819000482004081900048WP 2004 8 19 ASMF200408012 120040812A2781 SENSOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE TE FLAPS STUCK W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23216AM 49586 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING SLAT DISAGREE LIGHT TURNED ON WITH FLAPS UP. DURING CHECK TECHNICAL PERSONNEL DETECTED RT WING D SENSOR GOT STUCK. IT WAS CLEANED AND LUBRICATED AND SLAT/FLAP INDICATIONS RETURNED TO NORMAL, TEST WERE PERFORMED IAW MM 27-81-00. 2L72 4F4 FRTA6WE E9NE 20040819000512004081900051NM 2004 8 19 DHL2004783012 120040813A3242 BRAKE BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE RT MLG MALFUNCTIONED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01783DH 21999 RIGHT BRAKE GRABS WHEN APPLIED DURING TAXI. 2L73 4F4 F A3WE E2EA 20040819000532004081900053CE 2004 8 19 GLBA20030693 120040811A5210 STRUCTURE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE PAX DOOR HANDLE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03245GL UE245 CABIN DOOR HAS CORROSION AROUND HANDLE, REPAIRED IAW EO. 2L72 4T4 TRTA24CE E26NE 20040819000542004081900054EU 2004 8 19 AWXA200400908 120040805A5320D5348004320500 SILL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR SILL AT UPPER IB END BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGED AREAS OF R-2 DOOR SILL AT UPPER IB END, BOTH AT FR 68; FABRICATED A REPAIR DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201. 2L72 4F4 FRTA28NM E311NE 20040819000552004081900055CE 2004 8 19 GLBA20030697 120040811A5330 SKIN BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FUSLAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03122UX UE122 LOWER COMM ANTENNA SKIN CRACKED, REPAIRED SKIN. 2L72 4T4 TRTA24CE E26NE 20040819000572004081900057NM 2004 8 19 UPS04M42916 120040610A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C RT HORT STAB NR 20 BARREL NUT HOLE FOUND CORRODED REWORKED BARREL NUT HOLE NR 20 RT, REAMED TO 1.067 INCH IAW EO MD11-5510-1940 9-G. S/W SURFACE CORROSION BLENDED OUT FOUND EXCEEDED LIMIT 0.025 INCH DEEP REPAIR BUSHING SLEEVE FAB IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1 422B2 AT BARREL NUT HOLE NR 20 RT IAW EN:1206-04. REPAIR C/OUT IAW EN:120 6-04 AND EO MD11-5510-14904-G AT BARREL NUT HOLE NR 20 RT WITHIN LIMIT. 2L73 4F RTA22WE 20040819000592004081900059NM 2004 8 19 UPS04M42918 120040529A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, HORT STAB NR 15 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND S/W SURFACE POSN AT RT. REPAIR AT NR 15 RT BARREL NUT HOLE, MACHINE DOWN 0.050 INCH DEEP. BLENDED OUT TO 0.100 INCH DEEP FOUND OUT LIMIT. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. PR1422 B2 SEALANT APPLIED IAW EN:1181-04. REPAIR SLEEVE BUSHING INSTALLED IAW EO MD11-5510-19409-G AND EN:1181-04 AT BARREL NUT HOLE NR 15 RT WITHIN LIMIT, SATIS. 2L73 4F RTA22WE 20040819000602004081900060SO 2004 8 19 C2XA04SD007 120040812A3350 COVER EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT CRACKED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718120 145681 MOST FORWARD EMERGENCY LIGHT STRIP COVER CRACKED. REMOVED AND REPLACED MOST FORWARD EMERGENCY LIGHT STRIP COVER IAW 145XR AMM 33-50-12 2L72 4F4 FRT TE6CH 20040819000612004081900061SO 2004 8 19 C2XA04CL079 120040812A3320BR900022 BALLAST EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LAVATORY SHORTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2716541 145542 CLE FLIGHT NR 2131 CREW REPORTED AN ELECTRICAL ODOR IN CABIN DURING POST FLIGHT INSPECTION. MAINTENANCE INSPECTED AND FOUND THAT THE LAV LIGHT BALLAST HAD SHORTED OUT. MAINTENANCE REPLACED THE LAV LIGHT BALLAST. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040819000622004081900062SO 2004 8 19 C2XA04CL080 120040812A3397 WIRE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 CLE FLIGHT NR 2153, CREW REPORTED THAT THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR IS INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND FOUND A LOOSE CONNECTION ON THE EMERGENCY LIGHT. MAINTENANCE RESECURED THE CONNECTION. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00011ATTE6CH 20040819000642004081900064NM 2004 8 19 WLDA200464 120040802A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 33.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 33 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000662004081900066NM 2004 8 19 WLDA200460 120040802A5512ALC8101504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 3.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 3 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819000672004081900067SO 2004 8 19 MASA200400388 120040706A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL THRUST REVERSER ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07830MJ 145259 CAE311323 SUP/CLOSED- ASH 2811 IND. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH A ENG 1 REV DISAGREE CAUTION MESSAGE DURING TAKE OFF ROLL. MAINTENANCE DEFERRED E1 T/R IAW MEL 78-34-00 AND CONTINUED OPS. 7/9/04 MX RE-RIGGED AND OPS CHK OK. 2L72 4T4 FRTT00011ATTE6CH 20040819000682004081900068SO 2004 8 19 MASA200400412 120040718A323022260001401 PRIORITY VALVE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07853MJ 145464 SUP/CLOSED -ASH 2701 FROM CAE-PHL. THE LANDING GEAR WOULD NOT RETRACT DURING CLIMBOUT. IAW CFM CREW MADE 2ND ATTEMPT AND GEAR RETRACTED NORMALLY. MX TAKING A/C TO HANGER FOR TROUBLESHOOTING. MAINTENANCE REPLACED PRIORITY VALVE. 2L72 4T4 FRTT00011ATTE6CH 20040819000732004081900073NE 2004 8 19 HNAA0400069 220040722A7200PW123C ENGINE DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 2 FROZEN A HNAAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA07969HA123296628 468 AG00080 DURING CLIMB OUT FROM HHH CREW HEARD LOUD BANG FROM NR 2 ENGINE FOLLOWED BY TQ LOSS AND PROP AUTO FEATHERED. CREW SHUT ENG DOWN IAW CHECK LIST. REMOVE AND REPLACED ENGINE. 2H72 4T4 TRTA13NM E20NE 20040819000752004081900075NM 2004 8 19 DL73S040677 120040720A5330 SKIN BOEING737 737232 1384475NM PWA JT8 JT8D* NE FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27324DL 23096 FUSELAGE SKIN CRACKED AT STA 750 AND STR 18R ADJACENT TO AN EXISTING CHEM-MILL. AREA REPAIRED IAW ERA 092053-14. 2L72 4F4 FRTA16WE E2EA 20040819000762004081900076NM 2004 8 19 DL767040678 120040720A5730112T410314 SKIN BOEING767 767232 1385132NM GE CF6 CF680 30025NE RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27114DL 22226 RT LOWER WING SKIN SIDE LINK FITTING ATTACH FASTENER FOUND CRACKED. REPAIRED IAW ERA 091372-14AD. 2L72 4F4 FRTA1NM E13NE 20040819000772004081900077NM 2004 8 19 DL767040679 120040721A5753 WEDGE BOEING767 767232 1385132NM GE CF6 CF680 30025NE LT WING FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27114DL 22226 IB AFT FLAP TE WEDGE WAS FOUND WITH DAMAGE TO THE LOWER SKIN AND CORE. REPAIRED IAW ERA 091685-14. 2L72 4F4 FRTA1NM E13NE 20040819001042004081900104NM 2004 8 19 UPS04442923 120040817A3350 SWITCH BOEING747 747SR46 1384816NM EMERGENCY LIGHT JAMMED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 INSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH JAMS. INSTALLED NEW EMERGENCY CONTROL MODULE PER AMM 33-51-09 AND EO B747-3350-20899A, OPS CHECKED NORMAL. 2L74 4F RTA20WE 20040819001082004081900108NM 2004 8 19 UPS04M42912 120040529A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, HORIZONTAL STABILIZER NR 21 BARREL NUT HOLE FOUND CORROSION ON BOTTOM, BEARING AND SIDEWALL SURFACE. CORROSION AT BARREL NUT HOLE S/W & BEARING SURFACE REAMED TO 1.067 INCH & BLENDED OUT TO 0.0200 INCH, FOUND OUT OF LIMIT. REPAIR SLEEVE FAB & INSTALLED PER MD11-5510-19409-G.PR1422 B2 SEALANT APPLIED AT BLEND OUT VOIDS PER EN177-04. REPAIR SLEEVE INSTALLED AT NR 21 RT BARREL NUT HOLE PER EOMD1 1-5510-19409-G. REPAIR C/O AT BARREL NUT HOLE NR 21 RT PER EN1177-04. 2L73 4F RTA22WE 20040819001102004081900110NM 2004 8 19 DL73S040760 120040813A2121215201 GASPER FAN BOEING737 737232 1384475NM AIR COND BAY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27303DL 23075 DURING CRUISE SMELLED BURNING ODOR THAT REMAINED THROUGH LANDING. FOUND GASPER FAN C/B TRIPPED. RAN PACKS TO CLEAR ODOR. REPLACED FAN. 2L72 4F RTA16WE 20040819001122004081900112NM 2004 8 19 DL76S040762 120040813A3244B767300ERN TIRE BOEING767 767332 1382001NM NLG DAMAGED A DALAO OTHER C F.O.D. TXTAXI/GRND HDL 1 SO27121DE 23435 LEFT NOSE TIRE DAMAGED, MISSING A LARGE PIECE OF RUBBER. REPLACED LEFT NOSE TIRE ASSY. 2L72 4F RTA1NM 20040819001142004081900114NM 2004 8 19 DL73S040764 120040813A3397 WIRE BOEING737 737247 138448DNM BATTERY PACK BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27237WA 8823 23185 BOTH RED EMERGENCY LIGHTS INOP AT FWD GALLEY CLOSET INOP. FOUND BATTERY PACK WIRES AT APPROX STA 325 BROKEN AND CHAFED. REPAIRED AND RE-TERMINATED WIRE AT D9059 PIN 18. FUSES ALSO BLOWN IN FWD BATTERY PACK AT STA 400 AND REAR PACK AT STA 920. REPLACED PWR PACKS. CHECKS GOOD. 2L72 4F A16WE 20040819001162004081900116NM 2004 8 19 DL76L040767 120040816A5312141T2910126 BULKHEAD BOEING767 767332 1382001NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27180DN 25985 THE WEB OF THE CANTED BULKHEAD ON THE FWD SIDE OF THE NLG WHEEL WELL WAS FOUND GOUGED AT WL 175 AND LBL 22. THE GOUGE WAS REMOVED WITH A 1 X 2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 092714-14. 2L72 4F RTA1NM 20040819001182004081900118NM 2004 8 19 DL73S040769 120040817A53116546595141 FRAME BOEING737 737247 138448DNM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 FUSELAGE FRAME AT STATION 727A AND STRINGER 25L SUFFERED SERVICE DAMAGE FROM CARGO, AREA IS PSE F34. REPAIRED IAW ERA 092302-14. 2L72 4F A16WE 20040819001252004081900125EU 2004 8 19 AWXA200400898 120040805A5320D53471124200 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1292 LT BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED WEB Y1292 LT FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040819001272004081900127NM 2004 8 19 AALA20040826 120040807A1420 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21397AN 29604 MIA - EMERGENCY LIGHT AT ROW 31B INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 32A FOR EMERGENCY LIGHT AT SEAT 31B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040819001292004081900129 2004 8 19 AALA20040834 420040809A25655A33073 SLIDE BOEING737 737823 13844BZNM CABIN FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21921AN 29522 TUL - FORWARD GALLEY EMERGENCY DOOR SLIDE FAILED TO DEPLOY AUTOMATICALLY WHEN DOOR OPENED. DEPLOYED MANUALLY. REPLACED SLIDE FOR FORWARD GALLEY EMERGENCY DOOR AT STATION 328. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001312004081900131 2004 8 19 AALA20040825 420040811A2565D30654122 SLIDE BOEING757 757223 1384957NM L1 DOOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21627AA 24585 TPA - INADVERTENTLY DEPLOYED L1 SLIDE DURING TROUBLESHOOTING OF GIRT BAR. SLIDE DEPLOYMENT UNSUCCESSFUL. REPLACED L1 SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040819001332004081900133NM 2004 8 19 AALA20040829 120040803A5313 STRINGER BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21377AN 25446 AFW - STRINGER 25R AT STATION 439 HAS A CRACK OF ONE INCH ON THE VERTICAL LEG AFT OF THE LAST FASTENER HOLE OF THE STRINGER SPLICE. REPAIRED STRINGER S25R USING MRB 767 2598. STRINGER SPLICE EXTENDED BY TWO FASTENER ROWS BEYOND THE EDGE OF THE REPAIR DOUBLER. 2L72 4F RTA1NM 20040819001352004081900135 2004 8 19 AALA20040836 420040812A25655A33073 SLIDE BOEING737 737823 13844BZNM GALLEY DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21923AN 29524 TUL - FORWARD GALLEY DOOR EMERGENCY SLIDE DID NOT AUTOMATICALLY DEPLOY, DEPLOYED MANUALLY. REPLACED SLIDE FOR FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001372004081900137NM 2004 8 19 AALA20040830 120040803A5330 SKIN BOEING767 767323 1385205NM FUSELAGE DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21377AN 25446 AFW - FUSELAGE SKIN AND SPLICE PLATE AT STATION 434 BETWEEN S 25R AND S 24R IS DAMAGED AND CRACKED. DISCREPANCY AREA IS 5.5 INCH BY 5.5 INCH. REPAIRED DAMAGE AT THE SKIN AND AT THE BUTT SPLICE STRAP PER REPAIR INSTRUCTIONS IN PAGE 2 AND FIGURE 1 AND 2 OF MRB 767 2599. 2L72 4F RTA1NM 20040819001392004081900139EU 2004 8 19 AALA20040838 120040812A3230NAS5593 LOCK FOKKERF28 F28MK0100 4990807EU MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW211410E 11368 ORD - INFLIGHT T844/12 AFTER TAKEOFF SHORTLY AFTER SELECTING GEAR LEFT MAIN LANDING GEAR ANNUNCIATIED ON THE MFD. RECYCLED GEAR AND PROBLEM RETURN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ADJUSTED AND REPLACED KEYLOCK ON LEFT INBOARD GEAR DOOR LEG BUMPER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040819001402004081900140WP 2004 8 19 AALA20040839 120040811A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21452AA 49553 LAX - RIGHT HAND OVERHEAD EMERGENCY LIGHT AT STATION 1296 IS INOPERATIVE. REPLACED WIRE TO L794N20 ON L2 615 FOR RIGHT HAND OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040819001412004081900141NM 2004 8 19 SWAA042324 120040813A57536546481 SPINDLE BOEING737 7375H4 138449DNM LT & RT WING WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 WHEN FLAPS LOWERED TO 5, THE AIRCRAFT SHUTTERED. NO ROLL, FELT IN CONTROLS. REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP NR 1 AND NR 2 TOGGLES, SEQ CARRIAGE, SPINDLE. RT WING OUTBOARD AFT FLAP NR 7 AND NR 8 TOGGLES, SEQ CARRIAGE, SPINDLE PER MM. 2L72 4F RTA16WE 20040819001422004081900142NM 2004 8 19 SWAA042325 120040813A5751R1053M22 LIMITER BOEING737 7372H4 138448CNM MLG WW BINDING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 WITH FLAPS EXTENDED INFLIGHT, CONTROLS BIND IN ROLL IN BOTH DIRECTIONS. WITH FLAPS UP ROLL IS NORMAL (AUTOPILOT WILL STAY ENGAGED WITH FLAPS DOWN) FELT BINDING AGAIN IN BANK WHEN FLAPS EXTENDED FOR LANDING. REMOVED AND REPLACED AILERON FORCE LIMITER PER MM. 2L72 4F A16WE 20040819001432004081900143NM 2004 8 19 SWAA042326 120040813A5320BAC1506 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C3 CHECK, FOUND ZEE ANGLE AT BS 664, RBL 31.83, CRACKED. REPAIRED ZEE ANGLE PER EA. 2L72 4F RTA16WE 20040819001442004081900144 2004 8 19 SWAA042327 420040813A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29414WN 29820 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040819001632004081900163NM 2004 8 19 AWXA200400867 120040720A575365C263203 SKIN BOEING737 7373S3 1384711NM FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP WAS FOUND DELAMINATED AT WBL 262.0, JUST ABOVE NR 2 FLAP FAIRING. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF LT OUTBOARD FLAP AT WBL 262.0; CLEANED AND PREPARED AREA; FABRICATED A REPAIR DOUBLER; BONDED REPAIR TO FLAP IAW B737-300 SRM 51-70-10 FIG 30. 2L72 4F RTA16WE 20040819001642004081900164NM 2004 8 19 AWXA200400868 120040728A53156545812147 FLOORBEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 328 BETWEEN RBL 12 AND RBL 52, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CHORD AT BS 328 FROM RBL 12 TO RBL 52, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM UPPER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51-2 FIG 205. 2L72 4F RTA16WE 20040819001662004081900166NM 2004 8 19 SWAA042350 120040815A53116546595 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727A, STR 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040819001672004081900167EU 2004 8 19 MALA040516 120040803A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 DURING 6Y/4Y INSPECTION IN LCQ, DENT ON RT SIDE FUSELAGE AT STA 738.7 BELOW WL 113 MEASURES 1 X .045 DEEP. PERFORMED HFEC, NO DEFECTS NOTED. CUT OUT DAMAGED AREA, NDT NO CRACKS, FABRICATED DOUBLER-COUNTER SUNK, TREATED AND PRIMED IAW MESABA EO S53040. AIRCRAFT RELEASE DATE 8/5/04. 2L72 4T RTA52EU 20040819001682004081900168 2004 8 19 MALA040519 420040811A34206226190113 COMPUTER SAAB SF340 340B 7860101EU AHRS MALFUNCTIONED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 ON POWER UP C/BS F12 & F11 POPPED. TRIED RESETTING & POWERING UP ON INVERTER NR 2 THEN F11 POPPED. CAPT'S SIDE AVIONICS FAILED TO INITALIZE. AFTER RESETTING ALL BREAKERS & RESETTING PWR EVEN F11 & F12 STAYED IN. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER, ALL CKS GOOD IAW SAAB MM CH 34-20. S/N OFF 2846, P/N OFF 622-6190-113, S/N ON 2247, P/N ON 622-6190-113. 2L72 4T RTA52EU 20040819001692004081900169EU 2004 8 19 MALA040522 120040806A3340Q4681 LANDING LIGHT SAAB SF340 340B 7860101EU EXTERIOR INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15424XJ 340B424 AIRCRAFT WAS EN ROUTE TO ABR FROM MSP AND THE CREW NOTICED NO LANDING LIGHTS WORKING. DISPATCH DECIDED TO TURN THEM AROUND, BECAUSE OF THE LOADS FROM ABR TO PIR. MAINTENANCE RELAMPED RT AND LT LANDING LIGHTS (P/N Q4681), OPS CHECK GOOD. 2L72 4T RTA52EU 20040819001712004081900171EU 2004 8 19 MALA040515 120040807A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15535XJ E2371 DURING C-CHECK IN LCQ, NR 2 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESABA EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2H74 4F RTA49EU 20040820000012004082000001EA 2004 8 20 QXEA200400516 120040710A5240 STRUT CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DISENGAGED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09606QX6958 10023 PDX - FLIGHT 2473 - SERVICE DOOR WILL NOT OPEN PROPERLY. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-ENGAGED THE INNER AND OUTER UPLOCK STRUT SECTIONS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040820000022004082000002NM 2004 8 20 QXEA200400517 120040713A2810 LINE DHAV DHC8 DHC8202 2809007NM ZONE 400 LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09358PH14898 506 SEA - FLIGHT 2104 - FUEL WAS NOTED LEAKING ON THE NUMBER 2 INBOARD NACELLE. MAINTENANCE INSPECTED THE NACELLE AND FOUND THE FUEL LINE CONNECTING THE FLOW DIVIDER AND PUMP VALVE TO FIREWALL LOOSE. THE LINE WAS TORQUED AND THE OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040820000032004082000003NM 2004 8 20 SWAA042351 120040815A53106546529 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500B, LBL 17, WL 150, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040820000052004082000005NM 2004 8 20 SWAA042353 120040815A33506556633 LIGHT BOEING737 7377H4 1384404NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29404WN 27892 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040820000072004082000007 2004 8 20 SWAA042355 420040816A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040820000102004082000010SO 2004 8 20 CHQA000510 120040628A2150 A/C PACK EMB 145 EMB145LR 3260212SO NR 1 MALFUNCTIONED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11265 145226 ON CLIMBOUT AT ABOUT 3,000 FEET RECEIVED A PACK NR 1 PUTTING OUT STEAMING HOT AIR WITH BOTH CONTROLS IN FULL COLD POSITION. THEN RECEIVED SMOKE IN THE COCKPIT, DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD IMMEDIATELY. ACCOMPLISHED OVERWEIGHT LANDING AND RETURNED TO THE GATE. OPS CHECKED PACK NR 2 IAW EMB 145 AMM 21-51-00. DEFERRED PACK NR 1 IAW CHQ MEL 21-50-00-1 CAT C TICKET 11045. PERFORMED OVERWEIGHT LANDING INSPECTION PER EMB AMM 5-20-02. INSPECTION WAS GOOD. *S/D* MAINTENANCE REMOVED AND REPLACED THE DUAL TEMPERATURE CONTROL VALVE PER MAINTENANCE MANUAL. OPS CHECK GOOD. THIS CLEARS MEL 21-50-00-1 CAT C TICKET 11045. 2L72 4T RTT00011AT 20040820000112004082000011EU 2004 8 20 04FDEA02047 120040712A2780 COMPUTER AIRBUS310 A310203 3930313EU NR 2 SFCC MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25427FE 362 AFTER TAKEOFF NR 1 SYSTEM FAULT, FLAPS RETRACTED NORMAL FROM 20/20. NEXT RETRACTION GOT BOTH SYSTEM 1 & 2 FAULT. SLATS LOCKED AT 15 DEG. FOLLOWED QRH PROCEDURES, RECYCLED AND NO HELP. SET UP FOR SLATS 15 STUCK LANDING. SFCC NR 2 WAS REMOVED AND REPLACED DUE TO HARD FAULT AT BLOCK-IN REF A310 AMM 27-51-18-4. TROUBLESHOT BOTH SFCC COMPUTERS AND FOUND THE NR 2 SFCC WOULD CONTINUALLY FAULT THE RT KRUEGER. REPLACED THE RT KRUEGER FLAP RETRACT SWITCH IN REF TO AIRBUS AMM A310-20 0 27-51-18-4, 27-89-00-6. SYSTEM OPERATES AND CHECKS NORMAL. 2L72 4F RTA35EU 20040820000122004082000012NM 2004 8 20 DHL2004782009 120040702A3234A42006028305 SOLENOID BOEING727 727227 1384078NM MLG HANDLE FAILED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 REF ITEM 1P LP 371436 GEAR HANDLE STICKS IN OFF POSITION AND MUST BE FORCED INTO UP POSITION. REF ITEM 5M LP 371437 FOR REMOVE & REPLACE OF GEAR HANDLE SOLENOID. REMOVED AND REPLACED GEAR HANDLE LOCK SOLENOID IAW MM 32-31-16, NO HELP LEFT INSTALLED. 2L73 4F A3WE 20040820000132004082000013WP 2004 8 20 DHL2004807012 120040702A2611 WARNING LIGHT DOUG DC8 DC873F 302199FWP CARGO SMOKE ILLUMINATED A DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01807DH 45990 YELLOW MX LIGHT ILLUMINATED ON LWR CARGO SMOKE DETECTOR CODE AD16242{B} SYS OK LIGHT ILLUMINATED ALSO. TRANSFERRED TO DMI 17083 IAW MEL 26-10-1,CAT C PLACARD INSTALLED. 2L74 4F RT4A25 20040820000142004082000014CE 2004 8 20 GLBA20030660 120040628A5260 DOOR BEECH 1900 1900D 1154162CE AIRSTAIR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03118UX UE118 DOOR CABIN CORRODED. REPAIRED AIRSTAIR DOOR. 2L72 4T RTA24CE 20040820000172004082000017EU 2004 8 20 MALA040523 120040808A3230HP84830721 CONTROL VALVE SAAB SF340 SF340A 7850100EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL1599XJ 340A099 ON APPROACH TO MCW SELECTED GEAR DOWN, INTRANSIT LIGHT IN HANDLE ILLUMINATED. HYDRAULIC PUMP WOULD RUN, GUT GEAR DID NOT EXTEND. RECYCLED F7 C/B AND GEAR EXTENDED. MAINTENANCE INSPECTED A/C AND FOUND SAFE FOR FERRY FLIGHT FROM MCW TO MSP WITH GEAR EXTENDED. AIRCRAFT TO BE FLOWN IN NO ICING CONDITIONS AND AIRSPEED RESTRICTED TO 200 KNOTS. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE P/N ON/OFF HP84830-721, SN/OFF 0006, SN/ON 0017 IAW AMM 32-31-15-4. LANDING GEAR EXTENSION AND RETRACTION TESTS GOOD IAW 32-30-00. 2L72 4T RTA52EU 20040820000182004082000018EU 2004 8 20 MALA040525 120040804A2560 COVER BAC 146 AVRO146RJ85A1500097EU ESCAPE ROPE BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15525XJ E2350 CAPTAINS ESCAPE ROPE COVER BROKEN. RE-SAFETIED CAPT ESCAPED ROPE IAW AMM CH 25-60-04 201. 2H74 4F RTA49EU 20040820000192004082000019EU 2004 8 20 MALA040529 120040729A3350549132406 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15456XJ 340B456 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1706 REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. REPLACED 2 EACH CELL PACKS P/N 549-1324-06 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/8/04. 2L72 4T RTA52EU 20040820000202004082000020EU 2004 8 20 MALA040531 120040730A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15517XJ E2335 BATTERY PACK P/N 61-2275-1, S/N 9710084 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 61-2275-1 AND UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 7/31/04. 2H74 4F RTA49EU 20040820000222004082000022EU 2004 8 20 MALA040527 120040807A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15404XJ 340B404 DURING CAPACITY CHECK, POWER SUPPLY P/N 3301-51, S/N 1339 DEAD. REPLACED BATTERY ASSEMBLY P/N 3301-31 UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 8/11/04. 2L72 4T RTA52EU 20040820000232004082000023EU 2004 8 20 MALA040528 120040806A3350549132406 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15424XJ 340B424 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1603 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED 2 EACH CELL PACKS P/N 549-1324-06. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 8/11/04. 2L72 4T RTA52EU 20040820000252004082000025NM 2004 8 20 SWAA042357 120040816A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 14L AT BS 420, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040820000262004082000026NM 2004 8 20 AWXA200400785 120040717A3397BMS13311122 WIRE BOEING737 737301 1384611NM SEAT ROW 11 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 DURING 8-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 - 17 WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820000282004082000028EU 2004 8 20 AWXA200400787 120040716A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONES 241 & 263 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28629AW 076 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY LIGHTS FAILED TEST AT THE FLIGHT ATTENDANTS PANEL. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), AND POWER SUPPLY BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820000292004082000029NM 2004 8 20 AWXA200400788 120040718A335020121 CHARGER BOEING737 7373G7 1384595NM FUSELAGE FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28157AW 23779 PHX - EEL - EMERGENCY ESCAPE PATH LIGHTS INOP AT SEAT ROWS 19 -23 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820000312004082000031NM 2004 8 20 AWXA200400791 120040624A53106552878697 CREASE BEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-2 DOOR CREASE BEAM (INNER CHORD) AT BS 986. MAINTENANCE REMOVED CORRODED CREASE BEAM AT BS 986; FABRICATED A NEW REPLACEMENT CREASE BEAM PER DWG 65-5287697; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040820000322004082000032NM 2004 8 20 AWXA200400792 120040624A531065C807351 CREASE BEAM BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR CREASE BEAM (INNER CHORD) BETWEEN BS 950 TO BS 986. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 950 TO BS 986; FABRICATED A NEW REPLACEMENT CREASE BEAM; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20040820000332004082000033NM 2004 8 20 AWXA200400793 120040622A5320652072629 WEB BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK INTERGRANULAR CORROSION WAS FOUND NUMEROUS FASTENER HOLES ON FORWARD CARGO COMPARTMENT LOWER DOOR SILL WEB BETWEEN BS 440 TO BS 480. MAINTENANCE REMOVED CORRODED LOWER DOOR SILL WEB FROM BS 440 TO BS 480; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-20726; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9. 2L72 4F RTA16WE 20040820000352004082000035EU 2004 8 20 UPS04142860 120040723A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01128UP 0813 LAV EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT. 2L72 4F RTA35EU 20040820000362004082000036 2004 8 20 UPS04142862 420040731A25652LA00269900 SLIDE AIRBUSA300 A300F4622R 3930360EU L1 DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 L1 DOOR ESCAPE SLIDE AND LIGHT INOP. PLACED ON MEL 52-73-01-1 M285209 ASSIGNED. PART ORDERED. BUZZER OPS NORMAL. 2L72 4F RTA35EU 20040820000372004082000037NM 2004 8 20 UPS04242835 120040712A5343 FRAME BOEING727 72725C 138400HNM NLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, FRAME CRACKED AT BS 323 AT LOWER LOBE WALKWAY LEVEL, LEFT SIDE OF LOWER NOSE COMPARTMENT PRESSURE WEB AND FRAME REMOVED IAW SRM 51-30-2. REPLACEMENT FRAME FABRICATED IAW SRM 51-20-1. FRAME REPROTECTED IAW 51-10-02. FRAME CUT AND INSTALLED IAW SRM 51-30-2. REPAIR SPLICE FABRICATED IAW 51- 40-3 FIG 1. SPLICE PROTECTED IAW 51-10-02 AND INSTALLED IAW SRM 51- 30-2. FASTENERS INSTALLED IAW SRM 51-30-2. 2L73 4F A3WE 20040820000382004082000038NM 2004 8 20 UPS04242836 120040707A5230 STOP FITTING BOEING727 72725C 138400HNM FWD CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, FWD CARGO DOOR CUTOUT, NR 4 FWD STOP PAD IS CRACKED. STOP PAD LOCATED ON FWD EDGE FRAME OF DOOR CUTOUT IN FUSELAGE, REPAIR IN IAW EO B727-5230-0032 NOT SUITABLE FOR THIS STOP FITTING. REPLACEMENT OF STOP FITTING CARRIED OUT IAW BOEING DRW 65-20723 AND SRM 51-30-02. FWD CARGO DOOR RIG GAPS CHECKED AND FOUND SATISFACTORY IAW 52-31-01. 2L73 4F A3WE 20040820000392004082000039NM 2004 8 20 UPS04242837 120040706A5230 SKIN BOEING727 72725C 138400HNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C SUSPECT CRACK AFT CARGO DOOR FRAME SKIN FLANGE RADIUS OF NR 2 FWD STOP FITTING (FWD), REF FIG 1 FLAG NOTE 1 OF EO SECTION B-B DISPLACED DOOR SEAL IAW MM 51-30-00. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 FIG 4. RESULT: CRACK CONFIRMED ENDS MARKED. DUE TO CLOSE PROXIMITY OF CRACKS, THE FRAMES WILL BE REPLACED. FRAMES ORDERED. REMOVED AFT CARGO DOOR FRAME IAW 51-30-02. FRAME INSTALLED ON AFT CARGO DOOR IAW DRW 65C16422. OPERATIONAL AND LEAK CHECK OF DOOR C/W. 2L73 4F A3WE 20040820000412004082000041WP 2004 8 20 ARWA20040508 120040519A5312 PRESSURE PANEL DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 DURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STATION 12.000 AND STA 8.000 SUBFLOOR WAS FOUND WITH CORROSION, RBL 60. REPAIRED FUSELAGE NOSE FLOOR PRESSURE PANEL BETWEEN -12 TO FS 8 AND L22L IAW ELEVEN INC DRAWING AS11566 SHEET 1 THRU 4, DATED 05/26/04. ISSUED FAA FORM 8110-3, DATED 05/26/04, APPROVING THIS REPAIR. 2L74 4F 4A25 20040820000432004082000043WP 2004 8 20 IXA04000970 120040709A2750 ACTUATOR DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11828BX822862148 45993 AIR RETURN, AFTER T/O SLOT LIGHT REMAINED ON AFTER FLAP RETRACTED. CYCLED, SLOT LIGHT OUT WHEN EXTENDED, ON WHEN RETRACTED. THEN 10 MIN INTO FLT SLOT LIGHT WENT OUT WITH FLAPS RETRACTED. NEVER EXCEEDED 230 KTS, LIGHT CAME BACK ON WHEN ON THE GROUND, WHILE TAXIING INTO PARKING LOST HYD SYSTEM. MAINTENANCE INSPECTION OF FLAPS FOUND BROKEN LEFT I/B ACTUATOR ASSY BRACKET. HYDRAULIC LEAK COMING FROM BROKEN HYDRAULIC ELBOW ON SAME ACTUATOR ASSY. REMOVED AND REPLACED ACTUATOR ASSY PER DACO M/M 27-51-9, RESERVICED HYDRAULIC SYSTEM PER DACO 12-30-1, FLAPS AND HYDRAULIC SYSTEM OPS AND LEAK GOOD. SLOT LIGHTS OP CHECK GOOD. 2L74 4F RT4A25 20040820000442004082000044EU 2004 8 20 YENA200438 120040702A5210FE240004 CYLINDER DAMPER AIRBUS320 A320232 3930326EU ZONE 800 LEAKING A YENAK NONE O OTHER ININSP/MAINT 1 EA15558JB5929 1915 REF TSI 558-52-04-287, L1 DOOR ASSIST BOTTLE REQUIRES FREQUENT SERVICING. REMOVED AND REPLACED DOOR ASSIST BOTTLE. 2L72 4F RTA28NM 20040820000452004082000045EA 2004 8 20 COMA0460451 120040810A33976464 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01929CA 7035 FLIGHT 4988 EMERGENCY FLOOR PATH LIGHTS ARE INOP. REPLACED THE FLOOR LIGHTS CABLE ASSY. 2L72 4F RTA21EA 20040820000482004082000048NM 2004 8 20 AWXA200400795 120040623A5310693535214 SHEAR TIE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE AT BS 275, STR 15 RT. MAINTENANCE REMOVED CRACKED STRINGER SHEAR TIE AT BS 275, STR 15 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4A. 2L72 4F RTA16WE 20040820000502004082000050EU 2004 8 20 UPS04142712 120040713A3350 BULB AIRBUS300 A300B4622R 3930312EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01133UP 0817 EMERGENCY EXIT LIGHT ARM/DISARM ANNUNCIATOR SWITCH LIGHT BULB INOP. RELAMPED, OPS CHECK GOOD. 2L72 4F RTA35EU 20040820000522004082000052NM 2004 8 20 UPS04242701 120040709A5753 CARRIAGE BOEING727 727173C 1384059NM LT OB TE FLAP WORN A IPXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO01938UP 19506 ATB FL 330 IN CLIMB EXPERIENCED MODERATE VIBRATION. FOUND LEFT OUTBOARD TRAILING FLAP, INBOARD TRACK AFT ROLLER CLEARANCE OUT OF TOLERANCE. REPLACED ROLLER. 2L73 4F A3WE 20040820000532004082000053NM 2004 8 20 UPS04242702 120040622A5330 SKIN PANEL BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, ON REMOVAL OF SKIN PANEL CORROSION FOUND ON LWR SKIN PANEL LAP JOINT S4R BETWEEN BS 615 & BS 540. REPAIR CARRIED OUT IAW AAAE 2004-061-006. 2L73 4F A3WE 20040818000862004081800086NM 2004 8 18 AMTA200400119 120040205A3350D71702001 POWER SUPPLY BOEING737 73783N 13844HINM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11332TZ 30679 FOUND LEFT AFT O/W EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK CHARGER PER MM 33-51-06, OPS GOOD. (M) 2L72 4F RTA16WE 20040818000902004081800090NM 2004 8 18 AMTA200400122 120040205A5321 PANEL BOEING737 73783N 13844HINM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11323TZ 30033 FOUND C2 CARGO PANEL NR 1 HAS CORROSION. CORROSION BEYOND LIMITS PER SRM. FABRICATED NEW PANEL AND INSTALLED PANEL. 2L72 4F RTA16WE 20040818000972004081800097SO 2004 8 18 SIMA200419701 120040625A532014524131005 BRACKET EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21728AE 145328 SAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND INTERNAL FUSELAGE JUST INSIDE PASSENGER DOOR, TWO BRACKETS HAVE CORROSION. REMOVED AND REPLACED BRACKETS P/N 145-24131-005, 145-24131-007, IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040818001012004081800101NM 2004 8 18 AMTA200400204 120040226A2497 WIRE BOEING757 75733N 1384931NM GEN CONNECTOR DAMAGED A AMTAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 GL11558TZ 32592 EICAS MSG R GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. FOUND WIRES W5012-0004 AND -0003 FROM CONNECTOR D1394 CHAFED TO GROUND. REPAIRED WIRES PER WDM STD PRACTICES 20-23-00, GEN FUNCTIONS OPS NORMAL. (M) 2L72 4F RTA2NM 20040818001082004081800108EA 2004 8 18 ASOA04475 120040630A5714 RIB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11844AS 7317 DURING A C-CHECK IN MCN, THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT BATTERY RIB IN THE RIGHT WHEEL WELL AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20040818001222004081800122EU 2004 8 18 ALGA096464 120040722A6510C651A2001101 DISC PACK UROCOPEC120 EC120B 8680987EU TAIL ROTOR CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL 1263 FOUND ONE CRACKED DISC, IN TWO PLACES.REPLACED W/NEW PART BY FIELD MAINT. 1G72 3U NCR0001RD 20040818001252004081800125NE 2004 8 18 HEEA096490 220040622A75325044T08P10 BLEED VALVE BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE ENGINE MALFUNCTIONED E HEEAO OTHER MJ OVER TEMP WARNING INDICATION HOHOVERING 1 SW0359806 28140 WHILE HOVERING FOR TAKEOFF, NR 2 MGT STARTED RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH. 2G72 4U4 U H10SW E8NE 20040818001282004081800128EU 2004 8 18 HE66096088 120040706A28229A2045 PUMP UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIU2F NE FUEL BOOST FAILED E HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW03135CR418 0164 FAILED IN FLIGHT/ FUEL BOOST PUMP REPLACED. 1G72 3U3 U H88EU E34NE 20040818001352004081800135SW 2004 8 18 ALGA096399 120040720A6300406310405101 DISC PACK BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R DRIVE WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03937AL533 53383 FOUND EXCESSIVE PLAY AND RATCHETY. REPLACED W/NEW BY FIELD MAINT. 1G71 3U3 UO H2SW E1GL 20040818001452004081800145EA 2004 8 18 SWIA200413686 120040808A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07913SW 7597 STAB CHANEL 1 FALLS OFF LINE. REMOVED AND REPLACED MCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD. PN 7062-3 SN OFF 331. 2L72 4F4 FRTA21EA E15NE 20040818001502004081800150EU 2004 8 18 KBM2004F00151 120040521A7931642790041 TRANSMITTER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL PRESSURE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH869 3345 NO OIL PRESSURE INDICATION. REMOVED AND REPLACED OIL PRESS TRANSMITTER. 1G71 3U3 U H9EU E19EU 20040818001542004081800154EU 2004 8 18 KBM2004F00143 120040525A771230531366 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TORQUE INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 TORQUE INDICATOR, NEEDLE DOES NOT MOVE AT ALL. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001552004081800155NM 2004 8 18 WLDA200443 120040812A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 29. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 29 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001562004081800156EU 2004 8 18 KBM2004F00161 120040420A21210500847 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE BLOWER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 10 2300 AMP METER IN THE RED WHEN A/C ON. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040818001572004081800157EA 2004 8 18 SWIA200413687 120040811A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07934SW 7722 RT SIDE EXTERNAL EMERGENCY LIGHT BURNED OUT. RELAMPED RT SIDE EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040818001622004081800162NM 2004 8 18 WLDA200444 120040802A5512ALC8104504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 25.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 25 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001632004081800163NM 2004 8 18 WLDA200445 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA PW4062PW4062 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 ITEM: DURING 4-C CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 24.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 24 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040818001812004081800181NM 2004 8 18 P5CA0401136 120040810A2720964007004 COMPARATOR BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE RUDDER INOPERATIVE A P5CAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP23508MC 21644 RUDDER RATIO LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED RUDDER RATIO COMPARATOR. 2L74 4F4 F A20WE E23EA 20040818001942004081800194EU 2004 8 18 KBM2004F00174 120040519A33404572 LANDING LIGHT SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL EXTERIOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 LANDING LIGHT INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 U H9EU E4CE 20040819000142004081900014 2004 8 19 MWEA040147 420040812A256539361901 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE SERVICE DOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 BOTH FORWARD AND AFT GALLEY SERVICE DOOR GIRT BAR LATCH SUPPORT FITTINGS ARE CORRODED BEYOND REPAIR. FABRICATED AND INSTALLED FITTINGS. 2L72 4F4 F A6WE E9NE 20040819000192004081900019WP 2004 8 19 IXXA4001040 120040811A3220 DOOR DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NLG OPEN A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11603AL92883973 46003 AFTER TAKE OFF WITH THE GEAR UP THE CREW HEARD EXCESSIVE NOISE COMING FROM THE NOSE GEAR AREA. CREW CYCLED GEAR AND SOUND CONTINUED UPON INVESTIGATING NOSE GEAR AREA FOUND LT FWD GEAR DOOR OPEN, RESET DOOR IAW DC-8. OPS CHECK NORMAL NO DAMAGE NOTED. 2L74 4F4 FRT4A25 E2GL 20040819000292004081900029NM 2004 8 19 HNAA0400112 120040813A335061047811 BATTERY PACK DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE EMERGENCY LIGHT INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07810EX 308 WHILE IN ROUTINE MAINTENANCE IT WAS REPORTED THAT THE FIRST ROW OF EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED POWER SUPPLY AT THE 500 POSITION. OPERATIONAL CHECKS GOOD. 2H72 4T4 TRTA13NM E20NE 20040819000342004081900034EU 2004 8 19 RAIA00408006 120040805A612031056294 SWITCH JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE LT BETA PRESSUREINOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03572HK4575 41091 LT BETA LIGHT WENT OUT DURING TAXI. MAINTENANCE REMOVED AND REPLACED LT BETA PRESSURE SWITCH. 2L72 4T4 TRTA41NM E18NE 20040819001222004081900122EU 2004 8 19 AWXA200400895 120040805A5315D53112091200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FORWARD END OF FR 20. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 RT AT FR 20 IAW A320 SRM 51-42-11 FIG 8, 9 & 12. 2L72 4F RTA28NM 20040819001242004081900124EU 2004 8 19 AWXA200400897 120040805A5320D53112067201 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1546 RT AT FR 20. MAINTENANCE REMOVED CORRODED WEB Y1546 RT AT FR 20; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040819001462004081900146NM 2004 8 19 SWAA042329 120040813A33506104781 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29356SW 25251 DURING SCHEDULED SERVICE, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040819001482004081900148NM 2004 8 19 SWAA042331 120040813A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040819001502004081900150 2004 8 19 SWAA042338 420040814A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29406WN 27894 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040819001522004081900152NM 2004 8 19 SWAA042340 120040814A53306545776 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 972, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040819001542004081900154NM 2004 8 19 SWAA042342 120040815A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 980, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040819001562004081900156NM 2004 8 19 SWAA042344 120040815A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 65, WL 202, CRACKED. REMOVED AND REPLACED FRAME SECTION PER TI-153-018. 2L72 4F RTA16WE 20040819001582004081900158NM 2004 8 19 SWAA042348 120040815A53116546550 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040819001602004081900160NM 2004 8 19 AWXA200400864 120040725A57536546431255SP WEDGE BOEING737 7373S3 1384711NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT OUTBOARD FORE FLAP 106.5 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED DAMAGED ON UPPER SURFACE OF LT OUTBOARD FORE FLAP FROM WBL 307.11 LT TO 413.61 LT; CLEANED AND PREPARED AREA; FABRICATED REPAIR DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20040819001622004081900162NM 2004 8 19 AWXA200400866 120040727A53206546812170 FLOOR SUPPORT BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN BS 950 AND BS 966, LBL 18, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 950 TO BS 966, LBL 18, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12-13. 2L72 4F RTA16WE 20040820000062004082000006NM 2004 8 20 SWAA042354 120040816A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 FWD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040820000542004082000054NM 2004 8 20 UPS04242703 120040618A5753 FLAP TRACK BOEING727 72725C 138400HNM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, NR 4 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD-B. REPAIR CARRIED OUT IAW AAAE 2004-061-003. 2L73 4F A3WE 20040820000562004082000056NM 2004 8 20 AWXA200400751 120040627A53476545410200 SEAT TRACK BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .75 INCH CRACK WAS FOUND ON INBOARD SIDE OF SEAT TRACK FLANGE AT BS 727B, RBL 45. MAINTENANCE CUT OUT DAMAGED AREA OF SEAT TRACK FLANGE AT BS 727B, RBL 45. FABRICATED A FILLER, SHIM AND 2 EACH REPAIR STRAPS; INSTALLED REPAIR PARTS IAW AWA ER 03-5700-04187-SS1. 2L72 4F RTA16WE 20040820000612004082000061WP 2004 8 20 UPS04842902 120040716A574456423423 FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, LEFT WING FLAP HINGE STATION 3 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D. 2L74 4F RT4A25 20040820000622004082000062NM 2004 8 20 AWXA200400817 120040726A335032145410 EPSU AIRBUSA319 A319132 3930340NM ZONE 241 FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28813AW18244 1223 SFO - EEL - DURING 8-DAY CHECK; FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL) FAULTED. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820000662004082000066EU 2004 8 20 AWXA200400821 120040716A5321D5367150100000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK A 1 INCH CRACK WAS FOUND ON CABIN FLOOR PANEL 232MF. MAINTENANCE REMOVED CRACKED FLOOR PANEL 232MF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 10 D53671501; INSTALLED NEW REPLACEMENT PANEL IAW AWA T/C R1C25306. 2L72 4F RTA28NM 20040820000682004082000068EA 2004 8 20 04183667 120040701A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27667BR 7535 DURING INSPECTION THE RIGHT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040820000692004082000069EA 2004 8 20 04183674 120040701A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27674BR 7601 DURING INSPECTION THE LEFT HAND AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040820000822004082000082NM 2004 8 20 AWXA200400779 120040710A5310D53471209223 BEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 1-2. 2L72 4F RTA28NM 20040820000832004082000083NM 2004 8 20 AWXA200400780 120040710A5310D5347218920400 BEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT AT FR 68, INSTALLED NEW REPLACEMENT BEAM IAW A319 SRM 51-42-11 FIG 12 & 18. 2L72 4F RTA28NM 20040820000852004082000085EU 2004 8 20 AWXA200400782 120040712A5310D5347217220000 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LEFT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LEFT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040820000942004082000094SO 2004 8 20 CHQA000512 120040711A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11275 145345 DURING LATER PORTION OF THE FLIGHT, DETECTED ODOR IN THE COCKPIT AND FORWARD CABIN AREA. IT SMELLED LIKE BURNING PLASTIC AND THERE WAS NO VISIBLE SMOKE. VISUALLY INSPECTED RADAR, FORWARD ELECTRONICS BAY, BATTERY COMPARTMENT, BEHIND OVERHEAD CIRCUIT BREAKER PANEL, RELAYS BEHIND THE CAPTAIN AND FIRST OFFICER, WINDSHIELD HEAT, AND OPS CHECKED PACKS 1 & 2. NO EVIDENCE OF OVERHEATING, PITTING, ARCING, BURNING OR OTHER DEFECTS WERE NOTED. 2L72 4T RTT00011AT 20040820000952004082000095NM 2004 8 20 AWXA200400812 120040725A3397BMS13311122 WIRE BOEING737 73733A 1384673NM SEAT ROW 16 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 PHX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 16 LT. MAINTENANCE REPAIRED A BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820000972004082000097NM 2004 8 20 AWXA200400814 120040724A53406225135002 MOUNT BOEING737 73733A 1384673NM WX RADAR FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28166AW460468512 23627 ON CLIMBOUT OF PHX EN ROUTE TO MCI RECEIVED WEATHER RADAR FAIL ANTENNA MESSAGE, DUE TO WEATHER EN ROUTE TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR ANTENNA MOUNT PEDESTAL IAW BMM 34-41-11-4, OPERATIONAL CHECK WAS GOOD. VENDORS INCOMING FUNCTIONAL TEST OF WEATHER RADAR ANTENNA MOUNT PEDESTAL S/N 2024 CONFIRMED REASON FOR REMOVAL, UNIT FOUND TO HAVE DEFECTIVE ELEVATOR MOTOR. REPLACED DEFECTIVE MOTOR AND OVERHAULED UNIT IAW CMM 34-45-22, REV. 15. 2L72 4F RTA16WE 20040820001002004082000100NM 2004 8 20 AWXA200400824 120040624A5320143N808728 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK A .5625 INCH CRACK WAS FOUND IN INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, STR 13 RIGHT, WL 231, AT R-2 DOOR FRAME. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, STR 13 RT, WL 231; FABRICATED A NEW REPLACEMENT INTERCOSTAL AND CLIP; INSTALLED REPAIR PARTS IAW T/C M1C53612. 2L72 4F RTA2NM 20040820001032004082000103NM 2004 8 20 04FDEA01799 120040618A5744ARC050213 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.223 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78010, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040820001052004082000105NM 2004 8 20 AWXA200400830 120040723A5320D5347112420100 SHEAR PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RIGHT AFT SHEAR PLATE AFT AND OUTBOARD OF Y1292 RIGHT BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED RIGHT AFT SHEAR PLATE AFT AND OUTBOARD OF Y1292 RIGHT FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2L72 4F RTA28NM 20040820001072004082000107NM 2004 8 20 AWXA200400832 120040723A5310D5347218820400 BEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LEFT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LEFT AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 8 - 12 & 18. 2L72 4F RTA28NM 20040820001092004082000109NM 2004 8 20 AWXA200400834 120040723A5310D5347218920400 BEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RIGHT AT FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2L72 4F RTA28NM 20040820001122004082000112NM 2004 8 20 AWXA200400837 120040724A5347D5311281520200 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765 LT BETWEEN AT FR 16. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 LT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PART IAW A319 SRM 53-11-15 FIG 202. 2L72 4F RTA28NM 20040820001142004082000114NM 2004 8 20 04FDEA01850 120040624A5753ARC7490501 FITTING DOUG MD11 MD11 3023602NM ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING MID AND AFT HOLES FOUND WORN. RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING REMOVED & REPLACED AS PER EO 1-5750-7-5005 PT2 TITLE : WINGS - TRAILING EDGE DEVICES - INSPECT/MODIFY I/B FLAP VANE ATTACH FITTINGS STEP 32 AND FLAP VANE OPERATION CHECK CARRIED OUT. FOUND SATISFACTORY AS PER AMM 27-50-00. 2L73 4F RTA22WE 20040820001162004082000116 2004 8 20 QXEA200400513 420040711A342042000332501 COMPUTER BOMBDRDHC8 DHC8401 1390041NM ZONE 100 AHRS INOPERATIVE A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09415QX4030 37 4081 SEA - ON FLIGHT NUMBER 2382, RETURNED TO FIELD, UNEVENTFUL LANDING ACCOMPLISHED. HEADING MISMATCH ANNUNCIATION ON BOTH PFD'D AFTER TAKEOFF, (LEFT SIDE APPEARS CORRECT). TROUBLESHOT NR 2 AHRS SYSTEM TO BAD NR 2 AHRS COMPUTER. REMOVED AND REPLACED AHRS COMPUTER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040820001172004082000117NM 2004 8 20 CALA0400595 120040811A5320656571034 CHANNEL BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714346 23584 INSPECTION FOUND HAT CHANNEL FOR VHF ANTENNA CORRODED AT STA 727D, BL 0. A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040820001212004082000121NM 2004 8 20 CALA0400599 120040809A5330 SKIN BOEING757 757224 1384958NM FUSLEAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2757111 27301 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 215.25-223.5, S15R TO S16R, WL 188 JUST BELOW RT AOA VANE. THE SKIN WAS REPAIRED IAW ECRA 5310-04429. A DIP WAS ISSUED TO ACCOMPLISH AN INITIAL INSPECTION WITHIN 25,000 FLIGHT CYCLES AND TO PERFORM REPEAT INSPECTIONS EVERY 3,000 FLIGHT CYCLES. 2L72 4F RTA2NM 20040820001232004082000123NM 2004 8 20 SWAA042359 120040816A57436567172 FITTING BOEING737 7373H4 1384600NM LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED SERVICE CHECK, FOUND LT MLG FWD AND AFT STABILIZER FITTINGS CORRODED. REMOVED AND REPLACED LT MLG FWD AND AFT STABILIZER FITTINGS PER MM. 2L72 4F RTA16WE 20040820001252004082000125NM 2004 8 20 SWAA042361 120040816A5320BAC1490 ANGLE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 360, STR 8L, CRACKED. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20040820001312004082000131SO 2004 8 20 CHQA000513 120040706A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281 145391 LEFT HAND UPPER EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LEFT HAND UPPER EMERGENCY LIGHT PER EMB 145 MM 33-50-10 AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040820001342004082000134NM 2004 8 20 C1HA200479003 120040712A5730 PANEL BOEING727 727225 1384077NM RT WING EXHAUST DELAMINATED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15679MG 22557 RIGHT WING APU EXHAUST PANEL DELAMINATED AND CORRODED AT EXHAUST CUTOUT. 2L73 4F A3WE 20040820001362004082000136NM 2004 8 20 AWXA200400882 120040815A3350BR964411 LIGHT BOEING737 73733A 1384673NM SEAT ROW 4 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 LAX - EEL - DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820001382004082000138EU 2004 8 20 AWXA200400884 120040813A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28620AW 052 DEN - EEL - DURING 8-DAY CHECK THE RT MID CABIN EMERGENCY LIGHT BATTERY FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE RT MID CABIN EMERGENCY LIGHT BATTERY AT EMERGENCY POWER SUPPLY UNIT 12WL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820001422004082000142NM 2004 8 20 AWXA200400889 120040720A575465C26601181 SKIN BOEING737 7373S3 1384711NM NR 6 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .5 INCH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN NR 6 SLAT INBOARD AUXILIARY GUIDE ATTACH AREA 42 INCHES AND 45 INCHES FROM INBOARD END. MAINTENANCE CUT OUT CRACKED NR 6 SLAT SKIN 42 INCHES TO 57 INCHES FROM INBOARD END; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20040820001452004082000145NM 2004 8 20 AWXA200400892 120040720A575465C266047 SKIN BOEING737 7373S3 1384711NM NR 4 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH .5 INCH CRACKS WERE FOUND AT RIVET HOLES IN NR 4 SLAT BETWEEN SLAT STA 64.25 AND 78.25. MAINTENANCE CUT OUT CRACKS IN NR 4 SLAT 45.5 TO 61.5 INCHES FROM INBOARD END; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20040820001492004082000149NM 2004 8 20 AWXA200400848 120040803A7931ST104Z TRANSMITTER BOEING737 737277 1384570NM NR 1 ENG OIL FALSE INDICATIONA AWXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28178AW236456404 22645 ON CLIMBOUT OF LAS EN ROUTE FOR SFO AT FL 190 NR 1 ENGINE OIL PRESSURE DROPPED TO 10 PSI, FOLLOWED QRH AND SHUTDOWN NR 1 ENGINE, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSMITTER IAW BMM 79-032-011-4, OPERATIONAL CHECK OF OIL PRESSURE INDICATING SYSTEM WAS GOOD. VENDORS INCOMING FUNCTIONAL TEST OF OIL PRESSURE TRANSMITTER S/N 2516 CONFIRMED REASON FOR REMOVAL FOR ERRATIC OPERATION. DISASSEMBLY OF UNIT FOUND SYNCHRO BRUSHES BURNT, ARBOR TEETH WORN, AND A DEFECTIVE SOLDER STRIP. REPLACED DEFECTIVE PARTS AND OVERHAULED UNIT IAW CMM 31-59-1. 2L72 4F RTA16WE 20040820001502004082000150NM 2004 8 20 UPS04242840 120040712A5753 SKIN BOEING727 72725C 138400HNM LT WING TE FLAP DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, LEFT I/B FOREFLAP I/B END & UPPER SURFACE HAS DISBOND. REPAIRED IAW SRM 51-40-20. DURING OPS CHECKS THE O/B END WAS CONTACTING THE MIDFLAP AND BINDING. FOREFLAP RESKIMMED BUT DID NOT SOLVE PROBLEM. INSTALLED FOREFLAP REMOVED FROM A/C N945UP FOR TROUBLESHOOTING PER NRC 725261, NO BINDING EXPERIENCED. 2L73 4F A3WE 20040820001512004082000151NM 2004 8 20 UPS04242841 120040714A5755 PANEL BOEING727 72725C 138400HNM LT WING SPOILER DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, NR 5 SPOILER PANEL DISBOND (MINOR) LWR I/B SURFACE AT I/B CORNER FWD DOUBLER. ON INVESTIGATION FURTHER DISBOND FOUND ON UPPER SURFACE. SPOILER REPAIRED IAW SRM 51-40-20. NR 5 SPOILER PANEL ADJ/TEST CARRIED OUT PER MM 27-61-00/501 PARA 6H THROUGH 6M, 6O, 6P & Q. 2L73 4F A3WE 20040820001532004082000153NM 2004 8 20 UPS04242843 120040708A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON SKIN AT BS 253 S9L AFT OF NR 3 LT COCKPIT WINDOW CUTOUT. HFEC CARRIED OUT, CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW SRM 53-30-3 FIGURE 29. 2L73 4F A3WE 20040820001542004082000154NM 2004 8 20 UPS04242844 120040708A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, SUSPECT CRACK ON FWD RADIUS OF WING ANTI-ICE SCANNING LIGHT ON LT SIDE AT BS 680-700 APPROX & BETWEEN STR 14-15 LT. HFEC CARRIED OUT AND CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT IAW AAAE EO 2004-068-001R1. 2L73 4F A3WE 20040820001582004082000158NM 2004 8 20 UPS04242737 120040628A5754 WEB BOEING727 72725C 138400HNM NR 6 KRUGER FLAPCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, NR 6 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX L + R WEB CRACKED. REMOVED NR 6 KRUEGER FLAP ACTUATOR IAW MM 27-81-22. REMOVED BOTH CRACKED WEBS FOR FABRICATION IAW SRM 51-30-02. FABRICATED LT & RT WEBS AS PER DRAWING 65-16275. INSTALLED FABRICATED LT & RT WEBS IAW SRM 51-30-02 AND DRAWING 65-16275. 2L73 4F A3WE 20040820001612004082000161NM 2004 8 20 UPS04242759 120040625A5340 ANGLE BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON ANGLE ON O/B SIDE OF LOWER LEG OF BS 870 FITTING IN LT MWW. CRACK FOUND IN ANGLE, ANGLE REMOVED IAW SRM 51-30-2. NEW ANGLE FABRICATED AND FITTED IAW SRM 51-20-1, SRM 51-30-2 AND DRG 65-16330. 2L73 4F A3WE 20040820001632004082000163NM 2004 8 20 UPS04442825 120040710A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 200 LT FRAME WEB FOUND CRACKED BETWEEN 13A & STR 14A. BS 200 LT FRAME WEB CRACKED AREA REPAIRED AS PER RS R53-12-35175 FIG 3 AND EO B747-5310-20791-A. 2L74 4F RTA20WE 20040820001642004082000164NM 2004 8 20 UPS04442826 120040709A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, LT BS 340 WL 300 UPPER DECK FLOORBEAM FOUND 1 FASTENER HOLE CRACKED AT FRAME WEB. LT BS 340 UPPER DECK FLOORBEAM AREA FRAME WEB CRACK REPAIRED AS PER RS R53-12-35177 AND EO B747-5310-20786-A. 2L74 4F RTA20WE 20040820001662004082000166NM 2004 8 20 UPS04442828 120040712A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 460 RT FRAME WEB FOUND CRACKED AT STR -R14. BS 460 RIGHT FRAME WEB DOUBLER AT STR 14R CRACKED AREA REPAIRED AS PER RS R53-12-35179 AND EO B747-5310-20787-A. 2L74 4F RTA20WE 20040820001672004082000167EU 2004 8 20 AWXA200400853 120040807A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28648AW 770 DURING 8-DAY CHECK THE EMERGENCY LIGHT SYSTEM TEST FAILED FOR RT OVERWING BATTERY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820001682004082000168NM 2004 8 20 AWXA200400855 120040808A3350321454 EPSU AIRBUSA319 A319132 3930340NM ZONE 263 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28823AW386444934 1463 ATL - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14, 18, 22 LT, AND AFT GALLEY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY POWER SUPPLY UNIT (13WL), AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820001712004082000171NM 2004 8 20 AWXA200400858 120040624A5330141N3311 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK 3 EACH CRACKS WERE FOUND EMANATING FROM FASTENER HOLES IN FUSELAGE SKIN AT FORWARD UPPER CORNER OF L-1 DOOR CUTOUT BS 345, STR 9 LT, WL 285. MAINTENANCE CUT OUT CRACKED SECTION OF SKIN AT FORWARD UPPER CORNER OF L-1 DOOR CUTOUT; FABRICATED 2 EACH FILLERS, A DOUBLER, TRIPLER, & QUADRUPLER; INSTALLED REPAIR PARTS IAW AWA ER 19-5312-04203-ES1. 2L72 4F RTA2NM 20040820001732004082000173NM 2004 8 20 SWAA042365 120040816A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 942, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040820001742004082000174NM 2004 8 20 SWAA042366 120040816A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29473WN 33832 DURING SPV, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM. 2L72 4F RTA16WE 20040820001752004082000175 2004 8 20 SWAA042367 420040817A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040820001762004082000176 2004 8 20 SWAA042368 420040817A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040820001792004082000179NM 2004 8 20 SWAA042371 120040817A57536546430129 SKIN BOEING737 7373H4 1384600NM LT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD FOREFLAP PER MM. 2L72 4F RTA16WE 20040820001812004082000181NM 2004 8 20 DL777040771 120040816A3350D71702001 POWER SUPPLY BOEING777 777232 1385232NM EMERGENCY LIGHTCINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27862DA 29734 SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 45-56 ARE NOT TESTING. REPLACED POWER SUPPLY. 2L72 4F RTT00001SE 20040820001822004082000182NM 2004 8 20 SWAA042373 120040817A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29448WN 33721 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040820001852004082000185NM 2004 8 20 DL73S040747 120040806A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08 -15 REVEALED A SINGLE CRACKED FASTENER HOLE AT FS 400. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND PER ER/A 092151-14AD. 2L72 4F RTA16WE 20040820001872004082000187NM 2004 8 20 DLM88040749 120040808A5313 STRINGER DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27914DL 49545 CRACK IN NR 3 LT STRINGER AT JOINT WITH STA 160, CRACK IN NR 4 LT STRINGER AT JOINT WITH STA 160. 2L72 4F RTA6WE 20040820001882004082000188NM 2004 8 20 DL76L040750 120040809A3233 ACTUATOR BOEING767 767332 1382001NM MLG INOPERATIVE A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO27178DN 25143 AIR/GND DISAGREE STATUS MSG AND ICE DETECTOR FAULT ILLUM ON LIFT OFF. REPLACED RT TRUCK TILT ACTUATOR. 2L72 4F RTA1NM 20040820001922004082000192NM 2004 8 20 DL757040774 120040817A2133 OUTFLOW VALVE BOEING757 757232 1384965NM CABIN PRESSURE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27664DN 25012 CLIMBING THRU 20K LT PACK OFF LT ILLUM. RAN PACK OFF CKLIST STATUS MSG AUTO 1 INOP FOLLOWED BY RED CABIN ALT LT AND EICAS AUTO 2 INOP. EMERGENCY DESCENT TO 10K AND CABIN AUTO INOP. CHECKLIST COMPLETE. OUTFLOW VLV OBSERVED CLOSED. LT PACK TURNED ON APPEARED NORMAL. LANDED WITH PRESS IN MANUAL. T/S PER FIM, PRESS A/C WITH ENGS AT PWR. REPLACED FLOW CONTROL VLV PER MM BORROWED FROM UAL. RT PACK CHECKS OK. CLEARED AUTO 1 INOP MSG. REPLACED NR 2 PRESS CONT PER MM AS PRECAUTION. 2L72 4F RTA2NM 20040820001932004082000193NM 2004 8 20 SWAA042374 120040817A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040820001942004082000194 2004 8 20 DL76G040753 420040810A3440066500080405 TRANSCEIVER BOEING767 767332 1382001NM WX RADAR SYS INOPERATIVE A DALAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SO271609 30574 WX RADAR INOP. REPLACED WX RADAR XCVR AND INDICATOR. OPS CHECK OK. 2L72 4F RTA1NM 20040820001962004082000196NM 2004 8 20 AALA20040797 120040617A5311 FRAME BOEING767 767323 1385205NM TAIL CUT A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 AFW - WHILE ACCOMPLISHING C1945CB STEP E 3 CHORD WAS CUT AT 0.30 INCH FROM UPPER FASTENER OF REMAINING CHORD NOT 0.46 INCH AS ECO INSTRUCTS. AREA IS 1 INCH BY 1 INCH AT A DEPTH OF 1.3 INCHES. FILLED GAP WITH BMS5 95 SEALANT AND COMPLETED REPAIR PER ECO C1945 INSTRUCTIONS. 2L72 4F RTA1NM 20040820001992004082000199NM 2004 8 20 AALA20040795 120040725A3411 PITOT TUBE BOEING757 757223 1384957NM FUSELAGE MISSING A AALAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 SW21672AA 25337 ORD - INFLIGHT T725/25 AT INTERMEDIATE LEVEL OFF AT FL280 RIGHT ENGINE BEGAN TO SURGE BETWEEN 1.53 AND 1.66 EPR 91.5 TO 94.0 PERCENT N1 AT 670 TO 700C. EGT AND 87 TO 89 PERCENT SURGING CONTINUED AFTER AUTOTHROTTLE DISCONNECTED. NO THROTTLE MOVEMENT NOTED. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND RIGHT HAND ENGINE LEFT HAND MANIFOLD PF RAKE PITOT HEAD BROKEN OFF. ACCOMPLISHED TEMPORARY REPAIR PER MM AND NOTIFIED TECH SERVICES. MIA INSTALLED RAKE PITOT HEAD ON RIGHT HAND ENGINE LEFT HAND MANIFOLD PER AARD 72 34 13 2 WITHIN 50 FLIGHT HOURS AS INSTRUCTED PER TECH SERVICES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040820002002004082000200WP 2004 8 20 AALA20040802 120040802A1420 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21432AA 49350 ORD - CEILING EMERGENCY LIGHT AT ROWS 18 TO 21 INOPERATIVE. TIGHTENED LOOSE CONNECTOR ON BATTERY PACK FOR CEILING EMERGENCY LIGHT AT ROWS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040823000022004082300002 2004 8 23 SWAA042375 420040818A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040823000062004082300006NM 2004 8 23 SWAA042379 120040818A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C4 CHECK, FOUND LOWER RT KEEL BEAM CHORD AT BS 500A, STRINGER 28R, CORRODED. REPAIRED KEEL BEAM PER EA. 2L72 4F RTA16WE 20040823000082004082300008NM 2004 8 23 SWAA042381 120040818A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP AT BS 663, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM. 2L72 4F RTA16WE 20040823000112004082300011NM 2004 8 23 SWAA042384 120040818A53116546558 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040823000132004082300013NM 2004 8 23 QXEA200400627 120040817A3230 LANDING GEAR BOMBDRDHC8 DHC8401 1390041NM MAINS MALFUNCTIONED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09417QX 4086 FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE RVDT'S OUT OF RIG. THE RVDT'S WERE RIGGED AND THE OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040823000162004082300016NM 2004 8 23 QXEA200400589 120040815A323382910016005 ACTUATOR DHAV DHC8 DHC8202 2809007NM NLG BYPASSING A QXEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 NM09368PH216558918 512 SUP - YVR - FLIGHT 2276 - THE CREW ABORTED THE APPROACH WHEN AFTER SELECTING THE GEAR DOWN, THE NOSE LANDING GEAR DID NOT EXTEND. THE CHECKLIST WAS FOLLOWED AND THE GEAR WAS LOWERED USING THE ALTERNATE METHOD. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR ACTUATOR BYPASSING FLUID. THE ACTUATOR WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040823000182004082300018EA 2004 8 23 QXEA200400544 120040720A3260 SENSOR CNDAIRCL600 CL6002C10 1390015EA ZONE 700 OUT OF ADJUST A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09605QX6226 10022 DEN - FLIGHT 4167 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF, THE CREW RECEIVED A PROX SYSTEM FAULT 1 INCH STATUS MESSAGE ACCOMPANIED BY GEAR AND FLAP INDICATIONS FAILING TO DISAPPEAR AFTER CLEANUP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR WEIGHT OFF WHEELS NR 2 PROXIMITY SENSOR UNREASONABLY FAR. THE SENSOR WAS ADJUSTED AND THE OPERATONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040823000192004082300019NM 2004 8 23 QXEA200400552 120040720A5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING ON FLOORBOARD SUPPORT FLANGE AT APPROXIMATELY AT STATION 232. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20040823000242004082300024NM 2004 8 23 QXEA200400557 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X233 AND X235. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040823000262004082300026NM 2004 8 23 HNAA0400113 120040816A215078279010 ACM DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE AIR CON FAULTY A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07814EX195021611 318 FLIGHT NR 3785 ENROUTE, REPORTED THE DUCT TEMPERATURE WOULD NOT GO BELOW 55 DEGREES. DURING GROUND OPERATION THE TEMPERATURE WOULD NOT GO BELOW 70 DEGREES WITH ASSOCIATED SMOKE IN THE CABIN. MAINTNENANCE TROUBLESHOT SYSTEM AND FOUND THE ACM TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. 2H72 4T4 TRTA13NM E20NE 20040823000272004082300027EA 2004 8 23 QXEA200400623 120040807A5410 PAN CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 RT PYLON PRESSURE PAN CRACKED AT AFT HYDRO, FITTING. REMOVED RT PYLON PRESSURE PAN. DRILLED UP AND INSTALLED INTERNAL DOUBLER IN NEW PAN. INSTALLED NEW PAN AND COMPLETED INSTALLATION AT FASTENERS THROUGH NEW PAN IAW SRM 51-42-06. 2L72 4F4 FRTA21EA EOOO63EN 20040823000282004082300028NM 2004 8 23 QXEA200400598 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 TRACK NR 2 HAS LITE CORROSION AT X 404. BLENDED LITE CORROSION, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1, AREA 1.5 INCH LONG, .5 INCH WIDTH, .004 INCH DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2H72 4T4 TRTA13NM E00062EN 20040823000322004082300032EA 2004 8 23 COMA0460463 120040812A2611 DETECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE CARGO SMOKE MALFUNCTIONED A COMAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01785CA 7326 FLIGHT 5731, CARGO SMOKE WARNING. COULD NOT DUPLICATE. FOUND NO DEFECTS, REPLACED DISCHARGED FIRE BOTTLES 2L72 4F4 FRTA21EA E15NE 20040823000392004082300039WP 2004 8 23 ABXA040285 120040803A5313591140513 LONGERON DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 LONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02. 2L72 4F4 F A6WE E2EA 20040823000412004082300041WP 2004 8 23 ABXA040282 120040802A5330591142351 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 BULGE IN FUSELAGE SKIN AT CABIN OUTFLOW NOZZLE. REPLACED SECTION OF LONGERON FROM APPROXIMATELY STA. 955-990 IAW SRM. 2L72 4F4 F A6WE E2EA 20040823000422004082300042WP 2004 8 23 ABXA040283 120040803A533059114013 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001. 2L72 4F4 F A6WE E2EA 20040823000472004082300047SO 2004 8 23 C2XA04IA087 120040718A335020131A BATTERY PACK EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713969 145141 PILOT REPORTED THAT THE EMERGENCY LIGHTING DID NOT WORK WHEN TESTED DURING PREFLIGHT INSPECTION. THE ENGINES WERE RUN TO RECHARGE THE BATTERY PACKS AND AN OPERATIONAL CHECK OF THE LIGHTING SYSTEM WAS ACCOMPLISHED. THE EMERGENCY LIGHTS TESTED GOOD AND THE DISCREPANCY WAS CLEARED. 2L72 4F4 FRTT00011ATTE6CH 20040823000522004082300052SO 2004 8 23 C2XA04IA101 120040812A335066367 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715910 145455 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT A PORTION OF AISLE PATH LIGHTING NEAR THE EXIT ROW WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040823000542004082300054SO 2004 8 23 C2XA04IA088 120040720A33507287580507 LIGHT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 DURING PREFLIGHT INSPECTION THE CREW FOUND THE EMERGENCY LIGHT STRIP AT ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING AND CLEARED THE DISCREPANCY. 2L72 4F4 FRTT00011ATTE6CH 20040823000582004082300058 2004 8 23 ARWA20040801 420040815A344220671570157 TRANSCEIVER DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE WX RADAR SYS FAILED A ARWAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO19441J 45988 CLIMBING WEATHER RADAR DOES NOT PAINT WEATHER; AIRCRAFT RETURNED. REMOVED AND REPLACED WEATHER RT AND ANTENNA IAW MM 34-41-0 AND 34-41-1 GROUND TEST NORMAL. 2L74 4F4 F 4A25 1E8 20040823000602004082300060WP 2004 8 23 AALA20040854 120040817A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21245AA 49257 EMERGENCY LIGHTS AT SEAT 8 AB AND AFT GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT SEAT 8 AB AND AFT GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040823000612004082300061WP 2004 8 23 AALAA20040855 120040817A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217509 49803 EMERGENCY CEILING AISLE LIGHTS AT SEATS 23D AND 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING AISLE LIGHTS AT SEATS 23D AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040823000642004082300064EU 2004 8 23 AALA20040842 120040813A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217055A 462 BOS EMERGENCY LIGHTS AT FIRST CLASS RIGHT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS RT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA35EU E13NE 20040823000652004082300065WP 2004 8 23 AALA20040846 120040813A4990 O-RING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE APU OIL SYS LEAKING A AALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21276AA 49273 INFLIGHT T313/13, FLIGHT ATTENDANTS SMELLED AND SAW SMOKE IN CABIN. FIRST OFFICER REPORTED ODOR LIKE BURNING CLOTHING. RETURNED AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT IAW MCM CARD 21 92 12 AND ACCOMPLISHED WORK CARD 21 96 01. FOUND APU LOW ON OIL AND LEAKING. REPLACED O-RING ON OIL TANK DRAIN. NO FURTHER LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040823000672004082300067NM 2004 8 23 AALA20040844 120040813A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 EMERGENCY LIGHTS AT ROWS 30 THROUGH 43 INOPERATIVE. REPLACED BATTERY PACK ABOVE 3R ENTRY DOOR FOR EMERGENCY LIGHTS AT ROWS 30 THROUGH 43. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTT00001SEE00050EN 20040823000732004082300073CE 2004 8 23 DJFA2004019 120040811A7500 SEAL CESSNA650 650 2076802CE GARRTTTPE731TFE7313C WP BLEED AIR SYS LEAKING E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23311CW 6500011 DURING CLIMB THE NR 1 ENGINE FIRE LIGHT CAME ON. THE CREW RETARDED THE THROTTLES AND THE LIGHT WENT OUT. THEY RETURNED TO THE DEPARTURE AIRPORT WITH NO PROBLEMS. THE FIRE LIGHT WAS CAUSED BY A BLEED AIR LEAK. THE SEALS WERE CHANGED AND GROUND RUNS WERE SATISFACTORY. 2L72 4F4 F A9NM E6WE 20040823000762004082300076 2004 8 23 WLDA200459 420040813A3414HG280D5 CADC DOUG DC10 DC1030 3023501WP GE CF6 CF645A2 30020NE AIRSPEED IND INOPERATIVE A WRLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO1114075 46922 ITEM: RCH725/13 NGU/NAP REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPT'S INDICATOR, F/O'S INDICATED OK. RTO AT 105KTS. REMOVED AND REPLACED CADC, PERFORMED PITOT STATIC CHECK, FOUND ALL NORMAL. REMOVED AND REPLACED PITOT STATIC TUBE PRECAUTIONARY. PRESSURE CHECK ALL NORMAL. 2L73 4F4 F A22WE E23EA 20040823000782004082300078EA 2004 8 23 COMA0460466 120040817A27508575D100401 COUPLING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS BROKEN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5087 FLAPS FAIL MESSAGE. REPLACED BROKEN NR 4 FLEX DRIVE CABLE. 2L72 4F4 FRTA21EA E15NE 20040823000822004082300082 2004 8 23 WLDA200489 420040816A22104059001908 COMPUTER DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 1 INOPERATIVE A WRLAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO11275WA 48631 UNCOMMANDED ELEV MOVEMENT. CONSIDERABLE CONTROL COLUMN PULL FORCE REQUIRED DURING INITIAL ROTATION TO ATTAIN REQUIRED T/O CLIMBOUT PITCH ATTITUDE UNTIL 500-800 FT AGL. AFTER FLAP RETRACTION, FORCE REQUIRED RETURNED TO NORMAL, CNTRL COLUMN OSCILLATED(TWICE) BETWEEN FLAP RETRACT, SLAT RETRACT SPEED. AFTER SLAT RETRACTION RECD (MISC) NO AUTOLAND ALERT, CNTRL FORCES RETURNED TO NORMAL. DURING MANUALLY FLOWN DESCENT, APPROACH, CNTRL OSCILLATED, CREATED UNCOMMANDED NOSE DOWN MVMT WHEN STABLE ON FINAL.(ELEV FORCES HEAVIER THAN NORMAL DURING TAXI PRE-T/O CNTRL CHECK, SAME AFTER LANDING). REMOVED, REPLACED FCC1, CURRENT FAULT SHOWS ELEV LOAD FEEL ACTUATOR FAIL. PLACARDED ELEV LOAD FEEL SYS 1 CHANNEL INOP. 2L73 4F4 FRTA22WE E24NE 20040823000852004082300085NE 2004 8 23 HXS2004F2004B 220040705A7230 COMPRESSOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FOD E HXSAK NONE O OTHER ININSP/MAINT 1 AL05301TH 9022 ENGINE WAS BEING INSPECTED AT THE 100 HOUR INSPECTION INTERVAL AND THE MECHANICS FOUND THAT THE ENGINE HAD BEEN DAMAGED AT THE INLET COMPRESSOR BY FOD. ENGINE WAS REMOVED FROM SERVICE AND SENT FOR EVALUATION AND REPAIR. 1G71 3U3 U H9EU E19EU 20040823000882004082300088 2004 8 23 COMA0460459 420040813A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE AVIONICS MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01979CA8271 4966 7159 FLIGHT 5391 AHRS FAILURE DURING TAKEOFF. REPLACED THE NR 1 AHRS. 2L72 4F4 FRTA21EA E15NE 20040823000902004082300090EU 2004 8 23 AWXA200400827 120040710A5542D5547100000251 SKIN AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE RUDDER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 DURING B-04 CHECK AN AREA OF DELAMINATION WAS FOUND 3 INCHES FROM TOP OF RUDDER ON LT SIDE PANEL. MAINTENANCE CUTOUT DELAMINATED PLIES ON LT UPPER RUDDER AT FIN STA. 569; FABRICATED, AND BONDED CORE AND REPAIR PLIES TO RUDDER IAW A320 SRM 55-41-00, FIG. 217. 2L72 4F4 FRTA28NM E311NE 20040823000982004082300098EA 2004 8 23 04199642 120040717A3251 STEERING SYS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG INTERMITTENT A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27642BR ABORTED TAKE OFF DUE TO NOSEWHEEL STEERING FAILURE. PASSENGERS DEPLANED AT GATE. OP CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040823001012004082300101EU 2004 8 23 HAEA150 120040627A3244501110504 TIRE AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE MLG BLEW OUT E HAEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW05221TW 221 AIRCRAFT RT IB MAIN TIRE BLEW OUT ON TAKEOFF. AIRCRAFT DIVERTED. AIRCRAFT LANDED, NO INCIDENT. 2L72 4F4 F A7EU E7EA 20040823001022004082300102 2004 8 23 AWXA200400690 420040627A2565101659105 SLIDE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE L2 DOOR UNSAFETIED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW6302 22655 DURING PRE-FLIGHT PREPARATION, INFLIGHT NOTICED L-2 DOOR SLIDE HAD AN UNUSUAL INSTALLATION. UPON FURTHER EVALUATION OF THE SITUATION, MAINTENANCE DETERMINED THAT THE DOOR SLIDE WAS NOT PROPERLY CONNECTED AND THE PIN HOLDING THE GIRT BAR ASSY TO THE SLIDE HAD BECOME DETACHED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE. 2L72 4F4 FRTA16WE E2EA 20040819001262004081900126NM 2004 8 19 AWXA200400899 120040730A53136545767 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 RT AT BS 500C+5. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER 16 RT AT BS 500C+5; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, AND A STRINGER SPLICE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03 FIG 201. 2L72 4F RTA16WE 20040819001282004081900128NM 2004 8 19 AALA20040833 120040809A3350D72702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21920AN 29521 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1674 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001302004081900130NM 2004 8 19 AALA20040828 120040804A3350D71701100 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21902AN 29504 TUL - RIGHT HAND EMERGENCY EXIT LIGHT BATTERY PACK FAILED 15 MINUTE TEST PER CARD 2311. REPLACED BATTERY PACK FOR RIGHT HAND EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001322004081900132NM 2004 8 19 AALA20040827 120040808A5330 SKIN BOEING737 737823 13844BZNM FUSLEAGE DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21914AN 29515 TUL - SKIN DAMAGE AND CHORD DAMAGE ON RIGHT HAND FUSELAGE AT COCKPIT IN AREA 32 INCH BY 16 INCH. SKIN DAMAGE IN THREE AREAS. REMOVAL CUTOUTS ARE FIVE AND ONE HALF INCH BY THREE INCH, FOUR AND THREE FOURTH INCH BY 2 INCH AND NINE INCHS BY SEVEN AND ONE HALF INCHS. CHORD ANGLE DAMAGE IN ONE AREA REMOVAL CUTOUT ONE AND THREE FOURTH INCH BY SEVEN EIGHTS INCH. CUT OUT DAMAGED SKIN AND INSTALLED 0.063 T2024T3 DOUBLER. CUT OUT DAMAGED CHORD ANGLE AND REPAIRED PER ESO 61000 DATED 6 AUGUST 2004. 2L72 4F RTA16WE 20040819001342004081900134NM 2004 8 19 AALA20040831 120040809A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21920AN 29521 TUL - BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1695 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001362004081900136NM 2004 8 19 AALA20040832 120040809A3350D17102001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21920AN 29521 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACKS AT M1694 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001382004081900138NM 2004 8 19 AALA20040835 120040811A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21921AN 29522 BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 967 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040819001452004081900145 2004 8 19 SWAA042328 420040813A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29473WN 33832 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040819001472004081900147NM 2004 8 19 SWAA042330 120040813A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29379SW 26586 DURING SCHEDULED C1 CHECK, FOUND EEPLS COVER AT ROW 11 ABC, MISSING. REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040819001492004081900149 2004 8 19 SWAA042332 420040813A2565D31354 SLIDE BOEING737 7373T5 1384608NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040819001512004081900151NM 2004 8 19 SWAA042339 120040814A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 24L STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040819001532004081900153NM 2004 8 19 SWAA042341 120040815A33501000679 LIGHT BOEING737 7372H4 138448CNM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT FLICKERS. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040819001552004081900155NM 2004 8 19 SWAA042343 120040814A5310BAC1514 ANGLE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND L-ANGLES AT BS 293, RBL 67, WL 253, BS 348.2, LBL 68, WL 223, CRACKED. REMOVED AND REPLACED L-ANGLES PER SRM. 2L72 4F RTA16WE 20040819001572004081900157NM 2004 8 19 SWAA042345 120040815A533065C37790 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 860, STRINGER 1, WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040819001592004081900159NM 2004 8 19 AWXA200400863 120040728A575165C259112SP SKIN BOEING737 7373S3 1384711NM AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF RT AILERON WAS FOUND DELAMINATED AT WBL 480.5. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF RT AILERON AT WBL 480.5; CLEANED AND PREPARED AREA; FABRICATED NEW REPAIR PLIES; BONDED REPAIR PLIES TO AILERON IAW B737-300 SRM 51-70-04 FIG 14. 2L72 4F RTA16WE 20040819001612004081900161NM 2004 8 19 AWXA200400865 120040727A53206546812170 FLOOR SUPPORT BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN BS 954 AND BS 966, RBL 18, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 945 TO BS 966, RBL 18, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12-13. 2L72 4F RTA16WE 20040819001652004081900165EU 2004 8 19 MALA040514 120040807A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15535XJ E2371 DURING C-CHECK IN LCQ, NR 3 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESABA EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2H74 4F RTA49EU 20040819001702004081900170EU 2004 8 19 MALA040513 120040807A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15535XJ E2371 DURING C-CHECK IN LCQ, NR 1 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESABA EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2H74 4F RTA49EU 20040819001722004081900172EU 2004 8 19 MALA040520 120040811A7603251561 CONTROL CABLE BAC 146 AVRO146RJ85A1500097EU NR 2 ENGINE LOOSE A MALAE ENGINE SHUTDOWN P NO WARNING INDICATION DEDESCENT 1 GL15513XJ E2329 ON DESCENT NR 2 POWER LEVER FROZE IN POSITION N1 94 PERCENT HARD TO SHUT ENGINE DOWN ON APPROACH THE POWER LEVER CAME LOOSE AND WAS POS TO FUEL OFF ENGINE WINDMILLED APPROX 15 MIN AT 7/5 PERCENT N2. MAINTENANCE REPLACED NR 2 ENGINE CONTROL CABLE (P/N 251561), ALL CHECKS GOOD IAW AMM 76-11-17 DOWNLOAD SHOWS NO ENGINE PARAMETERS WHERE EXCEEDED DURING WINDMILLING IAW AMM 72-00-00 601 CONFIG 1. 2H74 4F RTA49EU 20040820000042004082000004NM 2004 8 20 SWAA042352 120040815A53306542765 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 525, STR 10R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040820000082004082000008 2004 8 20 SWAA042356 420040816A256563550101 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 R1 DOOR EVAC SLIDE WOULD NOT SLIDE INTO BRACKET. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040820000162004082000016EU 2004 8 20 MALA040526 120040729A5610 SCREW SAAB SF340 340B 7860101EU SIDE WINDOW BROKEN A MALAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL15435XJ 340B435 NOTED SCREWS BROKEN OUT ON F/O'S SIDE WINDOW. MAINTENANCE RETORQUED F/O'S SIDE WINDOW 56-10-05-04 NOTED 8 SCREWS BELOW TORQUE SIDE WIND. ON ATTACH SCREWS TORQUE CHECK GOOD AFTER RETORQUE. 2L72 4T RTA52EU 20040820000212004082000021EU 2004 8 20 MALA040524 120040803A2760HC921H0450004 PCB BAC 146 AVRO146RJ85A1500097EU AIRBRAKE MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15514XJ E2330 AIRBRAKE DEPLOYED/CONFIG WARNING. RETURNED TO GATE. AIRBRAKE RE-DEFERRED USING ORIGNAL DAY OF DISCOVERY. ON DESCENT INTO DTW AIRBRAKE DID NOT WORK. MAINTENANCE REPLACED PCB FROM LOG PAGE 1278197, REPLACED AIRBRAKE MON PCB IAW AMM 31-09-11, PERFORMED OPS CHECK IAW AMM 27-63-11, ALL CHECKS GOOD P/N HC921H0450-004. REMOVED FROM DMR, MXC NOTIFIED. 2H74 4F RTA49EU 20040820000302004082000030NM 2004 8 20 AWXA200400790 120040620A575465C26603 SKIN BOEING737 7373S3 1384711NM SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN LEFT L/E SLAT JUST OUTBOARD OF ENGINE PYLON, STAB STA 55.75. MAINTENANCE CUT OUT CRACK IN LEFT L/E SLAT AT STAB STA 55.75; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01-2 FIG 206. 2L72 4F RTA16WE 20040820000422004082000042WP 2004 8 20 ARWA20040509 120040519A5320 STRUCTURE DOUG DC8 DC863F 302198FWP SUBFLOOR CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 DURING AN A-CHECK INSPECTION THE FOLLOWING WAS FOUND; COCKPIT STA -12.000 SUBFLOOR WITH CORROSION, RBL 50. CLEANED UP CORROSION, TREATED AND PRIMED AREA IN ACCORDANCE WITH DC8 SRM 51-1-8. REPAIR COCKPIT BETWEEN STA 12 & RBL 49 SUBFLOOR WAS ACCOMPLISHED IAW AS ELEVEN INC DRAWING AS11566, SHEETS 1 THRU 4, DATED 0526/04 AND APPROVED BY FAA FORM 8110-3, DATED 05/26/04. 2L74 4F 4A25 20040820000462004082000046NM 2004 8 20 AWXA200400750 120040620A5320654587512 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER R-1 DOOR SILL UPPER WEB FRAME BETWEEN BS 299 & BS 326, RBL 63, WL 209. MAINTENANCE REMOVED CORRODED R-1 DOOR SILL UPPER WEB FRAME (ANGLE) FROM BS 299 & BS 326, RBL 63. FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45875; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3-4 & 6-8. 2L72 4F RTA16WE 20040820000602004082000060WP 2004 8 20 UPS04842901 120040722A57405644973502 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, NR 4 ALT BOOST PUMP BRACKET AND STRINGER 59 END FITTING AT XW 408 ARE CRACKED. REMOVED, FABRICATED AND REPLACED FITTING AND REPLACED BRACKET IAW DWG 3645611 AND 5644972 AND SRM 51-1-20D. 2L74 4F RT4A25 20040820000722004082000072NM 2004 8 20 UPS04242775 120040719A5312 BRACKET BOEING727 72725C 138400HNM BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, ON REMOVAL OF SECTION OF BULKHEAD AT BS 178, SUPPORT BRACKET FOR PNEUMATIC BOTTLE FOUND CRACKED. REMOVED SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-30-2. FABRICATED SUPPORT BRACKET IAW DRW60-6962 AND SRM 51-20-1 FIG 7, INSTALLED NEW FAB'D SUPPORT BRACKET FOR PNEUMATIC BRAKE BOTTLE IAW SRM 51-2 30-2. 2L73 4F A3WE 20040820000762004082000076NM 2004 8 20 UPS04442766 120040713A53117075000711N FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 400 LT FRAME I/B CHORD FOUND CRACKED BETWEEN STR 6 & STR 5. INBOARD CHORD REPLACED AS PER SRM 51-40-03 FIG 1. 2L74 4F RTA20WE 20040820000862004082000086EU 2004 8 20 AWXA200400783 120040712A5310D5347209001300 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 66 TO FR 68, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040820000872004082000087EU 2004 8 20 AWXA200400784 120040712A5310D5347218920000 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 68 TO FR 69, FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040820000902004082000090NM 2004 8 20 UPS04442771 120040713A5320 STIFFENER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, BS 400-420 LT STR - 9 LWR STIFFENER FOUND CRACKED. BS 400-420 LT STR 9 LOWER STIFFENER REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040820000922004082000092NM 2004 8 20 UPS04442773 120040713A5310 SHEAR TIE BOEING747 747200 1384847NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, COCKPIT - BS 340 LT FRAME TIE CLIP FOUND CRACKED AT STR 8. COCKPIT BS 340 LT FRAME STR 8 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040820000962004082000096NM 2004 8 20 AWXA200400813 120040723A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 13 LT STRIPPED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LEFT WAS LOOSE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820001062004082000106NM 2004 8 20 AWXA200400831 120040723A5310D5347209000200 BEAM AIRBUSA319 A319132 3930340NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RIGHT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 RIGHT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18. 2L72 4F RTA28NM 20040820001132004082000113NM 2004 8 20 04FDEA01849 120040624A5753ARC74903 TEE FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE FOUND WORN. LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE REAMED AS PER SRM 51-31-01 VOL 2, ORIGINAL DIAMETER=0.875 INCH, FINAL DIAMETER=0.895 INCH, REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78019, TITLE: WINGS - TRAILING EDGE FLAPS - LEFT HAND INBOARD FLAP VANE OUTBOARD (NR 1) TEE FITTING AFT HORIZONTAL BORE WEAR - REPAIR. 2L73 4F RTA22WE 20040820001222004082000122NM 2004 8 20 SWAA042358 120040816A57436937877 FITTING BOEING737 7373H4 1384600NM RT & LT MLG CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED SERVICE CHECK, FOUND RT AND LT MLG FWD OUTBOARD HANGER FITTINGS CORRODED. REMOVED AND REPLACED MLG FITTINGS PER EA. 2L72 4F RTA16WE 20040820001262004082000126NM 2004 8 20 SWAA042362 120040816A53156545812 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, RBL 20 TO RBL 50, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040820001372004082000137NM 2004 8 20 AWXA200400883 120040813A335032145410 EPSU AIRBUSA319 A319132 3930340NM ZONE 221 FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28805AW18676 1049 PHX - EEL - DURING E-01 CHECK THE FORWARD LT EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED FORWARD LT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820001392004082000139 2004 8 20 AWXA200400885 420040814A2565P4010021 BATTERY BOEING737 7373U3 13844CCNM ZONE 900 - LAVATDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28335AW 28740 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820001482004082000148EU 2004 8 20 AWXA200400846 120040803A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU SEAT ROW 19 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28654AW 1050 PHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT WALL CONNECTION SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820001862004082000186NM 2004 8 20 DL73S040748 120040806A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 INSPECTION OF THE STRINGER 10L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACKED FASTENER HOLE AT FS 500A AND AT FS 500B. THE CRACKS WERE REMOVED WITH CUTOUTS AND REPAIRED SEPARATELY WITH ALUMINUM REPAIR DOUBLERS PER THE B737 SRM AND PER ER/A 092153-14AD. 2L72 4F RTA16WE 20040820001902004082000190NM 2004 8 20 AWXA200400661 120040619A5270 SENSOR BOEING757 7572S7 1384962NM AFT PAX DOOR OUT OF ADJUST A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28903AW 23323 PHX - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR BWI RECEIVED LT AFT ENTRY DOOR OPEN INDICATION, REJECTED TAKEOFF AT APPROXIMATELY 90 KTS. MAINTENANCE INSPECTED THE L-4 DOOR AND ISSUED MEL 52-71-11, COND 1 -LT AFT DOOR INDICATION SYSTEM INOP-. ON 06/21/04, IN SFO, MAINTENANCE ADJUSTED THE SENSOR ON LT AFT ENTRY DOOR IAW BMM 52-71-00-5, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040820001952004082000195NM 2004 8 20 AALA20040794 120040801A2612710128676393C SENSOR BOEING757 757223 1384957NM RROYCERB211 RB211535E43754555NE RT ENGINE MALFUNCTIONED A AALAO OTHER J WARNING INDICATION APAPPROACH 1 SW21602AN 27053 31422 ORD - INFLIGHT T2252/01 ON FINAL RIGHT ENGINE FIRE INDICATION SHUT ENGINE DOWN AND FIRED BOTH BOTTLES. REPLACED BOTH ENGINE FIRE BOTTLES AND SQUIBS PER MM 26 21 01 4 FOR RIGHT HAND ENGINE AND REPLACED NR 1 TS5031 FIRE LOOP AND REPLACED NUMBER TWO CARD M684. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20040823000042004082300004 2004 8 23 SWAA042377 420040818A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29433LV 33716 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040823000152004082300015EA 2004 8 23 QXEA200400562 120040723A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA FWD CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX7049 10024 PDX - ON INSPECTION OF THE FORWARD CARGO BAY, THE CHIMNEY WAS FOUND DAMAGED AND TORN. MAINTENANCE REPLACED THE FORWARD CARGO BAY CHIMNEY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040823000202004082300020NM 2004 8 23 QXEA200400551 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING ON THE SEAT TRACK FLOORBOARD SUPPORT FLANGE AT APPROXIMATELY STATION 238. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20040823000222004082300022NM 2004 8 23 QXEA200400555 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X213.5 AND X223.5. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040823000232004082300023NM 2004 8 23 QXEA200400556 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X229.5 AND X230. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040823000252004082300025NM 2004 8 23 QXEA200400558 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 7 HAS MARKED CORROSION ON UPPER SURFACE OF CENTER FLANGE AT X242. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040823000362004082300036WP 2004 8 23 ABXA040287 120040804A5230591014167 PAN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FWD CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT FASTENER HOLE AT UPPER FORWARD CORNER. REPLACED FORWARD LOWER CARGO DOOR ON N.R. 0399 IAW DC-9 SRM. 2L72 4F4 F A6WE E2EA 20040823000372004082300037WP 2004 8 23 ABXA040288 120040804A5230591014167 PAN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FWD CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM. 2L72 4F4 F A6WE E2EA 20040823000452004082300045WP 2004 8 23 ABXA040291 120040804A523059101413 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FWD CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM. 2L72 4F4 F A6WE E2EA 20040823000512004082300051SO 2004 8 23 C2XA04SH484 120040817A532014528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713914 145430 DURING C CHECK THE EXTERNAL TEE REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA PERFORMED A DOUBLER REPAIR IAW SRM 53-24-02 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040823000622004082300062NM 2004 8 23 AALA20040853 120040812A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21923AN 29524 EMERGENCY LIGHT BATTERY IN CABIN AT M1695 FAILED 15 MINUTE TEST. REPLACED BATTERY PACK IN CABIN AT M1695 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040823000752004082300075EA 2004 8 23 COMA0460468 120040817A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS INSTALLED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01798CA6196 7348 FLIGHT 5017 FLAPS FAIL MESSAGE. REPLACED RT BPSU. 2L72 4F4 FRTA21EA E15NE 20040823000772004082300077NM 2004 8 23 HNAA0400114 120040817A3231 LINKAGE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LT MLG DOOR DIRTY A HNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA07811EX 201 FLIGHT NR 3716 REPORTED HAVING THE LT MAIN GEAR DOOR ADVISORY LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. AFTER GO AROUND IT WAS VERIFIED THAT THE DOOR WAS OPEN WITH GEAR UP. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBED ASSOCIATED GEAR DOOR ACTUATOR AND LINKAGES. SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040823000862004082300086EA 2004 8 23 COMA0460457 120040811A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE EMERGENCY LIGHT INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01983CA 7169 FLIGHT 5682 OVERHEAD EMERGENCY LIGHT AT ROW 11 IS INOPERATIVE. DEFERRED MAINT IAW MEL. 2L72 4F4 FRTA21EA E15NE 20040823000912004082300091WP 2004 8 23 IXXA0400101O 120040804A2611100064901 SMOKE DETECTOR DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE CARGO BAY BROKEN A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11830BX7596345 45973 DURING ROUTINE TAKEOFF FROM MIAMI LOWER CARGO COMPT FIRE LIGHT ILLUMINATED. AFTER SHUTDOWN, MECHANIC DISPLAY SHOWED FALSE ALARM. FIRE DEPARTMENT VERIFIED NO HEAT IN (D) PIT. DOOR OPENED AND NOTHING FOUND. OVERWEIGHT INSPECTION REQUIRED. T/S SMOKE SYSTEM AND REPLACED 2EA SDU'S IN (D) PIT AND 1 EA IN (B) PIT. RECHARACTERIZED SYSTEM AND COMPLETE INOP. ACFT RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20040823000962004082300096NM 2004 8 23 DHL2004745502 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A (C) CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED;R/H FUSE HAS A DENT AT BS 480 BELOW STR 23R. DAMAGE OUT OF LIMITS IAW B727 SRM 53-30-1,FIG.1,CUT OUT DAMAGED AREA AND FABBED FILLER FROM 2024-T3 .050 P.O.900980 DIM. 1.8750 INCH X 1.7500 INCH AND DOUBLER FROM 2024-T3 .083 P.O.900790 DIM.10 INCHES X 7.5 INCH IAW B727 SRM 53-30-3 FIG.3, PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 53-30-3 FIG.3 2L73 4F4 F A3WE E2EA 20040823001032004082300103EU 2004 8 23 HAEA151 120040629A3231 ARM AMD FALC20FALCON 2720302EU GE CF700 CF700* 30010NE MLG BINDING E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05295TW18634 5 ON DEPARTURE, GEAR DOORS FAILED TO RETRACT AFTER GEAR RETRACTION. AIRCRAFT DIVERTED FOR MAINTENANCE. CLEANED AND LUBRICATED EXTENSION ARM, GEAR SWING. OPS CHECK GOOD. 2L72 4F4 F A7EU E7EA 20040823001062004082300106SO 2004 8 23 LR7A04069 120040716A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321 FOUND LMLG WHEEL WELL SKIN CRACKED AT FS 597, LBL 35, WL 130. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2036. 2H74 4T A1SO 20040823001082004082300108SO 2004 8 23 LR7A04071 120040716A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND LT SIDE FUSELAGE SKIN WITH NUMEROUS DEEP CUTTING MARKS, WARPED, AND SUNKEN RIVETS. FS 777E-817E, LBL 80, WL140 - 160. REPLACED SKIN LT FS 777E - 817E, WL 140 - 195 IAW SRM SMP 583 CHP 51-60 AND 51-70. DRC 2039. 2H74 4T4 T A1SO E282 20040823001102004082300110SO 2004 8 23 LR7A04073 120040716A532133051119 FLOOR PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5211, FOUND RAMP DOOR LT FLOOR PANEL WARPED AT FS 809. FLOOR PANEL REPLACED IAW SRM SMP 583, CHP 51-60 AND 51-70. DRC 2043. 2H74 4T4 T A1SO E282 20040823001112004082300111SO 2004 8 23 LR7A04074 120040716A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE DELAMINATED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321 FOUND 4 IN. X 10 IN. AREA OF HONEYCOMB PANEL DELAMINATED AT LT MLG WHEEL WELL FS 520 - 530, WL 200. AND LT MLG POD CENTER FAIRING FS 512 - 596, WL 180-200. SKIN PANEL REPLACED IAW LAC MEA 382-53-04-046. DRC 2054. 2H74 4T4 T A1SO E282 20040823001122004082300112SO 2004 8 23 LR7A04075 120040716A53403700311LR FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5321 FOUND NLG ATTACH FITTINGS WITH PITTING CORROSION. FS196, BL 5 L/R, WL146. FITTINGS REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2064. 2H74 4T4 T A1SO E282 20040823001132004082300113SO 2004 8 23 LR7A04076 120040716A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE DEFORMED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5321 FOUND RAMP DOOR REAR TE BOTTOM EXTERIOR SKIN DEFORMED/NICKED AT FS 857, RBL 50. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2073. 2H74 4T4 T A1SO E282 20040823001172004082300117NM 2004 8 23 QXEA200400573 120040801A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA AFT PAX INOPERATIVE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09413QX6234 4060 AFT PASSENGER DOOR WILL NOT OPEN OR CLOSE. MAINTENANCE INSPECTED THE DOOR AND RESEQUENCED SAME. NUMEROUS OPERATIONAL CHECKS WERE PERFORMED WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040823001182004082300118NM 2004 8 23 ASMF200407036 120040730A5330 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE FUSELAGE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23861LF 49826 DURING TRANSIT CHECK WAS DETECTED APU DIVERTER FLUID AND FUSELAGE SKIN WITH DAMAGES. FINAL REPAIR WAS PERFORMED ON LT SIDE OF FUSELAGE SKIN IAW SRM 53-04 AT Y-1272 STATION, BETWEEN LT 23 AND 25 LONGERONS. DIVERTER FLUID WAS REPLACED IAW SRM 51-30-0 AND 51-10-4 AT Y-1334 STATION BETWEEN LT 28 LONGERON AND RIGHT 29 LONGERON. RT MAIN LANDING GEAR SENSOR WAS REPLACED IAW MM 32-60-05, TEST CORRECT. NO PILOTS OR MAINTENANCE REPORTS WERE IN THE LOGBOOK. 2L72 4F4 FRT E2EA 20040823001192004082300119NM 2004 8 23 ASMF200408004 120040803A7711 TRANSMITTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE EPR MALFUNCTIONED W ASMFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW23168PL 53174 725379 AIRCRAFT REJECTED TAKE OFF AT 80 KNOTS AND RETURNED TO PLATFORM, HIGH TEMPERATURE OF EGT, REACHED 660 DEGREE (C) AND 1.57 OF EPR, ON LT ENGINE. ENGINE INLET AND OUTLET, CHIP DETECTOR AND MAIN OIL FILTER WERE CHECKED, BEING CORRECT. EPR TRANSMITTER WAS REPLACED IAW MM 77-11-00, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040823001202004082300120WP 2004 8 23 04FDEA02319 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AT APPROXIMATELY 1 O`CLOCK POSITION, 15 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, THE SKIN IS DIMPLED. REWORKED DENT IAW DC 10 SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED AREA IAW NDT MANUAL 20-20- 00, NO CRACKS FOUND, DENT WITHIN LIMITS IAW MD 10-10 MM 34-11-01-2. PERFORMED INSPECTION OF NOTED DISCREPANT AREA. MEASUREMENT IS .004, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. REF. N/R N00229 2L73 4F4 FRTA22WE E23EA 20040823001212004082300121EU 2004 8 23 YENA200441 120040723A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE COCKPIT DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15568JB 2063 PASSENGER OBSERVED BURNING RUBBER SMELL IN ROW 19 LT SIDE. ODOR WENT AWAY AFTER FEW MINUTES.COMPLIED WITH INFO NOTICE 2004-T023TR. NO ABNORMALITIES NOTED, COULD NOT CONFIRM THE BURNING SMELL. OK FOR SERVICE. 2L72 4F4 FRTA28NM E311NE 20040823001222004082300122 2004 8 23 YENA200442 420040730A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LIVE TV ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15516JB104663570 1302 PASSENGER IN ROW 19 COMPLAINED OF A UNUSUAL SMELL, TURNED OFF LIVE TV AND SMELL DISAPPEARED. PERFORMED LIVE TV SYSTEM FUNCTION CHECKS AND INTEGRITY INSPECTION OF ROW 17 THRU 21. NO EVIDENCE OF JAMMING OR ELECTRICAL ODOR. CHECK PERFORMED IAW JB INFO NOTICE 2004-T023TR. OPS CHECK NORMAL. REMOVED SEB'S AT 19B AND 19E FOR PRECAUTIONARY MEASURES. MONITORED SYSTEM FOR 4 HOURS STILL NO FAULTS. SEAT SEB 19E-P/N 3042865-102, S/N 10011, TOTAL 5177 H AND TSI 3500 H. SEAT SEB 19B-P/N 3042865-102, S/N 2086, TOTAL 10,466 H AND TSI 3570 H. 2L72 4F4 FRTA28NM E40NE 20040823001232004082300123NM 2004 8 23 AALA20040852 120040812A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21923AN 29524 BATTERY IN CABIN AT M1694 FAILED TO PASS 15 MINUTE TEST FOR EMERGENCY LIGHTING. REPLACED BATTERY PACK AT CABIN M1694 FOR EMERGENCY LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040823001242004082300124 2004 8 23 USAABB04071 420040720A2565 LANYARD BOEING757 7572B7 1384964NM R1 DOOR SLIDE OUT OF POSITION A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19630AU 27808 CLT - PILOT REPORTED THE R1 DOOR IS DIFFICULT TO ARM. MAINTENANCE FOUND THE LANYARD AROUND SLIDE GIRT BAR. REPOSITIONED LANYARD. DOOR ARMING CHECKS GOOD. (M) 2L72 4F RTA2NM 20040823001252004082300125NM 2004 8 23 USAASB04097 120040722A33503004321 LIGHT BOEING737 7374B7 1384702NM R1 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19440US 24811 ORD - MAINTENANCE FOUND THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY EXIT LIGHT/SOCKET ASSEMBLY AT THE R1 DOOR. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040823001262004082300126NM 2004 8 23 C7WA200400031 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSLAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 E/E COMPARTMENT STRINGER 26 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2L73 4F A3WE 20040823001272004082300127NM 2004 8 23 C7WA200400030 120040609A5311 FRAME BOEING727 727232 1384082NM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND FUSELAGE FRAME UPPER CHORD CORRODED BS 950E AT STRINGER 27 RT. INSTALLED FRAME REPAIR IAW 727 SRM 53-10-4 FIGURE 2. (M) 2L73 4F A3WE 20040823001282004082300128NM 2004 8 23 C7WA200400029 120040609A5313 STRINGER BOEING727 727232 1384082NM FUSLEAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND E/E COMPARTMENT STRINGER 28 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2L73 4F A3WE 20040823001292004082300129NM 2004 8 23 C7WA200400028 120040609A5714 SKIN BOEING727 727232 1384082NM CENTER WING CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND WING CENTER SECTION UPPER SKIN CORRODED FS 825.95 RBL 50. INSTALLED REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M) 2L73 4F A3WE 20040823001312004082300131 2004 8 23 USAABB04072 420040730A2565140N275411 LIFTER BOEING757 757225 1384959NM L4 DOOR SLIDE BROKEN A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19600AU 22192 CLT - THE L4 DOOR GIRT BAR WAS VERY LOOSE. MAINTENANCE REPLACED THE LIFTER ASSEMBLY. (M) 2L72 4F RTA2NM 20040823001332004082300133NM 2004 8 23 USAA040338 120040614A5313 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU60500 22203 CLT - FOUND STRINGER CORRODED 5 INCH AREA, STATION 1456-1461 STRINGER 29R. INSTALLED STRINGER SPLICE PER EA 95613. (M) 2L72 4F RTA2NM 20040823001342004082300134NM 2004 8 23 USAASB04096 120040722A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19443US 24842 MCO - MAINTENANCE FOUND THE FORWARD GALLEY SERVICE DOOR EMERGENCY LIGHTS AND SEVERAL MID-CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1132 AND M1479 BATTERY PACKS. OPS CHECKS GOOD. (M) 2L72 4F RTA16WE 20040823001362004082300136EU 2004 8 23 USAABA04016 120040725A3350321431 BATTERY AIRBUS330 A330323 3930335EU R3 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19675US 0370 PHL - THE R3 DOOR EPSU FAILED TEST. MAINTENANCE REPLACED THE BATTERY. (M) 2L72 4F RTA46NM 20040823001392004082300139EA 2004 8 23 ASOA04430 120040614A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11849AS 7347 FLT 4469 - DURING APPROACH INTO ATL FROM ROA, THE CREW NOTICED AN ODD ODOR WHEN THE PACKS WERE ON THE ENGINE BLEED AIR AT HIGHER POWER SETTINGS ONLY. IT APPEARED TO BE A FAINT OIL OR HOT PLASTIC ODOR WHICH OCCURRED INTERMITTENTLY DURING APPROACH. THE AIRCRAFT LANDED SAFELY IN ATL. THE SMELL WAS NOT NOTICED AFTER LANDING UPON SWITCHING TO THE AUXILIARY POWER UNIT BLEED AIR. MAINTENANCE COULD NOT DUPLICATE THE ODD SMELL ON THE GROUND USING THE AUXILIARY POWER UNIT BLEED AIR. ALL EICAS ENVIRONMENTAL CONTROL SYSTEM INDICATIONS WERE NORMAL. (M) 2L72 4F RTA21EA 20040823001412004082300141EU 2004 8 23 ASOA04446 120040621A33503011210 LIGHT AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11631AS 362 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LGIHT ASSEMBLY ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040823001422004082300142NM 2004 8 23 USAASB04098 120040722A3234 SELECTOR BOEING737 737401 1384701NM MLG MALFUNCTIONED A USAAO OTHER O OTHER CLCLIMB 1 EA19405US 23885 PHL - FLT 1215 - AFTER TAKEOFF FROM JAX, EN ROUTE TO PHL, THE LANDING GEAR SELECTOR HANDLE WOULD NOT MOVE ABOVE THE OFF POSITION. CREW WAITED ONE MINUTE AND SELECTED GEAR SELECTOR HANDLE TO THE UP POSITION WITH NO PROBLEM. GEAR RETRACTED NORMALLY. OVERRIDED SWITCH WAS NOT USED. FLIGHT CONTINUED ONTO PHL WHERE IT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED LANDING GEAR CONTROL SYSTEM ADJUSTMENT AND SYSTEM TEST PER MM 32-31-00. JACKED AIRCRAFT AND SWUNG GEAR NUMEROUS TIMES. ALL OPERATIONAL CHECKS WERE NORMAL WITH GEAR SELECTOR. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20040823001432004082300143NM 2004 8 23 USAASB04100 120040725A33503004321 LIGHT BOEING737 7374B7 1384702NM L1 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19447US 24874 ORD - MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR EXTERIOR EMERGENCY LGIHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY EXIT LIGHT/SOCKET ASSEMBLY AT THE FORWARD MAIN ENTRY DOOR. OPERATIONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20040823001462004082300146NM 2004 8 23 USAABB04059 120040623A3397 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHT LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19645US 23897 CDG - FOUND FLOOR EMERGENCY LIGHTS FROM ROW 9 TO ROW 17, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTION BETWEEN ROWS 9 AND 10 AND SECURED IT. (M) 2L72 4F RTA1NM 20040823001502004082300150NM 2004 8 23 USAA040356 120040721A53306548240503 SKIN BOEING737 7374B7 1384702NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND SKIN CHAFED .030 INCH DEEP TO .000 INCH EDGE/1.5 INCH BY 4 INCH, FS 1129 TO STATION 1138 ABOVE S12L. REMOVED AND REPLACED SKIN PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20040823001512004082300151NM 2004 8 23 USAASB04081 120040627A335020131A BATTERY PACK BOEING737 737301 1384611NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19586US 23931 PIT - FOUND DURING WEEKLY CHECK, MAINTENANCE FOUND THE INTERIOR EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 AND THE EXTERIOR LIGHTS AT RIGHT OVERWING EXIT AND LEFT AFT FUSELAGE, EXTINGUISH AFTER 10 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POSITION NR 5. OPERAITONAL CHECK NORMAL. (M) 2L72 4F RTA16WE 20040823001522004082300152NM 2004 8 23 USAASB04101 120040726A335020131A BATTERY PACK BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US 23984 MCO - MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040823001532004082300153NM 2004 8 23 USAA040353 120040721A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU52038 23380 PIT - FOUND FORWARD PRESS BULKHEAD CRACKED 1 INCH, STATION 178 RBL 10. REPAIRED UNDER EO 5300V153 AND ON A INSPECTION PROGRAM. (M) 2L72 4F RTA16WE 20040823001552004082300155EU 2004 8 23 USAASA04071 120040715A2120 ODOR AIRBUSA319 A319112 3930323EU CABIN DETECTED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19724UW 1122 ATL - FLT 739 - EN ROUTE LGA-MSY - WHILE IN CRUISE, THE FLIGHT ATTENDANTS REPORTED A SLIGHT HAZE AND SMOKE ODOR IN THE CABIN. THE FIRST OFFICER VERIFIED THE CONDITION. THE SMOKE CHECK LIST WAS PERFORMED. THE SMOKE WENT AWAY WHEN THE RIGHT PACK WAS SHUTDOWN. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE RIGHT PACK SYSTEM AND CONFIRMED SMOKE COMING FROM RIGHT PACK. PLACED RIGHT PACK ON MEL. AFTERWARDS, MAINTENANCE ACCOMPLISHED AN OPERATIONAL TEST OF THE COCKPIT AND CABIN TEMPERTURE CONTROL. OPERATIONALLY CHECKED OK. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040823001562004082300156EU 2004 8 23 USAABA04015 120040626A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19671UW 0323 PHL - FIVE EPSU BATTERIES FAILED THE CAPACITY CHECK. MAINTENANCE REPLACED THE BATTERIES AT THE L1, L2, L3 R2 AND R3 DOORS. (M) 2L72 4F RTA46NM 20040823001572004082300157NM 2004 8 23 USAASB04075 120040623A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19777AU 24979 BOS - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT BATTERY WAS LOW. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040823001582004082300158EA 2004 8 23 ASOA04529 120040726A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 DURNG A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IN THE CARGO COMPARTMENT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040823001642004082300164EU 2004 8 23 ASOA04526 120040725A5210S5217669521200 PIN AEROSPATR72 ATR72212 8680945EU LATCH MISALIGNED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11637AS 383 FLT 4297 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS VERY HARD TO OPEN. MAINTENANCE RE-ADJUSTED THE UPPER AFT LATCH PIN ONTHE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040823001652004082300165EA 2004 8 23 ASOA04528 120040725A3397YAD4F RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT SHORTED A ASOAO OTHER J WARNING INDICATION CRCRUISE 1 SO11708EV 10060 FLT 4500 - DURING CRUISE FROM CVG-DFW, WITH THE EMERGENCY LIGHTS SWITCH IN THE ARMED POSITION, THE EMERGENCY LIGHTS CAME ON INTERMITTENTLY ACCOMPANIED BY A WHITE 'EMERGENCY LIGHTS ON' STATUS MESSAGE WITH NO OTHER ABNORMAL INDICATIONS. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE AC ESSENTIAL BUS SENSE RELAY K135 IN JUNCTION BOX ELEVEN ON PRINTED CIRCUIT BOARD FIVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040823001662004082300166EA 2004 8 23 ASOA04525 120040723A493069254517 VALVE CNDAIRCL600 CL6002B19 1900309EA FUEL SOLENOID FAILED A ASOAO OTHER BP SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION DEDESCENT 1 SO11925EV 7831 FLT 4390 - DURING DESCENT INTO MSP FROM DFW, THE AUXILIARY POWER UNIT PERFORMED AN AUTOMATIC SHUTDOWN WITH NO WARNING MESSAGE, ACCOMPANIED BY A HEAVY FUEL ODOR UPON SHUTDOWN. THE AIRCRAFT LANDED SAFELY IN MSP. MAINTENANCE REMOVED AND REPLACED THE FUEL SOLENOID VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040823001682004082300168NM 2004 8 23 AMTA200400875 120040714A3350 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11526AT 30735 EGRESS LIGHTS OUT AT MID CABIN FLOOR. RECONNECT EGRESS LIGHT PER WDM 33-51-13. OPS CHECK GOOD AT THIS TIME PER 33-51-00-5. (M) 2L72 4F RTA2NM 20040823001722004082300172NM 2004 8 23 2004F00239 120040305A29101079718 LINE BOEING727 727225 1384077NM HYD SYSTEM LEAKING A MYWAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19802MA 22433 WHILE IN CRUISE FLIGHT FROM SUX SYSTEM 'A' HYD SHOWED A SLOW FLUID LOSS. ACCOMPLISHED ABNORMAL PROCEDURES THEN DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. FLUID QTY AND LANDING 2 GALLONS. FOND NR 1 ENGINE CASE DRAIN LINE IN SECITON 48 LEAKING. INSTALLED TEMPORARY FLEX LINE FROM SECTION 48 THROUGH TO RIGID LINE FROM FILTER MODULE IN SECTION 48. REPLACED CASE DRAIN FILTERS AS PRECAUTIONARY MEASURE. RAN NR 1 AND 2 ENGINES, MOVED ALL FLIGHT CONTROLS THROUGH FULL TRAVEL. LEAK AND OPERATIONAL CHECK NORMAL. ACCOMPLISHED PER MM 29-11-41, 29-10-00 AND 20-10-12. AIRCRAFT RETURNED TO REVENUE SERVICE IN ATL. (M) 2L73 4F A3WE 20040823001732004082300173NM 2004 8 23 UPS04242966 120040803A5280 WEB BOEING727 72722C 138400FNM RT MLG WING DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, RT MLG WING DOOR UPPER FWD WEB CRACKED AT AFT END REPAIR CARRIED OUT IAW SRM 51-30-02 & 51-40-3. 2L73 4F A3WE 20040823001762004082300176NM 2004 8 23 UPS04M42926 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, HORIZONTAL STAB RIGHT NR 31 BARREL NUT HOLE FOUND CORRODED ON BOTTOM BEARING & SIDEWALL SURFACE. CORROSION REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.070 INCH DEEP, FOUND OUT LIMITS PER EO MD11-5510-19409-G. FAB & REPAIR CUTOUT AS PER EO MD11-5510 -19409-G & EN1220-04. APPLIED SEALANT PR1422B2 AT BARREL NUT NR 31 RT. REPAIR & INSTALLED SLEEVE BUSHING AT BARREL NUT NR 31 RT AS PER EO MD11 -5510-19409-G & EN:1220-04 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040823001772004082300177NM 2004 8 23 UPS04M42927 120040611A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, RT HORIZONTAL STAB NR 29 BARREL NUT HOLE FOUND CORRODED CORROSION ON S/W & BEARING SURFACE REMOVED & REAMED FOUND OUT OF LIMIT PER EO MD11-5510-19409-G. FAB & REPAIR SLEEVE BUSHING PER EO MD11-5510- 19409-G. APPLIED SEALANT AT BARREL NUT HOLE NR 29 RT PER 1210-04. REPAIR & INSTALLED CUTOUT AT BARREL NUT HOLE 29 RT PER EO MD11-5510-19409-G & EN:1210-04 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040823001792004082300179NM 2004 8 23 UPS04M42929 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, HORIZONTAL STAB NR 12 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & S/W SURFACE POSITION RIGHT. B/N HOLE AT NR 12 RIGHT, REAMED TO 0.988 INCH, S/W & BEARING SURFACE BLEND OUT TO 0.060 INCH DEEP, FOUND OUT OF LIMIT. FAB SLEEVE & REPAIR CUTOUT PER EO MD11 -5510-19409-G, PR1422B2 SEALANT APPLIED AT BLEND OUT VOIDS PER EN:1 237-04. REPAIR SLEEVE INSTALLED AT BARREL NUT HOLE NR 12 RT PER EO MD11-5 510-19409-G & EN:1237-07, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040823001802004082300180NM 2004 8 23 UPS04M42930 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, HORIZONTAL STAB NR 33 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDE WALL SURFACE POSITION RIGHT. CORROSION AT BARREL NUT HOLE NR 33 RIGHT, REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.050 INCH DEEP FOUND OUT OF LIMIT PER EO MD11-5510-19409-G. FAB SLEEVE BUSHING & REPAIR AT BARREL NUT HOLE NR 33 RIGHT PER EO MD11-5510-19409-G. PR1422 SEALANT APPLIED PER EN:1178-04 AT BARREL NUT HOLE NR 33 RT. REPAIR SLEEVE BUSHING & INSTALLED AT BARREL NUT HOLE NR 33 RT, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040823001812004082300181NM 2004 8 23 UPS04M42931 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, LEFT HORIZONTAL STAB NR 29 BARREL NUT FOUND CORROSION ON BOTTOM BEARING & S/W SURFACE. CORROSION AT BARREL NUT HOLE NR 29 LT, REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.030 INCH DEEP, FOUND OUT OF LIMIT. FAB SLEEVE & REPAIR BUSHING PER EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED PER EN:1186-04. REPAIR SLEEVE BUSHING INSTALLED AT BARREL NUT HOLE NR 29 LT. REPAIR CUTOUT AT BARREL NUT HOLE NR 29 LT FOUND WITHIN LIMIT PER EO MD11-5510-19409-G & EN1186-04. 2L73 4F RTA22WE 20040823001842004082300184NM 2004 8 23 UPS04M42934 120040620A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, LEFT HORIZONTAL STAB BARREL NUT HOLE NR 27 FOUND CORRODED ON BOTTOM & S/W SURFACE. CORROSION REMOVED AT BARREL NUT TO 0.080 INCH DEEP FOUND OUT OF LIMIT PER EN1226-04, ADVISE HOLE NR 27 LT ENLARGED. REPAIR & FAB SLEEVE BUSHING PER EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 27 LEFT. REPAIR SLEEVE BUSHING INSTALLED AT B/N HOLE NR 27 LEFT PER EO MD11-5510-1 9409-G & EN:1226-04 FOUND WITHIN LIMIT, SATISFACTORY. 2L73 4F RTA22WE 20040823001852004082300185NM 2004 8 23 UPS04M42935 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, LEFT HORIZONTAL STAB NR 6 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDEWALL SURFACE. CORROSION AT B/N HOLE NR 6 LEFT, REMOVED & BLEND TO 0.100 INCH DEEP OUT OF EO MD11-5510-19409-G LIMITS. PER EN1183-04 HOLE NR 6 LEFT REWORKED. FAB & REPAIR SLEEVE BUSHING PER EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED AT B/N HOLE NR 6 LEFT. INSTALLED SLEEVE BUSHING AT B/N HOLE NR 6 PER EO MD 11-5510-19409-G & EN:1183-04 FOUND WITHIN LIMIT, SATISFACTORY. 2L73 4F RTA22WE 20040823001872004082300187NM 2004 8 23 AALA20040862 120040808A335020131 BATTERY PACK BOEING767 767223 1385123NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21332AA 22331 LAX - EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM 31H TO 37H TEST CIRCUIT ONLY. REPLACED EMERGENCY LIGHTS CONTROL MODULE BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTS FROM 31H TO 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040823001882004082300188WP 2004 8 23 AALA20040860 120040818A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21224AA 49174 DEN - EMERGENCY LIGHTS AT COCKPIT AND FORWARD DOORS INOPERATIVE. REPLACED BATTERY PACK B5-23 AT STATION 211 FOR COCKPIT AND FORWARD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040823001902004082300190NM 2004 8 23 AALA20040873 120040816A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21925AN 29526 TUL - BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040823001912004082300191NM 2004 8 23 AALA20040872 120040816A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21925AN 29526 TUL - BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040823001922004082300192WP 2004 8 23 AALA20040863 120040819A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21458AA 49563 DEN - CEILING EMERGENCY LIGHTS AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK B5107 FOR CEILING EMERGENCY LIGHTS AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040823001932004082300193NM 2004 8 23 AALA20040874 120040816A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21925AN 29526 TUL - BATTERY BACK AT STATION 578 FOR EMERGENCY CABIN LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT STATION 578 FOR EMERGENCY CABIN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040823001972004082300197NM 2004 8 23 SWAA042390 120040819A57536573732 SKIN BOEING737 7373H4 1384600NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SPINDLE INSPECTION, FOUND AREA OF DELAMINATION ON OUTBOARD T/E FLAPS. REPAIRED OUTBOARD T/E FLAPS PER SRM. 2L72 4F RTA16WE 20040823002002004082300200NM 2004 8 23 SWAA042393 120040819A3350OL307IBPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29406WN 27894 DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC INOP. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20040823002012004082300201NM 2004 8 23 SWAA042394 120040819A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND STRINGER 27L AT BS 500C, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040823002022004082300202NM 2004 8 23 SWAA042395 120040819A3350604222 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29608SW 27928 DURING SPV, FOUND FWD EMERGENCY EXIT LIGHT INOP. RESECURED BATTERY CONNECTORS PER MM. 2L72 4F RTA16WE 20040823002032004082300203NM 2004 8 23 SWAA042396 120040819A335090083 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROWS 19 DEF, 23 DEF AND AFT RT GALLEY INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040823002042004082300204NM 2004 8 23 SWAA042397 120040819A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29424WN 29828 DURING SCHEDULED HC2D CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING LIGHT PER MM. 2L72 4F RTA16WE 20040825000012004082500001SO 2004 8 25 C2XA04TY154 120040820A3350110049 CHARGER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 DURING A SCHEDULED A-CHECK INSPECTION, THE EMERGENCY EXIT SIGN LOCATED ON THE FWD GALLEY WINDSCREEN WAS DISCOVERED TO BE INOP. MTX REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER IAW THE EMB AMM. EXIT SIGN OPS CHECKED NORMAL AND ACFT WAS RELEASED FOLLOWING COMPLETION OF THE A-CHECK INSPECTION. 2L72 4F RTT00011AT 20040825000022004082500002SO 2004 8 25 C2XA04TY155 120040820A33501317 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727523 145389 DURING A SCHEDULED A-CHECK INSPECTION, THE MAIN PAX DOOR EMERGENCY LIGHT WAS DISCOVERED TO BE INOP. MTX REMOVED AND REPLACED THE PAX DOOR EMERGENCY LIGHT BULB IAW THE EMB AMM. OPS CHECK OF THE LIGHT WAS SATISFACTORY AND THE ACFT WAS RELEASED FOLLOWING COMPLETION OF THE A-CHECK INSPECTION. 2L72 4F RTT00011AT 20040825000032004082500003NM 2004 8 25 SWAA042431 120040821A53116546555 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 867, STRINGER 27L TO STRINGER 27R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040825000062004082500006EA 2004 8 25 MASA200400246 120040504A3260864808 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07650ML12570370 7137 ASH 2888 ATL. AIRCRAFT RETURNED TO THE FIELD, NLG WILL NOT RETRACT. A/C WAS FERRIED TO PHL FOR REPAIRS. MX REPLACED THE ELECTRONIC PROXIMITY SENSOR. OPS CHECKED GOOD. 2L72 4F RTA21EA 20040825000092004082500009NM 2004 8 25 04233428 120040822A3397 TERMINAL DORNERDO32 DO328300 NM EMERGENCY LIGHT DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27428FJ 3193 FLOOR EMERGENCY LIGHTS INOP IN FIRST ROW. ADJUSTED TERMINALS ON STRIP IAW 33-51-12. OPS CHECK GOOD. 2H72 4T RTA55NM 20040825000102004082500010NM 2004 8 25 04234411 120040821A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27411FJ 3166 SECOND CEILING EMERGENCY LIGHT INOP. LIGHT WAS REMOVED AND REPLACED IAW 33-51-04. OPS CHECK GOOD. 2H72 4T RTA55NM 20040825000112004082500011NM 2004 8 25 04235406 120040822A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27406FJ 3156 CENTER FLOOR EMERGENCY LIGHTS INOP. RECYCLED POWER. OPS CHECK GOOD. 2H72 4T RTA55NM 20040825000122004082500012SO 2004 8 25 C2XA04BT092 120040819A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712540 145537 DURING SERVICE AND ROUTINE INSPECTION MAINTENANCE FOUND THE LT EMERGENCY LIGHT FORWARD LEADING EDGE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM 33-50-04, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20040825000152004082500015NE 2004 8 25 04233687 220040820A7261 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE OIL LOOSE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27687BR 7720 ON 08-20-04 LEFT ENG LOW OIL PRESSURE WARNING, ENG SHUTDOWN. RESECURED OIL PRESS LINE AND SERVICED 7 QTS OF OIL. MDC VERIFIED 10 PSI FOR 7.1 SEC AND 7 PSI FOR 151.7 SEC. 2L72 4F4 FRTA21EA E15NE 20040825000162004082500016EA 2004 8 25 MASA200400334 120040614A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA CARGO SMOKE ILLUMINATED A MASAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW077264V 7264 ASH 6460 SAN. CARGO SMOKE EICAS MESSAGE DURING TAXI IN. SYSTEM OPS CHECKED GOOD. NO DEFECTS NOTED. 2L72 4F RTA21EA 20040825000182004082500018EA 2004 8 25 MASA200400340 120040615A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW077305V 7305 ASH 6332 PHX. THE PILOT REPORTED THE MAIN CABIN DOOR STOW HANDLE WAS DIFFICULT TO STOW FROM THE INSIDE. MAINTENANCE IS CURRENTLY TROUBLE SHOOTING MX LUBED HANDLE AND OPS CHECK GOOD, NO PARTS USED. 2L72 4F RTA21EA 20050325000442005032500044WP 2005 3 25 IXXA0500012S 120040822A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM CORRODED AFT CARGO COMPARTMENT AT STA FS 1520.000. A MAJOR REPAIR WAS PERFORMED. REMOVED THE CORRODED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-8 PG 17, 18 AND SRM 53-2-0 PG 2P. FABRICATED FILLER ( AL 7075 T6 0.425) + REPAIR ANGLE (EXTENSION 7075 T6 511 0.150) IAW DC8 SRM 51-2-1 PG 1 SHEET. CLEANED, TREATED AND PRIMED AREA, FILLER REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED FILLER REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 18-14 SHEET IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050328001032005032800103SW 2005 3 28 ALG2005F00008 120041229A6440 CHIP DETECTOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL TAIL ROTOR MALFUNCTIONED E ALGAK NONE N FALSE WARNING ININSP/MAINT 1 SW03198H 3647 CAE835206 DURING TAKEOFF, AFTER MAINTENANCE INSPECTED TAIL ROTOR CHIP FROM FIRST OCCURRENCE OF FLICKERING LIGHT. DURING TAKEOFF, DURING LT TURN TAIL ROTOR CHIP LIGHT FLICKERED ON AND OFF FOR APPROXIMATELY 15 SECONDS THEN REMAINED OFF. AIRCRAFT RETURNED, MAINTENANCE REMOVED AND REPLACED CHIP PLUG ASSEMBLY, GROUND RUN AND OPS CHECK FLIGHT SHOWED NO CHIP INDICATION, AIRCRAFT RETURED TO SERVICE. (K) 1G71 3U3 U H2SW E4CE 20050329000012005032900001WP 2005 3 29 ASAA0480619 120041216A523059101413 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV CHECK, FORWARD CARGO BAY DOOR DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050329000122005032900012WP 2005 3 29 ASAA0480610 120041216A57305910502154 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, RIGHT WING STRUCTURE UNDER FUEL PANEL 1436 RUB STRIP IS GOUGED. REPLACED DAMAGED SECTION PR EA 5720-01258. (M) 2L72 4F RTA6WE 20050329000162005032900016WP 2005 3 29 ASAA0480620 120041216A53305936434129 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, FUSELAGE UNDERSIDE DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER EA 5330-01875. (M) 2L72 4F RTA6WE 20050329000172005032900017WP 2005 3 29 ASAA0480613 120041216A5313593666711 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, LONGERON 29R SPLICE IS CORRODED IN AFT CARGO COMPARTMENT AREA. REPLACED DAMAGED CORRODED SECTION OF LONGERON. (M) 2L72 4F RTA6WE 20050329000182005032900018WP 2005 3 29 ASAA0480621 120041216A523059101575 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, AFT CARGO DOOR FORWARD AND AFT LATCH CUTOUTS ARE BENT AND CRACKED. RECONTOURED ARE STOP DRILLED CRACKS. INSTALLED REPAIR ANGLES. (M) 2L72 4F RTA6WE 20050329000212005032900021WP 2005 3 29 ASAA0480602 120041214A532199579211 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL HAS CRACKED EDGE STRIP. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M) 2L72 4F RTA6WE 20050329000242005032900024WP 2005 3 29 ASAA0480607 120041216A575359100423 VANE DOUG DC9 DC983 3022083WP TE FLAPS WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, RIGHT WING FLAP OUTBOARD VANE INBOARD T/E IS WORN. REMOVED WORN AREA. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000272005032900027WP 2005 3 29 ASAA0480616 120041216A53105912995503 DOOR FRAME DOUG DC9 DC983 3022083WP OVERWING EXIT GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, TWO MOUNTING HOLES GOUGED AT BOTTOM FRAME OF LEFT OVERWING EXIT. INSTALLED DOUBLER PER EA 53-20-01679. (M) 2L72 4F RTA6WE 20050329000962005032900096WP 2005 3 29 ASAA0480606 120041216A575359100424 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, RIGHT WING OUTBOARD FLAP INBOARD VANE PREVIOUS L/E REPAIR IS CHAFED. REPLACED DAMAGED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000972005032900097WP 2005 3 29 ASAA0480609 120041216A57305951368 SKIN DOUG DC9 DC983 3022083WP RT WING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01962AS 53076 OKC - HV-CHECK, RIGHT WING INNER LOWER SKIN GOUGED JUST FORWARD OF DRAIN HOLE. REPLACED DAMAGED SECTION PER EA 5720-01259 AND -10702. (M) 2L72 4F RTA6WE 20050330000872005033000087NM 2005 3 30 S2YA04010 120040419A7931 TRANSDUCER DORNERDO32 DO328300 NM PWA 306 PW306B NE LT OIL PRESSURE ERRATIC A S2YAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL13358SK 3188 DURING FLIGHT, THE CREW NOTED AN ERRATIC INDICATION FOR THE LT OIL PRESSURE. THE CREW PERFORMED AN AIR-TURN-BACK AND MADE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM AND CLEANED THE OIL PRESSURE TRANSDUCER. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330000912005033000091NM 2005 3 30 S2YA04017 120040531A3244DR30621T TIRE DORNERDO32 DO328300 NM PWA 306 PW306B NE MLG DEBONDED A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL13354SK27 27 3126 DURING TAKEOFF OF FLIGHT, THE RT MAIN TIRE CAME APART. THE CREW MADE AN AIR-TURN-BACK AND AN EMERGENCY LANDING. THE CREW MADE A SAFE LANDING BUT REPORTED THE BRAKES FAILED. MX INSPECTED THE SYSTEM AND FOUND THE NR 3 TIRE TREAD DEBONDED AND DAMAGE TO BRAKES , THE KNUCKLE PIN SUPPORT AND THE MLG DOOR. REPLACED THE DAMAGED PARTS AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330000952005033000095NM 2005 3 30 S2YA04025 120040727A3040328550 CONTROL UNIT DORNERDO32 DO328300 NM PWA 306 PW306B NE WNDSLD HEAT CONTINOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13355SK 7014 3124 DURING TAKEOFF FOR FLIGHT, THE CREW NOTED SEVERAL MESSAGES FOR WINDSHIELD HEAT FAIL. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE. MX INSPECTED THE SYSTEM AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROL. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330000982005033000098CE 2005 3 30 S2YA04033 120040914A32301013841377 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MLG INOPERATIVE A S2YAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL1392SK 13914 UE92 DURING APPROACH OF FLIGHT, THE CREW WAS UNABLE TO EXTEND THE GEAR. THE CREW EXECUTED A MISSED APPROACH AND MANUALLY EXTENDED THE GEAR ACHIEVED 3 GREEN AND PROCEEDED TO LAND WITHOUT INCIDENT. THE AC WAS INSPECTED AND FERRIED BACK. MX REPLACED THE GEAR HANDLE AND RETURNED AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2L72 4T4 TRTA24CE E26NE 20050330000992005033000099NM 2005 3 30 S2YA04034 120040929A2150 BEARING DORNERDO32 DO328300 NM PWA 306 PW306B NE LT A/C PACK SEIZED A S2YAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL13356SK 1 3163 DURING FLIGHT, THE F/A REPORTED LOAD VIBRATION THAT THE CAPTAIN WAS ABLE TO CONFIRM. THE CREW MADE AN AIR-TURN-BACK. THE AC WAS INSPECTED BY MX WHO FOUND THE LT PACK WAS VENTING AIR. MX REPLACED THE LT PACK AND OPERATIONAL CHECKED THE COLD AIR UNIT ON A DIFFERENT AC AND DETERMINED THE BEARING HAD SEIZED MOST LIKELY BECAUSE OF THE VENTED AIR. AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. NOTE: THE COLD AIR UNIT HAD JUST BEEN REPLACED ON 9/28/04 AND DID MAKE ONE LEG. (K) 2H72 4T4 FRTA55NM E35NE 20050330001252005033000125CE 2005 3 30 KNI2005F00000 120041129A29102607003375 LINE LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP HYD SYSTEM FAILED E KNIAO OTHER O OTHER NRNOT REPORTED 1 EA05971K 7993 373 CREW REPORTED THAT LANDIND GEAR EXTENSION TOOK LONGER THAN NORMAL TO EXTEND. WHEN DOWN AND LOCKED WAS ACHIEVED, CREW NOTICED COMPLETE LOSS OF HYDRAULIC PRESSURE. NORMAL LANDING WAS MADE USING EMERGENCY BRAKES. JACKED AIRCRAFT AND PERFORMED GEAR SWINGS. FOUND CAUSE TO BE A PIN HOLE IN LT SPOILER DOWN LINE ON TOP OF CENTER WING SECTION. CORROSION IS PROBABLE CAUSE FOR PIN HOLE. (K) 2L72 4F4 F A10CE E6WE 20050330001532005033000153CE 2005 3 30 HYI2005F00000 120040823A3397W31K2M1G75 CIRCUIT BREAKER GRIMES CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LT CB PANEL FAILED E HYIAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NE012615G 402C0101 ON SHORT FINAL, CREW REPORTED SMELL OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF, SMELL DISSIPATED. MECHANIC FOUND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL AND CIRCUIT BREAKER FAILED. REPAIRED WIRING, REPLACED BREAKER AND RETURNED AIRCRAFT TO SERVICE. (NE01200406991) (K) 1L72 3O3 O A7CE E8CE 20050330001632005033000163EA 2005 3 30 DHF2005F00000 220041004A853075068 EXHAUST VALVE CESSNA150 150H 2071818CE LYC O320 O320E2D 41508EA ENGINE FAILED E DHFAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM0322254 15068171 L2063727A ENGINE LOST POWER, AND AN UNEVENTFUL FORCED LANDING WAS MADE. 0 LBS COMPRESSION ON NR 4 CYLINDER. INSPECTION REVEALED THAT THE MFG PN 75068, EXHAUST VALVE STEM/ FAILED. (NM07200501219) 1H71 3O3 O 3A19 E274 20050330001742005033000174CE 2005 3 30 KC82005F00004 120041118A2435730 STARTER GEN LEAR 25 25D 5170514CE GE CJ610 CJ6101 30006NE RT ENGINE VIBRATION E KC8AO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL23248CK 248 CREW FELT VIBRATION IN AIRCRAFT DURING CRUISE FLIGHT. FOUND RT STARTER GEN WAS CAUSING VIBRATION. REPLACED STARTER GEN WITH REPAIRED ASSEMBLY. PERFORMED ENGINE RUNS AND GENERATOR OPERATIONAL CHECKS IAW MM. (K) 2L72 4J4 J A10CE 1E16 20050330001782005033000178EA 2005 3 30 MASA200400450 120040813A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0797325 7325 EXPERIENCED NO EMERGENCY POWER INTERIOR AND EXTERIOR AT THE GATE PRIOR TO DEPARTURE. AIRCRAFT WAS FERRY FLIGHT VIA BIL TO PHX. MX CHARGED THE BATTERIES AND RELAMPED LIGHTS. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050331000042005033100004WP 2005 3 31 ASAA0580029 120040123A575359304964 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 RIGHT OUTBOARD FLAP INBOARD VANE CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050331000162005033100016WP 2005 3 31 ASAA0580039 120040123A5320SRO9520089 SPACER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, MID CARGO BAY DOOR BEAM SPACER IS CORRODED AT FASTENER HOLES. REPLACED DAMAGED SPACERS. (M) 2L72 4F RTA6WE 20050331000232005033100023WP 2005 3 31 ASAA0480624 120041227A53305924802510 SKIN DOUG DC9 DC983 3022083WP FS DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, FUSELAGE DENTED BETWEEN LONGERON 16R AND 17R. RECONTOURED DENT AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050401000202005040100020CE 2005 4 1 FPI2005F00005 120041118A3240RA16402706 ROTOR BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MLG BRAKES CRACKED E FPIAK NONE O OTHER ININSP/MAINT 1 SO156BW 368 TH292 RADIAL CRACK FOUND ON WEAR SURFACE WHEEL HALF ATTACHMENT SIDE. THIS WAS MFG REPLACEMENT PART (PN RA-164-02706). SUSPECT MDG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETECTED. (LEFT ROTOR) 1L72 3O3 O 3A16 E5CE 20050401000442005040100044EU 2005 4 1 KBM2005F00023 120040217A2560 INERTIA REEL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE SHOULDER HARNESSBROKEN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM 2167 INERTIA REEL IS BROKEN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404000122005040400012 2005 4 4 KBM2005F00013 420040722A34225050010902 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE DIRECTIONAL MALFUNCTIONED E KBMAO OTHER O OTHER CRCRUISE 1 WP1953SH 2009 DG, WILL NOT HOLD HEADING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404000592005040400059NE 2005 4 4 AMTA200401489 220041211A7323FFG052AE GOVERNOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE FAULTY A AMTAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL11552TZ106277229 32586 31804 ENGINE NR 1 WILL NOT DEVELOP POWER. REMOVED AND REPLACED FFG ON NR 1 ENGINE IAW MM 73-21-01-4, OPS CHECK NORMAL IAW MM 71-00-00-5, TESTS 1,2, 9, AND 10. (GL11200508815) (K) 2L72 4F4 FRTA2NM E12EU 20050404000832005040400083EA 2005 4 4 A6W2005F00001 120041025A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 INTERCOSTAL LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL 36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIT, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENERS. ALL WORK DONE IAW REO 601R-53-41-059, REV A AND BRAS STANDARD REPAIR 601R5. 2L72 4F4 FRTA21EA E15NE 20050404001052005040400105CE 2005 4 4 HYTA2005002 120041029A321326410143 SPRING CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA MLG CHAFED E HYTAK NONE O OTHER ININSP/MAINT 1 AL01900WA7713 208B0659 SHOT PEENED LOWER SURFACE OF MAIN GEAR CENTER SPRING IS BEING DAMAGED BY CONTACT WITH RIVETS AND SCREWS PROTRUDING FROM THE MLG COVER WHICH IS LOCATED BENEATH THE CENTER SPRING. THIS IS THE THIRD AIRCRAFT FOUND IN THIS CONDITION. 1H71 3T3 T A37CE E2NE 20050404000362005040400036EU 2005 4 4 KBM2005F00033 120040119A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19313LV686 3296 LAMINATED BEARING, WORN, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404000642005040400064 2005 4 4 KBM2005F00012 420041209A34205040017901 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19350SH 2957 LOOSE PARTS INSIDE, HORIZON GYRO, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404000972005040400097CE 2005 4 4 KCQ2005F00001 120041105A3233993880001 ACTUATOR BEECH 99 99 1154002CE PWA PT6 PT6A28 EA HARTZLHCB3T HCB3TN3 GL NLG CRACKED E KCQAK NONE O OTHER ININSP/MAINT 1 GL13799CZ 2833 U68 PCE41530 FOUND TOP CAP TO BE CRACKED AROUND CIRCUMFERENCE OF INTERIOR BORE. (GL13200503455) (K) 1L72 3T4 T A14CE E4EA 6 CP15EA 20050405000192005040500019WP 2005 4 5 ASAA0580014 120040123A523059101419 STRUCTURE DOUG DC9 DC983 3022083WP CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR LOWER AFT INTERIOR GOUGED. REMOVED DAMAGED SECTIONS. REPAIRED SECTIONS PER EA 5210-01168. (M) 2L72 4F RTA6WE 20050405000592005040500059WP 2005 4 5 ASAA0580042 120040124A5730ARB0975517 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RIGHT WING FUEL PANELS 1436 AND 1464 ARE CORRODED. REPLACED PANELS, AT XFS 58-70 AND XRS 324-353 RESPECTIVELY. (M) 2L72 4F RTA6WE 20050405001842005040500184EA 2005 4 5 MASA200400678 120041203A5220864807 PSEU CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07400MJ3 7309 ASH 2725 FROM STL TO PHL, PILOT REPORTED THE RIGHT OVERWING EMERGENCY EXIT CAUTION LIGHT ILLUMINATED. MAINTENANCE COMPLIED WITH MEL PROCEDURE FOR THE INDICATION SYSTEM. 12/04/04 MAINTENANCE REPLACED PSEU, OPS CHECK GOOD 2L72 4F RTA21EA 20050405001862005040500186NE 2005 4 5 MASA200400730 220041227A7261887055 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED A MASABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07173583279 7358 872628 CLOSED - ASH 6484 PHX TO MFR. - AIRCRAFT RETURNED TO THE FIELD AND DECLARED AN EMERGENCY DUE TO THE NR 2 ENGINE OIL PRESSURE FLUCTUATION. MX IS IN THE PROCESS OF TROUBLESHOOTING. OPEN PENDING RESOLUTION. 12/27 MAINTENANCE REMOVED AND REPLACED NR 2 EDP, OPS AND LEAKED CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20050405002002005040500200NM 2005 4 5 72300057 120041018A5320 REINFORCEMENT BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON REINFORCEMENT CHORD. 2L73 4F4 FRTA3WE E2EA 20050405002012005040500201NM 2005 4 5 72300058 120041021A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CRACKED FRAME UPPER FLANGE 1 INCH IN LENGTH. 2L73 4F4 FRTA3WE E2EA 20050405002022005040500202NM 2005 4 5 72300059 120041021A5530 ATTACH FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION IN BORE OF LT STAB HINGE BEARING LUG. 2L73 4F4 FRTA3WE E2EA 20050405002032005040500203NM 2005 4 5 72300060 120041021A5530 ATTACH FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION IN BORE OF RT STAB HINGE BEARING LUG. 2L73 4F4 FRTA3WE E2EA 20050406000072005040600007EA 2005 4 6 MASA200400641 120041116A2612355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA LT ENGINE BROKEN A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0737208 7208 ASH 2836 BNA-PHL - AIR TURN BACK DUE TO 14TH STAGE WARNING. MESSAGE REMAINED AFTER SHUTDOWN. MAINTENANCE FOUND A BAD LOOP IN THE LEFT HAND PYLON. WAITING PART INFORMATION. 11/17/04 MAINTENANCE REPLACED PYLON SENSE LOOP. 2L72 4F RTA21EA 20050406000082005040600008EA 2005 4 6 MASA200400649 120041122A2721 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA AILERONS OUT OF ALIGNMENTA MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0777260 7260 ASH 6268 MFR - THE PILOT REJECTED TAKEOFF FOR A TAKEOFF CONFIG MESSAGE. THEN NOTICED THE AILERON TRIM WAS VERY CLOSE TO THE LIMIT, HE CYCLED THE TRIM INTO THE MIDDLE OF THE GREEN WITH NO FURTHER DEFECTS. 2L72 4F RTA21EA 20050406000212005040600021NM 2005 4 6 72300062 120041026A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ANTENNA DOUBLER CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON SKIN DOUBLER. 2L73 4F4 FRTA3WE E2EA 20050406000232005040600023NM 2005 4 6 72300064 120041106A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SMALL AREAS OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050406000242005040600024NM 2005 4 6 72300065 120041117A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050406000292005040600029NM 2005 4 6 72300070 120041119A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON LOWER FUSELAGE SKIN. 2L73 4F4 FRTA3WE E2EA 20050406000302005040600030WP 2005 4 6 IXXA0500028S 120040814A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE AFT CENTER SECTION LOWER SKIN, REMOVED DOUBLER, FOUND SKIN CRACKED 4.500" STA 1520.00, L-29R AT FRAME AND ATTACH CLIP. REPAIR WAS ACCOMPLISHED. REMOVED DOUBLER IAW DC8 SRM 51-1-21 PG 1. REMOVED THE DAMAGED SKIN IAW DC8 SRM 53-2-1 PG 103-104 FIG 7 (SHEET 3) FABRICATED FINGER DOUBLER FILLER, IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 (SHEET 1) CLEANED, TREATED AND PRIMED AREA, FINGER DOUBLER, FILLER & DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED CONICAL SPACERS IAW DC8 SRM 51-1-26. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED FINGER DOUBLER, FILLER & DOUBLER IAW DC8 SRM 53-2-1 PG 99-100 FIG 7 ( SHEET1) DC8 SRM 51-1-20D PG 9, DC8 SRM 51-12L74 4F RT4A25 20050406000312005040600031WP 2005 4 6 IXXA0500029S 120040816A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FWD CENTER SECTION LOWER PLATING HAS INTERIM REPAIR BETWEEN STA FS 470.00 AND 480.00, L-31LH. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED SECTION, FABRICATED FINGER DOUBLERS AND FILLER AND DOUBLER. CLEANED, TREATED, AND PRIMED FINGER DOUBLERS AND FILLER AND DOUBLER. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED FINGER DOUBLERS, FILLER & DOUBLER WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050406000322005040600032WP 2005 4 6 IXXA0500027S 120040904A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE TAIL SECTION LONGERON CRACK DAMAGE AT STA 1785.00 L-17 LT. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 53-1-0 PG1, DC8 SRM 53-5-3 FIG 5 SHEET 1. REMOVED CRACKED LONGERON 171 IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW LONGERON ( EXTRUSION S 1616757) IAW DDC8 SRM 53-5-3 FIG 5 SHEET 1. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED NEW LONGERON IAW DC8 SRM 51-3-0 PG 1-2 DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG9. 2L74 4F RT4A25 20050406000332005040600033WP 2005 4 6 IXXA0500030S 120040817A5730 PANEL DOUG DC8 DC873F 302199FWP RT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP INTERIM REPAIRS BETWEEN STATIONS XFS. 32.500 AND XFS. 182.500. REPAIR ACCOMPLISHED. REMOVED DAMAGED SLANT PANEL UPPER CAP IAW EC8 SRM 51-1-20D PG 21, DC8 SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-21 PG1 DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050406000352005040600035WP 2005 4 6 IXXA0500031S 120040806A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LOWER CARGO COMPARTMENT FORWARD DOOR OUTER SKIN DENT, NICK DAMAGES AND INTERIM REPAIR AT STA 320.0000. REPAIR ACCOMPLISHED, REMOVED DAMAGED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING (2014T60 0.050"(P.N5779925-3N) IAW DC8 SRM 52-4-1 PG 3. CLEANED TREATED AND PRIMED AREA AND NEW PLATING IAW DC8 SRM 51-1-15 PG 1. APPLIED PRC SEALANT ON FAYING SURFACES AW DC8 SRM 51-1-15 PG1. INSTALLED NEW PLATING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050406000362005040600036WP 2005 4 6 IXXA0500032S 120040805A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT FORWARD DOOR PLATING WERE DAMAGE AND INTERIM REPAIRS STA 1160.000 AT 1220.000. REPAIR ACCOMPLISHED, REMOVED EXTERNAL PLATING WITH INTERIM REPAIR, CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED NEW PLATING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050406000382005040600038WP 2005 4 6 IXXA0500034S 120040830A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AT SECTION FITTING CORROSION DAMAGE BETWEEN STA 1680.00 AND 1690.00, L-36. REPAIR ACCOMPLISHED, REMOVED CORRODED FITTING AND THE CORROSION. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA AND INSTALLED NEW FITTNG PER DOUGLAS STRUCTURAL REAPIR MANUAL. 2L74 4F RT4A25 20050406000392005040600039WP 2005 4 6 IXXA0500035S 120040922A5712 RIB DOUG DC8 DC873F 302199FWP RT WING WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT STUB WING NR 4 STRUCTURE RIB WEAR DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED WORN RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED. INSTALLED NEW RIB ON RT WING NR 4 STUB WING PER DOUGLAS STRUCTURAL REPAIR MANUAL, REPAIR SPECIFICTION NR 2003-05, AND DRAWING NR 9753797. 2L74 4F RT4A25 20050406000502005040600050EA 2005 4 6 MASA200400633 120041111A2760 STOP CNDAIRCL600 CL6002B19 1900309EA SPOILERS OUT OF ADJUST A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775992 7401 ASH 9701 PKC-IAD REPOSITION FLIGHT FROM MAINTENANCE. ABORTED TAKEOFF DUE TO SPOILER CONFIG WARNING MESSAGE. THIS WAS THE SECOND OCCURANCE. MAINTENANCE FOUND THE PROBLEM TO OCCUR WHEN CHANNEL 2 IS IN CONTROL DUE TO THE SPOILERONS DRIFTING UP AND IS TROUBLESHOOTING TO FIND CAUSE. 11/12/2004 MAINTENANCE ADJUSTED THE STOPS, OPS CHEKED GOOD. 2L72 4F RTA21EA 20050406000642005040600064NM 2005 4 6 72300074 120041028A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH BY 8 INCH AREA OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050406000652005040600065NM 2005 4 6 72300075 120041020A5320 STIFFENER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH BY .5 INCH AREA OF CORROSION ON STIFFENER. 2L73 4F4 FRTA3WE E2EA 20050406000672005040600067NM 2005 4 6 72300077 120041027A5314 KEELBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.5 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION. 2L73 4F4 FRTA3WE E2EA 20050406000682005040600068NM 2005 4 6 72300078 120041027A5314 KEELBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION. 2L73 4F4 FRTA3WE E2EA 20050406000692005040600069NM 2005 4 6 72300079 120041016A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050406000702005040600070NM 2005 4 6 72300080 120041016A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON INTERIOR OF SKIN. 2L73 4F4 FRTA3WE E2EA 20050406000732005040600073EA 2005 4 6 MASA200400628 120041108A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0777331 7331 ASH 7116 CLE-IAD, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO PAX DOOR WARNING. CONTRACT MAINTENANCE EXERCISED THE DOOR HANDLE SEVERAL TIMES AND THE FAULT CLEARED. 2L72 4F RTA21EA 20050411001872005041100187NM 2005 4 11 72300010 120041024A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.25 INCH BY 3 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050411001922005041100192WP 2005 4 11 IXXA0500024S 120040827A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION A CORRODED BEAM WAS FOUND AT STA FS 1360.00 RBL 47". REPAIR WAS ACCOMPLISHED, CORROSION WAS REMOVED. FABRICATED FILLER & REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES AND INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050411001982005041100198NM 2005 4 11 72300013 120041026A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050412002872005041200287WP 2005 4 12 ASAA0580027 120040123A523059364351 SKIN DOUG DC9 DC983 3022083WP AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - DURING HV-CHECK, AFT CARGO BAY DOOR DENTED JUST BELOW TOP EDGE. RECONTOURED DOOR SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050413000952005041300095EU 2005 4 13 USAA041132 120041213A5347NRJ72002578C026 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED .040 INCH DEEP BY .6 INCH LONG BY .1 INCH WIDE, FRAME 46, Y=450 TRACK LOBE. CORROSION LEVEL 2, TASK NR J7-200-2578C-026. REMOVED AND REPLACED PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050414000552005041400055GL 2005 4 14 CHQA000562 220041006A7200 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A CHQAC ABORTED TAKEOFF KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 GL11280 145381 CAE312123 FLIGHT 3115 FROM ROC TO DCA - WHEN TAKEOFF POWER WAS ADDED THE FLIGHT DECK AND CABIN INSTANTLY FILLED UP WITH SMOKE. THE TAKEOFF WAS ABORTED AND THE PLANE WAS EVACUATED ON THE TAXIWAY. MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SMOKE TO COMING FROM THE LEFT HAND ENGINE WITH THE PACKS SELECTED AT A HIGH POWER SETTING. THE AIRCRAFT WAS FERRIED WITH THE LEFT PACK OFF TO IND FOR A POSSIBLE ENGINE CHANGE. MAINTENANCE BOROSCOPED THE ENGINE AND FOUND THE LEFT ENGINE 0 CARBON SEAL LEAKING. REMOVED AND REPLACED 0 CARBON SEAL. ENGINE RUNS WERE PERFORMED AND THE ENGINE OPS LEAK CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050414000562005041400056GL 2005 4 14 CHQA000563 220041009A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11280 9105 820 145381 CAE312123 DURING FLIGHT 3089 FROM CVG TO PHL, DURING TAKEOFF ROLL AT AROUND 85 KNOTS, SMOKE BEGAN TO ACCUMULATE IN THE CABIN ALONG WITH A BURNING SMELL. THE TAKEOFF WAS ABORTED AND THE SMOKE DISSIPATED RAPIDLY AND CLEARED AFTER POWER REDUCTION. ALL TEMPERATURES WERE NORMAL AND THERE WERE NO FIRE INDICATIONS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND IT TO BE SAFE FOR FERRY TO CMH WITH THE BLEEDS SELECTED OFF. IN CMH, MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW ROLLS ROYCE JOBCARD CE72-00-01. OPS AND LEAK CHECKED GOOD. NO SMOKE OR BURNING SMELL WAS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050414000572005041400057SO 2005 4 14 CHQA000564 120041011A3350 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260 145128 WHILE PERFORMING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM THE EMERGENCY LIGHTS ON THE FLOOR AFT OF THE EMERGENCY EXIT DOORS DID NOT ILLUMINATE ALONG WITH THE EXIT DOOR LOCATOR LIGHTS. REMOVED AND REPLACED STATIC INVERTER NR 5 AND NR 6 IAW EMB 145 MM 33-50-50. OPS CHECK GOOD AT THIS TIME AND DATE. 2L72 4T RTT00011AT 20050414000582005041400058SO 2005 4 14 CHQA000573 120041026A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11266 145241 EMERGENCY EXIT DOOR FLOOR PROXIMITY LIGHT IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050414000592005041400059SO 2005 4 14 CHQA000574 120041027A3350 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265 145226 EMERGENCY EXIT LIGHT OVER LEFT WING IS INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050414000632005041400063WP 2005 4 14 HXSD2004802 120040802A6420 GEARBOX HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL TAIL ROTOR MAKING METAL B HXSDO OTHER O OTHER NRNOT REPORTED 1 AL055134V 1103D PILOT REPORTED A CHIP LIGHT FOR THE TAIL ROTOR GEAR BOX. MECHANIC INVESTIGATED AND FOUND FOUR HAIR LINE SLIVERS ON THE CHIP PLUG ALL WHICH EXCEEDED LIMITS AS DESCRIBED BY THE MM. REMOVED THE GEAR BOX (PN 369D25400 SN 0295) AND INSTALLED SERVICEABLE GEAR BOX WITH SAME PN AND SN 0022220081. (AL05200402907) 1G71 3U3 U H3WE E4CE 20050414000662005041400066SO 2005 4 14 SIMA20041005 120041005A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21623AE 145109 DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FR 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE OMEGA BEAM. FABRICATED A FILLER AND DOUBLERS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142, REV 27) CHAPTERS 53-21-10, FIG 204. (SW21200500290) 2L72 4T4 FRTT00011ATTE6CH 20050414000682005041400068NM 2005 4 14 04FDEA03310 120041201A5720ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.510, REMAINING THICKNESS=0.506, MATERIAL REMOVED=0.004 AND REPAIRED AS PER FEDEX EA 1-5750-77983. 2L73 4F RTA22WE 20050414000702005041400070NM 2005 4 14 04FDEA03313 120041201A5720ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMATER = 1.094, FINAL DIAMETER = 1.149, AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-77983. 2L73 4F RTA22WE 20050414000842005041400084NM 2005 4 14 2005UALA00060 120040116A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 AFT PIT STA 1440 FRAME DENTED STR 26 LT AT INBD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050414000852005041400085NM 2005 4 14 2005UALA00061 120040116A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 AFT PIT STA 1500 FRAME DENTED AT STR 25 LT ON FRAME INBD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20050414000942005041400094EA 2005 4 14 A6WA20041213 120041213A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING WW CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 FOUND RIGHT MLG WHEEL WELL BATT RIB IS CRACKED 1.5 INCHES LONG IN UPPER AFT RADIUS. REPAIRED RIGHT MLG BATTERY RIB IAW CRJ BOMBARDIER REO 601R-57-51-046 REV B. (M) 2L72 4F RTA21EA 20040820000092004082000009NM 2004 8 20 DHL2004754023 120040710A3240 FUSIBLE PLUG BOEING727 727223 1384074NM MLG BRAKE MELTED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01754DH 22008 ND OCCASIONAL RT BRAKE STEERING ON POST FLIGHT INSPECTION NOTED RT INBOARD BRAKE SMOKING AND RT INBOARD TIRE FUSE PLUG MELTED AND TIRE DEFLATED. FIVE MINUTES LATER RT OUTBOARD TIRE DEFLATED. 2L73 4F A3WE 20040820000152004082000015EU 2004 8 20 MALA0404521 120040811A2930 UPLOCK VALVE SAAB SF340 340B 7860101EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15451XJ 340B451 HYDRAULIC CAUTION LIGHT ILLUMINATED INFLIGHT. MAINTENANCE REPLACED UPLOCK VALVE, PRESSURE SWITCH AND LEFT AND RIGHT EXPOSIVE BOLTS. 2L72 4T RTA52EU 20040820000242004082000024EU 2004 8 20 MALA040530 120040715A3350501122804 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL15421XJ 340B421 EMERGENCY POWER LIGHT ILLUMINATED AFTER START. EMERGENCY POWER SUPPLY P/N 501-1228-04, S/N 2142 UNIT APPEARS TO HAVE BEEN DROPPED. REPLACED SHORTED A2 PCB P/N 542-2635-01. UNIT PASSES CMM. AIRCRAFT RETURNED TO SERVICE 7/29/04. 2L72 4T RTA52EU 20040820000342004082000034NM 2004 8 20 DHL2004742004 120040708A2612 ELEMENT BOEING727 727225 1384077NM NR 3 FIRE WARN OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01742DH 21290 NR 3 FIRE PROTECTION SYSTEM GROUND DETECTOR CIRCUIT ANNUNCIATOR PULSES FAINTLY. ADJUSTED NR 3 FIRE PROTECTION SENSING ELEMENTS PER MM 26-11-01, OP'S CHECK NORMAL. 2L73 4F A3WE 20040820000402004082000040CE 2004 8 20 RK355001 120040709A3260M83536 RELAY BEECH MU300 400A 1155402CE MLG INDICATOR SHORTED E ERYAL ABORTED APPROACH N FALSE WARNING DEDESCENT 1 CE07767SB396 RK355 UPON APPROACH INTO SBA, EXTENDED GEAR, INDICATIONS SHOW THREE GREENS AND A RED LIGHT IN HANDLE. CONSULTED CHECKLIST, FOUND GEAR HANDLE WOULD NOT RAISE AND CIRCUIT BREAKER POPPED. PUSHED -J- HANDLE DOWN, CIRCUIT BREAKER IN, AND RAISED HANDLE - GEAR AND DOORS UP AND CLOSED. ATTEMPTED ANOTHER GEAR CYCLE, CIRCUIT BREAKER POPPED - NO GREEN - ONLY RED LIGHT IN HANDLE. PERFORMED EMERGENCY GEAR EXTENSION, GEAR AND DOORS DOWN AND CLOSED, MADE EMERGENCY LANDING VNY. 2H72 4F RTA16SW 20040820000472004082000047NM 2004 8 20 AWXA200400794 120040623A53306551625 SKIN BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK 5 EACH RIVETS WERE FOUND PULLING THROUGH FUSELAGE SKIN AT BS 947, STR 22 LT. MAINTENANCE REMOVED FUSELAGE SKIN FROM BS 907 TO BS 1016, STR 22 LT. FOUND CORRODED INNER DOUBLER AT BS 947, STR 22 LT, REMOVED INNER DOUBLER; FABRICATED A NEW REPLACEMENT DOUBLER PER DWG 65-51625; INSTALLED REPAIR PART AND FUSELAGE SKIN IAW B737-300 SRM 51-40-02, PARA 4. 2L72 4F RTA16WE 20040820000492004082000049NM 2004 8 20 AWXA200400796 120040623A531069353502 SHEAR TIE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 LCQ - MAJOR REPAIR - DURING C-12 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE AT BS 500A, STR 16 LT. MAINTENANCE REMOVED CRACKED STRINGER SHEAR TIE AT BS 500A, STR 16 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7. 2L72 4F RTA16WE 20040820000512004082000051EU 2004 8 20 UPS04142719 120040713A2611 SMOKE DETECTOR AIRBUS300 A300B4622R 3930312EU CARGO BAY INTERMITTENT A IPXAK NONE N FALSE WARNING ININSP/MAINT 1 SO01146UP BULK CARGO COMP SMOKE LIGHT COMES ON INTERMITTENTLY FOR 2 - 5 SECONDS DURING GROUND OPS, TAXI AND IN-FLIGHT. SYSTEM CHECKED OK IAW TSM 26-16-00. 2L72 4F RTA35EU 20040820000552004082000055NM 2004 8 20 UPS04242704 120040622A5753 FLAP TRACK BOEING727 72725C 138400HNM NR 4 FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C, NR 4 FLAP TRACK, AFT PAD-B HAS CORROSION IN BORE HOLES F & G. REPAIR CARRIED OUT IAW AAAE EO 2004-061-003. 2L73 4F A3WE 20040820000592004082000059NM 2004 8 20 AWXA200400754 120040623A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK 2 EACH CRACKS WERE FOUND IN FLOOR SUPPORT BEAM ON WEB AT FASTENER HOLE BS 707, BL 0, WL 204. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR SUPPORT BEAM BS 707, BL 0, WL 204. FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND A DOUBLER; INSTALLED REPAIR PARTS IAW AWA ER 03-5702-04184-ES2A. 2L72 4F RTA16WE 20040820000632004082000063EU 2004 8 20 AWXA200400818 120040726A2450630CC01Y1 CONTACTOR AIRBUS320 A320232 3930326EU ZONE 120 OVERHEATED A AWXAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP28619AW 527 ON CLIMBOUT, RECEIVED ECAM MESSAGES (ELECT DC ESSENTIAL BUSS SHED) & (CIRCUIT BREAKER TRIPPED L AVIONICS BAY), TURNED BACK FOR REPAIR. MX TROUBLESHOT WIRING FROM CIRCUIT BREAKER (1PH) TO GROUND, NO DEFECTS NOTED. R & R CIRCUIT BREAKER (1PH), RELAY (31XE), & SINGLE POLE 100A CONTACTOR (8PH) IAW AMM. AFTER CONTACTOR (8PH) REMOVED, LOOSE PARTS HEARD RATTLING INSIDE, CONTACTOR HOT TO TOUCH. DC BUSS SYS OPS CK GOOD. VENDORS FAILURE ANALYSIS OF CONTACTOR (8PH) CONFIRMED REASON FOR REMOVAL, DISASSEMBLY FOUND ADJUSTMENT NUTS LOOSE AND THE SUPPORT USED TO ATTACH PARTS WAS FOUND TO BE DISTORTED, UNIT WAS ALSO FOUND TO HAVE INTERNAL CONTAMINATION ON INSIDE COVER & WIRING. UNIT DEEMED UN-REPAIRABLE AND WAS SCRAPPED. 2L72 4F RTA28NM 20040820000642004082000064EU 2004 8 20 AWXA200400819 120040712A5320D5311282600100 RAIL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 12 AND FR 16. MAINTENANCE REMOVED AND REPLACED DUMMY RAIL Y503 LT FROM FR 12 TO FR 16 IAW A320 SRM 51-42-11 FIG 10 - 12 & 18. 2L72 4F RTA28NM 20040820000672004082000067NM 2004 8 20 AWXA200400822 120040624A5320143N808727 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT LT CABIN SIDEWALL BS 660, LBL 70, WL 231. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT LT CABIN SIDEWALL BS 660, LBL 70, WL 231; FABRICATED A NEW REPLACEMENT INTERCOSTAL AND CLIP; INSTALLED REPAIR PARTS IAW T/C M1C53612. 2L72 4F RTA2NM 20040820000702004082000070EU 2004 8 20 HAEA200400155 120040713A3260AI23802 DOWNLOCK SWITCH AMD FALC20FALCON 2720302EU NLG FAILED E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05240TW1477714777 40 ON DEPARTURE FROM ADS, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED ADS FOR MAINTENANCE. MAINTENANCE DISCOVERED FAULTY NLG DOWNLOCK ACTUATOR SWITCH AND REPLACED FAULTY SWITCH. SYSTEM OPERATIONAL CHECKS GOOD. 2L72 4F A7EU 20040820000742004082000074NM 2004 8 20 UPS04442764 120040713A5320AND101362401 FLOOR SUPPORT BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 400-420 BL 0 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED AT UPPER & LOWER FACE. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.063 X 2 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8, CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F RTA20WE 20040820000752004082000075NM 2004 8 20 UPS04442765 120040712A5347BAC15201567 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, BS 510-520 RBL 45 SEAT TRACK I/B FLANGE CHIPPED AND CORRODED. *S/D* CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 8 INCHES EXCEED SRM 51-10-01 FIG 1 LIMITS. SEAT TRACK REPLACED PER SRM 51-10-01 PG 8, CIC APPLIED IAW EO M-5100-2780E. 2L74 4F RTA20WE 20040820000782004082000078NM 2004 8 20 UPS04442768 120040713A53202024T30071IN BRACKET BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 1. COCKPIT BS 360 LT FRAME STR 1 SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040820000792004082000079NM 2004 8 20 UPS04442769 120040713A5320 SUPPORT ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 2. COCKPIT BS 360 LT FRAME STR 2 SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040820000842004082000084NM 2004 8 20 AWXA200400781 120040710A5310D53070011 BEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 66 TO FR 67, FABRICATED A NEW REPLACEMENT BEAM PER DWG D534-72172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18. 2L72 4F RTA28NM 20040820000882004082000088EU 2004 8 20 AWXA200400767 120040713A3350321454 EPSU AIRBUS320 A320232 3930326EU ZONE 263 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28603AW7269 426 661 LAS - EEL - DURING F-01 CHECK THE LEFT AFT EMERGENCY POWER SUPPLY UNIT (13WL) FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820000912004082000091NM 2004 8 20 UPS04442772 120040713A5310LS119471 SHEAR TIE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 420 LT FRAME TIE CLIP FOUND CRACKED AT STR 7. BS 420 LT FRAME STR 7 TIE CLIP REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040820000932004082000093NM 2004 8 20 AWXA200400823 120040624A5320143N808728 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK A .5 INCH CRACK WAS FOUND IN INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, WL 231, AT R-2 DOOR FRAME. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT RIGHT CABIN SIDEWALL BS 660, RBL 70, WL 231; FABRICATED A NEW REPLACEMENT INTERCOSTAL AND CLIP; INSTALLED REPAIR PARTS IAW T/C M1C53612. 2L72 4F RTA2NM 20040820000982004082000098NM 2004 8 20 AWXA200400815 120040724A33501012623 LIGHT BOEING737 737277 1384570NM SEAT ROW 9 LT FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28182AW 22649 PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 9 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820000992004082000099NM 2004 8 20 AWXA200400816 120040724A3350900535A POWER SUPPLY BOEING737 737277 1384570NM SEAT ROW 17 LT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28182AW 22649 PHX - EEL - DURING INSPECTION THE EMERGENCY LIGHTS SEAT ROW 15 LEFT AND AFT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNDER SEAT ROW 17 LEFT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040820001012004082000101 2004 8 20 AWXA200400825 420040716A2565416N21133 RETAINER BOEING757 757225 1384959NM GIRT BAR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 LCQ - MAJOR REPAIR - DURING C-10 CHECK CORROSION WAS FOUND IN THE R-4 DOOR GIRT BAR RETAINER BS 1664. MAINTENANCE REMOVED AND REPLACED R-4 DOOR GIRT BAR RETAINER PLATE AT BS 1664 IAW BMM 25-66-10-2. 2L72 4F RTA2NM 20040820001022004082000102NM 2004 8 20 04FDEA01798 120040618A5744ARC050213 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.224 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78010, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAPS - INBOARD HINGE BRACKET (WING SIDE) CORROSION - REPAIR. 2L73 4F RTA22WE 20040820001042004082000104NM 2004 8 20 AWXA200400829 120040724A5320D5311282720200 RAIL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED DUMMY RAIL Y503 LEFT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18. 2L72 4F RTA28NM 20040820001082004082000108NM 2004 8 20 AWXA200400833 120040724A5320D5311281820400 FLOOR SUPPORT AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 LEFT AT FR 17. MAINTENANCE CUT OUT CORRODED SECTION OF FLOOR SUPPORT Y254 LEFT AT FR 17; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14 FIG 201. 2L72 4F RTA28NM 20040820001112004082000111NM 2004 8 20 AWXA200400836 120040722A5315D5347220922300 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG D53472209245; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2L72 4F RTA28NM 20040820001152004082000115NM 2004 8 20 04FDEA01851 120040624A5510ALC8131502 CAP DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND HORIZONTAL STABILIZER NR 36R FOUND WITH CORROSION BEARING, SIDEWALL AND BOTTOM. CORROSION CLEAN-UP AND FOUND EXCEEDED LIMIT PER SB MD11- 55-023. RIGHT HAND HORIZONTAL STABILIZER NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78021 TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36R - CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20040820001192004082000119NM 2004 8 20 CALA0400597 120040730A5230143A61109 SKIN BOEING737 737724 13844BYNM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714731 28799 INSPECTION FOUND FORWARD CARGO SKIN DENTED JUST ABOVE THE HANDLE. THE SKIN WAS REPAIRED IAW ECRA 5231-01057. 2L72 4F RTA16WE 20040820001242004082000124NM 2004 8 20 SWAA042360 120040816A53116546558 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STR 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040820001272004082000127NM 2004 8 20 SWAA042363 120040816A27616936673 ACTUATOR BOEING737 7373H4 1384600NM RT WING LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29313SW 23335 AIR TURNBACK. CLIMBING THRU 8500, HYDRAULIC -A- SYSTEM FAILURE. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR O-RING PER MM. 2L72 4F RTA16WE 20040820001332004082000133EU 2004 8 20 HAEA00141 120040526A213314640113 OUTFLOW VALVE AMD FALC20FALCON 2720302EU AIR CONDITIONINGSTUCK E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05232TW269 269 32 WHILE ON CLIMBOUT FROM ELP CABIN WOULD NOT PRESSURIZE. RESET SYSTEM AND CABIN DID PRESSURIZE. CLIMBED TO 17,000 AND CABIN ALTITUDE HORN SOUNDED. AIRCRAFT DESCENDED AND LANDED AT LBB. 2L72 4F A7EU 20040820001402004082000140 2004 8 20 AWXA200400887 420040815A2213B546CCM0104 COMPUTER AIRBUSA319 A319132 3930340NM ZONE 120 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28805AW189816243 1049 EN ROUTE, FLT MANAGEMENT GUIDANCE COMPUTER NR 1 FAILED AND FMGC NR 2 FAULTED, FIRST OFFICER LOST MAP DISPLAY 3 TIMES, DIVERTED TO CMH & LANDED WITHOUT FURTHER DIFFICULTY. MX R & R FMGC NR 1 IAW T/C R2A22302, PERFORMED OPS TEST OF FMGC NR 1 & 2, BOTH CHECK GOOD. FUNCTIONAL TEST OF FMGC CONFIRMED REASON FOR REMOVAL, UNIT FAILED FREQUENCY MODULATION (FM) TESTS ON AUTOMATIC TEST EQUIPMENT. R & R A51 PROCESSOR CIRCUIT BOARD (PCB) (P/N E12843AC02) FOR (FM) TEST FAILURE, A52 PCB & A53 PCB FOR FM DBP & FM MP BITE DATA FAILURES, & FG EEPROMS FOR ARINC FAILURE. UNIT REPAIRED AND TESTED IAW CMM. 2L72 4F RTA28NM 20040820001432004082000143EU 2004 8 20 AWXA200400890 120040805A5347D53112092205 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 AT FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040820001462004082000146NM 2004 8 20 UPS04242839 120040630A5752 SKIN BOEING727 72725C 138400HNM AILERON TAB DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, LEFT I/B AILERON TAB DISBOND AT AFT I/B CORNER O/B END. AILERON TAB REPAIRED IAW SRM 51-40-20. 2L73 4F A3WE 20040820001472004082000147 2004 8 20 SWAA042364 420040816A256565C16820 CLIP BOEING737 7375H4 138449DNM L2 DOOR GIRT BARBROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SPV, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOOK, AFT MOUNTING SCREWS CLIP-NUT, BROKEN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CLIP-NUT PER MM. 2L72 4F RTA16WE 20040820001562004082000156NM 2004 8 20 UPS04242851 120040713A5753 FAIRING BOEING727 72725C 138400HNM NR 7 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, 7 FLAP TRACK SAILBOAT FAIRING HAS SUSPECT CRACK TO OUTER SKIN AT RIB ATTACH POINT (INDICATED ON SKIN). HFEC CONFIRMED CRACK AND MARKED END. REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1. 2L73 4F A3WE 20040820001592004082000159NM 2004 8 20 UPS04242757 120040712A2612 FIRE DETECTOR BOEING727 72725C 138400HNM MLG WW FALSE INDICATIONA IPXAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO01951UP 19850 INSPECTION TYPE:N/A, ATB - RETURN TO PHX DUE TO WHEEL WELL LIGHT ILLUMINATED IN FLIGHT. INSPECTED LT AND RT WHEEL WELL FIRE LOOPS, NO DAMAGE NOTED. COCKPIT WHEEL WELL FIRE SYSTEM TEST OK PER 727 MM 26-01-00. 2L73 4F A3WE 20040820001652004082000165NM 2004 8 20 UPS04442827 120040709A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, RIGHT BS 340 WL 300 UPPER DECK FLOORBEAM FOUND 1 EACH FASTENER HOLE CRACKED AT FRAME WEB. RIGHT BS 340 UPPER DECK FLOORBEAM AREA FRAME WEB CRACK REPAIRED AS PER RS R53-12-35177 AND EO B747-5310-20786-A. 2L74 4F RTA20WE 20040820001692004082000169EU 2004 8 20 AWXA200400856 120040808A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28633AW 082 DURING 8-DAY CHECK EMERGENCY LIGHTS FAILED PUSH BUTTON TEST AT RT OVERWING EMERGENCY POWER SUPPLY UNIT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040820001772004082000177 2004 8 20 SWAA042369 420040817A256565C19901 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040820001782004082000178 2004 8 20 SWAA042370 420040817A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040820001802004082000180NM 2004 8 20 SWAA042372 120040817A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20040820001842004082000184NM 2004 8 20 DL733040746 120040807A5330 SKIN BOEING737 737347 1384647NM FS S-L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308WA 23441 A SKIN CRACK WAS FOUND ALONG THE THE MILL LINE OF THE UNDERLYING BONDED DOUBLER JUST AFT OF FS 727D AND BELOW STRINGER 23L. THE CRACK WAS REMOVED WITH A 1.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092528-14, REV A. 2L72 4F RTA16WE 20040820001892004082000189NM 2004 8 20 DL764040751 120040809A3350 LIGHT BOEING767 767432ER 1385134NM SEAT 22A INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27842MH 29715 SEAT 22A EMERGENCY LIGHT INOP. REPLACED LIGHT. 2L72 4F RTA1NM 20040820002012004082000201WP 2004 8 20 AALA20040804 120040802A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21969TW 53619 SEA - EMERGENCY CEILING LIGHTS AT ROWS 28 AND 29 AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT ROWS 28 AND D29 AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040823000052004082300005NM 2004 8 23 SWAA042378 120040818A53106546569 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 986, STRINGER 24R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040823000072004082300007NM 2004 8 23 SWAA042380 120040818A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 STRINGER SPLICE AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040823000092004082300009NM 2004 8 23 SWAA042382 120040818A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727E, RBL 3 TO LBL 12, CORRODED. REPAIRED FLOORBEAM SECTION PER EA. 2L72 4F RTA16WE 20040823000102004082300010NM 2004 8 23 SWAA042383 120040818A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND STRINGER 7L AT BS 1010, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040823000122004082300012NM 2004 8 23 SWAA042386 120040818A53106546529 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500B, RBL 3, WL 148, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040823000142004082300014NM 2004 8 23 SWAA042387 120040818A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29443WN 29838 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040823000172004082300017NM 2004 8 23 QXEA200400565 120040725A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM PROPELLER MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09348PH 484 TAKEOFF WAS ABORTED DUE TO AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL. PERFORMED AUTOFEATHER TEST. TEST CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040823000292004082300029EA 2004 8 23 COMA0460460 120040813A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS UNRELIABLE A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01507CA3264 7796 FLIGHT 5034 FLAPS FAIL CAUTION MESSAGE. REPLACED THE BPSU. 2L72 4F4 FRTA21EA E15NE 20040823000302004082300030EA 2004 8 23 COMA0460461 120040813A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE MAINS LACK OF LUBE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA 7044 FLIGHT 5036 GEAR DISAGREE WARNING. COULD NOT DUPLICATE, RETRACTION AND EXTENSION CHECKS NORMAL. CLEANED AND LUBE NLG. 2L72 4F4 FRTA21EA E15NE 20040823000312004082300031EA 2004 8 23 COMA0460462 120040815A7931APTE142F1000130 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENG OIL MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01963CA6851 2982 7127 FLIGHT 5806, LT ENGINE OIL PRESSURE WARNING. REPLACED THE OIL PRESSURE TRANSDUCER. 2L72 4F4 FRTA21EA E15NE 20040823000332004082300033EA 2004 8 23 COMA0460464 120040812A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01507CA 7796 FLIGHT 5048, FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20040823000402004082300040WP 2004 8 23 ABXA040286 120040803A5310S914025501 BEAM DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE AFT CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 AFT LOWER CARGO DOOR BEAM NR 1 BOTH FORWARD AND AFT END FITTINGS CRACKED. REPLACED FITTINGS S914025-501 AND 3914025-502 IAW SRM 51-30-1 AND 51-30-5. 2L72 4F4 F A6WE E2EA 20040823000432004082300043WP 2004 8 23 ABXA040289 120040804A5230591014167 PAN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FWD CARGO DOOR DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FORWARD LOWER CARGO DOOR HAD DEFECT INDICATION IN OUTER PAN ALONG UPPER EDGE AT FORWARD STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM. 2L72 4F4 F A6WE E2EA 20040823000462004082300046NM 2004 8 23 USAA040342 120040614A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19607AU60500 22203 FOUND STRINGER CORRODED 20 INCH AREA, STATION 1446 STRINGER 28R. INSTALLED DOUBLERS PER EA 95586 AND SRM 51-70-11. (M) 2L72 4F4 FRTA2NM E12EU 20040823000482004082300048SO 2004 8 23 C2XA04IA100 120040808A3350110049 CHARGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712563 145612 DURING MAINTENANCE INSPECTION, THE LT FORWARD EMERGENCY EGRESS LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER AND OPERATIONALLY CHECKED WITH NO DEFECTS IAW MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040823000502004082300050SO 2004 8 23 C2XA04BT091 120040815A2120 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN/COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2717984 145246 CREW REPORTED, (STRONG FUEL ODOR IN AIRCRAFT WHILE APU IS RUNNING.) MAINTENANCE TROUBLESHOT NO DEFECTS FOUND AND PLACED THE AIRCRAFT ON MEL FOR FURTHER FOLLOWUP. STL MAINTENANCE OPS. CHECKED THE APU WITH BOTH PACKS NR 1 AND NR 2 RUNNING FOR 30 MINUTES, NO DEFECTS, NO FUEL ODOR NOTED AT THIS TIME. OPS CHECKED GOOD, MEL PLACARD ITEM REMOVED AND AIRCRAFT RETURNED TO SERVICE -SDR CLOSED- 2L72 4T4 FRTT00011ATTE6CH 20040823000562004082300056CE 2004 8 23 DXTA200400365 120040818A793199121641 TRANSDUCER CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENG OIL OUT OF ADJUST E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07358QS 5600455 PCEJCO349 LT ENGINE OIL PRESSURE REACHED 100 PSI PRIOR TO REACHING COMPUTED TAKE OFF POWER SETTING. REPLACED LT ENGINE OIL PRESSURE TRANSDUCER, ADJUSTED LT ENGINE OIL PRESSURE REGULATOR .5 TURN COUNTERCLOCKWISE OIL PRESSURE AT GROUND IDLE LOW 65 PSI AT TAKE OFF POWER 90 PSI PRESSURE WITHIN LIMITS. OPS AND LEAK CHECK OF TRANSDUCER GOOD, CHECK IAW MM CHAPTER 77-31-01, MM CHAPTER 79-20-01 AND 71-00-00. 2L72 4F4 FRTA22CE E25EA 20040823000632004082300063NM 2004 8 23 AALA20040841 120040814A1420 CONNECTOR BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21188AN 32382 SFO EMERGENCY EXIT LIGHT AT SEAT 20D INOPERATIVE. FOUND LOOSE SIDE WALL CONNECTOR AT SEAT 20D. SECURED LOOSE CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM E12EU 20040823000662004082300066WP 2004 8 23 AALA20040843 120040813A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2176201 53291 FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA6WE E9NE 20040823000682004082300068WP 2004 8 23 AALA20040847 120040814A1420D3899926WF355N CONNECTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE SMOKE DETECTOR SHORTED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW219305N 49395 INFLIGHT T1261 DFW SAT/14 AT 26,000 FEET LEVEL GOT AN INDICATION OF AFT CARGO FIRE. FOLLOWED QRH AND BOTH BOTTLES FIRED. LANDED WITHOUT INCIDENT. REPLACED NR 1 AND 2 CARGO BOTTLES. REPLACED COCKPIT CONTROL AND CONTROL PANEL. FOUND CONNECTOR SHORTED OUT ON AFT CARGO CEU. AIRCRAFT OUT OF SERVICE AND FERRIED TO DFW FOR REPAIRS TO THE AFT CARGO SMOKE DETECTOR SYSTEM. REPLACED AFT CARGO CEU CONNECTOR AND AFT CARGO CEU. REPLACED AFT CARGO NR 3 SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA6WE E9NE 20040823000702004082300070 2004 8 23 AALA20040857 420040817A2565D30654122 SLIDE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE L1 DOOR FAILED A AALAC ABORTED TAKEOFF O OTHER TXTAXI/GRND HDL 1 SW21676AN 29426 L1 SLIDE PARTIAL UNSUCCESSFUL DEPLOYMENT. DOOR DID NOT DISARM. SLIDE PACK FELL OUT ON JETBRIDGE. DOOR ASSIST BOTTLE DISCHARGED UPON ARRIVAL AT GATE WHEN DOOR WAS BEING OPENED BY GROUND CREW. REPLACED SLIDE AT DOOR ONE LT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM E12EU 20040823000722004082300072SO 2004 8 23 C2XA04TY146 120040810A534714530659011 SEAT TRACK EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LF1 AT THE MOST FORWARD END. MAINTENANCE REMOVED AND REPLACED SEAT TRACK LF1 IAW MM 53-01-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F4 FRT TE6CH 20040823000792004082300079EA 2004 8 23 COMA0460467 120040817A3220 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG DISCONNECTED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01915CA 7013 FLIGHT 5530 GEAR DISAGREE WARNING. NLG DID NOT RETRACT. FOUND NLG TORQUE LINKS DISCONNECTED. CONNECTED TORQUE LINKS, NO DEFECTS NOTES. 2L72 4F4 FRTA21EA E15NE 20040823000832004082300083EA 2004 8 23 QXEA200400628 120040816A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX6612 10010 MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY TORN. MAINTENANCE REPLACED THE CHIMNEY AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040823000872004082300087EA 2004 8 23 COMA0460458 120040813A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01927CA 7031 FLIGHT 5456 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20040823000922004082300092EA 2004 8 23 04216627 120040803A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR DEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27627BR 7233 PAX DOOR WARNING IN FLIGHT, S46 AND S47 FOUND IN PSEU FOR FWD AND AFT LATCHES. WHEN AIRCRAFT PRESSURIZED, BOTH LATCHES BACK OFF. REPLACED BONDING JUMPER IAW MM CH 52-11-00. PRESSURIZED TO MAX DIFF AND DOOR WARNING OP CK GOOD IAW 52-70-04. INSTALLED SPACER ON PAX ASSY ROD IRW MM 52-11-03. 2L72 4F4 FRTA21EA E15NE 20040823000932004082300093NM 2004 8 23 AWXA200400828 120040718A53306545776 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28328AW 23377 DURING 4-DAY CHECK CORROSION WAS FOUND ON SKIN AT AFT AIR PHONE ANTENNA UNDER AFT CARGO DOOR AT BS 794.6, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE CUTOUT DAMAGED SKIN AT AFT AIR PHONE ANTENNA BS 794.6, BETWEEN STR 27 LT AND STR 27 RT AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER, INSTALLED REPAIR PART IAW AWA ER 03-5331-04200-SS1. 2L72 4F4 FRTA16WE E2GL 20040823000942004082300094NM 2004 8 23 DHL2004745501 120040701A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK AT THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AT BS 380, BELOW STR 20R. DAMAGE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG.1 CUT OUT DAMAGED AREA DIM 1.7500 X 1.5 INCH AND FABBED DOUBLER FROM 2024 T3, .050,P.O. 900980. DIM 9.1250 INCH X 7.6250 INCH IAW B727 SRM 53-30-3 FIG.1 DOUBLER TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED IAW B727 SRM 53-30-3 FIG.1. 2L73 4F4 F A3WE E2EA 20040823000992004082300099GL 2004 8 23 ALG2004F00039 220040629A7200 ENGINE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL MALFUNCTIONED E ALGAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW033899C 45596 CAE895531 N2 DROOPED ON TAKEOFF, N2 WILL BEEP TO 98 PERCENT THEN DROOPS TO 96 PERCENT ON TAKE OFF, LINEAR ACTUATOR BEEP IS FULL UP. MAINTENANCE ADJUSTED N2 BEEP RANGE IAW 206L MM, OPS CHECK WAS GOOD. 1G71 3U3 U H2SW E1GL 20040823001002004082300100WP 2004 8 23 0401139884 120040625A2927 LIMITER DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE LT HYD QTY CRACKED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01677MC 47756 AIRCRAFT EXPERIENCED A TOTAL LOSS OF HYDRAULIC FLUID FROM THE LT SYSTEM AFTER RETRACTION OF LANDING GEAR DURING CLIMBOUT. COMPLIED WITH COM PROCEDURES AND THE FLIGHT RETURNED FOR AN UNEVENTFUL LANDING BACK AT MSP. IT WAS NOTED THAT THE RT HYDRAULIC SYSTEM MAINTAINED GOOD PRESSURE AND QUANTITY. MAINTENANCE FOUND THE LT HYDRAULIC SYSTEM FLUID QUANTITY LIMITER BROKEN AT THE INPUT PORT AND REPLACED IT. SYSTEM WAS RESERVICED, BLED, AND LEAK CHECKED AND ALL SYSTEM COMPONENTS OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20040823001042004082300104SO 2004 8 23 LR7A04067 120040716A5310 WINDOW FRAME LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND WINDSHIELD FRAME CRACKED AT FS 130, LBL 60, WL 251. REPAIRED IAW SRM SMP 583 FIG 53-30-25. DRC 2013. 2H74 4T4 T A1SO E282 20040823001152004082300115SO 2004 8 23 LR7A04078 120040716A5714 PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CENTER WING CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW SB382-57-55R1 PARA 1.B.3. HFEC FOUND FS 564 RT CENTER WING NR 2 PANEL LOWER SURFACE CRACKED APPROX .280 IN. AT CWS 63R. REPAIRED IAW LAC MEA 382-57-04-050 AND LOCKHEED SES GLD-1720 TN 0033, DWG SK382-57-278. DRC 2189. 2H74 4T4 T A1SO E282 20040823001162004082300116SO 2004 8 23 LR7A04079 120040716A5714 PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CENTER WING CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW HSP57141 FOUND RT CTR WING LOWER SURFACE NR 3 PANEL CRACKED APPROX. 3.0 IN. AT FS 597, CWS 62R AND NR 24 CW STRINGER CRACKED APPROX 14 IN. SAME LOCATION. REPAIRED IAW LAC MEA 382-57-04-051 AND LOCKHEED SES GLD-1720 TN 0034, DWG SK382-57-279. DRC 2191. 2H74 4T4 T A1SO E282 20040823001302004082300130SO 2004 8 23 SIMA20040501 120040720A27003621005009 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZONTAL STAB INOPERATIVE A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO17639AE 145182 ORD - FLT 4057 - DURING CLIMB, CREW REPORTED A PITCH TRIM 1 INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT, IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040823001322004082300132NM 2004 8 23 USAA040337 120040616A5330 SKIN PANEL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19600AU60209 22192 CLT - FOUND SKIN PANEL CRACKED .75 INCH, SKIN IN FORWARD UPPER CORNER OF L1 DOOR CUTOUT. INSTALLED DOUBLER, TRIPLER, FILLER PER EA 95587. (M) 2L72 4F RTA2NM 20040823001352004082300135NM 2004 8 23 USAASB04099 120040724A3350 LIGHT BOEING737 737401 1384701NM ROW 11 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19425US 23992 BWI - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER LIGHT AT SEAT ROW 11, LEFT SIDE, INOPERATIVE. MAINTENANCE ACTION PENDING. (M) 2L72 4F RTA16WE 20040823001372004082300137EA 2004 8 23 ASOA04522 120040720A5260601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11837AS 7271 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040823001402004082300140EA 2004 8 23 ASOA04432 120040617A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER CENTER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20040823001452004082300145NM 2004 8 23 USAA040358 120040720A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FLOOR SUPPORT CORRODED .5 INCH DIAMETER, FLOORBOARD SCREW HOLES FLOORBEAMS STATION 967-986.5, RBL 16. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20040823001472004082300147EA 2004 8 23 ASOA04523 120040720A521060031980103 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11904EV 7628 FLT 4460 - DURING A GROUND INSPECTION IN DFW, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND BROKEN OFF FROM THE AIRFRAME ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE TOP STEP HINGE ON THE PASSENGER DOOR AND DETERMINED THAT THE CAUSE OF THE STEP BREAKING OFF WAS DUE TO CORROSION. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040823001492004082300149NM 2004 8 23 USAA040355 120040720A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FLOORBEAM CORRODED .5 INCH BY .100 INCH, CABIN FLOORBEAM FS 967 RBL UPPER AFT BEAM EDGE. BLENDED CORRODED AREA, TREATED AND PRIMED PER SRM 53-60-51 FIG 101 DETAIL XV. CORROSION LEVEL 1, TASK C53-107-02. (M) 2L72 4F RTA16WE 20040823001542004082300154NM 2004 8 23 USAASB04092 120040715A2750 CONTROL UNIT BOEING737 7374B7 1384702NM TE FLAPS MALFUNCTIONED A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19775AU 24933 BUF - FLT 846 - DURING APPROACH, THE FLAP INDICATION SHOWED 2 AND 5 UNITS. THERE WAS NO ROLL ASSOCIATED WITH THE INDICATION. THE CREW PERFORMED A GO-AROUND. ON THE SECOND APPROACH, FLAP INDICATION WERE NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CYCLED FLAPS THROUGH THREE FULL CYCLES. FLAPS OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA16WE 20040823001592004082300159EA 2004 8 23 ASOA04517 120040718A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11881AS 7496 DURING A C-CHECK IN MCN, THE RIGHT INBOARD CLIP AT FS 484, RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD CLIP AT FS 484, RBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040823001612004082300161EA 2004 8 23 ASOA04519 120040718A5320601R950159 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11915EV 7754 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET. (M) 2L72 4F RTA21EA 20040823001622004082300162EA 2004 8 23 ASOA04521 120040719A14204871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11830AS 7236 DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR LIGHTS AT ROWS ONE C/D TO FIVE C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE SECURED TO LOOSE CONNECTION TO THE EMERGENCY FLOOR LIGHT STRIP FOR ROWS ONE C/D TO FIVE C/D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040823001632004082300163EU 2004 8 23 ASOA04527 120040725A1430NAS6304U17 BOLT AEROSPATR72 ATR72212 8680945EU PAX DOOR MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 FLT 4474 - DURING A GROUND INSPECTION IN TYS, THE PASSENGER DOOR WAS VERY HARD TO OPEN AND THE UPPER LEFT LOCKING PIN WOULD NOT ENGAGE. MAINTENANCE FOUND THE BOLT, WASHER AND NUT P/N NT113544CM, ON THE UPPER AFT LOCKING PIN CONNECTION ROD TO THE BELL CRANK MISSING. MAINTENANCE REPLACED THE MISSING BOLT, WASHER AND NUT ON THE PASSENGER DOOR AFT LOCKING PIN CONNECTION ROD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040823001672004082300167EA 2004 8 23 ASOA04524 120040723A5210601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 FLT 4310 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AND BOWING. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040823001692004082300169NM 2004 8 23 AMTA200400898 120040717A3397 TERMINAL BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND 8 DEF TO R2 DOOR INOPERATIVE EGRESS LIGHTS. RECONNECTED TERMINAL AT SEAT 8 DEF, OPS CHECKED GOOD. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040823001712004082300171EA 2004 8 23 ASOA04444 120040618A5743 RIB CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE RIGHT MAIN LANDING GEAR BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT MAIN LANDING GEAR BATTERY RIB ASSEMBLY IAW ASA EO 600-53-039A. (M) 2L72 4F RTA21EA 20040823001742004082300174NM 2004 8 23 UPS04242967 120040803A2170 BRACKET BOEING727 72722C 138400FNM WATER SEPARATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, RIGHT WATER SEPARATOR SUPPORT BRACKET CRACKED. REPAIR CARRIED OUT IAW SRM 51-10-6 & 51-40-3. 2L73 4F A3WE 20040823001782004082300178NM 2004 8 23 UPS04M42928 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, HORIZONTAL STAB NR 27 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & S/W SURFACE POSN RIGHT. CORROSION REMOVED, BLEND & REAMED AT BARREL NUT NR 27 RIGHT AT S/W SURFACE FOUND OUT LIMIT PER EO MD11-5510-19409-G. FAB SLEEVE BUSHING & PER EO M D11-5510-19409-G. REPAIR & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 27 RT PER EN:1176-04 & EO MD11-5510-19409-G, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040823001862004082300186NM 2004 8 23 AALA20040871 120040816A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21925AN 29526 TUL - BATTERY PACK FOR EMERGENCY CABIN LIGHTS AT STATION 360 FAILED 15 MINUTE TEST. REPLACED BATTERY PACK FOR EMERGENCY CABIN LIGHTS AT STATION 360. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040823001892004082300189NM 2004 8 23 AALA20040861 120040818A3350S283T0143 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21379AA 25448 SFO - EMERGENCY LIGHTS AT 2B THROUGH 6B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 2B THROUGH 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040823001962004082300196NM 2004 8 23 SWAA042389 120040819A275065C27506 TRANSMISSION BOEING737 7375H4 138449DNM TE FLAPS INOPERATIVE A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29528SW 26570 NO FLAP EXTENSION WITH NORMAL HYD, ALT FLAPS USED TO EXTEND LEADING EDGE. ALT FLAP DRIVE C/B TRIPPED. REMOVED AND REPLACED NR 3, 5 AND 6 FLAP TRANSMISSIONS AND JACKSCREWS PER MM. 2L72 4F RTA16WE 20040823001992004082300199 2004 8 23 SWAA042392 420040819A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040825000042004082500004SO 2004 8 25 C2XA04CL084 120040822A3350375911 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2722909 145459 CLE FLIGHT 2244 CREW REPORTED THAT THE OVERHEAD EXIT SIGN AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE EXIT SIGN AT ROW 12. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040825000052004082500005EA 2004 8 25 04235634BR 120040822A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF ADJUST A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27634BR 7287 FLAPS WILL NOT RETRACT PAST 8 DEGREES. FOLLOWED QRH AND RTF. THE FECU RESET AND PERFORMED ADJUSTMENT TEST OF LEFT AND RIGHT BPSU. NO DEFECTS NOTED AND OPS CHECK GOOD. 2L72 4F RTA21EA 20040825000072004082500007EA 2004 8 25 MASA200400263 120040513A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002C10 1390015EA EMERGENCY EXIT OUT OF ADJUST A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07507MJ 10077 ASH 7139 PDX, PILOT REPORTED THE LT OVERWING EMERGENCY EXIT WAS INDICATING OPEN WITH THE DOOR CLOSED. CREW WAS ABLE TO COMPLY THE MEL. ADJUSTED THE PX43 PROX SENSOR AND OPS CHECKS GOOD. NO PARTS. 2L72 4F RTA21EA 20040825000082004082500008EA 2004 8 25 04235628 120040822A5210 MOTOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR WEAK A VTZAK NONE O OTHER ININSP/MAINT 1 EA27628BR 7240 CABIN DOOR HEAVY TO OPEN. REMOVED AND REPLACED PAX DOOR COUNTERBALANCES. DOOR ASSIST MOTOR WEAK. 2L72 4F RTA21EA 20040825000132004082500013 2004 8 25 SWAA042432 420040822A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040825000142004082500014NM 2004 8 25 SWAA042433 120040822A53106546956 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 407, RBL 70 CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM. 2L72 4F RTA16WE 20040825000172004082500017EA 2004 8 25 MASA200400335 120040614A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STIFF A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0737178 7178 ASH 6021 PHX. MAIN CABIN DOOR HARD TO OPEN FROM INSIDE OF AIRCRAFT. MX CYCLED THE DOOR SEVERAL TIMES AND FOUND NO DISCREPANCIES. 2L72 4F RTA21EA 20040825000192004082500019EA 2004 8 25 MASA200400346 120040617A5210601R3181273 CABLE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR BROKEN A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07507MJ 10077 ASH 7104 DEN-AUS. UPON ARRIVAL IN AUS THE PAX DOOR WAS HARD TO OPEN. MX FOUND THE ICE BREAKER CABLE ATTACHED TO THE VENT FLAP BROKEN. A/C FERRIED TO PHL FOR REPAIR. MX REPLACED THE CABLE. 2L72 4F RTA21EA 20040825000202004082500020EA 2004 8 25 MASA200400350 120040617A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA CARGO SMOKE INTERMITTENT A MASAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SW0777286 7286 ASH 6032 SLC. CREW REPORTED AN INTERMITTENT CARGO SMOKE MESSAGE AND AFTER SEVERAL OF THESE THE CREW DISCHARGED THE BOTTLES AND DECLARED AN EMERGENCY. THERE WERE STILL INTERMITTENT MESSAGES AFTER THE DISCHARGING OF THE BOTTLES. ONCE ON THE GROUND IN SLC THE FIRE DEPARTMENT DETERMINED THERE WAS NO EVIDENCE OF SMOKE OR FIRE OCCURRING IN THE CARGO BAY. THE CREW REPORTED THAT ONCE ON THE GROUND THE MESSAGES NO LONGER OCCURRED AND ASSOCIATED IT WITH A HIGH MOISTURE CONTENT IN THE ATMOSPHERE IN THAT AREA. CARGO BOTTLES WERE PLACED ON MEL, THEN MX REPLACED THE RT AND LT FIRE BOTTLES, P/N 34600037-1 RT, S/N 19041F1, P/N 36500018-3 LT, S/N 31791D1. 2L72 4F RTA21EA 20040825000212004082500021EA 2004 8 25 MASA200400353 120040618A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A MASAF ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 SW077264V 7264 ASH 6418 BFL. CARGO SMOKE WARNING INDICATION, BOTH BOTTLES DISCHARGED. CONTRACT MX COMPLIED WITH THE REQUIRED MAINTENANCE ACTIONS AND DEFERRED THE CARGO SMOKE DETECTORS AND THE CARGO FIRE EXTINGUSHING SYSTEM. BOTH BOTTLES WERE REPLACED, FIRE DETECTION/MONITOR PANEL ASSY AND SMOKE DETECTOR. RT BTL P/N 34600037-1, S/N 18579F1, LT BTL P/N 36500018-3, S/N 28220D1. 2L72 4F RTA21EA 20040825000222004082500022 2004 8 25 SWAA042398 420040819A256563550 SLIDE BOEING737 7377H4 1384404NM L2 & R1 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29719SW 27853 DURING SCHEDULED MV2 CHECK, FOUND L2 AND R1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20040825000232004082500023NM 2004 8 25 SWAA042399 120040819A57536573731 SKIN BOEING737 7377H4 1384404NM LT WING SKIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29720WN 27854 DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED T/E FLAP PER EA. 2L72 4F RTA16WE 20040825000272004082500027EA 2004 8 25 MASA200400299 120040528A3230750006000D SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0737178335 7178 ASH 6164 RETURNED TO THE FIELD (PHX) FOR NOSE LANDING GEAR DOOR OPEN MESSAGE DISPLAYED ON EICAS. MX REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. OPS GOOD. 2L72 4F RTA21EA 20040825000282004082500028EA 2004 8 25 MASA200400327 120040611A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX STIFF A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777181 7181 ASH 2835 CLT. PAX DOOR HARD TO OPEN. MAINTENANCE INSPECTED DOOR AND NO DEFECTS NOTED. OPS CHECKED GOOD, NO PARTS USED. 2L72 4F RTA21EA 20040825000292004082500029EA 2004 8 25 MASA200400336 120040614A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO SMOKE DIRTY A MASAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW077264V 7264 ASH 6041 PHX. CARGO SMOKE EICAS MESSAGE DURING ENGINE SHUTDOWN. MX RESET AND CLEANED CONNECTOR AND OPS CHECKED GOOD. NO PARTS. 2L72 4F RTA21EA 20040825000302004082500030EA 2004 8 25 MASA200400362 120040621A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX STIFF A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0775995 7361 ASH 2698. THE PILOT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE IS CURRENTLY TROUBLE SHOOTING. DOOR OPS CHECKED GOOD. 2L72 4F RTA21EA 20040825000312004082500031EA 2004 8 25 MASA200400364 120040621A5220 DOOR CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT DAMAGED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07921FJ 15021 ASH 6433 PHX. CREW REPORTED THE LT FWD EMERGENCY EXIT MESSAGE ON THE ECIAS SCREEN. MX REMOVED AND INSTALLED THE DOOR OPS GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040825000352004082500035EA 2004 8 25 MASA200400380 120040630A5220 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT ILLUMINATED A MASAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07923FJ 15023 ASH 6599 DFW-PHX. RETURNED TO THE GATE DUE TO THE RT OVERWING EMERGENCY EXIT INDICATED OPEN. THE INDICATION SYSTEM WAS MEL'ED. MAINTENANCE REMOVED AND REINSTALLED DOOR, OPS CHECK OK. 2L72 4F RTA21EA 20040825000362004082500036NM 2004 8 25 AALA20040866 120040818A5697 TERMINAL BOEING767 767323 1385205NM WINDSHIELD SMOKE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21357AA 24038 EZE - TEN MINUTES AFTER TAKEOFF STRONG ELECTRICAL SMOKE SMELL IN COCKPIT. PERFORMED ELECTRICAL FIRE AND SMOKE EMERGENCY CHECKLIST BUT SMOKE NEVER ABATED. RETURNED TO EZE AND LANDED WITHOUT INCIDENT. FOUND SOURCE OF SMOKE IN J5 TERMINAL AT RIGHT HAND WINDSHIELD. REPLACED RIGHT HAND WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040825000382004082500038EA 2004 8 25 MASA200400291 120040524A323016215105 BRACKET CNDAIRCL600 CL6002B19 1900309EA NLG BENT A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0737178 7178 ASH 6185, RETURNED TO THE FIELD DUE TO THE NLG WOULD NOT RETRACT. MX REPLACED THE CENTER SENSOR AND BRACKET. 2L72 4F RTA21EA 20040825000392004082500039EA 2004 8 25 MASA200400205 120040416A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG LEAKING A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07650ML33 7137 ASH 2608 CLT. AFTER TAKEOFF WITH GEAR SELECTED UP, THE NOSE REMAINED EXTENDED. AFTER THE AURAL WARNING SOUNDED THE NOSE RETRACTED WITH NO FURTHER INPUT FROM THE FLIGHT CREW. A/C LANDED AT DESTINATION AIRPORT NORMALLY. MX IS TROUBLESHOOTING AT THIS TIME. MX REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD. 2L72 4F RTA21EA 20040825000412004082500041 2004 8 25 AALA20040867 420040816A2565 SLIDE FOKKERF28 F28MK0100 4990807EU RIGHT DEPLOYED A AALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW211463A 11483 TUL - RIGHT ONE DOOR SLIDE INADVERTANTLY DEPLOYED UNSUCCESSFULLY BY MAINTENANCE. REPLACED RIGHT ONE DOOR SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040825000422004082500042 2004 8 25 AALA20040870 420040817A25655A33073 SLIDE BOEING737 737332 1384616NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21922AN 29523 TUL - SLIDE DID NOT AUTO DEPLOY. MANUALLY DEPLOYED SLIDE. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040825000432004082500043WP 2004 8 25 AALA20040865 120040819A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21978TW 53628 ORD - OVERHEAD EMERGENCY LIGHTS AT ROWS 18 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AT B4104 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 18 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040825000452004082500045EA 2004 8 25 MASA200400278 120040519A4930388273010 FCU HONEYWELL CNDAIRCL600 CL6002B19 1900309EA APU LEAKING A MASAF ACTIVATE FIRE EXT. J WARNING INDICATION DEDESCENT 1 SW07571ML4763 P346C 7209 ASH 2940 YYZ. CREW DECLARED AN EMERGENCY ON DESCENT. CREW REPORTED THAT ON APU START UP THERE WAS AN APU FIRE WARNING INDICATION AND THE APU FIRE BOTTLE WAS ACTIVATED. CONTRACT MX INSPECTED THE APU AREA BUT FOUND NO SIGNS OF ACTUAL FIRE. THE APU FIRE EXTINGUSHING SYSTEM WAS DEFERRED, TREATING THE APU AS INOPERATIVE. MX REPLACED FCU. 2L72 4F RTA21EA 20040825000462004082500046NM 2004 8 25 04231411 120040818A5270 PSEU DORNERDO32 DO328300 NM CARGO DOOR DEFECTIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27411FJ 3166 DOOR RWP MESSAGE ASSOCIATED WITH CARGO DOOR RED OPEN ON DOOR PAGE. RETURNED TO FIELD. MX RESET PSEU AND INSPECTED CARGO DOOR. NO DEFECT NOTED. 2H72 4T RTA55NM 20040825000472004082500047SO 2004 8 25 C2XA04BT093 120040818A32347455503 LEVER EMB 145 EMB145LR 3260212SO MLG FAULTY A C2XAO OTHER SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 SW27139082674 2674 145465 CREW REPORTED, LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT. OPERATED NORMALLY ON SECOND TRY. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW EMB145 MM 32-32-02, OPS CHECK AND LANDING GEAR SWING GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040825000482004082500048NM 2004 8 25 AALA20040875 120040816A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21925AN 29526 TUL - BATTERY PACK AT STATION 967 FOR EMERGENCY CABIN LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AS STATION 967 FOR EMERGENCY CABIN LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040825000502004082500050NE 2004 8 25 AALA20040869 220040816A7261 ENGINE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE NR 2 LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21174AA 31308 31841 BDA - INFLIGHT T1270/16 SJU TO EWR. ABOUT 55 MINUTES AFTER TAKEOFF LOST EIGHT QUARTS OF OIL IN RIGHT ENGINE IN APPROXIMATELY 72 MINUTES. LANDED BDA WITHOUT INCIDENT. REPLACED NUMBER 2 ENGINE FOR HIGH OIL CONSUMPTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20040825000512004082500051NM 2004 8 25 AALA20040868 120040817A3230 CABLE BOEING737 737823 13844BZNM TE FLAPS BROKEN A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21918AN 29519 IAH - INFLIGHT T1068/17 AFTER TAKEOFF THE LANDING GEAR HANDLE COULD NOT BE RAISED. WHEN FLAPS WERE RAISED TO ZERO DEGREES THE CONFIGURATION WARNING HORN SOUNDED. RETURNED TO IAH AND LANDED WITHOUT INCIDENT. FOUND RIGHT HAND AIR TO GROUND SENSE CABLE BROKEN ON MAIN GEAR. REPLACED CABLE AND SPEEDBRAKE INTERLOCK VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040820000572004082000057NM 2004 8 20 AWXA200400752 120040620A5315654581080 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 312 BETWEEN LBL 5 AND RBL 11, WL 208. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOORBEAM AT BS 312 FROM LBL 5 TO RBL 11. FABRICATED A FLOORBEAM SPLICE AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20040820000582004082000058NM 2004 8 20 AWXA200400753 120040620A531565C3394016 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 294, FROM LBL 8 TO RBL 51, WL 208. MAINTENANCE CUT OUT CORRODED SECTION OF FLOORBEAM AT BS 294, FROM LBL 8 TO RBL 51. FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20040820000652004082000065EU 2004 8 20 AWXA200400820 120040712A5310D5347217220300 BEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28654AW 1050 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 65 TO FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040820000712004082000071NM 2004 8 20 UPS04242774 120040630A7110 LONGERON BOEING727 72725C 138400HNM NR 2 ENGINE COWLCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, ENGINE NR 2 LT FWD COWL UPPER LONGERON IS CRACKED AT ALIGNMENT PLATE. REMOVED LT FWD COWL UPPER LONGERON IAW SRM 51-30-02. FABRICATED NEW LONGERON PER DRAWING QF7122130-1AND SRM 54-10-06. INSTALLED NEW LONGERON IAW SRM 57-30-02. 2L73 4F A3WE 20040820000732004082000073NM 2004 8 20 UPS04242776 120040710A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, CORROSION ON SKIN NEXT TO FASTENER BS 470 S19R. FASTENER REMOVED FROM SUSPECT AREA IAW SRM 51-30-02. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-30-1. CORRODED SKIN TRIMMED OUT IAW SRM 53-30-3 FIG 14. AFTER TRIM OUT CORROSION FOUND ON LOWER SKIN, CORROSION REMOVED IAW SRM 51-10-06. LOWER SKIN TRIMMED IAW SRM 53-30-3, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2L73 4F A3WE 20040820000772004082000077NM 2004 8 20 UPS04442767 120040713A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 610-650 LBL 46 SEAT TRACK LIP FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.060 X 2 X 4 EXCEED SRM 53-10-01 FIG 1 LIMITS. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 6. 2L74 4F RTA20WE 20040820000802004082000080NM 2004 8 20 UPS04442770 120040713A5320 ATTACH ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, COCKPIT - BS 360 LT FRAME ATTACH SUPPORT ANGLE FOUND CRACKED AT STR 2A. COCKPIT BS 360 LT FRAME STR 2A SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20040820000812004082000081NM 2004 8 20 AWXA200400778 120040617A5330141N3311 BEAR STRAP BOEING757 7572S7 1384962NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - MAJOR REPAIR - DURING 8-DAY CHECK A CRACK WAS FOUND IN SKIN AND BEAR STRAP AT L-1 DOOR WAY FORWARD UPPER CORNER BS 350. MAINTENANCE CUT OUT CRACKS IN SKIN AND BEAR STRAP AT L-1 DOOR WAY FORWARD UPPER CORNER BS 350; PERFORMED HFEC OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, AND QUADRUPLER; INSTALLED REPAIR PARTS IAW AWA ER 19-531104167-BA1. 2L72 4F RTA2NM 20040820000892004082000089NM 2004 8 20 AWXA200400768 120040711A2932501310000 PRESSURE SWITCH AIRBUSA319 A319132 3930340NM NR 1 ENGINE CRACKED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28823AW 1463 LAX - EMERGENCY LANDING - FLT 0364 - EN ROUTE FROM IAD TO LAX RECEIVED ECAM MESSAGE NR 1 ENGINE GREEN HYDRAULIC PUMP LOW PRESSURE AND GREEN HYDRAULIC SYSTEM LOW PRESSURE, AS A PRECAUTION DECLARED EMERGENCY. MAINTENANCE FOUND NR 1 ENGINE GREEN HYDRAULIC PUMP PRESSURE SWITCH CRACKED AT WELD, REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 29-11-17. DUE TO FLUID LOSS REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-51-04, AND NR 1 ENGINE CASE DRAIN FILTER IAW AMM 29-11-43-03; LEAK AND OPERATIONAL CHECKS WERE GOOD. PART INFORMATION HAS BEEN ADDED TO THIS SDR. 2L72 4F RTA28NM 20040820001102004082000110NM 2004 8 20 AWXA200400835 120040723A5310D5347217220300 BEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28808AW 1088 MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT FROM FR 67 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 2-8. 2L72 4F RTA28NM 20040820001182004082000118WP 2004 8 20 CALA0400596 120040812A53475930566U71 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND LT MID SEAT TRACK CORRODED FROM STA 1098-1201, LBL 30. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2L72 4F A6WE 20040820001202004082000120WP 2004 8 20 CALA0400598 120040812A534759305475 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 200-218, RBL 22. A NEW SEAT TRACK WAS INSTALLED IAW SRM 53-05. 2L72 4F A6WE 20040820001282004082000128NM 2004 8 20 04FDEA01697 120040612A5744ARC0503 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402-407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.002 INCH, REMAINING THICKNESS = 0.425 INCH. COMPLIED WITH FEDEX EA 1-5740-76741, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040820001302004082000130NM 2004 8 20 04FDEA01699 120040612A5744ARC0503 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMIT PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.219 INCH. COMPLIED WITH FEDEX EA 1-5740-76742, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040820001322004082000132NM 2004 8 20 04FDEA01802 120040618A5744ARC0503 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG 402-407 ORIGINAL THICKNESS 0.517 INCH, MATERIAL REMOVED 0.004 INCH REMAINING THICKNESS 0.513 INCH & FOUND WITHIN LIMITS AS PER DWG TOLERANCE OF ARC0503. 2L73 4F RTA22WE 20040820001352004082000135NM 2004 8 20 04FDEA01829 120040620A5753ARC2512504 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER =1.327 INCH AND REPAIRED AS PER FEDEX EA 1-5750-78013, TITLE: WINGS - TRAILING EDGE FLAPS - RIGHT HAND INBOARD FLAP - OUTBOARD BRACKET PIVOT BORE CORROSION - REPAIR. 2L73 4F RTA22WE 20040820001412004082000141NM 2004 8 20 AWXA200400888 120040726A531369620541 STRINGER CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A .75 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 294.5, STR 11 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 294.5, STR 11 LT IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20040820001442004082000144NM 2004 8 20 AWXA200400891 120040809A53206545834131 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT RBL 50, BETWEEN BS 344 AND BS 360. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT RBL 50, FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20040820001522004082000152NM 2004 8 20 UPS04242842 120040708A5312 BULKHEAD BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, INSPECT CRACK ON BS 1183 BULKHEAD, SUSPECT CRACK IS LOCATED ON AFT SIDE OF BULKHEAD, WL 175 APPROX LBL 20. HFEC INSPECTION CARRIED OUT & CRACKS CONFIRMED AND ENDS MARKED. FASTENERS REMOVED AND CRACKS TRIMMED OUT IAW SRM 51-10-6, REPAIR CARRIED OUT IAW AAAE EO 2004-068-003 R1. 2L73 4F A3WE 20040820001552004082000155NM 2004 8 20 UPS04242850 120040708A531265C362891 BULKHEAD BOEING727 72725C 138400HNM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, CRACK ON FWD PRESSURE BULKHEAD AT WL 198 RBL 02. HFEC CARRIED, CRACK CONFIRMED AND END MARKED. REPAIR CARRIED OUT USING REPAIR KIT 65C36289-1. REPAIR CARRIED OUT IAW DRG 65C36289 & SRM 51-30-02. 2L73 4F A3WE 20040820001572004082000157NM 2004 8 20 UPS04242736 120040628A5754 WEB BOEING727 72725C 138400HNM NR 2 KRUGER FLAPCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT WEB CRACKED. REMOVED LT WEB TO FACILITATE IN FABRICATION OF NEW ONE IAW SRM 51-30- 02. FABRICATED NEW LT WEB IAW DRAWING 65-16269 AND INSTALLED ON NR 2 KRUEGER FLAP ACTUATOR TRUNNION SUPPORT BOX LT IAW DRAWING 65-162 69. 2L73 4F A3WE 20040820001602004082000160NM 2004 8 20 UPS04242758 120040715A5320 INTERCOSTAL BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, DURING REMOVAL OF BS 740 FITTING (LEFT) THE INTERCOSTAL LOCATED BETWEEN STR 20 & STR 21 FOUND TO BE CRACKED. FABRICATED NEW INTERCOSTAL IAW SRM 51-20-1 FIG 7. INSTALLED INTERCOSTAL IAW SRM 51-30-02 AND EO B727-5310-7477-E. 2L73 4F A3WE 20040820001622004082000162NM 2004 8 20 UPS04442824 120040710A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, BS 200 RIGHT FRAME WEB FOUND SEVERAL CRACK BETWEEN STR 13A & STR 14A. BS 200 RIGHT FRAME WEB CRACKED AREA REPAIRED AS PER RS R53-12-35175 FIG 4 AND EO B747-5310-20791-A. 2L74 4F RTA20WE 20040820001702004082000170NM 2004 8 20 AWXA200400857 120040808A3397 WIRE AIRBUSA319 A319132 3930340NM ZONE 242 DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28813AW15870 1223 LAX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 3, 6, 12, 16, AND 20 WERE FOUND INOPERATIVE. AIRCRAFT MAINTENANCE FERRIED TO LAS, MAINTENANCE REPAIRED EMERGENCY LIGHT WIRING AT CONNECTOR 7260VCS SEAT ROW 12, ALSO REPLACED EMERGENCY POWER SUPPLY UNIT (12WL); OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD. 2L72 4F RTA28NM 20040820001722004082000172NM 2004 8 20 AWXA200400859 120040726A5753654643727 WEDGE BOEING737 7373S3 1384711NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FLAP WAS FOUND SEPARATED AT THE AFT INBOARD CORNER, WATER WAS FOUND LEAKING FROM INSIDE FLAP AT SEPARATED SKIN, WBL 230.68 TO WBL 231.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT OUTBOARD FLAP SKIN AT AFT INBOARD CORNER; FABRICATED A REPAIR DOUBLER AND FILLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-03 FIG 3. 2L72 4F RTA16WE 20040820001832004082000183GL 2004 8 20 DL764040743 220040808A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 MAKING METAL A DALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO27828MH9770 29699 706206 AT FLT LEVEL 330 CREW HEARD 2 LOUD POPS FROM THE LT ENGINE. REDUCED PWR DIVERTED TO PHX. REPLACED ENGINE. 2L72 4F4 FRTA1NM E23EA 20041228000032004122800003NE 2004 12 28 AWXA200400660 220040618A7250761702 TURBINE BLADES BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 1 ENGINE OVERHEATED A AWXAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 WP28187AW 22654 P702980B ON TAKEOFF ROLL AT OAK EN ROUTE FOR LAS FELT A STRONG VIBRATION NR 1 ENGINE, REJECTED TAKEOFF AT 50 KTS AND PULLED OFF ONTO TAXIWAY WHERE EMERGENCY EQUIPMENT INSPECTED THE AIRCRAFT. TAXIED BACK TO GATE USING NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE IAW T/C R5M71002, FUNCTIONAL CHECK GOOD IAW T/C F5M71002.**SUPP** VENDOR TEARDOWN OF ENGINE S/N 702980 FOUND SECOND STAGE TURBINE BLADES FRACTURED BY AN APPARENT STRESS RUPTURE OR TENSILE OVERLOAD, IT WAS NOT POSSIBLE TO IDENTIFY PRIMARY FRACTURE. THIRD STAGE TURBINE BLADES EXHIBITED SIMILAR CHARACTERISTICS ALSO WITH NO IDENTIFIABLE PRIMARY FRACTURE. 2L72 4F4 FRTA16WE E2EA 20040820001912004082000191NM 2004 8 20 DLM90040773 120040817A3350RPS1B CHARGER DOUG MD90 MD9030 3023690NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27915DN 53395 FIRST CLASS FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND BATTERY CHARGER FOR FIRST CLASS FLOOR TRACK EMERGENCY LIGHTS. REPAIRED SHORTED WIRE IN FLOOR TRACK, ALL EMERGENCY LIGHTS OPN NORMAL. 2L72 4F RTA6WE 20040820001972004082000197NM 2004 8 20 AALA20040798 120040802A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21927AN 30077 TUL - EMERGENCY LIGHT BATTERY PACKS IN CABIN FAILED 15 MINUTE MINIMUM TIME PER CARD 2311. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040820001982004082000198WP 2004 8 20 AALA20040799 120040731A2822 COVER DOUG DC9 DC982 3022082WP BOOST PUMP LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW217548A 53030 RDU - INFLIGHT T1886/31 DURING FLIGHT FUEL SEEPING FROM LEFT INBOARD BOOST PUMP ACCESS PANEL. LANDED WITHOUT INCIDENT AT RDU. CLEANED, SEALED AND RETORQUED LEFT INBOARD BOOST PUMP COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040823000012004082300001NM 2004 8 23 QXEA200400609 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT TRACK NR 2 HAS LIGHT CHAFING AT 258.5. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1, AREA 1 INCH LONG, .375 INCH WIDE AND .002 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 5. 2H72 4T RTA13NM 20040823000032004082300003 2004 8 23 SWAA042376 420040818A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040823000212004082300021NM 2004 8 23 QXEA200400553 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X196 AND X200. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040823000382004082300038WP 2004 8 23 ABXA040284 120040803A53119919617501 FRAME DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 RT MAIN FRAME STA 699 WAS CRACKED IN FORWARD UPPER FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME RT 699 IAW EA 53400120-001-1. 2L72 4F4 F A6WE E2EA 20040823000492004082300049SO 2004 8 23 C2XA04BT090 120040815A2612 WARNING LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL APU FIRE DETECT FALSE INDICATIONA C2XAK NONE N FALSE WARNING ININSP/MAINT 1 SW2713989 145271 CREW REPORTED, (APU FIRE INDICATION DURING FLIGHT. PERFORMED QRH WITHOUT EXTINGUISHING HALON FIRE BOTTLE.) AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND PLACED THE APU ON MEL FOR FOLLOWUP. EWR MAINTENANCE PERFORMED FOLLOWUP AND TROUBLESHOT APU FIRE DETECTOR AND PERFORMED OPERATIONAL TEST ON APU FIRE DETECTOR SYSTEM IAW MM NR 26-12-00-810-802-A. NO PROBLEMS DETECTED AND OPS CHECKED GOOD. MEL PLACARD REMOVED AND CLEARED, AND AIRCRAFT RETURNED TO SERVICE -SDR CLOSED- 2L72 4T4 FRTT00011ATTE6CH 20040823000532004082300053SO 2004 8 23 C2XA04BT079 120040722A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712563 145612 MAINTENANCE REPORTED, DURING SERVICE CHECK, LT FRONT FAIRING WING FUSELAGE EMERGENCY LIGHT INOPERATIVE AND NR 1 AISLE PATH EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY IAW EMB145 NR 33-50-04, OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040823000552004082300055CE 2004 8 23 DXTA200400364 120040818A3210 LANDING GEAR CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL RIGHT BROKEN E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07961QS 7500061 AFTER A NORMAL LANDING AND ROLL-OUT, AIRPLANE WAS TRAVELING APPROX. 5-10 MPH. STARTED TURN TO EXIT RUNWAY, AIRCRAFT ABRUPTLY FELL ON RT WING AND SHUDDERED TO SUDDEN STOP. EMERGENCY SHUT DOWN WAS ACCOMPLISHED, UPON VISUAL INSPECTION FOUND THE RT MAIN LANDING GEAR BROKE IN HALF. ITEM IS UNDER INVESTIGATION. 2L72 4J4 FRTT00007WITE6CH 20040823000572004082300057NM 2004 8 23 WLDA200488 120040818A2710 WARNING LIGHT DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE AILERONS ILLUMINATED A WRLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11273WA 48519 AIR TURNBACK DUE TO AILERON DEFLECTED DISAGREE ALERT DISPLAYED AFTER TAKEOFF. DEACTIVATED TAKEOFF DEFLECTED AILERONS IAW MEL 27-13-2 CAT (C), ENTERED IN DMI M27AU1904-106. 2L73 4F4 FRTA22WE E24NE 20040823000692004082300069NM 2004 8 23 AALA20040850 120040813A2910AE2460060E0280 HOSE BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE HYD SYSTEM DAMAGED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21697AN 26977 AFTER FEAR UP RECEIVED LT HYDRAULIC QUANTITY STATUS MESSAGE WITH HYDRAULIC LIGHT. SECURED LT HYDRAULIC PUMPS WITH FLUID IN SYSTEM AND LOWERED GEAR AND FLAPS PRIOR TO SYSTEM LOSS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND IB RT MAIN GEAR EXTENSION AND REFRACTION LINE DAMAGED. INSTALLED FLEX LINE HOSE IAW GPM 17 13. CONTACTED TECH FOR FOLLOW UP. LGA REMOVED AND REPLACED RT MAIN GEAR EXTENSION AND RETRACTOR LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM E12EU 20040823000742004082300074NE 2004 8 23 AT0400015 220040731A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE LEFT SURGES A ZZDAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO15980AT 55039 LT ENGINE SURGED IN FLIGHT. ENGINE SHUT DOWN AS IT CONTINUED TO SURGE. 2L72 4F4 FTRA6WE E00061EN 20040823000802004082300080 2004 8 23 ARWA20040802 420040817A3442 INDICATOR DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE WX RADAR SYS INOPERATIVE A ARWAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO19441J 45988 WEATHER RADAR DOES NOT PAINT WEATHER NOR DOES IT WORK IN MAPPING MODE. TEST FUNCTION IS NORMAL; AIRCRAFT RETURNED. REMOVED AND REPLACED WHEATHER INDICATOR IN ACCORDANCE WITH MM 34-00; OPERATIONAL CHECK DUE; REMOVED AND REPLACED RADAR R/T IN ACCORDANCE WITH MM 34-00. CHECK SYSTEM OK IN ACCORDANCE WITH MM 34-41-0; FOR TEST FLIGHT, REFERENCE LOG PAGE 108142, ITEM 4: ON TEST FLIGHT RADAR OPERATIONAL CHECK NORMAL. 2L74 4F4 F 4A25 1E8 20040823000812004082300081NE 2004 8 23 0401356631 220040817A7530 MANIFOLD BOEING747 747251B 1384892NM PWA JT9 JT9D7R4D 52054NE BLEED SYSTEM BROKEN A NWAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL01631US 23111 715219 DURING TAKEOFF ROLL, THE CREW OBSERVED THE NR 3 ENGINE EPR INDICATION DECREASE WITH THE EGT INDICATION RISING INTO THE CAUTION RANGE. THE TAKEOFF WAS ABORTED AT 100 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE IAW FIM AND FOUND THE 3.5 BLEED MANIFOLD BROKEN. THE BROKEN MANIFOLD AND THE 8TH STAGE CHECK VALVE WERE REPLACED. AN ENGINE RUN TO TAKEOFF POWER WAS THEN PERFORMED WITH INDICATION WITHIN LIMITS. 2L74 4F4 F A20WE E3NE 20040823000842004082300084CE 2004 8 23 HAEA200400165 120040818A321023271004 LANDING GEAR LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE MAIN LACK OF LUBE E HAEAC ABORTED TAKEOFF W INADEQUATE Q C TOTAKEOFF 1 SW05324TW1138911389 324 LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT RETURNED TO BASE. MAINTENANCE LUBED LANDING GEAR AND PERFORMED GEAR SWING. CYCLED GEAR AT LEAST 20 TIMES WITH NO FAILURE. MAINTENANCE ITEM CLEARED. [CLOSED] 2L72 4J4 J A10CE 1E16 20040823000892004082300089NM 2004 8 23 200418 120040804A3260 PROXIMITY SENSOR DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE MLG DIRTY A KPVAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13808WP 026 AFTER GEAR UP SELECTION, RED NOSE GEAR LIGHT ILLUMINATED AND GEAR HANDLE ILLUMINATED AND STARTED FLASHING ON AND OFF. NO OTHER CAUTION LIGHTS ILLUMINATED. (MECHANIC) INSPECTED AND CLEANED NOSE GEAR PROXIMITY SENSOR AND PERFORMED TEST PROCEDURE IAW MM 62-61-00 PG. 202 SECTION D. NO DEFECT NOTED. 2H72 4T4 TRTA13NM E20NE 20040823001072004082300107SO 2004 8 23 LR7A04070 120040716A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND BELLY TO RT MLG WHEEL WELL SKIN CRACKED AT FS 537, RBL 43, WL 135. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2037. 2H74 4T4 T A1SO E282 20040823001092004082300109SO 2004 8 23 LR7A04072 120040716A53213567367 FLOOR PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5211, FOUND RAMP DOOR CENTER ACCESS FLOOR PANEL WARPED AT FS 809 - 856. CENTER FLOOR PANELS AT FS 809-832 AND FS 832-856 REPLACED IAW SRM SMP 583 CHP 51-60 & 51-70. DRC 2042. 2H74 4T4 T A1SO E282 20040823001382004082300138EA 2004 8 23 ASOA04429 120040613A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11877AS 7579 FLT 4542 - DURING A GROUND INSPECTION IN ATL, THE RIGHT FORWARD EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS NR 2 INVERTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040823001482004082300148NM 2004 8 23 USAA040354 120040722A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU52038 23380 PIT - FOUND FORWARD PRESSURE BULKHEAD CRACKED APPROX 1 INCH, STATION 178 FPBH, WL 218, LBL 10. REPAIRED UNDER EO 5300V153 UNDER INSPECTION PROGRAM. (M) 2L72 4F RTA16WE 20040823001602004082300160EA 2004 8 23 ASOA04520 120040719A14204871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11828AS 7213 FLT 4460 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTING AT ROWS 9 TO 14 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT CONNECTOR, FLEX LAMP P/N 362624, AT ROW 10, CABLE ASSY AT ROWS 9-14, AND THE FLOOR TRACK COVER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040823001702004082300170NM 2004 8 23 AMTA200400911 120040722A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 AFT EGRESS LIGHTING INOPERATIVE. RECONNECTED WIRE ON AFT EGRESS LIGHTS. OPS CHECK OK. (M) 2L72 4F RTA2NM 20040823001752004082300175NM 2004 8 23 UPS04242968 120040726A5320 ANGLE BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, ON REMOVAL OF RIGHT CONTROL COLUMN, CRACK FOUND ON SUPPORT ANGLE AT I/B SIDE OF COLUMN CUTOUT IN FLOOR, COMING FROM ANCHOR NUT HOLE. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-30-2. 2L73 4F A3WE 20040823001822004082300182NM 2004 8 23 UPS04M42932 120040617A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, HORIZONTAL STAB LEFT NR 30 BARREL NUT NR 30 HOLE FOUND CORRODED ON BOTTOM BEARING & SIDEWALL SURFACE. CORROSION AT BARREL NUT HOLE NR 30 LEFT, REMOVED & REAMED TO 1.178 INCH DEEP & BLEND OUT TO 0.010 INCH DEEP FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB PER EN:1218-04. APPLIED SEALANT PR1422B2 AT BARREL NUT NR 30 LEFT. REPAIR & INSTALLED SLEEVE BUSHING AT BARREL NUT NR 30 LEFT PER EO MD11-5510-19409 -G & EN:1218-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20040823001832004082300183NM 2004 8 23 UPS04M42933 120040611A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP INSPECTION TYPE:C, RIGHT HORIZONTAL STAB NR 32 BARREL NUT HOLE FOUND CORRODED. CORROSION ON BEARING S/W SURFACE REMOVED & REAMED TO 1.178 INCH & BLEND TO 0.035 INCH FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB PER EO MD11-5510-1 9409-G. PR1422B2 SEALANT APPLIED PER EN1211-04. REPAIR & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 32 RIGHT PER EO MD11-5510-19409-G. REPAIR CUTOUT AT B/N HOLE NR 32 RIGHT PER EO MD11-5510-19409-G &EN1211-04, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040823001942004082300194WP 2004 8 23 AALA20040864 120040819A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217547A 53029 DEN - OVERHEAD EMERGENCY LIGHTS AT SEATS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK M5107 FOR OVERHEAD EMERGENCY LIGHTS AT SEATS 27 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040823001952004082300195NM 2004 8 23 SWAA042388 120040817A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29772SW 27880 DURING SCHEDULED RON, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040823001982004082300198 2004 8 23 SWAA042391 420040819A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040825000242004082500024NM 2004 8 25 04235429 120040822A2110 PSU DORNERDO32 DO328300 NM CABIN MALFUNCTIONED A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27429FJ 3194 ABORTED TAKEOFF AT LOW SPEED DUE TO WATER LEAK FROM OVERHEAD BINS AT REAR OF CABIN. OPS CHECK IAW 21-10-00. NO DEFECT NOTED. FLIGHT REDEPARTED. 2H72 4T RTA55NM 20040825000252004082500025EA 2004 8 25 04233620 120040820A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX DEFECTIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27620BR 7179 PASSENGER DOOR HARD TO OPEN. OPS CHECK, NO TROUBLE FOUND. 2L72 4F RTA21EA 20040825000322004082500032EA 2004 8 25 MASA200400365 120040617A3230601R75206602K1 RESTRICTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0775996 7357 ASH 2914 JAX. LANDING GEAR UNSAFE AND NOSE LANDING GEAR DOOR INDICATION IN FLIGHT. MESSAGES DID CLEAR UNDER ITS OWN POWER AND LANDED WITHOUT INCIDENT. MX REPLACED THE EXT/RET RESTRICTOR VALVE. 2L72 4F RTA21EA 20040825000332004082500033EA 2004 8 25 MASA200400372 120040627A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX MALFUNCTIONED A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0777260 7260 ASH 6311 SBP-PHX. UPON ARRIVAL INTO PHX THE CREW WROTE UP THE MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE AND CANNOT OPEN FROM THE OUTSIDE. MX FOUND NO DEFECTS AND THE DOOR OPERATED NORMALLY. 2L72 4F RTA21EA 20040825000492004082500049EA 2004 8 25 MASA200400300 120040528A2612 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA APU BAY MALFUNCTIONED A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW07571ML 7209 ASH 2803 PIT. APU FAULT ON EICAS WITH MOMENTARY FIRE WARNING IN FLIGHT. NO EVIDENCE OF FIRE WAS FOUND. MX RESET THE APU CONTROL UNIT. BOTTLES WERE NOT DISCHARGED, NO FURTHER FAULTS WERE NOTED. NO PARTS. 2L72 4F RTA21EA 20040825000532004082500053WP 2004 8 25 MWEA040148 120040823A53403957317501 FITTING DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FLOOR SUPPORT FITTINGS AT FRAME STATION 430 BETWEEN NUMBER 30 AND 29 RIGHT LONGERON HAS MODERATE CORROSION ON THE UPPER SURFACE, ALSO NUT PLATES ARE CORRODED. FABRICATED AND INSTALLED FITTING AND INSTALLED TWO EACH NUT PLATES. 2L72 4F A6WE 20040825000542004082500054WP 2004 8 25 MWEA040149 120040823A53475936663405 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 AFT BAGGAGE PIT, RIGHT SEAT TRACK BETWEEN STATION 1212 AND 1325 HAS SEVERAL AREAS OF CORROSION. FABRICATED AND INSTALLED TRACK. 2L72 4F A6WE 20040825000562004082500056NM 2004 8 25 P5CA0401176 120040629A5524 STIFFENER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE ELEVATOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 STIFFENER CORRODED ON O/B SIDE ELEV, STA 406-5 LEFT HORIZONTAL STAB. REMOVED CORROSION FOUND OUT OF LIMIT PER SRM 55-20-01. REMOVED AND REPLACED STIFFENER AS PER SRM 51-30-02. 2L74 4F4 F A20WE E3NE 20040825000582004082500058EA 2004 8 25 MASA200400339 120040615A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STIFF A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0737178 7178 ASH 6266 PHX. THE PILOT REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE LUBRICATED THE CABIN DOOR. OPS CHECKED GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040825000602004082500060EA 2004 8 25 MASA200400316 120040605A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAILED A MASAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SW0747202 7202 ASH 2608 PHL. LAV SMOKE DETECTOR DID NOT ACTIVATE WITH PASSENGER CAUGHT SMOKING IN THE LAV. MX OPS CHECKED THE DETECTOR AND FOUND NO DEFECTS. NO PARTS USED. 2L72 4F RTA21EA 20040825000642004082500064NM 2004 8 25 SWAA042415 120040821A551265C25727 SKIN BOEING737 7373H4 1384600NM STABILIZER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND LT HORIZONTAL STAB LOWER SKIN AT STATION 144, RT STATION 117, AFT SPAR CRACKED. REPAIRED STAB SKIN PER SRM. 2L72 4F RTA16WE 20040825000662004082500066NM 2004 8 25 SWAA042418 120040821A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040825000672004082500067NM 2004 8 25 SWAA042419 120040821A53116546593 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500A, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040825000682004082500068 2004 8 25 SWAA042420 420040821A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040825000702004082500070NM 2004 8 25 SWAA042422 120040821A534065C346701 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR HINGE BOX PER SRM. 2L72 4F RTA16WE 20040825000722004082500072NM 2004 8 25 QXEA200400574 120040801A3097 WIRE HARNESS DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09356PH 502 SEA - FLIGHT 2056 - WHILE DEPARTING RDM THROUGH ABOUT -8 C, SELECTED ANTI-ICE A COUPLE OF MINUTES GOT A LEFT ELEVATOR HORN HEAT LIGHT. RAN CHECKLIST THEN ELECTED TO TURN OFF ELEVATOR HORN HEAT MINUTES LATER. TURNED IT BACK ON TO SEE IF IT WAS COOLED AND FUNCTIONAL. THIS TIME RIGHT ELEVATOR HORN HEAT CAUTION ILLUMINATED. CYCLING PRODUCED NO CHANGE AND A RIGHT ELEVEATOR HORN HEAT EVERY TIME. MAINTENANCE REPLACED WIRE HARNESS (SYDS-30-001-2) FOR RIGHT ELEVATOR HORN IAW STANDARD PRACTICES. PERFORMED ELEVATOR HORN SYSTEM TEST IAW AMM 30-16-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825000752004082500075NM 2004 8 25 QXEA200400559 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - CAMLOCK RECEPTACLE CORRODED OUTBOARD FLOORBOARD FLANGE OF SEAT TRACK NR 7 AT X243. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040825000802004082500080NM 2004 8 25 SWAA042402 120040819A53206920158 WEB BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 188 TO BS 196, STRINGER 17R, STRINGER 17L, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20040825000822004082500082NM 2004 8 25 SWAA042404 120040819A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND STRINGER 2L AT BS 380, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040825000842004082500084NM 2004 8 25 QXEA200400564 120040725A33506104789 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09379PH16905552 530 PSC - EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR AND LEFT HAND FORWARD EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PS1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825000852004082500085SO 2004 8 25 C2XA04IA104 120040818A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSDISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139556586 615 145075 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS ALL IAW EMB-145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825000862004082500086NM 2004 8 25 QXEA200400560 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - CORROSION AROUND CAMLOCK RECEPTACLE HOLES OUTBOARD FLOORBOARD FLANGE OF SEAT TRACK NR 7 AT X295 AND X310. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040825000902004082500090NM 2004 8 25 QXEA200400550 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING ON THE FLOORBOARD SUPPORT FLANGE AT APPROXIMATELY STATION 246. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20040825000932004082500093NM 2004 8 25 P5CA0401149 120040809A5330 SKIN BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LWR FUSELAGE PANEL NR 1913, EXTENSION SIDE HAS DELAMINATION. REMOVED DAMAGED AREA PER SRM 51-40-15, REPAIR PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825000952004082500095NM 2004 8 25 04213423 120040731A2430 GENERATOR DORNERDO32 DO328300 NM LEFT INOPERATIVE A VTZAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 EA27423FJ 3181 LOW SPEED ABORT DUE TO LT GENERATOR FAILURE. THE DC GENERATOR WAS REMOVED AND REPLACED. 2H72 4T RTA55NM 20040825000962004082500096NE 2004 8 25 QXEA200400561 220040721A72304114T15P02 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE VIBRATION A QXEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09600QX5120 10005 965223 BOI - FLIGHT 2520 ON CLIMB, RIGHT ENGINE N1 VIBRATION 1.8. REDUCED POWER/CHECKLIST, DROPPED TO 1.3. MAINTENANCE COMPLIED WITH INSPECTION OF FAN BLADES, LOOSENED STIFF BLADE. COMPLIED WITH VIBRATION CHECK, WITHIN LIMITS. PLACED ON RSI TO LUBE FAN BLADE TANGS IN NEXT 10 FLIGHT HOURS. MAINTENANCE REPLACED NR 2 ENGINE FAN BLADES IAW HORIZON AIR EO R-52-218. PERFORMED VIBRATION CHECK IAW CRJ MM TASK 71-00-00-720-806. OPERATIONAL CHECK GOOD. MAXIMUM VIBRATION .3 AT TOGA. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040825000972004082500097NM 2004 8 25 QXEA200400543 120040718A36207786863 SHUTOFF VALVE DHAV DHC8 DHC8202 2809007NM ZONE 600 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09345PH13523 476 PDX - FLIGHT 2228 NR 2 BLEED HOT MASTER CAUTION LIGHT CYCLES ON AND OFF. STOPPED CYCLING AFTER RUNNING CHECKLIST. CYCLING WOULD STOP ONLY WITH NR 2 BLEED OFF. MAINTENANCE REPLACED NR 2 HPSOV. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825000982004082500098NM 2004 8 25 QXEA200400539 120040713A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX - INBOARD FORWARD SEAT TRACK NR 4 HAS AREAS OF HEAVY CORROSION FROM STATION 201.000 TO 359.400. REPAIRED IAW RD 8-53-4473 AND RD 8-53-1102. 2H72 4T RTA13NM 20040825001002004082500100EA 2004 8 25 QXEA200400541 120040715A3080 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09609QX 10031 DEN - FLIGHT 4183 ANTI ICE DUCT WARNING MESSAGE. SYNOPTIC PAGE INDICATED LEFT WING AFFECTED. MESSAGE EXTINGUISHED WHEN TURNING WING ANTI ICE OFF PER CHECKLIST. MAINTENANCE COMPLIED WITH LEAK TEST OF WING ANTI ICE DUCTS. NO LEAKS NOTED. COMPLIED WITH OP TEST OF WING ANTI ICE CONTROL AND INDICATIONS. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825001012004082500101NM 2004 8 25 QXEA200400542 120040717A3010 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM DE ICE SYS ILLUMINATED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09402QX 4032 BOI - FLIGHT 2303 DE-ICE PRESSURE CAUTION LIGHT CAME ON AFTER AIRFRAME MODE SELECTED TO SLOW POSITION. AFTER CHECKLIST PROCEDURE, CAUTION LIGHT WENT OUT. LATER TURNED MODE SWITCH TO SLOW AGAIN AND DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. MAINTENANCE COMPLIED WITH MAINTENANCE PROCEDURE AND ALL OPS CHECK GOOD. DEFERRED IAW MEL 30-10-2(B). 2H72 4T RTA13NM 20040825001052004082500105NM 2004 8 25 QXEA200400584 120040806A5320 BRACKET DHAV DHC8 DHC8202 2809007NM ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - CRACKED BRACKET UNDER MAIN CABIN DOOR THRESHOLD APPROXIMATELY STATION X242.2. REPAIRED IAW DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040825001062004082500106NM 2004 8 25 QXEA200400581 120040806A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - CORROSION AT X252.300, X266.00, X280.00, X312.00, X240.50, X242, X234, X232, X244 AND X246. REPLACED NR 4 SEAT TRACK IAW RD 8-53-1102 AND DHC-8 SRM 51-40-11. 2H72 4T RTA13NM 20040825001092004082500109NM 2004 8 25 04219417 120040806A2913 PUMP DORNERDO32 DO328300 NM HYDRAULIC SYSTEMDEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27417FJ 3174 HYD PUMP A-FAILURE ON TAKEOFF AND GEAR WOULD NOT RETRACT. MX REMOVED AND REPLACED MAIN PUMP ASSY, OPS CHECK GOOD (JIC 29-11-04). PERFORMED MX PRACTICES AFTER EMERGENCY EXTENSION (JIC 32-31-00). 2H72 4T RTA55NM 20040825001102004082500110EA 2004 8 25 04232709 120040819A3010 THERMAL SWITCH CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM DEFECTIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27709BR 7850 ABORTED TAKEOFF DUE TO RIGHT WING ANTI ICE MESSAGE. REMOVED AND REPLACED THERMAL SWITCH. 2L72 4F RTA21EA 20040825001112004082500111NM 2004 8 25 04230427 120040817A3350 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27427FJ 3192 EMERGENCY FLOOR LIGHTING INOP. REMOVED AND REPLACED 5LK POWER SUPPLY. 2H72 4T RTA55NM 20040825001122004082500112SO 2004 8 25 C2XA04IA097 120040813A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727523 145389 IAH - FLIGHT 2070, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A CEILING PANEL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040825001132004082500113SO 2004 8 25 C2XA04IA098 120040813A3350602044 SIGN EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 CLE - FLIGHT 3473, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW 12 EMERGENCY EXIT FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040825001152004082500115NM 2004 8 25 P5CA0401141 120040812A5246 ACCESS PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 REFUELING PANEL 521BB IS DELAMINATED INSIDE RIGHT WING. REMOVED DELAMINATED AREA PER SRM 51-40-04, REPAIRED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825001172004082500117NM 2004 8 25 P5CA0401146 120040809A5320 SUPPORT ANGLE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FAIRING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CORROSION ON FWD SIDE OF WING TO BODY FAIRING SUPPORT ANGLE, AT BS 980 & AT RBL 36 AT I/B END OF PANEL 192. REMOVED CORROSION AREA PER 51-10-01 & SRM 51-30-02, FABRICATED REPAIRED. 2L74 4F4 F A20WE E3NE 20040825001182004082500118NM 2004 8 25 P5CA04011053 120040806A5345 STOP FITTING BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 STOP FITTING STA 1490 L1 BL20 HAS CORROSION AFT PIT. REMOVED FASTENERS TO FOM IAW 51-40-02, REMOVED CORROSION, MAX MATERIAL REMOVED IAW 53-10-01, OK TO TREAT. 2L74 4F4 F A20WE E3NE 20040825001192004082500119NM 2004 8 25 P5CA0401143 120040811A5320 FLOOR SUPPORT BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 BULK CARGO FLOOR SUPPORT IS CRACKED AT STA 240. REMOVED DAMAGED AREA, FABRICATED SUPPORT ANGLE & SPLICED IN PER SRM 57-30-02 & SRM 53-11-03, 51-10-02 & 51-10-06. 2L74 4F4 F A20WE E3NE 20040825001202004082500120NM 2004 8 25 P5CA0401144 120040809A5414 NOSE COWL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 NR 2 ENGINE NOSE COWL T/E TO CORE COWL HAS DELAMINATION. REPAIRED PER SRM 54-31-03. 2L74 4F4 F A20WE E3NE 20040825001252004082500125EA 2004 8 25 COMA0460452 120040813A5320601R35031241 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01409CA 7441 LEFT HAND ANGLE CRACKED, IAW REO 601R-53-61-004 REV B. 2L72 4F RTA21EA 20040825001262004082500126EA 2004 8 25 04176665 120040624A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27665BR 7534 DURING INSPECTION THE LEFT HAND FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825001282004082500128NM 2004 8 25 04230429 120040817A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27429FJ 3194 FLOOR EMERGENCY LIGHTING INOPERATIVE. 2H72 4T RTA55NM 20040825001292004082500129NM 2004 8 25 P5CA0401152 120040805A5330 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FUSELAGE FITTED PANEL 199BR HAS DELAMINATED. REMOVED DAMAGED AREA, REPAIRED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825001312004082500131NM 2004 8 25 P5CA0401139 120040809A5350 FAIRING BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE WING TO BODY DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DAMAGED TO WING TO BODY FAIRING PANEL 192RR. REMOVED DAMAGED AREA REPAIR PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825001322004082500132NM 2004 8 25 P5CA0401140 120040809A5320 SUPPORT ANGLE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CORROSION AT FUSELAGE EXTERNAL STRUCTURE, AT STA 1180 AFT OF LWR BEACON. REMOVED SUPPORT ANGLE, FABRICATED NEW ANGLE & INSTALLED PER SRM 51-10-01. 2L74 4F4 F A20WE E3NE 20040825001332004082500133NM 2004 8 25 P5CA0401151 120040806A5414 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NACELLE WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 PANEL 453DL AREA WORN OUT THRU & CRACKED ON BACK SIDE. FABRICATED NEW PANEL PER HARDNESS & CONDUCTIVITY & SRM 51-30-02. 2L74 4F4 F A20WE E3NE 20040825001342004082500134NM 2004 8 25 QXEA200400526 120040715A3610 SWITCH BOMBDRDHC8 DHC8401 1390041NM NR 2 NACELLE FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09400QX7556 4030 PDX - FLIGHT 2318 - AFTER STARTING DESCENT, THE CREW RAN THE EMERGENCY CHECKLIST AFTER THE NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 2 NACELLE DUCT LEAK OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825001372004082500137WP 2004 8 25 MWEA040137 120040811A53209936534165 SUPPORT DOUG DC9 DC982 3022082WP CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FLOOR SUPPORT INBOARD OF FORWARD SERVICE DOOR CORRODED, SUPPORT GOES FROM STATION 150-200. FABRICATED AND INSTALLED SUPPORT. 2L72 4F A6WE 20040825001402004082500140NM 2004 8 25 QXEA200400585 120040809A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8401 1390041NM MLG DOOR OUT OF ADJUST A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09413QX6301 4060 MSO - FLIGHT 2382 - THE MAIN LANDING GEAR DOORS OPENED BRIEFLY DURING FLIGHT. THE LEFT DOOR AND RIGHT DOOR AMBER LIGHTS ILLUMINATED WITH ASSOCIATED AIR NOISE. THE DOORS WERE OPEN FOR 2 SECONDS. MAINTENANCE INSPECTED THE AIRCRAFT AND INTERROGATED THE PSEU. MAINTENANCE FOUND THE RIGGING NEAR GAP TOO FAR. THE PROXIMITY SENSOR WAS RE-RIGGED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825001412004082500141NM 2004 8 25 DL73S040754 120040811A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 A CRACK WAS FOUND AT A FASTENER HOLE IN THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUT OUT IN THE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53-1163 AND ER/A 092229-14. 2L72 4F RTA16WE 20040825001432004082500143NM 2004 8 25 DL76L040756 120040811A2121211002939 FAN BOEING767 767332 1382001NM COCKPIT OVERHEATED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27190DN 28447 CREW REPORTED BURNT SMELL FROM COCKPIT VENTS MOMENTARY AND EICAS MESSAGE LEFT RECIRC FAN WITH ASSOCIATED OFF LIGHT. REPLACED LT RECIRC FAN PER M/M, REMOVED MCO/PLAC. 2L72 4F RTA1NM 20040825001442004082500144NM 2004 8 25 DL73S040758 120040811A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 INSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACKED FASTENER HOLE AT FS 727C. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 092157 -14AD. 2L72 4F RTA16WE 20040825001462004082500146EU 2004 8 25 MALA040507 120040709A33506122941 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15525XJ E2350 BATTERY PACK P/N 61-2294-1, S/N 2634 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/11/04. 2H74 4F RTA49EU 20040825001472004082500147EU 2004 8 25 MALA040509 120040709A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15429XJ 340B429 POWER SUPPLY P/N 501-1228-04, S/N 4585 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED 12 EACH CELLS P/N 549-1324-06, UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 7/15/04. 2L72 4T RTA52EU 20040825001482004082500148EU 2004 8 25 MALA040510 120040710A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15522XJ E2347 BATTERY PACK P/N 61-2275-1, S/N 9812852 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED AND CHARGED. PASSED CMM CHECKS. A/C RETURNED TO SERVICE 7/13/04. 2H74 4F RTA49EU 20040825001492004082500149EU 2004 8 25 MALA040505 120040709A33505491324406 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15423XJ 340B423 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1833 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 549-1324-06 AND TESTED GOOD. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/12/04. 2L72 4T RTA52EU 20040825001522004082500152EU 2004 8 25 MALA040504 120040704A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15424XJ 340B424 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2036 CAUSES LIGHT TO BE INOP. REPLACED CONVERTER V2. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/8/04. 2L72 4T RTA52EU 20040825001532004082500153EU 2004 8 25 MALA040503 120040730A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15445XJ 340B445 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2158 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AND RELMS K, K2, K3. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/8/04. REFER TO WO 369561 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20040825001542004082500154EU 2004 8 25 04173316 120040621A33506134051 BATTERY JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27316UE 41055 DURING INSPECTION THE FORWARD SECTION OF EMERGENCY ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. THE BATTERY PACK WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA41NM 20040825001562004082500156EA 2004 8 25 04165638 120040613A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27638BR 7311 DURING INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND DIM. THE BATTERY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825001572004082500157NM 2004 8 25 DL764040759 120040812A25301105011 COFFEEMAKER BOEING767 767432ER 1385134NM GALLEY SPARKS A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27840MH 29717 COFFEMAKER IN AREA 206, FIRST CLASS GALLEY, SPARKING FROM COLD WATER BUTTON. REPLACED SAME. 2L72 4F RTA1NM 20040825001592004082500159EA 2004 8 25 04152632B 120040602A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING HEAVY INSPECTION THE FLOORBEAM AT FS 280 WAS FOUND CRACKED. THE BEAM WAS REPAIRED PER MANUFACTURER INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE UPON INSPECTION COMPLETION. 2L72 4F RTA21EA 20040825001602004082500160EA 2004 8 25 04154632C 120040602A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING HEAVY CHECK THE ENGINE SUPPORT BEAM LOWER WEB LEFT HAND SIDE WAS FOUND CRACKED. THE WEB WAS REPAIRED PER MANUFACTURER INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040825001622004082500162NM 2004 8 25 QXEA200400530 120040718A521085217301005 DOOR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 JAMMED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09416QX1379 4083 SEA - FLIGHT 2421 - THE CREW REPORTS THE AFT PASSENGER DOOR IS JAMMED PARTIALLY OPEN. MAINTENANCE INSPECTED THE DOOR AND UNJAMMED SAME. OPERATIONAL CHECKS OF THE AFT PASSENGER DOOR WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825001632004082500163NM 2004 8 25 04223402 120040810A3260 PSEU DORNERDO32 DO328300 NM MLG DEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27402FJ 3147 RIGHT FADEC FAULT IN THE CLIMB PHASE. AIRCRAFT RETURNED TO FIELD. MX REMOVED AND REPLACED PSEU (JIC 32-61-12). OPS CHECK GOOD. 2H72 4T RTA55NM 20040825001652004082500165SO 2004 8 25 C2XA04SH477 120040807A33507287103507 CONTROL MODULE EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT WILL NOT TEST A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2724517 145332 SHV - DURING C-CHECK THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE FROM THE FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED THE LIGHTING CONTROL MODULE IAW EMB 135 AMM 33-21-01. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040825001662004082500166SO 2004 8 25 C2XA04IA092 120040807A33502013BR BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAO OTHER L NO TEST ININSP/MAINT 1 SW27139943281 3281 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825001672004082500167SO 2004 8 25 C2XA04IA093 120040807A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAO OTHER L NO TEST ININSP/MAINT 1 SW27139942283 2283 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825001682004082500168SO 2004 8 25 C2XA04IA094 120040807A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139944347 2987 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825001702004082500170SO 2004 8 25 C2XA04IA096 120040809A332072877537 LIGHT EMB 145 EMB145ER 3260211SO CABIN BURNED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2714930 145011 CRP - FLIGHT 2207, DURING POST FLIGHT INSPECTION THE CREW REPORTED A ELECTRIC BURNING SMELL COMING FROM THE FORWARD CABIN. MAINTENANCE REMOVED THE LIGHT BULB FROM ROW 6/7, AND MEL'D THE LIGHT UNDER MEL 33-20-001 CONTROL 044887, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/10/04, IAH MAINTENANCE REMOVED AND REPLACED THE SIDEWALL LIGHT FIXTURE AT SEAT 6A, IAW EMB-145 M/M 33-21-06, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040825001712004082500171SO 2004 8 25 C2XA04BT084 120040807A335020131A BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 EWR LOG SQUAWK HALF OF AISLE PATH LIGHTS OUT. REMOVED AND REPLACED NR 2 BATTERY PACK IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4F RTT00011AT 20040825001732004082500173NM 2004 8 25 SWAA042334 120040813A53306545776 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C2 CHECK, FOUND TEAR STRAP AT BS 890, STRINGER 24R, CRACKED. REPAIRED STRAP PER EA. 2L72 4F RTA16WE 20040825001762004082500176NM 2004 8 25 SWAA042335 120040814A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 550B, STRINGER 16L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040825001812004082500181 2004 8 25 AALA20040856 420040817A2565D30654122 SLIDE BOEING757 757223 1384957NM L1 DOOR DISLODGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21610AA 24486 MIA - L1 SLIDE PARTIAL UNSUCCESSFUL DEPLOYMENT. SLIDE FELL OUT ON JETBRIDGE. DOOR ASSIST BOTTLE DISCHARGED UPON ARRIVE AT GATE WHEN DOOR WAS BEING OPENED BY GROUND CREW. FOUND GIRT BAR ENGAGED DURING INSPECTION. REPLACED SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040825001832004082500183 2004 8 25 AALA20040859 420040817A2565 SLIDE AIRBUS300 A300B4605R 3930308EU L1 DOOR DEPLOYED A AALAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW217055A 462 CUN - L1 DOOR SLIDE PARTIALLY DEPLOYED ON JETBRIDGE WHEN DOOR OPENED BY FLIGHT ATTENDANT. REPLACED THE L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040825001842004082500184NM 2004 8 25 P5CA0401174 120040815A324140805 TRANSDUCER BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE ANTI SKID SYS FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23508MC 21644 AUTO BRAKES INOP. REPLACED ANTI-SKID TRANSDUCER NR 3 POSITION, SPIN CHECK NORMAL (NO LIGHT ILLUMINATE PER MM 32-43-00). 2L74 4F4 F A20WE E23EA 20040825001872004082500187NM 2004 8 25 P5CA0401172 120040816A3030 RELAY BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL AOA HEAT FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23453PA 30811 EICAS MESSAGE ON ENGINE START L AOA HEAT & R AOA HEAT. RESET RELAYS R1423 & R1424, PERFORMED GROUND TEST PER MM 30-31-00 & ENGINE RUNUP PER 71-00-00, OPS CHECK NORMAL. 2L74 4F4 FRTA20WE E23EA 20040825000262004082500026EA 2004 8 25 MASA200400285 120040523A5210 MECHANISM CNDAIRCL600 CL6002C10 1390015EA PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07509MJ 10094 ASH 7111 IAD. A PAX DOOR DIFFICULT TO OPEN. MX LUBED DOOR MECHANISM. NO FURTHER FAULTS WERE FOUND. NO PARTS USED. 2L72 4F RTA21EA 20040825000442004082500044EA 2004 8 25 MASA200400269 120040517A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0777278 7278 ASH 6156 PHX. AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT RETRACT. MX ADJUSTED A KNOCKED OUT OF POSITION EXTENSION PROX SENSOR. DID A GEAR SWING AND OPS CHECKED GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040825000592004082500059EA 2004 8 25 MASA200400352 120040618A2611YE4N023 RELAY CNDAIRCL600 CL6002B19 1900309EA SMOKE WARNING INOPERATIVE A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW077264V 7264 ASH 6110 PHX. CARGO SMOKE WARNING INTERMITTENT. MX REPLACED THE K7HL RELAY. 2L72 4F RTA21EA 20040825000632004082500063NM 2004 8 25 SWAA042414 120040821A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RIGHT WING NR 6 L/E SLAT SKIN PER SRM. 2L72 4F RTA16WE 20040825000692004082500069NM 2004 8 25 SWAA042421 120040821A5552183A8410 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSHING AND HARDWARE PER MM. 2L72 4F RTA16WE 20040825000732004082500073 2004 8 25 04230699 420040817A2220 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB DEFECTIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27699BR 7801 STAB TRIM FAILURE. DECLARED EMERGENCY AND DIVERTED TO HSV. LANDED UNEVENTFULLY. RESET HSTCU IAW CRJ FIM. 2L72 4F RTA21EA 20040825000782004082500078NM 2004 8 25 SWAA042400 120040819A3350OL307IBPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED MV3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS AT ROWS 13 ABC, 22 ABC, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM. 2L72 4F RTA16WE 20040825000992004082500099NM 2004 8 25 QXEA200400540 120040715A5320 STRAP DHAV DHC8 DHC8202 2809007NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX - GOUGE IN SPLINE STRAP, X264.10 NEXT TO RIGHT HAND FORWARD EMERGENCY EXIT DOOR, Z155.55, .022 DEEP .175 DIAMETER. REPAIRED IAW HORIZON AIR EA 2-53-565. 2H72 4T RTA13NM 20040825001032004082500103NM 2004 8 25 QXEA200400579 120040806A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - LEFT INBOARD SEAT TRACK NR 5 ATTACH AREA APPROXIMATELY X500.00 HAS CORROSION. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-4472. 2H72 4T RTA13NM 20040825001082004082500108EA 2004 8 25 04210620 120040727A5210 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LEAKING A VTZAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 EA27620BR 7179 MAIN CABIN DOOR SQUEAL. PLANE RETURNED TO FIELD AND PASSENGERS WERE DEPLANED AT THE GATE. 2L72 4F RTA21EA 20040825001212004082500121NM 2004 8 25 P5CA0401147 120040809A5350 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 PANEL NR 194 LR DELAMINATED IN SEVERAL PLACES. REMOVED DAMAGE & PREP PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825001222004082500122NM 2004 8 25 P5CA0401156 120040805A5350 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FUSELAGE FITTER PANEL NR 192 EER HAS DENT & DELAMINATION. REMOVED & CLEANED DAMAGED AREA PER SRM 51-40-15, APPLIED CURVED FIBERGLASS REPAIR SRM 51-40-03. 2L74 4F4 F A20WE E3NE 20040825001422004082500142NM 2004 8 25 DL73S040755 120040811A5315 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27308DL 23080 THE UPPER CAP OF THE FS 294.5 FLOORBEAM WAS FOUND CRACKED OUTBOARD OF RBL 45. THE DAMAGED SECTION OF CAP WAS CUT OUT AT RBL 28.5 AND A NEW SECTION SPLICED IN PER ER/A 092282-14. 2L72 4F RTA16WE 20040825001512004082500151EU 2004 8 25 MALA040508 120040709A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15525XJ E2350 BATTERY PACK P/N 61-2275-1, S/N 9812870 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 7/11/04. 2H74 4F RTA49EU 20040825001582004082500158EU 2004 8 25 AWXA200400689 120040626A5270 ACCESS PANEL AIRBUS320 A320231 3930325EU LT OVERWING OUT OF ADJUST A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28629AW 076 PHX - ABORTED TAKEOFF - FLT 0524 - AT LOW SPEED TAKEOFF, REJECTED TAKEOFF AT 40 KTS DUE TO INDICATION RELATED TO THE LT OVERWING EMERGENCY EXIT LIGHT ILLUMINATED. MAINTENANCE RE-INSTALLED THE LT OVERWING EXIT HATCH ACCESS PANEL AND ADJUSTED PROPERLY. OP'S CHECK AND INDICATION CHECKED GOOD. 2L72 4F RTA28NM 20040825001692004082500169SO 2004 8 25 C2XA04IA095 120040807A33502013BR BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139943131 1320 145291 IAH - FLIGHT 2699, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825001882004082500188NM 2004 8 25 P5CA0401168 120040810A5320 SUPPORT BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CORROSION ON SUPPORT STRUCTURE STA 940 LBL 3 TO RBL 3 REF KEEL BEAM AREA. REMOVE CORROSION AREA, FABRICATED WEB FLANG SRM 53-50-04, INSTALLED PER SRM 51-30-05. 2L74 4F4 F A20WE E3NE 20040825001892004082500189NM 2004 8 25 P5CA0401169 120040814A5343 FITTING BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CORROSION ON RIGHT MLG FITTING BB 1480 RBL 22. REPAIRED AREA PER SAA SK 920-001(SR)FAA FORM 811-3. 2L74 4F4 F A20WE E3NE 20040825001912004082500191SO 2004 8 25 C2XA04BT085 120040807A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 MCI LOG SQUAWK FWD OVER THE WING AISLE EXIT LOCATOR SIGN INOP. REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040825001922004082500192SO 2004 8 25 C2XA04BT086 120040808A3350 LIGHT EMB 145 EMB145ER 3260211SO CABIN MALFUNCTIONED A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2715932 145015 ATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHECK OK IAW EMB AMM 33-50-00. 2L72 4F RTT00011AT 20040825001932004082500193SO 2004 8 25 C2XA04BT087 120040811A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714904 145477 EWR LOG SQUAWK OVERHEAD EMERGENCY LIGHT BETWEEN ROW 7 AND 8 OUT. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BULB IAW EMB MM 33-50-08. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040825001952004082500195SO 2004 8 25 C2XA04IA099 120040815A3350602043 SIGN EMB 145 EMB145XR 3260214SO EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 RIC - DURING MAINTENANCE INSPECTION, THE FLOOR EXIT LIGHT AT ROW 12 RT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20040825001972004082500197NM 2004 8 25 P5CA0401170 120040814A5410 FRAME BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NACELLE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FRETTING & CRACKS IN FRAME AFT EDGE OF HYD COMPT. CUT OUT DAMAGE AREA PER SRM 53-10-04, FABRICATED ANGLE & PLATE INSTALLED PER SRM 53-10-02. 2L74 4F4 F A20WE E3NE 20040825001982004082500198EU 2004 8 25 AWXA200400675 120040605A5347D5337102400000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 LT INBOARD SEAT TRACK BETWEEN FR 36 AND FR 41. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 LT FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-21 FIG 11, 12 & 18. 2L72 4F RTA28NM 20040825002002004082500200EU 2004 8 25 AWXA200400676 120040604A5330D5347041020000 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FUSELAGE SKIN AT AFT IFPC ANTENNA CUTOUT BETWEEN FR 62 AND FR 63, AND STR 37 AND 63 LT. MAINTENANCE CUT OUT DAMAGED SKIN AT AFT IFPC ANTENNA; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 53-00-11 FIG 203 PG 211-216. 2L72 4F RTA28NM 20040825002012004082500201EU 2004 8 25 AWXA200400677 120040603A5347D5311283020000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK FILIFORM CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR RAIL Y81 RIGHT AT FR 16. MAINTENANCE REMOVED DAMAGED FLOOR RAIL Y81 RIGHT AT FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 51-42-11 PG 6-7. 2L72 4F RTA28NM 20040825002042004082500204EA 2004 8 25 04187703 120040705A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27703BR 7497 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825002052004082500205NM 2004 8 25 QXEA200400605 120040812A5310 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 2 HAS LIGHT CHAFING AT X 291.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1. AREA 1.0 INCH LONG, 3.8 INCHES WIDE AND .001 INCH DEEP. HFED INSPECTION AS PER 1-84-7A, PART 6 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040825002062004082500206WP 2004 8 25 AALA20040805 120040802A3230 LATCH DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21479AA 49654 MIA - INFLIGHT T1246/02 AFTER TAKEOFF GEAR FAILED TO RETRACT. RAN QRH WITH NO SUCCESS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC BY PASS HANDLE EXTENDED. ADJUSTED LOCK LATCH TAP SPRING IN LOCKING LATCH. STOWED AND LOCKED HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040825002072004082500207EA 2004 8 25 07187681 120040705A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERNAL INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27681BR 7680 DURING INSPECTION THE LEFT HAND AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE LIGHT WAS FOUND INOPERATIVE. 2L72 4F RTA21EA 20040825002082004082500208NM 2004 8 25 P5CA0401161 120040803A5280 SKIN BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE MLG DOOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 LEFT WING GEAR STRUT LWR DOOR AFT LWR END IS DELAMINATED AT LWR SIDE HAS EXFOLIATING CORROSION. REPAIRED IAW SRM 51-40-06 & 51-10-02. 2L74 4F4 F A20WE E3NE 20040825002102004082500210NM 2004 8 25 P5CA0401155 120040806A5350 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FUSELAGE FITTED PANEL 191WL HAS DELAMINATION ON EXTERIOR SIDE. REPAIRED PANEL 191WL PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825002112004082500211NM 2004 8 25 SWAA042406 120040820A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 8 DEF, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040825002132004082500213NM 2004 8 25 04221451 120040808A2121 FAN DORNERDO32 DO328300 NM CABIN CLOGGED A VTZAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27451FJ 3205 ON TAXI OUT, RECEIVED SMOKE LAV MESSAGE AND DARK SMOKE HAZE IN CABIN. AFT RECIRC FAN FILTER WAS CLOGGED. REMOVED AND REPLACED FILTER (21-21-01) AND PERFORMED FUNCTIONAL CHECK OF RECIRC FAN AND ECU. NO SMOKE NOTED. OPS CHECK GOOD (21-51-00). 2H72 4T RTA55NM 20040825002142004082500214 2004 8 25 04221424 420040808A3160 DISPLAY DORNERDO32 DO328300 NM COCKPIT INOPERATIVE A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27424FJ 3185 ABORTED TAKEOFF DUE TO MASTER CAUTION, CHECK PFD ON TAKEOFF ROLL, 70 KNTS. REMOVED AND REPLACED CAPT AND F/O PFD'S (31-61-00), ALL OPS CHECK GOOD AT THIS TIME. 2H72 4T RTA55NM 20040825002182004082500218NM 2004 8 25 AWXA200400717 120040620A532065528942 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND IN LOWER INBOARD FORWARD RADIUS OF FLOORBOARD CHANNEL CROSSBEAM AT BS 540, BL -0-. MAINTENANCE REMOVED AND REPLACED CRACKED FLOORBOARD CHANNEL ASSEMBLY AT BS 540, BL -0- IAW B737-300 BMM 20-50-11-2 FIG 202. 2L72 4F RTA16WE 20040825002192004082500219NM 2004 8 25 AWXA200400718 120040619A534069353642 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 312, STR 23 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 312, STR 23 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12. 2L72 4F RTA16WE 20040825002202004082500220NM 2004 8 25 AWXA200400719 120040619A534069353643 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 1006, STR 25 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, STR 25 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12. 2L72 4F RTA16WE 20040825002222004082500222NM 2004 8 25 AWXA200400721 120040620A5311654653949 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN INBOARD LEG OF LT FRAME AT BS 616, LBL 65, WL 201. MAINTENANCE CUT OUT DAMAGED PORTION OF INNER CHORD AT BS 616, LBL 65, WL 201 AND PREFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER AND STIFFENING ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1. 2L72 4F RTA16WE 20040825002232004082500223NM 2004 8 25 AWXA200400722 120040618A532065C326772 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON LT OUTBOARD SHEAR WEB BETWEEN BS 986 & BS 1016, AND LBL 35 & LBL 43, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 986 TO BS 1016 AND LBL 35 TO LBL 43. FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20040825002252004082500225NM 2004 8 25 AWXA200400724 120040620A532065317875 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER L-1 DOOR SILL UPPER WEB FRAME BETWEEN BS 314 & BS 340, LBL 49, WL 209. MAINTENANCE REMOVED CORRODED L-1 DOOR SILL UPPER WEB FRAME FROM BS 314 TO BS 340, LBL 49. FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-31787; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 2-3, 8 & 12. 2L72 4F RTA16WE 20040825002272004082500227NM 2004 8 25 AWXA200400749 120040620A53206545834255 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 310, RBL 11, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT STIFFENER AT BS 310, RBL 11. FABRICATED A NEW REPLACEMENT STIFFENER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 12. 2L72 4F RTA16WE 20040825002282004082500228NM 2004 8 25 SWAA042407 120040820A30402315 CONTROLLER BOEING737 7373H4 1384600NM WINDOW HEAT ARCED A SWAAO OTHER O OTHER CRCRUISE 1 SW29336SW 23940 AT FL 290, RIGHT COCKPIT NR 2 WINDOW PANE SHATTERED, ARCHING NOTED. REMOVED AND REPLACED RIGHT COCKPIT NR 2 WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20040825002292004082500229 2004 8 25 SWAA042408 420040820A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR PER MM. 2L72 4F RTA16WE 20040825002312004082500231NM 2004 8 25 SWAA042410 120040820A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 760, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040825002322004082500232 2004 8 25 SWAA042411 420040820A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040825002332004082500233NM 2004 8 25 SWAA042412 120040820A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 4, 5, 6 L/E SLATS SKIN CRACKED. REPAIRED RT WING L/E SLATS SKIN PER EA. 2L72 4F RTA16WE 20040825002372004082500237NM 2004 8 25 SWAA042425 120040821A3350D71702001 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED RON, FOUND LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040825002392004082500239NM 2004 8 25 QXEA200400533 120040714A33976519020 WIRE DHAV DHC8 DHC8202 2809007NM ZONE 100 EXPOSED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09355PH 500 PDX - FLIGHT 2151 - EMERGENCY FLOOR LIGHTING AT ROW 1 HAS EXPOSED WIRES. REMOVED AND REPLACED FORWARD SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825002402004082500240NM 2004 8 25 QXEA200400536 120040719A243023088008 GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09358PH7412 1251 506 MFR - FLIGHT 2149 - NR 2 DC GENERATOR HOT CAUTION LIGHT FLICKERING WITH ASSOCIATED MASTER CAUTION. RAN THE NR 2 DC GENERATOR HOT CHECKLIST AND LIGHT CONTINUED TO FLICKER. REMOVED AND REPLACED NR 2 STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825002412004082500241NM 2004 8 25 QXEA200400537 120040720A5260 DOOR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 LACK OF LUBE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09405QX 4047 BOI - FLIGHT 2390 - REAR AIRSTAIR DOOR IS HARD TO OPEN AND CLOSE. CLEANED AND LUBED AFT PASSENGER DOOR. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825002432004082500243NM 2004 8 25 AALA20040809 120040804A3350P4010051112 LIGHT BOEING757 757223 1384957NM ROW 26 INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21664AA 25298 SFO - EMERGENCY SEAT LIGHTS AT ROW 26 AND AFT INOPERATIVE. REPLACED EMERGENCY SEAT LIGHT ASSEMBLY AS ROW 26 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040825002442004082500244EU 2004 8 25 AALA20040810 120040805A3350BR964814 LIGHT AIRBUS300 A300B4605R 3930308EU SEAT 36G INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170072 515 JFK - EMERGENCY LIGHT INOPERATIVE AT SEAT 36G. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 36G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040825002462004082500246EA 2004 8 25 04186705 120040704A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27705BR 7470 DURING INSPECTION A CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825002472004082500247EA 2004 8 25 04184708 120040702A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27708BR 7575 DURING INSPECTION THE LEFT HAND EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825002482004082500248EA 2004 8 25 04186655 120040704A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27655BR 7457 DURING INSPECTION THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825002502004082500250NM 2004 8 25 P5CA0401157 120040804A5350 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FUSELAGE FITTING PANEL 192CO DELAMINATED ON INTERIOR SIDE. REPAIRED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825002532004082500253SO 2004 8 25 C2XA04SH483 120040816A531514521713005 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713914 145430 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED OUT OF LIMITS AT FRAME 20 IAW EMB 145 SRM 53-21-10. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825002552004082500255 2004 8 25 04203642 420040721A3420 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AHRS INOPERATIVE A VTZAO OTHER S AFFECT SYSTEMS CLCLIMB 1 EA27642BR IN CLIMB PHASE, NR 1 AHARS FAILURE. RTF AND PASSENGERS DEPLANED AT THE GATE. LEFT AHRS (1A1FP) WAS REMOVED AND REPLACED. OPS CHECK GOOD (REF 34-21-01). 2L72 4F RTA21EA 20040825002562004082500256NM 2004 8 25 AALA20040800 120040803A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21945AN 30085 MIA - EMERGENCY LIGHTS AT SEATS 27D TO BACK OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS FROM SEATS 27D TO BACK OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040825002572004082500257WP 2004 8 25 AALA20040803 120040802A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21432AA 49350 ORD - EMERGENCY LIGHT ABOVE RIGHT HAND FORWARD SERVICE DOOR AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND OVERHEAD FORWARD GALLEY SERVICE DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040825002582004082500258NM 2004 8 25 AALA20040793 120040731A2530 COFFEEMAKER BOEING757 757223 1384957NM GALLEY INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21636AM 24594 CLE - INFLIGHT T259/31 AIRCRAFT LANDED CLE WITH SMOKE REPORTED IN CABIN. FOUND BURNED WIRES IN NUMBER ONE COFFEEMAKER IN FIRST CLASS GALLEY. PLACARD NUMBER ONE COFFEEMAKER IN FIRST CLASS GALLEY AND REPLACED NUMBER ONE COFFEEMAKER IN FIRST CLASS GALLEY IN LAS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040825002592004082500259 2004 8 25 AALA20040807 420040802A25655A33073 SLIDE BOEING737 737823 13844BZNM CABIN PUNCTURED A AALAK NONE O OTHER ININSP/MAINT 1 SW21927AN 30077 TUL - EMERGENCY ESCAPE SLIDE HAS APPROXIMATELY 0.25 INCH HOLE CAUSING SLIDE TO DEFLATE. SLIDE SENT TO SHOP FOR REPAIR. REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040825002602004082500260WP 2004 8 25 AALA20040788 120040730A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217530 49922 DFW - EMERGENCY LIGHTS AT TAIL COMPARTMENT WALKWAY INOPERATIVE. REPLACED WIRES BETWEEN AL211 AND AL28 FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT WALKWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040825002672004082500267SO 2004 8 25 2004F00247 120040215A7810LW16697 PIPE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA LEFT EXHAUST CRACKED A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL013536B 317952205 L223968A THE PILOT NOTICED LOSS OF MANIFOLD PRESSURE FOLLOWED BY A LOUD RATTLING FROM THE RIGHT ENGINE. THE EXHAUST PIPE HAD BROKEN OFF ITS ATTACHMENT TO THE LEFT SIDE OF THE TURBOCHARGER TRANSITION. THE FAILURE OCCURRED IN THE FLANGE RADIUS. ALTHOUGH THERE WAS A POTENTIAL FOR FIRE, NO EVIDENCE OF EXHAUST STAINS OR HEAT DAMAGE WAS DETECTED. (M) 1L72 3O3 O A20SO E14EA 20040826000022004082600002NM 2004 8 26 04FDEA02363 120040804A5510ALC81062 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RIGHT HAND NR 14R BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. RIGHT HAND HORIZONTAL STABILIZER, BARREL NUT BORE NR 14R FITTING REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. 2L73 4F RTA22WE 20040826000042004082600004SO 2004 8 26 C2XA04CL081 120040817A335078241 INVERTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 CREW REPORTED THAT THE EMERGENCY LIGHTS WILL NOT TURN ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE POSITION 6 EMERGENCY LIGHT INVERTER. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040826000062004082600006SO 2004 8 26 C2XA04TY148 120040806A531514522460013 FLOORBEAM EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOPCAP AT FRAME 22. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F4 FRT TE6CH 20040826000082004082600008SO 2004 8 26 C2XA04TY151 120040810A531514529150001 ATTACH BRACKET EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CABIN TO GALLEY STEP-UP PLATE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F4 FRT TE6CH 20040826000102004082600010WP 2004 8 26 I5HA0358AAA 120040325A323085101D RELAY CVAC 340 340CVAC 242270AWP MLG INOPERATIVE A I5HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23584E 24 AFTER TAKEOFF FROM PIT EN ROUTE TO CVG, THE CREW WAS UNABLE TO RAISE THE LANDING GEAR HANDLE DUE TO THE 'UNLOCK SOLENOID' NOT RETRACTING. THE AIRCRAFT RETURNED TO PIT WHERE IT LANDED SAFELY. THE AIRCRAFT WAS FERRIED TO THE AIR TAHOMA, INC MAINTENANCE BASE IN COLUMBUS, OHIO WITH THE LANDING GEAR DOWN. THE NR 1 'UNLOCK RELAY' WAS REMOVED AND REPLACED THE AIRCRAFT WAS RETURNED TO SERVICE ON MARCH 25, 2004. (M) 2L72 4R 6A6 20040826000112004082600011EA 2004 8 26 ASOA04483 120040626A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA FLAPS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11927EV103981972 7844 FLT 4456 - DURING APPROACH INTO DFW FROM LBB, WHEN SELECTING THE FLAPS TO 45 DEGREES THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE INDICATIONG A FAILURE AT 30 DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY WAS DECLARED AS A PRECAUTION FOR EMERGENCY EQUIPMENT TO BE ON STANDBY. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS ELECTRONIC CONTROL UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040826000122004082600012NM 2004 8 26 04FDEA02537 120040821A5510 STRUCTURE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO COMPLY EA NR 1-5510-79807, STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE'S REWORKED BEYOND MFG S/B MD-11 55-023 REVISION 2 AND EO NR 1-5510-7-5000 LIMITS, MASTER EA COMPLIED WITH FEDEX E.A. NO. 1-5510-79807, STABILIZERS - HORIZONTAL STABILIZER BARREL NUT BORE'S REWORKED BEYOND BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO NR 1-5510-7-5000 LIMITS - MASTER E.A. 2L73 4F4 FRTA22WE E31N3 20040826000132004082600013NM 2004 8 26 2004UALA00687 120040722A2930285U0032 CIRCUIT CARD BOEING747 747422 1384935NM PWA 4056 PW4056 NE HYD INDICATOR MALFUNCTIONED A UALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29193UA 26890 THE NR 4 HYDRAULIC SYSTEM LOSS OF PRESSURE AND FLUID. QUANTITY AND PRESSURE FLUCTUATIONS DUE TO FAULTY HYDIM CARD. CARD REPLACED. AIRCRAFT HAS HAD NO FURTHER HYDRAULIC INDICATION PROBLEMS FOR LAST 8 FLIGHTS. 2L74 4F4 FRTA20WE E24NE 20040826000142004082600014EU 2004 8 26 AWXA200400761 220040711A73209387M15P11 ENGINE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU NR 1 SURGES A AWXAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP28307AW4338192 24634 APPROXIMATELY 3 MIN AFTER DEPARTURE FROM SJD EN ROUTE FOR PHX THE NR 1 ENGINE STARTED SURGING BETWEEN 25 TO 30 PERCENT, TURNED BACK TO SJD, JUST PRIOR TO SHUT DOWN AS PER THE CHECKLIST, SURGING STOPPED. MAINTENANCE ISSUED MEL 73-7, COND. 1. LT PMC INOP. ON 07/13/2004 MAINTENANCE REMOVED AND REPLACED MAIN ENGINE CONTROL, ENGINE RUN OPERATIONAL CHECK WAS GOOD. VENDORS FUNCTIONAL CHECK OF MAIN ENGINE CONTROL S/N WYG1082 COULD NOT CONFIRM REASON FOR REMOVAL. ALL SCHEDULES OPERATED WITHIN CMM LIMITS. CAN ASSEMBLY WAS REMOVED TO CHECK FOR SEPARATED SPRINGS OR FOD, NO DEFECTS WERE FOUND. TEST AND INSPECTION ACCOMPLISHED IAW CMM 73-21-16. 2L72 4F4 FRTA16WE E21EU 20040826000172004082600017NM 2004 8 26 04FDEA02368 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502, MATERIAL REMOVED = 0.003, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040826000202004082600020NM 2004 8 26 04FDEA02372 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11- 02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.398. COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040827000012004082700001NE 2004 8 27 VNAA0408010 220040816A7210 CHIP DETECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE RT REDUCTION G/BFAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07440JS 3058 DURING FLIGHT, THE CREW RECEIVED A RT REDUCTION GEARBOX CHIP DETECTOR INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND FOUND ALLOWABLE DEBRIS ON THE DETECTOR. MAINTNENANCE THEN CLEANED THE CHIP DETECTOR AND REPLACED THE FILTER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040827000042004082700004NM 2004 8 27 UPS04242972 120040806A5751 CASTING BOEING727 72722C 138400FNM AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, CORROSION ON LEFT O/B AILERON I/B CASTING. CASTING REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 20040827000082004082700008NM 2004 8 27 UPS04242984 120040730A5752 SKIN BOEING727 72722C 138400FNM AILERON TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, RT I/B AILERON TAB HAS SEPARATION AT TRAILING EDGE AND DELAMINATION AT I/B & O/B ENDS. REPAIR CARRIED OUT IAW SRM 51-40-20 & MM 27-10-05 & 51-80-3. 2L73 4F A3WE 20040827000092004082700009NM 2004 8 27 UPS04242985 120040803A7120 CROSSOVER TUBE BOEING727 72722C 138400FNM NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, DURING NDT OF NR 2 ENGINE MOUNTING COMPONENTS THE CROSSOVER STRUT WAS FOUND TO BE CRACKED. REPLACED CROSSOVER STRUT IAW SRM 51-30-02. 2L73 4F A3WE 20040827000102004082700010NM 2004 8 27 UPS04242986 120040804A5340 ANGLE BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, SUSPECT CRACK ON ANGLE IN RIGHT W/W OUTBOARD OF BS 870 FITTING AT LOWER END. NEW ANGLE FABRICATED & INSTALLED IAW SRM 51-20-1 & SRM 51-30-2. 2L73 4F A3WE 20040827000132004082700013NM 2004 8 27 SWAA042438 120040821A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 11L, (R2 DOOR UPPER HINGE CUTOUT). REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040827000162004082700016NM 2004 8 27 SWAA042441 120040823A5310141A880 WINDOW POST BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED 1/4D CHECK, FOUND L1 COCKPIT WINDOW POST CRACKED AT UPPER OUTBOARD CORNER. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20040827000172004082700017NM 2004 8 27 SWAA042442 120040823A53206545409 WEB BOEING737 7373H4 1384600NM MLG W/W CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 671, LBL 42. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20040827000202004082700020NM 2004 8 27 SWAA042435 120040821A335065C34691 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT 5 DEF. RELAMPED PER MM. 2L72 4F RTA16WE 20040827000222004082700022NM 2004 8 27 SWAA042455 120040824A324426123012 TIRE BOEING737 7377H4 1384404NM NR 2 MLG SEPARATED A SWAAC ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 SW29417WN 29822 NR 2 MLG TIRE TREAD SEPARATED DURING TAKEOFF. REMOVED AND REPLACED NR 2 MLG TIRE/WHEEL ASSY. ALSO REMOVED AND REPLACED LT WING INBOARD FORE AND AFT FLAPS DUE TO TIRE DAMAGE. 2L72 4F RTA16WE 20040827000232004082700023NM 2004 8 27 VNAA0408012 120040819A2740 CIRCUIT BREAKER DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE ELEVATOR TRIPPED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07424JS 3033 DURING CLIMBOUT, THE CREW RECEIVED AN ELEVATOR ASYMMETRY CAS MESSAGE THEN FLIGHT 2540 RETURNED TO PIT. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND TRIM CIRCUIT BREAKER POPPED. MAINTENANCE THEN RESET THE CIRCUIT BREAKER IN ACCORDANCE WITH WIRING MANUAL 20-10-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040827000262004082700026 2004 8 27 SWAA042458 420040825A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040827000272004082700027NM 2004 8 27 SWAA042459 120040825A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29087SW 22903 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20040827000282004082700028NM 2004 8 27 SWAA042461 120040825A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 360, STRINGER 14R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040827000292004082700029NM 2004 8 27 SWAA042462 120040825A53116546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 420, STRINGER 15L, CRACKED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040827000312004082700031NM 2004 8 27 SWAA042464 120040825A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 15L AT BS 374, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040827000322004082700032NM 2004 8 27 SWAA042465 120040825A53106545807 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR CUTOUT WEB BELOW THE UPPER HINGE, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040827000332004082700033NM 2004 8 27 SWAA042466 120040825A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 523, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040827000352004082700035NM 2004 8 27 UPS04242988 120040819A3350 LIGHT BOEING727 72725C 138400HNM EMERGENCY EXIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01950UP 19718 EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERIES IN FWD & AFT EXIT LIGHTS, ALL CHECK GOOD IAW MM 33-50. 2L73 4F A3WE 20040827000362004082700036NM 2004 8 27 UPS04542989 120040821A3350 POWER SUPPLY BOEING757 75724APF 1384969NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01438UP 25469 INSPECTION TYPE:N/A EMERGENCY LIGHT POWER SUPPLY DEAD. REPLACED EMERGENCY LIGHT POWER SUPPLY, OPS CHECK GOOD. 2L72 4F RTA2NM 20040827000372004082700037WP 2004 8 27 UPS04842977 120040817A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C, EXTERNAL FUSELAGE EXISTING REPAIR DOUBLER AT STA 70 L36 REQUIRES REMOVAL, ASSESSMENT, AND REPAIR IAW SRM 53-2-1 FIG 7 REF EO DC8-5330-12800 REPAIR 708-2R-01. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER, EXT DOUBLER, AND INTERNAL FINGER DOUBLERS PER SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040827000392004082700039WP 2004 8 27 UPS04842983 120040821A36201944301 PRECOOLER DOUG DC8 DC873F 302199FWP NR 3 PYLON OVERTEMP A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01802UP 46100 AT FL 370 ENGINE ANTI ICE WAS TURNED ON, SHORTLY AFTER MANIFOLD OVER TEMP LIGHT ILLUMINATED MANIFOLD TEMP (RT) REACHED RED ARC. COCKPIT FILLED WITH SMOKE AND FUMES. COMPLIED WITH CHECKLIST AND TURNED NR 3 ENG ANTI-ICE OFF. MANIFOLD TEMP RETURNED TO NORMAL. OVERTEMP LIGHT EXTINGUISHED AND SMOKE WAS EVACUATED. REMOVED AND REPLACED NR 3 ENG PRECOOLER CONTROL VALVE. LEAK CHECK OPS CHECK GOOD. 2L74 4F RT4A25 20040827000422004082700042NM 2004 8 27 UPS04M42987 120040822A3350 POWER SUPPLY DOUG MD11 MD11F 3023600NM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP TESTING EMERGENCY LIGHT SYSTEM 1 BATTERY LOW MESSAGE CAME ON. REMOVED AND REPLACED POWER SUPPLY EMERGENCY LIGHTING BATTERY IAW MM 33-51-01. SYSTEM OPS CHECK GOOD. 2L73 4F RTA22WE 20040827000432004082700043NM 2004 8 27 SWAA042468 120040825A531165C25228 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 727D, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040827000462004082700046SO 2004 8 27 CHQA000541 120040821A3350 WIRE EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT LOOSE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11838 145720 OVERWING EMERGENCY EXIT LIGHT AT ROW 12 INOP. INSPECTED AND FOUND WIRE W192-8712-20 CONNECTION INTO JACK J8031 LOOSE. RESECURED IAW EMB WM 20-50-00. OPS CHECK GOOD. 2L72 4F RTT00011AT 20040827000502004082700050SO 2004 8 27 CHQA000538 120040823A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11567 145698 DURING THE ROUTINE INSPECTION THE MAIN DOOR OVERHEAD EMERGENCY EXIT LIGHT AND THE OVERWING EMERGENCY EXIT LIGHT WERE BOTH FOUND TO BE INOP. REMOVED AND REPLACED MAIN DOOR AND OVERWING EMERGENCY EXIT LIGHT BULBS IAW EMB 145 MM 33-50-10. OPERATIONAL CHECK SATISFACTORY. 2L72 4T RTT00011AT 20040827000532004082700053EA 2004 8 27 COMA0460478 120040820A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01473CA 7668 FLIGHT 5014 LEFT REVERSER UNLOCK MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040827000542004082700054EA 2004 8 27 SWIA200413733 120040715A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW 7518 CARGO PIT FLOOR SUPPORT ANGLE FS 621.00 RBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-007 REV B. 2L72 4F RTA21EA 20040827000562004082700056SO 2004 8 27 SWIA200413707 120040813A2150 DUCT EMB 120 EMB120ER 3260203SO A/C PACK LOOSE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07190SW 120050 LEFT PACK MAKES A SQUEALING SOUND WITH LOW SELECTED. IN FLIGHT, PACK CREATES A HOT, SMOKEY SMELL UNTIL TURNED OFF. TIGHTENED CLAMPS AT LEFT PACK. COULD NOT DUPLICATE SMELL. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040827000572004082700057EA 2004 8 27 SWIA200413708 120040816A3350 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07934SW 7722 MAIN CABIN DOOR ENTRYWAY EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED ENTRYWAY EMERGENCY FLOOR FLOODLIGHT FIXTURE, REF CHAP 33-51-19 CRJ AMM. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040827000602004082700060EA 2004 8 27 SWIA200413711 120040814A3350 INVERTER CNDAIRCL600 CL6002B19 1900309EA NR 2 INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07929SW 7703 EMERGENCY LIGHT STRIP INOPERATIVE ON FRONT RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED NR 2 INVERTER FOR THE EMERGENCY LIGHT STRIP IAW MM 33-51-04. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040827000612004082700061SO 2004 8 27 CHQA000522 120040725A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11278 145370 DURING CRUISE THERE WAS A STRONG ELECTRICAL SMELL COMING FROM THE INSTRUMENT PANEL. THE SMELL ONLY LASTED A FEW SECONDS. INSPECTED AIRCRAFT FOR ELECTRICAL SMELL. NO SMELL NOTED. COULD NOT DUPLICATE. RAN APU AND CYCLED WINDSHIELD HEAT. NO DEFECTS NOTED IAW EMB 145AMM 34-22-00. 2L72 4T RTT00011AT 20040827000622004082700062SO 2004 8 27 SWIA200413712 120040816A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07292UX 120292 FIRST OVERHEAD EMERGENCY CABIN LIGHT INOPERATIVE. RELAMPED FIRST OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040827000642004082700064 2004 8 27 SWIA200413714 420040812A3418C818061 COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07568SW 120343 ON TAXI, STALL WARNING LIGHT ON MAP ILLUMINATED. REMOVED AND REPLACED STALL PROTECTOR COMPUTER IAW MM 27-34-02. ALSO REMOVED AND REPLACED STALL WARNING TEST PANEL IAW MM 27-34-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040827000652004082700065EA 2004 8 27 SWIA200413715 120040809A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07939SW 7742 FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11; 51-42-06. 2L72 4F RTA21EA 20040827000662004082700066EA 2004 8 27 SWIA200413716 120040809A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07939SW CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT FS 621.00 RBL 42.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" 2L72 4F RTA21EA 20040827000672004082700067NM 2004 8 27 WLDA200431 120040704A2710ARH7057515 ACTUATOR DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE AILERONS DEFECTIVE A WRLAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO11273 48519 LEVEL II ALERT AFTER SLAT RETRACTION, AILERON DEFLECTION DISAGREE AFTER T/O. A/C DIVERTED TO JFK. INSPECTED QUAD RINGS & ASSOCIATED LINKAGE, RAN FLIGHT CONTROLS. CHECKED FOR FLAIRING, PERFORMED RTS ON FCC 1&2 AILERON SYSTEM. ALL TESTS PASSED. DEFERRED AILERON DEFLECTION SYSTEM PER MEL 27-13-2 CAT-C DMI M27JL0404-09. REPLACED LOB DEFLECTED AILERON ACTUATOR. FUNCTION CHECK NORMAL PER MM 27-16-00. CLEARED DMI. 2L73 4F4 FRTA22WE E24NE 20040827000692004082700069NM 2004 8 27 WLDA200468 120040802A5510ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 29. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 29 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000702004082700070NM 2004 8 27 WLDA200471 120040802A5510ALC8104501 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 25. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 25 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000732004082700073NM 2004 8 27 WLDA200461 120040802A5510ALC8121502 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT BARREL NUT HOLE NR 1. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BARREL NUT HOLE NR 1 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000742004082700074NM 2004 8 27 WLDA200462 120040802A5510ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 36. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 36 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000762004082700076NM 2004 8 27 WLDA200465 120040802A5510ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 32. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 32 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000772004082700077NM 2004 8 27 WLDA200467 120040802A5510ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 30.PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 30 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000782004082700078NM 2004 8 27 WLDA200476 120040802A5510ALC8104501 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 18. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 18 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040830000032004083000003SO 2004 8 30 SWIA200413724 120040820A3350K00913 RELAY EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE EMERGENCY LIGHT FAULTY A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07232SW 120306 EMERGENCY FLOOR LIGHT (RED) BULB AT MAIN CABIN DOOR DOES NOT ILLUMINATE. REMOVED AND REPLACED RELAY K00913. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040830000052004083000005EA 2004 8 30 SWIA200413726 120040817A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07923SW5115 5115 7664 RT SPOILERON CAUTION MESSAGE. REMOVED AND REPLACED RT OB SPOILERON PCU AND FLIGHT SPOILER LEVER IAW MM 27-61-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040830000062004083000006SO 2004 8 30 SWIA200413727 120040820A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07565SW1008410084 120340 UPON FLAP RETRACTION AFTER LANDING, THE IB PAIR REPEATEDLY STUCK AT TEN DEGREES. REMOVED AND REPLACED RT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040830000072004083000007EA 2004 8 30 SWIA200413728 120040819A5240 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SERVICE DOOR STUCK A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07453SW 7743 UNABLE TO OPEN SERVICE DOOR. REMOVED AND REPLACED OUTER HANDLE ASSY ON SERVICE DOOR IAW SRM 51-11-06 AND 51-42-06. 2L72 4F4 FRTA21EA E15NE 20040830000092004083000009EA 2004 8 30 SWIA200413730 120040811A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07935SW 7725 FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPAIRED BROKEN WIRE LY3D22 IN RT SIDEWALL. EMERGENCY LIGHTING OPERATION CHECKED OKAY. 2L72 4F4 FRTA21EA E15NE 20040830000112004083000011EA 2004 8 30 SWIA200413732 120040822A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZ STAB TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07937SW 7735 STAB CHANNEL 1 INOPERATIVE. REMOVED AND REPLACED HSTCU IAW MM 27-41-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040830000122004083000012SO 2004 8 30 CHQA000536 120040821A2120 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11261SK 145144 DURING INITIAL CLIMB, LAV SMOKE WARNING ON EICAS. F/A CONFIRMED THERE WAS SMOKE IN LAV. EMERGENCY WAS DECLARED WITH ATL ATC AND AC SAFELY RETURNED TO FIELD. AC WAS FERRIED WITH BLEEDS OFF. MAINT FOLLOWED FIM FOR OIL ODOR, CAN NOT DUPLICATE SMELL, PULLED NOSE CONES OFF AND FOUND NO LEAKS AND BOROSCOPED INTAKES AND IGV'S AND FOUND NO FAULTS. CUSTOMER SERVICE MANIFOLD WAS PULLED AND NO ODOR WAS NOTED. AC WAS FLOWN ON TEST FLIGHT, FOUND SLIGHT ODOR TO BE EVIDENT. MAINT ISOLATED INDIVIDUAL BLEED SYS IN HIGH AND LOW POWER CLIMBS AND DIVES WITH NO LAV SMOKE INDICATION. MAINT PERFORMED ALL FIM TASKS AND COULD NOT FIND ANY DEFECTS. AC WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040830000152004083000015EA 2004 8 30 COMA0460473 120040816A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01479CA 7675 RT FS 621 FLOOR ANGLE CRACKED. CW 601R-53-61-004. 2L72 4F4 FRTA21EA E15NE 20040830000172004083000017EU 2004 8 30 MALA040536 120040820A3020 THERMISTER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE INTAKE HEAT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15426XJ 340B426 LT INTAKE ILLUMINATED IN FLIGHT. QRH COMPLETED, NOTIFIED DISPATCH/MECHANIC. LT AC GEN OPS OK, LT. APPEARS TO CYCLE EVERY 2 MINUTES OR LESS. AIR RETURN TO DTW. MAINTENANCE SWAPPED THERMISTORS (2 AND 3 WITH 4 AND 5) IN DEICE MODULE. RAN A/C FOR FIFTEEN MINUTES WITH INTAKE HEAT ON. ALL CHECKS GOOD IN DRY AND WET CONDITIONS. VISUALLY INSPECTED ALL DUCTS AND HEATING MATS, NO DEFECTS NOTED. 2L72 4T4 TRTA52EU E8NE 20040830000182004083000018NM 2004 8 30 F3LA200400088 120040819A5330 SKIN BOEING737 737317 138447PNM FUSELAGE DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED SKIN REPAIR AT BS 917, STR. 20L, REPAIR DOCUMENTATION NOT SATISFACTORY TO LEASOR. REMOVED EXISTING FUSELAGE REPAIRS AT BS 927 AND BS 896 COMMON TO STR. 20L. ENLARGED CUTOUTS TO INCLUDE FASTENER HOLE FROM PREVIOUS REPAIRS, MANUFACTURED STRUCTURAL FILLERS, A DOUBLER AND A TRIPLER. INSTALLED REPAIR PARTS AND APPLIED AERODYNAMIC SEAL TO NEW REPAIR PARTS IAW SRM 53-00-01, FIG. 229, DETAIL XIV AND EA B3-53R-10506. 2L72 4F RTA16WE 20040830000222004083000022NM 2004 8 30 04FDEA02528 120040819A5711 SPAR DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AREA AT XORS 730 TO XORS 755 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2L73 4F4 FRTA22WE E24NE 20040830000252004083000025NM 2004 8 30 04FDEA02532 120040819A5510ALC8055 BULKHEAD DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO TRIM OUT HORIZONTAL STABILIZER LT OPERATING BULKHEAD FITTING TO GAIN ACCESS FOR LT UPPER AFT PLANK NR 34L BARREL NUT REWORK. LT HORIZONTAL STABILIZER, OPERATING BULKHEAD FITTING TRIMMED OUT FOR ACCESS IAW EA 1-5510-79819. TITLE: STABILIZERS, HORIZONTAL STABILIZER, ACCESS TO REWORK BARREL NUT BORE 34 AND 35L, TRIMMING OF THE OPERATING BULKHEAD IAW S/B 55-023 REV. 2. 2L73 4F4 FRTA22WE E31N3 20040830000282004083000028NM 2004 8 30 04FDEA02566 120040825A3610 ISOLATOR DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE NR 2 MANIFOLD DEFECTIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25610FE 48603 MANIFOLD NR 2 FAILURE. INFLIGHT QRH COMPLIED WITH. LANDED CDG. PERFORMED DECAY CHECK IAW MM 36-00-02 WITH ALL OK, PERFORMED FLIGHT FAULT, REVIEW ON THE MFC FOUND (SENSOR ZONE 15 ELE A). DURING TEST FOUND BAD ISOLATION ON LOOP D1-98 REMOVED AND REPLACED MANIFOLD SENSING ELEMENT D1-98 IAW MM 36-23-07-4 , ALL TEST PASSED DUE TO LOOP REPLACEMENT, HAD TO REMOVED ELBOW DUCT, ELBOW STILL NEEDS TO BE REINSTALLED. ITEM IN WORK. INSTALLED ELBOW OVERPRESSURE VALVE IAW MM: 36-12-02-4 ITEM NOT CLOSED WAITING FOR RUN UP AND TEST. RUN ENGINE IAW JRH AND PERFORMED LEAK AND DECAY CHECK MM36-00-02, ALL TESTS PASSED, NO FAULTS RECORDED, ALL PARAMETERS NORMAL. 2L73 4F4 FRTA22WE E31N3 20040825000342004082500034EA 2004 8 25 MASA200400378 120040628A5210 CAM CNDAIRCL600 CL6002C10 1390015EA PAX DOOR LACK OF LUBE A MASAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SW07509MJ 10094 ASH 7080 CVG - ORD. THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. THE CREW REPOSITIONED THE AIRCRAFT SEVERAL TIMES IN AN ATTEMPT TO FREE THE DOOR, BUT WERE UNSUCCESSFUL. CONTRACT MAINTENANCE ALSO WAS UNABLE TO OPEN THE DOOR. THE AIRCRAFT WAS FERRIED TO DEN. MX LUBED THE LOCKING CAMS. CURRENTLY TROUBLESHOOTING. MAINTENANCE FOUND SEVERAL PARTS OUT OF RIG, RE-RIGGED THE DOOR AND RIG CHECK WAS FOUND GOOD. 2L72 4F RTA21EA 20040825000372004082500037EA 2004 8 25 MASA200400282 120040522A5210H341437 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW0775995 7361 ASH 2605 CLT. MAINTENANCE REPORTED THE EXTERIOR PASSENGER DOOR HANDLE FAILED TO UNLOCK AND OPEN THE MAIN CABIN DOOR WHEN EXERCISED. MX IS TROUBLESHOOTING THE DOOR AT THIS TIME. REPLACED HANDLE, OPS CHECK GOOD. 2L72 4F RTA21EA 20040825000402004082500040EA 2004 8 25 MASA200400265 120040516A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA RT MLG LOOSE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07650ML 7137 ASH 2928 PHL-DCA. DEPARTING PHL THE CAPTAIN REPORTED THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AND A GEAR UNSAFE CONDITION EXISTED. THE GEAR WAS PLACED BACK DOWN AND ABNORMAL SAFE LANDING WAS EXECUTED. MX FOUND THE RT MLG PROXIMITY SENSOR TARGET NOT SECURE. THE TARGET WAS SECURED, GEAR SWING PERFORMED AND AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. 2L72 4F RTA21EA 20040825000712004082500071NM 2004 8 25 SWAA042405 120040820A573065C25204 SKIN BOEING737 7375H4 138449DNM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 DURING SCHEDULED C4 CHECK, FOUND LT WING SKIN AT WING STATION 132, STRINGER 3, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040825000742004082500074NM 2004 8 25 04227428 120040814A3241 CONTROL BOX DORNERDO32 DO328300 NM ANTI SKID SYS MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27428FJ 3193 AFTER GEAR RETRACTION, CAS MESSAGE LT BRAKE TEMPERATURE ON EICAS. RETURNED TO FIELD. CLEANED BRAKE TEMP SENSOR, REMOVED AND REPLACED ANTI SKID CONTROL BOX IAW 32-42-21. OPS CHECK GOOD. 2H72 4T RTA55NM 20040825000832004082500083 2004 8 25 QXEA200400563 420040720A3410C17053AC03 ADC BOMBDRDHC8 DHC8401 1390041NM ZONE 200 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09404QX7264 7264 4046 SEA - FLIGHT 2319, AT 24,000 FT GOT A IAS MISMATCH. FOLLOWED CHECKLIST. SWITCHED TO NR 2 ADC. ON DESCENT NR 2 AIRSPEED WAS DECREASING. THE STANDBY AIRSPEED INCREASING WITH ELEVATOR FEEL, PITCH TRIM, SPOILER OUTBOARD, AND RUD CONTROL, CAUTION LIGHTS ILLUMINATED WITH AUTO PILOT AND YAW DAMPER FAIL. SWITCHED TO NR 1 ADC AND AIRSPEED RETURNED TO NORMAL AND THE CAUTION LIGHTS WENT OUT. CONTINUED WITHOUT FURTHER PROBLEMS. REMOVED AND REPLACED NR 1 ADU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825000872004082500087NM 2004 8 25 QXEA200400554 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 7 HAS SEVERAL MARKED AREAS OF CORROSION ON UPPER SURFACE OF CENTER FLANGE BETWEEN X204 AND X210. REPLACED NR 7 SEAT TRACK. 2H72 4T RTA13NM 20040825000882004082500088NM 2004 8 25 QXEA200400548 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING AT APPROXIMATELY STATION 396. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20040825000922004082500092NE 2004 8 25 04230678 220040817A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT LEAKING A VTZABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27678BR 7653 LEFT ENGINE SHUTDOWN FOR LOW OIL PRESSURE. EMERGENCY DECLARED AND DIVERTED TO CMH. LANDED UNEVENTFULLY. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE PROBLEM. 2L72 4F4 FRTA21EA E15NE 20040825001162004082500116NM 2004 8 25 P5CA0401150 120040809A5414 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 NACELLE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 NR 4 ENGINE PYLON PANEL 481C HAS DELAMINATION. REMOVED DAMAGE IAW SRM 51-40-15, BONDED APPLIED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825001242004082500124NE 2004 8 25 04214407 220040801A7314 SWITCH DORNERDO32 DO328300 NM PWA 306 PW306B NE FUEL PUMP MISINSTALLED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27407FJ 3157 LOW SPEED ABORT DUE TO LOW FUEL PRESSURE MESSAGE. FOUND LEFT JET PUMP SWITCH PUSHED. 2H72 4T4 FRTA55NM E35NE 20040825001272004082500127NM 2004 8 25 QXEA200400629 120040812A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - NR 1 ENGINE LOWER COWL AFT CUTOUT FOR OIL COOLER IS CHAFED AT LEFTHAND FORWARD CORNER. MAPPED DAMAGE FOR ENGINEERING. BLENDED DAMAGE SMOOTH AND DEEPEST POINT AFTER BLENDING ON RIGHT HAND IS .009 INCH AND LEFT HAND IS .020 INCH. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ULTRASONIC THICKNESS CHECK TO FIND ORG THICKNESS, ORG .086 INCH. REPAIRED LOWER COWL AND INSPECTED INLET PLATE. FOUND INLET PLATE TO BE PREVIOUSLY TRIMMED IAW RD 6-71-150 AND HORIZON AIR EA 6-71-150. 2H72 4T RTA13NM 20040825001302004082500130NM 2004 8 25 P5CA0401138 120040810A5753 FLAP TRACK BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE TE FLAPS DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DELAMINATION SEVERAL AREA, I/B FORE FLAP L/E RIGHT WING B/W FLAP TRACK. CLEANED AREA & REPAIRED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040825001392004082500139NM 2004 8 25 AWXA200400842 120040801A2910312N510157 TUBE BOEING757 7572S7 1384962NM LT PYLON LEAKING A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28901AW 23321 PHX - DIVERSION - FLT 0058 - AFTER TAKEOFF FROM LAS EN ROUTE FOR JFK RECEIVED EICAS MESSAGE M56 LT HYDRAULIC SYSTEM PRESSURE, HYDRAULIC QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE WARNING LIGHT ILLUMINATED, DIVERTED TO PHX FOR REPAIR. MAINTENANCE FOUND LT PYLON HYDRAULIC CASE DRAIN TUBE ASSEMBLY THAT RUNS TO FIRE SEAL DISCONNECT LEAKING. REMOVED AND REPLACED HYDRAULIC TUBE ASSEMBLY IN LT PYLON, LEAK CHECK WAS GOOD. 2L72 4F RTA2NM 20040825001612004082500161EA 2004 8 25 04154632 120040602A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING HEAVY INSPECTION THE FRAME DOUBLER AT FS 610 STR 10 WAS FOUND CRACKED. FRAME WAS REPAIRED PER MANUFACTURERS INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE WITH COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040825001752004082500175NM 2004 8 25 AALA20040837 120040809A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21902AN 29521 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED 15 MINUTE TEST. REPLACED BATTERY PACK AT M1671 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040825001772004082500177 2004 8 25 SWAA042336 420040814A25656556685 BRACKET BOEING737 7373H4 1384600NM ESCAPE SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE FWD UPPER MOUNT BRACKET CRACKED. REMOVED AND REPLACED FWD UPPER BRACKET PER MM. 2L72 4F RTA16WE 20040825001782004082500178NE 2004 8 25 AALA20040845 220040815A7230 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE ZONE 500 FAILED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21574AA 53151 717855 DFW - INFLIGHT T1446/15 COMPRESSOR STALL AT 17500 ON CLIMBOUT AND ENGINE NUMBER 1 AT 10LR FOR REMAINDER OF FLIGHT. OIL LEAK REPORTED WITHIN CLEAR OF RUNWAY. REPLACED ENGINE NUMBER 1 PER WORKCARD 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20040825001792004082500179NM 2004 8 25 AALA20040851 120040812A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21923AN 29524 TUL - BATTERY IN CABIN AT M1671 FAILED TO SUSTAIN EMERGENCY LIGHTING FOR THE REQUIRED 15 MINUTE MINIMUM. REPLACED BATTERY PACK IN CABIN AT M1671 FOR EMERGENCY LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040825001852004082500185NM 2004 8 25 P5CA0401148 120040809A5350 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSLEAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FUSELAGE PANEL 191OA, BOTH HAVE HEAVY CORROSION. REMOVED 2 EA SPLICE PLATES IAW 51-30-01. FOUND TO BE OUT OF LIMIT, FABRICATED NEW PLATES PER BOEING DRAWING 65B3878. 2L74 4F4 F A20WE E3NE 20040825001942004082500194SO 2004 8 25 C2XA04BT088 120040812A27613605409009 ACTUATOR EMB 145 EMB145ER 3260211SO LT SPOILERS BYPASSING A C2XAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW271293411751 145019 BTV LOG SQUAWK LEFT SPOILER REMAINED OPEN IN FLIGHT AFTER SPEED BRAKE LEVER WAS RETURNED TO CLOSE POSITION. THIS LEAD TO UNCOMMANDED LEFT ROLL OF AIRCRAFT ALONG WITH SPOILER FAIL MESSAGE. REMOVED AND REPLACED LEFT SPEED BRAKE ACTUATOR IAW EMB MM 27-62-02. OPS CHECK GOOD. 2L72 4F RTT00011AT 20040825001992004082500199 2004 8 25 AWXA200400585 420040531A3441HG1050AD04 COMPUTER BOEING757 757225 1384959NM ZONE 120 FAILED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 WP28915AW358996517 22209 PHX - DIVERSION - FLT 0778 - AFTER TAKEOFF FROM LAS EN ROUTE FOR BWI CENTER IRS ALIGN LIGHT BEGAN FLASHING WITH FLIGHT MANAGEMENT COMPUTER (FMC) MESSAGES -IRS MOTION & RESET IRS POSITION-. WITH V/S ON FL/CH SELECTED V/S MODE SELECTED ITSELF AND V-NAV WOULD NOT DESELECT. RT CONTROL DISPLAY UNIT FROZE UP FOR A WHILE WITH STANDBY FMC MESSAGE. DIVERTED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED CENTER INERTIAL REFERENCE UNIT IAW 34-21-01, OPERATIONAL CHECK WAS GOOD. *S/D* VENDORS FUNCTIONAL TEST OF INERTIAL REFERENCE UNIT S/N 123401 WAS NO FAULT FOUND. PERFORMED 24 HOUR BURN IN AND PERFORMANCE TEST, TESTS GOOD IAW CMM 34-21-13 REV 9. 2L72 4F RTA2NM 20040825002022004082500202EU 2004 8 25 AWXA200400678 120040607A5320D5323058520000 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON FORWARD CARGO DOOR SILL WEB BETWEEN FR 24A AND FR 28, STR 39 RT. MAINTENANCE REMOVED DAMAGED FORWARD CARGO DOOR SILL WEB FROM FR 24A TO FR 28, AT STR 39 RT; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 2-3, 8-9 & 12. 2L72 4F RTA28NM 20040825002152004082500215NM 2004 8 25 AWXA200400714 120040617A532065528941 CHANNEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1.5 INCH CRACK WAS FOUND IN FLOOR CHANNEL ASSEMBLY AT BS 540, LBL 6. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL ASSEMBLY AT BS 540, LBL 6; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-52894; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 16. 2L72 4F RTA16WE 20040825002242004082500224NM 2004 8 25 AWXA200400723 120040617A57536546430132 SKIN BOEING737 7373G7 1384595NM TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A DISBOND AREA WAS FOUND IN DOUBLER ON LOWER SURFACE OF LT INBOARD FORE FLAP 33-36 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED EXISTING REPAIR AND CLEANED AREA. FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 30. 2L72 4F RTA16WE 20040825002262004082500226NM 2004 8 25 AWXA200400748 120040620A53156545812100 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 328, FROM RBL 11 TO RBL 57, WL 208. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 328, FROM RBL 11 TO RBL 57. FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 20040825002342004082500234NM 2004 8 25 SWAA042413 120040821A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 10R, BS 506, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040825002382004082500238NM 2004 8 25 QXEA200400534 120040713A335061047811 BATTERY DHAV DHC8 DHC8202 2809007NM ZONE 100 FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09357PH4441 29 504 PSC - AFT CEILING AND RIGHT HAND AFT EGRESS EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED PS4 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825002422004082500242WP 2004 8 25 AALA20040801 120040801A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP FUSELAGE INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21237AA 49253 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 13 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040826000032004082600003SO 2004 8 26 CHQA000525 120040727A3350 BULB EMB 145 EMB145ER 3260211SO CONT O200 O200* 17020SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11281 145391 THE LT SIDE OVERWING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LT OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-07. OPS CHECK IS GOOD. 2L72 4F3 ORTT00011ATE252 20040826000092004082600009SO 2004 8 26 C2XA04TY147 120040806A531014542895401 GUSSET EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 15. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F4 FRT TE6CH 20040826000192004082600019NM 2004 8 26 04FDEA02371 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192. COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040826000222004082600022NM 2004 8 26 AWXA200400852 120040804A3150 WARNING HORN BOEING737 7373G7 1384595NM CONFIGURATION ACTIVATED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28307AW 24634 ON TAKEOFF AT SFO EN ROUTE FOR LAS TAKEOFF CONFIGURATION WARNING HORN SOUNDED, REJECTED TAKEOFF. TAXIED OFF RUNWAY, RESET TAKEOFF SETTINGS, DEPARTED WITHOUT FURTHER DIFFICULTY. DUE TO ANOTHER RECENT REJECTED TAKEOFF ON THIS AIRCRAFT FOR TAKEOFF CONFIGURATION WARNING A FOLLOW-UP HAS BEEN WRITTEN TO PERFORM A TAKEOFF WARNING SYSTEM TEST PER T/C A1B31009. MAINTENANCE PERFORMED TAKEOFF WARNING TEST PER AWA T/C A1B31009, NO DEFECTS WERE NOTED. PROBLEM RETURNED; SEE SDR AWXA200400879 FOR CORRECTIVE ACTION. 2L72 4F RTA16WE 20040827000052004082700005NM 2004 8 27 UPS04242973 120040729A5350 FAIRING BOEING727 72722C 138400FNM TAILCONE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C, VERTICAL STAB TIP FAIRING (TAIL CONE) DELAMINATED AT BOTTOM NEAR WEDGE. REPAIR CARRIED OUT IAW SRM 51-40-9 & 51-30-2. 2L73 4F A3WE 20040827000072004082700007NM 2004 8 27 UPS04242981 120040729A5543 SKIN BOEING727 72722C 138400FNM RUDDER TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, UPPER RUDDER TAB HAS DELAMINATION AT LWR LT SIDE UPPER RUDDER REPLACED IAW MM 27-20-11. 2L73 4F A3WE 20040827000182004082700018NM 2004 8 27 SWAA042443 120040822A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040827000212004082700021 2004 8 27 SWAA042436 420040821A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR FLOOR MOUNT FITTING PLATES CORRODED. REMOVED AND REPLACED FITTING PLATES PER MM. 2L72 4F RTA16WE 20040827000382004082700038WP 2004 8 27 UPS04842978 120040819A5511 RIB DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C, LEFT HORIZONTAL STAB L/E UPPER RIB CRACKED AT XFS 47.5. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 55-2-0 FIG 2. 2L74 4F RT4A25 20040827000402004082700040 2004 8 27 UPS04842990 420040821A2564 FASTENER DOUG DC8 DC873F 302199FWP LIFE RAFT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 INSPECTION TYPE:N/A FWD LIFE RAFT OPEN AND ONE SNAP BROKEN. REPAIRED SNAP AND CLOSED LIFE RAFT CORNER. 2L74 4F RT4A25 20040827000452004082700045EA 2004 8 27 SWIA200413673 120040807A2750 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07708SK 10156 FLAPS FAIL CAUTION MESSAGE DISPLAYED ON ED 1. ELECTRONICALLY RIGGED SFECU'S. OPERATIONAL CHECK GOOD PER MM 27-52-00. 2L72 4F RTA21EA 20040827000632004082700063SO 2004 8 27 SWIA200413713 120040814A5210 BOLT EMB 120 EMB120ER 3260203SO PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07213SW 120277 FORWARD ENTRY DOOR WILL NOT OPEN. ADJUSTED FORWARD DOOR FORWARD ECCENTRIC BOLT IAW MM 52-11-00 PAGE 504. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040827000712004082700071NM 2004 8 27 WLDA200472 120040802A5510ALC8104501 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 23. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 23 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040827000752004082700075NM 2004 8 27 WLDA200463 120040802A5510ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 35. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 35 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040830000202004083000020NM 2004 8 30 04FDEA02526 120040819A5711 SPAR DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, LOWER CHORD AT XORS 650 AREA FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2L73 4F4 FRTA22WE E24NE 20040830000212004083000021NM 2004 8 30 04FDEA02527 120040819A5711 SPAR DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AREA AT XORS 680 TO XORS 690 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2L73 4F4 FRTA22WE E24NE 20040830000292004083000029NM 2004 8 30 F3LA200400089 120040821A5310 STRUCTURE BOEING737 7373L9 1384470NM MLG WW CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3660 26440 ON WALK AROUND, MAINTENANCE REPORTED A 4-INCH CRACK IN RT FWD TOP WHEEL WELL. REPAIRED IAW SRM 53-10-51, PAGE 213, FIGURE 203. 2L72 4F RTA16WE 20040830000312004083000031CE 2004 8 30 DXTA200400368 120040824A7700 WARNING LIGHT CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LT ENGINE ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07996QS 7500196 AMBER (ENGINE OVERSPEED- LT) MESSAGE ON ADDITION OF POWER ITT WENT TO 860 DEGREE. FAN WENT UP EVENLY FOR BOTH ENGINES, RETARDED THROTTLES BEFORE INDICATORS HIT BLUE POINTER ON SUBSEQUENT POWER UPS. DID NOT NOTICE INDICATOR ON T/O TRY. 2L72 4J4 FRTT00007WITE6CH 20040830000332004083000033CE 2004 8 30 DXTA200400371 120040822A3260387 BULB CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL MLG INDICATOR INOPERATIVE E DXTAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL07996QS 7500196 RT MAIN GEAR LIGHT DID NOT ILLUMINATE AFTER GEAR WAS SELECTED DOWN. BLEW GEAR DOWN AND PULLED GEAR UPLOCK RELEASE HANDLE IN LAV IAW ABNORMAL CHECKLIST. REPLACED 2 DEFECTIVE RT GEAR DOWN ANNUNCIATOR BULBS W/2 NEW BULBS. VISUALLY INSP GEAR HARNESS AND FOUND OK. RESET EMERG BLOW DOWN AND GEAR MANUAL RELEASE SYSTEM. CYCLED GEAR 15 TIMES, PERFORMED HYD SYSTEM BLEED WITH AIRCRAFT ON JACKS. BLED RESERVOIR AND SERVICED TO 70 PERCENT (FULL AT PSI). SERVICED GEAR BLOW DOWN BOTTLE TO 1900 PSI, GEAR/ IND SYSTEM OPS NORMAL. WORK C/W IAW MM 32-60-00, 12-10-15. 2L72 4J4 FRTT00007WITE6CH 20040830000342004083000034NM 2004 8 30 04FDEA02550 120040823A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT SIDE STA 5-113-1541, LONGERON 25 FOUND CRACKED. REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 53-33-01 VOLUME II. 2L73 4F4 FRTA22WE E24NE 20040830000352004083000035CE 2004 8 30 JEM2004F00008 120040828A551045A21086004 BRACKET BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01400FT RK101 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE RIB AS WELL AS THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTO THE HORIZONTAL STABILIZER DRAIN HOLES NEAR THE SIDE ROLLER SUPPORT BRACKETS. THE RIB CRACK WAS NOT FOUND UNTIL THE ROLLER BRACKET WAS COMPLETELY REMOVED. 2H72 4F4 FRTA16SW E25EA 20040830000372004083000037NM 2004 8 30 04238451 120040825A2121 FAN DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN DEFECTIVE A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27451FJ 3205 LAV SMOKE MESSAGE WITH VISIBLE SMOKE. REMOVED AND REPLACED 16VE PANEL IA 31-12-12 AND LT HX FAN IAW 21-51-23. OPS CHECK GOOD. 2H72 4T4 FRTA55NM E35NE 20040830000382004083000038NM 2004 8 30 AALA20040894 120040820A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21924AN 29525 BATTERY PACK AT STATION 560 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 560 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040830000402004083000040NM 2004 8 30 AALA20040893 120040823A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21928AN 29528 BATTERY PACK AT STATION 727C RT FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727C RT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040830000412004083000041NM 2004 8 30 AALA20040892 120040823A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21928AN 29528 BATTERY PACK AT STATION 952 RT FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 952 RT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040830000422004083000042WP 2004 8 30 AALA20040889 120040823A1420 CONNECTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219627R 53597 AISLE EMERGENCY EXIT ARROW LIGHT AT FORWARD FIRST CLASS INOPERATIVE. REPINNED CONNECTOR FOR FORWARD EMERGENCY EXIT ARROW LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA6WE E9NE 20040830000452004083000045EA 2004 8 30 COMA0460481 120040821A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG UNRELIABLE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA9260 639 7043 FLIGHT 5783 GEAR DISAGREE WARNING. REPLACED THE NLG PRIORITY VALVE. 2L72 4F4 FRTA21EA E15NE 20040830000472004083000047NE 2004 8 30 WLDA200490 220040825A7261 ENGINE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 2 LEAKING A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11271 48518 723942 AIR TURNBACK DUE TO LOSS OF NR 2 ENGINE OIL QUANTITY. INDICATION BOXED "0", PERFORMED CHECKLIST NOTED OIL PRESSURE DECREASING; ENGINE WAS SHUTDOWN PERFORMED. REMOVED AND REPLACED NR 2 ENGINE PER WOA T/C 0105 AND MD-11 MM PROCEDURES. ACCOMPLISHED ENGINE RUN UP CHECK, ALL NORMAL. (CLOSED) 2L73 4F4 FRTA22WE E24NE 20040830000492004083000049EA 2004 8 30 SWIA200413723 120040818A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07588SW3565 3565 7069 FLIGHT SPOILERS SELECTED TO .2500 POSITION AND AIRCRAFT ROLLED LT. REMOVED AND REPLACED LT IB AND OB FLIGHT SPOILERS PCU IAW 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040830000542004083000054WP 2004 8 30 AALA20040898 120040825A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21427AA 49339 OVERHEAD EMERGENCY LIGHTS IN AFT ENTRY INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR OVERHEAD EMERGENCY LIGHTS IN AFT ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040830000552004083000055NM 2004 8 30 UPS04M42936 120040621A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, RT HORIZONTAL STAB BARREL NUT HOLE NR 05 FOUND CORRODED. CORROSION AT B/N HOLE NR 05 RT, REMOVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 10 INCH DEEP, FOUND OUT OF LIMIT, IAW EO MD11-5510-19409-G. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G.PR1422B2 SEALANT APPLIED IAW EN:12 30-04.REPAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-5510-19409-G AND EN: 1230-04 AT B/N HOLE NR 05 RT FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20040830000572004083000057NM 2004 8 30 UPS04M42938 120040610A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 15 BARREL NUT HOLE FOUND CORRODED. CORROSION AT S/W SURFACE B/N HOLE NR 15 LT, BLEND OUT 0.020 INCH FOUND EXCEED LIMIT. FAB REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN:1196-04 AT B/N HOLE NR 15 LT. REPAIR BUSHING SLEEVE INSTALLED IAW EO MD11-5510-19409-G AT B/N HOLE AT NR 15 LT. REPAIR ACCOMPLISHED AT B/N HOLE NR 15 LT FOUND WITHIN LIMIT IAW EN 1196-04 AND EO. 2L73 4F RTA22WE 20040830000582004083000058NM 2004 8 30 UPS04M42939 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 23 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND S/W SURFACE. CORROSION AT S/W SURFACE B/N HOLE NR 23 LT REMOVED AND REAMED TO 1.067 INCH AND BLEND TO 0.065 INCH FOUND OUT LIMIT IAW EO MD11-5510-19409-G. FAB REPAIR SLEEVE BUSHING IAW MD11-5510-19409-G. PR1422B2 SEALANT APPLIED AT B/N HOL E NR 23 LT IAW EN: 1182-04. REPAIR SLEEVE BUSHING INSTALLED AT B/N HOLE NR 23 LT IAW EN 1182-04 AND EO MD115510-19409-G WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040830000592004083000059NM 2004 8 30 UPS04M42940 120040617A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C HORIZ STAB LT NR 22 BARREL NUT HOLE FOUND CORRODED ON BOTTOM BEARING AND SIDEWALL SURFACE CORROSION AT S/W SURFACE AT B/N HOLE NR 22 LT, REMOVED AND REAMED TO 1.067 INCHES AND BLEND TO 0.005 INCH FOUND OUT OF LIMIT IAW EO MD11-5510-19409-G. REPAIR SLEEVE BUSHING FAB IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN:1216-04 AT B/N HOLE NR 22 LT. REPAIR AND INSTALLED CUTOUT AT BARRELL NUT HOLE NR 22 LT IAW EO MD11-5510-19409-G AND EN:1216-04 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20040830000602004083000060WP 2004 8 30 AALA20040897 120040824A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2116545 53027 AFT EMERGENCY LIGHTS ON ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS ON ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040830000612004083000061WP 2004 8 30 AALA200040896 120040824A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2116545 53027 BOTH RT AND LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR BOTH RT AND LT HAND OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040830000622004083000062CE 2004 8 30 GLBA20030702 120040823A5330 DOUBLER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FUSELAGE DAMAGED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03240GL UE240 EO 03-17 DOUBLER ON FUSELAGE AT NR 2 COMM ANT FS 393.25-408.25, CW EO 03-17 DOUBLER ON FUSELAGE AT NR 2 COMM ANT FS393.25-408.25. 2L72 4T4 TRTA24CE E26NE 20040830000632004083000063NM 2004 8 30 HNAA0400116 120040826A32605352011 SELECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NLG FAULTY A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07815EX314306909 321 RETURNED TO FIELD DUE TO HAVING THE NOSE GEAR INDICATING DOWN AFTER GEAR WAS SELECTED UP. GEAR WAS CYCLED DOWN AND THE CREW RECEIVED 3 GREENS. FLIGHT RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT WAS FERRIED FOR REPAIRS. MAINTENANCE FOUND THE GEAR SELECTOR HANDLE TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. GEAR WAS OPERATIONAL CHECKED SEVERAL TIMES WITH NO FAULTS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040830000662004083000066NM 2004 8 30 HNAA0400076 120040823A2930 TRANSMITTER DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE HYD SYSTEM LOOSE A HNAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 EA07997HA 507 AFTER TAKE OFF, NR 1 HYDRAULICS DROPPED TO .5 QTS. FOUND TRANSMITTER LOOSE. TIGHTENED AND ADJUSTED INDICATOR IAW MM 29-30-00. RUN UP CK GOOD. NO LEAKS NOTED. 2H72 4T4 TRTA13NM E20NE 20040830000742004083000074NM 2004 8 30 CALA0400610 120040823A5313BAC1498157 STRINGER BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 16L AT STA 500C. A NEW STRINGER SECTION WAS SPLICED IN IAW SRM 53-00-03. 2L72 4F4 FRTA16WE E2GL 20040830000752004083000075 2004 8 30 CALA0400611 420040823A2330RDAA341205 ELECTRICAL BOX BOEING767 767424ER 1385270NM GE CF6 CF680C2B7 NE SEAT 5AB FAILED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2769059 29454 FLT CREW REPORTED PROBLEMS WITH READING LIGHTS AT ROWS 1-6AB. PROBLEMS WITH INFLT ENTERTAINMENT SYS AND READING LIGHTS AT SEAT 5AB WHILE ENROUTE. SMOKE ODOR NOTICED WHILE FLT CREW ATTEMPTED TO RESET IFE SYS. SYS TURNED OFF AND SMOKE ODOR DISSIPATED. SYS LEFT OFF FOR REMAINDER OF FLT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND SEAT 5AB DIGITAL SEAT ELECTRONICS BOX(DSEB) FAN NOT WORKING. DSEB WAS PULLED OFF. UNIT AND WIRING WAS INSPECTED AND A LOT OF LINT OR DUST WAS FOUND CLOGGING FAN. IT IS SUSPECTED THAT LINT/DUST CAUSED THE FAN TO FAIL AND IN TURN CAUSED THE BOX TO OVERHEAT. THE DSEB AT SEAT 5AB WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE NORMAL. 2L72 4F4 FRTA1NM E13NE 20040830000762004083000076EU 2004 8 30 04FDEA02539 120040821A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25663FE 766 MDCC SIDE TRACK AT FR 35 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX 1 INCH. REMOVED AND REPLACED SIDE TRACK IAW SRM 51-40-21 2L72 4F4 FRTA35EU E13NE 20040830000782004083000078EU 2004 8 30 04FDEA02541 120040821A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25663FE 766 N00466 MAIN CABIN SEAT TRACK (0) AT APPROX FRAME 78 HAS CORROSION ON TOP OF LUGS AND IN BOTTOM OF SCALLOPS. REMOVED CORROSION ON MAIN CARGO TRACK (0) FR 78 IAW SRM 51-74-10. MATERIAL LOSS WAS 0.050 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105. REPAIRED SEAT TRACK (0) BETWEEN FRAMES 77.5-79 MAIN CARGO IAW SRM 53-10-16 PG 202. 2L72 4F4 FRTA35EU E13NE 20040830000802004083000080EU 2004 8 30 04FDEA02543 120040822A1420 CONNECTOR AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE MLG UPLOCK CORRODED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25442FE 353 NR 1 MLG DOOR WOULD NOT CLOSE ON GEAR RETRACTION. PUT GEAR DOWN IAW ECAM, RETURNED FOR LANDING. PERFORMED BITE CHECK OF PROX DET UNIT REF A310 M/M 32-31-71-4, RECEIVED BOX FAULT CODE (BOX LIGHT ON) CODE 64= 28VDC POWER SUPPLY NR 4 OR NR 3,SEE A310 TSM 32-61-00 FAULT ISOLATION PAGE 104.A310 TSM 32-61-00 PAGE 117 SUGGESTS TO CHECK C/B 1GB. FOUND SYS 1 MLG DOOR UPLOCK CONNECTOR CORRODED, REPLACED CONNECTOR AND REPINNED REMOVED AND REPLACED LT MLG UPLOCK ASSY OPS CHECK NORMAL. REMOVED AND REPLACED MLG DOOR ACTUATOR, WITH SERVICEABLE ACTUATOR, OPS CHECK NORMAL IAW MM 32-31-00 P. BLOCK 501. JACKED AC IAE MM 07-11-00-0 THRU STEP C 4. SWUNG GEAR SUCCESSFULLY, NO DEFECTS NOTED. 2L72 4F4 FRTA35EU E13NE 20040830000832004083000083NM 2004 8 30 04FDEA02546 120040822A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 48R SPLICE DOUBLER AT STA 5-116 TO STA 1541. DOUBLERS REMOVED PER SRM 51-33-01 VOLUME II. SPLICE DOUBLERS AFA7124-1, AFA7124-2, A5A7125-501 FABRICATED PER DWG AFA7124 AND A5A7125. PART MARKED AS PER FEDEX GMM 7-0-1001. THREE (3) EACH FABRICATED SPLICE DOUBLERS INSTALLED PER SRM 51-33-01 VOLUME II 2L73 4F4 FRTA22WE E24NE 20040830000872004083000087WP 2004 8 30 WX0400024 120040813A2560P4010021 BATTERY DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE FLASHLIGHT DISCHARGED A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19862GA 49556 AFTER SCHEDULED LANDING, MAINTENANCE REPORTED EMERGENCY FLASHLIGHT AT L-1 DOOR CHARGE LIGHT DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED BATTERY IAW MM 25-00-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20040830000882004083000088SO 2004 8 30 HUN2004F00000 220040430A73206538981A11 THROTTLE BODY DIAMONDA20 DA20C1 2990001GL CONT O240 IO240B 17063SO SNSNCHW69EK W69EK63 EA ENGINE MALFUNCTIONED D HUNAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 NM01556DC C0156 806359 AE3811A ON THREE OCCASIONS THIS AC HAD FUEL SYSTEM PROBLEMS. IN FEBRUARY THE ENGINE DIED AT IDLE/LOW POWER OPERATIONS. THE FUEL PUMP WAS REPLACED AND PROBLEM WENT AWAY (OUR OTHER DA-20C1, N6634DC, HAD THE SAME PROBLEM AND REMEDY). AT THE END OF APRIL 556DC LOST POWER AND SAFELY LANDED. THE ENGINE WOULD NOT RUN ABOVE 1500 RPM. THE FUEL PUMP WAS CHANGED AGAIN, AND THE PROBLEM WENT AWAY FOR A FEW DAYS. THE AC THEN HAD AN EMERGENCY LANDING DUE TO POWER FAILURE. TECH REP REPLACED THE THROTTLE BODY / METERING UNIT AND THE PROBLEM WENT AWAY. TECH DECLARED THE ISSUE RESOLVED AND RETURNED AC TO SERVICE. FEEL THERE MAY STILL BE ISSUES WITH THIS ENGINE/WOOD PROP/FUEL SYS CONFIG. THAT HAVE NOT BEEN DISCOVERED. UNKNOWN. 1L71 3O3 ONTTA4CH E7SO 5 NTA4CH 20040830000912004083000091EA 2004 8 30 COMA0460475 120040629A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01479CA 7675 LT LOWER ENGINE SUPPORT BEAM IS CRACKED. C/W REO 601R-53-61-366. 2L72 4F4 FRTA21EA E15NE 20040830000942004083000094EA 2004 8 30 COMA0460485 120040823A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01420CA 7451 LT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A. 2L72 4F4 FRTA21EA E15NE 20040830000952004083000095NM 2004 8 30 KPVA20042 120040121A2434PP794 CIRCUIT CARD DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 2 GEN FAILED A KPVAO OTHER J WARNING INDICATION TOTAKEOFF 1 WP13806WP 357 NR 2 DC GEN CAUTION LIGHT ILLUMINATED BRIEFLY ON TAKEOFF ROLL, ON BRIEFLY DURING TAXI IN. INSPECTED NR 2 DC CAUTION LIGHT AND DEFERRED IAW MEL 24-16. COMPLIED WITH MAINTENANCE PROCEDURES AND REQUIRED. CAT (B) 1/21/04, DUE 1/24/04. PLACARDS INSTALLED. REMOVED AND REPLACED CAUTION ANNUNCIATOR PANEL NR 2 CIRCUIT CARD IAW CMM CHAP 33-10-00 PAGE 701. OPS CHECK DC GEN SYSTEM CHECK GOOD IAW MM CHAP 24-31-00 PAGE 207-209. PLACARDS REMOVED. (M) 2H72 4T4 TRTA13NM E20NE 20040830000992004083000099EU 2004 8 30 04FDEA02547 120040823A5310 CROSSBEAM AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25421FE 342 QA PICKUP FLOORBEAM AT FWD FACE OF FR 33 BETWEEN Y450 AND Y953 WITH HAIR LINE CRACK. 2L72 4F4 FRTA35EU E3NE 20040830001002004083000100NM 2004 8 30 UPS04M42943 120040617A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, HORIZ STAB LT NR 19 BARREL NUT HOLE FOUND CORRODED ON BOTTOM BEARING AND SIDEWALL SURFACE. CORROSION ON B/N HOLE NR 19 LT. REMOVED AND REAMED IAW EO MD11-5510-19409-G FOUND OUT OF LIMIT. REPAIR AND FAB SLEEVE BUSHING FABRICATED IAW EO MD11 -5510-19409-G. PR1422B2 SEALANT APPLIED IAW EN.1215-04 AT,B/N HOLE NR 19 LT. REPAIR SLEEVE BUSHING INSTALLED AT B/N HOLE NR 19 LT IAW EO MD11-51 0-19409-G,FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20040830001032004083000103NM 2004 8 30 UPS04M42946 120040618A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C RT HORIZ STAB BARREL NUT HOLE NR 10 FOUND CORRODED ON THE SIDES. CORROSION AT B/N HOLE NR 10 RT, REMOVED AND REAMED IAW EO MD11-5510-19409-G FOUND LIMIT OUT. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G AT B/N HOLE AT NR 10 RT. PR1422B2 SEALANT APPLIED AT B/N HOLE NR 10 RT IAW EN. 1225-04.REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 10 RT IAW EO MD11-5510-19409-G AND EN.1225-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20040830001052004083000105NM 2004 8 30 UPS04M42949 120040610A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C LT HORIZ STAB NR 18 BARREL NUT HOLE FOUND CORRODED. CORROSION AT B/N HOLE NR 18 LT REMOVED AND REAMED, BLEND TO 1.067 INCHES FOUND EXCEEDED EO MD11-5510-19409-G LIMITS. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G.PR1422B2 SEALANT APPLIED AT B/N HOLE NR 18 LT IAW EN.1 197-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 18 LT IAW EO MD1 1-5510-19409-G AND EN. 1197-04 FOUND WITHIN LIMIT,SATISFACTORY. 2L73 4F RTA22WE 20040830001062004083000106NM 2004 8 30 ABXA040297 120040825A56105912880509 SEAL BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE L2 WINDOW TORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23707AX 22570 DURING R1 PREFLIGHT, DISCOVERED CAPTAINS NR 2 WINDOW CRANK BINDING TOWARDS CLOSE. FOUND L2 WINDOW SEAL TORN AND CATCHING ON WINDOW, REMOVED AND REPLACED L2 WINDOW SEAL IAW AMM 56-11-11-4. 2L72 4F4 FRTA1NM E3NE 20040830001072004083000107CE 2004 8 30 DXTA200400367 120040822A7700307081612 SENSOR RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP P2T2 INOPERATIVE E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07872QS4349 258472 P107328 DURING TAKEOFF ROLL NR 1 ENG TOOK 4-6 SECS TO ACHIEVE T/O POWER (95.5) PRIOR TO 80KTS, NR 1 ENG ROLLED BACK TO APPROX 93 PERCENT THEN UP TO 94 THEN BACK TO 91-20 PERCENT NR 2 ENG APR ACTIVATED AND ROLLED UP TO 98 PERCENT. (ABORTED T/O) REMOVED P2T2 SENSOR P/N 3070816-12, S/N 9918055H0994 AND INSTALLED NEW P2P2 SENSOR P/N 3070816-12 S/N 041789317272. COMPLIED WITH ENGINE RUN F/T. IAW LMM 72-02-15 REV. 3. 2L72 4F4 FRTA3EU E6WE 20040830001082004083000108EU 2004 8 30 DHL2004366005 120040824A2710 AILERON AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE WINGS MALFUNCTIONED A DHLABJA EMER. DESCENT DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01366DH 249 ON DEPARTURE AFTER SLAT RETRACTION AND COMPLETION OF LT TURN, A/C REQUIRED 30 DEG LT AILERON TO MAINTAIN WINGS LEVEL. FCPI CONFIRMED PROPER CONTROL DEFLECTIONS. JETTISONED FUEL AND RETURNED. DEFERRED RT NR 3 ROLL SPOILER IAW MEL 27-62-01-1, CAT. (C) CONTROL NR 17632. MECHANIC NOTIFIED. PLACARDED. 2L72 4F4 FRTA35EU E23EA 20040830001112004083000111EU 2004 8 30 04FDEA02548 120040823A5330A5377866920600 PLATE AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25421FE 342 THE FWD CARGO COMPARTMENT AFT MANHOLE BETWEEN FR38.1 AND FR38.2 ON THE LT SIDE OF THE MANHOLE BETWEEN STR55 AND STR53RT. EXISTING POCKETS REPAIRED WITH EXTERNAL DOUBLER. REPAIRED POCKETS AND NEW POCKETS FOUND WITH CORROSION MORE THAN 50 PERCENT OF FITTING THICKNESS.**** S/D COMING **** 2L72 4F4 FRTA35EU E3NE 20040830001142004083000114 2004 8 30 DHL2004764008 420040821A3414 INDICATOR BOEING727 727264 138408MNM PWA JT8 JT8D17 52049NE AIRSPEED MALFUNCTIONED A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01764AT 22984 RTO DUE TO SPEED CLACKER SOUNDING AT 80 KNOTS . WT = 169,000 IAS = 80 KNOTS OHT = 25 DEG. PA = 400. DEFERRED CLACKER IAW MEL 34-4-1 CAT B CONTROL NR 17604 C/W RTO INSP. IAW B727 MM 05-51-121. CAPTAINS MACH / AIRSPEED IND. REPLACED IAW MM CH 34-12-0 P.3. OPS CHECKS OK. 2L73 4F4 F A3WE E2EA 20040830001152004083000115EU 2004 8 30 WRNA200400009 120040814A2611CG7GF SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE CARGO BAY UNSERVICEABLE A WRNACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO05505TA 271 DURING TAKEOFF ROLL FLIGHT DECK SMOKE LIGHT ILLUMINATED ON F/E PANEL ALONG WITH SMOKE LIGHT ON MWP AND CONTINUOUS CHIME. TAKEOFF WAS REJECTED AT 105KTS AND AIRCRAFT RETURNED TO GATE. FOUND E&E SMOKE DETECTOR SATURATED WITH WATER. INVESTIGATION REVEALED THAT HEAVY RAIN SHOWERS WERE PRESENT DURING CARGO LOADING OPERATION. REPLACED SMOKE DETECTOR AND FUNCTIONAL CHECK CARRIED OUT IAW 26-11-11. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20040830001172004083000117SW 2004 8 30 ALGA096933 120040627A632023071895 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL765 53265 CAE847222 REMOVED GEAR DUE TO SPALLING AT LOW TIME, REPLACED PART WITH NEW ITEM. 1G71 3U3 UO H2SW E1GL 20040830001192004083000119SW 2004 8 30 ALGA096951 120040626A63206893672 PINION GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL765 53265 CAE847222 SPALLING ON GEAR TEETH, THIS IS A RECURRING PROBLEM IN C47B GEARBOXS, WHERE PINION GEARS WEAR PREMATURELY. REPLACED WITH NEW GEAR. 1G71 3U3 UO H2SW E1GL 20040830001232004083000123 2004 8 30 04239658 420040826A3418 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STALL WARNING FAILED A VTZAA UNSCHED LANDING FP FLT CONT AFFECTED NO WARNING INDICATION CRCRUISE 1 EA27658BR 7500 EVENT SUMMARY STATED THAT STALL FAIL. RETURN TO FIELD. INTERROGATED MDC AND FOUND NO STALL RELATED FAULTS. PERFORMED OPS CHECK AFTER RESETTING AIRCRAFT POWER AND FOUND NO DEFECTS WITH STALL SYSTEM AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20040830001262004083000126NM 2004 8 30 CALA0400608 120040823A533065C27755 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2761304 23355 INSPECTION FOUND A 1 INCH CRACK IN EXTERNAL SKIN BETWEEN STA 947.5 AND 967, S10L TO S11L (L-2 DOOR UPPER HINGE CUTOUT FORWARD CORNER RADIUS JUST BELOW THE RAIN GUTTER). A REPAIR WAS INSTALLED IAW SRM 53-60-01, FIGURE 205. A DIP WAS ISSUED TO REINSPECT THE AREA WHEN AIRFRAME HAS ACCUMULATED A TOTAL OF 60,000 CYCLES. THEN ACCOMPLISH REPETITIVE INSPECTIONS EVERY 4,000 CYCLES THEREAFTER AND WITHIN EVERY 15,000 CYCLES AFTER INITIAL, ACCOMPLISH MFEC INSPECTION OF BEARSTRAP INTERNALLY. 2L72 4F4 FRTA16WE E2GL 20040830001342004083000134SO 2004 8 30 SWIA200413607 120040724A27513069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAPS FALSE INDICATIONA SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07587333135 3067 120197 IN-FLIGHT AND ON GROUND MASTER CAUTION (FLAP) WITH DISAGREEMENT, ASYMMETRY AND CONTROL FAULT. REPLACED FLAP ENUNCIATOR UNIT WITH SERVICEABLE UNIT. REF EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040830001372004083000137NM 2004 8 30 QXEA200400571 120040729A2612 FIRE LOOP BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA NR 1 & 2 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09400QX 4030 DURING APPROACH THE CHECK FIRE DETECTOR MASTER WARNING ILLUMINATED ALONG WITH THE MASTER WARNING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT FIRE LOOPS 1 AND 2, THE 1 AND 2 ENGINE DETECTORS, FORWARD BAGGAGE, AND APU FIRE DETECTOR SYSTEMS. ALL SYSTEMS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040830001382004083000138NM 2004 8 30 DHL2004745505 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT FWD BS1090 BELOW STR 19L. DAMAGED AREA OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1; CUT OUT DAMAGED AREA AT STR 18L BS 1084 DIMENTION (1INCH DIA) AND FABRICATED DOUBLER (4.2500 INCH DIA) 2024 T3.0.63 PO NR 900781; FILLER (1 INCH DIA) 2024 T3.0.50 PO NR 900980; TREATED AND PRIMED IAW B727 SRM 51-10-2; INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 FIG 13 2L73 4F4 F A3WE E2EA 20040830001402004083000140NM 2004 8 30 AWXA200400844 120040728A534069353502 STRINGER CLIP BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MAJOR REPAIR, DURING C-19 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 500A, STR 16 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500A, STR 16 RT; FABRICATED A NEW REPLACEMENT TIE CLIP IAW DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8, PG. 1. 2L72 4F RTA16WE 20040830001412004083000141NM 2004 8 30 AWXA200400845 120040727A531065C80735183 DOOR FRAME BOEING737 73733A 1384673NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MAJOR REPAIR, DURING 4-DAY CHECK A 4 INCH CRACK WAS FOUND IN FORWARD CARGO DOOR LOWER FRAME AT UP LATCH BRACKET, BS 440. MAINTENANCE REMOVED CRACKED SECTION OF FORWARD CARGO DOOR LOWER FRAME; FABRICATED A NEW REPLACEMENT SECTION OF FRAME; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 2, AND S.B. 737-52A1100. 2L72 4F RTA16WE 20040830001422004083000142NM 2004 8 30 UPS04M42950 120040611A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, HORIZ STAB LT NR 33 BARREL NUT HOLE FOUND ON BOTTOM BEARING AND SIDE WALL SURFACE CORRODED. CORROSION AT B/N HOLE NR 33 LT, REMOVED AND REAMED IAW EO MD11-5510-19409-G TO 1.178 INCHES FOUND EXCEEDED LIMIT. REPAIR AND FAB SLEEVE IAW EO MD11-5510-19 409-G. APPLIED SEALANT PR1422B2 PER EN1219-04 AT B/N HOLE LT NR 33. REPAIR AND INSTALLED B/N HOLE NR 33 LT IAW EO MD11-5510-19409-G AND EN.1219-04 FOUND WITHIN LIMIT AND SATIS. 2L73 4F RTA22WE 20040830001432004083000143NM 2004 8 30 TSAA0436052 120040702A361032895625 PRECOOLER BOEING737 73776N 13844CHNM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13742AL 30830 ETOPS FLIGHT 352, CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLACED PRE-COOLER CONTROL VALVE AND PRE-COOLER CONTROL VALVE SENSOR. OPS CHECK GOOD AT 90 PERCENT N1 WITHOUT BLEED TRIP. COMPLETED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. FLIGHT VERIFICATION OKAY; CONTINUED FLIGHT. 2L72 4F4 FRTA16WE E2GL 20040830001452004083000145NM 2004 8 30 DL738040775 120040818A2750 FCU BOEING737 737832 13844CFNM TE FLAPS MALFUNCTIONED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27385DN 30348 LE FLAP TRANSIT LIGHT AMBERON FLAP RETRACT DURING TAKEOFF/ DEPARTURE. LE SLATS 2, 3 AMBER ILLUMINATED. AFTER CYCLING FLAPS TO 1 AND BACK TO UP IAW CHK LIST, LE SLATS 2,3 6 AND 7 TURNED AMBER. RETURNED FLAPS 15 FOR LANDING. 225 KNOTS MAX AIRSPEED DURING FLIGHT. FSEU FAULTED MULTIPLE PROX (MSG 27-81224). RAN ALT FLAPS/ SLATS TO EVEN SLATS. CLEARED FSEU. RAN FLAPS SLATS MULTIPLE TIMES WITH ALL INDICATIONS AND MOVEMENTS NORMAL. INTERMITTENT FAULT IAW M/M. 2L72 4F RTA16WE 20040830001462004083000146NM 2004 8 30 DL733040776 120040818A5330654577567 SKIN BOEING737 737347 1384647NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 CRACK REPAIR, THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 757 JUST BELOW STRINGER 19R RUNNING ALONG THE UNDERLYING BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 092756-14. 2L72 4F4 FRTA16WE E2GL 20040830001472004083000147NM 2004 8 30 DL75K040777 120040819A3260BCREF7816 LIGHT BOEING757 757232 1384965NM PWA 2037 PW2037 NE COCKPIT LOOSE A DALAO OTHER N FALSE WARNING APAPPROACH 1 SO276706Q 30422 CREW REPORTED THE NLG DOWN AND LOCKED GREEN LIGHT ASSY WOULD NOT ILLUM DURING APPROACH. CREW DECLARED EMERGENCY BUT LANDED WITHOUT INCIDENT. MTC REPORTS LIGHT ASSY MODULE WOULD NOT LOCK INTO POSITION AND WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 20040830001492004083000149EA 2004 8 30 04199626 120040717A2121 FAN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EXHAUST INOPERATIVE A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27626BR 7225 REPORT OF SMOKE IN CABIN. DECLARED EMERGENCY. RTF LANDED UNEVENTFULLY. PASSENGERS DEPLANED BY NORMAL DOOR ON TAXI WAY. EXHAUST FAN WAS REMOVED AND REPLACED. 2L72 4F4 FRTA21EA E15NE 20040830001512004083000151NM 2004 8 30 DL767040780 120040819A2121732591A FAN BOEING767 767232 1385132NM GE CF680 CF680A2 NE FWD CARGO INOPERATIVE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27114DL 22226 FORWARD EQ SUPPLY FAN 2 EICAS MSG WITH EQUIP COOLING SUPPLY FAN 2 CB POPPED STRONG ELECTRICAL FUMES IN COCKPIT, REPLACED FAN. 2L72 4F4 FRTA1NM E13NE 20040830001522004083000152NE 2004 8 30 DL76L040781 220040819A7261 BEARING BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE LEAKING A DALAK NONE K FLUID LOSS ININSP/MAINT 1 SO27180DN8885 25985 724314 NR 2 ENGINE REPLACED DUE OIL LEAK FROM NR 3 BEARING BREATHER. 2L72 4F4 FRTA1NM E24NE 20040830001532004083000153NM 2004 8 30 F3LA200400077 120040812A2730 WARNING LIGHT AIRBUSA319 A319111 3930336NM ELEVATOR ILLUMINATED A F3LAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM03921FR 2010 BLOCK TURN BACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. PERFORMED EFCS GROUND SCANS EFCS 1 AND 2. OPS CHECK NORMAL. NO FAULTS FOUND IAW MM 27-96-00-740-001 TSM. PERFORMED ELEVATOR AND AILERON TEST OF THE EFCS IAW MM 27-96-00 PB 001. NO FAULTS FOUND. PERFORMED ENGINE RUNS AND COULD NOT FIND ANY FAULTS. AIRCRAFT OPERATION IS NORMAL. NO FAULTS ON PFR'S. 2L72 4F RTA28NM 20040830001542004083000154NM 2004 8 30 QXEA200400593 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 SEAT RAIL NR 12 HAS LIGHT CORROSION AT STATION 177.00 TO 193.00, APPROXIMATELY 16 INCHES WHERE SEAT TRACK COVER RIDES. LIGHTLY BLENDED OUT CORROSION FROM SEAT TRACKS AS INDICATED. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .003 INCH WITHIN SERVICEABLE LIMITS IAW RD 8/4-53-884. 2H72 4T4 TRTA13NM E00062EN 20040830001552004083000155NM 2004 8 30 QXEA200400597 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 LIGHT CHAFING ON TRACK NR 2 AT X 489.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1. AREA AT TOP 1.2 INCH LONG, .125 INCH WIDTH, DEPTH .002 INCH. INSIDE CHANNEL 1.2 INCH LONG BY .5 INCH WIDTH, .002 DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2H72 4T4 TRTA13NM E00062EN 20040830001562004083000156EA 2004 8 30 QXEA200400622 120040807A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09615QX 10065 BULKHEAD CRACKED AT BATHTUB FITTING RT SIDE OF AFT PRESSURE BULKHEAD. REPAIRED IAW REO 670-53-61-034. 2L72 4F4 FRTA21EA EOOO63EN 20040830001572004083000157NM 2004 8 30 QXEA200400601 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 TRACK NR 2 HAS LIGHT CORROSION ON TOP FLANGE AT X 373.0. BLENDED LIGHT CORROSION, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 2.0 INCHES LONG, 3.8 INCH WIDE AND .003 INCH DEEP. HFEC INSP IAW 1-84-7A, PT 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T4 TRTA13NM E00062EN 20040830001582004083000158WP 2004 8 30 P9RA20040023 120040729A5248H2028B PROXIMITY SWITCH DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE TAIL CONE STICKING A P9RAO OTHER J WARNING INDICATION DEDESCENT 1 SO1114816 49370 IB FLIGHT, APPROXIMATELY 10 MINUTES BEFORE LANDING, TAIL CONE ANNUNCIATOR ILLUMINATED AND REMAINED ON. QRH PROCEDURE FOLLOWED. NO EMERGENCY DECLARED. UNEVENTFUL LANDING. FOUND DOOR PROXIMITY SWITCH STICKING. CLEANED AND LUBRICATED SWITCH.NO OTHER DEFECTS NOTED. OK FOR CONTINUED SERVICE. 2L72 4F4 F A6WE E2EA 20040830001612004083000161NM 2004 8 30 QXEA200400599 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 LIGHT CHAFING ON TRACK NR 2 AT 471.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1. AREA 1.2 INCH LONG, 1.2 INCH WIDTH, .003: DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, PART 6. 2H72 4T4 TRTA13NM E00062EN 20040830001622004083000162NM 2004 8 30 QXEA200400600 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 LIGHT CHAFING ON TRACK NR 2 AT X 456.0. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-844, STEP 1. AREA 1 INCH LONG, 1.4 INCH WIDE AND .003 INCH DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844 STEP 6. 2H72 4T4 TRTA13NM E00062EN 20040830001632004083000163WP 2004 8 30 MWEA040115 120040706A53505910456503 STRUCTURE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE TAILCONE OVERSIZED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48072 DURING TAILCONE DROP TEST, AFT CABIN DOOR ARMING PIN WOULD NOT ENGAGE DUE TO PIN HITTING COVER ABOVE DOOR. TRIMMED SLOT LONGER. 2L72 4F4 F A6WE E2EA 20040830001642004083000164EU 2004 8 30 ZJ62004F00000 120040723A7712 INDICATOR BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP ENGINE TORQUE MALFUNCTIONED E ZJ6AO OTHER O OTHER NRNOT REPORTED 1 EA11404GJ 754 RT ENG TORQUE AND RPM DROPPED. TORQ FELL TO APPROX 10 PERCENT REGARDLESS OF PWR LEVER POSITION. EGT WAS FLUCTUATING BETWEEN 450 DEGREES AND 650 DEGREES C. ENG RPM THEN STABILIZED AT 96 PERCENT WHILE TORQ REMAINED AT 10 TO 20 PERCENT REGARDLESS OF PWR LEVER POSITION. ON GROUND, WITH PWR LEVER IN GROUND IDLE RANGE, LT ENG TORQUE INDICATED 40 PERCENT, WHILE RT ENG WAS 5 PERCENT. LT ENG TORQUE GAUGE APPEARED TO BE STUCK AT 40 PERCENT EVEN THOUGH ENG AND PROP BEHAVED NORM. RT ENG PWR LEVER PUSHED FORWARD .7500 TRAVEL PRODUCED ONLY 30 PERCENT TORQUE. OIL PRESSURE AND TEMP F/F NORMAL. VISUALLY CHECKED WIRES AND LINKAGES AROUND NR 2 ENG. ENG RUN NORMAL IAW MM. NO DEFECTS NOTED. UNABLE TO DUPLICATE. PROBLEM. 2L72 4T4 TRTA21EU E4WE 20040830001652004083000165NM 2004 8 30 UPS04M42951 120040614A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 3 BARREL NUT HOLE FOUND CORRODED. CORROSION AT B/N NR 3 LT REMOVED AND REAMED TO 0.988 INCH AND BLEND OUT TO 0.050 INCH DEEP FOUND OUT OF EO MD11-5510-19409-G LIMIT. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 3 LT IAW EN.1212-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 3 LT IAW EO MD11-5510-19409-G AND EN.1212-04 FOUND WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040825000522004082500052EA 2004 8 25 MASA200400342 120040615A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STIFF A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0737178 7178 ASH 6317 PHX. PAX DOOR DIFFICULT TO OPEN. MX CYCLED THE DOOR AND FOUND NO FURTHER DISCREPANCIES. NO PARTS USED. 2L72 4F RTA21EA 20040825000552004082500055NM 2004 8 25 P5CA0401175 120040629A5347 SEAT TRACK BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 SEAT TRACK CORRODED & CRACKED B/W STA 580-560 LBL 62 UPPER DECK. REMOVED DAMAGE SECTION OF SEAT TRACK FROM STA 530-620 IAW SRM 51-30-08. NEW SECTION OF SEAT TRACK INSTALLED PER SRM 51-40-02, 51-11-25. 2L74 4F4 F A20WE E3NE 20040825000572004082500057EA 2004 8 25 MASA200400324 120040609A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX OUT OF RIG A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07509MJ 10094 ASH 7080 CVG-ORD. PAX DOOR WILL NOT OPEN. THE AIRCRAFT FERRIED TO TUS FOR FURTHER TROUBLESHOOTING. MX PERFORMED DOOR RIG CHECKS OF WHICH ALL CHECKED GOOD. LUBED THE DOOR AND PERFORMED NUMEROUS OPS CHECKS, ALL CHECKED GOOD. NO PARTS USED. 2L72 4F RTA21EA 20040825000612004082500061NM 2004 8 25 04206500 120040724A3610 PRESSURE VALVE DORNERDO32 DO328300 NM BLEED IAR DEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27500FJ PLANE RETURNED TO FIELD AFTER RECEIVING BLEED SOV CAS MESSAGE ON TAKEOFF, FOLLOWED BY LAV SMOKE CAS AT 1000 FT. BOTH INDICATIONS EXTINGUISHED WHILE RETURNING FOR LANDING. NO SMOKE WAS DETECTED. PASSENGERS DEPLANED AT THE GATE. LEFT MDPRSOV WAS REMOVED AND REPLACED, AND OPS CHECK GOOD ON REF TO 36-11-07. 2H72 4T RTA55NM 20040825000622004082500062EA 2004 8 25 MASA200400398 120040712A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07507MJ 10077 ASH 7162 DEN-CID. MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED DOOR, OPS CHECKED GOOD. 2L72 4F RTA21EA 20040825000652004082500065NM 2004 8 25 SWAA042417 120040821A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 480, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040825000762004082500076EA 2004 8 25 04207452 120040725A7732 SENSOR CNDAIRCL600 CL6002B19 1900309EA ENG VIBE DEFECTIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27452BR ENGINE MISCOMPARE. A/C LANDED UNEVENTFULLY AND PASSENGERS DEPLANED AT THE GATE. FOLLOWING COMPONENTS WERE REMOVED AND REPLACED: VIBROMETER 606KD, RT VIBE SENSOR, RT VIBE PUSHBUTTON 620KD. BORESCOPE INSPECTION WAS PERFORMED. 2L72 4F RTA21EA 20040825000772004082500077SO 2004 8 25 C2XA04CL082 120040819A3030CS500060D4A SENSOR EMB 145 EMB145LR 3260212SO COCKPIT BURNED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2713913 145438 CLEVELAND FLIGHT NUMBER 3247, ON DESCENT STRONG ELECTRICAL BURNING SMELL IN COCKPIT AND CABIN. FLIGHT ATTENDANT NOTED A SLIGHT HAZE IN CABIN. MAINTENANCE REPLACED PITOT/STATIC CURRENT SENSOR K0057 ON THE RIGHT DC POWER PANEL. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040825000792004082500079NM 2004 8 25 SWAA042401 120040819A531069353656 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 328, STRINGER 21L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040825000812004082500081NM 2004 8 25 SWAA042403 120040819A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 188, STRINGER 17R, STRINGER 17L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040825000892004082500089NM 2004 8 25 QXEA200400549 120040720A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09361PH 516 PDX - SEAT TRACK NR 4 HAS CORROSION FORMING AT APPROXIMATELY STATION 260. REPLACED NR 4 SEAT TRACK. 2H72 4T RTA13NM 20040825000912004082500091SO 2004 8 25 C2XA04IA102 120040817A291014570262403 HOSE EMB 145 EMB145LR 3260212SO HYD SYSTEM BROKEN A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2716951 145063 BPT - FLIGHT 2409, DURING CLIMB THE CREW REPORTED THE LOSS OF ALL HYDRAULIC FLUID FROM THE NUMBER ONE SYSTEM. THE AIRCRAFT RETURNED TO BPT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE INBOARD HOSE ASSEMBLY, SERVICED THE HYDRAULICS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825000942004082500094EA 2004 8 25 04213697 120040731A2432 CHARGER CNDAIRCL600 CL6002B19 1900309EA MASTER BATTERY INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27697BR 7787 APU AND MAIN BATTERY CHARGERS MESSAGES WHILE IN CLIMBING PHASE. RETURNED TO FIELD AND CHANGED PLANES. BOTH CHARGERS WERE REMOVED AND REPLACED. 2L72 4F RTA21EA 20040825001042004082500104NM 2004 8 25 QXEA200400580 120040806A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - RIGHT INBOARD NR 7 SEAT TRACK DAMAGED BEYOND LIMITS AT APPROXIMATELY X342.00. REPAIRED IAW DHC-8 SRM 51-40-11 AND RD 8-53-4473. 2H72 4T RTA13NM 20040825001072004082500107NM 2004 8 25 QXEA200400583 120040806A5320 HINGE DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - LAVATORY SERVICE PANEL LOWER FLANGE BY AFT END OF DOOR HINGE HAS CORROSION. REPAIRED IAW RD 8-53-2103 AND RD 8-53-3299. 2H72 4T RTA13NM 20040825001142004082500114EA 2004 8 25 04227624 120040814A3260 SQUAT SWITCH CNDAIRCL600 CL6002B19 1900309EA NLG DEFECTIVE A VTZAB EMER. DESCENT N FALSE WARNING CLCLIMB 1 EA27624BR 7211 AFTER TAKEOFF CREW RECEIVED GEAR DISAGREE WITH GEAR UP. WOW INPUT FAIL AND NOSE STEERING MESSAGE. CREW DECLARED AN EMERGENCY. ADJUSTED NLG WOW SENSORS AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2L72 4F RTA21EA 20040825001232004082500123NM 2004 8 25 P5CA0401171 120040816A2120 SMOKE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL COCKPIT DETECTED A P5CAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP23450PA 30808 THIRTY MINUTES PRIOR TO DEPARTURE, SMELLED SMOKE IN COCKPIT. NO MESSAGE DISPLAYED. INSPECTED LT MEC & REMOVED PANELS 516, 614, 414. NIL EVIDENCE OF ANY BURNING OR SMOKE FOUND, NO C/BS POPPED. 2L74 4F4 FRTA20WE E23EA 20040825001352004082500135EA 2004 8 25 04152632A 120040602A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27632BR 7268 DURING HEAVY CHECK THE FRAME DOUBLER WAS FOUND CRACKED AT FS 640 STR 10. THE FRAME WAS REPAIRED PER MANUFACTURER INSTRUCTIONS AND AIRCRAFT WAS RETURNED TO SERVICE ON COMPLETION OF INSPECTION. 2L72 4F RTA21EA 20040825001362004082500136EA 2004 8 25 04157710 120040605A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27710BR 7852 DURING INSPECTION THE LEFT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825001382004082500138NM 2004 8 25 P5CA0401145 120040809A5345 ANGLE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 L-ANGLE BROKEN AT STA 1940, L1 BIL 20 AFT CARGO AREA. REMOVED AND REPLACED BROKEN BRACKET PER SRM 51-30-02. NEW BRACKET FABRICATED PER SRM 53-11-23. 2L74 4F4 F A20WE E3NE 20040825001452004082500145EU 2004 8 25 MALA040506 120040709A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15525XJ E2350 BATTERY P/N 51-2275-1, S/N 9803378 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1. PASSED CMM TESTS. A/C RETURNED TO SERVICE 7/11/04. 2H74 4F RTA49EU 20040825001502004082500150EU 2004 8 25 MALA040511 120040714A3350610478 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15361PX 340B249 BATTERY PACK P/N 61-0478, S/N 16020 WAS DISCHARGED. CAPACITY CHECK FAILED. MAINTENANCE DEEP CYCLED UNIT. PASSES CMM CHECKS. 2L72 4T RTA52EU 20040825001552004082500155EA 2004 8 25 04167697 120040615A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27697BR 7787 DURING INSPECTION THE RIGHT HAND FUSELAGE OVERWING EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040825001642004082500164NM 2004 8 25 SWAA042333 120040813A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED 5Y CHECK, FOUND CABIN SIDEWALL EMERGENCY EXIT LIGHT LENS AT ROW 18 DEF, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040825001722004082500172NM 2004 8 25 QXEA200400531 120040715A3097697070212 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM PROPELLER DAMAGED A QXEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM09414QX 4061 PDX - FLIGHT 2317 PROP DE-ICE CAUTION LIGHT ILLUMINATED APPROXIMATELY 5 SECONDS AFTER ILLUMINATION OF NR 2 PROP DE-ICE ADVISORY LIGHT. COMPLIED WITH PROP DE-ICE CAUTION LIGHT CHECKLIST. PROP DE-ICE CAUTION LIGHT CONTINUED TO ILLUMINATE. MAINTENANCE REPLACED WIRE HARNESS. TEST OF PROP DE-ICING SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040825001742004082500174WP 2004 8 25 AALA20040840 120040812A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21474 49649 MIA - FORWARD MOST BLOCK OF CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK NEXT TO FORWARD LAVATORY FOR FORWARD MOST BLOCK OF CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040825001802004082500180NM 2004 8 25 AALA20040849 120040812A2780834503 SENSOR BOEING767 767323 1385205NM SLATS INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21381AN 25450 HNL - INFLIGHT T270/12 ON INITIAL CLIMBOUT BEFORE FLAP HANDLE MOVED LEADING EDGE FLAP ASYMMETRY LIGHT CAME ON. RETURNED TO HNL AND LANDED WITHOUT INCIDENT. DUPLICATED FAULT WITH SLATS. FOUND FAULT ASSOCIATED WITH NUMBER SIX SLAT SENSOR. REPLACED SENSOR SWITCH FOR NUMBER 6 INBOARD SLAT LEFT WING SENSOR NUMBER 281. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040825001822004082500182 2004 8 25 AALA20040858 420040817A2565D29982125 SLIDE DOUG DC9 DC982 3022082WP PAX DOOR DISLODGED A AALAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW217533A 49987 DCA - FORWARD ENTRY DOOR SLIDE PACK FELL OFF WHEN AGENT TRIED TO CLOSE THE DOOR. UNSUCCESSFUL DEPLOYMENT. REPLACED DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040825001862004082500186NM 2004 8 25 P5CA04011054 120040806A5210 SKIN BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE PAX DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CRACK IN LWR CORNER OF MAIN ENTRY DOOR. REPAIRED IN LWR FWD CORNER L1 DOOR IAW SRM 52-10-02. 2L74 4F4 F A20WE E3NE 20040825001902004082500190WP 2004 8 25 AALA20040806 120040801A2131 CONTROLLER DOUG DC9 DC983 3022083WP CABIN PRESSURE INOPERATIVE A AALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW21589AA 53252 DFW - INFLIGHT T1096/01 LOST PRESSURIZATION AT 31,000 FEET. PERFORMED EMERGENCY DESCENT. RETURNED TO DFW. REPLACED BOTH NUMBER 1 AND NUMBER 2 PRESSURE CONTROLLERS. ACCOMPLISHED COMPLETE SYSTEM TESTS PER MAINTENANCE MANUAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040825001962004082500196NM 2004 8 25 QXEA200400602 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 2 HAS LIGHT CHAFING AT 358.2. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1 AREA 1.0 INCH LONG, .5 INCH WIDE AND .002 INCH DEEP. HFEC INSP AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040825002032004082500203EU 2004 8 25 AWXA200400679 120040604A5320D5348004820100 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE AND LOWER SURFACE NUT PLATES OF R-2 DOOR SHAPE SILL BETWEEN FR 66 AND FR 68, Y1502 RIGHT. MAINTENANCE CUT OUT 3 EACH SECTIONS OF R-2 DOOR SHAPE SILL BETWEEN FR 66 AND FR 68, Y1502 RIGHT; FABRICATED 3 EACH FILLERS AND A REPAIR PLATE; INSTALLED REPAIR PARTS IAW A320 53-41-14, FIG 201 PG 202-212. 2L72 4F RTA28NM 20040825002092004082500209NM 2004 8 25 P5CA0401165 120040731A5753 FLAP TRACK BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE TE FLAPS DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DELAMINATION SEVERAL AREA O/B SIDE OF NR 2 FLAP TRACK AFT FAIRING R/W. REMOVED DAMAGED AREA PER SRM 51-40-15, BONDED REPAIRED PER SRM 51-40-12. 2L74 4F4 F A20WE E3NE 20040825002162004082500216NM 2004 8 25 AWXA200400715 120040620A53406545810517 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 18 RIGHT UPPER LEG STIFFENER, AFT SIDE OF BS 312. MAINTENANCE REMOVED CRACKED STRINGER TIE AT BS 312, STR 18 RIGHT; FABRICATED A NEW REPLACEMENT STRINGER TIE PER DWG 65-45810; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2L72 4F RTA16WE 20040825002212004082500221NM 2004 8 25 AWXA200400720 120040619A534069353641 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 1006, STR 24 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, STR 24 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12. 2L72 4F RTA16WE 20040825002512004082500251SO 2004 8 25 C2XA04SH482 120040815A531514530627001 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713914 145430 SHV - DURING C-CHECK, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3, FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825002522004082500252SO 2004 8 25 C2XA04TY152 120040813A531514521700007 FLOORBEAM EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 DURING A SCHEDULED 1C INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CORRODED AREA WAS SUBSEQUENTLY REMOVED AND A FILLER AND DOUBLER WAS INSTALLED IAW THE EMB SRM. ACFT WAS RELEASED FOLLOWING COMPLETION OF THE 1C INSPECTION. 2L72 4F RT 20040825002542004082500254NM 2004 8 25 SWAA042426 120040821A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND AFT RT AND LT EMERGENCY EXIT LIGHTS INOP. RELAMPED EMERGENCY LIGHTS PER MM. 2L72 4F RTA16WE 20040826000012004082600001NM 2004 8 26 04FDEA02529 120040819A5330 DOUBLER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 NR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TEAR STRAP AT STA 600 STR 9 RH PER SRM 53-30-4 FIG 9 2L73 4F4 FRTA3WE E2EA 20040826000052004082600005SO 2004 8 26 C2XA04TY153 120040816A531514532636401 FLOORBEAM EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714105 145649 DURING A SCHEDULED 1C INSPECTION CORROSION WAS FOUND BETWEEN FR 24 AND FR 25 ON THE LT OMEGA BEAM. MAINTENANCE CUTOUT THE CORRODED AREA, FAB A DOUBLER AND SHIMS AND REINSTALL IAW SRM 53-21-01. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL C-CHECK WORK. 2L72 4F4 FRT TE6CH 20040826000072004082600007SO 2004 8 26 C2XA04TY149 120040806A531514590181409 FLOORBEAM EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL GALLEY FLOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711106 145650 DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL JUST AFT OF THE COCKPIT DOOR STEP. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW SRM 53-21-10 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F4 FRT TE6CH 20040826000162004082600016NM 2004 8 26 04FDEA02367 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.071 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040826000232004082600023EA 2004 8 26 ASOA04463 120040628A5260601R3198045 STEP BOMBDR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 7317 DURING A C-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE BOTTOM STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. 2L72 4F4 FRTA21EA E15NE 20040827000112004082700011NM 2004 8 27 SWAA042454 120040824A57536546435274 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20040827000192004082700019NM 2004 8 27 SWAA042434 120040823A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 EMERGENCY EXIT LIGHT LENS LOOSE NEXT FWD F/A'S SEAT. REMOVED AND REPLACED LENS ASSY PER MM. 2L72 4F RTA16WE 20040827000252004082700025NM 2004 8 27 SWAA042457 120040825A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY SIGN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 R2 DOOR EMERGENCY EXIT SIGN MISSING LENS. REMOVED AND REPLACED R2 DOOR EMERGENCY EXIT SIGN LENS PER MM. 2L72 4F RTA16WE 20040827000442004082700044NM 2004 8 27 SWAA042472 120040825A55116547507 RIB BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STAB LOWER RIB CHORD AT STATION 120.30, CRACKED. REMOVED AND REPLACED LOWER RIB CHORD PER SRM, BAC DRAWING. 2L72 4F RTA16WE 20040827000512004082700051EA 2004 8 27 COMA0460470 120040823A5340601R53410591 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01477CA5851 7670 INTERCOSTAL ANGLE AT FS 484.00 LBL 36 IS CRACKED. PERFORMED A MAJOR REPAIR AT FS 484.00 LBL 36 BY CUTTING AWAY DAMAGED ATTACHMENT FLANGE, EDDY CURRENT AREA, FABBED NEW ANGLE AND INSTALLED IAW BOMBARDIER REO 601R-53-059 REV A. 2L72 4F RTA21EA 20040827000552004082700055EA 2004 8 27 SWIA200413706 120040816A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07930SW 7713 RUDDER TRIM WILL NOT MOVE NOSE RIGHT. REPAIRED BROKEN WIRE AT RUDDER TRIM SWITCH IAW CRJ WM CHAPTER 20-10-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040827000582004082700058SO 2004 8 27 SWIA200413709 120040818A3350 COVER EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07226SW 120296 AFT EMERGENCY FLOOR LIGHTING TRACK CAME APART. INSTALLED MISSING LAMP COVER AND RE-ASSEMBLED LIGHTING TRACK. OPERATIONAL CHECK GOOD IAW 33-50-00. 2L72 4T RTA31SO 20040830000022004083000002EU 2004 8 30 04FDEA02564 120040825A3230224TS05Y CONTROL MODULE AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE MLG INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25419FE 345 LANDING GEAR FAIL TO RETRACT ON TAKEOFF. QRH PROCEDURES FOLLOWED BUT GEAR HANDLE WOULD NOT RETRACT. OVER WEIGHT QRH PROCEDURES FOR LANDING COMPLETED. LANDED AT 290,000 LBS AT FPM SINK RATE, SMOOTH LANDING, NO CROSS WINDS FACT 26AUG04 05:03 PVG U T/S IAW TSM 32-30-00 FIG 109 DURING STEP 3 FOUND L/G CONTROL LEVER TO HAVE RATTLING INSIDE. REMOVED AND REPLACED LANDING CONTROL MODULE IAW 32-31-11-4 ACCOMPLISHED GEAR SWING IN THE NR 1 AND 2 POSITION BOTH OK. GEAR SWING AS IAW AMM 32-31-00 AIRCRAFT OK FOR SERVICE. BITE TEST OF 54GB NO FAULTS NOTED. 2L72 4F4 FRTA35EU E3NE 20040830000082004083000008EA 2004 8 30 SWIA200413729 120040821A2760 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07934SW 7722 ON TAXI OUT, DURING FLIGHT CONTROL CHECK, SPOILERON FAULT MESSAGE ILLUMINATES. REPLACED RT SPOILERON IB PCU IAW MM 27-62-01. REPLACED SECU NR 1 AS IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040830000102004083000010 2004 8 30 SWIA200413731 420040820A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07214SW 120280 LT STALL WARNING LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LT NR 1 STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040830000142004083000014EA 2004 8 30 COMA0460471 120040823A5320601R53611172 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA LYC O540 IO540B1A5 41532EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01477CA5851 7670 FLOOR SUPPORT ANGLE AT FS 621.00 RT SIDE IS CRACKED. PERFORMED A MAJOR REPAIR AT FS 621.00 RT SIDE BY CUTTING AWAY DAMAGED PORTIONS OF ASSY, TOUCH UP CUT AREA, INSTALL NEW STRAP AND REPAIR ANGLE IAW REO 601R-53-61-117 REV B. 2L72 4F3 ORTA21EA 1E4 20040830000232004083000023WP 2004 8 30 04FDEA02538 120040821A5315AGA384915 FLOORBEAM DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 AFT PIT, FLOORBEAM CAP BEAM AT STATION 1887.0 HAS EXFOLIATION. REMOVED FLOORBEAM IAW SRM 51-33-01 VOL II. INSTALLED NEW FLOORBEAM AGA 3849-15, (FABRICATED ON NON-ROUTINE N01875) IAW DWG AGA 3849 AND SRM 51-33-01 VOL II. REFERENCE NON-ROUTINE N01814. 2L73 4F4 F A22WE E23EA 20040830000242004083000024NM 2004 8 30 04FDEA02531 120040819A3150 DEU DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE NR 1 FAULTY A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25595FE 48553 ON DEPARTURE CLIMBING THROUGH 800 FEET, DEU 1,2,3 SHOWED RED(X) ACCOMPANIED BY MASTER WARNING LIGHT AND BELL, MASTER CAUTION LIGHT, AND ALL ALERTS INDICATING ON EAD. COULD NOT SILENCE WARNING HORN. INTERROGATED CFDS AND FOUND NR 1 DEU FAULTY. REMOVED AND REPLACED NR 1 DEU IAW MM 31-61-02-4, RTS PASSED. 2L73 4F4 FRTA22WE E31N3 20040830000392004083000039NM 2004 8 30 AALA20040891 120040823A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21928AN 29528 CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 952 LT FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 952 LT FOR CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040830000482004083000048CE 2004 8 30 GLBA20030703 120040823A5210 SKIN BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE PAX DOOR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03240GL UE240 COMPLIED WITH EO 04-14 REV 2 CORROSION ON DOOR SKIN. 2L72 4T4 TRTA24CE E26NE 20040830000512004083000051WP 2004 8 30 CALA0400616 120040825A5230 FLANGE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND A 3 INCH CRACK IN THE AFT CARGO DOOR FORWARD LOWER STOP FLANGE. REPAIRED IAW ECRA 5232-01047. 2L72 4F4 F A6WE E9NE 20040830000532004083000053NM 2004 8 30 CALA0400618 120040825A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-51, FIGURE 205. 2L72 4F4 FRTA16WE E2GL 20040830000702004083000070NE 2004 8 30 TSAA04790620 220040822A726169726881 BYPASS SWITCH BOEING737 737209 13844AENM PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A TSAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 WP13827AL3698 23913 NON-ETOPS FLIGHT 67, OGG-HNL: NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT-DOWN NR 1 ENGINE IAW QRH. REPLACED NR 1 ENGINE OIL FILTER BYPASS SWITCH IAW AMM 79-35-11. OPS/LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20040830000712004083000071SO 2004 8 30 CHQA000542 120040823A2120 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11292SK 145488 DURING FLIGHT THERE WAS AN UNUSUAL ODOR THAT FILLED THE COCKPIT AND FIRST THREE ROWS IN THE CABIN WHEN THE HEAT WAS TURNED UP ON THE NR 1 PACK. THE ODOR SOON DISSIPATED. OPS CHECKED PACK SYSTEM IAW FIM 21-20-00-310-801A. NO ODOR NOTED AT THIS TIME AND DATE. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040830000822004083000082NM 2004 8 30 04FDEA02545 120040822A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO CORROSION OBSERVED ON LONGERON 51R SPLICE BETWEEN AT STA 1701 TO STA 172. LONGERON 51R AND SPLICE REMOVED PER SRM 53-10-00 FIGURE 2 VOLUME 1. LONGERON AND SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME 1 AND INSTALLED PER SRM 51-33-01 VOLUME 1. 2L73 4F4 FRTA22WE E24NE 20040830000932004083000093NM 2004 8 30 AALA20040886 120040823A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21928AN 29528 BATTERY PACK AT STATION 565 RT FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 565 RT FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA16WE 20040830001012004083000101NM 2004 8 30 UPS04M42944 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C HORIZ STAB RT NR 9 BARREL NUT HOLE FOUND CORROSION BOTTOM BEARING AND SIDEWALL SURFACE. CORROSION REMOVED AND REAMED AT B/N HOLE NR 9 RT TO 0.988 INCH BLEND TO 0.050 INCH DEEP FOUND OUT OF LIMIT IAW EP MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. PR1422B2 SEALANT APPLIED AT NR 9 RT B/N HOLE IAW EN.1236-04. REPAIR SLEEVE BUSHING INSTALLED IAW EO MD11-5510-1 9409-G AT NR 9 B/N HOLE RT FOUND WITHIN LIMIT, SATISFACTORY. 2L73 4F RTA22WE 20040830001162004083000116EU 2004 8 30 ALGA096916 120040810A6510C631A1103101 DISC PACK UROCOPEC120 EC120B 8680987EU TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03510AL 1251 FOUND CRACKED LAMINATES ON DISC PACK. REPLACED WITH NEW PART IN FIELD. 1G72 3U NCR0001RD 20040830001212004083000121EU 2004 8 30 AWXA200400934 120040825A2120 ODOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE COCKPIT DETECTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28627AW 66 ON CLIMB OUT, AN ELECTRICAL BURNING ODOR NOTICED IN COCKPIT FOLLOWED BY SMOKE COMING FROM AIR CON VENTS IN COCKPIT & CABIN, DONNED O2 MASKS & TURNED BACK, WHEN EXITING RUNWAY RECEIVED PACK 1 OVRHT IND. A/C OUT OF SERVICE. MX FOUND ACM FROZEN, R & R ACM IAW AMM, OPS CK GOOD, NO SMOKE NOTED. NR 1 PACK STILL HAS LOW FLOW PROBLEM, REPLACED NR 1 PACK FLOW CONTROL VALVE IAW AMM, ANTI-ICE VALVE, BYPASS VALVE, AND NR 1 & 2 PACK SENSORS, SYS OPS NORM. INSP OF ACM FOUND TURBINE OUTLET LINED WITH CARBON RESIDUE THAT HAD A NOTICEABLE ODOR, UNIT NOT SEIZED, BUT HAD A HIGH TORQUE OF 56 IN. LBS. DISASSY FOUND TURBINE BEARING DAMAGED WITH A SEVERE RUB & OVRHT COND THAT RESULTED IN A SCORED BEARING JOURNAL ON SHAFT ASSY. 2L72 4F4 FRTA28NM E311NE 20040830001292004083000129NM 2004 8 30 0401426312 120040825A2530 OVEN BOEING747 747451 1384940NM PWA 4056 PW4056 NE GALLEY OVERHEATED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01672US 30267 DURING FLIGHT, SMOKE EMITTED FROM THE 2-7 OVEN AS IT OPERATED HOTTER THAN THE MEDIUM SETTING CAUSING THE SMOKE ALARM TO ACTIVATE. THE OVEN WAS TURNED OFF AND THE CIRCUIT BREAKERS PULLED AND THE SMOKE DISSIPATED SILENCING THE SMOKE ALARM. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OVEN CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F4 FRTA20WE E24NE 20040830001332004083000133SO 2004 8 30 SWIA200413606 120040722A3350 FIXTURE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM06290SW 120317 ROW 6 (EXIT) EMERGENCY LIGHT BROKEN FIXTURE. REPLACED ROW 6 (EXIT) EMERGENCY LIGHT FIXTURE. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040830001362004083000136CE 2004 8 30 962J1 120040621A5210259APP CHECK VALVE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE PAX DOOR BLOCKED B A UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 CE07962J 7128 5500453 DOOR SEAL LEAKING AFTER TAKEOFF, DOOR SEAL DID NOT INFLATE, DOOR SEAL CHECK VALVE HAD FAILED INTERNALLY CAUSING A BLOCKAGE OF AIR TO SEAL. 1L72 4F4 F A22CE E1NE 20040830001662004083000166NM 2004 8 30 UPS04M42952 120040618A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 12 FOUND CORRODED ON THE SIDES. CORROSION ON B/N HOLE NR 12 LT REMOVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 10 INCH DEEP FOUND LIMIT OUT IAW EO MD11-5510-19409-G. REPAIR AND SLEEVE FAB IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 12 LT IAW EN.1224-04.REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 12 LT IAW EO MD11-5510-19409-G AND EN.1224-04 FOUND WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040830001692004083000169NM 2004 8 30 UPS04M42955 120040621A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 09 FOUND CORRODED. CORROSION AT B/N HOLE NR 09 LT REMOVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 40 INCH DEEP IAW EO MD11-5510-19409-G FOUND EXCEEDED LIMIT. REPAIR AND FAB SL EEV BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N H OLE NR 09 LT IAW EN.1229-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOL E NR 09 LT IAW EO MD11-5510-19409-G AND EN. 1229-04 FOUND WITIN LIMIT,SATIS 2L73 4F RTA22WE 20040830001702004083000170NM 2004 8 30 UPS04M42956 120040620A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 34 FOUND CORRODED ON BOTTOM AND SIDEWALL SURFACE. CORROSION AT B/N HOLE NR 34 LT REMOVED AND REAMED TO 1.178 INCH BLEND TO 0.020 INCH DEEP FOUND EXCEED LIMIT IAW EO MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 34 LT IAW EN.1228-04. REPAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-55 10-19409-G AND EN1228-04 FOUND WITHIN LIMIT AND SATIS. 2L73 4F RTA22WE 20040830001712004083000171NM 2004 8 30 UPS04M42957 120040614A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 13 BARREL NUT HOLE FOUND CORRODED. CORROSION AT B/N HOLE NR 13 LT, REMOVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 80 INCH FOUND EXCEEDED IAW EO MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHIN G IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 13 LT AND EN.1213-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 13 LT IAW EO MD11-5510-19409-G AND EN.1213-04 FOUND WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040830001722004083000172NM 2004 8 30 UPS04M42958 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 11 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING SIDEWALL SURFACE CORROSION AT B/N HOLE NR 11 LT, REMOVED AND REAMED TO 0.988 INCH, 7 BLEND TO 0.0 30 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-19409-G.FAB AND REPAIR SL EEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 11 LT IAW EO MD11-5510-19409-G, EN.1185-04 AND EN.1257-04. REPAIR AND INSTALLED SLEEVE/B AT B/N HOLE NR 11 LT EO AND EN ABOVE/M,FOUND SATIS. 2L73 4F RTA22WE 20040830001732004083000173NM 2004 8 30 QXEA200400532 120040714A5210 SCREW DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE PAX DOOR LOOSE A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09359PH14542 514 CREW REPORTS INABILITY TO OPEN PASSENGER DOOR DUE TO LOOSE SCREW ON SUPPORT STRUT. MAINTENANCE REPLACED THE MISSING THREADED INSERT ON THE DOOR SUPPORT STRUT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040830001742004083000174NM 2004 8 30 ABXA040280 120040813A5610141T49183 SCREW BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE SLIDING WINDOW DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23707AX 22570 DURING MAINTENANCE INSPECTION AT BFI, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT CLOSE. NR 2 L WINDOW. REPLACED NR 2 LT WINDOW BALL SCREW AND NUT ASSEMBLY IAW MM CHAP. 56-11-04-4. 2L72 4F4 FRTA1NM E3NE 20040830001752004083000175WP 2004 8 30 04FDEA02320 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AT APPROX 7 O CLOCK POSITION 17.5 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, SKIN IS DIMPLED. APPROXIMATELY .060 INCHES. REWORKED DENT IAW SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED IAW NDT MANUAL 20-20-00, NO CRACKS FOUND, CHECKED LIMITS, WITHIN LIMITS IAW MM 34-11-01-2. PERFORMED INSPECTION (RVSM) OF NOTED DISCREPANT AREA, READING -0.004, FOUND TO BE WITHIN LIMITS IAW MM 34-11- 10-2. REF. NR N00225. 2L73 4F4 FRTA22WE E23EA 20040830001762004083000176WP 2004 8 30 04FDEA02321 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AT APPROXIMATELY 5 OCLOCK POSITION 13 7/10 INCHES FROM CENTER OF RT PRIMARY STATIC PORT, SKIN IS DIMPLED APPROX .014. REWORKED DENT IAW SRM 53-20-00 VOL I, DYE PENETRANT INSPECTED AREA IAW NDT MANUAL 20-20-00, NO CRACKS FOUND. CHECKED LIMITS, FOUND WITHIN LIMITS IAW MM 34-11-01-2. PERFORMED RVSM INSPECTION OF NOTED DISCREPANT AREA, MEASUREMENT IS -0.004, FOUND TO BE WITHIN LIMITS IAW MM 34-11-01-2. REF N/R N00224. 2L73 4F4 FRTA22WE E23EA 20040830001772004083000177WP 2004 8 30 04FDEA02322 120040730A5730ARC0267503 PANEL DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 CORROSION ON MATING SURFACE OF PANEL 541BB. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .032 INCHES, 7075-T6 IAW DRW NR ARC0267. MATERIAL THICKNESS AFTER BLEND OUT .020 INCHES, PART OUT OF LIMITS IAW DC10 SRM 57- 00-01 VOL I. RECIEVED NEW PANEL P/N ARC0267-503 IAW DAC DWG. DRW NR ARC0267. LOCATED, DRILL AND COUNTERSUNK FASTENER HOLES IAW SRM 51-31-01 VOL II. REF N/R N00123. 2L73 4F4 FRTA22WE E23EA 20040830001792004083000179NM 2004 8 30 QXEA200400527 120040716A28202950004201 ACTUATOR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09408QX6945 4050 FLIGHT 2391-THE CREW WAS UNABLE TO TRANSFER FUEL IN FLIGHT, IN EITHER DIRECTION. THE NR 2 FUEL VALVE REMAINED CLOSED. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEM AND REPLACED THE FUEL TRANSFER SHUT-OFF VALVE ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040830001822004083000182NE 2004 8 30 COMA0460479 220040818A7260 COVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE ACCESSORY G/B LOOSE A COMAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO01915CA 7013 FLIGHT 5486 LT ENGINE OIL PRESSURE WARNING. FOUND CRANKING PAD COVER ON ACCESSORY GEARBOX LOOSE. SECURED COVER AND SERVICED OIL SYSTEM. 2L72 4F4 FRTA21EA E15NE 20040830001852004083000185NM 2004 8 30 AWXA200400775 120040710A5320D5347112420000 SHEAR PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-3, 8-9, AND 18. 2L72 4F RTA28NM 20040830001902004083000190EU 2004 8 30 AWXA200400703 120040612A5315D5347217220000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON THE Y1292 BEAM BETWEEN FR 67-68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM AT Y1292 FR 67-68 IAW A320 SRM 51-42-11 PAGES 6 & 7. 2L72 4F RTA28NM 20040830001912004083000191EU 2004 8 30 AWXA200400704 120040612A5315D5347213320200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON THE Y1292 BEAM AT FR66. MAINTENANCE REMOVED AND REPLACED FLOORBEAM AT Y1292 FR66-68 IAW A320 SRM 51-42-11 PAGES 6,7,28 AND SRM 51-49-00 PAGES 2 AND 3 TABLE 1. 2L72 4F RTA28NM 20040830001932004083000193EU 2004 8 30 AWXA200400706 120040617A5347D5713014720000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LT OB Y1292 SEAT TRACK FR 36-41. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT Y1292 FR 36-41 IAW A320 SRM 51-42-11 FIGURES 12,18. 2L72 4F RTA28NM 20040830001942004083000194EU 2004 8 30 AWXA200400707 120040627A3350321454 EPSU AIRBUS320 A320231 3930325EU EMERGENCY LIGHT FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28633AW42899 082 DURING C-04 CHECK OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM FAILS BITE CK ON FWD FLT ATTENDANTS PANEL. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT IAW A320 AMM TASKS 33-51-38-000-001 AND 38-400-001. OPERATIONAL CHECK GOOD IAW A320 AMM SUB TASK 33-51-32 740-050-A. 2L72 4F RTA28NM 20040830001952004083000195NM 2004 8 30 AWXA200400708 120040628A53306545778 SKIN BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 MAJOR REPAIR-DURING C-04 CHECK HFEC INSPECTION OF LOG ITEM DENT, CRACK INDICATION NOTED ON FUSELAGE SKIN AT BS 937,3 INCH ABOVE S24R, APPROX 0.75 INCH LONG. MAINTENANCE INSTALLED A DOUBLER/TRIPLER REPAIR IAW SRM 53-00-01-3 FIG 229. 2L72 4F4 FRTA16WE E2GL 20040830002002004083000200WP 2004 8 30 04FDEA02312 120040730A5753ANB71131 ROLLER DOUG MD10 MD1010F 3022112WP ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 RT IB FLAP TRACK UPPER LOAD ROLLER WORN. REMOVED RT IB FLAP TRACK UPPER LOAD ROLLER AND REPLACED INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H, DUE 12-08-04. REF N/R N00646. 2L73 4F RTA22WE 20040830002042004083000204NE 2004 8 30 PCAA0406227 320040626A6197311479203 WIRE HARNESS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE HAMSTD14SF 14SF* NE NR 2 ENGINE GROUNDED A PCAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA13833EX 282 FLIGHT NR 3765 HAD TO RETURN TO GATE DUE TO HAVING THE NR 1 PROP FEATHER WHEN THE AUTOFEATHER SELECT SWITCH WAS SELECTED TO TEST. MAINTENANCE FOUND THE NR 2 ENGINE INTERFACE HARNESS SHOWING A STRAY GROUND TO THE TORQUE SIGNAL CONDITIONING UNIT. HARNESS WAS REPLACED. AIRCRAFT WAS GROUND RUN, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20040830002052004083000205NM 2004 8 30 QXEA200400545 120040720A52608521700003 DOOR BOMBDRDHC8 DHC8401 1390041NM ZONE 800 STICKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09405QX6981 4047 REAR AIRSTAIR DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED SAME. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040830002092004083000209NM 2004 8 30 0401075534 120040624A5315 FLOORBEAM BOEING757 757251 1384970NM PWA 2037 PW2037 NE FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01534US 24265 DURING (H) CHECK FOUND CRACK IN FLOORBEAM AT BS 700 LBL 45. REPAIRED IAW EA 55-199754. 2L72 4F4 FRTA2NM E17NE 20040830002102004083000210NM 2004 8 30 0401065534 120040624A5347 SEAT TRACK BOEING757 757251 1384970NM PWA 2037 PW2037 NE FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01534US 24265 DURING (H) CHECK FOUND CORROSION ON SEAT TRACK AT BS 1640 LBL 46. REPAIRED IAW EA 55-199278. 2L72 4F4 FRTA2NM E17NE 20040830002112004083000211NM 2004 8 30 DHL2004749006 120040720A33501000679 LIGHT BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE L1 DOOR EXIT INOPERATIVE A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01749DH 22013 ON FORWARD INSTRUMENT PANEL, LE FLAPS INDICATOR HAS RT LIGHT INOP. EMERGENCY EXIT LIGHT OVER L-1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB, OPS CK GOOD IAW BMM CH 33-10-0, P/N 327. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD IAW BMM CH 33-50-01, MM PROCEDURE 33-50-111. 2L73 4F4 FRTA3WE E2EA 20040830002132004083000213NM 2004 8 30 WLDA200433 120040724A2710 AILERON DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE WINGS MALFUNCTIONED A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11273 48519 AIR TURNBACK DUE TO AILERON DEFLECTION DISAGREE LEVEL 2 ALERT ON FLAP/SLAT RETRACTION. DEFERRED ITEM TO DMI M27JL2404-122 IAW MEL 27-13-2 CAT (C). NOTE: NO EMERGENCY DECLARED AND NO FUEL DUMPED. 2L73 4F4 FRTA22WE E24NE 20040830002162004083000216CE 2004 8 30 DXTA200400345 120040722A2612 FIRE DETECTOR CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENGINE MALFUNCTIONED E DXTAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 GL07367QS 5600367 LT ENGINE FIRE LIGHT CAME ON DURING TAXI, BOTH FIRE BOTTLES BLOWN. NO INDICATION ON ENG FIRE UPON EVACUATION. INSPECTED ENGINE WITH NO EVIDENCE OF FIRE, REMOVED AND REPLACED BOTH FIRE BOTTLES IAW MM CHAPTER 26-21-01, RAN ENGINE FOR 20 MINUTES AT VARIOUS POWER SETTINGS WITH NO ENGINE FIRE INDICATION. 2L72 4F4 FRTA22CE E25EA 20040830002202004083000220NM 2004 8 30 QXEA200400570 120040728A5270864202 PROXIMITY SENSOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE PAX DOOR OUT OF ADJUST A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09347PH* 480 FLIGHT RETURNED TO FIELD WHEN DURING CLIMB, THE CREW RECEIVED A PASSENGER DOOR WARNING. MAINTENANCE INSPECTED THE AC AND FOUND THE PROXIMITY SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040830002212004083000221NM 2004 8 30 QXEA200400572 120040728A2750 CIRCUIT BREAKER BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA TE FLAPS TRIPPED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09415QX 4081 WHEN THE FLAPS WERE SELECTED DOWN DURING THE APPROACH, THE FLAPS STOPPED MOVING AT 15 DEGREES. THE FLAP POWER CAUTION LIGHT THEN ILLUMINATED. IAW THE CHECKLIST, THE FLAP POWER CIRCUIT BREAKER WAS RESET. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED OPERATIONAL CHECKS IAW THE SL. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040830002222004083000222NM 2004 8 30 F3LA200400074 120040726A2912840002074 FILTER BOEING737 7373M8 1384615NM HYD SYSTEM A CRACKED A F3LAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM03303FL 156 25039 FLIGHT CREW REPORTED HYDRAULIC SYSTEM (A) QUANTITY DROPPED TO 23 PERCENT INFLIGHT FOLLOWED BY ENGINE DRIVEN HYDRAULIC PUMP LP LIGHT. NO OVERHEAT INDICATIONS. FOUND ACOUSTIC FILTER LEAKING. REPLACED (A) SYSTEM EMDP ACOUSTIC FILTER IAW MM 29-15-27. REPLACED NR 1 ENGINE EDP IAW MM 29-15-12. FLUSHED (A) HYDRAULIC SYSTEM IAW MM 29-15-00. 2L72 4F RTA16WE 20040830002232004083000223WP 2004 8 30 MWEA040122 120040720A5320993653497 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD SERVICE DOOR THRESHOLD SUBFLOOR AT FRAME STATION 168, CORRODED. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20040830002252004083000225NM 2004 8 30 HNAA0400072 120040729A532085320686001 THRESHOLD DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07982HA 380 PAX DOOR THRESHOLD CORRODED ON SILL PLATE. REMOVED AND REPLACED THRESHOLD. 2H72 4T4 TRTA13NM E20NE 20040831000012004083100001CE 2004 8 31 MQK2004F00000 120040621A324025SW12981 LINE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP EMERGENCY BRAKE MISINSTALLED D MQKAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA09513ML209 258641 NR 1, LT EMERGENCY BRAKE RIGID LINE FROM OUTER SHUTTLE VALVE TO INNER SHUTTLE VALVE STRIKING LT MAIN LANDING GEAR STRUT HOUSING WHEN STRUT IS COMPRESSED. (DURING LANDING, NOT WHILE AC IS PARKED) LINE IS MISROUTED/ NOT PROPERLY BENT. NO VISIBLE DAMAGE DONE TO BRAKE LINE, SMALL AMOUNT OF PAINT MISSING FROM STRUT HOUSING. (EA09200402501) 2L72 4F4 FRTA3EU E6WE 20040831000022004083100002NE 2004 8 31 A302004F00000 220040510A85303813 STUD PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2B NE NR 4 CYL PAD SHEARED E A30AA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL05444FM 285 318052096 L79968AC THROTTLES WERE SET AT 32 OF MANIFOLD PRESS. PROPS WERE SET AT 2300 RPM. ENG GAUGES WELL IN THE GREEN. THE RT ENG MANIFOLD STARTED TO DROP. TEMPS AND OIL PRESSURE REMAINED IN THE GREEN. THE EGT STARTED TO DROP. DUE TO LOSS OF MANIFOLD PRESS, SUSPECTED A TURBOCHARGER HAD FAILED. A SAFE LANDING WAS PERFORMED WITHOUT FURTHER INCIDENT. UPON INSPECTION, NR 4 CYL WAS FOUND TO HAVE 5 OF 6 CYL PAD STUDS SHEARED. THIS CAUSED CYL TO VIBRATE YET REMAIN ATTACHED TO CASE AND BREAK EXHAUST STACK WHICH IN TURN RESULTED IN LOSS OF MANIFOLD PRESS. NO EVIDENCE OF IMPACT WAS OBSERVED BETWEEN PISTON AND VALVE ASSY AND NO OTHER CYL BASE STUDS WERE OBSERVED TO HAVE FAILED. THE CAUSE OF FAILURE REMAINS UNDER INVESTIGATION. 1L72 3O3 O A20SO E14EA 20040831000062004083100006SO 2004 8 31 G9C2004F00000 120040720A7120102460002 MOUNT PIPER PA46 PA46500TP 7104622SO PWA PT6 PT6A42 52043NE ENGINE CRACKED B G9CRK NONE O OTHER ININSP/MAINT 1 CE01767TP600 4697036 HH1120 WHILE INSPECTING THE ENGINE MOUNT IAW THE INSTRUCTIONS OF PART 1, MFG SB 1103B, DATED NOV 11, 2003, CRACKS WERE DISCOVERED IN TWO OF THE ENGINE MOUNT TUBE MEMBERS ATTACHED TO THE RT NOSE GEAR ACTUATOR ATTACHMENT FOOT. THE SB SPECIFIES TO INSPECT THE ENGINE MOUNT ACTUATOR ATTACH FEET FOR CRACKS. 1L71 3O4 TRTA25SO E4EA 20040831000072004083100007EU 2004 8 31 KBM2004FAA 120040506A632035035101820 PULLEY SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE MGB UNDERTORQUED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 ENGINE TO MGB POWER SHAFT FORWARD PULLEY ATTACH HOLES ELONGATED DUE TO ATTACHMENT BOLT TORQUE LESS THAN MINIMUM TORQUE AT ORIGINAL INSTALLATION. REMOVED AND REPLACED. ASSELBL AT FACTORY DURING 5900 HR/ 12 YEAR INSPECTION. 1G71 3U3 U H9EU E19EU 20040831000082004083100008EU 2004 8 31 KBM2004F00186 120040506A1430 BOLT SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE COUPLING UNDERTORQUED E KBMAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 WP19215LA 2143 ENGINE TO MGB POWER SHAFT FORWARD COUPLING BOLT TO PULLEY FAIL TORQUE LOAD CHECK, COUPLING REJECTION MANDATORY. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040831000102004083100010CE 2004 8 31 ACE082304 120040823A3260 LIMIT SWITCH BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE NLG OUT OF ADJUST E YADAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03113AX UC41 PILOT REPORTED LANDING GEAR HANDLE WARNING LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. CREW RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR UP LIMIT SWITCH FOR PROPER OPERATION. 2L72 4T4 TRTA24CE E4EA 20040831000112004083100011EA 2004 8 31 COMA0460476 120040818A335060206 SIGN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE EMERGENCY EXIT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01914CA 7012 FLIGHT 5143 EMERGENCY EXIT SIGN AT CABIN DOOR IS INOPERATIVE. REPLACED SIGN. 2L72 4F4 FRTA21EA E15NE 20040831000152004083100015NE 2004 8 31 DL733040691 220040725A7497 WIRE BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE LT ENGINE IGNI SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27951WP 22951 722175 ON DESCENT, CREW SAW SPARK AND HEARD POP COMING FROM THE WHISKEY COMPASS. COPILOT EXTENDING COMPASS AND RECEIVED SMALL SHOCK. NO FURTHER ARCING AND NO DEFECTS WERE NOTED FOR REMAINDER OF DESCENT. DELTA MTC FOUND WHISKEY COMPASS LIGHTING WIRE SHORTED TO LT ENG IGNITION WIRE. SPLICED BOTH WIRES AND REPLACED DAMAGED TERMINAL. WHISKEY COMPASS LIGHTING AND ENG IGNITION OPS NORM. 2L72 4F4 FRTA16WE E2GL 20040831000162004083100016NM 2004 8 31 2004UALA00664 120040714A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 FRAME FLANGE DENTED AT BS 1400, STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040831000182004083100018NM 2004 8 31 2004UALA00666 120040714A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 DOOR 4R FLOOR SUPPORT INNER CHORD BROKEN OUT AND CORRODED AT BS 1681. MAJOR REPAIR ACCOMPLISHED. FLOOR SUPPORT REPAIR SPLICE. 2L72 4F4 FRTA2NM E17NE 20040831000192004083100019NM 2004 8 31 2004UALA00667 120040714A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 FRAME INNER FLANGE DENTED AT BS 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20040831000222004083100022WP 2004 8 31 MWEA040135 120040810A1420 CONNECTOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE ROW 23 LOOSE A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31809ME 48071 STANDBY LIGHT INOPERATIVE AT ROW 23, LT SIDE. SECURED LOOSE CONNECTION. 2L72 4F4 F A6WE E2EA 20040831000242004083100024SW 2004 8 31 ALG2004F00044 120040625A6340 TRANSMITTER BELL 407 407 1182206SW ALLSN 250C 250C47B GL ROTOR TORQUE MALFUNCTIONED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03557AL 53243 CAE847064 ON SECOND TAKE OFF OF THE DAY, ON TAKE OFF FROM LOOP OPS GALLIANO, TORQUE GAUGE READ ERRATIC AND EXCEEDED LIMITS. LANDED AND REFERRED TO MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE TORQUE TRANSMITTER, OPS CHECK WAS GOOD. 1G71 3U3 UO H2SW E1GL 20040831000272004083100027SO 2004 8 31 SWIA200413666 120040809A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE OB LT FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07189SW8909 8909 120048 WHILE SITTING ON THE GROUND, THE A/C DISPLAYED AN UNCOMMANDED ASYMMETRY PROBLEM. INSTALLED SERVICEABLE ACTUATOR ON OB LT FLAP. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040831000282004083100028EU 2004 8 31 04FDEA02441 120040811A5347 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 MAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16 2L72 4F4 FRTA35EU E13NE 20040831000302004083100030NM 2004 8 31 DL764040693 120040725A3350071701100 BATTERY BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE EMERGNECY LIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27833MH 29706 BATTERY PACK WILL NOT HOLD A CHARGE. REMOVED AND REPLACED BATTERY PACKS. ETOPS CATEGORY (E) : PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F4 FRTA1NM E13NE 20040831000312004083100031NM 2004 8 31 DL76P040694 120040725A3350 BULB BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27144DA NA 27584 ON LAYOVER FOUND EMERGENCY LIGHTS INOPERATIVE AT FWD F/A OVERHEAD AND AFT OVERHEAD AT SEAT 47 C AN E. RELAMPED OPERATION OK. 2L72 4F RTA1NM 20040831000342004083100034NM 2004 8 31 MWEA04124 120040723A521059100817 SKIN BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE PAX DOOR DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31904ME 55168 UPPER FORWARD CORNER OF PASSENGER DOOR SKIN EDGE IS BENT 1.00 INCH X 2.00 INCH. REMOVED DAMAGE AND INSTALLED DOUBLER. 2L72 4F4 FTRA6WE E00057EN 20040831000372004083100037WP 2004 8 31 MWEA040129 120040805A534339248472 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE LT MLG WW GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 KEEL TO SLANT PRESSURE PANEL ATTACH BRACKETS IN THE LT WHEEL WELL HAS SEVERAL GOUGES. FABRICATED AND INSTALLED FITTINGS. 2L72 4F4 F A6WE E2EA 20040831000382004083100038NM 2004 8 31 DHL2004745506 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS DENTS FWD BS 1090 ABOVE STR 18L. DAMAGED AREA OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIM 10 INCHES X 8 INCHES IAW SRM 53-30-3 FIG 1. DOUBLER TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED IAW SRM 53-30-3 FIG 1. 2L73 4F4 F A3WE E2EA 20040831000392004083100039WP 2004 8 31 MWEA040130 120040805A5330593600417 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 MODERATE CORROSION ON LOWER FUSELAGE BETWEEN STA 769 TO STA 807 IN THE AREA OF RT LOWER WING TO FUSELAGE FILLET RUB STRIP AT LONGERON RT 29 AND RT 28. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E2EA 20040831000422004083100042WP 2004 8 31 MWEA040131 120040805A53209936534 BRACKET DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FLOOR SUPPORT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD AND AFT BRACKETS FOR THE FLOOR SUPPORT BETWEEN STATION 148-200 RT OF FUSELAGE CENTER LINE ARE CORRODED. FABRICATED AND INSTALLED TWO EACH BRACKETS. 2L72 4F4 F A6WE E2EA 20040831000452004083100045NM 2004 8 31 P5CA0401122 120040706A5347 SEAT TRACK BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CORROSION UPPER DECK SEAT TRACK BS 540-580 RBL 46.65-WL 310. REMOVED AND REPLACED SEAT TRACK FROM BS 530-660, IAW SRM 53-10-05-53-30-08-53-30-02. 2L74 4F4 F A20WE E3NE 20040831000462004083100046NM 2004 8 31 P5CA0401123 120040615A5314 KEELBEAM BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 RT KEEL BEAM CORROSION FROM BS 1310 TO BS 1342. LT KEEL BEAM CORROSION FROM STA 1310 TO STA 1340. REPAIR IAW POLAR MA NR A5349-01-02. 2L74 4F4 F A20WE E3NE 20040831000472004083100047NM 2004 8 31 P5CA0401124 120040727A5520 WEB BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE LT OB ELEVATOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 WEB CRACK FOR CENTER WEIGHT, LT OB ELEVATORS OB ACTUATOR ELEV STA 256. REMOVED CRACKED WEB IAW SRM 51-30-02, FABRICATED WEB IAW SRM 55-20-02, INSTALLED WEB IAW SRM 51-30-02. 2L74 4F4 F A20WE E3NE 20040831000502004083100050NM 2004 8 31 CALA0400592 120040729A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 MAINTENANCE FOUND THE FUSELAGE SKIN DENTED AND CRACKED BETWEEN STA 500D + 10 AND 520, S12L. THE CRACK WAS 1.4 INCHES LONG. AN INTERIM REPAIR WAS INSTALLED IAW ECRA 5330-03361. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 12 MONTHS. 2L72 4F4 FRTA16WE E2GL 20040825002122004082500212NM 2004 8 25 04220429 120040807A7930 TRANSDUCER DORNERDO32 DO328300 NM THRUST REVERSER DEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27429FJ 3194 LEFT ENGINE LOW OIL PRESSURE INDICATION. WHILE ADVANCING THRUST LEVERS, PRESSURE DROP INTO YELLOW ARC. LANDED UNEVENTFULLY. REMOVED AND REPLACED LEFT ENGINE OIL TRANSDUCER (79-31-01). 2H72 4T RTA55NM 20040825002172004082500217NM 2004 8 25 AWXA200400716 120040620A53406545810517 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28306AW 24633 MCN - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 18 RIGHT LOWER LEG STIFFENER, AFT SIDE OF BS 312. MAINTENANCE REMOVED CRACKED STRINGER TIE AT BS 312, STR 18 RIGHT; FABRICATED A NEW REPLACEMENT STRINGER TIE PER DWG 65-45810; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2L72 4F RTA16WE 20040825002302004082500230NM 2004 8 25 SWAA042409 120040820A3350OL307IBPEGPL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29406WN 27894 DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC, INOP. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20040825002352004082500235 2004 8 25 SWAA042423 420040821A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20040825002362004082500236NM 2004 8 25 SWAA042424 120040821A575465C26686 SKIN BOEING737 7373H4 1384600NM RT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED RON, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040825002452004082500245SO 2004 8 25 C2XA04SH481 120040815A531514521700007 FLOORBEAM EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713914 145430 SHV - DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM/FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3, FIGURE 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040825002492004082500249NM 2004 8 25 QXEA200400603 120040812A5347 TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 2 HAS LITE CHAFING AT X 303.5. BLENDED LITE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA .5 INCH LONG, .25 INCH WIDE AND .001 INCH DEEP. HFEC INSP AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2H72 4T RTA13NM 20040825002662004082500266WP 2004 8 25 2004F00246 220040326A7230 BLADE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP NR 2 ENGINE CRACKED A LBWACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA25815DD 35A414 NR 2 RIGHT ENGINE FAILURE DURING TAKEOFF ROLL. TAKEOFF ABORTED. VISUAL INDICATES FAN BLADE CRACKED AT HUB AND SEPARATED. EVALUATION TO DETERMINE CAUSE BEING CONDUCTED BY HONEYWELL. (M) 2L72 4F4 F A10CE E6WE 20040826000152004082600015EA 2004 8 26 ASOA04484 120040705A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11828AS 7213 FLT 4140 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EXTERIOR RIGHT WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EXTERIOR RIGHT WING EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040826000212004082600021 2004 8 26 AWXA200400843 420040802A344146502003030314 ADIRU AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE ZONE 123 FAULTY A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28801AW9322 13 889 AIR TURN BACK, ON CLIMB OUT, EN ROUTE FOR YYZ AT APPROXIMATELY 4000 FT THE FO`S PRIMARY FLIGHT DISPLAY (PFD) SPEED TAPE INDICATED OVER SPEED. REDUCED SPEED TO 235 KTS AND WARNING EXTINGUISHED, AUTOPILOT DISCONNECTED, CAPTAINS PFD WAS NORMAL, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. THIS ADIRU (S/N 3419) HAS TWO PREVIOUS HISTORY EVENTS FOR OVERSPEED WARNING, UNIT IDENTIFIED AS A ROGUE COMPONENT. VENDORS FUNCTIONAL TEST OF ADIRU S/N 3419 CONFIRMED FAILURE OF UNIT FOR FAILING ATP STEP 8.9 "ADR DISC I/O EXTERNAL ADR IDW2". REPLACED REAR PANEL ASSEMBLY (A3) AND PERFORMED THERMAL CALIBRAT2L72 4F4 FRTA28NM E311NE 20040826000242004082600024NM 2004 8 26 2004UALA00743 120040726A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29926UA 26648 DAMAGED AREA EIGHT INCHES LONG ON FUSELAGE AFT OF REAR CARGO DOOR TEN INCHES FROM AFT DOOR FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040826000252004082600025NM 2004 8 26 2004UALA00759 120040730A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 R1 DOOR CUT-OUT FWD FRAME CRACKED JUST ABOVE STR 17R AT STA 294. MAJOR REPAIR ACCOMPLISHED. REMOVED THE CRACKED FRAME AND FABRICATED A REPAIR. 2L72 4F4 FRTA16WE E2GL 20040827000022004082700002NM 2004 8 27 UPS04242970 120040810A5411 FRAME BOEING727 72722C 138400FNM NR 2 NACELLE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, ENGINE NR 2 NACELLE UPPER FRAME CRACKED BETWEEN MID AND AFT HINGE POINTS. FABRICATED FRAME IAW SRM 54-10-06, FRAME REPLACED IAW SRM 51-30-02. 2L73 4F A3WE 20040827000032004082700003NM 2004 8 27 UPS04242971 120040809A5414 PANEL BOEING727 72722C 138400FNM NR 1 PYLON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, ENGINE NR 1 PYLON PANEL 5401 IS DELAMINATED INNER SURFACE FWD END ENG NR 1 PYLON PANEL 5401 REPAIRED IAW SRM 51-40-20. 2L73 4F A3WE 20040827000062004082700006NM 2004 8 27 UPS04242980 120040805A7830 DUCT BOEING727 72722C 138400FNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, NR 3 ENGINE THRUST REVERSER, SUSPECT CRACK ON INNER SURFACE OF JET PIPE DUCT ON AFT SIDE OF LT LATCH BOX FRAME FASTENERS. REPAIR CARRIED OUT IAW AAAE EO 2004-073-001 R1 UPS ENG FILE 727-78-20015. 2L73 4F A3WE 20040827000122004082700012NM 2004 8 27 SWAA042437 120040821A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND BS 967 FLOORBEAM CORRODED AT RBL 28, WL 208. REPAIRED FLOORBEAM PER ERO. 2L72 4F RTA16WE 20040827000142004082700014NM 2004 8 27 SWAA042439 120040823A53116545809 FRAME BOEING737 7373H4 1384600NM L1 DOOR CUTOUT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303.9, WL 212, LBL 58. REPAIRED FRAME PER SRM & BOEING S/B. 2L72 4F RTA16WE 20040827000152004082700015NM 2004 8 27 SWAA042440 120040823A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FUSELAGE LT CREASE BEAM CORRODED AT BS 877. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040827000302004082700030 2004 8 27 SWAA042463 420040825A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES GIRT BAR FLOOR BRACKET FITTINGS CORRODED. REMOVED AND REPLACED FLOOR BRACKET FITTINGS PER MM. 2L72 4F RTA16WE 20040827000342004082700034NM 2004 8 27 SWAA042467 120040825A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, STRINGERS 8L & 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040827000412004082700041 2004 8 27 UPS04842991 420040820A2565 SLIDE DOUG DC8 DC873F 302199FWP CABIN DETERIORATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 GIRT BAR CABLE UNHOOKED FROM RAFT. UPON FURTHER INSPECTION FOUND SEVERAL AREAS OF DETERIORATION ON SLIDE. REMOVED AND REPLACED DOOR SLIDE IAW MM 25-60-01-2. 2L74 4F RT4A25 20040827000472004082700047SO 2004 8 27 CHQA000539 120040817A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11274 145344 OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT ASSY IAW EMB 145 AMM 33-50-07-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040827000482004082700048SO 2004 8 27 CHQA000537 120040820A27403621001007 PITCH CONTROL EMB 145 EMB145LR 3260212SO STAB CONTROL DEFECTIVE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11264 7685 7685 145221 DURING FLIGHT 3192 FROM SDF TO LGA WHILE BEING VECTORED TO THE ILS, THE AIRPLANE PITCHED UP 9 DEGREES UP. THE PILOTS RAN THE QRH, AND RE-ESTABLISHED BACK UP PITCH TRIM. THE ALTIDUDE GAIN WAS APPROXIMATELY 800 FEET AND ATC DID NOT COMMENT. THE POWER WAS REDUCED UNTIL PITCH CONTROL WAS REGAINED. AN EMERGENCY WAS NOT DECLARED. THE AIRCRAFT LANDED ON RUNWAY 22 WITH THE BACK UP PITCH TRIM ENGAGED. REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 145 AMM 27-40-01. OPS CHECK GOOD AT THIS TIME AND DATE. 2L72 4T RTT00011AT 20040827000492004082700049SO 2004 8 27 CHQA000540 120040814A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11269 145293 FLOOR LEVEL EMERGENCY EXIT LIGHT STRIPS NR 4 AND 7 ARE INOP DUE TO BROKEN WIRING. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY EXIT LIGHT STRIPS NR 4 AND 7 IAW EMB 145 AMM 33-50-12 AND OPS CHECKS GOOD. 2L72 4T RTT00011AT 20040827000522004082700052EA 2004 8 27 COMA0460477 120040820A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01940CA 7048 FLIGHT 5495 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040827000592004082700059SO 2004 8 27 SWIA200413710 120040818A2731 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO ELEVATOR MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07215SW 120281 WHEN TAXIING TO GATE, TRIM AURAL WARNING GOING OFF IN GREEN BAND. REMOVED AND REPLACED BOTH ELEVATOR TRIM PROXIMITY SENSORS IAW EMB 120 MM 27-32-05. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040827000682004082700068SO 2004 8 27 SWIA200413717 120040819A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07218SW 120287 OVERHEAD BIN ROW 9 EXIT ROW LIGHT INOPERATIVE. REPLACED SPLICE IN GROUND WIRE AT EXIT LIGHT ASSY AT ROW 9. OPERATIONAL CHECK OK PER MM 33-50-00. 2L72 4T RTA31SO 20040827000722004082700072 2004 8 27 WLDA200458 420040812A3417HG280D5 ADC DOUG DC10 DC1030 3023501WP COCKPIT INOPERATIVE A WRLAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 SO11351 46922 NGU/NAP AIR TURNBACK DUE TO AIRSPEED INDICATOR FAILED AFTER TAKEOFF, INDICATING 90 KTS, F/O'S INDICATED SAME AS STANDBY A/S LATER ON. SELECT FLAP LIMIT AND SELECT ELEV FEEL MANUAL LIGHTS CAME ON. FOLLOWED PROCEDURES & RETURNED TO KNGU. REMOVED AND REPLACED AIR DATA COMPUTER. PERFORMED PITOT STATIC TEST FOUND NORMAL. 2L73 4F A22WE 20040830000012004083000001NM 2004 8 30 04FDEA02525 120040819A5711 SPAR DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT XORS 600 TO XORS 650 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR. 2L73 4F4 FRTA22WE E24NE 20040830000042004083000004 2004 8 30 SWIA200413725 420040814A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07562SW8452 8452 120336 FO'S AUTOPILOT KICKED OFF AT LEVEL OFF , 25,000 FT. REMOVED AND REPLACED AUTOPILOT COMPUTER IAW MM 22-10-02, OPERATIONAL CHECKED GOOD. 2L72 4T4 TRTA31SO E20NE 20040830000132004083000013EA 2004 8 30 COMA0460469 120040823A5320601R53410592 ANGLE CNDAIRCL600 CL6002B19 1900309EA LYC O540 IO540B1A5 41532EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01477CA5851 7670 INTERCOSTAL ANGLE AT FS 484.00 RBL 36 IS CRACKED. PERFORMED A MAJOR REPAIR AT F.S. 484.00 RBL 36 BY CUTTING AWAY DAMAGED ATTACHMENT FLANGE, EDDY CURRENT AREA, FABED NEW ANGLE AND INSTALLED IAW R.E.O 601R-53-059 REV A. 2L72 4F3 ORTA21EA 1E4 20040830000162004083000016 2004 8 30 2004UALA00771 420040812A2565 INDICATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE L3 DOOR SLIDE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29546UA 25367 DOOR 3L SLIDE INDICATOR WILL NOT ILLUMINATE. REPLACED LAMP. 2L72 4F4 FRTA2NM E17NE 20040830000322004083000032EU 2004 8 30 I262004F00000 120040709A2750 SWITCH ISRAEL1124 1124 4500102EU TE FLAP STUCK E I26AO OTHER O OTHER NRNOT REPORTED 1 NE05140VJ 435 FLAPS STUCK IN 12 DEGREE POSITION. FOUND THE NR 2 SWITCH STUCK IN CLOSED POSITION. REPLACED SLIDER ASSY. OPS CHECK GOOD. 2M72 4F A2SW 20040830000362004083000036CE 2004 8 30 JEM2004F00009 120040828A551045A21085004 BRACKET BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01400FT RK101 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER ROLLER BRACKET ASSY AREA, IT WAS DISCOVERED THE RIB AS WELL AS THE TWO SUPPORTING BRACKETS BEHIND THE RIB WHERE CRACKED. THE INSPECTION WAS ACCOMPLISHED BY USING A BORESCOPE AND INSERTING INTO THE HORIZONTAL STABILIZER DRAIN HOLES NEAR THE SIDE ROLLER SUPPORT BRACKETS. THE RIB CRACK WAS NOT FOUND UNTIL THE ROLLER BRACKET WAS COMPLETELY REMOVED. 2H72 4F4 FRTA16SW E25EA 20040830000432004083000043NM 2004 8 30 AMTA200400361 120040328A2730162700100 COMPUTER BOEING737 73783N 13844HINM ELEVATOR MALFUNCTIONED A AMTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL11318TZ 28247 ELEVATORY FEEL DIFFERENTIAL LIGHT ILLUMINATED. REMOVED AND REPLACED ELEVATOR FEEL COMPUTER IAW MM 27-31-37-4. COMPLIED WITH STEP 3G2 AND 3 MM 27-31-37-4 FEEL FORCE SYSTEM TEST AMM TASK 27-31-00-700-812. SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20040830000522004083000052WP 2004 8 30 CALA0400617 120040825A5730 SKIN DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716883 48073 INSPECTION FOUND A .5 INCH CRACK IN RT WING L/E SKIN AT STA XF 251 JUST FORWARD OF FUELING DOOR. THE SKIN WAS REPAIRED IAW SRM 57-06B, FIGURE 4. 2L72 4F4 F A6WE E9NE 20040830000682004083000068NM 2004 8 30 QXEA200400635 120040819A2611 WARNING LIGHT DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE SMOKE DETECTOR ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09355PH 500 THE SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY DURING THE APPROACH AND THEN AGAIN ON FLARE. MAINTENANCE INSPECTED THE AIRCRAFT AND SMOKE DETECTORS AND COULD NOT DUPLICATE THE WRITE-UP. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040830000722004083000072NM 2004 8 30 HNAA0400075 120040823A3234 SELECTOR PANEL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE MLG FAILED A HNAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA07940HA 156 NOSE WHEEL GEAR INDICATION WAS BLANK AFTER GEAR SELECTION WAS MADE. SMOKE CAME FROM NOSE WHEEL GREEN CAUTION LIGHT AREA. REMOVED AND REPLACED LANDING GEAR SELECTOR PANEL, OPS GOOD IAW 32-30-05 AND INPECTED FOR SECONDARY DAMAGE C/W NO DEFECTS NOTED. 2H72 4T4 TRTA13NM E20NE 20040830000812004083000081NM 2004 8 30 04FDEA02544 120040822A5313 LONGERON DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 48L SPLICE DOUBLER AT STA 5-113 TO STA 1541. REMOVED PER SRM 51-33-01 VOLUME II. THREE (3) EACH SPLICE DOUBLERS P/N A5A7124-1, A5A7124-2 AND A5A7125-501 FABRICATED PER DWG A5A7124 AND A5A7125; AND PART MARKED AS PER FEDEX GMM 7-0-1001. FABRICATED SPLICE DOUBLERS INSTALLED PER DWG A5A7124 AND A5A7125 AND SRM 51-33- 01 VOLUME II. 2L73 4F4 FRTA22WE E24NE 20040830000842004083000084EU 2004 8 30 DHL2004364014 120040820A3230 LANDING GEAR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE LEFT SLOW A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01364DH 141 LT MAIN GEAR TOOK 15 SECONDS LONGER THAN OTHER GEAR TO EXTEND,TO LOCK. 2L72 4F4 FRTA35EU E23EA 20040830000862004083000086 2004 8 30 63837 420040812A3418 VANE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE STALL WARNING DIRTY A AMWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07142ZV UE142 ON TAKEOFF ROLL AT V1,VR STALL WARNING HORN CAME ON AND SOUNDED CONTINUOUSLY AND DID NOT SHUT OFF. CREW ELECTED TO RETURN TO DEPARTURE. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. CLEANED STALL VANE, OPS CK NORMAL. 2L72 4T4 TRTA24CE E26NE 20040830000902004083000090EA 2004 8 30 COMA0460474 120040816A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01479CA 7675 CRACK FOUND TO FLANGE IN CABIN FLOOR LT SIDE INTERCOSTAL. C/W REO 601R-53-41-059. 2L72 4F4 FRTA21EA E15NE 20040830001122004083000112EU 2004 8 30 04FDEA02549 120040823A5330A5377868520200 PLATE AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25421FE 342 THE FWD CARGO COMPARTMENT FWD MANHOLE BETWEEN FR23 AND FR 24 ON RT SIDE BETWEEN STR RT 51 AND STR RT 49. THE EXISTING POCKETS REPAIRED WITH EXTERNAL DOUBLER AND NEW POCKETS FOUND CORROSION MORE THAN 50 PERCENT OF FITTING THICKNESS. ON LT SIDE OF MAN HOLE BETWEEN STR 55 AND STR 53RH 01 OFF POCKET ON INNER ROW RIVET FOUND CORROSION MR 50 PERCENT THICKNESS OF FITTING. SNRM: N00411, THE FOLLOWING CARGO COMPARTMENT FWD MANHOLE POCKETS FOUND, CORROSION AT LOCATIONS : (A) AFT OF FR23 ( RTSIDE FWD) 2 OFF POCKETS BETWEEN STR51RT AND STR 49 RT. (B) FWD OF FR 24( LTSIDE AFT ) 2 OFF POCKETS BETWEEN STR55 AND STR 53 RT.**** S/D COMING **** 2L72 4F4 FRTA35EU E3NE 20040830001202004083000120SW 2004 8 30 ALGA096827 120040807A6710406310406101 BUSHING BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL236 53357 FOUND RADIAL PLAY IN EXCESS OF LIMITS. REPLACED WITH NEW, BY O/H SHOP. 1G71 3U3 UO H2SW E1GL 20040830001272004083000127WP 2004 8 30 CALA0400609 120040820A5350 RELEASE CABLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE TAILCONE OUT OF RIG A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 THE TAILCONE PULL CHECK FROM THE INTERIOR RELEASE HANDLE, FAILED. THE CABLES WERE ADJUSTED IAW MM 53-53-00. 2L72 4F4 F A6WE E9NE 20040830001482004083000148NE 2004 8 30 DLM88040778 220040818A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 FAILED A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27986DL15072 53313 762074 INFLT SHUT DOWN DUE TO LOSS OF OIL QTY AND HIGH OIL TEMP. REPLACED ENGINE. 2L72 4F4 FRTA6WE E9NE 20040830001592004083000159NM 2004 8 30 QXEA200400596 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 TRACK NR 2 HAS CHAFES ON TOP FLANGE AT X 521.5. BLENDED LIGHT CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 1 INCH LONG BY .25 INCH WIDTH, .004 INCH DEPTH. HFEC INSP IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW 1400 RD 8/4-53-844, STEP 6. 2H72 4T4 TRTA13NM E00062EN 20040830001782004083000178WP 2004 8 30 04FDEA02324 120040730A5320SGA38571 ANGLE DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AFT LOWER CARGO, LOWER AFT CORNER OF DOOR CUT OUT, CLOSE OUT ANGLES CORRODED. REMOVED CORROSION IAW SRM 53-00-01 VOL I, FOUND TO BE OUT OF LIMITS. REMOVED ANGLES IAW SRM 51-31-01 VOL II PAGE 1. FABRICATED ANGLES IAW DAC DRG. AGA3881 AND AGA3857. LOCATED, DRILLED AND DEBURRED IAW SRM 51-31-01 VOL I PAGE 3. ALODINE AND PRIMED IAW MD 10- SRM 51-21-01 VOL II, PAGE 21. INSTALLED ANGLES IAW MD10 SRM 51-35-01 VOL II PAGE 1-3. REF N/R N00654. 2L73 4F4 FRTA22WE E23EA 20040830001802004083000180GL 2004 8 30 C2XA04BT089 220040815A726123054499 TUBE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A C2XAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW2716502 145166 ENROUTE, DIVERTED, CREW REPORTED, ENGINE NR 1 LOST OIL INFLIGHT. PERFORMED SHUTDOWN IAW QRH. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED PRESSURE OIL CONTROL TUBE TO ENGINE GEARBOX, OPS AND LEAK CHECKED GOOD REFERENCE MM NR 71-00-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040830001842004083000184NM 2004 8 30 ANCF200400018 120040716A3260 UPLOCK DOUG MD80 MD83 3023681NM MLG DOOR DIRTY W ANCFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO23583AN 53183 DURING CLIMB, WITH A SPEED OF 230 KTS, GEAR DOOR OPEN LIGHT CAME ON AND REMAINED ON FOR TEN MINUTES, THEN IT STARTED TO ILLUMINATE INTERMITTENTLY. THERE WAS NOT AN ABNORMAL CHECK. THEN DURING APPROACH WHEN LANDING GEAR WAS SELECT DOWN THE GEAR DOOR OPEN LIGHT TOOK MORE THAN ONE MINUTE AND THIRTY SECONDS TO GOES OFF. FLYBY THE CONTROL TOWER TO BE SURE THAT GEAR WAS DOWN AND THE DOORS WERE CLOSE. BITE ON PSEU WAS PERFORMED IAW AMM 32-60-04 PAGE 201. NO FAULT FOUND, TEST OK. LT AND RT MAIN LANDING GEAR DOOR UP LATCHES D1-25 AND D1-26 WERE CLEANED AND ADJUSTED. TEST WAS VERIFIED IAW AMM 32-60-05 PAGE 207. ALSO BOTH HYDRAULIC SYSTEMS WERE CHECKED FOR LEAKS AND FOUND NORMAL AND LEVEL CORRECT. 2L72 4F RT 20040830001872004083000187EU 2004 8 30 AWXA200400700 120040617A5347D5713014720200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON RT OB Y-1292 SEAT TRACK FR36-FR41. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT FR 36-4 IAW A320 SRM 51-42-11 PAGES 6,7,28 FIGURE 12. 2L72 4F RTA28NM 20040830001892004083000189EU 2004 8 30 AWXA200400702 120040617A5347D57130147200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON LT IB Y765 SEAT TRACK FR36-41. MAINTENANCE REMOVED AND REPLACED SEAT RACK SECTION ON LT SIDE IB OF Y765 IAW SRM 51-42-11 PAGES 6,7,39-41 FIGURES 12,18. 2L72 4F RTA28NM 20040830001982004083000198WP 2004 8 30 04FDEA02326 120040730A5751 COUNTERWEIGHT DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 RT WING TRAILING EDGE OB AILERON BALANCE WEIGHTS CORRODED AND 50 PERCENT OF PROTECTIVE PAINT IS MISSING. REMOVED AND REPLACED WEIGHT ASEMBLY IAW SB 57-119 AND CMM 57-51-02. REMOVED AND INSTALLED BUSHINGS IAW CMM 57-51-02, SB 57-119 AND EA 8-5750-77610. FLAP PEENED AND DYE PENETRANT INSPECT HOLES IAW EA 8-5750-77610. REF. N/R N00407 2L73 4F4 FRTA22WE E23EA 20040830001992004083000199WP 2004 8 30 04FDEA02327 120040730A7830 FAIRING DOUG MD10 MD1010F 3022112WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 NR 3 PYLON RT FAN REVERSER TOP CRACKED AND GOUGED AT STATION Y172. REPAIRED THRUST REVERSER FAIRING IAW EA 8-7830-77612. REMOVED AND INSTALLED SKIRT PANEL IAW SRM 51-35-01 VOL II. REF N/R N00555. 2L73 4F RTA22WE 20040830002032004083000203SO 2004 8 30 CHQA000511 120040629A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11274 145344 RT SIDE AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT SIDE, AFT EXTERNAL EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040830002072004083000207EU 2004 8 30 CX7A194J0441 120040722A26131734362450 DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT TAIL PIPE SATURATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03308CE 340B210 AFTER POWERING UP SYSTEMS DURING PREFLIGHT RT TAIL PIPE HOT CWP ILLUMINATED. 2L72 4T4 TRTA52EU E8NE 20040830002122004083000212SO 2004 8 30 CHQA000519 120040725A3350 LIGHT EMB 145 EMB145LR 3260212SO WRIGHTR3350 988TC18EA1 67038EA RT WING EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286 145443 RT OVER WING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE RT OVER WING EXIT LIGHT. OPS CHECK GOOD IAW EMB 145 MM 33-50-01. 2L72 4T4 RRTT00011ATE287 20040830002142004083000214NM 2004 8 30 QXEA200400630 120040813A2760 HINGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 RT IB SPOILER IB HINGE ARM IS CHAFING. BLENDED ABRASION DAMAGE AT RT IB SPOILER IAW SRM 51-41-00, PAGE 201-203. IB FUSELAGE ATTACH FITTING, REMOVED ONLY THE MINIMUM QUANTITY OF MATERIAL NECESSARY TO REMOVE DAMAGE. DID NOT DEEPEN DAMAGE. HFEC INSPECTION BLENDED AREA FOR CRACKS IAW -8/400 NDTM PART 6, 51-00-02. NO CRACKS NOTED. ETCHED ALODINED AND PRIMED IAW SRM 51-21-10 AND 51-25-10. APPLIED WHITE PAINT IAW SRM 51-25-05. 2H72 4T4 TRTA13NM E00062EN 20040831000142004083100014EU 2004 8 31 HAEA153 120040703A2130 CONTROLLER AMD FALC20FALCONE 2720305EU CABIN PRESSURE MALFUNCTIONED E HAEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW05285TW20797 285 AIRCRAFT DEPARTED ADS CLIMBING THROUGH 10,000 FT CABIN DID NOT PRESSURIZE. ALL SWITCHES CHECKED NORMAL. AIRCRAFT RETURNED TO ADS FOR MAINTENANCE. LANDING NORMAL. 2L72 4F A7EU 20040831000202004083100020NM 2004 8 31 2004UALA00668 120040714A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 MAIN CABIN STA 760-770, CREASE BEAM AT LBL60 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED AN EXTRUDED SECTION REPAIR. 2L72 4F4 FRTA2NM E17NE 20040831000522004083100052 2004 8 31 F3LA200400071 420040719A34603945128205 COMPUTER AIRBUSA318 A318111 3940019EU GE CFM56 CFM56* 13802NE FLT CONTROL INOPERATIVE A F3LAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03804FR 2482 2051 ON CLIMB OUT, FLIGHT CREW REPORTED ECAM: FLT CNT. FLT CTR 1 NR 2. RAN ECAM. RETURNED TO DEN WITHOUT INCIDENT AND LANDED OVERWEIGHT. TROUBLESHOT FLT CONT 1 AND 2 IAW TSM 27-93-00-810-949. REPLACED ELAC 1 IAW AMM 27-93-34-000-001. ELAC NR 1 OPS CHECKED NORMAL IAW AMM 27-93-00-710-001. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-11-991-016. CHECKED OKAY. 2L72 4F4 FRT E2GL 20040831000552004083100055EA 2004 8 31 SWIA200413667 120040808A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07442SW7612 7612 7609 AP PITCH TRIM, CAUTION MESSAGE IN FLIGHT. REMOVED AND REPLACED HSTA AND MCU IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040831000582004083100058WP 2004 8 31 IXXA0400098O 120040720A3220 SEAL DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE NLG DAMAGED A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW11823BX86410385 46064 DURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN THE NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT NOSE LANDING GEAR DOOR SEAL PARTIALLY HANGING OUT. THE DAMAGED SEAL WAS REMOVED. THE NGL AND DOORS WERE INSPECTED WITH NO DEFECTS NOTED AND INITIATED CARRY OVER ITEM NR 30084. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20040831000602004083100060SO 2004 8 31 SWIA200413670 120040809A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE LT IB FLAP MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07393SW9492 9492 120330 ON TAXI OUT, SELECTED FLAPS 15 DEGREES, THE LT IB FLAP WENT TO 45 DEGREES CAUSING AN ASYMMETRY. REPLACED LT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040831000612004083100061SO 2004 8 31 SWIA200413671 120040808A2121AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE CABIN FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07250YV9627 5048 120250 ON FIRST FLIGHT AFTER SAFETY CHECK, NOTICED A FAINT SMOKE ODOR. REPLACED LT GROUND COOLING FAN WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040831000652004083100065SO 2004 8 31 SWIA200413676 120040807A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO PWA PT6 PT6A41 52043EA TE FLAPS WORN A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07582SW 120350 AFTER TAKEOFF SELECTED FLAPS UP AND RECEIVED FLAP DISAGREEMENT. REMOVED AND REPLACED RT IB FLAP OB TRACK AND ALL ROLLERS ON RT IB FLAP IAW 27-50-02, OPERATIONAL CHECKS GOOD. 2L72 4T4 TRTA31SO E4EA 20040831000672004083100067EA 2004 8 31 SWIA200413609 120040716A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07917SW 7641 WITH RUDDER TRIM NOSE RT, WILL NOT RE-CENTER. REPLACED RUDDER/AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040831000682004083100068EA 2004 8 31 SWIA200413610 120040718A2741270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW7465 7465 7578 FLIGHT SPOILERS FAULT MESSAGE DISPLAYED ON ED-2. REMOVED AND REPLACED RIGHT HAND FLIGHT SPOILER NR 2 PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040831000702004083100070EA 2004 8 31 SWIA200413612 120040725A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT CONTAMINATED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07411SW 7067 FLOOR EMERGENCY LIGHTS BEHIND ROW 9 WILL NOT ILLUMINATE. CLEANED CONTAMINATED CONNECTION AT LAV. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040831000712004083100071WP 2004 8 31 ABXA040263 120040707A534056150401 FITTING DOUG DC8 DC863F 302198FWP PWA JT3D JT3D* 52039NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 FITTING CRACKED AT MOST FORWARD FASTENER HOLES. FABRICATED REPAIR PARTS IAW REA D853-49975MR. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW SRM 51-1-20B. 2L74 4F4 F 4A25 1E8 20040831000722004083100072WP 2004 8 31 ABXA040264 120040712A53135750198 LONGERON DOUG DC8 DC863 302198AWP PWA JT3D JT3D* 52039NE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 LT MAIN LANDING GEAR WHEEL WELL LONGERON 24 CRACKED ON LOWER FLANGE AT BOTTLE BOLT CAVITY. REPAIRED AREA IAW REA D853-49163MR. 2L74 4F4 F 4A25 1E8 20040831000732004083100073NM 2004 8 31 QXEA200400567 120040725A32345352011 SELECTOR PANEL DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 FAILED A QXEAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 NM09359PH192511759 514 THE CREW ABORTED THE APPROACH WHEN AFTER SELECTING THE GEAR DOWN, THE RT GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE. THE CREW COMPLIED WITH THE LANDING GEAR INDICATION MALFUNCTION CHECKLIST. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LANDING GEAR SELECTOR PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040901000012004090100001SO 2004 9 1 SWIA200413684 120040621A5420 ANGLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07270YV 120270 LT MAIN LANDING GEAR BAY, FORWARD BULKHEAD, LOWER STIFFENER ANGLE HAS A CRACK AT IB. RIVET. ( ITEM FOUND AT C-CHECK INSPECTION.) REPLACED ANGLE WITH THE MADE REPAIR PART IAW SRM 51-30-01, 51-40-00, 51-40-02, 51-40-05. REFERENCE SRM 54-10-02 FIG. 03 ITEM 230. 2L72 4T4 TRTA31SO E20NE 20040901000032004090100003NM 2004 9 1 AWXA200400735 120040705A2560P4010021 BATTERY BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28157AW 23779 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040901000062004090100006NM 2004 9 1 AWXA200400737 120040627A27502061141 SYNCRONIZER BOEING737 73733A 1384673NM GE CFM56 CFM56* 13802NE TE FLAPS FAULTY A AWXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP28173AW127322123 23632 FLIGHT CONTROL, ON APPROACH, ENROUTE FLAPS FAILED TO EXTEND BEYOND FLAPS 5, USED ALTERNATE FLAP PROCEDURES TO EXTEND FLAPS TO 15. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR IAW T/C 1B27001, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF FLAP POSITION INDICATOR S/N 1594 CONFIRMED REASON FOR REMOVAL FINDING THE RT SYNCHRO INOPERATIVE, AND THE LT SYNCHRO SLUGGISH. REPLACED RT SYNCHRO, AND CLEANED AND LUBRICATED THE LT SYNCHRO BEARINGS IAW CMM 27-50-03. 2L72 4F4 FRTA16WE E2GL 20040901000072004090100007EU 2004 9 1 AWXA200400738 120040612A5320D5348002034300 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK A 2 INCHES CRACK WAS FOUND ON RT AFT SHEAR PLATE OB OF Y1292 RT, AFT OF FR 68. MAINTENANCE REMOVED CRACKED SHEAR PLATE FROM FR 66 TO FR 68+10, Y1292; FABRICATED A NEW REPLACEMENT SHEAR PLATE IAW DWG 18D53480020; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8 & 12. 2L72 4F RTA28NM 20040901000092004090100009EU 2004 9 1 AWXA200400740 120040616A5753 SKIN AIRBUS320 A320231 3930325EU LT TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 1062 082 DURING C-04 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF LT IB FLAP AT IB END. MAINTENANCE CUTOUT DEBONDED AREA ON LOWER SURFACE OF LT IB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW E.R. 26-5752-04178-ES3. 2L72 4F RTA28NM 20040901000102004090100010EU 2004 9 1 AWXA200400741 120040616A5753 SKIN AIRBUS320 A320231 3930325EU TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK A DEBONDED AREA WAS FOUND AT REPAIR ON LOWER SURFACE OF LT OB FLAP AFT OF NR 2 SPOILER ACTUATOR. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF LT OB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW A320 SRM 57-53-00, FIG. 211. 2L72 4F RTA28NM 20040901000132004090100013NM 2004 9 1 AWXA200400744 120040628A5321D5367175301900 FLOOR PANEL AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK FOUND FLOOR PANEL 262BG MISSING AN INSERT WITH DELAMINATION TO BOTTOM OF LAMINATE. MAINTENANCE REPLACED INSERT AND PERFORMED BOND REPAIR TO BOTTOM LAMINATE OF FLOOR PANEL 262BG IAW SRM 53-02-00, FIG. 201. 2L72 4F4 FRTA28NM E311NE 20040901000142004090100014WP 2004 9 1 UPS04842868 120040704A53104654281 BRACKET DOUG DC8 DC871F 302199DWP PWA JT3D JT3D* 52039NE C2 DOOR GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C-3, B-PIT DOOR LINK HINGES ARE GOUGED/ WORN PORTION ON AIRFRAME (NOT DOOR). REMOVED 2 EACH EXISTING C2 DOOR LINK HINGE FITTINGS. RECEIVED NEW FITTING 2 EACH PN 4654281. LOCATED AND DRILLED TRANSFER HOLES FOR NEW HINGE FITTINGS IAW SRM 51-1-24. INSTALLED NEW DOOR LINK HINGE 2 EACH FIT TINGS IAW DC8 SRM 51-1-20D. 2L74 4F4 FRT4A25 1E8 20040901000152004090100015SW 2004 9 1 AC2A095337 120040603A3150430375002109 DISPLAY BELL 430 430 1182150SW ALLSN 250C 250C* GL EFIS FAULTY B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 DISPLAY IS UNREADABLE. REPLACED EFIS TUBE. 1G72 3U3 URTH9SW E4CE 20040901000162004090100016SW 2004 9 1 AC2A095338 120040528A7920206070180001 TUBE BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE OIL CORRODED B AC2AK NONE O OTHER ININSP/MAINT 1 SO0721460 4075 PART IS CORRODED. FOUND MANY CORROSION SPOTS ON TUBE WHEN REMOVED FROM PACKAGE FOR INSTALLATION. NEW PART. RETURNING TO MFG FOR CREDIT. 1G71 3U3 U H2SW E4CE 20040901000172004090100017SW 2004 9 1 AC2A095339 120040528A3110206070747001 TUBE BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL INSTRUMENT PANELCORRODED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO0721460 4075 PART IS CORRODED. FOUND CORROSION ON LINE DURING PRE-ASSEMBLE INSPECTION FROM STOCK ROOM. NEW PART. RETURNING TO MFG FOR CREDIT. 1G71 3U3 U H2SW E4CE 20040901000192004090100019GL 2004 9 1 YTRR095302 220040610A73202549170 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE MALFUNCTIONED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03239RA126 4039 GOVERNOR CANNOT BE ADJUSTED ABOVE 97 PERCENT N2. 1G71 3U3 U H2SW E4CE 20040901000202004090100020NM 2004 9 1 P5CA0401126 120040617A5753 SKIN BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE LT IB FORE FLAP ERODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LT WING IB FORE FLAP UPPER TRAILING EDGE WBL235 EROSION MIDDLE SECTION. REMOVED DAMAGE, APPLIED FIBERGLASS OVERLAY IAW SRM 51-40-15, APPLIED ANTISTATIC TO REPAIR IAW SRM 51-40-15, PAINTED IAW SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040901000222004090100022CE 2004 9 1 63455 120040729A3260H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG FAILED A AMWAO OTHER N FALSE WARNING CLCLIMB 1 CE07176YV UE176 AFTER TAKEOFF WHEN GEAR WAS RETRACTED THE LANDING GEAR IN-TRANSIT LIGHT REMAINED ILLUMINATED. CREW CONTACTED DISPATCH AND MAINTENANCE CONTROL. CREW WAS TOLD TO DIVERT. AIRCRAFT THEN DIVERTED, LANDED WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED RT UPLOCK SWITCH. OPS CK NORMAL. P/N H11-1541. 2L72 4T3 TRTA24CE E2NE 20040901000302004090100030EA 2004 9 1 SWIA200413681 120040808A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07597SW 7293 AFTER STARTUP A SPOILERONS FAULT MESSAGE DISPLAYED. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040901000312004090100031GL 2004 9 1 CHQA000520 220040724A7261 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE LEAKING A CHQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL11279SK 145379 CREW REPORTS ON CLIMB OUT AT HIGH POWER THEY EXPERIENCED A BURNING ODOR IN THE AIRCRAFT. THE POWER WAS DECREASED AND THE ODOR DISSIPATED. AS POWER WAS INCREASED THE BURNING ODOR CAME BACK. RAN BOTH ENGINES AT 98 PERCENT FOR 5 MINUTES AND AT GROUND IDLE FOR 3 MINUTES. PERFORMED THE ENGINE RUNS THREE TIMES WITH BOTH PACKS RUNNING AND THE WINDSHIELD HEAT ON. ALSO RAN THE APU. COULD NOT DUPLICATE THE BURNING ODOR. SD CREW REPORTS THEY ARE RETURNING TO THE GATE DUE TO A BURNING ODOR IN THE CABIN. OIL WAS FOUND TO BE LEAKING FROM THE NR 0 CARBON SEAL. REMOVED AND REPLACED NR 0 CARBON SEAL. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040901000322004090100032NM 2004 9 1 0401175534 120040617A5315 FLOORBEAM BOEING757 757251 1384970NM PWA 2037 PW2037 NE FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01534US 24265 DURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 365 RBL 25. REPAIRED IAW EA 55-198961. 2L72 4F4 FRTA2NM E17NE 20040901000332004090100033NE 2004 9 1 P5CA0401128 220040726A7261M832481261 PACKING BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 4 ENGINE LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP23921FT 21575 689166 NR 4 ENGINE IN OIL QTY DROPPED FROM 10.5 GAL BEFORE START TO 8.5 GAL AT IDLE. ON APPROACH INDICATION WENT TO ZERO WITH PRESSURE FLUXUATION B/W 40 AND 25 PSI. REMOVED CSD FOR OIL LEAK, INSTALLED CSD WITH NEW O-RING, OPS CHECK OK, LEAK CHECK OK, OIL PRESSURE NORMAL, OK FOR SERVICE IAW MM 24-11-01. 2L74 4F4 F A20WE E3NE 20040901000352004090100035CE 2004 9 1 ALG2004F00041 120040622A5610 WINDOW CESSNASTC STC206C 1182107CE ALLSN 250C 250C30P 03013GL COCKPIT DEPARTED E ALGAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SW03194H 45660 CAE895269 DURING FLIGHT AND POST FLIGHT, APPROX 3 MILES OFF THE BEACH, 14 MILES FROM BASE, PILOT ATTEMPTED TO CLOSE WINDOW AND PILOT SLIDING WINDOW POPPED OUT OF TRACK AND DEPARTED THE AIRCRAFT. UPON LANDING AT BASE DURING POST FLIGHT, PILOT DISCOVERED DAMAGE TO ONE OF THE TAIL ROTOR BLADES AND IMMEDIATELY TOLD MAINTENANCE AND LEAD PILOT. MAINTENANCE FOUND ONE TAIL ROTOR BLADE DAMAGED, REMOVED AND REPLACED MAIN INPUT SHAFT, FREE WHEELING UNIT, NR 1 THRU 8 TAIL ROTOR DRIVE SHAFTS, TAIL ROTOR GEAR BOX AND TAIL ROTOR HUB AND BLADES DUE TO SUDDEN STOPPAGE. 1H71 3O3 UNTA4CE E1GL 20040901000362004090100036 2004 9 1 HE66096544 420040708A3416C1952PC08 COMPUTER UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE ALTIMETER UNRELIABLE E HEEAO OTHER S AFFECT SYSTEMS CRCRUISE 1 SW03135CR1528 0164 COMPUTER CAUSING THE TRANSPONDER TO REPORT INACCURATE INFORMATION TO FLIGHT SERVICES. 1G72 3U3 U H88EU E34NE 20040901000372004090100037EU 2004 9 1 HE66096545 120040716A79316607190A PRESSURE SWITCH BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL OIL PRESSURE UNSERVICEABLE B HEEAO OTHER P NO WARNING INDICATION CRCRUISE 1 SW03202LF 2014 CAE280056 PRESSURE SWITCH FAILED AND REPLACED. 1G72 3U3 U H3AU E1GL 20040901000382004090100038EU 2004 9 1 HE66096552 120040721A251010570181 SEAT BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL COCKPIT CRUSHED B HEEAO OTHER O OTHER CRCRUISE 1 SW03202LF 2014 CRUSHABLE SEATS WERE CRUSHED. 1G72 3U3 U H3AU E1GL 20040901000392004090100039EU 2004 9 1 HE66096553 120040729A251010570213 SEAT BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL COCKPIT TORN E HEEAO OTHER O OTHER CRCRUISE 1 SW03202LF 2014 SEAT TORN, CUSHION HAS NO SUPPORT. 1G72 3U3 U H3AU E1GL 20040901000402004090100040NM 2004 9 1 04FDEA02456 120040812A5314 KEELBEAM BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A. 2L73 4F4 FRTA3WE E2EA 20040901000412004090100041NM 2004 9 1 HNAA0400062 120040707A532085310109 ANGLE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07933HA 134 DURING C CHECK, FOUND CORROSION OF AFT CAP ANGLE OF THE FPB AT STR 31 STARBOARD AND STR 31 PORT. REPAIRED IAW EO8-53-04-0423 BY PERFORMING ANGLE SPLICE IAW INTENT OF PREVIOUSLY APPROVED RD8-53-1395. NOTE THAT THE 85310026 SKIN IS CUT FOR ACCESS AND IS SPLICED BACK IN. 2H72 4T4 TRTA13NM E20NE 20040901000422004090100042NM 2004 9 1 UIEA200400122 120040712A3610777738561973961 VALVE BOEING747 747228F 1384895NM GE CF6 CF650* 30018NE NR 4 ENGINE ERRATIC A UIEAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 EA15536MC 21576 517879 NR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGING. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE DEACTIVATED, CLOSE AND PERFORMED ENGINE RUN UP, CHECK NORMAL, ENGINE RUN BY FLT CREW AND NR 4 ENGINE INSPECTED OK IAW MM 72-00-00, ITEM DEFFERED TO MEL 36-1. CONF NR M04-163. DMI M04-163 IS CLOSED 7/12/04 AT ORD. 2L74 4F4 F A20WE E23EA 20040901000462004090100046NM 2004 9 1 DHL2004762001 120040729A2782 SEAL BOEING727 7272B7 138407LNM PWA JT8 JT8D17 52049NE LE FLAP ACTUATORFAILED A DHLAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO01762AT 22162 LOSS OF ALL A-SYSTEM HYDRAULIC FLUID DURING FLAP EXTENSION 0 DEGREES TO 2 DEGREES. ACCOPLISHED CHECK LIST LANDED NORMALLY. RII OB SEAL BLOWN NR 2 LE FLAP ACTUATOR. REMOVED AND REPLACED NR 2 LE FLAP ACTUATOR IAW MM CH 27-81-22. OPS CHECK AND LEAK CHECK GOOD. 2L73 4F4 F A3WE E2EA 20040901000472004090100047WP 2004 9 1 ABXA040243 120040703A3260 WARNING LIGHT DOUG DC9 DC931 3022065WP PWA JT8 JT8D* NE MLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23938AX 47009 RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKE OFF. LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES FOLLOWING RECYCLING OF GEAR. UNABLE TO DUPLICATE. INSPECTED UPLOCK AND DOWNLOCK LIMIT SWITCHES AND VISIBLE WIRING IAW WIRING MANUAL. OPERATIONAL CHECK GOOD ON GEAR SWING. NO DEFECTS NOTED. 2L72 4F4 F A6WE E2EA 20040901000492004090100049 2004 9 1 380WL0001 420040820A2230756SUE44 COMPUTER BOEING737 7373G7 1384595NM GE CFM56 CFM56* 13802NE AUTOTHROTTLE MALFUNCTIONED A PIDAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO05380WL 23218 AUTO THROTTLE DOES NOT ACHIEVE REQUESTED TAKE OFF THRUST AND DISENGAGES DURING ALL PHASES OF FLIGHT. REPLACED AUTO THROTTLE COMPUTER IAW MM 22-31-10. TEST NORMAL. 2L72 4F4 FRTA16WE E2GL 20040901000502004090100050WP 2004 9 1 UPS04842869 120040702A53105645357 DOOR FRAME DOUG DC8 DC871F 302199DWP PWA JT3D JT3D* 52039NE CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3 B- PIT DOOR FRAME AFT SIDE CRACKED DOT NR Y52Y. MAT ID 2024-0 .071 PO 4255761 IAW SRM 52-2-0 AND 52-4-1. RECEIVED MATERIAL USED FOR REPAIR DOUBLER FROM HEAT TREAT. HEAT TREATED FROM 2024-T4 IAW TPS 1003 REV A. FABRICATED REPAIR DOUBLER IAW SRM 52-2-0. ALODINED IAW SRM 51-1-8. PRIMED IAW SRM 51-1-8. INSTALLED REPAIR DOUBLE R IAW SRM 51-1-21. 2L74 4F4 FRT4A25 1E8 20040901000532004090100053WP 2004 9 1 UPS04842877 120040702A53212772058 FLOORBOARD DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, STA 235 RBL 8 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBOARD. LOCATED NEW FLOORBOARD AND SPLICE PLATES. ALODINED AND PRIMED. INSTALLED FLOORBOARDS. ALL IAW SRM 51-3-0, 51-3-1, 51-1-8, AND 51-2-0. 2L74 4F4 FRT4A25 1E8 20040901000542004090100054WP 2004 9 1 UPS04842878 120040702A53472772660 SEAT TRACK DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, STA 1580 RBL 18 SEAT TRACK LOBES GOUGED AND OBLONGED. BLENDED OUT DAMAGED LOBES AND FOUND OUT OF LIMITS. REMOVED 4 HOLES SEAT TRACK PLUG P/N DC8-53B-007-002 PO NR SP0906208 AND INSTALLED IAW EO NR 5340-7779-B. ALL IAW SRM 53-2-0, 53-2-3, AND 51-3-0. 2L74 4F4 FRT4A25 1E8 20040901000552004090100055WP 2004 9 1 UPS04842879 120040702A53472772660 SEAT TRACK DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, SEAT TRACK (D) HAS WORN SCALLOPS AND LUGS BETWEEN FS 1560-1580 DOT NR D 973. BLENDED SEAT TRACK LUGS AND SCALLOPS, FOUND OUT OF LIMITS. OPEN FLOORBOARDS FROM FS 1495 TO 1690 LBL 16 TO LBL 32 IAW DC8 SRM 51-3-0 TO FOM, REMOVED SEAT TRACK AND EXISTING REPAIR SPLICES @ FS 1550-1590 LBL 24. LOCATED, DRILLED, AND DEBURRED SEAT TRACK. ALODINED AND PRIMED AND INSTALLED SEAT TRACK AND SPLICES. IAW SRM 53-2-0,53-7-1,51-2-0,53-2-3. 2L74 4F4 FRT4A25 1E8 20040901000572004090100057WP 2004 9 1 UPS04842881 120040701A5313564932743 LONGERON DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, FUSELAGE INTERIOR L 17 RT CRACKED FROM FS 1770 TO FS 1774. REMOVED L17R AT STA 1766 IAW SRM 51-1-20D. RECIEVED NEW LONGERON PN 5 649327-43. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED LONGERON IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F4 FRT4A25 1E8 20040901000582004090100058NM 2004 9 1 UPS04242999 120040802A575165192596 HINGE BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU LT OB AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, LT OB AILERON OB HINGE FITTING ON AIRCRAFT HAS A SUSPECT CRACK. NDT CARRIED OUT AND CRACK CONFIRMED. LT OB AILERON REMOVED IAW 27-10 -14. OB HINGE REMOVED IAW SRM 51-30-2. NEW HINGE INSTALLED IAW SRM 51-30-2.OB AILERON INSTALLED MM 27-10-14. 2L73 4F4 F A3WE E25NE 20040901000592004090100059EU 2004 9 1 DHL2004364012 120040710A32603115 BULB AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE MLG INDICATOR INOPERATIVE A DHLAO OTHER P NO WARNING INDICATION CLCLIMB 1 SO01364DH 141 NOSE GEAR INDICATOR ON PILOT'S LANDING GEAR PANEL DID NOT ILLUMINATE GREEN WHEN GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED THREE GREEN ON S/O PANEL. RELAMPED LANDING GEAR INDICATOR (P/N 3115) IAW M/M 33-13-00, OPS CHECKED GOOD. 2L72 4F4 FRTA35EU E23EA 20040901000602004090100060WP 2004 9 1 MWEA040133 120040810A534059524211 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 CORROSION AT G1 FORWARD ATTACH POINT JUST AFT OF POTABLE WATER SUPPLY FITTINGS AT FRAME STATION 200. FABRICATED AND INSTALLED FITTING. 2L72 4F4 F A6WE E2EA 20040901000612004090100061WP 2004 9 1 MWEA040134 120040810A532099365343 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 SUB FLOOR AT FRAME STATION 200 JUST AFT OF RT AFT GIRT BAR ATTACH FITTING, CORRODED. FABRICATED AND INSTALLED WEB. 2L72 4F4 F A6WE E2EA 20040901000632004090100063NM 2004 9 1 04FDEA02457 120040812A5314 KEELBEAM BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. 2L73 4F4 FRTA3WE E2EA 20040901000642004090100064NM 2004 9 1 04FDEA02459 120040812A5314 KEELBEAM BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LIMITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013. 2L73 4F4 FRTA3WE E2EA 20040901000652004090100065NM 2004 9 1 04FDEA02461 120040812A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 53-10-3 2L73 4F4 FRTA3WE E2EA 20040901000662004090100066NM 2004 9 1 04FDEA02462 120040812A2910BACH8A08NN0360T HOSE BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25262FE 21624 ON GEAR RETRACTION, HYD SYSTEM A QUANTITY WENT TO ZERO. NUMEROUS SAFETY WIRES BROKEN IAW EMERG PROC. BOTH A PUMPS OFF IMMEDIATELY, HYD FLUID SHUTOFFS CLOSED 5 MINUTES LATER, NR 1 AND NR 2 ENGINES SHUT DOWN APPROX 45 MINUTES AFTER THAT. FOUND LEAKING RT GEAR ACTUATOR RETURN LINE, RUPTURED. REPLACED BOTH PRESSURE AND RETURN LINES ACTUATOR AND OPS CHECKED IAW MM32-32-002-4. IAW MM 29-11-00-1TROUBLE SHOOTING SUPPLY SHUTOFF FOR LONGER THAN 5 MINUTES, CHECKED AND REPLACED A-SYSTEM CASE DRAIN AND PRESSURE FILTERS. NO PROBLEMS FOUND. SERVICED HYDRAULIC SYSTEM AND RAN ENGINES AND CYCLED ALL FLIGHT CONTROLS AND FLAPS TO BLEED ALL AIR FROM SYSTEM. OK FOR SERVICE. 2L73 4F4 FRTA3WE E2EA 20040901000692004090100069NM 2004 9 1 2004UALA00705 120040731A7830 DUCT BOEING757 757222 1384956NM PWA 2037 PW2037 NE THRUST REVERSER LEAKING A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29511UA 24799 RETURN TO FIELD DUE TO SMOKE IN THE FLIGHT DECK. FOUND A LEAKAGE ON THE BLEED DUCT CLAMP OF THE NR 1 ENGINE INBOARD REVERSER HOLD OPEN ACTUATOR. THE ACTUATOR WAS REPLACED. A PACK BURN-OUT PROCEDURE VERIFIED PROPER FUNCTIONING OF ACTUATOR. 2L72 4F4 FRTA2NM E17NE 20040901000712004090100071NE 2004 9 1 2004F00231 220040718A7321JFC16010823700 FUEL CONTROL CESSNA560 560XL 2076702CE PWA 545 PW545A NE RT ENGINE SHEARED E A UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL2521MA 1375 5605089 DB0182 AT 16,000 MSL CRUISE, RT ENGINE FLAMED OUT. INSPECTION FOUND ENGINE DRIVEN FUEL PUMP SHEARED. 2L72 4F4 FRTA22CE E00059EN 20040901000772004090100077NM 2004 9 1 DHL2004745540 120040803A5260 AIRSTAIR BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, REMOVE AFT AIRSTAIR INFLIGHT LOCK, FABRICATE AND INSTALL DOUBLER IAW SRM. REMOVED AFT AIRSTAIR INFLIGHT LOCK IAW SRM 51-30-2 FABRICATED DOUBLER FROM 2024-T3 .063 SIZE 9 .25 INCH X 4.75 INCH PO NR 900790 IAW SRM 53-30-3 TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2 INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 AND FCD52600001-001-B. 2L73 4F4 F A3WE E2EA 20040901000792004090100079NE 2004 9 1 HEEA096018 220040622A75325044T08P10 BLEED VALVE BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE NR 2 ENGINE MALFUNCTIONED B HEEAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW0359806 28140 WHILE HOVERING FOR TAKEOFF,NR 2 MGT STARTING RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH. 2G72 4U4 U H10SW E8NE 20040901000802004090100080EA 2004 9 1 HEEA096019 220040621A7321324473514 FUEL CONTROL BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA NR 1 ENGINE MALFUNCTIONED B HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SO031202T 33112 IN CRUISE FLIGHT, THE NR 1 ENGINE OUT LIGHT CAME ON, TORQUES SPLIT WITH NR 1 ENGINE LOW, RPM LIGHT CAME ON, LOW AUDIO CAME ON, CYCLIC CENTERING LIGHT CAME ON, AND NR 1 ENGINE N1 WENT TO 40 PERCENT. FOLLOWED CHECK LIST FOR LOW SIDE FUEL CONTROL FAILURE AND LANDED. MAINTENANCE REPLACED THE NR 1 ENGINE AUTOMATIC FUEL CONTROL UNIT. 1G72 4U4 U H4SW E22EA 20040901000812004090100081NE 2004 9 1 HEEA096020 120040614A7797 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL NR 2 BEEP MOTOR BURNED E HEEAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW0322342 760096 NR 2 ENGINE HAD RUNAWAY BEEP CAUSING A 30 PERCENT TORQUE SPLIT. RETARDED NR 2 THROTTLE TO 38 PERCENT TORQUE AND LANDED. MAINTENANCE FOUND THE WIRES FOR THE NR 2 NS BEEP MOTOR RUNNING BETWEEN CONNECTORS P314 AND P104 TO BE BURNED AND CHAFED AT FUSELAGE STATION 230. REPLACED WIRES. 1G72 3U3 U H1NE E1GL 20040901000852004090100085NM 2004 9 1 SWAA042516 120040829A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 463 TO BS 466, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA SRM. 2L72 4F RTA16WE 20040901000872004090100087 2004 9 1 SWAA042536 420040830A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901000882004090100088 2004 9 1 SWAA042537 420040830A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29758SW 27873 L2 DOOR EVAC SLIDE LOOSE. SECURED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901000902004090100090NM 2004 9 1 SWAA042539 120040830A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 727B, STR 25R, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20040830000302004083000030CE 2004 8 30 DXTA200400370 120040821A3222 STRUT CESSNA560 560XL 2076702CE PWA 545 PW545A NE NLG DAMAGED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07635QS 5605358 ON GEAR RETRACTION RED UNLOCK LIGHT ON GEAR. EXTENDED GEAR, 3 GREENS, NO RED LANDED UNEVENTFULLY. TROUBLESHOT LANDING GEAR SYSTEM. FOUND NLG STRUT NOT EXTENDING COMPLETELY, CAUSING UPLOCK LOCK TO CONTACT UPLOCK ROLLERS NOT ALLOWING GEAR TO RETRACT. DISASSEMBLED NOSE GEAR STRUT AND REBUILT STRUT IAW COMPONENT MM 32-20-01. REASSEMBLED NLG AS REQUIRED. SERVICED NOSE STRUT IAW MM 12-14-00. PERFORMED OP'S CHECK OF LANDING GEAR SYSTEM. OPS CHECK GOOD. 2L72 4F4 FRTA22CE E00059EN 20040830000442004083000044NM 2004 8 30 HNAA0400115 120040820A2910 O-RING DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE HYD SYSTEM LEAKING A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA07980HA 376 FLIGHT NR 3818 REPORTED TOTAL LOSS OF NR 2 HYDRAULIC SYSTEM CONTENTS. PRESSURE LOSS WAS FOR APPROX. 7 MINUTES, WITH NR 2 ENGINE RUNNING. MAINTENANCE FOUND UNION ON THE ASSOCIATED HYDRAULIC PRESSURE MANIFOLD TO HAVE A BAD O-RING. O-RING WAS REPLACED AND THE SYSTEM INSPECTED IAW CHECK 5-50-33. SYSTEM WAS SERVICED AND BLED AS NEEDED, AND OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. 2H72 4T4 TRTA13NM E20NE 20040830000642004083000064 2004 8 30 C1HA200478004 420040822A2565146110016 SLIDE BOEING727 727225 1384077NM PWA JT8 JT8D9 52048NE L2 DOOR TORN A C1HAK NONE O OTHER ININSP/MAINT 1 GL15678MG 22555 L-2 DOOR SLIDE INADVERTANTLY DEPLOYED DUE TO DOOR BEING ARMED. SLIDE INFLATED CORRECTLY AN THEN DEFLATED DUE TO A TEAR IN THE SLIDE. REMOVED AND REPLACED L-2 EVAC SLIDE IAW MM 25.60.15. 2L73 4F4 F A3WE E2EA 20040830000772004083000077EU 2004 8 30 04FDEA02540 120040821A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25663FE 766 N00509 MDCC SIDE TRACK AT FR 37 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX. 1 INCH. REMOVED AND REPLACED SIDE TRACK ADAPTER TRACK IAW A300 SRM 51-40-20. 2L72 4F4 FRTA35EU E13NE 20040830000792004083000079EU 2004 8 30 04FDEA02542 120040821A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25663FE 766 N00468 MAIN CABIN SEAT TRACK CORRODED FROM FR47 TO 50, TRACK 3R. REPAIRED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. 2L72 4F4 FRTA35EU E13NE 20040830000962004083000096CE 2004 8 30 2004F00259 120040117A5720101000111 WASHER BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA RT WING OUT OF POSITION A I5WAK NONE O OTHER ININSP/MAINT 1 SO05911SF BB1659 RT WING CENTER SECTION MAIN SPAR UPPER FITTING HAS A DEPRESSION, DUE TO THE WASHER NOT PROPERLY IN PLACE. DEPRESSION BLENDED TO A SMOOTH PROFILE WITH A .125 FINISH, ALL WORK DONE IAW FIELD REPAIR FR-KA-01188, REV A. (M) 1L72 4T3 T A24CE E2NE 20040830000972004083000097SO 2004 8 30 CHQA000532 120040809A5610 WINDSHIELD EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT OVERHEATED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL11278SK 145370 PILOT SMELLED SOMETHING, SAW SMOKE FROM UNDER GLARESHIELD FOR ABOUT 15 SECONDS. SMOKE AND ODOR DISSIPATED WITHIN 10-15 SECONDS. REMOVED GLARESHIELD, INSP WIRING AT WINDSHIELD, AREA UNDER GLARESHIELD AND CHECKED COOLING, DISPLAY COOLING FANS. NO PROBLEMS WERE FOUND. DURING TAXI IN ON REPO FLIGHT, WINDSHIELD BEGAN TO FOG UP. WINDSHIELD HEAT WAS TURNED OFF FOR 15 SECONDS, UPON TURNING IT BACK ON SOME BURNING PLASTIC OR RUBBER ODOR WAS PRESENT. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW AMM 56-10-01. PERFORMED OPERATIONAL CHECK OF WINDSHIELD HEAT. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040830001022004083000102NM 2004 8 30 UPS04M42945 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C LT HORIZ STAB NR 02 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND SIDEWALL SURFACE. CORROSION AT S/W SURFACE BLEND TO 0.100 INCH DEEP FOUND OUT OF LIMIT IAW E O MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409 -G AT B/N HOLE NR 2 LT. PR1422B2 SEALANT APPLIED IAW EN.1180-04 AT B/N HO LE NR 2 LT. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 02 LT IAW EO M D11-5510-19409-G AND EN,11804 FOUND WITHIN LIMIT,SATISFACTORY. 2L73 4F RTA22WE 20040830001042004083000104NM 2004 8 30 UPS04M42947 120040611A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C RH HORIZ STAB NR 11 BARREL NUT HOLE FOUND CORRODED. CORROSION ON B/N HOLE NR 11 RT REMOVED AND REAMED IAW EO MD11-5510-19409-G FOUND OUT OF LIMIT. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 11 RT IAW EN.1209-04.REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 11 RT IAW EO MD11-551019409-G AND EN, 1209-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20040830001242004083000124NM 2004 8 30 TIP2004F00004 120040429A5315141T511286 FLOORBEAM BOEING767 76733AER 1385230NM FUSELAGE CORRODED B TIPRO OTHER O OTHER NRNOT REPORTED 1 SO05637TW 25403 CABIN FLOORBEAM AT STA 303, RBL 54 THRU RBL 82. CORROSION OUT OF LIMITS. REPAIR REQUIRED. SRM 53-00-51. FLOORBEAM IS IN WET/GALLEY AREA, SPILLS IN AREA CORRODED BEAM. GALLEY NEED TO BE PROPERLY SEALED AND VAPOR BARRIER INSTALLED. TASK CARD NR S53-027-02. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS MAY NEED TO INCREASE INSPECTION INTERVAL IN THIS AREA. 2L72 4F RTA1NM 20040830001252004083000125WP 2004 8 30 CALA0400607 120040820A575459358071 SLAT TRACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW27819NY 49479 INSPECTION FOUND A 1.5 INCH CRACK IN NR 10 AUX TRACK SLAT CAN XOS 380.229. THE NR 10 AUX TRACK SLAT, CAN WAS REMOVED AND REPLACED IAW SRM 51-30-0 AND 51-20-0. 2L72 4F4 F A6WE E9NE 20040830001322004083000132NE 2004 8 30 DHL2004805010 220040826A72613051182030 CARBON SEAL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 1 ENGINE DETERIORATED A DHLAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01805DH 46125 NR 1 ENGINE LOOSES APROX. 1.5 QT/HR OF OIL. OIL PRESSURE STABLE AT 50 PSI OIL LOSS STOPPED AT 2 QT. PERFORMED T/S IAW M/M 71-00-00 FAULT 60 FOUND EVIDENCE OF OIL LEAKAGE ON LWR PORTION OF T/R AND DRAIN MAST. FOUND CARBON SEAL AT STARTER PAD DETERIORATED, REMOVED AND REPLACED CARBON SEAL P/N 305-118-203-0 IAW MM 72-60-0 RA. 2L74 4F4 FRT4A25 E2GL 20040830001392004083000139NM 2004 8 30 F3LA200400075 120040727A3150350E018312020 COMPUTER AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE COCKPIT FAILED A F3LAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 NM03909FR 3233 1761 AIR TURN BACK. FLIGHT CREW REPORTED NUMEROUS SYSTEM FAILURES (GPS, GPWS, NR 1 RA, NR 1 ILS, NR 1 ENGINE REVERSER, NR 1 FADEC). CHECKED LAST LEG ECAM REPORT AND WAS UNABLE TO VERIFY FAULTS WITH CREW OR AIRCRAFT. CREW STATED ALL (FAULTED) SYSTEMS OPERATED NORMALLY. ONLY SYSTEM REPORTING PROBLEMS WAS FWC NR 2. REPLACED FWC NR 2 IAW AMM 31-53-34 AND SYSTEMS OPERATED NORMALLY. 2L72 4F4 FRTA28NM E2GL 20040830001442004083000144NM 2004 8 30 TSAA0436053 120040702A36101296662 PRECOOLER BOEING737 73776N 13844CHNM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13742AL 30830 CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED TO KWA. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLACED PRE-COOLER CONTROL VALVE AND PRE-COOLER CONTROL VALVE SENSOR. OPS CHECK GOOD AT 90 PERCENT N1 WITHOUT BLEED TRIP. COMPLETED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. FLIGHT VERIFICATION OKAY; CONTINUED FLIGHT. 2L72 4F4 FRTA16WE E2GL 20040830001502004083000150NE 2004 8 30 DL76L040779 220040819A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27185DN33657 27961 727649 IN CLIMB OUT OF VCE. L SCV TEMP 1 AND L SCV TEMP 2 EICAS STATUS MSG DISPLAYED. LATER OIL QTY DROPPED TO 7 THEN 0 FLT DIVERTED TO LGW. LANDED SAFELY OVERWEIGHT/C ADDED 14 QTS OF OIL NO EXTERNAL LEAKS ENGINE CHANGED ETOPS CATEGORY (B): DIVERSION OR TURNBACK. 2L72 4F4 FRTA1NM E24NE 20040830001672004083000167NM 2004 8 30 UPS04M42953 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB NR 32 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND S/W SURFACE. CORROSION AT B/N HOLE NR 32 LT REMOVED AND REAMED TO 1.178 INCH AND BLEND TO 0.0 50 NR FOUND OUT LIMIT IAW EO MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT AT B/N HOLE NR 32 LT IAW EN 1187-04. REPAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-5510-19409-G AND E N.1187-04 AT B/N HOLE NR 32 LT FOUND WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040830001882004083000188EU 2004 8 30 AWXA200400701 120040617A5347D5713014720000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON RT IB Y-765 SEAT RACK FR36-41. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT FR 36-41 IAW A320 SRM 51-42-11 FIGURES 9,10,12,18. 2L72 4F RTA28NM 20040830002062004083000206NM 2004 8 30 WLDA200429 120040618A324426094712 TIRE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 6 SEPARATED A WRLAO OTHER D INFLIGHT SEPARATION LDLANDING 1 SO11277 TIRE CAP SEPARATION: NR 6 TIRE CAP SEPARATED AFTER LANDING AND HIT LT IB FLAP. REMOVED AND REPLACED NR 6 MAIN TIRE ASSEMBLY. SERVICED WITH DRY NITROGEN TO NORMAL LEVEL IAW MM. INSPECTED LT IB FLAP DAMAGE, FOUND NEGLIGIBLE IAW SRM 51-00-00. 2L73 4F4 FRTA22WE E24NE 20040830002172004083000217NM 2004 8 30 DXTA200400346 120040724A2910 SWITCH GULSTM200 200 4500308NM HYD PRESSURE MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07702QS 070 LOST RT HYDRAULIC SYSTEM IN FLIGHT, RT HYD LEVEL LOW MESSAGE DISPLAYED. SYSTEM PRESSURE 400-600 PSI, LANDED AIRCRAFT USING EMERGENCY BRAKE SYSTEM. REMOVED AND REPLACED BRAKE CONTROL VALVE, PERFORM EMERGENCY BRAKE CHECK IAW MM CHAPTER 32-30-710-802. REPLACED RT HYDRAULIC SYSTEM PRESSURE SWITCH WITH NEW SWITCH IAW MM 29-10-16-000-801. 2L72 4F RTA53NM 20040830002192004083000219NM 2004 8 30 QXEA200400566 120040722A2750 CONTROL UNIT BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA FLAP SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09539DS4036 4016 THE CREW RAN THE ABNORMAL CHECKLIST AFTER THEY RECEIVED A FLAP POWER CAUTION WHILE ON APPROACH. CIRCUIT BREAKER L-7 WAS RESET IAW THE CHECKLIST. THE CAUTION LIGHT WENT OUT AND THE FLAPS OPERATED NORMALLY. MAINTENANCE INSPECTED THE SERVICE LETTERS DH8-400-SL-27-004 AND 400-SL-27-002A. FLAP CONTROL C/B CL-72 WAS RESET TO COMPLY WITH FULL POST OF FLAP SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040831000032004083100003CE 2004 8 31 R2J2004F00000 120040629A575355110373 BRACE CESSNA501 501 2076603CE PWA JT15 JT15D1 52060NE LT WING FLAP MISMANUFACTURED A R2JRO OTHER O OTHER NRNOT REPORTED 1 EA21501CF5689 5010128 WHILE REINSTALLING LT WING FLAP CABLES DURING PHASE 5 INSPECTION, NOTICED CABLE RUN TOO CLOSE TO STRUCTURE. INVESTIGATION AND NOTIFIED MFG TECH SUPPORT. IT WAS DETERMINED LT BRACE 5511037-3 AND RIB 5525130, CABLE PASS THRU WERE INCORRECTLY LOCATED DURING MANUFACTURE. FACTORY IAW PROVIDED APPROVED DATA TO ENLARGE PASS THRU, IN LT WING. (EA21200406587) 1L72 4F4 F A27CE E1NE 20040831000132004083100013NM 2004 8 31 QXEA200400568 120040727A6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE AUTOFEATHER SYS OUT OF ADJUST A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09374PH 528 ABORTED TAKEOFF DUE TO AUTOFEATHER DID NOT ARM WITH TAKEOFF POWER SET AND 70 KNOTS OF AIRSPEED INDICATED. ADJUSTED NR 1 AND NR 2 AUTOFEATHER ARMING POTENTIOMETERS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040831000172004083100017NM 2004 8 31 2004UALA00665 120040714A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 LT FWD CROWN AT STA 440 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20040831000212004083100021 2004 8 31 2004UALA00669 420040715A3421 INDICATOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE COCKPIT MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29668UA 30024 RETURN TO FIELD DUE TO CAPTAIN'S HORIZONTAL SITUATION INDICATOR PROBLEM. CREW REPORTED THAT CAPT'S HSI STUCK IN WX TEST PATTERN AND ILS MODE. CAPT'S EHSI DISPLAY (P/N 622-7999-003, S/N 114851) WAS REPLACED. THE SHOP FOUND NO FAULTS WITH THE DISPLAY AND RETURNED IT TO SERVICE. THE LT EFIS CONTROL PANEL (622-5048-381, S/N 121958) ALSO WAS REMOVED AS A PRECAUTION. THE CONTROL PANEL PASSED ALL SHOP TESTS, INCLUDING ENDURANCE AND THERMAL TESTING TO SEE IF THE UNIT WOULD LOCK UP IF POWERED FOR AN EXTENDED PERIOD. NO FAULTS WERE FOUND ON THE EFIS CONTROL PANEL AND IT WAS RETURNED TO SERVICE. THERE IS NO EXPLANATION FOR THE REPORTED EVENT. TO DATE THERE HAS BEEN NO RECURRENCE OF THE EVENT ON THE AIRPLANE. 2L72 4F4 FRTA1NM E24NE 20040831000262004083100026WP 2004 8 31 MWEA040136 120040810A1420 CONNECTOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE ROW 11 LOOSE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 EMERGENCY LIGHT INOPERATIVE AT ROW 11 RT SIDE. SECURED LOOSE CONNECTION. 2L72 4F4 F A6WE E2EA 20040831000512004083100051WP 2004 8 31 ARWA20040704 120040719A5730 SKIN PANEL DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE RT WING CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING C-CHECK INSPECTION, RT WING BETWEEN XRS.428 AND XRS.463 AT STRINGER S-64 LOWER SKIN PANEL WITH CRACK, LENGTH 5.25 INCHES. 2L74 4F4 F 4A25 1E8 20040831000532004083100053NM 2004 8 31 QXEA200400546 120040720A2820AV24B1343D VALVE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 400 LEAKING A QXEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 NM09347PH1650216502 480 DURING POST FLIGHT FOUND FLUID ON OUTSIDE OF NR 1 ENGINE NACELLE. REMOVED AND REPLACED REFUEL/DEFUEL TRANSFER SHUT OFF VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040831000542004083100054NM 2004 8 31 QXEA200400538 120040718A2697 WIRE DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 200 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 CARGO BAY FORWARD SMOKE DETECTOR WIRES ARE BROKEN. REMOVED AND REPLACED WIRE 2612-1J3. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040831000592004083100059WP 2004 8 31 IXXA0400099O 120040720A3220510361A LINK DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE NLG BROKEN A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW11823BX86413385 46064 DURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ONGOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE JACKED AIRCRAFT, RETRACTED NLG AND FOUND NGL DOOR TIGHT AND POPPING OPEN. THE FORWARD NLG DOOR LINK ASSEMBLY WAS REMOVED AND REPLACED IAW ALL APPLICABLE MANUALS. 2L74 4F4 FRT4A25 E2GL 20040831000622004083100062EA 2004 8 31 SWIA200413672 120040806A274184897132 MOTOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE HOR STAB TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07702SK 10136 STAB CHANEL 2 INOPERATIVE. REMOVED AND REPLACED HSTA MOTOR NR 2 IAW MM 27-42-03. OPERATIONAL CHECK GOOD. P/N: 8489-713-1 S/N OFF: 495 2L72 4F4 FRTA21EA E15NE 20040831000632004083100063SO 2004 8 31 SWIA200413674 120040730A2730 SPRING EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE ELEVATOR WORN A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07560SW 120334 ON PREFLIGHT, NOTICED UNUSUALLY LIGHT ELEVATOR BACK PRESSURE. REPLACED ELEVATOR RETURN SPRING ON CAPTAIN'S SIDE. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040831000642004083100064SO 2004 8 31 SWIA200413675 120040803A2731 TRIM SWITCH EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07298SW 120328 RECEIVED ORAL (TRIM FAIL) FOLLOWED BY AP DISCONNECT. REMOVED AND REPLACED PILOTS TRIM SWITCH IAW MM 22-10-10, OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040831000662004083100066NM 2004 8 31 AWXA200400727 120040626A5315D5347209001000 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 66 IAW A319 SRM 51-42-11 PG. 6, 7, & 41, FIG. 18. REGISTRATION NR WAS CHANGED TO REFLECT THE CORRECT AIRCRAFT, THIS EVENT DID NOT OCCUR ON A/C 160. 2L72 4F4 FRTA28NM E311NE 20040831000692004083100069EA 2004 8 31 SWIA200413611 120040725A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07410SW 7066 STABILIZER TRIM (BOTH CHANNELS) DISENGAGED DURING CLIMB. REMOVED AND REPLACED F/O'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-05 AND 27-40-00. 2L72 4F4 FRTA21EA E15NE 20040901000022004090100002EA 2004 9 1 SWIA200413685 120040808A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07909SW2096 2096 03043 7558 (FLT. SPOILERS FAULT AND SPOILERONS FAULT) STATUS MESSAGES APPEARED ON TAXI-OUT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK OK. 2L72 4F4 FRTA21EA E15NE 20040901000042004090100004NM 2004 9 1 P5CA0401125 120040622A5753 ANGLE BOEING747 747283B 1384867NM LT WING TE FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LT WING IB MID FLAP IB FORE FLAP TRACK WBL535 CUT OUT IS CRACKED AT IB LEADING EDGE RIB. REMOVED CRACKED ANGLE IAW SRM 51-30-02, FABRICATED REPAIRED DOUBLER IAW SRM 51-40-02, FIG 2 TREATED AND PAINTED INST DOUBLER IAW SRM 51-30-02, INST ANGLE IAW SRM 51-30-02. 2L74 4F A20WE 20040901000112004090100011NM 2004 9 1 AWXA200400742 120040627A5315D5347217220500 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AFT OF FR 66. MAINTENANCE REMOVED BEAM Y1292 RT FROM FR 64 TO FR 66+5 INCH; FABRICATED A NEW REPLACEMENT BEAM; DRILLED SPLICE COUPLING TO FORWARD END OF NEW BEAM; INSTALLED NEW BEAM NR COUPLING IAW A319 SRM 51-42-11, FIG. 9-17. 2L72 4F4 FRTA28NM E311NE 20040901000272004090100027SO 2004 9 1 SWIA200413678 120040804A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE WING CRACKED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM0758733 120197 DISCOVERED CRACK ON THE FLAP TRACK (NEXT TO ROLLER) IMMEDIATELY OB OF THE NR 1 ENGINE NACELLE. REPLACED LT OB FLAP IB ROLLER BRACKET WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040901000282004090100028EA 2004 9 1 SWIA200413679 120040802A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW 7279 STAB CH 1 INOP MESSAGE. REMOVED AND REPLACED CAPTIANS STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040901000292004090100029EA 2004 9 1 SWIA200413680 120040810A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT DIRTY A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07929SW 7703 FRONT FLOOR EMERGENCY LIGHTS AND 1 SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. CLEANED CONNECTOR AT BATTERY NR 2. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040901000442004090100044SO 2004 9 1 C2XA04SH464 120040721A531514521713005 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2724517 145332 DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040901000482004090100048WP 2004 9 1 ABXA040242 120040701A3260 CONDUIT DOUG DC9 DC915 3022036WP PWA JT8 JT8D* NE LT MLG DOWNLOCK BROKEN A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23927AX 45717 AFTER GEAR RETRACTION ON CLIMBOUT, (LT GEAR UNSAFE) LIGHT ILLUMINATED, CYCLED GEAR, NORMAL INDICATION THEREAFTER. THE LT MAIN LANDING GEAR DOWNLOCK FLEX CONDUIT WAS BROKEN. REPLACED THE FLEX CONDUIT AND CONNECTOR IAW MM 20-50-01. 2L72 4F4 F A6WE E2EA 20040901000622004090100062WP 2004 9 1 ASMF200408008 120040808A2910392492 SERVO VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23803ML1418 49726 DURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN INTERIOR DOUBLE SERVO VALVE. IT WAS REPLACED IAW MM32-43-02, TEST WERE CORRECT. 2L72 4F4 FRTA6WE E2EA 20040901000722004090100072WP 2004 9 1 04FDEA02328 120040730A5414 SKIN DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 NR 2 PYLON AFT TRAILING EDGE WEDGE NEEDS TO BE RAN. REMOVED TRAILING EDGE ASSY AND SKIN ASSY IAW SRM 51-35-01 VOL II AND SRM 51-31-01 VOL II. FABRICATED NE TRAILING EDGE ASSY IAW DWG AVB7021, ASSEMBLED TRAILING EDGE IAW SRM 51-35-01 VOL II, INSTALLED TRAILING EDGE ASSY IAW SRM 51-35-02 VOL II, FABRICATED NEW SKIN IAW DWG AVB7091, INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II AND 51-31-01 VOL II. FOR ADDITIONAL WORK SEE N/R N01063, N00716, N01061, N01062, N00717, N01064 AND N01065. REF N/R N01024. 2L73 4F4 FRTA22WE E23EA 20040901000842004090100084NM 2004 9 1 SWAA042515 120040829A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 922, STRINGER 25L, CRACKED. REPAIRED SKIN PER EA, SRM. 2L72 4F RTA16WE 20040901000922004090100092 2004 9 1 SWAA042475 420040826A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901000952004090100095NM 2004 9 1 UPS04243019 120040825A21215007024620 FAN BOEING727 727185C 138406NNM CABIN COOLING INOPERATIVE A IPXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01954UP 19827 DURING CLIMB ACRID ODOR NOTED IN COCKPIT. CREW TURNED OFF GASPER FAN, ODOR WENT AWAY. GASPAR FAN DEACTIVATED AND PLACED ON MEL M286609 & MEL CLOSED ON LP 212332. REPLACED GASPER FAN PER B727 MM CH 21-23-22, GASPER FAN OPS CHECK NORMAL. 2L73 4F A3WE 20040901000962004090100096NM 2004 9 1 UPS04243022 120040825A3350 LIGHT BOEING727 72731C 1384011NM CABIN MALFUNCTIONED A IPXAO OTHER L NO TEST NRNOT REPORTED 1 SO01926UP 19233 FLT STA EMERGENCY LIGHT WAS COMING ON IN FLT IN ARM POST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW 33-50-00. OPS CHECK GOOD. 2L73 4F A3WE 20040901000982004090100098WP 2004 9 1 ABXA040299 120040815A5320375849601 FITTING DOUG DC8 DC863F 302198FWP INTERCOSTAL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 INTERCOSTAL END FITTING AT STA 1140, LONGERON 35 LEFT WAS CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-1-20D. 2L74 4F 4A25 20040901000992004090100099WP 2004 9 1 ABXA040301 120040814A53305779936 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 AFT FUSELAGE SKIN FORWARD OF NR 3 CARGO DOOR HAD BULGED REPAIR. REPAIRED AREA IAW REA D853-50277MR. 2L74 4F 4A25 20040901001092004090100109NM 2004 9 1 SWAA042523 120040829A55516551524 FITTING BOEING737 7373A4 1384585NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND RT & LT HORIZONTAL STAB FITTING, FWD & AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20040901001102004090100110NM 2004 9 1 SWAA042524 120040830A53106545409 WEB BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, RBL 36, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040901001112004090100111NM 2004 9 1 SWAA042525 120040830A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040901001122004090100112NM 2004 9 1 SWAA042526 120040829A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 515, STR 14R, BS 563, STR 10L, BS 583, STR 10L, BS 520, BL 0, CRACKED. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20040901001132004090100113NM 2004 9 1 SWAA042527 120040829A5330655298874 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 964, STR 22L, BS 972, STR 24L, BS 942, STR 24L, CRACKED. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20040901001152004090100115NM 2004 9 1 SWAA042529 120040829A5242654583011 SKIN BOEING737 7373H4 1384600NM E/E DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND E&E DOOR OUTER SKIN CRACKED. REMOVED AND REPLACED E&E DOOR PER MM. 2L72 4F RTA16WE 20040901001182004090100118 2004 9 1 SWAA042492 420040827A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 L1 DOOR EVAC SLIDE LOOSE. SECURED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001192004090100119NM 2004 9 1 SWAA042493 120040827A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29410WN 27897 DURING SCHEDULED RON, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040901001202004090100120 2004 9 1 SWAA042494 420040827A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29441WN 29837 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001222004090100122NM 2004 9 1 SWAA042496 120040827A53306545890 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040901001242004090100124NM 2004 9 1 SWAA042498 120040827A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 17 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040901001262004090100126NM 2004 9 1 SWAA042500 120040827A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BUTTSTRAP AT BS 908, STRINGER 14L, CRACKED. REPAIRED BUTTSTRAP PER SRM. 2L72 4F RTA16WE 20040901001312004090100131NM 2004 9 1 04FDEA02573 120040829A5311 FRAME BOEING727 727200 138407ENM BULKHEAD CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 RIGHT MLG WHEEL WELL 870 BULKHEAD I/B LWR SUPPORT FRAME IS CRACKED JUST I/B OF BLEED AIR SHUTOFF VALVE. 2L73 4F RTA3WE 20040901001322004090100132NM 2004 9 1 04FDEA02574 120040829A5320 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 38R SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED SPLICE FITTING AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040901001332004090100133NM 2004 9 1 04FDEA02575 120040829A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 34L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW FABRICATED SPLICE FITTING AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040901001342004090100134NM 2004 9 1 04FDEA02576 120040829A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CENTER CARGO COMPARTMENT AT STA 5-113 TO 1542 LONGERON 41L SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED WITH NEW SPLICE FITTING AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20040901001352004090100135NM 2004 9 1 CALA0400621 120040828A532069353656 ANGLE BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733637 27540 INSPECTION FOUND A 4 INCH CRACK IN UPPER ANGLE ON INTERCOSTAL ADJACENT TO CABIN FLOOR A/C DISTRIBUTION BAY AT STA 482B-520 IN FORWARD CARGO BIN. A NEW UPPER ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040901001372004090100137NM 2004 9 1 CALA0400623 120040829A5755 SKIN BOEING737 737524 1384721NM NR 6 SPOILER DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733637 27540 INSPECTION FOUND THE RT WING NR 6 SPOILER DENTED ABOVE ACTUATOR. THE SPOILER WAS REPAIRED IAW SRM 57-70-01. 2L72 4F RTA16WE 20040901001382004090100138NM 2004 9 1 CALA0400624 120040829A5755 SKIN BOEING737 737524 1384721NM NR 3 SPOILER DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733637 27540 INSPECTION FOUND THE LT WING NR 3 SPOILER DENTED ABOVE THE ACTUATOR. THE SPOILER WAS REPAIRED IAW SRM 57-70-01. 2L72 4F RTA16WE 20040901001402004090100140WP 2004 9 1 UPS04843027 120040819A53404772397U1 FITTING DOUG DC8 DC871F 302199DWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C, STATION 1776 LONG 10L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D. 2L74 4F RT4A25 20040901001462004090100146WP 2004 9 1 ABXA040303 120040828A520059103677 RIB DOUG DC9 DC933F 302207AWP P-DOME DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 P-DOME PLUG DOOR NR 9 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05. 2L72 4F A6WE 20040901001472004090100147NM 2004 9 1 P5CA0401182 120040827A2910 LINE BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE HYD SYSTEM LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23921FT 21575 VIA PHONE PATCH, CREW REPORTS 0 PSI/0 QTY ON NR 1 HYDRAULIC SYSTEM. INSTALLED TEMP FLEX LINE PER MM 20-11-18 & GMM 3-17-1, PLACED ITEM ON COI 921-163. LINE IS LOCATED AFT OF STATION 23600 ON LT SIDE. 2L74 4F4 F A20WE E3NE 20040901001492004090100149NM 2004 9 1 P5CA0401180 120040826A36103206257 RELIEF VALVE BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 2 ENGINE MALFUNCTIONED A P5CAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23534MC 21832 530278 NR 2 ENG INDICATE A FIRE AT 13:50- 6 MINUTES AFTER TAKEOFF. NACELLE TEMP IN THE FIRE ZONE. ENGINE FIRE PROCEDURE WAS ACCOMPLISHED, PULLED FIRE HANDLE, DID NOT DISCHARGE FIRE BOTTLES. OIL PRESSURE NORMAL. REMOVED AND REPLACED NR 2 ENG PRESSURE RELIEF VALVE PER AMM 36-11-03. OPERATIONAL & LEAK CHECK NORMAL & PERFORMED SHUT OFF VALVE, OPS CHECKS ALL NORMAL. 2L74 4F4 F A20WE E23EA 20040901001512004090100151NM 2004 9 1 SWAA042477 120040826A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 948, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040901001522004090100152NM 2004 9 1 SWAA042478 120040826A521065458492 GATE BOEING737 7373H4 1384600NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR AT LOWER AFT GATE, CRACKED. REMOVED AND REPLACED R2 DOOR PER MM. 2L72 4F RTA16WE 20040901001532004090100153NM 2004 9 1 SWAA042479 120040826A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 507, STRINGER 14R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040901001542004090100154 2004 9 1 SWAA042480 420040826A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001572004090100157NM 2004 9 1 SWAA042484 120040826A524065C34670 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND RT FWD SERVICE DOOR UPPER HINGE FITTING CASTING, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR HINGE FITTING PER SRM. 2L72 4F RTA16WE 20040901001592004090100159NM 2004 9 1 SWAA042503 120040828A5210507945264 BEAM BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR WEB BEAM AT DOOR STOP, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR PER MM. 2L72 4F RTA16WE 20040901001602004090100160NM 2004 9 1 SWAA042487 120040826A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SPV, FOUND STRINGER 1 AT BS 862, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040901001622004090100162NM 2004 9 1 SWAA042489 120040826A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040901001652004090100165NM 2004 9 1 SWAA042505 120040828A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 3 ABC, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20040901001662004090100166NM 2004 9 1 P5CA0401178 120040824A2821 FILTER BOEING747 747249F 1384849NM PWA JT9 JT9D70A 52054NE FUEL OIL DAMAGED A P5CAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP23920FT 22237 702238 NR 2 ENGINE COMPRESSOR STALL. VISUAL INSPECTION, REMOVED AND REPLACED FUEL & OIL FILTER, ENGINE IDLE RUN ACCEPTABLE PER AMM 71-00-00. 2L74 4F4 F A20WE E3NE 20040901001672004090100167NE 2004 9 1 P5CA0401179 220040825A7320 CONTROLLER BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 1 ENGINE OUT OF ADJUST A P5CAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 WP23355MC 23395 455430 NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. ADJUSTED MAIN ENGINE CONTROL PER AMM 73-00-00. 2L74 4F4 FRTA20WE E23EA 20040901001682004090100168NM 2004 9 1 SWAA042506 120040828A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 970, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040901001692004090100169NM 2004 9 1 SWAA042507 120040828A575465C26686 WEDGE BOEING737 7373A4 1384585NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED. REPAIRED NR 2 L/E SLAT WEDGE PER SRM. 2L72 4F RTA16WE 20040901001702004090100170 2004 9 1 SWAA042508 420040828A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 L2 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001722004090100172 2004 9 1 SWAA042510 420040829A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001732004090100173NM 2004 9 1 SWAA042511 120040828A52406969854 GUSSET BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER BAC DRAWING. 2L72 4F RTA16WE 20040901001762004090100176NM 2004 9 1 UPS04242777 120040708A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON SKIN AT BS 253 S9R, AFT OF NR 3 RT COCKPIT WINDOW CUTOUT. HFEC CARRIED OUT ON THE ABOVE AREA IAW NDT MANUAL 51-00-00 PT 6 FIG 4. FASTENERS REMOVED IAW SRM 51-30-02. DAMAGED AREA REMOVED AND CUT LINE TRIMMED IAW SRM 53-30-3 FIG 29. FABRICATED EXTERNAL DOUBLER AND FILLER PARTS IAW SRM 53-30-3 FIG 29. INSTALLED REPAIR AND FASTENERS IAW SRM 51-30-02 AND 53-30-3 FIG 29. 2L73 4F A3WE 20040901001782004090100178EA 2004 9 1 MASA200400407 120040716A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA PAX JAMMED A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0737178 7178 ASH 6438 PHX-TUS. CREW REPORTED THE MAIN CABIN DOOR JAMMED IN CLOSED POSITION. MAINTENANCE OP'S CHECKED GOOD. 2L72 4F RTA21EA 20040901001822004090100182WP 2004 9 1 DHL2004804519 120040713A5720 ANGLE DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LEFT WING INBOARD SLOT SUPPORT ANGLE CRACKED 1.000, XILD 7095.000. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE (AL 7075-0 0.063) IAWJ SRM 57-2-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 1, 13, 17. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02107. CLEANED, TREATED AND PRIMED NEW ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040901001832004090100183WP 2004 9 1 DHL2004804522 120040707A57203645611U BRACKET DOUG DC8 DC873F 302199FWP NR 4 FUEL TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21-9. 2L74 4F RT4A25 20040901001842004090100184WP 2004 9 1 DHL2004804510 120040705A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT NR 6 TRACK LUG WORN, STA 248.000 TO STA. 275.000. TRIMMED OUT DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES (AL 7075-T6 0.100, 0.125, 0.160) IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B (AREA AND SPLICES). INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14, SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20040901001852004090100185WP 2004 9 1 DHL2004804511 120040714A5280 SKIN DOUG DC8 DC873F 302199FWP MLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LEFT MLG INBOARD DOOR INTERNAL SKIN CRACKED 0.500 AT STA 912.000 (LWR PART). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED DOUBLER (AL 7075-T6 0.050) IAW SRM 52-2-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 52-2-0 PG 1-2. 2L74 4F RT4A25 20040901001862004090100186WP 2004 9 1 DHL2004804500 120040624A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT NR 3 TRACK PLUG LUG WORN, STA 689.000. REMOVED NR 3 TRACK PLUG, STA 689.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLUG IAW DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040901001882004090100188EA 2004 9 1 SWIA200413720 120040816A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07597SW5058 5058 7293 FLIGHT SPLR FAULT STATUS MESSAGE FLASHES ON AND OFF DURING FLIGHT. REMOVED AND REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040901001912004090100191EA 2004 9 1 MASA200400419 120040723A5270 SWITCH CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT OUT OF ADJUST A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW0717275 7275 ASH 6021 PHX. PILOT REPORTED A RIGHT EMERGENCY DOOR CAUTION MESSAGE IN FLIGHT. *S/D* MX PLACED ITEM ON MEL. MX ADJUSTED SWITCH AND INSULATION. 2L72 4F RTA21EA 20040901001922004090100192EA 2004 9 1 MASA200400422 120040723A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA LT PACK FROZEN A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07506MJ996 10073 ASH 7073 RDU-ORD. THE AIRCRAFT WAS RETURNED TO THE FIELD DUE TO THE ODOR OF SMOKE IN THE CABIN. UPON LANDING THE CREW REPORTED A LEFT PACK OVER HEAT MESSAGE. CONTRACT MAINTENANCE VERIFIED THE ODOR OF SMOKE BEING GENERATED BY THE LEFT PACK AND PLACED THE LEFT PACK ON DEFERAL. MX REPLACED THE ACM, OPS CHECK GOOD. 2L72 4F RTA21EA 20040901001932004090100193EA 2004 9 1 MASA200400427 120040726A5210HSP115B062350 PIN CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0775987 7405 ASH 2914 JAX. PAX DOOR HANDLE WOULD NOT STOW. AIRCRAFT WAS FERRIED TO PHL FOR REPAIR. PHL MX REPLACED THE OUTER HANDLE SHEAR PIN. 2L72 4F RTA21EA 20040901001942004090100194EA 2004 9 1 MASA200400443 120040808A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0775987 7405 ASH 2843 PWM-CLT. PAX DOOR WILL NOT OPEN FROM THE OUTSIDE. MX LUBED DOOR, OPS CHECKED GOOD. 2L72 4F RTA21EA 20040901001972004090100197EA 2004 9 1 MASA200400457 120040817A3233 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAO OTHER J WARNING INDICATION DEDESCENT 1 SW0777302 ASH 6460 SAN-PHX. DURING DESCENT AT GEAR EXTENSION THE CREW GOT A NOSE GEAR DOOR OPEN MESSAGE. MAINTENANCE REMOVED AND REPLACED THE NLG PRIORITY VALVE, OPS CHECK GOOD. 2L72 4F RTA21EA 20040901002002004090100200NM 2004 9 1 DL73S040787 120040802A2822 PUMP BOEING737 737232 1384475NM FUEL BOOST MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27301DL UNK 23073 ON TAKEOFF NR 2 TANK FWD BOOST PUMP C/B POPPED. FWD NR 2 TANK FWD BOOST PUMP TO MCO/PLCRD PER MEL 28-00-01B. NOTE: NR 2 TANK AFT BOOST PUMP ON MCO/CNTRL C08194634. REPLACED NR 2 AFT BOOST PUMP, S/N 10131125BMANUF, P/N 258000-5. MCO/PLCRD REMOVED. 2L72 4F RTA16WE 20040901002012004090100201NM 2004 9 1 DL76L040788 120040819A3030 COMPUTER BOEING767 767332 1382001NM EICAS MALFUNCTIONED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27176DN 25061 ON POWER UP FOR TAKEOFF PROBE HEAT EICAS DISPLAYED ALONG WITH 2 OR 3 OTHER MSGS. NO OVERHEAD LIGHTS WERE NOTED. T/S PER FIM 30-31-00 FIG 108 SHEET 1, HOOKED UP PITOT/STATIC TESTER PUMPED A/S TO 60 KNTS, RAN ENGINES TO TAKEOFF PWR NTF. POWERED PIMUS WITH ENGS RUNNING, PERFORMED N2 SPEED CARD BITE CK FOR BOTH LEFT RIGHT ENGS NTF. ALL SYSTEM RETURNED TO NML. REPLACED LT & RT EICAS COMPUTERS, NEEDS TAXI CHECK. ALSO REPLACED BOTH N2 SPEED CARDS ROBBED FROM 189. 2L72 4F RTA1NM 20040902000012004090200001NM 2004 9 2 DL75K040791 120040820A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO276705Y 30397 INBND CREW REPORTED INTERMITTENT RUBBER ODOR MID LAV AREA. OVERHEAD PANEL PULLED AND PERFORMED THROUGH INSPECTION. UNABLE TO LOCATE ANY AREAS OF CONCERN. ALL AREAS LOOKED TO BE NEW AND OK. 2L72 4F RTA2NM 20040902000022004090200002NM 2004 9 2 DL767040792 120040821A733041801104 PRESSURE SWITCH BOEING767 767232 1385132NM GE CF680 CF680A2 NE NR 2 ENGINE INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27115DA 22227 580175 RIGHT ENG FUEL FILTER EICAS MSG ON TAKEOFF, ATB. REPLACED NR 2 ENG FUEL FILTER/FUEL PRESS SW. NO DEBRIS FOUND. OK FOR SERVICE PER FIM 73-11-00 PG 106. 2L72 4F4 FRTA1NM E13NE 20040902000042004090200004WP 2004 9 2 DHL2004804516 120040709A57203645611U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 NR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040902000052004090200005WP 2004 9 2 DHL2004804514 120040625A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LEFT OUTER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 860.000. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040902000072004090200007WP 2004 9 2 DHL2004804513 120040715A53204641324 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 AFT FUSELAGE AFT LONGERON SPLICE FITTING CRACKED 1.000 AT STA 1690.000, L30R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 581-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040902000092004090200009WP 2004 9 2 DHL2004804523 120040707A57203645612U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 NR 4 ALT FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 4 ALT FWD BOOSTER PUMP IAW SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21-9. 2L74 4F RT4A25 20040902000102004090200010WP 2004 9 2 DHL2004804507 120040628A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT NR 4 TRACK LUG WORN, STA 1696.000. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040902000162004090200016NM 2004 9 2 WLDA200470 120040802A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 27. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 27 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040902000172004090200017NM 2004 9 2 04FDEA02577 120040829A5311 FRAME DOUG MD11 MD11 3023602NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CABIN - FUSELAGE FRAME AT STA 1721, LEFT HAND, S12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1721, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 53- 30-00 VOLUME II. FEDEX EA 1-5310-79742, FUSELAGE. TRACKING SRM REPAIR ON FRAME AT STATION 1721, LONGERON 12L, ISSUED FOR TRACKING. 2L73 4F RTA22WE 20040902000192004090200019WP 2004 9 2 04FDEA02476 120040814A5330ADA01409 PANEL DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 FWD CARGO SUMP PANEL IS CRACKED RT SIDE 960-980. REMOVED AND REPLACED PANEL IAW IAW DRWG ADA0140 AT MAE. 2L73 4F RTA22WE 20040902000232004090200023WP 2004 9 2 DHL2004804525 120040722A53204751820 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT FITTING CRACKED 1.000, STA. 702.000, RBL 25. REMOVED CRACKED FITTING AT STA 702.000 RBL 25 IAW DC8 SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FITTING IAW EA5320-029, DWG 4751820. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040902000252004090200025NM 2004 9 2 DHL2004745519 120040706A5754 FRAME BOEING727 727224 1384076NM NR 3 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, NR 3 SLAT INT FRAME BOTTOM AFT WS 525 IS CRACKED IN RADIUS. REMOVED NR 3 SLAT FOR SHEET METAL ACCESS IAW B727 M/M 27-81-11. REMOVED CRACKED RIB ON NR 3 SLAT IAW B727 SRM 51-30-2. FABRICATED RIB FROM 7075-T6 .032 SIZE 15 X 5.5 INCHES PO 900573 IAW B727 SRM 57-50-2. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED RIB IAW B727 SRM 51-30-2. INSTALLED NR 3 SLAT IAW B727 M/M 27-81-11. 2L73 4F A3WE 20040902000262004090200026NM 2004 9 2 DHL2004742005 120040723A3260 WARNING LIGHT BOEING727 727225 1384077NM MLG ILLUMINATED A DHLAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 SO01742DH 21290 GEAR UNSAFE LIGHT INDICATION. 2L73 4F A3WE 20040902000272004090200027EU 2004 9 2 AWXA200400922 120040823A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONE 221 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28629AW14191709 076 DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY BULLNOSE LIGHT AT SEAT ROW 4 RT INOPERATIVE. REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040902000292004090200029EU 2004 9 2 AWXA200400924 120040805A5315D5347217220000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040902000302004090200030SO 2004 9 2 CHQA000516 120040716A3350 LIGHT EMB 145 EMB145LR 3260212SO OVERWING EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11972 145440 FLOOR PROXIMITY LIGHTS STRIP RUNNING AFT TO OVERWING EXITS ARE INOP. REMOVED AND REPLACED CABIN FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CHECKS GOOD. 2L72 4T RTT00011AT 20040902000312004090200031EU 2004 9 2 AWXA200400916 120040820A3350079123 MODULE AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28639AW 471 DURING F-05 CHECK MAINTENANCE FOUND THE FORWARD LT PARTITION EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD LT PARTITION EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040902000332004090200033EU 2004 9 2 AWXA200400918 120040822A335032145410 EPSU AIRBUS320 A320232 3930326EU ZONE 263 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28605AW9339 4139 543 PHX - EEL - DURING E-02 CHECK MAINTENANCE FOUND THE LT AFT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040902000412004090200041EA 2004 9 2 COMA0460480 120040816A2913 PUMP CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYSTEM FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01719CA 7253 FLIGHT 5450 DURING CRUISE FLIGHT RECEIVED A HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND DIVERTED TO TYS. REPLACED FAILED NR 2 ENGINE DRIVEN HYDRAULIC PUMP. 2L72 4F RTA21EA 20040902000432004090200043EU 2004 9 2 DHL2004365001 120040626A32411766 SERVO VALVE AIRBUS300 A300B4203 3930306EU ANTI SKID SYSTEMINOPERATIVE A DHLAO OTHER P NO WARNING INDICATION LDLANDING 1 SO01365DH 149 LEFT MAIN ANTI SKID ON FWD LEFT WHEEL INOP. TRANSFERRED TO N/R 3831 W/O 24251. REMOVED AND REPLACED SERVO VALVE 1766 LEAK AND OPS CHECK NORMAL AS PER A300 MM 32-42-48. ANTI SKID TEST OF NR 1 WHEEL AND ANTI SKID SYSTEM, TEST IS NORMAL IAW A300 MM 32-42-00, THIS ACTION CLEARS. 2L72 4F RTA35EU 20040902000442004090200044EA 2004 9 2 MASA200400459 120040817A5270 TARGET CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR OUT OF ADJUST A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07922FJ 15022 ASH 6359 PHX. A RIGHT FORWARD EMERGENCY EXIT DOOR INDICATING OPEN WHEN DOOR WAS SHUT. THE EMERGENCY EXIT INDICATING SYSTEM WAS PLACED ON MEL. MAINTENANCE ADJUSTED THE TARGET, OPS CHECK GOOD. 2L72 4F RTA21EA 20040902000472004090200047NM 2004 9 2 DHL2004745560 120040702A5347 SEAT TRACK BOEING727 727224 1384076NM FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, COCKPIT F/E AFT TRACK HAS WORN OUT INDICATION LOCK HOLES ARE SCRATCHED. REMOVED & REPLACED DAMAGED TRACK P/N 806019-401 PO 427462 IAW 727 SRM 51-30-2. 2L73 4F A3WE 20040902000492004090200049WP 2004 9 2 MWEA040151 120040824A53479957871502 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FIRST OFFICER'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED SEAT TRACK TEE. 2L72 4F A6WE 20040902000512004090200051NM 2004 9 2 WLDA200475 120040802A5512ALC8104501 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE 19. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 19 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040902000532004090200053NM 2004 9 2 DHL2004765005 120040713A2610 FIRE WARNING BOEING727 727264 138408MNM CARGO BAY MALFUNCTIONED A DHLAO OTHER WN INADEQUATE Q C FALSE WARNING CRCRUISE 1 SO01765AT 23014 CARGO FIRE DETECTION PANEL FAULT LIGHT ILLUMINATED. RESET SYS AFTER IMPROPER TEST, SYS OPS CHECKED GOOD IAW B727 MM CHAPT 26. 2L73 4F A3WE 20040902000562004090200056NM 2004 9 2 DHL2004784004 120040626A2611 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01784DH 22001 ENGINE NR 3 DETECTOR CIRCUIT GROUND LIGHT FLICKERS ON IN FLIGHT. ADJUSTED NR 3 ENGINE FIRE LOOP DETECTOR IAW B727 M/M 26-11-01. CKS NORMAL ON GROUND. 2L73 4F A3WE 20040902000572004090200057CE 2004 9 2 HAEA200400157 120040714A32419544282 ANTI-SKID SYS LEAR 24 24 5170302CE NR 2 A/S GEN FAULTY E HAEAO OTHER S AFFECT SYSTEMS LDLANDING 1 SW05222TW1469914699 24161 ON LANDING YIP, PILOT REPORTED AIRCRAFT BEGAN TO SLIGHTLY VEER TO THE RIGHT. CREW APPLIED FULL FLIGHT CONTROL DEFLECTION IN AN ATTEMPT TO COUNTER ACT ANY CROSSWIND COMPONENT. CAPTAIN APPLIED ASYMMETRICAL BRAKING (MORE LEFT THAN RIGHT). AIRCRAFT CONTINUED TO VEER TO THE RIGHT AT WHICH TIME THE EMERGENCY BRAKE SYSTEM WAS ACTIVATED. THE AIRCRAFT DEPARTED THE PAVED SURFACE AND STOPPED A SHORT DISTANCE. NO DAMAGE TO AIRCRAFT. MAINTENANCE DISCOVERED NR 2 ANTI-SKID GENERATOR FAULTY. 2L72 4J A10CE 20040902000652004090200065CE 2004 9 2 ACE071504 120040715A5250MS171499 ROLL PIN BEECH 1900 1900C 1154161CE COCKPIT DOOR SHEARED E YADAK NONE O OTHER ININSP/MAINT 1 AL03114AX UC36 PIREP - COCKPIT DOOR HANDLE DOES NOT WORK FROM OUTSIDE. REPLACED SHEARED DOOR HANDLE ROLL PIN. 2L72 4T RTA24CE 20040830001682004083000168NM 2004 8 30 UPS04M42954 120040623A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 28 FOUND CORRODED. CORROSION AT B/N HOLE NR 28 LT REMOVED AND REAMED TO 1.178 INCHES AND BLEND TO 0. 06 INCH IAW EO MD11-5510-19409-G FOUND EXCEEDED LIMIT. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED PR1422B2 SEALANT AT B/N HOLE NR 28 LT IAW EN 1233-04. REPAIR AND INSTALLED SLEEVE BUSHING IAW EO MD11-51 0-19409-G AND EN.1233-04 FOUND WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040830001832004083000183NM 2004 8 30 QXEA200400632 120040818A5210 CAM DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE PAX DOOR INOPERATIVE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09347PH16680 480 CREW REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND CLEANED AND LUBED THE DOOR FRICTION GUIDES/CAMS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040830001862004083000186EU 2004 8 30 AWXA200400699 120040613A5347D5337111000100 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION (PITTING) WAS FOUND ON THE RT IB Y-765 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT Y765, FR 41-47 IAW A320 SRM 51-42-11 PAGES 6,7 28 FIGURE 12. 2L72 4F RTA28NM 20040830001962004083000196WP 2004 8 30 04FDEA02325 120040730A5751 COUNTERWEIGHT DOUG MD10 MD1010F 3022112WP GE CF6 CF6* 30020GL ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 226456 LT OB AILERON BALANCE WEIGHTS, 5 EACH HAVE CORROSION AND CAD PLATING MISSING. REMOVED AND REPLACED WEIGHT ASSEMBLY IAW CMM 57051-07, SB 57919. REMOVED CORROSION FROM HOLE AND INSTALLED BUSHING IAW SB 57-117 AND CMM 57-51-02 AND EA 8-5750-77610. FLAP PEENED AND DYE PENETRANT INSPECTION OF HOLES IAW EA 8-5750-77610. REF N/R N00777. 2L73 4F4 FRTA22WE E23EA 20040830002012004083000201WP 2004 8 30 04FDEA02313 120040730A5753ANB71131 ROLLER DOUG MD10 MD1010F 3022112WP ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 RT IB FLAP TRACK LOWER LOAD ROLLER WORN. REMOVED AND REPLACED LOWER LOAD ROLLER ON RT IB FLAP TRACK. INSTALLED AND TORQUED IAW EA 8-5750-80957 T.W. NR 8381H DUE 12-08-04. REF. N/R 00645 2L73 4F RTA22WE 20040830002082004083000208NM 2004 8 30 UPS04M42959 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C LT HORIZ STAB NR 35 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING AND SIDEWALL SURFACE. CORROSION AT B/N HOLE NR 35 LT REMOVED AND REAMED TO 1.13 INCH AND BLEND TO 0.05 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-19409-G. FAB AND REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOL E NR 35 LT IAW 1195-04. REPAIR AND INSTALLED B/N HOLE NR 35 LT IAW EO MD11-55 10-19409-G AND EN.1195-04 FOUND WITHIN LIMIT,SATIS. 2L73 4F RTA22WE 20040830002182004083000218CE 2004 8 30 CWQ2004F00008 120040303A301065525023 PICCOLO TUBE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D1 52060NE NR 1 ENGINE CORRODED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05348QS 5600348 DURING ROUTINE PHASE 1-4 INSP, THE MECH GRABBED THE LIP BLEED AIR FEED TUBE NR 1 ENGINE AND APPLIED PRESSURE BACK AND FORTH, A NOISE WAS HEARD BANGING AT EACH STROKE. AFTER FURTHER DISASSEMBLY (REMOVAL OF LIP) FOUND THE 6552502-3, PICCOLO ASSY ATTACH LEGS (2 EA) .3333 CRACKED, AND ALMOST BROKEN. AT THIS TIME THERE WAS NO DAMAGE TO THE LIP SKIN FROM CHAFFING. LOCATED AND INSTALLED A NEW PICCOLO ASSY USING SAME TYPE FASTENERS REMOVED. ATTACHED PICTURES. 2L72 4F4 FRTA22CE E1NE 20040830002242004083000224 2004 8 30 234TR0021 420040815A2210403889916 COMPUTER BOEING737 737228 13844AGNM PWA JT8 JT8D15A 52051NE AUTOPILOT INOPERATIVE A PIDAO OTHER O OTHER CRCRUISE 1 SO05234TR 23004 AUTO PILOT A SIDE KICKED OFF BY ITSELF AND THEN WILL NOT REENGAGE. REPLACED A CHANNEL FCC IAW MM 22-11-331 AND OPS CHECKED IAW MM 22-11-01. 2L72 4F4 FRTA16WE E2EA 20040830002262004083000226SO 2004 8 30 CHQA000514 120040708A3397 LIGHT EMB 145 EMB145LR 3260212SO CONT O520 IO520* 17032SO CABIN MISWIRED A CHQAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 GL11296 145514 FORWARD PROXIMITY LIGHT IS INOPERATIVE. INVESTIGATED PROBLEM AND FOUND WIRING HOOKED UP IMPROPERLY. REROUTED WIRING IAW MFG 145 AMM 33-50-50. OPS CHECK GOOD AT THIS TIME. 2L72 4T3 ORTT00011ATE5CE 20040831000052004083100005EU 2004 8 31 KBM2004F00187 120040506A6420350A33215001 SPIDER SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 T/R SPIDER BALL END WORN. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040831000092004083100009SO 2004 8 31 MASA200400414 120040719A2741 PITCH CONTROL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL 1 & 2 MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07845MJ 145502 RETURNED TO THE FIELD DUE TO A PITCH TRIM 1 AND 2 INOPERATIVE AND CAS MISCOMPARE MSG. MECHANIC RESET THE PITCH TRIM SYSTEM AND IT OPERATED NORMALLY. ALL MESSAGES CLEARED AND A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T4 FRTT00011ATTE6CH 20040831000122004083100012CE 2004 8 31 DXTA200400369 120040820A3260 UPLOCK CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL LANDING GEAR MALADJUSTMENT E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07979QS4932 BMC083 7500079 IN CRUISE FLT, NOSE GEAR WENT INTO A SERIES OF UNLOCKS (WITH RED LIGHT) AND RETRACTS. FOUND NOSE STRUT EXTENSION EXCEEDED 9.63 INCHES CAUSING NOSE GEAR NOT TO FULLY SEAT IN UPLOCK ASSY. DISASSEMBLED NOSE STRUT AND FOUND ORIFICE FITTING NOT TORQUED. REPACKED NOSE STRUT IAW 750 CMM 32-20-02. SERVICED NOSE STRUT IAW 750 MM 12-10-38. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. 2L72 4J4 FRTT00007WITE6CH 20040831000292004083100029NM 2004 8 31 DL757040692 120040725A335020131ASMI BATTERY BOEING757 757232 1384965NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27641DL 23995 EMERGENCY ESCAPE LIGHTING IN F/C VERY DIM ON TEST. REPLACED BATTERY PACK IN EMERGENCY ESCAPE PATH PWR SUPPLY M9101 IAW AMM. CKS GOOD. 2L72 4F4 FRTA2NM E17NE 20040831000352004083100035NM 2004 8 31 MWEA040123 120040723A521059100817 SKIN BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE PAX DOOR BENT A MWEAK NONE O OTHER ININSP/MAINT 1 GL31904ME 55168 LOWER CORNER OF PASSENGER DOOR SKIN IS BENT AT EDGE 1.00 INCH X 4.00 INCH. REMOVED DAMAGE, INSTALLED EXTERNAL DOUBLER. 2L72 4F4 FTRA6WE E00057EN 20040831000362004083100036WP 2004 8 31 MWEA040128 120040805A5312991556211 ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE PRESS BULKHEAD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 CABIN SIDE OF AFT PRESSURE BULKHEAD, A STIFFNER AT TWELVE O'CLOCK POSITION IS CRACKED ON OB END. FABRICATED AND INSTALLED ANGLE. 2L72 4F4 F A6WE E2EA 20040831000432004083100043NM 2004 8 31 P5CA0401127 120040618A5751 SKIN BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE LT IB AILERON DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 LT IB AILERON DELAMINATED LOWER SIDE WBL500 2 PLACES. REPAIR 2EA DAMAGED AREA WITH FIBER GLASS IAW SRM 51-40-15, APPLIED CONDUCTIVELY COATING, PRIMED AND PAINTED. 2L74 4F4 F A20WE E3NE 20040831000442004083100044NM 2004 8 31 P5CA0401121 120040712A5314 KEELBEAM BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 CORROSION ON KEELBEAM 2 PLACES, AT BS 1332 AND STA 1319 RT SIZE. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW MA NR A5349-01-02, WORK ACCOMPLISH ON T160-468. 2L74 4F4 F A20WE E3NE 20040831000482004083100048EU 2004 8 31 WRNA200040000 120040715A5270 SWITCH AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE CARGO DOOR DIRTY A WRNAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO05820SC 154 CARGO DOOR AND NOT LOCKED LIGHT ON, IN FLT. ALSO CARGO SWITCH FAULT LIGHT ON. DIVERTED TO GSO FOR REPAIR, 5200 GALS FUEL DUMPED FOR LANDING WT. REQUIREMENT. AIRCRAFT LANDED NORMAL. LUBED DOOR LOCK HANDLE SWITCH AND CLEANED STRIKER PLATES IAW SUP. MM 52-36-11 OPS CHECK MAIN CARGO DOOR, OPS CHECK GOOD LIGHT IND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20040831000492004083100049NM 2004 8 31 CALA0400591 120040804A53206552878U124 ANGLE BOEING737 737524 1384721NM GE CFM56 CFM56* 13802NE BS CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769603 27316 INSPECTION FOUND L-2 DOOR ZEE ANGLE CORRODED IN SEVERAL AREAS FROM BS 910-1016. THE ZEE ANGLE WAS REPLACED IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E2GL 20040831000742004083100074EA 2004 8 31 SWIA200413682 120040811A2741 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07918SW 7645 INFLIGHT, MACH TRIM AND CHANEL 1 STAB DISENGAGED. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL FOR IAW CRJ 200 MM 27-41-20. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040831000752004083100075EA 2004 8 31 SWIA200413683 120040807A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SERVICE LACK OF LUBE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07945SW 7770 UNABLE TO OPEN THE GALLEY ACCESS DOOR FROM OUTSIDE. ADJUSTED, CLEANED AND LUBED SERVICE DOOR AS REQUIRED IAW MM 52-41-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040901000252004090100025CE 2004 9 1 63428 120040728A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG MALFUNCTIONED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07176YV UE176 WHILE TAXING IN AFTER LANDING IN TPA. CAPTAIN FELT THAT THE LT BRAKE FELT SPONGY. THEN CALLED MAINTENANCE. BRAKES WAS BLEED, OPS CK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040901000512004090100051WP 2004 9 1 UPS04842874 120040702A5347S47553952400 SEAT TRACK DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, STA 595-600 RBL 36 SEAT TRACK LOBES ELONGATED/OBLONGED. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-2-3. REMOVED SEAT TRACK SECTION IAW SRM 51-3-0, DRILLED NEW SEAT TRACK SECTION TO FIT IAW SRM 51-1-24. INSTALLED IAW SRM 51-3-0 AND 51-3-1. 2L74 4F4 FRT4A25 1E8 20040901000522004090100052WP 2004 9 1 UPS04842876 120040702A5321S2772659 FLOORBOARD DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, STA 280 RBL 1 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION SECTION OF FLOORBOARD FAB SPLICE PLATES. ALODINED AND PRIMED. INSTALLED SPLICE PLATES AND SECTION OF FLOORBOARD IAW SRM 51-3-0, 51-3-1, 53-2-3 FIG 9, 51-1-8, AND 53-2-0. 2L74 4F4 FRT4A25 1E8 20040901000702004090100070NM 2004 9 1 HNAA0407101 120040711A496063D49845521 CONTROL PANEL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE GENERATOR STICKING A HNAAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07840EX28682 327 FLIGHT NR 3993 REPORTED AN ELECTRICAL ODOR DURING SHUTDOWN OF THE APU WITH THE ASSOCIATED CIRCUIT BREAKER N-8 POPPING. MAINTENANCE REMOVED AND REPLACED THE APU CONTROL PANEL DUE TO THE GENERATOR SWITCH STICKING IN THE ON POSITION. ALL OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040901000742004090100074EU 2004 9 1 04FDEA02336 120040801A5730 PANEL AIRBUS310 A310 EU GE CF6 CF680 30025NE RT WING DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25409FE 273 RT WING OB T/E PANEL ZONE 691 HAS 100 DENTS, OF WHICH 40 ARE DELAMINATED (TOP AND BOTTOM OF PANEL) ( AREA 2 INCHES X 12INCHES ) REMOVED DAMAGED T/E PNL AND INSTALLED NEW T/E PNL IAW A310/200 DWG 57243876. 2L72 4F4 FRTA35EU E13NE 20040901000892004090100089 2004 9 1 SWAA042538 420040830A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR PER MM. 2L72 4F RTA16WE 20040901000912004090100091NM 2004 9 1 SWAA042474 120040826A2821731085 FILTER BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE CLOGGED A SWAAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW29073SW 22673 687864 INFLIGHT SHUTDOWN/DECLARED EMERGENCY. ON CLIMBOUT NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED, REDUCED THRUST LIGHT WENT OUT. SHUTDOWN ENGINE. FOUND CARBON BUILD UP IN FILTER. REMOVED AND REPLACED OIL FILTER PER MM. 2L72 4F4 F A16WE E2EA 20040901001142004090100114NM 2004 9 1 SWAA042528 120040829A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 812, STR 18L, CRACKED. REPAIRED SKIN PER EA, SRM. 2L72 4F RTA16WE 20040901001162004090100116NM 2004 9 1 SWAA042530 120040829A531065C31308 DOOR FRAME BOEING737 7373H4 1384600NM CARGO BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C-1 CHECK, FOUND FWD CARGO DOOR AFT FRAME AT AFT LOWER STOP, CRACKED. REPAIRED DOOR FRAME PER BAC DRAWING. 2L72 4F RTA16WE 20040901001172004090100117NM 2004 9 1 SWAA042491 120040827A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 EEPLS COVERS AT LT & RT ROW 8 LOOSE. SECURED EEPLS COVERS PER MM. 2L72 4F RTA16WE 20040901001212004090100121NM 2004 9 1 SWAA042495 120040827A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040901001232004090100123 2004 9 1 SWAA042497 420040827A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C4 CHECK, FOUND L1 & R1 DOOR EVAC SLIDES GIRT BAR HOOKS LOOSE. SECURED L1 & R1 DOOR EVAC SLIDES GIRT BAR HOOKS PER MM. 2L72 4F RTA16WE 20040901001272004090100127NM 2004 9 1 SWAA042501 120040827A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE AT BS 908, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040901001302004090100130EU 2004 9 1 04FDEA02568 120040827A4920A4957082300200 DUCT AIRBUS300 A300B4605R 3930308EU ZONE 200 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25677FE 791 APU INTAKE ELBOW HAS MULTIPLE DEBONDS AND BULGES. REPAIRED APU INTAKE ASSY IAW A300-600 AMM 49-16-14 AND EA 6-4915-81873. 2L72 4F RTA35EU 20040901001362004090100136NM 2004 9 1 CALA0400622 120040829A5755 SKIN BOEING737 737524 1384721NM NR 7 SPOILER DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733637 27540 INSPECTION FOUND THE RT WING NR 7 SPOILER DENTED. THE SPOILER WAS REPAIRED IAW SRM 57-70-01. 2L72 4F RTA16WE 20040901001392004090100139EU 2004 9 1 UPS04143029 120040827A3350 POWER SUPPLY AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHT MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01124UP 0808 EXIT LIGHTS REMAIN ON AFTER TEST. REPLACED POWER SUPPLY UNIT PER 33-51-14-4. OPS CHECK GOOD. 2L72 4F RTA35EU 20040901001442004090100144WP 2004 9 1 ABXA040304 120040828A531059103677 RIB DOUG DC9 DC933F 302207AWP PRESS BULKHEAD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 PRESSURE DOME PLUG DOOR NR 4 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-02. 2L72 4F A6WE 20040901001482004090100148NE 2004 9 1 P5CA0401181 220040826A7200NA ENGINE BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 2 MALFUNCTIONED A P5CAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23534MC 21832 530278 DURING T/O AFTER ROTATION NR 2 ENG TEMP ROSE INTO THE YELLOW BAND & THE NACELLE TEMP WAS RISING RAPIDLY, THE THROTTLE WAS RETARDED & TEMP CAME DOWN. ENG FAILURE CHECK ACCOMPLISHED. NR 2 ENGINE REMOVED & REPLACED. 2L74 4F4 F A20WE E23EA 20040901001582004090100158NM 2004 9 1 SWAA042485 120040826A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB AT WBL 135.5, CRACKED. REPAIRED LT WING RIB CHORD PER SB, ERO. 2L72 4F RTA16WE 20040901001632004090100163 2004 9 1 SWAA042490 420040826A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001812004090100181WP 2004 9 1 DHL2004804520 120040715A53204641324 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 AFT FUSELAGE AFT LONGERON SPLICE FITTING CRACKED 1.000 AT STA 1690.000, L-26R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040901001902004090100190 2004 9 1 SWIA200413722 420040814A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTO PILOT FAILED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07224SW2014 2014 120294 AUTOPILOT ELEVATOR SERVO FAILURE ON FINAL APPROACH. REPLACED AUTOPILOT ENGAGE PANEL ASSY WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20040901001992004090100199EA 2004 9 1 MASA200400439 120040804A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX INOPERATIVE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07653ML 7039 ASH 2644 CLT. PAX DOOR WILL NOT CLOSE. MX IN THE PROCESS OF TROUBLESHOOTING. OPS CHECKED DOOR AND OPS CHECK GOOD. 2L72 4F RTA21EA 20040902000032004090200003WP 2004 9 2 DHL2004804512 120040708A57513652979 BRACKET DOUG DC8 DC873F 302199FWP RT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 RIGHT OUTBOARD AILERON LWR SECTION HINGE BRACKET 1.000 CRACKED, STA XA 752.000. REMOVED CRACKED BRACKET IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW BRACKET IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040902000152004090200015NM 2004 9 2 WLDA200469 120040802A5512ALC8103503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 28. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB LEFT BARREL NUT HOLE NR 28 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040902000182004090200018NM 2004 9 2 04FDEA02475 120040813A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 FORWARD CARGO, CORROSION OBSERVED ON LONGERON 43R STA 1125. TRIMMED OFF AS PER SRM 53-10-00 VOLUME 1. REPAIR LONGERON FABRICATED AND INSTALLED AS PER SRM 53-10-00 VOLUME 1. 2L73 4F RTA22WE 20040902000392004090200039NM 2004 9 2 WLDA200485 120040802A5330A5A70441 SKIN PANEL DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, WHILE PERFORMING J/C D929721 FOUND DAMAGE ON FUSELAGE SKIN PANEL AT BS STA 5-73 BETWEEN L48L AND L49L. PERFORMED REPAIR OF THE FUSELAGE SKIN PANEL PER EGAT EI W2004A53B. CONDITION CHECK SATISFACTORY. 2L73 4F RTA22WE 20040902000402004090200040NM 2004 9 2 CALA0400619 120040826A53306545772 SKIN BOEING737 7373T0 1384582NM FUSELAGE LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND SMOKING AND LOOSE RIVETS IN FUSELAGE SKIN AT STA 1006-1016, S2L TO S3L. REMOVED AND REPLACED DOUBLER IAW SRM 53-00-01, FIGURE 229, PAGE 332. 2L72 4F RTA16WE 20040902000422004090200042NM 2004 9 2 DHL2004764006 120040624A2612 FIRE DETECTOR BOEING727 727264 138408MNM CARGO BAY MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01764AT 22984 LOWER CARGO FIRE DETECTOR DOES NOT TEST PROPERLY. RED ANNUNCIATOR ON S/O PANEL, NOR RED ANNUNCIATOR ON FWD GLARESHIELD DOES NOT ILLUMINATE. RESET CARGO FIRE DETECTOR, SYS OPS GOOD IAW MM 26-10-0. 2L73 4F A3WE 20040902000542004090200054WP 2004 9 2 DHL2004807010 120040626A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP NR 2 WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01807DH 45990 MAIN CABIN SMOKE DETECTOR NR 2 WILL NOT TEST. NR 2 MAIN CABIN SMOKE DETECTOR OPS CHECK NORMAL IAW DC 8 MM 26-10-6, THIS CLEARS DMI 17026. 2L74 4F RT4A25 20040902000602004090200060NM 2004 9 2 UPS04242738 120040702A5320 WEB BOEING727 72725C 138400HNM TORQUE BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, CRACK EVIDENT AT LIGHTENING HOLE IN THE AFT ENTRY STAIRS AREA. CRACK LOCATED AT B-STA 1263 APPROX, LEFT SIDE OF TORQUE BOX VERTICAL WEB JUST OUTSIDE DOUBLER OF PREVIOUS REPAIR. CRACK STOP DRILLED PER SRM 51-10-1. HFEC INSPECTION CARRIED OUT AROUND STOP DRILL HOLE IAW B727 NDT M 51-00-00 FIG K. RESULT WAS THE CRACK WAS CONTAINED WITHIN STOP DRILL. AREA TRIMMED OUT WITHIN LIMITS IAW SRM 51-10-1. REMOVED DOUBLER FROM PREVIOUS REPAIR AND REPAIRED LIGHTENING HOLE IAW SRM 51-40-2. 2L73 4F A3WE 20040902000612004090200061NM 2004 9 2 UPS04542830 120040730A2780 SLAT BOEING757 75724APF 1384969NM RT/ LT SLATS OUT OF RIG A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01460UP 25481 DIVERSION - L/E SLAT DISAGREE MESSAGE AT FLAP EXT. ADJUSTED RIGHT SLATS NR 7, 8, 9, 10 IAW MM 27-81-00-5. ADJUSTED LT & RT SLATS O/B POSITION TRANS IAW MM 27-58-01-5. C/W BOW TS 1820 REV 998 SYSTEM OPS CHECKS NORMAL. 2L72 4F RTA2NM 20040902000642004090200064WP 2004 9 2 DHL2004873005 120040803A3260 WARNING LIGHT DOUG DC8 DC873F 302199FWP MLG ILLUMINATED A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01873SJ 46091 UPON LANDING GEAR EXTENSION LEFT LANDING GEAR LIGHT CAME ON IMMEDIATELY UPON LOWERING LANDING GEAR HANDLE. 2L74 4F RT4A25 20040902000682004090200068NM 2004 9 2 UPS04242854 120040705A5753 SKIN BOEING727 72725C 138400HNM RT WING TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, RIGHT WING O/B AFT FLAP HONEYCOMB FILLER DELAMINATED AT I/B END. AFT FLAP FITTINGS REMOVED FROM UNSERVICEABLE FLAP AND FITTED TO REPLACEMENT AFT FLAP IAW OHM 20-50-01 AND OHM 57-52-11. FLAP ASSY REPLACED IAW MM 27-51-12 AFT FLAP ADJUSTED IAW MM 27-51-12 PARA 5 SUB PARA 4A-G. INCLUSIVE ECCENTRIC ROLLERS ADJUSTED AS REQUIRED & SATISFIED IAW MM 27-51-00. 2L73 4F A3WE 20040902000692004090200069NM 2004 9 2 UPS04242855 120040706A5310 DOOR FRAME BOEING727 72725C 138400HNM AFT CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, SUSPECT CRACK ON AFT CARGO DOOR FRAME SKIN FLANGE RADIUS OF NR 3 FWD STOP FITTING (REF DETAIL I FIGURE 1 FLANGE 1 OF EO SECTION B-B). HFEC CONFIRMED CRACK AND MARKED END. REMOVED CARGO DOOR BALANCE MECHANISM IAW MM 52-31-53. REMOVED AFT CARGO DOOR FRAME IAW SRM 51-30-02. FRAMES INSTALLED IAW DRG 65C16422 & SRM 51-30-2. CARGO DOOR BALANCE MECHANISM REFITTED IAW MM 52-31-53. 2L73 4F A3WE 20040902000742004090200074NM 2004 9 2 SWAA042444 120040823A52106545871 BEAM BOEING737 7373Q8 1384670NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR NR 1 WEB BEAM CRACKED AT RIGHT CORNER. REMOVED AND REPLACED R1 DOOR PER MM. 2L72 4F RTA16WE 20040902000752004090200075NM 2004 9 2 SWAA042445 120040824A53306552988 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 937, STR 22R. REPAIRED SKIN PER SWA EA. 2L72 4F A16WE 20040902000762004090200076NM 2004 9 2 SWAA042446 120040824A53306545770 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 8L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20040902000772004090200077NM 2004 9 2 SWAA042447 120040824A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C4 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20040902000782004090200078NM 2004 9 2 SWAA042448 120040823A53116546543 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 11R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040902000792004090200079NM 2004 9 2 SWAA042450 120040824A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND LEFT WING RIB LOWER CHORD CRACKED AT WBL 135.5. REPAIRED RIB PER SWA EA. 2L72 4F RTA16WE 20040902000802004090200080NM 2004 9 2 SWAA042451 120040824A27306545166 PUSHROD BOEING737 7373H4 1384600NM ELEVLATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED THE FREEPLAY CHECK. REMOVED AND REPLACED RIGHT ELEVATOR CONTROL PUSH ROD ATTACH BOLTS PER MM. 2L72 4F RTA16WE 20040902000822004090200082NM 2004 9 2 SWAA042453 120040824A57536546434370 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20040902000842004090200084NM 2004 9 2 SWAA042531 120040829A5330655298871 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE BOX FUSELAGE SKIN CUTOUT AT LOWER RADIUS, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040902000852004090200085NM 2004 9 2 UPS04242761 120040712A5347 SEAT TRACK BOEING727 72725C 138400HNM COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, O/B SEAT TRACK SECTION FWD OF BS 740 LEFT SIDE CORRODED AT BS 740 & 751 ON HORIZONTAL FLANGE AND FWD END OF FLANGE FOUND BENDED BEYOND CLEANUP LIMITS. SEAT TRACK FABRICATED IAW SRM 51-20-01 & SRM 53-10-02. SEAT TRACK ALODINED AND PRIMED IAW SRM 51-10-02. SEAT TRACK INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20040902000882004090200088NM 2004 9 2 UPS04442750 120040713A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, COCKPIT - BS 360 RIGHT FRAME WEB FOUND CRACKED BETWEEN STR 6 AND STR 5. FRAME WEB REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F RTA20WE 20040902000902004090200090NM 2004 9 2 UPS04442752 120040713A5311 FRAME BOEING747 747200 1384847NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, U/D - BS 400 LEFT FRAME WEB FOUND CRACKED BETWEEN STR 9 AND STR 10A AS MARKED. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 11 AT M/D BS 400 LEFT BETWEEN STR 9 TO STR 10A. 2L74 4F RTA20WE 20040902000912004090200091WP 2004 9 2 UPS04842739 120040610A531156141605 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, AC COMPT STA 55 LONG 30-31 RIGHT CORR AT INTERSECTION OF FRAME TO T/R BOX LEG ANGLE. RECEIVED FRAME SECTION AND SPLICES FROM STRUCTURE CENTER WORK ACCOMPLISHED ON TIMCO N/R 5001. FAB 4 EA SPLICES 2-19 & 2-17 IAW TR 53-125, THEN HEAT TREATED. LOCATED, DRILLED, DEBURRED FRAME & SPLICE SECTION. ALODINED & PRIMED FRAME & SPLICES. INSTALLED REPAIRED ANGLES. INSTALLED TR PUMP BOX & TRANSFORMER. REMOVED CORROSION FOUND OUT OF LIMITS. 2L74 4F RT4A25 20040902000922004090200092WP 2004 9 2 UPS04842740 120040611A5340459764361 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, R/S CUSP FRAME 35 FWD & AFT CUSP FITTING ARE CORRODED AT FLOOR AT BOLTS B6 69. REMOVED CUSP FITTINGS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1- 8. INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-3-0, 51-3-1. 2L74 4F RT4A25 20040902000932004090200093WP 2004 9 2 UPS04842741 120040611A53145750371501 KEELBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3 LEFT W/W AT KEEL BEAM AT FS 922 TO 936 HAS A CRACK. REPAIRED IAW REO GO9853. 2L74 4F RT4A25 20040902000952004090200095NM 2004 9 2 DL73S040782 120040820A534365468305 FITTING BOEING737 737247 138448DNM STRUT SUPPORT CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 MLG SIDE STRUT SUPPORT FITTING AT FUSELAGE STATION 685 WAS FOUND WITH LUB BORE CORROSION ON BOTH THE RT AND LT SIDES. REPAIRED IAW ERA 092411-14. 2L72 4F A16WE 20040902000972004090200097NM 2004 9 2 DL73S040784 120040820A5330654577886 SKIN BOEING737 737247 138448DNM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 FUSELAGE SKIN SUFFERED GROUND DAMAGE AT STATION 969 BETWEEN STR 20R AND 21R. REPAIRED IAW ERA 092483-14. 2L72 4F A16WE 20040902000982004090200098NM 2004 9 2 DL73S040785 120040820A5711654540247 STIFFENER BOEING737 737247 138448DNM WING SPAR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 WING CENTER SECTION REAR SPAR STIFFENER FOUND CRACKED AT RBL 6.15. REPAIRED IAW ERA 092296-14. 2L72 4F A16WE 20040902000992004090200099NM 2004 9 2 UPS04242861 120040702A2701 YOKE BOEING727 72725C 138400HNM COCKPIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, PERFORM A GVI OF CAPT & F/O CONTROL YOKES & ATTACHED LINKAGE, PAYING ATTENTION TO CORROSION, BINDING OR LOOSENESS OF BEARINGS. ROTATE EACH CONTROL WHEEL FULL TRAVEL LEFT & RIGHT CHECKING FOR ANY STIFFENESS, BINDING OR RATCHETING OF MOVEMENT. OPERATE AILERON TRIM FULL TRAVEL IN EACH DIRECTION CHECKING FOR BINDING & FRICTION. GVI CARRIED OUT IAW UPS GMM 4-3-1. FOUND SATISFACTORY. BACKLASH ON CAPT'S CONTROL WHEEL ADJUSTED IAW OHM27-16-01 STEP 12P502 & RATCHETING FOUND REMOVED. AILERON TRIM & CENTERING SPRINGS REPLACED & ADJUSTED TO MAX. LIMIT PER OHM 27-11-01. ALL PULLEYS & LINKAGES LUBED IAW MM. TRIM SYS CHECKED & NO LAGGING FOUND. CONTROL COLUMNS RECONN. 2L73 4F A3WE 20040902001002004090200100NM 2004 9 2 UPS04442833 120040709A1430 BOLT BOEING747 747200 1384847NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, LT WING CENTER SECTION REAR SPAR WEB AT BS 1241 BULKHEAD FITTING CORROSION REVEALED BETWEEN BOLT NR 7, 8 AND 9. THICKNESS CHECK PER NTM PART 4,57-10-19 RESULT: NR 7 HOLE 0.335 INCH, NR 8 HOLE 0.350 INCH, NR 9 HOLE 0.370 INCH. NR 7, 8 & 9 FASTENER HOLES REAMED TO 0.375 INCH DIA PER UPS EO B747-5710-11129 FIG 6. FASTENER HOLES AREA CORROSION REMOVED AS PER SRM 21-10-01 & REPROTECTED AS PER SRM 51-12-02. 2L74 4F RTA20WE 20040902001012004090200101NM 2004 9 2 UPS04442834 120040712A541165B903082 RIB BOEING747 747200 1384847NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, NR 4 PYLON NAC STA 232 APPROX I/B RIB CRACKED AS MARK (JUST FWD OF PYLON VALVE PANEL CUTOUT). NR 4 PYLON RIB REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 8 AND SRM 51-30-02. 2L74 4F RTA20WE 20040902001022004090200102WP 2004 9 2 UPS04842845 120040715A5313 LONGERON DOUG DC8 DC873F 302199FWP AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 STATION 1770 LONG 17R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION IAW DWG 5649327 AND SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20040902001052004090200105WP 2004 9 2 UPS04842848 120040722A534037558401 FITTING DOUG DC8 DC873F 302199FWP CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, STATION 1220 AFT SIDE BATHTUB FITTING IS CRACKED BETWEEN LONG 33R AND 32.5R IN TORQUE BOX. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20040902001082004090200108NM 2004 9 2 AWXA200400928 120040729A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER TIE AT BS 807, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 807, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 7. 2L72 4F RTA16WE 20040902001102004090200110NM 2004 9 2 AWXA200400930 120040729A5330659187911 PANEL BOEING737 7373G7 1384595NM KEEL LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 LCQ - MAJOR REPAIR - DURING C-18 CHECK INSPECTION FOUND RIVETS WORKING AND LOOSE ON KEEL BEAM SKIN PANEL AT BS 640, AT BL 0, BETWEEN AIR CONDITIONING BAY DOORS. REMOVED, FABRICATED, AND INSTALLED NEW REPLACEMENT KEEL BEAM SKIN PANEL AT BS 640, AT BL 0 IAW AWA ER 03-5310-02085-JS1. 2L72 4F RTA16WE 20040902001132004090200113WP 2004 9 2 UPS04842743 120040613A53112537716 FRAME DOUG DC8 DC873F 302199FWP FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3 FWD PIT FRAME HAS CORROSION FWD SIDE AT STA 140 BETWEEN L34L AND L34R. REMOVED FASTENER TO FRAME IAW DC8 SRM 51-1-21D, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED FRAME SECTION. LOCATED AND DRILLED SPLICE ANGLE REPAIR AND FRAME IAW DC8 SRM 51-1-24. ALODINED AND PRIMED. INSTALLED FRAME, SPLICE AND GILLINER ATTACH IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040902001142004090200114EA 2004 9 2 COMA0460465 120040812A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01507CA3260 7796 FLIGHT 5126 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20040902001152004090200115EA 2004 9 2 VNAA0408004 120040722A2731 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERONS OUT OF ADJUST A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07229PS 7898 DURING TAKEOFF, THE CREW RECEIVED AN AILERON TRIM AND A CONFIG TRIM WARNING INDICATION AND ABORTED TAKEOFF. ALL TRIM INDICATIONS WERE NORMAL AFTER THE ABORTED TAKEOFF. HOWEVER, THE CREW ADJUSTED THE AILERON TRIM DUE TO BEING CLOSE TO THE ALLOWABLE TOLERANCE. ALL INDICATIONS WERE NORMAL AND FLIGHT 2355 ATTEMPTED ANOTHER TAKEOFF AND DEPARTED WITH NO FURTHER INCIDENTS. THIS REPORT WAS DERIVED FROM AN ASAP REPORT. 2L72 4F4 FRTA21EA E15NE 20040902001162004090200116NE 2004 9 2 VNAA0408003 220040808A7314 PUMP DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE FUEL SYSTEM FAILED A VNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07438JS 3056 DURING TAKEOFF, THE CREW RECEIVED A LOW FUEL PRESSURE MESSAGE AND ABORTED TAKEOFF. MAINTENANCE CONTROL DEFERRED THE ASSOCIATED FUEL PUMP SYSTEM WITH MEL 28-9 CODE-C. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040902001172004090200117EA 2004 9 2 VNAA0408005 120040729A5300 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AIRFRAME VIBRATION A VNAAO OTHER E VIBRATION/BUFFET DEDESCENT 1 GL07253PS 7934 AT 28,000, THE CREW FELT A MODERATE VIBRATION AND SLOWED TO 290 AND THE VIBRATION LESSENED. AFTER SELECTING THE FLAPS TO 20, THE VIBRATION INCREASED THEN LESSENED AGAIN. THE MODERATE VIBRATION CONTINUED UNTIL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT IN ACCORDANCE WITH BOMBARDIER AMM 32-20-00-210-801, 32-10-00-210-801, 27-64-00-710-801, 27-40-00-720-801 AND 27-54-00-310-801, NO DEFECTS WERE NOTED. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED AND AGAIN, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040902001192004090200119NM 2004 9 2 DHL2004764007 120040709A3150 PLATE BOEING727 727264 138408MNM YAW DAMP LIGHT SHORTED A DHLAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01764AT 22984 AT FL330 CREW SMELLED SMOKE OBSERVED SMOKE COMING FROM OVERHEAD PANEL AT YAW DAMPER SWITCHES. TURNED OFF LOWER YAW DAMPER AND OVERHEAD LIGHTS, SMOKE STOPPED. EMERGENCY LANDING AT ABQ. FOUND YAW DAMPER LIGHT PLATE SHORTED. REMOVED AND REPLACED LIGHT IAW B-727 M/M 33-10-0, SYS TEST NORMAL. 2L73 4F A3WE 20040902001232004090200123WP 2004 9 2 ASAA0480235 120040404A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01976AS 53452 PDX - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 6. RECONNECTED LOOSE CONNECTOR WIRE. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001262004090200126NM 2004 9 2 ASAA0410269 120040523A3350883200312 HOUSING BOEING737 737290C 138448VNM BATTERY INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - FOUND ROW 8 EMERGENCY LIGHT INOPERATIVE, FLOOR TRACK. REPLACED BATTERY RECEIVER HOUSING. (M) 2L72 4F A16WE 20040902001272004090200127NM 2004 9 2 ASAA0440125 120040507A2750655280773 ACCESSORY UNIT BOEING737 737490 1384715NM TE FLAPS INOPERATIVE A ASAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM01795AS219402251 28890 ANC - FOUND THE TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES ADVANCED TO TAKEOFF POWER. ABORTED TAKEOFF AT LESS THAN 50 KTS. REPLACED FLAP/SLAT ACCY UNIT. (M) 2L72 4F RTA16WE 20040902001282004090200128NM 2004 9 2 ASAA0410255 120040507A1420 CONNECTOR BOEING737 737210C 1384459NM BATTERY PACK LOOSE A ASAAO OTHER O OTHER LDLANDING 1 NM01744AS 21822 JNU - UP0N LANDING, EMERGENCY EXIT LIGHTS FLICKERED. RESET CONNECTORS TO BATTERY PACKS. (M) 2L72 4F A16WE 20040902001322004090200132EA 2004 9 2 ASOA04535 120040729A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11852AS 7369 DURING GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY FLOOR STRIP INOPERATIVE. MAINTENANCE FOUND THE FORWARD ORAGNE STRIP OF FLOOR EMERGENCY LIGHTING UNPLUGGED AND UNSECURED. MAINTENANCE RECONNECTED AND RESECURED THE LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCFAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040902001362004090200136EU 2004 9 2 ASOA04544 120040712A5720 BRACKET AEROSPATR72 ATR72212 8680945EU WING BOX CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT UPPER WING BOX BRACKETS AT FRAME 26 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT UPPER WING BOX BRACKETS AT FRAME 26 IAW SRM 51-25-04 AND 51-25-01. (M) 2H72 4T RTA53EU 20040902001372004090200137EU 2004 9 2 ASOA04543 120040712A5711S5397071635701 FRAME AEROSPATR72 ATR72212 8680945EU WING BOX CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT WEB WING BOX AT FRAME 28A WAS FOND TO BE CRAKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT WEB WING BOX AT FRAME 28A IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040902001392004090200139NM 2004 9 2 2004F00250 120040105A3250 PIN BOEING727 727231 1384079NM NLG STEERING BACKED OUT A FX7AD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 SO1954348 21967 LOSS OF STEERING DURING LINING UP FOR TAKEOFF RETURNED TO GATE. FOUND APEX PIN BACKED OUT OF STEERING KNUCKLE. INSTALLED APEX PIN AND OPS CHECK SYSTEM PER 32-51. INSPECTED AREA AND FOUND NO FURTHER DAMAGE A/C RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040902001482004090200148NM 2004 9 2 UIEA200400023 120040223A534765B6017654 SEAT TRACK BOEING747 7472F6B 1384807NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15534MC 21832 FORWARD CARGO COMPARTMENT SEAT TRACK CRACKED AT BS 576, APPROX RBL 48. REMOVED DAMAGED SEAT TRACK AS PER 747 SRM 51-30-01. INSTALLED SECTION OF SEAT TRACK IN FORWARD CARGO COMPARTMENT AT BS 576 RBL 48 P/N 65B601176-54. P/O NR 5075 LOT NR 01511488 REF 53-10-05 FIG 5. (M) 2L74 4F A20WE 20040902001502004090200150NE 2004 9 2 MEX2004036 220040127A732076960615 FCU DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NR 1 ENGINE FAILED A ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23755RA 49727 AIRCRAFT RETURN TO PLATFORM AS CONSEQUENCE OF ENGINE NR 1 SHOWS N2 46.5 PERCENT AND EGT 430. TRIM WAS ACCOMPLISHED AND PARAMETERS WERE WITHIN LIMITS. DURING OVERNIGHT SERVICE, THE FCU AND PRBC WERE REPLACED IAW MM 73-20-01 AND 75-31-01, RESPECTIVELY. TEST CORRECT IAW MM 71-00-01. (M) 2L72 4F4 FRTA6WE E9NE 20040902001532004090200153NM 2004 9 2 UIEA200400015 120040212A5414 SKIN BOEING747 747243B 1384830NM NR 3 PYLON WRINKLED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 DURING D-CHECK AT SIN, FOUND NR 3 PYLON HAS A WRINKLE CONDITION ON RIGHT SIDE. SKIN ASSEMBLY WAS TRIMMED TO REMOVE THE WRINKLED AREA. NDT INSPECTION OF THE REPAIR AREA, INCLUDING HFEC INSPECITON OF SKIN TRIMMED EDGES AND REPAIR FASTENER HOLES WAS PERFORMED TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. A NEW SKIN REPAIR DOUBLER ASSY WAS INSTALLED FROM FS 286-316. THE NEW SKIN REPAIR DOUBLER ASSY WAS MADE FROM TWO STAGGERED LAYERS OF TITANIUM SHEET AND INSTALLED IMMEDIATELY AFT OF THE TITANIUM SIN DOUBLER EXTENSION. THE NEW SKIN REPAIR DOUBLER ASSEMBLY FORWARD END WAS ATTACHED TO THE EXISING TITANIUM DOUBLER EXTENSION WITH A NEW TRIPLER MADE FROM TITANIUM SHEET. (M) 2L74 4F A20WE 20040902001542004090200154WP 2004 9 2 I5HA0258007 120040624A324434479 TIRE CVAC 580 580 2422806WP MLG DEPARTED A I5HAD RETURN TO BLOCK D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 GL23581P MFD - DURING PILOT TRAINING, AIRPORT MX CREWS NOTICED ONE OF THE TIRES MISSING OFF THE AIRCRAFT AS IT TAXIED BY WHILE ON THE TAXI-WAY. THE MX CREW NOTIFIED THE TOWER WHO IN TURN NOTIFIED CRW. THE AIRCRAFT TAXIED TO THE TARMAC AREA AND SHUTDOWN. THE MX AND INSPECTION DEPARTMENT WERE NOTIFIED BY THE CRW THAT THE NR 2 MAIN LANDING GEAR TIRE AND WHEEL ASSY WAS GONE. A MX CREW WAS DISPATCHED FOM THE COLUMBUS, OH MX BASE. FURTHER EXAMINATION BY THE MAINTENANCE CREW DETERMINED THAT THE OUTER BEARING HAD SEIZED WHICH RESULTED IN THE TIRE AND WHEEL ASSY SPINNING OFF THE AXLE. THE NR 1 TIRE AND WHEEL ASSY WERE REMOVED AND THE AXLE WAS INSPECTED BOTH VISUALLY AND WITH DYE PENETRANT. THERE WAS NOT DAMAGE TO THE AXLE2L72 4T RT 20040902001632004090200163NM 2004 9 2 USAA040380 120040721A5315 FLOORBEAM BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND BEAM CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BEAM, FS 993, RBL 14-44. MANUFACTURED NEW SUPPORT ANGLE PER BOEING DWG 65C19883. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20040902001652004090200165NM 2004 9 2 USAA040368 120040713A575465C266031 SKIN BOEING737 7373B7 1384580NM NR 3 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND TOP SKIN AND CORE MATERIAL DELAMINATED 3 INCH BY 4 INCH AREA, NR 3 SLAT INBOARD T/E CORNER. INSTALLED NEW CORE, INSTALLED FILLER AND UPPER DOUBLER PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040902001672004090200167NM 2004 9 2 USAA040365 120040729A5512 SKIN BOEING737 737301 1384611NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19576US50869 23741 PIT - FOUND SKIN CRACKED 2.05 INCH, FS 129 LOWER SKIN AT AFT SPAR LEFT HORIZ STAB. INSTALLED DOUBLER PER SRM 55-10-01. (M) 2L72 4F RTA16WE 20040902001692004090200169NM 2004 9 2 USAA040364 120040720A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19586US51238 23931 CLT - FOUND SKIN CRACKED 1 INCH LONG, FS 727D AND STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) 2L72 4F RTA16WE 20040902001732004090200173NM 2004 9 2 USAA040387 120040721A575465C26602108 SKIN BOEING737 7373B7 1384580NM NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19393US51331 23315 PIT - FOUND SKIN AND CORE BOND DELAMINATED 3 INCH BY 4 INCH AREA, UPPER INBOARD END T/E CORNER OF NR 5 SLAT. REMOVED DELAMINATED, UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040902001762004090200176EU 2004 9 2 ASOA04555 120040716A5753S5751211020500 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAP CAM CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURNG A C-CHECK IN YUL, THE RIGHT OUTBOARD FLAP CAM GUIDE NR 4 FROM INBOARD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP CAM GUIDE NR 4. (M) 2H72 4T RTA53EU 20040902001772004090200177EA 2004 9 2 ASOA04563 120040804A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27901EV 7616 FLT 4512 - DURING A GROUND INSPECTION IN BTR, THE LOWER LEFT EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR WAS FOUND WITH SEVERAL LAMPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE LOWER LEFT EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040902001782004090200178EA 2004 9 2 ASOA04566 120040805A5210 ROD END CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7328 FLT 4243 - DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS VERY DIFFICULT TO OPEN. MAINTENANCE COULD NOT DUPLICATE THE PASSENGER DOOR DISCREPANCY. THE PASSENGER DOOR HANDLES AND ROD ENDS WERE LUBRICATED FOR PREVENTATIVE MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040902001792004090200179EA 2004 9 2 ASOA04565 120040805A3350BF50390901 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11902EV 7620 FLT 4269 - DURING A GROUND INSPECTION IN DFW, THE EMEGENCY EXIT ILGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040902001802004090200180EA 2004 9 2 ASOA04564 120040805A3350BF10044004 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11829AS 7232 FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER AT THE FORWARD BULKHEAD BY THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE FORWARD BULKHEAD BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040902001812004090200181NM 2004 9 2 ASAA0410256 120040507A252086210144 BATTERY BOEING737 737298C 1384490NM SEAT PALLET DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 ANC - MAINTENANCE CHECK, FOUND SEAT PALLET 4-10 BATTERY LOW. REPLACED BATTERY. (M) 2L72 4F RTA16WE 20040902001822004090200182NM 2004 9 2 ASAA0410257 120040507A335086210144 BATTERY BOEING737 737298C 1384490NM EMERGNCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - MAINTENANCE CHECK, FOUND BULKHEAD 'EXIT TO REAR' LIGHT IS DIM. REPLACED BATTERY. (M) 2L72 4F RTA16WE 20040902001832004090200183NM 2004 9 2 ASAA0470006 120040628A5320143A750116 ANGLE BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01622AS 30165 OAK - DUIRNG C-CHECK, FOUND ZEE ANGLE CORRODED IN FORWARD CARGO COMPARTMENT AND LBL 21. REPLACED IAW SRM. (M) 2L72 4F RTA16WE 20040902001842004090200184NM 2004 9 2 ASAA0470004 120040628A5321453A2610 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01622AS 30165 OAK - DURING C-CHECK, FOUND AFT CARGO NR 2 FLOOR PANEL HAS CORROSION ON EDGES. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040902001852004090200185NM 2004 9 2 ASAA0470007 120040628A53201496377 ANGLE BOEING737 737790 13844CNNM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01622AS 30165 OAK - DURING C-CHECK, FOUND ZEE ANGLE CORRODED AT STATION 727 AS TO STATION 847. REPAIRED IAW SRM. (M) 2L72 4F RTA16WE 20040902001862004090200186WP 2004 9 2 ASAA0480363 120040430A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 LAX - DURING PREFLIGHT CHECK, FOUND SEVERAL EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001872004090200187NM 2004 9 2 ASAA0440099 120040406A3397 WIRE BOEING737 7374Q8 138447QNM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01772AS 25105 JNU - FOUND SIX ADJACENT TRACK LIGHTS INOPERATIVE SEAT ROWS 2-6. RECONNECTED LIGHT ASSEMBLY AT ROW 2. (M) 2L72 4F RTA16WE 20040902001882004090200188NM 2004 9 2 ASAA0440101 120040410A3350 LIGHT BOEING737 7374S3 1384711NM ROW 10-11 INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01786AS 24795 SEA - FOUND ROW 10-11 EMERGENCY AISLE LIGHTING DO NOT ILLUMINATE. REPLACED BOTH LIGHT ASSEMBLYS, OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 20040902001912004090200191CE 2004 9 2 2004F00265 120040513A2700 CONTROL CABLE CESSNA750 750 2076810CE FLT CONTROLS OUT OF RIG A UG8AA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL235115 7500018 CONTROL YOKES SHOW 25 DEGREE RIGHT BANK DURING STRAIGHT AND LEVEL. RIGHT AILERON IS UP ND LEFT ELEVATOR IS UP. PITCH CONTROL FORCE FEELS NORMAL. AMOUNT OF ELEVATOR/AILERON DISPLACEMENT INCREASES WITH SPEED. VERIFIED THAT AIRCRAFT FLIGHT CONTROL SURFACES NEED MINOR RIGGING ADJUSTMENTS AFTER INSTALLING SURFACE CONTROL TRAVEL TOOLS. ADJUSTED RIGHT ELEVATOR NEUTRAL POSITION. ADJUSTED RIGHT AILERON NEUTRAL POSITION. ADJUSTED RUDDER NEUTRAL POSITION. CHECKED AILERON, ELEVATOR AND RUDDER CABLE TENSIONS. ALL FLIGHT CONTROL SURFACES ADJUSTED IAW THE CE-750 MM 27-30-00. COMPLIED WITH AACI OPS FLIGHT CHECK. WITH AIRCRAFT IN STRAIGHT AND LEVEL FLIGHT, CONTROL YOKES ARE LEVEL AND TRIM POSITION INDICATIONS ARE NEU2L72 4J RTT00007WI 20040902001932004090200193NE 2004 9 2 Y2PA04017 220040712A7230 COMPRESSOR AMD FALC20FALCON 2720302EU GE CF700 CF7002D 30010NE NR 1 ENGINE DAMAGED A Y2PAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL23816AA 290 304H207B DURING RVSM FLT TESTING, IN LEVEL FLT AT FL375, NR 1 ENG FLAMED OUT. CREW DECLARED EMERGENCY, DRIFTED DOWN & ENGINE RE-STARTED AT FL290 USING AIRSTAT CHECKLIST. A/C RETURNED TO YIP & LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED NR 1 ENG TO DETERMINE CAUSE OF FLAME OUT. COMPRESSOR WAS BORESCOPED & FOD DAMAGE FOUND IN 6TH STAGE. DAMAGE BLENDED IAW GE SEI-187 MM 72-32-0. NR 1 ENG ANTI-ICE LINE FOUND TO BE CRACKED & REPAIR WELDED IAW THE USA JET GMM VOL 3, CHP 51, PAGE 5. ENG GIVEN A COMPRESSOR WASH & RUN TO CHECK PARAMETERS & FOR LEAKS. ENG RUN & CHECKED GOOD. A/C TEST FLOWN & A 'MAXIMUM ALTITUDE ACCELERATOIN TEST' PERFORMED IAW GE SEI-187 MM. TEST FLT SATISFACTORY & A/C RETURNED TO SERVICE. (M) 2L72 4F4 F A7EU E7EA 20040902001942004090200194NM 2004 9 2 2004F00266 120040223A2720 SERVO VALVE AIRBUSA319 A319132 3930340NM RUDDER INOPERATIVE A RJEFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23473TA 1140 DURING CLIMB, EXPERIENCED A STRONG VIBRATION ALL OVER A/C. A/C RETURNED TO SAL STATION FOR MX. AFTER LANDING AT SAL STATION, TECHS PERFORMED TROUBLESHOOTING IAW TSM 05-50-00. FOUND 3 RUDDER SERVO CONTROLS & HINGE BEARINGS OUT OF LIMITS. THE 3 RUDDER SERVO CONTROLS WERE REPLACED AND TESTED AS PER AS PER AMM 27-24-51. THE NR 3 HINGE BEARING (P/N MS14101-9) WAS REPLACED AND TESTED AS PER AMM 55-36-41. ALL TEST RESULTS ON BOTH, RUDDER AND HINGE BEARING WERE FOUND NORMAL. A FLIGHT TEST WAS PERFORMED. NO VIBRATION WAS FELT ON CLIMB, CRUISE, DESCENT AND BANK STAGES OF THE FIGHT. AIRCRAFT WAS RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040902001992004090200199EU 2004 9 2 2004F00268 120040425A771210542N02W01 INDICATOR FOKKERF27 F27MK600 4990706EU TORQUE INOPERATIVE A COEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM13703FE 10420 DURNG POEWR ADVANCE ON TAKEOFF, NR 1 TORQUE INDICATOR SHOWED '0'. CREW ABORTED TAKEOFF ROLL AND RETURNED TO THE RAMP. MAINTENANCE REMOVED AND REPLACED THE TORQUE INDCIATOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20040902002012004090200201NM 2004 9 2 ASAA0410353 120040713A53306545744545 SKIN BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STATION 727B PLUS 12, 3 INCHES ABOVE STATION 18L. REPAIRED SKIN BLENDOUT ER 04-3115. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040831000572004083100057SO 2004 8 31 SWIA200413669 120040805A3350D36604001 POWER SUPPLY EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07294SW1567 1567 120321 EXIT ROW LIGHTS ROW 9 WILL NOT ILLUMINATE. REPLACED AFT ELBP BATTERY PACK WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040901000052004090100005EU 2004 9 1 AWXA200400736 120040706A3350321430 BATTERY AIRBUS320 A320232 3930326EU SEAT ROW 11 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28603AW 661 AFTER ENGINE SHUTDOWN EMERGENCY LIGHTS DID NOT ILLUMINATE. MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERIES AT THE L-1 DOOR AND AT SEAT ROW 11 RT DISCHARGED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT L-1 DOOR AND SEAT ROW 11 RT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040901000082004090100008EU 2004 9 1 AWXA200400739 120040612A5753 SKIN AIRBUS320 A320231 3930325EU TE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT IB FLAP AT IB END. MAINTENANCE CUTOUT DISBOND AREA ON UPPER SURFACE OF LT IB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW E.R. 26-5752-04178-ES3. 2L72 4F RTA28NM 20040901000122004090100012NM 2004 9 1 AWXA200400743 120040627A5315D5347217220400 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AFT OF FR 66 TO FORWARD SIDE OF FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 LT FROM FR 66 TO FR 68 IAW A319 SRM 51-42-11, FIG. 2, 3, & 18. 2L72 4F4 FRTA28NM E311NE 20040901000232004090100023NE 2004 9 1 WLDA200427 220040614A73204059025907 CONTROLLER DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUEL SYSTEM FAILED A WRLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11279WA 48756 FLIGHT NR WOA8743 ACCORDING TO THE FLIGHT CREW (ENGINE 1 FUEL PUMPS OFF) LEVEL ONE ALERT IMMEDIATELY AFTER POWER FOR TAKEOFF, CAPT DISCONTINUED THE TAKEOFF EXITED THE RUNWAY, SWITCHED FUEL CONTROLLERS THE FUEL SYSTEM OP'S NORMALLY, TAXIED BACK FOR A NORMAL TAKEOFF. THE ALERT REILLUMINATED DURING CLIMB OUT, PLACED FUEL TO MANUAL AND THEN RETURNED TO AUTO THE SYSTEM OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT, MX T/S THE SYSTEM, REMOVED AND REPLACED FUEL SYS. CONTROLLER AND CONTROLLER FILL VALVE. OP'S OK. 2L73 4F4 FRTA22WE E24NE 20040901000242004090100024EU 2004 9 1 AWXA200400709 120040630A2782830A000001 ACTUATOR AIRBUS320 A320231 3930325EU ZONE 512 BINDING A AWXAO OTHER J WARNING INDICATION APAPPROACH 1 WP28620AW47565 052 ON DESCENT, EN ROUTE RECEIVED A SLAT FLAP DISAGREE LIGHT WITH SLATS LOCKED OUT BETWEEN POSITIONS ZERO AND ONE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEADING EDGE STRUCTURE ATTACHMENT SCREW LOOSE AND PROTRUDING FROM SKIN AT NR 2 SLAT AREA AFFECTING EXTENSION OF SLAT. AS A RESULT, THIS ALSO CAUSED NR 2 SLAT (B) ROTARY ACTUATOR BYPASS PIN TO EXTEND. REPLACED ATTACHMENT SCREW, AND AS A PRECAUTION REPLACED NR 2 SLAT (B) ROTARY ACTUATOR, OPERATIONAL CHECK OF SLAT / FLAP SYSTEM WAS GOOD. 2L72 4F RTA28NM 20040901000262004090100026EA 2004 9 1 COMA0460438 120040804A5320 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01821CA 7420 CARGO BAY LANDING PLATE CRACKED. IAW REO 601R-53-61-1102. 2L72 4F4 FRTA21EA E15NE 20040901000432004090100043WP 2004 9 1 ABXA040262 120040717A5610 LATCH DOUG DC9 DC941 302207NWP PWA JT8 JT8D* NE COCKPIT WINDOW LACK OF LUBE A ABXAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23963AX 47780 ON TAXI IN, DISCOVERED FIRST OFFICER'S WINDOW WOULD NOT OPEN. OPENED WINDOW, CLEANED AND LUBED LATCHING MECHANISM. WINDOW CHECKED GOOD IAW MM 56-10-03-4. 2L72 4F4 F A6WE E2EA 20040901000452004090100045SO 2004 9 1 C2XA04SH465 120040722A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2724517 145332 DURING (C) CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 2 FIG. 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040901000562004090100056WP 2004 9 1 UPS04842880 120040702A53472772660 SEAT TRACK DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3 SEAT TRACK E HAS WORN SCALLOPS AND LUGS BETWEEN FS 1400 AND 1410. BLEND AREA IAW UPS SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3, CUT OUT DAMAGE ON SEAT TRACK IAW EO 5340-7779B. ALODINED AND PRIMED CUT AREA, MAT ID PLUG SEAT TRACK P/N 53B-007-002 PO S P0906208 AND CHANNEL SEAT TRACK P/N 53B-007-006 PO SP09768935. INSTALLED PLUG SEAT TRACK AND CHANNEL SEAT TRACK IAW SRM 51-3-0. 2L74 4F4 FRT4A25 1E8 20040901000672004090100067EU 2004 9 1 04FDEA02463 120040812A29133508806 PUMP AIRBUS300 A300B4622R 3930312EU PWA 4158 PW4158 NE HYDRAULIC SYS LEAKING A FDEAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25719FD 388 LOST NEARLY ALL GREEN HYDRAULIC QUANITY DURING CRUISE AT FL 290. FOUND LT HYD PUMP SHAFT SEAL LEAKING. REMOVED AND REPLACED LT OR FWD HYD PUMP ON NR 2 ENG ISW M/M 29-11-32-4-1, OPS AND LEAK CHECK, GOOD. 2L72 4F4 FRTA35EU E24NE 20040901000682004090100068GL 2004 9 1 YTRR095305 220040613A732023070613 FUEL CONTROL BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL ENGINE MALFUNCTIONED B YTRAO OTHER G MULTIPLE FAILURE NRNOT REPORTED 1 SW0352192 52192 COULD NOT SHUT DOWN AIRCRAFT AFTER THROTTLE WAS CLOSED. 1G71 3U3 UNCH2SW E1GL 20040901000732004090100073EU 2004 9 1 04FDEA02330 120040731A1420 CONNECTOR AIRBUS330 A300* EU GE CF6 CF680 30025NE NR 2 ENGINE DAMAGED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25664FE 768 ON TAKE OFF ROLL APPROX 60 KTS ECAM MOMENTARALY CAME ON. NR 2 ENG REV PRESSURIZED- INDICATION WENT OUT ABOUT 100 KTS AND CONTINUED NORMAL TAKE OFF. APPROX 800 AGL INDICATION RETURNED TO ECAM AND STAYED ON. PROCEDURE WAS FOLLOWED TO PULL NR 2 THROTTLE TO IDLE AND NOT USE IT FOR THRUST. FACT 31JUL04 16:27 ROC R ON INITIAL MEL PROCEDURES FOR NR 2 ENGINE THRUST REVERSER. BELIEVED ENGINE WAS PRE SB GE 78-1086 UPON FURTHER INSPECTION FOUND TO BE POST SB GE 78-1086 REMOVED AND STOWED SOLENOID AND PRESSURE SWITCH CONNECTORS AND SOWED IAW MEL PROCEDURE 78-30-01-A, OK FOR SERVICE. ENT BY: 034759 RPT BY: 034759 2L72 4F4 FRTA26NM E13NE 20040901000752004090100075NM 2004 9 1 04FDEA02383 120040806A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE, OB CORRODED.**** S/D COMING **** 2L73 4F RTA22WE 20040901000782004090100078NM 2004 9 1 QXEA200400578 120040807A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 100 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09357PH 504 SEA FLIGHT NR 2279 AUTOFEATHER DID NOT ARM DURING TAKEOFF. PERFORMED AUTOFEATHER CHECK IAW FSM 3-146. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040901000822004090100082NE 2004 9 1 HEEA096021 120040612A6797 WIRE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30 03013GL COLLECTIVE STICKDAMAGED E HEEAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW0322342 760096 NR 2 ENGINE N2 BEEP UNCONTROLLABLE CAUSING 30 PERCENT TORQUE SPLIT. RETARDED NR 2 THROTTLE TO A SETTING OF 38 PERCENT AND LANDED. MAINTENANCE FOUND BAD WIRING IN THE COPILOT COLLECTIVE STICK. REWIRED THE COLLECTIVE STICK AND REPLACED THE GOVERNOR SWITCH. 1G72 3U3 U H1NE E1GL 20040901000862004090100086NM 2004 9 1 SWAA042517 120040829A5310573149 WINDOW FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND COCKPIT L1 WINDOW POST UPPER OUTBOARD CORNER CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20040901000932004090100093NM 2004 9 1 SWAA042476 120040826A53156546811 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, RBL 16 TO LBL 16, CORRODED. REPAIRED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20040901001022004090100102WP 2004 9 1 UPS04843017 120040813A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C2, FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 120-160 UNDER ADF ANTENNA MOUNTING LOCATION AT LONG 36. REMOVED EXISTING DOUBLER AT NR 1 ADF ANTENNA, CUT OUT DAMAGE AT NR 2 ADF ANTENNA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER BETWEEN STATION 105 AND 170 BETWEEN LONGERON 34L AND 35R IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040901001042004090100104WP 2004 9 1 UPS04843021 120040820A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01880UP 46080 EMERGENCY LIGHTS WILL NOT CAME ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2. ALL OPS CHECK NORMAL. 2L74 4F RT4A25 20040901001062004090100106NM 2004 9 1 SWAA042519 120040829A53126516300 BULKHEAD BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SPV, FOUND BULKHEAD WEB AT BS 178, RBL 10, WL, 234, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20040901001072004090100107NM 2004 9 1 SWAA042520 120040829A53116516301 FRAME BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SPV, FOUND FRAME AT LEFT BS 188, WL 207, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040901001082004090100108NM 2004 9 1 SWAA042522 120040829A53116546546 SHEAR TIE BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 827, STRINGER 26L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040901001252004090100125NM 2004 9 1 SWAA042499 120040827A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 12R, CRACKED. REPAIRED SKIN PER ERO. 2L72 4F RTA16WE 20040901001292004090100129WP 2004 9 1 MWEA040155 120040824A533059530501 FINGER DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE PUNCTURED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 SMALL PUNCTURE IN FUSELAGE SKIN AT FRAME STATION 229 AND LONGERON 22 NEAR FORWARD LAVATORY SERVICE PANEL. CUT OUT DAMAGE AND INSTALLED FINGER DOUBLER AND PLUG. 2L72 4F A6WE 20040901001412004090100141NM 2004 9 1 SWAA042470 120040825A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 188, RBL 30 AND BS 188, LBL 30, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20040901001422004090100142NM 2004 9 1 SWAA042471 120040825A53206545833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 178 TO BS 196.5, LBL 24 TO LBL 28, CRACKED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2L72 4F RTA16WE 20040901001452004090100145WP 2004 9 1 ABXA040302 120040830A5320J0602289 PAN DOUG DC9 DC914 3022034WP CARGO DOORWAY CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 WHILE PERFORMING AN X-RAY OF THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB, FOUND THE LOWER DOOR JAMB PAN PRIOR SERVICE REWORK REPAIR CORRODED BEYOND LIMITS. REMOVED AND REPLACED SERVICE REWORK DOOR JAMB PAN P/N J060228-9 IAW DC-9 SRM 53-05. 2L72 4F A6WE 20040901001502004090100150NE 2004 9 1 P5CA0401183 220040828A7261M832481216 SEAL BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 1 ENGINE OIL LEAKING A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23921FT 21575 689169 DURING CRUISE, NR 1 ENG OIL QTY GRADUALLY DECREASED, OIL PRESSURE & TEMP NORMAL, CLOSELY MONITERED OIL QTY, WHEN ZERO OIL PRESSURE INDICATED, GAUGE FLUCTUATED & OIL PRESSURE LIGHT FLICKERED, SHUTDOWN ENGINE, ENGINE FAILURE / SHUTDOWN CHECKLIST ACCOMPLISHED. OIL PRESSURE STAYED 20-30 PSI AFTER SHUTDOWN. INSPECTED NR 1 ENG, FOUND NR 1 EDP DRIVE SHAFT SEAL DETERIORATED. REMOVED AND REPLACED SEAL, PERFORMED INSP PER 72-00-00 & PERFORMED EDP TEST PER AMM 29-11-05. 2L74 4F4 F A20WE E3NE 20040901001552004090100155NM 2004 9 1 SWAA042481 120040826A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 13L AT BS 470, CRACKED. REPAIRED STRINGER SECTION PER ERO. 2L72 4F RTA16WE 20040901001612004090100161 2004 9 1 SWAA042488 420040826A25656949956 CABLE BOEING737 7375H4 138449DNM ESCAPE SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C2 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDE CABLES MISROUTED. ROUTED R2 AND L2 DOOR EVAC SLIDE CABLES PER MM. 2L72 4F RTA16WE 20040901001742004090100174NM 2004 9 1 SWAA042512 120040828A53106545874 DOOR FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME FWD OF TORQUE TUBE ACCESS PANEL UPPER FASTENER HOLE, CRACKED. REPAIRED DOOR FRAME PER SRM. 2L72 4F RTA16WE 20040901001752004090100175EA 2004 9 1 SWIA200413718 120040818A2820 PUMP CNDAIRCL600 CL6002B19 1900309EA RT XFER EJECTOR OBSTRUCTED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07967SW 7872 SITTING ON GROUND, FUEL TRANSFERS FROM MAIN TANKS TO CENTER TANK. REMOVED OBSTRUCTION IN RIGHT TRANSFER EJECTOR PUMP. OPERATIONAL CHECK GOOD IAW 28-13-01. 2L72 4F RTA21EA 20040901001802004090100180WP 2004 9 1 DHL2004804521 120040714A53204641324 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 AFT FUSELAGE AFT LONGERON SPLICE FITTING CORRODED AT STA 1690.000, L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORRODED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040901001872004090100187EA 2004 9 1 SWIA200413719 120040818A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER/AILERON MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07964SW 7868 AILERON TRIM WOULD NOT TRIM RIGHT. REPLACED AILERON/RUDDER TRIM PANEL AS NEEDED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040901001892004090100189SO 2004 9 1 SWIA200413721 120040818A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM0758733 120197 WITH FLAPS SELECTED TO 45 DEGREES, RECEIVED CONTROL FAULT AND SWS ON MAP PANEL. REPAIRED WIRE AS REQUIRED AT LT NACELLE ACTUATOR CONNECTOR. REPLACED LEFT NACELLE FLAP ACTUATOR AND RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08 AND MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1007, S/N OFF 0170. 2L72 4T RTA31SO 20040901001962004090100196EA 2004 9 1 MASA200400456 120040816A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT DIRTY A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07922FJ 15022 ASH 6301 PHX. A RIGHT FWD EMERGENCY EXIT DOOR INDICATING OPEN WHEN DOOR WAS SHUT. MX REMOVED, CLEANED AND REINSTALLED PROXIMITY SENSOR. 2L72 4F RTA21EA 20040902000062004090200006WP 2004 9 2 DHL2004804515 120040625A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LEFT INNER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 641.250. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B PG 1. INSTALLED REINFORCING ANGLE IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040902000082004090200008WP 2004 9 2 DHL2004804501 120040624A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN, STA 1215.000. REMOVED DETERIORATED PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040902000142004090200014WP 2004 9 2 ABXA040281 120040724A5330 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DENT IN FUSELAGE SKIN AT STA 837, LONGERON 22 RIGHT, 11 INCHES LONG X .75 INCH WIDTH X .020 INCH DEEP. INSTALLED PERMANENT REPAIR IAW COI 47242-001. 2L72 4F A6WE 20040902000222004090200022WP 2004 9 2 DHL2004804524 120040709A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT BEAM WEB CRACK 2.500, STA 960.000 RBL 59 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-7-3 PG 17-18, DC8 SRM 51-2-0 PG 78, DC8 SRM 51-2-1 (TR 51-130) JAN 26-04 FIG 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (7075-T6 51 AL 0.200) IAW DC8 SRM 51-2-1 (TR 51-130) FIG 1, SHEET 1-6, 10-12. CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW DC8 SRM 51-2-1 (TR 51-130), DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040902000242004090200024SO 2004 9 2 CHQA000524 120040728A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 GL11294 145497 WITH COCKPIT EMERGENCY LIGHT SWITCH IN THE ARMED POSITION, ROWS 1-7 FLOOR EMERGENCY PATH LIGHTS AND GALLEY EMERGENCY EXIT LIGHTS CAME ON. AIRCRAFT WAS FERRIED FROM IAD TO IND FOR MAINTENANCE. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY ASSEMBLY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECKS GOOD. 2L72 4T RTT00011AT 20040902000322004090200032 2004 9 2 AWXA200400917 420040822A2565D30665105 SLIDE AIRBUS320 A320231 3930325EU L-2 DOOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW268982396 091 PHX - EES - DURING 4-DAY CHECK THE L-2 DOOR SLIDE FAILED EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE, EMERGENCY LIGHT TEST WAS GOOD. 2L72 4F RTA28NM 20040902000362004090200036EU 2004 9 2 AWXA200400921 120040813A5340D534710870000 ATTACH FITTING AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK A .375 INCH CRACK WAS FOUND ON FR 68 TO FLOORBEAM Y1792 LT CONNECTING SECTION. MAINTENANCE REMOVED CRACKED FLOORBEAM TO FRAME CONNECTING SECTION; FABRICATED A NEW REPLACEMENT CONNECTING SECTION PER DWG 17D53471087; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040902000372004090200037NM 2004 9 2 WLDA200478 120040802A5512ALC8101503 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 14. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STABILIZER LEFT BARREL NUT HOLE NR 14 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040902000482004090200048WP 2004 9 2 MWEA040150 120040824A5320991555415 INTERCOSTAL DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 CORROSION ON INTERCOSTAL AT FRAME STATION 775 BETWEEN LONGERON 27 AND 28 LEFT. FABRICATED AND INSTALLED INTERCOSTAL. 2L72 4F A6WE 20040902000502004090200050NE 2004 9 2 MWEA040152 220040824A7200BR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE RIGHT VIBRATION A MWEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL31902ME 55166 RIGHT ENGINE HIGH VIBRATION ALERT. INSPECTED RIGHT ENGINE, NO DEFECTS FOUND. PERFORMED POWER ASSURANCE CHECK, SATISFACTORY. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FTRA6WE E00061EN 20040902000522004090200052WP 2004 9 2 DHL2004805007 120040713A2612 WARNING LIGHT DOUG DC8 DC873F 302199FWP NR 1 FIRE WARN ILLUMINATED A DHLAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO01805DH 46125 WHILE EN ROUTE NR 1 ENGINE FIRE DETECTION SYSTEM ACTIVATED. 2L74 4F RT4A25 20040902000592004090200059NM 2004 9 2 CALA0400606 120040819A215020405011 ACM BOEING737 7373T0 1384582NM A/C PACK BAY LEAKING A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW271432415612 23375 A FLIGHT ATTENDANT COMPLAINED OF SMOKE IN THE AFT CABIN AFTER TAKEOFF. THE AIR CONDITIONING SYSTEM HAD BEEN OCCASIONALLY GIVING OFF A SMOKY ODOR WHEN UNDER HIGH COOLING LOAD. THE ODOR DISSIPATED QUICKLY WHEN A HIGHER TEMPERATURE WAS SELECTED. THE FLIGHT WAS CONTINUED TO ITS ORIGINAL DESTINATION OF CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE LT ACM LEAKING. THE LT ACM WAS REMOVED AND REPLACED IAW MM 21-51-11. A BURNOUT WAS PERFORMED AFTER THE ACM REPLACEMENT. LEAK AND OPERATIONAL CHECKS WERE GOOD WITH NO ODORS DETECTED. 2L72 4F RTA16WE 20040902000622004090200062WP 2004 9 2 UPS04842831 120040801A5310 STRUCTURE DOUG DC8 DC871F 302199DWP RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 CORROSION IN RIGHT MLG WHEEL WELL. REMOVED CORROSION FROM RMLG W/2 PANEL. UT AREA FOUND MIN MATERIAL TO BE .048" THICK. PERFORMED HFEC INSP NO CRACKS FOUND. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5330-20826. DEFERRAL D285269 ASSIGNED AWAITING CLOSING LP AND CLOSING DEFERRAL. 2L74 4F RT4A25 20040902000632004090200063 2004 9 2 UPS04M42832 420040801A34521751780010004 TRANSPONDER DOUG MD11 MD11F 3023600NM E/E BAY ATC INOPERATIVE A IPXAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 SO01254UP INSPECTION TYPE:N/A, DIVERSION - BOTH ATC TRANSPONDER MODE C FUNC INOP. ATC REQUIRED DIV TO STN. *S/D* SWAPPED POSITIONS OF ATC TRANSPONDERS IAW 34-54-01. PERFORMED BITE CHECK ON BOTH ATC TRANSPONDERS CHECKED OK AS PER AMM 34-54-00 (OPERATIONAL TEST) POSITIONS OF X-PONDERS ATC 2 P/N 7517800-10004. 2L73 4F RTA22WE 20040902000662004090200066NM 2004 9 2 UPS04242852 120040702A5753 SKIN BOEING727 72725C 138400HNM LT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, CRACK ON I/B MID FLAP LOWER T/E SKIN AT I/B AFT FLAP ACTUATING ROD CUTOUT O/B AFT CORNER (LT). HFEC CONFIRMED CRACK AND MARKED END. DAMAGED AREA TRIMMED OUT IAW SRM 51-10-1. REPAIR CARRIED OUT IAW AAAE EO 2004-068-006. 2L73 4F A3WE 20040902000702004090200070NM 2004 9 2 UPS04242858 120040629A5752 SKIN BOEING727 72725C 138400HNM RT AILERON TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED ON UPPER SKIN AT INBOARD END AND OUTBOARD END. AILERON TAB REMOVED IAW MM 27-10-19. DAMAGE REPAIRED IAW SRM 51-40-20, AILERON TAB REINSTALLED IAW MM 27-10-19. 2L73 4F A3WE 20040902000732004090200073 2004 9 2 DHL2004783011 420040716A3442 RADAR BOEING727 727227 1384078NM WX RADAR SYS INOPERATIVE A DHLAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO01783DH 21999 RADAR INOP, FALLS OFF LINE. 2L73 4F A3WE 20040902000812004090200081 2004 9 2 SWAA042452 420040824A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVACUATION SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE CLIP BRACKET & SLIDE ASSY PER MM. 2L72 4F RTA16WE 20040902000832004090200083NM 2004 9 2 UPS04242760 120040705A5420 WEB BOEING727 72725C 138400HNM NR 2 ENG SUPPORTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE:C, CENTER ENGINE SUPPORT STRUCTURE, WEB CRACKED ON RT SIDE AT BS 1387. WEB REMOVED IAW SRM 51-30-02. WEB FABRICATED PER DRAWING 65-17555. WEB INSTALLED PER DRAWING 65-17555. 2L73 4F A3WE 20040902000862004090200086NM 2004 9 2 UPS04442748 120040709A5313 STRINGER BOEING747 747200 1384847NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C M/D - STA 2183 TO 2184 RIGHT NR 11 STRINGER END FOUND CRACKED. M/D STA 2183 TO STA 2184 RIGHT NR 11 CRACKED STRINGER REPAIRED AS PER SRM 53-10-03 FIGURE 4. 2L74 4F RTA20WE 20040902001032004090200103WP 2004 9 2 UPS04842846 120040719A5313 LONGERON DOUG DC8 DC873F 302199FWP AFT CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 STATION 1735 LONG 15R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 10 BETWEEN STATION 1720 TO 1766. 2L74 4F RT4A25 20040902001112004090200111EU 2004 9 2 AWXA200400931 120040805A5320D53475515256 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL PLATE BETWEEN FR 53 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL PLATE FROM FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT SILL PLATE PER DWG D53475575; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040902001222004090200122WP 2004 9 2 ASAA0480372 120040509A33500105610 MODULE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01975AS 53451 PDX - FOUND DURING CHECK, EMERGENCY TRACK LIGHTS INOPERATIVE AT ROWS 26-29. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001302004090200130WP 2004 9 2 ASAA0480434 120040514A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01947AS 53020 OKC - DURING C-CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001352004090200135EU 2004 9 2 ASOA04545 120040713A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE LEFT INBOARD SEAT TRACK BETWEEN FRAME 29 AND FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD SEAT TRACK BETWEEN FRAME 29 AND FRAME 36 IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20040902001382004090200138EU 2004 9 2 ASOA04547 120040713A5320 SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT BOTTOM WALL SUPPORT BETWEEN FRAME 16 AND FRAME 17, RBL 14 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT BOTTOM WALL SUPPORT BETWEEN FRAME 16 AND FRAME 17, RBL 14 IAW SRM 51-25-00 AND 51-25-01. (M) 2H72 4T RTA53EU 20040902001412004090200141SO 2004 9 2 2004F00252 120040112A4920 SCROLL GULSTMG1159 GIV 3980115SO APU ENGINE CRACKED A E7JAK NONE O OTHER ININSP/MAINT 1 NE03403QS 1403 DURING SCHEDULED MAINTENANCE, FOUND 3 INCH CRACK ON TURBINE SCROLL P/N 384600-9. APU REMOVED FOR REPAIR S/N P816. (M) 2L72 4F RTA12EA 20040902001442004090200144SO 2004 9 2 2004F00255 120040127A2752 ACTUATOR GULSTMG1159 G1159 3953505SO RT WING TE FLAP FAILED A O2GAA UNSCHED LANDING F FLT CONT AFFECTED LDLANDING 1 NE03524MM 85 FLAP FAILED TO EXTEND. REPLACED FLAP ACTUATOR DUE TO ASSYEMETRY GEAR FAILURE. (M) 2L72 4F RTA12EA 20040902001472004090200147WP 2004 9 2 ASAA0480452 120040526A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT MISINSTALLED A ASAAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 NM01961AS 53075 SEA - FOUND DURING PREFLIGHT, COCKPIT OVERHEAD FLOOD LIGHT FOUND INOPERATIVE UPON TEST. REROUTED MIS-CONNECTED FLOOR LIGHT WIRE. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001662004090200166NM 2004 9 2 USAA040369 120040719A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSLAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AT RIVET OUTBOARD OF RBL 57 AT WL 234 STATION 178 BULKHEAD. INSTALLED DOUBLER PER EO 5300V153. (M) 2L72 4F RTA16WE 20040902001682004090200168NM 2004 9 2 USAA040366 120040802A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55256 22956 PIT - FOUND SKIN CRACKED 1.5 INCH, STRINGER 21R STATION 757. CUTOUT DAMAGE, INSTALLED DOUBLERS PER SRM 53-00-01, FIG 229, DETAIL VII. (M) 2L72 4F RTA16WE 20040902001702004090200170NM 2004 9 2 USAA040379 120040721A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH AREA, FS 990, STATION 21, LEFT. FABRICATED NEW INTERCOSTAL PER 51-40-02. CORROSION LEVEL 1, TASK NR C53-202-01. (M) 2L72 4F RTA16WE 20040902001752004090200175EU 2004 9 2 ASOA04553 120040714A5330 SKIN AEROSPATR72 ATR72212 8680945EU FUSELAGE DENTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, A DENT IN THE LOWER FUSELAGE AT FS 10, NEAR STRINGER 21R WAS FOUND TO BE BEYOND LIMITS. MAINTENANCE REPAIRED THE SKIN AT FR 10, NEAR STRINGER 21R IAW SRM 53-00-00. (M) 2H72 4T RTA53EU 20040902001972004090200197NM 2004 9 2 ASAA0480279 120040416A1420 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01979AS 53471 LAX - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHT WERE FOUND INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED CONNECTOR AT ROW 2. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040902002022004090200202SO 2004 9 2 SIMA200422404 120040726A531514525381003 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21727AE 145326 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20040902002042004090200204SO 2004 9 2 SIMA20040901 120040726A3320BR900022 BALLAST EMB 135 EMB135LR 3260305SO LAV LIGHT INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21711PH 145235 RDU - FLT 4624 - CREW REPORTED WHILE ON THE GROUND THE LAVATORY SMOKE DETECTOR WENT OFF WITHOUT ANY VISUAL INDICATION OF SMOKE. THERE WAS A STRONG BURNING ODOR IN LAVATORY. MAINTENANCE REMOVED AND REPLACED A BALLAST CONVERTER IN LABATORY IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040902002062004090200206EA 2004 9 2 ASOA04452 120040625A1420M8372395R1005N CONNECTOR CNDAIRCL600 CL6002B19 1900309EA ENGINE LOOSE A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11834AS 7254 DURING CLIMB-OUT, JUST PRIOR TO LEVELING OFF AT 23,000 FT, GOT A TRIPLE CHIME MASTER WARNING FOR RT ENG LOW OIL PRESS WHICH IMMEDIATELY VANISHED BUT REPEATED A FEW MIN LATER. OIL PRESS STARTED TO FLUCTUATE BETWEEN 25 & 39 PSI, RT ENG LOW OIL PRESS MESSAGE INTERMITTENT YET FREQUENT. ENG SECURED. EMERGENCY DECLARED & DIVERT. SINGLE ENG LANDING PERFORMED WITHOUT INCIDENT. MX R & R RT ENG. UPON REMOVAL MX FOUND LOWER ENG COWL OIL SOAKED. SERVICED ENG WITH 5 QTS OF OIL. MX ALSO FOUND CONNECTOR ON OIL PRESS TRANSMITTER LOOSE. ENG RAN ON DELTA'S TEST CELL WITH NO LEAKS OR OIL CONSUMPTION. UPON ENG TEAR DOWN MX FOUND SEVERAL AGB CARBON SEALS LEAKING & REPLACED. OPS CHECKS GOOD. ENG RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20040903000022004090300002NM 2004 9 3 2004F00273 120040617A2750106081917 SWITCH BOEING727 727212 138407GNM NR 1 LE FLAP WORN A PCSAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO17598AJ 21947 AFTER TAKEOFF, NR 1 LEADIGN EDGE DEVICE WILL NOT RETRACT FLAP. AIRCRAFT DIVERTED BACK TO MDSD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 LEADING EDGE FLAP SWITCH PER B727 MM 27-82-1 AND OPERATION CHECK GOOD IAW B727 MM 27-82-0. AIRCRAFT WAS RETURNED BACK TO SERVICE. (M) 2L73 4F A3WE 20040903000032004090300003NM 2004 9 3 C7WA200400036 120040630A5330 SKIN BOEING727 7272J7 138400ENM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17128NA 20879 FOUND FUSELAGE SKIN CORRODED STRINGER 17 LT STATION 1183. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3A. REPAIR DOUBLER FABRICATED FROM 2024-T3, .080 BY 17 BY 11.80. (M) 2L73 4F A3WE 20040903000062004090300006EU 2004 9 3 USAA040429 120040806A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US15460 1052 CLT - FOUND FLOORBEAM WITH CORROSION 5 SQUARE INCHES BY .35 INCH AREA, FRAME 66-68. INSTALLED DOUBLER PER EA 95742. (M) 2L72 4F RTA28NM 20040903000072004090300007EU 2004 9 3 USAA040430 120040806A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US15460 1052 CLT - FOUND FLOORBEAM CORRODED 2 SQUARE INCHES BY .043 INCH AREA, FRAME 66Y 1292. INSTALLED DOUBLER PER EA 95743. (M) 2L72 4F RTA28NM 20040903000082004090300008NM 2004 9 3 C7WA200400015 120040428A1420MS242G4R18B31S8 CONNECTOR BOEING737 737231 1384079NM HYD SYSTEM BURNED A C7WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO1754354 21986 DURING CLIMB-OUT, NR 1 BLEED AIR TRIP LIGHT CAME ON WITH COCKPIT DUCT OVERHEAT LIGHT AND ANTI-ICE DUCT OVERHEAT LIGHT CAME ON ALL SIMUTANEOUSLY. CABIN PRESSURE WAS UNCONTROLLABLE. PERFORMED EMERGENCY DESCENT. PACK VALVE C/B POPPED, NR 2 BLEED AIR VALVE C/B POPPED. NR 2 ENGINE ANTI-ICE C/B POPPED. NR 1 ENGINE HYDRAULIC PUMP SYSTEM A LOW PRESSURE LIGHT CAME ON. HYDRAULIC QUANTITY DROPPED TO ZERO PRESSURE REMAINED NORMAL. HYDRAULIC SYSTEM 'A' FAILURE PROCEDURE ACCOMPLISHED FOR LANDING. ALT FLAP EXTENSION AND MANUAL GEAR EXTENSION PERFORMED. RETURNED TO DAYTON. FOUND CONNECTOR D4164 AND 1183 BULKHEAD SHORTED & BURNED ALL 31 PINS. REMOVED AND REPLACED D4164S AND D4164P AND ASSOCIATED PINS/SOCKETS. (M) 2L72 4F RTA16WE 20040903000112004090300011NM 2004 9 3 AMTA200400979 120040804A3411 PITOT HEAD BOEING757 75733N 1384931NM PITOT/STATIC MISSING A AMTAO OTHER D INFLIGHT SEPARATION DEDESCENT 1 GL11550TZ 32584 FOUND RT ENGINE EPR AND N1 FLUCTUATED SLIGHTLY AT THE TOP OF DESCENT. FOUND MISSING PF RAKE PITOT HEAD INBOARD SIDE PERFORMED TEMP REPAIR PER AMM 77-11-04-2. RAN ENGINE AT VARIOUS POWER SETTINGS NO FLUCTUATION NOTED AT THIS TIME. (M) 2L72 4F RTA2NM 20040903000142004090300014NM 2004 9 3 ASAA0480195 120040320A3397 WIRE DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01982AS 53473 PDX - FOUND TWO EMERGENCY TRACK LIGHT INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED, REPAIRED WIRING, LOOSE CONNECTOR WIRE. LIGHT THEN OPERATED PROPERLY. (M) 2L72 4F RT 20040903000162004090300016NM 2004 9 3 ASAA0440098 120040405A33978100022601 WIRE BOEING737 7374S3 1384711NM EMERGENCY LIGHT BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01786AS 24795 WHILE CLEARING MEL FOR MISSING LENS FOR THE FLOOR TRACK LIGHTING AT ROW 10, FOUND TRACK LIGHTING INOPERATIVE, ROWS 13-16 AND ROWS 21-23. REPAIRED BROKEN WIRES. (M) 2L72 4F RTA16WE 20040903000172004090300017 2004 9 3 AMTA200400481 420040425A2565 WARNING LIGHT BOEING757 75723N 1384973NM GIRT BAR ILLUMINATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11526AT 30735 GIRT BAR ENGAGEMENT LIGHT ILLUMINATED WITH EVACUATION SLIDE ARMING LEVER IN DISARM POS AT ENTRY DOOR 2R. (M) 2L72 4F RTA2NM 20040903000182004090300018NM 2004 9 3 USAABB04062 120040704A3350210310005 FUSE BOEING757 7572B7 1384964NM R4 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19622AU 27201 PIT - FOUND R4 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE M736 POWER SUPPLY. (M) 2L72 4F RTA2NM 20040903000192004090300019 2004 9 3 UIEA200400082 420040426A34604052508952 FMC BOEING747 74747UF 1384949NM FLT MANAGE INOPERATIVE A UIEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA15499MC 29260 FLT 605 - JFK - REMOVED AND REPLACED RIGHT FMC PER MM 34-61-01. INSTALLED FMC SOFTWARE PER MM 34-61-00 SYSTEM, OPS CHECK NORMAL PER MM 34-61-60/501. (M) 2L74 4F RT1384945 20040903000222004090300022NM 2004 9 3 UIEA200400139 120040802A323026702885 SEQUENCE VALVE BOEING747 7472D3B 1384805NM NLG MALFUNCTIONED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15505MC 21251 AFTER TAKEOFF, ON GEAR RETRACTION NOSE LANDING GEAR DOOR KEPT CYCLING. ATTEMPTED RE-CYCLE NO EFFECT. REMOVED AND REPLACED NOSE GEAR OPERATED DOOR SEQUENCE VALVE PER MM 32-34-08. PAGE 401-405 OPS AND LEAK CHECK NORMAL. (M) 2L74 4F RTA20WE 20040903000232004090300023NE 2004 9 3 2004F00275 220040720A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LEFT FIRE A SIMAFED ACTIVATE FIRE EXT. ENGINE SHUTDOWN RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 SW21322AC 320 127089 DURING TAXI, LEFT ENGINE FIRE INDICATOR ILLUMINATED, FIRE EXTINGUISHER DISCHARGED. REPLACED ENGINE. WAITING FOR TEARDOWN REPORT. (M) 2H72 4T4 TRTA53EU E20NE 20040903000262004090300026EU 2004 9 3 2004F00276 120040728A2910S2918056203200 LINE AEROSPATR42 ATR42300 8680920EU HYD SYSTEM LEAKING A SIMAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SW21141AE 141 DURING TAXI, THE GREEN SYSTEM LOW LEVEL LIGHT CAME ON THEREFORE, NO BRAKING ACTION. FOUND HYDRAULIC LINE WITH PIN HOLE. REPLACED METERING VALVE LINE. (M) 2H72 4T RTA53EU 20040903000282004090300028NM 2004 9 3 ASAA0410355 120040713A53006573742 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED WINDOW POST. INSTALLED DOUBLER AFTER STOP DRILLING. (M) 2L72 4F RTA16WE 20040903000292004090300029SO 2004 9 3 SIMA200421901 120040805A27503631001007 FCU EMB 135 EMB135LR 3260305SO TE FLAPS INOPERATIVE A SIMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SW21731BE 145356 FOUND FLAP FAIL MESSAGE. FLAPS STUCK IN FULL UP POSITION. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPERATIONAL CHECK OF FLAP CONTROL SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040903000302004090300030EA 2004 9 3 A6WA200440109 120040805A5743601R272100321 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31439AW 7753 FOUND LEFT MLG AFT TRUNNION BUSHING MIGRATED .006 NCH. REMOVED MIGRATED BUSHING. REAMED TRUNNION LUG BORE TO 1ST OVERSIZE AND INSTALLED 1ST OVERSIZE BUSHING IAW REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20040903000352004090300035EU 2004 9 3 ASOA04542 120040712A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FRAME 36 AND FRAME 38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 36 AND FRAME 38 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040903000372004090300037NM 2004 9 3 AMTA200400984 120040804A5315 FLOORBEAM BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND GALLEY G1B FLOOR BS 370-BS 370 RBL 58 TO BL 0 CORROSION. REMOVED AND REPLACED DAMAGED SECTION OF FLOORBEAM AT FS 365, RBL 9 TO RBL 69 IAW B757 SRM 53-00-51-2, FIG 203 AND 51-40-2. (M) 2L72 4F RTA2NM 20040903000382004090300038 2004 9 3 USAASA04078 420040805A2565D31517113 SLIDE AIRBUSA319 A319112 3930323EU RT DOOR DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19750UW 1315 DCA - THE AFT RIGHT DOOR SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE AFT RIGHT DOOR SLIDE ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040903000402004090300040NM 2004 9 3 AMTA200400989 120040804A5330 STRAP BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND CORROSION ON AFT CARGO DOOR CUTOUT LOWER INNER STRAP. REMOVED AND REPLACED STRAP IAW B757 SRM 51-40-02. (M) 2L72 4F RTA2NM 20040903000412004090300041EU 2004 9 3 ASOA04552 120040714A5753S5751203220300 RIB AEROSPATR72 ATR72212 8680945EU RT TE FLAP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 6 FOR THE CAM GUIDE NR 4 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND EPLACED THE RIGHT INBOARD FLAP LEADING EDGE PICKUP RIB NR 6 FOR THE CAM GUIDE NR 4 IAW SRM 51-25-03 AND 51-25-01. (M) 2H72 4T RTA53EU 20040903000422004090300042 2004 9 3 AMTA200400999 420040805A2565 GIRT BAR BOEING757 75723N 1384973NM L4 DOOR SLIDE CONTAMINATED A AMTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL11524AT 30233 FOUND 4L DOOR WILL NOT DISARM ALL THE WAY. REMOVED DEBRIS FROM GIRT BAR LATCH AREA, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040903000432004090300043NM 2004 9 3 USAA040384 120040720A5311 FRAME BOEING757 7572B7 1384964NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19623AU36152 27244 CLT - FOUND FRAME DENTED AT STATION 1400 FRAME LBL 2B. INSTALLED REPAIR ANGLE, TRIMMED OUT DENT AREA PER EA 95691. (M) 2L72 4F RTA2NM 20040903000442004090300044NM 2004 9 3 ASAA0410354 120040713A53306545744545 SKIN BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND SKIN BLENDOUT IS OUT OF LIMITS AT STAITON 727B 1 INCH BELOW STATION 17L. FINAL REPAIR WILL BE ON MIG 5-NR 4844359. (M) 2L72 4F RTA16WE 20040903000472004090300047NE 2004 9 3 AMTA200400022 220040106A73207898301 TRANSMITTER BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT ENGINE EEC MALFUNCTIONED A AMTAO OTHER J WARNING INDICATION CRCRUISE 1 GL11558TZ 32592 31858 JUST PRIOR TO DESCENT FL310 LEFT ENGINE SURGED ALL PARAMETERS. PERFORMED ENGINE RUN IAW MM 71-00-00. AT HIGHER POWER SETTINGS EEC UNLATCHED ENGINES REMAINED EVEN. EEC LATCHED BOTH ENGINES REMAINED EVEN. NO FAULTS NOTED WITH LEFT ENGINE. (M) 2L72 4F4 FRTA2NM E12EU 20040903000492004090300049NM 2004 9 3 SWAA042541 120040831A3350101073 LENS BOEING737 7373K2 13844BANM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29340LV 23738 FWD EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040903000502004090300050 2004 9 3 SWAA042542 420040831A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040903000522004090300052 2004 9 3 SWAA042544 420040831A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29462WN 32466 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040903000542004090300054NM 2004 9 3 SWAA042546 120040831A55116547507 RIB BOEING737 7373H4 1384600NM HORIZONTAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SPV, FOUND LT HORIZONTAL STAB LOWER RIB CHORD AT STATION 120, CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB RIB CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040907000032004090700003NM 2004 9 7 SWAA042554 120040831A53106545871 DOOR FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME AT 3RD STOP, CRACKED. REPAIRED DOOR FRAME PER SRM. 2L72 4F RTA16WE 20040907000042004090700004NM 2004 9 7 SWAA042555 120040831A5310 STRUCTURE BOEING737 7375H4 138449DNM DOOR FRAME CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE BOX FITTING CUTOUT AT LOWER CORNER, CRACKED. REPAIRED HINGE BOX FITTING PER EA. 2L72 4F RTA16WE 20040907000052004090700005NM 2004 9 7 SWAA042556 120040831A533065C323593 SKIN BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 467, BETWEEN STRINGER 28L AND STRINGER 28R, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040907000062004090700006NM 2004 9 7 SWAA042540 120040831A335020131 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29300SW 22940 AFT CENTER AISLE EMERGENCY EXIT LIGHTS ERRATIC. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040907000092004090700009NM 2004 9 7 SWAA042482 120040826A531069353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 360, STRINGERS 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20040907000102004090700010NM 2004 9 7 VNAA0408014 120040824A36004068B000002 VALVE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE BLEED AIR FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07439JS2990 3057 DURING CLIMBOUT, THE CREW RECEIVED A RT LOW PRESSURE VALVE FAILED INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LOW PRESSURE VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040907000112004090700011NM 2004 9 7 VNAA0408015 120040829A24201180001 GCU DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LEFT FAILED A VNAAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 GL07424JS23139483 3033 DURING TAKEOFF, THE CREW RECEIVED A LT GENERATOR FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE LT GENERATOR CONROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-31-03. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 20040907000122004090700012NM 2004 9 7 UPS04M42919 120040529A5512 PANEL DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C, LT HORIZONTAL STAB NR 1 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING S/W SURFACE. HOLE LT NR 01 BARREL NUT, REAMED TO 1.549 INCH PER MD11-5510-19409-G & MAT REMOVED 0.040 INCH DEEP K 0.450 INCH FOUND OUT LIMIT. FAB & REPAIR CUTOUT SLEEVE BUSHING PER EO MD11-5510-19409-G.PR 1422B2 SEALANT APPLIED PER EN1184-0 4. REPAIR & INSTALLED BUSHING SLEEVE PER EN:1181-04 & EO MD11-5510-1940 9-G. FOUND SATISFACTORY, WITHIN LIMIT. 2L73 4F RTA22WE 20040907000132004090700013NM 2004 9 7 UPS04M42728 120040616A71602242101567 SKIN DOUG MD11 MD11F 3023600NM NR 1 INLET COWL SEPARATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP INSPECTION TYPE:C2 NR 1 ENGINE NOSE COWL INTERNAL RIB IS SEPARATED FROM SKIN APPROX 4 TO 8 O'CLOCK POSITION. REMOVED AND REPLACED INLET COWL IAW M/M 71-11-01. 2L73 4F RTA22WE 20040907000142004090700014NM 2004 9 7 UPS04M42729 120040616A7160 SKIN DOUG MD11 MD11F 3023600NM NR 2 ENG INLET CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP INSPECTION TYPE:C2, NR 2 ENGINE INLET EXTERIOR UPPER RIGHT SEGMENT HAS 3 CRACKS AT FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 54-10-00 AND DWG PLAJC8311. 2L73 4F RTA22WE 20040907000172004090700017WP 2004 9 7 UPS04842744 120040614A53205615180591 FLOOR SUPPORT DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, MAIN CARGO AREA STA 25 RT SIDE CUSP MEMBRANE HAS CORROSION. REMOVED 2 FITTINGS FROM FS 25, REMOVED FLOOR SUPPORT ANGLES, REMOVED WEB, REMOVED CUSP ANGLES. FABBED CUSP ANGLES IAW DAC DWG 5615180. ALODINED & PRIMED. INSTALLED SUPPORT ANGLE, 2 ANGLE, FLOOR SUPPORT ANGLE, WEB IAW DC8 SRM 51-1-21, 51-20D, 51-3-0, 51-3-1. TWO FITTING FS 25 REMOVED FOM REPLACED ON UPS NR 712495 141495. 2L74 4F RT4A25 20040907000192004090700019WP 2004 9 7 UPS04842746 120040614A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, FWD PIT STA 270 TORQUE BOX ATTACH FITTING HAS CORROSION BETWEEN L33R AND L34R. REMOVED CORRODED FITTING, LOCATE NEW FITTING AND DRILL EXISTING FASTENER HOLES FAB REPAIR ANGLES, LOCATE, DRILL, FASTENER HOLES, TRIM ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND 51-1-21, 51-3-2. INSTALLED FITTING AND REPAIR ANGLES IAE DC8 SRM 51-1-21 AND 53-2-0. 2L74 4F RT4A25 20040907000222004090700022NM 2004 9 7 UPS04M42763 120040701A5347S49291477075T SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP INSPECTION TYPE:C STA Y 755 TO 859 X=-27.50 SEAT TRACK FOUND CORRODED. CORROSION AT SEAT TRACK STA Y755-859 AT X=-27.50 REMOVED FOUND EXCEED LIMIT. ORI THK=0.08 INCH & THK REMAIN=0.041 INCH. NEW SEAT TRACK & SPLICE FAB & INSTALLED PER SRM 53-70-00 F1, V1, REV 35, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040907000232004090700023NM 2004 9 7 WLDA200486 120040802A5350AKC75413 SKIN DOUG MD11 MD11 3023602NM TAIL CONE SCRATCHED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK IN TPE, WHILE PERFORMING J/C D929720 FOUND DAMAGE ON EXTENDED TAIL CONE LEFT LOWER SKIN AT BS STA 2176. PERFORMED REPAIR TO THE EXTENDED TAIL CONE LEFT LOWER SKIN PER EGAT EI W2004A53B. CONDITION CHECK SATISFACTORY. 2L73 4F RTA22WE 20040907000252004090700025NM 2004 9 7 UPS04M42921 120040611A5512 PANEL DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, RT HORIZONTAL STAB NR 1 BARREL NUT HOLE FOUND CORRODED. CORROSION AT ABOVE MENTION LOCATION REMOVED & REAMED TO 1.562 INCH & BLENDED FOUND OUT LIMIT. REPAIR SLEEVE BUSHING & FAB PER EO MD11-5510-19409-G APPLIED SEALANT PR1422B2 PER EN:1208-04. REPAIR & INSTALLED SLEEVE BUSHING AT NR 01 BARREL NUT RT AS EO MD11-5510-19409-G & EN:1208-04, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040907000262004090700026NM 2004 9 7 UPS04M42922 120040529A5512 PANEL DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C, HORIZONTAL STAB NR 30 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDEWALL SURFACE POSITION RT. CORROSION REAMED TO 1.178 INCH & BLEND TO 0.040 INCH FOUND OUT OF LIMIT. REWORKED CUTOUT AT NR 30 HOLE B/N RT AS PER EN:1175-04 & EO MD11-5510-194 09-G, FAB & REPAIR SLEEVE BUSHING. APPLIED PR 1422B2 SEALANT AT HOLE NR 3 0 B/N. REPAIR & INSTALLED AS PER EN1175-04 & EO MD11-5510-19409-G. 2L73 4F RTA22WE 20040907000302004090700030NM 2004 9 7 AWXA200400909 120040818A3397BMS13311122 WIRE BOEING737 73733A 1384673NM SEAT ROW 21 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28175AW 23634 DURING 4-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040907000322004090700032EU 2004 9 7 AWXA200400911 120040805A5320D5311209420300 WEB AIRBUS320 A320231 3930325EU FUSLAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB Y1546 RT AT FR 16. MAINTENANCE REMOVED AND REPLACED DAMAGED WEB Y1546 RT AT FR 16 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000332004090700033EU 2004 9 7 AWXA200400912 120040810A5321D53672023200 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK FOUND 3 EACH DELAMINATED AREAS ON AFT CARGO FLOOR PANEL 151GF. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 151GF FROM Y765 LT TO Y765 RT, FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20040907000362004090700036NM 2004 9 7 UPS04M42721 120040423A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C, SEAT TRACK FOUND CORRODED AT B STA 899-919 RBL 8.5. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH, THK REMOVED 0.024 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 VOL 1 REV 34. CORRODED SEAT TRACK CUTOUT AT STA 869-949 RBL 8.5 PER SRM 53-70-00 VOL 1 REV 34. NEW SEAT TRACK, SPLICE & SPLICE PLATE FABRICATED & INSTALLED PER SRM 53-70-00 VOL 1 REV 34. 2L73 4F RTA22WE 20040907000372004090700037NM 2004 9 7 UPS04M42722 120040423A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, SEAT TRACK FOUND CORRODED AT B STA 899-909 LBL 8.5. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH, THK REMOVED 0.018 INCH FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL 1 REV 34. CORROSION SEAT TRACK CUTOUT AT STA 869-929, LBL 8-5 AS PER SRM 53-70-00 VOL 1 REV 34. NEW SEAT TRACK, SPLICE & SPLICE PLATE FABRICATED AS PER SRM 53-70-00 VOL 1 REV 34. 2L73 4F RTA22WE 20040907000412004090700041NM 2004 9 7 DL757040794 120040821A3350 LAMP BOEING757 757232 1384965NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27654DL 24394 THE 43C OVERHEAD EMERGENCY LIGHT INOP. RELAMPED SAME. 2L72 4F RTA2NM 20040907000422004090700042NM 2004 9 7 DLM88040797 120040823A750013277505 DUCT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE BLOWN A DALAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27925DL 49712 718088 ON TAKEOFF RIGHT ENGINE FIRE LOOPS BOTH INDICATED RT ENGINE FIRE. TRIED TO RETARD RT THROTTLE BUT HANDLE WAS STIFF. RIGHT FUEL SHUTOFF SW ALSO STIFF. PULLED FIRE HANDLE AND FIRED BOTH FIRE BOTTLES AND RETURNED TO PBI. FOUND 13 STAGE BLEED AIR DUCT TO NOSE COWL BLOWN. NO DAMAGE TO COWL. FLIGHT CANCELED. REQUIRES BOTH TELEFLEX CABLES TO BE REPLACED. 2L72 4F4 FRTA6WE E9NE 20040907000432004090700043NM 2004 9 7 DL73G040799 120040823A2720 PCU BOEING737 737330 13844BJNM RUDDER LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27241DL 23833 A SYSTEM HYD RESERVOIR APPROX 1/4 FULL. SUSPECT POSSIBLE HYD LEAK ON ENG DRIVEN SIDE, GOOD PRESSURE. FOUND RUDDER PCU LEAKING. REPLACED SAME. 2L72 4F RTA16WE 20040907000442004090700044EA 2004 9 7 SWIA200413734 120040715A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA INTERCOSTAL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07429SW AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00, STR 14R. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED AT FS 625 STR 14R IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16. 2L72 4F RTA21EA 20040901000942004090100094 2004 9 1 UPS04143020 420040826A2565 HANDLE AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE STIFF A IPXAK NONE O OTHER ININSP/MAINT 1 SO01126UP 0810 SLIDE ARMING HANDLE ONLY MOVES HALF DISTANCE TO ARMED POSITION. EXERCISED HANDLE UNTIL FREE. NO ADDITIONAL BINDING NOTED. OK FOR CONTINUED SERVICE. 2L72 4F RTA35EU 20040901000972004090100097WP 2004 9 1 ABXA040300 120040815A5320375849602 FITTING DOUG DC8 DC863F 302198FWP INTERCOSTAL CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 INTERCOSTAL END FITTING AT STA 1160, LONGERON 35 RIGHT WAS CRACKED. END FITTING WAS REPLACED IAW DC-8 SRM 51-1-20D. 2L74 4F 4A25 20040901001002004090100100NM 2004 9 1 UPS04643024 120040826A324226124121A BRAKE ASSY BOEING767 767300 1385204NM NR 5 FIRE A IPXAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 SO01332UP INSPECTION TYPE:N/A NR 5 BRAKE FIRE ON TAXI INTO IAH. INSP C/W PER PG 791941 ITEM 3. REPLACED NR 5 BRAKE ASSY PER MM 32-41-08-4. 2L72 4F RTA1NM 20040901001012004090100101WP 2004 9 1 UPS04843016 120040818A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C2, STATION 70 LONGERON 35R AND END FITTING ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 70 AND 90, INSTALLED SPLICE AND REPLACED END FITTING IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040901001032004090100103WP 2004 9 1 UPS04843018 120040816A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C2, STATION 1280 LONG 35R FWD UPPER FLANGE OF FRAME HAS A HOLE AT RADIUS. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AND FILLER IAW EO DC8-5310-11728-A. 2L74 4F RT4A25 20040901001052004090100105NM 2004 9 1 SWAA042518 120040829A3350D71702001 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED SERVICE, FOUND FWD LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20040901001282004090100128NM 2004 9 1 SWAA042502 120040828A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29449WN 32469 DURING SCHEDULED RON CHECK, FOUND LT LOWER AFT & AFT SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20040901001432004090100143 2004 9 1 SWAA042473 420040825A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040901001562004090100156NM 2004 9 1 SWAA042483 120040826A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND RT CREASE BEAM AT BS 967 TO BS 983, CORRODED. REMOVED AND REPLACED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040901001642004090100164NM 2004 9 1 SWAA042504 120040828A33506104789 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PER MM. 2L72 4F RTA16WE 20040901001712004090100171NM 2004 9 1 SWAA042509 120040828A323365448105 ACTUATOR BOEING737 7373Y0 1384671NM RT MLG LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29682SW 23496 ON CLIMBOUT FROM LAX AT FL 238 THE RT MLG EXTENDED WITH THE HANDLE IN THE OFF POSITION. BOTH RED AND GREEN LIGHTS ILLUMINATED, SLOWED AIRCRAFT, GEAR RETRACTED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20040901001772004090100177EA 2004 9 1 MASA200400400 120040714A5270 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY DOOR ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07921FJ 15021 ASH 6410 PHX-COS. THE CREW REPORTED A LEFT EMERGENCY DOOR CAUTION MESSAGE. THE DOOR WAS CHECKED FOR SECURITY WITH NO DEFECTS NOTED AND THE INDICATION SYSTEM WAS DEFERRED. RESECURED TARGET. OPS CHECK GOOD, NO PARTS USED. 2L72 4F RTA21EA 20040901001792004090100179WP 2004 9 1 DHL2004804527 120040725A5754 SKIN DOUG DC8 DC873F 302199FWP RT WING LE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 RIGHT WING OUTBOARD FLAP L/E UPPER SKIN WORN, XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED-EDW27.5, DWG W27-R05 REV 1R. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING IAW ED-EDW 27.5, DWG W27-R05. FABRICATED SPLICE STRAP (AL 2024-T3 0.080) AND PLATING SEGMENT (AL 2024-T3 0.071) IAW ED EDW 27.5, DWG W27-R05. CLEANED, TREATED AND PRIMED AREA AND PLATING SEGMENT INTERNAL PART AND SPLICE STRAP IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG 9. INSTALLED SPLICE STRAP AND PLATING SEGMENT WITH NEW FASTENERS IAW DWG W27-R05, ED EDW 27.5, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040901001952004090100195EA 2004 9 1 MASA200400455 120040816A5220 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT FALSE INDICATIONA MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07922FJ 15022 ASH 6438 PHX. A RIGHT FORWARD EMERGENCY EXIT DOOR INDICATING OPEN WHEN DOOR WAS SHUT. MX REMOVED, CLEANED AND INSPECTED AND REINSTALLED DOOR. MX COULD NOT DUPLICATE FAULT. 2L72 4F RTA21EA 20040901001982004090100198NM 2004 9 1 WLDA200432 120040626A2432352060DM169A3 CHARGER DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE MASTER BATTERY DEFECTIVE A WRLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11271 48518 FRA/NKT AIR TURNBACK DUE TO LEVEL I BATTERY CHARGING ALERT ILLUMINATED DURING NORMAL CRUISE FLIGHT. ELECTRIC SCHEMATIC SHOWED 40V. BATTERY APPEARED TO BE CONTINUOUSLY CHARGED WITH NO DRAW. REMOVED & REPLACED BATTERY CHARGER IAW MM PROCEDURES. PERFORMED EMERGENCY POWER SYSTEM TEST, NO FAULT FOUND. 2L73 4F4 FRTA22WE E24NE 20040901002022004090100202NM 2004 9 1 DL764040789 120040820A3233 ARM BOEING767 767432ER 1385134NM NLG ACTUATOR CRACKED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27830MH 00841 29701 ON TAXI OUT, CREW REPORTED LOUD SNAP IN NOSE W/W AREA. ON MTC INSPECTION FOUND NOSE GEAR ACTUATOR ARM CRACKED. REPLACED ACTUATOR. 2L72 4F RTA1NM 20040902000112004090200011WP 2004 9 2 DHL2004804508 120040627A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT NR 2 TRACK PLUG LUG WORN, STA 1133.000. REMOVED WORN NR 2 TRACK PLUG, STA 1133.000 IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040902000122004090200012WP 2004 9 2 DHL2004804503 120040624A5711 FRAME DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LEFT JOINT FLAP FORMER CRACK, STA XW 122.000. FABRICATED ANGLE DOUBLER (2024T3 0.050) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-21A PG 1-4. 2L74 4F RT4A25 20040902000132004090200013WP 2004 9 2 DHL2004804502 120040624A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 MAIN CARGO COMPT NR 7 TRACK PLUG LUG WORN, STA 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20040902000202004090200020WP 2004 9 2 DHL2004804506 120040627A5711 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 RIGHT WING CTR L/E UPPER FORMER CRACKED 1.000, XFS 316.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENER IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20040902000212004090200021NM 2004 9 2 DL76K040793 120040821A3233 SHAFT BOEING767 767332 1382001NM NLG ACTUATOR BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27174DZ 29693 NOSE GEAR ACTUATOR SHAFT IS CRACKED. NOSE GEAR ACTUATOR REPLACED. 2L72 4F RTA1NM 20040902000282004090200028EU 2004 9 2 AWXA200400923 120040805A5320D5348002034200 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT SHEAR PLATE (TRAY) ON AFT SIDE OF L-2 DOOR, OUTBOARD OF BEAM Y1292 LT. MAINTENANCE REMOVED CRACKED LT AFT SHEAR PLATE ON AFT SIDE OF L-2 DOOR, OUTBOARD OF BEAM Y1292 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040902000342004090200034NM 2004 9 2 AWXA200400919 120040822A2560P20700012015 FLASHLIGHT AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28808AW 1088 FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040902000352004090200035EU 2004 9 2 AWXA200400920 120040805A5320D53475565210 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB AT WL -Z1500, FROM FR 53 TO FR 56; FABRICATED A NEW REPLACEMENT DOOR SILL WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040902000382004090200038NM 2004 9 2 DHL2004745559 120040630A5720 BRACKET BOEING727 727224 1384076NM FLAP TRACK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, LT WING LOWER WBL 203 NR 3 FLAP TRACK ANGLE SUPPORT FWD FAIRING HAS CRACK OVER PREVIOUS REPAIR O/B OF TRACK. FAB ANGLE SUPPORT ON LT WING NR 3 FLAP TRACK FROM 2024T3 .063 PO 900781 SIZE 9 X 1.5 INCH IAW B727 SRM 51-40-3. ALODINED & PRIMED IAW B727 SRM 51-10-2. INSTALLED ANGLE SUPPORT AT NR3 FLAP TRACK IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040902000452004090200045EU 2004 9 2 DHL2004367006 120040626A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 1 ENGINE INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01367DH 265 DURING PRE-DEPARTURE CHECK FOUND ENGINE NR 1 LOOP-A INOP. DEFERRED PER MEL 26-12-01-1, DMI 17031. S/P COMPLIED WITH. 2L72 4F RTA35EU 20040902000462004090200046EU 2004 9 2 HAEA152 120040630A3230A23801101 SWITCH AMD FALC20FALCON 2720302EU MLG FAULTY E HAEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05977TW33245 13 AFTER DEPARTING MSN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO MSN AND LANDED WITHOUT INCIDENT. 2L72 4F A7EU 20040902000552004090200055NM 2004 9 2 DHL2004754022 120040626A3240 CONTROL VALVE BOEING727 727223 1384074NM RT BRAKE ASSY LACK OF LUBE A DHLAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO01754DH 22008 RIGHT BRAKE DRAGGING, LOCKED-UP JUST AS AIRCRAFT PARKED. FOUND METERING VALVE OUT OF RIG ON RIGHT SIDE RIGGED VALVE IAW B727 M/M 32-41-11, LUBED CONTROL VALVE UPPER & LOWER, BLED NR 3, NR 4 BRAKE, BRAKES SYSTEM OPS CHECKS SERVICEABLE IAW B727 M/M 32-41-0. 2L73 4F A3WE 20040902000582004090200058NM 2004 9 2 CALA0400605 120040819A335020121 POWER SUPPLY BOEING737 737524 1384721NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2714628 27532 THE FIRST CLASS CABIN SEAT EMERGENCY LIGHTS WOULD NOT TEST. THE M1674 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-51. 2L72 4F RTA16WE 20040902000672004090200067NM 2004 9 2 UPS04242853 120040716A5710 FRAME BOEING727 72725C 138400HNM NR 2 TANK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, EVIDENCE OF CORROSION ON CENTER SECTION OF NR 2 TANK UPPER CHORD AT RBL 63.5 APPROX. ON INVESTIGATION CORROSION WAS FOUND TO BE EXTENSIVE. UPPER CHORD FWD SPAR CENTER SECTION REMOVED PER SRM 51-30-2, NEW CHORD SECTION CUT TO ACC INSTL IAW DRG LOR-444. REPAIR & INSTALATION CARRIED OUT IAW AAAE EO 2004-068-007. 2L73 4F A3WE 20040902000722004090200072EU 2004 9 2 DHL2004367007 120040716A4970 WARNING LIGHT AIRBUS300 A300B4203 3930306EU APU ILLUMINATED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01367DH 265 APU FAULT LIGHT ILLUMINATED IN FLT. PERFORMED ABNORMAL, APU WAS IN NORMAL POSITION. REPLACED ECB AS PRECAUTION, T/S PER FIM 49-00 WITH NO FAULT CODES FOUND. OPS CHECK APU PER 49-00-00 OK. 2L72 4F RTA35EU 20040902000872004090200087NM 2004 9 2 UPS04442749 120040711A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, BS 990 S7L STRINGER END FOUND CRACKED. STR REPAIRED AS PER 53-10-03 FIG 4 AT BS 990 STR 7L. 2L74 4F RTA20WE 20040902000942004090200094WP 2004 9 2 UPS04842742 120040626A53203641592N FITTING DOUG DC8 DC873F 302199FWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE:C-3 MAIN CABIN FS 25 LONGERON 22 END FITTING CRACKED. REMOVED FITTINGS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTINGS IAW DC8 SRM 51-1-20D, 51-3-0, 51-3-1. 2L74 4F RT4A25 20040902001042004090200104WP 2004 9 2 UPS04842847 120040720A532037533061 FITTING DOUG DC8 DC873F 302199FWP CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 STATION 990 LONGERON 23R END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D. 2L74 4F RT4A25 20040902001062004090200106WP 2004 9 2 UPS04842849 120040720A53405894282501 FITTING DOUG DC8 DC873F 302199FWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:C1 STATION 1170 BACKUP FITTING FWD SIDE IS CORRODED FOR FWD LOWER T-BOLT FITTING AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 5894282 AND SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20040902001072004090200107NM 2004 9 2 AWXA200400927 120040729A5340693535214 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER TIE AT BS 907, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 907, STR 4 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-05, FIG 6. 2L72 4F RTA16WE 20040902001092004090200109NM 2004 9 2 AWXA200400929 120040730A53106545855101 CREASE BEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR CREASE BEAM AT BS 820, RBL 70, WL 208.1. MAINTENANCE REMOVED CORRODED CREASE BEAM WEB FROM BS 807 TO BS 827, RBL 70, WL 208.1; FABRICATED A NEW REPLACEMENT SECTION OF CREASE BEAM WEB AND A REPAIR ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-12, FIG 1. 2L72 4F RTA16WE 20040902001122004090200112NM 2004 9 2 DHL2004748005 120040807A3350CM313 BULB BOEING727 727225 1384077NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH 22440 EMERGENCY EXIT LIGHTS UNARMED LIGHT FLICKERS. RELAMPED UNARMED LIGHT. EMERGENCY EXIT LIGHT SYS OP'S NORMAL IAW B-MM 33-50-01. INSTALLED 1EA BULB P/N CM313. 2L73 4F A3WE 20040902001182004090200118EA 2004 9 2 VNAA0408006 120040813A2741 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE STAB TRIM ILLUMINATED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07702PS 10135 DURING CLIMBOUT, THE CREW RECEIVED A MACH AND STAB TRIM FAIL INDICATION AND RETURNED TO CLT. MAINTENANCE INSPECTED AND RESET CIRCUIT BREAKERS CBP-1, F-1, P-2, R-4, R-3, AND F-1 AND THE MESSAGE CLEARED. THEN MAINTENANCE ALSO PERFORMED OPERATIONAL CHECKS ON THE STAB TRIM IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 27-140-120. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040902001202004090200120EU 2004 9 2 UPS04142688 120040711A5330 SKIN AIRBUSA300 A300F4622R 3930360EU FWD LWR DOOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01141UP 0824 FWD LOWER DOOR CUTOUT AT FWD UPPER CORNER HAS SKIN DAMAGE. REMOVED DAMAGE REF EO A300-5333-20304-B, FABRICATED DOUBLER, FILLER AND INSTALLED PER EO A300-5330-20304-B. THIS CLEARS D-279358. 2L72 4F RTA35EU 20040902001212004090200121NM 2004 9 2 AMTA200400988 120040804A5754 SKIN BOEING757 75723N 1384973NM NR 3 SLAT DELAMINATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND LEFT WING NR 3 SLAT, AFT SIDE, UPPER MID AREA HAS SEVERAL AREAS WITH DELAMINTION. REPAIRED NR 2 SLAT DELAMINATE AREA, LOWER INBOARD SURFACE IAW B757 SRM 51-70-10, REPAIR 7 FIG 16. (M) 2L72 4F RTA2NM 20040902001252004090200125WP 2004 9 2 ASAA0480476 120040707A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 LAX - DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY OVERHEAD FLOOR LIGHTS INOPERATIVE UPON TEST. RESEATED BATTERIES IN ASSOCIATED POWER SUPPLIES. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001312004090200131WP 2004 9 2 ASAA0480196 120040321A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS321641855 53018 DURING CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS REMAINED ILLUMINATED DURING CYCLE ON/OFF TEST. REPLACED ASSOCIATED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20040902001332004090200133EU 2004 9 2 ASOA04550 120040714A5320S5367800826802 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 38 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040902001462004090200146NM 2004 9 2 USAABB04066 120040711A3610 HEAT EXCHANGER BOEING757 7572B7 1384964NM BOTH CONTAMINATED A USAAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 EA19621AU 27200 CLT - FLT 1121 - CREW REPORTED AN OIL ODOR AND HAZE IN THE CABIN WHICH SET OFF THE 2L LAVATORY SMOKE DETECTOR. THE APU WAS INSPECTED AND NO LEAKS FOUND. THE PACKS WERE OPERATED AT HIGH TEMPERATURE FOR SEVERAL HOURS WITH NO ODOR NOTED. THE COMPLAINT WAS REPEATED ON 7/12/04. THE APU WAS AGAIN INSPECTED, AND METAL AS FOUND IN THE GEARBOX CHIP DETECTOR. THE APU WAS REPLACED. ON 7/23/04, FLT 1274, DIVERTED TO CLT DUE TO SMOKE IN THE COCKPIT. MAINTENANCE REPLACED THE LEFT AND RIGHT PRIMARY AND SECONDARY HEAT EXCHANGERS DUE TO RESIDUAL OIL FROM THE APU. (M) 2L72 4F RTA2NM 20040902001642004090200164NM 2004 9 2 USAA040367 120040713A5754 SKIN BOEING737 7373B7 1384580NM NR 4 SLAT CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND LOWER SKIN SURFACE CHAFED 2 INCH BY 1 INCH, NR 4 SLAT INBOARD TRAILING EDGE. REMOVED CHAFED AREA, BONDED, SEALED EDGE AND REFINISHED PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040902001742004090200174EU 2004 9 2 ASOA04567 120040806A2120 ODOR AEROSPATR72 ATR72212 8680945EU COCKPIT DETECTED A ASOAO OTHER BC SMOKE/FUMES/ODORS/SPARKS F.O.D. CLCLIMB 1 SO11636AS 375 DURING TAKEOFF FROM PFN-ATL, THE AIRCRAFT RECEIVED MULTIPLE BIRD STRIKES WITH ONE HITTING THE CAPTAINS WINDSHIELD AND ANOTHER ENTERING THE LT ENGINE INTAKE, FOLLOWED BY A STRONG ODOR IN THE AIRCRAFT. THE FLIGHT CONTINUED TO ATL WITH NO OTHER PROBLEMS NOTED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE BORESCOPED THE LT ENGINE WITH NO DAMAGES NOTED. MAINTENANCE ALSO PERFORMED A COMPERSSOR WASH, INCLUDING PROPELLER BLADE TRACK AND HUB PRESSURE CHECKS. NO DEFECTS WERE NOTED. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040902001962004090200196NM 2004 9 2 AMTA20040005 120040104A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 FOUND FOUR EMERGENCY FLOOR LIGHTS INOPERATIVE. RELAMPED AND RECONNECTED WIRES, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040903000012004090300001NM 2004 9 3 USAA040403 120040804A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU52228 23594 PIT - FOUND SKIN GOUGED .015 INCH TO .025 INCH DEEP, STATION 860-875 STRINGER 1, TO 2L TO 2R. DOUBLER REPAIR PER EA 78807. (M) 2L72 4F RTA16WE 20040903000042004090300004NM 2004 9 3 C7WA200400016 120040510A2913371380 PUMP BOEING727 727231 1384079NM PWA JT8 JT8D15A 52051NE NR 2 ENG HYD EXPLODED A C7WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO1754354 21986 700151 NR 1 SYSTEM A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, QUANTITY DECREASED TO 1.2 GALLONS. PERFORMED ASSOCIATED CHECK LIST. NR 2 ENGINE HYDRAULIC PUMP HAD A CATASTROPHIC FAILURE. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP. (M) 2L73 4F4 F A3WE E2EA 20040903000102004090300010NM 2004 9 3 C7WA200400035 120040630A5330 SKIN BOEING727 7272J7 138400ENM FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17128NA 20879 FOUND FUSELAGE SKIN CORRODED STRINGER 27 RIGHT STATION 500. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 6. REPAIR DOUBLER FABRICATED FRAME 2024-T3, .050 BY 31.25 BY 18. (M) 2L73 4F A3WE 20040903000132004090300013NM 2004 9 3 ASAA0410352 120040713A53306545775 SKIN BOEING737 737298C 1384490NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 FOUND FUSELAGE OUTER SKIN PILLOWING STATION 727A-727B STRINGER 23L. REMOVED DAMAGED SKIN, FABRICATED REPAIR, PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040903000362004090300036EA 2004 9 3 ASOA04533 120040728A3310S8287 TRANSFORMER CNDAIRCL600 CL6002B19 1900309EA COCKPIT CONSOLE BURNED OUT A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11903EV 7621 FLT 4742 - DURING APPROACH INTO DFW FROM MLU, ALL THREE CREW MEMBERS REPORTED SMELLING A STRONG ELECTRICAL SMOKE ODOR, BUT COULD NOT LOCALIZE THE SOURCE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE RAN THE ENGINES BUT COULD NOT DUPLICATE THE ODOR. MAINTENANCE THEN TURNED ON ALL THE LIGHTS AND FOUND THE LEFT NOSE LANDING LIGHT INOPERATIVE. THE LIGHT WAS REPLACED BUT WAS NO HELP. AFTER FOLLOWING THE SCHEMATICS IT WAS DETERMINED THAT TRANSFORMER T3LE WAS THE CAUSE OF THE ODOR. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT TRANSFORMER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040903000392004090300039NM 2004 9 3 USAA040361 120040726A531465621257 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19350US 23553 PIT - FOUND ELONGATED HOLES AND CHAFING ON UPPER CHORD, KEELBEAM LOWER CHORD, FS 700 TO FS 727 LBBL 6.15, FOUR EACH .4375 INCH DIAMETER. BLENDED, INSTALLED FREEZE PLUGS AND DOUBLER STRAP PER EA 78037. (M) 2L72 4F RTA16WE 20040903000482004090300048NM 2004 9 3 USAABB04057 120040617A3411851FJ1 PITOT TUBE BOEING757 7572B7 1384964NM EXTERIOR DAMAGED A USAAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 EA19624AU 27245 PHL - FLT 633 - CLIMBING THROUGH 15,500 FEET, THE CREW HEARD A LOUD BANG, FOLLOWED BY FLUCTUATION IN THE CAPTAIN'S AIRSPEED INDICATION, AND THE EICAS MESSAGES 'RUDDER RATIO' AND 'ELEV ASYM' AND A MACH AIRSPEED DISAGREE INDICATION. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE RADOME HAD COLLAPSD AND THAT THE NR 2 AUX PITOT TUBE WAS BENT. THE RADOME AND PITOT TUBE WERE REPLACED. (M) 2L72 4F RTA2NM 20040903000512004090300051 2004 9 3 SWAA042543 420040831A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040903000552004090300055NM 2004 9 3 SWAA042547 120040831A523065C36183 SKIN BOEING737 7373Q8 1384670NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR SKIN AT UPPER AFT CORNER, CRACKED. REPAIRED DOOR SKIN PER SRM. 2L72 4F RTA16WE 20040903000572004090300057NM 2004 9 3 SWAA042549 120040831A531065C346701 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE BOX FITTING, CRACKED. REMOVED AND REPLACED UPPER HINGE BOX FITTING PER SRM. 2L72 4F RTA16WE 20040903000602004090300060NM 2004 9 3 SWAA042552 120040831A5752654645522C TAB BOEING737 7375H4 138449DNM RT WING AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT AILERON TAB PER MM. 2L72 4F RTA16WE 20040907000022004090700002NM 2004 9 7 SWAA042553 120040831A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM ROW 8 ABC MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 PHOTOLUMINESCENT STRIP AT ROW 8 ABC, MISSING. INSTALLED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20040907000082004090700008EA 2004 9 7 VNAA0408018 120040831A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DETECTED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07221PS 7889 THE CREW REPORTED A BURNING ODOR AT ROWS 7 AND 8. MAINTENANCE INSPECTED AND NO DEFECTS WERE NOTED. 2L72 4F4 FRTA21EA E15NE 20040907000152004090700015NM 2004 9 7 UPS04M42730 120040616A7160 SKIN DOUG MD11 MD11F 3023600NM NR 2 ENG INLET CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP INSPECTION TYPE: C2, NR 2 ENGINE INLET EXTERIOR UPPER LT SEGMENT HAS 4 CRACKS AROUND FASTENER HOLES. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUT OUT, FABRICATED AND INSTALLED 2 FILLERS AND REPAIR DOUBLER IAW SRM 51-31-04 AND DWG AJC7558. 2L73 4F RTA22WE 20040907000242004090700024NM 2004 9 7 UPS04M42920 120040529A5510 PANEL DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, HORIZONTAL STAB NR 36 BARREL NUT HOLE FOUND CORROSION ON BOTTOM BEARING & SIDE WALL SURFACE. CORROSION AT BEARING & S/W REAMED TO 2.602 PER EN1179-04. BLEND OUT 0.090 INCH DEEP FOUND OUT OF LIMIT. REWORKED B/N HOLE NR 36 RT. FAB & REPAIR SLEEVE BUSHING PER EO MD11-5510-19409-G & EN1179-04, APPLIED SEALANT PR1422B2 AT B/N HOLE NR 36 RT. FAB REPAIR DOUBLER & FILLER USING 7075-T6-0.063 & 0.050 INCH. RT B/N HOLE NR 36, REPAIRED WITHIN LIMIT, SATISFACTORY. 2L73 4F RTA22WE 20040907000342004090700034NM 2004 9 7 AWXA200400913 120040810A5755654645165JP PANEL BOEING737 7373S3 1384711NM SPOILER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 DURING C-19 CHECK 6 EACH CRACKS WERE FOUND IN NR 6 SPOILER LOWER SKIN, WS 294 TO WS 306. MAINTENANCE CUT OUT DAMAGE IN NR 6 SPOILER LOWER SKIN, WS 294 TO WS 306; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10 FIG 30. 2L72 4F RTA16WE 20040907000392004090700039NM 2004 9 7 UPS04M42724 120040427A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C, AFT PRESSURE BULKHEAD STA 2007 FWD FACE TEE AT LONGERON 27 LBL 43 FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.125 INCH & 0.090 INCH, THK REMOVED 0.038 INCH & 0.005 INCH FOUND EXCEED LIMIT PER SRM 53-40-00 FIG 7 VOL 1 REV 34. CORRODED TEE LONGERON CUTOUT AT STA 2007 LBL 36-76 PER SRM 53-40-00 FIG 6 VOL 1 REV 34. NEW TEE CHORD REPAIR INSTALLED PER SRM 53-40-00 VOL 1 FIG 7 REV 34. 2L73 4F RTA22WE 20040907000462004090700046NM 2004 9 7 WLDA200487 120040802A5510ALC80551 FITTING DOUG MD11 MD11 3023602NM HORIZONTAL STAB OUT OF TRIM A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK IN TPE, WHILE PERFORMING EO 02-5510-098 REV 1, FOUND AN OVER TRIM ON FITTINGS OF LT & RT HORIZONTAL STAB OPERATION BULKHEAD. PERFORMED FITTING OF LT & RT HORIZONTAL STAB OPERATION BULKHEAD PER EGAT EI W2004A53B. REPAIR & CONDITION CHECK SATISFACTORY. 2L73 4F RTA22WE 20040907000492004090700049NM 2004 9 7 MWEA040153 120040824A24255D00271 RELAY BOEING717 717200 1383700NM EMERGENCY POWER INOPERATIVE A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31918ME 55180 EMERGENCY POWER SWITCH OFF ALERT CAME ON. REMOVED AND REPLACED BUS SENSING RELAY. 2L72 4F TRA6WE 20040907000512004090700051NM 2004 9 7 CALA0400612 120040824A53476545410199 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK AT STA 727B. THE CRACKED AREA WAS CUT OUT AND A REPAIR STRAP WAS INSTALLED IAW ECRA 5321-01200. 2L72 4F RTA16WE 20040907000522004090700052NM 2004 9 7 CALA0400613 120040824A532065C807351 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND ZEE ANGLE CORRODED AT R-2 DOOR, STA 967-986.5, RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02. 2L72 4F RTA16WE 20040907000532004090700053NM 2004 9 7 CALA0400614 120040824A53156546811 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT UPPER FLANGE STA 986.5 FROM BL 0 TO RBL 36. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20040907000542004090700054NM 2004 9 7 CALA0400615 120040825A533065C30802 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 A 2.5 INCH CRACK WAS FOUND IN THE RT FUSELAGE SKIN AT STA 727 UNDER THE EMERGENCY EXIT LIGHT. A SKIN REPAIR WAS INSTALLED IAW ECRA 5330-03090. 2L72 4F RTA16WE 20040907000572004090700057WP 2004 9 7 UPS04842892 120040707A53155613301503 FLOORBEAM DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, CABIN OVERWING AREA FS 960 FLOORBEAM CRACKED UNDER CUSP LOWER SIDE OF LIGHTENING HOLE RT. REMOVED DOUBLE SEAT TRACK & SPLICES. REMOVED WEB, GRILL & FASTENERS FROM FLOORBEAM. CUT OUT DAMAGED FLOORBEAM IAW DC8 REO GO9893 MAT ID FOR SPLICE ANGLE 7075-T660-6833 PO 444113. FAB SPLICE ANGLE. REC'D, LOCATED, DRILLED & DEBURRED FLOORBEAM. ALODINED & PRIMED REPAIR SPLICE ANGLE & FLOORBEAM. INSTALLED SPLICE ANGLE, FLOORBEAM, SEAT TRACK, WEB, GRILL. 2L74 4F RT4A25 20040907000602004090700060EU 2004 9 7 AWXA200400933 120040805A5347D5311209220000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y765 LT BETWEEN FR 20 AND FR 24. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 LT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000622004090700062NE 2004 9 7 DL76L040800 220040819A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27185DN33656 27961 727649 A/C DIVERTED INTO LGW WITH LOW OIL QTY AND STATUS L SAV TEMP 1 AND L SAV 2 ON LWR EICAS. ON ARR OIL UPLIFT REQUIRED 14 QTS. REPLACED ENGINE. 2L72 4F4 FRTA1NM E24NE 20040907000632004090700063NM 2004 9 7 DL757040801 120040823A2497 WIRE BOEING757 757232 1384965NM TRU DAMAGED A DALAO OTHER P NO WARNING INDICATION CRCRUISE 1 SO27602DL 22809 CIRCUIT BREAKER C-23 ON P-64 PANEL POPPED IN FLIGHT. BREAKER IS FOR TRANSFORMER RECTIFIER UNIT. REPAIRED DAMAGED WIRING OVER DRIP PAN IN E/E. 2L72 4F RTA2NM 20040907000652004090700065NM 2004 9 7 DL738040803 120040823A27803818001003 ACTUATOR BOEING737 737832 13844CFNM NR 1 BYPASSING A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO27384DA 30347 AFTER TAKEOFF UPON FLAP/SLAT RETRACTION THE LEADING EDGE SLATS LOCKED OUT. TROUBLESHOOTING PER MAINTENANCE MANUAL AND BOEING SERVICE BULLETIN, FOUND NUMBER 1 AND NUMBER 8 LEADING EDGE SLAT ACTUATORS BYPASSING. REPLACED BOTH ACTUATORS PER M/M, OPERATIONAL CHECKS OK. 2L72 4F RTA16WE 20040907000662004090700066NM 2004 9 7 DLM88040804 120040823A2910 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27985DL 53312 LEFT SYSTEM HYD QTY WENT TO 3 QTS. TURNED OFF LEFT ENG DRIVEN PUMP PER POM. RE-ENGAGED LEFT ENG HYD PUMP DURING FINAL APPROACH. LEFT HYD QTY EVENTUALLY WENT TO ZERO. FOUND BLUE FLEXIBLE PRESSURE LINE LEAKING IN TAIL CONE AREA. REPLACED FLEX LINE, LT ENG DRIVEN PUMP, TRANSFER PUMP AND FILTERS. FLUSHED LEFT HYD SYSTEM AND CLEANED AFT TAIL CONE AREA. 2L72 4F RTA6WE 20040907000692004090700069NM 2004 9 7 MASA200400436 120040730A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07448YV 448 PILOT REPORTED NUMEROUS CABIN EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK. 2H72 4T RTA13NM 20040907000722004090700072NM 2004 9 7 UPS04442818 120040712A5315 FLOORBEAM BOEING747 747200 1384847NM COCKPIT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, COCKPIT - BS 340 LBL 7-45 FLOORBEAM FOUND CORRODED AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.060 INCH X 2 INCH X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOORBEAM REPAIRED PER SRM 53-10-07 FIG 10 & CIC APPLIED IAW EO M5100-2780E. 2L74 4F RTA20WE 20040907000732004090700073NM 2004 9 7 UPS04442819 120040713A5313BAC1498194 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, U/D- BS 740-760 LEFT STR 3 STR END FOUND CRACKED. STRINGER REPAIR AS PER SRM 53-10-03 FIG 10 AT BS 740-760 LT STR 3. 2L74 4F RTA20WE 20040907000752004090700075NM 2004 9 7 SWAA042533 120040827A53126546568 BULKHEAD BOEING737 7377H4 1384404NM FUSELAGE CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29778SW 27883 DURING SCHEDULED HC2-CHECK, FOUND AFT PRESSURE BULKHEAD ABS 1016, BETWEEN STR 11R AND STR 12L, OIL CANNING. REPAIRED BULKHEAD SECTION PER SRM. 2L72 4F RTA16WE 20040907000762004090700076NM 2004 9 7 DL767040807 120040824A21206066223 FAN BOEING767 767232 1385132NM LEFT UNSERVICEABLE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27111DN 22223 ELECTRICAL ODOR IN COCKPIT ON 3 SEPARATE OCASSIONS, IT WAS ALSO SMELLED THROUGHOUT CABIN LASTING ONLY A FEW MINUTES THEN DISSIPATING. INSTRUCTED F/A TO TURN OFF CHILLERS AT FIRST OCCURRENCE AND IT CLEARED THEN IT RETURNED 2 MORE TIMES. FOUND LT RECIRC FAN TO BE AT FAULT (NOISY). REPLACED SAME. 2L72 4F RTA1NM 20040907000782004090700078EU 2004 9 7 AWXA200400900 120040807A5321D5367005100400 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK A 10 INCH CRACK WAS FOUND IN FLOOR PANEL 261PF. MAINTENANCE REMOVED CRACKED FLOOR PANEL BETWEEN FR 68 AND FR 70, Y1700 LT TO Y1700 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53670051; INSTALLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20040907000792004090700079EU 2004 9 7 AWXA200400901 120040805A5320D53112836200 DUMMY RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y189 BETWEEN FR 20 AND FR 23. MAINTENANCE REMOVED CORRODED RAIL Y189 FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000812004090700081EU 2004 9 7 AWXA200400903 120040805A5320D53112830200 DUMMY RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y81 RT BETWEEN FR 15 AND FR 16. MAINTENANCE REMOVED CORRODED RAIL Y81 RT FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000822004090700082EU 2004 9 7 AWXA200400904 120040805A5320D5347112420100 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT WEB SHEAR PLATE BETWEEN FR 69 AND FR 70, AFT AND OUTBOARD OF BEAM Y1292 RT. MAINTENANCE REMOVED CORRODED SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000832004090700083EU 2004 9 7 AWXA200400905 120040805A5320D53472098000 DUMMY RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y917 LT AFT SIDE OF FR 66. MAINTENANCE REMOVED CORRODED RAIL Y917 LT AFT SIDE OF FR 66; RECEIVED AND INSTALLED NEW REPLACEMENT RAIL IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000842004090700084NM 2004 9 7 AALA20040792 120040730A3350P2010031302 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21187AN 32381 JFK - EMERGENCY EXIT SIGN AT LEFT AFT MAIN ENTRY DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT SIGN AT LEFT AFT MAIN ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040907000852004090700085WP 2004 9 7 AALA20040789 120040731A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21287AA 49299 DFW - EMERGENCY ESCAPE PATH LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK S5 23 FOR EMERGENCY ESCAPE PATH LIGHTING IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040907000862004090700086WP 2004 9 7 AALA20040790 120040731A3350 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217512A 49806 DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040907000872004090700087WP 2004 9 7 AALA20040791 120040801A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21552AA 53034 DFW - OVERHEAD EMERGENCY LIGHT AT TAIL COMPARTMENT WALKWAY INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD TAIL COMPARTMENT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040907000882004090700088NM 2004 9 7 04212411 120040730A2430 GENERATOR DORNERDO32 DO328300 NM DC SYSTEM FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27411FJ 3166 LEFT DC GENERATOR FAILURE IN CLIMBING PHASE. PASSENGERS DEPLANED AT THE GATE. ENGINE BEING REMOVED AND REPLACED. 2H72 4T RTA55NM 20040907000912004090700091NM 2004 9 7 P5CA0401163 120040803A5730 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DELAMINATION ON PANEL LT WING LANDING LIGHT ENTRY DOOR SPLIT & DELAMINATION 4 X 8 INCHES UNDERSPEED TAPE. REMOVED DAMAGE & REPAIRED PER SRM 51-40-13. 2L74 4F4 F A20WE E3NE 20040907000922004090700092NM 2004 9 7 P5CA0401158 120040804A5753 FAIRING BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 FIX FAIRING NR 4 FLAP HAS AREA OF DELAMINATION. REMOVED DAMAGED AREA & BONDED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040907000942004090700094NM 2004 9 7 P5CA0401167 120040810A5321 FLOOR PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 CARGO PIT FLOOR PANEL STA 1680 THRU 1780 IS CRACKED & CORRODED. CUT OUT AND REMOVED DAMAGE, NO CRACK FOUND. CUT OUT FABRICATED & INSTALLED AS PER SRM 51-40-08 & 51-10-02. 2L74 4F4 F A20WE E3NE 20040907000952004090700095NM 2004 9 7 P5CA0401166 120040731A5753 FAIRING BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 FLAP TRACK DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DELAMINATION SEVERAL AREA OF NR 4 FLAP TRACK AFT FAIRING L/W. REMOVED DAMAGE AREA PER SRM 51-40-15, BONDED REPAIR PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040907000972004090700097EA 2004 9 7 04186649 120040704A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27649BR 7414 DURING INSPECTION THE LEFT HAND OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040907001002004090700100NM 2004 9 7 XEA200400606 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT RAIL NR 14 AND 15 HAVE LITE CORROSION AT STATION 622 AND 672, APPROXIMATELY WHERE SEAT TRACK COVER RIDES. BLENDED CORROSION OUT. REMOVED .005 INCH OF MATERIAL. TRACK FOUND TO BE WITHIN LIMITS, REF RD 8/4-53-884, STEP 1. PERFORMED HFEC IAW -8 400 NDTM, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001012004090700101NM 2004 9 7 QXEA200400608 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - LITE CORROSION TOP INBOARD FLANGE TRACK NR 2 AT X 568.0. BLENDED LITE CORROSION, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 2 INCHES LONG, .25 INCH WIDE AND .003 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS FOUND. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001022004090700102NM 2004 9 7 QXEA200400615 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 1 HAS LITE CHAFING AT X 107.8. BLENDED THE LITE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 1.5 INCH LONG, 3.8 INCH WIDE, .003 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001052004090700105EU 2004 9 7 2004UALA00730 120040807A5270 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY DOOR OUT OF ADJUST A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29461UA 1266 RETURNED TO FIELD TO SECURE AN OPEN AVIONICS DOOR. ADJUSTED DOOR PROXIMITY SWITCH. NO OTHER HISTORY OR FUTURE PROBLEMS. 2L72 4F4 FRTA28NM E40NE 20040907001062004090700106NE 2004 9 7 2004UALA00732 220040807A7230 COMPRESSOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE RT ENGINE STALLED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29604UA 21865 RT ENG COMPRESSOR EXPERIENCED A COMPRESSOR STALL. STALL STOPPED WHEN RT THROTTLE RETARDED. RESET BLEED ALL INDICATIONS NORMAL. ALL POST-COMPRESSOR STALL TROUBLESHOOTING ACCOMPLISHED IMMEDIATELY AFTER EVENT, NO DEFECTS FOUND. DECIDED TO WATCH ENG FOR ANY REPEAT STALLING, NO FURTHER ANOMALIES NOTED. ENGINE REMOVED AND INSTALLED ON ANOTHER AIRCRAFT FOR ENG REPOSITIONING PURPOSES ONLY WITH NO FURTHER STALLING EVENTS. THE AIRCRAFT AND ENGINE WAS RETIRED. CAUSE OF INITIAL EVENT WILL REMAIN 'UNKNOWN'. NO FURTHER ACTIONS REQUIRED. 2L72 4F4 FRTA1NM E3NE 20040907001072004090700107NM 2004 9 7 2004UALA00733 120040807A2420 CSD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29352UA 24320 RETURNED TO ORD DUE TO A NR 1 ENGINE GENERATOR DRIVE LIGHT. NR 1 CSD FAILED. OIL LOSS EVIDENT ON COWL, CSD EXTREMELY HOT ON ARRIVAL, SUSPECT INTERNAL FAILURE. REPLACED THE NR 1 CSD, EXCESSIVE METAL FOUND ON CHIP DETECTOR. SHOP FOUND EXTENSIVE INTERNAL CSD FAILURE 2L72 4F4 FRTA16WE E2GL 20040907001082004090700108NM 2004 9 7 2004UALA00734 120040708A2910 HYDRAULIC SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29592UA 28143 LANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC PRESSURE. RIGHT HAND ALTERNATING CURRENT MOTOR PUMP ASSY FAILED. REPLACED PUMP. 2L72 4F4 FRTA2NM E17NE 20040907001092004090700109EA 2004 9 7 04218701 120040805A3010 CLAMP CNDAIRCL600 CL6002B19 1900309EA LT ENGINE LOOSE A VTZAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 EA27701BR 7448 L-14TH DUCT WARNING MESSAGE ON CLIMBOUT WITH SINGLE ENGINE (LEFT ENGINE IDLE) APPROACH AND LANDING. EMERGENCY WAS DECLARED. MX FOUND DUCT CLAMP LOOSE IN LT PYLON AT COWL ANTI ICE DUCT. TIGHTENED AND REPOSITIONED CLAMPS. 2L72 4F RTA21EA 20040907001102004090700110NM 2004 9 7 QXEA200400611 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 1 HAS LITE CHAFING AT X 220. BLENDED LITE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA AT TOP 5 INCHES LONG, 3.8 INCHES WIDE .003 INCH DEEP, AT INSIDE CHANNEL 1.5 INCH LONG, .5 INCH WIDE, .006 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001142004090700114NM 2004 9 7 QXEA200400618 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 1 HAS LITE CORROSION TOP FLANGE AT X94.8. BLENDED OUT LITE CORROSION. MEASURED AND FOUND TO BE WITHIN LIMITS IAW DASH 8 Q400 RD 8/4-53-884, STEP 1. AREA OUTBOARD FLANGE .5 INCH LONG, 3.8 INCH WIDE AND .004 INCH DEEP. INBOARD FLANGE 3.5 INCH LONG, 3.8 INCH WIDE AND .006 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001172004090700117NM 2004 9 7 QXEA200400624 120040812A5410 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - OUTBOARD SPLINE COWL CLIP IS CRACKED ALONG EDGE OF WELD IN RADIUS ON NR 1 NACELLE. REMOVED CRACKED CLEAT AT NR 1 OUTBOARD FORWARD POSITION. LOCALLY FABRICATED REPLACEMENT CLEAT FROM .025 INCH TITANIUM MATERIAL IAW RD 8/4-71-032. COMPLETED INSTALLATION OF SPLINE COWL CLEAR USING MS20615-4M RIVETS PER RD 8/4-71-032. 2H72 4T RTA13NM 20040907001182004090700118NM 2004 9 7 QXEA200400625 120040812A5210 STEP BOMBDRDHC8 DHC8401 1390041NM ZONE 800 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - MAIN CABIN DOOR STEP ASSEMBLY FORWARD UPPER MOUNT FITTING CORRODED ON BOTTOM. REMOVED LIGHT SURFACE CORROSION ON FORWARD UPPER MOUNT FITTING USING A SCOTH BRITE PAD IAW D-8 400 SRM 51-21-00, TASK 51-21-00-350-801. 2H72 4T RTA13NM 20040907001202004090700120NM 2004 9 7 QXEA200400614 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 1 HAS LITE CHAFING AT X138.5. BLENDED THE CHAFE, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 1 INCH LONG, 3.8 INCH WIDE, .006 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001212004090700121NM 2004 9 7 QXEA200400613 120040811A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT TRACK NR 17 HAS CORROSION AT APPROXIMATELY STATION X226.00. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED .003 INCH MATERIAL. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001242004090700124EU 2004 9 7 UPS04142735 120040718A3350 LAMP AIRBUS300 A300B4622R 3930312EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01126UP 0810 EXIT SIGN ABOVE CREW ENTRY DOOR IS INOP. EMERGENCY LIGHTS TEST IS SHOWING FAULT. RELAMPED ALL 9 LAMPS IN EXIT SIGN 31WL1. 2L72 4F RTA35EU 20040907001252004090700125EU 2004 9 7 2004UALA00735 120040811A2910 HYDRAULIC SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE BLUE SYSTEM INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29409UA 462 RETURNED TO FIELD DUE TO LOSS OF BLUE SYSTEM HYDRAULICS. FOUND BLUE HYDRAULIC SYSTEM ELECTRIC PUMP PRESSURE FLEX LINE CHAFED. REPLACED CHAFED LINE AE707414-2. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040907001282004090700128NM 2004 9 7 AWXA200400776 120040715A3397BR963180 WIRE HARNESS BOEING737 73733A 1384673NM SEAT ROW 19 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 PHX - EEL - DURING 4-DAY CHECK FOUND A EMERGENCY ESCAPE PATH LIGHT WIRE PULLED OUT OF CONNECTOR AT SEAT ROW 19 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040907001332004090700133NM 2004 9 7 2004UALA00742 120040809A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SEAT 21-23 INTERMITTENT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29675UA 29243 EEL LIGHT STRIP FLASH INTERMITTENTLY AT ONLY SEATS 21, 22, 23 LEFT SIDE (END). REPLACED LIGHT PACK UNDERNEATH SEAT 23 AB. 2L72 4F4 FRTA1NM E24NE 20040907001352004090700135NM 2004 9 7 2004UALA00744 120040730A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29907UA 25007 AFT SECTION OF EEL LIGHT IS INOPERATIVE. REPLACE DEFECTIVE RIBBON. 2L72 4F4 FRTA16WE E2GL 20040907001372004090700137EU 2004 9 7 AWXA200400662 120040619A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 263 DISCHARGED A AWXAO OTHER L NO TEST NRNOT REPORTED 1 WP28603AW9931 219 661 DURING INSPECTION FOUND THE AFT LT EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040907001382004090700138EU 2004 9 7 AWXA200400663 120040620A2560P20700012015 FLASHLIGHT AIRBUS320 A320232 3930326EU ZONE 900 - LAVATINOPERATIVE A AWXAO OTHER L NO TEST NRNOT REPORTED 1 WP28604AW 1196 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT UNDER AFT FLIGHT ATTENDANT JUMPSEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT UNDER AFT FLIGHT ATTENDANT JUMPSEAT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040907001392004090700139NM 2004 9 7 AWXA200400664 120040620A3150BACC18Z3R CIRCUIT BREAKER BOEING737 73733A 1384673NM P006-02 CB PANELBROKEN A AWXAC ABORTED TAKEOFF JS WARNING INDICATION AFFECT SYSTEMS TOTAKEOFF 1 WP28173AW 23632 LAX - ABORTED TAKEOFF - FLT 0112 - ON TAKEOFF ROLL AT LAX EN ROUTE FOR LAS THE TAKEOFF WARNING CONFIGURATION HORN SOUNDED, REJECTED TAKEOFF AND FOUND THAT FLAP INDICATOR CIRCUIT BREAKER POPPED AND HAD BROKEN INTO PIECES. MAINTENANCE REMOVED AND REPLACED FLAP INDICATOR CIRCUIT BREAKER (C211) IAW AWM 27-81-11 PG 1 SHEET 1, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040907001402004090700140EU 2004 9 7 AWXA200400665 120040605A5347D5347217920000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 47 AND FR 64. MAINTENANCE REMOVED CORROSION AND FOUND ONLY THE AREA OF BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 55 AND FR 64 WAS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 FROM FR 55 TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK, A DOUBLER, AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 53-00-15 FIG 202 PG 207-211. 2L72 4F RTA28NM 20040907001432004090700143EU 2004 9 7 AWXA200400668 120040605A5347D5713014720000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 36 AND FR 41. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 RT FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11, FIG 9 & 18. 2L72 4F RTA28NM 20040907001442004090700144EU 2004 9 7 AWXA200400669 120040605A5347D5337111200000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y1292 LT OUTBOARD SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 LT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 10 & 12. 2L72 4F RTA28NM 20040907001462004090700146EU 2004 9 7 AWXA200400671 120040605A5347D5337111000100 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 RT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11, FIG 12, 13 & 18. 2L72 4F RTA28NM 20040907001472004090700147EU 2004 9 7 AWXA200400672 120040605A5347D5337111200100 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER SURFACE AND INSIDE THE TRACK CHANNEL OF BEAM Y1292 RT OUTBOARD SEAT TRACK BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 RT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 12, 13 & 18. 2L72 4F RTA28NM 20040907001492004090700149NM 2004 9 7 AWXA200400880 120040726A575465C266043 SKIN BOEING737 7373S3 1384711NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW AUXILIARY TRACK. MAINTENANCE CUT OUT DAMAGED AREA OF NR 3 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20040907001522004090700152NM 2004 9 7 2004UALA00746 120040807A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE LT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29919UA 25386 EMERGENCY EXIT LIGHT INOPERATIVE AT LEFT OVERWING EXIT. REPLACED LAMP. 2L72 4F4 FRTA16WE E2GL 20040907001542004090700154NM 2004 9 7 2004UALA00748 120040802A3350 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ROWS 15-24 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29828UA 1031 EMERGENCY SEAT TRACK LIGHTING INOPERATIVE AT ROWS 15, 16, 19, 20, 23 AND 24. WIRE HARNESS WAS INOPERABLE. REPAIRED WIRE HARNESS 350WL10 FOUND UNDER SEATS 23AND 24 ABC. 2L72 4F4 FRTA28NM E40NE 20040907001552004090700155NM 2004 9 7 2004UALA00750 120040726A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 46-54 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29118UA 28811 SEAT 46 ABC TO 54 ABC EMERGENCY LIGHTS IS INOPERATIVE. REPLACED FEEDER UNDER CARPET BY LEFT SIDE OF AFT GALLEY. 2L74 4F4 FRTA20WE E24NE 20040907001562004090700156NM 2004 9 7 QXEA200400575 120040803A30104100S00502 VALVE BOMBDRDHC8 DHC8401 1390041NM DE ICE SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09401QX5892 4031 SEA - FLIGHT 2399 WHEN AIRFRAME MODE SELECTOR SWITCH USED AT FAST AND SLOW, DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED. IT APPEARED ALWAYS TO HAPPEN UPON ILLUMINATION OF LEFT INTAKE AND RIGHT INBOARD TAIL. PSI WAS ALWAYS 19-20, COMPLIED WITH CHECKLIST. MAINTENANCE NR 5 DUAL DISTRIBUTOR VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040907001582004090700158NM 2004 9 7 2004UALA00752 120040727A1430 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE SEAT 52 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 SEAT 52 HJK EMERGENCY LIGHT OUT. REPAIRED CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20040902000712004090200071NM 2004 9 2 UPS04242859 120040629A5751 ROD BOEING727 72725C 138400HNM RT IB AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, RIGHT INBOARD AILERON TAB SUSPECT CRACK ON TAB ACTUATING ROD AT AFT END. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED. ACTUATING ROD REMOVED IAW 27-10-01. REPLACED AFT END OF ROD IAW SRM 51-30-02. REINSTALLED ACTUATING ROD IAW MM 27-10-01. 2L73 4F A3WE 20040902000892004090200089NM 2004 9 2 UPS04442751 120040709A5313 STRINGER BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C M/D - STA 1959 TO STA 1960 RIGHT NR 1 STRINGER END FOUND CRACK. M/D - STA 1959 TO STA 1960 RIGHT NR 1 STRINGER CRACK REPAIRED AS PER SRM 53-10-03 FIGURE 4. 2L74 4F RTA20WE 20040902000962004090200096NM 2004 9 2 DL73S040783 120040820A555365468725 ATTACH FITTING BOEING737 737247 138448DNM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 VERTICAL STABILIZER ATTACH LUGS FOUND CORRODED ON THE NR 3 AND NR 6 FORE AND AFT FACES. REPAIRED IAW ERA 092521-14. 2L72 4F A16WE 20040902001242004090200124NM 2004 9 2 ASAA0410186 120040331A335085210144 BATTERY PACK BOEING737 737298C 1384490NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE, FOUND SMOKE BARRIER EXIT TO THE REAR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. (M) 2L72 4F RTA16WE 20040902001292004090200129NM 2004 9 2 ASAA0410185 120040331A33508821004 BATTERY PACK BOEING737 737290C 138448VNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC- DURING MAINTENANCE CHECK, FOUND LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. (M) 2L72 4F A16WE 20040902001342004090200134EU 2004 9 2 ASOA04549 120040714A5310 STANCHION AEROSPATR72 ATR72212 8680945EU FUSELAGE BENT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT STANCHION UNDER THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE BENT BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT STANCHION UNDER THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-00. (M) 2H72 4T RTA53EU 20040902001712004090200171NM 2004 9 2 USAA040370 120040803A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND SKIN CRACKED .75 INCH, UNDER DOUBLER PLATE, FS 328 ABOVE STRINGER 17R AT SILL PLATE FASTENERS. REPAIRED PLATES AND FILLERS INSTALLED PER SRM 53-10-01 FIG 202. (M) 2L72 4F RTA16WE 20040902001892004090200189NM 2004 9 2 BJNA040502 120040503A2760654485112 ACTUATOR BOEING737 737282 13844ATNM NR 4 SPOILER LEAKING A BJNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP11344TM 23044 AFTER TAKEOFF, FLT CREW NOTICED HYD SYSTEM-A QUANTITY LOSS. A/C RETURNED TO MFE & MADE UNEVENTFUL OVERWEIGHT LANDING. B AND STANDBY HYD SYS NOT AFFECTED. MX DISCOVERED FLUID LEAKING FROM SHAFT SEALS ON NR 4 SPOILER ACTUATOR. SPOILER ACTUATORS ARE UNDER A-SYS HYD PRESS WHEN IN DOWN POSITION. FLUID LOSS FROM NR 4 SPOILER ACTUATOR DEPLETED A-SYS HYD FLUID. MX R & R NR 4 GROUND SPOILER ACTUATOR. DURING OPS CHECKS OF HYD SYS, IT WAS ALSO DISCOVERED THAT NR 2 HYD EDP WOULD NOT DEVELOP PRESSURE & WAS R & R. AS A PRECAUTION THE A-SYS HYD FILTERS WERE REPLACED. OPS & LEAK CHECKS COMPLETED IAW BOEING MM 27-62-72. A/C WAS RETURNED TO SERVICE AFTER OVERWEIGHT LANDING INSPECTION. (M) 2L72 4F RTA16WE 20040902001952004090200195EU 2004 9 2 2004F00267 120040707A32105800311064 BEARING PIAGIOP180 P180 6960204EU RT MLG CRACKED A VIBAK NONE O OTHER ININSP/MAINT 1 SO1329JS 596 1046 DISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION, NO FURTHER DAMAGE WAS NOTED IN THE SURROUNDING AREAS DURING INSPECTION PROCESS. (M) 1H72 3O RTA59EU 20040902002002004090200200EU 2004 9 2 SIMA200420902 120040726A33506013211 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21345SB 340B345 LAX - FLT 3093 - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT AT 8A TO BE INOPERATIVE. MAINTENANCE REMOVED AND RPELACED THE EMERGENCY BATTERY POWER SUPPLY 22LN IAW SAAB 340 AMM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040903000562004090300056NM 2004 9 3 SWAA042548 120040831A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 914, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040903000582004090300058NM 2004 9 3 SWAA042550 120040831A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 328, LBL 28 TO RBL 36, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20040903000592004090300059NM 2004 9 3 SWAA042551 120040831A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, RBL 65, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM, TI-153-018. 2L72 4F RTA16WE 20040907000212004090700021NM 2004 9 7 UPS04M42762 120040701A5347549291477075T SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP INSPECTION TYPE: C, STA Y 695 TO 755 SEAT TRACK FOUND CORRODED AT STA X=-27.50. CORROSION AT SEAT TRACK STA Y695-755 AT X=-27.50. CORROSION REMOVED FOUND EXCEEDED LIMIT. ORI,THK=0.100 INCH & REMAIN THK=0.050 INCH. NEW SEAT TRACK & SPLICE FAB AS PER SRM 53-70-00, F1, V1, R35. NEW SEAT TRACK & SPLICE INSTALLED AT STA Y695-755 AS PER SRM 53-70-00 F1, V1, R35, FOUND SATISFACTORY. 2L73 4F RTA22WE 20040907000312004090700031EU 2004 9 7 AWXA200400910 120040805A5347D53112087200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RAIL Y254 LT BETWEEN FR 16 AND FR 22. MAINTENANCE REMOVED DAMAGED RAIL Y254 LT FROM FR 16 TO FR 22; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000352004090700035NM 2004 9 7 UPS04M42720 120040426A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, MAIN DECK CABIN ALONG STA 1341, APPROX 77 INCH RBL FOUND SEAT TRACK CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH THK REMOVED 0.021 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 VOL 1 REV 34. CORRODED SEAT TRACK CUTOUT AT STA 1262-1391 RBL 75.25 PER SRM 53-70-00 VOL1 REV 34. NEW SEAT TRACK, SPLICE & SPLICE PLATE FABRICATED & INSTALLED PER SRM 53-70-00 VOL 1, REV 34. 2L73 4F RTA22WE 20040907000382004090700038NM 2004 9 7 UPS04M42723 120040423A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, SEAT TRACK FOUND CORRODED AT B STA 899-979 LBL 75. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH, THK REMOVED 0.020 INCH FOUND EXCEED LIMIT AS PER SRM 53-70-00 VOL 1 REV 34. CORRODED SEAT TRACK CUTOUT AT STA 909-989 LBL 75 AS PER SRM 53-70-00 VOL 1. NEW SEAT TRACK, SPLICE & SPLICE PLATE INSTALLED AS PER SRM 53-70-00 VOL 1 REV 34. 2L73 4F RTA22WE 20040907000402004090700040NM 2004 9 7 UPS04M42725 120040428A5330 SKIN DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, CORROSION FOUND ON THE AUX TANK UPPER SURFACE STA 1209 RBL 97 IN THE C R CABIN. RHS APPROX 97 STA 1209 LONGERON NR 18 AUX TANK UPPER SKIN CORROSION REMOVED PER SRM 57-20-00 FIG 12 ORIG THK APPROX 0.150 INCH REMAIN THK APPROX 0.106 INCH FOUND EXCEEDED LIMIT. REPAIR DOUBLER FABRICATED PER EN 1 188-04 & PROTECTED PER SRM 51-21-01 VOL 2 REV 35. REF TO UPS ENGINEERING FILE MD11-57-20016. 2L73 4F RTA22WE 20040907000472004090700047EU 2004 9 7 HAEA200400163 120040816A3240A23802102 SWITCH AMD FALC20FALCON 2720302EU NLG STICKING E HAEAO OTHER O OTHER LDLANDING 1 SW05232TW1483414834 32 ON LANDING AIRCRAFT HAD NO BRAKING. PILOT SELECTED NR 2 SYSTEM AND FUNCTION PROPERLY. NR 1 SYSTEM WORKED AFTER LANDING. MAINTENANCE FOUND NOSE STRUT SWITCH STICKING. REPLACED SWITCH. OPS CHECK GOOD. 2L72 4F A7EU 20040907000482004090700048EU 2004 9 7 AWXA200400932 120040805A5320D5348004820100 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING AT FR 67. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING AT FR 67; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000562004090700056WP 2004 9 7 UPS04842891 120040701A52305754075502 FITTING DOUG DC8 DC871F 302199DWP C-1 DOOR WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, A PIT DOOR AFT UPPER LOCK PIN GUIDE WORN. REMOVED DAMAGED FITTING DC8 SRM 51-3-0. ORIG MAT IS .250 IAW DAC DWG 5 754075. MAT REMAINING IS.104 AND FOUND TO BE WITHIN LIMITS IAW DC8 SRM 52-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040907000592004090700059 2004 9 7 UPS04M42895 420040810A2565MS25237369 SLIDE DOUG MD11 MD11F 3023600NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01275UP INSPECTION TYPE:N/A, FOUND DOOR R1 ESCAPE SLIDE REMOTE PRESSURE INDICATION INOP. BOTTLE PRESS CHECKED OK ON GAUGE. *S/D* REMOVED AND REPLACED IND BULBS, OPS CHECKS NORMAL. PLACARD REMOVED. THIS CLEARS DMI M285801. 2L73 4F RTA22WE 20040907000612004090700061NM 2004 9 7 DL733040796 120040823A57536546431280 WEDGE BOEING737 737347 1384647NM RT WING TE FLAPSDEBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 NR 4 FORE FLAP TE WEDGE WAS FOUND WITH A 42 INCH SECTION OF SKIN DISBONDED. REPAIRED PER ER/A 092865-14. 2L72 4F RTA16WE 20040907000772004090700077NM 2004 9 7 UPS04242993 120040730A5730 PANEL BOEING727 72722C 138400FNM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, PANEL ON LOWER SURFACE OF RT WING L/E FALSEWORK PANEL FSS 195 TO FSS 314 HAS DELAMINATION AT FWD EDGE. PANEL REMOVED IAW SRM 51-10-06. PANEL FABRICATED IAW DRG 65-21653 AND SRM 51-40-9. ON INSTALLATION OF PANEL, FUEL PIPE FOUND TO BE DAMAGED. FUEL PIPE FABRICATED REF CPT 3132. REPLACE FUEL PIPE. 2L73 4F A3WE 20040907000982004090700098NM 2004 9 7 QXEA200400604 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT RAIL NR 14 HAS LITE CORROSION AT STATION 589 TO 608, APPROXIMATELY WHERE SET TRACK COVER RIDES. BLENDED OUT CORROSION IN AFFECTED AREA. REMOVED .007 INCH OF MATERIAL. TRACK FOUND TO BE WITHIN LIMITS REF RD 8/4-53-884. PERFORMED HFEC IAW -8 400 NDTM PART 6 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907000992004090700099NM 2004 9 7 QXEA200400607 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 2 HAS GOUGE IN BETWEEN TOP FLANGES AT X 291.0. BLENDED GOUGE INSIDE CHANNEL, MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 1 INCH LONG, 1.2 INCH WIDE AND .005 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001032004090700103NM 2004 9 7 QXEA200400592 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT RAIL NR 12 AND NR 13 HAVE LITE CORROSION AT STATION 210 TO 220 APPROXIMATELY 15 INCHES WHERE TRACK COVER RIDES. LITELY BLENDED OUT CORROSION FROM SEAT TRACK AS INDICATED. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .004 INCH, WITHIN LIMITS PER RD 8/4-53-884. 2H72 4T RTA13NM 20040907001152004090700115NM 2004 9 7 QXEA200400619 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - THERE ARE CORROSION PITS ON SEAT TRACK AT X726 TO X729 AT Y 10L. BLENDED OUT CORROSION ON SEAT TRACK. REMOVED .022 INCH MATERIAL. TRACK IS FOUND TO BE WITHIN LIMITS REF RD 8/4-53-884. PERFORMED HFEC IAW 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001222004090700122NM 2004 9 7 QXEA200400610 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 2 CHAFED ON TOP FLANGE AT X 554.0. BLENDED LITE CHAFE, MEASURED, AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 1 INCH LONG, 1.4 INCH WIDE, .003 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-563-884, STEP 6. 2H72 4T RTA13NM 20040907001302004090700130NM 2004 9 7 2004UALA00739 120040723A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SEAT 36HJ INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29665UA 29237 EMERGENCY EEL LIGHT AT SEAT 36HJ IS INOPERATIVE. REPLACED SEAT HARNESS. 2L72 4F4 FRTA1NM E24NE 20040907001312004090700131NM 2004 9 7 2004UALA00740 120040726A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SEAT 10 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29664UA 29236 SEAT 10 EEL STRIP IS INOPERATIVE. REPLACED SEAT CABLE. 2L72 4F4 FRTA1NM E24NE 20040907001322004090700132NM 2004 9 7 2004UALA00741 120040804A3350 LIGHT BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29671UA 30026 FORWARD GALLEY EEL LIGHT INOPERATIVE. REPLACED LIGHT ASSY. 2L72 4F4 FRTA1NM E24NE 20040907001362004090700136CE 2004 9 7 ACE071204 120040712A5330 SKIN BEECH 1900 1900C 1154161CE FUSELAGE CORRODED E YADAK NONE O OTHER ININSP/MAINT 1 AL03113AX UC41 MAINTENANCE OBSERVED DEFORMATION OF FUSELAGE SKIN AT LAP JOINTS AT STATIONS 348.25 & 430.75 UNDER STRINGER 16. REPAIRS MADE INCLUDED REMOVAL OF EXFOLIATED SHIMS AND FAILED BONDING AGENT. PREVIOUS REPAIRS OF THIS TYPE AND ON THIS MODEL HAVE DISCLOSED PRIOR USE OF BARE ALUMINUM SHIMS AT LAP JOINTS. 2L72 4T RTA24CE 20040907001482004090700148NM 2004 9 7 04228424 120040815A2430 GENERATOR DORNERDO32 DO328300 NM RT DC SYSTEM FAILED A VTZAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 EA27424FJ 3185 RIGHT DC GEN FAILURE ON TAKEOFF ROLL. TAXI BACK TO GATE UNEVENTFULLY. MX REMOVED AND REPLACED BUSS POWER CONTROL UNIT. OPS CHECK GOOD. 2H72 4T RTA55NM 20040907001502004090700150NM 2004 9 7 AWXA200400881 120040720A575465C266023 SKIN BOEING737 7373S3 1384711NM NR 5 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 MCN - MAJOR REPAIR - DURING C-19 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN SKIN AT NR 5 SLAT ACTUATOR ATTACHMENT AREA. MAINTENANCE CUT OUT DAMAGED AREA OF NR 5 SLAT SKIN 42 INCHES TO 51 INCHES FROM INBOARD SIDE; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20040907001572004090700157NM 2004 9 7 AWXA200400594 120040602A21317638101 CONTROLLER BOEING737 7373G7 1384595NM ZONE 205 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28322AW324181599 25400 PHX - AIR TURNBACK - FLT 0488 - ON CLIMBOUT OF PHX EN ROUTE FOR DEN EXPERIENCED CABIN PRESSURE LOSS AT 26,000 FT, ONLY INDICATION WAS THE 10,000 FT HORN. TURNED BACK TO PHX, DID NOT DECLARE EMERGENCY. MAINTENANCE REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IAW IAW T/C F1B21001, OPERATIONAL CHECK WAS GOOD. VENDORS INCOMING FUNCTIONAL TEST OF CABIN PRESSURE CONTROLLER S/N HA2868 WAS NO FAULT FOUND. UNIT WAS DISASSEMBLED, TESTED EXTENSIVELY SEVERAL TIMES, AND RETURNED TO SERVICE IAW CMM 21-31-11 REV 13. 2L72 4F RTA16WE 20040907001592004090700159EU 2004 9 7 AWXA200400673 120040607A5320D5348004820100 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON UPPER OUTBOARD SURFACE OF L-2 DOOR SILL BEAM Y1502 LT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED DAMAGED SECTION OF L-2 DOOR SILL BEAM Y1502 LT FROM FR 66 TO FR 68; FABRICATED A 3 EACH FILLERS & 2 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW A320 53-41-14 FIG 201, PG 202-208 & 211-212. 2L72 4F RTA28NM 20040907001602004090700160NM 2004 9 7 04227418 120040814A3350 POWER SUPPLY DORNERDO32 DO328300 NM EMERGENCY LIGHT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27418FJ 3176 REMOVED AND REPLACED 6LK EMERGENCY POWER SUPPLY, OPS CHECK GOOD OF EMERGENCY LIGHTING SYSTEM IN REF TO JIC 33-51-01. 2H72 4T RTA55NM 20040907001632004090700163NM 2004 9 7 2004UALA00756 120040810A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 PYLON LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 3 PYLON UPPER LINK TO WING ATTACH FITTING HAS ONE FASTENER THAT HAS ROTATED, INBOARD VERTICAL FASTENER MOST AFT. 2L74 4F4 FRTA20WE E24NE 20040907001662004090700166EU 2004 9 7 AWXA200400674 120040605A5347D5337102400000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y1292 LT OUTBOARD SEAT TRACK BETWEEN FR 37 AND FR 41. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 LT FROM FR 37 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 51-42-11 FIG 12, 13 & 18. 2L72 4F RTA28NM 20040907001682004090700168WP 2004 9 7 AALA20040816 120040806A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21967TW 53617 OVERHEAD EMERGENCY EXIT LIGHTS IN VENTRAL STAIRWAY INOPERATIVE. REPLACED BATTERY PACK B528 FOR OVERHEAD EMERGENCY EXIT LIGHTS IN VENTRAL STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040907001692004090700169NM 2004 9 7 AALA20040823 120040809A3350 LIGHT BOEING737 737823 13844BZNM EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21967AN 29545 EMERGENCY EXIT IDENTIFIER FORWARD OF RIGHT HAND FORWARD SERVICE DOOR IS DAMAGED. FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 13D IS INOPERATIVE. REPLACED EMERGENCY EXIT IDENTIFIER ASSEMBLY AT RIGHT HAND FORWARD SERVICE DOOR. REPLACED FORWARD SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040907001702004090700170WP 2004 9 7 AALA20040824 120040809A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21491AA 49684 DFW - FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE SEAT 20D FOR FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040907001712004090700171 2004 9 7 AALA20040817 420040731A2565312540011 ACTUATOR BOEING767 767323 1385205NM OVERWING SLIDE INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21372AA 25199 SFO - OVERWING SLIDE DOOR ACTUATED UNSUCCESSFUL WHILE STILL PINNED. REPLACED BLOW DOWN ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2L72 4F RTA1NM 20040907001722004090700172WP 2004 9 7 AALA20040812 120040808A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21286AA 49298 DFW - BOTH EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR BOTH EXTERIOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040907001732004090700173WP 2004 9 7 AALA20040814 120040807A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21434AA 49452 ORD - EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040907001762004090700176WP 2004 9 7 CALA0400602 120040813A5347S0020023700 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1007-1098, BL 0 TO LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2L72 4F A6WE 20040907001822004090700182NM 2004 9 7 QXEA200400588 120040805A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION AT X518.00 AND X531.00. REPAIRED IAW RD 8-53-3644, DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20040907001842004090700184EA 2004 9 7 QXEA200400586 120040809A2721 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA RUDDERR TRIM MALFUNCTIONED A QXEAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM09611QX5908 10041 ONT - FLIGHT 4099 - ON TAKEOFF ROLL, AND ON CLIMBOUT, THE RUDDER TRIM WAS OBSERVED TO MOVE APPROXIMATELY 25 PERCENT LEFT DEFLECTION. ON BOTH OCCASIONS, IT DID NOT APPEAR THAT THE RUDDER ACTUALLY MOVED. ALL MOVEMENT INDICATIONS WERE UNCOMMANDED WITH THE AUTO PILOT OFF. MAINTENANCE INSPECTED THE AIRCRAFT AND THEN CYCLED THE SHIPS POWER. OPERATIONAL CHECKS OF THE RUDDER TRIM SYSTEM WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040907001862004090700186NM 2004 9 7 AWXA200400765 120040712A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28813AW15672 1223 PHX - EEL - DURING 4-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 3, 6, & 12 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040907001872004090700187EU 2004 9 7 AWXA200400766 120040711A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 263 FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28603AW3726132349 661 PHX - EEL - DURING E-01 CHECK FOUND THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040907001892004090700189NM 2004 9 7 SWAA042534 120040830A3233654482517 ACTUATOR BOEING737 7373Q8 1384670NM RT MLG LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW29695SW 23506 AIR TURNBACK, AFTER TAKEOFF GEAR LEVER SELECTED TO UP, ALL GEARS RETRACTED NORMAL. WHEN LEVER SELECTED TO OFF RT MLG CAME DOWN. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20040907001902004090700190NM 2004 9 7 SWAA042535 120040830A291065C268091134 LINE BOEING737 7373H4 1384600NM A-HYD SYSTEM LEAKING A SWAAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29332SW 23696 AIR TURNBACK, NR 1 ENGINE HYDRAULIC A-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE PER MM. 2L72 4F RTA16WE 20040907001912004090700191NM 2004 9 7 SWAA042513 120040829A53306545774544 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040907001922004090700192NM 2004 9 7 SWAA042514 120040829A53126546547 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB AT BS 727, LBL 14, WL 175, CRACKED. REPAIRED BULKHEAD WEB PER EA. 2L72 4F A16WE 20040907001932004090700193 2004 9 7 DL757040808 420040810A2565AS11712K0127 HOSE BOEING757 757232 1384965NM RT WING SLIDE FRAYED A DALAK NONE O OTHER ININSP/MAINT 1 SO27620DL 22910 RIGHT OFF WING SLIDE INFLATION HOSE FRAYED. REPLACED SAME. 2L72 4F RTA2NM 20040907001942004090700194NM 2004 9 7 DLM88040809 120040825A2520771921 BRACKET DOUG MD88 MD88 3023688NM SEAT 4C BROKEN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27951DL 49882 SEAT 4C SEATBELT (MALE END) BROKEN. ATTACH FITTING THAT BOLTS TO SEAT SHEARED OFF. REPLACED SEAT BELT BRACKET. 2L72 4F RTA6WE 20040907002002004090700200EU 2004 9 7 AALA20040818 120040802A3260A254310012 UPLOCK AIRBUS300 A300B4605R 3930308EU MLG DOOR FAILED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2159081 639 JFK - INFLIGHT T833/02 ON TAKEOFF NOSE GEAR DOOR SHOWED UNLOCKED ON BOTH SYSTEM NUMBER ONE AND TWO. ECAM MESSAGE NOSE GEAR DOOR UNSAFE. NO NOISE NOTED UNTIL GEAR HANDLE RETURNED TO NEUTRAL. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED FAULTY RIGHT HAND NOSE GEAR DOOR UPLOCK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040907002022004090700202NM 2004 9 7 SWAA042427 120040821A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIPS AT LT ROW 16 TO LT ROW 19, AND RT FWD SECTION WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20040907002042004090700204 2004 9 7 SWAA042429 420040821A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040907002062004090700206NM 2004 9 7 WLDA200437 120040802A5512ALC8131502 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT BARREL NUT HOLE NR 36. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BARREL NUT HOLE NR 36 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040907002092004090700209EU 2004 9 7 MALA040512 120040807A5347 SEAT TRACK BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15535XJ E2371 DURING C-CHECK IN LCQ, NR 4 SEAT TRACK HAS SEVERAL AREA'S OF CORROSION. REPAIRED BY REPLACING DAMAGED SECTION IAW MESABA EO A53026. AIRCRAFT RELEASE DATE 8/11/04. 2H74 4F RTA49EU 20040907002102004090700210EU 2004 9 7 MALA040517 120040803A31500006WS00 CONTROL PANEL SAAB SF340 340B 7860101EU DE ICE SYSTEM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15422XJ 340B422 ALL OVERHEAD LIGHT ILLUMINATED AS SOON AS GEAR CAME UP, ILLUMINATED DIM WHEN LIGHTS ILLUMINATED FOR WARNING, NO CHANGE WITH WEU TEST. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED WEU P/N 0006WS00, S/N ON 1567, S/N OFF 1586. REMOVED AND REPLACED ICE PROTECTION PANEL DUE TO L ALPHA LIGHT ASSY BEING SHORTED, P/N 7239021-506, S/N ON 207880, S/N OFF 921834. OPS CHECKS GOOD. 2L72 4T RTA52EU 20040907002112004090700211EU 2004 9 7 MALA040532 120040724A33506122741 BATTERY BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHTSFAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15530XJ E2364 BATTERY PACK P/N 6122751, S/N 9805509 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 61-2274-1 AND ALL TESTS GOOD IAW CMM. 2H74 4F RTA49EU 20040907002132004090700213NM 2004 9 7 WLDA200441 120040802A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT BARREL NUT HOLE NR 32. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BARREL NUT HOLE NR 32 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040908000012004090800001NM 2004 9 8 150AW0036 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS827 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000032004090800003NM 2004 9 8 150AW0038 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000052004090800005WP 2004 9 8 AALA20040909 120040828A3350 WIRE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW217548A 53030 RDU FORWARD GALLEY SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BROKEN BUTT SPLICE FOR WIRE TO FORWARD GALLEY SIDEWALL EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040908000062004090800006NM 2004 9 8 AALA20040917 120040829A3350 BATTERY PACK BOEING767 767323 1385205NM GE CF6 CF680C2B6 30025NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 DFW EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BOTTOM FORWARD LAVATORY FS3. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA1NM E13NE 20040908000072004090800007NM 2004 9 8 AALA20040906 120040827A3350 PLUG BOEING757 757231 1384950NM PWA 2037 PW2037 NE EMERGENCY LIGHT MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21723TW 29378 EMERGENCY FLOOR TRACK LIGHTING END PLUG MISSING AT SEAT 25C. INSTALLED END PLUG FOR EMERGENCY FLOOR TRACK LIGHTING AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM E17NE 20040908000082004090800008EU 2004 9 8 AALA20040913 120040829A3260DSB11021 SENSOR AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE MLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW2170073 516 INFLIGHT T 1165/28 GEAR WOULD NOT RAISE AFTER TAKE OFF IN GEAR POSITION SYSTEM 1. TRIED SYSTEM 2 IAW OPERATION MANUAL VOLUME 1. GEAR WOULD NOT RAISE. RETURNED FOR LANDING, LANDED WITHOUT INCIDENT. REPLACED RT BOGIE SYSTEM 1 AND 2 SENSOR AND REPLACED TARGET ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA35EU E13NE 20040908000102004090800010NM 2004 9 8 151AW0029 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 480 AT STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000132004090800013NM 2004 9 8 151AW0040 120040702A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER TIE CLIP CRACKED AT BS 727B AT STR 16 RT. REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20040908000142004090800014EU 2004 9 8 KBM2004F00191 120040807A6420350A33215001 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE T/R SPIDER WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 T/R SPIDER END BALL BEARINGS WORN BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040908000152004090800015SO 2004 9 8 FTU2004F00005 220040721A8530 SEAL BEECH 36 A36TC 1151603CE CONT O520 TSIO520UB 17040SO ENGINE DAMAGED B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05678DR EA216 AC ENGINE WAS DRIPPING OIL. ALL CYLINDERS LOOKED LIKE THEY HAVE BEEN REPLACED RECENTLY. FURTHER INVESTIGATION REVEALED MOST OF PUSH ROD HOUSING SEALS AT CYLINDER HEAD ATTACH POINT WERE DAMAGED OR NOT PROPERLY INSTALLED. IT HAS ALSO BEEN NOTICED THAT ECI PUSHROD HSG SEALS (GREEN) WHERE A LITTLE STIFFER THAN TCM (WHITE) SEALS. FURTHER INVESTIGATION REVEALED SOME OF CYLINDER HOLD DOWN NUTS WERE NOT INSTALLED ON CORRECT STUDS. ONE TYPE FOR THE OTHER 6 HOLD DOWN NUTS, AND A SPECIAL NUT PN 646312 FOR THE 7TH HOLD DOWN STUD. IT IS EVIDENT THAT THE 7TH STUD NUT NEEDS TO BE BETTER IDENTIFIED, DUE TO LOCATION OF 7TH STUD, WE FEEL THAT NUT SHOULD BE A 12 POINT NUT WITH A SPECIFIC COLORING TO INDICATE THE DIFFERENCE.1L71 3O3 O 3A15 E8CE 20040908000162004090800016 2004 9 8 MWEA040156 420040831A25655951782509 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE TAILCONE FAILED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31809ME 48071 TAIL CONE DID NOT DEPLOY WHEN TAIL CONE WAS DEPLOYED. FOUND SLIDE COVER NOT CORRECTLY ATTACHED TO HARD COVER. RECONNECTED SLIDE AND COVER ASSEMBLY. RETESTED TAIL CONE JETTISON AND SLIDE DEPLOYMENT. 2L72 4F4 F A6WE E9NE 20040908000212004090800021NM 2004 9 8 151AW0032 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 747 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000242004090800024EA 2004 9 8 D4O2004F00000 220040624A8520LW12186 NUT PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA CONNECTING ROD LOOSE E D4OAO OTHER RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE NRNOT REPORTED 1 EA2161MG 510 277405285 ENGINE SUFFERED CATASTROPHIC FAILURE. AT ENGINE TEARDOWN, THE NR 6 PISTON (FRAGMENTED), PISTON RINGS, CONNECTING ROD, ROD CAP, BEARINGS, ROD BOLTS, AND NUTS WERE FOUND IN THE OIL SUMP. ONE ROD BOLT WAS BROKEN AND ITS NUT WAS ON IT. THE OTHER ROD BOLT WAS NOT BROKEN AND ITS NUT WAS RECOVERED FROM THE OIL SUMP. ONE ROD BOLT WAS BROKEN AND ITS NUT WAS RECOVERED FROM THE OIL SUMP. POSSIBLE CAUSE IS A DEFECTIVE LOCK NUT. RECOMMEND CHECKING ROD NUT DRAG TORQUE WHEN ASSEMBLING CONNECTING RODS. 1L72 3O3 O 1A10 1E4 20040908000252004090800025CE 2004 9 8 240042 120040826A32341013841377 HANDLE BEECH 1900 1900D 1154162CE MLG FAILED A NSVAO OTHER J WARNING INDICATION DEDESCENT 1 EA27243CJ UE43 ON APPROACH LANDING GEAR DID NOT EXTEND. CREW PUMPED DOWN THE GEAR, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR HANDLE AND ACCOMPLISHED GEAR RETRACTION. OPS CHECKED IAW 32-30-01. 2L72 4T RTA24CE 20040908000262004090800026NM 2004 9 8 P9RA20040035 120040827A3350900835A BATTERY PACK BOEING727 7272J0 138407ENM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11906PG 20728 AIRCRAFT IN MAINTENANCE. CENTER FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 335001. 2L73 4F4 FRTA3WE E2EA 20040908000292004090800029CE 2004 9 8 2400421 120040826A32341013841377 HANDLE BEECH 1900 1900D 1154162CE MLG FAILED A NSVAO OTHER J WARNING INDICATION DEDESCENT 1 EA27243CJ UE43 ON APPROACH, LANDING GEAR DID NOT EXTEND. CREW PUMPED DOWN THE GEAR, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR HANDLE AND ACCOMPLISHED GEAR RETRACTION. OPS CHECKED IAW 32-30-01. 2L72 4T RTA24CE 20040908000322004090800032NM 2004 9 8 150AW0025 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 727B. STRINGER TIE CLIP REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040908000332004090800033NM 2004 9 8 150AW0029 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIP CRACKED AT STRINGER 6 RT BS 597. REPLACED STRINGER TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20040908000362004090800036SO 2004 9 8 C2XA04CL083 120040819A2150M83536 RELAY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL A/C PACK INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2726545 EMB145LR THE CREW REPORTED THE APU TEMP WENT AMBER DURING ENGINE START AND A STRONG ODOR OF FUEL IN THE COCKPIT. MAINTENANCE FOUND THE RT AIR CONDITIONING PACK DID NOT SHUT OFF DURING ENGINE START. THEY REPLACED RELAY K0320 AND THE APU OPERATED PROPERLY WITH NO ODOR OR TEMP SPIKE DURING ENGINE START. 2L72 4T4 FRTT00011ATTE6CH 20040908000382004090800038SO 2004 9 8 C2XA04TY157 120040820A532014524131009 CHANNEL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 DURING A SCHEDULED 4C INSPECTION THE PAX DOOR SILL U CHANNEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR SILL U CHANNEL IAW THE MFG SRM. AIRCRAFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION. 2L72 4F4 FRTT00011ATTE6CH 20040908000392004090800039SO 2004 9 8 C2XA04IA106 120040819A499049523971 THERMAL SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL APU INOPERATIVE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW27145421264 1264 145547 THE CREW REPORTED APU FAIL ON GROUND AND AUTO SHUTDOWN IN FLIGHT WITH A FUEL ODOR PRESENT. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE APU ON MEL 49-00-00 CONTROL NR 045133, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/21/04 THE AIRCRAFT RETURNED WHERE MAINTENANCE REMOVED AND REPLACED THE APU HIGH OIL TEMP SWITCH, AND REMOVED THE APU FROM MEL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040908000412004090800041NE 2004 9 8 0401436718 220040824A7200 ENGINE BOEING747 747251F 1384898NM PWA JT9 JT9D7J 52054NE NR 2 FIRE A NWAAF ACTIVATE FIRE EXT. AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 GL01618US 21122 662587 DURING TAXI IN, THE NR 2 ENGINE FIRE WARNING ANNUNCIATED. THE CREW SHUT DOWN THE ENGINE AND DISCHARGED THE LT FIRE BOTTLE FOR NR 2 ENGINE. THE FIRE WARNING CEASED. NO OTHER ABNORMAL ENGINE INDICATIONS WERE OBSERVED. MAINTENANCE INSPECTION FOUND EVIDENCE OF A FIRE AND THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E20EA 20040908000442004090800044NE 2004 9 8 AALA20040899 220040823A7261 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT MAKING METAL A AALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW219412W 53187 718037 ON CLIMB OUT LT ENGINE OIL STRAINER CLOGGED LIGHT ON MASTER CAUTION ILLUMINATED. STAYED IN LIMITS OIL TEMPERATURE AND OIL PRESSURE DURING CRUISE AFTER APPROXIMATELY ONE PLUS 45 INTO FLIGHT OIL TEMPERATURE CLIMBED OUT OF LIMITS. LT ENGINE SHUTDOWN ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. NORMAL SHUTDOWN WINDMILL 27 MINUTES MAX NR 1 20 PERCENT MAX NR TWO 27 PERCENT PRESSURE 322. LANDED WITHOUT INCIDENT. FOUND EXCESSIVE FERROUS METAL IN FILTER AND OIL TANK. REPLACED LT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRT E9NE 20040908000452004090800045NE 2004 9 8 DL76G040813 220040826A7200 ENGINE BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO271605 1811515422 30198 706114 PERFORM WIGGLE CK INSP OF NR 2 ENG 5TH STG VSV LEVER ARMS ME 01 OF EA 48-086303-12 REV A. REPLACED ENGINE ETOPS CATEGORY F: ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F4 FRTA1NM E13NE 20040908000462004090800046NM 2004 9 8 ABXA040298 120040824A5310 STRUCTURE BOEING767 767281 1385109NM GE CF6 CF680A 30025NE AIRFRAME VIBRATION A ABXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL23774AX 22789 AIRCRAFT HAD AN UNUSUAL VIBRATION. COCKPIT WAS OSCILLATING UP AND DOWN APPROXIMATELY 3 CYCLES IAW SECOND. SLOWED AC TO 280 KIAS, NO CHANGE. AFTER TRANSITION TO MACH NR, OSCILLATION ABATED AS THE IAS DECREASED THROUGH 270 KNOTS. ALL ENGINE INDICATIONS WERE NORMAL. VIBRATION WAS EVIDENT IN SEAT AND FLOOR OF COCKPIT. NO OSCILLATION/VIBRATION WAS FELT IN THE FLIGHT CONTROLS. ALTITUDE WAS 11,000 FEET THROUGH FL330. AT CRUISE, FL 350, .8A M, VIBRATION IS NOT NOTICEABLE. VISUAL INSP OF HORIZ, STAB JACKSCREW AND SURROUNDING AREA, NO DEFECTS NOTED. RAN STAB THROUGH FULL RANGE OF MOVEMENT. CHECKED GOOD. PERFORMED MXSP TEST 68. STAB CHECK GOOD. FUNCTIONAL CHECK FLIGHT PERFORMED. ALL SYSTEMS CHECKED GOOD. 2L72 4F4 FRTA1NM E13NE 20040908000522004090800052 2004 9 8 ASMF200408021 420040822A2230S254N1022 ACTUATOR BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE THRUST LEVER FAILED W ASMFC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW23801AM35625 25624 AIRCRAFT PERFORMED REJECTED TAKE OFF, DURING TAKE OFF RT AUTOMATIC THRUST LEVER WAS JAMMED. DURING MAINTENANCE REVISION, AUTOMATIC THRUST LEVER MOVEMENT WAS CHECKED AND SYSTEM WAS DEFERRED IAW MEL 22-30-1. DURING OVERNIGHT SERVICE, RT THRUST LEVER INTERLOCK WAS REPLACED IAW MM 78-34-03, TEST CORRECT AND DEFERRED REPORT WAS CLOSED. 2L72 4F4 FRTA2NM E17NE 20040908000542004090800054NM 2004 9 8 ANCF200400029 120040828A3000320115 VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE ANTI ICE FAILED W ANCFO OTHER J WARNING INDICATION CLCLIMB 1 SO23190AN101144310 53190 DURING INITIAL CLIMB RT ENGINE LOOP-A ILLUMINATED INTERMITTENTLY AT FIRST, THEN RT ENG FIRE HANDLE CAME (ON) WITH THE AURAL ALARM .WITH INCREASING OIL AND FUEL TEMPERATURE WITH EOAP ANNUNCIATION OF RT ENG VALVE AND RT ANTI-ICE (ON). PROCEDURE WAS ACCOMPLISH. WAS CHECKED UPPER FUEL HEATER TUBE AND WAS FOUND BROKEN IAW AMM 73-14-02 PAGE 202 TO 205. THE UPPER FUEL HEATER TUBE WAS REPLACE AND PERFORMED ENG RUN UP IAW AMM 71-00-00 P501 TEST OK. P/N. OFF. 780956 P/N ON. 780956 IAW AMM 75-10-01 PAGE 202-206 ITS WAS REPLACED RT ENG VALVE AND WAS PERFORMED OPERATIONAL TEST IS NOW OK. IAW AMM 73-14-02 PAGE 202/205 WAS REPLACED, AIR SHUT OFF VALVE. 2L72 4F4 FRT E9NE 20040908000552004090800055EU 2004 9 8 KBM2004F00195 120040602A6520350A33105803 CONTROL LEVER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE T/R GEARBOX DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P69 2347 TAIL ROTOR GEARBOX BELLCRANK LEVER IS REMOVED DUE TO BUSHING DEBONDED. REINSTALLED BELLCRANK LEVER. BOND IS GOOD. REBONDED GS NEEDED PRIOR TO INSTALLATION. 1G71 3U3 UNCH9EU E19EU 20040908000632004090800063SW 2004 9 8 KBM2004F00196 120040812A2933206075198005 RESISTOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUEL QTY IND INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 FUEL QUANTITY READING INTERMITTENTLY 35-40 GALLON. REPLACED R1 AND R2 RESISTOR WITH A NEW UNIT AND OPS CHECKED GOOD. 1G71 3U3 U H2SW E4CE 20040908000662004090800066EU 2004 9 8 KBM2004F00190 120040807A6720350A21136324 SUPPORT BRACKET SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE FUSELAGE CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 UNDERNEATH FLOOR T/R PEDAL BELLCRANK BRACKET SUPPORT IS CRACK. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040908000672004090800067EU 2004 9 8 KBM2004F00193 120040818A7921 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL COOLER BLOWEINOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 343 3141 MOTOR INOPERATIVE. INSTALLED NEW MOTOR. 1G71 3U3 U H9EU E19EU 20040908000682004090800068EU 2004 9 8 KBM2004F00211 120040602A2121050173 MOTOR SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL A/C BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 7 IN BLOWER MOTOR, NOT BLOWING COLD AIR. REMOVED AND REPLACED. 1G71 3U3 U H9EU E4CE 20040908000692004090800069EU 2004 9 8 KBM2004F00192 120040805A21210500846 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 AC INOPERATIVE RESET 1 AMP CIRCUIT BREAKER POPPED. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040908000712004090800071SW 2004 9 8 ALG2004F00040 120040628A7720 WARNING LIGHT BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE ILLUMINATED E ALGAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0341GH 45502 CAE860088 UPON HOVERING OUT EVERYTHING IN THE GREEN, TURNING DOWNWARD TO THE TAXI WAY LOOKING TO AVOID OBSTACLES GLANCING BACK AT INSTRUMENTS TOT RED LIGHT WAS ON, INDICATION WAS JUST ABOVE 810 DEGREES, BLEED AIR WAS ON. MAINTENANCE COMPLIED WITH A HOT END INSPECTION OF THE ENGINE NO DEFECTS WERE FOUND, OPS CHECK WAS GOOD. 1G71 3U3 U H2SW E1GL 20040908000722004090800072WP 2004 9 8 ASMF200407037 120040731A3030 HEATER DOUG DC9 DC987 3022087WP PITOT TUBE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23204AM 49404 AIRCRAFT RETURNED TO PLATFORM, PITOT STALL HEAT OFF LIGHT TURNED ON. DURING CHECK, TECHNICAL PERSONNEL CONFIRMED LT PITOT TUBE FAILURE. IT WAS REPLACED IAW MM 30-30-00, TEST CORRECT. 2L72 4F RTA6WE 20040908000732004090800073WP 2004 9 8 ASMF200408005 120040806A27802587794 CONTROL VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE LE FLAPS DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23751RA 49779 AIRCRAFT WAS SENT TO THE HANGAR TO ATTEND FLAPS DIFFERENCE INDICATIONS AND FLAPS DID NOT RETRACT COMPLETELY. FLAPS CONTROL VALVE AND INTERIOR FLAPS ACTUATORS WERE REPLACED IAW MM 27-50-01 AND 27-50-02, BUT FAIL CONTINUES. FLAPS CONTROL VALVE WAS REPLACED AGAIN AND FAIL WAS CORRECTED. DUE TO TESTS PERFORMING AUXILIARY HYDRAULIC PUMP WAS OVERHEATED. IT WAS REPLACED IAW 29-10-06, ALL TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E2EA 20040908000752004090800075NM 2004 9 8 HNAA0400109 120040810A6121 WIRE HARNESS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF* NE SYCHROPHASER CHAFED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07835EX 289 920318 FLIGHT NR 3822 HAD TO RETURN TO FIELD DUE TO THE RT PROP RPM SURGING ON CLIMB OUT. AIRCRAFT LANDED WITHOUT INCIDENT. CONDITION DID NOT EXIST WITH THE PROP SYNCHROPHASER OFF. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND CHAFED WIRES AT THE ENGINE HARNESS FOR THE SYCHROPHASER SYSTEM. WIRES WERE REPAIRED AND SYSTEM OPERATIONAL CHECKED. ALL CHECKS GOOD. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20040908000762004090800076CE 2004 9 8 PNSA040601 120040617A2720 ROLL PIN CESSNA208 208 2073702CE RUDDER PEDAL SHEARED E PNSAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 AL039304F 20800008 DURING TAXI LT RUDDER ROLL PIN PN NAS561C3-18 SHEARED CAUSING RUDDER PEDAL TO DISCONNECT AND CAUSE LOSS OF STEERING AND BRAKING ACTION ON LT SIDE. 1H71 3T NTA37CE 20040908000792004090800079EU 2004 9 8 KBM2004F00128 120040524A2121050143 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE A/C BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 AFT A/C BLOWER NOT WORKING. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040908000842004090800084EA 2004 9 8 COMA0460445 120040803A2133 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF341A NE CABIN PRESSURE OBSTRUCTED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01804CA 7352 FLIGHT 4952 AIRCRAFT WILL NOT PRESSURIZE. FOUND SAFETY WIRE IN OUTFLOW VALVE. REMOVED WIRE AND PRESSURE CHECK WAS NORMAL. 2L72 4F4 FRTA21EA E15NE 20040908000852004090800085EA 2004 9 8 COMA0460446 120040803A7932MS280343 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE RT ENGINE OIL MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01710CA 7241 FLIGHT 5492, RT ENGINE HIGH OIL TEMP. REPLACED THE OIL TEMP SENSOR. 2L72 4F4 FRTA21EA E15NE 20040908000862004090800086NE 2004 9 8 C8GA20040015 220040805A7261803686 GARLOCK SEAL BOEING727 727223 1384074NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE LEAKING A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15715AA 22470 685546 DURING CLIMB, AT APPROXIMATELY FL210, NR 1 ENGINE OIL QUANTITY BEGAN DROPPING RAPIDLY FOLLOWED BY OIL PRESSURE DROP AND WARNING LIGHT. PERFORM ENGINE INFLIGHT SHUT DOWN PROCEDURE. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT INCIDENT. FOUND GARLOCK SEAL LEAKING AT THE ENGINE DRIVEN HYDRAULIC PUMP. REPLACED SEAL. ENGINE RUN AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040908000872004090800087NM 2004 9 8 AWXA200400850 120040804A3397BMS13311122 WIRE BOEING737 73733A 1384673NM GE CFM56 CFM56* 13802NE SEAT ROW 23 LT LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT SPLICE SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040908000902004090800090NM 2004 9 8 UPS04M42960 120040614A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, RT HORT STAB NR 35 BARREL NUT HOLE FOUND CORRODED. CORROSION ON B/N HOLE NR 35 RT REMOVED, OPN BULKHEAD TRIMMED TO 0.26 INCH X 1.00 INCH TO GAIN ACCESS FOR REAMING FOUND EXCEEDED LIMIT IAW EO MD11-5510-1 9409-G.FAB AND REPAIR SLEEVE/B IAW EO MD11-5510-19409-G. REPAIR AND INSTALLED SLEEVE/B AT B/N HOLE NR 35 RT AND FAB REPAIR STRAP USING 7075-T-7351 IAW EN1214-04. REPAIR ACCOMPLISHED AT B/N HOLE NR 35 RT FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20040908000912004090800091NM 2004 9 8 UPS04M42961 120040529A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, RT HORIZ STAB BARREL NUT HOLE NR 6 FOUND CORRODED ON BOTTOM BEARING AND SI SIDEWALL AND SURFACE. CORROSION AT B/N HOLE NR 06 RT REMOVED AND REAMED TO 0.988 INCH AND BLEND TO 0.0 45 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-19409-G. FAB IAW REPAIR SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 AT B/N HOLE NR 06 RT IAW EN1235-04. REPAIR AND INSTALLED SLEEVE BUSHING AT B/N HOL E NR 06 RT IAW EO MD11-5510-19409-G AND EN1235-04 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20040908000932004090800093WP 2004 9 8 ABXA040294 120040810A53119919619506 FRAME DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23977AX 47513 RT AFT MAIN FRAME, STA. 775, AFT UPPER FLANGE WAS CRACKED BETWEEN POINTS G AND J. REPAIRED MAIN FRAME IAW EA 53400320-001-2. 2L72 4F4 F A6WE E2EA 20040908000952004090800095WP 2004 9 8 ABXA040296 120040817A32600080004003 CONTROL BOX DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE MLG MALFUNCTIONED A ABXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL23955AX619 47619 AFTER SELECTING GEAR DOWN, NOTED A RT GEAR UNSAFE LIGHT. THE LIGHT CHANGED FROM GREEN TO RED 3 TIMES. MISSED APPROACH AND CYCLED GEAR, UNLOCK REMAINED GREEN. (NOTE: INBOUND PROBLEM ON FLIGHT 194 8/16 OPS) PERFORMED SEVERAL GEAR SWINGS IAW AMM 32-60-00-2 WITH NO DEFECTS NOTED. REMOVED AND REPLACED PROX SWITCH CONTROL BOX AS PRECAUTION. ALL LANDING GEAR POSITION AND WARNING INDICATIONS NORMAL IAW AMM 32-00-00-2. 2L72 4F4 F A6WE E2EA 20040908000992004090800099NM 2004 9 8 AWXA200400769 120040710A5320D5347112420100 SHEAR PLATE AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-8, PG. 7-22. 2L72 4F4 FRTA28NM E311NE 20040908001032004090800103NM 2004 9 8 AWXA200400773 120040710A5315D534721720000 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68. FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2. 2L72 4F4 FRTA28NM E311NE 20040908001052004090800105NM 2004 9 8 WLDA200428 120040614A28202720121M51 VALVE DOUG MD11 MD11 3023602NM NR 1 TANK FAILED A WRLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11272WA 48437 AIRCRAFT N272WA FLT. NR WOA584 ON TAKEOFF ROLL, (TANK WING OVERFILL)LEVEL TWO ALERT, CREW ABORTED TAKEOFF TAXIED BACK TO THE GATE. MECHANIC FOUND NR 1 FILL VALVE FAILD, REPLACED THE VALVE SYSTEM CHECK NORMAL. 2L73 4F RTA22WE 20040908001062004090800106NM 2004 9 8 AWXA200400745 120040625A5321D5367180500200 FLOOR PANEL AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK FOUND CORROSION ON AFT SIDE CORNER OF FLOOR PANEL 261FF FROM FR 66 TO FR 68, AND Y1292 LT TO 1732 LT. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 261FF IAW AWA T/C C1D25310. 2L72 4F4 FRTA28NM E311NE 20040908001072004090800107NM 2004 9 8 AWXA200400746 120040626A5321D5361041900000 FLOOR PANEL AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 MAJOR REPAIR, DURING B-04 CHECK FOUND 2 EACH 1INCH CRACKS IN FLOOR PANEL 221EF. MAINTENANCE CUTOUT DAMAGE IN FLOOR PANEL 221EF, AND PERFORMED BOND REPAIR IAW A319 SRM 53-02-00, FIG. 202. 2L72 4F4 FRTA28NM E311NE 20040908001082004090800108SO 2004 9 8 CHQA000506 120040618A3320 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270SK 145304 EXIT ROW MARKER ON FLOOR FOUND INOPERATIVE. REMOVED AND REPLACED EXIT ROW LIGHT STRIP IAW MM CH 33-50-00. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040908001092004090800109SO 2004 9 8 CHQA000507 120040616A3350 LAMP EMB 145 EMB145LR 3260212SO WRIGHTR3350 981TC18EA1 67038EA OVERWING EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286 145443 RT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T4 RRTT00011ATE287 20040908001132004090800113EA 2004 9 8 SWIA200413743 120040612A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW PAX DOOR LOWER THRESHOLD FLOOR SUPPORT ANGLE CORRODED. ( ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED FLOOR SUPPORT ANGLE IAW CRJ 200 SRM CHAP. 51-42-01, 51-42-13, AND 51-42-21. 2L72 4F4 FRTA21EA E15NE 20040908001142004090800114NM 2004 9 8 QXEA200400523 120040713A5720 BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 RT WING LEADING EDGE HAS A CRACKED BLEED AIR ZEE BRACKET AT YW48. REPAIRED IAW 8-200 SRM 51-40-11 AND EA 2-57-267. 2H72 4T4 TRTA13NM E20NE 20040908001152004090800115NM 2004 9 8 QXEA200400518 120040711A5210 BUSHING DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 800 MISSING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09359PH14522 514 CREW REPORTED THE MAIN CABIN DOOR NOT OPENING FULLY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE THREADED BUSHING MISSING. A NEW BUSHING WAS INSTALLED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040908001162004090800116WP 2004 9 8 UPS04842883 120040630A5320 WEB DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, AFT PIT WEB CORRODED BETWEEN FS 1200 L35R. REMOVED WEB FROM STA 1160 TO 1220, MAT ID FOR WEB AND SPLICES 7075T6 .125 PO NR 424554.3 IAW DWG NR 3753772, FAB WEB AND SPLICES. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED WEB FROM STA 1160 TO 1220 L35R AND SPLICES IAW SRM 51-1-20D. AND T/R- 53-166. 2L74 4F4 FRT4A25 1E8 20040908001192004090800119EA 2004 9 8 SWIA200413744 120040820A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07908SW 7540 ON SHORT FINAL IB GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT MESSAGE. REMOVED AND REPLACED NR 2 SECU IAW MM 27-60-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040908001202004090800120EA 2004 9 8 SWIA200413745 120040822A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT MALFUNCTIONED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07917SW 7641 CEILING EMERGENCY EXIT SIGN DIM. REMOVED AND INSTALLED SERVICEABLE NR 2 BATTERY CHARGER UNIT. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040902002032004090200203SO 2004 9 2 SIMA200421602 120040802A261214534156401 CONTROL PANEL EMB 135 EMB135KL 3260302SO FIRE WARNING MALFUNCTIONED A SIMAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SW21817AE 145554 ORD - FLT 4269 - DURING FIRE TEST NO LIGHT IN THE BAGGAGE EXTINGUISHER BOTTLE INOPERATIVE ON EICAS. REPLACED FIRE PANEL AND BAGGAGE EXTINGUISHER BOTTLE, 337000271 S/N 41573D1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040902002052004090200205SO 2004 9 2 SIMA200421601 120040731A324431590 TIRE EMB 145 EMB145LR 3260212SO NR 2 SEPARATED A SIMAO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 SW21633AE 145148 FLT 3518 - XNA - ON TAKEOFF, NR 2 TIRE THREW THE TREAD. PERFORMED PRECAUTIONARY EMERGENCY LANDING IN DFW WITH NO INCIDENT. REPLACED NR 2 WHEEL ASSEMBLY AND REPLACED DAMAGED ENGINE NR 1 DAMAGED CORE VANES. A/C RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040903000092004090300009NM 2004 9 3 USAA040432 120040806A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH CIRCULAR AREA, SCREW HOLE ON FLOORBEAM T-CAP, STATION 1640 LBL 40. DAMAGE REMOVED, T-CAP REPLACED PER EA 95744. (M) 2L72 4F RTA2NM 20040903000152004090300015NM 2004 9 3 ASAA0410357 120040713A53306573742 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 FOUND FUSELAGE OUTER SKIN CRACKED. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040903000202004090300020CE 2004 9 3 2004F00270 120040419A55201016200111 BRACKET BEECH 1900 1900D 1154162CE RT STAB ELEVATORCORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO198153517931 UE147 AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M) 2L72 4T RTA24CE 20040903000212004090300021EU 2004 9 3 USAAEM04012 120040803A32349037B000102 CONTROL LEVER EMB ERJ170ERJ170100 EU MLG INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19808MD 17000021 LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE PILOT USED GEAR OVERRIDE TO RETRACT THE GEAR, IT CAME DOWN NORMALLY UPON EXTENSION. THE FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. (M) 2L74 4F RTA56NM 20040903000242004090300024NM 2004 9 3 ASAA0410356 120040713A53306573741 SKIN BOEING737 737298C 1384490NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND FUSELAGE OUTER SKIN CRACKED. REPAIRED CRACK AT CAPTAINS C-D WINDOW LOWER FORWARD CORNER BS 204.5. (M) 2L72 4F RTA16WE 20040903000252004090300025NM 2004 9 3 USAABB04074 120040804A335020131A BATTERY BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19653US 24894 CLT - FOUND FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 9 THROUGH ROW 17 LEFT INOPERATIVE. MAINTENANCE REPLACED THE M737 BATTERY. (M) 2L72 4F RTA1NM 20040903000272004090300027EU 2004 9 3 2004F00277 120040801A77143039242 SENSOR AEROSPATR42 ATR42300 8680920EU PWA PW121 PW121 52124NE RT ENGINE ERRATIC A SIMAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21141AE 141 120203 DURING CLIMB, RT ENGINE NP INDICATOR DROPPED FROM 86 PERCENT OT 65 PERCENT. CREW DECLARED EMERGENCY. REPLACED RIGHT ENGINE NP SENSOR. (M) 2H72 4T4 TRTA53EU E20NE 20040903000312004090300031 2004 9 3 UIEA200400081 420040424A34201491500102 INDICATOR BOEING747 747230B 1384889NM ADI INOPERATIVE A UIEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA15509MC 21221 ON TAKEOFF ABORTED FOR CAPTAINS AND FIRST OFFICER INSTRUMENT WARNING, ATT, AND MONITOR LIGHT WITH ASSOCIATED BELL. ALSO, ATT FLAG, WITH ADI INDICATOR ON CAPTAINS SIDE FULL DOWN. ABORT SPEED WAS APPROXIMATELY 85 KNOTS. REMOVED AND REPLACED CAPTAINS ADI, ACCOMPLISHED PER MM 34-21-00, AND INTERCHANGED INU POSITION LAND 3. ACCOMPLISHED MM 34-41-00. FUNCTIONAL CHECKED SATISFACTORY. NR 5 TIRE BLEW DURING ABORTED TAKEOFF. (M) 2L74 4F A20WE 20040903000322004090300032EU 2004 9 3 USAASA04075 120040729A3350321431 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19724UW 1122 THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. (M) 2L72 4F RTA28NM 20040903000332004090300033EA 2004 9 3 2004F00278 120040717A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA CABIN INOPERATIVE A FDKAK NONE L NO TEST ININSP/MAINT 1 SW07904FJ 15004 CREW REPORTED EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE TESTED SYSTEM AND COULD NOT DUPLICATE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS USED. (M) 2L72 4F RTA21EA 20040903000452004090300045WP 2004 9 3 MEX2004003 120040101A2720 PROXIMITY SENSOR DOUG DC9 DC987 3022087WP RUDDER MALFUNCTIONED A ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23205AM 49405 FLT 6428 - MEX-LAS - CAPTAIN REPORTED THAT DURING FLIGHT CONTROL TEST WITH THE RT RUDDER THE BLUE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' REMAINED ON. AT HANGAR, THE RUDDER PROXIMITY SENSORS WERE VERIFIED AND IT WAS DETECTED A TROUBLE IN ONE SENSOR TARGET. THE PROXIMITY SENSORS D1-33 AND D1-34 WERE ADJUSTED AND THE SYSTEM WAS TESTED IAW MM 27-20-00, ALL CORRECT. (M) 2L72 4F RTA6WE 20040903000532004090300053NM 2004 9 3 SWAA042545 120040831A53116978062 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME AT NR 5 STOP FITTING, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040907000072004090700007EA 2004 9 7 VNAA0408016 120040829A3411 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PITOT SYS MALFUNCTIONED A VNAAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 GL07250PS 7929 DURING CLIMBOUT, THE CREW RECEIVED A PITOT BASE HEAT, LT AOA, LT STATIC, AND LT PITOT HEAT CAS MESSAGES AND RETURNED TO PHL. MAINTENANCE INSPECTED AND RESET THE CIRCUIT BREAKERS IN ACCORDANCE WITH RJ-SL-00-00-1. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040907000162004090700016 2004 9 7 00145 420040527A341616007163 ALTIMETER LEAR 24 24D 5170311CE NR 1 FAILED E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05266TW1028110281 266 ON CLIMBOUT FROM KOSH THROUGH 6700 FT PILOTS ALTIMETER STOPPED CLIMBING. AIRCRAFT RETURNED TO POINT OF DEPARTURE FOR MAINTENANCE. REPLACED CAPTAIN'S ALTIMETER. 2L72 4J A10CE 20040907000182004090700018WP 2004 9 7 UPS04842745 120040616A53115613836 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, STA 35 AT LONGERON 22R CORRODED AT FRAME. REMOVED FRAME SECTION TO FOM FAB NEW FRAME SECTION AND SPLICES INSTALLED NEW FRAME SECTION AND SPLICES IAW DAC DWG 5613836 AND REO GO9859 AND DC8 SRM 51-1-21, 51-1-20D, 51-1-8. 2L74 4F RT4A25 20040907000202004090700020WP 2004 9 7 UPS04842747 120040614A5730576958989 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, RT WING L/E CENTER SECTION HAS CORROSION AROUND STALL WARNING SWITCH AND NUT PLATES. BASE DOUBLER FOR STALL WARNING SWITCH IS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 57-2-0. MAT ID 7075-T6 .063 PO 442960.4 FOR FAB OF NEW DOUBLER IAW DAC DWG 5769589. FAB NEW -89 DOUBLER. ALODINED AND PRIMED. INSTALLED DOUBLER. REMOVED STALL TRANSDUCER IAW DC8 MM 34-16-01. REINSTALLED STALL TRANSDUCER. OPS CHECKED GOOD IAW DC8 MM 34-16-00. 2L74 4F RT4A25 20040907000272004090700027EA 2004 9 7 VNAA0408013 120040820A2621 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU FIRE BOTTLE LOOSE A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07242JS 7911 THE CREW REPORTED THAT THE APU FIRE BOTTLE ARMED PUSH TO DISCHARGE GREEN LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND FOUND CONNECTOR 1PS1WA LOOSE. MAINTENANCE THEN RESECURED CONNECTOR 1PS1WA IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040907000282004090700028NM 2004 9 7 UPS04M42731 120040614A7160 SKIN DOUG MD11 MD11F 3023600NM NR 2 ENG INLET CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP INSPECTION TYPE:C2, NR 2 ENGINE INLET EXTERIOR SIDE LOWER FROM 4 TO 8 O'CLOCK HAS NUMEROUS CRACKS. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUTS. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLER IAW SRM 54-10-00 FIG 1B AND DWG ATC8311 IT-5. 2L73 4F RTA22WE 20040907000292004090700029EU 2004 9 7 AWXA200400926 120040805A5320D5348004320200 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK CORROSION WAS FOUND ON L-2 DOOR SILL, AT UPPER INBOARD END BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000502004090700050WP 2004 9 7 MWEA040154 120040825A53479957871501 SEAT TRACK DOUG DC9 DC981 3022081WP FUSELAGE WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 CAPTAIN'S AFT INBOARD SEAT TRACK IS WORN. FABRICATED AND INSTALLED CHANNEL. 2L72 4F A6WE 20040907000552004090700055EA 2004 9 7 COMA0460472 120040823A5210600315351001 FLANGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DENTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01477CA5851 7670 FWD AND AFT UPPER PASSENGER DOOR SEAL STRIKERS ARE DAMAGED. PERFORMED A MAJOR REPAIR TO FS 310.00 AND FS 349.00 UPPER PASSENGER DOOR SEAL STRIKER BY TRIMMING OUT DAMAGED AREAS, PERFORMED LPI, TOUCHED UP REWORKED AREA, FABBED STRAP AND INSTALLED IAW BOMBARDIR REO 601R-53-22-033 TYPE L. 2L72 4F RTA21EA 20040907000582004090700058WP 2004 9 7 UPS04842893 120040701A52305754075501 FITTING DOUG DC8 DC871F 302199DWP PIT DOOR WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, A PIT DOOR FWD UPPER LOCK PIN GUIDE FITTING WORN. REMOVED DAMAGED GUIDE FITTING IAW DC8 SRM 51-3-0. ORIG THICKNESS IS .250 REMAINING MAT .108 IAW DAC DWG 5754075. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 52-2-0. REC'D, LOCATED, DRILLED NEW GUIDE FITTING IAW DC8 SRM 51-1-24. REMOVED FASTENERS IN WEB. INSTALLED FITTING & FASTENERS IN WEB IAW DC8 SRM 51-1-21, 51-1-20D, & 51-1-20A. 2L74 4F RT4A25 20040907000642004090700064NM 2004 9 7 DL733040802 120040823A5330654577572 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 THE FUSELAGE SKIN WAS FOUND CRACKED AT FOUR LOCATIONS. THE CRACKS WERE ALL LOCATED ALONG THE EDGE OF THE UNDERLYING BONDED DOUBLER. A 1 INCH VERTICAL CRACK WAS FOUND AT FS 767 ABOVE STR 23R. A 3.5 INCH HORIZONTAL CRACK WAS JUST BELOW S-22R AT FS 760, A .25 INCH CRACK WAS JUST BELOW S-21R AT FS 760, AND A 1 INCH CRACK WAS JUST ABOVE S-21R AT FS 767. THE CRACKS WERE REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH DOUBLERS. 2L72 4F RTA16WE 20040907000672004090700067NM 2004 9 7 DL733040805 120040823A5330654577472 SKIN BOEING737 737347 1384647NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO273301 23181 TWO CRACKS WERE FOUND RUNNING ALONG THE BONDED SKIN DOUBLER LINE OF STRINGER 24L. ONE CRACK WAS JUST FWD AND THE OTHER JUST AFT OF A PREVIOUSLY INSTALLED SKIN REPAIR FOR REPAIR OF SIMILAR MILL LINE CRACKING. THE SKIN PANEL WAS CUT FROM THE STRINGER 20L LAP JOINT TO THE S-25L LAP JOINT AT FS 727C & 756. A NEW SKIN PANEL WAS SPLICED IN WITH ALUMINUM STRAP DOUBLERS PER ER/A 092754-14. 2L72 4F RTA16WE 20040907000702004090700070 2004 9 7 UPS04142829 420040731A25652LA00269900 INDICATOR AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 CREW ENTRY DOOR ESCAPE SLIDE INDICATOR INOP. REMOVED AND REPLACED ASPSU IAW 52-73-16-4, OPS CHECK NORMAL ON GROUND. PLACARD WAS REMOVED. CLEARED DEFERRAL M285209. 2L72 4F RTA35EU 20040907000932004090700093NM 2004 9 7 P5CA0401159 120040802A5532 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE HORIZONTAL STAB DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 HORIZONTAL STABLIZER RT PANEL NR 344 I/B DELAMINATED ON BACK SIDE. REMOVED AND BONDED AREA PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040907001042004090700104EA 2004 9 7 04186634 120040704A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27634BR 7287 DURING INSPECTION THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040907001122004090700112NM 2004 9 7 QXEA200400535 120040715A242011522183 GENERATOR BOMBDRDHC8 DHC8401 1390041NM ZONE 100 FAILED A QXEAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 NM09410QX751 751 4053 GEG - FLIGHT 2393 NR 2 AC CAUTION DURING TAKEOFF AT 60 KTS. NR 2 AC GENERATOR WOULD NOT RESET PER CHECKLIST. REMOVED AND REPLACED AC GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040907001162004090700116NM 2004 9 7 QXEA200400620 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT RAIL NR 11 HAS TWO EACH PITS OF CORROSION AT STATION 79 JUST ACROSS FROM RIGHT HAND EMERGENCY EXIT DOOR. BLEND .050 MATERIAL. TRACK OUT OF LIMITS REF RD 8/4-53-884. REMOVED AND REPLACED NR 11 SEAT TRACK. 2H72 4T RTA13NM 20040907001452004090700145EU 2004 9 7 AWXA200400670 120040605A5347D5347217820000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 RT INBOARD SEAT TRACK BETWEEN FR 47 AND FR 64. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 RT FROM FR 47 TO FR 64; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 53-00-15, FIG 202. 2L72 4F RTA28NM 20040907001532004090700153NM 2004 9 7 2004UALA00747 120040805A3350 LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29795UA 26927 3L CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. 2L72 4F4 FRTT0001SE E46NE 20040907001672004090700167NM 2004 9 7 AALA20040815 120040807A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21657AM 24615 DFW - EMERGENCY EXIT SIGN ABOVE LEFT AFT DOOR NUMBER 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN ABOVE LEFT AFT DOOR NUMBER 4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040907001742004090700174WP 2004 9 7 CALA0400600 120040813A53305911433 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, LONGERON 13L TO 14L. THE CRACKED AREA OF SKIN WAS CUT OUT AND FILLER AND A DOUBLER WERE INSTALLED IAW SRM 53-04, FIGURE 18 AND 51-10-3B. 2L72 4F A6WE 20040907001882004090700188 2004 9 7 04215650 420040802A2220 TRIM SYSTEM CNDAIRCL600 CL6002B19 1900309EA STAB INOPERATIVE A VTZAB EMER. DESCENT Z SIGNIFICANT FAILURE REPORT CRCRUISE 1 EA27650BR 7418 STAB TRIM FAIL EN ROUTE. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE LOCATION, DECLARED EMERGENCY. 2L72 4F RTA21EA 20040907001962004090700196 2004 9 7 MALA040535 420040817A34178220370123 ADC SAAB SF340 340B 7860101EU COCKPIT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15444XJ 340B444 ADC FAILED IN FLIGHT. PERFORMED QRH RESET CB'S F15 & F-14 ADC RETURNED AND FAILED A SECOND TIME. AIR RETURN TO DTW. MAINTENANCE REMOVED & REPLACED ADC P/N ON 622-4401-001, S/N ON 8129, P/N OFF 822-0370-123, S/N OFF 3304. OP CHECKS GOOD IAW THE SF340 MM CH 34-12-00-5. 2L72 4T RTA52EU 20040907002122004090700212EU 2004 9 7 MALA040518 120040717A5210RMRE050C TORQUE SHAFT BAC 146 AVRO146RJ85A1500097EU PAX DOOR INOPERATIVE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15505XJ E2313 MAIN DOOR WILL NOT OPERATE NORMALLY. MAINTENANCE REMOVED L-1 LOWER HINGE COVER, INSPECTED DOOR LIFTING MECHANISM, FOUND TO BE NOT OPERATING NORMALLY. INSPECTED A/C AND FOUND TO BE SAFE FOR ONE TIME FERRY FLIGHT FROM DFW TO MSP. VERIFIED SHOOT BOLTS ENGAGED. AIRCRAFT TO BE FERRIED FROM DFW TO MSP FOR REPAIR OF LT FWD MAIN PAX BOARDING DOOR MAIN CABIN DOOR NOT TO BE USED AS AN EMERGENCY EXIT. REMOVED AND REPLACED TORQUE SHAFT ROD END BEARING IAW CMM 52-10-14, P/N ON RMRE050C, OPS CHECKS GOOD. REINSTALLED LOWER HINGE COVER. 2H74 4F RTA49EU 20040908000192004090800019NM 2004 9 8 TSAA0477063 120040826A7711LG80A6 TRANSMITTER BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 1 ENG EPR INOPERATIVE A TSAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP13807AL 23443 ON TAKE-OFF ROLL THE NR 1 ENGINE ONLY INDICATED 1.76 EPR; THE THROTTLES WERE ADVANCED WITH NO RESPONSE FROM ANY INSTRUMENTS. REJECTED TAKE-OFF AND RETURNED TO GATE. REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND CLEARED THE PT2 INLET PROBE OF DEBRIS. RAN NR 1 ENGINE TO REFERENCE PARAMETERS IAW AMM 73-20-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A16WE E2EA 20040908000272004090800027 2004 9 8 KBM2004F00194 420040818A2312 DISPLAY SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE VHF RADIO INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P251 2347 VHF DISPLAY BAD. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040908000342004090800034NM 2004 9 8 151AW0037 120040702A5340 STRINGER CLIP BOEING737 7373G7 1384595NM STRINGER CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER TIE CLIP CRACKED AT BS 578 AT STR 9 RT. REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20040908000352004090800035NM 2004 9 8 151AW0038 120040702A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER TIE CLIP CRACKED AT BS 907 AT STR 6 RT. REPLACED TIE CLIP IAW SRM 51-10-02. 2L72 4F RTA16WE 20040908000372004090800037SO 2004 9 8 C2XA04TY156 120040819A532014528631403 CROSSBEAM EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714105 145649 DURING A SCHEDULED C CHECK INSPECTION, THE FWD CROSS MEMBER AT FRAME 20 WAS FOUND TO HAVE CORROSION AT BOTH ENDS. MANTENANCE REMOVED CORRODED AREAS, INSTALLED FILLER, SHIMS AND DOUBLER IAW THE MFG SRM. ACFT PENDING RELEASE UPON COMPLETION OF C-CHECK. 2L72 4F4 FRT TE6CH 20040908000472004090800047CE 2004 9 8 RDD2004F00000 120040519A8011S24752 CONTACTOR CONT CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO STARTER MOTOR FAILED W RDDRO OTHER O OTHER NRNOT REPORTED 1 WP21PKMPZ21 0428008 U20606130 532248 STARTER CONTACTOR REMAINED ENERGIZED AFTER START. AIRCRAFT WAS FLOWN THROUGH ONE ABBREVIATED CYCLE OF TAKE-OFF, PATTERN AND LANDING. UPON INSPECTION THE STARTER MOTOR WAS FOUND COMPLETELY DESTROYED. 1H71 3O3 O A4CE E8CE 20040908000602004090800060 2004 9 8 KBM2004F00209 420040628A34225050010902 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE COCKPIT INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 3535 2300 WILL NOT HOLD HEADING, REMOVED AND REPLACED DG. 1G71 3U3 UNCH9EU E19EU 20040908000772004090800077GL 2004 9 8 PNSA040604 320040628A6114 HUB CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA HARTZLH3B3M HCB3M GL PROPELLER DAMAGED E PNSAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL039820F 208B0410 BUA27129 SLUGGISH RESPONSE TO TAKEOFF POWER AND RPM/TORQUE DROPPED OFF AT FLIGHT IDLE POWER SETTINGS. AIRCRAFT MADE NORMAL LANDING WITH POWER LEVER FURTHER FORWARD THAN NORMAL. MAINTENANCE FOUND PROPELLER BLADE ANGLE IN HUB 2 DEGREES OFF AND BETA RING BENT. AT TEARDOWN BLADE HUB BOLTS WERE FOUND TO BE TIGHT AND BETA RING WAS REPLACED. 1H71 3T3 T A37CE E2NE 5 CP9NE 20040908000782004090800078EA 2004 9 8 PNSA040701 220040709A7313 LINE PIPER PA32 PA32301 7103207SO LYC O540 IO540K1G5 41532EA FUEL INJECTOR LOOSE E PNSAA UNSCHED LANDING KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL038470Y 328206012 DURING CLIMB WHEN POWER WAS REDUCED ENGINE FUEL PRESSURE DROPPED AND ENGINE POWER WAS PARTIALLY LOSS. AIRCRAFT RETURNED TO AIRPORT AND MAINTENANCE FOUND FUEL INJECTOR LINE HAD COME LOOSE. THIS WAS FIRST FLIGHT AFTER FUEL INJECTOR MAINTENANCE. 1L71 3O3 O A3SO 1E4 20040908000822004090800082SO 2004 9 8 C2XA04TY135 120040802A532014525422007 SILL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION THE RT FLOOR SILL WAS FOUND CORRODED AT FR 70. MAINT REMOVED AND REPLACED A NEW COUNTERSUNK FLOOR SILL ALLODINED AND INSTALL IAW 135/145 SRM 51-40-02;51-40-06 AND CPM 51-21-04. 2L72 4F4 FRTT00011ATTE6CH 20040908000922004090800092NM 2004 9 8 UPS04M42962 120040614A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE: C, LT HORIZ STAB BARREL NUT HOLE NR 31 FOUND CORRODED ON BOTTOM AND SIDEWALL SURFACE. CORROSION ON B/N HOLE NR 31 LT, REMOVED AND REAMED TO 1.178 INCH AND BLEND TO 0.0 75 INCH DEEP FOUND EXCEEDED LIMIT IAW EO MD11-5510-19409-G. REPAIR AND FAB SLEEVE BUSHING IAW EO MD11-5510-19409-G. APPLIED SEALANT PR1422B2 IAW EN 1227-04. REPAIR IAW INSTALLED SLEEVE BUSHING AT B/N HOLE NR 31 LT IAW EO MD 11-5510-19409-G AND EN1227-04 FOUND WITHIN LIMIT AND SATIS. 2L73 4F RTA22WE 20040908001102004090800110SO 2004 9 8 CHQA000508 120040618A3350 LIGHT EMB 135 EMB135KL 3260302SO ROW 7A INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11379 145606 EGRESS FLOOR STRIP LIGHTING FROM ROWS 7A TO 11A INOPERATIVE. REPLACED EGRESS LIGHTING STRIP IN AREA IAW 140 AMM 33-50-12. OPS CHECK GOOD. 2L72 4F RTT00011AT 20040908001122004090800112SW 2004 9 8 ALGA096565 120040717A6210206015001107 BLADE BELL 206 206L1 1182107SW MAIN ROTOR DEBONDED B ALGAK NONE O OTHER NRNOT REPORTED 1 SW03577E 3387 45577 DURING ROUTINE INSPECTION DISBOND WAS NOTED ON LOWER SURFACE OB OF GRIP FINGER. REPLACED UNIT W/NEW BLADE. 1G71 3U H2SW 20040908001212004090800121EU 2004 9 8 04FDEA02364 120040730A7714 SENSOR AIRBUS310 A310 EU GE CF6 CF680 30025NE T2 FAILED A FDEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO25429FE 364 429 77-15 0006235 30JUL04 IAH CLOSE R THREE TIMES DURING CLIMB NR2 ENG, SURGED A/C YAWED TO LT N1 CLIMB LIMIT EXCEEDED (ECAM) CL N' 100 PERCENT SURGE TO 115 PERCENT A/THR TRIPPED OFF LEVEL AT FL 290 CRUISE. ENG. N1 SURGE CR N1 91 PERCENT SURGED TO 105 PERCENT WITH A/C YAW SEVERAL TIME IN CRU. N2 EGT NORMAL. REPLACED T2 SENSOR, PERFORMED PULL TEST OF VSV FEEDBACK CABLE REF-73-21-01-5-B AND FOUND CABLE BINDING REPLACED SAME. 2L72 4F4 FRTA35EU E13NE 20040908001232004090800123EU 2004 9 8 S9HA095372 120040617A7931704A37642043 TRANSMITTER AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE OIL PRESSURE INOPERATIVE B S9HAK NONE N FALSE WARNING ININSP/MAINT 1 WP19351NT 1016 ENGINE OIL PRESSURE TRANSMITTER FAILED AFTER 0.0 HRS TSN. REPLACED WITH 3RD NEW TRANSMITTER . 1G72 3U3 U H11EU E19EU 20040908001242004090800124EU 2004 9 8 S9HA095371 120040617A7931704A37642043 TRANSMITTER AEROSPAS355 AS355* EU TMECA ARRIELARRIEL1 60030NE OIL PRESSURE INOPERATIVE B S9HAO OTHER P NO WARNING INDICATION CRCRUISE 1 WP19351NT2 1016 ENGINE OIL PRESSURE TRANSMITTER FAILED AFTER 1.5 HRS TSN. REPLACED WITH 2ND NEW TRANSMITTER WHICH FAILED AT 0.0 HRS TSN 1G72 3U3 U H11EU E19EU 20040908001252004090800125SW 2004 9 8 ALGA095348 120040616A6210206010200133 BLADE BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL MAIN ROTOR FLAKING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032155Z3237 3476 FOUND TRAILING EDGE EXTRUSION EXFOLIATED AT STA. 178.00. REMOVED BLADE FROM SERVICE. 1G71 3U3 U H2SW E4CE 20040908001262004090800126SW 2004 9 8 ALGA095354 120040617A6210206010200139 BLADE BELL 206 206B3 1181506SW MAIN ROTOR FLAKING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035011F2820 2564 MAIN ROTOR BLADE TRAILING EDGE EXFOLIATED APPROX. 14. 1G71 3U H2SW 20040908001282004090800128NM 2004 9 8 AWXA200400838 120040728A7797BACC63CN2016SN CONNECTOR BOEING737 73733A 1384673NM NR 2 ENG EGT DAMAGED A AWXAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 WP28173AW 23632 ABORTED TAKEOFF, ON TAKEOFF ROLL, ENROUTE, HAD NR 2 ENGINE EGT INDICATION OF 1250 DEGREE (C), REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED NR 2 ENGINE EGT CONNECTOR (D3304) AT ENGINE FIRE WALL. PERFORMED HIGH POWER ENGINE RUN, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040908001302004090800130 2004 9 8 AWXA200400840 420040730A3414 PITOT HEAD AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE AIRSPEED IND OBSTRUCTED A AWXAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 WP28620AW3691020967 052 ON 2ND ATTEMPT OF TAKEOFF EN ROUTE, CAPTS AIRSPEED IND SLOW TO INCREASE & 35 TO 40 KTS BELOW FO`S IND, REJECTED AT 80 KTS. MX R & R NR 1 ADIRU IAW T/C & NR 1 ADM, OPS CHK GOOD. AGAIN REJECTED T/O FOR CAPTS AIRSPEED IND 35 TO 40 KTS BELOW FO`S IND. MX R & R CAPTS PITOT PROBE IAW AMM, R & R NR 1 ADM IAW AMM DUE TO POSSIBLE CONTAM, & R & R HOSE BETWEEN PITOT PROBE & ADM. PERFORMED AIR DATA ADJUSTMENT, LEAK CHK GOOD. TEST OF ADIRU CONFIRMED FAILURE OF UNIT, REPLACED GYRO. INCOMING TEST OF ADM, NO FAULT FOUND, CALIBRATED UNIT & RETURNED TO SERVICE. AIRBUS PERFORMED FAILURE ANALYSIS OF ADM, HOSE, & PITOT PROBE. FOUND NO DEFECTS, BUT PITOT PROBE FOUND BLOCKED BY FOD. BLOCKAGE SEVERE ENOUGH TO RESTRICT AIRFLOW. 2L72 4F4 FRTA28NM E311NE 20040908001322004090800132NM 2004 9 8 WLDA200430 120040720A324426094712 TIRE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE MLG SEPARATED A WRLAO OTHER O OTHER LDLANDING 1 SO11277 NR 8 TIRE CAP SEPARATION: ON ARRIVAL FOUND NR 8 TIRE CAP SEPARATED AND RT IB FLAP OB EXTENSIVE DAMAGE. REMOVED AND REPLACED NR 8 MWA AND SERVICED TO CORRECT LEVEL. LEAK CHECKED IAW MM32-42-01. REMOVED AND REPLACED RT IB FLAP AND RT IB VANE ASSEMBLY IAW MM PROCEDURES. OPERATION CHECK NORMAL IN ALL RANGES. 2L73 4F4 FRTA22WE E24NE 20040908001372004090800137NE 2004 9 8 MALA040534 220040813A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FLUCTUATES A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15454XJ 340B454 GEE785770 A/C RETURNED AFTER TAKEOFF WITH THE LT ENGINE SHUTDOWN DUE TO PROP RPM FLUCTUATIONS. AIR RETURN TO FSD. MAINTENANCE REPLACED LT ENG ASSY, REF JOB CARD 7100-301 FOR OPS AND LEAK CHECKS AND WORK DETAILS. 2L72 4T4 TRTA52EU E8NE 20040908001402004090800140NM 2004 9 8 HNAA0408107 120040731A33506038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE EMERGENCY EXIT INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07835EX 289 FLIGHT REPORTED THE EMERGENCY EXIT LIGHT OVER THE CABIN DOOR AS BEING INOPERATIVE. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED THE BATTERY POWER SUPPLY AT POSITION NR 100. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040908001432004090800143NM 2004 9 8 DHL2004747005 120040804A3241423071 CONTROL UNIT BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE ANTI SKID SYS INOPERATIVE A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01747DH 22253 MAIN GEAR ANTI- SKID OB INOPERATIVE, (LIGHT REMAINED ILLUMINATED AND IB INOPERATIVE LIGHT WOULD NOT TEST. TO ADD , OB ANTI SKID ILLUMINATED WHILE ON APPROACH. REMOVED AND REPLACED ANTI-SKID CONTROLLER IAW MM 32-42-0. NO DEFECTS NOTED. 2L73 4F4 F A3WE E2EA 20040908001462004090800146NM 2004 9 8 C1HA200485007 120040808A1420 CONNECTOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE MLG DOOR DAMAGED A C1HAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL15685CA 22492 WHILE CONFIGURING FOR LANDING, LOWERED LANDING GEAR AND RECEIVED (3 GREEN) BUT ALSO DOORS ANNUNCIATOR ON FORWARD PANEL AND LT MAIN GEAR DOOR LIGHT ON FE PANEL. ACCOMPLISHED GO-AROUND IAW COM, CONTACTED MAINT. CONTROL AND RETURNED TO LAND. AFTER INSPECTING GEAR DOORS THROUGH VIEW PORT, NON EVENTFUL LANDING WITH NORMAL GEAR INDICATIONS. FOUND PIN PUSHED BACK AT L GEAR DOOR DOWN CONNECTOR. RE-TERMINATED CONNECTOR OPS CHECKED NORMAL, RE-TERMINATED R GEAR DOWN CONNECTOR, PRECAUTIONARY, OPS GOOD REF, 32-12-00. 2L73 4F4 F A3WE E2EA 20040908001482004090800148EU 2004 9 8 HAEA200400161 120040804A3260A24239108 UPLOCK SWITCH AMD FALC20FALCONE 2720305EU MLG FAILED E HAEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05285TW2086020860 285 AIRCRAFT DIVERTED. PILOTS REPORTED THAT THE GEAR WOULD RETRACT BUT THE GEAR DOORS WOULD NOT CLOSE. MAINTENANCE FOUND RT GEAR UPLOCK SWITCH BAD. REPLACED SWITCH, OPS CHECK GOOD. . 2L72 4F A7EU 20040908001492004090800149SO 2004 9 8 CHQA000528 120040720A3350 FILLER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT MISSING A CHQAK NONE O OTHER ININSP/MAINT 1 GL11285SK 145435 EMERGENCY FLOOR PROXIMITY LIGHTS STRIPS ARE MISSING FILLER STRIPS. INSTALLED FLOOR PROXIMITY FILLER STRIPS IAW AMM 33-50-12. 2L72 4T4 FRTT00011ATTE6CH 20040908001512004090800151 2004 9 8 KBM2004F00213 420040630A2312064105430 RADIO SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL VHF COMM INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 57 3403 POWER KNOB BROKEN AND RADIO OPERATES INTERMITTENTLY. REMOVED AND REPLACED VHF COMM RADIO. 1G71 3U3 U H9EU E4CE 20040908001522004090800152EU 2004 9 8 KBM2004F00214 120040808A7720646600251 PROBE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE TEMP MALFUNCTIONED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 PROBE INDICATES 130 DEGREES ALL THE TIME. INSTALLED NEW TSN 0.0 PROBE AND OPS CHECK GOOD. 1G71 3U3 U H9EU E19EU 20040908001552004090800155NM 2004 9 8 CALA0400594 120040808A21216454052 FAN BOEING737 737824 13844BZNM GE CFM56 CFM56* 13802NE LT PACK INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW273326210784 32402 THE FLIGHT ATTENDANTS REPORTED GRAY SMOKE IN THE CABIN IN THE AREA AROUND THE OVERWING EXIT WHILE ENROUTE. THE ENTERTAINMENT SYSTEM WAS SECURED, CABIN LIGHTS WERE TURNED OFF AND THE IFE CIRCUIT BREAKERS WERE PULLED. THE SMOKE DISSIPATED AND THE FLIGHT WAS CONTINUED TO ITS ORIGINAL DESTINATION OF AUA WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE LT RECIRCULATION FAN WAS RUN WITH THE IFE SYSTEM OPERATING FOR OVER TWO HOURS AND THE SMOKE COULD NOT BE DUPLICATED. THE LT RECIRCULATION FAN WAS REMOVED AND REPLACED IAW MM 21-25-02 AS A PRECAUTIONARY MEASURE. 2L72 4F4 FRTA16WE E2GL 20040908001562004090800156WP 2004 9 8 UPS04842888 120040715A5313 LONGERON DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE AFT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, STATION 1770 LONG. 17L IS CRACKED REMOVED,FABRICATED AND REPLACED LONGERON IAW DWG. 5649327,AND SRM. 51-1-20D,51-1-21 2L74 4F4 FRT4A25 E2GL 20040908001572004090800157NM 2004 9 8 QXEA200400576 120040806A7921 OIL COOLER BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 CRACKED A QXEAK NONE K FLUID LOSS ININSP/MAINT 1 NM09408QX 4050 OIL COOLER EXIT OUTLET CRACK AT BOTH FORWARD LOWER CORNERS. REPAIRED IAW EA 6-79-29 AND RD 84-74-004. 2H72 4T4 TRTA13NM E00062EN 20040908001592004090800159SO 2004 9 8 C2XA04CL078 120040806A33503025103 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 FLIGHT NR 3233, THE CREW REPORTED THAT THE RT SIDE EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT SYSTEM. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040910000012004091000001EU 2004 9 10 2004F00280 120040808A3250125X1 ROLL PIN BAG JETSTMJETSTM3101 1500215EU NOSE STEERING SHEARED A TRBAO OTHER O OTHER NRNOT REPORTED 1 EA11404GJ 754 NOSE WHEEL STEERING FAILED WHILE ENTERING RUNWAY. ADVISED TOWER OF ABORT AND REJECTED THE TAKEOFF AT VERY LOW SPEED, APPROX 20 KNOTS AND RETURNED TO HOME BASE. REMOVED AND REPLACED SHEARED ROLL PIN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 20040910000022004091000002NM 2004 9 10 USAASB04109 120040811A3397 WIRE BOEING737 737401 1384701NM EMERGENCY LIGHT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19425US 23992 BDL - MAINTENANCE REPORTED THE AFT RIGHT EXERIOR OVERWING EMERGENCY LIGHT BECAME INOPERATIVE WHEN RESTORING WIRING TO PROPER CONFIGURATION FROM A PREVIOUS EMERGENCY LIGHT PROBLEM AT SEAT ROW 11ABC. MAINTENANCE REPLACED SECTION OF DAMAGED WIRE W1150-029-020 IN ASSOCIATION WITH BOEING WIRING SPM, CHAPTER 20. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (M) 2L72 4F RTA16WE 20040910000032004091000003NM 2004 9 10 USAASB04106 120040809A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19449US 24893 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A CHARGER ASSEMBLY ALONG WTH TWO BATTERY PACKS. OPERATIONAL CHECK GOOD. USAA (M) 2L72 4F RTA16WE 20040910000042004091000004NM 2004 9 10 USAASB04107 120040810A3350606171 SOCKET BOEING737 737401 1384701NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19404US 23886 BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EVACUATION LIGHT AT SEAT 22 ABC INOPERATIVE. MAINTENANCE REPLACED THE SOCKET ASSEMBLY FOR SEAT MOUNTED EMERGENCY EVACUATION LIGHT AT SEAT 22 ABC. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040910000052004091000005 2004 9 10 USAABB04077 420040811A2565 SLIDE BOEING767 767201 1385125NM R1 DOOR MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 PHL - DURING ANNUAL R1 DOOR SLIDE OPERATIONAL CHECK, THE SLIDE FAILED TO DEPLOY FULLY. THE CORNER OF THE SLIDE CAUGHT ON A DIAGONAL STRAP. THE SLIDE WAS REPLACED. (M) 2L72 4F RTA1NM 20040910000062004091000006NM 2004 9 10 USAA040420 120040809A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND BULKHEAD SKIN CRACKED .75 INCH, STATION 178 BULKHEAD LBL 5.7 ABOVE WL 184, INBOARD SIDE. REMOVED CRACK AND INSTALLED DOUBLER PER EO 5300V155. (M) 2L72 4F RTA16WE 20040910000082004091000008NM 2004 9 10 USAA040408 120040804A5753 SKIN BOEING737 7374B7 1384702NM AFT FLAP DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 PIT - FOUND AFT FLAP DISBONDED 12 INCHES LONG BY 4 INCHES AREA, RIGHT OUTBOARD TRAILING EDGE OF AFT FLAP CENTER SECITON OF FLAP. REMOVED AND REPLACED PER MM 27-51-39. (M) 2L72 4F RTA16WE 20040910000102004091000010NM 2004 9 10 USAA040413 120040807A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US50706 23930 CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D S-23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M) 2L72 4F RTA16WE 20040910000112004091000011NM 2004 9 10 USAA040414 120040804A5330 SKIN BOEING737 737301 1384611NM BS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US50702 23930 CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727E S23L. INSTALLED DOUBLERS PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20040910000122004091000012NM 2004 9 10 USAA040415 120040811A5711654532422 SPAR BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, AFT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED FREEZE PLUG PER EA 78781. (M) 2L72 4F RTA16WE 20040910000162004091000016NE 2004 9 10 2004F00284 220040715A7200486246001 SPACER SKRSKYS64 S64F 8142610NE PWA JT8 JT8D* NE COMPRESSOR ASSY CRACKED A E8KLK NONE O OTHER ININSP/MAINT 1 NM09159AC 64084 COMPRESSOR ASSY WAS REMOVED FROM AN AIRCRAFT FOR A 1000 HOURS SCHEDULED HOT SECTION INSPECTION. DURING TEST RUN, THE ENGINE EXPERIENCED VIBES WHICH WERE OUT OF ACCEPTABLE LIMITS. THE ENGINE WAS DISASSEMBLED AND CHECKED FOR BALANCE AND WAS FOUND TO BE OUT OF BALANCE. THE CORE WAS DISASSEMBLED, AND DURING INSPECTION, THE 2-3 SPACER WAS FOUND TO HAVE 2 CRACKS ON THE AFT SIDE AT THE SLEEVE HOLES AND 1 CRACK AT THE FORWARD SIDE AT THE SLEEVE HOLE. THE CRACKED SPACER WAS SENT TO NDT AND FPI AND EDDY CURRENT WAS PERFORMED AND CONFIRMED THE CRACKS FROM THE VISUAL INSPECTION. DURING RESEARCH OF THE PREVIOUS WORK PERFORMED, THE PART NR 486246-001 INDICATED THE SPACER HAD BEEN SOT PEENED IAW SB 6414. E8KL (M) 2G72 4U4 F H6EA E2EA 20040910000172004091000017CE 2004 9 10 2004F00285 120040813A5310 STRUCTURE CESSNASTC STC206C 1182107CE AIRFRAME VIBRATION A ALGAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW031078N 45389 TRANSITION INTO CRUISE FLT PRODUCED A LATERAL LOW FREQUENCY VIBRATION, RETURNED TO ICY. MAINTENANCE VISUALLY INSPECTED AIRCRAFT FOR DISCREPANCY, NO DEFECTS NOTED THAT WOULD CAUSE A LATERAL VIBRATION, COMPLIED WITH A OPS CHECK FLIGHT AND NO LATERAL VIBRATION WAS PRESENT, VERY WINDY CONDITIONS. ALGA (M) 1H71 3O NTA4CE 20040910000252004091000025NM 2004 9 10 AMTA200400978 120040804A2760332150014 PCU BOEING757 75723N 1384973NM SPOILERS MALFUNCTIONED A AMTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL11516AT 27972 SPOILER LIGHT ILLUMINATED, EICAS MSG SPOILER DISPLAYED WITH SPOILERS SELECTED DOWN AIRPLANE WAS ON THE GROUND. PER FIM 27-61-00 PCA NR 8 FAULT WAS NOTED ON BITE TEST. REMOVED AND REPLACED PCA NR 8 PER 27-61-02-2. PERFORM TEST PER 27-61-022, NO MESSAGES OR LEAKS NOTED AT THIS TIME. (M) 2L72 4F RTA2NM 20040910000282004091000028NM 2004 9 10 USAA040406 120040729A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19444US38269 24862 CLT - FOUND SKIN CRACKED .625 INCH, BS 727D S23 LEFT. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M) 2L72 4F RTA16WE 20040910000302004091000030NM 2004 9 10 USAA040425 120040811A5320 MOUNT BOEING737 7373B7 1384580NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND MOUNT HOLE BORE, DAMAGE TO BORE OF MOUNT HOLE, AFT OUTBOARD MOUNT HOLE FOR RAM AIR DUCT LEFT SIDE. OVERSIZED HOLE, INSTALLED FREEZE PLUG PER EA 78847. (M) 2L72 4F RTA16WE 20040910000312004091000031NM 2004 9 10 USAA040434 120040731A5330 SKIN BOEING737 7374B7 1384702NM BS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41533 24548 PIT - PRESSURE DECK SKIN CRACKED 1 INCH, BEADED PRESS DECK, WHEEL WELL CEILING, BS 663.75 AT LBL 32. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-09 AND EA 78837. (M) 2L72 4F RTA16WE 20040910000322004091000032NM 2004 9 10 AMTA200401027 120040811A3350 LIGHT BOEING757 75723N 1384973NM CABIN LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11520AT 27976 FOUND ROW 32 SEAT CDF TRACK LIGHT FLOOR PATH ESCAPE LIGHTING INOPERATIVE. SECURED TRACK LIGHT, LIGHT OPS OK. (M) 2L72 4F RTA2NM 20040910000342004091000034NM 2004 9 10 AMTA200401006 120040808A2611 WARNING LIGHT BOEING757 75733N 1384931NM RT ENGINE ILLUMINATED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11559TZ 32593 FOUND EICAS STATUS MESSAGE, R TURB OH DET 1 DISPLAYED. PERFORMED FIM 26-13-00 ENGINE TURBINE COOLING OVERHEAT DETECTION BITE TO BLOCK 5 FIG 103 SHEET 3 THE COMPONENTS AND WIRE INTERFACE OPERATE CORRECTLY. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040910000392004091000039NM 2004 9 10 USAA040421 120040809A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND BULKHEAD SKIN CRACKED .5 INCH, BL 0, WL 186, STATION 178 BULKHEAD. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-10-08, FIG 203. (M) 2L72 4F RTA16WE 20040910000412004091000041NM 2004 9 10 USAA040435 120040804A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FUSELAGE FRAME CRACKED 1 INCH, AT BS 601 RIGHT, BOTTOM OF FRAME BELOW CABIN FLOOR. INSTALLED REPAIR ANGLE PER TR 53-62-01 AND EA 78833. (M) 2L72 4F RTA16WE 20040910000432004091000043NM 2004 9 10 USAA040433 120040723A53111131754 FRAME BOEING737 7374B7 1384702NM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FRAME CRACKED .5 INCH LONG, CRACK AT RIVET HOLE, FRAME 727F BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER REPAIR PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20040910000452004091000045EU 2004 9 10 USAA040427 120040806A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US15460 1052 CLT - FOUND FLOORBEAM CORRODED 5 SQUARE INCHES BY .030 INCH, FRAME 65-66 Y 765. INSTALLED DOUBLER PER EA 95741. (M) 2L72 4F RTA28NM 20040910000482004091000048NM 2004 9 10 UIEA200400143 120040807A75001J10500 VALVE BOEING747 747228F 1384895NM NR 4 ENGINE MALFUNCTIONED A UIEAEC ENGINE SHUTDOWN ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 EA15536MC 21576 MXP-ALA - AT 1741Z ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS EXPERIENCED THE NR 4 ENGINE FIRE INDICATION. N1 SET AT 106.0. PERFORMED A REJECTED IAW THE FHB. ONCE STOPPED, THE ENGINE FIRE CHECKLIST WAS ACCOMPLISHED. JUST PRIOR TO ROLLING, NR 4 ENGINE FIRE SWITCH FIRE LIGHT DID EXTINGUISH. AT 1741Z AFTER THE REJECT, THE BRAKE OVERHEAT LIGHT ILLUMINATED FOR ALL WING AND BODY GEAR. ALL OVERHEAT METERS INDICATED IN THE RED ZONE. TOW WAS 319.0 KGS, REJECT SPEED WAS 120 KTS. DURING NR 4 ENGINE INSPECTED NO SIGN OF FIRE NOTE. FIRE WARNING WAS INITIATED BY HEAT CAUSED BY LOOSE CLAMP ON HIGH STAGE VALVE DUCT AND CONSEQUENT AIR LEAK. CLAMP REPSOITIONED AND SECURED PROPERLY INSTALLED. PERFORMED NR 4 ENGINE PNEU2L74 4F A20WE 20040910000502004091000050NM 2004 9 10 UIEA200400142 120040804A3246215152 WHEEL BOEING747 74747UF 1384949NM LEFT MLG DAMAGED A UIEAO OTHER MJ OVER TEMP WARNING INDICATION LDLANDING 1 EA15418MC 32840 HOT BRAKES ON LEFT WING GEAR AND LEFT BODY GEAR. INSPECTION OF AFFECTED WHEELS AND BRAKES CARRIED OUT TASK, 5-51-10-202-001. NR 1 AND NR 6 AXLE INSPECTED FOR HEAT DAMAGE, NONE EVIDENT TASK 05-51-10-202-001. (M) 2L74 4F RT1384945 20040910000522004091000052NM 2004 9 10 UIEA200400140 120040820A32302670112M1 SEQUENCE VALVE BOEING747 7472D3B 1384805NM NLG FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15505MC 21251 AFTER TAKEOFF, ON GEAR RETRACTION NOSE LANDING GEAR DOORS KEPT CYCLING, ATTEMPTED RECYCLE NO EFFECT. REMOVED AND REPLACED NOSE GEAR, OPERATED DOOR SEQUENCE VALVE PER MM 32-34-08 PAGE 401-405, OPS AND LEAK CHECK NORMAL. UIEA (M) 2L74 4F RTA20WE 20040910000552004091000055NM 2004 9 10 UIEA200400146 120040812A32331U11715 ACTUATOR BOEING747 74747UF 1384949NM MLG MALFUNCTIONED A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15497MC 29258 - REJECTED TAKEOFF DUE TO WARNING BODY GEAR STEERING CONFIGURATION. GEAR CONTROL ON TAKEOFF ROLL AT 30 KNOTS. PERFORMED RECHECK FOR CORRECT DE-ACTIVATION, ALL CHECK OK. REMOVED BLANKS ON DE-ACTIVATED ACTUATOR. FOUND TRAPPED PRESSURE IN ACTUATOR. RELEASED TRAPPED HYDRAULIC PRESSURE, ACTUATOR HOT MESSAGE ERASED AFTER PRESSURE RELEASED. SYSTEM OPS CHECK AND CONFIGURATION PER DDPG 32-53-01. (M) 2L74 4F RT1384945 20040910000572004091000057SO 2004 9 10 SIMA200421902 120040806A3350M390791229 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21725AE 145312 FOUND RT CABIN EMERGENCY EXIT SIGN LIGHTING INOPERATIVE. REPLACED CONNECTOR AND PIN AT SPLICE 9124. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040910000582004091000058NM 2004 9 10 C7WA200400002 120040211A5270 WARNING LIGHT BOEING727 7272J0 138407ENM MLG DOOR ILLUMINATED A C7WAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SO17902PG 20725 FLT RETURN, LT AND RT GEAR DOORS LIGHT ILLUMINATED. RECYCLED GEAR LIGHTS REMAINED ON. INSPECTED MAIN LANDING GEAR DOORS, NO DISCREPANCIES FOUND. RERACKED MAIN LANDING GEAR ACCESSORY UNIT. CYCLED DOORS SEVERAL TIMES MLG DOOR INDICATORS CHECKED NORMAL PER MM 32-61-0. (M) 2L73 4F RTA3WE 20040910000592004091000059EA 2004 9 10 ASOA04518 120040718A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BULKHEAD CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11915EV 7754 DURNG A C-CHECK IN MCN, THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 L/R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY PRESSURE BULKHEAD RT CLIP AT FS 625, NEAR STRINGERS 14 L/R IAW ASA EO 600-53-0174. (M) 2L72 4F4 FRTA21EA E15NE 20040910000612004091000061NE 2004 9 10 2004F00287 220040317A72618073071 LINE BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 2 ENGINE LEAKING A MYWAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19802MA 22433 ON CLIMB-OUT FROM MEM, NR 2 ENGINE OIL PRESSURE DROPPED TO 12 PSI. FOLLOWED AOM ABNORMAL PROCEDURES 2-A-19-10. SHUT DOWN NR 2 ENGINE AND RETURNED TO MEM. TROUBLESHOT NR 2 ENGINE. DISCOVERED OIL LINE BETWEEN FUEL OIL COOLER AND GEAR BOX CHAFING WITH OIL PRESSURE LINE CAUSING LEAK. REMOVED AND REPLACED TWO NR 2 ENGINE OIL LINES IAW 79-20-1. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER. OPS CHECK NORMAL IAW 71-00, NO LEAKS. RETURNED AIRCRAFT TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20040910000632004091000063EU 2004 9 10 2004F00289 120040123A3610 TRANSDUCER AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE BLEED PRESSURE MALFUNCTIONED A SOKFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23462TA 1334 FLT LR622 - DURING CRUISE, BOTH ENGINES BLEED SYSTEMS FAULT ECAM WARNING CAME ON. BOTH BLEED SYSTEMS WENT TO CLOSED POSITION AND THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING, INSPECTION WAS PERFORMED TO THE BLEED SYSTEM AND REPLACED ENGINE NR 1 TRANSDUCER BLEED PRESSURE REGULATOR P/N ZRA1990030 (8HA1) PER AMM 36-11-16, PRB VALVE P/N 6714D060000 PER AMM 36-11-52. ALSO, THE FAN AIR VALVE CONTROL THERMOSTAT P/N 342B030000 WAS REPLACED PER AMM 36-11-43. PNEUMATIC SENSE LINE P/N 55615847001 WAS REPLACED PER AMM 36-11-52 ON ENGINE NR 2. THE SYSTEM WAS TESTED PER AMM 36-11-16, 36-11-52 AND 71-00-00, WITH SATISFACTORY RESULTS AND THE AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F4 FRTA28NM E40NE 20040913000032004091300003NM 2004 9 13 2004F00292 120040104A7312320115 VALVE BOEING727 727276 138408RNM NR 2 ENG FUEL FAILED A FX7AEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO19908PG 20951 ENGINE NR 2 SHUTDOWN FOR PRECAUTIONARY REASONS HIGH OIL TEMPERATURE A/C RETURNED TO MIAMI WITHOUT INCIDENT. FOND NR 2 ENGINE FUEL HEAT VALVE FAILED IN OPEN POSITION, SECURED SAME IN THE CLOSED POSITION PER MEL 73-2. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. (M) 2L73 4F RTA3WE 20040913000062004091300006EU 2004 9 13 ASOA04438 120040619A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11536AS 465 DURING A GROUND INSPECTION IN ATL, BOTH MIDDLE EMERGENCY CEILING LIGHTS AND HALF OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD MIDDLE EMERGENCY LIGHTS POWER SUPPLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040913000082004091300008CE 2004 9 13 2004F00293 120040812A26124940 CONTROL UNIT CESSNA750 750 2076810CE FIRE DETECTION INTERMITTENT A YYNAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL235113 7500013 FOUND LEFT ENGINE FIRE WARNING ILLUMINATED WITH APU RUNNING AND ENGINE OFF. FIRE DETECTION CONTROL UNIT CAUSING INTERMITTENT FIRE WARNINGS. LONG BEACH CESSNA SERVICE CENTER REMOVED AND REPLACED THE LEFT ENGINE FIRE WARNING CONTROL UNIT. OPERATIONAL TEST PERFORMED AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20040913000102004091300010EU 2004 9 13 USAA040431 120040806A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US15460 1052 CLT - FOUND FLOORBEAM CORRODED 2 SQUARE INCHES BY .035 INCH AREA, FRAME 66-68 Y1292. REMOVED CORROSION PER SRM 51-74-00. (M) 2L72 4F RTA28NM 20040913000112004091300011NM 2004 9 13 USAA040399 120040808A53201130120 SUPPORT BRACKET BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US50329 23935 PIT - FOUND THREE BRACKETS CRACKED, FORWARD .1875 INCH, AFT 1 INCH AND 1.5 INCH, FORWARD ENTRANCE DOOR TOP LINER SUPPORT BRACKET NEAR TOPGATE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20040913000132004091300013EU 2004 9 13 USAASA04073 120040722A335032145410 PSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19114UW 1148 DCA - THE EMERGENCY LIGHTS FAILED THE OPS TEST. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY EXIT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040913000142004091300014NM 2004 9 13 2004F00295 120040520A3230BACP30F7 PULLEY BOEING727 7272F9 138407DNM LT MLG DOOR FROZEN A PCSAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO17199AJ 21426 FLT CREW REPORTED, ON GEAR EXTENSION LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. MLG MANUALLY EXTENDED. A/C LANDED WITH NO FURTHER INCIDENT. MXE FOUND TWO FROZEN PULLEYS ON DOOR SAFETY VALVE CONTROL CABLES. REMOVED AND REPLACED PULLEYS IAW MM 20-20-4. ALSO, FOUND MLG DOOR SAFETY VALVES CABLES WERE OUT OF ADJUSTMENT. CABLES ADJUSTED IAW MM 32-34-0. OPERATIONS CHECK OK. LUBED LEFT MAIN LANDING GEAR IAW MM 12-21-1, PAGE 201. PERFORMED NORMAL AND EMERGENCY GEAR OPERATION IAW MM 32-52-0, PATE 501 AND MM 32-34-0, PAGE 507 TO INCLUDE INDICATION CHECKS. VISUALLY INSPECTED LEFT MAIN LANDING GEAR SIDE STRUT INSTALLATION FROM WHEEL WELL SIDE. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040913000152004091300015EU 2004 9 13 USAASA04072 120040717A335032145410 PSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19743UW 1277 THE EMERGENCY LIGHTS FAILED OPS TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040913000172004091300017NM 2004 9 13 USAASB04091 120040714A2170V1211 COALESCER BAG BOEING737 7373B7 1384580NM PACK BAY CONTAMINATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19504AU 23379 CLT - FLT 983 - EN ROUTE FROM MCI-CLT, CREW REPORTED ANODOR OF JET FUEL PRESENT IN THE CABIN WITH APU AIR ON. THEN ON DESCENT INTO CLT, THE JET FUEL ODOR BECAME PRESENT IN THE COCKPIT WITHOUT THE APU RUNNING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED BOTH THE LEFT AND RIGHT WATER SEPARATOR BAGS. NO FUEL OR OIL ODOR WAS NOTED. REMOVED AND REPLACED BAGS. RAN PACKS WITH APU AND ENGINES. ALL CHECK GOOD. (M) 2L72 4F RTA16WE 20040913000182004091300018EU 2004 9 13 2004F00296 120040625A7700S218526 INDICATOR FOKKERF27 F27MK600 4990706EU TGT MALFUNCTIONED A COEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM13702FE 10350 DURING CLIMB-OUT FROM SEA, NR 2 TGT INDICATOR FLUCTUATED BETWEEN 0 AND 8000 DEGREES. FLIGHT RETURNED TO SEA FOR TROUBLESHOOTING. MAINTENANCE REPLACED THE NR 2 TGT INDICATOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20040913000192004091300019CE 2004 9 13 2004F00297 120040611A2435 STARTER GEN LEAR 60 60LEAR 5170707CE RT ENGINE FAILED A O2GAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 NE0314TU 026 CREW NOTICED A FLUCTUATION OF AMPS IN THE RT GENERATOR BETWEEN 5-25 AMPS. MONITORED CONDITION FOR APPROX 20 MINUTES AT WHICH THE RT GEN DROPPED OFF LINE. CHANGED RT STARTER GENERATOR. (M) 2L72 4F RTA10CE 20040913000212004091300021EU 2004 9 13 2004F00299 120040712A2497 WIRE AEROSPATR42 ATR42300 8680920EU COCKPIT BROKEN A TRBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO21141AE 141 AUTOMATIC TAKEOFF POWER CONTROL SYSTEM LIGHT DID NOT ARM FOR TAKEOFF, ABORTED TAKEOFF. REPAIRED OPENED WIRE AT THE ATPCS PUSH-BUTTON SWITCH. (M) 2H72 4T RTA53EU 20040913000232004091300023NM 2004 9 13 USAA040362 120040726A53116546541504 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19575US50306 23740 PIT - FOUND FRAME CRACKED APPROX 1.025 INCH, STATION 663.75. INSTALLED REPAIR ANGLE PER EA 78568. (M) 2L72 4F RTA16WE 20040913000242004091300024NM 2004 9 13 USAA040363 120040727A531165C323946 FRAME BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19424US41084 23991 PIT - FOUND FRAME CRACKED APPROX 1.5 INCH, BS 601 FRAME INNER CHORD BELOW STRINGER 17R. INSTALLED REPAIR ANGLES PER EA 78575. (M) 2L72 4F RTA16WE 20040913000272004091300027NM 2004 9 13 USAASB04103 120040730A33501012721 LIGHT BOEING737 737301 1384611NM SEAT 7C INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19558AU 23512 ORD - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT AT SEAT 7C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOW LEVEL EMERGENCY ESCAPE PATH LIGHT AT SEAT 7C. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040913000302004091300030NM 2004 9 13 2004F00301 120040129A278210109592 ACTUATOR BOEING727 727224 1384076NM NR 2 SLAT INOPERATIVE A FX7AJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO1979750 22452 DURING THE AFTER T/O CHECKLIST, NR 2 LEADING EDGE SLAT EXTENDED INDICATION REMAINED ON BOTH FORWARD AND AFT ANNUNCIATOR LIGHTS DUMPED FUEL AND RETURNED TO KCVG WITHOUT INCIDENT. REPLACED NR 2 LEADING EDGE SLAT ACTUATOR PER MM 27-81-32. AIRCRAFT RETURNED TO SERVICE WITHOUT INCIDENT. (M) 2L73 4F A3WE 20040913000332004091300033 2004 9 13 2004F00302 420040305A2297 WIRE BOEING737 737231 1384079NM GOUND BROKEN A FX7AA UNSCHED LANDING O OTHER CLCLIMB 1 SO1964346 21633 AFTER TAKEOFF DURING CLIMB TO FLT LEVEL 230, DIRECTIONAL GYROS DRIFTED 15 TO 20 DEGREES AND WOULD NOT SLAVE, AUTOPILOT WOULD NOT ENGAGE AS WELL. DECIDED TO RETURN TO TUCSON WITHOUT INCIDENT. REMOVED AND REPLACED AILERON SERVO AND FOUND BROKEN GROUND WIRE AT TERMINAL STRIP REPAIRED BROKEN GROUND WIRE PER 20-30-11. PERFORMED OPS CHECK OFF AUTOPILOT AND GYRO SYSTEM PER MM 22-11-01. AIRCRAFT RETURNED TO SERVICE WITHOUT INCDIENT. (M) 2L72 4F RTA16WE 20040913000342004091300034SO 2004 9 13 2004F00303 120040502A561071159CB51023 WINDSHIELD GULSTMG1159 GIV 3980115SO COCKPIT CRACKED A O2GAO OTHER O OTHER CRCRUISE 1 NE03422ML 1367 AFTER TAKEOFF FROM KPBI ABOUT 40 MINUTES, THE RIGHT WINDSHIELD OUTER PLY CRACKED. CREW DESELECTED WINDSHIELD HEAT AND PULLED THE RESPECTIVE C/B IAW THE AIRCRAFT FLT MANUAL. AIRCRAFT COMPLETED FLIGHT WITHOUT FURTHER INCIDENT. REPLACED WINDSHIELD. (M) 2L72 4F RTA12EA 20040913000362004091300036EU 2004 9 13 ASOA04434 120040618A3350E01173110 NUT AEROSPATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11643AS 413 FLT 4197 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT BUTTON ON THE FLIGHT ATTENDANTS PANEL WAS FOUND STUCK IN THE ON POSITION. MAINTENANCE REINSTALLED THE LOCK NUT ON THE EMEGENCY LIGHT BUTTON SWITCH AT THE FLIGHT ATTENDANTS PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040907000452004090700045NM 2004 9 7 SWAA042532 120040830A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 935, STR 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040907000682004090700068NM 2004 9 7 DL757040806 120040822A5330141N83305 SKIN BOEING757 757232 1384965NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27612DL 22819 INSPECTION OF THE L1 DOOR CUTOUT UPPER FWD CORNER PER AD 2004-09-32 REVEALED A CRACK IN THE SKIN SURROUND BEAR STRAP. THE CRACK WAS REMOVED WITH A CUTOUT TO THE BEAR STRAP. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092906-14AD. 2L72 4F RTA2NM 20040907000712004090700071NM 2004 9 7 UPS04242821 120040707A7830 DOOR BOEING727 72725C 138400HNM THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 INSPECTION TYPE: C, ENGINE NR 1 THRUST REVERSER UPPER DOOR, INNER LWR SKIN HAS SUSPECT CRACK AT OUTBOARD TOP CORNER. HFEC INSPECTION CARRIED OUT IAW B727 NDTM PART 6 51-00-00 FIG 4. CRACK CONFIRMED AND MARKED. CRACK REMOVED IAW SRM 78-30-01. HFEC INSPECTION CARRIED OUT. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM SUPP 78-30-01. DYE PENETRANT INSPECTION CARRIED OUT. NO DEFECTS FOUND. 2L73 4F A3WE 20040907000742004090700074NM 2004 9 7 UPS04442820 120040713A5320 REVEAL BOEING747 747200 1384847NM L5 DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, M/D- BS 2231-2240, S16-17L, L5 DOOR CUTOUT FWD UPPER CORNER REVEAL FOUND CRACK. M/D BS 2231-2240 STR 16-17L L5 DOOR CUTOUT FWD UPPER CORNER REVEAL CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 91. 2L74 4F RTA20WE 20040907000802004090700080EU 2004 9 7 AWXA200400902 120040805A5320D53112087203 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT RAIL Y254 RT BETWEEN FR 16 AND FR 20. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT RAIL Y254 RT FROM FR 16 TO FR 23; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040907000892004090700089NM 2004 9 7 P5CA0401160 120040802A5730 ACCESS PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 RIGHT WING ACCESS PANEL 672 DB HAS CRACK & DELAMINATION. REMOVED DAMAGE AREA & BONDED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040907000962004090700096NM 2004 9 7 P5CA0401164 120040803A5730 PANEL BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DELAMINATION UNDER SPEED TAPE REPAIR LT WING, LOWER SERVICE WBL 175 FWD SPAR. REMOVED DAMAGE AREA RE-BONDED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040907001112004090700111NM 2004 9 7 UPS04242963 120040804A5280 STRUCTURE BOEING727 72722C 138400FNM LT MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, LT MLG WING DOOR AFT Z-SECTION CRACKED. Z-SECTION REMOVED IAW SRM 51-30-02 Z-SECTION FABRICATED IAW SRM 51-20-1 Z-SECTION INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20040907001132004090700113EA 2004 9 7 QXEA200400514 120040712A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 FORWARD CARGO COMPARTMENT CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040907001192004090700119NM 2004 9 7 QXEA200400626 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT TRACK NR 10 HAS CORROSION FROM X1 TO X5. BEGAN CORROSION REMOVAL AND BLENDED BEYOND .025 LIMITS AS PER RD 8/4-53-884. REMOVED FORWARD SPLICE RIVETS, NUTS AND BOLTS IN FRAMES, SEPARATED 10-11 SPLICE AFTER REMOVED FROM AIRCRAFT. DRILLED UP SPLICE BETWEEN 10 AND 11. INSTALLED 4 NUT PLATES ON TRACK IAW SRM 51-42-05. DRILLED UP SPLICE BETWEEN 10 7 11. MATCH DRILLED TO OLD SPLICE PLATES, INSTALLED 10/11 SPLICE WITH SAME TYPE HARDWARE AS REMOVED. INSTALLED DRIP REFLECTOR IAW Q400 SRM 51-42-05 AND BOLTED DRIP TRAYS BACK INTO PLACE. 2H72 4T RTA13NM 20040907001232004090700123NM 2004 9 7 QXEA200400612 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - TRACK NR 1 HAS LITE CORROSION BETWEEN THE LUGS AT X 200.0. BLENDED LIGHT CORROSION. MEASURED AND FOUND WITHIN LIMITS IAW RD 8/4-53-884, STEP 1. AREA 1.5 INCH LONG, .5 INCH WIDE AND .015 INCH DEEP. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-844, STEP 6. 2H72 4T RTA13NM 20040907001262004090700126NM 2004 9 7 QXEA200400616 120040811A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT TRACK NR 18 HAS CORROSION AT APROXIMATELY STATION X243.00. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED .003 MATERIAL. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040907001272004090700127NM 2004 9 7 04185404 120040703A21504068B00002 FLOW VALVE DORNERDO32 DO328300 NM RIGHT INOPERATIVE A VTZABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27404FJ 3150 DURING INITIAL DESCENT CREW REPORTED SMOKE IN THE CABIN AND DECLARED AN EMERGENCY. FLIGHT 6211 DIVERTED TO MKE. PASSENGERS DEPLANED ON TAXIWAY WITHOUT INJURY. THE RIGHT HAND FLOW CONTROL VALVE WAS FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040907001292004090700129 2004 9 7 AWXA200400777 420040715A34142083111 INDICATOR BOEING737 7373S3 1384711NM COCKPIT FAULTY A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28316AW51193702 23713 ON TAKEOFF, EN ROUTE, CAPTAINS AIRSPEED INDICATOR WAS INOPERATIVE, REJECTED TAKEOFF AT 80 KTS AND RETURNED TO GATE. MX ISSUED MEL 34-24, COND 1 (CAPT A/S INDICATOR INOP). WHEN ACFT ARRIVED MX R / R CAPTAINS AIRSPEED INDICATOR IAW BMM 34-12-21. TEARDOWN REPORT FOR MACH AIRSPEED INDICATOR S/N 681 CONFIRMED FAILURE OF UNIT FINDING AIRSPEED COUNTER STICKING. MX OVERHAULED UNIT, REPLACED LAMPS AND AIRSPEED MOTOR & PINS, AND ALSO ACCOMPLISHED SERVICE BULLETIN 2083-34-13, REV 4. CLEANED, CALIBRATED, AND PERFORMED OPERATIONAL TEST, UNIT RETURNED TO SERVICE IAW CMM 34-12-02. 2L72 4F RTA16WE 20040907001412004090700141EU 2004 9 7 AWXA200400666 120040605A5347D5311209220200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y1292 LT OUTBOARD SEAT TRACK BETWEEN FR 20 AND FR 23. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y1292 LT FROM FR 19+10 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 53-11-15 FIG 203. *S/D* PLEASE NOTE: CORROSION LEVEL DETERMINATION CHANGED TO REFLECT LEVEL 2 CORROSION. 2L72 4F RTA28NM 20040907001422004090700142EU 2004 9 7 AWXA200400667 120040605A5347D5311209220000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON BEAM Y765 LT INBOARD SEAT TRACK BETWEEN FR 20 AND FR 23. MAINTENANCE CUT OUT DAMAGED SECTION OF SEAT TRACK ON BEAM Y765 LT FROM FR 19+10 INCHES TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 53-11-15 FIG 203 PG 215-220. CORROSION LEVEL DETERMINATION CHANGED TO REFLECT LEVEL 2 CORROSION. 2L72 4F RTA28NM 20040907001612004090700161NM 2004 9 7 2004UALA00753 120040727A3350 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 ZONE-E CEILING EMERGENCY LIGHTS OUT ON BOTH SIDE OF CABIN AISLE. REPLACED BATTERY AND POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20040907001622004090700162NM 2004 9 7 2004UALA00755 120040810A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 4 NACELLE LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 RIGHT WING UPPER SURFACE ENGINE NR 4 NACELLE UPPER LINK WING FITTING HAS 1 SPINNING FASTENER WS 1168. 2L74 4F4 FRTA20WE E24NE 20040907001642004090700164NM 2004 9 7 2004UALA00757 120040810A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 PYLON LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 2 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING, ONE FASTENER HAS ROTATED AT INBOARD ROW UPPER HORIZONTAL FASTENER. 2L74 4F4 FRTA20WE E24NE 20040907001772004090700177NM 2004 9 7 CALA0400603 120040815A5311651630550 FRAME BOEING737 737524 1384721NM STA CUT A CALAK NONE O OTHER ININSP/MAINT 1 SW2769603 27316 INSPECTION FOUND A 3 INCH CUT IN WEB ON FRAME AT STA 219.8, RBL 20. A DOUBLER WAS INSTALLED IAW SRM 51-70-13. 2L72 4F RTA16WE 20040907001812004090700181NM 2004 9 7 QXEA200400587 120040805A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION AT X266.00, X280.00, X298.00, X312.00, X342.00, X363.00, X376.00, X2393.00, X405.00 AND X424.00. REPAIRED IAW RD 8-53-1342, DHC-8-200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20040907001852004090700185NM 2004 9 7 QXEA200400591 120040811A2430 RELAY DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE FAILED A QXEAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 NM09352PH16179 494 WITH BOTH ENGINES RUNNING AND CLEARED FOR PUSHBACK, THE DC BUSS ILLUMINATED, THE FMS WENT BLANK FOLLOWED BY A MAIN BATTERY HOT WARNING. THE MAIN BATTERY HOT CHECKLIST WAS RUN AND THE AIRCRAFT ENGINES WERE SHUTDOWN WHEN SMOKE WAS OBSERVED COMING FROM THE NR 2 ENGINE NACELLE BY THE RAMP CREW. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 2 STARTER GENERATOR, THE NR 2 GCU, MAIN BATTERY, STARTER GENERATOR CABLES ALONG WITH RELAYS 2431-K2, 8011-K4, 8011-K3, AND 8011-K5. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040907001952004090700195EA 2004 9 7 QXEA200400590 220040815A7200312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 500 MALFUNCTIONED A QXEAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM09401QX6175 2823 4031 PCEFA0060 GEG - FLIGHT 2337 AT 1000 FT NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN CALLED FOR OIL PRESSURE CHECKLIST. OIL PRESSURE WENT TO 0 AND OIL TEMP CLIMBED. CAPTAIN ASKED FOR ENGINE FAILURE CHECKLIST. BEFORE, COMPLETION OF CHECKLIST ENGINE MADE A BANG AND FAILED. SMOKE APPEARED IN COCKPIT AND FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. CFR CALLED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE SENT OUT FOR REPAIR. 2H72 4T4 TRTA13NM E00062EN 20040907001972004090700197EU 2004 9 7 MALA040538 120040823A2910HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU YELLOW HYD SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15526XJ E2351 YELLOW HYD SYSTEM OVERTEMP ANNUNCIATOR ILLUMINATED IN FLT. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 EDP P/N 521449, S/N ON F9932438, OFF MX653033 IAW 29-10-17, DID NOT FIX. REPLACED NR 3 ENGINE HYD ISOLATION VALVE P/N HTE9531-3, S/N ON 1190UB1/5, S/N OFF FRTR004AY IAW 29-10-14. OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20040907002032004090700203NM 2004 9 7 SWAA042428 120040821A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 15L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040907002052004090700205 2004 9 7 SWAA042430 420040821A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040907002082004090700208CE 2004 9 7 ACE062804 120040628A561010135402521 WINDSHIELD BEECH 1900 1900C 1154161CE COCKPIT CRACKED E YADAA UNSCHED LANDING O OTHER CRCRUISE 1 AL03113AX2576 UC41 PILOT REPORTED LEFT WINDSHIELD CRACKED ONE HALF HOUR INTO FLIGHT. RETURNED TO ORIGINAL AIRPORT. 2L72 4T RTA24CE 20040908000022004090800002NM 2004 9 8 150AW0037 120040525A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000172004090800017NM 2004 9 8 151AW0033 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 787 AT STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000222004090800022NM 2004 9 8 151AW0030 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 480 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000232004090800023NM 2004 9 8 151AW0031 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 727E AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. 2L72 4F RTA16WE 20040908000302004090800030WP 2004 9 8 ASMF200408022 120040826A7722 THERMOCOUPLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT ENGINE DAMAGED W ASMFK NONE N FALSE WARNING ININSP/MAINT 1 SW231003Y 48068 708420 DURING OVERNIGHT SERVICE WAS DETECTED RT ENGINE WITH HIGH EGT INDICATION. EGT INDICATION WAS CHECKED IAW MM 77-21-00 AND THERMOCOUPLE NR 4 WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 77-21-03. PT2 AND PT7 WERE CHECKED AND NO LEAKS WERE DETECTED, TRIMMING WAS PERFORMED IAW MM 71-00-00, BUT DURING TAKE OFF POWER TEST, THE MAXIMUM TAKE OFF 2.069 (2.06 OF EPR) WAS NOT REACHED, IT ONLY WAS REACHED 2.02. RT ENGINE WAS REPLACED IAW MM 71-00-00 AND TESTED IAW MM 77-00-01, ALL CORRECT. 2L72 4F4 F A6WE E9NE 20040908000312004090800031NM 2004 9 8 N150AW0003 120040525A5340 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05150AW 23218 STRINGER TIE CLIPS CRACKED AT THE FOLLOWING LOCATIONS: STRINGER 4 RT BS 727D, STRINGER TIE CLIPS REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040908000432004090800043NM 2004 9 8 F3LA200400092 120040902A5330 SKIN BOEING737 7373L9 1384470NM FUSELAGE DENTED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, COMPLIED WITH RW0000198, DENT IN FUSELAGE, AFT OF CARGO DOOR AT STA 500-500A. REMOVED DAMAGE, FABRICATED, LOCATED AND INSTALLED REPAIR IAW BAC 737-300 SRM 53-00-01, PROCEDURE V, DETAIL VII-IX AND SOPM 40-20-01. 2L72 4F RTA16WE 20040908000512004090800051NM 2004 9 8 ANCF200400028 120040824A5753 FAIRING BOEING767 767259 1385136NM PWA 4056 PW4056 NE RT FLAP DAMAGED W ANCFK NONE O OTHER ININSP/MAINT 1 SO23985AN 24618 DURING WALK AROUND FOUND DAMAGE TO THE RT EXTERIOR FAIRING FLAP. FAIRING WAS REMOVED IAW CDL 57-51-2 AND TRANS ITEM TO DMI 567. 2L72 4F4 FRTA1NM E24NE 20040908000592004090800059EU 2004 9 8 KBM2004F00198 120040626A21210500846 BLOWER MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE CABIN AIR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 WARM AIR IN FLIGHT, REMOVED AND REPLACED 7 INCH BLOWER MOTOR. 1G71 3U3 UNCH9EU E19EU 20040908000642004090800064EU 2004 9 8 KBM2004F00200 120040817A2435 ARMATURE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE STARTER GEN WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA865 4488 2143 ARMATURE WORN, SPARKS DURING, INTERMITTENT OPERATION. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040908000802004090800080EU 2004 9 8 KBM2004F00140 120040322A78100292808740 STRAP SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE HEAT SHIELD WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 ENGINE EXHAUST STACK HEAT SHIELD STRAP BRACKET IS WORN. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040908000942004090800094WP 2004 9 8 ABXA040295 120040811A53119923409502 FRAME DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23977AX 47513 RT FORWARD MAIN FRAME E CRACKED ON FORWARD FLANGE AT ZEE CLIP ATTACH FASTENERS, MIGRATES UNDER SPLICE PLATE RT (G) TO POINT (J) ON ES01144. REPAIRED MAIN FRAME IAW EA 53400120-001-2. 2L72 4F4 F A6WE E2EA 20040908000962004090800096WP 2004 9 8 ABXA040293 120040810A521059100817 SKIN DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE PAX DOOR DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23977AX 47513 FS 165 TO 200 PASSENGER DOOR LONGERON 16 LT SKIN DENTED. DAMAGE OUT OF LIMITS. REMOVED DAMAGED SKIN, FABRICATED DOUBLERS, REPAIRED IAW SRM 52-05. 2L72 4F4 F A6WE E2EA 20040908000982004090800098NM 2004 9 8 ANCF200400025 120040408A2780833605 PSEU DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE SLAT MALFUNCTIONED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23583AN 693 53183 TAKE OFF WAS DISCONTINUED SLATS DISAGREE LGT COME ON AND FLAPS /SLATS AURAL TAKE OFF WARNING SOUNDED AT APPROX 60 KTS FLAPS 6.3 GROUND RETURN.RT SLAT N3 SENSOR WAS RIGGING IAW AMM 32-08-00/102A AND 208. REPLACED PSEU IAW AMM 32-61-00/201 CHEEKED ALL SLAT PROX SENSORS FOR DC RESISTANCE FOUND INTO LIMITS PERFORMED TAKE OFF WARNING SYSTEM TEST IAW AMM 27-00-00 PAG 216B ALSO WITH TECHNICAL CAPTAIN I. CARDOSO PERFORMED TWO TAKE OFF SIMULATION WITH A/C AT 100 KNOTS AND FIRS SIMULATION FLAPS IN 6 DEGREES AND SECOND IN 8 DEGREES THE A/C NO PRESENT FAULTS AND AURAL WARNING NOT SOUND TEST SATISFACTORY IAW AMM 27-00-00POAG 216B. 2L72 4F4 FRT E2EA 20040908001002004090800100NM 2004 9 8 AWXA200400770 120040710A5347D5311281520000 SEAT TRACK AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 16. MAINTENANCE CUTOUT DAMAGE ON SEAT TRACK BEAM Y765, AT FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14, FIG. 202, PG. 211-212. 2L72 4F4 FRTA28NM E311NE 20040908001022004090800102NM 2004 9 8 AWXA200400772 120040708A53306545766 SKIN BOEING737 73733A 1384673NM GE CFM56 CFM56* 13802NE FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 DURING 4-DAY CHECK A 3.5 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN 4 INCHES ABOVE WING ROOT BETWEEN WINDOWS 11 AND 12, BETWEEN BS 500D+10 AND BS 520, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN LT FUSELAGE SKIN BETWEEN BS 500D+10 AND BS 520, STR 12 LT. PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5331-04191-RA1. 2L72 4F4 FRTA16WE E2GL 20040908001112004090800111WP 2004 9 8 UPS04842882 120040630A53112750825 FRAME DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FS 600RBL12LBL12CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, FLC BILGE FRAME HAS CORROSION AT FS 600 RBL 12. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT PART OF FRAME WITH CORROSION FAB NEW FRAME SECTION IAW DWG 5750886. SECTION HEAT TREATED TO 17075+6 FAB SPLICES AND STAPS. SPLICES HEAT TREATED, ALODINED AND PRIMED ON ALL PARTS OF REPAIR. LOCATED AND DRILLED AND INSTALLED REPAIR. IAW SRM 53-20, 51-1-8, AND 53-4-1. 2L74 4F4 FRT4A25 1E8 20040908001182004090800118WP 2004 9 8 UPS04842886 120040722A523057540751 FITTING DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE CARGO DOOR GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, C-1 DOOR AFT LOWER GUIDE PIN FITTING WORN GOUGED. REMOVED DAMAGED FITTING IAW UPS SRM 51-3-0. DAC DWG NR 5754075. FOUND TO BE OUT OF LIMITS IAW UPS SRM 53-2-0. RECEIVED NEW FITTINGS P/N NR SP 003923. LOCATED AND DRILLED AND DEBURRED FITTING. INSTALLED FITTING IAW SRM 51-1-21,51-1-24. 2L74 4F4 FRT4A25 1E8 20040908001272004090800127SW 2004 9 8 ALGA095355 120040617A6210206010200139 BLADE BELL 206 206B3 1181506SW MAIN ROTOR FLAKING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03167H 1629 2968 M/R BLADE T/E EXTRUSION EXFOLIATED AT APPROX. STA. 120.00. REMOVED BLADE FROM SERVICE AND INSTALLED A SERVICABLE UNIT. 1G71 3U H2SW 20040908001352004090800135SW 2004 9 8 ALGA096801 120040724A6210406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R BLADE BINDING E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03437AL79 53141 BINDING, AXIAL WEAR BEYOUND MAX, AND ROUGH. REPLACED WITH NEW PART IN FIELD. 1G71 3U3 UO H2SW E1GL 20040908001362004090800136NM 2004 9 8 DHL2004745504 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AFT BS 640 ABOVE STR 23 RT. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE DIM 2.5 INCHES X 2.2500 INCHES AND FABBED DOUBLER FROM 2024 T3 .080 PO NR 9001135 DIM 11.3750 INCHES X 8.5 INCHES IAW SRM 53-30-3 FIG 1. DOUBLER TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2 AND 53-30-3 FIG 1. 2L73 4F4 F A3WE E2EA 20040908001452004090800145NM 2004 9 8 C1HA200481002 120040807A3234A42006028305 SOLENOID BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE MLG INOPERATIVE A C1HAO OTHER J WARNING INDICATION CLCLIMB 1 GL15681CA 22020 ON TAKEOFF, UNABLE TO MOVE GEAR HANDLE FROM DOWN TO UP ON FIRST ATTEMPT. SECOND ATTEMPT NORMAL, REMOVED AND REPLACED LANDING GEAR CONTROL LEVER LOCK SOLENOID IAW MM 32-31-16. OPS CHECK WAS GOOD IAW MM 32-31-16. 2L73 4F4 F A3WE E2EA 20040910000132004091000013NM 2004 9 10 USAA040416 120040811A5711654532422 SPAR BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, RIGHT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED DOUBLER PER EA 78782. (M) 2L72 4F RTA16WE 20040910000272004091000027EU 2004 9 10 USAA040426 120040802A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US15460 1052 CLT - FOUND FLOORBEAM CORRODED 8 SQUARE INCHES BY .040 INCH, FRAME 66-68 Y1292. INSTALLED DOUBLER PER EA 95738. (M) 2L72 4F RTA28NM 20040910000292004091000029NM 2004 9 10 USAA040409 120040805A5321 FLOOR PANEL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU37799 24997 PIT - FOUND 1 INCH CRACK, MLG CORRUGATED PRESSURE BEAD FLOORING, BS 665 AT LBL 30. INSTALLED DOUBLER, FILLERS, ANGLED STIFFENER PER TYPICAL REP 53-60-04 FIG 1. (M) 2L72 4F RTA16WE 20040910000332004091000033NM 2004 9 10 AMTA200401025 120040811A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 FOUND EMERGENCY FLOOR LIGHTING AT ROW 10-12 OUT. RECONNECT WIRING TO LIGHT ASSEMBLY AT ROW 12, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20040910000362004091000036NM 2004 9 10 USAA040437 120040708A5330 SKIN BOEING737 7373B7 1384580NM FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND SKIN CORRODED .25 INCH BY .5 INCH SPOT, AFT PRESS BULKHEAD, AFT SIDE, STATION 1016 BL 0 . CLEANED LIGHT CORROSION PER SRM 51-21-31. (M) 2L72 4F RTA16WE 20040910000372004091000037NE 2004 9 10 AMTA200401035 220040812A7200 TAPE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT ENGINE TORN A AMTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL11528AT 30887 REJECTED TAKEOFF RIGHT ENGINE EPR ABNORMAL 80 KTS. FOUND SPEED TAPE TORN AWAY FROM PF RAKE AT 9 O'CLOCK POSITION REAPPLIED TAPE PER MM 77-11-04-2 ITEM ALREADY ON MCI C14U09-0104. (M) 2L72 4F4 FRTA2NM E12EU 20040910000382004091000038NM 2004 9 10 AMTA200401029 120040811A2613 WARNING LIGHT BOEING757 75733N 1384931NM LT MGL STRUT ILLUMINATED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11561TZ 33526 EICAS STATUS MSG L STRUT OVERHEAT DET 1 DISPLAYED. PERFORMED FIM 26-12-00, BLOCK 1 NO DEFECTS NOTED. (M) 2L72 4F RTA2NM 20040910000402004091000040NM 2004 9 10 USAA040424 120040811A5320 FLANGE BOEING737 7373B7 1384580NM RAM AIR DUCT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND ATTACH FLANGE CRACKED, 4 INCHES, LEFT RAM AIR INLET DUCT HANGAR ATTACHED TO LOWER SURFACE CETNER TANK. DURING REPLACEMENT, HOLE FOUND DAMAGED, OVERSIZED, FREEZE PLUG INSTALLED PER EA 78847. (M) 2L72 4F RTA16WE 20040910000422004091000042NM 2004 9 10 USAA040436 120040805A5553 FITTING BOEING737 7374B7 1384702NM VERTICAL STAB WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND LUG WITH WEAR ON BUSHING FACES,.005 INCH DEEP AND 1 INCH IN DIAMETER, VERT STAB AFT OUTBOARD ATTACH LUG BUSHINGS LT SIDES. REAMED AND REBUSHED PER EA 78920. (M) 2L72 4F RTA16WE 20040910000602004091000060NM 2004 9 10 2004F00272 120040408A5414652377261 PANEL BOEING727 727225 1384077NM NR 3 NACELLE MISSING A MYWAK NONE O OTHER ININSP/MAINT 1 SO19802MA 22433 DURING POST FLIGHT WALKAROUND AT PIT FORND PRESSURE RELIEF VENT PANEL MISSING FROM NR 3 ENGINE. INSPECTED NR 3 ENGINE IAW 71-10-11. PERFORMED HIGH POEWR ENGINE RUN UP. BLEED PRESSURE EQUAL ON BOTH SIDES PER MM 75-31-0. RETURNED TO AIRCRAFT TO SERVICE. (M) 2L73 4F A3WE 20040913000012004091300001EA 2004 9 13 ASOA04531 120040727A5320601R3117171 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F4 FRTA21EA E15NE 20040913000042004091300004NM 2004 9 13 BJNA040702 120040716A3350900835A BATTERY BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE IAW BOEING MM 33-51-31. THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATED NORMALLY. (M) 2L72 4F RTA16WE 20040913000092004091300009NM 2004 9 13 USAA040404 120040805A53471715896 CARGO TRACK BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU52228 23594 PIT - FOUND CARGO TIE DOWN CORRODED APPROX 2 FT AREA, FLOOR SUPPORT STATION 945 LEFT SIDE AFT CARGO COMPARTMENT. CARGO TIE DOWN SECTION MFG FROM SUPPLIED CCN 1715896 PER T/R 53-10-08. (M) 2L72 4F RTA16WE 20040913000122004091300012NM 2004 9 13 USAA040400 120040809A5414 SKIN BOEING737 737301 1384611NM LT WING PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US50329 23935 PIT - FOUND SKIN CRACKED .5 INCH, LEFT WING INBOARD OF PYLON L/E STATION 208. ROUTED CRACK OUT AND FILLED WITH SEALANT PER T/R 57-41-03. (M) 2L72 4F RTA16WE 20040913000162004091300016NM 2004 9 13 USAA040344 120040716A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US51857 23316 CLT - FOUND SKIN CRACKED 2 INCHES, TWO 4.5 INCHES AFT OF 867, 1 INCH BELOW STRINGER 15R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M) 2L72 4F RTA16WE 20040913000262004091300026SO 2004 9 13 SIMA200422409 120040723A532014522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21727AE 145326 DURING AN IMBV INSPECTION, THE GALLEY CENTER OMEGA BEAM WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/3307A, PARA 1 DATED JULY 23, 2004. (M) 2L72 4F RTT00011AT 20040913000322004091300032NM 2004 9 13 BJNA040704 120040716A33506104791 BATTERY BOEING737 737282 13844ATNM LT OVERWING INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURNG A MAINTENANCE WALK AROUND CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND BATTERY CHARGER ASSEMBLY P/N 6104789 FOR THE LEFT OVERWING EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE LEFT OVERWING EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M) 2L72 4F RTA16WE 20040913000372004091300037SO 2004 9 13 SIMA20040502 120040720A27413621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO HORIZONTAL STAB INOPERATIVE A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21709GB 145211 LGA - FLT 5023 - CREW ABORTED TAKEOFF AT 100 KTS DUE OT CONFIG WARNING FOR TRIM. TRIM INDICATED 7 UNITS ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040913000392004091300039NE 2004 9 13 2004F00305 220040525A7200 COMPRESSOR BOEING727 7272F9 138407DNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A PCSAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO17199AJ 21426 FLIGHT CREW REPORTED, AT FL370 100 MILES FROM SDQ, NR 2 ENGINE COMPRESSOR STALL AT FL370 (3 TIMES). ALL INDICATION FLUCTUATING. PRECAUTIONARY SHUTDOWN AT FL370, COMPLIED WITH APPROPRIATE SHUT DOWN PROCEDURES. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED VISUAL INSPECTED C-1 FAN BLADES AND T-4 TURBINE WHEEL NO EVIDENCE OF OIL OR DAMAGE IN AREAS RELATED TO THESE COMPONENTS. ALSO, INSPECTED ALL COMPONENTS ATTACHED FOUND OK. RAN ENGINE IAW THE AMM 72-00, OPERATIONAL CHECK GOOD. NO VIBRATION DUPLICATED. PRBC SCHEDULE ALSO VERIFIED. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F4 FRTA3WE E2EA 20040913000402004091300040NM 2004 9 13 USAASB04104 120040805A21501173T121 SWITCH BOEING737 737301 1384611NM LT A/C BAY MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19584US 23743 FLT DEPARTED WITH RT WING TO BODY OVERHEAT MEL 26-13 APPLIED. ON CLIMB-OUT, AT 8,000 FT, LT PACK TRIPPED OFF. AT 10,000 FT, CAPT ATTEMPTED TO RESET PACK 3 MORE TIMES AFTER COOLING BUT PACK WOULD NOT REMAIN ON. DECISION MADE TO RETURN TO FIELD AT MCI. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX PERFORMED RAM AIR SYS OPS TEST PER MM. OPS TEST GOOD. R & R LT ACM TURBINE INLET OVERHEAT SWITCH S1. RAN LT AIR CONDITIONING SYS. OPS CHECK GOOD. CLEARED RT WING TO BODY OVERHEAT MEL 26-13 BY TIGHTENING LEAKING CLAMPS IN RT AIR-CON BAY & RT WING LE. RAN ENGINES, AIR-CON SYS AND ANTI-ICE SYS. NO FURTHER AIR LEAKS NOTED & NO WING TO BODY OVERHEAT LIGHTS ILLUMINATED. A/C OK FOR SERVICE. (M) 2L72 4F RTA16WE 20040913000422004091300042NM 2004 9 13 USAASB04105 120040808A3260189929 UPLOCK SENSOR BOEING737 7374B7 1384702NM RT MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19437US 24559 AFTER TAKEOFF FROM PHL, EN ROUTE TO PBI, THE RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WITH THE GEAR UP. DECISION WAS MADE TO DIVERT TO CLT. ON GEAR EXTENSION, CREW RECEIVED A NORMAL GEAR INDICATION AS RED UNSAFE LIGHT EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED ANDR EPALCED THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR PER MM 32-61-21. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040913000432004091300043NM 2004 9 13 C7WA200400049 120040605A2730680005005 PCU BOEING727 7272J7 138400ENM LT ELEVATOR LEAKING A C7WAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17128NA 20879 IN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT .6 GALLONS. FOUND LEFT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LEFT ELEVATOR PCU IAW B727 MM 27-30-81, OPS AND LEAK CHECK GOOD. (M) 2L73 4F A3WE 20040913000442004091300044NM 2004 9 13 USAA040405 120040804A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU52228 23594 FOUND SKIN ATTACH HOLES WORN, SURFACE WEAR RIGHT WHEEL WELL LOWER KEEL BEAM ANGLE STATION 717-727. REPAIRED PER EA 78753 REWORK OF SURFACE WEAR. MOD PART INSTLALED 7150-T6511 ALUM EXTRUSION. (M) 2L72 4F RTA16WE 20040913000452004091300045NM 2004 9 13 C7WA200400037 120040630A5330 SKIN BOEING727 7272J7 138400ENM FUSELAGE CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17128NA 20879 FOUND FUSELAGE SKIN CRACKED STRINGER 21 LEFT STATION 1233. INSTALLED EXTERNAL SKIN REPAIR IAW B727 SRM 53-30-3 FIG 3. REPAIR DOUBLER, FABRICATED FROM 2024-T3, .080 BY 8 BY 7. (M) 2L73 4F A3WE 20040913000462004091300046EA 2004 9 13 ASOA04443 120040620A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN THE MCN, THE RIGHT FRAME FS 718, STRINGERS 10-11 ON THE AFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT FRAME FS 718, STRINGERS 10-11 ON AFT SIDE IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20040913000492004091300049NM 2004 9 13 UIEA200400133 120040728A541465B904511 SKIN BOEING747 7472D7B 1384803NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 DURING SCHEDULED MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248, NR 3 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVED THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20040913000532004091300053SO 2004 9 13 SIMA200422403 120040731A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21729AE 145343 ABI - DURING AN IMBV INSPECTION, THE SERVIEC DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED CENTER SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 26, 51-20-01,03, 51-40-02, 04,06. (M) 2L72 4F RTT00011AT 20040913000562004091300056CE 2004 9 13 2004F00309 120040619A2621 WARNING LIGHT BEECH 1900 1900D 1154162CE RT EXTINGUISHER FALSE INDICATIONA GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1987555 UE234 FLT 9238 - EYW/TPA - DURING FLIGHT, RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS. INSPECTED RIGHT ENGINE FIRE EXTINGUISHER BOTTLE WIRE CONNECTIONS AND DISCHARGE INDICATOR WIRE CONNECTIONS. COULD NOT DUPLICATE. OPERATIONAL CHECK OK. (M) 2L72 4T RTA24CE 20040913000582004091300058NM 2004 9 13 AMTA200400861 120040710A335020131A BATTERY BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND BULLNOSE EMERGENCY LIGHTS AT ROWS 22 AND 26 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AFTER FINDING CONNECTOR ON CHARGER DISCONNECTED IAW AMM 33-51-07-2. OPS CHECKS NORMAL. (M) 2L72 4F RTA2NM 20040913000602004091300060NE 2004 9 13 AMTA200400394 220040404A7200 ENGINE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LEFT SURGES A AMTAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL11528AT 30887 LEFT ENGINE SURGES AT TAKEOFF POWER NOTED SURGE IN EPR AND N1. ACCOMPLISHED TEST 13 PER AMM CHAPTER 71-00-00-5 UNLATCHED EEC, FLUCTUATION STOPPED. INSPECTED PF RAKES FOUND NR 2 HEAD ON OUTBOARD RAKE BROKEN SEE 1405/658 FOR ACCOMPLISHMENT OF TEMP REPAIR. (M) 2L72 4F4 FRTA2NM E12EU 20040913000632004091300063NM 2004 9 13 DHL2004762004 120040909A2612 ELEMENT BOEING727 7272B7 138407LNM PWA JT8 JT8D17 52049NE RN 3 FIRE DETECTOUT OF POSITION A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01762AT 22162 NR 3 FIRE DETETION CIRCUIT GROUND LIGHT ILLUMINATED. FOUND NR 3 ENG FIRE SENSOR ELEMENT TOUCHING A MOUNTING BRACKET. RE-POSITIONED ELEMENT, OPS CK GOOD IAW 26-11-00. 2L73 4F4 F A3WE E2EA 20040913000662004091300066NM 2004 9 13 0401505517 120040804A5320 FLOOR SUPPORT BOEING757 757251 1384970NM PWA 2037 PW2037 NE FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01517US 23205 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 377 RBL 45. REPAIRED IAW EA 55-200105. 2L72 4F4 FRTA2NM E17NE 20040913000682004091300068WP 2004 9 13 0401499915 120040804A5311 FRAME DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01965N 47417 DURING L-CHECK, FOUND CRACK IN FUSELAGE FRAME AT BS 1019 BELOW L14L. REPAIRED IAW EA 99-200165. 2L72 4F4 F A6WE E2EA 20040913000702004091300070NM 2004 9 13 AT0400017 120040905A3260DT2RA7 SWITCH BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE MLG INOPERATIVE A ZZDAO OTHER J WARNING INDICATION LDLANDING 1 SO15959AT 55021 3 GEAR UNSAFE ON EXTENSION OF GEAR. BAD SWITCH (S-189) REPLACED (P/N DT2R-A7) SENSING AND CONTROL MICRO SWITCH. 2L72 4F4 FTRA6WE E00061EN 20040913000712004091300071 2004 9 13 YENA200446 420040902A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN SMOKE A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15563JB1569 2006 ELECTRIC ODOR COMING FROM 26D. INFO NOTICE 2004-T023TR PERFORMED IN SAN AND FOUND SEB AT 26D WITH ELECTRICAL ODOR. LIVE TV PLACED ON MEL 25-22-03 CAT D, C/N L01825. REMOVED AND REPLACED SEB AT 26D IAW LTV MM 23-39-00, OPS CHECK NORMAL. MEL CLEARED. 2L72 4F4 FRTA28NM E40NE 20040913000722004091300072EA 2004 9 13 COMA0460497 120040901A5330 PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FUEL PANEL CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA 7306 FUEL PANEL CUTOUTS AT 540FB ANF 540EB BOTH HAVE CORROSION DETECTED AT THE AFT SIDE OF CUTOUTS. REPAIRED IAW REO 601R-57-21-03. 2L72 4F4 FRTA21EA E15NE 20040913000732004091300073NE 2004 9 13 COMA0460500 220040831A72505083T02P01 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TURBINE LEAKING A COMAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01912CA 7011 LT ENGINE LOW OIL PRESSURE WARNING IFSD. REPLACED THE NR 6 BEARING OIL SEAL. 2L72 4F4 FRTA21EA E15NE 20040913000742004091300074 2004 9 13 04FDEA02465 420040813A3418 SENSOR DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE AOA MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25586FE 48487 CAPTAINS PLI DROPPED TO FD PITCH BAR WHEN SLATS RETRACTED AND STICK SHAKER ACTUATED CAPTAINS SPEED INDICATOR BECAME RED, ALT MISS COMPARE, W/S DETECT FAIL ILLUMINATED, EVERYTHING WENT NORMAL WHEN SLATS EXTENDED. RETURNED TO MEM. FACT: REPLACED LT AOA SENSOR AFTER INTERROGATING NR 1 FCC SHOWING NR 1 AOA FAULTED FIVE TIMES OUT OF LAST SEVEN FLIGHTS. AFTER REPLACEMENT, REF MM 27-35-02-4, AOA SENSOR PASSED FCC RTS. AOA SENSOR REMOVED WAS NOT SMOOTH IN ITS MOVEMENT, VERY GRITTY. 2L73 4F4 FRTA22WE E31N3 20040913000752004091300075 2004 9 13 249TR0033 420040802A22301633930201 CONTROL UNIT BOEING737 7372K5 138448XNM PWA JT8 JT8D15 52051NE AUTOTHROTTLE INOPERATIVE A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO THROTTLE INOPERATIVE. REPLACED PDC CDU IAW MM 34-18-21 AND OPS CHECKED IAW MM 34-18-21 AND 22-31-01. 2L72 4F4 FRTA16WE E2EA 20040913000762004091300076NM 2004 9 13 QXEA200400525 120040714A5210 HINGE PIN DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE PAX DOOR STICKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09369PH13278 513 MAIN CABIN DOOR IS DIFFICULT TO OPERATE, STICKS. MAINTENANCE INSPECTED THE DOOR AND LUBRICATED THE HINGE PINS. DOOR OPERATES NORMALLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040913000772004091300077NM 2004 9 13 XNOA1192 120040713A2612 BATTERY BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE FIRE DETECTOR MALFUNCTIONED A XN0AO OTHER N FALSE WARNING DEDESCENT 1 GL2379754 21363 MAIN CARGO FIRE ALARM ILLUMINATED DURING DESCENT, VISUAL CHECK OKAY. LIGHT EXTINGUISHED SHORTLY AFTER. REMOVED AND REPLACED 2 EACH MAIN DECK SDU BATTERIES. SDU CHECKS GOOD IAW SECURE-A-PLANE MM. 2L73 4F4 F A3WE E2EA 20040913000782004091300078WP 2004 9 13 ANCF200400020 120040717A2913AS66411LS666 PUMP DOUG DC9 DC983 3022083WP HYDRAULIC SYS FAILED W ANCFO OTHER J WARNING INDICATION CRCRUISE 1 SO23593AN 4 53093 RT HYDRAULIC PRESS LOW LIGHT ON. RT HYDRAULIC PRESS 0 AND RT HYDRAULIC QUANTITY 19 QTS. THE RT HYDRAULIC PUMP WAS REPLACED IAW AMM 29-10-05 PAGE 201. THIS REPLACEMENT NO HELP. TRANSFER TO DMI 379 MEL 29-5 CAT C 2L72 4F RTA6WE 20040913000792004091300079NM 2004 9 13 DHL2004741009 120040804A2612 FIRE LOOP BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE AIRSTAIR SHORTED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01741DH 21931 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING DEPARTURE RAN ENTIRE ABNORMAL PROCEDURE TWICE LIGHT EXTINGUISHED ON RETURN TO IAH NR 2 THRUST LEVER AT IDLE FOR ENTIRE DECENT. FOUND SCREW TOUCHING FIRE LOOP IN AFT AIRSTAIR AREA LT SIDE REPOSITIONED FIRE LOOP, OP CK IS GOOD IAW M/M 26-12-0. 2L73 4F4 FRTA3WE E2EA 20040913000812004091300081NE 2004 9 13 NACA20040027 220040805A8530356994 CYLINDER HEAD DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 3 CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03779TA1224 1224 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL LOSS. REPLACED NR 3 CYLINDER DUE TO CRACKED HEAD. CHECKED GOOD. 2L74 4R4 R A781 5E8 20040913000822004091300082EA 2004 9 13 04193690 120040811A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE THRUST REVERSER OUT OF ADJUST A VTZAO OTHER N FALSE WARNING CLCLIMB 1 EA27690BR 7739 RT REV UNLOCKED MSG AFTER TAKEOFF. MECHANIC ADJUSTED RT ENG STOW SWITCH REF 78-37-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040913000842004091300084SO 2004 9 13 C2XA04BT076 120040710A335074441 LIGHT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL EMERGENCY EXIT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 DURING 5A INSPECTION, MAINTENANCE FOUND EMERGENCY EXIT SIGN OVER SERVICE DOOR, NOT OPERATING. REMOVED AND REPLACED EMERGENCY EXIT SIGN LIGHT OVER SERVICE DOOR IAW AMM NR 33-50-06. OPS. CHECKED GOOD. 2L72 4F4 FRTT00011ATTE6CH 20040913000852004091300085SO 2004 9 13 C2XA04IA103 120040816A3350110049 CHARGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040913000862004091300086SW 2004 9 13 9507272004 120040727A32602751008017 SWITCH SWRNGNSA226 SA226TB 8780406SW GARRTTTPE331TPE331* 01514WP MLG DIRTY E STZAO OTHER N FALSE WARNING APAPPROACH 1 AL0395AC 6413 T381 ON APPROACH, THE PILOTS SELECTED GEAR DOWN, DID NOT GET GREEN INDICATION FOR LT GEAR, CYCLED GEAR NUMEROUS TIMES, DECLARED AN EMERGENCY AND PERFORMED (FLY-BY) OF CONTROL TOWER TO VERIFY THAT THE GEAR WAS IN THE (DOWN AND LOCKED) POSITION. CREW AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TECHNICIANS CLEANED AND LUBRICATED THE LANDING GEAR BELLCRANK ASSY AND ENUNCIATOR SWITCHES. OPS CHECK AND GEAR SWING SATISFACTORY. 2L72 4T3 TRTA5SW E2WE 20040913000872004091300087NE 2004 9 13 04212402 220040730A7532 BLEED VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE STUCK A VTZAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA27402FJ 3147 PCECD0237 LT ENGINE HP BLEED VALVE STUCK OPEN DURING TAKE OFF. ABORTED TAKE OFF, PRSOV WAS REPLACED. 2H72 4T4 FRTA55NM E35NE 20040913000882004091300088NM 2004 9 13 ANCF200400019 120040716A323259390745501 ACTUATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE MLG DOOR MALFUNCTIONED W ANCFO OTHER J WARNING INDICATION CLCLIMB 1 SO23583AN27235 53183 ONCE AGAIN GEAR DOOR OPEN LIGHT CAME ON BUT THIS TIME WITH VIBRATION. RT MAIN LANDING GEAR DOOR ACTUATOR WAS REPLACED IAW AMM 32-32-04 PAGE 201 AND 32-10-00 PAGE 102 ITEM C STEP 2. IAW AMM 32-60-05 PAGE 207 THE LT TARGET WAS RIGGING. 2L72 4F4 FRT E2EA 20040913000892004091300089NM 2004 9 13 AWXA200400797 120040720A3397 CONNECTOR BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28324AW 23261 DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11 THRU 17 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED DAMAGED PIN ON CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040913000902004091300090EU 2004 9 13 AWXA200400798 120040720A3397E00528B3APNE CONNECTOR AIRBUS320 A320231 3930325EU SEAT ROW 17 LT DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 17 LT. MAINTENANCE REPLACED PINS IN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SIDEWALL BULKHEAD SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040913000912004091300091NM 2004 9 13 AWXA200400799 120040702A5320655169823 SPLICE BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-12 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER SPLICE AT BS 907, STR 25 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 907, STR 25 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW DWG 65-51698. 2L72 4F4 FRTA16WE E2GL 20040913000922004091300092NM 2004 9 13 AWXA200400800 120040703A5340693535214 STRINGER CLIP BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 DURING C-12 CHECK A .3750 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT STRINGER TIE AT BS 927, STR 24 LT. MAINTENANCE REMOVED AND REPLACED CORRODED STRINGER TIE AT BS 927, STR 24 LT IAW B737-300 SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20040913000932004091300093NM 2004 9 13 AWXA200400801 120040714A5315D5311272920000 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28807AW 1064 DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y254 RT BETWEEN FR 19 AND FR 20. MAINTENANCE CUTOUT DAMAGE ON BEAM Y254 RT FROM FR 19 TO FR 20; FABRICATED FILLERS AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-00-14, FIG. 204. 2L72 4F4 FRTA28NM E311NE 20040913000942004091300094NE 2004 9 13 ASMF200407023 220040721A732076960615 FCU DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE FAILED W ASMFD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SW23161PL108061329 49764 718075 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE HIGH TEMPERATURE INDICATION WHEN ALL CHARGES (ELECTRICAL, PNEUMATICAL, ETC) WERE APPLIED. THE N2 SETTINGS WERE ADJUSTED IAW M/M 71-00, ALL PARAMETERS WERE CORRECT. AT MEX THE FCU WAS REPLACED IAW M/M 73-20-01 AND ENGINE TESTED IAW M/M 1-00-0, ALL PARAMETERS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20040913000952004091300095NE 2004 9 13 200411 220040624A7200 ENGINE DHAV DHC8 DHC8103 1386005NM PWA 120 PW120 NE NR 1 MALFUNCTIONED A KPVAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP13805WP 353 (PIREP) JUST AS THE GEAR FULLY RETRACTED, THE NR 1 ENGINE TORQUE DROPPED 10 PERCENT, ACCOMPANIED BY A LOW HUMMING NOISE. ALL OTHER INDICATIONS NORMAL, NOISE CEASED AFTER LANDING.MECHANIC PERFORMED ENGINE MAINTENANCE RUN IAW MM 72-00-00 PG. 201. NO DEFECTS NOTED.(TEST FLIGHT) POST MAINTENANCE CHECK FLIGHT SATISFACTORY. 2H72 4T4 TRTA13NM E20NE 20040913000972004091300097NE 2004 9 13 2004UALA00772 220040816A7230 BLADE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 ENG COMPRESFAILED A UALAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29806UA 788 ABORTED TAKEOFF DUE TO NR 1 ENGINE COMPRESSOR STALL. FIRST STAGE COMPRESSOR BLADE (R3 BLADE) FAILURE. REPLACED ENGINE. 2L72 4F4 FRTA28NM E40NE 20040913000982004091300098NM 2004 9 13 F3LA200400073 120040723A3411C16195AA PROBE AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE PITOT SYSTEM INOPERATIVE A F3LAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 NM03906FR 358 1684 ABORTED TAKEOFF. FLIGHT CREW REPORTED THERE WAS NO AIRSPEED INDICATION ON CAPT'S SIDE. FO'S AIRSPEED WAS 80 KTS. FOUND CAPTAIN'S PITOT PROBE 9DA1 BAD. REPLACED PITOT PROBE IAW AMM 34-11-15-400-001. PERFORMED OPS AND LEAK CHECK AND AIRSPEED INDICATION TESTED NORMAL. 2L72 4F4 FRTA28NM E2GL 20040913000992004091300099NM 2004 9 13 0401206313 120040715A3350 LIGHT BOEING747 747451 1384940NM CABIN DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01673US 30268 DURING LINE CHECK, FOUND (E) ZONE LT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040913001002004091300100EU 2004 9 13 KBM2004F00207 120040814A6510350A33105B03 BELLCRANK SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR LOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 BUSHINGS LOOSE IN EXPANDABLE BOLT BOXES. REPLACED BELLCRANK WITH NEW. 1G71 3U3 UNCH9EU E19EU 20040913001012004091300101NM 2004 9 13 249TR0036 120040815A33501000679 LIGHT BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 R-1 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED R-1 EMERGENCY EXIT LIGHT. OPS CHECKS OK. 2L72 4F4 FRTA16WE E2EA 20040913001022004091300102NE 2004 9 13 KBM2004F00215 220040815A7261 GASKET SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL FILTER DEBONDED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 PILOT REPORTS ENGINE OIL PRESSURE INDICATION IS LOW AND LOW OIL PRESSURE LIGHT IS ON. FOUND RUBBER GASKET BELOW OIL FILTER HOUSING UNBONDED. REBONDED AND OPS CHECK GOOD. 1G71 3U3 U H9EU E19EU 20040913001052004091300105NM 2004 9 13 DHL2004746005 120040702A3240 BRAKE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE MLG MALFUNCTIONED A DHLAK NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01746DH 22252 BRAKES DRAGGING UNABLE TO DISENGAGE. T/S BRAKE SYST FOUND PNEUMATIC BRAKE HANDLE SLIGHTLY OFF DETENT STILL SAFETIED, BLED BRAKES, SAFETIED PNEUMATIC BRAKE HANDLE SYST. OPS CKD GOOD IAW MM 32-41-0. 2L73 4F4 F A3WE E2EA 20040913001062004091300106SO 2004 9 13 HUN2004F00001 220040430A7314653351A1 PUMP DIAMONDA20 DA20C1 2990001GL CONT O240 IO240B 17063SO SNSNCHW69EK W69EK63 EA FUEL SYSTEM FAILED D HUNAO OTHER O OTHER NRNOT REPORTED 1 NM01556DC C0156 806359 AE3811A ON THREE OCCASIONS THIS AC HAD FUEL SYSTEM PROBLEMS. IN FEB THE ENGINE DIED AT IDLE/LOW POWER OPERATIONS. THE FUEL PUMP WAS REPLACED AND PROBLEM WENT AWAY (OUR OTHER DA20C1, N6634DC, HAD THE SAME PROBLEM AND REMEDY). AT THE END OF APRIL 556DC LOST POWER AND SAFELY LANDED. THE ENGINE WOULD NOT RUN ABOVE 1500 RPM. THE FUEL PUMP WAS CHANGED AGAIN, AND THE PROBLEM WENT AWAY FOR A FEW DAYS. THE AC THEN HAD AN EMERGENCY LANDING DUE TO POWER FAILURE. TECH REP REPLACED THE THROTTLE BODY/METERING UNIT AND THE PROBLEM WENT AWAY. TECH DECLARED THE ISSUE RESOLVED AND RETURNED AC TO SERVICE. FEEL THERE MAY STILL BE ISSUES WITH THIS ENGINE/WOOD PROP/FUEL SYS CONFIG. THAT HAVE NOT BEEN DISCOVERED. UNKNOWN. 1L71 3O3 ONTTA4CH E7SO 5 NTA4CH 20040913001082004091300108NM 2004 9 13 04FDEA02382 120040805A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OB HOLE CORRODED. *** S/D COMING **** 2L73 4F RTA22WE 20040913001092004091300109NM 2004 9 13 04FDEA02470 120040813A5310 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IAW SRM 51-40-3 AND EA 7-5310- 70673. 2L73 4F4 FRTA3WE E2EA 20040913001102004091300110NM 2004 9 13 DHL2004754021 120040625A3260 SWITCH BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NLG DOOR OUT OF ADJUST A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01754DH 22008 IN FLIGHT, RED "DOORS" LIGHT ON FWD PANEL ILLUMINATED WHEN GEAR HANDLE PLACED IN UP POSITION, LIGHT EXTINGUSHED INTERMITENT. UPON T/S, FOUND RT NOSE GEAR DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND OPS CHECK GOOD IAW MM 32-62-11. 2L73 4F4 F A3WE E2EA 20040913001112004091300111NM 2004 9 13 QXEA200400529 120040716A7930 BYPASS VALVE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 500 OVERTEMP A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09413QX 4060 NR 1 ENGINE HIGH OIL TEMPERATURE. MAINTENANCE REPLACED NR 1 ACOC BYPASS VALVE AND ACOC FLAP ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040913001122004091300112EU 2004 9 13 AWXA200400688 120040603A5315D53472188202 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 2-3, 13-14, AND 16-18. 2L72 4F RTA28NM 20040913001132004091300113EU 2004 9 13 DHL2004363006 120040709A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE NR 2 ENGINE WILL NOT TEST A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01363DH 85 ENG NR 2 FIRE LOOP "B" DOES NOT TEST. DEFERRED IAW MEL 26-12-01-1, ASSIGNED CONTROL NR 17142, PLACARD INSTALLED, SP/CW. 2L72 4F4 FRTA35EU E23EA 20040913001142004091300114NM 2004 9 13 QXEA200400520 120040713A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 RT OB TRACK NR 11 SEAT ATTACH AREA CORROSION APPROXIMATELY X 500.00. REPAIRED IAW SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040913001152004091300115NM 2004 9 13 QXEA200400522 120040713A5310 DOOR FRAME DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 CRACKED BRACKET AT MAIN CABIN DOOR APERTURE FLOOR LEVEL STATION 240.500. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040907001752004090700175WP 2004 9 7 CALA0400601 120040813A53305911433 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT RIVET HOLE, STA 1380, BETWEEN LONGERON 13R AND 14R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 18. 2L72 4F A6WE 20040907001782004090700178WP 2004 9 7 CALA0400604 120040815A3350UNK FUSE DOUG DC9 DC981 3022081WP BATTERY PACK BLOWN A CALAK NONE L NO TEST ININSP/MAINT 1 SW2716883 48073 INSPECTION FOUND THE AFT FIVE ROWS OF EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN THE BATTERY PACK. 2L72 4F A6WE 20040907001792004090700179NM 2004 9 7 WLDA200434 120040806A5280ANB7216503 PANEL DOUG MD11 MD11 3023602NM ZONE 700 SEPARATED A WRLAD RETURN TO BLOCK D INFLIGHT SEPARATION TOTAKEOFF 1 SO11803 48474 ATL/IAH AIR TURNBACK DUE TO LEFT WHEEL WELL DOOR PANEL FELL OFF DURING TAKEOFF ROLL. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE & RETRACT CYLINDER. REPLACED LEFT MAIN OUTER DOOR. OPERATION CHECK & GEAR SWING CHECK ALL NORMAL PER MM PROCEDURES. 2L73 4F RTA22WE 20040907001802004090700180NM 2004 9 7 WLDA200442 120040802A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT BARREL NUT HOLE NR 30. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BARREL NUT HOLE NR 30 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040907001832004090700183NM 2004 9 7 2004UALA00765 120040808A3211 TRUNNION BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT MLG DAMAGED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29395UA 24670 LEFT MLG TRUNNION LINK WAS DAMAGED BY IMPROPER CORROSION REMOVAL. REPLACED LINK. 2L72 4F4 FRTA16WE E2GL 20040907001982004090700198EA 2004 9 7 VNAA0408008 120040815A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB FAILED A VNAAO OTHER J WARNING INDICATION CLCLIMB 1 GL07213PS 7879 DURING FLIGHT, THE CREW RECEIVED A MACH AND STAB TRIM AMBER CAS MESSAGE AND RETURNED TO GSO. MAINTENANCE THEN DISPATCHED MECHANICS FROM DAY. MAINTENANCE THEN RETRIEVED CODES FROM THE MDC AND RESET THE HSTCU AND PERFORMED A FUNCTIONAL TEST WHICH WAS GOOD IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 27-40-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040907001992004090700199NM 2004 9 7 VNAA0408009 120040816A5270 PROXIMITY SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE PAX DOOR OUT OF ADJUST A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07441JS 3059 DURING FLIGHT, THE DOORS LIGHT ON THE RED WARNING PANEL CAME ON. THE CREW THEN DIVERTED TO ELM. THE AIRCRAFT WAS THEN FERRIED TO PIT. MAINTENANCE THEN ADJUSTED THE PROXI SENSOR AND THE OVERCENTER LEVER IN ACCORDANCE WITH DORNIER MAITNENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040907002012004090700201EU 2004 9 7 AWXA200400906 120040804A5330D53470410200 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON SKIN AT IFPC FORWARD ANTENNA CUTOUT BETWEEN FR 60 AND FR 61. MAINTENANCE BLENDED OUT CORROSION ON SKIN AT IFPC FORWARD ANTENNA CUTOUT; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11 FIG 203. 2L72 4F RTA28NM 20040907002072004090700207NM 2004 9 7 WLDA200438 120040802A5512ALC8103504 PANEL DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C CHECK, PERFORMED INSPECTION PER EO 02-5510-098 REV 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RIGHT BARREL NUT HOLE NR 35. PERFORMED CORROSION REPAIR PER EO 02-5510-098 REV 1. CONDITION CHECK OF HORIZONTAL STAB RIGHT BARREL NUT HOLE NR 35 FOUND SATISFACTORY. 2L73 4F RTA22WE 20040908000042004090800004NM 2004 9 8 151AW0004 120040702A5313 STRINGER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 STRINGER 16 RT AT BS 500C HAS TWO CRACKS. REPAIRED CRACKS IAW SB737-53-1145. 2L72 4F RTA16WE 20040908000092004090800009WP 2004 9 8 AALA20040915 120040829A56105912290506 WINDSHIELD DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE COCKPIT CRACKED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21423AA 49335 INFLIGHT T1263/28 ORD ELP AT 31000 FEET FIRST OFFICERS WINDSHIELD BEGAN TO ARC. POWER SECURED TO WINDSHIELD. ARCING STOPPED. OUTER PLY OF FIRST OFFICERS WINDSHIELD CRACKED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICERS WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20040908000112004090800011CE 2004 9 8 2004F00274 120040823A3397 WIRE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LIGHT FAILED D O OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NE012615G 402C0101 ON SHORT FINAL, CREW REPORTED ODOR OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF. ODOR DISSIPATED. MAINTENANCE FOUND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL ON CIRCUIT BREAKER FAILED. REPAIRED WIRING REPLACED BREAKER AND RETURNED AIRCRAFT TO SERVICE. 1L72 3O3 O A7CE E8CE 20040908000182004090800018NM 2004 9 8 151AW0035 120040702A5311 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05151AW 23219 FUSELAGE FRAME CRACKED AT BS 847 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. 2L72 4F RTA16WE 20040908000652004090800065 2004 9 8 KBM2004F00199 420040802A3422103002301 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE DIRECTIONAL GYROINOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA289 2143 FLAG STAYS INOPERATIVE. REMOVED AND REPLACED DG. 1G71 3U3 U H9EU E19EU 20040908000702004090800070EU 2004 9 8 KBM2004F00212 120040602A7933646600251 PROBE SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL TEMP OIL FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 1032 3403 ENGINE OIL, TEMPERATURE FLUCTUATES INFLIGHT. REMOVED AND REPLACED TEMP OIL PROBE. 1G71 3U3 U H9EU E4CE 20040908000832004090800083SO 2004 9 8 C2XA04TY143 120040804A551014504980601 ATTACH BRACKET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL HORIZONTAL STAB WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715983 145239 A/C 983 WAS HERE FOR A MOD AND A 5A INSPECTION, UPON INSPECTING THE VERTICAL STAB,THE LT AND RT SPHERICAL BEARINGS WERE FOUND WORN. MAINT. ENLARGED BOTH LT AND RT SPHERICAL BEARING HOUSINGS AND INSTALL THE OVERSIZES BUSHINGS CALL FOR IN EC-55-10-01086. ALL WORK WAS IAW THIS EC(5510-01086). ALL WORK WAS COMPLIED WITH WITH ALL DEFLECTION CHECKS AND WAS RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T4 FRTT00011ATTE6CH 20040908000882004090800088EU 2004 9 8 AWXA200400851 120040804A2921E0218UUW030A RELAY AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE ZONE 120 FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28672AW 2193 ABORTED TAKEOFF AT BEGINNING OF TAKEOFF ENROUTE FOR LAS WHILE MOVING THRUST LEVERS FORWARD RECEIVED ECAM MESSAGE (HYDRAULIC YELLOW SYSTEM LOW PRESSURE; BRAKE ACCUMULATOR PRESSURE MONITOR), REJECTED TAKEOFF AT 50 KTS. MAINTENANCE PREFORMED GROUND SCAN AUTOMATIC FLIGHT SYSTEM AND OPERATIONAL TEST OF YELLOW HYDRAULIC SYSTEM, FOUND YELLOW SYSTEM ELECTRIC HYDRAULIC PUMP IN CONTINUOUS OPERATION AND POWER TRANSFER UNIT WITH AMBER INDICATION ON ECAM. REMOVED AND REPLACED RELAYS 3816GX AND 6MJ IAW TASK 29-13-00-810-816, OPERATIONAL CHECK WAS GOOD. PART NAME (6MJ); RELAY, MFG; AIRBUS, P/N; E0218UUU010A, LOC; ZONE 120 2L72 4F4 FRTA28NM E311NE 20040908000972004090800097SO 2004 9 8 2004F00232 120040715A56101159SCB310210 WINDSCREEN GULSTMG1159 GIV 3980115SO RROYCETAY TAYMK6108 NE COCKPIT CRACKED E O OTHER O OTHER CRCRUISE 1 EA07 1071 WINDSCREEN CRACKED DURING FLIGHT. 2L72 4F4 FRTA12EA E25NE 20040908001042004090800104NM 2004 9 8 AWXA200400774 120040710A5320D53472102206 SPLICE PLATE AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER IB SPLICE PLATE (COUPLING) BEAM Y1292 LT AT FR 68. MAINTENANCE REMOVED CORRODED UPPER IB SPLICE PLATE ON BEAM Y1292 LT AT FR 68. FABRICATED A NEW REPLACEMENT SPLICE PLATE; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2. 2L72 4F4 FRTA28NM E311NE 20040908001172004090800117WP 2004 9 8 UPS04842885 120040716A5347S2772660 SEAT TRACK DOUG DC8 DC871F 302199DWP PWA JT3D JT3D3 52039NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3 STA 65-75 RBL 36 SEAT TRACK LOBES OBLONGED. REMOVED FLOOR PANELS FS 70-170 FOM. REMOVED SEAT TRACK,DAMAGED OUT OF LIMITS IAW SRM 53-2-3. DRILLED NEW SEAT TRACK AND TRACK SPLICE TO FIT. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED FLOOR PANELS FS 70-170 IAW SRM 51-3-1. 2L74 4F4 FRT4A25 1E8 20040908001222004090800122EU 2004 9 8 04FDEA02366 120040804A3230224TS054Y MODULE AIRBUS310 A310 EU PWA JT9 JT9D* NE MLG FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25450FE 162 PDIS 450 32-60 0006380 05AUG04 MEM CLOSE R LOGPAGES: 00675737 GEAR HANDLE WOULD NOT RAISE. TRIED BOTH POSITIONS. GOT ALL 3 RED DOOR LIGHTS. BUT GEAR INDICATIONS SHOWED ALL 3 DOWN. CHECKED CONTROL BOX FOR FAULTS,NO FAULTS LOGGED, JACKED A/C RAN LANDING GEAR IN SYSTEM 1 AND SYSTEM 2, OPERATION NORMAL. REMOVED AND REPLACED LANDING GEAR ELECTRO VALVE MODULE IN REFERENCE WITH A 300-200 AMM 32-31-11-4, OPS NORMAL. RII:020225 PREMATURE REMOVAL/INSTALLATION OFF MFG 224TS054Y POS ONL SRL 315 ON MFG 224TS05Y SRL 787 TAG 665469. 2L72 4F4 FRTA35EU E20EA 20040908001332004090800133 2004 9 8 HE66096791 420040708A34163A433220F281 ALTIMETER UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE COCKPIT OUT OF TOLERANCEE HEEAO OTHER O OTHER NRNOT REPORTED 1 GL13135CR1611 0164 BOUNCES ALL OVER THE PLACE, NOT GOOD FOR IFR FLIGHT. 1G72 3U3 U H88EU E34NE 20040908001342004090800134SW 2004 9 8 ALGA096800 120040720A6210406310405101 BEARING BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R BLADE BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03697AL212 53374 BINDING, AXIAL WEAR BEYOND MAX., AND ROUGH. REPLACED WITH NEW PART IN FIELD. 1G71 3U3 UO H2SW E1GL 20040908001582004090800158SO 2004 9 8 C2XA04SH466 120040722A335020131A BATTERY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139753068 17 145163 DURING C-CHECK THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, THE ENSUUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040908001602004090800160NM 2004 9 8 04FDEA02369 120040805A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, OB AFT HINGE WITH IB PIVOT HOLE CORRODED**** S/D COMING **** 2L73 4F RTA22WE 20040908001632004090800163 2004 9 8 ALG2004F00045 420040618A3414 INDICATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL AIRSPEED INOPERATIVE E ALGAC ABORTED TAKEOFF I FLT. ATTITUDE INST. TOTAKEOFF 1 SW033896W 3197 CAE830679 TAKING OFF FOR FIRST FLIGHT OF THE DAY, AIRCRAFT HAD NO AIRSPEED ON INDICATOR. MAINTENANCE FOUND PLUG MISSING ON CAP ASSEMBLY FOR THE PITOT DRAIN SYSTEM. INSTALLED NEW PLUG IN CAP ALL WORK DONE IAW MM, COMPLIED WITH PITOT SYSTEM CHECK NO DEFECTS NOTED. 1G71 3U3 U H2SW E4CE 20040910000092004091000009NM 2004 9 10 USAA040410 120040731A57536546431285IR SKIN BOEING737 737301 1384611NM FOREFLAP GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US49309 23237 PIT - FOUND LEFT OUTBOARD FOREFLAP GOUGED, .3125 INCH WIDE BY .15 INCHE DEEP BY 2.5 INCH LONG, 30 INCHES FROM OUTBOARD END OF TOP SKIN, LEFT OUTBOARD FOREFLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER MM 27-51-37-4. (M) 2L72 4F RTA16WE 20040910000182004091000018WP 2004 9 10 ZIAA04067 120040804A3234 CONTROL HANDLE LKHEED188 188A 5262602WP MLG OUT OF RIG A ZIAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23343HA 1053 LANDING GEAR HANDLE APPEARS NOT TO GO TO THE FULL UP POSITION. RIGHT MAIN GEAR UNSAFE LIGHT STAYS ON. RIGGED RIGHT LANDING GEAR UPLOCK MECHANISM IAW L-188 MM 32-1-0. ZIAA (M) 2L74 4T RT4A22 20040910000242004091000024NM 2004 9 10 USAA040423 120040804A57206939228 SUPPORT ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND SUPPORT ANGLE CRACKED 1.125 INCH LONG, LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE AT REAR SPAR STAITON 243. REPLACED SUPPORT ANGLE PER BOEING DWG 69-39228, SRM 51-10-00. (M) 2L72 4F RTA16WE 20040910000262004091000026NM 2004 9 10 AMTA200401001 120040804A2741 TRANSMITTER BOEING757 75723N 1384973NM STAB TRIM MALFUNCTIONED A AMTAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL11516AT 27972 STABILIZER TRIM ON EICAS AND OVERHEAD LIGHT CAME ON PUSH BACK. REMOVED AND REPLACED THE LEFT STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER PER AMM 27-48-01-4. OPS CHECKED GOOD. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040910000472004091000047NM 2004 9 10 UIEA200400141 120040801A36103206254 RELIEF VALVE BOEING747 747243B 1384830NM NR 1 ENGINE LEAKING A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15517MC 23300 RHI/MXP - NR 1 ENGINE WOULD NOT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 108.5 AGAINST THE STOP. ALL OTHER INDICATIONS NORMAL. NR 3 ENG WOULD NT ATTAIN REQUIRED THRUST FOR T/OFF. WOULD ONLY ATTAIN 110.0 AGAINST THE STOP. ALL OTHER INDICATIONS NORMAL. REJECTED TAKEOFF. NR 1 ENGINE PERFORMED PNEUMATIC LEAK CHECK. NOTED RELIEF VALVE WITH EXCESSIVE LEAK. R & R ENG NR 1 RELIEF VALVE UNIT IAW MM 36-12-00. PERFORMED NR 1 THRUST CONTROL CABLE CHECK IAW MM 76-71-00. NR 3 PERFORME PNEUMATIC LEAK, NOTED PVR CLAMP LEAKING, RETORQUED CLAMP. PERFORMED NR 3 THRUST CONTROL CABLE CHECK IAW AMM 76-11-00. PER MCC ADJUSTED MAIN ENG CONTROL PART POWER TRIM 1-TURN CW IAW MM 71-00-00 TEST 5. (M) 2L74 4F A20WE 20040910000492004091000049NM 2004 9 10 UIEA200400144 120040816A5315 FLOORBEAM BOEING747 747243B 1384830NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15516MC 22507 DURING INCORPORATION OF SB 747-53A2459, FOUND CRACK AND OR ELONGATED FASTENER HOLES COMMON TO FRAMES AND UPPER DECK FLOORBEAM UPPER CHORDS AT BS 340/360. FLOORBEAM UPPER CHORDS AND WEBS REPAIRED PER SRM. AT BS 340, STOP DRILLED AND REPAIRED FRAME WEB. OPEN HOLE HFEC INSPECTED IMMEDIATELY ADJACENT TO THE REWORK AREA TO CONFIRM CRACK FREE CONDITION. AT BS 360, STOP DRILLED AND REPAIRED THE SHEAR DOUBLER. TRIMMED OUT THE FLOORBEAM UPPER DECK WEB AND THE FLOORBEAM UPPER DECK CHORD. HFEC INSPECTED ALL EXISTING HOLES TO CONFIRM CRACK FREE CONDITION BEFORE INSTALLING THE SPLICE PARTS. INSTALLED STRAP P/N 141U0048-45 PER SB 747-53A2459. REPAIR IS SUBJECT TO CONTINUOUS INSPECTIONS PER SB 747-53A2265/AD 91-11-01.2L74 4F A20WE 20040910000512004091000051NM 2004 9 10 UIEA200400152 120040823A573065B144809 PANEL BOEING747 7472D3B 1384805NM LT WING DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15505MC 21251 FOUND LER LEFT WING PANEL AT ILES 173.6 HAD DELAMINATION HEAT DAMAGE WHILE ON GROUND. THE PANELS WERE REPLACED IAW SRM 51-30-02 AND AMM 51-24-11. (M) 2L74 4F RTA20WE 20040910000532004091000053NM 2004 9 10 UIEA200400145 120040816A5330 SKIN BOEING747 747243B 1384830NM FUSELAGE SCRATCHED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15516MC 22507 DURING SCHEDULE MAINTENANCE, FUSELAGE SKIN DAMAGE WAS FOUND ADJACENT TO THE CARGO DOOR. THE SKIN DAMAGE WAS REMOVED BY BLENDING OUT THE DAMGAE. NO FASTENERS WRE AFFECTED BY THE BLEND OPERATION. HFEC SURFACE INSPECTED TO ENSURE NO DEFECTS EXIST. BOEING ADVISED THE REPAIR WAS STRUCTURALLY SATISFACTORY AS PERMANENT REPAIR. BOEING NOTED THE REPAIR IS OUTSIDE THE SSID AREA, AND DOES NOT IMPACT SSID INSPECTIONS. (M) 2L74 4F A20WE 20040910000652004091000065NE 2004 9 10 AMTA200400009 220040103A7320 CONNECTOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE LT EEC LOOSE A AMTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL11558TZ 32592 SHORTLY AFTER LEVEL OFF AT FL310, LEFT ENGINE SURGED, ALL PARAMETERS. TIGHTENED LOOSE CONNECTOR ON L EEC. PERFORMED PROCEDURES IAW FIM 71-06-00 FIG 102. NO FAULTS NOTED. (M) 2L72 4F4 FRTA2NM E12EU 20040913000202004091300020CE 2004 9 13 2004F00298 120040722A5610 WINDSHIELD CESSNA750 750 2076810CE COCKPIT CRACKED A O2GAO OTHER O OTHER DEDESCENT 1 NE03610GR777 7500163 PILOT WINDSHIELD CRACKED ON DESCENT INTO CLT. REMOVED AND REPLACED PILOTS WINDOW. (M) 2L72 4J RTT00007WI 20040913000252004091300025SO 2004 9 13 SIMA200422408 120040729A532014521713005 CHANNEL EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21729AE 145343 ABI - DURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 26, 51-20-03, 51-40-02 AND 51-40-04. (M) 2L72 4F RTT00011AT 20040913000292004091300029NM 2004 9 13 GAIA04089OP 120040722A33501000679 LIGHT BOEING727 727223 1384074NM COCKPIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW076806 19481 ON PREFLIGHT, FOUND EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED EXIT LIGHT FOR CHARGING AND INSTALLED SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040913000412004091300041NM 2004 9 13 C7WA200400034 120040630A5230MS200116 HINGE BOEING727 7272J7 138400ENM MAIN CARGO DOOR CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17128NA 20879 FOUND MAIN CARGO DOOR UPPER AFT HINGE SECTION CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AEI MM CHAPTER 52 PAGE 15. (M) 2L73 4F A3WE 20040913000482004091300048CE 2004 9 13 2004F00307 120040723A2110206SZC BEARING BEECH 200 B200 1152922CE FREON COMP DRIVEFAILED A DINAO OTHER O OTHER NRNOT REPORTED 1 EA13260G BB1525 AFT BEARING ON FREON COMPRESSOR BELT DRIVE FAILED, BURNED UP AND DISINTEGRATED. THE BEARINGS ARE SEALED, AND HAVE NON REPLACEMENT INTERVAL. REPLACED BOTH BEARINGS, QUILL SHIFT, AND BELT WITH NEW. WILL REPLACE BEARINGS ON A 1200 HOUR INTERVAL. (M) 1L72 4T A24CE 20040913000502004091300050EU 2004 9 13 2004F00308 120040721A3260602EN1046 UPLOCK SWITCH STBROSSD3 SD330 8100602EU NLG INOPERATIVE A DATAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL1358DD SH3008 WHILE COMING BACK FROM PIA-ASW, MLG WAS LOWERED, DURING APPROACH CHECKS. NLG INDICATION DID NOT GO 'GREEN'. INITIATED MISSED APPROACH & WENT INTO HOLDING PATTERN. FLT CREW CARRIED OUT EMERGENCY CHECKLIST & LOWERED MLG THE EMERGENCY METHOD. DECLARED EMERGENCY TO FORT WAYNE APPROACH. NLG INDICATION DID NOT COME UP EVEN BY EMERGENCY METHOD. THEN FLY THROUGH THE ASW 27 RUNWAY AT LOW ALTITUDE AND GOT CONFIRMATION FROM GROUND THAT ALL GEARS DOWN. LANDED WITHOUT INCIDENT. THE LANDING GEAR WAS PINNED IAW MEL 32-3 ON 7/21/2004 ON LOG PAGE 56969. THE AIRCRAFT WAS FLOWN TO MKE AND THE NOSE UPLOCK SWITCH WAS REPLACED. MEL 32-3 HAVE BEEN CLEARED. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A41EU 20040913000512004091300051NM 2004 9 13 UIEA200400134 120040728A541465B941004 SKIN BOEING747 7472D7B 1384803NM NR 4 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 DUIRNG SCHEDULE MAINTENANCE, FOUND CRACK DAMAGE AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248, NR 4 PYLON. TRIMMED THE NR 3 STIFFENER BASE BOTTOM TO REMOVE THE CRACK. TRIMMED THE SKIN ASSEMBLY AND WINDOW STRAP. NDT INSPECTED EACH REPAIR AREA, INCLUDING HFEC INSPECTION OF ALL REPAIR FASTENER LOCATIONS AND TRIMMED EDGES TO ENSURE ABSENCE OF CRACKS, CORROSION AND ANY OTHER DAMAGE. INSTALLED ALUMINUM FILLER AT EACH TRIMMED AREA. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NACELLE STATION 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20040913000522004091300052NM 2004 9 13 USAA040412 120040730A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 7 INCH AREA, INTERCOSTAL AROUND NUT PLATE. REMOVED DAMAGED AREA, INSTALLED DOUBLER AND FILLER PER SRM 51-70-11. (M) 2L72 4F RTA2NM 20040913000542004091300054EA 2004 9 13 ASOA04436 120040618A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040913000552004091300055EA 2004 9 13 ASOA04431 120040617A5210 BEARING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11920EV 7810 FLT 4448 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE LUBRICATED THE LOWER BEARING ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040913000572004091300057CE 2004 9 13 2004F00310 120040619A2621 WARNING LIGHT BEECH 1900 1900D 1154162CE RT EXTINGUISHER FALSE INDICATIONA GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO1987555 UE234 DURING FLIGHT, RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS CONTINUOUSLY. INSPECTED RIGHT ENGINE FIRE EXTINGUISHER BOTTLE WIRE HARNESS AND DISCHARGE INDICATOR. NO DEFECTS FOUND. OPS CHECK NORMAL. (M) 2L72 4T RTA24CE 20040913000592004091300059EU 2004 9 13 SIMA200409903 120040405A2910AE7064588 LINE SAAB SF340 340B 7860101EU HYD SYSTEM LEAKING A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21340RC 340B340 DURING CLIMB-OUT, CREW HEARD A POP IN THE NOSE GEAR AREA FOLLOWED BY MAIN ACCUMULATOR DROPPING TO ZERO. PERFORMED EMERGENCY EXTENSION OF LANDING EAR. LANDED WITH ZERO FLAPS. FOUND NLG ACTUATOR LINE BROKEN. REPLACED ACTUATOR LINE IAW AMM 29-11. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20040913000622004091300062EU 2004 9 13 MALA040561 120040901A2910AC29150132 LINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE HYDRAULIC SYS LEAKING A MALAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15529XJ E2363 DURING TAXI OUT, CAPT HEARD A LOUD POP, A LONG, STRONG LOW PITCH HISSING SOUND COMING FROM REAR OF AIRCRAFT. HYDRAULIC PANEL QUANTITY AND PRESSURE FOR GREEN SYS QUICKLY BLED TO ZERO AND ASSOCIATED QUANTITY, LOW PRESSURE AIR TO PRESSURE LIGHT ILLUMINATED. CABIN FILLED WITH SMOKE, SO CREW EVACUATED AIRCRAFT, BLEW FIRE BOTTLES. MAINT REMOVED REQUIRED INTERIOR COMPONENTS AND FLOORBOARDS, AFT CARGO PANEL 181 BL,CL,DL,EL,FL,GL, QL, RL, ET 182 NR,UR FOR CLEANING AND LINE REPLACEMENT. REPLACED HYD LINE. PERFORMED LEAK CHECK, SERVICED GREEN, YELLOW HYD, CLEANED HYD FLUID FROM BENEATH AFT CARGO FLOORING ON RT SIDE FWD AND AFT OF DOOR BEHIND PANELS. REPLACED LT FWD ESCAPE SLIDE PN D31050-105 SN/OFF1635, SN/ON 1419. 2H74 4F4 FRTA49EU E6NE 20040913000652004091300065EA 2004 9 13 04252620 120040907A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE A/C SYSTEM ODOR A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27620BR 7179 EVENT SUMMARY STATED STRANGE ODOR. REMOVED AND REPLACED LT AND RT WATER SEP COALESCE BAG'S. PERFORMED OPS CHECK WITH NO FURTHER ODOR NOTED AT THIS TIME REF AMM CH 21-51-13. 2L72 4F4 FRTA21EA E15NE 20040913000672004091300067WP 2004 9 13 0401489969 120040802A5320 STIFFENER DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK FOUND CRACKS IN VERTICAL STIFFENER AT BS 756 RBL 24. REPAIRED IAW EA 99-199103. 2L72 4F4 F A6WE E2EA 20040913001222004091300122EA 2004 9 13 COMA0460433 120040730A2750601R9300403 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01933CA15630 7040 FLIGHT 5768 FLAPS FAIL CAUTION DURING LANDING ROLL. REPLACED THE FLAP SELECTOR LEVER. 2L72 4F4 FRTA21EA E15NE 20040913001252004091300125NM 2004 9 13 04FDEA02471 120040813A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673. 2L73 4F4 FRTA3WE E2EA 20040913001262004091300126NM 2004 9 13 04FDEA02472 120040813A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1. 2L73 4F4 FRTA3WE E2EA 20040913001272004091300127NM 2004 9 13 04FDEA02473 120040813A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1. 2L73 4F4 FRTA3WE E2EA 20040913001282004091300128NM 2004 9 13 04FDEA02474 120040813A5315651758866 FLOORBEAM BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2, 51-30-8. 2L73 4F4 FRTA3WE E2EA 20040913001302004091300130EU 2004 9 13 AWXA200400713 120040613A5347D5347123320200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSLAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-04 CHECK CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 BETWEEN FR 47 AND FR 64. MAINTENANCE BLENDED OUT CORROSION ON RT IB SEAT TRACK Y765 FROM FR 47 TO FR 64 IAW SRM 51-74-00 FIG. 1, MATERIAL LOSS OUT OF LIMITS FROM FR 50 TO FR 60 REMOVED AND REPLACED SEAT TRACK IAW A320 SRM 53-00-15 FIG. 202. 2L72 4F RTA28NM 20040913001322004091300132NM 2004 9 13 AWXA200400728 120040626A5315D5347218920400 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW A319 SRM 51-42-11 FIGURES 2-18. 2L72 4F4 FRTA28NM E311NE 20040913001342004091300134NM 2004 9 13 AWXA200400730 120040626A5315D5347209001100 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 (2 PLACES) AT FR 64 AND FR 65. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 FROM FR 64 TO FR 65 IAW A319 SRM 51-42-11 FIG. 2, 3, 8, 18. 2L72 4F4 FRTA28NM E311NE 20040913001362004091300136NM 2004 9 13 AWXA200400732 120040627A5315D5347218820400 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 AT FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y1292 AT FR 68 IAW SRM 51-42-11 FIG. 2, 3, AND 18. 2L72 4F4 FRTA28NM E311NE 20040913001382004091300138NM 2004 9 13 AWXA200400734 120040627A5315D5347209300000 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 FROM FR 67 TO FR 68. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 67 TO FR 68 IAW SRM 51-42-11 FIG. 9-12, AND 18. 2L72 4F4 FRTA28NM E311NE 20040913001392004091300139CE 2004 9 13 62587 120040627A32341013841377 CONTROL HANDLE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA MLG SELECTOR MALFUNCTIONED A AMWAO OTHER O OTHER APAPPROACH 1 CE07173YV UE173 ON APPROACH TO LANDING. THE FIRST AND SECOND ATTEMPTS TO EXTEND LANDING GEAR FAILED. CREW WIGGLED HANDLE AND GOT GEAR TO EXTEND WITH ALL GEAR INDICATING DOWN LOCK. LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR HANDLE. OPS CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040913001492004091300149NM 2004 9 13 C8GA20040008 120040622A3411 PITOT LINE BOEING727 727225 1384077NM PWA JT8 JT8D* NE AIRSPEED OBSTRUCTED A C8GAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO15808EA 22439 DURING TAKE-OFF ROLL, THE FIRST OFFICER’S AIRSPEED INDICATOR READ 80 KNOTS AND THE CAPTAIN’S INDICATOR INDICATED ZERO KNOTS. ABORTED TAKE-OFF, CONTACTED ATC TO ADVISE THEM OF AN AIRSPEED INDICATION PROBLEM AND RETURNED TO RAMP WITH NO FURTHER INCIDENT. INSPECTED CAPTAINS PITOT PROBE AND FOUND DEBRIS LODGED IN PITOT TUBE. CLEAN DEBRIS AND BACK FLUSH PITOT LINE AND PERFORMED LEAK AND PITOT STATIC CHECK IAW MM 34-11-00. SYSTEM OPS CHECKS GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040913001512004091300151EU 2004 9 13 KBM2004F00164 120040716A7931704A37642043 TRANSMITTER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE OIL PRESS INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 591 2300 OIL PRESSURE TRANSMITTER, NO PSI READING. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040913001522004091300152NM 2004 9 13 UPS04243000 120040805A5753652163479 SKIN BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU LT WING TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C LT IB AFT FLAP LWR SKIN DELAMINATION AT IB END AND BELOW NR 7 CARRIAGE. AFT FLAP REMOVED IAW MM 27-51-02. NEW AFT FLAP INSTALLED IAW MM 27-51-02. 2L73 4F4 F A3WE E25NE 20040913001532004091300153NM 2004 9 13 UPS04243001 120040805A57536521630188 SKIN BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU RT FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, DELAM ON RT IB FORE FLAP UPPER SURFACE AT IB END. RT IB FLAP REPLACED REPLACED IAW MM27-51-01. 2L73 4F4 F A3WE E25NE 20040913001572004091300157WP 2004 9 13 DHL2004804504 120040627A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR. 1514: RT WING CTR. LE UPPER FORMER CRACKED 0.500 AT XFS 354.000. REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-21 PG.1, SRM 57-2-0 PG. 9-10 2L74 4F4 FRT4A25 E2GL 20040913001592004091300159WP 2004 9 13 DHL2004804505 120040627A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 RT WING CTR. LE UPPER FORMER CRACKED 0.500, XFS 347.750. CORR.: REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 57-2-0 PG. 9-10, SRM 51-1-21 PG.1. 2L74 4F4 FRT4A25 E2GL 20040913001872004091300187NM 2004 9 13 WLDA200480 120040802A5512ALC8101503 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 6.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 6 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040913001882004091300188NM 2004 9 13 WLDA200481 120040802A5512ALC8101503 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 4.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 4 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040913001892004091300189NM 2004 9 13 WLDA200482 120040802A5512ALC8101503 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 ITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 3.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 3 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040913001902004091300190NM 2004 9 13 WLDA200483 120040802A5512ALC8121501 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 1.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 1 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040913001922004091300192EU 2004 9 13 AWXA200400915 120040805A5310D53472284008 BEAM AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66. MAINTENANCE REMOVED CORRODED LONGITUDINAL BEAM ASSEMBLY Y460 RT AFT OF FR 66; FABRICATED A NEW REPLACEMENT BEAM ASSEMBLY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040913001952004091300195WP 2004 9 13 MWEA040138 120040811A53159911592501 CLIP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FLOORBEAM ELONGATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FLOORBEAM AND ATTACHMENT CLIP AT STATION 148.50 HAS ELONGATED HOLES APPROXIMATELY 15 INCHES RT OF AIRCRAFT CENTERLINE WHERE STICK PUSHER BRACKET BOLTS UP. FABRICATED AND INSTALLED NEW CLIP. 2L72 4F4 F A6WE E9NE 20040913001972004091300197WP 2004 9 13 MWEA040140 120040811A53209936553355 WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 SUBFLOOR WEB CORRODED UNDER GALLEY 1 WATER PAN. STA 155 AND RT OF BUTT LINE 44. FABRICATED AND INSTALLED WEB. 2L72 4F4 F A6WE E9NE 20040913001992004091300199WP 2004 9 13 DHL2004804533 120040731A53205755360 BRACKET DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 AFT ACCY. COMPT. BRACKET CRACKED 0.500, L-35R TO L-36, STA. 660.000. REMOVED CRACKED BRACKET IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW BRACKET (ALCLAD 7075-T651) IAW EA NR 5320-036, DWG 5755360. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP. IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-3-0 PG.1, SRM 51-3-1 PG.1. 2L74 4F4 FRT4A25 E2GL 20040913002002004091300200WP 2004 9 13 COOSDR040009 120040630A5512 PANEL DOUG DC8 DC862F 3021972WP PWA JT3D JT3D* 52039NE HORIZONTAL STAB CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 76459 46129 EMPENNAGE RT STAB LOWER SECTION STRINGER NR 4 WITH CRACK AT XFS 47 AND CORROSION AT XFS 45. 2L74 4F4 F 4A25 1E8 20040913002012004091300201NM 2004 9 13 0401296638 120040720A5420 WEB BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE NR 3 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01638US 23549 DURING (H) CHECK FOUND CRACK IN NR 3 PLYON ENGINE MOUNT BULKHEAD WEB. REPAIRED IAW EA 66-165162. 2L74 4F4 F A20WE E3NE 20040913002032004091300203 2004 9 13 KBM2004F00167 420040516A3422103002201 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE DIRECTIONAL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 DIRECTIONAL GYRO, WOULD NOT HOLD HEADING. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040913002042004091300204NM 2004 9 13 UPS04243002 120040804A5280 SKIN BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU LT MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, CRACK ON LT MLG WING DOOR INNER SKIN AT TE. HFEC CARRIED OUT AND CRACK CONFIRMED. CRACK STOP DRILLED IAW SRM 51-10-1.HFEC CARRIED OUT AND CRACK CONTAINED WITHIN DRILLED AREA. REPAIR CARRIED OUT IAW SRM 52-80-2 FIG 5. 2L73 4F4 F A3WE E25NE 20040913002062004091300206NE 2004 9 13 NACA20040025 220040630A853076270 CAM DOUG DC6 DC6 3021702WP PWA R2800 CB3 52026NE NR 12 CYLINDER FAILED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL03779TA873 873 45529 36710 NR 2 ENGINE SHUT DOWN DUE TO NR 12 CYLINDER DOUBLE SHORTED SECONDARY AND RUNNING ROUGH. REPLACED ENGINE DUE TO FRONT CAM FAILURE. CHECKED GOOD. 2L74 4R4 R A781 E264 20040913002072004091300207WP 2004 9 13 ASMF200408016 120040818A2410696233B CSD DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT GENERATOR MALFUNCTIONED W ASMFO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW23751RA2983 2973 49779 CAPTAIN REPORTED, DURING CLIMB CSD TEMPERATURE INCREASED UNTIL INDICATOR RED SECTION, INCREASING RISE TEMPERATURE, SHUTTING OFF CSD. REPORT WAS DEFERRED IAW MEL 24-1-1 CAT B. ENGINES RUN TEST WAS PERFORMED AT TAKEOFF THRUST (1.7 OF EPR'S) DURING 10 MINUTES, REACHING 115 DEGREES (C) AND TEMP RISE 5, SYSTEM AND WIRING WERE CHECKED BEING CORRECT. CSD HARNESS WAS DETECTED WITH DAMAGES AND A CONNECTOR WAS LOOSENED. CSD HARNESS WAS REPLACED IAW MM 24-11-1, TESTS WERE CORRECT. AFTER TAKEOFF CAPTAIN REPORTED CSD SHUTOFF IAW HIGH TEMPERATURE. DURING OVERNIGHT SERVICE, RIGHT CSD AND HEAT EXCHANGER AIR/OIL WERE REPLACED IAW MM, A HOST WAS DETECTED WITH DAMAGES, SO IT WAS REPLACED AND ALL TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20040913002112004091300211NM 2004 9 13 SDR040015 120040614A3150 WARNING LIGHT BOEING737 73781Q 13844GENM ENGINE ILLUMINATED A MYWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO19732MA 30618 DURING TAKEOFF ROLL, ENGINE LIGHT CAME ON AT F/O ANNUNCIATOR PANEL AND EEC ALTERNATE LIGHT CAME ON AT OVERHEAD PANEL. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. CHECKED BOTH ENGINES FOR FAULTS AND RECEIVED FAULT CODES 73-31671 AND 73-31672 AT NR 1 AND NR 2 ENGINES. PERFORMED ENGINE RUN AND COMPLIED WITH FIM TASK 73-28-TASK 807. NO FAULTS PRESENT AT THIS TIME. COMPLIED WITH SECOND ETOPS PDSC WITH NO DEFECTS FOUND AT THIS TIME. AIRCRAFT RETURNED TO REVENUE SERVICE IN SPM. 2L72 4F RTA16WE 20040913002122004091300212NE 2004 9 13 ASMF200407026 220040723A7250 TURBINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23861LF450994569 49826 716778 DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED IAW MM 71-00-02 ON RT ENGINE, DETECTING GUIDE VANE WITH CRACK OUT OF LIMITS ON SECOND STAGE OF TURBINE AT 5 HOURS POSITION APPROXIMATELY. RT ENGINE WAS REPLACED AND DURING TEST, FUEL FLOW INDICATION WAS INOPERATIVE. FUEL FLOW TRANSMITTER WAS REPLACED IAW MM 73-31-01, TEST CORRECT. 2L72 4F4 FRT E9NE 20040913002162004091300216EU 2004 9 13 AWXA200400925 120040805A5315D5347218820200 FLOORBEAM AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040913002202004091300220EU 2004 9 13 04FDEA02394 120040806A213381001C010300 OUTFLOW VALVE AIRBUS310 A310 EU GE CF6 CF680A3 30025NE CABIN PRESSURE INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25415FE 349 PDIS 415 21-30 0007170 FWD NR 1 OUTFLOW VALVE STUCK IN THE OPEN POSITION (AMBERARROW ON ECAM). NR 1 PRESS REGULATOR IN USE-ECAM SHOWED 0 V/S AND CABIN ALT. AT 260 FT. WHEN SWITCHED TO NR 2 REG. ECAM SHOWED ACTUAL V/S MATCHED A/C CLIMB RATE AND CABIN ALT. EQUALED A/C ALT. NO ECAM IND. THAT OUTFLOW VALVE FAULTED MEL 06AUG04 03:36 BOS R ACN RELEASED FOR SERVICE IAW MEL/CDL: 21-31-04-02-A CATEGORY: C , FACT 09AUG04 20:41 GSO R, REMOVED AND REPLACED REPLACEMENT VLV FOR NR 1 FWD POSITION IAW MM 21-31-12-4-01. TEST NORMAL. (MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY)FWD NR 1, INOP. VALVES DEACTIVATED IN CLOSED POSITION PERFORMED PRESSURIZATION CHECK IAW MM 21-31-00-5-01. 2L72 4F4 FRTA35EU E13NE 20040913002212004091300221CE 2004 9 13 DXTA200400355 120040805A323067275049 ACTUATOR CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL UPLOCK MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07950QS5205 7500050 WHILE IN CRUISE FLIGHT, AT FL310 AT MACH .86, CABIN PRESSURE DIFFERENTIAL AT 8.6 PSI, THE NOSE GEAR CYCLED DOWN AND UP. HAD RED UNLOCK LIGHT FLASHED MOMENTARILY THEN OUT. ITEM IS UNDER INVESTIGATION. CONNECTED DMU UNIT AND MONITORED LANDING GEAR LOGIC MODULE, REMOVED AND REPLACED UPLOCK ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION, ADJUSTMENT TEST CHECK IS GOOD ALSO EMERGENCY CABLE RELEASE IS GOOD. ALL WORK PERFORMED IAW MM. 2L72 4J4 FRTT00007WITE6CH 20040913002222004091300222NM 2004 9 13 ANCF200400024 120040408A278259370215503 ACTUATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE SLAT MALFUNCTIONED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23583AN 53183 TAKE OFF WAS DISCONTINUED TWO TIMES BY SLAT DISAGREE LIGHT CAME ON AND FLAP7SLAT AURAL TAKE OFF WARNIN SOUNDED. IT WAS AT APROX 60 KNOTS. IT WAS REPLACED RT CYLINDER SLAT ACTUATOR ACC AMM27-80-05/202. TEST BY LEAKS WAS SATISFACTORY P/N ON OFF 5937021-5503. S/N ON 2319 S/N OFF 02487 2L72 4F4 FRT E2EA 20040913002232004091300223 2004 9 13 KBM2004F00169 420040223A2312064101910 RADIO BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL VHF STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19667JM 3444 VHF IS STUCK ON SQUALCH NR 2. REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20040914000022004091400002NM 2004 9 14 MWEA040160 120040908A5244 PANEL BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FUSELAGE UNSECURE A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31918ME 55180 CLIMBING THROUGH 10,000FLT. ALTITUDE NO WATER PRESSURE FOR COFFEE, ALSO NO WATER PRESSURE IN EITHER LAVATORY. FOUND WATER SERVICE PANEL OPEN. SECURCURED PANEL, NO DAMAGE FOUND. 2L72 4F4 FTRA6WE E00061EN 20040914000032004091400003NM 2004 9 14 ASMF200408023 120040827A793142D1091A SWITCH DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE OIL FILTER FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23881LF5620 53051 725563 AIRCRAFT REJECTED TAKE OFF AT 97 KNOTS AND RETURNED TO PLATFORM (RT OIL STRAINER CLOGGING) LIGHT TURNED ON. MAIN OIL FILTER AND DIFFERENTIAL PRESSURE ALARM WERE REPLACED IAW MM 79-20-06 AND 79-35-01, RESPECTIVELY. REJECTED TAKE OFF INSPECTION WAS PERFORMED IAW MM 05-57-00 AND TESTS WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRT E9NE 20040914000062004091400006SO 2004 9 14 C2XA04IA113 120040831A335082321 LAMP EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD OVERHEAD EMERGENCY LIGHT AT SEAT 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRT TE6CH 20040914000072004091400007SO 2004 9 14 C2XA04IA114 120040831A33501317 BULB EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20040914000092004091400009EA 2004 9 14 COMA0460493 120040901A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA 7306 RT CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. 2L72 4F4 FRTA21EA E15NE 20040914000102004091400010NM 2004 9 14 ASMF200409001 120040904A3260833605 PROXIMITY SWITCH DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE MLG FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23160PL11902 49763 AIRCRAFT RETURNED TO PLATFORM, (SPOILER DEPLOYED) LIGHT TURNED ON. BITE TO PROXIMITY SWITCH UNIT WAS PERFORMED IAW MM 32-60-05 AND SPOILERS WERE INSPECTED IAW MM 27-62-00. RTS WAS PERFORMED AND PROXIMITY SWITCH UNIT WAS REPLACED IAW MM 32-60-05, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914000122004091400012NM 2004 9 14 04253405 120040909A2750 CONTROLLER DORNERDO32 DO328300 NM PWA 306 PW306B NE TE FLAPS FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 EA27405FJ 3155 FLAP CONTROL FAILURE AND FLAP ASSYM. WHILE IN FLIGHT. CREW COMPLIED WITH QRH BUT WAS UNABLE TO DO A ZERO FLAP LANDING IN ROA. FLIGHT DIVERTED. MX RESET FLAP SYSTEM IAW JIC 27-50-00. PERFORMED OPERATIONAL CHECK OF FLAP FROM 0 TO 32 DEGREES WITH NO FAILS. 2H72 4T4 FRTA55NM E35NE 20040914000142004091400014NM 2004 9 14 BJNA040808 120040825A5310 DOOR FRAME BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER AFT CORNER FRAME CRACKED. INSTALLED NEW LOWER AFT CORNER AT C1 DOOR IAW SRM 51-20-1 AND SB 737-52A1100 REV 4. (M) BJNA 2L72 4F4 FRTA16WE E2EA 20040914000182004091400018EU 2004 9 14 WRNA200400011 120040908A283030505411 ACTUATOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUEL JET VALVE UNSERVICEABLE A WRNAJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO05501TR 53 AFTER TAKE OFF AC REQUIRED A LOT OF AILERON TO KEEP LEVEL, 35 DEGREES. RETURNED TO AIRFIELD, WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY. OVERWEIGHT LANDING ACCOMPLISHED. LANDING NORMAL. FOUND NR 3 LT SPOILER SERVO BAD, REMOVED AND REPLACED SERVO CONTROL IAW 27-62-14, OP'S CHECKED SATISFACTORY. PERFORMED OVERWEIGHT LANDING INSPECTION AND FOUND AIRCRAFT IN AIRWORTHY CONDITION, NO DISCREPANCIES NOTED. CLEANED C/P AT RT FUEL JETTISON VALVE ACTUATOR. SECONDARY SYS CKS OK IAW 28-31-00. DEFERRED PRIMARY IAW MEL 28-31-02 CAT-C. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20040914000192004091400019EU 2004 9 14 AWXA200400993 120040909A5270893301 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU FWD CARGO DOOR FAULTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28602AW 565 AIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ECAM WARNING FOR FORWARD CARGO DOOR WARNING INDICATION, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED FORWARD CARGO DOOR AND FOUND IT SECURE, ISSUED MEL 52-70-01, COND. 1 (FWD CARGO DOOR INDICATION INOP), ORDERED PROXIMITY SENSOR. MAINTENANCE FOUND FORWARD CARGO DOOR PROXIMITY SENSOR POSITION TARGET OUT OF ADJUSTMENT; ADJUSTED TARGET IAW AMM 52-71-00-05, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040914000212004091400021EU 2004 9 14 AWXA200400995 120040813A5321D5367203100000 FLOOR PANEL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 152 EF DELAMINATED IN THREE AREAS. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 152 EF FROM FR 49 TO FR 53; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 231-236. 2L72 4F4 FRTA28NM E311NE 20040914000222004091400022EU 2004 9 14 AWXA200400996 120040813A5321D5367203700000 FLOOR PANEL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 152 MF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 152 MF FROM FR 56 TO FR 58; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 233-236. 2L72 4F4 FRTA28NM E311NE 20040914000232004091400023EU 2004 9 14 AWXA200400997 120040815A5320D534800203420000WEB AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN LT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 LT. MAINTENANCE REMOVED CRACKED LT AFT OB TRAY FROM FR 68 TO FR 69, Y1732 LT TO Y1792 LT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040914000242004091400024EU 2004 9 14 AWXA200400998 120040815A5320D534711242020000SHEAR PLATE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, AT STR 24 LT. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE FROM FR 69 TO FR 70, AT STR 24 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040914000252004091400025EU 2004 9 14 AWXA200400999 120040814A5347D5311281400200 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 16 AND FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FR 12 TO FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040914000272004091400027EU 2004 9 14 AWXA200401001 120040815A5320D53480020343 WEB AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK A 1.5 INCH CRACK WAS FOUND IN RT AFT OB TRAY (WEB) BETWEEN FR 68 AND FR 69, OB OF BEAM Y1292 RT. MAINTENANCE REMOVED CRACKED RT AFT OB TRAY FROM FR 68 TO FR 69, Y1292 RT; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040914000282004091400028EU 2004 9 14 MALA040553 120040818A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15502XJ E2307 DURING CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/0007383 REMOVED AS BAD FROM STOCK CAPACITY CHECK FAILED, 8/18/04 AND 8/25/04. MAINTENANCE REPLACED BATTERY ASSEMBLY 61-2275-1 UNIT PASSES CMM TESTS, RETURNED TO SERVICE 8/29/04. REFER TO WO NR 374052 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000302004091400030EU 2004 9 14 MALA040545 120040822A5541 FRAME BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE RUDDER CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15515XJ E2333 DURING C-CHECK INSPECTION, RUDDER HINGE A-FRAME AT RB 10 WAS FOUND WITH THE AFT RUDDER ATTACH BEARING OUT OF THE FRAME. THE A-FRAME WAS CHAFED AS WELL AS CHAFFING DAMAGE TO THE RUDDER. REPAIRS CARRIED OUT ON 409 NR 186829. 2H74 4F4 FRTA49EU E6NE 20040914000332004091400033EU 2004 9 14 MALA040544 120040822A5753 SKIN BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE FLAP TAB CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15515XJ E2333 DURING C-CHECK INSPECTION PERFORMED, CHAF MARKS FOUND ON RT FLAP TAB LOWER SKIN AT NR 2 HINGE POINT. MAINTENANCE REPAIRED ON 409 NR 186860. 2H74 4F4 FRTA49EU E6NE 20040914000342004091400034EU 2004 9 14 MALA040557 120040811A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15534XJ E2370 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/9810762 FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/17/04. REFER TO WO NR 373901 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000352004091400035EU 2004 9 14 MALA040558 120040807A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15534XJ E2370 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/9805520 FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/17/04. REFER TO WO NR 373758 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000362004091400036EU 2004 9 14 MALA040560 120040818A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15532XJ E2366 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/0008399 FAILED ON 8/18 AND 8/25/04. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/29/04. REFER TO WO NR 374244 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000382004091400038EU 2004 9 14 MALA040543 120040822A5753 SKIN BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE FLAP TAB CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15515XJ E2333 DURING C CHECK INSPECTION PERFORMED, CHAFF MARKS FOUND ON RT FLAP TAB LOWER SKIN AT NR 1 HINGE POINT. MAINTENANCE REPAIRED ON 409 NR 186861. 2H74 4F4 FRTA49EU E6NE 20040914000392004091400039EU 2004 9 14 MALA040555 120040818A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15508XJ E2318 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/9710074, FAILED CAPACITY CHECK, MAINTENANCE REPLACED BATTERY PACK ASSEMBLY PN 61-2274-1. UNIT PASSES ALL CMM TESTS. AIRCRAFT RETURNED TO SERVICE 8/19/04. REFER TO WO NR 374245 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000422004091400042NM 2004 9 14 04FDEA02644 120040904A5420ATL005511 PAN DOUG DC10 DC10 N/A-SDRNM GE CF6 CF66D 30020GL ZONE 400 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 NR 2 ENGINE RT FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER U-BOLT. REMOVED CENTER U-BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW SRM 51-35-01, VOL II. WELD REPAIRD IAW EA 8-5410-81450. INSTALLED PAN IAW SRM 51-31-01 VOL II. INSTALLED CENTER U-BOLT AND FITTING IAW SRM 51-31-01 VOL II. REFERENCE N/R N00899. 2L73 4F4 FRTA22WE E23EA 20040914000452004091400045SW 2004 9 14 KBM2004F00172 120040226A282076547 PRESSURE SWITCH BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUEL SYSTEM INOPERATIVE E KBMAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP1973DP 1015 2513 FUEL PUMP LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED FUEL PRESSURE SWITCH. 1G71 3U3 U H2SW E4CE 20040914000472004091400047 2004 9 14 YENA200439 420040720A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE RADIO SYS SMOKE A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15523JB3547 1506 FLT ATT REPORTED SMELLING SMOKE IN CABIN DURING APPROACH. PERFORMED INFO NOTICE 2004-TO23TR NO DISCREPANCY NOTICED. LIVE TV SYTEM FULLY OPERATIONAL. REMOVED AND REPLACED SEB AT 16E AS PRECAUTIONARY IAW INFO NOTICE. INSPECTED SEATS 14-18DEF. 2L72 4F4 FRTA28NM E40NE 20040908001292004090800129 2004 9 8 AWXA200400839 420040730A3414 INDICATOR AIRBUS320 A320231 3930325EU AIRSPEED INOPERATIVE A AWXAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 WP28620AW 052 ABORTED TAKEOFF, ON TAKEOFF, EN ROUTE, THERE WAS NO AIRSPEED INDICATION ON CAPTAINS AIRSPEED INDICATOR, REJECTED TO AT 80 KTS. MAINTENANCE FLUSHED CAPTAINS PITOT TUBE DRAIN LINES AND PERFORMED INTERFACE TEST IAW AMM 10-00-170-001 AND AMM 34-13-00-740-002. 2L72 4F RTA28NM 20040908001312004090800131EU 2004 9 8 DHL2004365002 120040722A5610 WINDSHIELD AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE COCKPIT CRACKED A DHLABJA EMER. DESCENT DUMP FUEL UNSCHED LANDING O OTHER CRCRUISE 1 SO01365DH 149 FO'S WINDSHIELD FRACTURED WHILE ENROUTE. 2L72 4F4 FRTA35EU E23EA 20040908001382004090800138EU 2004 9 8 MALA040533 120040813A793183465 SWITCH SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ENG OIL PRESSUREMALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15421XJ 340B421 RETURNED AFTER TAKEOFF DUE TO THE RT OIL PRESSURE LIGHT ON THE CWP ILLUMINATING. MAINTENANCE REMOVED AND REPLACED RT ENG PSI S/W PN 8346-5 AS IAW AMM 72-00-00 RNA AC FOR 10 MIN, OPS CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20040908001392004090800139SW 2004 9 8 ALGA096566 120040720A6210206015001119 BLADE BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03175AL1919 52117 LOWER SURFACE OB GRIP FINGER DOUBLER DEBONDED. FOUND CORROSION BETWEEN SKIN AND SPAR. REPLACED UNIT W/NEW BLADE. 1G71 3U3 UNCH2SW E1GL 20040908001412004090800141NM 2004 9 8 AWXA200400762 120040709A33501012721 LIGHT BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE SEAT ROWS 7, 11 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 DURING B2 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 7 AND 11 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT SEAT ROWS 7 AND 11 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E2GL 20040908001422004090800142EU 2004 9 8 AWXA200400763 120040711A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONE 241 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28631AW7999 3161 077 DURING 4-DAY CHECK EMERGENCY LIGHTS WOULD NOT PASS TEST AT THE PRESS TO TEST PANEL. MAINTENANCE REMOVED AND REPLACED THE LT OVER WING EMERGENCY POWER SUPPLY UNIT (11WL) AND BATTERY PACK; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040908001442004090800144NM 2004 9 8 DHL2004746006 120040827A3350S106 BATTERY BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01746DH 22252 ENTRY WAY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED ENTRY EMERGENCY EXIT LIGHT BATTERIES. OPS TEST NORMAL IAW M/M 33-50-71. 2L73 4F4 F A3WE E2EA 20040908001472004090800147NM 2004 9 8 F3LA200400069 120040701A2120 ODOR AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE CABIN DETECTED A F3LAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03906FR 1684 BLOCK TURN BACK. FLIGHT CREW REPORTED ODOR OF SMOKE IN THE CABIN NEAR ROW 20. INVESTIGATED CABIN FOR SMOKE ODOR, OPERATED BOTH ENGINES AND AIR CONDITIONING SYSTEM. INSPECTED ALL LAVATORIES AND CARGO BAYS. NO SMOKE ODOR NOTED, NO FAULTS NOTED. INSPECTED AVIONICS BAYS, NO SMOKE ODOR NOTED. INTERVIEWED SEVERAL PASSENGERS AT ROW 20. PASSENGERS STATED THEY DID NOT ODOR SMOKE. COMPLETED TASK 26-15-00-810-804. RELEASED AIRCRAFT FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20040908001502004090800150EA 2004 9 8 QXEA200400577 120040807A2720CC670511143 CONTROL PANEL CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FLIGHT DECK FAILED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09611QX5891 10041 FLIGHT 4199, ON TAKE OFF ROLL, THE CREW RECEIVED A MASTER WARNING FOR "CONFIG RUDDER" AND OBSERVED THE RUDDER TRIM CONTINUE TO MOVE OUT OF THE TAKE OFF RANGE. THE TAKE OFF WAS ABORTED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON/RUDDER CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040908001532004090800153 2004 9 8 HNAA0400070 420040727A34207003360941 AHRS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE COCKPIT FAILED A HNAAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 EA07940HA 156 WX RADAR FAILED IN FLIGHT DURING TURBULENCE. CND WX RADAR. PROBLEM OCCURRED AFTER LOSS OF THE NR 1 AHRS. REMOVED AND REPLACED NR 1 AHRU. WX RADAR AND AHRS OPS CHECK GOOD. 2H72 4T4 TRTA13NM E20NE 20040908001542004090800154WP 2004 9 8 CALA0400593 120040806A53202929169 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2718835 49439 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 1155 BETWEEN LT IB AND LT MID SEAT TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-5. 2L72 4F4 F A6WE E2EA 20040908001622004090800162NM 2004 9 8 QXEA200400547 120040720A2750 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 300 ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09410QX6272 4053 FLAP POWER CAUTION LIGHT CAME ON DURING APPROACH. RESET CIRCUIT BREAKER L-7 ACCORDING TO CHECKLIST. FLAPS OPERATED NORMALLY AND CAUTION LIGHT REMAINED OUT. COMPLIED WITH LS-27-002A. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040908001642004090800164NM 2004 9 8 WLDA200451 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 17.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 17 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040910000072004091000007NM 2004 9 10 USAA040407 120040806A5754 SKIN BOEING737 737301 1384611NM NR 4 SLAT ASSY CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19592US50576 23937 PIT - FOUND L/E SLAT CRACKED 3.5 INCHES, OUTBOARD, LOWER, TRAILING EDGE, NR 4 SLAT ASSEMBLY. INSTALLED DOUBLER PER SRM 57-43-01. (M) 2L72 4F RTA16WE 20040910000192004091000019 2004 9 10 A6WA200440114 420040816A3414 INDICATOR CNDAIRCL600 CL6002B19 1900309EA AIRSPEED INOPERATIVE A A6WAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL31412AW 7582 ABORTED TAKEOFF AT 110 KNOTS DUE TO STANDBY AIRSPEED INDICATOR READING ZERO KNOTS. TAKEOFF WEIGHT AT 49380 LBS. NO OVERHEAT. FOUND P3 DRAIN TUBE FULL OF WATER. PURGED P3 SYSTEM IAW 34 P3 AND S3 SYSTEM LEAK CHECK GOOD. STANDBY AIRSPEED ALTITUDE. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040910000212004091000021NM 2004 9 10 USAA040417 120040809A57530035711 SKIN BOEING737 7374B7 1384702NM TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU38461 24934 PIT - FOUND FLAP SKIN DELAMINATED WITH 6 INCH SPLIT IN T/E SKIN, 6 INCHES FROM INBOARD END OF RIGHT AFT FLAP, OUTBOARD AFT FLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20040910000222004091000022NM 2004 9 10 USAA040418 120040805A5553 ATTACH FITTING BOEING737 7374B7 1384702NM VERTICAL STAB WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND LUG WITH WEAR .005 INCH DEEP, 1 INCH DIAMETER, VERTICAL STAB AFT OUTBOARD ATTACH LUG RIGHT SIDE BUSHINGS. REBUSHED PER MM 55-30-00 AND DWG 65-52274. (M) 2L72 4F RTA16WE 20040910000232004091000023NM 2004 9 10 USAA040419 120040809A5343656717217 FITTING BOEING737 7373B7 1384580NM LT MLG SUPPORT CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND BEAM FITTING PITTED AND ELONGED, LEFT L/G SUPPORT BEAM STABILIZER BEAM LUG FITTING, ATTACH BOLT HOLES. REAMED HOLES AND INSTALLED FREEZE PLUGS AND REDRILLED HOLES TO ORIGINAL SIZE PER SRM 51-20-10 AND EA 78853. (M) 2L72 4F RTA16WE 20040910000352004091000035NM 2004 9 10 AMTA200401003 120040806A1420 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND EGRESS LIGHTS FROM 13DEF THROUGH 10 DEF INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT 12 DEF, RECONNECTED OPS CHECKS SATISFACTORY. (M) 2L72 4F RTA2NM 20040910000442004091000044NM 2004 9 10 USAA040422 120040723A5343658276427 SUPPORT BEAM BOEING737 7373B7 1384580NM LT MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND SUPPORT BEAM CORRODED .5 INCH BY .25 INCH, AND .375 INCH BY .25 INCH BY .25 INCH, CORROSION PITTING WITH WEAR, LEFT MLG SUPPORT BEAM, STAB BEAM LUG FITTING HOLES (3). 2L72 4F RTA16WE 20040910000462004091000046EU 2004 9 10 USAA040428 120040806A5315 FLOORBEAM AIRBUS320 A320214 3930316EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19107US15460 1052 CLT - FOUND FLOORBEAM CORRODED 3 SQUARE INCHES BY .039 INCH, FRAME 66 AT Y254. INSTALLED DOUBLER PER EA 95752. (M) 2L72 4F RTA28NM 20040910000542004091000054 2004 9 10 UIEA200400147 420040814A3100TD15073002 RELAY BOEING747 7472D3B 1384805NM P14 PANEL INOPERATIVE A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15506MC 21252 REJECTED TAKEOFF DUE TO TAKEOFF WARNING HORN AT 135KTS. STAB TRIM INDICATION SYSTEM TEST CUT OUT IAW MM 27-48-00. OPS NORMAL. STAB TRIM INDICATION AND CONTROL SYSTEM WITH MULTI GREEN BAND CUT OUT OPS NORMAL PER MM 27-48-00. REPLACED RELAY R-586 STAB TRIM GREEN BAND TIME DELAY RELAY PER MM 27-48-00. DURING GREEN BAND FUNCTION TEST NOSE STRUT FOUND TO BE OVER INFLATED. STRUT SERVICED, PRESSURE AND EXTENSION WITH GRAPH TOLERANCE PER MM 12-15-05. (M) 2L74 4F RTA20WE 20040913000052004091300005EA 2004 9 13 ASOA04440 120040620A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN MCN, THE CARGO COMPARMTENT DOOR FLOOR LANDING PLATE AT THE RIVET, FS 589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT DOOR FLOOR LANDING PLATED AT FS 589 IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20040913000072004091300007EU 2004 9 13 2004F00240 120040607A3150ED35E1000301 FDAU AEROSPATR72 ATR72212A 8680902EU E/E BAY SHORTED A TRBAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO21548AT 548 DURING CRUISE FILGHT AT 8,000 FEET, 210 KTS CREW NOTICED LIGHT ELECTRICAL SMOKE IN COCKPIT. DECLARED EMERGENCY AND RETURNED TO BASE. REMOVED AND REPLACED FLIGHT RECORDER. (M) 2H72 4T RTA53EU 20040913000222004091300022EA 2004 9 13 A6WA200440110 120040806A5330 PANEL CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31439AW 7753 ONE FASTENER HOLE ELONGATED FOR ATTACHING PANEL 131AL. REAMED HOLE FABRICATED FREEZE PLUG FROM 2025-T6 .3332 DIAMETER AND INSTALLED IAW BOMBARDIER, INC REO 601R-53-11-162. (M) 2L72 4F RTA21EA 20040913000282004091300028EU 2004 9 13 2004F00300 120040710A7712311649902 SENSOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENGINE MALFUNCTIONED A TRBAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO21440AM 440 127056 DURING APPROACH, RIGHT ENGINE TORQUE FLUCTUATED BETWEEN 20 PERCENT AND UP TO 80 PERCENT UNABLE TO CONTROL ENGINE WAS SHUTDOWN. REPLACED TORQUE SENSOR. (M) 2H72 4T4 TRTA53EU E20NE 20040913000312004091300031EA 2004 9 13 A6WA200440102 120040717A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31429AW 7711 FOUND FLOOR SILL SUPPORT ANGLE AT FS 621 RBL 45 IS CRACKED. PERFORMED A MAJOR REPAIR BY TRIMMING OUT CRACKED AREA OF SUPPORT AGNLE AND INSTALLING REPAIR ANGLE P/N 601R53-61-117-4 IAW BOMBARDIER REO 601R-53-61-117 REV B. (M) 2L72 4F RTA21EA 20040913000352004091300035EA 2004 9 13 ASOA04435 120040618A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040913000382004091300038NE 2004 9 13 2004F00304 220040617A7261 CHIP DETECTOR BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 2 ENGINE MISSING A PCSAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17794AJ 21243 688213 EN ROUTE TO MEXICO, THE NR 2 OIL QUANTITY DECREASED TO ZERO FOLLOWED BY A DROP IN OIL PRESSURE. PRECAUTIONARY SHUT DOWN NR 2 ENGINE. AIRCRAFT DIVERTED BACK TO MMMD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AND FOUND NR 4 BEARING CHIP METAL DETECTOR OFF. RE-INSTALLED CHIP DETECTOR PLUG LEAK CHECK GOOD IAW MM 72-00 AND PWA SERVICE BULLETIN 39-08. ENGINE SERVICED PER MM 12-13-1. AIRCRAFT RETURNED BACK TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20040913000612004091300061CE 2004 9 13 DELA20040002 120040819A216066004238 MOTOR LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE7313A 01518WP TEMP VALVE STUCK E DELAO OTHER J WARNING INDICATION DEDESCENT 1 CE03273MG 119 DURING DESCENT, THE CABIN TEMPERATURE CLIMBED TO AN UNCOMFORTABLE LEVEL. USE OF MANUAL CABIN TEMPERATURE MODE DID NOT CORRECT THE PROBLEM. T/S REVEALED THAT THE CABIN TEMPERATURE CONTROL VALVE TORQUE MOTOR WAS STUCK. REMOVAL AND REPLACEMENT OF THE TORQUE MOTOR WITH AN OVERHAULED UNIT CORRECTED THE PROBLEM. 2L72 4F4 F A10CE E6WE 20040913000642004091300064EU 2004 9 13 04FDEA02606 120040902A5350 FAIRING AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE FUSLEAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25453FE 267 SMIS 453 05-21 0003629 28JUN04 MC1 OPEN R WS-P 00026805 MOD TYPE H MOD NR C-CHECK REV NR PS ACCOMPLISH MAINTENANCE C-CHECK NR 002 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 28JUN04 19:47:42:3 BY:067708 S=M PLND: DATE:01AUG04 AT: LIS-VNMX ENT BY: 067708 ON: 28JUN04 19:47:42:3 S=M DURING C-CHECK, FOUND AFT LOWER FAIRING WITH CRACKS AND WEAR (INTERNALLY AND EXTERNALLY). PYLON SKIN AND FRAMES. FABRICATED NEW PARTS IAW EA 6-5480-55361. 2L72 4F4 FRTA35EU E3NE 20040913000692004091300069EU 2004 9 13 WRNA200400012 120040908A2830 DUMP VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUEL SYSTEM FAILED A WRNAJ DUMP FUEL O OTHER DEDESCENT 1 SO05501TR 53 WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY SELECTED. CLEANED C/P AT RT FUEL JETTISON VALVE ACTUATOR. SECONDARY SYS CHECK'S OK IAW 28-31-00. PRIMARY DEFERRED IAW MEL 28-31-02 CAT-C. 2L72 4F4 FRTA35EU E23EA 20040913002142004091300214NM 2004 9 13 DHL2004745555 120040805A5420 WEB BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NACELLE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; NR 3 NOSE COWL ANTI-ICE DUCT ATTACH ANGLE IS CRACKED ON NAL STA. 77.5 RIB 5 O'CLOCK POSITION. CUT ACCESS HOLE ON NR 3 ENG NOSE COWL AFT RIB WEB NAL STA 99.3 FOR ACCESS IAW SRM 53-10-3 FIG 3. REMOVED DAMAGED ANGLE AND FABED NEW FROM 2024-T3 1040 PO NR 9006720 DIM. 3.5 INCHES X3 INCHES IAW SRM 54-10-2 FIG. 1 TREATED AND PRIMED ANGLE IAW SRM 51-10-2 INSTALLED ANGLE IAW SRM 51-30-2. FABED WEB FROM 2024-T3 .032 DIM 7.2500 INCHES X 5.5 INCHES PO NR 9001000 IAW SRM 53-10-3 FIG3. TREATED AND PRIMED PART IAW SRM 51-10-2 INSTALLED WEB IAW SRM 53-10-3 FIG 3 2L73 4F4 F A3WE E2EA 20040913002172004091300217EA 2004 9 13 ASOA04445 120040620A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN MCN, THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT AFT PRESSURE WALL SIDE CLIPS AT FS 625. (M) 2L72 4F4 FRTA21EA E15NE 20040913002192004091300219WP 2004 9 13 COOSDR040005 120040630A32135759145508 STRUT DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE RT MLG CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 76459 46129 RT MLG SHOCK STRUT RETRACT PIN BOSS, INNER SURFACE CORRODED. 2L74 4F4 F 4A25 1E8 20040914000042004091400004NM 2004 9 14 ASMF200408024 120040828A2410696233B CSD DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT GENERATOR FAILED W ASMFA UNSCHED LANDING M OVER TEMP CRCRUISE 1 SW23162PL9398 49765 725568 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, HIGH TEMPERATURE ON RIGHT CSD. CSD WAS DEFERRED IAW MEL 24-1-1 AND AIRCARFT WAS DISPATCHED, ALL CORRECT. DURING OVERNIGHT SERVICE AT MEX, RT CSD WAS REPLACED IAW MM 24-10-01, TEST WAS CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914000052004091400005NE 2004 9 14 ASMF200408025 220040829A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LEFT MALFUNCTIONED W ASMFO OTHER M OVER TEMP TOTAKEOFF 1 SW23158PL3526011273 49761 725857 CAPTAIN REPORTED THAT DURING TAKE OFF, EGT REACHED 600 DEGREE (C) WITH OAT 38 DEGREE (C). AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, LT FAN AND TURBINE VISUAL INSPECTION WAS PERFORMED, ENGINE OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-00, PARAMETERS WERE WITHIN LIMITS IAW MM 72-00-00. 2L72 4F4 FRTA6WE E9NE 20040914000112004091400011EA 2004 9 14 SWIA200413776 120040830A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07941SW 7750 FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00; RBL 9.0; IB LOCATION. (ITEM FOUND AT C-CHECK INSPECTION.) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16 AND 51-21-11. 2L72 4F4 FRTA21EA E15NE 20040914000412004091400041NM 2004 9 14 DLM88040857 120040906A2720 PACKING DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RUDDER S/O VALVEDETERIORATED A DALAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27969DL 53172 SMOKE ALARM SOUNDED WITH ENGINE A/I ON. ODOR NOTED IN PACK SYSTEM. REPLACED O-RING AT RUDDER SHUTOFF VALVE. CLEANED AFT FUSELAGE SECTION AND COMPLETED ALTERNATE DUCT BURNOUT. CHECKS GOOD. 2L72 4F4 FRTA6WE E9NE 20040914000522004091400052NM 2004 9 14 C8GA20040011 120040713A3411 PITOT LINE BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 1 ENGINE OBSTRUCTED A C8GAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO15713AA 22469 DURING TAKE-OFF ROLL, UNABLE TO REACH TARGET TAKE-OFF EPR SETTING ON NR 1 ENGINE. ABORTED TAKE-OFF AND RETURNED TO BLOCKS. UPON RETURNED TO BLOCKS, TROUBLESHOOT THE EPR SYSTEM AND FOUND THE PT-2 INLET OBSTRUCTED. CLEARED OBSTRUCTION BUT EPR READING CONTINUES INDICATING HIGH DURING ENGINE RUN. DEFERRED THE NR 1 ENGINE EPR SYSTEM IAW MEL 77-1-1. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 77-1-1 ON 7/13/2004 UPON ARRIVING, CLEARED THE OBSTRUCTION ON THE PT-2 LINE AND PERFORMED THE NR 1 ENGINE EPR SYSTEMS CHECKS IAW MM 77-10-0 AND 72-00-0. GROUND RUN CHECKS GOOD AND MEL 77-1-1 WAS CLEARED AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20040914000552004091400055WP 2004 9 14 DHL2004804534 120040731A57203804001 CLIP DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUEL TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR. 2091: NR 1 ALT. TANK LWR SECTION INTERIOR CLIP CRACKED (STA. XRS 456.562 - 460.000, S-62L TO S-63L). REMOVED CRACKED CLIP IAW DC8 SRM 51-1-20D PG. 21. FABRICATED NEW CLIP (AL 7075-T651) IAW EA NR 5720-037, DWG 3864001. HEAT TREATED IAW DACO CP 7.00. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW CLIP IAW SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20040914000562004091400056WP 2004 9 14 DHL2004804532 120040712A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BELLY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 NR. 1072: EXTERNAL FUSELAGE-D BELLY DOOR AFT UPPER JAMB CORNER CRACKED 1.000, STA. 1440.000, L-26 TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD 2004-06-06, SB DC8 53-0-78 R1, DWG SR08530019 CONFIGURATION H, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW DWG SR08530019. CLEANED, TREATED AND PRIMED REPAIR AREA IAW SRM 51-1-8B. FABRICATED FILLER (AL 7075-T6 0.080) DOUBLER (AL 7075-T6 0.090) TRIPLER (AL 7075-T6 0.125) IAW DWG SR08530019. CLEANED, TREATED AND PRIMED FILLER, DOUBLER AND TRIPLER IAW SRM 51-1-8B. INSTALLED CONICAL WASHER IAW SRM 51-1-26. INSTALLED FILLER, DOUBLER AND TRIPLER IAW DWG SR08530019, SRM 51-1-20D PG.9, SRM 51-1-21 PG.1. PERFORMED REPETITIVE INSPECT2L74 4F4 FRT4A25 E2GL 20040914000572004091400057NM 2004 9 14 DHL2004745503 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT FUSE HAS A DENT AFT BS640 ABOVE STR 23R. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE DIM 2.5 INCH X 2.2500 INCH AND FABBED DOUBLER FROM 2024 T3 .080 PO NR 9001135 DIM 11.3750 INCH X 8.5 INCH IAW SRM 53-30-3 FIG 1. DOUBLER TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2 AND 53-30-3 FIG 1. 2L73 4F4 F A3WE E2EA 20040914000602004091400060EU 2004 9 14 CX7A194J0442 120040722A26131734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT TAILPIPE SATURATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03314CE 340B335 RT TAIL PIPE HOT CWP ILLUMINATED BEFORE STARTING ENGINES. 2L72 4T4 TRTA52EU E8NE 20040914000612004091400061WP 2004 9 14 DHL2004804530 120040725A5730 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LT OUTER WING OB STUB WING SKIN CORRODED (UPPER PART) XOLDO 67.000. PERFORMED MAJOR REPAIR IAW EDEDW 27.3, DWG W27 R03 REV. IR. REMOVED FASTENERS IAW SRM 51-3-0 PG.1, SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. TRIMMED OUT CORRODED AREA IAW ED EDW 27.3, DWG W27-R03. FABRICATED DOUBLER (AL 7075-T6 0.071) AND FILLER (AL 7075-T6 0.063) IAW ED EDW 27.3, DWG W27-R03. CLEANED, TREATED AND PRIMED AREA AND DOUBLER AND FILLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED DOUBLER AND FILLER WITH NEW FASTENER IAW ED EDW 27-3, DWG W27-R03, SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2L74 4F4 FRT4A25 E2GL 20040914000642004091400064NM 2004 9 14 F3LA200400082 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD, RBL 5.7, BELOW WL 207 IB OF RBL 5.7 AT LOWER RADAR ANTENNA MOUNT. PERFORMED REPAIR IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210, DETAIL VII. 2L72 4F RTA16WE 20040914000652004091400065NM 2004 9 14 F3LA200400083 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7 VERTICAL CORD AND ABOVE WL 207. REMOVED DAMAGE FROM BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-10-08. 2L72 4F RTA16WE 20040914000672004091400067NM 2004 9 14 F3LA200400084 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED TWO CRACKS AT BL 0, ABOVE WL 184.5 AT 188.0, 178 BULKHEAD. REPAIRED CRACKS AT BL 0 ABOVE WL 184.5 IAW SRM 53-10-08, FIG. 211, DETAIL VIII AND EA B3-53R-10470. 2L72 4F RTA16WE 20040914000682004091400068NM 2004 9 14 F3LA200400085 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSLEAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACKS ON 178 BULKHEAD AT IB SIDE OF LBL 5.7 VERTICAL CORD AND BELOW WL 207. REPAIRED CRACKS ON 178 BULKHEAD BELOW WL 207 IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210. 2L72 4F RTA16WE 20040914000692004091400069NM 2004 9 14 DHL2OO4745557 120040820A5542 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE RUDDER DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; RT VERT STAB RUDDER EXTERIOR SKIN (LWR RUDDER) AT ABOUT FIN STA. 162.5 SKIN SURFACE HAS SEVERAL DENTED CREASES. FABRICATED DOUBLER 7 INCHES X 2 INCHES, 2024T3 .032 PO NR 991797 IAW SRM 55-20-3 TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED DOUBLER REPAIR ON R/W VERT EXTERIOR SKIN LWR RUDDER IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20040914000702004091400070NM 2004 9 14 DHL2004745558 120040630A5753 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE TE FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT IB MID FLAP TE TOP SKIN DEBONDED AREA WBL 203. CUT OUT DAMAGED AREA OF L/W IB MID FLAP UPPER SKIN APPROX 4.2500 INCHES X 5.7500 INCHES IAW SRM 51-40 -20 FIG 30 FABRICATED ONE FILLER APPROX 4.2500 INCHES X 5.7500 INCHES AND TWO DOUBLERS APPROX 3 INCH X 4.2500 INCHES USING 2024-T3 .016 PO NR 900573 IAW SRM 57-50-2 FIG 3 CLEARED, PREPPED, APPLIED ADHESIVE, PRIMER ADHESIVE TO ALL MATING SURFACES BONDED, CURED, SANDED, CLEANED, TREATED AND PRIMED AND SEALED REPAIR IAW SRM 51-40-20-FIG 30. 2L73 4F4 F A3WE E2EA 20040914000742004091400074 2004 9 14 RAIA00407020 420040706A34604006719904 SERVO JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE COCKPIT MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03574HK14803 41093 FLIGHT DIRECTOR FAILED ON TAKEOFF ROLL. MAINTENANCE DEFERRED FLIGHT DIRECTOR IAW MEL. SUBSEQUENTLY CLEARED MEL BY REMOVING AND REPLACING YAW DAMPENER SERVO. 2L72 4T4 TRTA41NM E18NE 20040914000752004091400075NM 2004 9 14 F3LA200400087 120040819A5314 KEELBEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED KEELBEAM CORRODED AT STA 520 WHERE IT ATTACHES TO STRINGER 28-R. INSTALLED REPAIR TO RT. KEELBEAM AT CORRODED AREA BETWEEN BS 500D AND 520 IAW EA B3-53R-10478. 2L72 4F RTA16WE 20040914000782004091400078EU 2004 9 14 KBM2004F00210 120040809A2100 BRUSHES SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE CONDES MOTOR FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1737SH 2300 7 IN BRUSHES, CONDENSER MOTOR, UNIT INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040914000792004091400079NM 2004 9 14 04FDEA02186 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE FUSLEAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION SEAT TRACK BS 870, LBL 45, WL 208. REMOVED CORROSION ON SEAT TRACK STA 870 LBL 45, WL 208. REMOVED .040, 1 INCH X 1 INCH FROM .080. OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED, ALODINED AND PRIMED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK IAW SRM 53-10-1, 51-30-02, 51-30-08, 53-10-5 MM 51-20-021-7, 51-20-151-7. 2L73 4F4 FRTA3WE E2EA 20040914000802004091400080SO 2004 9 14 RAIA00408018 120040815A3244 TIRE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG SEPARATED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03815HK 145048 DURING POST FLIGHT INSPECTION AT STL FOUND LT IB TIRE RECAP TREAD MISSING. MAINTENANCE REMOVED AND REPLACED NR 3 MAIN LANDING GEAR AND TIRE ASSEMBLY. PERFORMED TIRE FAILURE INSPECTION AND REPAIRED FOD DAMAGE CAUSED BY TREAD SEPARATION. 2L72 4T4 FRTT00011ATTE6CH 20040914000812004091400081EU 2004 9 14 RAIA00408020 120040816A612031058993 TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03560HK 41076 75099 BOTH IEC FAULTED. MAINTENANCE REMOVED AND REPLACED NR 2 NTS PRESSURE TRANSDUCER. 2L72 4T4 TRTA41NM E18NE 20040914000832004091400083SO 2004 9 14 RAIA00408017 120040814A323023092900021 UPLOCK EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03801HK 145053 GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR UPLOCK ASSEMBLY. 2L72 4F4 FRTT00011ATTE6CH 20040914000852004091400085NM 2004 9 14 AMTA200400847 120040707A335020131A BATTERY PACK BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 NUMEROUS EMERGENCY EXIT LIGHTS INOPERATIVE. INSTALLED BATTERY PACK, OPS CHECK OK IAW MM 33-51-07. 2L72 4F4 FRTA2NM A12EU 20040914000862004091400086SO 2004 9 14 RAIA00408019 120040819A2913MPEV30086 PUMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT HYD SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03811HK9096 145256 LT HYDRAULIC PUMP INOPERATIVE. MAINTENANCE REMOVED AND REPLACE LT ELECTRIC HYDRAULIC PUMP. 2L72 4T4 FRTT00011ATTE6CH 20040914000882004091400088SO 2004 9 14 RAIA00408021 120040817A1420 CONNECTOR EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03801HK 145053 EMERGENCY LIGHTS AT 12A INOPERATIVE. MAINTENANCE RESECURED ELECTRICAL CONNECTOR. 2L72 4F4 FRTT00011ATTE6CH 20040914000902004091400090SO 2004 9 14 RAIA00408014 120040807A3610S2D226 SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 BLEED SYS LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03817HK 145058 BLEED LEAK INDICATION NR 2 BLEED. MAINTENANCE REMOVED AND REPLACED BLEED DUCT SEAL UNDER BAGGAGE COMPARTMENT. 2L72 4T4 FRTT00011ATTE6CH 20040914000922004091400092NM 2004 9 14 DHL2004752005 120040804A3260 ACCESSORY UNIT BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE MLG MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01752DH 22466 AFTER T/O, LANDING GEAR LEVER WOULD NOT MOVE PAST (OFF) POSITION. CONDUCTED ABNORMAL PROCEDURE T/O CONFIG WARNING HORN SOUNDED AT FLAPS 2 DEG. DIVERTED BACK TO KDAL IAW RE-RELEASE AT 0359Z (SR). REMOVED AND REPLACED LGAU IAW MM 32-09-121. OPS CK GOOD. LG HANDLE OPS CK GOOD IAW 32-32-11. OPS CK GOOD. 2L73 4F4 F A3WE E2EA 20040914000942004091400094SO 2004 9 14 2004F00233 120040702A36101159AC2002751 DUCT GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU TAIL SEPARATED E E ENGINE SHUTDOWN S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA071NA 309 COUPLING SEPARATED FROM END OF APU/GROUND START APU DUCT ASSY. 2L72 4F4 F A12EA E2EU 20040914000952004091400095 2004 9 14 UIEA200400095 420040525A25657A14124REVB SLIDE BOEING747 7472D7B 1384803NM UPPER DECK DOOR DEPLOYED A UIEAK NONE L NO TEST ININSP/MAINT 1 EA15523MC 21782 DURING TEST, THE UPPER DECK SLIDE FAILED TO FULLY DEPLOY. SLIDE (PN 7A14124, SN GU148 WAS REMOVED AND REPLACED WITH A NEW SLIDE PN 7A1248-36, SN G639. 2L74 4F RTA20WE 20040914000972004091400097NM 2004 9 14 UPS04243009 120040817A5311 FRAME BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 C FRAME LEG CRACKED AT BS 294, STR 9/10L. DAMAGED PORTION OF FRAME REMOVED IAW SRM 53-10-4. HFEC CARRIED OUT AROUND CUTOUT: NO DEFECTS FOUND. REPAIR CARRIED OUT IAW 53-10-4. 2L73 4F4 F A3WE E25NE 20040914000982004091400098CE 2004 9 14 231041 120040816A3000 CONTROL PANEL CESSNA150 152 2071835CE LYC O235 O235* 41505EA COCKPIT CORRODED A NSVAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27152CJ 15281682 SMOKE COMING FROM WING ICE CIRCUIT BREAKER PANEL, PULLED BREAKER APPEARED TO STOP SMOKING. MAINTENANCE OPENED PANEL, RT SIDE CORROSION NOTED. CLEANED CORROSION, REMOVED CIRCUIT ON WING ICE LIGHT MOVED HARD WIRE BRIDGE. ICE WING LIGHTS NOTED INOPERATIVE, WING ICE LIGHT MEL 33-11. 1H71 3O3 ONT3A19 E223 20040914001022004091400102NM 2004 9 14 UPS04443011 120040822A5340 FITTING BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, RT BS 1241 REAR SPAR UPPER SPLICE PLATE CRACK FOUND AT HOLE NR 6, APPROX 0.090 INCH IN LENGTH RUNNING AFT ( STR R28 TO R28) CRACKED HOLE REAMED TO 1.000 INCH IAW EO B747-5740-17032. 2L74 4F4 FRTA20WE E3NE 20040914001032004091400103NM 2004 9 14 P9RA20040024 120040801A278140173 PROXIMITY SENSOR BOEING737 737231 1384079NM PWA JT8 JT8D217C 52053NE NR 4 SLAT LOOSE A P9RAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1154344 21631 ON CLIMB OUT, NR 4 SLAT DID NOT INDICATE RETRACTED. RETURNED. NO EMERGENCY DECLARED. LANDING UNEVENTFUL. FOUND EXTEND PROXIMITY SWITCH LOOSE IN BRACKET. RESECURED SAME. OPERATIONALLY TESTED GOOD. 2L72 4F4 FRTA16WE E9NE 20040914001052004091400105GL 2004 9 14 KBM2004F00171 220040206A751067A258 ACTUATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ANTI-ICE SYS INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 695 2513 ENGINE ANTI-ICE MOTOR INTERMITTENT. REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20040914001072004091400107 2004 9 14 ASMF200407030 420040725A2565 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE PAX DOOR DISLODGED W ASMFK NONE W INADEQUATE Q C ININSP/MAINT 1 SW23505MD 49149 DURING TRANSIT CHECK, CAPTAIN REPORTED THAT FOOD SERVICES COMPANY PERSONNEL FELL DOWN THROUGH LT SERVICE DOOR SLIDE. LT SERVICE DOOR SLIDE WAS REINSTALLED IAW MM 25-62-01. DURING OVERNIGHT SERVICE, LT SERVICE DOOR SLIDE INSTALLATION WAS CHECKED IAW MM 25-62-01, ALL CORRECT. 2L72 4F4 F A6WE E2EA 20040914001112004091400111EU 2004 9 14 KBM2004F00208 120040819A2120060018 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE AIR CONDITIONINGBURNED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH9184 2957 BELT BURNED AND SNAPPED (AIR CONDITIONING). REPLACED BELT, EXPANSION VALVES, HIGH PRESSURE SWITCH AND RESERVICED SYSTEM TO 2.75 LBS OF R-138. 1G71 3U3 UNCH9EU E19EU 20040914001132004091400113 2004 9 14 ASMF200408010 420040809A3418 RELAY DOUG MD80 MD83 3023681NM PWA JT8 JT8D217A 52053NE STALL COMPUTER MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23831LF 53050 AIRCRAFT RETURNED TO PLATFORM, (SIF) LIGHT TURNED ON. SYSTEM WAS CHECKED AND RELAY R2-58 WAS DETECTED ON FLIGHT POSITION AFFECTING LT STALL COMPUTER. RELAY WAS REPLACED IAW MM 32-62-00 AND TESTED IAW MM 34-19-00, ALL CORRECT. 2L72 4F4 FRT E9NE 20040914001142004091400114NE 2004 9 14 KBM2004F00201 220040611A72609560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE LEAKING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV193 3296 SEAL LEAKING, REMOVED AND REPLACED WITH RECONDITIONED UNIT. 1G71 3U3 U H9EU E19EU 20040914001152004091400115EU 2004 9 14 KBM2004F00205 120040805A6730AC67244 SERVO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MAIN ROTOR RESTRICTED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH1170 2957 RESISTANCE FELT WHEN APPLYING LT INPUT ON CYCLE. REMOVED DEFECTIVE SERVO AND INSTALLED UNIT, RESISTANCE IS NO LONGER FELT. 1G71 3U3 UNCH9EU E19EU 20040914001162004091400116EU 2004 9 14 KBM2004F00203 120040613A21210500847 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE A/C BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH20 3345 NOT BLOWING COLD AIR, 7 IN BLOWER MOTOR, REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040914001202004091400120EA 2004 9 14 REX2004F00004 120040703A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG OUT OF POSITION A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258933B 7933 ON DESCENT RECEIVED GEAR DISAGREE (NOSE DOOR). QRH FOLLOWED HOWEVER, INDICATION REMAINED. GEAR MANUALLY LOWERED RECEIVED THREE GREEN, UNEVENTFUL LANDING. NOSE GEAR PROXIMITY SENSOR FOUND TO BE OUT OF POSITION. ADJUSTED IAW AMM, GEAR SWINGS PERFORMED AND OPERATIONAL CHECK OF STEERING PERFORMED. 2L72 4F4 FRTA21EA E15NE 20040914001212004091400121NM 2004 9 14 UIEA200400116 120040622A27801267481 DRIVE UNIT BOEING747 747271C 1384869NM GE CF6 CF650E2 30018NE SLATS UNSERVICEABLE A UIEAJA DUMP FUEL UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA15537MC 22403 DURING CLIMB LT L/E NR 2 AMBER LIGHT REMAINED ILLUMINATED. ALTERNATE PROCEDURES ACCOMPLISHED TO NO AVAIL. WITH NR 2 L/E DIRECTIONAL SW TO (UP), ALTERNATE L/E FLAP DRIVE C/B ON P6 TRIPS. 27000 KG FUEL DUMPED IAW FUEL JETTISON CHECKLIST AT FL140 TO MAX LANDING 295000 KG. REMOVED AND REPLACED L/E DRIVE UNIT IAW MM 27-81-03. FUNCTIONAL CHECK ACCOMPLISHED, ALL NORMAL. 2L74 4F4 F A20WE E23EA 20040914001222004091400122NM 2004 9 14 RIV2004F00000 120040703A3233651783012M ACTUATOR BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE RT MLG LEAKING A RIVAL ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO15364PA 21107 FLIGHT CREW WAS UNABLE TO EXTEND THE RT MLG ON AC. DURING INITIAL APPROACH, THE APPROACH WAS ABORTED AND THE CREW ALLEGEDLY ACCOMPLISHED ALL APPROPRIATE CHECKLIST ITEMS. THE RT MLG WOULD STILL NOT EXTEND USING THE MANUAL EXTENSION SYSTEM, ( THE GEAR APPEARED TO BE UNLOCKED BUT HANGING APPROX HALFWAY DOWN). AS THEY MANEUVERED THE AIRCRAFT, THE RT MLG FINALLY EXTENDED FULLY AND A SAFE LANDING WAS ACCOMPLISHED. THE AC WAS JACKED AND DURING A GEAR SWING THE INITIAL PROBLEM WAS DUPLICATED. THE RT MLG WOULD ONLY PARTIALLY EXTEND. THE RT MLG ACTUATOR, WAS THEN REPLACED. (THE RT MLG DOOR ACTUATOR WAS ALSO REPLACED DUE TO EVIDENCE OF LEAKAGE.) GEAR SWINGS WERE NORMAL. 2L73 4F4 FRTA3WE E2EA 20040914001242004091400124WP 2004 9 14 IMJ2004F00003 220040601A7314307085057 PUMP RAYTHNDH125 HAWKER800 7450004CE GARRTTTFE731TFE7315BR WP FUEL SYSTEM FAILED E IMJAO OTHER O OTHER NRNOT REPORTED 1 EA25256BC 258256 P91634 NR 2 ENGINE FUEL LIGHT ILLUMINATED IN FLIGHT. FUEL PUMP FAILED 2L72 4F4 FRTA3EU E6WE 20040914001292004091400129EA 2004 9 14 SWIA200413632 120040726A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07447SW 7677 FLIGHT SPOILERS FAULT IN FLIGHT. REMOVED AND REPLACED IB AND OB FLIGHT SPOILER ACTUATOR IAW 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF 5738, 5771. 2L72 4F4 FRTA21EA E15NE 20040914001312004091400131EA 2004 9 14 SWIA200413633 120040725A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07923SW4950 4950 7664 LT HAND SPOILERON INOPERATIVE. REMOVED AND REPLACED LT IB SPOILERON PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-62-01. 2L72 4F4 FRTA21EA E15NE 20040914001332004091400133EA 2004 9 14 SWIA200413637 120040727A273010231007 DAMPER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT ELEVATOR INTERMITTENT A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07461SW3147 7811 LT ELEVATOR FLUTTER DAMPER MESSAGE COMES ON INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED LT ELEVATOR OB FLUTTER DAMPER IAW AMM 27-34-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040914001362004091400136NE 2004 9 14 ASMF200407018 220040716A7530805373 PRBC DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT SIDE FAILED W ASMFK NONE MJ OVER TEMP WARNING INDICATION ININSP/MAINT 1 SW23803ML8568 1208 49726 728169 DURING TRANSIT CHECK WAS DETECTED HIGH TEMPERATURE ON LT ENGINE, REACHED 482 DEGREE F. ENGINE RUNNING WAS PERFORMED TO VERIFY EGT INDICATION APPLYING PNEUMATIC AND ELECTRICAL CHARGES GETTING MAXIMUM TEMPERATURE INDICATION OF 445 DEGREE F, BEING WITHIN LIMITS IAW MM 71-00-01. DURING OVERNIGHT SERVICE, LT PRBC AND P AND D VALVE WERE REPLACED IAW MM 75-31-01 AND 73-13-05, TESTS CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001392004091400139NM 2004 9 14 TIP2004F00000 120040505A53157073761505101303FLOORBEAM BOEING767 76733AER 1385230NM FUSELAGE CORRODED B TIPRO OTHER O OTHER NRNOT REPORTED 1 SO05637TW 25403 CABIN FLOORBEAM STA 1480, RBL 42, CORRODED. CORROSION OUT OF LIMITS IAW B767 SRM REPAIR REQUIRED. FLOORBEAM IS NEAR GALLEY AREA WHERE SPILLS OCCUR. NEED TO MAKE SURE OF PROPER CIC APPLICATION. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS. 2L72 4F RTA1NM 20040914001522004091400152EU 2004 9 14 USA2004F00089 120040617A5330 SKIN AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DENTED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19709UW 0997 FOUND DENT IN FUSELAGE SKIN, 1 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040914001552004091400155WP 2004 9 14 ASMF200407016 120040713A793142D1091A PRESSURE SWITCH DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ENGINE OIL FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23838AM10075 49397 716779 AIRCRAFT REJECTED TAKE OFF AT 60 KNOTS, (LT OIL STRAINER CLOGGING) LIGHT TURNED ON AND RETURNED TO PLATFORM. LOW OIL PRESSURE SWITCH AND MAIN OIL FILTER WERE REPLACED IAW MM 79-33-00 AND 79-20-06, RESPECTIVELY, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001582004091400158NM 2004 9 14 GAIA04085OP 120040702A33501000679 LIGHT BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE L-1 DOOR INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07751US 21513 POST FLIGHT FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20040914001592004091400159NE 2004 9 14 ASMF200407031 220040727A7261 FILTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ENGINE CLOGGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL7955 759 53175 725620 AIRCRAFT SUSPENDED TAKEOFF AND RETURNED TO PLATFORM, CAPTAIN REPORTED RT OIL FILTER CLOGGED LIGHT TURNED ON. LIGHT INDICATION WAS CHECKED AND ENGINE WAS TESTED AT 1.7 OF EPR AND LIGHT DID NOT TURN ON. AS A PRECAUTIONARY ACTION, OIL FILTER AND ALARM WERE REPLACED IAW MM 79-20-06 AND 79-35-01, TESTS CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001602004091400160WP 2004 9 14 ASMF200407027 120040724A2410 CSD DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LEFT FAILED W ASMFA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW23216AM 49586 718411 AIRCRAFT RETURNED OF FLIGHT, HIGH TEMPERATURE ON LT CONSTANT SPEED DRIVE (CSD), AND APU OUT OF SERVICE. LT CSD WAS CHECKED AND HIGH LEVEL OF OIL WAS DETECTED, OIL SERVICE WAS PERFORMED IAW MM 12-12-52, CSD AND APU WERE OPERATIVE, ALL CORRECT. DURING OVERNIGHT SERVICE, HEAT EXCHANGE ASSY AIR/OIL AND CONSTANT SPEED DRIVE WERE REPLACED IAW 24-10-01 AND 24-10-03, TESTS CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001612004091400161WP 2004 9 14 O9I2004F00000 220040630A732189352831 FCU GULSTM690TP 690A 0141722SW GARRTTTPE331TPE3315 01514WP NR 2 ENGINE FAILED E O9IAO OTHER O OTHER NRNOT REPORTED 1 NM09290PF 11290 P06285 THE NR 2 ENGINE FCU FAILED TO PROPERLY LIMIT FUEL TO THE ENGINE. DURING THE FINAL DECENT, THE FLIGHT CREW BROUGHT BACK THE THROTTLES TO THE FLIGHT IDLE POSITION FOR LANDING. IT WAS NOTED AT THAT TIME THAT THE NR 2 ENGINE WAS STILL PRODUCING 250 HP, A LEVEL HIGHER THAN NORMAL FOR THAT SETTING. THE FLIGHT CREW CONTACTED MAINTENANCE FOR ADDITIONAL INFORMATION. THE FLIGHT CREW ELECTED TO MAKE A PRECAUTIONARY SINGLE ENGINE LANDING. THE ENGINE WAS SHUT DOWN AND A SINGLE ENGINE LANDING WAS MADE WITHOUT INCIDENT. AFTER PERFORMING GROUND RUNS AND TROUBLESHOOTING PROCEDURES, FUEL CONTROL WAS FOUND TO HAVE FAILED. THE FUEL CONTROL WAS CHANGED WITH AN OVERHAULED UNIT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1H72 3T4 T 2A4 E4WE 20040914001632004091400163NM 2004 9 14 TIP2004F00002 120040429A5315141T510848 FLOORBEAM BOEING767 76733AER 1385230NM FUSELAGE CORRODED B TIPRO OTHER O OTHER NRNOT REPORTED 1 SO05637TW 25403 CABIN FLOORBEAM AT STA 325 RBL 24 THRU 54, CORROSION OUT OF LIMITS. B767 SRM, REPAIR REQUIRED. FLOORBEAM CORRODED BECAUSE OF GALLEY AREA LEAKS. GALLEY AREA NEEDS TO BE PROPERLY SEALED. AIRCRAFT WAS IN STORAGE FOR APPROX 2 YEARS. (TASK CARD NR S53-027-02) 2L72 4F RTA1NM 20040914001642004091400164NM 2004 9 14 TIP2004F00003 120040429A5315141T5106103 FLOORBEAM BOEING767 76733AER 1385230NM FUSELAGE CORRODED B TIPRO OTHER O OTHER NRNOT REPORTED 1 SO05637TW 25403 CABIN FLOORBEAM AT STA 287, RBL 20 THUR 82. CORROSION OUT OF LIMITS IAW B767 SRM REPAIR REQUIRED. FLOORBEAM UNDER WET AREA, SPILLS AND LEAKS CORRODED FLOORBEAM. GALLEY AREAS NEED MILAR VAPOR BARRIER INSTALLED AND SEALED AREA PROPERLY. AIRCRAFT WAS IN STORAGE FOR APPROX, 2 YEARS, MAY NEED TO INCREASE INSPECTION INTERVAL IN THIS AREA. 2L72 4F RTA1NM 20040914001682004091400168WP 2004 9 14 ANCF200400015 120040630A3244 TIRE DOUG DC9 DC983 3022083WP MLG FAILED W ANCFC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO23190AN 53190 DURING T/O, STRONG VIBE FELT ON MLG WITH SUDDEN LOSS OF PWR ON LT ENG. PARAMETER DE & INCREASED FROM 1.3-1.8 EPR CONSTANT UNTIL 10000 FT, LT ENG STABILIZED. RETURNED TO DEPART. NORM LANDING. LT MLG RED LIGHT CAME ON CONSTANT. LT MLG IB WHEEL, TREAD SEPARATION, RUPTURE OF TIRE CARCASS IN TREAD AREA. 2L72 4F RTA6WE 20040914001712004091400171EA 2004 9 14 SWIA200413603 120040720A27604916420 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07939SW 7742 RECEIVED GROUND SPOILERON, SPOILERONS AND FLIGHT SPOILERS FAULT STATUS MESSAGE. REPLACED SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N 49-164-20, S/N OFF 01389. 2L72 4F4 FRTA21EA E15NE 20040914001722004091400172EA 2004 9 14 SWIA200413604 120040719A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE APU BAY FIRE A SWIAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 NM07594SW3332 3332 7285 APU SHUT DOWN WITHOUT WARNING. ATTEMPTED RESTART. GROUND PERSONNEL ADVISED FLAMES PRESENT. DISCHARGED APU BOTTLE. INSPECTED APU COMPARTMENT AND AIRFRAME, NO FIRE DAMAGE NOTED. APU FIRE BOTTLE DISCHARGED. REPLACED APU WITH A SERVICEABLE UNIT IAW 49-10-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040914001732004091400173EU 2004 9 14 USA2004F00072 120040605A335032146210 EPSU AIRBUS330 A330323 3930335EU PWA 4158 PW4158 NE R2 DOOR WILL NOT TEST A USAAO OTHER L NO TEST NRNOT REPORTED 1 EA19678US 0388 EPSU R2 WOULD NOT TEST. MAINTENANCE REPLACED THE EPSU. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA46NM E24NE 20040914001802004091400180WP 2004 9 14 ASMF200407009 120040705A2910392492 SERVO VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D1 52044NE HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23205AM113822325 49405 DURING TRANSIT CHECK, HYDRAULIC LIQUID LEAK WAS DETECTED ON RT MAIN LANDING GEAR WELL, BOTH SYSTEMS WERE PRESSURIZED, BRAKES AND CONTROL SURFACES WERE ACTUATED AND LEAK WAS DETECTED ON ANTI-SKID RT DOUBLE SERVO VALVE. SERVO VALVE WAS REPLACED IAW MM 32-43-02, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20040914001812004091400181EU 2004 9 14 KBM2004F00188 120040506A6510350A34015002 DRIVE ASSY SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA 2143 T/R DRIVE (SHORT SHAFT) FORWARD COUPLING ATT BOLTS TO ENGINE TAKE OFF FLANGE FAIL TORQUE LOAD CHECK REQUIRES UNIT TO BE SENT TO MANUFACTURER FOR INSPECTION. ASSEMBLED AT FACTORY DURING 12 YEAR 5000 HOUR INSPECTION. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040914001842004091400184SO 2004 9 14 HFB2004F00000 220040709A7261560010715 LINE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO OIL PRESSURE CORRODED B HFBRO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW03812SR4957 414A0326 LT ENGINE LOST OIL PRESSURE. OIL PRESSURE LINE IN LT SIDE PANEL BY PILOT`S LT LEG HAD CORROSION HOLE IN IT. APPROXIMATELY 5 WEEKS LATER LT ENGINE LOST OIL PRESSURE AGAIN. OIL PRESSURE LINE UNDER FLOOR UNDER PILOTS SEAT HAD CORROSION HOLE IN IT. 1L72 3O3 O A7CE E8CE 20040914001882004091400188CE 2004 9 14 MWR2004F00000 120040722A2422 INVERTER BEECH 90 65A901 1152901CE PWA PT6 PT6A20 52043EA NR 1 FAILED D MWRGO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA1770264 2039 LM17 AIRCRAFT WAS RESENT TO MAINTENANCE FOR REPORTED SMOKE IN COCKPIT. PILOT REPORTED LOSS OF NR 1 INVERTER CIRCUIT BREAKER POPPED. TROBLESHOT PROBLEM TO PRIMARY INVERTER UNIT PC-17. 1L72 3T3 T 3A20 E4EA 20040914001902004091400190NM 2004 9 14 ASMF200408014 120040816A7711LG80E1 COMPUTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT EPR FAILED W ASMFK NONE J WARNING INDICATION CRCRUISE 1 SW23158PL10896 49761 725605 AIRCRAFT ARRIVED TO THE STATION WITH CAPTAIN REPORT (1.5 OF EPR'S DIFFERENCE BETWEEN ENGINES). TECHNICAL PERSONNEL WERE SENT TO THE STATION AND DURING TROUBLESHOOTING ANALYSIS RT EPR RT TRANSMITTER WAS REPLACED AND WATER TRAMP WAS DRAINED IAW MM 77-11-02 AND 73-20-03. PT2 AND PT7 LINES WERE CHECKED IAW CONDITION AND ENGINE RUN TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001912004091400191WP 2004 9 14 ASMF200408015 120040817A2410696233B CSD DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT FAILED W ASMFO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW23751RA2838814220 49779 CAPTAIN REPORTED THAT DURING CLIMB RT CSD REACH 180 DEGREES (C), BEING NOT POSSIBLE TO SHUTOFF AND R CSD OIL PRESS LOW LIGHT TURNED ON. ADDITIONALLY, DURING DESCEND WHEN THE APU WAS STARTED THE CSD TEMPERATURE COOL DOWN. TECHNICAL PERSONNEL PERFORMED CSD SHUTOFF TESTS CONFIRMING THE FAILURE. CSD AND RADIATOR WERE REPLACED IAW MM 24-10-01 AND 24-10-03 RESPECTIVELY, TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001922004091400192NM 2004 9 14 UIEA200400107 120040602A5414 SKIN BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 2 NACELLE CRACKED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 (D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE AND EXPOSED WINDOW STRAP SURFACE, ALONG WITH FASTENER HOLES, HFEC INSPECTED TO ENSURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .254. RIB INSTALLATION AT NAC STA .248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON NR 3 STIFFENER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS.2L74 4F4 F A20WE E23EA 20040914001942004091400194NM 2004 9 14 UIEA200400099 120040524A32321U11715 ACTUATOR BOEING747 74747UF 1384949NM GE CF6 CF680 30025NE LT MLG INOPERATIVE G UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15408MC 29261 TAKEOFF WARNING (CONFIGURATION BODY GEAR) DISPLAYED DURING TAKEOFF. CMC GAVE LT GEAR OB ACTUATOR SWITCH MESSAGE 32055. DEACTIVATED ALL ACTUATORS INDICATION SYS IAW MEL AND TRANSFERRED ITEM TO DMI. (DEACTIVATED RT OB CYLINDER IAW MEL). REMOVED AND REPLACED LT OB BODY GEAR STEERING ACTUATOR IWA MM. OPERATION AND INDICATION OF BODY GEAR STEERING CHECK NORMAL. 2L74 4F4 FRT1384945 E13NE 20040914001952004091400195NM 2004 9 14 UIEA200400112 120040607A5743 BEAM BOEING747 747243B 1384830NM GE CF34 CF34* NE LT WING LE CRACKED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15517MC 23300 LT WING FIXED LEADING EDGE NOSE BEAM UPPER CHORD AND LOWER CHORD AND WEB CRACKED AT ILES 1116.00. REMOVED FASTENERS IAW SRM, REMOVED DAMAGED UPPER AND LOWER CHORD BY CUTOUT METHOD IAW SRM REMOVED WEB IAW SRM. FABRICATED UPPER, AND LOWER CHORDS FROM SRM. FABRICATED WEB FROM SRM, TREATED AND PRIMED IAW SRM. INSTALLED PARTS IAW SRM. 2L74 4F4 F A20WE E15NE 20040914001962004091400196NM 2004 9 14 UIEA200400111 120040607A3234 HANDLE BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE LT MLG DOOR MALFUNCTIONED G UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15517MC 23300 DUE TO GEAR DOOR OPEN INDICATION: AFTER GEAR RETRACTION, RED DOOR OPEN LIGHT REMAINED ILLUMINATED. RAN SECTION 3 PROCEDURES, LT WING GEAR DOOR OPEN LIGHT ILLUMINATES WITH PRIMARY AND ALTERNATE DOOR SELECTION SWITCHES. DOOR IS OPEN WITH AIRCRAFT RUMBLE. UP ON INSPECTION OF LT WING GEAR DOOR, FOUND LT DOOR RELEASE HANDLE NOT FULLY ENGAGED IN THE UP AND CLOSED POSITION. POSITIONED DOOR HANDLE PROPERLY, LT WING DOOR CLOSED, CYCLED HANDLE 3 TIMES. DOOR OPERATION CHECK NORMAL IAW MM. NOTE: NO FUEL DUMPED. 2L74 4F4 F A20WE E23EA 20040914001992004091400199EU 2004 9 14 SDR2004045 120040626A3297D23198000 WIRE HARNESS AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT MLG DAMAGED A TRBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO21425MJ 425 LANDING GEAR WOULD NOT RETRACT AFTER TAKE0FF. AIRCRAFT RETURN TO THE AIRPORT. REPLACED RT MLG INTERMEDIATE HARNESS. 2H72 4T4 TRTA53EU E20NE 20040914002002004091400200EU 2004 9 14 SDR2004044 120040624A2121EVTA1925B FAN AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE AIR DIST SYSTEM FAILED A TRBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO21545AT856 545 WHEN NR 2 BLEED IS SELECTED A STRONG ODOR NOTED THROUGHOUT THE AIRCRAFT FOLLOWED BY AN ELECTRICAL SMOKE WARNING INDICATION. REPLACED AVIONICS AIR EXTRACTION FAN. 2H72 4T4 TRTA53EU E20NE 20040915000012004091500001CE 2004 9 15 ACE0910204 120040910A28221143890424 PUMP BEECH 1900 1900C 1154161CE FUEL BOOST RUPTURED E YADAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 AL03112AX 929 UC45 PILOT REPORTED FUEL LEAKING FROM LT ENGINE OB LOWER DRAIN. REPLACED LOW PSI FUEL PUMP DUE FAILED PRESSURE RELIEF DIAPHRAGM. 2L72 4T RTA24CE 20040915000032004091500003 2004 9 15 DHL2004752009 420040909A34142083081 INDICATOR BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE COCKPIT FAILED A DHLAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO01752DH 22466 F/O'S A/S INDICATOR FAILED ON T/O ROLE AT 80KIAS INDICATED 60 KIAS AT 165,000, LBS 18 DEGREES C, PA 830 IN NORMAL BRAKE ENERGY ZONE NOTE: 0 KIAS INDICATION IS THE SAME AS 60 KIAS THERE WAS NO A/S INDICATION IE NEEDLE MOVEMENT ON THE CO-PILOTS SIDE A/S FAILED FLAG WAS IN VIEW. R2 MACH AIRSPEED IND. IAW 34-12-01, PERFORMED PITOT STATIC CHECK IAW 34-12-01, OP + LK CK GOOD ALL TAPE AND HOSES REMOVED. 2L73 4F4 F A3WE E2EA 20040915000042004091500004SO 2004 9 15 C2XA04IA115 120040902A2844MS2915204 O-RING SUNDSTRANDEM EMB 135 EMB135LR 3260305SO PWA JT8 JT8D219 52053NE FUEL SOLENOID LEAKING A C2XAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2728518 145334 THE CREW REPORTED A FUEL SMELL IN THE CABIN WITH THE APU RUNNING. EWR MX INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 28-45-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2388, WHERE MAINTENANCE REMOVED AND REPLACED THE APU FUEL PRESSURE SWITCH O-RING, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATE9NE 20040915000052004091500005EU 2004 9 15 AWXA200400989 120040909A3350321430 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28639AW 471 8-DAY CHECK - DURING FUNCTIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM THE RT OVER WING EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE RT EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20040913000472004091300047CE 2004 9 13 2004F00306 120040701A8011400SG138Q STARTER LEAR 60 60LEAR 5170707CE NR 2 ENGINE INOPERATIVE A DELAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE03188TG 078 DURING NORMAL ENGINE START SEQUENCE, THE NR 2 ENGINE DID NOT ROTATE. CREW REPORTED BURNED ELECTRICAL SMELL AT NR 2 NACELLE. NR 2 STARTER WAS REPLACED WITH OVERHAULED UNIT AND START ACCOMPLISHED WITHOUT FAULT. THE FAILED UNIT WAS ORIGINALLY INSTALLED IN AN OVERHAULED CONDITION AND HAD ACCUMMULATED 5.7 HOURS AND 6 STARTS. (M) 2L72 4F RTA10CE 20040913001562004091300156CE 2004 9 13 63269 120040721A5610 SEAL BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA WINDOW BLOWN A AMWAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 CE07162ZV UE162 WHILE AIRCRAFT WAS ENROUTE, FO'S STORM WINDOW SEAL BLEW OUT CAUSING AIRCRAFT TO DEPRESSURIZE. CREW DESENDED TO UNDER 10,000 AND CONTINUED WITH NO FURTHER INCIDENT. RESECURED BOTTOM OF SEAL ON FO'S STORM WINDOW 2L72 4T3 TRTA24CE E2NE 20040913001602004091300160WP 2004 9 13 DHL2004804518 120040710A57545769859163 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT IB STUB WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR.2095: LT IB STUB WING ZEE PAN FITTING CRACK 4.000, STA XILD 43.188. REMOVED AND REPLACED CRACKED ZEE PAN FITTING, STA XILD 43.188 (LT IB STUB WING) IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1. 2L74 4F4 FRT4A25 E2GL 20040913001622004091300162SO 2004 9 13 LR7A04080 120040716A5320LS4112 WEB LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5324 FOUND RT MLG WHEEL WELL INTERCOASTAL BEAM OUTER CAP AND WEB CRACKED AT FS 493, RBL 68, WL 200. CAP AND WEB REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2210. 2H74 4T4 T A1SO E282 20040913001642004091300164SO 2004 9 13 LR7A04082 120040716A5321330511110 FLOOR PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE WARPED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5211 FOUND RAMP DOOR FS 762 - 857, RBL 40, RT FLOOR PANEL WARPED. FLOOR PANEL REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2231. 2H74 4T4 T A1SO E282 20040913001662004091300166SO 2004 9 13 LR7A04084 120040716A5312 BULKHEAD LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND RBL 61 BULKHEAD WEB CRACKED AT FS 614 - 617, WL260. REPLACED WEB AT FS 577 - 617, WL 252 - 270 IAW SMP583 CHP51-60 AND 51-70 AND LAC MEA 382-53-04-053. DRC 2245. 2H74 4T4 T A1SO E282 20040913001682004091300168NM 2004 9 13 ANCF200400022 120040727A2751 WARNING LIGHT DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE TE FLAPS ILLUMINATED W ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23583AN 53183 DURING TAKE OFF ROLL PASSING 80 KNOTS, FLAPS TAKE OFF WARNING CAME ON AND REJECTED TAKE OFF WAS PERFORMED ( FLAPS WERE SELECTED AL 11 DEGREE TAKE OFF, FLAPS TAKE OFF SELECTOR IN STOW POSITION AND FLAP READ OUT WERE 11 DEGREES). INSPECTION CHECK WAS PERFORMED BY HIGH ENERGY STOP IAW AMM 05-57-00 PAGE 601 FOUND IN NORMAL CONDITIONS. ROLLER NO CENTER WAS FOUND NO CENTERED IAW AMM 27-57-01 PAGE 203 ITEM B CHAPTER 7. THE PUSH ROD (A) WAS ADJUSTED WITH SATISFACTORY RESULTS. 2L72 4F4 FRT E9NE 20040913001692004091300169GL 2004 9 13 P5CA0401115 220040709A7310 DRAIN MAST BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 3 ENGINE LEAKING A P5CAE ENGINE SHUTDOWN K FLUID LOSS ININSP/MAINT 1 WP23452PA 30810 706221 AFTER ENGINE START, NR 3 ENGINE LEAKING FUEL, RETURNED TO THE GATE. FOUND FUEL LEAKING FROM DRAIN MAST, AFTER ENGINE START. SUSPECTED LEAK FROM STRUT DRAIN, DISCONNECTED DRAIN PIPE, WET SPAN ENGINE AT IDLE, STILL NO LEAKS EVIDENT, ENGINE COWL SECURED, OK FOR SERVICE. 2L74 4F4 FRTA20WE E23EA 20040913001702004091300170NM 2004 9 13 P5CA0401116 120040709A3610 VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 1 ENGINE MALFUNCTIONED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23505MC 21251 517343 ON ENGINE START-UP NR 1 ENGINE PYLON VALVE WILL NOT OPEN DURING MANUAL ENGINE START. REPOSITIONED PYLON VALVE IN ORDER TO ACHIEVE ENGINE START, OPS CHECK GOOD IAW MM 36-11-04. 2L74 4F4 FRTA20WE E23EA 20040913001722004091300172SW 2004 9 13 ALGA095990 120040707A6230412040104103 NUT BELL 412 412 1182202SW MAST CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XATAM A459 33169 FOUND CORROSION PITTING ON MAST NUT. REPLACED WITH NEW PART. 1G72 4U H4SW 20040913001732004091300173SW 2004 9 13 ALGA095992 120040707A6230412040101127 MAST BELL 412 412 1182202SW MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XATAM733 33169 FOUND CORROSION PITTING ON MAST. REPLACED WITH NEW PART. 1G72 4U H4SW 20040913001742004091300174SW 2004 9 13 ALGA095993 120040707A6230412040104103 NUT BELL 412 412 1182202SW MAST CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PTHUV7137 A130 33184 FOUND CORROSION PITTING ON MAST NUT. REPLACED WITH NEW PART. 1G72 4U H4SW 20040913001752004091300175SW 2004 9 13 ALGA095994 120040707A6230412040101117 MAST BELL 412 412 1182202SW MAIN ROTOR CORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03PTHUV7137 33184 FOUND CORROSION PITTING ON MAST. REPLACED WITH NEW PART. 1G72 4U H4SW 20040913001762004091300176SW 2004 9 13 HEEA096017 120040625A5620205032669277 WINDOW BELL 412 412 1182202SW PAX CABIN DEPARTED E HEEAO OTHER D INFLIGHT SEPARATION APAPPROACH 1 SW03108X 33115 DURING APPROACH TO LAND, A PASSENGER LEANED AGAINST THE WINDOW ON THE RT SIDE SLIDING DOOR AND THE WINDOW RELEASED AND WAS LOST. AIRCRAFT LANDED WITH NO FURTHER OR OTHER DAMAGE AND NO INJURIES. 1G72 4U H4SW 20040913001772004091300177CE 2004 9 13 GUU2004F00026 120040711A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ENGINE BROKEN A GUUAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO1747542 UE198 AFTER TAKEOFF, FIRE LOOP ENUNCIATOR AND RT T-HANDLE ILLUMINATED. THE RT ENGINE WAS SHUT DOWN AND THE FIRE EXTINGUISHER WAS FIRED. DECLARED AN EMERGENCY RETURN TO FLL. INSPECTED RT ENGINE. NO EVIDENCE OF FIRE OR FLUID LEAKS FOUND. FORWARD FIRE LOOP BROKEN AT FIREWALL CONNECTOR. REMOVED AND REPLACED FORWARD FIRE LOOP. REMOVED AND REPLACED RT ENGINE FIRE EXTINGUISHER BOTTLE. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040913001792004091300179NM 2004 9 13 ANCF200400026 120040807A2780 SLAT BOEING757 75728A 1384976NM RROYCERB211 RB211* 54555NE NR 10 OUT OF ADJUST W ANCFB EMER. DESCENT J WARNING INDICATION LDLANDING 1 SO23517NA 24260 EICAS MESSAGE LT SLAT DISAGREE DISPLAYED. WITH THE FLAP LEVER IN 1 BOTH FLAP POINTERS INDICATE .5. LT SLAT DISAGREE CHECK LIST ACCOMPLISHED AND MESSAGE REMAINED ON AFTER PROCEDURE COMPLETED. PERFORMED FIM PROCEDURE 27-81-00 PAGE 116 BLOCKS 1 AND 27 AND ADJUSTED SLAT NR 10 IAW AMM 27-81-00 PAGE 501. FESU BITE PROCEDURE WAS ACCOMPLISHED IAW FIM 27-51-00 FIGURE 104 SHEET 1 BLOCKS 1 AND 2 SHEET 2 BLOCKS 3, 4 AND 5. TEST COMPLETED OK. 2L72 4F4 FRTA2NM A12EU 20040913001812004091300181EU 2004 9 13 U30A200400009 120040726A2560PL22412LH055 GLOWSTRIP AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE SEAT ROW 2-5 DEFCRACKED A U30AK NONE O OTHER ININSP/MAINT 1 EA17262AV 1725 AFTER FLT 609, RSW-ORD, DURING MAINTENANCE, THE EMERGENCY FLOOR PATHWAY LIGHTING PHOTO LUMINESCENT STRIP BETWEEN SEAT ROWS 2 DEF AND 5 DEF WAS IDENTIFIED AS DAMAGED. MAINTENANCE REPLACED THE PHOTO LUMINESCENT STRIP BETWEEN ROWS 2 DEF AND 5 DEF IAW AMM 33-51-21-401 AND OPS CK OK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E2GL 20040913001822004091300182CE 2004 9 13 GLBA20030646 120040620A2121 ODOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA COCKPIT DETECTED A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03211GL UE211 SMELL OF ELECTRICAL SMOKE IN COCKPIT, INSPECTED A/C SYSTEMS, FOUND NO DEFECTS. 2L72 4T3 TRTA24CE E2NE 20040913001842004091300184WP 2004 9 13 ASMF200408013 120040814A2842050014001 COMPENSATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT SIDE FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23505MD14033 49149 CAPTAIN REPORTED DIFFERENCE BETWEEN LT AND RT FUEL INDICATORS. DURING COMPENSATORS TEST WAS DETECTED THAT THE RIGHT TANK HAD 2500 LBS, LT TANK HAD 2600 LBS AND CENTRAL TANK HAD 3000 LBS. FUEL WAS TRANSFERRED FORM PRINCIPAL TANKS TO CENTRAL TANK AND BOTH TANKS COMPENSATORS WERE REPLACED IAW 28-40-03, TESTS WERE CORRECT. 2L72 4F4 F A6WE E9NE 20040913002132004091300213NM 2004 9 13 DHL2004745531 120040716A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSELAGE SKIN PREVIOUS REPAIR HAS SKIN PILLOWING AT BS 1130-1144 ABOVE STR 26L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 53-30-1 FIG 1. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA 12.1250 INCHES X 8.1250 INCHES AND FABBED STRUCTURAL FILLER FROM 2024 T3 .063 PO NR 900920 DIM 22.2500 INCHES X 6.5 INCHES AND DOUBLER FROM 2024 T3 .071 PO NR 900781 DIM 20.2500 INCHES X 14.5 INCHES, PARTS TREATED, PRIMED AND INSTALLED SRM 53-30-3 FIG 5 & 51-10-2. REPAIR IS CATEGORY B. 2L73 4F4 F A3WE E2EA 20040913002152004091300215NE 2004 9 13 2004UALA00773 220040816A7261 PUMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 ENGINE FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29128UA 30023 NR 2 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE PROBLEM. FOUND FAILURE OF THE OIL PUMP IDLER GEAR BEARING SET DUE TO VIBRATIONS AND WEAR OF THE BEARING SET, THE BEARINGS FAIL AND STOP THE DRIVE TO THE OIL PUMP, CAUSING THE OIL PRESSURE TO DROP. THE BEARING SET IS AN OLD CONFIGURATION AND COA G-9621-0 WILL UPGRADE THE CONFIGURATION TO THE IMPROVED DESIGN. 2L74 4F4 FRTA20WE E24NE 20040913002182004091300218NM 2004 9 13 DHL2004745513 120040704A5730 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LEADING EDGE SKIN AT CUTOUT FOR NR 6 SLAT HAS BROKEN FASTENERS AND SHARP EDGES RW5-525. REMOVED NR 6 L/E SLAT IAW MM 27-81-11. REMOVED DAMAGED FASTENERS IAW SRM 51-30-2 REMOVED SHARP EDGES AT NR 6 SLAT CUTOUT IB TRACK IAW SRM 57-20-1. L/E FOUND TO BE CRACKED, STOP DRILLED IAW SRM 51-10-1, 57-30-4. NDT STOP DRILL IAW B727 NDT MM CH 51-00-00 DT6 FIG 23 NO DEFECTS NOTED. FABRICATED REPAIR PLATE 9 INCHES X 8 INCHES FROM 2024 T3 .063 PO NR 900920 IAW SRM 57-30-4 FIG 11. PARTS INSTALLED IAW SRM 57-30-4 FIG 11. INSTALLED NR 6 L/E SLAT AND OP CHECK IAW MM 27-81-11, 27-81-00. 2L73 4F4 F A3WE E2EA 20040914000162004091400016NM 2004 9 14 DHL2004745021 120040908A2612 FIRE LOOP BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE SHORTED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01745DH 20665 ENGINE NR3 FIRE PROTECTION SYSTEM DETECTOR CIRCUIT GRD LIGHT ON AT P63 PANEL ILLUMINATED DURING FLIGHT. LIGHT EXTINQUISED DURING DESCENT. FOUND LOOP TOUCHING COWLING. ADJUSTED LOOP TO MISS COWLING IAW MM 26-11-00 OPS CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040914000292004091400029EU 2004 9 14 MALA040556 120040813A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15363PX 340B260 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN 61-0478-9, SN/0202641 FAILED. MAINTENANCE REPLACED CELL PACK PN 55-2198-1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 8/18/04. REFER TO WO NR 373761 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20040914000312004091400031EU 2004 9 14 MALA040546 120040830A3350 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHTSINOPERATIVE A MALAK NONE L NO TEST NRNOT REPORTED 1 GL15410XJ 340B410 EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY 21LN, 23LN INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY 21LN AND 23LN. REFER TO 409 NR 222887, AND 222888 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20040914000442004091400044CE 2004 9 14 2004F00338 120040901A760366001592 CONTROL CABLE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE THROTTLE BROKEN E BKAAO OTHER R PARTIAL RPM/PWR LOSS APAPPROACH 1 SO1382TS 154 THROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891) 2L72 4J4 J A10CE 1E16 20040914000462004091400046NM 2004 9 14 DXTA200400372 120040826A3150 WARNING HORN AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE CONFIGURATION ACTIVATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07277QS 177 DURING T/O ROLL WITH POWER LEVERS IN T/O FOR APPROXIMATLEY 10-15 SECONDS AND AT APPROXIMATELY 40KNTS (NO TAKE OFF) CONFIG WARNING ACTIVATED REASON FOR WARNING CANNOT BE DETERMINED, CONFIGURATION WAS NORMAL FOR ALL SYSTEMS.- ITEM IS UNDER INVESTIGATION. 2K73 4F4 FRTA50NM E44NE 20040914000482004091400048NM 2004 9 14 375PA0023 120040826A335020131A BATTERY PACK BOEING737 7373Y0 1384671NM GE CFM56 CFM563B1 13802NE EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05375PA 23812 EMERGENCY FLOOR PATH LIGHTING FROM ROW 15 TO 21 IS INOPERATIVE. REPLACED BATTERY PACK AT STA 753 IAW MM 33-51-00. OPS CHECKS NORMAL. 2L72 4F4 FRTA16WE E2GL 20040914000532004091400053WP 2004 9 14 DHL2004804509 120040702A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR. 1071: EXTERNAL FUSELAGE PLATING WITH CRACKS 0.250, 0.750 AT STA. FS 1742.000, FS 1747.000, L-15L TO L-17L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG.7. REMOVED RIVETS IAW SRM 51-1-21 PG.1. TRIMMED OUT IAW SRM 53-2-1 PG.107-108 FIG.7. (SHEET 5 AND 3). CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FINGER DOUBLER (AL 7075-T6 0.040) FILLERS (AL 7075-T6 0.063) DOUBLER (AL 7075-T6 0.071) IAW SRM 53-2-01 PG. 99-100 FIG.7 SHEET 1. CLEANED, TREATED AND PRIMED FINGER DOUBLER, FILLERS AND DOUBLER IAW SRM 51-1-8B. INSTALLED CONICAL SPACER IAW SRM 51-1-26. INSTALLED FINGER DOUBLER, FILLERS AND DOUBLER IAW SRM 53-2-1 PG. 99-100 FIG.7 SHEET 1, SRM 51-1-21 PG.1, SRM 51-1-15 PG.1. 2L74 4F4 FRT4A25 E2GL 20040914000732004091400073 2004 9 14 RAIA00408025 420040824A3425HG2010AC02 AHRS EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK2783 145044 F/O ATTITUDE HEADING ERROR. MAINTENANCE REMOVED AND REPLACED AHRS. 2L72 4T4 FRTT00011ATTE6CH 20040914000822004091400082NM 2004 9 14 UIEA200400120 120040707A21317773961 CONTROLLER BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE CABIN PRESSURE FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15808MC 21048 GT 8237/03 RMS/DOV AUTO FAIL LIGHT CAME ON DURING FLIGHT: AUTO FAIL LIGHT CAME ON DURING CLIMB ABOUT 8000 FT A/C ALTITUDE OUTFLOW VALVES .2500 CLOSED USED MANUAL IAW ABNORMAL CHECK LIST TO CONTROL DIFFERENTIAL PRESSURE AT 4 PSID CONTINUED FLIGHT. GOING THROUGH FL 220 DIFFERENTIAL PRESSURE WENT TO 9.5 PSID, RATE OF CLIMB MAX OUT, BOTH PRESSURE RELIEF LIGHTS CAME ON, CABIN ALTITUDE WAS GOING THROUGH 10,000 FT. CABIN ALTITUDE MAX OUT AT 14,500 FT DESCENDED AIRCRAFT TO 10,000 FT. ALL INDICATION CAME BACK TO NORMAL. USED MANUAL CONTROL TO 4 PSID, AND DIVERTED. COMPLETED PRESSURIZATION CHECK IAW MM. UNABLE TO DUPLICATE PROBLEMS. AS PRECAUTION, CHANGED CABIN PRESSURE CONTROLLER, AND PRESSURIZED AC TO MM REF. 2L74 4F4 F A20WE E23EA 20040914001002004091400100NM 2004 9 14 UPS04243015 120040707A5310 WINDOW FRAME BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, REPLACE LT WINDOW FRAME AT BS 1100 P/N:65-19850-149. FRAME REPLACED WITH NEW FRAME IAW SRM 51-30-2. 2L73 4F4 F A3WE E25NE 20040914001062004091400106EU 2004 9 14 TCA001 120040624A7931113465AA PRESSURE SWITCH AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE OIL PRESSURE MALFUNCTIONED E E18AE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL25764LA 211 304572 LOST OIL PRESSURE IN FLIGHT, SHUT DOWN ENGINE, RESTART, OIL PRESSURE CAME BACK BUT LIGHT STAYED ON.REMOVED AND REPLACED OIL PRESSURE TRANSMITTER, CONDUCTED ENGINE RUN, ENSURED LIGHT EXTINGUISHED AND PROPER OIL PRESSURE INDICATION. OPS, LEAK CHECK GOOD. 2L72 4F4 F A7EU E7EA 20040914001082004091400108WP 2004 9 14 MV1R04231 120040616A3260KMXN2A SWITCH CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL LT MLG INTERMITTENT I MV1RO OTHER O OTHER NRNOT REPORTED 1 EA1739 6997 480 LT MLG DOWN AND LOCKED LIGHT INTERMITTENT. PERFORMED GEAR SWING AND PROBLEM VERIFIED. LT MAIN GEAR SWITCH INTERNAL WIRING LOOSE AT MOUNTING LUGS. INSTALLED NEW LOCK WASHERS AND RE TORQUED. RETRACTION CHECKS NORMAL IAW MM. 2L72 4R4 T 6A6 E282 20040914001122004091400112CE 2004 9 14 400AC0401 120040610A1430 BOLT BEECH 100 B100 1152919CE GARRTTTPE331TPE3315 01514WP LT TORQUE LINK FAILED I EGQAO OTHER O OTHER NRNOT REPORTED 1 EA17400AC BE12 PILOT REPORTED VIBRATION ON LANDING. INSP REVEALED THE LT MAIN GEAR TORQUE LINK PIVOT BOLT, MISSING. THE BOLT COULD NOT BE FOUND TO DETERMINE THE CAUSE. SUSPECT EITHER A FAILURE OF THE BOLT OR FAILURE OF THE SAFETY FEATURE TO PREVENT THE BOLT FALLING OUT. THE TORQUE LINK WAS REPLACED WITH NEW PARTS WITH NEW BOLT AND BUSHINGS. TIRES WERE REPLACED AS A PRECAUTION TO PRECLUDE UNKNOWN DAMAGE TO LINES THAT MIGHT CAUSE A FUTURE FAILURE. 1L72 4T4 T A14CE E4WE 20040914001192004091400119CE 2004 9 14 8343720 120040612A2797 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RUDDER YAW DAMP BROKEN A JJBAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 EA01834CA4376 UE378 YAW DAMP RUDDER BOOST, ENGAGED ON ITS OWN. REPAIRED WIRE AT NR W13 AT PIN A ON LT ENGINE P5 CONNECTOR AND REPLACED YR5-65 SENSOR. 2L72 4T3 TRTA24CE E2NE 20040914001252004091400125GL 2004 9 14 YNO2004F00001 120040610A5610GC33100014 WINDSHIELD BOMBDRBD700 BD7001A10 1390006GL RROYCEBR700 BR700710A110 NE COCKPIT CRACKED E YNOAO OTHER O OTHER NRNOT REPORTED 1 EA11917R 9008 12127 AC WAS ENROUTE, ON A 91 LEG, PILOTS NOTICED THE RT WINDSHIELD OUTER LAYER CRACKED. THE AC DIVERTED AND LANDED WITH NO PROBLEM. MFG SERVICE CENTER REPLACED THE WINDSHIELD AND AIRCRAFT IS RETURNED TO SERVICE. 2L72 4F4 FRTT00003NYE00057EN 20040914001282004091400128WP 2004 9 14 ASMF200407029 120040724A7540 WARNING LIGHT DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE ILLUMINATED W ASMFD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 SW23803ML 49726 728169 AIRCRAFT RETURNED TO PLATFORM, LT ENGINE WITH LOW POWER AND IN IDLE POSITION TEMPERATURE REACHED 485 DEGREE (C) OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THRUST LEVER TRIM WAS CHECKED IAW MM 76-11-00, LT ENGINE BLEED VALVES WERE LUBRICATED IAW MM 75-30-00, THERMOCOUPLE NR 4 WAS REPLACED IAW MM 77-21-03 AND TRIMMING WAS PERFORMED IN BOTH ENGINES IAW MM 71-00-01, TESTS CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001342004091400134CE 2004 9 14 8324875 120040628A33104520020 SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA PANEL LIGHTS BURNED A JJBAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA01832CA6107 UE406 OVERHEAD/SIDE PANEL LIGHTS WENT OUT, FOLLOWED BY SMOKE FROM CAPTAINS SIDE PANEL. 2L72 4T3 TRTA24CE E4EA 20040914001442004091400144EA 2004 9 14 SWIA200413598 120040719A3350 BULB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07909SW AFT CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB FOR AFT CEILING EMERGENCY LIGHT CRJ AMM 33-51-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040914001492004091400149CE 2004 9 14 YNO2004F00002 120040412A326065430087 UPLOCK SWITCH CESSNA500 S550 2076607CE PWA JT15 JT15D1 52060NE RT MLG INOPERATIVE E YNOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA1162NS 3330 S5500072 ON APRIL 12, 2004 AT APPROX 10:30 AM, AIRCRAFT WAS DEPARTING WHEN GEAR WAS SELECTED UP, THE RT MAIN GEAR WOULD NOT COME UP AND LOCK. THE PILOTS COMPLETED THE CHECKLIST, THE GEAR WAS SELECTED DOWN AND HAD AN ALL GEAR SAFE CONDITION. THE AIRCRAFT DIVERTED AND LANDED WITH NO PROBLEM. THE AIRCRAFT WAS FERRIED, FOR TROUBLESHOOTING AND REPAIRS. THE RT MAIN GEAR UPLOCK SWITCH WAS REPLACED WITH NEW, OPS TESTED AND AIRCRAFT RETURNED TO SERVICE. 1L72 4F4 FRTA22CE E1NE 20040914001512004091400151 2004 9 14 USA2004F00085 420040620A2565D30665109 SLIDE AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE PAX DOOR UNSERVICEABLE A USAAK NONE O OTHER ININSP/MAINT 1 EA19119US124084108 1268 THE RT SIDE REAR SERVICE DOOR HAS A SLIDE PACK STRAP EXTENDING OUT OF THE DOOR. MAINTENANCE REPLACED THE RT SIDE REAR SERVICE DOOR SLIDE ASSY. OK FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20040914001672004091400167EA 2004 9 14 A6WA200440074 120040608A3234 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE MLG SELECTOR FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31419AW 7633 LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. PARKING BRAKE SHUT-OFF VALVE MESSAGE AND ANTI-SKID IB MESSAGE. COMPLIED WITH QRH, RETURNED TO COS WITH UNEVENTFUL LANDING. REMOVED AND REPLACED GEAR SELECTOR HANDLE IAW MM FUNCTION AND OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040914001872004091400187NE 2004 9 14 KBM2004F00189 220040516A72619560137250 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MAGNETIC SEAL LEAKING E KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19884SH 2884 MO5 OUTPUT SHAFT MAGNETIC SEAL IS LEAKING. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040915000022004091500002NM 2004 9 15 ANCF200400030 120040909A2410 CSD DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT GENERATOR OVERSERVICED W ANCFO OTHER WMJINADEQUATE Q C OVER TEMP WARNING INDICATION CLCLIMB 1 SO23632CT 49632 RT CSD OIL TEMPERATURE REACHED THE RED ZONE. ABNORMAL PROCEDURE WAS ACCOMPLISHED SWITCHING RT GENERATOR OFF, RT CSD OIL TEMPERATURE STARTED TO COOL DOWN. THE OIL LEVEL WAS FOUND OVERFILL, IT WAS DRAINED AND PERFORMED FLUSHING CHECK POP OUTS MAGNETIC CHIP DETECTORS AND CHECK TEMPERATURE SENSOR IAW AMM 24-10-01 PAGE BLOCK 401 AND A83-24-891-R3. RUN UP IAW AMM 71-00-00. 2L72 4F4 FRT E9NE 20040915000062004091500006NM 2004 9 15 AWXA200400990 120040905A5321D5367175900300 FLOOR PANEL AIRBUSA319 A319132 3930340NM PWA 120 PW120A NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK A .5 INCH CRACK WAS FOUND IN AFT GALLEY FLOOR PANEL 262 EF. MAINTENANCE PERFORMED BOND REPAIR OF CRACKED FLOOR PANEL 262 EF IAW A319 SRM 53-02-00, FIG. 201, PG. 203-204, AND 206. 2L72 4F4 TRTA28NM E20NE 20040915000082004091500008NM 2004 9 15 AWXA200400992 120040902A53306545749 SKIN BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 DURING 4-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 23 LT, APPROXIMATELY 18 INCH AFT OF EXTERIOR EMERGENCY EXIT LIGHT. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACK EXISTS. REMOVED EXISTING REPAIR DOUBLER BETWEEN BS 727D AND BS 727E EXPOSING TWO PREVIOUS CUTOUTS IN SKIN; ONE 3 INCH FORWARD OF EMERGENCY EXIT LIGHT, AND ONE 6 INCH AFT OF EMERGENCY EXIT LIGHT. FABRICATED A REPAIR DOUBLER THAT WILL COVER ALL THREE CUTOUTS; INSTALLED REPAIR PART IAW AWA E.R. 03-5331-0427-HF1. 2L72 4F RTA16WE 20040915000092004091500009NM 2004 9 15 UPS04243062 120040817A5753 SKIN BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU LT OB MIDFLAP DEBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5 2L73 4F4 F A3WE E25NE 20040915000112004091500011NM 2004 9 15 UPS04243064 120040812A5330 SKIN BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 C-CRACKS ON CENTER POST OF COCKPIT WINDOWS, NR 1 LT AND NR 1 RT, LOWER IB CORNERS. HFEC CARRIED OUT AND CRACKS CONFIRMED. CRACKED SKIN REPLACED IAW AAAE EO 2004-077-004 AND UPS FILE NR 727-53-20157. 2L73 4F4 F A3WE E25NE 20040915000122004091500012NM 2004 9 15 UPS04243066 120040823A3350 LIGHT BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU COCKPIT DEFECTIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C-COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH ON P5 PANEL TO ON. LIGHT ASSEMBLY FOUND DEFECTIVE IAW WDM 33-51-01. LIGHT ASSY REPLACED IAW MM 33-50-01. FUNCTION CHECKED OK. 2L73 4F4 F A3WE E25NE 20040915000132004091500013NM 2004 9 15 UPS04243067 120040826A5320 ATTACH ANGLE BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, DURING INSPECTION OF SKIN REPAIR, AT 1334 LT SIDE AFT AIRSTAIRS, SKIN ATTACH ANGLE FOUND CORRODED. REPLACED ATTACH ANGLE IAW SRM 51-10-01. 2L73 4F4 F A3WE E25NE 20040915000162004091500016NM 2004 9 15 UPS04243072 120040906A3350 BATTERY BOEING727 72725C 138400HNM RROYCETAY TAY65154 EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01937UP 19302 INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT COME ON WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED BATTERY IN EACH EMERGENCY EXIT LIGHT. OPS CK GOOD REF MM 33-50-01. 2L73 4F4 F A3WE E25NE 20040915000172004091500017NM 2004 9 15 UPS04243076 120040813A5330 SKIN BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 217 STR 25L. AREA PAINT STRIPPED IAW MM 51-20-15. TRIMMED CORRODED AREA IAW SRM 53-30-03 AND REPAIRED AREA IAW SRM 53-30-3 FIG. 3. 2L73 4F4 F A3WE E25NE 20040915000182004091500018NM 2004 9 15 UPS04243077 120040822A5330 DOUBLER BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, CRACK ON DOUBLER RT SIDE BS 1444 APPROX. CRACK CUT OUT IAW SRM 51-40-02. HFEC CARRIED OUT IAW NDT MANUAL 51- 00-00 PT 6 FIG 4. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02. 2L73 4F4 F A3WE E25NE 20040915000212004091500021 2004 9 15 64407 420040830A3418 WARNING HORN BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE STALL WARNING ACTIVATED A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07142ZV UE142 DURING TAKEOFF ROLL STALL WARNING HORN STARTED SOUNDING. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. JACKED AC, CYCLED GEAR 5 TIMES CND ON GND. 2L72 4T4 TRTA24CE E26NE 20040915000232004091500023NM 2004 9 15 UPS04443046 120040818A534065B38600123 CLIP BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, BS 2040 LT FRAME ATT TIE CLIP FOUND CRACKED AT STR 24. M/D BS 2040 LT FRAME ATTACH CRACKED TIE CLIP AT STR 24 REPLACED IAW SRM 51-10-01 P8. 2L74 4F4 FRTA20WE E3NE 20040915000242004091500024EA 2004 9 15 QXEA200400648 120040828A5610601R3303318 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COCKPIT FAILED A QXEAA UNSCHED LANDING O OTHER CRCRUISE 1 NM09617QX1891 10130 THE FLIGHT DIVERTED WHEN THE CREW HEARD A LOUD BANG AND NOTICED THE FIRST OFFICERS WINDSHIELD HAD SHATTERED. MAINTENANCE INSPECTED THE A/C AND REPLACED THE RT WINDSHIELD. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040915000252004091500025EA 2004 9 15 SWIA200413759 120040826A4920 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07440SW 7589 FOLLOWING APU START, RECEIVED A (CARGO SMOKE) WARNING AND AURAL MESSAGE MOMENATARILY. INSPECTED APU ASSEMBLY AND DUCTING FOR LEAKS. STARTED APU SEVERAL TIMES WITH NO ANNOUNCED INDICATIONS, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040915000262004091500026NE 2004 9 15 J7B2004F00000 220040715A72503028601 BLADE CESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE ENGINE FAILED E J7BAO OTHER O OTHER NRNOT REPORTED 1 SW01409S 2156 5000238 PCE76509 HT BLADE FAILURE. 1L72 4F4 F A22CE E25EA 20040915000282004091500028EU 2004 9 15 DHL2004366003 120040718A29133508806 PUMP AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE HYD SYSTEM FAILED A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01366DH3776 3776 249 MLG WOULD NOT EXTEND ON LANDING. COMPLETE M/G EXT ABNORMAL PROCEDURE. LANDED WITH NO NOSEWHEEL STEERING. EXT TOOK 20 TURNS. WOULD NOT EXTEND DUE TO ITEM 1P. LOSS OF GREEN SYS HYD. RESTORED EXT/RET SYS TO NORMAL IAW MM. MANUAL HANDLE RETURNED TO NORMAL W/ 20 TURNS. MWP (HYD) AND GREEN TANK (LEVEL LO) LIGHT ILLUMINATED. QTY WAS AT BOTTOM OF YELLOW ARC. (HYD FLUID LOSS) ABNORMAL PROCEDURE COMPLETED. APPROX .5-1 GAL FLUID REMAIN. MWP (HYD) AND (PUMP PRESS LO) LIGHT ILLUMINATED. COMPLETED ABNORMAL PROCEDURE. NR 1 GREEN PUMP IS IN (DUMP) AND GREEN. ELEC PUMP(1)IS ON. REMOVED AND REPLACED O-RING ON GREEN SYS MANIFOLD IAW MM. REMOVED AND REPLACED NR 1 ENG DRIVEN PUMP IAW MM. OPS CK, LEAK CHECK GOOD. 2L72 4F4 FRTA35EU E23EA 20040915000292004091500029EA 2004 9 15 04253708 120040908A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27708BR 7575 STRONG FUEL ODOR ON ENGINE BLEEDS DURING CLIMB OUT. PERFORMED OPS CHECK OF PACKS SYSTEM IAW MM 21-51-00. COULD NOT DUPLICATE AT THIS TIME. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20040915000302004091500030NM 2004 9 15 BJNA040805 120040813A5320BAC150529222 FLOOR SUPPORT BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 LBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW THE SRM 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M) 2L72 4F4 FRTA16WE E2EA 20040915000312004091500031NM 2004 9 15 SWAA042560 120040901A5754 STIFFENER BOEING737 7377H4 1384404NM LT WING K FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29700GS 27835 DURING SCHEDULED HC2 CHECK, FOUND LEFT WING NR 1 L/E KRUGER FLAP OUTBOARD STIFFENER, CRACKED. REMOVED AND REPLACED FLAP PER MM. (M)SWAA 2L72 4F RTA16WE 20040915000332004091500033CE 2004 9 15 240041 120040826A3150 SOCKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE WARNING LIGHT LOOSE A NSVAK NONE P NO WARNING INDICATION ININSP/MAINT 1 EA27152MJ UE52 LT FIRE WALL FUEL VALVE AMP TEST FAILED TO ILLUMINATE. TEE HANDLE RETORQUED LT LIGHT BULB SOCKET. OPS CHECKED NORMAL. 2L72 4T4 TRTA24CE E26NE 20040915000352004091500035EU 2004 9 15 RAIA00408026 120040825A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE LEFT INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03552HK13043168 41057 5483-STL- LT GENERATOR WILL NOT COME ON LINE. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER GEN. 2L72 4T4 TRTA41NM E18NE 20040915000362004091500036SO 2004 9 15 RAIA00408029 120040825A3260852701 UPLOCK SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03813HK 14504 5696 -STL-BANDING NOISE COMING FROM NOSE BAY AREA AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED UP LOCK PROX SWITCH. 2L72 4T4 FRTT00011ATTE6CH 20040915000372004091500037NE 2004 9 15 RAIA00408027 220040825A741231058865 EXCITER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03561HK5883 41077 RT ENGINE WILL NOT LIGHT OFF. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IGNITION EXCITER. 2L72 4T4 TRTA41NM E18NE 20040915000422004091500042EA 2004 9 15 SWIA200413763 120040823A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07918SW 7645 ON APPROACH STAB TRIM CHANNEL 1 DISENGAGED. REMOVED AND REPLACED CAPTAINS STAB TRIM SWITCH AND STAB TRIM/MACH TRIM POND ASSY IAW MM 27-41-00 AND 27-41-25. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040915000432004091500043EU 2004 9 15 04FDEA02581 120040831A5320A2577181300600 PAN AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 REF. SNRM N00246 LWR FWD CARGO FR21 30 INCHES LT OF CENTER DATUM FLOOR CARGO ELECTRIC ROLLER PAN HAS CORROSION. REMOVED AND REPLACED WITH NEW ROLLER PAN IAW A310/200 SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040915000462004091500046EU 2004 9 15 04FDEA02584 120040831A5320R538D104820200 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 REF. SNRM N00257 MAIN DECK CARGO COMPT. AT FR 46 DUMMY TRACK IS CRACKED BETWEEN R1 AND R2 SEAT TRACKS. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040915000482004091500048NM 2004 9 15 UPS04443047 120040818A531069B031461 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, BS 1520 RT FRAME SHEAR TIE FOUND CRACKED AT STR 21. SHEAR TIE REPLACED IAW SRM 51-10-01 P8 AT M/D BS 1520 RT FRAME STR 21R. 2L74 4F4 FRTA20WE E3NE 20040915000492004091500049NM 2004 9 15 04FDEA02624 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING-OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000502004091500050NM 2004 9 15 04FDEA02625 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 SNRM N0453: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000532004091500053NM 2004 9 15 04FDEA02628 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 SNRM N0456: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000552004091500055NM 2004 9 15 04FDEA02630 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000572004091500057EA 2004 9 15 COMA0460496 120040901A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA 7306 INTERCOSTAL AT FS 484.00 BETWEEN RBL 27.00 AND RBL 36.00 HAS CRACKED OB LEG. REPAIRED IAW REO 601R-53-41-059. 2L72 4F4 FRTA21EA E15NE 20040915000602004091500060NM 2004 9 15 UPS04443026 120040821A5730 PLATE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE PLATE (BS 1241)FOUND CRACK AT HOLE NR 5 APPROX 0.060 INCH. RT WING REAR SPAR UPR SPLICE PLATE HOLE NR 5 CRACK FREE AT 1.00 INCH WAS REPAIRED IAW EO B747-5740-17032. 2L74 4F4 FRTA20WE E3NE 20040915000622004091500062NM 2004 9 15 UPS04443037 120040819A5347 SEAT TRACK BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C U/D- STA 545-560 RBL 28 SEAT TRACK IB FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 3 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. AND CIC APPLIED IAW EO NR M5100-2780-E. 2L74 4F4 FRTA20WE E3NE 20040915000632004091500063NM 2004 9 15 UPS04443038 120040817A534065B38600160 STRINGER CLIP BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, M/D- BS 2160 STR 2L, FRAME ATT. TIE CLIP FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 2 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED REF. SRM 51-10-01 P.8 , AND CIC APPLIED IAW EO NR M-5100-2780-E. 2L74 4F4 FRTA20WE E3NE 20040915000642004091500064NM 2004 9 15 UPS04443039 120040819A5347 SEAT TRACK BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D: BS 630-760 LBL 28 INCH SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.060 INCH X 1 INCH X 20 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS630 - BS650 LBL 28 INCH SEAT TRACK REPAIRED REF. SRM 53-10-05 FIG 1A. AND CIC APPLIED IAW EO NR M-5100-2780-E. 2L74 4F4 FRTA20WE E3NE 20040915000682004091500068NM 2004 9 15 UPS04443043 120040819A5347 SEAT TRACK BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D- STA 595-602 RBL 47 INCHES SEAT TRACK FOUND CRACK. U/D- STA 590- STA 650 RBL 47 INCHES SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A. 2L74 4F4 FRTA20WE E3NE 20040915000712004091500071NM 2004 9 15 UPS04443050 120040819A5313 STRINGER BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D STA 744-745 RT 2A STRINGER END FOUND CRACKED. U/D STA 744-745 RT STRINGER 2A REPAIRED IAW SRM 53-10-03 FIG.10 2L74 4F4 FRTA20WE E3NE 20040915000722004091500072NM 2004 9 15 2004F00340 120040628A326065178197 UPLOCK BOEING727 7272F9 138407DNM PWA JT8 JT8D17 52049NE LT MLG INOPERATIVE A PCSAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO17199AJ 21426 UPON GEAR EXTENSION IN GND LT GEAR WOULD NOT EXTEND. ACCOMPLISHED ABNORMAL OPERATION, GREEN GEAR LIGHTS, OUT AND RED DOORS LIGHT, GEAR LEVER DOWN AND MANUAL GEAR EXTENSION AT LT GEAR EXTENDED AT COMPLETION OF CHECK LIST. AC FERRY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT UPLOCK ACTUATOR IAW MM 32-32-61. ACCOMPLISHED LT MAIN LANDING GEAR WHEEL WELL DOOR RIGGING AND OPS CHECK NORMAL IAW MM 32-12-1. LUBRICATED LT MAIN LANDING GEAR SYSTEM IAW 12-21-01. ACCOMPLISHED OPS CHECK IAW MM 32-32-0. PERFORMED MANUAL EXTENSION IAW 32-24-0 PAGE 507 AND 508. OPS CHECK NORMAL. ACCOMPLISHED LT MLG UPLOCK ROTATION TORQUE CHECK IAW WORK CARD SP15, CHECKED OK. AC RETURNED TO SERVICE. (M) 2L73 4F4 FRTA3WE E2EA 20040915000732004091500073NM 2004 9 15 DHL2004748006 120040903A33501000679 LIGHT BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE L1 DOOR INOPERATIVE A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01748DH 22440 DURING PRE-DEPARTURE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT ASSY IAW MM 33-50-71/SYST, OPS CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20040915000742004091500074NM 2004 9 15 DHL2004762002 120040903A5210 LATCH BOEING727 7272B7 138407LNM PWA JT8 JT8D17 52049NE COCKPIT DOOR LACK OF LUBE A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01762AT 22162 COCKPIT ENTRY DOOR VERY DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. DOOR JAMS CLOSED AND KNOB WILL BARELY TURN. CLEANED AND LUBED COCKPIT ENTRY DOOR LATCH MECH. IAW MM 52-50-0. OPS CHECKS OK. 2L73 4F4 F A3WE E2EA 20040915000772004091500077EU 2004 9 15 AWXA200400971 120040815A5310D53472094002 BEAM AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y512 LT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y512 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 8. 2L72 4F4 FRTA28NM E311NE 20040915000852004091500085 2004 9 15 ASMF200407024 420040722A34142594466906 INDICATOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE AIRSPEED FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23169PL120497314 53175 CAPTAIN REPORTED THAT AT THE BEGINNING OF THE TAXI, APPEARED THE AIR SPEED A/S FLAG IN THE LT AIRSPEED INDICATOR. IT WAS PERFORMED A RESET AND THE CADC SWITCH WAS CHANGED OF POSITION, BUT THE TROUBLE CONTINUED. AIR SPEED INDICATOR WAS REPLACED AND SYSTEM TESTED IAW M/M 34-13-00, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040915000872004091500087EU 2004 9 15 JGV2004F00005 120040709A2820142G1243 VALVE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE73160 NE FUEL PURGE CRACKED B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE09128M 276 FUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPERATURE AT WELDING TIME. RECOMMEND NO SCREENS. 2L73 4F4 F A46EU E1NM 20040915000882004091500088 2004 9 15 MYW2004F00005 420040624A3461 FMC BOEING737 7378Q8 13844BXNM GE CFM56 CFM56* 13802NE COCKPIT FAILED A MYWAO OTHER G MULTIPLE FAILURE DEDESCENT 1 SO19734MA 30039 DURING DECENT INTO AIRPORT, AIRCRAFT EXPERIENCED DUAL FMC FAILURE. RECYCLED FMS CIRCUIT BREAKER. ACCOMPLISHED OPERATION TEST IAW MM. OPERATION NORMAL. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20040915000952004091500095 2004 9 15 ASMF200406024 420040621A3420HG280D80 ADC DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE COCKPIT FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23755RA5107 49727 DURING TRANSIT CHECK, CAPTAIN REPORTED FAST/SLOW FLAGS IN BOTH ADI´S AND DIFFERENCE OF 150 FEET BETWEEN ALTIMETERS. LT ADC WAS REPLACED IAW MM 34-16-01, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20040915001032004091500103NM 2004 9 15 ASMF200407006 120040703A27803920274525 CABLE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE SLAT CONTROL BROKEN W ASMFK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SW23160PL 49763 DURING OVERNIGHT SERVICE, SLAT NR 5 CONTROL CABLE WAS DETECTED BROKEN. CONTROL CABLE WAS REPLACED IAW MM 27-80-00, TEST CORRECT. DURING OVERNIGHT SERVICE, LT WING OPERATIONAL TEST OF SLAT NR 5 WAS PERFORMED IAW MM 27-80-00, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040915001042004091500104CE 2004 9 15 BWV2004F00000 120040604A8120 HOUSING BEECH 36 A36TC 1151603CE CONT O520 TSIO520* 17040SO TURBOCHARGER CRACKED B BWVRO OTHER O OTHER NRNOT REPORTED 1 CE0795HP 1702 YD026813 EA195 WHILE AIRCRAFT WAS UNDERGOING AN ANNUAL/PREBUY INSPECTION, IT WAS NOTED UPON EXAMINATION OF THE TURBOCHARGER OUTLET THAT A CRACK WAS FOUND RADIATING AROUND THE V-BAND CLAMP AREA. A SMALL AMOUNT OF MATERIAL REMAINED ATTACHING THE TAILPIPE TO TURBOCHARGER. LOSS OF THE TAILPIPE ASSEMBLY WOULD RESULT IN TURBOCHARGER EXHAUST GASES TO BE DIRECTED ONTO THE FIREWALL AND PENETRATION INTO THE CABIN AREA RESULTING IN A POSSIBLE UNCONTROLLABLE FIRE IN THE COCKPIT DIRECTLY AT THE PILOTS FEET WITH A POSSIBLE LOSS OF THE AIRCRAFT. (CE07200413597) 1L71 3O3 O 3A15 E8CE 20040915001052004091500105 2004 9 15 MYW2004F00007 420040607A3424S231A1205 DISPLAY BOEING737 7378Q8 13844BXNM GE CFM56 CFM56* 13802NE COCKPIT SHORTED A MYWAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19739MA 30670 DURING CRUISE, (ISFD) INTEGRATED STANDBY FLIGHT DISPLAY, DISPLAYED OUT OF ORDER MSG ONLY. AIRCRAFT DIVERTED. TROUBLESHOT SYSTEM. REMOVED AND REPLACED ISFD IAW 34-24-02. PERFORMED INSTALLATION TEST, TESTED NORMAL. RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20040915001062004091500106WP 2004 9 15 ASMF200407025 120040723A3397 WIRE HARNESS DOUG DC9 DC983 3022083WP LANDING LIGHT CRACKED W ASMFK NONE HJ ELECT. POWER LOSS-50 PC WARNING INDICATION ININSP/MAINT 1 SW23838AM 49397 DURING TRANSIT CHECK, CAPTAIN REPORTED POSITION LIGHTS TURNED ON, BREAKER DISCONNECTION. RT LANDING LIGHT WAS REPLACED AND POSITION AND LANDING LIGHTS TURNED ON. VOLTAGES WERE CHECKED AND WIRING BUNDLE WAS DETECTED CRACKED AND BURNED AT SLAT NR 2 ACCESS DOOR. WIRING BUNDLE WAS REPAIRED IAW WDM 33-41-01, TEST CORRECT. 2L72 4F RTA6WE 20040915001072004091500107NM 2004 9 15 ASMF200407028 120040724A213133990047 CONTROLLER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE AIR CONDITIONER FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23806AM12913 26273 726731 CAPTAIN REPORTED RT AIR CONDITIONING (PACK OFF) LIGHT TURNED ON CONTINUALLY AFTER ENGINE START AND WHEN ENGINE WAS IN IDLE POSITION, PNEUMATIC BLEED OF RT ENGINE WAS SHUTDOWN. PILOT CONTROLLER OF 14TH STAGE WAS REPLACED IAW MM 36-11-19, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20040915001162004091500116NM 2004 9 15 ASMF200408020 120040822A272095606 DRIVE ASSY DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE HORIZONTAL STAB FAILED W ASMFK NONE O OTHER APAPPROACH 1 SW23831LF249664165 53050 CAPTAIN REPORTED THAT DURING FINAL APPROACH HORIZONTAL STABILIZER FAILED, CIRCUIT BREAKERS D-9 AND D-11 WERE ACTIVATED AND FAIL CONTINUE WITH 2 DEGREES NOSE DOWN AND 3 DEGREES NOSE UP. SCREW GEAR, RELAYS AND WIRING AFTER ACCESSORIES COMPARTMENT WERE CHECKED AND NO DAMAGES WERE FOUND. DURING REVISION THE PRIMARY WAS DETECTED WITH DAMAGE. IT AND THE TRIM GEAR BOX WERE REPLACED IAW MM 27-40-01, TEST CORRECT. HORIZONTAL STABILIZER WAS OPERATED WITH AN ALTERNATE MOTOR, ALL CORRECT. 2L72 4F4 FRT E9NE 20040915001202004091500120NM 2004 9 15 SWAA042643 120040912A52106550573 GATE BOEING737 7373A4 1384585NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER GATE CRACKED. REMOVED AND REPLACED LOWER GATE PER MM. 2L72 4F RTA16WE 20040915001222004091500122NM 2004 9 15 SWAA042645 120040912A3350101114 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29732SW 27864 DURING SPV, FOUND 2 EACH OVERWING EMERGENCY EXIT LIGHT LENS, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040915001232004091500123NM 2004 9 15 UIEA200400150 120040824A21206203650 SEAL BOEING747 747228F 1384895NM AIR DISTRIBUTIONWORN A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15536MC 21576 MXP-BOM - WITH NR 1 PACK ONLY ON OPERATION AT FL280 AND 310, CABIN ALTITUDE WILL CONTINUE TO CLIMB AT 10 TO 20 FPM. IN CRUISE WITH BOTH OUTFLOW VALVES FULL CLOSED AND DIFF PRESSURE DECREASING FROM 8.4 PSI WITH NO DROP IN DUCT PRESS, DUCT PRESSURE 42 PSI. AFTER TURNING NR 2 PACK ON, CABIN ALT WILL RETURN TO NORMAL. PERFORMED ENGINE BLEED DISTRIBUTION SYSTEM OPERATIONAL TEST IAW MM 36-11-00, FOUND AIR LEAK FROM NR 1 PACK AIR SUPPLY DUCT TO PACK CONTROL SHUTOFF VALVE. REPLACED DUCT SEALS AND LEAK CHECKED OK. PERFORMED CABIN PRESSURE LEAKGATE TEST IAW 5-51-08 ALL WITHIN LIMITS. (M) 2L74 4F A20WE 20040915001242004091500124NM 2004 9 15 BJNA040806 120040825A335061047811 POWER SUPPLY BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE ESCAPE SLIDE INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11789TM 23046 AFT EMERGENCY ESCAPE SLIDE LIGHTS INOPERATIVE. REMOVED AND REPLACD THE AFT EMERGENCY LIGHT BATTERIES IAW AMM 31-51-71. (M) 2L72 4F4 FRTA16WE E2EA 20040915001262004091500126GL 2004 9 15 UIEA200400151 220040824A7250 TURBINE BLADES BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 3 ENGINE MISSING A UIEAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA15409MC 30558 706104 ON TAKEOFF ROTATION, ENGINE NR 3 HAD 2 COMPRESSOR STALLS. N1 ROLLED BACK AND RECOVERED, EGT REACHED 950 DEGREES CELSIUS. ON CLIMB-OUT AND CRUISE ENGINE OPERATED NORMAL. PERFORMED TEST 72-00-00-206-050-020. STALL INSPECTION, FOUND HPC STAGE 6, THREE BLADES 50 PERCENT MISSING. REMOVED AND REPLACED ENGINE IAW A717101GT1. ENGINE RUN UP AND LEAK CHECK, OPS NORMAL IAW B150201FT1 TEST 6 VIBES 2.1 AT N1 109.9. (M) 2L74 4F4 FRT1384945 E23EA 20040915001282004091500128NM 2004 9 15 BJNA040801 120040806A5330 SKIN BOEING737 737282 13844ATNM FUSELAGE CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT L1 DOOR LOWER HINGE CUTOUT AT BS 304. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIGURE 31. (M) 2L72 4F RTA16WE 20040915001312004091500131NM 2004 9 15 USAABB04069 120040721A1420 CONNECTOR BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19656US 26847 DUB - MAINTENANCE REPORTED THE CABIN FLOOR EMERGENCY LIGHTS AT SEAT ROWS 14 THROUGH 17L AND 24L INOPERATIVE. MAINTENANCE FOUND CONNECTORS AT SEAT ROWS 14L AND 24L. RECONNECTED CONNECTORS. ALL LIGHTS OPERATE NORMAL. (M) 2L72 4F RTA1NM 20040915001332004091500133NM 2004 9 15 USAABB04079 120040814A3397 WIRE BOEING767 767201 1385125NM ANNUNCIATOR LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 CDG - DURING DAILY CHECK, THE LEFT OVERWING FLOOR LIGHT ANNUNCIATORS FAILED TO ILLUMINATE. MAINTENANCE FOUND THE LOOSE CRIMP CONNECTION ON THE AFT ANNUNCIATOR, AND REPAIRED IT. (M) 2L72 4F RTA1NM 20040915001342004091500134NM 2004 9 15 SWAA04559 120040901A3350311500 LENS BOEING737 7373A4 1384585NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 SPV - FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. (M)SWAA 2L72 4F RTA16WE 20040915001382004091500138NM 2004 9 15 USAABB04078 120040811A3350 CONNECTOR BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19652US 24765 PHL - FOUND ESCAPE PATH LIGHT NEAR RIGHT MID LAVATORY DETACHED FROM ITS POWER SOURCE. MAINTENANCE RECONNECTED THE LIGHT. (M) 2L72 4F RTA1NM 20040915001392004091500139 2004 9 15 AMTA200401002 420040808A2565 GIRT BAR BOEING757 75723N 1384973NM ESCAPE SLIDE OBSTRUCTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND DOOR 2R WILL NOT ARM. REMOVED OBSTRUCTION, OPS CHECK OK. (M) 2L72 4F RTA2NM 20040915001412004091500141NM 2004 9 15 USAASB04018 120040214A52306546921528ME DOOR BOEING737 7373B7 1384580NM FWD CARGO OUT OF RIG A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19518AU55535 23704 EN ROUTE AT FL330, A/C LOST PRESS. CREW ACCOMPLISHED RAPID DESCENT OT 10,000 FT. OXY MASKS DEPLOYED DURING DESCENT. STANDBY & MANUAL PRESS MODES USED BUT NOT EFFECTIVE. OUTFLOW VALVE REPORTED TO BE FULLY CLOSED. A RUMBLING SOUND HEARD BENEATH THE FLOORBOARDS BY THE FORWARD & AFT CABIN CREW MEMBERS. FLT DIVERTED TO BNA & LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE SEAL AT LOWER PART OF FWD CARGO DOOR BLOWN OUT AT 7 PSI & DEPRESSURIZES A/C. RE-RIGGED FWD CARGO DOOR ROLLER FITTINGS & STOP PINS PER MM. REPLACED FORWARD CARGO DOOR THRESHOLD PLATE. PRESSURIZED A/C TO 7 PSI WITH NO DISCREP NOTED. (M) 2L72 4F RTA16WE 20040915001422004091500142WP 2004 9 15 2004F00343 120040806A82002D16205091 BELLMOUTH CVAC 440 440 2422902WP FUSELAGE CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION AND SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) 2L72 4R 6A6 20040915001432004091500143WP 2004 9 15 2004F00344 120040806A82002D16205041 DOOR CVAC 440 440 2422902WP FUSLEAGE CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 BAK - DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. DOOR REPLACED. (M) 2L72 4R 6A6 20040915001452004091500145NM 2004 9 15 USAABB04075 120040803A7500ETPU10003C PRESSURE SENSOR BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE LEFT ENGINE FAILED A USAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 EA19609AU35472 22205 31202 FLL - FLT 1409 - ON APPROACH TO FLL, AT APPROXIMATELY 1300 FEET AGL, LEFT ENGNE SHUT DOWN. NO FAULTS OR ABNORMAL CONDITIONS PRECEDED THIS EVENT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED ENGINE INLET, EXHAUST AND CHIP DETECTOR INSPECTIONS, PERFORMED BITE ON THE EEC, BVCU AND TPU. FAULT CODE 40 WAS FOUND ON THE TPU BITE. MAINTENANCE REPLACED THE TRANSIENT PRESSURE SENSOR. (M) 2L72 4F4 FRTA2NM E12EU 20040915001462004091500146NM 2004 9 15 AMTA200401062 120040820A2600644501 CARD BOEING757 75723N 1384973NM E/E BAY FAILED A AMTAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL11520AT 27976 STATUS MSG L ENG OH LP 1 DISPLAYED. INSTALLED CONTROL CARD. CHECKS GOOD. (M) 2L72 4F RTA2NM 20040915001472004091500147NM 2004 9 15 USAABB04065 120040713A3397609833 CONTACTOR BOEING767 767201 1385125NM EMERGENCY LIGHT BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 SNN - DURING DAILY CHECK, MAINTENANCE FOUND THE FORWAR4D LEFT FLOOR PATH EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TEST. MAINTENANCE FOUND CONTACT BROKEN ON FORWARD LEFT FLOOR PATH EMERGENCY LIGHT. REPLACED CONTACT IN ASSOCIATION WITH SWPM 20-30-17 AND WDM 33-51-17. PERFORMED SATISFACTORY OPERATIONAL TEST OF FLOOR PATH EMERGENCY LIGHTS IN ASSOCIATION WITH MM 33-51-00. (M) 2L72 4F RTA1NM 20040915001482004091500148EA 2004 9 15 A6WA200440115 120040821A361014459101 DUCT CNDAIRCL600 CL6002B19 1900309EA BLEED AIR FAILED A A6WAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL31418AW 7618 LEFT 10TH DUCT RED WARNING MESSAGE AFTER TAKEOFF BLEED AIR DUCT AURAL WARNING. COMPLIED WTH QRH MESSAGE WENT OUT AFTER REDUCING LEFT THROTTLE WHEN DUCT PSI FELL BELOW 60 PSI. REMOVED AND REPLACED 14TH STAGE DUCT AND 14TH STAGE SOV. OPS CHECK GOOD. CLEARED ON LOG PAGE 120506/1. THIS BLOWN DUCT CAUSED THE 10TH STAGE WARNING TO ILLUMINATE. (M) 2L72 4F RTA21EA 20040915001492004091500149NE 2004 9 15 HALA0400829 220040822A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE NR 2 FIRE A HALAC ABORTED TAKEOFF A FLAME/FIRE TOTAKEOFF 1 WP13478HA 55123 CREW REPORTED TO TAXI OUT, NR 2 ENGINE WENT TO 997C. ALOHA OBSERVED FLAMES COMING FROM NR 2 EXHAUST. ALSO, ACARS MESSAGE ENGINE SURGE. ENGINE CHANGE IN PROCESS. (M) 2L72 4F4 FTRA6WE E00057EN 20040915001542004091500154NM 2004 9 15 USAASB04111 120040816A3350210310005 FUSE BOEING737 7373B7 1384580NM CHARGER BLOWN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19376US 22955 MAINTENANCE REPORTED THE EMERGENCY LIGHT ABOVE THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REPLACED THE FUSES AT THE M1132 BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040915001562004091500156WP 2004 9 15 2004F00346 120040806A8200EA565AW3358 TRANSMITTER CVAC 440 440 2422902WP METHANOL SYS CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. TRANSMITTER REPLACED. (M) 2L72 4R 6A6 20040915001582004091500158CE 2004 9 15 2004F00348 120040625A2435400SG138Q STARTER LEAR 60 60LEAR 5170707CE NR 2 ENGINE INOPERATIVE A DELAK NONE O OTHER ININSP/MAINT 1 CE03188TG 078 DURING NORMAL ENGINE START SEQUENCE, THE NR 2 ENGINE DID NOT ROTATE. VISUAL INSPECTION REVEALED NO OBVIOUS ANOMALIES. NR 1 STARTER/GENERATOR TEMPORARILY SWAPPED TO NR 2. NR 2 ENGINE START ACCOMPLISHED WITHOUT FAULT. NR 1 STARTER/GENERATOR WAS RETURNED TO THE ORIGINAL POSITION AND THE NR 2 STARTER/GENERATOR WAS REPLACED WITH AN OVERHAULED UNIT. NR 2 ENGINE START ACCOMPLISHED WITHOUT FAULT. THE FAILED UNIT WAS ORIGINALLY INSTALLED IN AN OVERHAULED CONDITION AND HAD ACCUMMULATED 487.6 HOURS AND 340 STARTS. DELA (M) 2L72 4F RTA10CE 20040915001592004091500159WP 2004 9 15 2004F00349 120040806A8200312000 CHECK VALVE CVAC 440 440 2422902WP METHANOL SYS CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 BAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PART REPLACED. (M) 2L72 4R 6A6 20040915001612004091500161EA 2004 9 15 2004F00351 220040723A8500LW19340 CAMSHAFT PIPER PA31 PA31350 7103110SO LYC O540 LTIO540* 41533EA ENGINE WORN A FFSAK NONE O OTHER ININSP/MAINT 1 AL014301C1249 318353001 L245468A ENGINE OIL FILTER CONTAINED MANY FINE FLAKES OF FERROUS MATERIAL. PREVIOUS SOAP SAMPLE SHOWED ELEVATED IRON CONTENT. VALVE LIFT OF THE NR 3 AND NR 4 INTAKE VALVES WAS APPROXIMATELY .15 INCH LESS THAN THAT OF VALVES IN THE OTHER CYLINDERS. REMOVING THE NR 3 CYLINDER ALLOWED A VIEW OF SPALLED TAPPETS FOR THE NR 3 AND NR 4 INTAKE VALVES AND LOSS OF MATERIAL FROM THE TOE OF THEIR SHARED CAM LOBE. (M) 1L72 3O3 O A20SO E14EA 20040915001632004091500163SO 2004 9 15 2004F00352 120040624A55314002602 SPAR PIPER PA31 PA31350 7103110SO VERTICAL STAB CRACKED A FFSAK NONE O OTHER ININSP/MAINT 1 AL013536B22681 317952205 VISUAL INSPECTION OF VERTICAL FIN ATTACHMENT REVEALED APPARENT CRACK IN FRONT SPAR REINFORCING ANGLE AT RIGHT LOWER ATTACHMENT BUSHING. CRACK WAS VERIFIED BY DYE PENETRANT INSPECTION. (M) 1L72 3O A20SO 20040915001662004091500166EU 2004 9 15 2004F00353 120040818A261251216052 SENSOR AEROSPATR72 ATR72212 8680945EU ENG NACELLE ERRATIC A TRBAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO21434AT ABORTED TAKEOFF DUE TO RIGHT ENGINE FIRE WARNING INDICATION. REPLACED RIGHT ENGINE FIRE SENSING ELEMENTS. (M) 2H72 4T RTA53EU 20040915001672004091500167NM 2004 9 15 SWAA042557 120040901A5330 SKIN BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 25R, CRACKED. REPAIRED SIN PER SRM. (M) SWAA 2L72 4F A16WE 20040916000012004091600001EA 2004 9 16 A6WA200440116 120040819A2150 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA RT A/C PACK FAILED A A6WAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31422AW 7341 RIGHT PACK WILL NOT COOL CABIN IN AUTO OR MANUAL MODE, AIR RETURN. REMOVED AND REPLACED RIGHT PACK PRSOV IAW AMM 21-51-43. NO FIX. PLACED ON MEL. REPLACED AND TIGHTENED AIR DUCT AT CAPTAINS FEET AREA. OPS CHECK GOOD. REMOVED OFF MEL. (M) 2L72 4F RTA21EA 20040916000042004091600004NE 2004 9 16 2004F00356 220040807A753223075353 BLEED VALVE BELL 206 206B 1181511SW TMECA ARRIELARRIEL1 60030NE ENGINE FAILED E ALGAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 SW03198H 3647 WHILE HOVERING FOR TAKEOFF A LOUD BANG CAME FOR THE ENGINE COMPARTMENT FOLLOWED BY A TORQUE FLUCTUATION AND A RIGHT YAW. CHECKED ALL THE SYSTEMS ALL IN GREEN AND THEN HOVERED TO PARKING. MAINTENANCE INSPECTED COMPRESSOR FOR FOD AND LEAKS, NO DEFECTED NOTED. REMOVED AND INSPECTED PC AIR FILTER, FOUND CLEAN REINSTALLED PC FILTER ASSY. REMOVED AND REPLACED COMPRESSOR BLEED VALVE, AIRCRAFT GROUND RAN LEAK AND OPS CHECK, ALL SYSTEMS GOOD. AIRCRAFT OPERATIONAL CHECK FLOWN AND RETURNED TO SERVICE. WORK DONE IAW THE MANUFACTURES MM. (M) 1G71 3U3 U H2SW E19EU 20040913001162004091300116NM 2004 9 13 QXEA200400524 120040713A5720 BRACKET DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 LT WING FORWARD SPAR Z BRACKET IS CRACKED AT APPROXIMATELY STATION YW48.000. REPAIRED IAW SRM 51-40-11 AND EA 2-57-267. 2H72 4T4 TRTA13NM E20NE 20040913001172004091300117NM 2004 9 13 QXEA200400521 120040713A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX - RT OB TRACK NR 12 SEAT ATTACH AREA CORROSION, BARE METAL APPROXIMATELY X518.00. REPAIRED IAW SRM 51-40-00. 2H72 4T4 TRTA13NM E20NE 20040913001182004091300118NM 2004 9 13 QXEA200400519 120040713A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09360PH 515 PDX - RT OB TRACK NR 10 SEAT ATTACH AREA CORROSION APPROXIMATELY X424.00. REPAIRED IAW SRM 51-40-11. 2H72 4T4 TRTA13NM E20NE 20040913001192004091300119WP 2004 9 13 MWEA040145 120040812A53209936534161 SUPPORT ANGLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 PAX DOOR THRESHOLD FLOORBOARD ATTACH ANGLE CORRODED AT NUTPLATE FLANGE FORWARD AND AFT. FABRICATED AND INSTALLED SUPPORT ANGLE. 2L72 4F4 F A6WE E9NE 20040913001212004091300121NM 2004 9 13 04028 120040623A2612 FIRE LOOP BOEING747 747209B 138489BNM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE MALFUNCTIONED A KCSAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23715CK 22447 702415 NR 3 ENG FIRE IND IN FIRE SWITCH AND "B" LOOP AT 9.5 DURING CRUISE. "A" LOOP INOP. ENG SHUTDOWN AND BOTH FIRE BOTTLES DISCHARGED AND FIRELIGHT REMAINED ON. CONDITIONS BEFORE SHUTDOWN, OIL PRESSURE 47-PSI OIL TEMP 88. NO IGNITION OR ANTI-ICE. AFTER SHUTDOWN, OIL PRESSURE 17 WINDMILLING 45 MIN. 4 PSI PRESSURE FOR 6 MIN. DURING APPROACH AND LANDING, OIL TEMP 88. ENGINE STABLE THROUGHOUT. REMOVED AND REPLACED NR 3 (2EA) FIRE EXTINGUISHER BOTTLES IAW MM CH 26-21-03, SYS OPS CHECKS NORMAL. REMOVED AND REPLACED "A" AND "B" LWR AFT FIRE SENSOR ELEMENT IAW MM CH 26-11-02, SYS OPS CHECKS NORMAL. INSPECTED NR 3 ENG FOR ANY OTHER DEFECTS NO OTHER DEFECTS NOTED. ENG SHUT DOWN DUE TO FAULTS IND OF FIRE SENSOR ELEMENTS.2L74 4F4 FRTA20WE E3NE 20040913001232004091300123EA 2004 9 13 COMA0460437 120040730A26124759701 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT FIRE WARNING MALFUNCTIONED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01967CA20495 7134 FIRE FAIL CAUTION, LT ENGINE FIRE WARNING, IFSD LT ENGINE FOLLOWED BY RT ENGINE FIRE WARNING, AND APU FIRE WARNING. REPLACED THE FIREX CONTROLLER. 2L72 4F4 FRTA21EA E15NE 20040913001242004091300124CE 2004 9 13 DXTA200400354 120040806A26123101211050 FIRE DETECTOR CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RT ENGINE MALFUNCTIONED E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07951QS3202 7500151 AMBER FIRE DETECTOR FAIL R MESSAGE ILLUMINATED DURING CRUISE, DIVERTED AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. TROUBLESHOT AND FOUND THE ENGINE FIRE LOOP CHAFFED, REMOVED AND REPLACED THE RT ENGINE FIRE LOOP OPERATIONAL CHECK GOOD IAW MFG M/M CHAPTER 26-10-00. 2L72 4J4 FRTT00007WITE6CH 20040913001292004091300129NM 2004 9 13 QXEA200400631 120040819A1420473054 CONNECTOR DHAV DHC8 DHC8202 2809007NM PWA PW120 PW123 NE SMOKE DETECTOR LOOSE A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09368PH13483 512 CREW RECEIVED A SMOKE, MASTER WARNING, AND ANNUNCIATOR INDICATIONS ON TWO OCCASIONS. NO SMOKE OR ABNORMAL SMELLS WERE NOTICED. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE NR 2 SMOKE DETECTOR CONNECTOR PLUG NOT TIGHT. BOTH THE NR 1 AND 2 DETECTOR CONNECTOR PLUGS WERE REMOVED, CLEANED AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040913001312004091300131NM 2004 9 13 AWXA200400726 120040625A5320D534775320400 PLATE AIRBUSA319 A319132 3930340NM DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK CORROSION (4 SPOTS) WAS FOUND ON AFT CARGO DOOR SILL PLATE. MAINTENANCE REMOVED AND FABRICATED A NEW AFT CARGO DOOR SILL PLATE IAW A319 SRM 51-42-11 FIGURES 3,4,5,9 AND MFG DRAWING 17D53477153. 2L72 4F RTA28NM 20040913001332004091300133NM 2004 9 13 AWXA200400729 120040626A5315D5348004320500 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 AT FR 66. MAINTENANCE REPAIRED BEAM Y1732 DOOR SILL AT FR 66 IAW A319 SRM 53-41-14 FIG. 201. 2L72 4F4 FRTA28NM E311NE 20040913001352004091300135NM 2004 9 13 AWXA200400731 120040626A5315D5347209000300 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 FROM FR 64 TO FR 66 IAW A319 SRM 51-42-11 PG. 39 AND 41 FIG. 18. 2L72 4F4 FRTA28NM E311NE 20040913001372004091300137NM 2004 9 13 AWXA200400733 120040627A5315D5347209000200 FLOORBEAM AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW 1049 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 AT FR 66. MAINTENANCE REMOVED AND REPLACED BEAM Y765 AT FR 66 IAW A319 SRM 51-72-11 PG. 1 AND 2. 2L72 4F4 FRTA28NM E311NE 20040913001502004091300150EU 2004 9 13 KBM2004F00166 120040516A733260128503 GAUGE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D1 NE FUEL / OIL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 412 2009 FUEL AND ENGINE OIL PRESSURES READ ZERO IN FLIGHT. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040913001542004091300154EU 2004 9 13 CX7A194J0443 120040727A261289905202 FIRE DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE INOPERATIVE A CX7AFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL03309CE1806118061 340B201 AT 4000 FT, WE RECEIVED A MOMENTARY FIRE DET FAIL LT ON THE RT ENG. ABOUT 2 SEC AFTER IT WENT OUT WE RECEIVED A MOMENTARY RT ENG FIRE WARNING. PERFORMED ENG CHECK LIST AND LANDED (RT FIRE BOTTLE WAS DISCHARGED). ADJUSTED FIRE LOOPS AND CHANGED OUR FIRE DETECT CONTROL UNIT. 2L72 4T4 TRTA52EU E8NE 20040913001612004091300161 2004 9 13 HAEA200400156 420040713A3414B020081127 INDICATOR AMD FALCONFALCON20 2730103EU GE CF700 CF700* 30010NE COCKPIT SLUGGISH E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05314TW1394313943 314 ON DEPARTURE FROM ADS CAPTAINS AIRSPEED INDICATOR HAS 30-45 KNOT SPLIT FROM CO-PILOTS AIRSPEED INDICATOR. AIRCRAFT RETURNED TO ADS FOR MAINTENANCE. MAINTENANCE REPLACED CAPTAINS AIRSPEED INDICATOR. OPS TESTS GOOD. (CLOSED) 2L72 4F4 FRTA7EU E7EA 20040913001632004091300163SO 2004 9 13 LR7A04081 120040716A5320LS36423 INTERCOSTAL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION DRC 2210 ACCOMPLISHMENT FOUND INTERCOSTAL INBD CAP CRACKED CLOSE TO EXISTING REPAIR AT FS 494, RBL 62, WL 200. CAP REPLACED IAW SRM SMP 583 CHP51-60 & 51-70. DRC 2222. 2H74 4T4 T A1SO E282 20040913001652004091300165SO 2004 9 13 LR7A04083 120040716A5343 BEAM LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND FS 597 MLG BEAM IB CAP CRACKED AT RBL 62, WL 257. REPAIRED IAW LAC MEA 382-53-04-055. DRC 4422. 2H74 4T4 T A1SO E282 20040913001672004091300167SW 2004 9 13 AC2A094948 120040410A3000222325001027 GUIDE ARM BELL 430 430 1182150SW CORRODED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CV 49072 PIVOT POINT OF GUIDE CORRODED, SWOLLEN AND BROKE. 1G72 3U RTH9SW 20040913001782004091300178NM 2004 9 13 UIEA200400123 120040713A2611376 BULB BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE SMOKE DETECTOR FAILED A UIEAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 EA15506MC 21252 PO380/10 DXB/CGK LOWER CARGO AFT FIRE LIGHT CAME ON DURING TAKEOFF: LOWER CARGO AFT FIRE LIGHT CAME (ON) AT ROTATION. APPROPRIATE DRILLS CARRIED OUT. AIRCRAFT RETURNED TO DEPARTURE. CHECKED LOWER AFT CARGO FOR FIRE OR DAMAGE, NO EVIDENCE. BULK CARGO IS EMPTY. CHECKED DETECTORS, ALL LAMPS ARE WORING. RELAMPED AS A PRECAUTION IAW MM 26-16-00, TEST OK. NO FUEL DUMPED. 2L74 4F4 FRTA20WE E23EA 20040913001832004091300183EA 2004 9 13 QXEA200400528 120040715A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX5687 20 10041 THE FORWARD CARGO BAY FIRE DETECTION CHIMNEY SCREEN IS TORN AT THE CARGO DOOR AREA. THE CHIMNEY WAS REMOVED AND REPLACED WITH NEW. OPERATIONAL CHECKS ARE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040913001852004091300185NM 2004 9 13 WLDA200477 120040802A5510ALC8104501 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 15.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE 15 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040913001912004091300191EU 2004 9 13 AWXA200400914 120040805A5320D53112609200 DUMMY RAIL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y1203 RT AFT OF FR 15. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y1203 RT AFT OF FR 15; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040913001942004091300194NM 2004 9 13 WVE2004F00019 120040613A53116003603024 FRAME BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A WVERO OTHER O OTHER NRNOT REPORTED 1 EA09503SW 24180 RT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1 INCH LONG IN RADIUS OF FRAME FLANGE. POSSIBLE STRESS RELIEF CRACK. REPAIR IAW MFG REO 601R5-53-61-193 REV A. 2L72 4F4 FRTA16WE E2GL 20040913001962004091300196WP 2004 9 13 MWEA040139 120040811A5320993061267 CUSP WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FRAME STA 1309 LT CUSP MEMBRANE IS CRACKED FROM LIGHTNING HOLE TO LIGHTNING HOLE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20040913001982004091300198WP 2004 9 13 COOSDR040008 120040630A5512 PANEL DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE HORIZONTAL STAB CRACKED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 LT HORIZONTAL STABILIZER STA XFS 47 NR 1 UPPER STRINGER CRACKED. 2L74 4F4 F 4A25 1E8 20040913002022004091300202EU 2004 9 13 KBM2004F00117 120040720A6710704A34130141 CONTROL CABLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COLLECTIVE DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 RESISTANCE FELT IN COLLECTIVE AT UPPER END OF COLLECTIVE MOVEMENT. REPLACED O/S GOVE CABLE WITH NEW CABLE. 1G71 3U3 U H9EU E19EU 20040913002052004091300205NM 2004 9 13 DL73S040786 120040820A555165505781 FITTING BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27375DL 23602 HORIZONTAL STABILIZER, LT OB STAB, NR3 LUG, CORROSION. CORROSION WAS FOUND IN THE BORE OF THE LT OB STAB SECTION REAR SPAR UPPER ATTACH LUG DURING INSPECTION IAW E.O. 3-53025-3AD. THE BORE WAS OVERSIZED BEYOND THE E.O. LIMITS TO REMOVE DAMAGE AND AN OVERSIZED BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED IAW ER/A 092266-14AD. 2L72 4F4 F A16WE E2EA 20040913002082004091300208EU 2004 9 13 KBM2004F00217 120040818A2110 PULLEY SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE A/C COMPRESS OBSTRUCTED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH435 3787 IFS AIR CONDITIONING COMPRESSOR PULLEY CAME IN CONTACT WITH STRUT BAR. REPLACED STRUT BAR AND RESHIMMED PULLEY SO AS NOT MAKE CONTACT WITH STRUT. 1G71 3U3 U H9EU E19EU 20040913002102004091300210SO 2004 9 13 C2XA04TY134 120040802A532014530627001 CHANNEL EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION THE RT SIDE STEPUP BRACKET AFT OF PAX DOOR WAS FOUND CORRODED. MAINT. REMOVED AND REPLACED THE STEP UP BRACKET AND CENTER OMEGA BEAM IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL 4C WORK. 2L72 4F4 FRTT00011ATTE6CH 20040914000012004091400001CE 2004 9 14 64107 120040821A3260 SOCKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE ANNUNCIATOR DIRTY A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07176YV UE176 DISPATCH RECEIVED A CALL FROM MGW STATION THAT THEY HAD BEEN CONTACTED BY FLT 4740 AND INFORMED THAT THE AIRCRAFT DID NOT HAVE 3 GOOD DOWN AND LOCK INDICATIONS FOR MAIN LANDING. CREW WAS ADVISED TO FOLLOW CHECKLIST AND DIVERT. THEY LEARNED LATER THAT CREW HAD 3 GOOD DOWN AND LOCK INDICATOR AFTER TROUBLE SHOOTING LANDING GEAR DOWN LOCK INDICATOR. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. INDICATOR WRITTEN UP. CLEANED ANNUNCIATOR SOCKET AND REBULBED. 2L72 4T4 TRTA24CE E26NE 20040914000082004091400008EA 2004 9 14 COMA0460492 120040901A5310601R317725 ANGLE CNDAIRCL600 CL6002B19 1900309EA LYC O540 IO540B1A5 41532EA PAX DOORWAY CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01477CA5851 7670 PASSENGER DOOR AFT CLOSE OUT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR TO PASSENGER DOOR AFT DRAG ANGLE BY CUTTING AWAY DAMAGED AREA, LPI FABED REPAIR ANGLES AND INSTALLED IAW BOMBARDIER REO 601R-52-11-513. 2L72 4F3 ORTA21EA 1E4 20040914000132004091400013 2004 9 14 04251662 420040904A3420 AHRS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27662BR 7526 EVENT SUMMARY STATED THAT EFIS COMP MON POSTED AHRS 1 PITCH INOPERATIVE, AHRS 2 INTERMITTENT. RTN FROM FLT. NR 2 AHRS FAULTED. REMOVED AND REPLACED NR 2 AHRS. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040914000152004091400015NM 2004 9 14 BJNA040807 120040825A5310 DOOR FRAME BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER FORWARD CORNER FRAME CRACKED. INSTALLED NEW LOWER FORWARD CORNER AT C1 DOOR IAW SRM 51-20-1 AND SERVICE BULLETIN 737-52A1100 REV 4. (M) BJNA 2L72 4F4 FRTA16WE E2EA 20040914000172004091400017NM 2004 9 14 DHL2004745022 120040909A2612 FIRE LOOP BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01745DH 20665 ENG NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED ON P6-3. REPOSITIONED NR 3 ENGINE FIRE LOOP. RESECURED NR 3 ENGINE COWLING. TESTED GROUND FAULT SYSTEM IAW MM 26-11-00. OPS CHECKS NORMAL. 2L73 4F4 F A3WE E2EA 20040914000202004091400020EU 2004 9 14 AWXA200400994 120040815A5321D5367205000000 FLOOR PANEL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151 PF DELAMINATED ON AFT SIDE. MAINTENANCE REMOVED DELAMINATED AFT CARGO COMPARTMENT FLOOR PANEL 151 PF FROM FR 58 TO FR 59; FABRICATED A NEW REPLACEMENT FLOOR IAW A320 SRM 53-02-00, FIG. 209, PG. 233-236. 2L72 4F4 FRTA28NM E311NE 20040914000262004091400026EU 2004 9 14 AWXA200401000 120040814A5347D5311281520000 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 18 AND FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FR 18 TO FR 20; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-11-15, FIG. 203, PG. 209-212, 219-220. 2L72 4F4 FRTA28NM E311NE 20040914000322004091400032EU 2004 9 14 MALA040559 120040807A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15534XJ E2370 DURING SCHEDULED CAPACITY CHECK, BATTERY PACK PN/61-2275-1 SN/9801233 FAILED ON 8/7/04 AND 8/11/04. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 61-2274-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 8/17/04. REFER TO WO NR 373759 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000372004091400037EU 2004 9 14 MALA040552 120040818A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15511XJ E2325 DURING CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/9911208 REMOVED FAILED CAPACITY CHECK 8/18/04 & 8/25/04. MAINTENANCE REPLACED BATTERY PACK ASSEMBLY 61-2274-1 UNIT PASSES CMM TESTS, RETURNED TO SERVICE 8/29/04. REFER TO WO NR 374107 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000402004091400040EU 2004 9 14 MALA040554 120040818A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15520XJ E2345 DURING CAPACITY CHECK, BATTERY PACK PN 61-2275-1 SN/0006373 REMOVED FOR CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY 61-2274-1 UNIT PASSES CMM TESTS, RETURNED TO SERVICE 8/19/04. REFER TO WO NR 374269 FOR ADDITIONAL INFORMATION. 2H74 4F4 FRTA49EU E6NE 20040914000432004091400043EA 2004 9 14 HNAA0400082 120040907A6120 BETA SWITCH DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 1 ENGINE MALFUNCTIONED A HNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA07329EN 290 NR 1 ENGINE BETA LOCKOUT FAILURE AT 500 FT, ENGINE OSCILLATED AT 1000 PROP RPM, TORQUE REACHED 112 PERCENT FOR 1 SECOND (CREW RETARDED THE CONDITION LEVER AND PROP RPM DROPPED TO 900 OSCILLATION STOPPED) CONSULTED MM AND ENGINE PROGRAM MAN. DETERMINED AC DID NOT EXCEED LIMITS. DEACTIVATED BETA LOCKOUT SYSTEM IAW WITH MEL. C/W WORK CARD 61-20-10 AND GROUND RUN FOUND NO DEFECTS NOTED CLEAR MEL. 2H72 4T4 TRTA13NM E20NE 20040914000542004091400054WP 2004 9 14 DHL2004804517 120040709A57203645612U BRACKET DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR. 0519: NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 1 ALT. TANK FWD BOOSTER PUMP IAW SRM 51-3-0 PG.1 2L74 4F4 FRT4A25 E2GL 20040914000592004091400059NM 2004 9 14 DHL200474006 120040716A5320 WEB BOEING727 7272Q9 138448MNM PWA JT8 JT8D17R 52049NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 DURING A-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED. NOSE SECTION LWR LOBE INTERIOR BS 312 AND RT SIDE HORIZONTAL WALKING BEAM. CORROSION AT FRAME ATTACH CLIP; CUT OUT DAMAGED WEB SECTION (ATTACH CLIP) AT STA.312 AT HORIZ WALKWAY BEAM RT SIDE IAW SRM 51-40-2 7 INCH X 4 INCH. FABRICATED AND INSTALLED WEB FILLER AND SPLICE PLATE IAW SRM 53-10-2 FIG.1 AND 51-40-2 FIG.1 MAT. USED FILLER .050 7075-T6 7 INCH X 4 INCH P.O. 900780 SPLICE PLATE .063 7075-T6 2 INCH X 4 INCH P.O. 900861. ALL PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2. 2L73 4F4 FRTA3WE E2EA 20040914000712004091400071EU 2004 9 14 0401363232 120040818A3350321454 POWER SUPPLY AIRBUS320 A320211 3930320EU GE CFM56 CFM565A 13802NE EMERGENCY LIGHT SHORTED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01332NW3854438544 319 DURING FLIGHT, FUMES WERE REPORTED IN THE CABIN AND COCKPIT. NO SMOKE OR HEAT SOURCE WAS IDENTIFIED. THE OZONE FILTER WAS REPLACED, THEN ROW 11F EMERGENCY LIGHTS POWER SUPPLY SHORTED. REPLACED THE POWER SUPPLY AND TESTED OK. 2L72 4F4 FRTA28NM E29NE 20040914000722004091400072SO 2004 9 14 RAIA00408024 120040823A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL THRUST REVERSER ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03816HK 145055 THRUST REVERSER DISAGREE, NR 2. MAINTENANCE DEFERRED NR 2 T/R, IAW MEL. CLEARED DMI. REMOVED NR 2 THRUST REVERSER UPPER INBOARD STOW/TRANSIT SWITCH. 2L72 4T4 FRTT00011ATTE6CH 20040914000772004091400077SO 2004 9 14 GLBA20030655 120040625A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE EMERGENCY LIGHT DISCHARGED A GLBAK NONE L NO TEST ININSP/MAINT 1 NM03108UX4602 210 120108 EMERGENCY EXIT LIGHTS VERY DIM, REMOVED AND REPLACED BATTERY PACK. 2L72 4T4 TRTA31SO E20NE 20040914000872004091400087SO 2004 9 14 RAIA00408015 120040812A3244 TIRE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MLG SEPARATED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03819HK 145062 DURING POST FLIGHT INSPECTION AFTER PARKING AT STL, FOUND LT IB TIRE WITH RETREAD CAP MISSING. MAINTENANCE REMOVED AND REPLACED LT IB TIRE. INSPECTED AIRCRAFT. REPAIRED DAMAGE ASSOCIATED WITH TREAD SEPARATION. 2L72 4T4 FRTT00011ATTE6CH 20040914000892004091400089SO 2004 9 14 RAIA00408016 120040813A3610S2D226 SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 BLEED SYS LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03817HK 145058 NR 2 BLEED LEAK. MAINTENANCE REMOVED AND REPLACED SEAL AT RT T-PIPE IN CARGO BAY. 2L72 4T4 FRTT00011ATTE6CH 20040914000912004091400091NM 2004 9 14 UPS04243008 120040804A5280 WEB BOEING727 72722C 138400FNM RROYCETAY TAY65154 EU LT MLG WING DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 LT MLG WING DOOR LWR END WEB CRACKED. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC INSPECTION CARRIED OUT. CRACK CONTAINED IN STOP DRILLED HOLE. REPAIRED IAW 51-40-02. 2L73 4F4 F A3WE E25NE 20040914001012004091400101NM 2004 9 14 UPS04442995 120040823A3350 NUT BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE SWITCH ASSY LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: N/A, EMERGENCY LIGHTS ARM SWITCH INTERMITTENTLY INOPERATIVE. NOTICED UNARMED LIGHT ILLUMINATED. CYCLED SWITCH ON-ARM/ OFF AND GOT MIXED RESULTS. WILL NOT STAY ARMED IN ARM POSITION. TIGHTENED JAM NUT ON SWITCH ASSY. OPS CKS GOOD. 2L74 4F4 FRTA20WE E3NE 20040914001092004091400109EU 2004 9 14 KBM2004F00202 120040613A21210500847 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 NOT BLOWING COLD AIR, REMOVED AND REPLACED 7 IN BLOWER MOTOR. 1G71 3U3 U H9EU E19EU 20040914001172004091400117EU 2004 9 14 KBM2004F00206 120040812A2110 COMPRESSOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE A/CONDITIONER FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH104 2957 BELT BROKE, UPON INSPECTION FOR COMPRESSOR PULLEY AND CLUTCH BURNED UP. REPLACED BELT AND COMPRESSOR AND PULLEY ASSY. 1G71 3U3 UNCH9EU E19EU 20040914001232004091400123EA 2004 9 14 A6W2004F00000 120040617A5260 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR STAIR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31410AW 7490 PAX DOOR STAIR STRUCTURE AFT ANGLE, PN 601R31907-303, IS CRACKED .8 INCHES LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601R311719 IAW REO 601R53-41-059. 2L72 4F4 FRTA21EA E15NE 20040914001262004091400126CE 2004 9 14 AJC2004F00002 120040610A2751DT2RV212A7 POSITION SWITCH RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP TE FLAPS DAMAGED E AJCAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25261PA811 258587 DURING TAKEOFF, ENROUTE, THE LANDING GEAR HORN SOUNDED WHEN GEAR LEVER WAS PLACED IN UP POSITION, BOTH WITH FLAPS IN 15 DEGREE AND 0 DEGREE POSITION. CREW PLACED GEAR LEVER IN DOWN POSITION AND HORN SILENCED. CREW CIRCLED AND BURNED OFF FUEL AND RETURNED TO DEPARTURE AIRPORT AND LANDED SAFELY. DID NOT DECLARE EMERGENCY. AC WAS FERRIED TO HOME BASE FOR MAINTENANCE. UPON INVESTIGATION IT WAS FOUND THAT THE FLAP POSITION SWITCH WAS AT FAULT. REMOVED AND REPLACED RT THROTTLE QUADRANT FLAP SWITCH WITH NEW. PERFORMED OPS CHECK OF GEAR HORN SYSTEM. OPS CHECK, NORMAL AND AC RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20040914001302004091400130SO 2004 9 14 Q532004F00000 220040701A8520642399 CONNECTING ROD BEECH 36 B36TC 1151609CE CONT O520 TSIO520UB 17040SO NR 4 CYLINDER BENT D Q53EO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 NM118072G1289 EA537 527177 ROUGH RUNNING ENGINE, PULLED NR 4 CYLINDER FOUND CONNECTING ROD HAD SLIGHT BEND. CAM SHAFT LOBES FORWARD OF CYL 4, WORN OUT. 1L71 3O3 O 3A15 E8CE 20040914001372004091400137 2004 9 14 ASMF200407020 420040718A34426225135001 ANTENNA DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE RADAR DAMAGED W ASMFDA RETURN TO BLOCK UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW231075T6066 49724 AIRCRAFT RETURNED OF FLIGHT, RADAR WAS OUT OF SERVICE WITH (TR AND FAIL ON DISPLAY) LEGENDS. TRANSCEIVER RADAR WAS CHECKED, RACK AND UNIT CONNECTORS WERE CLEANED AND ANTENNA WAS CHECKED, ALL CORRECT. TRANSCEIVER WAS REINSTALLED AND TESTED IAW MM 34-41-00, ALL CORRECT. OVERWEIGHT INSPECTION WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. AIRCRAFT WAS DISPATCHED AND DURING CRUISE, RADAR FAILED AGAIN AND CREW PERFORMED UNSCHEDULED LANDING AT VER. TRANSCEIVER AND RADAR ANTENNA WERE REPLACED IAW MM 34-41-04 AND 34-41-01, RESPECTIVELY, TESTS CORRECT. DURING OVERNIGHT SERVICE, RADAR WAS CHECKED BY CONTINUITY AND ISOLATION IAW WDM 34-43-01AND 34-43-02 AND TESTED IAW MM 34-41-00, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040914001412004091400141NM 2004 9 14 USA2004F00067 120040602A335020121 CHARGER BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT INOPERATIVE A USAAO OTHER L NO TEST NRNOT REPORTED 1 EA19627AU 27805 FOUND EMERGENCY LIGHTS FOR RT SIDE OF ROWS 1 THROUGH 7 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERIES. 2L72 4F4 FRTA2NM A12EU 20040914001452004091400145EA 2004 9 14 SWIA200413600 120040715A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA STALL WARN SYS DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07976SW 7952 STALL PROTECTION SYSTEM WILL NOT PASS TEST. STALL FAIL MESSAGE. FOUND TB75-3 SOCKET -J- DAMAGED. REPLACED TB75-3 IAW MM 24-01-03, 20-18-70. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20040914001462004091400146GL 2004 9 14 ALG2004F00043 220040625A753223005366 BLEED VALVE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03361AL9870 9870 51212 CAE895014 WHILE HOVERING AND IN A RT PEDAL TURN PREPARING FOR TAKE OFF A LOUD BANG WAS HEARD AND AIRCRAFT YAWED MOMENTARILY LT THEN RT. RETURNED TO MAINTENANCE PAD AND SHUT DOWN AND NOTIFIED MAINTENANCE. MAINTENANCE REMOVED BLEED VALVE PN 23005366A, SN FF43547 AND INSTALLED BLEED VALVE PN 23005366 SN FF43634, OPS CHECK WAS GOOD. 1G71 3U3 U H2SW E1GL 20040914001542004091400154NM 2004 9 14 UIEA200400105 120040602A5414 SKIN BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 1 NACELLE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D-CHECK, DAMAGE WAS FOUND ON RT SIDE OF NR 1 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE, EXPOSED WINDOW STRAP SURFACE, ALONG WITH THE FASTENER HOLES, WERE HFEC INSPECTED TO ENSURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .254. RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON THE NR 3 STIFFENER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2L74 4F4 F A20WE E23EA 20040914001572004091400157SO 2004 9 14 2004F00234 120040707A56101159SCB310212 WINDSCREEN GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU COCKPIT CRACKED E O OTHER O OTHER DEDESCENT 1 EA071NA 2074 309 WINDSCREEN CRACK DURING FLIGHT. 2L72 4F4 F A12EA E2EU 20040914001622004091400162EU 2004 9 14 SDR2004036 120040601A324310025111Y00 MASTER CYLINDER AEROSPATR72 ATR72202 8680940EU PWA PW120 PW127 NE BRAKING SYSTEM FAILED A TRBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO21252AM 253 F/O`S LT BRAKE PEDAL HAS NO ACTION. REMOVED AND REPLACED F/O BRAKES MASTER CYLINDER. 2H72 4T4 TRTA53EU E20NE 20040914001652004091400165EA 2004 9 14 A6WA200440075 120040609A2410 IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NR 2 LOW A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31423AW 7636 GEN NR 2 CAS MESSAGE AFTER TAKEOFF. RETURNED TO CID. SERVICED NR 2 IDG IAW MM. OPS CHECK NORMAL. 2L72 4F4 FRTA21EA E15NE 20040914001702004091400170NE 2004 9 14 ASMF200406036 220040630A7230 BLADE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE COMPR DAMAGED W ASMFK NONE C F.O.D. ININSP/MAINT 1 SW23803ML 49726 728169 DURING TRANSIT CHECK, LT ENGINE BLADE WAS DETECTED WITH DAMAGE FROM FOD. BLADE WAS REPAIRED IAW MM 72-33-21, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040914001982004091400198NM 2004 9 14 USA2004F00081 120040606A272065C370539 PCU BOEING737 7374B7 1384702NM GE CFM56 CFM56* 13802NE RUDDER INOPERATIVE A USAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA19785AU383414982 25024 PILOT REPORTED A SLIGHT UNCOMMANDED RUDDER INPUT WHICH WAS DESCRIBED AS AN UNCONTROLLED RUDDER JERK. JERK WAS NOT ADVERSE OR SEVERE. CREW REPORTED NO RUDDER PEDAL MOVEMENT WAS DETECTED. (A) CHANNEL AUTOPILOT WAS ENGAGED AT TIME IN BOTH LNAV AND VNAV, FLT WAS IN SMOOTH AIR AT TIME OF OCCURRENCE. CREW DECIDED EVENT WAS NOT SIGNIFICANT ENOUGH TO WARRANT AN UNCOMMANDED RUDDER EMERGENCY PROCEDURE, BUT DID DECIDE TO DISENGAGE THE AUTOPILOT FOR REMAINDER OF FLIGHT. FLIGHT CONTINUED AND LANDED W/O FURTHER INCIDENT. MAINT REMOVED AND REPLACED RUDDER PCU ASSY. OPS CHECK AND LEAK CHECK GOOD. ALSO, REMOVED AND REPLACED YAW DAMPER COUPLER, FDR IAW MM AS DIRECTED BY MAINT CNTRL. OPS CHECKS GOOD. 2L72 4F4 FRTA16WE E2GL 20040915000102004091500010NM 2004 9 15 UPS04243063 120040816A5330 LAP JOINT BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, SUSPECT CORROSION AT LAP JOINT S19L BETWEEN BS 390 AND BS 441, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. REPAIR CARRIED OUT IAW AAAE 2004-077-006 AND UPS EO B727-5330-21003-A. 2L73 4F4 F A3WE E25NE 20040915000222004091500022EA 2004 9 15 04252621 120040907A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FAILED A VTZAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 EA27621BR 7186 FLAPS FAIL MSG AT 0 DEGREES. CYCLED POWER ON A/C PERFORMED. OPS CHECK OF FLAPS OPS CHECK OK, REF CRJ MM 27-54-00. 2L72 4F4 FRTA21EA E15NE 20040915000392004091500039EA 2004 9 15 SWIA200413760 120040829A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07905SW5590 5590 7437 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW MM 27-42-05. OPERATIONAL CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20040915000402004091500040EA 2004 9 15 SWIA200413761 120040824A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07915SW471 471 7615 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. INSTALLED A SERVICEABLE HSTCU. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040915000442004091500044EU 2004 9 15 04FDEA02582 120040831A5320R538D104820200 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 REF. SNRM N00261 MAIN DECK CARGO COMPT. AT FR 42 BETWEEN L1 AND L2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040915000452004091500045EU 2004 9 15 04FDEA02583 120040831A5320R5380104820200 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 MAIN DECK CARGO COMPT AT FR 40/41 BETWEEN R1 AND R2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK. 2L72 4F4 FRTA35EU E13NE 20040915000752004091500075NM 2004 9 15 P9RA20040038 120040906A3350284N140224 WARNING LIGHT BOEING757 757236 1384971NM RROYCERB211 RB211* 54555NE R4 DOOR SLIDE INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11522NA 25133 AIRCRAFT IN MAINTENANCE; ORD. 4R DOOR SLIDE ARMED LIGHT INOPERATIVE. REMOVED AND REPLACED DOOR ARM LIGHT ASSEMBLY. 2L72 4F4 FRTA2NM A12EU 20040915000802004091500080EA 2004 9 15 O2G2004F00002 120040624A7500GE4020T35604 REGULATOR CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE BLEED AIR FAILED E O2GAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NE03653AC 5153 807136 UPON ENGINE START, SMOKE APPEARED IN THE CABIN. REMOVED AND REPLACED CARBON SEAL, PRESSURIZING AIR REGULATING VALVE ON THE ENGINE, AND ECU. 2L72 4F4 FRTA21EA E15NE 20040915000822004091500082 2004 9 15 ASMF200408007 420040808A34214608000307 AHRS DOUG DC9 DC987 3022087WP PWA JT8 JT8D NE LT SIDE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23751RA7876 49779 AIRCRAFT RETURNED TO PLATFORM, AHRU NR 1. AIRCRAFT WAS SENT TO THE HANGAR AND DURING CHECK WERE DETECTED RT RMI FLAGS. AHRU NR 1 WAS REPLACED AND DURING WORKS THE SAME FAILURE APPEARED ON RT SIDE. AHUR NR 2 AND FLUX VALVE WERE REPLACED IAW 34-21-10 AND 34-21-06. AHRU NR 1 WIRING WAS CHECKED WDM 34-22-01. 2L72 4F4 FRTA6WE E2EA 20040915000932004091500093CE 2004 9 15 GUU2004F00025 120040628A55241016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO176954717808 UE189 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T3 TRTA24CE E2NE 20040915001092004091500109WP 2004 9 15 ASMF200407007 120040703A26218981501 EXTINGUISHER DOUG DC9 DC987 3022087WP PWA JT8 JT8D1 52044NE TAIL CONE ACTIVATED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23205AM2529893 49405 DURING TRANSIT CHECK, CAPTAIN REPORTED (EXTINGUISHER AGENT NR 1) LIGHT TURNED ON. FIRE EXTINGUISHER WAS DETECTED ACTIVATED BY HIGH TEMPERATURE IN TAIL CONE AND COMPRESSOR CLAMP WAS LOOSEN. FIRE EXTINGUISHER AND CLAMP WERE REPLACED IAW MM 26-20-00, LEAKS TEST CORRECT. DURING OVERNIGHT SERVICE, LEAKS CHECK WAS PERFORMED ON LT AUGMENTATION VALVE, LT FLOW CONTROL VALVE AND LT REGULATOR VALVE, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040915001132004091500113NM 2004 9 15 UIEA200400109 120040602A5414 SKIN BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE NR 4 NACELLE CRACKED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D-CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 4 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE AND EXPOSED WINDOW STRAP SURFACE ALONG WITH FASTENER HOLES, WERE HFEC INSPECTED TO ENSURE ABSENCE OF ANY CRACK OR OTHER DAMAGE. NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NAC STA .235 TO .254. RIB INSTALLATION AT NAC STA 248 WAS MODIFIED TO ACCOMMODATE NEW STEEL REPAIR ANGLES INSTALLATION ON NR 3 STIFFENER. AN ALUMINUM FILLER, FOR TRIMMED AREA OF INNER SKIN DOUBLER, WAS INSTALLED USING EXISTING NUT PLATE RIVETS. 2L74 4F4 F A20WE E23EA 20040915001192004091500119NE 2004 9 15 SWAA042642 220040912A72303400010220 BLADE BOEING737 7377H4 1384404NM CFMINTCFM567CFM567B2US 13802NE NR 2 ENGINE FOD A SWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW29707SA 27841 876538 AIR TURNBACK, DURING CLIMBOUT NOTICED A CONTINUOUS VIBRATION ON AIRCRAFT AND NR 2 ENGINE, VIBRATION METER AT 3 3/4. REDUCED POWER AND VIBRATION DECREASED. REMOVED AND REPLACED NR 2 ENGINE FAN BLADES NR 21 AND NR 9, PER MM. 2L72 4F4 FRTA16WE E2GL 20040915001212004091500121NM 2004 9 15 SWAA042644 120040912A5312BAC1518 STIFFENER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND VERTICAL STIFFENER AT BS 663, RBL 6, CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM. 2L72 4F RTA16WE 20040915001292004091500129 2004 9 15 UIEA200400148 420040814A34173751832 COMPUTER BOEING747 7472D7B 1384803NM NR 2 FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15524MC 21784 MIA/LAX - EN ROUTE AFTER LEAVING MIAMI THE F/O PRESSURE ALTIMETER FLUCTUATING UNCONTROLLABLE AND MACH INDICATOR FLAP ALTERNATELY COMING IN VIEW. WITH A DIFFERENCE IN MACH SPEED OF 6.5, CAPTAIN 79 MACH. F/O .19 MACH INDICATED. SUSPECT F/O CADS. REMOVED AND REPLACED CADC NR 2. OPS CHECK OK IAW REF MM 34-12-01. (M) 2L74 4F RTA20WE 20040915001302004091500130NM 2004 9 15 BJNA040809 120040825A5320BAC150529222 FLOOR SUPPORT BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 12 WITH LEVEL 2 CORROSION. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW BOEING 737 STRUCTURAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M) BJNA 2L72 4F RTA16WE 20040915001362004091500136NM 2004 9 15 BJNA040802 120040806A5330 SKIN BOEING737 737282 13844ATNM FUSELAGE CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT LOWER AFT CORNER OF R1 DOOR CUTOUT AT BS 344. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIG 26. (M) 2L72 4F RTA16WE 20040915001502004091500150NM 2004 9 15 AMTA200401067 120040821A3350 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT BROKEN A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11526AT 30735 EGRESS LIGHTS OUT AT ROWS 14-20. RETERMINATED WIRE AT ROW 14 IAW 33-51-01 WDM. OPS CHECK GOOD. (M) AMTA 2L72 4F RTA2NM 20040915001522004091500152NM 2004 9 15 USAABB04067 120040715A33501000679 LIGHT BOEING767 767201 1385125NM COCKPIT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19646US 23898 SNN - DUIRNG DAILY CHECK, MAINTENANCE FOUND THE FLIGHT DECK EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE L286 FLIGHT DECK EMERGENCY LIGHT ASSEMBLY IN ASSOCIATION WITH MM 33-51-01. PERFORMED SATISFACTORY OPERATIONAL CHECK IN ASSOCIATION WITH MM 33-51-00. (M) 2L72 4F RTA1NM 20040915001552004091500155EU 2004 9 15 USAABA04017 120040809A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19671UW 0323 PHL - EMERGENCY LIGHTS AT DOORS 1L, 4R AND 4L FAILED TESTING. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F RTA46NM 20040915001642004091500164EA 2004 9 15 A6WA200440119 120040824A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A A6WAO OTHER O OTHER DEDESCENT 1 GL31433AW 7289 LEFT WINDSHIELD SHATTERED FL20,000 DESCENT LEFT FORWARD PRESSURIZATION NORMAL. REPLACED LEFT WINDSHIELD PER AMM 56-11-01, LEAK AND OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20040916000072004091600007EA 2004 9 16 ASOA04439 120040619A5320601R31171178 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE LEFT INBOARD CLIP AND THE RIGHT INBOARD AND OUTBOARD CLIPS AT FS 484, BL 27 AND 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD CLIP AND THE RIGHT INBOARD AND OUTBOARD CLIPS AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040916000102004091600010EA 2004 9 16 ASOA04433 120040617A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD. (M) 2L72 4F RTA21EA 20040916000122004091600012 2004 9 16 USAABB04052 420040616A34256227999003 INDICATOR BOEING757 7572B7 1384964NM COCKPIT BURNED A USAAA UNSCHED LANDING BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CRCRUISE 1 EA19614AU38513 27145 IND - FLT 625 - AT CRUISE, FL350, CREW DETECTED STRONG ELECTRICAL ODOR. SHORTLY THEREAFTER, THE AIRCRAFT EXPERIENCED A LT ENGINE VIBRATION 3.8. AS THE CREW WAS TROUBLESHOOTING, THE F/O'S EHSI BEGAN TO FLICKER. CREW DECIDED TO DIVERT TO IND. EN ROUTE AND DESCENDING INTO IND, THE VIBRATION SUBSIDED AND THE ODOR ABATED. ON APPROACH, THE AIRCRAFT TOOK A LIGHTNING STRIKE. MAINTENANCE REPLACED THE F/O'S EHSI. FOR THE ENGINE VIBRATION, A CRACK WAS FOUND INT HE ELFT ENGINE SPINNER FAIRING, WHICH WAS REPLACED. (M) 2L72 4F RTA2NM 20040916000132004091600013NM 2004 9 16 USAABB04051 120040614A143011668411 NUT BOEING757 7572B7 1384964NM HEATER BURNED A USAAK NONE O OTHER ININSP/MAINT 1 EA19624AU 27245 CLT - WHILE ACCOMPLISHING A B-CHECK MAINTENANCE VISIT AN AREA OF DISCOLORATION ON THE CARGO LOADING JACKSCREW PAN OF THE AFT CARGO COMPARTMENT APPROXIMATELY 12-18 INCHES AFT OF THE FORWARD CARGO BULKHEAD WAS NOTED. FURTHER INVESTIGATION FOUND EVIDENCE OF A FIRE BELOW THE AFT CARGO COMPARTMENT FLOOR. THE IGNITION SOURCE OF THE FIRE APPEARS TO HAVE BEEN THE HEATER NUT ON THE HEATER FOR THE C-LAV FILL LINE. THE FAILED HEATER NUT APPEARS TO HAVE IGNITED THE ADJACENT FUSELAGE SKIN INSULATION BLANKETS SURROUNDING THE AFT LAVATORY SERVICE PANEL. MAINTENANCE REPAIRED ALL DAMAGED AREAS. THIS SYSTEM WILL BE DEACTIVATED ON ALL OF US AIRWAYS APPLICABLE AIRCRAFT. (M) 2L72 4F RTA2NM 20040916000142004091600014NE 2004 9 16 USAAEM04013 220040806A73204120T00P32 FADAC EMB ERJ170ERJ170100STD EU GE CF34 CF34* NE NR 1 ENGINE MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19811MD 17000028 FLT 1620 - ATL-PIT - ON CLIMB, CAPTAIN RECEIVED INDICATIONS OF NR 1 ENGINE POWER SURGE TEMPERATURE EXCEEDANCE AND FOUR FAULT MESSAGES. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE FADAC. PERFORMED GROUND RUN AND POWER ASSURANCE, NO DEFECTS NOTED. (M) 2L74 4F4 FRTA56NM E15NE 20040916000152004091600015EU 2004 9 16 2004F00311 120040427A2422WEF271500 INVERTER FOKKERF27 F27MK600 4990706EU NR 1 FAILED A COEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM13703FE 10420 NR 1 INVERTER FAILED IN FLIGHT AND WOULD NOT RESET. CRW ELECTED TO RETURN TO YVR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 INVERTER. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T A817 20040916000162004091600016NM 2004 9 16 USAABB04064 120040708A2497 WIRE HARNESS BOEING757 7572B7 1384964NM E/E COMPT CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 CLT - WHILE PERFORMING IN ROUTINE HYDRUALIC CHECK, FOUND BURNED WIRING ABOVE THE E2 RACK IN THE E/E COMPARTMENT. THREE WIRE BUNDLES WERE CHAFED AND ONE WIRE SHOWED SIGNS OF ARCING. MAINTENANCE ACCOMPLISHED REPAIRS PER THE SPWM AND ACCOMPLISHED US AIRWAYS EO 2404R92 TO ENSURE PROPER CLEARANCES TO PREVENT CHAFING. (M) 2L72 4F RTA2NM 20040916000172004091600017EU 2004 9 16 2004F00312 120040504A30301663214301 COMPUTER AIRBUS320 A320233 3930329EU PITOT HEAT FAILED A SOKFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23483TA 1509 SJO - FLT 631 - DURING CLIMB, ANTI-ICE ON NR 1 CAPTAIN PITOT PROBE WENT INOPERATIVE, AND AIRCRAFT RETURNED TO SAN JOSE. AT SJO, TECHS PERFORMED ANALYSIS PER AMM AND FOUND UNSERVICEABLE THE NR 1 PHC. NR 1 PHC WAS REPLACED PER AMM 30-31-34, AND AS PREVENTATIVE ACTION, REPLACED THE PITOT PROBE P/N C16195AA PER AMM 34-11-15. GROUND FUNCTIONAL CHECKS WERE SATISFACOTRY AND AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040916000182004091600018EU 2004 9 16 2004F00313 120040421A2910SD3736028 HOSE STBROSSD3 SD360 8100606EU HYD SYSTEM CRACKED A DATAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL13360SA SH3601 UPON BRAKE APP PRIOR TO MLG RETRACTION, FO HEARD A THUD. RETRACTED MLG NOTICED RT HYD IND ON CWP PRIOR TO ACCELERATION ALT. OBSERVED FALLING IND & HYD QTY GAUGE & 0 PRESSURE ON MAIN SYS PRESS GAUGE. CONTINUED TO CLIMB TO 2000 MSL. NORMAL EXTENSION FAILED. CONTACTED TOWER & ADVISED OF SITUATION. PERFORMED CLIMB CKS. REQUESTED VECTORS BACK TO SDF. PERFORMED 'LOSS OF CONTENTS' EMERGENCY CKLIST. REQUESTED A BOX BACK AROUND TO DISCUSS PROCEDURES FOR NO FLAP LANDING W/OUT BRAKES OR NWS. COMPLETED ALL CKS. APPROACH & LANDING WERE NORM. PROBLEM MEL'D IAW MEL 32-3. MEL 32-3 CLEARED ON 4/23/2004, NLG UPLINE HOSE R & R IAW SD3-60 MM. GEAR SWING OPS CK GOOD. LEAK CK GOOD. A/C RETURNED TO SERVICE. (M) 2H72 4T A41EU 20040916000222004091600022NE 2004 9 16 2004F00316 220040802A7260 LINE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE BYPASS FILTER OVERTORQUED A FX7AA UNSCHED LANDING WKJINADEQUATE Q C FLUID LOSS WARNING INDICATION CRCRUISE 1 SO1979749 22451 DURING CRUISE FLIGHT, ENGINE NR 3 OIL QUANTITY WENT OT ZERO FOLLOWED BY A LOSS OFF OIL PRESSURE AND INCREASE IN OIL TEMP. ACCOMPLISHED PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE AND DIVERTED TO SVMI. LANDED WITH NO INCIDENT, TROUBLESHOOT AND FOUND OVERTIGHTENED FILTER BYPASS PRESSURE PORT ON MAIN ENGINE OIL FILTER HOUSING. ACCOMPLISHED GEARBOX HOUSING BOSS THREAD REPAIR AS PER ENGINE MANUAL PWA 72-61-01, RAN ENGIEN LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F4 F A3WE E2EA 20040916000232004091600023SO 2004 9 16 SIMA200422407 120040731A53151452246013 FLOORBEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21729AE 145343 ABI - DURING AN IMBV INSPECTOIN, MAINTENANCE FOUND FLOORBEAM CORROSION IN CENTER FUSELAGE. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A REPAIR ANGLE, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-10 FIGURE 201. (M) 2L72 4F RTT00011AT 20040916000242004091600024NM 2004 9 16 USAABB04073 120040802A335020121 CHARGER BOEING767 767201 1385125NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19648US 23900 PHL - FOUND FLOOR LEVEL EMERGENCY LIGHTS FROM ROWS 21 THROUGH 26 RIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M) 2L72 4F RTA1NM 20040916000252004091600025NM 2004 9 16 USAASB04102 120040729A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19775AU 24933 PHL - MAINTENANCE REPORTED THE LEFT FORWARD ENTRY DOOR EMEGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040916000262004091600026SO 2004 9 16 SIMA200421903 120040805A3350 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21673AE 145797 ROC - FLT 4399 - CREW FOND THE FORWARD EMERGENCY LIGHTS INOPERATIVE ON THE PREFLIGHT INSPECTION. REPLACED NR 1 AND PACK NR 2 EMERGENCY BATTERY PACK AND NR 2 EMERGENCY BATTERY CHARGER ASSEMBLY IAW EMB 145MM 33-50-04. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM WITH NO DISCREPANCIES NOTED. A/C RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040916000282004091600028NE 2004 9 16 AMTA200400996 220040805A7200 TAPE BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE PEELING A AMTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL11550TZ 32584 FOUND RT ENGINE SURGE +- 10 EPR, +-5N1, +-20 EGT AND RISING EGT DURING CRUISE AND DESCENT (EAI ON AND OFF). EECS TURNED OFF PER MAINTENANCE CONTROL RT ENGINE RETURN TO NORMAL. FOUND TAPE PEELED OFF OF MISSING PF RAKE, RETAPED REF AMM 77-11-04-2, OPS CHECK GOOD AT VARIOUS POWER SETTINGS. (M) 2L72 4F4 FRTA2NM E12EU 20040916000292004091600029NM 2004 9 16 USAA040402 120040726A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19511AU52228 23594 PIT - FOUND FRAME DENTED 1 INCH BY 2 INCH, FRAME AT AFT CARGO AT STATION 827 BETWEEN STRINGER 24L AND 25L. CUT OUT DAMAGE AND INSTALLED DOUBLER PER TR 53-60-07. (M) 2L72 4F RTA16WE 20040916000312004091600031EU 2004 9 16 2004F00319 120040229A25603011790000999 ELECTRODE AIRBUSA319 A319112 3930323EU AED MISSING A USAAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 EA19716UW1920 1055 FLT 781 - DIVERTED DUE TO A MEDICAL EMERGENCY. ATTEMPTED TO USE THE AED, DISCOVERED BOTH ELECTRODES WERE MISSING. CARRIER COULD NOT DETERMINE WHAT HAPPENED TO THE ELECTRODES. REPLACED AED. (M) 2L72 4F RTA28NM 20040916000322004091600032CE 2004 9 16 2004F00320 120040714A2612 FIRE LOOP CESSNA208 208B 2073701CE ENGINE LOOSE A COEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM13880FE 208B0215 ENGINE FIRE LIGHT AND HORN CAME ON IN LEVEL FLIGHT. INDICATIONS CEASED ON APPROACH TO LANDING. ALL OTHR INDICATIONS NORMAL. PILOT DECLARED AN EMERGENCY. AIRCAFT LANDED WITHOUT INCIDENT. PILOT NOTED THAT NO FIRE EXISTED AND IT WAS A FALSE INDICATION. MECHANIC FOUND FIRE WIRE HAD COME OUT OF A BRACKET AND WAS LAYING ON ENGNE GEARBOX. FIRE WIRE WS RESECURED OT BRACKET AND THE FIRE SYSTEM CHECKED GOOD. THERE WAS NO FURTHER INDICATION DURING THE NEXT 7 DAYS. (M) 1H71 3T A37CE 20040916000342004091600034 2004 9 16 USAASA04031 420040331A256565757101 PUSH-PULL CABLE AIRBUS320 A320214 3930316EU OVERWING SLIDE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19115US 1171 THE LEFT OVERWING SLIDE CYLINDER HAS A BROKEN PUSH/PULL CABLE. MAINTENANCE REPLACED THE LEFT OVERWING SLIDE CYLINDER ASSEMBLY. OK FOR SERVICE. (M) 2L72 4F RTA28NM 20040916000352004091600035NM 2004 9 16 GAIA04088OP 120040717A33501000679 LIGHT BOEING727 727251 138408HNM L1 DOOR INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07279US 21158 L1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT ILGHT. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040916000372004091600037EU 2004 9 16 2004F00321 120040817A2121EVT3454H FAN AIRBUS320 A320233 3930329EU E/E BAY STUCK A RJEFA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO23486TA 1730 DURING CRUISE, VIBRATION UNDER CABIN FLOOR TO AFT GALLEY AREA, & BURNED ODOR AROUND COCKPIT & FORWARD GALLEY AREA FELT. AS PREVENTATIVE ACTION CREW OXYGEN USED. ECAM MESSAGE OF VENT BLOWER FAULT CAME ON. A/C DEVIATED FROM ITS NORMAL SCHEDULE FLT TO CUL. AFTER LANDING AT CUL STATION, INSPECTION OF AVIONICS VENTILATION SYS PERFORMED PER AMM & ALSO BITE TEST OF THE AEVC SYS PER AMM. FOUND THE VENT BLOWER STUCK & THE AEVC COMPUTER WITH FAULTY RESPONDED TO TEST, BOTH UNITS HAVE BEEN REPLACED & VENT BLOWER TESTED PER AMM, & AEVC TESTED PER AMM. RESULTS WERE SATISFACTORY. NO MORE A/C VIBRATION WAS FELT, NOR EVIDENCE OF BURN ODOR. TRANSIT DAILY CHECK WAS PERFORMED & AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040916000392004091600039NM 2004 9 16 USAA040401 120040808A5230 STRUCTURE BOEING737 737301 1384611NM CARGO DOOR TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US50329 23935 PIT - FOUND CARGO DOOR WITH TORN LIGHTENING HOLE, FORWARD DOOR. FABRICATED DOUBLER PER TR 52-30-09. (M) 2L72 4F RTA16WE 20040916000412004091600041 2004 9 16 2004F00322 420040803A61228210209E GOVERNOR STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA RT PROPELLER INOPERATIVE A DATAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 GL13167RC SH3038 HEARD AN ENGINE NOISE, SOUND CHANGE FROM RT ENGINE & CKD STATUS OF ENGINE & PRIMARY INSTURMENTS. RT ENGINE TORQUE GOING PAST REDLINE & INCREASING. ITT INCREASED SLIGHTLY THEN DROPPED TO 450 & DECREASING. CAPTAIN DECREASED RT ENGINE TORQUE 200 NR'S AT FIRST & TORQUE CONTINUED TO INCREASE EVEN AFTER TORQUE REDUCTION OF 600 NR WHILE ITT STILL DECREASING. NG & PROP RPM STABLE & FUEL FLOW & OIL TEMPS NORMAL. PERFORMED VITAL ACTIONS ENGINE CHECKLIST & PERFORMED SUBSEQUENT ACTIONS CHECKLIST. A/C LANDING WITH 1 ENGINE SHUTDOWN, BUT DIDN'T DECLARE AN EMERGENCY. EMERGENCY VEHICLES ON STANDBY. A/C LANDED WITHOUT INCIDENT. MECHANIC R & R PROP GOVERNOR IAW MM. OPS CK GOOD & A/C RETURNED TO SERVICE. (M) 2H72 4T4 T A41EU E4EA 20040916000422004091600042CE 2004 9 16 2004F00323 120040616A7500130936P4MCO600 TUBE BEECH 200 200BEECH 1152920CE LT BLEED AIR LEAKING A G1IAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL0125KA BB783 LEFT ENGINE BLEED AIR LIGHT ILLUMINATED IN FLIGHT. RETURNED TO DEPARTURE POINT AT FAIRBANKS. (M) 1L72 4T A24CE 20040916000432004091600043NM 2004 9 16 AMTA200400939 120040723A3244 TIRE BOEING757 75723N 1384973NM NR 7 FAILED A AMTAO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 GL11519AT 27975 NR 7 MAIN TIRE TREAD SEPARATED FROM TIRE. REMOVED AND REPLACED TIRE PE AMM 32-45-01-4. (M) 2L72 4F RTA2NM 20040916000442004091600044NE 2004 9 16 AMTA200400912 220040722A7250 SWITCH BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RT ENGINE FAILED A AMTAK NONE J WARNING INDICATION ININSP/MAINT 1 GL11552TZ 32586 RT TURB OVERHEAT DET 2 STATUS MESSAGE DISPLAYED. COMPLIED WITH FIM 26-13-00 FIG 104 AND FIG 103. REPLACED RIGHT ENGINE TURBINE COOLING OVERHEAT SWITCH NR 2. REF MM 26-13-01-4, OK FOR SERVICE. (M) 2L72 4F4 FRTA2NM E12EU 20040916000462004091600046NM 2004 9 16 AMTA200400922 120040726A3350 SOCKET BOEING757 75723N 1384973NM EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 FOUND 9 DEF EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT SOCKET ASSEMBLY IAW MM 33-51-11-403-059. (M) 2L72 4F RTA2NM 20040916000482004091600048NM 2004 9 16 AMTA200400977 120040804A5315 FLOORBEAM BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND AFT CABIN FLOOR SUPPORT BEAM AT FS 1681 FROM BL 0 TO RT DOOR SILL HAS EXFOLIATION CORROSION. CUT OUT DAMAGED SECTION AND FABRICATE AND INSTALLED DOUBLER REPAIR IAW B757 SRM 53-60-51. (M) 2L72 4F RTA2NM 20040916000492004091600049NM 2004 9 16 AMTA200400976 120040804A5320 FLOOR SUPPORT BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11514AT 27971 FOUND AFT CABIN FLOOR SUPPORT AT BL 0 FROM FS 1641 TO FS 1661 HAS EXFOLIATION CORROSION. CUT OUT DAMAGE SECTION, FABRICATION ANGLE, TREATED, ALODINED AND PRIMED, INSTALLED IAW B757 SRM 51-70-11, 51-20-01, 51-40-02. (M) 2L72 4F RTA2NM 20040916000512004091600051NM 2004 9 16 AMTA200400964 120040731A5321 FLOOR PANEL BOEING757 75733N 1384931NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11551TZ 32585 FOUND CORROSION ON FLOOR PANELS IN AFT CARGO PIT FROM STATION 1290 TO 1380. PANEL FABRICATED FROM PO 9601085027 2024 T3 .071. PANEL TO BE INSTALLED ON NR 1073 ITEM NR 2 ON M12A. TREATED AND PRIMED IAW SRM 51-21-02. (M) 2L72 4F RTA2NM 20040916000522004091600052EA 2004 9 16 ASOA04537 120040802A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11886AS 7531 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT FS 280, RBL 9. (M) 2L72 4F RTA21EA 20040916000542004091600054 2004 9 16 SWAA042647 420040912A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916000562004091600056NM 2004 9 16 SWAA042649 120040913A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20040916000582004091600058NM 2004 9 16 SWAA042620 120040909A531165650568 FRAME BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 994, RBL 44, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040916000602004091600060NM 2004 9 16 SWAA042652 120040913A53156545812 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT 328, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040916000622004091600062NM 2004 9 16 SWAA042630 120040910A57536546434301 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29610WN 27696 DURING SCHEDULED C3 CHECK, FOUND LT WING T/E AFT INBOARD FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20040916000642004091600064NM 2004 9 16 SWAA042632 120040910A57436549442 LINK BOEING737 7373A4 1384585NM RT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND RT WING STABILIZER LINK BETWEEN MAIN GEAR BEAM AND REAR SPAR, CORRODED. REMOVED AND REPLACED RT WING STABILIZER LINK PER MM. 2L72 4F RTA16WE 20040916000662004091600066NM 2004 9 16 SWAA042611 120040908A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040914000582004091400058WP 2004 9 14 DHL2004804529 120040725A5751 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RT WING AILERON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR. 0848: REPAIR OF DENT AND BROKEN CRACK TO RT WING IB AILERON UPPER PLATING AT XW 563.000 PERFORMED MAJOR REPAIR IAW ED-EDW 27-1, DWG W27-R01 REV IR. REMOVED EXISTING FASTENERS ON AREA IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. TRIMMED OUT DAMAGED AREA IAW DWG W27-R01, EDW 27-1. FABRICATED FILLER AND DOUBLER (AL 2024-T3 0.050) IAW DWG W27-R01, ED EDW 27-1. CLEANED, TREATED AND PRIMED AREA AND FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW DWG W27-R01, ED EDW 27-1, SRM 51-1-21 PG.1. FOR IB AILERON REBALANCE SEE NR 0896. FOR OPS CHECK SEE NR 0794. 2L74 4F4 FRT4A25 E2GL 20040914000632004091400063WP 2004 9 14 DHL2004804528 120040725A5751 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RT WING AILERON BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 RT WING OB AILERON LWR. SKIN DOUBLER BROKEN 0.250, XA 615.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDW 27.2, DWG W27-R02, REV 1R. REMOVED DAMAGED DOUBLER IAW DWG W27-R02, ED EDW 27.2. TRIMMED OUT PLATING SEGMENT(DAMAGED) IAW DWG W27-R02, ED EDW 27.2. FABRICATED FILLER AND DOUBLER (AL 2024-T3 0.050) IAW DWG W27-R02, ED EDW 27.2. CLEANED, TREATED AND PRIMED AREA, FILLER AND DOUBLER INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLER AND DOUBLER IAW DWG W27-R02, ED-EDW 27.2, SRM 51-1-21 PG.1-2. FOR REBALANCE SEE NR 0896. 2L74 4F4 FRT4A25 E2GL 20040914000932004091400093SO 2004 9 14 513041 120040513A8011MHB4014 STARTER PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2A GL RT ENGINE INOPERATIVE E LATAO OTHER O OTHER TXTAXI/GRND HDL 1 AL0346FA 1 1 INSTALLED NEW STARTER ON RT ENGINE. INITIAL START OF ENGINE NORMAL. AS A/C ATTEMPTED TO DEPART ITS FIRST DESTINATION, THE STARTER BENDIX WOULD SPIN BUT NOT ENGAGE THE FLYWHEEL. REPLACED BENDIX WITH SERVICEABLE ASSY. THIS IS THE SECOND SUCH FAILURE, STARTER BENDIX WE HAVE EXPERIENCED WITHIN THE FIRST THREE STARTS OF OPERATION. 1L72 3O3 O A20SO E14EA 5 CP33EA 20040914000992004091400099NM 2004 9 14 DHL2004745556 120040814A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING AN A-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; FUSELAGE SKIN REPAIR AT STA.441, STR.26R DOSE NOT COMPLY WITH SRM. REMOVED EXISTING FUSELAGE SKIN REPAIR AT STA.441 AND STR.26R, AND INSPECTED CUT-OUT OF SKIN,(4.8750 INCH X 1.5 INCH) IAW SRM 51-30-02, NDT MAN PART 6 51-00-00 FIG 23, FABRICATED AND INSTALLED NEW DOUBLER AND STRUCTURAL FILLER ON FUSELAGE SKIN AT STA.441 AND STR.26R IAW SRM 53-30-3 FIG.24 AND DWG.597-R01 REV.A W/8110-3 DATED 08-17-04. DOUBLER: 14 INCH X 10 INCH FROM 2024-T3 0.090 MATERIAL P.O.900755 AND STRUCTURAL FILLER: 16 INCH X 7 INCH, FROM 2024-T3 0.071 MATERIAL P.O. 900781. 2L73 4F4 F A3WE E2EA 20040914001042004091400104EU 2004 9 14 KBM2004F00168 120040722A7931704A47270101 GAUGE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE OIL PRESSURE READS LOW E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 OIL PRESSURE GAUGE READS LOW. REPLACED CLUSTER GAUGE WITH REPAIRED UNIT. 1G71 3U3 U H9EU E19EU 20040914001102004091400110EU 2004 9 14 KBM2004F00204 120040511A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 T/R HALF SHELLS WORN. REMOVED AND REPLACED 1G71 3U3 UNCH9EU E19EU 20040914001272004091400127CE 2004 9 14 ZSEA52504 120040525A212157033 FAN CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE COCKPIT FAILED E ZSEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 CE01555KT 1290 5500420 APPROXIMATELY 15 MILES FROM AIRPORT ON A FLIGHT, COCKPIT AND CABIN INDICATED SIGNS OF SMOKE/ FUMES WITH ELECTRICAL ODOR. ALL FANS WERE SHUTDOWN AND CHECKLISTS COMPLETED. WITHIN A COUPLE OF MINUTES, AIR BEGAN TO CLEAR AND LANDING WAS MADE A FEW MINUTES LATER. 2210 HOURS OF AC FLIGHT TIME REMAINED BEFORE SCHEDULED REPLACEMENT. 1L72 4F4 F A22CE E1NE 20040914001352004091400135NM 2004 9 14 ASMF200407017 120040714A71105930645501 COWLING DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT NOSE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23881LF8448 53051 725543 DURING TRANSIT CHECK WAS DETECTED A STRIKE ON LT NOSE COWLING OUT OF LIMITS. IT WAS 2 INCHES WIDE AND 3 INCHES LARGE, 0.335 INCHES DEEP. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE COWLING WAS REPLACED IAW MM 71-10-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20040914001382004091400138NM 2004 9 14 ASMF200407021 120040718A29105916460 CONTROL VALVE DOUG MD80 MD83 3023681NM PWA JT9 JT9D* NE HYD SYSTEM LEAKING W ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW23881LF 53051 DURING TRANSIT CHECK, HYDRAULIC LEAK WAS DETECTED ON RT LANDING GEAR CONTROL VALVE. LEAK WAS DETECTED ON CONTROL VALVE NIPPLE AND PRESSURE LINE. RT LANDING GEAR CONTROL VALVE WAS REPLACED IAW MM 32-32-01 AND IT WAS PERFORMED EXTENSION AND RETRACTION LANDING GEAR TEST IAW MM 32-32-01 AND 32-30-00, ALL CORRECT. 2L72 4F4 FRT E20EA 20040914001432004091400143EA 2004 9 14 SWIA200413597 120040719A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07440SW6038 6038 7589 HSTCU FAULTS IN MDC. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW AMM 27-42-01 AND HORIZONTAL STAB TRIM MOTOR CONTROL UNIT IAW AMM 27-42-05, OPERATIONAL CHECK GOOD. HSTCU P/N 7062-3, S/N OFF 831. 2L72 4F4 FRTA21EA E15NE 20040914001482004091400148SO 2004 9 14 HFB2004F00001 220040709A7261510010655 LINE CESSNA414 414A 2075907CE CONT O520 TSIO520* 17040SO OIL PRESSSURE CORRODED B HFBRO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03812SR4957 414A0326 LT ENGINE LOST OIL PRESSURE. OIL PRESSURE LINE IN LT SIDE PANEL BY PILOTS LT LEG HAD CORROSION HOLE IN IT. APPROXIMATELY 5 WEEKS LATER LT ENGINE LOST OIL PRESSURE AGAIN. OIL PRESSURE LINE UNDER FLOOR UNDER PILOTS SEAT HAD CORROSION HOLE IN IT. 1L72 3O3 O A7CE E8CE 20040914001532004091400153NM 2004 9 14 UIEA200400114 120040617A215071923811 ACM BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE NR 3 UNSERVICEABLE A UIEAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 EA15517MC 23300 AFTER TAKEOFF, NR 3 AIR CONDITIONING PACK STARTED MAKING LOW RUMBLING SOUND. SMELLED BURNING ODOR, TURNED NR 3 PACK OFF FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 3 AIR CYCLE MACHINE. GROUND OPERATION CHECK NORMAL IAW MM. 2L74 4F4 F A20WE E23EA 20040914001692004091400169 2004 9 14 ASMF200406035 420040630A3421 INDICATOR DOUG DC9 DC987 3022087WP COCKPIT FAILED W ASMFD RETURN TO BLOCK JG WARNING INDICATION MULTIPLE FAILURE TXTAXI/GRND HDL 1 SW23204AM3450 49404 AIRCRAFT RETURNED TO PLATFORM, AHRS AND FLIGHT DIRECTOR BUSES FAILED, (SIF) LIGHT TURNED ON, N2 INDICATION OUT OF LIMITS AND N1 INDICATION INOPERATIVE. CIRCUIT BREAKERS B5, F1, C11, F8, C1 AND F12 WERE TESTED IAW MM, ALL CORRECT. CIRCUIT BREAKERS C13, C4, C12, C3, E9, E21, E20, E8, C1, C2, C10 AND C11 WERE TESTED IAW MM. PS4 LINE WAS CLEANED AND ENGINE WAS RUNNING IAW MM 73-12-02, TEST CORRECT. N1 GENERATOR INDICATION WAS CHECKED, ALL CORRECT. DURING OVERNIGHT SERVICE, AHRS WAS REPLACED IAW MM, FD WITH STP AND STALL SYSTEM TESTS WERE PERFORMED IAW MM, RESPECTIVELY, ALL CORRECT. RT ENGINE TRIM WAS PERFORMED AND LT ENGINE INDICATION, ADJUSTMENT AND TEST WERE PERFORMED IAW MM, ALL CORRECT. 2L72 4F RTA6WE 20040914001742004091400174WP 2004 9 14 ASMF200407001 120040701A32463910097543 WHEEL DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE NLG DAMAGED W ASMFO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW23803ML3389 49726 DURING TRANSIT CHECK, CAPTAIN REPORTED STRONG VIBRATION IN NOSE LANDING GEAR. BOTH NOSE LANDING GEAR WHEEL WERE REPLACED IAW MM 32-40-00, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040914001752004091400175WP 2004 9 14 ASMF200407002 120040701A27601040T1005 ACTUATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE SPOILER DAMAGED W ASMFK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SW23505MD 49149 DURING OVERNIGHT SERVICE, GROUND SPOILER WAS DETECTED OUT OF SERVICE, AUTO SPOILER ACTUATOR WAS REPLACED AND SPOILER TRIMMING WAS PERFORMED AND TESTED AND FAILURE CONTINUE. OPERATIONAL TEST WAS PERFORMED AND BARS WERE ADJUSTED AND BUSHING AND ACTUATOR WERE REPLACED IAW MM 27-62-05 AND 27-60-00, RESPECTIVELY, TEST CORRECT. 2L72 4F4 F A6WE E2EA 20040914001972004091400197EU 2004 9 14 JGV2004F00004 120040709A2830142G1243 VALVE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE73160 NE FUEL DRAIN CRACKED B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE09128M 276 FUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPERATURE AT WELDING TIME. RECOMMEND NO SCREENS. 2L73 4F4 F A46EU E1NM 20040915000072004091500007NM 2004 9 15 AWXA200400991 120040905A52106523464 SNUBBER BOEING737 7373G7 1384595NM R-1 DOOR WEAK A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28308AW 24710 C-14 CHECK, DURING FUNCTIONAL CHECK OF PASSENGER DOOR SYSTEM FOUND THE R-1 DOOR SNUBBER WEAK. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR SNUBBER IAW AMM 52-41-71, PG. 1-3. 2L72 4F RTA16WE 20040915000142004091500014NM 2004 9 15 UPS04243068 120040823A5320 STRAP BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU FLOOR PANEL CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C ON INSP FLOOR PANEL SPLICE STRAP FOUND BADLY CORRODED AT BS 520 BETWEEN RBL 24 AND LBL 24. SPLICE STRAP REPLACED IAW SRM 51-20-01 2L73 4F4 F A3WE E25NE 20040915000192004091500019EU 2004 9 15 AWXA200400978 120040814A5347D53371110000 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND IN NUMEROUS PLACES ON LT IB SEAT TRACK BS 16408 TO BS 17255, FR 37 TO FR 39. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 LT FROM FR 37 TO FR 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F4 FRTA28NM E311NE 20040915000272004091500027GL 2004 9 15 C2XA04CL072 220040713A726123070366 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE LEAKING A C2XAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW27265455701 5701 145558 CAE312047 THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN ON CLIMB. THEY ALSO REPORTED A LAV SMOKE LITE WARNING. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040915000472004091500047NM 2004 9 15 ABXA040317 120040901A3260 LAMP BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE MLG INDICATOR INOPERATIVE A ABXAO OTHER L NO TEST APAPPROACH 1 GL23709AX 22572 LT MAIN GEAR DOWN (GREEN) INDICATION LIGHT INOPERATIVE. LIGHT INOPERATIVE WITH TEST BUTTON PUSHED. CREW PERFORMED A GO AROUND AT EWR. RELAMPED LT MAIN GEAR DOWN GREEN INDICATOR LIGHT AND RT MAIN GEAR DOWN GREEN INDICATOR LIGHT. OPS CHECKED OK. 2L72 4F4 FRTA1NM E3NE 20040915000512004091500051NM 2004 9 15 04FDEA02626 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 SNRM N0454: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000652004091500065NM 2004 9 15 UPS04443040 120040819A5347BAC1520792 SEAT TRACK BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D- BS 420-440 LBL 36 INCH SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 4 INCHES, EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPLACED IAW SRM 51-10-01 PG 8. AND CIC APPLIED IAW EO NR M-5100-2780E. 2L74 4F4 FRTA20WE E3NE 20040915000662004091500066NM 2004 9 15 UPS04443041 120040819A5347BAC1520792 SEAT TRACK BOEING747 747212B 1384886NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D BS 420-460 LBL 56 INCHES SEAT TRACK CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 2 INCH X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPLACED IAW SRM 51-10-01 PG 8, AND CIC APPLIED IAW EO NR M-5100-2780E. 2L74 4F4 F A20WE E3NE 20040915000692004091500069NM 2004 9 15 UPS04443044 120040819A5347 SEAT TRACK BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C U/D BS 613 RBL 9 INCHES, SEAT TRACK LIP 2EA BROKEN. U/D BS 610-650 RBL 9 INCHES, SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 4. 2L74 4F4 FRTA20WE E3NE 20040915000762004091500076EU 2004 9 15 AWXA200400969 120040814A5347D5337111200100 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK CORROSION WAS FOUND IN NUMEROUS AREAS OF RT OB SEAT TRACK Y1292, BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED RT OB SEAT TRACK Y1292, FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040915000862004091500086SO 2004 9 15 MUY2004F00000 120040714A2917587847 PRESSURE SWITCH PIPER PA32 PA32301T 7103209SO LYC O540 IO540* 41532EA HYD SYSTEM LEAKING E MUYAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL114355Y3 32R8429012 HYDAULIC PRESSURE SWITCH LEAKS INTERNALLY. LEAK IS VERY SLOW. OVER AN EXTENDED PERIOD OF TIME, HYDRAULIC RESEVOIR IS DEPLETED. LACK OF HYDRAULIC FLUID IN RESEVIOR CAUSED LT MAIN GEAR TO REMAIN UNSAFE DURING APPROACH AND LANDING. COMPONENT IS SEALED UNIT AND CNA NOT BE DISASSEMBLED TO DETERMINE CAUSE OF FAILURE. WHEN COMPONENT WAS PLACED ON TEST BENCH IT STARTED LEAKING AT 1000 PSI. RECOMMEND REGULAR INSPECTION INTERVAL TO DETECT SEEPAGE BEFORE LEAKS BECOME LARGE ENOUGH TO CAUSE ABOVE STATED FAILURE. (GL11200412252) (INC 1GL112004068) 1L71 3O3 O A3SO 1E4 20040915000992004091500099EA 2004 9 15 G1I2004F00001 220040722A8597 WIRE PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA ENGINE BROKEN D G1IAO OTHER O OTHER NRNOT REPORTED 1 AL01254SW 31715 L896581A AIRCRAFT LOST ELECTRICAL POWER. FOUND FIELD WIRE BROKEN AT RING TERMINAL WHERE WIRE ATTACHES TO LT ALTERNATOR. INSTALLED NEW RING TERMINAL ON WIRE AND REATTACHED TO ALTERNATOR. PROBABLE CAUSE OF FAILURE IS AGE AND VIBRATION. RECOMMENDED DETAILED INSPECTION OF ENGINE ELECTRICAL WIRING DURING ANY SCHEDULED MAINTENANCE WHEN COWLING IS REMOVED. (AL01200404501) 1L72 3O3 O A20SO E14EA 20040915001022004091500102NE 2004 9 15 ASMF200407005 220040703A73205010224A PUMP BOEING757 757200 1384950NM PWA 2037 PW2037 NE FUEL SYSTEM FAILED W ASMFK NONE M OVER TEMP ININSP/MAINT 1 SW23703AM27450 27203 726733 DURING TRANSIT CHECK, CAPTAIN REPORTED HIGH TEMPERATURE ON ENGINE NR 2 REACHED 648 DEGREES (F) DURING TAKE OFF. THE MAXIMUM TEMPERATURE IAW MM 71-00-01 IS 645 DEGREES (F), SO AIRCRAFT WAS SENT TO THE HANGAR AND RT ENGINE FUEL PUMP AND PURGE VALVE WERE REPLACED IAW MM 73-11-01 AND 75-32-03, RESPECTIVELY, TESTS CORRECT. 2L72 4F4 FRTA2NM E17NE 20040915001152004091500115SO 2004 9 15 G1I2004F00002 120040722A2420 BELT PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA RT ENG ALTERNATODISPLACED D G1IAO OTHER O OTHER NRNOT REPORTED 1 AL01254SW 31715 RL301261A AIRCRAFT LOST ELECTRICAL POWER. FOUND RT ENGINE ALTERNATOR BELT NOT ON THE PULLEY SYSTEM. REINSTALLED AND CORRECTLY TENSIONED ALTERNATOR BELT, OPS CHECK OF ELECTRICAL SYSTEM GOOD. PROBABLE CAUSE IS IDLER PULLEY BECAME LOOSE ALLOWING THE ALTERNATOR BELT TO JUMP OFF OF PULLEY SYSTEM. RECOMMEND THAT ALTERNATOR BELT TENSION BE CHECKED AT ALL SCHEDULED MAINTENANCE OF ENGINE. (AL01200404502) 1L72 3O3 O A20SO E14EA 20040915001252004091500125NM 2004 9 15 BJNA040803 120040812A5320BAC1505100361 INTERCOSTAL BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 306 LBL 12. REMOVED AND REPLACED FLOORBEAM INTERCOSTAL AT BS 306 LBL 12 IAW THE STRUCTURAL REPAIR MANUAL 53-30-2. (M) 2L72 4F4 FRTA16WE E2EA 20040915001372004091500137NM 2004 9 15 BJNA040804 120040813A5320BAC150519222 FLOOR SUPPORT BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-19222 IAW THE BOEING 737 STRUCTRUAL REPAIR MANUAL 51-10-1, 51-20-1 FIG 2 AND 51-30-5. INSTALLED IAW 51-30-2. (M)BJNA 2L72 4F RTA16WE 20040915001442004091500144EA 2004 9 15 2004F00345 120040118A3260840534 SQUAT SWITCH CNDAIRCL600 CL6002B16 1900305EA MLG DEFECTIVE A AJCAO OTHER J WARNING INDICATION CLCLIMB 1 EA25224F 5163 AIRCRAFT DEPARTED DMDW EN ROUTE TO KTEB, AFTER TAKEOFF THE GEAR FAILED TO RETRACT AND THE WEIGHT ON WHEELS INPUT FAIL LIGHT ILLUMINATED. THE CREW CONSULTED THE ABNORMAL PROCEDURES MANUAL AND USED THE MANUAL OVERRIDE TO RETRACT THE GEAR. ALL OF THE GEAR RETRACTED NORMALLY. THE A/C CONTINUED ONTO KTEB THE GEAR EXTENSION WAS NORMAL WITH 3 GREEN DOWN AND LOCKED LIGHTS AND THE LANDING WAS UNEVENTFUL. THE CREW DID NOT DECLARE AN EMERGENCY. UPON INVESTIGATION IT WAS DETERMINED THAT THE NR 1 OBD MAIN LAINDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH WAS DEFECTIVE. REMOVED AND REPLACD THE SWITCH IAW SP 601-2 MM CHAP 32-05-15. PERFORMED SATISFACTORY WOW FUNCTIONAL TEST IAW PS601601-2 MM, CHP 32-05-11. THE AIRCRAFT 2L72 4F RTA21EA 20040915001512004091500151NM 2004 9 15 AMTA200401071 120040822A2612 WARNING LIGHT BOEING757 75733N 1384931NM NR 1 ENGINE ILLUMINATED A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11561TZ 33526 EICAS STATUS MESSAGE L STRUT OH DET 1 DISPLAYED. PERFORMED FIM 26-12-00 BLOCK 1 NO DEFECTS ALSO RAN NR 1 ENGINE FOR SEVERAL MINUTES. (M) 2L72 4F RTA2NM 20040915001532004091500153NM 2004 9 15 USAASB04110 120040814A335020121 CHARGER BOEING737 737401 1384701NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19424US 23991 PHL - MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS AT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040915001602004091500160CE 2004 9 15 2004F00350 120040626A561010138402523 WINDSHIELD BEECH 1900 1900C 1154161CE COCKPIT CRACKED A FFSAO OTHER O OTHER CRCRUISE 1 AL01575Z 6124 UC136 PILOT'S OUTER WINDSHIELD PANE CRACKED. CRACKING OCCURRED DURING THE CRUISE PHASE OF THE FLIGHT AT FL 240 WITH WINDSHIELD HEAT ON. CRACKS DEVELOPED FROM LOWER INBOARD CORNER OF WINDSHIELD AND SPREAD UPWARD AND ACROSS THE AREA INCORPORATING THE HEATING ELEMENTS. (M) 2L72 4T RTA24CE 20040915001622004091500162EA 2004 9 15 ASOA04530 120040726A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14L/R WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625, NEAR STRINGERS 14 L/R IAW ASA EO 600-53-0174. (M) 2L72 4F RTA21EA 20040915001682004091500168NM 2004 9 15 SWAA042558 120040901A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED PM CHECK, FOUND AFT EMERGENCY EXIT OVERHEAD LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. SWAA (M) 2L72 4F RTA16WE 20040916000032004091600003NM 2004 9 16 2004F00354 120040721A5347BACB15201566718TSEAT TRACK BOEING747 7472D7B 1384803NM FUSELAGE CRACKED A T64RK NONE O OTHER ININSP/MAINT 1 SO03524MC 21784 DURING FA12 A-CHECK ACCOMPLISHING ROUTINE WORK CARD 02EM15002 INSPECTION OF MAIN CABIN FOUND MAIN CARGO DECK LEFT OUTBOARD FLOOR TRACK BROKEN OUT AT FUSELAGE STATION 1820. (M) T64R 2L74 4F RTA20WE 20040916000052004091600005NE 2004 9 16 2004F00357 120040804A53437620902018041 FITTING SKRSKYS76 S76 8143010NE NLG BROKEN A ALGAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW03705AL 760267 ON DEPARTURE HEARD LOUD BANG AS LANDING GEAR WAS RETRACTED. THE NOSE GEAR WOULD NOT LOCK IN THE UP POSITION, RETURNED TO HMA AND MAINTENANCE FOUND THE DOOR STRUT FITTING BROKEN. MAINTENANCE CONFIRMED THAT LANDING GEAR WAS DOWNED AND LOCKED AND FOUND FITTING P/N 76209-02018-043 WAS BROKEN ON THE NOSE GEAR. REPLACED FITTING AND NOSE GEAR STRUT. (M) 1G72 3U H1NE 20040916000062004091600006SW 2004 9 16 2004F00358 120040707A7100 COMPRESSOR BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL ENGINE STALLED A ALGAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW03272M 45365 ON FIRST TAKEOFF OF THE DAY, EXPERIENCED COMPRESSOR STALL. ABORTED TAKEOFF AND HOVERED TO NEAREST PARKING PAD AND REPORTED INCIDENT TO MAINTENANCE AND MANAGEMENT. MAINTENANCE VISUALLY INSPECTED INTAKE AREA FOR HARDWARE AND FROGS, INSPECTED COMPRESSOR BLADES AND FOUND NO DAMAGE. STARTED UP AND FLEW WITH NO FURTHER DISCREPANCIES. (M) 1G71 3U3 U H2SW E1GL 20040916000302004091600030EU 2004 9 16 2004F00318 120040713A7160 INLET AIRBUS320 A320233 3930329EU NR 1 ENGINE DEPARTED A RYNAA UNSCHED LANDING DRJINFLIGHT SEPARATION PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CE07951LF 460 AFTER TAKEOFF, NR 1 ENGINE INBOARD AND OUTBOARD FAN COWL DEPARTED AIRCRAFT. A SHUTTER WAS FELT BY THE AIRCREW AND THE NR 1 ENGINE INSTRUMENT LIGHTS FLASHED AMBER AND THEN WENT TO NORMAL. THE NR 1 ENGINE OIL QUANTITY LIGHT REMAINED AMBER. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL WITHOUT INCIDENT. INCIDENT UNDER INVESTIGATION. (M) 2L72 4F RTA28NM 20040916000332004091600033SO 2004 9 16 SIMA200409102 120040329A27403621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO HORIZONTAL STAB INOPERATIVE A SIMAO OTHER J WARNING INDICATION LDLANDING 1 SW21725AE 145312 DURING LANDING, CREW RECEIVED PITCH TRIM BACKUP AND MAIN INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040916000362004091600036EA 2004 9 16 ASOA04442 120040620A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DUIRNG A C-CHECK IN MCN, THE CARGO COMPARTMENT LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 IAW SRM 51-42-21. (M) 2L72 4F RTA21EA 20040916000682004091600068 2004 9 16 SWAA042613 420040909A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916000702004091600070NM 2004 9 16 SWAA042615 120040909A33501010427 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 BULLNOSE EMERGENCY EXIT LIGHT COVER AT ROW 4ABC, BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM. 2L72 4F RTA16WE 20040916000722004091600072NM 2004 9 16 SWAA042617 120040909A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 25R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040916000742004091600074NM 2004 9 16 SWAA042619 120040909A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727D, STRINGER 19R AND BS 727D, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040916000762004091600076NM 2004 9 16 DL767040816 120040827A2913 PUMP BOEING767 767232 1385132NM HYD SYSTEM FAILED A DALAO OTHER K FLUID LOSS LDLANDING 1 SO27115DA 22227 ON LANDING ROLL WHILE EXITING THE RUNWAY 26R LOST ALL CTR HYD FLUID. REPLACED ADP. 2L72 4F RTA1NM 20040916000802004091600080NM 2004 9 16 DL76G040821 120040829A2761 ACTUATOR BOEING767 767332 1382001NM NR 2 SPOILER LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO271604R 30180 AT CRUISE FLIGHT RECEIVED EIVCAS MSG RT HYD QTY AND RSVR LIGHT ON HYD PANEL. RT HYD QTY WAS .48 AT THIS TIME AND SUBSEQUENTLY DECREASED TO .32. AS PER ATL MCC TURNED OFF THE RT ENG HYD PUMP AND RT HYD ELECT DEMAND PUMP. QUANTITY STABILIZED. REPLACED O-RING ON NR 2 SPOILER FILTER PLUG LEAK CHECK OK. 2L72 4F RTA1NM 20040916000852004091600085WP 2004 9 16 AALA20040946 120040906A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219628W 53598 LAX - CABIN EMERGENCY LIGHT BATTERY PACK B527 INOPERATIVE. REPLACED BATTERY B527 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916000872004091600087NM 2004 9 16 AALA20040948 120040907A3350 LIGHT BOEING757 757223 1384957NM EMERGENCY EXIT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21661AA 25295 DFW - EMERGENCY EXIT IDENTIFIER L758 INOPERATIVE. RECONNECTED EMERGENCY EXIT IDENTIFIER L758. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040916000892004091600089NM 2004 9 16 SWAA042635 120040910A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040916000902004091600090NM 2004 9 16 SWAA042636 120040911A33507024091007 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29457WN 33856 AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040916000912004091600091 2004 9 16 SWAA042637 420040911A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040916000922004091600092NM 2004 9 16 SWAA042638 120040911A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20040916000932004091600093NM 2004 9 16 SWAA042627 120040910A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040916000942004091600094NM 2004 9 16 SWAA042628 120040910A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 732E TO 735E, STRINGER 25L AND BS 742E TO 745E, STRINGER 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040916000952004091600095NM 2004 9 16 SWAA042629 120040910A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040916000962004091600096NM 2004 9 16 SWAA042607 120040908A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED C1 CHECK, FOUND FWD CABIN FLOOR PHOTOLUMINESCENT EXIT STRIP, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20040916000972004091600097EA 2004 9 16 COMA0460498 120040901A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA 7306 CARGO LANDING PLATE CRACKED AFT OF FS 574.00 FRAME. REPAIRED IAW REO601R-53-61-690. 2L72 4F RTA21EA 20040916000982004091600098NE 2004 9 16 DLM90040824 220040824A7200 ENGINE DOUG MD90 MD9030 3023690NM IAE V2500 V2500A1 NE NR 2 FAILED A DALAEC ENGINE SHUTDOWN ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO27904DA27525 V20080 53384 V20080 AS POWER WAS PUSHED UP FOR TAKEOFF RIGHT ENGINE OIL PRESSURE LO LIGHT CAME ON AND OIL PRESSURE INDICATED ZERO. SHUT DOWN ENGINE AFTER APPROX 10 SECONDS. REPLACED ACCESSORY GEARBOX. 2L72 4F4 FRTA6WE E311NE 20040916000992004091600099NM 2004 9 16 DL777040825 120040830A2121S210W0035 FAN BOEING777 777232 1385232NM AFT UPPER SMOKE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27862DA 29734 RECIRC FAN STATUS MSG AFT UPPER RECIRC FAN IS OFF, IT CAUSED SOME SMOKE TO ENTER THE CABIN PRIOR TO SHUTTING DOWN THEN SMOKE DISSIPATED QUICKLY. MAT MTC MSG 21-24500. FOUND UPPER AFT RECIRC FAN CB TRIPPED. REPLACED SAME. 2L72 4F RTT00001SE 20040916001012004091600101EA 2004 9 16 COMA0460501 120040906A329717300122 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA RT MLG FAULTY A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01932CA 7038 FLIGHT 5396 DURING TAKEOFF RECEIVED AN OUTBOARD ANTI-SKID CAUTION. TAKEOFF WAS ABORTED AND RETURNED TO THE GATE. REPLACED THE RIGHT MLG OUTBOARD WHEEL SPEED TRANSDUCER WIRING HARNESS. 2L72 4F RTA21EA 20040916001032004091600103EA 2004 9 16 COMA0460503 120040904A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01951CA 7091 FLIGHT 5445 DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. PERFORMED AN OPERATIONAL CHECK OF CABIN DOOR INDICATION SYSTEM AND PERFORMED PRESSURIZATION CHECK. DISCREPANCY COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20040916001052004091600105EA 2004 9 16 COMA0460505 120040905A3260 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01918CA 7018 FLIGHT 5666 AFTER TAKEOFF RECEIVED A NOSE GEAR UP DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. RECONNECTED THE NLG TORQUE LINKS AND REPLACED BOTH TIRES. 2L72 4F RTA21EA 20040916001072004091600107NM 2004 9 16 DLM88040810 120040825A3350276005 FUSE DOUG MD88 MD88 3023688NM EMERGENCY LIGHT UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27906DL 49537 EMERGENCY AISLE LIGHTS INOP ROW 31 THRU 48 SECTION. REPLACED FUSE IN POWER SUPPLY. 2L72 4F RTA6WE 20040916001082004091600108NE 2004 9 16 DL76L040811 220040825A7230PW40603 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A DALAK NONE R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SO27187DN40456 27582 724687 DURING ENGINE RUN-UP NR 1 ENGINE STALLED. REPLACED NR 1 ENGINE. 2L72 4F4 FRTA1NM E24NE 20040916001102004091600110EA 2004 9 16 COMA0460489 120040830A5230 HANDLE CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR UNSECURE A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01924CA 7026 FLIGHT 5048 CARGO DOOR CAUTION MESSAGE, A/C WILL NOT PRESSURIZE. FOUND CARGO DOOR HANDLE NOT LATCHED. INSPECTED DOOR AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20040916001122004091600112EA 2004 9 16 COMA0460507 120040904A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01436CA9842 7482 FLIGHT 5688 DURING APPROACH AFTER SELECTING GEAR DOWN RECEIVED A GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY, ABORTED APPROACH, PERFORMED MANUAL GEAR EXTENSION AND LANDED SAFELY. REPLACED THE MLG SELECTOR VALVE. 2L72 4F RTA21EA 20040916001142004091600114EA 2004 9 16 COMA0470062 120040824A2760 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SPOILERS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01391CA 10108 FLIGHT 5451 FLIGHT SPOILERS AND SPOILERON CAUTION MESSAGE. COULD NOT DUPLICATE SYSTEM, TEST NORMAL. 2L72 4F RTA21EA 20040916001162004091600116NM 2004 9 16 SWAA042610 120040908A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM AT BS 727E, LBL 14, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040916001182004091600118NM 2004 9 16 SWAA042602 120040908A53116546548 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040916001202004091600120NM 2004 9 16 SWAA042604 120040908A53206551698 SPLICE BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICES AT BS 907, STRINGER 4R AND STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20040916001222004091600122 2004 9 16 SWAA042606 420040908A256565C16820 BRACKET BOEING737 7373H4 1384600NM R2 DOOR SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD ATTACH BRACKET, CRACKED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE BRACKET PER MM. 2L72 4F RTA16WE 20040916001242004091600124NM 2004 9 16 SWAA042585 120040904A2823405744 SHUTOFF VALVE BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE FAILED A SWAAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 SW29641SW 27714 856406 INFLIGHT SHUTDOWN, AT FL 330, NR 2 ENGINE RPM'S ROLLED BACK JUST PRIOR TO TOP OF DESCENT. ENGINE SHUT DOWN AND INFLIGHT ENGINE START PROCEDURES ACCOMPLISHED. ALL ENGINE PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 ENGINE FUEL SHUTOFF VALVE ACTUATOR AND CANNON PLUG D790 PER MM. 2L72 4F4 FRTA16WE E2GL 20040916001252004091600125NE 2004 9 16 COMA0460487 220040824A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT FAILED A COMAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO01797CA131372394 7344 807589 FLIGHT 4990 LT ENGINE ROLLBACK TO 50 PERCENT AFTER T/O. REPLACED LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20040916001262004091600126EA 2004 9 16 COMA0460488 120040825A3097 WIRE CNDAIRCL600 CL6002B19 1900309EA CENTER WING CRUSHED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01491CA 7756 FLIGHT 5344 WING ANTI ICE DUCT MESSAGE. REPAIRED CRUSHED WIRE UNDER CENTER WING LEADING EDGE. 2L72 4F RTA21EA 20040916001282004091600128WP 2004 9 16 AALA20040922 120040830A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21572AA 49458 SEA - AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916001302004091600130NM 2004 9 16 AALA20040923 120040831A339702018753 WIRE HARNESS BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21920AN 29521 BDL - CABIN EMERGENCY LIGHTS AT SEAT 22D INOPERATIVE. FOUND BROKEN WIRES FROM EMERGENCY LIGHT PIG TAIL FROM SEAT TO HARNESS. REPLACED HARNESS ASSEMBLY FOR BROKEN WIRES FROM EMERGENCY LIGHT PIG TAIL FROM SEAT TO HARNESS AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040916001322004091600132WP 2004 9 16 AALA20040920 120040829A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217514A 49891 LAX - AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916001342004091600134NM 2004 9 16 AALA20040919 120040829A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 DFW - EMERGENCY LIGHTS AT BOTTOM OF FIRST CLASS MOVIE SCREEN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT BOTTOM OF FIRST CLASS MOVIE SCREEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040916001352004091600135NM 2004 9 16 AALA20040910 120040828A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219412W 53187 LAX - AFT AND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR AFT AND FORWARD CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20040916001372004091600137 2004 9 16 SWAA042586 420040906A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 L1 DOOR EVACV SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001392004091600139NM 2004 9 16 SWAA042588 120040906A33506574550 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHTSMISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040916001412004091600141NM 2004 9 16 SWAA042590 120040904A5330655298871 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001432004091600143NM 2004 9 16 SWAA042592 120040907A53306545800 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN AT BS 277, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001452004091600145 2004 9 16 SWAA042594 420040907A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001472004091600147 2004 9 16 SWAA042596 420040907A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001492004091600149NM 2004 9 16 SWAA042598 120040907A335090083 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE EMERGENCY EXIT OVERHEAD LIGHT AND AFT ENTRY SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040916001502004091600150WP 2004 9 16 AALA20040949 120040907A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217519A 49896 DFW - AFT OVERWING HATCH EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING HATCH EXIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916001522004091600152NM 2004 9 16 AALA20040942 120040831A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21680AN 29590 DFW - EMERGENCY LIGHTS AT SEAT ROWS 27 THROUGH 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FOR SEAT ROWS 27 THROUGH 36. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040916001532004091600153WP 2004 9 16 AALA20040943 120040902A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21501AA 49738 SEA - SEVERAL AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916001542004091600154WP 2004 9 16 AALA20040944 120040902A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219401W 53137 DFW - OVERHEAD EMERGENCY LIGHTS AT BIN N020 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT BIN N020. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916001552004091600155WP 2004 9 16 AALA20040945 120040902A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21566AA 49348 AUS - EMERGENCY LIGHT BATTERY PACK AT AFT RIGHT LAVATORY FORWARD POSITION INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT LAVATORY FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916001562004091600156WP 2004 9 16 AALA20040950 120040907A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217519A 49896 DFW - FORWARD OVERWING HATCH EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING HATCH EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916001572004091600157NM 2004 9 16 AALA20040951 120040907A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 DFW - EMERGENCY LIGHT AT SEAT 20H INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040916001592004091600159NM 2004 9 16 SWAA042599 120040907A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 773, LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040916001612004091600161NM 2004 9 16 SWAA042572 120040903A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29437WN 29832 EEPLS AT ROW 1 ABC, MISSING. INSTALLED EEPLS LIGHT AND LENS PER MM. 2L72 4F RTA16WE 20040916001632004091600163 2004 9 16 SWAA042574 420040903A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001652004091600165NM 2004 9 16 SWAA042576 120040903A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY EXIT DISLODGED A SWAAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED RON, MID CABIN EMERGENCY EXIT SIGN, FELL DOWN. REINSTALLED SIGN PER MM. 2L72 4F RTA16WE 20040916001672004091600167 2004 9 16 SWAA042578 420040903A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001682004091600168EA 2004 9 16 COMA0470064 120040830A2780766389G CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A COMAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION APAPPROACH 1 SO01355CA4821 10067 FLIGHT 5692 SLATS FAIL CAUTION MESSAGE. REPLACED SFECU NR 2. 2L72 4F RTA21EA 20040916001692004091600169NM 2004 9 16 SWAA042486 120040826A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 465, RBL 70, TO BS 865, RBL 65, BS 817 TO BS 865 LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20040916001702004091600170NM 2004 9 16 SWAA042579 120040903A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT L2 DOOR UPPER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001712004091600171NM 2004 9 16 SWAA042580 120040903A57536546431279 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E FOREFLAP PER MM. 2L72 4F RTA16WE 20040916001722004091600172NM 2004 9 16 SWAA042581 120040903A522050797897 SKIN BOEING737 7373H4 1384600NM LT OVERWING DOORCRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING DOOR SKIN AT THE 12 O' CLOCK POSITION CRACKED. REMOVED AND REPLACED OVERWING DOOR PER MM. 2L72 4F RTA16WE 20040916001742004091600174NM 2004 9 16 SWAA042582 120040903A57546573714 SKIN BOEING737 7375H4 138449DNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT, DELAMINATED. REPAIRED SLAT PER EA. 2L72 4F RTA16WE 20040916001762004091600176 2004 9 16 SWAA042562 420040902A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001782004091600178 2004 9 16 SWAA042564 420040902A2565D31354 SLIDE BOEING737 7372T4 1384492NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 DURING SCHEDULED PM CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20040916001802004091600180NM 2004 9 16 SWAA042566 120040902A531165C25230 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, RBL 9, WL, 149, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040916002162004091600216EU 2004 9 16 AALA20040932 120040901A3260BDM3003 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG INOPERATIVE A AALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW2170073 516 SDQ - INFLIGHT UNABLE TO RETRACT LANDING GEAR. TRIED BOTH SYSTEMS. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. ACCOMPLISHED FAULT RETRIEVAL OF PROXIMITY DETECTOR UNIT. SHOWED FAULT CODE 30 CHANNEL 10 WITH BOX FAIL LIGHT ON. REPLACED DETECTOR UNIT 54GB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040916002182004091600218NM 2004 9 16 DL757040852 120040906A3244326001196 TIRE BOEING757 757232 1384965NM NR 2 MLG WHEEL SEPARATED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27666DN 25034 SUSPECT TIRE FAILURE ON T/O. REPLACED NR 2 MAIN WHEEL ASSY PER M/M TIRE CAP FAILURE. TIRE PRESS OK ON ARRIVAL. 2L72 4F RTA2NM 20040916002202004091600220NM 2004 9 16 DLM88040835 120040901A52409911582 BEAM DOUG MD88 MD88 3023688NM R1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27918DL 49583 CRACKED CLIP IN FWD EDGE OF NR 1 BEAM OF R1 DOOR. CRACKED FWD EDGE OF NR 4 BEAM OF R1 DOOR AEROMEXICO NRCS T0024037,T0024036. REPLACED R1 DOOR BEAM NR 4 AND CLIP ON BEAM NR 1. 2L72 4F RTA6WE 20040916002212004091600221EA 2004 9 16 COMA0460453 120040813A5320601R35031241 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01409CA 7441 RIGHT HAND ANGLE CRACKED. REPAIRED IAW REO 601R-53-61-004 REV B. 2L72 4F RTA21EA 20040916002222004091600222EA 2004 9 16 COMA0460454 120040629A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01784CA 7319 CRACK ON THE ENGINE SUPPORT BEAM RIGHT HAND SIDE. REPAIRED IAW REO 601R-53-61-870. 2L72 4F RTA21EA 20040916002232004091600223NM 2004 9 16 DL764040836 120040902A1420 CONNECTOR BOEING767 767432ER 1385134NM EMERGENCY LIGHT DISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27841MH 29714 SEATS 26AB THRU 32AB EMERGENCY PATH LIGHTS INOP ON PRE-DEPARTURE CHECK. FOUND POWER CABLE DISCONNECTED UNDER SEAT 26AB. RECONNECTED CABLE, TESTS GOOD. 2L72 4F RTA1NM 20040916002242004091600224NM 2004 9 16 DLM88040837 120040901A5210 BEAM DOUG MD88 MD88 3023688NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27923DL 49705 CRACKED FWD EDGE OF BEAM NR 2 ON L1 DOOR AEROMEX NRC T0024035, CRACKED AFT EDGE OF BEAM NR 1 ON L1 DOOR AEROMEX NRC T0024034. REPAIRED FWD EDGE OF BEAM NR 2 IAW SRM 52-05D FIG 31. REPAIRED AFT EDGE OF BEAM NR 1 IAW SRM 52-05D FIG 31. 2L72 4F RTA6WE 20040916002252004091600225NM 2004 9 16 DL73S040838 120040901A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER LOCATION AT FS 500. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092825-14AD. 2L72 4F RTA16WE 20040917000012004091700001SW 2004 9 17 2004F00365 120040730A3150407357015109 PANEL BELL 407 407 1182206SW COCKPIT SMOKE A ALGAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03406AL 53481 IN CRUISE FLIGHT, APPROXIMATELY FIVE MILES FROM SL23D THE CAUTION PANEL STARTED SMOKING. LANDED ON A DRILLING RIG AT ST96. MAINTENANCE REMOVED CAUTION PANEL (SN 516) AND INSTALLED SERVICEABLE CAUTION PANEL (SN 504). OPS CHECK WAS GOOD. (M) 1G71 3U O H2SW 20040917000022004091700002 2004 9 17 2004F00366 420040726A3422 RECEPTACLE BELL 206 206L4 1182110SW DIRECTIONAL GYROLOOSE E ALGAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW03170AL 730 52063 ON RUN UP FOR TAKEOFF, FOUND OFF FLAG ON THE DG AND SMELLED ELECTRICAL SMOKE FUMES IN THE COCKPIT. THE COMPONENT WAS SECURED AIRCRAFT RETURNED TO ARA FOR MAINTENANCE, AIRCRAFT REPLACED BY N547AL. MAINTENACNE NOTED OFF FLAG ON DIRECTIONAL GYRO, FOUND CONNECTOR RECEPTACLE LOOSE AND STRONG ODOR OF BURNED ODOR EMITTING FROM GYRO. REPLACED GYRO, POWERED UP AVIONICS VISUAL AND ODOR INSPECTION, FUNCTIONED CHECK OK. (M) 1G71 3U NCH2SW 20040917000032004091700003WP 2004 9 17 WX0400012 120040701A33504TL1110B SWITCH DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSFAILED A WXOAK NONE L NO TEST ININSP/MAINT 1 WP19863GA 49911 MAINTENANCE DISCOVERY AT DEN, EXTERNAL AFT EMERGENCY LIGHTS STAY ON AFTER THEY ARE TURNED OFF. MAINTENANCE REPLACED EMERGENCY LIGHTS SWITCH. LIGHTS OPERATIONALLY CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20040917000042004091700004SO 2004 9 17 2004F00381 120040108A5712 RIB GULSTMGV GULFSTREAMGV3980116SO WINGS CRACKED E E7JAK NONE O OTHER ININSP/MAINT 1 NE03508QS 631 DURING SCHEDULED MAINTENANCE, INSPECTED THE LEFT AND RIGHT OUTBOARD WING RIBS P/N 1159W53025-5 AND 6, DRY BAY FOR CRACKS. CHORD WISE CRACKS MEASURING APPROXIMATELY 4 INCHES IN LENGTH WERE DETECTED AT THE LOWER FORWARD RADIUS OF THE 5 AND 6 RIBS. (M) 2L72 4F RTA12EA 20040917000082004091700008NM 2004 9 17 2004F00370 120040729A5730 SKIN BOEING747 747228F 1384895NM RT WING CORRODED B T64RK NONE O OTHER ININSP/MAINT 1 SW15809MC 20887 DURNG FA02 A-CHECK ACCOMPLISHGIN ATLAS AIR ROUTINE WORK CARD 12M15002 INSPECTION OF RIGHT WING FOUND BULGE AT LOWER FRONT SPAR CAP, CORROSION IS REPORTED AS LEVEL 1 AND IS LOCAL. (M) T64R 2L74 4F A20WE 20040917000092004091700009GL 2004 9 17 2004F00371 220040723A7230 COMPRESSOR BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ENGINE STALLED A ALGAA UNSCHED LANDING RFJPARTIAL RPM/PWR LOSS FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW03171AL 52064 AT 3500 AGL AND 74 PERCENT TORQUE AIRCRAFT COMPRESSOR STALLED, TORQUE FLUCTUATED AND RETURNED TO NORMAL, NOSE OF AIRCRAFT SWUNG 15 DEGREES TO THE LEFT. AIRCRAFT POWER REDUCED AND THEN RETURNED TO CRE BASE. MAINTENANCE REMOVED AND REPLACED ENGINE ASSEMBLY. (M) 1G71 3U3 UNCH2SW E1GL 20040917000112004091700011NE 2004 9 17 2004F00373 120040704A63207635109600044 GEARBOX SKRSKYS76 S76C 8143008NE MAIN ROTOR MAKING METAL A ALGAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03864AL69 760557 AT A HOVER READY FOR TAKEOFF, AFTER INITIAL RUN UP AND PREPARING FOR TAKEOFF MAIN GEAR BOX LIGHT CAME ON. MAINTENANCE DISCOVERED METAL CHIP CONTAMINATION ON LEFT AND RIGHT MAIN GEAR BOX CHIP DETECTORS. TRANSMISSION REMOVED FROM SERVICE. (M) 1G72 3U NCH1NE 20040915000152004091500015NM 2004 9 15 UPS04243070 120040823A53206521655212 STIFFENER BOEING727 727108C 1384039NM RROYCETAY TAY65154 EU MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, HORIZONTAL STIFFNER CORRODED AFT OF APU EXHAUST PORT ON LOWER SURFACE OF UPPER PANEL AT 2 LOCATIONS. CORROSION FOUND TO BE OUTSIDE LIMITS. STIFFNER REMOVED IAW SRM 51-30-02. NEW STIFFNER INSTALLED IAW DRG 65-21655. 2L73 4F4 F A3WE E25NE 20040915000202004091500020NE 2004 9 15 04249402 220040905A7200303100IAW2 ENGINE DORNERDO32 DO328300 NM PWA 306 PW306B NE LEFT DEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27402FJ 3147 AFTER LIFT-OFF WHEN GEAR WAS RAISED THE LT ENGINE ITT ROSE TO 955 DEGREES C, NO-SYNCH ILLUMINATED, AND OIL TEMP ROSE TO 109 DEGREES C. CA CONTINUED CLIMB TO 3,000'MSL AND REDUCED THRUST IAW QRH. ITT WENT BELOW 955 TO AT 900 DEGREES, OIL TEMP REDUCED TO 85 DEGREES C. ATC WAS NOTIFIED. A/C RETURNED TO FIELD. MECHANIC REMOVED AND REPLACED RT ENGINE (SEE REMOVED ENGINE INFO IN SECTION 5 OF THIS SDR). 2H72 4T4 FRTA55NM E35NE 20040915000322004091500032WP 2004 9 15 01082304 120040823A261259585801 FIRE LOOP DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE LT ENGINE MALFUNCTIONED A A4JAK NONE N FALSE WARNING ININSP/MAINT 1 SO35934LK 48157 LT ENGINE FIRE LOOP IAI LIGHT ILLUMINATED. DEFERRED IAW MEL 26-1-1, CONTROL NR M-934-155. CAT C, DUE 09/02/04. PLACARDS INSTALLED M PROCEDURES C/W. 2L72 4F4 F A6WE E2EA 20040915000382004091500038 2004 9 15 RAIA00408028 420040825A3425HG2010AC02 AHRS EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RIGHT INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03813HK8987 8 145044 5648 - STL - RIGHT AHRS FAIL. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS. 2L72 4T4 FRTT00011ATTE6CH 20040915000412004091500041SO 2004 9 15 SWIA200413762 120040820A27503069001017 ANNUNCIATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07167311474 298 120190 AFTER FLAPS SELECTED 15 DEGREES,CONTROL FAULT AND ADVANCED SWS. REMOVED AND REPLACED ANNUNCIATOR WITH SERVICEABLE UNIT IAW 27-50-09. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040915000522004091500052NM 2004 9 15 04FDEA02627 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 SNRM N0455: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000542004091500054NM 2004 9 15 04FDEA02629 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING-OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040915000562004091500056EU 2004 9 15 04FDEA02631 120040824A5313AJ5361056722400 STRINGER AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25421FE 342 MDIS 421 53-10 0009094 03SEP04 SIN OPEN U FUSELAGE STRINGER 44 LT FRAME 13A TO 16A FOUND CORRODED AT MULTIPLE LOCATIONS. ENT BY: 086361 RPT BY: 086361 SHGN 03SEP04 07:32 SIN U SDR HAS BEEN SUBMITTED. ENT BY: 086361 RPT BY: 086361**** S/D COMING ****. 2L72 4F4 FRTA35EU E3NE 20040915000582004091500058 2004 9 15 UPS04143048 420040903A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE MAIN CABIN INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01129UP 0814 REF M287110 ESCAPE SLIDE DEPLOYED. REPLACED ESCAPE SLIDE ASSY IAW MM 25-61-21-4. OKAY FOR SERVICE. CLEARED DMI M287110. 2L72 4F4 FRTA35EU E24NE 20040915000612004091500061NM 2004 9 15 UPS04443036 120040818A5347 SEAT TRACK BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE:C U/D BS 560-590 LBL 29 INCH SEAT TRACK FLANGE CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 1 INCH X 20 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. CIC APPLIED IAW EO NR M5100-2780-E. 2L74 4F4 FRTA20WE E3NE 20040915000672004091500067NM 2004 9 15 UPS04443042 120040819A5313 STRINGER BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D STA 516-517 LT NR 4 STRINGER END FOUND CRACK. U/D STA 516-517 LT NR 4 CRACKED STRINGER REPAIRED IAW SRM 53-10-03 FIG 3. 2L74 4F4 FRTA20WE E3NE 20040915000702004091500070SO 2004 9 15 C2XA04IA110 120040821A259712315660401 HOLDER EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL COCKPIT SHORTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW27161472682 2682 145749 THE CREW REPORTED THAT A SPRING BEHIND THE F/O'S MAP HOLDER MADE CONTACT WITH AN EXPOSED WIRE CAUSING SMOKE. MAINTENANCE REMOVED AND REPLACED THE F/O'S MAP HOLDER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRT TE6CH 20040915000812004091500081WP 2004 9 15 ASMF200408006 120040807A2780833605 PROXIMITY SWITCH DOUG DC9 DC982 3022082WP SLATS DAMAGED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23491SH19636 49150 DURING TRANSIT CHECK, CAPTAIN REPORTED SLAT DISAGREE LIGHT TURNED ON. PSEU WAS TESTED SHOWING FAIL CODES 510 AND 580. PSEU WAS REPLACED IAW 34-19-01, BUT FAIL CONTINUED. LT SLAT SENSORS WERE CHECKED DETECTING FAIL IN SENSOR "C", SENSOR "C" AND ITS SPRING WERE LUBRICATED BUT FAIL CONTINUED. SENSOR "C" AND TX ANGLE ATTACK RT WERE REPLACED IAW MM 32-60-04 AND 27-80-06, TESTS CORRECT. 2L72 4F A6WE 20040915001012004091500101NE 2004 9 15 ASMF200407004 220040703A7320V3400283 SOLENOID VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS529 49643 718221 AIRCRAFT RETURNED TO PLATFORM, DIFFERENCE BETWEEN ENGINES PARAMETERS. LT FCU SOLENOID WAS REPLACED IAW MM 73-20-05 AND TEST IAW MM 73-20-01, ALL CORRECT. DURING ENGINE NR 1 START FAIL CONTINUED, AIR/GROUND SENSOR R2-308 WAS REPLACED, TEST CORRECT. FLIGHT WAS CANCELLED AND DURING OVERNIGHT SERVICE, FUNCTIONAL TEST AND ENGINE RUNNING WERE PERFORMED IAW MM 71-00-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20040915001272004091500127 2004 9 15 2004F00337 420040818A3460S703100000 COMPUTER BEECH 1900 1900D 1154162CE FLT DIRECTOR SHORTED A GUUAO OTHER J WARNING INDICATION APAPPROACH 1 SO1981546 UE187 FLT 9215 - TPA/MIA - DURING APPROACH, YAW DAMP/RUDDER BOOST FAIL ANNUNCIATOR ILLUMINATED, FOLLOWED BY LEFT AC BUS ANNUNCIATOR. ELECTRICAL SMELL OF SMOKE OBSERVED IN COCKPIT. REMOVED AND REPLACED FDR COMPUTER. OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA24CE 20040915001322004091500132NM 2004 9 15 USAABB04076 120040809A33501265 LIGHT BOEING767 7672B7 1385107NM ROW 24-29 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19656US 26847 CLT - FOUND AISLE EMERGENCY LIGHTS AT ROWS 24L AND 29R INOPERATIVE. MAINTENANCE REPLACED BOTH LIGHT ASSEMBLIES. (M) 2L72 4F RTA1NM 20040915001352004091500135NM 2004 9 15 2004F00341 120040707A275165DT1105139 INDICATOR BOEING727 727233 138408ANM TE FLAPS INOPERATIVE A PCSAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO17495AJ 20937 ON TAKEOFF FROM KMIA, OUTBOARD FLAP STAYED AT 20 DEGREES CREATING SPLIT FLAP CONDITION. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED OUTBOARD TRAIILNG EDGE FLAP INDICATOR IAW MM 27-56-10. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040915001572004091500157WP 2004 9 15 2004F00347 120040806A82002D162050515 TUBE CVAC 440 440 2422902WP METHANOL SYS CORRODED A JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 BAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSOIN ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) JRAA 2L72 4R 6A6 20040915001652004091500165EA 2004 9 15 A6WA200440118 120040711A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY DOOR FROZEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31428AW 7695 SERVICE/EMERGENCY DOOR EXTERIOR HANDLE IS FROZEN IN PLACE. REQUIRES LUBRICATION. LUBRICATED SERVICE/EMERGENCY DOOR EXTERIOR HANDLE IAW CRS 200 AMM SUBTASK 12-20-52-640-023 STEPS 3 AND 10. HANDLE IS NO LONGER STICKING. (M) 2L72 4F RTA21EA 20040916000092004091600009EU 2004 9 16 USAASA04034 120040403A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19106US 1044 THE LEFT AFT EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F RTA28NM 20040916000202004091600020EU 2004 9 16 2004F00314 120040722A2120 SMOKE AEROSPATR72 ATR72212 8680945EU COCKPIT DETECTED A TRBAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO21417AT 417 DURING TAXI, ELECTRICAL SMOKE IN CABIN. INSPECTED CABIN LIGHTING SYSTEM, INCLUDING LATERAL LIGHTS SOCKETS AND READING LIGHTS CIRCUIT BOARDS AND FOUND NO EVIDENCE OF DAMAGE THAT COULD CAUSE THE SMOKE IN THE CABIN. (M) 2H72 4T RTA53EU 20040916000452004091600045NM 2004 9 16 AMTA200400933 120040724A3150 WARNING LIGHT BOEING757 75733N 1384931NM RT TURBINE OHEATILLUMINATED A AMTAK NONE J WARNING INDICATION ININSP/MAINT 1 GL11552TZ 32586 EICAS STATUS MESSAGE 'RT TURBINE OVERHEAT DET 2' DISPLAYED. DEFERRED PER MEL 26-11-20. (M) 2L72 4F RTA2NM 20040916000472004091600047NM 2004 9 16 AMTA200400998 120040731A5330 PANEL BOEING757 75733N 1384931NM CARGO BAY CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11551TZ 32585 FOUND CORROSION AT FS 1380 C-2 PIT ON RIGHT SIDE PANEL. REMOVED RIGHT SIDE TRANSPANEL IAW SRM 51-40-02 AND REINSTALLED NEW IAW SRM 51-40-02 SEE M12A FOR OTHER WORK ACCOMPLISHED. (M) 2L72 4F RTA2NM 20040916000502004091600050EU 2004 9 16 ASOA04548 120040713A5320S5367800826902 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE RIGHT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INTERCOSTAL BETWEEN FRAME 38 AND FRAME 39 IAW SRM 51-25-00. (M) 2H72 4T RTA53EU 20040916000532004091600053NM 2004 9 16 SWAA042646 120040912A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT STRINGER 27L AT BS 949, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040916000552004091600055 2004 9 16 SWAA042648 420040912A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29762SW 27876 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916000572004091600057 2004 9 16 SWAA042650 420040913A2565D31354 SLIDE BOEING737 7375H4 138449DNM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916000592004091600059NM 2004 9 16 SWAA042651 120040913A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED A1 CHECK, FOUND 2 EACH SERVICE DOORS EGRESS LIGHTS INOP. RELAMPED EGRESS LIGHTS PER MM. 2L72 4F RTA16WE 20040916000612004091600061NM 2004 9 16 SWAA042653 120040913A531565C33940 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD AT BS 294.5, LBL 12, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040916000632004091600063NM 2004 9 16 SWAA042631 120040910A53116546539 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME CHORD AT BS 616, LBL 65, WL 200, CRACKED. REMOVED AND REPLACED FRAME CHORD SECTION PER SB. 2L72 4F RTA16WE 20040916000652004091600065NM 2004 9 16 SWAA042633 120040910A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916000672004091600067GL 2004 9 16 SWAA042612 220040909A7200332A1000 ENGINE BOEING737 7373Q8 1384670NM CFMINTCFM56 CFM563B1US GL NR 2 VIBRATION A SWAAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW29688SW 23254 721287 AT CLIMB POWER, NR 2 ENGINE HAD VIBRATION AND HUM-VIBRATION METER AT 5.0, REDUCING N1 TO 83 PERCENT VIBRATION METER WAS AT 4.0, AND HUM-VIBRATION METER SLIGHTLY LOWER. HUM-VIBRATION ONLY WENT AWAY WITH N1 BELOW 48 PERCENT. REMOVED AND REPLACED NR 2 ENGINE PER MT 371-00-01. 2L72 4F4 FRTA16WE E2GL 20040916000772004091600077NM 2004 9 16 DL76G040817 120040828A2460BACC18X25 CIRCUIT BREAKER BOEING767 767332 1382001NM COCKPIT TRIPPED A DALAC ABORTED TAKEOFF GJ MULTIPLE FAILURE WARNING INDICATION TOTAKEOFF 1 SO271608 30573 ABORTED T/O IN FCO 120 KNOTS NUMEROUS LIGHTS BELLS INDICATIONS ELECTRIC MALFUNCTION LOSS OF BUS ETC. C/B A-2 ON PANEL P6-1 DC STBY FOUND POPPED. REPLACED CB AND RELAY K109 STBY PWR AND RELAY K104 MAIN BATTERY. 2L72 4F RTA1NM 20040916000822004091600082EA 2004 9 16 COMA0460494 120040901A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA 7306 LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. 2L72 4F RTA21EA 20040916000842004091600084NM 2004 9 16 AALA20040941 120040901A1420 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21661AA 25295 MIA - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. RESEATED CONNECTOR AT SEAT TO WALL PLUG ON SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040916000862004091600086NM 2004 9 16 AALA20040947 120040906A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21771AN 29579 NRT - OVERHEAD EMERGENCY LIGHTS ON DOOR 4L AND LEFT HAND AISLE ROW 36 THROUGH 42 INOPERATIVE. REPLACED BATTERY PACK M33407 AT DOOR 4L FOR OVERHEAD EMERGENCY LIGHTS AT DOOR 4L AND LEFT HAND AISLE ROW 36 THROUGH 42. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040916000882004091600088NM 2004 9 16 SWAA042634 120040910A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001002004091600100NM 2004 9 16 DL757040827 120040831A335020121 POWER SUPPLY BOEING757 757232 1384965NM 34ABC INOPERATIVE A DALAO OTHER L NO TEST TXTAXI/GRND HDL 1 SO27633DL 23614 AFT EMERGENCY EXIT LIGHTS WILL NOT GO OUT WHEN BATTERY IS RESET. LT SIDE ONLY REAR. REPLACED EMERGENCY EXIT PWR SUPPLY M735 AND BATTERY PACK. 2L72 4F RTA2NM 20040916001022004091600102EA 2004 9 16 COMA0460502 120040906A7930 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GEARBOX OVERSERVICED A COMAO OTHER WMJINADEQUATE Q C OVER TEMP WARNING INDICATION CLCLIMB 1 SO01962CA 7123 FLIGHT 5207 DURING CLIMBOUT OF CVG RECEIVED AN OIL TEMPERATURE CAUTION ON ENGINE NR 2. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. DRAINED EXCESSIVE OIL FROM GEARBOX, PERFORMED GROUND RUNS WITH SATISFACTORY RESULTS. 2L72 4F RTA21EA 20040916001042004091600104EA 2004 9 16 COMA0460504 120040903A26213565000183 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA AFT E/E BAY DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01457CA12789 7612 FLIGHT 5350 AFTER TAKEOFF RECEIVED A CARGO BOTTLE LOW CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED BOTH FIRE EXTINGUISHING BOTTLES. 2L72 4F RTA21EA 20040916001062004091600106NM 2004 9 16 SWAA042608 120040908A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS AT BS 727D, LBL 3, RBL 3, RBL 8 AND BS 773, LBL 12, RBL 3, RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040916001092004091600109NE 2004 9 16 DL764040812 220040826A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680 30025NE NR 2 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27843MH11798 29716 706174 PERFORM WIGGLE CHECK INSP OF NR 1 ENGINE 5TH STG VSV LEVER ARMS. DUE NR 2 ENGINE CHANGE FOR VSV REPAIR. 2L72 4F4 FRTA1NM E13NE 20040916001112004091600111EA 2004 9 16 COMA0460506 120040903A3260 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG DISCONNECTED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01937CA 7044 FLIGHT 5780 AFTER TAKEOFF RECEIVED A GEAR UP DISAGREE WARNING. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. RECONNECTED THE NLG TORQUE LINKS AND REPLACED BOTH TIRES. 2L72 4F RTA21EA 20040916001132004091600113EA 2004 9 16 COMA0460486 120040822A5312601R961517 FITTING CNDAIRCL600 CL6002B19 1900309EA BULKHEAD SHEARED A COMAK NONE O OTHER ININSP/MAINT 1 SO01477CA5851 7670 LEFT AND RIGHT LOW PRESSURE AIR CONDITIONING DUCTS, BULKHEAD FITTINGS HAVE ALIGNMENT PINS MISSING. PERFORMED A MAJOR REPAIR AT FS 621.00 LT AND RT BY REMOVING DAMAGED BULKHEAD FITTINGS, AND INSTALLING NEW FITTINGS P/N 601R96151-7 AT BOTH LOCATIONS IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20040916001152004091600115NM 2004 9 16 SWAA042609 120040908A53136547869318 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R AT BS 747 AND BS 727E, CORRODED. REPAIRED STRINGER PER EA. 2L72 4F RTA16WE 20040916001172004091600117NM 2004 9 16 SWAA042601 120040908A335065C27093 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 27935 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20040916001192004091600119NM 2004 9 16 SWAA042603 120040908A53116546557 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040916001212004091600121NM 2004 9 16 SWAA042605 120040908A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 685, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040916001232004091600123NM 2004 9 16 SWAA042584 120040904A2612472622 FIRE DETECTOR BOEING737 7373H4 1384600NM NR 1 ENGINE FAILED A SWAAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 SW29369SW 26580 AIR TURN BACK, 1 TO 2 MINUTES AFTER DEPARTURE THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED, THEN NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. ALL LIGHTS EXTINGUISHED WHEN THROTTLES RETARDED FOR DESCENT. REMOVED AND REPLACED NR 1 ENGINE CONTROL PANEL AND NR 1 FIRE DETECTOR UNIT PER MM. 2L72 4F RTA16WE 20040916001272004091600127WP 2004 9 16 AALA20040908 120040828A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21939AS 49657 FIRST CLASS EMERGENCY LIGHTS ON OVERHEAD PANELS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FIRST CLASS EMERGENCY LIGHTS ON OVERHEAD PANELS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916001292004091600129NM 2004 9 16 AALA20040926 120040830A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 TUL - BATTERY PACK AT STATION 952 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1672 AT STATION 952 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040916001312004091600131NM 2004 9 16 AALA20040925 120040830A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 TUL - BATTERY PACK AT STATION 727 SEAT ROW 19 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727 SEAT ROW 19 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040916001332004091600133WP 2004 9 16 AALA20040921 120040830A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHTSINOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21562AA 49344 LAX - LEFT AND RIGHT HAND AFT OVERWING HATCH EMERGENCY LIGHTS AT L2 245 AND L2 246 INOPERATIVE. REPLACED BATTERY PACK B5105 FOR LEFT AND RIGHT HAND AFT OVERWING HATCH EMERGENCY LIGHTS AT L2 245 AND L2 246. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916001362004091600136EU 2004 9 16 AALA20040911 120040828A3350 SOCKET AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW2141063 506 MIA - EMERGENCY EXIT LIGHT ASSEMBLY MOUNTED ON AFT SIDE OF MID GALLEY WALL RIGHT HAND SIDE RIPPED OFF THE WALL. REPLACED BASE AND LENS OF MID GALLEY RIGHT HAND AFT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040916001382004091600138NM 2004 9 16 SWAA042587 120040906A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHTSMISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29404WN 27892 EEPLS HAS WIRES EXPOSED AT EMERGENCY EXIT ROW. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040916001402004091600140NM 2004 9 16 SWAA042589 120040904A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001422004091600142NM 2004 9 16 SWAA042591 120040904A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 350, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001442004091600144 2004 9 16 SWAA042593 420040907A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001462004091600146NM 2004 9 16 SWAA042595 120040907A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 AFT GALLEY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040916001482004091600148NM 2004 9 16 SWAA042597 120040907A3350582233 POWER SUPPLY BOEING737 7375H4 138449DNM EMERGENCY LIGHTSINOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED PM CHECK, FOUND AFT ENTRY AND AFT SERVICE EMERGENCY EXIT OVERHEAD LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER MM. 2L72 4F RTA16WE 20040916001512004091600151EA 2004 9 16 COMA0470063 120040828A2781 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLATS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01355CA 10067 FLIGHT 5042 SLATS FAIL MESSAGE. CLEARED FAULTS FROM SFECU. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040916001582004091600158NM 2004 9 16 AALA20040952 120040907A3350 LIGHT BOEING767 767323 1385205NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21398AN 29605 DFW - EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPLACED EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040916001602004091600160NM 2004 9 16 SWAA042600 120040907A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 858, LBL 3 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040916001622004091600162NM 2004 9 16 SWAA042573 120040903A2761654456114 ACTUATOR BOEING737 7373H4 1384600NM FLT SPOILER LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29313SW 23335 AIR TURNBACK, AIR RETURN TO DAL DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID AND PRESSURE. REMOVED AND REPLACED NR 6 INBOARD FLIGHT SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20040916001642004091600164 2004 9 16 SWAA042575 420040903A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001662004091600166 2004 9 16 SWAA042577 420040903A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29637SW 27710 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040916001732004091600173EA 2004 9 16 COMA0460491 120040827A3220750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01455CA7421 7592 FLIGHT 5633 NLG DOOR WARNING. REPLACED THE NLG DOOR SELECTOR VALVE. 2L72 4F RTA21EA 20040916001752004091600175NM 2004 9 16 SWAA042561 120040902A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 R1 AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENSES, MISSING. REMOVED AND REPLACED LIGHT LENSES PER MM. 2L72 4F RTA16WE 20040916001772004091600177 2004 9 16 SWAA042563 420040902A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 R2 DOOR EVAC SLIDE GIRT BAR AFT DOOR HOOK LOOSE. SECURED AFT GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20040916001792004091600179NM 2004 9 16 SWAA042565 120040902A57536546434370 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C3 CHECK, FOUND RT WING AFT INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20040916001812004091600181EA 2004 9 16 COMA0470065 120040910A2782766385C ACTUATOR CNDAIRCL600 CL6002C10 1390015EA NR 3 SLAT MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01331CA5055 10061 FLIGHT 5023 SLATS FAIL CAUTION MESSAGE. REPLACED THE NR 3 SLAT ACTUATOR. 2L72 4F RTA21EA 20040916001832004091600183EA 2004 9 16 COMA0470068 120040910A3350 SIGN CNDAIRCL600 CL6002C10 1390015EA EMERGENCY EXIT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01378CA 10097 FLIGHT 5639 EMERGENCY EXIT SIGN AT SERVICE DOOR IS INOP. RECONNECTED WIRES TO EXIT SIGN. 2L72 4F RTA21EA 20040916001842004091600184NM 2004 9 16 SWAA042567 120040902A531165C37565 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT BS 727, LBL 11, CRACKED. REPAIRED FRAME CHORD PER SB, ER. 2L72 4F RTA16WE 20040916001852004091600185NM 2004 9 16 SWAA042568 120040902A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 467, BETWEEN STRINGER 28L AND STRINGER 28R, CORRODED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916001862004091600186NM 2004 9 16 SWAA042569 120040902A3350D71702030 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29710SW 27844 DURING SCHEDULED RON, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040916001872004091600187NM 2004 9 16 SWAA042570 120040811A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29750SA 29802 DURING SPV, FOUND SEVERAL EMERGENCY EXIT LIGHTS THROUGHOUT CABIN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20040916001882004091600188NM 2004 9 16 SWAA042571 120040811A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 16 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040916001902004091600190EA 2004 9 16 COMA0460483 120040823A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01420CA 7451 LBL 27.00 FLOORBEAM CAP CRACKED. REPAIRED IAW CRJ SRM 51-40-11, 51-45-00, 51-42-10, 51-25-16, 51-41-02. 2L72 4F RTA21EA 20040916001922004091600192EA 2004 9 16 COMA0460490 120040829A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01523CA 7821 FLIGHT 5754 EMERGENCY FLOOR PATH LIGHT AT ROW 7 IS INOP. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040916001942004091600194EU 2004 9 16 AALA20040884 120040818A7120 MOUNT AIRBUS300 A300B4605R 3930308EU ENGINE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170054 461 RIGHT HAND OUTBOARD AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AND PAINTED PER ESO 30595. 2L72 4F RTA35EU 20040916001952004091600195WP 2004 9 16 AALA20040877 120040821A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21218AA 49168 RDU - CEILING EMERGENCY LIGHTS BETWEEN ROWS 18 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 18 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916001962004091600196WP 2004 9 16 AALA20040878 120040821A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21483A 49676 AUS - EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. REPLACED BATTERY PACK IN AFT RIGHT LAVATORY FOR EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916001992004091600199WP 2004 9 16 AALA20040880 120040821A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21482AA 49675 SEA - CEILING EMERGENCY LIGHT IN TAIL INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR CEILING EMERGENCY LIGHT IN TAIL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916002012004091600201WP 2004 9 16 AALA20040959 120040913A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219407R 49400 DFW - EMERGENCY CEILING LIGHTS AT SEATS 28 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY CEILING LIGHTS AT SEATS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040916002032004091600203NM 2004 9 16 DL73S040828 120040901A5312654588340 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27315DL 23087 INSPECTION OF THE FS 178 BULKHEAD PER AD 200-05-29 REVEALED A CRACK IN THE FLOOR WEB AT WL 207.5 AND RBL 28. THE CRACKED SECTION OF WEB WAS REMOVED AND REPLACED WITH A NEW PART PER ER/A 093110-14AD. 2L72 4F RTA16WE 20040916002052004091600205EU 2004 9 16 AALA20040876 120040821A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2190070 513 MIA - EMERGENCY LIGHTS FROM LEFT AISLE SEATS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM LEFT AISLE SEATS 19C TO 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040916002072004091600207NM 2004 9 16 DL76G040831 120040901A2421729825L IDG BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE NR 2 ENGINE UNSERVICEABLE A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271607B 00823 30388 704823 CREW REPORTS RIGHT IDG DRIVE LIGHT. LEFT HP VLV ALREADY ON MCO, DIVERTING TO JFK AS PRECAUTION. REPLACED RIGHT IDG, LEAK CHECKS AND OPS CHECKS GOOD. 2L72 4F4 FRTA1NM E13NE 20040916002092004091600209NM 2004 9 16 DL764040833 120040902A3310MS25306222 SWITCH BOEING767 767432ER 1385134NM COCKPIT LIGHT BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27843MH 29716 ON LANDING AFTER CLEARING RUNWAY GOT SMOKE IN THE COCKPIT, SMELLED LIKE RUBBER. FOUND LEFT RUNWAY TURNOFF LIGHT SWITCH SHORTED OUT AND BURNT WITH ASSOCIATED C/B POPPED. REPLACED SAME, RESET C/B, ALL CHECKS GOOD. 2L72 4F RTA1NM 20040916002112004091600211NM 2004 9 16 AALA20040935 120040901A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21666A 25300 DFW - FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER MOD M10798 FOR FORWARD CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040916002132004091600213NE 2004 9 16 AALA20049060 220040913A7200 ENGINE BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE RIGHT MALFUNCTIONED A AALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21789AN 30252 51213 ON CLIMB PASSING 12,000 A LOUD NOISE WAS HEARD FOLLOWED BY AN IMMEDIATE ROLLBACK ON THE RT ENGINE. SHORTLY THEREAFTER WERE INDICATIONS OF FIRE. THE LIGHT WENT OUT ALMOST IMMEDIATELY AS THE CHECKLIST WAS RUN. RETURNED TO BOS. TROUBLESHOOTING IN PROGRESS. REPLACED NUMBER TWO ENGINE DUE TO COMPRESSOR STALL AT 12000 FT. CLOSED. 2L72 4F4 FRTT00001SEE00050EN 20040916002152004091600215NM 2004 9 16 AALA20040934 120040901A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21666A 25300 DFW - EMERGENCY LIGHTS IN THE AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER MOD M00737 FOR EMERGENCY LIGHTS IN THE AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040917000052004091700005NE 2004 9 17 2004F00368 120040721A6540 WARNING LIGHT SKRSKYS76 S76C 8143008NE T/R GEARBOX ILLUMINATED A ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03864AL 760557 DURING TAKEOFF, INTERMEDIATE/TAIL ROTOR GEAR BOX LIGHT CAME ON DURING TAKEOFF, CIRCUIT BREAKER WAS PULLED, LIGHT WENT OUT, RESET CIRCUIT BREAKER, LIGHT CAME BACK ON. AIRCRAFT WAS LANDED BACK ON RIGHT AT ST164. MAINTENANCE REMOVED INTERMEDIATE AND TAIL ROTOR GEAR BOX CHIP DETECTORS, CLEANED AND REINSTALLED, GROUND RAN OPS CHECK WAS GOOD, NO FURTHER DEFECTS NOTED. (M) ALGA 1G72 3U NCH1NE 20040917000072004091700007NM 2004 9 17 2004F00369 120040729A575365B155351 BRACE BOEING747 747228F 1384895NM FLAP FAIRING CRACKED B T64RK NONE O OTHER ININSP/MAINT 1 SW15809MC 20887 DURING FA02 A-CHECK ACCOMPLISHING ATLAS AIR ROUTINE WORK CARD 11FM15002, INSPECTION OF LEFT WING FOUND NR 4 FLAP CANOE FAIRING TO TRACK FORWARD OUTBOARD FITTING CRACKED IN HALF. (M) T64R 2L74 4F A20WE 20040917000102004091700010EU 2004 9 17 2004F00372 120040726A2612B432M FIRE DETECTOR UROCOPEC120 EC120B 8680987EU ENGINE DIRTY A ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03513AL 1261 IN FLIGHT, HAD FLOWN APPROXIMATELY 12 MINUTES OUTBOUND, THEN HEARD GONG AND HAD ENGINE FIRE LIGHT INTERMITTENTLY. TURNED AROUND TO RETURN TO ICY AND LIGHT WENT OUT. ON FINAL TO ICY, LIGHT CAME BACK ON STEADY FOR 3 TO 5 SECONDS THEN WAS INTERMITTENT. MAINTENANCE CLEANED BOTTOM FIRE DETECTOR AND REMOVED UPPER REAR FIRE DETECTOR AND INSTLALED SERVICEABLE FIRE DETECTOR, FUNCTION CHECKED GOOD. (M) 1G72 3U NCR0001RD 20040917000172004091700017NE 2004 9 17 2004F00380 220040721A7320 BELLOWS SKRSKYS76 S76A 8143006NE TMECA ARRIELARRIEL1S1 60030NE FUEL CONTROL CONTAMINATED E ALGAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW03521AL 760132 ON TAKEOFF, THE NR 1 ENGINE STARTED TO SURGE. MAINTENANCE REMOVED FUEL CONTROL, FOUND WATER IN THE P1 BELLOWS REMOVED WATER AND REINSTALLED FUEL CONTROL, OPS CHECK WAS GOOD. (M) 1G72 3U3 U H1NE E19EU 20040917000182004091700018EU 2004 9 17 ASOA04539 120040712A5347NTA44768 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 37 TO FRAME 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 37 TO FRME 39 IAW SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RTA53EU 20040917000192004091700019EU 2004 9 17 ASOA04532 120040727A5712 RIB AEROSPATR72 ATR72212 8680945EU RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING A C-CHECK IN YUL, LEADING EDGE RIBS 6 AND 7 AT THE RIGHT INBOARD FLAP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED LEADING EDGE RIBS 6 AND 7 AT THE RIHT INBOARD FLAP IAW SRM 51-25-03 AND 51-25-01. (M) 2H72 4T RTA53EU 20040917000202004091700020WP 2004 9 17 GTIA040654 120040621A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND FLOORBOARD FASTENER INSERTS MISSING, TWO EACH STATION 200-260 LBL 24-25. UPON FURTHER INVESTIGATION FLOORBOARD PANEL FOUND TO BE BROKEN. FABRICATED FLOORBOARD. (M) 2L72 4F A6WE 20040917000212004091700021NM 2004 9 17 USAASB04034 120040320A2913 SEAL BOEING737 7373B7 1384580NM EDP LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19374US 22953 ON CLIMB-OUT FROM CLT, PASSING THROGH 7,000 FT, THE A-HYD SYSTEM EMDP LOW PRESSURE LIGHT ILLUMINATED, FOLLOWED SHORTLY THEREAFTER BY THE 'A' HYDRAULIC SYSTEM EDP LOW PRESSURE LIGHT. QUANITY FOR 'A' HYDRAULIC SYSTEM READ ZERO. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT WITHOUT FURTHER INCIDENT. DUE OT LOSS OF NOSE WHEEL STEERING, THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND THE NR 3 FLIGHT SPOILER ACTUATOR SEAL CUT AND LEAKING. REPLACED SEAL AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP, P/N 65075-06, PER MM 29-15-12. REPLACED FILTERS AND FLUSHED HYDRAULIC SYSTEM PER MM 29-15-00. RESERVICED HYDRAULIC RESERVOIR. LEAK TEST AND RUN UP TESTS NORMAL. (M) 2L72 4F RTA16WE 20040917000222004091700022NM 2004 9 17 AMTA200400995 120040805A1420 CONNECTOR BOEING757 75723N 1384973NM EMERGENCY LIGHT LOOSE A AMTAK NONE O OTHER ININSP/MAINT 1 GL11522AT 29330 FOUND EMERGENCY LIGHTS FLOOR PROXIMITY OUT FROM ROW 2 DEF FORWARD. SECURED LOOSE CONNECTOR AS REQUIRED. OPS NORMAL. (M) 2L72 4F RTA2NM 20040917000232004091700023WP 2004 9 17 GTIA040655 120040621A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FOUND FLOORBOARD BROKEN STATION 200-260 LBL 24-31. FABRICATED FLOORBOARD. (M) 2L72 4F A6WE 20040917000242004091700024NM 2004 9 17 AMTA200400215 120040229A3411 PITOT HEAD BOEING757 75733N 1384931NM PITOT STATIC SYSMISSING A AMTAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL11552TZ 32586 ENGINE SURGED DURING CONSTANT POWER AT 13,000 FT, ENGINE OPERATION NORMAL AFTER SURGE. THE ENGINE NEVER ACTUALLY HAD A SURGE/STALL IT WAS A FLUCTUATING PARAMETRS SITUATION. TROUBLESHOOT PER FIM 71-06-00 FIG 102. ONE PITOT HEAD MISSING ON THE PF RAKE 3 O'CLOCK POSITION. TEMP REPAIR PER MM 77-11-04/201. ENGIEN RUN OPERATION NORMAL. (M) 2L72 4F RTA2NM 20040917000252004091700025WP 2004 9 17 GTIA040647 120040604A5230 BEAM DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND AFT CARGO PIT HAS NUMEROUS BARE METAL AREAS AND CORROSION IN JAMB AREA. CORRSION ON JAMB BEAM OUT OF LIMITS. REMOVED JAMB BEAM. LOCATED AND DRILLED NEW JAMB BEAM. INSTALLED NEW JAMB BEAM. (M) 2L72 4F RTA6WE 20040917000262004091700026WP 2004 9 17 GTIA040648 120040605A5230 BEAM DOUG DC9 DC983 3022083WP CARGO DOOR DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 FTW - FOUND MID PIT JAMB BEAM HAS CORROSION ON REPAIR STRAP IN FASTENER HOLES AND ON LOWER FLANGE. MATERIAL LOSS FOUND OUT OF LIMITS. REMOVED JAMB BEAM. LOCATED AND DRILLED HOLES IN JAMB BEAM. INSTALLED JAMB BEAM. (M) 2L72 4F RTA6WE 20040917000272004091700027WP 2004 9 17 GTIA040650 120040619A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 200-1309 IS CORRODED AND GOUGED ALONG ENTIRE LENGTH, FS 494 IS OUT OF LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STATION 494 TO 532. LOCATED AND DRILLED NEW SEAT TRACK SECTION AND TWO NEW SPLICES. INSTALLED NEW SET TRACK SECTION. (M) 2L72 4F A6WE 20040917000282004091700028NM 2004 9 17 AMTA200400205 120040227A5321 FLOOR PANEL BOEING757 75733N 1384931NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11556TZ 32590 C-2 FLOOR HAS SEVERAL AREAS OF CORROSION FROM STATION 1465-1180. REPLACED FLOOR PANELS FROM STATION 1465-1330 AND 1330-1180 PER A MM 25-50-04-4 AND SRM 53-00-53-1. (M) 2L72 4F RTA2NM 20040917000292004091700029NM 2004 9 17 AMTA200400209 120040225A2612 WARNING LIGHT BOEING757 75733N 1384931NM LT ENGINE FALSE INDICATIONA AMTAO OTHER N FALSE WARNING DEDESCENT 1 GL11557TZ 32591 EICAS MESSAGE LT ENGINE OVERHEAT. COULD NOT DUPLICATE. OK FOR SERVICE. (M) 2L72 4F RTA2NM 20040917000302004091700030NE 2004 9 17 AMTA200400174 220040213A7421 IGNITER BOEING737 73783N 13844HINM CFMINTCFM567CFM567B2US 13802NE NR 1 ENGINE FAILED A AMTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL11303TZ 28648 LEFT ENGINE FAILED TO LIGHT OFF WITH RIGHT IGNITION SELECTED. REMOVED AND REPLACED NR 1 ENGINE RIGHT IGNITOR PLUG IAW MM 74-21-02-4. OK FOR SERVICE. (M) 2L72 4F4 FRTA16WE E2GL 20040917000322004091700032 2004 9 17 GTIA040646 420040706A2565 SLIDE DOUG DC9 DC981 3022081WP L1 DOOR MISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23819NK 48016 RSW - FLT 670 - FOUND FORWARD SLIDE IN L1 DOOR FOUND HOLDING PINS NOT CORRECT. REMOVED AND REPLACED FORWARD L1 EVAC SLIDE. (M) 2L72 4F A6WE 20040917000342004091700034NE 2004 9 17 AMTA200400199 220040224A7200 ENGINE BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE RIGHT MALFUNCTIONED A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11555TZ 32589 RT ENGINE SHUTDOWN ACCOMPLISHED DUE TO OIL PRESSURE AND QUANTITY ZERO, APPROX FL 300. REPLACED ENGINE IAW M57-71-04. (M) 2L72 4F4 FRTA2NM E12EU 20040917000362004091700036NM 2004 9 17 AMTA200400159 120040212A5321 FLOOR PANEL BOEING737 73783N 13844HINM CARGO BAY CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11304TZ 30675 C-2 CARGO PANELS HAVE CORROSION APPROX STATION 727A TO 727E. FOUND CORROSION OUT OF LIMITS PER SRM 53-00-53-1. REMOVED FLOOR PANEL. FABRIATED AND INSTALLED NEW PANEL. (M) 2L72 4F RTA16WE 20040917000382004091700038EA 2004 9 17 ASOA04514 120040715A5210601R389641 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR STIFF A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR HANDLE LINKAGE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040917000402004091700040EA 2004 9 17 ASOA04510 120040714A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11868AS 7474 DURING AN A-CHECK IN BTR, THE RIGHT SIDE FRAME AND DOUBLER AT FS 640, STRINGER 10R WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT SIDE FRAME AND DOUBELR AT FS 640, STRINER 10R IAW SRM 51-40-00. (M) 2L72 4F RTA21EA 20040917000452004091700045 2004 9 17 AMTA200400959 420040730A2565 GIRT BAR BOEING757 75723N 1384973NM R1 DOOR SLIDE DIRTY A AMTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL11523AT 30232 FOUND R1 DOOR WILL NOT ARM. REMOVED DEBRIS FROM UNDERNEATH GIRT BAR. SLIDE ENGAGE OPS NORMAL. (M) 2L72 4F RTA2NM 20040917000542004091700054EA 2004 9 17 ASOA04437 120040618A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11840AS 7290 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT CARGO FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040917000562004091700056EA 2004 9 17 A6WA200440108 120040805A5300 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31439AW 7753 FOUND DENT AND CREASE IN FUSELAGE SKIN AT FS 760 BETWEEN STRINGERS 8R AND 9R. REMOVED DAMAGE, FABRICATED EXTERNAL DOUBLER FROM 2024-T3 .050 INCH, AND INSTALLED EXTERNAL DOUBLER IAW BRAS EO 601R-53-5200B. (M) 2L72 4F RTA21EA 20040917000572004091700057EU 2004 9 17 ASOA04508 120040714A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11635AS3531 1088 372 DURING AN A-CHECK IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON TH PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040917000582004091700058NM 2004 9 17 USAASB04032 120040317A5210 DOOR BOEING737 737301 1384611NM MAIN PAX OPEN A USAAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 EA19356US 23559 AFTER TAKEOFF, CREW COULD NOT GET THE A/C TO PRESSURIZE. FLT ATTENDANT REPORTED AN AIR LEAK COMING FROM FWD ENTRY DOOR. ALL OTHER INDICATIONS NORMAL. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. MX FOUND FORWARD ENTRY DOOR PARTIALLY OPEN AND FALSLY LOCKED. PERFORMED VISUAL INSPECTION OF DOOR SEAL. OPERATED AND CLOSE DOOR. DOOR CHECKS GOOD. RA NR 2 ENGINE AND PRESSURIZED AIRCRAFT. NO LEAKS NOTD AT FORWARD ENTRY DOOR. MAINTENANCE ALSO FOUND TWELVE INCHES OF AFT CARGO DOOR SEAL BLOWN. REINSTALLED SEAL AND PERFORMED HULL LEAK RATE TEST PER MM 05-51-91. LEAK TEST GOOD. AS A FOLLOW UP, A RIGGING CHECK IS SCHEDULED TO BE ACCOMPLISHED ON THE FORWARD ENTRY DOOR. (M) 2L72 4F RTA16WE 20040917000622004091700062NM 2004 9 17 2004F00328 120040102A3350SG9442 LIGHT BOEING727 7272J0 138407ENM AFT GALLEY DISLODGED A P9RAK NONE O OTHER ININSP/MAINT 1 SO11910PG 22606 FOUND EMERGENCY LIGHTING STRIP IN FRONT OF AFT GALLEY IS PULLED LOOSE FROM FLOOR. SECURED EMERGENCY LIGHTING STRIP IAW SAFTGLO MM 33-60. (M) 2L73 4F RTA3WE 20040917000652004091700065NM 2004 9 17 2004F00330 120040112A3610BACC10DU450 CLAMP BOEING727 727233 138408ANM NR 3 ENGINE LOOSE A PCSAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO17994AJ 20942 FLT CREW REPORTED, AFTER ROTATION, RT DUCT PRESSURE EXCEEDED 100 PSI, ALSO WITH NR 3 ENG BLEED CLOSED FOR APPROX 2 MIN NR 3 ENG STRUT OHEAT LIGHT ILLUMINATED, CREW RETARDED THROTTLE & LIGHT STAYED ILLUMINATED. CREW RETURNED & MADE AN UNEVENTFUL OWEIGHT LANDING. MX PERFORMED AN OWEIGHT LANDING INSP PER MM, NO DEFECTS NOTED. MX TROUBLESHOT & INSP REVEALED PNEUMATIC LEAKS. FOUND NR 3 ENG BLEED VALVE & 13TH STAGE DUCT CLAMPS LOOSE. MX TIGHTENED LOOSE CLAMPS IAW SRM. MX R & R HIGH PRESSURE REGULATOR & 13TH STAGE MODULATING VALVES PER MM. MX RAN ENGINES AT PART POWER & TAKEOFF FOR FIVE MINUTES IAW MM. REPLACED VALVES & TIGHTEN CLAMPS OPS & LEAK CKD NORMAL. A/C RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20040917000682004091700068EA 2004 9 17 COMA0460508 120040907A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01494CA 7765 FLIGHT 5757 DURING PRE FLIGHT INSPECTION, FOUND THE FLOOR EMERGENCY LIGHTING INOPERATIVE, FERRIED AIRCRAFT. REPLACED ALL EMERGENCY BATTERY PACKS. 2L72 4F4 FRTA21EA E15NE 20040917000692004091700069NE 2004 9 17 NACA20040034 220040914A8500 ENGINE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 MALFUNCTIONED A NACAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AL03779TA2299 2299 45529 28737 ABORTED TAKE OFF DUE TO NR 2 ENGINE LOW FUEL FLOW AND LOW BMEP. PERFORMED 30 IN FIELD BARO ENGINE OP CHECK IAW OPS MANUAL SECT. 9.20. ALL PARAMETERS NORMAL, NO DEFECTS NOTED. 2L74 4R4 R A781 5E8 20040917000702004091700070EA 2004 9 17 COMA0460512 120040909A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01912CA 7011 FLAPS FAIL MESSAGE DURING PUSH BACK. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20040917000712004091700071EA 2004 9 17 COMA0460513 120040909A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE EMERGENCY LIGHT LOOSE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01952CA 7092 1ST SEGMENT OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM OPERATION NORMAL. 2L72 4F4 FRTA21EA E15NE 20040917000722004091700072NE 2004 9 17 COMA0460515 220040903A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT ENGINE OVERSERVICED A COMAE ENGINE SHUTDOWN WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO01806CA 7359 RT ENGINE OIL TEMP AT 162 DEGREES CIFSD ENGINE WAS OVER SERVICED BY 4 QTS OIL. REMOVED EXCESS OIL. 2L72 4F4 FRTA21EA E15NE 20040916000082004091600008NM 2004 9 16 2004F00359 120040721A573065B149627 PANEL BOEING747 7472D7B 1384803NM LT WING DELAMINATED B T64RK NONE O OTHER ININSP/MAINT 1 SO03524MC 21784 DURING FA12 A-CHECK ACCOMPLISHING ROUTINE WORK CARD 11M15002 INSPECTION OF LEFT WING UPPER SURFACE, FOUND LEFT LEADING EDGE INBOARD OF NR 1 PYLON PANEL VOIDED UPPER SURFACE WING STATION 1116 PANEL. T64R (M) 2L74 4F RTA20WE 20040916000192004091600019SO 2004 9 16 SIMA200422406 120040801A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21729AE 145343 DURING AN IMBV INSPECTION,T HE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SECTION OF THE FORWARD DIGITAL. FABRICATED TWO DOUBLERS, SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-10 AND 51-40-02. (M) 2L72 4F RTT00011AT 20040916000212004091600021EU 2004 9 16 2004F00315 120040116A2913 PUMP AIRBUS320 A320233 3930329EU YELLOW HYD SYS FAILED A RJEFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23453TA 747 DURING CRUISE, ECAM WARNING MESSAGE HYDRAULIC YELLOW ENGINE NR 2 PUMP LOW PRESS SHOWED ON SCREEN. THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING AT SAL, TECHNICIANS VERIFIED ENGINE HYDRAULIC PUMP PRESSURE PER AMM 29-13-00. A FALSE INDICATION WAS DETECTED, SYSTEM WAS DEVELOPING ITS REQUIRED PRESSURE SHOWED ON THE NORMAL GAGES. THE LOW PRESS INDICATION ON ECAM WAS ENTERED AS DEFERRED ITEM PER MEL 29-30-04. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20040916000272004091600027EA 2004 9 16 2004F00317 120040801A29136619002 PUMP CNDAIRCL600 CL6002D24 1390016EA NR 1 ENGINE LEAKING A FDKAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07906FJ167 15006 THE A/C RETURNED TO THE FIELD WITH THE NR 1 HYD WENT TO ZERO PRESSURE AND QUANTITY. IT WAS DETERMINED THAT THE NR 1 EDP FAILED. MAINTENANCE ALSO FOUND A CRACKED HYD LINE IN THE AFT EQUIPMENT BAY. MAINTENANCE REPLACED THE NR 1 DEP BUT WERE UNABLE TO INSTALL A FLEX LINE DUE TO THE LINE POSITON. CURRENTLY AOG FOR HYDRAULIC LINE. HYDRAULIC LINE TUBE ASSEMBLY P/N MM-670-75620-001. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20040916000382004091600038NM 2004 9 16 USAA040411 120040802A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 FOUND INTERCOSTAL CORRODED 18 INCHES BY 3 INCHES, STATION 377-395 RBL 12. REPAIRED PER BOEING DWG NR 141N5150. (M) 2L72 4F RTA2NM 20040916000402004091600040NM 2004 9 16 UIEA200400124 120040719A36009750304002 THERMAL SWITCH BOEING747 7472D7B 1384803NM RT WING FAILED A UIEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA15524MC 21784 SHORTLY AFTER LEVEL OFF AT FL30.0 RIGHT WING OVERHEAT LIGHT ILLUMINATED. CHECK LIST PERFORMED, LIGHT EXTINGUISHED BEFORE 5 MINUTES CONTINUED AGAIN, COMPLETED CHECKLIST LIGHT STAYED ON NR 3 AND NR 4 BLEED VALVES CLOSED, RIGHT ISOLATION VALVE CLOSED ZERO AIR PRESSURE NR 3 A/C PACK OPEN. CHECK RIGHT WING PYLON NR 3 AND NR 4 FOR LEAKAGE. FOUND LEAKAGE AT LEADING EDGE DRIVE UNIT NR 2 RIGHT DUCT. RIGHT WING AND LEAKAGE OF SEAL OUTBOARD OF L/E NR 2 RIGHT END MANIFOLD. REPLACED SEALS P/N 820-1-200 AND SEAL P/N 600-600 CHECK FOR LEAKAGE. ALL SATISFACTORY IAW 36-11-00. MEASURE WIRING FROM D4644 TO SWITCHES WITH ISOL TESTER ALL SATISFACTORY. CHECKED BLEED VALVE FOR LEAKAGE FOUND NORMAL. MEASURE WIRING WITH LIGHT 2L74 4F RTA20WE 20040916002172004091600217WP 2004 9 16 AALA20040933 120040901A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21408AA 49319 DTW - FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040916002192004091600219NM 2004 9 16 SWAA042449 120040823A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAMS CORRODED AT BS 344, LBL 9, BS 967, RBL 5, AND BS 986-987, LBL 26 TO LBL 35. REPAIRED FLOORBEAMS PER SRM AND ERO. 2L72 4F RTA16WE 20040916002262004091600226NM 2004 9 16 DL73S040839 120040901A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 848. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND PER ER/A 092824-14AD. 2L72 4F RTA16WE 20040917000122004091700012SW 2004 9 17 2004F00374 120040723A2435 BEARING BELL 206 206L1 1182107SW STARTER GEN LOOSE A ALGAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0360WJ 45276 DURING TAKEOFF FROM HA-340 THE TORQUE GUAGE FLUCTUATING 10 PERCENT. MAINTENANCE REMOVED AND REPLACED STARTER GENERATOR. BEARING LOOSE ON THE STARTER GENERATOR CAUSING TORQUE FLUCTUATION. CHANGED FUEL FILTER AND TOOK FUEL SAMPLE AND PERFORMED PNEUMATIC AIR LEAK TEST. PERFORMED ALL WORK IAW 206L-1 AND ROLLS ROYCE C-28 MM. (M) 1G71 3U H2SW 20040917000312004091700031NM 2004 9 17 AMTA200400151 120040211A5610 WINDOW BOEING737 73783N 13844HINM COCKPIT GOUGED A AMTAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL11303TZ 28648 PILOTS SLIDING WINDOW HAS GOUGED FROM CONTACTING HEX BOLTS FWD EDGE OF FRAME, UPPER CORNER. REMOVED AND REPLACED ELFT NR 2 SLIDING WINDOW IAW M/M56-12-11-4. (M) 2L72 4F RTA16WE 20040917000332004091700033WP 2004 9 17 GTIA040652 120040622A5321 FLOORBOARD DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23812NK 48021 FTW - FOUND MAIN CABIN STATION 1117 TO 1174 CENTER FLOOR PANEL HAVE SOFT/MUSHEY AND DAMAGE ON EDGE. FABRICATED CABIN FLOORBOARD. (M) 2L72 4F A6WE 20040917000352004091700035NM 2004 9 17 USAASB04031 120040316A3260189929 UPLOCK SENSOR BOEING737 737301 1384611NM LT MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19576US 23741 ORD - FLT 1082 - ON CLIMB-OUT FROM ORD, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AFTER FOLLOWING ABNORMAL PROCEDURE CHECKLIST, DECISION WAS MADE TO RETURN TO FIELD AT ORD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED LEFT MAIN LANDING GEAR ASSEMBLY AND PERFORMED POSITION INDICATION AND WARNING SYSTEM TEST PER MM 32-61-21. TEST CHECKED GOOD. INSPECTED AIRCRAFT AND FOUND SAFE FOR MAINTENANCE FERRY FLIGHT FROM ORD TO CLT. MAINTENANCE IN CLT REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR PER MM. PERFORMED GEAR SWING. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040917000372004091700037NM 2004 9 17 UIEA200400138 120040802A2810 FUEL TANK BOEING747 7472D7B 1384803NM CENTER WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 FOUND DURING D-CHECK, AT SIN, CORROSION AT WING CENTER SECTION UPPE SKIN AT REAR SPAR BETWEEN BL 0 AND RBL 11.33. CORROSION WAS BLENDED USING A 20:1 RATIO, 125 RHR OR BETTER AND REMAINING THICKINESS TO BE .381 INCH OR GREATER. BLENDED AREA WAS SHOP/FLAP PEENED AND REFINISHED WITH ALODINE 600 AND BMS 10-11, TYPE PRIMER. OPEN HOLES WERE HFEC INSPECTED TO ENSURE NO DEFECTS EXIST. BACB30PT FASTENERS WRE REPLACED WITH BACB30NZ10KX OR BACB30NW10KX HI-LOCKS WITH BACC30M10 COLLARS IN .0005/.0035 INCH INTERFERENCE FIT HOLES. BLENDED AREAS FILLED WITH SEALANT TO PREVENT ACCUMULATION OF MOISTURE. RESTORED FUEL BARRIER WITH MNS 5-81 TYPE 2. (M) 2L74 4F RTA20WE 20040917000392004091700039EA 2004 9 17 ASOA04512 120040714A524234455 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11863AS 7487 DUIRNG AN OVERNIGHT CHECK IN DFW, THE AVIONICS BAY DOOR HANDLE WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE ASSEMBLY. DURING INSTALLATION THE DOOR HANDLE CRACKED AROUND THE FLANGE. MAINTENANCE REMOVED AND REPLACED THE DOOR HANDLE DOOR ASSEMBLY AGAIN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040917000412004091700041WP 2004 9 17 GTIA040680 120040710A71605930645509 NOSE COWL DOUG DC9 DC982 3022082WP NR 2 NACELLE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND RIGHT INLET COWL HAS TWO CRACKS APPROX 8 INCHES IN LENGTH IN MOUNT RING FLANGE, INTERNALLY AT 4 AND 6 O'CLOCK POSITION. REMOVED NR 2 ENGINE INLET. INSTALLED SERVICEABLE NR 2 ENGINE INLET. (M) 2L72 4F A6WE 20040917000422004091700042WP 2004 9 17 GTIA040681 120040708A5230 STOP FITTING DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND FORWARD PIT LOWER DOOR STOP FITTING CRACKED AND DOOR STOP CORRODED. REMOVED CRACKED FITTING. INSTALLED NEW DOOR STOP FITTING. (M) 2L72 4F A6WE 20040917000432004091700043EA 2004 9 17 ASOA04497 120040711A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040917000592004091700059CE 2004 9 17 2004F00325 120040222A5321 FLOOR PANEL LEAR 55 55LEAR 5170702CE AFT FUSELAGE DELAMINATED A EXOAK NONE O OTHER ININSP/MAINT 1 SO17558HJ 048 DURING INSPECTION, FOUND FLOOR WAS DELAMINATING. THE PROBLEM IS A RESULT OF THE TOILET LEAKING AND CAUSING CORROSION, A REQUEST WAS GRANTED FROM LEARJET TO OPERATE A/C UNTIL 2/18/2004. AT WHICH TIME FLOOR WILL BE REPLACED. (M) 2L72 4F A10CE 20040917000742004091700074EA 2004 9 17 COMA0460511 120040909A3230750005000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01951CA5137 7091 GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE. 2L72 4F4 FRTA21EA E15NE 20040917000752004091700075EA 2004 9 17 COMA0460509 120040907A3620 SENSING ELEMENT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT PYLON DAMAGED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01431CA 7472 DURING CLIMB OUT OF RDU RECEIVED A LT 14TH STAGE DUCT WARNING, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE LT PYLON BLEED LOOP SENSING ELEMENT AW59WK. 2L72 4F4 FRTA21EA E15NE 20040917000762004091700076EA 2004 9 17 COMA0460510 120040909A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE ROW 1 LOOSE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01951CA 7091 EMERGENCY FLOOR PATH LIGHTING AT ROW 1 IS INOPERATIVE. SECURED LOOSE TRACK LIGHT SYSTEM, OPERATION NORMAL. 2L72 4F4 FRTA21EA E15NE 20040917000782004091700078NM 2004 9 17 372PA0069 120040909A5315 FLOORBEAM BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 SEVERAL AREAS OF CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 344. REPLACED SECTION OF (T) CAP IAW SRM 53-10-51. 2L72 4F4 FRTA16NE E2GL 20040917000792004091700079WP 2004 9 17 04FDEA02676 120040914A2750 WARNING LIGHT DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL TE FLAPS ILLUMINATED A FDEAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO2568051 47805 AFTER T/O AT 800 FT, HAD FLAP DISAGREE LIGHT ILLUMINATE . RUN RED TABS AND THE LIGHT DID NOT GO OUT. DUMPED APPROX. 20K OF FUEL. FLAPS EXTENDED THE LIGHT GOES OUT. THERE WERE NO ABNORMAL FLT CHARACTERISTICS WITH FLAPS CYCLING OR EXTENDED. T/S PER TAFI 27-50-00 H-VOLTAGE CHECKS AT TERMINALS S3-12 AND S3-43 ARE NORMAL, TAFI POINTS AT FLAP POS. INDICATOR. MEL: A/C RELEASED FOR SERVICE PER MEL/CDL: 27-06-01 CATEGORY: C EXPIRATION: 24SEP04 MEL 27-06-01: INBD FLAP DISAGREE FLAG - INOP. VERIFY AND RECORD IN AML/EAML FLAP OPERATION AND SYMMETRY PRIOR TO EACH DEPARTURE. 2L73 4F4 F A22WE E23EA 20040917000802004091700080EU 2004 9 17 04FDEA02677 120040914A3230D221270005 DAMPENER AIRBUS310 A310 EU GE CFM56 CFM562C 13802NE MLG INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25407FE 254 AFTER TAKEOFF YYC, ATTEMPTED TO RAISE GEAR, ABLE, TO THE INTERLOCK POSITION, INDICATED GEAR DOWN, UNLOCKED TRIED CYCLING GEAR AND CIRCUIT BREAKERS. NO LT GEAR PITCH DAMPENER POPPET EXTENDED. LT GEAR PITCH DAMPER REPLACED IAW AMM 32-11-15-4. NR 2 MAIN WHEEL REMOVED AND RE-INSTALLED IAW AMM12-37-32-0-01. NR 2 BRAKE REMOVED AND RE-INSTALLED IAW AMM 32-42-27-4-1. AXEL JACKED IAW AMM 07-12-00 SYSTEM TEST SERVICEABLE ON PROXIMITY SYS ELECTRONIC UNIT IAW AMM 32-00-00-5 RII:501311 PREMATURE REMOVAL/INSTALLATION OFF MFG D22127000-5 POS L SRL DRG45 TAG 651157. 2L72 4F4 FRTA35EU E2GL 20040917000812004091700081EU 2004 9 17 04FDEA02678 120040914A5347R538D104820200 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 MAIN CARGO DECK AT FRAME 47 BETWEEN TRACKS 1R AND 2R, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK AT FRAME 47 BETWEEN TRACKS 1R AND 2R IAW A310 SRM 51-40-21.**** S/D COMING **** 2L72 4F4 FRTA35EU E13NE 20040917000822004091700082EU 2004 9 17 04FDEA02679 120040914A5347A532782892000 SEAT TRACK AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 DAMAGED SEAT TRACK ADAPTER AT FRAME 61 CENTER LINE REF EA 6-5320-81893. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21 AND EA 6-5320-81893. **** S/D COMING **** 2L72 4F4 FRTA35EU E13NE 20040917000832004091700083EA 2004 9 17 COMA0460514 120040902A3297601R572221PE WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA 7043 FLIGHT 4948 GEAR DISAGREE WARNING DURING APPROACH. COULD NOT DUPLICATE, REPLACED THE NLG DOORS WIRING HARNESS. 2L72 4F4 FRTA21EA E15NE 20040917000842004091700084NM 2004 9 17 372PA0071 120040909A5315654583469 STRAP BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FLOORBEAM CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 STRAP CRACKED ON LOWER SURFACE OF FLOORBEAMS AT BS 312 AND BS 344 AT RBL 32. REPLACED STRAP IAW SRM 51-10-2. 2L72 4F4 FRTA16NE E2GL 20040917000862004091700086NM 2004 9 17 S04J32031 120040805A3244H49X192232PRUT TIRE BOEING747 747400 NM GE CF6 CF680C2* GL NR 11 BURST W SAJFC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP03 AFTER TAKE-OFF, AIRPORT FOUND SOME TIRE DEBRIS ON THE RUNWAY. A FEW MINUTES LATER, PILOT NOTICED THE NR 4 HYD FLUID IS LOSING AND DECIDED TO DIVERT. INITIAL INSPECTION REVEALED NR 11 MAIN GEAR TIRE BURST, FLUID RETURNING TUBE OF RT MAIN GEAR DOOR SEQUENCE VALVE CUT, RT WINGROOT REAR FAIRING DAMAGED, AND ONE HARNESS CLAMP ON RT BODY GEAR BROKEN. IAW RELATED MAINTENANCE CORRECTED THE DEFECTS. DIVERSION RESULTED FROM HYD FLUID LOSS, CAUSED BY THE HYD TUBE CUT. IT IS CONSIDERED AS A RESULT OF TIRE-BURST DEBRIS HITTING. CHI HAS ADVISED THE TIRE MANUFACTURER AND REQUESTED INVOLVING THE INVESTIGATION. 2L74 4F4 FRTA20WE E23EA 20040917000872004091700087NM 2004 9 17 QXEA200400672 120040908A261147305 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE CARGO BAY FAILED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09356PH1559115503 502 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKE-OFF THE CREW RECEIVED AN INTERMITTENT SMOKE DETECTOR WARNING FOR THE BAGGAGE COMPARTMENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH SMOKE DETECTORS IN THE BAGGAGE COMPARTMENT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040917000882004091700088NE 2004 9 17 DHL2004805011 220040914A7200 MEC DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 3 ENGINE SHUTDOWN A DHLAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 SO01805DH 46125 AFTER LANDING DURING TAXI INTO RAMP NR 3 ENGINE HAD AN UNCOMMANDED SHUTDOWN. REPLACED MEC IAW M/M 73-21-10. PERFORMED RUN AND POWER ASSURANCE IAW JRH 13.3 AND M/M 71-00-00. OPS AND LEAK CHECKS SERVICEABLE. 2L74 4F4 FRT4A25 E2GL 20040917000892004091700089NM 2004 9 17 CALA0400635 120040912A53306518420 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714337 23575 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 264 ABOVE S19L. THE SKIN WAS REPAIRED IAW ECRA 5330-03366. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW PART III WITHIN 50 FLIGHT CYCLES. 2L72 4F4 FRTA16WE E2GL 20040917000912004091700091NM 2004 9 17 CALA0400627 120040903A245091252ZC7C4001 RELAY BOEING737 737524 1384721NM GE CFM56 CFM563B1 13802NE P6 PANEL BURNED A CALAO OTHER O OTHER APAPPROACH 1 SW2717640 28901 ON FINAL APPROACH, A/C LOST MULTIPLE ELECTRICAL COMPONENTS INCLUDING NR 1 RADIO, NR 1 & 2 FWD FUEL PUMPS, ANTI-SKID, TR-1 SHOWED ZERO, AUTO BRAKE, YAW DAMPER, NR 1 ELEC HYD, EMERGENCY EXIT LIGHTS, NR 1 N 2, & FUEL FLOW GUAGE. A/C LANDED W/OUT PROBLEM. NR 1 TR CB PHASE A NR C806 FOUND POPPED. MX FOUND A1 CONNECTOR & CONTACT ON TRANSFER BUSS R3 RELAY BURNED. WIRING REPAIRED IAW SWP 20-10-13. R3 RELAY R/R, & TESTED IAW MM 24-21-00-501. NR 1 TR R/R AS A PRECAUTION IAW MM 24-21--31-401. OPS CHK GOOD. ENGINEERING CONCLUDED THAT EITHER THE TERMINAL LUG WAS LOOSE OR POSSIBLY ELECTRICAL DAMAGE OF A1 CONTACT POINTERS OF THE RELAY RESULTED DUE TO FREQUENT CONTACT ARCING. 2L72 4F4 FRTA16WE E2GL 20040917000932004091700093NM 2004 9 17 CALA0400638 120040902A5210 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE PAX DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND A .5 INCH CRACK IN THE MID INNER SKIN PANEL OF THE FORWARD ENTRY DOOR. THE SKIN WAS REPAIRED IAW ECRA 5211-01072. 2L72 4F4 FRTA16WE E2GL 20040917000942004091700094WP 2004 9 17 P9RA20040040 120040915A33506011779 POWER SUPPLY DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11135NJ 49440 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW MM. 2L72 4F4 F A6WE E2EA 20040917000962004091700096EA 2004 9 17 04258667 120040914A3220 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NOSE INOPERATIVE A VTZAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 EA27667BR 7535 NOSE GEAR DISAGREE. PERFORM TROUBLE SHOOTING FOR NOSE GEAR DISAGREE. PERFORM GEAR SWINGS. 2L72 4F4 FRTA21EA E15NE 20040917000972004091700097NM 2004 9 17 QXEA200400653 120040826A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 100 POROUS A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 RT OB SEAT TRACK, PITTED BETWEEN X367.75 AND X374.0, TRACK 19. BLENDED AREA OF PITTING AND FOUND TO BE OUT OF LIMITS. INSTALLED NEW TRACK IAW SRM 51-42-05 AND 51-40-15. 2H72 4T4 TRTA13NM E00062EN 20040917000982004091700098NM 2004 9 17 QXEA200400666 120040910A30104100S00502 VALVE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA DE-ICE SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09401QX3315 272 4031 NR 2336 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED, COMPLIED WITH CHECKLIST. NOTED THE SECOND IB LIGHT SEGMENT ON RT WING NOT ILLUMINATING DURING CYCLE. MAINTENANCE REPLACED NR 2 DUCAL DISTRIBUTION VALVE IAW AMM 30-11-16, PAGES 401-408. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040917000992004091700099NM 2004 9 17 QXEA200400652 120040829A5730 ACCESS PANEL BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 FUEL PANEL 622CT HAS CORROSION ON BOTTOM SURFACE AROUND SCREW HOLES. BLENDED CORROSION AREA IAW SRM 57-10-35-350-802, PARAGRAPH 1-6B(4). FOUND BLENDED AREA TO BE OUT OF LIMITS. REPLACED FUEL PANEL 622CT WITH NEW FROM STOCK. 2H72 4T4 TRTA13NM E00062EN 20040917001002004091700100NM 2004 9 17 QXEA200400651 120040829A5730 ACCESS PANEL BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 RT WING FUEL PANEL 624AT HAS CORROSION ON BOTTOM IB END IN TWO PLACES. BLENDED DAMAGED AREA IAW HDC 8400 SRM 57-20-35-350-801, PARAGRAPPH 1, 2, 3. 4. 5, ;A B1-4. REMOVED PANEL TOP SURGACE PAINT FOR MEASUREMENTS. PERFORMED THICKNESS CHECK OF PANEL AT BLENDED AREA FOUND TO OUT OF LIMITS IAW SRM 57-20-35-992-801. REPLACED WITH SERVICEABLE PANEL. 2H72 4T4 TRTA13NM E00062EN 20040917001042004091700104NM 2004 9 17 UPS04443115 120040817A571465B156972 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE CENTER TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT RBL 80 IN. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 PG8. 2L74 4F4 FRTA20WE E3NE 20040917001062004091700106NM 2004 9 17 UPS04443117 120040817A571465B1569712 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE CENTER TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 35. SHEAR TIE FTG REPLACED IAW SRM 51-10-01 P. 8. 2L74 4F4 FRTA20WE E3NE 20040917001082004091700108NM 2004 9 17 UPS04543126 120040914A5230 HINGE BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE CARGO DOOR BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01425UP 25370 MCD HINGE FWD AND AFT WORN FIFTH FROM FWD HINGE HAS THREE BROKEN HINGES. ACCOMPLISHED EO B757-5230-17511-B, APPENDIX A, REQUIRES DEFERRAL D287700 WAITING FOR NRC 431008. VISUALLY CHECKED ALL MCD PIANO HINGES ALL OTHER PIANO HINGES ARE IN SERVICEABLE CONDITION. REMOVED #5 MCD HINGE ASSY INSTALLED #5 PIAN O HINGE IAW SRM 51-40-2. 2L72 4F4 FRTA2NM E17NE 20040917001102004091700110WP 2004 9 17 UPS04843120 120040818A575356423422 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE TE FLAP HINGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C1, RT FLAP HINGE 3 FITTING HAS APPROX 6-8 IN LONG CRACK BETWEEN TRACK LANDS. REMOVED FLAP HINGE 3 FITTING. IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. FABED IAW SAA SK 708-840-2 FITTING SAME MFG P/N 5642342-2, FLAP LINK SUPPORT FITTING FROM 7050-T7451, AMS 4050,6.0 IN MAX THICKNESS. INSTALLED FITTING IAW SRM 51-1-20D AND 51-1-21. 2L74 4F4 FRT4A25 E2GL 20040917001122004091700112WP 2004 9 17 UPS04843122 120040913A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01802UP 46100 EMERGENCY LIGHTS OUT, REPLACED LIGHTING BATTERY PACK, OPS NORMAL. 2L74 4F4 FRT4A25 E2GL 20040917001172004091700117NM 2004 9 17 AWXA200400975 120040903A32601061226211 CIRCUIT CARD BOEING737 737301 1384611NM ZONE 205 FAULTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28324AW 23261 ON CLIMB OUT, ENROUTE, TAKEOFF CONFIGURATION WARNING HORN SOUNDED AT APPROXIMATELY 7000 FEET AND REMAINED ON UNTIL THROTTLES RETARDED TO IDLE, DIVERTED FOR REPAIR. MAINTENANCE REMOVED AND REPLACED AIR SENSING SQUAT SWITCH CIRCUIT CARD M0991 IAW BMM 32-09-20-724-015. PERFORMED TAKEOFF WARNING SYSTEM TEST IAW T/C A1B31009, TEST WAS GOOD. 2L72 4F RTA16WE 20040917001182004091700118NM 2004 9 17 04242412 120040829A8012 START VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE RIGHT DEFECTIVE A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27412FJ 3167 RT ATS VALVE FAILED OPEN ON DESCENT. REMOVED AND REPLACED ENGINE ATS VALVE. OPS CHECK GOOD IAW JIC 80-10-10. 2H72 4T4 FRTA55NM E35NE 20040917001202004091700120CE 2004 9 17 ACE08282004 120040828A53401144300665 STRINGER CLIP BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE FUSELAGE MISSING E YADAK NONE O OTHER ININSP/MAINT 1 AL03113AX42322 UC41 DURING SCHEDULED STRUCTURAL INSPECTION OF THE AREA, FOUND STRINGER CLIP PN. 114-430066-5 NEVER INSTALLED AND THE BULKHEAD AT FS 363.25 HAD CRACKS IN THE FLANGE ABOVE AND BELOW THE MISSING CLIP LOCATION. 2L72 4T4 TRTA24CE E4EA 20040917001212004091700121SO 2004 9 17 C2XA04IA107 120040823A3350110049 CHARGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714902 145496 DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE BACK HALF OF THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR (4) EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040917001222004091700122WP 2004 9 17 01083004 120040818A261259585801 FIRE LOOP DOUG DC9 DC9 3022002WP PWA JT8 JT8D9A 52048NE LT ENGINE OPEN A A4JAO OTHER J WARNING INDICATION CRCRUISE 1 SO35934LK 48157 LT ENGINE LOOP A (FIRE) LIGHT ILLUMINATED IN FLIGHT, FIRE DETECTOR LOOP ANNUNCIATOR, AND MASTER CAUTION LIGHT. FOUND SENSOR ELEMENT GROUND OUT. REPOSITIONED ELEMENT, OPS CHECK IAW MM 26-10-0. CHECKS GOOD. 2L72 4F4 F A6WE E2EA 20040917001232004091700123NM 2004 9 17 UPS04443051 120040819A5320 FLOOR SUPPORT BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, U/D BS 405-440 LBL 75-78, FLOOR SUPPORT ANGLE CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 INCH X 2 INCHES X 2 INCHES EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 435- BS 440 FLR SUPPORT ANGLE REPAIRED REF SRM 51-40-04 FIG 3, CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F4 FRTA20WE E3NE 20040917001242004091700124NM 2004 9 17 UPS04443052 120040818A5313 STRINGER BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 1 INSPECTION TYPE: C, M/D BS 980-1000 RT STR 14 STR END FOUND CRACKED. M/D BS 980-1000 STR 14R REPAIRED IAW SRM 53-10-03 FIG. 4. 2L74 4F4 FRTA20WE E3NE 20040917001252004091700125NM 2004 9 17 UPS04443053 120040816A531065B104865 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D BS 400, STR 13-14R FRAME OB ATTACH, SHEAR TIE FOUND CRACKED. BS 400 STR 13-14R FRAME OB ATTACH SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8. 2L74 4F4 FRTA20WE E3NE 20040917001262004091700126NM 2004 9 17 UPS04443055 120040817A5313 STRINGER BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D BS 2180-2200 LT STR 10 STR END FOUND CRACKED. M/D BS 2180-2200 LT STR 10 REPAIRED IAW SRM 53-10-03 FIG 13. 2L74 4F4 FRTA20WE E3NE 20040917001272004091700127NM 2004 9 17 UPS04443069 120040818A5313 STRINGER BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D- BS 1350-1370 RT STR 6 FOUND CRACKED AS MARKED. M/D- BS 1350-1370 RT STR 6 REPAIRED IAW SRM 53-10-03 FIG.5. 2L74 4F4 FRTA20WE E3NE 20040917001312004091700131NM 2004 9 17 UPS04443073 120040906A3350 BATTERY PACK BOEING747 747SR46 1384816NM PWA JT9 JT9D7A 52054NE EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 EMERGENCY LIGHT INOPERATIVE, PASSENGER AREA. REPLACED BATTERY PACK, OPS CHECK GOOD. 2L74 4F4 FRTA20WE E20EA 20040917001332004091700133EU 2004 9 17 AWXA200400946 120040815A5320D5347112420100 SHEAR PLATE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, STR 24 RT. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FR 69 TO FR 70, STR 24 RT; FABRICATED A NEW REPLACEMENT SHEAR PLATE, AND INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040917001342004091700134EU 2004 9 17 AWXA200400947 120040814A5320D5311282720000 DUMMY RAIL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON DUMMY RAIL Y503 LT BETWEEN FR 14 AND FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 LT FROM FR 14 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL, AND INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040917001352004091700135EU 2004 9 17 AWXA200400948 120040813A5542 SKIN AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE RUDDER ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK FOUND THE LT SIDE OF RUDDER DELAMINATED 16 INCHES FROM TOP, RUDDER STA 569 LT. MAINTENANCE CUTOUT DAMAGED AREA ON LT SIDE OF RUDDER 16 INCHES FROM TOP; PERFORMED BOND REPAIR IAW A320 SRM 55-41-00, FIG. 218, PG. 327-328. 2L72 4F4 FRTA28NM E311NE 20040917001362004091700136EU 2004 9 17 AWXA200400949 120040815A5321D5367005300100 FLOOR PANEL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK FOUND THE FLOOR PANEL 262 EF DELAMINATED, FR 66 - FR 68, Y765 R/H - Y1292 RT. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 262 EF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670053 AND A320 SRM 53-02-00, FIG. 209. 2L72 4F4 FRTA28NM E311NE 20040917001372004091700137EU 2004 9 17 AWXA200400950 120040814A5321D5367004800400 FLOOR PANEL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK FOUND GALLEY FLOOR PANEL 261 DF DELAMINATED, FR 66 - FR 68, Y765 L/H - Y765 RT. MAINTENANCE REMOVED DELAMINATED FLOOR PANEL 261 DF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670048 AND A320 SRM 53-02-00, FIG. 209. 2L72 4F4 FRTA28NM E311NE 20040917001382004091700138EU 2004 9 17 AWXA200400951 120040821A5321D5367002200000 FLOOR PANEL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK A 4 INCH CRACK WAS FOUND IN FLOOR PANEL 251 AF, FR 47 - FR 51, Y254 LT - Y254 RT. MAINTENANCE REMOVED CRACKED FLOOR PANEL 251 AF; FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 10D53670022 AND A320 SRM 53-02-00, FIG. 209. 2L72 4F4 FRTA28NM E311NE 20040917001392004091700139EU 2004 9 17 AWXA200400952 120040811A5270DHE1141 PROXIMITY SWITCH AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE L-2 DOOR BROKEN A AWXAK NONE P NO WARNING INDICATION ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK THE L-2 DOOR WARNING LIGHT DID NOT ILLUMINATE WHEN DOOR WAS ARMED AND HANDLE WAS RAISED. MAINTENANCE REMOVED AND REPLACED EMERGENCY DOOR HANDLE SHAFT PROXIMITY SWITCH IAW A320 AMM SUBTASK 52-71-11-020-051, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20040917001402004091700140EU 2004 9 17 AWXA200400953 120040820A5310D53472133202 BEAM AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y765 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT AT FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00. 2L72 4F4 FRTA28NM E311NE 20040917001412004091700141EU 2004 9 17 AWXA200400954 120040825A5321D5361060500100 FLOOR PANEL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK CORROSION WAS FOUND LOWER SIDE OF FLOOR PANEL 222 FF, FR 16, FR 20, RBL 45, RBL 60. MAINTENANCE REMOVED CORROSION ON LOWER SURFACE OF FLOOR PANEL 222 FF; FABRICATED A REPAIR DOUBLER; INSTALLED DOUBLER ON LOWER SURFACE OF FLOOR PANEL IAW AWA ER 26-5312-00151-BA1. 2L72 4F4 FRTA28NM E40NE 20040917001422004091700142EU 2004 9 17 AWXA200400955 120040820A5320D5348001921695 WEB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK A 1 INCH CRACK WAS FOUND LT AFT TRAY (WEB) OB OF Y1292 LT, AFT OF FR 68. MAINTENANCE REMOVED CRACKED LT AFT TRAY AT Y1292 LT, FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20040917001432004091700143EU 2004 9 17 AWXA200400956 120040820A5320D53480019217 WEB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK A 4 INCH CRACK WAS FOUND IN RT AFT TRAY (WEB) OB OF Y1292 RT, AFT OF FR 68. MAINTENANCE REMOVED CRACKED RT AFT TRAY AT Y1292 RT, FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20040917001442004091700144 2004 9 17 P9RA20040036 420040902A2565387 BULB BOEING757 757231 1384950NM PWA 2037 PW2037 NE 4L DOOR SLIDE INOPERATIVE A P9RAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO11720TW 30319 DOOR 4L SLIDE ARMED LIGHT INOPERATIVE. RELAMPED 4L SLIDE ARMED LIGHT SOCKET. 2L72 4F4 FRTA2NM E17NE 20040920000042004092000004NM 2004 9 20 04FDEA02610 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000072004092000007NM 2004 9 20 04FDEA02613 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000102004092000010NM 2004 9 20 QXEA200400673 120040908A5210 DOOR DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE ZONE 200 OBSTRUCTED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09362PH14312 518 MAINTENANCE FOUND THE MAIN CABIN DOOR DIFFICULT TO OPEN. UPON INSPECTION, MAINTENANCE FOUND THE FORWARD DRAFT WALL HITTING THE DOOR. THE WALL RETAINING SCREWS WERE TIGHTENED AND PROPER CLEARANCE WAS OBTAINED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040920000122004092000012NM 2004 9 20 QXEA00669 120040912A335040005130003 SWITCH DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE EMERGENCY LIGHT INTERMITTENT A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09379PH 530 FOUND FA EMERGENCY LIGHT SWITCH INTERMITTENT. MAINTENANCE REPLACED LIGHT SWITCH. ALSO REPLACED BATTERY PACKS PS1, PS2, PS3, PS6. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040920000132004092000013SO 2004 9 20 C2XA04BT096 120040908A33501317 BULB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713913 145438 DURING 1A INSPECTION MAINTENANCE FOUND THE RT OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT BULB IAW AMM NR 33-50-10. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040920000162004092000016SO 2004 9 20 CHQA000554 120040911A3350 BULB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11976RP 145322 LT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACE LT OVERWING EMERGENCY EXIT LIGHT BULB IAW MFG 145 AMM 33-50-07. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040920000202004092000020NM 2004 9 20 F3LA200400097 120040916A5315 FLOORBEAM BOEING737 7373L9 1384470NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN STA 294.5 AND 312, 10.5 INCHES FROM CENTER LT, CORRODED AT STA 312 END. REMOVED UPPER T-CHORD ON FLOOR SUPPORT AT LBL 10.5, STA 294.5 THRU 312, AND INSTALLED NEW UPPER T-CHORD IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20040920000222004092000022NM 2004 9 20 P5CA0401187 120040908A21337968853002 CONTROL UNIT BOEING747 74746NF 13848BTNM OUTFLOW VALVE INOPERATIVE A P5CAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP23453PA 30811 STATUS MESSAGE (OUTFLOW VALVE LT SIDE) APPEARED DURING CRUISE. BOTH OUTFLOW VALVES WOULD NOT OPERATE IN AUTO. REMOVED AND REPLACED LT SIDE ICU. 2L74 4F RTA20WE 20040920000232004092000023NM 2004 9 20 P5CA0401188 120040908A21337242822 ACTUATOR BOEING747 74746NF 13848BTNM OUTFLOW VALVE INOPERATIVE A P5CAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP23453PA 30811 STATUS MESSAGE (OUTFLOW VALVE RT SIDE) APPEARED DURING CRUISE, BOTH OUT FLOW VALVES WOULD NOT OPERATE IN AUTO. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR. 2L74 4F RTA20WE 20040920000242004092000024NE 2004 9 20 080963 220040816A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT FAILED A UHLAA UNSCHED LANDING RMJPARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION CLCLIMB 1 GL17123XS 123XS 108 WHILE CLIMBING THROUGH 6500 LT ENGINE TORQUE WENT ERRATIC AND ITT SPIKED TO 940 POSSIBLY 960 SHUTDOWN AND RETURNED TO THE FIELD. 2L72 4T4 TRTA52EU E8NE6 20040920000302004092000030EU 2004 9 20 04FDEA02675 120040911A5320 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 MCD AT FR 53 BETWEEN SEAT TRACKS 2L AND 3L, DUMMY TRACK IS CRACKED UNDERNEATH AT T-CAP RADIUS. REMOVED AND REPLACED CROSSBEAM, P/N A5381293420000 IAW A310 SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040920000312004092000031NM 2004 9 20 04240409 120040827A7930 GASKET DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE WORN A VTZAO OTHER J WARNING INDICATION CRCRUISE 1 EA27409FJ 3161 LT ENGINE OIL PRESSURE FLUCTUATING INTERMITTENTLY. REPAIRED BREATHER GASKET AND DID ENGINE RUN TEST. OPS CHECK GOOD. IAW 79-31-00 2H72 4T4 FRTA55NM E35NE 20040920000322004092000032NM 2004 9 20 QXEA200400671 120040908A2910 LINE DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE NR 1 HYD SYS LEAKING A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09365PH13600 526 FLIGHT RETURNED TO FIELD AFTER THE NR 1 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLEX LINE FROM THE ANTI SKID VALVE TO THE PRESSURE MANIFOLD. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040920000332004092000033NM 2004 9 20 HNAA0400118 120040901A291082950010273 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 HYD SYS CRACKED A HNAAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 EA07825EX 388 FLIGHT NR 3955, REPORTED THE NR 1 HYDRAULIC CONTENTS DROPPING ON LANDING. RUDDER ISO VALVE LIGHT ILLUMINATED THEN WENT OUT. FLIGHT LANDED WITHOUT INCIDENT. FLUID WAS NOTED AS LEAKING FROM THE LT FLAP AREA. MAINTENANCE FOUND THE SPOILER LIFT DUMP PRESSURE LINE TO BE CRACKED AND LEAKING. LINE WAS REPLACED AND THE AREA CLEANED AND OPERATIONAL CHECKS CARRIED OUT, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040920000342004092000034EU 2004 9 20 XNOA1200 120040916A3244 TIRE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE MLG FAILED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23474AS 219 DURING TAXI, HEARD LOUD BANG. SUSPECT TIRE BLOWN. (STATUS: ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20040920000352004092000035EU 2004 9 20 AWXA200400941 120040830A3350321452 EPSU AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE ZONE 263 FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28628AW47971 67 FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHTS IN AFT GALLEY WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20040920000362004092000036EU 2004 9 20 AWXA200400942 120040816A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE SEAT ROW 7 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28650AW 856 DURING P-05 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE FOUND A GROUND WIRE AT LIGHT ASSEMBLY CONNECTOR SEAT ROW 7 LT BROKEN, RE-TERMINATED GROUND WIRE, EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20040920000372004092000037NM 2004 9 20 AWXA200400943 120040822A3350321430 BATTERY AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE EMERGENCY LIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28823AW 1463 DURING P-06 CHECK EMERGENCY LIGHT SYSTEM TEST THE SYSTEM OK LIGHT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LT AND RT OVER WING BATTERY PACKS AT EMERGENCY POWER SUPPLY UNITS 11WL AND 12WL, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20040920000402004092000040NM 2004 9 20 042424251 120040829A2121 SWITCH DORNERDO32 DO328300 NM PWA 306 PW306B NE RECIRC FAN BURNED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27425FJ 3189 BURNING ODOR IN CABIN AFTER GEAR RETRACTION. PSBL SMOKE IN CABIN. MECHANIC FOUND DC TIE SWITCH AND RECIRCULATION FAN SWITCH OUT, RESET SWITCHES, PERFORMED OPS CHECK ON BOTH SYSTEMS. NO DEFECT NOTED IAW 24-10-00 AND 21-22-00. 2H72 4T4 FRTA55NM E35NE 20040920000412004092000041SO 2004 9 20 C2XA04CL085 120040823A33501317 BULB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713553 145585 CREW REPORTED THAT THE EMERGENCY LIGHT AT ROW 3 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB IN THE EMERGENCY LIGHT. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20040920000422004092000042NM 2004 9 20 04242428 120040829A3350 BATTERY DORNERDO32 DO328300 NM PWA 306 PW306B NE EMERGENCY LIGHT DEFECTIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27428FJ 3193 FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED 4LK EMERGENCY BATTERY. OPS CHECK GOOD IAW 33-51-01. 2H72 4T4 FRTA55NM E35NE 20040920000442004092000044EU 2004 9 20 AWXA200400957 120040815A5347D53472209200 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON SEAT RAIL BEAM AT Y1292 RT, BETWEEN FR 64 AND FR 66. MAINTENANCE REMOVED CORRODED SEAT RAIL BEAM FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040920000452004092000045CE 2004 9 20 DXTA200400390 120040912A3240 B-NUT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE BRAKE SYS LOOSE E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL07315QS 5600315 DURING TAXI ON CO-PILOTS SIDE, LT BRAKE PEDAL GOES NEARLY TO THE FLOOR BEFORE BRAKING ACTION IS FELT. INSPECTED ALL BRAKE MASTER CYLINDERS, FOUND PILOT LT PEDAL MASTER LEAKING. TIGHTENED B-NUT AND BLED BRAKE SYSTEM, NO LEAKS ON OTHER MASTER CYLINDERS OR ON BRAKES, SERVICED BRAKE RESERVOIR. TAXIED AIRCRAFT WITH PILOTS BRAKES OPERATING NORMALLY IAW 560 MM CHAPTER 32-42-02. 2L72 4F4 FRTA22CE E25EA 20040920000492004092000049EA 2004 9 20 VJ02004F00000 220040721A7310LW131754340 HOSE PIPER PA32 PA32300 7103212SO LYC O540 IO540* 41532EA FUEL SYSTEM FAILED E VJ0AO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 NM133014X 327940094 DURING OWNER REQUESTED OIL CHANGE FOUND LW-13175-4-340 HOSE GUSHING FUEL ON TO ENGINE. HOSE FAILED OVER 10 INCH SECTION. INSTALLED NEW TSO-C53A TYPE D HOSE. FAILED HOSE WAS ORIGINAL INSTALLED AT MFG OF AIRCRAFT. HOSE MFG 2Q78, OLD BLACK RUBBER STYLE. IF AC HAD ATTEMPTED FLIGHT A FIRE WAS HIGHLY PROBABLE. OWNER ADVISED TO HAVE ALL HOSE CHANGED AT NEXT INSPECTION. (NM09200412025) 1L71 3O3 O A3SO 1E4 20040920000712004092000071SW 2004 9 20 HJL2004F00000 120040712A32335630923 SPRING MOONEYM20 M20K 5870220SW CONT O360 TSIO360* 17025SO MLG ACTUATOR BROKEN D HJLAO OTHER O OTHER NRNOT REPORTED 1 SW17252YE 251081 LANDING GEAR ACTUATOR, PN R5329M24-1, OR MFG AC PN 880037-507, WOULD NOT FUNCTION MANUALLY OR ELECTRICALLY. ACTUATOR WAS SENT FOR INSPECTION. AFTER VERIFYING THAT ACTUATOR WOULD NOT FUNCTION, THE ACTUATOR WAS OPENED, INSPECTED, AND THE TORSION SPRING WAS FOUND TO HAVE BOTH TANGS BROKEN OFF OF SPRING. 1L71 3O3 O 2A3 E9CE 20040920000722004092000072CE 2004 9 20 CTU2004F00000 120040629A561010138402515 WINDSCREEN BEECH 90 C90 1152913CE PWA PT6 PT6A21 52043EA MCAULY4HFR344HFR34C762 NE COCKPIT CRACKED B CTURO OTHER O OTHER NRNOT REPORTED 1 GL21502SE1528 LJ740 PCE24357 891397 LT WINDSCREEN CRACKED DURING CRUISE, AT AN ALTITUDE OF BETWEEN 12,000 AND 16,000 FEET. FLIGHT WAS CONDUCTED AT NIGHT TIME WHILE ON AN IFR FLIGHT PLAN. AIRCRAFT WAS BEING OPERATED AS A LIFE FLIGHT. FLIGHT WAS CONDUCTED NORMALLY TO THE DESTINATION AIRPORT, NO EMERGENCY ACTIONS WERE REQUIRED. 1L72 3T4 T 3A20 E4EA 6 C3PNE 20040920000732004092000073EU 2004 9 20 JGV2004F00006 120040714A2822142G1243 VALVE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE73160 NE FUEL SYSTEM CRACKED B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE09128M 276 FUEL SUMP VERTICAL UPRIGHT FOR VALVE HOUSING. CRACKED THRU LOWER SOLDER WELD. FOUND AFTER SCREEN REMOVAL. CAUSE WELDING TEMP OR MATERIAL. DO NOT WELD ON SUMPS AND INCREASE MATERIAL THICKNESS. 2L73 4F4 F A46EU E1NM 20040920000752004092000075NM 2004 9 20 ASMF200408009 120040809A2150 A/C PACK BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LEFT INOPERATIVE W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23806AM 26273 CAPTAIN REPORTED, AFTER ENGINE STARTED (LT ENGINE BLEED) LIGHT TURNED ON AND LT AIR CONDITIONING PACKAGE WAS INOPERATIVE. ENGINE WAS ACCELERATED, BLEED SWITCH WAS RESEATED AND FAIL CONTINUE. ENGINE BLEED SWITCH WAS RESEATED AGAIN AND ENGINE WAS ACCELERATED, (LT ENGINE BLEED) LIGHT TURNED OFF AND LT AIR CONDITIONING PACKAGE WAS OPERATIVE IAW MM 36-10-00, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20040920000762004092000076NE 2004 9 20 ASMF200408019 220040821A7510320115 SHUTOFF VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFK NONE J WARNING INDICATION ININSP/MAINT 1 SW23838AM3221 49397 718220 CAPTAIN REPORTED, RT ENGINE NOSE COWLING ANTI-ICE VALVE INOPERATIVE, CIRCUIT BREAKER L-30 WAS ACTIVATED AND (R ENGINE ANTI-ICE) AND (R ENGINE VALVE) LIGHTS TURNED ON. NOSE COWLING ANTI-ICE VALVE WAS REPLACED IAW MM 75-10-03, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040920000792004092000079EU 2004 9 20 KBM2004F00118 120040609A6520350A27191004 CONTROL TUBE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 CHAFED CONTROL TUBE, WEAR SLEEVE WORN THRU, FURTHER INSPECTION OF TUBE FOUND WEAR TO BE WITHIN LIMITS. REPLACED ROD WITH SERVICEABLE UNIT. NEW HEATSHRINK OR WEAR SLEEVES INSTALLED. 1G71 3U3 U H9EU E19EU 20040920000812004092000081WP 2004 9 20 COOSDR040004 120040630A5330 SKIN DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE FUSELAGE CRACKED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 FUSELAGE NOSE SECTION, Y STA 215 FWD PASSENGER ENTRANCE DOOR, HOLD OPEN PIN-CUTOUT SKIN CRACKED. 2L74 4F4 F 4A25 1E8 20040920000822004092000082EU 2004 9 20 KBM2004F00115 120040320A78100292808740 STRAP SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE EXHAUST WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH 3141 EXHAUST HEAT SHRINK STRAP WORN. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040920000832004092000083NE 2004 9 20 KBM2004F00122 220040209A74219550175400 IGNITER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE WEAK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 IGNITER, WEAK START IN MORNING FIRST FLIGHT. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20040920000842004092000084WP 2004 9 20 ASMF200406033 120040629A2697 WIRE DOUG DC9 DC987 3022087WP SENSOR FAILED W ASMFED ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW23205AM 05101 49405 AIRCRAFT RETURNED TO PLATFORM, "LEFT AIR COND SUPPLY TEMP HI" LIGHT TURNED ON. BREAKER B1-251 WAS RESEATED, TEMPERATURE SENSOR AND THERMAL SWITCH WERE DISCONNECTED AND FAIL CONTINUE. ENGINES WERE SHUTDOWN AND LIGHT WAS DEFERRED IAW MEL 21-2. DURING OVERNIGHT SERVICE, SENSOR WIRING WAS REPAIRED IAW MM 20-50-01 AND WDM 21-61-04, TEST CORRECT. 2L72 4F RTA6WE 20040920000902004092000090NM 2004 9 20 WVE2004F00020 120040613A53116003603024 FRAME BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED B WVERO OTHER O OTHER NRNOT REPORTED 1 EA09503SW 24180 LT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1 INCH LING IN RADIUS OF FRAME FLANGE. POSSIBLE STRESS RELIEF CRACK. REPAIR IAW REO 601R-53-61-193 REV A. (EA09200402463) 2L72 4F4 FRTA16WE E2GL 20040920000932004092000093 2004 9 20 KBM2004F00178 420040517A3120704A47320011 CLOCK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INTERMITTENT E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 8 DAY CLOCK, INTERMITTENT. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040920000942004092000094NE 2004 9 20 KBM2004F00181 220040702A7230 TURBINE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 9692 N1 TURBINE RUB. REMOVED ASSY AND INSTALLED RENTAL 9301R. 1G71 3U3 U H9EU E19EU 20040920001012004092000101SW 2004 9 20 MV5RO55N 120040607A32203300385 BELLCRANK GULSTM690TP 690A 0141722SW GARRTTTPE331TPE3315 01514WP ROD END ATTACH FAILED B MV5RO OTHER O OTHER NRNOT REPORTED 1 GL11848CE7008 11303 THE BELLCRANK FOR THE LT NOSE GEAR AFT DOOR FAILED/ CRACKED AT THE ROD END UPPER ATTACH POINT AND FELL OVER IN THE WHEEL WELL WHILE THE GEAR WAS IN THE UP POSITION. WHEN THE DOWN POSITION WAS SELECTED THE GEAR COULD NOT EXTEND DUE TO THE ROD BEING IN THE WAY. FATIGUE OF THE BELLCRANK IS SUSPECT FOR THE FAILURE. (GL11200411826) 1H72 3T4 T 2A4 E4WE 20040916000692004091600069NM 2004 9 16 SWAA042614 120040909A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040916000712004091600071NM 2004 9 16 SWAA042616 120040909A3350311500 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 2 DEF, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040916000732004091600073NM 2004 9 16 SWAA042618 120040909A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040916000752004091600075NM 2004 9 16 DL76P040815 120040827A2432BA0601 BATTERY BOEING767 767332 1382001NM APU FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27143DA 25991 BURNING SMELL IN AFT PART OF CABIN APU RUNNING WITH PACKS ON. FOUND APU BATTERY FAILURE CAUSING ELECTRICAL SMELL WITH ASSOCIATED APU BATTERY CHARGER FAILED. REPLACED BATTERY AND CHARGER. 2L72 4F RTA1NM 20040916000782004091600078GL 2004 9 16 DL764040818 220040824A7297 WIRE HARNESS BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 2 ENGINE ARCED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27828MH 29699 706193 RT ELECTRIC HYD DEMAND PUMP INOP. REPLACED RT ELECTRIC UNIT, NO HELP. REPLACED RT PUMP, NO HELP. VERIFIED WIRING FROM ELECTRIC UNIT M896 TO TB 5042 115 AVAIL AT ALL TERMS. FOUND APPROX 98 AT PIN B OF D486 WIRING NEEDS TO BE MEGGED FROM TB 5042 TO D486. WIRE W288-002-02 NO CONTINUITY FROM D486 TO TB5042. FOUND HARNESS W288 ARCING TO RT ENG O/B PYLON FUSE PIN. REMOVED MIDSPAR FUSE PIN PER MM. SPLICED NEW WIRES INSTALLED NEW FUSE PIN, RII C/W. 2L72 4F4 FRTA1NM E23EA 20040916000792004091600079 2004 9 16 DL76L040820 420040829A23304062256700 CONTROLLER BOEING767 767332 1382001NM ENTERTAIN SYS ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27174DN 24802 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR FROM INFLIGHT ENTERTAINMENT CONTROL BOX. REPLACED CONTROLLER. 2L72 4F RTA1NM 20040916000812004091600081NM 2004 9 16 DL73S040822 120040829A3350RPS1 CHARGER BOEING737 737247 138448DNM EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27377DL 23604 FWD ZONE EMERGENCY FLOOR LIGHTS INOP. REPLACED CHARGER ASSY. 2L72 4F A16WE 20040916000832004091600083NM 2004 9 16 DL76L040823 120040830A3242233N321619 CONTROL PANEL BOEING767 767332 1382001NM COCKPIT SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27175DN 24803 AT PUSHBACK SMELLED SMOKE IN COCKPIT FROM OVERHEAD PANEL. FOUND ELECTRICAL ODOR COMING FROM YAW DAMPER/ANTI-SKID PANEL DAL P/N 311701432, S/N D00125. REPLACED PANEL. 2L72 4F RTA1NM 20040916001822004091600182EA 2004 9 16 COMA0470067 120040907A2782766385C ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RT SLAT FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01355CA 10067 FLIGHT 2225 DURING SRQ APPROACH RECEIVED A SLATS FAIL CAUTION, CREW DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED THE RIGHT OUTBOARD SLAT ACTUATOR. 2L72 4F RTA21EA 20040916001892004091600189EA 2004 9 16 COMA0470066 120040909A2781 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA SLATS ILLUMINATED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01331CA 10061 FLIGHT 5641 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK WAS NORMAL. RESET TRIP INDICATOR AT OUTBOARD SLAT ACTUATOR. 2L72 4F RTA21EA 20040916001912004091600191EA 2004 9 16 COMA0460484 120040823A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01420CA 7451 RIGHT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV A. 2L72 4F RTA21EA 20040916001932004091600193NM 2004 9 16 AALA20040885 120040823A3350D72702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21928AN 29528 BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040916001982004091600198NM 2004 9 16 AALA20040879 120040821A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21692AA 26972 LAX - AFT LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT LEFT HAND OVERWING EMERGENCY EXIT LIGHT AND FORWARD RIGHT HAND OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040916002002004091600200NM 2004 9 16 AALA20040924 120040830A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 TUL - BATTERY PACK FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040916002022004091600202NM 2004 9 16 AALA20040882 120040806A5740 FITTING BOEING767 767323 1385205NM LT WING DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21368AA 25195 AFW - LEFT HAND WING TERMINAL FITTING AT SPAR AT STATION 155 HAS BLENDOUT. AREA IS 0.30 AND DEPTH IS 0.135 INCH. DAMAGED AREA WAS BLENDED SMOOTH, VISUALLY INSPECTED, AND REFINISHED PER THE SRM. A REPLACEMENT FASTENER WITH 0.050 INCH CRES WASHER WAS INSTALLED WET WITH BMS526 SEALANT. 2L72 4F RTA1NM 20040916002042004091600204NM 2004 9 16 DLM88040829 120040901A5313 STRINGER DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27918DL 49583 CRACKED STRINGER 2 LT IN STA 160 AEROMEXICO NRC T0024065 CRACKED STRINGER 3 LT IN STA 160 AEROMEXICO NRC TOO24064 CRACKED STRINGER 4 LT IN STA 160 AEROMEXICO NRC T0024063 ABOVE STRINGERS REPAIRED IAW SRM 53-02 FIG 18. 2L72 4F RTA6WE 20040916002062004091600206NM 2004 9 16 DL733040830 120040901A25308606010000 OVEN BOEING737 7373B7 1384580NM L2 GALLEY ODOR A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27947WP 23376 ACRID SMOKE COMING FROM ELECTRICAL CONTROL PANEL ABOVE OVENS IN AFT GALLEY. FOUND L2 DOOR GALLEY OVEN AND CONTROLLER SMELLING OF SMOKE. CHECKED GALLEY AREA FOUND NO ELECT DAMAGE. RE-INSTALLED OVENS AND CONTROLLERS. REPLACED OVEN AND CONTROLLER. 2L72 4F RTA16WE 20040916002082004091600208NM 2004 9 16 DL76G040832 120040901A2421729825L IDG BOEING767 767332 1382001NM #2 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO271607B 30388 RIGHT GENERATOR DRIVE LIGHT ON, DISCONNECTED RIGHT GENERATOR. DIVERTED TO JFK. SWAPPED EQUIPMENT TO A/C 1521. REPLACED NR 2 IDG ON A/C 1607. 2L72 4F RTA1NM 20040916002102004091600210NM 2004 9 16 DLM88040834 120040901A5312 BULKHEAD DOUG MD88 MD88 3023688NM FUSLAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27918DL 49583 CRACKED WEB IN FWD FACE OF AFT P-DOME AT X=0. REPLACED WEB IN UPPER FWD EDGE OF AFT P-DOME AT X=0. 2L72 4F RTA6WE 20040916002122004091600212NM 2004 9 16 DL764040851 120040905A2121732591F FAN BOEING767 767432ER 1385134NM EQ EXHAUST UNSERVICEABLE A DALAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO27836MH 29709 FWD EQ SUPPLY FAN 1 AND FWD EQ EXHAUST FAN STATUS MSG. FOUND EXHAUST FAN AND MONITOR BAD. REPLACED EXHAUST FAN AND MONITOR. 2L72 4F RTA1NM 20040916002142004091600214WP 2004 9 16 AALA20040890 120040823A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219627R 53597 DFW - OVERHEAD EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040917000142004091700014SW 2004 9 17 2004F00375 120040622A2120 ODOR BELL 407 407 1182206SW CABIN DETECTED A ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03537AL 53230 IN FLIGHT, DURING FLIGHT OUT TO EI 296 A PAX COMPLAINED OF FUEL ODOR IN THE CABIN. INSPECTED ENGINE AT 100 PERCENT NR, FLEW AIRCRAFT NOTED NO PRESENCE OF FUEL ODOR. INSPECTED PAX CABIN AREA, NO FUEL LEAKS AT BACK WALL, FLOOR AREA, OR UNDER AFT FACING SEATS. INSPECTED OVERHEAD BAGGAGE COMPARTMENT, FOUND NO EVIDENCE OF FUEL LEAKS, CLOSED PANELS AND BACK SEATS, RELEASED AIRCRAFT TO SERVICE. ALGA (M) 1G71 3U O H2SW 20040917000152004091700015SW 2004 9 17 2004F00377 120040705A6340 WARNING LIGHT BELL 407 407 1182206SW M/R GEARBOX ILLUMINATED A ALGAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW03937AL 53383 DURING TAKEOFF, TRANSMISSION CHIP LIGHT STARTED TO FLICKER DURING TAKEOFF, RETURNED TO BASE. MAINTENANCE REMOVED CHIP DETECTOR AND INSPECTED NO CONTAMINATION WAS FOUND. CLEANED CHIP DETECTOR AND REINSTALLED FOUND OIL IN ONE OF THE CONNECTORS CLEANED AND REINSTALLED. COMPLIED WITH LEAK CHECK AND GROND RUN. (M) 1G71 3U O H2SW 20040917000472004091700047GL 2004 9 17 UIEA200400117 220040625A732095272DA10053 PACKING BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 4 ENGINE DAMAGED A UIEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15412MC 30559 706125 EICAS MESSAGE 'FUEL IMB' VISUALLY NOTED FUEL LEAK FROM NR 4 ENGINE. ACCOMPLISHED SHUTDOWN PROCEDURES FOR NR 4 ENGINE. TROUBLESHOT FOUND NR 4 ENGINE HMU PERFORMANCE PACKING BADLY DAMAGED. PACKING REPLACED IAW MM 73-21-14. GROUND RUN FOR LEAK CHECK TEST 2, ECU ACTUATOR GROUND TEST 12, AND IDLE LEAK CHECK TEST 3 IAW MM 71-00-00 PAGE 501, ALL FOUND NORMAL. A/C DIVERTED TO BKK. (M) 2L74 4F4 FRT1384945 E23EA 20040917000492004091700049EA 2004 9 17 ASOA04441 120040620A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11883AS 7504 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M0 2L72 4F RTA21EA 20040917000512004091700051NM 2004 9 17 BJNA040701 120040716A335037067001 BATTERY PACK BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD CABIN DOOR R1 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE FWD R1 CABIN DOOR IAW BOEING MM 33-51-81. THE FWD R1 CABIN DOOR EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M) 2L72 4F RTA16WE 20040917000532004091700053 2004 9 17 GTIA040675 420040716A2565 LANYARD DOUG DC9 DC982 3022082WP L1 DOOR SLIDE DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 TPA - FLT 486 - L1 DOOR EMERGENCY SLIDE LANYARD OUT. RE-INSTALLED LANYARD. (M) 2L72 4F A6WE 20040917000552004091700055EA 2004 9 17 2004F00324 120040629A56106003303026 WINDOW CNDAIRCL600 CL6002B16 1900305EA COCKPIT CRACKED A O2GAA UNSCHED LANDING O OTHER DEDESCENT 1 NE03601BE 5103 RIGHT WINDSHIELD OUTER PLY CRACKED DURING DESCENT INTO PBI. AIRCRAFT DIVERTED INTO FLL FOR MAINTENANCE SUPPORT. NO PASSENGERS ONBOARD. REPLACED WINDOW. (M) 2L72 4F RTA21EA 20040917001142004091700114EU 2004 9 17 AWXA200400972 120040904A3350321430 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ZONE 241 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28659AW 1166 DURING 4-DAY CHECK THE AFT SECTION OF SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS FAILED TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (11WL), FUNCTIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20040917001152004091700115EU 2004 9 17 AWXA200400973 120040904A3350321454 EPSU AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ZONE 242 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28640AW35296 448 DURING E-06 CHECK THE RT FORWARD RED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RT OVER WING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20040917001162004091700116NM 2004 9 17 AWXA200400974 120040903A2920NAS16128 PACKING AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE ZONE 190 LEAKING A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28821AW 1406 DIVERSION, ENROUTE, RECEIVED ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL INDICATION, DIVERTED FOR REPAIR. MAINTENANCE FOUND FLUID LEAKING FROM AN O-RING AT THE YELLOW HYDRAULIC SYSTEM BRAKE SELECTOR VALVE, REPLACED O-RING AND PERFORMED LEAK CHECK IAW AMM 32-42-11. 2L72 4F4 FRTA28NM E40NE 20040920000142004092000014NE 2004 9 20 GLBA20030717 220040910A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT FAILED A GLBAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 NM03255GL UE255 114218 RT ENGINE FAILED ON POWER UP FOR TAKEOFF, R&R ENGINE. 2L72 4T4 TRTA24CE E26NE 20040920000152004092000015GL 2004 9 20 CHQA000555 220040912A7261AE3007A ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQAC ABORTED TAKEOFF KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11261 1112411124 145144 CAE311421 DURING TAKEOFF ON FLIGHT 3098, AN OIL ODOR WAS NOTED IN THE COCKPIT. THE ODOR IS IN THE COCKPIT ONLY. THE ODOR IS ASSOCIATED WITH THE AIR CONDITION SYSTEM AND THE NR 1 PACK. MAINTENANCE PERFORMED AN ENGINE RUN AND NOTED THERE IS AN OILY ODOR WHEN THE NR 1 PACK IS ON. THE NR 1 ENGINE ALSO HAS A LOW OIL PRESSURE INDICATION. FURTHER INSPECTION REVEALED OIL LEAKING AND POOLING IN THE COMPRESSOR SECTION. REMOVED AND REPLACED THE NR 1 ENGINE IAW MFG JOB CARD CE720001. OPS CHECK AND LEAKS CHECKS GOOD WITH NO ODOR NOTED. 2L72 4T4 FRTT00011ATTE6CH 20040920000172004092000017NM 2004 9 20 AWXA200401028 120040901A3350100865 POWER SUPPLY BOEING757 7572G7 1384963NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHTSDISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 DURING C-11 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 15 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT THE L-2 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS GOOD. 2L72 4F4 FRTA2NM E12EU 20040920000252004092000025EU 2004 9 20 04FDEA02586 120040831A5320R538D104820200 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 MAIN DECK CARGO COMPT. AT FR 45 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM51-40-21. 2L72 4F4 FRTA35EU E13NE 20040920000262004092000026EU 2004 9 20 04FDEA02587 120040831A5320R538D104820200 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 REF. SNRM N00259, MAIN DECK CARGO COMPT. AT FR 43 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040920000432004092000043NM 2004 9 20 04FDEA02614 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 SNRM N0442: LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000472004092000047CE 2004 9 20 63720 120040807A2697 WIRE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FIRE BOTTLE BROKEN A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07126YV UE126 AIRCRAFT RETURN TO FIELD DUE TO FIRE EXT. DISCHARGE LIGHT ILLUMINATED. NO FURTHER INCIDENT. REPAIRED WIRE AT RT FIRE BOTTLE, OPS CK NORMAL. 2L72 4T4 TRTA24CE E26NE 20040920000802004092000080NE 2004 9 20 KBM2004F00123 220040205A74219550175400 IGNITER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE WEAK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 WEAK START IN MORNING FIRST FLIGHT OF THE DAY. REMOVED AND REPLACED IGNITER. 1G71 3U3 UNCH9EU E19EU 20040920000852004092000085WP 2004 9 20 ASMF200406034 120040629A272059140665565 ACTUATOR DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE RUDDER DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23751RA4045 49779 DURING OVERNIGHT SERVICE, WHEN RUDDER TEST WAS PERFORMED, RUDDER PEDALS WERE HARD DURING OPERATION. RUDDER HYDRAULIC PACKAGE AND RUDDER SHUTOFF VALVE WERE REPLACED IAW MM 27-20-08 AND 27-20-05, TESTS CORRECT. 2L72 4F4 FRTA6WE E2EA 20040920000922004092000092EU 2004 9 20 KBM2004F00177 120040517A5210852610 SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE PAX DOOR LOOSE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 LT CABIN DOOR SEAL LOOSE AND WORN. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040920000972004092000097WP 2004 9 20 ASMF20040801 120040801A282142D185 FILTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE FUEL SYSTEM CLOGGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23755RA3748616353 49727 726073 AIRCRAFT RETURNED TO PLATFORM, (RT FUEL STRAINER CLOGGING) LIGHT TURNED ON. MAIN FUEL FILTER AND DIFFERENTIAL PRESSURE ALARM WERE REPLACED IAW MM 73-12-01, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040920001102004092000110 2004 9 20 UIEA200400110 420040603A344020704090101 ANTENNA BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE RADAR INOPERATIVE G UIEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 EA15540MC 22508 ATB DUE TO BOTH RADARS INOPERATIVE: AFTER LEVEL OFF, BOTH RADAR SCREENS INOPERATIVE. SHOWED BLUE AZIMUTH LINES, BUT NO RANGE OR SWEEP. REPLACED RADAR ANTENNA. OPERATION CK IAW MM, ALL NORMAL. NOTE: NO FUEL DUMPED. 2L74 4F4 F A20WE E23EA 20040920001122004092000112NM 2004 9 20 USA2004F00054 120040531A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19527AU 23862 MAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10 AND THE OVERWING EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE FOUND POWER WIRE L7012A20 CHAFED TO STRUCTURE IN CEILING AREA. REMOVED DAMAGED WIRE SEGMENT AND RETERMINATED. ALSO, REPLACED FUSE (PN 21031-0005) IN FORWARD POWER SUPPLY. OPERATIONAL CHECK OF EMERGENCY LIGHTING NORMAL. 2L72 4F RTA16WE 20040920001172004092000117NM 2004 9 20 71004 120040710A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CRACKED B K NONE O OTHER ININSP/MAINT 1 SO19598AJ 21947 REMOVED AND REPLACE CRACKED AND CORRODED SEAT TRACK SECTIONS AT LBL45/BS420 TO BS560, BL0/BS680 TO BS720, LBL25/BS650 TO BS720 IAW B727 SRM 51-10-1, 51-30-2, 53-10-5 AND MM 51-20-21, 51-20-151. 2L73 4F A3WE 20040920001182004092000118EU 2004 9 20 KBM2004F00176 120040220A21500500346 BLOWER SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE CONDENSER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 CONDENSER BLOWER INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040920001192004092000119EU 2004 9 20 KBM2004F00180 120040530A7933646600251 PROBE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE OIL TEMP FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH 2884 OIL TEMP GUAGE FLUCTUATES. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040920001202004092000120NM 2004 9 20 ANCF200400014 120040625A323339567851 ACTUATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE MLG DOOR MALFUNCTIONED W ANCFO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO23583AN26176532 53183 AFTER TAKE OFF AND LANDING LEVER UP WITH LIGHTS OFF THERE WAS STRONG VIBRATION IN THE NOSE WHEEL COMPARMENT. THE LANDING GEAR WAS CYCLED AND VIBRATION CONTINUED. ACTUATOR CYLINDER WAS REPLACED IAW AMM 32-22-01 PAGE 203. TEST WAS PERFORMED WITH SATISFACTORY RESULTS. 2L72 4F4 FRT E2EA 20040920001222004092000122EA 2004 9 20 5040070604D 120040706A492038300779 COMBUSTION LINER CNDAIRCL600 CL6002B16 1900305EA APU ENGINE SEPARATED E S4WAK NONE O OTHER ININSP/MAINT 1 WP07807Z 1150 5040 BURNER CAN INTERIOR VANES SEPARATING. 2L72 4F RTA21EA 20040920001252004092000125NM 2004 9 20 USA2004F00076 120040607A335020131A BATTERY PACK BOEING737 7373B7 1384580NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19384US 22957 MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN THE AFT POSITION, TO BE WEAK. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040920001262004092000126NM 2004 9 20 USA2004F00080 120040605A291050602 SHUTTLE VALVE BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE HYD SYSTEM FAULTY A USAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 EA19563AU 23551 ENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING NOT AS MUCH EFFORT WAS REQUIRED. AC WAS FOUND IN SAFE CONDITION FOR MAINT FERRY FLIGHT. FERRY FLIGHT CREW REPORTED FLIGHT WAS NOT BAD ON TAKEOFF BUT THAT THERE WAS A DEFINITE PROBLEM ON LANDING. JUST AFTER FLARE, WENT TO PUSH OVER NOSE, FELT LIKE MECHANICAL BINDING. PUSHED HARDER AND IT RELEASED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINT REMOVED AND REPLACED THE (A) FLIGHT CONTROL SYS HYDRAULIC SHUTTLE VALVE. SYSTEM NOW FUNCTIONS SMOOTHLY AND ELEVATOR FEEL AND CENTERING IS NOW RESPONDING NORMAL. 2L72 4F4 FRTA16WE E2GL 20040920001272004092000127NE 2004 9 20 FF62004F00000 220040505A7200770441 MAGNETIC SEAL SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE ENGINE GALLED B FF6RK NONE O OTHER ININSP/MAINT 1 NM11111AK290 3092 SEAL LEAKING AFTER 200 HOURS. SEAL WAS GALLED. 1G71 3U3 UNCH9EU E19EU 20040920001292004092000129WP 2004 9 20 DBCR122D 220040614A7200 ENGINE CESSNA650 650 2076802CE GARRTTTPE731TFE7313C WP NR 1 FAILED E DBCAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL13260VP 6500190 87506 AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGRADE WITH OVERTEMP LIGHT. FLIGHT CREW SECURED NR 1 ENGINE AND RETURNED LANDING WAS UNEVENTFUL. INITIAL VISUAL INSPECTION SHOWED NO SIGN OF FOD DAMAGE TO COMPRESSOR OR HIGH PRESSURE TURBINE. ENGINE REMOVED BY MFG SPI FOR TEARDOWN AND INSPECTION. FOLLOW-UP WILL BE SUBMITTED WHEN CAUSE OF SHUTDOWN IS DETERMINED, TO INCLUDE PN AND TIME/CYCLES ON FAILED PART. 2L72 4F4 F A9NM E6WE 20040920001302004092000130WP 2004 9 20 COOSDR040003 120040630A5310 DOOR FRAME DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE Y STA CRACKED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 76459 46129 MAIN CARGO CABIN Y STA 480 AFT JAMB BETWEEN LONGERON 21 LT AND LONGERON 19 LT, FRAME WITH WEAR AND CRACKED. 2L74 4F4 F 4A25 1E8 20040920001312004092000131WP 2004 9 20 COOSDR040006 120040630A5330 SKIN DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 76459 46129 FUSELAGE FWD SECTION Y STA 498 AND Y STA 522 LONGERON 34 RT LEVEL SKIN CORRODED. 2L74 4F4 F 4A25 1E8 20040920001342004092000134NM 2004 9 20 04FDEA02704 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 33 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33L, REPAIRED AS PER EA 1-5510-81550. 2L73 4F RTA22WE 20040920001352004092000135NM 2004 9 20 04FDEA02705 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 32 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 32L, REPAIRED AS PER EA#1-5510-81549. 2L73 4F RTA22WE 20040920001362004092000136NM 2004 9 20 04FDEA02706 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 30 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 30L, REPAIRED AS PER EA 1-5510-81554. 2L73 4F RTA22WE 20040920001372004092000137NM 2004 9 20 04FDEA02707 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 28 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 28L, REPAIRED AS PER EA 1-5510-81548 2L73 4F RTA22WE 20040920001392004092000139NM 2004 9 20 04FDEA02709 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 20 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 20L, REPAIRED AS PER EA 1-5510-81552. 2L73 4F RTA22WE 20040920001412004092000141WP 2004 9 20 04FDEA02711 120040917A7120 BEARING DOUG DC10 DC1030F 3023504WP GE CF6 CF650* 30018NE ENGINE MOUNT MIGRATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 NR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTALLED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03. 2L73 4F4 FRTA22WE E23EA 20040920001432004092000143WP 2004 9 20 04FDEA02713 120040917A5315 FLOORBEAM DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 AFT PIT STA 1902 FLOOR SUPPORT FRAME T-CAP CORRODED UPPER SURFACE. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 2. CORROSION OUT OF LIMITS IAW FEDEX DC10 SRM 53-00-01 VOL I, PG 8. MATERIAL FOR T-CAP ANGLE IS 7075-T6 .063 P/O 353160.4 IAW DC 10 SRM 53-16-01 VOL 3 AND DAC DWG AGA3850. FAB'D T-CAP ANGLE IAW DAC DWG AGA3850. ALODINED AND PRIMED T-CAP ANGLE IAW DC10 SRM 51-21-01 VOL 2, INSTALLED ANGLE ON FRAME IAW DC10 SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20040920001442004092000144EU 2004 9 20 04FDEA02714 120040911A3230 POPPET VALVE AIRBUS310 A310203 3930313EU MLG DAMPER TRIPPED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25407FE 254 AFTER T/O YYC, ATTEMPTED TO RAISE GEAR, UNABLE TO THE INTERLOCK POS, LT GEAR PITCH DAMPENER POPPET EXTENDED. REQUIRE PITCH DAMPENER CPN 3212339 DAMPER. LT GEAR PITCH DAMPER REPLACED PER AMM 32-11-15-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG D22127000-5, ON MFG D22127000-5. 2L72 4F RTA35EU 20040920001462004092000146WP 2004 9 20 04FDEA02684 120040915A5753ARB11881 BLOCK DOUG MD10 MD1010F 3022112WP TE FLAP TRACK WORN A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25384FE 46617 ON TAKEOFF AT 200 FT GOT STALL WARNING AND SLAT DISAGREE. CLEANED UP PER CHECK LIST. KEPT GETTING PSEU FAIL LEVEL 1 AND SLAT DISAGREE LEVEL 2. ALERT IN CLEAN CONFIG. DIVERT TO MEM. DUMPED 19K LBS OF FUEL NORTH MEM. FOUND NR 4 SLAT, NR 10 TRACK WITH EXCESSIVE PLAY SIDE TO SIDE. FOUND RUB BLOCKS ON NR 10 TRACK WORN ALLOWING DIFFERENT READINGS ON PROX SENSORS. REMOVED AND REPLACED 6 (SIX) BLOCKS FOR NR 10 TRACK. ALSO ADJUSTED NR 2 SENSOR L2A REF MD10-10 MM 27-84-02-4. ALL CHECKS GOOD. PERFORMED SLAT POSITION SENSORS ADJUSTMENT/TEST PER MD10-10 27-84-0 2-5. ALL READINGS CHECK GOOD. PERFORMED RETURN TO SERVICE CHECK ON AOA IN FCC1 AND FCC2. ALL CHECKS GOOD. 2L73 4F RTA22WE 20040920001492004092000149NM 2004 9 20 SWAA042695 120040915A3233273A12011 ACTUATOR BOEING737 7377H4 1384404NM NLG LEAKING A SWAAO OTHER N FALSE WARNING CLCLIMB 1 SW29728SW 27860 AFTER RETRACTING LANDING GEAR, NOSE WHEEL EXTENDED WHEN HANDLE PLACED TO OFF. CYCLED GEAR, WORKED NORMAL. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20040920001512004092000151 2004 9 20 SWAA042697 420040916A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040920001532004092000153NM 2004 9 20 SWAA042699 120040916A335007912 COVER BOEING737 7372T4 1384492NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29721WN 22697 EEPLS COVER AT ROW 6 DEF, LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F A16WE 20040920001552004092000155NM 2004 9 20 SWAA042701 120040916A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER AT BS 325, STRINGER 28R, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20040920001572004092000157NM 2004 9 20 UPS04443075 120040905A3350 SIGN BOEING747 747121 1384871NM EMERGENCY EXIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:N/A EMERGENCY LIGHT AT ESCAPE ABOVE EXIT SIGN INOP. TURNS ON MOMENTARILY THEN SHUTS. REMOVED AND REPLACED LIGHT ASSY PER 33-51-07. OPS CHECK OKAY PER SAME REF. 2L74 4F A20WE 20040920001592004092000159WP 2004 9 20 UPS04843054 120040726A532056423434 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:C3 CUT OUT WEB ON RIGHT STA 3 AT RIVET AREA AND CHECK FOR CRACKS. REMOVED AND REPLACED RIGHT STA 3 FITTING. 2L74 4F RT4A25 20040920001612004092000161NM 2004 9 20 CALA0400630 120040908A5340694555510 FITTING BOEING757 757224 1384958NM CARGO DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2721108 27298 INSPECTION FOUND FORWARD CARGO DOOR SILL MOUNT FITTINGS NR 1, 2, 3, 4 & 5 CORRODED. THE CARGO DOOR SILL FITTINGS WERE REPLACED IAW SRM 51-40-02. 2L72 4F RTA2NM 20040920001632004092000163NM 2004 9 20 CALA0400632 120040911A531169366534 FRAME BOEING737 7373T0 1384582NM FUSLEAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 480, RBL 11. REPAIRED FRAME IAW SRM 53-00-07, FIGURE 206. 2L72 4F RTA16WE 20040920001652004092000165NM 2004 9 20 CALA0400634 120040912A532069353656 ANGLE BOEING737 7373T0 1384582NM INTERCOSTAL CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND A 1 INCH CRACK IN ANGLE ON INTERCOSTAL AT FORWARD AND AFT SCREW HOLES OF CABIN FLOOR STRUCTURE AT STA 380-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 53-30-51. 2L72 4F RTA16WE 20040920001672004092000167NM 2004 9 20 AALA20040930 120040823A5313 STRINGER BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2139367 25194 AFW - FUSELAGE STRINGER SECTION 46 AT S34L HAD CORROSION AT APPROXIMATELY STATION 1213 TO 1219. CORROSION AREA 3 FEET BY 5 INCHES. ACCOMPLISHED FUSELAGE FITTING AND STRINGER SPLICE REPAIR PER SRM 53 30 03 2. 2L72 4F RTA1NM 20040920001692004092000169NM 2004 9 20 AALA20040927 120040830A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 BATTERY PACK AT STATION 952 FOR EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1673 AT STATION 952 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040920001712004092000171NM 2004 9 20 AALA20040928 120040827A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 TUL - BATTERY PACK M1675 AT STATION 322 FOR EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1675 AT STATION 322 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040920001732004092000173NM 2004 9 20 AALA20040887 120040824A1420 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21379AA 25448 MIA - EMERGENCY EXIT LIGHT ON G2 FORWARD GALLEY INOPERATIVE. FOUND CONNECTOR LOOSE. SECURED CONNECTOR FOR EMERGENCY EXIT LIGHT ON G2 FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040920001752004092000175NM 2004 9 20 DL73S040840 120040902A3350 SOCKET BOEING737 737247 138448DNM SEAT ROW A-13 BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27373DL 23520 ON GO-AROUND IN ATL STRONG BURNING ODOR WAS DETECTED IN CABIN AND COCKPIT. ODOR DISSIPATED IN APPROX 3 MIN. REPLACED LIGHT SOCKET AT SEAT 13A. 2L72 4F A16WE 20040920001782004092000178WP 2004 9 20 AALA20040954 120040910A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21583AA 53160 SJC - COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040920001802004092000180WP 2004 9 20 AALA20040956 120040910A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW219621A 53592 AUS - B5-27 BATTERY PACK HAS A BROKEN CIRCUIT BOARD WHITE PLASTIC MOUNT ARM. REPLACED B5-27 BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040920001822004092000182NM 2004 9 20 AALA20040958 120040913A3350D71702002 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21797AN 30012 JFK - SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 30 THROUGH 44 CENTER AISLE INOPERATIVE. REPLACED BATTERY PACK M33401 FOR SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 30 THROUGH 44 CENTER AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040920001862004092000186NM 2004 9 20 SWAA042683 120040915A53116546552 FRAME BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 27R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040920001922004092000192EA 2004 9 20 COMA0460495 120040901A5280 SKIN CNDAIRCL600 CL6002B19 1900309EA NLG DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01779CA 7306 SKIN AFT OF NOSE LANDING GEAR DOOR CRACKED RIGHT HAND CORNER RADIUS. REPAIRED IAW REO 601R-53-11-048. 2L72 4F RTA21EA 20040920001942004092000194NM 2004 9 20 SWAA042675 120040915A3350100031 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040920001962004092000196NM 2004 9 20 SWAA042677 120040915A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040920001982004092000198NM 2004 9 20 SWAA042688 120040915A5313BAC1498 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L, AT BS 360, CORRODED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040920002002004092000200NM 2004 9 20 SWAA042690 120040915A53206551698 SPLICE BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20040920002022004092000202NM 2004 9 20 SWAA042692 120040915A53106520723 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME NR 5 STOP UPPER FLANGE, CRACKED. REMOVED AND REPLACED AFT FRAME SECTION PER ER. 2L72 4F RTA16WE 20040920002042004092000204NM 2004 9 20 SWAA042694 120040915A53106558280 DOOR FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR CUTOUT UPPER STUB FRAME FWD RADIUS, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20040921000012004092100001NM 2004 9 21 04FDEA02701 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 33 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 33R, REPAIRED AS PER EA 1-5510-81547. 2L73 4F RTA22WE 20040921000022004092100002NM 2004 9 21 04FDEA02702 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 36 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. REPAIRED AS PER EA 1-5510-81553, HORIZONTAL STABILIZER-BARREL NUT BORE 36L - REWORKED BEYOND S/B MD11-55-023 REV. 2 LIMITS. 2L73 4F RTA22WE 20040921000062004092100006WP 2004 9 21 04FDEA02718 120040917A5415 BEARING DOUG DC10 DC1030F 3023504WP ZONE 400 MIGRATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 NR 1 ENG PYLON AFT SPHERICAL BEARING ATTACH BOLT TORQUE STRIP BROKEN & THE BEARING MIGRATES. REMOVED AND REPLACED BEARING IAW DC 10-30 FEDEX MM 54-40-02-2, REMOVED CORROSION IAW DC10-30 FEDEX MM 54-40-02, REMOVED FUEL DRAIN LINE IAW FEDEX DC 10-30 MM 0- 50-01-0 20-50-02-2, REMOVED AFT BULKHEAD FITTING P/N AUB7025-33 IAW DC10-30 FEDEX SRM 51-31-01 VOL 2, LOCATED, DRILLED NEW AFT BULKHEAD FITTING IAW DAC DWG AUB7025 FEDEX DC10-0 SRM 51-31-01 VOL 2 P/N AUB 7025-33, INSTALLED FITTING IAW DAC DWG AUB7025 FEDEX SRM DC10-30 51-31-01, 51-38-01VOL 2. R/R FUEL DRAIN LINE IAW FEDEX DC10-30 M 20-50-01-2, 20-50-02-2 TORQUED USING T-8347G REAMED 2 UPPER HOLE IAW FEDEX DC10-30 MM 51-31-01 VOL 2, ALL FASTENERS INSTALLED. 2L73 4F RTA22WE 20040921000072004092100007NM 2004 9 21 04FDEA02719 120040917A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 CORROSION ON STR 28R, AROUND FASTENER HOLES ATTACHING KEELBEAM, STA 722, FWD CARGO BAY. CORROSION ON STR NR 28 RT AROUND FASTENERS HOLES ATTACHING KEELBEAM STA 727 FWD CARGO BAY. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMAGE AREA PER SRM 53-10-3 & SRM 51-30-2. 2L73 4F RTA3WE 20040921000082004092100008WP 2004 9 21 04FDEA02720 120040917A5415 BEARING DOUG DC10 DC1030F 3023504WP ZONE 400 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 NR 3 PYLON TOMBSTONE FITTING UPPER BEARING PITTED. REMOVED AND REPLACED NR 3 PYLON UPPER SPHERICAL BEARING IAW DC10-30 MM 54-40-02-2. 2L73 4F RTA22WE 20040921000092004092100009NM 2004 9 21 04FDEA02721 120040917A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 WHILE REMOVING CORROSION ON SHEAR TIE AT BS 1148 BETWEEN STRINGERS 28L AND 28R CORROSION WAS FOUND TO BE .100 PERCENT THROUGH THE FRAME. ALL WORK DONE PER E.A. 7-5310-55378 2L73 4F RTA3WE 20040921000132004092100013EA 2004 9 21 ASOA04598 120040814A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11878AS 7590 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT CLIPS AT FS 625. (M) 2L72 4F RTA21EA 20040921000142004092100014SO 2004 9 21 SIMA200423904 120040821A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 DURING IMBV INSPECTOIN, THE FORWARD DIGITAL WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE EXISTING FORWARD DIGITAL AND INSTALLED A NEW DIGITAL. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTERS 51-40-02 AND 51-20-01. (M) 2L72 4F RTT00011AT 20040921000152004092100015EU 2004 9 21 ASOA04579 120040809A33503011210 LIGHT AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11642AS 395 DURING A HANGAR INSPECTION IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040921000162004092100016EA 2004 9 21 ASOA04575 120040808A7930 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE OIL FALSE INDICATIONA ASOAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11922EV 7822 DURING CRUISE, AT APPROX 31,000 FT THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING MESSAGE. OIL PRESSURE BEGAN FLUCTUATING BETWEEN 30-32 PSI & THEN DROPPED TO 19 PSI. THE CREW REDUCED ENGINE TO IDLE WITH OIL PRESSURE CONTINUING TO FLUCTUATE BETWEEN 35-40 PSI. ALL OTHR ENGINE IDICATIONS REMAINED NORMAL. QRH PROCEDURES COMPLIED WITH AND AN EMERGENCY DECLARED. AIRCRAFT DIVERTED INTO AEX. DURING FINAL APPROACH AT APPROXIMATELY 5,000 FT THE OIL PRESSURE RETURNED TO NORMAL AND REMAINED THERE DURING A SAFE LANDING AND TAXI. LOCAL MAINTENANCE INSPECTED THE CHIP DETECTOR INDICATOR, OIL LEVEL AND THE OIL PRESSURE TRANSDUCER ON THE RIGHT ENGINE. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000172004092100017EA 2004 9 21 ASOA04569 120040807A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT CLIPS AT FS 625 IAW SRM 51-42-00. (M) 2L72 4F RTA21EA 20040921000192004092100019SO 2004 9 21 SIMA200423911 120040823A27503632001003 PDU EMB 145 EMB145LR 3260212SO TE FLAPS FAILED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21650AE 145417 ON FINAL APPROACH, FLAPS SELECTED TO MOVE FROM 22 TO 45 DEGREES. FLAPS STUCK AT 41 DEGREES WITH ACCOMPANYING FLAP FAIL AND FLAP CAUTION MESSAGES ON EICAS. REPLACED PDU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20040921000212004092100021EU 2004 9 21 USAASA04079 120040811A5330D5331034900300 PANEL AIRBUS320 A320214 3930316EU FUSELAGE MISSING A USAAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 EA19104UW 0863 DURING PREFLIGHT OF THE EXTERIOR, PANEL 192DT WAS FOUND MISSING. MAINTENANCE REPLACED THE RIGHT SIDE, WING TO BODY PANEL 192DT. (M) 2L72 4F RTA28NM 20040921000232004092100023SO 2004 9 21 SIMA200423902 120040821A532014521721007 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE 145314 DURING AN IMBV INSPECTION, THE AFT DIGITAL WAS FOUND CORRODED BEYOND SRM LIMITS. CUT OUT SECTION OF EXISTING DIGITAL STARTING 5.1 IN INBOARD OF THE LEFT SEAT TRACK AT FRAME 18 AND TREATED EDGES. AN ADDITIONAL AREA OF THE DIGITAL AT FRAME 18 OUTBOARD LEFT SEAT TRACK WAS CORRODED BEYOND SRM LIMITS. INSTALLED NEW DIGITAL IAW EMB REPAIR STATEMENT IC2003-145/3806 PARA 3 DATED AUGUST 16, 2004. (M) SIMA 2L72 4F RTT00011AT 20040921000252004092100025EA 2004 9 21 ASOA04572 120040808A5320601R31171117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040921000262004092100026EA 2004 9 21 ASOA04571 120040808A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 DURING A C-CHECK IN MCN, THE RIGHT INBOARD BRACKET AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT INBOARD BRACKET AT FS 280. (M) 2L72 4F RTA21EA 20040921000292004092100029EU 2004 9 21 ASOA04581 120040809A3397M22759 WIRE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11635AS 372 FLT 4276 - DURING A GROUND INSPECTION IN ATL, THE WIRING TO THE TWO AFT EMERGENCY FLOOR LIGHTS WAS FOUND BROKEN AND THE LENS COVER LOOSE. MAINTENANCE RESECURED THE WIRING AND LENS COVER ONTHE TWO AFT EMERGENCY FLOOR LIGHT TRACKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040921000322004092100032EA 2004 9 21 ASOA04585 120040810A5320601R311712115 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INTERCOSTALS AT FS 484, BL 27 TO 36 ON THE OUTBOARD SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT INTERCOSTALS AT FS 484, BL 27 TO 36 ON THE OUTBOARD SIDE IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040921000342004092100034EA 2004 9 21 ASOA04582 120040809A2741 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA STAB TRIM TRIPPED A ASOAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO11915EV 7754 FLT 4491 - DURING CLIMB-OUT FROM DFW-MSY, WHEN PASSING THROUGH 21,000 FEET THE CREW RECEIVED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON EICAS 1. QRH PROCEDURES WERE COMPLIED WITH AND ATTEMPTS TO REENGAGE THE STAB TRIM AND MACH TRIM WERE UNSUCCESSFUL, WITH THE MESSSAGE PERSISTING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO AEX, LANDING SAFELY. MAINTENANCE RESET THE CIRCUIT BREAKERS FOR THE HORIZONTAL STABILIZER TRIM ACTUATOR SYSTEM AND ALSO PERFORMED A STABILIZER TRIM SYSTEM TEST IAW AMM 27-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000352004092100035EA 2004 9 21 ASOA04580 120040809A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11846AS 7328 FLT 4243 - UPON ARRIVAL OF THE AIRCRAFT AT THE GATE, THE MAIN PASSENGER DOOR COULD NOT BE OPENED. MAINTENANCE WAS ABLE TO OPEN THE DOOR AND ALL PASSENGERS DEPLANED SAFELY. MAINTENANCE LUBRICATED THE MAN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000362004092100036EA 2004 9 21 ASOA04577 120040809A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280, LBL 9 AND RBL 9. (M) 2L72 4F RTA21EA 20040921000372004092100037EA 2004 9 21 ASOA04574 120040808A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY SPIDER DUCT BRACKET. (M) 2L72 4F RTA21EA 20040921000382004092100038EA 2004 9 21 ASOA04573 120040808A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 280. (M) 2L72 4F RTA21EA 20040921000432004092100043EA 2004 9 21 ASOA04588 120040812A1420487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11826AS 7210 FLT 9950 - DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 10 C-D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR TRACK LIGHTING AT ROW 10 C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000452004092100045EA 2004 9 21 ASOA04599 120040814A5320 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11878AS 7590 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20040921000462004092100046EA 2004 9 21 ASOA04596 120040814A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11878AS 7590 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, BL 27 TO 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT OUTBOARD CLIPS AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040921000472004092100047EA 2004 9 21 ASOA04602 120040815A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11878AS 7590 DURING A C-CHECK IN MCN, THE RT MLG WW BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046. (M) 2L72 4F RTA21EA 20040921000482004092100048EA 2004 9 21 ASOA04597 120040814A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11878AS 7590 DURING A C-CHECK IN MCN, THE RIGHT INBOARD CLIP AT FS 484, BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD CLIP AT FS 484, BL 27 TO 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040917000442004091700044NM 2004 9 17 AMTA200400948 120040728A33501013273 LIGHT BOEING757 75733N 1384931NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11556TZ 32590 FOUND SIDEWALL LT AFT LEFT EMERGENCY SLIDE INOPERATIVE. REMOVED AND REPLACED SIDEWALL LIGHT ASSEMBLY. OPS CHECK REF 33-21-30. (M) 2L72 4F RTA2NM 20040917000462004091700046NM 2004 9 17 AMTA200400918 120040722A2697 WIRE BOEING757 75733N 1384931NM OVERHEAT DETECT CHAFED A AMTAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL11552TZ 32586 RT TURBINE OVERHEAT DET 2 STATUS MESSAGE DISPLAYED. FOUND CHAFED WIRE JUST AFT OF DISCONNECT D40158P. REPAIRED PER WDM STANDARD PRACTICES CHAPTER 20. OPS CHECKS GOOD AT THIS TIME. (M) 2L72 4F RTA2NM 20040917000482004091700048EA 2004 9 17 A6WA200440104 120040718A5710 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31429AW 7711 AT LEFT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .004 WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED LEFT MLG AFT TRUNNION BUSHING AND INSTALLED FIRST OVERSIZE BUSHING P/N 601R5720113-21, IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20040917000502004091700050NM 2004 9 17 BJNA040703 120040716A3350900835A BATTERY BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 DURING A MAINTENANCE WALK AROUND CHECK, THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CARTRIDGE FOR THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IAW BOEING MM 33-51-81. THE AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT NOW OPERATES NORMALLY. (M) 2L72 4F RTA16WE 20040917000522004091700052WP 2004 9 17 GTIA040674 120040715A1420 CONNECTOR DOUG DC9 DC983 3022083WP AFT LAV SMOKE DEDIRTY A GTIAK NONE N FALSE WARNING ININSP/MAINT 1 GL23824NK 53015 ACY - FLT 1265 - AFT LAVATORY SMOKE ALARM GOES OFF CONTINUALLY. CLEANED CONNECTOR ON RT LAVATORY AS NEEDED. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20040917001192004091700119WP 2004 9 17 ARWA20040807 120040831A2797 BUSS CABLE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE AILERON BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 UPON INSPECTION, FOUND LT (LT) AILERON BUS CABLE BROKEN. ALSO FOUND LT AILERON BUS CABLE CRANK PULLEYS WORN. REMOVED DAMAGE CABLE AS REQUIRE IAW MM 27-10-0. FABRICATED NEW CABLE IAW SAMPLE IAW MM 91-10-12. INSTALLED NEW CABLE, ADJUSTMENT AND TEST FOUND NORMAL IAW MM 27-10-0. REMOVED AND REPLACED PULLEYS IAW MM 20-10-0. NO DEFECT NOTED AT THIS TIME. 2L74 4F4 F 4A25 1E8 20040917001292004091700129NM 2004 9 17 AALA20040901 120040825A1420 CONNECTOR BOEING767 767323 1385205NM GE CF6 CF680C2B6 30025NE EMERGENCY LIGHTSLOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21396AN 29603 EMERGENCY LIGHTS AT SEAT ROWS 28, 29, AND 30AB INOPERATIVE. RESECURED CONNECTOR AT SEAT 28AB FOR EMERGENCY LIGHTS AT SEAT ROWS 28 THROUGH 30AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA1NM E13NE 20040917001322004091700132EU 2004 9 17 AWXA200400945 120040806A5330D53480114208 DOUBLER AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AT PORTABLE WATER SERVICING CUTOUT FR 65 TO FR 66, STR 37 LT TO STR 41 LT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER; FABRICATED A NEW REPLACEMENT REINFORCEMENT DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. **SUPP** REGISTRATION NUMBER AND TIMES HAVE BEEN CHANGED TO REFLECT THE CORRECT AIRCRAFT. 2L72 4F4 FRTA28NM E311NE 20040920000032004092000003NM 2004 9 20 04FDEA02609 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING - OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000052004092000005NM 2004 9 20 04FDEA02611 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000082004092000008EU 2004 9 20 AWXA200401027 120040915A3397 WIRE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE READING LIGHT SHORTED A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP28622AW 054 ARCHING / SMOKE, FLIGHT CREW REPORTED WIRES IN CAPTAINS SLIDING WINDOW POST CONNECTED TO READING LIGHT SHORED OUT WITH VISIBLE ARCHING AND SMOKE, A SMALL HOLE BURNED THROUGH PLASTIC COVER. MAINTENANCE PULLED AND COLLARED CAPTAINS READING LIGHT CIRCUIT BREAKER, ISSUED MEL 33-10-01, COND. 1 COCKPIT/INST PANEL LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CAPTAINS READING LIGHT ON SLIDING WINDOW, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA28NM E311NE 20040920000182004092000018NM 2004 9 20 AWXA200401029 120040908A5315654580829 FLOORBEAM BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK CORROSION WAS FOUND ON THE UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 294.5 BETWEEN RBL 10 AND RBL 55, WL 208. MAINTENANCE REMOVED DAMAGED FLOORBEAM UPPER CHORD AT BS 294.5 FROM LBL 6 TO RBL 60; FABRICATED A NEW REPLACEMENT UPPER CHORD IAW DWG 65-45808; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 12. 2L72 4F4 FRTA16WE E21EU 20040920000212004092000021EU 2004 9 20 04FDEA02585 120040831A5320R538D10480200 DUMMY RAIL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 MAIN DECK CARGO COMPT. AT FR53 BETWEEN R1 AND R2 SEAT TRACK DUMMY TRACK IS CRACKED . REMOVED AND REPLACED DUMMY TRACK IAW A310-200 SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040920000382004092000038EU 2004 9 20 AWXA200400944 120040818A5320D5348004800100 SILL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE R-2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SHAPE SILL ASSEMBLY AT Y1750 RT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SHAPE SILL AT Y1750 RT, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20040920000482004092000048 2004 9 20 CRJ2004F00000 420040615A3418 GROUND WIRE CESSNA210 T210N 2073456CE CONT O520 TSIO520R 17040SO STALL WARNING DIRTY C CRJRO OTHER O OTHER NRNOT REPORTED 1 CE016227Y 21064301 WHEN PITOT HEAT IS ENGAGED, IT RENDERS THE STALL WARNING HORN INOPERABLE. STALL WARNING RESUMES WORKING PROPERLY WITH PITOT HEAT DISENGAGED. THE GROUND ON THE STALL WARNING UNIT WAS CLEANED. ALL OPERATIONS WORK PROPERLY. NOTE: THIS IS THE THIRD FINDING COME ACROSS WITH THIS AGE OF UNIT. (GL03200409830) 1H71 3O3 O 3A21 E8CE 20040920000782004092000078NM 2004 9 20 VJ12004F00000 120040604A7830 STIFFENER GULSTM200 200 4500308NM PWA 306 PW306B NE THRUST REVERSER CRACKED B VJ1RO OTHER O OTHER NRNOT REPORTED 1 SW05414KB 24 022 THE THRUST REVERSER ASSY HAS STIFFNER ANGLES THAT GO AROUND THE BARREL. THE POINT WHERE THE ANGLE ATTACHES IS CRACKED AT ONE LOCATION. SEVERAL OTHER THRUST REVERSER ASSY WERE EVALUATED ON AIRCRAFT IN HOUSE AND NO CRACKS WERE NOTED. IT APPEARS THAT THE ANGLE IN QUESTION WAS PRELOADED AND DRAWN DOWN TO THE CARRIAGE RATHER THAN BEING SHIMMED. 2L72 4F4 FRTA53NM E35NE 20040920000912004092000091SO 2004 9 20 CSA2004F00000 120040628A1430400188 BOLT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA LT MLG WORN E CSAAO OTHER O OTHER NRNOT REPORTED 1 AL013516A 317952106 PILOT RADIOED THAT LT MLG SAFE LIGHT WOULD NOT COME ON, VERIFIED BULB FUNCTION, OK. VERIFIED GEAR FULLY EXTENDED DURING FLY-BY BEFORE LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT STOPPED ON RUNWAY. PILOT REPORT GEAR SAFE LIGHT CAME ON AT TOUCHDOWN. MECHANIC INSPECTED GEAR AND FOUND ALL HOOKS FULLY ENGAGED. MOVED AIRCRAFT TO HANGAR, JACKED AIRCRAFT. LT DOWNLOCK HOOK MOVEMENT STIFF. REMOVED AND REPLACED 400-188 BOLT. INSPECTED AND REINSTALLED RT DOWNLOCK NECK BOLT. CLEANED AND LUBED LANDING GEAR. CYCLED GEAR 6 TIMES. NO DEFECTS NOTED. 1L72 3O3 O A20SO E14EA 20040920001882004092000188NM 2004 9 20 SWAA042685 120040915A53106520723 DOOR FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME AT NR 5 STOP, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040920001902004092000190 2004 9 20 SWAA042687 420040915A256565C16820 HOOK BOEING737 7373G7 1384595NM R1 DOOR GIRTBAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20040920001932004092000193EA 2004 9 20 COMA0460499 120040901A3350363782 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN FLOOR INOPERATIVE A COMAO OTHER L NO TEST NRNOT REPORTED 1 SO01954CA 7100 FLIGHT 5378 EMERGENCY FLOOR LIGHTS INOP ROW 9 THRU 12. REPLACED FLOOR LIGHT STRIP ROW 9 THRU 12. 2L72 4F RTA21EA 20040920001952004092000195 2004 9 20 SWAA042676 420040915A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR GIRTBAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW296231W 27933 L1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED L1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20040920001972004092000197 2004 9 20 SWAA042678 420040915A256565C16280 HOOK BOEING737 7373K2 13844BANM R1 DOOR GIRTBAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED R1 DOOR EVAC SLIDE GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20040920001992004092000199NM 2004 9 20 SWAA042689 120040915A575465C304621 SKIN BOEING737 737301 1384611NM NR 2 K FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND LT WING NR 2 L/E KRUEGER FLAP CRACKED. REMOVED AND REPLACED LT WING NR 2 L/E KRUEGER FLAP PER MM. 2L72 4F RTA16WE 20040920002012004092000201NM 2004 9 20 SWAA042691 120040915A5320BAC15171489 STRUCTURE BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, RBL 11 TO LBL 11, CORRODED. REMOVED AND REPLACED CHORD PER SRM. 2L72 4F RTA16WE 20040920002032004092000203NM 2004 9 20 SWAA042693 120040915A534065C27314 STRINGER CLIP BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20040920002052004092000205NM 2004 9 20 SWAA042654 120040913A53306573742 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 4R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040921000032004092100003NM 2004 9 21 04FDEA02703 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 35 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. EXCEEDED LIMIT BARREL NUT BORE NR 35L, REPAIRED AS PER EA 1-5510-81556. 2L73 4F RTA22WE 20040921000112004092100011NM 2004 9 21 04FDEA02723 120040917A5220 DOOR BOEING727 727200 138407ENM EMERGENCY EXIT CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 CORROSION LT FWD OVERWING ESCAPE HATCH, ALONG LWR EDGE UNDER PRESSURE SEAL. BLENDED CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1 & REPAIRED PER SRM 51-30-5 & 51-30-2. 2L73 4F RTA3WE 20040921000182004092100018SO 2004 9 21 SIMA200423903 120040820A532014525480003 SILL EMB 135 EMB135LR 3260305SO CARGO DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE 145314 DURNG AN IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CARGO DOOR CENTER SILL. INSTALLED NEW SILL IAW EMB SRM, SRM 145/1142 REV 26, 51-40-02 AND ETN EB 53-023 DATED APRIL 4, 2002. (M) 2L72 4F RTT00011AT 20040921000202004092100020SO 2004 9 21 SIMA200424303 120040829A2751 WARNING LIGHT EMB 145 EMB145LR 3260212SO TE FLAPS ILLUMINATED A SIMAO OTHER N FALSE WARNING LDLANDING 1 SW21624AE 145111 SGF - FLT 3940 - AIRCRAFT HAD A FLAP FAIL MESSAGE ON LANDING. EMERGENCY DECLARED. MAINTENANCE FOUND ASSOCIATED FLAP DRIVE TS FAIL MESSAGE ON CENTRAL MAINTENANCE COMPUTER. COMPLIED WITH FAULT ISOLATION MANUAL 27-51-00-810-804A. RESET FLAP SYSTEM WHILE RESETTING CIRCUIT BREAKERS. PERFORMED VISUAL INSPECTION OF ALL ASSOCIATED CONNECTOR AND FLEX SHAFT WITH NO DEFECTS NOTED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMA 2L72 4T RTT00011AT 20040921000302004092100030EA 2004 9 21 ASOA04578 120040809A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT ANGLES AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT ANGLES AT FS 625. (M) 2L72 4F RTA21EA 20040921000312004092100031NE 2004 9 21 ASOA04576 220040808A72616087T04P06 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A 30015NE RT ENGINE CLOGGED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11922EV2898 7822 DURING CRUISE FROM AEX-DFW, AT APPROXIMATELY 22,000 FT WHILE FERRYING THE AIRCRAFT TO DFW THE CREW RECEIVED A RT ENGINE OIL PRESSURE WARNING. THE QRH WAS COMPLIED WITH AND THE CREW WAS ABLE TO MAINTAIN ADEQUATE THRUST TO MAINTAIN LEVEL FLIGHT AT 22,000 FT. THE AIRCRAFT LANDED SAFELY IN DFW. AS A PRECAUTION FIRE AND MEDICAL VEHICLES FOLLOWED THE AIRCRAFT DURING A SAFE TAXI TO THE GATE. MAINTENANCE R & R THE RT ENGINE OIL LUBE AND SCAVENGER PUMP ASSEMBLY. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040921000332004092100033EA 2004 9 21 ASOA04584 120040810A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040921000412004092100041SO 2004 9 21 SIMA200423901 120040820A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED SERVICE DOOR SILL AND INSTALLED NEW SILL IAW EMB SRM 145/1142 REV 26, 51-40-02 EMB REPAIR STATEMENT IC2003-145/0818 DATED MAR 6, 2003 AND ETN EB 53-009 DATED 8/28/2001. (M) SIMA 2L72 4F RTT00011AT 20040921000492004092100049EA 2004 9 21 ASOA04587 120040812A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11826AS 7210 FLT 9950 - DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND FROM AFT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000502004092100050EA 2004 9 21 ASOA04592 120040813A5210600319801007 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP BRACKET ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000532004092100053EU 2004 9 21 ASOA04601 120040815A33503011052 COVER AEROSPATR72 ATR72212 8680945EU EXIT SIGN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11535AS 464 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN COVER AT ROW ONE WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN COVER AT ROW ONE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040921000582004092100058WP 2004 9 21 GTIA040741 120040819A3230 CONTROL VALVE DOUG DC9 DC982 3022082WP MLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23820NK 49126 AFTER TAKEOFF, AIRCRAFT SPEED APPROX 150 KNOTS THERE WAS NO DRAG 100 FEET AGL 12 DEGREE PITCH UPLEFT MAIN GEAR, GEAR WAS UP RED LIGHT STAYED ON AFTER GEAR RETRACTION GEAR DOOR OPEN LIGHT WAS NOT ON AND NOSE AND RIGHT MAIN GEAR LIGHTS NOT ON AT SPEED 200 KNOTS CLIMBING THROUGHOUT 3000 MSL CYCLED GEAR. GEAR UP NORMAL DURING APPROACH TO LANDING WITH GEAR DOWN THREE GREEN THE GEAR DOOR OPEN LIGHT STAYED ON LONGER THAN NORMAL APPROX 180 KNOTS SPEED. PERFORMED RIG CHECK OF LANDING GEAR CONTROL VALVE, JACK AND CYCLED GEAR. (M) 2L72 4F A6WE 20040921000592004092100059WP 2004 9 21 GTIA040742 120040822A3230 BEARING DOUG DC9 DC982 3022082WP TORQUE TUBE FAILED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23820NK 49126 FLT 380 - LT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. GEAR RECYLE SATISFACTORY. REPLACED BEARING ON LEFT TORQUE TUBE VERIFIED PROPER RIGGING. PERFORMED MULTIPLE GEAR SWINGS CHECKS GOOD. (M) 2L72 4F A6WE 20040921000602004092100060 2004 9 21 GTIA040743 420040820A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DISLODGED A GTIAO OTHER O OTHER TXTAXI/GRND HDL 1 GL23803NK 48087 FLT 1504 - RSW - UPON L1 DOOR CLOSURE AT PUSHBACK THE SLIDE PACK FELL OFF DOOR. RE-INSTALLED L1 SLIDE PACK ASSEMBLY. (M) 2L72 4F A6WE 20040921000622004092100062WP 2004 9 21 GTIA040755 120040809A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FOUND FLIGHT COMPARTMENT STATION 148.5 TO STATION 120.050 RIGHT SIDE BELOW CO-PILOT SEAT PANEL HAS CRACKED DAMAGE AT HAT CHANNEL SUPPORT. RUB STRIP DETACHED. FABRICATED FLOORBOARD. (M) 2L72 4F RTA6WE 20040921000642004092100064WP 2004 9 21 GTIA040748 120040817A3231 ROLLER DOUG DC9 DC982 3022082WP MLG DOOR OUT OF ADJUST A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23820NK 49126 DURING CRUISE FLIGHT, GEAR DOOR OPEN LIGHT CAME ON, PUT HYDRAULIC PUMPS ON HIGH AND LIGHT WENT OUT AFTER APPROXIMATELY 3 MINUTES. FOUND DOOR ROLLER TO HOOK CLEARANCE OUT OF ADJUSTMENT. ADJUSTED CLEARANCE. (M) 2L72 4F A6WE 20040921000662004092100066WP 2004 9 21 GTIA040738 120040802A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND FORWARD CABIN FLOOR SUPPORT CORROSION STATION 160-200 LBL 52-55. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040921000672004092100067WP 2004 9 21 GTIA040739 120040804A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND CABIN STATION 946 LBL 6 FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA6WE 20040921000692004092100069 2004 9 21 GTIA040744 420040822A2565 HOLDER DOUG DC9 DC982 3022082WP GIRT BAR OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 AFT GALLEY GIRT BAR NOT WORKING PROPERLY 'HOLDER'. ADJUSTED GIRT BAR HOLDER, OPS CHECK NORMAL. GTIA (M) 2L72 4F A6WE 20040921000712004092100071WP 2004 9 21 GTIA040747 120040816A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT BROKEN A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND LEFT FORWARD EMERGENCY EXIT DOOR LIGHT HAS A BROKEN WIRE. REPAIRED WIRE. (M) 2L72 4F RTA6WE 20040921000732004092100073WP 2004 9 21 GTIA040757 120040809A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FOUND FORWARD CABIN STATION 200 TO STATION 180 RBL 8 INCHES TO 36 INCHES FLOOR PANEL HAS SOFT/MUSHEY AND SEVERAL INSERTS CORRODED. FABRICATED FLOORBOARD. (M) GTIA 2L72 4F RTA6WE 20040921000742004092100074SO 2004 9 21 SIMA200423707 120040821A21332099L021100 VALVE EMB 135 EMB135LR 3260305SO CABIN PRESSURE MALFUNCTIONED A SIMAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW21730KW 145346 BOS - FLT 9302 - CREW EXPERIENCED RAPID DEPRESSURIZATION OF AIRCRAFT AND PERFORMED AN EMERGENCY DESCENT. LANDED SAFELY. REPLACED ELECTROPNEUMATIC VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040921000802004092100080EA 2004 9 21 SIMA200424301 120040827A3350YAD41 RELAY CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT MALFUNCTIONED A SIMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SW21515AE 10121 DURING TAXI OUT, EMERGENCY LIGHTS STARTED FLICKERING. REPLACED RELAY IN JUNCTION BOX 11. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA21EA 20040921000822004092100082SO 2004 9 21 SIMA200423702 120040819A531014521713005 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 ABI - DURING AN IMBV INSPECTION, THE CENTER BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORRODED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 26, 51-40-02 AND ETN EB 53-022R1. (M) 2L72 4F RTT00011AT 20040921000832004092100083WP 2004 9 21 GTIA040750 120040825A25303510005801 COFFEEMAKER DOUG DC9 DC983 3022083WP GALLEY ODOR A GTIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23825NK 53012 FLT 308 - DTW - A BURNING SULPHER ODOR IN FLIGHT DECK AND FORWARD GALLEY NO SMOKE WAS PRESENT F/A CHECKED GALLEY AND FOUND COFFEE MAKER C/B POPPED. REMOVED AND REPLACED FORWARD COFFEE MAKER. (M) 2L72 4F RTA6WE 20040921000842004092100084WP 2004 9 21 GTIA040752 120040826A3222 STRUT DOUG DC9 DC982 3022082WP NLG OUT OF ADJUST A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23821NK 49508 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT AND DOORS WOULD NOT CLOSE. RETURNED TO MYR. SERVICED AND ADJUSTED NOSE GEAR STRUT, JACKED NOSE OF A/C AND RETRACTED AND EXTENDED NOSE GEAR 4 TIMES WITHOUT ANY DEFECTS NOTED. (M) 2L72 4F A6WE 20040921000852004092100085WP 2004 9 21 GTIA040753 120040827A3222 STRUT DOUG DC9 DC982 3022082WP NLG DISCHARGED A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23821NK 49508 RED NOSE UNSAFE LIGHT ON W GEAR HANDLE UP. SERVICED NOSE STRUT. LUBED NOSE GEAR. INSPECTED NOSE GEAR LINKAGE AND DOORS. (M) 2L72 4F A6WE 20040921000862004092100086WP 2004 9 21 GTIA040758 120040806A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND CABIN STATION 200-256 FLOOR PANEL CRACKED. REPAIRED CABIN FLOOR PANEL. (M) GTIA 2L72 4F RTA6WE 20040921000872004092100087WP 2004 9 21 GTIA040761 120040829A5210 HANDLE DOUG DC9 DC981 3022081WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) GTIA 2L72 4F A6WE 20040921000882004092100088SO 2004 9 21 SIMA200423703 120040818A531114533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS, AT AFT BELLY FAIRING. BLENDED THE CHAFE ON STRINGER 19R AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE, TWO SHIMS. REPAIF DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-24-02 AND EMB REPAIR STATEMENT IC 2003-145/3093A. (M) 2L72 4F RTT00011AT 20040921000902004092100090SO 2004 9 21 SIMA200423709 120040822A2120 SMOKE EMB 135 EMB135KL 3260302SO CABIN DETECTED A SIMABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21843AE 145680 SAN - FLT 3155 - AIR TURN BACK DUE TO SMOKE SMELL IN CABIN. DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. PERFORMED DETAIL INSPECTION AND PERFORMED OPERAITONAL CHECK OF AIR CONDITIONING SYSTEM. PERFORMED ENGINE RUNS IAW AMM. NO DEFECTS NOTED AT THIS TIME. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040921000912004092100091SO 2004 9 21 SIMA200423708 120040822A5270 WARNING LIGHT EMB 145 EMB145LR 3260212SO CARGO DOOR ILLUMINATED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21617AE 145093 ORD - FLT 4015 - BAG EXT LIGHT ILLUMINATED DURING CLIMB-OUT, AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. PERFORMED OPERATIONAL CHECK OF FIRE DETECTIONS SYSTEM IAW EMB 145 AMM 26-10-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) SIMA 2L72 4T RTT00011AT 20040921000952004092100095SO 2004 9 21 SIMA200423704 120040812A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21831AE4924 145616 DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOND TO BE CORRODED BEYOND SRM LIMITS. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER FILTER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-10. (M) 2L72 4F RTT00011AT 20040921000962004092100096 2004 9 21 2004F00332 420040104A2565 SLIDE BOEING727 727200 138407ENM R1 DOOR DEPLOYED A P9RAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO11910PG 22606 AFTER PARKING, R1 SLIDE DEPLOYED INADVERTANTLY BY CREW AFTER PASSENGERS DEPLANED AND CLEANING CREW WAS ONBOARD. REMOVED AND REPLACED SLIDE IAW BMM 25-60-15. (M) 2L73 4F RTA3WE 20040921000982004092100098CE 2004 9 21 2004F00333 120040218A2910S3128E0235332E HOSE CESSNA750 750 2076810CE HYD SYSTEM LEAKING A UG8AK NONE K FLUID LOSS ININSP/MAINT 1 GL235112 7500010 DURING WALK-AROUND AFTER PARKIGN CREW NOTICED HYDRAULIC FLUID ON TAIL AND MADE WRITE UP ON SHUT DOWN AT LAS HYDRAULIC FLUID WAS POURING OUT OF THE LEFT ELEVATOR HINGE POINT CLOSEST TO THE VERTICAL STAB. MAINTENANCE FOUND ELEVATOR ACTUATOR HOSE HAD BEEN RUBBED THROUGH BY ELEV PCU. ACTUATOR HOSE WAS REPLACED, SYSTEM BLEED AND SERVICED. OPS AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4J RTT00007WI 20040921001002004092100100NM 2004 9 21 UIEA200400136 120040723A1420D25991 CONNECTOR BOEING747 747243B 1384830NM NR 4 ENGINE DAMAGED A UIEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15517MC 23300 AFTER TAKEOFF, NR 4 ENGINE INTERMITTENT FIRE WARNING 'A' LOOP FLUCTUATED. HOWEVER, 'B' LOOP DMI INOPERATIVE. SHUTDOWN NR 4 ENGINE JETTISION FUEL AND RETURNED. CLEANED AND CHECKED ALL CONNECTOR OF NR 4 ENGINE 'A' LOOP. NO FAULT FOUND AND GROUND TEST OK AS PER MM 26-11-00. REPAIRED CONNECTOR AS PER MM 26-11-00 AND GROUND TEST OK. (M) 2L74 4F A20WE 20040921001022004092100102WP 2004 9 21 GTIA040678 120040711A3150 WARNING SYSTEM DOUG DC9 DC983 3022083WP COCKPIT ILLUMINATED A GTIAK NONE N FALSE WARNING ININSP/MAINT 1 GL23831NK 49617 CADC ANNC ILLUMINATED. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M) 2L72 4F RTA6WE 20040921001032004092100103WP 2004 9 21 GTIA040679 120040710A5210 SKIN DOUG DC9 DC982 3022082WP L1 DOOR DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FOUND DENT ON LOWER EDGE OF L1 DOOR 10 INCHES BY 1 INCH BY .375 INCH. REMOVED DAMAGED 1 INCH BY 23 INCH. FABRICATED 3 DOUBLER AND 5 FILLER. INSTALLED DOUBLER AND FILLER. (M) 2L72 4F A6WE 20040921001042004092100104EA 2004 9 21 ASOA04498 120040711A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11871AS 7537 DURING A C-CHECK IN MCN, LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040921001062004092100106EA 2004 9 21 ASOA04499 120040711A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 DURING A C-CHECK IN MCN, THE OUTBOARD CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD CLIP AT FS 280, LBL 9 IAW SRM 51-42. (M) 2L72 4F RTA21EA 20040921001082004092100108EA 2004 9 21 ASOA04492 120040707A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA RT WING TE FLAP MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11835AS4309 43 7258 DURING APPROACH INTO TLH FROM DFW, THE FLAPS FAILED WHEN SELECTED TO TWENTY DEGREES. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN TLH. MAINTENANCE RE-RIGGED THE RIGHT INBOARD AND OUTBOARD FLAPS AND ALSO REMOVED AND REPLACED THE RIGHT BRAKE POSITION SENSOR UNIT (BPSU). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921001092004092100109NE 2004 9 21 ASOA04491 220040707A72304114T15P02 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11717EV 10088 FLT 4509 - DURING CRUISE FROM ONT-DFW, AT APPROXIMATELY 37,000 FEET THE CREW NOTICED THE RIGHT ENGINE FAN VIBRATION ENTER THE CAUTION RANGE OF 1.8 AND DECREASED THE ENGINE POWER, AT WHICH TIME THE FAN VIBRATION INCREASED TO 2.1. THE AIRCRAFT DIVERTED INTO TUS. DURING DESCENT AT APPROXIMATELY 24,000 FEET, THE FAN VIBRATION RETURNED TO THE NORMAL RANGE. THE AIRCRAFT LANDED SAFELY IN TUS. MAINTENANCE REMOVED AND LUBRICATED THE RIGHT ENGINE N1 FAN BLADES AND REINSTALLED THEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA EOOO63EN 20040921001102004092100110NE 2004 9 21 2004F00334 220040612A7250 TURBINE BLADES CESSNA500 500CESSNA 2076602CE PWA JD15 JT15D1A NE LT ENGINE ERODED A BLIAE ENGINE SHUTDOWN E VIBRATION/BUFFET APAPPROACH 1 GL1758TC 5000261 PCE77107 ON APPROACH TO ATW, LT ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE. AIRCRAFT LANDED WITHOUT INCIDENT. PILOT CALLED DIRECTOR OF MAINTENANCE. DIRECTOR TRAVELED TO ATW, PERFORMED LOSS OF OIL INSPECTION. REPLACED OIL PUMP DUE TO SUSPECTED SCAVENGE FAILURE. SERVICED OIL AND PERFORMED DRY MOTORING RUN. DISCOVERED A FAILED PRESSURE OIL LINE. REPLACED OIL LINE. PERFORMED GROUND RUN. NOISE AND VIBRATION LEVEL FOUND TO BE UNACCEPTABLE AND SHUTDOWN PERFORMED. PERFORMED BORESCOPE INSPECTION AND FOUND HIGH PRESSURE TURBINE BLADES SEVERLY ERODED. HOT SECTION TO BE REMOVED AND OVERHAULED. THIS ACTION HAS NOT BEEN INITIATED TO DATE. A/C REMAINS HANGARED AT ATW. (M) 1L72 4F4 F A22CE E25EA 20040921001132004092100113NE 2004 9 21 A6WA200440113 220040806A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 VIBRATION A A6WAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL31452AW 7835 873847 ENGINE 2 VIBRATION EXCEEDED LIMITS AT V1 WITH CONSTANT AIRFRAME VIBRATION INDICATION GOT OVER 3. REMOVED AND REPLACED NR 2 ENGINE DUE TO HIGH VIBRATION IAW AMM 72-10. (M) 2L72 4F4 FRTA21EA E15NE 20040921001152004092100115NE 2004 9 21 2004F00335 220040714A7200560890 SEAL SKRSKYS64 S64F 8142610NE PWA JFTD12JFTD12A4A 52047NE BLADES BROKEN B E8KLK NONE O OTHER ININSP/MAINT 1 NM09159AC1000 64084 COMPRESSOR ASSY REMOVED FROM A/C FOR A 1000 TSO SCHED HOT SECTION INSP. DURING INSP, EVIDENCE RUBBING BETWEEN OUTER SHROUD OF 1ST STAGE N1 BLADES & 1ST STATE OUTER AIRSEAL KNIFE EDGES. 1 BLADE BROKEN OUTER SHROUD. CONTACT BETWEEN DAMAGED TO OUTER SHROUD OF BLADES & KNIFE EDGES WORE DOWN SHROUD OF AIRSEAL IN 2 AREAS 180 DEGREES APART. RESEARCH INDICATED 1ST STAGE OUTER AIRSEAL INSTALLED IN NEW CONDITON. 1ST STAGE BLADE SET INCLUDED 46 BLADES, & 46 BLADES OVERHAULED. RADIAL CLEARANCE MEASURE BETWEEN AIRSEAL & 1ST STAGE BLADES DURING BUILD-UP OF COMPRESSOR .028 INCH. TURBINE CASE & AIRSEAL MEASURED IN THEIR CURRENT CONDITION FOR ROUNDNESS. FORWARD SNAP OF TURBINE CASE IS .016 INCH OUT OF ROUND & AFT SNAP I2G72 4U4 U H6EA E15EA 20040921001162004092100116NE 2004 9 21 2004F00336 120040722A6320643520017014 HOUSING SKRSKYS64 S64E 8142604NE M/R GEARBOX CRACKED B E8KLK NONE O OTHER ININSP/MAINT 1 NM09172AC 64061 MAIN GEAR BOX S/N A6-168 WAS REMOVED FOR OVERHAUL AND CRACK IN MAIN AFT SIDE OF INPUT FROM THE AIRCRAFT. DURING FPI, THERE WAS A CRACK FOUND IN THE LEFT INPUT BOTTOM SIDE APPROXIMATELY .5 INCH LONG, AND THE RIGHT SIDE WAS FOUND TO ALSO HAVE A CRACK INDICATION APPROXIMATLEY 1.25 INCH AND A SECOND AT .25 INCH IN LENGTH. E8KL (M) TONY CHECK THIS 2G72 4U H4EA 20040921001172004092100117EU 2004 9 21 DHL3642004015 120040821A53302024T3 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 FUSELAGE LAP SEAM 44L HAS A BULGE AND A RIVET POPPED JUST AFT OF FR 26. OPEN ACCESS PANELS FOR SHEETMETAL REPAIR AREA FRAME 26 STRINGER 43. CUT OUT LONGERON 43 TO FRAME 26. CUT OUT INNER SKIN DAMAGED AREA, PERFORMED HFEC AT CUTOUT AREA, NO CRACK INDICATED. AREA IS CORROSION FREE & PREVENTIVE BARRIER HAS BEEN RESTORED. AREA COMPLIES WITH THE AERODYNAMIC SMOOTHNESS REQUIREMENT. FABRICATED REPAIR DOUBLER, FILLER PLATE, PLUS FILLER. TREATED, PRIMED & INSTALLED REPAIR. FABRICATED AND INSTALLED SPLICE REPAIR. OK TO CLOSE ACCESS PANELS. 2L72 4F RTA35EU 20040921001182004092100118EU 2004 9 21 04FDEA02690 120040916A5320 FLOOR SUPPORT AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 BULK CARGO FR 64 FLOOR STRUCTURE ON LT CORNER UNDERNEATH, NOTED CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10 AND FOUND TO BE WITHIN LIMITS PER A310 SRM. TREATED, PRIMED, AND TOP COATED PER A310 SRM 51-23-10. 2L72 4F RTA35EU 20040921001192004092100119NM 2004 9 21 SWAA042704 120040916A534065C27314 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH STRINGER CLIPS AT BS 500B, STRINGER 25L AND BS 500C, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040921001212004092100121NM 2004 9 21 DHL2004742006 120040828A3350 LIGHT BOEING727 727225 1384077NM COCKPIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01742DH 21290 COCKPIT EMERGENCY EXIT LIGHT WILL NOT COME ON WHEN SWITCH TURNED ON. RESEATED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CHECKS NORMAL IAW B727 M/M 33-50-01. 2L73 4F A3WE 20040921001222004092100122WP 2004 9 21 DHL2004806002 120040828A2612 WARNING LIGHT DOUG DC8 DC873F 302199FWP COCKPIT ILLUMINATED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01806DH 46002 BELL FIRE DETECTOR CODE AD13477 B ILLUMINATED. TRANSFERRED TO DMI 17690 IAW MEL 26-10-1-A-1 CAT-C. PLACARDS INSTALLED, SYS OK LIGHT ILLUMINATED. 2L74 4F RT4A25 20040921001262004092100126 2004 9 21 SWAA042706 420040917A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040921001282004092100128NM 2004 9 21 SWAA042708 120040917A57536546434302 SKIN BOEING737 7375H4 138449DNM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29528SW 26570 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20040921001292004092100129NM 2004 9 21 SWAA042709 120040918A3320S417N3125SP SHIELD BOEING737 7377H4 1384404NM CAUTION PANEL OUT OF ADJUST A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29740SW 29276 ON DESCENT INTO BNA, FLIGHT ATTENDANT REPORTED STRONG BURNING SMELL FROM FWD LAV. NO VISIBLE SMOKE, SMOKE REMOVAL CONFIGURATION IMPROVED SMELL, BUT WAS STILL STRONG IN LAV. REPOSITIONED PLASTIC SHIELD ON PAX RETURN TO SEAT/ATTN CALL LIGHT PANEL IN FWD LAV PER MM. 2L72 4F RTA16WE 20040921001322004092100132NM 2004 9 21 SWAA042712 120040918A5210507946 BRACKET BOEING737 7373Y0 1384671NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR CUTOUT LOWER HINGE BRACKET CRACKED. REPAIRED LOWER BRACKET PER EA. 2L72 4F RTA16WE 20040921001342004092100134NM 2004 9 21 SWAA042714 120040918A533065C32356 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040921001372004092100137 2004 9 21 SWAA042717 420040919A25651061323 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 R2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040921001422004092100142EU 2004 9 21 DHL2004362008 120040727A5230RYLCS52740 ACTUATOR AIRBUS300 A300B4203 3930306EU CARGO DOOR OVERHEATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 CARGO DOOR ACTUATOR POPS C/B. REMOVED INNER & OUTER ACCESS PANELS AS REQ. TO ACCESS M.C.D. LATCH SHAFT AND DISCONNECTED FWD COUPLING FOUND BOLTS TWISTED AND BENT, AND FWD LATCH ACTUATOR LIMIT SWITCH OUT OF ADJUSTMENT IAW A-300 B 4 SAMM 52-36-11. REMOVED MAIN CARGO DOOR FWD LOCK-SHAFT. REMOVED MAIN CARGO DOOR CENTER TORQUE TUBE. REINSTALLED MAIN CARGO DOOR LATCH ACTUATOR, OPS CHECK NORMAL. REPLACED MAIN CARGO DOOR FWD SHAFT COUPLING BOLTS. ADJUSTED MAIN CARGO DOOR FWD LATCH ACTUATOR LIMIT SWITCH AND OPS CK NORMAL. INSTALLED O/S BOLTS IN REWORK AREA WITH FR PRIMER. REINSTALLED THE REMOVED INNER AND OUTER ACCESS PANELS IAW A-300 B4F SAMM 52-36-11. COMPLIED WITH PRESSURIZATION TEST IAW A-300 SAMM 05-53-00.2L72 4F RTA35EU 20040921001442004092100144NM 2004 9 21 DHL2004745523 120040706A5311 FRAME BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, AFT CARGO FRAME BS 1030 HAS A DENT INTO THE RADIUS ABOVE STR 25L. DAMAGED AREA OUT OF LIMITS IAW 727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED AREA DIM 1.75 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075-T6 .071 PO 900489 DIM 11.75 X 4 INCHES IAW 727 SRM 51-40-2 FIG 3. DOUBLER (ANGLE) TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-40-3 FIG 1. 2L73 4F A3WE 20040921001452004092100145NM 2004 9 21 DHL2004745530 120040715A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, RT FUSE HAS A CREASE IN THE SKIN BS 440 TO BS 520 BELOW STR 20R. REWORKED SKIN TO ORIGINAL CONTOUR AT BS 440-500 STR 20R-21R IAW 727 SRM 51-40-1. CUT OUT DAMAGED AREA BS 520 STR 20R-21R AND FABBED FILLER FROM 2024-T3 .050 PO 900980 DIM 5 X 2.875 INCHES AND DOUBLER FROM 2024 T3 .063 PO 900920 DIM 13 X 8 INCHES IAW 727 SRM 53-30-03 FIG 2. PARTS TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10-2 & 53-30-3 FIG 2. REPAIR IS CATEGORY-A. 2L73 4F A3WE 20040921001462004092100146NM 2004 9 21 DHL2004745525 120040706A5314 KEELBEAM BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, LT WHEEL WELL BS 870 & KEEL BEAM VERTICAL STIFFENER CRACK INDICATION NDT VERIFIED MED. REMOVED AND REPLACED LT W/W BS 870 KEEL BEAM VERTICAL STIFFENER IAW B727 SRM 51-30-2 PO 4274124, P/N 65-18636-377. 2L73 4F A3WE 20040921001472004092100147NM 2004 9 21 DHL2004745532 120040716A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, LT LOWER FUSELAGE STA 675 STR 26L HAS SKIN PILLOWING WITH A POPPED FASTENER. REMOVED FASTENERS AT BS 675 STR 26L IAW B727 SRM 51-30-2, DUE TO THE FURTHER EVALUATION NO CORROSION FOUND ON SKIN. STRINGER 26L AT BS 670 TO BS 685 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED STRINGER AND FABBED NEW FROM BAC 1498-99 PO 3357127 DIM 10.5625 INCHES LONG AND 2 SPLICES FROM BAL 1498-B1 PO 422371 DIM 10.75 AND 13.25 INCHES IAW B727 SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2, INSTALLED IAW B727 SRM 51-302. 2L73 4F A3WE 20040921001482004092100148NM 2004 9 21 DHL2004745536 120040724A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, AFT AIRSTAIR EXTERNAL SKIN CREASED AT BS 1323. CUT OUT DAMAGED AREA DIM 2 X 1.25 INCH AND FABBED DOUBLER FROM 2024 T3 .050 PO 9001189 DIM 5 X 5 INCHES IAW 727 SRM 52-10-2 FIG 3. DOUBLER TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 & 52-10-2 FIG 3. 2L73 4F A3WE 20040921001492004092100149NM 2004 9 21 DHL2004745563 120040820A5532 SKIN BOEING727 727224 1384076NM VERTICAL STAB DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, RT VERT STAB LWR AFT AREA AT ABOUT STA 1381 (TRAPAZOID) COMPOSITE PANEL IS DELAMINATED AROUND PREVIOUS REPAIR. CUT OUT DELAMINATED AREA OF RT VERTICAL STAB TRAPAZOID PANEL AT PREVIOUS REPAIR APPROX 8 INCHES DIA, FABRICATED FILLER APPROX 8 INCHES DIA AND DOUBLER APPROX 11.5 INCHES DIA FROM .016 2024T3 PO 900962. APPLIED ADHESIVE PRIMER AND BONDED REPAIR PARTS, CURED, SANDED, SMOOTH, CLEANED, PRIMED AND SEALED IAW B727 SRM 55-30-2 FIG 1 AND 51-40-20- FIG 30. 2L73 4F A3WE 20040921001502004092100150NM 2004 9 21 DHL2004745543 120040807A5754 RIB BOEING727 727224 1384076NM NR 5 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, NR 5 SLAT ACTUATOR ROD END O/B RIB IS CRACKED. REMOVED & REPLACED DAMAGED RIB 65-17276-9 PO 4175196 IAW 727 SRM 51-30-2 ON NR 5 SLAT O/B RIB. 2L73 4F A3WE 20040922000032004092200003WP 2004 9 22 GTIA040713 120040810A3350 LIGHT DOUG DC9 DC983 3022083WP COCKPIT INOPERATIVE A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23832NK 49618 FLL - FLT 900 - FOUND COCKPIT OVERHEAD EMERGENCY LIGHT ONE SIDE INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT ASSEMBLY. (M) 2L72 4F RTA6WE 20040922000042004092200004 2004 9 22 GTIA040714 420040809A2565D29982121 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR MISRIGGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 DTW - FOUND ESCAPE SLIDE IMPROPERLY RIGGED, PULL HANDLE NOT ATTACHED. REMOVED AND REPLACED R1 DOOR SLIDE PACK. (M) 2L72 4F A6WE 20040922000062004092200006 2004 9 22 GTIA040715 420040809A2565 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR MISRIGGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 FOUND R1 ESCAPE SLIDE IMPROPERLY RIGGED, PULL HANDLE NOT ATTACHED. ATTCHED MANUAL PULL HANDLE. (M) 2L72 4F A6WE 20040922000072004092200007 2004 9 22 GTIA040716 420040805A2565D29985103 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FLL - FOUND L2 DOOR EVAC SLIDE FELL DOWN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE. (M) 2L72 4F A6WE 20040922000092004092200009 2004 9 22 GTIA040708 420040807A2565 SLIDE DOUG DC9 DC981 3022081WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 FLT 642 - TPA - FOUND L2 SLIDE PACK FALLING OFF. RESECURED L2 SLIDE PACK AND COVER. (M) 2L72 4F A6WE 20040922000102004092200010WP 2004 9 22 GTIA040700 120040731A7160801407 GUIDE VANE DOUG DC9 DC983 3022083WP NR 2 ENGINE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23835NK 53044 NR 2 ENGINE IGV HAS CRACK AT 1:00 POSITION, UPON INSPECTION FOUND CRACK HAS PROGRESSED BEYOND LIMITS AND ALSO HAS CRACK AT BOTTOM OF SAME VANE. REMOVED AND INSTALLED NR 2 ENGINE IGV. (M) 2L72 4F RTA6WE 20040922000112004092200011WP 2004 9 22 GTIA040691 120040708A5755 SKIN DOUG DC9 DC982 3022082WP RT WING SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER TOP SIDE HAS DENTS AND AREAS OF DELAMINATED. REPAIRED AREA OF DELAMINATED. (M) 2L72 4F A6WE 20040922000132004092200013WP 2004 9 22 GTIA040696 120040729A2912AC7031H8K1 FILTER HOUSING DOUG DC9 DC981 3022081WP RT HYD SYS CRACKED A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23810NK 48015 JUST AFTER SELECTING SLATS EXTEND, RT HYD QTY FOLLOWED BY PRESSURE FELL TO ZERO. FOLLOWED QRH PROCEDURE AND LANDED STOPPING ON RUNWAY UNTIL MAINTENANCE CAME OUT TO SECURE DOORS. TOWED TO GATE. TSHOOT, FOUND RT SYSTEM PRESS FILTER HOUSING IN AFT AIRSTAIRS MISSING DELTA P INDICATOR ASSEMBLY. REMOVED AND REPLACED RT SYSTEM PRESSURE FILTER HOUSING. REMOVED AND REPLACED RT CASE DRAIN FILTER ELEMENT SERVICED RT HYDRAULIC SYSTEM. OPS AND LEAK CHECK BOTH FILTERS. NO DEFECTS NOTED. A/C OK FOR SERVICE. (M) 2L72 4F A6WE 20040922000152004092200015 2004 9 22 GTIA040694 420040801A2565 SLIDE DOUG DC9 DC982 3022082WP PAX DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 DTW - FLT 8111 - FOUND LEFT SLIDE PACK FELL OFF DOOR. INSTALLED SLIDE PACK. (M) 2L72 4F A6WE 20040922000172004092200017WP 2004 9 22 GTIA040693 120040708A5755 SKIN DOUG DC9 DC982 3022082WP LT WING SPOILER DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FOUND LT WING INBOARD FLIGHT SPOILER TOP SIDE HAS DENTS AND AREA OF DELAMINATED. REPAIRED DELAMINATED AREA. (M) 2L72 4F A6WE 20040922000182004092200018WP 2004 9 22 GTIA040697 120040802A5350 LANYARD DOUG DC9 DC983 3022083WP TAILCONE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23814NK 49619 FLL - INSPECT TAILCONE FOR PROPER INSTALLATION DUE OT PREVIOUS ITEM 262316-1. FOUND KEVLAR LANYARD IMPROPERLY ROUTED, RE-ROUTED TAILCONE KEVLAR LANYARD AND INSPECTED TAILCONE INSTALLATION. (M) 2L72 4F RTA6WE 20040922000192004092200019WP 2004 9 22 GTIA040698 120040731A3260 POSITION SWITCH DOUG DC9 DC982 3022082WP RT MLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL23801NK 48048 RIGHT RED GEAR UP AND LOCK LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. RECYCLED GEAR PER QRH. LIGHT WENT OUT ABOUT 45 SECONDS AFTER RETRACTION. LUBRICATED RT MAIN GEAR UPLOCK MECH. REMOVED AND REPLACED RT MLG POSITION SWITCH. REMOVED AND REPLACED SENSOR D1-27. (M) 2L72 4F A6WE 20040922000202004092200020 2004 9 22 GTIA040703 420040803A2565 LANYARD DOUG DC9 DC983 3022083WP SLIDE COVER MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FLL - FOUND SLIDE COVER QUICK DISCONNECT IS NOT ROUTED CORRECTLY. RE-ROUTED SLIDE COVER QUICK DISCONNECT. (M) 2L72 4F RTA6WE 20040922000212004092200021WP 2004 9 22 GTIA040436 120040311A5313 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FOUND LONGERON 30 STATION 1320 TO 1330 HAS CORROSION AROUND FASTENERS. REMOVED LONGEORN SPLICE BETWEEN STATION 1281-1309. REMOVED DAMAGED L30 FROM 1281-1348. LOCATED AND DRILLED NEW LONGEORN SECTION. INSTALLED L30 AND SPLICES. (M) 2L72 4F A6WE 20040922000222004092200022WP 2004 9 22 GTIA040437 120040322A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FOUND SEAT TRACK SEAT ATTACHMENT CORROSION SEAT NR 30 LEFT INBOARD AND OUTBOARD TRACKS OUT OF LIMITS AT STATION 1240 LEFT INBOARD. REMOVED LEFT INBOARD SEAT TRACK FS 1309-155. LOCATED AND DRILLED SEAT TRACK. INSTALLED SEAT TRACK. (M) 2L72 4F A6WE 20040922000232004092200023 2004 9 22 GTIA040711 420040808A2565113317 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23830NK 49932 FLL - FOUND R1 DOOR SLIDE FELL OFF DOOR AND ON TO GROUND. REMOVED AND REPLACED R1 DOOR SLIDE. (M) 2L72 4F A6WE 20040922000242004092200024WP 2004 9 22 GTIA040709 120040806A5260 STRAP DOUG DC9 DC982 3022082WP AIRSTAIR DOOR DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 ACY - FOUND STRAP DISCONNECTED ON AFT STAIR DOOR SLIDE. RECONNECTED STRAP ON AFT STAIR DOOR, OPS CHECK OK. (M) 2L72 4F A6WE 20040922000252004092200025WP 2004 9 22 GTIA040710 120040808A3230 LINK DOUG DC9 DC982 3022082WP CYLINDER BROKEN A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23804NK 49104 AFTER TAKEOFF LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. GAR SAFE LIGHT ILLUMINATED ON GEAR EXTENSION. REMOVED AND REPLACED LEFT MLG RETRACT CYLINDER LOWER LINKS. UPON INSPECTION FOUND LOWER LINK BROKEN. OPS CHECK GOOD. (M) 2L72 4F A6WE 20040922000262004092200026WP 2004 9 22 GTIA040704 120040804A3231 ROD DOUG DC9 DC982 3022082WP MLG DOOR OUT OF ADJUST A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23801NK 48048 AFTER GEAR RETRACTION RT MAIN RED INDICATOR LIGHT STAYED ON 15 SECOND LONGER THAN THE OTHER GEAR INDICATOR LIGHTS. RT HYD PRESSURE MOMENTARILY DROPPED TO 1500 PSI. ALL PUMPS ON HI/ON CRUISE ALT, FL 350, WHEN LEVELING OFF THE GEAR DOOR OPEN LIGHT FLICKERED ON AND THEN OFF AFTER THAT ALL WAS NORMAL. GEAR EXTENSION NORMAL, NO USUAL NOISE OR OTHER INDICATOR. REMOVED AND REPLACED LT AND RT MLG DOOR ACTUATORS. OPS AND LEAK CHECK GOOD, FOUND LT AND RT DOOR SEQUENCING ROD OUT OF RIG. ADJUSTED SEQUENCING DOOR ROD FOR THE LT AND RT MLG GEAR AS REQUIRED. OPERATIONAL CHECK GOOD. REF LOG PG 291777-1 AND 291777-2 FOR MLG DOOR ACTUATOR P/N'S AND S/N'S RIGGED MLG CONTROL VALVE AS REQUIRED. (M) 2L72 4F A6WE 20040922000272004092200027WP 2004 9 22 GTIA040705 120040805A3260 WARNING LIGHT DOUG DC9 DC982 3022082WP RT MLG ILLUMINATED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23801NK 48048 TPA - FLT 642 - RIGHT GEAR LIGHT 'RED' STAYS ON AFTER GEAR IS UP. NO GEAR DOOR OPEN LIGHT RECYCLE GEAR ALL NORMAL. SEE LOG PGS 291781-1N 2, 3 AND 291782-1, 2 AND 3 FOR FINDING AND CORRECTIONS. CYCLED MAIN GEAR SEVERAL TIMES. NO DISCREPANCY NOTED. GEAR PINS REMOVED. (M) 2L72 4F A6WE 20040922000282004092200028NM 2004 9 22 GTIA040706 120040807A2170 COALESCER BAG DOUG MD80 MD83 3023681NM CABIN AIR CONTAMINATED A GTIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23828NK 49823 LAX - FLT 874 - AFTER TAKEOFF, SMOKE STARTED COMING OT OF THE LEFT AFT LAV, DECLARED AN EMERGENCY AND LANDED ALL ELSE WAS NORMAL. FOUND OIL RESIDUE AT BOTH OF COALESCER BAGS. REMOVED AND REPLACED COALESCER BAGS. OPS AND LEAK CHECK NORMAL. RAN BOTH ENGINES AND RAN BOTH PACKS AT HIGH ENGINE POWER SETTINGS AND NO FAULTS NOTED. OK TO CONTINUE. (M) 2L72 4F RT 20040922000322004092200032SO 2004 9 22 SIMA200423905 120040820A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMGAED AREA. FABRICATED A FILLER, SHIMS AND EXTERNAL ANGLE. RPAIR DONE IAW EMB 145 SRM, SRM 145/1142, REV 26, CHAPTER 53-21-10. (M) 2L72 4F RTT00011AT 20040922000332004092200033SO 2004 9 22 SIMA200423906 120040822A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUTOUT OF THE DAMAGED AREA AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR DOUBLER, FILLER TWO SHIMS AND BOTTOM PLATE. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20040922000362004092200036SO 2004 9 22 SIMA200423908 120040820A532014529150001 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24-25. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 26, 53-22-10. (M) 2L72 4F RTT00011AT 20040922000382004092200038WP 2004 9 22 GTIA040682 120040727A3210 LANDING GEAR DOUG DC9 DC982 3022082WP LEFT MALFUNCTIONED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 WHILE IN FLARE RWY 13 THE LEFT MAIN LANGING GEAR INDICATION WENT FROM GREEN TO RED WITH ASSOCIATED VOCAL WARNING. WENT AROUND AFTER A MOMENTARY TOUCH. DURING THE GO THE GEAR INDICATION RETURNED TO NORMAL AND MADE THE CIRCUIT WITH GEAR DOWN. A NORMAL LANDING FOLLOWED. PERFORMED BITE CHECK OF PSU. NO DEFECTS NOTED AT THIS TIME. (M) 2L72 4F A6WE 20040922000392004092200039WP 2004 9 22 GTIA040683 120040727A3297 WIRE HARNESS DOUG DC9 DC982 3022082WP MLG INDICATOR DAMAGED A GTIAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL23817NK 49141 ON LANDING ROLL OUT, LT MAIN GEAR INDICATOR FLASHED RED AND AURAL WARNING SOUNDED WHILE TAXIING TO GATE. LIGHT AND WARNING CONTINUES. TROUBLESHOT SYSTEM FOUND BAD SPLICE IN WIRE BUNDLE. REMOVED AND REPLACED SPLICE. (M) 2L72 4F A6WE 20040922000412004092200041EA 2004 9 22 ASOA04511 120040714A5210H341421 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 FLT 4730 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND TO BE STUCK IN THE CLOSED POSITION AND WOULD NOT OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040922000432004092200043EA 2004 9 22 ASOA04516 120040717A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11881AS 7496 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040922000462004092200046NM 2004 9 22 USAA040389 120040726A5330 SKIN BOEING737 737401 1384701NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US43634 23886 PIT - FOUND SKIN CRACKED 1.5 INCH LONG, FORWARD SERVICE DOOR, LOWER AFT CORNER OF APERTURE STA 328. DOUBLER REPAIR INSTALLED PER SRM 53-10-01. (M) 2L72 4F RTA16WE 20040922000482004092200048NM 2004 9 22 USAA040392 120040722A575465C26601170 SKIN BOEING737 737301 1384611NM NR 1 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US 23559 PIT - FOUND TOP SKIN AND CORE BOND 3 INCH BY 3.5 INCH AREA DELAMINATED, NR 1 SLAT OUTBOARD T/E. REMOVED DELAMINATED, SKIN CORE 7 INSTALLED NEW AND TOP DOUBLER PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040922000512004092200051NM 2004 9 22 USAA040374 120040729A574065C3649222 FITTING BOEING737 7373B7 1384580NM RT WING SPAR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 FOUND AFT SPAR ATTACH FITTING CRACKED .25 INCH, LANDING GEAR BEAM AFT SPAR ATTACH FITTING, RIGHT WING AFT SPAR. MODIFIED PART INSTALLED PER EO 5702V054. (M) 2L72 4F RTA16WE 20040922000532004092200053NM 2004 9 22 USAA040377 120040721A5312 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND FRAME CRACKED .5 INCH, BELTFRAME STATION 767 AT STRINGER S14L. INSTALLED DOUBLER AND FILLERS PER SRM 53-00-07 PAGES 202-203. (M) 2L72 4F RTA16WE 20040922000542004092200054NM 2004 9 22 USAA040382 120040725A574363895 ATTACH FITTING BOEING737 7373B7 1384580NM RT MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND ACTUATOR ATTACH FITTING .25 INCH AREA, RIGHT MLG BEAM NR 6 SPOILER ACTUATOR ATTACH FITTING. INSTALLED NEW FITTING PER BMM 20-50-11-2-912-002 FIG 202. (M) 2L72 4F RTA16WE 20040922000562004092200056EA 2004 9 22 ASOA04488 120040706A3350BF50390901 COVER CNDAIRCL600 CL6002B19 1900309EA EXIT SIGN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11885AS 7521 DURING A C-CHECK IN MCN, THE LT FORWARD EMERGENCY EXIT SIGN COVER BY THE WARDROBE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EMERGENCY EXIT SIGN COVER BY THE WARDROBE. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20040922000572004092200057EA 2004 9 22 ASOA04486 120040706A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11845AS 7324 FLT 4242 - DURING A GROUND INSPECTION IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040922000582004092200058EU 2004 9 22 ASOA04489 120040706A2752 ACTUATOR AEROSPATR72 ATR72 EU LT WING TE FLAP LEAKING A ASOAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO11643AS 413 FLT 4145 - DURING CLIMB-OUT FROM VPS-ATL, AT APPROXIMATELY 6,000 TO 7,000 FEET THE CREW RECEIVED A LOW LEVEL MESSAGE ON THE BLUE HYDRAULIC SYSTEM. THE CREW FOLLOWED THE QRH AND SHUTOFF THE BLUE PUMPS. APPROXIMATELY FORTY MILES FROM ATL, A LOW LEVEL MESSAGE ON THE GREEN HYDRAULIC SYSTEM WAS RECEIVED. THE CREW FOLLOWED THE QUH AND SHUT OFF THE GREEN PUMP EXPERIENCING A TOTAL HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FLAP ACTUATOR. MAINTENANCE ALSO CYCLED THE FLAPS FIFTEEN TIMES WITHOUT ANY DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20040922000632004092200063EA 2004 9 22 COMA0460528 120040911A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NR 3 HYD SYS INOPERATIVE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01949CA23031 7080 FLIGHT 5492 GEAR DISAGREE WARNING. REPLACED THE SYSTEM 3 HYDRAULIC RESERVOIR. 2L72 4F4 FRTA21EA E15NE 20040922000642004092200064NM 2004 9 22 SB04125 120040919A33501012721 SOCKET BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE SEAT 22C DISCONNECTED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19384US 22957 MAINTENANCE REPORTED THE FLOOR EMERGENCY LIGHT AT SEAT ROW 22C WAS INOPERATIVE AND NOT CONNECTED TO THE SEAT. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT ROW 22C. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20040922000682004092200068EU 2004 9 22 HE66097244 120040910A6720 BEARING BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL BELLCRANK WORN B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03202LF 2014 BEARINGS ARE WORN CAUSING EXCESSIVE PLAY. 1G72 3U3 U H3AU E1GL 20040922000712004092200071SW 2004 9 22 ALGA097278 120040907A6420206011814113 HOUSING BELL 206 206L4 1182110SW ALLSN 250C 250C30 03013GL TAIL ROTOR PEELING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL1635 52280 BLUE EPOXY COATING PEELING. REPLACED W/SERVICEABLE HOUSING BY OVERHAUL SHOP. 1G71 3U3 UNCH2SW E1GL 20040922000752004092200075EA 2004 9 22 SWIA200413798 120040612A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW 7028 RT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTION.) SB 601R-53-055, REV-A STRUCTURAL REPAIR AT F.S. 718.00 RT BETWEEN STRINGERS 10 AND 12, PART-E INCORPORATED. 2L72 4F4 FRTA21EA E15NE 20040922000772004092200077SO 2004 9 22 SWIA200413800 120040908A5210 HANDLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE MAIN CABIN DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW 120281 FA CAN NOT OPEN MAIN CABIN DOOR. HANDLE ONLY MOVES .2500 IN BEFORE STICKING. LUBED PASSENGER DOOR. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040922000792004092200079SO 2004 9 22 SWIA200413802 120040910A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07393SW9496 9496 120330 RT IB FLAP DOES NOT FULLY RETRACT. REPLACED RT IB FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040917000902004091700090NM 2004 9 17 CALA0400636 120040914A53476545410199 SEAT TRACK BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712349 23587 INSPECTION FOUND A .5 INCH CRACK IN LT OB SEAT TRACK, OB FLANGE AT STA 727B. A REPAIR WAS INSTALLED IAW ECRA 5321-01202. 2L72 4F4 FRTA16WE E2GL 20040917000922004091700092NM 2004 9 17 CALA0400637 120040824A53156545410199 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSLEAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND A CRACK IN THE LONGITUDINAL FLOORBEAM UPPER CHORD AT ITS ATTACHMENT TO THE TRANSVERSE FLOORBEAM AT STA 727B, LBL 45.50. THE CRACK WAS LOCATED ON THE OB SIDE OF THE LONGITUDINAL FLOORBEAM AT THE FIRST HI-LOK FASTENER HOLE FORWARD OF STA 727B. THE CRACK RAN FROM THE AFT EDGE OF THE LONGITUDINAL FLOORBEAM TO THE HI-LOK FASTENER HOLE. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01200. 2L72 4F4 FRTA16WE E2GL 20040917001012004091700101WP 2004 9 17 MWEA040165 120040915A523059101419 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 MID CARGO DOOR OUTER PAN IS CRACKED APPROXIMATELY 1.6250 INCH IN RADIUS BELOW AFT LOCKING RECEPTACLE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20040917001032004091700103NM 2004 9 17 UPS04443114 120040817A571465B1569720 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE CENTER TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT RBL 10 IN. SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8. 2L74 4F4 FRTA20WE E3NE 20040917001052004091700105NM 2004 9 17 UPS04443116 120040817A571465B156971 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE CENTER TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C CTR TANK FRONT SPAR LOWER CHORD SHEAR TIE FOUND CRACKED AT LBL 65. SHEAR TIE REPLACED IAW SRM 51-10-01 PG 8. 2L74 4F4 FRTA20WE E3NE 20040917001072004091700107NM 2004 9 17 UPS04443118 120040817A571465B1569711 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE CENTER TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 75. SHEAR TIE REPLACED IAW SRM 51-10-01 P8. 2L74 4F4 FRTA20WE E3NE 20040917001092004091700109NM 2004 9 17 UPS04543127 120040914A5230210013 DOOR BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE CARGO INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01422UP 25324 MAIN CARGO DOOR WILL NOT CLOSE. COMPLY WITH DMP 52-32-1, REPLACED ARM SWICH IN P 81 PANEL IAW MM 52-32-13-4. OPS CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20040917001112004091700111WP 2004 9 17 UPS04843121 120040913A3350 LIGHT DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE EMERGENCY EXIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01701UP 45938 EMERGENCY EXIT LIGHTS DO NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK UNIT; SYSTEM OPS CHECK NORMAL IAW MM33-50-01-2. 2L74 4F4 FRT4A25 E2GL 20040917001132004091700113WP 2004 9 17 UPS04843128 120040819A5312SAASK807993X BULKHEAD DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C2, THE AFT PRESSURE BULKHEAD WEB APPROXIMATE 2 INCH CRACK AT RBL 3 STA.1766 FROM INSIDE 60 H0LE. REPAIRED AFT PRESSURE BULKHEAD WEB 2 INCH CRACK AT STA.1766 RBL 3 IAW SAA SK708-993 DATED 8/26/04, UPS EO DC8-5320-20956 DATED 09/08/04 & 8110-3 DATED 08/25/04. 2L74 4F4 FRT4A25 E2GL 20040920000012004092000001NM 2004 9 20 04FDEA02607 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000022004092000002NM 2004 9 20 04FDEA02608 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000062004092000006NM 2004 9 20 04FDEA02612 120040903A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F4 FRTA22WE E31N3 20040920000092004092000009EA 2004 9 20 04251709 120040904A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT INOPERATIVE A VTZAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 EA27709BR 7850 EVENT SUMMARY STATED PACK OVERPRESSURE ON TO RTG AND RECONFIGURED. CREW REPORT STATED STARTED TAKEOFF ROLL AND WE RECEIVED A LT PACK OVER PRESSURE CAUTION MSG. ABORTED THE TAKEOFF. CONTACTED MX CTRL AND WE DECIDED TO RESET PACK AND DEPART WITH BLEEDS ON THE APU. (RT PACK WAS DEFERRED). THE SUBSEQUENT TAKEOFF AND FLIGHT WAS WITHOUT INCIDENT. 2L72 4F4 FRTA21EA E15NE 20040920000112004092000011NM 2004 9 20 QXEA200400674 120040908A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 800 STICKING A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09400QX7811 4030 THE CREW REPORTED THE MAIN CABIN DOOR HANDLE DIFFICULT TO OPERATE. MAINTENANCE INSPECTED THE DOOR AND HANDLE, THEN CLEANED AND LUBED THE MAIN CABIN DOOR LATCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20040920000392004092000039WP 2004 9 20 ARWA20040806 120040830A3231510361C LINK ASSY DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NLG DOOR FAILED A ARWAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19784AL 46135 AFTER TAKEOFF, HAD A VIBRATION BELOW COCKPIT AREA RECYCLED LANDING; GEAR NO HELP; RETURNED TO DEPARTURE (KMIA. REMOVED AND REPLACED RT NOSE GEAR DOOR LINK ASSEMBLY IAW MM 32-22-2. OPERATIONAL CHECK NORMAL. 2L74 4F4 F 4A25 1E8 20040920000652004092000065CE 2004 9 20 R2J2004F00001 120040629A27505565200 CONTROL CABLE CESSNA501 501 2076603CE PWA JT15 JT15D1 52060NE TE FLAPS MISINSTALLED B R2JRO OTHER O OTHER NRNOT REPORTED 1 EA21501CF5689 5010128 DURING PHASE 5 INSPECTION, UPON REINSTALLING LT WING FLAP CABLES, NOTICED AIRCRAFT WAS DIFFERENT THAN MM DATA AS TO ROUTING OF FLAP CABLES ON LT OB BELLCRANK. EXPERIMENTED AND CONTACTED MFG TECH SUPPORT. FOUND DATA ON PG 27-50-01 PG 203 FIG 201 (SHEET 2) SHOWED CABLES REVERSED ON BELLCRANK GROOVES. THIS CAUSES CABLE INTERFERENCE WITH STRUCTURE. (EA21200406587) 1L72 4F4 F A27CE E1NE 20040920001062004092000106EU 2004 9 20 KBM2004F00175 120040529A6510350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 T/R PC LINK HAS RADIAL PLAY (.008) IN THE SPHERICAL BEARING AND A CRACK IN THE SILENT BUSH. REMOVED AND REPLACED. 1G71 3U3 U H9EU E4CE 20040920001132004092000113NE 2004 9 20 ASMF200408018 220040819A73207434968 SOLENOID DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT SIDE DAMAGED W ASMFK NONE J WARNING INDICATION CRCRUISE 1 SW23158PL 49761 725857 CAPTAIN REPORTED PILOTS AIR CONDITIONING CONTROLLER INSTABLE, BOTH ENGINES DID NOT DECELERATED UNDER 1.17 EPR IN IDLE AND ELECTRICAL FAILURE IN RT ENGINE LOOP B. TECHNICAL PERSONNEL PERFORMED THE FOLLOWING MAINTENANCE TASKS: AIR CONDITIONING TEMPERATURE SENSOR CABIN WAS CLEANED IAW MM 21-61-3. IDLE SOLENOID OF ENGINE NR 1 WAS REPLACED IAW MM 73-20-05 AND LOOP B REPORT WAS DEFERRED IAW MEL 26-1-1 CAT C. DURING OVERNIGHT SERVICE, RT ENGINE AMPLIFIER WAS REPLACED IAW MM 26-10-03, TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20040920001322004092000132WP 2004 9 20 COOSDR040007 120040630A5532 PANEL DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE VERTICAL STAB DEBONDED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 VERTICAL STABILIZER TRAILING EDGE SECTION, UPPER AND LOWER PANELS WITH SKIN DEBONDING. 2L74 4F4 F 4A25 1E8 20040920001892004092000189NM 2004 9 20 SWAA042686 120040915A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 930, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040920001912004092000191NM 2004 9 20 SWAA042674 120040914A2612 FIRE DETECTOR BOEING737 7373H4 1384600NM CARGO BAY FALSE INDICATIONA SWAAO OTHER N FALSE WARNING CRCRUISE 1 SW29365SW 26576 AT FL 350 FWD/AFT/BTL1/BTL2/BELL/WARNING MASTER CAUTION ILLUMINATED. THEN ALL EXTINGUISHED 10 SECONDS LATER, NO OTHER INDICATIONS. NO BOTTLES DISCHARGED. INSPECTED FWD AND AFT CARGO COMPARTMENTS, BAGGAGE CHECKED, NO ABNORMAL INDICATIONS. CARGO FIRE DETECTOR SYSTEM CHECKS GOOD PER MM. 2L72 4F RTA16WE 20040921000122004092100012 2004 9 21 04FDEA02683 420040914A3414 LINE AIRBUS310 A310203 3930313EU AIRSPEED IND OBSTRUCTED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25401FE 191 ON TAKEOFF ROLL AT 80KTS ON CAPT & F/O'S PFD THE AIRSPEED INDICATED 80KTS BUT BOTH STANDBY AIRSPEED INDICATORS WERE STILL SHOWING 60KTS AT 100KTS ON BOTH PFD` S THE STANDBY AIRSPEEDS WERE BOTH LESS THAN 80KTS. BLEW OUT STBY & NR 1/2 PITOT LINES. FOUND SMALL DEBRIS IN STBY AIRSPEED LINE. OP/C GOOD IAW A310-200 MM 34-11-15-6. NO CHANGE IN RVSM STATUS. 2L72 4F RTA35EU 20040921000222004092100022EA 2004 9 21 ASOA04586 120040810A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11872AS 7542 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 582.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040921000272004092100027EA 2004 9 21 ASOA04570 120040808A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11873AS 7549 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040921000402004092100040EA 2004 9 21 ASOA04589 120040812A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11827AS 7212 DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000422004092100042EA 2004 9 21 ASOA04603 120040816A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL FORWARD OF THE TIE DOWN AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72-589 IAW ASA EO 600-53-0095. (M) 2L72 4F RTA21EA 20040921000442004092100044WP 2004 9 21 GTIA040289 120040316A5320 SPLICE DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FOUND AFT PIT STATION 1307 LEFT FORWARD AND AFT FRAME SPLICE HAS CORROSION. AFT LEFT SPLICE FOND TO BE OUT OF LIMITS. FABRICATED NEW SPLICE. LOCATE AND DRILLED NEW SPLICE. (M) 2L72 4F A6WE 20040921000572004092100057EA 2004 9 21 ASOA04593 120040813A2751855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA RT WING MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11908EV 7654 UPON NORMAL TAKEOFF FROM DFW-CG, WHILE CLIMBING THROUGH APPROXIMATELY 14,000 FEET THE CREW RECEIVED AN AMBER FLAPS FAIL CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED, REPLACED AND RE-RIGGED THE BRAKE AND POSITION SENSOR UNIT BPSU. MAINTENANCE ALSO CHECKED THE RIGGING OF THE FLAPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000612004092100061WP 2004 9 21 GTIA040745 120040824A2820 LINE DOUG DC9 DC983 3022083WP FUEL MANIFOLD LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23832NK 49618 LGA - DRAINED FORWARD AUX TANK DUE TO FINDING FUEL IN SHROUD DRAIN. LOCATED LEAK AT INLET MANIFOLD LINE, REMOVED AND REPLACED O-RINGS. GTIA (M) 2L72 4F RTA6WE 20040921000632004092100063SO 2004 9 21 SIMA200423909 120040821A532014521713001 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE 145314 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED A CUT OUT OF THE DAMAGED AREA AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 26, CHAPTER 53-22-10 FIGURE 203 AND EMB REPAIR STATEMENT IC2003-145/3835 DATED AUGUST 18, 2004. (M) 2L72 4F RTT00011AT 20040921000892004092100089SO 2004 9 21 SIMA200423301 120040819A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZONTAL STAB MALFUNCTIONED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 SW21800AE 145425 YHZ - FLT 4819 - ON SHORT FINAL WITH AP DISCONNECTED AT APPROX 135 KTS IN VMC CONDITIONS THE CREW RECEIVED EICAS MESSAGES PITCH TRIM 1 AND 2 INOPERATIVE. PERFORMED FAULT ISOLATION PROCEDURES IAW ETN EM 27-022R1 NO LATCHED EICAS OR CMC MESSAGES FOUND. AS A PRECAUTIONARY PROCEDURE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 140 AMM CH 27-4-01 OPERATIONAL CHECK SATISFACTORY AT THIS TIME NO FURTHER DEFECTS NOTED. (M) 2L72 4F RTT00011AT 20040921001112004092100111EA 2004 9 21 A6WA200440111 120040717A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31429AW 7711 PASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 310 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 IAW BOMBARDIER REO 601R-53-22-033. (M) 2L72 4F RTA21EA 20040921001122004092100112EA 2004 9 21 A6WA200440112 120040717A5210 STRIKER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31429AW 7711 PASSENGER DOOR SEAL STRIKER HAS DAMAGE AT FS 349 APPROXIMATELY MID POINT OF DOOR OPENING. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 349 IAW BOMBARDIER REO 601R-53-22-033 REPAIR 4. (M) 2L72 4F RTA21EA 20040921001242004092100124 2004 9 21 04241662 420040828A34206229336400 AHRS CNDAIRCL600 CL6002B19 1900309EA NR 1 DEFECTIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27662BR 7526 EFIS COMP MON/ NR 1 AHARS ERRATIC. RETURNED TO FIELD. MX INTERROGATED MDC. FOUND NR 2 AHRS FAIL. REMOVED AND REPLACED NR 2 AHRS REF 34-20-00. CLEARED FCC FAULTS. 2L72 4F RTA21EA 20040921001252004092100125NM 2004 9 21 04242422 120040829A5250 DOOR DORNERDO32 DO328300 NM LAVATORY LOCKED A VTZAO OTHER S AFFECT SYSTEMS CRCRUISE 1 EA27422FJ 3180 PAX WAS USING LAV AND UPON TRYING TO EXIT, THE DOOR WOULD NOT UNLOCK. DIDN'T UNLOCK FROM OUTSIDE EITHER. FINALLY PAX USED SEATBELT EXTENSION TO PRY THE LOCK OPEN FROM INSIDE. MX REMOVED LAV DOOR, CLEANED IT, ADJUSTED IT. NO DEFETCS NOTED JIC 52-51-00. 2H72 4T RTA55NM 20040921001272004092100127NM 2004 9 21 SWAA042707 120040917A575465C26685 SKIN BOEING737 7373K2 13844BANM NR 2 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED C1 CHECK, FOUND 5 EACH CRACKS AT LT WING NR 2 L/E SLAT. REPAIRED NR 2 L/E SLAT SKIN PER SRM. 2L72 4F RTA16WE 20040921001352004092100135NM 2004 9 21 SWAA042715 120040918A533065C32356 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20040921001392004092100139NM 2004 9 21 DHL2004745518 120040706A5753 SKIN BOEING727 727224 1384076NM LT WING FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 C-CHECK, LT OTBD AFT FLAP LOWER SURF WBL 400 HAS 2 AREAS OF DELAMINATION. CUT OUT DELAM AREA. FABBBED ONE FILLER AND ONE DOUBLER. CLEARED, PREPED, APPLIED ADHESHIVE PRIMER & ADHESIVE TO ALL MATING SURFACES. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED, SEALED, REPAIR. CUT OUT DELAM AREA FROM UPPER SKIN. REMOVED AND REPLACED DAMAGED HONEYCOMB CORE AND FABBED ONE FILLER AND ONE DOUBLER. INSTALLED REPAIR, ALODINED, PRIMED AND SEALED IAW B727 SRM 51-40-20 FIG 30. 2L73 4F A3WE 20040921001432004092100143NM 2004 9 21 DHL2004745514 120040705A5347 SEAT TRACK BOEING727 727224 1384076NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, IN MAIN CABIN SEAT TRACK LBL 60 135 495 TO BS 515 SCALLOP IS WARN. CUT OUT DAMAGE SEAT TRACK IAW B727 SRM 53-10-2 FIG 7. FABRICATED SEAT TRACK DIM: 29.5 FROM PART NUMBER BAC 1520-841 PO 416740 IAW B727 SRM 53-10-2. TREATED & PRIMED ALL PARTS & AREA IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727 SRM 53-10-2 AT MAIN CABIN LBL 60 BS 495 TO 515. 2L73 4F A3WE 20040922000082004092200008 2004 9 22 GTIA040717 420040811A2565 LANYARD DOUG DC9 DC982 3022082WP TAILCONE SLIDE MISROUTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 ORD - FLT 433 - TAILCONE ESCAPE SLIDE LANYARDS NOT ROUTED CORRECTLY. ROUTED LANYARDS CORRECTLY. (M) 2L72 4F A6WE 20040922000302004092200030WP 2004 9 22 GTIA040699 120040729A3260833604 UPLOCK SENSOR DOUG DC9 DC982 3022082WP RT MLG MALFUNCTIONED A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23801NK 48048 THE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN HYD PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PUMPING, GEAR AND DOOR MECH ON RIGHT GEAR. NO DEFECTS NOTED REMOVED AND REPLACED RIGHT GEAR UPLOCK SENSOR. REMOVED AND REPLACED PROX SWITCH P/N 833703, ELECT UNIT. (M) 2L72 4F A6WE 20040922000402004092200040EA 2004 9 22 ASOA04513 120040715A5210601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11889AS 7538 FLT 4709 - DURING A GROUND INSPECTION IN DFW, THE BRACE ON THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040922000472004092200047NM 2004 9 22 USAA040391 120040721A575465C26601180 SKIN BOEING737 737301 1384611NM NR 6 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT- FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCH BY 3 INCH AREA, NR 6 SLAT TOP SURFACE OUTBOARD T/E. REMOVED DELAMINATED SKIN, INSTALLED NEW SECTION AND DOUBLER PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040922000502004092200050NM 2004 9 22 USAA040373 120040723A5312 BULKHEAD BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND BULKHEAD WEB CRACKED .5 INCH, FS 178 BULKHEAD WEB, B/L0, WL/L 186. INSTALLED DOUBLER, FILLER PER SRM 53-10-08 FIG 203. (M) 2L72 4F RTA16WE 20040922000742004092200074CE 2004 9 22 GLBA20030721 120040915A5260 HANDLE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE AIRSTAIR DOOR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03247GL UE247 AIRSTAIR DOOR HANDLE SHOWS SIGN OF CORROSION, REMOVED CORROSION AND REPAIRED. 2L72 4T4 TRTA24CE E26NE 20040922000802004092200080SO 2004 9 22 SWIA200413803 120040912A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT DISCHARGED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07577348669 8669 120199 MIDDLE SECTION OF EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040922000812004092200081EA 2004 9 22 SWIA200413804 120040911A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07423SW 7456 CENTER EMERGENCY EXIT LAMP INOPERATIVE. RE-LAMPED CENTER EMERGENCY EXIT LAMP. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040922000832004092200083EA 2004 9 22 SWIA200413806 120040910A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07961SW6621 6621 7857 STAB TRIM CHANEL 1 STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR, HORIZONTAL STAB MOTOR CONTROL UNIT AND HSTCU IAW AMM 27-42-01AND MM27-42-05. OPERATIONAL CHECK GOOD. P/N: 7060-9 S/N OFF: 1184 2L72 4F4 FRTA21EA E15NE 20040922000842004092200084EA 2004 9 22 SWIA200413807 120040908A2750601R590141 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07973SW 7949 ON TAKEOFF DURING FLAP RETRACTION, (FLAP FAIL) MSG AND FLAPS FAIL AT 18 DEGREES. INSTALLED SKEW DETECTION SOV. OPERATIONAL CHECK GOOD IAW CRJ MM 27-51-15.P/N: 601R59014-1 SN: A526 2L72 4F4 FRTA21EA E15NE 20040922000862004092200086EA 2004 9 22 SWIA200413809 120040906A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07943SW 7762 FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (ITEM FOUND AT C-CHECK INSPECTION). ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11 2L72 4F4 FRTA21EA E15NE 20040922000872004092200087WP 2004 9 22 UPS04843130 120040908A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01705UP 45949 EMERGENCY LIGHTS FADED DURING EMERGENCY LIGHTS TEST. REMOVED AND INSTALLED A SERVICEABLE LIGHTING BATTERY AND RELAY UNIT REF DC8 MM 30-50-01-2. TEST GOOD. 2L74 4F4 FRT4A25 E2GL 20040922000882004092200088WP 2004 9 22 04FDEA02685 120040914A3260806125 PROXIMITY SWITCH DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL MLG INOPERATIVE A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25389FE3417 3417 46623 AFTER TAKEOFF, ALL GEAR INDICATIONS REMAINED UNSAFE AFTER GEAR HANDLE WAS RAISED AND CHECKED IN, BOTH FRONT AND BACK PANELS. FOLLOWED QRH, CYCLED THE GEAR AND ALL LIGHTS WENT OUT. CONTINUED FLIGHT. TROUBLESHOT IAW DC10 TAFI CHAPTER 32-30-00, FAULT CODE-AA. NO GEAR WARNING HORN WHEN GEAR HANDLE IS PULLED OUT, PROXIMITY ELECTRONICS UNIT DETERMINED TO BE BAD. REMOVED AND REPLACED PROXIMITY SWITCH ELECTRONICS HOUSING IAW DC10-10 MM CHAPTER 32-61-01-2. ALL TESTS/CHECKS PASSED. 2L73 4F4 F A22WE E23EA 20040922000912004092200091EU 2004 9 22 04FDEA02693 120040916A5315A5397826720890 FLOORBEAM AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 BULK CARGO COMPT FLOOR STRUCTURE ON FR67 AT RT SIDE CORNER UNDERNEATH NOTED CRACK. REMOVED AND REPLACED BEAM IAW A310 SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040922000942004092200094EU 2004 9 22 04FDEA02696 120040916A5320A5327828920100 ADAPTER AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 TRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040922000952004092200095EU 2004 9 22 04FDEA02697 120040916A5320A5327828920100 ADAPTER AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 TRACK ADAPTER AT FR61 Y-450 IS CRACKED APPROX 6 INCHES LONG. REMOVED AND REPLACED TRACK ADAPTER IAW A310 SRM 51-40-21. 2L72 4F4 FRTA35EU E13NE 20040922000972004092200097WP 2004 9 22 04FDEA02699 120040916A5415 FITTING DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 1 PYLON CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 NR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIFIED MOUNT BOLT TO BE NAS64044. INSTALLED NEW BEARING ASSY WITH BOLT WET WITH SEALENT AND TORQUED IAW DC-10-30 AMM 54-40-02-2. 2L73 4F4 FRTA22WE E23EA 20040922000992004092200099EU 2004 9 22 AWXA200401031 120040910A5315D53472172200 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD AND AFT SIDE OF BEAM Y1292 LTAFT OF FR 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT AT FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F4 FRTA28NM E311NE 20040922001012004092200101EU 2004 9 22 04FDEA02691 120040916A5320A53974260204 FLOOR SUPPORT AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 BULK CARGO COMPT. FLOOR STRUCTURE, ON RT SIDE FR 66 TO FR 63 CORROSION ON TOP AND BENEATH SURFACE. REMOVED CORROSION IAW SRM 51-70-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING **** 2L72 4F4 FRTA35EU E13NE 20040922001032004092200103EA 2004 9 22 COMA0460524 120040915A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS ILLUMINATED A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01781CA 7312 FLIGHT 5890 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20040922001042004092200104EA 2004 9 22 COMA0460520 120040916A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01965CA 7131 RT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020. 2L72 4F4 FRTA21EA E15NE 20040922001062004092200106NM 2004 9 22 SWAA042719 120040919A53306573742 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 777, STRINGER 21L AND BS 797, STRINGER 22L. REPAIRED SKIN PER EA. 2L72 4F A16WE 20040922001102004092200110NM 2004 9 22 SWAA042723 120040920A52106552873 SKIN BOEING737 7373H4 1384600NM L2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENRTY DOOR SKIN AT UPPER AND LOWER HINGES CRACKED. REPAIRED DOOR SKIN PER SRM. 2L72 4F RTA16WE 20040922001112004092200111NM 2004 9 22 SWAA042724 120040920A53109078224 STRAP BOEING737 7373H4 1384600NM DOOR FRAME CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME UPPER HINGE CUTOUT LOWER CORNER CRACKED. REPAIRED DOOR FRAME UPPER HINGE CUTOUT PER EA. 2L72 4F RTA16WE 20040922001132004092200113NM 2004 9 22 SWAA042726 120040920A533065C33725 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT AFT CORNER, CRACKED. REPAIRED FWD ENTRY DOOR CUTOUT PER EA. 2L72 4F RTA16WE 20040922001142004092200114NM 2004 9 22 SWAA042727 120040920A53106545409 PRESSURE PANEL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, RBL 42, CRACKED. REPAIRED PRESSURE WEB PER SRM. 2L72 4F RTA16WE 20040922001172004092200117NM 2004 9 22 SWAA042730 120040920A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE BULKHEAD WEB AT BS 178, LBL 11, LBL 12 AND RBL 8.5, WL 234. REPAIRED BULKHEAD WEB PER SRM. 2L72 4F RTA16WE 20040922001192004092200119NE 2004 9 22 04244406 220040831A7532 BLEED VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE ENGINE FAILED A VTZAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 EA27406FJ 3156 ABORTED TAKEOFF DUE TO BLEED SOV FAILURE (HPSOV DID NOT OPEN AND LPSOV DID NOT OPEN ABOVE 80 PERCENT). MX INSPECTED BOTH ENGINES AND PERFORMED FUNCTIONAL CHECK FOR BOTH BSOV IAW JIC 71-03-03. NO FURTHER DISCREPANCIES AT THAT TIME. 2H72 4T4 FRTA55NM E35NE 20040922001202004092200120 2004 9 22 04237689 420040824A3418 STALL WARNING CNDAIRCL600 CL6002B19 1900309EA MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA27689BR 7737 STALL FAIL WITH FLAP MOVEMENTS. OPS CHECK STALL WARNING IAW CRJ MM 27-35-01. NO DEFECTS FOUND AT THIS TIME. A/C OK TO CONTINUE SERVICE. 2L72 4F RTA21EA 20040922001212004092200121EA 2004 9 22 04237665 120040824A5210 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CONTAMINATED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27665BR 7534 PAX DOOR SQUEAL. REMOVED GREASE AND DEBRIS FROM PAX DOOR SEAL, PRESSURIZED AC, NO DEFECTS NOTED REF CRJ MM 52-11-10. 2L72 4F RTA21EA 20040922001232004092200123NM 2004 9 22 DHL2004745542 120040803A5754 SUPPORT BOEING727 727224 1384076NM SLAT ACTUATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, NR 5 SLAT ACTUATOR ROD END I/B SUPPORT IS CRACKED. REMOVED NR 5 SLAT FOR ACCESS IAW 727 MM 27-81-11. REMOVED & REPLACED DAMAGED RIB P/N 65-17270U11 PO 4274276 IAW 727 SRM 51-30-2. REINSTALLED NR 5 SLAT IAW 727 MM 27-81-11. 2L73 4F A3WE 20040922001242004092200124NM 2004 9 22 DHL2004745554 120040630A5753 SKIN BOEING727 727224 1384076NM TE FLAP DEBONDED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, RT INBOARD MID FLAP T/E UPPER SKIN SHOW DISBONDED AREAS WBL 160 TO OUTBOARD. CUT OUT DELAMINATED ARE OF RW I/B MIDFLAP T/E UPPER SKIN APPROX 6.5 X 4.25 INCHES & 2 EA DOUBLERS APPROX 3 X 4.5 INCHES FROM 2024-T3 .016 PO 900962 IAW B727 SRM 57-50-2 FIG 3. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIR SURFACES, BONDED, CLEANED, TREATED, PRIMED & SEALED REPAIR IAW B727 SRM 51-40-20 FIG 30. 2L73 4F A3WE 20040922001262004092200126WP 2004 9 22 DHL2004805009 120040810A3241 CONTROL VALVE DOUG DC8 DC873F 302199FWP ANTI-SKID SYS MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01805DH 12064 46125 ANTI SKID LIGHT ON DIM DURING T/O ROLL, T/O WARNING HORN CHIRPS AFTER V1 AND THRU ROTATION. REMOVED AND REPLACED LT MLG STRUT OUTBOARD ANTI SKID CONTROL VALVE PER MM 32-43-3, OPS CHECK GOOD. 2L74 4F RT4A25 20040922001272004092200127NM 2004 9 22 SWAA042655 120040913A55526959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY, CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE BOLT AND BUSHING PER MM. 2L72 4F RTA16WE 20040922001292004092200129NM 2004 9 22 SWAA042657 120040914A53156546804 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAM AT BS 727B, LBL 24, CRACKED. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20040922001302004092200130NM 2004 9 22 SWAA042658 120040914A55536546874 DRAG BRACE BOEING737 7373A4 1384585NM LT VERT STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND LT VERTICAL STABILIZER AFT DRAG BRACE, CORRODED. REMOVED AND REPLACED LT VERTICAL STABILIZER DRAG BRACE PER SRM. 2L72 4F RTA16WE 20040922001312004092200131NM 2004 9 22 SWAA042659 120040914A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT UPPER HINGE, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040922001352004092200135NM 2004 9 22 DL76L040856 120040908A3240 BRAKE BOEING767 767332 1382001NM RT MLG FIRE A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SO27196DN 28453 AT GATE ARRIVAL NR 3 BRAKE HAD A GREASE FIRE. EXTINGUISHED FIRE, REMOVED TIRE AND BRAKE ASSEMBLY, INSPECTED AXLE FOR HEAT DAMAGE, NONE FOUND. INSTALLED NEW BRAKE ASSEMBLY AND NEW WHEEL ASSEMBLY, OPS CHECK OK. 2L72 4F RTA1NM 20040922001362004092200136NM 2004 9 22 SWAA042660 120040914A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040922001372004092200137NM 2004 9 22 SWAA042661 120040914A575365C30462 SKIN BOEING737 7373G7 1384595NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM. 2L72 4F RTA16WE 20040922001392004092200139NM 2004 9 22 SWAA042663 120040914A53306545776 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 931, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040922001402004092200140NM 2004 9 22 SWAA042664 120040914A53156545410 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, RBL 25, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20040922001412004092200141EA 2004 9 22 04236680 120040823A2741 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM FAILED A VTZAK NONE J WARNING INDICATION ININSP/MAINT 1 EA27680BR 7679 STAB TRIM/MACH FAIL. PERFORMED BITE CHECK OF HSTCU. CLEANED YOKE MOUNT DISC SWITCHES AND STAB/TRIM SWITCHES. PERFORMED OPS CHECK. NO DEFECTS NOTED. 2L72 4F RTA21EA 20040922001442004092200144EA 2004 9 22 COMA0460455 120040813A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01409CA 7441 CARGO LANDING CRACKED AT THRESHOLD FWD STOP, UNDER STOP ADJACENT TO HI-LITE. REPAIRED IAW REO 601R-53-61-690. 2L72 4F RTA21EA 20040922001452004092200145NE 2004 9 22 AALA20040914 220040829A7261 NUT BOEING767 767323 1385205NM GE CF6 CF680C2B6 30025NE SCAV PUMP LOOSE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21351AA 24032 690317 DFW - ABOUT 150 MILES FROM DFW OIL QUANTITY WENT TO ZERO AND OIL PRESSURE WENT TO APPROXIMATELY 23 PSI IN THE AMBER BAND. SECURED RIGHT HAND ENGINE PER QHR AS A PRECAUTION. NO OIL TEMPERATURE OR ENGINE TEMPERATURE ON ENGINE TEMPERATURE RED INDICATIONS. LANDED DFW WITHOUT INCIDENT. FOUND LOOSE NUTS ON OIL SCAVANGER PUMP. TIGHTENED LOOSE NUTS AND REFILLED OIL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20040922001462004092200146NM 2004 9 22 AALA2040903 120040824A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21370AA 25197 DFW - EMERGENCY LIGHTS ON AFT SIDE OF FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON AFT SIDE OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040922001472004092200147NM 2004 9 22 AALA20040796 120040610A5310 FAILSAFE BOEING767 767323 1385205NM CARGO DOORFRAME CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21361AA 24042 FAILSAFE FWD CARGO DOOR CUTOUT ANGLE HAS CORROSION REMOVAL BLENDOUTS ON LOWER SURFACE 2 LOCATIONS AT FASTENERS. DEPTH IS 0.030 INCH BY 0.021 INCH STA 591 & 527.65 SECTION 43 FWD CARGO. PERFORMED HIGH FREQUENCY EDDY CURRENT TO INSURE CRACK FREE. ROTOPEEN BLENDED AREA AND REFINISH THE BLENDED AREA WITH ALODINE AND 2 COATS OF BMS10 11 PRIMER. AFTER INSTALLATION OF FAILSAFE STRAP FABRICATE REPAIR STRAPS FROM 7075T7351 PLATE A MINIMUM OF 0.190 THICK. STRAP EXTENDS A MINIMUM OF .5 INCH BEYOND CENTER AT EACH FASTENER HOLE. FINISHED STRAP WITH ALODINE AND 2 COATS OF BMS10 11 PRIMER AND INSTALLED A STRAP AT EACH BLENDED LOCATION. ADJUST RIP LENGTH OF BOLTS TO ACCOMMODATE REPAIR STRAP. 2L72 4F RTA1NM 20040922001482004092200148EA 2004 9 22 COMA0460482 120040823A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A COMAK NONE O OTHER ININSP/MAINT 1 SO01981CA 7163 FLIGHT 5808 EMERGENCY LIGHTS AT RT OVERWING EXIT ARE INOP. FOUND WIRES DISCONNECTED. RECONNECTED WIRES AND LIGHTS OPERATE NORMAL. 2L72 4F RTA21EA 20040922001492004092200149NM 2004 9 22 DL73S040841 120040902A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27311DL 23083 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15 REVEALED A CRACKED FASTENER HOLE AT FS 631. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737-200 SRM AND ER/A 092799-14. 2L72 4F RTA16WE 20040922001512004092200151NM 2004 9 22 DL73S040844 120040904A335020121 CHARGER BOEING737 737232 1384475NM EMERGENCY LIGHT MALFUNCTIONED A DALAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO27303DL 23075 PRIOR TO TAXI OUT, F/A NOTIFIED FLT CREW THAT EMERGENCY LIGHTS SEAT MOUNTED FROM MIDDLE OF A/C TO BACK OF A/C WERE ILLUMINATED DIM. REPLACED M9013 BATTERY PACK, BASE TESTS GOOD. 2L72 4F RTA16WE 20040922001522004092200152NM 2004 9 22 DLM88040845 120040905A3520801386084 GENERATOR DOUG MD88 MD88 3023688NM SEAT 11ABC OXY DISCHARGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27911DL 49542 WHILE CLOSING PSU AT SEAT 11ABC THE O2 GENERATOR FIRED INADVERTENTLY. REPLACED GENERATOR. 2L72 4F RTA6WE 20040922001542004092200154NM 2004 9 22 DL76L040847 120040904A3350 LAMP BOEING767 767332 1382001NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27187DN 27582 EMERGENCY LIGHT INOP AT 36A/B. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA1NM 20040922001552004092200155NM 2004 9 22 DLM88040848 120040905A322039567851 LINK DOUG MD88 MD88 3023688NM NLG BROKEN A DALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO27935DL 49722 SEVERE VIBRATION FROM NOSE GEAR AREA ON TAKEOFF. FOUND LT NOSE GEAR DOOR LINK BROKEN. REPLACED LINK, CHECKED GOOD. 2L72 4F RTA6WE 20040922001562004092200156NM 2004 9 22 DL76L040850 120040905A361080217010 VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE MALFUNCTIONED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27187DN 9806086 27582 724169 ABORTED T/O PRIOR TO 80 KTS EICAS CAUTION LT ENGINE PRV W/AURAL CHIME. STATUS MSG L IDG VALVE. REMOVED AND REPLACED LT ENGINE PRV VALVE AND CONTROLLER. AIR SUPPLY BITE FAULTS PRV PRC AND FAS LAST 2 LEGS. FAULTS CLEARED ERASED. RAN ENGINE TO BLEED SHIFT AND T/O PWR 1.4 EPR NIL DEFECTS NOTED. IDG VALVE FWD TO MCO PER MEL 75-21-01C. 2L72 4F4 FRTA1NM E24NE 20040922001582004092200158NM 2004 9 22 DL76L040858 120040909A335020131A BATTERY PACK BOEING767 767332 1382001NM EMERGENCY LIGHT SHORTED A DALAO OTHER O OTHER CRCRUISE 1 SO27188DN 27583 CB P36 EMERGENCY LIGHTS WING RT POPPED, RESET OK. POPPED AGAIN AFTER 4 HRS, NOT RESET. REPLACED AFT RT AND CTR BATTERY PACKS, CHECK OK. 2L72 4F RTA1NM 20040922001802004092200180NM 2004 9 22 DLM90040862 120040909A2120 INSULATION DOUG MD90 MD9030 3023690NM A/C SUPPLY LOOSE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27901DA 53381 FLIGHT ATTENDANT OBSERVED EXTENSIVE AMOUNT OF SMOKE STRONG ODOR AND HOT AIR IN AFT CABIN PRIOR TO BOARDING. FOUND RIGHT A/C SUPPLY DUCT INSULATION OFF AND TAPE ON DUCT REMOVED TAPE AND REPLACED INSULATION. 2L72 4F RTA6WE 20040922001822004092200182NM 2004 9 22 DL764040864 120040912A3350 LIGHT BOEING767 767432ER 1385134NM AFT BULKHEAD DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27837MH 29710 EMERGENCY LIGHT DAMAGED AT FWD BULKHEAD AFT OF JUMPSEAT NR 108. REPLACED SAME. 2L72 4F RTA1NM 20040922001842004092200184NM 2004 9 22 AALA20040905 120040827A3350 PLUG BOEING757 757231 1384950NM EMERGENCY LIGHT MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21723TW 29378 DFW - EMERGENCY FLOOR TRACK LIGHTING END PLUG MISSING AFT OF SEAT 6A. INSTALLED END PLUG FOR EMERGENCY FLOOR TRACK LIGHTING AFT OF SEAT 6A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040922001882004092200188NM 2004 9 22 SWAA042641 120040911A53156545810 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD AT BS 312, RBL 20 TO LBL 20, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040922001892004092200189EU 2004 9 22 AWXA200400907 120040806A5347D5713014720200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK CORROSION WAS FOUND ON SEAT TRACK Y1292 LT BETWEEN FR 36 AND FR 41. MAINTENANCE REMOVED CORRODED SEAT TRACK FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20040922001902004092200190EU 2004 9 22 AWXA200400711 120040705A2910 SWITCH AIRBUS320 A320232 3930326EU HYD SYSTEM MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28603AW 661 EN ROUTE FROM PHX TO EWR AIRCRAFT DIVERTED TO ABQ FOR YELLOW HYDRAULIC LOW QUANTITY WARNING INDICATION. MAINTENANCE VERIFIED HYDRAULIC QUANTITY AS OK AND PLACED THE INDICATION SYSTEM ON THE MINIMUM EQUIPMENT LIST. MAINTENANCE REMOVED AND REPLACED YELLOW HYDRAULIC LOW LEVEL SWITCH IAW AMM 29-13-41-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040922001922004092200192NM 2004 9 22 QXEA200400617 120040811A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT TRACK NR 18 HAS CORROSION AT APPROXIMATELY STATION X259.00. REMOVED CORROSION IAW RD 8/4-53-884. REMOVED .002 MATERIAL. HFEC INSPECTION AS PER 1-84-7A, PART 6, 51-00-02. NO CRACKS NOTED. ALODINED AREA IW Q400 RD 8/4-53-884, STEP 6. 2H72 4T RTA13NM 20040922001932004092200193NM 2004 9 22 QXEA200400594 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT RAIL NR 12 HAS LITE CORROSION AT STATION 144 TO 160.00, APPROXIMATELY 16 INCHES WHERE SET TRACK COVER RIDES. LITELY BLENDED INSIDE OF SEAT TRACK AS INDICATED. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .003, WITHIN LIMITS PER RD 8/4-53-884. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884. 2H72 4T RTA13NM 20040922001942004092200194NM 2004 9 22 QXEA200400595 120040812A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - SEAT RAIL NR 12 HAS LITE CORROSION AT 111.00 TO 127.00, APPROXIMATELY 13 INCHES WHERE SEAT TRACK COVER RIDES. LITELY BLENDED INSIDE OF SEAT TRACK. MAXIMUM DEPTH OF MATERIAL REMOVED DOES NOT EXCEED .005 INCH, WITHIN LIMITS PER RD 8/4-53-884. PERFORMED HFEC IAW -8 400 NDTM PART 6-51-00-02. NO CRACKS NOTED. ALODINED AREA IAW Q400 RD 8/4-53-884. 2H72 4T RTA13NM 20040922001952004092200195EA 2004 9 22 04221634 120040808A3260 SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27634BR 7287 GEAR UP DISAGREE MDG POSTED (NOSE) ON GEAR RETRACTION. CREW DECLARED EMERGENCY, LANDED UNEVENTFULLY. REMOVED AND REPLACED NOSE GEAR PRIORITY VALVE, LEAK AND OPS CHECK GOOD REF MM 32-33-15. CHECKED AND ADJUSTED NOSE GEAR PROX SENSORS REF 32-61-05. ONLY SENSOR NEEDING SOME ADJUSTMENT WAS LT NOSE WEIGHT OFF WHEELS SWITCH. DESERVICED AND SERVICED NLG STRUT WITH NITRO & FLUID REF CRJMM 12-12-32. INSPECTED NLG FWD DOORS FOR PROPER FIT, NO ADJ REQURED REF CRJMM 32-22-01. INSPECTED NR 3 HYD SYSTEM WITH NO LEAKS OR DEFECTS NOTED REF 29-12-00. 2L72 4F RTA21EA 20040922001972004092200197WP 2004 9 22 AALA20040822 120040809A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY EXIT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21491AA 49684 DFW - AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN ABOVE SEAT 20D FOR AFT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040922001982004092200198NM 2004 9 22 AALA20040821 120040809A3350 LIGHT BOEING737 737823 13844BZNM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21967AN 29545 DFW - EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY AFT OF LEFT AND RIGHT AFT CABIN DOOR IS DAMAGED. REPLACED EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY FOR AFT LEFT AND RIGHT AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040922001992004092200199NM 2004 9 22 AALA20040811 120040808A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21361AA 24042 SFO - EMERGENCY LIGHTS AT L391, L644 AND L392 INOPERATIVE. REPLACED BATTERY PACK M733 FOR EMERGENCY LIGHTS AT L391, L644 AND L392. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040922002002004092200200NM 2004 9 22 AALA20040813 120040808A3397 WIRE BOEING767 767323 1385205NM EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21359AA 24040 SFO - EMERGENCY LIGHT AT SEAT 25H INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040922002012004092200201NM 2004 9 22 0401445517 120040802A5311 FRAME BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01517US 23205 DURING H-CHECK FOUND CORROSION ON FUSELAGE FRAME AT BS 1520 RBL 22. REPAIRED PER EA 55-200104. 2L72 4F RTA2NM 20040922002022004092200202SO 2004 9 22 CHQA000543 120040824A3350 POWER SUPPLY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11376SK 145578 OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY POWER SUPPLIES AND OVERWING EMERGENCY LIGHT. OPS CHECK GOOD PER MAINTENANCE MANUAL. 2L72 4F RTT00011AT 20040922002032004092200203SO 2004 9 22 CHQA000544 120040827A3040 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A CHQAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 GL11292SK 145488 ON DESCENT ON FLIGHT 7846 FROM PRV TO IAD AND ON DESCENT DURING FLIGHT 7837 FROM IAD TO CMH THERE WAS A BURNING ODOR IN THE COCKPIT. THE ODOR GOES AWAY WHEN ON THE GROUND. THE ODOR MAY POSSIBLY BE FROM THE WINDSHIELD HEAT ACTIVATION DURING DESCENT. IT IS A VERY OVERPOWERING SMELL THAT EVEN THE FLIGHT ATTENDANT COULD SMELL IT. FOUND THE RIGHT WINDSHIELD HEATING SENSOR BOLT LOOSE. RETORQUED BOLT DOWN IAW EMB 145 AMM 30-42-04-420-001-A00. OPS CHECKS GOOD. 2L72 4T RTT00011AT 20040923000052004092300005EU 2004 9 23 AWXA200401042 120040918A3244 TIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG FAILED A AWXAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 WP28640AW 448 EMERGENCY LANDING, ON TAKEOFF, EN ROUTE, THE NR 2 TIRE BLEW OUT CAUSING DAMAGE IN WHEEL WELL, LT WING, AND LT FLAPS, AIRCRAFT OUT OF SERVICE. EXAMINATION OF CASING FOUND TREAD MISSING 360º AROUND TIRE FROM SERIAL SIDE UPPER SIDEWALL TO OPPOSITE SERIAL SIDE SHOULDER. IN CROWN OF TIRE UNDER TREAD FABRIC WAS EXPOSED AND ABRADED WITH VERY LITTLE RUBBER & TEAR LINE EVIDENCE. THE OPPOSITE SERIAL SIDE SHOULDER IS TIGHT MOST OF THE WAY AROUND TIRE WITH A LOOSE SECTION AT 120º TO 215º. AT 200º THERE IS DAMAGE TO EDGE OF SHOULDER RIB WITH TEAR LINES IN UNDER TREAD RUBBER, THESE TEAR LINES INDICATE POSSIBLE INITIATION SITE. THERE WERE NO POLISHED AREAS ON EXPOSED SURFACES THAT INDICATE THIS WAS A WORKING SEPARATION. 2L72 4F4 FRTA28NM E40NE 20040923000062004092300006NM 2004 9 23 AWXA200401043 120040909A53206545834551 INTERCOSTAL BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK A 1 INCH CRACK WAS FOUND IN UPPER FORWARD LEG OF INTERCOSTAL (CHANNEL) AT BS 329, LBL 46, WL 208. MAINTENANCE REMOVED DAMAGED CHANNEL AT LBL 46 FROM BS 328 TO BS 344; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-45834; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 2 AND 8. 2L72 4F4 FRTA16WE E21EU 20040923000082004092300008NM 2004 9 23 AWXA200401045 120040909A53106517688165 CREASE BEAM BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK CORROSION WAS FOUND ON L-1 DOORWAY CREASE BEAM INNER CHORD BETWEEN BS 319 AND BS 357, LBL 58, WL 208. MAINTENANCE REMOVED CORRODED CREASE BEAM INNER CHORD FROM BS 319 TO BS 357, LBL 58; FABRICATED A NEW REPLACEMENT CREASE BEAM INNER CHORD IAW DWG 65-17688; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 8, & 12. 2L72 4F4 FRTA16WE E21EU 20040923000092004092300009NM 2004 9 23 AWXA200401046 120040909A575465C26602223 SKIN BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU NR 2 SLAT DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK AN AREA OF DISBONDED SKIN WAS FOUND ON OB END OF NR 2 SLAT WEDGE BETWEEN WBL 246.0 AND WBL 254.0 LT. MAINTENANCE REMOVED PREVIOUS REPAIR, DAMAGED SKIN AND HONEYCOMB ON NR 2 SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SRM 51-70-10, FIG. 32. 2L72 4F4 FRTA16WE E21EU 20040923000102004092300010NM 2004 9 23 AWXA200401047 120040907A57536646435278 WEDGE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK FOUND THE RT WING OB AFT FLAP DELAMINATED ON THE TRAILING EDGE IB CORNER. MAINTENANCE CUTOUT DAMAGE ON RT WING OB AFT FLAP AT TRAILING EDGE IB CORNER; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SRM 51-70-10, FIG. 31. 2L72 4F4 FRTA16WE E21EU 20040923000112004092300011NE 2004 9 23 COMA0460525 220040915A72616087T04P05 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENGINE MALFUNCTIONED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01716CA253099537 7250 FLIGHT 5260 LT ENGINE OIL PRESSURE WARNING. REPLACED THE LT ENGINE LUBE PUMP. 2L72 4F4 FRTA21EA E15NE 20040923000122004092300012EA 2004 9 23 COMA0460534 120040911A323016600101 UPLOCK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA249721798 7043 FLIGHT 5884 GEAR DISAGREE WARNING. REPLACED THE NLG UPLOCK ASSY. 2L72 4F4 FRTA21EA E15NE 20040923000132004092300013NM 2004 9 23 P5CA0401208 120040914A5753 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE LT WING TE FLAP CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LT WING MID FLAP ENTIRE CENTER SECTION PANEL HAS SEVERAL CORROSION SPOTS. REMOVED SURFACE CORROSION , PRIMED AND TREATED. 2L74 4F4 F A20WE E20EA 20040923000152004092300015NM 2004 9 23 P5CA0401209 120040914A5321 FLOOR PANEL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CARGO BAY CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FWD CARGO FLOOR PANEL HAS CORROSION. REMOVED SURFACE CORROSION, TREATED AND PRIMED. 2L74 4F4 F A20WE E20EA 20040923000172004092300017EA 2004 9 23 COMA0460521 120040916A5320 WEB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01965CA 7131 CARGO CAP WEB AT LIGHTING HOLE IB SIDE CRACKED FROM EXCESSIVE STRESS.IAW SRM 51-42-06, 51-42-13. 2L72 4F4 FRTA21EA E15NE 20040923000182004092300018EA 2004 9 23 COMA0460523 120040916A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01427CA 7460 LT FLOOR SUPPORT ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. 2L72 4F4 FRTA21EA E15NE 20040923000192004092300019NM 2004 9 23 AALA20040960 120040913A3350 BATTERY PACK BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 ALL EMERGENCY LIGHTS ON COACH SEATS 20 THROUGH 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON COACH SEATS 20 THROUGH 24. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 FRTT00001SEE00050EN 20040923000202004092300020NM 2004 9 23 AALA20040961 120040916A3350 LIGHT BOEING777 777223 1385213NM RROYCERB211 RB211TRENT89 NE CABIN DISLODGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21773AN 29583 LT EMERGENCY LIGHT HANGING DOWN IN FIRST CLASS GALLEY CLOSET. REPLACED DAMAGED EMERGENCY LIGHT ASSEMBLY IN FIRST CLASS GALLEY CLOSET EDGE. GROUND SYSTEM CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 FRTT00001SEE00050EN 20040923000222004092300022NM 2004 9 23 AALA20040963 120040916A3350 BATTERY PACK BOEING767 767223 1385123NM GE CF680 CF680A2 NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21335AA 22333 EMERGENCY EXIT SIGN LIGHT AT RT FORWARD GALLEY AT FLOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT RT HAD FORWARD GALLEY AT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 FRTA1NM E13NE 20040920001022004092000102NM 2004 9 20 USA2004F00053 120040526A282121SN04223 PRESSURE SWITCH BOEING767 7672B7 1385107NM GE CF6 CF680C2B7 NE FUEL FILTER FAULTY A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19651US 24764 695567 APPROXIMATELY TEN MINUTES AFTER TAKE-OFF, CREW RECEIVED THE (E/M`R ENG FUEL FILT). FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL FILTER AND THE FUEL FILTER PRESSURE SWITCH. 2L72 4F4 FRTA1NM E13NE 20040920001052004092000105WP 2004 9 20 MCC2004F00000 220040727A720033111U611G ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP MCAULY4HFR344HFR34C652 NE LEFT MAKING METAL E MCCAO OTHER O OTHER NRNOT REPORTED 1 SW112699Y246274483 AC666 P44496C 931687 APPROXIMATELY 15 MINUTES OUT, THE CHIP LIGHT ILLUMINATED AND OIL PSI STARTED TO DROP. ENGINE SECURED AND PROP FEATHERED. AIRCRAFT LANDED. PULLED CHIP DETECTER AND OIL FILTER AND FOUND METAL IN BOTH. APPEARS A BEARING IN THE GEAR BOX FAILED. ENGINE TO BE REMOVED. (GL11200412580) 2L72 4T4 TRTA8SW E4WE 6 C3PNE 20040920001382004092000138NM 2004 9 20 04FDEA02708 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 24 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER FEDEX EO 1-5510-7-5000-C3-PT1 FIG 03. CORROSION REPAIRED AS PER EA 1-5510-81561. 2L73 4F RTA22WE 20040920001402004092000140NM 2004 9 20 04FDEA02710 120040917A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 FUSELAGE FRAME AT STA 1601, LT L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN-FUSELAGE FRAME STA 1601, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOL I AND INSTALLED AS PER SRM 51-33- 01 VOL II. REFER TO EA 1-5310-79743. 2L73 4F RTA22WE 20040920001422004092000142WP 2004 9 20 04FDEA02712 120040917A5315 FLOORBEAM DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 AFT PIT STA 1902, 20 LBL TO 20 RBL FLOOR SUPPORT FRAME CORRODED TOP SIDE OF T-CAP. REMOVED FRAME T-CAP IAW DC10 SRM 51-35-01 VOL 3, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I. REMOVED DAMAGE IAW DC10 SRM 53-00-01 VOL I. FAB FILLER DOUBLER IAW DC10 SRM 51-00-01 VOL I AND DWG ABA3850, MAT ID FOR FILLER DOUBLER 7075-T6 .063 PO 456445.7 IAW DWG ABA3850, FRAME, FILLER AND DOUBLER ALODINED, PRIMED IAW DC10 SRM 51-21-01 VOL I. DOUBLERS HEAT TREATED IAW FORM QA-0084A, LOCATED, DRILLED DOUBLER IAW DWG AGA3850. INSTALLED DOULBER, FILLER AND FRAME IAW DC 10 SRM 51-35-01 AND 51-33-01 VOL 2. 2L73 4F RTA22WE 20040920001452004092000145WP 2004 9 20 04FDEA02715 120040917A5347 SEAT TRACK DOUG DC10 DC1030F 3023504WP ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 R/S AFT PIT STA 1841 TO 1902 OUTBOARD FLANG OF SEAT TRACK CORRODED. REMOVED CORROSION ON SEAT TRACK IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 21. FOUND TO BE OUT LIMITS, IAW FEDEX DC10 SRM 53-70-00 PG 21 VOL I, MAKE NEW SEAT TRACK IAW DAC DWG AGA3855, TREATMENT ALODINE PRIMER IAW FED EX DC10 SRM 51-21-01 VOL 2 PGS 24, 21 AND INSTALLED NEW SEAT TRACK IAW FEDX DC10-30 SRM 51-33-01 VOL 2 PG 1. 2L73 4F RTA22WE 20040920001472004092000147NM 2004 9 20 SWAA042703 120040916A5312BAC1514 STIFFENER BOEING737 7373G7 1384595NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT BS 1016, 3 O'CLOCK POSITION, CRACKED. REPAIRED STIFFENER PER SRM. 2L72 4F RTA16WE 20040920001482004092000148NM 2004 9 20 SWAA042705 120040916A5720115A4901 ANGLE BOEING737 7377H4 1384404NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED 5Y CHECK, FOUND LT WING SUPPORT ANGLE AT REAR SPAR PANEL BETWEEN SPOILER NR 5 AND SPOILER NR 6, CRACKED. REMOVED AND REPLACED ANGLE PER SRM. 2L72 4F RTA16WE 20040920001502004092000150NM 2004 9 20 SWAA042696 120040916A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29765SW 29805 LEFT FWD EEPLS HAS WIRES EXPOSED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20040920001522004092000152 2004 9 20 SWAA042698 420040916A256565C16820 HOOK BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW296231W 27933 L1 DOOR EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20040920001542004092000154NM 2004 9 20 SWAA042700 120040916A5552REP4M6 BEARING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR INPUT ROD AFT BEARING PER MM. 2L72 4F RTA16WE 20040920001562004092000156NM 2004 9 20 SWAA042702 120040916A3350311500 LENS BOEING737 7373Y0 1384671NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 4 DEF, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20040920001582004092000158NM 2004 9 20 UPS04543078 120040903A3350434093001 CONTROL PANEL BOEING757 75724APF 1384969NM EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01457UP 25478 INSPECTION TYPE:N/A P5 OVERHEAD PILOTS EMERGENCY LIGHTS CONTROL PANEL UNARMED INDICATION INOP. REMOVED & REPLACED DIODE MODULE PER SSM 33-51-01 PG 102. OPS CHECKS GOOD. 2L72 4F RTA2NM 20040920001602004092000160NM 2004 9 20 CALA0400629 120040909A53156546811 FLOORBEAM BOEING737 7373T0 1384582NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 967, LBL 35 TO RBL 35. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51, FIGURE 202, PAGE 207. 2L72 4F RTA16WE 20040920001622004092000162NM 2004 9 20 CALA0400631 120040910A5320654681282 PAN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND LT SIDE FLOOR PAN FOR VANITY FILL/DRAIN LINE CONNECTIONS CORRODED I/B OF Z-ANGLE BETWEEN STA 986.5 AND 1016. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040920001642004092000164NM 2004 9 20 CALA0400633 120040911A5315BAC1518399 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717321 23372 INSPECTION FOUND FLOORBEAM UPPER FLANGE CORRODED AT STA 986.5, LBL 45 TO RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-00-51, FIGURE 202 AND ECRA 5310-03851. 2L72 4F RTA16WE 20040920001662004092000166NM 2004 9 20 CALA0400620 120040826A2497 WIRE HARNESS BOEING767 767424ER 1385270NM WATER HEATER BURNED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2766057 29452 SMOKE WITH ELECTRICAL ODOR APPEARED IN CABIN SHORTLY AFTER TAKEOFF. ELECTRICAL SPARKING IN CEILING AREA FORWARD OF L-3 DOOR. LIGHTS & NSFSB SIGNS FLICKERED & PA SPEAKERS CRACKLED. HALON FIRE EXTINGUISHER WAS USED ON OVERHEAD AREA OF FORWARD CENTER LAV J. LANDED WITHOUT FURTHER PROBLEMS. PANEL ABOVE LAV-J OPENED FOR INSPECTION. MX FOUND A BURNT WIRING HARNESS AT A SUPPORTING CLAMP WITH EVIDENCE OF HEAT DAMAGE ON SURROUNDING STRUCTURE. THE W1276 HARNESS INCORPORATED WIRING FOR LAV HOT WATER HEATER, SPEAKERS & LIGHTS. WIRE BUNDLE WAS CHAFING ON EDGE OF HONEYCOMB WALL PANEL. WIRING HARNESS WAS REPAIRED & CLAMP SECURED. AN FCD WAS ISSUED TO INSPECT THE REMAINDER OF THE FLEET. 2L72 4F RTA1NM 20040920001682004092000168WP 2004 9 20 AALA20040931 120040831A3350 CHARGER DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21595AA 53285 EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGNECY LIGHTS IN CEILING BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040920001702004092000170NM 2004 9 20 AALA20040929 120040827A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21958AN 30091 BATTERY PACK M1674 AT STATION 322 FOR EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK M1674 AT STATION 322 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040920001722004092000172NM 2004 9 20 AALA20040895 120040820A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21924AN 29525 TUL - BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS FAILED TIME TEST. REPLACED BATTERY PACK AT STATION 727 FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040920001742004092000174WP 2004 9 20 AALA20040888 120040824A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21565AA 49347 SEA - AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B527 FOR AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040920001762004092000176NM 2004 9 20 CALA0400626 120040901A575465C26793 SKIN BOEING737 7373T0 1384582NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717356 23942 INSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT LOWER EXTERNAL SKIN AT WS 270. A REPAIR WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20040920001772004092000177WP 2004 9 20 AALA20040953 120040909A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217538A 49992 DFW - CEILING EMERGENCY EXIT LIGHTS BETWEEN ROWS 13 AND 16 AND ROWS 23 AND 26 INOPERATIVE. ADDITIONALLY, FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACKS FOR ROWS 13 AND 16 AND ROWS 23 AND 26. ALSO REPLACED FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040920001792004092000179WP 2004 9 20 AALA20040955 120040910A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21232AA 49179 DEN - EMERGENCY LIGHTS FROM 3DE TO 20DEF INOPERATIVE. REPLACED FORWARD BATTERY FOR EMERGENCY LIGHTS FROM 3DE TO 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040920001812004092000181WP 2004 9 20 AALA20040957 120040910A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21296AA 49308 DFW - EMERGENCY LIGHTING ABOVE SEATS 13, 14, AND 16 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTING ABOVE SEATS 13, 14, AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040920001832004092000183 2004 9 20 SWAA042679 420040915A2565D31354 SLIDE BOEING737 7373K2 13844BANM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040920001852004092000185NM 2004 9 20 SWAA042682 120040915A53156546812 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CHORD AT BS 947, LBL 54, CORRODED. REMOVED AND REPLACED CHORD SECTION PER ER. 2L72 4F RTA16WE 20040920001872004092000187NM 2004 9 20 SWAA042684 120040915A53306545776 SKIN BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SKIN AT BS 949, LBL 3, CORRODED. REPAIRED FUSELAGE SKIN PER BAC DRAWING AND SRM. 2L72 4F RTA16WE 20040921000042004092100004WP 2004 9 21 04FDEA02716 120040917A5347 SEAT TRACK DOUG DC10 DC1030F 3023504WP ZONE 200 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 MAIN CABIN, CARGO SEAT TRACK HAS 2 CRACKS AT LBL 24 & STA 1009 TO 1059 (MRK). REMOVED 2 FLOORBOARDS. REMOVED AND REPLACED SEAT TRACK IAW 51-31-01 VOL 2 OF FEDEX DC10-30 SRM MAT ID FOR SEAT TRACK 7929147-1350 IAW FEDEX DC10-30 SRM 53-42-01 FIG 4 SH1 VOL 3 MAT ID FOR SPLICES IAW DC10-30 FEDEX SRM 53-70-00 VOL 2 IS 4932154 P/O 458386.12 .050 7075T6 PO 446672.5. FABED SPLICES IAW DC 10-30 SRM FEDEX 53-70-00 FIG 1 VOL 1 SH 1 FABED SEAT TRACK IAW DC10 SRM FEDEX 51-31-01 VOL 2 & DAC DWG ACA7105 AND PRIMED IAW FEDEX DC10-30 SRM 51-21-01 VOL 2 PG 19-44. REMOVED AND REPLACED SEAT TRACK AND SPLICES IAW DC 10-30 FEDEX SRM 51-31-01 VOL 2 AND 70-00 VOL I, IR/R FLOORBOARDS IAW FED DC10-30 SRM. 2L73 4F RTA22WE 20040921000052004092100005WP 2004 9 21 04FDEA02717 120040917A5410AUB702533 FITTING DOUG DC10 DC1030F 3023504WP ZONE 600 MIGRATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 NR 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATES. REMOVED SPHERICAL BEARING IAW DC10-30MM FEDEX 54-40-02 HONED HOLE IAW DC 10-30 FEDX AMM 54-40-02-2, REMOVED DRAIN LINE IAW FEDEX DC10-30 MM 54-10-00, REMOVED NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01, INST NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01 VOL 2, REMOVED AFT BULKHEAD FITTING IAW FEDEX DC10-30 SRM 51-31-01 VOL 2 P/N AUB7025-33. LOCATED, DRILLED FITTING IAW DAC DWG AUB7075, INSTALLED NEW FITTING P/N AUB7025-33 IAW DAC DWG AUB 7025 FEDEX DC10-30 SRM 51-38-01 VOL 2, REAMED 2 EA HOLES IAW FEDEX DC10-30 SRM 51-31-01 VOL 2, INSTALLED FUEL DRAIN LINE IAW DC 10-30 MM 54-10-00. 2L73 4F RTA22WE 20040921000102004092100010WP 2004 9 21 04FDEA02722 120040917A5420 BUSHING DOUG DC10 DC1030F 3023504WP ZONE 400 WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25321FE 47836 NR 3 PYLON THRUST LINK PYLON LUGS HAS 2 WORN BUSHINGS. REMOVED AND REPLACED IAW FEDEX DC10 CMM 20-20-07. 2L73 4F RTA22WE 20040921000242004092100024SO 2004 9 21 SIMA200423912 120040823A323022250003 SOLENOID EMB 145 EMB145 3260210SO NLG MALFUNCTIONED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21613AE 145081 DFW - FLT 3819 - CAPTAIN REPORTED NOSE GEAR DOOR FAILED TO CLOSE AFTER GEAR RETRACTION. INSTALLED NEW NOSE LANDING GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) SIMA 2L72 4F RTT00011AT 20040921000282004092100028EA 2004 9 21 ASOA04583 120040809A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA TE MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11908EV 7654 DURING CLIMB-OUT FROM DFW-ELP, AT APPROXIMATELY 17,000 FEET THE CREW RECEIVED A FLAPS FAIL MESSAGE. QRH PROCEDURES WERE COMPLIED WITH. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION WITH THE AIRCRAFT LANDING SAFELY IN ELP. MAINTENANCE COMPLIED WITH ASA EO 600-27-0004A AND RESET THE FLAP SYSTEM CIRCUIT BREAKERS. NO EVIDENCE OF FLAP TWISTING OR DEFORMATION WAS FOUND. MAINTENANCE ALSO INSPECTED THE FLAPS ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000392004092100039EA 2004 9 21 ASOA04591 120040813A5210601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING AN A-CHECK IN BRT, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040921000512004092100051EA 2004 9 21 ASOA04590 120040813A5210601R3189311 PUSHROD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO11846AS 7328 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED THE PUSH ROD FROM THE PIVOT ASSEMBLY TO THE LATCH CAM TORQUE TUBE AND INSPECTED THE RIGGING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921000552004092100055EA 2004 9 21 A6WA200440117 120040529A7714 INDICATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 ENGINE MALFUNCTIONED A A6WAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL31403AW 7288 DURING CRUISE, NR 2 ENGINE N2 OVERSPEED BEYOND 100 PERCENT INDICATION ERRATIC AND UNCONTOLLABLE EVEN WHEN SELECTED TO FIGHT IDLE. COMPLIED WITH QRH ENGINE SHUTDOWN. TAT 41 DEGREES CELCIUS. ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED ALTERNATOR AND STATOR, N2 INDICATING, IAW AMM 73-21-07, OPS CHECK DURING GROUND RUN NORMAL. (M) 2L72 4F RTA21EA 20040921000562004092100056EA 2004 9 21 ASOA04595 120040814A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11878AS 7590 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT CARGO COMPARTMENT FLOOR SUPPORT ANGLES AT FS 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040921000682004092100068 2004 9 21 GTIA040740 420040817A2565 LANYARD DOUG DC9 DC983 3022083WP R1 SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23833NK 49449 R-1 SLIDE COVER LANYARD NOT CONNECTED. RECONNECTED SLIDE COVER LANYARD. (M)GTIA 2L72 4F RTA6WE 20040921000702004092100070WP 2004 9 21 GTIA040746 120040823A2421 GENERATOR DOUG DC9 DC983 3022083WP LEFT AC FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23825NK 53012 DTW - FOUND LOST LEFT AC GENERATOR QRH PROCEDURES FOLLOWED DESCENDED TO LOWER ALTITUDE STARTED APU POWER NORMAL CONTINUED FLT TO DTW. REMOVED AND REPLACED LEFT GENERATOR. (M) GTIA 2L72 4F RTA6WE 20040921000722004092100072WP 2004 9 21 GTIA040756 120040809A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LBL 36 INCHES FLOOR PANEL CRACKED SEVERAL INSERTS CORRODED. FABRICATED FLOOR BOARD. (M) GTIA 2L72 4F RTA6WE 20040921000752004092100075SO 2004 9 21 SIMA200423706 120040818A53201452172500 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21618AE 145097 DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED CORRODED AREA AND PERFORMED NDT INSPECTION. FILLED BLENDED AREA WITH EPOXY RESIN EA 934NA AND SANDED SMOOTH. FABRICATED THREE DOUBLERS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 26, 53-21-02. (M) 2L72 4T RTT00011AT 20040921000772004092100077WP 2004 9 21 GTIA040754 120040809A5321 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND FORWARD CABIN STATION 200 TO STATION 160 LBL 6 INCH RBL 6 INCH FLOOR PANEL HAS SEVERAL INSERTS CORRODED AND SOFT MUSHEY. FABRICATED FLOORBOARD. GTIA (M) 2L72 4F RTA6WE 20040921000782004092100078WP 2004 9 21 GTIA040762 120040829A2120 UNKNOWN DOUG DC9 DC982 3022082WP CABIN FUMES A GTIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23823NK 48020 FLL - FLT 380 - AFTER TAKEOFF FUMES FILLED A/C AND CAUSED AIR RETURN. PERFORMED A/C AIR CONDITION SYSTEM CHECK WITH ENGINES AT HIGH POWER SETTINGS. OPS CHECK NORMAL. (M) GTIA 2L72 4F A6WE 20040921000932004092100093SO 2004 9 21 SIMA200423705 120040814A53302024T3 SKIN EMB 135 EMB135KL 3260302SO NOSE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21831AE4924 145616 WHILE AIRCRAFT WAS UNDERGOING AN MBV INSPECTION A REPAIR FOR PREVIOUS BIRDSTRIKE DAMAGE WAS ACCOMPLISHED ON FORWARD UPPRE NOSE SKIN JUST AFT OF RADOME. REMOVED SECTION OF DAMAGED SKIN. FABRICATED A DOUBLER, FILLER AND L ANGLE. REPAIR DONE IAW EMB REAPIR STATEMENT IC2004-145/3719 DATED AUGUST 14 2004, IC2004-145/3731 DATED AUGUST 13, 2004 AND IC2004-145/3693 DATED AUGUST 11, 2004. (M) 2L72 4F RTT00011AT 20040921000942004092100094SO 2004 9 21 SIMA200423701 120040812A53302024T3 SKIN EMB 135 EMB135KL 3260302SO STATIC PORT GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21831AE4924 145616 DURING AN MBV INSPECTION, 10 GOUGES WERE FOUND BELOW RIGHT STATIC PORT AT STRINGER 19. BLENDED GOUGES TO REMOVE DAMAGE. FABRICATED A DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-1453686 DATED AUGUST 10, 2004 AND IC2004-145/3710 DATED AUGUST 11, 2004. (M) 2L72 4F RTT00011AT 20040921000992004092100099EA 2004 9 21 ASOA04494 120040709A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INTERMITTENT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11825AS 7207 FLT 4637 - DURING A GROND INSPECTION IN BTR, THE EMREGENCY FLOOR TRACK LIGHTING WOULD NOT ILLUMINATED WHEN THE EMERGENCY LIGHTS SWITCH WAS IN THE ON POSITION FOR APPROXIMATELY TEN SECONDS. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHTS BATTERY INVERTER. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040921001012004092100101NM 2004 9 21 UIEA200400137 120040802A541565B941383 FITTING BOEING747 7472D7B 1384803NM NR 1 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15523MC 21782 FOUND DURING D-CHECK AT SIN, DAMAGE WAS FOUND AT FASTENER HOLE IN THE FITTING AFT VERTICAL FLANGE. THE DAMAGE WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO .4521-4541 INCHES DIAMETER. AN OVERSIZE FASTENER AS THE SAME DESIGN TYPE REQUIRED, WAS INSTALLED AT THE AFFECTED LOCATION. ALL OTHER FITTING REWORK AND REFINISH ACCOMPLISHED IAW TERMINATING ACTION. (M) 2L74 4F RTA20WE 20040921001052004092100105EA 2004 9 21 ASOA04500 120040711A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27871AS 7537 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 484, LBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT LCIPS AT FS 484, LBL 27 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20040921001142004092100114NE 2004 9 21 2004FA0000695 220040816A7321324476812 FUEL CONTROL BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE LT ENGINE SEIZED B E8IAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL03698P 1110 BB1621 PCEPJ0213 PILOT NOTED UNCOMMANDED LEFT ENGINE TORQUE AND ITT INCREASE IN FILGHT ON INITIAL APPROACH TO MKE. NO RESPONSE TO POWER LEVER INPUT. PILOT SHUTDOWN ENGIEN AND DIVERTED TO RFD. DURING REMOVAL OF FCU FOR TROUBLESHOOTING NOTED FCU INPUT SHAFT COUPLING SHEARED, FORWARD FCU SHAFT BEARING FAILED, INPUT SHAFT SEIZED. FUEL NOTED IN HP FUEL PUMP/FCU COUPLING AREA. E8IA (M) 1L72 4T4 T A24CE E4EA 20040921001302004092100130NM 2004 9 21 SWAA042710 120040918A575465C26685 SKIN BOEING737 7373H4 1384600NM NR 6 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA. 2L72 4F RTA16WE 20040921001312004092100131NM 2004 9 21 SWAA042711 120040918A52109078224 BRACKET BOEING737 7373Y0 1384671NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR CUTOUT UPPER HINGE BRACKET CRACKED. REPAIRED UPPER BRACKET PER EA. 2L72 4F RTA16WE 20040921001382004092100138NM 2004 9 21 DHL2004745561 120040730A7110 SKIN BOEING727 727224 1384076NM NOSE COWL DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE NR 3 ENGINE NOSE COWL HAS 3 EA DENTS (1) NAC STA 88.4 O/B SIDE (2) NAC STA 68.5 O/B SIDE (3) NAC STA 63.5 TO STA 88.4 LWR SIDE. CUT OUT DAMAGED AREAS DIM 2.5625 X 1.4375, .4375 X 1.25, 4.5625 X .5625 AND FABBED DOUBLERS FROM 2024 T3 .040 PO 900825 DIM 6.1250 X 5, 5.5 X 4.375, & 7.25 X 4.125 IAW 727 SRM 54-30-3 FIG 8. DOUBLERS TREATED, PRIMED, & INSTALLED IAW 727 SRM 54-30-3 FIG 8. 2L73 4F A3WE 20040921001402004092100140NM 2004 9 21 DHL2004745562 120040820A5532 SKIN BOEING727 727224 1384076NM VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, RT VERT STAB- RUDDER EXTERIOR SKIN (LWR RUDDER) AT ABOUT FIN STA 162.5 SKIN SURFACE HAS SEVERAL DENTED CREASES. FABRICATED DOUBLER 7 X 2 INCHES. TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON R/W VERT EXTERIOR SKIN LWR RUDDER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040921001412004092100141NM 2004 9 21 DHL2004745564 120040817A5310 DOOR FRAME BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, C1 DOOR CENTER LOWER FRAME IS CRACKED. REMOVED CRACKED FRAME IN C-1 DOOR LWR IAW B727 SRM 51-30-2. FABRICATED FRAME ANGLE 7075 T6 .050 PO 900484, 6 X 9 INCHES IAW B727 SRM 52-30-1. TREATED AND PRIMED IAW SRM 51-10-2. REMOVED CORRODED T-ANGLE IAW SRM 51-302. REMOVED CORROSION FROM T-ANGLE FOUND TO BE WITHIN LIMITS MAT LOSS .003 IAW B727 SRM 51-10-6 & 52-30-1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED FRAME AND T-ANGLE IAW B727 SRM 51-30-2. 2L73 4F A3WE 20040922000022004092200002WP 2004 9 22 GTIA040688 120040722A5320 ANGLE DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23809NK 49503 FOUND AFT ACCY COMPARTMENT L-ANGLE CRACKED IN HALF AT FS 1463, 17 LBL, AFT SIDE OF FRAME. REMOVED DAMAGED ANGLE. FABRICATE NEW ANGLE. INSTALLED NEW ANGLE. (M) 2L72 4F RTA6WE 20040922000052004092200005WP 2004 9 22 GTIA040712 120040802A5320 STRAP DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23824NK 53015 FTW - FOUND AFT PIT STATION 1211 STRINGER 27L-25L FRAME STRAP CORRODED. REMOVED FRAME STRAP. FABRICATED NEW FRAME STRAP. INSTALLED FRAME STRAP. (M) 2L72 4F RTA6WE 20040922000142004092200014WP 2004 9 22 GTIA040707 120040809A2500 SLIDE DOUG DC9 DC983 3022083WP L2 DOOR DISCHARGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 RSW - FOUND L2 DOOR SLIDE PACK PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PACK. (M) 2L72 4F RTA6WE 20040922000342004092200034EA 2004 9 22 ASOA04490 120040707A3350OL3071BPEGPL LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11903EV 7621 DURING AN OVERNIGHT INSPECTION IN VPS, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040922000352004092200035SO 2004 9 22 SIMA200423907 120040820A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21726AE8518 145314 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED BEYOND SRM LIMITS. PERFORMED CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/3835 DATED AUGUST 18, 2004. (M) 2L72 4F RTT00011AT 20040922000372004092200037EA 2004 9 22 ASOA04496 120040710A5210H341421 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11835AS 7258 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO CLOSE. THE DOOR LATCH AND HANDLE WERE VERY STIFF. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE AND THE LOWER BEARING ASSEMBLY P/N MS21151-8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040922000422004092200042EU 2004 9 22 ASOA04493 120040709A6120C1466003 SERVO VALVE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT ENG PROP MALFUNCTIONED A ASOAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO11536AS4379 465 DUIRNG INITATION OF DESCENT FROM ATL-VPS, THE CREW EXPERIENCED A SURGE IN THE RIGHT ENGINE FROM 65 PERCENT TORQUE TO 35 PERCENT TORQUE AND BACK UP. NP WENT FROM 77-80 PERCENT PLUS. AT 100 PERCENT OVERRIDE THE NP WENT FROM 98-101.9 PERCENT. THE AIRCRAFT BEGAN TO YAW AND THE ENGINE FLUCTUATIONS WERE QUICK AND GETTING WORSE. THE CREW SHUTDOWN THE RIGHT ENGINE AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY IN VPS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE PROPELLER SERVO VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20040922000442004092200044EA 2004 9 22 ASOA04495 120040710A5210600319801007 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11851AS 7360 FLT 4748 - DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. THE PASSENGER DOOR ALSO CLOSED BY ITSELF UPON POWER UP. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR, AND ALSO REPOSITIONED THE SWITCH GUARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040922000452004092200045NM 2004 9 22 USAA040390 120040731A5753 ROLLER BOEING737 737301 1384611NM TE FLAP CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US49309 23237 PIT - FOUND SUPPORT FLAP ROLLER CHAFED .5 INCH BY 1 INCH AREA, FT AFT FLAP NR 1 OUTBOARD ROLLER ARM. REPLACED WITH AFT FLAP PER MM 27-51-39. (M) 2L72 4F RTA16WE 20040922000492004092200049NM 2004 9 22 USAA040383 120040722A532065458661108 STIFFENER BOEING737 7373B7 1384580NM FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US53829 22955 PIT - FOUND VERTICAL STIFFENER GOUGED .020 INCH, LT SIDE OF KEELBEAM AT STATION 634, INBOARD. FABRICATED AND REPLACED STIFFENER PER SRM 53-60-12 FIG 1. (M) 2L72 4F RTA16WE 20040922000552004092200055NM 2004 9 22 USAA040388 120040628A575465C266031 SKIN BOEING737 7373B7 1384580NM NR 3 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19389US52977 23311 PIT - FOUND SKIN AND CORE BOND WITH DELAMINATION 2 INCH AREA, LEFT WING NR 3 SLAT INBOARD AFT CORNER TOP SURFACE. REMOVED DAMGAED SKIN AND CORE, INSTALLED INTERNAL AND TOP DOUBLER AND NEW CORE MATERIAL PER BOEING SRM 51-70-10. (M) 2L72 4F RTA16WE 20040922000692004092200069EU 2004 9 22 IGAA097294 120040916A8011MHB6016 STARTER PARTENP68 P68C 6780105EU LYC O360 IO360A1A 41514EA RT ENGINE STUCK B IGAAO OTHER O OTHER NRNOT REPORTED 1 WP016602L564 32619OB STARTER WILL NOT DISENGAE FROM FLYWHEEL. SAME MALFUNCTION AS MFG SB 559, BUT SB 559 DOES NOT APPLY TO THIS PN. 1H72 3O3 O A31EU 1E10 20040922000782004092200078 2004 9 22 SWIA200413801 420040909A3418C818022 STICK SHAKER EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE STALL WARNING INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07308SW 120326 FOS STICK SHAKER INOPERATIVE. REMOVED AND REPLACED FOS STICK SHAKER IAW MM 27-34-04. OPERATIONAL CHECK SATISFACTORY. P/N: C-81802-2 S/N OFF: 641 2L72 4T4 TRTA31SO E20NE 20040922000822004092200082EA 2004 9 22 SWIA200413805 120040911A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07918SW6368 6368 7645 NR 2 STAB TRIM FAILED TO ENGAGE. REMOVED AND REPLACED HSTA, IAW CH. 27-42-01 AND REPLACED MCU IAW MM CH. 27-42-05. OPERATIONAL CHECK GOOD. P/N: 7062-3 S/N OFF: 117. 2L72 4F4 FRTA21EA E15NE 20040922000892004092200089NM 2004 9 22 04FDEA02686 120040915A2612774001 SMOKE DETECTOR BOEING727 727200 138407ENM PWA JT8 JT8D217C 52053NE CARGO BAY FAILED A FDEAA UNSCHED LANDING BN SMOKE/FUMES/ODORS/SPARKS FALSE WARNING CRCRUISE 1 SO25207FE72 72 22929 INFLIGHT AT FL330, THE MAIN CARGO SMOKE NR 1 (FORWARD) LT ILLUMINATED, FOLLOWED RED TABS AND PHASE ONES DIVERTED. WARNING LT WENT OUT ON FINAL APPROACH THREE CREW DETECTED A FAINT ABNORMAL ODOR AFTER LANDING AND CARGO DOOR OPEN. REMOVED AND REPLACED NR 1 SMOKE DETECTOR. PREMATURE REMOVAL, INSTALLATION OFF MFG 7740-01, ON MFG 7740-01. 2L73 4F4 FRTA3WE E9NE 20040922000932004092200093EU 2004 9 22 04FDEA02695 120040916A5347 SEAT TRACK AIRBUS310 A310203 3930313EU GE CF6 CF680A3 30025NE ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 SEAT TRACK AT FR 36 AFT APPROX 8 INCHES IS GOUGED. BLENDED AREA PER A310 SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS PER A310 SRM 53-10-16. REPAIRED BY REMOVING DAMAGED SECTION OF TRACK AND SPLICING IN A REPAIR SECTION PER A310 SRM 51-40-21 AND 53-10-16. 2L72 4F4 FRTA35EU E13NE 20040922001002004092200100NM 2004 9 22 AWXA200401032 120040909A53206545834551 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK A .8750 INCH CRACK WAS FOUND ON UPPER AFT LEG OF INTERCOSTAL AT BS 327, LBL 46, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT LBL 46 FROM BS 312 TO BS 328; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 8-12, PG. 38 AND 45. 2L72 4F RTA16WE 20040922001022004092200102EU 2004 9 22 04FDEA02692 120040916A5320A5397422220219 FLOOR SUPPORT AIRBUS310 A310 EU GE CF6 CF680A3 30025NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 BULK CARGO COMPT. FLOOR STRUCTURE FR66 LT SIDE , MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACE. REMOVED CORROSION IAW SRM 51-74-10, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED BEAM IAW SRM 51-40-21.**** S/D COMING **** 2L72 4F4 FRTA35EU E13NE 20040922001052004092200105EA 2004 9 22 COMA0470069 120040912A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01374CA3153 1059 10090 FLIGHT 5369 GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR SELECTOR VALVE. 2L72 4F4 FRTA21EA EOOO63EN 20040922001122004092200112NM 2004 9 22 SWAA042725 120040920A53116546529 BELTFRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29683SW 24008 DURING SCHEDULED 1/4D CHECK, FOUND BELTFRAME AT BS 500, STRINGER 24R, CORRODED. REPAIRED BELTFRAME PER SRM. 2L72 4F RTA16WE 20040922001222004092200122EA 2004 9 22 04237702 120040824A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT DIRTY A VTZAK NONE P NO WARNING INDICATION ININSP/MAINT 1 EA27702BR 7462 RIGHT EMERGENCY DOOR INDICATOR INOP. CLEANED AND LUBED RIGHT EMERGENCY DOOR PROX SENSOR AND PARAMETER SEAL. OPS CHECKED SEVERAL TIMES. NO FAULT NOTED AT THIS TIME. 2L72 4F RTA21EA 20040922001252004092200125NM 2004 9 22 DHL2004745516 120040705A5753 SKIN BOEING727 727224 1384076NM LT FORE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, LEFT I/B FORE FLAP LOWER SURF AT L/E WBL 124 HAS SKIN DELAMINATED. REMOVED LEFT I/B FORE FLAP IAW 727 MM 27-51-01, CUT OUT LWR SKIN 5.5 X 4.5 INCHES, FABBED FILLER 6.5 X 4.5 INCHES AND DOUBLER 9.5 X 6 INCHES FROM 2024-T3 .016 PO 900573 IAW 727 SRM 57-52-1 FIG 3 & 51-40-20 FIG 31, CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO MATING SURFACE, BONDED CURED, SANDED, CLEANED, ALODINED, PRIMED, SEALED REPAIR IAW 727 SRM 51-40-20- FIG 31. REINSTALLED LEFT I/B FORE FLAP IAW 727 MM 27-51-01. 2L73 4F A3WE 20040922001282004092200128NM 2004 9 22 SWAA042656 120040914A53306545765 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040922001332004092200133 2004 9 22 DL777040853 420040829A34426225136202 ANTENNA BOEING777 777232 1385232NM WX RADAR SYS FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27867DA 29743 EN ROUTE ATH CREW HEARD NOISE FROM WEATHER RADAR AREA AND LATER HAD WX SYSTEM MESSAGE. DIVERTED TO JFK. REPLACED RADAR ANTENNA AND DRIVE. 2L72 4F RTT00001SE 20040922001572004092200157EA 2004 9 22 04237670 120040824A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA LEFT FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27670BR CREW REPORT STATED APPLIED THRUST AND RECEIVED L PACK HI PRESS CAUTION MSG RIGHT AWAY. ABORTED TAKEOFF. TAXI'D OFF THE RUNWAY AND SENT ACARS TO DX. 2L72 4F RTA21EA 20040922001632004092200163WP 2004 9 22 AALA20040938 120040904A3350 FLASHLIGHT DOUG DC9 DC982 3022082WP L1 DOOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21579AA 53156 STL - L1 EMERGENCY EXIT DOOR FLASHLIGHT INOPERATIVE. REPLACED L1 EMERGENCY EXIT DOOR FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040922001642004092200164EU 2004 9 22 AALA20040939 120040905A2697 INSULATION AIRBUS300 A300B4605R 3930308EU WIRE BURNED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2170054 461 POP - MIN EQUIPMENT SMOKE MASTER WARNINGS STARTED AT TOP OF CRUISE 4-5X LASTING APPROX 30 SECS, WOULD CLEAR FOR APPROX 1-2 MINS, DIVERTED TO POP. INSPECTED EQUIPMENT BY AREA FOUND BURNED SPLICES ON LEFT RUNWAY TURN OFF LIGHT. PLACARD LEFT RUNWAY TURN OFF LIGHT PER MEL. CHECKED AND FOUND NO INDICATION OF BURNT WIRING. FOUND INSULATION AGAINST LIGHT ASSY BURNT. REPOSITIONED INSULATION. RUN WAY TURNOFF LIGHT CHECKS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20040922001762004092200176WP 2004 9 22 CALA0400628 120040904A53129911596505 BEAM DOUG DC9 DC982 3022082WP BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772821 49481 INSPECTION FOUND BULKHEAD BEAM WEB CORRODED AT STA 110, S30L. THE BEAM WEB WAS REPAIRED IAW ECRA 5310-04387. 2L72 4F A6WE 20040922001782004092200178NM 2004 9 22 DLM88040860 120040910A2910AS15508K0240 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM CHAFED A DALAO OTHER K FLUID LOSS CLCLIMB 1 SO27940DL 49813 LT HYD QTY BEGAN TO DECREASE IN CLIMBOUT FOLLOWED BY DECREASE IN PRESSURE. AFTER FOLLOWING QRH LT SIDE WENT BACK UP FROM 2 TO 17 QUARTS, PRESS REMAINED AT ZERO, PUMPS TURNED BACK OFF. FOUND HYD LINE CHAFED IN AIR CONDITION COMPARTMENT BEHIND P-DOME, LEFT SIDE. REPLACED SAME, LEAK CHECK OK. 2L72 4F RTA6WE 20040922001962004092200196WP 2004 9 22 AALA20040820 120040810A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21972TW 53622 DFW - CEILING EMERGENCY LIGHTS AT ROWS 26 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY B5107 FOR CEILING EMERGENCY LIGHTS AT ROWS 26 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040923000012004092300001EU 2004 9 23 XNOA1201 120040920A3242 VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE MLG BRAKES MALFUNCTIONED A XN0AD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL23474AS 219 ON PUSH BACK NR 5, 7 BRAKES LOCKED UP. REMOVED AND REPLACED ELECTRO VALVE IAW A300MM 32-42-11, BLED BRAKING SYS FROM FL COMPT. (STATUS: ORIG/CLOSED) 2L72 4F4 FRTA35EU E23EA 20040923000042004092300004EU 2004 9 23 AWXA200401041 120040920A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE EMERGENCY LIGHT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW 099 DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 RT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN GROUND WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20040923000212004092300021WP 2004 9 23 AALA20040962 120040916A3350 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21586AA 53249 OVERHEAD EMERGENCY LIGHTS AT ROWS 4 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 4 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 F A6WE E9NE 20040923000232004092300023EA 2004 9 23 COMA0460522 120040916A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE CARGO BAY CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01965CA 7131 CARGO FLOOR CAP CRACKED. IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-42-26. 2L72 4F4 FRTA21EA E15NE 20040923000262004092300026EU 2004 9 23 DXTA200400391 120040914A21708323712 COALESCER BAG BRAERO1000 BAE1251000 1500287EU PWA 305 PW305 NE CABIN AIR DIRTY E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07505QS7710 259005 ON DESCENT WITH POWER LEVERS AT IDLE NOTICED EXHAUST FUME ODOR IN CABIN. REMOVED COALESOR SOCK AND INSTALLED NEW IAW MFG M/M CHAPTER 21-50-13. RAN AIRCRAFT AND LEAK CHECKED, NO LEAKS NOTED, COULD NOT DUPLICATE SMELL AT IDLE ON GROUND. 2L72 4F4 FRTA3EU E35NE 20040923000272004092300027EU 2004 9 23 AWXA200401056 120040910A5315D53472193900 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 RT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-18. 2L72 4F4 FRTA28NM E40NE 20040923000282004092300028EA 2004 9 23 COMA0460529 120040914A2741601R517063 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01483CA5684 7689 FLIGHT 5328 STAB/MACH TRIM DISENGAGE. REPLACED THE STAB TRIM PANEL. 2L72 4F4 FRTA21EA E15NE 20040923000292004092300029EU 2004 9 23 AWXA200401057 120040910A5320D5348004320501 SILL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SILL FORWARD IB CORNER AT FR 66. MAINTENANCE REMOVED CORRODED R-2 DOOR SILL FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF SILL; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 8-12, AND 18. 2L72 4F4 FRTA28NM E40NE 20040923000302004092300030NM 2004 9 23 P9RA20040037 120040903A2421729825J IDG BOEING757 757231 1384950NM PWA 2037 PW2037 NE RT ENGINE INOPERATIVE A P9RAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11715TW 28483 72744 SYR. RT GENERATOR DRIVE LIGHT CAME ON AT APPROX. 60 KNOTS. REJECTED TAKE OFF AND RETURNED TO GATE. ISSUED MEL 24001. MAINTENANCE ENTRY 9/4/2004. REMOVED AND REPLACED RT IDG. 2L72 4F4 FRTA2NM E17NE 20040923000332004092300033CE 2004 9 23 DXTA200400382 120040903A3260 UPLOCK SWITCH RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS 258573 UPON GEAR RETRACTION, THE RT MAIN GEAR INDICATION (RED) STAYED ON. OPS CHECKED GEAR AND FOUND NO FAULT, ADJUSTED RT UPLOCK INDICATOR SWITCH TO INCREASE MOVEMENT 1 FLAT. OPS CHECKED GOOD IAW MM CHAPTER 32-10-25. 2L72 4F4 FRTA3EU E6WE 20040923000352004092300035NM 2004 9 23 DXTA200400380 120040905A3260W17049 LIGHT AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE MLG INDICATOR INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07210QS 211 ON APPROACH GEAR SELECTED DOWN LT GEAR INDICATOR INOP, TESTED GEAR LIGHTS AND LT GEAR LIGHTS FAILED TO TEST. ACCOMPLISHED GEAR NOT DOWN CHECKLIST IAW PILOT EMERGENCY PROCEDURES, USED ALTERNATE GEAR EXTENSION CHECKLIST TO LOWER INSURE GEAR DOWN. REPLACED BOTH BULBS ON CONFIGURATION PANEL FOR LT MAIN GEAR DOWN AND LOCKED INDICATION. OPS CHECK GEAR INDICATIONS NORMAL, COMPLETED LANDING GEAR OPERATIONAL CHECKS AFTER EMERGENCY EXTENSION IAW MM CHAPTER 32-002, OPS CHECK GOOD. 2K73 4F4 FRTA50NM E44NE 20040923000432004092300043NM 2004 9 23 ASMF200409004 120040911A7920471111172 HEAT EXCHANGER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23805AM2925229252 26272 726732 DURING TRANSIT CHECK, A LEAK WAS DETECTED ON OIL TANK TUBE SCUPPER AND FUEL/OIL HEAT EXCHANGER. LT ENGINE WAS STARTED AND LEAK INCREASED. FUEL/OIL HEAT EXCHANGER WAS REPLACED IAW MM 79-21-00, TEST CORRECT. DURING OVERNIGHT SERVICE, ENGINE RUNNING WAS PERFORMED IAW MM 71-00-00, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20040923000442004092300044WP 2004 9 23 ASMF200409007 120040919A3230 LINK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NLG JAMMED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23505MD 49149 CAPTAIN REPORTED THAT AFTER TAKEOFF, NOSE LANDING GEAR NOT RETRACTED, LIGHT ON, ABNORMAL PROCEDURE PERFORMED. AIRCRAFT SENT TO THE HANGAR AND NOSE LANDING GEAR OPERATIONAL TEST WAS PERFORMED. NOSE LANDING GEAR LINK WAS JAMMED DURING RETRACTION, THEREFORE NOSE LANDING GEAR WAS LUBRICATED IAW MM 32-30-00, TEST CORRECT. DURING OVERNIGHT SERVICE, A HYDRAULIC LEAK WAS DETECTED ON NOSE LANDING GEAR STRUT. NOSE LANDING GEAR O-RINGS WERE REPLACED IAW MM 32-21-02, TEST CORRECT. 2L72 4F4 F A6WE E9NE 20040923000472004092300047WP 2004 9 23 ASMF200409005 120040913A3232 ACTUATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NLG DOOR FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23501AM1172 1162 49188 AIRCRAFT RETURNED OF FLIGHT, NOSE LANDING GEAR DOOR WAS OPENED AND STRONG NOISE WAS HEARED BY CREW. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE LANDING GEAR DOOR ACTUATORS WERE REPLACED IAW MM 32-22-01, TEST CORRECT. 2L72 4F4 F A6WE E9NE 20040923000482004092300048WP 2004 9 23 ASMF200409006 120040914A325059142965509 VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NLG STEERING FAILED W ASMFO OTHER J WARNING INDICATION LDLANDING 1 SW23753RA 49587 AFTER LANDING, DURING TAXI, AIRCRAFT WAS NOT TURNED TO RT SIDE, BEING NECESSARY TO USE A TRUCK TO SEND THE AIRCRAFT TO PLATFORM. DURING MAINTENANCE REVISION, THE STEERING CABLE WAS DETECTED WITH DAMAGE. THE CABLE 268 WAS BROKEN. DURING OVERNIGHT SERVICE, CABLE 268 WAS REPLACED AND ADJUSTED IAW MM 32-51-03, TEST CORRECT. DURING OVERNIGHT SERVICE, STEERING CABLE 123D, BOTH NOSE LANDING WEAR WHEELS AND STEERING VALVE WERE REPLACED IAW MM 32-51-00, 32-40-02 AND 32-52-01, RESPECTIVELY, TEST WAS PERFORMED IAW MM 32-52-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040923000652004092300065 2004 9 23 RTE2004F00000 420040702A6113055032112 BULKHEAD CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160CTM GL PROP SPINNER CRACKED E RTEAK NONE O OTHER ININSP/MAINT 1 NM019379H227 730399 17266128 L4080727A DURING POST FLIGHT INSPECTION, FOUND SEVERAL SPINNER SCREWS LOOSE, AND ONE MISSING THAT HAD BEEN THERE AT PREFLIGHT. REMOVED SPINNER TO INVESTIGATE, AND FOUND FORWARD BULKHEAD CRACKED, WITH MANY SMALL PIECES MISSING. DURING PROPELLER REMOVAL TO REPLACE DAMAGED PARTS, FOUND PROPELLERS TO INSTALLED AND CLOCKED CORRECTLY, INCLUDING BOLT TORQUES IAW MFG MM. INSPECTION FOUND PROPELLER UNDAMAGED, AND IN AIRWORTHY CONDITION. NO APPARENT CAUSE COULD BE DETERMINED, DEFECTIVE PART FROM MFG SUSPECTED. TT 227 HOURS. ACCUMULATED IN LESS THAN A THREE MONTH PERIOD. PILOT REPORTED NO VIBRATION OR ANY OTHER OPERATIONAL CONCERNS. 1H71 3O3 ONT3A12 E274 5 NP910 20040923000662004092300066GL 2004 9 23 ALG2004F00038 220040607A7230 COMPRESSOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE STALLED E ALGAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW03361AL 51212 CAE895014 AIRCRAFT HAD COMPRESSOR STALL DURING TAKEOFF. MAINTENANCE INSPECTED ENGINE INLET AND COMPRESSOR AREA, FOUND EVIDENCE OF FROG INGESTION. INSPECTED ENGINE COMPRESSOR FOR DAMAGE NO DAMAGE WAS FOUND. PERFORMED ENGINE CHEMICAL WASH AND ENGINE POWER CHECK. OPS CHECK WAS GOOD. 1G71 3U3 U H2SW E1GL 20040923000752004092300075NM 2004 9 23 COOSDR040010 120040630A5314 KEELBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 AFT CARGO COMPARTMENT, STR 29L KEELBEAM, OB FLANGE CORRODED. 2L73 4F4 FRTA3WE E2EA 20040923000762004092300076NE 2004 9 23 KBM2004F00119 220040610A7321 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE COOLER BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH W26939 3141 MOTOR WILL NOT ROTATE WHEN POWER IS APPLIED. REPLACED MOTOR WITH REPAIR UNIT OPS, GOOD. 1G71 3U3 U H9EU E19EU 20040923000782004092300078NE 2004 9 23 KBM2004F00183 220040714A72619560115450 MAGNETIC SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE LEAKING A KBMAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP19966SH 3787 MAG SEAL LEAKING. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040923000802004092300080 2004 9 23 LU42004F00000 420040630A6122 FLYWEIGHT CESSNA206 206H 2073301CE LYC O540 IO540* 41532EA MCAULY3D36C B3D36C432 GL PROP GOVERNOR BROKEN B LU4RO OTHER O OTHER NRNOT REPORTED 1 WP197270C2400 381 20608051 GOVERNOR FAILED TO PRODUCE PRESSURE, UPON DISASSEMBLY FOUND BROKEN FLYWEIGHT DISC PN D20880, SPRING DRIVE PN C20886 DAMAGED, PN B208821, SPRING BROKEN. NOTE: NO IMPACT KNOWN PARTS SENT TO MFG FOR INSPECTION. 1H71 3O3 ORTA4CE 1E4 5 CP58GL 20040923000832004092300083CE 2004 9 23 LV02004F00000 120040509A3320AL5112 POWER SUPPLY CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN LIGHTS MALFUNCTIONED B LV0RO OTHER L NO TEST NRNOT REPORTED 1 CE01998BC 5500665 THE AL5112 POWER SUPPLY DOES NOT HAVE ENOUGH POWER TO LIGHT THE FORWARD CABIN FLUORESCENT BULBS. IT IS RATED TO LIGHT 52 INCHES OF BULB AND MFG HAS 2 BULBS EQUALING 69 INCHES INSTALLED. THIS IS THE WAY IT IS IN THE PARTS MANUAL. FOUND THE PROBLEM AFTER REPLACEMENT OF NUMEROUS PARTS IAW MFG TECH REPS THAT COULDN’T FIGURE OUT THE PROBLEM. FINALLY I GOT SOME ANSWERS FROM MFG AND WE CAME TO THE CONCLUSION THAT MFG CREATED A LIGHTING SYSTEM USING MFG PART, BUT SEEM TO HAVE OVERLOOKED THAT EACH POWER SUPPLY CAN ONLY POWER UP TO 52 INCHES OF BULB. 1L72 4F4 F A22CE E1NE 20040923000872004092300087EA 2004 9 23 WVE2004F00021 120040615A261324412047 ELEMENT CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343B1 NE LT ENGINE MISLOCATED B WVERA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 EA09330FX 5487 APPROXIMATELY 30 MINUTES AFTER DEPARTURE, THE LT ENGINE TAILCONE OVERHEAT LIGHT ILLUMINATED, ENGINE WAS SHUT DOWN, LIGHT WENT OUT AND AIRCRAFT RETURNED WITHOUT INCIDENT. THE FIRE DETECTION ELEMENT WAS FOUND TO BE CHAFING ON THE ELEMENT COVER. REPOSITIONED ELEMENT AND SWAPPED NR 1 AND NR 2 FIRE DETECTION UNITS FOR TROUBLESHOOTING. OPS CHECKED ON ENGINE RUN AND FOUND NO OTHER DEFECT. AN IN FLIGHT TEST WAS PERFORMED AND WAS SATISFACTORY. FIRE DETECTION ELEMENT IMPROPERLY POSITIONED. (EA09200402432) 2L72 4F4 FRTA21EA E15NE 20040923000882004092300088EU 2004 9 23 KBM2004F00152 120040523A6420355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH 3345 T/R HALF SHELLS WORN BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040923000962004092300096SW 2004 9 23 MPY2004F00000 120040712A7120600429503 HEAT SHIELD MOONEYM20 M20R 5870225SW CONT O550 IO550* SO MCAULY2A34C 2A34C* GL ENGINE MOUNT GOUGED B MPYRO OTHER O OTHER NRNOT REPORTED 1 SW17242MD250 290292 HEAT SHIELD PN 600429-503 WAS FOUND TO BE MAKING CONTACT WITH TUBULAR ENGINE MOUNT. THIS CONTACT CREATED A GOUGE APPROX .200 INCH LONG AND APPROX .045 INCH DEEP. 1L71 3O3 ORT2A3 E3SO 5 CP3EA 20040923000982004092300098NM 2004 9 23 USA2004F00074 120040613A3350321431 BATTERY BOEING767 767201 1385125NM GE CF6 CF680 30025NE L1 DOOR DISCHARGED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19650US 23902 FOUND L1 DOOR EPSU INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2L72 4F4 FRTA1NM E13NE 20040923000992004092300099NM 2004 9 23 ASFM200406029 120040625A1420 CONNECTOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE DIRTY W ASMFA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW23946AS 49658 AIRCRAFT RETURNED OF FLIGHT, "ANTENNA FAIL" LIGHT TURNED ON AND CAPTAIN TURNED OF RADAR. ANTENNA CONNECTOR WAS CLEANED AND CIRCUIT BREAKER WAS RESEATED IAW MM 34-41-01, AND AIRCRAFT WAS REFUELED, ALL CORRECT. DURING OVERNIGHT SERVICE, CONNECTOR WAS CLEANED IAW 31-10-04 AND WIRING WAS CHECKED IAW MM 34-43-02, TEST CORRECT IAW MM 34-41-00. 2L72 4F4 FRT E2EA 20040929000682004092900068WP 2004 9 29 AALA20040965 120040918A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219406W 53126 EMERGENCY LIGHTS AT L2 637 THROUGH 639 INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS AT L2 637 THROUGH 629. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040929000712004092900071EA 2004 9 29 COMA0460518 120040916A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01965CA 7131 FS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136. 2L72 4F RTA21EA 20040929000722004092900072NE 2004 9 29 AALA20040992 220040926A7230 FAN BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE DAMAGED A AALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW21454AA 49559 717338 INFLIGHT AFTER TAKEOFF LOUD VIBRATION REPORTED BY FLIGHT ATTENDANT. VIBRATION AT ROW 26 AND AFT. VERIFIED BY FIRST OFFICER. COULD NOT ISOLATE TO SPECIFIC ENGINE OR AIRFRAME. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND EVIDENCE OF BIRD STRIKE IN THE NUMBER 1 ENGINE INLET. PERFORMED BIRD STRIKE INSPECTION. REPLACED TWO EACH FAN BLADES IN NUMBER 1 ENGING PER WORK CARD 72-91-11. CONDUCTED PAST FAN BLADE REPLACEMENT ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20040929000742004092900074NM 2004 9 29 AALA20040989 120040922A5620AAP3080 WINDOW BOEING757 757223 1384957NM CABIN DELAMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21663AM 25297 SAN - THIRD WINDOW AFT OF L2 DOOR, AT SEAT 11A, FOUND BROKEN BY FLEET SERVICE CLERK AT DEPARTURE TIME. APPEARS TO BE DELAMINATED. CAUSE UNKNOWN. REPLACED WINDOW AT SEAT 11A AND REINSTALLED INNER WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040929000782004092900078WP 2004 9 29 0030 220040617A753297881271 BLEED VALVE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP LT ENGINE STUCK E CIEAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM03553V 67 35A141 P74430C AFTER T/O IFR CONDITIONS, PILOT NOTICED LT ENG UNABLE TO MAINTAIN N1 POWER & ITT WAS CLOSE TO MAX. RETURNED TO BASE. MX PERFORMED GROUND RUN & WAS ABLE TO VERIFY CONDITION ON GROUND. ENG SURGE VALVE SOLENOID PACK FOUND TO HAVE WATER CONTAMINATION. ENG REMOVED ENOUGH TO GAIN ACCESS TO SURGE VALVE, VALVE FOUND STUCK IN OPEN POSITION. REASON FOR MOISTURE NOT DETERMINED. SURGE VALVE & SURGE VALVE SOLENOID PACK REPLACED WITH SERVICEABLE OVERHAULED UNITS. ALL INNER CONNECT TUBING INSPECTED FOR CONDITION, SECURITY & CONTAMINATION, AND CLEANED. ENG REINSTALLED, RUN & CHECKED ON GROUND, FOUND NORMAL. THIS SDR WILL CONTAIN INFO FOR SURGE VALVE & AN ADDITIONAL UNIT WILL BE SUBMITTED FOR SURGE VALVE SOLENOID PACK. 2L72 4F4 F A10CE E6WE 20040929000802004092900080CE 2004 9 29 0032 120040620A2134E45C49 PRESSURE SWITCH AIRESRCH 1340414 LEAR 35 35A 5170602CE CABIN PRESSURE OUT OF LIMITS E CIEAK NONE L NO TEST ININSP/MAINT 1 NM03222BE 40520 35A0489 DURING PERFORMANCE OF A 2400 HOUR INSPECTION THE ABSOLUTE PRESSURE SWITCH FOR THE AURAL WARNING ON THE PRESSURIZATION SYSTEM, FAILED FUNCTION CHECK. THE UNIT IS TOO CLOSE THE SWITCH AND PROVIDE AURAL WARNING TO THE FLIGHT CREW AT 8,750 FEET + OR - 250 FT. THE SWITCH THEN OPENS DURING DESCENT PRIOR TO 7200 FEET. THE TEST ON THIS UNIT RESULTED IN THE SWITCH CLOSING AT 9,250 FT. THE POSITION WHEN THE SWITCH REOPENED WAS AT 8,400 FEET. THIS IS NOT A NORMAL STATUS REPLACEMENT TRACKED ITEM, THEREFORE REPLACEMENT DATE AND TIME WERE NOT CONFIRMED. REPLACEMENT WAS AFTER 4-9-01 AS THAT IS THE MANUFACTURED DATE OF THE SWITCH. 2L72 4F A10CE 20040929000852004092900085EU 2004 9 29 DXTA200400352 120040802A2120 ODOR BRAERO1000 HAWKER1000 7450005EU CABIN DETECTED E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07550QS 259050 WHILE CLIMBING THROUGH FL250 SELECTED ENGINE ANTI ICE ON, SHORTLY THEREAFTER NOTICED A STRONG BURNING SMELL IN THE COCKPIT. DE-SELECTING ANTI ICE, SMELL WENT AWAY, NO VISIBLE SMOKE WAS NOTICED. OPS CHECKED ANTI ICE SYSTEM, SYSTEM OPS CHECK GOOD IAW HAWKER 1000 MM CHAPTER 75-10-00. 2L72 4F RTA3EU 20040929000882004092900088WP 2004 9 29 AALA20040972 120040919A1420 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21228AA 49178 DFW - TAIL CONE RELEASE HANDLE EMERGENCY LIGHT INOPERATIVE. REPINNED TAIL CONE RELEASE HANDLE EMERGENCY LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040929000902004092900090NM 2004 9 29 AALA20040971 120040921A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21798AN 30797 DFW - EXTERIOR EMERGENCY LIGHT AT DOOR 1R INOPERATIVE. REPLACED BATTERY PACK AT DOOR 1R FOR EXTERIOR EMERGENCY LIGHT AT DOOR 1R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20040929000922004092900092NM 2004 9 29 AALA20040980 120040901A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959AN 30828 TUL - CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500 RIGHT FAILED TEST PER CARD 2904. REPLACED BATTERY PACK AT STATION 500 RIGHT FOR CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20040929000982004092900098 2004 9 29 DXTA200400373 420040825A34607014300901 CDU CESSNA750 750 2076810CE COCKPIT SMOKE E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL07977QS5094 7500077 DURING VECTORS TO FINAL, DU NR 1 FLASHED SEVERAL TIMES BETWEEN A BLANK SCREEN AND A RED X FOR ABOUT 5 SECONDS. CHECK DU NR 1 EICAS MESSAGE, FLASHED ONCE DURING THIS TIME. ACRID SMELL WAS PRESENT BUT SMOKE VISIBLE, DISPLAY RETURNED TO NORMAL. FOUND DUI UNIT SMOKED, REMOVED & REPLACED NR 1 DUI OPS CHECKED SATISFACTORY. ALL WORK DONE IAW CESSNA 750 MM CHAPTER 34-25-01. 2L72 4J RTT00007WI 20040929001032004092900103EA 2004 9 29 COMA0460537 120040918A3230555406 VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA11379 7043 FLIGHT 5481 DURING HSV APPROACH RECEIVED A GEAR DISAGREE CAUTION. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20040929001052004092900105EA 2004 9 29 COMA0460542 120040919A32344622 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01987CA20975 7199 FLIGHT 9472 AFTER TAKEOFF FROM ATL RECEIVED A LANDING GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20040929001082004092900108EU 2004 9 29 MALA040564 120040907A3234HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A1500097EU NLG MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15505XJ E2313 NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTION, GREEN LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED NLG RETRACT JACK P/N 104626002, S/N ON DH-0147-98, OFF DH-0082-96 AND LANDING SELECTOR VALVE P/N HTE9490-4, S/N ON FR022BC, OFF FTRF001AW AND RE-SHIMMED NLG STRIKER PLATE. OPS AND LEAK CHECK GOOD IAW AMM32-30-00. 2H74 4F RTA49EU 20040930000022004093000002 2004 9 30 HNAA0400083 420040917A3442MI585355 TRANSCEIVER DHAV DHC8 DHC8311 1386006EA WX RADAR INOPERATIVE A HNAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA07331EN 279 WEATHER RADAR SPOKING & WOULD NOT PAINT WEATHER. WEATHER RADAR FAILED DURING FLT TO CLT. DIVERTED TO FAY DUE TO WEATHER IN CLT. REMOVED AND REPLACED RADAR RT. OPS CHECK GOOD. 2H72 4T RTA13NM 20040930000142004093000014NM 2004 9 30 GAIA04091OP 120040831A3230656021136 ACCESSORY UNIT BOEING727 727251 138408HNM MLG INOPERATIVE A GAIAO OTHER J WARNING INDICATION CRCRUISE 1 SW07252US 19971 FLT 713 - SJU-MIA - DURING CRUISE, RIGHT MAIN GEAR RED LIGHT ILLUMINATED IN FLIGHT. FLIGHT CONTINUED TO SJU WHERE A LANDING WAS MADE WITHOUT INCIDENT. TROUBLE SHOT PER MM 32-61-01 AND FOUND LANDING GEAR ACCY UNIT TO BE AT FAULT. REMOVED AND REPLACED SAME PER AMM 32-09-121 PAGE 401/501 AND ACCOMPLISHED LANDING GEAR EXT/RET TEST PER MM 32-61-01 PATE 501/502. ALL TESTS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20040930000172004093000017EU 2004 9 30 A6WA200460034 120040831A2621 BOTTLE BAC 146 146200A 1500266EU NR 1 INTAKE DISCHARGED A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31290UE E2080 NR 1 INTAKE ASSEMBLY INBOARD FIRE BOTTLE EXCEEDS LOW WEIGHT LIMIT. REMOVED AND REPLACED FIRE BOTTLE. (M) 2H74 4F A49EU 20040930000212004093000021EA 2004 9 30 ASOA04606 120040817A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11874AS 7551 DURING A C-CHECK IN MCN, THE MAIN AVIONICS BAY DOOR HANDLE AT THE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE. (M) 2L72 4F RTA21EA 20040930000242004093000024SO 2004 9 30 SIMA200424704 120040826A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21828AE 145604 DURING CPCP INSPECTION, MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM. REPAIRED LEFT OMEGA BEAM IAW EMB 140 SRM 53-21-10 FIG 201. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040930000262004093000026SO 2004 9 30 SIMA200424701 120040903A1420 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY SIGN LOOSE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21621AE 145105 ORD - FLT 4315 - CREW REPORTED THE RIGHT EMERGENCY EXIT SIGN ON EMERGENCY EXIT OVERWING DOOR TO BE INOPERATIVE. MAINTENANCE FOUND CONNECTOR FOR EMERGENCY SIGN LOOSE. RECONNECTED CONNECTOR AND COMPLIED WITH AN OPERATIONAL CHECK WITH NO DEFECTS NOTED. (M) 2L72 4T RTT00011AT 20040930000322004093000032EU 2004 9 30 ASOA04617 120040822A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11632AS 338 FLT 4276 - DURING A GROUND INSPECTION IN ATL, THE AFT SECTOIN OF FLOOR EMERGENCY LIGHTING WAS FOUND WITH EVERY OTHER LIGHT OPERATING. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20040930000392004093000039EA 2004 9 30 ASOA04619 120040822A5320 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11917EV 7769 DURING A C-CHECK IN MCN, THE RIGHT SIDE ACCESS PANEL CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT SIDE ACCESS PANEL CORNER OF THE ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20040930000412004093000041EA 2004 9 30 ASOA04613 120040818A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11845AS 7324 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20040930000422004093000042EU 2004 9 30 ASOA04626 120040802A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD SEAT TRACK BETWEEN FRAME 35/36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD SEAT TRACK BETWEEN FRAME 35/36 IAW SRM 53-00-00, FIG 434 AND 53-21-04. (M) 2H72 4T RTA53EU 20040930000442004093000044EU 2004 9 30 ASOA04624 120040802A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FS 36 BETWEEN STRINERS 16R AND 16L, AND FS 38 BETWEEN STRINGERS 15R AND 15L WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FS 36 BETWEEN STRINGERS 16R AND 16L, AND FS 38 BETWEEN STRINGERS 15R AND 15L IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040930000632004093000063SO 2004 9 30 SIMA200425303 120040902A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R AT FRAME 52 AND 53 WAS FOUND TO BE CHAFED BEYOND SRM LIMITS. BLENDED CHAFED AREA SMOOTH. PERFORMED A DOUBLER ANGLE, TWO FILLERS, REPAIR DONE IAW EMB STATEMENT IC2004-145/3093A. (M) SIMA 2L72 4F RTT00011AT 20040930000672004093000067SO 2004 9 30 SIMA200424703 120040826A532014522170005 CHANNEL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21828AE 145604 SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND CORROSION ON SERVICE DOOR SILL PLATE. REMOVED AND REPLACED THE SERVICE DOOR SILL PLATE CHANNEL IAW EMB 140 SRM 51-40-02. AIRCRAFT AS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040930000762004093000076NE 2004 9 30 ASOA04651 220040827A72616087T04P06 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE FAILED A ASOAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11845AS 7324 FLT 4479 - DURING CRUISE FROM CHS-DFW, AT APPROXIMATELY 36,000 FEET THE LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED WITH THE OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. THE CREW COMPLIED WITH THE QRH AND UPON REDUCING THE LEFT ENGINE THE IDLE, THE OIL PRESSURE WENT UP TO 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LUBE AND SCAVENGER PUMP ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040930000802004093000080EU 2004 9 30 ASOA04632 120040803A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE RIGHT INBOARD FLAP NR 1 CAM GUIDE AT RIB 4 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP NR 1 CAM GUIDE AT RIB 4 IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000852004093000085NM 2004 9 30 C7WA200400023 120040609A5313 STRINGER BOEING727 727232 1384082NM CARGO BAY CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 720E CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M) 2L73 4F A3WE 20040930000952004093000095EA 2004 9 30 A6WA200440101 120040711A2132 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LT PACK ILLUMINATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31470ZW 7927 LEFT PACK HIGH PRESSURE CAS MESSAGE. PERFORMED OPERATIONAL CHECK OF LEFT PACK IAW AMM 21-60-00. OPS CHECK NORMALLY OF ENGINE BLEED/APU BLEED. NO FURTHER MAINTENANCE REQUIRED. (M) 2L72 4F RTA21EA 20040930000962004093000096EA 2004 9 30 ASOA04643 120040825A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NLG ILLUMINATED A ASOAO OTHER N FALSE WARNING APAPPROACH 1 SO11906EV 7642 FLT 4554 - DURING FINAL APPROACH TO DFW AND AEX, THE CREW RECEIVED A NOSE GEAR DISAGREE MESSAGE AND PERFORMED A MISSED APPROACH. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. AFTER COMPLYING WITH THE QRH THE GEAR INDICATED DOWN AND THREE GREEN LIGHTS WERE RECEIVED. THE AIRCRAFT LANDED SAFELY IN DFW WITH EMERGENCY TRUCKS FOLLOWING IT TO THE GATE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF FULL GEAR SWINGS FOR FIFTEEN CYCLES. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930001062004093000106EA 2004 9 30 ASOA04641 120040822A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURNG HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT CORNERS OF THE FUSELAGE SKIN AT FS 235, BL 6 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE LEFT SIDE FUSELAGE STRUCTURE AT FS 235, STRINGER 26 IAW BOMBARDIER REO 601R-53-11-802. THIS REPAIR IS VALID FOR 500 FLIGHT HOURS FROM THE TIME OF INCORPORATION. MAINTENANCE ALOS PERFORMED A TEMPORARY REPAIR TO THE RIGHT SIDE FUSELAGE SIN AT FS 235, BL 6 IAW BOMBARDIER REO 601R-53-11-047. THIS REPAIR IS VALID FOR 400 CYCLES FROM RETURNT O SERVICE. BOTH TEMPORARY REPAIRS ARE TO BE REINSPECTED EVERY 100 FLIGHT HOURS. THIS MRR WILL REMAIN OPEN PENDING COMPLETION OF THE PERMANENT REPAIRS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVI2L72 4F RTA21EA 20040930001142004093000114EU 2004 9 30 USAABA04020 120040830A335032146210 EPSU AIRBUS330 A330323 3930335EU L3 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19670UW 0315 PIT - FOUND DOOR 3L EPSU INOPERATIVE. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA46NM 20040930001242004093000124 2004 9 30 GTIA040685 420040728A2565 GIRT BAR DOUG DC9 DC982 3022082WP L2 DOOR SLIDE CONTAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FLT 861 - LGA - FOUND L2 DOOR GIRT BAR WILL NOT UNLOCK FROM THE FLOOR DOOR IS STILL ARMED. UNARMED L2 DOOR REMOVED EXCESS PAINT FROM GIRT BAR AND ATTACH BRACKETS. (M) 2L72 4F A6WE 20040930001252004093000125 2004 9 30 GTIA040686 420040707A2565 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR DEPLOYED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23803NK 48087 FTW - DEPLOYED L1 DOOR SLIDE FOR FUNCTIONAL CHECK. (M) 2L72 4F A6WE 20040930001282004093000128EA 2004 9 30 A6WA200440107 120040730A5743601R572100321 BUSHING CNDAIRCL600 CL6002B19 1900309EA RT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31430AW 7719 FOUND RIGHT MLG AFT TRUNNION BUSHING MIGRATED .35 INCH. REMOVED MIGRATED BUSHING. REAMED TRUNNION LUG BORE OT 1ST OVERSIZE AND INSTLALED 1ST OVERSIZED BUSHING, P/N 601R5721003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20040930001352004093000135NE 2004 9 30 USAAEM04015 220040902A73204120T00P32 FADEC EMB ERJ170ERJ170100 EU GE CF34 CF34* NE NR 1 ENGINE MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815MD319 17000034 NR 1 ENGINE FADEC WAS REMOVED DUE TO HISTORY OF FADEC FAULTS AND NO DISPATCH MESSAGE. MAINTENANCE REPLACED NR 1 ENGINE FADEC. (M) 2L74 4F4 FRTA56NM E15NE 20040930001392004093000139NM 2004 9 30 SWAA042807 120040927A53156545804 FLOORBEAM BOEING737 737301 1384611NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 259.5, LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2L72 4F RTA16WE 20040930001462004093000146NM 2004 9 30 SWAA042800 120040927A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040930001502004093000150WP 2004 9 30 ABXA040331 120040911A571155978342 SPAR DOUG DC8 DC863F 302198FWP RT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23814AX 46041 RIGHT WING INTERNAL FUEL TANK AT STA XRS 172 LOWER CENTER SPAR AND WEB HAD CRACK AND CORROSION AT SPAR CAP CRACK. CUT OUT DAMAGED AREA OF CENTER SPAR AND WEB IAW REA D857-49982MR. FABRICATED REPAIR PARTS IAW DAC DWG'S 5613912, 3642213, 3644709 AND SRO8570015. REINSTALLED STRUCTURE IAW DC-8 SRM. REPAIRED IAW REA D857-49982MR. 2L74 4F 4A25 20040930001542004093000154NM 2004 9 30 HNAA0400119 120040902A321310100125 STRUT DHAV DHC8 DHC8102 2809003NM LT MLG FAULTY A HNAAO OTHER O OTHER LDLANDING 1 EA07824EX25295 387 FLIGHT 3800 REPORTED THE LEFT MAIN LANDING GEAR STRUT DID NOT COMPRESS AFTER LANDING. MAINTENANCE FROM MIDDLETOWN ROAD TRIPPED TO PITTSBURGH TO REMOVE AND REPLACE THE LEFT HAND MAIN LANDING GEAR SHOCK STRUT. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040930001602004093000160WP 2004 9 30 ABXA040321 120040901A533059114034 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 APPROXIMATELY 1 INCH CRACK IN EXTERNAL SKIN JUST FORWARD OF RIGHT WIPER ACCESS PANEL. REPAIRED CRACK IN EXTERNAL SKIN IAW REA D953-50452MR. 2L72 4F A6WE 20040930001922004093000192NM 2004 9 30 SWAA042782 120040924A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 AFT BOTTOM EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20040930001932004093000193 2004 9 30 SWAA042783 420040924A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29458WN 33857 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040930001942004093000194 2004 9 30 SWAA042784 420040924A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 DURING SCHEDULED RON FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041001000032004100100003NM 2004 10 1 EIA2004081 120040903A5311 FRAME BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 FRAME STA. 380L CRACKED FLANGE AT STR 22 CUTOUT. REMOVED DAMAGED AND FABBED AND INSTALLED REPAIR IAW SRM 53-10-04 PG. 43-45 AND 53-10-02. 2L74 4F4 F A20WE E20EA 20041001000082004100100008NM 2004 10 1 UPS04M43192 120040820A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C HORZ STAB NR 31 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLEND AND REAMED TO 1.178 INCH AT B/N HOLE NR 31 RT FOUND OUT OF LIMITS. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 31 RT IAW EO MD11-5510-19409-H. REPAIR C/OUT AT B/N HOLE NR 31 RT IAW EO MD1 1-5510-19409-H AND EN:1302-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041001000202004100100020WP 2004 10 1 WX0400035 120040924A2741 BRAKE ASSY DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE TRIM MOTOR OVERHEATED A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19891GA 49423 AFTER DEPARTURE AT 10000 FT AGL F/O WAS HAND FLYING AIRCRAFT AND REPORTED TO CAPTAIN THAT PRIMARY TRIM SWITCHES ON BOTH CONTROL WHEELS FAILED. CAPTAIN TRIED YOKE SWITCHES AND SUITCASE HANDLES ON PEDESTAL, NEITHER WORKED. CAPTAIN CHECKED ALTERNATE TRIM SWITCHES, FOUND OPERATIONAL. CAPTAIN INSTRUCTED F/O TO TURN AUTOPILOT ON. CREW COMPLETED QRH PROCEDURES AND RETURNED TO AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRIMARY TRIM MOTOR/BRAKE ASSEMBLY OVERHEATING AND FAILING, REPLACED MOTOR/BRAKE ASSEMBLY. OPERATIONALLY CHECKED GOOD IAW MM 27-40-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20041001000262004100100026WP 2004 10 1 WX0400032 120040920A3350 LAMP DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE EMERGENCY LIGHT INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19948MA 49778 MAINTENANCE REPORTED EMERGENCY FLOOR LIGHT INOPERATIVE ROW 22. MAINTENANCE RE-LAMPED EMERGENCY LIGHT ROW 22, EMERGENCY FLOOR LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E9NE 20041001000272004100100027NE 2004 10 1 GJR2004F00001 220040901A7314TF9005 PUMP DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985* 52008NE FUEL SYSTEM INOPERATIVE B GJRRO OTHER O OTHER NRNOT REPORTED 1 NM01900KA 80 1676 LOSS OF FUEL PRESSURE. 1H71 3R3 R A806 5E1 20041001000322004100100032NM 2004 10 1 QXEA200400687 120040917A2760 HINGE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 LT OB SPOILER MIDDLE HINGE ASSEMBLY IS DAMAGED AT PCU TOGGLE LINK ATTACH POINT. PERFORMED HFEC IAW-8 400 NDTM PN 651-00-02. NO CRACKS NOTED. REPAIRED. 2H72 4T4 TRTA13NM E00062EN 20041001000352004100100035EU 2004 10 1 04FDEA02833 120040928A5730 PANEL AIRBUS310 A310 EU GE CF6 CF680A3 30025NE RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 PANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998 2L72 4F4 FRTA35EU E13NE 20041001000422004100100042NM 2004 10 1 CALA0400647 120040927A5730114N2106 SKIN BOEING757 757224 1384958NM RROYCERB211 RB211535E4 54555NE LT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2767134 29283 INSPECTION FOUND A 6 INCH CRACK IN LT WING LEADING EDGE SKIN. THE SKIN WAS REPAIRED IAW EA 5731-01010. 2L72 4F4 FRTA2NM E12EU 20041001000432004100100043EA 2004 10 1 SWIA200413861 120040925A2740 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB/MACH TRIM MALFUNCTIONED A SWIAL ABORTED APPROACH JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07930SW STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON TWICE DURING FLIGHT. REPLACED STAB TRIM/MACH TRIM CONTROL PANEL WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD IAW MM 27-00-00. 2L72 4F4 FRTA21EA E15NE 20041001000452004100100045NE 2004 10 1 SWIA200413863 220040924A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 SEIZED A SWIAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 NM07429SW8929 8929 7518 873018 AFTER TAKEOFF (ABOUT 500FT), ENGINE NR 2 FAILED. NR 2 STOPPED, AND ITT PEGGED. OIL PRESSURE DROPPED TO ZERO. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000502004100100050 2004 10 1 2004UALA00845 420040917A2565 BATTERY PACK BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE OVERWING SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29671UA 30026 NR 1 RT WING SLIDE SQUIB FAILS TO TEST. REPLACED BOTH LEFT AND RIGHT BATTERY PACKS AND RIGHT ESCAPE SYSTEM RELAY ASSY M1136. SYSTEM TEST 1 AND 2 CHECK NORMAL. 2L72 4F4 FRTA1NM E24NE 20041001000592004100100059 2004 10 1 P5CA0401230 420040929A3442 WARNING LIGHT BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE WX RADARS ACTIVATED A P5CAK NONE J WARNING INDICATION ININSP/MAINT 1 WP23355MC 23395 (ANT FAULT): MESSAGE ON BOTH NR 1 AND NR 2 WX RADARS. TRANSFERED TO DMI NR 33183 IAW MEL NR 34-23B. 2L74 4F4 FRTA20WE E23EA 20041001000642004100100064EA 2004 10 1 04269648 120040925A3030 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AOA INOPERATIVE A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27648BR 7406 LT AOA HEAT CIRCUIT BREAKER POPPED. REMOVED AND REPLACED LT AOA SENSOR IAW MM 30-31-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000662004100100066NM 2004 10 1 0401735801 120040927A28203161310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING CHAFED A NWAAK NONE K FLUID LOSS ININSP/MAINT 1 GL01581NW6938 32982 THE FUEL SUPPLY TUBE IN THE RT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED IAW EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041001000922004100100092NM 2004 10 1 04FDEA02814 120040924A2840360112004 CONTROL UNIT DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE FUEL SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 SO25605FE7637 7637 48514 IN CRUISE FLT, AT FL 330, AT APPROX TAKEOFF PLUS FOUR HOURS, RECEIVED (LEVEL 1 TANK 2 FUEL QTY LO) ALERT S.D. FUEL READINGS WERE: 1- 900 2- 0 3-900 AUX- 900 TAIL- 12900. FUEL INDICATIONS AND USAGE TO THAT POINT HAD BEEN NORMAL. FSC WAS IN AUTO, ALSO GOT LEVEL 1 ALERT (FUELMANF DRAIN) AND DRAIN WAS ILLUMINATED OVERHEAD IN THE GUARDED MANF SWITCH. GOT A LEVEL 2 FUEL QTY/USED CHECK ALERT AS WELL AS LEVEL 2 FUEL QTY FAULT ALERT CHECKLIST FOR FUEL MANF DRAIN DIRECTS CREW NOT TO PRESSURIZE CROSSFEED MANIFOLD AS A RESULT WE KEPT FSC IN AUTO AND DIVERTED TO KMSP. REMOVED AND REPLACED S.E.M AND FUEL QUAN. DATA CONTROL UNIT IAW M/M. SYS OP'S CHECKS NORMAL AT THIS TIME. OK TO CONTINUE. 2L73 4F4 FRTA22WE E31N3 20041001000942004100100094EA 2004 10 1 SWIA200413837 120040922A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07446SW 7666 LT SIDE EMERGENCY LIGHTS (OUTSIDE) ARE OUT. REMOVED AND REPLACED LT FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001000962004100100096SO 2004 10 1 SWIA200413839 120040918A33506225734002 LAMP EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07560SW 120334 EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AT AFT EMERGENCY EXIT. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041001000982004100100098EA 2004 10 1 SWIA200413841 120040912A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07597SW 7293 CAPTAIN'S TRIM SWITCH WILL NOT TRIM NOSE UP, NOSE DOWN OK. REMOVED AND REPLACED CAPTAIN TRIM SWITCH ON YOKE IAW CRJ200 MM 27-00-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041001001042004100100104EU 2004 10 1 QEM2004F00000 220040614A7250 TURBINE BLADES BOEING737 737300 1384610NM CFMINTCFM56 CFM563C1 13802EU TURBINE WHEEL CRACKED B QEMYO OTHER O OTHER NRNOT REPORTED 1 EA35GOGBE5655 GWN046RH 859133 THE HPT DISC WAS FOUND WITH 5 CRACKED FIR TREES. MFG WAS INFORMED AND HAVE REQUESTED THE HPT DISC AND HPT BLADES BE RETURNED FOR INVESTIGATION. HPT AND LPT NOZZLE WERE INSPECTED AND NO DEFECTS THAT COULD HAVE AFFECTED THE DISC NOTED. FUEL NOZZLES FLOW, WERE SATISFACTORY. THE ENGINE HAD EXPERIENCED AN OVER TEMPERATURE EVENT OF DURATION 33 SECONDS, PEAK EGT 975.5 DEG CAUSED BKA VBV SCHEDULING PROBLEM. 2L72 4F4 FRTA16WE E21EU 20041001001092004100100109CE 2004 10 1 IJAA016F 120040719A3260903610373 DOWNLOCK SWITCH BEECH 90 C90A 1152911CE PWA PT6 PT6* 52043EA RT MLG DIRTY E IJAAO OTHER O OTHER NRNOT REPORTED 1 CE07424EM LJ1351 RT MAIN GEAR DOWN LIGHT WOULD NOT COME ON WHEN LANDING GEAR WAS DOWN AND LOCKED. AIRCRAFT WAS LANDED WITHOUT INCIDENT. IT WAS DETERMINED THAT THE LANDING GEAR DOWN LOCK SWITCH WAS DIRTY WITH PAINT OVERSPRAY AND THE GEAR WAS RIGGED TO MIN TRAVEL OF DOWN LOCK PLUNGER. AFTER CLEANING AND CHECKING THE RIG OF THE GEAR, THE GEAR WAS OPERATED THROUGH 15 SATISFACTORY CYCLES. (CE07200415107) 1L72 3T3 TRT3A20 E2NE 20041001001112004100100111CE 2004 10 1 AHT2004F00000 120040227A52101313232C17 CLEVIS PIN BEECH 90 C90 1152913CE PWA PT6 PT6A20 52043EA HARTZLHCB4T HCB4TN3 GL PAX DOOR BROKEN B AHTRO OTHER O OTHER NRNOT REPORTED 1 GL11976JT LJ699 PILOT REPORTED A LOUD NOISE FROM THE CABIN DOOR FOLLOWED BY RAPID DEPRESSURIZATION. INSPECTION OF THE CABIN DOOR REVEALED A BROKEN CLEVIS PIN IN THE LINKAGE GOING TO THE FUEL UPPER LATCH HOOK. THE LATCH HOOK AND LINKAGE IN THIS AREA ARE ON A REPLACEMENT SCHEDULE REQUIRED FOR CONTINUED AIRWORTHINESS IN IAW MM CHAP 5-11-00 WHICH THIS PORT HAD NOT YET REACHED. 1L72 3T3 T 3A20 E4EA 6 CP40EA 20041001001152004100100115EU 2004 10 1 I7AL0002748 120040902A6420109013105115 TRUNNION AGUSTAA109 A109K2 0260502EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR OVERHEATED D I7LAK NONE O OTHER ININSP/MAINT 1 NM07901HC184 10033 UPON DAILY INSPECTION, MECHANIC FOUND ABNORMAL PLAY IN TAIL ROTOR ASSEMBLY. TRUNION- FURTHER INSPECTION FOUND SIGNS OF EXCESSIVE HEAT TO TRUNION ENAMEL PAINT DISCOLORED (BROWN). 1G72 3U3 URTH7EU E19EU 20041001001202004100100120GL 2004 10 1 R2J2004F00002 320040629A6114D3A32C90 HUB CESSNA206 U206F 2073333CE CONT O520 IO520* 17032SO MCAULY3A32C D3A32C90 GL PROPELLER CORRODED B R2JRO OTHER O OTHER NRNOT REPORTED 1 EA21841RQ2800 800 U20603273 766854 DURING STATEMENT OF CONDITION SURVEY FOUND PROPELLER HAD NOT BEEN OVERHAULED AT INTERNAL REQUIRED. WAS APPROX 2 YRS PART CALENDAR OVERHAUL REQUIREMENT SENT FOR OVERHAUL AND UPON TEARDOWN THE OVERHAUL SHOP SCRAPPED THE HUB DUE TO CORROSION AND BLADES DUE TO WEAR. NEW PROPELLER INSTALLED. THIS MODEL PROPELLER HAS NO LUBRICATION REQUIREMENTS OF MEANS. OH REQUIREMENTS ARE THERE FOR A REASON. PROP COULD HAVE FAILED. 1H71 3O3 O A4CE E5CE 5 CP21EA 20041001001282004100100128CE 2004 10 1 AIH2004F00000 120040907A32305141200201 UPLOCK HOOK CESSNA421 421C 2076016CE CONT O520 GTSIO520F 17032SO RT MAIN GEAR BROKEN B AIHRO OTHER O OTHER NRNOT REPORTED 1 GL111007G6500 421C0097 PILOT REPORTED LANDING GEAR WOULD NOT STAY RETRACTED. THE GEAR WOULD (SLAM) WHEN UP. THE LANDING GEAR EXTENDED PROPERLY AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERSONNEL JACKED UP THE AIR CRAFT AND DUPLICATED THE PROBLEM, INSPECTION REVEALED THE RT MAIN GEAR UPLOCK HOOK WAS BROKEN, ALLOWING THE UPLOCK SWITCH TO CLOSE WHICH CAUSED THE (SLAMMING). THE PART WAS REPLACED AND THE PROBLEM WAS FIXED, SUSPECT HIGH TIME CAUSED THE BREAK. THE NEW PART WAS MADE OF STEEL. THE OLD PART MADE OF ALUMINUM. (GL11200413886) 1L72 3O3 O A7CE E7CE 20041004000052004100400005NM 2004 10 4 USAA040523 120040812A5320 FLOOR SUPPORT BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 CLT - FOUND FLOOR SUPPORT CORRODED 1.5 INCH AREA BY .020 INCH DEEP, STATION 324-318 AND OBL, FLOORBEAM. REPAIRED PER SRM 51-10-02 AND DWG 141N5191. (M) 2L72 4F RTA2NM 20041004000082004100400008NM 2004 10 4 USAA040536 120040812A5347 SEAT TRACK BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 CLT - FOUND SEAT TRACK SECTION CORRODED 10 INCH SECTION, 1.5 INCH WIDE, RT OUTBOARD AFT SEAT TRACK, STATION 1635, RBL 45.5. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041004000092004100400009NM 2004 10 4 USAA040530 120040812A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY 1 INCH AREA, STATION 1661-1680 RBL 10. REPLACED UPPER CHORD PER SRM 53-60-51. (M) 2L72 4F RTA2NM 20041004000112004100400011NM 2004 10 4 USAA040558 120040908A5330 SKIN BOEING757 7572B7 1384964NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND SKIN DENTED 1 INCH BY 1 INCH BY .042 INCH DEEP, STATION 1620 STRINGER 19L. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 204. (M) 2L72 4F RTA2NM 20041004000132004100400013NM 2004 10 4 USAA040528 120040812A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED 2 INCH AREA, R1 DOORWAY, STATION 365-363. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-221-02, C53-222-03. (M) 2L72 4F RTA2NM 20041004000142004100400014NM 2004 10 4 USAA040550 120040806A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND UPPER T-CAP EMINATING FROM FASTENER HOLES, FS 345 AT RBL 58. CORROSION LEVEL 1 TASK NR C53-221-03, CR3-222-03. FABRICATED REPLACEMENT T-CAP AND INSTALLED PER EA 95747 AND SRM 51-20-07. (M) 2L72 4F RTA2NM 20041004000152004100400015NM 2004 10 4 USAA040526 120040812A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED 4 INCH AREA, STATION 340 LBL 29. DEFECTIVE PART REPLACED WTH IDENTICAL PART PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041004000162004100400016NM 2004 10 4 USAA040524 120040812A5320 SUPPORT FITTING BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND SUPPORT FITTING CORRODED 1 INCH BY .5 INCH AREA, STATION 365-375 RBL 12. REPLACED SUPPORT FITTING PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041004000172004100400017NM 2004 10 4 USAA040538 120040810A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH AREA, APPROX .025 INCH DEEP, FS 1640 FLOORBEAM RBL 60 AT SCREW HOLE. REMOVED DAMAGED AREA, REPLACED T-CAP PER EA 95735. (M) 2L72 4F RTA2NM 20041004000202004100400020NM 2004 10 4 USAA040563 120040910A5342 STRAP BOEING757 7572B7 1384964NM STABILIZER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND STABILIZER STRAP CRACKED .5 INCH, LOWER CHORD STATION 1280 RBL 24. REPAIRED PER SRM 53-10-51 FIG 202 DETAIL IV. (M) 2L72 4F RTA2NM 20041004000242004100400024EU 2004 10 4 ASOA04667 120040831A33502421658700000 MODULE AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT SHORTED A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11635AS 372 FLT 4258 - FOLLOWING TAKEOFF FROM ATL-DHN, THE FLIGHT ATTENDANT NOTICED SMOKE IN THE CABIN. THE PILOT VERIFIED WITH THE FILGHT ATTENDANT THAT NO FIRE WAS PRESENT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE FOUND A LOOSE WIRE SHORTING ON THE LIGHT SOCKET CLAMP OF THE PASSENGER SERVICE UNTI AT SEAT 13 A/B AND REMOVED AND REPLACED THE LIGHTING MODULE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20041004000272004100400027NM 2004 10 4 USAA040561 120040901A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US51571 23232 CLT - FOUND SKIN CRACKED 2.25 INCH LONG, FS 743 AT STRINGER 24L. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20041004000282004100400028NM 2004 10 4 USAA040562 120040806A5320 STRAP BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19356US45987 23559 PIT - FOUND STRAP CORRODED 65 INCHES BY 1.25 INCH AREA, AFT CARGO BIN, STRAP FROM BS 787-847. CORROSION LEVEL 1, TASK NR C53-202-01. REMOVED AND REPLACED STRAP, DRILLED AND REAMED AS REQUIRED PER BOEING DWG 65-47957. (M) 2L72 4F RTA16WE 20041004000312004100400031EU 2004 10 4 SIMA200425304 120040903A5330AL2024T3 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21347SB 340B347 ABI - DURING AN HMBV INSPECTION, THE CARGO RIGHT FRAME AT FS 677 FOUND A DENT 3 INCHES ABOVE THE FLOOR. RECONTOURED THE DENT AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007535, PARA 8 DATED AUGUST 31, 2004. (M) 2L72 4T RTA52EU 20041004000342004100400034EU 2004 10 4 USAA040566 120040909A5330 SKIN AIRBUSA319 A319112 3930323EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19762US11336 1358 PIT - FOUND SKIN DENTED 7 INCH BY 8 INCH BY .331 INCH, BETWEEN FRAME 3 AND 4, STRINGERS 22 AND 23 IN PITOT STATIC PORT RED BAND. TEMPORARY REPAIR, INSTALLED L ANGLES AND DOUBLERS PER EA 79115. (M) 2L72 4F RTA28NM 20041004000352004100400035NM 2004 10 4 USAABB04084 120040905A2750 CIRCUIT BREAKER BOEING767 7672B7 1385107NM TRANSFER BUSS TRIPPED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19651US 24764 SNN - FLT 71 - AFTER TAKEOFF, THE CREW COULD NOT RETRACT THE FLAPS. FLIGHT RETURNED TO SNN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE 115V RIGHT TRANSFER BUSS CIRCUIT BREAKER TRIPPED AND RESET IT. (M) 2L72 4F RTA1NM 20041004000372004100400037NM 2004 10 4 USAA040541 120040821A5410 PYLON BOEING757 757225 1384959NM RT ENGINE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU61650 22201 CLT - FOUND PYLON CORRODED THREE .5 INCHE HOLES, RIGHT ENGINE PYLON. INSTALLED FILLER PER EA 95777. (M) 2L72 4F RTA2NM 20041004000382004100400038NM 2004 10 4 USAA040540 120040817A5754 WEDGE BOEING757 757225 1384959NM NR 1 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU61650 22201 CLT - FOUND WEDGE ASSEMBLY DELAMINATED 2 INCH BY 2 INCH AREA, NR 1 SLAT T/E WEDGE AT OUTBOARD AUX TRACK. INSTALLED DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA2NM 20041004000402004100400040NM 2004 10 4 USAA040542 120040827A5320 STRAP BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19624AU35200 27245 CLT - FOUND STRAP CORRODED 2 INCHES LONG, STATION 1400 S-27L AT SKIN SPLICE. REMOVED DAMAGE AND INSTALLED REPAIR TRIPLER PER EA 95797. CORROSION LEVEL 1, TASK NR C53-155-02, C53-156-02. (M) 2L72 4F RTA2NM 20041004000412004100400041EA 2004 10 4 ASOA04668 120040831A5210601R3807413 FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING A C-CHECK IN MCN, THE AFT CABLE ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT CABLE ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20041004000472004100400047NM 2004 10 4 USAA040548 120040806A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOND FLOORBEAM HAS CORROSION EMINATING FROM FASTENER HOLES, STATION 365 AT RBL 60. INSTALLED FASTENERS PER SRM 51-40-02 AND EA 95736. (M) 2L72 4F RTA2NM 20041004000482004100400048NM 2004 10 4 USAA040543 120040819A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU61650 22201 CLT - FOUND FRAME WEB CRACKED .25 INCH, FROM LOWEST HOLE ON NR 6 STOP STRINGER 25R AT STATION 1380 FITTING. INSTALLED FRAME WEB SECTION PER EA 95755. (M) 2L72 4F RTA2NM 20041004000492004100400049EA 2004 10 4 ASOA04674 120040904A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11827AS 7212 DURING A GROUND INSPECTION IN DFW, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 AND NR 3 BATTERY CHARGER ASSEMBLIES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041004000502004100400050NM 2004 10 4 USAA040547 120040812A5315 FLOORBEAM BOEING757 7572B7 1384964NM FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU 27122 CLT - FOUND SUPPORT ANGLE CORRODED .5 INCH BY 1 INCH AREA, STATION 1663, LBL 56.5. REPAIRED PER SRM 51-10-2. (M) 2L72 4F RTA2NM 20041004000512004100400051NM 2004 10 4 USAA040525 120040903A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED 2 SPOTS, 1 INCH BY 2 INCH EACH, STATION 1661-1680 BL 0. REMOVED SURFACE CORROSION PER SRM 53-00-51. CORROSION LEVEL 1, TASK NR C53-251-03, C53-252-03. (M) 2L72 4F RTA2NM 20041004000542004100400054NM 2004 10 4 USAA040556 120040907A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US51571 23232 CLT - FOUND SKIN CRACKED 1.5 INCH LONG, FS 867 PLUS 2 STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2L72 4F RTA16WE 20041004000552004100400055EU 2004 10 4 ASOA04676 120040906A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11640AS 405 FLT 4517 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE TERMINAL OF THE EMERGENCY LIGHT SOCKET ON THE PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AND TERMINAL LUG P/N TA2206ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20041004000562004100400056EA 2004 10 4 ASOA04675 120040905A3350601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11827AS 7212 DURING AN A-CHECK IN BTR, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041004000612004100400061NM 2004 10 4 USAA040533 120040812A5730 SKIN BOEING757 7572B7 1384964NM WING WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND SKIN AND SPAR WEB WORN .360 INCH, .500 INCH, .225 INCH HOLES, FASTENER HOLES AT OUTBOARD FLAP TRACK FITTING. OVERSIZED HOLES AND INSTALLED FREEZE PLUGS PER EA 95714. (M) 2L72 4F RTA2NM 20041004000622004100400062NM 2004 10 4 USAA040532 120040812A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED .5 INCH BY .5 INCH AREA, STATION 310-324 LBL 19. REPLACED INTERCOSTAL PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041004000682004100400068CE 2004 10 4 DJX2004F00000 120040724A2720717 SOLENOID BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA RUDDER INOPERATIVE D DJXAO OTHER O OTHER NRNOT REPORTED 1 GL23946CE1185 BB1728 DURING A RUDDER BOOST TEST THE RT RUDDER PEDAL, REMAINED AT FULL DEFLECTION EVEN WITH THE ENGINES AT IDLE. BY TURNING THE SYSTEM OFF BOTH PDEALS WOULD RETURN TO CENTER. IF THE SYSTEM FAILED ON FINAL AND OR DURING TAKE OFF THE END RESULT COULD BE DEVASTATING. 1L72 4T3 T A24CE E2NE 20041004000702004100400070WP 2004 10 4 Z3M2004F00001 120040628A2420ALX8521 ALTERNATOR ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA ENGINE FAULTY E Z3MAO OTHER O OTHER NRNOT REPORTED 1 CE037036J83 0583 L2538142A ALTERNATOR FAILED WITHOUT ANY PREVIOUS INDICATIONS. REPLACED ALTERNATOR. 1G71 3O3 O H11NM E295 20041004000732004100400073SW 2004 10 4 HJL2004F00001 120040909A32332032071 SPRING MOONEYM20 M20R 5870225SW CONT O550 IO550* SO MLG ACTUATOR FAILED E HJLAO OTHER O OTHER NRNOT REPORTED 1 SW17326TJ16 244 290043 REPLACED (NO BACK) SPRING, INSP GEARS AND ACTUATOR IAW SB M20-282 AND SI 102000-1-901 REV 2. ON 9-3-2004, AFTER 16 HOURS, GEAR DOWN SAFETY LIGHT WOULD INDICATE UNSAFE CONDITION WHEN TAXIING AC AND TURNING RT AND LT. AC WAS PUT ON JACKS, GEAR WAS ELECTRICALLY EXTENDED, WHILE LIGHTLY PULLING DOWN ON EITHER IB MLG DOOR, MLG ACTUATOR WAS OBSERVED TO BACK OFF FROM DOWN POSITION. DISCOVERED WHILE PERFORMING A NORMAL RETRACT TEST. FOUND DOWNLOCK PRELOAD TO BE LOW INITALLY, BUT WAS WITHIN LIMITS AFTER GEAR RETRACTION CYCLE INDICATING GEAR GRADUALLY (BACKS OFF) AFTER SITTING PERIOD OF TIME. NOTE: MEASURED METAL THICKNESS OF SPRINGS, .066 NEW SPRING, .067 OLD SPRING, HSG SPRING SITS IN INDICATES .002 WEAR. 1L71 3O3 ORT2A3 E3SO 20041004000752004100400075EA 2004 10 4 GW12004F00003 220040702A73103032791 LINE PIPER PA42 PA42720 7104212SO PWA PT6 PT6A61 52043EA FUEL CONTROL FRACTURED B GW1RO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA03121LH3788 1407 425501049 PCE99121 PILOT REPORTED FUEL DRIPPING OUT OF COWLING ON SHUT DOWN. REMOVAL OF COWLING AND GROUND RUN OF ENGINE REVEALED FRACTURE OF HIGH PRESSURE FCU TO FUEL NOZZLE DELIVERY TUBE. TUBE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T4 T A23SO E4EA 20041004000802004100400080CE 2004 10 4 VJT2004F00000 120040830A793099121641 TRANSDUCER CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE RT ENGINE BROKEN E VJTAO OTHER O OTHER NRNOT REPORTED 1 EA0392B 6778 5500471 PCE71343 DURING GROUND MAINTENANCE RUN, RT OIL PRESSURE INPUT TO ZERO AND FLAGGED OFF. INSPECTION REVEALED END BROKE OFF TRANSDUCER AT CONNECTOR PLUG. REPLACED TRANSDUCER. OPERATIONAL AND LEAK TEST, SATISFACTORY. 1L72 4F4 F A22CE E1NE 20041004000832004100400083 2004 10 4 FGQ2004F00001 420040823A25615045164018088 INERTIA REEL CESSNA182 182T 2072703CE RESTRAINT CRACKED B FGQRO OTHER O OTHER NRNOT REPORTED 1 SO0135188606 18280999 ENERTIAL REEL FOR SHOULDER HARNESS MOUNT STRIPS CRACKED THROUGH TAPPED HOLES. 1H71 3O NT3A13 20041004000852004100400085EA 2004 10 4 UC22004F00001 220040819A853015F1995735 PUSHROD PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA NR 4 CYLINDER BENT B UC2RO OTHER O OTHER NRNOT REPORTED 1 GL194145A1882 2843150 WHILE PERFORMING SB388B THE NR 4 EXHAUST VALVE PUSHROD WAS FOUND BENT. THE NR 4 CYLINDER EXHAUST VALVE MUST HAVE STUCK AT SOME POINT CAUSING THE PUSHROD TO BEND. THIS MAY HAVE OCCURRED BECAUSE OF IMPROPER LEANING PROCEDURES DURING A CROSS COUNTRY FLIGHT OR POSSIBLY EXCESSIVE GROUND RUNNING. 1L71 3O3 O 2A13 E286 20041004000902004100400090SO 2004 10 4 GNB2004F00001 220040728A74141081806 BEARING CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MAGNETO DESTROYED E GNBAO OTHER O OTHER NRNOT REPORTED 1 SW01402SA499 E021A176R 402C0623 823470R DURING THE FIRST INITIAL 500 HOUR MAGNETO INSPECTION ON A FACTORY ENGINE. MAINTENANCE DISCOVERED AN ODD LOOKING LUBE ON BOTH MAGNETOS AND INSUFFICIENT AMOUNT IN WELL. THE LT MAGNETO BEARING LOOKED OK, HOWEVER, THE RT MAGNETO BEARING WAS UNUSABLE AND METAL TRANSFER WAS APPARENT. LUBRICANT TYPE, AND/OR LACK THEREOF, APPEARED TO BE THE CAUSE. PARTS BEING SENT TO MFG FOR EVALUATION. 1L72 3O3 O A7CE E8CE 20041004000952004100400095CE 2004 10 4 GNB2004F00000 120040825A2910S20010777 LINE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO HYD SYSTEM CRACKED E GNBAO OTHER K FLUID LOSS NRNOT REPORTED 1 SW0126156 402C0112 PILOT PRE-FLIGHT, HYDRAULIC RESERVOIR LOW. MAINTENANCE PRESSURE CHECKED SYSTEM, FOUND NR 6 PRESSURE LINE CRACKED AT BEND RADIUS. 1L72 3O3 O A7CE E8CE 20041004000982004100400098 2004 10 4 UIEA200400119 420040628A3440 INDICATOR BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE HSI MALFUNCTIONED A UIEAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 EA15522MC 21783 DURING CLIMB, WHEN CLEARED INS WAYPOINT AND SELECTING INS MDU, CDI ON C/A AND F/O HSI WOULD NOT CENTER X WHEN CLEARED VOR AND SELECTING ON INS MDU, HSI SHOWED ABOUT 30 DEGREE DIFFERENCE IN UPDATE. EXCESSIVE DIFFERENCE IN DRIFT ON ARRIVAL . 23400 FUEL DUMPED. AC RETURNED. INS CHECKED OUT IAW 34-41-00. HSI/ADI INTERFACE CHECKED ALL INDICATION IS NORMAL W/OUT REMARKS. 2L74 4F4 FRTA20WE E23EA 20041004001002004100400100EA 2004 10 4 WVB2004F00001 220040527A8500 UNKNOWN PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA UNKNOWN UNKNOWN E WVBAO OTHER O OTHER NRNOT REPORTED 1 AL014082T 318152089 L160968A ON 5/25/04, WHILE RETURNING, THE PILOT NOTICED AN INTERMITTENT LOSS IN MANIFOLD PRESSURE ON THE RT ENGINE. A GRADUAL LOSS OF OIL PRESSURE BEGAN TO DEVELOP SO THE PILOT SHUT DOWN THE ENGINE AS A PRECAUTIONARY MEASURE AND CONTINUED ON COURSE TO FAI. AIRPLANE LANDED WITHOUT PROBLEMS. MAINT THOROUGHLY INSPECTED THE ENGINE AND FOUND NO MAJOR DEFECTS. OIL WAS ADDED TO BRING THE LEVEL FROM FOUR TO ELEVEN QUARTS AND OPERATIONAL CHECK FLIGHT WAS CONDUCTED TO SEE IF THE PROBLEM PERSISTED. AFTER THE CHECK FLIGHT, THE OIL FILTER WAS REINSPECTED AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 3O3 O A20SO E14EA 20041004001042004100400104SO 2004 10 4 HPF2004F00001 120040728A2170552203 MOTOR PIPER PA46 PA46500TP 7104622SO PWA PT6 PT6* 52043EA EVAPORATOR FAILED B HPFRO OTHER O OTHER NRNOT REPORTED 1 WP093096P203 4697178 MOTOR MOUNT STUDS PULLED OUT ENABLING FAN TO JAM. MOTOR OVERHEATED AND PRODUCED ELECTRICAL SMOKE IN CABIN. CIRCUIT BREAKER FINALLY POPPED. PROBABLE CAUSE WAS EITHER OVERTORQUE OF MOTOR ATTACH NUTS OR DEFECTIVE CASE ON EVAPORATOR ASSEMBLY. THIS WAS AN ORIGINAL INSTALLATION NO PREVIOUS WORK HAS BEEN DONE ON THIS SYSTEM. 1L71 3O3 TRTA25SO E2NE 20041004001092004100400109SO 2004 10 4 2004F00388 120040920A6120 PROPELLER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE MALFUNCTIONED E GNOAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO15267AS 120198 20001112 UPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO LAND THE AIRCRAFT SGF FOR FUTHER INVESTIGATION, FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIP WAS CANCELLED, IT WAS A REPOSITIONING FLIGHT FROM LNC TO CRG. THE CAUSE IS STILL UNKNOWN AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20041004001122004100400112NM 2004 10 4 04FDEA02530 120040819A5330 SKIN BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 AFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360 2L73 4F4 FRTA3WE E2EA 20041004001142004100400114NM 2004 10 4 04FDEA02687 120040916A7830683L220G04 TRACK DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 ENGINE NR 3 LT T/R COWL UPPER SLIDER TRACK END FOUND WITH CRACK. REMOVED AND REPLACED AS PER AMM 78-33-01-4 AND REPAIR CARRIED OUT, PLS REFER TO FAA 8130-3 FORM TRACKING NR 5480 FOR FURTHER WORK DETAILS AND INSTALLED AS PER AMM 78-33-01-04 AND FUNCTIONAL TEST CARRIED AS PER AMM 78-30-00, FOUND SATIS. 2L73 4F4 FRTA22WE E31N3 20041004001152004100400115NM 2004 10 4 04FDEA02688 120040916A7830683L221G04 TRACK DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE TRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 ENGINE NR 2, RT, T/R COWL AT UPPER SLIDER TRACK END FOUND WITH CRACK. T/R COWL REMOVED AS PER AMM 78-33-01-4. REPAIR CARRIED OUT, REFER TO FAA 8130-3, FORM TRACKING NO. 5479 RIGHT HAND THRUST REVERSER COWL RE-INSTALLED AS PER AMM 78-33-01-4. ADJUSTMENT AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 78-30-00, FOUND SATIS. 2L73 4F4 FRTA22WE E31N3 20040930000342004093000034EU 2004 9 30 ASOA04628 120040802A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE NR 3 AND 4 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAPS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 3/4 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000372004093000037EU 2004 9 30 ASOA04623 120040802A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FS 36/38 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FS 36/38 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20040930000502004093000050EU 2004 9 30 USAABA04019 120040822A335032146210 POWER SUPPLY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 0342 PHL - DURING THE MCDU TEST, EPSU 3L WAS DISPLAYED. MAINTENANCE REPLACED THE EPSU AND BATTERY ASSEMBLY AT THE 3L DOOR. (M) 2L72 4F RTA46NM 20040930000522004093000052EU 2004 9 30 ASOA04630 120040802A5753 GUIDE AEROSPATR72 ATR72212 8680945EU TE FLAPS CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11530AS 453 DURING A C-CHECK IN YUL, THE NR 5 AND 6 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP AS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 5 AND 6 CAM GUIDES OUTBOARD ON THE LEFT INBOARD FLAP IAW AMM 20-21-12. (M) 2H72 4T RTA53EU 20040930000532004093000053NM 2004 9 30 USAASB04116 120040831A33503114981 REFLECTOR BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19391US 23313 MAINTENANCE REPORTED THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20040930000552004093000055SO 2004 9 30 SIMA200425311 120040903A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BEYOND LIMITS. REMOVED DAMGAED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-40-02. (M) 2L72 4F RTT00011AT 20040930000562004093000056SO 2004 9 30 SIMA200424702 120040826A532014522459003 CHANNEL EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21828AE 145604 SAW - DURNG CPCP INSPECTION, MAINTENANCE FOUND HAT BEAM CORRODED BETWEEN FRAMES 19 AND 20. HAT BEAM REPLACED IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20040930000682004093000068EU 2004 9 30 2004F00400 120040712A2120 ODOR AEROSPATR72 ATR72212 8680945EU COCKPIT DETECTED A SIMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO21377AT 377 ELECTRICAL HEAT AND SMELL COMING FROM THE CIRCUIT BREAKER PANEL BEHIND F/O SEAT. VISUALLY INSPECTED CIRCUIT BREAKER PANELS, WIRING AND CONTACTORS AND OFUND NO EVIDENCE OF ELECTRICAL DAMAGE. (M) 2H72 4T RTA53EU 20040930000752004093000075EA 2004 9 30 ASOA04615 120040821A5210CLREF2177 STRUT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LEAKING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 FLT 4619 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND HARD TO OPEN. MAINTENANCE REMOVED AND REPLACED THE AFT GAS STRUT AND ADJUSTED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930000782004093000078EA 2004 9 30 ASOA04645 120040825A5712 RIB CNDAIRCL600 CL6002B19 1900309EA WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20040930000942004093000094NM 2004 9 30 C7WA200400019 120040609A5730 SKIN BOEING727 727232 1384082NM CENTER WING CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO17511PE 20634 FOUND WING CENTER SECTION UPPER SKIN CORRODED RBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M) 2L73 4F A3WE 20040930000972004093000097EA 2004 9 30 ASOA04640 120040823A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11867AS 7463 FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040930001032004093000103EA 2004 9 30 ASOA04649 120040826A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11916EV 7757 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040930001042004093000104NM 2004 9 30 USAASB04117 120040902A27512061141 INDICATOR BOEING737 7373B7 1384580NM TE FLAP MALFUNCTIONED A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19376US55373 22955 BOS - FLT 2022 - ON APPROACH TO BOS, FROM DCA, THE RIGHT FLAP LAGGED BEHIND THE LEFT FLAP TO THE POINT WHERE SELECTING FLAPS TO 25 UNITS, FLAPS ASSYMETRY PROTECTION TOOK PLACE. CREW ACCOMPLISHED A GO AROUND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACD THE FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD PER MM 27-58-01. CYCLED FLAPS UP AND DOWN THROUGH FULL TRAVEL SEVERAL TIMES. NO FLAP SPLIT NOTED ON GROUND. VISUAL INSPECTION OF FLAPS REVEALS NO PROBLEMS. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA16WE 20040930001052004093000105 2004 9 30 USAASB04112 420040818A3400 STATIC LINE BOEING737 7373B7 1384580NM E/E COMPT LOOSE A USAAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 EA19374US 22953 PHL - FLT 477 - EN ROUTE FROM PHL-RDU, CREW REPORTED THE FIRST OFFICER ALTIMETER, AIRSPEED AND VSI WENT INOPERATIVE. CREW ALSO REPORTED THAT ON TAKEOFF ROLL, THE AUTO THROTTLES DISENGAGED AND THE N1 BUGS SLOWED TO ZERO. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESECURED THE QUICK DISCONNECT PITOT STATIC LINES OT THE NR 2 AIR DATA COMPUTER. OPERATIONAL CHECK GOOD PER MM 34-12-00. (M) 2L72 4F RTA16WE 20040930001372004093000137NM 2004 9 30 SWAA042804 120040927A53126546568 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP LAP SPLICE AT BS 1016, STRINGER 23R, CRACKED. REPAIRED BULKHEAD PER ER. 2L72 4F RTA16WE 20040930001512004093000151WP 2004 9 30 ABXA040329 120040811A533057503223 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23814AX 46041 AFT CARGO LONGERON 36, BLEEDING CORROSION FROM BOTH SIDES FROM STA 1080 - 1120. REPAIRED AREA IAW REA D853-49986MR. 2L74 4F 4A25 20040930001582004093000158WP 2004 9 30 ABXA040324 120040903A551159225802 SPAR CAP DOUG DC9 DC931 3022065WP RT HORZ STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23923AX 47165 RIGHT HORIZONTAL STABILIZER FORWARD LOWER OUTBOARD SPAR CAP CRACKED APPROXIMATELY 3.25 INCHES. REPAIRED LOWER OUTBOARD SPAR CAP IAW REA D955-50424MR. 2L72 4F A6WE 20040930001672004093000167WP 2004 9 30 ABXA040312 120040820A5310 SKIN DOUG DC8 DC863 302198AWP TORQUE BOX CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23817AX 45928 LEFT WHEEL WELL AFT TORQUE BOX LOWER SKIN, STA 980, INSIDE TORQUE WELL, CORRODED. REPAIRED AREA IAW REA D853-50008MR, REV A. 2L74 4F 4A25 20040930001682004093000168NM 2004 9 30 P5CA0401200 120040914A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LEFT WING UPPER SKIN 24 INCHES FWD OF SPAN WISE BEAM NR 2 HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20040930001702004093000170NM 2004 9 30 P5CA0401202 120040914A5347 SEAT TRACK BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 CABIN LEFT SEAT TRACK HAS CORROSION SPOTS. REMOVED CORROSION .020 MATERIAL WITHIN LIMITS. 2L74 4F4 F A20WE E20EA 20040930001742004093000174WP 2004 9 30 ABXA040333 120040927A7797 WIRE DOUG DC8 DC863F 302198FWP NR 3 ENGINE FRAYED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 DURING LINE MAINTENANCE, FOUND NR 3 ENGINE EPR WIRING HARNESS CHARRED AND FRAYED DUE TO PREVIOUS PNEUMATIC LEAK. REPLACED NR 3 ENGINE EPR WIRES 7E57SA24N AND 3E573A24N BETWEEN CONNECTOR P1-1449 AND GROUND 825. 2L74 4F 4A25 20040930001782004093000178NM 2004 9 30 P5CA0401206 120040914A5314 KEELBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 KEEL BEAM APPROX STA 1093 HAS BOTTOM SURFACE CORROSION. REMOVED CORROSION, AFTER WORK IT IS 0.061, OK PER SRM 52-10-01. 2L74 4F4 F A20WE E20EA 20040930001832004093000183WP 2004 9 30 ABXA040327 120040915A3097 WIRE DOUG DC9 DC932F 3022067WP ICE SENSOR BROKEN A ABXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23905AX 47147 IN CLIMB, BOTH MASTER CAUTIONS ILLUMINATED, DIVERTED TO SGF. INSTALLED NEW LEFT THERMAL CONTROL AMPLIFIER, BITE TEST SHOWED PROBLEM IN SENSOR ON CIRCUIT. FOUND WIRES ON LEFT ICE PROTECT TEMP HIGH SENSOR BROKEN, SPLICED WIRES IAW DC-9 MM 20-50-1. OPS CHECKED GOOD. 2L72 4F A6WE 20040930001842004093000184NM 2004 9 30 HNAA0400123 120040924A215078279810 ACM DHAV DHC8 DHC8102 2809003NM CABIN COOLING FAULTY A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07805EX129362773 228 FLIGHT 3942 REPORTED SMOKE IN THE CABIN WITH THE APU RUNNING AND AN ASSOCIATED VIBRATION WAS FELT. APU WAS SHUTDOWN. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. SYSTEM OPERATIONAL CHECKS WERE COMPLIED WITH. ALL CHECKS GOOD. 2H72 4T RTA13NM 20040930001852004093000185WP 2004 9 30 ABXA040318 120040821A531059568791 DOOR FRAME DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23928AX 47392 CRACKED MAIN ENTRY DOOR FRAME WEB AT STA 207. REPAIRED WEB IAW DC-9 SRM 51-70-4. 2L72 4F A6WE 20040930001902004093000190NM 2004 9 30 SWAA042780 120040924A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 875 TO BS 887, STRINGER 4L TO STRINGER 4R, WORN. REPAIRED SKIN PER ACO AND EA. 2L72 4F RTA16WE 20040930001912004093000191 2004 9 30 SWAA042781 420040924A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041001000052004100100005NM 2004 10 1 EIA2004082 120040902A5315 FLOORBEAM BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 MAIN DECK FLOOR BS 460 LBL 65 FLOORBEAM WEB CRACKED AT UPPER EDGE. REMOVED AND REPLACED STA 460 FLOORBEAM WEB IAW SRM 53-10-07 FIG 11 AND 51-30-02. 2L74 4F4 FRTA20WE E20EA 20041001000102004100100010NM 2004 10 1 UPS04M43194 120040822A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C HORZ STAB NR 34 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT B/N HOLE NR 34 RT REMOVED, BLENDED AND REAMED TO 1.162 INCHES FOUND OUT OF LIMIT. FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 34 RT IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 34 RT IAW EO MD 11-5510-19409-H AND EN:1307-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041001000152004100100015CE 2004 10 1 64691 120040908A3110 ANNUNCIATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE INSTRUMENT PANELMALFUNCTIONED A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE07142ZV UE142 IN FLIGHT, CREW NOTICED SEVERAL ANNUNC ILLUM AND EXTINGUISHED WITH AN ELECTRICAL SMELL IN COCKPIT. ON LANDING THE RT PROP WENT INTO FEATHER. A/C LANDED WITHOUT FURTHER INCIDENT. NO FUMES NOTED INS CB PANELS, INSTRUMENT PANEL. 2L72 4T4 TRTA24CE E26NE 20041001000212004100100021WP 2004 10 1 WX0400036 120040924A3350 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE EMERGENCY LIGHT INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19864GA 49912 MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS, ROW 31 TO 35 AND EMERGENCY POWER OVERHEAD LIGHTS, ROW 25, 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK IAW 33-53-00. LIGHTS ROW 31 TO 35 OPERATIONALLY CHECK GOOD. MAINTENANCE REPLACED BULBS AT ROWS 25, 29 AND 33 LIGHTS OPERATIONALLY CHECKED GOOD IAW 33-53-00. AIRCRAFT RETURNED TO SERVICE 2L72 4F4 F A6WE E2EA 20041001000312004100100031EA 2004 10 1 QXEA200400686 120040922A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 UPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL, IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CRACKED AT TWO PLACES. REPAIRED IAW EA R-53-205 AND REO 670-53-11-042 AND REO 670-53-11-043. 2L72 4F4 FRTA21EA EOOO63EN 20041001000602004100100060NM 2004 10 1 P5CA0401228 120040922A2420 GCU BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 1 MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23454PA 30812 AFTER SWITCHING FROM APU TO SHIPS POWER RECEIVED EICAS MSG (ELEC GEN OFF 1), (ELEC GEN OFF 2), (ELEC GEN OFF 3). SWAPPED NR 1 AND NR 2 GCU, RECYCLED C/B'S, ENGINE START NORMAL IAW AMM 71-00-00. 2L74 4F4 FRTA20WE E23EA 20041004000032004100400003NM 2004 10 4 USAASB04119 120040907A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19516AU 23702 PIT - MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN FORWARD GALLEY OVERHEAD, HAS LOW CHARGE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20041004000122004100400012NM 2004 10 4 USAA040557 120040908A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND INTERCOSTAL CORRODED 1 INCH AREA, STATION 345 LBL 20. REPLACED WITH IDENTICAL PART PER SRM 51-10-02, 53-10-51, 53-00-51. (M) 2L72 4F RTA2NM 20041004000182004100400018NM 2004 10 4 USAA040537 120040803A5320 PAN BOEING757 7572B7 1384964NM GALLEY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19612AU39393 27124 CLT - FOUND AFT GALLEY FLOOR PAN CORRODED .5 INCH BY .5 INCH, FLOOR SURFACE FROM RBL 51 TO LBL 51, STATION 1720. FABRICATED REPAIR PAN PART AND INSTALLED WITH FILLER AND DOUBLER PER SRM 53-60-51 FIG 203. (M) 2L72 4F RTA2NM 20041004000212004100400021EA 2004 10 4 ASOA04670 120040901A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11821AS 7194 DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SREVICE. (M) 2L72 4F RTA21EA 20041004000332004100400033EA 2004 10 4 ASOA04673 120040829A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-74-00. (M) 2L72 4F RTA21EA 20041004000432004100400043EA 2004 10 4 ASOA04666 120040831A33506100976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11703EV 10038 FLT 4509 - DURING A GROUND INSPECTION IN DFW, AN EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041004000632004100400063NM 2004 10 4 USAA040531 120040812A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERRCOSTAL CORRODED 18 INCHES BY 3 INCH AREA, STATION 377-395 RBL 12. REPAIRED PER BOEING DWG 141N5150. 2L72 4F RTA2NM 20041004000652004100400065EU 2004 10 4 I7LA0002746 120040905A6420109013105115 TRUNNION AGUSTAA109 A109K2 0260502EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR OVERHEATED D I7LAO OTHER O OTHER NRNOT REPORTED 1 NM07901HC6 10033 SEPT 5, 2004. AIRCRAFT TT: 3518.7 UPON 25 HOUR INSPECTION, TAIL ROTOR TRUNION ENAMEL PAINT DISCOLORED. SIGNS OF EXCESSIVE HEAT. 1G72 3U3 URTH7EU E19EU 20041004001032004100400103SO 2004 10 4 FGQ2004F00002 120040823A281039824803 FUEL CAP PIPER PA34 PA34220T 7103420SO FUEL TANK CRACKED B FGQRO OTHER O OTHER NRNOT REPORTED 1 SO0169BP 1107 3449085 BOTH FUEL CAPS PN 39824-803 FOUND CRACKED AT LATCH PIVOT WHERE ROLL PIN RETAINS LATCH LEVER TO CAP BODY. 1L72 3O A7SO 20041004001062004100400106 2004 10 4 MALA040537 420040821A2210 COMPUTER BAC 146 AVRO146RJ85A1500097EU COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15522XJ E2347 AFTER TAKEOFF TRP FAILED, UNABLE TO RESET. SUBSEQUENTLY, FTC ELTRIM YD STALL IDNTZ FGC1 YD1 NO CAT 3 ALL ILLUMINATED. A/P AND A/T FAILED. AIR RETURN TO DTW. MAINTENANCE REVEIWED AND CLEARED FAULTS. PERFORMED HARD RESET AND RTS ON DFGC, Y/D, TRIM SYSTEM, TRP, THRUST CNTRL SYS ALL CHECKS GOOD. 2H74 4F RTA49EU 20041004001072004100400107 2004 10 4 WLDA200435 420040806A3457 GPS DOUG DC10 DC1030 3023501WP COCKPIT MALFUNCTIONED A WRLAA UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 SO11351 46922 IRN/INN AIR TURNBACK DUE TO GPS SYSTEM UNRELIABLE AFTER TAKEOFF, MULTIPLE FAULTY INDICATIONS. INTERROGATED MCDU'S AND GPS SYSTEMS, PRECAUTIONARY SHUTDOWN ALL NAV SYSTEMS AND AIRCRAFT POWER. CHECKED VISUALLY PITOT TUBES AND STATIC SENSORS FOR DEBRIS/BLOCKAGE, FOUND ALL CLEAR. POWERED UP AIRCRAFT AND NAVIGATION/GPS SYSTEM, BITE CHECKED OPS NORMAL ON GROUND. BITE CHECKED PITCH & ROLL COMPUTERS ELF LOAD FEEL, ALL OK. UPDATED FLIGHT PLAN DATA, CROSS CHECKED ALL INDICATIONS AND DATA VERIFIED CORRECT ON GROUND. 2L73 4F A22WE 20041004001082004100400108SO 2004 10 4 2004F00387 120040920A6120 PROPELLER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE MALFUNCTIONED E GNOAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO15267AS 120198 20001112 UPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO LAND THE AIRCRAFT SGF FOR FUTHER INVESTIGATION. FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIP WAS CANCELLED, IT WAS A REPOSITIONING FLIGHT FROM LNC TO CRG. THE CAUSE IS STILL UNKNOWN AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20041004001112004100400111 2004 10 4 249TR0037 420040821A2230 SWITCH BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE THROT DISENGAGE MALFUNCTIONED A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05249TR 22598 AUTO THROTTLES WOULD NOT ARM. PLACED AUTO THROTTLE ON MEL 22-4. REPLACED LEFT AUTO THROTTLE DISENGAGE SWITCH AND CHECKED NORMAL PER MM 22-31-0. 2L72 4F4 FRTA16WE E2EA 20041004001182004100400118NM 2004 10 4 04FDEA02396 120040809A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, OB AFT HINGE PIVOT HOLE OB FLANGE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD FLANGE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.503, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.499. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001222004100400122NM 2004 10 4 04FDEA02400 120040809A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.406. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001232004100400123EU 2004 10 4 ASOA04467 120040629A33503011162 COVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27634AS 370 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT COVER AT THE BOTTOM OF THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT COVER AT THE BOTTOM OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041004001242004100400124EA 2004 10 4 ASOA04482 120040704A5210601R3198045 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041004001252004100400125EU 2004 10 4 AALA20040808 120040804A2822 PUMP AIRBUS300 A300B4605R 3930308EU GE CF6 CF680 30025NE CENTER FUEL TANKINOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2170079 619 ENROUTE, AIR INTERRUPTED ON ACCOUNT OF FUEL FEED PROBLEMS. LANDED WITHOUT INCIDENT. TROUBLESHOOTING IN PROGRESS. --OPEN-- 2L72 4F4 FRTA35EU E13NE 20041004001262004100400126NM 2004 10 4 04FDEA02442 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 DENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041004001272004100400127NM 2004 10 4 04FDEA02443 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 DENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041004001282004100400128NM 2004 10 4 04FDEA02444 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 DENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041004001292004100400129NM 2004 10 4 04FDEA02445 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 DENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1 2L73 4F4 FRTA3WE E2EA 20041004001302004100400130NM 2004 10 4 04FDEA02446 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 DENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041004001312004100400131NM 2004 10 4 04FDEA02012 120040707A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.504; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.502 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001322004100400132NM 2004 10 4 04FDEA02013 120040707A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LT WING OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER:1.093; FINAL DIAMETER: 1.096 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001352004100400135NM 2004 10 4 2004UALA00736 120040806A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 EXTERNAL FUSELAGE SKIN HAS 2 LIGHTNING STRIKES JUST BELOW FWD CARGO DOOR STA 582 AND 529 AT STR 27R, DEPTH WAS MEASURED TO BE .100. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041004001362004100400136NM 2004 10 4 2004UALA00737 120040806A3350 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE ROW 16 ABC DISCONNECTED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29596UA 28749 EMERGENCY EXIT LIGHT INOP ABOVE SEAT 16ABC. FOUND DISCONNECTED CONNECTOR UNDER OVERHEAD SEALING PANEL. RECONNECTED. 2L72 4F4 FRTA2NM E17NE 20041004001372004100400137NM 2004 10 4 2004UALA00738 120040811A1420BACC45FN105S CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCONNECTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 EXIT INDICATOR LIGHTS AT DOORS 4L AND 4R INOPERATIVE. FOUND CONNECTORS D6634 AND D6674 DISCONNECTED FROM INVERTER M10834. RECONNECTED WIRING. SYSTEM OPERATES NORMALLY. 2L72 4F4 FRTA2NM E17NE 20041004001382004100400138NM 2004 10 4 2004UALA00749 120040723A3350BPS73 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INTERMITTENT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29122UA 29168 EVACUATION PATH LIGHTING AT RIGHT SIDE OF D-ZONE COMES ON AND OFF AT INTER. REPLACED BATTERY ABOVE DOOR 3R. 2L74 4F4 FRTA20WE E24NE 20041004001412004100400141NM 2004 10 4 2004UALA00761 120040731A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 CABIN OVERWING FRAME BODY STA 616L CRACKED AT BOTTOM FASTENER BELOW FLOOR LEVEL. REMOVED CRACKED AREA, FABRICATED AND INSTALLED ANGLE. 2L72 4F4 FRTA16WE E2GL 20041004001432004100400143NM 2004 10 4 2004UALA00763 120040802A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 FUSELAGE SKIN IS DENTED AT STA 357, 3 INCHES BELOW STR 20R AND NEXT TO A BUTT JOINT. INSTALLED DOUBLER AND TRIPLER. 2L72 4F4 FRTA16WE E2GL 20041004001482004100400148NM 2004 10 4 AWXA200400710 120040701A27512061141 INDICATOR BOEING737 737301 1384611NM FLAPS DEFECTIVE A AWXAO OTHER N FALSE WARNING APAPPROACH 1 WP28325AW16380513 23260 SNA - EMERGENCY LANDING - FLT 0653 - ON DESCENT INTO PHX EN ROUTE FROM SNA AIRCRAFT EXPERIENCED A FLAP LOCKOUT AND WOULD NOT EXTEND WHEN SELECTING FLAPS 1. MAINTENANCE REMOVED AND REPLACE FLAP POSITION INDICATOR PER T/C R1B27001. PERFORMED TRAILING EDGE FLAP BYPASS VALVE OPERATIONAL CHECK IAW F1B27013. OPERATIONAL CHECKS WERE GOOD. VENDORS PRETEST OF FLAP POSITION INDICATOR S/N 522 CONFIRMED REASON FOR REMOVAL, UNIT FAILED FOR TRANSMITTER POSITION DISAGREE ON R/H POSITION TRANSMITTER DIAL, ALSO FOUND LIGHTS INOPERATIVE. DISASSEMBLY OF UNIT FOUND R/H SYNCHRO OUT OF ADJUSTMENT AND LAMPS DS1, AND DS3 BURNT OUT. ADJUSTED SYNCHRO AND REPLACED BURNT LAMPS, FUNCTIONAL CHECK C/W IAW OEM 27-50-07, REV. 5. 2L72 4F RTA16WE 20041004001522004100400152SO 2004 10 4 CHQA000529 120040729A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11286 145443 EMERGENCY LIGHTING INOP. FOUND QUICK DISCONNECT ON SEAT 7A DISCONNECTED FROM WIRING. INSTALLED NED QUICK DISCONNECT IAW WM 20-50-01. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041005000012004100500001 2004 10 5 P9RA20040030 420040808A2565767 BULB BOEING757 757231 1384950NM R4 SLIDE BURNED OUT A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO11715TW 28483 AIRCRAFT IN MAINTENANCE, SAT R4 DOOR SLIDE (ARMED) LIGHT FAILED TO ILLUMINATE.RELAMPED SOCKET. LIGHT WORKS NORMAL IAW MM 331100. 2L72 4F RTA2NM 20041005000022004100500002NM 2004 10 5 04FDEA02447 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 STRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041005000032004100500003NM 2004 10 5 04FDEA02449 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 STRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041005000042004100500004NM 2004 10 5 04FDEA02450 120040811A5313 STRINGER BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 STRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358 2L73 4F4 FRTA3WE E2EA 20041005000082004100500008NM 2004 10 5 04FDEA02373 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041005000112004100500011NM 2004 10 5 04FDEA02376 120040805A5710ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.004 REMAINING THICKNESS = 0.498. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20041005000132004100500013NM 2004 10 5 04FDEA02378 120040805A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH PIVOT IB HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.015. REMAINING THICKNESS = 0.487. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041005000162004100500016NM 2004 10 5 04FDEA02381 120040805A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING OB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.203. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041007000112004100700011 2004 10 7 SWAA042865 420041003A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000132004100700013NM 2004 10 7 SWAA042867 120041003A53116520723 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20041007000282004100700028WP 2004 10 7 AALA20041018 120041001A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213515 49892 RDU - EMERGENCY LIGHTS ABOVE AFT STAIRS INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR EMERGENCY LIGHTS ABOVE AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000302004100700030NM 2004 10 7 AALA20041022 120041001A3350D71702001 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21665AA 25299 MIA - EMERGENCY LIGHT BY RIGHT AFT LAVATORY INOPERATIVE. FOUND WIRE DISCONNECTED AT EMERGENCY LIGHT RIGHT HAND AFT LAVATORY. REPOSITIONED WIRE FOR EMERGENCY LIGHT AT RIGHT HAND AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041007000322004100700032NM 2004 10 7 SWAA042847 120040930A53106545874 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME CUTOUT AT UPPER STOP, CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20041007000342004100700034NM 2004 10 7 SWAA042849 120040930A53106545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.5, LBL 32, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041007000362004100700036NM 2004 10 7 SWAA042851 120040930A55526545166 CONTROL ROD BOEING737 7373T0 1384582NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB OUTBOARD CONTROL ROD END WORN. REMOVED AND REPLACED LEFT OUTBOARD CONTROL ROD PER MM. 2L72 4F RTA16WE 20041007000392004100700039EA 2004 10 7 VNAA0409002 120040920A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY DOOR FALSE INDICATIONA VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07245PS 7919 THE CREW REPORTED RECEIVING A RT EMERGENCY DOOR WARNING LIGHT IN FLIGHT. THE CREW ENSURED THE DOOR WAS INDEED CLOSED. MAINTENANCE CONTROL THEN DEFERRED THE EMERGENCY DOOR INDICATING SYSTEM WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE-C. 2L72 4F4 FRTA21EA E15NE 20041007000402004100700040EA 2004 10 7 VNAA0409001 120040910A2612 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF343B1 NE FIRE WARNING ILLUMINATED A VNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL07708PS 10160 THE CREW REPORTED RECEIVING A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE CONTROL HAD THE CREW RESET THE CIRCUIT BREAKERS CBP-1, N1, AND N2, IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-10-00 AND THE MESSAGE CLEARED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041007000422004100700042EA 2004 10 7 VNAA0410001 120041001A2612 FIRE LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07209PS 7874 THE CREW REPORTED RECEIVING A APU FIRE FAIL AMBER CAS MESSAGE. THE FIRE LOOP-A WAS FAILING TO TEST. MAINTENANCE CONTROL DEFERRED THE APU FIRE DETECTION SYSTEM WITH THE CREW WITH 26-12-01, CODE-C. 2L72 4F4 FRTA21EA E15NE 20041007000442004100700044SO 2004 10 7 C2XA04TY166 120040925A531114523509401 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716927 145006 DURING SCHEDULED INSPECTION FRAMES 68 AND 70 AT STRINGER 13R WERE FOUND CHAFED. REPAIRED CHAFED AREAS BY BLENDING THE DAMAGED AREA IAW EC 5310-01292. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041007000462004100700046NM 2004 10 7 QXEA200400694 120041004A5240 COVER BOMBDRDHC8 DHC8401 1390041NM SERVICE DOOR WORN A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09402QX7888 4032 CREW REPORTS THE AFT SERVICE DOOR WILL NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE DOOR AND FOUND THE EXTERNAL HANDLE STRIKING THE AFT FLAP COVER. THE FLAP COVER, SPRING, AND HINGE PIN WERE REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041007000482004100700048 2004 10 7 SWAA042810 420040928A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041007000502004100700050NM 2004 10 7 SWAA042812 120040928A5320BAC15171489 CHANNEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND ZEE CHORD AT BS 270, LBL 11, CORRODED. REMOVED AND REPLACED CHORD SECTION PER SRM. 2L72 4F RTA16WE 20041007000522004100700052SO 2004 10 7 C2XA04CL092 120040912A3350375911 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714991 145278 CLE- FLIGHT 2267, CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 12. ALL OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20041007000532004100700053SO 2004 10 7 C2XA04CL093 120040917A324423094003401 TIRE EMB 145 EMB145XR 3260214SO RT MLG FAILED A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2712163 14500811 CLE- FLIGHT 2230, CREW REPORTED THAT THE NR 3 MAIN TIRE BLEW ON TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT THE NR 3 TIRE HAD BLOWN AND CAUSED DAMAGE TO THE RIGHT INBOARD FLAP. ALSO FOUND DAMAGE TO THE NR 2 ENGINE INLET GUIDE VANES AT THE 5 O'CLOCK POSITION. APPLIED SPEED TAPE TO THE DAMAGED AREA OF THE RIGHT INBOARD FLAP AND PLACED ON DMI FOR 100FC AS PER EMBRAER FACSIMILE REF IC2004-145/4377. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED BACK TO SERVICE. 2L72 4F RT 20041007000542004100700054WP 2004 10 7 ABXA040334 120040927A7797 WIRE HARNESS DOUG DC8 DC863F 302198FWP EPR SYSTEM BURNED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 DURING LINE MAINTENANCE INVESTIGATION OF NR 3 ENGINE EPR PROBLEM, FOUND THE EPR WIRING HARNESS, THRUST BRAKE WIRING AND THRUST REVERSER EMERGENCY DUMP VALVE WIRING CHARRED AND FRAYED DUE TO A PREVIOUS PNEUMATIC DUCT LEAK. REPLACED WIRE NR 3H406E24, 3H2156B24, 3E41L24, 3E379F24, 3E572A24N, 3E573A24N, 3E342K22-RD, 3E378D22-YE, 3E343K22-BL, 3K402C20, 3K404A20N, 3K405J20, 3K438A20N, 3K434A20N IN PYLON LEADING EDGE. ACCOMPLISHED ON ABX NON ROUTINES 105, 106, 107. ALL SYSTEMS OPS CHECKED GOOD IAW DC-8 MM. 2L74 4F 4A25 20041007000552004100700055NM 2004 10 7 AALA20041023 120041001A3350BPS73 SIGN BOEING757 757223 1384957NM EMERGNECY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21643AA 24601 DFW - AFT RIGHT HAND CABIN DOOR EXIT ARROW MARKER SIGN LIGHT AFT OF THE DOOR IS BROKEN. REPLACED THE AFT RIGHT HAND CABIN DOOR INTERIOR EXIT ARROW MARKER SIGN LIGHT AFT OF THE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041007000572004100700057NM 2004 10 7 SWAA042853 120041001A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 20R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041007000592004100700059NM 2004 10 7 CALA0400648 120040929A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 12 TO RBL 58. A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20041007000612004100700061NM 2004 10 7 CALA0400649 120040929A53476546816 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND SEAT TRACK CORRODED AT STA 892, RBL 24.5. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. 2L72 4F RTA16WE 20041007000632004100700063NM 2004 10 7 SWAA042856 120041001A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041007000652004100700065NM 2004 10 7 SWAA042858 120041001A55526625183 BUSHING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C3 CHECK, LT ELEVATOR NR 1 TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB NR 1 HINGE BUSHING PER MM. 2L72 4F RTA16WE 20041007000662004100700066NM 2004 10 7 P5CA0401238 120041001A5512 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE HORIZONTAL STAB CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RT HORIZONTAL STAB T/E UPPER SURFACE ENTIRE LENGTH SKIN SEVERAL AREA HAS CORROSION. REMOVE CORROSION FROM SEVERAL AREAS, TREATED & PRIMED PER SRM 51-10-01, 55-10-01, 51-10-02. 2L74 4F4 F A20WE E20EA 20041007000672004100700067NM 2004 10 7 P5CA0401239 120041001A5313 BEAM BOEING747 747123 1384873NM PWA JT8 JT8D7A 52053NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT, LONGITUDNAL BEAM AT STA 2040-2060-2080 LBL 30 IS CRACKED. REMOVED DAMAGE SECTION, FABRICATED NEW PART & INSTALLED PER SRM 51-40-04. 2L74 4F4 F A20WE E2EA 20041007000682004100700068NM 2004 10 7 SWAA042836 120040929A53306545765 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 581, STRINGER 2L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041007000702004100700070NM 2004 10 7 SWAA042815 120040928A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SPV, FOUND 2 EACH BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 13 ABC, 17 ABC, INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20041007000722004100700072 2004 10 7 SWAA042817 420040928A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000762004100700076 2004 10 7 SWAA042859 420041001A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29374SW 26582 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000782004100700078WP 2004 10 7 ABXA040345 120040928A53203924028501N FITTING DOUG DC9 DC941 302207NWP CENTER WING SEC CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 LONGERON END FITTING CRACKED AT RIGHT CANTED KEEL AREA, LONGERON 29 RIGHT. REMOVED AND REPLACED LONGERON END FITTING AT CANTED KEEL AREA IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20041007000802004100700080WP 2004 10 7 AALA20041007 120040930A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21461AA 49566 OVERHEAD EMERGENCY LIGHTS A ROWS 13 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACKS FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 THROUGH 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000822004100700082WP 2004 10 7 AALA20041009 120040929A2741 MOTOR DOUG DC9 DC982 3022082WP TRIM DRIVE FAILED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21275AA 49272 DFW - INFLIGHT T1675/29 BOTH PRIMARY AND ALTERNATE TRIM FAILED. LANDED DFW WITHOUT INCIDENT. REPLACED PRIMARY AND ALTERNATE DRIVE MOTORS AND POWER SUPPLY FOR ALTERNATE DRIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000842004100700084NM 2004 10 7 SWAA042837 120040930A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 19R, BS 747, STRINGER 20R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041007000862004100700086NM 2004 10 7 SWAA042839 120040930A335010107451 LENS BOEING737 7377H4 1384404NM EMERGENCY SIGN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29434WN 32454 DURING SCHEDULED MV3 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20041007000882004100700088NM 2004 10 7 SWAA042841 120040930A53306545774 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 777, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041007000902004100700090NM 2004 10 7 SWAA042843 120040930A5551 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND RT AND LT HORIZONTAL STAB FITTINGS FWD AND AFT SPAR CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20041008000042004100800004SO 2004 10 8 C2XA04CL096 120040922A335074441 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSLOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713949 145057 EWR FLIGHT 2167- CREW REPORTED THE EMERGENCY LIGHT IN FRONT OF SEAT 3BC WAS INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND RESECURED THE ELECTRICAL CONNECTORS AND THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. 2L72 4T RTT00011AT 20041008000072004100800007SO 2004 10 8 C2XA04TY162 120040910A555114504980602 SUPPORT EMB 145 EMB145ER 3260211SO STAB BEARING GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715926 145005 VERTICAL STABILIZER TO HORIZONTAL STABILIZER RIGHT SPHERICAL BEARING HOUSING WAS GOUGED. REWORKED HOUSING PER EC5510-01089. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041008000092004100800009SO 2004 10 8 C2XA04SH503 120040923A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139793905 2720 145181 SHV- DURING C-CHECK THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND THE NR 1 EMERGENCY LIGHT BATTERY DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041008000112004100800011SO 2004 10 8 C2XA04TY161 120040831A2560P4010030 BATTERY EMB 145 EMB145LR 3260212SO FLASHLIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712900 145511 TYS, DURING A SCHEDULED INSPECTION, THE CAPTAINS FLASHLIGHT BATTERY REQUIRES CHARGING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE CAPTAINS FLASHLIGHT, OPERATIONAL CHECKED GOOD IAW EMB-145-AMM-33-50-16. AIRCRAFT RELEASED TO SERVICE. 2L72 4T RTT00011AT 20041008000122004100800012GL 2004 10 8 C2XA04IA091 220040806A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LEFT LEAKING A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2712921103737106 145354 CAE311297 DURING DESCENT THE CREW REPORTED ODOR AND SMOKE HAZE IN THE COCKPIT AND CABIN WITH A LAV SMOKE WARNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED GOOD. ALL IAW EXPRESSJET TASK CARD 6271001, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20041008000142004100800014NM 2004 10 8 SWAA042883 120041004A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727D, BS 727B, STRINGER 14R. REPAIRED SKIN PER RA. 2L72 4F RTA16WE 20041008000162004100800016NM 2004 10 8 QXEA200400667 120040912A33506104789 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09368PH 508 512 SEA - FORWARD CABIN OVERHEAD EMERGENCY EXIT SIGN INOP, FORWARD CABIN EMERGENCY EXIT SIGN INOP, FORWARD RT EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE REPLACED NR 2 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000192004100800019SO 2004 10 8 C2XA04BT095 120040904A3350P4010030 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714907 145468 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND THE NR 2 EMERGENCY FLASHLIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY FLASHLIGHT BATTERY IAW EMB 145 AMM 33-50-16. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041008000202004100800020SO 2004 10 8 C2XA04CL088 120040903A33501380 BULB EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 DURING PREFLIGHT FOR FLIGHT 2180 OUT OF CLE THE CREW DISCOVERED THE GALLEY EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN BULBS AND IT OPERATED PROPERLY. FLIGHT 2180 CONTINUED WITHOUT FURTHER INCIDENT. 2L72 4F RTT00011AT 20041008000222004100800022NM 2004 10 8 CALA0400652 120040928A5730114N210619 SKIN BOEING757 757224 1384958NM LT WING DEBONDED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733103 27293 INSPECTION FOUND LT WING UPPER SURFACE FIXED L/E FAIRING SKIN DEBONDED AT WS 400 (JUST AFT OF NR 4 SLAT). REPAIRED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20041008000252004100800025NM 2004 10 8 CALA0400655 120040927A5315143N50561 FLOORBEAM BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733103 27293 INSPECTION FOUND UPPER SURFACE OF CABIN FLOORBEAM CORRODED AT STA 740, LBL 14 TO RBL 8. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA2NM 20041008000262004100800026NM 2004 10 8 CALA0400656 120040930A575465C26793 SKIN BOEING737 7373T0 1384582NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND A 1 INCH CRACK IN THE NR 3 SLAT LOWER SKIN AT O/B MAIN TRACK. A REPAIR WAS INSTALLED IAW SRM 57-43-01. 2L72 4F RTA16WE 20041008000332004100800033NM 2004 10 8 SWAA042819 120040928A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 787, STRINGER 24L, BS 727E, STRINGER 20R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041008000342004100800034 2004 10 8 SWAA042822 420040929A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29738CB 27870 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040930001772004093000177NM 2004 9 30 P5CA0401204 120040914A5347 SEAT TRACK BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 MAIN DECK CARGO COMPT SEAT TRACK HAS CORROSION. REMOVED CORROSION, PRIMED & TREATED. 2L74 4F4 F A20WE E20EA 20040930001802004093000180WP 2004 9 30 ABXA040319 120040907A53205912494501 PAN DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 FORWARD LOWER CARGO DOOR PAN WAS CORRODED OUT OF LIMITS. REPLACED FORWARD LOWER CARGO DOOR PAN IAW DC-9 MM. 2L72 4F A6WE 20040930001862004093000186NE 2004 9 30 P5CA0401184 220040905A7200 ENGINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 1 MALFUNCTIONED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP23920FT 22237 702264 NR 1 ENGINE SHUT DOWN, EGT WENT OFF SCALE, N1 WENT 20 PERCENT, N2 14 PERCENT & OIL PRESSURE 5 PSI. REPLACED NR 1 ENGINE PER WORK CARD MM 71-00-02 & 71-08-07, ALL OPS CK NORMAL. 2L74 4F4 F A20WE E3NE 20040930001882004093000188NM 2004 9 30 P5CA0401186 120040906A2750 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL TE FLAPS ILLUMINATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23454PA 30812 EICAS WARNING CONFIG FLAPS & CONFIG STAB. RESET NR 3 GCU PER MM 24-20-00, ALL SYSTEMS CHECKED NORMAL, GROUND TEST PASSED. 2L74 4F4 FRTA20WE E23EA 20040930001982004093000198NM 2004 9 30 EIA2004076 120040904A5313 STRINGER BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 STRINGER 14R CRACKED AT BS 2200. REMOVED DAMAGE, FABBED REPAIR IAW SRM 51-30-02. 2L74 4F4 F A20WE E20EA 20040930002002004093000200NM 2004 9 30 EIA2004088 120040902A5315 FLOORBEAM BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 MAIN DECK FLOORBEAM FWD SIDE (J) CHANNEL CORRODED BS 460 LBL 9. FABBED AND INSTALLED REPAIR PARTS, STA 460 LOWER CHORD LBL9 IAW SRM 51-40-04 FIG. 1 AND 51-30-02. 2L74 4F4 F A20WE E20EA 20041001000072004100100007NM 2004 10 1 UPS04M43191 120040812A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORZ STAB NR 4 LT BARREL NUT HOLE FOUND CORRODED AT BOTTOM SIDEWALL AND BEARING SURFACE. CORROSION AT B/N HOLE NR 4 LT REMOVED, BLENDED AND REAMED TO 0.944 INCH, FOUND OUT OF LIMIT FAB SLEEVE AND BUSHING IAW EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA AND INSTALLED SLEEVE BUSHING AT B/N HOLE NR 4 LT IAW EO MD11-5510-19409-H. REPAIR CUT OUT AT B/N HOLE NR 4 LT IAW EO MD 11-5510-19409-H AND EN:1296-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041001000142004100100014 2004 10 1 UPS04M43217 420040928A2565 SWITCH DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE EVACUATION SLIDEOUT OF ADJUST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP 48575 EVACUATION SLIDE REMOTE PRESSURE PTT LIGHT ILLUM ALL THE TIME. REF. M288525. L1 DOOR SLIDE REMOTE PRESS LIGHT SWITCH ADJUSTED, AND TESTED AND FOUND OK, DEFFERRAL M288525 CLEARED. 2L73 4F4 FRTA22WE E24NE 20041001000232004100100023WP 2004 10 1 WX0400031 120040915A3350 BATTERY DOUG DC9 DC982 3022082WP PWA JT8 JT8D NE EMERGENCY LIGHT DISCHARGED A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19890GA 49371 MAINTENANCE REPORTED AFT SERVICE DOOR AND AFT ENTRANCE DOOR EMERGENCY EXIT LIGHTED SIGNS INOPERATIVE, OVERHEAD EMERGENCY EXIT LIGHTS AFT FLIGHT ATTENDANT STATION, OVERHEAD EMERGENCY EXIT LIGHT ROW 2 AND OVERHEAD EMERGENCY EXIT LIGHTS ROWS 31 TO 33 INOPERATIVE. MAINTENANCE RE-LAMPED AFT SERVICE DOOR, AFT ENTRANCE DOOR, OVERHEAD’S AT FLIGHT ATTENDANT STATION AND ROW 2 EMERGENCY EXIT LIGHTS AND REPLACED BATTERIES AT OVERHEAD EMERGENCY EXIT LIGHTS ROWS 31 TO 33. ALL MAINTENANCE ACCOMPLISHED IAW 33-53-01. ALL EMERGENCY EXIT LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20041001000252004100100025WP 2004 10 1 WX0400033 120040920A3620 SEAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE LT PACK LEAKING A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19861GA 49557 AFTER NORMAL TAKEOFF ROLL AT APPROXIMATELY 600 FT TO 800 FT AGL MASTER WARNING LIGHT ILLUMINATED, TRIGGERED BY TAIL COMPARTMENT TEMPERATURE HIGH LIGHT. CREW FOLLOWED QRH PROCEDURES AND RETURNED TO AIRPORT, NO EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE FOUND BLEED LEAK IN TAIL COMPARTMENT. AIRCRAFT FERRIED FOR REPAIR. MAINTENANCE REPLACED 2 EACH PERRY SEALS ON THE LT PACK IAW MD80-MM 36-00-00. SYSTEM OPERATIONALLY CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20041001000332004100100033CE 2004 10 1 DXTA200400395 120040916A282090363512 CHECK VALVE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE FUEL SYSTEM LEAKING E DXTAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07316QS 5600516 A STRONG FUEL SMELL WAS NOTED IN THE CABIN WHILE AT CRUISE. FOUND PRE-CHECK VALVE LEAKING, INSTALLED NEW VALVE WITH NEW PACKINGS IAW MM CHAPTER 28-22-00. OPS CHECKS AND LEAK CHECKS GOOD. 2L72 4F4 FRTA22CE E25EA 20041001000442004100100044SO 2004 10 1 SWIA200413862 120040928A3350 LAMP EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07190SW 120050 FRONT CABIN EXIT LIGHT NEAR MAIN CABIN DOOR IS INOPERATIVE. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041001000482004100100048GL 2004 10 1 QR92004F00000 220040706A7230E230397911C ADAPTER ALLSN BELL 206 206B 1181511SW ALLSN 250C 250C20J 03013GL COUPLING SHEARED B QR9RO OTHER O OTHER NRNOT REPORTED 1 SO09672663988 490 CAC42634 5131 CAE272692 ENGINE REMOVED FROM SERVICE FOR ENGINE CHIP LIGHT ILLUMINATION, FOLLOWED BY ENGINE FAILURE DURING PINNACLE LANDING. TEAR DOWN ANALYSIS REVEALED COUPLING ADAPTER SHEARED AT PILOT DIAMETER CAUSING FAILURE. (SO09200408990) 1G71 3U3 U H2SW E4CE 20041001000492004100100049NM 2004 10 1 2004UALA00844 120040919A4920 CARBON SEAL BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU ENGINE FAILED A UALAA UNSCHED LANDING KH FLUID LOSS ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29511UA 24799 APU AUTO SHUT DOWN DUE TO LOSS OF OIL PRESSURE. SHOP FINDINGS REVEALED DRIVEN COMPRESSOR FRONT CARBON SEAL ASSEMBLY LEAKED. THE INTERNAL LIP SEAL WAS PINCHED BY THE WAVE WASHER AND EXCESSIVE ABRAIDABLE MATERIAL IMPEEDED CARBON TRAVEL. THE DRIVEN COMPRESSOR WAS REMOVED AND OVERHAULED. THE CARBON SEAL ASSEMBLY IS REPLACED DURING DRIVEN COMPRESSOR ASSEMBLY. 2L72 4F4 FRTA2NM E17NE 20041001000582004100100058NM 2004 10 1 P5CA0401229 120040928A1420 CONNECTOR BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL OIL TEMP SENSOR DIRTY A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23496MC 29257 704880 NR 2 ENGINE OIL ITEM INDICATION. CLEANED ELECTRICAL CONNECTOR ON OIL TEMPRATURE SENSOR, NR 2 ENGINE INDICATION OK, IAW AMM 71-00-00. 2L74 4F4 FRT1384945 E23EA 20041001000632004100100063NM 2004 10 1 04FDEA02809 120040923A5753 HINGE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03. 2L73 4F4 FRTA22WE E31N3 20041001000752004100100075WP 2004 10 1 COOSDR040019 120040823A5315 FLOORBEAM DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE FUSELAGE CRACKED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 MAIN CARGO CABIN Y, STA 1380 FLOORBEAM UPPER CAP AFT FLANGE CRACKED. 2L74 4F4 F 4A25 1E8 20041001000762004100100076NM 2004 10 1 HNAA0400090 120040929A531185320103109 FRAME DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR. THIS EO8-53-04-0632 PERFORMS SPLICE REPAIR TO X222 FRAME WHICH WAS REMOVED FOR WIDESPREAD CORROSION. THIS IS A MAJOR REPAIR. 2H72 4T4 TRTA13NM E20NE 20041001000772004100100077NM 2004 10 1 HNAA0400094 120040929A531185330043103 FRAME DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHECK, FOUND CORROSION ON SKIN FLANGES OF THE X488 FRAME WHICH WOULD REQUIRE FRAME LEG REPAIRS. DUE TO CONCURRENT, REMOVED AND REPLACED OF STR 31S IN THIS AREA, DECISION MADE TO REPAIR DAMAGE BY REPLACING DAMAGED SECTION OF THE FRAME. THIS EO8-53-04-0658 ACCOMPLISHES REPAIR. 2H72 4T4 TRTA13NM E20NE 20041001000782004100100078NM 2004 10 1 HNAA0400097 120040929A5751 SKIN DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE AILERON DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 THIS EO8-57-04-0678 PERFORMS REPAIR FOR DENTED RT AILERON LOWER SKIN (P/N 85740055). NOTED DENT REPORTED AS OIL CANNING. REPAIR CONSISTS OF DRILLING OUT CENTER OF DENT TO RELIEVE OIL CANNING THEN INSTALLING EXTERNAL DOUBLER. THIS EO IS A MAJOR REPAIR. 2H72 4T4 TRTA13NM E20NE 20041001000792004100100079NM 2004 10 1 HNAA0400089 120040929A531185320318113 FRAME DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR WHICH RESULTED IN SPLICE REPAIR OF STR 31S . THIS EO PERFORMS SPLICE REPAIR TO X202 FRAME WHICH WAS REMOVED FOR WIDE SPREAD CORROSION. THIS IS A MAJOR REPAIR. 2H72 4T4 TRTA13NM E20NE 20041001000802004100100080NM 2004 10 1 HNAA0400095 120040929A531385310027121 STRINGER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 THIS EO8-53-04-0670 PERFORMS REPAIR FOR STR 30S FOR CORROSION. THIS IS A MAJOR REPAIR. 2H72 4T4 TRTA13NM E20NE 20041001000822004100100082WP 2004 10 1 MWEA040173 120040923A533059114053 DOUBLER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 A DENT ON FUSELAGE SKIN IS 1.7500 INCH LONG BY 1.3750 INCH WIDE LOCATED .3750 INCH BELOW LONGERON 4 LT AND AT FRAME STA 218, MAXIMUM DEPTH .021. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20041001000842004100100084WP 2004 10 1 COOSDR040033 120040823A53403640887U FITTING DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 MAIN CARGO CABIN FROM Y STA 960 TO Y STA 980 FITTINGS, CORRODED. 2L74 4F4 F 4A25 1E8 20041001000862004100100086NM 2004 10 1 COOSDR040026 120040817A5330 SKIN BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 AFT CARGO COMPARTMENT, NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT THE INTERNAL SURFACE. 2L73 4F4 FRTA3WE E2EA 20041001000872004100100087NM 2004 10 1 HNAA0400091 120040929A531185321156107 FRAME DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHECK, FOUND CORROSION UNDER CABIN FLOOR WHICH RESULTED IN SPLICE REPAIR OF STR 31S. THIS EO8-53-04-0630 PERFORMS SPLICE REPAIR TP X253 FRAME WHICH WAS REMOVED TO FACILITATE INSTALLATION OF REPLACEMENT SECTION OF STR31S. THIS IS A MAJOR REPAIR. 2H72 4T4 TRTA13NM E20NE 20041001000892004100100089NM 2004 10 1 04FDEA02811 120040923A5311 FRAME DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 TRANSVERSE FRAME AT LT STA Y= 1721 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 FLIGHT CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-DTA. 2L73 4F4 FRTA22WE E31N3 20041001000912004100100091NM 2004 10 1 04FDEA02813 120040923A3620 PNEUMATIC SYSTEM DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE PNEUMATIC SYSTEMMALFUNCTIONED A FDEAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 SO25594FE 48552 ON CLIMB OUT FROM ZSPD GOT LEVEL 3 ALERT AIR MANF 2 FAIL. COMPLIED /W QRH, DUMPED FUEL, LANDED RJBB. ACN RELEASED FOR SERVICE IAW MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 03OCT04) MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 INOPERATIVE.**** S/D COMING**** 2L73 4F4 FRTA22WE E31N3 20041004000022004100400002NM 2004 10 4 USAASB04123 120040911A493036177501 FUEL CONTROL BOEING737 7374B7 1384702NM APU MALFUNCTIONED A USAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 EA19777AU51273 24979 MIA - FLT 724 - FLIGHT DEPARTED MIA WITH THE NR 1 ENGINE CSD ON MEL FOR AN OIL LEAK. CON CLIMB-OUT, EN ROUTE TO CLT, THE APU GENERATOR DROPPED OFF LINE AT 700 FEET ABOVE GROUND LEVEL. CREW ATTEMPTED TO RESET THE GENERATOR WITH NO HELP. TWO MINUTES LATER, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU AUTO SHUTDOWN. FLIGHT RETURNED TO FIELD AT MIA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOED AND REPLACED APU FUEL CONTROL UNIT AND THE APU COMBUSTOR ASSEMBLY, P/N 3604524. OPS CHECK AND LEAK CHECK GOOD. CLEARED NR 1 ENGINE CSD MEL BY REMOVING AND REPLACING THE CSD, P/N 735511A. (M) 2L72 4F RTA16WE 20041004000222004100400022EA 2004 10 4 ASOA04665 120040831A5320601R31171179 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 484, LBL 27 AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20041004000232004100400023NM 2004 10 4 USAA040559 120040822A5320 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, TIE CLIP CRACKED, STATION 827 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M) 2L72 4F RTA16WE 20041004000302004100400030EU 2004 10 4 SIMA200425301 120040905A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21397AE 340B397 SPS - FLT 3270 - DURING PREFLIGHT, CREW FOUND THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE DUE TO EMERGENCY ILGHT SWITHC LEFT IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLY BATTERIES S/N 1248, 1078, 1292 AND 1106 IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20041004000322004100400032EU 2004 10 4 SIMA200425305 120040902A53117252813485 FRAME SAAB SF340 340B 7860101EU CARGO BAY DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21347SB 340B347 ABI - DURING AN HMBV INSPECTION, THE CARGO RIGHT FRAME AT STATION 640 WAS FOUND DENTED 5 INCHES ABOVE THE FLOOR. RECONTOURED THE FRAME AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SAAB REPAIR STATEMENT 340SDS007535, PARA 6 DATED AUGUST 21, 2004. (M) 2L72 4T RTA52EU 20041004000362004100400036NM 2004 10 4 USAASB04121 120040910A2741AVR869 RELAY BOEING737 7374B7 1384702NM STAB TRIM FAILED A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19440US 24811 PIT - FLT 1451 - ON CLIMB-OUT FROM PIT, EN ROUTE TO PBI, CREW REPORTED THE STABILIZER TRIM WAS INOPERATIVE IN BOTH ELECTRIC AND MANUAL. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE R63 PHASE SEQUENCE RELAY, THE R64 STABILIZER TRIM CONTROL RELAY, P/N 9123-8071, AND THE R66 STABILIZER TRIM SAFETY RELAY, P/N 9123-8071. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20041004000392004100400039NM 2004 10 4 USAA040552 120040823A5754 SKIN BOEING757 7572B7 1384964NM NR 9 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19624AU 27245 CLT - FOUND SLAT CRACKED .75 INCH, NR 9 SLAT COVE SKIN CRACKED AT INBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M) 2L72 4F RTA2NM 20041004000422004100400042EA 2004 10 4 ASOA04672 120040902A2741 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA STAB TRIM ILLUMINATED A ASOAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 SO11705EV 10051 FLT 4201 - DURING CRUISE FROM DFW-DCA, AFTER LEVELING OFF AT APPROX 37,000 FEET THE CREW RECEIVED STABILIZER TRIM AND MACH TRIM CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND THE STABILIZER/MACH TRIM WOUND NOT RE-ENGAGE. AFTER COMPLYING WITH THE QRH BY REDUCING THE AIR SPEED TO .070 MACH A STALL FAIL CAUTION MESSAGE OCCURRED AND THE STALL PROTECT WAS TURNED OFF PER THE QRH. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO INTO CVG, LANDING SAFELY. MAINTENANCE IS CURRENTLY PERFORMING TROUBLESHOOTING TO DETERMINE THE APPROPRIATE CORRECTIVE ACTION. THE AIRCRAFT REMAINS GROUNDED UNTIL THE CORRECTIVE ACTION HAS BEEN MADE. THIS MRR WILL REMAIN OPEN PENDING THE APPROPRIATE REPAIRS. (M) 2L72 4F RTA21EA 20041004000442004100400044NM 2004 10 4 USAA040539 120040820A5751 SKIN BOEING757 757225 1384959NM AILERON DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU61650 22201 CLT - FOUND AILERON COMPOSITE AND SEPARATED 2 INCH BY 5 INCH AREA, LEFT AILERON, INBOARD LOWER CORNER. REPAIR PLYS INSTALLED, DISBOND CHECKED, SANDED, PRIMED AND PAINTED PER EA 95798 AND SRM 51-70-17. (M) 2L72 4F RTA2NM 20041004000462004100400046NM 2004 10 4 USAA040551 120040823A5754 SKIN BOEING757 7572B7 1384964NM NR 9 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19624AU35200 27245 CLT - FOUND SLAT CRACKED.5 INCH, NR 9 SLAT COVE SKIN CRACKED AT OUTBOARD MAIN TRACK. FABRICATED NEW PANEL PER DRAWING 114N4003. (M) 2L72 4F RTA2NM 20041004000522004100400052NM 2004 10 4 USAA040544 120040819A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU61650 22201 CLT - FOUND FRAME WEB CRACKED .375 INCH, FS 1440 BETWEEN STRINGER 25R AND 27R FROM LOWEST HOLE DOWN AT NR 6 STOP FITTING. INSTALLED FRAME WEB REPAIR AT STATION 1440 BETWEEN STRINGER 25R AND 27R PER EA 95775. (M) 2L72 4F RTA2NM 20041004000572004100400057NM 2004 10 4 USAASB04118 120040906A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19777AU 24979 CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHTS IN THE AFT GALLEY ARE BLINKING AND WON'T ILLUMINATE AND STAY ON WHEN SELECTED. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 20041004000582004100400058NM 2004 10 4 USAA040527 120040903A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED 2 INCH AREA, FS 335, LBL 40. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041004000712004100400071NE 2004 10 4 GJR2004F00000 220040901A7314TF9005 PUMP DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985* 52008NE FUEL SYSTEM FAILED B GJRRO OTHER O OTHER NRNOT REPORTED 1 NM01900KA 1676 LOSS OF FUEL PRESSURE. 1H71 3R3 R A806 5E1 20041004000872004100400087CE 2004 10 4 VJT2004F00001 120040825A2760602EN166 SWITCH CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE RT SPEEDBRAKE SHORTED E VJTAO OTHER O OTHER NRNOT REPORTED 1 EA0392B 6776 5500471 PCE71343 PILOT REPORTED SPEED BRAKES WOULD NOT DEPLOY. CONFIRMED MALFUNCTION DURING GROUND TEST. TROUBLESHOT SYSTEM. FOUND DEFECTIVE SWITCH S202 (RT RETRACT LIMIT). REPLACED SWITCH IAW MM, OPERATIONAL TEST SATISFACTORY. 1L72 4F4 F A22CE E1NE 20041004001102004100400110SO 2004 10 4 2004F00389 120040917A6120 PROPELLER EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE MALFUNCTIONED E GNOAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO15267AS 120198 20001112 UPON TAKEOFF, PIC REPORTED THAT THE LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO ABORTED THE LAST LEG FROM LNC TO CRG AND CHOSE TO LAND SGF WHERE AFTER A GROUND RUN UP DETERMINED THAT THE LT NP WAS READING CORRECTLY. THIS LEG WAS A REPOSITIONING LEG AND NO REVENUE PASSENGERS ON BOARD. THE CAUSE FOR THIS DISCREPANCY IS YET UNKNOWN. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20041004001132004100400113WP 2004 10 4 UPS04843131 120040916A2150 COOLING TURBINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ACM ODOR A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01802UP 46100 DURING CRUISE NOTICED VERY BAD BURNING SMELL COMING FROM RT SIDE OF AIRCRAFT BEHIND REAR JUMPSEATS NOT ELECTRICAL SMELL R MANIFOLD TEMP 240 C R PACK ON AND OFF NO CHANGE. LT PACK SYSTEM CKD GOOD NO SMELL. RT SYSTEM HAS OIL SMELL FOUND RT ACM BAD DEFERRED IAW MEL 21-39. PLACARD INSTALLED. GRD RAN ENGINE AT PWR PERFORMED MANIFOLD AIR ABNORMAL TEMPERATURE INDICATION TEST. FOUND L/H TEMP BULB READING LOW. FOUND SKYDROL OVER SERVICED BY APPROX.5 GALS. RAN BOTH PACKS NO ABNORMAL SMELL. TEMP O ALL WORK IAW MM 36-00-00. 2L74 4F4 FRT4A25 E2GL 20041004001202004100400120NM 2004 10 4 04FDEA02398 120040809A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, OB AFT HINGE PIVOT HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.504, MATERIAL REMOVED = 0.010, REMAINING THICKNESS = 0.494. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001212004100400121NM 2004 10 4 04FDEA02399 120040809A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.090. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001342004100400134NM 2004 10 4 2004UALA00731 120040807A2150BACR13CF2AB RELAY BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT A/C PACK FAILED A UALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 WP29528UA 25018 CABIN TEMPERATURE STUCK IN FULL HOT. RT PACK TEMP VLV WOULDN'T DRIVE COLD--RPL K56, REF WDM21-51-23 . VALVE WILL NOW DRIVE COLD. 2L72 4F4 FRTA2NM E17NE 20041004001402004100400140NM 2004 10 4 2004UALA00760 120040730A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 MID CABIN HAS A CRACKED INTERCOSTAL AT STA 540 RBL 2 AND LBL 2. REPAIRED THE FLOOR INTERCOSTALS. 2L72 4F4 FRTA16WE E2GL 20041004001422004100400142NM 2004 10 4 2004UALA00762 120040801A5320 CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 STA 500D STR 8R HAS CRACKED CLIP. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20041004001472004100400147 2004 10 4 583CC0004 420040826A221075130A4Q80 TRANSFER VALVE BOEING737 737291 138448WNM YAW DAMPER INOPERATIVE A PIDAO OTHER O OTHER NRNOT REPORTED 1 SO05583CC 21069 YAW DAMPER WILL NOT ENGAGE WHEN SELECTED. YAW DAMPER PLACED ON MEL 22-3-1. 08/27/2004: REPLACED TRANSFER VALVE PER MM 22-11-71 AND 22-12-01. OPS AND LEAK CHECK NORMAL. 2L72 4F A16WE 20041004001512004100400151SO 2004 10 4 CHQA000531 120040727A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378 145593 EXTERNAL EMERGENCY EXIT LIGHT OVER RT WING IS INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY EXIT LIGHT BULB IAW 145 MM 33-50-02. 2L72 4F RTT00011AT 20041005000092004100500009NM 2004 10 5 04FDEA02374 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.0.396 COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041005000142004100500014NM 2004 10 5 04FDEA02379 120040805A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING T IB HOLE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062. FINAL DIAMETER = 1.199. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041007000152004100700015NM 2004 10 7 SWAA042869 120041003A57536546435277 SKIN BOEING737 7373Y0 1384671NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED SERVICED CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20041007000172004100700017NM 2004 10 7 SWAA042871 120041003A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 22L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041007000192004100700019WP 2004 10 7 AALA20041021 120041002A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21400AA 49311 TPA - CEILING EMERGENCY LIGHTS AT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000212004100700021WP 2004 10 7 AALA20041015 120041001A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21419AA 49331 DEN - OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000232004100700023WP 2004 10 7 AALA20041011 120041003A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21275AA 49272 DFW - CEILING EMERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT FORWARD GALLEY AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000252004100700025WP 2004 10 7 AALA20041014 120041002A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21430AA 49342 AUS - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000272004100700027NM 2004 10 7 AALA20041012 120041002A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21637AM 24595 JFK - EMERGENCY LIGHTS AT SEATS 26D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041007000292004100700029WP 2004 10 7 AALA20041017 120041001A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21407AA 49318 DEN - AUXILLIARY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5105 FOR AUXILLIARY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000372004100700037EA 2004 10 7 VNAA0409004 120040927A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY DOOR FALSE INDICATIONA VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07245PS 7919 THE CREW REPORTED RECEIVING AN EMERGENCY DOOR WARNING INDICATION. THE CREW ENSURED THE EMERGENCY DOOR WAS IN FACT CLOSED. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICATION SYSTEM WITH 52-70-03 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041007000692004100700069 2004 10 7 04FDEA02567 420040826A3414 PITOT TUBE DOUG MD11 MD11 3023602NM PITOT/STATIC SYSOBSTRUCTED A FDEAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO25605FE 48514 ON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN, LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. B Y TOUCHDOWN, F/O'S INDICATOR READ 156 KNOTS, CAPTAINS READ 118 KNOTS IN YELLOW. FOLLOWED T/S PER FIM34-11-02 AND FOUND A/S TOLERANCE BET CAPT AND F/O BEYOND LIMIT REF FIG 103 TABLE. PHYSICALLY INSPECTED PITOT PROBES FOUND SMALL DEBRIS ON CAPT PROBE WHEN PURGED. REMOVED AND REPLACED CAPT PROBE & NR 1 CADC PER MM 34-16-01 AND MM 34-11-01. PERFORMED SYS TEST PER MM 34-16-01-5, SATISFACTORY. COMPLIED W/ MTSI 34-10/9654 STEPS 1-6, SATISFACTORY. 2L73 4F RTA22WE 20041007000712004100700071NM 2004 10 7 SWAA042816 120040928A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW 28401 DURING SPV, FOUND PHOTOLUMINESCENT STRIPS AT ROW 20 ABC, 20 DEF, WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20041008000062004100800006SO 2004 10 8 C2XA04CL099 120040925A5210 SPLINE EMB EMB 145 EMB145ER 3260211SO DOOR HANDLE STRIPPED A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2714925 145004 THE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND REPLACED THE INSIDE DOOR HANDLE. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20041008000082004100800008NM 2004 10 8 SWAA042845 120040930A57536546486 WEDGE BOEING737 7373T0 1384582NM RT WING FLAP SEPARATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD T/E MID FLAP WEDGE SEPARATED. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20041008000132004100800013SO 2004 10 8 C2XA04IA120 120040919A339737591 WIRE EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2723139 145731 MKE - FLIGHT 2843, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN LEAD ON THE LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20041008000152004100800015SO 2004 10 8 C2XA04RI007 120040922A3350 POWER SUPPLY EMB 145 EMB145 3260210SO EMERGENCY LIGHT MALFUNCTIONED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING PREFLIGHT CHECK, CREW REPORTED EXIT ROW EMERGENCY LIGHTS (2) TO BE INOPREATIVE. MAINTENANCE PERFORMED POWER SUPPLY RESET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041008000242004100800024NM 2004 10 8 CALA0400654 120040924A5347140N20692 SEAT TRACK BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733103 27293 INSPECTION FOUND LT CABIN SEAT TRACK FLANGE CORRODED AT STA 720-740, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02, PAGE 12. 2L72 4F RTA2NM 20041008000272004100800027NM 2004 10 8 CALA0400657 120040930A2560ACREM1A MEGAPHONE BOEING757 757224 1384958NM L1 DOOR INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2733103 27293 THE L-1 DOOR MEGAPHONE WAS FOUND INOPERATIVE. THE MEGAPHONE WAS REPLACED IAW DRAWING 2560DD10088. 2L72 4F RTA2NM 20041008000352004100800035NM 2004 10 8 QXEA200400690 120040926A2750FE282004 CONTROL MODULE BOMBDRDHC8 DHC8401 1390041NM TE FLAPS FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09417QX578 4086 SUN - FLIGHT 2341 - ON THE APPROACH, WHEN FLAPS WERE SELECTED DOWN, THE FLAPS STOPPED MOVING AT 15 DEGREES. THE LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLAP CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000372004100800037NM 2004 10 8 P5CA0401240 120041001A5511 RIB BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE HORIZONTAL STAB CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RT HORIZONTAL STAB O/B RIB ASSY AT STAB BL 421.50 IS CRACKED. REMOVED CRACK AREA, NO FURTHER DEFECT FOUND. TREATED & PRIMED PER SRM 55-10-01 & 51-10-02. 2L74 4F4 F A20WE E20EA 20041008000382004100800038NM 2004 10 8 P5CA0401235 120041001A5320 FLOOR SUPPORT BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT FLOOR LONGITUDINAL BEAM AT STA 1960-2080 AT LBL 38 IS CRACKED. REMOVED DAMAGE AREA, INSTALLED NEW PARTS PER SRM 51-40-03, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20041008000392004100800039NM 2004 10 8 P5CA0401237 120041001A5711 SPAR BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 LT WING REAR SPAR LWR FIXED T/E PANEL I/B LWR BEAM AT WBL 128 HAS CORROSION AT FWD TENSION TRES. REMOVE CORRODED DOUBLER, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 51-40-02. 2L74 4F4 F A20WE E20EA 20041008000402004100800040NM 2004 10 8 P5CA0401231 120041001A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RT WING L/E UPPER SKIN BETWEEN WING STATIONS 445-476 LOWER SURFACE IS DELAMINATED. REMOVED PANEL & SENT TO COMPOSITE SHOP, REPAIRED & REINSTALLED PER SRM 51-40-09. 2L74 4F4 F A20WE E20EA 20041008000422004100800042NM 2004 10 8 P5CA0401232 120041001A5311 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 MAIN DECK CARGO COMPT SUPPORT FRAME AT STRINGER 10R, BODY STATION 1660, RBL 28 IS CRACKED. REMOVE FRAME, INSTALLED NEW SUPPORT FRAME, TREATED & PRIMED PER SRM 51-30-01 & 51-30-02. 2L74 4F4 F A20WE E20EA 20041008000442004100800044NM 2004 10 8 QXEA200400645 120040817A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 COUNTERSINKS IN PANEL 522BT HAVE FRETTING. BLENDED AND CLEANED FRETTING CORROSION ON 12 COUNTERSINKS WITH SCOTCH BRITE. MAPPED PANEL 522BT FOR ENGINEERING. HFEC INSPECTION BLENDED AREAS FOR CRACKS IAW D8-400 NDTM, PART 1, 51-00-06. NO CRACKS NOTED. INSTALLED NEW PANEL 522BT FROM STOCK IAW D-8 400 AMM 57-11-01, PARAGRAPN 1-4 A-B. 2H72 4T RTA13NM 20041008000452004100800045NM 2004 10 8 CALA0400661 120041005A5314656212526 KEELBEAM BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714605 27318 RIGHT KEEL BEAM HAS TWO NUT PLATES THAT APPEAR TO HAVE CORROSION UNDER THEM AT STATION 724 AND 721. FABRICATED AND INSTALLED REPAIR PER EC/RA 5311-01204. 2L72 4F RTA16WE 20041008000462004100800046WP 2004 10 8 CALA0400662 120041005A532099115598 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772824 49484 FUSELAGE INTERCOSTAL AFT ATTACH ANGLE CRACKED AT INBOARD CORNER STATION 120 BELOW AND OUTBOARD OF FIRST OFFICERS BRIEFCASE BOX. INSTALLED FABRICATED ANGLE PER SRM 51-30-5. 2L72 4F A6WE 20041008000492004100800049NM 2004 10 8 AT0400020 120041005A33508039251 POWER SUPPLY BOEING717 717200 1383700NM EMERGENCY LIGHT INOPERATIVE A ZZDAK NONE L NO TEST ININSP/MAINT 1 SO15990AT 55134 UPON SERVICE CHECK, (ONE) EMERGENCY LIGHT BULB IN COCKPIT FAILED TO ILLUMINATE UPON TEST. RELAMPED, NOW BOTH BULBS OUT. TRIED ANOTHER BATTERY PACK, NO CHANGE. NOW (2) BATTERY PACKS INOPERATIVE. RELAMPED, BOTH BULBS (2 MC316) OPS CHECK GOOD WITH A KNOWN GOOD BATTERY PACK. INSTALLED BOTH BAD PACKS ON AT FORWARD GALLEY OUTBOARD WALL, OTHER AT FORWARD AISLE CEILING, OPS CHECK GOOD. 2L72 4F TRA6WE 20041008000512004100800051NM 2004 10 8 QXEA200400638 120040814A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 LIGHT FRETTING IN COUNTER SINKS OF PANEL 622BT. REPAIRED IAW DHC-8-400 SRM 51-26-10 AND AMM 57-11-01-400-801, PAGE 408-409, PARAGRAPH 4 A, C, D (1-2). 2H72 4T RTA13NM 20041008000532004100800053NM 2004 10 8 QXEA200400646 120040819A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 COUNTERSINKS IN PANEL 522CT HAVE FRETTING. REMOVED CORROSION FROM COUNTERSINKS ON PANEL 522CT WITH SCOTCH BRITE. MAPPED FOR ENGINEERING. OK TO INSTALL NEW FROM STOCK 522CT PANEL IAW D-84 AMM 57-11-01-400-801, PARAGRAPH 1-4, A-D (1-8). 2H72 4T RTA13NM 20041008000542004100800054NM 2004 10 8 QXEA200400639 120040814A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - LITE FRETTING CORROSION FROM 14 COUNTER SINKS AT FORWARD EDGE OF PANEL USING SCOTCH BRITE ON AFT EDGE OF PANEL. NO MEASUREMENTS TAKEN, FRETTING DAMAGE AND REMOVED CORROSION FROM REMAINING 42 COUNTER SKINS USING SCOTCH BRITE. NO MEASUREMENTS TAKEN. MEASURED AND MAP COUNTER SINKS FOR ENGINEERING EVALUATION. HFEC INSPECTED BLENDS FOR CRACKS IAW D8-400 NDTM PART 1, 51-00-06. NO CRACKS NOTED. REPLACED PANEL WITH NEW FROM STOCK. 2H72 4T RTA13NM 20041008000552004100800055NM 2004 10 8 QXEA200400684 120040918A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 PDX - RIGHT HAND INBOARD CABIN SEAT TRACK BETWEEN X10.1 AND X102.5 HAS WIDE SPREAD CORROSION ON SEAT MOUNT SURFACE AND INSIDE CHANNEL. REPAIRED IAW HORIZON AIR EA 6-53-414. 2H72 4T RTA13NM 20041008000562004100800056EA 2004 10 8 COMA0460550 120040927A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01933CA 7040 FLIGHT 5742 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20041008000572004100800057NM 2004 10 8 QXEA200400656 120040904A5320 THRESHOLD BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - AFT CARGO DOOR LOWER THRESHOLD HAS SURFACE CORROSION ON EXTERIOR OF VERTICAL FACE. REMOVED LITE SURFACE CORROSION AROUND SCREW HOLES IAW DHC-8-400 SRM 51-21-00, PARAGRAPH 1-4A, STEP 1, 2 AND 4. HFEC INSPECTION AS PER 1-84-7A, PT 6, 51-00-02, NO CRACKS NOTED. REPAIRED IAW SRM 51-21-04 AND 51-21-00. 2H72 4T RTA13NM 20041008000592004100800059NM 2004 10 8 QXEA200400657 120040826A5420 BRACKET BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - LEFT NACELLE OUTBOARD BRACKET ABOVE NR 3 FLAP TRACK CRACKED APPROXIMATELY 27 INCHES AFT OF REAR SPAR. REPAIRED IAW HORIZON AIR EA 6-54-309. 2H72 4T RTA13NM 20041008000622004100800062WP 2004 10 8 ABXA040339 120040921A57115951702501 SPAR CAP DOUG DC9 DC941 302207NWP RIGHT WING CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 RIGHT WING REAR SPAR UPPER CAP WAS CRACKED RIGHT BUTT LINE 2. REPAIRED AREA IAW DC-9 SRM. 2L72 4F A6WE 20041008000632004100800063WP 2004 10 8 ABXA040340 120040921A5714519486525 SKIN DOUG DC9 DC941 302207NWP WING CTR SEC. CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 TEE CAP FS 618, LONGERON 30, HAD POPPED AND BULGING WEB SEEN FROM AFT SIDE. REPAIRED AREA IAW REA D953-50780 MR. 2L72 4F A6WE 20041008000642004100800064WP 2004 10 8 ABXA040341 120040922A27205912801501 CRANK ASSY DOUG DC9 DC941 302207NWP RUDDER CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 RUDDER CRANK ASSEMBLY IN AFT ACCESSORY / TAIL WAS BLEEDING RUST. REPLACED RUDDER CRANK ASSEMBLY IAW DC-9 MM. 2L72 4F A6WE 20041008000652004100800065WP 2004 10 8 ABXA040342 120040922A5411995816161 SPAR CAP DOUG DC9 DC941 302207NWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 LEFT PYLON FORWARD UPPER SPAR CAP CRACKED AT SECOND FASTENER INBOARD OF FUSELAGE LOFT LINE. REPAIRED IAW JOB CARD EA 54100011-102 AND EA 54100011-001. 2L72 4F A6WE 20041008000672004100800067WP 2004 10 8 ABXA040344 120040925A57535910041504 VANE DOUG DC9 DC941 302207NWP RT WING FLAP DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 RIGHT FLAP INBOARD FIXED VANE UPPER SURFACE AT XRS 164, LOCATED BETWEEN CHAFE STRIPS WAS DELAMINATED BEYOND LIMITS OF 15 SQ INCHES. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM. 2L72 4F A6WE 20041008000682004100800068EA 2004 10 8 COMA0460555 120040911A49901603662 OIL COOLER CNDAIRCL600 CL6002B19 1900309EA APU CRACKED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01468CA12298 7649 FLIGHT 5220 APU OIL PRESSURE CAUTION MESSAGE. REPLACED THE APU OIL COOLER. 2L72 4F RTA21EA 20041008000742004100800074NM 2004 10 8 SWAA042888 120041005A3350100031 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29331SW 23695 OVERHEAD AISLE LIGHT AT ROW 20 DEF LOOSE. SECURED LIGHT PER MM. 2L72 4F RTA16WE 20041008000752004100800075 2004 10 8 SWAA042889 420041005A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041008000802004100800080NM 2004 10 8 ABXA040346 120041006A5210 PANEL BOEING767 767281 1385109NM PAX DOOR OUT OF ADJUST A ABXAO OTHER O OTHER NRNOT REPORTED 1 GL23783AX 23016 MAIN CABIN DOOR GOT JAMMED, WOULD NOT GO ALL THE WAY CLOSED OR OPEN. MAINTENANCE FOUND DOOR PANEL OFF TRACK AT CEILING. PUT PANEL BACK ON TRACK. OPERATED DOOR THROUGH CYCLE, CHECKED OK IAW AMM 52-11-00. 2L72 4F RTA1NM 20041008000832004100800083NM 2004 10 8 SWAA042892 120041005A33506104778 BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND AFT DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041008000842004100800084NM 2004 10 8 SWAA042893 120041005A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20041008000852004100800085NM 2004 10 8 SWAA042894 120041005A575365464352C SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD FLAP PER MM. 2L72 4F RTA16WE 20041008000892004100800089NM 2004 10 8 SWAA042824 120040929A335090083 BATTERY BOEING737 7372T4 1384492NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED C1 CHECK, FOUND CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. RESEATED CANNON PLUG AT BATTERY PER MM. 2L72 4F A16WE 20041008000902004100800090NM 2004 10 8 SWAA042825 120040929A55526959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29384SW 26590 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT AND BUSHING PER MM. 2L72 4F RTA16WE 20041008000912004100800091NM 2004 10 8 SWAA042826 120040929A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041008000942004100800094NM 2004 10 8 QXEA200400679 120040918A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM MAIN CABIN UNKNOWN A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09400QX 4030 THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND PERFORMED OPERATIONAL CHECKS. THE CHECKS WERE GOOD AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000982004100800098WP 2004 10 8 AALA20041000 120040927A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170425 49337 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D, 14D, AND 26D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D, 14D, AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041008000992004100800099NM 2004 10 8 AALA20040999 120040927A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219412W 53187 TAIL COMPARTMENT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR TAIL COMPARTMENT EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20041008001012004100800101NM 2004 10 8 QXEA200400650 120040907A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY DEFECTIVE A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09355PH1557314153 500 THE CREW OBSERVED AN INTERMITTENT SMOKE WARNING WHILE IN FLIGHT. THE SYSTEM TESTS NORMALLY. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 SMOKE DETECTOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008001022004100800102NM 2004 10 8 QXEA200400658 120040901A5753 FLAP TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - LEFT HAND NACELLE NR 3 OUTBOARD FLAP TRACK MOUNTING SUPPORT BEAM HAS A 1 INCH CRACK ALONG TOP ATTACH FLANGE, APPROXIMATELY 7 INCHES FROM AFT END. REPAIRED IAW HORIZON AIR EA 6-54-310 AND R/D 8/4-54-201. 2H72 4T RTA13NM 20041008001042004100800104NM 2004 10 8 QXEA200400663 120040831A5414 DOOR BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - AFT EDGE OF NR 1 ENGINE NACELLE DOOR 412BL NEW CRACKS AT SPOT WELDS. REMOVED CRACKED SECTION AND Z-MEMBER. FABRICATED NEW IAW RD 8/4-71-79. COMPLETED REPAIR IAW DHC-84 SRM 51-25-05-320-801, PAGE 201. 2H72 4T RTA13NM 20041008001052004100800105NM 2004 10 8 QXEA200400662 120040827A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - TRACK NR 11 HAS PITTING AND CORROSION FROM X46.0 TO X80.0. REPAIRED IAW HORIZON AIR EA 6-53-386 AND RD 8/4-53-971. 2H72 4T RTA13NM 20041008001092004100800109NM 2004 10 8 QXEA200400640 120040818A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - PANEL 622CT COUNTER SINKS HAVE FRETTING. REMOVED CORROSION FROM COUNTER SKINS ON FUEL PANEL 622CT USING SCOTCH BRITE. COMPLETED CLEANING FRETTING CORROSION USING SCOTH BRITE. MAPPED FOR ENGINEERING. REPLACED PANEL WITH NEW FROM STOCK. 2H72 4T RTA13NM 20041008001122004100800112NM 2004 10 8 QXEA200400644 120040817A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - COUNTERSINKS IN PANEL 522AT HAVE FRETTING. REMOVED CORROSION AND DAMAGE. NO MEASUREMENTS MADE. MAPPED COUNTERSINKS FOR ENGINEERING. HFEC INSPECTED BLENDED PANEL FOR CRACKS IAW D8/400 NDTM PART 1, 51-00-06/ NO CRACKS NOTED. INSTALLED NEW PANEL 522AT IAW DASH-8 400 AMM 57-11-01, PARAGRAPH 1-4A-D1, 2. 2H72 4T RTA13NM 20041008001142004100800114EA 2004 10 8 COMA0460546 120040928A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA 7134 LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041008001152004100800115EA 2004 10 8 COMA0460547 120040928A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA 7134 CARGO FLOOR LBL 27 HAS CORROSION. REPAIRED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-41-21. 2L72 4F RTA21EA 20041008001172004100800117NM 2004 10 8 SWAA042832 120040929A5755654645262N SKIN BOEING737 7375H4 138449DNM LT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 LEFT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED LEFT WING NR 4 GROUND SPOILER PER MM. 2L72 4F RTA16WE 20041008001182004100800118NM 2004 10 8 SWAA042827 120040929A53116546552 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 827, STRINGER 8L, CRACKED. REMOVED AND REPLACD FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041008001192004100800119NM 2004 10 8 QXEA20044681 120040920A2160 SWITCH DHAV DHC8 DHC8202 2809007NM OVERTEMP INOPERATIVE A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09348PH16763 484 LWS - FLIGHT 2192 - DURING DESCENT, THE FLT COMPT DUCT HOT CAUTION LIGHT ILLUMINATED. THE CHECKLIST WAS PERFORMED AND THE LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLIGHT SYSTEM DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008001212004100800121 2004 10 8 SWAA042872 420041004A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041012000012004101200001EU 2004 10 12 MALA040601 120040924A3350330151 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15428XJ 340B428 BATTERY PACK 3301-51, S/N 2061 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CAPACITY CHECK FAILED P/N 3301-31. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/27/04. 2L72 4T RTA52EU 20041012000022004101200002EU 2004 10 12 MALA040591 120040910A3350330131 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15407XJ 340B407 BATTERY POWER SUPPLY P/N 3301-51, S/N 1266 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CAPACITY CHECK FAILED. P/N 3301-31. UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/15/04. 2L72 4T RTA52EU 20041012000032004101200003EU 2004 10 12 MALA040590 120040909A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15403XJ 340B403 DURING SCHEDULED CAPACITY CHECK, BATTERY POWER SUPPLY P/N 3301-51, S/N 1317 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 AND UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/15/04. 2L72 4T RTA52EU 20041012000042004101200004EU 2004 10 12 MALA040596 120040918A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15506XJ E2314 BATTERY PACK 61-2275-1, S/N 9712156 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/24/04. 2H74 4F RTA49EU 20041012000052004101200005EU 2004 10 12 MALA040597 120040918A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15536XJ E2372 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK P/N 61-2274-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/21/04. 2H74 4F RTA49EU 20041012000072004101200007EU 2004 10 12 MALA040600 120040924A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15428XJ 340B428 BATTERY POWER SUPPLY P/N 3301-51, S/N 1358 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/24/04. 2L72 4T RTA52EU 20041012000082004101200008 2004 10 12 SWAA042906 420041006A2565D31354 SLIDE BOEING737 7373A4 1384585NM L1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C3 CHECK, FOUND L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041012000092004101200009EU 2004 10 12 MALA040572 120040922A2150 MOTOR SAAB SF340 340B 7860101EU A/C COMPRESSOR FAILED A MALAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15415XJ 340B415 DURING START OF THE RT ENGINE SMOKE WAS PRESENT IN THE REAR OF THE CABIN. CREW SHUT ENGINE DOWN AND DEPLANED PASSENGERS. MAINTENANCE DETERMINED SMOKE WAS CAUSED FROM SUPPLEMENTAL AIR. MAINTENANCE REPLACED COMPRESSOR MOTOR. 2L72 4T RTA52EU 20041012000112004101200011WP 2004 10 12 MWEA040182 120041001A3620 SLIP JOINT DOUG DC9 DC981 3022081WP TAIL LEAKING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31803ME 48029 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON. FOUND SLIP JOINT ON LEFT PACK LEAKING, REPOSITIONED SLIP JOINT. LEAK CHECKED GOOD. 2L72 4F A6WE 20041012000162004101200016EU 2004 10 12 MALA040588 120040908A33505521981 BATTERY SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL1599XJ 340A099 BATTERY PACK 61-0478-9, S/N 92 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CAPACITY CHECK FAILED. P/N 55-2198-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/24/04. 2L72 4T RTA52EU 20041004000102004100400010NM 2004 10 4 USAA040529 120040812A5320 INTERCOSTAL BOEING757 7572B7 1384964NM R1 THRESHOLD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND INTERCOSTAL CORRODED 3 SQUARE INCHES EMANATING FROM SCREW HOLES, THRESHOLD AT R1 DOOR. REMOVED AND REPLACED DOOR THRESHOLD INTERCOSTAL PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041004000192004100400019NM 2004 10 4 UIEA200400169 120040922A5711 SPAR BOEING747 747230B 1384889NM RT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 FOUND DURING SCHEDULED MAINTENANCE, CORROSION ON FRONT SPAR WEB, FSS 979.27, LOWER CHORD, LEFT SIDE. BLENDED OUT CORROSION WITH 125 RT FINISH. HFEC INSPECTED OPEN FASTENER HOLES, TO ENSURE DEFECT FREE CONDITION. FLAP PEEN BLENDED SURFACES. FABRICATED AND INSTALLED A 0.071 INCH THICK 7075-T6 DOUBLERS AND A FITTED FILLER. REPLACED THE RIB POST AT WS 972. (M) 2L74 4F A20WE 20041004000252004100400025EU 2004 10 4 USAA040564 120040909A5330 SKIN AIRBUSA319 A319112 3930323EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19762US11336 1358 PIT - FOUND SKIN DENTED 7 INCH BY 7 INCH BY .250 INCH DEEP, BETWEEN FRAME 4/5 AND STRINGERS 22 AND 23 IN RED STATIC PORT BAND. TEMPORARY REPAIR INSTALLED L ANGLES AND DOUBLER PER EA 79115. (M) 2L72 4F RTA28NM 20041004000262004100400026NM 2004 10 4 USAA040560 120040906A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US54937 22953 CLT - FOUND SKIN CRACKED 4.3125, LT SIDE FUSELAGE STATION 18 AT STATION 75. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M) 2L72 4F RTA16WE 20041004000292004100400029NM 2004 10 4 GAIA04092OP 120040914A5330 SKIN BOEING727 727223 1384074NM FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076809 19484 DURING PS CHECK, A 2 INCH CRACK WAS FOUND ON THE RIGHT SIDE OF THE NOSE WHEEL WELL AT FS 290. REPAIRED WHEEL WELL IAW THE 727 SRM CH 51-40-2 FIG 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 20041004000452004100400045NM 2004 10 4 USAA040545 120040819A5311 FRAME BOEING757 757225 1384959NM FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19605AU61650 22201 CLT - FOUND FRAME FLANGE DENTED AND CRACKED .5 INCH, FRAME FLANGE STATION 620 BETWEEN STRINGER 24L AND 25L. INSTALLED FRAME REPAIR ANGLE PER EA 95709. (M) 2L72 4F RTA2NM 20041004000532004100400053NM 2004 10 4 USAASB04122 120040911A335020121 POWER SUPPLY BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19375US 22954 PIT - FOUND MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 21 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK, P/N 2013-1A FOR AFFECTED SEAT ROWS. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 20041004000592004100400059NM 2004 10 4 USAA040534 120040811A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND FLOORBEAM CORRODED EMINATING FROM FASTENER HOLES, UPPER T-CHORD OF FLOORBEAM, STATION 324 AT RBL 53.5, RBL 57.5 AND RBL 59.09. CUT AND REMOVED DAMAGED SECTION OF TEE CHORD, FABRICATED REPLACEMENT PARTS AND INSTALLED PER EA 95729. (M) 2L72 4F RTA2NM 20041004000602004100400060NM 2004 10 4 USAA040535 120040806A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19610AU39309 27122 CLT - FOUND UPPER CHORD WITH CORROSION, EMINATING FROM FASTENER HOLES, FS 377 RBL 1, UPPER CHORD ON UPPER SURFACE. FABRICATED REPAIR CHORD PER SRM 53-00-51 FIG 203 AND EA 95751. (M) 2L72 4F RTA2NM 20041004000842004100400084CE 2004 10 4 T4C2004F00000 120040614A1430NAS464P26 BOLT CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO MLG BROKEN E T4CAO OTHER O OTHER NRNOT REPORTED 1 SO17567RS 1090 510032 THIS AIRCRAFT WAS STOPPED WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION, A BOLT NAS464P4-26 AND ADJUSTING SCREW 0841113-1 WERE BROKEN. UNSURE WHICH WAS BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOURS. (SO17200411551) 1L72 3O3 O A7CE E8CE 20041004000862004100400086CE 2004 10 4 T4C2004F00001 120040614A14300841113 SCREW CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO MCAULY3AF32C3AF32C87 GL MLG BROKEN E T4CAO OTHER O OTHER NRNOT REPORTED 1 SO17567RS 1090 510032 762395 THIS AIRCRAFT WAS STOPPED, WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION A BOLT NAS 464P4-26 AND ADJUSTING SCREW 0841113-1 WERE BROKEN. NOT SURE WHICH BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOURS. (SO17200411551) 1L72 3O3 O A7CE E8CE 5 CP22EA 20041004000912004100400091EU 2004 10 4 I7LA0002728 120040812A6420109013105115 TRUNNION AGUSTAA109 A109K2 0260502EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR OVERHEATED E I7LAO OTHER O OTHER NRNOT REPORTED 1 NM07901HC509 10033 UPON 25 HOUR INSPECTION, SIGNS OF HEAT NOTED. ENAMEL PAINT WAS BROWN-DISCOLORED. 1G72 3U3 URTH7EU E19EU 20041004001012004100400101EU 2004 10 4 USA2004F00077 120040531A2120 CART EMB ERJ170ERJ170100 EU GE CF34 CF34* NE CABIN ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19808MD 17000021 ON INITIAL CLIMB THE FLIGHT ATTENDANT INFORMED THE CAPTAIN THAT SHE SMELLED FUMES IN THE CABIN AND ALSO THOUGHT SHE SAW SMOKE. AS A PRECAUTION THE CAPTAIN RETURNED TO DEPARTURE AIRPORT. A NON EMERGENCY LANDING WAS MADE. MAINTENANCE RAN ENGINE ON GROUND AT IDLE WITH PACKS ON. NO EVIDENCE FOUND OF SMOKE OR BURNING ODOR. AIRSTART CART SOURCE OF SMELL IN CABIN. REMOVED AIR CART FROM SERVICE. 2L74 4F4 FRTA56NM E15NE 20041004001052004100400105NM 2004 10 4 SWAA042802 120040927A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 860, LBL 8 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041004001162004100400116NM 2004 10 4 AWXA200401036 120040918A2822568126713004 PUMP BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUEL BOOST INTERMITTENT A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28168AW5931311291 23629 EN ROUTE WITH LT CENTER FUEL TANK PUMP OFF AND RT CENTER FUEL TANK PUMP ON, CROSS FEED VALVE CLOSED, NR 2 ENGINE WAS DRAWING FUEL SLOWLY FROM RT CENTER TANK AND ALSO RT MAIN TANK, DIVERTED, DUE TO WEATHER. MAINTENANCE TROUBLESHOT FUEL SYSTEM; NO DEFECTS FOUND. WHEN AIRCRAFT ARRIVED AS A PRECAUTION THE RT CENTER FUEL TANK BOOST PUMP REPLACED IAW BMM 28-22-41, OPERATIONAL CHECK WAS GOOD. PROBLEM RECURRED, RT WING TANK BURNED FUEL CONTINUOUSLY BEFORE CENTER TANK WAS EMPTY. MX R & R ALL THREE RT FUEL TANK BOOST PUMP CHECK VALVES IAW BMM. TEST FOUND FUEL BOOST PUMP SLOW TO RE-PRIME DUE TO AN ERODED HOUSING. 2L72 4F4 FRTA16WE E2GL 20041004001172004100400117NM 2004 10 4 04FDEA02395 120040809A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLECORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.097. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001192004100400119NM 2004 10 4 04FDEA02397 120040809A5753ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, OB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.082, FINAL DIAMETER=1.097. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041004001332004100400133NM 2004 10 4 04FDEA01998 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 SEAT TRACK CROWN AT STA 1171, LBL 47.5 FOUND WORN. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I. 2L73 4F RTA22WE 20041004001392004100400139NM 2004 10 4 2004UALA00751 120040726A3350BPS73 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29196UA 28715 FIRST CLASS LEFT SIDE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY ASSY. 2L74 4F4 FRTA20WE E24NE 20041004001442004100400144NM 2004 10 4 HNAA0400086 120040921A3231858601 PSEU DHAV DHC8 DHC8201 2809001NM MLG INOPERATIVE A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07985HA 479 AFTER GEAR RETRACTION ALL GEAR DOOR INDICATED OPEN AND LF MAIN GEAR UNSAFE LIGHT ILLUM. PERFORMED ALT GEAR EXT AND RETURNED TO FIELD. INSP GEAR, NO DEFECTS NOTED. FOUND PSEU FAULTS WITH ALL GEAR DOOR AND LF MAIN GEAR. REMOVED AND REPLACED PSEU AND PERFORMED NEAR FAR CHECKED GOOD, SYS CHECKED GOOD. ACFT RELEASED FOR EVAL FLT DUE TO GEAR UNSAFE LIGHT AFTER GEAR RETRACTION. MX ACTION COMPLETE SUBJECT TO SAT EVAL FLT EVAL FLT SATISFACTORY. MORE INFO TO FOLLOW. 2H72 4T RTA13NM 20041005000152004100500015NM 2004 10 5 04FDEA02380 120040805A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.412" MATERIAL REMOVED = 0.003. REMAINING THICKNESS = 0.409. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041007000042004100700004EA 2004 10 7 QXEA200400692 120040929A5751 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 RT AILERON UPPER HALF OF LEADING EDGE HAS VARIOUS AREAS OF CHAFING FROM APPROXIMATELY WS 282.00 TO WS 353.00. REPAIRED IAW CRJ SRM 51-21-11 AND SRM 51-12-20. 2L72 4F RTA21EA 20041007000052004100700005NM 2004 10 7 SWAA042814 120040928A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 1016, LBL 1 TO RBL 37, CORRODED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041007000062004100700006 2004 10 7 SWAA042835 420040929A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000072004100700007NM 2004 10 7 SWAA042861 120041002A335065C27093 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041007000082004100700008 2004 10 7 SWAA042862 420041002A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29374SW 26582 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000092004100700009 2004 10 7 SWAA042863 420041002A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000102004100700010 2004 10 7 SWAA042864 420041003A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000122004100700012 2004 10 7 SWAA042866 420041003A2565 BOTTLE BOEING737 7373H4 1384600NM SLIDE DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 2481 23940 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE LOW PRESSURE IND. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000142004100700014NM 2004 10 7 SWAA042868 120041003A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 18 TO RBL 44, CORRODED. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20041007000312004100700031NM 2004 10 7 SWAA042846 120040930A2560PH22300L GLOWSTRIP BOEING737 7373T0 1384582NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND ALL PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED ALL PHOTOLUMINESCENT STRIPS PER EA. 2L72 4F RTA16WE 20041007000332004100700033NM 2004 10 7 SWAA042848 120040930A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING T/E FLAP PER MM. 2L72 4F RTA16WE 20041007000352004100700035NM 2004 10 7 SWAA042850 120040930A555265C2638415M ATTACH FITTING BOEING737 7373T0 1384582NM LT ELEVATOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND LT ELEVATOR TAB ATTACH LUG FOR INBOARD CONTROL ROD BROKEN. REMOVED AND REPLACED LEFT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20041007000732004100700073NM 2004 10 7 SWAA042818 120040928A335061047811 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29712SW 27846 DURING SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED OVERWING LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041007000742004100700074NM 2004 10 7 QXEA200400649 120040903A5297 WIRE BOMBDRDHC8 DHC8401 1390041NM PROX SENSOR DAMAGED A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09411QX6705 4055 GEG - FLIGHT 2427 - FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF AND CLIMBING, THE CREW RECEIVED A FUSELAGE DOOR WARNING LIGHT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE PROX SENSOR WIRE FOR AFT BAG DOOR FAULTY. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041007000752004100700075NM 2004 10 7 SWAA042873 120041004A27316552819 COMPUTER BOEING737 7373H4 1384600NM E/E COMPARTMENT FAULTY A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW29389SW 26592 AIR TURNBACK, DURING CLIMB ELEVATOR FEEL DIFF PRESSURE LIGHT ILLUMINATED FOR 10 MINUTES. LIGHT EXTINGUISHED AFTER 10 MINTES THEN ILLUMINATED AGAIN. LIGHT EXTINGUISHED ON DESCENT. HYDRAULIC PRESSURE AND QUANTITY NORMAL. REMOVED AND REPLACED MAIN HYDRAULIC RETURN FILTERS AND ELEVATOR FEEL COMPUTER PER MM. 2L72 4F RTA16WE 20041007000772004100700077NM 2004 10 7 SWAA042860 120041001A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29673AA 23251 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041007000792004100700079EA 2004 10 7 QXEA200400660 120040907A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 800 STUCK A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09601QX7067 10009 THE MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE AIRCRAFT AND LUBRICATED THE LATCH PINS AND PERFORMED OPERATIONAL CHECKS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041007000812004100700081WP 2004 10 7 AALA20041008 120040930A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2177421 49333 EMERGENCY LIGHT AT TAIL COMPARTMENT SLIDE HANDLE INOPERATIVE. RESPLICED WIRES FOR EMERGENCY LIGHT AT TAIL COMPARTMENT SLIDE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000832004100700083WP 2004 10 7 AALA20041006 120040930A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219409F 53121 DFW - EMERGENCY ESCAPE PATH LIGHTING AT ROWS 10 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING AT ROWS 10 THROUGH 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041007000852004100700085NM 2004 10 7 SWAA042838 120040930A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041007000872004100700087 2004 10 7 SWAA042840 420040930A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041007000892004100700089NM 2004 10 7 SWAA042842 120040930A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29698SW 23176 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500A + 2, STRINGER 10R, BS 500A + 10, STRINGER 10R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041008000012004100800001SO 2004 10 8 C2XA04IA126 120041005A3350B6245 LIGHT EMB 135 EMB135LR 3260305SO SERVICE DOOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714514 145303 IAH- FLIGHT 2621, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041008000052004100800005SO 2004 10 8 C2XA04BT102 120040927A3397 WIRE EMB 145 EMB145 3260210SO READING LIGHT LOOSE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2713964 145123 CREW REPORTED, SMOKE CAME FROM FIRST OFFICERS YOKE READING LIGHT AFTER LANDING. MAINTENANCE IN MSN DEACTIVATED FIRST OFFICER'S CHARTHOLDER LIGHT AND RELEASED THE AIRCRAFT IAW MEL 33-10-00 CAT-C CONTROL 046503. UPON ARRIVAL INTO EWR MAINTENANCE SECURED CHARTHOLDER WIRES AND OPS CHECKED LIGHTS, OPS CHECKED GOOD IAW EMB145 MM 33-11-01. NO SMOKE NOTED. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041008000232004100800023NM 2004 10 8 CALA0400653 120040929A5330143N3650 SKIN BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2733103 27293 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 760-780 BETWEEN S17L AND 18L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 204. A DIP WAS ISSUED TO REPEAT INSPECTION AT A THRESHOLD OF 37,500 FLIGHT CYCLES WITH SUBSEQUENT INSPECTION EVERY 3,000 FLIGHT CYCLES. 2L72 4F RTA2NM 20041008000312004100800031NM 2004 10 8 QXEA00668 120040912A33506104789 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09379PH8871 530 AFT TWO LIGHTS OF ROW 1 FLOOR EMERGENCY LIGHTS ARE INOP. MAINTENANCE INSTALLED NEW FLOOR LIGHT STRIP WITH NO HELP. CHECKED VOLTAGE AT BATTERY POWER SUPPLIES AND FOUND PS4 DISCHARGED. REPLACED BATTERY POWER SUPPLY PS4. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000322004100800032NM 2004 10 8 QXEA200400675 120040914A5270 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT PAX OUT OF ADJUST A QXEAK NONE O OTHER ININSP/MAINT 1 NM09416QX 4083 AFT PASSENGER DOOR WILL NOT CLOSE. FOUND AFT PASSENGER DOOR OFF CENTER, RE-CENTERED DOOR AS REQUIRED. OPENED AND CLOSED RIGHT HAND AFT PASSENGER DOOR SEVERAL TIMES. OPERATIONAL CHECK GOOD. NO OTHER DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000362004100800036NM 2004 10 8 P5CA0401236 120041001A5315 FLOORBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT FLOORBEAM LBL 38 STA 1980 IS CRACKED. REMOVED DAMAGE AREA, REPAIRED ANGLE, PRIMED & TREATED PER SRM 51-40-03. 2L74 4F4 F A20WE E20EA 20041008000482004100800048WP 2004 10 8 CALA0400664 120041005A5280593058317 BEAM DOUG DC9 DC982 3022082WP LT MLG DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772824 49484 LEFT MAIN LANDING GEAR DOOR PAN CRACKED AFT OUTBOARD SIDE OF DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-05 FIG 28. 2L72 4F A6WE 20041008000522004100800052NM 2004 10 8 QXEA200400637 120040814A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 LITE FRETTING IN COUNTER SINKS OF PANEL 622AT. REPAIRED IAW DHC-8-400 SRM 51-26-10 AND AMM 57-11-01-400-801, PAGE 408-409, PARAGRAPH 4 A, C, D (1-2). 2H72 4T RTA13NM 20041008000602004100800060NM 2004 10 8 QXEA200400655 120040831A5414 DOOR BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - FORWARD AND AFT EDGES OF NR 2 ENGINE NACELLE DOOR 422BL HAS CRACKS AT AFT WELDS. CUT OFF DAMAGED SECTION OF SKIN AT AFT EDGE LAND CHECKED CUT EDGE FOR CRACKS. NO CRACKED NOTED. FABRICATED NEW SKIN FROM TITANIUM. REPAIRED IAW HORIZON AIR EA 6-71-157. 2H72 4T RTA13NM 20041008000662004100800066WP 2004 10 8 ABXA040343 120040923A5320595603423 INTERCOSTAL DOUG DC9 DC941 302207NWP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 INTERCOSTAL END FITTING CRACKED AT STA 1072, LEFT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20041008000732004100800073NM 2004 10 8 SWAA042887 120041005A57536546435274 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20041008000882004100800088NM 2004 10 8 SWAA042823 120040929A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29740SW 29276 EEPLS COVER AT ROW 8 DEF, LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041008000922004100800092NM 2004 10 8 SWAA042821 120040928A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29301SW 22941 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 14L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041008000952004100800095EA 2004 10 8 QXEA200400680 120040917A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 800 STUCK A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09601QX7120 10009 DEN - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR STICKS WHEN TRYING TO OPEN. MAINTENANCE INSPECTED THE DOOR AND LUBRICATED THE DOOR LATCH PINS AND LATCH CAMS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041008000962004100800096NM 2004 10 8 AALA20040996 120040924A3350 BATTERY PACK BOEING767 767323 1385205NM EMERGNECY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139367 25194 SFO - EMERGENCY LIGHTS ON LEFT SIDE OF FIRST CLASS AND IN LAVATORY INOPERATIVE. REPLACED BATTERY PACK M735 AND SEAT 2A AFT LIGHT ASSEMBLY FOR EMERGENCY LIGHTS ON LEFT SIDE OF FIRST CLASS AND IN LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041008000972004100800097NM 2004 10 8 AALA20040997 120040924A3350BPS73 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21199AN 32393 SEAT MOUNTED AND EXIT DOOR EMERGENCY LIGHTS AFT OF OVERWING INOPERATIVE. REPLACED BATTERY PACKS IN AFT SECTION FOR SEAT MOUNTED AND EXIT DOOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041008001002004100800100 2004 10 8 AALA20040993 420040923A2565 BOTTLE BOEING757 757223 1384957NM ESCAPE SLIDE FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW21614AA 24490 MIA - L1 DOOR SLIDE PARTIALLY DEPLOYED. SLIDE FELL ONTO JETBRIDGE AND DID NOT OPEN WITH ASSIST BOTTLE DISCHARGE. INSPECTED FORWARD ENTRY DOOR HINGES AND DOOR FRAME. NO DAMAGE NOTED. REINSTALLED DOOR SLIDE ASSEMBLY AND REPLACED L1 DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041008001062004100800106NM 2004 10 8 QXEA200400664 120040906A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - NR 11 SEAT TRACK HAS PITTING AND CORROSION FROM X46.0 TO X80.0. REPAIRED IAW RD 8-4-53-884 AND RD 8/4-53-971. 2H72 4T RTA13NM 20041008001072004100800107NM 2004 10 8 QXEA200400665 120040908A5522 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 300 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - LEFT HAND ELEVATOR TRAILING EDGE LOWER SURFACE IS DENTED APPROXIMATELY 10 INCHES FROM INBOARD END. REMOVED PAINT AND MAPPED FOR ENGINEERING. REPAIRED IAW RD 8/4-55-174 AND HORIZON AIR EA 6-55-83. 2H72 4T RTA13NM 20041008001202004100800120NM 2004 10 8 QXEA200400681 120040920A2160 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09348PH16763 484 LWS - FLIGHT 2192 - DURING DESCENT, THE FLT COMPT DUCT HOT CAUTION LIGHT ILLUMINATED. THE CHECKLIST WAS PERFORMED AND THE LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLIGHT SYSTEM DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041012000102004101200010NM 2004 10 12 MWEA040181 120041001A3397C930213920 WIRE HARNESS BOEING717 717200 1383700NM COCKPIT CHAFED A MWEAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 GL31912ME 55175 EMERGENCY LIGHTS CHARGING CIRCUIT BREAKER TRIPPED. FOUND WIRE BUNDLE CHAFING ON CORNER OF RIGHT LAVATORY OXYGEN PNEUMATIC SYSTEM CONTROLLER, REPAIRED THREE WIRES. 2L72 4F TRA6WE 20041012000122004101200012WP 2004 10 12 MWEA040177 120040927A533059360071 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 DURING EVALUATION OF WATCH ITEM 7130 THE DENT NO LONGER MEETS THE REQUIRMENTS OF CONDITION, DUE TO THE DENT BEING WITHIN 1 INCH OF LONGERON 20 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041012000132004101200013WP 2004 10 12 MWEA040178 120040928A5543 SKIN DOUG DC9 DC982 3022082WP RUDDER TAB CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RUDDER TAB HAS A SMALL AREA OF CORROSION/DELAMINATION ON LEFT BOTTOM FORWARD SIDE. CUT OUT DAMAGED AREA AND INSTALLED LEADING EDGE. 2L72 4F A6WE 20041012000142004101200014EU 2004 10 12 MALA040540 120040818A2150M4401D8A MOTOR SAAB SF340 340B 7860101EU AIR CONDITIONER ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL15427XJ 340B427 WHILE ON APPROACH TO YKF NOTICED A SLIGHT ODOR OF SOMETHING POSSIBLY BURNING. AFTER SHUTTING DOWN AT YKF OPENED THE COCKPIT DOOR AND FOUND A NOTICABLY STRONG ODOR IN THE CABIN. MAINTENANCE FROM LP 1033139 REMOVED AND REPLACED MOTOR SUPP AC, RAN SUPP AC OPS CHECK GOOD, NO ODOR AT THIS TIME. S/N OFF 663, SN ON 269. 2L72 4T RTA52EU 20041012000172004101200017EU 2004 10 12 MALA040593 120040914A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15501XJ E2208 BATTERY PACK P/N 61-2275-1, S/N 9909154 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED, AND PASSED CMM CHECKS. A/C RETURNED TO SERVICE 9/18/04. 2H74 4F RTA49EU 20041012000182004101200018EU 2004 10 12 MALA040594 120040914A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15522XJ E2347 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK 61-2274-1 AFTER CAPACITY CHECK FAILED. UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/24/04. 2H74 4F RTA49EU 20041012000202004101200020EU 2004 10 12 MALA040602 120040924A3350330131 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15428XJ 340B428 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY AFTER CAPACITY CHECK FAILED. P/N 3301-31 UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/28/04. 2L72 4T RTA52EU 20041012000222004101200022 2004 10 12 MALA040583 420040910A3416641119001 ALTIMETER SAAB SF340 340B 7860101EU FIRST OFFICERS MALFUNCTIONED A MALAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL15452XJ 340B452 DURING CLIMBOUT OF MSP, NOTICED THE F/O'S ALTIMETER BEGIN TO LAG ABOUT 500 FEET BEHIND THE CAPTAINS ALTIMETER. WHEN LEVELED OUT AT 7000 FEET THE F/O ALTIMETER READ ABOUT 400 FEET LOWER THAT CAPTAINS AND STANDBY ALTIMETERS. MAINTENANCE REPLACED F/O'S ALTIMETER P/N ON-OFF 64111-900-1, S/N ON 2519, S/N OFF 4069. NR 2 PITOT/STATIC SYSTEM OPS/LEAKS CHECSK GOOD IAW SF340 MM CH 34. 2L72 4T RTA52EU 20041012000242004101200024NM 2004 10 12 SWAA042907 120041006A5330654576972 SKIN BOEING737 7373Q8 1384670NM KEEL CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED SERVICE CHECK, FOUND KEEL BEAM SKIN AT BS 500, CORRODED. REMOVED AND REPLACED SKIN SECTION PER EA. 2L72 4F RTA16WE 20041012000252004101200025NM 2004 10 12 SWAA042908 120041006A53306574447 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 877, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041012000282004101200028NM 2004 10 12 SWAA042911 120041006A555165C25798 FITTING BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C3 CHECK, FOUND LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT NR 1 ELEVATOR TABS HINGE HARDWARE PER MM. 2L72 4F RTA16WE 20041012000292004101200029EU 2004 10 12 MALA040585 120040923A2920 PTU BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM OVERHEATED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15524XJ E2349 APPROX 25 MIN INTO FLIGHT AT ALT 29000 THE GREEN SYSTEM HIGH TEMP CAUTION LIGHT ILLUMINATED. COMPLETED QRH AND SHUT GREEN SYSTEM OFF. HIGH TEMP LIGHT WENT OFF ABOUT A MINUTE LATER. MAINTENANCE INSPECTED HYD SYSTEM, NO LEAKS NOTED. PERFORMED DECAY TEST, OK. NOTED PTU OVERTEMPING PRESSURE CYCLING ERRATICLY. REPLACED PTU IAW 29-20-17, FAULT ISOLATION 29-30-00 FIGURE 111. TEST FLIGHT SATISFACTORY. COMPLETED POST FLIGHT WALKAROUND, NO DISC NOTED AT THIS TIME. 2H74 4F RTA49EU 20041012000302004101200030EU 2004 10 12 MALA040586 120040926A2913521449 PUMP BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 GREEN SYS HYD HI TEMP LIGHT ILLUMINATED ON FLIGHT PERFORMED QRH, NOTIFIED DISPATCH AND MAINTENANCE CONTROL AND RETURNED TO MSP. MAINTENANCE T/S AND SUSPECT NR 3 EDP P/N 521449, S/N OFF F9727550, S/N ON F1217006ACH, IAW AMM 29-10-17, 201 OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20041012000312004101200031EU 2004 10 12 MALA040579 120040922A2910HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15524XJ E2349 GREEN HYD HI TEMP OCCURRED EN ROUTE QRH WAS FOLLOWED AND HI TEMP LIGHT WENT OUT AFTER 30 SEC. AIR RETURN TO GPT. MAINTENANCE REPLACED GREEN ISOLATION VALVE P/N ON OFF HTE9531-3, S/N ON FR052A, S/N OFF FR046BA IAW AMM 29-10-14 201, OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20041012000322004101200032EU 2004 10 12 MALA040578 120040917A2910HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15526XJ E2351 EN ROUTE TO ATL, YELLOW HYD SYSTEM HI TEMP LIGHT ILLUMINATED. FOLLOWED QRH AND RETURNED TO MEM. MAINTENANCE REMOVED & REPLACED NR 2 ISOLATION VALVE P/N HTE9531-3 IAW RJ MM CH 29-10-14 201. RAN A/C ON GROUND 30 MINUTES, ACTUATING ALL HYDRAULICALLY ACTUATED COMPONENTS EXCEPT LANDING GEAR, NO HI TEMP ILLUMINATION NOTED. LEAK CKS ARE GOOD. A/C OK FOR SERVICE. 2H74 4F RTA49EU 20041012000332004101200033NM 2004 10 12 C1HA200497012 120040912A5754 SPAR BOEING727 727270 138408PNM NR 3 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 3 SLAT FWD SPAR CRACKED AT SLAT STA 177 FWD OF ACTUATOR CONNECTION. INSTALLED REPAIR DOUBLERS. 2L73 4F RTA3WE 20041012000342004101200034NM 2004 10 12 C1HA200497014 120040913A5754 SKIN BOEING727 727270 138408PNM NR 4 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 4 SLAT LEADING EDGE LOWER SKIN IS CRACKED AT AERODYNAMIC FENCE AFT LOWER MOUNT AREA (MARKED). REPAIRED PER SRM. 2L73 4F RTA3WE 20041012000362004101200036WP 2004 10 12 MWEA040157 120040908A57309919459509 PANEL DOUG DC9 DC982 3022082WP RT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 RIGHT WING TOP PANEL NR 1428 HAS INTERGRANULAR CORROSION AROUND ONE FASTENER. FABRICATED AND INSTALLED PANEL. 2L72 4F A6WE 20041012000372004101200037WP 2004 10 12 MWEA040158 120040908A57309919459509 PANEL DOUG DC9 DC982 3022082WP LT WING CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LEFT WING UPPER SURFACE PANEL 1325C HAS INTERGRANUALAR CORROSION AROUND SEVERAL FASTENERS. FABRICATED AND INSTALLED PANEL. 2L72 4F A6WE 20041012000382004101200038NM 2004 10 12 C1HA200497016 120040925A5754 SKIN BOEING727 727270 138408PNM NR 4 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 PLACES AT AERODYNAMIC FENCE MOUNTING AREA (MARKED). REPAIRED 2 CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1. TRANSFERRED TO LOG PAGE B 20238 ITEM 3 DUE TO RII INSPECTION RII ACCOMPLISHED. 2L73 4F RTA3WE 20041012000392004101200039WP 2004 10 12 MWEA040183 120041004A2160 GASKET DOUG DC9 DC981 3022081WP TAIL CONE FAILED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31803ME 48029 GEAR RETRACTION MASTER WARNING AND TAIL COMPARTMENT HIGH TEMPERATURE ILLUMINATED. FOUND BLOWN GASKET, REMOVED AND REPLACED GASKET AT SUPPLY TEMPERATURE SENSOR. 2L72 4F A6WE 20041012000402004101200040NM 2004 10 12 SWAA042896 120041005A552365C35943 ROD END BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29632SW 27707 DURING SCHEDULED C4 CHECK, LT AND RT ELEVATOR TABS FAILED FREEPLAY CHECK. REMOVED AND REPLACED BOTH NR 1 ELEVATOR TABS ROD END HARDWARE PER MM. 2L72 4F RTA16WE 20041012000422004101200042NM 2004 10 12 SWAA042898 120041005A53156935366 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND FLOORBEAM SHEAR WEB AT BS 500, LBL 69, CORRODED. REMOVED AND REPLACED FLOORBEAM SHEAR WEB PER SRM. 2L72 4F RTA16WE 20041012000432004101200043 2004 10 12 SWAA042899 420041005A25656557463 FITTING BOEING737 7373H4 1384600NM SLIDE GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FWD AND AFT FITTIGS PER SRM. 2L72 4F RTA16WE 20041012000442004101200044NM 2004 10 12 SWAA042900 120041006A27506943533 CONTROL CABLE BOEING737 7373Y0 1384671NM LT WING TE FLAPBROKEN A SWAAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW29308SA 23498 UPON DEPLOYMENT OF FLAPS 30, AIRCRAFT ROLLED TO THE LEFT, YOKE DEFLECTION TO THE RIGHT APPROX 40 DEGREES. REMOVED AND REPLACED LT WING LT INBOARD T/E FLAP BOOM CABLES PER MM. 2L72 4F RTA16WE 20041012000452004101200045NM 2004 10 12 SWAA042901 120041006A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 22R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041012000462004101200046WP 2004 10 12 MWEA040166 120040915A3150 WARNING LIGHT DOUG DC9 DC982 3022082WP TAIL CONE FALSE INDICATIONA MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31810ME 48072 TAIL CONE ANNUCIATOR ILLUMINATED. INSPECTED TAIL CONE LOCK/LATCH INSTALLATION, RESET CABLE LOCKBALL. OK FOR CONTINUED SERVICE. 2L72 4F A6WE 20041012000472004101200047SO 2004 10 12 C2XA04SH497 120040922A531314525771011 STRINGER EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713979 145181 SHV - DURING C-CHECK STRINGER 17L WAS FOUND TO BE CORRODED BETWEEN FRAME 61 TO 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041012000492004101200049SO 2004 10 12 C2XA04SH500 120040923A532014521700005 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929 145009 SHV - DURING C-CHECK THE LEFT HAND OMEGA SHAPE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000502004101200050SO 2004 10 12 C2XA04SH501 120040923A532014530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929 145009 SHV - DURING C-CHECK THE LT HAND OMEGA BEAM ASSEMBLY WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000512004101200051SO 2004 10 12 C2XA04SH502 120040923A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716571 145633 SHV - DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM HAT SECTION IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041012000542004101200054SO 2004 10 12 C2XA04TY165 120040922A521014524000001 STOP EMB 145 EMB145ER 3260211SO PAX DOOR ELONGATED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716927 145006 DURING SCHEDULED INSPECTION THE TWO UPPER COMMON TO MAIN DOOR STOPS AT FRAME 18 AND STRINGER 61 WERE ELONGATED. OVERSIZED HOLES, AND REWORKED PER ED5310-01291. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041012000562004101200056SO 2004 10 12 C2XA04BT101 120040921A3350 STUD EMB 145 EMB145XR 3260214SO EMERGNECY LIGHT CORRODED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2721144 145741 CREW REPORTED, EMERGENCY LIGHTS CAME ON WHEN SIDE WALL CEILING LIGHTS ARE TURNED ON. MAINTENANCE FOUND GROUND STUD GS8008DC TO BE CORRODED. REBONDED STUD IAW EMB145 33-50-50. AFTER REPAIR FOUND NR 3 BATTERY PACK FOR EMERGENCY LIGHTS POSITION THREE WAS DISCHARGED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK POSITION NR 3. OPS CHECKED EMERGENCY LIGHTING SYSTEM GOOD IAW EMB145 33-50-04. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041012000572004101200057SO 2004 10 12 C2XA04SH511 120041003A532014520380411 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2734111 145659 DURING VISUAL INSPECTION AT C-CHECK THE CENTER OMEGA BEAM WAS CORRORDED AT FRAME 20. REMOVED AND REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041012000632004101200063SO 2004 10 12 C2XA04BT100 120040922A1430 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 DURING SERVICE AND ROUTINE INSPECTION ON RON BTV, MAINTENANCE FOUND SEVERAL FORWARD CABIN EMERGENCY LIGHTS AND LT HAND FORWARD EXTERNAL EMERGENCY LIGHTS INOPERATIVE IN ALL MODES. RESECURED CONNECTOR TO NR 1 EMERGENCY LIGHT BATTERY AS REQUIRED, OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041012000652004101200065WP 2004 10 12 MWEA040167 120040919A3260 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP MLG OUT OF ADJUST A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31809ME 48071 RIGHT LANDING GEAR INDICATORS REMAINED RED, THE RED GEAR LIGHT WENT OUT IN ABOUT 10 MINUTES. CONFIRMED CORRECT GAP AT RIGHT GEAR UP PROXIMITY SENSOR, ADJUSTED SHIMMING TO MEET REQUIREMENTS, PERFORMED ADJUSTMENT TEST. OPERATIONS CHECK GOOD. 2L72 4F A6WE 20041012000662004101200066WP 2004 10 12 MWEA040163 120040914A523059101419 PAN DOUG DC9 DC982 3022082WP AFT CARGO CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 AFT CARGO DOOR OUTER PAN IS CRACKED APPROXIMATELY ONE INCH BELOW AFT DOOR. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041012000672004101200067WP 2004 10 12 MWEA040164 120040914A5330591022887 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 OUTWARD DENT IN FUSELAGE AT STATION 1342 1.5 INCHES BELOW LONGERON 7 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041012000682004101200068WP 2004 10 12 MWEA040170 120040921A531099115233 SHEAR TIE DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 SHEAR TIE AT STATION 294 ABOVE LONGERON 17 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED NEW FORMER. 2L72 4F A6WE 20041012000692004101200069SO 2004 10 12 C2XA04SH504 120040927A33501317 LAMP EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714516 145323 SHV - DURING A SERVICE CHECK THE LEFT EXTERIOR EMERGENCY LIGHT FORWARD OF THE LEFT WING WAS FOUND BLOWN. MAINTENANCE REPLACED THE AFFECTED LAMP IAW EMB 135AMM 33-50-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000702004101200070SO 2004 10 12 C2XA04CL097 120040922A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAO OTHER L NO TEST NRNOT REPORTED 1 SW2713965 145125 CLE FLIGHT 2863, THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHTS AND (2) FLOOR STRIPS INOPERATIVE. MAINTENANCE RESET ELECTRICAL POWER AND THE SYSTEM OPERATIONAL TEST WAS GOOD. 2L72 4F RTT00011AT 20041012000712004101200071SO 2004 10 12 C2XA04IA118 120040909A335066367 LIGHT EMB 145 EMB145ER 3260211SO CABIN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 DURING REFLIGHT INSPECTION THE CREW REPORTED THE SECOND AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTION ON THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED GOOD IAW EMB-145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000742004101200074NE 2004 10 12 DJFA2004021 220041006A7261 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT SHUTDOWN E DJFAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 EA23583CW4356 13 5600123 PCE108513 CREW REPORTED, MASTER WARNING & LT OIL PRESS WARNING LIGHTS ILLUMINATED. LT OIL PRESS ZERO. LT ENGINE SECURED AN APPROPRIATE CHECKLIST ACCOMPLISHED. ATC NOTIFIED LT ENGINE SHUTDOWN & PRIORITY REQUESTED. AT 3,000 FT, RT ENG PULLED BACK TO 65 PERCENT N2 & OIL PRESS DROPPED TO 50 PSI IN YELLOW ARC. THE RT ENGINE N2 SET BACK TO APPROX 75 PERCENT, & OIL PRESSURE HAD RETURNED TO ABOVE 60 PSI, IN THE GREEN ARC. AN EMERGENCY THEN DECLARED, & AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED LT ENG RELIEF VALVE HOUSING PN 3108036-01R, 2 CHECK VALVES PN 3119587-01, AND REPLACED OIL FILTER FOR ANALYSIS. OIL PRESS FOR RT ENGINE FOUND WITHIN LIMITS, & DISCREPANCY COULD NOT BE DUPLICATED. A/C RETURNED TO SERVICE. 2L72 4F4 FRTA22CE E25EA 20041012000772004101200077WP 2004 10 12 04FDEA02436 120040811A2432 CONTROL UNIT DOUG MD10 MD1010F 3022112WP BATTERY MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25391FE 46625 IN CRUISE FLIGHT RECEIVED BATTERY DISCHARGING ALERT, BATTERY VOLTAGE WAS 29V. DIVERTED TO TPA. AFTER LANDING GOT: BATTERY CHARGER INOP ALERT. FACT: TROUBLESHOT PER FIM 24-30-01. REMOVED AND REPLACED EPCU PER MM 24-08-01-4. PERFORMED RTS PER MM 24-08-01-5. REMOVED AND REPLACED RELAY R2-5784 PER SMP AS PRECAUTIONARY. 2L73 4F RTA22WE 20041012000782004101200078EU 2004 10 12 04FDEA02437 120040811A5320 DUMMY RAIL AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 UPPER MAIN CABIN BETWEEN D & E HAS 3EA DUMMY TRACK WITH CORROSION (LEVEL 2) AND 1EA DUMMY TRACK CRACKED (2 INCHES IN LENGTH) BETWEEN FR 52 AND 53. REMOVED AND REPLACED 4EA DUMMY TRACKS. 2L72 4F RTA35EU 20041012000792004101200079EU 2004 10 12 04FDEA02438 120040811A5320 DUMMY RAIL AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 UPPER MAIN CABIN FR48 BETWEEN TRACK D & E HAS 1EA DUMMY TRACK WITH CORROSION BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DUMMY TRACK IAW A310 SRM 51-72-10. 2L72 4F RTA35EU 20041012000822004101200082WP 2004 10 12 04FDEA02478 120040814A5320ACA382014 INTERCOSTAL DOUG DC10 DC1010F 3022111WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25366FE 46602 NR 3 AC BAY DOOR CTR VERTICAL FRAME CRACKED APPROX 12 INCHES FROM TOP OF DOOR. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-35-01 & SRM 51-33-01 AT MAE. 2L73 4F A22WE 20041012000832004101200083WP 2004 10 12 04FDEA02359 120040804A3260 WARNING LIGHT DOUG DC10 DC1030 3023501WP MLG FALSE INDICATIONA FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25308FE 48297 RT MAIN GEAR LIGHT ON S/O PANEL SHOWED UNSAFE AFTER GEAR RETRACTION. F/O PANEL SHOWED NORMAL. IAW RED TABS RECYCLED LANDING GEAR. LANDING GEAR EXTENDED NORMAL WITH 4 GREEN ON BOTH PANELS. FOLLOWING RETRACTION RT MAIN RED LIGHT ON S/O PANEL STILL STAYED ILLUMINATED. ALL GEAR LIGHTS ON F/O PANEL OUT. APPROX 35 MIN INTO FLIGHT RED LIGHT ON S/O PANEL WENT OUT. ALL LIGHTS TEST NORMAL. BITE CHECK ON PROX BOX, NO FAULTS. MEASURE RT MLG UP LOCKOUT OF LIMITS AND ADJUSTED IAW DC1030AMM 32-34-03-2. OK TO CONTINUE. 2L73 4F A22WE 20041012000842004101200084EU 2004 10 12 04FDEA02361 120040804A2612420812000 FIRE LOOP AIRBUS300 A300F4605R 3930327EU NR 1 ENGINE MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25659FE 757 ON CLIMBOUT PASSING APPROX 3,000 FT MSL RECEIVED ECAM ALERT FOR B-LOOP FAULT ON NR 1 ENGINE. CONTINUED CLIMB TO 11,000 MSL AND SLOWED A/C TO TROUBLESHOOT, DURING CLIMB FAULT LIGHT FLICKERED A COUPLE OF TIMES AND THEN REMAINED STEADY. ACCOMPLISHED ECAM PROC, AND TURNED LOOP OFF, SINCE A-LOOP WAS ALREADY DEFERRED DECISION WAS MADE TO RTB. NO FURTHER ACTIONS REQUIRED. *S/D* REMOVED AND REPLACED LOWER B-LOOP FIRE DETECTION HARNESS REF MM 26-12-12-04 02. OPS CHECKED GOOD. OK FOR SERVICE. 2L72 4F RTA35EU 20041012000862004101200086 2004 10 12 04FDEA02498 420040818A34174045053914 ADC AIRBUS310 A310203 3930313EU NR 2 MALFUNCTIONED A FDEAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SO25427FE3124 3124 362 AT 80 KTS THE F/O CALLED NO AIRSPEED. REJECTED T/O MAX SPEED 85 KTS. F/O HAD NO AIRSPEED INDICATIONS ON PFD, F/O PITOT PROBE BAGGED AND STATIC LINE PURGED WITH DRY N2 FROM NR 2 ADC, NO BLOCKAGE OR CONTAMINATION FOUND. CHANGED NR 2 ADC PER AMM SUPPLEMENT 34-11-34-4. NR 2 ADC OPERATIONAL TEST PER AMM 34-10-00-5-01, CHECKS SERVICEABLE. PREMATURE REMOVAL/INSTALLATION OFF MFG 4045053-914. 2L72 4F RTA35EU 20041012000892004101200089WP 2004 10 12 04FDEA02580 120040830A5248AKC7011 HINGE DOUG DC10 DC1010 3022110WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25366FE 46602 COMPLY WITH EA 8-5240-80594 DOORS SERVICE TAILCONE PATIO DOOR HINGE REPAIR P/N AKC7011 (RHS). COMPLIED WITH E/A/8-5240-80594. 2L73 4F A22WE 20041012000922004101200092NM 2004 10 12 04FDEA02552 120040823A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FRAME DAMAGED AT BS 1166, BETWEEN STRINGER 3 AND 4 RT. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 1166 BETWEEN STR 3 & 4 IAW SRM 51-40-3. 2L73 4F RTA3WE 20041012000942004101200094EU 2004 10 12 04FDEA02554 120040824A5313A5361056722400 STRINGER AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25421FE 342 FUSELAGE STRINGER 44 LT FRAME 13A TO 16A FOUND CORRODED AT MULTIPLE LOCATIONS REF SRM 53-10-00 FIG 102. CORROSION IS OUT OF LIMIT. (OPEN) 2L72 4F RTA35EU 20041012000952004101200095EU 2004 10 12 04FDEA02558 120040824A3230A252791 SEQUENCE VALVE AIRBUS310 A310203 3930313EU MLG MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25442FE 353 ON INITIAL TAKEOFF RETRACTED GEAR AND LT MLG REMAINED DOWN AND LOCKED WITH RED UNLOCK LIGHT ILLUMINATED ON BOTH LANDING GEAR PANELS. PLACED GEAR HANDLE DOWN AND GOT 3 GREEN NO RED LANDED UNEVENTFUL SYSTEM 1 SELECTED. PER FLIGHT CREW DEBRIEF, THE DOOR OPEN LIGHT WAS NOT ILLUMINATED AT ANY POINT DURING THE ATTEMPTED GEAR RETRACTION OR THE SUBSEQUENT GEAR EXTENSION. PERFORMED MEMORY RECALL TEST ON PROXIMITY DETECTOR UNIT WITH NO FAULTS RECORDED. ALSO PERFORMED SYSTEM TEST ON SAME UNIT WITH RESULTS COMING BACK NORMAL. TROUBLESHOOTING TO CONTINUE. PERFORMED GENERAL ADJ/TEST PER A310-200 COMPLETED MAIN GEAR SEQUENCE VALVE PER A310-200 MM 32-31-37-4. PERFORMED GEAR SWING INDICATIONS NORMAL. 2L72 4F RTA35EU 20041012000962004101200096EU 2004 10 12 04FDEA02559 120040824A2910 O-RING AIRBUS300 A300B4605R 3930308EU HYD SYSTEM TORN A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO25659FE 757 AT 100 NM FROM GDL, LOST GREEN HYDRAULIC SYSTEM, GRAVITY GEAR EXTENSION AND LANDING NORMAL. PUMPS OFF AT 2300 PSI. FOUND EVIDENCE OF LEAKAGE ON ENGINE NR 1 PYLON. AFTER CLEANANCE AND INSPECTION FOUND GREEN PRESSURE SW LEAKING HYD DUE TO O-RING FAILURE, REPLACED O-RING IAW 29-11-62-4, SERVICED GREEN HYD SYS IAW AMM 12-12-29-0, CLEANED GREEN HYD SYS PUMP DELIVERY FILTER IAW AMM 29-11-42-3 AND GREEN SYS PUMP CASE DRAIN FILTER IAW AMM 29-11-36-3-02. RESTORED FREE FALL EXTENSION SYSTEM IAW AMM 32-33-00-2. RAN ENG NR 1 IAW JRH 5A, FOR 15 MINUTES, SHUT DOWN ENGINE AND INSPECTED PYLON AREA FOR LEAKS. NO LEAKS FOUND, GREEN HYD FLUID LEVEL AND PRESSURE INDICATIONS WERE NORMAL. OK FOR SERVICE. 2L72 4F RTA35EU 20041012000992004101200099NM 2004 10 12 C1HA200479002 120040708A5320 INTERCOSTAL BOEING727 727225 1384077NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15679MG 22557 INTERCOSTAL BETWEEN STA 1148-1166 AND STR 28L TO 27L IS CORRODED. 2L73 4F A3WE 20041012001002004101200100NM 2004 10 12 C1HA200479001 120040708A5312 BULKHEAD BOEING727 727225 1384077NM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15679MG 22557 LEFT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD UPPER CHORD IS CRACKED AT O/B CORNER, STA 950 BL 60L. 2L73 4F A3WE 20041012001012004101200101NM 2004 10 12 04FDEA02495 120040817A5510ALC80552 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - RT OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. REPAIR COMPLIED TO FEDEX EA 1-5510-80321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - RIGHT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. 2L73 4F RTA22WE 20041012001032004101200103NM 2004 10 12 C1HA200497004 120040912A575465172769 RIB BOEING727 727270 138408PNM NR 4 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF SLAT ACTUATOR PISTON ROD END MOUNTING BOLT WS 410. CRACK = 0.500. REPLACED RIB. 2L73 4F RTA3WE 20041012001052004101200105NM 2004 10 12 C1HA200497003 120040912A575465172769 RIB BOEING727 727270 138408PNM NR 4 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF SLAT ACTUATOR PISTON ROD END WS 408 (MARKED) CRACK = 0.490. REPLACED RIB. 2L73 4F RTA3WE 20041012001072004101200107NM 2004 10 12 C1HA200497008 120040911A575465172761888 RIB BOEING727 727270 138408PNM NR 5 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 RT WING NR 5 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 2 EA ON THE LEFT AS MARKED (5 EA CRACKS TOTAL 1 EA PREVIOUSLY STOP DRILLED). REPLACED RIB. 2L73 4F RTA3WE 20041012001082004101200108WP 2004 10 12 MWEA040176 120040923A3297 WIRE DOUG DC9 DC982 3022082WP MLG LATCH DAMAGED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31809ME 2651 48071 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. REMOVED AND REPLACED MAIN LANDING GEAR UPPER LATCH ASSEMBLY. REPLACED AND REPLACED WIRES G228D20RD AND G229D20BL FROM CONNECTOR P1-1345 TO R5-1150. 2L72 4F A6WE 20041012001092004101200109NM 2004 10 12 C1HA200497009 120040911A5754 RIB BOEING727 727270 138408PNM NR 7 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 RT WING NR 7 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 1 EA ON THE LEFT AS MARKED. REPLACED RIB. 2L73 4F RTA3WE 20041012001102004101200110NM 2004 10 12 C1HA200497010 120040920A5754692848211 RIB BOEING727 727270 138408PNM NR 3 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 3 SLAT O/B CAP END SKIN IS CRACKED. CRACK=8 INCHES. REPLACED RIB. 2L73 4F RTA3WE 20041012001112004101200111NM 2004 10 12 C1HA200497013 120040908A5330 SKIN BOEING727 727270 138408PNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 WING CENTER BOX LWR SKIN EXFOLIATED AT S-4C LBL 24 STA 825.95. INSTALLED REPAIR DOUBLER. 2L73 4F RTA3WE 20041012001122004101200112WP 2004 10 12 MWEA040179 120040928A32205910086503 DOOR DOUG DC9 DC981 3022081WP NLG NOT CLOSED A MWEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL31814ME 48010 A NOISE FROM NOSE LANDING GEAR AREA. FOUND NOSE LANDING GEAR OPEN, CLOSED AND LUBRICATED DOOR. 2L72 4F A6WE 20041012001132004101200113SO 2004 10 12 C2XA04CL090 120040903A335074441 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713908 145465 CLE - FLIGHT 2004, THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIGN DISCONNECTED. MAINTENANCE RESECURED THE CONNECTORS AND THE SIGN OPERATIONALLY CHECKED GOOD. 2L72 4T RTT00011AT 20041012001142004101200114SO 2004 10 12 C2XA04TY164 120040917A33501317 BULB EMB 135 EMB135ER 3260203SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714505 145192 TYS, DURING A NORMAL ROUTINE CHECK THE EMERGENCY LIGHT AT SEAT 9C WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE BULB IAW EMB 145-AMM 33-50-02. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20041012001152004101200115NM 2004 10 12 SWAA042902 120041006A53306545800 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 270, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041004001452004100400145NM 2004 10 4 2004UALA00764 120040808A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 FUSELAGE SKIN HAS TWO DENTS AT STA 393 AND STR 16L. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER. 2L72 4F4 FRTA16WE E2GL 20041004001462004100400146NM 2004 10 4 UPS04443013 120040825A3350 LIGHT BOEING747 747123 1384873NM EMERGENCY EXIT INOPERATIVE A IPXAO OTHER O OTHER CRCRUISE 1 SO01676UP 20101 EMERG EXIT LIGHTS INOP. FOUND BROKEN LT ASSY AT POS 580 RT R/R'D LT ASSY, C/B STILL OPENS. CONTROL PANEL NO HELP, FOUND 1 OHM TO GND AT D1561JP1N6. ACCOMPLISHED EO B747-3350-20943-A. LTS TEST GOOD. 2L74 4F A20WE 20041004001492004100400149 2004 10 4 P9RA20040029 420040807A2565767 BULB BOEING757 757236 1384971NM EMERGENCY LIGHT BURNED OUT A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962PG 24119 AIRCRAFT IN ORD, MAINTENANCE. EMERGENCY LIGHT AT DOOR 4R INOPERATIVE. RELAMPED EMERGENCY LIGHT AT DOOR 4R. 2L72 4F RTA2NM 20041005000052004100500005EA 2004 10 5 ASOA04464 120040629A5320601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL AND RBL 27 TO LBL AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F4 FRTA21EA E15NE 20041005000062004100500006SO 2004 10 5 C2XA04TY113 120040723A532014525523001 ATTACH BRACKET EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL CARGO DOOR BENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A 4C INSPECTION THE CARGO DOOR RAMP ANGLE SUPPORTS AT FR.66 AND FR.67 WERE FOUND BENT. MAINT. REMOVED AND REPLACED THE CARGO DOOR RAMP ANGLE SUPPORTS IAW SRM 51-40-02. 2L72 4F4 FRTT00011ATTE6CH 20041005000102004100500010NM 2004 10 5 04FDEA02375 120040805A5753ARC198413 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP IB AFT HINGE OB PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 FINAL DIAMETER = 1.095. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041005000122004100500012NM 2004 10 5 04FDEA02377 120040805A5753 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OB FLAP, IB AFT HINGE WITH PIVOT HOLE IB CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED 2L73 4F RTA22WE 20041007000012004100700001NM 2004 10 7 MWEA040159 120040907A2410 WARNING SYSTEM BOEING717 717200 1383700NM RT GENERATOR FALSE INDICATIONA MWEAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL31918ME 55180 LEVEL TWO ALERT GENERATOR RIGHT WITH NO VOLTS OR FREQUENCY. -- PERFORMED SATISFACTORY TEST OF SYSTEM. ALL SYSTEMS, OPERATIONS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F TRA6WE 20041007000032004100700003NM 2004 10 7 SWAA042875 120041004A53116547959 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 794, RBL 25, WL 155, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041007000162004100700016NM 2004 10 7 SWAA042870 120041003A57536546430 SKIN BOEING737 7373Q8 1384670NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM. 2L72 4F RTA16WE 20041007000182004100700018WP 2004 10 7 AALA20041020 120041001A335060030451 CONTACTOR DOUG DC9 DC983 3022083WP BATTERY PACK LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219402W 53138 OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. ADJUSTED AND CLEANED BATTERY CONTACTS FOR OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041007000202004100700020WP 2004 10 7 AALA20041019 120040930A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21445AA 49471 AUS - EMERGENCY LIGHTS AT 21DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT 21DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000222004100700022WP 2004 10 7 AALA20041016 120041001A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21419AA 49331 DEN - OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B1107 FOR OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000242004100700024WP 2004 10 7 AALA20041013 120041002A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21488AA 49681 MSP - CEILING EMERGENCY LIGHTS AT ROW 28 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR CEILING EMERGENCY LIGHTS AT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000262004100700026WP 2004 10 7 AALA20041010 120041003A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21275AA 49272 DFW - CEILING EMERGENCY LIGHTS AT ROW 14 AND 20 INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 14 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041007000382004100700038EA 2004 10 7 VNAA0409003 120040920A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DETECTED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07228PS 7897 THE CREW REPORTED A BURNING PLASTIC ODOR TOWARDS THE AFT CARGO BAY. MAINTENANCE RAN THE AIRCRAFT, INSPECTED, AND RAN THE ENVIRONMENTAL CONTROL SYSTEM IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 36-00-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041007000412004100700041EA 2004 10 7 VNAA0409005 120040929A5755CC670170835 FITTING CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF343B1 NE SPOILERS FAILED A VNAAK NONE O OTHER ININSP/MAINT 1 GL07702PS863 10135 DURING A ROUTINE INSPECTION, IN ACCORDANCE WITH BOMBARDIER AMM 57-73-27-220-802, MAINTENANCE FOUND THAT THE RIGHT HAND INBOARD SPOILER HINGE FITTING WAS CRACKED. MAINTENANCE IS CURRENTLY PERFORMING SERVICE BULLETIN 670BA-57-006, REPLACEMENT OF HINGE FITTING. 2L72 4F4 FRTA21EA E15NE 20041007000432004100700043EA 2004 10 7 VNAA0410002 120041001A2910D97C00614 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT HYD SYSTEM FAILED A VNAAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL07249PS712 7926 THE CREW REPORTED THAT THE HYDRAULIC ACTUATOR WOULD NOT CLOSE WHEN YOU PUSH THE LEFT HAND FIRE BUTTON. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC ACTUATOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041007000452004100700045SO 2004 10 7 C2XA04CL091 120040910A32348271011 CONTROL LEVER EMB 145 EMB145ER 3260211SO MLG MALFUNCTIONED A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2714925 145004 AFTER TAKEOFF FROM CLE FLIGHT CREW HAD TO CYCLE THE LANDING GEAR HANDLE TWICE TO GET THE LANDING GEAR TO RETRACT. AIRCRAFT RETURNED TO CLE LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKED GOOD. 2L72 4F RTT00011AT 20041007000472004100700047NM 2004 10 7 SWAA042809 120040928A3350101073 LENS BOEING737 7377H4 1384404NM EMERGNECY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29787SA 29812 AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041007000492004100700049 2004 10 7 SWAA042811 420040928A25656557463 FITTING BOEING737 7373H4 1384600NM GIRTBAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND L1 DOOR EVAC SLIDE FWD AND AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20041007000512004100700051NM 2004 10 7 SWAA042813 120040928A53156545812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 344, RBL 1 TO RBL 8, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20041007000562004100700056NM 2004 10 7 SWAA042852 120041001A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 FWD RT EMERGENCY EXIT PHOTOLUMINESCENT STRIP LOOSE. SECURED EMERGENCY EXIT PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20041007000582004100700058NM 2004 10 7 SWAA042854 120041001A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING WALK AROUND INSPECTION FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 505, BS 515, STRINGER 16R. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041007000602004100700060NM 2004 10 7 SWAA042855 120041001A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 767, BS 750, STRINGER 18L. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041007000622004100700062NM 2004 10 7 CALA0400650 120040930A575365C366642 BRACKET BOEING737 7373T0 1384582NM FLAP TRACK FAIR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND RIGHT WING NR 6 FLAP TRACK FAIRING HORSE COLLAR BRACKET BENT AND CRACKED. THE CRACK WAS 1 INCH LONG. THE HORSE COLLAR BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20041007000642004100700064NM 2004 10 7 SWAA042857 120041001A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED A2 CHECK, FOUND 2 EACH BULL NOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 1 DEF, 2 ABC. RELAMPED BOTH LIGHTS PER MM. 2L72 4F RTA16WE 20041007000912004100700091NM 2004 10 7 SWAA042844 120040930A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER AT ROW 8 ABC, WORN. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041008000022004100800002SO 2004 10 8 C2XA04RI009 120040928A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 RIC- DURING ROUTINE INSPECTION, MAINTENANCE FOUND LT OVER THE WING EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED BULB AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. 2L72 4F RT 20041008000032004100800003SO 2004 10 8 C2XA04RI008 120040926A335008806 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712921 145354 RIC- DURING ROUTINE INSPECTION, MAINTENANCE FOUND RT AFT EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED BULB AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. 2L72 4T RTT00011AT 20041008000102004100800010SO 2004 10 8 C2XA04BT094 120040827A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 CREW REPORTED TWO LOWER EMERGENCY LIGHT PANELS ARE INOPERATIVE. MAINTENANCE RECHARGED AND OPS CHECKED EMERGENCY LIGHT STRIPS IAW 33-50-00 CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041008000172004100800017NM 2004 10 8 QXEA200400670 120040913A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09369PH7820 280 513 PSC - TWO FORWARD EMERGENCY LIGHTS OUT (FLOOR PATH LIGHTING). MAINTENANCE REPLACED BATTERY PACK PS-5. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000182004100800018SO 2004 10 8 C2XA04SH499 120040921A3350110049 CHARGER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717513 145292 DURING A PREFLIGHT INSPECTION IT WAS FOUND THAT THE SECOND AND THIRD EMERGENCY LIGHT FLOOR STRIPS FROM THE FRONT OF THE AISLE WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 BATTERY CHARGER ASSEMBLY. THE EMERGENCY LIGHTS OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041008000212004100800021NM 2004 10 8 CALA0400651 120040929A2701BACB10CF25PP BEARING BOEING737 7373T0 1384582NM CONTROL COLUMN WORN A CALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW2717328 23458 THE HORIZONTAL STABILIZER TRIM STARTED GRINDING ON APPROACH TO MSP WITH THE AUTOPILOT ENGAGED. THE AUTOPILOT WAS TURNED OFF AND THE YOKE SWITCHES WERE ACTUATED. THE CREW HEARD THE GRINDING NOISE AGAIN IN COCKPIT AND AFT GALLEY AREA, THEN THE HORIZONTAL STABILIZER STOPPED MOVING. THE CREW TRIED TO MOVE THE STABILIZER USING THE HAND CRANK TO NO AVAIL. THE AIRCRAFT LANDED AT MSP WITHOUT INCIDENT. MAINTENANCE FOUND THE STAB TRIM SHAFT BEARING ON F/O SIDE IN THE CONTROL STAND HAD FAILED. THE LT AND RT BEARINGS WERE REPLACED IAW CMM 27-09-46. IN ADDITION, THE F/O'S STAB CONTROL WHEEL AND CONTROL STAND STAB SHAFT WERE REPLACED. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20041008000282004100800028NM 2004 10 8 QXEA200400696 120040919A30104100S00502 VALVE BOMBDRDHC8 DHC8401 1390041NM DE-ICE SYSTEM MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09409QX3525 4051 DE-ICE PRESSURE CAUTION LIGHT ILLUMINATED DURING CRUISE. COMPLIED WITH CHECKLIST AND NOTED DE-ICE PRESSURE NORMAL. OBSERVING ICE PROTECTION PANEL, NR 3 INBOARD BOOT ON RIGHT WING AND NR 4 INBOARD BOOT ON LEFT WING FAILED TO ILLUMINATE NORMALLY DURING CYCLE. MAINTENANCE REPLACED DUAL DISTRIBUTOR VALVE NR 3 ON LEFT HAND WING AND LEADING EDGE 513AL. OPERATIONAL AND FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000292004100800029EA 2004 10 8 QXEA200400677 120040907A1430 FASTENER CNDAIRCL600 CL6002C10 1390015EA RT TE FLAP SHEARED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX 10005 ON RIGHT HAND FLAP SHROUD (TRAILING WING BOX) BETWEEN NR 3 AND NR 4 FLAP CANOE HAS FOUR PLACES SHOWING SHEARED RIVET HEADS IN FLAP COVE. REPLACED FASTENERS PER SRM 51-42-06-001-001. 2L72 4F RTA21EA 20041008000302004100800030NM 2004 10 8 QXEA200400678 120040912A5410 SUPPORT ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09404QX 4046 LEFT HAND LOWER COWL CONE SUPPORT ANGLE CRACKED. LEFT HAND SIDE AT ATTACH POINT TO TOP DECK. REMOVED CRACKED SUPPORT ANGLE. REPAIRED IAW RD 8/4-71-016. 2H72 4T RTA13NM 20041008000472004100800047NM 2004 10 8 CALA0400663 120041005A52105079454 SKIN BOEING737 7373T0 1384582NM L1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 L1 DOOR CRACK FOUND ON INNER SKIN AFT EDGE ON NR 6 STOP PIN CUTOUT FROM THE TOP. REPAIRED CRACK PER EC/RA 5210-01798. 2L72 4F RTA16WE 20041008000582004100800058NM 2004 10 8 AT040021 120041006A5320 BRACKET BOEING717 717200 1383700NM CURTAIN ROD LOOSE A ZZDAA UNSCHED LANDING O OTHER CLCLIMB 1 SO15934AT 55070 CURTAIN ROD AT BUSINESS CLASS FELL OF DURING TAKEOFF, HITTING PASSENGER. FOUND RIGHT SIDE BRACKET LOOSE ON HEADER ASSY, RESECURED AS NEEDED. 2L72 4F TRA6WE 20041008000612004100800061NM 2004 10 8 QXEA200400654 120040828A5730 ACCESS PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - LEFT HAND WING CUTOUT FLANGE FOR ACCESS PANEL 524BT HAS FRETTING DAMAGE AT BOTH ENDS OF MATING SURFACE. BLENDED OUT FRETTING CORROSION. DAMAGE FOUND TO BE BEYOND LIMITS. MAPPED AND SENT TO ENGINEERING. REPAIRED IAW HORIZON AIR EA 6-57-232 AND RD 8/4 57-352. 2H72 4T RTA13NM 20041008000692004100800069EA 2004 10 8 COMA0460556 120040915A3411 PITOT LINE CNDAIRCL600 CL6002B19 1900309EA CONTAMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01969CA 7141 FLIGHT 4990 EFIS COMP MON MESSAGE DURING T/O. REMOVED WATER FROM PITOT STATIC SYSTEM. 2L72 4F RTA21EA 20041008000712004100800071NM 2004 10 8 SWAA042885 120041005A53156546548 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 727A, RBL 44, CRACKED. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20041008000722004100800072NM 2004 10 8 SWAA042886 120041005A5310573149 WINDOW POST BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D-CHECK, FOUND L1 COCKPIT WINDOW POST UPPER RT CORNER CRACKED. REPAIRED WINDOW POST PER SRM. 2L72 4F RTA16WE 20041008000772004100800077NM 2004 10 8 AT0400019 120040927A2761NAS16126 O-RING BOEING717 717200 1383700NM RT SPOILER ACT DEFECTIVE A ZZDAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO15974AT 55034 HYDRAULIC RIGHT QUANTITY LOW ANNUNCIATION IN-FLIGHT. FOLLOWED QRH. FLUID LEVEL AT 3.9 WHEN PUMPS SHUT OFF. INCREASED AFTER HYDRAULIC PUMPS SHUT OFF. FOUND HYDRAULIC LEAK AT RIGHT O/B SPOILER ACT PRESSURE FITTING. REMOVED AND REPLACED O-RING AT PRESSURE FITTING. REF MM 27-67 LEAK AND OPS CHECK GOOD. 2L72 4F TRA6WE 20041008000782004100800078NM 2004 10 8 SWAA042890 120041005A3350417A611019C MODULE BOEING737 7377H4 1384404NM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29715SW 27849 EMERGENCY EXIT LIGHTS STAY ON AFTER SHUT DOWN. REMOVED AND REPLACED AFT LIGHTING MODULE PER MM. 2L72 4F RTA16WE 20041008000792004100800079EA 2004 10 8 QXEA200400693 120041005A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 RIGHT HAND INBOARD CABIN SEAT TRACK HAS HEAVY CORROSION BETWEEN FS 349 AND FS 464. REPAIRED IAW CRJ 700 TASK 53-00-49-000-801-A01 AND HORIZON AIR EA R-53-208. 2L72 4F RTA21EA 20041008000812004100800081NM 2004 10 8 ABXA040347 120041001A2150 CONTROL VALVE BOEING767 767281 1385109NM A/C PACK FAILED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23787AX 23020 INBOUND CREW REPORTED ODOR DURING RIGHT AC PACK OPERATION AND ERRATIC OPERATION OF IT'S CONTROL SYSTEM. FOUND SEVERAL ELECTRICAL CONNECTORS LOOSE ON THE RT AC PACK FLOW CONTROL VALVE. RESEATED AND TIGHTENED CONNECTORS. RAN PACK, OPS CHECKED GOOD. 2L72 4F RTA1NM 20041008000822004100800082 2004 10 8 SWAA042891 420041005A25656549956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041008000872004100800087NM 2004 10 8 SWAA042820 120040928A53306545776 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041008000932004100800093NM 2004 10 8 SWAA042831 120040929A53126546568 BULKHEAD BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 15L, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20041008001222004100800122WP 2004 10 8 CALA0400658 120040929A53132777948 LONGERON DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772824 49484 CABIN TOP FUSELAGE STA 674 LONG 1, RT SIDE CRACKED 0.25 INCHES. REMOVED AND REPLACED PER SRM 53-00-02, PG 49, FIG 18. 2L72 4F A6WE 20041012000062004101200006EU 2004 10 12 MALA040599 120040922A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15520XJ E2345 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK AFTER CAPACITY CHECK FAILED P/N 61-2274-1. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/28/04. 2H74 4F RTA49EU 20041012000192004101200019EU 2004 10 12 MALA040592 120040912A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15507XJ E2316 BATTERY PACK WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK P/N 61-2274-1 AFTER CAPACITY CHECK FAILED. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/24/04. 2H74 4F RTA49EU 20041012000232004101200023NM 2004 10 12 MWEA040162 120040909A53105910158113 DOOR FRAME BOEING717 717200 1383700NM AFT CARGO DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31903ME 55167 FORWARD SECTION OF AFT CARGO COMPARTMENT DOOR FRAME DAMAGED. REMOVED AND REPLACED DOUBLER. 2L72 4F TRA6WE 20041012000352004101200035WP 2004 10 12 MWEA040169 120040921A5230591014167 PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 FORWARD BAGGAGE PIT DOOR, FORWARD PAN FLANGE CRACKED. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041012000592004101200059SO 2004 10 12 C2XA04SH513 120041003A532014532636401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING VISUAL INSPECTION AT C-CHECK THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WERE CORRORDED. REPAIRED OMEGA BEAM USING DOUBLER REPAIR IAW 53-22-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041012000602004101200060WP 2004 10 12 MWEA040171 120040922A323259390745501 ACTUATOR DOUG DC9 DC982 3022082WP MLG DOOR MALFUNCTIONED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31809ME 48071 RIGHT MAIN LANDING GEAR UNDSAFE LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED MAIN LANDING GEAR INNER DOOR ACTUATOR. 2L72 4F A6WE 20041012000622004101200062EU 2004 10 12 MALA040571 120040913A2130 CONTROL UNIT SAAB SF340 340B 7860101EU CABIN PRESSURE MALFUNCTIONED A MALAO OTHER P NO WARNING INDICATION CRCRUISE 1 GL15416XJ 340B416 LOST PRESSURIZATION AT 25,000 FT DESCENDED TO 10,000 FT NOTE CABIN ALTITUDE FOLLOWED TO -1. FOUND C/B G7 POPPED. RESET, SWITCHED TO MANUAL MODE, FOUND IT CONTROLLED PRESSURIZATION SYSTEM. MAINTENANCE REPLACED PRESSURIZATION CONTROL UNIT. 2L72 4T RTA52EU 20041012000642004101200064EU 2004 10 12 MALA040575 120040915A3241 VALVE BAC 146 AVRO146RJ85A1500097EU ANTI SKID SYS MALFUNCTIONED A MALAK NONE J WARNING INDICATION NRNOT REPORTED 1 GL15527XJ E2352 ANTI-SKID SYSTEM INOP. BOTH YELLOW AND GREEN SYSTEM. MAINTENANCE REPLACED ANTI-SKID VALVE. 2H74 4F RTA49EU 20041012000732004101200073SO 2004 10 12 C2XA04IA121 120040920A33507287577505 SIGN EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 IAH- FLIGHT 2606, DURING PREFLIGHT INSPECTION THE EMERGENCY EXIT SIGN ON THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000752004101200075 2004 10 12 MWEA040161 420040910A2230 THROTTLE BOEING717 717200 1383700NM ENGINE FAILED A MWEAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL31910ME 55174 AUTO THROTTLES FAILED TO ADVANCE, SET POWER MANUALLY, THEN V SPEED INDICATIONS WERE LOST. PERFORMED RETURN TO SERVICE TEST, FOR FLIGHT CONTROL COMPUTER AND ENGINE ELECTRONIC CONTROLLER. PASSED, AIR DATA INTERTIAL REFERENCE SYSTEM CHECKS GOOD. OK FOR SERVICE. 2L72 4F TRA6WE 20041012000882004101200088NM 2004 10 12 04FDEA02500 120040818A5310 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION ON FWD FLANGE OF FRAME SHEAR TIE AT BS 480 BETWEEN STR 27L AND 28L. *S/D* REMOVED CORROSION ON FWD FLANGE OF FRAME SHEAR TIE STA 480 BETWEEN STR 27L AND 28L. REMOVED 021. 1 X 1 INCH FROM .063, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS FROM .071 7075.T6 LOT 562290, BAC1490-2865. ALODINED, PRIMED AND INSTALLED NEW SHEAR TIE, REPAIR PART IAW SRM 51-10-6, 51-30-02, 53-10-1, 53-10-4, FED EX MM 51-20-021-7, 51-20-151-7, FED-EX EA 7-5310-70677. 2L73 4F RTA3WE 20041012001042004101200104WP 2004 10 12 MWEA040175 120040924A53209961689501 PAN DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 FORWARD WATER SERVICE PAN LIP CORRODED AT FRAME STATION 155. FABRICATED AND INSTALLED SUPPORT. 2L72 4F A6WE 20041012001162004101200116WP 2004 10 12 CALA0400659 120041002A5347SR095301157003 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2772824 49484 RIGHT CENTER SEAT TRACK CORRODED FROM STA 229-235, APPROX 35 INCHES. INSTALLED SEAT TRACK PER SRM 51-30-0 & 53-05, FIG 4H. 2L72 4F A6WE 20041012001172004101200117NM 2004 10 12 CALA0400660 120041001A575465C26799 SKIN BOEING737 7373T0 1384582NM NR 1 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 NR 1 SLAT LOWER SKIN CRACKED AT TWO RIVETS FWD OF I/B AUX TRACK. REPAIRED SLAT SKIN PER SRM 57-43-01. 2L72 4F RTA16WE 20041012001202004101200120NM 2004 10 12 C1HA200479005 120040916A3260 UPLOCK SENSOR BOEING727 727225 1384077NM LT MLG MALFUNCTIONED A C1HAO OTHER N FALSE WARNING CLCLIMB 1 GL15679MG 22557 AFTER DEPARTURE THE LEFT MAIN LANDING GEAR UNSAFE LIGHT (RED) REMAINED ILLUMINATED. COMPLIED WITH COM PROCEDURES AND LIGHT REMAINED ON DURING FLIGHT. REMOVED AND REPLACED LT UPLOCK SENSOR IAW MM 32-61-81. OPS CHECK GOOD. 2L73 4F A3WE 20041012001222004101200122NM 2004 10 12 SWAA042874 120041004A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 RT FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20041012001272004101200127NM 2004 10 12 C1HA200497002 120040913A5754651728613 RIB BOEING727 727270 138408PNM NR 4 SLAT GOUGED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 4 SLAT O/B SIDE CHAFED & GOUGED. REPLACED RIB. 2L73 4F RTA3WE 20041012001292004101200129EA 2004 10 12 COMA0460543 120040928A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 CRACK FOUND ON RIGHT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20041012001302004101200130NM 2004 10 12 C1HA200476005 120040804A5315 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15676MG 22554 CORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEANED, TREATED & INSTALLED REPAIR DOUBLER. 2L73 4F A3WE 20041012001322004101200132NM 2004 10 12 SWAA042833 120040929A5755654645262A SKIN BOEING737 7375H4 138449DNM RT WING SPOILER DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 RT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED RT NR 5 GROUND SPOILER PER MM. 2L72 4F RTA16WE 20041012001332004101200133NM 2004 10 12 SWAA042834 120040929A53306545829 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 378, STRINGER 28L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041012001352004101200135NM 2004 10 12 SWAA042828 120040929A53216935366 FLOOR PANEL BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 380 TO BS 410, LBL 68, CORRODED. REMOVED AND REPLACED SHEAR WEB SECTION PER SRM. 2L72 4F RTA16WE 20041012001362004101200136 2004 10 12 SWAA042829 420040929A256565C19901 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041012001392004101200139NM 2004 10 12 AALA20041005 120040928A3350 SOCKET BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21928AN 29528 BOS - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED SOCKET FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20041012001402004101200140NM 2004 10 12 AALA20041003 120040927A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21759AN 32638 DFW - ALL SEAT MOUNTED EMERGENCY LIGHTS IN COACH CLASS ARE INOPERATIVE. REPLACED BATTERY PACK AT RIGHT 3 DOOR M33401 FOR ALL SEAT MOUNTED EMERGENCY LIGHTS IN COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041012001422004101200142NM 2004 10 12 AALA20041002 120040927A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21795AN 30257 JFK - EMERGENCY LIGHTS AT SEAT 37C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041012001432004101200143WP 2004 10 12 AALA20040998 120040925A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21493AA 49731 DEN - AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT B528 FOR AFT EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041012001442004101200144NM 2004 10 12 AALA20041004 120040927A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21788AN 30011 JFK - AFT EMERGENCY LIGHTS AT CENTER SEATS INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMERGENCY LIGHTS AT CENTER SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041012001452004101200145WP 2004 10 12 AALA20041001 120040927A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21497AA 49735 MIA - INTERIOR OVERWING DOORS AND BOTH AFT DOORS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR INTERIOR OVERWING DOORS (6011779) AND BOTH AFT DOORS (60030451) EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041012001462004101200146WP 2004 10 12 AALA20040994 120040924A3350P4010051111 MODULE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW213507A 49801 DEN - AFT SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR AFT SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041012001472004101200147NM 2004 10 12 SWAA042876 120041004A291065C26839 LINE BOEING737 7373H4 1384600NM HYD SYSTEM CHAFED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29344SW 24152 DIVERSION, COMPLETE B-SYSTEM HYDRAULIC FAILURE. REMOVED AND REPLACED HYDRAULIC LINE ON B-SYSTEM PUMP. 2L72 4F RTA16WE 20041012001522004101200152NM 2004 10 12 SWAA042881 120041004A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS AT BS 747, BS 755, STRINGER 24L, BS 727D, STRINGER 22R, BS 747, STRINGER 18R. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20041012001562004101200156NM 2004 10 12 SWAA042935 120041009A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 435 AND BS 485, STRINGER 26R. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041012001572004101200157NM 2004 10 12 SWAA042942 120041010A53106545871 DOOR FRAME BOEING737 7373H4 1384600NM R2 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT SIDE FRAME AT THIRD STOP FITTING CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041012001582004101200158NM 2004 10 12 SWAA042943 120041010A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 747, LBL 10, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041012001592004101200159NM 2004 10 12 SWAA042944 120041010A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, RBL 8, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041012001602004101200160NM 2004 10 12 SWAA042945 120041010A5315BAC1509100146 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, LBL 12, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041012001612004101200161NM 2004 10 12 SWAA042946 120041010A57436937877 FITTING BOEING737 7373T0 1384582NM LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED SERVICE CHECK, FOUND LT WING MLG AFT STABILIZER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2L72 4F RTA16WE 20041012001642004101200164NM 2004 10 12 SWAA042918 120041007A57536546431280 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED RON, FOUND RT WING OUTBD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20041012001652004101200165NM 2004 10 12 SWAA042926 120041008A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 749, STRINGER 19R, BS 800, STRINGER 18R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041012001662004101200166NM 2004 10 12 SWAA042927 120041008A57536546435278 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20041012001682004101200168NM 2004 10 12 SWAA042929 120041008A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 727E + 5, BELOW STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041012001832004101200183NM 2004 10 12 SWAA042917 120041007A335065C27093 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20041012001852004101200185NM 2004 10 12 SWAA042939 120041010A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED SERVICE CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 8 DEF, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20041012001872004101200187 2004 10 12 SWAA042948 420041009A3417HG480B43 ADC BOEING737 7373H4 1384600NM E/E BAY FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29342SW 24133 F/O'S AIRSPEED IND, AND F/O`S ALTIMETER WARNING FLAGS IN VIEW. F/O`S AIR SPEED NEEDLE CYCLED 0 TO 360 TO 0, EVERY 2 MINUTES. DURING LAST 20 MINUTES OF FLIGHT F/A REPORTED BURNED ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED NR 2 ADC PER MM. 2L72 4F RTA16WE 20041012001892004101200189WP 2004 10 12 04FDEA02491 120040817A78309077U51G02 DUCT DOUG DOUG DC10 DC1010F 3022111WP ZONE 400 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 SEVERAL GOUGES ON FORWARD COMPARTMENT COOLING DUCT INSIDE NR 1 OUTBOARD THRUST REVERSER AT NR 1 ENGINE, (NR 1 OUTBOARD THRUST REVERSER UPPER COOLING DUCT). REMOVED DUCT, REPAIRED IAW EA 8-7830-77634, AND DC10 SRM 51-21-01 VOL 2, AND REINSTALLED IAW DC10 MM 20-50-02. REFERENCE NON-ROUTINE N00929. 2L73 4F A22WE 20041012001912004101200191NM 2004 10 12 SWAA042940 120041010A57126545444 RIB BOEING737 7373H4 1384600NM RT WING TANK CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND RT WING TANK UPPER RIB CHORD AT WING STATION 114, STRINGER 1, CRACKED. REPAIRED RIB PER ER. 2L72 4F RTA16WE 20041012001962004101200196EU 2004 10 12 04FDEA02435 120040806A2810A5715062800051 FUEL TANK AIRBUS310 A310203 3930313EU ZONE 500 CRACKED A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO25431FE 316 AT BLOCK IN, FOUND LT OUTER WING FUEL TANK LEAKING FROM BOTTOM OF WING JUST OUTBD OF RIB NR 20, JACK 05, TRACK 08. FUEL COMING OUT OF DRAIN HOLE ON BOTTOM OF WING JUST FWD OF OVAL ACCESS PANEL. MX FOUND LT NR 8 SLAT TRACK CANISTER TO HAVE APPROX 1 - 2 INCH CRACK. AFTER FURTHER INVESTIGATION A SLAT TRACK ROLLER WAS FOUND IN AREA. IT IS BELIEVED THAT THE FREE MOVING ROLLER CAUSED THE DAMAGE TO THE CANISTER. INSPECTION OF SLAT SYSTEM REVEALED NO MISSING ROLLER AND APPEARS THAT ROLLER WAS IN AREA FROM PREVIOUS MAINTENANCE TO SLAT SYSTEM. CANISTER HAD WELD REPAIR ACCOMPLISHED IN SHOP AND WAS REINSTALLED ON A/C. 2L72 4F RTA35EU 20041012001982004101200198NM 2004 10 12 04FDEA02452 120040811A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 STRINGER DENTED AT BS 950 18, STRINGER 7 LT. *S/D* STR 7 LT ORIGINALLY FOUND OUT OF LIMITS (NO DENTS ALLOWED). REMOVED DENT BY BENDING EDGE OF STRINGER. MATERIAL LOSS A AS ALLOWABLE & STRINGER IS IN LIMITS PER SRM 53-10-1. ALODINED & PRIMED BLEND AREA PER FED EX MM 51-20-151-7. 2L73 4F RTA3WE 20041012002002004101200200NM 2004 10 12 04FDEA02454 120040811A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 BS 848 STR 7R UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE AREA OF STRINGER 7 RT AT BS 848, FABRICATED, ALODINE, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & PER FED EX EA 7-5310-55358. 2L73 4F RTA3WE 20041012002022004101200202EU 2004 10 12 04FDEA02887 120041007A5320 ROLLER TRAY AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 AFT CARGO FLOOR STRUCTURE FR 60, RT SIDE ROLLER TRAY STRUCTURE NOTED CORROSION TOP TO UNDERNEATH NUTPLATES AS MARKED. REMOVED CORROSION ON RT SIDE ROLLER TRAY STRUCTURE AT FR 60 2 EA AREAS. MAX MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW A310 SRM 51-74-10 AND 53-10-15 PG 108. TREATED AND PRIMED AND TOPCOATED IAW A310 SRM 51-75-10. 2L72 4F4 FRTA35EU E3NE 20041013000032004101300003WP 2004 10 13 0401819911 120040824A5330 SKIN DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01961N 47405 DURING L-CHECK, FOUND CRACK IN FUSELAGE NOSE SKIN AROUND FASTENERS AT BS 76.5 LBL 15 TO LBL 21. REPAIRED IAW EA 99-200584. 2L72 4F4 F A6WE E2EA 20041013000042004101300004NM 2004 10 13 2004UALA00870 120040908A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 FUSELAGE SKIN DENTED AT BS 780 AND STR 17L. DOUBLER-TRIPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041013000052004101300005NM 2004 10 13 2004UALA00871 120040928A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 MAIN CABIN FLOORBEAM AT STA 1640 RBL 58 TOP RAIL CORRODED. FABRICATED & INSTALLED NESTED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041013000072004101300007NM 2004 10 13 2004UALA00873 120040928A5320 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 MAIN CABIN FLOOR STA 1681.8 SHEAR WEB CORRODED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041013000082004101300008NM 2004 10 13 2004UALA00874 120040928A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 CABIN FLOORBEAM AT STA 325 BETWEEN RBL 44 AND RBL 58 CORRODED ON TOP CAP OF BEAM. FABRICATED & INSTALLED DOUBLER REPAIR. FABRICATED & INSTALLED ANGLE REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041013000102004101300010NM 2004 10 13 2004UALA00876 120040917A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 FWD PIT FRAME DENTED AT BS 580 STR 23L. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041013000122004101300012NM 2004 10 13 2004UALA00878 120040917A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT STA 1400, FWD SHEAR TIE IS CORRODED BETWEEN STR 27L AND 28L. FABRICATED & INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20041013000132004101300013NM 2004 10 13 ATC0376 120040513A2697 EXTINGUISHER BOEING737 7374Y0 1384705NM CFMINTCFM56 CFM563C1 13802EU CARGO BAY MISWIRED E LH6YO OTHER O OTHER NRNOT REPORTED 1 EA35511HE 24511 CARGO FIRE SUPRESSION/DETECTION, FORWARD CARGO BAY INCORRECT INSTALLATION. DURING A C1-CHECK, FOUND; FIRE DETECTION, AAE LTD SYSTEM TEST CARRIED OUT. DURING TEST, FOUND THAT BY TRIPPING A SYSTEM C/B ISOLATED THE B SENSORS. TRIPPING THE B SYSTEM ISOLATED THE A SENSORS. OUTPUT WIRING AT THE C/B (2 OFF) FOUND TO BE INCORRECTLY WIRED. OUTPUT REWIRED IAW AAE WIRING DIAGRAM. FIRE SUPRESSION-AAE LTD SYSTEM TEST CARRIED OUT. DURING TEST, FOUND THAT WIRING TO NR 1 AND NR 2 EXTINGUISHERS WAS TRANSPOSED. NR 1 WIRING CONNECTED TO LT (NR 2) EXTINGUISHER AND NR 2 WIRING CONNECTED TO RT (NR 1) EXTINGUISHER. DEFECT RECTIFIED BY REPOSITIONING WIRING TO CORRECT LOCATIONS. 2L72 4F4 FRTA16WE E21EU 20041013000152004101300015 2004 10 13 YENA200448 420040930A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEAT 19B ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15547JB4402 4402 1849 AT CRUISE REPORT FROM FA THAT THEY THOUGHT THEY SMELLED SMOKE, TURNED OFF GALLEY SHED CONFM ELECTRICAL, HAD THEM TURN OFF MASTER TV, WENT AWAY, WITH 10 MINS OFF NO FURTHER SMELL. PERFORMED VISUAL INSP OF ALL TV IN CABIN. ALL WORKING OK, ACCOMPLISHED INFO NOTICE 2004-TO23TR. CREW REPORTED THEY SMELLED SMOKE IN THE AREA OF 19ABC. REMOVED AND REPLACED SEB AT 19B AS PRECAUTIONARY. NO ODORS WERE PRESENT. 2L72 4F4 FRTA28NM E40NE 20041013000162004101300016EU 2004 10 13 USAA040521 120040902A5321 FLOOR PANEL AIRBUSA321 A321211 3930370EU FUSLEAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19166US12095 1436 FOUND CARGO FLOOR PANEL DAMAGED, FLOOR CARGO PANEL IN FORWARD BIN, 73 INCHES AFT FORWARD CARGO BULKHEAD, 17 INCHES LT OF CENTERLINE. TEMPORARY REPAIR, REMOVED DAMAGE, INSTALLED TAPE IAW TYPE REPAIR 53-02-01. (M) 2L72 4F RTA28NM 20041013000172004101300017EU 2004 10 13 MALA040595 120040915A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15360PX 340B220 POWER SUPPLY PN 501-1712-02 SN/ 1546 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACKS, 2 EACH PN 549-1324-06. UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/18/04. REFER TO WO NR 375472 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20041013000462004101300046WP 2004 10 13 P9RA20040044 120041001A335041B004AD0763 BATTERY DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1110801 49127 AIRCRAFT IN MAINTENANCE, SYR. CENTER ISLE EMERGENCY LIGHTS INOPERATIVE.REMOVED AND REPLACED BATTERIES AT CENTER ISLE LIGHT POWER SUPPLY IAW MM. 2L72 4F4 F A6WE E9NE 20041013000552004101300055NM 2004 10 13 AWXA200401080 120040929A2560P4010021 BATTERY BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. ISSUED MEL 25-121, WHEN AIRCRAFT ARRIVED, MAINTENANCE REMOVED AND REPLACED BATTERIES IN FORWARD CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E21EU 20041013000572004101300057EU 2004 10 13 AWXA200401082 120040930A335026335090001 EPSU AIRBUS320 A320232 3930326EU ZONE 241 FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28605AW13154412 543 DURING 4-DAY CHECK EMERGENCY LIGHT TEST THE LT OVER WING EMERGENCY POWER SUPPLY UNIT INDICATED EXTERNAL LOAD. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), AND BATTERY PACK, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041013000602004101300060EU 2004 10 13 AWXA200401085 120040926A5320D53472092000 BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y765 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 66 TO FR 70; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472092; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20050210001362005021000136NM 2005 2 10 DHL2005743501 120041217A5347606549 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3843038430 22438 MAIN PASSENGER CABIN STA 740-770 LBL 23 SEAT TRACK HAS CORROSION. REMOVED CORROSION, FOUND OUT OF LIMITS BETWEEN STA 760-770 IAW B727 SRM 51-20-2. ORIG MAT .420 MAT REMOVED .030 FROM LOBE. MEASURED WITH PEMCO CALIPERS H61290 DUE DATE 17 MAY 05. REMOVED SEAT TRACK STA 760-840. DRILLED AND DEBURRED NEW TRACK FROM EXTRUSING BAC 1520-840 7075T651 PO NR 0331867 IAW B727 SRM 51-30-5. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041008000432004100800043NM 2004 10 8 P5CA0401234 120041001A5315 FLOORBEAM BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 BULK CARGO COMPT FLOORBEAM LBL 30 STA 1980 & 2000 IS CRACKED. REMOVED DAMAGE AREA, REPAIR ANGLE, TREATED & PRIMED PER SRM 51-40-03. 2L74 4F4 F A20WE E20EA 20041008000502004100800050EA 2004 10 8 COMA0460553 120040928A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA 7134 CARGO FLOOR CAP IS CORRODED. REPAIRED IAW CRJ SRM 51-42-06, 61-42-21 AND 51-42-24 AND 51-40-11. 2L72 4F RTA21EA 20041008000702004100800070NM 2004 10 8 SWAA042884 120041005A53126545819 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED RON, FOUND RT NLG WHEEL WELL WEB AT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20041008000762004100800076NM 2004 10 8 QXEA200400682 120040915A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNSECURE A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09406QX7735 4048 SEA - FLIGHT 2309 - THE TAKEOFF WAS ABORTED WHEN THE CREW RECEIVED AN AFT BAGGAGE DOOR WARNING LIGHT. MAINTENANCE INSPECTED THE DOOR AND FOUND THE HANDLE POPPED OUT. THE HANDLE WAS SECURED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008000862004100800086NM 2004 10 8 SWAA042895 120041005A55516551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20041008001032004100800103NM 2004 10 8 QXEA200400661 120040827A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - TRACK NR 11 HAS CORROSION FROM X10.5 TO X42.5. REPAIRED IAW HORIZON AIR EA 6-53-386. 2H72 4T RTA13NM 20041008001082004100800108NM 2004 10 8 QXEA200400636 120040824A3040 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM COCKPIT ILLUMINATED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09417QX 4086 PDX FLIGHT 2434 WINDSHIELD CONTROL CAUTION ILLUMINATED IN FLIGHT. PERFORMED CHECKLIST. PILOTS WINDSHIELD IS JUST BARELY WARM, CO-PILOTS WINDSHIELD IS COLD, ICE FORMED INSIDE. C/W FIM WINDSHIELD CONTROL CAUTION FAULT ISOLATION PROCEDURE PER TASK 30-40-00-810-805. CHECKED CDS FOR FAULTS, NONE NOTED. PERFORMED OPS TEST OF PILOT WINDSHIELD ANTI-ICING SYSTEM AND COPILOT WINDSHIELD AND PILOT SIDE WINDOW ANTI-ICING SYSTEM. ALL CHECK GOOD. NO CAUTION LIGHTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041008001102004100800110NM 2004 10 8 QXEA200400647 120040826A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09402QX 4032 PDX - THERE IS PITTING AND CHAFING NR 17 SEAT TRACK AT APPROXIMATELY X32.50 TO X38.00. BLENDED AREA OF PITTING AND FOUND TO BE OUT OF LIMITS IAW RD 8/4-53-884. INSTALLED NEW TRACK IAW DASH-8-400 SRM 51-40-10 AND SRM 51-42-05. 2H72 4T RTA13NM 20041008001112004100800111NM 2004 10 8 QXEA200400643 120040817A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 PDX - COUNTERSINKS FOR 523AT HAVE FRETTING. REMOVED CORROSION FROM 2 COUNTERSINK HOLES ON FORWARD EDGE OF PANEL USING SCOTCH BRITE. REMOVED CORROSION FROM REMAINING COUNTERSINK HOLES, BLENDED DAMAGE. MEASURED ALL HOLES, 4 HOLES OVERSIZED. MAPPED AND ROUTED TO ENGINEERING. HFEC INSPECTED BLENDS FOR CRACKS IAW D8/400 NDTM, PART M, 51-00-06, NO CRACKS NOTED. INSTALLED NEW PANEL 523AT IAW AMM TASK 57-11-01-400-801, PARAGRAPH 4D, STEP 9-12, PAGE 410 AND 57-11-01-400-801, PARAGRAPH 5, PAGE 410-411. 2H72 4T RTA13NM 20041008001132004100800113EA 2004 10 8 COMA0460544 120040928A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 CRACK FOUND ON LEFT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20041008001162004100800116NM 2004 10 8 ABXA040338 120040921A3350A062013 LIGHT BOEING767 767231 1385131NM COCKPIT INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23783AX 23016 OVERHEAD PANEL EMERGENCY LIGHTS BACKGROUND LIGHTING DIM/INOP. REPLACED EMERGENCY LIGHT AND CREW OXYGEN LIGHT PLATE. OPS CHECKED GOOD IAW B767 AMM 33-13-07. 2L72 4F RTA1NM 20041012000152004101200015EU 2004 10 12 MALA040587 120040830A3350330121 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15410XJ 340B410 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 1348 REPORTED INOP. UNIT FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY P/N 3301-31 UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/17/04. 2L72 4T RTA52EU 20041012000272004101200027 2004 10 12 SWAA042910 420041006A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29781WN 30601 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041012000412004101200041NM 2004 10 12 SWAA042897 120041005A53206546816 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT WEB AT BS 807 TO BS 887, LBL 70, CORRODED. REMOVED AND REPLACED FLOOR WEB SECTION PER SRM. 2L72 4F RTA16WE 20041012000482004101200048SO 2004 10 12 C2XA04SH498 120040922A531314525768017 STRINGER EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713979 145181 DURING C-CHECK STRINGER 19L WAS FOUND TO BE CORRODED. REPLACED STRINGER P/N 145-25768-017 USING SPLICE REPAIR TO THE AFFECTED STRINGER IAW EMB 145 SRM 53-00-03 ITEM 7 FIGURE 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041012000522004101200052SO 2004 10 12 C2XA04IA119 120040916A3234355022002 CONTROL LEVER EMB 145 EMB145ER 3260211SO MLG MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW27129461358513585 145052 LCH - FLIGHT 2705, ON DEPARTURE THE CREW REPORTED, RECEIVED AN AIR/GROUND FAILURE MESSAGE AND THE LANDING GEAR LEVER WAS STUCK IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED EXTENSION/RETRACTION CHECKS WITH NO DEFECTS NOTED, ALL IAW EMB-145 MM 32-32-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000532004101200053SO 2004 10 12 C2XA04CL095 120040920A3230355022002 CONTROL UNIT EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW27165611354613546 145610 CLE FLIGHT 3181, CREW REPORTED THAT THE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. ALL OPERATIONAL CHECKS WERE GOOD. PERFORMED TEST FLIGHT, AND TEST FLIGHT WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041012000802004101200080EU 2004 10 12 04FDEA02439 120040811A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 MDC ON RT SEAT TRACK NR 3 FR53 NOTED CORROSION INSIDE SCALLOP HOLES AND ON FLANGE. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW A310/200 SRM 53-10-16. 2L72 4F RTA35EU 20041012000852004101200085EU 2004 10 12 04FDEA02362 120040804A3260BDM3003 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25674FE 781 AFTER TAKEOFF RETRACTED GEAR AUTOTHROTTLES DISENGAGED, SAW BOTH THE MAIN GEAR ON THE FORWARD PANEL SHOWED DOWN & LOCKED. NOSE GEAR STOWED UP AND LOCKED, OVERHEAD INDICATION SHOWED UP & LOCKED. PROXIMITY DETECTOR UNIT FAULT CODE INDICATES INTERNAL FAULT. REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT PER AIRBUS M/M 32-31-71-4, OPS CHECKED NORMAL. ON LANDING GEAR DOOR FWD PANEL-B INOP. PERFORMED AUTOTHROTTLES CHECK AS PER M/M 22-37-00-02. PERFORMED AUTOTHROTTLES SYSTEMS LAND TEST IAW AIRBUS MM 22-40-00. AUTOTHROTTLES REMAINED ENGAGED. 2L72 4F RTA35EU 20041012000932004101200093WP 2004 10 12 04FDEA02553 120040823A5753 SUPPORT DOUG DC10 DC1010 3022110WP TE FLAPS CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25366FE 46602 COMPLY WITH EA 8-5750-80595 WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-80595, WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK. 2L73 4F A22WE 20041012001242004101200124NM 2004 10 12 C1HA200497007 120040913A5315 FLOORBEAM BOEING727 727270 138408PNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24. 2L73 4F RTA3WE 20041012001412004101200141WP 2004 10 12 AALA20040995 120040924A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21590AA 53253 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041012001482004101200148NM 2004 10 12 SWAA042877 120041005A53106546546 SHEAR TIE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 847, STRINGER 25R, CORRODED. REPAIRED SHEAR TIE PER EA. 2L72 4F RTA16WE 20041012001492004101200149NM 2004 10 12 SWAA042878 120041005A5314656212518 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM AT BS 727, RBL 6.30, CRACKED. REPAIRED KEEL BEAM PER EA. 2L72 4F RTA16WE 20041012001692004101200169 2004 10 12 SWAA042930 420041008A25656557463 BRACKET BOEING737 7373Y0 1384671NM ESCAPE SLIDE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE FWD MOUNTING BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2L72 4F RTA16WE 20041012001732004101200173NM 2004 10 12 SWAA042920 120041007A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 460 TO BS 500+10, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20041013000562004101300056NM 2004 10 13 AWXA200401081 120040930A335032145410 EPSU AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE ZONE 242 FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28802AW21564 924 DURING 4-DAY CHECK RT OVER WING EMERGENCY POWER SUPPLY UNIT (EPSU) AND AFT ESPU FAILED EMERGENCY TEST. MAINTENANCE REMOVED AND REPLACED RT OVER WING EPSU (12WL) AND AFT EPSU (13WL) AND BATTERY PACKS; OPERATIONAL CHECK WAS GOOD. PART NAME; EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 1355, TT; 21564, TC; 8764, LOC; ZONE 263 2L72 4F4 FRTA28NM E40NE 20041013000612004101300061EU 2004 10 13 AWXA200401086 120040926A5320D53472172200 BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, FORWARD AND AFT OF FR 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D534-72172; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20041013000622004101300062EU 2004 10 13 AWXA200401087 120040926A5320D53472133200 BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM IAW DWG 18D53472133; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20041013001132004101300113EA 2004 10 13 SWIA200413867 120040805A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07430SW 7523 RT FS 621 FLOOR SUPPORT ANGLE IS CRACKED ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. ( ITEM FOUND AT C-CHECK INSPECTION). INSTALLED REPAIR PARTS IAW STEPS 5 AND 6 OF MFG 601R-53-61-117, PN 601R53-61-004-6 (ANGLE), 1R53-61-117-6 (RT ASSY). 2L72 4F4 FRTA21EA E15NE 20041013001142004101300114EA 2004 10 13 SWIA200413868 120040805A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 30070NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07430SW SUPPORT ANGLES ARE CRACKED AT RBL 9.0 AND LBL 9.0 FS 280.0 WL 73.5. (ITEM FOUND AT C-CHECK INSPECTION.) REMOVED AND INSTALL NEW ANGLE AT 9.0 IAW SRM CRJ 200 51-24-06 AND 51-42-21. 2L72 4F4 FRTA21EA E15NE 20041013001172004101300117 2004 10 13 SWIA200413871 420040929A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE TRIM SYSTEM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07587331033210332 120197 ELECTRIC TRIM DOES NOT FUNCTION ABOVE 180 KTS.REMOVED AND REPLACED ELECTRIC TRIM MOTOR, REFERENCE 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041013001202004101300120EA 2004 10 13 SWIA200413874 120040920A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07944SW 7764 INTERCOSTAL HAS A CRACKED RETURN FLANGE, FS 484.00 LBL 36.0. ( ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-53-41-059 REV "A" . 2L72 4F4 FRTA21EA E15NE 20041014000022004101400002NE 2004 10 14 ASMF200410009 220041010A732176960613 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE MALFUNCTIONED W ASMFD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SW23216AM381425486 49586 718411 AIRCRAFT RETURNED TO PLATFORM, DURING ENGINES STARTING, LT ENGINE WAS UNDER IDLE MINIMUM THRUST REQUIREMENTS, ABNORMAL PROCEDURE WAS APPLIED AND BUT REMAIN THE SAME CONDITION AND FUEL FLOW WAS UNSTABLE. ACCELERATION CAM WAS SERVICED AND WATER TRAMP WAS DRAINED, PARAMETERS WERE CORRECT. DURING OVERNIGHT SERVICE, OPERATIONAL TEST WAS PERFORMED TO LT ENGINE IAW MM 71-00-00, ALL CORRECT. ADDITIONALLY AS PRECAUTIONARY ACTION FCU WAS REPLACED IAW MM 73-20-01, OPERATIONAL TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20041014000092004101400009NM 2004 10 14 DL73S040951 120041007A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 THE LOWER AFT CORNER OF THE RIGHT WING SCANNING LIGHT CUTOUT AT FS 530 WAS FOUND WITH A .5 INCH CRACK IN THE SKIN. THE CRACK WAS REMOVED WITH A SMALL CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094021-14. 2L72 4F RTA16WE 20041014000122004101400012NM 2004 10 14 SWAA042952 120041011A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 18L, CRACKED. REPAIRED SKIN PER EA AND SRM. 2L72 4F RTA16WE 20041014000132004101400013NM 2004 10 14 SWAA042953 120041011A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT RT BS 188, RBL 30-LBL 30, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041014000142004101400014NM 2004 10 14 SWAA042954 120041011A53156545833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND 2 EACH CRACKS ON FLOOR WEB AT BS 188 TO BS 196, RBL 28-LBL 28. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20041014000152004101400015 2004 10 14 SWAA042949 420041011A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041014000182004101400018SO 2004 10 14 MASA200400483 120040829A276014533022409 CONTROL UNIT EMB 145 EMB145LR 3260212SO SPOILERS FAILED A MASAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW07826MJ7312 2109 145214 AIRCRAFT ROLLED TO THE RIGHT UPON DEPLOYMENT OF SPEED BRAKES. MAINTENANCE TROUBLESHOT TO A FAILED SPOILER CONTROL UNIT. THE FAILED SPOILER CONTROL UNIT WAS REMOVED AND REPLACED, A TEST FLIGHT WAS SATISFACTORY. 2L72 4T RTT00011AT 20041014000192004101400019SO 2004 10 14 MASA200400504 120040907A4930M832481210 O-RING EMB 145 EMB145LR 3260212SO APU LEAKING A MASAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07827MJ 145217 STRONG FUEL SMELL IN CABIN. MX IDENTIFIED IT WAS COMING FROM THE APU BLEED SYSTEM. MEL'D THE APU AND CONTINUED OPERATIONS 9/9/04. MAINTENANCE TIGHTENED FUEL LINES AND REMOVED AND REPLACED BOTH O-RINGS ON BOTH SIDES OF MAXIMUM TO START FITTINGS. 2L72 4T RTT00011AT 20041014000202004101400020 2004 10 14 MASA200400533 420040917A2210M8353610024M RELAY EMB 145 EMB145LR 3260212SO RUDDER CONTROL FAILED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07831MJ 145273 RUDDER SYSTEM 2 FAILED RESULTING IN AN INOP AUTO PILOT. MAINTENANCE REPLACED THE RUDDER CONTROL RELAYS. 2L72 4T RTT00011AT 20041014000212004101400021SO 2004 10 14 MASA200400544 120040927A21214611028900 FAN EMB 145 EMB145LR 3260212SO NR 2 PACK ODOR A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07860MJ1957 145773 MGM PACK NR 2 FAN (RECIRC FAN) PRODUCES ELECTRICAL SMELL. PLACED ON MEL AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT 10/2/04. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FAN. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041014000242004101400024NM 2004 10 14 CALA0400667 120041008A53306546568524 SKIN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 APB SKIN CORROSION AT BL 0, 6 INCHES ABOVE Y-ATTACH CHORD. REPAIRED PER BOEING DRAWING 65C28106. 2L72 4F RTA16WE 20041014000252004101400025SO 2004 10 14 MASA200400499 120040904A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT THE ROW 3 EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT. 2L72 4T RTT00011AT 20041014000272004101400027EA 2004 10 14 MASA200400501 120040906A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0727318 7318 THE OVERHEAD EMERGENCY LIGHT IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BULB. 2L72 4F RTA21EA 20041014000312004101400031SO 2004 10 14 MASA200400509 120040908A3350744424 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSINOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07853MJ 145464 RIGHT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED THE EXIT SIGN. 2L72 4T RTT00011AT 20041014000322004101400032SO 2004 10 14 MASA200400515 120040909A3350744424 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07853MJ 145464 DURING OVERNIGHT MAINTENANCE HAD A ROW 12 SIDE WALL EMERGENCY EXIT SIGN INOPERATIVE. MX CURRENTLY TROUBLESHOOTING. MAINTENANCE REPLACED EXIT SIGN ASSY. 2L72 4T RTT00011AT 20041014000332004101400033EA 2004 10 14 MASA200400516 120040910A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07650ML 7036 DURING PREFLIGHT, THE SERVICE DOOR LOWER EXIT SIGN WAS INOP. MAINTENANCE REPLACED THE LIGHT. 2L72 4F RTA21EA 20041014000342004101400034NM 2004 10 14 DL73S040932 120040927A5330 SKIN BOEING737 737232 1384475NM L1 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 THE FUSELAGE SKIN AT THE L1 DOOR OPENING WAS FOUND CRACKED AT THE CUTOUT EDGE JUST ABOVE THE LOWER AFT CORNER. THE CRACKS WERE SMALL AND TYPICAL OF BAC S/B 737-53-1083. THE CRACKS WERE TRIMMED OUT OF THE SKIN AND REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER THE BAC S/B AND ER/A 093452-14. 2L72 4F RTA16WE 20041014000382004101400038NM 2004 10 14 MASA200400449 120040812A2760H188C INDICATOR DHAV DHC8 DHC8202 2809007NM SPOILER INOPERATIVE A MASAD RETURN TO BLOCK FN FLT CONT AFFECTED FALSE WARNING TXTAXI/GRND HDL 1 SW07449YV5717 449 THE CREW RETURNED THE AIRCRAFT TO THE GATE DUE TO THE LEFT SPOILER INDICATING OPPOSITE OF DEFLECTION. CONFIRMED THAT THE FAULT WAS AN INDICATION ERROR AND FERRIED THE AIRCRAFT TO PHX. MX HAS TROUBLESHOT TO AN INDICATOR AND ARE AWAITING PART. 8/13 MAINTENANCE CHANGED OUT SURFACE POSITION INDICATOR. OPS CHECK GOOD. 2H72 4T RTA13NM 20041014000392004101400039NM 2004 10 14 MASA200400453 120040814A3231858601 PSEU DHAV DHC8 DHC8202 2809007NM MLG DOOR INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07455YV6220 455 A/C DIVERTED TO GJT DUE TO AFTER TAKEOFF THE RIGHT GEAR DOOR WOULD NOT CLOSE. THE CREW RECYCLED THE GEAR AND THE RIGHT MAIN DID NOT EXTEND. MX REPLACED THE PSEU AND SEQUENCE CALVE. SELECTOR VALVE P/N 57420-5A, S/N 938, TSN 1347 CSN 1318 WAS ALSO REPLACED. 2H72 4T RTA13NM 20041014000412004101400041EA 2004 10 14 MASA200400491 120040902A3234533443 LEVER CNDAIRCL600 CL6002D24 1390016EA MLG INOPERATIVE A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07922FJ699 15022 RTF AFTER GEAR RETRACTION THE CREW HAD A GEAR DISAGREE MESSAGE. 9/2/04 MAINTENANCE REPLACED LANDING GEAR SELECTOR LEVER. OPS CHECK GOOD. 2L72 4F RTA21EA 20041014000422004101400042EA 2004 10 14 MASA200400494 120040903A2435 SHAFT SUNDSTRANDEM CNDAIRCL600 CL6002B19 1900309EA IDG FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW077291Z1408912 06612386 7291 THE CREW ABORTED TAKEOFF FOR A NR 2 IDG CAUTION MESSAGE ON TAKEOFF ROLL. MX PLACED THE ITEM ON DEFERRAL. 9/5/04 MAINTENANCE REPLACED NR 2 IDG. 2L72 4F RTA21EA 20041014000432004101400043NM 2004 10 14 DL777040942 120041002A21214100945A FAN BOEING777 777232 1385232NM CABIN FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27861DA 29952 RECIRC FAN STATUS MSG CAME ON SHORTLY AFTER F/A`S REPORTED SMELLING SMOKE THE SMOKE DISAPPEARED QUICKLY. MAT SHOWS UPPER FWD REC FAN FAILED OVERHEATED FWD TO MCO AND PLACARD PER MEL 21-25-01 MAINT PROC APPLIED. 2L72 4F RTT00001SE 20041014000452004101400045EA 2004 10 14 MASA200400425 120040725A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0775998 7336 EMERGENCY FLOOR LIGHTS INOP. MX CONNECTED THE LIGHTS. OPS CHECK GOOD. 2L72 4F RTA21EA 20041014000462004101400046SO 2004 10 14 MASA200400437 120040731A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07860MJ 145773 THE AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20041014000472004101400047SO 2004 10 14 MASA200400458 120040817A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07848MJ 145530 SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT SIGN. 2L72 4T RTT00011AT 20041014000492004101400049SO 2004 10 14 MASA200400464 120040819A335066367 LIGHT EMB 145 EMB145LR 3260212SO ROW 8 & 9 INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07842MJ 145457 ON OVERNIGHT MAINTENANCE FOUND ROW 8 & 9 EMERGENCY FLOOR LIGHT STRIP INOP. MAINTENANCE REPLACED LIGHT. 2L72 4T RTT00011AT 20041014000502004101400050SO 2004 10 14 MASA200400471 120040823A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07830MJ 145259 ON RON MX FOUND NR 2 AND NR 3 FLOOR EMERGENCY LIGHTS INOPERATIVE. MX REPLACED THE INVERTER, OPS CHECK GOOD. 2L72 4T RTT00011AT 20041014000512004101400051EA 2004 10 14 MASA200400472 120040824A3350362624 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 EMERGENCY FLOOR LIGHTS OUT. MX RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041014000522004101400052NM 2004 10 14 DL73S040953 120041007A53156545410513 FLOORBEAM BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27301DL 23073 INSPECTION OF THE LBL AND RBL 24.82 LONGITUDINAL FLOORBEAMS OVER THE CENTER WING REVEALED CRACKS IN THE BEAM WEB AND CAP AT THE AILERON QUADRANT CUTOUTS AT FS 679. THE CRACKS ARE TYPICAL OF AD 2001-17-18. THE CRACKED AREA WAS REPAIRED BY REPLACING THE BEAM CHORDS, TRIMMING THE BEAM WEB, AND INSTALLING ALUMINUM REPAIR DOUBLERS PER ER/A 094024-14AD. 2L72 4F RTA16WE 20041014000542004101400054SO 2004 10 14 MASA200400484 120040829A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO CARGO SMOKE ILLUMINATED A MASAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW07851MJ 145572 DURING TEST THE BAGGAGE SMOKE DETECTOR LIGHT WOULD NOT ILLUMINATE. RESET SYSTEM AND THE SYSTEM TESTED WITH NO DEFECTS. 2L72 4T RTT00011AT 20041014000562004101400056SO 2004 10 14 MASA200400479 120040827A3350744424 SIGN EMB 145 EMB145LR 3260212SO RT OVERWING INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 RIGHT OVERWING EMERGENCY EXIT SIGN INOP. MX REPLACED THE SIGN ASSY AND IT OPERATED NORMALLY. THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20041014000572004101400057NM 2004 10 14 DL764040935 120040929A2780 TARGET BOEING767 767432ER 1385134NM NR 8 SLAT MISSING A DALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO27831MH 29702 ON APPROACH TO FLL WITH FLAPS 20 GOT L/E SLAT ASYM. DUE TO LONG RUNWAY UNAVAIL FLL AND FLAPS 20 REQUIREMENT FOR LANDING DIVERTED TO MIA. PSEU FAULTED TARGET FOR NR 8 SLAT OUTBD SENSOR. INSPECTED TARGET AND FOUND MISSING. REPLACED TARGET FOR SENSOR 238, OPS CHECK OK. 2L72 4F RTA1NM 20041014000602004101400060NM 2004 10 14 DL73S040954 120041009A8097 WIRE BOEING737 737232 1384475NM COCKPIT BROKEN A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27309DL 23081 WHILE TURNING NR 1 ENG START SWITCH TO START ENG GOT LOUD POP ALONG WITH SPARK FROM BEHIND OVERHEAD PANEL. MTC FOUND 2 BROKEN WIRES BEHIND PANEL THAT CHAFED FROM RUBBING WHISKEY COMPASS EACH TIME IT IS STOWED. REPAIRED WIRES AND REPLACED SWITCH AS PRECAUTION. 2L72 4F RTA16WE 20041014000622004101400062EA 2004 10 14 MASA200400492 120040902A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0727314 7314 EXTERIOR EMERGENCY LIGHT INOP. CREW C/W MEL PROCEDURES WITH MAINTENANCE CONTROL. 9/2/04 MX REPLACED LIGHT. 2L72 4F RTA21EA 20041014000632004101400063SO 2004 10 14 MASA200400495 120040902A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07834MJ 145340 COCKPIT EMERGENCY LIGHT INOP. MX RELAMPED IAW 33-20-00. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041014000642004101400064NM 2004 10 14 CALA0400668 120041008A53126546568519 STIFFENER BOEING737 7373T0 1384582NM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 LOWER LT SIDE OF APB STIFFENER CORRODED. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106. 2L72 4F RTA16WE 20041014000662004101400066EA 2004 10 14 MASA200400520 120040911A335020131A BATTERY PACK CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSDISCHARGED A MASAK NONE L NO TEST ININSP/MAINT 1 SW07910FJ 15010 ALL EMERGENCY LIGHTS INOPERATIVE. MX FOUND THE EMERGENCY LIGHTS SWITCH IN THE ARMED POSITION AND THE GROUND POWER HAD BEEN REMOVED FROM THE AIRCRAFT FOR AN EXTENDED PERIOD. THE EMERGENCY LIGHTS BATTERY PACKS WERE REMOVED AND REPLACED AND THE SYSTEM CHECKED NORMALLY. 2L72 4F RTA21EA 20041014000682004101400068EA 2004 10 14 MASA200400529 120040915A3350 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT TRIPPED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 DURING PREFLIGHT, THE EMERGENCY LIGHTS WERE ON IN THE ARM POSITION WITH ALL BUSSES POWERED. MAINTENANCE FOUND THE C/B FOR THE EMERGENCY LIGHTS POPPED AND RESET IT. OPS CHECK WAS NORMAL. 2L72 4F RTA21EA 20041014000702004101400070EA 2004 10 14 MASA200400534 120040918A3350 CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MALFUNCTIONED A MASAK NONE L NO TEST ININSP/MAINT 1 SW0777275 7275 DURING PREFLIGHT THE MAIN CABIN DOOR EMERGENCY FLOOD LIGHT WAS INOP. MAINTENANCE REPLACED THE NR 2 BATTERY CHARGER. 2L72 4F RTA21EA 20041014000722004101400072EA 2004 10 14 MASA200400538 120040922A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0727314 7314 SECOND CABIN CEILING EMERGENCY LIGHT INOP. PLACED ON MEL AND RELEASED AIRCRAFT. 9/22/04 MAINTENANCE RELAMPED AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20041014000732004101400073SO 2004 10 14 MASA200400523 120040912A272015793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO NR 2 HYD SYS INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07831MJ8796 145273 RETURNED TO FIELD DUE TO RUD 1 AND RUD 2 INOP MESSAGES IN FLIGHT. MX REPLACED THE NR 2 HYD SYSTEM PRESSURE SWITCH. A/C DEPARTED WITHOUT FUTHER INCIDENT. 2L72 4T RTT00011AT 20041014000742004101400074SO 2004 10 14 MASA200400526 120040913A5210 STOP EMB 145 EMB145LR 3260212SO PAX DOOR LOOSE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07837MJ 145367 PAX DOOR TOP FLAP WOULD NOT CLOSE. CONTRACT MAINTENANCE WAS CALLED OUT TO THE FIELD AND FOUND A DOOR STOP LOOSE. RESECURED THE DOOR STOP AND THE DOOR OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041014000762004101400076 2004 10 14 ARWA20040804 420040822A3413066500011001 INDICATOR DOUG DC8 DC863F 302198FWP FAILED A ARWAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19441J 45988 DURING TAXI, FIRST OFFICER'S VERTICAL SPEED INDICATOR (VSI) DISPLAY SHOWS REPEATER ANNUNCIATOR. FAILURE AND NO NEEDLE. REMOVED AND REPLACED TCAS/VSI AT FIRST OFFICER'S SIDE. CHECK SYSTEM ON GROUND OK IN ACCORDANCE WITH MM 34-12-0 AND 34-11-1. 2L74 4F 4A25 20041014000772004101400077NE 2004 10 14 ARWA20040803 220040819A7261 ENGINE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 4 LEAKING A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19791AL435282115 46150 669510 DURING CLIMBOUT OF MGGT NOTICED NR 4 ENGINE LOSS OF OIL QUANTITY, OIL PRESSURE AND LIGHT. PROCEEDED TO SHUTDOWN ENGINE ACCORDING TO CHECKLIST. REMOVED AND REPLACED ENGINE NR 4 S/N 669510, AND INSTALLED ENGINE S/N P671066 IN ACCORDANCE WITH ARROW AIR JOB CARD DC8UN-003. ADJUSTMENT AND TEST NR 4 ENGINE IN ACCORDANCE WITH DC-8 MM 71-00; FOUND NORMAL PARAMETER. 2L74 4F4 F 4A25 1E8 20041014000782004101400078NE 2004 10 14 MASA200400392 320040710A614078249050 PCU DHAV DHC8 DHC8202 2809007NM HAMSTD14SF 14SF23 NE NR 2 ENGINE INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07446YV7032 446 MFG960330 THE AIRCRAFT DIVERTED TO GJT WITH THE LOSS OF CONTROL OF THE NR 2 ENGINE TORQUE IN FLIGHT. MX REPLACED THE PCU, MFC AND FUEL PUMP WITH ALL ENGINE RUN CHECKS AFTERWARD CHECKING GOOD. MFC P/N 3244853-18, S/N C31148V, FUEL PUMP P/N 5008269H, S/N 2433. 2H72 4T RTA13NM 6 CP7NE 20041014000802004101400080NM 2004 10 14 MASA200400416 120040721A612030005000056 CONTROL UNIT DHAV DHC8 DHC8201 2809001NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE NR 1 ENGINE FAILED A MASAD RETURN TO BLOCK O OTHER NRNOT REPORTED 1 SW07987HA791 425 TM123325 MFG951218 RETURNED TO THE GATE DUE TO AN UNCOMMANDED AUTOFEATHER OF NR 1 ENGINE. MEL'D AUTOFEATHER SYSTEM AFTER VERIFYING IT WAS AT FAULT. 7/21 MAINTENANCE REPLACED TSCU, OPS CHECKED GOOD. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20041014000822004101400082SO 2004 10 14 RAIA00408022 120040820A7830 RELAY EMB 145 EMB145LR 3260212SO THRUST REVERSER MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03816HK 145055 NR 2 T/R DISAGREE MESSAGE. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL. CLEARED DMI. REMOVED AND REPLACED C-4 THRUST REVERSER RELAY NR 2. 2L72 4T RTT00011AT 20041014000832004101400083EU 2004 10 14 RAIA00408023 120040822A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03574HK 41093 STL - ESCAPE PATH LIGHTING INOP AT SEATS 2A AND 3A. MAINTENANCE RESEATED CONNECTOR AT PATH LIGHT. 2L72 4T RTA41NM 20041014000852004101400085SO 2004 10 14 MASA200400441 120040807A2611FDS765A2 SENSOR EMB 145 EMB145LR 3260212SO LAVATORY INOPERATIVE A MASAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07838MJ8131 145384 RETURNED TO GATE AT CLT DUE TO THE LAV SMOKE ANNUNCIATOR CAME ON DURING TAXI. NO SMOKE NOTED MX C/W MEL PROCEDURES. 8/8/04 MAINTENANCE REPLACED A SMOKE SENSOR. 2L72 4T RTT00011AT 20041014000862004101400086SO 2004 10 14 MASA200400445 120040810A2621 WARNING LIGHT EMB 145 EMB145LR 3260212SO CARGO EXTINGUISHILLUMINATED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07851MJ 145572 A BAGGAGE SYSTEM (FIRE EXT) NO TEST MESSAGE. MAINTENANCE RESECURED THE RELAY AND OPERATIONAL CHECKED GOOD. 2L72 4T RTT00011AT 20041014000882004101400088NM 2004 10 14 DL73S040958 120041010A2761273001067 ACTUATOR BOEING737 737232 1384475NM NR 1 SPOILER FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27302DL 23047 AFTER LANDING A-SYS HYD QTY DROPPED TO 0. REPLACED NR 1 SPOILER ACTUATOR FOR LEAKING. 2L72 4F RTA16WE 20041014000892004101400089NM 2004 10 14 CALA0400669 120041008A531265465568520 STIFFENER BOEING737 7373T0 1384582NM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 STIFFENER ON LWR RT SIDE OF APB IS CORRODED AT RBL 1. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106. 2L72 4F RTA16WE 20041014000912004101400091NM 2004 10 14 DL76L040936 120040924A2780 SENSOR BOEING767 767332 1382001NM LE SLAT CONTAMINATED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27196DN 28453 L/E SLAT ASSY LIGHT AFTER TAKEOFF. ATB INTO ATL. FOUND SENSORS CONTAMINATED WITH GREASE. 2L72 4F RTA1NM 20041014000932004101400093NM 2004 10 14 DL75A040945 120040929A2710BACC2C4AD065 CONTROL CABLE BOEING757 757212 1384951NM LEFT OVERIDE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27750AT 23126 HMV-3 VISIT IN DFW. CABLE WORN, AILERON CABLE WORN AT LEFT WING OVERRIDE QUADRANT. CABLE FOUND TO BE IN POSITION A1B-4 AND PN BACC2C4AD06518FG. REPLACED CABLE PER OPN 2000 AND INSTALLED RECOMMENDED OPTIONAL CABLE PN BACC2C4CD06518FG ON RC 1388-1392 WITH RII INSPECTION CW. 2L72 4F RTA2NM 20041014000982004101400098EA 2004 10 14 MASA200400413 120040718A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNSECURE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07653ML 7039 CREW REPORTED EMERGENCY LIGHTS AT ROW 2 & 3 INOP. MX RESECURED FLOOR CONNECTOR, OPS CHECK GOOD. 2L72 4F RTA21EA 20041014001022004101400102NM 2004 10 14 CALA0400672 120040926A5311BAC1517706 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 RT MAIN FRAME CRACKED. INSTALLED DOUBLER PER ECRA 5311-01158. 2L72 4F RTA16WE 20041014001042004101400104NM 2004 10 14 CALA0400674 120041008A21216454052 FAN BOEING737 737824 13844BZNM CABIN ODOR A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2736272 31590 HEAVY BURNING SMELL IN AFT CABIN AREA. STARTED QRH FOR AIR CONDITIONING/ SMOKE FUMES. SMELL DISSIPATED. REPLACED RT RECIRCULATION FAN PER AMM 21-25-02. 2L72 4F RTA16WE 20041014001062004101400106NM 2004 10 14 DL764040930 120040928A2781851801 SENSOR BOEING767 767432ER 1385134NM RIGHT WING MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27838MH 29711 AT APPROX 20 MINUTES INTO FLT WHILE STILL IN CLIMB RECEIVED WARNING L/E ASYMMETRY WARNING FLICKERED ON AND OFF SEVERAL TIMES, STAYED ON CONTINOUSLY. FIFTEEN MINS LATER WARNING WENT OFF AND STAYED OFF, FLAPS OPS NORMALLY ON DESCENT AND APPROACH. REPLACED RIGHT INBOARD NR 8 SLAT SENSOR. DIVERTED TO HNL DUE L/E SLAT AYSM MESSSAGE REQUIRED FLAPS 20 APPROACH. OGG RWY TO SHORT FOR THIS APPROACH. 2L72 4F RTA1NM 20041012000212004101200021EU 2004 10 12 MALA040598 120040918A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15504XJ E2311 BATTERY PACK 61-2275-1, S/N 9812849 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY CELL PACK AFTER CAPACITY CHECK FAILED. P/N 61-2274-1 UNIT PASSES CMM TESTS. A/C RETURNEDTO SERVICE 9/24/04. 2H74 4F RTA49EU 20041012000262004101200026NM 2004 10 12 SWAA042909 120041006A3350OL307IBPEGL LAMP BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29526SW 26568 DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 2 DEF, INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20041012000552004101200055SO 2004 10 12 C2XA04IA124 120040925A335082311 SIGN EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2719966 145131 IAH - FLIGHT 2458, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE GALLEY OVERHEAD EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE LIGHT ASSEMBLY, OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012000612004101200061WP 2004 10 12 MWEA040168 120040920A56105912290501 WINDSHIELD DOUG DC9 DC981 3022081WP COCKPIT CRACKED A MWEAA UNSCHED LANDING O OTHER CRCRUISE 1 GL31803ME 48029 CAPTAIN'S WINDSHIELD CRACKED HORIZONTAL AND VERTICAL. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD. 2L72 4F A6WE 20041012000722004101200072SO 2004 10 12 C2XA04CL098 120040923A3350 CHARGER EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139654112 332 145125 THE CREW REPORTED THE EXIT ROW EMERGENCY LIGHTS AND (2) FLOOR STRIPS DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM AND REPLACED THE BATTERY AND THE CHARGER ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTT00011AT 20041012000762004101200076EU 2004 10 12 04FDEA02391 120040806A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25409FE 273 LOWER FUSELAGE BULK CARGO PIT LATERAL FLOORBEAM AT FR66 LT OF CENTERLINE HAS EXFOLIATED CORROSION AROUND FASTENER HOLE (LEVEL 2). REMOVED DAMAGED AREA, FABRICATED FILLER, ANGLE AND INSTALLED IAW A310/200 SRM 53-10-15 AND 51-25-00. 2L72 4F RTA35EU 20041012000812004101200081WP 2004 10 12 04FDEA02477 120040814A5330AFA015345 PANEL DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 CTR CARGO SUMP PNL 1741-1721 CRACKED AND CORRODED RT SIDE. REMOVED AND REPLACED IAW DRWG AFA0153 AT MAE. 2L73 4F RTA22WE 20041012000872004101200087WP 2004 10 12 04FDEA02499 120040818A7120CF66D MOUNT DOUG DC10 DC1010 3022110WP NR 2 ENGINE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25366FE 46602 COMPLY WITH EA8-7120-79336 ENGINE MOUNTS ALIGNMENT PIN MINOR CORROSION REPAIR. COMPLIED WITH EA 8-7120-79336. 2L73 4F A22WE 20041012000902004101200090NM 2004 10 12 C1HA200492015 120040715A3350 LIGHT BOEING727 727212 138407GNM CABIN MALFUNCTIONED A C1HAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15292AS 21458 UPON POWER TRANSFER FROM APU TO GENERATORS EMERGENCY LIGHTS ILLUMINATED WHILE IN THE ARMED POSITION. GATE RETURN INITIATED. SWITCHED TO GROUND POWER, RESET EMERGENCY LIGHT SYSTEM, OPS CHECKED NORMAL, PER M/M 33-50-01. OK TO CONTINUE. 2L73 4F A3WE 20041012000912004101200091NM 2004 10 12 04FDEA02551 120040823A5330 SKIN BOEING727 727200 138407ENM FUSLEAGE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FUSELAGE SKIN CHAFED STA 720D 12 STR 19L. *S/D* REPAIRED DAMAGED UPPER SKIN AT BS 720D PLUS 12 STR 19L PER SRM 53-30-3 DETAIL 2 & FED EX SR27-57-056 DRAWING. 2L73 4F RTA3WE 20041012000972004101200097EU 2004 10 12 04FDEA02561 120040825A2910 HYDRAULIC SYSTEM AIRBUS300 A300B4605R 3930308EU GREEN SYS MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25659FE 757 REJECTED T/O AT APPROXIMATLEY 80 KIAS STANDARD POWER SET AT 109 N1 ON BOTH ENGINES. ECAM WARNING OF LOW HYDRAULIC PRESSURE ON NR 2 PUMP. RETURNED TO RAMP FOR INSPECTION. INSPECTED ALL AIRCRAFT EXTERIOR FOR OBVIOUS LEAKS, NONE FOUND. SUSPECT RIGHT HAND SIDE OF GREEN HYD SYS CAVITATED MOMENTARILY WHILE SUCTION WAS PERFORMED FROM GREEN SYS TANK. SERVICED GREEN SYSTEM TO TOP HAT INDICATION IAW AMM 12-12-29-0. CREW RAN BOTH ENGINES FOR 2 MINUTES, ALL INDICATIONS ARE NORMAL HYD QTY REMAINS STABLE. OK FOR SERVICE. 2L72 4F RTA35EU 20041012000982004101200098NM 2004 10 12 04FDEA02562 120040824A3411 PITOT HEAD DOUG MD11 MD11 3023602NM CAPTAIN'S OBSTRUCTED A FDEAA UNSCHED LANDING G MULTIPLE FAILURE DEDESCENT 1 SO25605FE 48514 ON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. BY TOUCHDOWN, F/O'S INDICATOR READ 156 KNOTS, CAPTAINS READ 118 KNOTS IN YELLOW. FACT: NUMEROUS FAULTS ON FAULT REVIEW, ADC 1 & 2, FMC 1 & 2, ELEV LD FEEL ACT AND ELEV ACT RIB AND LOB. T/S PER FIM, FOUND A/S TOLERANCE BETWEEN CAPT AND F/O BEYOND LIMIT. FOUND SMALL DEBRIS IN CAPT PITOT PROBE. PURGED, REMOVED AND REPLACED CAPT PROBE & NR 1 CADC. 2L73 4F RTA22WE 20041012001022004101200102NM 2004 10 12 04FDEA02496 120040817A5510ALC80552 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80321, TITLE: STABILIZER - HORIZONTAL STABILIZER - RIGHT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. REPAIR COMPLIED TO FEDEX EA 1-5510-80321, TITLE: STABILIZERS - HORIZONTAL STABILIZER - RIGHT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. 2L73 4F RTA22WE 20041012001062004101200106NM 2004 10 12 C1HA200497006 120040912A5754651729414 RIB BOEING727 727270 138408PNM NR 3 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF ACTUATOR PISTON ROB END MOUNTING NUT (MARKED) WS 519. CRACK = 1 INCH. REPLACED RIB. 2L73 4F RTA3WE 20041012001182004101200118NM 2004 10 12 C1HA200479004 120040913A3260 WARNING LIGHT BOEING727 727225 1384077NM MLG ILLUMINATED A C1HAO OTHER N FALSE WARNING DEDESCENT 1 GL15679MG 22557 UPON LANDING, GEAR EXTENSION, NOSE LEFT & RIGHT MAIN LANDING GEAR RED UNSAFE LIGHTS ILLUMINATED WITH ALL GREEN DOWN AND LOCKED LIGHT. PERFORMED COM PROCEDURES. ALL INDICATIONS NORMAL. PERFORMED GEAR INDICATION FUNCTIONAL TEST IAW MM 31-09-121. COULD NOT DUPLICATE. SYSTEM GROUND CHECK GOOD. 2L73 4F A3WE 20041012001192004101200119NM 2004 10 12 C1HA200492016 120040714A7700 WARNING LIGHT BOEING727 727200 138407ENM PWA JT8 JT8D* NE NR 1 ENGINE ILLUMINATED A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15292CA 21458 696657 AFTER DEPARTURE NR 1 ENGINE BYPASS INDICATOR ILLUMINATED. PERFORMED COM 2-72-19 PROCEDURE. RETURNED TO DFW CHANGED NR 1 ENG MAIN OIL FILTER REF MM 79-15-00. RAN ENG, INSPECTED FILTER, NO PARTICAL FOUND REF MM 71-00-00. INSPECTED NO DEBRIS NOTED REF P&W MM 72-00, SUBSEQUENT NR 1 ENGINE CHANGE. 2L73 4F4 FRTA3WE E2EA 20041012001212004101200121NM 2004 10 12 C1HA2004006 120040919A3230 ACCESSORY UNIT BOEING727 727225 1384077NM MLG MALFUNCTIONED A C1HAO OTHER J WARNING INDICATION CLCLIMB 1 GL15679MG 22557 ON GEAR RETRACTION LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. COM PROCEDURES FOLLOWED. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW M/M 32-09-121, OPS CHECK IAW M/M 32-09-121 PG 501. OK FOR SERVICE. 2L73 4F A3WE 20041012001252004101200125NM 2004 10 12 C1HA200497011 120040913A5315 FLOORBEAM BOEING727 727270 138408PNM FUSLEAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24. 2L73 4F RTA3WE 20041012001312004101200131EA 2004 10 12 COMA0460554 120040928A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 CARGO FLOORBEAM CAP IS CORRODED. REPAIRED IAW CRJ SRM 51-42-21. 2L72 4F RTA21EA 20041012001342004101200134EA 2004 10 12 COMA0460545 120040928A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01937CA 7044 CARGO FLOORBEAM CAP CRACKED. REPAIRED IAW CRJ SRM 51-42-13. 2L72 4F RTA21EA 20041012001372004101200137 2004 10 12 SWAA042830 420040929A256565C19901 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041012001502004101200150NM 2004 10 12 SWAA042879 120041005A5320BAC1505 GUSSET BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER STOP FITTING GUSSET CRACKED. REMOVED AND REPLACED DOOR GUSSET PER SRM. 2L72 4F RTA16WE 20041012001512004101200151NM 2004 10 12 SWAA042880 120041004A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500D, BS 520, STRINGER 12L. 2L72 4F RTA16WE 20041012001622004101200162NM 2004 10 12 SWAA042947 120041010A52106529994 PIN BOEING737 7377H4 1384404NM L1 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 L1 DOOR WILL NOT OPEN. REMOVED AND REPLACED L1 DOOR GUIDE ARM PIN AND LOWER RETAINING SCREW PER MM. 2L72 4F RTA16WE 20041012001722004101200172NM 2004 10 12 SWAA042919 120041007A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 200, RT SIDE. REPAIRED FRAME PER T1-153-018. 2L72 4F RTA16WE 20041013000012004101300001EU 2004 10 13 MALA040589 120040908A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15505XJ E2313 BATTERY PACK 61-2275-1 SN/2715 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED AND PASSES CMM CHECKS. A/C RETURNED TO SERVICE 9/14/04. REFER TO WO NR 375413 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20041013000062004101300006NM 2004 10 13 2004UALA00872 120040928A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 MAIN CABIN BODY STATION 680 TO 740 LBL 63 FLOOR CREASE BEAM HAS SEVERAL AREAS OF CORROSION. REPLACED CREASE BEAM. 2L72 4F4 FRTA2NM E17NE 20041013000142004101300014WP 2004 10 13 04FDEA02868 120041004A2570S392945221 BLANKET DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE ZONE 100 BURNED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25316FE 48314 IN CENTER ACCESSORY COMPARTMENT AT THE LT AND RT FUSELAGE FEED THROUGH FOR THE PNEUMATIC SUPPLY DUCTS 1-2 AND 1-3 HAVE FUSELAGE INSULATION BLANKETS SEVERELY BURNED AROUND THE DUCT. A/C FUSELAGE WAS INSTALLED WITH OLD TYPE OF INSULATION BLANKET. (P/N 3929452-2) BLANKET WAS NOT SECURED AND LAND ON TOP OF LT AND RT PNEUMATIC DUCTS LOCATED IN CAC AND CAUSED BLANKET TO BURN. CORRECTIVE ACTION: PNEUMATIC DUCTS FOR SYSTEM 1 AND 3 IN CAC INSPECTED FOR ANY KIND OF CRACK AND NO DEFECT IS NOTED. RECOVER DUCTS WITH HEAT RESISTANCE INSULATION BLANKET. OPS. AND LEAK CHECK GOOD PER CMM 20-20-01. EMP 435071, 224967, AND QA144239. 2L73 4F4 FRTA22WE E23EA 20041013000592004101300059EU 2004 10 13 AWXA200401084 120040926A5315D53472188200 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT, AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F4 FRTA28NM E40NE 20041013000832004101300083WP 2004 10 13 MWEA040180 120041001A5320993061237 CUSP WEB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSLEAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 CUSP MEMBRANE IS CRACKED AT STATION 1245 LT SIDE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20041013001182004101300118EA 2004 10 13 SWIA200413872 120040920A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07944SW 7764 FS 280.00 RT FLOORBEAM RBL 9.0 OB ATTACH ANGLE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-20 AND 51-23-00. 2L72 4F4 FRTA21EA E15NE 20041014000072004101400007NM 2004 10 14 DL73S040931 120040927A531065479592 DOOR FRAME BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 INSPECTION OF THE C2 DOOR OPENING FRAME AT FS 794 PER AD 93-14-10 REVEALED CRACK IN THE DOOR FRAME WEB AND FLANGE JUST BELOW THE NR 5 DOOR STOP FITTING. THE CRACKS WERE REMOVED WITH A CUT OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND AN EXTERNAL ALUMINUM SKIN DOUBLER PER ER/A 093455 -14AD. 2L72 4F RTA16WE 20041014000082004101400008NM 2004 10 14 DL76L040941 120041002A2510 MOTOR BOEING767 767332 1382001NM COPILOT SEAT FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27172DN 24775 F/O'S SEAT BEGAN MOVING UNCOMMANDED, MOTOR IN SEAT BEGAN SMOKING THEN BURNED OUT C/B POPPED. FWD TO MCO AND PLACARD PER MEL 25-11-01A C/B PULLED AND COLLARD. 2L72 4F RTA1NM 20041014000102004101400010NM 2004 10 14 SWAA042950 120041011A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041014000112004101400011NM 2004 10 14 SWAA042951 120041011A335065C27095 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY, FWD SERVICE, AFT ENTRY, AFT SERVICE DOORS AND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20041014000262004101400026SO 2004 10 14 MASA200400500 120040905A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07825MJ 145179 DURING PREFLIGHT NOTICED EMERGENCY LIGHTING AT THE OVERWING EXITS WERE INOP. MAINTENANCE WAS NOTIFIED AND RELAMPED THE LIGHTS AS NEEDED. AIRCRAFT CONTINUED OPERATIONS. 2L72 4T RTT00011AT 20041014000302004101400030EA 2004 10 14 MASA200400505 120040907A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0797325 7325 EMERGENCY DOME LIGHT IN CENTER ROW INOP. RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041014000402004101400040NM 2004 10 14 MASA200400478 120040826A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY INOPERATIVE A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07455YV1053 455 RETURNED TO THE FIELD DUE TO THE CARGO SMOKE DETECTOR ANNUNCIATOR WAS INTERMITTENT IN FLIGHT. EVERYTHING WAS REMOVED FROM THE CARGO COMPARTMENT AND THE SMOKE DETECTOR WAS DEFERRED WITH THE CREW. A/C DEPARTED WITHOUT FURTHER INCIDENT. 8/27/04 MAINTENANCE REPLACED SMOKE DETECTOR. 2H72 4T RTA13NM 20041014000442004101400044NM 2004 10 14 DL76G040952 120041007A2612 CIRCUIT CARD BOEING767 767332 1382001NM FIRE PANEL INTERMITTENT A DALAO OTHER N FALSE WARNING CLCLIMB 1 SO271602 29694 ON DEPARTURECLIMBING THRU 1000 FT DISCRETE FIRE LIGHT ILLUM WITH NO AURAL OR OTHER VISUAL INDICATIONS, LIGHT EXT PASSING THRU 4000 FT. REPLACED AFOLTS CARD. 2L72 4F RTA1NM 20041014000552004101400055SO 2004 10 14 MASA200400512 120040909A783083990168 SWITCH EMB 145 EMB145LR 3260212SO THRUST REVERSER WORN A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07851MJ 145572 E2 THRUST REVERSER DISAGREE EICAS MSG. AIRCRAFT DIVERTED TO PIT. MAINTENANCE C/W MEL PROCEDURES FOR THRUST REVERSER. 9/10 MAINTENANCE REPLACED DEPLOY SWITCH. 2L72 4T RTT00011AT 20041014000582004101400058NM 2004 10 14 DL76G040943 120041003A2530 ODOR BOEING767 7673P6 1385105NM FWD GALLEY DETECTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271501P 24983 F/A IN FWD GALLEY REPORTED AN ELECTRICAL ODOR. LEAD F/A COULD NOT SMELL ANY UNUSUAL ODOR. ODOR STOPPED SOON AFTER INITIALLY DETECTED. F/A WHO COMPLAINED REPORTED IT MAY BE THE BUN WARMER. BUN WARMER SHOULD BE CHECKED. CHECKED FWD GALLEY AREA. NO PROBLEMS FOUND. FWD TO MCO AND PLACARD PER MEL 25-20-01B. C/B COLLARED. 2L72 4F RTA1NM 20041014000612004101400061EA 2004 10 14 MASA200400489 120040831A33501317 BULB CNDAIRCL600 CL6002C10 1390015EA RT OVERWING BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07503MJ 10058 MAINTENANCE FOUND THE RIGHT HAND AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE PLACED THIS ON MEL. 9/1 MX RELAMPED, OPS CHECK GOOD. 2L72 4F RTA21EA 20041014000672004101400067EA 2004 10 14 MASA200400524 120040913A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 2 INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 ROW 2 FLOOR EMERGENCY LIGHT STRIP INOP. PLACED ON MEL. 9/19/04 MX REMOVED AND REPLACED THE LIGHT STRIP. 2L72 4F RTA21EA 20041014000692004101400069EA 2004 10 14 MASA200400530 120040916A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07919FJ 15019 EMERGENCY LIGHTS INOP. MAINTENANCE RESET THE SYSTEM, OPS GOOD. 2L72 4F RTA21EA 20041014000712004101400071EA 2004 10 14 MASA200400535 120040918A3350 LENS CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT MISSING A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07902FJ 15002 CENTER AISLE EMERGENCY EXIT LENS COVER WAS MISSING. MAINTENANCE REPLACED THE LENS COVER. 2L72 4F RTA21EA 20041014000902004101400090NM 2004 10 14 CALA0400671 120040926A5311BAC1517706 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 LT MAIN FRAME CRACKED. REPAIRED PER ECRA 5311-01158. 2L72 4F RTA16WE 20041014000922004101400092NM 2004 10 14 DL757040944 120041003A2120 A/C PACK BOEING757 757232 1384965NM RIGHT SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27638DL 23761 RIGHT PACK CYCLED OFF AND ON DURING APPROACH. PASSENGER CABIN REPORTED SOME LITE SMOKE PROBABLY FROM RIGHT PACK. SECURED RIGHT PACK. NO BITE ON RIGHT PACK CONTROLLER, VERIFIED OK. RAN RIGHT PACK ON GROUND WITH RECIRC / GASPER ON. F/A NOTED SMELL WAS NOT ELECTRICAL. RIGHT PACK OPS AND INDICATION OK. OK FOR SERVICE. 2L72 4F RTA2NM 20041014000942004101400094NE 2004 10 14 DL757040947 220041005A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 MELTED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO27658DL10497 24420 728705 DURING T/O ROLL, PRIOR TO 60 KNT, AS POWER CAME UP TO T/O POWER, A LOUD BANG OCCURRED WITH LEFT ENGINE READING OIL PRESSURE ZERO, N1 ZERO. ACCOMPLISHED ABORT. REPLACING NUMBER ONE ENGINE. 2L72 4F4 FRTA2NM E17NE 20041014000952004101400095NM 2004 10 14 DLM88040948 120041005A4920 APU DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE AFT SMOKE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27914DE13240 P80122 49957 P80122 APU CAUSED SMOKE IN THE CABIN AFTER LANDING IN LGA WITH LAV SMOKE DETECTOR GOING OFF. FOUND APU LEAKING OIL INTO INLET. PERFORMED PNEUMATIC SYSTEM DUCT BURN OUT OPN 5089. ALL NORMAL NO SMOKE OR ODOR IN CABIN, ALSO DEF APU PER MEL 49-00-01A. 2L72 4F4 FRTA6WE E2EA 20041014000962004101400096SO 2004 10 14 MASA200400389 120040709A3350 LIGHT EMB 145 EMB145LR 3260212SO BULKHEAD INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 THE FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOP. MX RESECURED THE LIGHT ASSEMBLY AND IT OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20041014000972004101400097SO 2004 10 14 MASA200400391 120040710A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07837MJ 145367 CREW REPORTED THE LT WING FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED AND IT OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041014000992004101400099EA 2004 10 14 MASA200400420 120040723A3350 SOCKET CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT UNSECURE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0717172 7172 A FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. MX SECURED LAMP TO LAMP SOCKET. 2L72 4F RTA21EA 20041014001012004101400101NM 2004 10 14 DL73S040949 120041005A5330 SKIN BOEING737 737232 1384475NM STA STR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27315DL 23087 FOUND ON X-2 LETTER CK, 3.5 INCH CRACK IN FUSELAGE SKIN STA 944 AND STR 25 RIGHT. REPAIRED PER SRM 53-30-3 FIG 48. 2L72 4F RTA16WE 20041014001032004101400103NM 2004 10 14 CALA0400673 120041008A53116546568578 FRAME BOEING737 7373T0 1384582NM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 CORROSION ON BS 1016 PRESSURE CHORD. INSTALLED NEW CHORD PER SRM 53-80-08. 2L72 4F RTA16WE 20041014001052004101400105NM 2004 10 14 DL76S040928 120040928A2910272T45002362 TUBE BOEING767 767332 1382001NM HYD SYSTEM UNSERVICEABLE A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27136DL 23146 C-HYD QTY DRAINED TO 0 WITH SUBSEQUENT C-SYS FAILURE. FOUND CRACKED HYD LINE RT WHEEL WELL REF IPC 32-31-55- 01 ITEM 519. INSTALLED INTERIM LINE. LEAK CHECK OK. LINE TO BE INSPECTED WITHIN 175 FLT HRS AND REPLACED WITH PERMANENT LINE WITHIN 350 FLT HRS, NEEDS NEW LINE DAL P/N 321204711. 2L72 4F RTA1NM 20041014001072004101400107NM 2004 10 14 DL73S040938 120040930A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334DL 23105 THE FUSELAGE SKIN WAS FOUND WITH A 2.7 INCH CRACK RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE THE STRINGER 25R SKIN LAP JOINT AT FS 930. THE CRACKED AREA WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 093963-14. 2L72 4F RTA16WE 20041014001102004101400110NM 2004 10 14 DL75K040950 120041006A5610141T480150 WINDSHIELD BOEING757 757232 1384965NM COCKPIT FAILED A DALAO OTHER M OVER TEMP CRCRUISE 1 SO27696DA 29728 RT FWD WINDSHIELD OUTER PANE SHATTERED AT FL410, INNER PANE OK. ARC ACROSS WINDSHIELD. REPLACED WINDSHIELD. 2L72 4F RTA2NM 20041014001142004101400114WP 2004 10 14 04FDEA02464 120040813A5753ARC0503 HINGE BRACKET DOUG DC10 DC1030 3023501WP LT OUTBD FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25326FE 47813 C/W WITH EA 8-5740-78234 WING LT OTBD FLAP OUTBD HINGE BRACKET, ACT MOUNT HOLES REPAIR P/N ARC0503. COMPLIED WITH EA 8-5740-78234 TO INCLUDE REV A WINGS LT OUTBD FLAP, OUTBD HINGE BRACKET ACTUATOR MOUNT HOLES REPAIR, P/N ARC0503 AT MAE. 2L73 4F A22WE 20041014001162004101400116NM 2004 10 14 04FDEA02467 120040813A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CRACKED STRINGER 15 LT AT BS 720B 4 INCHES. *S/D* REPAIRED STR 15L, BS 720B 4 INCHES IAW SRM 53-10-3. 2L73 4F RTA3WE 20041014001182004101400118NM 2004 10 14 04FDEA02469 120040813A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FWD CARGO COMPARTMENT FRAME DENTED STA 500 BETWEEN STR 22L AND 23L. *S/D* REMOVED DAMAGE AREA OF FRAME BS 500 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3. 2L73 4F RTA3WE 20041014001202004101400120NM 2004 10 14 04FDEA02534 120040819A5510ALC80551 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80320. TITLE: STABILIZERS - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. REPAIR COMPLIED TO FEDEX EA 1-5510-80320, TITLE: STABILIZERS - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. 2L73 4F RTA22WE 20041014001222004101400122WP 2004 10 14 04FDEA02433 120040811A5320ADA0140 PANEL DOUG MD10 MD1010F 3022112WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 FWD CARGO SUMP PANEL CRACKED & CORRODED STA 920 TO 940. REMOVED AND REPLACED PANEL IAW SRM 51-21-01 AND DRWG ADA 0140 AT MAE. 2L73 4F RTA22WE 20041014001242004101400124NM 2004 10 14 04FDEA02493 120040817A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CRACKED OUTER FRAME ANGLE STA 804.5 STR 14R. *S/D* REMOVED & REPLACED ANGLE AT BS 804.5 STR 14R PER SRM 51-30-2 & 51-10-1. 2L73 4F RTA3WE 20041014001252004101400125NM 2004 10 14 04FDEA02483 120040816A7830 TRACK DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 ENGINE NR 1: RIGHT HAND THRUST REVERSER COWL UPPER SLIDER TRACK END FOUND CRACKED. NR 1 ENGINE RIGHT HAND THRUST REVERSER COWL ELECTRICAL CONNECTOR DISCONNECT, THRUST REVERSER COWL REMOVED. REPAIR CARRIED OUT ON UPPER SLICK TRACK END REFER TO FAA FORM 8130-3, FORM TRACKING NUMBER 5382 (7009567-000) FOR FURTHER WORK DETAILS BY RHOR AERO SERVICES ASIA PTE LTD. THRUST REVERSER COWL REINSTALLED AS PER MM 78-33-01-4. LATCH ADJUSTMENT/TEST CARRIED OUT AS PER MM 78-33-10-5. ELECTRICAL CONNECTOR RECONNECTED AS PER MM 71-50-05-4. FUNCTIONAL TEST CARRIED OUT AS PER MM 78-30-00, FOUND SATISFACTORY. 2L73 4F RTA22WE 20041014001262004101400126NM 2004 10 14 UIEA200400157 120040917A5312 BULKHEAD BOEING747 7472D7B 1384803NM FUSELAGE CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15528MC 22472 DURING SCHEDULED MAINTENANCE, FS 1350 BULKHEAD WED FOUND CORRODED NEAR STRINGER 1L LEVEL OF CORROSION, LEVEL 1, MINOR. TRIMED OUT CORRODED AREA. REMOVED NICKS, SCRATCHES, GOUGES, BURRS AND SHARP EDGES FROM THE REPAIR PART. PERFORMED HFEC INSPECTION TO ENSURE CRACK FREE CONDITION. REPAIR DOUBLER WAS MADE FROM .063 INCH THICK 7075-T6 MATERIAL. (M) 2L74 4F RTA20WE 20041014001282004101400128EU 2004 10 14 A6WA200460038 120040923A5553 ANGLE BAC 146 146200A 1500266EU FUSE TO STAB CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31156TR E2156 FOUND CRACK ON THE VERTICAL STAB TO FUSELAGE CLOSING ANGLE RIGHT SIDE AT APPROX FRAME 45. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015004. (M) 2H74 4F A49EU 20041014001292004101400129EU 2004 10 14 A6WA200460036 120040903A5311 FRAME BAG BAE146BAE146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31156TR E2156 FOUND CRACK JUST AFT OF FRAME 29 RIGHT EMANATING FROM A RIVET. MAINTENANCE REQUESTED A REPAIR FROM BAE SYSTEMS REF AVMAX 656-2015002. (M) 2H74 4F RTA49EU 20041014001342004101400134NM 2004 10 14 USAA040582 120040826A575465C26602263 SKIN BOEING737 7374B7 1384702NM SLAT CHIPPED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SLAT WITH .25 INCH CHIP IN EDGE MATERIAL, NR 2 SLAT OUTBOARD OF INBOARD ALTERNATE TRACK. REMOVED DAMAGE, INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M) 2L72 4F RTA16WE 20041014001352004101400135NM 2004 10 14 USAA040565 120040906A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND SKIN CRACKED 2 INCHES, FS 124-126 AFT SPAR LOWER SURFACE LEFT HORIZ STAB. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS PER TR 55-10-07B. (M) 2L72 4F RTA16WE 20041014001362004101400136NM 2004 10 14 USAASB04120 120040908A3233651781914 ACTUATOR BOEING737 737301 1384611NM NLG W/W MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19558AU 23512 BOS - FLT 2037 - AFTER TAKEOFF FROM BOS, CLIMBING THROUGH 800 FEET, CAPTAIN RETRACTED LANDING GEAR AND RECEIVED AN UNSAFE NOSE GEAR INDICATION. CAPTAIN ACCOMPLISHED CHECKLIST AND EXTENDED LANDING GEAR. NORMAL GEAR INDICATIONS WERE RECEIVED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK ACTUATOR PER MM 32-33-21. PERFORMED SATISFACTORY GEAR SWING. OPERATIONAL CHECK AND LEAK DHECK GOOD. (M) 2L72 4F RTA16WE 20041014001392004101400139EU 2004 10 14 2004F00403 120040910A2910SD3730748XA LINE STBROSSD3 SD330 8100602EU HYDRAULIC SYS LEAKING A DATAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL13336MV SH3018 DURING THE CLIMB-OUT WHEN THE GEAR WAS RAISED, THE FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R ILGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. THE EMERGENCY, CRUISE AND DESCENT CHECKLISTS WRE COMPLETED. THE ATC WAS NOTIFIED AND IT WAS REQUESTED TO LAND IMMEDIATELY. THE AIRCRAFT LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STATIONED ALONG THE RUNWAY. A MECHANIC FROM MKE WAS DISPATCHED TO MCI. THE RIGHT MAIN GEAR DOWNLOCK HYDRAULIC LINE HAD A HOLE IN IT. THE HYDRAULIC LINE WAS REMOVED AND REPLACED IAW THE SD3-30 MM CH 32. THE HYDRAULIC FLUID WAS REPLENISHED IAW SD3-30 MM, CH 12-10-29. THE GEAR SWING WAS NOT COMPLETED A2H72 4T A41EU 20041014001422004101400142 2004 10 14 2004F00405 420040913A34000660402600 RECEIVER BEECH 300 300BEECH 1152930CE COCKPIT ODOR A RU3AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW1573 FF8 ON FINAL APPROACH KLN-88 RECEIVER FLICKERED AND THE SCREEN WENT BLANK. A STRONG ELECTRICAL ODOR PREVAILED THROUGH OUT THE CABIN. KLN-88 WAS TURNED OFF AND AIRCRAFT LANDED WITHOUT INCIDENT. APPARENT CAUSE WAS KLN-88 POEWR SUPPLY FAILURE. (M) 2L72 4T A24CE 20041014001502004101400150NM 2004 10 14 USAA040621 120040917A53201133482 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, FRAME 847, STRINGER STRINGER S4R. DRILLED NEW CLIP AND REPLACED CLIP PER SRM 53-40-03. (M) 2L72 4F RTA16WE 20041014001522004101400152NM 2004 10 14 USAA040616 120040821A5330 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SKIN CLIP CRACKED .5 INCH, 706 LT AND S12. REPLACED CLIP PER SRM 51-40-03. (M) 2L72 4F RTA16WE 20041014001542004101400154NM 2004 10 14 USAA040622 120040917A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND STUB FRAME CRACKED .5 INCH LONG, STATION 360, S11L. FABRICATED NEW CLIP AND INSTALLED PER SRM 51-40-02 AND BOEING DWG 60-48985. (M) 2L72 4F RTA16WE 20041015000012004101500001EA 2004 10 15 ASOA04662 120040830A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11858AS 7417 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 21 IN THE CARGO COMPARTMENT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M0 2L72 4F RTA21EA 20041015000022004101500002NM 2004 10 15 USAA040580 120040815A5310141N5810455 BEAM BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 FOUND BEAM CORRODED 7 INCHES BY 4 INCHES AND TWO INCH CRACK, STATION 297, LBL 22. REPLACED BEAM PER EA 9579, SRM 51-10-02. (M) 2L72 4F RTA2NM 20041015000042004101500004NM 2004 10 15 AMTA200401157 120040919A5310 CREASE BEAM BOEING757 75723N 1384973NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11522AT 29330 FOUND CORROSION ON CREASE BEAM STATION 1240 RBL 67.5 WL 208. REPAIRED DAMAGE PER SRM 51-70-12 FIG 1. (M) 2L72 4F RTA2NM 20041015000052004101500005NM 2004 10 15 USAA040579 120040820A5320141N5810492 STRAP BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND DOUBLER STRAP CORRODED 6 SQUARE INCHES, STATION 290, LBL COCKPIT FLOOR LEVEL. FABRICATED AND INSTALLED DOUBLER STRAP PER EA 95679, SRM 51-40-02, DWG 141N5810. (M) 2L72 4F RTA2NM 20041015000062004101500006NM 2004 10 15 USAA040568 120040903A5330 BEAR STRAP BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU63100 22198 CLT - FOUND BEAR STRAP CRACKED, L2 DOOR FORWARD UPPER CORNER AT FASTENER HOLE. DAMAGE REMOVED, DOUBLER AND TRIPLER OVER FILLER PER EA 95799. (M) 2L72 4F RTA2NM 20041015000072004101500007NM 2004 10 15 USAA040570 120040902A5310 DOOR FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU63100 22198 CLT - FOUND FRAME CRACKED .25 INCH, E-E ACCESS DOOR AT FRAME WEB TO FLANGE CORNER RADIUS. DAMAGE AREA REPAIRED IAW EA 95806. (M) 2L72 4F RTA2NM 20041015000092004101500009NM 2004 10 15 USAA040623 120040917A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, STRINGER CLIP, CABIN OVERHEAD BS 601 S6L. INSTALLED NEW CLIP PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20041015000102004101500010NM 2004 10 15 USAA040627 120040905A5320 SUPPORT ANGLE BOEING737 7374B7 1384702NM CARGO TRACK CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SUPPORT ANGLE CORRODED 1 INCH BY .5 INCH AREA, AFT CARGO RT TRACK SUPPORT ANGLE ABOVE STRINGER 26R. REMOVED AND REPLACED ANGLE PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-202-01. (M) 2L72 4F RTA16WE 20041015000112004101500011NM 2004 10 15 USAA040628 120040828A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH WIDE, BETWEEN STATION 947 AND 967 RBL 18. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20041015000132004101500013NM 2004 10 15 USAABB04085 120040911A2610233N620413 PANEL BOEING757 7572B7 1384964NM COCKPIT MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19611AU 27123 SXM - FLT 1442 - AFTER TAKEOFF, THE CREW RECEIVED THE EICAS MESSAGES 'AFT CARGO FIRE' AND 'FWD CARGO FIRE.' THE QRH PROCEDURES WERE FOLLOWED AND THE BOTTLES FIRED. THE FLIGHT RETURNED TO SXM. MAINTENANCE INSPECTED THE CARGO FIRE SYSTEM AND COULD NOT FIND ANY DISCREPANCIES. AN ELECTRICAL SMELL WAS NOTED IN THE COCKPIT, AND IT WAS DISCOVERED THAT HEAVY CONDENSATION FROM THE OVERHEAD HAD BEEN DRIPPING ON THE CENTER PEDISTAL FIRE TEST CONTROL MODULE. THE MODULE WAS REPLACED. THE SYSTEM WAS TESTED, INCLUDING AN ENGIEN RUN, AND CHECKED SATISFACTORILY. (M) 2L72 4F RTA2NM 20041015000152004101500015NM 2004 10 15 USAA040583 120040902A5312 CHANNEL BOEING737 7374B7 1384702NM BULKHEAD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND RADIAL CHANNEL CORRODED 1 SQUARE INCH, AFT PRESSURE BULKHEAD. REMOVED CORROSION, MANUFACTURED AND INSTALLED RADIAL CHANNEL PER EO 5302V112. (M) 2L72 4F RTA16WE 20041015000162004101500016NM 2004 10 15 USAA040584 120040905A5240 CHANNEL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND Z-CHANNEL APPROXIMATELY 3 INCHES LONG, NUMEROUS AREAS, RIGHT AFT SERVICE DOOR Z-CHANNEL STAITON 961-992. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED Z-CHANNEL, CLEANED AND TREATED FOR CORROSION, INSTALLED NEW CHANNEL PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20041015000182004101500018NM 2004 10 15 USAA040617 120040920A5730 PANEL BOEING737 7374B7 1384702NM LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND WING PANEL CRACKED 3 INCHES, LEFT ENGINE PYLON, WING UPPER SURFACE FIXED PANEL AFT INBOARD EDGE. INSTALLED DOUBLER AND SEALED PER TYP REPAIR 54-50-14A. (M) 2L72 4F RTA16WE 20041015000212004101500021NM 2004 10 15 USAA040624 120040908A5330 SKIN BOEING737 7374B7 1384702NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SKIN CHAFED 1 INCH BY .250 INCH WIDE BY .006 INCH DEEP, STAITON 879 BETWEEN STRINGER 1L AND 2L. INSTALLED DOUBLER, TRIPLER PER SRM 53-00-01 FIG 231. (M) 2L72 4F RTA16WE 20041015000222004101500022NM 2004 10 15 USAA040625 120040917A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND ATTACH ANGLE CORRODED THREE AREAS, APPROX 1.5 INCH BY 6 INCHES, STATION 947 FROM RT ZEE ANGLE TO LEFT ZEE ANGLE. MANUFACTURED AND INSTALLED NEW ANGLE PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20041015000242004101500024NM 2004 10 15 USAA040593 120040829A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH WIDE AREA, FS 947 FLOORBEAM TOP FLANGE RBL 0. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED/SPLICE UPPER FLANGE OF FLOORBEAM PER TYPICAL REPAIR 53-60-02 REV A. (M) 2L72 4F RTA16WE 20041015000252004101500025NM 2004 10 15 AMTA200401155 120040918A3230 ACTUATOR BOEING757 757200 1384950NM DOWNLOCK LEAKING A AMTAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11512TZ 26635 LOSS OF HYDRAULIC FLUID FROM LEFT SYSTEM DURING CLIMB-OUT. FOUND HYDRAULIC LINE TO HYDRAULIC BLOCK ON DOWNLOCK ACTUATOR LEAKING. REMOVED AND REPLACED HYDRAULIC LINE, CYCLED SYSTEM, SERVICED HYDRAULIC TO FULL. OPS CHECK, LEAK CHECK GOOD. OK FOR FLIGHT, PER FIM 32-30-00 FIG 103. (M) 2L72 4F RTA2NM 20041015000282004101500028EA 2004 10 15 REXA04015 120040920A2750 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS TRIPPED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258515F 7515 ON APPROACH FLAPS FAILED AT 20, QRH FOLLOWED, UNEVENTFUL LANDING. CIRCUIT BREAKER RESET PERFORMED, FLAPS PLACED ON 72 HOURS WATCH PER AD 98-20-01. (M) 2L72 4F RTA21EA 20041015000322004101500032EA 2004 10 15 ASOA04664 120040825A5340601R950159 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE RAM AIR SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RAM AIR SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52. (M) 2L72 4F RTA21EA 20041015000332004101500033EA 2004 10 15 ASOA04661 120040830A5210 ROLLER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11841AS 7300 DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR UPPER ROLLER LOCKS P/N 6003189534, ADJUSTED THE DOOR HANDLE P/N 601R389643 AND LUBRICATED THE HANDLE ROLLER P/N 601R3189465. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M0 2L72 4F RTA21EA 20041015000352004101500035NM 2004 10 15 USAA040657 120040921A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND FLOOR SUPPORT HAS TWO CRACKS .25 INCH, NR 6 SLAT BOARD, 1 AT 4 INCH AND 1 AT 5 INCH OUTBOARD OF DEICING TUBE, 1 AT 5 INCH. CLEANED, TREATED AND PRIMED, REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20041015000372004101500037NM 2004 10 15 USAA040655 120040922A5414 DOUBLER BOEING737 7373B7 1384580NM LT NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND DOUBLER AND SKIN CRACKED .75 INCH LONG, OPENING FOR ACCESS PANEL 5727L, LEFT PYLON NACELLE STATION 180 OUTBOARD SIDE. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M) 2L72 4F RTA16WE 20041015000382004101500038NM 2004 10 15 BJNA040901 120040806A5230 CROSSBEAM BOEING737 737282 13844ATNM C-1 DOOR CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 DURING C-CHECK INSPECTION FOUND C-1 DOOR LOWER CROSS BEAM HAS WEB CRACK NEAR AFT CORNER. FABRICATED FILLER, .875 INCH BY 5 INCH AND 5 INCH BY 4 INCH MATERIAL USED 2024T3.050. INSTALLED REPAIR IAW SB 737-52A1100, REV 4 AND SRM 51-30-2 AND 51-10-2. (M) 2L72 4F RTA16WE 20041015000392004101500039SO 2004 10 15 2004F00410 120040516A49101159B31380073 DOUBLER GULSTMG1159 GIV 3980115SO APU BAY CORRODED A O2GAK NONE O OTHER ININSP/MAINT 1 NE03195WS 1050 FOUND CORROSION ON DOUBLER OF APU ACCESS OPENING LOWER FORWARD CORNER. FOUND DURING 24 MONTH INSPECTION. REPAIRED DOUBLER. (M) 2L72 4F RTA12EA 20041015000402004101500040NM 2004 10 15 USAA040599 120040822A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, STATION 807 STRINGER 4L. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-00-00. (M) 2L72 4F RTA16WE 20041015000412004101500041NM 2004 10 15 USAA040567 120040904A5210 SKIN BOEING757 7572B7 1384964NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND DOOR CRACKED .5 INCH, BS 440, BL 0 MEC DOOR INNER SKIN AND FRAME CRACKED UNDER MOUNT FOR BUMPER PAD. REPAIRED PER EA 95817. (M) 2L72 4F RTA2NM 20041015000422004101500042NM 2004 10 15 USAA040606 120040917A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 345 LBL 02. REPAIRED T-CAP PER SRM 53-00-51. (M) 2L72 4F RTA2NM 20041015000442004101500044NM 2004 10 15 USAA040598 120040822A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND CLIP CRACKED .5 INCH, STATION 827 STRINGER 4L TIE CLIP. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-00-00. (M) 2L72 4F RTA16WE 20041015000452004101500045NM 2004 10 15 USAA040608 120040917A5320 WEB BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND WEB CORRODED 1 INCH AREA, STATION 345 AND 365 RBL 65. REPLACED WEB PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041015000462004101500046NM 2004 10 15 USAA040604 120040917A5320 STIFFENER BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND STIFFENER CORRODED 1 INCH, STATION 331 RBL 04. REPLACED STIFFENER PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041015000502004101500050EA 2004 10 15 A6WA200440132 120040913A3230 TRUNNION CNDAIRCL600 CL6002B19 1900309EA MLG CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 FOUND RIGHT MAIN LANDING GEAR, FORWARD TRUNNION, AFT BUSHING HAS PITTING ON FACE OF BUSHING. PERFORMED A MAJOR REPAIR TO PITTED RIGHT MAIN LANDING GEAR FORWARD TRUNNION AFT BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-2003-41 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M) 2L72 4F RTA21EA 20041015000522004101500052NM 2004 10 15 UIEA200400167 120040922A5740 FITTING BOEING747 747230B 1384889NM WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 WHILE PERFORMING EO 4757A087, REAR SPAR UPPER CHORD AND SIDE BODY INSPECTION. CORROSION STILL EXIST ON THE UPPER REAR SPAR INTERNAL SPLICE FITTING AFTER INCORPORATING NR 5 HOLE DIA MAX OF 1.40 INCHES WITH SLEEVED BOLT REPAIR. LEVEL 1 MINOR. REAMED HOLE NR 5 TO FINAL SIZE OF 1.50 INCHES TO COMPLETELY REMOVED THE CORROSION. PERFORMED OPEN HOLE HFEC TO ENSURE HOLE IS DAMAGE FREE. INSTALLED SLEEVED BOLT REPAIR. (M) 2L74 4F A20WE 20041015000532004101500053 2004 10 15 2004F00412 420040815A2300 RADIO CESSNA560 560XL 2076702CE COCKPIT DISLODGED A AJCAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA25102FS 5605318 ON BEGINNING DEPARTURE FROM KSWF, WHEN THE STANDBY COMMUNICATION RADIO HEAD SLID OUT OF ITS RACK APPROXIMITY SIX INCHES ON INITIAL ACCELERATION FOR TAKEOFF. THE TAKEOFF WAS ABORTED AT SEVENTY KNOTS WITHOUT INCIDENT. THE AIRCRAFT RETURNED TO THE CESSNA SERVICE CENTER ON SITE FROM WHICH IT HAD DEPARTED. INVESTIGATION REVEALED THAT THE RADIO UNIT WAS DISLODGED FROM THE INSTRUMENT PANEL. THE UNIT WAS RESECURED IAW THE CESSNA 560XL MM CH 23-80-01. A SATISFACTORY GROUND OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA22CE 20041015000552004101500055EA 2004 10 15 04286692 120041012A3242 BRAKE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT MALFUNCTIONED A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27692BR 7759 EVENT SUMMARY STATES 90 KNOTS STARTED TO YAW LT AND RT. C/W RTO INSPECTION FOUND LT IB BRAKE HARD TO TURN REF CHT 05-51-27. REMOVED AND REPLACED LT IB BRAKE REF CHT 32-43-26. 2L72 4F4 FRTA21EA E15NE 20041015000572004101500057NM 2004 10 15 04FDEA02928 120041013A3210656021132 SOLENOID BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE MLG LOCK FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25245FE 22016 PDIS 245 32-10 0006358 12OCT04 LAX CLOSE R LOGPAGES: 00900921 LANDING GEAR LEVER LATCH FAILED TO RAISE ON TAKEOFF PAST OFF POSITION. RAN QRH. CHECK/RESET LEVER LATCH CB (IAW QRH) AND PULLED AURAL WARNING CB (QRH) AND RETURNED. 2L73 4F4 FRTA3WE E2EA 20041015000582004101500058WP 2004 10 15 04FDEA02929 120041013A5753NRC6062519 FITTING DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 COMPLY WITH EA 8-5750-82057. WINGS LT IB FLAP VANE ASSY, REPAIR OF O SIZED HOLES IN CHANNEL FITTINGS CLOSING ACTION ON 10/12/04.ON N/R S00010. COMPLIED WITH EA 8-5750-82059. 2L73 4F4 F A22WE E23EA 20041015000602004101500060SO 2004 10 15 SWIA200413905 120041011A5310 WINDOW POST EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07270YV 120270 LT PILOTS TO DV WINDSHIELD POST CRACKED LOWER FORWARD CORNER AT FS 3010. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH SB 120-53-0072 REV 0 21 FEB 00. REPAIR WORK PERFORMED IAW SRM 51-40-00. 2L72 4T4 TRTA31SO E20NE 20041015000632004101500063NM 2004 10 15 2004UALA00901 120041003A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 AFT PIT STA 1400, FRAME LT SIDE AT STR 27L IS DENTED. INSTALLED J-ANGLE DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041015000642004101500064NM 2004 10 15 2004UALA00909 120040920A5754 ARM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29648UA 25285 LT IB AFT FLAP, IB HINGE ARM CRACKED BOTH SIDES AT ATTACH POINT TO MAIN FLAP. REPAIRED & INSTALLED FITTING. 2L72 4F4 FRTA1NM E24NE 20041015000662004101500066EA 2004 10 15 SWIA200413908 120040927A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07945SW FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OB RETURN FLANGE; FS 484.00 LBL 36.0. (ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F4 FRTA21EA E15NE 20041015000672004101500067EA 2004 10 15 SWIA200413909 120040927A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE INTERCOSTAL CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07945SW 7770 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00, STR 14R. (ITEM FOUND AT C-CHECK INSPECTION.) CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2L72 4F4 FRTA21EA E15NE 20041015000692004101500069NM 2004 10 15 SB04144 120041012A3260 WARNING LIGHT BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE MLG ILLUMINATED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19591US 23936 PIT FL 1286 UPON GEAR RETRACTION, THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. THE QRH PROCEDURE WAS FOLLOWED (SELECT GEAR DOWN), AND THE CREW RECEIVED THREE GREEN INDICATIONS. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWUNG THE GEAR WITHOUT ANY ABNORMALITIES. A GEAR LUBRICATION WAS PERFORMED. 2L72 4F4 FRTA16WE E2GL 20041015000712004101500071WP 2004 10 15 DHL2004801509 120040902A5511 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 2044: RT HORIZONTAL STABILIZER IB. L/E LWR. FORMER CRACKED 1.000 XFS 47.500. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20041012001232004101200123NM 2004 10 12 C1HA200497005 120040912A5754 RIB BOEING727 727270 138408PNM NR 3 SLAT CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15697CA 23052 NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF ACTUATOR PISTON ROD END AT WS 515 (MARKED). REPAIRED RIB. 2L73 4F RTA3WE 20041012001262004101200126SO 2004 10 12 C2XA04SH505 120040929A33501317 LAMP EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 SHV - DURING SERVICE/ROUTINE CHECK THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMP IAW EMB 145AMM 33-50-09. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041012001282004101200128SO 2004 10 12 C2XA04BT097 120040911A21508152403 ACM EMB 145 EMB145LR 3260212SO CABIN COOLING ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2712563 145612 CREW REPORTED, PUNGENT BURNING OR MELTING SMELL OCCURRED DURING THE LAST FIVE MINUTES OF FLIGHT. TURNED OFF NR 2 PACK AND SMELL WENT AWAY. MAINTENANCE INSPECTED PACK NR 2 SYSTEM AREA, CLEANED RAM AIR DUCT. OPS CHECKED GOOD IAW EMB 145 MM 21-60-00. AIRCRAFT RETURNED TO SERVICE. SDR REMAINS OPEN PENDING MFG NAME AND S/N DATA. 2L72 4T RTT00011AT 20041012001382004101200138EA 2004 10 12 QXEA200400659 120040902A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 800 STIFF A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09601QX7035 10009 DEN - FLIGHT 4436 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE INSPECTED THE MAIN CABIN DOOR AND LUBRICATED THE DOOR LATCH PINS AND LATCH CAMS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041012001532004101200153NM 2004 10 12 SWAA042882 120041005A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 16R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041012001542004101200154NM 2004 10 12 SWAA042904 120041006A53116546548 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041012001552004101200155NM 2004 10 12 SWAA042905 120041006A575465C26685 SKIN BOEING737 7373A4 1384585NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C3 CHECK, FOUND LT WING L/E NR 2 SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER SRM. 2L72 4F RTA16WE 20041012001632004101200163NM 2004 10 12 SWAA042936 120041009A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 480, STRINGER 17R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041012001672004101200167NM 2004 10 12 SWAA042928 120041008A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED C3 CHECK, FOUND FWD EMERGENCY EXIT OVERHEAD LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041012001702004101200170 2004 10 12 SWAA042931 420041008A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R1 DOOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT WORN. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041012001712004101200171 2004 10 12 SWAA042937 420041010A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29728SW 27860 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041012001742004101200174 2004 10 12 SWAA042923 420041007A2565D31354 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29732SW 27864 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041012001752004101200175NM 2004 10 12 SWAA042924 120041007A335065C27095 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29753SW 29848 DURING SCHEDULED 5Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM. 2L72 4F RTA16WE 20041012001762004101200176NM 2004 10 12 SWAA042925 120041007A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29614SW 28033 DURING SCHEDULED C3 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE BETWEEN ROWS 22 AND 23. SECURED LENS PER MM. 2L72 4F RTA16WE 20041012001772004101200177NM 2004 10 12 SWAA042932 120041008A53306545776653 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED PM CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS BETWEEN BS 500C AND BS 500C + 17, STRINGER 15L. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041012001782004101200178NM 2004 10 12 SWAA042912 120041004A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER FWD CORNER CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041012001792004101200179NM 2004 10 12 SWAA042913 120041004A5330141A880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 1/4D CHECK, FOUND R1 COCKPIT WINDOW C/D POST CRACKED AT UPPER CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041012001802004101200180NM 2004 10 12 SWAA042914 120041005A2612356104 FIRE DETECTOR BOEING737 7377H4 1384404NM MLG W/W FAULTY A SWAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW29790SW 30604 DIVERSION, MLG W/W FIRE IND LIGHT ILLUMINATED. REMOVED AND REPLACED MLG W/W M270 FIRE DETECTOR PER MM. 2L72 4F RTA16WE 20041012001812004101200181NM 2004 10 12 SWAA042915 120041007A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, BELOW STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041012001822004101200182NM 2004 10 12 SWAA042916 120041007A53306545771 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C+16, ABOVE STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041012001842004101200184NM 2004 10 12 SWAA042938 120041010A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 793, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041012001862004101200186NM 2004 10 12 04FDEA02497 120040817A5510ALC80551 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO CARRY OUT REPAIR PER FEDEX EA 1-5510-80320, TITLE: STABILIZER - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. SNRM N1212: REPAIR COMPLIED TO FEDEX EA 1-5510-80320, TITLE: STABILIZERS - HORIZONTAL STABILIZER - LEFT HAND OPERATING BULKHEAD REPAIR AFTER EXCEEDING BOEING S/B MD-11 55-023 REVISION 2 LIMITS. 2L73 4F RTA22WE 20041012001882004101200188NM 2004 10 12 04FDEA02490 120040817A5311 FRAME BOEING727 727200 138407ENM FUSELAGE BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 FRAME BENT BS 950F AT STR 26 LT, AFT CARGO BAY. *S/D* FRAME DENT BS 950F AT STR 26 LT AFT CARGO FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F RTA3WE 20041012001902004101200190NM 2004 10 12 SWAA042933 120041009A5522657378435 SKIN BOEING737 7372H4 138448CNM ELEVATOR DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED A1 CHECK, FOUND RT ELEVATOR T/E SKIN DELAMINATED. REPAIRED ELEVATOR SKIN PER EA. 2L72 4F A16WE 20041012001922004101200192NM 2004 10 12 SWAA042941 120041010A55536547450 FITTING BOEING737 7373H4 1384600NM TAIL CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT AND LT REAR SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED FIN PER ER. 2L72 4F RTA16WE 20041012001932004101200193WP 2004 10 12 04FDEA02410 120040809A3251 COLLAR DOUG DC10 DC1030 3023501WP NLG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25313FE 48311 NLG LOWER STEERING SUPPORT COLLAR ASSY CRACKED THROUGH AT FWD SIDE. *S/D* REMOVED AND REPLACED NLG COLLAR ASSY (LOWER COLLAR) WITH NEW PART. 2L73 4F A22WE 20041012001942004101200194NM 2004 10 12 04FDEA02306 120040730A5347AGA385527 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 AFT CARGO RIGHT HAND SEAT TRACK X=20 HAS EVIDENCE OF CORROSION AT STA 1955. CORROSION AT AFT CARGO RIGHT HAND SEAT TRACK X=20 REMOVED AS PER SRM 51-21-01 VOL 2. MATERIAL REMOVED=0.010 INCH, ORIGINAL THICKNESS=0.090 INCH, REMAINING THICKNESS=0.080, FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIG 3 VOL I (MINIMUM THICKNESS=0.060 INCH). REWORKED AREA REPROTECTED AND PAINTED AS PER SRM 51-21-01 VOL 2. 2L73 4F RTA22WE 20041012001952004101200195NM 2004 10 12 SWAA042934 120041009A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041012001972004101200197NM 2004 10 12 04FDEA02451 120040811A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 STRINGER DENTED AT BS 950C 18, STRINGER 7 LT. *S/D* REPAIRED STR 7L BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358. 2L73 4F RTA3WE 20041012001992004101200199NM 2004 10 12 04FDEA02453 120040811A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 BS 848 STR 7L UPPER FLANGE OF STRINGER IS DENTED AND GOUGED. *S/D* REMOVED DAMAGE AREA OF STRINGER AT BS 848, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR IAW SRM 53-10-3 & FED EX EA 7-5310-55348. 2L73 4F RTA3WE 20041012002012004101200201NM 2004 10 12 04FDEA02455 120040811A5315BAC150529222 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION (C53-224-01, 1) FLOORBEAM STRUCTURE BS 344 LBL 31 TO LBL 58 WL 208. *S/D* REMOVED AND REPLACED UPPER FLOORBEAM CHORD AND REPAIR ANGLES AT BS 344, LBL 65-RBL 16, WL 208 IAW SRM 27-53-007. 2L73 4F RTA3WE 20041013000582004101300058EU 2004 10 13 AWXA200401083 120040926A5320D53112827202 DUMMY RAIL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF DUMMY RAIL Y503, AT FR 16. MAINTENANCE REMOVED DUMMY RAIL Y503, AT FR 16; INSTALLED A NEW REPLACEMENT RAIL IAW A320 SRM 51-42-1, FIG. 9-12. 2L72 4F4 FRTA28NM E40NE 20041013001162004101300116EA 2004 10 13 SWIA200413870 120040925A2711601R5122623SW CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON/RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW 7578 AILERON WILL TRIM TO LT BUT NOT TO RT. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTOL PANEL. OPERATIONAL CHECK GOOD. P/N: 601R51226-23SW. 2L72 4F4 FRTA21EA E15NE 20041014000012004101400001 2004 10 14 ASMF200410007 420041008A34204608000307 AHRS DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NR 2 FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23753RA158 49587 AIRCRAFT RETURNED OF FLIGHT, 30 DEGREES OF COURSE VARIATION AND CAPTAIN HSI WITH 15 DEGREE OF DIFFERENCE IN RESPECT TO THE COMPASS. DURING CHECK, SWITCH WAS DETECTED IN NORMAL POSITION, HSI CAPTAIN OPERATING NORMALLY, CAPTAIN COURSE WITH 10 DEGREE OF DIFFERENCE IN RESPECT TO THE COMPASS, HSI FIRS OFFICES FELT 5 DEGREE, FIRST OFFICER COURSE WITH 10 DEGREE DIFFERENCE WITH RESPECT TO THE COMPASS AND AN AHRS NR 2 MODE BASIC LIGHT TURNED ON. AHRS NR 1 WAS RESEATED AND RESTORED AND AHRS NR 2 WAS DEFERRED IAW MM 34-38. DURING OVERNIGHT SERVICE AHRS NR 2 WAS REPLACED IAW MM 32-2-10, TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20041014000172004101400017SO 2004 10 14 MASA200400475 120040826A2611FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY WILL NOT TEST A MASAK NONE L NO TEST ININSP/MAINT 1 SW07850MJ6083 145568 THE LAV SMOKE DETECTOR WOULD NOT TEST. MX REPLACED THE SMOKE DETECTOR AND THE SYSTEM TESTED NORMALLY. THE A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20041014000232004101400023NM 2004 10 14 CALA0400666 120041008A5311654653935 FRAME BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717345 23583 LEFT MAINFRAME CRACKED. REPAIRED PER ECRA 5311-01158 AND SRM 51-40-20. 2L72 4F RTA16WE 20041014000352004101400035NM 2004 10 14 DL76L040933 120040929A2120 ODOR BOEING767 767332 1382001NM AFT GALLEY DETECTED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27172DN 24775 RETURNED TO GATE DUE TO STRONG ELEC ODOR IN AFT GALLEY NEAR 2R DOOR, OTHER REPORTS BY F/A'S AND PAX INDICATED SMELL RESEMBLED BURNING OIL. CHECKED ALL TRASH AND STORAGE COMPARTMENTS IN AFT GALLEY AND LAV, CHECKED LIGHT FIXTURES AND ABOVE CEILING PANELS, NO TRACE OF BURN SMELL OR PHYSICAL DAMAGE. OPERATED PACKS AND ALL ELECTRICAL EQUIPMENT IN AFT GALLEY AND LAVS. ALSO CHECKED AFT CARGO COMPARTMENT. 2L72 4F RTA1NM 20041014000362004101400036NM 2004 10 14 DL76L040934 120040929A2530 ODOR BOEING767 767332 1382001NM MID GALLEY DETECTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27193DN 28450 MID GALLEY FREEZER GAVE OFF AN ELECTRICAL SMELL. DEACTIVATE FREEZER AND FWD TO MCO. C/B PULLED AND COLLARED. 2L72 4F RTA1NM 20041014000482004101400048EA 2004 10 14 MASA200400460 120040818A3350BR9279232 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A MASAK NONE L NO TEST ININSP/MAINT 1 SW07514MJ 10116 A LAV FLOOR LEVEL EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT WAS PLACED ON MEL. 8/19/04 MAINTENANCE REMOVED AND REPLACED GALLEY FWD EMERGENCY LIGHT. 2L72 4F RTA21EA 20041014000592004101400059SO 2004 10 14 MASA200400488 120040831A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 A SIDE WALL EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE CYCLED THE LIGHT SWITCH AND COULD NOT DUPLICATE THE FAULT. 2L72 4T RTT00011AT 20041014000792004101400079NM 2004 10 14 MASA200400409 120040717A2711LA11A2118 ACTUATOR DHAV DHC8 DHC8202 2809007NM AILERON TRIM INOPERATIVE A MASAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW07455YV371 455 DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A UNCOMMANDED AILERON TRIM RUNAWAY. MAINTENANCE IS STILL IN THE PROCESS OF TROUBLESHOOTING THE PROBLEM. 7/17 MAINTENANCE REPLACED ACTUATOR AND POTENTIOMETER (P/N 1423-100-0). 2H72 4T RTA13NM 20041014001092004101400109NE 2004 10 14 DL76L040940 220041002A7200PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 SHUTDOWN A DALAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 SO27186DN28170 27962 727717 AT TOD - A/T ON LEFT ENGINE SHUTDOWN, RESTARTED AFTER 5 MINUTES. UNDER INVESTIGATION. 2L72 4F4 FRTA1NM E24NE 20041014001112004101400111NE 2004 10 14 04FDEA02261 220040728A7230 FAN AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 ENGINE OUT OF BALANCE A FDEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO25684FE 802 IN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9, VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 80 - 60 PERCENT. *S/D* PERFORMED FAN TRIM BALANCE ON NR 2 ENG IAW A300-600 MM REF 72-21-00-2. ENGINE VIB INDICATED 0.2 UNITS AFTER FAN TRIM BALANCE. OK FOR SERVICE. 2L72 4F4 FRTA35EU E13NE 20041014001132004101400113EU 2004 10 14 04FDEA02440 120040811A5400 PYLON AIRBUS310 A310203 3930313EU NR 1 ENGINE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 NR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54-50-00 AND 54-54-11 FIG 201 AND 54-54-51 FIG 206 BETWEEN PYLON STA 1059 AND STA 1115. 2L72 4F RTA35EU 20041014001152004101400115NM 2004 10 14 04FDEA02466 120040813A533065139131 SKIN PANEL BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25284FE 22621 C/W EA 7-5330-80590 FUSELAGE SKIN REPAIR AT BS 1009 AND STRINGER 30 P/N 65-13913-1. COMPLIED WITH EA 7-5330-80590, FUSELAGE SKIN REPAIR AT BS 1009 STRINGER 30. 2L73 4F RTA3WE 20041014001172004101400117NM 2004 10 14 04FDEA02468 120040813A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CRACKED STRINGER 15 RT BS 720B 4 INCHES. *S/D* REPAIRED STR 15R AT BS 720B 4 INCHES PER SRM 53-10-3. 2L73 4F RTA3WE 20041014001192004101400119NM 2004 10 14 04FDEA02533 120040819A5510ALC8055 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 300 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 TO TRIM OUT HORIZONTAL STABILIZER RIGHT HAND OPERATING BULKHEAD FITTING TO GAIN ACCESS FOR RIGHT HAND UPPER AFT PLANK NR 34R BARREL NUT REWORK. RIGHT HAND HORIZONTAL STABILIZER, OPERATING BULKHEAD FITTING TRIMMED OUT FOR ACCESS AS PER FEDEX EA 1-5510-79826. TITLE: STABLIZERS - HORIZONTAL STABILIZER ACCESS TO REWORK BARREL NUT BORE 34 & 35R. TRIMMING OF THE OPERATING BULKHEAD PER BOEING S/B MD-11 55-023 REV 2. 2L73 4F RTA22WE 20041014001212004101400121WP 2004 10 14 04FDEA02535 120040820A5311ABA7348U3 FRAME DOUG DC10 DC1010 3022110WP N/A CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING PASSENGER TO FRIGHTER CONVERSATION FOUND ON FWD ACCESSORY COMPARTMENT AT STA 459 RT SIDE, 1 CRACK 5 INCHES LONG ON FRAME AND 1 CRACK ON LOWER FLANGE OF THE .90 INCH. REPLACED FRAME PER SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAGE 1-12. 2L73 4F A22WE 20041014001232004101400123NM 2004 10 14 04FDEA02563 120040825A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 COMPLY WITH EO 7-5310-7-3367 PT 9 FOR CRACK IN 783.95 FRAME RT. *S/D* COMPLIED WITH EO 7-5310-7-3367 PT 9. 2L73 4F RTA3WE 20041014001312004101400131EU 2004 10 14 USAA040519 120040828A5321 FLOOR PANEL AIRBUSA321 A321211 3930370EU CARGO BAY DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19166US12095 1436 PIT - FOUND CARGO FLOOR PANEL EDGE DAMAGED, 33 INCH AFT OF FORWARD EDGE DOOR CUOUT BY THRESHOLD EDGE. TEMPORARY REPAIR, REMOVED DAMAGE, INSTALLED TAPE PER TYP REPAIR 53-02-01. (M) 2L72 4F RTA28NM 20041014001372004101400137EU 2004 10 14 USAASA04085 120040906A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19755US 1331 MSP - FLT 33 - EN ROUTE PHL-SEA - WHILE IN CRUISE FLIGHT, AT FL350, THE RIGHT WINDSHIELD STARTED ARCING FROM THE LOWER CORNER TO THE UPPER LEFT CORNER. THE CIRCUIT BREAKERS FOR THE WINDSHIELD WERE PULLED, BUT THE ARCING CONTINUED UNTIL THE OUTER LAYER OF WINDSHIELD SHATTERED. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONALLY CHECKS OK. ALSO, REPLACED THE WINDSHIELD HEAT COMPUTER AS A PRECAUTIONARY MEASURE. (M) 2L72 4F RTA28NM 20041014001432004101400143NE 2004 10 14 2004F00406 220040827A72003044800 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT FAILED A GUUAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO1749543 UE181 FLT 9187 - MHH/FLL - DUIRNG APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSY. OPERATIONAL CHECK NORMAL. (M) 2L72 4T4 TRTA24CE E26NE 20041014001472004101400147NM 2004 10 14 BJNA040907 120040918A5753654643089 SKIN BOEING737 737282 13844ATNM TE FLAP DAMAGED A BJNAK NONE C F.O.D. ININSP/MAINT 1 WP11789TM 23046 FOUND THE LEFT INBOARD FORE FLAP TRAILING EDGE DAMAGED FROM POSSIBLE FOD. REMOVED AND REPLACED THE LEFT INBOARD FORE FLAP IAW THE AMM 27-51-41. (M) 2L72 4F RTA16WE 20041014001492004101400149NM 2004 10 14 USAA040620 120040917A5320 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND ATTACH CLIP CRACKED .5 INCH, FRAME 827, STRINGER S4R. REMOVED OLD TIE CLIP AND INSTALLED NEW ONE PER SRM 53-40-03. (M) 2L72 4F RTA16WE 20041015000082004101500008NM 2004 10 15 USAABB04082 120040901A1430H516508BAC NUT BOEING757 757225 1384959NM RT WING UNKNOWN A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19601AU 22193 CLT - FLT 877 - AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE 'TE FLAP ASYM' AND FLAPS WOULD NOT MOVE. AIRCRAFT RETURNED TO CLT. ON FINAL, AT APPROXIMATELY FIFTY FEET AGL, VIOLENT BUFFETING WAS EXPERIENCED. MAINTENANCE FOUND THE INBOARD COUPLING OF THE TORQUE TUBE BEARING SUPPORT SEPARATED AT WING STATION 388 RIGHT. THE COUPLING WAS RECONNECTED AND THE FLAP ADJUSTED. (M) 2L72 4F RTA2NM 20041015000172004101500017NM 2004 10 15 USAA040615 120040917A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND INTERCOSTAL CRACKED .25 INCH, JUST AFT OF FRAME AT STATION 500B OUTBOARD STRINGER 26R. REPLACED INTERCOSTAL PER SRM 53-00-00. (M) 2L72 4F RTA16WE 20041015000192004101500019NM 2004 10 15 USAA040618 120040917A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND INTERCOSTAL CRACKED 6 PLACES, 1 INCH TO 1.5 INCH CRACKS, CENTER LINE OF FLOOR STATION 380-400, TOP OF INTERCOSTAL. FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-02 AND BOEING DWG 69-35365. (M) 2L72 4F RTA16WE 20041015000302004101500030EA 2004 10 15 REXA04016 120040923A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA UNKNOWN A REXAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO258969A 7969 FLAP FAILED ON DEPARTURE AT ZERO FROM DTW. SYSTEM RESET PER FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS PER AD 98-20-01. (M) 2L72 4F RTA21EA 20041015000652004101500065EA 2004 10 15 SWIA200413907 120040927A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TRANSVERSE BM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07945SW 7770 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED IB AND OB; FS 280.00 RBL 9.0. (ITEM FOUND AT C-CHECK INSPECTION.) CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-42-13, 51-21-11 AND 51-25-16. 2L72 4F4 FRTA21EA E15NE 20041015000682004101500068GL 2004 10 15 2021092004 120041004A322011907004 STRUT CIRRUSSR SR20 05628AJGL CONT IO360 IO360* 17025CE NOSE LAND GEAR CRACKED E YD5RK NONE O OTHER ININSP/MAINT 1 GL15109CD2586 1009 WHILE PERFORMING AN ANNUAL INSPECTION IT WAS NOTED THE NOSE LANDING GEAR STRUT ASSY P/N 11907-004 HAD TWO SMALL CRACKS. THE AREA IN QUESTION IS LOCATED JUST AFT OF THE INTERSECTION OF THE (ROUND) STRUT ASSEMBLY AND THE LT AND RT (BOXED) SECTIONS THAT ATTACH THE STRUT ASSY TO THE ENGINE MOUNT. IN THIS AREA THERE ARE GUSSET PIECES. ONE ON THE LT, AND ONE ON THE RT. THEY ARE LOCATED ON THE IB SIDE OF THE (BOXED) SECTIONS. AT THE AFT/TOP OF WHERE THE GUSSETS ARE WELDED TO THE BOXED SECTIONS ARE WHERE THE CRACKS ARE LOCATED. DURING AN ANNUAL INSPECTION THIS AREA DESERVES A CLOSE LOOK. 1L71 3O3 ONTA00009CHE1CE 20041015000742004101500074WP 2004 10 15 DHL2004801506 120040901A5720 ANGLE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 1391: RT CTR L/E (L) ANGLE CRACKED 0.750 AT XFS 526.000. REMOVED CRACKED L ANGLE IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW L ANGLE (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED L ANGLE WITH NEW FASTENERS IAW SRM 57-2-0 PG. 1, SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041015000752004101500075WP 2004 10 15 ASMF200410005 120041007A2910 MODULATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE HYD FILTER LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW231003Y 48068 DURING LT ENGINE STARTING CAPTAIN REPORTED LT HYDRAULIC SYSTEM LEAKAGE AND PRESSURE DROP TO ZERO. DURING REVISION THE TECHNICAL PERSONNEL DETECTED THAT THE LEAK WAS FROM A LINE OF THE MAIN FILTERS MODULE. LINE WAS TIGHTENED AND HYDRAULIC FLUID RECHARGED. TESTS WERE PERFORMED IAW MM 78-31-04, ALL CORRECT. 2L72 4F4 F A6WE E9NE 20041015000942004101500094EA 2004 10 15 COMA0460549 120040927A2913848847 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYD SYSTEM MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01447CA7941 7552 FLIGHT 5821 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP. 2L72 4F4 FRTA21EA E15NE 20041015000952004101500095EA 2004 10 15 COMA0460551 120040921A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01951CA22326 7091 FUSELAGE SKIN IS CRACKED AT STATION 210, GROUND PACKING BRAKE CABLE.PERFORMED REO NR 661-53-11-563 GENERAL REPAIR TO FS. 202.75 AT B.L. 23.71 PRESSURE BULKHEAD. 2L72 4F4 FRTA21EA E15NE 20041015000972004101500097NM 2004 10 15 DHL2004780503 120040909A5754 RIB BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NR 3 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A C-CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; NR 3 SLAT IB AND OB ACT. ATTACH FRAMES WS 515 ARE CRACKED IN RADIUS. STOP DRILLED CRACKS IAW SRM 57-50-3 FIG 9 ON NR 3 SLAT IB AND OB ACT. ATTACH FRAMES AT WS 515, FABRICATED REPAIR DOUBLERS FROM .032 CRES AISI321 PO NR 900878 DIMENSIONS .7500 INCH X 3.5 INCHES X .7500 INCH IAW SRM 57-50-3 FIG 9, PRIMED REPAIR DOUBLERS IAW SRM 51-10-2 INSTALLED REPAIR DOUBLERS IAW SRM 57-50-3 FIG 9 AND 51-30-2 REMOVED NR 3 SLAT IAW MM 27-81-11, REINSTALLED NR 3 SLAT IAW MM 27-81-11. 2L73 4F4 F A3WE E2EA 20041015001002004101500100EA 2004 10 15 04267670 120040923A3241 BRAKE CNDAIRCL600 CL6002B19 1900309EA ANTI SKID SYS INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27670BR 7561 OB ANTI-SKID FAILED. OPENED DM 2674114-1 MEL 32-44-01 CAT B, OB ANTI-SKID MSG POSTED, (M) PROCEDURES C/W. 2L72 4F RTA21EA 20041018000042004101800004EA 2004 10 18 SWIA200413924 120040816A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 INTERCOSTAL AD FS 484.0 RBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059. REPAIR TO INTERCOSTALS FS 484 BL 27-00-36-00. 2L72 4F4 FRTA21EA E15NE 20041018000052004101800005NM 2004 10 18 2004UALA00894 120041004A3610 CHECK VALVE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 ENGINE FAILED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 WP29653UA 25391 NR 2 ENGINE COMPRESSOR STALL. REPLACED ENGINE DUE TO UNABLE TO ROTATE. UPON SHOP TEARDOWN OF ENGINE, ROOT CAUSE OF THE SURGE WAS DETERMINED TO BE CATASTROPHIC FAILURE OF THE PNEUMATIC 8TH STAGE CHECK VALVE. 2L72 4F4 FRTA1NM E24NE 20041018000162004101800016EU 2004 10 18 AWXA200401090 120040926A5315D53472189200 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FR 67 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F4 FRTA28NM E40NE 20041018000172004101800017EU 2004 10 18 AWXA200401091 120040926A5347D53112092206 SEAT TRACK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y1292 RT AT FR 20. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y1292 RT FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK AND 3 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-15, FIG. 203, PG. 219-220. 2L72 4F4 FRTA28NM E40NE 20041018000202004101800020EU 2004 10 18 AWXA200401094 120040930A5321D536160500100 FLOOR PANEL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 222FF IAW T/C C1D25306. 2L72 4F4 FRTA28NM E40NE 20041018000212004101800021EA 2004 10 18 SWIA200413932 120041013A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07959SW 7840 (STALL FAIL) CAUTION MESSAGE DURING CLIMB. REPAIRED A BROKEN WIRE AND INSTALLED NEW PIN AND CONNECTOR ON FO'S STICK SHAKER. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041018000222004101800022SO 2004 10 18 SWIA200413933 120041004A3397 GROUND WIRE EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE EXIT SIGN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07578SW 120346 EMERGENCY EXIT SIGN ABOVE FA JUMPSEAT DOES NOT ILLUMINATE. REPAIRED GROUND WIRE AT LIGHT ASSY. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041018000232004101800023SO 2004 10 18 SWIA200413934 120041005A1420 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07188SW 120039 UPON RETRACTING FLAPS AFTER DEPARTURE, GOT FLAP CONTROL FAULT. FOUND MOISTURE IN BOTH OB FLAP ACTUATOR CONNECTOR PLUGS, CLEANED AND REINSTALLED CONNECTOR PLUGS. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041018000242004101800024EA 2004 10 18 SWIA200413884 120041003A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RUDDER MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07925SW 7682 RUDDER TRIM RANAWAY TO THE LT WHILE TRYING TO TRIM AIRCRAFT IN THE CLIMB. RETURNED TO AIRPORT. REMOVED AND REPLACED RUDDER TRIM/AIL TRIM PANEL ASSY. OPERATIONAL CHECK GOOD. PN OFF 601R51227-13 2L72 4F4 FRTA21EA E15NE 20041018000252004101800025SO 2004 10 18 C2XA04BT104 120041006A3350M8353610024L RELAY EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716961 145103 EWR- CO3479, CREW REPORTED, (PASSENGER EMERGENCY EXIT SIGN CIRCUIT BREAKER POPS WHEN THE NO SMOKING SIGN IS TURNED ON). MAINTENANCE REMOVED AND REPLACED RELAY K8601. OPS CHECKED GOOD IAW EMB145 AMM 33-23-50. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20041018000262004101800026SO 2004 10 18 C2XA04IA128 120041008A4930211171 PRESSURE SWITCH EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL APU FUEL SYSTEM MALFUNCTIONED A C2XAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW2728518 145334 THE CREW REPORTED THAT THE APU STARTED IN FLIGHT WITH APPROXIMATELY THREE SECONDS OF APU FIRE MESSAGE, AND FUEL SMELL IN CABIN WHEN ON GROUND AND SWITCHING PACKS TO APU. THE AIRCRAFT LANDED WITH NO INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 CONTROL NUMBER 046935, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED ON 10/10/04 WHERE MAINTENANCE REMOVED AND REPLACED THE APU FUEL PRESSURE SWITCH, CLEANED THE APU FIRE LOOP CONNECTOR PLUG AND OPERATIONAL CHECKED WITH NO DEFECTS. THE APU WAS REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20041018000272004101800027NM 2004 10 18 ASMF204410010 120041012A2121 FAN BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE CABIN ODOR W ASMFK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW23801AM335453313 25624 DURING TRANSIT CHECK, CAPTAIN REPORTED STRONG ELECTRICAL CABLE BURNED ODOR. TECHNICAL PERSONNEL PERFORMED BITE TO APU CONTROL UNIT SHOWING MESSAGE CURRENT LAS RUN LOW OIL PRESS. APU WAS DEFERRED IAW MEL 49-11-1. BURNED ODOR IN PILOTS CABIN AND GALLEY. SMOKE IN AIR CONDITIONING SYSTEM PROCEDURE WAS PERFORMED IAW MM 21-00-01. RIGHT RECIRCULATION FAN WAS DISCONNECTED AND ODOR DISAPPEARS. IT WAS DISPATCHED INOPERATIVE IAW MEL 24-28-1. DURING OVERNIGHT SERVICE, APU WAS REPLACED IAW MM 49-00-01 AND RIGHT RECIRCULATION FAN WAS REPLACED IAW MM 21-25-01. OPERATIONAL TEST WAS PERFORMED IAW MM 21-00-01 AND M6-11-00, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20041018000302004101800030WP 2004 10 18 ARWA20040907 120040928A5330 SKIN DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3B 52039NE FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 DURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; DISCREPANCY: FORWARD LOWER CARGO COMPARTMENT STA 230 BETWEEN LONG. 36 AND LONG 35R, SKIN WITH CORROSION. 2L74 4F4 F 4A25 1E8 20041018000352004101800035EU 2004 10 18 MALA040581 120040922A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT INOPERATIVE A MALAO OTHER L NO TEST NRNOT REPORTED 1 GL15366PX 340B267 EMERGENCY LIGHTS 3LN, 4LN, AND 42LN INOPERATIVE. (LT AND RT EXTERIOR LIGHTS AND RT AFT COVE LIGHT) MAINTENANCE REMOVED AND REPLACED 24LN EMERGENCY POWER SUPPLY IAW SMM 33-50-10. P/N ON/OFF 60-1321-1. S/N ON 18225 S/N OFF 14587. 2L72 4T4 TRTA52EU E8NE 20041018000362004101800036EU 2004 10 18 MALA040577 120040914A49204501690A APU BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE APU BAY SHUTDOWN A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15527XJ E2352 APU-AUTO SHUTDOWN IN FLIGHT. AFTER TAKEOFF THE APU AUTO SHUTDOWN AND NR 1 ENGINE WAS ALREADY ON MEL. AIR RETURN TO GRB. MAINTENANCE DEFERRED APU DUE TO AUTO SHUTDOWN IAW MEL 49-00-1 (C) C/B PULLED PLACARDED, ENTERED INTO DRM MOX NOTIFIED. MAINTENANCE REMOVED AND REPLACED APU P/N 4501690A S/N ON SP-E977535 S/N OFF SP-E977531 IAW MAL T/C APU CHANGE LEAK AND OPS CHECK GOOD REMOVED FROM DMR MXC NOTIFIED 1376. 2H74 4F4 FRTA49EU E6NE 20041018000372004101800037EU 2004 10 18 MALA040582 120040830A3350330131 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST NRNOT REPORTED 1 GL15410XJ 340B410 FWD EXIT PAX LIGHT OUT. BATTERY POWER SUPPLY PN 3301-51 SN/1381. MAINTENANCE REPLACED BATTERY ASSEMBLY PN 3301-31. UNIT PASSES CMM CHECKS 2L72 4T4 TRTA52EU E8NE 20041018000452004101800045 2004 10 18 SB04135 420040928A22104051601935 CONTROL PANEL BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE COCKPIT FAULTY A USAAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 EA19353US3041430414 23556 DURING A HEADING CHANGE, THE AUTOPILOT ROLLED THE AIRCRAFT INTO A 40 DEGREE BANK BEFORE THE PILOT COULD DISCONNECT IT. MAINTENANCE REPLACED THE MODE CONTROL PANEL. 2L72 4F4 FRTA16WE E2GL 20041018000532004101800053WP 2004 10 18 ABXA040335 120040920A53305911412191 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 NUMEROUS AREAS OF CORROSION ON SKIN BELOW THE FORWARD LOWER CARGO DOOR. REPAIRED SKIN BELOW FORWARD LOWER CARGO DOOR IAW REA D953-50781MR. 2L72 4F4 F A6WE E2EA 20041018000542004101800054WP 2004 10 18 ABXA040336 120040921A53403924028801N FITTING DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 END FITTING AT LONGERON 29 RT ON AFT SIDE OF STA. 604 WAS CRACKED. REMOVED AND REPLACED END FITTING AT LONGERON 29 RT, STA. 604 IAW SRM 51-30-5. 2L72 4F4 F A6WE E2EA 20041014001082004101400108NM 2004 10 14 DL73S040939 120040930A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334DL 23105 THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST ABOVE STRINGER 16L AT FS 525. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND PER ER/A 093927-14. 2L72 4F RTA16WE 20041014001302004101400130NM 2004 10 14 USAA040522 120040901A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU49585 23706 PIT - FOUND SKIN CRACKED 1.125 INCH LONG, STATION 727D PLUS 18 INCHES STRINGER 22L FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20041014001322004101400132NM 2004 10 14 UIEA200400163 120040921A541065B940511 PYLON BOEING747 747230B 1384889NM NR 2 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, NR 2 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-FS 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION WAS ACCOMPLISHED AT EACH REPAIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DEFECT FREE CONDITION. (M) 2L74 4F A20WE 20041014001482004101400148NM 2004 10 14 USAA040656 120040918A5343 FITTING BOEING737 7373B7 1384580NM MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND FITTING CRACKED .5 INCH, RT MLG SUPPORT FITTING NR 2 HOLE 5:30 POSITION. REPLACED RT MLG SUPPORT FITTING AND INSTALLED UPPER WING CHORD DOUBLER PER EO 5702V054, EA 78985 AND 78986. (M) 2L72 4F RTA16WE 20041014001512004101400151NM 2004 10 14 USAA040585 120040830A5320 CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SLIP CRACKED .5 INCH, STATION 685 LLT AND S12 SKIN CLIP CRACKED IN RADIUS. REPLACED CLIP PER SRM 51-40-03. (M) 2L72 4F RTA16WE 20041014001532004101400153NM 2004 10 14 USAA040586 120040911A5410 PYLON BOEING737 7374B7 1384702NM LT ENGINE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 FOUND NACELLE WITH .5 INCH CRACK, LT ENGINE PYLON, NR 1527L ACCESS, OUTBOARD EDGE LIP. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M) 2L72 4F RTA16WE 20041014001552004101400155NM 2004 10 14 USAA040629 120040909A534765C80736259 CARGO TRACK BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND TIEDOWN TRACK CORRODED .5 INCH BY 3 INCH AREA, STATION 727F AT LBBL 17.10. REPLACED SECTION OF TIE DOWN TRACK PER SRM 53-00-53 PAGE 205. (M) 2L72 4F RTA16WE 20041015000032004101500003NM 2004 10 15 AMTA200401165 120040921A3350 CONNECTOR BOEING757 75733N 1384931NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11552TZ 32586 BULLNOSE EMERGENCY LIGHT AT SEAT 36 DEF INOPERATIVE. FOUND CONNECTOR D42656 DISCONNECTED. RECONNECTED IAW WDM 33-51-15. OPS CHECK GOOD IAW AMM 33-51-00-5. (M) 2L72 4F RTA2NM 20041015000262004101500026NM 2004 10 15 USAA040597 120040829A52306547952518 TEE FITTING BOEING737 7374B7 1384702NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND LOWER T-CHORD CRACKED 1.25 INCH, AFT CARGO DOOR. REPLACED T-CHORD ANGLE AND LOWER INNER SKIN PER SRM 52-30-02 AND 52-30-01. (M) 2L72 4F RTA16WE 20041015000272004101500027NM 2004 10 15 AMTA200401156 120040917A3350 FUSE BOEING757 75723N 1384973NM EMERGENCY LIGHT FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 FOUND R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED R-2 DOOR POWER PACK FUSE PER 33-51-07-2. OPS CHECK GOOD PER 33-51-06-2. (M) 2L72 4F RTA2NM 20041015000292004101500029EA 2004 10 15 REXA04014 120040920A2750 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS TRIPPED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258409 7409 ON APPROACH FLAPS SELECTED 30 FAILED AT 20. QRH FOLLOWED EMERGENCY DECLARED LANDING UNEVENTFUL. RESET CIRCUIT BREAKER, PLACED FLAP ON 72 HOUR WATCH PER AD 98-20-01. (M) 2L72 4F RTA21EA 20041015000342004101500034NM 2004 10 15 USAA040594 120040826A5347 MOUNT BOEING737 7374B7 1384702NM LAVATORY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND LAVATORY MOUNT CORRODED 2 SQUARE INCH AREA, LEFT OUTBOARD LAV MOUNT STATION 947. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED LAV MOUNT PER SRM 51-10-00. (M) 2L72 4F RTA16WE 20041015000482004101500048NM 2004 10 15 USAA040571 120040903A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU63100 22198 CLT - FOUND SKIN CRACKED 5.125 INCH, BS 1720 PLUS 15 INCHES BETWEEN STRINGER 12 AND 13R. CUT OUT DAMAGE, FABRICATED FLUSH SKIN DOUBLER PER SRM 53-00-01 FIG 206. (M0 2L72 4F RTA2NM 20041015000542004101500054EA 2004 10 15 SWIA200413899 120041005A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07461SW 7811 (STAB CH1 INOP) MESSAGE IN FLIGHT INTERMITTENTLY. REMOVED AND REPLACED HSTCU IAW CRJ MM 27-41-01. REMOVED AND REPLACED FO SIDE STAB DISCONNECT SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. SWITCH PN 996-0013 SN OFF 0304. 2L72 4F4 FRTA21EA E15NE 20041015000562004101500056NE 2004 10 15 513NA0010 220041004A7260M06626AB GEARBOX BOEING757 7572T7 1384914NM RROYCERB211 RB211535E43754555NE LT ENGINE VIBRATION A PIDAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO05513NA 23895 ON TAXI OUT, HAD EICAS MESSAGE: LT OIL FILTER. FOUND METAL ON CHIP DETECTOR FOR HIGH SPEED GEAR BOX. REPLACED MAIN OIL FILTER AND SCAVENGE FILTER AND RAN ENGINE. LT ENGINE HAD VIBRATION DURING POWER RUN. SENT MECHANICS. 10/10/2004: REPLACED HIGH SPEED GEAR BOX MODULE IAW RR MM 72-00-61. PERFORMED OPS AND LEAK CHECK IAW MM 72-00-00. NO VIBRATION NOTED. CHECKED CHIP DETECTORS, NO METAL NOTED. AFTER TEAR-DOWN OF GEARBOX (06 MODULE): STARTER IDLE GEAR RACE HOUSING FAILED. STARTER IDLER GEAR RACE HOUSING TO 06 CASE MOUNT HOLES ELONGATED. ELONGATED MOUNT HOLES CAUSED IDLER GEAR TO WOBBLE, RESULTING IN FAILURE. HP FUEL PUMP DRIVE GEAR THAT ROTATES ALONG WITH THE STARTER IDLER GEAR LOST 2 TEETH. 2L72 4F4 FRTA2NM E12EU 20041015000612004101500061EA 2004 10 15 SWIA200413906 120040927A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLRBM TO TRANSBMCRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07945SW 7770 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED IB AND OB; FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-21-11, 51-25-16. 2L72 4F4 FRTA21EA E15NE 20041015000622004101500062 2004 10 15 XIW2004F00000 420040630A34429151301 CIRCUIT CARD BOEING747 747400 NM RADAR SYSTEM INOPERATIVE B XIW2O OTHER O OTHER NRNOT REPORTED 1 CE07GVFAR 225 OPERATOR NOTIFIED MFG 7/6/04 OF PROBLEM WITH RADAR SN 231, REPORTED AS HAVING A BURNING ODOR. MFG NOTIFIED FAA. RECEIVED A TEARDOWN PERFORMED. PROBABLE ROOT CAUSE WAS FAILURE OF TANTALUM CAP C79 ON MPEG CARD. CAP FAILED SHORT, CAUSING OVER CURRENT CONDITION ON +12VDC BUS, WHICH CAUSED FERRITE BEAD L5 (MPEG CARD) AND FLYBACK FET Q24 AND RECTIFIER Z5 (POWER SUPPLY 915121) TO FAIL. STOPPED DRAWING AC INPUT CURRENT IN A (FAIL-SAFE) MODE. THIS IS AN ISOLATED SERVICE INCIDENT, WITH NO SIMILAR OCCURANCES IN MORE THAN 7 YEARS OF PRODUCT OPERATION OF SEVERAL HUNDRED UNITS IN USE. NO PLANS FOR FURTHER ACTION. 2L74 4F RTA20WE 20041015000732004101500073WP 2004 10 15 DHL2004801511 120040902A5531 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR 2094: VERTICAL STAB L/E FORMER CRACKED 0.500 AT ZRS 173.000 (LT). REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 21.PERFOMED STOP DRILL AND FABRICATED ANGLE. DOUBLER IAW SRM 55-2-0 PAGE 7,8 CLEANED TREATED AND PRIMED IAW SRM 51-1-8B.INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE9. 2L74 4F4 FRT4A25 E2GL 20041015000912004101500091WP 2004 10 15 0401809607 120041001A57535910134190 SKIN DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW15759 47234 DURING M-CHECK FOUND CRACKED IN RT WING TRAILING EDGE FLAP UPPER STRINGER AT WING STATION 235. REPAIRED IAW EA 96-200350. 2L72 4F4 F A6WE E2EA 20041015000992004101500099 2004 10 15 ANCF200400032 420040930A3431 INDICATOR BOEING767 767284 1385184NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED W ANCFL ABORTED APPROACH G MULTIPLE FAILURE APAPPROACH 1 SO23988AN 24742 (ERRONEOUS NAV. INDICATIONS, ILS UNREADABLE, HDG UNREADABLE, THERE IS A DIFFERENT INFORMATION BETWEEN L AND R. ALL A/P DOES NOT ENGAGE AND DOES NOT MAINTAIN ALTITUDE) PERFORMED ILS TEST IAW AMM 34-31-00 PG 501-508, NOTHING ABNORMAL FOUND, ALL TASK WERE PERFORMED AND NO FAULT FOUND. PERFORMED PITOT STATIC TEST IAW AMM 34-11-00 PG 501-506. ALL TASK WERE PERFORMED AND NO FAULT FOUND. PERFORMED AUTOLAND TEST 40 IAW FIM 22-00-03 FIG 118 TEST SATISFACTORY. PERFORMED MCDP CHECK IAW AMM 22-00-02 NO FAULT FOUND, SYSTEM OK FOR SERVICE. 2L72 4F4 FRTA1NM E24NE 20041018000072004101800007EA 2004 10 18 SWIA200413926 120040816A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AP BULKHEAD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 FS 625 OBLIQUE ANGLE IS CRACKED APPROX .65 INCH LONG ON RT SIDE OF AFT PRESSURE BULKHEAD AT STR 14R. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35-012-52 IAW CRJ 200 SRM 51-42-06. 2L72 4F4 FRTA21EA E15NE 20041018000082004101800008EA 2004 10 18 SWIA200413927 120040816A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 FS 280.00 ANGLES AT RBL9/LBL9 IB AND OB ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED NEW ANGLES AT RBL9/LBL9 AT FS 280.00 IAW CRJ SRM 51-42-13, 51-42-21, 51-22-00. 2L72 4F4 FRTA21EA E15NE 20041018000092004101800009EA 2004 10 18 SWIA200413928 120040816A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 RT AFT FLOORBOARD ATTACHMENT ANGLE CRACKED AT RIGHT OUTBOARD AT EDGE OF FRAME 621.0. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ALL REPAIR PARTS IAW REO NR 601R-53-61-117. 2L72 4F4 FRTA21EA E15NE 20041018000102004101800010 2004 10 18 SWIA200413929 420041012A3418 STICK SHAKER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CAPTAINS INTERMITTENT A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07903SW 7425 CAPTAINS STICK SHAKER INTERMITTENT. REPLACED CAPTAINS STICK SHAKER CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041018000122004101800012WP 2004 10 18 DHL2004801553 120040927A5753 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE TE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 1130: LT OB FLAP L/E UPPER PART PLATING WORN, XF 345.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG R51-R08, FAA FORM 8110-3 DATED 09-24-2004. REMOVED FASTENERS IAW SRM 51-1-21. TRIMMED OUT DAMAGED SKIN SEGMENT IAW DWG W51-R08. FABRICATED NEW SKIN SEGMENT (AL2024-T3 0.063) INTERNAL SPLICE DOUBLER (2024-T3AL 0.071) IAW DWG W51-R08. CLEANED, TREATED AND PRIMED REPAIRED AREA NEW SKIN SEGMENT INTERIOR, INTERNAL SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO ALL FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT AND INTERNAL SPLICE DOUBLER IAW DWG W51-R08. 2L74 4F4 FRT4A25 E2GL 20041018000382004101800038 2004 10 18 MALA040576 420040914A3442 TRANSCEIVER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE WX RADAR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15370PX 340B300 RADAR STABILIZATION APPEARS TO BE INOPERATIVE RADAR RETURNS ARE DISTORTED WHEN AIRCRAFT PITCH AND OR BANK ANGLE IS ALTERED. WX RADAR FAILED INFLIGHT. AIR RETURN TO MSP. MAINTENANCE COULD NOT DUPLICATE RADAR SYS AND STABILIZATION OP CHECKS GOOD IAW SF340 M/M CHAP 34. 2L72 4T4 TRTA52EU E8NE 20041020000082004102000008NM 2004 10 20 ASAA0410365 120040809A5311BAC15171470 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CHAFED FRAME. REPAIRED FRAME. (M) 2L72 4F4 FRTA16WE E2EA 20041020000122004102000012EU 2004 10 20 A6WA200460039 120040921A5330 SKIN BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 FOUND DENTS ON THE EDGE OF THE REAR CARGO DOOR CUT OUT SKIN FORWARD AND AFT, REPAIR IN PROGRESS. (M) 2H74 4F4 F A49EU E6NE 20041020000132004102000013NM 2004 10 20 ASAA0410382 120040821A5310BAC14902642 SHEAR TIE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON SHEAR TIE. REMOVED, FABRICATED AND INSTALLED SHEAR TIE. (M) 2L72 4F4 FRTA16WE E2EA 20041020000142004102000014NM 2004 10 20 ASAA0410373 120040817A5347 SEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON FLOOR SEAT TRACK FLANGE STATION 500A THROUGH S TO 500B LBL 45 WL 208. REPLACES SEAT TRACK BS 480-520 LBL 45 WL 200. (M) 2L72 4F4 FRTA16WE E2EA 20041020000152004102000015NM 2004 10 20 ASAA0410359 120040801A33508821004 BATTERY PACK BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 FOUND AFTER RECON, FLOOR EMERGENCY LIGHTS ON SEAT PALLET 8-5 WILL NOT SHUT OFF. REPLACED SEAT PALLET BATTERY PACK, OPS OK. (M) 2L72 4F4 F A16WE E2EA 20041020000162004102000016NM 2004 10 20 ASAA0410384 120040828A531065671406 BEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. (M) 2L72 4F4 FRTA16WE E2EA 20041020000172004102000017NM 2004 10 20 ASAA0410385 120040830A534069353507 STRINGER CLIP BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON STRINGER CLIP. BLENDED CORROSION, FOUND OUT OF LIMITS, FABRICATED AND INSTALLED. (M) 2L72 4F4 FRTA16WE E2EA 20041020000182004102000018NM 2004 10 20 ASAA0410386 120040830A53116937411 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON FRAME. REMOVED DAMGAED PARTS, FABRICATED AND INSTALLED REPAIR PARTS. (M) 2L72 4F RTA16WE 20041020000212004102000021NM 2004 10 20 ASAA0440151 120040816A5320BAC1496377 ANGLE BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE LEFT ZEE ANGLE FROM STATION 750 TO 790 IS CORRODED. REMOVED AND REPLACED AFT CARGO COMPARTMENT ZEE ANGLE FROM STATION 750 TO 790. REF SRM 53-60-53 PGS 208-209 FIG 204. (M) 2L72 4F RTA16WE 20041020000222004102000022NM 2004 10 20 ASAA0440150 120040816A533065C31240 DOUBLER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01765AS 25102 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE REINFORCEMENT DOUBLER FORWARD SIDE CARGO DOOR FORWARD FRAME CORRODED BETWEEN STRINGER 26R AND 24R. REMOVED AND REPLACED DOUBLER PER SRM 51-70-11 PAGES 1-6. (M) 2L72 4F RTA16WE 20041020000282004102000028NM 2004 10 20 UIEA200400156 120040910A7500 LINE BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE PR VALVE BROKEN A UIEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15517MC 23300 455808 AFTER TAKEOFF NR 4 ENGINE FIRE WARNING SOUND. PEAK EGT 976 FOR 11 SECONDS. GOT A RED BALL, SHUTDOWN THE ENGINE IAW FHB FIRE INDICATION WENT OUT WHEN NR 4 ENGINE FIRE SWITCH WAS PULLED. PERFORMED NR 4 ENGINE VISUAL INSPECTION NO EVIDENCE OF FIRE. PERFORMED BOROSCOPE INSPECTION OF BLADES OF HPC STAGES 1-7-12-13 AND 14. HPT STAGE 1 AND 2, LPT STAGE 1 AND 2, FOUND ALL SATISFACTORY IAW AMM 72-00-00. REMOVED AND REPLACED ENGINE NR 4 IAW AMM 71-00-02. PERFORMED ENGINE TEST RUN IAW AMM 71-00-00. FINDINGS WERE VARIABLE BLEED VALVE FEED BACK CABLE TO MEC FAILED CAUSING PRESSURE RELIEF VALVE TO DUMP BLEED LOAD CAUSING FIRE WARNING. ALSO, FOUND SENSE LINE TO PRV BROKEN ON INITIAL INSPECTION. (M) 2L74 4F4 F A20WE E23EA 20041020000292004102000029NM 2004 10 20 UIEA200400162 120040921A541065B941004 PYLON BOEING747 747230B 1384889NM NR 1 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, NR 1 PYLON CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION WAS ACCOMPLISHED AT EACH REAPIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DEFECT FREE CONDITION. (M) 2L74 4F A20WE 20041020000332004102000033EU 2004 10 20 A6WA200460044 120040921A5410 FAIRING BAC 146 146200A 1500266EU NR 4 PYLON DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 FOUND NR 4 ENGINE PYLON NOSE FAIRING NR 484B FORWARD EDGE HAS FRETTING DAMAGE, REPAIR IN PROGRESS. (M) 2H74 4F A49EU 20041020000342004102000034NM 2004 10 20 USAA040596 120040826A5320 ANGLE BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND ZEE ANGLE CORRODED TWO AREAS 1 INCH, WEB SUPPORT AT STATION 992 RBL 24. FABRICATED AND REPLACED ZEE ANGLE PER BOEING DWG PL 69-77477. (M) 2L72 4F RTA16WE 20041020000352004102000035NM 2004 10 20 USAA040573 120040901A5320 INTERCOSTAL BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND INTERCOSTAL CORRODED 8 SQUARE INCH, BETWEEN STATION 1660-1680, RBL 55. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-10-02. CORROSION LEVEL 1, TASK NR C53-251-03 AND C53-252-03. (M) 2L72 4F RTA2NM 20041020000382004102000038NM 2004 10 20 USAA040576 120040821A5230 STRUCTURE BOEING757 757225 1384959NM CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND AFT CARGO DOOR CORRODED 1 INCH BY 1 INCH AREA, AFT CARGO 21 INCHES FORWARD OF AFT DOOR EDGE WEB. REPLACED DAMAGED WEB PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041020000412004102000041NM 2004 10 20 AMTA200401094 120040830A2612 FIRE LOOP BOEING757 75723N 1384973NM NR 2 ENGINE OUT OF POSITION A AMTAO OTHER N FALSE WARNING DEDESCENT 1 GL11514AT 27971 FOUND ENGINE FIRE LP2 DISPLAYED INTERMITTENTLY DURING DESCENT. REPOSITIONED NR 2 ENGINE FIRE DETECTION LOOP REF B757 AMM 26-11-01. (M) 2L72 4F RTA2NM 20041020000462004102000046NM 2004 10 20 USAA040587 120040831A573065C26603101 SKIN BOEING737 7374B7 1384702NM WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SKIN CRACKED 1 INCH, LOWER LEADING EDGE SKIN FORWARD OF OUTBOARD ALT SLAT TRACK. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PE SRM 57-43-01, FIG 206. (M) 2L72 4F RTA16WE 20041020000472004102000047NM 2004 10 20 USAA040588 120040825A5340 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND TIE CLIP CRACKED .125 INCH, STATION 847 S10R ATTACH TIE CLIP. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-20-02. (M) 2L72 4F RTA16WE 20041020000512004102000051EU 2004 10 20 A6WA200460045 120040921A5410 FAIRING BAC 146 146200A 1500266EU NR 1 PYLON CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 NR 1 ENGINE PYLON NOSE FAIRING NR 451 AT FORWARD EDGE HAS FRETTING DAMAGE. REPAIR IN PROGRESS. (M) 2H74 4F A49EU 20041020000522004102000052NM 2004 10 20 UIEA200400174 120040923A3350BACC45FT16245 CONNECTOR BOEING747 747243B 1384830NM EMERGENCY LIGHT INOPERATIVE A UIEAO OTHER J WARNING INDICATION CRCRUISE 1 EA15516MC 22507 AIRCRAFT EMERGENCY LIGHT FLICKER MOST OF THE FLIGHT. FOUND SEVERAL PUSHED BACK PINS AT CONNECTOR EMERGENCY LIGHT PANEL. ACCOMPLISHED GROUND CHECK OK PER MM 33-51-10. (M) 2L74 4F A20WE 20041020000532004102000053NM 2004 10 20 USAA040659 120040910A5540 STRUCTURE BOEING737 7373B7 1384580NM RUDDER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER CRACKED 1 INCH WITH DELAMINATION, LOWER LEFT LEADING EDGE. REMOVED DAMAGE, INSTALLED REPAIR PLYS PER EA 79025, SRM 51-70-17. (M) 2L72 4F RTA16WE 20041020000542004102000054EU 2004 10 20 USAASA04084 120040903A335032145410 PSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW 0844 PHL - THE EMERGENCY POWER SUPPLY UNIT IN THE AFT LEFT POSITION FAILED THE TEST. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPS CHECK NORMAL. (M) 2L72 4F RTA28NM 20041020000562004102000056NM 2004 10 20 AMTA200401081 120040826A2612 FIRE LOOP BOEING757 75723N 1384973NM RT ENGINE INTERMITTENT A AMTAO OTHER N FALSE WARNING CRCRUISE 1 GL11514AT 27971 RIGHT ENGINE FIRE LOOP 2 DISPLAYS INTERMITTENTLY ON STATUS PAGE. OPS CHECKED PER AMM 26-11-00-5, COULD NOT DUPLICATE SWAPPED LOOP 1 CARD WITH LOOP 2 CARD PART NR 332T301181 FOR BOTH NO S/N FOR BOTH, PER MX CONTROL. (M) 2L72 4F RTA2NM 20041020000572004102000057NM 2004 10 20 AMTA200401080 120040827A3350 LIGHT BOEING757 75723N 1384973NM CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND EMERGENCY EGRESS LIGHTING, ROWS 5 FED THROUGH 9 FED, ARE OUT. RECONNECTED LIGHT ASSEMBLIES IAW AMM 33-51-11-3, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20041020000582004102000058NM 2004 10 20 AMTA200401089 120040827A3350 LIGHT BOEING757 75723N 1384973NM CABIN DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 FOUND EMERGENCY EGRESS LIGHTING, FRONT RIGHT AFT LAV, AREA OUT. RECONNECTED LIGHT ASSEMBLIED IAW AMM 33-51-11-3. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20041020000612004102000061NE 2004 10 20 HALA0400914 220040912A7200 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 SHUTDOWN A HALAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 WP13477HA 55122 13355 FLT 514 - OGG - NR 2 ENGINE INFLIGHT SHUTDOWN, RETURNED TO LIH, WHERE AN UNEVENTFUL LANDING WAS MADE. REPAIR IN WORK. (M) 2L72 4F4 FTRA6WE E00061EN 20041020000622004102000062NM 2004 10 20 ASAA0410367 120040809A534069353521 STRINGER CLIP BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON STRINGER CLIP. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. (M) 2L72 4F RTA16WE 20041020000642004102000064NM 2004 10 20 ASAA0410364 120040807A5313BAC1498156 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CHAFED STRINGER. REPAIRED STRINGER. (M) 2L72 4F RTA16WE 20041020000662004102000066NM 2004 10 20 ASAA0410383 120040824A5313 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 56432 PAE - FOUND CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. (M) 2L72 4F RTA16WE 20041020000682004102000068NM 2004 10 20 USAA040574 120040821A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND FRAME AND CLIP CRACKED .375 INCH AND .5 INCH, STATION 680 STRINGER 21L FRAME AND CLIP. REPLACED DAMAGED FRAME AND STRINGER CLIP PER EA 95653, SRM 53-30-07. (M) 2L72 4F RTA2NM 20041020000702004102000070NM 2004 10 20 USAA040665 120040830A5510 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH, RIGHT HORIZ STAB, R-8 CLEVIS BUSHING. MADE NEW BUSHINGS WITH AMS 4640 PER SRM 55-10-10. (M) 2L72 4F RTA16WE 20041020000722004102000072NM 2004 10 20 USAA040668 120040830A5510 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, LEFT HORIZ STABILIZER STAB NR 9 LUG. MADE NEW BUSHING PER SRM 55-10-10. (M) 2L72 4F RTA16WE 20041020000732004102000073NM 2004 10 20 USAA040669 120040830A5510 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BUSHING CORRODED .25 INCH BY .125 INCH AREA, LEFT HORIZONTAL NR 12 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M) 2L72 4F RTA16WE 20041020000742004102000074NM 2004 10 20 USAA040660 120040910A5542 SKIN BOEING737 7373B7 1384580NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER WITH COMPOSITE DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, STATION 180 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M) 2L72 4F RTA16WE 20041020000752004102000075NM 2004 10 20 USAA040646 120040922A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US51693 23317 CLT - FOUND SKIN CRACKED 1 INCH, STATION 945.5, .5 INCH ABOVE STRINGER 24R. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20041020000762004102000076NM 2004 10 20 USAA040648 120040923A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US51693 23317 CLT - FOUND SKIN CRACKED 1.5 INCH, STATION 870, .5 INCH BELOW STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20041020000782004102000078NM 2004 10 20 USAA040650 120040916A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US53224 22959 PIT - FOUND STRINGER CRACKED 2 INCHES, STRINGER 20L, STATION 727D. DOUBLER AND TRIPLER REPAIR DOUBLERS PER SRM 53-00-01 FIG 228. (M) 2L72 4F RTA16WE 20041020000812004102000081EU 2004 10 20 USAASA04086 120040914A3350321431 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19724UW 1122 LGA - FOUND LT EMERGENCY POWER SUPPLY UNIT BATTERY FAULT. MAINTENANCE REPLACED THE LT EMERGENCY POWER SUPPLY UNIT BATTERIES. OPS CHECKED OK. (M) 2L72 4F RTA28NM 20041020000822004102000082NM 2004 10 20 USAA040610 120040920A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US51552 23231 CLT - FOUND FUSELAGE SKIN CRACKED 1.2 INCH, STRINGER 18R AT STATION 749. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20041020000852004102000085EU 2004 10 20 USAASA04087 120040916A304066642870 COMPUTER AIRBUSA321 A321211 3930370EU WINDSHIELD HEAT MALFUNCTIONED A USAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA19162UW 1412 PHL - FLT 167 - EN ROUTE PHL-PHX - AFTER TAKEOFF, RECEIVED 'R WSHLD HEAT, R WNDW HEAT' ECAM WARNINGS. CREW ALSO NOTICED AN ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT. FLT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 WINDSHIELD HEAT COMPUTER. OPERATIONALLY CHECKED OK. (M) 2L72 4F RTA28NM 20041020000862004102000086NM 2004 10 20 USAA040661 120040910A5542 SKIN BOEING737 7373B7 1384580NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER WITH COMPOSITE DAMAGE 4 INCH BY 5 INCH SINGLE LAYER, STATION 170 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M) 2L72 4F RTA16WE 20041020000872004102000087NM 2004 10 20 USAA040600 120040914A5512 SKIN BOEING737 7374B7 1384702NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND SKIN CRACKED, 1.125 INCH, STATION 125.5 RT HORIZ STAB LOWER SURFACE AT AFT SPAR. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS PER TYPICAL REPAIR 55-10-07B. (M) 2L72 4F RTA16WE 20041020000882004102000088NM 2004 10 20 USAA040581 120040819A5753 SKIN BOEING757 757225 1384959NM TE FLAPS DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND TRAILING EDGE FLAPS DELAMINATED 6 INCHES, INBOARD MAIN FLAP AT OUTBOARD TRAILING EDGE. REPLACED TRAILING EDGE WEDGE PER BOEING DWG 113N2600. (M) 2L72 4F RTA2NM 20041020000912004102000091NM 2004 10 20 BJNA040904 120040919A2560P4010021 BATTERY PACK BOEING737 737282 13844ATNM FLASHLIGHT INOPERATIVE A BJNAK NONE O OTHER ININSP/MAINT 1 WP11344TM 23044 FOUND CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M) 2L72 4F RTA16WE 20041020000932004102000093EA 2004 10 20 ASOA04659 120040830A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11824AS 7203 FLT 4435 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041020000942004102000094NM 2004 10 20 USAA040662 120040910A5542 SKIN BOEING737 7373B7 1384580NM RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER WITH CHAFE MARKS .25 INCH BY .20 INCH, STATION 174 AT LEFT LEADING EDGE. REMOVED DAMAGE AND APPLIED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M) 2L72 4F RTA16WE 20041020000962004102000096NM 2004 10 20 USAA040613 120040917A53206545783 SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND ANTENNTA SUPPORT CRACKED .5 INCH BY .25 INCH CRACK TWO PLACES, BETWEEN STATION 500A AND 500B BL0, VHF CUTOUT STRUCTURE. MFG CHANNEL, ALODINED, PRIMED PER DWG 65-45783 SRM 53-10-00. (M) 2L72 4F RTA16WE 20041020000972004102000097NM 2004 10 20 USAA040635 120040919A57126545445 RIB BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RIB CRACKED .5 INCH, RIGHT WING AT RIB STATION 135.5, LOWER CHORD. DOUBLER INSTALLED PER EA 79058. (M) 2L72 4F RTA16WE 20041020000982004102000098NM 2004 10 20 USAA040636 120040827A5320113974315 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND FLOOR CHANNEL CRACKED .125 INCH, STATION 867 RBBI 3.00 FLOOR CHANNEL AFT CARGO NUTPLATE HOLE. CRACK REMOVED AND FILLER AND DOUBLER INSTALLED PER SRM 51-70-11. (M) 2L72 4F RTA16WE 20041020000992004102000099NM 2004 10 20 USAA040638 120040910A5542 SKIN BOEING737 7373B7 1384580NM RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER COMPOSITE CHAFED 1 INCH BY .125 INCH, RUDDER LOEWR LEFT EDGE 9.5 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, REINSTALLED HARDWARE AND REFINISHED PER SRM 51-70-17 AND EA 79025. (M) 2L72 4F RTA16WE 20041020001002004102000100NM 2004 10 20 USAA040639 120040831A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER CRACKED WITH DELAMINATION AND PEELING, RUDDER LOWER LEFT LEADING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2L72 4F RTA16WE 20041020001012004102000101NM 2004 10 20 USAA040653 120040922A5311 BELTFRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BELTFRAME CRACKED .125 INCH, IN FRAME AT FS 767 LOWER OVERHEAD BIN ATTACH POINT, RIGHT SIDE. INSTALLED REPAIR ANGLES 1 AND 2 PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20041020001022004102000102NM 2004 10 20 USAA040654 120040921A5320 ATTACH ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND ATTACH ANGLE CRACKED 1 INCH LONG, BS 538, STRINGER 22, PACK RAM AIR INLET AREA. FABRICATED AND INSTALLED REPAIR ANGLES PER TR 53-50-03. (M) 2L72 4F RTA16WE 20041020001052004102000105NM 2004 10 20 BJNA040906 120040919A33506104781 BATTERY PACK BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M) 2L72 4F RTA16WE 20041020001072004102000107NM 2004 10 20 USAA040614 120040917A57301135627 SKIN BOEING737 7374B7 1384702NM PYLON CUTOUT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND PYLON CUT OUT CRACKED APPROX 1 INCH, NR 2 ENGINE PYLON ACCESS PANEL NR 5827R AFT INBOARD CORNER. INSTALLED DOUBLER PER TYP REPAIR 54-30-07. (M) 2L72 4F RTA16WE 20041020001102004102000110NM 2004 10 20 USAA040632 120040822A5320 DUCT BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52401 23700 PIT - AIRCO PAC INLET DUCT CRACKED 1 INCH, BS 538 S22 PACK RAM AIR INLET LEFT SIDE. INSTALLED DOUBLER PER TYPICAL REPAIR 53-50-03. (M) 2L72 4F RTA16WE 20041020001112004102000111NM 2004 10 20 USAA040634 120040828A5210 STRUCTURE BOEING737 7373B7 1384580NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND FORWARD ENTRY DOOR CRACKED 1 INCH, LOWER FORWARD FRAME CORNER. REMOVED DAMAGE, REPAIRED WITH ANGLES PER SRM 51-70-13. (M) 2L72 4F RTA16WE 20041020001132004102000113NM 2004 10 20 USAA040640 120040825A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER COMPOSITE SKIN CHAFED .25 INCH BY .125 INCH SINGLE LAYER CHAFE MARKS, RUDDER LEFT LEADING EDGE AT STATION 174. REMOVED DAMAGE, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2L72 4F RTA16WE 20041020001142004102000114EU 2004 10 20 A6WA200460035 120040903A5330 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31156TR E2156 FOUND CRACK JUST AFT OF FRAME 39 LEFT EMANATING FROM A RIVET. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015001. (M) 2H74 4F RTA49EU 20041020001162004102000116NM 2004 10 20 USAA040637 120040831A5542 SKIN BOEING737 7373B7 1384580NM RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER CHAFED 1 INCH BY .125 INCH, LOWER LT EDGE 9.5 INCH FROM TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17. (M) 2L72 4F RTA16WE 20041020001172004102000117NM 2004 10 20 USAA040642 120040826A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND COMPOSITE RUDDER SKIN WITH WEAR AND KNIFE EDGING, RUDDER RIGHT LOWER EDGE. REMOVE DAMAGE, INSTALLED REPAIR PLYS, SEAL AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2L72 4F RTA16WE 20041020001182004102000118NM 2004 10 20 USAA040645 120040918A5314 KEELBEAM BOEING737 7373B7 1384580NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND KEEL BEAM .1875 INCH DIAMETER METAL WEAR AROUND FASTENER HOLES, L/N KEEL BEAM LOWER FLANGE BETWEEN BS 704-727. DOUBLER STRAP INSTALLED PER EA 79006. (M) 2L72 4F RTA16WE 20041020001192004102000119NM 2004 10 20 USAA040611 120040917A5320 INTERCOSTAL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND INTERCOSTAL CRACKED .5 INCH IN LENGTH, INTERCOSTAL MOUNTED TO FRAMES AT 500A AND B, JUST AFT OF 500A. REPLACED INTERCOSTAL PER SRM 53-10-02. (M) 2L72 4F RTA16WE 20041020001202004102000120NM 2004 10 20 USAA040612 120040917A5320 SUPPORT ANGLE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND SUPPORT ANGLE CRACKED 4 INCHES, AFT SIDE OF FRAME AT STATION 500 FORWARD OF VHF ANTENNA CUTOUT. REPLACED ANGLE WITH SAME PART PER SRM 53-10-00 DWG 65-45783. (M) 2L72 4F RTA16WE 20041020001232004102000123NM 2004 10 20 ASAA0410369 120040813A5313BAC1498156 STRINGER BOEING737 737200 1384453NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CHAFED STRINGER. REMOVED AND REPLACED CHAFED STRINGER. (M) 2L72 4F A16WE 20041020001252004102000125NM 2004 10 20 ASAA0410374 120040817A5347BAC15201432 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION C53-107-01-03 ON SEAT TRACK BS 827-867 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK BS 827-867 LBL 25, WL 208. (M) 2L72 4F RTA16WE 20041020001272004102000127NM 2004 10 20 USAA040609 120040826A5313 STRINGER BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND STRINGER CRACKED .5 INCH, STRINGER 5A, BS 1138. INSTALLED NEW PART, ANGLES, FILLER SPER TYPICAL REPAIR 53-80-04. (M) 2L72 4F RTA16WE 20041020001292004102000129NM 2004 10 20 371PA0049 120040926A5350 DRAG ANGLE BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE RT RAM AIR DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 DRAG ANGLE CRACKED ABOVE RT RAM AIR DOOR. REPAIRED IAW EA 53-250. 2L72 4F4 FRTA16NE E2GL 20041020001302004102000130NM 2004 10 20 371PA0060 120040921A5320654962156 INTERCOSTAL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 AFT CARGO DOOR FWD HOLD OPEN LATCH WEB CRACKED. REPLACED INTERCOSTAL IAW SRM 51-10-2 AND SRM 51-40-02. 2L72 4F4 FRTA16NE E2GL 20041020001312004102000131NM 2004 10 20 371PA0061 120040920A5320 ATTACH ANGLE BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 ATTACH ANGLE CRACKED AT BS 807 AND RBL 20. REPLACED ANGLE IAW SRM 53-60-15 AND SRM 51-40-02. 2L72 4F4 FRTA16NE E2GL 20041020001332004102000133NM 2004 10 20 P5CA0401252 120041017A8011 WARNING LIGHT BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL START VALVE ILLUMINATED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA15453PA 30811 706364 ENGINE NR 3 (START VALVE) EICAS MESSAGE, QPH CHECK ACCOMPLISHED. TRANSFERRED TO DMI NR 33262 IAW MEL 80-11-01. 2L74 4F4 FRTA20WE E23EA 20041020001342004102000134NM 2004 10 20 P5CA0401253 120041018A5753 FLAP TRACK BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 6 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 NR 6 FLAP TRACK AFT ATTACHMENT IB BLOCK OB HOLE CORRODED ON WING AT STA 353. REMOVED CORROSION, OPEN HOLE HFEC PERFORMED OK, REPAIRED IAW SRM 51-10-01. 2L74 4F4 F A20WE E20EA 20041020001352004102000135EU 2004 10 20 RAIA00410006 120041014A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE EMERGENCY LIGHT INOPERATIVE A RAIAO OTHER L NO TEST ININSP/MAINT 1 CE03558HK 41071 3660- BWI- SECTION OF FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE RESEATED CONNECTOR BETWEEN ROW 2 AND 3. 2L72 4T4 TRTA41NM E18NE 20041020001362004102000136 2004 10 20 RAIA00410011 420041018A3418 COMPUTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL STALL WARNING INOPERATIVE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03835HK 145670 STALL PROTECTION SYSTEM NR 1 INOPERATIVE AND STALL PROTECTION SYSTEM. MAINTENANCE RERACKED AND CLEANED CONNECTOR OF STALL PROTECTION COMPUTER. 2L72 4T4 FRTT00011ATTE6CH 20041020001372004102000137NM 2004 10 20 371PA0055 120040921A5752 TAB BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE RT AILERON DELAMINATED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 RT AILERON TAB IS DELAMINATED AT OB END. REPLACED RT AILERON TAB MM 27-11. 2L72 4F4 FRTA16NE E2GL 20041020001382004102000138NM 2004 10 20 371PA0059 120040920A5320 TRANSITION PANEL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE APU BLEED DUCT BROKEN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 TRANSITION PANEL AT APU BLEED DUCT AT BS 767 BROKEN. REPLACED PANEL IAW SRM 51-20-1 AND SRM 51-40-1. 2L72 4F4 FRTA16NE E2GL 20041020001392004102000139EU 2004 10 20 AWXA200401131 120041016A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU IAE V2524 V2524A5 NE SEAT ROW 4 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28656AW 1079 DURING E-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT HARNESS AT SEAT ROW 4 LT IAW AMM 33-51-18-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20041020001402004102000140NM 2004 10 20 371PA0065 120040916A5311 FRAME BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FRAME CRACKED AT RIVET AB BS 460 AND STR 25 LT. REPAIRED IAW SRM 51-70-11. 2L72 4F4 FRTA16NE E2GL 20041020001422004102000142NM 2004 10 20 AWXA200401089 120041004A3240 BRAKE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE MLG SEIZED A AWXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP28182AW 22649 ABORTED TAKEOFF, FLT 0109, ON TAKEOFF, EN ROUTE WHEN APPROACHING V1 THE AIRCRAFT NOSE STARTED TO ROTATE ON ITS OWN, LOWERED NOSE AND REJECTED TAKEOFF AT 138 KTS. MAINTENANCE PERFORMED HORIZONTAL STABILIZER TRIM TEST, ALL TRIM INDICATIONS AGREE WITH (B) DIMENSION THROUGH FULL RANGE OF TRAVEL, NO AERODYNAMIC REASON TO EXPLAIN EARLY ROTATION. NR 3 AND 4 BRAKES SEIZED AND FUSE PLUGS BLOWN ON BOTH TIRES DUE TO REJECTED TAKEOFF. REPLACED NR 3 AND 4 WHEEL/TIRE, AND BRAKE ASSEMBLIES IAW T/C R4M32013 AND R4M32014. AS A PRECAUTION, REPLACED NR 1 AND 2 WHEEL/TIRE, AND BRAKE ASSEMBLIES IAW T/C R4M32013 AND R4M32014. 2L72 4F4 FRTA16WE E2EA 20041020001432004102000143NM 2004 10 20 371PA0081 120040914A5320 SCUFF PLATE BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE CARGO DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 AFT CARGO DOOR CUT OUT FWD AND AFT SCUFF PLATES CRACKED. REPAIRED IAW MFG PROCESS SPEC. 5975 AND 8.6. 2L72 4F4 FRTA16NE E2GL 20041020001442004102000144NM 2004 10 20 371PA0082 120040915A5315 FLOORBEAM BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FLOORBEAM AT BS 967 CORRODED ON THE AFT SIDE AT RBL 18. REPAIRED FLOORBEAM IAW SRM 53-00-51. 2L72 4F4 FRTA16NE E2GL 20041020001452004102000145NM 2004 10 20 371PA0083 120040917A5315 FLOORBEAM BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FLOORBEAM AT BS 967 CORRODED AT LBL 18. REPAIRED IAW SRM 53-00-51. 2L72 4F4 FRTA16NE E2GL 20041020001462004102000146WP 2004 10 20 04FDEA02950 120041018A7830536L379G13 FRAME DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 NR 2 ENGINE RT THRUST REVERSER TRAILING EDGE AFT FLANGE CRACKED APPROXIMATELY 6 INCHES FROM BOTTOM. COMPLIED WITH MFG EA 8-7830-81496 2L73 4F4 FRTA22WE E23EA 20041020001472004102000147WP 2004 10 20 04FDEA02951 120041018A5410AUB7054501 PANEL DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ZONE 400 MISALIGNED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46621 NR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENTILATOR PANEL REPAIR. 2L73 4F4 FRTA22WE E23EA 20041015000902004101500090NE 2004 10 15 KBM2004F00218 220041005A75329550158260 BLEED VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 BLEED VALVE STUCK OPEN IN FLIGHT. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20041015000922004101500092SO 2004 10 15 K4S2004F00000 220040618A8500 ENGINE CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO RIGHT FAILED E K4SAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP23747CA 421C0850 227835R ON 6/18/04, RT ENGINE FAILED AT CRUISE AT 15,500 FT. ENGINE WAS SECURED AND EMERGENCY LANDING MADE. FLIGHT WAS PART 91 REPOSITIONING WITH NO PASSENGERS OR CARGO. (WP23200408767) 1L72 3O3 O A7CE E7CE 20041015000962004101500096EA 2004 10 15 COMA0460552 120040925A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01781CA5852 7312 FLIGHT 5908 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F4 FRTA21EA E15NE 20041018000032004101800003EA 2004 10 18 SWIA200413923 120040816A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW 7536 INTERCOSTAL AT FS 484 LBL 36 CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH MFG REO 601R-53-41-059 REPAIR TO INTERCOSTALS FS 484 DL 27-00-36-00. 2L72 4F4 FRTA21EA E15NE 20041018000062004101800006EA 2004 10 18 SWIA200413925 120040816A5312 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AP BULKHEAD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07431SW FS 625 OBLIQUE ANGLE IS CRACKED ON LT SIDE OF AFT PRESSURE BULKHEAD, APPROX .65 INCH LONG. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED ANGLE PN 601R-35012-51 IAW CRJ 200 SRM 51-42-06. 2L72 4F4 FRTA21EA E15NE 20041018000112004101800011EA 2004 10 18 SWIA200413930 120041011A2740 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB/MACH TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07954SW 7815 STAB TRIM NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL IAW CRJ MM 27-41-15 AND 20. OPERATIONAL CHECK GOOD. PN 601R51706-3 2L72 4F4 FRTA21EA E15NE 20041018000182004101800018EU 2004 10 18 AWXA200401092 120040925A5321D5367005000200 FLOOR PANEL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 261FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 261FF IAW T/C C1D25310. 2L72 4F4 FRTA28NM E40NE 20041018000192004101800019EU 2004 10 18 AWXA200401093 120040925A5321D5367003600500 FLOOR PANEL AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED CORRODED FLOOR PANEL 262FF IAW T/C C1D25310. 2L72 4F4 FRTA28NM E40NE 20041018000282004101800028NM 2004 10 18 UPS04443271 120040926A5313 STRINGER BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C FWD CARGO STA 860-880 S47L STRINGER CORROSION FOUND. FWD CARGO BS 860-880 STR 47L STRINGER REPAIRED IAW SRM 53-10-03 FIG 1 DUE TO BLEND OUT DEPTH 0.040 INCH , WIDTH 1 INCH AND LENGTH 2 INCHES OUT OF SRM 53-10-01 FIG LIMITATION. 2L74 4F4 F A20WE E20EA 20041018000292004101800029NM 2004 10 18 UPS04M43286 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE-C, HORZ STAB NR 21 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 21 RT BARREL NUT HOLE REMOVED, BLENDED AND REAMED TO 1.067 INCH. FOUND OUT OF LIMIT FAB SLEEVE BUSHING IAW EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 21 RT AND INSTALLED SLEEVE BUSHING IAW EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 21 RT IAW EO MD11-5510-19409-H AND EN 1248-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041018000522004101800052WP 2004 10 18 ABXA040337 120040921A534039240292N FITTING DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 END FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0, ARE CRACKED AND CORRODED. REMOVED AND REPLACED END FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0 IAW SRM 51-30-5. PN: 3924029-2N AND 3924029-1N. 2L72 4F4 F A6WE E2EA 20041018001132004101800113NM 2004 10 18 04FDEA02458 120040812A5314 KEELBEAM BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 N00636 CORROSION, ON KEELBEAM STR 29L .950F 3 ON FLANGE AROUND FASTENER. ** SD COMING ** 2L73 4F4 FRTA3WE E2EA 20041020000012004102000001NM 2004 10 20 ASAA0410372 120040813A53206585378189 WEB BOEING737 737200 1384453NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND AFT WEB SECTION DAMAGED. REPLACED WEB. (M) 2L72 4F4 F A16WE E2EA 20041020000232004102000023EU 2004 10 20 A6WA200460040 120040921A5755 STRUCTURE BAG BAE146BAE146200A 1500266EU AIRBRAKE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 AIRBRAKE STRUCTURE AFT OF FRAME 50 VERTICAL STIFFENER HAS A CRACK RADIATING FROM RIVET. REPAIR IN PROGRESS. (M) 2H74 4F RTA49EU 20041020000322004102000032EA 2004 10 20 ASOA04660 120040830A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11909EV 7658 DURING HANGAR MAINTENANCE IN MCN, THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR WERE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041020000422004102000042NM 2004 10 20 AMTA200401090 120040828A3350 LIGHT BOEING757 75723N 1384973NM CABIN MALFUNCTIONED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 FOUND EMERGENCY LIGHT ON JUST AFT L1 DOOR IN 2 LOCATIONS. REMOVED AND REPLACED LIGHT ASSEMBLY AS PER 33-51-05, OPS CHECK OK. (M) 2L72 4F RTA2NM 20041020000452004102000045NM 2004 10 20 USAA040592 120040829A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH WIDE AREA, BETWEEN STATION 967 AND 986.5 AT RBL 18. REPLACED FLOOR SUPPORT PER SRM 51-40-03. (M) 2L72 4F RTA16WE 20041020000482004102000048NM 2004 10 20 USAA040589 120040824A53401133482 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND TIE CLIP CRACKED .25 INCH, STATION 847 - 4L INTERIOR TIE CLIP. REPLACED TIE CLIP PER SRM 53-40-03. (M) 2L72 4F RTA16WE 20041020000492004102000049NM 2004 10 20 USAA040590 120040824A53401133482 STRINGER CLIP BOEING737 7374B7 1384702NM FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND TIE CLIP CRACKED .24 INCH, INTERIOR TIE CLIP STATION 807 10R. REPLACED TIE CLIP PER SRM 53-40-03. (M) 2L72 4F RTA16WE 20041020000502004102000050NM 2004 10 20 USAA040569 120040826A5311 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19603AU63100 22198 CLT - FOUND FRAME CRACKED 1 INCH LONG, LT MLG WW, FS 1060, SAME LEVEL AT LOWER WING SURFACE, TEE CAP. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED PER SRM 51-70-12. (M) 2L72 4F RTA2NM 20041020000592004102000059EU 2004 10 20 USAA040520 120040828A5321 FLOOR PANEL AIRBUSA321 A321211 3930370EU CARGO BAY DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19166US12095 1436 PIT - FOUND CARGO FLOOR PANEL DAMAGED, 137 INCHES AFT FORWARD CARGO BIN BULKHEAD, 18 INCHES RIGHT OF CENTERLINE. TEMPORARY REPAIR, REMOVED DAMAGED, INSTALLED TAPE PER TYP REPAIR 53-02-01. (M) 2L72 4F RTA28NM 20041020000632004102000063NM 2004 10 20 ASAA0410363 120040806A5310AND101341204 DOOR FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON E/E BATTERY DOOR CUTOUT FORWARD FRAME. REPAIRED DOOR FRAME, CUTOUT. (M) 2L72 4F RTA16WE 20041020000652004102000065NM 2004 10 20 ASAA0410358 120040730A534069353521 STRINGER CLIP BOEING737 737298C 1384490NM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED NEW AND INSTALLED. (M) 2L72 4F RTA16WE 20041020000792004102000079NM 2004 10 20 UIEA200400175 120040923A3350BACR13CD2 RELAY BOEING747 747243B 1384830NM EMERGENCY LIGHT INOPERATIVE A UIEAO OTHER J WARNING INDICATION CRCRUISE 1 EA15516MC 22507 EMERGENCY LIGHT FLICKER DURING FLIGHT. FOUND RELAYS ON EMERGENCY LIGHTS UNSECURED, RESECURED RELAYS OPS CHECK OK IAW MM 33-51-07. REMOVED AND REPLACED BOTH RELAYS ON EMERGENCY LIGHT CNTL PANEL LIGHTS OPS OK PER MM 33-51-07. (M) 2L74 4F A20WE 20041020000842004102000084NM 2004 10 20 BJNA040903 120040903A2560P4010021 BATTERY PACK BOEING737 737282 13844ATNM FLASHLIGHT INGESTED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11789TM 23046 FORWARD FLIGHT ATTENDANT UPPER EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M) 2L72 4F RTA16WE 20041020000902004102000090EA 2004 10 20 A6WA200440130 120040907A2750860010018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A A6WAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL31441ZW 7777 FLAP FAIL MESSAGE ILLUMINATED AT 13000 FT, COMPLIED WITH QRH PERFORMED ZERO FLAP LANDING, BRAKES APPLIED AT LESS THAN 80 KNOTS, MAX BRAKES TEMP INDICATION WAS '2'. TOUCHDOWN AT 172 KNOTS. REMOVED AND REPLACED FECU IAW AMM 27-51-05. COMPLIED WITH OPS CHECK OF FLAP SYSTEM IAW AMM, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20041020001062004102000106NM 2004 10 20 USAA040644 120040918A5314 KEELBEAM BOEING737 7373B7 1384580NM FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND KEEL BEAM WITH DEEP METAL WEAR .1875 INCH AT FASTENER HOLES, KEEL BEAM LOEWR FLANGE BETWEEN BS 727-704. INSTALLED STRAP DOUBLER PER EA 79007. (M) 2L72 4F RTA16WE 20041020001092004102000109NM 2004 10 20 USAA040633 120040828A5230 WEB BOEING737 7373B7 1384580NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND AFT CARGO INNER WEB CRACKED .25 INCH, LIGHTENING HOLE AFT OF SPRING MOUNT. REMOVED DAMAGE, INSTALLED DOUBLER PER EA 78996. (M) 2L72 4F RTA16WE 20041020001212004102000121NM 2004 10 20 USAA040670 120040820A5320 SUPPORT BOEING737 7373B7 1384580NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND SUPPORT HAS 15 OVERSIZED HOLES, BS 540 BETWEEN RIGHT INBOARD AND OUTBOARD SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-52. (M) 2L72 4F RTA16WE 20041020001242004102000124NM 2004 10 20 ASAA0410377 120040818A5330 SKIN BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND FUSELAGE SKIN IS GOUGED AT BS 902 STRINGER 19R. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20041020001262004102000126NM 2004 10 20 USAA040607 120040917A5320 STRAP BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND STRAP CORRODED 1 INCH, STATION 324 RBL 63. REPLACED ANGLE/STRAP IAW SRM 51-10-02. (M) 2L72 4F RTA2NM 20041020001492004102000149WP 2004 10 20 04FDEA02952 120041018A2540 LAVATORY DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ZONE 200 NOT SEATED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25392FE 46626 LAVATORY PAPER AND WASTE RECEPTACLE DOES NOT SEAL CORRECTLY. RESEALED LAVATORY PAPER AND WASTE RECEPTALE IAW MD10-10 SRM 51-41-01 VOL II AND EA 8-2540- 82478, SEALING OF FORWARD LAVATORY TRASH SHOUT. 2L73 4F4 FRTA22WE E23EA 20041020001512004102000151NM 2004 10 20 371PA0074 120040918A5320654583471 STRAP BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FLOORBEAM BROKEN A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 STRAP ON LOWER SIDE OF FLOORBEAM AT BS 312 TO BS 328 AT RBL 45 BROKEN. REPLACED STRAP IAW SRM 51-10-2. 2L72 4F4 FRTA16NE E2GL 20041020001532004102000153EU 2004 10 20 AWXA200401129 120041014A2840IC5059110207 COMPUTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUEL QTY INOPERATIVE A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28652AW1330812171 953 AFTER TAKEOFF EN ROUTE LOST ALL FUEL QUANTITY INDICATIONS, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE R/R FUEL QTY INDICATION COMPUTER (FQIC) IAW AMM 28-42-34, OS CHK GOOD. FUNCTIONAL TESTING OF FQIC S/N 1772 PRODUCED NO FAILURES OR FAULTS. UNIT SENT TO TESTING FACILITY WHERE UNIT PASSED INITIAL TESTING WITH NO FAULTS NOTED. UNIT THEN FORWARDED TO EUROPE FOR IN DEPTH TESTING. PERFORMED A PRODUCTION ACCEPTANCE TEST, ENGINEERING ACCEPTANCE TEST, AN ENGINEERING PRODUCTION TEST ON SYSTEM RIG THAT INTERROGATED THE FAULT LOG, TWO SEPARATE 40-HOUR TEMPERATURE AND VIBRATION TESTS, AND FINALLY OPERATIONALLY GROUND TESTED ON AIRCRAFT, & NONE OF THE TESTS COULD PRODUCE A FAULT, UNIT RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E40NE 20041020001542004102000154EU 2004 10 20 AWXA200401130 120040925A5315D5347209001000 FLOORBEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292, UNDER LT AFT LAVATORY AT FR 66. MAINTENANCE REMOVED FLOORBEAM Y1292 LT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-71-11. 2L72 4F4 FRTA28NM E40NE 20041020001572004102000157EA 2004 10 20 OG52004F00003 220041004A853073938 INTAKE VALVE LYC PIPER PA44 PA44180 7104402SO LYC O360 O360A1H 41514EA NR2 CYLINDER FRACTURED B OG5RO OTHER O OTHER NRNOT REPORTED 1 GL21295ND1521 4496030 L2524636A DURING CRUISE FLIGHT PILOT EXPERIENCED SURGING M/P ON LT ENGINE AND VIBRATION ON FINAL. INSPECTION FOUND NR 2 CYLINDER INTAKE VALVE FRACTURED WITH PIECES IN NR 2 AND NR 3 COMBUSTION CHAMBERS. CYLINDER HEAD AND PISTON TOPS DAMAGED IN BOTH CYLINDERS FROM CONTACT WITH VALVE PIECES. (GL21200500265) 1L72 3O3 O A19S0 E286 20041020001582004102000158EU 2004 10 20 AALA20041048 120040928A5311 FRAME AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2177080 626 FRAME CORROSION FOUND AT BULKHEAD AFT END OF FORWARD CARGO AT BOTTOM BETWEEN STRINGER 52 RT AND 54 RT AT STATION 39. REPAIRED THE FRAME 39 BULKHEAD IAW ESO 30595 DATED 9/22/04 REPAIR NR 40 531000 3693. (CLOSED) 2L72 4F4 FRTA35EU E13NE 20041020001602004102000160EU 2004 10 20 SA04095 120041013A5610SPSA3201022 WINDOW AIRBUSA321 A321211 3930370EU CFMINTCFM56 CFM563B1US GL COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19165US13020 1431 THE FIRST OFFICER AFT WINDOW OUTER PANE CRACKED DURING CRUISE. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S AFT FIXED WINDOW. OPERATIONALLY CHECKED OK. OK FOR SERVICE. 2L72 4F4 FRTA28NM E2GL 20041020001642004102000164SO 2004 10 20 C2XA04CL102 120041006A2120 ODOR EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL APU DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2714516 145323 THE CREW REPORTED THE APU SHUTDOWN IN FLIGHT WITH A STRONG FUEL ODOR IN THE COCKPIT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE APU. NO FUEL ODOR WAS PRESENT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATION. 2L72 4F4 FRTT00011ATTE6CH 20041020001672004102000167WP 2004 10 20 DHL2004801523 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 NR. 1101: MAIN CARGO COMPARTMENT NR 1 TRACK PLUG LUGS WORN, STA 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041020001682004102000168WP 2004 10 20 DHL2004801546 120040909A5520 ANGLE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT VERTICAL STABILIZER LWR ANGLE CRACKED 1.500, ZR 47.000 (RT) REAR SPAR PLANE. PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 16A SHEET 1-2 PAGES 44 ABCD. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-5 FIG 16A SHEET 1-2. FABRICATED SHIM (AL2024-T3 0.125) FILLER (AL7075-T6 0.160) ANGLE (STEEL 17.7PH 0.079) IAW SRM 53-2-5 PAGES 44 ABCD FIG 16A (SHEET 1-2). PERFORMED HEAT TREATMENT TO STEEL ANGLE IAW SRM 51-1-6. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA, SHIM AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED SHIM, FILLER AND ANGLE IAW SRM 53-2-5 FIG 16A (SHEET 1-2) PAGE 44 ABCD. 2L74 4F4 FRT4A25 E2GL 20041020001702004102000170WP 2004 10 20 DHL2004801525 120040904A5730 PANEL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT WING T/E LOWER PANEL INTERNAL SKIN DELAMINATED (STA. XW 5.000 - 97.000). REMOVED DELAMINATED LT WING T/E LOWER PANEL (XW 5.000 - 97.000) IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LT WING T/E LOWER PANEL IAW SRM 51-3-0. 2L74 4F4 FRT4A25 E2GL 20041020001732004102000173WP 2004 10 20 DHL2004801520 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPARTMENT NR 7 TRACK LUGS WORN, STA. 250.000. CUT OUT WORN SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041020001742004102000174SO 2004 10 20 MASA200400415 120040720A335066903 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07833MJ 145327 DURING MAINTENANCE, FOUND 1ST SECTION OF FLOOR EMERGENCY LIGHTING STRIP WOULD NOT ILLUMINATE. DEFERRED IAW MEL 33-50-00-2. MAINTENANCE REPLACED THE LIGHTING STRIP ON 7/20/04. OPS CHK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20041020001752004102000175WP 2004 10 20 DHL2004801521 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 REF. NR. 1105: MAIN CARGO COMPARTMENT NR 6 TRACK PLUG LUGS WORN, STA. 250.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S277660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041020001762004102000176WP 2004 10 20 DHL2004801522 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 1103: MAIN CARGO COMPARTMENT. NR 4 TRACK PLUG LUGS WORN, STA. 322.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041020001772004102000177WP 2004 10 20 UPS04843306 120040911A5310 FINGER DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE-C3 SHEARED FASTENERS AND CORROSION UNDER FINGER DOUBLER STA 880-900 BL 0. CUT OUT DAMAGE TO WEB AND FINGER DOUBLER. FABRICATED FILLER, FINGER DO DOUBLER, AND DOUBLER IAW SRO DWG 5645332. INSTALLED ALL REPAIR PARTS IAW SAA SK772-069. 2L74 4F4 FRT4A25 E2GL 20041020001782004102000178WP 2004 10 20 DHL2004801556 120040927A53404633996 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 0988: AFT ACCY COMPARTMENT FLOORBEAM CEILING FITTING CRACKED 0.500 AT STA. 660.000. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG.1. SRM 51-1-21 PG.1. FABRICATED NEW FITTING (AL7075-T7351) IAW DWG 4333996. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND FITTING IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW FITTING IAW DWG 4633996, SRM 51-3-0 PG.1, SRM 51-1-21 PG.1. 2L74 4F4 FRT4A25 E2GL 20041020001932004102000193EU 2004 10 20 HCM2004F00002 120041001A6730SC8042 SERVO UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE CENTER INTERMITTENT E HCMAO OTHER O OTHER NRNOT REPORTED 1 WP1311QM 1566 340 3751 23003 DURING STARTUP, THE PILOT NOTICED THAT THE CYCLIC CONTROL WAS STIFF IN THE FORE/AFT POSITION. HE ATTEMPTED TO ADJUST THE FRICTION AND FOUND IT RELEASED. THE CYCLIC CONTROL JUMPED FORWARD. AS HE PULLED BACK, HE FELT THE CONTROL APPEARED TO BE INTERMITTENT AND GRABBING. UPON INSPECTION BY THE MECHANIC, IT WAS FOUND THA THE INPUT LEVER WAS STUCK. IT WAS POSSIBLE TO MOVE THE LEVER WITH EXCESSIVE FORCE THE AIRFRAME MFG IS INVESTIGATING THE MATTER. 1G72 3U3 U H9EU E00054EN 20041020002002004102000200CE 2004 10 20 H7O2004F00000 120040916A251005142132 CYLINDER CESSNA172 172R 2072401CE LYC O360 IO360A1A 41514EA SEAT BROKEN D H7OEO OTHER O OTHER NRNOT REPORTED 1 EA219754F2249 17280037 ROD END SNAPED OFF THE LOCK CYLINDER WHILE BEING USED. 1H71 3O3 ONT3A12 1E10 20041020002032004102000203NM 2004 10 20 ASMF200409013 120040929A324442831 CONTROL PANEL DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE AUTOBRAKE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23161PL38124 49764 AIRCRAFT RETURNED TO PLATFORM, CONFIGURATION AUDIBLE ALARM WAS ACTIVATED AND AUTO SPOILER FAIL LIGHT WAS DEFERRED BY MEL. TAKEOFF CONFIGURATION WAS CHECKED BEING CORRECT. DURING OVERNIGHT SERVICE AUTO SPOILERS AND CONFIGURATION ALARM WERE CHECKED. AUTO BRAKE CONTROL PANEL WAS REPLACED IAW MM 32-44-01, TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E2EA 20041020002052004102000205NM 2004 10 20 SWAA043024 120041018A53116546548 FRAME BOEING737 7373H4 1384600NM AFT CARGO COMPT CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 747, FROM RBL 5 TO RBL 20 CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041021000032004102100003NM 2004 10 21 USAA040692 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 727B, S8R, S9R. DOUBLER INSTALLED PER SRM 53-00-07 FIG 202. (M) 2L72 4F RTA16WE 20041021000062004102100006NM 2004 10 21 ASAA0440157 120040825A5320BAC1496377 ANGLE BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND AFT CARGO COMPARTMENT ZEE ANGLE CORRODED. REPLACED ZEE ANGLE. (M) 2L72 4F RTA16WE 20041021000072004102100007NM 2004 10 21 ASAA0440159 120040828A5311 FRAME BOEING737 7374S3 1384711NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT LOWER LEG CIRCUMFERENTIAL FRAME BETWEEN CENTER FLOOR SUPPORTS 727B MATERIAL OUT OF LIMITS ON UT INSPECTION. REF SRM, ORIGINAL THICKNESS .063 INCH, REMAINING .055 INCH. INSTALLED DOUBLER REPAIR ON CIRCUMFERENTIAL FRAME BETWEEN CENTER FLOOR SUPPORTS AT STATION 727B PER SRM. (M) 2L72 4F RTA16WE 20041021000112004102100011NM 2004 10 21 ASAA0440158 120040830A5753 SKIN BOEING737 7374S3 1384711NM FORE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND RIGHT WING FORE FLAP DENTED ON LOWER SURFACE. CUT OUT DAMAGED AREA, INNER CORE REPLACEMENT AND BONDED EXTERNAL DOUBLER. (M) 2L72 4F RTA16WE 20041021000152004102100015NM 2004 10 21 USAA040685 120040929A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19586US51695 23931 CLT - FOUND SKIN CRACKED 1 NCH, STATION 943 STRINGER 24L. INSTALLED DOUBLER IAW EA 95872A. (M) 2L72 4F RTA16WE 20041021000162004102100016NM 2004 10 21 USAA040673 120040929A5310 SHEAR TIE BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU63825 22193 FOUND SHEAR TIE CORRODED .5 INCH BY .5 INCH, STATION 1320 ABOVE STRINGERS 27R AND 26R. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-40-00. (M) 2L72 4F RTA2NM 20041021000192004102100019EU 2004 10 21 ASOA04750 120040927A33503011210 LIGHT AEROSPATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11641AS 387 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMEGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20041021000202004102100020EA 2004 10 21 ASOA04751 120040927A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11830AS 7236 FLT 4219 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP FORWARD OF THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041021000212004102100021EA 2004 10 21 A6WA200440138 120040929A3260 BRACKET CNDAIRCL600 CL6002B19 1900309EA CENTER SENSOR BENT A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31429AW 7711 SELECTING GEAR UP RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MSG. PERFORMED QRH AND RETURNED TO FIELD. PERFORMED QRH AND RETURNED TO FIELD. FOUND BRACKET FOR NOSE LANDING GEAR CENTERED SENSOR BENT. REMOVED AND REPLACED BRACKET AND ADJUSTED SENSOR PS14GA IAW AMM 32-61-05, C/W GEAR SWING. NO DEFECTS NOTED. (M) 2L72 4F RTA21EA 20041021000232004102100023EA 2004 10 21 ASOA04752 120040927A3350BF50390901 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO11848AS 7339 FLT 4686 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER BY THE PASSENGER DOOR WAS FOUND MISSING. MAINTENANCE INSTALLED A NEW COVER AND ALSO REMOVED AND REPLACED THE LAMP ON THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041021000242004102100024EA 2004 10 21 ASOA04753 120040927A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11854AS 7382 FLT 4472 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041021000272004102100027NM 2004 10 21 USAA040695 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 867, S8L, S9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M) 2L72 4F RTA16WE 20041021000282004102100028NM 2004 10 21 USAA040674 120040929A5330 SKIN BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 CLT - FOUND SKIN REPAIR FILLER CORRODED .6 INCHES BY .2 INCHES, BETWEEN STATION 1316 OUTBOARD OF STRINGER 27R BELOW TRANSITION ANGLE. FABRICATED AND INSTALLED NEW REPAIR FILLER. (M) 2L72 4F RTA2NM 20041021000292004102100029NM 2004 10 21 USAA040672 120040929A5330 STRINGER CLIP BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU63825 22193 CLT - FOUND TIE CLIP CORRODED 3 INCHES LONG, STATION 1300 STRINGER 28R TO 27R. FABRICATED NEW TIE CLIP AND REPLACED PER SRM 51-20-01. (M) 2L72 4F RTA2NM 20041021000322004102100032NM 2004 10 21 ASAA0410394 120040911A531565549091 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON FLOORBAM UPPER CHORD. REPAIRED FLOORBEAM UPPER CHORD AFT FLANGE. (M) 2L72 4F RTA16WE 20041021000332004102100033NM 2004 10 21 USAA040679 120040924A5240 BRACKET BOEING737 7374B7 1384702NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41104 24558 PIT - FOUND BRACKET CRACKED .5 INCH, FORWARD SERVICE DOOR LOWER AFT CORNER INTERNAL BRACKET. REPLACED BRACKET WITH MANUFACTURED BRACKET PE SRM 52-10-02. (M) 2L72 4F RTA16WE 20041021000342004102100034NM 2004 10 21 USAA040680 120040826A5311 FRAME BOEING737 7374B7 1384702NM FS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US41214 24556 PIT - FOUND FRAME CRACKED .125 INCH, RIVET FAR SIDE AIR RAIL SUPPORT STATION 727F LEFT SIDE. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M) 2L72 4F RTA16WE 20041021000362004102100036NM 2004 10 21 USAA040682 120040916A534065617777 FITTING BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND STRINGER END FITTING CRACKED .25 INCH, STRINGER 15L AFT OF STATION 360. INSTALLED NEW PART PER BOEING DWG 65-17685 ND SRM 51-40-02, 51-10-02, 51-40-03. (M) 2L72 4F RTA16WE 20041021000372004102100037NM 2004 10 21 ASAA0410390 120040905A5310654656911 SHEAR TIE BOEING737 737* NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON SHEARTIE, FORWARD AND AFT SIDES. FOUND CORROSION BLENDOUT TO BE 'OUT OF LIMITS'. REMOVED, FABRICATED AND INSTALLED SHEAR TIE. (M) 2L72 4F RTA16WE 20041021000382004102100038NM 2004 10 21 USAA040690 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, FRAME FS 747, S8R S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M) 2L72 4F RTA16WE 20041021000402004102100040NM 2004 10 21 ASAA0410392 120040909A5310654654820 SHEAR TIE BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND SHEAR TIE CRACKED AT 2 FASTENER HOLE LOCATIONS. REMOVED AND REPLACED SHEAR TIE. (M) 2L72 4F RTA16WE 20041021000422004102100042NM 2004 10 21 USAA040691 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 727D, S8R, S9R. CUT OUT CRACK, INSTALLED FILLER PLUG AND DOUBLER PER SRM 53-00-07 FIG 202. (M) 2L72 4F RTA16WE 20041021000442004102100044NM 2004 10 21 ASAA0410396 120040912A531365516983 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND ELONGATED FASTENER HOLE IN STRINGER 18L UPPER FLANGE AT BS 905. REMOVED DISCREPANT AREA, INSTALLED REPAIR STRINGER SPLICE. (M) 2L72 4F RTA16WE 20041021000452004102100045NM 2004 10 21 USAA040684 120040910A53201128323 WEB BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND WEB CORRODED NUMEROUS AREAS, 12 INCHES LONG, AFT CARGO THRESHOLD AND ADJACENT STRAP JUST INBOARD. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M) 2L72 4F RTA16WE 20041021000472004102100047NM 2004 10 21 USAA040694 120040910A5311 FRAME BOEING737 7374B7 1384702NM BS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, BS 747, S8L, S9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07, FIG 202. 9M) 2L72 4F RTA16WE 20041021000512004102100051NM 2004 10 21 ASAA0440142 120040731A5320BAC1496377 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 OAK - FOUND LOWER FUSELAGE BELOW AFT CARGO COMPARTMENT BILGE LEFT Z-ANGLE AT STATION 727-847 HAS CORROSION ON THE UPPER SURFACE AT SEVERAL PLACES. MARKED IN RED. REMOVED CORRODED Z-ANGLE ON LEFT SIDE STATION 727-847. INSTALLED NEW Z-ANGLE IN REF SRM 51-40-02 PAGE 3. (M) 2L72 4F RTA16WE 20041021000542004102100054NM 2004 10 21 ASAA0440160 120040902A5414313A1200108 SKIN BOEING737 7374S3 1384711NM RT PYLON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND RIGHT PYLON SKIN GOUGED AT INBOARD NACELLE. INSTALLED WEAR STRIP. (M) 2L72 4F RTA16WE 20041021000562004102100056NM 2004 10 21 USAA040688 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH CRACK, FRAME BS 867 S8R, S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07. (M) 2L72 4F RTA16WE 20041021000572004102100057NM 2004 10 21 USAA040689 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, FRAME BS 827, S8R, S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M) 2L72 4F RTA16WE 20041021000592004102100059EA 2004 10 21 A6WA200440142 120041001A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA CARGO BAY DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31435AW 7724 FOUND CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHOR NUTS IN AREA OF CARGO DOOR OPENING. REMOVED MINOR CLASS 1 CORROSION IN AREA OF AFT CARGO ANCHOR NUTS BY HAND BURNISHING WITH SCOTCHBRIGHT IAW CRJ 200 SRM 51-21-11 PAGE 31. TREATED, PRIMED AND PAINTED AREAS IAW CRJ 200 SRM 51-21-06 PAGE 1. (M) 2L72 4F RTA21EA 20041021000602004102100060WP 2004 10 21 ASAA0480484 120040809A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 PDX LINE CHECK, FOUND THREE EMERGENCY LIGHTS INOPERATIVE IN TAILCONE AREA AFT OF BULKHEAD. REPLACED POWER SUPPLY, BATTERY PACK. LIGHTS THEN OPERATED PROPELY. (M) 2L72 4F RTA6WE 20041021000612004102100061NM 2004 10 21 ASAA0440162 120040902A5414313A106577 PANEL BOEING737 7374S3 1384711NM RT PYLON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND RIGHT PYLON PANEL NR 5829R HAS TWO GOUGES IN DOUBLER. INSTALLED REPAIR STRAP AND DOUBLER. (M) 2L72 4F RTA16WE 20041021000632004102100063NM 2004 10 21 SWAA043032 120041019A5340907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED UPPER HINGE BOX PER MM. 2L72 4F RTA16WE 20041021000652004102100065EA 2004 10 21 VNAA0410005 120041008A5270 INDICATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO DOOR INOPERATIVE A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05259PS 7945 CREW REPORTED THAT CARGO DOOR INDICATION DID NOT WORK. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CODE C. 2L72 4F4 FRTA21EA E15NE 20041021000662004102100066EA 2004 10 21 VNAA0410007 120041015A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO DOOR ILLUMINATED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL05206PS 7860 CREW REPORTED A CARGO DOOR MESSAGE IN FLIGHT. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CAT-C. 2L72 4F4 FRTA21EA E15NE 20041021000672004102100067EA 2004 10 21 VNAA0410008 120041011A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY DOOR ILLUMINATED A VNAAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL05262PS 7962 CREW REPORTED, RECEIVED A LEFT EMERGENCY DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE LEFT EMERGENCY DOOR WARNING 57-70-3 CODE C. 2L72 4F4 FRTA21EA E15NE 20041021000692004102100069 2004 10 21 SWAA043014 420041018A25656557463 FITTING BOEING737 7373Q8 1384670NM R2 DOOR SLIDE DIRTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 F/A HAD DIFFICULTY DISARMING R2 DOOR EVAC SLIDE. CLEANED R2 DOOR EVAC SLIDE GIRT BAR FLOOR ATTACH FITTING PER MM. 2L72 4F RTA16WE 20041021000702004102100070NM 2004 10 21 SWAA043015 120041018A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041021000722004102100072NM 2004 10 21 SWAA043017 120041018A3350101331 LENS BOEING737 7373Q8 1384670NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041021000732004102100073NM 2004 10 21 SWAA043018 120041018A534365C10300 GUSSET BOEING737 7375H4 138449DNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND NLG ACTUATOR UPPER ATTACH FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG ACTUATOR GUSSET PER SRM. 2L72 4F RTA16WE 20041021000742004102100074NM 2004 10 21 SWAA043019 120041018A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 DURING SCHEDULED MV1D CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041021000752004102100075NM 2004 10 21 SWAA043020 120041018A53306545770 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 690, STRINGER 4L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041021000762004102100076NM 2004 10 21 SWAA043022 120041018A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041021000772004102100077NM 2004 10 21 SWAA042989 120041015A57536546435334 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT FLAP PER MM. 2L72 4F RTA16WE 20041021000782004102100078EA 2004 10 21 MASA200400463 120040819A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A MASAO OTHER O OTHER CRCRUISE 1 SW0727191 7191 ASH 2296 VIA CLE-PHL, EXPERIENCED EMERGENCY LIGHTS FLUCTATING IN FLIGHT. UPON ARRIVAL IN PHL. MAINTENANCE REPLACED THE EMERGENCY BATTERIES AND CHARGER. AIRCRAFT WAS RETURNED TO SERVICE. P/N FOR BATTERIES IS 2013-1A AND S/N ON ONLY AVAIL 55218, 65083, 68124 AND 79736. CHARGER P/N BA5-0933-901 ONLY S/N ON AVAIL 13426, 16216, 16739 AND 17421. 2L72 4F RTA21EA 20041021000792004102100079NM 2004 10 21 MASA200400490 120040901A3350 LAMP DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07437YV 437 ASH 6203 PHX-FLG, ON F/A'S PANEL EMERGENCY GREEN LIGHT WILL NOT ILLUMINATE. PHX LINE MX RELAMPED AND OPS CHECKED GOOD. 2H72 4T RTA13NM 20041021000802004102100080SO 2004 10 21 MASA200400508 120040908A3350 LIGHT EMB 145 EMB145LR 3260212SO LT OVERWING INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2765, THE LT OVERWING EMERGENCY LIGHT INOP. ON CALL MAINTENANCE ADJUSTED THE LIGHT ASSEMBLY AND PERFORMED AN OPERATIONAL CHECK. 2L72 4T RTT00011AT 20041021000812004102100081EA 2004 10 21 MASA200400531 120040916A3350BM50018903 LENS CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSMISSING A MASAK NONE O OTHER ININSP/MAINT 1 SW07902FJ 15002 ASH 6451 PHX, OVERHEAD EMERGENCY LIGHT SIGN BETWEEN THE EXIT ROWS HAS A RED LENS MISSING. MX REPLACED THE RED LENS COVER. 2L72 4F RTA21EA 20041021000822004102100082SO 2004 10 21 MASA200400545 120040927A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07825MJ 145179 ASH 2646 DCA-CAE, 3RD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT, OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20041021000832004102100083NM 2004 10 21 MASA200400547 120040927A3350 SWITCH DHAV DHC8 DHC8201 2809001NM EMERGENCY LIGHT MALFUNCTIONED A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW07987HA 425 ASH 7015 PHX DRO, EMERGENCY EXIT LIGHT DOES NOT GO OFF WITH SWITCH OFF OPERATION. REMOVED AND REPLACED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH. CHECKED GOOD AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2H72 4T RTA13NM 20041021000842004102100084WP 2004 10 21 AALA20041040 120041010A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21437AA 49455 DFW - TAIL STAIRS EMERGENCY PATH LIGHT WHITE EXIT MARKERS INOPERATIVE. REPLACED DAMAGED WIRE TO TAIL STAIRS EMERGENCY PATH EXIT MARKERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041021000852004102100085WP 2004 10 21 AALA20041041 120041012A335060040351 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21489AA 49682 PHX - EMERGENCY LIGHTS AT AFT RIGHT HAND LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT RIGHT HAND LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041018001242004101800124SO 2004 10 18 2004F00401 220040930A8530AEC631377 CYLINDER HEAD CESSNA206 U206 2073306CE CONT O520 IO520* 17032SO ENGINE SEPARATED E O OTHER J WARNING INDICATION CRCRUISE 1 AL059417G U20601617 CYLINDER HEAD SEPARATED FROM BARREL IN CRUISE . 1H71 3O3 O A4CE E5CE 20041018001832004101800183EU 2004 10 18 EKL2004F00001 120040625A2150060018 BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE AIR COND BROKEN B EKLRO OTHER O OTHER NRNOT REPORTED 1 WP07955TV36 3246 9629 DURING FLIGHT, PILOT HAD INFLIGHT HYDRAULIC FAILURE, UPON EXECUTING THE HYDRAULIC SYSTEM FAILURE PROCEDURES, NOTICE AIR CONDITIONING SYS OUTPUT AIR BECAME WARM. THE AC WAS LANDED AT CLOSEST AIRPORT, SAFELY AND W/O FURTHER INCIDENT. UPON INSP OF HYDRAULIC AND AIR COND SYSTEM, THE SYSTEM DRIVE BELTS WERE RECOVERED. AIR COND BELT CAME APART AT SEAM WHERE TWO ENDS CAME TOGETHER. WHICH COULD POSSIBLY WHIPPED AROUND AND ENGAGED HYD BELT CAUSING IT TO BREAK, DISCONTINUING DRIVE OF HYD PUMP AND HYD SYSTEM FAILURE. NEW TYPE DRIVE BELT ON HYD PUMP HAS BEEN INSTALLED (THICKER AND MORE DURABLE BELT) AND PULLEY SYST. (WP07200413792) 1G71 3U3 U H9EU E19EU 20041018001912004101800191NE 2004 10 18 ASMF200409009 220040925A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RIGHT SIDE DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23169PL360236440 53175 718240 DURING BOROSCOPIC INSPECTION TO THE ENGINE NR 2, DAMAGES OUT OF LIMITS WERE DETECTED, NEAR TO THE 14TH STAGE OF BOROSCOPIC POINT, RT SIDE. ENGINE WAS REPLACED IAW MM 71-00-00, TEST WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20041020000042004102000004NM 2004 10 20 ASAA0410366 120040809A53406935352Y1 STRINGER CLIP BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON STRINGER CLIP. REMOVED OLD STRINGER CLIP AND INSTALLED NEW STRINGER CLIP. (M) 2L72 4F4 FRTA16WE E2EA 20041020000112004102000011NM 2004 10 20 ASAA0410375 120040817A5313BAC1498159 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON STRINGER BS 787 PLUS 5 INCHES STRINGER 22R WL 155. REMOVED AND REPLACED STRINGER BS 773-792 STRINGER 22R, WL 5. (M) 2L72 4F4 FRTA16WE E2EA 20041020000252004102000025NM 2004 10 20 ASAA0410380 120040821A5313BAC1498117 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON STRINGER. REMOVED DAMAGE, FABRICATED AND INSTALLED STRINGER REPAIR. (M) 2L72 4F RTA16WE 20041020000302004102000030NM 2004 10 20 UIEA200400166 120040921A541265B8904938 BULKHEAD BOEING747 747230B 1384889NM NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSEMBLY FORWARD ANGLE FRAMES OF THE NR 3 PYLON LHS AND RHS WERE FOUND CRACKED. STOP DRILLED THE CRACK ENDS PER 747 SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY PICKING UP ALL EXISTING FASTENER LOCATIONS AFFECTED BY THE REPAIR PARTS WITH HI-LOK FASTENERS. (M) 2L74 4F A20WE 20041020000372004102000037NM 2004 10 20 USAA040577 120040820A5313143N3110 STRINGER BOEING757 757225 1384959NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND STRINGER CORRODED 2 SQUARE INCHES, STRINGER 28L AT BS 656, STATION 648. REPLACED STRINGER SECTION PER SRM 53-00-03. (M) 2L72 4F RTA2NM 20041020000392004102000039NM 2004 10 20 USAA040575 120040821A5230 WEB BOEING757 757225 1384959NM AFT CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND AFT CARGO DOOR CORRODED 1 INCH BY 1 INCH, 22 INCHES AFT OF FORWARD EDGE, WEB. REPLACED DAMAGED WEB PER SRM 51-40-02. (M) 2L72 4F RTA2NM 20041020000402004102000040EA 2004 10 20 A6WA200440131 120040913A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG TRUNNION CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31421ZW 7346 LEFT MAIN LANDING GEAR, FORWARD TRUNNION, AFT BUSHING HAS PITTING ON FACE OF BUSHING. PERFORMED A MAJOR REPAIR TO PITTED LEFT MAIN LANDING GEAR FORWARD TRUNNION AFT BUSHING BY REMOVING BUSHINGS AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-003-41, IAW BOMBARDIER INC REO 601R-27-21-003 REV B. (M) 2L72 4F RTA21EA 20041020000442004102000044NM 2004 10 20 USAA040591 120040826A5320 CLIP BOEING737 7374B7 1384702NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19434US 24556 PIT - FOUND CLIP WITH CHAFE WEAR .75 INCH BY .1875 INCH BY .050 INCH DEEP, STATION 277 BETWEEN S2L AND S3L. REPLACED CLIP PER BOEING DWG 65-49806. (M) 2L72 4F RTA16WE 20041020000552004102000055NM 2004 10 20 UIEA200400164 120040921A541065B940512 PYLON BOEING747 747230B 1384889NM NR 3 CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, NR 3 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. NDT INSPECTION WAS ACCOMPLISHED AT EACH REPAIR AREA AND HFEC INSPECTION OF ALL TRIMMED EDGES AND ALL REPAIR FASTENER LOCATIONS TO ENSURE DEFECT FREE CONDITION. (M) 2L74 4F A20WE 20041020000602004102000060EA 2004 10 20 A6WA200440125 120040909A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31438AW 7748 WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 27R-26R AT FS 257 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5344. (M) 2L72 4F RTA21EA 20041020000692004102000069NM 2004 10 20 USAA040664 120040830A5510 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, RT HORIZ STAB R-10 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M) 2L72 4F RTA16WE 20041020000772004102000077NM 2004 10 20 USAA040649 120040916A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US53244 22959 PIT - FOUND SKIN TEAR, .5 INCH ALONG 1.75 INCH OF DOOR, RIGHT AFT SERVICE DOOR OUTSIDE SKIN FORWARD SIDE EDGE FORWARD OF HANDLE. REPAIRED PER SRM 52-00-01. (M) 2L72 4F RTA16WE 20041020000802004102000080NM 2004 10 20 USAA040631 120040921A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49206 23704 CLT - FOUND SKIN CRACKED 2.25 INCH, .5 INCH ABOVE STRINGER 25R SKIN LAP AT STATION 764. INSTALLED DOUBLER/TRIPLER AND FILLER PER SRM 53-00-01 FIG 229. (M) 2L72 4F RTA16WE 20041020000832004102000083NM 2004 10 20 USAA040651 120040916A5342 FITTING BOEING737 7373B7 1384580NM HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US53224 22959 PIT - FOUND CORNER FITTING CRACKED 5 INCHES, RIGHT TOP CORNER FITTING INSIDE HORIZ STAB INTERSECTING, PRIMARY AND THRUST BEAM. REPLACED ANGLE PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20041020000892004102000089NM 2004 10 20 USAA040602 120040917A5315 FLOORBEAM BOEING757 7572B7 1384964NM FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND FLOORBEAM CORRODED 130 INCHES, FS 365.25 ENTIRE FLOORBEAM. REPLACED TEE CAP PER TR 53-15-01. (M) 2L72 4F RTA2NM 20041020000922004102000092NM 2004 10 20 USAA040652 120040922A5310 WINDOW FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52642 23700 PIT - FOUND WINDOW FRAME CRACKED .25 INCH, UPPER OUTBOARD CORNER OF CAPTAIN WINDOW FRAME. REMOVED DAMAGE, DOUBLER INSTALLED PER SRM 53-10-01. (M) 2L72 4F RTA16WE 20041020000952004102000095NM 2004 10 20 USAA040641 120040826A5542 SKIN BOEING737 7373B7 1384580NM RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND RUDDER COMPOSITE SKIN DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, RUDDER RIGHT SIDE AT FS 180 10 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M) 2L72 4F RTA16WE 20041020001032004102000103NM 2004 10 20 USAA040663 120040903A534065479738 ANGLE BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND ANGLE CRACKED 2 INCHES, RT WING ROOT, BS 540 AT S22R. REPLACED CREASE BEAM SECTION PER SRM 51-40-00. (M) 2L72 4F RTA16WE 20041020001042004102000104NM 2004 10 20 BJNA040905 120040919A33506104789 BATTERY PACK BOEING737 737282 13844ATNM EMERGENCY LIGHT INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 FOUND LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-31. (M) 2L72 4F RTA16WE 20041020001122004102000112 2004 10 20 UIEA200400172 420040923A34201491500102 INDICATOR BOEING747 747243B 1384830NM ADI FAILED A UIEAJA DUMP FUEL UNSCHED LANDING O OTHER CRCRUISE 1 EA15540MC 22508 CAPTAINS ADI FAILED. INSTRUMENT WARNING LIGHT AND ATTITUDE LIGHT, UNABLE OT SWITCH TO NR 3 INU DUE TO BEING INOPERATIVE. REMOVED AND REPLACED CAPTAINS ADI IAW MM 34-41-05, OPS NORMAL. REMOVED AND REPLACED NR 1 AND NR 3 INU IAW MM 34-41-03 CHECKS ALL SYSTEM OPERATE NORMAL. FUEL DUMPED 59.4 KGS. (M) 2L74 4F A20WE 20041020001412004102000141EU 2004 10 20 WRNA200400015 120041015A36009786904 VALVE AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 ENGINE LEAKING A WRNAC ABORTED TAKEOFF JM WARNING INDICATION OVER TEMP TOTAKEOFF 1 SO05820SC 154 517935 NR 2 ENGINE EXCEEDED 960 DEGREE C DURING TAKE OFF (REACHED 962 DEGREE C FOR APPROX. 10 SECONDS W9TH AMBER EGT LIGHT) N1 WAS INDICATING 100.2 PERCENT. ABORTED THE TAKE OFF. AT IDLE NR 2 ENG 24.8 N1, 601 EGT, 66.4N2, 1700 F/F. CHECKED NR 2 ENGINE INLET AND EXHAUST. NO DAMAGE NOTED. FOUND HP VALVE AND TUBE ASSY LEAKING. REMOVED AND REPLACED HP VALVE AND TUBE ASSY. OP'S CHECK AND LEAK CHECK IAW 36-11-12 AND 72-00-00 ENGINE RUN UP (5 MINUTES) ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20041020001552004102000155WP 2004 10 20 NACA20040047 120041018A2751BZR31 WARNING SWITCH DOUG DC6 DC6B 3021712WP PWA R2800 R2800* 52026NE TE FLAPS FALSE ACTIVATIONA NACAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL037919C 43554 TAKE-OFF WARNING HORN ON TAKE-OFF ROLL. REMOVED AND REPLACED FLAP POSITION WARNING SWITCH. 2L74 4R4 R 6A4 5E8 20041020001632004102000163EA 2004 10 20 COMA0460572 120041012A261347259701 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE OVERHEAT DETECT MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01779CA125096289 7306 FLIGHT 5263 LT ENGINE JET OVERHEAT CAUTION MESSAGE. REPLACED THE FIRE/OVERHEAT CONTROL UNIT. 2L72 4F4 FRTA21EA E15NE 20041020001662004102000166WP 2004 10 20 DHL2004801536 120040913A2822112304 VOLUTE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUEL PUMP CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 1746: NR 1 MAIN TANK FEED PUMP VOLUTE CRACKED. REMOVED AND REPLACED VOLUTE ASSY ON NR 1 MAIN TANK FEED PUMP IAW MM 28-10-6 PG. 201-205. 2L74 4F4 FRT4A25 E2GL 20041020001872004102000187EA 2004 10 20 5040093004 120040930A291060075239511 LINE CNDAIRCL600 CL6002B16 1900305EA HYD SYSTEM FAILED E S4WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP07807Z 5514 5040 MAIN LANDING GEAR FAILED TO RETRACT. REPLACED NR 3 HYDRAULIC LINE P/N 600-75239-511. 2L72 4F RTA21EA 20041020002042004102000204EA 2004 10 20 VNAA0410009 120041010A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY DOOR ILLUMINATED A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL05262PS 7962 CREW REPORTED, RECEIVED A LEFT EMERGENCY DOOR CAS MESSAGE AT 25000 FEET. MAINTENANCE CONTROL DEFERRED THE LEFT EMERGENCY DOOR WARNING 57-70-3 CODE C. 2L72 4F4 FRTA21EA E15NE 20041020002062004102000206EA 2004 10 20 VNAA0410003 120041005A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO DOOR ILLUMINATED A VNAAO OTHER J WARNING INDICATION CRCRUISE 1 GL05228PS 7897 DURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE WITH NO CHANGE IN CABIN PRESSURE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CODE C 2L72 4F4 FRTA21EA E15NE 20041021000012004102100001NM 2004 10 21 ASAA0440155 120040825A5414311A1450 SKIN BOEING737 7374S3 1384711NM LT PYLON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND LEFT PYLON SKIN GOUGES. INSTALLED WEAR STRAP PER EA 5430-01135. (M) 2L72 4F RTA16WE 20041021000082004102100008NM 2004 10 21 ASAA0440147 120040816A5320BAC496377 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01765AS 25102 OAK - FOUND LOWRE FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE Z-ANGLE AFT OF DOOR CUTOUT FS 867 TO AFT BULKHEAD IS CORRODED, ALONG ENTIRE LENGTH. INSTALLED NEW Z-ANGLE ON RT AFT SIDE FROM STATION 867 TO AFT BULKHEAD, PER SRM 51-40-02 PAGES 3 AND 4 PAR B. (M) 2L72 4F RTA16WE 20041021000092004102100009NM 2004 10 21 ASAA0440143 120040730A5320BAC1496377 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 OAK - FOUND LOWR FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE RT Z-ANGLE AT FS 727 TO 787 HAS CORROSION ON THE UPPER SURFACE AT SEVERAL PLACES, MARKED IN RED. REMOVED RT Z-ANGLE AFT CARGO COMPARTMENT FS 727-787. INSTALLED NEW Z-ANGLE FROM FS 727-787. (M) 2L72 4F RTA16WE 20041021000132004102100013NM 2004 10 21 ASAA0410388 120040905A531165465692 FRAME BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND FRAME DAMAGED. REPAIRED FRAME BY INSTALLING DOUBLER. (M) 2L72 4F RTA16WE 20041021000262004102100026NM 2004 10 21 USAA040678 120040826A5311 FRAME BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BELL FRAME CRACKED .125 INCH, SIDE AIR SUPPORT RIVET STATION 908 AND S-9. DOUBLER INSTALLED PER SRM 53-60-07, FIG 201, SRM 53-00-07, FIG 201. (M) 2L72 4F RTA16WE 20041021000312004102100031NM 2004 10 21 ASAA0410395 120040911A531065671406 BEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. (M) 2L72 4F RTA16WE 20041021000482004102100048NM 2004 10 21 USAA040683 120040915A5315BAC1505100246 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US40827 24554 PIT - FOUND FLOORBEAM T-CAP CORRODED, STATION 344, LBL 12 TO RBL 12, 10 PERCENT OF .080 INCH REMOVED, THREE AREAS .020 INCH DEEP. CORROSION LEVEL 1, TASK NR C53-107-01. INSTALLED NEW T-CAP PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20041021000522004102100052NM 2004 10 21 ASAA0440154 120040825A5414311A1450 SKIN BOEING737 7374S3 1384711NM LT PYLON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND LEFT PYLON SKIN HAS GOUGES. INSTALLED WEAR STRAP PER EA 5430-01134. (M) 2L72 4F RTA16WE 20041021000582004102100058NM 2004 10 21 ASAA0410393 120040909A53136552928 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND STRINGER 19R CRACKED .250 INCH AT 2 HOLE LOCATIONS. REMOVED DAMAGED/CRACKED STRINGER, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20041021000862004102100086 2004 10 21 AALA20041042 420041008A256529985103 SLIDE DOUG DC9 DC982 3022082WP GALLEY DOOR DISCHARGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21288AA 49300 MSP - AFT GALLEY DOOR SLIDE PRESSURE OUT OF LIMITS. REPLACED SLIDE AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021000882004102100088NM 2004 10 21 AALA20041046 120041013A1420 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21680AN 29590 JFK - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 27D INOPERATIVE. SECURED CONNECTOR AT SEAT 27D FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041021000892004102100089WP 2004 10 21 AALA20041045 120041014A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217530 49922 DFW - EMERGENCY EXIT CEILING LIGHTS AT FORWARD ENTRY DOOR AND ROW 25 INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY EXIT CEILING LIGHTS AT FORWARD ENTRY DOOR AND ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021000902004102100090WP 2004 10 21 AALA20041044 120041013A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT CROSSED A AALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW21941AS 49925 DFW - EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS INOPERATIVE. FOUND CONNECTORS CROSS CONNECTED. RECONNECTED CONNECTORS FOR EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021000912004102100091NM 2004 10 21 AALA20041047 120041012A3350 SOCKET BOEING767 767323 1385205NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139364 24045 DFW - EMERGENCY LIGHT AT SEAT 39B INOPERATIVE. RESEATED SOCKET FOR EMERGENCY LIGHT AT SEAT 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041021000922004102100092NM 2004 10 21 AALA20041037 120041008A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21351AA 24032 JFK - EMERGENCY LIGHTS AT ROWS 20AB TO 24AB INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR EMERGENCY LIGHTS AT ROWS 20AB TO 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041021000932004102100093WP 2004 10 21 AALA20041028 120041007A3350 SWITCH DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959U 49704 DFW - FLIGHT ATTENDANT SWITCH WILL NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH AND AFT CARGO EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021000952004102100095NM 2004 10 21 AALA20041025 120041006A1420 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW2139356 24037 DFW - EMERGENCY ESCAPE LIGHTING CONNECTOR BROKEN AT SEAT 35AB. REPLACED EMERGENCY ESCAPE PATH LIGHTING CONNECTOR AT SEAT 25AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041021000962004102100096EU 2004 10 21 AALA20041026 120041006A3350321441 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2111060 470 JFK - EMERGENCY LIGHT EXIT SIGN AT DOOR 3L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT DOOR 3L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041021000982004102100098WP 2004 10 21 AALA20041030 120041007A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21433AA 49451 DEN - EMERGENCY LIGHTS AT AFT ATTENDANT CEILING AND AFT STAIR AREA INOPERATIVE. REPLACED BATTERY PACK AT AFT RIGHT HAND LAVATORY FOR EMERGENCY LIGHTS AT AFT ATTENDANT CEILING AND AFT STAIR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041021000992004102100099WP 2004 10 21 AALA20041031 120041007A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21433AA 49451 DEN - CEILING EMERGENCY LIGHTS FROM SEATS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20DEF FOR CEILING EMERGENCY LIGHTS FROM SEATS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041021001002004102100100WP 2004 10 21 AALA20041029 120041007A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21482AA 49675 DFW - EMERGENCY ESCAPE PATH LIGHTING IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHTING IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021001012004102100101NM 2004 10 21 AALA20041038 120041009A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21362AA 24043 LAX - LEFT AFT EXTERIOR EMERGENCY LIGHTS INOPERTIVE. REPLACED BATTERY PACK FOR LEFT AFT EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041021001032004102100103WP 2004 10 21 AALA20041049 120041015A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21494AA 49732 SFO - EMERGENCY LIGHTS AT RIGHT HAND FORWARD EMERGENCY EXIT OVERWING DOOR AND LEFT HAND SERVICE DOOR CEILING INOPERATIVE. REPLACED BATTERY PACK B5103 (6011779 FROM HONEYWELL) AND B5107 (60030451 FROM HONEYWELL). SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021001052004102100105NM 2004 10 21 AALA20041051 120041015A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21797AN 30012 LAX - EMERGENCY ESCAPE PATH LIGHT AT ROWS 30 TO 44CEF INOPERATIVE. REPAIRED FAULTY WIRING AT CONNECTOR D3204J AND REPLACED BATTERY PACKS AT POSITIONS M33406 AND M33404 FOR EMERGENCY ESCAPE PATH LIGHTING AT ROWS 30 TO 44CEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041021001072004102100107NM 2004 10 21 AALA20041053 120041017A2810 CAP BOEING757 757223 1384957NM FUEL STORAGE LEAKING A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21611AM 24487 MIA - INFLIGHT T671/17 RIGHT HAND WING FUEL LEAK. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED CAP AND O-RING FOR RIGHT HAND FUEL TANK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041021001092004102100109 2004 10 21 AALA20041055 420041016A2565D30656126 SLIDE BOEING757 757223 1384957NM CABIN DOOR FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21647AM 24605 MIA - CABIN SERVICES CONTRACTOR INADVERTANTLY DEPLOYED SLIDE WHILE OPENING L4 DOOR. SLIDE DROPPED OUT AND DOOR ASSIST BOTTLE DISCHARGED BUT SLIDE FAILED TO INFLATE. REPLACED SLIDE AND RESERVOIR FOR EMERGENCY SLIDE AT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041021001112004102100111NM 2004 10 21 SWAA043033 120041019A33506556633 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED C3 CHECK, FOUND OVERHEAD OVERWING EMERGENCY EXIT LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041021001132004102100113NM 2004 10 21 SWAA043035 120041019A53206546568 STRAP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD STRAP AT BS 1016, RBL 2, WL 208, CORRODED. REMOVED AND REPLACED STRAP PER SRM. 2L72 4F RTA16WE 20041021001152004102100115NM 2004 10 21 SWAA042991 120041016A2121215201 FAN BOEING737 7373H4 1384600NM E&E BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29394SW 27380 APPROX 8 MINUTES BEFORE LANDING PAX REPORTED SMELLED SMOKE. AFTER ENGINE SHUTDOWN AT THE GATE SMELL GOT WORSE, IT WAS A STRONG ACRID SMELL. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20041021001172004102100117NM 2004 10 21 SWAA042993 120041016A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 410, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041021001202004102100120NE 2004 10 21 AALA20041061 220041015A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LEFT INOPERATIVE A AALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW21266AA 49291 ACT - T/323 EN ROUTE DFW - PVR LEFT HAND ENGINE COMPRESSOR STALLS AND HIGH EGT. LANDED ACT WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE. 2L72 4F4 F A6WE E9NE 20041021001222004102100122NM 2004 10 21 SWAA043026 120041018A53106546818 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 747 TO BS 867, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2L72 4F RTA16WE 20041021001242004102100124NM 2004 10 21 SWAA042968 120041012A2121215201 FAN BOEING737 7375H4 138449DNM E/E BAY FAULTY A SWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29512SW 24189 AIR TURNBACK, F/A AND PAX COMPLAINED OF BURNING SMELL. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20041021001322004102100132NM 2004 10 21 SWAA042978 120041013A335065CD27093 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29771SA 27879 DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20041021001342004102100134NM 2004 10 21 SWAA042998 120041016A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 312, STRINGER 25R, BS 386, STRINGER 17R, BS 390, STRINGER 17R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041021001362004102100136NM 2004 10 21 SWAA043000 120041016A575465C26603138A WEDGE BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM. 2L72 4F RTA16WE 20041021001382004102100138 2004 10 21 SWAA042979 420041014A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041021001402004102100140 2004 10 21 SWAA042981 420041014A256565C16820 HOOK BOEING737 7373H4 1384600NM R1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE FWD GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20041021001422004102100142NM 2004 10 21 SWAA042983 120041014A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 813, STRINGER 19L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041021001442004102100144NM 2004 10 21 SWAA043002 120041016A335065C27093 LIGHT BOEING737 7373H4 1384600NM EMERGENCY EXIT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041021001452004102100145GL 2004 10 21 YTRR096993 220040819A73202549170 GOVERNOR BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE MALFUNCTIONED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW09913RL66 2913 THE GOVERNOR WAS INSTALLED AND AFTER 65.8 HOURS N2 WAS NOT ADJUSTABLE ABOVE 97 PERCENT. THE GOVERNOR WAS REPLACED AND THE PROBLEM DISAPPEARED. 1G71 3U3 U H2SW E4CE 20041022000012004102200001SO 2004 10 22 SWIA200413958 120041005A2730 PUSHROD EMB 120 EMB120ER 3260203SO ELEVATOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 BOTH LEFT AND RIGHT ELEVATOR PUSH RODS AT ELEVATORS HAVE CORRODED ROD ENDS AND ASSOCIATED HARDWARE. ITEM FOUND AT C-CHECK INSPECTION. BOTH LT AND RT ELEVATOR PUSHROD ROD ENDS AND HARDWARE REPLACED IAW 27-31-04. 2L72 4T RTA31SO 20041022000022004102200002EA 2004 10 22 SWIA200413983 120041015A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07720SW 7297 CLIMBING OUT OF FCA CO-PILOTS STAB TRIM SWITCH RAN AWAY TO A VALUE OF 1.0 NOSE DOWN WITH NO RESPONSE WHEN TRIMMING TO THE NOSE UP POSITION. REPLACED CO-PILOTS STAB TRIM SWITCH P/N 309-4334. OPERATIONAL CHECK GOOD IAW 27-41-05. 2L72 4F RTA21EA 20041022000042004102200004SO 2004 10 22 MASA200400557 120041002A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07839MJ 145416 ASH 2706 DCA, CREW REPORTED THE AFT CEILING EMERGENCY LIGHT INOP. MAINTENANCE RESECURED THE LIGHT ASSEMBLY AND PERFORMED OPS CHECKS. 2L72 4T RTT00011AT 20041022000062004102200006SO 2004 10 22 MASA200400558 120041002A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 ASH 2834 CLT, FLOOR STRIP EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOP. MAINTENANCE REPLACED THE STRIP LIGHT AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20041022000082004102200008EA 2004 10 22 SWIA200413912 120041011A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07913SW6778 6778 7597 SPOILERONS FAULT STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW MM 27-60-00. 2L72 4F RTA21EA 20041022000092004102200009SO 2004 10 22 SWIA200413913 120041010A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07292SW9852 9852 120319 FLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT NACELLE FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000102004102200010SO 2004 10 22 SWIA200413914 120041012A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07294SW6343 6343 120321 FLAP CENTRAL FAULT ON RETRACTION. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000122004102200012EA 2004 10 22 SWIA200413916 120041010A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM DIRTY A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07445SW 7651 MACH TRIM AND STAB TRIM CAUTION MESSAGES INFLIGHT AT CRUISE ALTITUDE. CLEANED PILOTS SIDE SWITCH. PERFORMED TEST OF HSTCU, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000132004102200013EA 2004 10 22 SWIA200413917 120041008A2721 CONTROL KNOB CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM STUCK A SWIAL ABORTED APPROACH F FLT CONT AFFECTED NRNOT REPORTED 1 NM07432SW 7548 LEFT RUDDER TRIM KNOB STICKS ALLOWING TRIM TO RUN TO FULL DEFLECTION. INSTALLED SERVICEABLE AILERON/RUDDER TRIM PANEL IAW 27-00-07, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000142004102200014SO 2004 10 22 SWIA200413918 120041011A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0757734 120199 F/A REPORTS EMERGENCY LIGHT INOPERATIVE ON RIGHT SIDE OF AIRCRAFT. RELAMPED EMERGENCY LIGHT ON RIGHT SIDE OF AIRCRAFT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000152004102200015SO 2004 10 22 SWIA200413919 120041002A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07232SW 120306 EMERGENCY FLOOR LIGHTING SYSTEM HAS ONE BULB INOPERATIVE. REMOVED AND REPLACED BROKEN SPLICE WITH NEW ENVIRONMENTAL SPLICE, OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041022000172004102200017EA 2004 10 22 MASA200400559 120041002A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA LT OVERWING INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717337 7337 ASH 6154 PHX, PILOT REPORTED A RT OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT LIGHT. 2L72 4F RTA21EA 20041022000182004102200018SO 2004 10 22 MASA200400568 120041006A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07826MJ 145214 ASH 2802 CLT - IAD, THE CREW REPORTED THE THIRD EMERGENCY CEILING LIGHT AFT OF FORWARD BULKHEAD IN CABIN INOPERATIVE. THE LIGHT WAS RELAMPED AND OPERATIONALLY CHECKED GOOD. 2L72 4T RTT00011AT 20041022000192004102200019EA 2004 10 22 MASA200400573 120041010A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07715SF 7115 ASH 2605 BOS, LEFT ROW 2 OVERHEAD EMERGENCY LIGHT INOP. LIGHT WAS DEFERRED PER MEL 33-51-01-1. MAINTENANCE RESECURED CONNECTOR OPS CHECKED GOOD. 2L72 4F RTA21EA 20041022000202004102200020EA 2004 10 22 MASA200400576 120041012A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 ASH 6264 FROM PHX-SAN, THE FORWARD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT AND IT OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20041022000242004102200024EA 2004 10 22 SWIA200413977 120041018A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07945SW 7770 RIGHT SIDE WINDOW CRACKED. REMOVED AND REPLACED RIGHT SIDE COCKPIT WINDOW PER CRJ 200 MM 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R-33033-12, S/N OFF 02328H1890. 2L72 4F RTA21EA 20041022000252004102200025EA 2004 10 22 SWIA200413978 120041017A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07927SW4820 4820 7693 FLT SPOILERS FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED SPOILER ELECTRONIC CONTROL UNIT IAW 27-60-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000322004102200032EA 2004 10 22 SWIA200413940 120041016A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY INOPERATIVE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07416SW 7089 REAR CARGO SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000332004102200033SO 2004 10 22 SWIA200413941 120041014A5210 ROLLER EMB 120 EMB120ER 3260203SO PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07290SW 120317 PAX DOOR IS HARD TO OPEN (UNLOCK). ADJUSTED PAX DOOR ROLLERS IAW EMB 120 MM 52-11-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000342004102200034EA 2004 10 22 SWIA200413842 120040913A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07455SW 7760 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00, RBL 9.0 INBOARD AND OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, AND 51-21-11. 2L72 4F RTA21EA 20041022000352004102200035EA 2004 10 22 SWIA200413843 120040913A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07455SW FUSELAGE PULLEY INTERCOSTAL HAS A CRACK ON OUTBOARD RETURN FLANGE; LEFT SIDE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117. REV "B". 2L72 4F RTA21EA 20041022000362004102200036EA 2004 10 22 SWIA200413844 120040913A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07455SW CARGO PIT AFT BULKHEAD FLOOR ANGLE CRACKED; FS 621.00 RBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20041022000412004102200041EA 2004 10 22 SWIA200413972 120041005A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW EVIDENCE OF CORROSION FOUND ON INSIDE OF PAX DOOR FROM FS 310.00 TO FS 349.00 AT STR 16P. ITEM FOUND AT C-CHECK INSPECTION. THREE SUPPORT ANGLES REPLACED IAW CRJ SRM 51-40-11 AND 51-42-06. 2L72 4F RTA21EA 20041022000422004102200042SO 2004 10 22 SWIA200413959 120041005A4910 MOUNT EMB 120 EMB120ER 3260203SO APU CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 LOWER ROD ENDS ON UPPER APU MOUNT SUPPORT RODS SEVERELY CORRODED. ITEM FOUND AT C-CHECK INSPECTION. ROD ENDS REPLACED. REF. 49-11-02. 2L72 4T RTA31SO 20041022000432004102200043EA 2004 10 22 SWIA200413960 120041005A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 STA 280, LBL, OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, 51-25-16, 51-21-11. 2L72 4F RTA21EA 20041022000442004102200044EA 2004 10 22 SWIA200413961 120041005A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 STA 280, RBL, BOTH INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00, 51-42-21, 51-25-16, AND 51-21-11. 2L72 4F RTA21EA 20041022000482004102200048EA 2004 10 22 SWIA200413778 120040830A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07941SW AFT EQUIPMENT COMPARTMENT INTERCOSTAL ANGLE CRACKED; FS 625.00; STR 14R. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2L72 4F RTA21EA 20041022000502004102200050EA 2004 10 22 SWIA200413780 120040903A2780 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07708SK 10156 SLATS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED NR 2 SFECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000512004102200051EA 2004 10 22 SWIA200413781 120040903A3350 BULB CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07703SK 10139 RIGHT OVERWING EXIT LOWER EMERGENCY LIGHT INOP. RELAMPED LOWER EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000542004102200054EA 2004 10 22 SWIA200413774 120040906A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07410SW7407 7407 7066 FIRST FLIGHT OF DAY TRIM CHECK, STAB TRIM 2 FAILED. REMOVED AND REPLACED BOTH HST AND MOTOR CONTROL UNIT IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 597. 2L72 4F RTA21EA 20041022000562004102200056SO 2004 10 22 SWIA200413921 120041011A27523203001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07268UE9774 9774 120207 FLAP CONTROL FAULT WITH THE INBOARD PAIR FLASHING. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000622004102200062EA 2004 10 22 SWIA200413852 120040923A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07423SW1053410534 7456 AFTER ENGINE START SPOILERONS STATUS MESSAGE. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041022000632004102200063GL 2004 10 22 YTRR096991 220040824A732023078029 HYDROMECH UNIT BELL 407 407 1182206SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW09594RL500 53594 CAE847645 AIRCRAFT REPORTED A PLA HARD FAULT THAT WAS TRACED DOWN TO THE HMU. HMU SENT TO ROLLS ROYCE FOR INSPECTION. 1G71 3U3 UO H2SW E1GL 20041022000642004102200064NM 2004 10 22 P5CA0401245 120041011A5730 PANEL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RIGHT WING I/B FIXED T/E LWR PNL, I/B EXTENDED CHORD HAS CRACK 2 INCHES LONG AT WS 440. REMOVE CHORD INSTALLED NEW CHORD AS PER SRM 51-30-02. 2L74 4F4 F A20WE E20EA 20041022000652004102200065NM 2004 10 22 P5CA0401246 120041011A5311 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 MAIN DECK CEILING AREA FRAME WEB STA 960 STR 5R CRACKED. STOP DRILL CRACK PER SRM 51-30-02, 53-10-04, 51-00-00. 2L74 4F4 F A20WE E20EA 20041022000662004102200066NM 2004 10 22 P5CA0401247 120041011A5313 STRINGER BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FUSELAGE STRINGER AT 10R HAS CRACK B/W STA 1372-1392. REMOVED DAMAGE AREA, REPLACED WITH NEW STRINGER AS PER SRM 53-10-03. 2L74 4F4 F A20WE E20EA 20041022000672004102200067NM 2004 10 22 P5CA0401248 120041011A5522 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RIGHT I/B ELEVATOR LWR SURFACE SKIN HAS DELAMINATION. REMOVED DAMAGE AREA, INSTALLED NEW PER SRM 51-40-04. 2L74 4F4 F A20WE E20EA 20041022000702004102200070CE 2004 10 22 GLBA20030690 120040806A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03150GL UE150 CRACK ON FUSELAGE FS 150.60. REPAIRED CRACK. 2L72 4T RTA24CE 20041022000742004102200074NM 2004 10 22 RYNA2075 120040327A2820MS29513330 O-RING BOEING757 757200 1384950NM FUEL SYSTEM FAULTY A RYNAO OTHER O OTHER NRNOT REPORTED 1 CE07929RD 23929 DURING CRUISE FLIGHT (FUEL CONFIG) LIGHT ILLUMINATED AND THE EICAS ADVISORY MESSAGE (FUEL CONFIG) WAS DISPLAYED. ACCOMPLISHED THE FUEL CONFIGURATION CPM PROCEDURES AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MANIFOLD (O-RING) IN PYLON AT STATION 287.9. LEAK CHECK NORMAL. 2L72 4F RTA2NM 20041022000752004102200075CE 2004 10 22 4018 120040804A2612 WARNING LIGHT CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL FIRE LOOP FALSE ACTIVATIONE BSYAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07108AN 208B0975 PCEPC0988 011015 ON TAKEOFF OUT OF BTR HAD ENGINE FIRE DETECT LIGHT COME ON, ABORTED TAKEOFF. MAINT CHECKED FOR BLEED AIR LEAKS, CHECKED FIRE LOOP FOR RUBBING NO DEFECTS NOTED, RAN AIRCRAFT AT FULL POWER COULD NOT DUPLICATE FIRE LIGHT. 1H71 3T3 T A37CE E4EA 5 CP60GL 20041022000772004102200077GL 2004 10 22 YTRR097021 220040825A732023070606 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED B YTRAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW0965DD 1235 ENGINE WOULD NOT ACCELERATE ABOVE IDLE. REPLACEMENT OF THE FUEL CONTROL UNIT ALEVIATED THE PROBLEM. THE FUEL CONTROL WAS OVERHAULED. 1G71 3U3 U H2SW E1GL 20041025000012004102500001EA 2004 10 25 MASA200400462 120040818A335020131A BATTERY PACK CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT DISCHARGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07918FJ 15018 ASH 6268 PHX, EMERGENCY LIGHTS WERE LEFT ON. MAINTENANCE TROUBLESHOT AND FOUND THE BATTERIES DRAINED. MX REPLACED THE EMERGENCY BATTERIES. OPS CHECK GOOD. S/N OFF 85536, 85547, 85524 AND 85533. 2L72 4F RTA21EA 20041025000032004102500003EA 2004 10 25 SWIA200413853 120040922A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07447SW 7677 AT ALTITUDE HAD STAB TRIM AND MACH TRIM CAUTION LIGHTS COME ON. REMOVED AND REPLACED THE CAPTAINS TRIM DISCONNECT SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000082004102500008EA 2004 10 25 SWIA200413901 120041010A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07408SW 7055 RIGHT WINDSHIELD SHATTERED. REMOVED AND REPLACED RIGHT WINDSHIELD ASSY IAW MM 56-11-01. P/N OFF NP-139321-10, S/N OFF 01208144243. 2L72 4F RTA21EA 20041025000092004102500009 2004 10 25 SWIA200413889 420041001A22166225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER SERVO MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07586SW1033010330 120354 LEFT RUDDER PEDAL FEELS LIKE IT IS SCRAPING SOMETHING. REPLACED RUDDER SERVO. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041025000112004102500011EU 2004 10 25 TXER096973 120040716A6410355A12004008 BLADE AEROSPAS355 AS355* EU TAIL ROTOR DELAMINATED B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09151TA3000 2601 TAIL ROTOR BLADE HAS DELAMINATION. 1G72 3U H11EU 20041025000122004102500012EA 2004 10 25 SWIA200413785 120040906A2750601R930045 LEVER CNDAIRCL600 CL6002B19 1900309EA FLAP CONTROL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07964SW RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED FLAP SELECTOR HANDLE. OPERATIONAL CHECK GOOD. P/N 601R93004-5, S/N OFF 0654. 2L72 4F RTA21EA 20041025000152004102500015EA 2004 10 25 SWIA200413788 120040910A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DIRTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07417SW 7400 FLIGHT ATTENDANT COULD NOT OPEN MAIN CABIN DOOR FROM INSIDE AIRCRAFT. CLEANED AND REMOVED DEBRIS FROM FUSELAGE CUTOUT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000172004102500017 2004 10 25 SWIA200413790 420040908A22156225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07226SW 120296 DURING FLIGHT RUDDER TRIM WILL DEFLECT THE BALL HALFWAY OUT OF CENTER UNCOMMANDED. REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-11-00. 2L72 4T RTA31SO 20041025000182004102500018 2004 10 25 SWIA200413791 420040906A22156225734002 SERVO EMB 120 EMB120ER 3260203SO ELEVATOR WEAK A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07587339345 9345 120197 ELECTRIC TRIM WEAK ABOVE 180 KNOTS INDICATED AIRSPEED. REMOVED AND REPLACED ELECTRIC TRIM (ELEVATOR) SERVO IAW 27-32-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000202004102500020EA 2004 10 25 SWIA200413793 120040909A2750 POTENTIOMETER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF ADJUST A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07405SW 7029 RIGHT FLAP INDICATES 22 DEGREES AT 20 DEGREE SETTING. ADJUSTED RIGHT FLAP POSITION POTENTIOMETER IAW MM 27-55-01. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041020000062004102000006NM 2004 10 20 ASAA0410379 120040819A5310BAC1489233 SHEAR TIE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 26L AND 27L. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM. (M) 2L72 4F4 FRTA16WE E2EA 20041020000092004102000009NM 2004 10 20 ASAA0410376 120040816A33508821004 BATTERY PACK BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 FOUND RT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FUSES IN AFT BATTERY PACK. (M) 2L72 4F4 F A16WE E2EA 20041020000102004102000010NM 2004 10 20 ASAA0410371 120040813A71606585378202 COWLING BOEING737 737200 1384453NM PWA JT8 JT8D17 52049NE NR 2 ENG NOSE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND NR 2 ENGINE NOSE COWL AFT LIP REPAIR WORN/DENTED. REMOVED AND REPLACED LOWER AFT CAP. (M) 2L72 4F4 F A16WE E2EA 20041020000192004102000019NM 2004 10 20 ASAA0410370 120040812A33508821004 BATTERY PACK BOEING737 737298C 1384490NM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - FOUND RIGHT OVERWING EMERGENCY EXIT LOWR INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT BATTERY PACK ASSEMBLY PER AMM. (M) 2L72 4F RTA16WE 20041020000202004102000020NE 2004 10 20 ASAA0440153 220040818A7200 ENGINE BOEING737 7374Q8 138447QNM GE CFM56 CFM56* 13802NE UNKNOWN MALFUNCTIONED A ASAAEA ENGINE SHUTDOWN UNSCHED LANDING ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 NM01771AS 25104 857283 EN ROUTE AT 31,000 FT, CREW FELT BUMP AND VIBRATION LASTING LESS THAN A MINUTE. ALL ENGINE GAUGED AND SYSTEMS WERE NORMAL. EVERYTHING SMOOTHED OUT. LATER, WHILE DESCENDING THROUGH 10,000 FT, ENGINE EXPERIENCED COMPRESSOR STALL WITH SEVERE VIBRATION. CREW SHUT DOWN ENGINE FOLLOWING QRC/QRH PROCEDURES AND ACCOMPLISHED SINGLE ENGINE LANDING. REMOVED AND REPLACED ENGINE. (M) 2L72 4F4 FRTA16WE E2GL 20041020000242004102000024EU 2004 10 20 A6WA200460041 120040921A5310 GUSSET BAC 146 146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 AIRBRAKE STRUCTURE AFT OF FRAME 50 RIGHT SIDE GUSSET CRACKED. REPAIR IN PROGRESS. (M) 2H74 4F A49EU 20041020000262004102000026NM 2004 10 20 ASAA0410381 120040821A534069353521 STRINGER CLIP BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - CORROSION FOUND ON STRINGER CLIP. REMOVED DAMAGE, FABRICATED AND INSTALLED STRINGER CLIP. (M) 2L72 4F RTA16WE 20041020000272004102000027NM 2004 10 20 ASAA0410368 120040808A33508821004 BATTERY PACK BOEING737 737290C 138448VNM EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - FOUND SMOKE BARRIER LIGHT INOPERATIVE FOR EMERGENCY EXIT. INSTALLED SERVICEABLE BATTERY, OPS CHECK OK. (M) 2L72 4F A16WE 20041020000312004102000031NM 2004 10 20 UIEA200400173 120040921A5730 SKIN BOEING747 747230B 1384889NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, FOUND CORROSION ON LEFT WING TOP SKIN UPPER SURFACE AT APPROXIMATELY WBL 143, JUST FORWARD OF STRINGER 30. THE CORROSION WAS REMOVED BY BLENDING. HFEC INSPECTED THE SKIN SURFACE TO ENSURE DAMAGE AND DEFECT FREE. FLAP PEEN THE BLENDED AREA AND PROTECTIVE FINISH APPLIED. CORROSION INHIBITING COMPOUNDS WERE APPLIED TO THE REWORKED AREA. (M) 2L74 4F A20WE 20041020000362004102000036NM 2004 10 20 USAA040578 120040820A5320 STRAP BOEING757 757225 1384959NM STABILIZER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19604AU62264 22199 CLT - FOUND STABILIZER STRAP CRACKED .5 INCH, STATION 560, SECTION 43, LBL 15. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M) 2L72 4F RTA2NM 20041020000432004102000043EU 2004 10 20 A6WA200460043 120040921A5280 SKIN BAC 146 146200A 1500266EU LT MLG DOOR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31181US E2042 FOUND LEFT MLG DOOR HAS A CRACK ON FORWARD CUT OUT FOR THE SIDE STAY ON INNER SKIN ON LOWER FORWARD CORNER OF DISHED SKIN, REPAIR IN PROGRESS. (M) 2H74 4F A49EU 20041020000672004102000067EA 2004 10 20 A6WA200440129 120040908A2910 MANIFOLD CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401AW 7280 HYDRAULIC 3B RUNS CONTINUOUSLY EVEN WITH SWITCH IN OFF POSITION AND CIRCUIT BREAKER PULLED HYDRAULIC QUANTITY DURING FLT WAS 95 PERCENT. REMOVED AND REPLACED PRESSURE MANIFOLD ASSEMBLY FOR ACMP HYD SYSTEM NR 3 A/B IAW AMM 29-12-05. (M) 2L72 4F RTA21EA 20041020000712004102000071NM 2004 10 20 USAA040666 120040830A5510 BUSHING BOEING737 7373B7 1384580NM HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND BUSHING CORRODED .25 INCH BY .25 INCH AREA, RIGHT HORIZ STAB R10 LUG. MADE NEW BUSHING AMS 4640 PER SRM 55-10-10. (M) 2L72 4F RTA16WE 20041020001082004102000108NM 2004 10 20 USAA040508 120040819A5320 WEB BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND WEB CRACKED .25 INCH LONG, STATION 1040 BL 0 JUST ABOVE CENTER PLUG OF PRESSURE WEB. MANUFACTURED REPAIR DOUBLER AND FILLER, PLATE/DOUBLER PER SRM 53-80-08 FIG 201. (M) 2L72 4F RTA16WE 20041020001152004102000115NM 2004 10 20 USAA040643 120040831A53201137215 STIFFENER BOEING737 7373B7 1384580NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 PIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BETWEEN STATION 312-328 RBL 11. REPLACED STIFFENER PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M) 2L72 4F RTA16WE 20041020001222004102000122NM 2004 10 20 USAA040603 120040917A5320 STIFFENER BOEING757 7572B7 1384964NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU39019 27148 CLT - FOUND STIFFENER CORRODED 1 INCH, STATION 324 TO 418, BL 0. REPLACED STIFFENER PER SRM 51-10-02. (M) 2L72 4F RTA2NM 20041020001282004102000128NM 2004 10 20 371PA0053 120040920A5320 ANGLE BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 THRESHOLD Z-ANGLE AT L2 DOOR HAS CORROSION AT CLIP NUT HOLES. REPLACED Z-ANGLE PER DWG. 65-52878497. 2L72 4F4 FRTA16NE E2GL 20041020001322004102000132NM 2004 10 20 371PA0066 120040913A5320 ANGLE BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 CORROSION ON RIGHT TRANSIT IN ANGLE BETWEEN BS 867 AND BS 902. REPAIRED IAW SRM 53-60-53 AND SRM 51-10-02. 2L72 4F4 FRTA16NE E2GL 20041020001482004102000148NM 2004 10 20 C8GA20040022 120041001A2150 DUCT BOEING727 727230 1384080NM PWA JT8 JT8D15 52051NE AC PACK LOOSE A C8GAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO15357KP 20675 FLT 705 CLEARED FOR TAKEOFF, A LOUD BANG WAS HEARD AT 1.4 EPR CHECK. TAXI CLEAR OF RUNWAY AND PERFORMED A SECOND CHECK ON THE DE-ICE PAD WITH SAME RESULTS. AIRCRAFT RETURNED TO RAMP AND UPON INSPECTION FOUND THE PRESSURE RELIEF VALVE ON PACK DISTRIBUTION DUCT LOOSE. ADJUSTED THE SAME, RAN ENGINES WITH NO TROUBLE FOUND AND PACKS OPERATED NORMAL IAW MM 21-21-0 AND 72-00. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041020001502004102000150NM 2004 10 20 371PA0067 120040914A5320 SCUFF PLATE BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FWD CARGO DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FWD AND AFT SCUFF PLATES OF FWD CARGO DOOR CUTOUT CRACKED IN RADIUS. REPAIRED IAW MFG PROCESS SPEC. 5975, 8.6. 2L72 4F4 FRTA16NE E2GL 20041020001612004102000161EA 2004 10 20 04288690 120041014A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LAV SMOKE DETECTILLUMINATED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27690BR 7739 EVENT SUMMARY STATES ABORTED TAKE OFF FOR LAV SMOKE MSG. C/W HES REJECTED TAKEOFF INSP CHECK IAW MM 05-51-27. NFF PERFORMED POWER CYCLING OF ENGINES, PACKS AND REVERSERS. ALL FUNCTIONS OPERATE NORMAL REF 71-00-00 AND 21-51-00. 2L72 4F4 FRTA21EA E15NE 20041020001652004102000165EA 2004 10 20 04289703 120041015A2120 SMOKE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LAVATORY DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27703BR 7467 EVENT SUMMARY STATES SMOKE INDICATION/ODOR IN LAV, RTF. IN APPR STATUS. 2L72 4F4 FRTA21EA E15NE 20041020001712004102000171WP 2004 10 20 DHL2004801526 120040904A5711 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT WING CENTER L/E UPPER FORMER CRACKED 0.500, STA XFS 366.500. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1, SRM 57-2-0 PG. 9-10 2L74 4F4 FRT4A25 E2GL 20041020001992004102000199CE 2004 10 20 N210TM1 120041007A3232MS20392119 CLEVIS PIN CESSNA CESSNA210 210 2073402CE CONT O470 IO470* 17026SO UPLOCK ACTUATOR FAILED E XVQAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 SO17210TM 60 57172 NOSE GEAR FAILED TO EXTEND DUE TO BROKEN CLEVIS PIN IN NOSE GEAR UPLOCK SYSTEM. 1H71 3O3 ORT3A21 E1CE 20041021000052004102100005NM 2004 10 21 ASAA0440156 120040825A5320655384425 FLOOR SUPPORT BOEING737 7374S3 1384711NM FS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT CORRODED. REPLACED SECTION OF FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20041021000102004102100010NM 2004 10 21 ASAA0440145 120040731A531069407128 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT BILGE STATION 927-947 RT SHEAR TIE CORRODED. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE. (M) 2L72 4F RTA16WE 20041021000122004102100012NM 2004 10 21 ASAA0440163 120040904A531065479573 DOOR FRAME BOEING737 7374S3 1384711NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND AFT CARGO COMPARTMENT DOOR JAMB WEB IS CORRODED. REPLACED WEB. (M) 2L72 4F RTA16WE 20041021000182004102100018EA 2004 10 21 ASOA04754 120040927A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING A C-CHECK IN MCN, THE FORWARD BRACKET ON THE LEFT FUSELAGE FRAME FS 718, STRINGER 10-11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT FUSELAGE FRAME FS 718, STRINGER 10-11 IAW ASA EO 600-53-0066. (M) 2L72 4F RTA21EA 20041021000252004102100025NM 2004 10 21 USAA040687 120040909A5210507945272 SKIN BOEING737 7374B7 1384702NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FORWARD ENTRANCE DOOR CRACKED TWO PLACES .25 INCH EACH, INTERIOR DOOR SKIN AT 1ST AND 2ND DOOR STOPS. INSTALLED DOUBLER PER TR 52-10-16. (M) 2L72 4F RTA16WE 20041021000352004102100035NM 2004 10 21 USAA040681 120040916A575465C26602223 SKIN BOEING737 7374B7 1384702NM NR 2 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND NR 2 SLAT WITH 4 CRACKS .125 INCH, TWO .375 INCH CRACKS AND .0625 INCH CRACK, 4 RIVET HOLES, LOWER SKIN UNDER ACTUATOR ATTACH AREA. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01 FIG 206. (M) 2L72 4F RTA16WE 20041021000392004102100039NM 2004 10 21 USAA040686 120040909A5320 SPLICE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND STRINGER SPLICE CRACKED .25 INCH, STATION 908 AND STRINGER 4L. INSTALLED NEW SPLICE PER SRM 51-40-02 AND 51-40-03. (M) 2L72 4F RTA16WE 20041021000412004102100041NM 2004 10 21 ASAA0410389 120040905A534069366001 STRINGER CLIP BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A K NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND STRINGER HAS MECHANICAL DAMAGE TO STRINGER CLIP. REMOVED DAMAGED STRINGER CLIP, FABRICATED NEW STRINGER CLIP AND INSTALLED. (M) 2L72 4F RTA16WE 20041021000432004102100043NM 2004 10 21 USAA040693 120040910A5311 FRAME BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - FOUND FRAME CRACKED .5 INCH, FRAME BS 727F, S8L, S9L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER PER SRM 53-00-07, FIG 202. (M) 2L72 4F RTA16WE 20041021000462004102100046NM 2004 10 21 ASAA0440161 120040902A5414313A1200106 SKIN BOEING737 7374S3 1384711NM RT PYLON GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FOUND RIGHT PYLON SKIN GOUGED AT OUTBOARD NACELLE. BLENDED GOUGE AND INSTALLED WEAR STRIP. (M) 2L72 4F RTA16WE 20041021000492004102100049NM 2004 10 21 ASAA0440164 120040911A533065C323654 SKIN BOEING737 7374S3 1384711NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01786AS 24795 OAK - FUSELAGE EXTERNAL STATION 540-1016 AT FS 837 BELOW AFT PIT DOOR REQUIRES REPLACEMENT PER EM 5330-01579, STEP 8. REMOVED EXTERNAL SKIN LAP JOINT REPAIR AT FS 837, STRINGER 25R BELOW AFT CARGO DOOR. ACCOMPLISH INTERIM REPAIR PER EA. PERM REPAIR TO BE ACCOMPLISHED WITHIN 6000 FLT CYCLES OR SEPT 2006 WHICH EVER OCCURS FIRST. (M) 2L72 4F RTA16WE 20041021000532004102100053NM 2004 10 21 ASAA0440148 120040813A5320BAC1496377 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01765AS 25102 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT, BILGE Z-ANGLE FROM STATION 727 RT TO CARGO DOOR HAS CORROSION, STATION 767. REMOVED AND REPLACED AFT CARGO Z-ANGLE FROM STATION 727 TO RT CARGO DOOR STATION 767 RT SIDE. (M) 2L72 4F RTA16WE 20041021001022004102100102WP 2004 10 21 AALA20041039 120041010A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21559AA 53089 ATL - EMERGENCY EXIT SIGNS OVER ROW 20AB AND 20DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGNS OVER ROWS 20AB AND 20DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021001312004102100131NM 2004 10 21 SWAA042975 120041013A53116545632 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041021001332004102100133NM 2004 10 21 SWAA042997 120041016A5330654576653 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 273, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041021001352004102100135 2004 10 21 SWAA042999 420041016A25656557463 GIRT BAR BOEING737 7373H4 1384600NM L1 DOOR SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR FWD FLOOR ANCHOR LOOSE. REMOVED AND REPLACED FLOOR ANCHOR PER MM. 2L72 4F RTA16WE 20041021001372004102100137NM 2004 10 21 SWAA043001 120041016A57536546435335 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20041021001392004102100139NM 2004 10 21 SWAA042980 120041014A53126517582 STIFFENER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SPV, FOUND 5 EACH CRACKS ON BULKHEAD VERTICAL BEAM WEB AT BS 178, LBL 5.7 TO RBL 17.1. REMOVED AND REPLACED BEAM WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20041021001412004102100141 2004 10 21 SWAA042982 420041014A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041021001432004102100143NM 2004 10 21 SWAA042984 120041014A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 486, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041021001462004102100146GL 2004 10 21 YTRR096994 220040819A732123070606 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE MALFUNCTIONED B YTRAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW09913RL8643 2913 FUEL CONTROL WAS OVERHAULED. INSTALLED AND AFTER 164.1 TSO THE START ACCELERATE COULD NOT BE ADJUSTED AND THE ENGINE WOULD HANG AT 60 PERCENT N1 AND COULD NOT BE INCREASED FURTHER. 1G71 3U3 U H2SW E4CE 20041022000052004102200005EA 2004 10 22 SWIA200413910 120040927A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07945SW CARGO COMPARTMENT FLOOR ATTACH ANGLE IS CRACKED; FS 621.00 LBL 38.0. ITEM FOUND AT C-CHECK INSPECTION. CRACKED ATTACH ANGLE REPAIRED IAW CRJ REO #601R-53-61-117. REV "B". 2L72 4F RTA21EA 20041022000112004102200011EA 2004 10 22 SWIA200413915 120041011A274170608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07909SW7455 7455 7558 STAB TRIM CH2 AND MACH TRIM WILL NOT ENGAGE. REPLACED HSTCU, OPERATIONAL CHECK GOOD IAW 27-41-01. 2L72 4F RTA21EA 20041022000212004102200021EA 2004 10 22 SWIA200413920 120041005A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY FALSE ACTIVATIONA SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07433SW 7550 SMOKE CARGO ILLUMINATED ON GROUND. REMOVED AND REPLACED NR 2 SMOKE DETECTOR IAW 26-15-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000222004102200022EA 2004 10 22 SWIA200413975 120041016A3350 BATTERY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07918SW 7645 EMERGENCY LIGHTS AFT OF EXIT ROW INOPERATIVE. REMOVED EMERGENCY BATTERY AND CLEANED CONTACTORS, RE-INSTALLED AFT BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000402004102200040EA 2004 10 22 SWIA200413900 120041006A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07929SW 7703 STAB TRIM CH1 INOPERATIVE STATUS MESSAGE APPEARED SEVERAL TIMES. REPLACED PILOT AND CO-PILOT TRIM SWITCHES IAW MM 27-41-05, OPERATIONAL CHECKED GOOD. 2L72 4F RTA21EA 20041022000462004102200046EA 2004 10 22 SWIA200413963 120041005A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW TRANSVERSE BEAM LOWER FLANGE CRACKED AT FS LBL 9. ITEM FOUND AT C-CHECK INSPECTION. BEAM REPAIRED IAW CRJ REO 601R-53-11-171. 2L72 4F RTA21EA 20041022000472004102200047EA 2004 10 22 SWIA200413777 120040830A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07941SW TRANSVERSE BEAM IS CRACKED; FS 280.00; RBL 11.0; LOWER FLANGE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACKED LOWER FLANGE AT RBL 110 STA 280 IAW CRJ REO 601R-53-11-171 REV A. 2L72 4F RTA21EA 20041022000572004102200057 2004 10 22 SWIA200413783 420040903A3418 WARNING SYSTEM EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07218SW 120287 STALL WARNING WILL NOT CLEAR ON MAP. REPLACED STALL WARN PANEL PER MM 27-34-08. OPERATIONAL CHECK OK. P/N: 120-34428-505. 2L72 4T RTA31SO 20041022000582004102200058SO 2004 10 22 SWIA200413784 120040906A3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203SO RT MLG STRUT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07251YV 120251 ELEC AND DOOR LIGHT ON MAP ILLUMINATED, STICK SHAKER OPERATED CONTINUOUSLY, SMOKE ALARM IN LAVATORY. REPLACED RIGHT MLG SHOCK ABSORBER PROXIMITY SENSOR AND HARNESS IAW EMB 120 MM 32-01-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000692004102200069NM 2004 10 22 P5CA0401250 120041011A5740 ATTACH FITTING BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RIGHT WING L/E AFT ATTACHED FRAME (FSSI) TO WING FRONT SPAR UPPER CHORD HAS CRACKED AFT FSSI 335. REMOVED CRACK T-ANGLE & INSTALLED NEW T-ANGLE PER SRM 51-30-02. 2L74 4F4 F A20WE E20EA 20041025000022004102500002CE 2004 10 25 JGV2004F00007 120040618A2497 STUD LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP PDU SHORTED B JGVRO OTHER O OTHER NRNOT REPORTED 1 CE09314XS 974618 048 ACCOMPLISHED A MODIFICATION TO THE POWER DISTRIBUTION PANEL TO SUPPORT AN AVIONICS MOD. THE SYSTEM WAS CHECKED OK AND INSPECTED THE TERMINAL STUD FOR SECURITY. THE STUD WAS TIGHT AND THE CONNECTION WAS SECURE. AFTER DELIVERY THE AC HAD ELECTRICAL PROBLEMS. IT WAS FOUND TO HAVE A BURNED SPOT WHERE THE NEW WIRE WAS INSTALLED AND THE STUD WAS SOOSE. REMOVED THE PANEL AND HAD IT REPAIRED AND REINSTALLED TO RETURN THE AIRCRAFT TO SERVICE. SUGGESTED THAT SB 31-245 SHOULD BE ACCOMPLISHED BUT THE CUSTOMER DECLINED. RECOMMEND AD NOTE BE WRITTEN TO MAKE SB 31-245 MANDATORY. THIS HAS HAPPENED BEFORE. (CE09200403890) 2L72 4F4 FRTA10CE E6WE 20041025000052004102500005SO 2004 10 25 SWIA200413855 120040922A2750 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM0758733 120197 PILOT REPORTS CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25 DEGREES. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPERATIONAL CHECK GOOD. P/N 120-6920-615CON, S/N OFF 120182. 2L72 4T RTA31SO 20041025000222004102500022EA 2004 10 25 SWIA200413795 120040907A3350 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07906SW 7510 EMERGENCY FLOOR LIGHTING FROM ROW 18 BACK INOPERATIVE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER IAW MM 33-61-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000252004102500025EA 2004 10 25 SWIA200413973 120041005A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FS 625 LEFT INTERCOSTAL STR 14 LEFT CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20041025000262004102500026CE 2004 10 25 DXTA200400366 120040819A7330 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 2 ENG FUEL ILLUMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07882QS 258482 P107571 AT BEGINNING OF TAKEOFF ROLL, ENGINE 1 FUEL LIGHT ILLUMINATED, REDUCED POWER AND LIGHT WENT OUT. REMOVED NR 1 ENGINE UNSERVICEABLE FUEL FILTER, NO FOREIGN MATERIAL WAS FOUND IN FILTER, INSTALLED NEW FUEL FILTER. AS A PRECAUTION, REMOVED NR 2 ENGINE FUEL FILTER, NO FOREIGN MATERIAL FOUND, INSTALLED A NEW FILTER ELEMENT. LEAK AND OPERATIONAL CHECK WAS FOUND TO BE SATISFACTORY, ALL WORK ACCOMPLISHED IAW TFE 731-5BR LMM CHAPTER 73-21-02. 2L72 4F4 FRTA3EU E6WE 20041025000272004102500027EA 2004 10 25 SWIA200413753 120040823A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07453SW 7743 FS 280 LEFT HAND FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-42-13, 51-21-11. 2L72 4F RTA21EA 20041025000302004102500030SO 2004 10 25 SWIA200413756 120040827A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07234SW 120308 AFT MOST WHITE LIGHT ON FLOOR EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING AND RELAMPED EMERGENCY LIGHT IAW MM 33-51-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000322004102500032EA 2004 10 25 SWIA200413758 120040827A2797855D1009 WIRE CNDAIRCL600 CL6002B19 1900309EA BRAKE POSITION DAMAGED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW9718 9718 7034 FLAP FAIL CAUTION WHEN SELECTING FLAPS FROM 0 DEGREES TO 8 DEGREES. REPAIRED WIRING AND REPLACED RIGHT BPSU IAW WM 20-00-00 AND 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000332004102500033EA 2004 10 25 SWIA200413796 120040623A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07907SW 7511 LEFT FS 625 OBLIQUE ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND INSTALLED NEW ANGLE P/N: 601-35012-51 IAW CRJ 200 SRM 51-42-06. 2L72 4F RTA21EA 20041025000342004102500034EA 2004 10 25 SWIA200413797 120040623A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07907SW 7511 SUPPORT ANGLES CRACKED RBL 9.0 AND LBL 9.0 FS 280.0 WL 73.5. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SUPPORT ANGLES AT FS 280.00, WL 73.5, RBL 9, LBL 9, IAW CRJ 200 SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20041025000352004102500035SW 2004 10 25 ALGA096983 120040812A6230206010440001 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1G71 3U3 UNCH2SW E1GL 20041025000362004102500036SW 2004 10 25 ALGA096984 120040812A6230206010421003 BUSHING BELL 206 206L4 1182110SW ALLSN 250C 250C47B GL SWASHPLATE WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW09265AL1495 52280 TEFLON FABRIC SHOWING THROUGH, EXCESSIVE PLAY BETWEEN LINK AND COLLECTIVE LEVER. REPLACED WITH NEW PART. 1G71 3U3 UNCH2SW E1GL 20041025000372004102500037SW 2004 10 25 ALGA096985 120040812A6230206010441001 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1G71 3U3 UNCH2SW E1GL 20041025000382004102500038SW 2004 10 25 ALGA096986 120040812A6230206010421011 BUSHING BELL 206 206L4 1182110SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW09265AL1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1G71 3U3 UNCH2SW E1GL 20041025000392004102500039SW 2004 10 25 ALGA096987 120040812A6230206010421011 BEARING BELL 206 206L4 1182110SW ALLSN 250C 250C47B GL SWASHPLATE DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03265AL1495 52280 TEFLON FABRIC SHOWING THROUGH. REPLACED WITH NEW PART. 1G71 3U3 UNCH2SW E1GL 20041025000402004102500040NM 2004 10 25 TSAA0171060 120040811A7710 ENGINE BOEING737 737277 1384570NM NR 1 FALSE INDICATIONA TSAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP13183AW 22650 NON-ETOPS FLIGHT 64, HNL-ITO: ABORTED TAKEOFF DUE TO 4 THRUST LEVER SPLIT. WITH THE NR 1 LEVER FORWARD OF THE NR 2, THE NR 2 ENGINE INDICATES 2.0 EPR WHILE THE NR 1 ENGINE INDICATED 1.7 EPR. JET-CAL THE NR 1 AND NR 2 ENGINES IAW FORM M-215, GROUND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20041025000412004102500041SO 2004 10 25 SWIA200413826 120040917A27503082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 NM0716731233 233 120190 ON FINAL APPROACH WITH FLAPS 45 DEGREES, RECEIVED A FLAP CONTROL FAULT AND DISAGREEMENT LIGHTS. REMOVED AND REPLACED BOTH NACELLE FLAP ACTUATORS IAW MM REF 27-50-00. OPERATIONAL CHECK GOOD. P/N: 308200-1007, S/N OFF: 0163. 2L72 4T RTA31SO 20041025000422004102500042EA 2004 10 25 SWIA200413648 120040725A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07936SW 7726 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041025000432004102500043EA 2004 10 25 SWIA200413649 120040725A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07936SW 7726 FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041025000462004102500046EA 2004 10 25 SWIA200413845 120040924A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07916SW6080 7634 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW CRJ 200 MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 884. 2L72 4F RTA21EA 20041025000472004102500047EA 2004 10 25 SWIA200413846 120040925A335083963 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07409SW 7056 ONE CEILING EMERGENCY LIGHT IS OUT. RELAMPED AFT CENTER CEILING EMERGENCY LIGHT WITH SERVICEABLE BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000482004102500048EA 2004 10 25 SWIA200413847 120040925A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW2909 2909 7279 COULD NOT GET STAB CHANNEL NR 2 TO ENGAGE. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1095. 2L72 4F RTA21EA 20041025000502004102500050 2004 10 25 SWIA200413817 420040727A31706229820008 CONCENTRATOR CNDAIRCL600 CL6002B19 1900309EA DCU MISINSTALLED A SWIAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM07909SW 7558 INADVERTENTLY A TECHNICIAN INSTALLED A CRJ700 DCU IN A CRJ200 AND DAMAGED THE DCU. INSPECTED DCU2 RACK CONNECTION AND WIRING AS REQUIRED. NO DEFECTS NOTED. INTERNAL CORRECTIVE ACTION, EA IMPLEMENTED TO INSTALL POLORIZING KEYS IN ALL CRJ200 AIRCRAFT DCU MOUNTING RACKS. 2L72 4F RTA21EA 20041025000552004102500055EA 2004 10 25 SWIA200413822 120040919A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM07979SW 7954 ABORTED TAKEOFF CONFIG TRIM WITH TAKEOFF CONFIG OK RUDDER TRIM. REMOVED AND REPLACED RUDDER TRIM PANEL, OPERATIONAL CHECKS GOOD IAW 27-21-00. 2L72 4F RTA21EA 20041025000562004102500056SO 2004 10 25 SWIA200413823 120040916A3350 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07284YV 120284 FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD EMERGENCY BATTERY PACK IAW MM 33-50-02. OPERATIONAL CHECK GOOD. P/N 366-04-001, S/N OFF 1240/07-96. 2L72 4T RTA31SO 20041025000582004102500058SO 2004 10 25 SWIA200413825 120040911A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07295SW8111 7335 120322 RECEIVED A CONTROL FAULT WARNING DURING LANDING ROLL. REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000592004102500059NM 2004 10 25 SWAA043021 120041018A53116546520 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED AT BS 380, BS 400, BS 440, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041025000622004102500062EA 2004 10 25 SWIA200413827 120040913A2750601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA UNIT-SKEW MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07465SW 7845 FLAPS FAIL MESSAGE ON TAXI. REMOVED AND REPLACED SKEW DETECTION UNIT IAW MM 27-10-01. OPERATIONAL CHECK GOOD. P/N 601R59014-1, S/N OFF A431. 2L72 4F RTA21EA 20041025000642004102500064EA 2004 10 25 SWIA200413829 120040916A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07909SW 7558 ON TAXI STATUS MESSAGE FLT SPOILERS FAULT. REMOVED AND REPLACED RIGHT HAND INBOARD FLIGHT SPOILERS PCU IAW 27-62-01 CRJ MM, OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF 5625. 2L72 4F RTA21EA 20041025000652004102500065 2004 10 25 SWIA200413830 420040916A3418C818022 SERVO EMB 120 EMB120ER 3260203SO STICK SHAKER INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07288SW1947 1947 120316 RIGHT STALL SHAKER INOPERATIVE. INSTALLED SERVICEABLE SERVO STICK SHAKER ON NR 2 SIDE. OPERATIONAL CHECK GOOD. P/N C-81802-2, S/N ON 408, S/N OFF 298. 2L72 4T RTA31SO 20041025000662004102500066SO 2004 10 25 SWIA200413831 120040914A3350C818022 LIGHT EMB 120 EMB120ER 3260203SO CABIN MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07567SW 120342 ONE FORWARD EMERGENCY EXIT RED LIGHT, FLOOR LEVEL, IS MISSING. INSTALLED SERVICEABLE FORWARD RED EMERGENCY LIGHT ON FLOOR AS REQUIRED, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000682004102500068EA 2004 10 25 SWIA200413833 120040917A274170608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07923SW 7664 STAB TRIM AND MACH TRIM CAUTION MESSAGES CAME ON DURING TAXI. REMOVED AND INSTALLED SERVICEABLE HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000712004102500071SW 2004 10 25 ALGA096917 120040810A6710406310405101 LINK BELL 407 407 1182206SW ALLSN 250C 250C47B GL MAIN ROTOR DRIVECRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL485 53265 FOUND P/C LINK BEARING BINDING; RATCHETY AND HAS AXIAL WEAR. REPLACED WITH NEW PART IN FIELD. 1G71 3U3 UO H2SW E1GL 20041025000722004102500072SO 2004 10 25 SWIA200413875 120041002A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAL ABORTED APPROACH JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07294SW 120321 FLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED WITH ASSOCIATED CONTROL FAULT. REPLACED FLAP CONTROL UNIT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000732004102500073EA 2004 10 25 SWIA200413876 120041001A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM07410SW1037510375 FLAP FAIL MESSAGE DURING FLAP RETRACTION OUT OF SLC. RETURN TO FIELD. REPLACED FECU IAW MM 27-51-05 AND LEFT NR 5 FLAP FLEX SHAFT IAW CRJ 200 MM 27-53-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000742004102500074EA 2004 10 25 SWIA200413877 120040930A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07465SW 7845 ONE OF THE CABIN CEILING EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED MIDDLE CEILING EMERGENCY LIGHT IAW 33-00-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000752004102500075 2004 10 25 SWIA200413878 420040926A3418 COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07250YV 120250 STALL SYSTEM NR 1 WILL NOT TEST. REPLACED NR 1 AOA TRANSDUCER, NR 1 STALL WARNING COMPUTER AND STALL WARNING PANEL ASSY. CLEANED MPU CONNECTOR. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 14882-304, P/N C-81817-1, S/N ON 955, S/N OFF 1101, P/N C-81806-1MODA, S/N ON 681, S/N OFF 391. 2L72 4T RTA31SO 20041025000762004102500076NM 2004 10 25 CALA0400678 120041015A53306545775 SKIN BOEING737 7373T0 1384582NM STA CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 INSPECTION FOUND A 2.8 INCH CRACK IN EXTERIOR FUSELAGE SKIN JUST AFT OF FRAME STA 727E ABOVE S23R. A REPAIR WAS INSTALLED IAW ECRA 5330-03375 AND A DIP WAS ISSUED TO COMPLETE A REPAIR ASSESSMENT WITHIN 12 MONTHS AND PROVIDE REPAIR/INSPECTION THRESHOLDS. THE REPAIR IS ACCEPTABLE FOR 12 MONTHS. 2L72 4F RTA16WE 20041025000772004102500077NM 2004 10 25 CALA0400679 120041015A53306545774575 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2770352 23590 A WALKAROUND INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D TO STA 727E, S22L TO S24L. THE SKIN WAS REPAIRED IAW ECRA 5330-03376. 2L72 4F RTA16WE 20041025000782004102500078NM 2004 10 25 SWAA042921 120041007A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND 7EA FUSELAGE FRAMES CRACKED AT BS 727B, BS 727D, BS 747, BS 867, BS 907, BS 380, AND BS 400, BETWEEN STR 8L- STR 9L. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20041025000792004102500079NM 2004 10 25 SWAA042922 120041007A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND 12 EA FUSELAGE FRAMES CRACKED AT BS 727B, BS 727D, BS 747, BS 787, BS 827, BS 867, BS 907, BS 380, BS 400, BS 440, BS 480 AND BS 500A, BETWEEN STR 8R- STR 9R. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20041025000802004102500080NM 2004 10 25 SWAA043003 120041016A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED RT LIGHT LENS PER MM. 2L72 4F RTA16WE 20041025000812004102500081 2004 10 25 NACA20040030 420040826A6122SU1861 GOVERNOR DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE HAMSTD43E 43E60 NE NR 2 INOPERATIVE A NACAE ENGINE SHUTDOWN O OTHER TOTAKEOFF 1 AL036174C589 589 44075 56476 N204891 NR 2 PROPELLER OVERSPEED, UNCONTROLLABLE, WOULD NOT FEATHER. FOUND PROPELLOR GOVERNOR INOPERATIVE. REPLACED PROP GOVERNOR. LEAK AND OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 6 CP871 20041025000822004102500082NM 2004 10 25 SWAA043004 120041016A53306545765 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 519, STRINGER 16L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041025000832004102500083NM 2004 10 25 SWAA043005 120041016A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29465WN 33829 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXTERIOR LIGHT PER MM. 2L72 4F RTA16WE 20041025000842004102500084NM 2004 10 25 SWAA043006 120041017A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 430, STRINGER 17R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041025000852004102500085NM 2004 10 25 SWAA043007 120041017A3397GD1220 TERMINAL BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED A1 CHECK, EMERGENCY EXIT LIGHTS WILL NOT TURN OFF WITH ARMED SWITCH IN OFF POSITION. SECURED GROUND TERMINAL AT AFT F/A PANEL PER MM. 2L72 4F RTA16WE 20041025000862004102500086NM 2004 10 25 SWAA043008 120041017A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041025000872004102500087NM 2004 10 25 SWAA043009 120041017A5330654576654 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS AT BS 451, BS 486, BS 503, STRINGER 16R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041025000882004102500088NM 2004 10 25 SWAA043010 120041017A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500C + 13, BS 500D + 8, STRINGER 15L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041025000892004102500089NM 2004 10 25 SWAA043011 120041017A53116546529 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT FWD CARGO COMPT, BS 500, RBL 20, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041025000902004102500090NM 2004 10 25 SWAA043012 120041017A53126545409 PRESSURE PANEL BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 32, CRACKED. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041025000912004102500091NM 2004 10 25 P5CA0401243 120041008A3020BACR13602 RELAY BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL ANTI ICE SYSTEM FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23454PA 30812 AFTER ENGINE START, STATUS MSG NAI-VLV NR 3 DISPLAYED. REPLACED ANTI-ICE VALVE RELAY PER AMM 30-21-00, OPERATIONAL CHECK OK ON ENGINE RUN. 2L74 4F4 FRTA20WE E23EA 20041025000922004102500092GL 2004 10 25 P5CA0401244 220041011A73131303M31G12 MANIFOLD BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 2 ENG FUEL MALFUNCTIONED A P5CAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 WP23452PA 30810 706220 NR 2 ENGINE FUEL LEAK. REPLACED LT FUEL MANIFOLD PER AMM 73-11-16, PERFORMED ENGINE RUN PER AMM 71-00-00. 2L74 4F4 FRTA20WE E23EA 20041025000932004102500093SO 2004 10 25 SWIA200413948 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025000942004102500094SO 2004 10 25 SWIA200413949 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 0.00 (CENTER). ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025000952004102500095SO 2004 10 25 SWIA200413950 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW SRM 51-40-02. 2L72 4T RTA31SO 20041025001072004102500107NM 2004 10 25 P5CA0401242 120041004A2780 FLAP BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 2 LT MALFUNCTIONED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23921FT 21575 NR 2 LEFT LEADING EDGE WOULD NOT COME UP PNEUMATICALLY, OK ELECTRICALLY. RECYCLED FLAPS PNEUMATICALLY, NO HELP. TRANSFERRED TO DMI 33203. 2L74 4F4 F A20WE E3NE 20041025001082004102500108NE 2004 10 25 NACA20040026 220040804A7261 FILTER BOEING727 72723 1384004NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE CARBONED A NACAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 AL03992AJ269 269 19428 649003 NR 3 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE/BYPASS LIGHT ILLUMINATED ON CLIMBOUT. REMOVED NR 3 ENGINE OIL SCREEN, INSPECTED AND FOUND CARBON ON FILTER. REPLACED FILTER WITH NEW. OP AND LEAK CHECK GOOD. 2L73 4F4 F A3WE E2EA 20041025001102004102500110NM 2004 10 25 SWAA042986 120041015A3350311500 LENS BOEING737 7373Q8 1384670NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 2 ABC, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041025001122004102500112 2004 10 25 SWAA042988 420041015A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C1 CHECK, FOUND L1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041025001132004102500113SO 2004 10 25 SWIA200413943 120041011A3320 BALLAST EMB 120 EMB120ER 3260203SO LAV LIGHT SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07236SW 120312 DURING PASSENGER DEPLANING, MOMENTARILY SMELLED SMOKE AND NOTICED C/B A30 POPPED. REPLACED LAV LIGHT BALLAST AND RESET BREAKER A30, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025001142004102500114SO 2004 10 25 SWIA200413944 120041013A27203211001003 CONTROL UNIT EMB 120 EMB120ER 3260203SO HYD SYS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07189SW1973 1973 120048 ABOVE 230KIAS FULL NOSE RIGHT TRIM ON TRIM WHEEL (RUDDER) DOES NOT CENTER THE BALL. REPLACED RUDDER PCU, OPERATIONAL CHECK GOOD IAW 27-22-00. 2L72 4T RTA31SO 20041025001162004102500116EA 2004 10 25 SWIA200413885 120040929A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07446SW 7666 AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING LIGHT BULB AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 33-01-05. 2L72 4F RTA21EA 20041025001182004102500118SO 2004 10 25 SWIA200413887 120041004A27503203001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07167315355 2511 120190 MULTIPLE FLAP CONTROL FAULTS WITH DISAGREEMENT AND ASYMMETRY LIGHTS ON THE GROUND AND IN THE AIR. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025001202004102500120EA 2004 10 25 SWIA200413965 120041005A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW FS 409 + 128 RIGHT VERTICAL BEAM AT RBL 18 LOWER OUTBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALL REPAIR PIECES IAW CRJ ERO 601R-53-41-248 REV "NC" AND 601R-53-41-056 REV "NC". 2L72 4F RTA21EA 20041025001222004102500122EA 2004 10 25 SWIA200413967 120041005A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW FS 409 + 128 RIGHT VERTICAL BEAM AT RBL 27 LOWER INBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-056 "NC" . 2L72 4F RTA21EA 20041025001232004102500123 2004 10 25 NACA20040028 420040821A61225U1881 GOVERNOR DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE HAMSTD43E 43E60 NE NR 1 PROP UNCONTROLLABLE A NACAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03779TA48 48 45529 P33192 175852 NR 1 PROPELLER UNCONTROLLABLE, WOULD NOT FEATHER. OVERSPEED TO APPROXIMATELY 3300. INSPECTED ENGINE FINGER SCREENS, NO NOTEABLE FINDINGS. REPLACED NR 1 PROPELLER GOVERNOR. CHECKED GOOD. 2L74 4R4 R A781 5E8 6 CP871 20041025001252004102500125EA 2004 10 25 SWIA200413974 120041005A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW CARGO PIT EXISTING FLOOR SUPPORT ANGLE REPAIR IS CRACKED; FS 621.00, LBL 40.0. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 601R-53-61-117 REV. B. 2L72 4F RTA21EA 20041025001272004102500127EA 2004 10 25 SWIA200413902 120041008A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07441SW RIGHT SPOILERON STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON, INBOARD PCU (NR 2 HYD SYS) WITH A SERVICEABLE UNIT IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001292004102500129NM 2004 10 25 CALA0400675 120041012A5330 SKIN BOEING737 7373T0 1384582NM FUSLEAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717345 23583 DENT IN FUSELAGE BS 837 - STR 19L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20041025001312004102500131SO 2004 10 25 SWIA200413894 120040724A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE RIGHT FLOOR PROP AT FRAME 13 CRACKED. ITEM FOUND AT C-CHECK. REPAIRED RIGHT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10. 2L72 4T RTA31SO 20041025001332004102500133EA 2004 10 25 SWIA200413858 120040927A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07932SW2719 2719 7714 AP PITCH TRIM CAUTION MESSAGE APPEARED IN DESCENT. REMOVED AND REPLACED HSTCU PER AMM 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041020001522004102000152NM 2004 10 20 AWXA200401128 120041012A53306545774575 SKIN PANEL BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 DURING 8-DAY CHECK A 2.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E STR 24 LT. MAINTENANCE CUTOUT DAMAGE AND PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.R. 03-5331-04285-RC1. TEMPORARY REPAIR, INSPECTION REQUIRED AT 60,000 FLIGHT CYCLES. 2L72 4F4 FRTA16WE E2GL 20041020001562004102000156 2004 10 20 FE62004F00001 420040727A3422ST3400 INDICATOR AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE731* 01518WP COCKPIT INACCURATE B FE6RO OTHER O OTHER NRNOT REPORTED 1 NM112FQ 167 THE SANDEL TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADINGS GREATER THAN 350 DEGREES OR LESS THAN 0 DEGREE. THIS PROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TESTING OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION IS SOFTWARE. THE ST3400 TAWS/RMI IS NOT RECOMMENDED FOR NAVIGATION AT THIS TIME. 2L73 4F4 F A46EU E6WE 20041020001592004102000159NM 2004 10 20 371PA0084 120041004A5340 ATTACH FITTING BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 HFEC INSPECTION OF PREVIOUS REPAIR INDICATES A CRACK AT THE BS 616 STUB BEAM TO LONGITUDINAL FLOORBEAM ATTACH POINT AT LBL 45.5. FURTHER INVESTIGATION DETERMINED THAT THE DAMAGE TO BE A PREVIOUS PLUG INSTALLED IN THE FASTENER HOLE. REPAIRED AREA IAW MFG MESSAGES: NR 1-PHPIP, NR 1-QHJ76, MFG NR 1-QMG7D. 2L72 4F4 FRTA16NE E2GL 20041020001722004102000172WP 2004 10 20 DHL2004801528 120040902A5511 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 2047: RT HORIZONTAL STABILIZER IB L/E UPPER FORMER CRACKED 1.000, XFS 60.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG. 7-8. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 55-2-0 PG. 7-8. 2L74 4F4 FRT4A25 E2GL 20041020001792004102000179NM 2004 10 20 04FDEA02898 120041011A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 SNRM N0631: MAIN DECK, SEAT TRACK RBL 47.5 CRACKED AT STA 5-53. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 SHT 1 VOL I. 2L73 4F4 FRTA22WE E31N3 20041020001962004102000196CE 2004 10 20 H48A2004002 120040824A271151155464 PUSHROD CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO LT AILERON TRIM FAILED E H48AO OTHER O OTHER NRNOT REPORTED 1 WP135614C 414A0203 AILERON TRIM PUSH ROD ASSY (PN 51155464) FAILED, CAUSING THE AILERON TRIM TAB TO BIND IN THE UP POSITION. AIRCRAFT LANDED AT AN AUXILIARY AIRFIELD WITHOUT INCIDENT. PUSH ROD REPLACED WITH NEW MFG PUSH ROD ASSY (PN 51155464). OLD PUSH ROD, ROD END BEARING FAILED. THERE IS NO TIME REPLACEMENT OF THIS PUSH ROD. IT IS ESTIMATED THAT THE ROD END HAD APPROXIMATELY 12,487.2 HOURS AT THE TIME OF FAILURE. (WP13200409631) 1L72 3O3 O A7CE E8CE 20041021000022004102100002EA 2004 10 21 A6WA200440143 120040921A5320 CHANNEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31402AW 7281 FOUND CARGO DOOR, FORWARD TRACK SUPPORT CHANNEL IS CRACKED. REMOVED CRACKED SUPPORT CHANNEL AND INSTALLED NEW SUPPORT CHANNEL IAW CRJ SRM 51-42-06. (M) 2L72 4F RTA21EA 20041021000142004102100014NM 2004 10 21 ASAA0440144 120040730A5347654538446 CARGO TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 OAK - FOUND LOWER FUSELAGE AREA BELOW AFT CARGO COMPARTMENT, BILGE RT STATION 947 CORRODED AROUND THE DOWN FITTINGS. MARKED DOT 1025. REMOVED CORRODED CARGO TIE DOWN TRACK AND INSTALLED NEW CARGO TIE DOWN TRACK SECTION AND REPAIR SPLICE AT AFT CARGO COMPARTMENT BILGE RT STATION 917-947. (M) 2L72 4F RTA16WE 20041021000172004102100017EA 2004 10 21 ASOA04748 120040925A5210601R319801 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11842AS 7304 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR IAW CRJ200 MM 52-10-00. (M) 2L72 4F RTA21EA 20041021000222004102100022EA 2004 10 21 ASOA04749 120040927A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11843AS 7310 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20041021000302004102100030NM 2004 10 21 ASAA0410391 120040910A531565549073 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION BOTTOM LOWER LOBE OF FLOORBEAM. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20041021000502004102100050NM 2004 10 21 ASAA0440146 120040730A53106545871140 DOOR FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 OAK - FOUND DOOR RT FORWARD SERVICE LOWER AFT FITTING SUPPORT FASTENER HOLE CRACKED INSIDE LOWER DOOR MARKED 1023. SPLICED IN NEW DOOR, FRAME AND INSTALLED DOUBLER AT RT FORWARD SERVICE DOOR LOWER AFT CORNER. (M) 2L72 4F RTA16WE 20041021000552004102100055NM 2004 10 21 ASAA0410397 120040913A5310655073334 STRUCTURE BOEING737 7372X6C 1384552NM MLG WW CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND CORROSION AT RIGHT MLG WHEEL WELL ON CHORD. CUTOUT DAMAGED AREA AND SPLICE IN NEW AREA PER SRM. (M) 2L72 4F RTA16WE 20041021000622004102100062 2004 10 21 DJFA2004027 420041011A34256226A5205 COMPUTER BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315BR WP FLT DIRECTOR INOPERATIVE E DJFAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 EA23801CW10261 258012 KAUS-KLIT TRIP ID NR 708818. CREW REPORTED YAW DAMPER WOULD ENGAGE AFTER TAKE OFF. FDC CONTROLLER, FLIGHT DIRECTOR ON LT SIDE FLAGGED OFF DURING ILS APPROACH. AIRCRAFT DIVERTED WITH AN UNEVENTFULL LANDING. MAINTENANCE ISSUED MEL 34-20-1. MAINTENANCE ISSUED MEL 34-20-1. 14 OCTOBER, 2004 AN OVERHAULED FLIGHT DIRECTOR WAS INSTALLED. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20041021000712004102100071 2004 10 21 SWAA043016 420041018A256569849956 CABLE BOEING737 7373Q8 1384670NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041021001042004102100104EU 2004 10 21 AALA20041050 120041015A3350P4010051124 LIGHT AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2190070 513 JFK - EMERGENCY LIGHTS AT LEFT SIDE SEAT 18C THROUGH 28C INOPERATIVE. REPLACED UNIT AND BATTERY PACK (BPS73 FROM RADIANT POWER) FOR EMERGENCY LIGHTS AT LEFT SIDE SEAT 18C THROUGH 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041021001082004102100108WP 2004 10 21 AALA20041054 120041016A3897 WIRE DOUG DC9 DC982 3022082WP HEATER SHORTED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21237AA 49253 MCO - INFLIGHT T2226/16 HAZY SMOKE AND SHARP ELECTRICAL WIRE BURNING SMELL COMING FROM FIRST CLASS LAVATORY WAS REPORTED 40 MINUTES AFTER TAKEOFF. PERFORMED QRH SMOKE PROCEDURE AND SMOKE AND SMELL DISSIPATED. FOUND FORWARD LAVATORY WATER TANK SHORTING. PLACARD FORWARD LAVATORY WATER TANK HEATER PER MEL. 2L72 4F A6WE 20041022000032004102200003NM 2004 10 22 MASA200400552 120040929A3350 SIGN DHAV DHC8 DHC8202 2809007NM EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07434YV 434 ASH 6211 PHX-FLG, THE EMERGENCY EXIT SIGN ABOVE THE MAIN CABIN DOOR WILL NOT ILLUMINATE. MX REPOSITIONED LIGHT ASSEMBLY SOCKET AND SYSTEM CHECKED NORMALLY. 2H72 4T RTA13NM 20041022000162004102200016NM 2004 10 22 P5CA0401251 120041012A3697 WIRE BOEING747 747230B 1384889NM GE CF6 CF650C2 30018NE BLEED VALVE CHAFED A P5CAO OTHER S AFFECT SYSTEMS CRCRUISE 1 EA15508MC 21644 530349 NR 3 ENGINE BLEED VALVE CLOSED, LIGHT STAYS ON AT CRUISE PWR & POPPED C/B AT LANDING. REPAIRED CHAFED WIRE PYLON TO HIGH STAGE BLEED VALVE PER WPM CH 20-10-13, OPERATIONAL CHECK OK. 2L74 4F4 F A20WE E23EA 20041022000232004102200023EA 2004 10 22 SWIA200413976 120041017A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAK NONE L NO TEST ININSP/MAINT 1 NM07429SW 7518 DURING PREFLIGHT FOUND FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000272004102200027SO 2004 10 22 SWIA200413935 120040823A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW 120151 SURFACE CORROSION FOUND ON FLOOR SUPPORT AT FS 4214.0 - FS 5118-0 LT FLOORBEAM. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT REPAIRED IAW EMBRAER REF 1C2004-145/4092 DATE AUG 31, 2004. 2L72 4T RTA31SO 20041022000282004102200028SO 2004 10 22 SWIA200413936 120040823A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW FRAME 9 LEFT AND RIGHT CRACKED AT STRINGER 9 CABIN AREA. ITEM FOUND AT C-CHECK INSPECTION. FRAME 9 LEFT AND RIGHT AT STRINGER 9 REPAIRED IAW EMB SB 120-53-0073 STEPS 3C AND 3E. 2L72 4T RTA31SO 20041022000292004102200029SO 2004 10 22 SWIA200413937 120040823A5712 RIB EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW LEFT WING FORWARD RIB 21 IS CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-12-02 & 57-20-07 FIG 203. 2L72 4T RTA31SO 20041022000302004102200030SO 2004 10 22 SWIA200413938 120040823A5712 RIB EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW LEFT WING FORWARD RIB 17 CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1 AND 51-12-02. 2L72 4T RTA31SO 20041022000312004102200031SO 2004 10 22 SWIA200413939 120040823A5712 RIB EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07196SW RIB ATTACH ANGLE CRACKED ON RIGHT WING, RIB 21, TOP SURFACE OF RIB, BETWEEN STRINGERS 3 AND 4. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PART IAW EMB 120 SRM 51-25-00, 51-40-00, 51-30-01, 51-40-01, 51-40-02, 51-40-05 AND REF 57-20-07 FIG 6 ITEM 90. 2L72 4T RTA31SO 20041022000372004102200037EA 2004 10 22 SWIA200413984 120040727A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07935SW 7725 RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041022000382004102200038EA 2004 10 22 SWIA200413985 120040727A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07935SW LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ITEMS IAW 601R-53-61-117-1, -3, AND -79 COMPLIED WITH REO 601R-53-61-117. 2L72 4F RTA21EA 20041022000392004102200039SO 2004 10 22 SWIA200413772 120040902A27523431001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07237SW1071 1071 120314 FLAP DISAGREEMENT RETRACTING FLAPS ON GROUND. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000492004102200049EA 2004 10 22 SWIA200413779 120040902A335020131A CHARGER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW2544 2544 EMERGENCY EXIT SIGN OVERHEAD OF CABIN AT ROW 8 INOPERATIVE. REMOVED AND REPLACED NR 1 AND NR 2 ELBP IAW MM 33-51-04 AND REPLACED NR 2 ELBP CHARGER. OPERATIONAL CHECK GOOD. P/N 2013-1A, S/N OFF 83335. 2L72 4F RTA21EA 20041022000532004102200053SO 2004 10 22 SWIA200413773 120040901A3320 BULB EMB 120 EMB120ER 3260203SO COCKPIT BURNED OUT A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM07227SW 120304 INFLIGHT SMELLED ELECTRICAL BURNING, NOTED BULB ABOVE 3A OUT AND DARK. REPLACED CABIN LIGHT BULB AT SEAT 3A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041022000732004102200073WP 2004 10 22 P9RA20040032 120040827A5350 TAIL CONE DOUG DC9 DC982 3022082WP DEPLOYED A P9RAK NONE O OTHER ININSP/MAINT 1 SO1110801 49127 AIRCRAFT IN MAINTENANCE-TOL. TAIL CONE WAS INADVERTENTLY DEPLOYED BY RAMP SERVICE PERSONNEL. REINSTALLED TAIL CONE IAW MM 535300. SFB MAINTENANCE ENTRY 8/27/2004. INSPECT TAIL CONE EVACUATION SLIDE FOR PROPER INSTALLATION. INSPECTED SLIDE IAW MM 256200. NO DEFECTS NOTED. 2L72 4F A6WE 20041025001352004102500135EA 2004 10 25 SWIA200413860 120040926A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07412SW113698838 7101 WHEN FLAPS ARE SELECTED OUT OF 20 DEGREES, YELLOW LINE ON AIRSPEED TAPE APPEARS MOMENTARILY ALONG WITH WINDSHEAR FAIL STATUS MESSAGE. REMOVED AND REPLACED FECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001372004102500137EA 2004 10 25 SWIA200413904 120041007A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07979SW 7954 SPOILERON FAULT MESSAGE. REMOVED AND REPLACED RIGHT SPOILER OUTBOARD PCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-62-01. P/N ON 27000-7, S/N ON MAL4403, OFF 7720. 2L72 4F RTA21EA 20041025001382004102500138SO 2004 10 25 SWIA200413956 120041005A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOOR SUPPORT STRUCTURE AT FR 13 - FR 38, STR 15L. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025001432004102500143SO 2004 10 25 MASA200400408 120040717A335082324 SIGN EMB 145 EMB145LR 3260212SO ROW 12 CEILING INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07834MJ 145340 AIRCRAFT WAS ON RON LAST NIGHT AND SCHEDULED FOR A ROUTINE INSPECTION. DURING THE WALKAROUND DISCOVERED ROW 12 CEILING EMERGENCY EXIT SIGN LIGHT INOP. MAINTENANCE REPLACED THE LIGHT, OPERATIONAL CHECK GOOD. 2L72 4T RTT00011AT 20041025001442004102500144EA 2004 10 25 SWIA200413968 120041005A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FS 460 RIGHT FLOORBEAM RBL 9.0 OUTBOARD FITTING IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-42-21. 2L72 4F RTA21EA 20041025001472004102500147EA 2004 10 25 SWIA200413982 120041015A27508004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA UNIT-SKEW MALFUNCTIONED A SWIAD RETURN TO BLOCK JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07955SW1620 1620 7817 FLAPS DEGRADED WHEN FLAPS SELECTED TO TAKEOFF SETTING. FLAPS DEGRADED STATUS MESSAGE. REMOVED AND REPLACED SKEW DETECTION UNIT IAW CHAPTER 27-51-15 CRJ MM. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001482004102500148NM 2004 10 25 SWAA043030 120041019A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20041025001492004102500149NM 2004 10 25 SWAA043031 120041019A57536546435277 SKIN BOEING737 7373H4 1384600NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29321SW 23342 DURING SCHEDULED C4 CHECK, FOUND LEFT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LEFT AFT T/E FLAP PER MM. 2L72 4F RTA16WE 20041025001502004102500150NM 2004 10 25 SWAA043039 120041019A55106551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT HORIZONTAL STABILIZER FITTING FWD AND AFT SPARS CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB FITTING PER SRM. 2L72 4F RTA16WE 20041025001512004102500151NM 2004 10 25 SWAA043040 120041019A53106546529 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH SHEAR TIES AT BS 500, RBL 12 AND LBL 19, CORRODED. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20041025001522004102500152EA 2004 10 25 SWIA200413880 120040915A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07594SW8004 8004 7285 SPOILERONS FAULT NR 1 SYSTEM PCU INOPERATIVE. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT IAW 27-62-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001532004102500153EA 2004 10 25 SWIA200413881 120040928A2760 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS OUT OF RIG A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07909SW 7558 FLT SPOILER FAULT STATUS MESSAGE APPEARS AFTER LANDING. RIGGED LEFT SPOILERONS INBOARD/OUTBOARD PCUS IAW MM 27-62-01. RIGGED LEFT AND RIGHT FLIGHT SPOILER OUTBOARD PCU IAW CRJ MM 27-62-01. REPLACED NR 1 AND NR 2 SECUS IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD IAW CRJ 200 FIM 27-63-00. P/N 49-164-20, S/N OFF 03259, 03020, P/N OFF 49-164-05, S/N OFF 102. 2L72 4F RTA21EA 20041025001562004102500156EA 2004 10 25 SWIA200413969 120041005A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FUSELAGE FLOOR SUPPORT INTERCOSTAL AT STA 484.00 INBOARD FLANGE AT RBL 27 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. 2L72 4F RTA21EA 20041025001592004102500159EA 2004 10 25 SWIA200413810 120040906A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07943SW 7762 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20041025001612004102500161SO 2004 10 25 SWIA200413896 120040716A5712 RIB EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07186SW 120034 LEFT WING AT RIB 8 WING TO WEB CLIP IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED SUPPORT BRACKET IAW SRM 51-25-00, 51-40-00. 2L72 4T RTA31SO 20041025001632004102500163EA 2004 10 25 SWIA200413898 120041007A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07461SW 7811 STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED MCU AND HSTCU IAW CRJ MM 27-40-00 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 8396-3, S/N OFF 1078. 2L72 4F RTA21EA 20041025001652004102500165WP 2004 10 25 AALA20041033 120041006A3233 ACTUATOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21221AA 49172 LAX - INFLIGHT T13956 SNA TO STL. UNABLE TO RETRACT NOSE LANDING GEAR. FLIGHT CREW CYCLED GEAR THREE TIMES AND NOSE GEAR DID NOT RETRACT, RED LIGHT WAS ON. LANDED LAX WITHOUT INCIDENT. LANDING WEIGHT WITHIN LIMITS. PERFORMED BITE TEST ON NOSE GEAR UPLOCK PSEU. NO FAULTS NOTED. REMOVED AND REPLACED NOSE GEAR BUNGEE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041025001672004102500167WP 2004 10 25 AALA20041034 120040929A2497 WIRE DOUG DC9 DC983 3022083WP ELECTRICAL DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21569AA 49351 TUL - WIRE CABLE NR 3X3D2C AND 3X3C2C TO LEFT HAND AUXILLARY RELAY AT FORWARD LOWER EXTERNAL POWER CONTACTOR SHOWS SIGNS OF OVERHEATING. REMOVED AND REPLACED WIRE CABLE 3X3D2C AND 3X3C2C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041025001692004102500169NM 2004 10 25 CALA0400677 120041014A531465621257 KEELBEAM BOEING737 7373T0 1384582NM FUSLEAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 LEFT KEEL BEAM UPPER SURFACE OF OUTBOARD FLANGE WORN INTO BY NUT PLATES AT STATION 716, 720, AND 723. REPAIRED IN ACCORDANCE WITH EC/RA 5311-01206 AND EC/RA 5311-01207. 2L72 4F RTA16WE 20041025001712004102500171SO 2004 10 25 SWIA200413891 120040724A5310 WINDOW FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 F/O'S SIDE FORWARD OF DV WINDOW FRAME 9 IS CRACKED. ITEM FOUND AT C-CHECK. COMPLIED WITH SB 120-53-0073 ON F/O'S SIDE FORWARD OF DV WINDOW AT FRAME 9 AS REQUIRED. 2L72 4T RTA31SO 20041025001732004102500173SO 2004 10 25 SWIA200413893 120040724A5313 RIB EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 AFT OF DV CAPTAIN'S SIDE FRAME 13 HAS CRACKED RIB (MARKED). ITEM FOUND AT C-CHECK. REMOVED AND REPLACED CRACKED RIB ON FRAME 13 BEHIND CAPTAIN'S DV WINDOW WITH A SERVICEABLE UNIT. 2L72 4T RTA31SO 20041025001742004102500174NM 2004 10 25 SWAA042903 120041006A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D CHECK, FOUND 6 EACH FRAMES AT BS 787, BS 867, BS 907, STRINGER 8R, BS 827, BS 867, BS 907, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041025001752004102500175EA 2004 10 25 SWIA200413811 120040906A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07943SW 7762 FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 43 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV. B. 2L72 4F RTA21EA 20041025001762004102500176NM 2004 10 25 SWAA043041 120041020A335020131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29386SW 26601 LEFT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT WITHOUT BEING SWITCHED ON. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20041025001772004102500177NM 2004 10 25 SWAA043042 120041021A335020131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT FAULTY A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29386SW 26601 FWD RIGHT EMERGENCY EXIT AND BOTH OVERWING EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2L72 4F RTA16WE 20041025001782004102500178 2004 10 25 SWAA043043 420041020A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041025001792004102500179NM 2004 10 25 SWAA043044 120041020A53306545765 SKIN BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29728SW 27860 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN UNDER AIRPHONE ANTENNA AT BS 500 + 8, CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041025001802004102500180NM 2004 10 25 SWAA043045 120041020A3350612825 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29331SW 23695 DURING SCHEDULED A1 CHECK, FOUND LEFT AFT CABIN BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041025001812004102500181NM 2004 10 25 SWAA043046 120041020A55526625183 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED C3 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 AND NR 2 TAB BUSHINGS PER MM. 2L72 4F RTA16WE 20041025001822004102500182NM 2004 10 25 SWAA043047 120041020A3350610478 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041025001832004102500183NM 2004 10 25 SWAA043048 120041021A3350100885 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29787SA 29812 THREE EACH FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041025001842004102500184 2004 10 25 SWAA043049 420041021A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041025001862004102500186 2004 10 25 SWAA043051 420041021A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041025001882004102500188NM 2004 10 25 SWAA043053 120041021A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727E, STRINGER 21R AND BS 727E, STRINGER 21L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041025001902004102500190NM 2004 10 25 SWAA043054 120041021A53146545765 KEELBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM AT BS 500D, CORRODED. REPAIRED KEEL BEAM PER EA. 2L72 4F RTA16WE 20041025001922004102500192NM 2004 10 25 SWAA043056 120041005A3350612825 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING SPV, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041026000042004102600004NM 2004 10 26 SWAA043061 120041021A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663.75, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041026000082004102600008NM 2004 10 26 SWAA043065 120041021A53156920158 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB FROM RIGHT BS 188 TO BS 196, CRACKED. REPAIRED FLOORBEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041026000112004102600011EU 2004 10 26 AWXA200400938 120040806A5330D53480115208 DOUBLER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 MCN - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FUSELAGE SKIN AROUND WASTE SERVICE COMPARTMENT CUTOUT BETWEEN FR 65 & FR 66, STRINGERS 35 & 39 RT. MAINTENANCE REMOVED CORRODED REINFORCEMENT DOUBLER FROM FR 65 TO FR 66, AND STRINGERS 35 TO 39 RT; FABRICATED A NEW REPLACEMENT DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041026000152004102600015NM 2004 10 26 UPS04242996 120040709A5730 SKIN BOEING727 72722C 138400FNM LT WING TIP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, 0.5 INCH CRACK IN LOWER WING SKIN AT LEFT WING TIP, APPROX 8 INCHES FROM TIP AND JUST FWD OF STRINGER FAIRING. CRACK STOP DRILLED IAW SRM 51-10-1. CRACK CONTAINED WITHIN DRILLED AREA. HOLE DRILLED IN RIB COMMON TO REPAIR SCHEME FOR NDT. HFEC CARRIED OUT ON 8 FASTNER HOLES, NO DEFECTS FOUND. CUT OUT CARRIED OUT IAW EO 2004-073-005. DOUBLER FABRICATED. DOUBLER INSTALLED. ALL AREA REPROTECTED. 2L73 4F A3WE 20041026000162004102600016NM 2004 10 26 UPS04242997 120040809A5730 PANEL BOEING727 72722C 138400FNM LT WING ERODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, LT WING LOWER FIXED L/E PANEL FSS 262 TO FSS 312 ERRODED ALONG L/E AT O/B END. PANEL REMOVED IAW 51-30-2. PANEL DERIVETED FROM BRACKET IAW 51-30-2. FUEL DRAIN PIPES DISCONNECTED IAW MM 29-00-00. PANEL FABRICATED IAW DRG 65-21653. PANEL AND ATTACH BRACKET INSTALLED IAW 51-30-2. PANEL SEALED IAW SRM 20-60-01. FUEL DRAIN PIPES RECONNECTED. 2L73 4F A3WE 20041026000202004102600020WP 2004 10 26 UPS04842863 120040715A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, RT HORIZONTAL STAB L/E HAS SCREWS PULLED THROUGH SKIN AT XFS 178.750. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-2-1 FIG 4. 2L74 4F RT4A25 20041026000252004102600025 2004 10 26 UPS04142817 420040730A2565 SWITCH AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE STUCK A IPXAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01137UP 0810 AT DEPARTURE ENTRY DOOR SLIDE WARNING HORN & LT SOUNDED. RECONNECTED CONNECTOR ON ASPSU. RESET SLIDE TEST SWITCH ON DOOR HANDLE SLIDE. OPS CHECK NORMAL IAW AMM CH 25. 2L72 4F RTA35EU 20041026000262004102600026NM 2004 10 26 04FDEA02492 120040817A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 CORROSION ON FLOORBEAM BS 312 WL 208 LBL 3-47 AT FASTENER AND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM STA 312, W/L 208, LBL 3-47, AT FASTENER & NUT PLATE HOLES, REMOVED 5 X 2 INCH LBL 3 FROM .090. LBL 4 4 X 2 X .0015 INCH. LBL 20 6 X 2 X .005 INCH, LBL 47, 3 X 2 X .0020 INCH, FOUND TO BE IN LIMITS. REMOVED 3 X 2 X .015 FROM .090, OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS FROM BAC 1490-2730 7075- T6 .063 LOT 568596, FILLER 2024T3 .080 LOT 556309, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 51-30-02, FED EX SR 27-53-017A, FED EX MM 51-20-021-7, 51-30-151-7. 2L73 4F RTA3WE 20041026000272004102600027EU 2004 10 26 04FDEA02494 120040817A3260DSB11001 SENSOR AIRBUS310 A310222 3930315EU MLG FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25450FE 162 AFTER TAKEOFF GEAR WOULD NOT RETRACT WITH EITHER SYS, AIRCRAFT HAD SYMTEMS OF THINKING IT WAS STILL ON GROUND. AUTOPILOT INOP, CABIN PRESS REGULATORS INOP. AFTER BLOCK IN ACARS DIDN`T RECOGNIZE THAT AIRCRAFT HAD TAKEN OFF. T/S PROX BOX FAULT CODE ARE 05, 06, 07, 03, 04, 12, 13, 14, 10, 11, FAULTS ARE SYS 1 AND 2 GEAR PROX SENSORS. REMOVED AND REPLACED LANDING GEAR POSITION SENSOR SWITCH (10GB) ON 400VU PER 32-61-00-5. REPLACED BOGIE BEAM SENSORS 8GA, 9GA, 11GA AND 12GA PER M/M 32-00-00-4. PERFORMED NUMEROUS GEAR RETRACTIONS ON BOTH SYS 1 AND 2 WITH NO FAULTS. ACFT OK FOR SERVICE. 2L72 4F RTA35EU 20041026000302004102600030EA 2004 10 26 SWIA200413814 120040827A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07589SW3992 3992 7072 LT OUTBOARD SPOILERONS FAULT WITH SPOILERONS STATUS MESSAGE. REMOVED AND REPLACED LT OUTBOARD SPOILERON PCU IAW MM 27-82-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041026000322004102600032NM 2004 10 26 UPS04242965 120040803A5312 PANEL BOEING727 72722C 138400FNM LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, CRACK FOUND ON SKIN IN LT W/W I/B SKIN JUST BEHIND BRACKET FOR PLUMB BOB. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER IAW SRM 51-40-2. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2. 2L73 4F A3WE 20041026000342004102600034SO 2004 10 26 SIMA200427802 120040930A274032100801 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZONTAL STAB FAILED A SIMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW21620AE 145102 EN ROUTE TO LIT AIRCRAFT EXPERIENCED DUAL PITCH TRIM FAILURE. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20041026000352004102600035 2004 10 26 2004F00413 420041009A3442 TRANSCEIVER AIRBUS320 A320233 3930329EU WX RADAR SYS MALFUNCTIONED A RJEFA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO23464TA 1353 AFTER TAKEOFF, WEATHER RADAR 1 INOPERATIVE, NAV GPWS TERR DET FAULT AND NAV PRED W/S DET FAULT MESSAGES CAME ON ECAM. AIRCRAFT RETURNED TO IAH STATION. THE AIRCRAFT LANDED WITHOUT INCIDENT AND ON GRUOND IT WAS PERFORMED TEST OF THE WEATHER RADAR AND W/S SYSTEM PER AMM 34-41-00, RESULTS WERE NORMAL. ALSO RESET AND TEST OF THE GPWS WAS PERFORMED PER AMM 34-48-00. NO DISCREPANCIES WERE NOTED AND THE AIRCRAFT RETURNED TO OPERATION. (M) 2L72 4F RTA28NM 20041026000372004102600037 2004 10 26 GTIA040770 420040903A2565 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE MISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23808NK 49504 ACY - FOUND AFT SLIDE CONTAINER DEPLOYMENT LANYARD MANUAL DEPLOYMENT HAND STRAP AND TAILCONE DEPLOYMENT LANYARD IMPROPERLY INSTALLED. CORRECTED INSTALLATION OF CONTAINER AND TAILCONE DEPLOYMENT LANYARDS. ALSO, CORRECTED INSTALLATION OF MANUAL DEPLOYMENT HAND STRAP. (M) 2L72 4F RTA6WE 20041026000432004102600043EU 2004 10 26 BMAS040009 120040924A3350 BATTERY PACK BAG JETSTMJETSTM3101 1500215EU EMERGENCY LIGHT DISCHARGED A B16AK NONE L NO TEST ININSP/MAINT 1 NE05535PA 687 MAINTENANCE REPORTED THE TWO MOST FORWARD EMERGENCY LIGHTS ARE NOT ILLUMINATED. ALL OTHERS WORK. REMOVED FORWARD EMERGENCY LIGHT BATTERY PACKS. CLEANED TERMINAL CONTACTS AND REINSTALLED IAW J31 MM CH 33-50-10. PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHTING IAW J31 MM CH 33-50-00. FUNCTIONAL TEST GOOD. (M) 2L72 4T RTA21EU 20041026000472004102600047 2004 10 26 GTIA040760 420040829A2565 GIRT BAR DOUG DC9 DC983 3022083WP L2 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 FLL - FLT 702 - AFT GIRT BAR LOOSE ON L2. TIGHTENED SCREW AT ATTACHMENT POINT. (M) 2L72 4F RTA6WE 20041026000492004102600049WP 2004 10 26 GTIA040769 120040903A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2L72 4F A6WE 20041026000562004102600056EU 2004 10 26 ASOA04761 120040910A5315 FLOORBEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE FLOORBEAM AT FRAME 36 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AT FRAME 36 IAW SRM 51-25-01. (M) 2H72 4T RT 20041026000602004102600060EU 2004 10 26 ASOA04766 120040913A5330S5367240822800 DOUBLER AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK, THE DOUBLER SPLICE ON FRAME 39, STRINGER 14R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER SPLICE ON FRAME 39, STRINGER 14R IAW SRM 51-25-01. (M) 2H72 4T RT 20041026000612004102600061EA 2004 10 26 ASOA04678 120040907A3350110049 CHARGER CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11702EV 10035 DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY PACK CHARGER ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041026000632004102600063WP 2004 10 26 GTIA040786 120040901A55205930497502 TAB DOUG DC9 DC981 3022081WP RT ELEVATOR DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FOUND RIGHT ANTI-FLOAT TAB DELAMINATED AT OUTBOARD TIP. REMOVED RT ELEVATOR ANTI-FLOAT TAB. INSTALLED RT ELEV ANTI-FLOAT TAB. (M) 2L72 4F A6WE 20041026000642004102600064 2004 10 26 USAASA04050 420040525A2565 LANYARD AIRBUSA319 A319112 3930323EU SLIDE ASSY MISSING A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19710UW 1019 THE ESCAPE SLIDE RELEASE LANYARD AND SURVIVAL KIT LANYARD WERE FOUND NOT INSTALLED, ON THE SLIDE IN THE L1 DOOR POSITION, WHEN SLIDE WAS REMOVED FOR ACCESS DURING THE HEAVY MAINTENANCE VISIT. MAINTENANCE REPLACED THE SLIDE ASSEMBLY. OK FOR SERVICE. THE SHOP REPLACED MISSING STRAPS. (M) 2L72 4F RTA28NM 20041026000652004102600065SO 2004 10 26 SIMA200427910 120041002A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO HORIZONTAL STAB INOPERATIVE A SIMAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SW21808AE 145519 ON FINAL APPROACH CREW RECEIVED PITCH TRIM 1-2 INOPERATIVE ON EICAS. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026000672004102600067NE 2004 10 26 GTIA040768 220040901A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23826NK 49391 726974 FOUND INDICATOR FOR BEARING NR 4 AND NR 5 TEMP IND BLACK. REMOVED AND REPLACED NR 2 ENGINE. (M) 2L72 4F4 FRTA6WE E9NE 20041026000692004102600069WP 2004 10 26 GTIA040781 120040915A7160 NOSE COWL DOUG DC9 DC983 3022083WP NR 1 ENGINE DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 NR 1 ENGINE INLET COWL INNER BARREL 'DYNA RONR' WOVEN WIRE MESH DELAMINATING 3 O'CLOCK TO 9 O'CLOCK. INSTALLED CONDITION 2 REPAIR ON LEFT NR 1 ENGINE LOWER NOSE COWL, C/O NR 254595-2. (M) 2L72 4F RTA6WE 20041026000722004102600072NM 2004 10 26 UIEA200400177 120040924A31101201 LATCH BOEING747 7472F6B 1384807NM INSTRUMENT PANELLOOSE A UIEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA15534MC 21832 GROUND ABORT F/O'S FORWARD INSTRUMENT PANEL CAME OUT ON TAKEOFF ROLL. ABORTED AT 60 KNOTS. RESECURED F/O'S FORWARD INSTRUMENT PANEL IAW MM 31-10-00. ALL INSTRUMENT, OPS CHECK GOOD. (M) 2L74 4F A20WE 20041026000762004102600076WP 2004 10 26 GTIA040778 120040912A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2L72 4F A6WE 20041026000802004102600080SO 2004 10 26 SIMA200427806 120040928A331018261 POTENTIOMETER EMB 135 EMB135KL 3260302SO COCKPIT LIGHTS INOPERATIVE A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW21848AE 145710 DCA - FLT 4753 - ELECTRICAL SMELL IN COCKPIT WITH POPPED OVERHEAD LIGHT CIRCUIT BREAKER ISSUED MEL 33-1. REPLACED NR 1 COCKPIT OVERHEAD LIGHT DIMMER SWITCH, MEL CLOSED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026000812004102600081WP 2004 10 26 GTIA040777 120040912A3260833703 PROXIMITY SENSOR DOUG DC9 DC982 3022082WP LT MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CRCRUISE 1 GL23817NK 49141 LGA - FLT 7501 - THE LEFT LANDING GEAR UNAFE LIGHT IS ILLUMINATED RED WITH AURAL WARNING. T/S THE MLG POSITION INDICATION AND DETERMINED THE MLG DOWN AND LOCKED SENSOR HARNESS INCORPORATED DEFECTIVE SPLICES. REMOVED AND REPLACED THE PROX SENSOR AND HARNESS COMPLETE. (M) 2L72 4F A6WE 20041026000822004102600082NE 2004 10 26 GTIA040780 220040911A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217A 52053NE LEFT VIBRATION A GTIAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL23810NK 48015 708572 FLT 197 - LGA - LEFT ENGINE UNUSUAL NOISE AND VIBRATION ON CRUISE POWER CHECK (L) HYD PUMP OFF PACK (L) OFF AND NOT CHANGES. REMOVED AND REPLACED NR 1 ENGINE. (M) 2L72 4F4 F A6WE E9NE 20041026000832004102600083WP 2004 10 26 GTIA040783 120040916A3220 STRUT DOUG DC9 DC983 3022083WP NLG UNDERSERVICED A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23835NK 53044 MCO - FLT 927 - AIR RETURN BACK TO MCO, DUE TO THE NOSE WHEEL WOULD OT FULLY RETRACT AFTER TAKEOFF. INSPECTED NOSE GEAR AND FOUND STRUT UNDERSERVICED. SERVICED PER MM 32-21-02, LEAK CHECK GOOD. PERFORMED NLG RETRACTION TEST. NLG STRUT PISTON DID REQUIRE SEVERAL WIPE DOWNS TO CLEAN GRIT FROM CHROME. (M) 2L72 4F RTA6WE 20041026000862004102600086WP 2004 10 26 GTIA040759 120040828A5210 LATCH DOUG DC9 DC983 3022083WP L1 DOOR CONTAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23808NK 49504 MYR - FLT 1582 - FOUND LATCH ON L1 DOOR HARD TO OPEN AND SET IN GUST LOCK. CLEANED DEBRIS FROM DOOR OPEN LATCH ON L1 DOOR. (M) 2L72 4F RTA6WE 20041026000872004102600087WP 2004 10 26 GTIA040773 120040906A1420 CONNECTOR DOUG DC9 DC983 3022083WP FIRE LOOP DAMAGED A GTIAO OTHER N FALSE WARNING DEDESCENT 1 GL23831NK 49617 FLT 912 - MCO - ON DESCENT INTO ORD PASSING 12,000 LEFT ENGINE FIRE DETECTOR LOOP B-LOOP LIGHT CAME ON. SWITCHED TO LOOP 'A' TESTED OK. REMOVED LOOP 'B' ELEMENT CONNECTORS. CLEANED AND REINSTALLED. (M) 2L72 4F RTA6WE 20041026000902004102600090EA 2004 10 26 A6WA200440141 120041001A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31435AW 7724 FOUND CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHORING NUTS IN AREA OF CARGO DOOR OPENING. (M) 2L72 4F RTA21EA 20041026000912004102600091SO 2004 10 26 SIMA200426903 120040901A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 ABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMGAED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4061B DATED AUGUST 31, 2004. (M) 2L72 4F RTT00011AT 20041026000922004102600092EU 2004 10 26 ASOA04764 120040911A5310 CREASE BEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE RIGHT CREASE BEAM BETWEEN FRAME 39/40 WAS FOUND TO CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT CREASE BEAM BETWEEN FRAME 39/40 IAW SRM 51-25-03 AND 51-25-01. (M) 2H72 4T RT 20041026000962004102600096EU 2004 10 26 ASOA04755 120040909A5347NTA44768 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 13 TO FRAME 17 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SEAT TRACK BETWEEN FRAME 13 TO 17 IAW SRM 53-00-00. (M) 2H72 4T RT 20041026001012004102600101SO 2004 10 26 SIMA200426902 120040902A273014569409601 DAMPENER EMB 135 EMB135LR 3260305SO LT AILERON DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21731BE 145356 DURING AN IMBV INSPECTION, THE LEFT AILERON DAMPENER FITTING WAS FOUND DAMAGED. REMOVED THE DAMGAED FITTING AND INSTALLED NEW FITTING IAW EMB SERVICE BULLETIN 145-27-0061. (M) 2L72 4F RTT00011AT 20041026001022004102600102WP 2004 10 26 GTIA040789 120040927A3213 STRUT DOUG DC9 DC982 3022082WP NLG DAMAGED A GTIAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL23801NK 48048 ACY - FLT 1174 - AFTER TAKEOFF FELT RUMBLE WHICH FELT LIKE NOSE GEAR DOOR NOT CLOSING. RECYCLED NOSE GEAR AND UNSAFE LIGHT ILLUMINATED. PER MNCTL DIRECTION, RECYCLED GEAR AGAIN, LIGHT CAME ON AND THEN WENT OUT. CONTINUED FLIGHT. SERVICED NOSE STRUT. ALL OTHER INSPECTIONS, NO FAULTS FOUND. (M) 2L72 4F A6WE 20041026001052004102600105GL 2004 10 26 SIMA200427801 220040928A72008166243 THERMOSTAT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21709GB 145211 BURNING SMELL IN COCKPIT WHEN ANTI-ICE KICKED ON. ALSO, BLEED 1 OVERTEMP CAME ON WHEN ICE PROTECTION CYCLED. REMOVED AND REPLACED NR 1 ENGINE FAN AIR CONTROL THERMOSTAT IAW EMB 135 MM 36-11-06. OPS CHECK GOOD. PERFORMED OPERATOINAL CHECK OF ANTI-ICING SYSTEM IAW EMB 135 MM 30-00-00-700-802 A WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20041026001112004102600111WP 2004 10 26 AALA20041057 120041011A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 FORWARD NR 1 GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD NR 1 GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 F A6WE E9NE 20041026001122004102600112WP 2004 10 26 AALA20041058 120041011A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 FORWARD NR 1 SPOT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD NR 1 SPOT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 F A6WE E9NE 20041026001192004102600119EU 2004 10 26 2004UALA00622 120040628A5310 DOOR FRAME AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY DEFORMED A UALAK NONE O OTHER ININSP/MAINT 1 WP29419UA 487 FWD LOWER E AND E DOOR FWD FRAME SECTION AND CENTER INTERCOSTAL JUST FWD OF DOOR HANDLE DEFORMED DUE TO IMPACT WITH TOW BAR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FRAME AND INTERCOSTAL REPLACED. 2L72 4F4 FRTA28NM E40NE 20041026001202004102600120NM 2004 10 26 2004UALA00925 120041010A5753 HINGE FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29655UA 25393 LT WING IB FLAP OB HINGE FITTING CRACKED AFT VANE. SUPPLEMENTAL DATA UPDATE REPAIRED FITTING WITH ANGLE AND FILLER REPAIR. 2L72 4F4 FRTA1NM E24NE 20041026001212004102600121NM 2004 10 26 2004UALA00937 120041013A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29902UA 25002 RT FUSELAGE SKIN BELOW THE AFT CARGO DOOR FROM STA 820 TO 835 BETWEEN STR 25R AND 26R HAS SEVERAL BLEND OUTS. INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20041026001222004102600122SO 2004 10 26 C2XA04IA135 120041019A3397375921 WIRE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL EMERGNECY LIGHT LOOSE A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2714942 145037 CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS INOPERATIVE. RESECURRED THE WIRE AT THE LIGHT. OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20041026001262004102600126NM 2004 10 26 DL73G040979 120041013A2431 CHARGER BOEING737 73735B 13844BMNM GE CFM56 CFM56* 13802NE BATTERY PACK UNSERVICEABLE A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27224DA 105257 24269 CREW REPORTED SMELL IN COCKPIT. BATTERY OVERHEATED AND VOLTAGE APPROXIMATELY 18 VOLTS. SMOKE COMING FROM TOP OF BATTERY. REPLACED BATTERIES AND CHARGER. 2L72 4F4 FRTA16WE E2GL 20041026001272004102600127NM 2004 10 26 04FDEA02953 120041019A5310 YOKE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY HAS DAMAGE, TRANSVERSE FRAME. MAIN CARGO DECK STA 535 LT 9G NET YOKE ASSY ATTACHED TRANSVERSE FRAME, FLANGE DAMAGED AREAS AT 02 LOCATIONS, TRIMMED AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503. 2L73 4F4 FRTA22WE E13NE 20041026001282004102600128SO 2004 10 26 C2XA04BT108 120041013A335037591 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716919 145393 DURING INSPECTION FOUND CENTER AISLE EMERGENCY LIGHT AT ROW 12 INOPERATIVE. REMOVED THE CENTER AISLE EMERGENCY LIGHT ASSY. OPS CHECK OK. 2L72 4T4 FRTT00011ATTE6CH 20041026001302004102600130EU 2004 10 26 DHL2004363517 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING-C CHECK, DISCREPANCY AS FOLLOWS, N/R 3876, FR. 34 TO FR. 38.2 RBL 78 SEAT TRACK FLANGES OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR34 TO FR38.2 RBL 78 IAW A-300 SRM 53-10-20 / 51-30-30. INSTALLED NEW SEAT TRACK FROM FR34 TO FR38.2 AT RBL 78 IAW A-300 SRM 53-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLY WHITE IAW SRM 51-40-10 AND SRM 51-40-12. MATERIAL USED, 60-22457, PO NR 243002234. 2L72 4F4 FRTA35EU E23EA 20041026001312004102600131SO 2004 10 26 C2XA04SH507 120041001A532014530644405 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING VISUAL INSPECTION AT C-CHECK LT OMEGA BEAM AT FRAME 38 WAS CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01157 AND SRM 53-21-10. 2L72 4F4 FRTT00011ATTE6CH 20041026001362004102600136EA 2004 10 26 QXEA200400721 120041014A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 COCKPIT FLOORBEAM WITH CAMLOCK RECEPTACLES ON IT AT JUST FORWARD OF FS 280 HAS CORROSION ON TOP OF C CHANNEL. REPAIRED IAW REO 670-53-1-095 AND SRM 51-42-06-001-001. 2L72 4F4 FRTA21EA EOOO63EN 20041026001382004102600138EU 2004 10 26 DHL2004363520 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, 3891, FR18 - FR26.5 RBL 38 INCH MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR18 - FR26.5 AT RBL 38 INCH IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR18 - FR26.5 AT RBL 38 INCH IAW SRM 53-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLYWHITE IAW SRM 51-40-10 AND A-300 51-40-12. MATERIAL USED 60-22457, PO NR 24302234. 2L72 4F4 FRTA35EU E23EA 20041026001432004102600143EU 2004 10 26 DHL2004363524 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, N/R, 3870 FR. 30 - FR 35 LBL 36 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 30 TO FR. 35 AT LBL 36 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 30 - FR. 35 AT LBL 36 IAW A-300 SRM 53-10-10 / 51-10-40. 2L72 4F4 FRTA35EU E23EA 20041026001462004102600146NM 2004 10 26 UPS04443377 120040923A5712 RIB BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C, RT WING L/E OLES 1453 NR25 VC FLAP OB ROTARY IB SUPPORT RIB FWD MOUNT HOLE CRACKED. RT WING L/E OLES NR25 VC FLAP OB ROTARY ACTUATOR IB SUPPORT RIB REPAIRED IAW HX RSNR R-57-41-35205, DVI THE AFFECTED AREA AT C- CHECK INTERVALS NOT TO EXCEED 18 MONTHS FOR SIGNS OF CORROSION, CRACK AND DEGRADATION OF SUBJECT REPAIR. IAW UPS EO NR B747-5740-21181 APPENDIX A FOR REFERENCE. 2L74 4F4 F A20WE E20EA 20041026001472004102600147EA 2004 10 26 04293639 120041019A3230 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27639BR 7313 EVENT SUMMARY STATED GEAR DISAGREE MSG AFTER TAKEOFF. NOSE GEAR WILL NOT RETRACT.REMOVED AND REPLACED MLG PRIORITY VALVE. 2L72 4F4 FRTA21EA E15NE 20041026001482004102600148SO 2004 10 26 CHQA000570 120041019A3350 BULB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11290SK 145474 LT SIDE ADT EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED LT AFT EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20041026001512004102600151SO 2004 10 26 CHQA000571 120041021A3350 LIGHT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11844RP 145620 EMERGENCY FLOOR LIGHTING NEXT TO SEAT 7A AND 8A IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP NEXT TO SEAT 7A AND 8A IAW AMM 33-50-12. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20041026001532004102600153NM 2004 10 26 UPS04543375 120041020A7110 ACCOUSTIC LINER BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE RT ENGINE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01458UP 25479 INSPECTION TYPE: N/A MECHANIC INSPECTION, RT ENG NOSE COWL ACOUSTIC MESH LINER DELAMINATED. REMOVED DEBRIS FROM IGV ACCOMPLISHED BOROS INSPECTION IP AND HP COMPR IAW M/M 72-00-00-6. FOUND SINGLE BLADE IP 2 BENT WITHIN LIMITS IAW M/M 72-00-00 PARA 03. 2L72 4F4 FRTA2NM E12EU 20041026001552004102600155NM 2004 10 26 CALA0400686 120041023A53156545815 FLOORBEAM BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712327 23457 INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 344, RBL 45 TO LBL 12. THE CORRODED AREA OF FLOORBEAM UPPER CHORD WAS REMOVED AND A NEW UPPER CHORD AND SPLICES WERE INSTALLED IAW SRM 53-10-51. 2L72 4F4 FRTA16WE E2GL 20041026001572004102600157NE 2004 10 26 CALA0400682 220041019A7200 LINE BOEING777 777224 1385225NM GE GE90 GE9090B NE NR 2 ENGINE CLOGGED A CALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2778005 27581 900283 NR 2 ENG INDICATED A RAPID LOSS OF OIL, FOLLOWED BY LOW OIL PRESSURE IND. CREW SHUTDOWN NR 2 ENG & DIVERTED FLT, LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND NR 2 ENG C-SUMP LINE CLOGGED WITH COKE AT 9 O'CLOCK STRUT UNDER AFT CENTER BODY. LINE CLEARED. ENGINE SERVICED & RUN AT IDLE & PART POWER FOR 5 MINS. OPS CHKD GOOD WITH NO LEAKS NOTED. NR 2 ENG REMOVED FOR TROUBLESHOOTING & TEARDOWN TO DETERMINE CAUSE OF FAILURE. COKE SHEDDING OCCURRED WHICH LEADS TO COKE BUILD-UP & RESULTED IN CLOGGING OF C-SUMP LINE. SEVERAL CORRECTIVE ACTIONS WERE IMPLEMENTED AS A RESULT OF THIS FAILURE INCLUDING MONITORING LEVELS OF COKE SHEDDING & INCREASED EMPHASIS ON ENG MX REGARDING CLEANING & INSP OF BEARING COMPARTMENTS 2L72 4F4 FRTT00001SEE00049EN 20041021000872004102100087WP 2004 10 21 AALA20041043 120041008A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21262AA 49290 DFW - EMERGENCY LIGHTS FOR SEAT ROWS 19 AND FORWARD INOPERATIVE. REPAIRED WIRING UNDER SEAT ROW TRACK 9 FOR EMERGENCY LIGHTS FOR SEAT ROWS 19 AND FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021000942004102100094WP 2004 10 21 AALA20041024 120041005A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219302B 49528 PHX - EMERGENCY LIGHTS IN AFT RIGHT LAVATORY INOPERATIVE. REPLACED BATTERY B527 FOR EMERGENCY LIGHTS AT AFT RIGHT HAND LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041021000972004102100097WP 2004 10 21 AALA20041027 120041006A3350 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21458AA 49563 DFW - RIGHT HAND EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. CLEANED AND RESEATED CONNECTORS ON RIGHT HAND AFT EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021001062004102100106WP 2004 10 21 AALA20041052 120041016A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170404 49315 RDU - EMERGENCY EXIT LIGHTS IN FIRST CLASS CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR EMERGENCY EXIT LIGHTS IN FIRST CLASS CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041021001102004102100110CE 2004 10 21 GLBA20030706 120040830A5320 BRACKET BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03192GL UE192 LEFT L-BRACKET PATCH CRACKED FUSELAGE SKIN MEETS DORSAL FIN AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACED L-BRACKET PATCH REF EO 04-VE192-02. 2L72 4T RTA24CE 20041021001122004102100112NM 2004 10 21 SWAA043034 120041019A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 847, RBL 18, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041021001142004102100114NM 2004 10 21 SWAA042990 120041016A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING THRU CHECK FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 466 AND BS 470, ABOVE STRINGER 16R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041021001162004102100116 2004 10 21 SWAA042992 420041016A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29617SW 27700 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041021001182004102100118NM 2004 10 21 SWAA042994 120041016A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041021001192004102100119NM 2004 10 21 SWAA042995 120041016A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041021001212004102100121NM 2004 10 21 SWAA043025 120041018A531165C25230 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, FROM RBL 8.10 TO RBL 13.80, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041021001232004102100123NM 2004 10 21 SWAA042996 120041016A53126546568582 STRUCTURE BOEING737 7373H4 1384600NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND 2 EACH CRACKS AT AFT PRESSURE BULKHEAD Y-CHORD AT BS 1016, STRINGER 6L AND STRINGER 6R. REPAIRED Y-CHORD SECTIONS PER EA. 2L72 4F RTA16WE 20041021001252004102100125NM 2004 10 21 SWAA042969 120041013A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29406WN 27894 FWD RT EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041021001262004102100126NM 2004 10 21 SWAA042970 120041013A3350101331 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041021001272004102100127 2004 10 21 SWAA042971 420041013A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041021001282004102100128NM 2004 10 21 SWAA042972 120041013A57536546431280 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20041021001292004102100129 2004 10 21 SWAA042973 420041013A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041021001302004102100130NM 2004 10 21 SWAA042974 120041013A53116546529 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29396SW 27690 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041022000072004102200007EA 2004 10 22 SWIA200413911 120041007A2750 CONTROL CABLE CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07973SW 7949 AFTER T/O, FLAP FAIL CAUTION MSG APPEARED. RIGGED BPSU PER MM 27-51-10-830-801. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000452004102200045EA 2004 10 22 SWIA200413962 120041005A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW TRANSVERSE BEAM UPPER FLANGE CRACKED AT STA 280 LBL 9. ITEM FOUND AT C-CHECK INSPECTION. BEAM REPAIRED IAW CRJ REO 601R53-11-136. REV "NC". 2L72 4F RTA21EA 20041022000522004102200052EA 2004 10 22 SWIA200413782 120040904A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07978SW 7953 MACH TRIM WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ MM 27-41-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000592004102200059SO 2004 10 22 SWIA200413849 120040921A2150 RCCB EMB 120 EMB120ER 3260203SO LT A/C PACK MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07581SW 120349 ON DESCENT INTO IAH, NOTICED BURNING SMELL IN COCKPIT. SHORTLY AFTER, THERE WAS AUDIBLE CHATTER IN WHAT SOUNDED LIKE A RELAY OPENING/CLOSING. REPLACED LEFT PACK RCCB. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041022000602004102200060EA 2004 10 22 SWIA200413850 120040923A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07960SW 7853 DURING CRUISE GOT THE FLIGHT SPOILERS STATUS MESSAGE. AFFECTED THE RIGHT INBOARD FLIGHT SPOILERON. REMOVED AND REPLACED RIGHT INBOARD FLIGHT SPOILER PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000612004102200061EA 2004 10 22 SWIA200413851 120040919A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07961SW557 557 7857 STAB CH1 INOP AND MACH TRIM MESSAGES IN CLIMB (FL240). CLEANED BOTH TRIM SWITCHES AND REPLACED HSTCU IAW CRJ MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000682004102200068NM 2004 10 22 P5CA0401249 120041011A5311 FRAME BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 AFT CARGO COMPT SECONDARY FRAME B/W STA 1740 & 1760 LBL 30 IS CRACKED. REMOVED DAMAGE FRAME & INSTALLED NEW FRAME PER SRM 51-30-02. 2L74 4F4 F A20WE E20EA 20041022000712004102200071CE 2004 10 22 231042 120040816A3397 CONTROL PANEL BEECH 1900 1900D 1154162CE WIND DEICE SMOKE A NSVAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27152MJ UE52 SMOKE COMING FROM WING ICE CIRCUIT BREAKER PANEL, PULLED BREAKER APPEARED TO STOP SMOKING. MAINTENANCE OPENED PANEL RIGHT SIDE & CORROSION NOTED, CLEANED CORROSION, REMOVED CIRCUIT ON WING ICE LIGHT, MOVED HARD WIRE BRIDGE ICE WING LIGHTS, NOTED INOP WING ICE LIGHT MEL 33-11. 2L72 4T RTA24CE 20041022000722004102200072NM 2004 10 22 SWAA043036 120041019A531165C25229 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727D, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041022000762004102200076NM 2004 10 22 F3LA200400086 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON OTBD SIDE OF LBL 5.7 BELOW WL 207 ON 178 BULKHEAD. REPAIRED CRACKS ON 178 BULKHEAD BELOW WL 207 PER EA B3-53R-10470 AND SRM 53-10-08 FIG 210. 2L72 4F RTA16WE 20041025000042004102500004EA 2004 10 25 SWIA200413854 120040923A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07595SW 7292 DURING TAKEOFF FROM ABQ, AT AN ALTITUDE OF 450 FT AGL THE STAB TRIM AND MACH TRIM DISCONNECTED AS SOON AS THE FLAPS WERE MOVED FROM 20 DEGREES TO 8 DEGREES. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR, MCU AND STAB TRIM SWITCH IAW 27-46-00, 27-42-61, 27-42-05, 27-42-05. PERFORMED OPERATIONAL CHECKS IAW 27-40-00, 27-42-04, 27-42-05. P/N 7062-3, S/N OFF 63. 2L72 4F RTA21EA 20041025000132004102500013EA 2004 10 25 SWIA200413786 120040906A274170623 MOTOR CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07961SW5636 5636 7857 STAB TRIM CHANNEL 1 DISENGAGED IN FLIGHT. REPLACED MOTOR CONTROL UNIT FOR STAB TRIM. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000142004102500014SO 2004 10 25 SWIA200413787 120040909A3350 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07579SW 120347 AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE FOR EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000242004102500024EA 2004 10 25 SWIA200413964 120041005A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 CLIP AT FS 202.75 AND LEFT STRINGER 21 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-23-00. 2L72 4F RTA21EA 20041025000292004102500029EA 2004 10 25 SWIA200413755 120040823A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07453SW 7743 FS 625 RIGHT HAND INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20041025000522004102500052EA 2004 10 25 SWIA200413819 120040919A2760270003 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOIL MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07407SW1244212442 7034 LEFT INBOARD SPOILERON PCU SPOOL FAIL. REMOVED AND REPLACED SPOILERON INBOARD PCU IAW 27-62-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000532004102500053EA 2004 10 25 SWIA200413820 120040920A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07438SW4767 4767 7574 STAB CHANNEL 1 INOPERATIVE. INSTALLED SERVICEABLE HORIZONTAL ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 183. 2L72 4F RTA21EA 20041025000572004102500057EA 2004 10 25 SWIA200413824 120040918A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07448SW 7678 TEST NR 2 FOR CARGO OVERHEAT CONTINUALLY INDICATED A (OVERHEAT) FIRE. NO (OVERHEAT) FIRE WAS OBSERVED AND NO SMOKE. REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW MM 26-15-01. OPERATIONAL CHECK GOOD. P/N 473597-19, S/N OFF 1839. 2L72 4F RTA21EA 20041025000702004102500070NE 2004 10 25 SWIA200413835 220040919A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT POWER LOSS A SWIAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 NM07408SW8525 8525 7055 807249C LEFT ENGINE QUIT AT 500 FT AGL ON APPROACH INTO SLC. N1 AND N2 ROLLED BACK AND ITT WENT RED. REMOVED AND REPLACED ENGINE ASSY IAW MM 71-00-00, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041025001062004102500106NM 2004 10 25 P5CA0401241 120041004A27821267629 PDU BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL LE FLAPS MALFUNCTIONED A P5CAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 WP23453PA 30811 A/C RETURN TO BLOCK DUE TO EICAS MESSAGE FLAP PRIMARY, FLAP DRIVE FOLLOWED BY STATUS MESSAGE L/E MULTI DRIVE, FLAP SYSTEM MONITOR. REPLACED NR 2 RIGHT HAND LED PDU & TESTED ELECTRICALLY NORMAL. 2L74 4F4 FRTA20WE E23EA 20041025001852004102500185NM 2004 10 25 SWAA043050 120041021A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29372SW 26599 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041025001872004102500187NM 2004 10 25 SWAA043052 120041021A533065457654 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041025001892004102500189NM 2004 10 25 SWAA043066 120041021A53116546540 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 616, LBL 65, WL 200, CRACKED. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20041025001912004102500191 2004 10 25 SWAA043055 420041021A256563550 SLIDE BOEING737 7377H4 1384404NM R1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED HC2D CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041025001942004102500194NM 2004 10 25 SWAA043058 120041021A57536546435236 SKIN BOEING737 7372H4 138448CNM RT WING FLAP DEBONDED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 RIGHT WING OUTBOARD AFT T/E FLAP DEBONDING. REMOVED AND REPLACED OUTBOARD AFT T/E FLAP PER MM. 2L72 4F A16WE 20041026000012004102600001NE 2004 10 26 MALA040542 220040828A7200200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 MALFUNCTIONED A MALAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15519XJ E2344 NR 2 ENG FIRE INDICATION AFTER T/O ENG WAS SHUT DOWN AND EXT NR 1 BLOWN, QRH COMPLETED. A/C FERRIED FROM PHL TO MSP FOR REPAIRS TO NR 2 ENGINE AND FIRE SEAL COWL AREA. FOUND EVIDENCE OF EXCESSIVE HEAT NEAR FUEL AND LUBE LINE AT 6 O`CLOCK POSITION, APPEARS TO BE COMING FROM COMBUSTION CHAMBER, ALSO HAS DAMAGE TO FIRE SEAL. THIS A/C WAS INSPECTED IAW MESABA REQUIREMENTS AS LISTED ON ENG. FERRY TASK CARD AND WAS SAFE 4 A 1 TIME FERRY FLIGHT. ALSO REMOVED & REPLACED NR 2 ENG ASSY P/N ON/OFF 2-003-040-15, S/N OFF PO7768, S/N ON PO7865 IAW JOB CARD 7100-502, REPLACED ZONE 2 COWL ASSY P/N ON/OFF HC711H0500-092B, S/N OFF SB/BAE1421, S/N ON SB/BAE1433 IAW AMM 71-10-17, 201. ALL CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20041026000022004102600002EU 2004 10 26 MALA040541 120040827A2612 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 ENGINE FALSE INDICATIONA MALAFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15519XJ E2344 NR 2 ENGINE FIRE INDICATION AFTER TAKEOFF. EMERGENCY CHECKLIST COMPLETED. NR 2 ENGINE NR 1 EXTINGUISHER USED . AIRBORNE APPROX 7 MINS. AFTER ENGINE SHUTDOWN TO TOUCHDOWN. MX PERFORMED FDAMS DOWNLOAD. FIRE EVENT=NO CHANGE IN ENG PARARMETERS, NR 2 ENG. WINDMILLED 3.1 MIN NO PSI, NH BELOW 2 PERCENT=5 SEC NL BELOW 2 PERCENT=NONE. C/W ENG MM 72-00-00 INSP/CHK-09 PG 802 PARA 1C. ALL CHECKS GOOD. VISUAL ENGINE, OPS/ELEC CHKS DETECT SYS, ALL GOOD. REMOVED AND REPLACED NR 2 ENG (1) FIRE BOTTLE, NO C/B'S POPPED. NO DOWELS EYES FLAGGED. R&R PCB (WA3). ALL WORK DONE IAW MM. OPS CHECK FIRE DETECT & EXTINGUISH SYS ALL GOOD. GROUND RAN ENG FOR 1 HOUR, NO DISCREPANCY'S NOTED. 2H74 4F4 FRTA49EU E6NE 20041026000062004102600006NM 2004 10 26 SWAA043063 120041021A57546573714 SKIN BOEING737 7373T5 1384608NM LT WING SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED. REPAIRED NR 1 L/E SLAT PER SRM. 2L72 4F RTA16WE 20041026000122004102600012EU 2004 10 26 AWXA200400939 120040805A5320D53480048202 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW 054 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL UPPER OUTBOARD SCUFF PLATE ATTACH FITTING BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED L-2 DOOR SHAPE SILL FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SHAPE SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041026000142004102600014NM 2004 10 26 UPS04242994 120040730A5754 RIB BOEING727 72722C 138400FNM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, NR 6 SLAT I/B RIB AT ACTUATOR ROD END IS CRACKED. ROD END DISCONNECTED IAW MM 27-81-32. ROD END RIBS DERIVETED IAW SRM 51-30-02. RIBS REMOVED IAW SRM 51-30-02. ON REMOVAL O/B RIB AND CENTER CHANNEL FOUND CRACKED. NEW CENTER CHANNEL, I/B AND O/B RIBS INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20041026000222004102600022WP 2004 10 26 UPS04842865 120040715A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C, FUSELAGE EXTERIOR SKIN IS CRACKED AT STATION 1745 AT LONGERON 15R. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER, FINGER DOUBLER IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20041026000232004102600023WP 2004 10 26 UPS04842866 120040702A53474755395 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, SEAT TRACK-C HAS WORN LUGS AND SCALLOPS BETWEEN FS 1300-1315 (DOT D976). BLENDED OUT OF LIMITS IAW DC8 SRM 53-2-3. DIMENSION AFTER BLEND OUT OUT OF LIMITS. REMOVED DAMAGE FROM SEAT TRACK MAT ID FOR PLUG 7452952 -3 MAT ID FOR SEAT TRACK CH 7452952-7. LOCATED, DRILLED, DEBURRED PLUG AND CHANNEL. ALODINED AND PRIMED. INSTALLED PLUG IAW DC8 SRM 51-3-0, 53-2-3, 53-7-1, 51-2-0. 2L74 4F RT4A25 20041026000392004102600039SO 2004 10 26 SIMA200427204 120040926A27403621005009MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZONTAL STAB INOPERATIVE A SIMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW21681AE 14500824 ON FINAL TO ORD WITH FLAPS AT 9 DEGREES AND SPEED BRAKES TRANSFERRING OPEN TO CLOSE, RECEIVED EICAS MESSAGE PITCH TRIM MAIN INOP AND PITCH TRIM BACK UP FAIL. CHECKLIST PROCEDURES FOLLOWED AND MESSAGE CLEARED. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20041026000482004102600048WP 2004 10 26 GTIA040785 120040830A5310 DOOR FRAME DOUG DC9 DC981 3022081WP FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 FTW - FOUND AFT PIT DOOR JAM CORROSION. REMOVED CORROSION. FABRICATED DOOR BEAM REPAIR. INSTALLED REPAIR PARTS. (M) 2L72 4F A6WE 20041026000532004102600053SO 2004 10 26 SIMA200426909 120040923A335078812 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21648AE 145225 CREW REPORTED THE EMEGENCY LIGHT POSITION 3 IN CABIN TO BE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AND CHARGER AT POSITION 3 BUT DID NOT FIX THE PROBLEM. THE LIGHT STRIP WAS REPLACED AND AN OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20041026000572004102600057NM 2004 10 26 GAIA04168OP 120040930A32301U1085 SEQUENCE VALVE BOEING727 7272J0 138407ENM LT MLG CRACKED A GAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07284KH 21108 FLT 715 - ELP-FWA - ON TAKEOFF DURING GEAR RETRACTION THE FLIGHT CREW NOTICED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ELP WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND LEFT MLG SEQUENCE VALVE LEAKING FROM A CRACK IN THE HOUSING. REMOVED AND REPLACED SEQUENCE VALVE AND NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND FILTERS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20041026000702004102600070WP 2004 10 26 GTIA040779 120040911A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE ASSEMBLY. (M) 2L72 4F A6WE 20041026000732004102600073SO 2004 10 26 SIMA200426906 120040917A532014522178005 SILL EMB 135 EMB135LR 3260305SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21732DH 145358 ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB REPAIR STATEMENT IC 2003/145-0818 DATED MARCH 6, 2003, AND AMERICAN EAGEL ENGINEERING TECHNICAL NOTICE EB 53-009. (M) 2L72 4F RTT00011AT 20041026000782004102600078WP 2004 10 26 GTIA040775 120040827A2560 LENS DOUG DC9 DC981 3022081WP SMOKE GOGGLES CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 F/O'S SMOKE GOGGLE LENS CRACKED (2) ALL 3 GOGGLES NEED BAG REPLACED. REMOVED AND REPLACED F/O'S SMOKE GOGGLES. (M) 2L72 4F A6WE 20041026000852004102600085EA 2004 10 26 REXA04019 120041007A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258733G4394 7733 FLAPS FAIL ON APPROACH. EMERGENCY DECLARED QRH FOLLOWED ZERO FLAP LANDING UNEVENTFUL. RESET SYSTEM PER AD 98-20-01, FLAPS PLACED ON 72 HOUR WATCH. (M) 2L72 4F RTA21EA 20041026000972004102600097EU 2004 10 26 ASOA04756 120040910A5311 DOUBLER AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DUIRNG A C-CHECK IN YUL, THE DOUBLER ON FRAME 40, STRINGER 17L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON FS 40, STRINGER 17L IAW SRM 51-25-01. (M) 2H72 4T RT 20041026001062004102600106NM 2004 10 26 GTIA040788 120040924A3260 UPLOCK SENSOR DOUG MD80 MD83 3023681NM LT MLG MALFUNCTIONED A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23822NK 49392 DTW - FLT 706 - DURING CLIMB, AFTER RETRACTION LEFT GEAR UNSAFE LIGHT. REMOVED AND REPLACED LEFT MLG UP AND LATCH SENSOR P/N 833605, PROX BOX P/N 833703 AND PROX SWITCH. (M) 2L72 4F RT 20041026001072004102600107 2004 10 26 GTIA040772 420040830A2565 GIRT BAR DOUG MD80 MD83 3023681NM ESCAPE SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 DTW - FOUND L2 DOOR SLIDE GIRT BAR HOLDING LATCH ON COWL IS LOOSE. INSTALLED OVERSIZE FASTENERS ON L2 DOOR SLIDE GIRT BAR HOLDING LATCH. INSTALLED SLIDE PACK. (M) 2L72 4F RT 20041026001082004102600108SO 2004 10 26 SIMA200426901 120040918A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21732DH 145358 ABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A DATED SEPT 16, 2003 AND EMB 145 SRM, SRM EMB 145/1142 REV 27, CHAPTER 53-24-02. (M) 2L72 4F RTT00011AT 20041026001132004102600113WP 2004 10 26 AALA20041059 120041011A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 F A6WE E9NE 20041026001152004102600115WP 2004 10 26 IXXA0400113O 120041019A2612 WARNING LIGHT DOUG DC8 DC862F 3021972WP PWA JT3D JT3D3 52039NE CARGO FIRE FALSE ACTIVATIONA IXXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW1171CX 652241517 45961 DURING CRUISE AT FL 370 LOWER CARGO COMPARTMENT FIRE WARNING ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. CREW RETURNED AND LANDED WITHOUT INCIDENT. UPON LANDING MAINTENANCE INSPECTED ALL LOWER CARGO COMPARTMENTS AND FOUND NO EVIDENCE OF FIRE. REF DMI NR 30653, CAT (C) NFD 10/31/04, IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20041026001322004102600132WP 2004 10 26 UPS04843363 120040921A534046473651 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE-C, CRACKED FITTING IN MAIN CABIN SUBFLOOR, STA 978-980 IN CORNER, LBL 66. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20041026001622004102600162NM 2004 10 26 04FDEA02974 120041022A5754 VANE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING IB FLAP VANE, IB TEE FITTING BORES HAVE CORROSION AND AFT HOLE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL2 AND REPAIRED AS PER FEDEX EA 1-5750-81571. 2L73 4F4 FRTA22WE E31N3 20041026001632004102600163EU 2004 10 26 DHL2004363527 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3893, FR. 18 - FR. 26.5 RBL 18 MAIN CABIN SEAT TRACK CORRODED OUT LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 18 - FR. 26.5 RBL 18 IAW A-300 SRM 53-10-10 / 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 53-10-10 / 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 18 TO FR 26.5 RBL 18 IAW A-300 SRM 35-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLY WHITE IAW A-300 SRM 51-40-10 AND A-300 51-40-12. 2L72 4F4 FRTA35EU E23EA 20041026001642004102600164WP 2004 10 26 ASMF200410011 120041014A2797V3601 SWITCH DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE DAMAGED W ASMFD RETURN TO BLOCK JH WARNING INDICATION ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23751RA 49779 AIRCRAFT RETURNED TO PLATFORM, DURING TAXING TAKE OFF ALARM WAS ON COULD NOT CANCEL IT. TECHNICAL PERSONNEL PERFORMED TAKE OFF CONFIGURATION TEST AND CHECK SLAT, FLAPS, AND SPOILERS, PARKING BRAKES, STABILIZER AND AURAL WARNING WERE CHECK BUT FAIL CONTINUED. DURING ELECTRICAL CHECK SWITCH S1-491 WAS DETECTED DAMAGED. IT WAS REPLACED IAW WDM 27-52-00 AND TESTED IAW MM 27-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20041026001652004102600165CE 2004 10 26 GM82004F00001 120040922A2434991059111RX ALTERNATOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE FAILED D DATAO OTHER O OTHER NRNOT REPORTED 1 SW0576LU 330 17281150 ALTERNATOR, HIGH FIELD RESISTANCE. 1H71 3O3 ONT3A12 1E10 20041026001662004102600166SO 2004 10 26 SWIA200413993 120041020A27503431001001 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE NACELLE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07563SW8619 8619 120338 FLAP DISAGREEMENT EVERY TIME FLAPS ARE PUT UP. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR IAW MM 27-50-00, OPERATIONAL CHECKED GOOD. 2L72 4T4 TRTA31SO E20NE 20041026001672004102600167EA 2004 10 26 QXEA200400726 120041019A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 CORROSION ON BULKHEAD WEB JUST ABOVE FLOOR SUPPORT BEAM AT STATION FS280.0 AT APPROXIMATELY 25 DEGREES LT BL. REPAIRED IAW EA R-53-214. 2L72 4F4 FRTA21EA EOOO63EN 20041026001692004102600169EA 2004 10 26 COMA0460581 120041017A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE EMERGENCY LIGHT DISCONNECTED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01934CA 7042 FLIGHT 5152 EMERGENCY FLOOR LIGHT ROW 2-5 ARE INOPERATIVE. RECONNECTED LOOSE WIRE AT ROW 5. 2L72 4F4 FRTA21EA E15NE 20041026001722004102600172 2004 10 26 RAIA00410014 420041018A34180861DT5 VANE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL AOA MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03835HK1189 145670 RECEIVED EICAS SPS1 INOPERATIVE, SPS ADVANCE, AND AMBER AOA FLAG ON CAPTAIN PFD. MAINTENANCE REMOVED AND REPLACED AOA VANE ON NR 1 SIDE . 2L72 4T4 FRTT00011ATTE6CH 20041026001742004102600174EU 2004 10 26 DXTA200400428 120041017A3240 BRAKE ASSY BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305 NE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07548QS 259048 WHEN APPLYING THE BRAKES FROM THE LT SEAT, THE FIRST APPLICATION RESULTS IN ALMOST NO BRAKING ACTION. THE PEDALS GO TO THE STOPS WITH VERY LITTLE RESULTS. BREAKING ACTION RETURNS TO NORMAL AFTER THE PEDALS ARE RELEASED AND RE-APPLIED. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA3EU E35NE 20041026001752004102600175 2004 10 26 DXTA200400425 420041016A22107014940901 CONTROLLER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL AUTOPILOT SYS MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07923QS 7500023 WITH AUTOPILOT ENGAGED, IN A LT TURN, LVL FLIGHT MASTER WARNING ILLUMINATED + CAS MESSAGE RETRIM RT WING DOWN WAS DISPLAYED. THIS HAPPENED TWICE, IN EACH CASE THE AUTOPILOT WAS DISENGAGED BY PILOT. WINGS LEVELED AND LIGHTS EXTINGUISHED. COMPLETED INSPECTION OF THE AUTOPILOT SYSTEM, AND THE AILERON SYSTEM IAW CHAPTERS 22-10-01, AND 27-10-00 (RESPECTIVELY) OF THE M/M. NO DISCREPANCIES WERE NOTED. TENSIONS, TRAVELS AND OPERATIONS WERE SATISFACTORY. 2L72 4J4 FRTT00007WITE6CH 20041026001772004102600177 2004 10 26 RAIA00410015 420041018A344480069425 WARNING SYSTEM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03825HK13052 145510 TAKE-OFF CONFIG WARNING LIGHT ON. MAINTENANCE REMOVED AND REPLACED AURAL WARNING UNIT. 2L72 4T4 FRTT00011ATTE6CH 20041026001782004102600178EU 2004 10 26 RAIA00410016 120041019A7930 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE ILLUMINATED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03562HK 41078 76077 RT ENGINE OIL CONTAMINATION CAPTION ILLUMINATED. MAINTENANCE INSPECTED CHIP DETECTOR FOR CONTAMINANTS AND CLEANED. 2L72 4T4 TRTA41NM E18NE 20041026001792004102600179 2004 10 26 371PA0085 420041018A2210253884 INDICATOR BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE YAW DAMPER FALSE INDICATIONA PIDAK NONE O OTHER NRNOT REPORTED 1 SO05371PA 23543 YAW DAMPER INDICATOR INDICATES FULL RT. REPLACED YAW DAMPER INDICATOR. SYSTEM OPS CHECKS GOOD IAW MM 22-12-01.. 2L72 4F4 FRTA16NE E2GL 20041026001832004102600183EU 2004 10 26 MALA040621 120041019A7720 GAUGE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ITT ERRATIC A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15445XJ 340B445 RT SIDE ITT INDICATOR FELL ABOUT 300 DEGREES APPROXIMATELY 20 MIN AFTER DEPARTURE SHOWING AT 530 VS 830. ALL OTHER ENGINE PARAMETERS WERE NORMAL BOTH ANALOG AND DIGITAL SHOWED THE DROP. AC RETURNED TO DEPARTURE, MAINTENANCE PERFORMED ITT CAL CHECK OF RT ENG FOUND ITT GAGE GIVING ERRATIC READINGS REMOVED AND REPLACED ITT GAUGE ALL CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20041026001842004102600184 2004 10 26 MALA040615 420041015A34206226320002 INDICATOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15451XJ 340B451 AFTER DEPARTING FO SIDE DCP FLAG APPEARED ON BOTH EADI AND EHSI THEIR FUNCTIONS ON THE FO DCP DID NOT WORK AND THE OBS SELECTOR FOR THE FO DOES NOT WORK. AC RETURNED, MAINTENANCE REMOVED AND REPLACED DCP SN OFF 439 SN ON 260 PN-622-6320-002. PERFORMED FUNCTIONAL CHECK IAW MM34-24-25-2. OPS CHECKS GOOD. LEITNER 12689. 2L72 4T4 TRTA52EU E8NE 20041026001852004102600185EU 2004 10 26 MALA040614 120041015A7710 POWER LEVER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT PROPELLER OUT OF RIG A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15423XJ 340B423 WITH T/O PWR CL MAX, THE LT PROPELLER IS UNABLE TO REACH 1396RPM. AIR RETURN MAINTENANCE TRANSFERD TO 409 CARD NR 182085 CONT CARD NR 040131, DISC NR 1 NEED TO SWAP PROP RPM GUAGES. NR 1 SWAPPED GAUGES WAS A NO FIX. DISC NR 2 NEED TO RE-RIG LT PROP BETA TUBE. NR 2 RE-RIGGED LT PROP BETA TUBE, WAS A NO FIX. DISC NR 3 FOUND LT POWER LEVER CABLE OUT OF RIG AT PCU. RE-RIGGED LT POWER LEVER CABLE AT PCU IAW 76-10-00-5.OPS CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20041026001862004102600186NE 2004 10 26 MALA040613 220041013A7220CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT SEIZED A MALAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL15438XJ 340B438 RT CHIP DETECT LIGHT ILLUMINATED ENROUTE ON DESCENT ITT OVERTEMP LIGHT ILLUMINATED SO WE SHUT DOWN THE ENGINE. MAINTENANCE INSPECTED, CORE SEIZED UP. REMOVED AND REPLACED RT ENGINE SN/0N 785770, SN/OFF 785738 IAW TASK CARD 7100-310R, SEE WORK PACKAGE 10-13-04 FOR DETAILS. 2L72 4T4 TRTA52EU E8NE 20041026001882004102600188EU 2004 10 26 MALA040619 120041008A79304052T92P01 SOCKET SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CHIP DETECTOR INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15437XJ 340B437 DURING DEPARTURE WHILE LEVEL A 4000 FEET THE R-CHIP DETECT ANNUNCIATOR ILLUMINATED NUMEROUS TIMES. QRH CONSULTED ENGINE PARAMETERS NORMAL. CALLED MXCTRL, ADVISED TO RETURN. MAINTENANCE, UPON INSPECTION NOTED RT CHIP DETECTOR CONNECTOR PLUG SOCKET LOOSE. REMOVED AND REPLACED CHIP DETECTOR IAW GE 72-00-00. NO DEBEIS NOTED ON OLD CHIP DETECTOR. CLEANED AREA, RAN ENGINE AT VARIOUS POWER SETTINGS FOR 30 MINUTES NO FAULTS NOTED. S/N ON TED19434 S/N OFF TED13652. 2L72 4T4 TRTA52EU E8NE 20041026001892004102600189EU 2004 10 26 AWXA200401152 120041009A1420E0052R8B3APNE CONNECTOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEAT ROW 7 LT DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28668AW 1764 DURING BC-2 CHECK FOUND A DAMAGED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 7 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20041026001902004102600190EU 2004 10 26 DHL2004363529 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3883, BL 0 FR. 26 TO FR. 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 26 - FR. 30 AT BL 0 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 26 - FR. 30 AT BL 0 IAW SRM 53-10-10 / 51-10-40. MATERIAL USED, P/N 60-22457, PO NR 24302234. 2L72 4F4 FRTA35EU E23EA 20041026001912004102600191SW 2004 10 26 ALGA097744 120041001A6510407340340103 DISC PACK BELL 407 407 1182206SW ALLSN 250C 250C47B GL TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03647AL 53357 CRACKED LAMINATE/REPLACED WITH NEW. 1G71 3U3 UO H2SW E1GL 20041026001952004102600195NM 2004 10 26 04FDEA02870 120041005A7830683L221G04 SLEEVE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 ENG 1R T/R TRANSLATING SLEEVE UPPER SLIDING TRACK AFT EDGE FOUND CRACKED. CRACK REPAIRED REFER FAA FORM 8130-3 NO 5488(J009681-000) FOR WORK DETAILS. 2L73 4F4 FRTA22WE E31N3 20041026001962004102600196NM 2004 10 26 04FDEA02871 120041005A7830683L218G07 SLEEVE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 ENG 2L T/R TRANSLATING SLEEVE UPR SLIDING TRACK AFT EDGE FOUND CRACKED. CORRECTIVE ACTION: SNRM N0308: CRACK REPAIRED REFER FAA FORM 8130-3 NO 5489(J009682-000) FOR WORK DETAILS. 2L73 4F4 FRTA22WE E31N3 20041026001992004102600199NM 2004 10 26 AWXA200401095 120041004A2560P20700012015 FLASHLIGHT AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE ZONE 900 - LAVATINOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28825AW 1527 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE L-1 DOOR EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20041026002012004102600201NM 2004 10 26 371PA0069 120040916A5320 INTERCOSTAL BOEING737 737306 13844BGNM GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 INTERCOSTAL FROM BS 966 TO BS 986 AT RBL 18 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL IAW SRM 51-30-00. 2L72 4F4 FRTA16NE E2GL 20041026002022004102600202NM 2004 10 26 371PA0070 120040920A5330 SKIN BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 R1 DOOR CUT OUT, LOWER AFT CORNER HAS SUSPECT CRACK, VERIFIED BY HFEC. REPAIRED IAW SRM 53-10-01. 2L72 4F4 FRTA16NE E2GL 20041027000012004102700001EA 2004 10 27 04295703 120041021A3610 VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27703BR 7467 EVENT SUMMARY STATED LAV SMOKE DETECTOR AURAL WARNING. INSPECT LAV SMOKE DETECTOR CONNECTOR AND WIRING. REMOVED AND REPLACED SPINNER. PERFORM FIM. INSPECT 10TH STAGE DUCT AND DUCTS TO ACM. PERFORMED BORESCOPE INSPECTION. INSTALLED 2 FAN BLADES. REMOVED AND REPLACED PRESSURE REGULATING VALVE. RUN ENGINES 2 TIMES SEPARATELY.THIS WORK ORDER IS STILL IN WORK: APPR STATUS. 2L72 4F4 FRTA21EA E15NE 20041027000022004102700002WP 2004 10 27 04FDEA02981 120041022A5753ANB74342 ROLLER DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 RT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT SPOTTED AREA IAW EA8-5750-81494. ORIGINAL LUG THICKNESS WAS 1.015 INCH FINAL LUG THICKNESS .990 INCH. SEE NR N01176 2L73 4F4 FRTA22WE E23EA 20041027000052004102700005NM 2004 10 27 C8GA20040024 120041021A3260106122615 PROXIMITY SWITCH BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE MLG FAILED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15715AA56141 22470 AFTER TAKE-OFF, TAKE-OFF WARNING SOUNDED WHEN FLAPS SELECTED FROM 5 TO 2 DEGREES. HORN SILENCED WHEN CYCLED BACK TO 5 DEGREES. CYCLED GEAR AND GEAR HANDLE STUCK IN DOWN POSITION. AIRCRAFT RETURNED TO AIRPORT. TAKE-OFF HORN SOUNDED AGAIN WHEN FLAPS SELECTED FROM 25 TO 30 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND GEAR AIR SENSE PROXIMITY SWITCH FAILED. REPLACED PROXIMITY SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041027000072004102700007EU 2004 10 27 04FDEA02984 120041023A7830 WARNING LIGHT AIRBUS330 A300* EU GE CF6 CF680C2A5 NE ECAM ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25669FE 774 PDIS 669 78-30 0007382 23OCT04 MEM CLOSE U LOGPAGES: 00926331 CLEARED FOR TAKE-OFF , STABILIZED ENGINES AT 40 PERE NT N1, THEN APPLIED TAKEOFF POWER. ALMOST IMMDEIATLY RECIEVED AMBER ECAM NR1 ENG REV PRESSURIZED REJECTED TAKEOFF AND RETURNED TO GATE. ENT BY: 103508 RPT BY: 068992 FACT 23OCT04 10:14 MEM U IAW MEL 78-30-01A DIRECTIONAL PILOT VALVE AND PRESSURE SWITCH CONNECTOR PLUGS DISCONNECTED IAW MEL. ITEM ST ILL REMAINS ON MEL 78-30-01A, OK TO CONTINUE ENT BY: 103508 RPT BY: 103508****S/D COMING**** 2L72 4F4 FRTA26NM E13NE 20041027000082004102700008EU 2004 10 27 04FDEA02985 120041023A5320 ADAPTER AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 RT FR.41-42, BETWEEN SEAT TRACKS NR 2 AND 3, CLS ADAPTER TRACK HAS CORROSION AT BOTH ENDS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED CLS ADAPTER IAW SRM 51-72-10. 2L72 4F4 FRTA35EU E13NE 20041027000092004102700009EA 2004 10 27 04287703 120041013A2150 ACM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT SMOKE A VTZAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA27703BR 7467 EVENT SUMMARY STATES THAT RETURN FROM FLIGHT. SMOKE TOILET CAUTION MSG AFTER TAKEOFF. SMOKE VISIBLE IN TOILET AND AFT CABIN. REMOVED AND REPLACED RT ACM REF MM 21-52-00 AND REMOVED AND REPLACED WATER SEPARATOR SOCK REF MM 21-52-00. 2L72 4F4 FRTA21EA E15NE 20041027000102004102700010NM 2004 10 27 371PA0051 120041008A5314 KEELBEAM BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 LT KEELBEAM HAS CORROSION AFT OF BS 540 AND COMMON TO A PREVIOUSLY INSTALLED REPAIR SPLICE. REPAIRED IAW EA 53-257. 2L72 4F4 FRTA16NE E2GL 20041027000122004102700012NM 2004 10 27 371PA0058 120040928A5320 SILL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 AFT CABIN, AFT ENTRY DOOR LOWER SILL ASSEMBLY FROM BS 947.5 TO BS 986.5 HAS CORROSION. REPAIRED IAW SRM 53-60-15. 2L72 4F4 FRTA16NE E2GL 20041027000142004102700014NM 2004 10 27 371PA0072 120040917A5320 INTERCOSTAL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 INTERCOSTAL FROM BS 1006 TO BS 1016 AT RBL 37 HAS CORROSION AT CLIP NUT HOLES. REPLACED INTERCOSTAL IAW SRM 51-40-1. 2L72 4F4 FRTA16NE E2GL 20041027000152004102700015NM 2004 10 27 371PA0073 120040918A5320 INTERCOSTAL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 INTERCOSTAL HAS CORROSION AT BS 294 TO BS 312 AT RBL 12. REPLACED INTERCOSTAL IAW SRM. 2L72 4F4 FRTA16NE E2GL 20041027000182004102700018NM 2004 10 27 UPS04443350 120040924A524065B0989142 GATE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE R5 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C M/D- R5 DOOR UPR GATE CRACKED. (BS 2240 TO 2280, STR R16 TO R17) UPPER GATE REPLACED IAW MM 20-51-01. 2L74 4F4 F A20WE E20EA 20041027000202004102700020WP 2004 10 27 04FDEA02909 120041011A5210ABA71881 STOP DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL ZONE 800 BROKEN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25371FE 46609 COMPLY WITH E.A.8-5210-82059.REWORK OF ABA7188-1 FITTING TO REPLACE ABA7156-501 FOR R1 DOOR. CLOSING ACTION ON 10/11/04. ON N/R S00024. COMPLIED WITH EA 8-5210-82059 2L73 4F4 F A22WE E23EA 20041027000212004102700021NM 2004 10 27 UPS04443328 120041001A532065B172236 PLATE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C, CRACK FOUND AT BS 1241 WL 200 RT SPLICE PLATE NR 5 BOLT HOLES BORE CRACK STILL REVEALED AFTER THE HOLE OVERSIZED TO DIA 1.200 INCH. RT SPLICE PLATE REPLACED IAW EO B747-5740-4366. 2L74 4F4 F A20WE E20EA 20041027000232004102700023EU 2004 10 27 155122 120041020A2910 SWIVEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE HYD LINE CRACKED A UHLAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL17360SZ 340A006 FLT 7925, DURING TAXI TO RUNWAY, HYDRAULIC LIGHT ILLUMINATED, HYDRAULIC PUMP RAN CONT, HYDRAULIC QTY ON THE MAIN AND OB WENT TO 0, BIG 1800 PSI, EMERGENCY 2500 PSI. INSPECTED AND FOUND RT OB BRAKE SWIVEL TO BE CRACKED. REMOVED AND REPLACED RT BRAKE SWIVEL, LEAK CHECK GOOD, IAW M/M 32-42-35-2. 2L72 4T4 TRTA52EU E8NE6 20041027000242004102700024EA 2004 10 27 04294634 120041020A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT INOPERATIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27634BR 7287 EVENT SUMMARY STATED THAT RT PACK OVERPRESSURE ON TAKEOFF ROLL. DUE TO LT PACK BEING CONSIDERED INOPERATIVE IAW MEL 21-61-01, THE APU IS REQUIRED TO BE USED ON T/O. IF AVAILABLE IAW FSM PG 5-14-1. USING APU BLEED AIR TO SUPPLY THE REMAINING PACK DURING T/O PREVENTS THE HIGH PRESSURE MSG. AIRCRAFT IS OK TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041027000302004102700030NM 2004 10 27 371PA0075 120040915A5315 FLOORBEAM BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FLOORBEAM AT BS 312 FROM RBL 9 TO LBL 34 HAS CORROSION. REPAIRED IAW SRM 51-10-51 AND SRM 53-10-51. 2L72 4F4 FRTA16NE E2GL 20041027000312004102700031NM 2004 10 27 QXEA200400703 120041005A5330 SKIN PANEL DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 REPAIR FUSELAGE SKIN PANELS LOCATED AT STATION X 123- X 167 BETWEEN STRINGERS 31S AND 33S. REPAIRED SKIN PANELS IAW EA'S 2-53-575B AND 2-53-575C. 2H72 4T4 TRTA13NM E20NE 20041027000322004102700032WP 2004 10 27 04FDEA02914 120041011A5753ARC01541 HINGE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSION, AND COMPLIED WITH EA 8-5750-81473 REF NR N00295. 2L73 4F4 FRTA22WE E23EA 20041027000342004102700034CE 2004 10 27 GM82004F00004 120040922A2434991059111RX ALTERNATOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE SHORTED D DATAO OTHER O OTHER NRNOT REPORTED 1 SW0578LU 561 17281159 ALTERNATOR, FIELD SHORT TO GROUND, ROTOR JAMMED. 1H71 3O3 ONT3A12 1E10 20041027000362004102700036EU 2004 10 27 UPS04143335 120041008A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE EMERGENCY EXIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01149UP 0832 LAV EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT. 2L72 4F4 FRTA35EU E24NE 20041027000382004102700038EA 2004 10 27 QXEA200400698 120040930A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 CABIN FLOORBEAM LOCATED AT FS 280.00 HAS CRACK AT WL 69.95, EXTENDING FROM RBL 8.2 TO RBL 10.1. REPAIRED IAW EA R-53-209. 2L72 4F4 FRTA21EA EOOO63EN 20041027000402004102700040EU 2004 10 27 DHL2004363510 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, NR 3868 FRAME 34-FRAME 38.2 LBL 78 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW SRM 51-40-11. NR 3868, REMOVED SEAT TRACK FROM FR 34-FR. 38.2 LBL 78 INCHES IAW SRM 53-10-10 OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 34-FR. 38.2 LBL 78 IAW SRM 51-10-40 AND SRM 51-30-30. TREATED AND PRIMED AREA (SEAT TRACK) AS REQUIRED REF: SRM 51-40-10 AND SRM 51-40-12. 2L72 4F4 FRTA35EU E23EA 20041027000412004102700041CE 2004 10 27 MYN2004F00001 120040928A27410560051101 CHAIN CESSNA172 172S 2072439CE LYC O360 IO360A1A 41514EA TRIM SYSTEM FAILED B MYNRO OTHER O OTHER NRNOT REPORTED 1 GL11830MA595 172S8954 FORWARD TRIM CHAIN TO CABLE LINK IS COMING APART. HAVE TO REPLACE FORWARD CABLE ASSY. 1H71 3O3 ONT3A12 1E10 20041027000432004102700043EA 2004 10 27 QXEA200400705 220041008A7261312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 400 LEAKING A QXEAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 NM09409QX7036 1893 4051 FLIGHT 2564, AFTER APPLYING TAKE-OFF POWER, SMOKE WAS NOTICED IN THE COCKPIT AND CABIN. THE TAKE-OFF WAS ABORTED. AFTER SHUTDOWN, OIL WAS NOTED LEAKING FROM THE NR 2 ENGINE. MAINTENANCE INPSECTED THE AIRCRAFT AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20041027000442004102700044WP 2004 10 27 P9RA20040047 120041012A335060030431 POWER SUPPLY DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1114816 49370 AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM. 2L72 4F4 F A6WE E9NE 20041027000462004102700046EA 2004 10 27 04270645 120040926A2914 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYDRAULIC SYSTEMINOPERATIVE A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27645BR 7383 HYD 3B PUMP CAUTION MSG, INOPERATIVE. FOUND CB G11 OUT. RESET, OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041027000512004102700051NM 2004 10 27 2004UALA00882 120040917A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 FWD PIT MAIN FRAME AT BS 540, BETWEEN STR 24L- STR 25L, DENTED ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED A DOUBLER REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20041027000532004102700053NM 2004 10 27 2004UALA00884 120040914A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT FRAME AT BS 1440 IS DENTED BETWEEN STRINGERS 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041027000552004102700055NM 2004 10 27 2004UALA00886 120040911A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 MAIN CABIN STA 1641 AND RBL 26 TO CENTER LINE, PREVIOUS FLOORBEAM REPAIR CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLES, STRAP AND BEAM SECTION. 2L72 4F4 FRTA2NM E17NE 20041027000572004102700057NM 2004 10 27 2004UALA00888 120040909A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 CABIN FLOORBEAM CAP CORRODED BS 310, RBL 44. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED L ANGLE DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041027000612004102700061EA 2004 10 27 COMA0460561 120040930A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FALSE INDICATIONA COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01458CA 7613 FLIGHT 5004 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20041027000682004102700068CE 2004 10 27 GM82004F00005 120040922A2434991059111 ALTERNATOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE INOPERATIVE D GM8SO OTHER O OTHER NRNOT REPORTED 1 SW0579LU 581 17281163 ALTERNATOR, INOPERATIVE. 1H71 3O3 ONT3A12 1E10 20041027000742004102700074SO 2004 10 27 HBE2004F00000 220040921A7314M3050 IMPULSE COUPLINGSLICK CESSNA180 180J 2072622CE CONT O470 O470S 17026SO MAGNETO BROKEN E HBECO OTHER O OTHER NRNOT REPORTED 1 AL059950N785 02050295 18052605 DURING FLIGHT THE IMPULSE COUPLING ON THE RT MAGNETO FAILED CAUSING THE MAGNETO HOUSING TO FAIL AS WELL. DO NOT KNOW PROBABLE CAUSE. REPLACED WITH NEW MAGNETO. 1H71 3O3 O 5A6 E273 20050608000602005060800060NE 2005 6 8 GUU2005F00015 220041009A7250 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUAK NONE O OTHER ININSP/MAINT 1 SO298153517351 UE147 DURING POST FLIGHT WALK-AROUND, FOUND A HOLE IN NR 2 ENGINE IB EXHAUST STACK. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS INTERNAL DAMAGE. REPLACED RT POWER SECTION MODULE. POWER ASSURANCE RUN AND LEAK CHECK COMPLIED WITH. ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2L72 4T4 TRTA24CE E26NE 20050608000652005060800065NE 2005 6 8 GUU2005F00016 220040915A7250 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUAK NONE O OTHER ININSP/MAINT 1 SO2969547163987956 UE189 PCE114446 DURING AM ENGINE RUNUPS, RT ENGINE WENT INTO FEATHER AND WOULD NOT COME OUT, ALL OTHER PARAMETERS NORMAL. AFTER FURTHER INSPECTION, DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2L72 4T4 TRTA24CE E26NE 20041025000062004102500006SO 2004 10 25 SWIA200413856 120040921A2910 PRESSURE SWITCH EMB 120 EMB120ER 3260203SO HYD SYSTEM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07580SW 120348 RUDDER SPEED SWITCH LIGHT ILLUMINATED ON MAP. REPLACED BOTH RUDDER GREEN SYSTEM AND BLUE SYSTEM HYDRAULIC PRESSURE SWITCHES WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025000162004102500016SO 2004 10 25 SWIA200413789 120040910A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM0758733 120197 ON TAXI OUT WITH FLAP SELECTOR 15 DEGREES, FLAPS WERE STILL AT 0 DEGREES. REMOVED AND REPLACED LEFT & RIGHT NACELLE FLAP ACTUATORS IAW MM 27-50-00. OPERATIONAL CHECK GOOD. LT P/N: 308200-1007, S/N OFF: 0242 RT, P/N: 308200-1007, S/N OFF: 0405. 2L72 4T RTA31SO 20041025000192004102500019EA 2004 10 25 SWIA200413792 120040909A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07443SW 7638 ONE CEILING EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000212004102500021EA 2004 10 25 SWIA200413794 120040910A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW 7279 STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED BOTH TRIM SWITCHES IAW MM 27-41-30. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000312004102500031EA 2004 10 25 SWIA200413757 120040825A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07926SW 7687 RUDDER TRIM RESPONDS VERY SLOWLY WHEN SELECTED TO THE LEFT. REMOVED AND REPLACED RUDDER TRIM PANEL IAW 27-24-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000972004102500097SO 2004 10 25 SWIA200413952 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 0.00 (CENTER). ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW SRM 51-25-00, 51-40-02, AND 51-40-05. 2L72 4T RTA31SO 20041025000992004102500099SO 2004 10 25 SWIA200413954 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. BUTTPLATE REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025001012004102500101NM 2004 10 25 SWAA043027 120041019A3260 LANDING GEAR BOEING737 7372H4 138448CNM NOSE MALFUNCTIONED A SWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW29082SW 22731 ON APPROACH TOWER REPORTED NLG TO BE PARTIALLY EXTENDED, HAD THREE GREEN GEAR IND. WENT AROUND CYCLED GEAR, THREE GREEN LIGHTS, VISUAL CHECK THRU GEAR INSP WINDOW ALL NORMAL. VISUALLY INSP NLG AND PROX SWITCHES. NO DEFECTS PER MM. 2L72 4F A16WE 20041025001032004102500103NM 2004 10 25 SWAA043029 120041019A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 EEPLS COVER AT ROW 7 DEF AND ROW 8 DEF, LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041025001052004102500105NM 2004 10 25 SWAA043038 120041019A53106546957 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 500 + 15, LBL 65, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041025001342004102500134 2004 10 25 SWIA200413859 420040926A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL PROTECTIONMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM07412SW 7101 AFTER ROTATION ON TAKEOFF 300 FT AGL STALL FAIL CAUTION MSG ILLUMINATED. REMOVED AND REPLACED STALL WARNING COMPUTER IAW MM 27-35-01, OPERATIONAL CHECK GOOD. P/N 39-951-002-08, S/N OFF 589. 2L72 4F RTA21EA 20041025001362004102500136EA 2004 10 25 SWIA200413879 120040929A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07986SW 7967 DURING FLAP RETRACTION AFTER LANDING, FLAPS FAIL MESSAGE ON ED-1 APPEARED. RE-RIGGED FLAP SYS BPSU IAW AMM 27-52-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001542004102500154SO 2004 10 25 SWIA200413882 120040928A2120 ODOR EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM0757734 120199 AT 27,000 FT, SMOKE WARNING ILLUMINATED. VISIBLE SMOKE REPORTED IN CABIN. AIRCRAFT WAS DESCENDED WITH BLEED/PACK CONFIGURATION IN LOW/LOW, SMOKE CLEARED. REMOVED LEFT ACM & GROUND COOLING FAN, INSPECTED COMPONENTS FOUND NO DEFECTS. INSPECTED INLETS AND OUTLETS TO HEAT EXCHANGER ACM & GROUND COOLING FAN, FOUND NO OIL/FLUID RESIDUE. PRESSURE WASHED HEAT EXCHANGER, REPLACED HOSE FRAYED FROM WATER SEPARATOR TO SPRAY NOZZLE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025001582004102500158SO 2004 10 25 SWIA200413957 120041005A5313 RIB EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 RIB AT FRAME 13 CRACKED (AS MARKED). ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW SRM 51-40-02, 51-30-01, AND 51-25-00. 2L72 4T RTA31SO 20041025001622004102500162EA 2004 10 25 SWIA200413897 120041003A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAD RETURN TO BLOCK JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07430SW7105 7105 7523 SPOILERON FAULT ON TAXI OUT, RETURNED TO GATE. REMOVED AND REPLACED NR 1 SYSTEM LEFT HYDRAULIC INBOARD FLIGHT SPOILERON PCU IAW MM 27-62-01. REPLACED LOW PRESSURE SWITCH FOR HYDRAULIC SYSTEM 3B. P/N 211C223-461A. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001702004102500170SO 2004 10 25 SWIA200413890 120040724A5310 WINDOW FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 CAPTAIN'S SIDE FORWARD OF DV WINDOW FRAME 9 IS CRACKED. ITEM FOUND AT C-CHECK. COMPLIED WITH SB 120-53-0073 ON CAPTAIN'S SIDE FORWARD OF DV WINDOW AT FRAME 9 AS REQUIRED. 2L72 4T RTA31SO 20041025001722004102500172SO 2004 10 25 SWIA200413892 120040724A5713 STRINGER EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 LEFT WING FUEL CELL STRINGER CRACKED FORWARD OF INBOARD DEFUEL PANEL (MARKED). ITEM FOUND AT C-CHECK. COMPLIED WITH LEFT WING STRINGER NR 10 BETWEEN RIB NR 5 AND RIB NR 6 REPAIR PER SRM 57-20-03. 2L72 4T RTA31SO 20041025001932004102500193NM 2004 10 25 SWAA043057 120041021A32601899 SENSOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 SW29304SW 22944 AIR TURNBACK, RIGHT MLG RED WARNING LIGHT ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR PER MM. 2L72 4F RTA16WE 20041025001952004102500195NM 2004 10 25 SWAA043059 120041021A53306545766 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 10R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041025001962004102500196NM 2004 10 25 SWAA043060 120041021A5315BAC1509100146 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 907 + 8, RBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041026000132004102600013EU 2004 10 26 AWXA200400940 120040814A5347D5713014720300 SEAT TRACK AIRBUS320 A320231 3930325EU CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK CORROSION WAS FOUND IN NUMEROUS AREAS ON RT OUTBOARD SEAT TRACK BETWEEN BS 15900 & BS 18101, AND FR 36 & FR 41. MAINTENANCE REMOVED CORRODED SEAT TRACK SECTION AT Y1292 RT FROM FR 36 TO FR 41; RECEIVED NEW REPLACEMENT SECTION OF SEAT TRACK AND INSTALLED REPAIR PART IAW A320SRM 51-72-11. 2L72 4F RTA28NM 20041026000182004102600018NM 2004 10 26 AWXA200400879 120040812A275121EN1076 SWITCH BOEING737 7373G7 1384595NM ZONE 102 INTERMITTENT A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28307AW 24634 T/O WARNING HORN SOUNDED AT APPROX 70 KT WITH ALL SETTINGS NORMAL, & AFTER T/O THRUST WAS MET. FLAPS 1, TRIM 4.7, ALL GREEN LIGHTS SET FOR FLAPS & SLATS, REJECTED T/O & RETURNED TO GATE. MX CHECKED SECURITY & ADJUSTMENT OF STAB T/O WARNING SWITCHES PER BMM, & SPEED BRAKE T/O WARNING SWITCH IAW BMM, NO DEFECTS NOTED. FOUND FLAP T/O WARNING SWITCH INCONSISTENTLY MAKING & BREAKING AT DIFFERENT PLUNGER DEPTHS. R & R, ADJUSTED FLAP SWITCH IAW BMM. DUE TO HISTORY OF CONFIGURATION WARNING PROBLEMS R & R AURAL WARNING MODULE IAW BMM, & PRINTED CIRCUIT CARD IAW BMM, OPS CK GOOD. FUNCTIONAL CHECK COULD NOT CONFIRM REASON FOR REMOVAL, UNIT TESTED GOOD. 2L72 4F RTA16WE 20041026000212004102600021WP 2004 10 26 UPS04842864 120040713A5712 RIB DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE: C1, RIGHT WING LEADING EDGE LOWER RIB IS CRACKED AT FASTENER HOLE AT XFS 601. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20041026000332004102600033SO 2004 10 26 SIMA200426904 120040915A531014521713005 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21732DH 145358 DURING AN IMBV INSPECTION THE GALLEY CENTER BEAM WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMGAED AREA. FABRICATED A U SHAPE DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 PARA 5 FIG 204 SHEET 2. (M) 2L72 4F RTT00011AT 20041026000382004102600038NE 2004 10 26 GTIA040784 220040916A7220780830 GUIDE VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE LT ENGINE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23831NK 49617 FOUND LT ENGINE INLET GUIDE VANES CRACK FOUND ON 3 VANES AT 3 O'CLOCK POSITION. REMOVED AND REPLACED INLET CASE. (M) 2L72 4F4 FRTA6WE E2EA 20041026000412004102600041EA 2004 10 26 2004F00414 120040929A7714829599 SENSOR CNDAIRCL600 CL6002D24 1390016EA GE CF34 CF34* NE NR 2 ENG N2 FAILED A FDKAC ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 SW07905J 15005 194208 ABORTED TAKEOFF DUE TO A RIGHT FADEC CAUTION MESSAGE FOLLOWED BY A RIGHT ENGINE FLAMEOUT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RIGHT ENGINE N2 SPEED SENSOR AND OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20041026000452004102600045 2004 10 26 GTIA040764 420040904A2565 SLIDE DOUG DC9 DC981 3022081WP L2 DOOR DISLODGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23819NK 48016 LGA - FLT 9950 - L2 DOOR SLIDE FALLING OUT. FOUND L2 DOOR SLIDE PACK FALLING OUT RESECURED PACK. (M) 2L72 4F A6WE 20041026000512004102600051EU 2004 10 26 ASOA04762 120040910A5315 FLOORBEAM AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FS 39, STRINGERS 14L AND 14R AND AT FRAME 40, STRINGERS 14L AND 14R WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 39, STRINGERS 14L AND 14R AND AT FRAME 40, STRINGERS 14L AND 14R IAW SRM 51-25-01 AND 51-25-04. (M) 2H72 4T RT 20041026000662004102600066WP 2004 10 26 GTIA040776 120040831A7120K22199SA31 ISOLATOR DOUG DC9 DC982 3022082WP NR 2 ENGINE OUT OF ADJUST A GTIAK NONE O OTHER ININSP/MAINT 1 GL23823NK 48020 NR 2 ENGINE PYLON FORWARD LOWER ISOLATOR, ALIGNMENT MARKS ARE OUT OF LIMITS. REMOVED AND REPLACED LOWER FORWARD ISOLATOR. (M) 2L72 4F A6WE 20041026000682004102600068 2004 10 26 GTIA040782 420040916A2565D29982113 SLIDE DOUG DC9 DC982 3022082WP R1 DOOR OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23821NK 49508 FOUND R1 DOOR EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVACUATION SLIDE. (M) 2L72 4F A6WE 20041026000712004102600071 2004 10 26 SIMA200427201 420040925A2213701700082428 COMPUTER EMB 135 EMB135KL 3260302SO NR 1 MALFUNCTIONED A SIMAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SW21811AE 145529 ON TAXI OUT RUDDER PEDALS JAMMED. REPLACED NR 1 INTEGRATED COMPUTER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026000752004102600075EA 2004 10 26 ASOA04677 120040829A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11827AS 7212 FLT 4739 - DURING CLIMB-OUT FROM LEX-DFW, WITH THE LEFT PACK DEFERRED THE CREW RECEIVED A RIGHT PACK HIGH PRESSURE MESSAGE. THE QRH WAS COMPLIED WITH BUT THE RIGHT PACK WOULD NOT RESET. SOME PASSENGERS WERE REPORTED AS FEELING ILL AND DIZZY WITH THE COCKPIT BECOMING VERY HOT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CVG, LANDING SAFELY. MAINTENANCE RESET THE RIGHT PACK AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041026000772004102600077SO 2004 10 26 SIMA200427909 120040919A5330 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21620AE 145102 ABI - A 12 INCH BY 8.5 INCH DOUBLER FROM A PREVIOUS REPAIR WAS REMOVED FOR EVALUATION DUE TO PROXIMITY OF AN ADDITIONAL DENT AT FRAME 64 STRINGER 20L. RECONTOURED THE ADDITIONAL DENT AND PERFORMED AND EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A NEW REPAIR DOUBLER, FILLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/4345 PARA 3 DATED SEPT 16, 2004. (M) 2L72 4T RTT00011AT 20041026000932004102600093EU 2004 10 26 ASOA04765 120040912A5320 INTERCOSTAL AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE LEFT INTERCOSTAL BETWEEN FRAME 38/39, STRINGER 17L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INTERCOSTAL BETWEEN FRAME 38/39 STRINGER 17L IAW SRM 51-25-01. (M) 2H72 4T RT 20041026001092004102600109SO 2004 10 26 SIMA200426702 120040922A1420 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT LOOSE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21705AE 145184 RDU - FLT 4572 - CREW REPORTED THE FORWARD OVERHEAD EMREGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR ON LIGHT. MAINTENANCE RECONNECTED THE CANNON PLUG. AN OPERATIONAL CHECK WAS COMLIED WITH AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026001182004102600118NM 2004 10 26 AWXA200401148 120041001A5310654656010 SHEAR TIE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 947, BETWEEN STR 26 AND 27 LT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 947, STR 26 AND 27; FABRICATED A NEW REPLACEMENT SHEAR TIE IAW DWG 65-46560; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 2, 3, AND 8. 2L72 4F4 FRTA16WE E2GL 20041026001582004102600158NM 2004 10 26 CALA0400683 120041022A53306545775 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769311 23362 INSPECTION FOUND A 1.8 INCH CRACK IN FUSELAGE SKIN 3 INCHES AFT OF STA 727D AND BELOW S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03090. 2L72 4F4 FRTA16WE E2GL 20041026001712004102600171SO 2004 10 26 RAIA00410013 120041018A7500AS568226 SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03816HK 145055 NR 1 ENGINE BLEED LEAK IN FLIGHT. MAINTENANCE REMOVED AND REPLACED BLEED SEALS IN CARGO BAY. 2L72 4T4 FRTT00011ATTE6CH 20041026001942004102600194NM 2004 10 26 04FDEA02869 120041005A3350KD4L030 RELAY DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 200 DEFECTIVE A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25585FE 48481 CABIN EMERGENCY LIGHTING NOT ILLUMINATED WHEN SWITCHED (ON). CABIN EMERGENCY LIGHTING TROUBLESHOOTING CARRIED OUT IAW FIM 33-51-00. FOUND RELAY R2-5700 AT FAULT. REMOVED AND REPLACED RELAY R2-5700 IAW STANDARD WIRING PRACTICES. OPERATIONAL CHECK CARRIED OUT IAW AMM 33-52-01. 2L73 4F4 FRTA22WE E31N3 20041026001982004102600198WP 2004 10 26 04FDEA02873 120041005A5240AKC70112 HINGE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL ZONE 800 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 COMPLY WITH EA 8-5240-82048. TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011. CLOSING ACTI0N ON 10/05/04. ON N/R S00019 COMPLIED WITH EA 8-5240-82048. 2L73 4F4 F A22WE E23EA 20041027000222004102700022NM 2004 10 27 DHL2004780514 120040930A5532 SKIN BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER APPROX STA FIN 177 (LT SIDE RUDDER). DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-40-1 FABRICATED DOUBLER 2024T-3 .040 4.5 X 2.5 PO NR 9001359 IAW SRM 55-40-2 AND 55-20-3 TREATED AND PRIME IAW SRM 51-10-2 INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20041027000262004102700026WP 2004 10 27 R2J2004F00004 220040915A722031018303 DUCT MTSBSIMU2 MU2B40 5780440CE GARRTTTPE331TPE33110 01514WP ENGINE FAILED B R2JRO OTHER O OTHER NRNOT REPORTED 1 EA21361MA4055 429SA P36200 ENGINE EGT SUDDENLY ROSE IN FLIGHT AND POWER HAD TO BE REDUCED. SAFE LANDING ACCOMPLISHED AT HOME BASE TROUBLESHOOTING REVEALED THE COMPRESSOR CROSSOVER DUCT (DIFFUSER) HAD FAILED, CAUSING LOW COMPRESSOR PERFORMANCE. A VANE HAD BROKEN OFF AND LODGED, PREVENTING CATASTROPHIC FAILURE OF COMPONENTS DOWNSTREAM. INVESTIGATION REVEALED THIS PART WAS REQUIRED TO BE REPLACED WITH AN UPGRADED DUCT LESS PRONE TO FAILURE AT ETH ENGINE TBO EXTENSION, WHICH WAS RECORDED IN THE MAINTENANCE RECORDS AS HAVING BEEN ACCOMPLISHED AT AN EARLIER TIME AND THE ENGINE CERTIFIED TO MEET THE 5400 HOUR TBO. (EA21200502933) 1H72 3T4 TRTA10SW E4WE 20041027000522004102700052NM 2004 10 27 2004UALA00883 120040917A5320 TEAR STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 BS 1400 STR 27L-28L TEAR STRAP AND SHEAR TIE CORRODED. 2L72 4F4 FRTA2NM E17NE 20041027000652004102700065CE 2004 10 27 GM82004F00000 120040922A2434991059111RX ALTERNATOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE FAILED D GM8SO OTHER O OTHER NRNOT REPORTED 1 SW0576LU 63 17281150 ALTERNATOR, HIGH FIELD RESISTANCE. 1H71 3O3 ONT3A12 1E10 20041027000662004102700066CE 2004 10 27 GM82004F00002 120040922A2434991059111RX ALTERNATOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE FAILED D GM8SO OTHER O OTHER NRNOT REPORTED 1 SW0576LU 237 17281150 ALTERNATOR, HIGH FIELD RESISTANCE. 1H71 3O3 ONT3A12 1E10 20041027000702004102700070CE 2004 10 27 2004F00416 120041018A5730310R SKIN CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO LT WING CRACKED E K NONE O OTHER ININSP/MAINT 1 GL11134JR7073 310R2117 DURING MAINTENANCE WORK ON THE LT CENTER WING LOCKER BAY COMPARTMENT FUEL TANK, MAINTENANCE FOUND A WING SKIN CRACK OF 3.0 INCH AT APPROX WING STATION 60.00 AND FUSELAGE STATION 54.00. THE CRACK RUNS NEAR THE LT LANDING GEAR UP AND DOWN MECHANISM SUPPORT STRUCTURE. TWO OTHER CRACKS FOUND NEAR THE SAME AREA A .75 INCH AND A .5 INCH. A DAMAGE REPORT WAS SENT TO MFG, WAITING FOR ENGINEERING RECOMMENDATIONS. THERE WERE NO SIGNS OF EXISTING REPAIRS OR MODIFICATION ON THE DAMAGED AREA. 1L72 3O3 O 3A10 E5CE 20041027000712004102700071CE 2004 10 27 XZA2004F00000 120040923A3234551417527 HANDLE CESSNA500 S550 2076607CE PWA JT15 JT15D4 52112NE LANDING GEAR STUCK B XZARO OTHER O OTHER NRNOT REPORTED 1 EA1797SK 4416 S5500127 LANDING GEAR WOULD NOT EXTEND WITH ACTUATION OF SELECTOR HANDLE DOWN. EMERGENCY EXTENSION WAS ACTIVATED, AC LANDED WITH OUT INCIDENT. AFTER JACKING AND INSPECTING SYS, IT WAS FOUND THAT LANDING GEAR HANDLE WOULD MOVE UP AND DOWN, BUT THE SPRING LOADED IN AND OUT MOTION WAS STUCK OUT. THIS CAUSED THE DOWN SWITCH NOT TO MAKE CONTACT WITH THE HANDLE, AND NOT ALLOWING THE LANDING GEAR TO EXTEND. LUBRICATION OF THE SPRING AND SLIDER PORTION OF THE SELECTOR HANDLE WITH SPRAY LUBRICATE FREED UP THE MECHANISM AND ALLOWED CONTACT BETWEEN THE SWITCH AND HANDLE. THE ONLY REQUIREMENT FOUND FOR LUBRICATION OF MECHANISM IS DURING INSTALLATION, WHICH AFTER A PERIOD OF TIME COULD LEAD TO STICKING OF HANDLE AND SLIDER. 1L72 4F4 FRTA22CE E1NE 20041027000762004102700076SW 2004 10 27 KHS2004F00000 120040823A2911MS28775212 O-RING BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NR1 HYD ACCUM CUT E KHSAO OTHER O OTHER NRNOT REPORTED 1 NM11144WA HT291 30524 NR 1 HYD SYSTEM ACCUMULATOR O-RING (PN MS28775-212) FAILURE, CAUSING LOSS OF HYDRAULIC FLUID IN THAT SYSTEM. NR 1 SYSTEM WAS SHUT OFF AND AIRCRAFT RETURNED TO AIRPORT ON NR 2 SYSTEM WITH NO FURTHER INCIDENT. NR 1 HYDRAULIC ACCUMULATOR O-RING, (PNMS28775212). BATCH NR 64909 REPLACED, HYDRAULIC FLUID REFILLED AIRCRAFT. GROUND RUN LEAK CHECK PERFORMED, TEST FLIGHT PERFORMED. AIRCRAFT RELEASED FOR RETURN TO SERVICE. 1G71 4U4 U H4SW E22EA 20041027000822004102700082EA 2004 10 27 ONQ2004F00000 220040810A8520LW12697 CRANKSHAFT CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA ENGINE BROKEN E ONQAO OTHER O OTHER NRNOT REPORTED 1 SO116454M 15284736 L2193615 CRANKSHAFT BROKE IN HALF. CRACK WAS LATERAL ACROSS THE THROW IN FRONT OF THE MIDDLE JOURNAL AND BEHIND THE NR 1 AND NR 2 CRANK PIN. CRACKSHAFT MARKINGS W5340 BS N50. ENGRAVED ON END R19119-1 AND S91660-1. LOWER END OVERHAULED, CASE INSPECTED AND CONDEMNED AFTER DISASSEMBLY. 1H71 3O3 ONT3A19 E223 20041027000902004102700090EA 2004 10 27 UIEA200400182 120041008A533074747UF SKIN MNMITEM18 M18LA 5870108EA LYC O145 O145B1 41502EA FUSELAGE SCRATCHED A UIEAO OTHER O OTHER NRNOT REPORTED 1 EA01498M 23151 107 STA 2577-2598 RBL 12 LOWER SKIN 3 EACH SCRATCHES. SCRATCHED AREA SMOOTHED OUT IAW SRM 53-00-01 FIG 101. PROTECTED AREA IAW SRM 51-20-01. PERFORMED HFEC INSPECTION ON THE EXTERNAL SKIN NO CRACKS FOUND. 1L71 3O3 O A803 TC210 20041027000922004102700092CE 2004 10 27 MGO2004F00000 120040909A3350 SCREW BEECH B300 B300 1159232CE PWA PT6 PT6* 52043EA BATTERY HOLDER CHAFED G MGORO OTHER O OTHER NRNOT REPORTED 1 CE09300TM FL50 WHILE COMPLYING WITH TIME SCHEDULE REPLACEMENT OF THE EMERGENCY EXIT LIGHT BATTERIES, FOUND THAT THE BATTERIES HAD LEAKED ACID AND CORRODED THE BATTERY HOLDERS. FOUND THE BATTERY HOLDER SCREWS HAD CHAFFED THROUGH THE BATTERY SIDE LABEL AND SHORTED BATTERY TO EXIT LIGHT ASSY CAUSING THE BATTERIES TO OVERHEAT AND BOIL ACID OUT. FILED HEAD OFF BUTTON HEAD SCREW AND APPLIED TEFLON TAPE FOR CHAFE PROTECTION. RECOMMEND BATTERY HOLDER MOUNTING SCREWS BE CHANGED FROM BUTTON STYLE TO COUNTER SUNK SCREWS. (CE09200404792) 2L72 4T3 TRTA24CE E2NE 20041027000992004102700099SO 2004 10 27 ZVS2004F00000 220041009A7414 IMPULSE COUPLINGSLICK BEECH 58 58 1152740CE CONT O550 IO550C SO MAGNETO BROKEN D ZVSRO OTHER O OTHER NRNOT REPORTED 1 SO113101B 98110601 TH1901 684270 PILOT REPORTED DEAD LT MAGNETO, RT ENGINE. TROUBLESHOT AND FOUND IMPULSE COUPLING CAM ASSY BROKEN. THE PAWL RIVETS HAD COME LOOSE AND SEPARATED. THE MAG BEARINGS WERE STIFF BUT DID NOT SEEM TO BE THE CAUSE. 1L72 3O3 O 3A16 E3SO 20041027001002004102700100SO 2004 10 27 OG52004F00002 120041007A1430NAS82066X BOLT PIPER PA28 PA28R201 7102816SO LYC O360 IO360A1A 41514EA LT WING ATTACH WORN B OG5RO OTHER O OTHER NRNOT REPORTED 1 GL21283ND773 2844025 DURING SCHEDULED INSPECTION, WING ATTACH BOLT WAS FOUND TO BE LOOSE. THIS SAME BOLT HAD BEEN REPLACED IAW EO 1 YEAR PRIOR. AT THAT TEIM 3 OTHER AC IN OUR FLEET WERE SIMIALRLY REPAIRED. MFG HAS BEEN CONTACTED AND IS WORKING ON REPAIR. (GL21200500264) 1L71 3O3 O 2A13 1E10 20041027001052004102700105EU 2004 10 27 SWAA043079 220041022A7532121664 SHAFT BOEING737 7373H4 1384600NM CFMINTCFM56 CFM562AFR 13802EU NR 1 ENGINE INOPERATIVE A SWAAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SW29343SW 24151 AIR TURNBACK, UNABLE TO STAY BELOW MAX CONTINUOUS EGT DURING CLIMBOUT TO FL 26, NR 1 EGT WAS 900 DEGREES TO 910 DEGREES AT CLIMB N1. REMOVED AND REPLACED NR 1 ENGINE VBV MOTOR SHAFT PER MM. 2L72 4F4 FRTA16WE E21EU 20041027001062004102700106EA 2004 10 27 COMA0460586 120041020A5330601R3114627 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01940CA24672 7048 DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011) 2 CRACKS WERE FOUND IN THE PRESSURE FLOOR SKIN FORWARD AND AFT TO FS 461.0, BETWEEN BL 0.0 AND RBL 9.0. THE FORWARD CRACK 2.25 INCH IN LENGTH. THE AFT CRACK WAS 1 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9-29-2003. 2L72 4F RTA21EA 20041027001082004102700108EA 2004 10 27 COMA0470075 120041022A27505913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA LEFT UNRELIABLE A COMAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01355CA5227 10067 FLIGHT 5880 FLAP FAULT STATUS MESSAGE. REPLACED THE LT INBOARD SKEW DETECTOR. 2L72 4F RTA21EA 20041027001102004102700110NM 2004 10 27 SWAA043094 120041025A335090083 BATTERY BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 19 DEF, INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041027001112004102700111NM 2004 10 27 SWAA043104 120041025A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 765, STRINGER 21R, BS 870, STRINGER 23R. REPAIRED SKIN SECTIONS PER EA AND SRM. 2L72 4F RTA16WE 20041027001162004102700116NM 2004 10 27 SWAA043068 120041022A53116517684 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 303.9, STRINGER 16L, CRACKED. REPAIRED FRAME SECTION PER SB AND SRM. 2L72 4F RTA16WE 20041027001172004102700117NM 2004 10 27 SWAA043069 120041022A53116546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 807, BL 0, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041027001182004102700118NM 2004 10 27 SWAA043070 120041022A53206545833 STIFFENER BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR STIFFENER UPPER CHORD AT BS 270, LBL 6, WL 207.5, CORRODED. REPAIRED FLOOR STIFFENER UPPER CHORD PER EA. 2L72 4F RTA16WE 20041027001192004102700119NM 2004 10 27 SWAA043071 120041022A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 945, STRINGER 21R AND STRINGER 21L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041027001202004102700120NM 2004 10 27 2004UALA00960 120041014A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29660UA 27115 EEL LIGHTS INOP BY ROWS 15AB THRU 19AB. REPLACED POWER STRIP. 2L72 4F4 FRTA1NM E24NE 20041027001212004102700121SO 2004 10 27 C2XA04SH524 120041022A321014571035005 BEARING CAP EMB 145 EMB145ER 3260211SO LT MLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK FOUND THE LEFT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01. 2L72 4F RTT00011AT 20041027001222004102700122SO 2004 10 27 C2XA04SH523 120041022A321014571035413 BEARING CAP EMB 145 EMB145ER 3260211SO LT MLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK FOUND THE LEFT MAIN GEAR AFT BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01. 2L72 4F RTT00011AT 20041027001232004102700123EA 2004 10 27 COMA0460574 120041021A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01977CA 7157 FLIGHT 5483 FLAPS FAIL MESSAGE. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20041027001242004102700124EA 2004 10 27 COMA0460575 120041021A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01797CA 7344 FLIGHT 5376 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20041027001272004102700127NM 2004 10 27 AALA20041062 120041020A3350 LIGHT BOEING757 757223 1384957NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21692AA 26972 SFO - AISLE EMERGENCY EXIT LIGHTS AT 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY ON SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041027001282004102700128NM 2004 10 27 SWAA043087 120041025A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29364SW 26575 FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20041027001292004102700129NM 2004 10 27 SWAA043088 120041025A53116546520 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 400 AND BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041027001302004102700130NM 2004 10 27 SWAA043089 120041025A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 480, LBL 69, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041027001312004102700131NM 2004 10 27 SWAA043090 120041025A53156546809 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB AT BS 947.5, LBL 37 CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER ER. 2L72 4F RTA16WE 20041027001322004102700132SO 2004 10 27 C2XA04SH517 120041014A532014521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION CORRODED AT FRAME 20. REPLACED THE BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041027001332004102700133SO 2004 10 27 C2XA04CL103 120041006A4920 ODOR EMB 145 EMB145LR 3260212SO APU DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2716559 145603 CREW REPORTED THAT DURING START OF APU THERE WAS A STRONG ODOR OF FUEL IN THE CABIN. MAINTENANCE OPERATIONALLLY CHECK AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041027001342004102700134NM 2004 10 27 2004UALA00849 120040921A2120 SMOKE BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DETECTED A UALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 WP29548UA 25396 EICAS MESSAGE INDICATING SMOKE IN FORWARD EQUIPMENT COMPARTMENT. *S/D* CAUSE IS UNKNOWN. SINCE NO SMOKE SOURCE WAS FOUND (NO RELATED EQUIPMENT FAILURES), FWD EQUIPMENT COOLING FILTER WAS ALSO REPLACED. 2L72 4F4 FRTA2NM E17NE 20041027001352004102700135NM 2004 10 27 2004UALA00850 120040923A2781 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLATS ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29676UA 30028 LEADING EDGE SLAT ASYMMETRY EICAS DISPLAYED. ACCOMPLISHED APPROPRIATE FAULT ISOLATION MANUAL, AND AIRCRAFT MAINTENANCE MANUAL PROCEDURES. BITE TESTED THE FSEU, AND PSEU, INSPECTED ALL TARGETS. OPERATED THE FLAPS ELECTRICALLY AND HYDRAULICALLY. NO FAULTS FOUND UNABLE TO DUPLICATE INTERMITTENT EICAS MESSAGE. 2L72 4F4 FRTA1NM E24NE 20041027001372004102700137SO 2004 10 27 C2XA04CL104 120041007A4920 BLEED VALVE EMB 145 EMB145LR 3260212SO APU ODOR A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2716559 145603 THE CREW REPORTED STRONG SMELL OF FUEL IN CABIN AND COCKPIT DURING APU START. BLEED VALVE REPLACED AN OPERATIONALLY CHECKED OK. 2L72 4T RTT00011AT 20041027001382004102700138SO 2004 10 27 C2XA04SH510 120041002A574114567045002 TORQUE BOX EMB 145 EMB145ER 3260211SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING C-CHECK EDDY CURRENT INSPECTION OF THE RIGHT WING INBOARD TORQUE BOX INDICATED A CRACK AT THE FORWARD TWO HI-LOK POSITION. REAMED THE AFFECTED HI-LOK HOLES TO THE NEXT OVERSIZE IAW EMB SRM 51-40-04. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041027001392004102700139SO 2004 10 27 C2XA04TY167 120041011A532014522459003 SUPPORT ANGLE EMB 145 EMB145XR 3260214SO GALLEY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718101 145590 DURING C-CHECK RAMP SUPPORT ANGLE IN THE GALLEY AT FRAME 20, STATION 5633.0 WAS FOUND CORRODED. REPLACE THE RAMP SUPPORT ANGLE IAW EMB SRM 51-21-04 AND CMP 51-21-04. 2L72 4F RT 20041027001412004102700141SO 2004 10 27 C2XA04SH515 120041010A532014530628001 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED BETWEEN FRAMES 23 AND 25. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-22-10. 2L72 4T RTT00011AT 20041027001422004102700142SO 2004 10 27 C2XA04SH518 120041014A532014521700005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-21-10, FIGURE 201. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041027001462004102700146NM 2004 10 27 2004UALA00791 120040820A2120 SMOKE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29668UA 30024 RETURNED TO FIELD DUE TO SMOKE IN COCKPIT. 2L72 4F4 FRTA1NM E24NE 20041027001482004102700148NM 2004 10 27 2004UALA00902 120041002A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE AFT CARGO PIT DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 AFT CARGO PIT STA 1420 FRAME DENTED ON UPPER FLANGE BY STR 26L. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041027001492004102700149NM 2004 10 27 2004UALA00903 120040929A5310 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE CREASE BEAM CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 CABIN CREASE BEAM SHEAR WEB AT LBL 70.5 FROM STA 960 TO 984 IS CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR WEB. 2L72 4F4 FRTA2NM E17NE 20041027001502004102700150SO 2004 10 27 C2XA04BT105 120041009A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712957 145080 DURING INSPECTION FORWARD LOWER AND CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER 1 INVERTER. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041027001512004102700151SO 2004 10 27 C2XA04BT107 120041010A2120 ODOR EMB 145 EMB145LR 3260212SO COCKPIT DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2711547 145563 CREW REPORTED STRONG BURNING SMELL OF OIL IN COCKPIT DURING ENTIRE FLIGHT. RAN ENGINES AND APU AND COULD NOT DUPLICATE ITEM. 2L72 4T RTT00011AT 20041027001522004102700152SO 2004 10 27 C2XA04SH519 120041001A532014521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING INSPECTION THE LEFT OMEGA BEAM FOUND TO BE CORRODED AT FRAME 19A-23. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159. 2L72 4F RTT00011AT 20041027001532004102700153NM 2004 10 27 SWAA043095 120041025A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29454WN 29851 DURING SPV, FOUND EEPLS COVER AT OVERWING EXIT MISSING. INSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041027001552004102700155NM 2004 10 27 SWAA043105 120041025A55316546872 SPAR BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD LUGS CORRODED. REPAIRED VERTICAL STAB PER ER. 2L72 4F RTA16WE 20041027001572004102700157NM 2004 10 27 SWAA043080 120041023A335020131A BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED RON, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041027001592004102700159 2004 10 27 SWAA043082 420041023A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041027001622004102700162NM 2004 10 27 CALA0400687 120041024A5315BAC1505100246 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712327 23457 INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, LBL 6 TO RBL 6. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. 2L72 4F RTA16WE 20041027001632004102700163SO 2004 10 27 C2XA04BT109 120041014A33502013A BATTERY EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714959 145091 CREW REPORTED OVERWING EMERGENCY LIGHT AND GALLEY EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20041027001652004102700165NM 2004 10 27 CALA0400680 120041019A53216546801 FLOORBOARD BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712327 23457 INSPECTION FOUND UPPER AFT FLANGE OF CABIN FLOORBOARD CORRODED AT NUT PLATE HOLE, STA 360, RBL 2. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51. 2L72 4F RTA16WE 20041027001672004102700167SO 2004 10 27 C2XA04SD009 120041019A33501317 BULB EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 DURING INSPECTION RIGHT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT WING EMERGENCY LIGHT BULB. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041027001682004102700168EA 2004 10 27 COMA0470073 120041012A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA NR 1 FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01642CA2526 10125 FLIGHT 5860 EDP NR 1 INOP WARNING. REPLACED THE EDP. 2L72 4F RTA21EA 20041027001722004102700172NM 2004 10 27 SWAA043107 120041025A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 747, FROM RBL 9 TO RBL 13, WL 146, CORRODED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20041027001732004102700173EA 2004 10 27 COMA0460568 120041003A3230601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01949CA23224 7080 FLIGHT 5994 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20041027001742004102700174SO 2004 10 27 C2XA04SH520 120041001A532014521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING INSPECTION THE LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159. 2L72 4F RTT00011AT 20041028000012004102800001CE 2004 10 28 CNQ2004FAAAA 120041001A3240631701339 LINE CESSNA525 525A 2076615CE WILINTFJ44 FJ442A GL BRAKE ASSY BROKEN B CNQDO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP05567JP1281 525A0011 THE AIRCRAFT WAS ON A FERRY FLIGHT WITH GEAR DOWN DUE TO A DAMAGED LANDING GEAR DOOR. UPON LANDING, THE AIRCRAFT HAD NO BRAKES AND HYDRAULIC FLUID WAS STREAMING FROM THE LT WHEEL WELL. DURING CLOSER INSPECTION IT WAS NOTED THAT THE HARD, BRAKE LINE IN THE LEFT WHEEL WELL HAD BROKEN IN HALF. THIS IS THE SECOND OCCURANCE OF SUCH A FAILURE ON THIS MODEL AIRCRAFT. 1L71 4F4 FRTA1WI E3GL 20041028000022004102800002NE 2004 10 28 21200003AAA 220041015A7200 ENGINE BOEING767 767300 1385204NM GE CF6 CF680C2B7 NE NR 1 VIBRATION H E ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW99VPBAZ 30111 704956 NR 1 ENGINE INFLIGHT SHUTDOWN DUE TO VIBRATION. 2L72 4F4 FRTA1NM E13NE 20041028000032004102800003NM 2004 10 28 AWXA200401088 120040930A1420BACC63BV22B19SN CONNECTOR BOEING757 7572G7 1384963NM LT MLG SHORTED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28909AW 24522 ON CLIMB OUT OF PHX EN ROUTE TO MSP WHEN SELECTING LANDING GEAR UP THE LANDING GEAR WOULD NOT RETRACT, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT WIRING AND FOUND SHORT TO GROUND ON PIN 11 OF L/H MAIN LANDING GEAR TILT SENSOR CONNECTOR D40084J. REMOVED PINS 11 AND 12 FROM CONNECTOR D40084J AND RESISTANCE DISAPPEARED. REPLACED CONNECTOR D40084J IAW WDM REF. D280N012. PERFORMED LANDING GEAR RETRACTION TEST IAW BMM 32-32-00, TILT SENSOR TEST IAW BMM 32-09-07, L/H LANDING GEAR TRANSDUCER TEST IAW BMM 32-41-06, AND BRAKE TEMPERATURE TEST IAW BMM 32-46-00, ALL TESTS WERE GOOD. 2L72 4F RTA2NM 20041028000062004102800006NM 2004 10 28 BB04087 120040930A3397 WIRE BOEING767 7672B7 1385107NM IAE V2527 V2527A5 NE EMERGENCY LIGHT BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19656US 26847 CDG FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE, ROWS 13-18 LT. MAINTENANCE4 FOUND AND REPAIRED A BREAK IN THE WIRING. 2L72 4F4 FRTA1NM E40NE 20041028000092004102800009WP 2004 10 28 ARWA20040905 120040930A2697 WIRE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE FIRE DETECTION BROKEN A ARWAK NONE N FALSE WARNING ININSP/MAINT 1 SO19661AV 45969 NR 2 ENGINE FIRE DETECTION TEST FIRE SHUTOFF LEVER LIGHTS VERY DIM AND C/B POPPED OUT. REPAIRED WIRES OF FIREWALL DISC. BOX ENGINE NR 2 IAW MM 20-50-1. PERFORMED OPERATIONAL CHECK TEST DETECTION SYSTEM IAW M/M 26-10-0, FOUND NORMAL. 2L74 4F4 F 4A25 1E8 20041028000112004102800011EA 2004 10 28 ASOA04466 120040629A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27885AS 7521 DURING A (C) CHECK, THE RT IB CLIP AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT IB CLIP AT FS 280. 2L72 4F4 FRTA21EA E15NE 20041028000132004102800013NE 2004 10 28 04FDEA02329 220040730A7200 CASE DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 NR 2 ENG LT FAN CASE MOST AFT FRAME FOUND CRACKED AT 10 O'CLOCK POSITION. STOP DRILL AS PER AMM 72-33-00-81 AND CONFIRMED CRACK TERMINATED BY STOP DRILL BY FLOURESCENT PENETRANT INSPECTION (FPI) AS PER AMM 70- 10-05-21. 2L73 4F4 FRTA22WE E13NE 20041028000152004102800015NM 2004 10 28 04FDEA02332 120040801A5512ALC8103504 SKIN PANEL DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT HORIZONTAL STABILIZER NR 35R BARREL NUT BORE FOUND WITH CORROSION, CLEANED UP AND FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80293. 2L73 4F4 FRTA22WE E13NE 20041028000162004102800016NM 2004 10 28 04FDEA02333 120040801A5753ARC2512504 BRACKET DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 OB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03. 2L73 4F4 FRTA22WE E13NE 20041028000222004102800022 2004 10 28 AWXA200400764 420040710A344146502003030314 ADIRU AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE ZONE 123 FAILED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 WP28819AW14137314 1395 AIR TURN BACK, ON CLIMB OUT, EN ROUTE, RECEIVED ADR NR 1 FAULT MESSAGE, SWITCHED TO ADR NR 3 AND LOST NAV DISPLAY AND PRIMARY FLIGHT DISPLAY INTERNAL REF INFO, TURNED BACK FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 1 AIR DATA INERTIAL REFERENCE UNIT (ADIRU) IAW T/C R2A34304, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF ADIRU S/N 2540 CONFIRMED FAILURE OF UNIT, PERFORMED THERMAL CALIBRATION AND ACCOMPLISHED SB 101-34-56 REPLACING THE PCB ASSEMBLY LOW VOLTAGE POWER SUPPLY AND MONITOR. TESTED IAW CMM TP1011, REV. 23. 2L72 4F4 FRTA28NM E311NE 20041028000232004102800023SO 2004 10 28 C2XA04TY120 120040726A532014529495004 SUPPORT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE RT FWD FLOORBOARD SUPPORT SILL IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR BOARD SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF THE 4C INSPECTION. 2L72 4F4 FRTT00011ATTE6CH 20041028000252004102800025SO 2004 10 28 C2XA04TY122 120040726A532014522215407 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION THE CENTER OMEGA BEAM UNDER THE LAV FLOOR WAS CORRODED. MAINTENANCE CLEANED UP THE DAMAGE AREA, BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02;03 AND CPM 51-21-04 AND 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F4 FRTT00011ATTE6CH 20041028000322004102800032EA 2004 10 28 ASOA04471 120040629A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7318 7317 DURING (C) CHECK, THE AVIONICS BAY DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS BAY DOOR HANDLE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20041028000342004102800034EA 2004 10 28 ASOA04474 120040630A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA RIGHT SEIZED A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11920EV12191 7810 DURING CLIMB-OUT FROM DFW-BTR, AT APPROXIMATELY 8,000 FT THE FLT ATTENDANT NOTICED AN ODOR IN THE CABIN FOLLOWED BY WHITE SMOKE AT THE TOP OF THE CABIN. SHORTLY AFTERWARDS THE CREW NOTICED AN ODOR IN THE COCKPIT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DELCARED. THE AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. DURING APPROACH THE FLIGHT ATTENDANT REPORTED THAT THE SMELL AND SMOKE HAS DISAPPEARED. MAINTENANCE FOUND THE RIGHT ACM LOCKED UP AND THE ACM TURBINE SECTION FULL OF OIL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM AND THE COALESCER BAG. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041028000352004102800035EA 2004 10 28 ASOA04480 120040701A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27885AS 7521 DURING (C) CHECK, THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT SIDE FS 484 INTERCOSTAL AT BL 36 AND THE CLIP AT BL 27 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041028000372004102800037EA 2004 10 28 ASOA04469 120040629A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27885AS 7521 DURING (C) CHECK, THE AVIONICS DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS DOOR HANDLE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20041025000072004102500007EA 2004 10 25 SWIA200413942 120041013A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STAB MOTOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07954SW2186 2186 7815 FFOD STAB CH 2 WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT PER AMM 27-42-05. OPERATIONAL CHECK PER AMM 27-40-00 AND 27-41-00 GOOD. 2L72 4F RTA21EA 20041025000102004102500010EU 2004 10 25 TXER096972 120040728A6410355A12004008 BLADE AEROSPAS355 AS355* EU TAIL ROTOR CRACKED B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09747WB768 2768 CRACK AT TRAILING EDGE NEAR TRIM TAB. 1G72 3U H11EU 20041025000232004102500023SO 2004 10 25 SWIA200413947 120041005A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FUSELAGE SEAT TRACK CORRODED BEYOND LIMITS AT FR 38, 479.00 LT. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-40-02, 51-22-00. 2L72 4T RTA31SO 20041025000282004102500028EA 2004 10 25 SWIA200413754 120040823A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07453SW 7743 FS 280 RIGHT HAND FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041025000442004102500044EA 2004 10 25 SWIA200413650 120040725A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07936SW 7726 FS 621 FLOOR SUPPORT ANGLE LEFT HAND SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV-B. 2L72 4F RTA21EA 20041025000492004102500049EA 2004 10 25 SWIA200413848 120040922A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07597SW 7293 CAPT SIDE TRIM SWITCH WILL COMMAND THE SURFACE NOSE DOWN BUT NOT NOSE UP. REMOVED AND REPLACED CAPTAINS TRIM SWITCH IAW 27-41-30. OPERATIONAL CHECK GOOD. P/N 309-4334. 2L72 4F RTA21EA 20041025000512004102500051EA 2004 10 25 SWIA200413818 120040919A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STUCK A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07413SW 7102 MAIN CABIN DOOR WOULD NOT OPEN FROM BOTH INSIDE OR OUTSIDE. FREED DOOR UP, CYCLED OPEN & CLOSED, LOCKED & UNLOCKED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000542004102500054EA 2004 10 25 SWIA200413821 120040920A274170608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07592SW6121 6121 7279 STAB CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000602004102500060NM 2004 10 25 SWAA043023 120041018A53156546810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS ON FLOORBEAMS AT BS 986.5, LBL 52 TO RBL 52, BS 947, RBL 53. REPAIRED FLOORBEAM SECTIONS PER SRM. 2L72 4F RTA16WE 20041025000612004102500061CE 2004 10 25 DJFA2004015 120040801A7910 CAP RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315R 01518WP NR 1 ENG OIL UNSECURE E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING WKJINADEQUATE Q C FLUID LOSS WARNING INDICATION CLCLIMB 1 EA23728TA 258364 P107302 AFTER DEPARTURE FIVE MINUTES INTO THE CLIMB THE NR 1 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW LEVELED AT 270 FT AND THE OIL PRESSURE WAS SLOWLY GOING DOWN, THE OIL PRESSURE LIGHT FLICKERED ON AND OFF AND AT THAT POINT THE CREW DECIDED TO SHUTDOWN THE NR 1 ENGINE. AFTER LANDING AT FTY MAINTENANCE PERSONNEL FOUND THE OIL CAP OFF, SERVICED THE ENGINE WITH 4.5 QTS OF OIL AND PERFORMED GROUND RUNS AND LEAK CHECKED. ALL GROUND RUNS FOUND SATISFACTORY. 2L72 4F4 FRTA3EU E6WE 20041025000632004102500063EA 2004 10 25 SWIA200413828 120040913A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA AILERONS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07947SW 7786 AILERON TRIM GOES LEFT BUT OCCASIONALLY WILL NOT TRIM TOWARD RIGHT WING DOWN. REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000672004102500067EA 2004 10 25 SWIA200413832 120040909A273010231007 DAMPENER CNDAIRCL600 CL6002B19 1900309EA AILERONS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07432SW8170 8170 7548 LEFT FLUTTER DAMPER STATUS MESSAGE APPEARED INFLIGHT. REPLACED FLUTTER DAMPER IAW MM 27-34-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025000692004102500069EA 2004 10 25 SWIA200413834 120040921A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07426SW6987 6987 7468 STAB CH 1 INOPERATIVE INFLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW AMM 27-42-01 AND MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD. HSTCU P/N 8396-3, S/N OFF 1159. 2L72 4F RTA21EA 20041025000962004102500096SO 2004 10 25 SWIA200413951 120041005A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOOR SUPPORT STRUCTURE AT FR 38 - 40, STR 15R. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025000982004102500098SO 2004 10 25 SWIA200413953 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 FUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025001002004102500100SO 2004 10 25 SWIA200413955 120041005A5315 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 CORROSION FOUND AROUND A/NUT HOLES AS MARKED ON FLOOR SUPPORT STRUCTURE AT FR 14 - FR 39, STR 15R. ITEM FOUND AT C-CHECK INSPECTION. BUTTPLATE REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041025001022004102500102NM 2004 10 25 SWAA043028 120041019A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29446WN 29842 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041025001042004102500104NM 2004 10 25 SWAA043037 120041019A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND 7 EACH CRACKS ON FUSELAGE FRAMES FROM BS 787 TO BS 907, STRINGER 8R AND BS 787, BS 827, STRINGER 8L. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041025001092004102500109 2004 10 25 SWAA042985 420041015A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041025001112004102500111NM 2004 10 25 SWAA042987 120041015A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR, LT OVERWING EXIT, AFT ENTRY DOOR, SIDE MOUNTED EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20041025001152004102500115EA 2004 10 25 SWIA200413945 120041011A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07440SW 7589 CAPTAINS SIDE TRIM SWITCH STICKS. REMOVED AND REPLACED PITCH TRIM SWITCH (CAPTAINS SIDE) WITH SERVICEABLE UNIT IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001172004102500117EA 2004 10 25 SWIA200413886 120041002A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07938SW 7741 FLAPS FAIL MESSAGE APPEARED WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001192004102500119SO 2004 10 25 SWIA200413888 120041001A2750 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAPS DIRTY A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07268UE 120207 AFTER SELECTING FLAPS 15 DEGREES, FLAP WARNING CONTROL FAULT ASSOC WITH FLAP AND ADV SWS ON MAP PANEL. CLEANED FLAP TRACKS AND CONNECTORS. ALL SYSTEM'S OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025001212004102500121EA 2004 10 25 SWIA200413966 120041005A5310 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW FS 409 + 128 LEFT VERTICAL BEAM AT LBL 27 LOWER INBOARD FLANGE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BEAM IAW CRJ REO 601R-53-41-056. 2L72 4F RTA21EA 20041025001242004102500124NE 2004 10 25 NACA20040029 220040824A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 4 CRACKED A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL0399330862 862 43576 35205 NR 4 ENGINE SHUT DOWN DUE TO OIL LOSS. NR 4 CYLINDER CRACKED. REPLACED NR 4 CYLINDER. OP AND LEAK CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20041025001262004102500126NM 2004 10 25 SWAA043013 120041017A5320BAC1505 GUSSET BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER FWD STOP FITTING GUSSET CRACKED. REPAIRED GUSSET PER SRM. 2L72 4F RTA16WE 20041025001282004102500128EA 2004 10 25 SWIA200413903 120041009A2750855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA BRAKE MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07938SW4037 4037 7741 FLAP FAIL MESSAGE ON TAXI OUT AT 13 DEGREES. REMOVED AND REPLACED RIGHT BPSU PER CRJ MM 27-51-10. REMOVED AND REPLACED NR 2 INBOARD FLAP ACTUATOR AND NR 1 RIGHT INBOARD FLAP ACTUATOR IAW CRJ MM 27-53-01. OPERATIONAL CHECK GOOD. NR 1 P/N 852D100-19, S/N OFF 4483. NR 2 P/N 852D100-19, S/N OFF 4487. 2L72 4F RTA21EA 20041025001302004102500130NM 2004 10 25 CALA0400676 120041008A52306547952537 SKIN BOEING737 7373T0 1384582NM AFT CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 AFT CARGO DOOR HAS PREVIOUS REPAIR REQUIRING REPLACEMENT. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED PRIMED AND INSTALLED NEW DOUBLER PER EC/RA 5232-01049. 2L72 4F RTA16WE 20041025001322004102500132EA 2004 10 25 SWIA200413857 120040925A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07924SW65 65 7681 STAB CHANNEL 2 AND MACH TRIM DISENGAGED AND COULD NOT BE RE-ENGAGED. INSTALLED SERVICEABLE HSTCU IAW CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-41-00. 2L72 4F RTA21EA 20041025001392004102500139EA 2004 10 25 SWIA200413946 120041011A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 NM07918SW5707 5707 7645 FLAPS FAIL MESSAGE ON APPROACH TO LANDING. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041025001402004102500140EA 2004 10 25 MASA200400332 120040614A3350364911 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07591ML 7388 ASH 2810 YUL - CLT, EMERGENCY EXIT FLOOR STRIPS INOP. CONTRACT MX TROUBLESHOOTING, MX REPLACED LIGHTING STRIP AND BATTERY. BATTERY PART NR 2013-1A. 2L72 4F RTA21EA 20041025001412004102500141SO 2004 10 25 MASA200400390 120040709A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07847MJ 145517 ASH 2994 DCA, CREW REPORTED THE EMERGENCY EXIT LIGHT AT GALLEY INOP. MX TROUBLESHOT TO BAD POWER SUPPLY. MX REPLACED THE POWER SUPPLY ASSY. 2L72 4T RTT00011AT 20041025001422004102500142EA 2004 10 25 MASA200400406 120040716A335020131A BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07653ML 7039 ASH 2668 PHL - GSP, CREW REPORTED THE EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK. 2L72 4F RTA21EA 20041025001552004102500155SO 2004 10 25 SWIA200413883 120040929A2120 ODOR EMB 120 EMB120ER 3260203SO COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 NM07215SW 120281 ON TAKEOFF ROLL BOTH PILOTS SMELLED SMOKE AND LAV SMOKE DETECT ALARM SOUNDED. C/B POPPED. REMOVED AND REPLACED RCCB 0208 WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041025001572004102500157EA 2004 10 25 SWIA200413970 120041005A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 FUSELAGE FLOOR SUPPORT INTERCOSTAL AT STA 484.00 INBOARD FLANGE AT LBL 27 + OUTBOARD FLANGE AT LBL 36 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV "A". 2L72 4F RTA21EA 20041025001602004102500160SO 2004 10 25 SWIA200413895 120040724A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07268UE 120207 LEFT FLOOR PROP AT FRAME 13 CRACKED. REPAIRED LEFT FLOOR PROP AT FRAME 13 IAW SRM 53-10-10 PAGES 214 - 220. 2L72 4T RTA31SO 20041025001642004102500164NE 2004 10 25 AALA20041032 220041006A73208061865 EEC BOEING767 767323 1385205NM GE CF6 CF680C2B6F 30025NE RT ENGINE INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21368AA 25195 695306 DFW - INFLIGHT T997/06 RIGHT ENGINE FUEL VALVE MESSAGE WITH RIGHT ENGINE VALVE LIGHT ON APPROXIMATELY 40 MINUTES AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE MAIN ENGINE CONTROL PER MCM 71 95 20 AND 73 94 02. REPLACED FIRE LEVER PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E13NE 20041025001662004102500166WP 2004 10 25 AALA20041035 120041010A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21951U 49245 DFW - AFT ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B527 FOR AFT ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041025001682004102500168WP 2004 10 25 AALA20041036 120041010A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21951U 49245 DFW - TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B527 FOR TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041026000052004102600005NM 2004 10 26 SWAA043062 120041021A521065458712 FRAME BOEING737 7375H4 138449DNM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AT AFT INBOARD LOWER STOP CRACKED. REMOVED AND REPLACED SERVICE DOOR PER MM. 2L72 4F RTA16WE 20041026000072004102600007NM 2004 10 26 SWAA043064 120041021A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS FROM BS 570 TO BS 602, STRINGER 4L. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041026000102004102600010EU 2004 10 26 AWXA200400937 120040829A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 221 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28625AW 064 CMH - EEL - DURING 8-DAY CHECK THE LEFT FORWARD EMERGENCY LIGHT BATTERY PACK FAULTED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE LEFT FORWARD EMERGENCY POWER SUPPLY UNIT 10WL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041026000172004102600017NM 2004 10 26 UPS04242998 120040804A5330 DOUBLER BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BS 304 BETWEEN S8L AND S10L. AFTER BLENDING CORROSION FOUND TO BE EXTENSIVE. ACCESS PROVIDED AND A 1 INCH CRACK FOUND IN UPPER FWD ENTRY DOOR. AREA REPAIRED IAW QUERY RESPONCE AAAE-2004-073-31. 2L73 4F A3WE 20041026000192004102600019NM 2004 10 26 UPS04242887 120040802A5755 SPOILER BOEING727 72725C 138400HNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 RT WING GROUND SPOILER WEB JUST BELOW ACTUATOR HAS CRACK IN LOWER CHORD. REPAIRED .75 INCH CRACK IN L-ANGLE IAW 727 SRM 51-40-04 FIG 1. 2L73 4F A3WE 20041026000242004102600024WP 2004 10 26 UPS04842867 120040629A52405750988 SKIN DOUG DC8 DC871F 302199DWP L2 DOOR BENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, CABIN FWD LOWER CORNER OF L2 DOOR BENT AND TURN METAL. FAB ANGLE DOUBLER, Z-ANGLE SHIM, INNER SKIN SHIM, AND DOUBLER SKIN. ALODINED 2 SHIMS, DOUBLER INNER, PRIMED 2 SHIMS & DOUBLER INNER SKIN. RECEIVED HEAT TREAT. LOCATED & DRILLED. ALODINED ANGLE DOUBLER. PRIMED ANGLE DOUBLER, INSTALLED ANGLE DOUBLER, 2 SHIMS, DOUBLER INNER SKIN. ALL IAW DC8 SRM 51-1-21, 52-2-5, 51-1-8, 52-3-1, 52-2-0. 2L74 4F RT4A25 20041026000292004102600029EA 2004 10 26 SWIA200413813 120040828A2121AE0405A02 FAN CNDAIRCL600 CL6002B19 1900309EA GALLEY ODOR A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07589SW 7072 GALLEY FAN GETS HOT AND SMELLS LIKE SMOKE. REPLACED GALLEY EXHAUST FAN ASSY. OPERATIONAL CHECK GOOD. P/N AE0405A02, S/N OFF 0739. 2L72 4F RTA21EA 20041026000502004102600050SO 2004 10 26 SIMA200428703 120041001A2560PL078009120 FLASHLIGHT EMB 135 EMB135KL 3260302SO CABIN ODOR A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21846AE 145692 STRONG ELECTRICAL ODOR IN FORWARD CABIN. ODOR ISOLATED TO FLIGHT ATTENDANTS FORWARD FLASHLIGHT. REPLACED FLIGHT ATTENDANTS FORWARD FLASHLIGHT IAW EMB 145 MM 25-60-00, OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20041026000542004102600054EA 2004 10 26 A6WA200440139 120040929A2150 ACM CNDAIRCL600 CL6002B19 1900309EA LEFT ODOR A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31431AW 7256 VERY STRONG ACRID SMELL COMING FROM AIR CONDITIONING PACKS. GOT WORSE WHEN TEMP CHANGES. REMOVED AND REPLACED LEFT ACM IAW AMM 21-51-10. (M) 2L72 4F RTA21EA 20041026000552004102600055SO 2004 10 26 SIMA200426905 120040915A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21732DH 145358 DURING AN IMBV INSPECTION, THE FORWARD GALLEY FLOOR DIGITAL WAS FOUND CORRODED. CUT OUT A DAMAGED SECTION FROM EXISTING DIGITAL AND CLEANED AREA. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 AND 51-40-06. (M) 2L72 4F RTT00011AT 20041026000592004102600059EU 2004 10 26 ASOA04763 120040910A5210 SKIN AEROSPATR72 ATR72 EU PAX DOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK, AFT LOWER CORNER SKIN AND RIVET ON THE PAX DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT LOWER CORNER SKIN AND RIVET ON THE PASSENGER DOOR AIW SRM 52-11-00, FIG 412. (M) 2H72 4T RT 20041026000622004102600062EU 2004 10 26 USAASA04049 120040514A49209560161520 RING AIRBUS320 A320214 3930316EU APU TURBINE LEAKING A USAAA UNSCHED LANDING KHJFLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA19101UW13804 0936 PIT - FLT 127 - EN ROUTE PHL-SAN, WITHT NE NR 2 ENGINE INTEGRATED DRIVE GENERATOR IDG ON MINIMUM EQUIPMENT LIST MEL, THE AUXILIARY POWER UNIT APU, SHUTDOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE IDG AND REMOVED THE MEL. THE APU WAS THEN PLACED ON MEL. THE APU WAS LATER REPLACED DUE TO AN INTERNAL OIL LEAK. THE SHOP REPLACED THE REAR TURBINE BEARING CARBON SEAL. (M) 2L72 4F RTA28NM 20041026000792004102600079SO 2004 10 26 SIMA200427301 120040929A27413621005009M2 CONTROL UNIT EMB 145 EMB145LR 3260212SO HORIZONTAL STAB MALFUNCTIONED A SIMAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW21621AE 145105 ORD - FLT 4190 - CREW NOTED A DUAL PITCH TRIM FAIL IN FLIGHT. CREW RESET THE SYSTEM AND CONTINUED WITH NO OTHER FAULTS REPORTED. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20041026000942004102600094WP 2004 10 26 GTIA040787 120040913A7120K22199SA31 ISOLATOR DOUG DC9 DC981 3022081WP NR 1 ENGINE OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23810NK 48015 DTW - VERIFY LOWER FORWARD VIBRATION ISOLATOR ALIGNMENT MARKS ARE WITHIN LIMITS. REMOVED AND REPLACED FORWARD LOWER NR 1 ENGINE ISOLATOR MOUNT. (M) 2L72 4F A6WE 20041026000952004102600095WP 2004 10 26 GTIA040790 120040928A3260 TARGET DOUG DC9 DC981 3022081WP LT MLG DOOR OUT OF ADJUST A GTIAO OTHER J WARNING INDICATION CRCRUISE 1 GL23811NK 48017 FLL - FLT 1265 - FOUND MAIN GEAR DOOR OPEN LIGHT ON AT CRUISE ALT WENT OUT WITH RT HYD PUMP ON. ADJUSTED LEFT GEAR DOOR SENSOR TARGET. (M) 2L72 4F A6WE 20041026000982004102600098EU 2004 10 26 ASOA04757 120040910A5347 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 38 AND 39 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT SEAT TRACKS BETWEEN FRAME 38 AND 39 IAW SRM 51-25-04 AND 51-25-03. (M) 2H72 4T RT 20041026000992004102600099SO 2004 10 26 SIMA200426907 120040916A532014522178005 SILL EMB 145 EMB145LR 3260212SO SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21620AE 145102 ABI - DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVD THE EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 51-20-01-51-20-03, 51-40-02, 51-40-04 AND 51-40-06. (M) 2L72 4T RTT00011AT 20041026001032004102600103EU 2004 10 26 ASOA04758 120040910A5347NTA44768 SEAT TRACK AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE LEFT SEAT TRACK BETWEEN FRAME 39 TO 40 AND THE RIGHT SEAT TRACK BETWEEN FS 41-43 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT SEAT TRACK BETWEEN FRAME 39 TO 40 AND THE RIGHT SEAT TRACK BETWEEN FRAME 41 AND 43 IAW SRM 51-25-04 AND 51-25-03. (M) 2H72 4T RT 20041026001042004102600104EU 2004 10 26 ASOA04759 120040910A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK IN YUL, THE RIGHT FLOOR SUPPORT BETWEEN FS 38/39, STRINGER 17R AND THE LEFT FLOOR SUPPORT BETWEEN FS 39/40, STRINGER 17L WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SUPPORT BETWEEN FS 38/39, STRINGER 17R AND THE LEFT FLOOR SUPPORT BETWEEN FS 39/40, STRINGER 17L IAW SRM 51-25-01. (M) 2H72 4T RT 20041026001172004102600117EU 2004 10 26 MALA040618 120041017A7110 COWL FLAP SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15451XJ 340B451 RT OB COWL OPENED IN FLIGHT. RT ENG COWL FLAP APPEARED TO BE OPEN DURING FLIGHT. AC RETURNED, MAINTENANCE REMOVED AND REPLACED RT ENG FWD COWL, GOOD TO GO. 2L72 4T4 TRTA52EU E8NE 20041026001252004102600125NM 2004 10 26 DL73S040969 120041015A3350276005 FUSE BOEING737 737247 138448DNM PWA JT8 JT8D15 52051NE BATTERY PACK UNSERVICEABLE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27377DL 23604 ON PREFLIGHT CHECK FWD CABIN EMERGENCY LIGHTS FAILED TO TEST. FOUND ONE BAD FUSE IN FWD BATTERY RACK. REPLACED SAME. CHECKS OK 2L72 4F4 F A16WE E2EA 20041026001342004102600134NM 2004 10 26 P5CA0401256 120041019A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 RT WING UPPER SKIN HAS CORROSION AT WING STATION 697 MID SPAR. BLENDED OUT CORROSION, WITHIN LIMITS IAW SRM 57-30-01 AND 57-30-03. 2L74 4F4 F A20WE E20EA 20041026001682004102600168EA 2004 10 26 QXEA200400725 120041019A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 CORROSION ON BULKHEAD WEB JUST ABOVE FLOOR WEB APPROXIMATELY RT BL 12.0, REPAIRED IAW EA R-53-514. 2L72 4F4 FRTA21EA EOOO63EN 20041026001702004102600170 2004 10 26 RAIA00410012 420041018A3452 TRANSPONDER EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL TCAS INTERMITTENT A RAIAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 CE03820HK 145064 TRANSPONDER LOST MODE-C CAPABILITY, ALSO TCAS FAILED. MAINTENANCE PERFORMED TRANSPONDER TEST AND TCAS SYSTEM TEST. BOTH OPS CHECKED GOOD. 2L72 4F4 FRTT00011ATTE6CH 20041026001762004102600176CE 2004 10 26 DXTA200400426 120041017A3260 WARNING LIGHT CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL MLG ILLUMINATED E DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07942QS 7500024 AFTER TAKE-OFF GEAR WAS SELECTED UP, GREEN LIGHTS WENT OUT, RED LIGHT STAYED ON (GEAR WAS CYCLED BUT THE OUTCOME WAS THE SAME. ) ITEM IS UNDER INVESTIGATION. 2L72 4J4 FRTT00007WITE6CH 20041026001872004102600187EU 2004 10 26 MALA040616 120041016A242031342002 GENERATOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT AC SYSTEM INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15442XJ 340B442 LT AC GENERATOR INOPERATIVE. AIR RETURNED. MAINTENANCE REPLACED LT AC GEN PN ON OFF 31342-003 SN OFF 99042 SN ON 99041 IAW JOB CARD 242102 NO FIX. REMOVED AND REPLACED LT AC GCU PN ON OFF 51634-002, SN OFF 514 SN ON 490 IAW AMM 24-21-01. OPS CHECKS GOOD. 2L72 4T4 TRTA52EU E8NE 20041026001932004102600193EU 2004 10 26 HE66097817 120041021A771230571821 TORQUEMETER BOLKMS105 BO105LSA1 5626021EU ALLSN 250C 250C28 03013GL ENGINE UNSERVICEABLE B HEEAO OTHER N FALSE WARNING CRCRUISE 1 SW03202LF 2014 FLUCTUATING OVER 40 PERCENT WITH NO CHANGE IN N1 OR TOT. 1G72 3U3 U H3AU E1GL 20041027000032004102700003EA 2004 10 27 04293621 120041019A3260 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27621BR 7186 EVENT SUMMARY STATED GEAR DISAGREE. ADJUSTED SWITCH. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041027000042004102700004EA 2004 10 27 04294621 120041020A3260 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27621BR 7186 EVENT SUMMARY STATED GEAR DISAGREE. REMOVED AND REPLACED SWITCH AND PERFORMED GEAR SWINGS. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041027000112004102700011NM 2004 10 27 371PA0056 120040921A5247 INTERCOSTAL BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE APU DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 APU DOOR INTERCOSTAL CRACKED AT HINGE ATTACH BOLT. REPAIRED IAW SRM 51-70-11. 2L72 4F4 FRTA16NE E2GL 20041027000132004102700013NM 2004 10 27 371PA0062 120040920A5311 FRAME BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FRAME CRACKED AT RIVET AT BS 500 AND STR 25LT. REPAIRED IAW SRM 51-70-11. 2L72 4F4 FRTA16NE E2GL 20041027000172004102700017EA 2004 10 27 QXEA200400709 120041010A3320BC50531903 SOCKET CNDAIRCL600 CL6002C10 1390015EA SERV DOOR LIGHT BURNED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM09601QX 10009 ON FLIGHT NR 4308 NOTICED AN UNUSUAL SMELL IN THE COCKPIT AND CABIN AREAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SOURCE OF THE SMELL TO BE THE FLUORESCENT TUBE SOCKET IN THE GALLEY SERVICE DOOR LIGHT. SOCKET ASSEMBLY WAS BURNED. DISCONNECTED POWER FROM THE SOCKET ASSEMBLY AND PLACED ON MEL 33-23-2 #343889. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20041027000292004102700029 2004 10 27 BQT2004F00000 420040910A344240007643201 DISPLAY EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA RADAR FAILED E BQTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NE0549BA 110301 FLIGHT WITH CARGO ON BOARD, PILOT SAID RADAR SCREEN WENT BLANK. SHORTLY AFTER HE SAID THE COCKPIT STARTED TO FILL UP WITH SMOKE. RADIOED TOWER AND DIVERTED FROM INTENDED DESTINATION TO CLOSEST AIRPORT. LANDED WITHOUT INCIDENT WITH THE LOCAL FIRE DEPT STANDING BY. MECHANIC DROVE TO INSPECT THE AIRCRAFT. FOUND WHEN POWER WAS APPLIED WITH THE RADAR ON. THE INDICATOR WOULD START TO SMOKE SIGNIFICANTLY. THE RADAR INDICATOR WAS REMOVED AND THE SYSTEM WAS MEL. PROBABLE CAUSE: COMPONENT AGE. (NE05DAD200400035) 1L72 4T4 T A21SO E4EA 20041027000372004102700037NM 2004 10 27 UPS04443337 120041012A3350 BULB BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01675UP 20390 MAIN CARGO DECK CEILING EMERGENCY LIGHT FWD OF L1 DOOR HAS ONE BULB INOPERATIVE AND VERY DIM. REMOVED AND REPLACED MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST FWD OF L1 DOOR IAW MM 33-51-07. OPS CKS NORMAL. 2L74 4F4 F A20WE E20EA 20041027000472004102700047EA 2004 10 27 04278705 120041004A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MALFUNCTIONED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27705BR 7470 A/C 705 HAD 2 FLAP FAIL ON OCT 4TH. FLAP FAIL AT 20 DEGREES AT 12NOON (RESET FECU, OPS CHK GOOD)FLAP FAIL AT 0 DEGREE AT 2PM (REMOVED AND REPLACED LT FLAP BPSU, OPS CHK GOOD), FLAP FAIL GREATER 5 DEG ON OCT 7TH (BITE TESTED FECU OPS CHECK GOOD). 2L72 4F4 FRTA21EA E15NE 20041027000482004102700048NM 2004 10 27 2004UALA00879 120040917A5320146N871227 SUPPORT ANGLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 MAIN CABIN STA 1681 FRAME SUPPORT ANGLE CORRODED AT STR 17R AT CREASE. SUPPLEMENTAL DATA UPDATE CORRODED SUPPORT ANGLE WAS FABRICATED AND REPLACED. 2L72 4F4 FRTA2NM E17NE 20041027000592004102700059CE 2004 10 27 092904 120040929A2435300SGL138Q4 STARTER GEN CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT ENGINE MELTED E W9FAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA072 552 5605333 DB0679 LT ENGINE FAILED TO START. SEVERE ARCING ON COMMUTATOR, AND BRUSHES. CAUSING BRUSHES TO MELT. 2L72 4F4 FRTA22CE E00059EN 20041027000842004102700084CE 2004 10 27 MW82004F00001 120041001A5711364300566 PLATE BEECH 58 58 1152740CE CONT O550 IO550* SO SPAR CORRODED B MW8RO OTHER O OTHER NRNOT REPORTED 1 SO016788W TH1389 SPAR KIT PN 58-4008-9S WAS ORDERED FROM MFG AND UPON INSPECTION OF KIT, PITTING WAS NOTICED ALONG THE EDGE OF THE LT PLATE PN 36-430056-6. AFTER CLEANING SOME OF THE PRIMER OFF, THE PITTING WAS NOTICED ON THE ALUMINUM ITSELF. THIS COULD POSSIBLY BE FROM CORROSION. SINCE THE ORIGIN OF THE PITTING WAS NOT KNOWN A NEW PLATE IS BEING ORDERED FROM MFG. RECOMMEND INSPECTION OF ALL SPAR KIT PLATES BEFORE INSTALLATION. 1L72 3O3 O 3A16 E3SO 20041027000892004102700089EU 2004 10 27 PG92004F00013 120040929A6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19170PA2192 2637 T/R SPAR FOUND TO HAVE 5 INCH LONG SPANWISE SPAR CRACK, FOUND BY PILOT UPON TURN AROUND CHECK. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED ENTIRE T/R BLADE WITH SERVICEABLE UNIT. RETURN HELICOPTER TO SERVICE. 1G71 3U3 U H9EU E19EU 20041027001042004102700104NM 2004 10 27 2004UALA00952 120041016A5711 SPAR BOEING757 757222 1384956NM PWA 2037 PW2037 NE WING DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 DAMAGE FOUND AT WBL 265 WING FRONT SPAR AT THE DRY BAY ACCESS HOLE NUT PLATE ATTACHMENT. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS IN 3 HOLES AND INSTALLED NEW DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041027001072004102700107EA 2004 10 27 COMA0460587 120041022A3150601R5172813 WARN PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT STICKING A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01818CA 7408 FLIGHT 5539 AURAL WARNINGS CYCLING ON AND OFF. REPLACED AUDIO WARNING PANEL. 2L72 4F RTA21EA 20041027001122004102700112SO 2004 10 27 C2XA04SH528 120041022A322014524475003 BEARING CAP EMB 145 EMB145LR 3260212SO NLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING C-CHECK NOSE GEAR RIGHT BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-01. 2L72 4T RTT00011AT 20041027001142004102700114SO 2004 10 27 C2XA04SH525 120041022A321014571033005 BEARING CAP EMB 145 EMB145ER 3260211SO RT MLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK FOUND THE RIGHT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED BEARING CAP IAW 32-10-01. 2L72 4F RTT00011AT 20041027001152004102700115NM 2004 10 27 SWAA043067 120041022A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKED. REPAIRED RIB CHORD PER ER. 2L72 4F RTA16WE 20041027001262004102700126SO 2004 10 27 C2XA04CL107 120041013A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713949 145057 CREW REPORTED THE LAST THREE ROWS OF AISLE EMERGENCY LIGHTING INOPERATIVE. FOUND LOOSE CONNECTION ON THE LIGHTS AND RECONNECTED. ITEM REPEATED ON THE NEXT FLIGHT AND MAINTENANCE REPLACED THE NUMBER 6 EMERGENCY INVERTED. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041027001362004102700136SO 2004 10 27 C2XA04SH516 120041010A532014532636401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2718982 145223 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLE REPAIR IAW SRM 53-21-10. 2L72 4T RTT00011AT 20041027001442004102700144EU 2004 10 27 2004UALA00789 120040828A2424740120C CONTROL UNIT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 GENERATOR FAULTY A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29474UA 1475 NR 2 GENERATOR FAULT ECAM MESSAGE. *S/D* NR 2 GENERATOR CONTROL UNIT REPLACED. 2L72 4F4 FRTA28NM E40NE 20041027001472004102700147NM 2004 10 27 2004UALA00792 120040820A2120 SMOKE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE COCKPIT DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29668UA 30024 RETURNED TO FIELD DUE TO SMOKE IN COCKPIT. 2L72 4F4 FRTA1NM E24NE 20041027001542004102700154NM 2004 10 27 SWAA043096 120041024A3350100031 LIGHT BOEING737 7373G7 1384595NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 DURING SCHEDULED SERVICE CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20041027001562004102700156NM 2004 10 27 SWAA043106 120041025A5755654645262A PANEL BOEING737 7373H4 1384600NM LT WING SPOILER CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED D-CHECK, FOUND LT WING NR 4 SPOILER PANEL OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2L72 4F RTA16WE 20041027001602004102700160NM 2004 10 27 SWAA043083 120041023A575465C26686 SKIN BOEING737 7373H4 1384600NM NR 1 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED C3 CHECK, FOUND LT WING NR 1 L/E SLAT SKIN CRACKED. REPAIRED L/E SLAT SKIN PER EA. 2L72 4F RTA16WE 20041027001612004102700161NM 2004 10 27 SWAA043084 120041023A3350612825 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED RON, FOUND BULL NOSE EMERGENCY EXIT LIGHTS AT ROWS 1 ABC AND 5 ABC INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041027001662004102700166NM 2004 10 27 CALA0400681 120041021A53306518420 SKIN BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716607 27320 INSPECTION FOUND A .5 INCH CRACK IN PILOT'S FORWARD WINDOW POST SKIN AT NR 1 WINDSHIELD UPPER O/B CORNER, STA 196.5, S6L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-10-01, FIGURE 210. 2L72 4F RTA16WE 20041027001702004102700170NM 2004 10 27 SWAA043085 120041024A2120215201 FAN BOEING737 7372H4 138448CNM E&E BAY FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29092SW 22964 DECLARED EMERGENCY, STRONG ELECTRICAL ODOR IN THE CABIN FOLLOWED BY THE GASPER FAN C/B OPENING. AFTER C/B OPENED THE ODOR LESSENED. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F A16WE 20041027001712004102700171NM 2004 10 27 SWAA043097 120041024A33506574550 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29414WN 29820 DURING SCHEDULED MV2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT EVAC SLIDE LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20041028000102004102800010NM 2004 10 28 SB04136 120040929A36101074922 SHUTOFF VALVE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT ENGINE FAULTY A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19524AU4149741497 23859 ENROUTE, AIRCRAFT EXPERIENCED A PNEUMATIC DUCT PRESSURE SPLIT OF 46 PSI RT AND 6 PSI LT. WHEN LT BLEED IS TURNED OFF, LT PRESSURE EQUALS RT AT APPROXIMATELY 36 PSI. ALTITUDE WARNING HORN SOUNDED AS CABIN GRADUALLY ASCENDED THROUGH 10,000 FEET. FLIGHT DESCENDED TO 10,000 FEET TO REGAIN CABIN PRESSURE. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE PRSOV MM 36-11-16. OPERATIONAL CHECK GOOD AT ALL POWER SETTINGS. PRESSURIZED AIRCRAFT TO 6 PSI AND MAINTAINED FOR 15 MINUTES. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA16WE E21EU 20041028000192004102800019EU 2004 10 28 04FDEA02365 120040805A783032142368 VALVE AIRBUS310 A310 EU PWA JT9 JT9D* NE THRUST REVERSER INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25447FE 251 PDIS 447, 78-30 0007040 05AUG04 CAE OPEN ON T/O AT 43 PERCENT N1,GOT REV UNLOCK LIGHT. MEL 05AUG04 05:40 CAE R ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15AUG04 MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2)1. THRUST REVERSER, INOPERATIVE. THRUST REVERSER IS DEACTIVATED R&R MASTER ACTUATOR - NO HELP R & R RT FEEDBACK MECHANISM, PRESSER REG. VALVE FACT TUL 10 AUG 04 2L72 4F4 FRTA35EU E20EA 20041028000262004102800026EA 2004 10 28 ASOA04465 120040629A5347601R310329 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 DURING A (C) CHECK, THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS559 + 32 TO FS 559 + 80 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT SEAT TRACK FORWARD OF THE LAVATORY AT FS 559 +80. 2L72 4F4 FRTA21EA E15NE 20041028000292004102800029NM 2004 10 28 UIEA2004118 120041006A5330 SKIN BOEING747 74747UF 1384949NM DENTED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15498MC 29259 DENT FOUND IN THE FUSELAGE SKIN RT SIDE AT STATION 2596. ACCOMPLISHED DENT REPAIR ON FUSELAGE SKIN RT SIDE STATION 2596 STRINGER 42 AREA IAW SRM 53-00-01 FIG 215 DETAIL I. (M) 2L74 4F RT1384945 20041028000362004102800036EA 2004 10 28 ASOA04479 120040701A3320 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LAVATORY ODOR A ASOAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27925EV 7831 DURING CRUISE, THE CREW NOTICED A HOT PLASTIC TYPE SMELL FROM THE LAVATORY AREA. UPON INVESTIGATION THE CREW DETERMINED THE LAVATORY OCCUPIED LIGHT WOULD NOT EXTINGUISH WHICH WAS CAUSING THE SMELL. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LAVATORY LIGHT WITH THE SWITCH IN THE ON AND OFF POSITIONS. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041028000382004102800038EA 2004 10 28 ASOA04481 120040702A361020035008067 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BLEED SYSTEM INTERMITTENT A ASOAO OTHER J WARNING INDICATION DEDESCENT 1 SO27903EV6225 7621 DURING DESCENT, THE CREW RECEIVED A 14 TH STAGE DUCT MESSAGE. THE QRH WAS COMPLIED WITH AND THE THRUST LEVER WAS REDUCED TO IDLE AT WHICH TIME THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT BLEED LEAK CONTROL UNIT. ENGINE RUNS AND OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041028000392004102800039EA 2004 10 28 ASOA04468 120040629A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CLIMATE CONTROL DIRTY A ASOAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27884AS 7513 FOLLOWING CLIMB OUT, UPON LEVELING OFF AT APPROX 31,000 FEET, CREW BEGAN NOTICING A SMELL, JET A FUMES COMING THROUGH THE VENTS IN THE COCKPIT ONLY. AFTER DESCENDING TO 24,000 FEET, CREW ATTEMPTED TO ISOLATE THE SMELL BY SHUTTING DOWN THE LT PACK BUT THE SMELL PERSISTED. THE AC DIVERTED. CREW DID NOT DECLARE AN EMERGENCY BUT ALERTED FIRE AND RESCUE AS A PRECAUTION. AC LANDED SAFELY. MAINT REMOVED AND REPLACED LT AND RT COALESCER BAGS AND RAN BOTH ENGINES AT ALL POWER SETTINGS FOR 1.5 HOURS IN ADDITION TO USING AUX POWER UNIT BLEEDS. NO FUEL SMELLS OCCURRED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041029000012004102900001SW 2004 10 29 MV5R055NA 120040625A5521 RIB MOONEYM20 M20C 5870208SW LYC O360 O360* 41514EA ELEVATOR CRACKED B MV5RO OTHER O OTHER NRNOT REPORTED 1 GL116034Q5288 3237 REMOVED LT ELEVATOR FOR CRACKED OB RIB PN 430004 AND DAMAGED SKIN. SENT FOR RESKINED THE ELEVATOR WITH OUT CHANGING THE RIB. RETURNED THE ELEVATOR TO GET THE RIB CHANGED AND THEY INSTALLED .2500 INCH HYLOCK FASTENERS IN THE BALANCE WEIGHT INSTEAD OF .1875 IRON RIVETS PN 430026999. WITH THE HYLOCK COLLARS STICKING OUT, THE BALANCE OF THE ELEVATOR WOULD CHANGE IF ICE BUILD UP. (GL11200406179) 1L71 3O3 O 2A3 E286 20041029000032004102900003NM 2004 10 29 CALA040067A 120041008A5313BAC1498156 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716310 23361 STRINGER 26 RT IS CORRODED AT STA 1006-1016. INSTALLED NEW STRINGER PER SRM 51-10-02. 2L72 4F RTA16WE 20041029000062004102900006EA 2004 10 29 HUN2004FAAA 220040917A7414M3513 ROTOR SLICK PIPER PA44 PA44180 7104402SO LYC O360 LO360A1G6 41514EA HARTZLHCC2Y HCC2YR2 GL ANTI-DRIVE END SHEARED B HUNRO OTHER O OTHER NRNOT REPORTED 1 NM015331Y 02071564 4496163 L75871A AU11204B COMPLETE FAILURE OF THE RT MAGNETO ON THE RT ENGINE. THIS COMPLETE FAILURE OCCURRED TWICE WITH TWO MAGNETOS. THE FIRST MAGNETO (SN 02071564) FAILED WITH A TOTAL TIME OF 529.1. THE SECOND MAGNETO (SN 04041941) FAILED WITH A TOTOAL TIME OF 166.6. BOTH FAILURES WERE THE RESULT OF THE ANTI-DRIVE END OF THE ROTOR, SHEARING OFF BELOW THE ROTOR GEAR(M3827) AT THE BASE OF THE CAM SLOT. 1L72 3O3 O A19S0 1E10 5 CP920 20041029000072004102900007 2004 10 29 237TR0006S 420040705A2230 TRANSMITTER BOEING737 737228 13844AGNM THROTTLE OUT OF ADJUST A PIDAO OTHER O OTHER TOTAKEOFF 1 SO05237TR 23007 AUTO THROTTLE SHUTS OFF ON TAKE-OFF. ADJUSTED THROTTLE POSITION TRANSMITTERS PER MM 22-31-81. 2L72 4F RTA16WE 20041029000082004102900008SO 2004 10 29 C2XA02CL09A 120040920A3230 LANDING GEAR EMB 145 EMB145LR 3260212SO MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716561 145610 STL FLIGHT 2162, CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM, AND CYCLED LANDING GEAR SEVERAL TIMES. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE 2L72 4T RTT00011AT 20041029000092004102900009EA 2004 10 29 HUN2004FBBB 220040917A7414M3513 ROTOR SLICK PIPER PA44 PA44180 7104402SO LYC O360 IO360A1A 41514EA HARTZLHCC2Y HCC2YR2 GL ANTI-DRIVE END FAILED B HUNRO OTHER O OTHER NRNOT REPORTED 1 NM015331Y166 04041941 4496163 L75871A AU11204B COMPLETE FAILURE OF THE RT MAGNETO ON THE RT ENGINE. THIS COMPLETE FAILURE OCCURRED TWICE WITH TWO MAGNETOS. THE FIRST MAGNETO (SN 02071564) FAILED WITH A TOTOAL TIME OF 529.1. THE SECOND MAGNETO (SN 04041941) FAILED WITH A TOTAL TIME OF 166.6. BOTH FAILURES WERE THE RESULT OF THE ANTI-DRIVE END OF THE ROTOR, SHEARING OFF BELOW THE ROTOR GEAR (M3827) AT THE BASE OF THE CAM SLOT. 1L72 3O3 O A19S0 1E10 5 CP920 20041029000102004102900010NM 2004 10 29 249TR0031A 120040710A33501000679 LIGHT BOEING737 7372K5 138448XNM CABIN INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD. 2L72 4F RTA16WE 20041029000242004102900024NM 2004 10 29 2004UALA00920 120040911A5300 BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE MLG WW UNKNOWN A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 LT AND RT WHEEL WELL CANTED BEAMS. INSTALLED DOUBLER TO MLG CANTED BEAMS. 2L72 4F4 FRTA2NM E17NE 20041029000262004102900026NM 2004 10 29 DL733040960 120041011A5330654577616 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27304WA 23345 FUSELAGE SKIN DENTED AT STA 827 BETWEEN STR 26R - 28R. REPAIRED IAW ERA 093986-14. 2L72 4F RTA16WE 20041029000282004102900028NM 2004 10 29 DL73G040963 120041013A2432401767 BATTERY BOEING737 73735B 13844BMNM E/E BAY OVERHEATED A DALAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27224DA 24269 CREW REPORTED SMELL IN COCKPIT. FOUND BATTERY OVERHEATED. REPLACED BATTERY AND CHARGER PER AMM. OPS CHECKS NORMAL. AIRED OUT COCKPIT. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20041029000322004102900032EU 2004 10 29 2004UALA00896 120040925A3350 LAMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29498UA 1865 RED EMERGENCY ESCAPE PATH LIGHT ON BULKHEAD FORWARD OF SEAT ROW 1ABC INOPERATIVE. REPLACED LAMPS. 2L72 4F4 FRTA28NM E40NE 20041029000352004102900035NM 2004 10 29 2004UALA00928 120041011A5340 STRINGER CLIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29902UA 25002 TWO EA STRINGER CLIPS ARE CRACKED AT STA 460 STR 6 LT AND STA 420 STR 4 LT. MAJOR REPAIR ACCOMPLISHED. REPLACED BOTH STRINGER CLIPS. 2L72 4F4 FRTA16WE E2GL 20041029000372004102900037NM 2004 10 29 2004UALA00929 120041011A5230 BEAM BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 TWO CRACKS WERE DISCOVERED AT THE FWD END OF THE LWR BEAM OF THE AFT CARGO DOOR. ONE CRACK AT A FASTENER HOLE IN THE VERTICAL FLANGE OF THE OUTBOARD TEE CHORD AND THE OTHER AT THE FASTENER HOLE IN THE WEB. THE TEE CHORD CRACK IS 0.375 INCH LONG AND WEB CRACK EXTENDS FROM THE HOLE TO THE EDGE OF THE WEB. CRACKING AT THIS LOCATION IS CAUSED BY FATIGUE. MAJOR REPAIR ACCOMPLISHED. 2L72 4F4 FRTA16WE E2GL 20041029000422004102900042 2004 10 29 SWAA043110 420041026A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041029000432004102900043NM 2004 10 29 SWAA043111 120041026A5531 SPAR BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STAB PER ER. 2L72 4F RTA16WE 20041029000452004102900045NM 2004 10 29 SWAA043113 120041026A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND 4 EACH CRACKS ON FRAMES AT BS 787, STRINGER 8R, BS 827, BS 867, BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041101000022004110100002SO 2004 11 1 LR7A04105 120041001A5230 CAP LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5211 FOUND CARGO RAMP RT FS 793 CHINE CAP CRACKED AT WL 168, RBL 57. REPAIRED PER SRM SMP 583 52-60-03. 2H74 4T A1SO 20041101000032004110100003SO 2004 11 1 LR7A04106 120041001A531238848215 CAP LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LT MLG FS 577 BEAM OUTER CAP CRACKED AT WL 228, LBL 67. REPACED CAP IAW DWG 388482 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041101000042004110100004SO 2004 11 1 LR7A04107 120041001A5310 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LT MLG FS 497 UPPER BOW BEAM CRACKED AT WL 200, LBL 63. REPAIRED IAW SRM SMP 583 53-40-14. 2H74 4T A1SO 20041101000052004110100005NM 2004 11 1 SWAA043126 120041027A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, STRINGER 13L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041101000072004110100007NM 2004 11 1 2004UALA00966 120040929A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 CABIN CREASE BEAM SHEAR WEB AT RBL 70.5 FROM STA 960 TO 984 CORRODED. FABRICATED NEW SHEAR WEB. 2L72 4F4 FRTA2NM E17NE 20041101000082004110100008NM 2004 11 1 2004UALA00921 120041008A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSLEAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29655UA 25393 FLOORBEAM STA 246 STIFFENER AT RBL 15 IS CRACKED. CRACKS CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED AND INSTALLED NEW BRACKET. 2L72 4F4 FRTA1NM E24NE 20041101000092004110100009NM 2004 11 1 2004UALA00930 120041011A3350 LIGHT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29905UA 25005 AFT EEL STRIP IN FRONT OF AFT GALLEY INOP. REPLACED GALLEY EEL SEGMENT. 2L72 4F4 FRTA16WE E2GL 20041101000102004110100010EU 2004 11 1 2004UALA00940 120041013A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29428UA 523 EMERGENCY LIGHTS TEST FAIL, FAULTS EXT LOADS FWD LT. AMPERAGE READING ON RECEIPT 0.00. CHANGED LIGHTS. AMPERAGE READING WAS .870 (NORMAL) AFTER REPACK. 2L72 4F4 FRTA28NM E40NE 20041101000112004110100011NM 2004 11 1 2004UALA00905 120040911A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT FRAME DENTED STA 1540 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041025001452004102500145SO 2004 10 25 SWIA200413980 120041016A275012064207615CON SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM075873398 98 120197 RECEIVED FLAP CONTROL FAULT WHEN SELECTING FLAPS 15. REPLACED FLAP HANDLE. OPERATIONAL CHECK GOOD REFERENCE 27-00-00. 2L72 4T RTA31SO 20041025001462004102500146EA 2004 10 25 SWIA200413981 120041017A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07938SW 7741 LEFT SIDE WINDOW SHATTERED. REMOVED AND REPLACED LEFT SIDE WINDOW REF MM 56-12-01. P/N OFF 601R33033-11, S/N OFF 02201H1672. 2L72 4F RTA21EA 20041026000032004102600003 2004 10 26 MALA040539 420040824A22104068300904 COMPUTER BAC 146 AVRO146RJ85A1500097EU E/E BAY MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15523XJ E2348 THRU 12,000 FT A/P KICKED OFF WITH ELEVATOR TRIM FAULT AND WINDSHEAR INOPERATIVE LIGHT CA SIDE FD ALSO FAILED. PFD AND ND ALSO FLICKERED AND CAME BACK WITH AN ALT FLG. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED DFGC, OP CHECKS GOOD. P/N ON/OFF 4068300-904, S/N ON 98040314, S/N OFF 96080249, ALL CHECKS GOOD IAW RJ MM. 2H74 4F RTA49EU 20041026000092004102600009EU 2004 10 26 AWXA200400935 120040827A3350321430 BATTERY AIRBUS320 A320231 3930325EU ZONE 241 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 CMH - EEL - DURING 4-DAY CHECK THE LEFT OVERWING EMERGENCY LIGHT BATTERY FAULTED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LEFT OVERWING EMERGENCY POWER SUPPLY UNIT 11WL, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041026000282004102600028NE 2004 10 26 SWIA200413812 220040908A7320 EEC EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM07227SW 120304 AT 10,000 FT THE LT ENGINE LOST POWER AND TORQUE DROPPED TO 20 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUT-DOWN. REPLACED LT ENGINE EEC AND TORQUE CONDITIONER ENGINE HARNESS. ENGINE RUN PER MM 71-00-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041026000312004102600031NM 2004 10 26 UPS04242964 120040730A5754 ACCESS PANEL BOEING727 72722C 138400FNM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01945UP 19094 INSPECTION TYPE: C, NR 7 SLAT INNER SKIN ACCESS PANEL, EXISTING REPAIR DOUBLER IS CRACKED. NR 7 SLAT INNER SKIN ACCESS PANEL REMOVED FOR ACCESS IAW SRM 51-30-02 & CRACKED DOUBLER REPLACED IAW SRM 51-30-02. 2L73 4F A3WE 20041026000362004102600036EU 2004 10 26 ASOA04760 120040910A5320 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11631AS 362 DURING A C-CHECK, LT ZEE FLOOR SUPPORT BETWEEN FRAME 39 AND 40 AND THE RT ZEE FLOOR SUPPORT BETWEEN FRAME 39 AND 41 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ZEE FLOOR SUPPORT BETWEEN FRAME 39 TO 40 AND THE RIGHT ZEE FLOOR SUPPORT BETWEEN FRAME 39/41 IAW SRM 51-25-01. (M) 2H72 4T RT 20041026000402004102600040SO 2004 10 26 SIMA200427302 120040928A2120 ODOR EMB 135 EMB135KL 3260302SO NR 1 A/C PACK DETECTED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21847AE 145707 CREW REPORTED A PACK 1 OVERLOAD MESSAGE INFLIGHT WITH A STRONG ODOR THROUGH REMAINDER OF FLT. PERFORMED GROUND RUNS AND OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEMS WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026000422004102600042SO 2004 10 26 SIMA20047205 120040926A27503631001007 FCU EMB 135 EMB135LR 3260305SO TE FLAPS INOPERATIVE A SIMAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW21706RG 145194 ON TAKEOFF ROLL AT 25KIAS, RECEIVED SPOILERS DEPLOYED MESSAGE. TAKEOFF WAS ABORTED. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026000442004102600044 2004 10 26 GTIA040774 420040909A2565 CABLE DOUG DC9 DC981 3022081WP L2 DOOR GIRT BARMISINSTALLED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23810NK 48015 FLL - FOUND L2 DOOR EMERGENCY EXIT SLIDE GIRT BAR CABLE ROUTED IMPROPELY. REROUTED CABLE. (M) 2L72 4F A6WE 20041026000462004102600046NE 2004 10 26 GTIA040771 220040903A7230 BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 1 ENGINE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 696426 FOUND NR 1 ENGINE HAS 5 LPT BLADES LOOSE AT 5 LBS. REMOVED AND REPLACED NR 1 ENGINE. (M) 2L72 4F4 FRTA6WE E9NE 20041026000522004102600052SO 2004 10 26 SIMA200426701 120040920A2741 CONNECTOR EMB 135 EMB135KL 3260302SO PITCH TRIM DAMAGED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21804AE 145487 CREW REPORTED A PITCH TRIM CONFIG WARNING ON EICAS DURING TAKEOFF. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED PIN C ON CONNECTOR J0886. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20041026000582004102600058EA 2004 10 26 A6WA200440146 120041010A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31436AW 7734 FOUND RIGHT 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE AT FS 625, RIGHT SIDE, IAW CRJ 200 SRM 51-92-21. (M) 2L72 4F RTA21EA 20041026000742004102600074EA 2004 10 26 A6WA200440144 120041003A30007858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AIR DATA HEAT MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31409AW 7447 INTERMITTENT RIGHT STATIC HEAT, TAT PROBE HEAT, RT AOA HEAT, RT PITOT HEAT MESSAGE INFLIGHT ONLY. REMOVED AND REPLACED AIR DATA HEAT CONTROLLER IAW AMM 30-31-15. OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20041026000842004102600084WP 2004 10 26 GTIA040765 120040903A7120K22199SA31 ISOLATOR DOUG DC9 DC983 3022083WP NR 1 ENGINE OUT OF LIMITS A GTIAK NONE O OTHER ININSP/MAINT 1 GL23802NK 53168 DTW - FOUND NR 1 UPPER ISOLATOR REQUIRES CHANGE, OUT OF LIMITS. REMOVED AND REPLACED NR 1 UPPER FORWARD VIBRATION ISOLATOR. (M) 2L72 4F RTA6WE 20041026000882004102600088 2004 10 26 GTIA040767 420040905A2565 HANDLE DOUG DC9 DC983 3022083WP L1 SLIDE DISCONNECTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 L1 SLIDE INFLATION CABLE NOT CONNECTED TO MANUAL INFLATION HANDLE. CONNECTED L1 SLIDE INFLATION CABLE TO MANUAL INFLATION HANDLE. (M) 2L72 4F RTA6WE 20041026000892004102600089WP 2004 10 26 GTIA040766 120040822A5210 HANDLE DOUG DC9 DC982 3022082WP L1 DOOR LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 FLL - FOUND L1 DOOR HANDLE LOOSE. TIGHTENED L1 DOOR HANDLE. (M) 2L72 4F A6WE 20041026001002004102600100GL 2004 10 26 SIMA200427303 220040927A7200 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 2 SMOKE A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21838AE 145651 CREW REPORTED LAV SMOKE WARNING MESSAGE AFTER TAKEOFF. THIS IS THE SECOND OCCURENCE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW AE W/C 72-000-00 OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTT00011ATTE6CH 20041026001232004102600123EA 2004 10 26 SWIA200413971 120041005A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW VERTICAL BEAM CRACKED AT FS 559, RBL 9.0 IB LOWER FASTENER. (ITEM FOUND AT C-CHECK INSPECTION). REPAIRED IAW CRJ REO 601R-53-41-057 REV NC 13. 2L72 4F4 FRTA21EA E15NE 20041026001292004102600129NM 2004 10 26 UPS04443353 120040921A5312 BULKHEAD BOEING747 747121 1384871NM PWA JT9 JT9D3 52050NE RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C, RT WLG W/W FWD BULKHEAD IB MID AREA CORROSION REVEALED AT STA 1241 RBL 2-6. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.082 INCH X 1 INCH X 5 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS. BULKHEAD REPAIRED REFER SRM 57-10-06 FIG 3, CIC APPLIED IAW M-5100-2780-E. 2L74 4F4 F A20WE E20EA 20041026001372004102600137EU 2004 10 26 CX7A194J0454 120041020A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE E/E BAY FALSE ACTIVATIONA CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03305CE5256 340B202 HAD TO REJECT TAKEOFF DUE TO AVIONICS SMOKE LIGHT, NO SMOKE SMELL OR FIRE. REPLACED AVIONICS SMOKE DETECTOR. 2L72 4T4 TRTA52EU E8NE 20041026001402004102600140EU 2004 10 26 YENA200450 120041020A2121EVT3454H FAN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN SEIZED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15523JB12904 1506 DURING CRUISE, LOUD VIBRATION AND A SLIGHT BURNING ODOR APPEARED. TURNED THE BLOWER SWITCH TO OVERRIDE AND ALL PROBLEMS IMMEDIATELY DISAPPEARED. PERFORMED TSM TASK 24-00-00-810-823 AND NO DEFECTS NOTED. AIRCRAFT RELEASED IAW MEL 21-26-01. LATER DISCOVERED BLOWER FAN SEIZED. REPLACED BLOWER FAN IAW AMM 21-26-51-04, FAN OPERATION CHECKED GOOD. 2L72 4F4 FRTA28NM E40NE 20041026001412004102600141NM 2004 10 26 QXEA200400723 120041019A272082410608005 TRIM PANEL BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 200 STUCK A QXEAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM09410QX6877 4053 FLIGHT 2350 - ON FINAL, APPROXIMATELY 6 MILES OUT, THE CREW ATTEMPTED TO TRIM THE AC RUDDER. WHEN THE RUDDER TRIM SWITCH WAS RELEASED, THE RUDDER CONTINUED TO TRIM TO FULL LT RUDDER. THE AIRCRAFT WAS NEVER UNCONTROLLABLE, AND THE CREW WAS ABLE TO CENTER THE RUDDER TRIM AND THE LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM PANEL DUE TO A STUCK SWITCH. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20041026001492004102600149SO 2004 10 26 CHQA000567 120041016A3350 LAMP EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGNECY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11375SK 145569 LT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED INOPERATIVE LIGHT. OPS CHECK GOOD IAW MM 33-51-00. 2L72 4F4 FRTT00011ATTE6CH 20041026001522004102600152NM 2004 10 26 2004UALA00919 120040909A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 SKIN, BS 580 S-15L TO S-18L IS DAMAGED. ACCOMPLISHED PARTIAL SKIN REPLACEMENT WITH SKIN DOUBLER SPLICES AND TRIPLER SPLICES. ACCOMPLISHED STRINGER REPAIR USING STRINGER SPLICES. 2L72 4F4 FRTA2NM E17NE 20041026001542004102600154NM 2004 10 26 04FDEA02966 120041022A5533 STRUCTURE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR APPROX ZFR 564 RT EXTRUSION. EXTERIOR SURFACE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EA 1-5530-81578. 2L73 4F4 FRTA22WE E31N3 20041026001562004102600156NE 2004 10 26 EM01018 220041014A73204120T00P31 FADEC EMB ERJ170ERJ170100 EU GE CF34 CF34* NE ZONE 100 FAULTY A USAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA19803MD1322 17000015 193133 CREW RECEIVED (ENGINE NR1 NO DISPATCH MESSAGE). THE FLIGHT RETURNED TO THE GATE.MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FADEC. 2L74 4F4 FRTA56NM E15NE 20041026001732004102600173CE 2004 10 26 DXTA200400427 120041015A3240 BRAKE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE MLG MALFUNCTIONED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07399QS 5600510 RT BRAKE PEDAL GOES TO FLOOR ON TAXI OUT FOLLOWED BY NORMAL BRAKE ACTION FOLLOWED BY SOFT RT PEDAL ON BOTH CAPT/FO SIDES FOR SEVERAL CYCLES. NO FLUID LEAKS FOUND. FLUID LEVEL NORMAL. ACCUMULATOR NORMAL. T/S BRAKE SYSTEM. PERFORMED ON-GROUND MODE TEST AND ANTISKID SELF TEST IAW MM 32-42-00 PARAGRAPH (2). PRESSURE CHECKED AT 800 PSI. TAXIED AIRCRAFT AND TESTED BRAKE SYSTEM WITH ANTI-SKID ON AND OFF. FOUND TO BE SERVICEABLE AT THIS TIME. 2L72 4F4 FRTA22CE E25EA 20041026001822004102600182EU 2004 10 26 MALA040617 120041016A3230643500300 HANDLE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE MLG SELECTOR INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15514XJ E2330 VIBRATION IN CLIMBOUT AND LT GEAR WARNING LT AND GEAR HANDLE LIGHT TOGETHER INTERMITTENTLY. AIR RETURN. FOR VIBRATION AT 270 KNOTS WITH LT MLG UNSAFE INDICATION WITH GEAR HANDLE LIGHT. MAINTENANCE DUE TO VIBRATION, INSPECTED AND ADJUSTED SPOILER SEALS ON BOTH WINGS. DURING GEAR SWING, GEAR HANDLE LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED LANDING GEAR HANDLE OPS CHECKED GOOD. OK FOR SERVICE. PN/ ON/OFF 6435-003-00 S/N ON 063-98 S/N OFF 100-99 2H74 4F4 FRTA49EU E6NE 20041026001972004102600197EU 2004 10 26 04FDEA02872 120041005A3260 PROXIMITY SENSOR AIRBUS310 A310 EU GE CF6 CF680A3 30025NE MLG MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25415FE 349 GEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAULTS. PERFORMED SYS TEST WITH THE FOLLOWING SENSOR FAULTS, 03 (LT BOGIE SYS 1), 04 (RT BOGIE SYS 1), 05 (NOSE CENTERED SYS 1), 06 (LT MLG SHOCK SYS 1), 07 (RT MLG SHOCK SYS 1), 10 (LT BEAM SYS 2), 11 (RT BEAM SYS 2), 12 (NOSE CENTERED SYS 2), 13 (LT MLG SHOCK SYS 2), 14 (RT MLG SHOCK SYS 2). ONLY THING IN COMMON IS PROX BOX. SUSPECT BAD PART FROM STOCK REF WRI 32-60/7307. REMOVED AND REPLACED PROX DETECT CONTROL UNIT 54GB. PERFORMED SYSTEM TEST OF PROX BOX PER SAME. ALL PREVIOUS SENSOR FAULTS HAVE NOW CLEARED AND SYSTEM TEST GOOD. OK FOR CONTINUED SERVICE. 2L72 4F4 FRTA35EU E13NE 20041026002002004102600200SO 2004 10 26 CHQA000569 120041018A3350 POWER SUPPLY EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11372SK 145538 MAIN DOOR EMERGENCY EXIT SIGN, COCKPIT STEP EXIT SIGN, EMERGENCY LIGHT AT ROW 3 CEILING, AND MAIN CABIN DOOR EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NR 1 IAW MM 33-50-04. OPS CHECK GOOD. 2L72 4F4 FRTT00011ATTE6CH 20041027000062004102700006WP 2004 10 27 04FDEA02982 120041022A5753ANB74341 FITTING DOUG MD10 MD1010F 3022112WP GE CF34 CF343B1 NE ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND ALL HOLES HAVE EVIDENCE OF PITTING. REMOVED CORROSION AND PITTING FROM LUG AND BORES. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM57-20-00 VOL.I PAGE 16. INSTALLED BUSHINGS ON NR N01175. BLENDED FLAT SPOTS IAW EA 8-5750-81495. SEE N/R N01174. 2L73 4F4 FRTA22WE E15NE 20041027000162004102700016NM 2004 10 27 UPS04243352 120041017A2612 CONTROL UNIT BOEING727 727185C 138406NNM RROYCETAY TAY65154 EU NR 3 ENG FIRE MALFUNCTIONED A IPXAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SO01940UP 19826 WHEN F/O TURNED OFF F/D ALTITUDE HOLD, RECEIVED AN INTERMITTENT FIRE WARNING. THE F/O TAPPED THE GLARE SHIELD AND THE FIRE WARNING LIGHT AND BELL CAME ON STEADY. ENGINE NR 3 WAS SHUTDOWN IAW PROCEDURES AND UNEVENTFUL. SIMULATED CREW ACTION BY TAPPING ON GLARE SHIELD-NO DEFECTS FOUND. CHECK RESISTANCE OF BOTH A AND B LOOPS-NO DEFECTS FOUND. RAN NR 3 ENG AND CHECKED DUCT LEAKS, NO DEFECTS FOUND. AS PRECAUTIONARY REMOVED AND REPLACED NR 3 ENG FIRE DETECTOR CONTROL UNIT. OPS CHECK GOOD. REF MM 26-11-21. 2L73 4F4 F A3WE E25NE 20041027000192004102700019NM 2004 10 27 UPS04543351 120041004A5330 SKIN BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01454UP 25475 INSPECTION TYPE-C, CORROSION FWD OF APU INLET BOX BS 1790 4 INCHES IB OF STR6R. REMOVED AND REPLACED STRAP AT APU INLET BOX IAW SRM 51-40-02. 2L72 4F4 FRTA2NM E12EU 20041027000252004102700025NM 2004 10 27 SB04147 120041021A335020131A BATTERY PACK BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19524AU 23859 FOUND EXTERIOR EMERGENCY LIGHTS OVER R1 AND L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. 2L72 4F4 FRTA16WE E21EU 20041027000332004102700033EU 2004 10 27 SA04093 120041002A335032145410 EPSU AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19732US13583 1203 THE AFT LT EMERGENCY POWER SUPPLY UNIT FAULTED DURING TEST. MAINTENANCE REPLACED THE AFT LT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F4 FRTA28NM E37NE 20041027000392004102700039NM 2004 10 27 04277426 120041003A2913 PUMP DORNERDO32 DO328300 NM PWA 306 PW306B NE HYDRAULIC SYSTEMDEFECTIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27426FJ AJ738 3190 HYDRAULIC B FAILURE, DIVERTED. MECHANIC REMOVED AND REPLACED SYSTEM B HYD PUMP. LEAK AND OPS CHECK GOOD. 2H72 4T4 FRTA55NM E35NE 20041027000422004102700042WP 2004 10 27 ABXA040350 120041011A531059101639 DOOR FRAME DOUG DC9 DC933F 302207AWP PWA JT8 JT8D11 52044NE FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 CRACKED AT SHEAR PIN RECEPTICLE ON P-DOME, 11:00 POSITION. REPAIRED IAW REA D953-50852MR AND SRD 5934886-510. 2L72 4F4 F A6WE E2EA 20041027000502004102700050NM 2004 10 27 2004UALA00881 120040917A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT FRAME DENTED AT BS 1460 AND STR 26L, ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER ANGLE. 2L72 4F4 FRTA2NM E17NE 20041027000542004102700054NM 2004 10 27 2004UALA00885 120040913A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT MAIN FRAME AT BS 1420, STR 26L IS DENTED. INSTALLED REINFORCING ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041027000562004102700056NM 2004 10 27 2004UALA00887 120040909A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT STA 1600 BETWEEN STR 28R AND 29R, SHEAR TIE IS CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20041027000582004102700058NM 2004 10 27 2004UALA00889 120040929A2410 PLANETARY GEAR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE WORN A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29339UA 24243 DIVERTED UNDER AMBER ALERT WITH NR 2 ENGINE MOVED TO IDLE DUE TO NR 2 GENERATOR PROBLEM. REPLACED CSD AND CSD OIL COOLER. SHOP FOUND A WORN PLANETARY GEAR USED FOR INTERNAL CSD LUBRICATION. 2L72 4F4 FRTA16WE E2GL 20041027000602004102700060NE 2004 10 27 NACA20040045 220041006A8530356993 CYLINDER HEAD DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4ENGINE CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL0343872501 501 533294 P31426 DISCREPANCY: NR 4 ENGINE SHUT DOWN DUE TO LOW COMPRESSION INDICATION ON NR 2 CYLINDER. FOUND NR 2 CYLINDER WITH CRACKED HEAD. REPLACED NR 2 CYLINDER. CHECKED GOOD. 2L74 4R4 R A781 5E8 20041027000642004102700064SO 2004 10 27 FYO2004F00000 120040909A6100 PROPELLER PIPER PA32 PA32300 7103212SO LYC O540 IO540* 41532EA HARTZLHCC2Y HCC2YR1 GL MALFUNCTIONED E FYOAO OTHER O OTHER NRNOT REPORTED 1 AL0531589 327840135 CH3352B PILOT STATED THAT DURING CRUISE FLIGHT, PROPELLER WENT TO FINE PITCH, AND OPERATION OF GOVERNOR CONTROLS HAD NO EFFECT. UPON GROUND RUN UP IT WAS FOUND THAT PROP WOULD NOT CYCLE. REMOVED FROM SERVICE. UNKNOWN CAUSE FOR FAILURE AT THIS TIME. (AL05200401344) 1L71 3O3 O A3SO 1E4 5 CP920 20041027000672004102700067CE 2004 10 27 GM82004F00003 120040922A2434991059111RX ALTERNATOR CESSNA172 172R 2072401CE LYC IO360 IO360L2A EA ENGINE FAILED D GM8SO OTHER O OTHER NRNOT REPORTED 1 SW0577LU 453 17281154 ALTRNATOR, LOW FIELD RESISTANCE. 1H71 3O3 ONT3A12 1E10 20041027000752004102700075SO 2004 10 27 FMA2004F00000 220041004A7414M3081 CONTACTOR SLICK CESSNA207 T207 2073612CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL MAGNETO DEFECTIVE E FMAAO OTHER O OTHER NRNOT REPORTED 1 AL01207DG696 00061446 20700070 280244R EC1716B PILOT REPORTED MISFIRE DURING MAG CHECK. TROUBLESHOOTING REVEALED RIVETING OF GROUND SIDE OF CONTACT TO MOUNTING BASE HAD FAILED ALLOWING ELECTRICAL CONTACT TO RATTLE IN BASE. 1H71 3O3 O A16CE E5CE 5 CP25EA 20041027000812004102700081EU 2004 10 27 PG92004F00014 120040927A641035JA12004008 BLADE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR CRACKED E PG9AO OTHER O OTHER NRNOT REPORTED 1 WP19890AK1358 2138 T/R SPAR FOUND CRACKED DURING COMPLIANCE OF SB 05.11R5. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED T/R BLADE WITH NEW UNIT. RETURNED HELICOPTER TO SERVICE. 1G71 3U3 UNCH9EU E19EU 20041027000942004102700094CE 2004 10 27 CVU2004F00000 120040923A3710442CW PUMP BEECH 80 65B80 1152812CE LYC O720 IO720A1B 41546EA HARTZLHCA3V HCA3VK2 GL LT ENGINE VACUUMFAILED E CVUAO OTHER O OTHER NRNOT REPORTED 1 WP1344MA 979 LD412 VACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR DAY) 1L72 3O3 O 3A20 1E15 5 CP6EA 20041027001092004102700109EA 2004 10 27 COMA0470076 120041023A3230533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG UNRELIABLE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01317CA2119 10055 FLIGHT 5077 GEAR DISAGREE WARNING. REPLACED THE SELECTOR VALVE. 2L72 4F RTA21EA 20041027001252004102700125 2004 10 27 COMA0460576 420041020A34103995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA WINDSHEAR MALFUNCTIONED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01920CA138598825 7022 FLIGHT 5816 WINDSHEAR FAIL STATUS MESSAGE. REPLACED THE STALL PROTECTION COMPUTER. 2L72 4F RTA21EA 20041027001432004102700143NM 2004 10 27 2004UALA00788 120040827A5754114N3002 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT DEBONDED A UALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP29526UA 24994 RIGHT INBOARD LEADING EDGE WEDGE DISBONDED FROM SLAT. *S/D* A SECTION OF THE NR 6 SLAT TRAILING EDGE WEDGE SEPARATED FROM THE SLAT ASSEMBLY. DURING DISASSEMBLE OF THE SLAT WEDGE FOR REPAIR, COMPONENT SHOP FOUND EVIDENCE OF CORROSION ON THE ALUMINUM HONEYCOMB CORE AND SKIN WHICH ALSO MIGHT BE THE CAUSE OF THE DISBOND OF THE SLAT WEDGE. REPLACED TRAILING EDGE WEDGE. 2L72 4F4 FRTA2NM E17NE 20041027001582004102700158NM 2004 10 27 SWAA043081 120041023A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29338SW 23960 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 23R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041027001642004102700164EA 2004 10 27 COMA0460557 120041004A2910AE7127631 LINE CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01986CA 7174 FLIGHT 5092 HYDRAULIC SYSTEM 1 LOW PRESSURE WARNING. REPLACED LEAKING LINE ASSY IN ROA. 2L72 4F RTA21EA 20041028000052004102800005WP 2004 10 28 ARWA20040904 120040929A32104771392501 PIN DOUG DC8 DC863F 302198FWP MLG DAMAGED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19441J 45988 DURING UP-LATCH CHECK THE GEAR NOT LATCHED, LIGHT ILLUMINATED AND PERFORMED ABNORMAL CHECKLIST, THEN BOTH GEAR NOT LATCHED AND DOOR NOT LATCHED REMAINED ILLUMINATED. REMOVED RT GEAR ASSY SENT TO AAR LANDING GEAR; REPAIRED STUD ASS PART NR 5759145508 ON RT GEAR ASSY S/N 539658. REMOVED LANDING GEAR, DUE TO ACTUATOR STUD LOOSE ON RT GEAR ASSY. REMOVED RT GEAR ASSY. IN ACCORDANCE WITH M/M 32-11-1. INSTALLED RT MAIN GEAR IN ACCORDANCE WITH M/M 32-11-1. PERFORMED GEAR ADJUSTMENT TEST IN ACCORDANCE WITH M/M 32-11-1. OPERATIONAL CHECK OK. 2L74 4F 4A25 20041028000072004102800007NE 2004 10 28 ARWA20040902 220040927A7532563883 BLEED VALVE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 4 ENGINE DEFECTIVE A ARWAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO19345JW 46042 DURING LINE UP FOR TAKE-OFF, NR 4 ENGINE FAIL TO ACCELERATE. FOUND DEFECTIVE SURGE BLEED VALVE. REMOVED AND REPLACED NR 4 SURGE BLEED VALVE IAW MM 75-30-3 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN-UP IAW MM 71-00 ALL PARAMETERS NORMAL. 2L74 4F4 F 4A25 1E8 20041028000082004102800008NE 2004 10 28 ARWA20040903 220040927A7200 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 VIBRATION A ARWAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SO19661AV5664496 45969 671023 NR 2 ENGINE VIBRATES AT 1.2 EPR ON THE GROUND AND IN FLIGHT. REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR TASK CARD DC-8 UN-003. OPERATIONAL CHECK SATISFACTORY. 2L74 4F4 F 4A25 1E8 20041028000122004102800012NM 2004 10 28 04FDEA02460 120040812A5320 ANGLE BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25246FE 22068 N00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICATED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7 2L73 4F4 FRTA3WE E2EA 20041028000312004102800031EA 2004 10 28 ASOA04473 120040630A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PASSENGER DOOR BROKEN A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27848AS 7338 7339 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN ON THE FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041028000332004102800033EA 2004 10 28 ASOA04470 120040629A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11885AS 7521 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625. (M) 2L72 4F RTA21EA 20041029000042004102900004WP 2004 10 29 TCA001AA 220041019A7200 ENGINE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110 01514WP HARTZLHCB3T HCB3T* GL LEAKING E E18AE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23396RY 23291 TC281 54312 BUA20791 ENGINE LOST OIL PRESSURE IN FLIGHT. ENGINE WAS SHUT DOWN 2L72 4T4 TRTA8SW E4WE 6 CP15EA 20041029000112004102900011NM 2004 10 29 2004UALA00904 120040911A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE STR 25L & 26L DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT FRAME STA 1480 IS DENTED BETWEEN STR 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041029000122004102900012NM 2004 10 29 2004UALA00910 120040920A5740 SUPPORT FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29648UA 25285 RIGHT WING INBOARD MAIN FLAP REAR SIDE LINKAGE SUPPORT FITTING CRACKED, INBOARD AND OUTBOARD SIDES. MAJOR REPAIR ACCOMPLISHED. REPAIRED & INSTALLED SUPPORT FITTING. 2L72 4F4 FRTA1NM E24NE 20041029000132004102900013NM 2004 10 29 2004UALA00911 120040930A5753 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29649UA 25286 RIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP HINGE WITH REPAIR ANGLES AND FILLER. 2L72 4F4 FRTA1NM E24NE 20041029000362004102900036NM 2004 10 29 2004UALA00965 120041018A5320 DOUBLER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 AFT RT GALLEY AREA, STA 1700 BETWEEN RBL 42 AND RBL 56, DOUBLER PLATE CORRODED, (FLOOR DOUBLER). CORROSION DAMAGE FOUND. AFT DECK PLATE REPAIRED USING DOUBLER AND TRIPLER. PIN BEAM WAS REPLACED, AND A REPAIR TO THE BS 1701 FLOOR BEAM WEB ACCOMPLISHED FOR ACCESS TO REMOVE THE PIN BEAM. 2L72 4F4 FRTA2NM E17NE 20041029000392004102900039NM 2004 10 29 2004UALA00793 120040831A2810382222 CAP AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE FUEL CELL WRONG PART A UALAA UNSCHED LANDING WK INADEQUATE Q C FLUID LOSS CRCRUISE 1 WP29823UA 952 FLIGHT DIVERTED DUE TO POSSIBLE FUEL LEAK. INCORRECT CAP ASSEMBLY INSTALLED. REPLACED CAP WITH CORRECT PART NUMBER. 2L72 4F4 FRTA28NM E40NE 20041029000412004102900041 2004 10 29 SWAA043109 420041026A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29762SW 27876 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041101000122004110100012NM 2004 11 1 2004UALA00912 120040929A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29649UA54320 25286 MAIN CABIN SEAT TRACK LBL 88 AT BS 747.5 TO 808 BROKEN, CRACKED AND CORRODED. DAMAGED SEAT TRACK REPLACED. 2L72 4F4 FRTA1NM E24NE 20041101000132004110100013 2004 11 1 DL76L040964 420041013A23301301851100 MONITOR BOEING767 767332 1382001NM CABIN OVERHEATED A DALAA UNSCHED LANDING MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27182DN 25987 DIVERTED TO YYT DUE TO REPORTED SMOKE FUMES IN THE CABIN. MTC FOUND AN OVERHEAD VIDEO MONITOR AT 18AB OVERHEATED. MTC FOUND ALL THREE COOLING HOLES OBSTRUCTED, TWO WERE BLOCKED BY SUPPORT BRACKETS AND THE REMAINING ONE BY DUST. ALSO FOUND AN AFT COFFEEMAKER ELEMENT LOOSE AND CONTACTING SOME OLD COFFEE GROUNDS. 2L72 4F RTA1NM 20041101000162004110100016EA 2004 11 1 COMA0460573 120041011A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FALSE ACTIVATIONA COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01797CA 7344 FLIGHT 4943 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND FOUND NO DEFECTS. 2L72 4F RTA21EA 20041101000172004110100017NM 2004 11 1 2004UALA00768 120040808A3211656337820600U LINK ASSY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 RIGHT MLG WAS DAMAGED BY IMPROPER CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. REPLACED LINK. 2L72 4F4 FRTA16WE E2GL 20041101000202004110100020NM 2004 11 1 2004UALA00891 120041003A7797420990 WIRE HARNESS BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EGT INDICATOR FAILED A UALAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29216UA24931 30549 222002 RIGHT ENGINE EGT INDICATION PROBLEMS. RIGHT ENGINE EGT INDICATION VERY ERRATIC. FLIGHT 0945-03 FRA-ORD, DIVERTED TO LHR. WIRING CHECKS PIN-TO-PIN, AND PIN-TO-GROUND ACCOMPLISHED OK. CONTINUITY CHECKS NORMAL. REPLACED WO623 HARNESS PER AMM 73-21-73. (PW IPC 73-21-00-21-001). ACCOMPLISHED TESTS AND HIGH POWER RUN - EGT STEADY, CHANNELS A & B READ THE SAME. THE TIMES GIVEN BELOW FOR THE REMOVED HARNESS ARE ESTIMATED. 2L72 4F4 FRTT0001SE E46NE 20041101000212004110100021EU 2004 11 1 2004UALA00892 120041001A2910 TRANSMITTER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29433UA 589 FLIGHT EXPERIENCED GREEN HYDRAULIC SYSTEM LOSS OF QUANTITY. GREEN SYSTEM TRANSMITTER ON NR 1 ENGINE BROKEN AND LEAKED GREEN SYSTEM HYDRAULIC FLUID. REPLACED GREEN SYSTEM TRANSMITTER. 2L72 4F4 FRTA28NM E40NE 20041101000222004110100022SO 2004 11 1 C2XA04BT098 120040918A14207281000561 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY LIGHTSCONTAMINATED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2721144 145741 EMERGENCY LIGHTS STAYED ON IN ARM POSITION. DOWNPOWERED ACFT & RESELECTED ARMING SWITCH, EMERGENCY LIGHTS OPS CHECKED GOOD. AFTER ARRIVING, EMERGENCY LIGHTS ARE ON WHEN SWITCH IS IN THE ARM POSITION, WHEN F/A TURNS CABIN LIGHTS OFF EMERGENCY LIGHTS GO OFF. MX REMOVED & REPLACED ALL FOUR BATTERY PACKS, ACFT OPS CHECKED GOOD. ON PREFLIGHT, EMERGENCY LIGHTS COME ON WHEN SIDEWALL & CEILING LIGHTS ARE TURNED ON, EMERGENCY LIGHTS ARMED POSITION. MX REMOVED & REPLACED CONTROL MODULE ASSEMBLY WHICH DID NOT CURE PROBLEM. TROUBLESHOT DOWN TO FAULTY CANNON PLUG P8906, MEGAHOMED CANNON PLUG P8906, NO FAULTS FOUND. CLEANED METAL CHIPS OUT OF PLUG P8906, OPS CHECKED EMERGENCY LIGHTS GOOD. ACFT RETURNED TO SERVICE. 2L72 4F RT 20041101000232004110100023NM 2004 11 1 2004UALA00834 120040904A7500 BLEED AIR SYS AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 OVERHEATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29814UA 862 RETURN TO FIELD WITH A NR 2 BLEED AIR FAULT. BLEED AIR FAULT GENERATED BY NR 2 BLEED SYSTEM OVERTEMPERATURE. FOUND FAULTY FAV THERMOSTAT, 2L72 4F4 FRTA28NM E40NE 20041101000262004110100026NM 2004 11 1 2004UALA00837 120040909A2613896373 SENSING ELEMENT BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29916UA 25383 722174 ENGINE NR 2 OVERHEAT LIGHT ILLUMINATED. OVERHEAT DETECTION LOOP-A WAS INOPERATIVE THE PREVIOUS DAY ELIMINATING REDUNDANCY FEATURE OF THE OVERHEAT DETECTION SYSTEM. PERFORMED TROUBLESHOOTING OF OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE M1122 CORE LOOP-B FAILED INSULATION RESISTANCE CHECK. REMOVED AND REPLACE BOTH LOOP A & B CORE DETECTOR ELEMENTS M1122. 2L72 4F4 FRTA16WE E2GL 20041101000272004110100027NM 2004 11 1 2004UALA00943 120041016A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29654UA53418 25392 FLIGHT DECK FLOORBEAM AT STA 246 FORWARD FACE STIFFENER CRACKED LOWER CORNER AT LBL 25. BOEING SERVICE BULLETIN RECOMMENDED ROUTINE INSPECTION IN PLACE TO MONITOR THIS CRACKING OF STA 246 FLOORBEAM. CRACKING OCCURS DUE TO HIGHER THAN INITIALLY ANTICIPATED LOADING. REMOVED & REPLACED STIFFENER. 2L72 4F4 FRTA1NM E24NE 20041101000282004110100028NM 2004 11 1 2004UALA00944 120041015A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 AFT PIT FRAME DENTED BS 1500 STR 25L TO STR 26L. INSTALLED "J" ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000302004110100030NM 2004 11 1 2004UALA00946 120041016A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME DENTED AT BS 1600 STR 26R. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000312004110100031NM 2004 11 1 2004UALA00947 120041016A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000342004110100034NM 2004 11 1 2004UALA00794 120040831A2781390FW04A10 PROXIMITY SENSOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 SLATS MALFUNCTIONED A UALAO OTHER N FALSE WARNING LDLANDING 1 WP29363UA 24532 LANDED DCA UNDER AMBER ALERT DUE TO LEADING EDGE SLAT PROBLEM. *S/D* AMBER INTRANSIT LIGHT ON NR 2 SLAT, OVERHEAD ANNUNCIATOR PANEL STAYS AMBER WITH SLAT DOWN AND LOCKED. SLAT INTRANSIT LIGHT ON FWD INSTRUMENT PANEL ALSO STAYS ON. RAN FLAPS THROUGH FULL CYCLE SEVERAL TIMES AND OPERATED NORMALLY. REPLACED NR 2 L/E SLAT PROX SENSOR S164 PER MM27-88-11. ALL INDICATIONS OPS CHECK GOOD. 2L72 4F4 FRTA16WE E2GL 20041101000352004110100035NM 2004 11 1 2004UALA00795 120040819A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 FRAME AT STATION 1400 DENTED ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000362004110100036NM 2004 11 1 2004UALA00796 120040819A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 FRAME AT STA 1420 IS DENTED BETWEEN STR 25-26L. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR DOUBLER INSTALLED. 2L72 4F4 FRTA2NM E17NE 20041101000372004110100037NM 2004 11 1 2004UALA00797 120040819A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 FRAME AT STA 1500 DENTED ABOVE STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000452004110100045NM 2004 11 1 2004UALA00805 120040825A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 CABIN FLOORBEAM UPPER CHORD SURFACE CORRODED AT BS 1660 RBL 54. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000472004110100047EA 2004 11 1 COMA0460584 120041015A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01797CA16960 7344 FLIGHT 5222 FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED BPSU. 2L72 4F RTA21EA 20041101000502004110100050EA 2004 11 1 COMA0460562 120041007A5346 BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE SUPPORT CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 CRACK ON THE ENGINE SUPPORT BEAM RIGHT HAND SIDE. PERFORMED REO 601R-53-61-366. 2L72 4F RTA21EA 20041101000522004110100052NM 2004 11 1 2004UALA00852 120040927A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALAK NONE O OTHER ININSP/MAINT 1 WP29177UA 24384 EEL INOP CROSS AISLE AT LAV 110. *S/D* SECURED WIRE UNDER THE CARPET. 2L74 4F4 FRTA20WE E24NE 20041101000542004110100054 2004 11 1 2004UALA00854 420040924A2565 SLIDE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE L1 DOOR DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29398UA 24673 DOOR 1 LEFT SLIDE PACK FELL OUT. GIRT BAR DISENGAGED FROM GIRT BAR RETAINERS (CLIPS USED FOR STOWING GIRT BAR WHEN SLIDE IS DISARMED) ON SLIDE COMPARTMENT COVER AND FELL INTO BRACKETS (FLOOR FITTINGS THAT KEEP SLIDE ATTACHED TO AIRCRAFT DURING DEPLOYMENT), RESULTING IN A PARTIAL SLIDE DEPLOYMENT. SLIDE WAS INSPECTED PER NORMAL OVERHAUL PROCEDURES. FLIGHT ATTENDANTS HAVE BEEN ADVISED TO ENSURE GIRT BAR IS STOWED PROPERLY WHEN DISARMING A DOOR. 2L72 4F4 FRTA16WE E2GL 20041101000552004110100055NM 2004 11 1 2004UALA00855 120040829A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 1640 RBL 52. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR CHORD. 2L72 4F4 FRTA2NM E17NE 20041101000562004110100056NM 2004 11 1 2004UALA00856 120040904A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 BS 620 STRINGER 16L HAS OVERSIZED HOLES. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER WITH NEW STRINGER SPLICE SECTION AND REINSTALLED 3 EACH SHEAR TIES. 2L72 4F4 FRTA2NM E17NE 20041101000572004110100057NM 2004 11 1 2004UALA00857 120040907A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 AFT PIT FRAME DENTED AT BS 1460 BETWEEN STR 25L TO STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000622004110100062 2004 11 1 SWAA043116 420041026A25656557463 LATCH BOEING737 7373H4 1384600NM L2 GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29647SW 27717 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR FWD FLOOR LATCH LOOSE. SECURED L2 DOOR EVAC SLIDE FWD FLOOR LATCH PER MM. 2L72 4F RTA16WE 20041101000652004110100065EA 2004 11 1 COMA0470074 120041021A2751 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01355CA 10067 FLIGHT 5537 FLAP FAULT STATUS MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041101000662004110100066WP 2004 11 1 AALA20041063 120041010A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21959U 49704 DFW - AFT OVERWING EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041101000672004110100067NM 2004 11 1 AALA20041064 120041023A3350 LIGHT BOEING757 757223 1384957NM L1 DOOR BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21653A 24611 DFW - L1 DOOR FORWARD EXIT SIGN ASSEMBLY IS BROKEN. REPLACED L1 DOOR FORWARD EXIT SIGN LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041101000682004110100068NM 2004 11 1 AALA20041065 120041023A3350 SHROUD BOEING767 767323 1385205NM EMERGENCY LIGHT MISSING A AALAK NONE L NO TEST ININSP/MAINT 1 SW21372AA 25199 MIA - ESCAPE PATH LIGHTING AT 24R MISSING SHROUD ASSEMBLY LIGHT. REPLACED ESCAPE PATH LIGHTING 24R SHROUD ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041101000692004110100069WP 2004 11 1 AALA20041066 120041022A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217518A 49895 SAT - EMERGENCY EXIT LIGHT IN COCKPIT R1 SERVICE DOOR IS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT IN COCKPIT R1 SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041101000702004110100070 2004 11 1 AALA20041067 420041023A2565 SLIDE AIRBUS300 A300B4605R 3930308EU L3 DOOR INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2170054 461 BOS - L3 DOOR SLIDE INFLATION BOTTLE FOUND AT ZERO. REMOVED AND REPLACED SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041101000712004110100071NM 2004 11 1 2004UALA00918 120041006A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 AFT PIT FRAME DENTED ON INBOARD FLANGE AT STA 1520 BETWEEN STR 25L AND 27L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED PIECE. FABRICATED AND INSTALLED SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000722004110100072NM 2004 11 1 2004UALA00806 120040825A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 CREASE BEAM WEB CORRODED ON UPPER SURFACE STA 1406 TO 1413. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB. 2L72 4F4 FRTA2NM E17NE 20041101000742004110100074NM 2004 11 1 2004UALA00907 120041006A4920 APU BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE APU BAY INOPERATIVE A UALAD RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP29673UA 29241 RETURNED TO THE FIELD WHEN THE LT GENERATOR WENT OFF LINE AND THE APU WOULD NOT START. APU START SWITCH AND APU ELECTRONIC CONTROL UNIT WERE REPLACED PREVIOUSLY DUE TO APU ALTITUDE STARTING PROBLEMS. THE ECU TESTED WITHIN LIMITS. APU START SWITCH WAS NOT ROUTED BACK TO HOME SHOP. THE APU DID NOT EXPERIENCE ANY OTHER EVENTS. 2L72 4F4 FRTA1NM E24NE 20041101000752004110100075EU 2004 11 1 2004UALA00893 120040907A5242 STRUCTURE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29482UA 1584 DENT ON AFT RT CORNER OF 811 AVIONICS DOOR STRUCTURE. DOUBLER AND TRIPLER REPAIR INSTALLED IN ACCORDANCE WITH AIRBUS RAS/031172/019/2004 (MAJOR REPAIR). 2L72 4F4 FRTA28NM E40NE 20041101000772004110100077NM 2004 11 1 2004UALA00913 120040928A5411 SPAR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 NACELLE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29649UA 25286 NR 2 NACELLE UPPER SPAR WEB IS CRACKED SEVERAL PLACES AS SEEN THROUGH ACCESS 446BL. REPAIRED UPPER SPAR WEB WITH DOUBLER AND FILLER JUST FWD OF PYLON AFT BLKHD PER SRM 54-53-01, FIG 208. PER SB 767-54-0092 R1 PROBABLE CAUSE OF CRACKING IS FLEXING OF PYLON MIDSPAR WEB. 2L72 4F4 FRTA1NM E24NE 20041101000792004110100079NM 2004 11 1 2004UALA00915 120040903A5347145T5313 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA50063 27115 CABIN SEAT TRACK STA 755, AND RBL 85 CRACKED. DAMAGED SEAT TRACK REPLACED. 2L72 4F4 FRTA1NM E24NE 20041101000822004110100082NM 2004 11 1 2004UALA00860 120040907A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 AFT PIT FRAME DENTED, BS 1440 IS DENTED 2 PLACES BETWEEN STR 25L AND STR 26L ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20041101000832004110100083NM 2004 11 1 2004UALA00861 120040907A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 AFT PIT FRAME DENTED BS 1420 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME UPPER FLANGE WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20041101000852004110100085NE 2004 11 1 2004UALA00898 220041006A7200 BLADES BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 ENGINE FAILED A UALAJA DUMP FUEL UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP29180UA 25224 LOSS OF NR 3 ENGINE. DECLARED EMERGENCY AND DUMPED FUEL. LOSS OF ALL OIL QUANTITY AND NO N1 INDICATION. T1 BLADES BROKEN. IN-FLIGHT SHUTDOWN OF THE #3 ENGINE WAS DUE TO THE FRACTURE OF SEVEN T-1 BLADES THAT CAUSED AN INBALANCE TO THE ENGINE CREATING MASSIVE SECONDARY DAMAGE TO THE ENGINE. THE CAUSE OF THE T-1 BLADE FRACTURE HAS BEEN DETERMINED TO BE THREE HPT DUCT STOPS LIBERATING LOSE FROM THE TURBINE NOZZLE. THESE STOPS ARE HELD IN PLACE BY BOLTS IN THE TURBINE NOZZLE MODULE. ROOT CAUSE OF THE IFSD HAS BEEN DETERMINED TO BE IMPROPER TORQUE OF THE BOLTS THAT RETAIN THE DUCT STOPS AND DUCT SEGMENTS. THE CORRECTIVE ACTION WAS TO REMOVE ENGINE FROM SERVICE AND OVERHAULED TO THE RING CASE CONFIGURATION. 2L74 4F4 FRTA20WE E24NE 20041101000862004110100086NM 2004 11 1 2004UALA00899 120041003A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 FLOOR SUPPORT AT STATION 1708 TO 1720 AND AT STR 14L TO 16L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000872004110100087NM 2004 11 1 2004UALA00908 120040920A5347145T5213 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29648UA54432 25285 MID CABIN SEAT TRACK AT STA 725 AND STA 759, APPROX LBL 90, AFT END CRACKED. *S/D* DAMAGED SEAT TRACKS WERE REPLACED. 2L72 4F4 FRTA1NM E24NE 20041101000902004110100090NM 2004 11 1 SWAA043117 120041026A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29520SW 25319 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041101000932004110100093NM 2004 11 1 SWAA043120 120041026A52406976425 FITTING BOEING737 7373T5 1384608NM SRVC DOOR HINGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED DOOR HINGE FITTING PER SRM. 2L72 4F RTA16WE 20041101000942004110100094 2004 11 1 2004UALA00838 420040911A3425 SYMBOL GENERATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 NAV DISPLAYFAILED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29425UA FCDMK1008915508 FLIGHT INSTRUMENT DISPLAY PROBLEM. CAPTAINS NAV DISPLAY BLANKED OUT. BLANKING CAUSED BY CAPT NAV DISPLAY UNIT. DISPLAY UNIT REPLACED. SHOP TEST OF THE DISPLAY UNIT FOUND INTERMITTENT BLANKING CONDITION SUSPECT SYMBOL GENERATOR CARD. 2L72 4F4 FRTA28NM E40NE 20041101000982004110100098NM 2004 11 1 2004UALA00842 120040916A5270 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE PAX DOOR ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29383UA 24658 ABORTED TAKEOFF AT 105 KTS AND RETURNED TO GATE DUE TO A FORWARD ENTRY DOOR WARNING. *S/D* DOOR OPERATION NORMAL. SECURED DOOR LIGHT SENSOR TARGET. 2L72 4F4 FRTA16WE E2GL 20041101001002004110100100NM 2004 11 1 2004UALA00808 120040902A2133 OUTFLOW VALVE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN PRESSURE FAILED A UALABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29658UA 27113 FLIGHT RETURNED TO FIELD WITH CABIN PRESSURE FAULTS. THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE FAILED. THE VALVE WAS NOT DEACTIVATED PER THE MEL CAUSING A LOSS OF CABIN PRESSURIZATION ON THE SUBSEQUENT FLIGHT. THE VALVE WAS RE-DEFERRED PER THE MEL AND REPLACED AT THE NEXT MAINTENANCE OPPORTUNITY WITH NO FURTHER PROBLEMS. LINE QA IS CONDUCTING A INVESTIGATION INTO THE CIRCUMSTANCES. 2L72 4F4 FRTA1NM E24NE 20041101001042004110100104NM 2004 11 1 SWAA043098 120041025A53156545410366 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM CHORD PER EA. 2L72 4F RTA16WE 20041101001052004110100105NM 2004 11 1 SWAA043099 120041025A5310BAC1505 GUSSET BOEING737 7375H4 138449DNM DOOR FRAME CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER FWD FRAME AT LOWER STOP FITTING GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER SRM. 2L72 4F RTA16WE 20041101001072004110100107NM 2004 11 1 DLM90040975 120041016A3246M90MAIN WHEEL DOUG MD90 MD9030 3023690NM MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27906DA 53386 ON OVERNIGHT WALKAROUND TRANSIT CHECK - AMT FOUND DAMAGE TO NR 2 MLG WHEEL ASSY AND BRAKE. DAMAGE OCCURRED WHEN THE INSIDE KEY OF NR 2 WHEEL ASSY HOLDING BOLT SHEARED AND THE KEY BACKED OUT STRIKING THE NR 2 BRAKE ASSY. THE KEY WAS HELD IN PLACE BY THE BRAKE ROTOR CUT OUTS AND CONTINUED TO ROTATE WITH THE WHEEL ASSY. REPLACED WHEEL AND BRAKE. 2L72 4F RTA6WE 20041101001082004110100108EA 2004 11 1 COMA0460560 120041004A3150 COMPUTER CNDAIRCL600 CL6002B19 1900309EA CONFIGURATION MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01796CA 7338 FLIGHT 5685 CONFIG RUDDER AND CONFIG TRIM WARNING DURING T/O. COULD NOT DUPLICATE. NO DEFECTS FOUND. A/C RETURNED TO SERVICE. 2L72 4F RTA21EA 20041101001092004110100109EA 2004 11 1 COMA0460564 120041007A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 LEFT HAND FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041101001112004110100111NM 2004 11 1 2004UALA00967 120041019A5753 FITTING BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT WING TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29654UA 25392 RIGHT WING INBOARD FLAP CENTER EXTERNAL HINGE FITTING INBOARD AND OUTBOARD FLANGES ARE CRACKED. 2L72 4F4 FRTA1NM E24NE 20041101001122004110100112NM 2004 11 1 2004UALA00969 120041021A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT LWR FUSELAGE SKIN DAMAGED BETWEEN STA 1393 AND 1420. DAMAGE CAUSED BY CARGO LOADER. DENTS AND CREASES REMOVED FROM THE FUSELAGE SKIN IN TWO SECTIONS. ONE EXISTING SKIN DOUBLER WAS REMOVED AND REPLACED WITH LARGER DOUBLER TO INCORPORATE ONE SECTION OF NEW DAMAGE. AN ADDITIONAL DOUBLER AND SPLICE DOUBLER WAS INSTALLED OVER REMAINING DAMAGED SECTION. SPLICE DOUBLER SPLICES AN EXISTING SKIN DOUBLER AND THE NEW SKIN DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041101001132004110100113NM 2004 11 1 2004UALA00955 120041017A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 LEFT FUSELAGE SKIN DENTED AT FRAME STA 761, BETWEEN STRINGERS 16L AND 15L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER - TRIPLER AND FILLERS. 2L72 4F4 FRTA2NM E17NE 20041101001142004110100114NM 2004 11 1 2004UALA00956 120041017A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 FUSELAGE SKIN AND DOUBLER DENTED AT STA 600 STR 19L IN 3 PLACES ON SKIN AND ONE ON DOUBLER. INSTALLED SKIN SPLICE REPAIR WITH DOUBLER, SPLICE DOUBLERS AND FILLERS. 2L72 4F4 FRTA2NM E17NE 20041101001152004110100115NM 2004 11 1 2004UALA00957 120041017A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 DURING ACCOMPLISHMENT OF A SKIN SPLICE REPAIR FROM BS 590 TO BS 640, DAMAGE TO STR 16L WAS FOUND IN THIS AREA. SKIN AND STRINGER DAMAGE CAUSED BY TYPICAL JETWAY DAMAGE. NEW SECTION OF STRINGER WAS SPLICED IN FOR REPAIR PURPOSES. 2L72 4F4 FRTA2NM E17NE 20041101001192004110100119NM 2004 11 1 2004UALA00931 120041011A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE L1 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29377UA 24642 EMERGENCY EXIT LIGHT AT DOOR 1L AND 2R INOP. REPLACED LAMP. 2L72 4F4 FRTA16WE E2GL 20041101001212004110100121NM 2004 11 1 2004UALA00922 120041009A5330 BEAR STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 AFT PIT AT STA 1415 BETWEEN STRINGER 26R & 27R BEAR STRAP CORRODED. AREA FASTENER WERE REMOVED AND CORROSION WAS BLENDED AND REMOVED. 2L72 4F4 FRTA2NM E17NE 20041101001232004110100123EA 2004 11 1 COMA0460567 120041007A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01912CA 7011 CRACK FOUND ON RIGHT WING PLANK. PERFORMED CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20041101001252004110100125NM 2004 11 1 DHL2004745517 120040705A5330 SKIN BOEING727 727224 1384076NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, FUSELAGE SKIN BS 1100 RT OF STR 1 CRACK INDICATION FROM FAST HOLE SKATE ANGLE SUPPORT NR 2 ENG NOSE COWL. NDT VERIFIED. CUT OUT CRACKED AREA SIZE .375 X .375 INCH AT STR 1 BS 1100 IAW S/B 727 53 02 04 AND SRM 53-30-3 FIG 3, FABRICATED DOUBLER REPAIR FROM 2024 T3 .063 SIZE 10.8 X 11.5 INCH PO 900790 IAW B727 SRM 53-30-3, TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 51-30-2 & S/B 727-53A0204 R-3. 2L73 4F A3WE 20041101001262004110100126NM 2004 11 1 DHL2004745537 120040704A5711 SPAR BOEING727 727224 1384076NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, 4 INCH CRACK ON DOUBLER FWD OF FWD EDGE OF UPPER MAIN SPAR LOCATED ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 (RIGHT WING). CUT OUT SKIN SPLICE SIZE 10.25 X 2.5 INCH ON L/E SKIN ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 IAW B727 SRM 51-10-1. FABRICATED SPLICE PLATE FROM 2024-T3 .050 SIZE 10.25 X 2.5 INCH PO 900980 AND SPLICE REPAIR FROM 2024-T3 .050 SIZE 6 X 2.5 INCH PO 900980 IAW B727 SRM 51-40-2, TREATED AND PRIMED PARTS AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-40-2. 2L73 4F A3WE 20041027001132004102700113SO 2004 10 27 C2XA04SH526 120041022A321014571033005 BEARING CAP EMB 145 EMB145ER 3260211SO RT MLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE RIGHT MAIN GEAR AFT BEARING CAP FOUND PITTED. REPLACED THE BEARING CAP IAW 32-10-01. 2L72 4F RTT00011AT 20041027001402004102700140SO 2004 10 27 C2XA04SH514 120040929A532014521713003 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712934 145019 DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED THE DEFECTIVE BEAM IAW SRM 51-40-02. 2L72 4F RTT00011AT 20041027001692004102700169EA 2004 10 27 COMA0460582 120041018A3000 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ACTIVATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01739CA 7273 FLIGHT 5499 A/I DUCT WARNING DURING CLIMB. COULD NOT DUPLICATE. INSPECTED A/I SYSTEM, FOUND NO DEFECT. 2L72 4F RTA21EA 20041027001752004102700175EA 2004 10 27 COMA0460570 120041011A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01797CA 7344 FLIGHT 5011 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, FOUND NO DEFECTS. 2L72 4F RTA21EA 20041028000142004102800014NM 2004 10 28 04FDEA02331 120040801A5510ALC8101504 SKIN PANEL DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 RT HORIZONTAL STABILIZER NR 3R BARREL NUT BORE FOUND WITH CORROSION, CLEAN UP OF CORROSION FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80289. 2L73 4F4 FRTA22WE E13NE 20041028000172004102800017NM 2004 10 28 04FDEA02334 120040801A5753ARC2512504 BRACKET DOUG MD11 MD11 3023602NM GE CF6 CF680 30025NE ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25607FE 48547 RT WING, IB FLAP OB HINGE (FLAPSIDE) PIVOT HOLE NR 1 IB BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03. 2L73 4F4 FRTA22WE E13NE 20041028000182004102800018 2004 10 28 HNAA0400073 420040803A3460066401302 CONTROL HEAD DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE COCKPIT SMOKE A HNAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07931HA 132 CREW NOTICED SMOKE AND SMELLED ODOR COMING FROM KNS 660, CREW TURNED OFF KNS 660 SMOKE AND ODOR WENT AWAY. KNS 660 REMOVED FOR INSPECTION FOUND NO DEFECTS, ALSO REMOVED RADAR DISPLAY UNIT, NO DEFECTS NOTED. PLACED KNS 660 ON MEL. 2H72 4T4 TRTA13NM E20NE 20041028000202004102800020CE 2004 10 28 YDB2004FBBB 120040721A32402407003487 TUBE LEAR 25 25D 5170514CE GE CJ610 CJ6108 30006NE BRAKES UNSERVICEABLE A YDBRO OTHER O OTHER NRNOT REPORTED 1 SO094488W5000 367 PILOT REPORTED BRAKES WERE VERY WEAK ON LANDING ROLL OUT. FOUND LARGE AMOUNT OF HYDRAULIC FLUID ON AFT PORTION OF AIRCRAFT BELLY. T/S AND FOUND LT ENGINE HYDRAULIC PRESSURE LINE LEAKING AT SUPPORT CLAMP IN TAIL COMPARTMENT. ADEL SUPPORT CLAMP RUBBER CUSHION WAS COLLAPSED AND LINE WAS CHAFING ON CLAMP BODY. LINE CHAFED THROUGH AND DEPLETED HYDRAULIC SYSTEM. 2 CLAMPS SUPPORT THIS LINE, OTHER CLAMP WAS ALSO COLLAPSED AND CHAFING ON THIS LINE BUT NOT LEAKING. REPLACED LINE AND CLAMPS WITH NEW AND INSPECTED OTHER HYDRAULIC LINES IN AIRCRAFT FOR SAME CONDITION, NONE FOUND. 2L72 4J4 J A10CE 1E16 20041028000212004102800021NM 2004 10 28 EE4Y040009 120040817A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN, AT B STA 1050 FROM LBL 63 INCHES TO RBL 56 INCHES FLOORBEAM UPPER CHORD WITH HEAVY CORROSION IN SEVERAL PLACES. 2L73 4F4 FRTA3WE E2EA 20041029000142004102900014EU 2004 10 29 2004UALA00779 120040820A2910D9347025400000 B-NUT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYD SYSTEM LOOSE A UALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP29417UA 483 LANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC SYSTEM. *S/D* AIRCRAFT EXPERIENCED GREEN HYDRAULIC QUANTITY LOSS INFLIGHT. FOUND B-NUT LOOSE AT BRAKE PRESSURE ACCUMULATOR. TIGHTENED B-NUT, NO LEAKS. 2L72 4F4 FRTA28NM E40NE 20041029000462004102900046NM 2004 10 29 SWAA043114 120041026A53156545833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND 2 EACH CRACKS ON FLOOR WEB BETWEEN BS 188 AND BS 196, AT STRINGER 17L AND STRINGER 17R. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20041101000012004110100001SO 2004 11 1 LR7A04104 120041001A53123914911 CAP LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 588 - FS 597, WL187 SHELF OUTER TEE CORRODED AT RBL 67. REPLACE TEE CAP IAW DWG 391491 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041101000062004110100006NM 2004 11 1 SWAA043115 120041026A5753 SKIN BOEING737 7373H4 1384600NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29647SW 2586 27717 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING T/E INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED RT WING FOREFLAP PER MM. 2L72 4F RTA16WE 20041101000252004110100025NM 2004 11 1 2004UALA00836 120040909A2820125334D1 VALVE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CROSS FEED INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29182UA 25279 NR 2 CROSS FEED VALVE CLOSED AND UNABLE TO USE FUEL IN NR 2 RSV TANK. VALVE BODY COULD NOT BE DRIVEN OPEN BY THE ELECTRICAL ACTUATOR. VALVE BODIES ARE FLOWN TO FAILURE. THERE HAVE BEEN TWO OF THESE VALVE BODIES REPLACED IN THE LAST 12 MONTHS WITH AN MTBUR OF 786,875. THIS HIGH REMOVAL FIGURE IS DUE TO THE LARGE POPULATION OF THESE VALVES ON THE 757, 767 AND 747 FLEETS. 9/29/04- FLEET EG PARTICIPATED IN A UNIT TEST AND TEAR DOWN OF THE CROSSFEED VALVE UNIT MR28202 S/N 85402. THE VALVE BUTTERFLY SHAFT O-RINGS WERE AGED AND SWELLED, CREATING SLUGGISH ROTATION OF THE SHAFT. 2L74 4F4 FRTA20WE E24NE 20041101000292004110100029NM 2004 11 1 2004UALA00945 120041016A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 CABIN FLOORBEAM CAP AT BS 1640 RBL 51 TO RBL 60 IS CORRODED BEYOND ALLOWABLE LIMITS. MAJOR REPAIR ACCOMPLISHED. TYPICAL FLOOR STRUCTURE CORROSION. INSTALLED STRAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000382004110100038NM 2004 11 1 2004UALA00798 120040817A5330 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 AFT CABIN SHEAR WEB HAS AREA OF CORROSION AT APPROX BS 1681 THRU 1699 RBL 44 THRU 54. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB. 2L72 4F4 FRTA2NM E17NE 20041101000392004110100039NM 2004 11 1 2004UALA00799 120040817A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 AFT CABIN FLOORBEAM AT BS 1640 IS CORRODED RBL 18 THRU 58. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW T-CAP AND REPAIR STRAPS. 2L72 4F4 FRTA2NM E17NE 20041101000462004110100046EA 2004 11 1 COMA0460583 120041015A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01926CA6292 7027 FLIGHT 5468 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. REPLACED THE PSEU. 2L72 4F RTA21EA 20041101000492004110100049NM 2004 11 1 SWAA043086 120041024A57436937877 FITTING BOEING737 7373H4 1384600NM RT & LT WING CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED SERVICE CHECK, FOUND BOTH RT AND LT FWD OUTBOARD MLG HANGER FITTINGS CORRODED. REMOVED AND REPLACED BOTH RT AND LT HANGER FITTINGS PER EA. 2L72 4F RTA16WE 20041101000512004110100051EA 2004 11 1 COMA0460565 120041007A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01435CA 7473 RIGHT HAND FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041101000632004110100063EA 2004 11 1 COMA0460579 120041020A5330601R3114627 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01940CA24672 7048 DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011), 1 CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN NEAR FS 461.0 BETWEEN BL0.0 AND RBL 9.0. THE CRACK 2.25 INCH IN LENGTH. THE PRESSURE FLOOR SKIN WAS REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9/29/03. 2L72 4F RTA21EA 20041101000782004110100078NM 2004 11 1 2004UALA00914 120040928A5753 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT WING FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29649UA 25286 LEFT WING INBOARD FLAP CENTER EXTERNAL HINGE IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED HINGE WITH REPAIR ANGLES. 2L72 4F4 FRTA1NM E24NE 20041101000892004110100089SO 2004 11 1 C2XA04SH521 120041001A335020121A BATTERY EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712934 145019 DURING INSPECTION THE LAST THREE AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY IAW 33-50-04. 2L72 4F RTT00011AT 20041101000962004110100096NE 2004 11 1 2004UALA00840 220040914A7200 ENGINE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE NR 2 FAILED A UALAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING KEJFLUID LOSS VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 WP29795UA 26927 LOSS OF OIL PRESSURE IN NR 2 ENGINE AND ENGINE VIBRATION. MAINTENANCE FOUND METAL ON THE MASTER & NR 4 BEARING CHIP DETECTORS, & METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED IN SEA. TEARDOWN REVEALED THE THRUST BALANCE CAVITY ROTATING OUTER SEAL CAUGHT FIRE & BURNED AWAY. SUBSEQUENT HEAT DISTRESS LIBERATED LARGE CHUNKS OF BOTH THE STATIC & ROTATING THRUST BALANCE CAVITY OUTER SEALS. SLIGHTLY OVER 7 LBS. OF MATERIAL CENTRIFUGED OUTWARD INTO ROTOR, CREATING APPROX 2100 OZ-IN OF UNBALANCE & THE RESULTANT HIGH VIBRATION. RESULTANT DAMAGE TO NR 4 BEARING, & ITS CARBON SEALS ACCOUNTED FOR OIL LOSS. ROOT CAUSE FOR FIRE IS UNDER PWA INVESTIGATION & WILL TAKE SEVERAL MONTHS. 2L72 4F4 FRTT0001SE E46NE 20041101001032004110100103NM 2004 11 1 DL73S040966 120041014A2530 CONNECTOR BOEING737 737247 138448DNM COFFEEMAKER SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27244WA 331 23518 AFT GALLEY NR 2 COFFEEMAKER C/B POPPED. LATER TRASH CAN FILLED UP WITH WATER. WATER SUPPLY SHUT OFF. REMOVED BOTH COFFEEMAKERS. FOUND ARCING ON NR 2 COFFEEMAKER CANNON PLUG. TURNED WATER SUPPLY ON. CANNOT FIND SOURCE OF LEAK. REPLACED BOTH COFFEEMAKERS AND PLUG. 2L72 4F A16WE 20041101001062004110100106NE 2004 11 1 DL76P040974 220041016A7250PW40603 TURBINE BOEING767 767332 1382001NM PWA 4090 PW4090 52119NE NR 2 ENGINE DAMAGED A DALAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO27144DA47901 27584 724150 ON T/O ROLL APPROX 130 KTS CREW EXPERIENCED LOUD BANG AND FLASH FOLLOWED BY YAW TO THE RIGHT. EGT REPORTED OFF SCALE ON RT ENG. PASSENGERS REPORTED SMOKE FROM ENG. BOTH FIRE BOTTLES AND RTO PERFORMED. MTC FOUND METAL IN THE TAILPIPE AND EGT RECORDED AT 729 FOR 56 SEC. REPLACED ENGINE. 2L72 4F4 FRTA1NM E46NE 20041101001242004110100124NM 2004 11 1 CALA0400684 120041022A53156545810 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712327 23457 INSPECTION FOUND THE UPPER FLANGE OF FLOORBEAM CORRODED AT NUT PLATE HOLE, STA 312, RBL 8. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-10-51. 2L72 4F RTA16WE 20041101001282004110100128NM 2004 11 1 DHL2004745521 120040706A5532 PANEL BOEING727 727224 1384076NM VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, VERTICAL FIN BASE COMPOSITE PANEL LT SIDE BELOW AND FWD OF THE NR 2 ENGINE CHANGE FIXTURE CAVITY WITH DENTS. CUT OUT 3 EA SHARP DENTED AREAS APPROX 2.25 X .5 INCH, 2.25 X .5 INCH & 1 DIA. FABRICATED 2 EA FILLERS APPROX 2.25 X .5 INCH & 1 EA FILLER APPROX 1 INCH DIA AND 2 EA DOUBLERS APPROX 4 INCH DIA & 9 X 3.75 INCH FROM 2024-T3 .016 PO 900962. CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIRS SURFACES FOR BONDING. BONDED, CLEANED, TREATED, PRIMED & SEALED REPAIR. ALL MAINTENANCE ACTIONS ACCOMPLISHED IAW B727 SRM 55-30-1 FIG 2, 51-40-6 FIG 2, 55-30-2 FIG 1 & 51-40-20 FIG 30. 2L73 4F A3WE 20041101001292004110100129NM 2004 11 1 DHL2004745524 120040706A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, LT FUSE HAS DENTS FWD BS 620 ABOVE STR 27L. DAMAGED AREA OUT OF LIMITS IAW B727 SRM53-30-1 FIG 1. CUT OUT DAMAGED AREA 14.125 X 4.75 INCH AND FABBED FILLER FROM 2024 T3 .050 PO 9001118 DIM 14.125 X 1.125 INCH AND DOUBLER FROM 2024 T3 .063 PO 900920 DIM 22.125 X 10.875 INCH IAW B727 SRM 53-30-3 FIG 3. PARTS TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER AND FILLER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041101001332004110100133NM 2004 11 1 2004UALA00949 120041016A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1540 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041101001342004110100134NM 2004 11 1 DHL2004745527 120040711A5230 HINGE BOEING727 727224 1384076NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C- CHECK, MAIN DECK CARGO DOOR HINGE AFT UPPER SECTION CRACKED. REMOVED & REPLACED DAMAGED HINGE SECTION P/N 20001-16-7200 PO 9912233 DIM 18 INCHES LONG PER S/B AEI 01-01 OPS CHECK ACCOMPLISHED ON NR 90350. 2L73 4F A3WE 20041101001362004110100136NM 2004 11 1 DHL2004745535 120040722A5260 SKIN BOEING727 727224 1384076NM AIRSTAIR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, AFT AIRSTAIR EXTERNAL SKIN CREASED AND DENTED AT BS 1263. CUT OUT DAMAGED AREA AT AFT AIRSTAIR EXT SKIN 2.75 X 2 INCH IAW B727 SRM 52-10-2, FABRICATED DOUBLER REPAIR FROM 2024 T3 .050 PO 9001124 DIM 5.875 X 5 INCH IAW B727 SRM 52-10-2. PARTS TREATED AND PRIMED IAW B727 SRM 52-10-2, INSTALLED DOUBLER REPAIR IAW B727 SRM 52-10-2. 2L73 4F A3WE 20041101001402004110100140NM 2004 11 1 SWAA043100 120041025A53106517684 DOOR FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CUTOUT FWD LOWER FRAME WEB CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM. 2L72 4F RTA16WE 20041101001422004110100142 2004 11 1 2004UALA00932 420041011A2565 SLIDE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE L1 DOOR DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29913UA 25291 DOOR 1L SLIDE PACK FELL OUT. SHOP FINDINGS SHOWED THAT SLIDE NEEDED REPACKING. SLIDE WAS INSPECTED, REPACKED AND RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20041101001442004110100144SO 2004 11 1 C2XA04CL105 120041011A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A O OTHER O OTHER NRNOT REPORTED 1 SW2714974 145161 CREW REPORTED THE NR 2 AND 3 EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED THE EMERGENCY LIGHT INVERTED. OPERATIONAL CHECK OK. 2L72 4F RTT00011AT 20041101001452004110100145NM 2004 11 1 DL757040967 120041013A5240 CLIP BOEING757 757232 1384965NM L-2 DOOR GIRTBARBROKEN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27686DA 27589 L-2 DOOR SLIDE DEPLOYED WHILE ARMED WHEN OPENED FROM THE OUTSIDE. FOUND GIRT BAR RETAINING CLIP BROKEN ON ONE END. SUSPECT INTERFERENCE WITH GIRT BAR END FITTING BEING DETACHED FROM FLOOR FITTING. REPLACED CLIP. 2L72 4F RTA2NM 20041101001462004110100146NM 2004 11 1 DLM88040976 120041016A3030851AH HEATER DOUG MD88 MD88 3023688NM RUDDER PITOT INOPERATIVE A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO27909DE 53418 PITOT/STALL HEAT OFF LIGHT ON ANNC PANEL WITH NO CURRENT GOING TO RUDDER LIMITER. REPLACED PITOT TUBE. 2L72 4F RTA6WE 20041102000012004110200001NM 2004 11 2 DL76K040978 120041017A24227077603 STATIC INVERTER BOEING767 767332 1382001NM E/E BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27178DZ 3009 007 30596 SMOKE IN C/P, DIVERT TO GSO. INVERTER UNDER EVALUATION AND FOUND CHOKE ASSY 708371-3 BURNT. REPLACED SAME. 2L72 4F RTA1NM 20041102000032004110200003NM 2004 11 2 SWAA043127 120041027A53106546805 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS CRACKED AT BS 821, LBL 70, BS 773, RBL 7.5. REMOVED AND REPLACED WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20041102000042004110200004NM 2004 11 2 SWAA043128 120041027A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND 3 EACH FRAMES CRACKED AT BS 787, STRINGER 8L, REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041102000052004110200005NM 2004 11 2 SWAA043129 120041027A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 787, RBL 13, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041102000062004110200006NM 2004 11 2 SWAA043130 120041027A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 737, BS 837, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041102000082004110200008NM 2004 11 2 SWAA043132 120041027A53116546541 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 663.75, STRINGER 14R AND STRINGER 14L. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041102000102004110200010NM 2004 11 2 SWAA043121 120041027A3350BR9442 LIGHT BOEING737 7373Y0 1384671NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT NEXT TO FLIGHT ATTENDANT SEAT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041102000132004110200013 2004 11 2 DL75K040968 420041014A2565 GIRT BAR BOEING757 757232 1384965NM R-1 DOOR LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27644DL 23998 DOOR 1R SLIDE LIGHT INOP WHEN DOOR IS ARMED. ADJUSTED GIRT BAR. 2L72 4F RTA2NM 20041102000152004110200015EU 2004 11 2 DHL2004364013 120040806A3260BED201 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU NLG MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01364DH 141 COULD NOT RAISE LANDING GEAR HANDLE ON SYSTEM 2. COMPLIED WITH ABNORMAL PROC. DID RAISE GEAR ON SYSTEM 1. PROBES ON MWP WAS CAPT PITOT LIGHT ON S/O PANEL. COMPLIED WITH ABNORMAL PROC. PERFORMED FIM 22.23.00. REMOVED AND REPLACED PROX DETECTOR. SYS TESTS NORMAL REF AMM 32.61.12. SYS OPS NORMAL REF AMM 30.31.0. 2L72 4F RTA35EU 20041102000162004110200016 2004 11 2 SWAA043073 420041022A256561620468 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF LIMITS A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EVAC SLIDE IND OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041102000192004110200019NM 2004 11 2 SWAA043076 120041022A55526959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM. 2L72 4F RTA16WE 20041102000202004110200020NM 2004 11 2 SWAA043077 120041022A53306545766 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500C, STRINGER 10R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041102000212004110200021NM 2004 11 2 SWAA043078 120041022A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 971, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041102000222004110200022NM 2004 11 2 SWAA043101 120041025A57126545445 RIB BOEING737 7375H4 138449DNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKED. REPAIRED RT WING RIB CHORD PER EA. 2L72 4F RTA16WE 20041102000232004110200023NM 2004 11 2 SWAA043102 120041025A53126546568 BULKHEAD BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND 4 EACH CRACKS ON BULKHEAD SKIN AT BS 1016, PANELS 1, 2, 5 AND 7. REPAIRED BULKHEAD PER EA. 2L72 4F RTA16WE 20041102000292004110200029NM 2004 11 2 2004UALA00868 120040908A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 EXTERNAL FUSELAGE SKIN EXPERIENCED DAMAGE FROM JETWAY OPERATION CAUSING DENTS AT STA 600-620 BETWEEN STR 15 LT AND 17 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER - TRIPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041102000302004110200030SO 2004 11 2 C2XA04CL106 120041011A3397GS8506DC WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A K NONE L NO TEST ININSP/MAINT 1 SW2713990 145277 DURING MAINTENANCE THE NR 2 AND 3 AISLE PATH EMERGENCY LIGHTING WERE INOPERATIVE. RESECURED GROUND WIRE AND SYSTEM CHECKED GOOD. 2L72 4T RTT00011AT 20041102000312004110200031NM 2004 11 2 2004UALA00933 120041012A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AFT CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29331UA 24192 EMERGENCY LIGHTS AT REAR OF AIRCRAFT INOP EEL STRIP. REPLACED AFT EEL STRIP. 2L72 4F4 FRTA16WE E2GL 20041102000332004110200033NM 2004 11 2 2004UALA00936 120041014A335021007 SWITCH BOEING757 757222 1384956NM PWA 2037 PW2037 NE L4 DOOR SIGN SHORTED A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29568UA 26674 EMERGENCY LIGHT TEST SWITCH AT 4L DOOR IS INOPERATIVE, SHORTED S10295. *S/D* REPLACED SWITCH. 2L72 4F4 FRTA2NM E17NE 20041102000352004110200035NM 2004 11 2 DHL2004745533 120040717A5753 SKIN BOEING727 727224 1384076NM RT WING FORFLAP PUNCTURED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, RT WING INBD FOREFLAP L/E WS 224 HAS A PUNCTURE AND AT WS 335 L/E HAS ONE (1) DENT. REFER TO NR 96459 FOR DENT REPAIR. CUT OUT DAMAGED AREA AND FABBED FROM 2024 T3 .050 PO 9001189 DIM 4 X 4 INCH AND 2 EA DOUBLERS FROM 2024 T3 .063 PO 900790 DIM 8 X 4 INCH EACH IAW 727 SRM 57-50-4 FIG 2. PARTS TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10-2 & 57-50-4 FIG 2. 2L73 4F A3WE 20041102000372004110200037NM 2004 11 2 SWAA043092 120041025A532065C27314 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND 5 EACH SHEAR TIES AT BS 500, STR 15R, BS 663.75, STR 10L AND STR 10R, BS 706, STR 10L AND STR 10R, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20041102000402004110200040EU 2004 11 2 2004UALA00766 120040814A2822568127202 PUMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUEL BOOST INOPERATIVE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29451UA 865 LEFT TANK PUMP NR 2 ECAM, NR 1 PUMP WAS PREVIOUSLY DEFERRED. THE LEFT WING TANK NR 2 FUEL BOOST PUMP WAS INOPERATIVE. REPLACED LEFT WING TANK FUEL NR 2 FUEL BOOST PUMP. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20041102000412004110200041NM 2004 11 2 2004UALA00769 120040811A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 AFT CARGO DOOR AT STA 795 STR 23 - 24 RT TO THE BEAR STRAP REQUIRES REPLACEMENT OF LWR SKIN SECTION DAMAGED FROM A PREVIOUS REPAIR. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER. 2L72 4F4 FRTA16WE E2GL 20041102000442004110200044EU 2004 11 2 2004UALA00777 120040819A3510MF20010 OXYGEN MASK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT MISRIGGED A UALAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 WP29437UA 655 FLIGHT DIVERTED DUE TO LOW COCKPIT OXYGEN PRESSURE. MASK WAS NOT STORED PROPERLY IN THE STORAGE BOX. IMPROPER STORAGE CAN ENGAGE THE 02 TEST VALVE, WHICH WILL ALLOW THE O2 TO VENT. THE MASK IS NOW STORED PROPERLY. 2L72 4F4 FRTA28NM E40NE 20041102000452004110200045NM 2004 11 2 CALA0400685 120041023A532065C807351 ANGLE BOEING737 737524 1384721NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716607 27320 INSPECTION FOUND CABIN FLOOR R-2 ENTRYWAY Z-ANGLE CORRODED AT STA 943-993, RBL 50. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20041102000462004110200046WP 2004 11 2 DHL2004805008 120040807A3241 CONTROL BOX DOUG DC8 DC873F 302199FWP ANTI SKID SYS FAILED A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01805DH 46125 INTERMITTENT ANTI-SKID LIGHT ON T/O, LIGHT FLICKERED DIMLY ON AND OFF. REMOVED AND REPLACED ANTI-SKID CONTROL BOX , OPERATIONAL CHECK OK PER M/M 32-43-0. 2L74 4F RT4A25 20041102000482004110200048NE 2004 11 2 2004UALA00962 220041014A7200 ENGINE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE NR 2 SURGES A UALAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 WP29676UA 30028 NR 2 ENG SILENT SURGE FLAGGED BY AIRCRAFT. THIS EVENT WAS A SILENT SURGE THAT WAS REPORTED BY THE ENGINEER WHO MONITORS THE ECM. THE EPR WAS BELOW 1.25. THE AIRCRAFT AND FLIGHT CREW DID NOT REPORT THIS EVENT. SURGE CHECKS WERE ACCOMPLISHED ON THE ENGINE WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA1NM E24NE 20041102000492004110200049NM 2004 11 2 DHL2004780006 120040807A324026011825 BRAKE ASSY BOEING727 727223 1384074NM NR 4 DRAGGING A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01780DH 22006 RT BRAKE VERY SENSITIVE AND DRAGGING. FOUND NR 4 BRAKE TO HAVE LOOSE PADS, CAUSING BINDING. REMOVED AND REPLACED NR 4 MAIN BRAKE ASSY IAW B727 M/M 32-41-32. REPLACED NR 4 MAIN TIRE AND WHEEL ASSY IAW B727 M/M 32-45-01. 2L73 4F A3WE 20041102000512004110200051NM 2004 11 2 2004UALA00950 120041016A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENT DAMAGE FROM CARGO LOADING. INSTALLED J-ANGLE DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041102000532004110200053NM 2004 11 2 SWAA043125 120041027A53306545890 BEAR STRAP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT ABOVE LOWER DOOR HINGE FITTING, BEAR STRAP CRACKED. REPAIRED BEAR STRAP PER SRM. 2L72 4F RTA16WE 20041102000542004110200054EA 2004 11 2 ASOA04655 120040825A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA E/E DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE MAIN AVIONICS BAY DOOR HANDLE AS FOUND CRACKED AT THE BASE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE MAIN AVIONICS BAY DOOR HANDLE. (M) 2L72 4F RTA21EA 20041102000582004110200058NM 2004 11 2 AMTA200401245 120041002A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DAMAGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 1 TO ROW 5. SPLICED WIRE PER WIRING DIAGRAM MANUAL 20-30-12. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 20041102000592004110200059NM 2004 11 2 UIEA200400159 120040920A572065B10538120 SUPPORT BOEING747 7472D3B 1384805NM FUSELAGE CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15505MC 21251 DURING OVERNIGHT, EXTERNAL IMPACT BY A FOREIGN OBJECT CAUSED BY A TORNADO. AN INSPECTION OF THE AIRCRAFT WAS CARRIED OUT AND IT WAS OBSERVED THAT AT BS 1034 RBL 104, THE UNDERWING FAIRING SUPPORT LOWER CHORD WAS CRACKED AT THE OUTBOARD FLANGE. THE LONGITUDINAL CRACK IS APPROXIMATE 3 INCHES LONG. THERE WERE NO OTHER REPAIRS WITHIN 12 INCHES OF THIS DAMAGE. TRIMMED OFF THE CRACKED AREA. NDT INSPECTED TO CONFIRM NO CRACK OF DEFECT EXISTS AT THE TRIMMED EDGE AND REPAIRED AREA. FABRICATED REPAIR PART FROM REPAIR ANGLE 7075-0 AND HEAT TREATED TO T6 AFTER FORMING. PERFORMED ULTRASONIC INSPECTION OF THE ANGLE AFTER FORMING TO ENSURE DEFECT FREE CONDITION. BOEING CONCURRED THAT THE REPAIR IS STRUCTURALLY ACEPTAB2L74 4F RTA20WE 20041102000602004110200060 2004 11 2 HALA0400943 420040922A23307002299001 VIDEO MONITOR BOEING767 767300 1385204NM PAX CABIN OVERHEATED A HALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP13590HA 33467 LAS - VIDEO IN FRONT OF 24/25 HJ OVERHEATED AND PRODUCED SMOKE. INSPECTED VIDEO MONITOR AND CONNECTORS, NO EVIDENCE OF BURNING. MONITOR SHROUD FASTENERS DAMAGED DURNG REMOVAL. MONITOR MPN 700-2299-001. (M) 2L72 4F RTA1NM 20041102000612004110200061NM 2004 11 2 UIEA200400158 120040917A3241 LIMITER BOEING747 74747UF 1384949NM ANTI SKID SYSTEMMALFUNCTIONED A UIEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA15497MC 29258 ILLUMINATION OF EICAS ANTI-SKID INTERMITTENT CAUTION WITH LONG HISTORY. REMAINS ILLUMINATED FOR PERIODS OF ONE MINUTE AND MORE UP TO TEN MINUTES PERIODS STATUS MSG. ANTI-SKID BRAKE LIMITER EXTINGUISHED DURING DESCENT, BUT INTERMITTENT EICAS REMAIN THROUGH ROLLOUT. AIRCRAFT DIVERTED TO DOH. CARRIED OUT BITE TEST ON BRAKE SYSTEM AS PER AMM 32-42-00, ANTI-SKID PASS. (M) 2L74 4F RT1384945 20041102000622004110200062NM 2004 11 2 UIEA200400170 120040920A2611 SMOKE DETECTOR BOEING747 74747UF 1384949NM CABIN MALFUNCTIONED A UIEAO OTHER N FALSE WARNING CLCLIMB 1 EA15492MC 29253 IMMEDIATELY AFTER TAKEOFF 'EICAS MSG'. WITH SMOKE DETECTOR MAKING LOUD BEEPING NOISE. AFTER 1 HOUR EICAS MSG WENT AWAY AND SMOKE DETECTOR STOPPED BEEPING, NO SMOKE DETECTED. ALL ASSOCIATED DUCTING CHECKED FROM CREW REST AREA TO STATION 950. NIL ABNORMALITIES FOUND. SMOKE DETECTOR CHECKED AND ASSOCIATED WIRES CHECKED OK. (M) 2L74 4F RT1384945 20041102000632004110200063EA 2004 11 2 ASOA04658 120040829A5210601R3198041 HINGE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO11857AS 7411 DURING A C-CHECK IN MCN, THE TOP STEP HINGE ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE IS REMOVING AND REPLACING THE OTP STEP HINGE ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20041102000652004110200065EA 2004 11 2 A6WA200440126 120040908A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31438AW 7748 DURING LIGHTNING STRIKE DAMAGE INSPECTION OF RIGHT FUSELAGE FOUND AREA BETWEEN STRINGER 26R-27R AT FS 243 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .007 INCH. CUT OUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5342. (M) 2L72 4F RTA21EA 20041102000662004110200066EA 2004 11 2 A6WA200440128 120040830A5220601R330501 HANDLE CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH LACK OF LUBE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31403AW 7288 CREW ESCAPE HATCH OUT HANDLE IS STUCK. LUBRICATED OUTER HANDLE SHAFT, WORKED HANDLE FREE AND LUBED SHAFT WITH DC33. (M) 2L72 4F RTA21EA 20041102000672004110200067EU 2004 11 2 2004F00419 120040912A3230664700560A4D CONTROL UNIT AIRBUS320 A320233 3930329EU MLG MALFUNCTIONED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23482TA 1482 DURING CLIMB, AFTER FLAPS RETRACTION A/C DID NOT ACCELERATE MORE THAN 235 KNOTS. BOTH PFDS AND STANDBY AIRSPEED SHOWED THE SAME MESSAGE. AIRCRAFT RETURNED TO SAL FOR MAINTENANCE. AFTER LANDNG, THE WIRING ON THE VMO/MMO SWITCH WAS CHECKED AND TROUBLESHOOTING WAS PERFORMED PER TASK TSM 34-13-00-810-912, AND NR LGCIU WAS REPLACED DUE TO ERRONEOUS FAULT PER AMM 32-31-71. NO FAULTS WERE NOTED. A FLIGHT TEST WAS PERFORMED TO VERIFIED ALL SYSTEMS AND ITS RESULTS WERE SATISFACTORY. AIRCRAFT RETURNED TO NORMAL OPERATION. (M) 2L72 4F RTA28NM 20041102000682004110200068NM 2004 11 2 UIEA200400178 120040929A323365B015029 ACTUATOR BOEING747 747243B 1384830NM MLG MALFUNCTIONED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15540MC 22508 ON TAKEOFF OUT OF BOG, A NOISE WAS HEARD RIGHT AT ROTATION. ALL SYSTEMS INDICATED NOTHING ABNORMAL. HOWEVER, WHEN THE GEAR WAS RETRACTED THE RIGHT BODY GEAR PRI AND ALT DOOR LIGHTS WERE ON ALONG WITH THE RED DOOR OPEN AND RED GEAR LIGHTS. THE LIGHTS EXTINGUISHED AFTER APPROX 2 MINUTES. (M) 2L74 4F A20WE 20041102000712004110200071CE 2004 11 2 RU3A0415 120041008A2910 HYDRAULIC SYSTEM LEAR 60 60LEAR 5170707CE MAIN MALFUNCTIONED A A UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW1554 009 WHILE LOWERING GEAR BOTH HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED. THE PRESSURE FLUCTUATED TO THE TOP OF THE YELLOW ARC, THEN CAME BACK TO NORMAL AND BOTH HYDRAULIC PRESS LOW LIGHTS WENT OUT. RAISED THE GEAR AND BOTH HYDRAULIC PRESSURE LIGHT CAME ON AND THE NOSE GEAR UNSAFE LIGHT STAYED ON, AGAIN THE HYDRAULIC PRESSURE FLUCTUATED BUT RETURNED TO A NORMAL READING AND THE PRESSURE LIGHTS WENT OUT. DECLARED EMERGENCY, BURNED FUEL LOAD DOWN, DISCUSSED PROBLEM WITH MAINTENANCE FACILITY. LOWERED GEAR NORMALLY AND AGAIN THE PRESSURE LIGHTS CAME ON FOR SEVERAL SECONDS AND THEN WENT OFF. LANDED SAFELY WITHOUT USE OF SPOILERS OR THRUST REVERSERS. (M) 2L72 4F RTA10CE 20041102000732004110200073EU 2004 11 2 2004F00422 120040826A5610NP1588013 WINDOW AEROSPATR72 ATR72212 8680945EU COCKPIT CRACKED A SIMABH EMER. DESCENT DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO21440AM3747 440 DURING CRUISING, THE CAPTAIN WINDSHIELD CRACKED. REPLACED CAPTAIN WINDSHIELD ASSEMBLY. (M) 2H72 4T RTA53EU 20041102000742004110200074NM 2004 11 2 AMTA200401148 120040916A3350 SOCKET BOEING757 75723N 1384973NM EMERGENCY LIGHTSDISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11514AT 27971 AFT FIVE EGRESS LIGHTS INOPERATIVE. RECONNECTED SOCKET/PIN, REF MM 33-51-05, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20041102000762004110200076NM 2004 11 2 UIEA200400161 120040921A5711 SPAR BOEING747 747230B 1384889NM LT WING CORRODED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND LEFT WING SKIN FORWARD OF FRONT SPAR OLES 1378-1387, 1410, 1438-1447. CORROSION WAS REMOVED BY BLENDING. NDT INSPECTED TO CONFIRM DAMAGE FREE CONDITION. BLENDED AREAS WERE FLAP PEENED, ALODINE 1200 AND BMS 10-11 TYPE II PRIMER APPLIED. CUSTOM FILLERS WRE INSTALLED. TO RMOVED CORROSION AT OLES 1410, THE EXISTING CUTOUT IN THE SKIN LOCATED 4 INCHES OUTBOARD IS ENLARGED. SKIN FILLER IS SEGMENTED SO AS NOT TO BE LONGER THAN 8 INCHES. THREE REPAIR PLATES WRE MADE FROM .096 INCH THICK 2024-T3 ALUMINUM. (M) 2L74 4F A20WE 20041102000772004110200077 2004 11 2 UIEA200400155 420040918A3414A4321710016 INDICATOR BOEING747 7472D7B 1384803NM AIRSPEED MALFUNCTIONED A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15523MC 21782 ABORTED TAKEOFF, CAPTAINS AIRSPEED INDICATED 80 KNOTS. FIRST OFFICERS INDICATED 0. AIRCRAFT RETURNED TO BLOCKS CAPTAIN IND 100 KNOTS, F/O'S IND 0. CHECKED BRAKE TEMPERATURE FOR POSSIBLE HIGH ENERGY STOP. INDICATED NORMAL RANGE, NO FURTHER INSPECTION REQUIRED PER MM 5-5-10. REINSTALLED BOTH INDICATORS AFTER CHECKED HOSES AND CONNECTIONS. PERFORMED PITOT-STATIC TEST WITH TESTER, AIR DATA TEST SET. SYSTEM LEAK CHECKED NORMA, INSPECTION NORMAL AS PER MM 34-11-00 AND 34-13-05. REF TO DMI NR M04-069/ F/O'S MACH IND HAS FLA IN VIEW. (M) 2L74 4F RTA20WE 20041102000782004110200078EU 2004 11 2 2004F00423 120040826A5610NP1588013 WINDOW AEROSPATR72 ATR72212 8680945EU COCKPIT CRACKED A TRBABH EMER. DESCENT DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO21440AM3747 440 DURING CRUISING, THE CAPTAIN WINDSHIELD CRACKED. REPLACED CAPTAIN WINDSHIELD ASEMBLY. (M) 2H72 4T RTA53EU 20041102000802004110200080NE 2004 11 2 2004F00424 220040506A7200 ENGINE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR 1 STALLED A CEDAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 SW05140CA 140 251048A ON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M) 2L72 4J4 J A10CE 1E16 20041102000822004110200082NM 2004 11 2 2004F00425 120040825A571165B010284 SPAR BOEING747 747206B 1384856NM RT WING CRACKED A Q2SAK NONE O OTHER ININSP/MAINT 1 NE03746SA 21111 DURING REPLACEMENT OF THE WING REAR SPAR LOEWR CHORD SPLICE PLATE FITTING H-11 BOLTS AS P[ER BOEING SB 747-57A2309, CRACK WAS FOUND COMMON TO THE RIGHT WIND REAR SPAR LOWER CHORD ONLY AT FASTENER CODE 'C' LOCATION. HOLE 'C' REAMED TO 1.316 INCH DIAMETER. NDT INSPECTIONS CONFIRMED NO MORE DAMAGE EXISTS. FREEZE PLUG FABRICATED AND INSTALLED PER SRM 51-10-08. THIS AIRCRAFT BECOMES UNAIRWORTHY 12 MONTHS FROM THE DATE OF THE 8110-3 APPROVAL DOCUMENT, UNLESS A NEW FAA FORM 8110-3 IS ISSUED PRIOR TO THAT TIME FINDING COMPLIANCE TO FAR 25.571. (M) 2L74 4F RTA20WE 20041102000832004110200083EU 2004 11 2 2004F00426 120040820A275146797648010 INDICATOR AEROSPATR72 ATR72212 8680945EU TE FLAPS FAILED A TRBAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO21348AE 349 ON APPROACH WHEN SELECTED 30 DEGREES OF FLAPS IT STAYED IN THE UP POSITION. REPLACED FLAP INDICATOR. (M) 2H72 4T RTA53EU 20041102000842004110200084NM 2004 11 2 2004F00427 120040601A561069B10028101 WINDSHIELD BOEING747 747228F 1384895NM COCKPIT CRACKED A Q2SAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 NE03751SA 22678 CAPTAINS NR 1 WINDOW STARTED ARCING FIVE HOURS INTO FLIGHT THEN CRACKED SHORTLY AFTER. COMPLIED WITH EMERGENCY/ABNORMAL CHECKLIST IAW QRH. REMOVED AND REPLACED CAPTAINS NR 1 L1 WINDOW IAW AMM 56-11-01. (M) 2L74 4F A20WE 20041102000852004110200085NM 2004 11 2 AMTA200401268 120041010A1420 CONNECTOR BOEING757 75733N 1384931NM LT ENGINE DISCONNECTED A AMTAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL11552TZ 32586 LEFT GEN OFF DISPLAYED GEN OFF LIGHT ILLUMINATED CONDITION RETURNED TO NORMAL AFTER GENERATOR SWITCH RESET. REMOVED AND REPLACED LT ENGINE PYLON DISCONNECT CONNECTOR D1014P. LEFT IDG CHECKS OF REF AWM 20-63-00. (M) 2L72 4F RTA2NM 20041102000902004110200090NM 2004 11 2 DL76G040990 120041025A2780834503 SENSOR BOEING767 7673P6 1385105NM GE CF6 CF680C2* GL RT WING SLAT UNSERVICEABLE A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO271501P 24983 LE SLAT ASYM EICAS MSG AND LEADING EDGE CAUTION LIGHT WHEN FLAPS WERE SELECTED FROM 1 TO UP AFTER TO. REMOVED AND REPLACED RT NBR 12 OB SLAT PROX SWITCH S294 IAW MM OPS CH GOOD ETOPS CATEGORY (B) DIVERSION OR TURNBACK 2L72 4F4 FRTA1NM E23EA 20041102000922004110200092EU 2004 11 2 DHL2004363535 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3871, FR. 30 - FR. 38.2 LBL 18 SEAT TRACK FLANGES CORRODED OUT OF LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 30- FR 38.2 AT LBL 18 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR 26.5 - FR 38.2 AT LBL 18 IAW SRM 53-10-10 / 51-10-40. TREATED AND PRIME AND POLYWHITE IAW SRM 51-40-10 AND A-300 SRM 51-40-12. MATERIAL USED FOR SEAT TRACK, 60-22457, PO 24302234. 2L72 4F4 FRTA35EU E23EA 20041102000972004110200097SO 2004 11 2 LR7A04111 120041001A5541 ANGLE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5511, FOUND RUDDER TRIM ACTUATOR MOUNT ASSY LT AND RT MAIN ATTACH ANGLES CRACKED AND WORN AT FS 1129, VSS 98, LBL 2 AND RBL 2. REPAIRED IAWEA 382-55-04-069. NR 0297. 2H74 4T4 T A1SO E282 20041102000992004110200099SO 2004 11 2 LR7A04113 120041001A53433723323 BEAM LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323, FOUND LT MLG FS 557 UPPER BOW BEAM OUTER TEE CAP CRACKED AT WL 232, LBL 67. REPLACED TEE CAP IAW DWG 372332 AND SRM SMP 583 51-70. NR 0384. 2H74 4T4 T A1SO E282 20041102001032004110200103WP 2004 11 2 NACA20040051 120040617A5311 FRAME DOUG DC6 DC6A 3021706WP PWA R2800 R2800* 52026NE FUSELAGE CRACKED A NACAK NONE O OTHER ININSP/MAINT 1 AL0399330 43576 RT FUSELAGE CIRCUMFERENTIAL AT STA. R460 CRACKED APPROXIMATELY 3 INCHES ABOVE FLOOR LEVEL. REPLACED ANGLE WITH THE SAME TYPE AND MATERIAL .090 7075 T6. FABRICATED AND INSTALLED REPAIR (L) AND STRAP WITH REFERENCE TO DOHM FIG. 11-52 AND FIG. 12-10 SHEET 2. 2L74 4R4 R 6A3 5E8 20041102001052004110200105 2004 11 2 SWIA200413996 420041020A22166225734002 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER PEDAL BINDING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07216SW1361 1361 120285 LT RUDDER PEDAL BINDING AT MID AND BOTTOM TRAVEL. REPLACED RUDDER SERVO MOTOR. OPERATIONAL TEST GOOD. 2L72 4T4 TRTA31SO E20NE 20041102001072004110200107EA 2004 11 2 SWIA200413998 120041018A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07907SW 7540 OVERHEAD EMERGENY LIGHT INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AS NEEDED, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041102001092004110200109EA 2004 11 2 SWIA200413999 120041020A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07439SW9187 9187 7578 IB AND OB GROUND SPOILER FAULT MESSAGE SPOILERON MESSAGE. REPLACED SECU, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041102001112004110200111EA 2004 11 2 SWIA200414001 120041022A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB TRIM MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07463SW3514 3514 7820 INTERMITTENT STAB TRIM CH 1 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. PN 4062-3 SN OFF 1102 2L72 4F4 FRTA21EA E15NE 20041102001122004110200112SO 2004 11 2 LR7A04194 120041028A5714 SPAR LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CENTER WING CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 653 4590 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5302, FOUND CENTER WING FRONT SPAR WEB CRACKED AT FS 517, CWS 20.5R, WL 273. REPAIRED IAW EA 382-53-04-088. NR 0017. 2H74 4T4 T A1SO E282 20041102001202004110200120NM 2004 11 2 DL76S040997 120041028A2910 HOUSING BOEING767 767332 1382001NM GE CF680 CF680A2 NE SPOILER ACTUATORFRACTURED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27133DN 24982 CENTER HYD SYSTEM FAILURE ON TAKEOFF. QUANTITY ZERO RETURNED. FOUND NBR 6 SPOILER ACTUATOR HOUSING CRACKED. REPLACED NR 6 SPOILER PCA IAW MM 27-61-02. 2L72 4F4 FRTA1NM E13NE 20041102001232004110200123EU 2004 11 2 04FDEA02996 120041027A7830 THRUST REVERSER AIRBUS310 A310 EU PWA JT9 JT9D7R4E1 52054NE NR 1 INOPERATIVE A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25447FE 251 PDIS 447 78-30 0007243 27OCT04 MCI OPEN U NR 1 REVERSER UNLOCK LITE ON T/O. REJECTED T/O AT 70 KNOTS. MEL 27OCT04 05:03 MCI U ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 06NOV04 (MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOPERATIVE, THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.) MOCC CONTROL NR 212950, EXP DATE 11/06/04. C/0212950 ENT BY: 042537 RPT BY: 042537. 2L72 4F4 FRTA35EU E3NE 20041102001252004110200125GL 2004 11 2 ALG2004F00060 220041010A720023005290 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 MAKING METAL E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031547N 760088 CAE890287S AFTER TAKEOFF, NR 1 ENGINE CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. THE MECHANIC REMOVED, CLEANED, AND INSPECTED NR ENGINE CHIP PLUGS. SMALL HAIR LIKE SILVER WAS DISCOVERED. UPON CLEANING THE CHIP PLUGS, COMPLIED WITH GROUND RUN AND LEAK CHECK, NO DISCREPANCY WAS NOTED, AC RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20041102001282004110200128SO 2004 11 2 MASA200400039 120040120A2120 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07826MJ 145214 ASH 2754. XNA. LIGHT SMOKE IN THE CABIN, SMELLED LIKE HOT DUCTING TO CREW. MECHANIC OPS CHECKED AIR CONDITIONING SYSTEMS. NO DEFECTS NOTED. SMOKE DISSIPATED. NO FURTHER PROBLEMS. NO PARTS USED. 2L72 4T4 FRTT00011ATTE6CH 20041103000012004110300001NM 2004 11 3 04FDEA02995 120041026A2422 WARNING LIGHT DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE COCKPIT ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25620FE 48791 ON TAKEOFF, POSSIBLE LIGHTING STRIKE. SHORTLY AFTER RECEIVED (EPGS FAULT) AND (EMERG PWR ON) ALERTS. ALL BUSSES POWERED, ALL GENERATORS OUTPUT NORMAL. REFD QRH AT SAME TIME CAPT'S NO DEFECTS DISPLAYED (MAP FAIL ALERT. SELECTED CAPT ON FMS2 AND CONTINUED ON (OPERATION WITH A SINGLE FMS) IAW QRH. RECEIVED BUSS L EMERGY AC OFF) ALERT SELECTED (EMERG PWR OFF) AND REGAINED FLIGHT DISPLAY DATA. DEVERTED TO KPDX AND DECLARED AN EMERGENCY PERFORMED LIGHTING STRIKE INSPECTION IAW MM 05-53-01-6. NO DEFECTS NOTED. REMOVED AND REPLACED LT EMERGENCY SENCE RELAY AND RESET EPGS FAULTS IAW 24-20-00.FIG 101 AND PERFORMED RTS OF EPCU. TEST PASSED A/C OK FOR SERVICE. 2L73 4F4 FRTA22WE E24NE 20041103000022004110300002WP 2004 11 3 0401939153 120041026A2750 PULLEY DOUG DC9 DC914 3022034WP PWA JT8 JT8D9A 52048NE TE FLAPS WORN A NWAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL018912E 45829 ON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND THE RT FLAP INDICATOR WAS AT 30 DEGREES. CREW EXECUTED MISSED APPROACH PROCEDURES TO ALLOW TIME FOR COM PROCEDURE COMPLIANCE. FLIGHT EVENTUALLY MADE A SAFE UNEVENTFUL LANDING WITH 20 DEGREES OF FLAPS AT MSP. MAINTENANCE FOUND LOW CABLE TENSION ON THE FLAP BUS CABLES, A WORN PULLEY, AND A WORN CABLE. PULLEY AND CABLE WERE REPLACED AND CABLES WERE RETENTION AND RIGGED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 20041103000032004110300003SO 2004 11 3 RAIA00410022 120041026A521014539935401 CABLE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL PAX DOOR FROZEN A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03806HK 145112 3606- ALB PASSENGER DOOR WILL NOT CLOSE. MAINTENANCE INSPECTED MAIN PASSENGER DOOR, FOUND FWD AND AFT LOCK BOX CABLE FROZEN. REMOVED AND REPLACED CABLES. 2L72 4F4 FRTT00011ATTE6CH 20041103000042004110300004WP 2004 11 3 SE28102004 120041020A335020131A CHARGER DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE EMERGENCY LIGHT FAILED A A4JAK NONE L NO TEST ININSP/MAINT 1 SO35933JK 48159 DURING B-CHECK MAINTENANCE FOUND THE AFT HALF OF THE EMERGENCY PATH TRACK WOULD NOT COME ON. REMOVED AND REPLACED EMERGENCY PATH LIGHTING BATTERY AND BATTERY CHARGER IAW MM 33-53-1. OPS CHECKS GOOD. 2L72 4F4 F A6WE E2EA 20041103000072004110300007 2004 11 3 SWIA200414015 420041024A3418 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AOA VANE MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07416SW 7089 CAPTAINS 1.27 STALL GREEN LINE SHOWS 280 KTS AT FLIGHT LEVEL 290 WHEN CO-PILOT'S IS NOT EVEN VISIBLE. NO STALL TAPE INDICATION. REMOVED AND REPLACED BOTH LT AND RT AOA VANES IAW MM 27-35-05. OPERATIONAL CHECK GOOD IAW AMM 27-35-01. PN 45150340 SN OFF 338 AND SN OFF 332. 2L72 4F4 FRTA21EA E15NE 20041103000082004110300008EA 2004 11 3 SWIA200414016 120041020A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERON INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07941SW 7750 AILERON TRIM INOPERATIVE. REMOVED AND REPLACED AILERON TRIM PANEL IN REFERENCE WITH MM 27-00-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041103000102004110300010EA 2004 11 3 SWIA200414017 120041025A2752854D10020 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAP FAILED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07446SW6272 6272 7666 FLAPS FAIL CAUTION MESSAGE ON APPROACH. FLAPS FAILED AT ZERO. REMOVED AND REPLACED NR 4 FLAP ACTUATOR IAW MM 27-53-01, 27-53-05. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041103000112004110300011NM 2004 11 3 AWXA200401160 120041026A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU SEAT ROW 23 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA16WE E21EU 20041103000122004110300012EU 2004 11 3 AWXA200401161 120041026A2560P4010021 BATTERY AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FLASHLIGHT DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28638AW 455 EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE AFT GALLEY EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20041103000132004110300013NM 2004 11 3 AWXA200401162 120041002A53206562175104 FLOOR SUPPORT BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER CHORD OF FLOOR SUPPORT AT BS 298, RBL 31, WL 208. MAINTENANCE REMOVED FLOOR SUPPORT UPPER CHORD FROM BS 294 TO BS 312 AT RBL 31; FABRICATED A NEW REPLACEMENT SECTION OF CHORD IAW DWG 65-62175; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 4, 8. 2L72 4F4 FRTA16WE E2GL 20041103000152004110300015NM 2004 11 3 AWXA200401164 120041002A53426545805121 ANGLE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, LBL 4, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM UPPER TEE CAP AT BS 294, FROM LBL 25 TO RBL 55; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW SRM 53-10-51, FIG. 205. 2L72 4F4 FRTA16WE E2GL 20041103000172004110300017SO 2004 11 3 LR7A04115 120041001A53203393943 FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5324 FOUND RMLG FS 617 AFT FAIRING TENSION TIE UPPER FITTING CRACKED AT WL 158, RBL 68. REPLACED FITTING IAW DWG 339394 AND SRM SMP 583 51-70. NR 0413. 2H74 4T4 T A1SO E282 20041103000192004110300019SO 2004 11 3 LR7A04117 120041001A5312 PRESSURE PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5316 FOUND FS 477 RT UPPER PRESSURE PANEL AFT SIDE WEB RADIUS CRACKED AT WL 272, RBL 29-35. REPAIRED AND REINFORCED IAW SB 382 53-50 R1 AND DWG SK382-53-167. NR 0416. 2H74 4T4 T A1SO E282 20041103000232004110300023SO 2004 11 3 LR7A04121 120041001A5320 ANGLE LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LOWER LBL 60 CHINE ANGLE CRACKED AT FS 617 - 637. REPAIRED IAW SRM SMP 583 53-40-26. NR 0481. 2H74 4T4 T A1SO E282 20041103000262004110300026SO 2004 11 3 LR7A04124 120041001A5311 FRAME LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE MISLOCATED A LR7AK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5313 FOUND FUSELAGE FRAME MIS-DRILLED HOLE DAMAGE AT FS 250, WL 158, LBL 70. REPAIRED IAW LAC MEA 382-53-04-074. NR 0440. 2H74 4T4 T A1SO E282 20041103000372004110300037NE 2004 11 3 04056 220041020A7200 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7A 52054NE NR 1 SEPARATED A KCSAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 GL23709CK 20247 662253 NR 1 ENGINE SEPARATED FROM AIRCRAFT ON CLIMBOUT AT FL180. 2L74 4F4 F A20WE E20EA 20041103000442004110300044NM 2004 11 3 AWXA200401165 120041002A5313BAC1498155 STRINGER BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK CORROSION WAS FOUND ON IB SIDE OF STRINGER 27 RT, BETWEEN BS 986 AND BS 1006. MAINTENANCE CUTOUT DAMAGE ON STRINGER 27 RT FROM BS 986 TO BS 1006; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND A SPLICE REPAIR; INSTALLED REPAIR PARTS IAW SRM 53-00-03, FIG. 201. 2L72 4F4 FRTA16WE E2GL 20041103000462004110300046NM 2004 11 3 AWXA200401167 120041001A5320653103501 ANGLE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN FORWARD SCUFF PLATE ATTACH ANGLE AT L-1 DOOR ENTRYWAY BS 298, STR 17 LT. MAINTENANCE REMOVED CRACK IN FORWARD SCUFF PLATE ATTACH ANGLE AT L-1 DOOR ENTRYWAY BS 298, STR 17 LT. PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. TREATED AND PRIMED AREA, REPAIR ACCOMPLISHED IAW SRM 53-10-15, FIG. 101. 2L72 4F4 FRTA16WE E2GL 20041103000482004110300048NM 2004 11 3 AWXA200401169 120041026A531065353642 SHEAR TIE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN FRAME FOOT CLIP AT BS 986, STR 25 RT. MAINTENANCE REMOVED AND REPLACED FRAME FOOT CLIP AT BS 986, STR 25 RT IAW SRM 51-40-02, FIG. 3, 4, 6, 7, AND 8. 2L72 4F4 FRTA16WE E2GL 20041103000512004110300051NM 2004 11 3 AWXA200401171 120041003A5310654656445 SHEAR TIE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 987, BETWEEN STR 26 RT AND STR 27 RT IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 987, BETWEEN STR 26 RT AND STR 27 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE IAW DWG 65-46564-45; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 3, 4, 6, 7, AND 8. 2L72 4F4 FRTA16WE E2GL 20041103000552004110300055WP 2004 11 3 AALA20041070 120041025A3350 CHARGER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21424AA 49336 EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES ARE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20041103000562004110300056EU 2004 11 3 WRNA200400014 120041007A3230C23005302 DAMPENER AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE RT PITCH INOPERATIVE A WRNAO OTHER J WARNING INDICATION CLCLIMB 1 SO05505TA 271 AFTER TAKE OFF UNABLE TO MOVE GEAR HANDLE TO UP POSITION. FOLLOWED ABNORMAL PROCEDURES. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED RT PITCH DAMPENER IAW 32-11-15. AIRCRAFT JACKED AND GEAR SWING COMPLIED WITH OP'S CHECK GOOD IAW 7-11-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA35EU E23EA 20041103000582004110300058NM 2004 11 3 04FDEA02973 120041022A5754 FITTING DOUG MD11 MD11F 3023600NM GE CF6 CF680C2* GL ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING IB FLAP VANE, OB TEE FITTING BORE HOLES HAVE CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81570. 2L73 4F4 FRTA22WE E23EA 20041103000592004110300059NM 2004 11 3 04FDEA02980 120041022A5311 FRAME BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25461FE 22548 WHILE COMPLING WITH EA 7-5310-64946 A F/U FOUND FRAME REPAIR NOT TO BE DONE IAW SRM AT BS 680 STR 24R NEED TO COMPLY WITH EA 7-5310-55392 ** SD ** COMING REPAIRED IAW EA 7-5310-55392. 2L73 4F4 FRTA3WE E2EA 20041103000602004110300060CE 2004 11 3 65858 120041015A79311013890235 TRANSDUCER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE OIL PRESSURE FLUCTUATES A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07171ZV UE171 RT OIL PRESSURE WAS FLUCTUATING FROM 60-95 PSI AIRCRAFT DIVERTED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED OIL PRESSURE TRANSDUCER AND FILTER. P/N 101-389023-5 S/N 7034-5-380 2L72 4T4 TRTA24CE E26NE 20041103000632004110300063NE 2004 11 3 65837 220041014A7200PT6A67DGG GAS GENERATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE ENGINE MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE07218YV UE218 DURING CRUISE, OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED, OIL PRESSURE GAUGE INDICATED 50 AND SLOWLY DROPPING, CREW SECURED LT ENGINE AND DECLARED AND EMERGENCY AND LANDED. REMOVED AND REPLACED LT GAS GENERATOR, POWER SECTION AND PROPELLER, RIGGED ENGINE, PERFORMED GROUND RUN NO LEAKS NOTED. P/N PT6A67DGG S/N 114371. 2L72 4T4 TRTA24CE E26NE 20041103000642004110300064EU 2004 11 3 04FDEA02958 120041020A5610 WINDSHIELD AIRBUS330 A300* EU GE CF6 CF680C2A5 NE COCKPIT FAILED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25659FE 757 56-10 0007810 20OCT04 MEM CLOSE L/P: 00949119 CAPT FWD WINDSHIELD OUTER PANEL SHATTERED AT FL 310 REMOVED CAPTAINS WINDSHIELD REF A 300-600 MM 56-11-1 1-4. R/I IAW MM 56-11-11-4 MFG NP175201-1 SRL 96113H6246 ON MFG NP175201-5 SRL 04278H7866 AIRBUS 56-11-11-4. OPS CKD GOOD IAW MOCC REMOVED AND REPLACED LT TEMP CONTROLLER AND LT HAND WINDOW PROTECTION UNIT IN REF TO MM 30-42-51-4 OPS CKD GOOD. 2L72 4F4 FRTA26NM E13NE 20041029000152004102900015NM 2004 10 29 2004UALA00480 120040514A5100 UNKNOWN BOEING757 757222 1384956NM PWA 2037 PW2037 NE UNKNOWN UNKNOWN A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29545UA 25323 DURING CLIMBOUT COULD NOT MAINTAIN NORMAL AIRSPEED AND PITCH ATTITUDE. FLIGHT LEVEL 300-340 MAX EPR 1.45. FLIGHT DATA RECORDER INDICATED AIRCRAFT WAS OPERATING WITHIN THE NORMAL FLIGHT ENVELOPE PARAMETERS. 2L72 4F4 FRTA2NM E17NE 20041029000162004102900016 2004 10 29 DLM90040981 420041018A2330RDAV980501 MONITOR DOUG MD90 MD9030 3023690NM CABIN ROW 13AB ODOR A DALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27903DA 53383 VISIBLE SMOKE COMING OUT OF OVHD PNL 13AB WITH ACRID SMELL. SUSPECT VIDEO MONITOR OR SEAT BELT NO SMOKING LIGHT. REPLACED INOP, ACRID SMELLING VIDEO MONITOR AT 13 AB PER MM. PERFORMED OPS TEST OF ENTERTAINMENT SYS, OPS CHECK NORMAL. SEAT BELT NO SMOKING LIGHTS CHECK NORMAL. 2L72 4F RTA6WE 20041029000172004102900017NM 2004 10 29 DL757040982 120040118A3320059341 BALLAST BOEING757 757232 1384965NM MIDCBN/ROW 31DEFBURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27655DL 24395 ACRID SMELL MID CABIN FOUND SIDEWALL LIGHT BALLAST AT ROW 31DEF BURNT, INOP. REPLACED BALLAST LIGHTS, OPS NORMAL. 2L72 4F RTA2NM 20041029000182004102900018NM 2004 10 29 DL76L040983 120041018A2910NAS161208A PACKING BOEING767 767332 1382001NM RIGHT PYLON DAMAGED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27184DN UNK 27111 RIGHT SYSTEM HYDRAULIC QUANTITY LOW. FOUND DELTA P PACKING BLOWN OUT ON HYD PRESSURE MODULE IN RT ENG STRUT. REPLACED DELTA P AND PACKINGS PER AMM, LEAK CHECK OK. 2L72 4F RTA1NM 20041029000192004102900019NM 2004 10 29 DLM88040984 120041017A492038005041 TURBINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D NE APU FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27969DL13779 P80123 53172 P80123 SMOKE ODOR IN THE CABIN. REPLACED APU FOR LEAKAGE. 2L72 4F4 FRTA6WE E2EA 20041029000202004102900020NM 2004 10 29 2004UALA00784 120040825A3350BPS73 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EMERGENCY LIGHTS INOP LT OW 2 EA AFT. REPLACED POWER SUPPLY M7919 AND RELAMPED. 2L74 4F4 FRTA20WE E24NE 20041029000212004102900021NM 2004 10 29 DLM88040970 120041015A499038761864 SWITCH DOUG MD88 MD88 3023688NM APU LEAKING A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27969DL 53172 ON T/O FLT ATTENDANT REPORTED SMOKE IN THE CABIN AND LAVATORY SMOKE DETECTORS GOING OFF, ATB BACK TO JAX. FOUND APU INLET CONTAMINATED WITH APU OIL. PERFORMED OPN 5088 AND OPN 5089 DUCT BURNOUT. OIL LEAK FROM APU LOW OIL PRESSURE SWITCH BODY. DEACTVATED APU AND FORWARD TO MCO AND PLACARD. 2L72 4F RTA6WE 20041029000222004102900022NM 2004 10 29 DL75K040971 120041015A3243326002025 BRAKE ASSY BOEING757 757232 1384965NM NR 5 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO2767171 30839 FOUND BY MTC NR 5 BRAKE DAMAGE STATOR REVOLVING WITH ROTOR AND IDICATOR PIN DAMAGED. REPLACED NR 5 BRAKE ASSY AND NR 5 MAIN WHEEL ASSY. 2L72 4F RTA2NM 20041029000232004102900023NM 2004 10 29 DL76S040972 120041015A335020121 CHARGER BOEING767 767332 1382001NM ROW 35 INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27126DL 24076 EMERGENCY LIGHTS INOP ROW 35 AFT BOTH SIDES. REPLACED M9010 BATTERY CHARGER ASSY. 2L72 4F RTA1NM 20041029000252004102900025NM 2004 10 29 2004UALA00786 120040826A2120 SMOKE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DETECTED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29308UA 23669 ACRID SMOKE IN THE CABIN. CHECKED ALL CABIN LIGHTS AND ALL GALLEY EQUIPMENT, RAN BOTH PACKS, RECIRC FAN AND ENG BLEEDS, CHILLERS AND OVENS. VISUAL CHECK FOR HYD AND OIL LEAKS. PERFORMED A VERIFICATION FLIGHT. ALL SYSTEM FOUND NORMAL. SMOKE ODOR COULD NOT BE DUPLICATED. 2L72 4F4 FRTA16WE E2GL 20041029000272004102900027NM 2004 10 29 DL76L040961 120041011A2120 ODOR BOEING767 767332 1382001NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27187DN 27582 ELEC ODOR REPORTED AFTER T/O. ODOR SEEMED TO BE COMING FROM MID GALLEY NEAR ENTERTAINMENT SYSTEM. RAN ENGINES, PACKS, AND SYSTEMS. UNABLE TO DUPLICATE. 2L72 4F RTA1NM 20041029000292004102900029NM 2004 10 29 2004UALA00938 120041013A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE UNKNOWN A UALAK NONE O OTHER ININSP/MAINT 1 WP29902UA 25002 BLEND OUT ON RT FUSE SKIN AT STA 410 STR 26R IS BEYOND LIMITS. INSTALLED DOUBLER AND FILLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20041029000302004102900030NM 2004 10 29 2004UALA00939 120041014A2910 HYDRAULIC SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RIGHT LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29663UA 27160 FLIGHT DIVERTED DUE TO RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. REPLACED RIGHT SYSTEM EDP. NO FURTHER REPORTS NEXT 20 AC CYCLES. 2L72 4F4 FRTA1NM E24NE 20041029000312004102900031NM 2004 10 29 2004UALA00895 120041003A335060243 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29514UA 24839 EEL LIGHTS INOP FROM ROW 31 TO AFT LAV. REPLACED POWER STRIP. 2L72 4F4 FRTA2NM E17NE 20041029000332004102900033NM 2004 10 29 2004UALA00926 120041008A2420 IDG BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT ENGINE VIBRATION A UALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 WP29657UA 27112 DIVERTED WHEN LEFT ENGINE INDICATED IDLE FUEL FLOW AND IDLE THRUST. SHOP FOUND LOG PISTON FAILURE ON REMOVED LT IDG. CORRESPONDENCE BETWEEN COMPONENTS ENGINEERING, POWER PLANT ENGINEERING, SUNDSTRAND, AND PWA, INDICATES THERE IS A POTENTIAL ANOMALY FOR A WORN IDG TO INTRODUCE NOISE INTO THE N2 SPEED TRANSDUCER THROUGH THE ENGINE GEARBOX DUE TO UNSTEADY LOADING BY THE IDG. IT IS SURMISED THAT AN UNSTEADY N2 SIGNAL TO THE ENGINE FADEC MAY ACCOUNT FOR THE INABILITY OF THE ENGINE TO ACCELERATE. 2L72 4F4 FRTA1NM E24NE 20041029000342004102900034EU 2004 10 29 2004UALA00927 120041011A5610 WINDSHIELD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29429UA 539 FIRST OFFICERS WINDSHIELD ARCING AND CRACKING. MOISTURE INGRESSION THROUGH A SEAL. WINDSHIELD REPLACED. 2L72 4F4 FRTA28NM E40NE 20041029000382004102900038NM 2004 10 29 2004UALA00953 120041017A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME DENTED STA 1440, BETWEEN STR 25L AND 28L. *S/D* MAJOR REPAIR ACCOMPLISHED. TYPICAL DAMAGE TO THE AFT PIT FRAMES DUE TO CARGO LOADING. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041029000402004102900040NM 2004 10 29 2004UALA00954 120041017A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 FWD PIT FRAME DENTED AT STA 580 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. TYPICAL DAMAGE TO THE FORWARD PIT FRAMES DUE TO CARGO LOADING. CUT OUT DAMAGE & INSTALLED NESTED ANGLE REPAIR OUTSIDE FRAME SECTION. 2L72 4F4 FRTA2NM E17NE 20041029000442004102900044NM 2004 10 29 SWAA043112 120041026A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 3L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041101000142004110100014NM 2004 11 1 DLM88040973 120041016A29107952170553 LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE HYD SYSTEM LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27913DE 49956 726835 LEFT HYD QTY DROPPED TO 3 WITH AMBER LIGHT ON. GOOD PRESS OF 3000 QTY, NOW MOVING BETWEEN 3 AND 16 QTS. AMBER LIGHT GOING ON AND OFF WITHOUT REGARD TO QTY SHOWING. FOUND LEAKING HYD RETURN LINE ON LEFT REV CONTROL VALVE. TIGHTENED LINE AND LEAK CK'ED GOOD. CLEANED APU INLET AREA, RAN APU AND PACKS. NO FOUL ODOR NOTED IN CABIN. 2L72 4F4 FRTA6WE E9NE 20041101000152004110100015EA 2004 11 1 COMA0460571 120041012A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01797CA 7344 FLIGHT 5370 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20041101000182004110100018NM 2004 11 1 2004UALA00821 120041002A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 FLOORBEAM T-CAP AT BS 365 RBL 0 TO RBL 64 R CORRODED SEVERAL LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000242004110100024NE 2004 11 1 2004UALA00835 220040908A73208063215 MEC BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 MALFUNCTIONED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29375UA348994663 24640 856186 RETURNED TO ORD WITH NR 2 ENGINE SURGE. REPLACED MAIN ENGINE CONTROL (MEC) AND ENGINE RAN NORMAL. RIGGED THE VSV AND VVB AND TRIMMED. 2L72 4F4 FRTA16WE E2GL 20041101000332004110100033EA 2004 11 1 COMA0470072 120041002A26136007300 SENSOR CNDAIRCL600 CL6002C10 1390015EA LT MLG BRAKE MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01658CA 10148 FLIGHT 5519 BRAKE OVERHEAT WARNING DURING T/O. REPLACED THE LT OUTBD BRAKE TEMP SENSOR. 2L72 4F RTA21EA 20041101000402004110100040NM 2004 11 1 2004UALA00800 120040817A5320 WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 FLIGHT DECK FLOOR WEB CRACKED ON VERTICAL LEG AT FIRST FASTENER AFT OF STA 199 BULKHEAD ON RT SIDE OF AIRCRAFT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB. 2L72 4F4 FRTA2NM E17NE 20041101000432004110100043NM 2004 11 1 2004UALA00803 120040807A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 MAIN CABIN AT STA 365, RBL 45 TO RBL 60, FLOORBEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000482004110100048EA 2004 11 1 COMA0460577 120041020A5320601R38303253 CHANNEL CNDAIRCL600 CL6002B19 1900309EA SVCE DOOR CUTOUTCORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01940CA24672 7048 FLIGHT UPON COMPLIANCE OF COMAIR TASK CRJ-2-841010, THE SERVICE DOOR CUTOUT LOWER SILL CHANNEL WAS FOUND CORRODED. THE CHANNEL WAS REMOVED AND REPLACED WITH A NEW PART USING THE CRJ SRM STANDARD PRACTICES. 2L72 4F RTA21EA 20041101000592004110100059EA 2004 11 1 COMA0460569 120041001A2913887055 PUMP CNDAIRCL600 CL6002B19 1900309EA NR 2 HYD SYSTEM MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01979CA2385 7159 FLIGHT 5361 NR 2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION. REPLACED THE RT EDP. 2L72 4F RTA21EA 20041101000612004110100061SO 2004 11 1 C2XA04BT103 120041004A335020131A BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27199663074 3074 145131 EWR- CO2899, DURING SERVICE CHECK MAINTENANCE FOUND THE AFT EMERGENCY LIGHT FAILING TO LIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK NR 4 IAW EMB 145 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041101000762004110100076NM 2004 11 1 2004UALA00900 120041003A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29570UA 26678 AFT PIT STA 1440 FRAME LT SIDE AT STR 27L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000802004110100080NM 2004 11 1 2004UALA00916 120041006A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 AFT PIT STA 1420 ABOVE STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED PIECE. FABRICATED AND INSTALLED SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000882004110100088NM 2004 11 1 SWAA043108 120041025A5330655298873 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT LOWER CORNER SKIN CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041101000912004110100091NM 2004 11 1 SWAA043118 120041026A53106517685 DOOR FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME NEAR 4TH STOP FITTING FROM BOTTOM, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041101000922004110100092NM 2004 11 1 SWAA043119 120041026A533065458001133 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR LOWER AFT CORNER SKIN CUTOUT CRACKED. REPAIRED DOOR CUTOUT SKIN PER EA. 2L72 4F RTA16WE 20041101000952004110100095 2004 11 1 2004UALA00839 420040911A34256227998003 EADI BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT BURNED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29529UA45574 25019 ELECTRICAL ODOR IN FLIGHT DECK AND EADI BLANKING OUT. REPLACED EADI. REMOVED UNIT HAD CAPACITOR A3C31 FOUND TO BE BURNED & CRACKED. SHOP REPLACED CAPACITOR AND BURNED-IN CRT. 2L72 4F4 FRTA2NM E17NE 20041101000972004110100097NM 2004 11 1 2004UALA00841 120040910A2421 CONTROL UNIT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE ELECTRICAL BUSS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29658UA 27113 ELECTRICAL UTILITY BUSS PROBLEM. LT AND RT UTILITY BUSS TRIPPED ABOUT 20 MINUTES OUT. UNABLE TO RESET AND THE AIRCRAFT RETURNED TO IAD. RELAYS K148 (SYS 1 AIR/GND) AND K10109 (UTIL/GALLEY PWR FLT RESET) WERE REPLACED AS A PRECAUTION. M116 BUSS POWER CONTROL UNIT (BPCU) ALSO REPLACED. THE DIRECT CAUSE OF THEN ANOMALY IS UNKNOWN; HOWEVER, IT HAS NOT RECURRED SINCE REPLACEMENT OF COMPONENTS. 2L72 4F4 FRTA1NM E24NE 20041101001022004110100102NM 2004 11 1 DLM88040965 120041013A2497 WIRE DOUG MD88 MD88 3023688NM F/C ELECT OUTLETBURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27915DE 53420 F/C ELECT 110 OUTLET WIRING BURNED HOLES IN FUSELAGE. REPLACED OUTLET, EXECUTED FLEET CAMPAIGN. 2L72 4F RTA6WE 20041101001162004110100116NM 2004 11 1 DHL2004752006 120040804A3260656021132 ACCESSORY UNIT BOEING727 727223 1384074NM RT MLG MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01752DH 22466 AFTER GEAR RETRACTION, RIGHT MAIN LANDING GEAR UNSAFE LIGHT AND DOOR LIGHT REMAIN ILLUMINATED. PERFORM ABNORMAL PROC ON 6.2.70. LANDING GEAR EXTENDED NORMALLY. REDISPATCHED TO KDAL AT 0811 PER JRM. REMOVED & REPLACED LGAU & OPS CK GOOD PER B727 MM 32-09-121, AS A PRECAUTIONARY MEASURE, PERFORMED LANDING GEAR EXT, RETRACT TEST & OPS CK GOOD IAW B727 MM 32-32-00. 2L73 4F A3WE 20041101001172004110100117EU 2004 11 1 DHL2004364016 120040824A5311 FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 IN CONJUCTION WITH DHL2004364015, REMOVE & REPLACE DOUBLER AT FRA, 26 & LONGERON 43 LEFT. REMOVED FLOOR PANEL, SIDE WALL PANEL TO GAIN ACCESS TO REPAIR AT STR 43L, FR 26. REMOVED REPAIR DOUBLER AT STR 43L, FR 26, CUT-OUT UPPER SKIN AND BONDED DOUBLER IN AREA. TRIMMED OUT DISBONDED LOWER SKIN DOUBLER. PERFORMED DEBOND CHECK AT LAP SEAM STR 43L FR 26, NO DEBOND NOTED. ACCOMPLISHED HFEC INSP FUSELAGE SKIN CUT OUT AND FASTENERS HOLES. NO CRACKS NOTED. ACCOMPLISHED ULTRASONIC THICKNESS TEST ON FOUR SKIN PANELS IN REWORKED AREA FOUND SKIN PANELS WITHIN A-300 SRM LIMITS. ALL FASTENERS IN REWORK AREA HAS 2 D OR GREATER ED AND HOLE SIZES ARE WITHIN LIMITS. TREATED ALL REPAIR PARTS. INSTALLED REPAIR. 2L72 4F RTA35EU 20041101001182004110100118NE 2004 11 1 2004UALA00941 220041012A7200 ENGINE BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 1 SURGES A UALAC ABORTED TAKEOFF CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP29177UA 24384 NR 1 ENGINE SURGE ON TAKEOFF. NOTED LOSS THRUST PRIOR TO ROTATION. C5 BLADE FAILED DUE TO FOD IMPACT. ENGINE WAS REMOVED AND OVERHAULED. THE 5TH STAGE COMPRESSOR BLADE WAS FOUND DAMAGED. THE CAUSE OF THE DAMAGE APPEARS TO BE FOD. 2L74 4F4 FRTA20WE E24NE 20041101001222004110100122EA 2004 11 1 COMA0460559 120041005A3220 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA MLG DISCONNECTED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01416CA 7450 FLIGHT 5710 GEAR DISAGREE WARNING. FOUND NLG TORQUE LINKS DISCONNECTED. RECONNECTED LINKS AND A/C FERRIED TO MAINTENANCE FOR REPAIR OF DAMAGED TORQUE LINKS AND GEAR DOOR. 2L72 4F RTA21EA 20041101001322004110100132NM 2004 11 1 2004UALA00843 120040911A5230 ATTACH BRACKET BOEING757 757222 1384956NM PWA 2037 PW2037 NE CARGO DOOR CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29505UA 24626 FOUND THREE ATTACH BRACKETS CRACKED ON FORWARD PIT DOOR ALONG UPPER EDGE. LOOSE ATTACH BOLTS BETWEEN THE UPPER LONGITUDINAL CHORD AND FORWARD CARGO DOOR CORNER BRACKETS AND/OR FRAMES AT STATION 572, 580, AND 588 WERE LOOSE THAT EVENTUALLY, DUE TO REPETITIVE BENDING AND REDISTRIBUTION OF PRIMARY LOAD PATH, RESULTED IN THE FATIGUE AND FAILURE OF THE ATTACH CLIPS. 2L72 4F4 FRTA2NM E17NE 20041101001392004110100139NM 2004 11 1 SWAA043091 120041025A53106547979 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT BS 857, LBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041101001432004110100143NE 2004 11 1 2004UALA00942 220041012A7200 ENGINE BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 SURGES A UALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29117UA 28810 LOUD BANG ON TAKEOFF. NR 2 ENGINE SURGE. ENGINE EXPERIENCED A GROUP 3 SURGE, ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION. ENGINE EXPERIENCED OPEN CLEARANCES IN THE REAR OF THE COMPRESSOR AND SURGED. ENGINE WAS REMOVED FROM SERVICE AND OVERHAULED. 2L74 4F4 FRTA20WE E24NE 20041101001492004110100149NM 2004 11 1 DL76L040977 120041017A2780S283T00610 SENSOR BOEING767 767332 1382001NM LEFT WING UNSERVICEABLE A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27171DN 30255 24759 L/E SLAT DISAGREE LIGHT FOLLOWED BY L/E SLAT ASSY LIGHT. BITE CHECK PERFORM FAULTS S287. REMOVED AND REPLACED S287 PER AMM, CYCLED FLAPS/SLATS SEVERAL TIMES, NO FAULTS. OPS CHECK NORMAL. 2L72 4F RTA1NM 20041102000072004110200007 2004 11 2 SWAA043131 420041027A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29733SA 27865 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041102000092004110200009NM 2004 11 2 SWAA043133 120041027A53156546809 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM FWD FLANGE AT BS 946, LBL 54, CRACKED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041102000122004110200012NM 2004 11 2 SWAA043123 120041027A5753 SKIN BOEING737 7373H4 1384600NM LT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW BN1071 24152 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING FOREFLAP PER MM. 2L72 4F RTA16WE 20041102000242004110200024NM 2004 11 2 SWAA043103 120041025A534065C27314 STRINGER CLIP BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29694SW 23061 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 4R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041102000282004110200028NM 2004 11 2 2004UALA00867 120040908A5414 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE PYLON DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 NR 2 PYLON EXISTING FASTENER HOLES IN THE RT AND LT FWD PYLON SKINS ARE LARGER THAN ALLOWABLE LIMITS. *S/D* REPAIRED OVERSIZED HOLES WITH FREEZE PLUG REPAIRS. 2L72 4F4 FRTA2NM E17NE 20041102000382004110200038NM 2004 11 2 2004UALA00924 120041010A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29655UA 25393 FLOORBEAM STA 246 STIFFENER AT APPROX RBL 20 IS CRACKED. CRACK CAUSED BY CYCLIC DEFLECTION FATIGUE. FABRICATED & INSTALLED NEW STIFFENER. 2L72 4F4 FRTA1NM E24NE 20041102000392004110200039NM 2004 11 2 SWAA043093 120041025A531065C26402 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 727D TO BS 747, RBL 70, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041102000472004110200047NM 2004 11 2 2004UALA00961 120041016A7722 INDICATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 EGT MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29332UA 24193 DIVERTED TO MCI DUE TO HIGH ENGINE GAS TEMPERATURE READING IN NR 1 ENGINE. REVIEWED CHRONIC EGT INDICATION HISTORY, ACCOMPLISHED CONTINUITY CHECK FROM EGT CIRCUIT BREAKER TO D442 CONNECTOR AND HAND-OVER-HAND INSPECTION OF WIRING BETWEEN CIRCUIT BREAKER AND INDICATOR. CHECKED CONNECTOR D442 PINS AND SOCKETS FOR DAMAGE, RETENSION OR PUSHED BACK SOCKETS. NO FAULTS FOUND. REPLACED EGT INDICATOR. ACCOMPLISHED ENGINE POWER RUN TO CONFIRM SYSTEM OPERATION. COMPONENT SHOP TEST FOUND NO FAULTS ON REMOVED EGT INDICATOR UNIT. 2L72 4F4 FRTA16WE E2GL 20041102000522004110200052NM 2004 11 2 2004UALA00951 120041016A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1600 STR 25L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENT DAMAGE FROM CARGO LOADING. INSTALLED J-ANGLE DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041102000572004110200057NM 2004 11 2 AMTA200401244 120041002A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT BROKEN A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 FOUND DOOR 2R EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE IN FLOOR EGRESS LIGHTS IN FORWARD CABIN. EMERGENCY EXIT LIGHT AT D2 OPS CHECK OK. REF AWM 20-00-10. (M) 2L72 4F RTA2NM 20041102000642004110200064EA 2004 11 2 A6WA200440127 120040909A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31438AW 7748 WHILE PERFORMING LIGHTNING STRIKE DAMAGE INSPECTION FOUND RIGHT FUSELAGE AREA BETWEEN STRINGER 24R-25R AT FS 220-235 TO BE PREVIOUSLY BLENDED BEYOND LIMITS OF SRM 53-00-31. BLEND DEPTH .010 INCH. CUTOUT DAMAGED SECTION AND INSTALLED LOCALLY FABRICATED DOUBLER AND FILLER IAW BRAS EO 601R-53-5343. (M) 2L72 4F RTA21EA 20041102000752004110200075 2004 11 2 UIEA200400181 420041006A341737571832 CADC BOEING747 7472D7B 1384803NM NR 2 FAILED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15528MC 22472 HKG/BEL - AFTER DEPARTURE NR 2 ALTIMETER BECAME ERRATIC WITH ALT ALERT SOUNDING ENTER FOLLOWED BY AIRSPEED MACH INDICATOR FLAG AND SAT IND OF .05, SUSPECT RN 2 CADC FAILED. CHANGED NR 2 CADC IAW MM 34-12-01/401. CADC NR 2 OPERATIONAL TEST IAW MM 34-12-00 SATISFACTORY. PITO/STATIC SYSTEM CHECK CARRIED OUT SATISFACTORY. NO LEAKAGE, AIRSPEED AND ALTIMETER READING AGREE WITH TESTER. (M) 2L74 4F RTA20WE 20041102000932004110200093SO 2004 11 2 LR7A04108 120041001A53203393943 FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5324 FOUND RMLG FS 477 FWD FAIRING TENSION TIE SUPPORT FITTING CRACKED AT WL 158, RBL 68. REPLACED FITTING IAW DWG 339394 AND SRM SMP 583 51-70. NR 0280. 2H74 4T4 T A1SO E282 20041102000942004110200094SO 2004 11 2 LR7A04109 120041001A53403393943 FITTING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG FS 617 AFT FAIRING TENSION TIE FITTING CRACKED AT WL 158, LBL 68. REPLACED FITTING IAW DWG 339394 AND SRM SMP 51-70. NR 0283. 2H74 4T4 T A1SO E282 20041102000952004110200095SO 2004 11 2 LR7A04110 120041001A5311 FRAME LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE GOUGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5324, FOUND FS 477 FRAME GOUGED AT WL 184, RBL 83. REPAIRED PER SRM SMP 583 51-140-22. NR 0293. 2H74 4T4 T A1SO E282 20041102001192004110200119NM 2004 11 2 DL76K040996 120041027A5280113T820148A DOOR BOEING767 767332 1382001NM GE CF6 CF680C2B6F 30025NE RT MLG MISSING A DALAO OTHER D INFLIGHT SEPARATION APAPPROACH 1 SO27177DZ 29698 RT MAIN LANDING GEAR LOWER STRUT DOOR MISSING UPON ARRIVAL. FERRIED A/C TO FOR FURTHER EVALUATION. 2L72 4F4 FRTA1NM E13NE 20041103000162004110300016EU 2004 11 3 DHL2004362015 120041026A1420 CONNECTOR AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE MLG DIRTY A DHLAO OTHER J WARNING INDICATION DEDESCENT 1 SO01362DH 84 RT MAIN GEAR GREEN DOWN LIGHT ON FORWARD PANEL COMES ON INTERMITTENT WITH MWP ANTI-SKID OFF LIGHT. LANDING GEAR LEVER LOCK ON SYSTEM 1. COULD NOT DUPLICATE ON GROUND. CLEANED PROX SENSORS AND CONNECTOR ON RT GEAR. PERFORMED TEST OF PROXIMITY DETECTOR UNIT IAW M/M 32-61-00. OPS CK GOOD ON GROUND. 2L72 4F4 FRTA35EU E23EA 20041103000222004110300022SO 2004 11 3 LR7A04120 120041001A5312 PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FS 550 CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG BAY FS 550 PANEL RISERS CORRODED AT WL 190 AND WL 195, LBL 62. REPAIRED IAW EA 382-53-04-079. NR 0480. 2H74 4T4 T A1SO E282 20041103000292004110300029EU 2004 11 3 DHL2004363534 120041012A5330 SKIN AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3912, AFT. FUSELAGE SKIN HAS DENT AT FR 77 AND STR 22R. BLENDED OUT AREA, FOUND DENT BEYOND LIMITS IAW SRM 53-10-10. CUT OUT DAMAGE AREA SRM 53-10-10. PERFORMED HFEC OF CUT-OUT AREA NTM PT 1 51-31-05. NO DISCREPANCIES NOTED. INSTALLED DOUBLER, MATERIAL USED ALCLAD 2024 T3 0.100 SIZE 10 INCHES X 15 INCHES SRM 53-10-10. TREATED AND PRIME AREA AS REQUIRED AND APPLY PRC REF: A-300 51-40-10 AND SRM 51-60-00 / 51-40-20 PAINT PREPPED AND PAINTED IAW SRM 51-40-12 PAGE BLOCK 1. 2L72 4F4 FRTA35EU E23EA 20041103000322004110300032SO 2004 11 3 C2XA04CL108 120041020A3350 LIGHT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL SERVICE DOOR INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714939 145030 FLIGHT NR 2805, THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. SIR REMAINS OPEN PENDING ADDITIONAL INFORMATION 2L72 4F4 FRTT00011ATTE6CH 20041103000352004110300035 2004 11 3 T2BA4 420041018A2397 WIRE BEECH 1900 1900C 1154161CE PWA PT6 PT6* 52043EA PA SYSTEM LOOSE E T2BAO OTHER O OTHER TXTAXI/GRND HDL 1 SO15172TE UB24 PA SYSTEM INOPERATIVE, DEFFERRED IAW MEL 23-1 AND 23-2, PERFORMED PUBLIC ANNOUNCEMENT USING THE BULL HORN, PROCEEDED WITH FLIGHT, RETURNED TO HOME BASE AND PERFORMED TROUBLESHOOTING OF PA SYSTEM, FOUND A LOOSE WIRE, REPAIRED, SIGNED OFF WRITE UP AND RELEASED AIRCRAFT FOR FLIGHT. 2L72 4T3 TRTA24CE E2NE 20041103000382004110300038SO 2004 11 3 LR7A04196 120041025A5311 FRAME LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 272 4606 DURING SCHEDULED (A) CHECK INSPECTION IAW JOB CARD HA1200 FOUND FS 836 FRAME WEB CRACKED AT LBL 68, WL 197. REPAIRED IAW EA 382-53-04-089. GMM133 ITEM M3. 2H74 4T4 T A1SO E282 20041103000392004110300039NM 2004 11 3 250TR0037 120041022A5320 SUPPORT BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE RADAR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 SUPPORT FOR RADAR TR RACK CRACKED. REPAIRED IAW SRM 51-40-3. 2L72 4F4 FRTA16WE E2EA 20041103000402004110300040NM 2004 11 3 250TR0051 120041022A5320 ATTACH ANGLE BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 ATTACH ANGLE CRACKED UNDER THRESHOLD AT BS 480 AND STR26RT IN FORWARD CARGO BIN. REPLACED ANGLE IAW MFG DWG. 69-16784 AND SRM 51-30-0. 2L72 4F4 FRTA16WE E2EA 20041103000412004110300041NM 2004 11 3 250TR00531 120041022A5320 ATTACH ANGLE BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 INTERCOSTAL WEB ATTACH ANGLE CRACKED AFT SIDE OF FRAME AT BS 500 AT STR 28 RT IN FORWARD CARGO BIN. REPLACED ANGLE IAW MFG DWG. 69-37261 AND SRM 51-30-2. 2L72 4F4 FRTA16WE E2EA 20041103000422004110300042NM 2004 11 3 250TR0054 120041022A5320 WEB BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 WEB FROM BS 490 TO BS 500 AT STR 26 RT IS CRACKED. REPLACED WEB IAW MFG DWG. 65-20726 AND SRM 51-30-2. 2L72 4F4 FRTA16WE E2EA 20041103000432004110300043NM 2004 11 3 250TR0056 120041022A5313 STRINGER BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION ON STR 27 RT JUST FORWARD OF BS 360. REPAIRED IAW EA NR 53-291 AND SRM 53-10-3. 2L72 4F4 FRTA16WE E2EA 20041103000452004110300045NM 2004 11 3 AWXA200401166 120041005A5315654581283 FLOORBEAM BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK A 2 INCH CRACK WAS FOUND IN FLOORBEAM WEB AT BS 328, RBL 28, WL 208. MAINTENANCE CUTOUT DAMAGED AREA IN FLOORBEAM WEB AT BS 328, RBL 28; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5335-04295-RC1. 2L72 4F4 FRTA16WE E2GL 20041103000472004110300047NM 2004 11 3 AWXA200401168 120041015A53106616932000 SHEAR TIE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD SIDE OF FRAME FOOT AT BS 480, BETWEEN STRINGERS 25 AND 26 LT. MAINTENANCE REMOVED SHEAR TIE, SUPPORT CLIP, AND DAMAGED SECTION OF FRAME AT BS 480, BETWEEN STRINGERS 25 AND 26 LT; FABRICATED A SHEAR TIE, SUPPORT CLIP, AND FILLER; INSTALLED REPAIR PARTS IAW SRM 53-00-07, FIG. 203. 2L72 4F4 FRTA16WE E2GL 20041103000492004110300049NM 2004 11 3 AWXA200401170 120041002A5753 SKIN BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK 11 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BETWEEN SLAT STA. 51.75 AND 74.65 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF NR 3 SLAT LOWER SKIN FROM S.S. 51.75 LT TO S.S. 74.65 LT; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW SRM 57-43-01, FIG. 206. 2L72 4F4 FRTA16WE E2GL 20041103000502004110300050NM 2004 11 3 250TR0040 120041022A5320 SUPPORT CHANNEL BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 DRAIN MAST UPPER SUPPORT CHANNEL FROM BS 986 TO BS 1006 AT STR 25 LT HAS CORROSION. REPLACED SUPPORT CHANNEL IAW SRM 53-10-2. 2L72 4F4 FRTA16WE E2EA 20041103000652004110300065NE 2004 11 3 04FDEA02959 220041020A7200 ENGINE BOEING727 727100 1384036NM PWA JT8 JT8D7B 52053NE NR 2 OVERTEMP A FDEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25192FE 19085 PDIS 192 79-10 0009533 20OCT04 MEM OPEN U LOGPAGES: 00949069 ENG NR 2 AND NR 3 OIL TEMPS BOTH IN THE YELLOW BAND AND OCCASSIONALLY SPIKING INTO THE RED DURING CLIMBOUT BOTH ENGINE HAD TO BE KEPT ABOVE IDLE TO MAINTAIN LOWER TEMPS. 2L73 4F4 FRTA3WE E2EA 20041103000672004110300067NM 2004 11 3 04FDEA02961 120041021A5531 SPAR DOUG MD11 MD11F 3023600NM GE CFM56 CFM563B1 13802NE ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BETWEEN ZID 92.50 TO ZFR 424.219 LT SKIN EXTERIOR SURFACE FOUND CORRODED. REMOVED & REPAIRED AS PER FEDEX EA 1-5530-81581. 2L73 4F4 FRTA22WE E2GL 20041103000692004110300069NM 2004 11 3 04FDEA02963 120041021A5531 SPAR DOUG MD11 MD11F 3023600NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR, ZID 92.50 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION AREA REPAIRED AS PER FEDEX EA 1-5530-81582. 2L73 4F4 FRTA22WE E23EA 20041103000712004110300071WP 2004 11 3 DHL2004801557 120040927A534058004713 FITTING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FITTING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 AFT ACCY COMPT SPLICE FITTING HAS CRACKS 1.000, 0.500 STA. 640.000 TO STA. 660.000, L-32R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 PG.1, DWG 5800471. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG. 21. FABRICATED SPLICE FITTING (AL7075-T651) IAW DWG 5800471. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND SPLICE FITTING IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED SPLICE FITTING WITH NEW FASTENERS IAW SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20041103000732004110300073WP 2004 11 3 DHL2004801561 120041005A57403645612 BRACKET DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT WING NR 1 ALT TANK BOOSTER PUMP BRACKET CRACKED (FWD). PERFORMED MAJOR REPAIR IAW DWG W51-R11, FAA FORM 8110-3 DATED 10-04-04. REMOVED CRACKED BRACKET IAW SRM 57-1-0 PG.1, SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, SRM 51-3-0 PG.1. FABRICATED NEW BRACKET (AL7075-T651) IAW DWG W51-R11. PERFORMED HEAT TREATMENT IAW DPS 7.00. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW BRACKET IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.9, SRM 51-3-0 PG.1. 2L74 4F4 FRT4A25 E2GL 20041103000752004110300075WP 2004 11 3 DHL2004801559 120040929A5414 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 PYLON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 DURING POSITIVE CHECK FOUND 1.000 CRACK IN NR 1 PYLON FRONT LWR SECTION (STA. XW 487.000 - 508.977 CANT, S-63) PERFORMED MAJOR REPAIR IAW MFG NR 1-OG81S, FAA FORM 8110-3 DATED 09-10-04. REPAIR SKETCH JCT03432. REMOVED FASTENERS IAW SRM 51-1-20D PG.21. CUT OUT DAMAGED SECTION IAW MFG MESSAGE NR 1-0G81S, REPAIR SKETCH JCT03432. PERFORMED SHOT PEENING OF AREA ADJACENT TO THE TRIMMOUT IAW MFG MESSAGE NR 1-OG81S, REPAIR SKETCH JCT03432, DPS 4.999-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FASTENERS IAW SRM 51-1-20D PG.9. VISUALLY INSPECT THE REWORKED AREA AT EVERY C CHECK, NOT TO EXCEED 24 MONTHS. REFER TO NR 1982 FOR LEAK CHECK. 2L74 4F4 FRT4A25 E2GL 20041103000772004110300077WP 2004 11 3 DHL2004801513 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 4 TRACK PLUG LUGS WORN, STA 1575.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103000792004110300079WP 2004 11 3 DHL2004801519 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN, STA. 320.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103000812004110300081WP 2004 11 3 DHL2004801517 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 2 TRACK PLUG LUGS WORN, STA 113.000. REMOVED WORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103000822004110300082WP 2004 11 3 DHL2004801516 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN, STA. 1130.000. REMOVED WORN PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103000832004110300083NM 2004 11 3 UPS04243383 120041008A5320 WEB BOEING727 727185C 138406NNM RROYCETAY TAY65154 EU BS BL 35 WL1 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE-C BS 740 LOWER WEB RT BL 35 WL160 APPROX SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4 CRACKS CONTAINED WITHIN FASTENER HOLE. REPAIR PARTS FABRICATED IAW SRM 53-10-09. REPROTECTED REP PARTS AND DAMAGED AREA IAW SRM 51-10-02. SEALANT APPLIED IAW SRM 51-20-04. 2L73 4F4 F A3WE E25NE 20041103000842004110300084NM 2004 11 3 UPS04243397 120041004A5751 HINGE BOEING727 727185C 138406NNM RROYCETAY TAY65154 EU RT IB AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR SPAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02 2L73 4F4 F A3WE E25NE 20041103000852004110300085NM 2004 11 3 UPS04443391 120040925A532065B132613 LINK BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE-C FX- KEEL BEAM BOX INNER HORIZ SUPPORT LINK CORRODED AT BS 1460 WL 118. CORROSION MACHINED OFF AT BOTH SIDE VERTICAL RIBS 0.030 INCH AT BOTTOM HORIZ RIB 0.020 INCH . KEEL BEAM BOX INNER HORIZ SUPPORT LINK REPLACED IAW HX RS NR R-53-49-35206 AND UPS RA NR 747-53-20195. 2L74 4F4 F A20WE E20EA 20041103000862004110300086WP 2004 11 3 04FDEA02987 120041025A5330 PANEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL ZONE 300 CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 N12347, DURING PASSENGER TO FREIGHT COVERSION: ON PANEL 7208-1 RT SIDE, FOUND BY ULTRASONIC INSPECTION NR 1 HOLE WITH CRACK L .2500 INCH AT 1INCH FROM BOTTOM. POSITION NR 3, SHORE AIRCRAFT AS REQUIRED IAW SB 55-16, REPLACE CRACKED PANEL IAW SB 55-16 FIG 4 GRUP 1 AND EA 8-510-70126. 2L73 4F4 F A22WE E23EA 20041103000872004110300087WP 2004 11 3 04FDEA02988 120041025A5313S492982814400 LONGERON DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING PAX TO FREIGHT CONVERSION FOUND INTERNAL FUSELAGE STA 791-808, STR 27, RT VANE DOOR WITH CORROSION AND EXFOLATION. REMOVE SCUFF PLATE FOR ACCESS OPEN SKIN, REPLACE DAMAGE SECTION OF LONGERON 27 AND REINSTALL SKIN IAW SRM 51-33-01 PAG 34-47;AND SCUFF PLATE. 2L73 4F4 F A22WE E23EA 20041103000882004110300088WP 2004 11 3 04FDEA02989 120041025A5313S492982814400 LONGERON DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING PAX TO FREIGHT CONVERSION FOUND INTERNAL FUSELAGE STA 791-808, STR 27, RT VANE DOOR WITH CORROSION AND EXFOLATION REMOVED SCUFF PLATE FOR ACCESS OPEN SKIN, REPLACE DAMAGE SECTION OF LONG 27 AND REINSTALL SKIN IAW SRM 51-33-01 PAGE 34-47; AND SCUFF PLATE. 2L73 4F4 F A22WE E23EA 20041103000892004110300089WP 2004 11 3 04FDEA02990 120041025A5330 SKIN DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF HAVING REPLACE SKIN P/N AGA3108-1 FRAME AND SHEAR TIE AT STA 1986 ,PN AGA3783-3/-25 FRAME ,SHEAR TIE AT STA 1975 P/N, AGA3183-3/-23. REWORK INVOLVED AREA IAW EA 8-5310-77036. 2L73 4F4 F A22WE E23EA 20041103000902004110300090EU 2004 11 3 DHL2004363509 120041005A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3898, RBL 36 BETWEEN FRAME AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA/FRAME IS TO FRAME 19 RBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FROM FR 15 TO FR. 19 AT RBL 36 IAW SRM 51-30-30. INSTALLED NEW SEAT TRACK FROM FR.15 TO FR. 19 AT RBL 36 IAW 51-10-40 AND SRM 51-30-30. TREATED AND PRIMED AREA AS REQUIRED SEAT TRACK SRM 51-40-10 AND 51-40-12. 2L72 4F4 FRTA35EU E23EA 20041103000912004110300091EU 2004 11 3 DHL2004363511 120041005A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF680C2* GL FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3899 LBL 36 BETWEEN FRAME 15 AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA FRAME 15 TO FRAME 19 LBL 36 FOUND OUT OF LIMITS SRM 53-10-00. REMOVED SEAT TRACK FOR REPAIR IAW SRM 51-30-30/51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 15 TO FR. 19 AT LBL 36 IAW SRM 51-10-40/51-30-30. TREATED AND PRIMED AREA AS REQUIRED (SEAT TRACK) SRM 51-40-10/51-40-12. 2L72 4F4 FRTA35EU E23EA 20041103000922004110300092EU 2004 11 3 04FDEA02923 120041012A5311 FRAME AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 N00197, INCOMING CONDITION, JUST FORWARD OF FR 10 LT SIDE IS A DENT (2 INCH X 2 INCH X .090 INCH) WHICH IS OUT OF LIMITS IAW SRM TABLE 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER, FILLER IAW EA 6-5330-55382 AND SRM 51-71-70, EO-356-09-04-007-2/-4, DWG R536 11016, AND RAS AS/285/2004. 2L72 4F4 FRTA35EU E13NE 20041103000932004110300093EU 2004 11 3 04FDEA02924 120041012A5311 FRAME AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 N00196 INCOMING CONDITION, JUST FORWARD OF FRAME 10 RT SIDE IS A DENT 1 INCH X .5 INCH X .050 INCH WHICH IS OUT OF LIMITS IAW SRM 53-10-00 TABLE 102. INSTALLED REPAIR DOUBLER AND FILLER C/W EA 6-5330-55381 AND SRM 51- 71-70, TECHNICAL REQUEST OE-356-09-04-007-2/-4 AND MFG DWG R536 11020. 2L72 4F4 FRTA35EU E13NE 20041103000942004110300094NM 2004 11 3 04FDEA02925 120041012A5713 STRINGER DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 SNRM N0896: LT WING UPPER STRINGER (S12) END FOUND CRACKED AT INSIDE ACCESS PANEL 536AB. REPAIR CARRIED OUT AT LEFT HAND WING UPPER STRINGER 12 END AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS PER SRM 51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I. 2L73 4F4 FRTA22WE E31N3 20041103000952004110300095NM 2004 11 3 AWXA200401120 120041007A532065468221 SHEAR WEB BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK A 2 INCH CRACK WAS FOUND IN RT SHEAR WEB FORWARD OF FRAME AT BS 580, STR 17. RT MAINTENANCE CUTOUT DAMAGE ON RT SHEAR WEB FROM BS 578 TO BS 597, STR 17 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW SRM 51-70-13, FIG. 1. 2L72 4F4 FRTA16WE E2GL 20041103000962004110300096EA 2004 11 3 QXEA200400700 120040930A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 CABIN FLOORBEAM, AFT SIDE OF FS 280 BULKHEAD, UPPER SURFACE IS CORRODED IN MULTIPLE LOCATIONS BETWEEN LBL 36 AND RBL 16. REPAIRED IAW HORIZON AIR EA R-53-209 AND CRJ SRM 51-21-06, PARAGRAPH 3A, B, D, PAGE 2 AND 4. 2L72 4F4 FRTA21EA EOOO63EN 20041103000972004110300097NM 2004 11 3 AWXA200401121 120041002A532065528941 CHANNEL BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK A .9375 INCH CRACK WAS FOUND IN CHANNEL AT BS 540, BETWEEN BL (0) AND LBL 24. MAINTENANCE REMOVED CRACKED CHANNEL AT BS 540, FROM BL (0) TO LBL 24; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-52894; INSTALLED REPAIR PARTS IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20041103000982004110300098NM 2004 11 3 AWXA200401122 120041002A532065528942 CHANNEL BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK A 1.0625 INCH CRACK WAS FOUND IN CHANNEL AT BS 540, BETWEEN BL (0) AND RBL 24. MAINTENANCE REMOVED CRACKED CHANNEL AT BS 540, FROM BL (0) TO RBL 24; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-52894; INSTALLED REPAIR PARTS IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20041103001002004110300100WP 2004 11 3 04FDEA02874 120041005A5753NRC6068 SUPPORT DOUG DC10 DC1010F 3022111WP GE CF6 CF66D 30020GL TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 LT/RT OB FLAPS-FLAP VANE SUPPORTS CORROSION REWORK. CLOSING ACTION ON 10/04/04. ON N/R S00018. COMPLIED WITH EA 8-5750-82049. 2L73 4F4 F A22WE E23EA 20041103001012004110300101CE 2004 11 3 DXTA200400424 120041014A282123061826 FUEL FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL SYSTEM INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07953QS 7500153 CAE330325 FUEL FILTER BYPASS L CAS MESSAGE CAME ON AT POWER APPLICATION FOR TAKE-OFF ( NO NOTICABLE CHANGE IN ENGINE OPERATION, ABORTED TAKE OFF. INSTALLED NEW FILTER ELEMENT. TEST RAN ENGINE WITH NO FURTHER DEFECTS NOR LEAKS. WORK PERFORMED IAW MM CHAPTER 71-00 AND MM CHAPTER 73-21-400. 2L72 4J4 FRTT00007WITE6CH 20041103001022004110300102NM 2004 11 3 P5CA0401255 120041019A5313 STRINGER BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 AFT CARGO COMPARTMENT LT BS 1600 STRINGER 39L AND STRINGER 40L CRACKED. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-10-04. 2L74 4F4 F A20WE E20EA 20041103001032004110300103NM 2004 11 3 371PA0054 120040918A5315 FLOORBEAM BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FLOORBEAM AT BS 344 HAS CORROSION FROM LBL 40 TO RBL 20. REPAIRED IAW SRM 53-10-51. 2L72 4F4 FRTA16NE E2GL 20041103001042004110300104NM 2004 11 3 P5CA0401257 120041019A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 RT WING FIXED L/E UPPER SKIN B/W WING STATION 570 AND 600 LWR SURFACE DELAMINATED. REMOVED PANEL REPAIRED AND REINSTALLED IAW SRM 51-30-02. 2L74 4F4 F A20WE E20EA 20041103001082004110300108CE 2004 11 3 HYTA2005001 120041020A321026410143 SPRING CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MLG CHAFED E HYTAO OTHER O OTHER NRNOT REPORTED 1 AL01540ME6817 208B0540 FLEXING OF MLG SPRING CAUSES CENTER SPRING TO CONTACT MLG COVER PN 2611103-10 WHICH IS LOCATED BENEATH THE CENTER SPRING. TWO RIVETS HAD WORN INTO THE CENTER SPRING LOWER SURFACE. THESE RIVETS ARE THE CENTER IB RIVETS THAT FASTEN A FAIRING AT EACH END OF THE COVER. SUGGEST ELIMINATING THE CENTER RIVET AND INSTALLING TWO RIVETS FURTHER OB AND OFF CENTER AT BOTH FAIRINGS. THE CENTER SPRING WAS ALSO CONTACTING SCREWS THAT SECURE A COVER THAT ACCESSES THE MLG DEICE PLUMBING. THESE SCREWS COULD BE .1250 INCH SHORTER. NO DAMAGE EXCEEDED .005 INCHES IN DEPTH. ALSO RECOMMEND VINYL CHAFE TAPE ON LOWER SURFACE OF CENTER SPRING. 1H71 3T3 T A37CE E4EA 20041103001122004110300112NM 2004 11 3 COOSDR040013 120040817A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSLEAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN AT B STA 480 FROM RBL 62 INCHES TO LBL 65 INCHES FLOORBEAM UPPER CHORD WITH CORROSION IN SEVERAL PLACES. 2L73 4F4 FRTA3WE E2EA 20041103001172004110300117 2004 11 3 FE62004F00002 420040727A3422ST3400 INDICATOR BRAERODH125 HS125700A 4230170EU TAWS/RMI MALFUNCTIONED B FE6RO OTHER O OTHER NRNOT REPORTED 1 NM11455BK NA0256 THE SANDEL TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADING GREATER THAN 359 DEGREES OR LESS THAN 0 DEGREES. THIS PROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TESTING OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION IS SOFTWARE. THE ST34 TAWS/RMI IS NOT RECOMMENDED FOR NAVIGATION AT THIS TIME. 2L72 4F A3EU 20041103001202004110300120EA 2004 11 3 LN32004F00000 120040801A27206007510129 PCU CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE RUDDER LEAKING E LN3AO OTHER O OTHER NRNOT REPORTED 1 WP07604RT 5497 EXPERIENCING MULTIPLE OCCURRENCES IN WHICH THE RUDDER PCU (PN 600-75101-29) HAS DEVELOPED LEAKS AROUND THE OUTPUT SHAFT DEEMING THE ACTUATORS UNSERVICABLE. CONDITION SEEMS TO MANIFEST AFTER COLD SOAKING. LEAKS ARE NORMALLY MINIMAL AND WITHIN MM LIMITS WHEN TESTED ON GROUND. 2L72 4F4 FRTA21EA E15NE 20041103001242004110300124SO 2004 11 3 VIB2004F00000 220041006A8520654084A1 CAMSHAFT BEECH 36 A36 1151604CE CONT O550 IO550B SO ENGINE SPALLED A VIB6O OTHER O OTHER NRNOT REPORTED 1 NM03245TS341 E3318 684095 FOLLOWING REMOVAL OF CYLINDERS FOR REPLACEMENT DUE TO LOW COMPRESSION, LIFTERS WERE REMOVED FOR INSPECTION. FOUND NR 1 CYL EXHAUST LIFTER BADLY PITTED AND SPALLED ON PTCE AND CHIPPED ON EDGES. DAMAGE TO CAMSHAFT OCCURRED AS A RESULT. ENGINE REMOVAL FOR REPAIR WILL BE NECCESSARY. LIFTER PN 653877. 1L71 3O3 O 3A15 E3SO 20041103001252004110300125NM 2004 11 3 COOSDR040018 120040817A5714 PLATE BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE WING CENTER SEC CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 LT WING, FRONT SPAR LOWER CHORD PLATE FROM FSS 731 TO FSS 759, WITH CORROSION. 2L73 4F4 FRTA3WE E2EA 20041103001262004110300126NM 2004 11 3 COOSDR040025 120040817A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN, BS 950F, WL 208 FLOORBEAM UPPER CHORD CORRODED. 2L73 4F4 FRTA3WE E2EA 20041103001312004110300131NE 2004 11 3 ALG2004F00054 120040916A261230326E7 AMPLIFIER SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL FIRE WARNING UNSERVICEABLE E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03702AL20099 760243 CAE890262S ON TAKE OFF, IN FLIGHT, THE NR 1 FIRE WARNING LIGHTS AND TONE CAME ON, HAD NO OTHER INDICATION OF FIRE. MAINTENANCE REMOVED CONTROL AMPLIFIER AND INSTALLED SERVICEABLE AMPLIFIER, OPS CHECK WAS GOOD. 1G72 3U3 U H1NE E1GL 20041103001342004110300134 2004 11 3 ASMF200410013 420041017A341810000165101 TRANSMITTER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE NR 1 FAILED W ASMFO OTHER J WARNING INDICATION CRCRUISE 1 SW23861LF12736 49826 CAPTAIN REPORTED THAT DURING CRUISE STALL INDICATION FAILURE LIGHTS TURNED ON CONSTANTLY. DURING TEST IT WAS DETECTED THAT COMPUTERS REPORTED TX POS FLAPS AND SYSTEM DIFFERENCE FLAPS FAILURES. AIRCRAFT WAS SENT TO THE HANGAR AND POSITION FLAPS TRANSMITTERS WERE REPLACED IAW MM. DURING OVERNIGHT SERVICE WAS DETECTED DIFFERENCE IN TRANSMITTERS ANGLE ATTACK SIGNAL. BOTH TRANSMITTER ANGLE ATTACKS WERE REPLACED AND STALL COMPUTERS WERE TESTED IAW MM 34-19-00 AND 34-19-01, ALL CORRECT. 2L72 4F4 FRT E9NE 20041105000032004110500003NM 2004 11 5 SWAA043166 120041029A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520+2, STR 12L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041105000042004110500004NM 2004 11 5 SWAA043172 120041102A3350 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041105000052004110500005 2004 11 5 SWAA043178 420041101A2565D31354 SLIDE BOEING737 7373G7 1384595NM R1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29690SW 23783 DURING SCHEDULED C3 CHECK, FOUND R1 & R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 & R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041105000072004110500007NM 2004 11 5 SWAA043155 120041029A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN 937 & BS 947, STRINGER 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000092004110500009NM 2004 11 5 SWAA043157 120041027A53306545774 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 827, STR 25L. REPAIRED SKIN PER SRM. 2L72 4F A16WE 20041105000112004110500011 2004 11 5 SWAA043140 420041028A256565C19901 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29354SW 25219 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVACUATION SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2L72 4F RTA16WE 20041105000122004110500012 2004 11 5 SWAA043169 420041102A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29430WN 33659 L1 DOOR EVACS SLIDE FELL OUT. REINSTALLED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041105000142004110500014NM 2004 11 5 SWAA043171 120041102A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY AND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED LIGHTS PER MM. 2L72 4F RTA16WE 20041105000162004110500016SO 2004 11 5 LR7A04137 120041001A5312 PRESSURE PANEL LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND RH FS 597 - 617 PRESSURE PANEL CRACKED AT, WL 260, RBL 61. REPAIRED IAW LAC MEA 382-53-04-071. 2H74 4T A1SO 20041105000182004110500018NM 2004 11 5 SWAA043179 120041102A53106547951 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT AFT WEB CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20041105000192004110500019NM 2004 11 5 SWAA043180 120041102A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 927 BETWEEN STRINGER 26R AND STRINGER 27R, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041105000202004110500020NM 2004 11 5 SWAA043181 120041102A53156545410366 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM WEB AT BS 664, BL 0, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER EA AND SB. 2L72 4F RTA16WE 20041101000192004110100019NM 2004 11 1 2004UALA00890 120041002A2121 FAN BOEING747 747422 1384935NM PWA 4056 PW4056 NE COCKPIT/CABIN FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29180UA 25224 FLIGHT CREW REPORTED BURNING ODOR FROM THE COCKPIT & FIRST CLASS AREA. THE EQUIPMENT COOLING SUPPLY FAN MOTOR FAILED. REPLACED THE FAN ASSEMBLY. 2L74 4F4 FRTA20WE E24NE 20041101000322004110100032EA 2004 11 1 COMA0460563 120041007A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01912CA 7011 CRACK FOUND ON RIGHT WING PLANK. PERFORMED CRJ REO 601R-57-21-130. 2L72 4F RTA21EA 20041101000422004110100042NM 2004 11 1 2004UALA00802 120040807A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 AFT CABIN FLOORBEAM AT STA 1661, RBL 54 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR. 2L72 4F4 FRTA2NM E17NE 20041101000442004110100044NM 2004 11 1 2004UALA00804 120040825A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 LEFT HAND CREASE BEAM HAS A LARGE AREA OF CORROSION AT BS 686, JUST FORWARD OF THE L2 CABIN DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE. 2L72 4F4 FRTA2NM E17NE 20041101000532004110100053NM 2004 11 1 2004UALA00853 120040928A3600 WARNING LIGHT BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE BLEED SYSTEM ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29783UA 26950 BLEED LOSS WING LEFT AND BLEED LOSS BODY LEFT EICAS MSGS. ALSO HYD PRESS DEMAND CI MSG. FOUND THE LOWER FLOW CONTROL VALVE INSTALLATION CLAMP BROKEN WITH APPRECIABLE BLEED AIR LEAKAGE. FURTHER INVESTIGATION OF THE CLAMP FOUND FAILURE OCCURED AT A SPOT WELD ADJACENT TO THE LOOP THAT SECURES THE TIGHTENING TEE BOLT TO THE CLAMP ASSEMBLY. AS A RESULT, THE CLAMP LOST ALL TENSION. THE CLAMP WAS REPLACED AND LEAK CHECK ACCOMPLISHED. 2L72 4F4 FRTT0001SE E46NE 20041101000582004110100058NM 2004 11 1 2004UALA00858 120040907A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 FRAME IS DENTED AT BS 1560, LBL 8, UNDER THE CARGO FLOOR, ON THE UPPER FLANGE. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20041101000642004110100064NE 2004 11 1 COMA0460580 220041018A72616087T04P06 PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENG OIL PRESSMALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01473CA6518 7668 FLT 5651 LT ENGINE OIL PRESSURE WARNING. REPLACED THE ENGINE OIL PUMP. 2L72 4F4 FRTA21EA E15NE 20041101000842004110100084NM 2004 11 1 2004UALA00862 120040907A5320 SILL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 AFT CABIN AT BS 1681, RBL 55, THE R4 DOOR LOWER SILL WAS FOUND CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED DOOR SILL AT R-4 DOOR WITH A DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041101000992004110100099NM 2004 11 1 2004UALA00807 120040901A2612G718505 CONTROL PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLIGHT DECK MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29311UA 23672 CARGO FIRE LIGHT FLICKERING ON CARGO SUPPRESSION PANEL. CREW REPORTED THAT CARGO FIRE LIGHT FLICKERING ON CARGO SUPPRESSION PANEL WITH NO OTHER INDICATION OR FAULTS. REMOVED AND REPLACED FIRE DETECTION AND SUPPRESSION CONTROL PANEL. SYSTEM CHECKED NORMAL. 2L72 4F4 FRTA16WE E2GL 20041101001012004110100101NM 2004 11 1 2004UALA00774 120040817A1430 SCREW BOEING757 757222 1384956NM PWA 2037 PW2037 NE L2 GIRTBAR LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29563UA 26665 DOOR 2L GIRT BAR LIGHT DOES NOT ILLUMINATE WITH DOOR CLOSED AND ARMED. MOUNTING SCREW FOR FLOOR ATTACH FITTING WAS BACKED OUT AND DID NOT ALLOW GIRT BAR TO ENGAGE FLOOR FITTING. SCREW WAS SECURED AND DOOR ARMS NORMALLY. 2L72 4F4 FRTA2NM E17NE 20041101001102004110100110EA 2004 11 1 COMA0470071 120040930A5610NP1393226 WINDOW CNDAIRCL600 CL6002C10 1390015EA COCKPIT CRACKED A COMAO OTHER O OTHER LDLANDING 1 SO01398CA3301 10112 FLIGHT 5249 CO-PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW. 2L72 4F RTA21EA 20041101001312004110100131NM 2004 11 1 DHL2004784005 120040806A2610 WARNING LIGHT BOEING727 727227 1384078NM NR 3 DETECTED ILLUMINATED A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01784DH 22001 NR 3 DETECTOR CIRCUIT GROUND, AMBER LIGHT ON. DEFERRED NR 3 GROUND FAULT DETECTOR SYSTEM LIGHT IAW MEL 26-9-1 CAT C DMI 17439. 2L73 4F A3WE 20041101001382004110100138 2004 11 1 SWAA043072 420041022A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041101001472004110100147NM 2004 11 1 DHL2004741010 120040804A2613 OVERHEAT LOOP BOEING727 7272Q9 138448MNM AFT BODY MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01741DH 21931 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED CLIMBING THROUGH FL 160. RAN ABNORMAL PROCEDURE. RETURNED TO IAH. A/C SHUT DOWN AFTER LANDING AND TOWED TO PARKING. FOUND LT AFT BODY FIRE LOOP BREAKING DOWN DURING OPERATION OF ENGINES & SYSTEMS. REMOVED AND REPLACED FIRE LOOP IAW B727 MM 26-14-1. OPS CHECKS GOOD ON RUN IAW B727 MM 26-14 & ASTAR JRH. 2L73 4F RTA3WE 20041102000022004110200002SO 2004 11 2 C2XA04SH533 120041021A323414532170401 CONTROL LEVER EMB 145 EMB145LR 3260212SO MLG DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713955 145075 DURING CLIMBOUT OF BNA GEAR SELECTED UP AND DID NOT RETRACT. AIRCRAFT DIVERTED TO SHV AND LANDED WITH OUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CHECKED GOOD. 2L72 4T RTT00011AT 20041102000112004110200011 2004 11 2 SWAA043122 420041027A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED C2 CHECK, FOUND R2 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED BOTH R2 AND L1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041102000142004110200014EU 2004 11 2 DHL2004366004 120040807A5315 FLOORBEAM AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01366DH 249 DURING A-7 CHECK, FWD CARGO FLOOR ATTACH FITTINGS HAVE CORROSION STR 42 FWD & AFT SIDE FRAME 31 & FWD SIDE FRAME 32. REMOVED FLOOR PANELS FOR ACCESS TO FLOORBEAM AREA FWD LOWER CARGO COMPT. CUT OUT DAMAGE AREA FLOORBEAM FRAME NR 32 RBL 19 AREA FWD LOWER CARGO. REMOVED LITE CORROSION ON FLOOR ATTACH FITTINGS FWD AFT SIDE FRAME 31 & FWD SIDE FRAME 32. MAT LOSS LESS THAN .001 INCH WITHIN LIMITS. TREATED & PRIMED FRAME 31 FWD & AFT SIDE. INSTALLED REPAIR FLOORBEAM FRAME 32 RBL 19. MAT USED & 10136-1201 T-ANGLE PO 2336062 LOT 2915UBUR SIZE 42.25 INCH, 2024 T-3 .063 PO 2424592 LOT 440-462 SIZE 8.25 INCH; 2024 .071 PO 8319629 LOT 6F05CG2T SIZE 16.25 INCH. HEAT TREATED PARTS. CLOSED AREA FWD LOWER CARGO COMPT.2L72 4F RTA35EU 20041102000172004110200017NM 2004 11 2 SWAA043074 120041022A5751 SKIN BOEING737 7373H4 1384600NM LT WING AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 102 23694 DURING SCHEDULED SERVICE CHECK, FOUND LT WING AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON PER MM. 2L72 4F RTA16WE 20041102000362004110200036NM 2004 11 2 DHL2004745534 120040720A5753 SKIN BOEING727 727224 1384076NM RT WING FOREFLAPDENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, RT WING I/B FOREFLAP L/E HAS A DENT WS 335. DAMAGED FOUND TO BE OUT OF LIMIT IAW B727 SRM 57-50-1 FIG 3. CUT OUT DAMAGED AREA & FABBED FILLER FROM 2024 T3 .050 PO 900980 DIM 2.6875 INCH X 2.5 INCH & 2 EA DOUBLERS FROM 2024 T3 .063 PO 900790 DIM 5.75 X 3.25 INCH & 5.75 X 2.25 INCH IAW B727 SRM 57-50-4 FIG 2. PARTS TREATED & PRIMED IAW B727 SRM 51-10-2 PARTS INSTALLED IAW B727 SRM 57-50-4 FIG 2. 2L73 4F A3WE 20041102000422004110200042NM 2004 11 2 2004UALA00770 120040812A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29395UA 24670 FUSE SKIN PANEL IS GOUGED AT BS 294, 12 INCHES BELOW LT ENTRY DOOR UPPER HINGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SKIN PANEL. 2L72 4F4 FRTA16WE E2GL 20041102000562004110200056NM 2004 11 2 UIEA200400160 120040921A575365B159591 FAIRING BOEING747 747230B 1384889NM NR 1 WORN A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, FOUND NR 1 MOVABLE CANOE PRIMARY DOOR FAIRING BEARINGS WORN. HOLE ELONGATION WAS FOUND IN TWO LOCATIONS. OVERSIZED THE HOLES TO A MAXIMUM DIAMETER OF .7827 INCHES. DRY PNETRANT INSPECTED THE AFFECTED AREA TO ENSURE DEFECT FREE CONDITION. INSTALLED ALUMINUM ALLOY REPAIR SLEEVE AT EACH AFFECTED HOLE, AND INSTALLED DESIGN TYPE BEARINGS USING SHRINK FIT AND ROLLER SWAGGING METHOD. THE STRUCTURE RESTORED TO ORGINAL DESIGN REQUIREMENTS. (M) 2L74 4F A20WE 20041102000702004110200070NE 2004 11 2 2004F00421 220041004A7200 ENGINE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR 2 SHUTDOWN A CEDAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 SW05233CA 133 AT FL370, THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED TO LIT WITHOUT INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOUR REQUEST AFTER MAINTENANCE HAS COMPLETED ITS INSPECTION. 2L72 4J4 J A10CE 1E16 20041102000792004110200079NM 2004 11 2 AMTA200401269 120041009A2420 GCU BOEING757 75733N 1384931NM APU FAILED A AMTAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL11552TZ 32586 LEFT GEN OFF, FOR T/S SWAPPED APU GCU P/N 734284F, S/N 6094 WITH LEFT ENGINE GCU P/N 734284F S/N 5859 BY EMPLOYEE NR 120887. PRESENT POSITION APU GCU S/N 5859, L ENGINE GCU S/N 6094. (M) 2L72 4F RTA2NM 20041102000812004110200081EA 2004 11 2 ASOA04656 120040829A3350601R461041 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN CONTAMINATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11886AS 7531 DURING CRUISE FROM ATL-YUL, THE CABIN EMERGENCY LIGHTS ILLUMINATED ON AND OFF TWICE. SUBSEQUENT TEST OF THE GREEN FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE ALSO. THE AIRCRAFT LANDED SAFELY IN YUL. MAINTENANCE FOUND MOISTURE IN THE EMERGENCY FLOOR LIGHT TRACKS AND REMOVED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041102000912004110200091WP 2004 11 2 UPS04843415 120041026A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE EMERGENCY LIGHT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01812UP 46112 EMERGENCY LIGHTS BATTERY LOW ON PREFLIGHT CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CK GOOD. 2L74 4F4 FRT4A25 E2GL 20041102000962004110200096SO 2004 11 2 SWIA200414006 120041022A2120 SMOKE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE CABIN/COCKPIT DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07215SW 120281 DURING ENGINE START, CABIN FILLED WITH SMOKE. INSPECTED BOTH LT AND RT PACKS FOUND OPERATING NORMAL. STARTED RT ENGINE. OPERATIONAL CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20041102001002004110200100WP 2004 11 2 ASMF200410015 120041019A291037723745503 SHUTOFF VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RUDDER FAILED W ASMFO OTHER O OTHER DEDESCENT 1 SW23583MD14929 49659 CAPTAIN REPORTED LOSS OF HYDRAULIC FLUID OF THE RT SYSTEM AND LANDING GEAR DOORS DID NOT OPEN IN A NORMAL WAY, OPENING THEM MANUALLY. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, RUDDER SHUTOFF VALVE WAS REPLACED IAW MM 27-20-09 AND MAIN LANDING GEAR DOORS WERE TESTED IAW MM 32-30-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20041102001042004110200104 2004 11 2 SWIA200413995 420041024A3418C818022 SERVO EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE STICK SHAK INOPERATIVE A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07221SW1500 1500 120290 CAPTAIN'S STICK SHAKER INOPERATIVE. REMOVED AND REPLACED CAPTAIN'S STICK SHAKER. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041102001132004110200113SO 2004 11 2 LR7A04195 120041028A5330 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 653 4590 DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5301, FOUND RT FS 407 EXTERNAL ESCAPE HATCH FWD UPPER CORNER CUTOUT CRACKED AT WL 226, RBL 80. REPAIRED IAW SRM SMP 583 53-40-50. NR 0027. 2H74 4T4 T A1SO E282 20041102001212004110200121NM 2004 11 2 DL733040998 120041028A2131 CONTROLLER BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU CABIN PRESSURE MALFUNCTIONED A DALAB EMER. DESCENT G MULTIPLE FAILURE CRCRUISE 1 SO27948WP 23259 AT 26K ALT CABIN BEGAN TO RISE RAPIDLY, EMERGENCY DESCENT WAS INITIATED. THE CABIN REACHED 15K, MASKS DROPPED. PERFORMED ALL REQUIRED TESTS, NO TROUBLE FOUND. 2L72 4F4 FRTA16WE E21EU 20041102001292004110200129NM 2004 11 2 SB04149 120041026A335020121 CHARGER BOEING737 7373B7 1384580NM FORWARD CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19528AU 24410 MAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041103000062004110300006EA 2004 11 3 SWIA200414014 120041024A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07432SW 7548 A STRONG FUEL SMELL COMES INTO THE CABIN WHEN SHUTTING DOWN NR 1 ENGINE AFTER LANDING WITH THE APU RUNNING. CHECKED VENT SYSTEM. PRESSURIZED A/C WITH ALL SYSTEMS AND PERFORMED SHUTDOWN PROCEDURES. NO INDICATION OF FUEL SMELL NOTED. NO DISCREPANCIES NOTED. 2L72 4F4 FRTA21EA E15NE 20041103000182004110300018SO 2004 11 3 LR7A04116 120041001A5312 BULKHEAD LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC3215 FOUND NLG BAY FS 93 BULKHEAD CRACKED ADJACENT TO FWD NLG DOOR LT HINGE FITTING AT WL 156, LBL 16.REPAIRED IAW SRM SMP 583 53-30-10 AND 53-30-1. NR 0415. 2H74 4T4 T A1SO E282 20041103000212004110300021SO 2004 11 3 LR7A04119 120041001A5312 PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG BAY FS 540 PANEL RISERS CORRODED AT WL 189, LBL 62. REPAIRED IAW EA 382-53-04-072. NR 0480. 2H74 4T4 T A1SO E282 20041103000362004110300036CE 2004 11 3 T2BA3 120041006A284211438904019 SENSOR BEECH 1900 1900C 1154161CE PWA PT6 PT6* 52043EA FUEL QTY MALFUNCTIONED E T2BAO OTHER J WARNING INDICATION CRCRUISE 1 SO15172TE UB24 LT FUEL QUANTITY ANNUNCIATOR ILLUMINATED THROUGHOUT ENTIRE FLIGHT 20 MINUTE FLIGHT, PERFORMED TROUBLESHOOTING OF FUEL INDICATING SYSTEM, FOUND THE LOW FUEL QTY. SENSOR TO BE MALFUNCTIONING, REPLACED PART IAW MANUFACTURERS RECOMENDATIONS, PERFORMED AN OPERATIONAL CHECK, SYSTEM WORKS PROPERLY, SIGNED OFF WRITE UP AND RELEASED AIRCRAFT FOR FLIGHT. 2L72 4T3 TRTA24CE E2NE 20041103000522004110300052NM 2004 11 3 AWXA200401172 120041014A534066142101 STRINGER CLIP BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK A .3750 INCH CRACK WAS FOUND IN STRINGER CLIP AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP; INSTALLED REPAIR PART IAW ER 03-5311-04295-ES1. 2L72 4F4 FRTA16WE E2GL 20041103000612004110300061WP 2004 11 3 DHL2004801009 120041013A2612 FIRE LOOP DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 1 ENGINE MALFUNCTIONED A DHLAFBA ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01801DH 46033 IN CRUISE FLT FIRE WARNING INDICATION ON NR 1 ENG. PERFORMED EMERGENCY CHECKLIST, LANDED AT ICT, FIRE WARNING PERSISTED THROUGHT OUT DESENT AND LANDING. TRANSFERED FIRE LOOP A ON DUAL LOOP SYSTEM TO DMI 18127 MEL REF 26-2-3 CAT C. DMI EXPIRES IN 10 CONSECUTIVE CALANDER DAYS. PLACARD INSTALLED IN NR 1 ENGINE IB AND OB FIRE WITH NEW BOTTLES REF MM 26-2. R/R NR 1 ENG RT FAN CASE DETECTOR ASSY PER DC-8 M/M 26-10-1 OPS CHECKS SERVICABLE. GROUND RAN AND TAXI A/C PER JRH ON "A" LOOP. NO DEFECTS NOTETHIS CLEARS DMI 18127 2L74 4F4 FRT4A25 E2GL 20041103000622004110300062WP 2004 11 3 P9RA20040046 120041012A335060030431 POWER SUPPLY DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1114816 49370 AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHTS INOPERATIVE AT ROW 26. REMOVED AND REPLACED POWER SUPPLY IAW MM. 2L72 4F4 F A6WE E9NE 20041103000662004110300066NM 2004 11 3 04FDEA02960 120041021A5531 SPAR DOUG MD11 MD11F 3023600NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR BERWEEN ZFR 389.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5530-81580. 2L73 4F4 FRTA22WE E23EA 20041103000702004110300070NM 2004 11 3 04FDEA02964 120041021A5531 SPAR DOUG MD11 MD11F 3023600NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT BETWEEN FWD CTR SPAR TO AFT CTR SPAR ZFR 328.0 LT SKIN EXTERIOR SURFACE FOUND CORRODED. CORROSION REMOVED & WITHIN LIMIT AS PER SRM55-00-01VOL1. 2L73 4F4 FRTA22WE E23EA 20041103000722004110300072WP 2004 11 3 DHL2004801560 120040927A55445656226 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RUDDER RIB CRACKED 1.000 ZR 105.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG.1, DWG 5656226. REMOVED CRACKED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB IAW SRM 55-6-1 PG.4 FIG.2 SHEET 2 DWG 5656226, SRM 51-1-4 PG.1. DPS 3.69-4. PERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG 1-13-17, DPS 7.00-1. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND RIB IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG.1, SRM 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20041103000742004110300074WP 2004 11 3 DHL2004801558 120041003A5330 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 AFT ACCY COMPT. INTERNAL SKIN CORRODED, STA 1640.000 TO STA. 1660.000, L-26 - L-27R PERFORMED MAJOR REPAIR IAW DWG W51-R04 FAA FORM 8110-3 DATED 10-01-04. REMOVED REPAIR DOUBLER IAW DWG W51-R04. REMOVED CORROSION IAW SRM 51-1-8 PAG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. TRIMMED OUT DAMAGED AREA IAW DWG W51-R04. FABRICATED EXTERNAL REPAIR DOUBLER (7075-T6AL 0.040) REPAIR TRIPLER (7075-T6AL 0.080) AND 2EA FILLERS (7075-T6 0.071, 0.032) IAW DWG W51-R04. CLEANED, TREATED AND PRIMED AREA, EXTERNAL REPAIR DOUBLER, REPAIR TRIPLER AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED FILLERS, REPAIR TRIPLER, EXTERNAL REPAIR DOUBLER IAW DWG W51-R04, SRM 51-1-2L74 4F4 FRT4A25 E2GL 20041103000762004110300076WP 2004 11 3 DHL2004801515 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA 952.000. CUT OUT WORN SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103000782004110300078WP 2004 11 3 DHL2004801514 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 4 TRACK PLUG LUGS WORN, STA 1580.000. REMOVED ORN PLUG IAW SRM 51-3-0 PG. 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103000802004110300080WP 2004 11 3 DHL2004801518 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA. 956.000. CUT OUT WORN SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IAW SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW SRM 51-3-0 PG. 1-2. 2L74 4F4 FRT4A25 E2GL 20041103001232004110300123WP 2004 11 3 COOSDR040035 120040816A573056488911 PANEL DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE LT WING CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 LT WING, FIXED PANEL NR 571, PN 5648891-1, WITH CORROSION AND DELAMINATED AT SEVERAL PLACES. 2L74 4F4 F 4A25 1E8 20041103001332004110300133SW 2004 11 3 2004F00417 120040928A2150 BEARING AIRESRCH SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP COOLING TURBINE SEIZED E E ENGINE SHUTDOWN BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 GL27620PA 49521 AC533 WHILE TAXIING TO THE RAMP AFTER LANDING, THE PILOT REPORTED A SMELL OF SMOKE IN THE CABIN AREA. FOLLOWING INVESTIGATION, IT WAS DETERMINED THAT THE ENVIRONMENTAL COOLING TURBINE BEARINGS HAD FAILED. THE TURBINE WAS REPLACED AND ALL ENVIRONMENTAL SYSTEMS CHECKED NORMALLY. 2L72 4T4 TRTA8SW E4WE 20041105000082004110500008NM 2004 11 5 SWAA043156 120041029A53306554767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STRINGER 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000102004110500010 2004 11 5 SWAA043139 420041028A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041105000232004110500023NM 2004 11 5 SWAA043187 120041102A57126545445 RIB BOEING737 7373H4 1384600NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND RT WING RIB AT WING STATION 135.5, LOWER AFT END CRACKED. REPAIRED RIB PER ER. 2L72 4F RTA16WE 20041105000252004110500025NM 2004 11 5 SWAA043188 120041102A531565C25723 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM LOWER CHORD AT BS 616, LBL 64, CRACKED. REPAIRED FLOORBEAM CHORD PER ER. 2L72 4F RTA16WE 20041105000262004110500026 2004 11 5 SWAA043189 420041102A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041105000282004110500028NM 2004 11 5 SWAA043165 120041028A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 19L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000312004110500031NM 2004 11 5 SWAA043174 120041102A3350100031 SIGN BOEING737 7373Q8 1384670NM EMERGENCY LIGHT WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGNCY EXIT SIGN WORN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20041105000352004110500035NM 2004 11 5 SWAA043161 120041029A21206577461 DUCT BOEING737 7373H4 1384600NM COCKPIT RESTRICTED A SWAAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW29325SW 23689 EQUIPMENT COOLING LIGHT ILLUMINATED. AUTOPILOT SYS DISCONNECTED AND FUMES ENTERED COCKPIT. FOUND INSTRUMENT COOLING AIRFLOW TO CAPT'S & F/O'S INSTRUMENT PANELS RESTRICTED. CLEANED DISTRIBUTION DUCT AND OPS CK GOOD PER MM. 2L72 4F RTA16WE 20041105000362004110500036NM 2004 11 5 SWAA043162 120041028A53306545769 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LT CUTOUT OF EXTERNAL A/C ACCESS HOOK UP. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041105000382004110500038 2004 11 5 SWAA043167 420041101A2565 GIRT BAR BOEING737 7372H4 138448CNM R2 DOOR SLIDE INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 18468679 22731 R2 DOOR EVACUATION SLIDE GIRT BAR WOULD NOT ARM AT FLOOR BRACKETS. REMOVED AND REPLACED SLIDE ASSY PER MM. 2L72 4F A16WE 20041105000392004110500039NM 2004 11 5 SWAA043168 120041031A3260 WARNING LIGHT BOEING737 7373H4 1384600NM MLG FALSE INDICATIONA SWAAO OTHER N FALSE WARNING APAPPROACH 1 SW29372SW 26599 RIGHT MLG UNSAFE LIGHT INDICATION DURING GEAR EXTENSION. RECYCLED GEARS AND GREEN LIGHTS ILLUMINATED. INSPECTED MLG POSITION SENSOR. NO DEFECT NOTED. MLG OPS CK GOOD PER MM 2L72 4F RTA16WE 20041105000422004110500042NM 2004 11 5 SWAA043164 120041028A53306551625 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 927 & BS 935, STR 24R TO STR 25R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000452004110500045NM 2004 11 5 SWAA043136 120041026A5753654648142 CARRIAGE BOEING737 7372H4 138448CNM LT WING TE FLAP SHEARED A SWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW29092SW 22964 DURING T/E FLAP EXTENSION, HEARD LOUD THUD, NEEDED RT AILERON TO FLY LEVEL. FOUND LT WIN INBD T/E FLAP CARRIAGE SPINDLE SHEARED. REMOVED AND REPLACED LT INBD T/E FLAP CARRIAGE ASSY PER MM. 2L72 4F A16WE 20041105000472004110500047NE 2004 11 5 SWAA043138 220041026A7250305391 GUIDE VANE BOEING737 7375H4 138449DNM GE CFM56 CFM56* 13802NE NR 1 ENGINE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 856168 DURING SCHEDULED C3 CHECK, FOUND NR 1 ENG 1ST STAGE LPT NGV CRACKED AT L/E. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20041105000482004110500048NM 2004 11 5 SWAA043154 120041029A53306560552 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STRINGER 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000512004110500051SO 2004 11 5 LR7A04096 120041001A5311 FRAME LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5321 FOUND FS 277 BELLY FRAME CORRODED AT WL 126 LBL 5 - LBL 10. REPLACED FRAME IAW DWG 356119 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041105000522004110500052SO 2004 11 5 LR7A04097 120041001A53113568595 FRAME LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5321 FOUND FS 317 BELLY FRAME CORRODED AT WL 126, LBL 1 - RBL 3. REPLACED FRAME IAW DWG 356119 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041105000542004110500054SO 2004 11 5 LR7A04099 120041001A53153556712L2R FITTING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HSP53262 FOUND FS 477 LT AND RT LOWER BEAM ATTACHMENT FITTINGS CRACKED AT WL 143, LBL 61 AND RBL 61. REPLACED FITTINGS IAW DWG 356245 AND SRM 583 51-70. 2H74 4T A1SO 20041108000032004110800003NM 2004 11 8 EIA2004135 120041007A5320 WEB BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE WHEEL WELL CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 1.1 INCH CRACK ON NOSE WHEEL WELL BOX WEB, STA. 340, RBL 15, WL 150. REMOVED DAMAGED WEB, FABBED AND INSTALLED REPLACEMENT PARTS IAW ECRA 470-53-207-2 2L74 4F4 F A20WE E20EA 20041108000052004110800005NM 2004 11 8 EIA2004096 120040713A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 27A R FROM BS 320-340 HAS SEVERAL FASTENER HOLES CRACKED. REMOVE DAMAGE, FAB & INSTL NEW STRINGER PER SRM 51-20-01 & 51-30-02. 2L74 4F A20WE 20041108000062004110800006NM 2004 11 8 EIA2004100 120040603A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 WEB BETWEEN FLOORBEAM STA 320-330, STR 12L IS CRACKED. REMOVED DAMAGED WEB, FAB & INSTL PER B747 SRM 51-30-02, 51-10-02, 51-20-01, & SOPM 20-41-02 2L74 4F A20WE 20041108000072004110800007NM 2004 11 8 EIA2004095 120040630A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSLEAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 FLOORBEAM MAIN CABIN BS 1740 RBL 33-99 HAS 4 ELONGATED HOLES COMMON TO SEAT TRACK. REMOVE DAMAGED SECTION OF TEE CHORD BEAM BS 1740 RBL 33.99 & REPLACE WITH NEW SECTION PER B747 SRM 53-10-07 & 51-30-02 2L74 4F A20WE 20041108000082004110800008NM 2004 11 8 EIA2004106 120040923A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 420 FLOORBEAM UPPER DECK, UPPER CHORD FWD FLANGE. HOLE AT RBL 52.0 WAS REAMED TO MAX 0.34 DIAM, WITH CRACK INDICATIONS REMAINING. MUST BE REPAIRED PER SB. REPAIR HOLE BS 420, RBL 52.0 FWD HORIZ FLANGE PER SB 747-53-2439, FIG 9, SHT 1-6 2L74 4F A20WE 20041108000102004110800010NM 2004 11 8 EIA2004105 120040907A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 41L STA 260-280 FOUND CRACKED DURING INSULATION BUY BACK. R&R STRINGER SECTION 41L @ STA 260-280, PER B747 SRM 51-30-02, PG 2-3 & 8-9 2L74 4F A20WE 20041108000112004110800011NM 2004 11 8 EIA2004101 120040602A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 31A CRACKED AT FS 500L. FAB & INSTL NEW STR & SPLICE CHANNELS PER B747 SRM 53-10-03, SHTS 6&7, 51-30-02, PGS 2-3 & 8-9. 2L74 4F A20WE 20041108000122004110800012EA 2004 11 8 COMA0460593 120041101A2820228143 PUMP CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01431CA9933 7472 FLIGHT 4973 FUEL INBALANCE CAUTION MESSAGE. REPLACED THE CROSS FLOW PUMP. 2L72 4F RTA21EA 20041108000132004110800013EA 2004 11 8 COMA0470077 120041031A5230 LATCH CNDAIRCL600 CL6002C10 1390015EA CARGO DOOR DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01659CA 10153 FLIGHT 5540 CARGO DOOR CAUTION MESSAGE. LATCH BUTTON ON DOOR HANDLE STUCK. CLEANED PUSH BUTTON, OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041108000162004110800016EA 2004 11 8 COMA0460594 120041101A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA RADAR ALTIMETER UNSECURE A COMAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO01995CA 7229 FLIGHT 5532 F/O'S RADAR ALTIMETER IS INTERMITTENT. RESECURED COAX CONNECTOR ON NR 2 RADIO ALTIMETER. 2L72 4F RTA21EA 20041108000182004110800018NM 2004 11 8 CALA0400699 120041102A3350 SIGN BOEING737 7373T0 1384582NM LEFT AFT CABIN SHORTED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2777303 23354 THE LEFT AFT EMERGENCY EXIT SIGN WAS FOUND SHORTED. THE EXIT SIGN WAS REPLACED. 2L72 4F RTA16WE 20041108000192004110800019NM 2004 11 8 P5CA0401266 120041030A80117401793 STARTER BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 1 ENGINE MALFUNCTIONED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 689169 NR 1 ENGINE WOULD NOT TURN ON, PYLON VALVE & START VALVE INDICATES OPEN. REPLACED STARTER, OPS CHECK OK PER AMM 80-11-00. 2L74 4F4 F A20WE E3NE 20041108000202004110800020NM 2004 11 8 P5CA0401267 120041031A7697 CONNECTOR BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE ENGINE DIRTY A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23920FT 22237 702192 FUEL CONDITION ACTUATOR NR 1 ENGINE CIRCUIT BREAKER POPPED ON ENGINE START. REMOVED, CLEANED & REINSTALLED CONNECTOR AT J14-P, PERFORMED SYSTEM CHECK, GOOD PER AMM 76-11-00. 2L74 4F4 F A20WE E3NE 20041108000222004110800022NM 2004 11 8 04296421 120041022A2430 GCU DORNERDO32 DO328300 NM DC GENERATOR MALFUNCTIONED A VTZAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 EA27421FJ 3179 A/C HAD A GENERATOR DIFFERED, APU FAILED, DIVERSION TO ROA. MX REMOVED AND REPLACED DC GCU IAW JIC 24-31-03. OPS CHECK GOOD. CLEANED APU GENERATOR CONNECTORS IRT 49-10-10. REMOVED AND REPLACED BPCU IAW JIC 24-61-10, OPS CHECK GOOD. A/C OK TO CONTINUE SERVICE. 2H72 4T RTA55NM 20041108000272004110800027SO 2004 11 8 RAIA00410024 120041029A2913100FU001100 FUSE EMB 145 EMB145LR 3260212SO HYD PUMP FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03811HK 145256 PIT - NUMBER 1 ELECTRIC HYD PUMP INOP. MAINTENANCE REMOVED AND REPLACED NUMBER 1 HYD PUMP FUSE. 2L72 4T RTT00011AT 20041108000282004110800028SO 2004 11 8 RAIA00410025 120041031A5610 SEAL EMB 145 EMB145ER 3260211SO COCKPIT WINDOW FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03826HK 145016 NOISES NOTED WHILE CLIMBING THROUGH 15,000 FT. PRESSURIZATION REMAINED UNCHANGED. MAINTENANCE INSPECTED AND FOUND F/O'S TEMP SEAL TAPE HAD BLOWN AWAY FROM SEAL. RESEAL F/O'S SEAL WITH SPEED TAPE. 2L72 4F RTT00011AT 20041108000292004110800029WP 2004 11 8 RAIA00410026 220041031A7421Y2092 IGNITER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33112UHR WP RIGHT ENGINE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03574HK 41093 76110 STL - RIGHT ENGINE HUNG START AT 20 PERCENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IGNITERS. 2L72 4T4 TRTA41NM E4WE 20041108000312004110800031EU 2004 11 8 RAIA00411001 120041102A302031055016 SENSOR JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03552HK4203 41057 LEFT IEC FAIL WITH ENGINE ANT-ICE SELECTED ON. MAINTENANCE REPLACED LEFT ENGINE PT2 SENSOR. 2L72 4T RTA41NM 20041108000352004110800035EA 2004 11 8 04277703 120041003A4920 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY CONTAMINATED A VTZAB EMER. DESCENT BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 EA27703BR 7467 LAV SMOKE INDICATION. DECLARED EMERGENCY RTF, LANDED SAFELY. MX PERFORMED ENGINE RUN WITH APU ON, GOT OIL SMELL AND FOUND OIL IN APU ENCLOSURE. 2L72 4F RTA21EA 20041108000362004110800036EA 2004 11 8 04306636 120041101A3260 BRACKET CNDAIRCL600 CL6002B19 1900309EA TARGET LOOSE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27636BR 7307 MX FOUND RIGHT MLG UPLOCK PROXIMITY SENSOR TARGET BRACKET LOOSE. MANUAL MANIPULATION OF THE TARGET WITH THE GEAR RETRACTED CAUSED GEAR TO GO FROM SAFE TO UNSAFE AND PRODUCE A GEAR DISAGREE WARNING. TIGHTENED, ADJUSTED, AND SAFETIED PROXIMITY SENSOR TARGET TO WITHIN LIMITATIONS OF CRJ AMM 32-61-05. SYSTEM OP CHECK GOOD DURING RETRACT CHECK. 2L72 4F RTA21EA 20041108000372004110800037NM 2004 11 8 04276406 120041002A3244 TIRE DORNERDO32 DO328300 NM NLG OUT OF ROUND A VTZAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA27406FJ 3156 VIBRATION IN NOSE LANDING GEAR DURING CLIMB. RTF. MX PERFORMED DETAILED INSPECTION OG NLG, NOSE GEAR BAY, NOSE GEAR DOORS, RADOME. NO DEFECTS NOTED, FOUND NLG TIRES OUT OF ROUND. REMOVED AND REPLACED LT & RT TIRES IAW DORNIER 328 JIC 32-41-01, LANDING GEAR INSPECTION JIC 32-11-00. 2H72 4T RTA55NM 20041108000382004110800038EA 2004 11 8 04299634 120041025A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27634BR 7287 EVENT SUMMARY STATES THAT FLAP FAIL AT 8 DEGREES. REMOVED AND REPLACED BPSU REF CRJMM 27-51-10. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108000412004110800041EA 2004 11 8 04301709 120041027A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM DISCONNECTED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27709BR 7850 ANTI ICE DUCT WARNING MESSAGE DURING FLIGHT. CREW RTF. MX RECONNECTED CONNECTOR TO BLCU, REPINNED SLICE SP20WK, REMOVED AND REPLACED TEFLON SHOULDER WASHER AT TB40WK. 2L72 4F RTA21EA 20041108000432004110800043EA 2004 11 8 04251625 120040904A2910 TUBE CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYSTEMLEAKING A VTZABA EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27625BR 7214 EVENT SUMMARY STATED EMERGENCY DECLARED FOR HYD 2 LOW PSI MSG. A/C LANDED SAFELY AT GATE. REMOVED AND REPLACED RT LOWER FAIRING. REMOVED AND REPLACED RETURN TUBE ASSY, RESERVOIR TUBE ASSY, FILL TUBE ASSY FOR NR 2 HYD. INSTALLED SCREWS ON RT ENGINE PYLON. 2L72 4F RTA21EA 20041108000442004110800044EA 2004 11 8 04276686 120041002A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS FALSE ACTIVATIONA VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27686BR 7715 UPON TAKEOFF, RECEIVED LOW SPEED ABORT. CREW CLEARED SPOILER FAULT, AND DID ANOTHER UNEVENTFUL TAKEOFF. 2L72 4F RTA21EA 20041108000452004110800045EA 2004 11 8 04279694 120041005A3320 BALLAST CNDAIRCL600 CL6002B19 1900309EA LAVATORY SMOKE A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27694BR 7768 BLUE SMOKE IN AFT OF CABIN DUE TO BAD LAV LIGHT BALLAST. 2L72 4F RTA21EA 20041108000482004110800048NM 2004 11 8 04243424 120040830A7797 WIRE HARNESS DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DEFECTIVE A VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27424FJ 3185 PCECD0088 ABNORMAL N2 INDICATIONS ON THE RT ENGINE DURING TAKEOFF. ABORTED TAKEOFF AT 65 KNOTS. MX REMOVED AND REPLACED OUTER WIRING HARNESS IAW JIC 73-20-04. 2H72 4T4 FRTA55NM E35NE 20041108000502004110800050EA 2004 11 8 04292703 120041018A3620 LINE CNDAIRCL600 CL6002B19 1900309EA 10TH STAGE BLEEDLEAKING A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27703BR 7467 EVENT SUMMARY STATED THAT SMOKE IN THE LAV INDICATION, EMERGENCY DECLARED. REMOVED AND REPLACED 10TH STAGE BLEED LINES. DID LEAK CHECK. 2L72 4F RTA21EA 20041108000512004110800051NM 2004 11 8 P5CA0401264 120041029A242128B26313B GENERATOR BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 1 ENGINE MALFUNCTIONED A P5CAD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 EA15920FT 22237 702192 NR 1 ENGINE GENERATOR FEEDER FAULT. REMOVED AND REPLACED NR 1 ENGINE GENERATOR PER AMM 24-21-01, SYSTEM OPS CHECK OK. 2L74 4F4 F A20WE E3NE 20041108000522004110800052NM 2004 11 8 P5CA0401265 120041029A242128B26313B GENERATOR BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE FAILED A P5CAD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 EA15920FT 22237 702238 NR 2 ENGINE GENRATOR WILL NOT COME ON LINE. REMOVED AND REPLACED NR 2 ENGINE GENERATOR, OPS CHECK OK PER AMM 24-21-01. 2L74 4F4 F A20WE E3NE 20041108000542004110800054EA 2004 11 8 09272651 120040928A3020 VALVE CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FAILED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27651BR 7426 EVENT SUMMARY STATED REJECTED TAKEOFF AT 40KT DUE TO LT COWL ANTI-ICE CAUTION MSG. TROUBLESHOOTING CONFIRMED THE PROBLEM, AND RTG. REMOVED AND REPLACED LT COWL ANTI ICE VALVE REF AMM 30-22-01. PERFORMED OPS CHECK OF ANTI ICE. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108000552004110800055EA 2004 11 8 0927270609 120040928A2840 COMPUTER CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27706BR 7553 EVENT SUMMARY STATED FUEL WARNING AND FUEL IMBALANCE INDICATIONS AFTER TAKEOFF; DECLARED EMERGENCY; LANDED UNEVENTFULLY. REMOVED AND REPLACED FUEL COMPUTER IAW CRJ AMM 28-41-16, OPS CHECK GOOD. INDICATIONS NORMAL. 2L72 4F RTA21EA 20041108000562004110800056EA 2004 11 8 04252647 120040904A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A VTZAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA27647BR 7399 ON DESCENT F/A NOTICED ELECTRICAL SMELL THAT WENT AWAY ON FINAL. INSPECTED CABIN FOUND NO EVIDENCE OF BURNING. INSPECTED AVIONICS BAY. FOUND NO EVIDENCE OF BURNING REF AMM 33-21-00 & WM 20-11-00. A/C OK TO CONTINUE SERVICE AT THIS TIME. 2L72 4F RTA21EA 20041108000572004110800057EA 2004 11 8 042526490 120040907A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAO OTHER L NO TEST NRNOT REPORTED 1 EA27649BR 7414 FWD EMERGENCY FLOOR TRACK LIGHTS INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT POWER STRIP REF MM 33-51-01. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108000582004110800058EA 2004 11 8 04252659 120040907A4910 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SHUTDOWN A VTZAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA27659BR 7509 APU AUTO SHUTDOWN WITH OIL TEMP MSG. OPENED DM2514110-1 IAW MEL 49-10-01 CAT C. 2L72 4F RTA21EA 20041108000592004110800059NE 2004 11 8 04252702 220040907A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT INOPERATIVE A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27702BR 7462 LEFT ENGINE WOULD NOT SHUTDOWN WHEN THRUST LVR SET TO CUT OFF. C/W TWO ENGINE START/SHUTDOWN SEQUENCES IAW AMM 71-00-00-868-807. NO DEFECTS WERE NOTED DURING EITHER SHUTDOWN. OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041108000602004110800060EA 2004 11 8 0425262109 120040907A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WINGS FAILED A VTZAO OTHER O OTHER NRNOT REPORTED 1 EA27621BR 7186 FLAPS FAIL MSG AT 0 DEG. CYCLED POWER ON A/C PERFORMED. OPS CHECK OF FLAPS. OPS CHECK OK REF CRJ MM 27-53-00. 2L72 4F RTA21EA 20041108000622004110800062EA 2004 11 8 04270621 120040926A3230 VALVE CNDAIRCL600 CL6002B19 1900309EA NLG INOPERATIVE A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27621BR 7186 ON APPROACH, GEAR DISAGREE PROCEEDED WITH MISSED APPROACH. MANUAL GEAR EXTENSION, ABLE TO TAXI TO THE GATE. REMOVED AND REPLACED NLG PRIORITY VALVE, NLG SELECTOR VALVE, NR 3 A-HYD SYS ACMP PUMP, NLG BYPASS VALVE, MLG SELECTOR VALVE. 2L72 4F RTA21EA 20041108000632004110800063 2004 11 8 RAIA00409015 420040918A34177000700967 ADC JETAIRJETSTMJETSTM4101 1500501EU NR 2 INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03553HK195611363 41066 PIT - ADC NR 2 FAILED. MAINTENANCE REMOVED AND REPLACED NR 2 ADC. 2L72 4T RTA41NM 20041108000642004110800064 2004 11 8 RAIA00409013 420040917A3442 TRANSCEIVER JETAIRJETSTMJETSTM4101 1500501EU WX RADAR SYS INOPERATIVE A RAIAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 CE03562HK 41078 SYR - WEATHER RADAR INOP. MAINTENANCE RESET POWER AND OPS CHECKED. 2L72 4T RTA41NM 20041108000662004110800066NE 2004 11 8 RAIA00409011 220040914A732131059007 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE RT ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03567HK5179 41085 75126 XNA - RT ENGINE OIL PRESSURE ZERO AND RPM FLUX. MAINTENANCE REMOVED AND REPLACED 32 ENGINE FUEL CONTROL. 2L72 4T4 TRTA41NM E18NE 20041108000682004110800068 2004 11 8 RAIA00409014 420040917A34427008470822 TRANSCEIVER JETAIRJETSTMJETSTM4101 1500501EU WX RADAR SYS INOPERATIVE A RAIAA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 CE03572HK13404362 41091 PIT - WEATHER RADAR INOP. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR RT. 2L72 4T RTA41NM 20041108000692004110800069EA 2004 11 8 0426168709 120040917A3230 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG INOPERATIVE A VTZAB EMER. DESCENT O OTHER APAPPROACH 1 EA27687BR 7720 GEAR DISAGREE/NOSE DOOR WARNING ON APPROACH. REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE S/N ON 0521, S/N OFF 2058 REF AMM 32-33-10. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108000702004110800070 2004 11 8 RAIA00408032 420040829A34180020BN4 COMPUTER EMB 145 EMB145LR 3260212SO STALL WARNING MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03835HK862 145670 ALB - STALL PROTECTION SYSTEM NR 1 INOP. MAINTENANCE REMOVED AND REPLACED NR 1 STALL PROTECTION COMPUTER. 2L72 4T RTT00011AT 20041108000712004110800071EU 2004 11 8 RAIA00409024 120040924A3244 TIRE JETAIRJETSTMJETSTM4101 1500501EU NLG UNDERSERVICED A RAIAC ABORTED TAKEOFF W INADEQUATE Q C TOTAKEOFF 1 CE03553HK 41066 NOSE WHEEL STEERING UNRESPONSIVE AND AIRCRAFT PULLS RIGHT. MAINTENANCE SERVICED RIGHT MAIN TIRE AND FLIGHT CREW DID HIGH SPEED TAXI CHECK. 2L72 4T RTA41NM 20041108000722004110800072EU 2004 11 8 RAIA00409021 120040922A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A RAIAD RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 CE03564HK9442 379 41081 STL - LEFT GENERATOR WENT OFF LINE WHEN POWER LEVERS WERE PUSHED FORWARD. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER/GENERATOR. 2L72 4T RTA41NM 20041108000732004110800073SO 2004 11 8 RAIA00409023 120040926A32511170A180001 POTENTIOMETER EMB 145 EMB145 3260210SO NLG STEERING FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03801HK1520315203 145053 RIC - WHEN TURNING LEFT STEERING PRODUCED A RATCHETING SOUND WITH NO STEERING MOVEMENT UNTIL TILLER OR RUDDER PEDALS MOVED ABOUT 10 DEGREES. MAINTENANCE REMOVED AND REPLACED STEERING FEEDBACK POT. 2L72 4F RTT00011AT 20041108000742004110800074EU 2004 11 8 RAIA00409022 120040923A243651539019E GCU JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A RAIAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 CE03564HK1411119 41081 STL - LEFT ENGINE GENERATOR DROPPED OFF LINE DURING TAXI. MAINTENANCE REMOVED AND REPLACED GCU. 2L72 4T RTA41NM 20041108000782004110800078WP 2004 11 8 ABXA040363 120041031A5330564932957 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 FUSELAGE EXTERIOR SKIN BULGED AND FASTENERS HEAD SHEARED LEFT SIDE OF TAILSKID FAIRING. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED DOUBLER REPAIR, TREATED, ALODINED AND PRIMED IAW DC-8 SRM 51-1-21, 53-2-1, 51-1-8, 51-1-20, AND REA D853-50297-MR. 2L74 4F 4A25 20041108000802004110800080WP 2004 11 8 ABXA040366 120041030A533057552713 SKIN DOUG DC8 DC863F 302198FWP FUSLEAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 FORWARD CARGO RIGHT SIDE FROM STA 200 - 220, BETWEEN LONGERON 33 RIGHT - 34 RIGHT, SKIN CORRODED WITH BROKEN RIVETS. REMOVED SHEAR TIES, INSTALLED FINGER DOUBLERS, EXTERNAL DOUBLERS, FILLER AND INTERNAL DOUBLERS AND SHEAR TIES IAW REA D853-50304-MR AND DC-8 SRM 51-1-21 AND 51-1-20D. ALODINED AND PRIMED PARTS IAW DC-8 SRM 51-1-8. INSTALLED DRAIN COVER IAW DC-8 SRM 51-1-21. 2L74 4F 4A25 20041108000862004110800086SO 2004 11 8 RAIA00409003 120040905A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03824HK 145498 STL - MID CABIN OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE RE-SECURED ELECTRICAL CONNECTOR TO OVERWING EXIT LIGHT ASSY. 2L72 4T RTT00011AT 20041108000882004110800088 2004 11 8 RAIA00409004 420040906A3418 VANE JETAIRJETSTMJETSTM4101 1500501EU AOA SYS OUT OF POSITION A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03553HK 41066 CHO - STALL WARNING INDICATION ON TAKEOFF ROLL. MAINTENANCE FOUND LT AOA VANE IN VERTICAL POSITION AND REPOSITIONED VANE TO NEUTRAL POSITION. 2L72 4T RTA41NM 20041108000932004110800093NM 2004 11 8 04274421 120040930A291342152 PUMP DORNERDO32 DO328300 NM HYD SYSTEM OVERTEMP A VTZAO OTHER MJ OVER TEMP WARNING INDICATION DEDESCENT 1 EA27421FJ 3179 HYD PUMP-A OVERHEAT CAS MESSAGE ON DESCENT. THEREFORE EMERGENCY LANDING GEAR EXTENSION. MX REMOVED AND REPLACED HYDRAULIC A-PUMP IAW JIC 29-11-04 OPS CHECK & LEAK CHECK GOOD. RESET GEAR EMERGENCY EXTENSION IAW JIC 32-31-00. 2H72 4T RTA55NM 20041108000942004110800094EA 2004 11 8 04268681 120040925A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27681BR 7680 CREW REPORT STATED DURING CLIMB RECEIVED A PROX SYS FAULT STATUS MSG. RESET PER QRH, MSG CLEARED. REMOVED AND REPLACED PSEU. PROX SYSTEM TEST GOOD. 2L72 4F RTA21EA 20041108000952004110800095EA 2004 11 8 04302671 120041028A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN AIR CONTAMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27671BR 7572 EVENT SUMMARY STATED THAT RTN FROM FLT. SMOKE TOILET CAUTION MSG AFTER T/O. RAN PACKS OFF BOTH APU AND ENGINES. COULD NOT FIND EVIDENCE OF SMOKE. REMOVED AND REPLACED LAV SMOKE DETECTOR. REMOVED AND REPLACED BOTH COALESCER BAGS. 2L72 4F RTA21EA 20041108000962004110800096EU 2004 11 8 RAIA00407010 120040716A5220 DOOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY EXIT UNSECURE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03564HK 41081 STL - EMERGENCY EXIT WARNING DURING TAKEOFF ROLL. MAINTENANCE RE-SECURED AFT EMERGENCY EXIT. NO OTHER DEFECTS NOTED. 2L72 4T RTA41NM 20041108000992004110800099SO 2004 11 8 RAIA00410003 120041008A77147013348949 DAU EMB 145 EMB145LR 3260212SO NR 1 MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03812HK10092 145373 STL - LEFT ENGINE LOW N1. MAINTENANCE REMOVED AND REPLACED NR 1 DAU. 2L72 4T RTT00011AT 20041108001002004110800100NE 2004 11 8 04271659 220040927A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 VIBRATES A VTZAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 EA27659BR 7509 CREW REPORT STATED, SETTING THRUST FOR TAKEOFF CREW NOTICED A LEFT HAND N2 VIBE GAUGE AND ABORTED THE TAKEOFF. TAXIED TO THE GATE. WO HAS BEEN OPENED. NOW IS IN APPR STATUS. 2L72 4F4 FRTA21EA E15NE 20041108001022004110800102NM 2004 11 8 P5CA0401259 120041020A361065B9453216 DUCT BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 4 ENGINE RUPTURED A P5CAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA15355MC 23395 530389 NR 4 ENGINE FIRE/FAULT LOOPS A&B BOTH SHOWED A CONTINUOUS RISE IN TEMP, CLOSED BLEED AIR VALVE, TEMPRATURE DROPPED TO NORMAL. RETARDED THROTTLE TO IDLE. T/S & FOUND S-DUCT IN PYLON RUPTURED. REPLACED DUCT & CLAMPS PER AMM 36-11-00, NO LEAKS NOTED. 2L74 4F4 FRTA20WE E23EA 20041108001042004110800104EU 2004 11 8 RAIA00409017 120040921A2750TY175802 SELECTOR JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03559HK 41075 XNA - WHEN FLAPS SELECTED TO 9 DEGREES FOR TAKEOFF, WENT TO 15 DEGREES. MAINTENANCE REMOVED AND REPLACED FLAP SELECTOR HANDLE. 2L72 4T RTA41NM 20041101001272004110100127NM 2004 11 1 DHL2004745541 120040804A5340 BRACKET BOEING727 727224 1384076NM AIRSTAIR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, AFT AIRSTAIRS LT SIDE STA 1223 BRACKET ABOVE FLOW CNTL VALVE CRACKED (MARKED IN RED). REMOVED AIRSTAIRS LT SIDE STA 1223 BRACKET 951209 ABOVE CNTL VALVE IAW B727 SRM 51-30-2, FABRICATED BRACKET 951209 FROM 2024-T3 .032 SIDE 21 X 2 INCH PO 9001135 IAW B727 SRM 53-10-2, TREATED AND PRIMED 951209 PART IAW 727 SRM 51-10-2, REINSTALLED BRACKET 951209 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041101001302004110100130NM 2004 11 1 DHL2004753001 120040806A3210 DEFLECTOR BOEING727 727223 1384074NM LT MLG TIRE INTERFERENCE A DHLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01753DH 22468 EXPERIENCED SEVERE VIBRATION SHAKING WHOLE ACFT IMMEDIATELY AFTER LIFT OFF VIBRATION STOPPED AFTER GEAR WAS RETRACTED. FOUND LEFT MAIN GEAR LEFT TIRE GRAVEL DEFLECTOR RUBBING/TOUCHING TIRE. ADJUSTED DEFLECTOR PER MM 32-11-61, NO DEFECTS NOTED. NO ABNORMAL WEAR NOTED DUE TO TOUCHING. 2L73 4F A3WE 20041101001352004110100135NM 2004 11 1 DHL2004745529 120040712A5313 STRINGER BOEING727 727224 1384076NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, STR 21 RT IS CORRODED JUST FWD OF STA 740 BULKHEAD. CUT OUT DAMAGED SECTION OF STRINGER 730 TO 740 DIM 10 INCHES AND FABBED STR FROM BAC 149G-131 PO 3323107 DIM 10 INCHES & SPLICE FROM BAC 1498-142 PO 900878 DIM 14 INCHES IAW 727 SRM 53-10-3 FIG 1. PARTS TREATED, PRIMED & INSTALLED IAW 727 SRM 51-10-2 & 53-10-3 FIG 1. 2L73 4F A3WE 20041101001482004110100148SO 2004 11 1 C2XA04BT106 120041010A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714939 145030 CREW REPORTED EMERGENCY SIGN ABOVE ROW 12 LEFT SIDE INOPERATIVE. REPLACED THE NUMBER 4 INVERTED. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041102000182004110200018NM 2004 11 2 SWAA043075 120041022A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041102000252004110200025NM 2004 11 2 2004UALA00864 120040908A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 EXTERIOR FUSELAGE AT BS 760, STR 16L, SKIN DENTED OUT OF LIMITS 2 PLACES. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER - TRIPLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041102000262004110200026NM 2004 11 2 2004UALA00865 120040908A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 FUSELAGE STRINGER REPAIR SPLICE AT BS 570, STR 16L REQUIRES REPLACEMENT AND REPOSITIONING DUE TO SKIN SPLICE REPAIR AND SHARING OF COMMON FASTENERS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041102000322004110200032NM 2004 11 2 2004UALA00934 120041012A5743 SUPPORT BEAM BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE RT MLG CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29902UA 25002 RIGHT MLG SUPPORT BEAM TO REAR SPAR FITTING CRACKED. REPLACED MLG SUPPORT BEAM FITTING. 2L72 4F4 FRTA16WE E2GL 20041102000342004110200034NM 2004 11 2 SWAA043124 120041027A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041102000502004110200050NE 2004 11 2 DHL2004804004 220040812A7261 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE NR 2 LEAKING A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01804DH 46124 ACFT EXPERIENCED A SUDDEN LOSS OF OIL QUANTITY AND PRESSURE THAT CAUSED THE FLIGHT CREW TO PERFORM EN ROUTE ENGINE SHUTDOWN OF THE NR 2 ENGINE. 2L74 4F4 FRT4A25 E2GL 20041102000552004110200055 2004 11 2 2004F00418 420040819A22007771378001 COUPLER BOEING747 747230B 1384889NM LT WING FAILED A Q2SAA UNSCHED LANDING O OTHER CRCRUISE 1 NE03740SA 21380 EN ROUTE FROM PANC TO RDSI AT FL320, IN CRUISE MODE, WHEN HF NR 1 MIC IS KEYED THE FOLLOWING DISCREPANCY WAS NOTED, 'WITH AUTOPILOT ENGAGED AND AUTOTHROTTLES ENGAGED, AIRCRAFT EXPERIENCED THREE SEVERE RIGHT YAWS. THE LAST TWO WERE WITH THE AUTOTHROTTLES DISENGAGED. AIRCRAFT MADE AN UNEVENTFUL RETURN TO PANC. REMOVED AND REPLACED NR 1 HF COUPLER IAW AMM 23-11-03. AUTOPILOT FUNCTIONS PROPERLY IAW AMM 22-10-00. (M) 2L74 4F A20WE 20041102000722004110200072EA 2004 11 2 REXA04020 120041007A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A REXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO258908D1581 7908 FLAP FAILURE ON TAXI. REMOVED AND REPLACED FECU, FLAP ELECTRONIC CONTROL UNIT. (M) 2L72 4F RTA21EA 20041102000862004110200086EA 2004 11 2 ASOA04657 120040829A5210601R314291 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11862AS 7476 DURING APPROACH INTO ATL FROM DHN, THE CREW RECEIVED A RED PASSENGER DOOR EICAS MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE FLIGHT ATTENDANT REPORTED HEARING AIR SLOW IN THE DOOR AREA AND THAT THE DOOR HANDLE HAD POPPED OVER THE TOP DEAD CENTER POSITION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE ADJUSTED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041102000872004110200087NM 2004 11 2 UIEA200400171 120040922A3697 WIRE BOEING747 7472D7B 1384803NM BLEED SYSTEM DAMAGED A UIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15526MC 22337 DURING CLIMB AT FL15.0, NR 4 ENG NACELLE 'B' IND WENT OT 6.0. 'A' IND 3.1. THRUST LEVEL 110.0, N1 & EGT NORMAL ON ALL ENGS. 'B' IND RETURNED TO 3.5 AT FL25.0 WITH CLIMB POWER SET. NR 4 ENG 'A' & 'B' INDS WENT TO 8,0 & EGT ON NR 4 ENG WENT TO 940 & NR 4 THRUST LEVER RETARDED & FHB PROCEDURES COMPLIED WITH. NR 2 BLEED AIR VALVE CLOSED HI STAGE LIGHT REMAINED ON & 'A' & 'B' INDS RETURNED TO 3.0. FOUND RT CORE LOOP CONNECTOR WIRING DAMAGED. R & R CONNECTOR. REPAIRED SERVERAL WIRES AT DIFFERENT LOCATIONS ON ENG ACCY PER MM. FOUND OVER PRESSURE VALVE LEAKING DURING LEAK CHECKS. R & R OVER PRESS VALVE ACC MM. LEAK CHECK SATISFACTORY. CHKD ALL DUCTS ON ENG & NO DEFECTS FOUND. R & R OVER PRESSURE VALVE ACC P2L74 4F RTA20WE 20041102000882004110200088EA 2004 11 2 ASOA04654 120040828A3350362624 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO11820AS 7188 DURING AN OVERNIGHT CHECK IN SHV, THE EMERGENCY FLOOR LIGHT SECTION AT ROW 1-C WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 1-C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20041102000892004110200089NM 2004 11 2 UIEA200400154 120040901A5347631101174 SEAT TRACK BOEING747 7472D7B 1384803NM FUSELAGE DAMAGED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15526MC 22337 MAIN DECK SEAT TRACK CROWN DAMAGE 3 INCHES AT STATION 1802. DAMAGED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 51-10-05. (M) 2L74 4F RTA20WE 20041102000982004110200098SO 2004 11 2 LR7A04112 120041001A5312 PRESSURE PANEL LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323, FOUND LT FS 597-617 PRESSURE PANEL CRACKED AT, WL 260, LBL 61. REPAIRED IAW EA 382-53-04-070. NR 0307. 2H74 4T4 T A1SO E282 20041102001012004110200101WP 2004 11 2 NACA20040050 120040724A5330 SKIN DOUG DC6 DC6A 3021706WP PWA R2800 R2800* 52026NE FUSELAGE DAMAGED A NACAK NONE O OTHER ININSP/MAINT 1 AL0399330 43576 HOLE IN FUSELAGE AFT OF THE REAR CARGO DOOR AT STA 807.5L TO 822L. REMOVED DAMAGE AND FABRICATED A NEW PATCH FROM 0.80 7075-T6. REF: DOHM FIGURE 12-22. 2L74 4R4 R 6A3 5E8 20041102001022004110200102EA 2004 11 2 QXEA200400727 120041023A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE FWD CARGO BAY TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09600QX7249 10005 DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND THE FORWARD CARGO BAY CHIMNEY DAMAGED. MAINTENANCE REMOVED AND REPLACED THE CHIMNEY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041102001062004110200106EA 2004 11 2 SWIA200413997 120041021A27106225734002 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT AILERON MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07980SW 7955 DURING FFOD AILERON CHECK, FOUND LT AILERON WOULD NOT RETURN TO CENTER POSITION. INSTALLED SERVICEABLE LT AILERON POSITION TRANSDUCER IAW MM 27-15-15 OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041102001142004110200114NE 2004 11 2 DL777040991 220041026A7310FK21039 LINE BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 2 ENGINE CHAFED A DALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27860DA14988 29951 FUEL LEAK FROM ENG AFTER START, FOUND FUEL LEAKING FROM LINE BETWEEN FMU AND DRAIN CANISTER. REMOVED AND CLEANED FMU DUMP FILTER REF 73-21-13-100-801. REMOVED DRAIN LINE DUE DAMAGE AT CLAMP AREA INSTALLED NEW LI PURCHASED FROM AA P/N FK21039, AA P/N 4066928 PERF ENG RUN, L CHK ALL NORMAL. OK FOR SERVICE. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F4 FRTT00001SEE00050EN 20041102001152004110200115NE 2004 11 2 DL738040992 220041026A7320 PUMP BOEING737 737832 13844CFNM GE CFM56 CFM567B24 NE FUEL SYSTEM FAILED A DALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO273753 10026 29671 889458 RT ENG FAILED CLIMBING THUR 28000. ALL INDICATIONS PRIOR TO FAILURE WERE NORMAL. REPLACED NR 2 HMU AND FUEL PUMP. 2L72 4F4 FRTA16WE E00055EN 20041102001162004110200116NM 2004 11 2 DL73S040993 120041026A2560 FUSE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE EMERGENCY LIGHT FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27309DL 23081 EMERGENCY LIGHTS AT R2 DOOR AND AFT AISLE EXIT INOPERATIVE. REPLACED BLOWN FUSES IN POWER SUPPLY FOR LIGHTS. 2L72 4F4 FRTA16WE E2EA 20041102001182004110200118NM 2004 11 2 DL757040995 120041028A5415012N888710 FITTING BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27621DL 22911 REPAIR OF OVERSIZED HOLE IN NR 2 PYLON SIDE LINK FITTING. REPAIRED IAW VA 69201AD. 2L72 4F4 FRTA2NM E17NE 20041102001242004110200124NM 2004 11 2 04300411 120041026A3350 LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27411FJ 3166 AFT SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MECHANIC ADJUSTED ELECTRICAL CONTACTS ON EMERGENCY FLOOR LIGHTING. 2H72 4T4 FRTA55NM E35NE 20041103000092004110300009SO 2004 11 3 LR7A04114 120041001A5343 BEAM LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL MLG CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG FS 557 BOW BEAM CRACKED AT WL 156, LBL 64. REPAIRED BEAM IAW SRM SMP 583 53-40-12. NR 0398. 2H74 4T4 T A1SO E282 20041103000142004110300014NM 2004 11 3 AWXA200401163 120041002A534269374024 ANGLE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE HORIZONTAL STAB CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55, WL 208. MAINTENANCE REMOVED CORRODED HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 69-37402; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 12 AND 13. 2L72 4F4 FRTA16WE E2GL 20041103000202004110300020SO 2004 11 3 LR7A04118 120041001A5315 FLOORBEAM LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5314 FOUND FS 245 FLOORBEAM CORRODED AT WL 146, LBL 32 - 52. REPAIRED IAW EA 382-53-04-077. NR 0456. 2H74 4T4 T A1SO E282 20041103000252004110300025SO 2004 11 3 LR7A04123 120041001A5311 FRAME LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND FS 647 FRAME CRACKED AT WL 281, LBL 20. REPAIRED IAW SRM SMP 583 51-140-22. NR 0496. 2H74 4T4 T A1SO E282 20041103000272004110300027NM 2004 11 3 HNAA0400129 120041027A215078279010 ACM DHAV DHC8 DHC8102 2809003NM PWC 150 PW150A EA CABIN ENVIRON ODOR A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07808EX2892 2892 299 FLIGHT NR 3802 REPORTED A STRONG ODOR EMIITING FROM THE ACM. MAINTENANCE REMOVED AND REPLACED THE ACM. OPERATIONAL CHECKS GOOD. SYSTEM RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20041103000312004110300031 2004 11 3 EM04019 420041022A25654A40302 SLIDE EMB ERJ170ERJ170100 EU GE CF34 CF34* NE L1 DOOR DEPLOYED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19808MD1064 17000021 FLIGHT 1684, UPON ARRIVING IN PIT FOUND THE GIRT BAR WAS INADVERTENLY RELEASED FROM THE DOOR CLIP CAUSING PARTIAL SLIDE DEPLOYMENT ON THE 1L DOOR SLIDE. MAINTENANCE REPLACED SLIDE AND SERVICED DOOR PNEUMATIC BOTTLE. 2L74 4F4 FRTA56NM E15NE 20041103000342004110300034NM 2004 11 3 XNOA1204 120041027A2781 POSITION SWITCH BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE TE FLAPS OUT OF ADJUST A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2376753 21249 NR 6 LED FAILED TO RETRACT. ADJUSTED NR 6 LEADING EDGE FLAP POS SWITCH IAW MM CH. 27-82-11. 2L73 4F4 F A3WE E2EA 20041103000532004110300053NE 2004 11 3 AALA20041068 220041022A7230 COMPRESSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT ENGINE STALLED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW219306T 49567 717856 T512/22 RT ENGINE COMPRESSOR STALL CLIMBING THROUGH 17,000 MEAN SEA LEVEL. AIRSPEED 320 KTS, EGT 700-750 DEGREES C. DID NOT SHUTDOWN TIL TOUCHDOWN. ALL OTHER INDICATIONS NORMAL UNTIL TOUCHDOWN AND EGT STARTED TO RISE. REPLACED RT ENGINE IAW MCM 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA6WE E9NE 20041103000542004110300054NM 2004 11 3 AALA20041069 120041025A339764649 CABLE BOEING757 757231 1384950NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21722TW 29385 EMERGENCY FLOOR LIGHTING SYSTEM PLASTIC COVER BROKEN AND LIGHTING TRACK PULLED OUT AT ROW 12. REPLACED CONDUCTOR CABLE FROM ROW 7 TO ROW 16 FOR EMERGENCY FLOOR TRACK LIGHTING. ALSO REPLACED LIGHT ELEMENT AND SECURED COVER FOR EMERGENCY LIGHT AT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM E17NE 20041103000572004110300057NM 2004 11 3 04FDEA02965 120041021A5520 STRUCTURE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2* GL STABILIZER CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT REAR SPAR ZFR 510 RT EXTRUSION, EXTERIOR SURFACE FOUND CORRODED. REMOVED AS PER SRM 51-21-01 VOL II & REPAIRED AS PER FEDEX EA NR 1-5530-81577. 2L73 4F4 FRTA22WE E23EA 20041103001052004110300105EU 2004 11 3 DHL2004363530 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3887, FR.18-FR. 26.5 RBL 98 SEAT TRACKS MAIN CABIN CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACKS FROM FR 18 TO FR 26.5 AT RBL 98 IAW SRM 51-30-30. REPLACED SEAT TRACK IAW SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 18 TO FR 26.5 AT RBL 98 IAW SRM 53-10-10/51-10-40. MATERIAL USED, PN 60-22457, PO NR 24302234. 2L72 4F4 FRTA35EU E23EA 20041103001062004110300106GL 2004 11 3 EVA07022004 220040702A7200 ENGINE BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 3 FLAMED OUT W QOCFO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP03416MC 32838 DURING AIRCRAFT DESCENT AT 30000 FT, ENGINE NR 3, NR 4 FLAMED OUT WHILE ENCOUNTERING HEAVY RAIN AND MODERATE TURBULENCE. BOTH ENGINES WERE BACK TO NORMAL AFTER RESTART. THIS CASE IS BEEN DETERMINED AS WEATHER CAUSED IFSD (IN-FLIGHT SHUT DONE) AT OCT/2004. MFG IS GOING TO REVISE THE FADEC VBV SCHEDULE TO OPEN VBV TO PREVENT SEPARATED ICE FROM GETTING INTO HPC/COMBUSTOR AT 1Q/2005. 2L74 4F4 FRT1384945 E23EA 20041103001072004110300107WP 2004 11 3 IXXA0400114O 120041024A32300080004003 CONTROL BOX DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE MLG BURNED A IXXAB EMER. DESCENT J WARNING INDICATION LDLANDING 1 SW1141CX 7467010 46129523 DURING LANDING, ON GEAR EXTENSION NO GREEN LIGHTS FOR GEAR DOWN AND LOCKED. C/B ON DC BUS 1 RESET NO HELP. VISUAL INDICATORS ON WING AND NOSE GEAR DOWN ALL CHECKED, GEAR DOWN AND LOCKED. CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE FOUND CONNECTOR P1-44 DISCONNECTED AT F/O'S INSTRUMENT PANEL AND RECONNECTED. REPLACED L/G PROXIMITY BOX AND THE SYSTEMS OPERATIONAL CHECK WAS NORMAL IAW ALL APPLICABLE MANUALS. 2L74 4F4 F 4A25 1E8 20041103001112004110300111WP 2004 11 3 COOSDR040030 120040823A5740 FITTING DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE LT WING TE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 RT AND LT WING TRAILING EDGE SUPPORT, CANOE FITTING OB/IB HOLES ID CORRODED AT STA XF=97.906, STA XF=219.498 AND STA XF=399.723. 2L74 4F4 F 4A25 1E8 20041103001132004110300113NM 2004 11 3 COOSDR040023 120040817A5730 SKIN BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE CENTER WING CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 WING CENTER SECTION LOWER SKIN AFT SECTION BETWEEN LBL 30 AND RBL 30 SKIN OUTER FACE CORRODED. 2L73 4F4 FRTA3WE E2EA 20041103001162004110300116NM 2004 11 3 ASMF200410012 120041017A80103927966 SHUTOFF VALVE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23945AS252734602 49643 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE SHUTOFF VALVE DID NOT OPEN. SHUTOFF VALVE WAS REPLACED IAW MM 80-10-02, TESTS WERE CORRECT. 2L72 4F4 FRT E9NE 20041103001212004110300121NM 2004 11 3 COOSDR040037 120040823A5753 SKIN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU LT WING OB FLAP DELAMINATED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23359UA 24452 LT WING, OB FORE FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 300 AND AT WBL 210. 2L72 4F4 FRTA16WE E21EU 20041105000012004110500001NM 2004 11 5 SWAA043153 120041029A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STRINGER 4L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000242004110500024NM 2004 11 5 SWAA043176 120041102A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041105000432004110500043NM 2004 11 5 SWAA043134 120041027A53306523693 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 271, STR 15L AND STR 9L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000462004110500046NM 2004 11 5 SWAA043137 120041028A53126545819 PRESSURE PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED SERVICE CHECK, FOUND NLG W/W LT SIDE WEB CRACKED AT BS 203.8. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20041105000502004110500050SO 2004 11 5 LR7A04095 120041001A5312 BEAM LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 BOW BEAM CAP CRACKED AT WL 152, RBL 63. REPAIRED IAW SRM SMP 583 53-40-12. 2H74 4T A1SO 20041108000012004110800001NM 2004 11 8 EIA2004092 120040715A5320 SPLICE BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STA 520, STR 12R, STRINGER SPLICE FOUND CRACKED ON REMOVAL. REMOVED CRACKED SPLICE, LOCATED, DRILLED AND INSTALLED NEW SPLICE IAW SRM 51-30-02, PGS 2-3 AND 8-9. 2L74 4F4 F A20WE E20EA 20041108000042004110800004NM 2004 11 8 EIA2004132 120041016A5315 STRAP BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE FLOORBEAM CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 UPPER DECK FLOORBEAM STRAP HAS EXFOLIATION CORROSION, STA 420R, 3 INCHES IB FUSELAGE SKIN. REPLACED STRAP IAW SRM 51-30-02, PGS 8-9, 51-30-05, FIG 4, AND 51-30-02, PGS 8-9 2L74 4F4 F A20WE E20EA 20041108000322004110800032EU 2004 11 8 RAIA00410007 120041014A3060ANN60 FUSE JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR36B5JFR36C1103GL DE ICE SYSTEM BLOWN A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03561HK 41077 001330 STL - LEFT PROP DE-ICE FAILED. MAINTENANCE REMOVED AND REPLACED DE-ICE FUSE. 2L72 4T RTA41NM 6 CP15NE 20041108000332004110800033NM 2004 11 8 04291404 120041017A7732 SENSOR DORNERDO32 DO328300 NM DEFECTIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27404FJ 3150 ABORTED TAKEOFF PRIOR TO 50 KNOTS DUE TO ENGINE VIB CAS MSG. MX REMOVED AND REPLACED VIBRATION SENSOR. 2H72 4T RTA55NM 20041108000342004110800034NM 2004 11 8 04292424 120041018A3610 SHUTOFF VALVE DORNERDO32 DO328300 NM ENGINE DEFECTIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27424FJ 3185 ABORTED TAKEOFF FOR RT PACK FAILURE. MX REMOVED AND REPLACED ENGINE PRSOV IAW 36-10-03. 2H72 4T RTA55NM 20041108000392004110800039EA 2004 11 8 COMA0460592 120041029A32347179015 CONTROL HANDLE CNDAIRCL600 CL6002B19 1900309EA INSTRUMENT PANELMALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01926CA26719 7027 FLIGHT 5029 GEAR DISAGREE WARNING. REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. 2L72 4F RTA21EA 20041108000402004110800040EA 2004 11 8 04288621 120041014A3260 UPLOCK CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A VTZAO OTHER N FALSE WARNING CLCLIMB 1 EA27621BR 7186 EVENT SUMMARY STATES NOSE GEAR DISAGREE. PERFORMED GEAR SWINGS REF MM 32-30-00. OPS CHECK GOOD. NFF ON SEU MM 32-61-00. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK ASSY MM 32-33-05. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108000462004110800046NM 2004 11 8 04284804 120041010A5270 COVER AIRBUSA319 A319132 3930340NM DOOR HANDLE LOOSE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27804BR 2296 ABORTED TAKEOFF DUE TO LT OVERWING DOOR WARNING. MX SECURED HANDLE COVER. NO DEFECTS NOTED. 2L72 4F RTA28NM 20041108000472004110800047EA 2004 11 8 04308636 120041103A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B19 1900309EA MLG DIRTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27636BR 7307 CREW SELECTED GEAR UP AFTER LIFT OFF AND RECEIVED FLUCTUATING UP/BARBER POLE/UP/BARBER POLE/ETC WITH ACCOMPANYING AURAL AND VISUAL GEAR DISAGREE WARNINGS. EXTENDED GEAR MANUALLY AND LANDED AT NEAREST AIRPORT IN ACCORDANCE WITH QRH. MX FOUND HEAVY FILM OF GREASE AND DIRT ON PROX SWITCHES. CLEANED GREASE OFF. SERVICED STRUTS. 2L72 4F RTA21EA 20041108000672004110800067 2004 11 8 RAIA00409012 420040915A3417 PITOT LINE EMB 145 EMB145LR 3260212SO NR 1 ADC CONTAMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03812HK 145373 PIT - ADC NR 1 FAIL INDICATION. MAINTENANCE DRAINED WATER FROM PITOT SYSTEM DRAIN. 2L72 4T RTT00011AT 20041108000892004110800089SO 2004 11 8 RAIA00409008 120040912A213122250N030201 CONTROL UNIT EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03830HK7960 145313 STL - LOST CABIN PRESSURE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER. 2L72 4T RTT00011AT 20041108001012004110800101NE 2004 11 8 P5CA0401258 220041018A7260773190001 GEARBOX BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE MALFUNCTIONED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA15920FT 22237 702238 WHEN STARTING NR 2 ENGINE, N2 WENT 62.5 PERCENT IMMEDIATELY. NR 2 GENRATOR CAME ON LINE IMMEDIATELY, NO N1 INDICATION, OIL QTY WENT FROM FULL TO 3/4. REPLACED GEARBOX ANGLE PER AMM 72-61-03. OPERATIONAL & LEAK CHECK OK PER AMM 71-00-00. 2L74 4F4 F A20WE E3NE 20041108001052004110800105SO 2004 11 8 RAI00409018 120040917A52701205044700 SPRING EMB 145 EMB145LR 3260212SO CARGO DOOR DAMAGED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03814HK 145046 MSY - BAGGAGE DOOR OPEN LIGHT WILL GO OUT. BAG DOOR DOES NOT SECURE. MAINTENANCE REMOVED AND REPLACED DOOR VENT DOOR SPRING. 2L72 4T RTT00011AT 20041108001072004110800107 2004 11 8 RAIA00409020 420040920A34177000700967 ADC JETAIRJETSTMJETSTM4101 1500501EU NR 1 FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03569HK13865697 41088 SPI - NR 1 ADC FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 ADC. 2L72 4T RTA41NM 20041108001082004110800108 2004 11 8 RAIA00408031 420040827A3400C16221GC03 CONTROL UNIT EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03834HK7974 4448 145269 RIC - INTEGRATED STANDBY INSTRUMENT SYSTEM DISPLAYED ALTITUDE WARNING. MAINTENANCE REMOVED AND REPLACED ISIS CONTROL. 2L72 4T RTT00011AT 20041108001112004110800111GL 2004 11 8 RAIA00408034 220040831A7532 LINE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL BLEED VALVE DISCONNECTED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03820HK 145064 311108 DEN - LEFT ENGINE LOW N1 MESSAGE ON TAKEOFF ROLL. MAINTENANCE FOUND NR 1 ENGINE COMPRESSOR ACCELERATION BLEED CONTROL VALVE LINE DISCONNECTED, RE-SECURED LINE, INSPECTED ALL BLEED LINES FOR SECURITY AND LEAKAGE. 2L72 4F4 FRTT00011ATTE6CH 20041108001142004110800114SO 2004 11 8 RAIA00409018 120040917A52701205044700 SPRING EMB 145 EMB145LR 3260212SO CARGO DOOR FAILED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03814HK 145046 MSY - BAGGAGE DOOR OPEN LIGHT WILL GO OUT. BAG DOOR DOES NOT SECURE. MAINTENANCE REMOVED AND REPLACED DOOR VENT DOOR SPRING. 2L72 4T RTT00011AT 20041108001212004110800121EU 2004 11 8 DJFA2004007 120040526A5730 SKIN BRAERODH125 BAE125800A 1500285EU WING LE CORRODED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23867CW 258067 DURING INSPECTION OF THE WING AFTER LEADING EDGES WERE REMOVED CORROSION WAS FOUND ON THE WING SKIN SURFACES WERE THE LEADING EDGES FIT ON. RAYTHEON AIRCRAFT WAS NOTIFIED AND A FIELD REPAIR FOR REMOVING THE CORROSION WAS APPROVED. ALL CORROSION WAS CLEANED AND SURFACES INSPECTED AND PRIMED. 2L72 4F RTA3EU 20041108001222004110800122CE 2004 11 8 DJFA2004011 120040725A3411 PITOT TUBE CESSNA500 550 2076604CE OBSTRUCTED E DJFAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA23283CW 5500713 AIRCRAFT DEPARTED KUVA AND DURING TAKEOFF ROLE AT ABOUT 50 KTS THE PILOTS NOTICED THE RT AIRSPEED WAS STILL AT 0. ABORTED TAKEOFF AND RETURNED TO FBO. THE MAINTENANCE PEOPLE CLEANED A BUG FROM INSIDE THE PITOT TUBE AND PERFORMED A HIGH SPEED TAXI WITH BOTH AIRSPEEDS, WORKS OK. 1L72 4F A22CE 20041108001232004110800123EU 2004 11 8 DJFA2004003 120040404A7930326180120013 REGULATOR VALVE AMD FALC50FALCON50MYST2730106EU ALIDSGTFE731TFE7313AR WP ENG OIL PUMP FAILED E DJFAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA23551CW3000 3000 51 DURING THE CLIMB THE PILOTS NOTICED THE NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS DESCENDING THREW 25 PSI. AT THAT POINT THE PILOTS SHUT DOWN THE NR 3 ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. 2L73 4F4 F A46EU E6WE 20041108001242004110800124EA 2004 11 8 04254682 120040908A3000 LOOP CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM INOPERATIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27682BR 7691 ANTI ICE DUCT WARNING POSTED ON T/O ROLL. REMOVED AND REPLACED LT WHEEL WELL LOOP A41WK REF AMM 36-21-04. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20041108001262004110800126NM 2004 11 8 CALA0400690 120041029A5730114N2106 SKIN BOEING757 757224 1384958NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2767134 29283 INSPECTION FOUND AN 8 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 421-471. REPAIR WAS ACCOMPLISHED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20041108001272004110800127NM 2004 11 8 CALA0400691 120041030A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 328-360. THE SEAT TRACK SECTION WAS REPLACED IAW SRM 53-00-52 AND 51-40-02. 2L72 4F RTA16WE 20041108001282004110800128NM 2004 11 8 CALA0400692 120041031A5313BAC1498155 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND STRINGER 28R CORRODED IN E&E COMPARTMENT AT STA 319 - 322.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20041108001292004110800129NM 2004 11 8 CALA0400693 120041031A53156545815 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND UPPER AND LOWER SURFACES OF FLOORBEAM UPPER CAP CORRODED AT STA 344, RBL 10-LBL 20. THE FLOORBEAM CHORD WAS REPAIRED IAW SRM 53-10-51, FIGURE 205. 2L72 4F RTA16WE 20041108001312004110800131EA 2004 11 8 COMA0460585 120041027A5210601R3199831 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01940CA24672 7048 FLIGHT DURING HEAVY MAINTENANCE CHECK (NO ASSOCIATED TASK CARD APPLIED), THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE SEVERELY CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH BOMBARDIER REO 601R-52-11-567. 2L72 4F RTA21EA 20041108001352004110800135SO 2004 11 8 LR7A04193 120041013A5330 SKIN PANEL LKHEED382 382G 526414USO FUSELAGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND RT MLG BAY FS 575 SIDEWALL SKIN CORRODED AT WL 161, RBL 62. REPAIRED IAW LAC MEA 382-53-04-084. 2H74 4T A1SO 20041108001382004110800138 2004 11 8 DJFA2004001 420040411A34256226189002 COMPENSATOR BEECH MU300 400A 1155402CE COCKPIT MALFUNCTIONED E DJFAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 EA23755TA2443 RK324 DURING FLIGHT AIRCRAFT EXPERIENCED A PFD FAILURE AND LOST BOTH PF'S. PILOTS CONTACTED CENTER AND RECEIVED VECTORS, LANDED WITH NO FURTHER PROBLEMS. 2H72 4F RTA16SW 20041108001412004110800141GL 2004 11 8 RAIA00407012 220040721A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03825HK 145510 DEN - LEFT ENGINE HIGH ITT UPON SETTING T/O TRUST. MAINTENANCE INSPECTED NR 1 ENGINE AND PERFORMED ENGINE RUN. ALL INDICATIONS NORMAL IAW ROLLS ROYCE MM 72-00-00. 2L72 4T4 FRTT00011ATTE6CH 20041108001422004110800142NM 2004 11 8 04269410 120040925A32222311030000 SHOCK ABSORBER DORNERDO32 DO328300 NM NLG DEFECTIVE A VTZABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27410FJ 3165 ON CLIMBING PHASE, GEAR DISAGREE. CREW DECLARED EMERGENCY AND RETURNED TO FIELD. NLG SHOCK STRUT WAS REMOVED AND REPLACED. GEAR SWING GOOD. 2H72 4T RTA55NM 20041108001442004110800144EA 2004 11 8 04257621 120040913A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27621BR 7186 FLAPS HALF SPEED. UPON INTERROGATING FECU, FOUND FAULTS 1) FECU 2) FECU/BPSU MISRIG, 3) EITHER BPSU. CHECKED RIGGING OF FECU & BPSUS AND NOTICED FECU GIVING ERRONIOUS POTENTIOMETER READINGS. REMOVED AND REPLACED FECU IAW MM 27-51-05. PERFORMED RIGGING OF BPSUS IAW MM 27-51-10. OPERATIONAL CHECK OF FLAPS GOOD REF MM 27-54-00. NO FURTHER FLAP FAIL OR FLAPS HALFSPEED MSGS NOTED AT THIS TIME. 2L72 4F RTA21EA 20041108001462004110800146EU 2004 11 8 DJFA2004017 120040812A28218975131 FILTER BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP NR 2 ENGINE BLOCKED E DJFAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA23845CW 258045 P91196 DURING TAKEOFF THE NR 2 ENGINE FUEL BYPASS LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE FBO. FUEL FILTER WAS REPLACED, LEAK CHECKED AND FOUND TO BE OK. 2L72 4F4 FRTA3EU E6WE 20041108001482004110800148EA 2004 11 8 04260627 120040916A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27627BR 7233 OVERBOARD COOL FAIL MSG ON T/O ROLL. PER MXC OPENED DM2604307-1 PER MEL 21-24-06 CAT C PLACARD AND M-PROC C/W. 2L72 4F RTA21EA 20041108001492004110800149SO 2004 11 8 RAIA00407011 120040714A3240429513 CONTROL UNIT EMB 145 EMB145LR 3260212SO BRAKES FAILED A RAIAO OTHER J WARNING INDICATION LDLANDING 1 CE03829HK8989 145281 YOW - AIRCRAFT RAN OFF END OF RUNWAY SUSPECT TOTAL BRAKE FAILURE. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT. 2L72 4T RTT00011AT 20041108001532004110800153EA 2004 11 8 04262664 120040918A2910 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYSTEMINOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27664BR 7528 LEFT ENG HYD SOV C/B POPPED. REMOVED AND REPLACED ACTUATOR HYD SOV IAW CRJ IAW CRJ AMM 29-11-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108001542004110800154NM 2004 11 8 P5CA0401269 120041101A27302566A30A SENSOR BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE AOA MALFUNCTIONED A P5CAO OTHER N FALSE WARNING CRCRUISE 1 WP23355MC 23395 STICK SHAKER ACTIVATING INTERMITTENTLY IN STEADY STATE CRUISE FLIGHT, C/B PULLED. REPLACED LT AOA SENSOR PER AMM 27-32-01, OPS CHECK OK PER AMM 27-32-00. 2L74 4F4 FRTA20WE E23EA 20041108001562004110800156NM 2004 11 8 P5CA0401271 120041101A80117265747 START VALVE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE FAILED A P5CAED ENGINE SHUTDOWN RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 EA15920FT 22237 702115 NR 3 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. REPLACED START VALVE NR 3 ENGINE, AMM 80-11-04, OPS CHECK OK. 2L74 4F4 F A20WE E3NE 20041108001572004110800157WP 2004 11 8 DJFA2004013 220040630A7250 BLADE BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP NR 2 ENGINE BROKEN E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA23816CW 258016 P91103 AT FLIGHT LEVEL 390 FT THE CREW HEARD A LOUD THUMP AND VIBRATION ON THE NR 2 ENGINE. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED AT DAL WITH NO FURTHER PROBLEMS. AFTER FURTHER INSPECTION IT WAS FOUND THAT THERE WERE SOME TURBINE BLADES MISSING. ENGINE WAS REMOVED AND A LOANER ENGINE WAS INSTALLED. GARRETT IS CURRENTLY IN THE TEAR DOWN MODE OF THE ENGINE AND DO NOT KNOW THE EXACT FAILED PART. 2L72 4F4 FRTA3EU E6WE 20041108001582004110800158EA 2004 11 8 04283703 120041009A2120 FAN CNDAIRCL600 CL6002B19 1900309EA LAVATORY SMOKE A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27703BR 7467 LAV SMOKE INDICATION WITH FAINT HAZE. SMOKE DISAPPEARED AFTER C/BS PULLED FOR QRH. MX REMOVED AND REPLACED LAV EXHAUST FAN AND SMOKE DETECTOR. 2L72 4F RTA21EA 20041108001592004110800159EA 2004 11 8 04282621 120041008A3230750006000 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27621BR 7186 AIR RETURN FOR GEAR DISAGREE MESSAGE AFTER TAKEOFF. NOSE GEAR NEVER SHOWED UP AND LOCKED. MX REMOVED AND REPLACED NLG PRIORITY VALVE IAW CRJ 32-33-45. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IAW CRJ 33-22-20. PERFORMED GEAR SWINGS IAW 32-30-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108001612004110800161EU 2004 11 8 RAIA00410021 120041024A7930 CHIP DETECTOR JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE CONTAMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03553HK 41066 SYR - ON TAKEOFF, LEFT OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE CLEANED AND INSPECTED CHIP DETECTOR. 2L72 4T RTA41NM 20041108001632004110800163EU 2004 11 8 RAIA00410018 120041020A3260AIR136070 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03565HK 41082 STL - UPON GEAR RETRACTION, THE RED GEAR LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LT MLG UPLOCK SWITCH. 2L72 4T RTA41NM 20041108001652004110800165EA 2004 11 8 04303658 120041029A3097 WIRE CNDAIRCL600 CL6002B19 1900309EA ANTI ICE DAMAGED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27658BR 7500 EVENT SUMMARY STATED RIGHT WING ANTI-ICE DUCT FAIL. REPAIRED CHAFED WIRE PER 20-11-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108001672004110800167SO 2004 11 8 LR7A04089 120040809A5512 SKIN LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 664 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND LT HORIZONTAL STAB UPPER SURFACE SKIN CRACKED AT FS 1090, HSS 196, WL 282. REPAIRED PER SRM SMP 583 55-20-06. 2H74 4T A1SO 20041108001682004110800168SO 2004 11 8 LR7A04090 120040809A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 664 4698 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND CARGO RAMP SKIN CRACKED AT BL 0 LAP JOINT, FS 737 - 784, WL 141, IN TWO LOCATIONS, 10.0 INCHES AND 16.0 INCHES. REPAIRED IAW LAC MEA 382-53-04-060. 2H74 4T A1SO 20041108001692004110800169SO 2004 11 8 LR7A04091 120040809A5230 INTERCOSTAL LKHEED382 382G 526414USO CARGO DOOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 1335 4698 DURING SCHEDULED B2 INSPECTION NR 0094 ACCOMPLISHMENT FOUND CARGO RAMP INTERCOSTAL CRACKED FS 761 - 784, BL 0, WL 141. REPAIRED PER SRM SMP 583 51-140-19. 2H74 4T A1SO 20041108001712004110800171WP 2004 11 8 DJFA2004014 220040801A7261 OIL CAP RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315R 01518WP NR 1 ENGINE UNSECURE E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA23728TA 258364 P107302 AFTER DEPARTURE FIVE MINUTES INTO THE CLIMB THE NR 1 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW LEVELED AT 270 FT AND THE OIL PRESSURE WAS SLOWLY GOING DOWN, THE OIL PRESSURE LIGHT FLICKERED ON AND OFF AND AT THAT POINT THE CREW DECIDED TO SHUT DOWN THE NR 1 ENGINE. AFTER LANDING AT FTY MAINTENANCE PERSONEL FOUND THE OIL CAP OFF. SERVICED THE ENGINE WITH 4.5 QTS OF OIL AND PERFORMED GROUND RUNS AND LEAK CHECKED. ALL GROUND RUNS FOUND SATISFACTORY. 2L72 4F4 FRTA3EU E6WE 20041108001742004110800174EU 2004 11 8 RAIA00410008 120041014A3060C40567 BRUSH BLOCK JETAIRJETSTMJETSTM4101 1500501EU PROP HEAT FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03550HK 41039 STL - RIGHT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED BRUSH BLOCK ON NR 2 PROP. 2L72 4T RTA41NM 20041108001752004110800175EA 2004 11 8 04304675 120041030A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27675BR 7635 EVENT SUMMARY STATED THAT AFTER TAKEOFF FLAP FAIL INDICATION RTF. REMOVED AND REPLACED FECU MM 27-51-05. 2L72 4F RTA21EA 20041108001772004110800177SO 2004 11 8 LR7A04065 120040715A5340351767LR FITTING LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 1167 4698 DURING FS 617 TENSION TIE TUBE REPLACEMENT, LP 15480 ITEM M2, FOUND LT & RT UPPER TENSION TIE FITTINGS AT LT & RT BL 62, CRACKED AT 1 EA FASTENER HOLE. CRACKS NOT VISIBLE WITH FITTING INSTALLED. REPLACED TENSION TIE FITTINGS IAW SRM SMP 583 51-10 (G) AND 51-70. LP 15480, ITEM M2. 2H74 4T A1SO 20041108001792004110800179CE 2004 11 8 HAEA200400162 120040804A3222 STRUT LEAR 24 24B 5170306CE NLG DISCHARGED E HAEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW05233TW1587510610 24B221 NOSE GEAR FAILED TO FULLY RETRACT AFTER T/O FROM MKE. GEAR WAS EXTENDED, DETERMINED NO EMERGENCY EXISTED AND RETURNED FOR NORMAL LANDING. MAINTENANCE DETERMINED THE STRUT WAS UNDER INFLATED. STRUT SERVICED AND MAINTENANCE RECORDED. AIRCRAFT DEPARTED NO FURTHER PROBLEMS. 2L72 4J A10CE 20041108001802004110800180SO 2004 11 8 LR7A04085 120040728A5330 SKIN LKHEED382 382G 526414USO FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 757 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND FS 420 LOWER FUSELAGE SKIN DENTED AT LBL 30, WL 127. REPAIRED IAW SRM SMP 583 51-140-12. NR 0008. 2H74 4T A1SO 20041108001812004110800181SO 2004 11 8 LR7A04086 120040728A5343 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 757 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG FS 557 BOW BEAM CRACKED APPROX. 1.0 INCH AT LBL 64, WL 156. REPAIRED IAW SRM SMP 583 53-40-12. 2H74 4T A1SO 20041108001822004110800182SO 2004 11 8 LR7A04087 120040728A5343 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 757 4763 DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG FS 497 BOW BEAM CRACKED APPROX. 1.0 INCH AT LBL 64, WL 156. REPAIRED IAW SRM SMP 583 53-40-12. 2H74 4T A1SO 20041108001842004110800184NE 2004 11 8 RAIA00410002 220041002A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE LEFT FAILED A RAIAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 CE03553HK 41066 76101 PIT - LEFT ENGINE QUIT 2 FEET ABOVE GROUND ON LANDING. MAINTENANCE PERFORMED GROUND RUN, NO DEFECTS NOTED. 2L72 4T4 TRTA41NM E18NE 20041108001852004110800185NM 2004 11 8 DL767040957 120041010A2120 ODOR BOEING767 767232 1385132NM GE CF680 CF680A2 NE CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27104DA 22216 580130 RAN ENGINES AND PACKS. INSPECTED AIRCRAFT, UNABLE TO DUPLICATE. 2L72 4F4 FRTA1NM E13NE 20041108001862004110800186 2004 11 8 RAIA00410004 420041012A34607013348940 DAU EMB 145 EMB145 3260210SO NR 2 MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03809HK5695 145187 AVP - NR 2 GENERATOR OVERLOAD, ICE DETECT FAIL, YAW DAMPENER FAIL, AND APU BLEED LEAK MESSAGE. MAINTENANCE DEFERRED AUTO PILOT MEL 22-10-00, APU PER MEL 28-22-01 AND GROUND RAN NR 2 ENGINE. REMOVED AND REPLACED DAU. 2L72 4F RTT00011AT 20041108001882004110800188EA 2004 11 8 04252691 120040904A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR INOPERATIVE A VTZAO OTHER N FALSE WARNING CLCLIMB 1 EA27691BR 7740 PROX SYS FAULT ON CLIMBOUT. DEFERRED CARGO DOOR IND REF MEL 52-70-04. REMOVED CARGO DOOR IND CABLE. 2L72 4F RTA21EA 20041108001912004110800191SO 2004 11 8 RAIA00410010 120041017A3260853704 UPLOCK SENSOR EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03818HK 145059 DSM - NOSE LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED FORWARD UPLOCK PROX SENSOR. 2L72 4T RTT00011AT 20041108001932004110800193EA 2004 11 8 5336001 120040812A2797CD75C22 WIRE HARNESS CNDAIRCL600 CL6002B16 1900305EA AFT BAY SHORTED E ERYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07212RR6350 5336 AFTER DEPARTURE AND DURING CLIMB (TEB) NOTICED STAB CH 1 INOP ANNUNCIATION ON EICAS. RETURNED TO AIRPORT (TEB). MAINTENANCE TROUBLESHOT TO MCU (MOTOR CONTROL UNIT), REPLACED MCU, OPS CHECK AND RETURN TO SERVICE. DEPARTED TEB AND UPON ARRIVING BAF, STAB CH 1 INOP ANNUNCIATION INDICATED ONCE AGAIN. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE PROBLEM. DEPARTED TEB AND UPON ARRIVAL AT CYUL, STAB CH 1 INOP ANNUNCIATION INDICATED A THIRD TIME. MAINTENANCE TROUBLESHOT ENTIRE STAB TRIM CONTROL SYSTEM AND FOUND BAD WIRE IN JP255 CONNECTOR IN AFT BAY. REPLACED ENTIRE WIRE FROM P255 TO P256. F/T STAB SYSTEM IAW M/M 27-40-00 AND RETURN TO SERVICE. 2L72 4F RTA21EA 20041108001982004110800198SO 2004 11 8 LR7A04103 120041001A5320 TEE FITTING LKHEED382 382G 526414USO FUSELAQGE CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 - FS 577, WL 163 SHELF OUTER TEE CORRODED AT RBL 67. REPLACED TEE IAW DWG 375977-2 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041108002002004110800200 2004 11 8 SWAA043143 420041028A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29634SW 27937 DURING SCHEDULED SERVICE CHECK, FOUND BOTH R1 & R2 DOOR EVACUATION SLIDES OUT OF ADJUST. REPOSITIONED BOTH SLIDES PER MM. 2L72 4F RTA16WE 20041108002022004110800202 2004 11 8 SWAA043145 420041028A256565C10820 GIRT BAR BOEING737 7377Q8 1384418NM L1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29799SW 28209 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MM. 2L72 4F RTA16WE 20041108002042004110800204NM 2004 11 8 SWAA043147 120041028A57126545445 RIB BOEING737 7375H4 138449DNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER RIB CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED RIB CHORD PER SWA EA. 2L72 4F RTA16WE 20041108002082004110800208 2004 11 8 SWAA043193 420041103A25656949956 CABLE BOEING737 7372H4 138448CNM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29091SW 22963 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F A16WE 20041108002102004110800210NM 2004 11 8 SWAA043206 120041103A57536546434302 SKIN BOEING737 7373Q8 1384670NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND RT WING TRAILING EDGE INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E INBOARD AFT FLAP PER MM. 2L72 4F RTA16WE 20041108002142004110800214NM 2004 11 8 SWAA043192 120041103A2560PH22300L GLOWSTRIP BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29708SW 27842 EMERGENCY PHOTOLUMINESCENT FLOOR STRIP FROM ROW 4 DEF TO ROW 7 DEF LOOSE. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20041108002162004110800216SO 2004 11 8 C2XA04RI011 120041023A335078812 LAMP EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718102 145643 EWR - FLIGHT 3315 - CREW REPORTED EMERGENCY EXIT LIGHT STRIP AT ROW 12 RT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP ASSY. ALL OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20041108002202004110800220NM 2004 11 8 SWAA043209 120041104A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP AT ROW 8 ABC, MISSING. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20041108002212004110800221NM 2004 11 8 SWAA043210 120041104A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR HINGE CUTOUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041108002222004110800222 2004 11 8 SWAA043211 420041104A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29645SW 28330 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE DOOR GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041108002232004110800223NM 2004 11 8 SWAA043212 120041104A57536546434368 SKIN BOEING737 7375H4 138449DNM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT INBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041108002252004110800225NM 2004 11 8 SWAA043214 120041104A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 360, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041108002272004110800227NM 2004 11 8 371PA0068 120040914A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FLOORBEAM AT BS 946 HAS CORROSION AT CLIP NUT HOLES FROM LBL 18 TO RBL 18. REPAIRED PER SRM 53-00-51 AND SRM 53-60-51. 2L72 4F RTA16NE 20041109000012004110900001NM 2004 11 9 QXEA200400739 120041029A2710 CONNECTOR DHAV DHC8 DHC8202 2809007NM RUDDER DISCONNECTED A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09355PH16238 500 PDX - FLIGHT 2201 - FLIGHT RETURNED TO GATE AFTER THE CREW NOTICED NO INDICATION ON THE RUDDER AND AILERON TRIM INDICATORS. MAINTENANCE RECONNECTED THE CANNON PLUG ON THE AILERON AND RUDDER TRIM PANEL. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND THE CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041103001222004110300122WP 2004 11 3 COOSDR040034 120040823A5320564668923 COVER DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE MAIN CABIN DAMAGED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 MAIN CARGO CABIN Y STA 119, Z0, -X 20 COVER, DAMAGED. 2L74 4F4 F 4A25 1E8 20041105000022004110500002NM 2004 11 5 SWAA043158 120041027A53106547978 CREASE BEAM BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE RT CREASE BEAM WEB CRACKED AT BS 639. REPAIRED WEB PER SRM & SWA EA. 2L72 4F A16WE 20041105000062004110500006NM 2004 11 5 SWAA043185 120041102A53156546810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, RBL 17, RBL 27, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20041105000132004110500013NM 2004 11 5 SWAA043170 120041102A3350101073 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29773SA 27881 LEFT FWD EMERGENCY EXIT LIGHT MISSING LENS. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041105000152004110500015SO 2004 11 5 LR7A04136 120041001A5330 SKIN LKHEED382 382G 526414USO FUSELAGE GOUGED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND FS 477 SKIN GOUGED AT WL 184, RBL 83. REPAIRED PER SRM SMP 583 51-140-12. 2H74 4T A1SO 20041105000172004110500017SO 2004 11 5 LR7A04138 120041001A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LOWER RBL 60 CHINE ANGLE CRACKED AT FS 617 - 637. REPAIRED IAW SRM SMP 583 53-40-26. 2H74 4T A1SO 20041105000222004110500022NM 2004 11 5 SWAA043184 120041102A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 727D, RBL 18, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041105000272004110500027NM 2004 11 5 SWAA043190 120041102A53306518420 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND R1 WINDOW POST UPPER OUTBOARD SKIN CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000372004110500037NM 2004 11 5 SWAA043163 120041028A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, STR 16R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000412004110500041NM 2004 11 5 SWAA043151 120041030A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29477WN 33988 AFT EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041105000532004110500053SO 2004 11 5 LR7A04098 120041001A5312 BEAM LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD FOUND RT MLG FS 557 UPPER BOW BEAM CRACKED AT WL 200, RBL 62. REPAIRED IAW SRM SMP 583 53-40-14. 2H74 4T A1SO 20041108000172004110800017NM 2004 11 8 CALA0400698 120041102A3397 WIRE BOEING737 7373T0 1384582NM CHARGER BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2777303 23354 INSPECTION FOUND THE EMERGENCY LIGHTS AT SEATS 12ABC TO 20ABC INOPERATIVE. TROUBLESHOOTING FOUND A BROKEN WIRE AT PIN 18 ON AFT BATTERY CHARGER UNIT. THE WIRE WAS REPAIRED AND OPERATIONAL CHECKS WERE NORMAL. 2L72 4F RTA16WE 20041108000212004110800021NM 2004 11 8 P5CA0401272 120041101A8011 VALVE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE FAILED A P5CAE ENGINE SHUTDOWN G MULTIPLE FAILURE TXTAXI/GRND HDL 1 EA15920FT 22237 702269 NR 4 ENGINE START VALVE FAILED TO OPEN IN GROUND START, DUCT PRESSURE IS 40 PSI. NR 4 ENGINE START VALVE MANUAL OPS OK DEFERRED PER DDPG 80-2. 2L74 4F4 F A20WE E3NE 20041108000232004110800023NM 2004 11 8 P5CA0401261 120041017A5330 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CANNING A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 BS 2360 TO 2380 STRINGER LEFT IS OIL CANNING. PERFORM HFEC, NO CRACKS. REMOVED AND REPLACED SKIN PER SRM 51-10-02. 2L74 4F4 F A20WE E20EA 20041108000242004110800024NM 2004 11 8 P5CA0401262 120041017A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 LEFT WING STATION 382 UPPER SURFACE ON TOP PANEL BY STRUT DELAMINATED & CRACKED. REMOVE PANEL & REBONDED, REINSTALLED PER SRM 51-10-09. 2L74 4F4 F A20WE E20EA 20041108000302004110800030NM 2004 11 8 04278426 120041004A2731 RELAY DORNERDO32 DO328300 NM ELEVATOR TRIM FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27426FJ 3190 AFTER DEPARTURE, CREW RECEIVED NORMAL ELEVATOR TRIM FAIL INDICATION. RETURNED TO FIELD SAFELY. MX REMOVED AND REPLACED RELAYS 42CC AND 45CC IAW JIC 27-32-00. 2H72 4T RTA55NM 20041108000652004110800065SO 2004 11 8 RAIA00409016 120040918A3010MS3566070 RELAY EMB 145 EMB145LR 3260212SO ANTI ICE SYSTEM INOPERATIVE A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03836HK 145695 STL - WING/STAB ANTI-ICE FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED ANTI-ICE SYSTEM RELAYS K0528 AND K0552. 2L72 4T RTT00011AT 20041108000752004110800075WP 2004 11 8 ABXA040362 120041031A5330577992549 SKIN DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 EXTERIOR LOWER FUSELAGE SKIN CRACKED AND BULGED AT LONGERON 35 RIGHT, FS 102. REMOVED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21. REINSTALLED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-20D. REPAIRED SKIN IAW REA D853-50299MR. ALODINED AND PRIMED REPAIR DOUBLER IAW DC-8 SRM 51-1-8. 2L74 4F 4A25 20041108000762004110800076WP 2004 11 8 ABXA040364 120041030A532057501992 SUPPORT DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 RIGHT FUSELAGE STA 915 - 935, SUPPORT BRACE OUTBOARD OF LONGERON 24 RIGHT, EXFOLIATED. REPAIRED AREA IAW REA D853-50298-MR. 2L74 4F 4A25 20041108000772004110800077WP 2004 11 8 ABXA040365 120041030A5330577331153 DOUBLER DOUG DC8 DC863F 302198FWP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 AREAS OF CORROSION NOTED ON LOWER SKIN AROUND OUTFLOW VALVE (AFT ACCESSORY COMPARTMENT) FROM FLOOR FRAME 1620 - 1640, LONGERON 34 RIGHT TO 34 LEFT. REMOVED ALL SUBSTRUCTURE AND FASTENERS COMMON TO REPAIR AREA TO FACILITATE REPAIR. REMOVED ALL CORROSION IAW DC-8 SRM 53-2-0. COMPLIED WITH REA D853-50305-MR AND D853-50305-MR REV A. ALODINED AND PRIMED ALL PARTS IAW DC-8 SRM 51-1-8. REINSTALLED ALL SUBSTRUCTURE AND FASTENERS COMMON TO REPAIR AREA IAW DC-8 SRM 51-1-20D. 2L74 4F 4A25 20041108000832004110800083EU 2004 11 8 RAIA00409002 120040903A3260AIR035668 SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03556HK 41073 STL - LANDING GEAR SELECTOR RED LIGHT REMAINED ON AFTER RAISING GEAR. MAINTENANCE REMOVED AND REPLACED NR 2 UPLOCK SWITCH. 2L72 4T RTA41NM 20041108000842004110800084SO 2004 11 8 RAIA00409005 120040907A36107276045 FILTER EMB 145 EMB145 3260210SO NR 2 ENGINE DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03801HK 145053 BLEED NR 2 OVERTEMP INDICATION. MAINTENANCE REMOVED AND REPLACED NR 2 ENG FAN AIR VALVE FILTER. 2L72 4F RTT00011AT 20041108000852004110800085SO 2004 11 8 RAIA00409009 120040914A801135059106 STARTER EMB 145 EMB145LR 3260212SO NR 2 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03825HK 145510 AUS - ENGINE NR 2 WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 2 STARTER. 2L72 4T RTT00011AT 20041108000872004110800087SO 2004 11 8 RAIA00409007 120040911A361014521167410 DUCT EMB 145 EMB145LR 3260212SO BLEED AIR SYS DISTORTED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 STL - BLEED NR 2 LEAK INDICATIONS. MAINTENANCE REMOVED AND REPLACED BLEED AIR DUCT. 2L72 4T RTT00011AT 20041108000912004110800091EA 2004 11 8 04274655 120040930A3240 BRAKE ASSY CNDAIRCL600 CL6002B19 1900309EA NR 4 STICKING A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27655BR 7457 EVENT SUMMARY STATES THAT AIRCRAFT PULLS HARD TO RIGHT. PERFORMED INSP OF WHEELS AND BRAKES. FOUND NR 4 BRAKE STICKING. CLEANED AND TESTED IAW MM 32-43-00. CHECKS GOOD ON TAXI CHECK BY CREW. 2L72 4F RTA21EA 20041108000972004110800097NM 2004 11 8 04259421 120040915A3260 WARNING LIGHT DORNERDO32 DO328300 NM MLG ILLUMINATED A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27421FJ 3179 IN DESCENT PHASE CREW HAD A HYD SYS-A FAIL AMBER CAS. CREW DID UNSAFE GEAR INDICATION PROCEDURE IN ORDER TO USE THE EMERGENCY GEAR HANDLE TO LOWER THE GEAR. ON BASE LEG GEAR WAS LOWERED & CREW GOT THREE GREEN LIGHTS, THEREFORE MADE A NORMAL LANDING. MX RESET CIRCUIT BREAKERS AND LANDING GEAR AFTER EMERGENCY EXTENSION. 2H72 4T RTA55NM 20041108001092004110800109NE 2004 11 8 RAIA00408033 220040829A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE LEFT MALFUNCTIONED A RAIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CE03555HK 41072 75093 TRI - ABORTED TAKEOFF DUE TO HIGH EGT AT LOW POWER SETTING ON LEFT ENGINE. MAINTENANCE PERFORMED GROUND RUN,BUT COULD NOT DUPLICATE REPORTED PROBLEM. 2L72 4T4 TRTA41NM E18NE 20041108001132004110800113SO 2004 11 8 RAIA00409026 120040928A276014533022409 CONTROLLER EMB 145 EMB145LR 3260212SO SPOILERS MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03844HK195 14500838 EWR - SPOILER FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED SPOILER CONTROL UNIT. 2L72 4T RTT00011AT 20041108001322004110800132SO 2004 11 8 LR7A04190 120041013A53433723312 BEAM LKHEED382 382G 526414USO MLG CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND LT MLG BAY FS 557 LOWER BOW BEAM TEE CAP CRACKED AT WL 171, LBL 66. REPLACED BOW BEAM IAW DWG 372330 AND SRM SMP 583 51-70 AND 53-40-02. 2H74 4T A1SO 20041108001332004110800133SO 2004 11 8 LR7A04191 120041013A5320 ANGLE LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND LOWER LBL 60 CHINE ANGLE CRACKED AT FS 617, WL 142. REPAIRED IAW ARM SMP 583 53-40-26. 2H74 4T A1SO 20041108001342004110800134SO 2004 11 8 LR7A04192 120041013A53203730051R STIFFENER LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 719 4763 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND RT MLG BAY LOWER SKIN SPLICE STIFFENER FLANGE CRACKED AT FS 537, WL 175, RBL 62. REPLACED SKIN SPLICE FS 537 - 557 IAW SRM SMP 583 51-70. 2H74 4T A1SO 20041108001432004110800143EA 2004 11 8 04257624 120040913A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA CABIN COOLING INOPERATIVE A VTZAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 EA27624BR 7211 CREW REPORT STATED THAT WITH ONE PACK DEFERRED, RECEIVED PACK OVER PRESSURE WARNING ON T/O ROLL. ABORTED T/O. RESET AND SUCCESSFULLY TOOK OFF. NO RETURN TO GATE. 2L72 4F RTA21EA 20041108001452004110800145EA 2004 11 8 04256621 120040912A2710 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA AILERON ILLUMINATED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27621BR 7186 CREW REPORT STATED TAKEOFF ROLL SET THRUST, ACCELERATED TO 40KTS OR SO AND TAKEOFF CONFIG AILERON WARNING ILLUMINATED. TRIMS WERE SET CORRECTLY AND TAKEOFF CONFIG WAS ON DURING INITIAL ROLL ON RUNWAY. THEN ABORTED TAKEOFF, CONTACTED MAINT AND DISPATCH AND PROCEEDED WITH ANOTHER TAKEOFF UNEVENTFUL. 2L72 4F RTA21EA 20041108001472004110800147EA 2004 11 8 04268664 120040924A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27664BR 7528 FLAPS FAIL AT 30 DEGREES. RECORDER FAULTS FLAP CNTL LEVER, WIRING, UNSPECIFIED. RESET FECU REF 27-50-00. OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20041108001502004110800150CE 2004 11 8 4019 120040813A2612 WARNING LIGHT LEAR 25 25D 5170514CE GE CJ610 CJ6108 30006NE ENGINE FIRE ILLUMINATED E BSYAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION APAPPROACH 1 GL07228SW 228 251800 ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES. 2L72 4J4 J A10CE 1E16 20041108001522004110800152EA 2004 11 8 04269693 120040925A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STABILIZER INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27693BR 7761 STAB TRIM/MACH TRIM MSG. RESET HSTCU. NO FAULTS FOUND NOTED. FUNC IAW 27-40-00. 2L72 4F RTA21EA 20041108001552004110800155NM 2004 11 8 P5CA0401270 120041101A2820 FUEL SYS BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE RT WING LEAKING A P5CAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA15920FT 22237 A/C RETURN TO BLOCK DUE TO FUEL GOING OVERBOARD FROM RIGHT WING VENT BOX. DRAINED SURGE TANK, CHECKED FUELING SYSTEM PER AMM 28-21-00, CHECKS NORMAL WITH ALL PUMPS RUNNING & FUELING DUCTS PRESSURIZED. 2L74 4F4 F A20WE E3NE 20041108001602004110800160SO 2004 11 8 RAIA00410020 120041022A3230 PACKING EMB 145 EMB145LR 3260212SO NLG DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03813HK 145044 STL - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED PACKING ON NOSE LANDING GEAR. 2L72 4T RTT00011AT 20041108001892004110800189NM 2004 11 8 CALA0400688 120041028A575465C26793 SKIN BOEING737 7373T0 1384582NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712327 23457 INSPECTION FOUND A .25 INCH CRACK IN NR 3 SLAT SKIN BELOW ACTUATOR. A DOUBLER WAS INSTALLED ON LOWER SKIN IAW SRM 57-43-01. 2L72 4F RTA16WE 20041108001922004110800192EA 2004 11 8 04272698 120040928A3350 PANEL CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DEFECTIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27698BR 7799 EMERGENCY LIGHTS STAYED ON WITH SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS PANEL. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108001952004110800195NM 2004 11 8 2004UALA00963 120041017A3260 SQUAT SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GRD SENSING MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29366UA 24535 DUE TO LOSS OF CABIN PRESSURE, AIRCRAFT DESCENDED TO A LOWER ALTITUDE CAUSING ADDITONAL FUEL BURN. FLIGHT DIVERT- TO BNA FOR ADDITIONAL FUEL. SUSPECTED GND SENSING SQUAT SW M990 FAILED. REPLACED M990 AS PRECAUTION AND ADJUSTED MLG SAFETY SENSOR. 2L72 4F4 FRTA16WE E2GL 20041108001972004110800197SO 2004 11 8 LR7A04102 120041001A5541 BEAM LKHEED382 382G 526414USO RUDDER CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5511 FOUND RUDDER INTERNAL AUX BEAM AND STIFFENERS WITH CRACKS AT FS 1128.5, BL 0, VSS 10. REPAIRED IAW SRM SMP 583 51-140-18. BALANCE CHECK CARRIED OUT IAW SMP 583 51-50, PARA D. 2H74 4T A1SO 20041108001992004110800199NM 2004 11 8 SWAA043142 120041028A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND RT FUSELAGE CREASE BEAM WEB CORRODED BETWEEN BS 380 AND BS 420. REPAIRED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20041108002012004110800201NM 2004 11 8 SWAA043144 120041028A3350PL2230LH00 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER STRIPS BROKEN AT ROWS 22, 13, 11, 3 AND 1. REMOVED AND REPLACED COVER STRIPS PER MM. 2L72 4F RTA16WE 20041108002032004110800203NM 2004 11 8 SWAA043146 120041028A53116546540 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 16L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20041108002052004110800205NM 2004 11 8 SWAA043148 120041028A571465C257231 BEAM BOEING737 7375H4 138449DNM CENTER WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED 1/2D CHECK, FOUND CENTER WING LONGITUDINAL BEAM CRACKED AT BS 616, LBL 45.57. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20041108002072004110800207NM 2004 11 8 SWAA043152 120041029A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29303SW 22943 DURING SCHEDULED C1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS BETWEEN BS 450 & BS 500A, STRINGER 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041108002092004110800209SO 2004 11 8 CV2XASH04543 120041102A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711119 145677 DURING C-CHECK THE LEFT OMEGA SHAPE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041108002112004110800211NM 2004 11 8 234TR0022 120041030A5312 BULKHEAD BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 AFT SIDE OF BS 1016 BULKHEAD AT BL 0 CORRODED. REPAIRED PER SB737-53A1075. 2L72 4F RTA16WE 20041108002132004110800213SO 2004 11 8 C2XA04SH542 120041029A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713118 145675 DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. 2L72 4F RT 20041108002182004110800218SO 2004 11 8 C2XA04BT113 120041025A335078241 INVERTER EMB 145 EMB145 3260210SO FUSELAGE FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716961 145103 EWR - CREW REPORTED, FORWARD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY EXIT SIGN INVERTER. OPS CHECKED GOOD IAW EMB145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041108002242004110800224NM 2004 11 8 SWAA043213 120041104A3350OL307IBPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29716SW 27850 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 9 ABC INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20041108002262004110800226NM 2004 11 8 371PA0064 120040916A5311 FRAME BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FRAME CRACKED IN RADIUS AT BS 480 AND STR 25 LT. REPAIRED PER SRM 51-70-11. 2L72 4F RTA16NE 20041108002282004110800228NM 2004 11 8 371PA0071 120040920A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FWD CABIN FLOORBEAM AT BS 294.5 HAS CORROSION FROM LBL 12 TO RBL 45. REPAIRED PER SRM 53-10-51. 2L72 4F RTA16NE 20041109000022004110900002SO 2004 11 9 LR7A04197 120041103A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 4606 DURING CARGO LOADING NOTED CARGO IMPACT DAMAGE FS 880 - 888 CARGO DOOR EXTERNAL SKIN AT RBL 10, WL 205. REPAIRED IAW LAC MEA 382-53-04-090. LP 18093, GMM133 ITEM M3. 2H74 4T A1SO 20041109000032004110900003EA 2004 11 9 QXEA200400729 120041019A5310 BEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - NUT PLATE CHANNEL CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDE ON BEAM 280. REPAIRED IAW SRM 51-40-11, 51-21-00, 51-25-01. 2L72 4F RTA21EA 20041109000052004110900005EA 2004 11 9 QXEA200400731 120041019A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - CORROSION ON FLOORBEAM AT STATION FS 280.0 ON TOP FLANGE FROM LEFT HAND BL 30.0 TO RIGHT HAND BL 40.0. REPAIRED IAW HORIZON AIR EA R-53-212. 2L72 4F RTA21EA 20041109000072004110900007EA 2004 11 9 QXEA200400733 120041020A5280 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 700 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - LEFT HAND MAIN LANDING GEAR DOOR INBOARD DOOR SECTION HAS CRACK AT OUTER TIP FROM LEADING EDGE. REPAIRED IAW SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20041109000082004110900008EA 2004 11 9 QXEA200400734 120041020A5280 DOOR CNDAIRCL600 CL6002C10 1390015EA ZONE 700 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - RIGHT HAND MAIN LANDING GEAR DOOR INBOARD DOOR SECTION HAS CRACK AT OUTER TIP FROM LEADING EDGE. REPAIRED IAW CRJ 700 SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20041109000102004110900010EA 2004 11 9 QXEA200400716 120041015A5210 ATTACH ANGLE CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 MAIN CABIN DOOR ASSEMBLY TO MAIN CABIN DOOR SHELL AFT ATTACH ANGLE CRACKED APPROXIMATELY IN MIDDLE OF DOOR. REPAIRED IAW HORIZON AIR EA R-52-190 AND REO 670-52-11-072. 2L72 4F RTA21EA 20041109000112004110900011EA 2004 11 9 QXEA200400717 120041014A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX - FLOORBEAM FS 280 IS CRACKED TOP FLANGE 12 INCHES FROM CENTER RIGHT SIDE. REPAIRED IAW REO 670-53-11-045 AND HORIZON AIR EA R-55-211. 2L72 4F RTA21EA 20041109000182004110900018NM 2004 11 9 371PA0076 120040918A5320 INTERCOSTAL BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 INTERCOSTAL FROM BS 312 TO BS 328 AT LBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2L72 4F RTA16NE 20041109000202004110900020WP 2004 11 9 ABXA040360 120041019A52303926046503N FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 UPPER AFT STOP PAD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-9 SRM. 2L72 4F A6WE 20041109000242004110900024NM 2004 11 9 QXEA200400711 120041017A5270 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR FALSE INDICATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09400QX 4030 SEA - FLIGHT 2314 - THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF, AND DURING THE CLIMB, THE CREW RECEIVED A DOOR WARNING FOR THE FORWARD BAGGAGE DOOR. MAINTENANCE INSPECTED THE AIRCRAFT DOOR AND INTERROGATED THE PSEU. NO DISCREPANCIES WERE NOTED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041109000262004110900026NM 2004 11 9 371PA0052 120040915A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 FLOORBEAM AT BS 986 HAS CORROSION AT CLIP NUT HOLES FROM LBL 36 TO RBL 36. REPAIRED PER SRM 53-00-51. 2L72 4F RTA16NE 20041109000292004110900029WP 2004 11 9 ABXA040355 120041022A32105924841 TRUNNION DOUG DC9 DC941 302207NWP RT MLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 BOTH FORWARD TRUNNIONS EARS INNER SURFACES PITTED AND CORRODED ON RIGHT MAIN LANDING GEAR TRUNNION. REPAIRED AREA IAW REA D932-50887MR. 2L72 4F A6WE 20041109000312004110900031NM 2004 11 9 371PA0048 120040929A5280 SKIN BOEING737 737306 13844BGNM MLG DOOR DELAMINATED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 LEFT AND RIGHT MAIN LANDING GEAR DOORS HAVE DELAMINATION IN THE SKIN AT THE DOOR ATTACH FITTING. REPAIRED DAMAGE PER SRM 51-70-17 AND EA 53-258. 2L72 4F RTA16NE 20041109000332004110900033NM 2004 11 9 SWAA043236 120041106A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041109000362004110900036EA 2004 11 9 SWIA200414050 120041030A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07410SW 7066 THIRD AFT EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED 3RD AFT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD IAW MM 33-00-00. 2L72 4F RTA21EA 20041109000402004110900040EA 2004 11 9 SWIA200414027 120041027A261247259701 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA FIRE DETECTOR MALFUNCTIONED A SWIAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 NM07413SW1301013010 7102 ATTEMPT APU START AIRBORNE, RECEIVED APU FIRE MESSAGE AND AURAL, THEN FIRE FAIL (APU). REMOVED AND REPLACED FIRE CONTROL UNIT IAW 26-00-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109000422004110900042NM 2004 11 9 SWAA043219 120041105A5530 CLEVIS BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND VERTICAL STABILIZER AFT SPAR RT AND LT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED VERTICAL STABILIZER PER ER. 2L72 4F RTA16WE 20041109000442004110900044NM 2004 11 9 SWAA043221 120041105A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME AT LT BS 188, WL 208, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041109000462004110900046NM 2004 11 9 SWAA043224 120041105A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME SECTION AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041109000472004110900047EA 2004 11 9 SWIA200414043 120041101A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07710SK 10170 SPLR/STAB FAULT STATUS AND RUD LIMIT FAULT STATUS MSGS DISPLAYED. REMOVED AND REPLACED NR 1 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N C13045BA03, S/N OFF 767. 2L72 4F RTA21EA 20041109000482004110900048SO 2004 11 9 SWIA200414044 120041101A5210 DOOR EMB 120 EMB120ER 3260203SO MAIN CABIN BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07186SW 120034 MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED DOOR, CLEANED AND REPLACED HARDWARE IAW 52-10-00. 2L72 4T RTA31SO 20041109000492004110900049SO 2004 11 9 SWIA200414045 120041102A5753 ROLLER EMB 120 EMB120ER 3260203SO TE FLAPS BINDING A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07189SW 120048 CONTROL FAULT ON OUTBOARD PAIR OF FLAPS OCCURS AT TWO BARS OF FLAPS, WILL NOT RESET. REMOVED AND REPLACED ALL 4 ROLLERS OF LEFT OUTBOARD FLAP IAW 27-50-12. CLEANED CANNON PLUGS OF BOTH RIGHT AND LEFT OUTBOARD FLAPS. OPERATIONAL CHECKED GOOD. 2L72 4T RTA31SO 20041109000502004110900050SO 2004 11 9 SWIA200414008 120041025A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07587331956 100 120197 RECEIVED A FLAP CONTROL FAULT WHEN SELECTING FLAPS 25. REMOVED AND REPLACED LEFT NACELLE ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000512004110900051EA 2004 11 9 SWIA200414009 120041026A274170623 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED DEDESCENT 1 NM07916SW1217812178 7634 DURING DESCENT AP PITCH TRIM CAUTION ILLUMINATED. REPLACE HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW CRJ MM 27-40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 8316-3, S/N OFF 1080. 2L72 4F RTA21EA 20041109000532004110900053EA 2004 11 9 SWIA200414011 120041021A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA FLUTTER DAMPER TWISTED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07430SW7693 7693 7523 FLUTTER DAMPER STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR FLUTTER DAMPER IAW 27-34-05. REPAIRED TWISTED WIRE PAIR CR7B22WHY & CR81322BLU BETWEEN CONNECTORS J300 AND P268. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109000552004110900055SO 2004 11 9 SWIA200414013 120041014A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RT RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07189SW2574 2574 RIGHT RUDDER JAMMED. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW MM 27-22-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000562004110900056NM 2004 11 9 QXEA200400714 120041018A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM AFT CARGO FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09360PH* 2399 515 SEA - FLIGHT 2071 - THE CREW REPORTED AN INTERMITTENT SMOKE WARNING IN CRUISE FLIGHT. THERE WAS NO EVIDENCE OF SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 AFT CARGO PIT FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041109000572004110900057 2004 11 9 QXEA200400713 420041016A22107003974730 COMPUTER DHAV DHC8 DHC8202 2809007NM FLT GUIDANCE MALFUNCTIONED A QXEAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM09360PH230906778 515 RDM- AFTER TOUCHDOWN, BOTH MAIN GEAR ON THE GROUND, NOSE IN THE AIR, RT AILERON APPLIED FOR CROSSWINDS, CONTROL COLUMN FROZE IN PLACE AND HAD TO BE OVERPOWERED. BOTH PITCH AND ROLL STUCK IN PLACE. AIRCRAFT ACCOMPLISHED AN UNEVENTFUL TAXI TO THE GATE. FIRST OPERATION CHECK FLIGHT FAILED. MAINTENANCE REPLACED BOTH FLIGHT GUIDANCE COMPUTERS, AND THE AFCS CONTROL PANEL. SECOND OPERATIONAL CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. AFCS CONTROL PANEL S/N 90101208 (6778 TSR), NR 2 FLIGHT GUIDANCE COMPUTER S/N 96064529 (3317 TSR). 2H72 4T RTA13NM 20041109000582004110900058NM 2004 11 9 SWAA043237 120041106A531065458075 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR FRAME CUTOUT BELOW UPPER HINGE STUB FRAME CRACKED. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20041109000592004110900059NM 2004 11 9 SWAA043244 120041105A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041109000602004110900060 2004 11 9 SWAA043245 420041107A25656557463 FITTING BOEING737 7373H4 1384600NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR GIRT BAR FWD AND AFT FLOOR ATTACH FITTINGS CORRODED. REMOVED AND REPLACED FWD ENTRY DOOR GIRT BAR FITTINGS PER SRM. 2L72 4F RTA16WE 20041109000612004110900061NM 2004 11 9 234TR0026 120041030A5313 STRINGER BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 CORROSION ON STR 28 LT FROM BS 985 TO BS 1016. REPAIRED DAMAGED SECTION PER SRM 53-10-3. 2L72 4F RTA16WE 20041109000622004110900062NM 2004 11 9 SWAA043228 120041106A335010107451 COVER BOEING737 7373K2 13844BANM EMERGENCY SIGN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 FWD ENTRY EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20041109000632004110900063NM 2004 11 9 SWAA043229 120041106A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29726SW 27858 DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 9 ABC AND 11 ABC, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041109000652004110900065NM 2004 11 9 250TR0055 120041022A5330 SKIN BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION ON INSIDE OF FUSELAGE SKIN BETWEEN STR 24 RT AND STR 25 RT AT BS 1016+4. REPAIRED PER EA 53-294. 2L72 4F RTA16WE 20041109000672004110900067NM 2004 11 9 234TR0023 120041030A5320 STIFFENER BOEING737 737228 13844AGNM BULKHEAD CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 BS 1016 BULKHEAD FORWARD SIDE CHANNEL STIFFENER AT BL 0 HAS CORROSION. REPAIRED PER SB 737-53A1075. 2L72 4F RTA16WE 20041109000712004110900071SO 2004 11 9 SWIA200413994 120041021A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO OUTBOARD FLAP MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07188SW5461 5458 120039 FLAP CONTROL FAULT OUTER FLAPS STUCK 2 BARS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW 27-50-09. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000732004110900073SO 2004 11 9 SWIA200414028 120041027A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07251YV 120251 ONE RED EMERGENCY LIGHT BURNED OUT IN ROW 6. INSTALLED NEW BULB, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000752004110900075 2004 11 9 SWAA043195 420041103A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041109000792004110900079EA 2004 11 9 QXEA200400719 120041015A5310 BEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX - BEAM FS 280 TOP FLANGE HAS NUMEROUS SPOTS OF CORROSION ON EITHER SIDE OF COCKPIT ENTRANCE. REPAIRED IAW SRM 51-12-00. 2L72 4F RTA21EA 20041109000822004110900082SO 2004 11 9 SWIA200414029 120041027A2121AE1711AA0 FAN EMB 120 EMB120ER 3260203SO RT PACK SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07299SW7896 7896 120329 ON GROUND RIGHT PACK FILLED CABIN WITH SMOKE. REPLACED RIGHT GROUND COOLING FAN. OPERATIONAL CHECKED GOOD. 2L72 4T RTA31SO 20041109000842004110900084NM 2004 11 9 SWAA043230 120041107A324426066712 TIRE BOEING737 7373H4 1384600NM LT MLG FAILED A SWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW29322SW 23343 ON TAKEOFF FROM (JAN) HEARD LOUD NOISE SIMILAR TO A DOOR OR WINDOW OPEN, EVERYTHING ELSE NORMAL, DOOR HANDLE IN PROPER POSITION. FOUND THE NR 1 MAIN TIRE BURST ON TAKEOFF, DAMAGED 5 EACH NR 1 ENGINE FAN BLADES, 1 EACH ACOUSTIC PANEL, INNER AND MID MLG DOORS, LMLG SUPPORT SHELF PANEL, DENT ON FUSELAGE AND INBOARD MID FLAP. REMOVED AND REPLACED NR 1 MAIN TIRE AND WHEEL PER MM. 2L72 4F RTA16WE 20041109000852004110900085 2004 11 9 SWAA043238 420041106A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2L72 4F RTA16WE 20041109000872004110900087SO 2004 11 9 SWIA200414046 120041101A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07268UE2063 2063 120207 NACELLE FLAPS CREATE CONTROL FAULT - DO NOT EXTEND WITH INBOARD AND OUTBOARD FLAPS. MEGGED ALL FLAP ACTUATORS CONNECTORS IAW EMB MM 27-50-00. REPLACED FLAP ANNUNCIATOR. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE ACTUATOR PER MM 27-50-00. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041109000892004110900089NM 2004 11 9 250TR0038 120041022A5340 STRINGER CLIP BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 AFT SIDE OF TIE CLIP AT BS 1006 AND STR 27 LT HAS CORROSION. REPLACED TIE CLIP PER SRM 51-10-1. 2L72 4F RTA16WE 20041109000902004110900090NM 2004 11 9 250TR0039 120041022A5320 CLIP BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 FRAME TO SKIN ATTACH CLIP HAS CORROSION AT BS 967 BETWEEN STR 26 LT AND STR 25 LT. REPLACES ATTACH CLIP PER SRM 51-10-1. 2L72 4F RTA16WE 20041109000912004110900091NM 2004 11 9 250TR0045 120041022A5343654610913 BEAM BOEING737 7372K5 138448XNM MLG DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 AFT LUG ON THE RIGHT MAIN GEAR BEAM ARM HAS AN INDICATION OF A DEFECT. REPLACED WALKING BEAM ARM PER 737 MM 32-11-00. 2L72 4F RTA16WE 20041109000932004110900093 2004 11 9 SWIA200414019 420041026A3418C12851BA01 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STALL PROTECTIONMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07973SW STALL FAIL CAUTION MESSAGE SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT IAW CRJ MM 27-35-01. OPERATIONAL CHECK GOOD. P/N C12851BA01, S/N OFF 495. 2L72 4F RTA21EA 20041109000952004110900095EA 2004 11 9 SWIA200414021 120041026A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA APU DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07432SW 7548 STRONG SMELL OF FUEL UPON STARTING THE APU AFTER LANDING. INSPECTED APU ENCLOSURE AND ENGINE LEFT SIDE. NO FUEL LEAKING. ALL AREAS INSPECTED WERE DRY. RAN APU AND BOTH PACKS. NO FUEL SMELL NOTED. ALL CHECKS GOOD. 2L72 4F RTA21EA 20041109001022004110900102EA 2004 11 9 SWIA200414030 120041027A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07437SW7348 7348 7564 FLIGHT SPOILER FAULT CAUTION MESSAGE DURING TAXI OUT. REMOVED AND REPLACED NR 1 SECU IAW MM 27-60-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109001032004110900103EA 2004 11 9 SWIA200414031 120041030A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY MALFUNCTIONED A SWIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM07440SW 7589 IN CRUISE AT FL 330, SMOKE CARGO MESSAGE DIVERTED TO COS, FIRED BOTTLES IN CARGO BAY. REMOVED AND REPLACED LEFT AND RIGHT CARGO FIRE BOTTLES; REPLACED BOTH FORWARD AND AFT SMOKE DETECTORS IAW 26-15-01. OPERATIONAL CHECK GOOD. P/N 36500018-3, S/N OFF 4274801, P/N 34600037-1, S/N OFF 21098F1. 2L72 4F RTA21EA 20041109001052004110900105EA 2004 11 9 SWIA200414033 120041029A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07953SW 7813 ON DESCENT INTO SBA, CAPTAINS SIDE WINDOW CRACKED FROM LOWER FRONT TO UPPER REAR. REMOVED AND REPLACED CAPTAINS SIDE WINDOW IAW CRJ MM 56-12-01. P/N 601R-33033-11, S/N OFF 03013H4162. 2L72 4F RTA21EA 20041109001062004110900106SO 2004 11 9 SWIA200414034 120041029A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07232SW 120306 RED FLOOR LIGHTING MISSING AT EXIT 9B AND 9C. INSTALLED NEW RED EMERGENCY LIGHTING FLOOR RECEPTACLE IAW EMB 120 MM 33-52-01. READJUSTED EMERGENCY FLOOR LIGHTING COVER AND REPAIRED SECOND FORWARD RED LAMP. OPERATIONAL CHECK GOOD IAW 33-51-00. 2L72 4T RTA31SO 20041109001072004110900107SO 2004 11 9 SWIA200414035 120041025A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07214SW 120280 PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109001082004110900108NM 2004 11 9 250TR0044 120041022A5320 ANGLE BOEING737 7372K5 138448XNM FUSLEAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 DRAG ANGLE CRACKED UNDER LEFT FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-290. 2L72 4F RTA16WE 20041109001092004110900109NM 2004 11 9 250TR0047 120041022A5340 ATTACH ANGLE BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 ATTACH ANGLE AT BS 663 BELOW WALL TO FLOOR TRANSITION ANGLE CRACKED, RIGHT SIDE. REPLACED ATTACH ANGLE PER SRM 51-10-2 AND SRM 53-10-2. 2L72 4F RTA16WE 20041109001102004110900110NM 2004 11 9 250TR0046 120041022A5320 SCUFF PLATE BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 FORWARD CARGO THRESHOLD FWD AND AFT CORNER SCUFF PLATES CRACKED. REPAIRED PER BOEING SPEC BAC5975. 2L72 4F RTA16WE 20041109001112004110900111NM 2004 11 9 250TR0048 120041022A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 FORWARD CARGO INTERCOSTAL WEB CRACKED UNDER THRESHOLD AT STR 26 RT AT BS 460+10. REPAIRED PER SRM 51-40-3 AND SRM 51-30-02. 2L72 4F RTA16WE 20041109001122004110900112NM 2004 11 9 250TR0058 120041022A5313 STRINGER BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION ON STR 26 LT BETWEEN BS 986 AND BS 1006. REPAIRED PER EA 53-292 AND SRM 53-10-1. 2L72 4F RTA16WE 20041109001132004110900113NM 2004 11 9 250TR0053 120041022A5340 ATTACH ANGLE BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 INTERCOSTAL WEB ATTACH ANGLE CRACKED AFT SIDE OF FRAME AT BS 500 AT STR 28 RT IN FORWARD CARGO BIN. REPLACED ANGLE PER BOEING DWG 69-37261 AND SRM 51-30-2. 2L72 4F RTA16WE 20041109001152004110900115WP 2004 11 9 ABXA040353 120041022A57435924841 ATTACH FITTING DOUG DC9 DC941 302207NWP RT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 DURING ROUTINE GEAR CHANGE, FOUND CORROSION BEYOND LIMITS ON THE RIGHT MAIN LANDING GEAR ATTACH FITTING FORWARD LUG FORWARD FACE AND FORWARD LUG AFT FACE. REPAIRED ATTACH FITTING LUGS BY SPOT FACING AND INSTALLING WASHERS TO REGAIN BLUE PRINT DIMENSIONS IAW REA D932-50887MR. 2L72 4F A6WE 20041109001162004110900116SO 2004 11 9 SWIA200414025 120041024A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07268UE9382 9378 120207 CONTROL FAULT WITH ASSOCIATED MAP WARNING LIGHTS CAME ON DURING TAXI AND ONCE DURING APPROACH. REPLACED FCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109001182004110900118SO 2004 11 9 C2XA04BT110 120041017A3350110049 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714953 145071 BTV, DURING SERVICE AND ROUTINE CHECK ON RON, MAINTENANCE FOUND THE PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041109001192004110900119NM 2004 11 9 750WL0009 120041103A33505417N509 SOCKET BOEING757 757200 1384950NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 ROW 30 EMERGENCY FLOOR TRACK LIGHT INTERMITTENT. REPLACED FLOOR LIGHT SOCKET PER MM 33-51-11. OPS CHECKS GOOD. 2L72 4F RTA2NM 20041109001212004110900121EA 2004 11 9 QXEA200400699 120040930A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - CABIN FLOORBEAM LOCATED AT FS 280.00 HAS A SERIES OF CRACKS EXTENDING FROM RIVET HOLE AT WL 72.00 BETWEEN RBL 10.5 AND RBL 12.0. REPAIRED IAW HORIZON AIR EA R-53-209. 2L72 4F RTA21EA 20041109001232004110900123EA 2004 11 9 QXEA200400695 120040930A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - CABIN FLOORBEAM LOCATED AT FS 280.00 HAS TWO CRACKS IN UPPER FLANGE, LOCATED AT LBL 13.00. CRACKS RUN FROM RIVET HOLE TO AFT EDGE OF FLANGE. REPAIRED IAW HORIZON AIR EA R-53-209. 2L72 4F RTA21EA 20041109001252004110900125WP 2004 11 9 ABXA040357 120041006A5420591326266 ATTACH ANGLE DOUG DC9 DC933F 302207AWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 NR 1 PYLON UPPER ATTACH ANGLE WAS CRACKED. REPAIRED ATTACH ANGLE IAW DC-9 SRM 54-04. 2L72 4F A6WE 20041109001262004110900126WP 2004 11 9 ABXA040356 120041006A53159922393501 FLOORBEAM DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 CUT OUT AND REPAIR ANGLE ON FLOORBEAM AT FS 294, CORRODED RIGHT BUTT LINE 6. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20041109001272004110900127EA 2004 11 9 SWIA200414040 120041023A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07457SW 7773 CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 LBL 40. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AT F.S 621.00, LBL -40, IAW CRJ REO 601R-53-61-117, REV "B". 2L72 4F RTA21EA 20041109001292004110900129NE 2004 11 9 ABXA040368 220041102A7314378200 PUMP DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE RT ENGINE FUEL DEFECTIVE A ABXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION APAPPROACH 1 GL23923AX1019 47165 657025 RIGHT ENGINE FLAMED OUT ON SHORT FINAL TO ILN, SPEED 135 KT, ALT 2100. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP IAW DC-9 MM 73-10-01-2. REMOVED AND REPLACED NR 2 ENGINE FCU IAW DC-9 MM 73-20-01-2. 2L72 4F4 F A6WE E2EA 20041109001312004110900131WP 2004 11 9 ABXA040349 120041009A5610 FRAME DOUG DC9 DC932 3022066WP COCKPIT WINDOW DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN, PREVENTING IT'S USE AS AN EMERGENCY EXIT. FOUND CAPTAIN'S AFT WINDOW TRIM DAMAGED BEYOND REPAIR. CUT AWAY DAMAGED AREA. CLEARVIEW WINDOW OPERATIONAL CHECK GOOD. 2L72 4F A6WE 20041109001332004110900133EA 2004 11 9 SWIA200414038 120041023A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07457SW 7773 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00 LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-25-16 AND 51-21-11, RII 53-401. 2L72 4F RTA21EA 20041109001352004110900135EA 2004 11 9 SWIA200414047 120041102A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA FLIGHT SPOILERS MALFUNCTIONED A SWIAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07946SW 7776 ON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE ON ED 2. REMOVED AND REPLACED NR 2 SECU PER MM 27-61-05. REPLACED LEFT HAND INBOARD PCU PER MM 27-60-00. OPERATIONAL CHECK GOOD. P/N: 49-164-06, S/N OFF: 01724. 2L72 4F RTA21EA 20041109001372004110900137NM 2004 11 9 250TR0057 120041022A5330 SKIN BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CRACK AT FORWARD END OF OXYGEN SERVICE PANEL CUTOUT. REPAIRED PER EA 53-288 AND SRM 53-30-3. 2L72 4F RTA16WE 20041109001392004110900139 2004 11 9 SWAA043199 420041103A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE DOOR CABLE PER MM. 2L72 4F RTA16WE 20041109001412004110900141NM 2004 11 9 SWAA043201 120041104A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 TWO EACH FUSELAGE SKIN CRACKS AT BS 432, STRINGER 17L AND BS 495, STRINGER 16R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041109001422004110900142NM 2004 11 9 SWAA043202 120041104A53306545766 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 767, STRINGER 19R AND BS 927, STRINGER 25R. REPAIRED SKIN SECTIONS PER EA AND SRM. 2L72 4F RTA16WE 20041109001432004110900143NM 2004 11 9 SWAA043231 120041105A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041109001442004110900144NM 2004 11 9 SWAA043232 120041105A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 440, STRINGER 26L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000212004110500021NM 2004 11 5 SWAA043182 120041102A5311BAC1490 GUSSET BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT FWD LOWER STOP FITTING GUSSET, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR GUSSET PER SRM. 2L72 4F RTA16WE 20041105000292004110500029 2004 11 5 SWAA043177 420041102A2565D31354 SLIDE BOEING737 7372H4 138448CNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041105000302004110500030 2004 11 5 SWAA043173 420041102A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041105000322004110500032 2004 11 5 SWAA043175 420041102A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041105000332004110500033NM 2004 11 5 SWAA043159 120041027A53116546540 FRAME BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED PM CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM & SWA EA. 2L72 4F A16WE 20041105000342004110500034NM 2004 11 5 SWAA043160 120041028A5320907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29616SW 27699 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR CUTOUT LOWER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM. 2L72 4F RTA16WE 20041105000402004110500040NM 2004 11 5 SWAA043150 120041030A27506555541 BEARING BOEING737 7373H4 1384600NM RT WING TE FLAPSBROKEN A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29653SW 28398 SUSPECT SINGLE SPINDLE T/E FLAPS FAILURE, AT FLAPS 5 180 KNOTS HEARD LOUD POP, EXPERIENCED SLIGHT YAW AND SLIGHT ROLL, VERY CONTROLLABLE. NORMAL LANDING. REMOVED AND REPLACED RT INBOARD T/E FLAP BOOM CABLE DRUM BEARING PER MM. 2L72 4F RTA16WE 20041105000442004110500044NM 2004 11 5 SWAA043135 120041027A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 8L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041105000492004110500049SO 2004 11 5 LR7A04094 120041001A5312 TEE FITTING LKHEED382 382G 526414USO BULKHEAD CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 TO FS 577, WL 175 OUTER SHELF TEE CORRODED AT RBL 67. REPLACED TEE IAW DWG 372478 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041105000552004110500055NE 2004 11 5 C8GA20040018 220040818A7230 COMPRESSOR BOEING727 727230 1384080NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE STALLED A C8GAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO15357KP 20675 700568 FLT 707 FROM KPHX TO KMCI. AFTER SETTING MAX POWER, THE NR 2 ENGINE COMPRESSOR STALL TRIPPING THE PACKS OFF. ABORTED TAKEOFF AND RETURNED TO RAMP WITH NO FURTHER INCIDENT. INSPECTED NR 2 ENGINE FOR DAMAGE WITH NO DEFECTS NOTED IAW B727 MM 71-00 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041108000022004110800002NM 2004 11 8 EIA20041130 120040616A5312 PRESSURE PANEL BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE FUSELAGE DELAMINATED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 MAIN CABIN STA 1380, RBL 75.9, PRESSURE DECK WEB SHOWS EVIDENCE OF DELAMINATION. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR IAW SRM 51-10-07, FIG 251-30-05 PGS 6-9, AND 51-30-02. 2L74 4F4 F A20WE E20EA 20041108000092004110800009NM 2004 11 8 EIA2004104 120040512A5310 STRUCTURE BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 CRACK IN OUTER RING CHORD, STA 140R AT STR 22. STOP DRILL CRACK AT STA 140R, STR 22. NDT VERIFIED NO CRACK CONDITION REMAINED. ALODINED & PRIMED. REPAIRED PER EO 53-747-1730-04 REV A & SB 747-53-2355 FIG 5, PG 52, & 70-2138-05-0715 2L74 4F A20WE 20041108000142004110800014EA 2004 11 8 COMA0460595 120041102A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01940CA 7048 FLIGHT 5152 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20041108000252004110800025NM 2004 11 8 P5CA0401263 120041027A2820 FUEL CELL BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE RT WING OVERSERVICED A P5CAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA15509MC 21221 FUEL SPILL RIGHT WING. FOUND NR 4 MAIN OVER FILLED. DRAINED RIGHT SURGE TANK IAW 28/21/00, RESET SYSTEM & CONTINUED FUELING. CHECK OF VOLUMETRIC SYSTEM IAW 28-21-00 SATISFACTORY. 2L74 4F4 F A20WE E23EA 20041108000262004110800026EA 2004 11 8 COMA0460591 120041029A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01914CA2226819422 7012 FLIGHT 5776 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP PDU. 2L72 4F RTA21EA 20041108000422004110800042NE 2004 11 8 04243425 220040830A7250 TURBINE BLADES DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DAMAGED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27425FJ 3189 PCECD0155 BURNING SMELL ON TAKEOFF. DURING BORESCOPE INSPECTION OF RT ENGINE 1ST STAGE HPT BLADE, MX FOUND LEADING EDGE COATING LOOSE. ENGINE IS BEING CHANGED, WAS BAD FROM STOCK. 2H72 4T4 FRTA55NM E35NE 20041108000492004110800049SO 2004 11 8 RAIA00408030 120040827A324431590 TIRE EMB 145 EMB145LR 3260212SO NR 3 SEPARATED A RAIAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 CE03811HK 145256 PIT - UPON INSPECTION AT PIT, FOUND NR 3 TIRE TREAD HAD COME OFF. MAINTENANCE REMOVED AND REPLACED NR 3 TIRE, INSPECTED AIRCRAFT AND REPAIRED DAMAGE TO AIRFRAME AND ENGINE, AS REQUIRED. 2L72 4T RTT00011AT 20041108000532004110800053NM 2004 11 8 04253420 120040909A5610001A561A0000215 WINDSHIELD DORNERDO32 DO328300 NM COCKPIT CRACKED A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27420FJ 3178 RIGHT OUTBOARD WINDOW CRACKED DURING CLIMB PHASE. RTF AND REMOVED AND REPLACED WINDOW. 2H72 4T RTA55NM 20041108000612004110800061EA 2004 11 8 04252652 120040907A1420 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A VTZAO OTHER L NO TEST NRNOT REPORTED 1 EA27652BR 7429 RIGHT FWD EMERGENCY LIGHT INOP. RECONNECTED CONNECTOR ON EMERGENCY BATTERY REF AMM 33-51-04. OPS CHECK GOOD. 2L72 4F RTA21EA 20041108000792004110800079WP 2004 11 8 ABXA040367 120041030A532097596121 CUSP WEB DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23811AX 46113 MAIN CABIN AT FS 1164 - 1170 AND LONGERON 21 RIGHT (CUSP) HAD CORROSION. REPAIRED AREA IAW DC-8 SRM 51-1-8 AND REA D853-50301-MR. 2L74 4F 4A25 20041108000822004110800082SO 2004 11 8 RAIA00409010 120040914A325012302328403 TILLER EMB 145 EMB145LR 3260212SO NLG STEERING INOPERATIVE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03810HK9308 145231 PIT - AFTER LANDING HAD NO NW STEERING WITH TILLER. MAINTENANCE REMOVED AND REPLACED TILLER ASSY. 2L72 4T RTT00011AT 20041108000902004110800090GL 2004 11 8 RAIA00411002 220041102A7532 BLEED VALVE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE STICKING A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03829HK 145281 311453 PIT - ATTCS HAS NO MARGIN. MAINTENANCE INSPECTED ENGINE COMPRESSOR BLEED SYSTEM. FOUND LOWER COMPRESSOR AIR BLEED VALVE TO BE STICKING. CLEANED VALVE. 2L72 4T4 FRTT00011ATTE6CH 20041108000922004110800092EA 2004 11 8 04272706 120040928A2840 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM ILLUMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27706BR 7553 EVENT SUMMARY STATED FUEL WARNING AND FUEL IMBALANCE INDICATIONS AFTER TAKEOFF; DID NOT DECLARE EMERGENCY; LANDED UNEVENTFULLY. OPENED WORK ORDER AND STILL IN APPR STATUS. 2L72 4F RTA21EA 20041108000982004110800098EA 2004 11 8 04259702 120040915A3110 LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27702BR 7462 ALL COCKPIT OVERHEAD PANEL LIGHTS FLICKERING. REMOVED AND REPLACED LAMP DRIVER UNIT REF 31-41-07. OPS CHECK NORMAL. 2L72 4F RTA21EA 20041108001032004110800103NE 2004 11 8 P5CA0401260 220041024A7421CH31785 IGNITER BOEING747 747341 13848AMNM GE CF6 CF650E2 30018NE NR 3 ENGINE FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23355MC 23395 517967 NR 3 ENGINE IGNITION INOP ON START. REPLACED BOTH IGNITER PLUGS PER AMM 74-21-02 & SYSTEM OPS TEST OK PER AMM 74-00-00/501. 2L74 4F4 FRTA20WE E23EA 20041108001062004110800106NE 2004 11 8 RAIA00409019 220040920A72613104053 TUBE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114GR 01514NE NR 1 ENGINE LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03550HK 41039 75018 COU - LEFT OIL CAP LOW INDICATION LIGHT CAME ON, SHUT DOWN ENGINE. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE TURBINE BEARING SUPPLY TUBE. 2L72 4T4 TRTA41NM E18NE 20041108001122004110800112EU 2004 11 8 RAIA00409025 120040926A1420 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE DAMAGED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03558HK 41071 SYR - RIGHT ENGINE TORQUE INDICATION ERRATIC. MAINTENANCE REPAIRED RIGHT ENGINE TORQUE RING CONNECTOR. 2L72 4T RTA41NM 20041108001372004110800137NE 2004 11 8 DJFA2004010 220040712A7200 ENGINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE NR 1 AND 2 SHUTDOWN E DJFAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 EA23455CW RK365 PCEJA0511 AIRCRAFT DEPARTED KDUC TO KRSW AT FL410. AFTER STARTING DESCENT, THE PILOTS NOTICED THAT BOTH ENGINES WERE OUT. DURING DESCENT THE CREW TRIED STARTING THE NR 2 ENGINE, IT DID NOT START. TRIED THE NR 1 ENGINE IT WOULD NOT START. TRIED THE NR 2 ENGINE AGAIN AND IT STARTED AT ABOUT FL170, DID NOT TRY THE NR 1 ENGINE AGAIN. THE CREW THEN DIVERTED TO KSRQ. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. THIS INCIDENT IS BEING INVESTIGATED BY THE NTSB AND AT THIS POINT THERE HAS BEEN NO CONCLUSION OF THE CAUSE OF THE FAILURE. 2H72 4F4 FRTA16SW E25EA 20041108001642004110800164EA 2004 11 8 COMA0460588 120041028A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR UNSECURE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01712CA 7244 FLIGHT 5812 CABIN DOOR HANDLE CAUTION MESSAGE. FOUND DOOR HANDLE NOT STOWED. OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS FOUND. 2L72 4F RTA21EA 20041108001662004110800166EA 2004 11 8 COMA0460558 120041005A3150 COMPUTER CNDAIRCL600 CL6002B19 1900309EA RUDDER CONFIG MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01796CA 7338 FLIGHT 5426 CONFIG RUDDER AND CONFIG TRIM WARNING DURING T/O. COULD NOT DUPLICATE. HIGH SPEED TAXI SATISFACTORY. A/C RETURNED TO SERVICE. 2L72 4F RTA21EA 20041108001702004110800170NM 2004 11 8 04286425 120041012A2121 FAN DORNERDO32 DO328300 NM CABIN COOLING STALLED A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27425FJ 3189 CAS MESSAGE FOR HX FAN FAILURE WHILE TAXIING. MX REMOVED AND REPLACED FAN. 2H72 4T RTA55NM 20041108001722004110800172SO 2004 11 8 LR7A04100 120041001A55113726651R SPAR CAP LKHEED382 382G 526414USO CORRODED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5511 FOUND RT FORWARD SPAR UPPER CAP CORRODED AT FS 1043, HSS 58R - 63R, WL 248. REPLACED BEAM CAP IAW DWG 372665 AND SRM SMP 583 51-70. 2H74 4T A1SO 20041108001732004110800173SO 2004 11 8 LR7A04062 120040623A5512 SKIN LKHEED382 382G 526414USO STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 321 4698 DURING SCHEDULED A1 INSPECTION PER JOB CARD HA1201 FOUND LT HORIZONTAL STAB UPPER SURFACE SKIN CRACKED APPROX 1.0 INCH AT FS 1093, HSS 221 L, WL 283. REPAIRED IAW SRM SMP 583 55-20-06. LP 15420, ITEM M3. 2H74 4T A1SO 20041108001762004110800176 2004 11 8 RAIA00410017 420041019A3414 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU AIRSPEED INDICATDISCONNECTED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03572HK 41091 PIT - ON TAKEOFF, CAPTAIN'S AIRSPEED NEVER CAME ALIVE, COMPARATOR ERROR AS WELL. MAINTENANCE INSPECTED ADC NR 1 FOUND LOOSE QUICK DISCONNECT RESCUED. 2L72 4T RTA41NM 20041108001782004110800178NE 2004 11 8 HAEA200400164 220040816A7200CF7002D2 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE LEFT FLAMED OUT E HAEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW05295TW160519268 5 245U272 DURING NORMAL CRUISE CLIMB TO FL350 ATC ISSUED 30 DEGREE HEADING CHANGE FOR TRAFFIC. ONCE CLEAR TRAFFIC ATC ISSUED VECTORS DIRECT RZC. A RIGHT TURN WAS INITIATED WITH THE AUTOPILOT. BEFORE THE AIRCRAFT WAS ESTABLISHED IN THE TURN THE RIGHT TURN, THE LT ENGINE FLAMED OUT. A DESCENT WAS REQUESTED AND GRANTED TO FL250. AS THE AIRCRAFT PASSED FL290 THE LT ENGINE WAS REGAINED. A REQUEST TO FL310 WAS REQUESTED AND GRANTED. NO EMERGENCY DECLARED, NO PRIORITY HANDLING. NO FURTHER PROBLEMS DURING THE FLIGHT. UPON ARRIVAL KADS PERFORMED VISUAL INSPECTION THROUGH THE INLET, THE EXHAUST AND UNDER THE COWLING USING NORMAL PREFLIGHT PROCEDURES. NO DAMAGE EVIDENT. 2L72 4F4 F A7EU E7EA 20041108001832004110800183 2004 11 8 RAIA00410001 420041005A346023076628 FADEC EMB 145 EMB145LR 3260212SO COCKPIT FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03840HK1220012200 145341 EWR - RUDDER HARD OVER PROTECTION FAIL, E2 ATC SOV OPN, E2 IDLE STP FAIL. MAINTENANCE REMOVED AND REPLACED FADEC 2A. 2L72 4T RTT00011AT 20041108001872004110800187 2004 11 8 RAIA00410005 420041012A34217003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU COCKPIT MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03571HK15500 41090 SLT - NR 1 ATTITUDE FAIL AT APPROX 52 KTS DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER. 2L72 4T RTA41NM 20041108001902004110800190EU 2004 11 8 RAIA00410009 120041015A3010 BOOT JETAIRJETSTMJETSTM4101 1500501EU DE ICE SYSTEM LEAKING A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03563HK 41079 AIRFRAME DE-ICE FAULT ON CCT 2 DURING TAXI OUT FAILED. MAINTENANCE FOUND DE-ICE BOOTS LEAKING FROM LEFT O/B HORIZONTAL BOOT, LEFT WING MIDDLE BOOT, AND LEFT OUTBOARD BOOT. INSTALLED PATCHES. 2L72 4T RTA41NM 20041108001942004110800194SO 2004 11 8 LR7A04088 120040808A612054H60117 PROPELLER LKHEED382 382G 526414USO HAMSTD54H 54H60117 NE NR 1 ENGINE OVERSPEED A LR7AE ENGINE SHUTDOWN O OTHER APAPPROACH 1 AL03404LC 4028 4763 235459 NR 1 ENGINE OVERSPEED TO 106 PERCENT IN BOTH MECHANICAL AND NORMAL GOVERNING ON FINAL APPROACH. SHUTDOWN IAW QRH. THREE ENGINE FERRY FLIGHT TO ANC FOR REPAIR. AT ANC REPLACED NR 1 PROP ASSY PER JOB CARD HN6101 AND ENGINE RUN PER HN7101. 2H74 4T A1SO 6 CP906 20041108001962004110800196SO 2004 11 8 LR7A04101 120041001A5312 PANEL LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 477 BULKHEAD PANEL CRACKED NEAR EXISTING REPAIR AT RBL 81, WL 180. REPLACED PANEL IAW 3707784 AND SRM SMP 51-70. 2H74 4T A1SO 20041108002062004110800206NM 2004 11 8 SWAA043149 120041028A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED 1/4D CHECK, FOUND MLG W/W BEADED PRESS WEB CRACKED AT BS 664, LBL 31.5. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041109000062004110900006EA 2004 11 9 QXEA200400732 120041019A5320 SILL CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - AFT BAG DOOR LOWER FORWARD SILL CHAFED, FORWARD OF FORWARD STOP FITTING. REPAIRED IAW CRJ700 SRM 51-25-01. 2L72 4F RTA21EA 20041109000122004110900012EA 2004 11 9 QXEA200400718 120041014A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX - BEAM FS 280 HAS A POSSIBLE CRACK LEFT SIDE BELOW T-BRACKET ATTACH POINT FOR SEAT RAIL BEAM. REPAIRED IAW REO 670-53-11-045. 2L72 4F RTA21EA 20041109000132004110900013EA 2004 11 9 QXEA200400720 120041013A5310 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX - THE COCKPIT BACK WALL AFT SIDE RIGHT HAS NUMEROUS SPOTS OF CORROSION AT FLOOR LEVEL AT BEAM FS 280. REPAIRED IAW HORIZON AIR EA R-53-211 AND REO 670-53-11-051. 2L72 4F RTA21EA 20041109000152004110900015NE 2004 11 9 QXEA200400715 220041017A7320311697503 ECU DHAV DHC8 DHC8102 2809003NM PWA 120 PW123D 52152NE ZONE 500 MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09361PH10968 516 PDX - FLIGHT 2192 DURING CLIMB NR 2 ENGINE MANUAL CAUTION LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL CHECKLIST, NO HELP. TORQUE ROSE 10 PERCENT WHEN LIGHT CAME ON. MAINTENANCE REPLACED NR 2 ENGINE ECU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20041109000192004110900019NM 2004 11 9 QXEA200400710 120041014A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT PAX STUCK A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09415QX2124 4081 CREW REPORTS THE AFT PORT PASSENGER DOOR IS JAMMED. MAINTENANCE INSPECTED THE DOOR AND FREED IT FROM ITS PARTIALLY CLOSED POSITION. THE DOOR WAS OPERATED SEVERAL TIMES WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041109000212004110900021WP 2004 11 9 ABXA040361 120041019A53119919617501N FRAME DOUG DC9 DC931 3022065WP FUSLEAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 LEFT FORWARD MAIN FRAME STA 699 CRACKED AT FORWARD AND AFT FLANGE. REQUIRED REPLACEMENT PER NEA 53400100-002-30. REMOVED AND REPLACED LEFT MAIN FRAME IAW EA 53400321-001-2 AND DC-9 SRM. 2L72 4F A6WE 20041109000222004110900022SO 2004 11 9 C2XA04RI010 120041026A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO LAVATORY DIRTY A C2XAO OTHER N FALSE WARNING CRCRUISE 1 SW2716919 145393 IAD - FLIGHT 3293 CREW REPORTED LAV SMOKE WARNING IN FLIGHT, NO SMOKE VISIBLE. CREW FOLLOWED QRH PROCEDURE. IAD MAINTENANCE CLEANED SMOKE DETECTOR SENSOR AND PERFORMED LAV SMOKE FIM TASK 26-14-00. ALL OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041109000232004110900023NM 2004 11 9 QXEA200400704 120041005A5330 SKIN PANEL DHAV DHC8 DHC8202 2809007NM FUSLEAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - REPAIR FUSELAGE SKIN PANELS LOCATED AT STATION X167 AND X240.5 BETWEEN STRINGERS 31 AND 33 STARBOARD. MAINTENANCE REPAIRED THE SKIN PANELS IAW EA'S 2-53-576A AND 2-53-576B. 2H72 4T RTA13NM 20041109000252004110900025NM 2004 11 9 371PA0050 120040925A5320 ANGLE BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 DRAG ANGLE CRACKED ABOVE LEFT RAM AIR DUCT. REPAIRED PER EA 53-250. 2L72 4F RTA16NE 20041109000272004110900027NM 2004 11 9 371PA0057 120040928A5313 STRINGER BOEING737 737306 13844BGNM FUSLEAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 CORROSION ON STR 25 LT AT BS 360 BEHIND E-2 RACK. REPAIRED PER SRM 53-10-03 AND EA 53-255. 2L72 4F RTA16NE 20041109000282004110900028EA 2004 11 9 QXEA200400712 120041013A274184897131 MOTOR CNDAIRCL600 CL6002C10 1390015EA ZONE 300 FAILED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09607QX1363 896 10024 PDX - FLIGHT 2554 - WHILE AT CRUISE, THE CREW RECEIVED AN AURAL WARNING FOR TRIM IN MOTION. THE AUTO PILOT WAS DISCONNECTED WITH NO CHANGE. THE STAB TRIM WAS DISCONNECTED AND THE WARNING CEASED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NR 1 HSTA MOTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041109000302004110900030WP 2004 11 9 ABXA040354 120041005A531199196181 FRAME DOUG DC9 DC932F 3022067WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 LEFT MAIN FRAME AT STA 718, CRACKED BEYOND LIMITS IN WHEEL WELL AREA AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME IAW DC-9 SRM. 2L72 4F A6WE 20041109000322004110900032NM 2004 11 9 SWAA043227 120041105A2560PH22300L GLOWSTRIP BOEING737 7373Q8 1384670NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29695SW 23506 EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 DEF, LOOSE. SECURED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20041109000342004110900034EA 2004 11 9 SWIA200414053 120041103A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA ROW 5 BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07429SW 7518 CEILING EMERGENCY LIGHT POD AT ROW 5 INOPERATIVE. RELAMPED EMERGENCY LIGHT CEILING POD AT ROW 5. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109000352004110900035SO 2004 11 9 SWIA200414049 120041102A27203081401003 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER PEDAL JAMMED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07583SW1057210572 120351 DURING CLIMBOUT BOTH, CAPTAIN AND FIRST OFFICER'S, RIGHT RUDDER PEDAL WAS JAMMED. REMOVED AND REPLACED BLUE SYSTEM ACTUATOR ON RUDDER IAW MM 27-22-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000372004110900037EA 2004 11 9 SWIA200414051 120041104A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER DEDESCENT 1 NM07953SW 7813 FIRST OFFICER'S SIDE WINDOW CRACKED ON DESCENT TO LAX. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW 56-12-01. P/N OFF NP139322-001, S/N OFF 03080H9346. 2L72 4F RTA21EA 20041109000382004110900038SO 2004 11 9 SWIA200414052 120041103A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW5279 4303 120039 FLAP DISAGREEMENT AT 45 DEGREES OUTBOARD PAIR AT 25 DEGREES AND FLASHING. REPLACED CANNON PLUG ON LEFT OUTBOARD FLAP ACTUATOR IAW WM 20-50-01 AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000392004110900039NM 2004 11 9 SWAA043235 120041106A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 273, STRINGER 16L AND BS 911, STRINGER 23R. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041109000412004110900041NM 2004 11 9 SWAA043218 120041105A53206545815 FLOOR SUPPORT BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FWD GIRT BAR FLOOR SUPPORT ANGLE AT BS 345, LBL 56, CORRODED. REMOVED AND REPLACED GIRT BAR FLOOR ANGLE PER SRM. 2L72 4F RTA16WE 20041109000432004110900043NM 2004 11 9 SWAA043220 120041105A5510 CLEVIS BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTINGS FWD AND AFT SPAR CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER SRM. 2L72 4F RTA16WE 20041109000452004110900045NM 2004 11 9 SWAA043222 120041105A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041109000642004110900064SO 2004 11 9 C2XA04BT111 120041019A335020131A POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714920392 145380 EWR - CREW REPORTED, EMERGENCY LIGHTS AT EXIT ROWS ARE REAL DIM. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY UNDER FLOORBOARD IAW EMB145 MM 333-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041109000662004110900066SO 2004 11 9 C2XA04BT114 120041027A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714907 145468 AFT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN BULB. OPS CHECKED GOOD IAW EMB 145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041109000682004110900068NM 2004 11 9 234TR0025 120041030A5313 STRINGER BOEING737 737228 13844AGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 CORROSION ON STR 26 RT FROM BS 1006 TO BS 1016. REPLACED DAMAGED SECTION PER SRM 51-10-1 AND SRM 51-40-04. 2L72 4F RTA16WE 20041109000702004110900070NM 2004 11 9 371PA0077 120040916A5320 INTERCOSTAL BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 INTERCOSTAL FROM BS 328 TO BS 344 AT LBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2L72 4F RTA16NE 20041109000722004110900072SO 2004 11 9 SWIA200414007 120041015A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07271YV 120271 FLOOR EMERGENCY LIGHT AT FORWARD END INOPERATIVE. REPAIRED BROKEN WIRE ON FORWARD (RED) FLOOR EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109000742004110900074NM 2004 11 9 SWAA043194 120041103A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 272, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041109000762004110900076NM 2004 11 9 SWAA043196 120041103A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT SIGN ABOVE FWD SERVICE DOOR CRACKED. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20041109000782004110900078NM 2004 11 9 SWAA043207 120041103A3242 BRAKE BOEING737 7377H4 1384404NM MLG MALFUNCTIONED A SWAAO OTHER O OTHER TXTAXI/GRND HDL 1 SW29746SW 29798 BRAKES VERY INEFFECTIVE WITH INCREASING PEDAL PRESSURE DOWN TO 70 KNOTS WHERE ANTISKID ACTIVATED. BRAKES CHECK WITHIN LIMITS PER MM. 2L72 4F RTA16WE 20041109000802004110900080EA 2004 11 9 QXEA200400706 120040929A5320 DRIP TRAY CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - DRIP TRAY ON LEFT HAND SIDE CONNECTED TO AFT FLOORBEAM FOR COCKPIT IS CRACKED IN SEVERAL PLACES. REPAIRED IAW HORIZON AIR EA R-53-208. 2L72 4F RTA21EA 20041109001172004110900117NM 2004 11 9 250TR0049 120041022A5313 STRINGER BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION AROUND NUT PLATE IN STR 28 LT AT BS 500 IN FORWARD CARGO BIN. REPAIRED PER SRM 53-10-3. 2L72 4F RTA16WE 20041109001532004110900153SO 2004 11 9 C2XA04IA127 120041003A3260355022002MOD4 CONTROL UNIT EMB 145 EMB145ER 3260211SO MLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW27129461002410024 145052 IAH - FLIGHT 2830, THE CREW REPORTED AN AIR/GROUND FAIL IN FLIGHT AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). OPERATIONALLY CHECKED WITH NO DEFECTS, ALL IAW EMB-145 AMM 32-32-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041109001552004110900155 2004 11 9 C2XA04BT099 420040922A34207013270965 RMU EMB 145 EMB145LR 3260212SO NR 2 BURNED OUT A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2714573 145638 ALB - CREW REPORTED, BURNING SMELL FOLLOWED BY GOING BLANK NR 2 RMU. MAINTENANCE REMOVED AND REPLACED NR 2 RMU IAW AMM 23-81-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041109001562004110900156SO 2004 11 9 SWIA200414002 120041022A5210 DOOR EMB 120 EMB120ER 3260203SO CABIN OBSTRUCTED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07250YV 120250 MAIN CABIN DOOR WOULD NOT OPEN DUE TO F/A SEAT BLOCKING HANDLE. INSPECTED OPERATION OF FLIGHT ATTENDANT SEAT AND EMERGENCY EXIT DOORS IAW 52-21-03. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041109001572004110900157NM 2004 11 9 QXEA200400738 120041103A27207G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM RUDDER FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09364PH13992 524 PDX - FLIGHT 2059 - FLIGHT RETURNED TO FIELD. DURING THE CLIMB THE CREW RECEIVED A FULL RUD PRESSURE CAUTION LIGHT. MAINTENANCE FOUND THE NEW SWITCH 7G773 FAILED. THE BAD SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041109001582004110900158NM 2004 11 9 371PA0079 120040916A5320 INTERCOSTAL BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 INTERCOSTAL AT BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. 2L72 4F RTA16NE 20041109001592004110900159NM 2004 11 9 SWAA043215 120041104A53156545833 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND 2 EACH FLOORBEAM WEBS CRACKED AT BS 243, RBL 14 AND LT BS 188 TO LT BS 196. REMOVED AND REPLACED FLOOR WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20041109001602004110900160 2004 11 9 SWAA043203 420041103A25656949956 CABLE BOEING737 7373Q8 1384670NM R2 DOOR GIRT BARFRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE DOOR GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE GIRT BAR CABLE PER MM. 2L72 4F RTA16WE 20041109001612004110900161NM 2004 11 9 SWAA043233 120041105A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 933, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041109001622004110900162 2004 11 9 SWAA043240 420041106A25656949956 CABLE BOEING737 7373Y0 1384671NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29664WN 23495 DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2L72 4F RTA16WE 20041109001632004110900163NM 2004 11 9 372PA0055 120040909A5315 FLOORBEAM BOEING737 737306 13844BGNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 AFT CABIN FLOORBEAM AT BS 947 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 46 TO RBL 46. REPLACED T-CAP PER SRM 53-00-51 AND SRM 53-60-51. 2L72 4F RTA16NE 20041109001642004110900164NM 2004 11 9 252TR0027 120040929A3350 BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05252TR 23001 LEFT EXTERIOR AND INTERIOR OVERWING EXIT LIGHTS OUT. REPLACED BATTERY PACK ON LT EXTERIOR AND INTERIOR EXIT LIGHTS. CHECKS GOOD PER MM 31-51-51. 2L72 4F RTA16WE 20041109001662004110900166SO 2004 11 9 C2XA04CL111 120041101A1420P8503 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714930 145011 CLE - FLIGHT 2562, THE CREW REPORTED THE AFT HALF OF THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND RESEATED THE CONNECTOR AT THE AFT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20041109001682004110900168SO 2004 11 9 C2XA04SH530 120041025A322014524475003 BEARING CAP EMB 145 EMB145ER 3260211SO NLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE LEFT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02. 2L72 4F RTT00011AT 20041109001702004110900170SO 2004 11 9 C2XA04SH541 120041027A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED BEAM IAW 51-40-02. 2L72 4T RTT00011AT 20041109001712004110900171 2004 11 9 C2XA04CL109 420041026A34227014300901 DISPLAY EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW27165615347 5347 145610 CLE FLIGHT 2109 - THE CREW REPORTED AN ELECTRICAL SMELL/SMOKE DURING TAXI AFTER THE EICAS DISPLAY WENT BLANK THEN CAME BACK ON. MAINTENANCE REPLACED THE EICAS DISPLAY DU-870. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20041109001732004110900173 2004 11 9 SWAA043204 420041103A25656949956 CABLE BOEING737 7373Q8 1384670NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOE EVAC DOOR SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041109001742004110900174NM 2004 11 9 SWAA043216 120041104A53106546817 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 460 TO BS 480, RBL 65, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20041109001752004110900175NM 2004 11 9 SWAA043191 120041103A335007912 COVER BOEING737 7375H4 138449DNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29511SW 24188 EEPLS LIGHT STRIP FROM ROW 1 ABC TO ROW 3 ABC, LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20041109001772004110900177NM 2004 11 9 SWAA043234 120041105A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29754SW 29849 DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041109001782004110900178SO 2004 11 9 SWIA200414003 120041022A27523082001007 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07268UE4371 4371 120207 RECEIVED FLAP CONTROL FAULTS. REPLACED RIGHT NACELLE ACTUATOR WITH SERVICEABLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109001792004110900179SO 2004 11 9 SWIA200414004 120041022A2750 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS CONTAMINATED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07295SW 120322 FLAP CONTROL FAULT ON TAXI OUT. RERACKED FLAP CONTROL UNIT IAW AMM 27-50-06 PAGE 401. CLEANED MOISTURE FROM LEFT AND RIGHT FLAP ACUTATOR CANNON PLUG. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041109001802004110900180SO 2004 11 9 SWIA200414005 120041022A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO OUTBOARD FLAP MALFUNCTIONED A SWIAL ABORTED APPROACH F FLT CONT AFFECTED LDLANDING 1 NM07188SW8913 8913 120039 RETRACTED FLAPS FROM 15 TO UP AND GOT A DISAGREEMENT ON THE OUTBOARD PAIR, PROBLEM CLEARED AFTER APPROX 1 MIN. LANDING IN SLC, SELECTED FLAPS 45 AND GOT A DISAGREEMENT ON THE OUTBOARD PAIR. PROBLEM CLEARED AFTER LANDING. REPLACED RIGHT OUTBOARD FLAP ACTUATOR, OPERATIONAL CHECK GOOD IAW 27-50-09. 2L72 4T RTA31SO 20041109001812004110900181NM 2004 11 9 371PA0080 120040927A5720 ANGLE BOEING737 737306 13844BGNM CLOSEOUT PANEL CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 CORROSION IN ANGLE FOR LEFT WHEEL WELL TO WING CLOSEOUT PANEL. REPLACED ANGLE PER BAC DWG 65-45687. 2L72 4F RTA16NE 20041109001822004110900182NM 2004 11 9 371PA0063 120040921A5320 CHANNEL BOEING737 737306 13844BGNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 LOWER ANTENNA SUPPORT CHANNEL HAS SEVERAL CRACKS. REPLACED ANTENNA CHANNEL PER SRM 51-10-02. 2L72 4F RTA16NE 20041109001842004110900184SO 2004 11 9 C2XA04SH531 120041023A531314529180017 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING C-CHECK STRINGER 19R WAS FOUND GOUGED BETWEEN FRAME 52 AND 53. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW 53-24-02. 2L72 4T RTT00011AT 20041109001862004110900186 2004 11 9 237TR0007 420041011A22301795600160309 CONTROL UNIT BOEING737 737228 13844AGNM AUTOTHROTTLE MALFUNCTIONED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05237TR 23007 AUTO THROTTLE INOP. PLACED AUTO THROTTLE ON MEL 22-4. 10/19/2004: REPLACED NR 2 LVDT. AUTO THROTTLE CHECKS NORMAL PER MM 22-31-81. 2L72 4F RTA16WE 20041109001872004110900187SO 2004 11 9 SWIA200413989 120041020A2797 WIRE EMB 120 EMB120ER 3260203SO AILERONS BROKEN A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07251YV 120251 AILERON DISCONNECT LIGHT DOES NOT LIGHT WHEN AILERON DISCONNECTED. REPAIRED BROKEN WIRES AT CONNECTOR ON AILERON QUADRANT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041110000022004111000002EU 2004 11 10 AWXA200401193 120041017A5315D5347218900 FLOORBEAM AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 9-12. 2L72 4F4 FRTA28NM E311NE 20041110000032004111000003NM 2004 11 10 2004UALA00981 120041026A3210 PIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT MLG TRUNNION WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 RT MLG TRUNNION PIN HAS CHROME WORN OFF END. REPLACED TRUNNION PIN. 2L72 4F4 FRTA16WE E2GL 20041110000042004111000004NM 2004 11 10 2004UALA00991 120041028A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 FRAME IS DENTED AT STATION 1440, STRINGER 25L, UPPER IB FLANGE. TYPICAL CARGO PIT DENT DAMAGE DUE TO CARGO LOADING. INSTALLED NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041110000062004111000006EU 2004 11 10 AWXA200401195 120041017A5347D5311209220500 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT IB SEAT TRACK Y765 FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20041110000082004111000008EU 2004 11 10 AWXA200401197 120041017A5320D53471124200 SHEAR PLATE AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT SHEAR PLATE, OB OF Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT Y1292 FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20041110000092004111000009EU 2004 11 10 AWXA200401198 120041017A5320D53480048201 SILL AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER OB EDGE OF R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION R-2 DOOR LOWER CENTER SCUFF PLATE SHAPE SILL AT Y1546, FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT SECTION OF SHAPE SILL; INSTALLED REPAIR PART IAW SRM 51-42-11. 2L72 4F4 FRTA28NM E311NE 20041110000122004111000012NM 2004 11 10 MASA200400617 120041031A3350 LAMP DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE EMERGENCY LIGHTSINOPERATIVE A MASAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW07449YV 449 THE AIRCRAFT RETURNED TO GATE WITH FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT AND RELAMPED THE SYSTEM. OPS CHECKED GOOD. 2H72 4T4 TRTA13NM E20NE 20041110000152004111000015EU 2004 11 10 MALA040649 120041024A2132 WARNING LIGHT BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE CABIN PRESSURE FALSE INDICATIONA MALAG O2 MASK DEPLOYED N FALSE WARNING CRCRUISE 1 GL15501XJ E2208 FA AROUND 17,000 FT CABIN HIGH ALT LIGHT ILLUMINATED. 02 MASKS DROPPED FROM CEILING BEFORE THEY COULD DROP IN ALTITUDE. THIS WAS A REPOSITION FLIGHT. NO PAX ON BOARD. O2 GENS GOOD RESTOWED MASKS REF AMM 0501. 2H74 4F4 FRTA49EU E6NE 20041110000162004111000016NE 2004 11 10 2004UALA00983 220041024A7230 COMPRESSOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE NR 1 ENGINE STALLED A UALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29671UA 30026 COMPRESSOR STALL REPORTED ON NR 1 ENGINE, ON CLIMB, ENGINE SELF RECOVERED AND CONTINUED NORMAL OPERATION. 2L72 4F4 FRTA1NM E24NE 20041110000182004111000018 2004 11 10 KBM2004F00224 420040920A34225050010902 GYRO SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE DIRECTIONAL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA212 2143 DIRECTIONAL GYRO, INOPERATIVE (RED FLAG), WILL NOT HOLD HEADING. REMOVED AND REPLACED DIRECTIONAL GYRO. 1G71 3U3 U H9EU E19EU 20041110000192004111000019EU 2004 11 10 AWXA200401201 120041017A5315D534721900000 FLOORBEAM AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11. 2L72 4F4 FRTA28NM E311NE 20041110000212004111000021EA 2004 11 10 COMA0460590 120041030A3350362624 LAMP CNDAIRCL600 CL6002B19 1900309EA PWA PT6 PT6A27 52043EA EMERGENCY LIGHT INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO27403CA 7428 FLIGHT 5118, EMERGENCY FLOOR PATH LIGHTS INOPERATIVE, ROWS 2 THRU 5. REPLACED STRIP LAMP. 2L72 4F4 TRTA21EA E4EA 20041110000232004111000023WP 2004 11 10 AALA20041088 120041101A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21554AA 53084 NR 1 FLEX PANEL EMERGENCY PATH LIGHTING AND NR 2 AND NR 3 OVERHEAD EMERGENCY ESCAPE PATH LIGHTING AT STATIONS 925, 812 AND 642 INOPERATIVE. REPLACED BATTERY PACKS FOR NR 1 FLEX PANEL EMERGENCY PATH LIGHTING (BATTERY PACK B5 28) AND NR 2 (BATTERY PACK B5 104) AND NR 3 (BATTERY PACK B5 102) OVERHEAD EMERGENCY ESCAPE PATH LIGHTING AT STATIONS 925, 812 AND 642. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20041110000272004111000027EA 2004 11 10 MASA200400599 120041024A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775992 7401 ABORTED TAKE OFF AND RETURNED TO GATE FOR SPOILER CONFIGURATION WARNING MESSAGE ON TAKE OFF ROLL. MECHANIC SENT AND REPLACED THE NR1 SECU. PART INFORMATION TO FOLLOW. 2L72 4F4 FRTA21EA E15NE 20041110000282004111000028EA 2004 11 10 SWIA200414042 120041030A2611 CONNECTOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE LAVATORY SMOKE LOOSE A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07709SK 10159 LAV SMOKE MESSAGE CAME ON DURING TAKEOFF ROLL. RE-SECURED LOOSE CONNECTOR PLUG. OPERATIONAL CHECK GOOD IAW MM 26-16-00. 2L72 4F4 FRTA21EA E15NE 20041110000322004111000032NM 2004 11 10 AT0400022 120041105A2120 ODOR BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE TRASH CAN DETECTED A ZZDABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO15949AT 55003 A/C DIVERTED DUE TO POSSIBLE BURNING ODOR COMING FROM GALLEY / R-1 DOOR AREA. INSPECTED AIRCRAFT AND FOUND ODOR COMING FROM GALLEY TRASH CAN. RAN AIRCRAFT AND NO ODORS NOTED. ALL SYSTEMS CHECK GOOD. TRASH CAN BAGGED AND PLACED IN FORWARD CARGO COMPARTMENT. 2L72 4F4 FTRA6WE E00061EN 20041110000342004111000034NM 2004 11 10 DHL2004754026 120041003A3240 METERING VALVE BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE MLG BRAKE LEAKING A DHLAO OTHER KE FLUID LOSS VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01754DH 22008 NR 3 AND NR 4 MLG BRAKES DRAGGING. REMOVED AND REPLACED MLG BRAKE METERING VALVE, RT BRAKE SPRING CARTRIDGE, AND RIGGED RT AND LT BRAKE CONTROL LINKAGE IAW MM 32-41-11 AND 32-41-01. LEAK, FUNCTIONAL, AND OPS CHECKS GOOD MM 32-41. 2L73 4F4 F A3WE E2EA 20041110000372004111000037EA 2004 11 10 SWIA200414026 120041028A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07446SW 7666 (FLAPS FAIL) CAUTION MESSAGE ON APPROACH, AFTER SELECTING FLAPS 8. REPLACED LT IB NR 1 AND NR 2 FLAP ACTUATORS WITH SERVICEABLE UNITS IAW MM 27-53-01. P/N: 852D100-19, S/N OFF: 3561, P/N: 852D100-19, S/N OFF: 3612. 2L72 4F4 FRTA21EA E15NE 20041110000412004111000041 2004 11 10 04302639 420041028A3418 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STALL WARNING FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27639BR 7313 EVENT SUMMARY STATED STALL FAIL. REMOVED AND REPLACED RT AND LT MACH TRANSDUCER. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041110000422004111000042EA 2004 11 10 QXEA200400737 120041031A26129847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CARGO FIRE DETECDAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX6494 10041 MAINTENANCE FOUND THE FORWARD CARGO BAY FIRE DETECTION CHIMNEY DAMAGED WHILE PERFORMING THE LINE CHECK. THE CHIMNEY WAS REPLACED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041110000442004111000044EU 2004 11 10 RAIA00410023 120041026A3233AIR864861 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114HR 01514NE MLG UPLOCK MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03566HK 41084 RED GEAR HANDLE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED UP-LOCK ACTUATOR. 2L72 4T4 TRTA41NM E18NE 20041110000472004111000047 2004 11 10 XNOA1208 420041102A3422 GYRO AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE COCKPIT FLUCTUATES A XN0AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23373PC 218 ON CLIMB, ATT LIGHT ON ADI CAME ON. CAPT ADI SHOWED 6 DEGREE NOSE HIGH. CAPT AND F/O HSI SHOW 6 DEGREE DIFFERENCE. LINE-UP AFTER 5 MINUTE LEVEL FLIGHT. REMOVED AND REPLACED NR 1 VERTICAL GYRO AND NR 3 DIRECTIONAL GYRO, BOTH SYSTEMS OPS CK GOOD IAW AMM 34-25-00.(STATUS:ORIG/CLOSED) 2L72 4F4 FRTA35EU E23EA 20041110000512004111000051CE 2004 11 10 ACE103004 120041030A323311238002223 ACTUATOR BEECH 1900 1900C 1154161CE PWA PT6 PT6A60A 52043NE MLG ERRATIC E YADAO OTHER J WARNING INDICATION APAPPROACH 1 AL03114AX UC36 PILOT REPORTED, AFTER 3 GEAR EXTENSION CYCLES AND THE QRH MANUAL EXTENSION PROCEDURE, NOSE GEAR GREEN LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE COULD NOT DUPLICATE (SUSPECT INTERMITTENT SWITCHES) AND REPLACED NOSE GEAR ACTUATOR. 2L72 4T4 TRTA24CE E4EA 20041110000522004111000052NE 2004 11 10 MALA040620 220041010A7200 TRIMMER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15445XJ 340B445 FROM MM1 DELTA SHIFT 59 TO LT QRH COMPLIED WITH NO FIX 80-84 NG AVOIDED 94-98-WAS NOT AVOIDED. AIR RETURN TO MSP. MAINTENANCE FOUND LT ENGINE TO BE TRENDING NORMAL COMPLETED STEPS LISTED ON CONTINUATION CARDS LISTED BELOW, REPLACED RT ENGINE T4.5 TRIMMER ALL CHECKS GOOD. AT THIS TIME IAW TREND DATA HISTORY FOR FDR READINGS. REMOVED AND REPLACED RT T4.5 TRIMMER, PERFORMED ITT FUNCTIONAL CHECK AND PERFORMED GPA RUNS ALL CHECKS NORMAL AT THIS TIME. REF CONT CARD LISTED BELOW FOR FURTHER DETAILS. 2L72 4T4 TRTA52EU E8NE 20041110000532004111000053SW 2004 11 10 MV52004F00001 120040921A2710 PULLEY GULSTM690TP 690A 0141722SW GARRTTTPE331TPE33110T WP HARTZLHCB3T HCB3TN5 GL AILERONS FOD B MV5RA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 GL11690HM 11159 WHILE IN FLIGHT, PILOT EXPERIENCED SEVERE AILERON BINDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER INSPECTION OF THE COMPLETE AILERON SYSTEM, IT IS SUSPECTED THAT FOD HAD COME IN CONTACT BETWEEN THE AFT AILERON PULLEY AND CABLE ASSEMBLY. THE AILERON BALANCE CABLE, AFT PULLEY, FORWARD AND AFT AILERON CABLE ASSEMBLIES WERE REPLACED. THE CABLES WERE RIGGED AND TRAVELS CHECKED IAW MM. THE ENTIRE AC BELLY WAS INSPECTED AND CLEANED FOR ANY FOD. THE AIRCRAFT WAS TEST FLOWN WITH ALL FLIGHT CONTROL OPERATIONS NORMAL. (GL11200414316) 1H72 3T4 T 2A4 E4WE 6 CP15EA 20041110000542004111000054NM 2004 11 10 CALA0400695 120041101A53206552878529 WEB BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND LOWER SIDE OF WEB CORRODED BELOW S17L, JUST FORWARD OF STA 1016. INSTALLED DOUBLER IAW SRM 51-70-130, FIGURE 1. 2L72 4F4 FRTA16WE E2GL 20041110000562004111000056NM 2004 11 10 CALA0400697 120041029A5330 SKIN BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 MAINTENANCE NOTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STRINGER 22L, BETWEEN STA 727D AND 727E. THE SKIN WAS REPAIRED IAW ECRA 5330-03388. 2L72 4F4 FRTA16WE E2GL 20041108001102004110800110SO 2004 11 8 RAIA00409001 120040901A2611 WARNING LIGHT EMB 145 EMB145LR 3260212SO LAV SMOKE ILLUMINATED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03837HK 145255 IAD - LAV SMOKE MESSAGE DURING CLIMB. MAINTENANCE PERFORMED OPS CHECK OF BOTH ENGINE AND APU BLEED AIR SYSTEMS AND COULD NOT DUPLICATE MALFUNCTION. 2L72 4T RTT00011AT 20041108001152004110800115CE 2004 11 8 4021 120040823A3297 WIRE LEAR 35 35A 5170602CE NLG BROKEN E BSYAO OTHER N FALSE WARNING APAPPROACH 1 GL0756EM 144 SELECTED GEAR DOWN ON APPROACH INTO MKC AND HAD NO NOSE GEAR DOWN & LOCK INDICATION, BLEW GEAR DOWN WITH EMERGENCY AIR BOTTLE STILL NO NOSE GEAR DOWN & LOCK LIGHT, LANDED AIRCRAFT NO PROBLEM. MAINTENANCE FOUND BROKEN WIRE AT RESTOR P/C BOARD IN NOSE BAGGAGE COMPARTMENT. REATTACHED WIRE, OPS CHECKS GOOD. 2L72 4F A10CE 20041108001252004110800125NM 2004 11 8 CALA0400689 120041029A5730114N2106 SKIN BOEING757 757224 1384958NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719136 29285 INSPECTION FOUND A 6.5 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 421 T0 471. REPAIRED IAW EA 5731-01010, REV D. 2L72 4F RTA2NM 20041108001302004110800130NM 2004 11 8 CALA0400694 120041101A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 277 - 294.5. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-52, 53-00-52, 53-30-52, AND 51-40-02. 2L72 4F RTA16WE 20041108001362004110800136NE 2004 11 8 DJFA2004005 220040622A7261 FILTER BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE ENGINE OIL LEAKING E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA23427CW RK27 PCEJA0146 DURING FLIGHT THE LEFT OIL PRESSURE ANNUNCIATOR WAS DROPPING. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CAUSE WAS FOUND, OIL FILTER WAS LEAKING THIS WAS CAUSED BY A CHIPPED O-RING ON THE OIL FILTER HOUSING. 2H72 4F4 FRTA16SW E25EA 20041108001622004110800162EA 2004 11 8 COMA0460589 120041027A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA MLG ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01929CA 7035 FLIGHT 5822 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL CHECKS AND INSPECTION OF LANDING GEAR FOUND NO DEFECTS. 2L72 4F RTA21EA 20041108002122004110800212SO 2004 11 8 C2XA04CL112 120041102A335072875561180000 LIGHT EMB 145 EMB145XR 3260214SO CABIN LOOSE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714143 145739 CLE- FLIGHT 2708, CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHT STRIP BY THE CABIN DOOR WAS DETACHED FROM THE FLOOR. MAINTENANCE INSPECTED AND RESECURED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20041108002152004110800215NM 2004 11 8 SWAA043205 120041103A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED C4 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 727C, STRINGER 23R AND BS 727D, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041108002172004110800217NM 2004 11 8 250TR0041 120041022A5313 STRINGER BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION ON STR 26 RT FROM BS 1006 TO BS 1016. REPLACED STRINGER SECTION PER SRM 51-10-1. 2L72 4F RTA16WE 20041108002192004110800219 2004 11 8 SWAA043208 420041104A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR GIRT BARFRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041109000142004110900014EA 2004 11 9 QXEA200400722 120041014A5510 PIN CNDAIRCL600 CL6002C10 1390015EA ZONE 300 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09606QX 10023 PDX - HORIZONTAL STAB HINGE BOLT PIVOT PINS HAVE STEPWEAR DAMAGE TO THE ANTI ROTATION LUGS. REPAIRED IAW HORIZON AIR EA R-53-23. 2L72 4F RTA21EA 20041109000162004110900016WP 2004 11 9 ABXA040351 120041015A2133 OUTFLOW VALVE DOUG DC8 DC863 302198AWP CABIN PRESSURE MALFUNCTIONED A ABXAO OTHER J WARNING INDICATION DEDESCENT 1 GL23825AX 46115 DURING DESCENT, CABIN PRESS WENT TO 2000 FT/MIN. RATE OF CLIMB UP TO 9500 CABIN ALT WITH NO CONTROL EITHER MANUALLY OR AUTOMATICALLY. RECOVERED AT FL 19000. COULD NOT DUPLICATE. CREW VERBAL, HEAVY RAINS LEAVING ILN. SUSPECT ICE BUILD-UP. INSPECTED OUTFLOW VALVE SUGAR SCOOP AND ASSOCIATED LINKAGE. CLEANED AND RESEATED CANNON PLUG CONNECTOR AT VALVE ACTUATOR. NO DISCREPANCY NOTED. TESTED OUTFLOW VALVE, GOOD REF DC-8 AMM 21-31-04-5-0001. 2L74 4F 4A25 20041109000862004110900086EA 2004 11 9 SWIA200414037 120041023A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07457SW 7773 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. CLIPS REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-42-13 AND 51-21-11, RII 53-402. 2L72 4F RTA21EA 20041109000882004110900088NM 2004 11 9 250TR0036 120041022A5330 SKIN BOEING737 7372K5 138448XNM FUSELAGE BULGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 SKIN BULGING AROUND RIVETS AT SERVICE INTERPHONE JACK AT STR 23 LT AND BS 1040 AT THE AFT PRESSURE BULKHEAD DOOR. REPAIRED PER EA 53-287. 2L72 4F RTA16WE 20041109000922004110900092EA 2004 11 9 SWIA200414018 120041014A27508004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA UNIT-SKEW MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07973SW298 298 7949 FLAP FAIL MESSAGE. LANDED FLAPS UP. REPLACED SKEW DETECTION UNIT IAW MM 27-51-15. COMPLIED WITH RIGGING CHECK OF BPSU'S IAW TASK 27-51-220-802. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20041109000942004110900094 2004 11 9 SWIA200414020 420041026A34183995100208 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA STALL PROTECTIONMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM07429SW9141 9141 7518 STALL FAIL CAUTION MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER PER M/M 27-35-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109001202004110900120EA 2004 11 9 SWIA200414036 120041027A2711 SWITCH CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07978SW 7953 AILERON TRIM SWITCH INOPERATIVE. REPLACED AILERON TRIM/RUDDER TRIM PANEL WITH SERVICEABLE UNIT. ALL CHECK GOOD. 2L72 4F RTA21EA 20041109001222004110900122EA 2004 11 9 QXEA200400701 120040930A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - CABIN FLOORBEAM, AFT SIDE OF FS 280 BULKHEAD UPPER FLANGE, LOWER SURFACE IS CORRODED AT LBL 1.0, LBL 3.5 AND LBL 13.5 TO LBL 17. REPAIRED IAW HORIZON AIR EA R-53-209 AND CRJ SRM 51-21-06, PARAGRAPH 3A, B, D, PAGE 2 AND 4. 2L72 4F RTA21EA 20041109001242004110900124EA 2004 11 9 QXEA200400697 120040930A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - CABIN FLOORBEAM LOCATED AT FS 280.00 HAS CRACK AT WL 69.95, EXTENDING FROM LBL 8.9 TO LBL 10.7. REPAIRED IAW HORIZON AIR EA R-53-209. 2L72 4F RTA21EA 20041109001502004110900150EA 2004 11 9 SWIA200413986 120040710A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 CLIP AT LBL 9 INBOARD AT FS 280.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP AT LBL 9 INBOARD FS 280.0 IAW CRJ 200 AMM TASK 51-42-13 AND 51-42-21. 2L72 4F RTA21EA 20041109001522004110900152EA 2004 11 9 SWIA200413988 120040710A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 INTERCOSTAL ANGLE AT FS 484 LBL 27 OUTBOARD CRACKED AT TOP FASTENER. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE IAW BRAS STANDARD REPAIR 601R-53-0029. 2L72 4F RTA21EA 20041109001542004110900154SO 2004 11 9 C2XA04IA125 120040930A27403621001013 CONTROL UNIT EMB 145 EMB145ER 3260211SO HORIZONTAL STAB MALFUNCTIONED A C2XAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW27149457638 7638 145049 IAH- FLIGHT 2225, DURING CRUISE, THE CREW REPORTED A/P FAIL & AUTO TRIM FAIL MESSAGES, WITH PITCH TRIM INDICATIONS BEING ERRATIC, WITH BOTH SYSTEMS STILL FUNCTIONING. THE CREW ALSO REPORTED CONTROLLABILITY ISSUES ABOVE 240KTS WITH ROLLING 20 DEGREES TO EITHER SIDE, WITH CONTROL RETURNING BELOW 240KTS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU) TO BE BAD. MAINTENANCE REMOVED AND REPLACED THAT HSCU, OPERATIONALLY CHECKED IN ACCORDANCE WITH EMB-145 MM 27-40-01 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041109001722004110900172NM 2004 11 9 SWAA043242 120041106A5753 SKIN BOEING737 7375H4 138449DNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29527SW 1787 26569 DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041110000052004111000005EU 2004 11 10 AWXA200401194 120041017A5347D53472190205 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FR 68 AND FR 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FR 68 TO FR 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 9-12. 2L72 4F4 FRTA28NM E311NE 20041110000102004111000010NM 2004 11 10 DL75K041013 120041103A2121731376 FAN BOEING757 757232 1384965NM PWA 2037 PW2037 NE E/E COMPARTMENT FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27650DL 24390 AIRCRAFT DIVERTED WITH SMOKE IN CABIN. FOUND THE EQUIPMENT COOLING SUPPLY FAN BAD. REPLACED FAN. 2L72 4F4 FRTA2NM E17NE 20041110000172004111000017NM 2004 11 10 AWXA200401238 120041025A3350100865 POWER SUPPLY BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28914AW 22208 DURING C-10 CHECK FOUND THE EMERGENCY LIGHT BATTERY CHARGER ABOVE L-2 DOOR ENTRYWAY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY ABOVE L-2 DOOR ENTRYWAY, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA2NM E12EU 20041110000202004111000020SO 2004 11 10 MASA200400537 120040920A26114504113 APU EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL APU BAY SMOKE A MASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07855MJ8731 145614 CLOSED - ASH 2673 PIT. AIRCRAFT RETURNED TO THE GATE. CREW REPORTED SMOKE AND ODOR IN THE CABIN. MAINTENANCE ISOLATED THE PROBLEM TO THE APU. MAINTENANCE CLEARED THE CABIN OF SMOKE AND ODOR AND DEFERRED THE APU. 9/22/04 MAINTENANCE REMOVED AND REPLACED THE APU. 2L72 4T4 FRTT00011ATTE6CH 20041110000262004111000026EU 2004 11 10 AWXA200401215 120041018A5347D57130147203 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 36 AND FR 41. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42-11. 2L72 4F4 FRTA28NM E311NE 20041110000302004111000030SO 2004 11 10 63710292004 120041029A27501159SCC5063 CONTROL UNIT GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE FLAPS DEFECTIVE E N93AO OTHER J WARNING INDICATION CRCRUISE 1 SO13509QS3282 637 UNCOMMANDED STAB, FLAP/STAB SYS FAIL CH B, FLAP STAB MX REQ CAS MESSAGES. 2L72 4F4 FRTA12EA E00057EN 20041110000312004111000031NE 2004 11 10 SPAA0400072 220041023A7230 COMPRESSOR BOEING737 7372T4 1384492NM PWA JT8 JT8D17 52049NE ENGINE STALLED A SPAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28703S 22529 P700543 POST SHOP REPAIR OF ENGINE S/N P700543 , OPERATIONAL TEST FLIGHT UNSATISFACTORY. ENGINE EXHIBITS CONTINUOUS COMPRESSOR STALLS AT TOP OF CLIMB, 37FL. ACCOMPLISHED UNSCHEDULED RETURN TO FIELD. ENGINE TO BE REMOVED FROM AIRPLANE AND PLACED IN SHOP FOR DISCREPANCY CAUSE AND REPAIR. 2L72 4F4 F A16WE E2EA 20041110000382004111000038EU 2004 11 10 04FDEA03006 120041101A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 RT FR 40 TO 54, SEAT TRACK NR 3R HAS 8 AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK RAIL AT MDC RT FR 40 TO 44.5 NR 3 R IAW SRM 51-72-10. 2L72 4F4 FRTA35EU E13NE 20041110000392004111000039EU 2004 11 10 04FDEA03007 120041101A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 FROM NR N00373 MCD FR 18, NR 3 RT SEAT TRACK HAS 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REPAIRED SEAT TRACK AT FR 18, NR 3, RT SIDE IAW SRM 53-12-16 BY CUTTING OUT OLD SECTION AND SPLICING NEW SECTION. 2L72 4F4 FRTA35EU E13NE 20041110000432004111000043EU 2004 11 10 CX7A194J0456 120041031A612078249052 PCU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ENGINE FLUCTUATES A CX7AE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL03317CE 6296 340B352 GEE785412 RT ENGINE TRQ FLUCTUATED 5-10 PERCENT ON CLIMB OUT OF KDAY. F/O REPORTED NOTICEABLE YAW DURING TRQ FLUCTUATIONS. RAN ERRATIC ENGINE CHECKLIST. LOCKED OUT TRQ MOTOR. PROBLEM DISAPPEARED. APPROX. 8000 FT IN DESCENT PROBLEM REOCCURRED, CREW RAN CHECKLIST AGAIN AND SHUT ENGINE DOWN. 2L72 4T4 TRTA52EU E8NE 20041110000452004111000045NM 2004 11 10 C1HA200481003 120041031A5210 SEAL BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE DOOR GATES UNSECURE A C1HAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15681CA 22020 A/C PRESSURIZATION, WOULD NOT HOLD PRESSURIZATION ABOVE 15000 ON ONE PACK WITH CARGO HEAT OUTFLOW CLOSED. FOUND GATE SEALS ON THE L1 AND L2 DOORS NOT SECURED. SECURED SEAL IAW MM 52-11-71 PERFORMED ADJ/TEST IAW MM 21-31-00 OPS CK OKAY. 2L73 4F4 F A3WE E2EA 20041110000552004111000055NE 2004 11 10 CALA0400696 220041101A7200 ENGINE BOEING737 737724 13844BYNM GE CFM56 CFM567B24 NE NR 1 VIBRATION A CALAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 SW2727722 28789 875398 THE NR 1 ENGINE BEGAN TO VIBRATE AND THE EGT ROSE TO GREATER THAN 710 DEGREES WHILE ON FINAL APPROACH. HE VIBRATION AND EGT RISE WERE ACCOMPANIED BY ENGINE POWER LOSS. THE ENGINE WAS NOT SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ENGINEERING CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE VIBRATION AND EGT RISE WAS DUE TO FAILURE OF THE NR 4 BEARING. 2L72 4F4 FRTA16WE E00055EN 20041110000672004111000067EA 2004 11 10 O2G2004F00003 120040208A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE NLG FAILED E O2GAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE03601VH 5043 AFTER TAKEOFF, GEAR WAS RETRACTED. WOW INPUT FAIL LIGHT ILLUMINATED AND THE NOSE GEAR FAILED TO RETRACT. (MAINS RETRACTED NORMALLY). EXTENDED LANDING GEAR AND RETURNED. TROUBLESHOT SYSTEM AND FOUND A DEFECTIVE PROX SWITCH IN NOSE GEAR HARNESS. REPLACED SWITCH, OPS CHECK GOOD AND RETURNED AIRCRAFT TO SERVICE. (NE03200405858) 2L72 4F4 FRTA21EA E15NE 20041110000692004111000069NM 2004 11 10 COOSDR040028 120040817A5510 BEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE HORIZONTAL STAB DAMAGED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 LT HORIZONTAL STABILIZER, T/E UPPER BEAM REPAIR. 2L73 4F4 FRTA3WE E2EA 20041110000712004111000071CE 2004 11 10 ML22004F00001 120040909A2611 CONNECTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A6 52043EA OVERHEAT WARNINGMISINSTALLED B ML2RK NONE W INADEQUATE Q C ININSP/MAINT 1 GL03843E 5052 UE339 COMPLIED WITH FIRST 5000 HR INSPECTION OF BLEED AIR WARNING SWITCH CONNECTIONS. FOUND LT AND RT CONNECTORS SWAPPED. THIS CONDITION WOULD WARN THE CREW OF A POSSIBLE BLEED AIR OVERHEAT CONDITION ON THE WRONG SIDE OF THE AIRCRAFT. THE CREWS ACTION WOULD BE TO SHUT DOWN THE GOOD BLEED AIR SYSTEM AND LEAVE THE COMPROMISED SYSTEM OPERATING. IN THE EVENT OF AN ACTUAL FAILURE THE AIRCRAFT COULD EXPERIENCE LOSS OF PRESSURIZATION OR FIRE WITHOUT CREW WARNING. THERE WERE NO LOG ENTRIES FOR WORK ON THIS SYSTEM IN THE PAST. SUGGEST INSPECTION OF THIS SYSTEM SOONER AND MORE OFTEN THEN 5000 HOURS, OR INSTALLING CONNECTORS THAT CAN NOT BE SWAPPED. 2L72 4T3 TRTA24CE E4EA 20041110000742004111000074WP 2004 11 10 UO22004F00007 220040129A7210307217810 BEARING LEAR 35 35A 5170602CE GARRTTTFE731TFE7312B WP FAN GEARBOX FAILED A UO2RO OTHER O OTHER NRNOT REPORTED 1 GL1935TJ 13594 137 P74120 1 EA PLANETARY BEARING FAILED, CAUSING MASSIVE CHAIN REACTION FAILURE WITHIN FAN GEARBOX. 2L72 4F4 F A10CE E6WE 20041110000752004111000075NM 2004 11 10 COOSDR040029 120040817A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE DAMAGED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN, BS 1070, FLOORBEAM DAMAGED. REPAIRED. 2L73 4F4 FRTA3WE E2EA 20041110000812004111000081NM 2004 11 10 ASMF200410019 120041024A2821699151 STRAINER DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RT ENGINE CLOGGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23881LF 53051 725563 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE STRAINER CLOGGED LIGHT TURNED ON. ENGINE WAS RESTARTED AND ACCELERATED TURNING OFF THE LIGHT IAW MM 79-35-00. AS A PRECAUTIONARY ACTION, AT GDL THE FILTER WAS REPLACED IAW MM 79-20-06, TESTS WERE CORRECT. 2L72 4F4 FRT E9NE 20041110000852004111000085EU 2004 11 10 M7K2004F00008 120040909A6510350A34302000 DRIVE SHAFT UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE TAIL ROTOR LOOSE A M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19803MH1381 3735 23069 SUBSEQUENT TO THE DISCOVERY OF A VERY LOOSE COUPLING ON ANOTHER COMPANY AIRCRAFT, A SPECIAL INSPECTION OF OUR OTHER LIKE MODEL AIRCRAFT WAS INITIATED. THIS AIRCRAFT HAD TWO (2) OF THE SIX (6) SPECIAL ATTACHMENT RIVETS JUST BEGINNING TO LOOSEN WHEN A LITTLE MORE THAN NORMAL INSPECTION FORCE WAS APPLIED TO THE RIVET HEADS SQUARE SUPPORT BASE. 1G72 3U3 U H9EU E00054EN 20041110000862004111000086EU 2004 11 10 M7K2004F00009 120040908A6510350A34302000 DRIVE SHAFT UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE TAIL ROTOR FAILED E M7KAO OTHER O OTHER NRNOT REPORTED 1 WP19802MH1480 3707 23096 DURING ROUTINE MAINTENANCE INSPECTION OF THE TAIL ROTOR DRIVESHAFT, CENTER SECTION, AFT COUPLING RIVETED ATTACHMENT ONE OF THE SPECIAL RIVET SUPPORT BLOCKS WAS FOUND TO BE NOT SQUARE TO SHAFT CENTERLINE. FURTHER DETAILED EXAMINATION SHOWED ENTIRE COUPLING MOVEMENT RADIALLY RELATIVE TO SHAFT EXCEEDS .1250 INCH. SUSPECT DRIVESHAFT FAILURE IMMANENT. 1G72 3U3 U H9EU E00054EN 20041110000872004111000087NM 2004 11 10 04FDEA03023 120041105A7312 FIRE WARNING BOEING727 727100 1384036NM NR 2 ENGINE FALSE ACTIVATIONA FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25193FE 19142 ENGINE FIRE INDICATION NR 2 ENGINE. RAN RED TABS, SHUT DOWN ENGINE, DID NOT FIRE BOTTLES. INDICATION EXTINGUISHED AFTER 10 SEC, BEFORE POWER LEVER WAS MOVED TO IDLE, INDICATION OCCURED DURING CLIMB ABOUT 7,000 FT, 90 PERCENT N1, EPR 1.85. ALSO ENGINE WAS WINDMILLED FOR APPROX, 15 MIN. ALL ENGINE INDICATIONS WERE NORMAL, INCLUDING OIL PRESSURE & QUANTITY WHEN ENGINE WAS SHUT DOWN. REMOVED AND REPLACED FUEL DEICING MANIFOLD ASSY. PER MM 73-14-012-4. ENG. LEAK CHECKS COMPLETED PER ENG. CHANGE WORK CARDS. RII 095438 ENT BY: 453197 RPT BY: 096901. 2L73 4F RTA3WE 20041110000882004111000088NM 2004 11 10 04FDEA03031 120041108A5311 FRAME BOEING727 727100 1384036NM N/A DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FRAME DENTED AT BS 1090, STR 23 LT. REPAIRED PER SRM 51-40-3. 2L73 4F RTA3WE 20041110000892004111000089EU 2004 11 10 04FDEA03008 120041101A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 MCD FR 15 NR 2 LT SEAT TRACK HAS 1 AREA OF CORROSION SCALLOP HOLES AND ON NR 2 RT SEAT TRACK WITH 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REMOVED CORROSION ON NR 2 LT SEAT TRACK AND NR 2 RT SEAT TRACK, FOUND TO BE OUT OF LIMITS ON (2EA) TRACKS. REMOVED AND REPLACED 2 EACH TRACKS IAW A300-600 SUPPLEMENT SRM FREIGHTER 53-12-16 AND 51-40-21. 2L72 4F RTA35EU 20041110000922004111000092NM 2004 11 10 DLM88041006 120041101A2120 CLAMP DOUG MD88 MD88 3023688NM LT A/C PACK DUCTWORN A DALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO27990DL 53342 FLOW CONTROL LIGHT CAME ON AT FL330 CABIN WOULD NOT HOLD PRESSURIZATION. CABIN ALT LIGHT CAME ON AS CABIN WENT ABOVE 10,000 FT. CABIN GOT AS HIGH AS 12,500 FT IN DESCENT. FLOW FROM AIR VENTS VERY LOW. FOUND LT PACK TURBINE OUTLET DUCT DISCONNECTED AT LOWER ATTACH POINT. REF: IPC 21-20-00-06B ITEM 300. REPLACED CLAMP AND SECURED DUCT. ALSO FOUND HOSE ITEM 45 WORN. REPLACED SAME. PRESSURIZED AIRCRAFT, ALL INDICATIONS NORM. 2L72 4F RTA6WE 20041110000932004111000093NM 2004 11 10 DLM88041008 120041101A3397 WIRE DOUG MD88 MD88 3023688NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27935DL 49722 AFT CABIN EMERGENCY AISLE LIGHTS INOP. FOUND BROKEN WIRE AT LIGHT ASSY L2-846 AND REPLACED INOP PWR SUPPLY B5-212. 2L72 4F RTA6WE 20041110000952004111000095NM 2004 11 10 04FDEA03022 120041105A5270 WARNING LIGHT BOEING727 727200 138407ENM AIRSTAIR FALSE ACTIVATIONA FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25204FE 22926 AFT AIRSTAIR LIGHT ILLUMINATED AFTER TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 15NOV04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. MEM R CHECK AFT AIRSTAIR UP POSITION FOR ADJUSTMENT, PER MM 52-70-001-5 NO FAULTS NOTED. CHECKED AFT AIRSTAIR UP LOCK SWITCH FOR ADJUSTMENT, PER MM 52-70-001-5, NO FAULTS NOTED. R&R AFT AIRSTAIRS_UP LOCK SWITCH AS PRECAUTIONARY PER MM 52-70-001-5. 2L73 4F RTA3WE 20041110000972004111000097NM 2004 11 10 04FDEA03001 120041030A5610 SEAL DOUG MD11 MD11 3023602NM COCKPIT WINDOW LEAKING A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25584FE 48436 EXTREMELY LOUD NOISE FROM CAPT'S SLIDING WINDOW COULDN'T HEAR RADIO'S OR F/O AT APPROX 9000 FT. ABORTED FLIGHT AND RETURNED TO SFS. REMOVED AND REPLACED LT SLIDING WINDOW SEAL AIRFRAME SIDE PER IPC 56-12-10-01 ITEM 470. PRESSURIZATION FOR LEAK CHECK PER MM 21-00-00-2, NO LEAK FOUND. A/C OK FOR SERVICE. 2L73 4F RTA22WE 20041110000982004111000098NM 2004 11 10 SWAA043259 120041107A534365C10300 GUSSET BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29310SW 22949 DURING SCHEDULED RON, FOUND NLG ACTUATOR SUPPORT FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG ACTUATOR SUPPORT GUSSET PER SRM. 2L72 4F RTA16WE 20041110000992004111000099NM 2004 11 10 SWAA043267 120041108A53106547980 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS CORRODED AT RT BS 727C TO 727D AND LT BS 847 TO BS 867. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20041110001002004111000100NM 2004 11 10 04FDEA03002 120041030A2782651781823 ACTUATOR BOEING727 727200 138407ENM NR 1 SLAT MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25219FE 21102 NR 1 SLAT LED FAILED TO RETRACT AND INDICATING AMBER ON FLAP RETRACTION TO FLAPS 2 IN FLIGHT. REMOVED AND REPLACED NR 1 SLAT ACTUATOR AS PER M/M 27-81-03-4, OP CKS NORM. 2L73 4F RTA3WE 20041110001012004111000101EU 2004 11 10 04FDEA03003 120041030A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 MDCC ZONE 260 15 INCHES TO RT OF CTR TRACK 2R BETWEEN FR 72 AND 80 HAS 2EA AREA OF CORROSION AT (1) FR 77 (2) 10 INCHES AFT OF FR76. WHILE WORKING AREA OF CORROSION FOUND 6 EACH MORE AREAS OF CORROSION. REPAIRED SEAT TRACK BY REMOVING DAMAGED SECTION AND SPLICING IN A NEW SECTION IAW A300-600 SRM 53-10-16. 2L72 4F RTA35EU 20041110001022004111000102WP 2004 11 10 04FDEA03004 120041030A5347 SEAT TRACK DOUG DC10 DC1030 3023501WP ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 MAIN CARGO DECK SHORT SEAT TRACK FITTING IS CORRODED AT RBL 89 STA 1821 TO 1853. REMOVED CORROSION IAW SRM 53-70-00 VOL 1, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED FLOOR PANELS IAW M/M 53-21-04-2. REMOVED DAMAGED TRACK IAW SRM 51-31-01. NEW SEAT TRACK FAB ON TRAVLER T4/467895 IAW SRM 51-10-01. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01. INSTALLED FLOOR PANELS IAW M/M 53-21-04-2. 2L73 4F A22WE 20041110001032004111000103EU 2004 11 10 04FDEA03005 120041101A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 MAIN CARGO DECK NR 2 DUMMY SEAT TRACK BETWEEN FR 54.0 TO 54.1 HAS 3 INCHES OF CORROSION .050 INCH DEEP. TRACK IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10. 2L72 4F RTA35EU 20041110001052004111000105NM 2004 11 10 SWAA043258 120041108A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500D, LBL 16 TO LBL 21, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041110001072004111000107NM 2004 11 10 DL73S040999 120041028A53306545778556 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27319DL 23091 THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK RUNNING ALONG THE BONDED DOUBLER EDGE JUST BELOW STRINGER 23R BETWEEN FS 927 & 947. AN EXISTING SKIN DOUBLER WAS IN AN ADJACENT FRAME BAY. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS CUT OUT OF THE SKIN, AND BOTH AREAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 094642-14, REV A. 2L72 4F RTA16WE 20041110001082004111000108NM 2004 11 10 DLM88041000 120041029A3000750033503 TUBE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE ANTI ICING BROKEN A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO27983DL 53247 718044 ON CLIMBOUT RECEIVED FIRE DET LOOP LIGHT IN A POSITION ALONG WITH LEFT FIRE HANDLE AND MASTER WARNING LIGHTS DURING QRH PROCEDURE TESTED BOTH LOOPS AND GOT ABNORMAL TEST. FOUND LEFT ENGINE RIGHT SIDE AFT ANTI-ICING TUBE BROKEN. REPLACED ANTI-ICING TUBE. 2L72 4F4 FRTA6WE E9NE 20041110001092004111000109 2004 11 10 DL738041001 420041030A2330231702138 VIDEO DISPLAY BOEING737 737832 13844CFNM CABIN FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27374DA 29622 APPROX 2.5 HRS INTO FLT, FLIGHT ATTENDANT REPORTED STRONG ELEC FUMES AFT OF OVERWING EXITS. AT SAME TIME VIDEO SCREENS RETRACTED/EXTENDED ON THEIR OWN AFT OF ROW 23. VIDEO 3 C/B WAS POPPED. FLT CREW PULLED REMAINING VIDEO C/B`S AND ENTERTAINMENT C/BS. FUMES IMMEDIATELY DISSIPATED. REPLACED VIDEO DISTRIBUTION UNIT AT SEAT 20ABC. 2L72 4F RTA16WE 20041110001102004111000110NM 2004 11 10 DL73S041003 120041030A26117213000000 SMOKE DETECTOR BOEING737 737247 138448DNM LAVATORY FALSE ACTIVATIONA DALAO OTHER N FALSE WARNING CRCRUISE 1 SO27243WA 23517 LAV SMOKE LIGHT CAME ON IN FLIGHT. SILENCED ALARM AND F/A INVESTIGATED. NO SIGN OF SMOKE. TESTED LAV SMOKE DETECTORS PER M/M. CHECKS GOOD. 2L72 4F A16WE 20041110001112004111000111NM 2004 11 10 DLM88041005 120041031A2133 OUTFLOW VALVE DOUG MD88 MD88 3023688NM CABIN PRESSURE STUCK A DALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO27905DE 53410 LOSS OF PRESSURIZATION AT FL 280. EMERGENCY DESCENT TO 10,000 FT. CABIN ALTITUDE GOT UP TO A MAX OF 11,000 FT. OUTFLOW VLV APPEARED FULL CLOSED WITH FLOW LIGHT ON AT CONTROLLER. CABIN CONTINUED TO CLIMB. BOTH PACKS OPERATING NORMAL. REMOVED INSULATION FROM OUTFLOW VALVE AND SECURED PROPERLY. 2L72 4F RTA6WE 20041110001332004111000133EU 2004 11 10 04FDEA02888 120041007A5310 STRUCTURE AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 AFT CARGO COMPARTMENT ON RT SIDE MID, FR 54 DOWN TO FR 58, 10 AREAS OF CORROSION NOTED TOP TO UNDERNEATH CLIP NUTS. REMOVED CORROSION AND CHECKED LIMITS IAW A310 SRM 53-10-15. FOUND TO BE WITHIN LIMITS AND REPROTECTED AREAS IAW A310 SRM 53-10-15 AND 51-75-10. 2L72 4F RTA35EU 20041110001352004111000135NM 2004 11 10 04FDEA02918 120041011A5320AGA7087512 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 MAIN DECK, HAT SECTION CORRODED AT STA 1887 RBL 17 AFTER FLOOR PANEL 293BF REMOVED FOR FABRICATION. MAIN DECK, CORRODED HAT SECTION AT STA 1887 RBL 17 REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED AND REWORKED AS PER DWG AGA7087 PAINT TOUCHED UP AND PART MARKED AS PER SRM 51-21-01 VOL II GMM 7-0-1001. NEW HAT INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041110001372004111000137NM 2004 11 10 04FDEA02837 120040928A5414 SKIN BOEING727 727200 138407ENM NR 1 PYLON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 COMPLY WITH EA 7-5450-80610 PYLON STRUCTURE NR 1 ENG PYLON UPPER SKIN REPAIR. COMPLIED WITH EA 7-5450-80610, REPLACED SKIN SECTION AND INSTALLED EXT SPLICE DOUBLER. 2L73 4F RTA3WE 20041110001392004111000139NM 2004 11 10 04FDEA02799 120040922A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 CORROSION EXT SKIN, BS 470 WL 148 CORROSION WHERE MOD S ANT MOUNTS. *S/D* REPAIRED PER SRM 53-30-1 AND 53-30-3. 2L73 4F RTA3WE 20041110001412004111000141NM 2004 11 10 04FDEA02615 120040903A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.190 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041110001432004111000143NM 2004 11 10 04FDEA02617 120040903A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.400 INCH, MATERIAL REMOVED=0.006 INCH, REMAINING THICKNESS=0.394 INCH AND REPAIRED AS PER EA 1-5750- 80344, TITLE: WINGS - LEFT OUTBOARD FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041110001452004111000145NM 2004 11 10 04FDEA02935 120041015A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RIGHT HAND WING FOUND OUTBOARD FLAP INBOARD STOP FITTING CRACKED, DURING DVI. STOP FITTING REMOVED & REPLACED AS PER SRM51-31-01VOL2 & SRM 51-33-01 VOL2. 2L73 4F RTA22WE 20041115000012004111500001 2004 11 15 AALA20041111 420041108A3424 DISPLAY DOUG DC9 DC982 3022082WP TURN AND BANK INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW217522A 49899 EWR-MIA, LIGHT SMOKE WITH ELECTRIC BURNING SMELL AT CRUISE. EMERGENCY FIRE SMOKE CHECK LIST COMPLETED. SMOKE ABATED UNTIL LANDING. SMOKE REAPPEARED IN COCKPIT AREA. FOUND NUMBER ONE NAVIGATION DISPLAY BURNED. REPLACED NUMBER ONE NAVIGATION DISPLAY MODE SELECT PANEL SYMBOL GENERATOR CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000022004111500002WP 2004 11 15 AALA20041103 120041104A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21258AA 49288 PHX - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000052004111500005NM 2004 11 15 AALA20041109 120041106A3350 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21683A 25340 DFW - EMERGENCY LIGHT AT L569 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT L569. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041115000102004111500010NM 2004 11 15 SWAA043291 120041110A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 846, STRINGER 25R CORRODED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041115000112004111500011NM 2004 11 15 SWAA043273 120041109A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER BETWEEN BS 695 AND BS 706, STRINGER 17L, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20041115000122004111500012 2004 11 15 SWAA043278 420041109A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2L72 4F RTA16WE 20041115000142004111500014NM 2004 11 15 0401965502 120041102A5310 DOOR FRAME BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01502US 23191 DURING L-CHECK FOUND CRACKED HOLE NR 7 AT UPPER CORNER OF NR 1 LT PASSENGER DOOR JAMB. REPAIRED PER EA 55-200848. 2L72 4F RTA2NM 20041115000152004111500015NM 2004 11 15 CALA0400709 120041109A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2779011 29859 THE EXTERIOR EMERGENCY EXIT LIGHTS AT R-4 DOOR FAILED FUNCTIONAL CHECK. THE BATTERY PACK AT M33409 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-06-906-802. 2L72 4F RTT00001SE 20041115000172004111500017NM 2004 11 15 SWAA043290 120041110A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041115000182004111500018WP 2004 11 15 CALA0400702 120041106A53205936442M3 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2783870 48056 INSPECTION FOUND A 1 INCH CRACK IN WEB AT STA 1212 ABOVE LONGERON 24R IN AFT BAGGAGE BIN, RBL 6 TO RBL 14. A PAN SECTION AND SPLICE DOUBLER WERE INSTALLED IAW ECRA 5311-01211. 2L72 4F A6WE 20041115000192004111500019WP 2004 11 15 AALA20041079 120041024A3350P4010049 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219404V 53140 DFW - EMERGENCY LIGHTS FROM ROW 3 TO 19 FLICKER. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT ROWS 3 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041115000202004111500020NM 2004 11 15 AALA20041080 120041029A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21772AN 29580 DFW - DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTS BATTERY PACKS IN BUSINESS CLASS FAILED TIME TEST. REPLACED BATTERY PACKS AT L2 FOR BUSINESS CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041115000212004111500021EU 2004 11 15 AALA20041081 120041029A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170079 619 JFK - AFT RIGHT HAD SIDE SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT RIGHT HAND SIDE SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041115000262004111500026NM 2004 11 15 CALA0400707 120041109A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM ROW 1 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2779011 29859 THE FORWARD INTERIOR EMERGENCY EXIT LIGHTS AT ROW 1 FAILED FUNCTIONAL CHECK. THE BATTERY PACK AT M33093 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-06-960-802. 2L72 4F RTT00001SE 20041115000272004111500027WP 2004 11 15 0401959875 120041026A3310 RHEOSTAT DOUG DC9 DC951 3022051WP COCKPIT FAILED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01784NC 48109 DURING CRUISE, THE CAPTAIN'S BRIEFCASE LIGHT BEGAN TO SMOKE AND EMIT ACRID FUMES INTO THE COCKPIT. CREW PULLED THE CIRCUIT BREAKER TO THE MAP AND BRIEFCASE LIGHT CIRCUIT AND THE SMOKE STOPPED. FLIGHT CONTINUED TO A NORMAL SAFE LANDING AT ROC. MAINTENANCE AT STL ON 27OCT REPLACED THE RHEOSTAT CONTROLLER TO THE LIGHT AND CLEARED THE MEL THAT ROC ASSIGNED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041115000282004111500028WP 2004 11 15 AALA20041102 120041104A3350P4010049 LIGHT DOUG DC9 DC982 3022082WP ROW 15DEF BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21495AA 49733 ATL - EMERGENCY LIGHTS AT ROW 15DEF BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000292004111500029NM 2004 11 15 CALA0400700 120041103A53209078224 STRAP BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND A .75 INCH CRACK IN H-STRAP LEFT L1 UPPER HINGE CUTOUT AT STA 312. THE H-STRAP WAS REMOVED AND A NEW H-STRAP WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20041115000302004111500030NM 2004 11 15 CALA0400701 120041104A531365C35777 STRINGER BOEING737 7373T0 1384582NM STA CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND STRINGER 23L CORRODED APPROXIMATELY 2 INCHES AFT OF STA 887 FRAME. A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20041115000312004111500031NM 2004 11 15 AALA20041089 120041102A3397 WIRE HARNESS BOEING737 737823 13844BZNM EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21971AN 29547 SFO - EMERGENCY LIGHTS AT SEAT 16D INOPERATIVE. RECONNECTED HARNESS AT SEAT BOX UNIT FOR EMERGENCY LIGHTS AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATIONS. 2L72 4F RTA16WE 20041115000322004111500032WP 2004 11 15 AALA20041091 120041102A1420 CONNECTOR DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21288AA 49300 LAX - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. SECURED LOOSE CONNECTOR UNDER SEAT 5E FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000342004111500034WP 2004 11 15 AALA20041090 120041102A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21480AA 49655 DFW - OVERHEAD EMERGENCY LIGHT AT FORWARD GALLEY SERVICE DOOR DIM. REPLACED LIGHT ASSEMBLY FOR OVERHEAD EMERGENCY LIGHT AT FORWARD GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000372004111500037WP 2004 11 15 0401899607 120041001A5753 SKIN DOUG DOUG DC9 DC932 3022066WP TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW15759 00172 47232 DURING M-CHECK FOUND CRACK IN NR 3 INBOARD FLAP SKIN AT XLFS=255. REPAIRED PER EA 99-200363. 2L72 4F A6WE 20041115000412004111500041NM 2004 11 15 SWAA043295 120041110A53116547960 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS, 847, RBL 21, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20041115000432004111500043 2004 11 15 SWAA043279 420041109A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2L72 4F RTA16WE 20041115000442004111500044NM 2004 11 15 0401546313 120040914A3350 LIGHT BOEING747 747451 1384940NM CABIN DISCONNECTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01673US 30268 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21R - 31R AND FROM 51L-66L. RECONNECTED LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20041115000452004111500045NM 2004 11 15 DL75K041014 120041104A2530 COFFEEMAKER BOEING757 757232 1384965NM AFT GALLEY DIRTY A DALAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO276716C 30838 FAINT SMELL, POSSIBLE BURNING ELECTRICAL TYPE ODOR NOTICED BY AFT GALLEY AREA. NOTICED BY F/A ON DESCENT. UTILITY BUSSES WERE TURNED OFF. NO SMELL NOTICED. FOUND COFFEEMAKER DIRTY WITH COFFEE GROUNDS. 2L72 4F RTA2NM 20041115000472004111500047NM 2004 11 15 CALA0400710 120041109A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM SEATS 32-45 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2779011 29859 THE EMERGENCY LIGHTS AT SEATS 32-45 AND R-3 DOOR FAILED FUNCTIONAL TEST. THE BATTERY PACK AT M33401 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-06-960-802. 2L72 4F RTT00001SE 20041115000482004111500048NM 2004 11 15 CALA0400711 120041109A3350D71702030 BATTERY PACK BOEING777 777224 1385225NM SEATS 16-28 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2779011 29859 THE EMERGENCY LIGHTS AT ROWS 16-28 FAILED FUNCTIONAL TEST. THE BATTERY PACK AND POWER SUPPLY WERE REMOVED AND REPLACED IAW MM 33-51-06-960-803 AND 33-51-06-960-802. 2L72 4F RTT00001SE 20041115000492004111500049NM 2004 11 15 CALA0400712 120041109A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM L-4 DOOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2779011 29859 THE EXTERIOR EMERGENCY LIGHTS AT L-4 DOOR FAILED FUNCTIONAL TEST. THE BATTERY PACK AT M33407 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-06-960-802. 2L72 4F RTT00001SE 20041115000512004111500051NM 2004 11 15 DL76S041009 120041102A2782 ROD BOEING767 767332 1382001NM SLAT ACTUATOR BENT A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27121DE 23435 RIGHT WING INBD L/E SLAT OUTBD ACTUATOR ROD BENT DAMAGING L/E PANEL AND CAUSING A SLAT ASSYM. REPLACED ROD WITH NEW. ADJUSTMENT MADE ON OPN 7007. DRIVE ROD INSTALLATION OK /INSP. 2L72 4F RTA1NM 20041115000532004111500053WP 2004 11 15 0401829911 120040901A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01961N 47405 DURING L-CHECK FOUND CRACK IN SKIN IN UPPER FORWARD CORNER OF FORWARD SERVICE DOOR JAMB. REPAIRED PER EA 99-199627. 2L72 4F A6WE 20041115000542004111500054NM 2004 11 15 0401835516 120040903A5320 FLOOR SUPPORT BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01516US 23204 DURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 345 BL 0. REPAIRED PER EA 55-200413. 2L72 4F RTA2NM 20041115000572004111500057NM 2004 11 15 0401886309 120041011A3397 WIRE BOEING747 747451 1384940NM EMERGENCY LIGHT DISCONNECTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND C-ZONE LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED WIRES. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20041115000582004111500058NM 2004 11 15 AALA20041096 120041103A2910 LINE BOEING757 757223 1384957NM UPLOCK ACTUATOR FAILED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21637AM 24595 DFW - TWENTY MINUTES AFTER TAKEOFF LEFT HYDRAULIC SYSTEM LOST ALL FLUID. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UNLOCK ACTUATOR PRESSURE LINE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041115000592004111500059WP 2004 11 15 0401799883 120040903A5320 STRAP DOUG DC9 DC951 3022051WP DOOR FRAME CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01671MC 47660 DURING LINE CHECK FOUND CRACK IN AFT PRESSURE DOOR FRAME STEEL SPLICE STRAP J060110-93. REPAIRED PER EA 98-200540. 2L72 4F RTA6WE 20041115000602004111500060 2004 11 15 SWAA043260 420041108A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED A2 CHECK, FOUND 2 EACH GIRT BAR CABLES MISROUTED AT R2 AND L2 DOOR EVAC SLIDES. REROUTED CABLES PER MM. 2L72 4F RTA16WE 20041115000632004111500063NM 2004 11 15 0401526631 120040907A3350 POWER SUPPLY BOEING747 747251B 1384892NM EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01631US 23111 DURING LINE CHECK, FOUND ZONE-C FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20041115000642004111500064 2004 11 15 0401456624 420040828A2330 ELECTRICAL BOX BOEING747 747251B 1384892NM SEAT 36FG ODOR A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01624US 21706 BURNING SMELL NOTICED IN AREA BY DOOR 3. SMELL WAS MOST PRONOUNCED IN ROWS 35-39D-G. SEB'S AT THE BOTTOM OF SEATS -E- AND -F- FELT HOT TO TOUCH. TURNED OFF ENTERTAINMENT SYSTEM POWER. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. REPLACED SEAT 36FG SEB, NO HELP. DEFERRED PER MEL 23-30C-NRT, REPLACED SEAT 36FG SEB. NOW ALL FUNCTIONS CHECKED OK. 2L74 4F A20WE 20041115000712004111500071 2004 11 15 SWAA043285 420041110A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29412WN 29818 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041115000722004111500072 2004 11 15 SWAA043275 420041109A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED C2 CHECK, FOUND R1 & R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041115000732004111500073 2004 11 15 SWAA043280 420041109A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29095SW 23054 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041115000742004111500074WP 2004 11 15 0401919621 120041019A273039181655501 RELIEF VALVE DOUG DC9 DC932 3022066WP ELEVATOR MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL01621NW 47544 CREW REPORTED ELEVATOR BINDING AT THE HALFWAY POINT OF DEFLECTION. THIS OCCURRED DURING TAKEOFF ROTATION, CLIMB, AND LANDING. MAINTENANCE ADJUSTED A FAIRING FOR THE UPPER CONTROL TAB ARM TO RELIEVE PRESSURE ON UPPER ELEVATOR SKIN FOR CLEARANCE OF LEADING EDGE OF CONTROL TAB. FUNCTION CHECK WAS GOOD BUT PROBLEM RE-OCCURRED DURING PREFLIGHT FOR DEPARTURE. MAINTENANCE REPLACED THE POWER RETURN RELIEF VALVE AND THE ELEVATOR LOAD FEEL AND CENTERING MECHANISM. 2L72 4F A6WE 20041115000752004111500075NM 2004 11 15 SWAA043246 120041104A291065C268761 MODULE BOEING737 7373Y0 1384671NM MLG WW LEAKING A SWAAA UNSCHED LANDING K FLUID LOSS NRNOT REPORTED 1 SW29699SW 23826 AIR TURNBACK, DECLARED EMERGENCY. HYDRAULIC B-SYSTEM FAILURE. REMOVED AND REPLACED B-SYSTEM HYDRAULIC MODULE PER MM. 2L72 4F RTA16WE 20041115000762004111500076NM 2004 11 15 SWAA043247 120041108A3350100031 SIGN BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 FWD GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY SIGN PER MM. 2L72 4F RTA16WE 20041115000772004111500077NM 2004 11 15 SWAA043248 120041108A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29468WN 33858 EEPLS AT FWD GALLEY COVER MISSING. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041115000792004111500079 2004 11 15 SWAA043250 420041108A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041115000812004111500081EU 2004 11 15 AWXA200401256 120041025A5347D53371110010000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 42 AND FS 43. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115000852004111500085NM 2004 11 15 2004UALA01012 120041102A7160 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENG INLET PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 NR 1 ENG INLET COWL OUTER SURFACE PUNCTURED-DELAMINATED AT THE 2 O`CLOCK POSITION APPROXIMATELY 30 INCHES FROM FWD END. DAMAGE WAS FOUND ON INLET COWL WAS PERMANENTLY REPAIRED. 2L72 4F4 FRTA16WE E2GL 20041115000872004111500087NM 2004 11 15 04FDEA03065 120041109A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO, SEAT TRACK FOUND WORN AT LT STA 752 - 760, X= 25. REMOVED FROM L/H STA Y= 745 - Y= 815, X= 25 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND INSTALLED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041115000882004111500088NM 2004 11 15 04FDEA03066 120041109A5313 LONGERON DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO, LONGERON FOUND DENT AT RT STA 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND. 2L73 4F RTA22WE 20041115000892004111500089NM 2004 11 15 04FDEA03067 120041110A5311 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA 1681, LONGERON 12. FOUND WITH DENT/CHAFFED. REMOVED PER SRM 51-33-01 VOLUME II. REPAIR DOUBLER FABRICATED PER SRM. REPAIR DOUBLER INSTALLED PER SRM 51-33-01 VOLUME II. REFER TO EA 1-5310-79792, FUSELAGE MAINFRAME TRACKING OF CATEGORY B REPAIRS ON FRAME. NEXT INSPECTION IS SET TO 16,292 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES THEREAFTER. 2L73 4F RTA22WE 20041115000912004111500091NM 2004 11 15 04FDEA03071 120041110A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION AT FLOORBEAM UPPER AND LOWER SURFACE BS 344 LBL 10 - RBL 10. REPAIRED FLOORBEAM BS 344 LBL 10 - RBL10 PER SRM 53-10-1 AND FEDEX SR 27-53-007. 2L73 4F A3WE 20041115000922004111500092NM 2004 11 15 04FDEA03072 120041110A5310 BEAM BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25233FE 21327 CORROSION ON LONGITUDINAL BEAM BS 750 - 840, RBL 25, WL 208. REPAIRED PER SRM 53-10-1, 51-20-4, 51-30-2, 51-70-1. 2L73 4F A3WE 20041115000932004111500093NM 2004 11 15 04FDEA03073 120041111A55116520656 SPAR BOEING727 72722 1384002NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION ON LT HORIZONTAL STAB INTERNAL UPPER FRONT SPAR CHORD STAB STA 64. REPAIRED IAW SRM 51-10-6, 51-30-2, 51-10-2, 55-10-5. 2L73 4F A3WE 20041115000942004111500094EU 2004 11 15 AWXA200401190 120041102A2932C60AA0062 PRESSURE SWITCH AIRBUS320 A320231 3930325EU NR 1 ENGINE FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28632AW48325 81 ONT - ABORTED TAKEOFF - FLT 0083 - ON TAKEOFF ROLL AT ONT EN ROUTE FOR PHX RECEIVED ECAM MESSAGE HYDRAULIC GREEN ENGINE 1 PUMP LOW PRESSURE, REJECTED TAKEOFF AT 70 KTS AND RETURNED TO GATE. VERIFIED GREEN HYDRAULIC SYSTEM QUANTITY AND PRESSURE, ISSUED MEL 29-30-04, COND. 6, NR 1 ECAM ENGINE PUMP LOW PR INDICATIONS INOP. WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE SWITCH IAW AMM 29-11-17, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041115000952004111500095NM 2004 11 15 AWXA200401191 120041002A5330654576555 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - MAJOR REPAIR - DURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 518, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 518, STR 12 LT; FABRICATED A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-04301-ES1. 2L72 4F RTA16WE 20041115000962004111500096NM 2004 11 15 AWXA200401192 120041023A33973404302 WIRE HARNESS BOEING737 73733A 1384673NM EMERGENCY LIGHT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 MCN - EEL - DURING C-18 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED IN SEVERAL LOCATIONS THROUGH OUT CABIN BETWEEN BS 340 AND BS 947. MAINTENANCE REPAIRED DAMAGE ON EMERGENCY ESCAPE PATH LIGHT HARNESS; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041115000992004111500099 2004 11 15 2004UALA00994 420041028A2565 VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29UA VALVE ASSEMBLY PASSED LOW VOLUME LEAK CHECK AT 3000 PSI FOR 24 HOURS. DURING FILL PROCESS AT 1500 PSI THE VALVE SEPARATED FROM CYLINDER AT BOTTLE ADAPTER. THE CRACKED FITTING WAS MADE OF ALUM 7075-T6 OR 2024-T4. NEW FITTINGS MADE OF SUPERIOR MATERIAL 7075-T73 ARE NOW AVAILABLE AND ARE BEING SPECIFIED TO BE USED AS REPLACEMENT TO FITTINGS FOUND TO BE DEFECTIVE DURING SHOP CHECKS. THIS FITTING REPLACEMENT IS THE SUBJECT OF AIR CRUISERS SIL 25-181 REV-1. 2L72 4F4 FRTA28NM E40NE 20041115001002004111500100 2004 11 15 2004UALA00995 420041029A2565 BRACKET AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SLIDE ASSY BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29UA SLIDE ASSEMBLY STEP BRACKET BROKEN. STEP BRACKETS OF SLIDE/RAFTS (LT & RT) ARE THE TWO BOTTOM ATTACHMENT POINTS THAT HOLD THE SLIDE/RAFT ONTO THE AIRCRAFT DOOR. THESE PARTS ARE STICKING OUT OF THE WHOLE ASSEMBLY AND ARE LIABLE TO DAMAGE ESPECIALLY DURING TRANSPORTATION AND HANDLING. WHEN THE ASSEMBLY IS DROPPED ACCIDENTALLY THE BRACKETS ARE THE IMPACT POINTS. REPLACE BRACKETS AS REQUIRED. 2L72 4F4 FRTA28NM E40NE 20041109000042004110900004EA 2004 11 9 QXEA200400730 120041018A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09607QX 10024 PDX - FLOORBEAM 280 CRACKED. REPAIRED IAW CRJ 51-42-06 AND REO 670-53-11-045. 2L72 4F RTA21EA 20041109000092004110900009EA 2004 11 9 QXEA200400708 120040929A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09603QX 10011 PDX - DRIP TRAY ON RIGHT HAND SIDE CONNECTED TO COCKPIT AFT FLOORBEAM IS CRACKED IN SEVERAL PLACES. REPAIRED IAW HORIZON AIR EA R-53-208. 2L72 4F RTA21EA 20041109000522004110900052SO 2004 11 9 SWIA200414010 120041026A21501945463 HEAT EXCHANGER EMB 120 EMB120ER 3260203SO RT A/C PACK SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07299SW 120329 RIGHT PACK PUTS SMOKE IN THE CABIN WHEN IT IS RUN ON THE APU BLEED. REMOVED AND REPLACED RIGHT HEAT EXCHANGER IAW EMB 120 MM 21-50-03. OPERATIONAL CHECK GOOD. P/N 194546-3, S/N OFF 10-576. 2L72 4T RTA31SO 20041109000542004110900054EA 2004 11 9 SWIA200414012 120041023A2612 FIRE WARNING CNDAIRCL600 CL6002B19 1900309EA APU FALSE ACTIVATIONA SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07413SW 7102 ON FINAL WHEN SWITCHING BLEEDS TO APU, APU FIRE WARNING FOLLOWED BY APU SHUTDOWN & APU FAULT CAUTION MESSAGE. ALSO NOTE DOOR INHIB - APU FIRE WARNING LASTED ONLY 2-3 SECONDS. COMPLIED WITH REINSPECT OF APU COMPARTMENT WITH NO DEFECTS NOTED. CLEARED FAULTS FROM APU ECU. REPLACED DOOR UP AND DOOR DOWN RELAY IAW AMM 24-01-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109000692004110900069SO 2004 11 9 C2XA04BT112 120041026A2612902081 MODULE EMB 145 EMB145LR 3260212SO FIRE CONTROL FAULTY A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW27139979871 7469 145298 EWR - CREW REPORTED, APU FIRE (WARNING) INFLIGHT. MAINTENANCE INSPECTED APU COMPARTMENT AND APU FOR EVIDENCE OF FIRE. NO SIGNS OF FIRE WERE FOUND, PERFORMED OPS CHECK OF SYSTEM. OPS CHECKED GOOD. REMOVED AND REPLACED FIRE CONTROL MODULE IAW EMB 145 26-12-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041109000772004110900077SO 2004 11 9 C2XA04IA137 120041102A2120 ODOR EMB 135 EMB135LR 3260305SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW2714516 145323 IAH - FLIGHT 2389 THE CREW REPORTED THAT THE APU LET OUT A STRONG FUEL SMELL WHEN STARTED IN DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE VERIFIED PROPER OPERATION OF THE APU IN ACCORDANCE WITH EMB 135 AMM 49-00-00. NO FUEL SMELL NOTED AT THAT TIME AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041109000812004110900081NM 2004 11 9 QXEA200400707 120041011A6120 AUTOFEATHER SYS DHAV DHC8 DHC8202 2809007NM MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09351PH 490 BLI - FLIGHT 2157 AUTOFEATHER SYSTEM FAILED TO ARM DURING TAKEOFF ROLL. TAKEOFF ABORTED BELOW 60 KTS. MAINTENANCE COMPLIED WITH AUTOFEATHER SYSTEM AND POWER UPTRIM CHECK IAW DHC-8 AMM 71-00-00-868-027, PAGE 560-562. TEST CHECK GOOD. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041109000832004110900083 2004 11 9 SWAA043197 420041103A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29316SW 23338 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041109000962004110900096WP 2004 11 9 ABXA040348 120041005A2710 BRACKET DOUG DC8 DC861 3021952WP RT FAIRLEAD BENT A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23847AX 46031 DECLARED EMERGENCY, DURING RT TURNS IN FLT AILERONS HARD TO MOVE IN POWERED MODE. WHEN AILERONS DEPOWERED, OPS NORM. FOUND RT FAIRLEAD BRACKET BENT & INTERFERRING WITH CABLE DUE TO BROKEN BUS AILERON CABLE RUNS. REPLACED BRACKET STA RW XRS 380. REPLACED DAMAGED PULLEY ON LT AILERON BUS CRANK & BROKEN AILERON BUS CABLE PULLEY RT I/B AILERON HINGE. FABBED & INSTALLED NEW LINE ON LT WING AILERON TAB LOCKOUT CYLINDER EXTEND LINE BTW TUBE CLAMP & SLEEVE/B-NUT AT CYLINDER. REPLACED LT AILERON TAB LOCKOUT CYLINDER, CABLE 365495-536 RUN AB-A, CABLE 3763151-501 RUN AB-B, LT WING AILERON BUS CABLE P/N 3654950-536 RUN AB-D. ADJ/TEST & THROW CHECKED GOOD. ADJUSTED LT O/B AILERON DAMPER & THROW CHECKED. OPS GOOD. 2L74 4F 4A25 20041109000972004110900097SO 2004 11 9 SWIA200414022 120041027A2611 BATTERY EMB 120 EMB120ER 3260203SO SMOKE DETECTOR INOPERATIVE A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07218SW 120287 SMOKE DETECTOR SOUNDED INFLIGHT, F/A REPORTED NO INDICATION OF SMOKE IN LAV. INSPECTED DETECTOR AND INSTALLED SERVICEABLE BATTERY. FOUND NO EVIDENCE OF SMOKE/FIRE IN LAV OR SURROUNDING AREA. 2L72 4T RTA31SO 20041109000982004110900098EA 2004 11 9 SWIA200414023 120041024A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7701 EMERGENCY LIGHT, OVERHEAD IN AISLE AT ROW 10 BURNED OUT. RELAMPED EMERGENCY LIGHT AT ROW 10 AS NEEDED, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109000992004110900099NM 2004 11 9 250TR0042 120041022A5313 STRINGER BOEING737 7372K5 138448XNM FUSLEAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION OF STR 25 LT FROM BS 986 TO BS 1006. REPAIRED PER SRM 53-10-2. 2L72 4F RTA16WE 20041109001002004110900100NM 2004 11 9 250TR0043 120041022A5311 FRAME BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 CORROSION UNDER NUT PLATE ON FRAME AT BS 1006 AT RBL 5. REPLACED FRAME SECTION PER SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20041109001012004110900101NM 2004 11 9 250TR0050 120041022A5320 ATTACH ANGLE BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 ATTACH ANGLE CRACKED UNDER THRESHOLD AT BS 460 AND STR 26 RT IN FORWARD CARGO BIN. REPLACED ANGLE PER BOEING DWG 69-16784 AND SRM 51-30-02. 2L72 4F RTA16WE 20041109001042004110900104SO 2004 11 9 SWIA200414032 120041029A2750 SKIN EMB 120 EMB120ER 3260203SO NACELLE FLAP CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07221SW 120290 RIGHT NACELLE FLAP IS CRACKED ON BOTTOM SKIN. REPLACED RIGHT NACELLE FLAP, OPERATIONAL CHECK GOOD. WORK PERFORMED IAW MM 27-50-02. 2L72 4T RTA31SO 20041109001142004110900114EA 2004 11 9 SWIA200414024 120041026A27604916420 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07962SW 7859 SPOILERON FAULT MESSAGE CAME ON IN FLIGHT. REMOVED AND REPLACED SECU NR 2 IAW MM 27-61-15. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109001282004110900128EA 2004 11 9 SWIA200414041 120041023A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07457SW 7773 CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 40. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20041109001302004110900130SO 2004 11 9 C2XA04TY170 120041026A531114523524001 FRAME EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714977 145175 DURING C-CHECK FOUND FRAME 64 DENTED AT STRINGER 16L. RECONTOURED DENT PERFORMED NDI AND INSTALLED A DOUBLER REPAIR IAW EC5330-01229. 2L72 4T RTT00011AT 20041109001322004110900132 2004 11 9 SWAA043239 420041106A25656949956 CABLE BOEING737 7373H4 1384600NM DOOR SLIDES MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29636WN 27709 DURING SCHEDULED PM CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES GIRT BAR CABLES MISROUTED. REROUTED R2 AND L2 DOOR CABLES PER MM. 2L72 4F RTA16WE 20041109001342004110900134EA 2004 11 9 SWIA200414039 120041023A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07457SW 7773 FUSELAGE PULLEY INTERCOSTAL OUTBOARD FLANGE CRACKED; FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED IAW CRJ REO 601R53-41-059 REV "A". 2L72 4F RTA21EA 20041109001362004110900136NM 2004 11 9 370WL0001 120041009A3350 LAMP BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05370WL 24011 SEAT ROW 8 ABC EMERGENCY AISLE LIGHT INOP. RELAMPED 8 ABC EMERGENCY AISLE LIGHT. OPS NORMAL. 2L72 4F RTA16WE 20041109001382004110900138NM 2004 11 9 SWAA043198 120041103A53146562125 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29334SW 23938 DURING SCHEDULED C2 CHECK, FOUND LT FWD KEEL BEAM AT BS 520, OUTBOARD LEG, CORRODED. REPAIRED KEEL BEAM PER SRM. 2L72 4F RTA16WE 20041109001402004110900140NM 2004 11 9 SWAA043200 120041104A335010107451 SIGN BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 FWD EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20041109001482004110900148EA 2004 11 9 SWIA200414048 120041030A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07702SK1576 1576 10136 SPLR/STAB FAULT, PITCH FEEL AND RUDDER LIMIT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SFECU PER CRJ 700 MM 27-50-00/27-51-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109001652004110900165EA 2004 11 9 QXEA200400724 220041019A7200312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 500 MALADJUSTMENT A QXEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09409QX6214 64 4051 PCEFA0101 ONT - FLIGHT 2359 JUST BEFORE STARTING DESCENT FROM 23,000 FT NOTICED SMOKE IN COCKPIT AND CABIN. DIVERTED TO ONT. DURING DESCENT AROUND 14,000 FT, HEARD AN UNEXPLAINED BANG WITH VERY SLIGHT YAW, NO CAUTION OR WARNING LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE NR 2 ENGINE. 2H72 4T4 TRTA13NM E00062EN 20041109001672004110900167SO 2004 11 9 C2XA04SH529 120041025A322014524475003 BEARING CAP EMB 145 EMB145ER 3260211SO NLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK RIGHT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02. 2L72 4F RTT00011AT 20041109001692004110900169WP 2004 11 9 ABXA040352 120041019A3350 LAMP DOUG DC8 DC863F 302198FWP EMERGENCY LIGHT INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23812AX 46126 EMERGENCY EXIT LIGHTS ARMED AMBER LIGHT INOPERTATIVE. RELAMPED, OPS CHECKED GOOD IAW DC-8 MM 33-50-02. 2L74 4F 4A25 20041109001762004110900176NM 2004 11 9 QXEA200400702 120041005A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH 520 PDX - REPAIR FUSELAGE SKIN AT STATION 110 BETWEEN STRINGER 31R AND 32R. PERFORMED REPAIR IAW EA 2-53-574A. 2H72 4T RTA13NM 20041109001832004110900183 2004 11 9 SWAA043241 420041106A25656949956 CABLE BOEING737 7375H4 138449DNM L2 & R2 DOORS MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29527SW 26569 DURING SCHEDULED A2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES GIRT BAR CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC CABLES PER MM. 2L72 4F RTA16WE 20041109001852004110900185 2004 11 9 251TR0011 420041010A2565 BOTTLE BOEING737 737228 13844AGNM SLIDE DISCHARGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05251TR 23792 FOUND L-1 DOOR SLIDE PRESSURE GAUGE IN RED BAND. REPLACED L-1 DOOR SLIDE PER MM 25-60-00. 2L72 4F RTA16WE 20041109001882004110900188EA 2004 11 9 SWIA200413990 120041016A3350 LENS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07937SW 7735 FORWARD CABIN DOOR FLOOR LEVEL EMERGENCY EXIT LIGHT BROKEN AND MISSING LENS COVER. REMOVED AND REPLACED LIGHT LENS AND FIXTURE PER AMM 33-51-18, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041109001892004110900189GL 2004 11 9 SWAA043225 220041105A7320936M57P19 MEC BOEING737 7373H4 1384600NM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE FAULTY A SWAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW29649SW 27719 AIR TURNBACK, DURING CLIMBOUT EXPERIENCED 4 SERIES OF ABRUPT NR 2 ENGINE ROLLBACKS, BETWEEN 800 FT AND 2000 FT AT 2000 FT PULLED NR 2 ENGINE THRUST BACK ABOUT 10 TO 20 PERCENT. REMOVED AND REPLACED FUEL PUMP AND MEC PER MM. 2L72 4F4 FRTA16WE E2GL 20041109001902004110900190 2004 11 9 SWAA043226 420041105A2565D31354 SLIDE BOEING737 7372H4 138448CNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041110000012004111000001NM 2004 11 10 2004UALA00976 120041021A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 MAIN CABIN, STA 324, RBL 24-RBL 63, UPPER SURFACE OF FLOORBEAM CORRODED. INSTALLED REPAIR STRAP. 2L72 4F4 FRTA2NM E17NE 20041110000072004111000007EU 2004 11 10 AWXA200401196 120041017A5347D53112092206 SEAT TRACK AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON OB SEAT TRACK Y1292 RT FROM FR 20 TO THE AFT SIDE OF FR 23. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 RT FROM FR 20 TO FR 23; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SRM 51-42-11, FIG. 11-18. 2L72 4F4 FRTA28NM E311NE 20041110000112004111000011SO 2004 11 10 MASA200400570 120041008A3350744426 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY EXIT INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07836MJ 145359 THE AIRCRAFT WAS ON R.O.N. AND SCHEDULED FOR A ROUTINE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE 3D WALL EMERGENCY EXIT SIGN LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20041110000132004111000013NM 2004 11 10 2004UALA00982 120041027A3260 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE MLG DOOR ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29118UA 28811 DURING CLIMBOUT (GEAR DOOR) EICAS MESSAGE ILLUMINATED. CAUSE UNDETERMINED. CMC FAULT ISOLATED PROBLEM TO NOSE GEAR DOOR SENSORS. SENSORS CHECKED AND CLEANED AND BITE CHECK ACCOMPLISHED. AT THIS TIME AIRCRAFT HAS ACMULATED 27 ADDITIONAL CYCLES WITH NO FURTHER REPORTS OF PROBLEM. 2L74 4F4 FRTA20WE E24NE 20041110000222004111000022WP 2004 11 10 AALA20041087 120041101A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21466AA 49596 SEVERAL AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT STATION 1190 FOR AFT CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20041110000242004111000024WP 2004 11 10 AALA20041085 120041030A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21436AA 49454 DURING EMERGENCY LIGHT CHECK OVERHEAD EMERGENCY LIGHTS AT STA 982 RT AND LT, STA 1039 LT AND STATION 1096 RT AND LT WERE INOPERATIVE. REPLACED BATTERY PACK AT STA 1057 RT FOR OVERHEAD EMERGENCY LIGHTS AT STA 982 RT AND LT, 1039 LT AND 1096 RT AND LT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA6WE E9NE 20041110000292004111000029NM 2004 11 10 USAA040712 120040909A575465C26603102 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 UPPER AND LOWER SKIN, 2 INCH SQUARE AREA, DELAMINATION, NR 4 SLAT CTR AREA NEAR AUX TRACK, TOP AND BOTTOM SKIN. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL. INSTALLED NEW CORE AND TOP DOUBLERS, REFINISHED IAW SRM 57-43-02. 2L72 4F4 FRTA16WE E21EU 20041110000402004111000040EU 2004 11 10 EHA2004F00002 120040703A2840 WARNING LIGHT BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1E 60030NE FUEL FILTER ILLUMINATED E EHAAO OTHER O OTHER NRNOT REPORTED 1 AL03141LG 7503 NR 1 AND NR 2 FUEL FILTER LIGHT ILLUMINATED DURING FLIGHT. THE NR 1 CAME ON FIRST, THEN THE NR 2 CAME ON A MINUTE LATER. PILOT LANDED AIRCRAFT, CALLED FOR MECHANIC. REMOVED FUEL FILTERS, INSPECTED FOR WATER, NONE FOUND. REMOVED AND REPLACED ENGINE AIRFRAME FILTERS. STARTED AIRCRAFT, NO OTHER DISCREPANCIES WERE NOTED. PERFORMED MOC. NO DISCREPANCIES FOUND. 1G72 3U3 UNCH13EU E19EU 20041110000462004111000046NE 2004 11 10 DL76L041007 220041101A7261PW40603 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 FAULTY A DALAK NONE O OTHER ININSP/MAINT 1 SO271200K47081 28457 724685 NR 2 ENGINE REPLACED DUE TO HIGH OIL CONSUMPTION. 2L72 4F4 FRTA1NM E24NE 20041110000682004111000068CE 2004 11 10 KNI2004F00000 120040927A30201019100201 VANE BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE HINGE CRACKED E KNIRK NONE O OTHER ININSP/MAINT 1 EA0560AR 2000 BB1743 DURING PHASE INSPECTION, FOUND THE LT ICE VANE CRACKED THRU IN THE CENTER OF THE HINGE. UPON MORE INVESTIGATION, FOUND THE HINGE PIN HAD WORKED ITS WAY OUT OF THE HINGE. EVENTUALLY IT WORE A HOLE THRU THE DUCT SIDE WALL AND PROCEEDED TO COME OUT OF THE HINGE EVEN FURTHER. FINALLY WITH ONLY HALF THE HINGE SUPPORTED BY THE PIN, IT CRACKED IN THE MIDDLE OF THE LAST SEGMENT OF THE HINGE AT BOTH ENDS. POSSIBLY A BETTER WAY OF RETAINING THE PIN COULD BE DEVISED. (IE: A LOOP IN THE HINGE PIN SECURED TO THE HINGE WITH A FASTENER) 1L72 4T4 T A24CE E4EA 20041110000732004111000073SW 2004 11 10 IIFR004F 120041013A5320206031200037 ANGLE BELL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL BOX BEAM CRACKED E IIFRO OTHER O OTHER NRNOT REPORTED 1 SW032193X 3506 CAE270541 LT LOWER CAP ANGLE PN 206-031-200-037 CRACKED 5.250 IN. MEASURED FROM THE FORWARD TIP OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND 5.625 IN. FROM THE FORWARD TIP OF THE CAP ANGLE ON THE VERTICAL SECTION GOING THROUGH RIVET HOLE. ENCLOSED ARE 2 EA. PICTURES OF THE CRACK FOR YOUR REVIEW. THE CRACK WAS FOUND DURING NORMAL MAINTENANCE. DO NOT KNOW THE CAUSE, NOR HAVE PREVENTIVE RECOMMENDATION. THE CAP ANGLE IS BEING REPLACED WITH LIKE PART. 1G71 3U3 U H2SW E4CE 20041110000782004111000078NM 2004 11 10 ASMF200410016 120041022A2421729825J IDG BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT GENERATOR FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23801AM255694181 25624 CAPTAIN REJECTED TAKEOFF AT 70 KTS, RT GENERATOR WAS OUT OF ITS BAR AND DRIVE LIGHT TURNED ON. STARTED THE APU AND RESEATED THE SYSTEM RECOVERING THE GENERATOR. PERFORMED A SECOND ATTEMPT BUT AT 80 KTS REJECTED TAKEOFF DUE TO THE GENERATOR WAS OUT OF ITS BAR AND APU GENERATOR FAILED. DURING MAINTENANCE CHECK, EICAS REPORTED RT GENERATOR WITHOUT FREQUENCY AND VOLTAGE AND IDG WAS WITH FILTER PIN POPPED. IDG WAS REPLACED IAW MM 24-11-01. REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14, DETECTING WHEEL 6 DEFLATED, WHEEL 2 WITH 50 PSI AND BRAKES 5 AND 6 WITH HYDRAULIC BLOCKAGE. 1, 2, 5 AND 6 WHEELS AND BRAKES WERE REPLACED IAW MM 32-45-01 AND 32-41-10, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20041110000792004111000079NM 2004 11 10 ASMF200410017 120041023A5210 MECHANISM BOEING757 7572Q8 1384972NM PWA JT8 JT8D219 52053NE PAX DOOR OUT OF ADJUST W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23806AM 26273 AIRCRAFT REJECTED TAKEOFF AT 80 KTS, AFT CABIN DOOR LIGHT TURNED ON. CAPTAIN REPORTED THAT DURING TAXING, LIGHT TURNED OFF AND TURNS ON AGAIN AT PLATFORM. CAPTAIN REQUESTED TO FLT ATTENDANTS TO CHECK THE DOOR, LINKING THE SLIDE BAR TURNING OFF THE LIGHT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-51-14 AND DOOR CLOSING MECHANISM AND SLIDE ACTIVATION BAR WERE ADJUSTED AND LUBRICATED IAW MM 51-11-00, ALL CORRECT. 2L72 4F4 FRTA2NM E9NE 20041110001042004111000104NM 2004 11 10 DL73S041012 120041102A53136546877143 SHEAR BEAM BOEING737 737232 1384475NM S-, FS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27329DL 23101 A 1 INCH CRACK WAS FOUND EMANATING FROM A FASTENER HOLE AT THE AFT END OF THE STRINGER 18A SHEAR BEAM WEB AT FS 727 ON THE LT SIDE OF THE AIRCRAFT. THE CRACK EXTENDED TO THE AFT EDGE OF THE PART AND FWD OF THE END FASTENER HOLE. THE CRACK WAS REPAIRED WITH AN ALUMINUM CHANNEL AND RADIUS BLOCK PER ER/A 094762-14, REV A. 2L72 4F RTA16WE 20041110001122004111000112NM 2004 11 10 04FDEA03033 120041108A552165174402 RIB BOEING BOEING727 727100 1384036NM RT ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE FM504 18863 RT ELEVATOR NR 5 HINGE SUPPORT RIB ELEVATOR STA 136.50 PREVIOUS REPAIR AT I/B LOWER FLANGE IS CRACKED. REPLACED PER E.O. 7-5510-7-5001 PT 2. 2L73 4F RTA3WE 20041110001142004111000114NM 2004 11 10 04FDEA03035 120041108A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FWD CARGO FRAME STA 660 DENTED STR 24 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-4 AND 53-10-1. 2L73 4F RTA3WE 20041110001152004111000115NM 2004 11 10 04FDEA03036 120041108A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FWD CARGO STA 540 FRAME DENTED AT STR 24 LT & 25 LT. REPAIRED PER SRM 51-40-3, 51-30-5, 53-10-2, 51-10-2, 51-30-2, 51-20-1, 51-20-4, 53-10-1. 2L73 4F RTA3WE 20041110001172004111000117NM 2004 11 10 04FDEA03038 120041108A5310 DOOR FRAME BOEING727 727100 1384036NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 BS 1108 AFT CARGO DOOR FRAME AT STR 26 HAS A OPEN HOLE IN UPPER FLANGE. REPAIRED AFT CARGO DOOR FRAME PER FED EX EA 7-5310-825111. 2L73 4F RTA3WE 20041110001192004111000119WP 2004 11 10 04FDEA02991 120041025A5743 SUPPORT DOUG DC10 DC1010 3022110WP MLG CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION TO P-F/ACF RT WING INTERNAL T-EDGE STRUCTURE STA XORS 264 ON MAIN LANDING GEAR SUPPORT FOUND SEVERAL AREA WITH CORROSION. REMOVE CORROSION PER SRM 51-21-01 PAGE 28, NDI CHECK PROTECT AND INSTALLED NEW FASTENERS. 2L73 4F A22WE 20041110001212004111000121NM 2004 11 10 04FDEA02881 120041006A291359718607 PUMP BOEING727 727200 138407ENM HYD SYSTEM MALFUNCTIONED A FDEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO25495FE 21669 NR 2 B-PUMP LOW PRESS LIGHT ILLUMINATED WITH APPROX 1.4 GALS LOSS IN B-QTY. TURNED NR 2 B-PUMP OFF, GROUND CREW FOUND HYD LEAK IN B-PUMP AREA, B-SPOILER SWITCH TURNED OFF. REMOVED AND REPLACED CASE DRAIN FILTER REF 727-200 M/M 29-12-021-2. STILL NEEDS LEAK CHECK. INSTALLED NEW HYD PUMP. SERVICED HYD FLUID AND LEAK CHECKED. NO LEAKS NOTED. 2L73 4F RTA3WE 20041110001232004111000123WP 2004 11 10 04FDEA02862 120041001A5753ARC19912 FITTING DOUG DC10 DC1010 3022110WP RT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 COMPLY WITH 8-5750-82047- RIGHT O/B HINGE LUG CORROSION REPAIR. COMPLIED WITH EA 8-5750-82047 RIGHT O/B FLAP O/B HINGE LUG CORROSION REPAIR (P/N ARC 1991-2). AT MAE ENT BY: 497234 RPT BY: 497234 2L73 4F A22WE 20041110001272004111000127NE 2004 11 10 04FDEA02866 220041003A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR 3 OVERTEMP A FDEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25318FE466376248 46837 NR 3 ENGINE OVERTEMP ON TAKEOFF AT 700 FT AGL. TEMP ROSE TO 984 DEG FOR 30 SECONDS. SHUT DOWN ENGINE. TRIED RETARDING THROTTLE TO COOL ENGINE BUT WHEN THROTTLE WAS INCREASED N1 AND N2 CONTINUED TO DETERIORATE. NR 3 ENG IS APPROVED FOR REMOVAL. DURING INSPECTION OF EXHAUST FOUND METAL IN TAILPIPE. 2L73 4F4 F A22WE E23EA 20041115000092004111500009NM 2004 11 15 SWAA043283 120041110A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29611SW 27697 FWD OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20041115000352004111500035WP 2004 11 15 0401979763 120041105A2120 ODOR DOUG DC9 DC951 3022051WP CABIN DETECTED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL01763NW 47396 ON APPROACH, FLIGHT ATTENDANT REPORTED BRIEF HOT ELECTRICAL ODOR AROUND ROWS 8-16. NO SMOKE WAS OBSERVED. ALL INDICATIONS WERE NORMAL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CEILING AND SIDEWALL AND EMERGENCY LIGHTS. NO TROUBLE FOUND. RAN PACKS WITH NO ODORS OR IRREGULARITIES NOTED. OPERATIONAL CHECK GOOD. 2L72 4F RTA6WE 20041115000362004111500036NM 2004 11 15 0401875518 120041005A5320 TEE FITTING BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01518US 23206 DURING H-CHECK FOUND CRACKED TEE CLIP FITTING ON AFT SIDE OF FRAME AT BS 1681 STR 13 RT. REPAIRED PER EA 55-201106. 2L72 4F RTA2NM 20041115000392004111500039NM 2004 11 15 SWAA043293 120041110A5753 SKIN BOEING737 7375H4 138449DNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29515SW 2128 25154 DURING SCHEDULED A1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E FLAP PER MM. 2L72 4F RTA16WE 20041115000522004111500052NM 2004 11 15 DL73S041015 120041104A5330654577655 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 INSPECTION OF THE SKIN PER AD 2004-18-06 REVEALED A 4.7 INCH CRACK ALONG THE BONDED DOUBLER LINE JUST ABOVE STRINGER 24L BETWEEN FS 937 & 947. THE CRACK WAS ADJACENT TO AN EXISTING REPAIR DOUBLER FOR ANOTHER SKIN CRACK CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT AND THE EXISTING REPAIR WAS REMOVED. THE NEW AND PREVIOUS CUTOUT WERE REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 094732-14AD. 2L72 4F A16WE 20041115000622004111500062NM 2004 11 15 0401536311 120040909A3350 POWER SUPPLY BOEING747 747451 1384940NM EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01671US 26477 DURING LINE CHECK, FOUND ZONE -A- AND -B- FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20041115000682004111500068WP 2004 11 15 0401779616 120040927A215020495055 COOLING TURBINE DOUG DC9 DC932 3022066WP LT ACM SYSTEM LEAKING A NWAAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01616NW 47229 FOLLOWING TAKEOFF, THE FLIGHT ATTENDANT REPORTED SMOKE IN THE LEFT AFT LAVATORY AND THE LAVATORY ALARM SOUNDED SOON THERE AFTER. NO MENTION OF COM PROCEDURE COMPLIANCE OR OF ANY SUSPECTED CAUSE OF SMOKE. THE FLIGHT RETURNED TO MSP AND LANDED UNEVENTFULLY. PILOT STATED THAT THE SMOKE BEGAN TO CLEAR ON LANDING. MAINTENANCE FOUND EVIDENCE OF OIL IN THE LEFT AIR CYCLE MACHINE OUTLET DUCTS BUT NO TRACE OF OIL UPSTREAM OF ACM. THE LEFT ACM, APU, AND LEFT WATER SEPARATOR WERE ALL REPLACED. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041115000862004111500086NM 2004 11 15 04FDEA03064 120041109A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK, L1 DOOR WAY SEAT TRACK FOUND CORROSION BETWEEN STA 425 - 445. REMOVED PER SRM 51-31-01 VOLUME II. SEAT TRACK P/N ABA760-505 FABRICATED PER DOUGLAS DRAWING ABA7680 AND SRM 51-35-01 USING ABA760-5070 RAW MATERIAL. FABRICATED SEAT TRACK INSTALLED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20041115000972004111500097NM 2004 11 15 2004UALA00992 120041028A5230 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE CARGO DOOR GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 FWD PIT DOOR EXTERNAL SKIN AFT BOTTOM EDGE GOUGED. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041115001102004111500110EU 2004 11 15 AWXA200401214 120041016A5321D5367204100200 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 MCN - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON CORNER OF AFT CARGO COMPARTMENT FLOOR PANEL 161AF UNDER PADDING. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL 161AF, FABRICATED A NEW REPLACEMENT FLOOR PANEL, INSTALLED PANEL IAW A320 SRM 53-02-00. 2L72 4F RTA28NM 20041115001112004111500111EU 2004 11 15 AWXA200401221 120041030A5321D5361012500195 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 MCN - MAJOR REPAIR - DURING C-04 CHECK A 6 INCH CRACK WAS FOUND IN FLOOR PANEL 221AF. MAINTENANCE REMOVED CRACKED FLOOR PANEL FROM FS 12 TO FS 16 AND -Y81 TO -Y512; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG B5D53610125AND A320 SRM 53-02-00, FIG. 209. 2L72 4F RTA28NM 20041115001152004111500115NM 2004 11 15 04FDEA03063 120041109A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO, SEAT TRACK FOUND WORN AT RT STA 999, X= - 8. TRIMMED OUT PER MD-11 SRM 53-70-00 VOLUME I FIGURE 1. REPAIR PARTS FABRICATED AND INSTALLED PER MD-11 SRM 53-70-00 VOLUME I FIGURE1. 2L73 4F RTA22WE 20041115001162004111500116NE 2004 11 15 AWXA200401111 220041006A7297 WIRE HARNESS AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE DAMAGED A AWXAA UNSCHED LANDING RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 WP28626AW40017675 65 V0048 ON CLIMB-OUT AT FL 300, CLIMBING 1200 FPM, 290 KTS ECAM INDICATED ENG 2 COMP VANE WITH INSTRUCTION AVOID THRUST CHANGE, IF ENGINE STALL, ENG MASTER 2 OFF. REDUCED VERT SPEED AS ACRFT CLIMBED THRU FL 310 TO MINIMIZE LEVEL OFF THRUST CHANGES. WITHIN 100 FT OF LEVEL OFF NR 2 ENG COMP STALLED & ENG SHUTDOWN, SELECTED MASTER 2 TO OFF POSITION. NR ENG EGT 585-587 DEG PRIOR TO STALL, NR 1 ENG AT 465 DEG., NO FLUCTS IN FUEL FLOW OR NI / N2, TURNED BACK, LANDED W/OUT EVENT. MX TROUBLESHOT WIRING PERFORMING A DETAILED INSPECTION OF EEC CONNECTOR 4000KS J2 PINS. ENG INVEST CONCLUDED THIS EVENT CAUSED BY LOSS OF POSITION FEEDBACK TO EEC FROM VSV CHANNEL A DUE TO DAMAGED EEC CORE WIRE HARNESS, HARNESS WAS REPLACED. 2L72 4F4 FRTA28NM E311NE 20041115001172004111500117NM 2004 11 15 AWXA200401112 120041002A534769403523 GALLEY TRACK BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY LOWER OUTBOARD TRACK AT BS 294, RBL 42, WL 208. MAINTENANCE REMOVED CORRODED SECTION OF FORWARD GALLEY LOWER OUTBOARD TRACK FROM BS 277 TO BS 294, RBL 42; FABRICATED A NEW REPLACEMENT SECTION OF TRACK; INSTALLED REPAIR PART IAW B737-300 SRM 51-42-02. 2L72 4F RTA16WE 20041115001182004111500118NM 2004 11 15 AWXA200401113 120041002A5320654581216 STIFFENER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK A 5/8 INCH CRACK WAS FOUND IN STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, LBL 28, WL 207. MAINTENANCE REMOVED CRACKED STIFFENER AT BS 328, LBL 28, WL 207; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20041115001192004111500119EU 2004 11 15 AWXA200401243 120041110A3397E0261CF20 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 9 RT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28653AW 1003 DURING 8-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES AT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041115001202004111500120NM 2004 11 15 AWXA200401244 120041103A5754 SKIN BOEING737 7373Y0 1384671NM SLAT ASSY DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-15 CHECK, AN AREA OF DISBOND WAS FOUND ON LT WING NR 3 SLAT INBOARD TRAILING EDGE TIP BETWEEN SLAT STA 12.25 AND 15.25 LT. MAINTENANCE REMOVED DISBONED NR 3 SLAT SKIN; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG. 30. 2L72 4F RTA16WE 20041115001222004111500122NM 2004 11 15 AWXA200401246 120041021A5311146N1025 FRAME BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 DURING C-09 CHECK, A 1/64 INCH CRACK WAS FOUND IN FASTENER HOLE OF LEFT AFT GALLEY FRAME AT FLOORBEAM BS 1681, LBL 64. MAINTENANCE REAMED OUT CRACKED FASTENER HOLE IN FRAME AT BS 1681, LBL 64; FABRICATED 2 EACH FREEZE PLUGS; INSTALLED REPAIR PARTS IAW E.R. 19-5365-00046-JS2A. 2L72 4F RTA2NM 20041115001232004111500123EU 2004 11 15 AWXA200401247 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 43 AND FS 44. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 43 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001262004111500126EU 2004 11 15 AWXA200401250 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 39 AND FS 40. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 39 TO FS 40; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001282004111500128EU 2004 11 15 AWXA200401252 120041025A5347D5337111001000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, FRETTING CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 46 AND FS 47. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 43 TO FS 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001302004111500130EU 2004 11 15 AWXA200401254 120041025A5347D53371110010000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 44 AND FS 45. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 44 TO FS 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001312004111500131NM 2004 11 15 AWXA200401114 120041009A2611PPA120200PPA1202SMOKE DETECTOR AIRBUSA319 A319132 3930340NM FWD LAV ZONE 221MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28830AW111772765 1565 EN ROUTE FROM LAS TO JFK RECEIVED SMOKE DETECTOR CONTROL UNIT MESSAGE, DIVERTED TO PHX FOR REPAIR. MAINTENANCE TROUBLESHOT IAW TSM 26-17-00-810-803, REMOVED AND REPLACED LAVATORY A SMOKE DETECTOR (1WQ) IAW 26-17-15, OPERATIONAL CHECK WAS GOOD. VENDORS FUNCTIONAL TEST OF SMOKE DETECTOR S/N 2207 WAS NO FAULT FOUND, ALL FUNCTIONS TESTED WITHIN MANUFACTURERS SPECIFICATIONS. AS PRECAUTION THE UNIT CELL WAS CLEANED. 2L72 4F RTA28NM 20041115001332004111500133NM 2004 11 15 2004UALA00971 120041023A21202156204 SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE EQUIP COOLING FAILED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29548UA 25396 FORWARD EQUIPMENT SMOKE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE, REPLACED FORWARD EQUIPMENT COOLING SMOKE SENSOR. 2L72 4F4 FRTA2NM E17NE 20041115001362004111500136NM 2004 11 15 2004UALA00974 120041025A3242 BRAKE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE MLG SMOKE A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29648UA 25285 HEAVY SMOKE COMING FROM 4F MAIN TIRE WHEN TAXIING INTO GATE. BRAKE MR 32357 DASH 2181 REPLACED. 4F TIRE REPLACED. 3F TIRE REPLACED AS MATE. CLEANED INSIDE 4F AXLE AND FOUND PAINT DISCOLORATION. OUTSIDE OF AXLE FOUND NO DAMAGE TO CADMIUM PLATING. ACCOMPLISHED BOROSCOPE OF 4F AXLE, FOUND DISCOLORATION OF GREEN PRIMER, ACCOMPLISHED HEAT DAMAGE INSP. 2L72 4F4 FRTA1NM E24NE 20041115001372004111500137 2004 11 15 2004UALA00975 420041025A2565 GIRT BAR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE 1L DOOR SLIDE LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29916UA 25383 GIRT BAR DOOR 1L DOES NOT STAY IN PLACE. SHOP FINDINGS FROM INSPECTION OF THE SLIDE UNIT REVEALED A LOOSE GIRT BAR SLEEVE. THE LOOSE GIRT BAR WAS REPAIRED AND THE SLIDE UNIT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20041115001382004111500138EU 2004 11 15 AWXA200401132 120041016A3397D9299200900200 WIRE HARNESS AIRBUS320 A320232 3930326EU SEAT ROW 9 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28656AW 1079 PHX - EEL - DURING E-01 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT HARNESS AT SEAT ROW 9 LT IAW AMM 33-51-18-04, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041115001392004111500139NM 2004 11 15 AWXA200401133 120041017A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM ZONE 242 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28660AW12880 1234 LAX - EEL - DURING 4-DAY CHECK, FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041115001402004111500140NM 2004 11 15 AWXA200401134 120041017A335020131A POWER SUPPLY BOEING737 737301 1384611NM SEAT ROW 11 LT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 PHX - EEL - THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 11-17 LT DID NOT TURN OFF DURING BREAKER RESET FOR EMERGENCY LIGHT TEST. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041115001442004111500144NM 2004 11 15 2004UALA00998 120041030A3397 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE TERMINAL BLOCK BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29649UA 25286 FOUND WIRES W298-021-08, W1046-913-08, W1046 -012-10, W1046-028-12. BURNED AT TB 5132 TERMINAL BLOCK INSIDE P37. REPLACED TERMINAL STRIP TB5132 IN P37 PANEL. 2L72 4F4 FRTA1NM E24NE 20041115001452004111500145EU 2004 11 15 AWXA200401098 120040925A5320D53112818204 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT Y254 LT AT FR 16. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT Y254 LT AT FS 16; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG D53112816; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041115001462004111500146EU 2004 11 15 AWXA200401099 120040925A5320D5347217220400 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM Y1292 LT BETWEEN FR 66 AND FR 67, LT AFT GALLEY AREA. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 LT FROM FS 66 TO FS 67; INSTALLED NEW REPLACEMENT FLOORBEAM IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001472004111500147EU 2004 11 15 AWXA200401100 120040924A5312D5337081500000 FITTING AIRBUS320 A320232 3930326EU PRESSURE BLKHD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, A 2 INCH CRACK WAS FOUND ON SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LT, FS 35. MAINTENANCE REMOVED CRACKED SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LEFT, FS 35; FABRICATED A NEW REPLACEMENT FITTING PER DWG D53370800; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041115001522004111500152WP 2004 11 15 04FDEA02940 120041015A5753ARC25122 HINGE FITTING DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 RIGHT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE GOUGED. REMOVED DAMAGE I/A/W DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81491 REFERENCE NON-ROUTINE NR N00412. 2L73 4F A22WE 20041115001542004111500154WP 2004 11 15 04FDEA02941 120041015A5753ARC25121 HINGE FITTING DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE PITTED. REMOVED DAMAGE, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57- 52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00417. 2L73 4F A22WE 20041115001632004111500163NM 2004 11 15 04FDEA03014 120041103A5230 SKIN BOEING727 72722 1384002NM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE BM211 18863 AFT CARGO DOOR EXTERNAL SKIN GOUGED AT LWR EDGE, 17 INCH FROM AFT EDGE. REPAIRED SKIN IAW SRM 52-00-3. 2L73 4F A3WE 20041115001652004111500165NM 2004 11 15 04FDEA02943 120041017A2730 ROD END DOUG MD11 MD11F 3023600NM ELEV FEEL ACT DAMAGED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25594FE 48552 ON T/O, THE ACFT ROTATED EXTREMELY SLOW DUE TO ABNORMALLY HEAVY NOSE. CONTACTED GOC TO VERIFY LOAD. AFTER DISCUSSION WITH MX IT WAS DETERMINED THAT PAST HISTORY OF JET SUGGESTED FLT CONTROL PROBLEM. EMERGENCY DECLARED, FUEL DUMPED TO LANDING WEIGHT, CONTROL CHECK ACCOMPLISHED. FOLLOWED BY AUTOLAND. REMOVED AND REPLACED THE DUPLEX ACT ROD END BOLT PER 27-32-01-4, CKD CLEARANCE OF THE ELEV LOAD FEEL ACT ROD END BOLT AND MECH IN ALL POS REF MD11MM 27-32-01-4. ALL CHK GOOD. ADJ THE AG CAM MARK WITH THE AH LEG PER MM 27-30-00-5 FOR THE BUS TUBE ASSY. RII C/W R/R FCC 1 AND FCC 2 PRECAUTIONARY. FCC RTS'S C/W. C/W THE CAT3B RTS. REF MD11 AMM 22-00-00-5. 2L73 4F RTA22WE 20041115001662004111500166NM 2004 11 15 04FDEA02944 120041018A5753ARC74901 TEE FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES, LEFT HAND INBOARD FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20041115001672004111500167NM 2004 11 15 04FDEA02945 120041018A5753ARC74901 TEE FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LEFT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. LEFT HAND WING INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT. BORES REPAIRED AS PER EA NR 1-5750-77964, TITLE: WINGS-TRAILING EDGE AND TRAILING EDGE DEVICES, LEFT HAND INBOARD FLAP VANE ATTACH FITTINGS REWORK. 2L73 4F RTA22WE 20041115001712004111500171WP 2004 11 15 04FDEA02590 120040831A5753ARC1455509 VANE DOUG MD10 MD1010F 3022112WP LT OB FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 BFM CLOSE R COMPLY WITH EA NR 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK ENT BY: 527637 RPT BY: 527637 FACT 01 SEP04 04:30 BFM U COMPLIED WITH EA 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK RII:497214, ENT BY: 527637 RPT BY: 527637. 2L73 4F RTA22WE 20041115001722004111500172NM 2004 11 15 04FDEA02591 120040901A53131D0590T LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 51R BETWEEN STA Y= 1681 AND STA Y= 1701. CENTER CARGO, BETWEEN STA Y= 1681 AND STA Y= 1701, CORRODED LONGERON 51R REMOVED PER SRM 51-33-01 VOLUME I. LONGERON SPLICE FABRICATED PER SRM 53-10-00 FIGURE 2 VOLUME I AND INSTALLED PER SRM 51-33-01 VOLUME I. 2L73 4F RTA22WE 20041115001732004111500173EU 2004 11 15 AWXA200400976 120040815A5315D5347209800000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y919 LT AT FS 66. MAINTENANCE REMOVED CORRODED BEAM Y919 LT AT FS 66, INSTALLED NEW REPLACEMENT BEAM IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001742004111500174NM 2004 11 15 04FDEA02621 120040903A5753ARC198413 BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS , LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041115001752004111500175NM 2004 11 15 04FDEA02622 120040903A5753ARC198413 BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.077 INCH AND REPAIRED AS PER EA NR1-5750-80344, TITLE: WINGS, LT OUTBOARD FLAP, I/B FLAP SIDE HINGE. BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041115001782004111500178EU 2004 11 15 AWXA200400979 120040815A5315D5347218920000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW SECTION OF REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001792004111500179NM 2004 11 15 04FDEA02785 120040921A5753ARC199114 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.504 INCH, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.006 INCH, AND REPAIRED AS PER EANR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041115001802004111500180NM 2004 11 15 04FDEA02899 120041011A2740AJG70055501 MOTOR DOUG MD11 MD11F 3023600NM ZONE 300 LEAKING A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO25615FE MX341132 48767 DURING WALK AROUND FOR TEST FLIGHT, FOUND HYDRAULIC FLUID LEAKING FROM STAB ACCESS PANEL ENT BY: 497948 RPT BY: 096450. HORIZONTAL STABILIZER NR 2 HYDRAULIC MOTOR AND BRAKE REMOVED AND REPLACED AND LEAK CHECK AND FUNCTIONAL TEST SATISFACTORY. 2L73 4F RTA22WE 20041115001842004111500184NM 2004 11 15 AWXA200401009 120040911A3350100865 POWER SUPPLY BOEING737 737301 1384611NM SEAT ROW 17 LT FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, THE EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE FROM SEAT ROW 11 LEFT TO SEAT ROW 17 LEFT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY AT SEAT ROW 17 LEFT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041115001852004111500185NM 2004 11 15 AWXA200401010 120040911A33501000679 LIGHT BOEING737 737277 1384570NM EMERGENCY EXIT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28186AW 22653 FLIGHT CREW REPORTED THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041115001892004111500189NM 2004 11 15 AWXA200401014 120040905A5315D5347217220300 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT AT FS 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041115001902004111500190NM 2004 11 15 AWXA200401015 120040908A5315D5347228400800 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y465 BETWEEN FS 64 AND FS 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y465 RT FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11. 2L72 4F RTA28NM 20041115001922004111500192 2004 11 15 2004UALA01005 420041101A2565 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE SLIDE LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29648UA 25285 POSITION 1 EMERGENGY ESCAPE SLIDE SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST. DEFECT CAUSED BY LOW BATTERY. REPLACED LEFT HAND BATTERY PACK. 2L72 4F4 FRTA1NM E24NE 20041115001932004111500193EU 2004 11 15 04FDEA03021 120041104A2410 SWITCH AIRBUS310 A310222 3930315EU NR 1 GENERATOR MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25452FE 313 RTD AT ESSA 19R FOR NR 1GEN FAULT AND MASTER CAUTION AT 60 KTS. ACCOMPLISHED RTO CKLST AND RETURNED TO GATE. NR 1 GEN, DID NOT AUTOCONNECT ON STARTUP, HAD TO ADVANCE THROTTLE AND RESET GEN 1 SW. ON TAXI BACK GEN 1 MADE CLICKING SOUND CONNECTING AND DISCONNECT SEVERAL TIMES AND FINALLY STAYED CONNECTED UNTIL SHUTDOWN. A/C RELEASED FOR SERVICE PER MEL 24-11-01. REMOVED AND REPLACED NR 1 GCU AS PER MM:24-22-12-4. NR 1 ENGINE RUN PERFORMED BY EMP NR 181214. NR 1 GEN CAME ON LINE NORMAL. 2L72 4F RTA35EU 20041115001942004111500194WP 2004 11 15 04FDEA02915 120041011A5753ARC19842 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 RIGHT HAND OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE CORRODED (INBOARD SUPPORT). REMOVED CORROSION IAW DACCMM 57-52-02. ETCHED AND PEENED IAW DACCMM PERCENT &-52-02 AND 20-11-02. FABBED BUSHING IAW DACCMM 57-52-02 AND EA8-5750-81472. CAD PLATED BUSHING IAW QQ-P- 416TC AT BY OUTSIDE VENDOR PO NR 460364, THEN INSTALLED IAW DACCMM 57-52-02 FINAL HONED BUSHING TO A BORE OF .8752 IAW DACCMM 57-52-02 USING TOOL TWS8725 DATE 6-18-05. 2L73 4F RTA22WE 20041115001952004111500195WP 2004 11 15 04FDEA02916 120041011A5753ARC25121 HINGE FITTING DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DACCMM 57-52-01, BORE FOUND OUT OF LIMITS, GENERATED RFTS, RECEIVED FEDEX EA8-5750-81492, REPAIRED BORE IAW DACCMM 57-52-01 AND FEDEX EA8-5750-81492. SEE NR N00416. 2L73 4F RTA22WE 20041115001962004111500196NM 2004 11 15 04FDEA03040 120041108A5347 SEAT TRACK BOEING727 72722 1384002NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 SEAT TRACK GOUGED AT BS 740, RBL 45, WL 208. REPAIRED SEAT TRACK PER SRM 53-10-5. 2L73 4F A3WE 20041115001972004111500197NM 2004 11 15 04FDEA03041 120041108A5340 STRINGER CLIP BOEING727 72722 1384002NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 STRINGER CLIP CRACKED, STR 5L, BS 1010. REPLACED PER SRM 51-30-2, 51-30-5 2L73 4F A3WE 20041115001992004111500199NM 2004 11 15 04FDEA03043 120041108A5313 STRINGER BOEING727 72722 1384002NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 MAIN CARGO BAY HAS GOUGE ON STRINGER 9R AT BS 600. 2L73 4F A3WE 20041115002022004111500202NM 2004 11 15 04FDEA03080 120041111A5315 FLOORBEAM BOEING727 727247 138408FNM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25233FE 21327 CORROSION WHILE WORKING EO 7-5340-82473, FOUND CORROSION ON FLOORBEAM SPLICE AT BS 344, RBL 18. REPAIRED PER SRM 53-10-1, 51-10-2, 51-30-2, 51-30-5, 51-30-8, AND FED EX SRD 27-53-007. 2L73 4F A3WE 20041115002052004111500205NM 2004 11 15 04FDEA02634 120040903A7830 TRACK DOUG MD11 MD11F 3023600NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 ENG NR 2, LEFT THRUST REVERSER TRANSLATING SLEEVE TOP SLIDE TRACK AFT EDGE FOUND WITH SUSPECTED CRACK AT AFT EDGE. 2L73 4F RTA22WE 20041115002082004111500208EU 2004 11 15 AWXA200401204 120041017A5315D53112091200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT BETWEEN FS 16 AND FS 20. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14, FIG 102. 2L72 4F RTA28NM 20041115002092004111500209EU 2004 11 15 AWXA200401205 120041017A5320D53112067200 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT OUTBOARD WEB Y1698 BETWEEN FS 20 AND FS 21. MAINTENANCE REMOVED CORRODED SECTION OF RT OUTBOARD WEB Y1698 FROM FS 20 TO FS 21; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115002102004111500210EU 2004 11 15 AWXA200401206 120041018A5347D53371112000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115002132004111500213WP 2004 11 15 04FDEA02638 120040904A5730ARC0264508 PANEL DOUG DC10 DC1010F 3022111WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 RIGHT WING TRAILING EDGE PANEL 641 EB HAS MANY AREA OF DELAMINATION. REPAIRED RIGHT WING TRAILING EDGE PANE 641EB BY FABRICATING AND BONDING INNER AND OUTER SKIN, HONEYCOMB CORE AND INNER DOUBLER IAW EA 8-5710-7763, DAC DWG ARC0264 AND TPS 1001 REV E, REFERENCE N/R N00882. 2L73 4F A22WE 20041115002152004111500215NM 2004 11 15 AWXA200401153 120041005A53476545410200 SEAT TRACK BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN LT INBOARD SEAT TRACK BEAM AT BS 727B, LBL 24.75. MAINTENANCE TRIMMED OUT CRACK IN LT INBOARD SEAT TRACK BEAM AT BS 727B, LBL 24.75; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, SHIM, AND 2 EACH STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5702-04293-SS2. 2L72 4F RTA16WE 20041115002162004111500216NM 2004 11 15 AWXA200401154 120041003A53306545765100 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST ABOVE LAP SEAM AT BS 500D+10, STR 10 RT. MAINTENANCE CUTOUT CRACK IN FUSELAGE SKIN AT BS 500D+10, STR 10 RT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED 2 EACH FILLERS AND A DOUBLER; INSTALLED REPAIR PARTS IAW T/C M1A53108. 2L72 4F RTA16WE 20041115002172004111500217NM 2004 11 15 AWXA200401155 120041002A5315654581292 FLOORBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON BEAM AT BS 328, BETWEEN RBL 11 AND RBL 21, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF TEE CAP BEAM AT BS 328, FROM RBL 11 TO RBL 21; FABRICATED 2 EACH REPAIR ANGLES AND A NEW REPLACEMENT SECTION OF CHORD; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205. 2L72 4F RTA16WE 20041115002192004111500219NM 2004 11 15 AWXA200401157 120040930A53306552988117 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 1 3/16 INCH, CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF L-2 DOOR BS 963, STR 17 LT. MAINTENANCE STOP DRILLED CRACK AT LOWER FORWARD CORNER OF L-2 DOOR BS 963, STR 17 LT. FABRICATED AN INNER, MIDDLE, AND OUTER PATCH, AND 3 EACH TAPERED FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG 203. 2L72 4F RTA16WE 20041115002202004111500220NM 2004 11 15 04FDEA02790 120040921A5753ARC199114 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.190 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041115002212004111500221NM 2004 11 15 04FDEA02791 120040921A5753ARC199114 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.403 INCH, REMAINING THICKNESS=0.400 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS LEFT AND RIGHT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041115002222004111500222NM 2004 11 15 04FDEA02792 120040921A5753ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING FOUND CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30. 2L73 4F RTA22WE 20041115002232004111500223EU 2004 11 15 04FDEA02793 120040921A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 MDCC SEAT TRACK R1 BETWEEN FRAME 73-80 HAS 7EA DISCREPANT AREAS 5EA AREAS THAT ARE CORRODED AND GOUGED AND 2EA AREAS THAT ARE GOUGED. REMOVED AND REPLACED R1 SEAT TRACK FRAME 73-80 IAW A310 SRM 51-40-21 AND SRM 53-10-16. 2L72 4F RTA35EU 20041115002242004111500224EU 2004 11 15 04FDEA02794 120040921A5320 STRUCTURE AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 AFT CARGO COMPT FWD OF FS 54.2 BILGE AREA NOTED SPOT OF CORROSION AROUND THE HOLE PLUG. REPAIRED BILGE AREA IAW EA 6-5330-55370. 2L72 4F RTA35EU 20041115002252004111500225EU 2004 11 15 04FDEA02795 120040921A5315 FLOORBEAM AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 AFT CARGO COMPT FS 63 FLOOR STRUCTURE, ON LEFT SIDE 3EA AREAS OF CORROSION ON TOP SURFACE AND UNDERNEATH FLOOR STRUCTURE. REMOVED AND REPLACED FLOOR STRUCTURE BEAM IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20041109001452004110900145NM 2004 11 9 QXEA200400736 120041030A2613 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM CABIN FALSE INDICATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09413QX 4060 YYC - FLIGHT 2335 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED A FLIGHT COMPARTMENT AND CABIN DUCT HOT CAUTION LIGHTS. THE DUCT TEMPS WERE NORMAL. CABIN WOULD NOT PRESSURIZE AFTER CYCLING THE AUTO AND MANUAL BLEED SWITCHES. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEARED THE MESSAGES IAW Q-400 FIM. MAINTENANCE WAS UNABLE TO DUPLICATE THE WRITE-UPS WHILE PERFORMING THE OPERATIONAL CHECKS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041109001462004110900146NM 2004 11 9 371PA0078 120040918A5315 STRAP BOEING737 737306 13844BGNM FLOORBEAM CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05371PA 23543 STRAP ON PREVIOUS BLEND OUT ON FLOORBEAM AT BS 328 AT LBL 12 HAS CORROSION. REMOVED STRAP AND REPAIRED FLOORBEAM PER SRM 53-10-51. 2L72 4F RTA16NE 20041109001472004110900147NM 2004 11 9 151AW0041 120040923A3350 BULB BOEING737 7373G7 1384595NM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05151AW 23219 LEFT OVERWING FWD EMERGENCY LIGHT BULB IS OUT. REPLACED BULB, CHECKS GOOD. 2L72 4F RTA16WE 20041109001492004110900149NM 2004 11 9 250TR0052 120041022A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05250TR 22597 INTERCOSTAL WEB FROM BS 500A TO BS 500B AT STR 26 LT IN FORWARD CARGO BIN IS CRACKED. REPLACED WEB AND ATTACH ANGLE PER BOEING DWG 69-41473 AND DWG 69-51411 AND SRM 51-30-0. 2L72 4F RTA16WE 20041109001512004110900151EA 2004 11 9 SWIA200413987 120040710A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07407SW 7034 CLIP AT RBL 9 OUTBOARD AT FS 280.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP AT RBL 9 O/B FS 280.0 IAW CRJ 200 SRM CH 51-42-13 AND 51-42-21. 2L72 4F RTA21EA 20041110000352004111000035EU 2004 11 10 KBM2004F00230 120040921A771230573166 GAUGE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE TORQUE STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 2300 TORQUE GAUGE STUCK AT 75 PERCENT. REPLACED WITH SERVICEABLE GAUGE. 1G71 3U3 UNCH9EU E19EU 20041110000362004111000036NM 2004 11 10 QXEA200400735 120041030A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA AFT CARGO DOOR OPEN A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09400QX8185 4030 FLIGHT ABORTED THE TAKE-OFF AFTER THE CREW RECEIVED A DOOR WARNING FOR THE AFT CARGO DOOR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR HANDLE POPPED OUT. THE HANDLE WAS SECURED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20041110000802004111000080WP 2004 11 10 ASMF200410018 120041024A8010 START VALVE DOUG DC9 DC987 3022087WP RT ENGINE INOPERATIVE W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23754RA 49641 AIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. TECHNICAL PERSONNEL OPENED MANUALLY THE VALVE. AT GDL, PNEUMATIC LINE OF START VALVE WAS REPLACED IAW MM 80-10-01, ALL CORRECT. 2L72 4F RTA6WE 20041110000942004111000094NM 2004 11 10 DL76G041011 120041103A2510824251615 MOTOR BOEING767 767332 1382001NM COCKPIT SEAT FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271602 29694 DIVERTED INTO PHX DUE TO F/O SEAT SMOKE AND SPARKS INFLIGHT FOUND F/O SEAT ELECTRIC DRIVE MOTOR FAULTED AND C/B POPPED. REPLACED MOTOR. 2L72 4F RTA1NM 20041110000962004111000096NM 2004 11 10 04FDEA03030 120041108A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 AFT CARGO FRAME DENTED AT BS 990, STR 26R. REPAIRED PER SRM 51-40-3. 2L73 4F RTA3WE 20041110001132004111000113NM 2004 11 10 04FDEA03034 120041108A5311 FRAME BOEING727 727100 1384036NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 TOP FLANGE OF FRAME AT BS 640, RBL 32, WL 150 IS DENTED. REPAIRED PER SRM 53-10-1, 51-30-5, 51-20-4, 51-30-2, 51-10-1, 53-10-2 AND 51-40-3 2L73 4F RTA3WE 20041110001162004111000116NM 2004 11 10 04FDEA03037 120041108A5313 STRINGER BOEING727 727100 1384036NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 GOUGE ON UNDERSIDE FLANGE OF STR 19 RT, BS 488, WL 174. REPAIRED STR 19 RT IAW SRM 53-10-3 FIG 1 AND 53-10-1. 2L73 4F RTA3WE 20041110001182004111000118NM 2004 11 10 04FDEA03039 120041108A5340 STRINGER CLIP BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 STRINGER CLIP CRACKED BS 1108 LT STR 20. REPLACED STRINGER CLIP PER SRM 51-30-2. 2L73 4F RTA3WE 20041110001202004111000120EU 2004 11 10 04FDEA02880 120041005A2840 INDICATOR AIRBUS310 A310203 3930313EU FUEL QTY MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25428FE 248 REACHING CRUISE FL330 THE RIGHT OUTER TANK QUANTITY BEGAN DECREASING BY 4 TO 5 HUNDRED INCREMENTS FROM 6300 LBS TO 2500 LBS ON THE ECAM AND ON THE OVERHEAD. REFERENCE QRH AND HAD SYMPTOMS OF A FUEL LEAK. RETURNED TO RENO, TURNED OFF THE RIGHT OUTER FUEL PUMPS AND LEAKS STOPPED, TANK STOPPED DECREASING. ON RETURNING THE RIGHT OUTER QUANTITY CAME BACK TO NORMAL 6300 LBS. PRECAUTIONARY- MEL 28-42-01-01: ALL (IDENTIFY LEFT OR RIGHT). OUTER TANK INDICATIONS INOP. EITHER FUEL TO KNOWN QTY OR, AFTER REFUELING VERIFY TANK QTY WITH MAG MEASURING STICKS AND RECORD IN AML/EAML. 2L72 4F RTA35EU 20041110001222004111000122EU 2004 11 10 04FDEA02882 120041006A77146360004591 INDICATOR AIRBUS300 A300F4605R 3930327EU ENGINE N2 MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25680FE 794 WITH POWER SET ON TAKEOFF NR 2 ENGINE N2 ANALOG INDICATION SHOWED APPROXIMATELY 20 LESS THAN THE DIGITAL INDICATION. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 2 ENG N2 GAUGE PER AIRBUS M/M 77-12-21-4, OPS CHECKED PER ENG RUN PER JRH. NORMAL INDICATIONS FOLLOWED. 2L72 4F RTA35EU 20041110001242004111000124NM 2004 11 10 04FDEA02863 120041001A5753 STRUCTURE DOUG MD11 MD11 3023602NM TE FLAPS CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 037 48481 LEFT WING, OUTBOARD FLAP, INBOARD AFT HINGE LOCATION MID ATTACHMENT FITTING SUSPECTED CRACKED. LEFT WING, OUTBOARD FLAP ASSEMBLY P/N NRC6753-503. REMOVED AND REPLACED PER AMM 27-50-30. 2L73 4F RTA22WE 20041110001252004111000125EU 2004 11 10 04FDEA02864 120041003A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 MDCC 62 INCHES TO LEFT OF CTR FR 16A IS CORROSION ON TRACK 5R. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-10-16. 2L72 4F RTA35EU 20041110001262004111000126EU 2004 11 10 04FDEA02865 120041003A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 MDCC 67 INCHES TO RIGHT OF CTR FR 54.3 FLOORBEAM CRACKED .4 INCH ON FWD AND AFT SIDE. REPAIRED AREA IAW A310/200 SRM 53-10-15, FIG 201. 2L72 4F RTA35EU 20041110001282004111000128NM 2004 11 10 04FDEA02867 120041004A7160128012459 SEGMENT DOUG MD11 MD11 3023602NM ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE FOUND WITH CORROSION. ENGINE NR 2 INLET BELLMOUTH TRANSITION RING LOWER SURFACE CORROSION REPAIR CARRIED OUT. 2L73 4F RTA22WE 20041110001302004111000130NM 2004 11 10 04FDEA02891 120041007A5320ADA35481 BRACKET DOUG MD11 MD11 3023602NM ZONE 200 MISALIGNED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 MAIN DECK, NEW ANGLE BRACKET P/N ADA3548-1 FOR INTERCOSTAL ADA8392-1 INSTALLATION AT STA Y= 775 TO STA Y= 791.75 LONGERON 7L FOUND MISALIGNED WITH FUSELAGE TRANSVERSE FRAME EXISTING HOLE. NEW ANGLE BRACKET FABRICATED PER DAC DWG ADA3852 AND PART MARKED P/N FX ADA3852-3 PER FEDEX GMM 7-0-1000. NEW ANGLE BRACKET INSTALLED PER FEDEX EO 1-5310-7-5002 REV 02 PART 2, FUSELAGE - MAINFRAME - INTERCOSTAL INSTALLATION INSPECTION/ PASSENGER TO FREIGHTER CONFIGURARTION DISCREPANCIES. COMPLIED WITH FEDEX EA 1-5310-74761, FUSELAGE - MAINFRAME - DEVIATION TO EO 1-5310-7- 5002. 2L73 4F RTA22WE 20041110001322004111000132NM 2004 11 10 04FDEA02893 120041008A5713ARB75101 STRINGER DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LEFT HAND WING (S10) STRINGER END FOUND CRACK INSIDE FUEL TANK PANEL 538AB. STRINGER NR 10 CRACK REMOVED AS PER SRM 57-20-00 FIG 10 VOL I & INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II & SRM 57-20-00 FIG 10 VOL I. 2L73 4F RTA22WE 20041110001342004111000134EU 2004 11 10 04FDEA02889 120041007A5347 SEAT TRACK AIRBUS310 A310222 3930315EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 MAIN CARGO DECK FR 45.5, NR 1 SEAT TRACK LEFT SIDE, WITH 1 EA AREA OF CORROSION NOTED INSIDE SCALLOP HOLES. REMOVED CORROSION IAW A310 SRM 53-10-15, AND FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-16 PG 103 FIG 101. TREATED AND PRIMED AREA IAW A310 SRM 53-25-10. 2L72 4F RTA35EU 20041110001362004111000136NM 2004 11 10 04FDEA02836 120040928A5510ALC8106Y1 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 14 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REPLACED AS PER SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20041110001382004111000138NM 2004 11 10 04FDEA02838 120040928A5743 BEAM BOEING727 727200 138407ENM ZONE 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 COMPLY WITH EA 7-5710-82042 WINGS RIGHT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. COMPLIED WITH EA 7-5710-82042 REAMED HOLE, FLAP PEENED AND INSTALLED REPAIR BUSHING. 2L73 4F RTA3WE 20041110001402004111000140NM 2004 11 10 04FDEA02800 120040922A5313BAC1498142 STRINGER BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 NUMEROUS AREAS OF CORROSION FOUND AT FWD PIT BILGE AREA FROM STA 560 TO STA 580 AT STR 28L. REMOVED DAMAGED AREA FROM STA 550 - 590 IAW SRM 51-10-3 FIG 1 PG 4. FABBED 2EA STRINGERS FROM BAC1498-142 7075-T62, BATCH 318127, FABBED 3EA SPLICES FROM BAC1498-132 PO MST0009960. INSTALLED NEW PARTS IAW SRM 51-30-2. 2L73 4F RTA3WE 20041110001422004111000142NM 2004 11 10 04FDEA02616 120040903A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.191 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041110001442004111000144NM 2004 11 10 04FDEA02618 120040903A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE FOUND CORRODED. LEFT WING - O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOT FACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.394 INCH, MATERIAL REMOVED=0.004 INCH, REMAINING THICKNESS=0.390 INCH AND REPAIRED AS PER EA 1-5750-80344, TITLE: WINGS - LEFT OUTBOARD FLAP - I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041115000062004111500006NM 2004 11 15 AALA20041101 120041103A3350 LIGHT BOEING757 757223 1384957NM EMERGENCY SIGN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21657AM 24615 MIA - LEFT ONE DOOR TWO EACH EMERGENCY EXIT LIGHTS ARE BROKEN. REPLACED TWO EMERGENCY EXIT SIGNS AT LEFT ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041115000082004111500008WP 2004 11 15 AALA20041108 120041106A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21474 49649 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 24 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 24 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000162004111500016 2004 11 15 SWAA043298 420041110A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 & L2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 L1 AND L2 DOOR EVAC SLIDES WOULD NOT ARM. SWAPPED SLIDE POSITIONS PERT MM. 2L72 4F RTA16WE 20041115000222004111500022WP 2004 11 15 0401949609 120041004A5711 SPAR CAP DOUG DC9 DC932 3022066WP RT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING M-CHECK FOUND CORROSION ON RT WING SPAR CAP AT XRS 267. REPAIRED PER EA 96-200541. 2L72 4F A6WE 20041115000232004111500023WP 2004 11 15 CALA0400704 120041108A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2783870 48056 INSPECTION FOUND BELL FRAME CORRODED AT STA 1320 ABOVE LONGERON 30. REPAIRED BELL FRAME IAW SRM 53-03, PAGE 4A AND SRM 53-01, FIGURE 2, PAGE 3. 2L72 4F A6WE 20041115000242004111500024NM 2004 11 15 CALA0400705 120041109A532050826162 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT UPPER FORWARD CORNER OF FORWARD ENTRY DOOR SURROUND STRUCTURE BETWEEN STA 309 AND 312, S4L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2L72 4F RTA16WE 20041115000332004111500033WP 2004 11 15 AALA20041092 120041102A2820 PRESSURE SWITCH DOUG DC9 DC982 3022082WP FUEL SYSTEM INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2116545 53027 FUEL ANOMALY WITH CROSSFEED VALVE OPEN AND ONE LEFT FUEL PUMP OFF. FUEL IS BURNED FROM RIGHT TANK ONLY. ATTEMPTS TO TURN OFF BOTH LEFT PUMPS RESULTS IN LEFT LOW PRESSURE LIGHT ILLUMINATED. LANDED RDU WITHOUT INCIDENT. CHECKED FUEL CROSSFEED FROM LEFT TO RIGHT AND RIGHT TO LEFT. FOUND ALL TO BE NORMAL. FOUND LEFT PRESSURE INLET SWITCH WORKING INTERMITTENTLY. REPLACED FUEL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000382004111500038 2004 11 15 SWAA043292 420041110A25656949956 CABLE BOEING737 7375H4 138449DNM L2 DOOR SLIDE MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29515SW 25154 DURING SCHEDULED A1 CHECK, FOUND R2 AND L2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED CABLES PER MM. 2L72 4F RTA16WE 20041115000402004111500040 2004 11 15 SWAA043294 420041110A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29422WN 29826 DURING SCHEDULED HC2 CHECK, FOUND R1 AND L1 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 AND R1 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041115000502004111500050NM 2004 11 15 SWAA043284 120041110A32336544825815 ACTUATOR BOEING737 7373Q8 1384670NM RT MLG LEAKING A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29687SW 23388 RIGHT MLG DOWN AND LOCKED DURING FLIGHT. GEAR HANDLE WAS OFF AND ALL OTHER LANDING GEARS STAYED UP AND LOCKED. RIGHT MLG CAME UP WHEN HANDLE WAS RAISED. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20041115000562004111500056NM 2004 11 15 0401925518 120040930A5347 SEAT TRACK BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01518US 23206 DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT BS 365 RBL 45. REPAIRED PER EA 55-201067. 2L72 4F RTA2NM 20041115000612004111500061WP 2004 11 15 0401511232 120040907A2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501WP CARGO BAY FALSE INDICATIONA NWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01232NW 46961 EN ROUTE TO LGW AT FL370, NR 1 FORWARD CARGO SMOKE DETECTOR LIGHT ILLUMINATED. PERFORMED COM PROCEDURE AND LIGHT EXTINGUISHED. FLIGHT DIVERTED TO PIK. DURING DESCENT, BOTH FIRE BOTTLES WERE DISCHARGED. FLIGHT LANDED WITHOUT INCIDENT. INSPECTED FORWARD CARGO COMPARTMENT FOR EVIDENCE OF FIRE, NONE FOUND. REPLACED NR 1 AND NR 2 CARGO FIRE EXTINGUISHING BOTTLES. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20041115000652004111500065NM 2004 11 15 DL75K041017 120041105A2121216001003 FAN BOEING757 757232 1384965NM DISTRIBUTION BAYSEIZED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27694DA 29726 FL370 F/A`S REPORTED ELECTRICAL FUMES THROUGHOUT CABIN. COMPLETED SMOKE OR FUMES ELECT CHECK LIST AND DIVERTED TO PHX. FOUND RIGHT RECIRCULATION FAN SEIZED. REPLACED FAN. 2L72 4F RTA2NM 20041115000662004111500066NM 2004 11 15 SWAA043261 120041107A3350604222 BATTERY BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041115000692004111500069NM 2004 11 15 0401755810 120040925A2820316N310012 FUEL LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING PNL 611 CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01590NW4640 32990 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041115000702004111500070NM 2004 11 15 0401765814 120040926A2820316N310012 FUEL LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING PNL 611 CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01594NW3614 32994 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041115000802004111500080NM 2004 11 15 04FDEA03079 120041111A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FLOORBEAM CORRODED RBL 18, W/L 200. REPAIRED PER SRM 53-10-8 2L73 4F A3WE 20041115000832004111500083EU 2004 11 15 2004UALA00935 120041013A2133VFT300A1 OUTFLOW VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN PRESSURE FAULTY A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29419UA 487 UNABLE TO PRESSURIZE THE CABIN. REPLACED FAULTY SKIN AIR OUTLET VALVE. 2L72 4F4 FRTA28NM E40NE 20041115000982004111500098NM 2004 11 15 2004UALA00993 120041028A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 AFT MAIN CABIN FLOORBEAM CORRODED, BS 1660 MID-SECTION DOOR R-4, LOWER SILL. INSTALLED T-CAP SPLICE AND ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041115001132004111500113NM 2004 11 15 2004UALA00977 120041025A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 CABIN FLOOR LT CREASE BEAM INNER CHORD ANGLE CORRODED STA 676 TO STA 680, LBL 64. FABRICATED & INSTALLED NEW CHORD ANGLE. 2L72 4F4 FRTA2NM E17NE 20041115001272004111500127EU 2004 11 15 AWXA200401251 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 41 AND FS 42. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 41 TO FS 42; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001322004111500132 2004 11 15 2004UALA00970 420041024A3416 VIBRATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE ALTIMETER MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29569UA 26677 FLIGHT DIVERTED TO ORD WITH A STANDBY ALTIMETER VIBRATOR. 2L72 4F4 FRTA2NM E17NE 20041115001412004111500141NE 2004 11 15 AWXA200401135 220041017A75302607MK2 ACTUATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENGINE FAULTY A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28647AW153447116 762 ORD - ABORTED TAKEOFF - FLT 0738 - ON TAKEOFF AT ORD EN ROUTE FOR LAS, RECEIVED NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AT 65 KTS. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, ENGINE RUN OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF VSV ACTUATOR S/N 2607950 WAS NO FAULT FOUND. UNIT OPERATED PER MANUFACTURERS SPECS AT AMBIENT AND ELEVATED TEMPERATURES, RIG TEST ALSO FOUND NO DEFECTS. UNIT WAS OPENED TO CHECK FOR FUEL LACQUERING; NONE WAS FOUND, REASSEMBLED UNIT AND PERFORMED FINAL TEST IAW CMM 73-32-61. 2L72 4F4 FRTA28NM E40NE 20041115001432004111500143NM 2004 11 15 AWXA200401137 120041004A575465C267995 SKIN BOEING737 73733A 1384673NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, 2 EACH 3/4 INCH CRACKS WERE FOUND IN LOWER SKIN OF NR 1 SLAT BELOW OUTBOARD MAIN TRACK SLAT STA 355 - 357. MAINTENANCE CUTOUT DAMAGE IN NR 1 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, FIG 206. 2L72 4F RTA16WE 20041115001512004111500151WP 2004 11 15 04FDEA02939 120041015A5753 ROLLER DOUG DC10 DC1010 3022110WP ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE4660528032 46605 RIGHT WING INBOARD FLAP INBOARD MOST FORWARD TOP ROLLER IS WORN. REMOVED AND REPLACED RIGHT WING INBOARD FLAP INBOARD TRACK MOST FORWARD TOP ROLLER I/A/W DC10-10 MAINTENANCE MANUAL 20-50-02-2 AND EA 8-5750-81490. REFERENCE NON-ROUTINE NR N00776. 2L73 4F A22WE 20041115001562004111500156NM 2004 11 15 04FDEA02933 120041014A5730ARB2889502 SKIN PANEL DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 FOUND WITH APPROXIMATELY 13 INCH CRACKED. RIGHT WING LEADING EDGE SKIN PANEL W/ STA XORS = 799 CRACKED . REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-79779, TITLE: WINGS, BASIC WING STRUCTURE, RIGHT LEADING EDGE SKIN CRACK BY SLAT NR 7. 2L73 4F RTA22WE 20041115001572004111500157NM 2004 11 15 04FDEA02934 120041014A5347ADA83891 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48481 MAIN CARGO DECK STA 810 LEFT REFERENCE X= 47.5 SEAT TRACK DAMAGED. MAIN CARGO DECK STA 810 LEFT REFERENCE X= 47.5 DAMAGED SEAT TRACK SECTIONAL CUT-OUT AND REMOVED BETWEEN STA 765 AND STA 825 AND SECTIONAL REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20041115001622004111500162EU 2004 11 15 04FDEA03013 120041103A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 AREAS OF CORROSION ON SCALLOP HOLES NR 3 LEFT SEAT TRACK AS MARKED. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 51-72-10 AND 51-40-21. 2L72 4F RTA35EU 20041115001762004111500176NM 2004 11 15 04FDEA02623 120040903A5753ARC198414 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INCH, AND REPAIRED AS PER EA NR 1-5750-80340, TITLE: WINGS, RT OUTBOARD FLAP, I/B (FLAP SIDE) BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041115001832004111500183NM 2004 11 15 AWXA200401008 120040911A335020121 CHARGER BOEING737 7373G7 1384595NM EMERGENCY LIGHT FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, FOUND THE AFT GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER AT BS 968 LT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041115001862004111500186NE 2004 11 15 AWXA200401011 220040910A7300MS9967016 PACKING BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 1 ENGINE TORN A AWXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP28182AW 22649 P708359B EN ROUTE, NR 1 ENG SHUTDOWN AT 27,000 FT, ATTEMPTED RESTART WITHOUT SUCCESS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX FOUND SEALS ON PRESS DUMP VALVE INPUT FUEL LINE TORN & LEAKING. REPLACED SEALS, ENGINE RUN OPERATIONAL CHECK WAS GOOD. MX R/R LT FUEL S/O VALVE & ACT ASSY IAW AWA, OPS CHK GOOD. INSPECT OF GATE VALVE ASSY FOUND UNIT TO OPERATE NORMALLY. A GOUGE FOUND IN 1 OF BLADE SEAL HOUSINGS, DAMAGE NOT SUFFICIENT ENOUGH TO HAVE CAUSED PROBLEM. UNIT O-HAULED IAW CMM, & MODIFIED PER SB 61163-28-03. TEST & DISASSY OF FUEL S/O VALVE ACTUATOR FOUND NUMEROUS DISCREP, BUT VALVE OPERATED NORMAL. UNIT O-HAULED IAW CMM. ENG IN FLT SHUTDOWN ATTRIBUTED TO TORN SEALS ON PRESS DUMP VALVE INPUT FUEL LINE. 2L72 4F4 FRTA16WE E2EA 20041115002032004111500203NM 2004 11 15 04FDEA02632 120040903A5730ARB74063 PANEL DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LEFT WING UPPER SURFACE XIS=247 FWD SIDE FOUND CORROSION. LEFT WING UPPER SURFACE XIS=247 FWD SIDE REPAIRED AS PER EA NR 1-5710- 81539, TITLE: WINGS LT WING UPPER SURFACE, CORROSION BLEND OUT AT XORS 144.25. 2L73 4F RTA22WE 20041115002122004111500212WP 2004 11 15 04FDEA02636 120040903A3260 DOWNLOCK SENSOR DOUG DC10 DC1010F 3022111WP MLG MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO2568054 47808 AFTER RAISING THE GEAR HANDLE DURING TAKEOFF, THE RIGHT MAIN GEAR INDICATED UNSAFE (RED) ON BOTH PANELS. RECYCLED THE GEAR IAW THE QRH. AFTER RAISING THE GEAR THE SECOND TIME,THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON FOR ABOUT ONE MINUTE, THEN WENT OUT. FACT, R/R RIGHT HAND MLG DOWN LOCK PROXIMITY SENSORS D1-43 AND D1-82 PER DC10 MM 32-61-03-2. SYSTEM OPS CHECK NORMAL. OK FOR SERVICE. 2L73 4F A22WE 20041115002142004111500214NM 2004 11 15 AWXA200401060 120040826A53206546912 FLOOR SUPPORT BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT UPPER "T" CAP BETWEEN BS 986.5 AND BS 1016, LBL 6 TO LBL 18. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 986.5 TO BS 1016, LBL 6 TO LBL 18; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR SUPPORT IAW DWG 65-17688. 2L72 4F RTA16WE 20041115002292004111500229WP 2004 11 15 04FDEA02099 120040717A5751NRC6041503 FITTING DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25359FE 46635 WINGS-OUTBD AILERON, ACTUATOR ATTACH FITTING REWORK. CLOSING ACTION ON 07/16/04. ON N/R S00014, COMPLIED WITH EA8-5750-79553. 2L73 4F RTA22WE 20041115002302004111500230WP 2004 11 15 04FDEA02639 120040904A5753 ROLLER DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 LEFT WING INBOARD FLAP INBOARD TRACK 1 EACH AFT UPPER SMALL ROLLER IS PITTED. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK AFT UPPER SMALL LOAD ROLLER IAW FEDEX EA> 8-5750-81449. ORIGINAL COPY OF EA 8-5750-81449 IS ATTACHED TO FEDEX N/R N00910, REFERENCE N/R N00925. 2L73 4F RTA22WE 20041115002342004111500234EU 2004 11 15 AWXA200401216 120041017A5315D5347218820200 FLOORBEAM AIRBUS320 A320231 3930325EU CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED SECTION BEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115002352004111500235EU 2004 11 15 AWXA200401217 120041018A5347D53371112001 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON RT CABIN SEAT TRACK Y1292 BETWEEN FR 41 AND FR 47. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y1292 FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115002362004111500236NM 2004 11 15 AWXA200401016 120040904A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, THE FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERIES WOULD NOT CHARGE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK OF FLASHLIGHT WAS GOOD. 2L72 4F RTA28NM 20041116000012004111600001NM 2004 11 16 AWXA200401017 120040905A5330654576777 SKIN BOEING737 7373G7 1384595NM FUSELAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK, A 1/2 INCH CREASE WAS FOUND IN EXTERIOR FUSELAGE SKIN AT BS 405, BETWEEN STR 16 LT AND STR 17 LT. MAINTENANCE CUTOUT DAMAGE IN EXTERIOR FUSELAGE SKIN AT BS 405, FROM STR 16 LT TO STR 17 LT. PERFORMED A HFEC INSPECTION OF THE CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 226, PG 291-293. 2L72 4F RTA16WE 20041116000022004111600002NM 2004 11 16 04FDEA02840 120040928A5315 FLOORBEAM BOEING727 727277 138408SNM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 BFM CLOSER C/W WITH EA7-5321-82044 FUSELAGE, FLOORBEAM UPPER CORD REPAIR STA 950 AT BL 21.0 ENT BY: 497236 RPT BY: 497236 FACT 28SEP04 23:10. BFM U COMPLIED WITH EA 7-5321-82044. REMOVED CORROSION, TREATED AREA AND INSTALLED REPAIR ANGLE ENT BY: 497236 RPT BY: 497236. 2L73 4F RTA3WE 20041116000032004111600003NM 2004 11 16 AWXA200401222 120041104A3397BMS13311122 WIRE BOEING737 7373G7 1384595NM SEAT ROW 5 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28160AW 23782 DURING 8-DAY CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT INOPERATIVE. MAINTENANCE RE-TERMINATED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116000042004111600004NM 2004 11 16 AWXA200401223 120041104A33501012721 LIGHT BOEING737 737277 1384570NM SEAT ROW 13 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 DURING 8-DAY CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT ROW 13 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116000052004111600005NM 2004 11 16 04FDEA02841 120040929A5313AFA7093501 LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 CENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902 FOUND WITH CORROSION CRACK. CENTER CARGO, LONGERON 39R LOCATED BETWEEN STA Y= 1887 TO Y= 1902. REMOVED PER SRM 53-10-00 VOLUME I. NEW LONGERON FABRICATED PER DRAWING NR: AFA7093. REPAIR SPLICE REWORKED PER SRM 51-31-01 VOLUME II. FABRICATED LONGERON AND REPAIR SPLICE. INSTALLED PER SRM 53-10-00 VOLUME I. 2L73 4F RTA22WE 20041116000062004111600006NM 2004 11 16 04FDEA02842 120040929A5320BAC14981416 CHANNEL BOEING727 727277 138408SNM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 FWD LWR CARGO A/C COMPT STR 27L BETWEEN F/S 720F TO 740, PROTECTIVE FINISH PEELING AND MINOR SURFACE CORROSION IN HAT CHANNEL. REMOVED CORROSION IAW SRM 51-10-6 PG 6, PARG 4. ORIG MAT .095, AFTER REWORK .075 .020 MAT LOSS, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 PG 1, DETAIL I. REPAIRED HAT CHANNEL IAW SRM 53-10-3 MAT ID HAT CHANNEL BATCH NR 0000032659/MST0000666. REMOVED DAMAGED SECTION IAW SRM 53-10-3. HAT SECTION FABRICATED FROM (BAC1498-147/16), SPLICES FABBED FROM (BAC1498-131/16). 2L73 4F RTA3WE 20041116000072004111600007EU 2004 11 16 04FDEA02843 120040929A5320 THRESHOLD AIRBUS310 A310203 3930313EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25410FE 356 AFT PIT AREA (BULK) THRESHOLD BETWEEN FS 67 AND FS 69 FOR BULK DOOR CUTOUT HAS CORROSION ON FITTINGS UNDER AND AROUND NUT PLATES AND FASTENERS. REMOVED CORROSION MATERIAL LOSS IN AREA MINUS LONGITUDINAL SECTION IS .008 INCH AND FOUND TO BE IN LIMITS IAW SRM 51-74-10 AND 53-17-13. REMOVED LONGITUDINAL SECTION DUE TO OUT OF LIMITS MATERIAL LOSS NOTED .019, AND REPLACED AND TREATED AREAS AND SECTION ALL IAW SRM 51-74-10, 53-17-13, AND 51-40-20. 2L72 4F RTA35EU 20041116000082004111600008NM 2004 11 16 AWXA200401224 120041104A2560P2070001101 FLASHLIGHT BOEING757 7572S7 1384962NM ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28906AW 23568 FLIGHT CREW REPORTED THE LT FORWARD ENTRY WAY EMERGENCY FLASHLIGHT HAD A LOW BATTERY. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY AT THE LT FORWARD ENTRY WAY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20041116000092004111600009NM 2004 11 16 04FDEA03000 120041030A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 1372-1376 LBL 47. WORN SEAT TRACK ON CABIN AT STA 1372-1376, LBL 47 REPAIRED AS PER SRM 53-70-00, SHEET 1, FIG 1 VOL II. 2L73 4F RTA22WE 20041116000122004111600012EU 2004 11 16 AWXA200400982 120040814A5320D531122242010500FITTING AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON FITTING AT FORWARD FACE OF FS 20, ABOVE R-1 DOOR LOWER AFT GIRT FITTING Y1730 RT. MAINTENANCE REMOVED CORRODED FITTING AT FS 20, Y1730 RT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000142004111600014EU 2004 11 16 AWXA200400984 120040815A5320D5348004320500 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON R-2 DOOR LOWER SHAPE SILL BETWEEN FS 66 AND FS 68. MAINTENANCE CUTOUT DAMAGED AREA OF R-2 DOOR SHAPE SILL AT Y1732 RT, FROM FS 66 TO FS 68; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG 201, PG 207-213. 2L72 4F RTA28NM 20041116000172004111600017NM 2004 11 16 AWXA200400987 120040902A3242214571 BRAKE ASSY BOEING757 7572S7 1384962NM NR 3, RT MLG DAMAGED A AWXAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP28902AW204203664 23322 AFTER ARRIVAL IN PHX EN ROUTE FROM LAS, FLIGHT CREW NOTICED HYDRAULIC FLUID WAS LOW ON QUANTITY GAUGE, FURTHER INSPECTION REVEALED DAMAGE TO NR 3 BRAKE ASSEMBLY. IT APPEARS BRAKE ROD DISCONNECTED CAUSING NR 3 BRAKE TO ROTATE SHEARING HYDRAULIC LINES AND TEMPERATURE SENSOR WIRES. NR 3 BRAKE ROD CONTACTED THE NR 7 BRAKE ROD DIRECTLY BEHIND IT CAUSING THE NR 7 BRAKE ROD TO BEND. MAINTENANCE REMOVED AND REPLACED THE NR 3 BRAKE ASSEMBLY IAW T/C R4M32604. REPLACED NR 3 AND NR 7 BRAKE RODS IAW BMM 32-11-19-4, AND REPLACED WIRING AND CONDUIT FROM JUNCTION BOX TO CONNECTOR D022656. REMOVED AND REPLACED HYDRAULIC FLEX LINE PER T/C R4M32604, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTA2NM 20041116000182004111600018NM 2004 11 16 AWXA200400988 120040826A532065524576 DRIP TRAY BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON BULKHEAD FLOOR WEB AT BS 1035, RBL 5, AFT OF RT AFT LAVATORY. MAINTENANCE REMOVED CORRODED BULKHEAD FLOOR WEB AT BS 1035, RBL 5; FABRICATED A NEW REPLACEMENT FLOOR WEB AND REINFORCEMENT STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02, PARA. 6B. 2L72 4F RTA16WE 20041116000192004111600019EU 2004 11 16 AWXA200400958 120040815A5347D5347220920100 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK Y765 RT, FORWARD OF FS 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK Y765 RT AT FS 66; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 18. 2L72 4F RTA28NM 20041116000202004111600020EU 2004 11 16 AWXA200400959 120040826A5320D5347112420000 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK, A 3 INCH CRACK WAS FOUND ON AFT SHEAR PLATE AT STR 24 LT, BETWEEN FS 69 AND FS 70. MAINTENANCE REMOVED CRACKED AFT SHEAR PLATE AT STR 24 LT, FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000212004111600021EU 2004 11 16 AWXA200400960 120040821A5321D5367180500500 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF R-2 DOOR FLOOR PANEL 262 FF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 262FF IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041116000242004111600024EU 2004 11 16 AWXA200400963 120040820A5320D5347112420000 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON AFT SHEAR PLATE AT STR 24 RT, BETWEEN FS 69 AND FS 70. MAINTENANCE REMOVED CORRODED AFT SHEAR PLATE AT STR 24 RT, FROM FS 69 TO FS 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000272004111600027NM 2004 11 16 AWXA200401078 120040918A5321D5367324200000 FLOOR PANEL AIRBUSA319 A319132 3930340NM CARGO BAY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, THE EDGE OF AFT CARGO COMPARTMENT FLOOR PANEL 151VF WAS FOUND DELAMINATED BETWEEN FS 53 AND FS 56. MAINTENANCE REMOVED AFT CARGO COMPARTMENT FLOOR PANEL 151VF, AND FABRICATED A NEW REPLACEMENT PANEL IAW A319 SRM 53-02-00, FIG. 209. 2L72 4F RTA28NM 20041116000292004111600029WP 2004 11 16 04FDEA02910 120041011A5753ARC01541 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 3 HAS CORROSION IN BORE. REMOVED CORROSION IAW DACCMM 57-44-07. BEGINNING BORE 2.5850 INCH FINAL 2.626 INCH MATERIAL. REMOVED .041 INCH. FABRICATED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81473. ACCOMPLISHED MPI IAW DPS 4.704. CAD PLATED BUSHING IAW DACCMM 57-44-07. ALODINED AND PRIMED BORE IAW DC10 SRM 51-21-01 VOLUME II. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-07. 2L73 4F RTA22WE 20041116000312004111600031EU 2004 11 16 AWXA200401040 120040919A3397ABS0374A24 WIRE AIRBUS320 A320232 3930326EU SEAT ROW 15 L/H BACKED OUT A AWXAK NONE O OTHER ININSP/MAINT 1 WP28651AW 866 DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE FOUND A WIRE PULLED FROM CONNECTOR 7260VC), RE-PINNED WIRE, OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20041116000342004111600034NM 2004 11 16 04FDEA02845 120040929A2820AAL72891 LINE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO25585FE 48481 CENTER CARGO COMPARTMENT, LT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, A CRACKED OF 1.1/8 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1781, 1 1/8 INCH CRACKED AT THE FUEL SHROUD LINE. REPAIRED PER FEDEX EA #1-2822-79763, FUEL SYSTEMS, FUEL SHROUDS AND DRAINS, CRACK REPAIR ON TUBE FOR TAIL TANK. 2L73 4F RTA22WE 20041116000362004111600036NM 2004 11 16 04FDEA02847 120040929A2930 INDICATOR BOEING727 727233 138408ANM HYD SYSTEM FAILED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25278FE1019910199 22345 HYDRAULIC SYSTEM A QUANTITY INDICATOR WENT TO 0.2 GALLONS ON FLAP RETRACTION. QRH PROCEDURES RECOVERED QTY TO 1.2 GALLONS. ENT BY: 014562 RPT BY: 241937 FACT 29SEP04 11:20, MEM R REMOVED AND REPLACED INDICATOR IAW 727-200 M /M 31-00-011-4. OPS CHECK GOOD. ENT BY: 014562 RPT BY: 014562 R/I 29SEP04 11:21MEM R R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG B711-1 POS P1 SRL 742 TAG 663103 ON MFG B711-1 SRL B967924, TAG 477437. 2L73 4F RTA3WE 20041116000372004111600037NM 2004 11 16 AWXA200401139 120040930A5330654577810 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN LOWER FORWARD RADIUS OF R-2 DOOR LOWER HINGE CUTOUT AT BS 951, ST 16 RT. MAINTENANCE CUTOUT DAMAGE IN R-2 DOOR LOWER HINGE CUTOUT AT BS 951, ST 16 RT; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG 207. 2L72 4F RTA16WE 20041116000382004111600038NM 2004 11 16 AWXA200401140 120041001A52105007945438 BEAM BOEING737 73733A 1384673NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 1 1/8 INCH CRACK WAS FOUND IN L-1 DOOR BEAM AT LOWER FORWARD CORNER AT BS 313, STR 16 LT. MAINTENANCE CUTOUT DAMAGE IN L-1 DOOR BEAM AT LOWER FORWARD CORNER BS 313, STR 16 LT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, FIG 1. 2L72 4F RTA16WE 20041116000412004111600041NM 2004 11 16 AWXA200401143 120041015A5320654581238 SPLICE PLATE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 5/16 INCH CRACK WAS FOUND IN SPLICE PLATE AT BS 348, BETWEEN STR 20 RT AND STR 21 RT. MAINTENANCE REMOVED CRACKED SPLICE PLATE AT BS 348, STR 20 - 21 RT; FABRICATED A NEW REPLACEMENT SPLICE PLATE PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, & 8. 2L72 4F RTA16WE 20041116000462004111600046NM 2004 11 16 04FDEA03048 120041108A5310 SHEAR TIE BOEING727 727247 138408FNM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25233FE 21327 FOUND THE SHEAR TIE AT BS 380 BETWEEN STR 15 AND 16 TO REQUIRE REPLACEMENT DUE TO PREVIOUS CARGO NET BARRIER STRAP. INSTALLATION TO EXTEND UNDER THE FRAME AS OPPOSED TO OVER AS PER VENTURA AEROSPACE DWG 2987. REPAIRED PER SRM 53-10-4 FIG 11. 2L73 4F A3WE 20041116000472004111600047NM 2004 11 16 04FDEA02967 120041022A5531AMC7101502 SPAR CAP DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE FOUND CORRODED. EMPENNAGE, UPPER VERTICAL STAB AT FWD CTR SPAR APPROX BETWEEN ZFR 300 TO 340 RT SKIN EXTERIOR SURFACE CORROSION AREA REPAIRED AS PER FEDEX EA NR 1- 5530-81579, TITLE: STABILIZERS, UPPER VERTICAL STABILIZER, RT FORWARD CENTER SPAR CAP, CORROSION REPAIR. 2L73 4F RTA22WE 20041116000482004111600048NM 2004 11 16 04FDEA02946 120041018A5753ARC74901 FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT WING, INBOARD FLAP VANE INBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE: WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT HAND INBOARD FLAP VANE ATTACH FITTING REWORK. 2L73 4F RTA22WE 20041116000502004111600050NM 2004 11 16 04FDEA02948 120041018A5310 SHEAR TIE BOEING727 727225 1384077NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25461FE 22548 CORROSION ON SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R. REPAIRED SHEAR TIE BS 950F BETWEEN STRS 29R AND 28R PER SRM 53-10-4 FIG 15. 2L73 4F A3WE 20041116000512004111600051NM 2004 11 16 AWXA200401144 120041005A5313BAC1498155 STRINGER BOEING737 73733A 1384673NM CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON SIDE OF STRINGER 28 RT, BETWEEN BS 312 AND BS 322. MAINTENANCE CUTOUT DAMAGED SECTION OF STRINGER 28 RT, FROM BS 312 TO BS 322; FABRICATED A REPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201. 2L72 4F RTA16WE 20041116000532004111600053NM 2004 11 16 04FDEA03016 120041104A5313BAC1498138 STRINGER BOEING727 72722 1384002NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 STR L23 DAMAGED AT BS 376 TO 388. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 20041116000562004111600056NM 2004 11 16 AWXA200401024 120040905A5321D5367180500500 FLOOR PANEL AIRBUSA319 A319132 3930340NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF R-2 DOOR FLOOR PANEL 262 FF. MAINTENANCE REMOVED AND REPLACED R-2 DOOR FLOOR PANEL 262 FF IAW T/C C1D25310. 2L72 4F RTA28NM 20041116000572004111600057NM 2004 11 16 AWXA200401025 120040905A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319132 3930340NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF FLOOR PANEL 261 FF. MAINTENANCE REMOVED AND REPLACED R-2 FLOOR PANEL 261 FF IAW T/C C1D25310. 2L72 4F RTA28NM 20041116000592004111600059NM 2004 11 16 AWXA200401158 120040914A575465C267933 SKIN BOEING737 73733A 1384673NM NR 4 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, 4 EACH 3/8 INCH CRACKS WERE FOUND IN NR 4 SLAT LOWER SKIN BETWEEN SLAT STA 42 - 78. MAINTENANCE CUTOUT DAMAGE IN NR 4 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, FIG 206. 2L72 4F RTA16WE 20041116000602004111600060EU 2004 11 16 AWXA200401207 120041018A5347D57130147200 SEAT TRACK AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 6 PLACES ON RT CABIN SEAT TRACK Y765 BETWEEN FS 36 AND FS 41. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y765 FROM FR 36 TO FR 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 12-18. 2L72 4F RTA28NM 20041116000622004111600062WP 2004 11 16 04FDEA02986 120041025A5320AGA30681 SPLICE DOUG DC10 DC1010 3022110WP ZONE 100 DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING TO MODIFICATION AND TRANSITION CHECK, AFT CARGO COMPT FOUND AT STA 1821-1841 STR 36 RT WITH EXISTING REPAIR. REPLACE LONGERONS AND SPLICES PER SRM 51-33-01 PAGE 34-47, PART REPLACED:AGA3068-1, AGA3068-501, AFA3114-503, AFA3114-504. 2L73 4F A22WE 20041116000642004111600064 2004 11 16 2004UALA00984 420041025A2565 PROXIMITY SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE L1 DOOR GIRT BARMALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29578UA 26694 DOOR 1L SLIDE LIGHT WILL NOT COME ON WHEN DOOR IS ARMED. REPLACED DEFECTIVE GIRT BAR PROXIMITY SENSOR. 2L72 4F4 FRTA2NM E17NE 20041116000652004111600065NE 2004 11 16 AWXA200401225 220041104A7261QA05954 FILTER AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE CLOGGED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28625AW 064 ON TAKEOFF AT LAS EN ROUTE TO PHX, WHEN TAKEOFF POWER WAS APPLIED RECEIVED NR 2 ENGINE OIL FILTER CLOG MESSAGE ON ECAM, OIL PRESSURE WAS VERY HIGH, REJECTED TAKEOFF LESS THAN 40 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL SCAVENGE FILTER IAW AMM 79-22-44-000-010, ENGINE RUN OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E311NE 20041116000662004111600066WP 2004 11 16 04FDEA02901 120041011A5730ARB09391 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 LEFT WING SKIN LOWER SURFACE IS CORRODED, STATION XORS 799 APPROX 19 INCHES AFT OF FORWARD SPAR CAP. SKIN HAS SMALL AMOUNTS OF PITTING. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW EA 8-5710-81493. ORIGINAL MATERIAL THICKNESS IS .096 INCH, REMOVED .028 INCH AT FORWARD SPOT LEAVING .068 INCH, REMOVED .024 INCH AT AFT SPOT LEAVING .072 INCH REMAINING. FLAP PEENED AREAS IAW MD10 CMM 20-11-01. ALODINE AND PRIMED IAW DC10 SRM 51-21- 01 VOL II. REINSTALLED FASTENERS IAW DC10 SRM 51-33-01 VOL II. LEAKED CHECKED IAW MD10 MM 28-00-02-2 WITH NO LEAKS NOTED. REFERENCE NON-ROUTINE N00687. 2L73 4F RTA22WE 20041116000682004111600068NM 2004 11 16 2004UALA01006 120041101A2781 SWITCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 9 SLAT OUT OF RIG A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29653UA 25391 DIVERTED TO JFK DUE TO LEADING EDGE FLAP INDICATION PROBLEM. FOUND NR 9 LE SLAT SWITCH S303 OUT OF RIG. SHIMMED SWITCH TO ACHIEVE PROPER SWITCH TARGET GAP. 2L72 4F4 FRTA1NM E24NE 20041116000692004111600069NM 2004 11 16 2004UALA01014 120041030A2120 DUCT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MIX CHAMBER LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29318UA 23950 FUSELAGE SKIN LOCATED DIRECTLY BELOW DUCT ASSY SHOWS SIGNS OF PEELED PAINT DUE TO MIX CHAMBER DUCT ASSY HOT AIR LEAK. MIX MUFF DUCT OF DUCT ASSEMBLY LOCATED IN MIX CHAMBER AIR DISTRIBUTION BAY AT APPROXIMATE STA 540, BL 0 BLOWN CAUSING HOT AIR TO ESCAPE AND DAMAGE THE STRUCTURE BENEATH.REPAIRED FUSELAGE SKIN FROM FS 520 - 526 BETWEEN STRINGER 26L AND 27L AND REPLACED DUCT ASSEMBLY. 2L72 4F4 FRTA16WE E2GL 20041116000712004111600071EU 2004 11 16 04FDEA02931 120041014A2133 OUTFLOW VALVE AIRBUS310 A310203 3930313EU CABIN PRESSURE INOPERATIVE A FDEAA UNSCHED LANDING S AFFECT SYSTEMS NRNOT REPORTED 1 SO25409FE 273 NR 2 SYSTEM FWD AND AFT OUTFLOW VALVES REMAINED FULLY OPEN. ENT BY: 105221 RPT BY: 011927 MEL 14 OCT 04 04:44, LAX R ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-02-A CATEGORY: C EXPIRATION: 24OCT04 "MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY) INOP. VALVES DEACTIVATED IN CLOSED POSITION, OR VALVE REMOVED, BLANKING PLATE INSTALLED. NR 2 FWD AND AFT OUTFLOW VALVES INOPERATIVE: DEACTIVATED CLOSED. PERFORMED MXP. C/0211633, ENT BY: 105221 RPT BY: 105221. 2L72 4F RTA35EU 20041116000732004111600073WP 2004 11 16 04FDEA02917 120041011A5340ACA3039511 FITTING DOUG MD10 MD1010F 3022112WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 CRACKED LONGERON END FITTING, AFT OF RIGHT HAND AIR CONDITIONING DOOR CUTOUT, LONGERON 35R, STA 535. REMOVED END FITTING IAW FEDEX SRM 51-35-01 VOLUME II PAGE 1, AREA ALODINED AND TREATED IAW FEDEX DC10 SRM 51-21-01 VOLUME II PAGE 1, RECEIVED NEW END FITTING P/N ACA3039-511CLIP LONG END; PO 462215.1;LOCATED AND DRILLED HOLES IAW FEDEX DC10 SRM51-35-01 VOLUME II PAGE 1. INSTALLED NEW END FITTING IAW FEDEX DC10 SRM 51-35-01 VOLUME II PAGE 1 AND 51-33-01 VOLUME II PAGE 1. 2L73 4F RTA22WE 20041116000762004111600076NM 2004 11 16 04FDEA02922 120041012A5330 SKIN BOEING727 727225 1384077NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25461FE 22548 CORROSION ON INNER SKIN BS 720C LBL 5 WL 136. BLENDED CORROSION ON INNER SKIN AT BS 720C BL 0 AND ON SHEARTIE BS 720C RBL 5 - LBL5 W/L 136. BOTH AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1 AND 53-30-1 FIG 1. FABRICATED REPLACEMENT SHEARTIE BAC1490-2785, 707556X.050 INCH NR 563248. INSTALLED REPAIR BS 720C RBL5 - LBL 5 PER SRM 53-10-4, FIG 15. REMOVED DAMAGED SECTION OF INTERSKIN, FABRICATED REPAIR PLATE 2024T3X.125 NR 525155 AND INSTALLED REPAIR BS 720C BL 0 W/L 136 PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 20041116000772004111600077NM 2004 11 16 04FDEA02192 120040726A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25626FE 48445 DURING PASSENGER TO FREIGHT CONVERSION, THE APPLICATION FEDEX EO 1-5510-7- 5000C2 (S/B 55-023) THE FOLLOWING BARREL NUT BORE HOLES WERE OUT LIMITS PER FEDEX EO (A.D.2003-22-8) REQUIRE 8110 APPROVAL: HOLES: 5 RT; 14LT: 23 LT; 28 LT; 28RT; 34 LT; 34RT; 35RT; 35LT; AND 36LT. STABILIZER HORIZONTAL, BARREL NUT BORE REWORK/REPAIR PER EA 1-5510-77052 FEDEX RELEASE DATE 07/23/04. 2L73 4F RTA22WE 20041116000782004111600078EU 2004 11 16 04FDEA02193 120040726A2612CG7PO SMOKE DETECTOR AIRBUS300 A300F4605R 3930327EU CARGO BAY INOPERATIVE A FDEAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO25669FE 774 AFTER T/O AFT AND BULK SMOKE ECAM ALERT, AIRBORNE ABORT BACK TO MEM, FOLLOWED ECAM PROCEDURES. ENT BY: 029496 RPT BY: 118583 MEL 26-16-01: FWD, AFT AND BULK) ALL SMOKE DETECTION SYSTEMS INOP. NO CARGO IS TO BE CARRIED WITH AFFECTED LOWER DECK COMPARTMENTS. MEM R TROUBLESHOT PER TSM 26-16-00 FIG 102, NO FAULTS NOTED PERFORMED ADJUSTMENT TEST PER MM 26-16-00-5. NO FAULTS NOTED. REPLACED ALL FOUR AFT AND BULK SMOKE DETECTORS PRECAUTIONARY PER MM 26-16-11. OPS CHECK OK. 2L72 4F RTA35EU 20041116000792004111600079NM 2004 11 16 AWXA200401185 120041003A53306545765602 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 MCN - MAJOR REPAIR - DURING C-18 CHECK A 4 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 500C+5, STR 10 RT JUST ABOVE LAP SEAM. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 500C+5, STR 10 RT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 3 EACH FILLERS, A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20041116000802004111600080NM 2004 11 16 AWXA200401186 120041027A53302024T3050 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING 4-DAY CHECK, A 1 7/8 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 24 LT. MAINTENANCE CUTOUT CRACK IN FUSELAGE SKIN AT BS 727E, STR 24 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20041116000822004111600082NM 2004 11 16 04FDEA02977 120041022A5753ARC7480501 TEE FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, INBOARD AFT HOLE CORRODED AND OUTBOARD HOLE (03 OFF) CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. RIGHT HAND WING, INBOARD FLAP VANE INBOARD SUPPORT FITTING, REMOVED AND REPLACED AS PER AMM 27-50-24 FUNCTIONAL TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-00-860-801. 2L73 4F RTA22WE 20041116000842004111600084NM 2004 11 16 AWXA200401189 120041002A53306545765100 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 1/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 500C+5, STR 10 LEFT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 500C+5, STR 10 LT AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-04301-ES2. 2L72 4F RTA16WE 20041116000852004111600085NM 2004 11 16 AWXA200401177 120041028A2910AE2463921G0181 HOSE AIRBUSA319 A319132 3930340NM RT MLG DOOR ACT RUPTURED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28804AW 1043 AFTER TAKEOFF FROM BOS EN ROUTE TO LAS, GREEN HYDRAULIC SYSTEM LOST FLUID DURING LANDING GEAR RETRACTION, TURNED BACK TO BOS AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED HYDRAULIC FLEX LINE (A) AND FITTING AT R MAIN GEAR DOOR ACTUATOR AS PER STANDARD PRACTICES, LEAK AND OPERATIONAL CHECKS WERE GOOD. AS A PRECAUTION, REPLACED GREEN HYDRAULIC SYSTEM ENGINE DRIVEN PUMP AND 3 EACH FILTERS. SUPP PART INFORMATION HAS BEEN ADDED TO THIS SDR. PART NAME; SWIVEL, JOINT ASSY, MFG; EATON FLUID, P/N; AE84760Z, LOC; RT MLG DOOR ACTUATOR. 2L72 4F RTA28NM 20041116000902004111600090NM 2004 11 16 04FDEA03054 120041108A2997861555 RECEPTACLE CANNON DOUG MD11 MD11F 3023600NM AUX HYD PUMP BURNED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25608FE3564 3564 48548 NR 1 AUX HYD PUMP ELECTRIC POWER PLUG WAS FOUND BURNED. ENT BY: 500170 RPT BY: 500170 FACT 09NOV04 00:50, TPE R NR 1 AUX HYD PUMP PLUG REPLACED PER SMP AND PER MD-11, W/D 29-21-01 WIRING CHECKED NML. PRECAUTIONARY RCCB(B 1-625) AND NR 1 AUX HYD PUMP REPLACED ALSO. PREMATURE REMOVAL/INSTALLATION OFF MFG 861555. 2L73 4F RTA22WE 20041116000912004111600091NM 2004 11 16 04FDEA03055 120041109A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 MECHANICAL DAMAGE ON FLOORBEAM BS 720 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8 2L73 4F A3WE 20041116000932004111600093NM 2004 11 16 04FDEA03057 120041109A5714 PANEL DOUG MD11 MD11 3023602NM WING CENTER BOX CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25627FE 48446 DURING PASSENGER TO FREIGHT CONVERSION, FOUND STA 1179, STA 1189, 1219 AND 1229 X= -100 BEFORE INSTALL PANEL ASSY FOR CARGO MOD, FOUND MANY SEVERE CORROSION ON UPPER SKIN OF CTR BOX. REMOVED CORROSION, REMOVED FASTENERS, PERFORMED DYE CHECK RESIDUAL THICKNESS OUT LIMIT, PERFORMED SHOT PEEN THE REWORK AREA CHECK FOR CRACKS AND PROTECT ALODINE AND PRIME (REF EA 1-5710-81787). 2L73 4F RTA22WE 20041116000972004111600097NM 2004 11 16 04FDEA02743 120040919A5320S2645716 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 AFT CARGO, RT LONGERON SPLICE AT STA Y= 1855 TO Y= 1870, STRINGER 38R FOUND CRACKED. AFT CARGO, CRACKED RT LONGERON SPLICE AT STA Y= 1855 TO Y= 1870, STRINGER 38R REMOVED PER SRM 51-31-01 VOLUME I. SPLICE MACHINE, FABRICATED PER SRM 31-10-00 VOLUME I FIGURE 2. REPAIR SPLICE INSTALLED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041116000992004111600099NM 2004 11 16 04FDEA02745 120040919A5320AJC76711 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 AFT CARGO, WASTE TANK LEFT AT STAY = 1988, STRINGER END NR 8 FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK LEFT AT STAY = 1988, STRINGER END NR 8 SPLICE FITTING REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041116001012004111600101NM 2004 11 16 AWXA200401173 120041003A5313654577677 STRINGER BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON STRINGER 27 LEFT AT BS 987. MAINTENANCE REMOVED CORRODED SECTION OF STRINGER 27 LT FROM BS 967 TO BS 1006; FABRICATED A NEW REPLACEMENT STRINGER PER DWG 65-45776; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, 7, AND 8. 2L72 4F RTA16WE 20041116001032004111600103NM 2004 11 16 AWXA200401175 120041015A5347BAC1520792 SEAT TRACK BOEING737 73733A 1384673NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, CORROSION WAS FOUND ON INBOARD FLANGE OF SEAT TRACK AT BS 480, RBL 45. MAINTENANCE CUTOUT DAMAGED SECTION OF SEAT TRACK FROM BS 334 TO BS 500 AT RBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK AND A FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-52, FIG 202. 2L72 4F RTA16WE 20041116001042004111600104NE 2004 11 16 AWXA200401176 220041028A75301685MK7 ACTUATOR AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE NR 1 ENGINE VSV FAILED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28820AW15185 1397 ON TAKEOFF AT EWR EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "ENG 1 COMPRESSOR VANE FAILURE", REJECTED TAKEOFF AT 68 KTS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE VARIABLE STATOR VANE (VSV) ACTUATOR IAW T/C R5M75303, PERFORMED HIGH POWER ASSURANCE TEST, NR 1 ENGINE CHECKED GOOD. FUNCTIONAL TEST OF VSV ACTUATOR CONFIRMED REASON FOR REMOVAL. TEST REVEALED FAULTS WITH LINEAR VARIABLE DISPLACEMENT TRANSMITTER BONDING RESISTANCE AND VOLTAGE, PISTON VELOCITIES, AND INTERNAL LEAKAGE. DISASSEMBLY FOUND A DEFECTIVE TORQUE MOTOR, LACQUER LEVEL 3 ON FILTER SCREENS, AND SEVERAL WORN SEALS. REPLACED ALL DEFECTIVE PARTS, CALIBRATED VOLTAGES, CLEANED THE PISTON AND SLEEVE ASSEMBLIES, AND PERFORMED FINAL TEST IAW CMM. 2L72 4F4 FRTA28NM E40NE 20041116001072004111600107NM 2004 11 16 04FDEA02817 120040925A3020 RELAY DOUG MD11 MD11F 3023600NM ANTI ICE SYSTEM FAILED A FDEAE ENGINE SHUTDOWN S AFFECT SYSTEMS DEDESCENT 1 SO25623FE 48794 ENG 2 ANTI-ICE OFF LIGHT CAME ON AT TOP OF DESCENT WITH ENG ANTI-ICE SELECTED ON. UNABLE TO DIVERT CLEAR ICING SO SHUT DOWN ENG 2 AS A PRECAUTION. REPLACED RELAY R2-5527. SYSTEM CKS OK PER FIM 30-22-07. RAN NR 2 ENG AND PERFORMED ENGINE NOSE COWL ANTI-ICE SYSTEM CHECK PER JRH, NO DEFECTS NOTED, OK FOR SERVICE. 2L73 4F RTA22WE 20041116001082004111600108WP 2004 11 16 04FDEA02818 120040927A2820ARL0124109 TUBE DOUG DC10 DC1010F 3022111WP ZONE 400 CRACKED A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO2568058 46705 LEFT WING LEADING EDGE UPPER PYLON FUEL SAXAPHONE LINE IS CRACKED AT MOUNTING POINT. REMOVED, REPAIRED, REINSTALLED FUEL LINE IAW FEDEX EA 8-2822-77635. 2L73 4F A22WE 20041116001112004111600111NM 2004 11 16 AWXA200401115 120041011A2560P2070001214 FLASHLIGHT BOEING737 7373G7 1384595NM ZONE 900 INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28307AW 24634 DURING INSPECTION, THE AFT GALLEY UPPER EMERGENCY FLASHLIGHT FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY UPPER EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116001162004111600116EU 2004 11 16 AWXA200401241 120041023A5321D536114900100 FLOOR PANEL AIRBUS320 A320231 3930325EU PAX CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL 222FF. MAINTENANCE BLENDED OUT CORROSION ON PASSENGER CABIN FLOOR PANEL 222FF; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW ER 26-5312-00151-BA1. 2L72 4F RTA28NM 20041116001172004111600117EU 2004 11 16 AWXA200401242 120041017A5320D53471124200 SHEAR PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT SHEAR PLATE BETWEEN FS 69 AND FS 70, OUTBOARD OF BEAM Y1292. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE FROM FS 69 TO FS 70, AT Y1292; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2, 3, & 11. 2L72 4F RTA28NM 20041116001192004111600119NM 2004 11 16 04FDEA02667 120040910A5512ALC8101504 SKIN DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 8 RIGHT HAND BARREL NUT BORE, FOUND EXCEEDED LIMIT. CORROSION REPAIRED AS PER EA 1-5510-80349 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 8R, CORROSION REPAIR SB MD11-55-023 REV2 AND EO 1-5510-7-5000. 2L73 4F RTA22WE 20041110000902004111000090EU 2004 11 10 04FDEA03009 120041101A5347 SEAT TRACK AIRBUS300 A300F4605R 3930327EU FUSELGAE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25667FE 771 MDCC TRACK 3 R SECTION 27 INCHES TO RT OF CTR BETWEEN FR 74 AND FR 80 HAS 3 EACH AREAS OF CORROSION. (1) FR 74, (2) FR77, (3) FR 78, WHILE WORKING CORROSION FOUND 4EA ADDITIONAL AREAS OF CORROSION, REQUIRE REMOVAL AND EVACUATE. REMOVED AND REPLACED SEAT TRACK IAW A300- 600 SRM 51-72-10 AND 53-18-16 AND 53-12-16. REPLACEMENT SEAT TRACK WAS FABRICATED ON SRM N00559. 2L72 4F RTA35EU 20041110000912004111000091WP 2004 11 10 04FDEA03010 120041102A5730ARC0533505 PANEL DOUG DC10 DC1010 3022110WP ZONE 600 DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 RIGHT WING PANEL NR 661 EB IS DISBONDED AT FINGER DOUBLER AT MIDDLE FASTENER HOLE. REPAIRED BY FABRICATING AND BONDING NEW INNER AND OUTER SKIN, DOUBLER AND CORE IAW DAC DWG ARC0633 AND FEDEX EA 8-5710-81508. REMOVED AND REINSTALLED HINGED PANEL 661 EB SEAL RETAINER AND SEAL IAW DC10 SRM 51-35-01 AND 51-31-01 VOL 2. 2L73 4F A22WE 20041110001062004111000106NM 2004 11 10 SWAA043266 120041108A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM WEBS AT BS 400, LT AND BS 344 RT, CORRODED. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20041110001292004111000129WP 2004 11 10 04FDEA02890 120041007A5753ARC2512 HINGE DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 COMPLY WITH EA 8-5750-82050 RT INBOARD FLAP MOUNTED HINGE PIVOT BORE REPAIR. COMPLIED WITH EA8-5750-82050. 2L73 4F A22WE 20041110001312004111000131NM 2004 11 10 04FDEA02892 120041007A5510E01551075000 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 TO COMPLY WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORES IN EXCESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356). COMPLIED WITH FEDEX EA 1-5510-80350, TITLE: STABILIZERS - HORIZONTAL STABILIZER - MASTER EA - REWORK TO BARREL NUT BORES IN EXCESS OF FEDEX EO 1-5510- 7-5000 (BOEING SB MD11-55-023 REV 2.) FAA AD 2003-22-08 (AMENDMENT 39-13356). 2L73 4F RTA22WE 20041115000032004111500003WP 2004 11 15 AALA20041110 120041106A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217520A 49897 LAX - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5107 FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000042004111500004NM 2004 11 15 AALA20041114 120041011A5415 FITTING BOEING767 767323 1385205NM RT PYLON OVERSIZED A AALAK NONE O OTHER ININSP/MAINT 1 SW21382AN 25451 AFW - RIGHT HAND PYLON LINK LOWER BEARINGS ON BOTH SIDES LOOSE IN THE LOWER FITTINGS. VISUALLY CHECKED BORE HOLES FOR CRACKS. INSTALLED BEARINGS WET WITH BMS5 26 SEALANT IPC/DRAWING NUMBER 311T2287 14 AND 13. 2L72 4F RTA1NM 20041115000072004111500007WP 2004 11 15 AALA20041104 120041105A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217550 53032 BOS - CEILING EMERGENCY LIGHTS BETWEEN ROWS 8D AND 11D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 8D AND 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041115000132004111500013NM 2004 11 15 SCNA04015 120041108A3350 LIGHT BOEING737 737800* NM ROW 11&12 LOOSE A SCNAK NONE O OTHER UKUNKNOWN 1 GL15PHHZX 28248 CREW DISCOVERED EMERGENCY FLOOR TRACK LIGHTING LOOSE BETWEEN ROWS 11 & 12. MAINTENANCE SECURED LOOSE FLOOR TRACK LIGHTING AT ROWS 11 & 12, OPS CHECKED GOOD. 2L72 4F RTA16WE 20041115000252004111500025NM 2004 11 15 CALA0400706 120041109A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM L-2 DOOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW2779011 29859 THE EMERGENCY EXIT LIGHTS AT L-2 DOOR FAILED FUNCTIONAL CHECK. THE BATTERY PACK AT POWER SUPPLY M33099 WAS REPLACED IAW MM 33-51-06-960-802. 2L72 4F RTT00001SE 20041115000422004111500042NM 2004 11 15 SWAA043274 120041109A3350604222 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29653SW 28398 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041115000462004111500046NM 2004 11 15 SCNA0413 120040910A7932 B-NUT BOEING737 7378Q8 13844BXNM ENGINE OIL LOOSE A SCNAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15804SY 30689 ENGINE NR 2 OIL PRESSURE AND QUANTITY LOW IN FLIGHT. FOUND LOOSE LINE ON ENGINE TGB. TIGHTENED LINE AND LEAK CHECKED GOOD. 2L72 4F RTA16WE 20041115000552004111500055NM 2004 11 15 DL73S041016 120041104A5330654577416 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 INSPECTION OF THE FUSELAGE SKIN PER AD 2004-18-06 REVELED A 4 INCH LONG CRACK RUNNING ALONG THE BONDED DOUBLER EDGE AT STRINGER 18L AND FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 094729-14AD. 2L72 4F A16WE 20041115000672004111500067WP 2004 11 15 0401789956 120040928A2710 DRAIN DOUG DC9 DC931 3022065WP FUSELAGE CLOGGED A NWAAB EMER. DESCENT F FLT CONT AFFECTED CRCRUISE 1 GL01923RW 47183 AT CRUISE SPEED AND ALTITUDE, THE AIRCRAFT WOULD NOT TURN WITH AUTOPILOT. CREW CANCELLED AUTOPILOT AND WAS STILL UNABLE TO TURN THE CONTROL WHEEL BY HAND. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDED TO A LOWER WARMER ALTITUDE. CREW FELT A SNAP AND THEN CONTROL WAS MUCH EASIER BUT NOT NORMAL. BY FINAL APPROACH, AIRCRAFT CONTROL WAS NORMAL AND THE LANDING AT MSP WAS UNEVENTFUL. MAINTENANCE FOUND THE LEFT DRAIN FOR THE SLANT PANEL PARTIALLY CLOGGED AND THE RIGHT DRAIN COMPLETELY CLOGGED. UPON REMOVING THE CENTER FLOORBOARDS, FOUND WATER INSIDE OF SLANT PANEL BOX. REMOVED ALL DEBRIS AND WATER, CLEARED DRAIN LINES, AND LEAK CHECKED. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041115000782004111500078 2004 11 15 SWAA043249 420041108A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29791SW 27886 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041115000822004111500082NM 2004 11 15 AALA20041121 120041111A3350 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21682AA 25339 DFW - AFT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D IS BROKEN. REPLACED AFT EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041115000902004111500090NM 2004 11 15 04FDEA03068 120041110A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 MECHANICAL DAMAGE ON FLOORBEAM STA 700 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8 2L73 4F A3WE 20041115001022004111500102NE 2004 11 15 AALA20041082 220041029A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LEFT SHUTDOWN A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW21258AA 49288 709928 DURING CRUISE WITH NO WARNING CREW HEARD A BOOM & LT ENGINE STARTED TO ROLL BACK ACCOMPANIED BY SEVERE VIBRATION & SMOKE IN COCKPIT & CABIN. SMOKE DISSIPATED RAPIDLY, SEVERE VIBRATION CONTINUED TO LANDING, ENGINE CONTINUED TO ROTATE. LANDED WITHOUT INCIDENT. FIRE PERSONNEL REPORTED A LARGE FUEL LEAK. BOTH FIRE HANDLE AND ENGINE FUEL WERE OFF. LEAK STOPPED AFTER APPROX 20 MIN. VISUAL INSPECTION ON GROUND INDICATED MAJOR DAMAGE TO COMPRESSOR BLADES. ENGINE TIME APPROX 12 MINUTES. REPLACED LT ENGINE. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING PER MAINTENANCE MANUAL WORKCARD 21-92-12. REMOVED AND REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20041115001092004111500109NM 2004 11 15 2004UALA01003 120041029A5420 BRACE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 PYLON DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 NR 2 PYLON DIAGONAL BRACE HOLE BORES WERE FOUND MISLOCATED. ESTABLISHED CORRECT LOCATION OF DIAGONAL BRACE HOLE. MACHINED AND INSTALLED OVERSIZE BUSHING. 2L72 4F4 FRTA2NM E17NE 20041115001252004111500125EU 2004 11 15 AWXA200401249 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 38 AND FS 39. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 38 TO FS 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001292004111500129EU 2004 11 15 AWXA200401253 120041025A5347D53371110010000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 45 AND FS 46. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 45 TO FS 46; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001342004111500134NM 2004 11 15 2004UALA00972 120041024A5270 WARNING LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CARGO DOOR ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29656UA 25394 AFT CARGO DOOR EICAS MESSAGE. TRIED 4 TIMES, UNABLE TO DUPLICATE FAULT ON GROUND. 2L72 4F4 FRTA1NM E24NE 20041115001482004111500148NM 2004 11 15 04FDEA02619 120040903A5753ARC198413 BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING , O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. LEFT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.503 INCH, MATERIAL. REMOVED=0.006 INCH, REMAINING THICKNESS=0.497 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS, LT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041115001492004111500149NM 2004 11 15 04FDEA02620 120040903A5753ARC198413 BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. SNRM N0448: LT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4 ORIGINAL THICKNESS=0.514 INCH, MATERIAL REMOVED=0.009 INCH, REMAINING THICKNESS=0.505 INCH AND REPAIRED AS PER EA NR 1-5750-80344, TITLE: WINGS, LEFT OUTBOARD FLAP, I/B FLAP SIDE HINGE BRACKET PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041115001532004111500153NM 2004 11 15 04FDEA02671 120040910A5510ALC8103503 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 29 LEFT BARREL NUT BORE FOUND EXCEEDED LIMIT. SNRM N1061: CORROSION REPAIRED AS PER EA 1-5510-80355 HORIZONTAL STABILIZER. BARREL NUT BORE 29L. REWORKED BEYOND SB MD11-55-023 REV2 LIMIT. 2L73 4F RTA22WE 20041115001552004111500155NM 2004 11 15 04FDEA02932 120041014A5347ABA7680505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 FORWARD CABIN, MOST OUTBOARD LEFT SIDE SEAT TRACK AT APPROX STA 430-450 FOUND TOP SURFACES WITH CORROSION. SNRM N0083, FORWARD CABIN, STA 430-450 MOST OUTBOARD LEFT SIDE SEAT TRACK. CORROSION REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II AND SRM 51-33-01 VOL II.. 2L73 4F RTA22WE 20041115001582004111500158NM 2004 11 15 04FDEA02936 120041015A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 MAIN CARGO DECK STA Y= 132 RT SEAT TRACK X= -47.5 SEAT TRACK DAMAGED. MAIN CARGO DECK STA Y= 1321 RT SEAT TRACK X= -47.5 SEAT TRACK DAMAGED AREA, SECTIONAL CUT-OUT OF SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I BETWEEN STA 1321 AND STA 1361 OF RBL 47.5. 2L73 4F RTA22WE 20041115001602004111500160NM 2004 11 15 04FDEA03011 120041102A2910 LINE BOEING727 7272D4 138407UNM HYD SYSTEM LEAKING A FDEABH EMER. DESCENT DEACTIVATE SYST/CIRCUITS KSJFLUID LOSS AFFECT SYSTEMS WARNING INDICATION DEDESCENT 1 SO25287FE 21849 WHILE DESCENDING ON GLIDESLOPE, ELEVATOR LOW PRESSURE LIGHT FLICKERED, CROSS CHECKED WITH HYDRAULIC PANEL AND NOTICED "A" SYSTEM AT ABOUT 1 QT. C/W QRH PROCEDURES. ENT BY: 448879 ADDED MPN BACH8A06NN0300T CPN 0109172 QTY 1 HOSE MSN 904416 ENT BY: 448879 . FOUND BRAIDED LINE ON LT BODY GEAR DOOR ACTUATOR RUPTURED. ORDERED HOSE CPN 0109172 MSN 904416. ENT BY: 448879 FACT 02NOV04 22:35 MCI R. REMOVED AND REPLACED BODY DOOR ACTUATOR LINE FOLLOWING FX MM 32-32-081-4, LEAK CHECK GOOD. ALSO, FOLLOWED FX MM 29-11-000-1 CASE DRAIN AND PRESSURE FILTER CHECK/REPLACEMENT. NO CONTAMINATION FOUND. LEAK CHECK GOOD. ENT BY: 393294 RPT BY: 393294. 2L73 4F A3WE 20041115001612004111500161WP 2004 11 15 04FDEA03012 120041031A26124059027903 CONTROLLER DOUG MD10 MD1010F 3022112WP E/E BAY MALFUNCTIONED A FDEAF ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SO25385FE533 533 46619 FWD LOWER CARGO SMOKE ALERT DURING FLT, EXTINGUISHED 2 FIRE AGENTS. AFTER 1ST BOTTLE DISCHARGED THE ALERT EXTINGUISHED, DID NOT NOTICE WHICH DETECTOR IN FWD CARGO CAUSED ALERT. IN PROGRESS OF REPLACING BOTH FIRE EXTING BOTTLES AND SQUIBS, ALSO WILL REPLACE ALL 4 FWD CARGO SMOKE DETECTORS. AFTER COMPLETION SYSTEMS NEED TO BE OPS CHECKED PER MM. REMOVED AND REPLACED MSC PRECAUTIONARY OPS CHECKS GOOD PER M/M 31-42-00. REMOVED AND REPLACED NR 2 FIREX BOTTLE AND CARTRIDGE PER M/M 26-22-01-4 AND 26-22-03-4. OPS CHECKS GOOD. 2L73 4F RTA22WE 20041115001642004111500164NM 2004 11 15 04FDEA02942 120041016A5713ARB75131 STRINGER DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LEFT HAND WING UPPER STRINGER (S13) END FOUND CRACKED AT INSIDE ACCESS PANEL 535BT. LEFT HAND WING UPPER STRINGER (S13) SLOT OUT CRACKED AREA AT STRINGER END AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I. 2L73 4F RTA22WE 20041115001692004111500169NM 2004 11 15 04FDEA02588 120040831A5340AGA7115514 FITTING DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CAC COMPARTMENT, BETWEEN STA Y= 6-90 AND STA Y= 6-100 LONGERON 43R END SPLICE FITTING FOUND CRACKED. CAC COMPARTMENT - STA Y= 6-90 AND STA Y= 6-100 CRACKED SPLICE AT LONGERON 43R. REMOVED PER SRM 51-31-01 VOLUME II. NEW SPLICE FITTING FABRICATED PER DWG AGA7115; PAINTED PER SRM 51-21-01 VOLUME II AND PART MARKED FX AGA7115-514 PER FEDEX GMM 11-0-1001. NEW SPLICE FITTING INSTALLED PER 51-33-01 VOLUME 1 AND DWG AGA7115. 2L73 4F RTA22WE 20041115001772004111500177EU 2004 11 15 AWXA200400977 120040814A5347D53371110001 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BS 8433 TO BS 9500, FS 14 TO FS 24. MAINTENANCE REMOVED CORRODED SEAT TRACK Y765 RT FROM FS 14 TO FS 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001812004111500181WP 2004 11 15 04FDEA02900 120041011A5753ARC0154 STOP DOUG DC10 DC1010 3022110WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 RT WING INBD FLAP REWORK OF UPSTOP MOUNT HOLE IN ARC0154 HINGE ASSY. COMPLIED WITH E.A.8-5750-82056. 2L73 4F A22WE 20041115001822004111500182NM 2004 11 15 AWXA200401007 120040911A3350GMW15 FUSE BOEING737 7373G7 1384595NM EMERGENCY LIGHT BLOWN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 DURING FUNCTIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, FOUND THE ESCAPE PATH LIGHT AT SEAT ROW 17 LT INOPERATIVE, BULB REPLACEMENT NO HELP. MAINTENANCE REPLACED BLOWN FUSES ON BATTERY CHARGER AT BS 968 RT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041115001872004111500187NE 2004 11 15 AWXA200401012 220040910A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 FAILED A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28651AW 866 V10223 ON TAKEOFF AT ORD EN ROUTE FOR PHX, WHEN FLEX THRUST APPLIED HEARD A LOUD BANG WITH MOMENTARY STALL INDICATED ON ECAM, REJECTED TAKEOFF AND UPON CLEARING RUNWAY NOTICED NR 1 ENGINE N2 VIB AT 7.4, SHUTDOWN ENGINE AND RETURNED TO GATE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF INLET AND EXHAUST AREAS AND FOUND NO APPARENT DAMAGE. INSPECTED 7TH AND 10TH STAGE BLEED VALVES AND FOUND METAL SHAVINGS IN 7TH STAGE AT THE 1 O'CLOCK AND 7 O'CLOCK POSITIONS. REMOVED AND REPLACED NR 1 ENGINE IAW T/C R5M71302, OPERATIONAL CHECK WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20041115001882004111500188NM 2004 11 15 AWXA200401013 120040905A5320D53472102200 COUPLING AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON LOWER SURFACE OF UPPER COUPLING (BEAM SPLICE) AT Y1292 RT, FORWARD OF FS 68. MAINTENANCE REMOVED CORRODED COUPLING AT Y1292 RT, FS 68; FABRICATED A NEW REPLACEMENT COUPLING; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041115002012004111500201NM 2004 11 15 2004UALA01013 120041102A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 FUSELAGE FRAME CRACKED AT BS 188 WL 208.1 LT SIDE. INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA16WE E2GL 20041115002062004111500206EU 2004 11 15 AWXA200401202 120041017A5320D53480043202 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF L-2 DOOR SILL AT Y1350 BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGE IN L-2 DOOR SILL AT Y1350 FROM FS 66 TO FS 68; FABRICATED A REPAIR ANGLE, FILLER, AND PLATE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201. 2L72 4F RTA28NM 20041115002072004111500207EU 2004 11 15 AWXA200401203 120041017A5320D53112087205 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT Y254 RT BETWEEN FS 16 AND FS 20. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR SUPPORT Y254 RT FROM FS 16 TO FS 20; FABRICATED A NEW REPLACEMENT SECTION OF FLOOR SUPPORT AND 4 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-11-14, 202. 2L72 4F RTA28NM 20041115002182004111500218NM 2004 11 15 AWXA200401156 120041011A5320654964911 ANGLE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN ANGLE AT LOWER FORWARD CORNER OF L-1 DOOR BS 315, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE AT LOWER FORWARD CORNER OF L-1 DOOR BS 315, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-49649; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG. 3, 4, AND 8. 2L72 4F RTA16WE 20041115002272004111500227EU 2004 11 15 04FDEA02797 120040921A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 BULK CARGO COMPT FLOOR STRUCTURE FS 65 ON LT SIDE, MID AND RT SIDE AREA NOTED CORROSION ON TOP AND UNDERNEATH SURFACES. REMOVED AND REPLACED BEAM IAW A310 SRM 53-10-15. 2L72 4F RTA35EU 20041115002382004111500238NM 2004 11 15 04FDEA02839 120040928A5743 SUPPORT BEAM BOEING727 727277 138408SNM MLG CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 CLOSER COMPLY WITH EA NR 7-5710-82041 WINGS, LEFT MLG SUPPORT BEAM CORROSION AT FLAP TRACK MOUNT. BFM U COMPLIED WITH EA7-5710-82041 REAMED HOLE, FLAP PEENED AREA , INSTALLED REPAIR BUSHING AND WASHER ENT BY: 497236 RPT BY: 497236. 2L73 4F RTA3WE 20041116000102004111600010EU 2004 11 16 AWXA200400980 120040815A5315D5347217220100 FLOORBEAM AIRBUS320 A320231 3930325EU CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON Y1292 RT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM PER DWG 18D53472172; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000152004111600015EU 2004 11 16 AWXA200400985 120040815A5313D5348006225000 GUSSET AIRBUS320 A320231 3930325EU STRINGER CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON GUSSET STRINGER 26 RT AT FORWARD SIDE OF FS 66. MAINTENANCE REMOVED CORRODED GUSSET STRINGER 26 RT AT FORWARD SIDE OF FS 66; FABRICATED A NEW REPLACEMENT GUSSET PER DWG 18D53480062; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 8-17. 2L72 4F RTA28NM 20041116000252004111600025NM 2004 11 16 AWXA200401076 120040922A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, THE LT AFT EMERGENCY FLASHLIGHT FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BATTERY IN LT AFT EMERGENCY FLASHLIGHT, OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20041116000262004111600026NM 2004 11 16 AWXA200401077 120040928A212087292325V04 COMPUTER AIRBUSA319 A319132 3930340NM ZONE 120 MALFUNCTIONED A AWXAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 WP28822AW13749 1410 DURING CLIMB-OUT OF LAS EN ROUTE FOR PHL AT 7000 FT, RECEIVED ECAM WARNING AVIONICS VENT SKIN AIR VALVE FAULT, FOLLOWED ECAM INSTRUCTIONS THAT RESULTED WITH AN ECAM VENT BLOWER FAULT AND VENT EXTRACT FAULT, AS A RESULT LOST WEATHER RADAR, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER EVENT. MX REMOVED AVIONICS EQUIPMENT VENTILATION COMPUTER IAW AMM 21-26-34-4, AND AVIONICS VENT FILTER AND HOUSING IAW AMM 21-26-42-920-001, OPERATIONAL CHECKS WERE GOOD. SUPP - VENDOR INCOMING FUNCTIONAL TEST OF AVIONICS EQUIPMENT VENTILATION COMPUTER S/N VL2062001616 COULD NOT DUPLICATE REASON FOR REMOVAL. ACCOMPLISHED SERVICE BULLETINS 87292325-21-008 AND 87292325-21-011, TESTED UNIT. 2L72 4F RTA28NM 20041116000322004111600032NM 2004 11 16 04FDEA02992 120041025A5743 SUPPORT DOUG MD11 MD11F 3023600NM MLG DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25599FE 48598 DURING AIRPLANE'S CONVERSION P-F/ACF RT WING INTERNAL T/E STRUCTURE STA XORS 264 LWR SIDE MAIN LANDING GEAR SUPPORT BOLT DRAIN OBSTRUCTED AND NUTS ON TL WITH RUST. REMOVE TRUNNION SUPPORT FITTING AND HEAVILY CORRODED ARB0621:BLEND OUT, NDI , PROTECT AREA, INSTALL NEW FASTENERS. 2L73 4F RTA22WE 20041116000422004111600042NM 2004 11 16 04FDEA03045 120041108A5315 FLOORBEAM BOEING727 72722 1384002NM CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FOUND CORROSION ON FLOORBEAM AT BS 620 BL O - LBL 8 (C53-111-01(3)). CORROSION REMOVED ON FLOORBEAM FOUND TO BE OUT OF LIMITS. FLOORBEAM TO BE REPAIRED ON N00920. 2L73 4F A3WE 20041116000432004111600043NM 2004 11 16 2004UALA00979 120041019A2710 CONTROL CABLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AILERONS MISROUTED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29202UA 24717 AILERON CONTROL CABLE FRAYED. CABLE GUIDE DAMAGED ON AILERON BUSS DRUM. DAMAGED DUE TO MISROUTING OF CABLE. SUSPECT CABLE WAS MISROUTED DURING HEAVY MAINTENANCE VISIT. BOTH ITEMS REPLACED. 2L72 4F4 FRTA16WE E2GL 20041116000442004111600044NM 2004 11 16 04FDEA03046 120041108A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION FLOORBEAM STA 620 LWR CHORD LWR SURFACE CORRODED LBL 8 AROUND NUTPLATE HOLE. REPAIRED PER SRM 53-10-1, 53-10-8 2L73 4F A3WE 20041116000582004111600058NM 2004 11 16 AWXA200401026 120040909A5330 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING 8-DAY CHECK, A 3 3/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT RT TAIL AREA FORWARD OF OUTFLOW VALVE BS 927, STR 23 RT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229, DETAIL XI. 2L72 4F RTA16WE 20041116000612004111600061EU 2004 11 16 AWXA200401218 120041018A5347D533711100100000SEAT TRACK AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON RT CABIN SEAT TRACK Y765 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION RT CABIN SEAT TRACK Y765 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 12. 2L72 4F RTA28NM 20041116000742004111600074NM 2004 11 16 04FDEA03074 120041111A55116520656 SPAR BOEING727 72722 1384002NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION LT HORIZONTAL STAB UPPER FRONT SPAR CHORD INTERNAL SURFACE IN AREAS FROM STAB STA 4.45 TO STAB STA 33. REPAIRED IAW SRM 51-10-6. 51-30-2, 51-10-2, 55-10-5. 2L73 4F A3WE 20041116000872004111600087NM 2004 11 16 AWXA200401150 120041005A533065457722 SKIN BOEING737 73733A 1384673NM FUSELAGE WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A WORN AREA WAS FOUND ON DOUBLER (SKIN) WHERE VERTICAL FIN MEETS FUSELAGE BETWEEN BS 867 AND BS 887, STR 1 RT AND STR 2 RT. MAINTENANCE REMOVED WORN DOUBLER FROM BS 867 TO BS 887, STR 1 RT TO STR 2 RT; FABRICATED A NEW REPLACEMENT DOUBLER PER DWG 65-45772; INSTALLED REPAIR PART IAW EO 55-32-01, FIG 2, PG 9. 2L72 4F RTA16WE 20041116000982004111600098NM 2004 11 16 04FDEA02744 120040919A5313AFA7093501 LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 AFT CARGO, RT LONGERON 38R AT STA Y= 1860 FOUND CORRODED AND CRACKED. AFT CARGO, CORRODED AND CRACKED RT LONGERON 38R BETWEEN STA Y= 1787 AND Y= 1890, REMOVED PER SRM 51-31-01 VOLUME II. NEW LONGERON FABRICATED PER DWG AFA7093 AND PAINTED PER SRM 51-21-01 VOLUME II. FABRICATED LONGERON AND REPAIR PARTS INSTALLED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041116001102004111600110EU 2004 11 16 AWXA200401097 120040925A5320D53475765000 BEAM AIRBUS320 A320232 3930326EU CARGO DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT BULK CARGO DOOR SILL BEAM Y1500 RT, BETWEEN FS 60 AND FS 62. MAINTENANCE CUTOUT DAMAGED AREAS OF AFT BULK CARGO DOOR SILL BEAM Y1500 RT AT FS 60, FS 61, AND FS 62; FABRICATED 3 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW ER 26-5341-04278-RC1. 2L72 4F RTA28NM 20041116001122004111600112NM 2004 11 16 AWXA200401116 120040930A5315141N516048 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN TRANSVERSE FLOORBEAM AT BS 334, BETWEEN RBL 2 AND RBL 39. MAINTENANCE REMOVED FLOORBEAM AT BS 334, FROM RBL 2 TO RBL 39; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBEAM PER DWG 141N5160. 2L72 4F RTA2NM 20041116001132004111600113NM 2004 11 16 AWXA200401117 120040930A5315141N51604102 FLOORBEAM BOEING757 757225 1384959NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN TRANSVERSE FLOORBEAM AT BS 334, BETWEEN RBL 2 AND RBL 39. MAINTENANCE REMOVED FLOORBEAM AT BS 334, FROM RBL 2 TO RBL 39; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOORBEAMS PER DWG 141N5160. 2L72 4F RTA2NM 20041116001182004111600118NM 2004 11 16 04FDEA02666 120040910A53131D0414T LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CENTER CARGO COMPARTMENT AT BETWEEN STATION 5-73 TO 5-113, LONGERON 52 FOUND CORRODED. CORRODED LONGERON AT CENTER CARGO COMPARTMENT, BETWEEN STATION 5-73 TO STATION 5-113 LONGERON 52 TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 FIG 2 VOL I. 2L73 4F RTA22WE 20041116001202004111600120NM 2004 11 16 04FDEA02668 120040910A5512ALC8103504 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 32 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 32R. REPAIRED AS PER EA NR 1-5510-81559, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 32R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041116001212004111600121NM 2004 11 16 04FDEA02669 120040910A5511ALC8131502 SPAR CAP DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 36 RIGHT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 36R. REPAIRED AS PER EA NR 1-5510-81544, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 36R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041116001242004111600124NM 2004 11 16 04FDEA02480 120040814A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR UPPER CHORD XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1042 CORROSION REMOVED PER SRM 51-21-01 VOLUME II, COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041116001252004111600125NM 2004 11 16 04FDEA02481 120040814A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR UPPER CHORD XORS= 1079 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1079 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041116001262004111600126NM 2004 11 16 04FDEA02997 120041027A5347AEA7579501 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK AT STA 1369 RBL 75 FOUND CORRODED. CABIN SEAT TRACK AT STA 1369 RBL 75 CORROSION AREA REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041116001272004111600127EU 2004 11 16 04FDEA02998 120041028A21209354M89G01 DUCT AIRBUS310 A310203 3930313EU NR 1 ENGINE LEAKING A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25427FE 362 ENGINE FIRE NR 1 ENG (NAC FIRST WENT TO 120 DEG). SHUT DOWN, PULLED FIRE HANDLE AND COMPLIED WITH ECAM/QRH. ENT BY: 439732 RPT BY: 056165 SHGN 28OCT04 16:06 MEM R PER FLT CREW DEBRIEF ENGINE SHUT DOWN OIL PRESSURE NORMAL AND FIRED NR 1 BOTTLE THEN FIRE WARNING WENT. REMOVED NR 1 FIRE BOTTLE FOR REMOVE AND REPLACE. FOUND HIGH PRESSURE TURBINE COOLING AIR DUCT BLOWN OUT ON TOP OF ENGINE REF THE GE ENGINE M/M 72-53-09, REMOVED AND REPLACED THE UPPER HIGH PRESSURE AIR RECOUP TUBE. 2L72 4F RTA35EU 20041116001282004111600128NM 2004 11 16 AWXA200401062 120040922A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 7 LT INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 FLIGHT CREW REPORTED, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116001292004111600129EU 2004 11 16 AWXA200401063 120040923A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 221 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28652AW 953 DURING 4-DAY CHECK, FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM THE FORWARD LT EMERGENCY LIGHT BATTERY FAILED TEST AT EMERGENCY POWER SUPPLY UNIT (10WL). MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041116001302004111600130NM 2004 11 16 AWXA200401064 120040909A53206545834551 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK, A 1/4 INCH CRACK WAS FOUND IN TIE STRAP AT BS 343, LBL 45, WL 200. MAINTENANCE REMOVED TIE STRAP AT BS 343, LBL 45, WL 200 AND STOP DRILLED CRACK; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR DOUBLER; REINSTALLED TIE STRAP IAW B737-300 SRM 53-10-51, FIG 204. 2L72 4F RTA16WE 20041116001332004111600133NM 2004 11 16 04FDEA02672 120040910A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 13 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. 2L73 4F RTA22WE 20041116001352004111600135NM 2004 11 16 04FDEA01831 120040621A5512ALC8101 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 8 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND NR 8 BARREL NUT BORE. REPAIRED AS PER FEDEX EA 1-5510-78023 - STABLIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE 8R. AUTHORIZATION TO BORE THROUGH THE BOTTOM (MD-11 SB 55-023 REV 1) 2L73 4F RTA22WE 20041116001392004111600139NM 2004 11 16 04FDEA01835 120040621A5712ARC70551 FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORRODED. RIGHT HAND WING, OUTBOARD FLAP VANE NR 3 TEE FITTING AFT BOLT HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. ORIGINAL HOLE SIZE DIA 0.3125 INCH FINAL HOLE SIZE DIA 0.375 INCH REPAIR CARRIED OUT AS PER EA 1-5750-78016. TITLE: WINGS, TRAILING EDGE FLAPS, RT O/B FLAP VANE NR 3 TEE FITTING CORROSION REPAIR. 2L73 4F RTA22WE 20041116001402004111600140NM 2004 11 16 AWXA200400886 120040813A270010605813 MOTOR BOEING737 737277 1384570NM LT MLG WW VALVE BINDING A AWXAA UNSCHED LANDING EFJVIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 WP28182AW 22649 ON CLIMB-OUT OF PHX EN ROUTE FOR SJC AT APPROXIMATELY 3000 FT, FLIGHT CONTROLS SHOOK VIOLENTLY FROM SIDE TO SIDE AS IF IN SEVERE TURBULENCE. NOTICED FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, ADJUSTED AILERON TRIM AND ONCE AILERON INPUT WAS ACHIEVED VIBRATION SMOOTHED OUT. WHEN SLOWING TO FLAP EXTENSION SPEED THE FEEL DIFFERENTIAL LIGHT WENT OUT AND VIBRATION DISAPPEARED. MAINTENANCE PERFORMED A VISUAL CHECK OF ELEVATOR TRIM TABS AND HINGE POINTS, NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED "A" SYS FLIGHT CONTROL MODULAR PACKAGE IAW BMM 27-009-200-4. MAINTENANCE ALSO FOUND 4 EACH CONNECTORS AT "A" SYS MODULAR PACKAGE WORN AND DETERIORATED, REPLACED CONNECTOR. 2L72 4F RTA16WE 20041116001412004111600141EU 2004 11 16 AWXA200401255 120041025A5347D5337111001000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT OUTBOARD SEAT TRACK BETWEEN FS 42 AND FS 43. MAINTENANCE REMOVED CORRODED RT OUTBOARD SEAT TRACK FROM FS 42 TO FS 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116001472004111600147NM 2004 11 16 AWXA200401184 120040929A575465C266067 SKIN BOEING737 73733A 1384673NM NR 5 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, 18 CRACKS WERE FOUND AT FASTENER HOLES IN LOWER SURFACE SKIN OF NR 5 SLAT BETWEEN SLAT STA 150 AND SLAT STA 235. MAINTENANCE CUTOUT DAMAGE ON LOWER SURFACE SKIN OF NR 5 SLAT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, FIG 206. 2L72 4F RTA16WE 20041116001502004111600150NM 2004 11 16 AWXA200400849 120040803A361034185 SEAT AIRBUSA319 A319132 3930340NM NR 1 ENGINE LEAKING A AWXAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CLCLIMB 1 WP28814AW 1281 AFTER TAKEOFF AT JFK EN ROUTE TO PHX, RECEIVED ECAM MESSAGE "AIR ENG 1 BLEED ABNORMAL PRESSURE", NR 1 ENGINE BLEED VALVE WOULD NOT OPEN, DIVERTED TO BWI FOR REPAIR. MX T/S PER TSM 36-11-00-810-809A, BLEED PRESSURE REGULATOR VALVE FAILED 20 PSI TEST PER STEP 2, REMOVED AND REPLACED BLEED PRESSURE REGULATOR IAW AMM 36-11-52-04. ALSO, REPLACED NR 1 ENGINE HIGH PRESSURE VALVE (HPV) IAW AMM 36-11-51-04, AND AS A PRECAUTION REPLACED TEMPERATURE LIMITATION SOLENOID THERMOSTAT IAW AMM 36-11-55-000-001. OPERATIONAL AND LEAK CHECK WAS GOOD. SUPP - VENDORS INCOMING TEST OF PRESSURE REGULATOR VALVE S/N 00513 CONFIRMED REASON FOR REMOVAL, UNIT FAILED INTERNAL LEAKAGE TEST. 2L72 4F RTA28NM 20041116001542004111600154EU 2004 11 16 04FDEA02727 120040918A3230D224260003 DAMPER AIRBUS310 A310203 3930313EU PITCH FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25427FE 362 ON TAKEOFF FROM IAD, GEAR WOULD NOT RETRACT ON BOTH SYSTEM 2 OR SYSTEM 1. CHECK QRM, HOLD FOR FUEL BURN. APPROACH TO 19R IAD NORMAL. ENT BY: 262258 RPT BY: 053758. T/S PROBLEM, FOUND ACTUATOR LOW IN FLUID AND PRESSURE. THE ACTUATOR IS LEAKING FLUID ,THE PART NEEDS CHANGED. REMOVED AND REPLACED RIGHT MLG PITCH DAMPER PER MM 32-11-15-4-02. OP'S GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE M/M 32-31-11-4. 2L72 4F RTA35EU 20041116001562004111600156NM 2004 11 16 04FDEA02729 120040919A5512ALC8101503 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 3 LEFT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 3L. REPAIRED AS PER EA NR 1-5510-81562, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 3L. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041116001572004111600157NM 2004 11 16 04FDEA02754 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.501 INCH, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041116001582004111600158NM 2004 11 16 04FDEA02755 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.095 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041116001622004111600162NM 2004 11 16 04FDEA02759 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041116001632004111600163NM 2004 11 16 04FDEA02730 120040919A5512ALC8101503 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 4 LEFT BARREL NUT BORE FOUND EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 4L. REPAIRED AS PER EA NR 1-5510-81545, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 4L, REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041116001662004111600166WP 2004 11 16 04FDEA02820 120040927A5330AYB70301 SKIN DOUG DC10 DC1010F 3022111WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION, FROM STATION 1350 TO 1521 L48L TO L48R. COMPLIED WITH FEDEX EA 8-5330-77624, SKIN SPLICE REPAIR AT STATION 1350-1521. REFERENCE NON ROUTINE N01775. 2L73 4F A22WE 20041116001672004111600167NM 2004 11 16 04FDEA02503 120040819A5320NFA6310 SPLICE DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK, RIGHT HAND SIDE STA 5-113 STA 1541 LONGERON 25 FOUND CRACKED. MAIN DECK, RIGHT HAND SIDE STA 5-11 TO STA 1541 DAMAGED. LONGERON 25 CUT, REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 53-33-01 VOLUME II. 2L73 4F RTA22WE 20041116001702004111600170NM 2004 11 16 04FDEA02972 120041022A5713UNKNOWN STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 RIGHT HAND WING LEADING EDGE STRINGER AT STA XORS 799 FOUND CRACKED. RIGHT HAND WING LEADING EDGE STRINGER AT STA XORS 799 CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 18, VOLUME I. 2L73 4F RTA22WE 20041116001722004111600172WP 2004 11 16 UPS04843451 120041009A5720 CHANNEL DOUG DC8 DC871F 302199DWP STA. XFS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE: C3, LT WING LEADING CENTER SECTION LOWER SUPPORT U-CHANNEL HAS A CRACK AT AFT 2 FASTENERS 2 INCHES LONG STA XFS 510. STOPPED DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DWG 5770375 AND DC-8 SRM 51-1-21 & 51-1-20D. 2L74 4F RT4A25 20041116001732004111600173WP 2004 11 16 UPS04843463 120041109A3350 LIGHT DOUG DC8 DC871F 302199DWP COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP OVER COURIER SEAT & IN COCKPIT CEILING. RELAMPED PER MM 33-50-02-2, CK'S OK. 2L74 4F RT4A25 20041116001752004111600175EU 2004 11 16 MALA040664 120041029A7810 TAIL CONE BAC 146 AVRO146RJ85A1500097EU NR 2 ENGINE DETACHED A MALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 GL15533XJ E2367 GROUND CREW FOUND TAILCONE ON GROUND AFTER PUSHBACK. BY THE TIME GROUND CREW FOUND CONE AND NOTIFIED DISPATCH AND MAINTENANCE CONTROL, A/C HAD DEPARTED DSM. MAINTENANCE CONTROL AND DISPATCH NOTIFIED CREW TO RETURN TO DSM. WHEN A/C RETURNEDTO DSM, FOUND TAILCONE CAME FROM NR 2 ENGINE. MAINTENANCE INSPECTED AND REINSTALLED ORGINAL TAIL CONE. FOUND DENT AT 3:00 POSITION DIMENSIONS 1.10 INCHES WIDE, .55 INCHES LONG, .027 INCHES DEEP. PERFORMED VISUAL INSPECTION 51-10-02-1, & FIG 51-10-21. DENT IS ALLOWABLE DAMAGE. NO FURTHER ACTION REQUIRED. 2H74 4F RTA49EU 20041116001762004111600176EA 2004 11 16 COMA0460607 120041108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 INTERCOSTAL AT FS 484.00 CRACKED AT LBL 36. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20041116001782004111600178EU 2004 11 16 UPS04143462 120041109A5610TAG967201 WINDSHIELD AIRBUSA300 A300F4622R 3930360EU COCKPIT FAILED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01125UP 0809 INSPECTION TYPE:N/A CAPTS WINDSHIELD OUTER PANE SHATTERED. REMOVED AND REPLACED CAPT WINDSHIELD SRT 56-11-11-4. 2L72 4F RTA35EU 20041116001802004111600180NM 2004 11 16 UPS04443444 120041030A532065B0793684 SPLICE BOEING747 747200 1384847NM ZONE 211 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C M/D - BS 400, STR 23-24L, FRAME I/B CHORD O/B FACE ATT SPLICE FOUND CRACK. BS 400 STR 23-24L FRAME SPLICE REPLACED PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20041116001812004111600181NM 2004 11 16 UPS04443445 120041030A531165B01716505 FRAME BOEING747 747200 1384847NM ZONE 211 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 460 BTN STR 13L AND 14L FRAME WEB FOUND CRACKED. CRACKED FRAME WEB REPLACED PER SRM 51-10-01. 2L74 4F RTA20WE 20041116001832004111600183EU 2004 11 16 MALA040663 120041027A5220 DOOR SAAB SF340 340B 7860101EU EMERGENCY EXIT MISINSTALLED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 POST FLIGHT NOTED EMERGENCY OVERWING EXIT DOOR INCORRECTLY INSTALLED. MAINTENANCE FOUND OVERWING EXIT DOORS INSTALLED IN OPPOSITE POSITIONS. INSTALLED DOOR IN CORRECT LOCATION, ALL CHECKS GOOD. 2L72 4T RTA52EU 20041116001862004111600186EU 2004 11 16 MALA040662 120041027A2150 BELT SAAB SF340 340B 7860101EU A/C PACK FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15408XJ 340B408 ON PREFLIGHT, WHEN CREW TURNED ON SUPPLEMENTAL AC SYSTEM, A SMOKY HAZE IN CABIN. MAINTENANCE CONFIRMED AC SYSTEM CAUSING PROBLEM. MAINTENANCE REMOVED AND REPLACED BELT & COVER. 2L72 4T RTA52EU 20041116001872004111600187EU 2004 11 16 MALA040666 120041030A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, FLOOR SUPPORT FRAME CORRODED AT FS 231 BL 0. MAINTENANCE REPAIRED IAW MESABA EO S53102. A/C WAS RELEASED 11/07/04. 2L72 4T RTA52EU 20041116001892004111600189EA 2004 11 16 COMA0460609 120041110A3260864808 PSEU CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01868CA5137 627 7427 FLIGHT 5245 PROX SYSTEM CHANNEL-C MESSAGE. REPLACED THE PSEU. 2L72 4F RTA21EA 20041116001922004111600192WP 2004 11 16 UPS04843450 120041010A5720 INTERCOSTAL DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE: C3, RT WING CENTER L/E INTERCOSTAL IS CRACKED AT XFS 387.750. STOP DRILLED CRACK AT STA XFS 387.750 IAW SRM 57-02-00-0 FIG 002. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 57-02-00-0 FIG 2 & DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20041116001932004111600193WP 2004 11 16 UPS04843457 120041009A5711 FRAME DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE: C3, LT WING LEADING EDGE OUTER SECTION STA XFS-759 UPPER FORMER HAS A CRACK AT AFT FASTENER. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG19, 51-1-20D &51-1-21. 2L74 4F RT4A25 20041116001972004111600197NM 2004 11 16 UPS04443484 120041028A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, LT BS 360 UPPER DECK FLOORBEAM ONE EA FASTENER HOLE CRACK REVEALED AT FLOORBEAM WEB AND FRAME WEB DOUBLER LAYER FOR DETAILS BS 360, WL 280 TO 320. LEFT BS 360 FLOORBEAM WEB & FRAME WEB CRACK REPAIRED AND FLOORBEAM WEB SECTIONAL REPLACED PER SRM 53-10-07 FIG 11 & HX RS R53-15-35211 & FRAME WEB REPLACED PER SRM 51-10-01 & HX RS R53-15-35211 AND UPS EO B747-5310-21306-A. 2L74 4F RTA20WE 20041116001982004111600198NM 2004 11 16 UPS04443485 120041101A531165B01711635 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C U/D- BS 360 LEFT FRAME WEB DOUBLER FOUND CRACKED AT STR L10A (AFT FACE). U/D BS 360 LEFT FRAME WEB DOUBLER REPLACE PER HX NRC 5613 FOR THE SUBJECT FRAME WEB REPLACEMENT DETAIL. REF HX RS R53-15-35211 AND UPS EO B747-5310-21306-A. 2L74 4F RTA20WE 20041116001992004111600199NM 2004 11 16 UPS04443486 120041029A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- LEFT BS 360 FRAME & DOUBLER S24AL STR CUTOUT CRACKED. M/D- LEFT BS 360 FRAME & DOUBLER REPAIRED AS PER HX RS R53-12-35213 AND UPS EO B747-5310-21311-A. 2L74 4F RTA20WE 20041116002012004111600201NM 2004 11 16 UPS04443488 120041101A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D-BS 500 RIGHT FRAME WEB DOUBLER (AFT FACE) FOUND CRACKED. STR-R11 BS 500 RIGHT FRAME AT STR 11 CRACKED REPAIRED PER HX RS R53-10-35214, ALL CRACK STOPPED AT THE STOP HOLES, CONFIRMED BY NDT. 2L74 4F RTA20WE 20041116002022004111600202NM 2004 11 16 UPS04443489 120041028A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C RIGHT BS 360 UPPER DECK FLOORBEAM ONE FASTENER HOLE CRACK FOUND AT FRAME WEB BS 360, WL 280 TO 320. BS 360 RT FRAME WEB CRACKED AREA REPAIRED PER HX RS R53-15-35211 BY CRACKED FRAME WEB DOUBLER REPLACED & FRAME WEB REINFORCEMENT PER THE HX RS R53-15-35211 AND UPS EO B747-5310-21306-A. 2L74 4F RTA20WE 20041116002032004111600203NM 2004 11 16 UPS04443490 120041029A5711 SPAR BOEING747 747200 1384847NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, RIGHT WING - MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411. 2L74 4F RTA20WE 20041116002042004111600204NM 2004 11 16 UPS04443491 120041029A5711 SPAR BOEING747 747200 1384847NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, RIGHT WING - MID SPAR UPPER CHORD FASTENER 2EA EDGE FOUND CRACK BETWEEN WS 440 - WS 460. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 440 - 460. 2L74 4F RTA20WE 20041116002052004111600205NM 2004 11 16 SWAA043223 120041105A53116546520 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND 4 EACH FRAME SECTIONS CRACKED AT BS 400, STRINGER 8R, BS 380 STRINGER 8L, BS 440, STRINGERS 8L & 8R. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041116002062004111600206 2004 11 16 UPS04243347 420041014A2565 SLIDE BOEING727 72725C 138400HNM COCKPIT OUT OF LIMITS A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 EMERGENCY ESCAPE SLIDE PRESSURE IS BELOW LIMITS. REMOVED EMERGENCY ESCAPE SLIDE PER MM 25-60-15. 2L73 4F A3WE 20041117000012004111700001 2004 11 17 SWAA043331 420041113A2565D31354 CABLE BOEING737 7373H4 1384600NM R2 DOOR GIRT BARFRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041117000032004111700003NM 2004 11 17 SWAA043330 120041113A5753 SKIN BOEING737 7373H4 1384600NM RT FORE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 2742 27703 DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED RT FORE FLAP PER MM. 2L72 4F RTA16WE 20041117000042004111700004NM 2004 11 17 SWAA043332 120041114A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 379, EQUIPMENT COOLING EXHAUST CUTOUT, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20041117000052004111700005NM 2004 11 17 SWAA043333 120041114A53156546812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, LBL 54, CRACKED. REPAIRED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20041117000062004111700006NM 2004 11 17 SWAA043334 120041114A53156546812 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, BETWEEN RBL 47 TO LBL 47, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER ER. 2L72 4F RTA16WE 20041117000072004111700007NM 2004 11 17 SWAA043335 120041114A57536937880 CARRIAGE BOEING737 7375H4 138449DNM RT WING FLAPS WORN A SWAAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW29508SW 24185 WHEN FLAPS SELECTED TO 5 DEGREES, HALF WAY BETWEEN 2 & 5 DEGREES FELT VIBRATION, AS FLAPS MOVE INTO WHITE BAND OF 5 DEGREES, VIBRATION WORSE. REMOVED AND REPLACED RT INBOARD FORE FLAP INBOARD AND OUTBOARD CARRIAGES, PER MM. 2L72 4F RTA16WE 20041117000082004111700008NM 2004 11 17 SWAA043336 120041114A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29619SW 28035 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BETWEEN BS 860 AND BS 872, STRINGER 1, CHAFING. REPAIRED SKIN SECTION PER EA. 2L72 4F RTA16WE 20041117000092004111700009NM 2004 11 17 SWAA043337 120041114A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 771, LBL 13, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041117000102004111700010NM 2004 11 17 UPS04443341 120040926A5315 FLOORBEAM BOEING747 747121 1384871NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FWD CARGO STA 960 RBL 45 FLOOR SUPPORT CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 01 LIMITS. FLOORBEAM FLANGE REPAIRED PER SRM 54-40-04 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20041117000112004111700011NM 2004 11 17 UPS04443343 120041015A3350 BATTERY PACK BOEING747 747123F NM ESCAPE SLIDE INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01677UP 20391 EMERGENCY EXIT LIGHTS IN RIGHT ESCAPE SLIDE DOOR FRAME INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-04, OPS CHECK GOOD. 2L74 4F A20WE 20041117000122004111700012NM 2004 11 17 UPS04643023 120040815A2720BACC2C4003821FG CONTROL CABLE BOEING767 767300 1385204NM RUDDER CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01326UP 27752 INSPECTION TYPE: ETOP, RUDDER CONTROL CABLE RB IS MISROUTED AND IS CHAFING AGAINST PULLEY SUPPORT BRACKET AT BS 240, LBL 5, WL 199. REMOVED, INSPECTED TO BE IN SERVICEABLE CONDITION, PROPERLY ROUTED / INSTALLED, RIGGED AND FUNCTIONAL TESTED GOOD. 2L72 4F RTA1NM 20041117000132004111700013 2004 11 17 UPS04843348 420041008A3423 EADI DOUG DC8 DC873F 302199FWP COCKPIT FAILED A IPXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01866UP 45966 ELECTRICAL BURNING SMELL FROM F/O'S SIDE DURING APPROACH FOR APPROX 10 - 15 SECONDS. ALL FLUORESCENT LIGHTS WERE OFF. TURNED ON ALL LIGHTS, RAN BOTH PACKS, OPERATED ALL NAVIGATION COMPT, INSPECTED ALL WIRES AT F/O'S INSTRUMENT PANEL, NO ELECTRICAL BURNING SMELL NOTED. REMOVED AND REPLACED F/O'S EADI AS PER MM 34-23-01-4 FOR HIGH TEMP AND PRECAUTIONARY OPS CKS NORMAL. OK FOR SERVICE. 2L74 4F RT4A25 20041117000142004111700014NM 2004 11 17 UPS04M43344 120041011A26122240153503 FIRE DETECTOR DOUG MD11 MD11F 3023600NM NR 1 ENGINE INOPERATIVE A IPXAO OTHER N FALSE WARNING DEDESCENT 1 SO01253UP FIRE DET 1 FAULT WARNING DURING DESCENT ON A/C STATUS PAGE NO OTHER WARNINGS OR INDICATIONS (INOP ASSY) REF M289275 REF M289275, CFDS FLIGHT FAULTS SHOW UPPER RIGHT INTERMITTENT FAULT. REPLACED UPPER FIRE DETECTOR FOR NR 1 ENG PER MM 26-11-03, TESTS GOOD. 2L73 4F RTA22WE 20041117000152004111700015NM 2004 11 17 UPS04M43345 120041014A2612 HARNESS DOUG MD11 MD11F 3023600NM NR 1 ENGING FIREDAMAGED A IPXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01253UP FIRE WARNING SYSTEM GIVING SPORADIC & INCONSISTENT POSITIVE INDICATION. NR 1 ENGINE SHUT DOWN AS PRECAUTION. REPLACED NR 1 ENG FIRE WARNING HARNESS IN REF TO MM 71-50-04. 2L73 4F RTA22WE 20041117000172004111700017 2004 11 17 UPS04143418 420041028A2565 BUTTON AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE STICKING A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01135UP 0818 ENTRY DOOR ESCAPE SLIDE TEST BUTTON STICKS DURING TEST. CLEANED TEST BUTTON, OPS NORMAL. 2L72 4F RTA35EU 20041117000182004111700018EU 2004 11 17 UPS04143419 120041028A3510 OXYGEN MASK AIRBUSA300 A300F4622R 3930360EU COCKPIT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01122UP 0807 F/O OXYGEN MASK WILL NOT TEST. INSTALLED SERVICEABLE CREW QUICK DOWNING OXYGEN MASK AND STOWAGE BOX ASSY IAW MM 35-12-51-4. 2L72 4F RTA35EU 20041117000192004111700019WP 2004 11 17 UPS04843416 120041027A3350 SWITCH DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 EMERGENCY EXIT LIGHTS ARM SWITCH INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS ARM SWITCH. OPS CHECK GOOD PER DC8 MM33-50. 2L74 4F RT4A25 20041117000202004111700020WP 2004 11 17 AALA20041116 120041110A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21233AA 49180 DFW - TAIL CONE WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE WALKWAY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117000232004111700023NM 2004 11 17 UPS04243259 120040917A1430QF71210093 BOLT BOEING727 72722C 138400FNM NR 3 ENGINE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C, NR 3 ENGINE FWD AND AFT CRANE BEAMS SHOULDER BOLTS HAVE CAD PLATING DAMAGE. BOLTS REPLACED IAW MM 71-10-32. 2L73 4F A3WE 20041117000252004111700025WP 2004 11 17 UPS04843253 120040907A5220 DOOR FRAME DOUG DC8 DC871F 302199DWP EMERGENCY EXIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, LEFT FWD EMERGENCY EXIT DOOR IS CRACKED AT UPPER FWD CORNER OF FRAME. TWO CRACKS VISIBLE .5 INCH AND 1.5 INCH IN LENGTH. STOP DRILLED 2 EA CRACKS. NDT VERIFIED STOP DRILLS TERMINATES CRACKS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 52-2-0 FIG 2. 2L74 4F RT4A25 20041117000262004111700026WP 2004 11 17 UPS04843254 120040908A5312 PRESSURE BLKHD DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND RBL 35. REMOVED EXISTING REPAIR DOUBLERS AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUTOUT. FABRICATED REPAIR DOUBLERS & FILLER AND INSTALLED IAW SRO DWG 8530009 AND SB 53-73. 2L74 4F RT4A25 20041117000272004111700027WP 2004 11 17 UPS04843255 120040908A5312 PRESSURE BLKHD DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, F/S 1766 FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED 65 INCHES ABOVE FLOOR AND LBL 35. REMOVED EXISTING REPAIR AND CUT OUT CRACKED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED FILLER, FINGER DOUBLER, & DOUBLER INSTALLED IAW SRO DWG 853007 AND SB 53-73. 2L74 4F RT4A25 20041117000302004111700030WP 2004 11 17 UPS04843264 120040911A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, LONGERON 14L CRACKED AT CANTED FRAME STA 1740. CUT OUT DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLE & FILLER AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 11. 2L74 4F RT4A25 20041117000322004111700032WP 2004 11 17 UPS04843266 120040905A5714 WEB DOUG DC8 DC871F 302199DWP CENTER WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, CENTER WING FS 700 LEFT CRACK IN WEB EXTENDED PAST REPAIR. REMOVED EXISTING REPAIR. CUT OUT DAMAGED WEB. FABRICATED WEB & SPLICE DOUBLER AND INSTALLED IAW DC-8 SRM 53-2-0. 2L74 4F RT4A25 20041117000332004111700033NM 2004 11 17 UPS04443493 120041114A3350 LIGHT BOEING747 747123 1384873NM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 AFT EMERGENCY EXIT LIGHT INOP AT ENTRY DOOR. RELAMPED, OP'S CHECKED GOOD. 2L74 4F A20WE 20041117000352004111700035NM 2004 11 17 SWAA043316 120041111A3350101331 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29336SW 23940 LT OVERWING EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041117000362004111700036NM 2004 11 17 SWAA043317 120041112A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 TWO FUSELAGE SKIN CRACKS BETWEEN BS 445 AND BS 485, BETWEEN STRINGERS 18R AND 19R. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041117000382004111700038 2004 11 17 SWAA043319 420041113A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29750SA 29802 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041115001122004111500112 2004 11 15 AWXA200401119 420041012A3460B398BCM0109 COMPUTER AIRBUS320 A320231 3930325EU NR 1 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP28629AW 076 ON TAKEOFF, NR 1 ENG DID NOT PRODUCE TAKEOFF THRUST, EPR ONLY AT 1.31, REQUIRED EPR 1.42, REJECTED TAKEOFF AT 95 KTS. MX TROUBLESHOT SYS, WITH ENGINES NOT RUNNING FOUND EPR MISMATCH BETWEEN ENGINE NR 1 & 2 AT FLEX MAXIMUM CONTINUOUS THRUST (MCT) AND TOGA POSITIONS. NR 1 ENG ECAM DISPLAYED AT FLEX / MCT 1.306, NR 2 ENGINE HAD 1.287. RESET NR 2 FMGC & BOTH ENGINES EPR'S MATCHED PERFECTLY NR 1 ENG 1.274, & NR 2 ENG 1.273. R & R NR 2 FMGC IAW T/C R2A22303, AND NR 1 ENG THROTTLE CONTROL UNIT IAW AMM, ENG RUN OPS CHECK GOOD. FMGC WAS NO FAULT FOUND, UNIT WAS SUBJECTED TO NUMEROUS TESTS AND PASSED ALL SUCCESSFULLY. FMGC S/N 664 WAS EXCHANGED AT VENDOR. 2L72 4F RTA28NM 20041115001142004111500114NM 2004 11 15 04FDEA03062 120041109A574465192607 HINGE FITTING BOEING727 72722 1384002NM CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION ON RT WING O/B AILERON I/B CTR FITTING A/C SIDE IS CORRODED ON LOWER SURFACE. REPAIRED PER MM 27-10-031-2, SRM 51-30-2, 51-30-5. 2L73 4F A3WE 20041115001212004111500121NM 2004 11 15 AWXA200401245 120041102A5752654645520 TAB BOEING737 737300 1384610NM RT AILERON DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-15 CHECK AN AREA OF DISBOND WAS FOUND ON RT AILERON TAB AT OUTBOARD AFT CORNER BETWEEN WBL 479.75 AND WBL 480 RT. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-06, FIG 13. 2L72 4F RTA16WE 20041115001242004111500124EU 2004 11 15 AWXA200401248 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FS 35 AND FS 36. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FS 35 TO FS 36; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041115001352004111500135NM 2004 11 15 2004UALA00973 120041024A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY EXIT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29303UA 23644 AFT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK IN CEILING CENTER LEFT SIDE NEAR DOOR 2L. 2L72 4F4 FRTA16WE E2GL 20041115001422004111500142NM 2004 11 15 AWXA200401136 120040930A5315141N5112 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 LCQ - MAJOR REPAIR - DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 365.25, BETWEEN RBL 28 AND RBL 43. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CAP AT BS 365.25 FROM RBL 28 TO RBL 43; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, FIG 201. 2L72 4F RTA2NM 20041115001502004111500150WP 2004 11 15 04FDEA02938 120041015A5753ARC25121 HINGE FITTING DOUG DC10 DC1010 3022110WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00416. 2L73 4F A22WE 20041115001592004111500159WP 2004 11 15 04FDEA02937 120041015A5753ARC25122 HINGE FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT, OUTBOARD LUG FACE, OUTER SURFACE CORRODED. REMOVED CORROSION FROM LUG FACE, FOUND TO BE OUT OF LIMITS IAW DC10 CMM 57-52-01. COMPLIED WITH FEDEX EA 8-5750-81475, WINGS, RIGHT HAND INBOARD FLAP OUTBOARD HINGE PIVOT OVERSIZE BORE REPAIR. REFERENCE NON-ROUTINE N00985. 2L73 4F RTA22WE 20041115001682004111500168NM 2004 11 15 AWXA200401138 120041003A5330654576656 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST ABOVE LAP SEAM AT BS 465, STR 10 RT. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT BS 465, STR 10 RT; FABRICATED 2 EACH FILLERS AND A DOUBLER; INSTALLED REPAIR PARTS IAW EO 5330-01003. 2L72 4F RTA16WE 20041115001702004111500170NM 2004 11 15 04FDEA02589 120040831A5313AGA75171 LONGERON DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK, LT SIDE STA Y= 6-90 TO STA Y= 1130 LONGERON 13L FOUND CRACKED. MAIN DECK, LEFT SIDE STA Y= 6-90 TO STA Y= 1130 LONGERON 13L CUT AND REMOVED PER SRM 51-31-01 VOLUME II. LONGERON SPLICE FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. REPAIR PARTS AND EXISTING SPLICE INSTALLED PER SRM 53-10-00 TYPE 1 VOLUME I AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20041115001912004111500191NM 2004 11 15 2004UALA01004 120041029A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 STATION 1500 STRINGER 25L FRAME DENTED AFT PIT. TYPICAL CARGO PIT DENT DAMAGE DURING CARGO LOADING. CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041115001982004111500198NM 2004 11 15 04FDEA03042 120041108A5320 WEB BOEING727 72722 1384002NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED, STA 880-890 RBL 47, WL 206. REPAIRED PER SRM 51-30-2, 51-30-5, 51-10-3, 51-10-2 2L73 4F A3WE 20041115002002004111500200NM 2004 11 15 04FDEA03044 120041108A5320 WEB BOEING727 72722 1384002NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED AT STA 880-890, LBL 47, WL 206. REPLACED VERTICAL WEB PER SRM 51-10-2, 51-30-2 & SRM 51-30-5. 2L73 4F A3WE 20041115002112004111500211WP 2004 11 15 04FDEA02635 120040903A3260 DOWNLOCK SENSOR DOUG DC10 DC1010F 3022111WP MLG MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO2568054 47808 TPA CLOSER AFTER RAISING THE GEAR HANDLE DURING TAKEOFF,THE RIGHT MAIN GEAR INDICATED UNSAFE (RED) ON BOTH PANELS. RECYCLED THE GEAR IAW THE QRH. AFTER RAISING THE GEAR THE SECOND TIME,THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON FOR ABOUT ONE MINUTE, THEN WENT OUT. ENT BY: 004631 RPT BY: 096848 FACT 03SEP04 19:27 TPA R R & R RT MLG DOWN LOCK PROXIMITY SENSORS D1-43 AND D1-82 PER DC10 MM 32-61-03-2. SYSTEM OPS CHECK NORMAL. OK FOR SERVICE. 2L73 4F A22WE 20041115002262004111500226EU 2004 11 15 04FDEA02796 120040921A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 MDCC SEAT TRACK L4 FRAME 74-80 HAS 5EA CORRODED AREAS. REPAIRED SEAT TRACK BY SPLICING IAW A310 SRM 51-22-00, 51-40-21 AND 53-10-16. 2L72 4F RTA35EU 20041115002282004111500228EU 2004 11 15 04FDEA02798 120040921A5320 ANGLE AIRBUS310 A310203 3930313EU FUSLEAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 BULK CARGO COMPT FLOOR STRUCTURE FS 67 2EA AREAS OF CORROSION NOTED ON TOP AND BOTTOM SURFACES. REMOVED AND REPLACED PROFILE ANGLE IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20041115002322004111500232WP 2004 11 15 04FDEA02641 120040904A5730ARB1242 DOUBLER DOUG DC10 DC1030F 3023504WP ZONE 500 TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 LEFT WING LEADING EDGE CAVITY, CORRUGATED SKIN TORN ABOVE ANTI-ICE TELESCOPE DUCT, STA XORS 372. REMOVED AND INSTALLED TELESCOPING DUCT IAW DC10 MM 30-11-01-2. REPAIRED DAMAGED SKIN IAW FEDEX EA 8-5710-81456 STEP 1-10, REFERENCE N/R N00730. 2L73 4F RTA22WE 20041115002332004111500233WP 2004 11 15 04FDFEA02637 120040904A5730ARC04689 SKIN DOUG DC10 DC1010F 3022111WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25058FE 46705 LEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN IAW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PRIMED CONTACT UPPER SURFACE IAW DC 10 SRM 51021-01 VOL II, MARKED FX ARC0468-9 FOR SKIN PART AND FX ARC0468 DOUBLER PART IAW FEDEX GMM 7-0-1001, REFERENCE N/R N01745. 2L73 4F A22WE 20041115002372004111500237NM 2004 11 15 AWXA200401038 120040918A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 21 LT INOPERATIVE A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28326AW 23258 FLIGHT CREW REPORTED, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116000112004111600011EU 2004 11 16 AWXA200400981 120040815A5320D5348001920000 SILL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD INBOARD END OF L-2 DOOR SILL AT FS 66. MAINTENANCE CUTOUT DAMAGED AREA OF L-2 DOOR SILL AT Y1732 LT, FROM FS 66 TO FS 68; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG 201, PG. 207-213. 2L72 4F RTA28NM 20041116000222004111600022EU 2004 11 16 AWXA200400961 120040820A5315D5347218820000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LEFT BETWEEN FS 68 AND FS 69. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT, FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000232004111600023EU 2004 11 16 AWXA200400962 120040820A5315D53472172200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 67 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT, FROM FS 67 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000302004111600030EU 2004 11 16 AWXA200401039 120040919A3397ABS0374A24 WIRE AIRBUS320 A320231 3930325EU SEAT ROW 9 RT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28634AW 091 DURING 4-DAY CHECK, A BROKEN WIRE WAS FOUND ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041116000332004111600033NM 2004 11 16 04FDEA02844 120040929A7312 CONNECTOR BOEING727 7272S2F 1384O81NM PRESSURE SWITCH DAMAGED A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25209FE 22931 NR 3 ENG ICING LIGHT CAME ON 5 MIN AFTER T/O LIGHT FLICKERED FOR 2 MIN THEN ON STEADY. QRH COMPLIED WITH RTN TO MEM, LIGHT STILL ON AT BLOCK IN ENT BY: 038459 RPT BY: 096894. FOUND FUEL FILTER DIFFERENTIAL PRESS SWITCH AND CONNECTOR PINS PUSHED BACK MEM AVIONICS SHOP. REPLACED CONNECTOR. ALSO, R/R'D FUEL FILTER DIFF PRESS SWITCH.. 2L73 4F A3WE 20041116000352004111600035NM 2004 11 16 04FDEA02846 120040929A2820AAL72891 LINE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE K FLUID LOSS ININSP/MAINT 1 SO25585FE 48481 CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, A CRACKED OF 1 1/4 INCH FOUND AT THE FUEL SHROUD LINE. CENTER CARGO COMPARTMENT, LEFT SIDEWALL AREA AT APPROXIMATELY AT STA Y= 1801, 1 1/4 INCH CRACKED AT THE FUEL SHROUD LINE REPAIRED PER FEDEX EA NR 1-2822-79763, FUEL SYSTEMS, FUEL SHROUDS AND DRAINS. CRACK REPAIR ON TUBE FOR TAIL TANK. 2L73 4F RTA22WE 20041116000402004111600040NM 2004 11 16 AWXA200401142 120041015A5310654581239 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, FOUND A 3/8 INCH CRACK IN SHEAR TIE AT BS 348, BETWEEN STR 20 RT AND STR 21 RT. MAINTENANCE REMOVED CRACKED SHEAR TIE AT BS 348, STR 20 - 21 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, & 8. 2L72 4F RTA16WE 20041116000522004111600052NM 2004 11 16 AWXA200401096 120041004A5270 WARNING LIGHT BOEING737 7373G7 1384595NM PAX DOOR FALSE INDICATIONA AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28157AW 23779 ON TAKEOFF ROLL AT LAS EN ROUTE FOR SFO, MASTER CAUTION LIGHT ILLUMINATED WITH FORWARD OR AFT ENTRY DOOR WARNING LIGHT ON FORWARD OVERHEAD PANEL, REJECTED TAKEOFF AT 90 KTS. MAINTENANCE PERFORMED FORWARD ENTRY DOOR ADJUSTMENT TEST IAW T/C F1C52002, OPERATIONAL CHECK WAS GOOD. ACCOMPLISHED HIGH ENERGY STOP/SEIZED BRAKE INSPECTION IAW T/C F8M32001, NO DISCREPANCIES WERE NOTED. 2L72 4F RTA16WE 20041116000552004111600055WP 2004 11 16 04FDEA02637 120040904A5730ARC04689 SKIN DOUG DC10 DC1010F 3022111WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN IAW DAC DWG ARC0468, BONDED SKIN AND DOUBLER IAW TPS 1001 REV E AND DAC DWG ARC0468 AND EA 9-5710-81448. ALODINED AND PRIMED CONTACT UPPER SURFACE IAW DC 10 SRM 51021-01 VOL II, MARKED FX ARC0468-9 FOR SKIN PART AND FX ARC0468 DOUBLER PART IAW FEDEX GMM 7-0-1001. REFERENCE N/R N01745. 2L73 4F A22WE 20041116000672004111600067EU 2004 11 16 AWXA200401101 120040926A5320D53480043205 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28657AW 1083 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND AT NUT PLATE HOLE ON FORWARD INBOARD CORNER OF R-2 DOOR SILL AT FS 66. MAINTENANCE CUTOUT CORRODED NUT PLATE HOLE ON R-2 DOOR SILL AT FS 66; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW ER 26-5341-04279-RC2. 2L72 4F RTA28NM 20041116000702004111600070WP 2004 11 16 04FDEA02930 120041014A5753ARC0154 HINGE DOUG DC10 DC1010 3022110WP LT INBD FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 BFM CLOSE R COMPLY WITH EA 8-5750-82054 WINGS, INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE ASSY ENT BY: 497234 RPT BY: 497234 FACT 14OCT04 05:49. BFM U COMPLIED WITH EA 8-5750-82054 WINGS INBD FLAP REWORK OF UPSTOP MOUNT HOLES IN ARC0154 HINGE ASSY AT MAE ENT BY: 497234 RPT BY: 497234. 2L73 4F A22WE 20041116000752004111600075NM 2004 11 16 2004UALA00985 120041027A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE CARGO BAY DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 AFT CARGO PIT FRAME AT BS 1340 AND STR 26L DENTED UPPER INBD FLANGE. TYPICAL DENT DAMAGE FROM CARGO LOADING. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041116000832004111600083NM 2004 11 16 AWXA200401188 120041031A26126130348 WIRE BOEING737 737300 1384610NM ZONE 701 BROKEN A AWXAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 WP28331AW 23747 DURING TAXI OUT, THE "APU DET INOP" ANNUNCIATOR LIGHT ILLUMINATED INTERMITTENTLY, SWITCHED APU TO OFF AND APPROXIMATELY 2 MINUTES LATER RECEIVED AN APU FIRE INDICATION. PULLED APU FIRE HANDLE AND DISCHARGED THE APU FIRE BOTTLE. MAINTENANCE TROUBLESHOT AND FOUND FIRE DETECTION WIRE BROKEN AT GROUND IN APU BAY UNDER TUB ISSUED MEL 26-8, COND. 1. "APU FIRE DETECTION SYSTEM INOP". WHEN AIRCRAFT ARRIVED IN PHX FIRE DETECTION WIRE WAS RETERMINATED, FIRE BOTTLE REPLACED, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116000882004111600088NM 2004 11 16 AWXA200401151 120040930A5330141N3311 BEAR STRAP BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 LCQ - MAJOR REPAIR - DURING C-10 CHECK A 3/8 INCH CRACK WAS FOUND IN BEAR STRAP AT FORWARD UPPER CORNER OF L-1 DOOR CUTOUT BETWEEN BS 333 AND BS 350. MAINTENANCE TRIMMED OUT CRACK IN BEAR STRAP AT FORWARD UPPER CORNER OF L-1 DOOR AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A FILLER, DOUBLER, TRIPLER, AND SHIMS; INSTALLED REPAIR PARTS IAW ER 19-5312-04790-RC3. 2L72 4F RTA2NM 20041116000922004111600092NM 2004 11 16 04FDEA03056 120041109A5311 FRAME BOEING727 72722 1384002NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FRAME BS 1030 LT AT STR 24 AND 25, DENTED. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 20041116000962004111600096NM 2004 11 16 04FDEA02742 120040919A5347ACA7104517 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 MAIN DECK, SEAT TRACK AT STA Y= 715, X= -7.5 FOUND BASE DAMAGED. MAIN DECK, DAMAGED SEAT TRACK REMOVED FROM STA Y= 655 TO STA Y= 735 X= -7.5 PER SRM 51-31-01. SEAT TRACK FABRICATED PER SRM 50-70-00 VOLUME I, FIGURE 1. SEAT TRACK INSTALLED PER SRM 51-31-01. 2L73 4F RTA22WE 20041116001002004111600100EU 2004 11 16 04FDEA02746 120040920A5330A53985240204 SKIN AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25421FE 342 AFT FUSELAGE SKIN EXTERIOR BETWEEN FRAME 90-91 AND STRINGER 5 LT TO 8 LT CORROSION FOUND ON FASTENERS HEAD AND SKIN EXTERIOR SURFACE. ENT BY: 275296 RPT BY: 275296 FACT 20SEP04 05:35 SIN U REPAIR CARRIED OUT PER EA 6-5310-77951. RII BY L3420(SIAEC). ENT BY: 275296 RPT BY: 275296 2L72 4F RTA35EU 20041116001022004111600102NM 2004 11 16 AWXA200401174 120041014A53206517684642 INTERCOSTAL BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 1 1/16 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 294, STR 7 L/H. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 294, STR 7 LEFT; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW ER 03-5311-04295-ES1. 2L72 4F RTA16WE 20041116001052004111600105NM 2004 11 16 04FDEA02815 120040924A5511ALC8121 SPAR CAP DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 1 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000 C3 PT1 FIGURE 03. CORROSION REPAIRED AS PER EA 1-5510-80352 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 1L, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041116001062004111600106EU 2004 11 16 04FDEA02816 120040925A7714636014601 TACHOMETER AIRBUS300 A300B4605R 3930308EU NR 2 ENG N1 MALFUNCTIONED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25654FE1123011230 738 ON TAKEOFF SETTING OF STANDARD POWER, ENG 2 N1 GAUGE STOPPED AT APPROX 80 PERCENT (ANALOG/DIGITAL). RTO AT APPROX 100 KTS, NO ADVERSE YAW NOTED. ALL OTHER ENG 2 GAUGES APPEARED NORMAL AND CLOSE TO ENG 1 READINGS, ENT BY: 446285 RPT BY: 075405 FACT. REMOVED AND REPLACED NR 2 N1 GAUGE OPS CK OK REF A300MM 77-11-21-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 63601-460-1, POS NR 2 SRL 1134, TAG 660518, ON MFG 63601-460-1, SRL 1026, TAG 650528. 2L72 4F RTA35EU 20041116001152004111600115EU 2004 11 16 AWXA200401240 120041022A5330D53230345200 SKIN AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON SKIN IN FORWARD CARGO COMPARTMENT BETWEEN STR 39 LT AND STR 42 LT, FS 33 AND FS 34. MAINTENANCE CUTOUT DAMAGE IN SKIN BETWEEN STR 39 LT AND STR 42 LT, FS 33 AND FS 34; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW A320 SRM 53-00-11, FIG 220. 2L72 4F RTA28NM 20041116001232004111600123NM 2004 11 16 04FDEA02479 120040814A5711ARB74132 SPAR CAP DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER ABOUT XORS= 1090 TO XORS= 1094 FOUND WITH CORROSION AND FIXED TRAILING EDGE PANEL FOUND BULGING. RT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER XORS= 1090 TO XORS= 1094 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041116001322004111600132WP 2004 11 16 04FDEA02484 120040816A5330ADA3139501 SKIN DOUG DC10 DC1010F 3022111WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 RIGHT HAND PRIMARY STATIC PORT HAS EXTERNAL DOUBLER WITHIN 18 INCHES OF CONTROLLED AREA AT FOUR O'CLOCK POSITION AT FUSELAGE STATION 869 AT LONGERON 48 RIGHT. REMOVED AND REPLACED SKIN AND DOUBLERS IAW FEDEX EA 8-5330-81438, FUSELAGE SKIN SPLICE REPAIR AT STA 913 L48R TO CARGO DOOR CUTOUT REPAIR. REFERENCE NON-ROUTINE N00312. 2L73 4F A22WE 20041116001382004111600138NM 2004 11 16 04FDEA01834 120040621A5512ALC8101502 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 EMPENNAGE, RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT HOLE FOUND WITH CORROSION ON BOTTOM AND FOUND EXCEEDED LIMIT PER S/B MD-11 55-023. EMPENNAGE, RIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE REPAIRED AS PER FEDEX EA 1-5510-78028, TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 5R, BLEND OUT EXCEEDING LIMITS IN THE FLOOR OF THE BORE (MD-11 S/B 55-023 REV 1). 2L73 4F RTA22WE 20041116001462004111600146NM 2004 11 16 AWXA200401183 120041008A534069489856 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 5/16 INCH CRACK WAS FOUND IN FRAME TO STRINGER ATTACH CLIP AT BS 360, STR 11 LT. MAINTENANCE REMOVED DAMAGED FRAME ATTACH CLIP AT BS 360, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-48985; INSTALLED REPAIR PART IAW ER 03-5312-04295-RC3. 2L72 4F RTA16WE 20041116001492004111600149EU 2004 11 16 AWXA200400847 120040803A2150 POPPET VALVE AIRBUS320 A320232 3930326EU ZONE 192 WORN A AWXAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 WP28664AW 1162 1621 AFTER TAKEOFF FROM PHX EN ROUTE FOR IAH, HEARD A LOUD AIR NOISE IN CABIN AND RATE OF CLIMB INCREASED TO 1000 FT PER MINUTE. HAD NO AIRFLOW IN COCKPIT, TURNED OFF RT PACK PER MX CONTROL, THERE WAS NO INCREASE IN FLOW FROM LT PACK, WHEN HIGH PRESSURE VALVES OPENED AIR FLOW INCREASED. THE LT PACK WAS ALREADY ON MEL, TURNED BACK TO PHX FOR REPAIR. MX TROUBLESHOT PACK PROBLEMS AND FOUND RT PACK CONTROLLER FAULTING DURING TEMPERATURE CONTROL TEST. REMOVED AND REPLACED RT PACK CONTROLLER IAW AMM 21-51-34. MEL ON LT PACK (HOT AIR FAULT) WAS CORRECTED BY REPLACING TRIM AIR VALVE (14HK) IAW AMM 21-63-19. DURING TROUBLESHOOTING FOUND THE RE-CIRCULATION FILTER DIRTY, REPLACED FILTER. 2L72 4F RTA28NM 20041116001512004111600151EU 2004 11 16 AWXA200400964 120040820A5320D5348004320300 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28655AW 1075 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FORWARD INBOARD END OF R-2 DOOR SILL AT FS 66. MAINTENANCE REMOVED 2 EACH ANGLES ON R-2 DOOR SILL AT FR 66 AND CUTOUT CORROSION ON SILL; FABRICATED A NEW 2 EACH REPAIR ANGLES AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14. 2L72 4F RTA28NM 20041116001552004111600155WP 2004 11 16 04FDEA02728 120040915A3610 DUCT DOUG MD10 MD1010F 3022112WP NR 2 ENGINE LEAKING A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25398FE 46634 DURING CLIMB-OUT LEVEL1 ENG 2 ANTI-ICE DISAGREE OCCURRED 3-4 TIMES. EN ROUTE AT FL310 AIR MANF 2 FAIL LEVEL 3 DUMPED 10K, LANDED AT KDEN AS PER RED TABS. AIR SYS CONTROLLER SHUTOFF BLEED AND PACK AT ALTITUDE NR 2 MANIF FAILED PRESSURE DECAY TEST PER MM 36-00-01-5. FOUND NR 2 ENG AIR DUCT AAM7414-1 IN FWD LEFT SIDE OF CTR CARGO COMPT LEAKING. REMOVED AND REPLACED HYD CLAMPS AND AIR LINE CLAMPS ON TWO VERTICAL BRACES NEXT TO AFT END OF DAMAGED DUCT. ALSO, REMOVED TOP AND BOTTOM FASTENERS ON TWO BRACES TO ALLOW R/R`D OF MANIFOLD DUCT. INSTALLED NEW DUCT PERFORMED PNEUMATIC SYS NR 2 DECAY, TEST IAW MD-10-10 M/M SUPP 36-00-02-5 AND WING ANTI-ICE SYS TEST IAW MD-10-10 M/M 30-11-00-5. BOTH TESTS PASSED. 2L73 4F RTA22WE 20041116001692004111600169NM 2004 11 16 04FDEA02970 120041022A275118129952F1 INDICATOR BOEING727 727227 1384078NM TE FLAPS MALFUNCTIONED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25487FE 21490 INBOARD FLAP ASYM INDICATION UPON RETRACTION. REMOVED AND REPLACED INBD FLAP POSITION INDICATOR PER MM 27-52-021-2, OPS CHECK NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 18-1299-5-2F1 POS 2 SRL 0778AN TAG 680660 ON MFG 2061-13-1 SRL 252 TAG 258731. 2L73 4F A3WE 20041116001742004111600174EU 2004 11 16 MALA040668 120041101A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 IS CORRODED BETWEEN FS 294-339. TRACK WAS REPLACED IN THIS AREA IAW MESABA EO S53060. A/C WAS RELEASED 11/07/04. 2L72 4T RTA52EU 20041116001772004111600177NE 2004 11 16 P55CA0401273 220041107A7321R41013764 ACTUATOR BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FUEL CONTROL MALFUNCTIONED A P5CAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP23920FT 22237 702192 IN CLIMB AT 9200 FT, NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASHES OF LIGHT FROM LT SIDE. WIND MILL TIME 50 MINUTES, OIL PRESSURE 5 PSI, N1 22 PERCENT N2 18 PERCENT, FIRE SWITCHED PULLED & NR 1 EDP SUPPLY OFF. REVIEWED EXCEEDANCE FOUND TO BE WITHIN LIMITS, ENGINE VISUAL INSPECTION ACCOMPLISHED, FOUND FUEL CONTROL ACTUATOR C/B OPEN. REPLACED FUEL CONTROL MOTOR ACTUATOR PER AMM 73-00-00, PERFORMED ENGINE RUN UP OK. 2L74 4F4 F A20WE E3NE 20041116001792004111600179NM 2004 11 16 UPS04443443 120041029A5315 FLOORBEAM BOEING747 747200 1384847NM ZONE 222 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D BS 330, BET STR 13-14R, APPROX RBL 70-75 FLOORBEAM WEB FOUND CRACK. U/D FLOORBEAM WEB REPAIRED AS PER SRM 53-10-07 FIG 11. 2L74 4F RTA20WE 20041116001842004111600184EU 2004 11 16 MALA040672 120041103A3297 DIODE BAC 146 AVRO146RJ85A1500097EU MLG INDICATOR SHORTED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15510XJ E2323 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. WITH GEAR HANDLE UP, RED INTRANSIT LIGHT ON, GREEN DOWN AND LOCKED (3) REMAINED ON C/B B2 POPPED. MAINTENANCE FOUND DIODE BLOCK SHORTED. SWAPPED PINS A-B TO SPARE DIODE AT GC2 BLOCK IAW AMM. COMPLETED OPERATIONAL CHECKS OF LANDING GEAR CONTROL SYSTEM IAW AVRO AMM 32-30-00. ALL CHECKS GOOD. 2H74 4F RTA49EU 20041116001852004111600185EU 2004 11 16 MALA040674 120041104A2910HTE95313 ISOLATION VALVE BAC 146 AVRO146RJ85A1500097EU HYD SYSTEM MALFUNCTIONED A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15532XJ E2366 GREEN HYDRAULIC HIGH TEMP LIGHT ILLUMINATED. QRH FOLLOWED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED ISOLATION VALVE IAW AMM 29-30-00-01. P/N ON & OFF HTE9531-3, S/N ON FRO33BC, OFF FRO42BC. OPS CHECKS GOOD. NO LEAKS NOTED. 2H74 4F RTA49EU 20041116001912004111600191EA 2004 11 16 COMA0460611 120041031A4900 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SHUTDOWN A COMAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01952CA 7092 FLIGHT 5028 APU SHUTDOWN. COULD NOT DUPLICATE. APU OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041116002002004111600200NM 2004 11 16 UPS04443487 120041029A5311 DOUBLER BOEING747 747200 1384847NM FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C M/D- LEFT BS 400 FRAME S15L DOUBLER CRACKED AT STR CUTOUT. DOUBLER REPAIRED AS PER HX RS R53-10-35210 AND UPS EO B747-5310-21303-A. 2L74 4F RTA20WE 20041116002082004111600208NM 2004 11 16 UPS04443340 120040926A5315 FLOORBEAM BOEING747 747121 1384871NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, FWD CARGO STA 840 RBL 30 FLOOR SUPPORT CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 2. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20041117000212004111700021NM 2004 11 17 UPS04243257 120040924A5321 FLOOR PANEL BOEING727 72722C 138400FNM E/E BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C, E/E FLOOR PANEL RIGHT SIDE BS 440 TO 400 HAS ONE CRACK. CRACK STOP DRILLED IAW 51-10-1. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACK CONTAINED. AREA REPAIRED IAW SRM 51-40-2. 2L73 4F A3WE 20041117000422004111700042NM 2004 11 17 UPS04443329 120040927A5710 SPLICE BOEING747 747121 1384871NM WING SPAR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT BS 1241 STR R28 UPPER WING REAR SPAR SPLICE PLATE HOLE NR 4 FOUND CRACK AT SPLICE PLATE AT 12 O'CLOCK POSITION APPROX 0.080 INCH LONG. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032 & RIGHT SPLICE PLATE REPLACED AS PER EO B747-5740-4366 DUE NR 5 HOLE ON SPLICE PLATE CRACK EXCEED LIMIT. 2L74 4F A20WE 20041117000442004111700044NM 2004 11 17 UPS04443331 120040924A5712 RIB BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT WING L/E NR 17 VC FLAP O/B ARM O/B ROTARY ACTUATOR SUPPORT RIB AT ILES 764 APP. FOUND UPPER CHORD MID SPAN AREA CRACK AS MARKED. L/E RIB REPAIRED AT ILES 764 AS PER SRM 57-20-03 FIG 3. 2L74 4F A20WE 20041117000452004111700045NM 2004 11 17 UPS04443332 120040924A531065B017072 SPLICE BOEING747 747121 1384871NM FUSELAGE FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D BS 280, S22-23R FRAME SPLICE FOUND CRACK. BS 280 STR 22 TO 23R FRAME SPLICE REPLACED AS PER SRM 51-30-02. 2L74 4F A20WE 20041117000472004111700047NM 2004 11 17 AALA20041122 120041110A3350 LIGHT BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21631AA 24589 DFW - BOTH EMERGENCY LIGHTS AT SEAT 17 BROKEN. REPLACED LIGHT ASSEMBLY FOR BOTH EMERGENCY LIGHTS AT SEAT 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041117000482004111700048WP 2004 11 17 0401909953 120040922A5320 STIFFENER DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND CRACKS IN VERTICAL STIFFENERS AT BS 756 L28R, L28L AND ABOVE L26L. REPAIRED PER EA 99-200337. 2L72 4F A6WE 20041117000502004111700050NE 2004 11 17 MALA040605 220041002A7261200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 4 LEAKING A MALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15518XJ E2337 AIRCRAFT WAS IN FLIGHT WHEN NR 4 ENGINE OIL PSI AND QUANTITY WENT TO ZERO. CREW SECURED THE ENGINE AND LANDED IN MSP. CREW SHUTDOWN ENGINE, A/C DIVERTED TO MSP. OIL QUANTITY READ 0 OIL PSI BETWEEN 20 & 40 PSI N2 REMAINED AT APPROX 20 PERCENT. MAINTENANCE REMOVED & REPLACED NR 4 ENG P/N 2-003-040-15, S/N ON PO7742, OFF PO7864 IAW JOB CARD 7100-502 REF JOB CARD FOR OP'S & LEAK CHECKS. 2H74 4F4 FRTA49EU E6NE 20041117000512004111700051EU 2004 11 17 MALA040606 120040916A3230D49412001 CONTROL UNIT SAAB SF340 340B 7860101EU MLG MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15422XJ 340B422 LANDING GEAR WOULD NOT EXTEND, CYCLED BREAKER AND CHECKED GOOD. A/C TO BE FERRIED FROM LFT-MEM FOR REPAIR OF LANDING GEAR DISCREPANCIES. MAINTENANCE REPLACED LANDING GEAR CONTROL UNIT P/N ON AND OFF D494-12-001, S/N ON 64/4-96, OFF 673/05-98. ALL TESTS PASS, OK FOR SERVICE. 2L72 4T RTA52EU 20041117000522004111700052 2004 11 17 MALA040607 420040925A2565D31050105 SLIDE BAC 146 AVRO146RJ85A1500097EU GALLEY DOOR DISLODGED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15522XJ E2347 GALLEY DOOR SLIDE FELL OFF AND HIT THE GROUND WHEN THE DOOR WAS OPENED. MAINTENANCE REPLACED DOOR SLIDE ASSEMBLY RT FWS PAX DOOR. P/N D31050-105. ALL CHECKS GOOD AT THIS TIME. 2H74 4F RTA49EU 20041117000552004111700055EU 2004 11 17 MALA040628 120040904A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON VERTICAL FLANGE OF SEAT TRACK BL 18.3 STA 298 ABOVE FLOORBOARD. REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117000572004111700057EU 2004 11 17 MALA040624 120041014A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15443XJ 340B443 DURING 4K INSPECTION IN BNA, NOTED LT UPPER FLANGE OF FRAME STA 258 (FUSELAGE) CORRODED. REPAIRED IAW EO S53108. 2L72 4T RTA52EU 20041117000602004111700060WP 2004 11 17 UPS04843056 120040724A5320 WEB DOUG DC8 DC871F 302199DWP MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, LEFT MAIN LANDING GEAR WHEEL WELL, AFT AND BEHIND FLAP CABLE DRUM WEB IS CORRODED. REMOVED AND REPLACED LEFT STA 3 FLAP SUPPORT FITTING AND REPAIRED CORRODED WEB. 2L74 4F RT4A25 20041117000612004111700061WP 2004 11 17 UPS04843057 120040715A5230 FIRST AID KIT DOUG DC8 DC871F 302199DWP C1 DOOR WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE: C3, C-1 DOOR FWD LOWER GUIDE PIN FITTING WORN. REMOVED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. ORIG MAT .250 IAW DAC DWG 5754075 MAT REMAINING .130, LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20041117000632004111700063NM 2004 11 17 SWAA043296 120041110A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 827, BS 907, STRINGER 8L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041117000652004111700065NM 2004 11 17 UPS04443466 120041101A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D - BS 480-520 RBL 62 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 8 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS. REPAIR PER SRM 53-10-05 FIG 1A. CIC APPLIED IAW UPS EO M-5100-2780-E. 2L74 4F RTA20WE 20041117000662004111700066NM 2004 11 17 UPS04443467 120041101A531165B01716511 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D - BS 460 LT FRAME O/B CHORD FOUND CRACKED BETWEEN STR-12A & STR-13. BS 460 LEFT O/B CHORD REPLACED PER SRM 51-10-01. 2L74 4F RTA20WE 20041117000672004111700067NM 2004 11 17 UPS04443468 120041029A531065B01715558 SHEAR ANGLE BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 440, APPROX STR 16L, FRAME ATT SHEAR ANGLE FOUND CRACK. CRACKED SHEAR ANGLE REPLACED PER SRM 51-10-01. 2L74 4F RTA20WE 20041117000682004111700068WP 2004 11 17 UPS04843279 120041005A3397 WIRE DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSDAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 INSPECTION TYPE:N/A FLT DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND REPAIRED WIRE TO PIN 9 OF CONNECTOR P1-1345, OP CHECK'S GOOD PER MM 33-50-01-2. 2L74 4F RT4A25 20041117000692004111700069WP 2004 11 17 UPS04843280 120041004A5320 WEB DOUG DC8 DC871F 302199DWP SUBFLOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE:C2 AC BAY SUBFLOOR WEB CRACKED BETWEEN STA 8 & STA 16 AT L21L. REPAIRED IAW DC-8 SRM 51-1-21A & UPS EO DC8 5350-7876-A. 2L74 4F RT4A25 20041117000782004111700078NM 2004 11 17 SWAA043302 120041111A3350101114 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29353SW 24889 DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20041117000792004111700079NM 2004 11 17 SWAA043303 120041111A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041117000802004111700080NM 2004 11 17 SWAA043304 120041111A53306545766 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C1 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 270, STRINGER 16L AND BS 945, STRINGER 24L. REPAIRED SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041117000812004111700081 2004 11 17 SWAA043305 420041111A2565D31354 SLIDE BOEING737 7373A4 1384585NM R1 &R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C1 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041117000822004111700082NM 2004 11 17 SWAA043306 120041111A3350604222 BATTERY BOEING737 7373A4 1384585NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C1 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP WITH FWD AND AFT SWITCHES. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041117000872004111700087NM 2004 11 17 UPS04443083 120040818A5320654U613114 STRAP BOEING747 747212B 1384886NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, FX- BS 1241 LEFT WL 174-170 BETWEEN FX EXTERNAL INTERNAL LONGERON AREA FITTING ATTACH SPLICE STRAP FOUND CORROSION AS MARKED. CORROSION BLEND OUT WITH REMAIN THICKNESS 0.100 INCH REFER SB 747-53-2283 R4 SPLICE STRAP REPLACED EO B747-5310-1093-N. 2L74 4F A20WE 20041117000882004111700088NM 2004 11 17 UPS04443090 120040909A335090084 POWERPACK BOEING747 747200 1384847NM EMERGNECY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 2 AFT MOST O/H EMERGENCY LIGHTS IN UPPER DECK INOP. FOUND POWER PACK RIGHT SIDE STA 630 MAIN DECK INOP. PANEL LOWERED, PACK NTS. REF REQ A822639 JP VAUGHN 95768. CHARGED BATTERY PACK, CHECKS GOOD. 2L74 4F RTA20WE 20041117000902004111700090NM 2004 11 17 SWAA043309 120041111A5753 SKIN BOEING737 7375H4 138449DNM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 1178 26568 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041117000922004111700092NM 2004 11 17 SWAA043311 120041111A55306552490 BEAM BOEING737 7373H4 1384600NM VERTICAL STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB RT T/E BEAM AT STATION 79, CRACKED. REMOVED AND REPLACED BEAM SECTION PER SRM. 2L72 4F RTA16WE 20041117000932004111700093NM 2004 11 17 SWAA043312 120041111A531165C26402 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB AT RIGHT BS 727D TO RIGHT BS 727E, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20041117000942004111700094NM 2004 11 17 SWAA043313 120041111A53306518420 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND CAPTAINS NR 1 C-D WINDOW POST UPPER CORNER SKIN CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041117000962004111700096NM 2004 11 17 SWAA043315 120041111A57126545445 RIB BOEING737 7375H4 138449DNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RT WING RIB CHORD PER EA. 2L72 4F RTA16WE 20041117000972004111700097NE 2004 11 17 MALA040580 220040920A7261200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 3 LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15529XJ E2363 NR 3 ENG LOW PRESS LIGHT ILLUM INFLIGHT, COMFIRMED 25 PSI. SHUT DOWN ENG. ENG WINDMILLED AT 16 PERCENT N2 WITH ABOUT 5 PSE OIL PRESSURE. SHUTDOWN UNTIL LANDING TIME WAS 15-20 MIN. TIME BELOW 2 PERCENT WAS 5 MIN. RETURNED TO MEM. INSPECTED NR 3 ENG, FOUND .0625 INCH CHIP ON NR 4 BEARING SCAVENGE LINE. INSPECTED OIL PUMP & FOUND SHAFT SPLINES DAMAGED & APPEAR TO BE SPUN. A/C INSPECTED AND FOUND SAFE FOR FOR INTENDED FERRY FLIGHT FROM MEM TO MSP. NR 3 ENGINE CHANGE DUE TO OIL PRESSURE LOSS AND POSSIBLE OIL PUMP FAILURE. MX REMOVED & REPLACED NR 3 ENG P/N ON & OFF 2-003-040-15, S/N ON P07686, S/N OFF P07770 IAW J/C 7100-502, OPS CHECK GOOD. 2H74 4F4 FRTA49EU E6NE 20041117000982004111700098EU 2004 11 17 MALA040574 120040915A3230AIR123404 TORQUE LINK SAAB SF340 340B 7860101EU MLG WORN A MALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL15430XJ 340B430 UNABLE TO RETRACT LANDING GEAR WITHOUT PUSHING DOWNLOCK RELEASE. MAINTENANCE WHILE JACKING AIRCRAFT NOTED RT SHOCK STRUT FAILED TO EXTEND AND UPPER TORQUE LINK HAD EXCESSIVE PLAY. REMOVED AND REPLACED UPPER TORQUE LINK (P/N ON AIR123494, P/N OFF AIR123404, S/N ON PV082A381, S/N OFF PIP986) IAW SAAB AMM CH 32-11-15-4. SERVICED RT SHOCK STRUT IAW SAAB AMM CH 12-30-32-3. ALSO REMOVED AND REPLACED RELAY 8GA (P/N ON & OFF MS27400-17) OPS CHECK GOOD. 2L72 4T RTA52EU 20041117001002004111700100WP 2004 11 17 UPS04843365 120040920A532057738443 INTERCOSTAL DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, AFT MAIN CARGO FS 1750 L36 INTERCOSTAL FWD OF VERTICAL BEAM CRACKED. REMOVED INTERCOSTAL IAW SRM 51-1-21 & 51-3-0. FABBED INTERCOSTAL ON TRAVLER 0007 PER DWG 5773844. INSTALLED REPLACED INTERCOSTAL IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20041117001012004111700101WP 2004 11 17 UPS04843367 120040918A53203779762U501 FITTING DOUG DC8 DC871F 302199DWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, LONGERON 10R END FITTING CRACKED AT FS 674. REMOVED AND REPLACED LONGERON 10R END FITTING FS 674-680 IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20041117001042004111700104NM 2004 11 17 UPS04M43464 120041109A2820 ISOLATION VALVE DOUG MD11 MD11F 3023600NM TAIL TANK INOPERATIVE A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01250UP AT APPROX 4 HRS AFTER DEPARTURE, THE FUEL QTY/USED CHECK LEVEL 2 ALERT DISPLAYED. OBSERVED THAT FUEL TANK QUANTITY WAS APPROX 5000 LBS LESS THAN FUEL BURN AMOUNT FROM FUEL TOTALIZER. ISOLATED ALL TANKS AND OBSERVED THAT TAIL TANK QUANTITY CONTINUED TO DECREASE AT A RATE OF APPROX 100 LBS EVERY 5 MINUTES. DEFERRED TAIL TANK ISO VLV M291016. RE-ACTIVATED TAIL TANK ISO VALVE IAW SMP PROCEDURE 28-21-19. THIS CLEARS DEFERRAL M291016. 2L73 4F RTA22WE 20041117001102004111700110NM 2004 11 17 UPS04243032 120040826A5753 SUPPORT BRACKET BOEING727 727108C 1384039NM NR 5 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, SUPPORT BRACKET FOR NR 5 FWD FLAP TRACK FAIRING FOUND CRACKED ON O/B SIDE OF NR 5 FLAP TRACK. SUPPORT BRACKET REMOVED IAW SRM 51-30-02, NEW ANGLE FABRICATED IAW SRM 51-20-01, ANGLE PROTECTED IAW SRM 51-10-01, ANGLE INSTALLED ON FLAP TRACK IAW SRM 51-30-02. 2L73 4F A3WE 20041117001122004111700112NM 2004 11 17 UPS04443479 120041101A532065B01835110 SUPPORT FITTING BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D- BS 420 RIGHT FRAME STR 6 STOP SUPPORT FITTING FOUND CRACKED AS MARKED. STOP FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20041117001132004111700113NM 2004 11 17 UPS04443480 120041028A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, RIGHT BS 340 UPPER DECK FLOORBEAM, ONE HOLE CRACK FOUND AT FRAME WEB. ONE HOLE CRACK FOUND AT FLOORBEAM WEB BS 340 WL 280 TO 320. RIGHT BS 340 UPPER DECK FLOORBEAM WEB & FRAME WEB REPAIRED AS PER HX RS R53-15-35211 AND UPS EO B747-5310-21306-A. 2L74 4F RTA20WE 20041117001142004111700114NM 2004 11 17 UPS04443481 120041029A5711 SPAR BOEING747 747200 1384847NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, LT WING MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. LEFT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411. 2L74 4F RTA20WE 20041117001152004111700115NM 2004 11 17 UPS04443482 120041029A5311 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- BS 440, BELOW STR 31L, FRAME WEB FOUND CRACK. BS 440 STR 13L FRAME WEB SECTIONAL REPLACED PER HX RS R53-12-35212 FOR DETAIL AND UPS EO B747-5310-21298-A. 2L74 4F RTA20WE 20041117001162004111700116NM 2004 11 17 UPS04443483 120041030A53117075T60032IN DOUBLER BOEING747 747200 1384847NM FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- BS 440 BELOW STR 13L FRAME ATT DOUBLER FOUND CRACKED. BS 440 FRAME DOUBLER REPLACED PER HX RS R53-12-35212 FOR DETAIL AND UPS EO B747-5310-21298-A. 2L74 4F RTA20WE 20041117001172004111700117NM 2004 11 17 UPS04443354 120040921A5712 RIB BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RIGHT WING L/E OLES 1409 APPROX NR 25 V/C FLAP I/B ROTARY I/B SUPPORT RIB FWD MOUNT HOLE CRACK. RIGHT WING L/E OLES 1409 APPROX NR 25 VC FLAP I/B ROTARY ACTUATOR I/B SUPPORT RIB REPAIRED AS PER HX RS R-57-41-35202, DVI THE AFFECTED AREA AT C-CHECK INFORVALS NOT TO EXCEED 18 MONTHS FOR SIGNS OF CORROSION, CRACKS & DEGRADATION OF SUBJECT REPAIR, SEE DETAIL PER UPS EO B747-5740-21183-A FOR REFERENCE. 2L74 4F A20WE 20041117001182004111700118NM 2004 11 17 UPS04443355 120040923A5311141U1008303 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D- BS 360, S24-25L FRAME FOUND CRACK AS MARKED. FRAME SEGMENT REPLACED & REPAIRED AS PER HX RS R53-12-35203 & UPS EO B747-5310-21180-A. 2L74 4F A20WE 20041117001202004111700120NM 2004 11 17 UPS04443358 120040925A5312 BULKHEAD BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, LEFT BS 1480 BULKHEAD APU DUCT CUTOUT 1EA FASTENER HOLE CRACK FOUND RUNNING DOWNWARD APPROX 0.060 INCH LENGTH BS 1480, LBL 100. LEFT BS 1480 BULKHEAD APU DUCT CUTOUT WEB REPAIRED AS PER EO B747-5310-3100-C FIG 4. 2L74 4F A20WE 20041117001212004111700121NM 2004 11 17 UPS04443378 120040922A5313 STRINGER BOEING747 747121 1384871NM BATTERY BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, EMP- BATTERY COMPT RIGHT STR 13 AFT END FOUND CRACKED AT FS 2658. BATTERY COMPT RIGHT STR 13 & STRAPS REPLACED AS PER SRM 51-10-01 PG 8 AT BS 2658 AREA. 2L74 4F A20WE 20041117001232004111700123NM 2004 11 17 AALA20041094 120041103A3350D71701100 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21766AN 32880 EZE - EMERGENCY LIGHT PATH FROM ROW 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT 3R DOOR FOR EMERGENCY LIGHT PATH FROM ROW 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041117001242004111700124WP 2004 11 17 UPS04843452 120041010A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE: C3, RIGHT WING O/B L/E RIB IS CRACKED WITH CORROSION AT XFS 772.500. REMOVED FASTENERS AND CORROSION IAW DD-8 SRM 51-1-21 & 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG 19 & 57-2-0 FIG 2. 2L74 4F RT4A25 20041117001252004111700125WP 2004 11 17 UPS04843307 120040907A5320 CUSP WEB DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, HEAVY CORROSION ON CUSP, LT SIDE MAIN CABIN, STA 1153. REMOVED TEE ANGLE AND L-ANGLE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED FILLER IAW SAA SK772-604. INSTALLED FILLER AND REINSTALLED T-ANGLE & L-ANGLE IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20041117001282004111700128EU 2004 11 17 MALA040647 120041006A2560HC251H0368008 COVER BAC 146 AVRO146RJ85A1500097EU ESCAPE ROPE BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15525XJ E2350 THE ESCAPE ROPE LEFT PANEL IS BROKEN. CAPT ESCAPE ROPE COVER BROKEN AND KEEPS FALLING OUT. MAINTENANCE REPLACED LEFT ESCAPE ROPE PANEL P/N HC251H0368-008. 2H74 4F RTA49EU 20041117001302004111700130NM 2004 11 17 UPS04443322 120040928A5740 FITTING BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, LEFT BS 1241 WL 180 UPPER SPLICE PLATE NR 5 FASTENER HOLE TWO CRACKS REVEALED AT SPLICE PLATE MATING SURFACE BOTH CRACKS APPROX .25 INCH IN LENGTH. BOLT HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2L74 4F A20WE 20041117001312004111700131EU 2004 11 17 MALA040623 120041012A5320 RISER SAAB SF340 340B 7860101EU FLOOR SUPPORT CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15443XJ 340B443 DURING 4K INSPECTION IN BNA, FLOOR RISER LBL 18.3 STA 294.0 CORRODED AT LOWER END. REPAIRED IAW SRM 51-40-21 REFER TO NON-ROUTINE 210660/12518 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20041117001342004111700134NM 2004 11 17 UPS04443092 120040815A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, LT BS 340 UPPER DECK FLOORBEAM FOUND TWO EACH FASTENER HOLES CRACKED AT FRAME WEB BS 340 LT UPPER DECK FLOORBEAM CRACKED FRAME WEB REPAIRED AS PER HX RS R53-12-35182 & UPS EO B747-5310-20986-A. 2L74 4F A20WE 20041117001372004111700137NM 2004 11 17 UPS04443095 120040816A5311 FRAME BOEING747 747211B 1384809NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D: BS 400 STR 15L FRAME CRACKED. M/D- BS 400 STR 15L CRACKED FRAME REPAIRED AS PER HX RS R53-12-35187 & UPS EO B747-5310-20990-A. 2L74 4F RTA20WE 20041117001392004111700139NM 2004 11 17 UPS04443097 120040814A5313 LONGERON BOEING747 747212B 1384886NM RT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C, RT MLG WW OVERWING LONGERON UPPER SURFACE CORROSION REVEALED AT STA 1335, RBL 126. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.230 X 3.5 X 3.5 INCH, EXCEED SRM 53-10-01 FIG 1 LIMITS, LONGERON REPAIRED PER HX RS R53-41-35194 & UPS EO B747-5310-21016-A. CIC APPLIED IAW EO M5100-2780-E. 2L74 4F A20WE 20041117001402004111700140NM 2004 11 17 UPS04443112 120040912A3350 BATTERY PACK BOEING747 747121 1384871NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 20353 INSPECTION TYPE: C, EMERGENCY LIGHT INOP CREW SERVICE DOOR (ONE). REMOVED AND REPLACED BATTERY PACK X327 IAW 33-51-00, OPS NORMAL. 2L74 4F A20WE 20041117001442004111700144WP 2004 11 17 UPS04843101 120040819A53403755822U513 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C2, BATHTUB FITTING CORRODED AT STA 340 BETWEEN L35R & L34R. REMOVED BATHTUB FITTING PER SRM 51-1-20D. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING & REPAIR ANGLES PER SRM 51-1-20D, 53-2-0 FIG 2D. 2L74 4F RT4A25 20041117001472004111700147WP 2004 11 17 UPS04843165 120040830A53403649112 FITTING DOUG DC8 DC871F 302199DWP LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE:C2 LONGERON 36 END FITTING CRACKED AT STA 203. REMOVED AND REPLACED END FITTING REF DC8 SRM 51-1-20D. 2L74 4F RT4A25 20041117001522004111700152NM 2004 11 17 UPS04M43153 120040807A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 26 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM S/W BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 26 LT AT BEARING S/W BLENDED & REAMED TO 1.067 INCH, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING AS PER EO MD11-5510-19409-H. PR1 422B1/2 SEALANT APPLIED AT BLEND AREA & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 26 LT AS PER EO MD11-551 0-19409-H & EN:1291-04, FOUND SATISFACTORY. 2L73 4F RTA22WE 20041117001532004111700153NM 2004 11 17 UPS04M43154 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 1 RIGHT BARREL NUT HOLE FOUND CORROSION ON BOTTOM S/W & BEARING SURFACE. CORROSION AT NR 1 BARREL NUT HOLE RIGHT REMOVED, BLEND & REAMED TO 1.549 INCH, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT AFFECTED BARREL NUT HOLE NR 1 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT NR 1 BARREL NUT HOLE RIGHT PER EO MD11-5 510-19409-H & EN1256-04, FOUND SATISFACTORY. 2L73 4F RTA22WE 20041117001562004111700156NM 2004 11 17 UPS04243273 120040920A5340 FITTING BOEING727 72722C 138400FNM TAIL SKID CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE:C, SUSPECT CRACK FROM LT TERMINAL FITTING FOR STABILIZING LINK LWR IN TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02. 2L73 4F A3WE 20041117001572004111700157NM 2004 11 17 UPS04M43281 120040804A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 17 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION AT NR 17 LT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 17 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 17 LT PER EO MD11-5510-19409-H & EN 1288-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041117001592004111700159WP 2004 11 17 UPS04843308 120040903A531256119433N BULKHEAD DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, FWD SIDE OF FS 70 BULKHEAD LOWER CHORD HAS INTERGRANULAR CORROSION AT LONGERON 32R. FOUND INTERGRANULAR CORROSION OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. REMOVED STA 70 LOWER FWD CHORD BETWEEN LONGERONS 32R & 33R. FABRICATE AND ONE -9 DOUBLER AND TWO -11 SPLICE DOUBLERS IAW DC-8 SRM 53-2-5 FIG 8C. SPLICED IN NEW SECTION OF CHORD AND INSTALLED THE -9 DOUBLER & -11 SPLICE DOUBLERS IAW DC-8 SRM 53-2-5 FIG 8C. 2L74 4F RT4A25 20041117001602004111700160NM 2004 11 17 SWAA043323 120041112A3350101327 LENS BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND SIDEWALL EMERGENCY EXIT LIGHT LENS AT ROW 11 ABC, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041117001612004111700161WP 2004 11 17 AALA20041097 120041107A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 7D INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170404 49315 FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7D INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001632004111700163WP 2004 11 17 AALA20041095 120041104A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21479AA 49654 DEN - CEILING EMERGENCY LIGHTS AT STATIONS 1296 AND 1336 INOPERATIVE. REPLACED BATTERY PACK B527 FOR CEILING EMERGENCY LIGHTS AT STATIONS 1296 AND 1336. SYSTEM GROUND CHECKED NORMAL OPERTION. 2L72 4F A6WE 20041117001642004111700164NM 2004 11 17 UPS04M43291 120040729A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 25 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 25 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 25 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BULKHEAD NUT HOLE NR 25 RIGHT PER EO MD11-5510-19409-H & EN 1270-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041117001672004111700167NM 2004 11 17 UPS04543334 120041011A5730 PANEL BOEING757 75724APF 1384969NM LT WING BIRD STRIKE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01437UP 25468 BIRD STRIKE LEFT WING LWR INBOARD SURFACE PANEL. DAMAGE MEASURED MORE THAN 8 INCHES DIAMETER DELAMINATION 511FB. REMOVED PANEL 511FB FOR REPAIR TD0559172. REINSTALLED SAME PANEL WITH SERVICEABLE REPAIR FROM SIA. OK FOR SERVICE. 2L72 4F RTA2NM 20041117001682004111700168NM 2004 11 17 UPS04443447 120041101A5313BAC15171551 STRINGER BOEING747 747200 1384847NM ZONE 224 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D - BS 440-460 RIGHT STR-12 FWD END FOUND CRACKED & DEFORMED. CRACKED STRINGER REPLACED AT BS 440-460 RIGHT STR 12 PER SRM 51-10-01. P/N BAC1517-1551-2024T4. 2L74 4F RTA20WE 20041117001702004111700170WP 2004 11 17 AALA20041105 120041103A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 7D BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21575AM 53152 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT 7D IS BROKEN. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY FOR SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001722004111700172EU 2004 11 17 MALA040665 120041030A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, UPPER CAP OF BOTTOM FRAME AT FS 258 IS CORRODED AT FLOOR LEVEL AND WAS REPAIRED IAW MESABA EO S53102. A/C WAS RELEASED 11/07/04. 2L72 4T RTA52EU 20041117001732004111700173NM 2004 11 17 UPS04443369 120040924A5312 BULKHEAD BOEING747 747121 1384871NM LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LEFT MLG WW AFT BULKHEAD APU BLEED AIR DUCT CUTOUT I/B UPPER AREA CRACKED AT STA 1480, LBL 100. LEFT BLG W/W AFT BULKHEAD APU BLEED AIR DUCT CUTOUT WEB REPAIRED AS PER EO B747-5310-3100-C FIG 4. 2L74 4F A20WE 20041117001742004111700174WP 2004 11 17 UPS04843371 120040921A5340 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, MAIN CARGO FS 781 RBL 62 BOOT FITTING CRACKED AT RADIUS FWD AND AFT SIDES BELOW FLOORLINE. REMOVED BOOT FITTING AT FS 781 RBL 62 IAW SRM 51-1-21. FABRICATED BOOT FITTING IAW SAA SK 729-576. INSTALLED BOOT FITTING IAW SRM 51-1-20D & 51-1-8. 2L74 4F RT4A25 20041117001792004111700179WP 2004 11 17 AALA20041117 120041110A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21291AA 49303 DFW - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 26 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 23 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001822004111700182EU 2004 11 17 MALA040632 120040906A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK VERTICAL FLANGE BL 0 STA 298 ABOVE FLOORBOARD. REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117001842004111700184EU 2004 11 17 MALA040641 120040917A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15441XJ 340B441 DURING 4K INSPECTION IN BNA, NOTED DENT IN RIGHT FUSELAGE SKIN STA 339. REPAIRED IAW EO S53009. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041117001852004111700185EU 2004 11 17 MALA040644 120040930A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 6Y/4Y INSPECTION IN BNA, NOTED FLOOR FLANGE AT STA 294 BL 0 CORRODED. REPAIRED IAW SRM. AIRCRAFT RETURNED TO SERVICE 10/5/04. 2L72 4T RTA52EU 20041117001872004111700187EU 2004 11 17 MALA040635 120040909A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED ATTACH ANGLE DIPS AT FWD END OF SEAT TRACK BL 0 & LBL 18.3 CORRODED. FABRICATED AND INSTALLED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041115002312004111500231WP 2004 11 15 04FDEA02640 120040904A5730ARC0254501 PANEL DOUG DC10 DC1030F 3023504WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 LEFT WING LOWER TRAILING EDGE PANE 541KB DELAMINATED INTERIOR SURFACE. REMOVED INNER SKIN, OUTER SKIN, DOUBLER AND CORE IAW FEDEX EA 8-5750-81445. BONDED NEW INNER SKIN, OUTER SKIN DOUBLER AND CORE IAW FEDEX EA 8-5750-81445 AND TPS 1001 REV E, REFERENCE N/R N00794. 2L73 4F RTA22WE 20041116000132004111600013EU 2004 11 16 AWXA200400983 120040829A5321D5367320500000 FLOOR PANEL AIRBUS320 A320231 3930325EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND ON UPPER SURFACE OF AFT CARGO COMPARTMENT FLOOR PANEL 151DF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151DF, FS 50 TO FS 53, Y1292 LT TO Y1292 RT; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20041116000162004111600016EU 2004 11 16 AWXA200400986 120040815A5315D5347217220000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 LT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041116000282004111600028NM 2004 11 16 AWXA200401079 120040918A5321D5367228200200 FLOOR PANEL AIRBUSA319 A319132 3930340NM CARGO BAY CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, 2 EACH CRACKS WERE FOUND IN AFT CARGO COMPARTMENT FLOOR PANEL. MAINTENANCE REMOVED AFT CARGO COMPARTMENT FLOOR PANEL AT FS 56 TO FS 58, Y500 LT TO Y500 RT, AND FABRICATED A NEW REPLACEMENT PANEL IAW A319 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20041116000392004111600039NM 2004 11 16 AWXA200401141 120041001A5310654587512 CREASE BEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON R-1 DOOR OUTER CHORD (CREASE BEAM ANGLE) BETWEEN BS 299 AND BS 324, RBL 62, WL 209. MAINTENANCE REMOVED DAMAGED R-1 DOOR OUTER CHORD FROM BS 299 TO BS 324, RBL 62; FABRICATED A NEW REPLACEMENT CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3, 4, & 8. 2L72 4F RTA16WE 20041116000452004111600045NM 2004 11 16 04FDEA03047 120041108A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION (C53-224-01) AT FLOORBEAM UPPER CHORD AT BS 620, LBL 45-65, WL 208. 2L73 4F A3WE 20041116000492004111600049NM 2004 11 16 04FDEA02947 120041018A5753ARC74901 FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) BUSHING BORES EXCEEDED LIMIT. RIGHT HAND WING, INBOARD FLAP VANE OUTBOARD TEE FITTING, ALL (3) EXCEEDED LIMIT BORES REPAIRED AS PER EA NR 1-5750-77965, TITLE:WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, RIGHT HAND INBOARD FLAP VANE ATTACH FITTING REWORK.. 2L73 4F RTA22WE 20041116000632004111600063NM 2004 11 16 04FDEA03049 120041108A5310 SHEAR TIE BOEING727 727247 138408FNM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25233FE 21327 FOUND THE SHEAR TIE AT BS 380 BETWEEN STR 14 AND 15 TO REQUIRE REPLACEMENT DUE TO PREVIOUS CARGO NET BARRIER STRAP. INSTALLATION TO EXTEND UNDER THE FRAME AS OPPOSED TO OVER AS PER VENTURA AEROSPACE DWG 2987. REPAIRED PER SRM 53-10-4 FIG 11. 2L73 4F A3WE 20041116000722004111600072WP 2004 11 16 04FDEA02911 120041011A5753ARC01542 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 RIGHT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW FEDEX EA8-5750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME II. BEGINNING SURFACE 1.255 INCH. FINAL INBOARD 1.2400 INCH OUTBOARD 1.2360 INCH. MATERIAL REMOVED INBOARD .015 INCH OUTBOARD .019 INCH FOUND OUT OF LIMITS IAW DACCMM 57-44-07. SEE NR N00962. 2L73 4F RTA22WE 20041116000812004111600081NM 2004 11 16 AWXA200401187 120041027A5330 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING 4-DAY CHECK, A 2 3/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 747, STR 24 LT. MAINTENANCE CUTOUT CRACK IN FUSELAGE SKIN AT BS 747, STR 24 LT; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20041116000862004111600086NM 2004 11 16 AWXA200401149 120040930A533065184201046 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C18 CHECK, A 3/4 INCH CRACK WAS FOUND IN CAPTAINS WINDSHIELD OUTBOARD POST AT UPPER CORNER BS 217, WL 259.5. MAINTENANCE CUTOUT DAMAGED SKIN AT UPPER OUTBOARD CORNER OF CAPTAINS WINDSHIELD; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY THAT NO CRACKS EXIST; FABRICATED A FILLER AND A DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-01, FIG 210. 2L72 4F RTA16WE 20041116000892004111600089NM 2004 11 16 04FDEA03053 120041108A2997861555 RECEPTACLE CANNON DOUG MD11 MD11F 3023600NM HYD PUMP BURNED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25608FE3564 3564 48548 NR 1 AUX HYD PUMP ELECTRIC POWER PLUG WAS FOUND BURNED. ENT BY: 500170 RPT BY: 500170 FACT 09NOV04 00:50 TPE R NR 1 AUX HYD PUMP PLUG REPLACED PER SMP AND PER MD-11, W/D 29-21-01 WIRING CHECKED NML. PRECAUTIONARY RCCB (B1-625) AND NR 1 AUX HYD PUMP REPLACED ALSO. PREMATURE REMOVAL/INSTALLATION OFF MFG 86155. 2L73 4F RTA22WE 20041116000942004111600094NM 2004 11 16 04FDEA03058 120041109A5714 PANEL DOUG MD11 MD11 3023602NM WING CENTER BOX CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25627FE 48446 FOR SAME DEFECT AND RECOMMENDED ACTION SEVERAL CORROSION ON PANEL ASSY UPPER SKIN CTR BOX WING. 2L73 4F RTA22WE 20041116000952004111600095NM 2004 11 16 04FDEA03059 120041109A5714 SKIN DOUG MD11 MD11 3023602NM WING CENTER BOX CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25627FE 48446 SEVERAL CORROSION ON PANEL ASSY UPPER SKIN CTR BOX WING. 2L73 4F RTA22WE 20041116001092004111600109WP 2004 11 16 04FDEA02819 120040927A5730ARC0264507 PANEL DOUG DC10 DC1010F 3022111WP WING DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL BY FABRICATING AND BONDING NEW INNER SKIN, OUTERSKIN, DOUBLER AND CORE IAW DC10 DRAWING ARC0264 AND EA8-5710-77620. 2L73 4F A22WE 20041116001142004111600114NM 2004 11 16 AWXA200401118 120041004A5320141N5160478 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-10 CHECK, INTERGRANULAR CORROSION WAS FOUND ON AFT SIDE OF AFT THRESHOLD DRAIN OF R-1 DOOR THRESHOLD (INTERCOSTAL) AT NUT PLATE HOLES BS 370, WL 208.1. MAINTENANCE REMOVED CORRODED INTERCOSTAL AT BS 337, WL 208.1; FABRICATED AND INSTALLED A NEW REPLACEMENT INTERCOSTAL PER DWG 141N5160. 2L72 4F RTA2NM 20041116001222004111600122NM 2004 11 16 04FDEA02670 120040910A5512ALC8103503 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 31 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31L. REPAIRED AS PER EA NR 1-5510-80358, TITLE: HORIZONTAL STABILIZER BARREL NUT BORE 31L. REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041116001362004111600136NM 2004 11 16 04FDEA01832 120040621A5512ALC81012 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 10 BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78022 TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 10R - CORROSION REPAIR PER BOEING SB MD-11 55-023 REV 1 AND FEDEX EO 1-5510-7-5000. 2L73 4F RTA22WE 20041116001372004111600137NM 2004 11 16 04FDEA01833 120040621A5512ALC8103502 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND BARREL NUT NR 28 BEARING AND BOTTOM SURFACE CORROSION BLENDED OUT EXCEEDED LIMIT. EMPENNAGE, HORIZONTAL STABILIZER RIGHT HAND NR 28 BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-78029, TITLE: STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE NR 28R, THIN FLOOR CONDITION, BORE THROUGH, (MD-11 S/B 55-023 REV 1). 2L73 4F RTA22WE 20041116001422004111600142NM 2004 11 16 AWXA200401179 120041030A33501012621 LIGHT BOEING737 737277 1384570NM R2 DOOR INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 FLIGHT CREW REPORTED R-2 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116001452004111600145NM 2004 11 16 AWXA200401182 120041011A53406916970501 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN FRAME TO STRINGER ATTACH CLIP AT BS 348, STR 15 LT. MAINTENANCE REMOVED DAMAGED FRAME ATTACH CLIP AT BS 348, STR 15 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 69-16970; INSTALLED REPAIR PART IAW ER 03-5312-04295-RC3. 2L72 4F RTA16WE 20041116001522004111600152NE 2004 11 16 04FDEA02725 220040917A75326272484 BLEED VALVE AIRBUS300 A300B4622 3930401EU IAE V2524 V2524A5 NE NR 1 ENGINE MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25716FD2135 2135 358 BLEED VALVE 1 FAULTED AFTER TAKEOFF. NO RESET, RAN NR 1 ENG AT THE GATE. NO FAULTS NOTED. RAN ENGS AT T/O POWER FOR 5 MIN. NO FAULTS NOTED. INTERROGATED PNEU SYST CONTROLLERS. NO FAULTS STORE IN MEMORY FOR ANY FLIGHT LEG, STILL T/S. TALKED TO MOCC. SINCE THERE WAS NO FAULTS STORED, AGREED TO REMOVE AND REPLACE THE CONTROLLERS AS PRECAUTIONARY. RAN ENG AT THE GATE, PERFORMED VALVE SWITCH OVER FROM HIGH STAGE TO LOW STAGE. OPS CK GOOD. NO FAULT NOTED IAW A300 JRH. 2L72 4F4 FRTA35EU E40NE 20041116001532004111600153NM 2004 11 16 04FDEA02726 120040918A5753ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING CRACKED. RT WING, OUTBOARD FLAP ATTACHMENT STOP FITTING REMOVED AND REPLACED PER SRM 51-31-01 VOLUME 1. 2L73 4F RTA22WE 20041116001592004111600159NM 2004 11 16 04FDEA02756 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.400 INCH, REMAINING THICKNESS=0.391 INCH, MATERIAL REMOVED=0.009 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041116001682004111600168NM 2004 11 16 04FDEA02504 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, AT XORS= 713 UPPER CHORD FOUND WITH CORROSION. LEFT WING, REAR SPAR, XORS= 713 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041116001822004111600182NM 2004 11 16 UPS04443446 120041101A5311 FRAME BOEING747 747200 1384847NM ZONE 222 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D - BS 360 RT FRAME WEB FOUND CRACKED AT STR-2A. THE CRACK WAS PREVIOUS REPAIRED PER SRM 54-40-02 FIG 1. THE CRACK CONFIRMED NIL ADDITIONAL CRACK BEYOND THE FASTENER HOLES. 2L74 4F RTA20WE 20041116001952004111600195WP 2004 11 16 UPS04843436 120041103A56105613217517 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 CAPTAIN'S SLIDING WINDOW OPENING MECH BROKEN. REPLACED CAPT'S CLEARVIEW WINDOW PER MM 56-10-03-4. 2L74 4F RT4A25 20041117000022004111700002NM 2004 11 17 SWAA043329 120041112A5753 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 1032 24185 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. 2L72 4F RTA16WE 20041117000162004111700016NM 2004 11 17 UPS04M43346 120041014A2612 CONTROL UNIT DOUG MD11 MD11F 3023600NM NR 1 ENG FIRE FALSE INDICATIONA IPXAO OTHER N FALSE WARNING DEDESCENT 1 SO01253UP INSPECTION TYPE:N/A DURING DESCENT NR 1 ENGINE FIRE WARNING (AUDIBLE ONLY) WAS OBSERVED BUT INTERMITTENT. THROTTLE WAS RETARDED TO IDLE. CONSISTENT WITH PROCEDURE & ALL INDICATIONS CEASED. ENGINE WAS LEFT AT IDLE, EMERGENCY WAS DECLARED & LANDING WAS UNEVENTFUL. SWAPPED APU FDCU WITH NR 1 ENG FDCU AND PERFORMED SYS OPERATION TEST PER AMM 26-11-02, SYS OPS CKS GOOD. OK FOR SERVICE. 2L73 4F RTA22WE 20041117000222004111700022NM 2004 11 17 UPS04243258 120040921A5312 PRESSURE PANEL BOEING727 72722C 138400FNM NOSE WHEEL WELL CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C, LT NOSE WHEEL WELL HAS CRACKS ON FASTENER ROW, BS 243, 4 INCHES BELOW FWD PRESSURE PANEL OPENING. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACKS CONFIRMED. FILLER AND DOUBLER FABRICATED AND INSTALLED IAW SRM 51-40-02. 2L73 4F A3WE 20041117000242004111700024WP 2004 11 17 UPS04843252 120040909A5712 RIB DOUG DC8 DC871F 302199DWP STUB WING CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, RT WING I/B STUB WING RIB XILD 42 HAS A DEEP CHAFF. REMOVED DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AROUND CUTOUT. FABRICATED REPAIR ANGLES (2 EA) & FILLER AND INSTALLED IAW DC-8 SRM 57-2- 0. 2L74 4F RT4A25 20041117000282004111700028WP 2004 11 17 UPS04843262 120040909A5320 PAN DOUG DC8 DC871F 302199DWP PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, RADIOGRAPHIC (X-RAY) INSP DETECTED A CRACK ON THE FWD LEFT EMERGENCY OV OVERWING EXIT ON THE UPPER AFT JAMB CORNER APPROX .562 INCH IN LENGTH. NDT VERIFIED CRACK EXISTS IN INTERNAL DOOR PAN. TRIMMED EDGE OF INTERNAL DOOR PAN TO REMOVE CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. TRIM OUT FOUND WITHIN LIMITS IAW DC-8 SRM 53-2-0 FIG 6. 2L74 4F RT4A25 20041117000292004111700029WP 2004 11 17 UPS04843263 120040903A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, POSSIBLE CRACK IN UPPER WING SKIN (LT) AT FASTENER ON AFT SIDE OF STRINGER 15, JUST O/B OF RIB AT XRS 74. NDT VERIFIED CRACK 1 INCH IN LENGTH. CUT OUT DAMAGED AREA 1.375 INCH DIAMETER. NDT VERIFIED NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED IAW DC-8 SRM 57-2-1. 2L74 4F RT4A25 20041117000342004111700034WP 2004 11 17 UPS04843492 120041113A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT INOPERATIVE A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01818UP 46108 CAPTAIN SLIDING WINDOW WILL NOT OPEN. LUBED UPPER CATCH ON SLIDING WINDOW. OP CHECKS GOOD. WINDOW OPENS EASILY. 2L74 4F RT4A25 20041117000372004111700037 2004 11 17 SWAA043318 420041112A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29649SW 27719 L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041117000412004111700041NM 2004 11 17 SWAA043322 120041112A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29325SW 23689 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041117000562004111700056EU 2004 11 17 MALA040633 120040909A5347 GALLEY TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON RT GALLEY INBOARD TRACK & PROFILE. REPLACED TRACK & PROFILE PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117000732004111700073NM 2004 11 17 UPS04M43289 120040822A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP INSPECTION TYPE: C, HORIZONTAL STAB NR 29 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 29 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.178 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 29 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 29 LEFT PER EO MD11-5510-19409-H & EN 1308-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041117000742004111700074NM 2004 11 17 UPS04M43290 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP INSPECTION TYPE:C, HORIZONTAL STAB NR 30 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 30 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 30 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 30 LEFT PER EO MD11-5510-19409-H & EN 1252-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041117000862004111700086EU 2004 11 17 UPS04143087 120040908A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY EXIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01130UP 0815 LAV EMERGENCY EXIT LIGHT INOP. RELAMPED LAV EMERGENCY EXIT LIGHT. 2L72 4F RTA35EU 20041117000892004111700089NM 2004 11 17 SWAA043308 120041111A3350101114 LAMP BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20041117000952004111700095NM 2004 11 17 SWAA043314 120041111A55536546874 DRAG BRACE BOEING737 7373H4 1384600NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB REAR SPAR BODY RT AND LT DRAG BRACES CORRODED. REMOVED AND REPLACED DRAG BRACES PER SRM. 2L72 4F RTA16WE 20041117001062004111700106EA 2004 11 17 COMA0460600 120041108A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 INTERCOSTAL AT FS 484.00 CRACKED AT RBL 36. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20041117001112004111700111WP 2004 11 17 UPS04843035 120040824A3350 LIGHT DOUG DC8 DC871F 302199DWP EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01705UP 45949 EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE ON PREFLIGHT TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL. 2L74 4F RT4A25 20041117001322004111700132NM 2004 11 17 UPS04243393 120041006A5280 DOOR BOEING727 727185C 138406NNM RT WING MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C, BRACKET CRACKED ON WING DOOR FWD OF HINGE CASTING. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-20-01. 2L73 4F A3WE 20041117001492004111700149WP 2004 11 17 UPS04843167 120040831A555156545017 ATTACH ANGLE DOUG DC8 DC871F 302199DWP HORIZONTAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE: C2, LEFT HORIZONTAL STAB L/E ATTACH ANGLE CRACKED AT LOWER I/B CORNER. REMOVED HORIZONTAL STAB SIDE ROLLER BEARING, TRACK, AND ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21 AND MM 55-10-00-2. INSTALLED NEW ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21. REINSTALLED SIDE LOAD ROLLER AND TRACK PER SRM 51-3-0, AND MM 55-10-00-2. 2L74 4F RT4A25 20041117001552004111700155EU 2004 11 17 MALA040630 120040905A5347 GALLEY TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON RT GALLEY INBOARD TRACK & PROFILE. REPLACED TRACK & PROFILE PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117001622004111700162EU 2004 11 17 MALA040653 120041024A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 DURING DENT REPAIR IN LAN, DENT IN RIGHT FUSELAGE AT SL1614, STA 309 2.5 INCHES BELOW 1ST CABIN WINDOW. REPAIRED PER EO S53259 & SAAB STATEMENT 340SDS007765. 2L72 4T RTA52EU 20041117001752004111700175WP 2004 11 17 AALA20041084 120041030A3350 CONTACTOR DOUG DC9 DC983 3022083WP BATTERY DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW219615W 53562 AISLE EMERGENCY LIGHT AT ROWS 5, 7, 13 AND 16 INOPERATIVE. CLEANED ELECTRICAL CONTACTS IN FORWARD CABIN EMERGENCY LIGHT BATTERY PACK FOR ROWS 5, 7, 13, AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041117001762004111700176NM 2004 11 17 AALA20041083 120041030A3350 CONNECTOR BOEING777 777223 1385213NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21751AN 30798 SEAT MOUNTED EMERGENCY LIGHTS AT 1G AND 3G INOPERATIVE. RESECURED LOOSE CONNECTORS UNDER SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041117001782004111700178NM 2004 11 17 UPS04443470 120041101A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C U/D - BS 480-520 RBL 44 SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. REPAIR PER SRM 53-10-05 FIG 1A. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F RTA20WE 20041117001832004111700183EU 2004 11 17 MALA040634 120040909A5320 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED WEB STA 288-294 CORRODED RBL 36 TO LBL 36. REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041117001902004111700190NM 2004 11 17 AALA20041071 120041025A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21950AN 30087 ORD - ALL AIRCRAFT EMERGENCY LIGHTS FAILED WHILE PERFORMING CARD 0299. REPLACED ALL BATTERY PACKS FOR ALL AIRCRAFT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20041117001912004111700191 2004 11 17 AALA20041077 420041027A256562771117 SLIDE BOEING777 777223 1385213NM L1 DOOR FAILED A AALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW21752AN 30260 GIG - DURING SERVICING L1 MAIN ENTRY DOOR WAS INADVERTENTLY DEPLOYED BY AGENT AND SLIDE FAILED TO INFLATE. SLIDE ASSEMBLY NOT AVAILABLE AT GIG FOR REPLACEMENT. DEACTIVATED LEFT ONE MAIN ENTRY DOOR AND PLACARD PER MEL 52 02. ISOLATED FIRST CLASS SEATS FROM ROWS 1 THROUGH 3 ACROSS. REPLACED L1 DOOR SLIDE IN MIA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041117001922004111700192WP 2004 11 17 AALA20041072 120041027A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21290AA 49302 PHX - BATTERY CHARGER AT STATION 902R FOR CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY AT STATION 902R FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001932004111700193EU 2004 11 17 AALA20041074 120041026A3260 PROXIMITY SENSOR AIRBUS300 A300B4605R 3930308EU MLG MALFUNCTIONED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW217062A 474 MIA - INFLIGHT T896/26 AFTER TAKEOFF ECAM INDICATED GEAR RETRACT WARNING. UNSAFE GEAR RETRACTION. AFTER GEAR WAS SAFELY DOWN AND LOCKED RECEIVED LANDING GEAR RETRACTION INOPERATIVE MESSAGE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PERFORMED BITE TEST OF PROXIMITY UNIT. NO FAULTS NOTED. CLEANED PROXIMITY DETECTORS ON RIGHT AND LEFT MAIN GEARS. REPLACED PROXIMITY DETECTOR UNIT AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041117001942004111700194WP 2004 11 17 AALA20041075 120041027A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21416AA 49327 DFW - OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY B549 FOR OVERWING EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001952004111700195WP 2004 11 17 AALA20041076 120041027A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21416AA 49327 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D AND 17D INOPERATIVE. REPLACED THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY AT 12D AND 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001962004111700196WP 2004 11 17 AALA20041078 120041028A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21487AA 49680 ATL - EMERGENCY LIGHTS FROM 20D TO 31D INOPERATIVE. REPLACED BATTERY PACK AT 20D FOR EMERGENCY LIGHTS FROM 20D TO 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001972004111700197NM 2004 11 17 UPS04243324 120041007A3350 BATTERY BOEING727 72725C 138400HNM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:N/A FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES, NO HELP. REMOVED AND REPLACED EMERGENCY EXIT ASSY & NEW BATTERIES INSTALLED. OPS CHECK OK. 2L73 4F A3WE 20041117002012004111700201EU 2004 11 17 MALA040567 120040904A7620231301201 CONTROLLER BAC 146 AVRO146RJ85A1500097EU OVERSPEED MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15529XJ E2363 AFTER TAKEOFF, REDUCED ENGINE NR 1 FAILED AT APPROXIMATELY 500 FT ENGINE SEEMED TO SIMPLY LOOSE POWER TO ZERO OIL PRESSURE. REMAINED AT 10 TO 12 PSI FOR REMAINDER OF FLIGHT. N2 MAINTAINED 15 PERCENT AND N1 MAINTAINED 25 PERCENT ENGINE FAILED IN MBS. MAINTENANCE COMPLETED WINDMILLING INSPECTION DURATION WAS LESS THAN 2 HOURS. INSPECTED ALL CHIP DETECTORS, FOUND RT OVERSPEED SENSOR P14 READING 2.8K. MAINTENANCE REPLACED OVERSPEED CONTROLLER P/N 2-313-012-01, S/N OFF 1280, S/N ON 970130701183 IAW 72-00-00-601 1M, 1C, 1M2 AS PRECAUTIONARY REPLACED HMA P/N 2-193-330-10, S/N OFF 98AGU716, S/N ON 4AGU261 IAW 7310-504. COMPLETED POWER CHECK. 2H74 4F RTA49EU 20041117002022004111700202EU 2004 11 17 MALA040640 120040916A5320 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15441XJ 340B441 DURING 4K INSPECTION IN BNA, NOTED WEB CORRODED STA 288-294. REPAIRED IAW THE SRM. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2L72 4T RTA52EU 20041117002032004111700203NM 2004 11 17 AALA20041120 120041111A33506011779 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21682AA 25339 DFW - OVERWING EMERGENCY LIGHT AT LEFT HAND MID WING INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT AT LEFT HAND MID WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041117002052004111700205WP 2004 11 17 AALA20041125 120041105A3350 SOCKET DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21430AA 49342 TUL - EMERGENCY ESCAPE LIGHTS IN OVERHEAD SWITCH PANEL INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY ESCAPE LIGHTS IN OVERHEAD SWITCH PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117002082004111700208NM 2004 11 17 0401466309 120040831A3350 LIGHT BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REPAIRED LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20041117002092004111700209EU 2004 11 17 MALA040636 120040909A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK LBL 18.3 STA 294 TO 310. REPAIRED IAW EO S53079. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20050114000272005011400027EU 2005 1 14 SA04087 120040917A3350CM44 BULB AIRBUS320 A320214 3930316EU EMERGENCY LIGHT BURNED OUT A USAAK NONE L NO TEST ININSP/MAINT 1 EA19102UW 844 PIT - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. THE AFT EMERGENCY POWER SUPPLY UNIT SHOWS INT AND EXT FLASHING RED LED'S. THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT, MID-CABIN INDICATES A CONTINUOUS RED LED. MAINTENANCE PLACED SYSTEM ON MEL. RELAMPED EMERGENCY LIGHT ASSEMBLIES FIN 32WL AND FIN 33WL. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041117002152004111700215NM 2004 11 17 04FDEA03109 120041115A5220 FRAME BOEING727 72722 1384002NM EMERGENCY DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION LT FWD EMERGENCY ESCAPE DOOR UNDER SIDE OF LWR FRAME BACK SIDE OF OUTER SKIN 7 INCH UP FROM LWR AFT CORNER. 2L73 4F A3WE 20041118000012004111800001NM 2004 11 18 04FDEA03100 120041112A5754BAC1503100046 STRUCTURE BOEING727 72722 1384002NM LE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 LT WING I/B MID FLAP TRAILING EDGE CHORD CRACKED AT THE I/B AFT FLAP ACTUATION ROD CUT OUT. REPAIRED PER SRM 51-40-4, 51-30-2, OHM 20-50-01, 20-50-02. 2L73 4F A3WE 20041118000022004111800002EU 2004 11 18 04FDEA03101 120041112A5347 SEAT TRACK AIRBUS310 A310222 3930315EU CARGO BAY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 MAIN DECK CARGO COMPARTMENT, RT NR 3 SEAT TRACK BETWEEN FS 37 AND FS 38 CORRODED BEYOND LIMITS. CUT SEAT TRACK BETWEEN FS 37 AND FS 38 TO END OF SEAT TRACK AT FS 38.2 IAW A310 SRM 53-10-16, FIG 208. FABRICATED NEW SEAT TRACK IAW A310 SRM 53-10-16 AND TREATED, PRIMED, AND TOP-COATED IAW A310 SRM 51-21-10. INSTALLED NEW SEAT TRACK IAW A310 SRM 51-40-21. WORK DOCUMENTED ON NRC NR N00946. 2L72 4F RTA35EU 20041118000032004111800003NM 2004 11 18 04FDEA03081 120041111A5512 SKIN BOEING727 72722 1384002NM HORIZONTAL STAB BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 RT HORIZ STAB UPPER SKIN HAS SHEARED FASTENER AND SKIN BULGE 31 INCH FROM TRAILING EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN FOUND TO BE CORRODED BEYOND LIMITS AND WILL BE REPLACED ON FED EX W/C N01050. 2L73 4F A3WE 20041118000042004111800004NM 2004 11 18 04FDEA03090 120041111A5753ARC05532 BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LT WING OUTBOARD FLAP HINGE FWD FAIRING SUPPORT BRACKET FOUND CRACKED AT INBOARD LOWER. BRACKET REMOVED AND REPLACED PER SRM 51-05-01 VOLUME II. 2L73 4F RTA22WE 20041118000082004111800008EU 2004 11 18 04FDEA03086 120041111A2611 WARNING LIGHT AIRBUS300 A300B4605R 3930308EU SMOKE ALERT ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25651FE 728 TOOK OFF OUT OF KMEM AND AT 1800 FT, A MIN EQUIP SMOKE ALERT WARNING ECAM INDICATION. REQUESTED TO LAND ASAP ALERT WAS CONFIRMED, QRH COMPLIED, NO EVIDENCE OF SMOKE ALERT STAYED UNTIL SHORT FINAL FOR RWY 18L ON SHORT FINAL ALERT WENT AWAY FOLLOWED BY SLATS/FLAPS FAULT LIGHT. LANDED WITH SLATS/FLAPS 15/20. REMOVED AND REPLACED AVIONICS MIN. EQUIPMENT SMOKE DETECTOR IAW A-300 MM26-15-12-4.OP'S TEST GOOD. 2L72 4F RTA35EU 20041118000102004111800010NM 2004 11 18 04FDEA03088 120041111A5730 SKIN DOUG MD11 MD11F 3023600NM ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LT WING UPPER SURFACE STA XOS=772, ON PREVIOUS METAL FILLER REPAIR FOUND EXISTING BLENDOUT EXCEEDED SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET. NR 2 LIMITS. BLENDOUT DIMENSION: LENGTH=1.5 INCH, WIDTH= 1.25 INCH, DEPTH=0.0052 INCH; ORIGINAL THICKNESS= 0.312 INCH, REMAINING=0.262 INCH. L/H WING, TAPERED UPPER CENTER, OUTER SKIN PANEL SURFACE LOCATED AT STA XROS= 772, FRONT SPAR LINE - EXISTING BLENDOUT REPAIR CARRIED OUT PER SRM 57-10-00, VOLUME 1, FIGURE 32 SHEET 2 AND 9. COMPLIED WITH FEDEX EA 1-5720-77972, WINGS - LT HAND TAPERED UPPER / CENTER OUTER SKIN PANEL - REWORK 2L73 4F RTA22WE 20041118000112004111800011NM 2004 11 18 04FDEA03089 120041111A5713ARB751111 STRINGER DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 LT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACKED AS VIEWED FROM ACCESS PANEL NR 536AB. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20041118000132004111800013NM 2004 11 18 04FDEA03092 120041112A5510ALC810Y2 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25618FE 48754 CORROSION REMOVED ON NR 26 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED (P/N ALC8107Y2) PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20041118000162004111800016NM 2004 11 18 04FDEA03107 120041115A5315 FLOORBEAM BOEING727 72722 1384002NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION MECHANICAL DAMAGE ON FLOORBEAM BS 680 UPPER CHORD LWR SURFACE AT LBL 64 WL 208. 2L73 4F A3WE 20041118000172004111800017NM 2004 11 18 04FDEA03108 120041115A5311 FRAME BOEING727 72722 1384002NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FRAME BS 1010 LT BETWEEN STR 24 AND 25 DENTED. 2L73 4F A3WE 20041118000182004111800018WP 2004 11 18 04FDEA03083 120041111A3030102JE2FG PROBE DOUG MD10 MD1010F 3022112WP TAT MALFUNCTIONED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25396FE 46630 TAT PROBE HEAT ALERT AFTER TAKEOFF CB POPPED. RETURNED TO MEM. REMOVED AND REPLACED TAT PROBE IAW MD-10 AMM 34-16-02-2. OP CHECKS GOOD. 2L73 4F RTA22WE 20041118000192004111800019NM 2004 11 18 04FDEA03082 120041111A5311 FRAME BOEING727 72722 1384002NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 FRAME BS 990 LT AT STR 24 DENTED. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 20041118000202004111800020NM 2004 11 18 04FDEA03095 120041112A5313 LONGERON DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO, EXISTING REPAIR ON FRAME AT RT STA Y= 1681, LONGERON 12R FOUND WITH DENT/CHAFFED. REPAIRED PER SRM 53-30-00 VOLUME I, FIGURE 1 AND SRM 51-33-01 VOLUME II. RE-INSPECTION TO BE ACCOMPLISHED AT 16,292 FLIGHT CYCLES WITH REPETITIVE INSPECTION THEREAFTER OF EVERY 9,500 FLIGHT CYCLES. REFER TO FEDEX EA 1-5310-79793, FUSELAGE - MAIN FRAME - TRACKING OF CATEGORY B REPAIRS ON FRAME. 2L73 4F RTA22WE 20041118000222004111800022NM 2004 11 18 04FDEA02732 120040919A5512ALC81042 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 16 RT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 16R. REPAIRED AS PER EA NR 1-5510-81543, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 16R, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041118000232004111800023NM 2004 11 18 04FDEA02736 120040919A5512ALC81041 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 18 LT BARREL NUT BORE EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 18L. REPAIRED AS PER EA NR 1-5510-80360, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 18L, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041118000242004111800024NM 2004 11 18 AWXA200401102 120041005A21317638102 CONTROLLER BOEING737 7373G7 1384595NM ZONE 205 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28309AW3988 888 24711 EN ROUTE FROM PHX TO MCI WHEN LEVELING OFF AT FL 330, NOTICED CABIN ALTITUDE WAS AT 9500 AND CABIN RATE OF CLIMB WAS +400 FPM. SELECTED STANDBY MODE AND INCREASED RATE, NO CHANGE, SELECTED MANUAL MODE AND FULLY CLOSED THE OUT FLOW VALVE (OFV), BUT OFV WAS ALREADY FULL CLOSED. CABIN ALTITUDE HORN SOUNDED AND CABIN ALTITUDE WENT TO 10,500, STARTED DESCENT AND CABIN ALTITUDE STABILIZED AND REMAINED STABLE AT 5000-6000 WITH AIRCRAFT HOLDING AT 10,000 FT. DIVERTED INTO ABQ, LANDED WITHOUT FURTHER EVENT. MX REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS MX FERRIED TO PHX. 2L72 4F RTA16WE 20041118000262004111800026NM 2004 11 18 04FDEA01730 120040614A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.224 INCH. COMPLIED WITH FEDEX EA NR 1-5740-76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041118000272004111800027EU 2004 11 18 AWXA200400965 120040804A5210FE1740011 CYLINDER AIRBUS320 A320231 3930325EU L-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28622AW8724 054 DURING C-04 CHECK, THE L-1 DOOR DAMPER WAS FOUND LEAKING. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER ASSEMBLY IAW AMM 52-11-14-04. 2L72 4F RTA28NM 20041118000292004111800029EU 2004 11 18 AWXA200400967 120040814A5347D571301472020000SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 DURING C-04 CHECK, CORROSION WAS FOUND IN NUMEROUS AREAS ON THE OUTBOARD SEAT TRACK Y1292 LT, BETWEEN FS 37 AND FS 39. MAINTENANCE REMOVED CORRODED SEAT TRACK Y1292 LT FROM FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041118000302004111800030NM 2004 11 18 AWXA200400968 120040805A53136561777505 STRINGER BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING C-18 CHECK, A 5/8 INCH CRACK WAS FOUND IN FORWARD CABIN STRINGER 14 LT AT BS 354. MAINTENANCE REMOVED CRACKED SECTION OF STRINGER 14 LT AT BS 354; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20041118000352004111800035NM 2004 11 18 04FDEA01732 120040614A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEEDED LIMITS PER CMM 57-52-03, PAGES 442 - 443. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.253 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76743, WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20041118000362004111800036NM 2004 11 18 04FDEA01735 120040615A5347ABA7680505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 FOUND MAIN DECK SEAT TRACK CORROSION AT STA 460 LEFT HAND MOST OUTBOARD. MAIN DECK SEAT TRACK FOUND CORROSION AT STA 460 LEFT HAND MOST OUTBOARD REMOVED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2. THE CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 PG 7 VOL 1. THE ORIGINAL THK 0.1 INCH REMAIN THK 0.051 INCH TO 0.099 INCH. THE NEW SEAT TRACK INSTALLED AS PER SRM 51-31-01 VOL 2 AND SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20041118000382004111800038NM 2004 11 18 04FDEA02738 120040919A5512ALC81042 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 20 RT BARREL NUT BORE EXCEEDED LIMITS. RIGHT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 20R, REPAIRED AS PER EA NR 1-5510-80359, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 20R, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041118000402004111800040WP 2004 11 18 04FDEA02821 120040927A5311 FRAME DOUG DC10 DC1010F 3022111WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 MAIN CABIN FUSELAGE STATION 1821 HAS CORROSION AT LOWER FRAME END, AS SEEN FROM BULK PIT UPPER TORQUE BOX. CORROSION EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL 1. FABRICATED AND INSTALLED REPAIR IAW DC10 SRM 50-30-00 FIGURE 5, VOLUME 1. REFERENCE NON ROUTINE N01499. 2L73 4F A22WE 20041118000422004111800042WP 2004 11 18 04FDEA02823 120040927A5730ARC2541502 PANEL DOUG DC10 DC1010F 3022111WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 641CR HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77617. REFERENCE NON ROUTINE N00169. 2L73 4F A22WE 20041118000442004111800044WP 2004 11 18 04FDEA02825 120040927A5730ARC21562 PANEL DOUG DC10 DC1010F 3022111WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 636HL HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77614. REFERENCE NON ROUTINE N00323. 2L73 4F A22WE 20041118000472004111800047NM 2004 11 18 04FDEA02766 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.188 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118000482004111800048NM 2004 11 18 04FDEA02767 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.405 INCH, REMAINING THICKNESS=0.402 INCH, MATERIAL REMOVED=0.003 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118000502004111800050EU 2004 11 18 04FDEA02769 120040920A5320A5377866920600 FITTING AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25421FE 342 THE FOLLOWING FWD CARGO COMPT AFT MANHOLE POCKETS HAD CORROSION AT LOCATIONS: (A) ON LT SIDE OF MANHOLE 6 OFF POCKETS CORROSION BETWEEN FS 38.1 TO FS 38.2. REPAIR C/W AS PER EA 6-5310-77946 AND ALSO REFER TO N00411, N00412 AND N00488. RII BY L3167(SIAEC). 2L72 4F RTA35EU 20041118000512004111800051EU 2004 11 18 2004UALA01015 120041103A2822 PUMP AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUEL BOOST MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29456UA 1128 RIGHT TANK FUEL BOOST PUMPS FAULTED AND UNABLE TO CORRECT FUEL IMBALANCE. DUE TO FUEL IMBALANCE WITH BOTH RIGHT WING NR 1 AND 2 BOOST PUMPS INOPERATIVE. THE AIRCRAFT DIVERTED, RT WING NR 2 BOOST PUMP CONTACTS WERE CLEANED AND THE NR 1 RIGHT WING BOOST PUMP WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20041118000542004111800054NM 2004 11 18 2004UALA01017 120041104A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1660 TO 1680 LBL 50 TO LBL 55. TYPICAL FLOOR STRUCTURE CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA2NM E17NE 20041118000562004111800056WP 2004 11 18 04FDEA02826 120040927A5730ARC0267504 PANEL DOUG DC10 DC1010F 3022111WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 RIGHT WING TRAILING EDGE PANEL 641BB DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-77621, REFERENCE NON ROUTINE N00419. 2L73 4F A22WE 20041118000582004111800058EU 2004 11 18 04FDEA02680 120040914A5410A54611937500 FAIRING AIRBUS310 A310203 3930313EU ZONE 400 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25411FE 359 NR 1 ENGINE PYLON FAIRING DENTED, FORWARD PYLON TO NACELLE FAIRING. REPAIRED FAIRING BY REFORMING TO ORIGINAL CONTOUR AND INSPECTING USING HFEC PER AIRBUS NTM FOR CRACKS, NO CRACKS WERE NOTED. ALL WORK DONE PER EA 6-5480-73051A PART 3 AND A310 SRM 54-50-00 FIG 201. 2L72 4F RTA35EU 20041118000622004111800062EU 2004 11 18 04FDEA02748 120040920A5311A5361056002300 FRAME AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25421FE 342 FUSELAGE FRAME 14A FWD AND AFT FACE AT VICINITY OF STRINGER 44 LT FOUND CORRODED. REPAIR C/W AS PER EA 6-5310-77955. RII BY L4724. 2L72 4F RTA35EU 20041118000662004111800066NM 2004 11 18 04FDEA02752 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.509 INCH, REMAINING THICKNESS=0.504 INCH, MATERIAL REMOVED=0.005 INCH, AND REPAIRED AS PER EA NR 1-5750- 79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118000682004111800068WP 2004 11 18 04FDEA02827 120040927A5512ALC7426502 PANEL DOUG DC10 DC1010F 3022111WP ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL IAW FEDEX EA 8-5510-81466. 2L73 4F A22WE 20041118000692004111800069WP 2004 11 18 04FDEA02828 120040927A5512ALC70611 PANEL DOUG DC10 DC1010F 3022111WP ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LEFT HORIZONTAL STABILIZER, 1 EACH PANEL AT STA XE203.5, COMPOSITE PANEL AT AFT SPAR TOP DELAMINATED. REPAIRED BY FABRICATION AND BONDING NEW OUTER AND INNER SKIN, DOUBLERS AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5510-81441. REFERENCE NON-ROUTINE N00148. 2L73 4F A22WE 20041118000732004111800073NM 2004 11 18 04FDEA02760 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE OUTBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.505 INCH, REMAINING THICKNESS=0.502 INCH, MATERIAL REMOVED=0.003 INCG, AND REPAIRED AS PER EA NR 1-5750- 79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118000742004111800074WP 2004 11 18 04FDEA02832 120040927A5512ALC7425502 PANEL DOUG DC10 DC1010F 3022111WP ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, INNER DOUBLER, OUTER DOUBLER AND CORE IAW TPS 1001 REV E AND FEDEX EA 8-5510-81466. RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE FAIRING PANEL. REFERENCE NON-ROUTINE N00138. 2L73 4F A22WE 20041118000752004111800075NM 2004 11 18 AWXA200401065 120040925A2560P4010021 BATTERY BOEING757 7572S7 1384962NM ZONE 800 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28906AW 23568 FLIGHT CREW REPORTED, THE EMERGENCY FLASHLIGHT AT L-4 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN EMERGENCY FLASHLIGHT AT L-4 DOOR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20041118000792004111800079NM 2004 11 18 AWXA200401068 120040921A5320D53480048203 SILL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON R-2 DOOR SHAPE SILL OUTBOARD EDGE FORWARD OF FS 68. MAINTENANCE REMOVED DAMAGED AREA OF R-2 DOOR SHAPE SILL FORWARD OF FS 68; FABRICATED A NEW REPLACEMENT SECTION OF SILL; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041118000802004111800080NM 2004 11 18 AWXA200401018 120040905A5321D5361060500000 FLOOR PANEL AIRBUSA319 A319132 3930340NM CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON AFT SIDE OF LT FORWARD FLOOR PANEL 221 FF. MAINTENANCE REMOVED AND REPLACED LT FORWARD FLOOR PANEL 221 FF IAW C1D25306. 2L72 4F RTA28NM 20041118000812004111800081NM 2004 11 18 AWXA200401019 120040905A5320D5347209400800 FLOOR SUPPORT AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y465 BETWEEN FS 64 AND FS 66. MAINTENANCE REMOVED CORRODED BEAM Y465 FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-49-00, FIG. 1, PG 1-13. 2L72 4F RTA28NM 20041118000832004111800083NM 2004 11 18 AWXA200401109 120041002A5753 SKIN BOEING737 73733A 1384673NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, FOUND THE RT OUTBOARD FLAP DELAMINATED ON THE LOWER INBOARD END BETWEEN WBL 230.68 AND WBL 234.68. MAINTENANCE REMOVED DELAMINATION ON RT OUTBOARD FLAP LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20041118000852004111800085NM 2004 11 18 AWXA200401022 120040908A53302024T3050 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW 22649 DURING 4-DAY CHECK, A 1 1/2 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727A, STR 16 RT. MAINTENANCE REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA OF SKIN AT BS 727A, STR 16 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-200 SRM 53-30-3, FIG 48. 2L72 4F RTA16WE 20041118000872004111800087WP 2004 11 18 04FDEA02897 120041009A5753NRC6062520 VANE DOUG DC10 DC1010F 3022111WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568052 47806 WINGS, RT INBD FLAP VANE ASSY, REPAIR OF OVERSIZED HOLES ON CHANNEL FITTINGS. COMPLIED WITH EA 8-5750-82058. 2L73 4F A22WE 20041118000882004111800088NM 2004 11 18 04FDEA02578 120040829A5311AFA00203 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CABIN, FUSELAGE FRAME AT STA 1701, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1701, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5310-79741, FUSELAGE, MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1701, LONGERON 12L, ISSUED FOR TRACKING. 2L73 4F RTA22WE 20041118000892004111800089NM 2004 11 18 04FDEA02579 120040829A5311AFA0028 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 CABIN, FUSELAGE FRAME AT STA 1681, LEFT HAND, L12, FOUND DENTED. DENTED AREA TRIMMED OUT AT CABIN, FUSELAGE FRAME STA 1681, LEFT HAND LONGERON 12 AND REPAIR CARRIED OUT AS PER SRM 53-30-00 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. FEDEX EA NR 1-5310-79739, FUSELAGE, MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1681, LONGERON 12L, ISSUED FOR TRACKING. 2L73 4F RTA22WE 20041118000902004111800090NE 2004 11 18 AWXA200401033 220040917A7320 FMU AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE MALFUNCTIONED A AWXAE ENGINE SHUTDOWN RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 WP28626AW 65 V0048 ON DESCENT INTO LAS EN ROUTE FROM ORD AT APPROXIMATELY 17,000 FT, RECEIVED ECAM MESSAGE NR 2 ENGINE VANE FAILURE, ENGINE THEN SPOOLED DOWN AND ECAM INDICATED NR 2 ENGINE FAILED. FOLLOWED ECAM INSTRUCTIONS AND SECURED NR 2 ENGINE; DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE PERFORMED ELECTRICAL CHECKS PER TSM 75-30-00-810-806; VARIABLE STATOR VANE (VSV) AND LINKAGE CHECK PER AMM 75-32-42-06, MAGNETIC CHIP DETECTOR INSPECTION PER T/C I5M72314, AND WINDMILL INSPECTION OF BLADES, NO DEFECTS NOTED. A/C MX FERRIED TO PHX, REMOVED AND REPLACED NR 2 ENGINE FUEL METERING UNIT (FMU) IAW T/C R5M73306, AND FUEL PUMP IAW T/C R5M73304. 2L72 4F4 FRTA28NM E311NE 20041118000922004111800092EU 2004 11 18 AWXA200401035 120040918A3610 UNION AIRBUS320 A320232 3930326EU NR 2 ENGINE LEAKING A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28638AW 455 AFTER TAKEOFF FROM PHX EN ROUTE FOR BWI RECEIVED ECAM MESSAGE NR 2 ENGINE BLEED FAULT: TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FAN AIR VALVE CONTROL THERMOSTAT 7170HM2 IAW AMM 36-11-43-04, ALSO REPLACED DEFECTIVE LINE THAT CONNECTS TO FAN AIR VALVE AND THERMOSTAT 7170HM2, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF TEMPERATURE CONTROL THERMOSTAT S/N 03205 FINDING THE UNION WAS CROSS THREADED CAUSING AIR TO LEAK AT SENSE LINE. REPLACED DAMAGED UNION IAW CMM 36-11-44, AND COMPLIED WITH SB 342-36-06. UNIT TESTED AND RETURNED TO SERVICE. 2L72 4F RTA28NM 20041118000942004111800094EU 2004 11 18 AWXA200401048 120040910A5320D53480043202 SILL AIRBUS320 A320232 3930326EU L-2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR SILL AT FORWARD INBOARD CORNER FS 66. MAINTENANCE REMOVED DAMAGED AREA OF L-2 DOOR SILL AT FS 66; FABRICATED A FILLER AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG 201. 2L72 4F RTA28NM 20041118000952004111800095EU 2004 11 18 AWXA200401049 120040910A5315D53472189200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 64 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041118000962004111800096EU 2004 11 18 AWXA200401050 120040910A5315D53472172201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT ON FORWARD SIDE OF FS 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT ON FORWARD SIDE OF FS 67; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041118000972004111800097EU 2004 11 18 AWXA200401051 120040910A5347D53472133200 SEAT TRACK AIRBUS320 A320232 3930326EU CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON RAIL Y1292 LT AT FS 66. MAINTENANCE REMOVED CORRODED SECTION OF RAIL Y1292 LT FROM FS 64 TO FS 66; FABRICATED A NEW REPLACEMENT SECTION OF RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041118000982004111800098EU 2004 11 18 AWXA200401052 120040910A5315D53472133200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON RAIL Y1292 RT AT FS 66. MAINTENANCE REMOVED CORRODED SECTION OF RAIL Y1292 RT AT FS 66; FABRICATED A NEW REPLACEMENT SECTION OF RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041118001002004111800100EU 2004 11 18 AWXA200401054 120040910A5315D53472075001 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1732 RT AFT OF FS 65. MAINTENANCE REMOVED CORRODED BEAM Y1732 RT AT FS 65; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG 2-3, 8, 10-11, AND 18. 2L72 4F RTA28NM 20041118001052004111800105NM 2004 11 18 AWXA200401227 120041003A5320143N83392 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-10 CHECK, A 1 5/16 INCH CRACK WAS FOUND IN R-2 DOOR LOWER HINGE INTERCOSTAL AT BS 660. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT R-2 DOOR LOWER HINGE BS 660; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, FIG 12. 2L72 4F RTA2NM 20041118001062004111800106NM 2004 11 18 AWXA200401069 120040921A5320D53471124200 SHEAR PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON LEFT AFT OUTBOARD SHEAR PLATE FORWARD OF FS 70 AT Y1292, STR 24 LT. MAINTENANCE REMOVED DAMAGED LT AFT OUTBOARD SHEAR PLATE AT FS 70 AT Y1292, STR 24 LT; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 2 & 3, 8 & 9, & 62. 2L72 4F RTA28NM 20041118001072004111800107NM 2004 11 18 04FDEA02764 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, OUTBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.405 INCH, REMAINING THICKNESS=0.396 INCH, MATERIAL REMOVED=0.009 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118001082004111800108EU 2004 11 18 AWXA200401208 120041018A5347D53371110000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 8 PLACES ON LEFT CABIN SEAT TRACK Y765 BETWEEN FS 41 AND FS 47. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y765 FROM FS 41 TO FS 47; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041118001102004111800110EU 2004 11 18 04FDEA02593 120040901A5320 SEAL AIRBUS310 A310222 3930315EU DRIP PAN WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25453FE 267 DURING C CHECK, FOUND DAMAGED DRIP PAN SEAL AND WORN SUPPORT HOLES ON PANEL 147CZ AND 148CZ. GEN ITEM 41C0508. PANELS REPAIRED ON N00056 AND N00057 PER EA 6-5315-81014. 2L72 4F RTA35EU 20041118001152004111800115EU 2004 11 18 AWXA200401219 120041018A5320D53230585200 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FORWARD CARGO COMPARTMENT SILL WEB BETWEEN FS 26 AND FS 27. MAINTENANCE REMOVED CORRODED FORWARD CARGO COMPARTMENT SILL WEB FROM FS 24 TO FS 28; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041118001172004111800117EU 2004 11 18 AWXA200401220 120041018A5320D5347556521000 WEB AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL WEB (SHEET COVER) BETWEEN FS 52 AND FS 56. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT DOOR SILL WEB FROM FS 52 TO FS 56; FABRICATED A NEW REPLACEMENT SECTION OF WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2 & 3. 2L72 4F RTA28NM 20041118001202004111800120NM 2004 11 18 AWXA200401071 120040921A5321D5361060500100 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, CORROSION WAS FOUND ON UPPER SURFACE OF R-1 DOOR ENTRY WAY FLOOR PANEL 222 FF AT THE FORWARD AND INBOARD EDGES. MAINTENANCE REMOVED CORRODED FLOOR PANEL 222 FF AND INSTALLED NEW REPLACEMENT FLOOR PANEL IAW AWA T/C C1D25306. 2L72 4F RTA28NM 20041118001222004111800122NM 2004 11 18 AWXA200401073 120040921A5320D5347218920400 FLOOR SUPPORT AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041118001252004111800125EU 2004 11 18 AWXA200401075 120040912A5320D5348004200300 FITTING AIRBUS320 A320232 3930326EU R2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, A 1 INCH CRACK WAS FOUND IN R-2 DOOR LOWER AFT CORNER FITTING AT FS 67, STR 20 RT. MAINTENANCE REMOVED CRACKED R-2 DOOR CORNER FITTING AT FS 67, STR 20 RT; FABRICATED A NEW REPLACEMENT CORNER FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041116001312004111600131NM 2004 11 16 2004UALA00986 120041027A5320 SILL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 BS 1380-1442 RT AND STR 26R, DOOR SILL IS CORRODED AT TOP AND BOTTOM. 2L72 4F4 FRTA2NM E17NE 20041116001342004111600134NM 2004 11 16 04FDEA01830 120040620A5710ARC2512504 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25587FE 48489 RIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.254 INCH AND REPAIRED AS PER FEDEX EA NR 1-5750- 78013, TITLE: WINGS, TRAILING EDGE FLAPS, RIGHT HAND INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20041116001432004111600143NM 2004 11 16 AWXA200401180 120041031A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 8 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28326AW 23258 EMERGENCY ESCAPE PATH LIGHT INOPERATIVE SEAT ROW 8 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041116001442004111600144NM 2004 11 16 AWXA200401181 120041002A52106529382 BEAM BOEING737 73733A 1384673NM DOOR GATE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND ON LOWER FORWARD CORNER OF L-1 DOOR AT LOWER GATE BEAM WEB, BS 314, STR 16 LT. MAINTENANCE CUTOUT DAMAGE IN LOWER GATE BEAM WEB OF L-1 DOOR; FABRICATED A REPAIR DOUBLER AND FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, FIG 1. 2L72 4F RTA16WE 20041116001482004111600148NM 2004 11 16 04FDEA02673 120040910A5512ALC81041 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 15 LEFT HAND BARREL NUT BORE FOUND EXCEEDED LIMIT. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 15L. REPAIRED AS PER EA NR 1-5510-81560, TITLE: HORIZONTAL STABILIZER-BARREL NUT BORE 15L. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041116001602004111600160NM 2004 11 16 04FDEA02757 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE OUTBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041116001612004111600161NM 2004 11 16 04FDEA02758 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE, ACTUATOR ROD END HOLE INBOARD SPOTFACE ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.408 INCH, REMAINING THICKNESS=0.401 INCH, MATERIAL REMOVED=0.007 INCH, AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041116001642004111600164NM 2004 11 16 04FDEA02501 120040818A5310AGA7134 SHEAR TIE DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 AFT CARGO, AFTER FLOOR PANEL NR 187DF REMOVAL FOR ACCESS, CORROSION FOUND AT STA 1964 BETWEEN LONGERON 47L AND 48L. AFT CARGO, STA 1964 BETWEEN LONGERON 47L AND 48L SHEAR TIE CLIP. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041116001652004111600165NM 2004 11 16 04FDEA02502 120040818A5311AGA72161 FRAME DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 AFT CARGO, AFTER REMOVAL OF DOOR CUTOUT AFT LOWER LINER, CORROSION FOUND ON FRAME SIDE SURFACE AT STA 1959. AFT CARGO, CORROSION ON FRAME SIDE SURFACE AT STA 1959 REMOVED PER SRM 53-00-01 FIGURE 3 VOLUME I. MATERIAL THICKNESS= 0.130 INCH, MATERIAL REMOVED= 0.025 INCH, MATERIAL REMAINING= 0.105 INCH WITHIN LIMITS PER SRM 53-00-01 FIGURE 3 VOLUME I. 2L73 4F RTA22WE 20041116001712004111600171NM 2004 11 16 04FDEA02731 120040919A5512ALC81041 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 25 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. CORROSION REPAIRED AS PER EA 1-5510-81558 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 25L, REWORKED BEYOND SB MD11-55-023 REV2 LIMIT. 2L73 4F RTA22WE 20041116001882004111600188EU 2004 11 16 MALA040667 120041101A5321 FLOOR PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, O/B FLOOR PANEL SUPPORT IS CORRODED FROM FS 583 TO FS 622 LT SIDE. MAINTENANCE REPAIRED IAW SRM 51-70-20, 51-40-60. A/C WAS RELEASED 11/07/04. 2L72 4T RTA52EU 20041116001902004111600190EA 2004 11 16 COMA0460610 120041110A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5816 FLAPS FAILED CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM IAW AD 98-20-01. 2L72 4F RTA21EA 20041116001942004111600194NM 2004 11 16 UPS04543435 120041103A4900 APU BOEING757 75724APF 1384969NM APU BAY FAILED A IPXABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO01420UP 23907 INBOUND TO ALB APU FAILED. EMERGENCY DECLARED. IAW 24-00-1, TS PER FIM 49-11-00 FIG 103, SYS CHECK OK. CHECKED APU OIL, SYSTEM FULL. OK TO CONTINUE. 2L72 4F RTA2NM 20041116001962004111600196WP 2004 11 16 UPS04843437 120041028A7830 SPRING DOUG DC8 DC871F 302199DWP PEDESTAL LOCKOUTFAILED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01729UP 46029 NR 1 & 4 ENGINE REVERSERS WENT INTO REVERSE IN FLIGHT. REINSTALLED NR 1 & 4 T/R LOCKOUT SPRINGS PER MM 76-11-00, OPS CHECK GOOD. REINSTALLED PNLS 573A AND 573B PER MM 53-21-01 AND REINSTALLED CAPT AND CO-PILOTS SEATS PER MM 25-11-01. RESET STALL WARNING C/B. 2L74 4F RT4A25 20041116002072004111600207NM 2004 11 16 UPS04443339 120040922A5347 CARGO TRACK BOEING747 747121 1384871NM CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D- BS 1720 LBL 97 TIE DOWN TRACK CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.060 X 1 X 5 INCH EXCEED SRM 53-10-01 LIMITS. SEAT TRACK REPAIRED REF SRM 53-10-05 FIG 1A. CIC APPLIED IAW UPS EO M5100-2780-E. 2L74 4F A20WE 20041117000312004111700031WP 2004 11 17 UPS04843265 120040909A5310 DOOR FRAME DOUG DC8 DC871F 302199DWP L1 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, L1 DOOR HAS A CRACK ON THE LOWER FWD DOOR JAMB STARTING FROM THE EDGE AND TERMINATES AT THE FASTENER HOLE. CUT OUT CRACK ON FWD LOWER CORNER OF L1 DOOR JAMB OUTER SKIN AND INTERNAL DOUBLER. NDT VERIFIED NO CRACKS NOTED AT CUT OUTS. FABRICATED REPAIR DOUBLER, TRIPLER, AND FILLER. INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-0 FIG 15. 2L74 4F RT4A25 20041117000432004111700043NM 2004 11 17 UPS04443330 120040927A5710 SPLICE BOEING747 747121 1384871NM WING SPAR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RT BS 1241 STR R28 UPPER WING REAR SPAR SPLICE PLATE HOLE NR 4 FOUND CRACK AT INTERNAL SPLICE FITTING AT 7 O'CLOCK POSITION APPROX 0.080 INCH LONG. CRACKED HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2L74 4F A20WE 20041117000532004111700053 2004 11 17 MALA040608 420041001A2565 SLIDE BAC 146 AVRO146RJ85A1500097EU CABIN UNSECURE A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15505XJ E2313 AFT RIGHT SLIDE NEEDS TO BE RESECURED. MAINTENANCE RESECURED SLIDE AS REQUIRED. 2H74 4F RTA49EU 20041117000592004111700059EU 2004 11 17 MALA040631 120040906A5512 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED 4 DENTS ON RT HORIZONTAL STABILIZER UPPER SKIN. REPAIRED 2 DENTS PER EO S55017, 2 ARE WITHIN LIMITS PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117000622004111700062WP 2004 11 17 UPS04843071 120040906A3213 AXLE DOUG DC8 DC873F 302199FWP RT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 RIGHT MAIN GEAR BEAM AXLE HAS CORROSION NR 3 POSITION. REMOVED RIGHT MLG BOGIE BEAM PER MM 32 11 08 2 (SKYPULSKI 92222), INSPECTED INNER CYL BOGIE PIVOT, OK TO INSTALL. REPLACED RT MLG BOGIE BEAM IAW MM032 11 80 2. 2L74 4F RT4A25 20041117000642004111700064NM 2004 11 17 UPS04443465 120041030A531165B0793685 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D - BS 400, S23-24R FRAME I/B CHORD O/B FACE ATT SPLICE FOUND CRACK. FRAME SPLICE REPLACED PER SRM 51-10-01. 2L74 4F RTA20WE 20041117000712004111700071NM 2004 11 17 UPS04M43287 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP INSPECTION TYPE: C, HORIZONTAL STAB NR 18 RIGHT BARREL NUT HOLE FOUND CORRODED ON BEARING SURFACE. CORROSION AT NR 18 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT B/N HOLE NR 18 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 18 RIGHT PER EO MD11-5510-19409-H & EN 1247-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041117000762004111700076NM 2004 11 17 SWAA043300 120041111A3350101073 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT DETACHED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 FWD OVERHEAD EMERGENCY EXIT LIGHT LENS DETACHED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041117000912004111700091NM 2004 11 17 SWAA043310 120041111A5753 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29526SW 1426 26568 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041117001052004111700105NE 2004 11 17 MALA040612 220041010A7320230349306 ECU BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 ENGINE FLUCTUATES A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 NR 2 ENGINE EGT ERRATIC FLUCUATES -50C TO 603C T/O. AIR RETURN TO DTW. MAINTENANCE REPLACED NR 2 ENGINE ECU IAW MM 77, OPS CHECK GOOD IAW MM P/N ON & OFF 2-303-493-06, S/N ON 7ALG570, S/N OFF 3AGT92 & THERMOCOUPLE HARNESS P/N ON & OFF 2-310-089-02 IAW AMM 77-00-00 PG BLOCK 501. 2H74 4F4 FRTA49EU E6NE 20041117001072004111700107EA 2004 11 17 COMA0460601 120041108A5330 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 RIGHT FS 718 FRAME CRACKED. REPAIRED IAW SB 601R-53-055. 2L72 4F RTA21EA 20041117001092004111700109EU 2004 11 17 UPS04143034 120040827A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU LAVATORY INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01121UP 0806 LAV EMERGENCY LIGHT INOP. RELAMPED LAV EMERGENCY LIGHT. 2L72 4F RTA35EU 20041117001192004111700119NM 2004 11 17 UPS04443356 120040925A5240 DOUBLER BOEING747 747121 1384871NM L1 DOOR SKIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, M/D- L1 DOOR SKIN LOWER HINGE DOUBLER FOUND CRACKED. DOUBLER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 8 & 51-30-02. 2L74 4F A20WE 20041117001222004111700122NM 2004 11 17 AALA20041093 120041102A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21185AN 32379 MIA - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24D INOPERATIVE. FOUND CONNECTOR LOOSE UNDER SEAT 24D. RECONNECTED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041117001262004111700126NM 2004 11 17 UPS04543385 120041020A3350 GUARD BOEING757 75724APF 1384969NM LIGHT SWITCH INOPERATIVE A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01455UP 25476 ON PRE-FLT FOUND EMERGENCY LIGHT SWITCH GUARD NOT OPERATING PROPERLY. ON T/S FOUND SWITCH GUARD SPRING MECHANISM TO BE BROKEN. SWITCH GUARD REPLACED REF IPC 33-51-08 FIG 4 AND EMERGENCY LIGHT OPS TEST IAW MM 33-51-00-5 PAR 4, FOUND NORMAL. A/C OK FOR SERVICE. 2L72 4F RTA2NM 20041117001272004111700127NM 2004 11 17 UPS04643387 120041020A2560MXP21000 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01309UP 27740 3 SMOKE GOGGLES NOT USABLE DUE TO STRETCHED STRAPS. REPLACED THREE SMOKE GOGGLES ON SEAT, THIS CLEARED DEFERRAL M289838. 2L72 4F RTA1NM 20041117001332004111700133NM 2004 11 17 UPS04443091 120040815A5315 FLOORBEAM BOEING747 747212B 1384886NM FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:C, RIGHT BS 340 UPPER DECK FLOORBEAM FOUND ONE FASTENER HOLE CRACKED AT FRAME WEB. FLOORBEAM REPAIRED AS PER HX RS R53-12-135182 & UPS EO B747-5310-20986-A. 2L74 4F A20WE 20041117001412004111700141WP 2004 11 17 UPS04843098 120040819A53203750257U1 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE: C2, FS 450 L31L SPLICE FITTING CRACKED. REMOVED AND REPLACED SPLICE FITTING AT FS 450 L31L. 2L74 4F RT4A25 20041117001502004111700150WP 2004 11 17 UPS04843168 120040828A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE LIGHTNING STRIKEA IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE:C2 LIGHTNING STRIKES ON FUSE EXTERIOR STA 415 BETWEEN L5R & L6R. BURNISHED DAMAGE AREA PER SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL THICKNESS OUT OF LIMITS, .020' TO .053, PER NDT SPM 04-00-06. CUT OUT DAMAGED AREA PER 53-2-1 FIG 7. FABBED AND INSTALLED DOUBLER, FILLER & FINGER DOUBLER PER SRM 53-2-1 FIG 7, 51-1-8, 51-1-21, 51-1-26, 51-1-20D. 2L74 4F RT4A25 20041117001512004111700151NM 2004 11 17 UPS04M43152 120040601A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 1 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION AT NR 1 BARREL NUT HOLE BEARING S/W SURFACE REMOVED & REAMED TO 1.549 INCH, FOUND OUT LIMITS. FAB SLEEVE BUSHING PER EO MD11-5510-19409- H. PR1422B1/2 SEALANT APPLIED AT BLEND OUT AREA & INSTALLED SLEEVE BUSHING AS PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 1 LT IS WITHIN LIMITS AS PER EN1273-04. 2L73 4F RTA22WE 20041117001542004111700154 2004 11 17 UPS04M43129 420040914A2565 WARNING LIGHT DOUG MD11 MD11F 3023600NM ESCAPE SLIDE ILLUMINATED A IPXAK NONE N FALSE WARNING ININSP/MAINT 1 SO01252UP GALLEY DOOR SLIDE PRESSURE LIGHT ILLUMINATED. RELAMPED, OPS NORMAL. 2L73 4F RTA22WE 20041117001582004111700158NM 2004 11 17 UPS04443323 120040930A5730 SKIN BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, RT BS 1241 WL 178 WING REAR SPAR UPPER SPLICE FITTING AREA FOUND HOLE NR 7 CRACKED AT WING UPPER SKIN. HOLE CRACK REWORKED AND OVERSIZED AS PER EO 5740-17032-B. 2L74 4F A20WE 20041117001652004111700165EA 2004 11 17 COMA0460597 120041105A7110A33721 ROD CNDAIRCL600 CL6002B19 1900309EA COWL SUPPORT LOOSE A COMAA UNSCHED LANDING RS PARTIAL RPM/PWR LOSS AFFECT SYSTEMS CRCRUISE 1 SO01478CA 7671 FLIGHT 5013 LT THRUST LEVER JAMMED INFLIGHT. FOUND CORE COWL SUPPORT ROD JAMMING THE ENGINE CONTROLS. REINSTALLED SUPPORT ROD. THRUST CONTROLS OPERATE NORMALLY. 2L72 4F RTA21EA 20041117001662004111700166EU 2004 11 17 MALA040603 120041001A29104204002 PTU BAC 146 AVRO146RJ85A1500097EU GREEN HYD SYSTEMMALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15532XJ E2366 GREEN HYD HIGH TEMP ILLUMINATED DURING FLIGHT QRH COMPLETED RETURNED MSP. REPLACED PTU P/N 4204002, S/N OFF OH-78, S/N ON LM-54 IAW AVRO AMM 29-20-17 201, OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20041117001712004111700171EU 2004 11 17 MALA040671 120041104A339760207 CONNECTOR SAAB SF340 340B 7860101EU EMERGENCY LIGHT BROKEN A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15443XJ 340B443 HORIZONTAL EXIT MARKER 34LN INOP. MAINTENANCE FOUND LIGHT ASSEMBLY CONNECTOR BROKE. REPLACED ASSEMBLY WITH NEW UNIT P/N 6020-7. 2L72 4T RTA52EU 20041117001862004111700186EU 2004 11 17 MALA040645 120041001A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 6Y/4Y INSPECTION IN BNA, NOTED FLOOR FLANGE AT STA 236.5 CORRODED. REPAIRED IAW SRM. AIRCRAFT RETURNED TO SERVICE 10/5/04. 2L72 4T RTA52EU 20041117001892004111700189WP 2004 11 17 AALA20041073 120041026A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21441AA 49460 LGA - LEFT AND RIGHT EMERGENCY EXIT LIGHTS AT ROW 21 ARE INOPERATIVE. RESEATED BATTERY PACKS AT B5105 FOR EMERGENCY EXIT LIGHTS AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117001982004111700198NM 2004 11 17 UPS04443312 120040924A5410 WEB BOEING747 747121 1384871NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, NR 2 PYLON - DURING ACCOMPLISHMENT EO ON AFT LOWER SPAR WEB, 1EA NON STANDARD REPAIR PATCH FOUND INSTALLED ON LOWER SPAR WEB JUST AFT OF REAR END MOUNT BULKHEAD. DEFECTIVE AREA AFT LOWER SPAR WEB REPAIR CARRIED OUT AS PER SRM 54-10-03 FIG 23 AT NAC STA 218 TO NAC STA 228.5 LBL 1 TO LBL 7 AREA. 2L74 4F A20WE 20041117002002004111700200NM 2004 11 17 SWAA043252 120041108A53116546532 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 480, BETWEEN STRINGER 20R AND STRINGER 21R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041117002072004111700207WP 2004 11 17 AALA20041118 120041110A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW217525A 49917 DTW - LOWER EMERGENCY EXIT LIGHT MARKER BETWEEN FIRST CLASS GALLEY AND FIRST CLASS SEATS INOPERATIVE. FOUND BROKEN WIRE IN FLOOR NEAR LIGHT. SPLICED NEW WIRE FOR LOWER EMERGENCY EXIT LIGHT MARKER BETWEEN FIRST CLASS GALLEY AND FIRST CLASS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041117002102004111700210EU 2004 11 17 MALA040643 120040930A5347 CARGO TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 6Y/4Y INSPECTION NOTED PREVIOUS REPAIR AT BL 0 STA 640-658.5 ON CARGO TRACKS CORRODED. MAINTENANCE REPAIRED IAW SRM. 2L72 4T RTA52EU 20041117002162004111700216NM 2004 11 17 04FDEA03097 120041112A2740 CONTROL VALVE DOUG MD11 MD11F 3023600NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 HFEC INSPECTION CARRIED OUT ON HORIZONTAL STABILIZER TRIM CONTROL VALVE AND CRACK FOUND AT UPPER CONTROL VALVE BORE APPROXIMATELY 0.25 INCH LENGTH FROM PRESSURE PASSAGE BORE. REMOVED AND REPLACED PER AMM 27-43-42-4. OPERATION CHECK CARRIED-OUT PER AMM 27-40-00-5. P/N ON: AJG7041-5545, S/N ON: RON549, FEDEX SERVICEABLE TAG NR: 629223. 2L73 4F RTA22WE 20041117002172004111700217WP 2004 11 17 04FDEA03098 120041112A5720 SKIN DOUG DC10 DC1010 3022110WP LT WING WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON LT WING FIX TE LWR SKIN WORN STA XORS 270 . REPLACE SKIN PER SRM 513501 PAGE 1-12. 2L73 4F A22WE 20041118000052004111800005EU 2004 11 18 04FDEA03102 120041112A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 RT NR 3 SEAT TRACK HAS 8 AREAS OF CORROSION ON SCALLOP HOLES AND FLANGE. REMOVED CORRODED SEAT TRACK FROM FS 46.5 TO FS 54 IAW A310 SRM 51-72-10. INSTALLED NEW SEAT TRACK IAW A310 SRM 51-40-21 AND AIRBUS DWG NR 53811923200. 2L72 4F RTA35EU 20041118000092004111800009NM 2004 11 18 04FDEA03087 120041111A5347FXSRM531054 SEAT TRACK BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25186FE 18872 RT UPPER LOBE BS480, RBL40, SEAT TRACK CORRODED AROUND RIVET. FABRICATED SEAT TRACK IAW SRM 53-10-5 PG 4, WITH MAT ID AND MPN 60-6549/7075-T6511. LOCATED AND DRILLED HOLES IAW SRM 51-30-0. (TRAVELER NR T4/470482) AND ALODINED AND PRIMED IAW SRM 51-10-2 PG 1 AND 2. INSTALLED SEAT TRACK IAW SRM 51-30-2 PG.1 2L73 4F A3WE 20041118000342004111800034NM 2004 11 18 04FDEA01731 120040614A5753ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.282 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76743, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20041118000462004111800046EU 2004 11 18 04FDEA02765 120040920A5340A5377866920600 FITTING AIRBUS310 A310222 3930315EU CARGO BAY CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25421FE 342 THE FOLLOWING FWD CARGO COMPT FWD MANHOLE POCKETS HAD CORROSION AT LOCATIONS: (A) AFT OF FS 23 RT SIDE CTR PORTION 2 OFF POCKETS BETWEEN STR 51 RT AND STR 49RT. REPAIR C/W AS PER EA 6-310-77945 AND ALSO REFER TO N00411 AND N00412. RII BY L3167(SIAEC) Y: 275296 RPT BY: 275296. 2L72 4F RTA35EU 20041118000552004111800055NM 2004 11 18 2004UALA01018 120041104A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 MAIN CABIN FLOOR SUPPORT CORRODED AT STA 1640 TO 1660 LBL 50 TO LBL 55. TYPICAL FLOOR STRUCTURE CORROSION. REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA2NM E17NE 20041118000612004111800061EU 2004 11 18 AWXA200401002 120040910A2597 WIRE AIRBUS320 A320231 3930325EU SLIDE OPEN A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28645AW9272 1268 A7269 238 FLIGHT CREW REPORTED EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, AND 5 REMAIN ON AND WILL NOT RESET. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), PROBLEM STILL EXISTS, OHMED L-1 DOOR SLIDE WIRING AND FOUND OPEN READING. REPLACED L-1 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, FUNCTIONAL CHECKS OF EMERGENCY LIGHT SYSTEM AND L-1 DOOR SLIDE WERE GOOD. PART NAME; EPSU, MFG; DIEHL GMBH, P/N; 3214-54, S/N; 7123, TT; 22115, TC; 8589, TSR; 3888. LOC; ZONE 221. 2L72 4F RTA28NM 20041118000642004111800064NM 2004 11 18 04FDEA02750 120040920A5313AJC76751 STRINGER DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 AFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L FROM BOTTOM SUSPECT CRACKED. AFT CARGO, WASTE TANK AT STA Y= 1988 STRINGER END NR 45L SPLICE FITTING. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041118000712004111800071WP 2004 11 18 04FDEA02830 120040927A5343NRC6021523 BEAM DOUG DC10 DC1010F 3022111WP ZONE 700 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 DURING REMOVAL OF ZERT FITTING BUSHING ON LEFT HAND MAIN LANDING GEAR TRUCK BEAM, FOUND BUSHING TO BE THREADED BUSHINGS, NOT PRESS BUSHING. INSTALLED NEW ZERK FITTING IAW FEDEX EA 8-3212-81257 PART 1 DC10 LANDING GEAR MAIN LANDING GEAR TRUCK BEAM BORE REPAIR AUTHORIZATION. REFERENCE NON-ROUTINE N01937. 2L73 4F A22WE 20041118000782004111800078NM 2004 11 18 AWXA200401067 120040905A57536546486155 WEDGE BOEING737 7373G7 1384595NM TE FLAPS DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK, FOUND THE LT INBOARD MID FLAP WEDGE DISBONDED AT THE OUTBOARD END. MAINTENANCE CUTOUT DISBONDED AREA ON LT INBOARD MID FLAP WEDGE AT OUTBOARD END FROM WBL 170.5 TO WBL 175.0; FABRICATED FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS TO FLAP IAW SRM 51-70-10, FIG 31. 2L72 4F RTA16WE 20041118000932004111800093NM 2004 11 18 AWXA200401037 120040918A2560P4010021 BATTERY BOEING737 73733A 1384673NM ZONE 900 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING 4-DAY CHECK, THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041118001022004111800102NM 2004 11 18 04FDEA02761 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.089 INCH, FINAL DIAMETER=1.091 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118001032004111800103NM 2004 11 18 04FDEA02762 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE PIVOT HOLE INBOARD SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL THICKNESS=0.503 INCH, REMAINING THICKNESS=0.498 INCH, MATERIAL REMOVED=0.005 INCH, AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118001112004111800111EU 2004 11 18 AWXA200401209 120041016A5321D5361014900100 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, FOUND R-1 DOOR ENTRY FLOOR PANEL DELAMINATED. MAINTENANCE REMOVED AND REPLACED R-1 DOOR ENTRY FLOOR PANEL IAW T/C C1D25306. 2L72 4F RTA28NM 20041118001192004111800119NM 2004 11 18 AWXA200401070 120040921A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, CORROSION WAS FOUND ON CORNER OF FLOOR PANEL 261 FF. MAINTENANCE REMOVED CORRODED FLOOR PANEL 261 FF, INSTALLED NEW REPLACEMENT PANEL IAW AWA T/C C1D25310. 2L72 4F RTA28NM 20041118001242004111800124NM 2004 11 18 04FDEA03027 120041108A5330 SKIN BOEING727 72722 1384002NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 BS 294, STR 21 RT, DENTS AROUND 3 FASTENERS. REPAIRED PER SRM 53-30-1, 53-30-3. 2L73 4F A3WE 20041118001272004111800127NM 2004 11 18 04FDEA02597 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.221 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041118001282004111800128EU 2004 11 18 AWXA200401234 120041106A335032145410 EPSU AIRBUS320 A320232 3930326EU ZONE 242 FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28651AW2328623275 866 DURING 8-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE RT OVERWING EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041118001292004111800129NM 2004 11 18 04FDEA02555 120040824A5712ARB2850506 RIB DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041118001312004111800131EU 2004 11 18 04FDEA02557 120040824A5347 SEAT TRACK AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25663FE 766 MAIN DECK SEAT TRACK L3 AT FRAME 38 HAS A SCREW HOLE ON FLANGE TORN OUT. REMOVED DAMAGED SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201, INSTALLED NEW SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16, FIG 201. 2L72 4F RTA35EU 20041118001332004111800133NM 2004 11 18 AWXA200401003 120040910A3260189929 PROXIMITY SENSOR BOEING737 7373G7 1384595NM NLG DEFECTIVE A AWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28303AW 24010 ON DESCENT INTO PHX EN ROUTE FROM AUS, AFTER LANDING GEAR EXTENDED, RECEIVED AN INTERMITTENT HORN AND FLASHING UNSAFE NOSE GEAR LIGHT. PROBLEM OCCURRED AFTER BOTH NORMAL AND MANUAL GEAR EXTENSIONS, AS A PRECAUTION REQUESTED EMERGENCY EQUIPMENT STANDBY. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK SENSOR S846 IAW BMM 32-61-41-4, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041118001342004111800134NM 2004 11 18 AWXA200401004 120040905A5315D5347217220200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 RT BETWEEN FS 66 AND FS 68. MAINTENANCE REMOVED CORRODED FLOORBEAM Y1292 RT FROM FS 66 TO FS 68; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041118001352004111800135NM 2004 11 18 AWXA200401005 120040905A5315D5347209400800 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, GALVANIC CORROSION WAS FOUND ON BEAM Y765 LT AT FS 66. MAINTENANCE REMOVED CORRODED BEAM Y765 LT AT FS 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041118001392004111800139NM 2004 11 18 04FDEA02770 120040920A5343 ANGLE BOEING727 727225 1384077NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25462FE 22550 RT MLG WHEEL WELL VERTICAL L-ANGLE CRACKED BS 870 RBL 6 FWD OF APU LWR CORNER . REMOVED AND REPLACED RT WHEEL WELL VERTICAL L-ANGLE BS 870 RBL 6 IAW SRM 51-30-5, 51-30-2, AND 51-10-2. 2L73 4F A3WE 20041118001412004111800141EU 2004 11 18 04FDEA02681 120040912A5320 ANGLE AIRBUS310 A310222 3930315EU WING ROOT CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 FOUND CRACK AROUND 1 OFF FASTENER ON LT WING ROOT TO FUSELAGE LOWER REINFORCEMENT PICK UP ANGLE PLATE AT FS 40/41. ISSUED AND COMPLIED WITH EO 6-5310-7-5003 REV 04 PT 1. CRACK STOP DRILLED, ROTOTEST PERFORMED. PAGE BLOCK 1 FAXED TO RECORDS AND INSPECTION REPORT SENT TO AIRBUS FIELD SERVICE SUPPORT. PERFORMED BY SIAEC AT B-CHK. 2L72 4F RTA35EU 20041118001422004111800142EU 2004 11 18 04FDEA02682 120040914A3411 PITOT LINE AIRBUS310 A310203 3930313EU PITOT STATIC SYSOBSTRUCTED A FDEAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25401FE 191 ON TAKEOFF ROLL AT 80KTS ON CAPT AND FO'S PFD THE AIRSPEED INDICATED 80KTS BUT BOTH STANDBY AIRSPEED INDICATORS WERE STILL SHOWING 60KTS AT 100KTS ON BOTH PFDS THE STANDBY AIRSPEEDS WERE BOTH LESS THAN 80KTS. R BLEW OUT STBY AND NR 1/2 PITOT LINES. FOUND SMALL DEBRIS IN STBY AIRSPEED LINE. OP/C GOOD IAW A310-200 MM 34-11-15-6. NO CHANGE IN RVSM STATUS. 2L72 4F RTA35EU 20041118001432004111800143WP 2004 11 18 04FDEA02855 120041001A5410AUB7054501 VENTILATOR PANEL DOUG DC10 DC1010F 3022111WP ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 NR 3 PYLON TOP PANEL 487DR HAS THREE AREAS OF CRACKS. REPAIRED VENTILATOR ASSY P/N AUB7054-501 IAW FEDEX EA 8-5480-77611. LOCATED AND DRILLED VENTILATOR ASSY IAW DC10 SRM 51-31-01 VOL II. VENTILATOR ASSEMBLY TO BE INSTALLED UNDER FEDEX OPS 43R-FIT. REFERENCE NON-ROUTINE N00166. 2L73 4F A22WE 20041118001452004111800145NM 2004 11 18 04FDEA02598 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.221 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041118001472004111800147NM 2004 11 18 04FDEA02600 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.408 INCH, MATERIAL REMOVED=0.006 INCH, REMAINING THICKNESS=0.402 INCH AND REPAIRED AS PER EA NR 1-5750- 80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041118001482004111800148NM 2004 11 18 AWXA200401159 120041005A53306545772169 SKIN BOEING737 73733A 1384673NM FUSELAGE WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A WORN AREA WAS FOUND ON FUSELAGE SKIN WHERE VERTICAL FIN MEETS FUSELAGE AT BS 967, STR 2 LT. MAINTENANCE BLENDED DAMAGED SKIN AT BS 967, STR 2 LT; FABRICATED WEAR STRIPS PER DWG 65-45772; INSTALLED REPAIR PARTS IAW ER 03-5331-04293-RA2. 2L72 4F RTA16WE 20041118001492004111800149WP 2004 11 18 04FDEA03020 120041104A5410ASL0046 LONGERON DOUG DC10 DC1010 3022110WP ZONE 400 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 FOUND LONGERON FLANGE CHAFED BEYOND LIMITS, AREA 2.5 INCHED LONG BY 0.250 INCHES WIDE, COMPLETELY THROUGH .063 INCH FLANGE, NR 2 RIGHT HAND COWL, JUST AFT OF CENTER HINGE POINT. FABRICATED REPAIR AND INSTALLED REPAIR IAW FEDEX EA 8-5410-81503. 2L73 4F A22WE 20041118001502004111800150NM 2004 11 18 04FDEA02505 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, REAR SPAR, XORS= 690 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 UPPER CHORD CORROSION, REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR CORROSION AND CRACK REPAIR 2L73 4F RTA22WE 20041118001512004111800151NM 2004 11 18 04FDEA01973 120040706A5610 SEAL DOUG MD11 MD11F 3023600NM WINDOW TORN A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25578FE AA11 48458 DURING CLIMB-OUT PASSING FL250, A LOUD NOISE BEGAN FROM LEFT SLIDING WINDOW. NOISE CONTINUED AT VARIOUS ALTITUDES. TRIED ALL ALTITUDES FROM FL250 TO FL350. NOISE DIDN'T STOP UNTIL 9,000 FEET AND 245 KNOTS. DP, WHEN IT STOPPED WAS 3.7 CABIN ALTITUDE WAS 930 FEET. NOISE WAS INTOLERABLE TO ALLOW CONTINUANCE OF FLIGHT. RETURNED TO MEM. BULB SEAL ATTACHED TO SLIDING WINDOW TORN UPPER FWD CORNER. REMOVED AND REPLACED LEFT SLIDING CLEARVIEW WINDOW, REF MD-11 M/M 56-12-01-4. PRESSURIZED A/C TO CHECK FOR LEAKS. NONE NOTED. 2L73 4F RTA22WE 20041118001532004111800153NM 2004 11 18 04FDEA01970 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.224 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041118001542004111800154NM 2004 11 18 04FDEA01969 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.222 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041118001582004111800158NM 2004 11 18 04FDEA02957 120041020A7830491B1330000179 FRAME DOUG MD11 MD11F 3023600NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 ENG NR 1 LEFT HAND T/R COWL TOP AT FORWARD FRAME FOUND CRACKED. FRAME CRACKED REPAIR AS PER DRAWING SRZ78-002. 2L73 4F RTA22WE 20041118001592004111800159NM 2004 11 18 04FDEA02506 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT HAND WING, REAR SPAR, UNKNOWN TO XORS= 620 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 600 TO XORS= 620 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041118001602004111800160NM 2004 11 18 04FDEA02507 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, AT XORS 600 TO XORS 611 LOWER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 611 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041118001612004111800161NM 2004 11 18 04FDEA02508 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, XORS= 720 UPPER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 720 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041118001622004111800162NM 2004 11 18 04FDEA02509 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, AT XORS 690 TO XORS 700 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 TO XORS= 700 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041118001632004111800163NM 2004 11 18 04FDEA01988 120040706A5753ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.254 INCH, AND REPAIRED AS PER EA NR 1-5750-76787, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. 2L73 4F RTA22WE 20041118001642004111800164NM 2004 11 18 04FDEA01989 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 870 - STA 890, RBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 850 TO STA 950, RBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041118001662004111800166NM 2004 11 18 AWXA200401146 120041007A53206553594501 REVEAL BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A 3/4 INCH CRACK WAS FOUND IN R-1 DOOR CUTOUT AFT UPPER REVEAL BS 315 TO BS 328, STR 8 RT. MAINTENANCE REMOVED CRACKED R-1 DOOR CUTOUT AFT UPPER REVEAL; FABRICATED A NEW REPLACEMENT REVEAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 1 & 8. 2L72 4F RTA16WE 20041118001672004111800167WP 2004 11 18 04FDEA02859 120041001A5730ARC06272 PANEL DOUG DC10 DC1010F 3022111WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 66CT HAS SEVERAL AREAS OF DELAMINATION. REPAIRED BY REMOVING DAMAGE, FABRICATING AND BONDING NEW SKIN, CORE AND DOUBLERS IAW DAC DWG ARC0627 AND EA 8-5710-77619, REFERENCE NON-ROUTINE N00129. 2L73 4F A22WE 20041118001692004111800169WP 2004 11 18 04FDEA02860 120041001A5240ARC70112 DOOR DOUG DC10 DC1010 3022110WP TAILCONE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25371FE 46609 COMPLY WITH EA8-5240-82045, TAILCONE PATIO DOOR HINGE REPAIR P/N ARC7011-2. CLOSING ACTION ON 10/01/04. ON N/R S00013. COMPLIED WITH EA 8-5240-82045. 2L73 4F A22WE 20041118001702004111800170WP 2004 11 18 04FDEA01843 120040622A5712ARB1086 RIB DOUG DC10 DC1010 3022110WP LT LEADING EDGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25387FE 46621 LT FIXED LEADING EDGE SLAT TRACK RIB GAUGE REPAIR XOS 427.4. COMPLIED WITH FED EX EA 8-5740-79537, LT FIXED LEADING EDGE SLAT TRACK RIB GOUGE REPAIR XOS 477.41. 2L73 4F A22WE 20041118001712004111800171WP 2004 11 18 04FDEA01844 120040623A3260 CONDUIT DOUG DC10 DC1010F 3022111WP LT MLG UPLOCK MISROUTED A FDEAO OTHER WN INADEQUATE Q C FALSE WARNING CLCLIMB 1 SO2568056 47810 WITH GEAR HANDLE UP THERE IS AN UNSAFE LEFT MAIN INDICATION ON BOTH PANELS. FOLLOWD QRH STEPS AND CYCLED GEAR LIGHTS REMAINED. RETURNED TO MEM. FOUND LT MLG UPLOCK SENSOR CONDUIT MIS-ROUTED BENEATH SENSOR LINK , WHICH PREVENTED THE SENSOR FROM MOVING IN RANGE OF THE TARGET. PROPERLY REROUTED CONDUIT ABOVE SENSOR LINK AS OUTLINED IN ILLUSTRATION IN DC-10 MM 32-61-03-2 FIGURE 202/SHEET 1. FOUND SENSOR TO TARGET GAP WITHIN LIMITS REF:MM 32-61032. SENSOR OPS CHECKED GOOD. REF:MM32-61-03-2. PRIMARY AND SECONDARY INDICATIONS NORMAL. 2L73 4F A22WE 20041118001722004111800172NM 2004 11 18 AWXA200401123 120041001A531165465604 FRAME BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FRAME AT BS 947, INBOARD SIDE OF STR 27 RT. MAINTENANCE CUTOUT DAMAGE ON FRAME AT BS 947, STR 27 RT; FABRICATED A FILLER REPAIR; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG 204. 2L72 4F RTA16WE 20041118001732004111800173NM 2004 11 18 AWXA200401124 120041001A531165465632 FRAME BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FRAME AT BS 967, INBOARD SIDE OF STR 27 RT. MAINTENANCE CUTOUT DAMAGE ON FRAME AT BS 967, STR 27 RT; FABRICATED A FILLER REPAIR; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG 203. 2L72 4F RTA16WE 20041118001742004111800174NM 2004 11 18 AWXA200401125 120041001A534069353522 STRINGER CLIP BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER CLIP FORWARD OF BS 967, STR 25 RT. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 967, STR 25 RT; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 14. 2L72 4F RTA16WE 20041118001752004111800175NM 2004 11 18 AWXA200401126 120041004A53116517684157 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 1 INCH CRACK WAS FOUND IN FRAME AT BS 294, STR 7 LT. MAINTENANCE REMOVED CRACKED FRAME AT BS 294, STR 7 LT; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2L72 4F RTA16WE 20041118001762004111800176NM 2004 11 18 AWXA200401127 120041004A53106614210 SHEAR TIE BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 3/8 INCH CRACK WAS FOUND IN SHEAR TIE (CLIP) AT BS 294, STR 11 LT. MAINTENANCE REMOVED CRACKED CLIP AT BS 294, STR 11 LT; FABRICATED A NEW REPLACEMENT CLIP PER DWG 66-14210; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2L72 4F RTA16WE 20041118001772004111800177WP 2004 11 18 04FDEA02645 120040904A5320AGA74319 LINER DOUG DC10 DC1030F 3023504WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 AFT LOWER CARGO COMPARTMENT FORWARD THRESHOLD ATTACH EAR IS CRACKED. WELD REPAIRED AFT CARGO DOOR LINER IAW FEDEX EA 8-5320-81459. REFERENCE N/R N00682. 2L73 4F RTA22WE 20041118001782004111800178WP 2004 11 18 04FDEA02771 120040920A5410AUB71103 VENTILATOR PANEL DOUG DC10 DC1030F 3023504WP ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 NR 3 PYLON VENT PANEL 487 DR HAS SEVERAL CRACKS. ROUTED OUT CRACKS IN WELDED AREA, FABRICATED FILLER AND WELDED IAW FEDEX EA 8-5480-31457. REMOVED AND REPLACED CRACKED BRACKET, FABRICATED BRACKET IAW DOUGLAS DWG AUB 7054, REINSTALLED SKIN IAW DC10-30 SRM 51-35-01 VOL II. REFERENCE N/R N00689. 2L73 4F RTA22WE 20041118001832004111800183NM 2004 11 18 UPS04443495 120041030A532065B01715547 WEB BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- BS 440 BETWEEN STR 13AL AND 14L FRAME WEB FOUND CRACKED. CRACKED FRAME WEB REPLACED PER SRM 51-10-01. 2L74 4F RTA20WE 20041118001842004111800184NM 2004 11 18 UPS04443499 120041026A5310144U00313 PANEL BOEING747 747200 1384847NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, LT WLG W/W FWD CANTED BULKHEAD LOWER AREA CRACKED AT STA 1241, LBL 94 AS MARKED (CLOSEOUT PANEL). CANTED BULKHEAD LT CLOSEOUT PANEL REPLACED AS PER UPS EO B747-5310-2758-E APPENDIX E. 2L74 4F RTA20WE 20041118001852004111800185NM 2004 11 18 UPS04443500 120041029A531165B01716515 DOUBLER BOEING747 747200 1384847NM FUSELAGE FRAME CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, M/D- BS 460, BETWEEN STR 13-14L, FRAME DOUBLER FOUND CRACK. FRAME DOUBLER REPLACED PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20041118001862004111800186NM 2004 11 18 04FDEA03118 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 20 RT, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041118001882004111800188NM 2004 11 18 2004UALA01030 120041109A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 CABIN FLOORBEAM CAP AT BS 310 CORRODED RBL 44. FABRICATED & INSTALLED NESTED ANGLE REPAIR WITH FILLERS & SHIMS. 2L72 4F4 FRTA2NM E17NE 20041118001892004111800189NM 2004 11 18 2004UALA01038 120041109A212065C280023 DUCT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AC DIST BAY FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29318UA 23950 SKIN, STRINGER AND FRAME HEAT DAMAGE FROM FS 516.5 TO 540. STR 26 TO 28. SUPPLEMENTAL DATA UPDATE - MIX MUFF DUCT OF DUCT ASSEMBLY LOCATED IN MIX CHAMBER AIR DISTRIBUTION BAY AT APPROXIMATE STA 540, BL 0 BLOWN CAUSING HOT AIR TO ESCAPE AND DAMAGE THE STRUCTURE BENEATH. MAJOR REPAIR ACCOMPLISHED. 2L72 4F4 FRTA16WE E2GL 20041118001912004111800191WP 2004 11 18 O3X09098801 220040909A726131081331 LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT NACELLE CRACKED A O3XAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO03880TE231 91 2129604 880 P66138 AC DEPARTED, RT ENGINE LOST OIL PRESSURE DURING CLIMB. ENGINE OIL PRESSURE WARNING LIGHT CAME ON AND ENGINE RPM STARTED TO FLUCUTATE AND EGT WENT TO 750 DEGREES (C). RT ENGINE STOPPED AND FEATHER WAS PULLED AND ENGINE SHUT DOWN. AC RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. ON INSP RT ENGINE NACELLE WAS COVERED WITH OIL. LINE TO PROPELLER GOVERNOR HAD CRACKED CLOSE TO FITTING END GOING TO PROP GOVERNOR. THIS RESULTED IN LOSS OF OIL, OIL PRESSURE AND OVERTEMPING ENGINE. SAME LINE WAS CAUSE OF AN EARLIER OIL LEAK, WAS REPLACED WITH NEW LINE AT THAT TIME. EXCESSIVE ENGINE VIBRATION IS SUSPECTED. PROPELLER BALANCE WAS 13, WITHIN EXPECTABLE LIMITS. ENGINE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.2L72 4T4 TRTA56EU E4WE 20041118001922004111800192EA 2004 11 18 A6WA200440159 120041018A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31422AW 7341 PAX DOOR OUTER HANDLE CAUTION MESSAGE APPEARED IN FLIGHT COMPLIED WITH QRH AND LANDED AT NEAREST SUITABLE AIRPORT DURING CLIMB THR FL210. INSPECTED PAX DOOR LOCKING MECHANISM, NO DEFECTS NOTED, CYCLED DOOR CLOSED AND OPEN SEVERAL TIMES. NOT MESSAGE APPEARED ON GROUND. 2L72 4F4 FRTA21EA E15NE 20041118001932004111800193NM 2004 11 18 USAA050822 120040901A5753 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B1US GL TE FLAP WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 MID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FIG 208. 2L72 4F4 FRTA16WE E2GL 20041118001942004111800194EA 2004 11 18 A6WA200440157 120041018A3210 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31437AW 7744 RT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .041. REMOVED ORIGINAL BUSHING IAW MM 20-26-00-910-802, REAMED WING TRUNNION IAW REO 601R-57-21-003B, INSTALLED NEW 1ST OVERSIZED BUSHING IAW REO 601R-57-21-003B AND REAMED INNER DIAMETER IAW DRG 601R85007. 2L72 4F4 FRTA21EA E15NE 20041118001952004111800195EA 2004 11 18 ASOA04680 120040910A335058728 TRACK CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27889AS 7538 DURING A GROUND INSPECTION, THE FORWARD EMERGENCY FLOOR LIGHTING FROM ROW 5 FORWARD WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED AND REMOVED MOISTURE FROM THE FORWARD EMERGENCY FLOOR LIGHT TRACK AT ROW 5 FORWARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041118001962004111800196EU 2004 11 18 ASOA04807 120041019A3350LP1670 BULB AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27533AS 460 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO HAVE 2 BULBS INOPERATIVE. MAINTENANCE DEFERRED THE EMERGENCY FLOOR LIGHT STRIP IAW MEL NR 33-50-2, CAT C EXPIRING ON 10/29/04. UPON COMPLIANCE WITH SP450 BY MAINTENANCE THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO OPERATE PROPERLY WITH THE BULBS HAVING BEEN INSTALLED AS REQUIRED. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041118001972004111800197NM 2004 11 18 M562004F00005 120040726A5340 MOUNT BOEING737 737400 138449ANM CFMINTCFM56 CFM563C1 13802EU TOILET CORRODED I M56BO OTHER O OTHER NRNOT REPORTED 1 EA0537NY 17852 23976 MAIN CABIN BSTA 947, WL 208, LBL 53, TOILET WALL MOUNT PLATE HAS CORROSION ON TOP SURFACE. FABRICATED NEW MOUNT PLATE CLIPS. C1, C2, C3 INSP 8/4/04. 2L72 4F4 FRTA16WE E21EU 20041118001982004111800198NM 2004 11 18 USAA040806 120040908A5753654643430 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE TE FLAPS DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041118001992004111800199NM 2004 11 18 C7WA200400050 120040922A5313 STRINGER BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 STRINGER 29 RT CORRODED AT STA 950A. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED REPAIR ON RT FLANGE IAW SB 727-0170. 2L73 4F4 F A3WE E2EA 20041118002012004111800201CE 2004 11 18 FFS2004F00004 120040907A52601015141047 LATCH BEECH BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA AIRSTAIR DOOR BROKEN A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575F UC99 THE AFT UPPER CAMLOCK LATCH WAS BROKEN. THE SHAFT ROTATED PROPERLY AS THE DOOR HANDLE WAS ROTATED TO THE LOCK POSITION, BUT APPROXIMATELY HALF OF THE LIP OF THE CAMLOCK WAS MISSING MAKING IT UNABLE TO CAPTURE THE LATCH POST. TOTAL TIME ON PART UNKNOWN. 2L72 4T4 TRTA24CE E4EA 20041119000012004111900001NM 2004 11 19 M562004F00006 120040704A5315 FLOORBEAM BOEING737 737400 138449ANM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED I M56BO OTHER O OTHER NRNOT REPORTED 1 EA0537NY 17852 23976 SURFACE CORROSION ON FLOORBEAM AT STA 348, 15 INCHES LT AND RT OF BL0. REMOVED CORROSION AND TREATED REPAIRED AREA. C1, C2, C3 INSP 8/4/04. 2L72 4F4 FRTA16WE E21EU 20041119000022004111900002NM 2004 11 19 GAIA04140 120040910A5730 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE LT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND LT WING L/E SKIN WS549 CRACKED. REF FASI NR 86708 STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-30-4. 2L73 4F4 F A3WE E2EA 20041119000052004111900005NM 2004 11 19 GAIA04163 120040910A5315 FLOORBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE S760,BL0,LBL20 DAMAGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FLOOR SUPPORT AT BS 760, BL0 TO LBL20 DAMAGED. REF FASI NR 87006, REPLACED FLOOR SUPPORT PN 65-25589-5 IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20041119000062004111900006 2004 11 19 O2G2004F00007 420041026A3452CTL92E CONTROL PANEL CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE ATC TRANSPONDER FAILED E O2GAO OTHER O OTHER CRCRUISE 1 NE03601BE 5103 TRANSPONDER CONTROL PANEL INTERMITTENTLY INOPERATIVE. REMOVED AND REPLACED TRANSPONDER CONTROL PANEL. 2L72 4F4 FRTA21EA E15NE 20041119000082004111900008EU 2004 11 19 ASOA04822 120041005A5753 BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT WING FLAP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE OMEGA BRACKET ON THE LT WING IB FLAP FITTING AT RIB 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OMEGA BRACKET ON THE LT WING IB FLAP FITTING AT RIB 9 IAW SRM 51-25-04. 2H72 4T4 TRTA53EU E20NE 20041119000122004111900012EA 2004 11 19 ASOA04831 120041024A5320601R9515935 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE RT AIR CYCLE MACHINE SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT AIR CYCLE MACHINE SUPPORT BRACKET IAW SRM 51-42-00. 2L72 4F4 FRTA21EA E15NE 20041119000152004111900015EU 2004 11 19 BMAC040010 120041026A3297 WIRE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP DOWNLOCK SWITCH BROKEN A B16AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE05529PA 771 LT MLG IN TRANSITION LIGHT REMAINED ILLUMINATED IN FLIGHT. REPAIRED BROKEN WIRE ON LT MLG DOWNLOCK SWITCH. PERFORMED FUNCTIONAL TEST OF POSITION AND WARNING SYSTEM IAW J-31 MM 32-60-00, CHECKS GOOD. 2L72 4T4 TRTA21EU E4WE 20041119000162004111900016NE 2004 11 19 ALG2004F00066 220040908A7200 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE NR 2 MALFUNCTIONED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03863AL 760536 2055TEC ON TAKEOFF, T-5 WAS IN THE YELLOW AND 51 DEGREES HOTTER THAN THE NR 2 ENGINE, RETURNED TO DEPARTURE AND DID POWER CHECK AND THE NR 1 ENGINE FAILED CHECK. MAINTENANCE REMOVED NR 1 ENGINE ASSY, SN 2055TEC, AND INSTALLED SERVICEABLE ENGINE ASSY SN 20537TEC. (SW03200410323) 1G72 3U3 UNCH1NE E19EU 20041119000172004111900017EU 2004 11 19 KBM2004F00221 120040921A7712303731366 GAUGE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TORQUE STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P 2347 TORQUE GAUGE STUCK AT 70 PERCENT. REPLACED WITH SERVICEABLE GAUGE. 1G71 3U3 UNCH9EU E19EU 20041119000192004111900019EU 2004 11 19 KBM2004F00225 120040907A6710704A34130141 CONTROL CABLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COLLECTIVE BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV 3296 COLLECTIVE CABLE BINDING, REPLACED CABLE AS NEEDED. 1G71 3U3 U H9EU E19EU 20041119000212004111900021EU 2004 11 19 KBM2004F00229 120040901A2150060018 BELT SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE AIR CON BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 76 2300 AIR CONDITIONER BELT BROKE DURING FLIGHT. REPLACED BELT. 1G71 3U3 UNCH9EU E19EU 20041119000222004111900022EA 2004 11 19 ASOA04798 120041015A5297601R578953 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR OUT OF POSITION A ASOAK NONE O OTHER ININSP/MAINT 1 SO27875AS 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH. MAINTENANCE REPOSITIONED THE PASSENGER DOOR CONNECTOR HARNESS AND TRIMMED EXCESS HEAT SHRINK OFF THE WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119000272004111900027NM 2004 11 19 USAA040710 120040910A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 FRAME, .5 INCH CRACK, BS907, S-8L-S-9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER IAW SRM 53-00-07, FIG 202. 2L72 4F4 FRTA16WE E21EU 20041119000282004111900028NM 2004 11 19 USAA040718 120040908A575465C26601197 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 1 SLAT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 TOP SKIN, CORE BOND, 1 INCH SQUARE AREA, NR 1 SLAT IB TE UPPER SURFACE. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10 AND 09. 2L72 4F4 FRTA16WE E21EU 20041119000292004111900029NM 2004 11 19 USAA040719 120041006A5320 WEB BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 CHORD, .7500 INCH X 1.5 INCH X .080 INCH DEEP GOUGE, BS 591 AT RBBL 40 WEB LOWER CHORD RT AIRCO BAY. CUT OUT DAMAGE, INSTALLED FILLER AND STRAPS IAW EA79114. 2L72 4F4 FRTA16WE E21EU 20041119000302004111900030NM 2004 11 19 USAA040739 120041014A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 FLOORBEAM, 2 INCHES, 57.5 INCHES, CORRODED, STA 1640, BL0, RBL 57.5. SPLICED NEW SECTION OF T-CAP IAW TR 53-15-01. 2L72 4F4 FRTA2NM E12EU 20041119000312004111900031NM 2004 11 19 USAA040821 120040930A5420 CHANNEL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 2 NACELLE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, CHANNEL WITH A 4 INCH LONG CRACK IN LOWER CHANNEL AT NR 2 NAC, STA 345. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041119000332004111900033NM 2004 11 19 USAA040808 120040910A5754 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, O5, TOP SKIN- CORE BOND, 2 INCH AREA. NR 4 SLAT IB END TOP SURFACE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041117000392004111700039 2004 11 17 SWAA043320 420041114A256563550 SLIDE BOEING737 7377H4 1384404NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29753SW 29848 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041117000402004111700040NM 2004 11 17 SWAA043321 120041112A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 515, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041117000462004111700046NM 2004 11 17 SWAA043307 120041111A5753 SKIN BOEING737 7373A4 1384585NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 1060 23505 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING FLAP PER MM. 2L72 4F RTA16WE 20041117000492004111700049EU 2004 11 17 MALA040611 120041004A2560D31050105 SLIDE BAC 146 AVRO146RJ85A1500097EU RIGHT FWD DEPLOYED A MALAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL15512XJ E2326 RIGHT FWD SLIDE BLOWN BY RAMP AGENT. MAINTENANCE REPLACED RT FWD SLIDE P/N ON/OFF D31050-105, S/N ON 1549, S/N OFF 1719. REPLACED IAW JOB CARD 2560-501 AND JC 0437. 2H74 4F RTA49EU 20041117000542004111700054EU 2004 11 17 MALA040626 120041013A7600M83726282001P RELAY SAAB SF340 340B 7860101EU MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15361PX 340B249 AFTER DEPARTURE FROM MSP GEAR RETRACTED UP, FLIGHT IDLE STOP OPEN LIGHT REMAINED ON. AIR RETURN TO MSP. MAINTENANCE REPLACED TIME DELAY RELAY P/N M83726-28-2001P AS NEEDED. PERFORMED OPERATIONAL TEST OF F1 STOP MECH IAW AMM 76-10-60. OPS CHECK GOOD. 2L72 4T RTA52EU 20041117000582004111700058EU 2004 11 17 MALA040622 120041012A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15443XJ 340B443 DURING 4K INSPECTION NOTED LAV FLOOR PANEL OUTBOARD SUPPORT FLANGE CORRODED AT STA 272.0. REPAIRED IAW SRM 51-20-42, 51-40-21. 2L72 4T RTA52EU 20041117000702004111700070NM 2004 11 17 UPS04443469 120041101A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, U/D - BS 498 RBL 44 SEAT TRACK CRACKED. CRACKED SEAT TRACK REPAIRED PER SRM 53-10-05 FROM BS 480-520. 2L74 4F RTA20WE 20041117000722004111700072NM 2004 11 17 UPS04M43288 120040822A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP INSPECTION TYPE:C, HORIZONTAL STAB NR 32 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 32 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.130 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 32 LEFT & INSTALLED SLEEVE BUSHING PER EOMD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 32 LT PER EO MD11-5510-19409-H & EN 1309-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041117000752004111700075EU 2004 11 17 MALA040675 120041104A3246 BEARING SAAB SF340 340B 7860101EU MLG WHEEL WORN A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15362PX 340B258 AIRCRAFT IS HARD TO CONTROL WHILE BRAKING. A/C WILL NOT TURN RIGHT WHILE BRAKING, ALSO BRAKES MAKING A HOWLING NOISE. MAINTENANCE FOUND RIGHT O/B MAIN TIRE BEARINGS EXCESSIVELY WORN, CAUSING TIRE TO WOBBLE AND BRAKES TO HOWL. REPLACED RIGHT O/B MAIN TIRE AND BRAKE ASSEMBLY. ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20041117000772004111700077NM 2004 11 17 SWAA043301 120041111A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 EEPLS COVER AT ROW 1 ABC, LOOSE. SECURED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041117000832004111700083EA 2004 11 17 COMA0460599 120041110A5210601R3199831 SKIN CNDAIR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01941CA24580 7050 7050 FLIGHT DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH COMAIR ENGINEERING AUTHORIZATION EA 10-5210-00499. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20041117000842004111700084EU 2004 11 17 MALA040629 120040905A5320 WEB SAAB SF340 340B 7860101EU FWD ENTRYWAY CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED FWD ENTRY WAY WEB CORRODED STA 288-294. REPLACED WEB PER SRM. AIRCRAFT RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117000852004111700085 2004 11 17 UPS04143086 420040909A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01159UP 0005 INSPECTION TYPE:N/A EVACUATION SLIDE WARNING LIGHT INOP, DFRD M287411. RESET ASPSU, OPS NORMAL, REF AMM 52-73-00-5. 2L72 4F RTA35EU 20041117000992004111700099WP 2004 11 17 UPS04843364 120040918A53203779762U501 FITTING DOUG DC8 DC871F 302199DWP LONGERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, LONGERON 6R END FITTING CRACKED STA 674. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. 2L74 4F RT4A25 20041117001022004111700102WP 2004 11 17 UPS04843368 120040918A532037549182 FITTING DOUG DC8 DC871F 302199DWP CUSP WEB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, RIGHT UPPER CUSP FITTING CRACKED STA 1174. REMOVED AND REPLACED CRACKED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20041117001032004111700103WP 2004 11 17 UPS04843370 120040921A531046473651 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, CRACKED FITTING IN MAIN CABIN SUBFLOOR, FS 978-980 IN CORNER, LBL 66. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 20041117001082004111700108EA 2004 11 17 COMA0460608 120041031A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA COCKPIT DETECTED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01507CA 7796 FLIGHT 4940 ODOR IN COCKPIT LIKE BURNED RUBBER. COULD NOT DUPLICATE. OPERATIONAL CHECK OF AC SYSTEM NORMAL. NO BURNED RUBBER. 2L72 4F RTA21EA 20041117001292004111700129EU 2004 11 17 MALA040650 120041028A2620AE711192 TUBE BAC 146 AVRO146RJ85A1500097EU FIRE EXTINGUISHECONTAMINATED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15534XJ E2370 DURING NR 1 CARGO FIRE EXTINGUISHER CHANGE FOUND FLEX TUBE P/N AE711192, UNION P/N AN832 SOLID LINE P/N AE40114-4 FILLED WITH UNKNOWN SUBSTANCE. MAINTENANCE REMOVED AND REPLACED RIGID AND FLEXIBLE LINE IAW AMM CH 26, ALL CHECKS GOOD. 2H74 4F RTA49EU 20041117001352004111700135NM 2004 11 17 UPS04443093 120040815A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, LT BS 360 UPPER DECK FLOORBEAM FOUND ONE EACH FASTENER HOLE CRACKED AT FRAME WEB. FRAME REPAIRED AS PER HX RS R53-12-35184 & UPS EO B747-5310-20987-A. 2L74 4F A20WE 20041117001362004111700136NM 2004 11 17 UPS04443094 120040816A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D BS 380 STR 17L FRAME CRACKED. FRAME REPAIRED AS PER HX RS R53-12-35186 & UPS EO B747-5310-20989-A. 2L74 4F A20WE 20041117001382004111700138NM 2004 11 17 UPS04443096 120040816A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, M/D- BS 500, STR 14R FRAME FOUND CRACKED. M/D BS 500 STR 14R CRACKED FRAME REPAIRED AS PER HX RS R53-12-35185 & UPS EO B747-5310-20988A. 2L74 4F A20WE 20041117001422004111700142WP 2004 11 17 UPS04843099 120040819A53403755822505N FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE:C2 A-PIT FS 300 BATHTUB FITTING BETWEEN L34L & L33L HAS HEAVY CORROSION. REMOVED BATHTUB FITTING. FABBED REPAIR ANGLES PER SRM 53-2-0 FIG 2B. INSTALLED NEW FITTING AND REPAIR ANGLES PER SRM 53-2-0 FIG 2B, 51-1-20D. 2L74 4F RT4A25 20041117001432004111700143WP 2004 11 17 UPS04843100 120040823A5530SRO9538005 ATTACH ANGLE DOUG DC8 DC871F 302199DWP VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE:C2 VERT STAB LOWER FRONT SPAR EXTERNAL DRAG ANGLE CRACKED AT STA 1756. REMOVED DOUBLER PER SRM 51-3-0, 51-1-21. STOP DRILLED CRACK PER SRM 53-2-0, NDT VERIFIED STOP DRILL PER SPM 06-10-01.001. FABBED REPAIR ANGLE FROM S25043-17-7PH .080. HEAT TREATED PER AMS 2759 & SRM 51-1-6. INSTALLED ANGLE PER SRM 53-2-5 FIG 16A, 51-1-20D, 51-1-15, SAA SK-708-048. 2L74 4F RT4A25 20041117001452004111700145 2004 11 17 UPS04143140 420040923A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE ILLUMINATED A IPXAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01156UP 0845 ESCAPE SLIDE WARNING LIGHTS BEGAN FLASHING INFLIGHT FOLLOWED BY WARNING HORN. SEATED DOOR HANDLE AND CONDITION CLOSED. PERFORMED RIG CHECK AND OPS CHECK PER MM 52-10-20-5, ALL CHECK GOOD. THIS CLEARS M288227. 2L72 4F RTA35EU 20041117001462004111700146WP 2004 11 17 UPS04843164 120040831A53403750330519 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE: C2, LONGERON 32R SPLICE FITTING CRACKED FROM STA 620 TO STA 640. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 20041117001482004111700148WP 2004 11 17 UPS04843166 120040830A53403755822506N FITTING DOUG DC8 DC871F 302199DWP LOWER CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 INSPECTION TYPE: C2, BATHTUB FITTING CRACKED AT STA 280 L27L. REMOVED CRACKED FITTING. FABBED REPAIR PARTS FROM BAC1503-100163 PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING AND REPAIR PARTS PER SRM 53-2-0 FIG 2D, 51-1-8, 51-1-20D, 51-3-0, 51-1-15. 2L74 4F RT4A25 20041117001692004111700169WP 2004 11 17 UPS04843453 120041010A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB IS CHAFED THROUGHT AT XS 515-720. BLENDED CHAFED AREA IAW DC-8 SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2, 57-3-1 & 51-1-20D. 2L74 4F RT4A25 20041117001772004111700177WP 2004 11 17 AALA20041086 120041031A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21983TW 53633 STL - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041117001802004111700180EU 2004 11 17 MALA040625 120041027A5550 SKIN SAAB SF340 SF340A 7850100EU STABILIZER DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 DURING 4Y/2Y INSPECTION IN BNA, NOTED 7 DENTS IN LT UPPER STAB SKIN. FIVE ARE WITHIN LIMITS PER THE SRM & 2 WERE DELAMINATED AND REPAIRED PER EO S55017. 2L72 4T RTA52EU 20041117001812004111700181EU 2004 11 17 MALA040627 120040904A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15412XJ 340B412 DURING 4Y/2Y INSPECTION IN BNA, NOTED BL 0 FLOORBOARD ATTACH ANGLE CORRODED AT STA 294. FABRICATED & REPLACED ANGLE PER THE SRM. AIRCRAFT WAS RETURNED TO SERVICE 9/7/04. 2L72 4T RTA52EU 20041117001882004111700188EU 2004 11 17 MALA040642 120040918A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15441XJ 340B441 DURING 4K INSPECTION IN BNA, NOTED DAMAGE TO SEAT TRACK LBL 18.3 STA 344. REPAIRED IAW THE SRM. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041117001992004111700199 2004 11 17 SWAA043251 420041108A2565D31354 GIRT BAR BOEING737 7373Q8 1384670NM R2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR BROKEN. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041117002062004111700206NM 2004 11 17 AALA20041123 120041110A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21783AN 30004 DFW - SEAT EMERGENCY ESCAPE PATH LIGHT IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY ESCAPE PATH LIGH IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041117002132004111700213NM 2004 11 17 04FDEA03103 120041112A5347FX6970 SEAT TRACK BOEING727 72722 1384002NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25186FE 18872 FWD CARGO SEAT TRACK RT SIDE AT PFM BOX HAS A GOUGED/WORN LOBE. REMOVED FWD CARGO SEAT TRACK RT SIDE AT PFM BOX IAW SRM 51-30-02. CHECKED LIMITS IAW SRM 53-10-05. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SECTION OF SEAT TRACK UNDER TRAVELER NR T4/469064. TREATED AND PRIMED IAW SRM 51-10-02. LOCATED, DRILLED AND INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 51-30-02. 2L73 4F A3WE 20041117002142004111700214EU 2004 11 17 04FDEA03104 120041113A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 MAIN DECK CARGO COMPARTMENT ZONE 230 SEAT TRACK ADAPTERS, (6 EACH) AT LEFT SIDE FS 33, 35, 36, AND 37 AND ONE EA AT FS 38 IS GOUGED. BLENDED OUT GOUGES AND FOUND ANOTHER CLA GOUGED AT FS 32, ALL BLENDED OUT BEYOND LIMITS. REMOVED AND REPLACED CARGO LOADING ADAPTERS AT NOTED LOCATIONS IAW SRM 51-72-10. 2L72 4F RTA35EU 20041118000072004111800007EU 2004 11 18 04FDEA03085 120041111A5270 SWITCH AIRBUS310 A310203 3930313EU PAX DOOR OUT OF RIG A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25409FE 273 RIGHT CABIN DOOR INDICATED UNLOCKED AS SOON AS PRESSURIZED. AIR TURN BACK, REMOVED AND REPLACED R-1 DOOR SWITCH RIG AND OPS CHECK GOOD IAW A310 AMM 52-71-11. 2L72 4F RTA35EU 20041118000142004111800014NM 2004 11 18 04FDEA03093 120041112A5510ALC810Y2 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON NR 14 RT BARREL NUT BORE FOUND EXCEEDED LIMITS. FITTING REMOVED AND REPLACED (P/N ALC8106Y2) PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20041118000152004111800015NM 2004 11 18 04FDEA03094 120041112A5313 LONGERON DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO, LONGERON FOUND DENT AT RT STA Y= 1547, LONGERON 13. SMOOTHENED PER SRM 51-00-00 VOLUME I, PAGES 1 AND 2. HFEC INSPECTION CARRIED OUT PER DAC NDT SPM REV. 11, CHAPTER 06.10.01.001, NO CRACK FOUND. 2L73 4F RTA22WE 20041118000282004111800028EU 2004 11 18 AWXA200400966 120040811A5210FE1740011 DAMPER AIRBUS320 A320231 3930325EU L-1 DOOR BYPASSING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW12620 077 DURING C-04 CHECK, THE L-1 DOOR DAMPER ASSEMBLY HAD NO DAMPENING EFFECT. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR DAMPER CYLINDER ASSEMBLY IAW AMM 52-11-14-04. 2L72 4F RTA28NM 20041118000322004111800032NM 2004 11 18 AWXA200400854 120040807A2612BACC45FT1212S CONNECTOR BOEING757 757225 1384959NM ZONE 120 BROKEN A AWXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28913AW 22207 ON MAINTENANCE FERRY EN ROUTE FROM LCQ TO PHX AT FL 390, RECEIVED RT ENGINE FIRE INDICATION FOLLOWED BY MULTIPLE EICAS AND STATUS MESSAGES. FIRED THE RT ENGINE FIRE BOTTLE AND APPROXIMATELY 10 MINUTES LATER RECEIVED LT ENGINE FIRE EICAS MESSAGE AND WARNING BELL. DIVERTED TO DFW AND CONTINUED TO RECEIVE INTERMITTENT EICAS AND STATUS MESSAGES UNTIL AIRCRAFT WAS ON SHORT FINAL APPROACH, (RAT SELF DEPLOYED). MX REMOVED AND REPLACED ELECTRONIC WARNING SYSTEM POWER SUPPLIES "A"/"B" IAW BMM 31-51-04-401. ELECTRONIC WARNING SYSTEM "B" STILL FAILS TEST PER FIM 31-51-00. REPLACED EMI FILTER MODULE IAW BMM 31-51-01-4, PROBLEM STILL EXISTS. 2L72 4F RTA2NM 20041118000412004111800041WP 2004 11 18 04FDEA02822 120040927A5753ARC2512501 HINGE DOUG DC10 DC1010F 3022111WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LEFT HAND INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT OUTBOARD BORE CORRODED. CORROSION EXCEEDS CMM 57-52-01 LIMITS. REPAIRED IAW FEDEX EA 8-5750-77622. REFERENCE NON ROUTINE N00490. 2L73 4F A22WE 20041118000572004111800057EU 2004 11 18 04FDEA02747 120040920A5311A5361055400200 FRAME AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25421FE 342 FUSELAGE FRAME 13A FWD AND AFT FACE AT STRINGER 44 LT FOUND SIGNS OF CORROSION. REPAIR C/O AS PER EA 6-5310-77954. RII L4724 (SIAEC). 2L72 4F RTA35EU 20041118000602004111800060 2004 11 18 04FDEA02141 420040720A3416 WARNING LIGHT DOUG MD11 MD11F 3023600NM COCKPIT ILLUMINATED A FDEAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO25596FE 48554 AT 100KTS, CAPT RECEIVED AN "ALT" ALERT IN PFD AT ROTATION F/O LOST ALL AIRSPEED, ALT INDICATIONS. APPROX 1 MIN LATER RECIEVED 3X FADEC ALTN, SEL ELEV FEEL MANUAL AND RED SLOW SPEED ZIPPER IN FO PFD. QRH PROCEDURES ACCOMP, CADC-1 WAS GOOD. ISOLATED CADC-2 OFF. PER CREW DEBRIEF ALL CAPT, F/O IND NORMAL WITH F/O CADC SISP S/W TO F/O ON 1. T/S PER FIM 34-16-00. DURING CADC-2 ADJ/TEST PER MM. GOT INTERMITTENT ADC FAIL YELLOW FAULT BALL. R/R`D CADC-2 PER MM AND PERFORMED OP`S TEST/INTERFACE TEST AND CAT3B RTS TEST MM. ALL TESTS NORMAL. PERFORMED SAME ON CADC-1 AND FOUND NORMAL. INSPECTED PITOT TUBES/STATIC PORTS FOR OBSTRUCTIONS AND NONE FOUND. A/C OK FOR SERVICE AND REMAINS CAT3B. 2L73 4F RTA22WE 20041118000632004111800063EU 2004 11 18 04FDEA02749 120040920A5311A5361138920000 FRAME AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25421FE 342 FOUND CORROSION AT FUSELAGE FRAME 12A AFT FACE AT VICINITY OF STRINGER 44LH. REPAIR C/W AS PER EA 6-5310-77952. RII BY L4724. 2L72 4F RTA35EU 20041118000652004111800065NM 2004 11 18 04FDEA02751 120040920A5320A6A71231 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 CRACKED. CRACKED AREA AT CENTER ACCESSORY COMPARTMENT, LONGERON 38R END SPLICE AT BETWEEN STA Y= 6-100 TO STA Y= 1139 TRIMMED OUT AS PER SRM 53-00-01 VOL I AND EA NR 1-5310-77963 FIGURE 2. REPAIR STRAP FABRICATED AND INSTALLED AS PER EA NR 1-5310-77963, TITLE: FUSELAGE, MAIN FRAME, CAC COMPARTMENT BODY STATION 6-100, LONGERON 38 (RT) SPLICE REPAIR. 2L73 4F RTA22WE 20041118000672004111800067NM 2004 11 18 04FDEA02753 120040920A5753ARC199113 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORRODED. LEFT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.079 INCH, FINAL DIAMETER=1.081 INCH AND REPAIRED AS PER EA NR 1-5750-79750, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118000762004111800076NM 2004 11 18 AWXA200401066 120040921A5280 STRUCTURE AIRBUSA319 A319132 3930340NM RT MLG DOOR DAMAGED A AWXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 WP28804AW 1049 ON CLIMB-OUT OF PHX EN ROUTE TO RNO AT FL 200, FELT STRONG AIRFRAME VIBRATION ASSOCIATED WITH A WITH A LOAD RUMBLE, REDUCED SPEED FROM 340 KTS TO 320 KTS AND VIBRATION WENT AWAY, LANDING LIGHTS RETRACTED AT FL 100. MAINTENANCE PERFORMED ELEVATOR FREE PLAY CHECK; LT AND RT ELEVATOR SERVOS ARE WITHIN LIMITS. FOUND RT MLG RAMP DOOR MAIN ATTACH POINT HOLES ELONGATED CAUSING DOOR TO VIBRATE, REMOVED AND REPLACED RT MLG RAMP DOOR ASSEMBLY IAW T/C R4M32308. ALSO, REPLACED BUSHING ON LT MLG FIXED DOOR LOWER ATTACH POINT, OPERATIONAL TEST AND CLEARANCE CHECKS WERE GOOD. 2L72 4F RTA28NM 20041118000772004111800077NM 2004 11 18 AWXA200400631 120040609A212165771 BLOWER BOEING737 7373G7 1384595NM ZONE 202 DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28308AW284236228 24710 ON CLIMB-OUT OF PHX EN ROUTE FOR GEG, EQUIPMENT COOLING "OFF" LIGHT ILLUMINATED, SYSTEM INOPERATIVE IN NORMAL AND ALTERNATE, DIVERTED TO LAS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED LOW FLOW SENSORS M100 AND T-464 IAW BMM 21-58-43, AND REPLACED AIR FILTER FOR EQUIPMENT BLOWER FANS, ALTERNATE SYSTEM OPERATIONAL CHECK WAS GOOD. NORMAL EQUIPMENT COOLING FAN STILL INOPERATIVE; ISSUED MEL 21-27, COND. 2 "EQUIPMENT COOLING SUPPLY FAN INOP". SUPP - ON 06/15/2004 MAINTENANCE REMOVED AND REPLACED THE MAIN EXHAUST EQUIPMENT COOLING FAN IAW BMM 21-58-12. SUPP - EXHAUST EQUIPMENT COOLING FAN S/N 6579 FAILED FUNCTIONAL CHECK AT REPAIR VENDOR FOR LOW RPM. FOUND BEARINGS ROUGH AND BINDING. 2L72 4F RTA16WE 20041118000822004111800082NM 2004 11 18 AWXA200401020 120040905A521090100722 SNUBBER BOEING737 7373G7 1384595NM L-1 DOOR WEAK A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK, THE L-1 DOOR SNUBBER FAILED STEP 4.1 OF T/C I1A52001 FOR WEAK OPERATION. MAINTENANCE REMOVED AND REPLACED L-1 DOOR SNUBBER IAW BMM 52-11-71-4, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041118001092004111800109EU 2004 11 18 04FDEA02592 120040901A5530 FORK AIRBUS310 A310203 3930313EU VERTICAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 VERTICAL STAB STA 690/RIB 21 HINGE FORK NR 6 IS CORRODED. REMOVED AND REPLACED HINGE ARM ASSY IAW A310-200 AMM55-36-46-4-01, FUNCTIONAL TEST GOOD IAW A310-200 AMM 27-20-00-5. 2L72 4F RTA35EU 20041118001132004111800113WP 2004 11 18 04FDEA02595 120040901A5753ARC2512 HINGE DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 COMPLY WITH EA 8-5750-80598, WINGS LT INBD FLAP INBD MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COMPLIED WITH EA 8-5750-80598. 2L73 4F RTA22WE 20041118001142004111800114WP 2004 11 18 04FDEA02596 120040901A5753ARC0154 HINGE DOUG MD10 MD1010F 3022112WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 COMPLY WITH EA 8-5754-80608, WINGS, LEFT INBD FLAP, OUTBD HINGE BRACKET, UPSTOP MOUNT HOLE REPAIR P/N ARC 0154. COMPLIED WITH E.A.8-5754-80608. 2L73 4F RTA22WE 20041118001162004111800116NM 2004 11 18 04FDEA03075 120041111A55126572796 SKIN BOEING727 72722 1384002NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 RT HORIZ STAB UPPER SKIN LOWER SURFACE HAS CORROSION (C55-300-10(2)) EMANATING FROM BONDED DOUBLERS 33 INCHES FROM AFT EDGE AND 30 INCH FROM I/B EDGE. RT HORIZONTAL STAB UPPER SKIN LOWER SURFACE FOUND TO BE OUT OF LIMETS REPAIRED PER FED-EX EA 7-5510-82519 AND FED-EX EA 7-5510-82518. 2L73 4F A3WE 20041118001182004111800118WP 2004 11 18 04FDEA02848 120040930A5711 SPAR DOUG DC10 DC1010F 3022111WP LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO256805165522 47805 FUEL LEAK LT WING REAR SPAR AREA AT XORS STATION 346 LOWER CHORD ANGLE. INSPECTED AREA WITH HFEC AND DETECTED A CRACK INDICATION ALONG HORIZONTAL FLANGE INTO RADIUS AND UP VERTICAL FLANGE. TOTAL LENGTH OF CRACK IS APPROXIMATELY 4.650 INCH. 2L73 4F A22WE 20041118001232004111800123NM 2004 11 18 AWXA200401074 120040921A5315D53472172204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT FORWARD AND AFT OF FS 67. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 67 TO FS 68; FABRICATED A NEW REPLACEMENT SECTION OF BEAM PER DWG 18D53472172; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041118001262004111800126WP 2004 11 18 04FDEA02912 120041011A5744ARC01541 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750-81473. PRIMED LUGS IAW DC109 SRM 57-21-01 VOLUME II. BEGINNING BORE 1.255 INCH REMOVED .0200 INCH FINAL 1.2360 INCH. FOUND TO BE WITHIN LIMITS IAW DACCMM 57-44-07. 2L73 4F RTA22WE 20041118001362004111800136NM 2004 11 18 AWXA200401006 120040905A5347D5311282720100 SEAT TRACK AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28809AW 1111 DURING BC-4 CHECK, CORROSION WAS FOUND ON DUMMY RAIL Y503 LT AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 LT AT FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG 9-12, PG. 23-28. 2L72 4F RTA28NM 20041118001562004111800156NM 2004 11 18 04FDEA01986 120040706A5753ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.248 INCH, AND REPAIRED AS PER EA NR 1-5750-76787, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. APPROVED AS A TEMPORARY REPAIR UNTIL DAMAGE TOLERANCE ASSESSMENT IS ACCOMPLISHED. 2L73 4F RTA22WE 20041118001792004111800179WP 2004 11 18 04FDEA02861 120041001A5330AYB70301 SKIN PANEL DOUG DC10 DC1010F 3022111WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION FROM STATION 1350 TO 1521, L48L TO L48R. COMPLIED WITH FEDEX EA 8-5330-77624, SKIN SPLICE REPAIR AT STATION 1350-1521 REPAIR. REFERENCE NON-ROUTINE N01775. 2L73 4F A22WE 20041119000032004111900003NM 2004 11 19 GAIA04147 120040910A5347 SEAT TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE WRONG PART A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK STA 344-480, LBL 24.75 IS NOT IN COMPLIANCE WITH DRW NR 2902. REF FASI NR 86788 REMOVED AND REPLACED SEAT TRACK IAW DRW NR 2902. 2L73 4F4 F A3WE E2EA 20041119000042004111900004NM 2004 11 19 GAIA04149 120040910A5347 SEAT TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE WRONG PART A GAIAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND SEAT TRACK, STA 344-480, RBL 24.75 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR 86790, REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902. 2L73 4F4 F A3WE E2EA 20041119000092004111900009EA 2004 11 19 ASOA04808 120041020A3350BR9729232 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A SERVICE CHECK, THE FORWARD EMERGENCY FLOOD LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOD LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119000112004111900011NM 2004 11 19 ASOA04816A 120041002A5320S5397081624901 ANGLE BOEING737 737790 13844CNNM PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27623AS 30166 DURING A C-CHECK, THE FRAME AND ANGLE AT FR28A ON THE RT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FRAME AND ANGLE AT FR 28A ON THE RT SIDE IAW WITH SRM 51-25-01. 2L72 4F4 TRTA16WE E20NE 20041119000142004111900014NM 2004 11 19 USAA040797 120040912A5210313A1355650 ANGLE BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE AFT DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, Z-ANGLE, 4 INCHES LONG, CORROSION; LEVEL 1 TASK NR C53-107-01 AFT ENT DOOR Z-ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG. 2L72 4F4 FRTA16WE E2GL 20041119000182004111900018EU 2004 11 19 KBM2004F00223 120040910A6410355A09103601 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19215LA960 2143 BEARING HALF SHELLS WORN AND TORN. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20041119000242004111900024EA 2004 11 19 ASOA04793 120041012A3350GE1495X LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27830AS 7236 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119000382004111900038EU 2004 11 19 KBM2004F00219 120040824A21210500847 MOTOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE BLOWER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH100 3141 A/C INOPERATIVE. REMOVED AND REPLACED 7 INCH BLOWER MOTOR. 1G71 3U3 U H9EU E19EU 20041119000422004111900042NM 2004 11 19 USAA040738 120041014A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 FLOORBEAM, 2 INCH X 57.5 INCH, CORROSION, STA 1640, BL0 TO LBL 57.5. SPLICED NEW T-CAP SECTION IAW TR 53-15-01. 2L72 4F4 FRTA2NM E12EU 20041119000432004111900043EU 2004 11 19 ASOA04818 120041003A5320S5367800821602 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE Z-FLOOR SUPPORT BETWEEN FR 39-41 ON THE RT SIDE NEAR THE THRESHOLD WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE Z-FLOOR SUPPORT BETWEEN FR 39-41 ON THE RT SIDE NEAR THE THRESHOLD IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041119000442004111900044WP 2004 11 19 Y2PA04023 120040923A3297 GROUND WIRE DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE DN LIMIT SWITCH BROKEN E Y2PAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL23194US 47016 NO GEAR INDICATION ON LT MAIN GEAR, EITHER RED OR GREEN. CREW DECLARED AN EMERGENCY AND DIVERTED. CREW FOLLOWED COM PROCEDURES WITH NO HELP. LT GEAR INDICATION DOES NOT TEST (RED AND GREEN LIGHTS INOPERATIVE). AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC SENT TO TROUBLESHOOT. REMOVED AND REPLACED LT MLG DOWN LIMIT SWITCH IAW MM AND DISCREPANCY REMAINED. THE R2-28 RELAY WAS REMOVED AND REPLACED IAW MM AND DISCREPANCY REMAINED. THEN FOUND A BROKEN GROUND WIRE AT THE DOWN LIMIT SWITCH CONNECTOR PLUG. GROUND WIRE WAS REPAIRED AND THE GEAR INDICATION SYSTEM THEN OPERATIONALLY CHECKED GOOD IAW MM 32-60-0. 2L72 4F4 F A6WE E2EA 20041119000452004111900045WP 2004 11 19 ZIAA04082 120040928A2612702120 FIRE LOOP LKHEED188 188A 5262602WP ALLSN 501D 501D13A 03004GL NR 3 ENGINE FALSE INDICATIONA ZIAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DEDESCENT 1 GL23346HA 188A1043 SHUTDOWN NR 3 ENGINE DUE TO ZONE 1 FIRE WARNING AT 2004Z. DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED ZONE 1 FIRE LOOP IAW L188 MM 26-1-0. NO FIRE WARNING NOTED ON EXTENDED GROUND RUN AT 847 DEGREES. 2L74 4T4 TRT4A22 E282 20041119000512004111900051NM 2004 11 19 GAIA04096 120040910A5312 PRESSURE PANEL BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NOSE WW RT SIDE WEB STA 268.25 HAS MANY REPAIRS OVERLAPPED. REF FASI NR 86351, INSTALL DOUBLER REPAIR IAW SRM 51-40-2 AND S/E 727 53-0145, REV 1. 2L73 4F4 F A3WE E2EA 20041119000522004111900052NM 2004 11 19 GAIA04097 120040910A5312 PRESSURE PANEL BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DAMAGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NOSE WHEEL WELL LT WEB AT STA 268.25, PREVIOUS REPAIRS OVERLAPPING AND NO SPACING BETWEEN REPAIRS. REF FASI NR 86352, REMOVED EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR IAW SB 727-53-145 REV 1 AND SRM 51-40-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041119000532004111900053NM 2004 11 19 GAIA04098 120040910A5312 PRESSURE PANEL BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DAMAGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NOSE WHEEL WELL UPPER WEB AT STA 294.5, PREVIOUS REPAIRS OVERLAPPING AND NO SPACING BETWEEN REPAIRS. REF FASI NR 86354, REMOVED EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR IAW SB 727-53-145 REV 1 AND SRM 51-40-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041119000542004111900054NM 2004 11 19 GAIA04104 120040910A5521 SPAR BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE RT ELEVATOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND RT ELEVATOR REAR SPAR CRACKED. REF FASI NR 86374 REPLACED RT ELEVATOR REAR SPAR IAW SB 727-55-0089, REV 1. 2L73 4F4 F A3WE E2EA 20041119000552004111900055NM 2004 11 19 GAIA04112 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CANNING A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN OIL CANNED BETWEEN BS446, BS460 ABOVE STR 19 LT. REF FASI NR 86517, CUT OUT DAMAGED AREA DIM 7.5 X 3.375. INSTALLED REPAIR IAW FVCI DWG NR 53-04396-1. 2L73 4F4 F A3WE E2EA 20041119000582004111900058EA 2004 11 19 ASOA04794 120041013A3350GE1495X LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27902EV 7620 DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119000592004111900059EU 2004 11 19 ASOA04823 120041005A5320 ANGLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE FRAME TO INTERCOSTAL ANGLES AT FR 23D AND LT AND RT STRINGER 1 IN THE WING BOX WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FRAME TO INTERCOSTAL ANGLES AT FR 23D AND LT AND RT STRINGER 1 IN THE WING BOX IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041119000612004111900061SW 2004 11 19 ALG2004F00070 120041025A7712 GAUGE BELL 407 407 1182206SW ALLSN 250C 250C30P 03013GL TORQUE OVERTORQUED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03627AL 53284 CAE847064 DURING TAKEOFF, TORQUE GAUGE OVERTORQUED WITH NO OTHER EXCEDENCES. THE MECHANIC DRIED THE MOISTURE FROM TORQUE TRANSMITTER, COMPLIED WITH GROUND RUN AND AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 UO H2SW E1GL 20041119000632004111900063NM 2004 11 19 USAA040705 120040921A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 PIT,Q2, FLOOR SUPPORT .1250 INCH X .2500 INCH AREA, CORROSION, LEVEL 1; TASK NR C53-107-02. FLOOR SUPPORT, BETWEEN STA 312 AND 344, APPROX. 10 INCHES LT OF CENTER. CLEANED, TREATED, PRIMED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-06B. 2L72 4F4 FRTA16WE E21EU 20041119000672004111900067EU 2004 11 19 DAT2004F00006 120040910A2910SD33730748XA LINE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA HYD SYSTEM LEAKING E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13336MV SH3018 DURING CLIMB OUT, WHEN GEAR WAS RAISED, FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R LIGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. EMERGENCY CRUISE AND DESCENT CHECKLISTS WERE COMPLETED. THE ATC WAS NOTIFIED AND IT WAS REQUESTED TO LAND IMMEDIATELY. AIRCRAFT LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STATIONED ALONG THE RUNWAY. MECHANIC WAS DISPATCHED. RT MAIN GEAR DOWNLOCK HYDRAULIC LINE HAD A HOLE IN IT. HYDRAULIC LINE WAS REMOVED AND REPLACED IAW MM. HYDRAULIC FLUID WAS REPLENISHED IAW MM. GEAR SWING WAS NOT COMPLETED AND THE GEAR WAS PINNED. 2H72 4T4 T A41EU E4EA 20041119000682004111900068NM 2004 11 19 USAA040721 120041001A5320 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 ZEE ANGLE, 1 TO 2 INCHES OF CORROSION; 5 PLACES, CORROSION; LEVEL 1; TASK NR C53-107-01, AFT ENTRY DOOR Z ANGLE STA 962-986. 2L72 4F4 FRTA16WE E21EU 20041119000692004111900069GL 2004 11 19 ALG2004F00068 220041026A7230 COMPRESSOR BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE STALLED E ALGAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW031067D 45435 ON FINAL APPROACH, MC486 POWER WAS REDUCED, THE COMPRESSOR BEGAN TO STALL, AC LANDING WAS UNEVENTFUL. MECHANIC INSPECTED ENGINE INLET AND COMPRESSOR AREA, COMPLIED WITH AIR LINE LEAK CHECK, TIGHTENED 2 GOVERNOR LINE FITTINGS, RINSED THE ENGINE AND FOUND EVIDENCE OF GRASS PARTICLES. GROUND RAN, LEAK CHECKED THE ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E1GL 20041119000702004111900070NM 2004 11 19 ASAA0470013 120040830A5512186A14015 SKIN BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE HORZONTAL STAB DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 DENT ON LT LE HORIZONTAL STABILIZER. ACCOMPLISHED PERMANENT REPAIR. 2L72 4F4 FRTA16WE E00055EN 20041119000712004111900071NM 2004 11 19 USAA040701 120041006A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE BENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 SUPPORT, .2500 INCH X 20 INCH AREA, BENT/LIFTING METAL, BS540 BETWEEN IB AND OB SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E21EU 20041119000722004111900072NM 2004 11 19 USAA040702 120040910A554265C2584151 STRUCTURE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 RUDDER, 1 INCH LENGTH, WEAR WITH KNIFE EDGING, LOWER TR EDGE. SCALED DAMAGE IAW EA79025. 2L72 4F4 FRTA16WE E21EU 20041119000742004111900074NM 2004 11 19 USAA040753 120041015A5310 STRUCTURE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 CHORD, .750 INCH AREA, CORROSION, STATION 1360 TO 1450 RBL 22. REPLACED CHORD SECTION IAW EA 95871. 2L72 4F4 FRTA2NM E12EU 20041119000752004111900075NM 2004 11 19 USAA040790 120041002A5240 CHANNEL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FWD SERVICE DOORCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT,Q5, Z-CHANNEL, 4 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SERVICE DOOR Z-CHANNEL. REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20041119000782004111900078NM 2004 11 19 USAA040791 120040930A532065538443 FLOOR SUPPORT BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, ANGLE/TRACK, 2 INCH CORROSION, LEVEL 1; TASK NR C53-202-01 AFT CARGO CORE, FLOOR TIE DOWN TRACK, STA 859 LBL 17.20. SPLICED REPAIR SECTION INTO FLOOR TRACK IAW SRM 53-00-53. 2L72 4F4 FRTA16WE E2GL 20041119000792004111900079NM 2004 11 19 USAA040788 120040925A5310 KEELBEAM BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT Q5, KEEL BEAM, 2 INCHES X 40 INCHES AREA CORROSION; LEVEL 1 TASK NR C53-208-01, L KEEL BEAM STA 500D-540. REMOVED AND REPLACED, SPLICED IN NEW SECTION IAW TYP REP 53-60-09. 2L72 4F4 FRTA16WE E2GL 20041119000802004111900080NM 2004 11 19 USAA040776 120041024A5510 PIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU HINGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19448US38880 24892 PIT, C3, PIN ASSEMBLIES- 1INCH X 1INCH AREA, CORROSION; NO LEVEL OR TASK LT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IWA WA 79359/ DRAFT EO 5502V025. 2L72 4F4 FRTA16WE E21EU 20041119000812004111900081 2004 11 19 SDR2004080 420041004A3440959960714562 TRANSCEIVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE AVIONICS RACK ERRATIC A TRBAO OTHER N FALSE WARNING DEDESCENT 1 SO21408AT152 5123 408 DURING DESCENT THE GEAR POSITION INDICATOR LIGHTS, THE CREW ALERTING SYSTEM AND THE GPWS AMBER LIGHT CAME ON AND OFF THREE TIMES. REPLACED THE RADIO ALTIMETER TRANSCEIVER UNIT. 2H72 4T4 TRTA53EU E20NE 20041119000822004111900082SO 2004 11 19 1386100304 120041003A5210 INFLATION SYS GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU DOOR SEAL INOPERATIVE E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13486QS 1386 DURING DESCENT AT 5000 FT, DOOR SEAL DEFLATED AND 4 MINUTES LATER RE-INFLATED. THE MASKS DID NOT DROP. MAIN ENT DOOR SEAL INFLATION SYS, WATER IN SEAL INFLATION SYS. INSTALLED DOOR SEAL MODIFICATION AC SERV CHANGE KITS-ASC 424 AND 438B-COMBINED KITS INTRODUCE NEW TUBING, VENT LINES, CONDENSER INSTALLATION PN 1159SB48802-27(TUBE), 1159SB48800-1(DUCT), 1159SB40709-21(VENT PLUG), 1159SB48830-1/3(HOSE ASSY), REGULATOR 3215634-5 AND FILTER NP 31004- INTRODUCTION OF ASC ARE INTENDED TO EXTRACT EXCESS MOISTURE CONTENT IN SYS AND IMPROVEMENT OF MFG OF REGULATOR INCREASES FLOW AND IMPROVED FILTER INCREASES REMOVAL OF CONTAMINANTS. 2L72 4F4 FRTA12EA E25NE 20041119000832004111900083CE 2004 11 19 EHA2004F00004 120040714A323025800 SELECTOR VALVE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A60A 52043NE COCKPIT FLOOR INOPERATIVE E EHAAO OTHER O OTHER NRNOT REPORTED 1 AL03514RD BL5 LT MAIN GEAR FAILED TO RETRACT. FOUND NITROGEN EXTENSION VALVE OPEN. CLOSED NITROGEN EXTENSION VALVE. SERVICED SYSTEM PROCEDURE FOR (AFTER EMER EXTENSION). SYSTEM OPS CHECK NORMAL. REF MM8101 1L72 4T4 T A24CE E4EA 20041119000842004111900084NM 2004 11 19 USAA040780 120041022A5320 STIFFENER BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU38514 24996 PIT, FPBH INSP, STIFFENER TWO CRACKS, .5000 INCH X .7500 INCH LENGTH. STA 178 FPBH WL 218 UNDER HORIZON STIFFENER. DOUBLER INSTALLED IAW EO 5300V153, JOB CARD MK-42-93801. 2L72 4F4 FRTA16WE E21EU 20041119000852004111900085EU 2004 11 19 ASOA04819 120041004A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE RT SEAT TRACK BETWEEN FR39 AND FR40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT SEAT TRACK BETWEEN FR39 AND FR40 IAW SRM 51-25-04. 2H72 4T4 TRTA53EU E20NE 20041119000862004111900086EU 2004 11 19 ASOA04821 120041005A5320 BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE WING TO FARING BRACKET AT FR 23D AND BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE WING TO FARING BRACKET AT FR 23D AND BL0 IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041119000892004111900089NE 2004 11 19 GUU2004F00028 220040827A72003044800 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 2 FAILED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO174954315662 UE181 PCEPS0005 DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LT AT 500 FT, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUT DOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: SUSPECT NR 2 PT BLADE FAILURE. 2L72 4T4 TRTA24CE E26NE 20041119000902004111900090EA 2004 11 19 O2G2004F00004 120041008A3260 PROXIMITY SWITCH CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE RT MLG FAILED E O2GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE03601VH4778 5043 ON GEAR RETRACTION AFTER TO THE RT GEAR DOWN LIGHT REMAINED ON IN THE DOWN AND LOCK INDICATION. GEAR RETRACTED AND EXTENDED AS REPORTED BY TOWER. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTED RT LANDING GEAR AND FOUND TAPE AND PAINT ON GEAR UPLOCK PROXIMITY SWITCH. TAPE AND PAINT REMOVED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119000922004111900092NM 2004 11 19 USAA040782 120041023A5330 SKIN PANEL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, SKIN PANEL, REMOVED AND REPLACED SKIN PANEL AT BS 980 FROM S20R-S25R. REMOVED AND REPLACED SKIN PANEL DUE TO TEMPORARY REPAIRS; REPAIR TOO CLOSE TO LAP JOINTS; IAW EO 79060. 2L72 4F4 FRTA16WE E2GL 20041119001002004111900100NM 2004 11 19 USAA040764 120041020A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19374US 22953 CLT, RON, SKIN-1 INCH CRACK, BS 727E AT STRINGER 22R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. 2L72 4F4 FRTA16WE E2GL 20041119001042004111900104EU 2004 11 19 ASOA04788 120041009A3350M2275941249 WIRE AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BROKEN A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27630AS 149 336 DURING A GROUNG INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND ILLUMINATING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE TO THE PASSENGER DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20041119001062004111900106 2004 11 19 UIEA200400179 420041001A341046300181300413 INU BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE COCKPIT FAILED A UIEAO OTHER J WARNING INDICATION CLCLIMB 1 EA15808MC 21048 ON CLIMB OUT, NR 1 INS WARNING LIGHT CAME ON. ON CLIMB OUT NR 1 INS WARNING LIGHT CAME ON. NR 1 ADI AND HEADING FAILED. SELECTED NR 3 ATTITUDE AND COMPASS. APPROX 3 MINUTES LATER NR 3 INS WARNING LIGHT CAME ON. BOTH SCREENS WENT BLANK AND SHUT DOWN. REMOVED AND REPLACED NR 1 AND NR 3 INS NAVIGATION UNIT IAW MM 34-41-03/ 401 AND 501. OPS CHECK OK. 2L74 4F4 F A20WE E23EA 20041119001072004111900107WP 2004 11 19 COOSDR040020 120040823A5330 SKIN DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE TAIL SECTION CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 FUSELAGE TAIL SECTION, FROM Y STA 1530 TO Y STA 1633 BETWEEN LONGERON 24L AND LONGERON 32L UPPER AND LOWER FUSELAGE SKIN CORRODED. 2L74 4F4 F 4A25 1E8 20041119001082004111900108NM 2004 11 19 C7WA200400047 120040922A5310 SHEAR TIE BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 SHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11. MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES. 2L73 4F4 F A3WE E2EA 20041119001092004111900109NM 2004 11 19 USAA040793 120041023A5320 THRESHOLD BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT,Q5, THRESHOLD, 2 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01 AFT CARGO DOOR THRESHOLD S25R. INSTALLED THRESHOLD IAW DWG 65-47957. AFT CARGO DOOR THRESHOLD S25R. 2L72 4F4 FRTA16WE E2GL 20041119001142004111900114NM 2004 11 19 USAA040779 120041022A5312 STIFFENER BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU BULKHEAD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU38514 24996 PIT, FPBH INSP, STIFFNER 1 INCH CRACK IN LENGTH, STA 178 UNDER HORIZON STIFFNER WL 218 RT SIDE. DOUBLER INSTALLED IAW EO 5300V153, JOB CARD MK42-93801. 2L72 4F4 FRTA16WE E21EU 20041119001152004111900115NE 2004 11 19 GUU2004F00027 220040915A72003044700 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RIGHT FAILED A GUUAO OTHER O OTHER TXTAXI/GRND HDL 1 SO1769547 UE189 DURING AM ENGINE RUNUPS, RT ENGINE WENT INTO FEATHER AND WOULD NOT COME OUT. ALL OTHER PARAMETERS NORMAL. AFTER FURTHER INSPECTION, DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: SUSPECT NR 2 PT BLADE FAILURE. 2L72 4T4 TRTA24CE E26NE 20041119001162004111900116CE 2004 11 19 GUU2004F00030 120040922A55201016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178755416640 UE227 AT SCHEDULED ROUTINE MAINTENANE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20041119001172004111900117EA 2004 11 19 ASOA04784 120041007A3350BF10044004 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27859AS 7421 DURING C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY ABOUT THE SERVICE DOOR. 2L72 4F4 FRTA21EA E15NE 20041119001192004111900119NM 2004 11 19 USAA040697 120041004A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19587US51935 23932 SKIN, 1 INCH CRACK, STRINGER 24R, BETWEEN STA 727D AND 727E. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229. 2L72 4F4 FRTA16WE E21EU 20041119001202004111900120SW 2004 11 19 EHA2004F00003 120040713A2910212076190001 LINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA HYD SYSTEM CHAFED E EHAAO OTHER K FLUID LOSS NRNOT REPORTED 1 AL03398EH 30766 HYDRAULIC LEAK FROM AREA OF CARGO HOOK. TRACED TO TAIL ROTOR SAS LINK HYDRAULIC LINE CHAFED BY FUEL VENT LINE. REPLACED LINE, REROUTED AND SECURED FUEL VENT LINE. LEAK CHECKED AND MOC FLIGHT GOOD. (AL03200404250) 1G71 4U4 U H4SW E22EA 20041119001222004111900122EA 2004 11 19 A6WA200440156 120041016A4900 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL31450AW 7823 IN FLIGHT, STARTED APU, SMELLED JET FUEL, TURNED APU OFF- NO MESSAGES DISPLAYED. INSPECTED TAIL COMPARTMENT AND APU COMPARTMENT FOR LEAKAGE. FOUND NONE. RUNUP APU. OPS CHECK IAW MM 49-10-00. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119001252004111900125SO 2004 11 19 O2G2004F00006 120041014A7711 LINE GULSTMG1159 GIV 3980115SO RROYCESPEY SPEY5118 54523EU NR 2 ENGINE P3 LEAKING E O2GAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NE03624BP 1093 RT ENGINE WOULD NOT MAKE EPR OF THE DAY, RETORQUE P3 SPLITTER. PERFORMED ENGINE POWER RUN, OPS CK GOOD. 2L72 4F4 FRTA12EA E2EU 20041119001272004111900127 2004 11 19 SWAA043338 420041115A2565D31354 SLIDE BOEING737 7373Q8 1384670NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29688SW 23254 L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041119001332004111900133NM 2004 11 19 SWAA043346 120041115A531069353656 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE AT BS 360, BETWEEN STRINGERS 14L AND 15L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041119001342004111900134NM 2004 11 19 SWAA043347 120041115A53306545766 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 482 + 16, STRINGER 10L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041119001372004111900137 2004 11 19 SWAA043367 420041117A25656949956 CABLE BOEING737 7373Q8 1384670NM L2 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED SLIDE CABLE PER MM. 2L72 4F RTA16WE 20041119001382004111900138NM 2004 11 19 SWAA043368 120041117A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 540, STRINGER 16L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041119001392004111900139NM 2004 11 19 SWAA043369 120041117A2560P22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 DURING SCHEDULED C2 CHECK, FOUND FWD EPPLS PHOTOLUMINESCENT STRIPS WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM. 2L72 4F RTA16WE 20041119001412004111900141NM 2004 11 19 SWAA043371 120041117A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED FROM BS 727E TO BS 727D AND BETWEEN STRINGERS 5R AND 6R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20041119001422004111900142NM 2004 11 19 SWAA043372 120041117A3350BR2013 LIGHT BOEING737 7377H4 1384404NM ROW 1 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 DURING SCHEDULED RON, FOUND EEPLS AT ROW 1 ABC, INOP. RECONNECTED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041119001432004111900143NM 2004 11 19 SWAA043373 120041117A335007912 COVER BOEING737 7377H4 1384404NM ROW 1 ABC MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29796SW 27889 DURING SCHEDULED RON, FOUND EEPLS COVER AT ROW 1 ABC, MISSING. REMOVED AND REPLACED EPPLS COVER PER MM. 2L72 4F RTA16WE 20041119001462004111900146EA 2004 11 19 VNAA0410013 120041030A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE BIRD STRIKE A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05220PS 7887 AFTER LANDING AT CLT THE PILOT OF FLIGHT 2421 REPORTED A BIRD STRIKE BELOW THE CAPTAIN'S WINDSHIELD. A BIRD STRIKE INSPECTION WAS PERFORMED AND TWO DENTS WERE FOUND ON THE FORWARD FUSELAGE AT FS 589 & FS 202. THE AIRCRAFT WAS FERRIED TO CAK WHERE PSA MAINTENANCE PERFORMED TEMPORARY REPAIRS IAW BOMBARDIER REO 601R-53-61-1193 AND REO 601R-53-11-828. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119001502004111900150NE 2004 11 19 VNAA0411001 220041107A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RIGHT MALFUNCTIONED A VNAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL05705PS 10144 GEE965516 ON TAKEOFF ROLL THE RT ENGINE FAILED TO MAKE RATED POWER AND THE CREW OF FLIGHT 2219 ABORTED THE TAKEOFF AND RETURNED TO THE GATE. TARGET POWER WAS 89.1 PERCENT, THE ENGINE SPOOLED TO 80.2 PERCENT. PSA MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND PERFORMED A POWER ASSURANCE CHECK OF THE RT ENGINE IAW THE CRJ700 POWERPLANT GROUND RUN MANUAL. NO DEFECTS WERE NOTED AND ALL ENGINE PARAMETERS WERE NORMAL. THE AIRCRAFT WAS THEN RELEASE FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041122000012004112200001EA 2004 11 22 QXEA200400746 120041108A5730 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 PDX - RIGHT HAND WING UPPER SURFACE TRAILING EDGE APPEARS CRACKED, RIGHT HAND INBOARD END OF INBOARD MULTIFUNCTION SPOILER. REPAIRED IAW CRJ 700 MM 29-10-00-870-801-A01, SRM 51-42-06 AND SRM 51-41-21. 2L72 4F RTA21EA 20041122000022004112200002EA 2004 11 22 QXEA200400747 120041103A5315 FLOORBEAM CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09604QX 10019 PDX - FLOOR SUPPORT BEAM AT X280 IS CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDES OF COCKPIT ENTRANCE. REPAIRED IAW REO 670-51-11-045. 2L72 4F RTA21EA 20041122000032004112200003NM 2004 11 22 QXEA200400752 120041028A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - RIGHT HAND FORWARD FUSELAGE FORWARD BAGGAGE DOOR INTERNAL CUT OUT SURROUND STRUCTURE, LOWER SILL INNER PLATE SEVERAL AREAS OF SURFACE CORROSION ON TOP SURFACE OF PLATE FS X1.00 TO X32.40 WL 100.032. 2H72 4T RTA13NM 20041122000042004112200004NM 2004 11 22 QXEA200400753 120041026A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FUSELAGE INT AFT, X704 TO X747, RIGHT HAND Y9.290, INBOARD EQUIPMENT SEAT RAIL IS CORRODED ON UPPER SURFACE AND INSIDE CLAW PORTION FROM X704 TO X747. REPAIRED IAW HORIZON AIR EA 6-53-437 AND RD 8/4-53-1021. 2H72 4T RTA13NM 20041122000062004112200006NM 2004 11 22 QXEA200400758 120041030A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - RIGHT HAND INBOARD FLAP YW STATION 60.90, THE UPPER FLAP SURFACE HAS A 1 INCH DIAMETER FOULING MARK INTO THE METAL FROM CHAFING WITH THE UPPER SHROUD. REPAIRED IAW HORIZON AIR EA 6-57-245 AND RD 8/4-57-375, STEPS 3-6. 2H72 4T RTA13NM 20041122000072004112200007NM 2004 11 22 QXEA200400773 120041113A5710 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - FUEL PANEL 522AT HAS ALL COUNTERSINK THAT HAVE PITTING CORROSION. REPLACED IAW WORK CARD 500ME2860266. 2H72 4T RTA13NM 20041122000082004112200008NM 2004 11 22 QXEA200400764 120041027A5753 FLAP TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 600 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - EXTERIOR PLATING DAMAGED ON THE RIGHT HAND NR 4 FLAP TRACK INBOARD SIDE ALONG THE SIDE ROLLER PATH. REPAIRED IAW HORIZON AIR EA 6-57-246 AND RD 8/4-57-379. 2H72 4T RTA13NM 20041122000102004112200010NM 2004 11 22 HNAA0400131 120041112A243050309008 BUSS BAR DHAV DHC8 DHC8102 2809003NM NR 1 GENERATOR FAULTY A HNAAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 EA07807EX21037953 292 FLIGHT 3798 BWI TO LGA HAD TO DIVERT TO PHL DUE TO THE NR 1 DC GEN FAILING AND THEN THE NR 2 DC GEN FAILING. AIRCRAFT BRIEFLY ON BATTERY POWER. NAVS, PRESSURIZATION, AND ANTI-ICE SYSTEMS WERE LOST. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED ALL ENGINE CONNECTORS AND WING ROOT CONNECTORS. THE BUSS BAR PROTECTION UNIT WAS REPLACED. AIRCRAFT WAS GROUND RUN, ALL SYSTEMS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041117002042004111700204NM 2004 11 17 AALA20041124 120041111A3397 WIRE BOEING767 767223 1385123NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21335A 22333 LAX - EMERGENCY LIGHT IN FIRST CLASS GALLEY AISLE ON LEFT HAND SIDE INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY LIGHT IN FIRST CLASS GALLEY AISLE ON LEFT HAND. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041117002112004111700211EU 2004 11 17 MALA040637 120040909A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON SEAT TRACK BL 0 STA 294-310. REPAIRED IAW EO S53079. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041117002122004111700212NM 2004 11 17 04FDEA03105 120041111A323065404675 ACTUATOR BOEING727 727233 138408ANM NLG DOWNLOCK MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25222FE 20933 NOSE GEAR WOULD NOT EXTEND DURING APPROACH. RED NOSE LIGHT ILLUMINATED. UPON LEVEL OFF IE UNLOADING, THE A/C NOSE GEAR EXTENDED, NORMAL LANDING. REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK ACT, IAW B727-200MM 32-33-011-4, ACFT STILL REQUIRES JACKING FOR OPS CK AND RII. JACKED ACFT AND PERFORMED RETRACTION TEST PER MM32-33-000-5. NO DEFECTS FOUND. NO LEAKS FOUND. OK FOR SERVICE. 2L73 4F RTA3WE 20041118000062004111800006NM 2004 11 18 04FDEA03106 120041115A5311 FRAME BOEING727 72722 1384002NM FUSLEAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 AFT CARGO FRAME DENTED AT BS 970, STR 26R. 2L73 4F A3WE 20041118000122004111800012NM 2004 11 18 04FDEA03091 120041112A5713ARB751111 STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BOOSTER PROGRAM, RT WING STRINGER 11 END FOUND WITH APPROXIMATELY 11.5 INCH CRACK AS VIEWED FROM ACCESS PANEL NR 636AB. ARB751-1. REMOVED PER SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20041118000212004111800021NM 2004 11 18 04FDEA03110 120041115A3411ACP803017 PLATE DOUG MD11 MD11F 3023600NM ZONE 100 MISSING A FDEAK NONE ISPFLT. ATTITUDE INST. AFFECT SYSTEMS NO WARNING INDICATION ININSP/MAINT 1 SO25582FE 48420 BOTH LT AND RT PRIMARY STATIC PORTS ARE MISSING THEIR RUB PLATES. REF: MD11 IPC CHAPTER 34-11-60-01, ITEM 322. DISCREPANCY FOUND DURING "C" CHECK MAINTENANCE. (OPEN) 2L73 4F RTA22WE 20041118000252004111800025EU 2004 11 18 AWXA200400936 120040827A2121 BEARING TECHNOFAN AIRBUS320 A320231 3930325EU ZONE 128 FAILED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28625AW 675 064 EN ROUTE FROM PHX TO MCO, SMELLED A BURNING ELECTRICAL ODOR WITH VISIBLE SMOKE IN COCKPIT, WHILE DIVERTING TO DFW APPROXIMATELY 2 MILES LATER VENT EXTRACT FAULT LIGHT ILLUMINATED. MAINTENANCE PLACED SYSTEM ON MEL AND DEACTIVATED EXTRACT FAN. UPON ARRIVAL AT FIRST MAINTENANCE STATION, REPLACED AVIONICS COOLING (EXTRACT) FAN IAW AMM 21-26-51-04, OPERATIONAL CHECK WAS GOOD. SUPP - VENDOR CONFIRMED FAILURE OF AVIONICS COOLING FAN S/N 675, UNIT SEIZED, COULD NOT PERFORM INCOMING FUNCTIONAL CHECK. FOUND THE FRONT BEARING BROKEN, REAR BEARING LOOSE AND WORN, AND FRONT FLANGE CENTER HOLE WORN. REPLACED DEFECTIVE PARTS AND PERFORMED FUNCTIONAL TEST IAW CMM 21-26-42, REV 6. 2L72 4F RTA28NM 20041118000312004111800031NM 2004 11 18 04FDEA02737 120040919A5512ALC81041 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 19 LT BARREL NUT BORE EXCEEDED LIMITS. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 19L. REPAIRED AS PER EA NR 1-5510-80357, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 19L, REWORK BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20041118000372004111800037NM 2004 11 18 04FDEA01739 120040615A5744ARC0154 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORRODED. RT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS=0.493 INCH, REMAINING THICKNESS=0.442 INCH, MATERIAL REMOVED=0.051 INCH. REPAIR CARRIED OUT AS PER FEDEX EA 1-5740-76744, TITLE: WINGS, LEFT AND RIGHT INBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041118000392004111800039NM 2004 11 18 04FDEA02740 120040919A5512ALC81041 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON NR 23 LT BARREL NUT BORE FOUND EXCEEDED LIMITS PER EO 1-5510-7-5000-C3-PT1 FIGURE 03. LEFT HAND HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 23L. REPAIRED AS PER EA NR 1-5510-81551, TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 23L. REWORKED BEYOND S/B MD11-55-023 REVD 2 LIMITS. 2L73 4F RTA22WE 20041118000432004111800043WP 2004 11 18 04FDEA02824 120040927A5730ARC0264507 PANEL DOUG DC10 DC1010F 3022111WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77620, REFERENCE NON ROUTINE N00125. 2L73 4F A22WE 20041118000452004111800045NM 2004 11 18 2004UALA01007 120041030A2530 RECEPTACLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY BURNED A UALAO OTHER A FLAME/FIRE NRNOT REPORTED 1 WP29174UA 24381 FLAME CAME OUT OF SERVICE OUTLET AFTER SWITCHING TO EXTERNAL POWER BY DOOR 1L. ELECTRICAL OUTLET AT DOOR 1 LEFT WAS FOUND MELTED. OUTLET WAS REPLACED AND OP CHECKED GOOD. ENGINEERING WILL EVALUATE THE ELECTRICAL OUTLET TO LOOK FOR POSSIBLE DEFECTS. ENGINEERING ALSO CREATED CALLOUT EG3435 TO CHECK DOOR 1 LEFT SERVICE OUTLET WIRING TO LOOK FOR ANY POSSIBLE CAUSES. 2L74 4F4 FRTA20WE E24NE 20041118000492004111800049NM 2004 11 18 04FDEA02768 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORRODED. RT WING, OUTBOARD FLAP, INBOARD AFT HINGE ACTUATOR ROD END HOLE, INBOARD ATTACHMENT CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.189 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118000522004111800052WP 2004 11 18 04FDEA02831 120040927A5310AFA73955 LINER DOUG DC10 DC1010F 3022111WP ZONE 100 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 AFT PIT DOOR JAMB AFT SIDE THRESHOLD PANEL HAS HOLE PUNCTURES ON IT. WELD REPAIRED IAW FEDEX EA 8-5320-77632, REFERENCE NON-ROUTINE. 2L73 4F A22WE 20041118000592004111800059EU 2004 11 18 04FDEA02875 120041005A5310 FITTING AIRBUS310 A310222 3930315EU FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25418FE 343 MOD TYPE H MOD NR C-CHECK REV NO, PS ACCOMPLISH MAINTENANCE C-CHECK NR 004. DURING C-CHECK WHILE ACCOMPLISHING EO 6-5710-7-3322 FOUND CRACK AT FWD FITTING FRAME 47, HOLE NR 41. ITEM WAS REPAIRED ON N00606 PER FEDEX EA 6-5710-77088. 2L72 4F RTA35EU 20041118000702004111800070WP 2004 11 18 04FDEA02829 120040927A5730ARC2906503 PANEL DOUG DC10 DC1010F 3022111WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 541CR HAS MANY AREA OF DELAMINATION. REPAIRED PANEL 541CR BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2906 AND FEDEX EA 8-5710-77618. REFERENCE NON-ROUTINE N00163. 2L73 4F A22WE 20041118000722004111800072 2004 11 18 04FDEA02921 420041012A3160 DISPLAY AIRBUS310 A310203 3930313EU COCKPIT INTERMITTENT A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25431FE 316 ON TAKEOFF ROLL BOTH SGU`S WENT BLANK AT APPROX 85 KNOTS, THEN REAPPEARED AT 105-110 KNOTS THEY WENT BLANK AGAIN EXCEPT FOR SYSTEM DATA NOT AVAILABLE CAUTION ON EACH DISPLAY, SGU'S HAD BEEN RESET ON PRE FLIGHT DUE TO SAME PROBLEM T/O AT 110KNOTS WITH NO ADDITIONAL PROBLEMS. REPLACED SDAC IAW A310 AMM CH 31-55-22-4. OPS CKS GOOD. 2L72 4F RTA35EU 20041118000842004111800084NM 2004 11 18 AWXA200401021 120040905A52106523464 SNUBBER BOEING737 7373G7 1384595NM L-2 DOOR WEAK A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK, THE L-2 DOOR SNUBBER FAILED STEP 4.1 OF T/C I1A52002 FOR WEAK OPERATION. MAINTENANCE REMOVED AND REPLACED L-2 DOOR SNUBBER IAW BMM 52-11-71-4, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041118000862004111800086WP 2004 11 18 04FDEA02896 120041008A5330ADA3139501 DOUBLER DOUG DC10 DC1010 3022110WP FUSELAGE MISINSTALLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25389FE 46623 DURING B SERVICE AT LAX AND RVSM UPGRADE, FOUND PREVIOUS SRM REPAIR INFRINGING UPON RT NORMAL STATIC PORT CONTROLLED AREA. SELECTED REPAIR IS NOT APPLICABLE TO SPEIFIC AREA PER EA 8-5320-77995. REPAIR WAS REMOVED AND APPROPRIATE REPAIR INSTALLED PER SRM 53-20-00, PAGE 93, SHT1, FIG 9. ALSO EA NR 8-5320-77995 IS C/W. ALSO, CHECK N/R #'S 6, 36, 37, 41 AND 42. 2L73 4F A22WE 20041118000912004111800091EU 2004 11 18 AWXA200401034 120040918A2910AE84760Z SWIVEL AIRBUS320 A320231 3930325EU GREEN HYD SYS BROKEN A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP28637AW 099 ON LANDING AT CMH EN ROUTE FROM LAS, WHEN LANDING GEAR EXTENDED LOST GREEN HYDRAULIC FLUID, MANUALLY EXTENDED GEAR, LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE RT MAIN LANDING GEAR DOOR ACTUATING CYLINDER FORWARD FLEX HOSE SWIVEL JOINT ASSEMBLY BROKEN OFF, REPLACED ACTUATING CYLINDER SWIVEL AND FLEX HOSE IAW AMM 32-31-35-04, LEAK CHECK GOOD. 2L72 4F RTA28NM 20041118000992004111800099EU 2004 11 18 AWXA200401053 120040910A5315D53472188200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 RT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041118001012004111800101EU 2004 11 18 AWXA200401055 120040915A5321D5367320200000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28656AW 1079 DURING BC-4 CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF DISBONDED. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED NEW FLOOR PANEL 131EF IAW A320 SRM 53-02-00, FIG 206. 2L72 4F RTA28NM 20041118001042004111800104NM 2004 11 18 04FDEA02763 120040920A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, INBOARD HINGE INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.096 INCH AND REPAIRED AS PER EA NR 1-5750-79749, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041118001122004111800112WP 2004 11 18 04FDEA02594 120040901A5753ARC2512 HINGE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25399FE 48262 WINGS, RT INBD FLAP AFT HINGE ASSY ARC2512,PIVOT BORE CORROSION. COMPLIED WITH E.A.8-5750-80602. 2L73 4F RTA22WE 20041118001212004111800121NM 2004 11 18 AWXA200401072 120040921A5315D53472188204 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28810AW 1116 DURING BC-4 CHECK, EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT AT FS 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FS 68 TO FS 69; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20041118001302004111800130NM 2004 11 18 04FDEA02556 120040824A5712ARB2850505 RIB DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK AREA AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041118001372004111800137WP 2004 11 18 04FDEA03050 120041108A5310 DOOR FRAME DOUG DC10 DC1030F 3023504WP FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 FUSELAGE CORROSION/GOUGES ON MAIN CARGO DOOR FRAME. COMPLIED WITH EA 8-5310-82067. FUSELAGE CORROSION GOUGES ON MAIN CARGO DOOR FRAME. 2L73 4F RTA22WE 20041118001402004111800140NM 2004 11 18 AWXA200401178 120041031A5270350E5151331 CONCENTRATOR AIRBUSA319 A319132 3930340NM ZONE 120 MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28809AW35192488 1111 ON CLIMB OUT, RECEIVED R-2 DOOR WARNING (OPEN) IND AT 7,000 FT, 12,000 FT, & 17,000 FT RESPECTIVELY, F/A REPORTED HEARING LEAK, TURNED BACK & LANDED WITHOUT FURTHER EVENT. MX INSP R-2 DOOR & FOUND IT SECURE WITH ALL SEALS IN PLACE, ISSUED MEL COND 1 "R-2 DOOR WARNING INDICATION INOP". MX TROUBLESHOT PER TSM & REPLACED SDAC IAW AMM, PRESSURIZED A/C, NO LEAKS NOTED. VENDORS INCOMING TEST OF SDAC S/N 1174 CONFIRMED REASON FOR REMOVAL, SYNCHRO INPUT TEST FAILED DUE TO DEFECTIVE INPUT 2 BOARD. REPLACED DEFECTIVE INPUT 2 BOARD AND PERFORMED FUNCTIONAL TEST IAW CMM 31-55-34, REV. 9. 2L72 4F RTA28NM 20041118001522004111800152NM 2004 11 18 04FDEA01971 120040706A2997D23396 WIRE DOUG MD11 MD11F 3023600NM ZONE 200 BURNED A FDEAF ACTIVATE FIRE EXT. A FLAME/FIRE NRNOT REPORTED 1 SO25587FE 48489 MAIN DECK CABIN AT STA 775 (RT) WIRE NR`S. C029-1-6AL, C029-2-6AL AND C029-3-6AL FND BURNT. GVI ON THE BURNT WIRES SURROUNDING AREAS,CONDUCTIVITY INSP PER DAC NDT SPM PART 06-10-01-001 REV11 ON M/D STA 775R FRAME/SKIN FND ACCEPTABLE RANGE. BURNT CABLES, REPAIRED USING COPALUM SPLICE PER BOEING SWPM20-30-13, CONDUCTIVITY/INSULATION. RESISTANCE CHECK PER SWPM29-21-01 SATIS. AIRPLANE POWER ASSURANCE CHECK/PHASE IMBALANCE TEST CARRIED OUT ON BOTH AUX HYD PUMP SATIS PER AMM29-21-01, SUBSEQUENT OPS CHK CARRIED OUT ON BOTH AUX HYD PUMPS. ALSO, FOUND SATIS PER AMM29-21-01-700-801. FEDEX EA 1-2920-79801 'HYD POWER-AUXILIARY HYD PUMP WIRING, SPLICE REPAIR COMPLIED WITH. 2L73 4F RTA22WE 20041118001552004111800155WP 2004 11 18 04FDEA03017 120041104A78309055M59G07 DUCT DOUG DC10 DC1010 3022110WP ZONE 400 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 NR3 ENGINE PNEUMATIC DRIVE MOTOR PNEUMATIC SUPPLY DUCT ADEL CLAMP MOUNT TAB BROKEN OFF. REMOVED, WELD REPAIRED AND REINSTALLED NR 3 ENGINE PNEUMATIC DRIVE MOTOR SUPPLY DUCT IAW DC10 MM 36-14-02-4 AND FEDEX EA 8-7830-81506. REFERENCE NON-ROUTINE N01094. 2L73 4F A22WE 20041118001802004111800180NM 2004 11 18 04FDEA02894 120041008A5713ARB75101 STRINGER DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 RIGHT HAND WING UPPER STRINGER END (S10) FOUND CRACK INSIDE FUEL TANK ACCESS PANEL 638AB. RIGHT HAND WING UPPER STRINGER END (S10) TRIMMED OUT CRACKED AREA AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED REPAIRED ANGLES AS PER SRM 51-33-01 AND SRM 57-20-00 FIG 10 VOL I. 2L73 4F RTA22WE 20041118001812004111800181NE 2004 11 18 04FDEA03018 220041102A7297 CONNECTOR DOUG MD11 MD11F 3023600NM GE CF6 CF66D1A 30020NE NR 1 ENGINE LOOSE A FDEAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO25394FE655461 46628 451454 AFTER SETTING MAX PWR AND ABOVE 90 KTS T/O ROLL RECEIVED ENG FAIL LIGHT, NR 1 ENG ROLLED BACK. REJECTED T/O. FOUND FIREWALL CONNECTOR NR P1-8002 NOT PROPERLY SECURED ON THE NR 1 PYLON. INSPECTED PLUG, NO DEFECTS NOTED. SECURED CONNECTOR. OPERATED ENGINE NR 1 TO TAKEOFF TARGET N1 ENGINE CHK GOOD. CHECKED CDP FOR CRACKS AND LEAKS, NONE FOUND. ENG'S READINGS WAS DOWNLOADED FROM FLT DATA RECORDER. ADJ PART POWER TRIM ON MEC FOR NR 2 ENG, DUE TO IT BEING HIGH. MAX POWER ASSURANCE WAS PERFORMED ON NR 1 AND NR 2 ENG. READINGS NORMAL. OK TO CONTINUE. REMOVED AND REPLACED NR 1 ENG FUEL FILTER . NO CONTAMINATES NOTED. RAN ENG, NO LEAKS NOTED. HIGH SPEED TAXI PERFORMED BY FLT CREW. ALL PARAMETERS WERE G2L73 4F4 FRTA22WE E23EA 20041118001822004111800182WP 2004 11 18 P9RA20040022 120040620A272059140665573 POWERPACK DOUG DC9 DC982 3022082WP RUDDER MALFUNCTIONED A P9RAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO11698264924023773 49486 DECENT INTO IAH, AT 10,000 FEET, 250 KNOTS, LOUD RUMBLE OCCURED WITH SPEED BRAKE STOWED ACCOMPANIED BY SHARP ROLL RIGHT. EMERGENCY DECLARED. LANDED IN IAH UNEVENTFUL. REMOVED AND REPLACED RUDDER POWER PACK IAW MM 272008. OPS CHECKED GOOD. 2L72 4F A6WE 20041119000072004111900007 2004 11 19 A6WA200440149 420041013A3414 INDICATOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AIRSPEED CONTAMINATED A A6WAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 GL31423AW 7636 ON TAKEOFF ROLL THROUGH 80 KNOTS, STANDBY AIRSPEED INDICATION REMAINED AT 0 KNOTS. INSPECTED STANDBY SYSTEM AND FOUND WATER TO BE IN SYSTEM. PURGED WATER FROM SYSTEM AND PERFORMED LEAK CHECK IAW MM 34-11-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041119000132004111900013EA 2004 11 19 ASOA04835 120041025A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 IAW EO600-57-039A. 2L72 4F4 FRTA21EA E15NE 20041119000252004111900025NM 2004 11 19 N129QS0401 120040816A324069382354 ROD BOEING737 7377BC 1384509NM RT BRAKE PEDAL DISCONNECTED E BJ6AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NE03129QS 30329 DURING TAXI, CAPTAIN REPORTED HIS RT BRAKE PEDAL INOPERATIVE. PEDAL REPORTED AS (HARD). AC RETURNED TO BLOCKS, MECHANIC FOUND CAPTAINS RT BRAKE PEDAL INTERCONNECT TO CO-PILOTS PEDAL DISCONNECTED. HARDWARE FOR THE INTERCONNECT ROD WAS FOUND IN A PARTS BAG ATTACHED TO THE ROD. FOLLOW-UP INVESTIGATION FOUND THAT THE AC HAD JUST LEFT MAINTENANCE. A CONTRACT MECHANIC FAILED TO RECONNECT THE ROD AFTER MAINTENANCE. THIS OVERSIGHT WAS COMPOUNDED BECAUSE THE MECHANIC FAILED TO FOLLOW THE MM, DISCONNECTING ROD ON THE WRONG END. INSPECTOR OF THAT WORK ONLY INSPECTED THE ROD END THAT SHOULD HAVE BEEN DISCONNECTED DURING MAINTENANCE. 2L72 4F RTA16WE 20041119000482004111900048NM 2004 11 19 GAIA04108 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND EE COMPARTMENT, BS 400, STR 25R FRAME ANGLE HAS CUT. REF FASI NR 86452, REPAIRED EE COMPARTMENT FRAME ANGLE IAW SRM 53-10-4, FIG 11. 2L73 4F4 F A3WE E2EA 20041119000942004111900094NM 2004 11 19 BJNA041001 120041005A33506013211 BATTERY PACK BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 LT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2EA 20041119000962004111900096NM 2004 11 19 AMTA200401322 120041025A26100205K0S600 SWITCH BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT ENGINE OUT OF LIMITS A AMTAO OTHER J WARNING INDICATION APAPPROACH 1 GL11517AT 27973 (R TURB OH DET 2) STATUS MSG CAME ON MOMENTARLY, JUST PRIOR TO LANDING. PERFORMED FIM 26-13-00, FIG 103 AND 104, NO DEFECTS NOTED. IAW FIM 26-13-00, FIG 103, BLOCK 49, SWITCH OUT OF LIMITS AT 97.4 OHMS. REMOVED AND REPLACED SWITCH IAW AMM26-13-01-4. OPS TEST GOOD. 2L72 4F4 FRTA2NM E12EU 20041119000982004111900098NM 2004 11 19 USAA040774 120041015A5310 BEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US38961 24863 PIT, FPBH INSP, VERTICAL CORD-.750 INCH LONG CRACK. IB RADIUS OB VERTICAL CORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA79303. 2L72 4F4 FRTA16WE E21EU 20041119001022004111900102NM 2004 11 19 USAA040796 120040905A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, FLOOR SUPPORT 1 INCH 10 INCH AREA. CORROSION; LEVEL 1; TASK NR C53-107-02 LOCATED AT STA 986.5 TO 1016, RBL 3.54 TO RBL 18.25. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041119001032004111900103EA 2004 11 19 ASOA04781 120041007A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27859AS 7421 DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105. 2L72 4F4 FRTA21EA E15NE 20041119001112004111900111SO 2004 11 19 1392100204 120041002A26136006508 SENSOR GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU BRAKE TEMP FAILED E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13492QS 1392 BRAKE OVERHEAT (AMBER) MASTER CAUTION LIGHT CAME ON. BRAKE PAGE CONFIRMED A LT WHEEL (RT SIDE BRAKE) OVERHEAT WILL TEMP ABOVE 800 DEG. THEN, THE INDICATION WENT TO 252 DEG FOR THAT SAME BRAKE AND THE TEMP OVERHEAT AMBER LIGHT WENT OUT. THE TEMP LATER STARTED TO CLIMB SLOWLY. AT 285 DEG, THE TEMP SPIKED TO ABOVE 800 DEG WITH THE BRAKE OVERHEAT LIGHT COMING ON AGAIN. DURING DECENT FOR PRECAUTIONARY LANDING THE TEMP DROPPED BACK TO 285 DEG, (NOT LONG AFTER RE-SPIKING) JUST PRIOR TO TOUCHDOWN, THE BRAKE TEMP WENT TO NORMAL AT 31 DEG AND STAYED THERE UNTIL SHUTDOWN. FOUND BRAKE TEMP SENSOR FAILED, REMOVED AND REPLACED. OPS CHECKED GOOD. MX IAW GIV CMPCODE 324297. 2L72 4F4 FRTA12EA E25NE 20041119001122004111900112EA 2004 11 19 A6WA200440136 120040916A2930 LINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HYD QTY IND CHAFED A A6WAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31422AW 7341 NR 1 HYDRAULIC QUANTITY INDICATOR 35 PERCENT AT FL310 WITH NORMAL PRESSURE (3000 PSI). FOUND NR 1 EAP SUCTION LINE CHAFED THROUGH. NO DAMAGE TO PRESSURE LINE. REPAIRED LINE IAW AMM 20-22-00. LEAK AND OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041119001182004111900118NM 2004 11 19 USAA040671 120040928A5754 SUPPORT ANGLE BOEING767 7672B7 1385107NM GE CF6 CF680C2B2 30025NE NR 7 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655US 25257 CRACK IN NR 7 SLAT SUPPORT ANGLE. NR 7 SLAT LOWER T/E, 54 INCHES FROM OB END. REPLACED WITH FABRICATED ANGLE IAW SRM 51-40-02. 2L72 4F4 FRTA1NM E13NE 20041119001262004111900126NM 2004 11 19 GAIA04142 120040910A7160 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 2 ENG INLET CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NR 2 ENGINE INLET INTERIOR RT SIDE STA 1183 CRACKED. REF FASI NR 86722 CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR IAW SRM 54-10-3, FIG 9. 2L73 4F4 F A3WE E2EA 20041119001282004111900128 2004 11 19 SWAA043357 420041116A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041119001302004111900130NM 2004 11 19 SWAA043343 120041115A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29744SW 29490 DURING SPV, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041119001352004111900135NM 2004 11 19 SWAA043348 120041115A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 790, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041119001362004111900136NM 2004 11 19 SWAA043366 120041117A323365448105 ACTUATOR BOEING737 7373H4 1384600NM RT MLG FAULTY A SWAAO OTHER J WARNING INDICATION APAPPROACH 1 SW29372SW 26599 DECLARED EMERGENCY, WHEN LOWERING LANDING GEAR, RT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR, STILL UNSAFE. MANUAL GEAR EXTENSION OK. REMOVED AND REPLACED RT MLG DOWNLOCK ACTUATOR PER MM. 2L72 4F RTA16WE 20041119001442004111900144NM 2004 11 19 SWAA043374 120041117A52106545800 SKIN BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FUSELAGE SKIN AT LOWER HINGE CUTOUT, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041119001482004111900148EA 2004 11 19 VNAA0410010 120041020A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO DOOR FALSE ACTIVATIONA VNAAO OTHER N FALSE WARNING CLCLIMB 1 GL05229PS 7898 DURING CLIMBOUT THE CREW REPORTED A CARGO DOOR CAS MESSAGE WITH NO CHANGE IN CABIN PRESSURE. THE CAS MESSAGE WENT OUT AT 11,000 FEET. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C. 2L72 4F4 FRTA21EA E15NE 20041122000112004112200011EA 2004 11 22 04321626 120041116A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN ODOR A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27626BR 7225 EVENT SUMMARY STATES THAT 1888 IAD-CRW ON 626BR HAS DECLARED AN EMERGENCY AND RETURNED TO THE FIELD FOR MX. SMOKE IN THE CABIN. REMOVED AND REPLACED BOTH WATER SEPARATER COALESCER BAGS REF 21-51-13. PERFORMED GROUND RUNS. NO FURTHER DEFECTS NOTED REF 21-51-00. 2L72 4F RTA21EA 20041122000132004112200013EA 2004 11 22 04311684 120041106A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27684BR 7708 EVENT SUMMARY STATED THRUST REVERSER UNLOCK MESSAGE IN FLIGHT. OPENED DM 3114105-1 MEL 78-30-01 CAT B. RIGHT THRUST REVERSER UNLOCK MESSAGE ON ROTATION, (M) PROCEDURES C/W, ITEM PLACARD AND TRANSFERRED TO SUMMARY OF DEF ITEMS. REMOVED AND REINSTALLED RT ENGINE COWLS REF AMM 71-10-00. 2L72 4F RTA21EA 20041122000142004112200014NE 2004 11 22 04317679 220041112A7532 BLEED VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE MALFUNCTIONED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27679BR 7662 EVENT SUMMARY STATED BLEED MISCONFIG, ABORTED TAKEOFF, RTG. REMOVED AND REPLACED LT ENG 10TH STAGE BLEED VALVE IAW MM 36-11-04. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041122000152004112200015EA 2004 11 22 04310683 120041104A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27683BR 7692 FAINT ODOR OF BURNING RUBBER, RTF. APU BLEED CAUSING ODOR IN COCKPIT. INSPECTED APU & ACM. PERFORMED OPERATIONAL CHECKS OF APU AND APU FLOWS / ACMS REF AMM 21-51-00 & 49-10-00, OPS CHECKS GOOD. NO RUBBER ODOR NOTED. ALLOWED APU & ACMS TO OPERATE FOR OVER 2 HOURS AND AT DIFFERENT TEMPERATURE SETTINGS. COULD NOT DUPLICATE DISCREPANCY. RELEASED A/C FOR SERVICE. 2L72 4F RTA21EA 20041122000162004112200016EA 2004 11 22 04319639 120041114A5200 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE OPEN A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27639BR 7313 EVENT SUMMARY STATED THAT MX ACCESS PANEL DOOR OPEN. INSPECTED PANEL AND DEFECTS FOUND TO DOOR OR AIRFRAME. OK TO CONTINUE SERVICE. 2L72 4F RTA21EA 20041122000192004112200019NM 2004 11 22 SWAA043341 120041017A3397D10750 PIN BOEING737 7377H4 1384404NM CONNECTOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SPV, FOUND FWD CENTER CEILING EMERGENCY EXIT LIGHT INOP. RESEATED PIN 13 ON CONNECTOR D10750 PER MM. 2L72 4F RTA16WE 20041122000202004112200020NM 2004 11 22 SWAA043358 120041116A53306545866 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED C1 CHECK, FOUND 2 EACH SKIN CRACKS AT LOWER KEEL BEAM BETWEEN BS 660 AND BS 724, AND BETWEEN RBL 6.30 AND LBL 6.30. REPAIRED KEEL BEAM SKIN SECTIONS PER EA. 2L72 4F RTA16WE 20041122000212004112200021NM 2004 11 22 SWAA043359 120041116A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 5R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041122000222004112200022EA 2004 11 22 04311677 120041106A7797 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA RT ENG N1 DAMAGED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27677BR 7652 EVENT SUMMARY STATED THAT RIGHT ENG N1 DROPPED ON T/O ROLL. REMOVED AND REPLACED RIGHT ALTERNATOR IN REF TO SPEC PROC 10 GE MM 72-00-00. REMOVED AND REPLACED RIGHT ENGINE BLUE HARNESS IN REF TO CRJ MM 77-11-03. 2L72 4F RTA21EA 20041122000232004112200023NM 2004 11 22 UPS04443501 120041030A5730 SKIN BOEING747 747200 1384847NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, RT WING - CRACK FOUND ON RT WING UPPER SKIN AT BS 1241 UPPER SPLICE PLATE AREA AT HOLE NR 11 BY APPROX 0.040 INCH LONG RUNNING FWD. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK PROCESS CARD UW653051. 2L74 4F RTA20WE 20041122000242004112200024NM 2004 11 22 UPS04443502 120041101A5740 FITTING BOEING747 747200 1384847NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, RT BS 1241 WING REAR SPAR UPPER SPLICE PLATE AREA HOLE NR 5 FOUND CORROSION APPROX 0.040 INCH AT UPPER SPLICE FITTING. HOLE CRACKS REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER SOPM 20-50-03 AND WORK PROCESS CARD UW656931. 2L74 4F RTA20WE 20041122000262004112200026NM 2004 11 22 SWAA043342 120041115A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29736SA 27868 DURING SPV, FOUND AFT FUSELAGE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM. 2L72 4F RTA16WE 20041122000272004112200027EA 2004 11 22 04311672 120041107A2410 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 GENERATOR FAILED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27672BR 7594 EVENT SUMMARY STATED THAT NR 1 IDG AND GEN FAIL DURING T/O. OPENED DMI DM 3124151-1 IAW CRJ MEL 24-11-01-01 CAT A. C/W M PROCEDURE, PLACARD AND TRANSFERRED TO SUMMARY OF DEFERRED ITEMS. 2L72 4F RTA21EA 20041122000292004112200029NM 2004 11 22 SWAA043375 120041117A53156545410366 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED CHORD PER EA. 2L72 4F RTA16WE 20041122000312004112200031NM 2004 11 22 UPS04443314 120040923A5411 SPAR BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, NR 3 PYLON NAC STA 222 AFT LOWER SPAR WEB I/B SIDE CRACK IS FOUND AS MARK. NR 3 PYLON NAC STA 222 I/B SIDE AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 23. 2L74 4F A20WE 20041122000322004112200032NM 2004 11 22 EIA2004139 120041103A5312 BULKHEAD BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 1241 BULKHEAD CANTED WEB, RBL 30, HAS CRACK AT LOWER CORNER OF AIR DUCT CUTOUT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-177-2 AND B747 SRM 51-10-01. 2L74 4F A20WE 20041122000332004112200033NM 2004 11 22 04FDEA03133 120041116A3020 WARNING LIGHT DOUG MD11 MD11F 3023600NM OVERHEAT SYS ILLUMINATED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25621FE 48792 ON CLIMB-OUT AT 14K MSL ENG 2 A-ICE DUCT LEVEL 3 ALERT WITH AURAL WARNING. FOLLWED QRH CHECKLIST AND SHUTDOWN NR 2 ENGINE RETURN TO ONT. OPENED NR 2 ENGINE COWLS FOR INSPECTION, REMOVED ANTI-ICE VALVE HEAT SHIELD, AND REMOVED TWO DUCT ELBOW JOINT HEAT SHIELD FOR DUCT OVER HEAT AND LEAK CHECK INSP ALL DUCTS AND CLAMPS FOUND NO BLOWN DUCTS AND NO VISUAL LEAKS OR DAMAGED. INSP CONNECTORS ON NR 2 ENGINE COWL A/I VALVE. NO PROBLEMS CHECKED FOR 28V ON P1-8245 PIN A VOLTAGE CHECK GOOD FOUND 28VDC AT PIN A REF WDM 30-22-02 SH 1. NR 2 ANTI-ICE VALVE, AND MONITORING SYSTEM HAS BEEN MEL'ED. 2L73 4F RTA22WE 20041122000342004112200034NE 2004 11 22 EIA2004107 220041007A7200 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 3 MALFUNCTIONED A EIAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NM09481EV 19896 662327 ON TAKE OFF ROLL, NR 3 ENGINE WOULD NOT SPOOL UP. THRUST LEVER AT 3/4 TRAVEL, EPR 1.034, N1 42.3 PERCENT, N2 95.8 PERCENT, EGT 761 DEG, FUEL FLOW 4795. REMOVED NR 3 EVC. OP'S AND LEAK CHECK OK PER MM 75-31-01. PERFORMED ALTERNATE EVC TRIM TEST NR 08A PER MM 71-00-00. CHECK OK. DMI NR 457 FOR 60 HRS MAX FLY BACK LIMIT FOR NORMAL EVC TRIM ADJ AND TEST. NON-MEL. 2L74 4F4 F A20WE E20EA 20041122000352004112200035NM 2004 11 22 EIA2004102 120040520A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STRINGER 37R AT STA 300R CRACKED AT FASTENER HOLE FOR STRINGER CLIP. REMOVED AND REPLACED DAMAGED STRINGER SECTION PER B747 SRM 51-30-02, PG 32, 51-30-05, PG 5-6, 51-30-02 PG 2-3, AND 51-20-01,PG 11 AND 14-20. 2L74 4F A20WE 20041122000362004112200036NM 2004 11 22 EIA2004103 120040512A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 CRACK IN OUTER RING CHORD, STA 140R AT STR 20. STOP DRILL CRACK STA 140R AT STR 20. NDT VERIFIED NO CRACK CONDITION REMAINING, ALODINED AND PRIMED. REPAIRED PER EO53-747-1730-04 REV A, AND SB 747-53-2355, FIG 5, PG 52 AND 70-2138-05-0715. 2L74 4F A20WE 20041122000372004112200037NM 2004 11 22 EIA2004108 120041007A3232 LEVER BOEING747 747132 1384882NM MLG DOOR FROZEN A EIAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09479EV 19898 LEFT WING GEAR DOOR, PRIMARY AND ALTERNATE LIGHTS INDICATE DOOR NOT CLOSED. LANDING GEAR COMES DOWN WITH SELECTOR IN OFF POSITION. LEFT WING GEAR DOOR SAFETY LEVER FOUND FROZEN, CLEANED LEVER AND ALL OUTPUT RODS TO DOOR ACUATOR. LUBED ALL EYEBOLTS TO DOOR ACTUATOR RELEASE LINKAGE PER MM 32-32-29. LANDING GEAR HANDLE AND ALL DOOR SYSTEM OPERATIONS CHECKED NORMAL 2L74 4F A20WE 20041122000382004112200038NM 2004 11 22 EIA2004099 120040508A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 UPPER FLOORBEAM, CORROSION AT STA 720 RBL 84.0 WL 199 UNDER FLOOR BOARD. REMOVED FLOORBEAM AT STA 720 LBL TO RBL 15, PER B747 SRM 53-10-07. 2L74 4F A20WE 20041122000422004112200042GL 2004 11 22 04FDEA03136 220041117A7200 FAN BLADE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL NR 1 ENGINE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 CRACKED SEALANT/AXIAL AND RADIAL PLAY AT 29 EACH FAN DISCHARGE VANES, INSIDE NR 1 ENGINE, ON OUTER SHROUD. REMOVED AND REINSTALLED STAGE ONE FAN BLADES TO FACILITATE INSPECTION/REPAIR OF OUTLET GUIDE VANES. INSPECTED 29 OUTLET GUIDE VANES. NO METAL TO METAL CONTACT FOUND. REMOVED AND REPLACED ONE (1) OUTLET GUIDE VANE. ALL WORK DONE IAW MD10-10 AMM 72-22-00 AND FEDEX EA 8-7222-82158. REFER TO FAA FORM 8130-3 TRACKING NR 0733/1158. REFERENCE NON-ROUTINE N00413. 2L73 4F4 FRTA22WE E23EA 20041122000432004112200043WP 2004 11 22 04FDEA03137 120041117A5753ARC19842 HINGE FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 RIGHT WING OUTBOARD FLAP INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING GALLED. MEASURED BORE DIAMETER AT 1.1725, FOUND TO BE BEYOND DAC MD10 CMM 57-52-02 LIMITS OF 1.150. FABRICATED, INSTALL AND FINAL HONE REPAIR BUSHING IAW DAC CMM 57-52-02 AND EA 8-5750-81509, WING RIGHT HAND OUTBOARD FLAP INBOARD HINGE FITTING PIVOT BORE-REPAIR. REFERENCE NON-ROUTINE N00184. 2L73 4F RTA22WE 20041122000442004112200044WP 2004 11 22 04FDEA03138 120041117A5410ASL0046 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON HAS 2 EACH GOUGES UNDER AFT HINGE. REMOVED AFT FITTING IAW DC10 SRM 51-31-01 VOL II. CUT OUT DAMAGED AREA IAW FEDEX EA 8-5410- 81531, NACELLES/PYLON, NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON, REPAIR. REINSTALLED AFT FITTING IAW DC10 SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041122000472004112200047NM 2004 11 22 EIA2004137 120041020A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 540, UPPER DECK FLOORBEAM, UPPER FORWARD SIDE OF CHORD LBL3 THRU LBL6 HAS EXFOLIATING CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CHORD PER B747 SRM 53-30-03, FIGURE 1, ALONG WITH MM 51-30-05 AND 51-20-02. 2L74 4F A20WE 20041122000482004112200048WP 2004 11 22 04FDEA03139 120041117A5410ASL0046 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 NR 3 ENGINE OUTBOARD CORE COWL UPPER LONGERON WORN AFT OF CENTER HINGE. REMOVED DAMAGED AREA IAW FEDEX EA 8-5410-81518, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX EA 8-5410-81518, NACELLES/PYLON, NR 3 ENGINE RIGHT HAND CORE COWL UPPER LONGERON REPAIR. REFERENCE NON-ROUTINE N00176. 2L73 4F RTA22WE 20041122000502004112200050WP 2004 11 22 04FDEA03141 120041117A5410ASL0046 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 NR 1 ENGINE INBOARD CORE COWL UPPER LONGERON IS CRACKED AFT OF CENTER HINGE. REPAIRED IAW FEDEX EA 8-5410-81514, NACELLES/PYLON, NR 1 ENGINE RIGHT HAND CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00166. 2L73 4F RTA22WE 20041122000512004112200051WP 2004 11 22 04FDEA03142 120041117A5753 ROLLER DOUG MD10 MD1010F 3022112WP ZONE 500 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT WING INBOARD FLAP INBOARD TRACK AREA LOWER AFT LARGE ROLLER PLATING WORN ON SIDE OF ROLLER. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK LOWER AFT LARGE ROLLER IAW FEDEX EA 8-5750-81513, WING, INBOARD FLAP, INBOARD ROLLER TORQUE REQUIREMENT, CLARIFICATION. REFERENCE NON-ROUTINE N00606. 2L73 4F RTA22WE 20041122000532004112200053NM 2004 11 22 EIA2004129 120040811A5340 STRINGER CLIP BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STRINGER 23L CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 52-10-03, FIG 4 2L74 4F A20WE 20041122000552004112200055NM 2004 11 22 EIA2004120 120040930A5314 KEELBEAM BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CORROSION CRACK, KEEL BEAM, RT LWR CHORD IB LEG AT STA 1313. TRIM 5.0 INCHES INBOARD LWR FLANGE OF VERTICAL AND HORIZONTAL LEGS. HFEC INSPECTED, FOUND CRACK AND CORROSION FREE. SHOT PEENED AND REFINISHED PER EN EA 53-0827. BOEING MESSAGE 1-OJ18O, 1-OUNOI, AND 1-P5OSK. 2L74 4F RTA20WE 20041122000572004112200057NM 2004 11 22 04FDEA03121 120041116A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK SEAT TRACK FOUND WITH THREE (3) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP AT STA Y= 635, X= -8. CUT AND REMOVED AT STA Y= 625 TO Y= 655, X= 8 PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041122000582004112200058WP 2004 11 22 04FDEA03122 120041116A5753ARC19842 HINGE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46605 RIGHT WING OUTBOARD FLAP INBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, BORE WAS FOUND TO BE OUT OF LIMITS, ETCHED LUG BORE, ROTO PEENED LUG BORE AND CAD PLATED LUG BORE, FABRICATED BUSHING AND CAD PLATED AND INSTALLED AND HONED TO FINAL SIZE IAW DAC CMM 57-52-02, 20-11-02, 20-11-01 AND EA 8-5750-81530 RIGHT HAND OUTBOARD FLAP, INBOARD HINGE BRACKET OVERSIZE PIVOT BORES REPAIR. REFERENCE NON-ROUTINE N00131. 2L73 4F RTA22WE 20041122000602004112200060NM 2004 11 22 EIA2004087 120040902A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 BS 1000 EXTERIOR SKIN EXFOLIATED STR 41R-40R (AC BAY). REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 48 AND 51-30-02. 2L74 4F A20WE 20041122000612004112200061NM 2004 11 22 EIA2004085 120040902A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 STR 37R CRACKED AT STA 990 IN FWD CARGO PIT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM B747 53-10-03. 2L74 4F A20WE 20041122000622004112200062NM 2004 11 22 EIA2004072 120040903A5330 SKIN BOEING747 747121 1384871NM WINDOW BELT CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 WINDOW BELT BS 660-680 LEFT INTERIOR IS CORRIODED. REMOVED CORROSION PER B747SRM 51-10-01, NDT DETERMINED OUT OF LIMITS, FABBED AND INSTALLED REPAIR PER ECRA 480-53-171-2. 2L74 4F A20WE 20041122000652004112200065NM 2004 11 22 EIA2004077 120040911A5710 STRUCTURE BOEING747 747121 1384871NM RT MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 RT WING GEAR WELL HAS SURFACE CORROSION AROUND FASTENER HOLES AT BS 1336-1338 AND OVERWING LONGERON. REPAIRED RT OVERWING LONGERON BS 1326-1345 PER ECRA 480-53-170-2. 2L74 4F A20WE 20041122000672004112200067NM 2004 11 22 EIA2004080 120040902A5310 FORGING BOEING747 747121 1384871NM LT WINDOW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 MAIN CABIN INTERIOR LEFT WINDOW FORGING AND STR 22 L CORRODED BETWEEN BS 300-320. REMOVED CORROSION, STR 22L OUT OF LIMITS REPLACED STR PER B747 SRM 51-30-02 FROM BS 220-406. 2L74 4F A20WE 20041122000722004112200072NM 2004 11 22 EIA2004059 120040720A5320 FITTING BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 1 EA HOLE HAS BREAKUP CONDITION ON CENTER OF STRINGER END FITTING NR 21L AT BS 1241 AFT LT SIDE UPPER. REMOVED AND INSTALLED NEW END FITTING PER B747 51-30-02 PAGES 8-9 AT BS 1241 STR 21L. FABRICATED AND INSTALLED NEW STR NR 21L AT BS 1241-1265 PER B747 SRM 51-30-02 PAGES 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR NR 21L PER B747 SRM 51-30-02 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9. 2L74 4F A20WE 20041122000752004112200075NM 2004 11 22 EIA2004052 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 17L IS CRACKED AT STA 2340. REMOVED FASTENERS FOR ACCESS, PERFORMED HFEC ON SURFACE. CRACKED CONTAINED BY FASTENER HOLES. FABRICATED REPAIR U-CHANNEL. TREATED, PRIMED, AND INSTALLED U-CHANNEL PER B747 SRM 53-10-03 FIG 2, 51-10-01 FIG 7, BSOPM 21-41-00 PAGES 7-9 AT STR 17L STA 2340. 2L74 4F A20WE 20041122000772004112200077NM 2004 11 22 EIA2004071 120040829A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 AFT BELLY SKIN STR R51, CORROSION CRACK APPROX 1 INCH LONG BS 1860: CUT OUT BADLY CORRODED SKIN, CLEANED CORROSION FROM STRINGER: DOUBLER WITHIN LIMITS IAW 53-30-03: RII: ACCOMPLISHED ECI PER B747 NDT MANUAL D6-7170, PART 6, 51-00-00, FIG 623, NO DEFECT DETECTED. LAY OUT FASTENER PATTERN, PICK UP HOLES, FABRICATE DOUBLER AND FILLER AND INSTALL REPAIR PER 747 SRM 53-30-03, FIG 37A. RESTORED ORIGINAL FINISH PER 747 MM 20-24-11. 2L74 4F A20WE 20041122000782004112200078NM 2004 11 22 EIA2004045 120040707A3150 WARNING LIGHT BOEING747 747121 1384871NM PWA JT9 JT9D7F 52054NE NR 4 ENGINE ILLUMINATED A EIAAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09480EV 20348 602202 AFTER TAKEOFF (3000 FT), NR 4 ENGINE FIRE SWITCH ILLUMINATED BELL SOUNDED AND MACELL INDICATOR READ APPROX 9.5 ON A/B LOOPS PERFORMED ENGINE SHUT DOWN IAW EMERGENCY CHECKLIST NR 4 THRUST LEVER WOULD NOT MOVE FWD OF REFERENCE NR 2 AND NR 4 ENG ICING LIGHT ILLUMINATED. HOLD OPEN TILL FINAL FIX IS KNOWN. 2L74 4F4 F A20WE E20EA 20041122000812004112200081 2004 11 22 2004UALA01032 420041101A2565 HOSE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE OUT OF POSITION A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29409UA 462 SLIDE HOSE WAS PACKED INTO ONE FOLD ON THE RIGHT FRONT CORNER. SLIDE ASSEMBLY PREVIOUSLY PACKED INCORRECTLY. REPACKED SLIDE TO SPECIFICATIONS. 2L72 4F4 FRTA28NM E40NE 20041122000872004112200087NM 2004 11 22 EIA2004056 120040719A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM09470EV 20653 STA 300 LOWER LOBE FRAME, 3 EXTRA HOLES WERE DRILLED AND PLUGGED INTO THE 141U1021-21 DOUBLER AND 1 OF THE EXTRA HOLES IS COMMON TO THE 141U1021-9 FRAME AT THE STR 27A 4H CLIP LOCATION. LOCATED AND DRILLED NEW -9 FRAME, DISCREPENT HOLES NOT DRILLED IN NEW FRAME. FRAME PER SERVICE BULLETIN 747-53-2272 REV 18 AND DRAWING 624110003 SH 3A, 4D. 2L74 4F A20WE 20041122000882004112200088NM 2004 11 22 EIA2004048 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 24L IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION, ALODINED, PRIMED AND INSTALLED STR FILLER AND HAD SECTION PER BOEING 747 SRM 51-10-03 FIG 4. REMOVED AND REINSTALLED FOR ACCESS END CAP FITTING PER 747 SRM 51-30-02 PAGES 12-15. 2L74 4F A20WE 20041122000892004112200089NM 2004 11 22 EIA2004061 120040720A5320 FITTING BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 1 EA HOLE HAS BREAKUP CONDITION ON THE CENTER OF STRINGER END FITTING NR 19 BS 1241 LEFT AFT SIDE. REMOVED AND INSTALLED STR END FITTING AT BS 1241 STR 19L. REMOVED AND REPLACED STR NR 19L AT BS 1241-1265. REMOVED AND REPLACED WEB AT BS 1241-1260 STR NR 19L PER SRM 51-30-02 PAGES 8-9, SRM 51-20-01 PAGES 11, 14-20 AND SRM 51-10-02 PAGES 7-8. PRIMED PER BSOPM 20-41-02 PAGES 7-9. 2L74 4F A20WE 20041122000932004112200093NM 2004 11 22 EIA2004053 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 24R IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED HAT SECTION AND STR FILLER PER B747 SRM 53-10-03 FIG 4 PAGES 12-13. REMOVED AND REINSTALLED FOR ACCESS END CAP FITTING PER B747 SRM 51-30-01 PAGES 12-15 AT BS 2360 STR 24R. 2L74 4F A20WE 20041122000942004112200094NM 2004 11 22 EIA2004049 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 25L IS CRACKED AT END CAP FITTING STA 2360, AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 4. REMOVED AND REINSTALLED FOR ACCESS END CAP FITTING PER B747 SRM 51-30-02 PAGES 12-15 AT BS 2360 STR 25L. 2L74 4F A20WE 20041122000952004112200095NE 2004 11 22 2004UALA01019 220041106A7261 LINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 ENGINE OBSTRUCTED A UALAA UNSCHED LANDING KJAFLUID LOSS WARNING INDICATION FLAME/FIRE CRCRUISE 1 WP29429UA 539 NR 1 ENGINE OIL QUANTITY DECREASED FROM 15 TO 7 QUARTS. AFTER LANDING THERE WAS SMOKE AND A SMALL FIRE FROM THE EXHAUST AREA. EXCESSIVE COKING OF THE NR 5 BEARING COMPARTMENT OIL SCAVENGE LINE CAUSED OVER PRESSURIZATION OF THE COMPARMENT. OIL WAS FORCED PASS THE NR 5 CARBON SEAL AND INTO THE EXHAUST GAS PATH. ESCAPED OIL IN THE TEC FLASHED AFTER ENGINE SHUT DOWN. REPLACED OIL SCAVENGE LINE. 2L72 4F4 FRTA28NM E40NE 20041122000962004112200096 2004 11 22 2004UALA01025 420041101A2565 TAPE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29452UA 955 HINGE TAPE IN SLIDE RAMP SEPARATED DURING OVER PRESSURE. THE TAPE SEPARATION COULD BE ATTRIBUTED TO ADHESIVE FAILURE. THE UNIT WAS SENT TO OEM (AIRCRUISERS) FOR REPAIR. 2L72 4F4 FRTA28NM E40NE 20041122000972004112200097 2004 11 22 2004UALA01026 420041101A2565 TAPE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ESCAPE SLIDE SEPARATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29821UA 944 SLIDE RAMP HINGE TAPE SEPARATED DURING OVER PRESSURE TEST. THE TAPE SEPARATION COULD BE ATTRIBUTED TO ADHESIVE FAILURE. THE UNIT WAS SENT TO OEM (AIRCRUISERS) FOR REPAIR. 2L72 4F4 FRTA28NM E40NE 20041122001002004112200100WP 2004 11 22 04FDEA03127 120041116A5753ARC19842 HINGE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25388FE 46622 RIGHT WING OUTBOARD FLAP, INBOARD SUPPORT, PIVOT ATTACH POINT, INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHING, FOUND TO BE OUT OF LIMITS, INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA 8-5750-83939, WING, RIGHT HAND OUTBOARD FLAP, INBOARD HINGE BRACKET, OVERSIZE PIVOT BORES, REPAIR. REFERENCE NON-ROUTINE. 2L73 4F RTA22WE 20041122001012004112200101WP 2004 11 22 04FDEA03128 120041116A5245 DOOR DOUG MD10 MD1010F 3022112WP A/C PACK DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 REPAIR DOUBLER AT FUSELAGE STATION 500-518, NR 3 PACK DOOR, LONGERON 31R-32R NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND IF REPETITIVE INSPECTIONS ARE REQUIRED. COMPLIED WITH FEDEX EA 8-5240-83841 PART 1, FUSELAGE, REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR DOUBLER AT STATION 500-518, NR 3 PACK DOOR. 2L73 4F RTA22WE 20041122001032004112200103WP 2004 11 22 04FDEA03130 120041116A5350AKC70055 FRAME DOUG MD10 MD1010F 3022112WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 CRACKED/TORN DOUBLER ON TAIL CONE FRAME AT STATION YN2164, LEFT HAND UPPER DOWER PIN AREA. REMOVED EXISTING DOUBLER AND INTERCOSTAL IAW MD10 SRM 51-35-01 VOL II. STOP DRILLED CRACK IAW MD10 SRM 53-30-00 VOL I. PERFORMED HFEC TO VERIFY CRACK ENDS AT STOP DRILL IAW NDT SPM 01-10-01- 001. FABRICATED NEW DOUBLER AND INSTALLED ALONG WITH INTERCOSTAL IAW MD10 SRM 53-30-00 PAGE 11 AND EA 8-5352-83943, TAILCONE, FRAME CRACK AT Y2165 AND MD10SRM 51-33-01. REFERENCE NONROUTINE N00864. 2L73 4F RTA22WE 20041122001042004112200104WP 2004 11 22 04FDEA03131 120041116A5350AKC7122 STRAP DOUG MD10 MD1010F 3022112WP ZONE 300 TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 TORN RESTRAINING STRAP ON TAIL CONE RAMP AT U-BAR. REPLACED STRAP ON TAIL CONE RAMP AT RESTRAINING U-BAR IAW FEDEX EA 8-5352-83938. REFERENCE NON-ROUTINE N00859. 2L73 4F RTA22WE 20041122001062004112200106NM 2004 11 22 2004UALA01020 120041108A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29661UA 27158 NOSE COMPARTMENT AT STATION 247 APPROXIMATELY AT RBL 77 FLOORBEAM P-N 141T5104-7 WAS FOUND CRACKED AT WL 195.50. 2L72 4F4 FRTA1NM E24NE 20041122001072004112200107NM 2004 11 22 2004UALA01027 120041101A2560 SURVIVAL KIT BOEING777 777222 1385219NM PWA PW4077PW4077 NE ESCAPE SLIDE MISINSTALLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29769UA 26921 SURVIVAL KIT PACKED IN INCORRECT LOCATION AND LOCATOR LIGHT BATTERY CORD WRAPPED AROUND THE BATTERY. SLIDE WAS PACKED INCORRECTLY AT OVERHAUL JAN 04, BUT NOT ORDERED FOR AN A/C UNTIL OCT 04. WHEN SLIDE INSTALLATION WAS ATTEMPTED, IT WAS REJECTED DUE TO BEING OVERSIZE. SLIDE WAS NOT INSTALLED ON A/C. SLIDE WAS REPACKED AND MADE SERVICEABLE. 2L72 4F4 FRTT0001SE E46NE 20041122001082004112200108 2004 11 22 2004UALA01034 420041108A2565 BATTERY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE ESCAPE SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29661UA 27158 LEFT AND RIGHT HAND OVERWING SLIDE SQUIB FAILS TEST. REMOVED AND REPLACED LT OVERWING BATTERY IN ACCORDANCE WITH AMM. 2L72 4F4 FRTA1NM E24NE 20041122001092004112200109NM 2004 11 22 2004UALA01043 120041111A3350 LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT BURNED OUT A UALAK NONE L NO TEST ININSP/MAINT 1 WP29930UA 26655 EMERGENCY EXIT EXTERIOR LIGHT AT DOOR 1R INOP. LAMP HAD REPORTEDLY "BURNED OUT" AND WAS REPLACED BY MAINTENANCE. 2L72 4F4 FRTA16WE E2GL 20041122001102004112200110NM 2004 11 22 04FDEA03116 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 27L. AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122001122004112200112NM 2004 11 22 AALA20041129 120041113A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21344AN 33083 SFO - FORWARD RIGHT HAND DOOR AND THREE EACH OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK M731 FOR FORWARD RIGHT HAND DOOR AND THREE EACH OVERWING EXIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA1NM 20041122001132004112200113WP 2004 11 22 AALA20041130 120041113A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21469AA 49599 SFO - CEILING EMERGENCY LIGHTS ABOVE SEATS 23, 24, AND 26 INOPERATIVE. REPLACED BATTERY PACK AT ROWS 23 VOR CEILING EMERGENCY LIGHTS ABOVE SEATS 23, 24, AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20041122001142004112200114NM 2004 11 22 2004UALA01045 120041111A3397 WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN LIGHTS CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29176UA 24383 FOUND SPARK ON F-C SEAT 3A CEILING PANEL, F-C ALL SIDE WALL LIGHT AND CEILING LIGHT INOPERATIVE. WIRE BUNDLE W2884 WAS FOUND TO HAVE CHAFED AGAINST A STOW BIN CUT OUT, WHICH HAD LOST ITS PROTECTIVE "CATERPILLAR" COVER. THE WIRE HARNESS, FROM DM8470 TO DM8468, WAS REPLACED AND SECURED PER WDM 33-21-11. THE PROTECTIVE "CATERPILLAR" COVER WAS ALSO REPLACED. 2L74 4F4 FRTA20WE E24NE 20041122001152004112200115NM 2004 11 22 2004UALA01036 120041109A5310 SHEAR WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29903UA 25003 STA 194 SHEAR WEB IS CRACKED AT WL 208 LBL 16. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20041122001162004112200116NM 2004 11 22 2004UALA01037 120041109A2150 A/C PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE RIGHT SMOKE A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29572UA 26682 CREW REPORTS SMOKE IN CABIN, ISOLATED TO RT PACK. ACM ON RT PACK HOT AFTER 15 MINS SHUTDOWN POSSIBLY DUE TO A FROZEN ACM. REPLACED ACM. 2L72 4F4 FRTA2NM E17NE 20041122001172004112200117 2004 11 22 2004UALA01046 420041111A3442 TRANSCEIVER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE WX RADAR SYSTEM INOPERATIVE A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29654UA 25392 RETURNED DUE TO AN INOPERATIVE WEATHER RADAR. REPLACED BOTH THE WX RADAR R-T UNIT, AND THE WX RADAR SCANNER. THERE HAVE BEEN NO FURTHER REPORTS OF WX RADAR PROBLEMS TO DATE. 2L72 4F4 FRTA1NM E24NE 20041122001182004112200118NM 2004 11 22 2004UALA01029 120041109A5320 PLATE BOEING757 757222 1384956NM PWA 2037 PW2037 NE GALLEY CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT GALLEY AREA RT SIDE STA 1681-1691 RBL 52 GALLEY DECK PLATE UPPER SURFACE CORRODED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041122001222004112200122WP 2004 11 22 AALA20041126 120041112A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21931TW 49527 MSP - OVERHEAD LIGHT ABOVE AFT EXIT WALL INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR OVERHEAD LIGHT ABOVE AFT EXIT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20041122001242004112200124WP 2004 11 22 AALA20041127 120041113A3350 LIGHT DOUG DC9 DC983 3022083WP SEAT 27D INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21433AA 49451 DFW - AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 27D INOPERATIVE. REPLACED THE AFT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20041122001262004112200126NM 2004 11 22 04FDEA03112 120041115A5311 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK CARGO COMPARTMENT, RT STA 535 FRAME FOUND CHAFED AT UPPER AND LOWER YOKE MOUNTING AREA. TRIMMED OUT AND REPAIRED PER FEDEX DRAWING SRZ-53-503 AND SRM 51-31-01 VOLUME I. 2L73 4F RTA22WE 20041122001292004112200129NM 2004 11 22 04FDEA03115 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 25L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122001322004112200132WP 2004 11 22 04FDEA03125 120041116A78309043M76GO2 MANIFOLD DOUG MD10 MD1010F 3022112WP ZONE 400 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46605 NR 3 ENGINE LT HAND THRUST REVERSER COOLING DUCT ON THRUST REVERSER UPPER SIDE HAS CHAFING DAMAGE. WELD REPAIRED DUCT BY WELDING IAW FEDEX EA 8-7830-83937, NR 3 LEFT HAND THRUST REVERSER FORWARD COOLING MANIFOLD CHAFED. REPAIR, REINSTALLED NR 3 ENGINE LEFT HAND THRUST REVERSER COOLING UPPER DUCT IAW MD10 MM 78-00-00. REFERENCE NON-ROUTINE N00899. 2L73 4F RTA22WE 20041122001352004112200135NM 2004 11 22 04FDEA02510 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, AT XORS 680 TO XORS 687 LOWER CHORD AREA FOUND WITH CORROSION. N1819 ¾ LEFT HAND WING, REAR SPAR, XORS= 680 TO XORS= 687 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR , CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20041122001362004112200136WP 2004 11 22 04FDEA02772 120040920A5410ARB25831 FITTING DOUG DOUG DC10 DC1030F 3023504WP ZONE 400 NICKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 LEFT HAND WING PYLON AFT ATTACH CLEVIS FITTING FORWARD LOBE HAS NICK. BLENDED AREA IAW DC10 SRM 57-00-01 VOL I, FOUND TO BE WITH IN LIMITS IAW DC10 SRM 57-00-01 VOL I, AND EA 8-5742-81464, PRIMED IAW DC10 SRM 51-21-01 VOL II. REMOVED APPROXIMATELY 0.060 INCH. REFERENCE N/R N01272. 2L73 4F RTA22WE 20041122001372004112200137NM 2004 11 22 04FDEA02002 120040707A5347A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 1059 - 1065, LBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 1049 TO STA 1129 LBL 47.5 REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS AND FABRICATED SEAT TRACK INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041122001402004112200140WP 2004 11 22 04FDEA02773 120040920A5330 SKIN DOUG DC10 DC1030F 3023504WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 REPAIR DOUBLER ON RIGHT HAND FUSELAGE STA 1781 TO 1815 BETWEEN L-29R AND L-30R, NOT IAW DC10-30 SRM. REMOVED REPAIR DOUBLERS IAW DC10-30 SRM 51-33-01 VOL II AND 51-35-01 VOL II. FABRICATED FINGER DOUBLERS AND EXTERNAL DOUBLERS AND INSTALLED IAW DC10-30 SRM 53-20-00 VOL I, 51-33-01 VOL II AND 51-35-01 VOL II. REFERENCE N/R N01311. 2L73 4F RTA22WE 20041122001412004112200141WP 2004 11 22 04FDEA02774 120040920A2140AAM717165 PIPE DOUG DC10 DC1030F 3023504WP ZONE 100 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 AFT CARGO COMPARTMENT HEATING PIPE BROKEN AT STA 1910. REMOVED PIPING LINE FOR REPAIR IAW DC10 MM 20-10-01. CUT OUT AND FABRICATED AND WELDED IN NEW SECTION IAW FEDEX EA 8-2140-81471. INSTALLED PIPING AT AFT CARGO COMPARTMENT IAW DC10-30 MM 20-10-01, LEAK CHECK PIPING IAW DC10-30MM36-00-00 AND INSTALLED FLOORING IAW DC10-30 SRM 51-31-01 VOL II. REFERENCE N/R N01349. 2L73 4F RTA22WE 20041122001422004112200142NM 2004 11 22 04FDEA01999 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 1119, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041122001442004112200144NM 2004 11 22 04FDEA02001 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 1090, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041122001462004112200146WP 2004 11 22 04FDEA02018 120040707A3411 STATIC PORT DOUG MD10 MD1010F 3022112WP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 RIGHT PRIMARY STATIC PORT FAILS RVSM CONVEXITY AND CONCAVITY AND WAVINESS INSPECTION IAW WORK CARD 34C1501 STEP 9 AND 10. REMOVED AND REPLACED RIGHT HAND PRIMARY STATIC PORT IAW FEDEX MD10-10 MM 34-11-01-2, PERFORMED WAVINESS INSPECTION IAW FEDEX MD10-10 MM 34-11-01, CHECKED GOOD, PERFORMED PITOT/STATIC CHECK OF CAPT'S, F.O. AND AUX SYSTEMS IAW FEDEX MD10-10 MM 34-16-00-5, ALL SYSTEMS LEAK CHECKED GOOD. PERFORMED OPERATIONAL CHECK OF RIGHT HAND STATIC PORT HEATER IAW FEDEX MD10-10 MM 34-16-00-5, OPERATIONAL CHECK GOOD. 2L73 4F RTA22WE 20041122001482004112200148WP 2004 11 22 04FDEA02020 120040707A5753 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386F 46620 LEFT HAND OUTBOARD FLAP, UPPER SKIN, INBOARD SECTION, NUMEROUS DAMAGED RIVETS. REMOVED DAMAGED FASTENERS IAW DC10 SRM 51-31-01 VOL II. FABRICATED REPAIR STRAPS IAW DC10 SRM 51-20-00 VOL I AND DC10 SRM 51-21-01 VOL II. INSTALLED REPAIR STRAPS IAW DC10 SRM 57-20-00 VOL I. REFERENCE N/R N00469. 2L73 4F RTA22WE 20041122001492004112200149NM 2004 11 22 04FDEA01968 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERIAL REMOVED=0.016 INCH, REMAINING THICKNESS=0.454 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502. 2L73 4F RTA22WE 20041118001322004111800132WP 2004 11 18 04FDEA02902 120041011A5753ARC25122 FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 RIGHT HAND INBD FLAP PIVOT POINT OUTBOARD BORE HAS GROOVE MARK. REMOVED CORROSION IAW DAC CMM 57-52-01. BEGINNING DIAMETER 1.1875 INCH FINAL 1.2552 INCH . FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475 MPI IAW DACCMM 5752-01 AND DPS 4.704 CAD PLATED, INSTALLED AND HONED BUSHING IAW DACCMM 57-52-01. 2L73 4F RTA22WE 20041118001382004111800138EU 2004 11 18 04FDEA02560 120040824A7830 PANEL AIRBUS300 A300B4605R 3930308EU ZONE 400 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25677FE R633024 791 NR 2 ENGINE O/B T/R, LOWER FWD HINGE PNL IS CHIPPED OFF IN TWO PLACES ON THE FWD SIDE. REPAIRED DAMAGED BLOWOUT DOOR PER EA 6-7830-81874. (OPEN) 2L72 4F RTA35EU 20041118001442004111800144WP 2004 11 18 04FDEA02856 120041001A3411 STATIC PORT DOUG DC10 DC1010F 3022111WP ZONE 100 FAILED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LEFT PRIMARY STATIC PORT FAILS WAVINESS CHECK. REMOVED LEFT HAND STATIC PORT AND REPLACED HEAT SINK IAW FEDEX DC10 MM 34-11-01-2. REMOVED STATIC PORT AND BLENDED OUT GOUGE ON LEFT HAND RUB PLATE IAW DC10 SRM 53-00-02 VOL 1 AND DC10 SRM 51-71-00 VOL II. INSTALLED LEFT HAND PRIMARY STATIC PORT AND HEAT SINK IAW DC10 MM 34-34-11-01-2. INSTALLED LEFT HAND PRIMARY STATIC PORT HEATER ASSEMBLY IAW DC10 MM 34-11-01-2. PERFORMED CONVECTIVITY AND WAVINESS INSPECTION, WITHIN LIMITS IAW FEDEX DC10 MM 34-11-01-2. PERFORMED STATIC LEAK CHECK IAW DC10 MM 34-11-00-2. BOTH CAPTAINS AND FIRST OFFICERS PORTS CHECK GOOD. 2L73 4F A22WE 20041118001462004111800146NM 2004 11 18 04FDEA02599 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOT FACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.392 INCH, MATERIAL REMOVED=0.003 INCH, REMAINING THICKNESS=0.389 INCH AND REPAIRED AS PER EA NR 1-5750- 80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041118001572004111800157NM 2004 11 18 04FDEA02956 120041020A7830683L220G02 COWLING DOUG MD11 MD11F 3023600NM ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 ENG NR 3 LEFT HAND T/R COWL AT UPPER SLIDER TRACK END FOUND CRACKED. UPP SLIDER TRACK REPAIRED AS PER FAA FORM 8130-3 TRACKING NR 5590 (J009773-000). 2L73 4F RTA22WE 20041118001652004111800165NM 2004 11 18 AWXA200401145 120041001A5754 SKIN BOEING737 73733A 1384673NM SLAT ASSY DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-18 CHECK, A DISBOND AREA WAS FOUND ON UPPER SURFACE OF NR 6 LEADING EDGE SLAT AT THE INBOARD END WBL 254.40 - 257.90 RT. MAINTENANCE CUTOUT DAMAGED SECTION ON NR 6 LEADING EDGE SLAT; FABRICATED A FILLER AND DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10, FIG 31. 2L72 4F RTA16WE 20041118001682004111800168NM 2004 11 18 04FDEA02489 120040817A5311SRZ53503 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 MAIN DECK, LEFT SIDE 9G NET ATTACH YOKE ASSEMBLY AT FRAME STA Y= 535 FOUND WITH GOUGE MARK. MAIN DECK, LEFT SIDE 9G NET ATTACH YOKE ASSEMBLY FRAME AT STA Y= 535 CARRIED OUT REPAIR AS PER DWG NR: SRZ-53-503 AND SRM51-31-01 VOLUME II. 2L73 4F RTA22WE 20041118001872004111800187NM 2004 11 18 2004UALA01024 120041106A4990 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE APU OIL SYS ILLUMINATED A UALAA UNSCHED LANDING KHJFLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 WP29547UA 25368 APU SHUTDOWN IN DUE TO OIL QTY MESSAGE AND RIGHT GENERATOR OFF EICAS MESSAGE. 2L72 4F4 FRTA2NM E17NE 20041118002002004111800200NE 2004 11 18 UIEA200400185 220041016A7200 ENGINE BOEING747 74747UF 1384949NM GE CF6 CF680C2B6F 30025NE NR 4 MALFUNCTIONED A UIEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15408MC 29261 NR 4 ENGINE NOT MAKING TO THRUST. (RTO) REJECTED TAKE OFF DUE TO NR 4 ENGINE NOT MAKING TAKE OFF THRUST. PERFORMED POWER ASSURANCE CHEDK (TEST 10), ALL WITHIN LIMITS IAW MM 71-00-00. 2L74 4F4 FRT1384945 E13NE 20041119000102004111900010EA 2004 11 19 ASOA04815 120041023A5210601R3167013 STEP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 10020 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR NEXT TO THE ATTACH LINK WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041119000202004111900020EU 2004 11 19 KBM2004F00227 120040927A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE T/R BLADE WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 492 2300 T/R BLADE WORN. REMOVED AND REPLACED HALF SHELLS. 1G71 3U3 UNCH9EU E19EU 20041119000232004111900023EA 2004 11 19 ASOA04797 120041015A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27875AS 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH. THE PASSENGERS WERE DEPLANED AND THE AIRCRAFT REPOSITIONED ON THE RAMP. MAINTENANCE INSPECTED THE PASSENGER DOOR INTERNALLY AND EXTERNALLY. NO FAULTS OR DEFECTS WERE FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041119000472004111900047NM 2004 11 19 GAIA04102 120040910A5310 BEAM BOEING BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE BULKHEAD CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FWD 1183 BULKHEAD VERTICAL BEAM LBL 36.8 HAS 2 CRACKS. REF FASI NR 86370, STOP DRILLED CRACKED AREA ON FWD BULKHEAD 1183 VERTICAL BEAM AND INSTALLED REPAIR KIT ANGLES IAW SB 727-52-0192. 2L73 4F4 F A3WE E2EA 20041119000492004111900049NM 2004 11 19 GAIA04109 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND VERT CREASE IN FUSELAGE SKIN AT STA 545 BETWEEN STR 19 AND 21R. REF FASI NR 86507 INSTALL DOUBLER REPAIR IAW SRM 53-30-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041119000562004111900056NM 2004 11 19 GAIA04114 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1055 ABOVE STR 20R. REF FASI NR 86520, ACCOMPLISHED DOUBLER REPAIR IAW WITH SRM 53-30-3, FIG 13. 2L73 4F4 F A3WE E2EA 20041119000602004111900060EU 2004 11 19 HXS2004F00004 120040909A6320 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MGB MAKING METAL B HXSDO OTHER O OTHER NRNOT REPORTED 1 AL056302Y2261 9007 PILOT REPORTED MGB CHIP LIGHT. INVESTIGATION REVEALED METALIC CHIPS ON THE BEVEL REDUCTION GEAR BOX THAT EXCEEDED SERVICABILITY STANDARDS. REMOVED GEARBOX AND FOUND EPICYCLIC HAS A BAD BEARING WHICH IS THE SOURCE OF THE METAL. SENT EPICYCLIC AND BEVEL GEAR BOX FOR REPAIR OF CYCYLIC AND INSPECTION OF BEVEL GEAR BOX FOR CROSS METAL CONTAMINATION. 1G71 3U3 U H9EU E19EU 20041119000652004111900065NM 2004 11 19 USAA040677 120040921A534065B578393 ANCHOR FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 ANCHOR FITTINGS; CORROSION; LEVEL 1; TASK NR C53-107-02, ANCHOR FITTINGS AT STA 993R. REPLACED FITTINGS IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E21EU 20041119000662004111900066NM 2004 11 19 USAA040698 120041004A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19587US51935 23932 SKIN, 3.125 INCH CRACK, AT STRINGER 25R, STATION 727E. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229. 2L72 4F4 FRTA16WE E21EU 20041119000932004111900093NM 2004 11 19 BJNA041002 120041005A33506104791 BATTERY PACK BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 RT SIDE EMERGENCY OVER-WING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA16WE E2EA 20041119000952004111900095NE 2004 11 19 AMTA200401248 220041001A7200 ENGINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE NR 1 VIBRATION A AMTAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL11161AT 1219 14784 NR 1 ENGINE DEVELOPED VIBRATION AT FL390. VIBRATION FOLLOWED THROTTLE MOVEMENT AND FELT IN CABIN WITH SELECTOR IN (LOW) AND EITHER (A) OR (B) LATCHED. INSPECTED CHIP DETECTORS AND FILTERS, NO DEBRIS NOTED. INSP ENGINE FOR DAMAGE, NONE NOTED. COMPLIED WITH BOROSCOPE, NO DEFECTS NOTED. PERFORMED GROUND SURVEY AND TRIM BALANCE. COMPLIED WITH CLAPPER LUBE. ENGINE OK FOR SERVICE. 2L73 4F4 F A23WE E12EU 20041119001132004111900113NM 2004 11 19 USAA040781 120040916A5320 INTERCOSTAL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, INTERCOSTAL, HOLE DAMAGE. LIGHTENING HOLE DAMAGE, STA 294.5 + 312 LBL 10 INCH INTERCOSTAL FLOORBEAM LIGHTENING HOLE DAMAGE. FABRICATED WEB AND INSTALLED SAME IAW 53-10-51, FIG 1, PG 17. 2L72 4F4 FRTA16WE E2GL 20041119001212004111900121CE 2004 11 19 A2B2004F00000 120040829A212150041 MOTOR 50041 BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA BLOWER FAILED E A2BAO OTHER O OTHER NRNOT REPORTED 1 GL1593ZC 2499 BB654 DURING OPERATION SMOKE WAS NOTICED IN THE COCKPIT AND A PRCAUTIONARY LANDING WAS MADE. MAINTENANCE FOUND THE FORWARD EVAPORATOR BLOWER MOTOR, WHEN OPERATED ON HIGH, BEGAN TO SLOW AND SMOKE AFTER APPROXIMATELY 15 MINUTES. SUSPECTED THAT THE PROBLEM WAS IN THE ARMATURE WINDINGS. 1L72 4T3 T A24CE E2NE 20041119001322004111900132NM 2004 11 19 SWAA043345 120041115A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND STINGER CLIP AT BS 706, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041119001402004111900140NM 2004 11 19 SWAA043370 120041117A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727A, STRINGER 5L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041119001452004111900145NE 2004 11 19 04317684 220041112A7261 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT SHUTDOWN A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27684BR 7708 EVENT SUMMARY STATED RIGHT ENG SHUT DOWN IN FLT DUE TO LOW OIL PRESSURE. REMOVED AND REPLACED AGB CARBON SEALS FOR IDG, ATS AND HYDRAULIC PUMP IAW AMM 72-60-00. OIL CONSUMPTION RUNS COMPLIED WITH AMM 71-00-00. 2L72 4F4 FRTA21EA E15NE 20041119001492004111900149EA 2004 11 19 VNAA0410011 120041018A5200 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO DOOR FALSE ACTIVATIONA VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL05244PS 7912 DURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C. 2L72 4F4 FRTA21EA E15NE 20041122000092004112200009EA 2004 11 22 VNAA0411002 120041107A5710 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING BIRD STRIKE A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05202PS 7858 AFTER SHUTDOWN IN DAY EVIDENCE OF A BIRD STRIKE ON THE RT WING INBOARD LEADING EDGE WAS REPORTED BY THE CREW OF FLIGHT 2461. PSA MAINTENANCE INSPECTED THE AREA AND FOUND THE DAMAGE TO BE OUT OF LIMITS FOR CONTINUED SERVICE. PSA MAINTENANCE THEN REMOVED & REPLACED THE DAMAGED RT WING INBOARD LEADING EDGE PANEL WITH A SERVICEABLE UNIT IAW CRJ200 AMM 57-41-01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041122000402004112200040WP 2004 11 22 04FDEA03134 120041117A5411ASL0046 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 NR 3 INBOARD COWLING UPPER LONGERON CHAFED UNDER RUB STRIP. FABRICATED AND INSTALLED DOUBLER IAW FEDEX EA 8-5410-81527, NACELLES/ PYLONS, NR 3 ENGINE INBOARD CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00471. 2L73 4F RTA22WE 20041122000492004112200049WP 2004 11 22 04FDEA03140 120041117A5710ARC0357504 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 PANEL NR 641 LB, RIGHT WING INBOARD TRAILING EDGE HAS DELAMINATION IN NUMEROUS AREAS. REPAIRED PANEL NR 641LB BY FABRICATING AND BONDING NEW SKINS, DOUBLER AND CORE IAW TPS 1001 REV E AND DAC DWG ARC0357 ANF FEDEX EA 8-5710-81521, WINGS, RIGHT HAND LOWER AILERON CLOSURE, LOWER TRAILING EDGE FAIRING PANEL. REFERENCE NON-ROUTINE N00919. 2L73 4F RTA22WE 20041122000562004112200056NM 2004 11 22 04FDEA03120 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 36R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122000662004112200066NM 2004 11 22 EIA2004075 120040814A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 PER EO 53-747-1587-00 REV H FOUND 3 FASTENER HOLES CRACKED AT BS 340 LBL 10, 16 AND 48. FABRICATED AND INSTALLED REPAIR PER SB 747-53A2431. 2L74 4F A20WE 20041122000762004112200076NM 2004 11 22 EIA2004068 120040830A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 AFT BELLY SKIN, BS 1800 LBL APPROXIMATELY 2 INCH BELT FRAME CORRODED AT SKIN CONTACT AREA WITH SHEAR TIE CLIP. CUT OUT DAMAGED CLIP, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B747 SRM 53-10-04, FIG 3. 2L74 4F A20WE 20041122000832004112200083 2004 11 22 2004UALA01040 420041109A2565 PROXIMITY SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE L2 DOOR INOPERATIVE A UALAK NONE P NO WARNING INDICATION ININSP/MAINT 1 WP29526UA 24994 DOORS 2L AND 2R ARMED LTS DO NOT COME ON WITH DOORS ARMED. GIRT BAR ANN LIGHT L406 FOR DOOR 2R FOUND SHORTED - REPLACED LIGHT. 2R FORWARD AND REAR PROXIMITY SENSORS FOUND BAD - BOTH SENSORS REPLACED. 2L72 4F4 FRTA2NM E17NE 20041122000842004112200084NM 2004 11 22 2004UALA01041 120041110A2613 OVERHEAT LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE WING-BODY MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29369UA 24538 DIVERTED TO COS DUE TO WING BODY OVERHEAT INDICATION. EXPERIENCED RIGHT WING BODY OVERHEAT WARNING IN FLIGHT WITH ENGINE SUPPLYING AIR. ISOLATED TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP M1204. REPLACED OVERHEAT DETECTOR LOOP M1204. SYSTEM OPERATIONAL CHECKED NORMAL. 2L72 4F4 FRTA16WE E2GL 20041122000852004112200085EU 2004 11 22 2004UALA01042 120041111A5330 SKIN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29422UA 503 THREE DENTS ALONG RIGHT SIDE OF NOSE WHEEL OPENING FROM CONTACT WITH GROUND EQUIPMENT. DOUBLER AND TRIPLER INSTALLED. 2L72 4F4 FRTA28NM E40NE 20041122000922004112200092NM 2004 11 22 EIA2004057 120040719A5315 FLOORBEAM BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 MAIN DECK FLOORBEAM (UPPER CHORD) AT STA 1720, BETWEEN RBL 11.33 AND RBL 33.99 CHORD IS CORRODED AND HAS AN OVERSIZE HOLE IN THE AFT FLANGE (APPROX 348 INCH) AND ONE OVERSIZED HOLE IN THE FORWARD FLANGE (APPROX 258 INCH). REMOVED DAMAGED FLOORBEAM CHORD AND REPLACED WITH NEW SECTION AT STA 1720 RBL 11.33 - 33.999 PER B747 SRM 53-10-07 PAGES 51-54 FIG 12, SHEET 1-4. 2L74 4F A20WE 20041122000982004112200098NM 2004 11 22 EIA2004050 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 23R IS CRACKED AT END CAP FITTING, STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 4. REMOVED AND REINSTALLED END CAP FITTING PER B747 SRM 51-30-02 PAGES 12-15. REMOVED FOR ACCESS SHEAR TIES AND PREPARED PER B747 SRM 53-10-04 FIG 4. 2L74 4F A20WE 20041122001022004112200102WP 2004 11 22 04FDEA03129 120041116A5245 DOOR DOUG MD10 MD1010F 3022112WP A/C PACK DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 REPAIR DOUBLER AT RIGHT HAND FUSELAGE STATION 495-535, NR 2 PACK DOOR 5 INCHES FROM TOP OF DOOR NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IS IN ACCORDANCE WITH FAA APPROVED DATA AND IF REPETITIVE ARE REQUIRED. COMPLIED WITH FEDEX EA 8-5240-83842 PART 1, FUSELAGE, REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR DOUBLER AT STATION 495-535, NR 2 PACK DOOR. REFERENCE NON-ROUTINE N01022. 2L73 4F RTA22WE 20041122001202004112200120NM 2004 11 22 2004UALA01035 120041109A5310 SHEAR WEB BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29903UA 25003 STA 194 SHEAR WEB IS CRACKED AT WL 208 RBL 16. REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20041122001252004112200125NM 2004 11 22 04FDEA03111 120041115A7830 TRACK DOUG MD11 MD11F 3023600NM TRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE R592044 48754 NR 1 ENGINE, RT TRUST REVERSER UPPER SLIDER TRACK CRACKED. R / R PER WORK CARD 78T3901-R. 2L73 4F RTA22WE 20041122001272004112200127NM 2004 11 22 04FDEA03113 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25618FE 48754 BARREL NUT BORE NR 19L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIR PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122001512004112200151WP 2004 11 22 04FDEA02903 120041011A5753ARC05021 HINGE DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LEFT WING OUTBOARD FLAP INBOARD HINGE, LOCATION NR 4 BORE CORRODED. REMOVED CORROSION IAW DACCMM 57-44-08, INSPECTED IAW DACCMM 57-44-08 AND 20-11-02. PEENED IAW DACCMM 57-44-08 AND 20-11-01. PRIMED IAW DC10 SRM 51-21-01 VOL. II. FABBED BUSHING IAW DACCMM 57-44-08 AND EA 8-5750-81470. CAD PLATED BUSHING IAW DACCMM 57-44-08 AND 20-10-01. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-08. BEGINNING BORE 2.300 INCH FINAL BORE 2.3414 INCH MATERIAL REMOVED .0414 INCH IAW DACCMM 57-44-08. 2L73 4F RTA22WE 20041122001522004112200152NM 2004 11 22 AWXA200401199 120041004A531165548929 FRAME BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-18 CHECK, A 1 1/8 INCH CRACK WAS FOUND IN UPPER FLANGE OF FRAME AT BS 344 ABOVE AND OUTBOARD OF STR 23 LT. MAINTENANCE CUTOUT DAMAGED SECTION OF FRAME FLANGE AT BS 344, FROM STR 22 LT TO STR 23 LT; FABRICATED A CHANNEL REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11, FIG 1. 2L72 4F RTA16WE 20041122001552004112200155NM 2004 11 22 04FDEA01967 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.380 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.378 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001582004112200158NM 2004 11 22 04FDEA01963 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, PIVOT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 2.256 INCH, FINAL DIAMETER=2.329 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001592004112200159NM 2004 11 22 04FDEA01962 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD LOWER MOUNT HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 0.516 INCH, FINAL DIAMETER= 0.596 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001602004112200160NM 2004 11 22 04FDEA01961 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.218 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041122001622004112200162NM 2004 11 22 04FDEA01959 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.414 INCH; MATERIAL REMOVED 0.005 INCH; REMAINING THICKNESS: 0.409 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041122001672004112200167EU 2004 11 22 AWXA200401212 120041018A5347D57130147202 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND IN 5 PLACES ON LT CABIN SEAT TRACK Y1292 BETWEEN FS 36 AND FS 41. MAINTENANCE REMOVED CORRODED SECTION LT CABIN SEAT TRACK Y1292 FROM FS 36 TO FS 41; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-42-11. 2L72 4F RTA28NM 20041122001692004112200169NM 2004 11 22 AWXA200401228 120041003A5320143N83393 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 DURING C-10 CHECK, A 1 3/8 INCH CRACK WAS FOUND IN L-2 DOOR LOWER HINGE INTERCOSTAL AT BS 660. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT L-2 DOOR LOWER HINGE BS 660; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 143N8339, AND A CLIP; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041122001702004112200170WP 2004 11 22 04FDEA02913 120041011A5410AL00463 LONGERON DOUG MD10 MD1010F 3022112WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 NR 1 ENGINE LEFT HAND CORE COWL UPPER CHAFE STRIP WORN. FABRICATED DOUBLER, FILLERS, AND STRAP FOR LONGERON REPAIR IAW FEDEX EA8-7110-81487. INSTALLED LONGERON REPAIR IAW DC10 SRM 51-35-01 VOLUME II. FABRICATED RUB STRIP IAW DAC DWG NSL6016. INSTALLED RUB STRIP IAW DC10 SRM 51-35-01 VOLUME II. SEE NR N00192. 2L73 4F RTA22WE 20041122001712004112200171NM 2004 11 22 04FDEA01873 120040629A2613 WARNING LIGHT BOEING727 727227 1384078NM NR 3 STRUT ILLUMINATED A FDEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25490FE 21493 NR 3 STRUT OVERHEAT LIGHT ILLUMINATED APPROX 2 MIN AFTER T/O AT 2000 AGL, QUIET EPR PWR NR 3 ENG PWR PULLED TO IDLE AND OUR HEAT LIGHT WENT OUT APPROX 1 1/2 MIN AFTER POWER PLACED AT IDLE. NORM LANDING WITH NR 3 ENG AT IDLE POWER. A/C CALLED IN EMERGENCY, AND MADE NORMAL LANDING. 2L73 4F A3WE 20041122001722004112200172WP 2004 11 22 04FDEA01875 120040629A5313AGA7810503 STRINGER DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING P TO F MODIFICATION AND TRANSITION CHECK, AFT CGO AT STA 1801-1821, 1887-1902-1921. FOUND STRINGER 52 WITH CORROSION. REMOVED AND REPLACED STRINGER IAW SRM 51-33-01 PAGE 34, 47 AND SRM 51-35-01 PAGE 1-12. 2L73 4F A22WE 20041122001762004112200176NM 2004 11 22 04FDEA01975 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.217 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001772004112200177NM 2004 11 22 04FDEA01976 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.410 INCH, MATERIAL REMOVED=0.005 INCH, REMAINING THICKNESS=0.405 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502. 2L73 4F RTA22WE 20041122001832004112200183NM 2004 11 22 04FDEA02029 120040708A5312AEA76212 PRESSURE PANEL DOUG MD11 MD11F 3023600NM ZONE 100 CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL RT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1. FEDEX EA NR 1-5330-76794 WAS ISSUED FOR TRACKING AND REPETITIVE INSPECTION. 2L73 4F RTA22WE 20041122001852004112200185EU 2004 11 22 SA04106 120041115A5610NP1653115 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 EA19728UW12336 1155 CLT-FLT 514, ENROUTE MYR - CLT, DURING FLIGHT, CREW RECEIVED AN ECAM MESSAGE, "ANTI-ICE L WINDSHIELD". AT THAT TIME, THE WINDSHIELD BEGAN TO ARC WHICH LED TO THE WINDOW PANE CRACKING. THE CREW FOLLOWED THE QRH PROCEDURES. FLIGHT LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. OK FOR SERVICE. 2L72 4F RTA28NM 20041122001862004112200186NM 2004 11 22 0401995519 120041110A5311 FRAME BOEING757 757251 1384970NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01519US 23207 DURING "H" CHECK, FOUND CORROSION ON FRAME AT BS 1400 BETWEEN S27L AND S28L. REPAIRED PER EA 55-201126. 2L72 4F RTA2NM 20041122001872004112200187WP 2004 11 22 0402009860 120040916A5310 DOOR FRAME DOUG DC9 DC951 3022051WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01769NC 47757 DURING L-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR JAMB AT LOWER FORWARD AND AFT CORNERS. REPAIRED PER EA 98-200689. 2L72 4F RTA6WE 20041122001892004112200189NM 2004 11 22 USAA040729 120040917A5320 CHANNEL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - Q4, Z-CHANNEL, CORROSION; 1 INCH DIAMETER AREA, LEVEL 1, TASK NR C53-107-01, MED LOWER THRESHOLD, STA 312-344. MANUFACTURED AND INSTALLED NEW Z-CHANNEL IAW DWG 65-17688. 2L72 4F4 FRTA16WE E21EU 20041122001902004112200190NM 2004 11 22 USAA040727 120040917A5320 WEB BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - Q4, WEB DAMAGED, 11 INCHES LONG, AFT OF STA 986.5 FLOOR LEVEL AFT OF AFT ENTRY DOOR. MANUFACTURED WEB AND INSTALLED IAW SRM 51-10-02 AND DWG NR 65C33533. 2L72 4F4 FRTA16WE E21EU 20041122001922004112200192EU 2004 11 22 BA04028 120041105A324431546 TIRE AIRBUS330 A330323 3930335EU MLG SEPARATED A USAAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 EA19672UW 2745 333 FRA - ON TAKEOFF FROM FRA, THE NR 4 TIRE LOST ITS RECAP. THE RUBBER PUNCTURED THE RIGHT INBOARD SPOILER AND DENTED THE LEADING EDGE OF THE RIGHT INBOARD FLAP. MAINTENANCE REPLACED THE NR 3 AND NR 4 TIRES, AND PERFORMED AN INTERIM REPAIR TO THE SPOILER FOR A FERRY FLIGHT TO CLT. SUBSEQUENTLY, THE SPOILER WAS REPLACED AND A REPAIR ISSUED FOR THE FLAP DENTS. 2L72 4F RTA46NM 20041122001932004112200193NM 2004 11 22 SB04138 120041004A335020131A BATTERY PACK BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19784AU 25023 CLT - MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS AT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122001942004112200194EU 2004 11 22 BA041024 120041017A3350321431 BATTERY AIRBUS330 A330323 3930335EU R1 AND L4 DOORS FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 333 PHL - FOUND THE R1 AND L4 DOOR EPSU'S FAULTY. MAINTENANCE REPLACED THE BATTERY PACKS. 2L72 4F RTA46NM 20041122001962004112200196NE 2004 11 22 BA04029 220041110A75326764B040000 BLEED VALVE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE LT ENGINE FAILED A USAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA19676UW 0375 PHL - FLT98 - DURING CRUISE, ENROUTE FROM PHL TO LGW, CREW REPORTED THE NR 1 ENGINE HP BLEED VALVE FAILED IN THE CLOSED POSITION. CREW ATTEMPTED TO CORRECT THE PROBLEM BUT THE VALVE REMAINED CLOSED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE APPLIED MEL 36-1101. SUBSEQUENTLY, THE HP BLEED VALVE WAS REPLACED. 2L72 4F4 FRTA46NM 20041122001982004112200198EU 2004 11 22 SA04096 120041018A335032145410 EPSU AIRBUSA319 A319112 3930323EU ZONE 200 FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19741UW12908 1269 PIT - CABIN EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE MID-CABIN, FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041122002012004112200201EU 2004 11 22 EM04022 120041115A3297 CONNECTOR EMB ERJ170ERJ170100 EU MLG WOW DAMAGED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19808MD 17000021 FLIGHT 1759, PIT TO ATL - AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. THE CREW FOLLOWED QRH PROCEDURES AND RETURNED TO PIT. MAINTENANCE, TROUBLESHOT CMC AND FOUND NOSE GEAR WEIGHT ON WHEELS SENSOR ONE BAD. REMOVED AND REPLACED CONNECTOR ON NOSE GEAR WEIGHT ON WHEELS SWITCH ONE. OPERATIONAL TEST CHECKS GOOD. 2L74 4F RTA56NM 20041122002022004112200202EU 2004 11 22 SA04098 120041019A2611 WARNING LIGHT AIRBUSA319 A319112 3930323EU CARGO SMOKE DET INTERMITTENT A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19721UW 1095 MSY - FLIGHT 972 ENROUTE MSY-PHL, AFTER TAKEOFF, A FORWARD CARGO SMOKE WARNING CAME ON INTERMITTENTLY. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL TEST. THE SYSTEM OPERATIONALLY CHECKED OK. 2L72 4F RTA28NM 20041122002032004112200203NM 2004 11 22 USAA040775 120041024A5510 PIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RT HORIZ HINGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19448US38880 24892 PIT - C3, PIN ASSEMBLIES, 1 INCH BY 1 INCH AREA, CORROSION; NO LEVEL OR TASK. RT HORIZ HINGE PINS (INNER AND OUTER) HORIZ STAB. REMOVED AND REPLACED INNER AND OUTER HINGE PIN ASSY IAW EA 79359/ DRAFT EO 5502V025. 2L72 4F4 FRTA16WE E21EU 20041122002042004112200204NM 2004 11 22 USAA040707 120040921A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19541AU52643 23700 SUPPORT ZEE ANGLE, .2500 INCH BY .1250 INCH AREA, CORROSION; LEVEL; TASK C53-202-1; BS 727A TO 787 AT AFT CARGO S-25R. 2L72 4F4 FRTA16WE E21EU 20041122002052004112200205NM 2004 11 22 USAA040726 120040917A5310 CREASE BEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 WEB, 1 INCH AREA, CORROSION; NO LEVEL OR TASK, UPPER AND LOWER SURFACE CREASE BEAM, LT SIDE STA 948, 965. MANUFACTURED WEB FROM ALUM MATERIAL IAW SRM 53-60-15. 2L72 4F4 FRTA16WE E21EU 20041122002072004112200207NM 2004 11 22 SB04126 120040919A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19528AU 24410 CLT - MAINTENANCE REPORTED THE SEAT MOUNTED AND BULL NOSE EMERGENCY ESCAPE PATH LIGHTING, IN THE MID-CABIN, INOPERATIVE. MAINTENANCE TROUBLESHOT PROBLEM TO THE MID-CABIN BATTERY PACKS. REMOVED AND REPLACED MID-CABIN BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002092004112200209 2004 11 22 SB04132 420040926A3441 IRU BOEING737 737301 1384611NM COCKPIT OUT OF ALIGNMENTA USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19353US 23556 PVD - FLT491 - DURING TAKEOFF FROM PVD, THE ATTITUDE FLAG CAME INTO VIEW. BOTH THE FMC AND PMC WERE INOPERATIVE AND ON MEL AT THE TIME. FLIGHT RETURNED TO FIELD AT PVD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REALIGNED BOTH IRU'S. SYSTEMS CHECK OK. 2L72 4F RTA16WE 20041122002112004112200211NM 2004 11 22 USAA040758 120041018A5330 SKIN BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US43929 23989 CLT - RON, SKIN 1.5 INCH CRACK, BS 727D AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. 2L72 4F4 FRTA16WE E21EU 20041122002122004112200212NM 2004 11 22 0556 120040901A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US 23232 1.5 INCH LONG CRACK IN SKIN AT STATION 867+2 STRINGER 24R. 2L72 4F RTA16WE 20041122002132004112200213NM 2004 11 22 USAA040773 120041024A5312 BULKHEAD BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19777AU38518 24979 PIT - C2, BULKHEAD SKIN, 1 INCH CRACK, FWD PRESSURE BULKHEAD RBL 57, WL 210. INSTALLED DOUBLER IAW SRM 53-10-08 FIG 211. 2L72 4F4 FRTA16WE E21EU 20041122002172004112200217NE 2004 11 22 USA2004F00098 220040918A73204120T00P32 FADEC EMB ERJ170ERJ170100 EU GE CF34 CF34* NE NR 2 ENGINE MALFUNCTIONED A USAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA19810MD423 17000026 AIRCRAFT RETURNED TO GATE. NO TAKEOFF DATA, NR ENGINE POWER LIMIT 77 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FADEC. 2L74 4F4 FRTA56NM E15NE 20041122002182004112200218NM 2004 11 22 USAA040716 120040909A5754 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 UPPER SKIN, 1.5 INCH SQ AREA DELAMINATED; NR 4 SLAT IB T/E. REMOVED DELAMINATED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER AND REFINISHED IAW SRM 57-40-02 AND 51-70-10. 2L72 4F4 FRTA16WE E21EU 20041122002212004112200221NM 2004 11 22 USAA040675 120040903A5740 HINGE FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU GROUND SPOILER WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 HINGE FITTING WORN .0625 INCH AT PIVOT POINT NR 5 GROUND SPOILER OB AND WBL 169.25. FABRICATED NEW PART IAW MFG DRG 69-39228. 2L72 4F4 FRTA16WE E21EU 20041122002222004112200222NM 2004 11 22 USAA040676 120040826A534065B578393 ANCHOR FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 ANCHOR FITTINGS, .1250 INCH BY .1250 INCH AREA, CORROSION: LEVEL 1; TASK NR C53-107-02 ANCHOR FITTINGS (2) STA 993L. REPLACED FITTINGS IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E21EU 20041122002242004112200224EU 2004 11 22 BA04026 120041025A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 333 PIT - EMERGENCY LIGHTS AT THE R1 AND L4 DOORS DID NOT ILLUMINATE WHEN GROUND POWER FAILED. MAINTENANCE REPLACED THE 12WL AND 17WL EPSU BATTERIES. 2L72 4F RTA46NM 20041122002262004112200226NM 2004 11 22 EIA2004054 120040719A5312 PRESSURE PANEL BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 FUSELAGE INTERIOR, STA 1420, LBL 10 TO RBL 10 CORROSION ON UPPER SURFACE OF WHEEL WELL PRESSURE DECK WEB. REMOVED DAMAGED AREA. FABRICATED REPAIR FILLER AND DOUBLERS. INSTALLED REPAIR DOUBLERS AND FILLERS PER B747 SRM 53-10-07 FIG 2. 2L74 4F A20WE 20041122002272004112200227NM 2004 11 22 EIA2004055 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 MAIN DECK STA 160 FRAME STRINGER 6L HAS 1 EA EXISTING ELONGATED HOLE AT STRINGER CLIP LOCATION (APPROX ELONG DIAMETER .350 INCH) STR 6L P/N 65B 14211-13. REMOVED AND REPLACED STR 6L AT STA 140 TO STA 200 PER B747 SRM 51-30-02 PAGES 2,3,5; FIG 7 PAGE 32. 2L74 4F A20WE 20041122002322004112200232NM 2004 11 22 EIA2004044 120040701A3232 ACTUATOR BOEING747 747132 1384882NM MLG DOOR INOPERATIVE A EIAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM09481EV 19896 AT FLIGHT LEVEL 34.0 .88M 300 KNTS GEAR DOOR OPEN LIGHT CAME ON. CHECKED LANDING GEAR PANEL, FOUND LEFT BODY GEAR DOOR OPEN LIGHT IN BOTH PRIMARY AND ALT. AFTER DESCENT TO 22.0 270 KNTS, THE PRIMARY LIGHT WENT OUT THE ALT STAYED ON THE GEAR HANDLE WAS UP. REMOVED AND INSTALLED LEFT BODY GEAR DOOR ACTUATOR PER MM 32-33-27. ALSO ADJUSTED TARGETS FOR PRIMARY AND ALT SWITCHES, OPS CHECKED PER MM 32-61-10. 2L74 4F A20WE 20041122002342004112200234NM 2004 11 22 EIA2004066 120040720A5320 FITTING BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 4 EA HOLES HAVE BREAKUP CONDITION ON THE CENTER OF STRINGER END FITTING NR 25 BS 1241 RT AFT SIDE. REMOVED AND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGES 8-9, AT BS 1241 STR 25R. FABRICATED AND INSTALLED NEW STR 25R AT BS 1241-1265 PER B747 SRM 51-30-02 PAGED 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR 25R PER B747 SRM 51-30-02 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9. 2L74 4F A20WE 20041122002372004112200237NM 2004 11 22 USAA040708 120040901A5315 FLOORBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU52643 23700 T-CAP, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 328 BL 0, RBL 59 INCH, 3 AREAS. INSTALLED NEW T CAP PER SRM 53-10-51. 2L72 4F4 FRTA16WE E21EU 20041122002402004112200240NM 2004 11 22 EIA2004098 120040515A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 28A CRACKED AT BS 500 L. FABRICATED INSTALLED NEW STRINGER SECTION PER B747 SRM 51-30-05, 51-10-02, 51-30-02, AND SOPM 20-41-02. 2L74 4F A20WE 20041122002422004112200242NM 2004 11 22 EIA2004127 120041012A335090084 POWER SUPPLY BOEING747 747121 1384871NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09480EV 20348 CREW DOOR EMERGENCY SILL LIGHT INOP. REPLACED POWER SUPPLY FOR EMERGENCY LIGHT AT EMERGENCY CREW DOOR AND ACCOMPLISHED SATISFACTORY SYSTEM CHECK. 2L74 4F A20WE 20041122002432004112200243NM 2004 11 22 EIA2004128 120041012A3350S1356B37 LIGHT BOEING747 747121 1384871NM L5 DOOR INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09480EV 20348 EMERGENCY LIGHT AT L-5 DOOR INOP (CENTER POSITION). REPLACED EMERGENCY LITE ASSY AND PERFORMED SATISFACTORY SYSTEM TEST. 2L74 4F A20WE 20041122002442004112200244NM 2004 11 22 EIA2004134 120041009A5710 SUPPORT BEAM BOEING747 747273C 1384896NM RT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 RT WING STA 665-685, TRAILING EDGE SUPPORT BEAM, LOWER CHORD CRACKED ON FORWARD SIDE. REPAIRED RT WING TRAILING EDGE SUPPORT BEAM, LOWER CHORD BETWEEN WS 665-685, PER ECRA 470-57-227-2, REV A. 2L74 4F A20WE 20041122002492004112200249NM 2004 11 22 SB04133 120040926A3397 WIRE BOEING737 737301 1384611NM EMERGENCY LIGHT FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 CLT - MAINTENANCE REPORTED TWO EMERGENCY EXIT LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED A BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002502004112200250NM 2004 11 22 USAA040789 120041002A5315 FLOORBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B1US GL FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT - Q5, FLOORBEAM TEE CAP, .1250 INCH BY .1250 INCH (6 AREAS), CORROSION; LEVEL 1; TASK NR C53-107-02, TOPS OF FLOORBEAMS IN AROUND SCREW HOLES STA 1016-986.5. REMOVED CORROSION, TREATED, PRIMED, REPLACED 10 INCHES OF T-CAP IAW SRM 53-60-51. 2L72 4F4 FRTA16WE E2GL 20041122002522004112200252NM 2004 11 22 USAA040711 120040930A5320 SPLICE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 CRACK SPLICE, .5 INCH LONG, STA 908 AND STR 4R, SPLICE. MANUFACTURED NEW SPLICE IAW 51-20-01, 51-20-05. 2L72 4F4 FRTA16WE E21EU 20041122002542004112200254NM 2004 11 22 EIA2004097 120040713A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 24A BETWEEN BS 300-320 HAS ELONGATED FASTENER HOLES. REMOVE DAMAGE, FAB AND INSTALLED NEW STRINGER PER B747 SRM 51-30-02, 51-20-01, AND 51-30-02. 2L74 4F A20WE 20041122002552004112200255NM 2004 11 22 EIA2004091 120040526A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 CORROSION, FS 1960 STR 46R-46L. REMOVED EXTERNAL SKIN DOUBLER, INTERNAL SKIN BONDED DOUBLER AND EXISTING STRUCTURES, INCLUDING SHEAR AND STRINGER TIES, STRINGER SPLICE AT BS 1960 FROM STR 46R-50R. NO CORROSION FOUND ON INTERNAL AND EXTERNAL SKIN FROM STR 46L-46R AT BS 1960. REINSTALLED EXTERNAL SKIN DOUBLER AND EXISTING STRUCTURES PER B-747 SRM 51-30-02, PG 8-9, AND REINSTALLED INTERNAL BONDED SKIN DOUBLER PER B747 SRM 53-30-03, FIG 38. 2L74 4F A20WE 20041122002562004112200256NM 2004 11 22 EIA2004131 120040526A5312 PRESSURE PANEL BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 MAIN CABIN STA 1460, RBL 120 HAS SURFACE CORROSION AT UPPER MAIN WHEEL WELL PRESS WEB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-07, FIG 2, PGS 4-10. 2L74 4F A20WE 20041122002572004112200257EU 2004 11 22 SA04101 120041027A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING O OTHER CLCLIMB 1 EA19736US14080 1209 RIC - FLT 121 EN ROUTE, RIC - CLT. WHILE ON CLIMB-OUT FROM RIC, AT ABOUT 9,000 FEET, THE CREW NOTED ELECTRICAL ARCING OF THE FIRST OFFICER'S WINDOW. THE CIRCUIT BREAKER FOR THE WINDOW ANTI-ICE WAS PULLED, HOWEVER, THE OUTER PANE OF THE WINDOW CRACKED ANYWAY. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDOW. OK FOR SERVICE. 2L72 4F RTA28NM 20041122002582004112200258NM 2004 11 22 SB04148 120041024A33501012623 LIGHT BOEING737 737301 1384611NM SEAT 10C INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US 23935 PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002602004112200260NM 2004 11 22 EIA2004143 120041106A5310 STRUCTURE BOEING747 747273C 1384896NM MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 1480, LBL 74.92, TOP OF MLG BOX HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2P-1. 2L74 4F A20WE 20041122002612004112200261NM 2004 11 22 EIA2004144 120041106A5312 PRESSURE PANEL BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 SURFACE CORROSION ON PRESSURE WEB COMMON TO LONGITUDINAL FLOORBEAM MATING SURFACE AT BS 1480, LBL 11.33. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2PL. 2L74 4F A20WE 20041122002652004112200265NM 2004 11 22 USAA040720 120040903A5340 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 CLIP, 1 INCH CRACK, FRAME TO LONGERON CLIP INTERIOR FUSELAGE, STA 344, STR 11R. MFG AND INSTALLED REPLACEMENT CLIP IAW MFG DWG 69-38939. 2L72 4F4 FRTA16WE E21EU 20041122002662004112200266NM 2004 11 22 SB04152 120041107A29136507506 PUMP BOEING737 7373B7 1384580NM NR 2 ENGINE LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19396US4586437374 23318 BOS - FLT2039 - ON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, THE B SYSTEM HYDRAULIC FLUID BEGAN TO DECREASE AND THE B SYSTEM ENGINE DRIVEN PUMP LOW PRESSURE LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND B SYSTEM PRESSURE FILTER. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20041122002682004112200268NM 2004 11 22 USAA040784 120041001A5754 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 1 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT - Q5, NR 1 SLAT, .2500 INCH CRACK, NR 1 SLAT L/E LOWER SURFACE AFT ROW OF RIVETS. DOUBLER INSTALLED IAW 57-43-01. 2L72 4F4 FRTA16WE E2GL 20041122002702004112200270EU 2004 11 22 EM04021 120041030A32309037B000102 CONTROL LEVER EMB ERJ170ERJ170100 EU ZONE 100 INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19808MD618 17000021 FLIGHT 1628, MKE TO PHL - LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION ON TAKEOFF. THE CREW RETURNED TO THE FIELD LANDED WITHOUT INCIDENT. MAINTENANCE, REMOVED AND REPLACED THE LANDING GEAR HANDLE. OPERATIONAL CHECK IS GOOD. 2L74 4F RTA56NM 20041123000022004112300002WP 2004 11 23 04FDEA03179 120041122A5754 SKIN DOUG DC10 DC1010 3022110WP NR 1 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2510060 46970 LT, INBD SIDE, NR 1 SLAT HAS APPROX. 56 INCH LONG CRACK ON INNER SURFACE, BOTTOM EDGE BELOW CLOSEOUT WEB. FASTENERS MISSING/PULLED. INSTALLED NEW NR 1 SLAT LT S/N MAC86 PER AMM 27-80-01-4 PARA 3(B) 1-13. RIGGED AND ADJUSTED LT NR 1 SLAT PER MM 27-80-01-4 3(B) 14-23. 2L73 4F A22WE 20041123000042004112300004SW 2004 11 23 ALGA097931 120040120A6410206016201131 BLADE BELL 206 206L1 1182107SW TAIL ROTOR UNKNOWN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031081K838 45407 C/W 206L-04-127 REV B PT 3/ SENT TO REPAIR STATION. 1G71 3U H2SW 20041123000092004112300009CE 2004 11 23 DXTA200400448 120041115A213152770114 CONTROLLER CESSNA560 560XL 2076702CE CABIN AIR INOPERATIVE E DXTAC ABORTED TAKEOFF BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 GL07645QS3901 5605145 DURING T/O ROLL, AT 70 KIAS A LOUD BANG FROM TAIL AREA FOLLOWED BY A PRESSURE BUMP. STRONG SMOKE ODOR, NONE VISIBLE. COULDN’T DETERMINE WHERE SMOKE ODOR WAS COMING FROM, SEEMED TO COME FROM AIR VENTS. GND IDLE LIGHT REMAINED ILLUM UNTIL 1000 FT AGL. PRESS SEEMED TO RETURN TO NORMAL & SMOKE ODOR DISSIPATED. PAX IN SEAT 5 HEARD & SMELLED SAME. RAN A/C SYS, & UNCONTROLL IN TEST MODE. OPENED OUTFLOW VLVE ACCESS PNL, CHKD FOR LOOSE FITTINGS, REMOVED PARTICULAR TRAP & CHKD FOR WATER, NONE PRESENT. REMOVED & CLEANED COALESCER SOCK, INST & SAFETIED. PERFORMED MX CHK ON SYS, FAILED CALIBR CHK ON AMBIENT & 1000 FT ABOVE. SWK NR 5 POSS RELATED TO SMOKE ODOR. R & R CONTROLLER. OPS CHK GOOD, IAW 560 XL-MM CH 21-30-00.2L72 4F RTA22CE 20041123000112004112300011NE 2004 11 23 SWIA200414087 220041109A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT POWER LOSS A SWIAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 NM07597SW100826388 7293 807081C ON DESCENT RT ENGINE N1, SPOOLED DOWN, ITT INCREASED TO 800 DEGREES, AND A BANG WAS HEARD. N1 DID NOT RESPOND TO THRUST LEVER ADVANCEMENT. ENGINE WAS LEFT AT IDLE UNTIL LANDING. REMOVED AND REPLACED RT ENGINE PER CRJ MM 71-00-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041123000162004112300016SO 2004 11 23 C2XA04IA129 120041017A3350B6245 LIGHT EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2712519 145366 IAH - FLIGHT 2800, DURING CREW PREFLIGHT THE FORWARD EMERGENCY EXIT LIGHTS WAS INOPERATIVE. REMOVED AND REPLACED THE DEFECTIVE LIGHT. 2L72 4F RTT00011AT 20041123000182004112300018SO 2004 11 23 C2XA04IA138 120041107A3397W764850720 WIRE EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714171 14500859 IAH - FLIGHT 2916, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON IN THE ARM POSITION. MAINTENANCE CYCLED THE EMERGENCY LIGHT SWITCH AND THE LIGHTS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. DURING PREFLIGHT INSPECTION FOR FLIGHT 3460, THE CREW REPORTED THE EMERGENCY LIGHTS CAME ON WITH THE CABIN LIGHTS. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE UNDER THE BULKHEAD, OPERATIONALLY CHECKED LIGHTS WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20041123000192004112300019SO 2004 11 23 C2XA04SH539 120041026A532014532636401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 24. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT APPROVED FOR SERVICE. 2L72 4F RTT00011AT 20041123000202004112300020SO 2004 11 23 C2XA04SH535 120041026A532014532637401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 24. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW 53-22-01. AIRCRAFT APPROVED FOR SERVICE. 2L72 4F RTT00011AT 20041123000212004112300021SO 2004 11 23 C2XA04SH537 120041026A532014530646401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 54. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01168. AIRCRAFT APPROVED FOR SERVICE. 2L72 4F RTT00011AT 20041123000222004112300022NM 2004 11 23 QXEA200400742 120041108A2750 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM TE FLAPS ILLUMINATED A QXEAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09402QX 4032 PDX - THE CREW REPORTED THAT THE FLAP POWER CAUTION LIGHT ILLUMINATED AND THAT THE CHECKLIST WAS RUN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO CURRENT FAULTS IN THE CDS. THE FLAP CIRCUIT BREAKER WAS CYCLED AND THE CAUTION LIGHT EXTINGUISHED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123000232004112300023NM 2004 11 23 QXEA200400741 120041105A2751756158 TORQUE SENSOR DHAV DHC8 DHC8202 2809007NM FLAP FAULTY A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09375PH8652 2258 529 BLI - FLIGHT 2279 - FLIGHT DIVERTED TO BLI WHEN DURING THE CLIMB THE CREW RECEIVED A FLAP POWER CAUTION. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLAP TORQUE SENSOR UNIT. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123000242004112300024SO 2004 11 23 C2XA04IA140 120041105A33507287580501 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2717513 145292 IAH- FLIGHT 2119, DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN EMERGENCY LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041123000252004112300025SO 2004 11 23 C2XA04SD008 120040918A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713949 145057 EMERGENCY LIGHTS BELOW COCKPIT DOOR AND ABOVE MAIN CABIN DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER AS PER THE EMB AMM 33-50-11. EMERGENCY LIGHTS OPERATIONALLY CHECKED NORMAL AND AIRCRAFT WAS RELEASED. 2L72 4T RTT00011AT 20041123000262004112300026SO 2004 11 23 C2XA04CL100 120041006A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2748901 145501 CLE - FLIGHT 3351, THE CREW REPORTED THE EXIT ROW AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20041123000282004112300028SO 2004 11 23 C2XA04SH532 120041026A532014530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 38 WAS FOUND CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-23-10 AND EC5320-01168. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041123000302004112300030CE 2004 11 23 DXTA200400444 120041112A3220 WHEEL CESSNA750 750 2076810CE NLG NOISY E DXTAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL07984QS 7500084 DURING FLIGHT, LOUD BANGING NOISE FROM NOSE WHEEL. NOSE WHEEL DROPS A LITTLE AND THEN IS SLAMMED BACK UP MAKING LOUD CLUNK. HAPPENED APPROX 8 TIMES IN A 4 HR FLIGHT. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20041123000312004112300031CE 2004 11 23 DXTA200400445 120041112A3241 ANTI-SKID SYS CESSNA560 560XL 2076702CE MLG INOPERATIVE E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07626QS 5605126 ON APPROACH, BROUGHT THE LANDING GEAR DOWN BOTH ANTI-SKID INOP AND LOW BRAKE PRESSURE ANNUNCIATORS REMAINED ILLUMINATED. CYCLED THE GEAR AND RAN THE CHECKLIST, THE POWER BRAKES CB WAS IN WHEN RUNNING THE CHECKLIST. EMERGENCY BRAKES WERE USED TO STOP AIRCRAFT. UNDER INVESTIGATION. 2L72 4F RTA22CE 20041123000322004112300032CE 2004 11 23 DXTA200400446 120041113A3230 LANDING GEAR CESSNA750 750 2076810CE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07912QS 7500012 AFTER TAKEOFF LANDING GEAR HANDLE PLACED IN THE UP POSITION A LOUD CLUNK WAS HEARD, GOT THE RED UNSAFE AND GREEN NOSE GEAR LIGHT. PLACED GEAR IN THE DOWN POSITION AND GOT 3 GREEN LIGHTS THE GEAR HANDLE WOULD NOT MOVE UP OR DOWN. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20041123000332004112300033NM 2004 11 23 QXEA200400744 120041109A3350DSC4042 RELAY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A QXEAO OTHER O OTHER TOTAKEOFF 1 NM09379PH 530 SEA-ON FLIGHT 2111, DURING TAKEOFF, F/A REPORTED EMERGENCY LIGHTS FLICKERED ON THEN OFF 3 TIMES AND REMAINED OFF FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RELAYS 3351-K3-K4. EMERGENCY LIGHTS SYSTEM CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123000352004112300035NM 2004 11 23 QXEA200400768 120041113A3610 ODOR BOMBDRDHC8 DHC8401 1390041NM CABIN DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09405QX 4047 PDX FLT 9851 THERE IS A SMOKY BLEED AIR SMELL COMING FROM AIR CONDITIONING VENTS AFTER ENGINE START. SMELL EVENTUALLY CLEARS OUT. OPERATED BOTH ENGINE BLEEDS AND AIRCRAFT PACKS TO PURGE POSSIBLE CONTAMINATION. NO OIL SMELLS OR OTHER UNUSUAL ODORS NOTED AFTER REPEATED RUNS AT VARIOUS POWER SETTINGS, BLEED FLOW SETTINGS AND TEMPERATURE SETTINGS. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20041123000362004112300036NM 2004 11 23 QXEA200400767 120041113A3610 ODOR BOMBDRDHC8 DHC8401 1390041NM BLEED AIR SYS DETECTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09405QX 4047 PDX FLIGHT 2307 GETTING OIL SMELL APPARENTLY COMING FROM BLEEDS. MAINTENANCE PERFORMED HIGH AND LOW POWER RUNS WITH BOTH ENGINES, ONE BLEED AT A TIME. RAN CABIN AND COCKPIT TEMPS HIGH AND LOW, NO NOTICEABLE OIL SMELL IN AIRCRAFT FROM EITHER BLEED. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123000372004112300037EU 2004 11 23 DHL2004363533 120040915A5730 SKIN AIRBUS300 A300B4203 3930306EU RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, RT WING L/E UPPER SKIN 1.5 INCH CRACK JUST RIGHT UP I/B SIDE JACK SCREW NR 3. CUT OUT DAMAGE SECTION OF L/E SKIN AT RT WING. PERFORMED HFEC OF CUTOUT AREA, NO DISCREPANCIES NOTED. INSTALLED DOUBLER AND FILLERS AS REQUIRED TO RT WING L/E UPPER SKIN REF: A-300 SRM 57-34-11. MATERIAL USED 2014-0.063 HEAT TREATMENT PER A-300 SRM 51-40-30 / PO MATERIAL / 24302423 HEAT TREATED TO T6. SIZE FILLER 2014 T6 0.063, 26 X 18 INCHES (2) STRAPS SPLICES 2014 T6 0.063 20 X 5 INCHES, 4 SPLICE STRAPS (2) 2014T6 0.063 9 X 1.5 INCH AND (2) 2014 T6 0.063 7 X 1.5 INCH. TREATED AND PRIMED AREA / FILLERS AND DOUBLERS, APPLY COAT PAINT POLY GRAY REF: A-300 SRM 51-40-10 AND A-300 SRM 51-40-12. 2L72 4F RTA35EU 20041123000392004112300039WP 2004 11 23 DHL2004806005 120041110A3260H141003 DOWNLOCK SWITCH DOUG DC8 DC873F 302199FWP MLG FAULTY A DHLAO OTHER P NO WARNING INDICATION CLCLIMB 1 SO01806DH 46002 LEFT GEAR EXTENDED LIGHT WAS SLOW TO ILLUMINATE. WARNING HORN DID NOT SOUND WITH FLAPS 35 DEGREES SELECTED. REMOVED AND REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH & PERFORMED GEAR SWING IAW DC-8 M/M 32-60-0, OPS CHECKS SERVICEABLE P/N H14-1003. 2L74 4F RT4A25 20041123000412004112300041SO 2004 11 23 C2XA04SH552 120041115A532014521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715912 145439 DURING CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041123000422004112300042SO 2004 11 23 C2XA04TY174 120041113A532014521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714933 145018 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 22. REMOVED THE CORRODED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5320-01131 AND SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041119000372004111900037EA 2004 11 19 ASOA04782 120041007A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING A C-CHECK, THE LT AND RT IB AND OB CLIPS AT FS280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACIG THE LT AND RT IB AND OB CLIPS AT FS280. 2L72 4F4 FRTA21EA E15NE 20041119000462004111900046NM 2004 11 19 GAIA04099 120040910A5320 FITTING BOEING BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NLG UPLOCK CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NLG UPLOCK ACTUATOR FITTING, CRACKED. REF FASI NR 86355, REMOVED AND REPLACED NLG UPLOCK ACTUATOR FITTING IAW SRM 51-30-2. 2L73 4F4 F A3WE E2EA 20041119000502004111900050NM 2004 11 19 GAIA04094 120040910A5320 ANGLE BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND AFT AIR STAIR ANGLE SUPPORT BS1263, RBL25, CRACKED. REF FASI NR 86322, ACCOMPLISHED REPAIR TO AFT STAIR ACTUATOR SUPPORT ANGLE IAW SB 53-0129, FIG 3. 2L73 4F4 F A3WE E2EA 20041119000572004111900057NM 2004 11 19 AMTA200401350 120041101A5522 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE ELEVATOR DEBONDED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 RT ELEVATOR OB UPPER SURFACE DOUBLER HAS DISBONDED IN 2 PLACES. ELEVATOR STA 312.673. REPAIRED CONDUCTIVE FRAME BY BONDING IAW B757 SRM 55-20-01-1 AND BOEING DRW NR 183N2003. 2L72 4F4 FRTA2NM E12EU 20041119000622004111900062EU 2004 11 19 USAA040601 120040916A5730 ACCESS PANEL AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT WING MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW20689 0337 MISSING PANEL AND ADJACENT STRUCTURE DAMAGED. RT WING IB LOWER SURFACE BETWEEN T/E FLAP AND UNDERCARRIAGE BODY. FABRICATED AND INSTALLED PANEL. REPAIRED STRUCTURE. 2L72 4F4 FRTA46NM 20041119000642004111900064NM 2004 11 19 USAA040667 120040927A5315 FLOORBEAM BOEING767 7672B7 1385107NM GE CF6 CF680C2B2 30025NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655US 25257 FLOORBEAM BS 1480, LBL36, 5.5 INCHES X 3 INCHES, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-51. 2L72 4F4 FRTA1NM E13NE 20041119000732004111900073NM 2004 11 19 USAA040703 120040902A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 FLOOR SUPPORT, .5 INCH CRACK, DAMAGE AREA FLOORBEAM, STA727B, LBBL 8-10. MODIFIED REPAIR ANGLE IAW TR 53-10-06B, INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E21EU 20041119000762004111900076NM 2004 11 19 USAA040787 120040912A53206546812169 FLOOR SUPPORT BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT, Q5, FLOOR SUPPORT, 4 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02 FLOOR SUPPORT, STA 986.5 RT BL0. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-60-51. 2L72 4F4 FRTA16WE E2GL 20041119000772004111900077NM 2004 11 19 USAA040737 120041014A5320 CHANNEL BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 CHANNEL, .5 INCH AREA, CORROSION, BETWEEN STATIONS 345 AND 324 BL0. REPLACED FLOOR SUPPORT IAW SRM 51-10-02. 2L72 4F4 FRTA2NM E12EU 20041119000872004111900087EA 2004 11 19 ASOA04824 120041021A5210601R319801 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A C-CHECK, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. 2L72 4F4 FRTA21EA E15NE 20041119000882004111900088 2004 11 19 LNX2004F00000 420040919A3442IN812A DISPLAY SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP RADAR FAILED A LNXAO OTHER O OTHER CRCRUISE 1 SO17438MA AC721B DURING ENROUTE CRUISE FLIGHT, THE CREW NOTE SMOKE FROM THE INSTRUMENT PANEL. THE RADAR CIRCUIT BREAKER TRIPPED. THE FLIGHT DIVERTED WITHOUT INCIDENT. THE RADAR INDICATOR WAS SUBSEQUENTLY REMOVED FOR REPAIR, REINSTALLED AND RETURNED TO SERVICE. 2L72 4T3 TRTA8SW E2WE 20041119000972004111900097NM 2004 11 19 USAA040778 120041022A5312 BULKHEAD BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU38514 24996 PIT, FPBH INSP, FPBH WEB-.3750 INCH CRACK, STA 178 FWD PRESSURE BULKHEAD LT RADAR ANTENNAE MOUNT. DOUBLER INSTALLED IAW EO 53-V153, JOB CARD MK-4293801. 2L72 4F4 FRTA16WE E21EU 20041119000992004111900099NM 2004 11 19 USAA040767 120041026A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US 24552 CLT, RON, SKIN- INCH CRACK, BS727E AT STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 231. 2L72 4F4 FRTA16WE E21EU 20041119001012004111900101NM 2004 11 19 USAA040763 120041020A5330 SKIN BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US43823 23986 CLT, RON, SKIN-1.250 CRACK, BS 942 STRINGER 24L. INSTALLED DOUBLER IAW EA 95924. 2L72 4F4 FRTA16WE E21EU 20041119001052004111900105SW 2004 11 19 ALG2004F00071 120041016A5210 STRIKER BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL PILOT DOOR OUT OF ADJUST E ALGAO OTHER O OTHER HOHOVERING 1 SW03177AL 52157 CAE895744 AT A HOVER, PILOTS DOOR WILL NOT STAY CLOSED, RETURNED TO LANDING PAD. MAINTENANCE ADJUSTED PILOTS DOOR AND STRIKER PLATES IAW THE MM. NO FURTHER DISCREPANCIES NOTED. 1G71 3U3 UNCH2SW E1GL 20041119001102004111900110EA 2004 11 19 ASOA04802 120041015A5315601R3117117 CLIP CNDAIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOORBEAM CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 7608 DURING A C-CHECK, THE LT OB CLIP ON THE FLOORBEAM AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT OB CLIP ON THE FLOORBEAM AT FS 484, LBL 36 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041119001232004111900123NE 2004 11 19 GUU2004F00029 220040930A72103033260 TUBE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT AFT FERRULE CRACKED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1787554 UE227 DURING LANDING ON DECENT AT 4,000 FT, LT ENGINE LOST POWER. CREW SECURED ENGINE. REMOVED AND REPLACED TUBE ASSY P3 BLEED LINE AT LT FUEL CONTROL UNIT. OPERATION CHECK NORMAL. 2L72 4T4 TRTA24CE E26NE 20041119001242004111900124CE 2004 11 19 GUU2004F00032 120040921A55201016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178755416640 UE227 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20041119001292004111900129NM 2004 11 19 SWAA043365 120041116A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041119001312004111900131NM 2004 11 19 SWAA043344 120041115A5754654642286 SKIN BOEING737 7372H4 138448CNM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29103SW 23109 RIGHT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 5 L/E SLAT PER MM. 2L72 4F A16WE 20041119001472004111900147EA 2004 11 19 VNAA0410012 120041022A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 1 HYD SYSTEM FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL05708PS344 10160 DURING CRUISE THE CREW REPORTED A NR 1 HYDRAULIC SYSTEM HIGH TEMP CAUTION MESSAGE. TWO SECONDS LATER O/B SPLRON, O/B FLT SPLRS, O/B GND SPLRS, & HYD 1 LOW PRESS CAUTION MESSAGES WERE RECEIVED. THE CREW ELECTED TO DIVERT FLIGHT 2219 TO DAY WHERE MAINTENANCE WAS AVAILABLE. MAINTENANCE REMOVED & REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ200 AMM 29-11-01. FUNCTIONAL & LEAK TEST WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041122000052004112200005NM 2004 11 22 QXEA200400775 120041113A5310 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - FUEL PANEL 522CT HAS VARIOUS CORROSION AROUND FASTENER HOLES. REPLACED IAW HORIZON AIR WORK CART 500ME2860266. 2H72 4T RTA13NM 20041122000172004112200017 2004 11 22 SWAA043339 420041115A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR GIRT BARMISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM. 2L72 4F RTA16WE 20041122000182004112200018NM 2004 11 22 SWAA043340 120041115A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E + 3, STRINGER 23L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041122000252004112200025NM 2004 11 22 UPS04543497 120041116A5610 LATCH BOEING757 75724APF 1384969NM R2 WINDOW BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01408UP 23730 INSPECTION TYPE:N/A PILOT REPORT - R2 WINDOW DIFFICULT TO LATCH. CHECKED LATCH HANDLE OPERATION WRT MM 56-11-02-5, OPS OK. 2L72 4F RTA2NM 20041122000282004112200028NM 2004 11 22 SWAA043360 120041116A53306545765 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 500A, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041122000392004112200039NM 2004 11 22 EIA2004094 120040512A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 SKIN CRACKS AT BS 335-345, STR 3AL AND 9L. REMOVE DAMAGE, FAB AND INSTALLED REPAIR PER ECRA 470-53-165-2. 2L74 4F A20WE 20041122000452004112200045NM 2004 11 22 EIA2004141 120041105A5730 SKIN BOEING747 747273C 1384896NM CENTER WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 1180 LBL 95-100 CENTER TANK UPPER SKIN HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-270-2. 2L74 4F A20WE 20041122000462004112200046NM 2004 11 22 EIA2004142 120041105A5700 SKIN BOEING747 747273C 1384896NM CENTER WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 1200, LBL 98.5, UPPER SKIN CENTER TANK HAS CORROSION. REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-270-2. 2L74 4F A20WE 20041122000522004112200052NM 2004 11 22 04FDEA03119 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 24R AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122000542004112200054NM 2004 11 22 EIA2004126 120041011A33503004185 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 5R EMERGENCY DOOR (BUSSEL) LIGHT INOPERATIVE. REMOVED AND INSTALLED 5R EMERGENCY LIGHT, REF: MM 33-51-06, PG 401 OPS CHK NORMAL. 2L74 4F A20WE 20041122000742004112200074NM 2004 11 22 EIA2004067 120040803A3350 LIGHT BOEING747 747212B 1384886NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 EMERGENCY LIGHT OVER STAIRWELL STA 480 INOP DURING GROUND CHECK. EMERGENCY LIGHT ASSY REPLACED PER MM 33-51-00 PAGE 201 AND 501. 2L74 4F A20WE 20041122000802004112200080 2004 11 22 2004UALA01031 420041101A2565 SLIDE BOEING777 777222 1385219NM PWA PW4077PW4077 NE DOOR 2 PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29772UA 26930 ESCAPE SLIDE HAS A PUNCTURE ON LOWER INFLATION CHAMBER. PATCHED PER AIR CRUISERS CMM 25-61-32 WITH THREE INCH CIRCLE--PRESSURE TESTED, NO LEAKS. CAUSE OF PUNCTURE IS UNKNOWN. 2L72 4F4 FRTT0001SE E46NE 20041122000902004112200090NM 2004 11 22 EIA2004060 120040720A5414 SKIN BOEING747 747273C 1384896NM NR 1 PYLON GOUGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 PYLON NR 1 I/B SURFACE EXISTING REPAIR MISSING FASTNERS AND IS GOUGED AT AFT LOWER SECTION STA 221.90. REMOVED EXISTING REPAIR DOUBLER FROM PYLON NR 1 LOWER I/B SKIN. FABRICATED AND INSTALLED NEW REPAIR PER B747 SRM 51-30-02 PAGES 8, 9, 38 AND B747 SRM 54-30-03 FIG 35. 2L74 4F A20WE 20041122000912004112200091NM 2004 11 22 EIA2004051 120040719A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 25R IS CRACKED AT END CAP FITTING STA 2360 TO AFT PRESSURE BULKHEAD. REMOVED DAMAGED AREA, FABRICATED STR FILLER AND HAT SECTION. ALODINED, PRIMED AND INSTALLED STR FILLER AND HAT SECTION PER B747 SRM 53-10-03 FIG 1 PAGES 2A-4. REMOVED AND REINSTALLED OR ACCESS END CAP FITTING PER B747 SRM 51-30-02 PAGES 12-15 AT BS 2360 STR 25R. 2L74 4F A20WE 20041122001112004112200111NM 2004 11 22 04FDEA03117 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 16R, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122001212004112200121 2004 11 22 2004UALA01021 420041105A34369650976003212212COMPUTER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EGPWS MALFUNCTIONED A UALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP29365UA 24534 ABORTED TAKE OFF AT 80 KNOTS, DUE TO A WINDSHEAR ALERT. EGPWS COMPUTER WAS REPLACED. SUBSEQUENT SHOP TESTING SHOWED NO FAULTS FOUND, AND NO RECORD OF WINDSHEAR WARNING BEING GIVEN. 2L72 4F4 FRTA16WE E2GL 20041122001312004112200131WP 2004 11 22 04FDEA03124 120041116A5751ARC121053 SKIN DOUG MD10 MD1010F 3022112WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46605 LEFT WING INBOARD AILERON LOWER SKIN BILGED, (CORRODED). REMOVED LOWER INBOARD AILERON SKIN IAW DC10 SRM 57-35-01 VOL II, FABRICATED INTERNAL DOUBLERS AND SKIN IAW DAC DWG ARC1210-1 AND EA 8-5710-81531, LEFT HAND LOWER AILERON SKIN DELAMINATION. REPAIR, BONDED SKIN AND DOUBLER IAW TPS 1001, ALODINE AND PRIMED ALL PARTS IAW DC10 SRM 51-21- 01 VOL II, INSTALLED ALL PARTS IAW DC10 SRM 51-35-01 VOL II, INSTALLED ACCESS OPENING PANELS IAW DC10 SRM 51031-01 VOL II. REFERENCE NON-ROUTINE N00700. 2L73 4F RTA22WE 20041122001342004112200134WP 2004 11 22 04FDEA03019 120041104A5410ASL0046 LONGERON DOUG DC10 DC1010 3022110WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25367FE 46605 REMOVED UPPER COWL CHAFE STRIPS AND FOUND LONGERON FLANGE CHAFED AREA 2.5 INCHES LONG BY 1.5 INCHES WIDE JUST AFT OF CENTER LINE, NR 1 ENGINE RIGHT HAND COWL. REPAIRED DAMAGED LONGERON IAW FEDEX EA 8-5410-81504. 2L73 4F A22WE 20041122001382004112200138NM 2004 11 22 04FDEA02003 120040707A5347AFA7789518 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FWD CABIN, SEAT TRACK AT STA 465 - 495, APPROXIMATELY LBL 58 CORRODED. FWD CABIN, SEAT TRACK AT STA 465 TO STA 495, LBL 58 CUT AND REMOVED PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND INSTALLED PER SRM 53-70-00 FIGURE 1 VOLUME 1 AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20041122001452004112200145NM 2004 11 22 AWXA200401235 120041106A3397 CONNECTOR BRUCE BOEING737 7373Y0 1384671NM EMERGENCY LIGHT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28331AW 23747 DURING INSPECTION, THE EMERGENCY LIGHT CONNECTOR WAS FOUND BROKEN OFF INSIDE GALLEY CART AREA AT AFT GALLEY SIDEWALL. MAINTENANCE REMOVED AND REPLACED AFT GALLEY SIDEWALL EMERGENCY LIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041122001472004112200147WP 2004 11 22 04FDEA02019 120040707A5310 DOOR FRAME DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 26197 FORWARD PIT, FORWARD DOOR FRAME STATION 886 HAS CORROSION. DOOR FRAME FOUND TO BE OUT OF LIMITS. CUT AND REMOVED CORRODED FRAME SECTION, CUT WEB TO FOM. FABRICATED -15, -13 AND WEB REPAIR DOUBLER AND INSTALLED REPAIR COMPONENTS IAW DC10 SRM 51-31-01 VOL II, PERCENT 3-50-00 VOL I, 53-00-01, 51-21-01 VOL II AND 51-35-01 VOL III. FABRICATION OF FRAME SECTION ADA 0055-3 TO BE ACCOMPLISHED ON N/R 00727. FABRICATION OF -11 SPLICE ANGLE TO BE ACCOMPLISHED ON N/R N00728. REFERENCE N/R 00060. 2L73 4F RTA22WE 20041122001542004112200154WP 2004 11 22 04FDEA02904 120041011A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25392FE70219 46626 RIGHT HAND PRIMARY STATIC PORT FAILS RVSM INSPECTION FOR EXTERNAL DOUBLER MISMATCH RATIO IAW DC10 SRM 53-00-02 NOTE 2 (FIG 1 SHEET 2). REMOVED EXISTING FUSELAGE SKIN REPAIR ON FORWARD EDGE OF FORWARD CARGO DOOR CUTOUT DOUBLERS, FABRICATED NEW EXTERNAL DOUBLER, INTERIOR DOUBLER AND FILLER IAW EA8-5330-81482 AND FEDEX DC10/MD11 SRM 53-50-10 FIGURE 20. ALODINED AND PRIMED PARTS IAW DC10 SRM 51-20-01 VOLUME II. INSTALLED REPAIR IAW EA8-5330-81482 AND FEDEX DC10/MD11 SRM 53-33-01 VOLUME II. SEE NR N00531. 2L73 4F RTA22WE 20041122001572004112200157NM 2004 11 22 04FDEA01964 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.460 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.458 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0503. 2L73 4F RTA22WE 20041122001612004112200161NM 2004 11 22 04FDEA01960 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.217 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041122001632004112200163NM 2004 11 22 04FDEA01958 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.415 INCH; MATERIAL REMOVED 0.011 INCH; REMAINING THICKNESS: 0.404 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20041122001732004112200173WP 2004 11 22 04FDEA01934 120040703A5711 SPAR DOUG DC10 DC1030 3023501WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPECTION OF BUSHING IAW DAC SPM 20-30-02 AND EA 8-5710-77571. NO DEFECTS NOTED. CAD PLATING ACCOMPLISHED BY OUTSIDE VENDOR ON PO NR 448912. INSTALLED RIGHT HAND WING BUSHING STATION XW 255.000 LOWER SPAR BEAM OUTBOARD HOLE, HOLE "C", PER PAGE 9 OF 18 OF EO 8-5750-7-5000 PART 2 IAW EA 8-5710-77571. 2L73 4F A22WE 20041122001742004112200174NM 2004 11 22 04FDEA01945 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.219 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001782004112200178NM 2004 11 22 04FDEA01977 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERIAL REMOVED=0.002 INCH, REMAINING THICKNESS=0.468 INCH, AND FOUND WITHIN LIMITS AS PER DRAWING ARC0502. 2L73 4F RTA22WE 20041122001802004112200180WP 2004 11 22 04FDEA02026 120040707A2700 CONTROL CABLE DOUG MD10 MD1010F 3022112WP ZONE 200 CROSSED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25386FE 46620 AFT PIT BEHIND STATION 1967, 36 INCHES, LEFT BUTT LINE CABLES CROSSED BELOW MAIN CABIN FLOOR. OPENED CEILING PANELS AND REMOVED LEFT HAND VERTICAL ACCESS PANELS. REMOVED AND REPLACED PULLEYS AND 2 EACH CABLES, RIGGED AND OPS CHECKED GOOD, ROUTE CHECKED AND INSTALLED AND REMOVED CABLE BLOCKS IAW MD 10 MM 27-20-00 AND 20-50-02. REFERENCE N/R N00946 2L73 4F RTA22WE 20041122001842004112200184SO 2004 11 22 CHQA000586 120041121A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11261 145144 LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED THE COAT CLOSET EMERGENCY BATTERY IAW JOBCARD E33-50-04-720-001. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041122001912004112200191NM 2004 11 22 BB04089 120041116A335020121 CHARGER BOEING767 7672B7 1385107NM EMERGENCY LIGHT INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19653US 24894 CLT - FOUND LEFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. 2L72 4F RTA1NM 20041122001952004112200195EU 2004 11 22 BA04024 120041017A3350321431 BATTERY AIRBUS330 A330323 3930335EU R1 AND L4 DOORS FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19672UW 333 PHL - FOUND THE R1 AND L4 DOOR EPSU'S FAULTY. MAINTENANCE REPLACED THE BATTERY PACKS. 2L72 4F RTA46NM 20041122002142004112200214NM 2004 11 22 0402026624 120041114A3350 BATTERY BOEING747 747251B 1384892NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING LINE CHECK, FOUND ZONE 'D' AND 'E' FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20041122002162004112200216NM 2004 11 22 USA2004F00096 120040904A5610141T4800 WINDSHIELD BOEING767 767201 1385125NM GE CF6 CF680C2B2 30025NE COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19649US24331 23901 EN ROUTE, AT FL380, THE CAPTAINS WINDSHIELD CRACKED. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD. 2L72 4F4 FRTA1NM E13NE 20041122002252004112200225EU 2004 11 22 SA04105 120041110A3260848401 PROXIMITY SENSOR AIRBUSA319 A319112 3930323EU MLG FAULTY A USAAO OTHER N FALSE WARNING APAPPROACH 1 EA19765US 1371 PHL - FLT 77 ,EN ROUTE CUN - PHL, UPON LANDING GEAR EXTENSION IN PHL, RECEIVED ALL THREE GEAR DOWN UNSAFE LIGHT INDICATIONS. THE CREW RECYCLED THE LANDING GEAR AND SUBSEQUENTLY RECEIVED THREE GREEN, DOWN AND LOCKED INDICATIONS. FLIGHT CONTINUED TO LANDING WITHOUT FURTHER INCIDENT. AFTER LANDING, RECEIVED ECAM MESSAGE, "L/G DISAGREE". MAINTENANCE FOUND A FAULTY RIGHT HAND, GEAR DOOR PROXIMITY SENSOR. REPLACED THE SENSOR AND PERFORMED BITE CHECK OF LGCIU SYSTEM. ALL CHECKS OK. 2L72 4F RTA28NM 20041122002302004112200230NM 2004 11 22 EIA2004064 120040720A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STA 220-240 RT, STR 14R FOUND TO BE DAMAGED UPON REMOVAL. FABRICATED NEW STRINGER AT STR 14R FROM STA 220-240 RT PER B747 SRM 51-20-01 PAGES 11, 14-21. LOCATED DRILLED STRINGER PER B747 SRM 51-30-05 PAGE 5. ALODINED AND PRIMED STR PER B747 SRM 51-10-02 PAGES 6-7, BSOPM 21-40-02 PAGES 7-9, AND INSTALLED EAC 70-213B-02-0069. 2L74 4F A20WE 20041122002332004112200233NM 2004 11 22 EIA2004063 120040720A5313 STRINGER BOEING747 747273C 1384896NM FUSELAGE BROKEN A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 38R IS BROKEN AT STA 1000 AFT AT BATH TUB FITTING. REMOVED, FABRICATED AND REPLACED STR 38R AT STA 1000 PER SRM 53-10-03, 51-10-02, 51-10-06, 51-30-02 PAGES 2A, 2B, 3, 4, 4A, BAC 149B-147 PAGES 2-3, BAC 149B-131, AND SRM 53-11-04 PAGES 14-15. 2L74 4F A20WE 20041122002362004112200236NM 2004 11 22 USAA040714 120040911A5754 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 NR 2 SLAT, 3 INCH BY 3 INCH AREA, DELAMINATION, INBD AND OTBD ENDS LOWER SKIN. REPLACED CORE, INSTALLED DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20041122002412004112200241NM 2004 11 22 EIA2004093 120040522A5312 PRESSURE PANEL BOEING747 747273C 1384896NM NLG WW CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 NOSE WHEEL WELL SIDEWALL, LT SIDE HAS 6 INCH CRACK BETWEEN BS 264.5 AND 270.5, WL 154. REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS. INSTALLED PARTS PER B747 RM 53-10-04, FIG 116. 2L74 4F A20WE 20041122002462004112200246NM 2004 11 22 SB04129 120040920A2420BACR13CF2AB RELAY BOEING737 7374B7 1384702NM P6 PANEL UNRELIABLE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19440US 24811 CLT - FLT 1183 - FLIGHT DEPARTED CLT WITH THE NR 1 GENERATOR ON MEL 24-1. ON CLIMB-OUT, EN ROUTE TO MYR, CREW REPORTED, LOST THE LEFT TRANSFER BUSS. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT CLT. TRANSFER BUSS CAME BACK ON DURING SHORT FINAL APPROACH. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. REPLACED TRANSFER BUSS CONTROL RELAY R349 AS PRECAUTIONARY. CLEARED MEL 24-1ON NR 1 GENERATOR WITH THE REPLACEMENT OF THE NR 1 GCU. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002472004112200247NM 2004 11 22 SB04150 120041028A2121 ODOR BOEING737 7373B7 1384580NM CABIN DETECTED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19390US 23312 PIT - FLT470 - ON CLIMB-OUT FROM PIT, EN ROUTE TO ORD, THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE FORWARD GALLEY. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED ENGINE RUN, LOADED ELECTRICAL SYSTEM, OPERATED BOTH PACKS, CHECKED ALL GALLEY EQUIPMENT AND COULD NOT DUPLICATE CONDITION INDICATED. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20041122002482004112200248NM 2004 11 22 USAA040699 120041006A5315 FLOORBEAM BOEING767 7672B7 1385107NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655US 25257 FLOORBEAM, 2 INCH AREA, CORROSION, STA 278, RBL70. FABRICATED NEW (T) CAP AND SUPPORT ANGLES, REPLACED IAW SRM 53-00-51. 2L72 4F4 FRTA1NM E21EU 20041122002642004112200264EU 2004 11 22 BA04027 120041108A335032146210 POWER SUPPLY AIRBUS330 A330323 3930335EU L3 DOOR (15W) INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19674UW 342 PHL - FOUND EPSU AT THE L3 DOOR INOPERATIVE. MAINTENANCE REPLACED THE EPSU (15W). 2L72 4F RTA46NM 20041122002672004112200267NM 2004 11 22 USAA040736 120041013A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 STRINGER, 1 INCH BY 10, CORROSION, STA 640 TO 650 STRINGER 29R. REMOVED DAMAGE AND INSTALLED NEW SECTION OF STRINGER IAW SRM 53-00-03. 2L72 4F4 FRTA2NM E12EU 20041122002712004112200271NM 2004 11 22 EIA2004140 120041105A5700 SKIN BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 SKIN AT BS 1140, LBL 98.58, LBL 110 AT BUTT JOINT OVER MID SPAR HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-269-2. 2L74 4F A20WE 20041123000072004112300007NM 2004 11 23 MASA200400156 120040320A2910570347 LINE DHAV DHC8 DHC8202 2809007NM NR 2 HYD PUMP CRACKED A MASAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07456YV 456 ASH NR 7062. EGE-DEN. A/C LOST ALL HYD FLUID ON THE NR 2 HYD SYSTEM AND LANDED IN DEN. MX FOUND THE NR 2 STANDBY LINE OFF OF THE NR 2 PUMP CRACKED. MX REPLACED THE LINE, PUMP, AND INSPECTED THE EDP, AND FILTERS FOR CONTAMINATION. 2H72 4T RTA13NM 20041123000152004112300015NM 2004 11 23 SWAA043401 120041120A3350610478 BATTERY BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED RON, FOUND BOTH L1 & R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20041123000292004112300029SO 2004 11 23 C2XA04SH534 120041026A532014521700007 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 22 WAS FOUND CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041123000402004112300040 2004 11 23 DHL2004363008 420041111A3414 PITOT LINE AIRBUS300 A300B4203 3930306EU NR 1 ADC SEPARATED A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01363DH 85 DURING TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATED ON THE CAPTAIN'S AIRSPEED INDICATOR WHILE THE FIRST OFFICER'S CORRECTLY INDICATED 90KTS. TAKEOFF WAS ABORTED (293,000LBS, 90KTS, 8DEGC, NO THRUST REVERSER USED. FOUND PITOT LINE OFF OF NR 1 ADC. PERFORMED LOW LEVEL LEAK CHECK IAW A-300 M/M 34-11-10. 2L72 4F RTA35EU 20041123000442004112300044SO 2004 11 23 C2XA04IA122 120040919A2121526484 FAN EMB 145 EMB145LR 3260212SO FWD AVIONICS BURNED OUT A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW27489017180 7180 145501 HSV - FLIGHT 2184, THE CREW REPORTED A PLASTIC SMELL COMING FROM THE PACK VENTS. MAINTENANCE PLACED THE LEFT FORWARD ELECTRONIC COMPARTMENT FAN ON MEL 21-26-00 CTL 046030, AND THE AIRCRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT STL FROM FLIGHT 2035 ON 09-21-04 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED ELECTRONIC COMPARTMENT FAN, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATION. 2L72 4T RTT00011AT 20041123000452004112300045CE 2004 11 23 DXTA200400432 120041025A1420 CONNECTOR HONEYWELL RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP FUEL FILTER LOOSE E DXTAC ABORTED TAKEOFF N FALSE WARNING TXTAXI/GRND HDL 1 GL07872QS 258472 P107467 ENGINE NR 2 FUEL LIGHT CAME ON AT BEGINNING OF TAKEOFF ROLL, ABORTED TAKEOFF. REMOVED NR 2 ENG FUEL FILTER, INSTALLED NEW FUEL FILTER, SEATED FUEL FILTER CONNECTOR FULLY PERFORMED HIGH POWER RUN UP SYSTEM OPS AND LEAK CHECK GOOD AT THIS TIME. ALL ABOVE WORK DONE IAW HONEYWELL CMM 73-21-02. 2L72 4F4 FRTA3EU E6WE 20041123000472004112300047SO 2004 11 23 C2XA04IA134 120041016A3350REBC410J2000CB RELAY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT MALFUNCTIONED A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2741104 145646 IAH - FLIGHT 3272, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY AFTER LANDING ACCOMPANIED BY EMERGENCY LIGHT NOT ARMED EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAY K0275, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20041123000512004112300051NM 2004 11 23 SWAA043376 120041118A3350604222 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BATTERY PER MM. 2L72 4F A16WE 20041123000532004112300053NM 2004 11 23 SWAA043378 120041118A335007912 LIGHT BOEING737 7377H4 1384404NM GALLEY LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 FWD EEPLS STRIP NEAR FWD GALLEY LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20041123000562004112300056NM 2004 11 23 SWAA043381 120041118A5310571769 WINDOW POST BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND CAPT'S NR 1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED NR 1 WINDOW POST PER SRM. 2L72 4F RTA16WE 20041123000572004112300057NM 2004 11 23 DHL2004762005 120041109A3260H1010154 POSITION SWITCH BOEING727 7272B7 138407LNM MLG INOPERATIVE A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01762AT 22162 DURING CLIMBOUT RED UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE IN EITHER THE UP OR OFF POSITION. NORMAL DOWN INDICATIONS FOR LANDING. REPLACED NOSE GEAR POSITION SWITCH, OPS NORMAL ON GROUND IAW MM 32-61-71. 2L73 4F A3WE 20041123000582004112300058SO 2004 11 23 C2XA04SH540 120041023A534314567419401 SUPPORT EMB 145 EMB145XR 3260214SO MLG DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713118 145675 DURING C-CHECK THE LEFT MAIN GEAR FORWARD BEARING CAP WAS FOUND TO HAVE ELONGATED BOLT HOLES. REPLACED THE BEARING CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041123000642004112300064WP 2004 11 23 DHL2004801010 120041019A5250 DOOR FRAME DOUG DC8 DC873F 302199FWP COCKPIT DOOR CONTAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH 46047 COCKPIT DOOR STICKS, ALMOST IMPOSSIBLE TO GET BACK IN COCKPIT. REMOVED DEBRRIS FROM LOWER PART OF DOOR JAMB. COCKPIT DOOR OP'S CHECK OK PER DC-8 MM 52-00-00. 2L74 4F RT4A25 20041123000662004112300066NM 2004 11 23 DHL2004783013 120040831A3240 BRAKE ASSY BOEING727 727264 138408MNM MLG STICKS A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01764AT 22984 RIGHT BRAKE GRABS. BLED RIGHT SIDE BRAKES & INSPECTED. TAXIED AIRCRAFT, PER JRH 9.1 COULD NOT DUPLICATE. BRAKES CHECK GOOD IAW MM 32-41-0. 2L73 4F A3WE 20041123000672004112300067EU 2004 11 23 DHL2004362010 120040831A3350CM3270 BULB AIRBUS300 A300B4203 3930306EU EMERGENCY LIGHT INOPERATIVE A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01362DH 84 EMERGENCY EXIT LIGHT DISARM ANNUNC INOP. EMERGENCY EXIT LIGHT DISARM ANNUNC INOP. RELAMPED ANNUNCIATOR EMERGENCY EXIT LIGHT; OPS CK GOOD IN ARM AND DISARM MODES AS PER MM 33-51-00. P/N:CM3270. 2L72 4F RTA35EU 20041123000692004112300069SO 2004 11 23 C2XA04CL114 120041107A2120 SMOKE EMB 145 EMB145ER 3260211SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2717928 145007 CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECK OF THE APU AND ENGINES WITH THE BLEED AND PACKS ON. NO DEFECTS NOTED. 2L72 4F RTT00011AT 20041123000702004112300070SO 2004 11 23 C2XA04SH553 120041112A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714117 145674 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041123000712004112300071EU 2004 11 23 DHL2004363514 120040915A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, UPPER FUSELAGE, RIGHT SIDE, DENT AT FRAME 1, STRINGER 26 R. FOUND DENT OF FRAME 1 STRINGER 26 RIGHT, OIL CANNING OUT OF LIMITS PER A-300 SRM 53-11-00. MADE CUT OUT AT SKIN DAMAGED AREA IAW A-300 SRM 53-11-00 FIG 703. HFEC INSPECTED SKIN CUTOUT EDGES, FR 1 STR 26R, IAW A-300 NTM 51-31-05 AND NO CRACK INDICATIONS NOTICED. INSTALL SKIN REPAIR DOUBLER AT FUSELAGE RT SIDE AFT OF FR 1 AT STR 26 RT IAW A-300 SRM 53-11-00 FIG 703 MATERIAL USED 2024 T3 .050 AND .063 SIZE OF DOUBLER 10 X 8 INCHES. 2L72 4F RTA35EU 20041123000732004112300073SO 2004 11 23 C2XA04SH536 120041026A532014530644405 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 50. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5320-01168. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041123000742004112300074NM 2004 11 23 SWAA043382 120041118A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 665, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA. 2L72 4F RTA16WE 20041123000752004112300075NM 2004 11 23 CALA0400715 120041111A53306545774575 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2747332 23570 INSPECTION FOUND A 0.2 INCH CRACK IN LT FUSELAGE SKIN 5.6 INCH AFT OF STA 727D AT STRINGER 22L TO 23L. REPAIRED IAW ECRA 5331-01167. 2L72 4F RTA16WE 20041123000762004112300076NM 2004 11 23 CALA0400716 120041117A534769403521 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND G-1 GALLEY HOLD DOWN SEAT TRACK CORRODED AT STA 277-294.5 FROM BL 0 TO RBL 43. THE CORRODED SECTION OF TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, FIGURE 202, REPAIR 1. 2L72 4F RTA16WE 20041123000782004112300078NM 2004 11 23 CALA0400718 120041118A532065516989 SPLICE BOEING737 7373T0 1384582NM STRINGER CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND A 0.65 INCH CRACK IN STRINGER 4R SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20041123000792004112300079NM 2004 11 23 CALA0400719 120041116A3350D71701100 BATTERY PACK BOEING737 737724 13844BYNM EMERGENCY LIGHT FAILED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A FORWARD CABIN EMERGENCY LIGHT BATTERY PACK FAILED. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06-960-805. 2L72 4F RTA16WE 20041123000822004112300082NM 2004 11 23 QXEA200400776 120041116A27202379003001 REGULATOR DHAV DHC8 DHC8202 2809007NM RUDDER FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09360PH7939 5130 515 PDX - FLIGHT 2048 - AIRCRAFT RETURNED TO FIELD AFTER THE RUDDER PRESSURE CAUTION LIGHTS CAME ON DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED RUDDER DUAL PRESSURE REGULATOR AND PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS WERE GOOD, NO DEFECTS NOTED. 2H72 4T RTA13NM 20041123000832004112300083NM 2004 11 23 QXEA200400779 120041116A243023088008 GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 DC SYS INOPERATIVE A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09357PH1983 1033 504 PDX - ON FLT NR 2126, NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED DURING APPROACH. RESET PER CHECKLIST. NR 1 DC GENERATOR CAUTION LIGHT RE-ILLUMINATED DURING LANDING. RESET AGAIN PER CHECKLIST. REMOVED AND REPLACED NR 1 DC STARTER GENERATOR. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123000862004112300086CE 2004 11 23 DXTA200400385 120040908A2750 CONTROL HANDLE CESSNA500 560CESSNA 2076750CE TE FLAPS STUCK E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07320QS 5600321 DURING FLIGHT THE FLAPS DEPLOYED AT 7 DEGREES AND FLAP CONTROL LEVER IS STUCK IN POSITION. ADJUSTED FLAP PRESELECT LEVER AND OPERATIONAL CHECK GOOD, PERFORMED WORK IAW 560 CITATION MM CHAPTER 27-51-00. 2L72 4F RTA22CE 20041123000872004112300087CE 2004 11 23 DXTA200400386 120040908A3230 ARM CESSNA560 560XL 2076702CE EMERGENCY BOTTLEUNSECURE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07695QS 5605293 DURING CLIMB OUT, THE GEAR UNLOCK LIGHT CAME ON, RECYCLED GEAR AND PROBLEM DID NOT GO AWAY. ACCOMPLISHED AIR TURN BACK TO MRY. FOUND THE EMERGENCY GEAR BOTTLE ARM NOT SAFETIED AND THE ARM PARTIALLY ACTUATED SUPPLYING NITROGEN TO THE GEAR EXTEND SYSTEM. RESET GEAR BOTTLE, BLED HYDRAULIC SYSTEM AND OPERATED ALL HYDRAULIC SYSTEMS, OPERATIONAL CHECK GOOD. WORK PERFORMED IAW CHAPTER 32-01-00, 12-12-01, AND 12-13-01 OF THE CITATION 560XL MM. 2L72 4F RTA22CE 20041123000892004112300089SO 2004 11 23 C2XA04RI013 120041106A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2718982 145223 IAH - MX, DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK POSITION 3. OPERATIONAL TESTS WERE PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041123000922004112300092NM 2004 11 23 SWAA043383 120041118A53156545410366 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 665, BL 0, CRACKED. REPAIRED CHORD PER EA. 2L72 4F RTA16WE 20041123000932004112300093NM 2004 11 23 SWAA043384 120041118A53126545409 PRESSURE PANEL BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB AT BS 663.75, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA. 2L72 4F RTA16WE 20041123000942004112300094NM 2004 11 23 QXEA200400774 120041113A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09407QX 4049 PDX - FUEL PANEL 622AT HAS ALL COUNTERSINKS THAT HAVE PITTING CORROSION. REPLACED IAW WORK CARD 600ME2860267. 2H72 4T RTA13NM 20041123000972004112300097NM 2004 11 23 QXEA200400755 120041028A5320 ANGLE BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - AFT PASSENGER ENTRY DOOR SURROUND STRUCTURE LOWER SILL EDGE ANGLE HAS CORROSION ON TOP SURFACE. REPAIRED IAW HORIZON AIR EA 6-53-440 AND RD8-4-53-1037. 2H72 4T RTA13NM 20041123000982004112300098SO 2004 11 23 C2XA04TY171 120041106A33501317 BULB EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2726141 145733 DURING 4A INSPECTION, MAINTENANCE FOUND THE GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BULB AND OPS CHECK WAS GOOD IAW EMB 145XR AMM 33-50-10. AIRCRAFT RELEASED FOLLOWING THE COMPLETION OF THE SCHEDULED CHECK. 2L72 4F RT 20041123001032004112300103 2004 11 23 SWAA043400 420041119A25656557463 BRACKET BOEING737 7375H4 138449DNM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BOTH L1 DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER SRM. 2L72 4F RTA16WE 20041123001042004112300104CE 2004 11 23 DXTA200400328 120040625A3260S13771 UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAO OTHER N FALSE WARNING DEDESCENT 1 GL07953QS 7500153 DURING DESCENT & TRANSITION TO LEVEL FLIGHT, PILOT HEARD A CLUNK & FELT THIS IN THE FLOOR. THE F/O SAW A RED UNLOCK LIGHT & A GREEN NOSE GEAR LIGHT FLASH ON THEN OFF. THERE WAS NO AMBER OR RED AIRSPEED INDICATIONS, AIRCRAFT AT 340 KTS, HYDRAULICS NORMAL, LANDING UNEVENTFUL, POST FLIGHT INSPECTION OK. 2L72 4J RTT00007WI 20041123001052004112300105SO 2004 11 23 C2XA04IA139 120041106A251012315660401 HOLDER EMB 145 EMB145LR 3260212SO COCKPIT MAP SHORTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW27129004493 1997 145511 BRO - FLIGHT 2572, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST OFFICER'S CHART HOLDER LIGHT STARTED SMOKING WITH AN ELECTRICAL SHORT. MAINTENANCE DEACTIVATED THE CHART HOLDER LIGHT AND PLACED IT ON MEL 33-10-00 CONTROL 051512 CATEGORY-C AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHART HOLDER, REMOVED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041123001102004112300110NM 2004 11 23 UPS04443379 120041004A524065B100881 STOP BOEING747 747121 1384871NM L3 DOOR BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, L3 DOOR AFT NR 3 DOOR STOP FITTING FOUND BROKEN. M/D L3 DOOR AFT NR 3 STOP FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20041123001112004112300111EU 2004 11 23 DXTA200400389 120040911A2120 SMOKE BRAERO1000 BAE1251000 1500287EU CABIN DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07520QS NA1008 DURING TAXI OUT FOR A REPOSITION FLIGHT, THE AUX AND PAC WARNING LIGHT CAME ON, FOLLOWED BY THE REAR BAGGAGE SMOKE WARNING LIGHT. SMOKE BEGAN TO FILL THE CABIN AREA, PERFORMED EMERGENCY EVACUATION FOR FLIGHT CREW. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20041123001122004112300112CE 2004 11 23 DXTA200400388 120040911A32401206P27 PRESSURE SWITCH CESSNA500 560CESSNA 2076750CE BRAKE ASSY FAILED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07348QS30 5600348 DURING LANDING BRAKES FAILED COMPLETELY, EMERGENCY BRAKE SOURCE WAS USED TO STOP AIRCRAFT. REMOVED AND REPLACED PRESSURE PUMP RELAY P/N M12415602, REMOVED AND REPLACED HIGH PRESSURE SWITCH. OPS AND LEAK CHECK GOOD, BLED BRAKES AS REQUIRED, ALL WORK DONE IAW CITATION 560 MM CHAPTER 32-42-09 &32-42-00. 2L72 4F RTA22CE 20041123001132004112300113NM 2004 11 23 UPS04M43156 120040807A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 26 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM S/W & BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 26 RIGHT REMOVED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. SLEEVE BUSHING FAB PER EO MD11-5510-19409-H. APPLIED SEALANT PR142 2B1/2 & INSTALLED PER SLEEVE BUSHING AT BARREL NUT NR 26 RIGHT PER EO MD11-5510- 19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 26 RIGHT FOUND WITHIN LIMIT PER EO MD11 -5510-19409-H & EN:1287-04 & SATISFACTORY. 2L73 4F RTA22WE 20041123001142004112300114NM 2004 11 23 UPS04M43157 120040804A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 14 LEFT BARREL NUT FOUND CORRODED ON BOTTOM S/W & BEARING SURFACE. CORROSION REMOVED & REAMED TO 0974 INCH AT BARREL NUT HOLE NR 14 LEFT FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED PR1422B1/2 AT BLEND OUT AREA AT BARREL NUT HOLE NR 14 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 14 LEFT PER EO MD11-5510-19409-H & EN 1290-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123001162004112300116NM 2004 11 23 UPS04M43159 120040808A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 23 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 23 LT, REMOVED, BLENDED & REAMED TO 1.067 INCH. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H AT BARREL NUT HOLE NR 23 LEFT. REPAIR CUTOUT AT BARREL NUT HOLE NR 23 LEFT, FOUND WITHIN LIMIT PER EO MD11-5510-19409-H & EN:1289-04 & FOUND SATISFACTORY. 2L73 4F RTA22WE 20041123001172004112300117NM 2004 11 23 UPS04M43160 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 9 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2, AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 9 LEFT PER EO MD11-5510- 19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 9 LEFT PER EO MD11-5510-19409-H & EN:1 250-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123001232004112300123 2004 11 23 UPS04843503 420041114A2561 LIFE VEST DOUG DC8 DC871F 302199DWP COCKPIT TORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:N/A, F/O'S LIFE VEST WORN. REMOVED AND REPLACED F/O'S LIFE VEST. TAG# 956523. 2L74 4F RT4A25 20041123001252004112300125SO 2004 11 23 C2XA04SH550 120041109A532014532637401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715912 145439 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-22-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041123001272004112300127NE 2004 11 23 DXTA200400443 220041110A7261311960401 OIL FILTER CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENGINE MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07372QS 5600372 PCEJCO544 LEFT ENGINE EXCEEDED 95LB OIL PRESSURE WHEN COMPUTED TAKEOFF POWER SET ON TAKEOFF. REMOVED OIL FILTER AND INSTALLED NEW OIL FILTER. PERFORMED OPERATIONAL CHECK, AND LEAK CHECK. NO LEAKS NOTED. ADJUSTED THE OIL PSI REGULATOR VALVE, OPS CHECK GOOD, LEAKED CHECK OK. ALL WORK PERFORMED IAW CHAPTER 79-20-01 OF THE P&WC JT15D MM. 2L72 4F4 FRTA22CE E25EA 20041123001302004112300130GL 2004 11 23 DXTA200400433 220041028A731077878 PRESSURE SWITCH CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL FUEL FILTER DEFECTIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07949QS 7500049 CAE330049 AT POWERING UP FOR TAKEOFF THE AMBER FUEL FILTER BYPASS R CAS MESSAGE CAME ON, ABORTED TAKEOFF. TROUBLESHOT AND FOUND FUEL FILTER DPI SWITCH DEFECTIVE. REMOVED WITH NEW SWITCH. OPS CHECK AND LEAK CHECKED GOOD. WORK DONE IAW ROLLS ROYCE AE3007C MM CHAPTER 73-37-10. 2L72 4J4 FRTT00007WITE6CH 20041123001352004112300135NM 2004 11 23 UPS04M43162 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 6 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.974 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. PR1422B1/2 SEALANT APPLIED AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 6 LEFT PER EO MD11-5510-1 9409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 6 LEFT FOUND WITHIN LIMIT PER EO MD11- 5510-19409-H & EN:1254-04 FOUND SATISFACTORY. 2L73 4F RTA22WE 20041123001372004112300137NM 2004 11 23 UPS04M43170 120040926A5754ARB2850505 FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, LEFT WING LEADING EDGE NR 16 TRACK ROLLER FITTING FOUND CRACKED. LEFT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. LEFT WING LEADING EDGE NR 16 SLAT TRACK FITTING REMOVED PER SRM 51-33-01 V2.R35. NEW NR 16 ROLLER SUPPORT FITTING HOLE PICKED UP PER SRM 51-31-01 V2.R35. LEFT WING L/E NR 16 SLAT TRACK ROLLER SUPPORT FITTING REPLACED PER SRM 51-35-01 V.2 R.35. LEFT WING NR 16 SLAT TRACK INSTALLED PER AMM 27-80-32-R.50. 2L73 4F RTA22WE 20041123001382004112300138EU 2004 11 23 MALA040638 120040910A5532 SKIN SAAB SF340 340B 7860101EU STAB DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED 14 DENTS IN RT STAB TOP SKIN. DENTS ARE WITHIN ALLOWABLE LIMITS. CLUSTERS AT INBOARD AND REPAIRED IAW EO S55017. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041123001392004112300139EU 2004 11 23 MALA040646 120041002A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15451XJ 340B451 DURING 6Y/4Y INSPECTION IN BNA, NOTED DENT 20 INCHES FWD OF PAX DOOR OPENING, LT FUSELAGE SKIN. REPAIRED IAW EO S53254. AIRCRAFT RETURNED TO SERVICE 10/5/04. 2L72 4T RTA52EU 20041123001412004112300141NM 2004 11 23 0401615807 120040920A2820316N310012 FUEL LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01587NW5878 32986 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200472. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041123001422004112300142NM 2004 11 23 0401625804 120040920A2820316N310012 FUEL LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01584NW6232 32984 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200233. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041123001432004112300143NM 2004 11 23 0401595656 120040322A2820316N310012 FUEL LINE BOEING757 757251 1384970NM PWA 2037 PW2037 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01556NW7589 33392 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 56-197969. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041123001442004112300144NM 2004 11 23 0401605657 120040920A2820316N310012 FUEL LINE BOEING757 757251 1384970NM PWA 2037 PW2037 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01557NW6959 33393 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 56-199804. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041123001452004112300145NM 2004 11 23 0401583137 120040920A3250D59839 CENTERING CAM MESSIER AIRBUSA319 A319114 3930350NM NLG SHOCK OUT OF POSITION A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01337NB 1008 1685 AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR HANDLE AND RETRACT LANDING GEAR. RETURNED TO DTW AND LANDED UNEVENTFULLY. FOUND NOSE GEAR STRUT CENTERING CAM 90 DEGREES OUT OF POSITION. REALIGNED CENTERING CAM AND REASSEMBLED NOSE GEAR STRUT. SERVICED NOSE GEAR STRUT AND ACCOMPLISHED FUNCTIONAL CHECKS PER AMM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20041123001462004112300146NM 2004 11 23 0401565816 120040919A2820316N310012 FUEL LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01596NW3210 32996 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-200234. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041123001472004112300147NM 2004 11 23 0401635806 120040920A2820316N310012 FUEL LINE BOEING757 757351 1384991NM PWA 2037 PW2040 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01586NW5994 32987 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EA 58-199805. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041123001482004112300148CE 2004 11 23 DXTA200400412 120041004A3234 SELECTOR CESSNA650 650 2076802CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07791QS 6507091 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE, COULD NOT RETRACT GEAR. JACKED AIRCRAFT AND PREPARED FOR GEAR SWINGS. NOTED GEAR SELECTOR HANDLE OPERATED NORMALLY WITH AIRCRAFT IN AIR MODE. APPLIED HYDRAULIC POWER AND PERFORMED NORMAL GEAR RETRACTION WITH NO DISCREPANCIES NOTED. CONTINUED OPERATING LANDING GEAR THROUGH 5 COMPLETE CYCLES WITH NO DISCREPANCIES NOTED. 2L72 4F A9NM 20041123001492004112300149NE 2004 11 23 DXTA200400414 220041005A7200 ENGINE CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LEFT SHUTDOWN E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07322QS 5600421 WHILE BEING VECTORED FOR A VISUAL APPROACH, THE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED, FOLLOWED BY THE LEFT ENGINE UNCOMMANDED SHUT DOWN. DECLARED EMERGENCY AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E25EA 20041123001502004112300150NM 2004 11 23 UPS04243184 120040908A5330 SKIN BOEING727 727173C 1384059NM FUSELAGE DEFORMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, SKIN DEFORMATION AT STR 11R BS 1342 (RT SIDE OF NR 2 ENGINE FIREWALL). CUT OUT DAMAGED SECTION OF SKIN & PREVIOUS REPAIR DOUBLER REMOVED IAW SRM 53-30-3G FIG 3A. HFEC CARRIED OUT AROUND CUTOUT AND HOLES COMMON TO REPAIR IAW BOE 727 NDT MANUAL 51-00-00 PT 6 FIG 4 AND FIG 16, NO DEFECTS. INSTALLED REPAIR PARTS IAW SRM 53-30-03. 2L73 4F A3WE 20041123001512004112300151NM 2004 11 23 UPS04243236 120040829A5200 DOOR BOEING727 727173C 1384059NM TAIL SKID CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK AT ATTACH LUG OF TAIL SKID DOOR AND STRUT. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00. RESULT - CRACK CONFIRMED. INSTALLED NEW TAIL SKID DOOR IAW MM 32-71-61. TAIL SKID TESTED SATISFACTORY IAW MM 32-71-01. 2L73 4F A3WE 20041123001532004112300153NM 2004 11 23 UPS04243238 120040909A5710653414414 FRAME BOEING727 727173C 1384059NM CENTER WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK ON WING CENTER SECTION AT BS 775 RBL 45 ON LOWER FLANGE. HFEC CARRIED OUT IAW NDT M 51-00-00. RESULT - CRACKS CONFIRMED. FWD SECTION OF CHORD REMOVED AT BS 740 - BS 780 RBL 45 IAW 51-30-2. CENTER SECTION CHORD FWD SECTION AT RBL 45 BS 740 - 780 INSTALLED. 2L73 4F A3WE 20041123001542004112300154NM 2004 11 23 UPS04243239 120040901A5755651734757A SPOILER BOEING727 727173C 1384059NM NR 14 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, NR 14 SPOILER PANEL HAS EVIDENCE OF DELAM AT LOWER I/B CORNER. NR 14 SPOILER PANEL REPLACED IAW MM 27-61-01. 2L73 4F A3WE 20041123001552004112300155NM 2004 11 23 UPS04243240 120040903A5755659892433 ANGLE BOEING727 727173C 1384059NM NR 2 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, NR 2 SPOILER ACTUATOR SUPPORT CASTING ANGLE CRACKED AT LOWER INBOARD ATTACH POINT. REPLACED ANGLE IAW SRM 51-30-02. REINSTALLED NR 2 SPOILER ACTUATOR IAW 27-61-81. 2L73 4F A3WE 20041123001562004112300156NM 2004 11 23 UPS04243241 120040901A5752652172642 TAB BOEING727 727173C 1384059NM RT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED AT OUTBOARD UPPER TRAILING EDGE. AILERON TAB REPLACED IAW MM 27-10-19. 2L73 4F A3WE 20041123001582004112300158EA 2004 11 23 QXEA200400771 120041111A324060072941 METERING VALVE CNDAIRCL600 CL6002C10 1390015EA ZONE 700 FAILED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09607QX7912 10024 BUR - FLIGHT 2556 - THE CREW REPORTED SUBSTANTIAL LEFT BRAKE FADE UPON LANDING. THE LEFT INBOARD BRAKE FELT COLD. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE INBOARD BRAKES METERING VALVE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041122000122004112200012EA 2004 11 22 04311671 120041106A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27671BR 7572 EVENT SUMMARY STATED SMOKE INDICATION IN THE LAV/CABIN. RAN ENG AND PACKS. OPS CHECK GOOD IAW 21-51-00. INSP LAV DETECTOR AND CABIN AND LAV LIGHTS. OPS CHECK GOOD IAW 33-20-00 & 26-16-00. 2L72 4F RTA21EA 20041122000302004112200030NM 2004 11 22 UPS04443313 120040925A5411 SPAR BOEING747 747121 1384871NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, A 3 INCH CRACK WAS FOUND AT LOWER WEB AT NAC 220 OF NR 3 PYLON AT PER O/B SIDE. NR 3 PYLON NAC STA 220 O/B SIDE AFT LOWER SPAR WEB REPAIRED AS PER SRM 54-10-03 FIG 23. 2L74 4F A20WE 20041122000412004112200041WP 2004 11 22 04FDEA03135 120041117A2540 SEAL DOUG MD10 MD1010F 3022112WP ZONE 900 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 LAVATORY WASTE/TRASH CAN SEALS WORN (HAVE GAP). FOUND BY FEDEX QA. COMPLIED WITH EA 8-2540-83940, EQUIPMENT/FURNISHING, LAVATORY WASTE COMPARTMENT SEALS- REPAIR. 2L73 4F RTA22WE 20041122000592004112200059NM 2004 11 22 EIA2004086 120040902A5310 FORGING BOEING747 747121 1384871NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 LT WINDOW FORGING AND STR 22L CORROSION BETWEEN BS 360-380. REMOVE CORROSION, STRINGER 22L FOUND OUT OF LIMITS, REMOVED AND REPLACED STRINGER FROM BS 220-400 PER B747 SRM 51-30-02. 2L74 4F A20WE 20041122000632004112200063NM 2004 11 22 EIA2004073 120040902A5312 PRESSURE PANEL BOEING747 747121 1384871NM LT MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 RT WING GEAR WW PRESSURE DECK HAS SURFACE CORROSION SEVERAL AREAS BETWEEN BS 1319-1337 10 INCH INBD OF FUSELAGE SKIN. REMOVED CORROSION PER B747 SRM 51-10-01 AND 53-10-07 FOUND OUT OF LIMITS, REMOVED DAMAGE , FABRICATED REPAIR PARTS AND INSTALLED PER B747SRM 53-10-07 AND 51-30-02. 2L74 4F A20WE 20041122000642004112200064NM 2004 11 22 EIA2004074 120040902A5315 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE GOUGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 MAIN CABIN DECK FLOORBEAM DOUBLER GOUGED AT BS 460 LBL 10 TO 63 AND CORRODED. REMOVED AND REPLACED UPPER T- CHORD AT STA 460 FROM LBL10 TO RBL 112 B747SRM 53-10-07 FIG 11 AND 51-30-02. 2L74 4F A20WE 20041122000682004112200068NM 2004 11 22 EIA2004089 120040830A5313 STRINGER BOEING747 747121 1384871NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 STR 33L BS 1740 CRACKED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER B747 SRM 53-10-23 FIG 2, 53-10-03 AND 51-30-02. 2L74 4F A20WE 20041122000702004112200070 2004 11 22 2004UALA01023 420041107A3460 COMPUTER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLT MANAGE FAILED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29651UA 25389 RIGHT FMC CDU FAILED. RIGHT CDU WAS REPLACED. SHOP COULD NOT DUPLICATE CDU BLANKING DURING HOT, COLD AND VIBRATION OPERATION ON BENCH. AS A PRECAUTION, SHOP REPLACED COMPONENTS A6A2Q7, A6A2Q8, A6A2U16, A2A2U45, A2A2U48 IN CDU. THE CDU (MR40219-185) WAS REMOVED AND RETURNED TO THE SHOP. SHOP FOUND THE DISPLAY WAS DIM BUT NOT BLANK AND REPLACED THE CRT AND YOKE ASSEMBLY. 2L72 4F4 FRTA1NM E24NE 20041122000712004112200071NM 2004 11 22 EIA2004058 120040720A5340 FITTING BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 5 EA HOLES HAVE BREAK-UP CONDITION ON CENTER OF STRINGER END FITTING NR 23 AT THE END OF BS 1241 AFT 4H SIDE. REMOVED AND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGES 8-9 AT BS 1241 STR 23L. FABRICATED AND INSTALLED NEW STR NR 23L AT BS 1241-1265 PER B747 SRM 51-30-02 PAGES 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR 23L PER B747 51-30-01 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9. 2L74 4F A20WE 20041122000732004112200073NM 2004 11 22 EIA2004046 120040707A2600 WARNING LIGHT BOEING747 747121 1384871NM EXT DISCHARGE INOPERATIVE A EIAAFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09480EV 20348 NR 4 ENGINE LEFT AND RIGHT FIRE BOTTLE DISCHARGE LIGHT FAILED TO ILLUMINATE AFTER DISCHARGE BUTTON PRESSED. VERIFIED BY SQUIB TEST AT F/E PANEL. REMAIN OPEN TILL FINAL RESULTS ARE KNOWN. 2L74 4F A20WE 20041122000792004112200079NM 2004 11 22 EIA2004069 120040830A5330 SKIN BOEING747 747212B 1384886NM FUSLEAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 AFT BELLY SKIN STRINGER R51 BS 1800 CORROSION BULGE VISIBLE FROM EXTERIOR. CUTOUT BADLY CORRODED SKIN AREA. REMOVED CORROSION FROM STRINGER. DOUBLER WITHIN LIMITS IAW 53-30-03. RII INSP: ACCOMPLISHED ECI PER B747 NDT MANUAL D-6-7170, PART 6, 51-00-00 FIG 23, NO DEFECT DETECTED: LAY OUT PATTERN FOR FASTENERS, PICKED UP HOLES, FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PER SRM 53-30-03, FIG 37A. RESTORED ORIG FINISH PER 747MM 20-24-11. 2L74 4F A20WE 20041122000862004112200086NM 2004 11 22 EIA2004070 120040829A5330 SKIN BOEING747 747212B 1384886NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09486EV 20888 AFT BELLY SKIN, STRINGER R51, BS 1820. CUT OUT BADLY CORRODED SKIN, CLEANED CORROSION FROM STRINGER R51: INSIDE CUT OFF IAW SRM 53-30-03. RII: ACCOMPLISHED ECI PER B747 NDT MANUAL D6-7170, PART 6, 51-00-00, FIG 623, NO DEFECT DETECTED. LAY OUT FASTENER PATTERN, PICK UP HOLES, FABRICATE DOUBLER AND FILLER AND INSTALL REPAIR PER 747 SRM 53-30-03, FIG 37A. RESTORED ORIGINAL FINISH PER 747 MM 20-24-11. 2L74 4F A20WE 20041122000992004112200099WP 2004 11 22 04FDEA03126 120041116A5753ARC25122 HINGE DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46605 RIGHT HAND INBOARD FLAP, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, FOUND TO BE OUT OF LIMITS, FABRICATED OVERSIZE REPAIR BUSHING, INSTALLED AND HONED BUSHING IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81529, WINGS, RIGHT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE AND STRAP BLENDOUT, REPAIR. REFERENCE NON-ROUTINE. 2L73 4F RTA22WE 20041122001052004112200105WP 2004 11 22 04FDEA03132 120041116A5730ARC0585501 ACCESS PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT WING ACCESS PANEL NR 541JB HAS 4 EACH DENTS ON LOWER SURFACE. REPAIRED LEFT HAND WING ACCESS PANEL P/N ARC0585, BY FABRICATING AND BONDING NEW INNER AND OUTER SKINS, DOUBLER AND CORE IAW FEDEX EA 8-5710-81522 AND TPS 1001 REV E AND DAC PRINT ARC0585. REFERENCE NONROUTINE N00990. 2L73 4F RTA22WE 20041122001192004112200119NM 2004 11 22 2004UALA01028 120041108A5755 SPOILER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 2 VIBRATION A UALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 WP29832UA 1321 NR 2 SPOILERS APPEAR TO BE FULLY UP INTO THE AIRSTREAM CAUSING AIRFRAME VIBRATION DURING FLIGHT. THE LT AND RT NR 2 SPOILER SERVO CONTROLS WERE PREVIOUSLY DEFERRED. DEFERRAL PROCEDURE USING A SPECIAL MAINTENANCE KEY FOR SPOILER DEACTIVATION WAS FOUND NOT CORRECTLY ACCOMPLISHED. THAT CAUSED THE SPOILER SERVO CONTROLS NOT BEING IN THE OPERATIONAL POSITION, SUBSEQUENTLY CAUSING THE SURFACES FREE-FLOATING IN FLIGHT. RE-ADJUSTING THE MAINTENANCE DEVICE ON THE CONCERNED SPOILER SERVOCONTROLS TO THE OPERATIONAL POSITION FOR CONTINUAL DEFERRAL CORRECTED THE PROBLEM. 2L72 4F4 FRTA28NM E40NE 20041122001232004112200123WP 2004 11 22 AALA20041128 120041113A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21433AA 49451 DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16 COME ON WHEN THE FLIGHT ATTENDANT SWITCH IS PLACED IN ON POSITION. REPLACED BATTERY PACK B5102 FOR CABIN CEILING EMERGENCY LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F RTA6WE 20041122001282004112200128NM 2004 11 22 04FDEA03114 120041115A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 23L, AFTER CORROSION REMOVAL FOUND EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041122001302004112200130WP 2004 11 22 04FDEA03123 120041116A36101897403 PRECOOLER DOUG MD10 MD1010F 3022112WP ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46605 CRACKED, SEAL SUPPORT CHANNEL (2 PLACES) ON NR 1 ENGINE BLEED AIR PRE-COOLER, TOP INBOARD SIDE. WELD REPAIRED IAW FEDEX EA 8-5410-81536. REFERENCE NON-ROUTINE NOO409. 2L73 4F RTA22WE 20041122001332004112200133NM 2004 11 22 04FDEA02601 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.497 INCH, MATERIAL REMOVED=0.004 INCH, REMAINING THICKNESS=0.493 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041122001392004112200139NM 2004 11 22 04FDEA02004 120040707A5347A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN CABIN, SEAT TRACK AT STA 775, APPROXIMATELY LBL 8.5 CROWN WORN. MAIN CABIN, SEAT TRACK AT STA 745 TO STA 785, LBL 8.5. REMOVED PER SRM 51-33-01 VOLUME I. NEW SEAT TRACK SPLICE FABRICATED AND INSTALLED PER SRM 53- 70-00 FIGURE 1 VOLUME I AND SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20041122001562004112200156NM 2004 11 22 04FDEA01965 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.222 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001642004112200164NM 2004 11 22 04FDEA02926 120041012A5713ARB75111 STRINGER DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 LEFT HAND WING UPPER STRINGER (S11) END FOUND CRACKED AT INSIDE ACCESS PANEL 536CB. REPAIR CARRIED OUT AT LT WING STRINGER 11 AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS PER SRM51-33-01 VOL II AND SRM 57-20-00 FIG 10 VOL I. 2L73 4F RTA22WE 20041122001652004112200165EU 2004 11 22 AWXA200401210 120041029A5210FE174004 DAMPER AIRBUS320 A320231 3930325EU L-1 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, THE L-1 DOOR ASSIST DAMPER PRESSURE WAS LOW. MAINTENANCE REMOVED L-1 DOOR ASSIST DAMPER PERCUSSION MECHANISM AND REPLACED TWO EACH PACKINGS. REINSTALLED L-1 DOOR ASSIST DAMPER IAW A320 AMM 52-10-00, LEAK AND OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041122001682004112200168EU 2004 11 22 AWXA200401213 120041018A5320D53475777206 GUSSET AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SPLICE PLATE (GUSSET) AT LOWER AFT CORNER OF DOOR CUTOUT FS 62. MAINTENANCE REMOVED CORRODED PLATE GUSSET Y1492 RT, FS 62; FABRICATED A NEW REPLACEMENT PLATE GUSSET; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041122001752004112200175NM 2004 11 22 04FDEA01974 120040706A5753ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.217 INCH, AND REPAIRED AS PER EA NR 1-5740-76786, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041122001792004112200179WP 2004 11 22 04FDEA02025 120040707A5730 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25386FE 46620 RIGHT HAND WING TRAILING EDGE INBOARD LOWER PANEL NUMBER 641 BB HAS NUMEROUS DENTS IN ITS UPPER SURFACE. REPAIRED BY FABRICATING AND BONDING NEW METAL OUTER SKIN, CORE, INNER SKIN AND INNER DOUBLER IAW TPS 1001 REV E AND DWG ARC 2067 AND EA 8-5710-77592. REFERENCE N/R N00699. 2L73 4F RTA22WE 20041122001822004112200182NM 2004 11 22 04FDEA02028 120040708A5312AEA76211 PRESSURE PANEL DOUG MD11 MD11F 3023600NM ZONE 100 CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 FUSELAGE OIL CANNING FOUND ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470. FUSELAGE, MAXIMUM DEPTH OF THE OIL CANNING ON CENTER LANDING GEAR WHEEL WELL LEFT VERTICAL WEBS FROM STA 1394.5 TO STA 1470 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLUME 1. FEDEX EA NR 1-5330-76794 WAS ISSUED FOR TRACKING AND REPETITIVE INSPECTION 2L73 4F RTA22WE 20041122001972004112200197NM 2004 11 22 SB04146 120041017A33501012623 LIGHT BOEING737 7373B7 1384580NM MID CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19390US 23312 CLT - PILOT REPORTED THE EMERGENCY EXIT ROW EVACUATION LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002062004112200206NM 2004 11 22 USAA040730 120041007A5310 SHEAR TIE BOEING757 757225 1384959NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU 22193 SHEAR TIE, 2 INCH SQUARE, CORROSION, STA 1280 BETWEEN STRINGERS 29R, 28R. FABRICATED AND REPLACED PARTS IAW MFG DRWG 146N2006. 2L72 4F4 FRTA2NM E21EU 20041122002082004112200208NM 2004 11 22 SB04127 120040919A335020131A BATTERY BOEING737 7374B7 1384702NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS, AT CABIN SEAT ROWS 12 THROUGH 19, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY ASSEMBLY M1136. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002102004112200210NM 2004 11 22 USAA040777 120041022A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19779AU38514 24996 PIT - RON, SKIN WITH .5000 INCH CRACK, FWD STA 380 BETWEEN STR 28R AND BL0. INSTALLED DOUBLER IAW EA 79322. 2L72 4F4 FRTA16WE E21EU 20041122002152004112200215WP 2004 11 22 0402019760 120041104A3222 STRUT DOUG DC9 DC941 302207NWP NLG DISCHARGED A NWAAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 GL01760NW 47288 AT ABOUT 3,000 FEET DURING CLIMB-OUT, CREW COULD NOT COMPLETE THE UPLATCH CHECK. COM PROCEDURES COMPLIED WITH AND AFTER NUMEROUS GEAR OPERATION AND INDICATION PROBLEMS, THE AIRCRAFT LOST PRESSURIZATION AT 13,000 FEET. PER A FILED ASR, THE CREW DECLARED AN EMERGENCY, DESCENDED TO 10,000 FEET, AND RETURNED TO DTW. CABIN OXYGEN MASKS DID NOT DEPLOY AND THE LANDING WAS UNEVENTFUL. MAINTENANCE RESERVICED THE NOSE LANDING GEAR STRUT AND ADJUSTED THE GEAR DOOR LATCH MECHANISM ROLLER ASSEMBLY TO HOOK CLEARANCE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041122002192004112200219NM 2004 11 22 USAA040706 120040921A5551 FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 PIT - Q2, R-1 LUG .1250 BY .2500 INCH AREA, CORROSION; NO LEVEL OR TASK, RT HORIZ STAB R-1 LUG. CLEANED CORROSION, REMOVED AND REPLACED BUSHING, CAB PLATED IAW SRM 55-10-10, NDTM 0-4-53-10. 2L72 4F4 FRTA16WE E21EU 20041122002202004112200220EU 2004 11 22 USA2004F00097 120040529A335032145410 EPSU AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE EMERGENCY LIGHT FAULTY A USAAO OTHER L NO TEST NRNOT REPORTED 1 EA19757UW6634 1342 THE EMERGENCY LIGHTS FAILED THE TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. SYSTEM CHECKS, OK. 2L72 4F4 FRTA28NM E37NE 20041122002282004112200228NM 2004 11 22 EIA2004047 120040710A3350 SIGN BOEING747 747212B 1384886NM PAX DOOR INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09485EV 20712 UPPER DECK DOOR EXIT SIGN INOP (WILL NOT ILLUMINATE) DEFERRED PER MEL 33-15. 2L74 4F A20WE 20041122002292004112200229NM 2004 11 22 EIA2004062 120040720A5320 FITTING BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 4 EA HOLES HAVE BREAKUP CONDITION ON CENTER OF STRINGER END FITTING NR 23 AT THE BS 1241 AFT RT SIDE. REMOVED AND INSTALLED NEW END FITTING PER B747 SRM 51-30-02 PAGE 8-9 AT BS 1241 STR NR 23R. FABRICATED AND INSTALLED NEW STRINGER NR 23 RT STA 1241 PER B747 SRM 51-30-02 PAGES 8-9. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB AT BS 1241-1258 STR, 23R PER B747 SRM 51-30-02 PAGES 2-3 AND B747 SRM 51-30-02 PAGES 8-9, REPLACED STR 23 AT BS 1241-1265 RT. 2L74 4F A20WE 20041122002392004112200239NM 2004 11 22 EIA2004133 120041014A5230 SKIN BOEING747 747273C 1384896NM CARGO DOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 AFT LWR CARGO DOOR, 3RD LWR ACCESS PANEL, INNER SKIN CORRODED. REMOVED DAMAGE AND REPAIRED PER ECRA 470-52-240-2. 2L74 4F A20WE 20041122002452004112200245 2004 11 22 SA04100 420041025A2330RDAX443110 ELECTRICAL BOX AIRBUSA321 A321211 3930370EU SEAT OVERHEATED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19172US 1472 LAX - A PASSENGER DETECTED SMOKE AND AN ELECTRICAL ODOR AT ROWS 17-21, ON BOTH LEFT AND RIGHT SIDES OF THE CABIN. AT THE SAME TIME, AUDIO OF THE IN FLIGHT ENTERTAINMENT (IFE) SYSTEM FAILED. POWER WAS REMOVED FROM THE IFE SYSTEM AND THE SMOKE AND ODOR WENT AWAY. MAINTENANCE PLACED SYSTEM ON MEL. DURING TROUBLESHOOTING, FOUND THE ROW 17 DEF SEAT ELECTRONICS BOX (SEB) WITH SIGNS OF OVERHEATING AT CONNECTOR J1. MAINTENANCE REPLACED THE SEB. THE SYSTEM WAS STILL INOPERATIVE. DURING LATER TROUBLESHOOTING, REPLACED THE IFE CABLE BETWEEN ROWS 16 AND 17 ON THE RIGHT SIDE. SYSTEM OPS CHECKED OK. 2L72 4F RTA28NM 20041122002512004112200251NM 2004 11 22 USAA040786 120041029A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT - Q5, FLOOR SUPPORT, .1250 INCH BY .1250 INCH AREA, CORROSION; LEVEL 1; TASK NRC53-107-02, FASTENER HOLE AT STA 947 RBL 20. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, SHIM AND FILLER IAW EA 79192. 2L72 4F4 FRTA16WE E2GL 20041122002622004112200262NM 2004 11 22 EIA2004145 120041106A5310 STRUCTURE BOEING747 747273C 1384896NM MLG WW CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 1480 MCD, CORROSION ON WHEEL WELL CHORDS AND STRIP, LBL 98-0 - LBL 57.5, AND LBL 35.0 - RBL 21.0. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-215-2PL. 2L74 4F A20WE 20041123000062004112300006 2004 11 23 DXTA200400454 420041120A2210 AUTOPILOT SYS CESSNA750 750 2076810CE COCKPIT MALFUNCTIONED E DXTAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL07939QS 7500193 DURING GO AROUNDS (AFTER A COUPLE APPROACHES) THE AUTO-PILOT DISENGAGED MULTIPLE TIMES AFTER IT WAS RE-ENGAGED IN STABILIZED CLIMB/LEVEL OFF AND IN LEVEL FLIGHT. ON SECOND MISSED APPROACH BOTH FMS UNITS FAILED FOR ABOUT 30 SECONDS ALONG WITH THE AUTO-PILOT DISENGAGEMENT. DOWNLOADED EICAS LIMIT FILES FOR TEAM X TO REVIEW 11/20 NO FAULTS LOGGED ALL SYSTEMS CHECK NORMAL. MAINTENANCE CONTROL REQUEST ANOTHER OCF FOR GO AROUND WITH AVIONICS TECH ALONG TO GATHER MORE INFO. ALL WORK ACCOMPLISHED I/A/W CE-750 M/M CHAPTER 22-10-02. 2L72 4J RTT00007WI 20041123000132004112300013NM 2004 11 23 ASAA0410409 120040929A53306545767541 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 STRINGER 14L AT BS 500-540 REQUIRES REWORK TO CHANGE SHIMMING REQUIREMENTS. REMOVED EXISTING REPAIR, FABRICATED -7, -6, AND -2 DOUBLER`S AND REINSTALLED. 2L72 4F4 FRTA16WE E2EA 20041123000172004112300017SO 2004 11 23 C2XA04BT115 120041030A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715941 145035 CREW REPORTED, EMERGENCY EXIT LIGHT INVERTER INTERMITTENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041123000272004112300027SO 2004 11 23 C2XA04CL101 120041006A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713965 145125 CLE FLIGHT 3292 - THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20041123000492004112300049EU 2004 11 23 DHL2004363501 120040921A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, N/R 5678, MAIN CABIN SEAT TRACK HAS CORROSION LBL 20 FR 17. REMOVED CORROSION AT MAIN CABIN SEAT TRACK AT FR 17 LBL 20 IAW A-300 SRM 51-40-11 PG 1. FOUND AREA TO BE OUT OF LIMITS IAW A-300 SRM 53-10-00. REMOVED SEAT TRACK FOR REPAIR IAW A-300 SRM 53-10-10. INSTALLED SEAT TRACK ACCOMPLISHED ON N/R 3879 P/N 60-22457, P/O 24302234. 2L72 4F RTA35EU 20041123000522004112300052NM 2004 11 23 SWAA043377 120041118A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN OVERHEAD INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20041123000542004112300054NM 2004 11 23 SWAA043379 120041118A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW BN1089 23939 DURING SCHEDULED C2 CHECK, FOUND LT WING T/E OUTBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED LT FORE FLAP PER MM. 2L72 4F RTA16WE 20041123000722004112300072NM 2004 11 23 DHL2004745020 120040901A3350 BATTERY BOEING727 727224 1384076NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 EMERGENCY EXIT LIGHTS WOULD NOT COME ON DURING STBY POWER CHECK. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT BATTERY IAW B727 MM 33-50-101, OPS CHECKED GOOD. 2L73 4F A3WE 20041123000802004112300080NM 2004 11 23 QXEA200400745 120041114A33506104781 BATTERY DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHT INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH17875114 513 SEA - FORWARD CABIN OVERHEAD EMERGENCY LIGHT, FORWARD RIGHT HAND EMERGENCY LIGHT AND RIGHT HAND OUTSIDE EMERGENCY LIGHT ARE ALL INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PS2. ALL EMERGENCY LIGHTS OPERATIVE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123000812004112300081NE 2004 11 23 AT0400023 220041110A7200BR700715A130 ENGINE BOEING717 717200 1383700NM RROYCEBR700 BR700710A110 NE NR 2 FAILED A ZZDAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 SO15945AT 55008 ENGINE FAILURE ON CLIMBOUT, LOUD BANG. ENGINE RPM LOW, RUNAWAY TGT, STARBOARD ENGINE. REMOVED AND REPLACED NR 2 ENGINE. 2L72 4F4 FTRA6WE E00057EN 20041123000842004112300084CE 2004 11 23 DXTA200400416 120041005A28218975131 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 2 ENGINE ACTIVATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07811QS 258614 P107774 ENG 2 FUEL ANNUNCIATOR LIGHT CAME ON DURING TAKEOFF ROLL. REPLACED THE NR 2 FUEL FILTER IAW TFE-731-5 HONEYWELL LMM CHAPT 73-21-02, LEAK CHECK GOOD. 2L72 4F4 FRTA3EU E6WE 20041123000912004112300091NM 2004 11 23 SWAA043403 120041120A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND BS 188 STUB FRAMES CRACKED AT STR 17L & STR 17R. REMOVED AND REPLACED FRAMES PER SRM. 2L72 4F RTA16WE 20041123000992004112300099EA 2004 11 23 QXEA200400766 220041113A7200312162701 ENGINE BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 500 LEAKING A QXEAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09408QX6320 2309 4050 PCEFA0102 PDX FLIGHT 2410 FLIGHT ATTENDANTS REPORT A STRONG ODOR LIKE DIRTY SOCKS IN CABIN WHILE IN DESCENT. NOTICED IN COCKPIT A LITTLE BIT OF ODOR AS WELL. MAINTENANCE REPLACED THE ENGINE FOR STATICLY LEAKING. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20041123001012004112300101NM 2004 11 23 SWAA043404 120041120A53216545833 WEB BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOOR WEBS CRACKED AT BS 188 TO BS 196, STR 17L & STR 17R. REPAIRED WEBS PER SRM. 2L72 4F RTA16WE 20041123001022004112300102SO 2004 11 23 C2XATY172 120041106A3350P2070011100 FLASHLIGHT EMB 145 EMB145XR 3260214SO COCKPIT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2726141 145733 DURING 4A INSPECTION, MAINTENANCE FOUND THE EMERGENCY FLASH LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY FLASH LIGHT AND OPS CHECK WAS GOOD IAW EMB 145XR AMM 33-50-10. AIRCRAFT WAS RELEASED FOLLOWING THE SCHEDULED INSPECTION. 2L72 4F RT 20041123001062004112300106NM 2004 11 23 UPS04443315 120040929A5720 FITTING BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, RIGHT BS 1241 WL 180 UPPER WING SPLICE PLATE FITTING NR 5 FASTENER HOLE CRACK REVEALED RUNNING AFT HOLE CRACK EXCEED EO LIMIT. REF NRC 6676 FOR REPLACEMENT OF SPLICE PLATE. 2L74 4F A20WE 20041123001182004112300118NM 2004 11 23 QXEA200400769 120041113A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT PAX DOOR JAMMED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09416QX2319 4083 BIL - FLIGHT 2411 - CREW REPORTS THE AFT CABIN DOOR IS JAMMED. MAINTENANCE INSPECTED THE DOOR AND FREED THE SAME. SEVERAL OPERATIONAL CHECKS WERE PERFORMED AND ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123001192004112300119NM 2004 11 23 QXEA200400770 120041111A2750C1486561 POWER UNIT BOMBDRDHC8 DHC8401 1390041NM ZONE 200 FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09403QX6305 4037 PDX - FLIGHT 2309 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED A FLAP DRIVE CAUTION DURING CLIMB. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLAP POWER UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123001262004112300126SO 2004 11 23 C2XA04SH549 120041109A532014532636401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715912 145439 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041123001292004112300129CE 2004 11 23 DXTA200400435 120041029A215073838415 ACM CESSNA650 650 2076802CE CABIN COOLING LEAKING E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07790QS1005 6507090 WHEN APU BLEED AIR VALVE SWITCH IS TURNED ON HOT NOXIOUS AIR RUMBLES INTO CABIN AT AN OVER COMPENSATING RATE. REMOVED LEAKING PAX ACM AND INSTALLED AN OVERHAULED UNIT, REMOVED 2 COALESCER SOCKS AND INSTALLED 2 NEW SOCKS. LEAK CHECK GOOD, ALL WORK PERFORMED IAW CE650 MM CHAPTER 21-50-01. 2L72 4F A9NM 20041123001312004112300131CE 2004 11 23 DXTA200400436 120041029A3260 CONNECTOR CESSNA650 650 2076802CE CENTER SWITCH LOOSE E DXTAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL07779QS 6507079 LANDING GEAR WOULD NOT RETRACT, GEAR HANDLE WOULD NOT MOVE. TROUBLESHOT AND FOUND CONNECTOR (PN2) LOOSE ON NOSE WHEEL OFF CENTER SWITCH CONNECTOR. RE-SECURED CONNECTOR AND PERFORMED A GEAR SWING IAW CITATION 650 MM 32-30-00, OPS CHECK GOOD. 2L72 4F A9NM 20041123001322004112300132NM 2004 11 23 UPS04M43161 120040817A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 4 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED BLEND & REAMED TO 0.974 INCH AT BARREL NUT HOLE NR 4 RIGHT FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 4 RIGHT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 4 RIGHT FOUND WITHIN LIMIT PER EO MD11-5510-19409-H & EN:1303-04 FOUND SATISFACTORY. 2L73 4F RTA22WE 20041123001332004112300133CE 2004 11 23 DXTA200400431 120041023A3260327 BULB CESSNA500 560CESSNA 2076750CE MLG INDICTOR BURNED OUT E DXTAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL07335QS 5600335 RIGHT MAIN GEAR INDICATOR LIGHT INOP, EMERGENCY/ABNORMAL CHECKLIST ACCOMPLISHED. PERFORMED TROUBLESHOOTING AND RAN LANDING GEAR WILL NOT EXTEND CHECKLIST, FOUND THE MLG LIGHT BULBS BURNED OUT. REMOVED AND REPLACED RIGHT MAIN GEAR INDICTING LIGHT IAW CESSNA CE-560 MM 33-11-01. 2L72 4F RTA22CE 20041123001342004112300134CE 2004 11 23 DXTA200400429 120041021A21301103P0912 PRESSURE SWITCH CESSNA750 750 2076810CE CABIN PRESSURE MALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07970QS 7500070 DURING TAKEOFF ROLL THE RIGHT HP DUCT OVERPRESSURE WARNING LIGHT CAME ON, ABORTED TAKEOFF. REMOVED & INSTALLED A NEW RT OVER PRESSURE SWITCH IAW CESSNA-750 MM CHAPTER 36-11-00. OPS AND LEAK CHECKED GOOD. 2L72 4J RTT00007WI 20041123001572004112300157NM 2004 11 23 UPS04243242 120040905A5330 LAP JOINT BOEING727 727173C 1384059NM FUSELAGE SKIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, RIVETS PULLED BETWEEN BS 810-830 STR 4L, CORROSION AT LAP JOINT OUT OF LIMITS IAW SRM 53-30-1. CORRODED SKIN TRIMMED OUT. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-30-1. 2L73 4F A3WE 20041123001592004112300159 2004 11 23 UPS04143132 420040917A2565 WARNING LIGHT AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE ILLUMINATED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01156UP 0845 DURING CLIMB, THE MAIN ENTRY DOOR SLIDE PRESSURE WARNING LIGHT AND ALARM SOUNDED. EMERGENCY SLIDE WAS DISARMED AND WARNING LIGHT AND ALARM WERE SILENCED. PERFORMED OPERATIONAL TEST ON EMERGENCY ESCAPE SLIDE WARNING OF THE MAIN ENTRY DOOR PER M/M 52-73-00-5. OPS CHECK GOOD. 2L72 4F RTA35EU 20041123001602004112300160NM 2004 11 23 0401855518 120041005A5340 FITTING BOEING757 757251 1384970NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01518US 23206 DURING H-CHECK FOUND CRACK IN FITTING ON AFT SIDE OF FRAME AT BS 1681 S13R. REPAIRED PER EA 55-201106. 2L72 4F RTA2NM 20041123001642004112300164NM 2004 11 23 UPS04443475 120041031A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, U/D BS 330 RBL 61 FLOORBEAM UPPER CHORD FOUND CRACKED AS MARKED. U/D - BS 330 RBL 58 TO MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F RTA20WE 20041123001672004112300167WP 2004 11 23 UPS04843472 120041110A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT STUCK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 INSPECTION TYPE:N/A CAPT'S L2 WINDOW WILL NOT OPEN. UPPER WINDOW FRAME LOCK BAR STUCK WOULD NOT RELEASE. CLEANED & LUBRICATED MECHANISM. OPS CHECK NORMAL IAW MM 56-10-03-5. 2L74 4F RT4A25 20041123001682004112300168NM 2004 11 23 UPS04M43471 120041111A3411 COMPUTER DOUG MD11 MD11F 3023600NM PITOT STATIC SYSFAILED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01251UP 48744 INSPECTION TYPE:N/A SHORTLY AFTER TAKEOFF LOSS OF ACCURATE AIRSPEED AND ALTITUDE, VERTICAL SPEED, HEADING AND COURSE GUIDANCE. SAI ALL FAIL, YAW DAMP ALL FAIL LEVEL TWO ALERTS ALSO DISPLAYED. NUMEROUS OTHER ALERTS DISPLAYED. COMPLIED WITH ERRATIC AIRSPEED LOSS CHECKLIST AND LANDED. ATB TO ONT. CLEANED DEBRIS FROM NR 1 PITOT TUBE. REPLACED NR 1 CADC PER MM 34-16-01, TEST GOOD. ACCOMPLISHED PITOT STATIC LEAK CHECK PER MM 34-11-00, TEST GOOD. 2L73 4F RTA22WE 20041123001692004112300169 2004 11 23 UPS04843088 420040910A256551561004DGDME SLIDE DOUG DC8 DC871F 302199DWP PAX DOOR DEPLOYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:N/A ESCAPE SLIDE DEPLOYED WHILE ATTEMPTING TO CLOSE MAIN ENTRY DOOR. REF M287491. REPLACED SLIDE AS PER MM 25-60-02-2, S/N INSTALLED 36-22 THIS CLEARS M287491. 2L74 4F RT4A25 20041123001722004112300172EA 2004 11 23 COMA0460605 120041108A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 LEFT HAND CARGO FLOOR ANGLE FS 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041123001742004112300174NM 2004 11 23 SWAA043324 120041112A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND SKIN AT BS 530, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041123001752004112300175 2004 11 23 SWAA043325 420041112A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041123001762004112300176 2004 11 23 SWAA043326 420041112A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE BROKEN. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041123001772004112300177NM 2004 11 23 SWAA043327 120041112A5753 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29627SW 1628 27935 DURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E FLAP PER MM. 2L72 4F RTA16WE 20041123001792004112300179CE 2004 11 23 DXTA200400405 120040924A324631418 WHEEL CESSNA650 650 2076802CE MLG DEPARTED E DXTAO OTHER D INFLIGHT SEPARATION TXTAXI/GRND HDL 1 GL07785QS 6507085 AFTER LANDING, DURING TAXI ROLL OUT THE NOSE WHEEL ASSEMBLY DEPARTED THE AIRCRAFT. AIRPLANE CAME TO A COMPLETE STOP ON NOSE STRUT. ACCOMPLISHED HIGH DRAG SIDE LOAD AND FOD INSPECTION IAW CE650 MM CH 5-50-00, FOUND LT MAIN LANDING GEAR TAXI LIGHT DAMAGED. REMOVED DAMAGED FORK AND PISTON ASSEMBLY, REBUILT LOWER BARREL ASSY, INSTALLED NEW FORK AND PISTON INTO UPPER BARREL IAW CESSNA 650 CMM CHAPTER 32-20-01. INSTALLED NEW WHEEL ASSEMBLY AND SERVICED NLG STRUT IAW CESSNA 560 MM 12-10-38, GEAR SWING COMPLETED IAW CESSNA 650 MM CHAPTER 32-30-00. 2L72 4F A9NM 20041123001802004112300180CE 2004 11 23 DXTA200400406 120040914A3230 ROLLER CESSNA750 750 2076810CE LANDING GEAR OUT OF ADJUST E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07989QS BMC098 7500089 PASSING FL340 CLIMBING TO FL410 EXPERIENCED A LOUD THUMP WITH A NOTICEABLE AIRCRAFT SHIMMY, GEAR UNLOCK LIGHT ILLUMINATED AND REMAINED ON UNTIL DESCENDING THROUGH FL150. DURING DESCENT ANOTHER BUMP AND SHIMMY LIGHT WENT OUT, GEAR EXTENDED NORMALLY FOR LANDING. COMPLIED WITH GEAR SWING AND FOUND NOSE GEAR UPLOCK ROLLER NOT MAKING PROPER CONTACT WITH UPLOCK SWITCH. MEASURED NOSE STRUT EXTENSION AND FOUND TO BE OVER LIMITS. REMOVED AND REPLACED NOSE STRUT ASSEMBLY. COMPLIED WITH GEAR SWING AND FUNCTIONAL CHECKS, TAXI CHECK FOR STEERING. ALL CHECKS SATISFACTORY IAW CESSNA 750 MM CHAPTER 32-30-00. 2L72 4J RTT00007WI 20041123001822004112300182NM 2004 11 23 UPS04243396 120041004A5310 FITTING BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C, TO GAIN ACCESS FOR NDT PLEASE REMOVE FASTENERS BETWEEN STR 23 & 24 BS 740 FITTING RIGHT. REMOVED FASTENERS IAW SRM 51-30-02. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED, ENDS MARKED. REF UPS EO B727-5310-7477-E FOR FITTING REPLACEMENT. 2L73 4F A3WE 20041123001832004112300183EA 2004 11 23 COMA0460602 120041108A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 LEFT FS 718 FRAME CRACKED. REPAIRED IAW SB 601R-53-055. 2L72 4F RTA21EA 20041123001842004112300184EA 2004 11 23 COMA0460603 120040916A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01965CA 7131 FS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584. 2L72 4F RTA21EA 20041123001862004112300186CE 2004 11 23 DXTA200400336 120040712A3260 BULB CESSNA500 560CESSNA 2076750CE MLG INDICATOR INOPERATIVE E DXTAA UNSCHED LANDING P NO WARNING INDICATION DEDESCENT 1 GL07800QS 5600598 RIGHT GEAR POSITION INDICATOR LIGHT SEEMS INOPERATIVE, ROTARY TEST IN FLIGHT SHOWED ONLY TWO GREEN LIGHTS. NO GEAR HORN BELOW 150 KTS UNDER 70 PERCENT N2. TROUBLESHOT SYSTEM, FOUND LIGHT & BULBS TO BE INOP. REMOVED AND REPLACED BULBS, OPERATIONAL CHECK GOOD. ALL WORK PERFORMED IAW 560 MM SECTION 33-10-00. RESET EMERGENCY BLOW DOWN BOTTLE AND SERVICED AS NECESSARY, PLACED AIRCRAFT ON JACKS AND PERFORMED SEVERAL GEAR RETRACTION, ALL CHECKED GOOD. REMOVED AIRCRAFT FROM JACKS, ALL WORK DONE IAW CESSNA 560 MM SECTION 32-31-08. 2L72 4F RTA22CE 20041123001902004112300190NM 2004 11 23 UPS04443380 120040923A571265B078466 RIB BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, RIGHT WING L/E OLES 1421 NR 25 VC FLAP I/B ROTARY O/B SUPPORT RIB FWD MOUNT HOLE CRACKED. SUPPORT RIB REPLACED AS PER SRM 51-10-01 PG 8. NR 25 VC FLAP REF MM 27-81-02 RIGGING & OPERATION CHECK CUTOUT PER MM 27-81-00. 2L74 4F A20WE 20041123001922004112300192NM 2004 11 23 UPS04443388 120040928A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, CRACK REVEALED ON RIGHT BS 1241 FUSELAGE SKIN AT ONE EA HOLE AREA BS 1241, WL 170 TO 180. BS 1241 RIGHT FX SKIN REPAIRED AS PER SRM 53-30-03 FIG 59. 2L74 4F A20WE 20041123001932004112300193NM 2004 11 23 UPS04443389 120040928A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, CRACK REVEALED ON LEFT BS 1241 FUSELAGE SKIN AT TWO EA HOLES. LT BS 1241 FUSELAGE SKIN REPAIR AS PER SRM 53-30-03 FIG 59. 2L74 4F A20WE 20041123001942004112300194NM 2004 11 23 SWAA043276 120041109A55526959227 BUSHING BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW 26598 DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED TAB FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM. 2L72 4F RTA16WE 20041123001962004112300196NM 2004 11 23 UPS04M43293 120040802A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 31 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 31 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.178 FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 31 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 31 LEFT PER EO MD11-5510-19409-H & EN 1292-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123001972004112300197NM 2004 11 23 UPS04M43296 120040801A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 20 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 20 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 20 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 20 RIGHT PER EO MD11-5510-19409-H & EN 1284-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123002002004112300200NM 2004 11 23 SWAA043268 120041109A52106951337 PIN BOEING737 7377H4 1384404NM L1 DOOR MIGRATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29432WN 33715 FWD ENRTY DOOR WOULD NOT OPEN. REMOVED AND REPLACED FWD ENTRY DOOR GUST LOCK PIN PER MM. 2L72 4F RTA16WE 20041123002062004112300206NM 2004 11 23 SWAA043286 120041110A53306545766 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 934, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F A16WE 20041123002072004112300207NM 2004 11 23 UPS04243403 120041004A5340 TERMINAL BOEING727 727185C 138406NNM TAIL SKID BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, TAIL SKID BAY STABILIZING LINKS UPPER AND LOWER LEFT AFT TERMINALS CRACKED AND LOWER AFT RIGHT TERMINAL CRACKED. INSTALLED NEW UPPER AND LOWER LEFT AFT TERMINALS ON TAILSKID BAY, FABRICATED LOWER AFT RIGHT TERMINAL AND FITTED IAW SRM 51-30-2. 2L73 4F A3WE 20041123002092004112300209NM 2004 11 23 UPS04243406 120041005A5230 BRACKET BOEING727 727185C 138406NNM FWD CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, FWD CARGO DOOR BRACKETS CRACKED AT UPPER AFT HINGE ATTACH POINT. REMOVED BRACKETS IAW 51-30-02. NEW BRACKETS FABRICATED IAW BOEING DRAWING 69-18203. NEW BRACKETS INSTALLED IAW 51-30-02. 2L73 4F A3WE 20041123002112004112300211EU 2004 11 23 UPS04143386 120041021A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01133UP 0816 INSPECTION TYPE:N/A LAV EXIT LIGHT INOP. RELAMPED LAV EXIT LIGHT. 2L72 4F RTA35EU 20041123002182004112300218NM 2004 11 23 UPS04243275 120040912A5320 FITTING BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C, EVIDENCE OF CRACK ANGLE FITTING RIGHT SIDE ON SHELF MID WAY UP 950 AFT RIGHT WALL. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-10-01, 51-10-02, 51-30-2 & SOH M 20-10-03 FIG 9. 2L73 4F A3WE 20041123002192004112300219NM 2004 11 23 UPS04M43282 120040812A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 35 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 35 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.130 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 35 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 35 LEFT PER EO MD11-5510-19409-H & EN 1298-04 FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20041123002232004112300223NM 2004 11 23 SWAA043349 120041115A53116517684 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND RT FRAME WEB CRACKED AT BS 303, FWD LOWER STOP FITTING. REMOVED AND REPLACED FRAME WEB PER SRM. 2L72 4F RTA16WE 20041123002242004112300224NM 2004 11 23 UPS04M43084 120040909A3350 CIRCUIT BREAKER DOUG MD11 MD11F 3023600NM EMERGENY LIGHT TRIPPED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP 48578 INSPECTION TYPE:N/A EMERGENCY LIGHTS ARE ON WHEN EMERGENCY LIGHT SWITCH IS IN THE ARM POSITION. FOUND EMERGENCY LIGHTS CONTROL C/B POPPED. RESET C/B AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM REF AMM 33-50-00, CHECKS GOOD AT THIS TIME. 2L73 4F RTA22WE 20041123002252004112300225 2004 11 23 UPS04M43085 420040909A2565 LIGHT DOUG MD11 MD11F 3023600NM R1 DR EVAC SLIDEMALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP 48768 INSPECTION TYPE:N/A R1 DOOR EVAC SLIDE PRESS TO TEST LIGHT STAYS ON PERMANENTLY. REF DMI M287400. PERFORMED TEST OF REMOTE PRESSURE INDICATOR ASSY IAW MM 25-61-04. FOUND STATISFACTORY. THIS CLOSES DMI M287400. 2L73 4F RTA22WE 20041123002272004112300227NM 2004 11 23 SWAA043350 120041115A531265465682 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS AT BS 1016 PRESSURE BULKHEAD DOME WEB CENTER SECTION AT 7 O'CLOCK AND 12 O'CLOCK POSITION. REPAIRED WEB SECTIONS PER EA. 2L72 4F RTA16WE 20041123002312004112300231EU 2004 11 23 MALA040657 120041019A5210557092 GUARD SAAB SF340 340B 7860101EU PAX DOOR MISSING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15420XJ 340B420 TWO SCREWS MISSING FROM TOP OF CABIN ENTRY DOOR. DAMAGE TO RAIN FLAP & TOP OF CABIN BOARDING DOOR. MAINTENANCE INITIATED PWI TO REPLACE RAIN GUARD P/N 55-709-2 AND COVER ASSY P/N 55-174-3. 2L72 4T RTA52EU 20041123002322004112300232EU 2004 11 23 MALA040660 120041021A2497 WIRE SAAB SF340 340B 7860101EU DC GENERATOR BROKEN A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15445XJ 340B445 RIGHT DC GEN FELL OFF LINE IN FLIGHT. CREW PERFORMED QRH AND RIGHT DC GEN DID NOT COME BACK ON LINE. MAINTENANCE FOUND TERMINAL WIRE-A BROKEN. REPAIRED IAW SF3 WIRE MANUAL CHAP 20-20-00, OPS CHECK OF DC STARTING/GENERATOIR SYSTEM GOOD IAW 24-30-005. 2L72 4T RTA52EU 20041124000022004112400002NM 2004 11 24 GAIA04124 120040910A5720 SUPPORT BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE RT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING FRONT SPAR WS 726, NR 8 SLAT ACTUATOR OB PLATE TRUNNION SUPPORT CRACKED. REF FASI NR 86620, REMOVED AND REPLACED NR 8 SLAT SUPPORT PLATES IAW SB 57-0130, REV 3. 2L73 4F4 F A3WE E2EA 20041124000032004112400003NM 2004 11 24 GAIA04129 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 380 DENTED ABOVE STR 7 AND 6 RT. REF FASI NR 86678 CUT OUT DAMAGED AREA DIM 1.0 X 3.50 AND 1.0 X 3.0. INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000052004112400005NM 2004 11 24 AMTA200401312 120041025A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT LOOSE A K NONE L NO TEST ININSP/MAINT 1 GL11517AT 27973 EGRESS TRACK HAS LIGHTS INOPERATIVE BETWEEN SEATS 28 DEF AND 30 DEF. CONNECTED LOOSE WIRE. OPS CHECK NORMAL. OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20041124000072004112400007EA 2004 11 24 REXA04021 120041011A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258598B 7598 FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET IAW AD 98-20-01 FLAPS PLACED ON 72 HOUR MONITORING. 2L72 4F4 FRTA21EA E15NE 20041124000092004112400009NM 2004 11 24 GAIA04118 120040910A5720 ANGLE BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE RT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING L/E FWD STA 130 OB CHORD ANGLE CRACK. REF FASI NR 86591, STOP DRILLED CRACK AREA AND INSTALL ANGLE REPAIR IAW SRM 57-20-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000122004112400012NM 2004 11 24 GAIA04125 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND EXISTING FUSELAGE SKIN REPAIR DOUBLER AT STA 410 AND STR 21 RT HAS TOOLING SET MARKS AND DOES NOT COMPLY WITH SRM 53-30-3, FIG 3. REF FASI NR 86628, CUT OUT DAMAGED AREA DIM 13.75 X 10.75. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, FIG 3. 2L73 4F4 F A3WE E2EA 20041124000132004112400013NM 2004 11 24 ASAA0410401 120040920A5330 BUTT JOINT BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON BUTT SPLICE. REMOVED AND REPLACED BUTT SPLICE. 2L72 4F4 FRTA16WE E2EA 20041124000142004112400014EA 2004 11 24 A6WA200440173 120041028A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FS 280, RBL 9 OB ANGLE PN 601R31113-58 IS CRACKED IN RADIUS AT WL73. REMOVED AND REPLACED ANGLE WITH PRE-FABBED ANGLE IAW REO 601R53-11-171 REV A AND BRAS EO 601R-53-5447 AND M. 2L72 4F4 FRTA21EA E15NE 20041124000152004112400015NM 2004 11 24 GAIA04126 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND DENT IN FUSELAGE FRAME AT STA 1090, STR 25 LT. REF FASI NR 86673, CUT OUT DAMAGED AREA DIM 1.125 X 1.0 INSTALLED SPLICE IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000172004112400017NM 2004 11 24 GAIA04132 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SO07180AX 20041 DURING C-CHECK INSPECTION, FOUND MAIN CABIN FRAME AT BS 520, ABOVE STR 17 RT, DENTED. REF FASI NR 86681, CUT OUT DAMAGED AREA DIM 1.0 X 2.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000192004112400019NM 2004 11 24 GAIA04136 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 600 ABOVE STR 17 RT, DENTED. REF FASI NR 86685, CUT OUT DAMAGED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000252004112400025NM 2004 11 24 GAIA04170OP 120041012A324221147M BRAKE ASSY BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE NR 1 MLG DRAGGING A GAIAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07750US 21512 DURING LANDING, FLIGHT 750 IAG-MSP: VIBRATION IN LANDING GEAR DURING LANDING AND TAXI. LANDING WAS MADE WITHOUT INCIDENT. FOUND NR 1 MLG BRAKE DRAGGING. REMOVED AND REPLACED NR 1 MLG BRAKE ASSEMBLY AND REINSTALLED NR 1 MLG WHEEL ASSEMBLY. LEAK CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041124000272004112400027EA 2004 11 24 REXA04024 120041029A3231864808 PSEU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG DOOR MALFUNCTIONED A REXAO OTHER S AFFECT SYSTEMS CRCRUISE 1 SO258836A2821 7836A UNCOMMANDED NOSE DOOR DEPLOYMENT. QRH FOLLOWED, EMERGENCY DECLARED, UNEVENTFUL LANDING. REMOVED AND REPLACED PSEU. PERFORMED GEAR SWINGS IAW AMM. 2L72 4F4 FRTA21EA E15NE 20041124000282004112400028EU 2004 11 24 SIMA200427804 120041001A335066362 LIGHT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROW 3A INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21376AE 340B376 EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROW 3A INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA52EU E8NE 20041124000292004112400029EU 2004 11 24 SIMA200427203 120040927A3350 CONNECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY SIGN LOOSE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21388AE 340B388 EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE. RESECURED GALLEY CONNECTOR OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200500061) 2L72 4T4 TRTA52EU E8NE 20041124000302004112400030SO 2004 11 24 SIMA200427901 120040930A532014522178005 SILL EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21835AE4976 145634 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE CORRODED AREA AND FOUND TO BE WITHIN REPAIRABLE LIMITS STATED IN AEAI ETN EB53-032R1. FABRICATED A DOUBLER. REPAIR DONE IAW AEAI ETN EB 53-032R1. 2L72 4F4 FRTT00011ATTE6CH 20041124000312004112400031SO 2004 11 24 SIMA200428402 120041010A3350110049 CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21852AE 145736 CREW REPORTED THE FORWARD OVERHEAD DOME EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY CHARGER IAW MM 33-50-00. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20041124000322004112400032EA 2004 11 24 A6WA200440172 120041028A5320601R3111358 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FS 280, RBL 9 IB ANGLE PN 601R3113-58 IS CRACKED IN RADIUS AT WLK 73. REMOVED AND REPLACED ANGLE WITH NEW ANGLE PN 601R3113-58 IAW SRM 51-42-06 AND 51-42-21. 2L72 4F4 FRTA21EA E15NE 20041124000342004112400034NM 2004 11 24 GAIA04131 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED E GAIAK NONE O OTHER ININSP/MAINT 1 GL13180AX 20041 DURING C-CHECK INSPECTION FUND MAIN CABIN FRAME AT BS 500 ABOVE STR 17 RT DENTED. REF FASI NR 86680, CUT OUT DAMAGED AREA DIM 1.0 X 2.0. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000372004112400037NM 2004 11 24 ASAA0470017 120040930A3350 BATTERY PACK BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE EMERGENCY LIGHT INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02618AS 30543 DURING ROUTINE MAINTENANCE FOUND FWD ROW EMERGENCY TRACK LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. 2L72 4F4 FRTA16WE E00055EN 20041124000382004112400038SO 2004 11 24 SIMA200428704 120041013A3350BA50933901 BATTERY PACK EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21678AE 14500813 CREW REPORTED NO FORWARD EMERGENCY FLOOR LIGHTS ON IN CABIN WHEN TESTED. AIRCRAFT WAS INSPECTED AND FERRIED FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200500258) 2L72 4T4 FRTT00011ATTE6CH 20041124000412004112400041NM 2004 11 24 GAIA04138 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 660 ABOVE STR17,16 RT, DENTED. REF FASI NR 86687, CUT OUT DAMAGED AREA DIM 1.0 X 2.25 AND 1.0 X 2.25. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000432004112400043EA 2004 11 24 REXA04013 120040703A3260 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE NLG DOOR OUT OF POSITION A REXAO OTHER N FALSE WARNING APAPPROACH 1 SO258933B419 7933 ON DESCENT, RECEIVED GEAR DISAGREE (NOSE DOOR). QRH FOLLOWED HOWEVER, INDICATION REMAINED. GEAR MANUALLY LOWERED, RECEIVED 3 GREEN, UNEVENTFUL LANDING. NOSE GEAR PROXIMITY SENSOR FOUND TO BE OUT OF POSITION. ADJUSTED IAE MM 32-61-05, GEAR SWINGS PERFORMED AND OPERATIONAL CHECK OF STEERING PERFORMED. 2L72 4F4 FRTA21EA E15NE 20041124000442004112400044SO 2004 11 24 SIMA200427904 120040921A532014522461003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21732DH8464 145358 CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT A SECTION OF THE OMEGA BEAM TO REMOVE DAMAGE. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS. REPAIR DOEN IAW EMB 145SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-22-10, FIG 203. (SW21200500268) 2L72 4F4 FRTT00011ATTE6CH 20041124000452004112400045NM 2004 11 24 ASAA0470011 120040822A53201496377 ANGLE BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 AFT CARGO COMP RT ZEE ANGLE CORRODED. REMOVED AND REPLACED ZEE ANGLE IAW SRM. 2L72 4F4 FRTA16WE E00055EN 20041124000462004112400046SO 2004 11 24 SIMA200427908 120040930A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21834AE4998 145631 THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. CUT OUT DAMAGED SECTION OF THE OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-22-10, FIG 201. (SW21200500286) 2L72 4F4 FRTT00011ATTE6CH 20041124000492004112400049NM 2004 11 24 AMTA200401308 120041022A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A K NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 EMERGENCY FLOOR LIGHTING OUT AT SEATS 15,17 AND 28-30. RELAMPED LIGHTS AT 15, 17. RECONNECTED WIRING AT ROW 28-30. OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20041124000502004112400050EA 2004 11 24 REXA04022 120041013A2750860D10018 FCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS FAILED A REXAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO258673D 7673 FLAP FAILURE AT PUSH BACK. REMOVED AND REPLACED FECU. (FLAP ELECTRONIC CONTROL UNIT) 2L72 4F4 FRTA21EA E15NE 20041124000532004112400053NM 2004 11 24 GAIA04145 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 1342. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 54-30-3, FIG 7. 2L73 4F4 F A3WE E2EA 20041124000552004112400055NM 2004 11 24 USAA040811 120040827A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT, Q5, FLOOR SUPPORT, 3 INCH CRACK (BROKEN) AT STA 540 RBL 2. REPLACED FLOOR SUPPORT IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20041124000572004112400057NE 2004 11 24 ASOA04778 220041006A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF343B1 NE RIGHT FOD A ASOAC ABORTED TAKEOFF CAJF.O.D. FLAME/FIRE WARNING INDICATION TOTAKEOFF 1 SO27722EV 10127 DURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN AIRCRAFT ACCOMPANIED BY A COMPRESSOR STALL ON THE RT ENGINE ALONG WITH THE TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL AND NO FIRE INDICATIONS PRESENT. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED, LANDING SAFELY WITH FLAPS SELECTED AT 20 DEGREES. MAINTENANCE FOUND FOD DAMAGE TO THE RT ENGINE COMPRESSOR STAGES 1 THROUGH 5. MAINTENANCE REMOVED AND REPLACED RT ENGINE. MRR WILL REMAIN OPEN, PENDING ENGINE TEARDOWN REPORT. 2L72 4F4 FRTA21EA E15NE 20041124000612004112400061EA 2004 11 24 ASOA04814 120041023A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS7462 7421 DURING A GROUND INSPECTION, THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041122001502004112200150NM 2004 11 22 04FDEA02006 120040707A2611 SMOKE DETECTOR BOEING727 727233 138408ANM NR 4 MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25258FE 20940 CLIMBING THROUGH 16,000 FT, NR 4 MAIN CARGO SMOKE LIGHT ILLUMINATED. RAN QRH PROCEDURES. LIGHT EXTINGUISHED. SHORTLY AFTER LEVELING AT FL 230, NR 4 SMOKE WARNING REOCCURRED. TEST OF SYSTEM SHOWED BAD NR 4 SENSOR, IE TEST NOT GOOD. REMOVED AND REPLACED NR 4 DETECTOR AS PER 727 200-26-16-011-4, OPS CKS GOOD MEL REMOVED. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 7740-01. 2L73 4F RTA3WE 20041122001532004112200153NM 2004 11 22 AWXA200401200 120041103A33503114981 REFLECTOR BOEING737 7373G7 1384595NM FUSELAGE INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 LEFT FUSELAGE EXTERIOR EMERGENCY ESCAPE LIGHT AFT OF WING TO BODY FAIRING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FUSELAGE EXTERIOR EMERGENCY ESCAPE LIGHT ELECTRICAL SOCKET, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041122001662004112200166EU 2004 11 22 AWXA200401211 120041017A5321D5361014900000 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, FOUND CORROSION ON L-2 DOOR ENTRY WAY FLOOR PANEL 221FF. MAINTENANCE REMOVED AND REPLACED L-2 DOOR ENTRY WAY FLOOR PANEL 221FF IAW T/C C1D25306. 2L72 4F RTA28NM 20041122001812004112200181NM 2004 11 22 04FDEA02027 120040708A5753ARC74901 FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORRODED. RT WING, INBOARD FLAP VANE TEE-FITTING INBOARD MOST AFT ATTACHING HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2 - 4. ORIGINAL DIAMETER = 0.8755 INCH, FINAL DIAMETER = 0.882 INCH, MAXIMUM ALLOWABLE DIAMETER = 0.8755 INCH. EXCEEDED LIMITS PER EO NR 1-5750-7-5005A PART 2, INSPECT/ MODIFY INBOARD FLAP VANE ATTACHING FITTINGS SB MD11-57-034 AND MD 11-57-065 (RT WING) COMPLIED WITH FEDEX EA NR 1-5750-76788, WINGS, RIGHT INBOARD FLAP VANE, TEE FITTING CORRODED. 2L73 4F RTA22WE 20041122001992004112200199 2004 11 22 SA04097 420041019A2565D30664105 SLIDE AIRBUS320 A320214 3930316EU ZONE 200 UNSERVICEABLE A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19105UW6104 868 LAX - THE SLIDE INTENDED TO REPLACE THE SLIDE IN THE FORWARD LEFT POSITION CAME APART PRIOR TO BEING INSTALLED. MAINTENANCE INSTALLED PREVIOUS SLIDE. 2L72 4F RTA28NM 20041122002002004112200200NM 2004 11 22 SB04134 120040928A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19530AU 24412 BOS - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTS, AT SEAT ROWS 17 THROUGH 20, WOULD ILLUMINATE AND THEN QUICKLY EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT CABIN. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002232004112200223EU 2004 11 22 BA04025 120041025A3350321431 BATTERY AIRBUS330 A330323 3930335EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19672UW 333 PIT - EMERGENCY LIGHTS AT THE R1 AND L4 DOORS DID NOT ILLUMINATE WHEN GROUND POWER FAILED. MAINTENANCE REPLACED THE 12WL AND 17WL EPSU BATTERIES. 2L72 4F RTA46NM 20041122002312004112200231NM 2004 11 22 EIA2004065 120040720A5320 FITTING BOEING747 747273C 1384896NM FUSELAGE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 1 EA HOLE HAS BREAKUP CONDITION ON THE STRINGER END FITTING AT BS 2141 LEFT AFT SIDE, STR 21L LOWER. REMOVED AND REPLACED END FITTING AT BS 1241 STR 21L, LOWER. REMOVED AND REPLACED STRINGER NR 21L LOWER BS 1241-1260. REMOVED AND REPLACED INTERCOSTAL WEB AT B.S 1241-60 STR 21L LOWER PER B747 SRM 51-20-01, SRM 51-30-02 PAGES 8, 9. ALODINED PER B747 SRM 51-10-02 PAGES 7-8, PRIMED PER BSOPM 20-41-02 PAGES 7-9. 2L74 4F A20WE 20041122002352004112200235NM 2004 11 22 EIA2004109 120040920A572065B172235 SPLICE BOEING747 747SR46 1384816NM LT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 LEFT WING UPPER SIDE OF BODY SPLICE, LT WING AT REAR SPAR OPEN HOLE NR 4 FOUND CRACK. HOLE CONCENTRICALLY REAMED 1.375 IN DIAMETER IN SPLICE FITTING ONLY. OPEN HOLE HFEC INSP PERFORMED. FREEZE PLUG FAB'D AND INSTALLED COMMON TO SPLICE FITTING ONLY PER SRM 51-10-08. REAMED HOLE TO 1.0 INCH. ALODINE, PRIMER, FAB'D RETENTION WASHER, HEAT TREAT AND CAD PL. INSTALLED ORIGINAL TYPE BOLT PER EN EA-53-0822 BOEING MESSAGE: I-OAGAS, I-ODB6A, I-P8ZOS, I-PKIOB, AND I-PTITL. 2L74 4F RTA20WE 20041122002382004112200238NM 2004 11 22 USAA040724 120040917A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 FLOOR TRACK, 3 INCHES LONG BY 4 INCHES WIDE, CORROSION; NO LEVEL OR TASK, STA500+ 16 INCHES AT LBL17. FABRICATED AT MACHINE SHOP TO DUPLICATE ORIGINAL IAW SRM 53-00-53, FIG 202. 2L72 4F4 FRTA16WE E21EU 20041122002532004112200253NM 2004 11 22 SB04154 120041111A33501012721 LIGHT BOEING737 737301 1384611NM SEAT 8C DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU 23512 PHL - PILOT REPORTED THE EMERGENCY LIGHT AT SEAT 8C INOPERATIVE. MAINTENANCE REATTACHED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041122002592004112200259NM 2004 11 22 EIA2004138 120041021A5311 FRAME BOEING747 747273C 1384896NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 BS 360 RT STRINGER 15-16 RT, FOUND WEB OF LOWER FRAME CRACKED. FABRICATED AND INSTALLED REPAIR PER ECRA 470-53-267-2. 2L74 4F A20WE 20041122002632004112200263NM 2004 11 22 SB04131 120040925A291065446915 MODULE BOEING737 7374B7 1384702NM HYD SYSTEM FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19435US4133741337 24557 CLT - FLT 1021 - AFTER TAKEOFF FROM CLT, CAPTAIN REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR HYDRAULIC MODULE PER MM 32-32-61. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20041123000012004112300001NM 2004 11 23 DHL2004741011 120041119A2612 FIRE LOOP BOEING727 7272Q9 138448MNM NR 3 ENGINE INOPERATIVE A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01741DH 21931 DURING THE ENGINE FIRE PROTECTION TEST, FOUND NR 3 ENGINE SYS "B" LIGHT WON'T COME ON SYS "A" LT OK. FIRE DETECTION SYS ON NR 3 ENGINE SYS "B" DEFERRED IAW MEL 26-6 SYS "A" WORKS OK PLACARD INSTALLED CTRL NR 18526. WORKING DMI (18526) NR 3 ENGINE FIRE DET SYS "B" LT INOP. NR 3 ENG SYS "B" LOOP CHECK FOUND LOOSE TERMINAL, TIGHTENED SAME IAW MM 26-11-0, CHECKS GOOD PLACARD REMOVED. 2L73 4F RTA3WE 20041123000082004112300008WP 2004 11 23 DJFA2004033 220041118A726130752071 OIL TANK BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP NR 2 ENGINE LEAKING E DJFAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 EA23851CW 258051 P91211 HOU - MAF TRIP ID NR 731960. CREW REPORTED THAT DURING APPROACH TO MAF THE NR 2 ENGINE OIL PRESSURE DROPPED TO 10 PSI. ENGINE WAS SHUT DOWN AND SECURED. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE DISCOVERED A SMALL PIN HOLE IN THE RIGHT ENGINE OIL TANK. OIL TANK WAS REPLACED AND ENGINE OIL WAS SERVICED. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20041123000102004112300010NM 2004 11 23 ASAA0410400 120040920A5315 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 CORROSION ON FLOORBEAM AT FLANGE AROUND NUT PLATE. REMOVED CORROSION, AND REPAIRED FLOORBEAM. 2L72 4F4 FRTA16WE E2EA 20041123000122004112300012SO 2004 11 23 RAIA00411008 120041109A2130C1431234 CONTROL VALVE EMB 145 EMB145LR 3260212SO A/C PACK TEMP INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03835HK1975 145670 8088- IAD- UNABLE TO CONTROL CABIN TEMP WITH RT PACK, LT PACK TEMP DEFERRED. MAINTENANCE CHECKED RT TEMP CONTROL WITH NO DEFECTS NOTED, AND REMOVED AND REPLACED LT PACK DUAL TEMP CONTROL VALVE. 2L72 4T RTT00011AT 20041123000142004112300014SO 2004 11 23 C2XA04IA142 120041104A33503025103 LIGHT EMB 145 EMB145ER 3260211SO FUSELAGE INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712934 145019 CRP - DURING MAINTENANCE INSPECTION, THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041123000342004112300034NM 2004 11 23 DHL2004750044 120041103A3350 BATTERY BOEING727 7272M7 138407SNM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01750DH 21951 BOTH EMERGENCY EXIT LIGHTS INOP ON PREFLIGHT. REPLACED EMERGENCY EXIT LIGHTS BATTERIES, CKS GOOD NOW. 2L73 4F A3WE 20041123000382004112300038SO 2004 11 23 C2XA04SH547 120041107A3350744412 SIGN EMB 135 EMB135LR 3260305SO AFT GALLEY INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2727523 145389 SHV- 2269, DURING SERVICE/ROUTINE CHECK THE EMERGENCY EXIT SIGN ON THE BACK OF THE AFT GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSEMBLY IAW EMB135 AMM 33-50-15. THE EXIT SIGN OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041123000462004112300046EU 2004 11 23 DHL2004362016 120041113A30406800021300 REGULATOR AIRBUS300 A300B4203 3930306EU WINDSHEILD HEAT FAILED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01362DH 84 AT FL350 CAPT FORWARD WINDSHIELD STARTED ARCING WHICH RESULTED INTO CRACKING. PERFORMED ASSOCIATED ABNORMAL PROCEDURE, DESCENDED TO FL240. REPLACED CAPT'S FWD WINDOW ASSY PER A/B M/M 56-11-11, REPLACED CAPT'S WINDOW HEAT REG PER A/B M/M 30-42-0. WINDOW OPS AND LEAK CHECKS SERVICEABLE. 2L72 4F RTA35EU 20041123000502004112300050EU 2004 11 23 DHL2004363502 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, N/R 3869, FR 34-38.2 LBL 58 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FR 34-38.2 LBL 58 IAW A-300 SRM 51-30-29. FABRICATED NEW SEAT TRACK AS PER EXAMPLE IAW A-300 51-10-40. TREATED, PRIMED AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FR 34 TO FR 38.2 AT LBL 58 IAW A-300 SRM 53-10-10. 2L72 4F RTA35EU 20041123000602004112300060NM 2004 11 23 DHL2004747008 120041110A3350 LIGHT BOEING727 727224 1384076NM CABIN DISLODGED A DHLAO OTHER O OTHER CRCRUISE 1 SO01747DH 22253 EMERGENCY EXIT LIGHT FELL OFF MOUNT DURING FLIGHT. SECURED LIGHT ASSEMBLY, OPS CHECK GOOD IAW 727 MM CH 33-50. 2L73 4F A3WE 20041123000622004112300062EU 2004 11 23 DHL2004365004 120040926A3240 SERVO VALVE AIRBUS300 A300B4203 3930306EU NR 7 BRAKE DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01365DH 149 AFTER T/O BRAKE HOT LIGHT ON MWP ILLUMINATED. WHEEL NR 7 BRAKE LIGHT ILLULMINATED. BRAKE HOT ABNORMAL PROCEDURES COMPLETED. SERVO UCV FOUND DIRTY. CLEANED, A/C TAXI PERFORMED OK AND STATIS IAW MM 32-42-48. 2L72 4F RTA35EU 20041123000652004112300065EU 2004 11 23 DHL2004363513 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, N/R 3894, FR 26.5 - FR 32.5 RBL 18 MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR 26.5 TO FR 32.5 AT RBL 18 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. NEW SEAT TRACK P/N 7075 T6 511 / TMS 60-22457 TREATED AND PRIMED / POLY WHITE AND INSTALLED NEW SEAT TRACK FROM FRAME 26.5 TO FRAME 32.5 RBL 18 MAIN CABIN REF A-300 SRM 51-10-40 / A-300 SRM 51-30-30 / A-300 SRM 51-40-10 / A-300 SRM 51-40-12. 2L72 4F RTA35EU 20041123000682004112300068SO 2004 11 23 C2XA04IA136 120041017A3350 CONNECTOR EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DIRTY A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2712519 145366 DURING PREFLIGHT CREW REPORTED THE EMERGENCY LIGHT BESIDE THE MAIN DOOR WAS INOPERATIVE. FOUND THE ELECTRICAL CONNECTION AT THE LIGHT TO BE DIRTY. CLEANED THE CONNECTION AND OPERTIONALLY CHECKED GOOD. 2L72 4F RTT00011AT 20041123000772004112300077NM 2004 11 23 CALA0400717 120041118A532065516989 SPLICE BOEING737 7373T0 1384582NM STRINGER CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 4L SPLICE AT STA 907. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20041123000902004112300090NM 2004 11 23 SWAA043402 120041120A5320BAC1505 ANGLE BOEING737 7373Y0 1384671NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD ANGLE CRACKED AT LBL 5.8, WL 196. REMOVED AND REPLACED ANGLE SECTION PER SRM. 2L72 4F RTA16WE 20041123000952004112300095NM 2004 11 23 QXEA200400756 120041029A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FUSELAGE INT FORWARD, X0 TO X47, LEFT HAND Y9.5, INBOARD FORWARD SEAT RAIL IS CORRODED ON UPPER SURFACE FROM X0 TO X47. REPAIRED IAW HORIZON AIR EA 6-53-447 AND RD8/4-53-1038. 2H72 4T RTA13NM 20041123001002004112300100NM 2004 11 23 SWAA043386 120041119A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 FUSELAGE SKIN CRACKED AT BS 376, STR 8L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041123001082004112300108NM 2004 11 23 UPS04M43155 120040801A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 36 BARREL NUT RIGHT FOUND CORRODED AT BOTTOM S/W & BEARING SURFACE. CORROSION AT NR 36 BARREL NUT HOLE RIGHT REMOVED, BLEND & REAMED TO 0.100 INCH FOUND OUT OF LIMIT. SLEEVE BUSHING AT BARREL NUT HOLE NR 36 RIGHT CLEANED, SMOOTHED & PROTECTED PER SRM 51-21-01 V2R35. EXISTING SLEEVE BUSHING INSPECTED & REUSED. APPLIED 1422B1/2 & BARREL NUT INSTALLED PER MD11-5510-19409-H & FOUND WITHIN LIMIT AS PER EN:1286-04. 2L73 4F RTA22WE 20041123001152004112300115NM 2004 11 23 UPS04M43158 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 2 BARREL NUT HOLE RIGHT FOUND CORRODED ON BOTTOM & BEARING SURFACE. CORROSION AT NR 2 BARREL NUT HOLE RIGHT, BLEND, REMOVED & REAMED TO 1.035 INCH FOUND OUT LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 2 RIGHT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 2 RIGHT PER EO MD11-55 10-194O9-H & EN:1255-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123001242004112300124CE 2004 11 23 DXTA200400363 120040817A783065680 DIODE CESSNA500 560CESSNA 2076750CE THRUST REVERSER FAILED E DXTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL07320QS 5600321 THE LEFT THRUST REVERSER DEPLOYED IN FLIGHT. REMOVED AND REPLACED DIODES NR 169 AND 171, ALSO REMOVED AND REPLACED LEFT T/R SELECTOR VALVE. LEFT T/R OPS AND LEAK CHECKS GOOD, WORK DONE IAW CITATION 560 MM CHAPTER 78-31-01. 2L72 4F RTA22CE 20041123001362004112300136NM 2004 11 23 UPS04M43169 120040716A5720ARB2850506 SUPPORT FITTING DOUG MD11 MD11F 3023600NM SLAT TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, RIGHT WING LEADING EDGE SLAT TRACK NR 16 ROLLER SUPPORT FITTING CRACKED. RIGHT WING NR 16 SLAT TRACK REMOVED PER MM 27-80-32 R.50. RIGHT WING LEADING EDGE NR 16 TRACK FITTING REMOVED PER SRM 51-33-01, 51-35-01 V2.R35. NEW NR 16 ROLLER SUPPORT FITTING HOLE PICKED UP PER SRM 51-31-01 V2.R35. RIGHT WING L/E NR 16 SLAT TRACK ROLLER SUPPORT FITTING REPLACED PER SRM 51-35-01 V.2.R35. RIGHT WING NR 16 SLAT TRACK INSTALLED PER AMM27-80-32-R.50. 2L73 4F RTA22WE 20041123001662004112300166NM 2004 11 23 0401846624 120041004A3350 BATTERY PACK BOEING747 747251B 1384892NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING LINE CHECK, FOUND E-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20041123001732004112300173NM 2004 11 23 QXEA200400743 120041110A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY DIRTY A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09375PH12091 529 SEA - FLIGHT 2119 - DURING CRUISE FLIGHT, THE CREW RECEIVED A MASTER WARNING WITH ASSOCIATED SMOKE WARNING LIGHT. THIS OCCURRED TWICE DURING FLIGHT, HOWEVER, THE FLIGHT ATTENDANTS DID NOT OBSERVE, OR SMELL, ANY SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND THE NR 1 AND NR 2 CARGO SMOKE DETECTORS. DUST WAS OBSERVED ON BOTH. THE DETECTORS WERE CLEANED AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041123001812004112300181NM 2004 11 23 UPS04243395 120041004A5312 PRESSURE PANEL BOEING727 727185C 138406NNM NLGWW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, CRACK FOUND ON NWW LEFT SIDEWALL JUST BELOW LEFT AFT SIDE PRESSURE PANEL. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREAS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-40-02. 2L73 4F A3WE 20041123001872004112300187CE 2004 11 23 DXTA200400334 120040709A2130 SELECTOR KNOB CESSNA560 560XL 2076702CE CABIN PRESSURE OUT OF POSITION E DXTAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL07690QS 5605090 DURING CRUISE AT 22,000 FT, MASTER WARNING CAME ON FOR LOSS OF CABIN PRESSURIZATION. DECLARED EMERGENCY AND DESCENDED DOWN TO 10,000 FT, PROBLEM WENT AWAY. DIVERTED AND AIRCRAFT LANDED SAFELY. FOUND SELECTOR KNOB POINTING INCORRECTLY, REPOSITIONED CABIN SOURCE SELECTOR KNOB, KNOB INDEX LINE POINT TO ALL SOURCES CORRECTLY. 2L72 4F RTA22CE 20041123001892004112300189CE 2004 11 23 DXTA200400337 120040712A5270 PROXIMITY SWITCH CESSNA560 560XL 2076702CE EMERGENCY EXIT OUT OF ADJUST E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07606QS 5605338 ON TAKEOFF ROLL OUT OF LUK, THE EMERGENCY CAUTION LIGHT ILLUMINATED, ABORTED TAKEOFF. REMOVED EMERGENCY EXIT DOOR, REMOVED EMERGENCY EXIT PROX SWITCH FROM DOOR JAM, PERFORMED VISUAL INSPECTION OF SWITCH AND WIRING, NO DEFECTS NOTED. ADJUSTED PROX SWITCH TO WITHIN TOLERANCE AFTER REINSTALLATION. REINSTALLED EMERGENCY EXIT DOOR, PERFORMED MANUAL OPS CHECK OF DOOR HANDLE, NO DEFECTS NOTED. WORK PERFORMED IAW CESSNA 560XL MM CHAPTER 57-20-00 AND 21-30-00. 2L72 4F RTA22CE 20041123001982004112300198NM 2004 11 23 DXTA200400374 120040826A3150221150M05 ACTUATOR AMD FALC50FALCON2000 2730170NM PITCH FEEL FAILED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07277QS 177 DURING TAKEOFF ROLL WITH POWER LEVERS IN TAKEOFF FOR APPROXIMATELY 10-15 SECONDS AND AT 40 KNTS NO TAKEOFF CONFIGURATION WARNING ACTIVATED. REASON FOR WARNING CANNOT BE DETERMINED, CONFIGURATION WAS NORMAL FOR ALL SYSTEMS. REPLACED PITCH FEEL ACTUATOR IAW F2000 PROCEDURE 27-318. COMPLIED WITH OPS CHECKS IAW F2000 PROCEDURES 27-014, 31-301, 27-308, 27-309, 27-312, & 27-314, ALL CHECKS SATISFACTORY. 2K73 4F RTA50NM 20041123002042004112300204CE 2004 11 23 DXTA200400379 120040901A32401206P27 PRESSURE SWITCH CESSNA500 560CESSNA 2076750CE BRAKE SYSTEM FAILED E DXTAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07348QS304 5600348 DURING TAXI AFTER LANDING, THE RIGHT AND LEFT BRAKE PEDALS WENT TO THE FLOOR WITH NO BRAKES ON BOTH LEFT AND RIGHT SIDES. AFTER PUMPING A COUPLE OF TIMES, BRAKES CAME BACK FULL, THEN FAILED AGAIN, THEN CAME BACK AGAIN, STOPPED PLANE AND GOT TUGGED IN. REMOVED AND REPLACED BRAKE LOW PRESSURE SWITCH WITH NEW AND NEW O-RING, PERFORMED ANTI-SKID SYSTEM FUNCTIONAL TEST, ALL CHECKS GOOD AND NO LEAKS DETECTED. NO DEFECTS NOTED AT THIS TIME, ALL WORK PERFORMED IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20041123002052004112300205CE 2004 11 23 DXTA200400378 120040831A275099145101 RESOLVER CESSNA750 750 2076810CE TE FLAPS FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07942QS3914 7500024 UPON SELECTING FLAPS 5 DEGREES THE SLATS EXTENDED BUT FLAPS DID NOT, GOT AMBER FLAPS FAIL, FLAP PICTORIAL WENT AMBER AND FLAP RESET BUTTON ILLUMINATED. MOVED FLAPS TO ZERO AND DEPRESSED FLAP RESET AMBER MESSAGE WENT OUT. SELECTED FLAPS 5 DEGREES AND WARNING RETURNED. RIGHT WING RESOLVER HAD INTERMITTENT VOLTAGE OUTPUT. REMOVED AND REPLACED RIGHT FLAP RESOLVER IAW CESSNA 750 MM CHAPTER 27-52-00. ACCOMPLISHED FULL FLAP RIG MECHANICAL AND ELECTRICAL IAW CESSNA 750 MM CHAPTER 27-50-00, FLAP SYSTEM OPERATIONALLY CHECKS GOOD. 2L72 4J RTT00007WI 20041123002142004112300214NM 2004 11 23 UPS04243376 120041020A3510 OXYGEN MASK BOEING727 727173C 1384059NM 2ND OBSERVER INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:N/A, 2ND OBSERVER O2 MASK INOP. REMOVED AND REPLACED 2ND OBSERVER O2 MASK IAW 35-11-41. OPS & LEAK CHECK GOOD. PLACARD REMOVED. DEFERRAL CLOSED (M289816). 2L73 4F A3WE 20041123002172004112300217 2004 11 23 SWAA043288 420041110A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29397SW 27691 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20041123002292004112300229NM 2004 11 23 UPS04243441 120041107A3350 BATTERY BOEING727 72722C 138400FNM EMERGENCY LIGHT DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 FOUND EMERGENCY LIGHT SWITCH IN ON POSITION, BATTERIES DISCHARGED. REPLACED BATTERIES, NOW OPS GOOD. 2L73 4F A3WE 20041123002302004112300230NM 2004 11 23 PCAA0406225 120040620A3260 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003NM MLG MALADJUSTMENT A PCAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA13846EX 326 FLIGHT 3720 HAD TO RETURN TO FIELD DUE TO HAVING THE RIGHT AND LEFT MAIN GEAR UNSAFE LIGHTS ILLUMINATE AFTER THE GEAR WAS RETRACTED. THE CREW USED THE ALTERNATE EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE THE CONDITION. IT WAS FOUND THAT THE LANDING GEAR UPLOCK PROXIMITY SENSOR NEEDED TO BE ADJUSTED. GAP WAS ADJUSTED AND THE GEAR WAS OPERATED SEVERAL TIMES. ALL SYSTEMS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041124000242004112400024NM 2004 11 24 GAIA04130 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BA 400 ABOVE STR 7 AND 6 RT DENTED. REF FASI NR 86679, CUT OUT DAMAGED AREA DIM 1.0 X 2.125 AND 1.0 X 4.0. INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG. 2L73 4F4 F A3WE E2EA 20041124000262004112400026NM 2004 11 24 AMTA200401301 120041021A3350 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 INTERIOR EGRESS FLOOR LIGHTS INOPERATIVE AT FORWARD CABIN. RE-CONNECT FWD CABIN EGRESS FLOOR LIGHT IAW 33-55-11-3. OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20041124000402004112400040NM 2004 11 24 ASAA0410360 120040805A33508821004 BATTERY PACK BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE ROW16 DEF DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 ROW 16 DEF, LED LIGHT FOR EMERGENCY LIGHT NOT WORKING. REPLACED BATTERY AT ROW 16 DEF, OPS CHECK NORMAL. 2L72 4F4 F A16WE E2EA 20041124000482004112400048NM 2004 11 24 GAIA04133 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND BS540 FRAME WITH DENTS INTO THE RADIUS. REF FASI NR 86682, ACCOMPLISHED ANGLE REPAIR IAW SRM 51-40-9, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000542004112400054NM 2004 11 24 USAA040812 120040829A5320 CLIP BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, CLIP EST. .125 INCH STA 500D S 8L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40. 2L72 4F4 FRTA16WE E2GL 20041124000592004112400059EU 2004 11 24 ASOA04780 120041007A3350 LIGHT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING PRE-FLIGHT CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. UPON COMPLETION OF THE PRE-FLIGHT CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR ILLUMINATED. MAINT INSPECTED THE EMERGENCY LIGHTS SYSTEM INCLUDING THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20041124000622004112400062EU 2004 11 24 ASOA04817 120041002A5320 ANGLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE ANGLE FIXED ON FR 36L, STRINGER 14L ON THE FORWARD SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE FIXED ON FR 36L, STRINGER 14L ON THE FORWARD SIDE IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041124000642004112400064EA 2004 11 24 A6WA200440158 120041016A3000 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ANTI- ICE SYSTEMILLUMINATED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31435AW 7724 LT COWL ANTI-ICE AMBER CASS ILLUMINATED WHEN COWL ANTI-ICE SWITCH TURNED OFF. COMPLIED WITH QRH MESSAGE EXTINGUISHED 14TH STAGE BLEED CLOSED. 2L72 4F4 FRTA21EA E15NE 20041124000662004112400066EU 2004 11 24 ASOA04816 120041002A5311S5397071635701 FRAME AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE FRAME AND ANGLE AT FR 28A ON THE RT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FRAME AND ANGLE AT FR28A ON THE RT SIDE IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041124000672004112400067NM 2004 11 24 GAIA04113 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE BULGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND SKIN BULGED AT STA 1030, STR 27R. REF FASI, CUT OUT DAMAGE AREA S DIM 12.5 X 3.25 AND 7.25 X 3.25 INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000692004112400069EA 2004 11 24 ASOA04810 120041021A5730 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A C-CHECK, THE RT WING PLANK AT APPROXIMATELY WS 148 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT WING PLANK AT APPROXIMATELY WS 148 IAW EO600-57-0134A. 2L72 4F4 FRTA21EA E15NE 20041124000702004112400070CE 2004 11 24 GUU2004F00034 120041015A2120 ODOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT DETECTED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1787554 UE227 DURING FLIGHT, MILD ODOR OF FUEL IN COCKPIT WITH LT BLEED AIR VALVE ON. RAN AIRCRAFT SYSTEMS. OPERATIONAL CHECKS GOOD. NO FUMES NOTED. COULD NOT DUPLICATE. 2L72 4T4 TRTA24CE E26NE 20041124000712004112400071CE 2004 11 24 O2G2004F00008 120041022A32460228 BEARING CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D1 52060NE NR 1 WHEEL WORN E O2GAO OTHER O OTHER TXTAXI/GRND HDL 1 NE0323YZ 5600638 RUMBLE FROM LT MAIN GEAR. REMOVED AND REPLACED MAIN WHEEL BEARING, WHEEL AND TIRE. 2L72 4F4 FRTA22CE E1NE 20041124000722004112400072CE 2004 11 24 GUU2004F00031 120040922A55201016200131 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO178755416640 UE227 AT SCHEDULED ROUTINE MAINTENANCE, LT CTR ELEVATOR HINGE BRACKET SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED LT CTR ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20041124000742004112400074NM 2004 11 24 GAIA14093 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND EXTERNAL POWER DOOR SKIN CUT. REF FASI NR 86303 REPAIRED RT EXTERNAL POWER DOOR IAW SRM 53-30-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000772004112400077NM 2004 11 24 ASAA0410404 120040928A53306545776531 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSLEAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 SKIN DAMAGED. REPAIRED DAMAGE ON SKIN LAP. 2L72 4F4 FRTA16WE E2EA 20041124000802004112400080NM 2004 11 24 GAIA04165 120040910A5310 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND R-2 DOOR CUT OUT FORWARD FRAME INNER CHORD CRACKED AT STRINGER 17 RT. REF FASI NR 87020, CUT OUT DAMAGE, INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000812004112400081EA 2004 11 24 ASOA04681 120040910A3350BR9279232 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7304 DURING HANGER MAINTENANCE, THE EMERGENCY FLOOR FLOOD LIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR FLOOD LIGHT AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041124000822004112400082EU 2004 11 24 ASOA04770 120040928A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27533AS17130932 460 DURING AN A-CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY ON THE PASSENGER DOOR AND THE POWER SUPPLY AT 61 WL. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041124000832004112400083SW 2004 11 24 ALG2004F00062 120040914A334001077006303 POWER SUPPLY BELL 206 206B3 1181506SW ALLSN 250C 250C20B 03013GL STROBE LIGHT BURNED E ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW035743B 3056 CAE831662 IN FLIGHT, NOTED A ODOR OF ELECTRICAL WIRE BURNING AND (CLICK) FROM OVERHEAD CONSOLE, SAW ANTI-COLLISION LIGHT OFF. TURNED SWITCH BACK ON, SMELLED ODOR AGAIN AND SWITCH TURNED OFF BY ITSELF. FOUND ELECTRICAL ODOR COMING FROM STROBE LIGHT POWER SUPPLY, REPLACED POWER SUPPLY CHECKED GOOD. 1G71 3U3 U H2SW E4CE 20041124000842004112400084NM 2004 11 24 GAIA04164 120040910A5347 SEAT TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE MISMANUFACTURED A GAIAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK BS 620 AT LBL 24.75 IS NOT IAW DWG NR 2902. REF FASI NR 87014, REPLACED SEAT TRACK WITH PN BAC 1520-792 IAW SRM 53-10-2, FIG 7 AND DWG NR 2902. 2L73 4F4 F A3WE E2EA 20041124000852004112400085EU 2004 11 24 KBM2004F00228 120040922A7712305731366 GAUGE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TORQUE STUCK E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 6 2300 TORQUE GAUGE STUCK, REPLACED WITH SERVICEABLE UNIT. ROBBED FROM 350SH. 1G71 3U3 UNCH9EU E19EU 20041124000862004112400086EA 2004 11 24 A6WA200440133 120040909A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31438AW 7748 MWC 121, LIGHTNING STRIKE DAMAGE AT FS 202.75, STR 22R. BLEND DAMAGED AND ENSURED AREA IS CRACK FREE IAW REO 601R-53-11-814. 2L72 4F4 FRTA21EA E15NE 20041124000882004112400088NM 2004 11 24 GAIA04171OP 120041019A7500BACG10R3816 GASKET BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NR 3 ENGINE BLOWN A GAIAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW07284KH 21108 657572 DURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BLOWN GASKET AND LOOSE CLAMPS AND DUCT LEAKS. REMOVED AND REPLACED GASKET AND TIGHTENED CLAMPS. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20041124000892004112400089 2004 11 24 A6WA200440145 420041010A2210 COMPUTER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PITCH CONTROL MALFUNCTIONED A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31449AW 7818 ON COMMAND OF AUTOPILOT DISENGAGEMENT, PITCH CONTROL DID NOT DISENGAGE FOR APPROX 5-10 SECONDS. 2L72 4F4 FRTA21EA E15NE 20041124000912004112400091EA 2004 11 24 A6WA200440137 120040921A5320 SUPPORT CHANNEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31402AW 7281 MWC 189, CARGO DOOR FORWARD TACK SUPPORT CHANNEL IS CRACKED. REMOVED CRACKED SUPPORT CHANNEL AND INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-42-06. 2L72 4F4 FRTA21EA E15NE 20041124000922004112400092NM 2004 11 24 M562004F00003 120040704A5347 SEAT TRACK BOEING737 737400 138449ANM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED I M56BK NONE O OTHER ININSP/MAINT 1 EA0537NY 23976 LT IB SEAT TRACK HAS SURFACE CORROSION FROM STA 348-370. REMOVED AND REPLACED SEAT TRACK. C1, C2, C3 INSP 8/4/04. 2L72 4F4 FRTA16WE E21EU 20041124000932004112400093EU 2004 11 24 ASOA04820 120041004A5312 PRESSURE PANEL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE PRESSURE WEB BETWEEN FR39 AND FR40 ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PRESSURE WEB BETWEEN FR39 AND FR40 ON THE RT SIDE IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041124000962004112400096NE 2004 11 24 ALG2004F00061 120040916A261230326E7 AMPLIFIER SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL NR 1 FIRE WARN INOPERATIVE E ALGAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW03702AL 760243 ON TAKE OFF, IN FLIGHT THE NR 1 FIRE WARNING LIGHTS AND TONE CAME ON, HAD NO OTHER INDICATION OF FIRE. MAINTENANCE REMOVED CONTROL AMPLIFIER AND INSTALLED SERVICEABLE AMPLIFIER, OPS CHECK WAS GOOD. 1G72 3U3 U H1NE E1GL 20041124000972004112400097SW 2004 11 24 ALG2004F00063 120040831A2821 DRAIN BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL FUEL FILTER OPEN E ALGAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW03116AL 2389 CAE834402 AFTER TAKE OFF, WAS NOTIFIED BY RADIO OF LEAKING FUEL IN FLIGHT, LANDED, EVACUATED PASSENGERS AND PERFORMED EMERGENCY SHUTDOWN, NOTIFIED MAINTENANCE. MAINTENANCE FOUND EXTERNAL FUEL FILTER DRAIN OPEN, CLOSED DRAIN, COMPLIED WITH GROUND RUN LEAK CHECK, NO DEFECTS NOTED. 1G71 3U3 U H2SW E4CE 20041124000982004112400098NM 2004 11 24 USAA040794 120041019A5320 INTERCOSTAL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, INTERCOSTAL, .5000 INCH AND .2500 INCH, 2 BRACKETS, CORROSION; NO LEVEL OR TASK. E11 DOOR FRAME AT SWITCH NR 3196 INSIDE OF FRAME, BL0, STA 203.8. FABRICATED ANGLES, REPLACED IAW SRM 53-00-04. 2L72 4F4 FRTA16WE E2GL 20041124001002004112400100EU 2004 11 24 ALG2004F00065 120040909A7712 WARNING LIGHT UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE ENGINE FALSE ACTIVATIONE ALGAA UNSCHED LANDING J WARNING INDICATION HOHOVERING 1 SW03526AL 1281 34087 ARRIVED AT E1107A TO PICK UP 1 PASSENGER, LOADED PASSENGER WHILE RUNNING. COMPLETED THE PRE TAKEOFF CHECKS AND BROUGHT AIRCRAFT TO A HOVER. DURING TAKEOFF THE 1.5 SECOND WARNING WENT OFF AND NOTICED THA THE TORQUE ON THE VEMD WAS UNDERLINED AND THE NEEDLE HAD BOUNCED PAST THE MAX LIMIT. EVENT OCCURRED DURING HOVER FLIGHT IAW PILOT OVER TORQUE INSPECTION WAS PERFORMED IAW CHAPTER 05-50-00602 OF THE MM, NO DEFECTS NOTED. 1G72 3U3 UNCR0001RD E34NE 20041124001012004112400101SW 2004 11 24 KBM2004F00232 120040917A6320206031509001 DRAG PIN BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL M/R GEARBOX CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 SPIKE MOUNT CRACKED JUST FORWARD OF DOG LEG RADIUS. CAUSE UNKNOWN, SENT FOR EVALUATION. INSTALLED SERVICEABLE SPIKE MOUNT. 1G71 3U3 U H2SW E4CE 20041124001052004112400105NM 2004 11 24 ASAA0470015 120040830A5320BAC1496377 ANGLE BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 Z-ANGLE CORRODED. REPLACED Z-ANGLE. 2L72 4F4 FRTA16WE E00055EN 20041124001082004112400108NM 2004 11 24 USAA040819 120040828A5754 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 1 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2L72 4F4 FRTA16WE E2GL 20041124001122004112400112NM 2004 11 24 ASAA0410405 120040928A5330654776531 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2L72 4F4 FRTA16WE E2EA 20041124001152004112400115EA 2004 11 24 A6WA200440169 120041028A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SERVICE DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 SERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAMP PLATE IAW SRM 51-41.02. 2L72 4F4 FRTA21EA E15NE 20041124001162004112400116NM 2004 11 24 USAA040823 120040829A5320 CLIP BOEING BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 CLIP, EST. .125 INCH CRACK, STA 500D SGL. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, 51-40. 2L72 4F4 FRTA16WE E2GL 20041124001192004112400119NM 2004 11 24 GAIA04153 120040910A5315 FLOORBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE MISMANUFACTURED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND CABIN FLOORBEAM IS NOT IAW DWG NR 2902. REF FASI NR 86793 REMOVED AND REPLACED FLOORBEAM IAW DWG NR 2902 AND SRM 53-10-2, FIG 7. 2L73 4F4 F A3WE E2EA 20041124001202004112400120EA 2004 11 24 ASOA04785 120041008A5210 BEARING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE EXTREMELY DIFFICULT TO CLOSE AND OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR INNER BEARING ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041124001212004112400121SW 2004 11 24 ALG2004F00059 120041011A6230 WARNING LIGHT BELL 214 214ST 1182106SW GE CT7TS CT72A 30030NE TRANSMISSION ACTIVATED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03392AL A96 28114 FIVE MINUTES AFTER TAKEOFF, AC815 TRANSMISSION CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. MECHANIC REMOVED, CLEANED, AND INSPECTED ALL TRANSMISSION CHIP PLUGS, NO CONTAMINANTS NOTED. CONNECTOR PLUGS WERE EXAMINED AND FOUND SERVICEABLE. AC WAS RETURNED TO SERVICE. 2G72 4U4 U H10SW E8NE 20041124001222004112400122EA 2004 11 24 A6WA200440134 120040909A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31438AW 7748 MWC 122, LIGHTNING STRIKE DAMAGE AT FS 235.00, STR 15R. BLENDED DAMAGE AND ENSURED ARE IS CRACK FREE IAW REO 601R-53-11-814. 2L72 4F4 FRTA21EA E15NE 20041124001242004112400124NM 2004 11 24 USAA040810 120040828A5340 STRINGER CLIP BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, STRINGER CLIPS, .5000 INCH AND .1250 INCH CRACKS, STA 578, STR S9R. CLIP REPLACED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E2GL 20041124001252004112400125NM 2004 11 24 USAA040807 120040909A5531 SPAR BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, ANGLE SUPPORT .7500 INCH CRACK, VERT STAB SPAR ANGLE FOR RIB 163.90 FRONT LT SIDE. INSTALLED DOUBLER AND SHIM IAW EA 79100. 2L72 4F4 FRTA16WE E2GL 20041124001272004112400127NM 2004 11 24 GAIA04150 120040910A5300 SEAT TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE MISMANUFACTURED A GAIAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND CABIN SEAT TRACK BS 344-480, RBL45.5 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902. 2L73 4F4 F A3WE E2EA 20041124001282004112400128NM 2004 11 24 GAIA04166 120040910A5754 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 5 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED. REF FASI NR 87058, INSTALLED REPAIR DOUBLER IAW SRM 57-50-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124001292004112400129NM 2004 11 24 GAIA04172OP 120041029A33501000679 LIGHT BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE COCKPIT INOPERATIVE A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07751US 21513 NO FLIGHT FWA: COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041124001302004112400130EU 2004 11 24 SIMA200426910 120040925A3397 TERMINAL SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE EMERGENCY LIGHT LOOSE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21391AE 340B391 DURING ROUTINE SCHEDULED MAINTENANCE IT WAS NOTED THE OVERHEAD EMERGENCY LIGHT AT SEAT 10A WAS INOPERATIVE. LIGHT WAS DEFERRED IAW MEL AT THIS TIME AND AC WAS RETURNED TO SERVICE. MAINTENANCE FOUND A LOOSE WIRE AT ROW 10A. WIRE TERMINAL END WAS RESECURED. OPERATIONAL CHECK WAS GOOD AND AC WAS RETURNED TO SERVICE. (SW21200500057) 2L72 4T4 TRTA52EU E8NE 20041124001312004112400131CE 2004 11 24 WVE2004F00022 120040909A5630660011510 WINDOW LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP EMERGENCY EXIT CRACKED B WVERK NONE O OTHER ININSP/MAINT 1 EA09931FD 124 DURING ROUTINE MAINTENANCE THE CABIN WINDOW IN THE EMERGENCY EXIT WAS FOUND CRACKED BEYOND LIMITS. NEW WINDOW SN 5754 RECEIVED FOR REPLACEMENT, INSTALLED IAW MM, SEALANT INTRUDED BETWEEN THE WINDOW PLIES AT THREE HI-LOCKS. WINDOW AGAIN WAS REPLACED. REPLACEMENT WINDOW INSTALLED AND NO PROBLEMS NOTED. MANUFACTURE EVALUATE. (EA09200403044) 2L72 4F4 FRTA10CE E6WE 20041124001332004112400133EA 2004 11 24 ASOA04828 120041024A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED AT THE AFT IB CORNERS UNDER THE ACCESS PANEL BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES IAW EO 600-53-0070. 2L72 4F4 FRTA21EA E15NE 20041124001342004112400134EA 2004 11 24 ASOA04833 120041024A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE RT CLIP AT FS 625 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT CLIP AT FS 625 IAW SRM 51-42-00. 2L72 4F4 FRTA21EA E15NE 20041124001372004112400137NM 2004 11 24 AMTA200401346 120041101A5330 DOUBLER BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 REMOVE EXISTING DOUBLER AND ACCOMPLISH FWD LAV (A) UPPER ATTACHMENT REINFORCEMENT DOUBLER EO 75725AD2937. REPLACED EXISTING DOUBLER WITH REINFORCEMENT DOUBLER IAW EO757-25AD-2937. 2L72 4F4 FRTA2NM E12EU 20041124001392004112400139NM 2004 11 24 USAA040820 120040901A5310 CREASE BEAM BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT, Q5, CREASE BEAM WEB 1 INCH CRACK. LT CREASE BEAM BS 616-639. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041124001412004112400141NM 2004 11 24 GAIA04143 120040910A5314 ANGLE BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE KEELBEAM CRACKED A GAIAO OTHER O OTHER NRNOT REPORTED 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND KEELBEAM PANEL COVER ANGLE CRACKED LT SIDE BS 870. REF FASI NR 86737 CUT OUT DAMAGED AREA DIM 1 X 8 INSTALLED ANGLE REPAIR IAW SRM 51-40-3. 2L73 4F4 F A3WE E2EA 20041124001432004112400143EA 2004 11 24 ASOA04771 120040928A4930S9412138 O-RING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU LEAKING A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27823AS P949 7196 DURING CRUISE, THE CREW NOTICED A SUBTLE ODOR OF FUEL/OIL PERMEATING THE COCKPIT AND CABIN. THE AIRCRAFT LANDED SAFELY. UPON INSPECTION FUEL WAS FOUND LEAKING FROM THE AUSILIARY POWER UNIT(APU). MAINTENANCE REMOVED AND REPLACED THE APU FUEL FILTER HOUSTIN O-RING. OPS AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041124001442004112400144NM 2004 11 24 ASAA0470016 120040830A5753113A39107 CARRIAGE BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE TE FLAP UNKNOWN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02624AS 30778 MODIFICATION OF FLAP CARRIAGE REQUIRED. ACCOMPLISHED EA 5750-01976. 2L72 4F4 FRTA16WE E00055EN 20041124001452004112400145NM 2004 11 24 GAIA04116 120040910A5230 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE C-3 DOOR DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND CREASE IN C-3 DOOR SKIN AFT EDGE AT STR 22, RT. REF FASI NR 86524, CUT OUT DAMAGE AREA DIM 1.50 X 1.25 INSTALL DOUBLER REPAIR IAW SRM 52-003, FIG 3. 2L73 4F4 F A3WE E2EA 20041124001482004112400148EA 2004 11 24 ASOA04829 120041024A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED AT THE FIRE LOOP CLIP BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 60053-0072. 2L72 4F4 FRTA21EA E15NE 20041124001492004112400149EU 2004 11 24 ASOA04830 120041024A3350E0062B1A4AC0A SWITCH AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT MALFUNCTIONED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING A GROUND INSPECTION, THE COCKPIT EMERGENCY LIGHT SWITCH FAILED. WHEN SELECTED TO THE ARM POSITION THE LIGHTS ARE ON AND WHEN SELECTED TO THE ON POSITION, THE SWITCH SPRINGS BACK TO THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IAW ATR 72-JIC 33-51-07. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20041124001502004112400150EA 2004 11 24 ASOA04837 120041026A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105. 2L72 4F4 FRTA21EA E15NE 20041124001522004112400152SO 2004 11 24 SIMA200427906 120040929A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21834AE4998 145631 LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT SECTION OF THE LT OMEGA BEAM. FABRICATED AN EXTERNAL DOUBLER, PLATE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-21-10. (SW21200500286) 2L72 4F4 FRTT00011ATTE6CH 20041124001532004112400153EU 2004 11 24 ASOA04832 120041024A33503011210 LIGHT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE PAX DOOR INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS2279 383 DURING AN A-CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041124001562004112400156EA 2004 11 24 ASOA04834 120041024A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A C-CHECK, THE OB CLIPS AT FS 625, STRINGER 15R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 625, STRINGER 15R IAW SRM 51-42-00. 2L72 4F4 FRTA21EA E15NE 20041124001582004112400158NM 2004 11 24 USAA040809 120040903A575465C266022 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INSTALLED NEW TOP SKIN IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041124001592004112400159EA 2004 11 24 ASOA04800 120041015A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A C-CHECK, THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO 601R-53-61-1179. 2L72 4F4 FRTA21EA E15NE 20041124001602004112400160EA 2004 11 24 A6WA200440175 120041027A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MAINS MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31406AW 7402 WHEN C/W QRH FOR GEAR DISAGREE, MLG DID NOT EXTEND WHEN LANDING. MANUAL RELEASE HANDLE WAS PULLED PERFORMED OPS TEST OF MANUAL RELEASE SYSTEM FOR LANDING GEAR. NO FAULTS FOUND, ALL CHECKED IAW AMM32-34-00. 2L72 4F4 FRTA21EA E15NE 20041129000042004112900004NM 2004 11 29 USAA040746 120041010A52306547952524 STIFFENER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU AFT CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52509 23856 PIT, C5; STIFFENER ANGLE, 3.5 INCH CRACK, LOWER AFT CORNER OF CARGO DOOR IN STIFFENER ANGLE. DEFECTIVE PART REPLACED WITH IDENT PN IAW JOB CARD J3-51-52301. 2L72 4F4 FRTA16WE E21EU 20041129000052004112900005NM 2004 11 29 USAA040750 120041015A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US54028 22958 PIT, C3; SKIN, .2500 INCH CRACK, BETWEEN STR 13/16R AND FRA 947.5. 11 INCH W X 9.5 INCH H FILLER, ALONG WITH 10 INCH W X 13.5 H DOUBLER IAW SRM 53-60-01, FIG 207. 2L72 4F4 FRTA16WE E2GL 20041129000072004112900007CE 2004 11 29 GUU2004F00037 120041029A21507756355 ACM BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE CABIN COOLING INOPERATIVE A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO1787554 UE227 DURING FLIGHT, STRONG EXHAUST ODOR IN COCKPIT AND CABIN WHEN BOTH BLEEDS ARE OPEN. DISSIPATES SOME WITH BLEED IN ENVIRONMENTAL OFF. MAINTENANCE FERRY. REMOVED AND REPLACED AIR CYCLE MACHINE. OPERATIONAL CHECKS NORMAL. 2L72 4T4 TRTA24CE E26NE 20041129000122004112900012NM 2004 11 29 USAA040744 120041011A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52509 23856 PIT, C5; SKIN WITH .5 INCH GOUGE, STA 767 AT 22L JUST BELOW STRINGER. DRILLED HOLE TO .250 INCH DIA, INSTALLED RIVET WET IAW SRM 53-00-01, FIG 219. 2L72 4F4 FRTA16WE E21EU 20041129000162004112900016CE 2004 11 29 GUU2004F00039 120041031A28203037677 LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE LEAKING A GUUAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO1787554 UE227 DURING FLIGHT, STRONG EXHAUST ODOR PRESENT IN AIRCRAFT WITH BLEED OPEN. REMOVED AND REPLACED FUEL LINE AT LT ENGINE COMPRESSOR INLET. OPERATIONAL CHECKS NORMAL. NO SMELL NOTED. 2L72 4T4 TRTA24CE E26NE 20041129000202004112900020NM 2004 11 29 UIEA200400191 120041112A542065B94109 STRAP BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 4 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE, FOUND CRACK NR 4 PYLON AT AFT MOUNT BULKHEAD FRAME STRAP. SUBJECT CRACK WAS LOCATED ALONG THE STRUT UPPER SKIN ASSY LOWER EDGE. CRACK AFT END WAS CONTAINED WITH A STOP HOLE IN THE STRAP. THE REPAIR AREA WAS NDT INSPECTED, INCLUDING HFEC INSPECTION OF ALL REPAIR HOLES. THE AREA WAS REINFORCED WITH TWO EXTERIOR 0.063 INCH THICK LAYERS OF TITANIUM DOUBLERS WITH PROFILES TO MATCH THE BULKHEAD STRAP PROFILE AND SPAN ACROSS THE SUBJECT CRACK. THE REPAIR AREA IS TO BE REPEAT DETAIL VISUAL INSPECTED EVERY 18 MONTHS OR C-CHECK INTERVAL, 2L74 4F4 F A20WE E23EA 20041129000212004112900021NM 2004 11 29 UIEA200400197 120041115A5754 SPAR BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 16 KRUG FLAP CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 16 KRUEGER FLAP FRONT SPAR. TRIMMED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FILLERS AND REPAIR CHANNELS. REFINISHED SPARS TO DESIGN STANDARD. DETAIL VISUAL INSPECTION TO BE ACCOMPLISHED OF THE REPAIR AREA AT C-CHECK INTERVALS, NOT TO EXCEED 18 MONTHS, FOR SIGNS OF DEGRADATION INCLUDING CRACKS, CORROSION AND LOOSE FASTENERS. TO ISSUE EO TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2L74 4F4 F A20WE E23EA 20041129000222004112900022NM 2004 11 29 UIEA200400194 120041115A542065B9081351 FAIRING BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 2 PYLON DELAMINATED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, DELAMINATION WAS FOUND ON NR 2 PYLON FAIRING ASSY. AT THE AFFECTED AREA, SKIN AND CORE WERE TRIMMED FROM THE OB SKIN SIDE AND REPLACEMENT CORE AND SKIN WERE SPLICED BY BONDING IAW SRM 51-40-06. IT WAS FURTHER REINFORCED BY LOCAL DOUBLER WITH POTTED FASTENERS. PERFORM DETAIL VISUAL INSPECTION, INCLUDING COIN TAP OF THE FAIRING AT THE SUBJECT REPAIR AREAS, EVERY C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST, FOR DELAMINATION, CRACKING OR LOOSE FASTENERS. EO TO BE ISSUED TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2L74 4F4 F A20WE E23EA 20041129000232004112900023EA 2004 11 29 ASOA04789 120041009A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX LACK OF LUBE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27833AS 7246 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR PANELS, LUBRICATED THE DOOR PIVOT POINTS AND CYCLED THE DOOR SEVERAL TIMES. NO DEFECTS WERE NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129000252004112900025NM 2004 11 29 C7WA200400045 120040922A5330 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 FUSELAGE LOWER SKIN AT STA 720B, STR 28 RT CORRODED. INSTALLED EXTERNAL SKIN REPAIR IAW SRM 53-30-3, FIG 1 DOUBLER MATERIAL USED, 2024-T3 X.160 INCH X 27 INCHES X 28.5 INCHES. 2L73 4F4 F A3WE E2EA 20041129000302004112900030EA 2004 11 29 ZJW2004F00000 220041026A8520 CRANKCASE GULSTM500 500B 0141106SW LYC O540 IO540B1A5 41532EA ENGINE DAMAGED E ZJWAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE05411JF 500B101435 L853948 ENGINE LOST POWER DUE TO LOSS OF OIL. ENGINE WAS CAGED IN OMA AND LANDED SAFELY. GROUND INSPECTION SHOWED HOLE IN CRANKCASE. PROBABLY ROD CAP SEPARATION DUE TO ROD BEARING FAILURE. 1H72 3O3 O 6A1 1E4 20041129000312004112900031SO 2004 11 29 63710112004 120041011A2750 CONTROL SYSTEM GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE TE FLAPS MALFUNCTIONED E N93AO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO13509QS 637 ON TAKEOFF WHEN FLAPS WERE SELECTED UP THE STOPPED AT APPROX 7 DEGREES. FLAPS WERE CYCLED BUT THEY WOULD NOT MOVE (UP AND DOWN). ON TAXI IN, HOWEVER THE FLAPS WERE SELECTED TO 10 DEGREES THEN UP. THEY WENT UP AND ARE WORKING NORMAL. TECH DISPATCHED PERFORMED OPERATIONAL CHECK OF SYS, NO FAULT FOUND. AIRCRAFT DEPARTED AND ARRIVED AS SCHEDULED. 2L72 4F4 FRTA12EA E00057EN 20041129000352004112900035EA 2004 11 29 A6WA200440170 120041028A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FS 280 UNDER FLOORBEAM AT RBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FABRICATED REPAIR ANGLE AND FILLER FROM S-6744-3 AND S6744-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK FASTENERS. ALL WORK DONE IAW REO 601R-53-11-131 REV A AND EO 601R-53-5547. 2L72 4F4 FRTA21EA E15NE 20041129000382004112900038SO 2004 11 29 SIMA200428403 120041010A3350110049 POWER SUPPLY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21656AE 145740 CREW REPORTED THE AFT SECTION, ROW 12, FLOOR PROXIMITY, OVERHEAD EXIT LIGHT, AND SEVERAL FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 POWER SUPPLY TO CORRECT THE PROBLEM. THE NR 1,3, AND 4 POWER SUPPLY UNITS AND ALL 4 BATTERIES WERE ALSO CHANGED AS A PRECAUTION. ALL WORK AND OPERATIONAL CHECKS WERE DONE IAW THE MM. (SW21200500265) 2L72 4T4 FRTT00011ATTE6CH 20041129000392004112900039EA 2004 11 29 A6WA200440148 120041001A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31435AW 7724 CARGO FLOOR LANDING PLATE HAS MINOR CLASS 1 CORROSION AT FLOOR PANEL ANCHOR NUTS IN AREA OF CARGO DOOR OPENING. REMOVED MINOR CLASS 1 CORROSION IN AREA OF AFT CARGO ANCHOR NUTS BY HAND. BURNISHING WITH SCOTCHBRITE IAW SRM 51-21-11 PG 31. TREATED, PRIMED AND PAINTED AREAS IAW SRM 51-21-06, PG 1. 2L72 4F4 FRTA21EA E15NE 20041129000432004112900043NM 2004 11 29 USAA040801 120041002A5320 FLOOR SUPPORT BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US22956 22956 PIT, Q5, FLOOR SUPPORT WITH .2500 INCH X .3750 INCH CRACKS, END OF FLOOR SUPPORT, STA 540 LT AND RT OF BL-0. REMOVED AND REPLACED IAW SRM 53-21-00. 2L72 4F4 FRTA16WE E2GL 20041123000432004112300043NM 2004 11 23 DHL2004747007 120041110A3234 CONTROL LEVER BOEING727 727224 1384076NM MLG OUT OF ADJUST A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01747DH 22253 DURING TAKEOFF ROLL AT MIO LEFT MAIN GEAR UNSAFE LIGHT FLICKERED OFF AND ON. OPS CHECKED LANDING GEAR CONTROL LEVER POS SWITCH IAW ASTAR MM 32-61-11 PG 401. INDICATIONS NORMAL AT THIS TIME. ALT TEST OK MM 32-61-21 PG 501. 2L73 4F A3WE 20041123000482004112300048SO 2004 11 23 C2XA04IA112 120040829A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714938 145029 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED AISLE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041123000552004112300055NM 2004 11 23 SWAA043380 120041118A5310571769 WINDOW POST BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND F/O'S NR 1 WINDOW UPPER OUTBOARD POST CRACKED. REPAIRED NR 1 WINDOW POST PER SRM. 2L72 4F RTA16WE 20041123000592004112300059SO 2004 11 23 C2XA04RI012 120041102A27503631001007 CONTROL UNIT EMB 145 EMB145LR 3260212SO TE FLAPS INOPERATIVE A C2XAO OTHER J WARNING INDICATION APAPPROACH 1 SW27169763936 145171 CREW REPORTED FLAP FAIL AND SPS ADV FAIL MESSAGES ON EICAS DURING LANDING. CREW DECLARED EMERGENCY AND LANDED WITH OUT INCIDENT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041123000612004112300061CE 2004 11 23 DXTA200400381 120040906A282123061826 FUEL FILTER CESSNA750 750 2076810CE RT ENGINE BYPASSING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07937QS 7500137 FUEL FILTER BYPASS -R- CAS MESSAGE ILLUMINATED DURING TAKEOFF ROLL AT 50 KTS ALL OTHER INDICATIONS NORMAL, ABORTED TAKEOFF. REMOVED AND REPLACED FUEL FILTER ON RIGHT ENGINE REF ROLLS ROYCE MM CHAPTER 73-30-00. OPS CHECK AND LEAK CHECK GOOD, INSPECT BYPASS IMPENDING BUTTON FOUND LINT IN FILTER, BUT NO METAL. 2L72 4J RTT00007WI 20041123000632004112300063CE 2004 11 23 CQWR2004002 120040826A289765782324 WIRE HARNESS CESSNA CESSNA500 560CESSNA 2076750CE TRANSMITTER BURNED B DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL05342QS5585 1069A 5600324 DURING INSPECTION FOUND RT WING OUTBOARD FUEL QTY TRANSMITTER WIRING HARNESS BURNED BETWEEN WIRE SHIELDING AND TERMINAL. FILED SERVICE CONDITION REPORT 161544 WITH CESSNA/CITATION. COPIES OF REPORTS, SUPPORTING DOCUMENTATION AND PICTURES SENT TO PMI AND OPERATOR. 2L72 4F RTA22CE 20041123000852004112300085SO 2004 11 23 C2XA04SH548 120041107A532014521712005 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041123000882004112300088CE 2004 11 23 DXTA200400384 120040908A793223063236 SENSOR CESSNA750 750 2076810CE ENGINE OIL QTY FAULTY E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07986QS 7500086 AT 80 KIAS AMBER MASTER WARNING ILLUMINATED WITH LOW AMBER OIL LEVEL LOW-R CAS MESSAGE, TAKEOFF ABORTED. EICAS INDICATES 1 QUART LOW AND SIGHT GAUGE INDICATES 1 QUART LOW. REMOVED AND REPLACED FAULTY OIL LEVEL SENSOR. OPERATIONAL AND LEAK CHECK GOOD, WORK PERFORMED IAW ROLLS ROYCE AE3700C MM CHAPTER 79-35-20. 2L72 4J RTT00007WI 20041123000962004112300096NE 2004 11 23 SWAA043385 220041118A7200CFM563 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 1 OVERHEATED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW29626SW 27702 856644 AIR TURNBACK, NR 1 ENG EGT OVERHEAT LIGHT INDICATION ABOVE 55 PERCENT POWER. REMOVED AND REPLACED NR 1 ENG PER MM. 2L72 4F4 FRTA16WE E2GL 20041123001072004112300107NM 2004 11 23 UPS04443316 120040929A5711 SPAR BOEING747 747121 1384871NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, LEFT BS 1241 WL 180 WING REAR SPAR KICK FITTING NR 1 FASTENER HOLE CRACK REVEALED AT WEB FORWARD LAYER APPROX .0937 INCH IN LENGTH RUNNING O/B AND LOWER. LEFT BS 1241 WING REAR SPAR KICK FITTING NR 1 FASTENER HOLE REWORKED AS PER EO 5740-17032 WORK DETAIL. 2L74 4F A20WE 20041123001092004112300109NM 2004 11 23 UPS04243394 120041005A5340 FITTING BOEING727 727185C 138406NNM WING CENTER SECTCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C DURING REMOVAL OF RIGHT 740 FITTING CORROSION FOUND ON CENTER WING SECTION FRONT SPAR UPPER CHORD AT RBBL 65-70 APPROX CORROSION REMOVED IAW SRM 51-10-06. REPAIR ANGLES FABRICATED IAW SRM 53-30-03. HFEC CARRIED OUT ON ABOVE AREA IAW B727-NDTM 51-00-00 PT 6 FIG 4, NO DEFECTS FOUND. 2L73 4F A3WE 20041123001202004112300120EA 2004 11 23 QXEA200400772 120041110A324061903 FUSE CNDAIRCL600 CL6002C10 1390015EA BRAKES FAILED A QXEAO OTHER J WARNING INDICATION LDLANDING 1 NM09607QX7912 10024 PDX - FLIGHT 2556 - THE CREW REPORTED SUBSTANTIAL LEFT BRAKE FADE DURING LANDING. THE LT OUTBOARD BTMS INDICATES 04 AND THE LT INBOARD BTMS INDICATES 00. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NR 2 VOLUMETRIC FUSE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041123001212004112300121CE 2004 11 23 DXTA200400341 120040717A3250 LINKAGE CESSNA750 750 2076810CE STEERING TILLER DISCONNECTED E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07987QS4427 7500087 NOSE WHEEL STEERING (TILLER AND PEDALS) FAILED ON TAXI IN, NO CAS MESSAGES RECEIVED. HYDRAULIC QUANTITY/PRESSURE WAS GOOD (55 PERCENT /3100 PSI), AIRCRAFT WAS TOWED BACK IN. REMOVED POWER STEERING UNIT AND REPLACED WITH OVERHAULED UNIT, INSPECTED LINKAGE FROM TILLER WHEEL TO MIXER AND NOTED DISCONNECTED. OBTAINED NEW CONTROL ASSEMBLY CABLE AND INSTALLED ON AIRCRAFT, PERFORMED RIGGING OF ENTIRE SYSTEM TRAVEL AND TENSION CHECKS/OPS CHECK GOOD. PERFORMED TAXI TEST, AIRCRAFT TAXIS GOOD ALL WORK IAW 750 M/M CHAPTER 32-50-00. 2L72 4J RTT00007WI 20041123001222004112300122CE 2004 11 23 DXTA200400340 120040716A783021681 LIMIT SWITCH CESSNA500 560CESSNA 2076750CE THRUST REVERSER MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07334QS 5600434 DURING FLIGHT THE LT THRUST REVERSER LIGHT CAME ON, ACCOMPLISHED AIR TURNBACK TO PBI. REMOVED RIGHT AND LEFT DEPLOY SWITCHES FROM LEFT THRUST REVERSER, INSTALLED NEW SWITCHES. ALL WORK DONE IAW CITATION 560 WIRING MANUAL CHAPTER 78-30-01. PERFORMED OPERATIONAL CHECK AND FLIGHT, SYSTEM OPS CHECKED GOOD. 2L72 4F RTA22CE 20041123001402004112300140EU 2004 11 23 MALA040639 120040910A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15418XJ 340B418 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON FLOOR FRAME STRUCTURE STA 231 TO 288 AND RBL 36 TO LBL 36. AREAS OUT OF LIMITS, REPAIRED PER THE SRM. AIRCRAFT RETURNED TO SERVICE 9/11/2004. 2L72 4T RTA52EU 20041123001522004112300152NM 2004 11 23 UPS04243237 120040909A1430NAS11057 BOLT BOEING727 727173C 1384059NM NR 2 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, NR 2 ENG MOUNT FITTING RIGHT SIDE HAS ONE CORRODED ATTACH BOLT ON UPPER SURFACE OF HORIZONTAL FIRE WALL. BOLT REPLACED. 2L73 4F A3WE 20041123001612004112300161WP 2004 11 23 0401729604 120040925A5320 STIFFENER DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING H-CHECK FOUND CRACK IN VERTICAL STIFFENERS AT BS 756 BULKHEAD X=22 AND X=-22. REPAIRED PER EA 96-199903. 2L72 4F A6WE 20041123001622004112300162EA 2004 11 23 04317650 120041112A3050 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA STAB TRIM ACTIVATED A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27650BR 7418 CREW REPORT STATED THAT STAB/MACH TRIM CAUTION MESSAGE DURING DESCENT INTO IAD. PERFORMED BITE SYSTEM TEST OF STAB/MACH TRIM IAW MM 27-41-00. 2L72 4F RTA21EA 20041123001632004112300163NM 2004 11 23 UPS04443474 120041111A335060B400534 BATTERY BOEING747 747123F NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE:N/A CREW SERVICE DOOR EMERGENCY SILL LIGHTS INOPERATIVE. REPLACED X327 EMERGENCY LIGHT BATTERY POWER UNIT FOR X-326 AND X325, LIGHTS OPS CHECKS GOOD. 2L74 4F A20WE 20041123001702004112300170SO 2004 11 23 C2XA04IA123 120040923A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714974 145161 OKC - FLIGHT 2964, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS BETWEEN ROWS THREE AND SEVEN DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPS CHECKED WITH NO DEFECTS ALL IAW EMB-145 MM 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041123001712004112300171NM 2004 11 23 SWAA043297 120041110A5315BAC1509100146 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29757LV 29850 DURING SCHEDULED 5Y CHECK, FOUND FLOORBEAM AT BS 772, BETWEEN LBL 3 AND RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041123001852004112300185EA 2004 11 23 COMA0460604 120041108A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 FS 574 FRAME SUPPORT ANGLE HAS MISDRILLED HOLD. REPAIRED IAW REO 601R-53-61-1187. 2L72 4F RTA21EA 20041123001952004112300195NM 2004 11 23 UPS04M43292 120040729A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, HORIZONTAL STAB NR 34 LEFT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 34 LEFT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 34 LEFT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 34 LEFT PER EO MD11-5510-19409-H & EN 1282-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123002022004112300202EA 2004 11 23 COMA0460606 120041108A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01783CA 7315 CARGO DOOR LANDING PLATE IS CRACKED AT FS 574. REPAIRED IAW REO 601R-53-61-690. 2L72 4F RTA21EA 20041123002082004112300208NM 2004 11 23 UPS04243405 120041005A2710 FITTING BOEING727 727185C 138406NNM LT OB AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C, LEFT O/B AILERON TAB MAST FITTINGS HAVE PITTING CORROSION AROUND BUSHINGS. ON INVESTIGATION LEFT O/B AILERON TAB FITTINGS FOUND TO BE OUTSIDE LIMITS. LEFT O/B AILERON TAB REPLACED IAW 27-10-19. 2L73 4F A3WE 20041123002122004112300212 2004 11 23 SWAA043287 420041110A25656949956 CABLE BOEING737 7373H4 1384600NM SLIDE GIRT BAR MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED RON, FOUND L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED CABLES PER MM. 2L72 4F RTA16WE 20041123002132004112300213NM 2004 11 23 UPS04243410 120041011A5320 INTERCOSTAL BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, ON REMOVAL OF INTERCOSTAL TO FACILITATE RIGHT FITTING REPLACEMENT AT BS 740, A CRACK WAS FOUND. REPLACED INTERCOSTAL WEB IAW SRM 51-20-04. 2L73 4F A3WE 20041123002152004112300215NM 2004 11 23 UPS04243382 120041005A5730 SKIN BOEING727 727185C 138406NNM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, SUSPECT CRACK AT FWD UPPER CORNER OF LEFT WING ICE LIGHT CUTOUT. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED, ENDS MARKED. DOUBLER AND FILLER INSTALLED IAW SRM 53-30-03. WEIGHT OF REPAIR 2.37 LBS. 2L73 4F A3WE 20041123002212004112300221NM 2004 11 23 QXEA200400765 120041029A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 DELAMINATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - RIGHT HAND OUTBOARD FLAP HAS TWO AREAS OF DELAMINATION ON THE LOWER SURFACE. REPAIRED IAW RD 8/4-57-383 AND HORIZON AIR EA 6-57-247. 2H72 4T RTA13NM 20041123002282004112300228WP 2004 11 23 UPS04843372 120040924A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE: C, A-PIT DOOR AFT TORQUE BOX FS 340 FWD UPPER FRAME HAS EXFOLIATION CORROSION FROM L33R TO L34R. REPAIRED DAMAGED FRAME AT FS 340 IAW SRM 53-2-0 FIG 2. REMOVED, FABRICATED & INSTALLED 2 INTERCOSTALS IAW DWG 9754020 & SRM 51-1-21 & 51-1-21 & 51-1-20D. FABRICATED & INSTALLED REPAIR DOUBLER FOR TORQUE BOX WEB IAW SRM ADDENDUM DC8-5350-7876-A. 2L74 4F RT4A25 20041124000082004112400008NM 2004 11 24 GAIA04139 120040910A5730 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE LT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND LT WING L/E CAVITY WS110-130 FWD. SKIN BUCKLED AND CRACKED. REF FASI NR 86706, STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 12. 2L73 4F4 F A3WE E2EA 20041124000182004112400018NM 2004 11 24 GAIA04135 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND MAIN CABIN FRAME AT BS580 ABOVE STR17,STR16 RT, DENTED. REF FASI NR 86684, CUT OUT DAMAGE AREA DIM 1.0 X 6.0, INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000212004112400021SO 2004 11 24 SIMA200427907 120040929A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21834AE4998 145631 LT OMEGA BEAM BETWEEN FRAME 24 AND 25 WAS FOUND CORRODED. CUT OUT DAMAGED SECTION OF THE OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145-1142, REV 27) CHAPTER 53-22-10. (SW21200500286) 2L72 4F4 FRTT00011ATTE6CH 20041124000332004112400033 2004 11 24 REXA04023 420041026A2561 G SWITCH ARTEX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258696C4525 2472 01752 7696 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2L72 4F4 FRTA21EA E15NE 20041124000362004112400036SO 2004 11 24 SIMA200427913 120040930A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21835AE4976 145634 THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUT OUT A SECTION OF DAMAGED OMEGA BEAM. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-21-10, FIG 201. (SW21200500283) 2L72 4F4 FRTT00011ATTE6CH 20041124000392004112400039SO 2004 11 24 SIMA200427915 120041005A335066903 LIGHT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21726AE 145314 FORWARD FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPLACED FORWARD PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20041124000472004112400047SO 2004 11 24 SIMA200428702 120041006A532014521725001 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21623AE 145109 DURING MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED AREA TO REMOVE CORROSION. FABRICATED 2 INTERNAL DOUBLERS. REPAIR DONE IAW ETN EM 53-036R2. (SW21200500290) 2L72 4T4 FRTT00011ATTE6CH 20041124000512004112400051NM 2004 11 24 ASAA0410402 120040928A53306545776531 LAP JOINT BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON EXTERNAL SKIN LAP JOINT. REPAIRED DAMAGE ON SKIN LAP. 2L72 4F4 FRTA16WE E2EA 20041124000582004112400058 2004 11 24 ASOA04779 420041006A34100856KV10 PROBE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AIR DATA SENSOR BIRD STRIKE A O OTHER J WARNING INDICATION DEDESCENT 1 SO27846AS7037 7328 DURING FERRY FLT, RECEIVED NR 1 & 2 AIRSPEED, ALTITUDE FAIL MESSAGE. NR 1 HORIZ SITUATION INDICATOR WAS UP TO 45 FT OFF FROM STANDBY COMPASS. CREW ALSO RECEIVED GROUND PROXIMITY WARNING WITH GEAR WARNING HORN, FLAP WARNING ACTIVE. ALTITUDE INDICATIONS SHOWED NOSE LOW LT TURN WHEN ACTUALLY AC LEVEL IN RT TURN. EMERGENCY DECLARED, AC LANDED SAFELY. MAINT FOUND DAMAGED PITOT SYS FROM BIRDSTRIKE HAD NOT BEEN DEACTIVATED PROPERLY FOR FERRY FLT CAUSING STATIC SYSTEM TO BE PRESSURIZED. MAINT REMOVED & REPLACED PITOT/STATIC PROBE. OPS AND LEAK CHECKS GOOD. AC FERRIED, FOR COMPLETION TO REPAIR DAMAGE TO FUSELAGE FROM BIRDSTRIKE. 2L72 4F4 FRTA21EA E15NE 20041124000752004112400075NM 2004 11 24 GAIA04111 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED, RT FORWARD CORNER OF EE DOOR CUT OUT. REF FASI NR 86516, ACCOMPLISHED DOUBLER REPAIR IAW WITH SRB 53-30-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000872004112400087NM 2004 11 24 GAIA04167 120040910A5310 DOOR FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAO OTHER O OTHER NRNOT REPORTED 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR FRAME CRACKED AT UPPER AFT LATCH ROLLER. REF FASI NR 87126, ACCOMPLISHED WEB REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124001022004112400102NM 2004 11 24 GAIA04095 120040910A5754 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 5 SLAT DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND RT WING NR 5 SLAT L/E EXTERIOR SKIN RIPPLED AND DENTED ACROSS 2 RIB ASSY. REF FASI NR 86332, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124001062004112400106GL 2004 11 24 ALG2004F00069 220041025A7200 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 MAKING METAL E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03522AL 760236 CAE890100S ON CLIMB OUT NR 1 ENGINE CHIP LIGHT ILLUMINATED, PILOT RETURNED TO AIRPORT. THE MECHANIC REMOVED AND REPLACED NR 1 ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20041124001072004112400107NM 2004 11 24 GAIA04151 120040910A5347 SEAT TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE MISINSTALLED A GAIAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND SEAT TRACK NOT INSTALLED IAW DWG NR 2902. REF FASI NR REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902. 2L73 4F4 F A3WE E2EA 20041124001172004112400117NM 2004 11 24 USAA040795 120041023A5311 FRAME BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, FRAME .2500 INCH X .2500 INCH- 6 EA AREAS, CORROSION; LEVEL 1; TASK NR C53-208-01 AROUND FASTENER HOLES - STA 847 FRAME BETWEEN S26R, ES25R. SPLICED IN NEW FRAME SECTION IAW EA 79270. 2L72 4F4 FRTA16WE E2GL 20041124001182004112400118EA 2004 11 24 ASOA04803 120041015A5310 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A C-CHECK, THE LT AND RT SIDE ENGINE SUPPORT BEAMS AT BL36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT SIDE ENGINE SUPPORT BEAMS AT BL36.20 IAW EO600-53-0070. 2L72 4F4 FRTA21EA E15NE 20041124001232004112400123NM 2004 11 24 USAA040815 120040901A5320 CLIP BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE BULKHEAD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, CLIP 1 INCH CRACK, STR 19 AND STA 986 BULKHEAD. INSTALLED CLIP IAW SRM 5-40-02. 2L72 4F4 FRTA16WE E2GL 20041124001262004112400126NM 2004 11 24 GAIA04148 120040910A5347 SEAT TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE MISMANUFACTURED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK BS 344-480 LBL 45.5 NOT IN COMPLIANCE WITH DWG 2902. REMOVED AND REPLACED SEAT TRACK BS 344-480, LBL 45.5 WITH PN BAC 1520-792 IAW SRM 53-10-2, FIG 7 AND DWG 2902. 2L73 4F4 F A3WE E2EA 20041124001322004112400132CE 2004 11 24 WVE2004F00023 120040921A32306632303002005 CABLE LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE7312 01518WP MLG FREEFALL SYSMALADJUSTMENT B WVERO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA09416FX 113 LT AND RT GEAR IN TRANSIT LIGHTS REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE FREEFALL CONTROL LEVER WAS BUMPED OUT OF ITS NORMAL (UP) POSITION AND WHEN THE GEAR WAS SELECTED DOWN AND IT COMPLETED ITS CYCLE THE MAIN LANDING GEAR INBOARD DOOR FREEFALL CABLE WOULD NOT ALLOW THE IB MLG DOOR UPLOCK SWITCH TO SEND A CLOSE SIGNAL, BECAUSE IT WAS ADJUSTED TO TIGHT. PROPER ADJUSTMENT OF CABLE IAW MM 32-33-02. (EA09200403107) 2L72 4F4 FRTT00008WIE6WE 20041124001472004112400147EU 2004 11 24 Y2PA04024 120040922A3260327 LAMP AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE NLG INDICATOR BURNED OUT E Y2PAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL23827AA 298 NOSE GEAR INDICATOR LIGHT INOPERATIVE ON APPROACH. CREW CLIMBED OUT TO PERFORM CHECKLIST PROCEDURES. PROCEDURE B WAS USED. ALL INDICATIONS NORMAL EXCEPT FOR GREEN LIGHT. CREW PERFORMED A FLYBY OF THE TOWER AND TOWER CONFIRMED NOSE GEAR STRAIGHT AND NORMAL. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT SHUTDOWN ON TAXI WAY AND NOSE GEAR VISUALLY INSPECTED. GEAR APPEARED NORMAL AND AIRCRAFT TAXIED TO CUSTOMS. MAINTENANCE CONTACTED, VERIFIED THAT THE NOSE GEAR INDICATOR LIGHT (LAMP) WAS BURNED OUT. INDICATOR WAS RELAMPED AND THE OPS CHECK OF THE LIGHT WAS GOOD IAW MM. GEAR SWING NOT REQUIRED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A7EU E7EA 20041129000032004112900003NM 2004 11 29 USAA040749 120041006A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US 22958 PIT, C3; SKIN, (3 EA) CRACKS; 1 INCH, 2.7 INCHES AND 1 INCH, AFT OF 727E-747, S18R. INSTALLED REPAIRS IAW SRM 53-00-01, FIG 228. 2L72 4F4 FRTA16WE E21EU 20041129000062004112900006NM 2004 11 29 USAA040754 120041012A5314 KEELBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52509 23856 PIT, C5, KEELBEAM, 2 INCH LONG CRACK, KEELBEAM RT SIDE JUST AFT OF STA 540. INSTALLED REPAIR ANGLE IAW EA 79268. 2L72 4F4 FRTA16WE E21EU 20041129000082004112900008CE 2004 11 29 GUU2004F00035 120041105A324030204A BRAKE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT MLG MALFUNCTIONED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1781546 UE187 RT BRAKES INEFFECTIVE. REMOVED AND REPLACED NR THREE AND NR 4 BRAKE ASSEMBLIES OPERATIONAL CHECK NORMAL. 2L72 4T4 TRTA24CE E26NE 20041129000092004112900009NE 2004 11 29 GUU2004F00038 220041029A7314AN83312D ELBOW BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENG FUEL PUMPLOOSE A GUUAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SO1787554 UE227 DURING FLIGHT, STRONG EXHAUST ODOR IN COCKPIT AND CABIN SEEMED TO DISSIPATE WHEN LT ENVIRONMENTAL TURNED OFF. SECURED ELBOW AT LOW PRESSURE FUEL PUMP. NO LEAKS NOTED. OPERATIONAL CHECKS NORMAL. 2L72 4T4 TRTA24CE E26NE 20041129000102004112900010NM 2004 11 29 UIEA200400189 120041111A575365B149392 RIB BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE RT WING CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE. FOUND CRACK AT RT VARIABLE CAMBER FLAP HINGE RIB ASSEMBLY. TRIMMED THE FLANGE TO REMOVE THE DAMAGE. HFEC THE AFFECTED AREA TO ENSURE DEFECT FREE CONDITION. THE REPAIR AND RESTORATION WAS ACCOMPLISHED TO RESTORE TO THE ORIGINAL STRUCTURE. DETAIL VISUAL INSPECT THE AFFECTED AREA AT C-CHECK INTERVALS NOT TO EXCEED 18 MONTH FOR SIGNS OF CORROSION, CRACKS AND DEGRATION OF SUBJECT REPAIR. EO TO ACCOMPLISH INSPECTION AT 18 MONTH INTERVALS. 2L74 4F4 F A20WE E23EA 20041129000172004112900017NM 2004 11 29 UIEA200400188 120041108A793141809104 TRANSMITTER BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL OIL PRESSURE FAILED A UIEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA15498MC19300 29259 704925 NR 3 ENGINE OIL PRESSURE DROPPED TO RED LINE 30 MINUTES FROM DEPARTURE. ENGINE SHUTDOWN IAW CHECK LIST. REMOVED AND REPLACED THE OIL PRESSURE TRANSMITTER IAW AMM 79-32-01 AND REPLACED THE OIL PRESSURE SWITCH IAW AMM 79-33-01. 2L74 4F4 FRT1384945 E23EA 20041129000292004112900029SO 2004 11 29 130810132004 120041013A5210 SEAL GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU PAX DOOR DEFECTIVE E N93AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO13408QS 1308 ON TAKEOFF, DOOR SEAL EMITTED A LOUD SQUEAL AND POP. AFTER LANDING, DOOR SEAL WAS DEFLATED PRIOR TO OPENING MAIN CABIN DOOR. MAIN ENTRANCE DOOR SEAL INFLATION SYSTEM CONTAINED MOISTURE. INSTALLED DOOR SEAL MODIFICATION AC SERVICE CHANGE KITS-ASC 424 AND 438B-COMBINED KITS INTRODUCE NEW TUBING, VENT LINES, CONDENSER INSTALLATION PN 1159SB48802-27(TUBE). 1159SB48800-1(DUCT ASSY) 1159SB40709-21(VENT PLUG) 115SB48830-1/3(HOSE ASSY) REGULATOR PN 3215634-5 AND FILTER PN 31004. INTRODUCTION OF ASC ARE INTENDED TO EXTRACT EXCESS MOISTURE CONTENT IN SYS AND IMPROVEMENT OF MFG OF REGULATOR INCREASES FLOW AND IMPROVED FILTER INCREASES REMOVAL OF CONTAMINANTS. CABIN PRESSURIZATION WAS NOT LOST. 2L72 4F4 FRTA12EA E25NE 20041129000332004112900033EA 2004 11 29 ASOA04796 120041013A5210601R31707651 STEP CNDAIR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27719EV 10099 10099 DURING A C-CHECK, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. 2L72 4F4 FRTA21EA EOOO63EN 20041129000362004112900036SO 2004 11 29 637102404 120041023A27405913114 RESOLVER GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE STABILIZER DEFECTIVE E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13509QS 637 AT FL410 AFTER 3.1 HRS OF FLIGHT, RECEIVED AN AMBER (UNCMDED STAB) MSG ALONG WITH (FLAP STAB SYS FAIL) AND (FLAP STAB MAINT REQ) MSG. HORIZONTAL STABILIZER SYSTEM AND RESOLVER. VERIFIED RESOLVER (SATB) WIRING TO THE FCU. REMOVED AND REPLACED RESOLVER IAW GV MM 27-43-01 PG 401-403. COMPLIED WITH STAB RESOLVER. ADJUSTMENT IAW MM 27-43-01 PG 501-503. PERFORMED FLAP SYS OPERATIONAL CK IAW MM WITH NO DEFECTS NOTED. 2L72 4F4 FRTA12EA E00057EN 20041129000402004112900040NM 2004 11 29 USAA040804 120040910A5755 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR1 SPOILER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT, Q5, TOP SKIN - CORE BOND 1 INCH AREA, DELAMINATION, LT WING NR 1 SPOILER AT AFT OB CORNER - TOP SURFACE. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041129000452004112900045NM 2004 11 29 USAA040799 120041002A5315 FLOORBEAM BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, FLOORBEAM, 3 INCH CRACK (BROKEN) .400 INCH CRACK, STA 540 LBL 1 AND LBL 19 SUPPORT). REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 53-21-00. 2L72 4F4 FRTA16WE E2GL 20041129000462004112900046NM 2004 11 29 USAA040803 120040910A575465C266032 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA17383US55352 22956 PIT, Q5, TOP SKIN AND CORE BOND, 3.5 INCH AREA. DELAMINATION, NR 4 SLAT OB END TOP SURFACE. REMOVED DAMAGE, INSTALLED NEW CORE SECTION AND DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041129000482004112900048EA 2004 11 29 ASOA04811 120041020A2740 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE HORIZONTAL STAB MALFUNCTIONED A ASOAO OTHER G MULTIPLE FAILURE DEDESCENT 1 SO27856AS 7404 DURING DESCENT THROUGH APPROX 18,000 FT, THE STAB TRIM (BOTH CHANNELS) AND THE MACH TRIM DISENGAGED. THE CREW COMPLIED WITH THE QRH BY ATTEMPTING TO RESET THE STAB AND MACH TRIM WITH NO SUCCESS. THE CREW REQUESTED EMERGENCY VEHICLES BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY WITH THE FLAPS SELECTED TO 20 DEGREES. MAINT RESET THE HORIZONTAL STAB TRIM CONTROL UNIT AND STAB TRIM CHANNELS. MAINT ALSO DISENGAGED AND RE-ENGAGED THE STAB TRIM AND MACH TRIM SYSTEM NUMEROUS TIMES. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129000492004112900049EA 2004 11 29 ASOA04805 120041015A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING A C-CHECK, THE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS625. 2L72 4F4 FRTA21EA E15NE 20041129000512004112900051NM 2004 11 29 ASAA0410408 120040928A53306545767541 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSLEAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2L72 4F4 FRTA16WE E2EA 20041129000532004112900053EA 2004 11 29 ASOA04786 120041007A5320601R311719 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING A C-CHECK, THE IB INTERCOSTAL AT FS 484, RBL 27 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041129000542004112900054SW 2004 11 29 ALG2004F00067 120041027A5210 LATCH BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL PAX DOOR CRACKED E ALGAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 SW0315Q 2235 DURING FLIGHT, LT REAR PASSENGER DOOR POPPED OPEN IN FLIGHT AC LANDED ON SS154 THE DOOR WAS SHUT AND SECURED. AFTER TAKE OFF THE DOOR POPPED OPEN AGAIN AIRCRAFT LANDED. THE MECHANIC FOUND A 3 INCH CRACK ABOVE THE LOWER LATCH. THE DOOR WAS REMOVED AND REPLACED. 1G71 3U3 U H2SW E4CE 20041129000572004112900057SO 2004 11 29 145410082004 120041008A32601159SCAV4571 DOWNLOCK SWITCH GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU NLG FAILED E N93AO OTHER O OTHER NRNOT REPORTED 1 SO13454QS 1454 NOSE WHEEL STEERING FAIL MESSAGE ON LANDING. NOSE WHEEL STEERING INOPERATIVE. TROUBLESHOOTING REVEALED HIGH RESISTANCE IN NOSE LANDING GEAR DOWNLOCK SWITCH. REMOVED AND REPLACED. OPERATIONAL CHECKS GOOD. AC LANDED, ON REPOSITION FLIGHT-NO PASSENGERS, 3 CREW MEMBERS. 2L72 4F4 FRTA12EA E25NE 20041129000582004112900058NM 2004 11 29 COOSDR040038 120040902A5730 SKIN BOEING BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU LT WING FLAP DELAMINATED A EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23359UA 1915 24452 LT WING, OB AFT FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 240. 2L72 4F4 FRTA16WE E21EU 20041129000612004112900061NM 2004 11 29 USAA040802 120040921A5414 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE RT PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, SKIN, 6 INCH CRACK, RT PYLON LOWER PAN FROM NAC 319 AFT TO END. REMOVED AND REPLACED SKIN AND INSTALLED DOUBLER IAW SRM 51-70-13. 2L72 4F4 FRTA16WE E2GL 20041129000662004112900066SO 2004 11 29 SIMA200428701 120041011A33502013114 POWER SUPPLY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21630AE 145132 CREW REPORTED THE EMERGENCY LIGHTS AT SEATS 8 THRU 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20041129000672004112900067NM 2004 11 29 USAA040818 120040827A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, SKIN .300 INCH LONG CRACK, LOWER RADIUS OF LOWER HINGE CUTOUT. INSTALLED DOUBLER IAW TYP REP 52-10-13. 2L72 4F4 FRTA16WE E2GL 20041129000682004112900068NM 2004 11 29 C7WA200400044 120040922A5313 STRINGER BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 STRINGER 28 RT CORRODED AT STA 990. REPLACED DAMAGED KEELBEAM SECTION IAW EO NR 1M-727-53-0236 AND DRAWING 65-56441-8. 2L73 4F4 F A3WE E2EA 20041129000702004112900070CE 2004 11 29 GW12004F00002 120040731A3222420257 PISTON BEECH MU300 400BEECH CE NLG STRUT CRACKED B GW1RO OTHER O OTHER NRNOT REPORTED 1 EA0365RA 4205 RJ9 DURING ROUTINE 3000 CYCLE, LANDING GEAR INSPECTION, MM, PN 128-590001-9C2, CHAP 5-20-01, PG 3, ITEM O, 3, MPI (FLUORESCENT MAGNETIC PARTICAL INSPECTION) REVEALED TWO (2) CRACKS INDICATION ON THE LEGS OF THE NLG FORK. ITEM WAS SCRAPPED AND REPLACED WITH A NEW PART. 2H72 4F RTA16SW 20041129000712004112900071 2004 11 29 JRAA0520043 120040520A5311 BELTFRAME CVAC STC STC440 RROYCEDART DART54210 54522EU FUSELAGE CORRODED E JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 DURING A SCID INSPECTION, CORROSION WAS FOUND ON RT BELTFRAME STATION 665.0 AT FLOOR LINE. APPROX. 8.5 INCHES OF THE BELTFRAME IS CORRODED AT THE FLOORBEAM ATTACH POINT. SOME OF THE CORROSION EXTENDS BELOW THE FLOOR LINE. REPAIR IN PROGRESS AT THIS TIME. 2L72 4R4 TT 6A6 E5EU 20041129000732004112900073NM 2004 11 29 C7WA200400043 120040922A5330 SKIN BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 FUSELAGE LOWER SKIN AT STA 990 STR 28 RT. CORRODED AND TWO RIVETS MISSING. INSTALLED EXTERNAL SKIN REPAIR IAW SRM. 53-30-3 FIG 3. DOUBLER MATERIAL USED, 2024-T3 X .125 INCH X 17 INCHES X 11 INCHES. 2L73 4F4 F A3WE E2EA 20041129000772004112900077CE 2004 11 29 Z5F2004F00004 120040911A2731 ACTUATOR CESSNA525 525 2076601CE WILINTFJ44 FJ44 66000GL ELEVATOR TRIM FROZEN E Z5FAA UNSCHED LANDING SJ AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 NE03135CS824 5250520 WHILE IN CRUISE AT FL370, CREW DISCOVERED THAT THE ELEVATOR TRIM, BOTH ELECTRIC AND MANUAL WAS FROZEN. AUTOPILOT DISCONNECTED AND AVIONICS CAUTION ILLUMINATED. CREW DECLARED AN EMERGENCY AND WAS CLEARED TO DESCEND AND LAND. AC LANDING WAS UNEVENTFUL. MAINTENANCE FOUND ELEVATOR TRIM ACTUATOR TO BE FROZEN (ICE) FROM WATER INTRUSION. IT WAS DETERMINED THE WATER CAME FROM AIRCRAFT WASH THAT HAD BEEN PERFORMED PRIOR TO DEPARTURE. ACTURATOR WAS CLEANED, INSPECTED AND LUBRICATED. THE AC WAS THEN OPERATIONALLY CHECKED IN FLIGHT WITH NO REPEAT OCCURRENCE. 1L72 4F4 FRTA1WI E3GL 20041129000782004112900078EU 2004 11 29 DAT2004F00007 120040204A1430B3339 BOLT STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA HARTZLHCB5M HCB5MP3 GL PROPELLER CRACKED E DATAK NONE O OTHER ININSP/MAINT 1 GL13937MA613 SH3040 PS84296 EVA2141 DURING THE SCHEDULED MAINTENANCE AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE RT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WITH NEW ONES PURCHASED FRO MFG UND PO 009048. AD WAS COMPLIED WITH IAW MFG SERVICE INSTRUCTIONS. AIRCRAFT WAS RETURNED TO SERIVCE. 2H72 4T4 T A41EU E4EA 6 CP44GL 20041129000802004112900080NE 2004 11 29 T482004F00000 220040820A7230500809501 MANIFOLD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 ENGINE CRACKED B T48RO OTHER O OTHER NRNOT REPORTED 1 GL09802NK 53168 718236 NR 2 ENGINE WAS REMOVED FOR T-4 BLADE NOTCH BREAKOUT AND COMPRESSOR STALLING. TEARDOWN CONFIRMED THAT ONE T-4 BLADE HAD NOTCH BREAKOUT. FURTHER DISASSEMBLY REVEALED A BROKEN 8TH STAGE BLEED MANIFOLD WITH DIFFUSER INNER FAN DUCT AND DIFFUSER OUTER FAN DUCT LINER DELAMINATION ASSOCIATED WITH THE 8TH STAGE BLEED VALVE BEING STUCK OPEN DUE TO THE LOSS OF 8TH STAGE BLEED VALVE MANIFOLD PRESSURE. 2L72 4F4 FRTA6WE E9NE 20041129000812004112900081NM 2004 11 29 M562004F00000 120040721A5531 SPAR BOEING737 7374Y0 1384705NM CFMINTCFM56 CFM563C1 13802EU RT VERT STAB CORRODED I M56BO OTHER O OTHER NRNOT REPORTED 1 EA0537NY 17852 23976 VERTICAL STABILIIZER REAR SPAR RT CHORD CORROSION BETWEEN FIN STA 66.35 AND 90.30. CORROSION ON SURFACE ONLY FROM .018 INCH TO .084 INCH DEEP. BLENDING CORROSION IAW MFG ENGINEERING INSTRUCTIONS. 2L72 4F4 FRTA16WE E21EU 20041129000852004112900085NM 2004 11 29 USAA040722 120040912A534769773081 MOUNT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LAVATORY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 MOUNT, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, AFT LAV MOUNT, STA 947, RBL25. REMOVED AND REPLACED LAV MOUNT IAW SRM 51-10-2, 51-40-00. 2L72 4F4 FRTA16WE E21EU 20041129000862004112900086NM 2004 11 29 USAA040723 120040916A5320BAC1496377 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19432US41131 24554 ZEE ANGLE, 8 AREAS, .2500 INCH SPOTS, CORROSION; LEVEL 1; TASK NR C53-202-01, RT ZEE ANGLE FROM STA 727B TO 767. DEFECTIVE PART REPLACED WITH ID PN, ZEE ANGLE SPLICE IAW SRM 53-60-53-201. 2L72 4F4 FRTA16WE E21EU 20041129000872004112900087NE 2004 11 29 USAASA04028 220040320A72003053557170 BEARING AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE ENG LPT MODULE SPALLED A USAAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 EA19709UW15721 0997 779500 EN ROUTE, DURING APPROACH, AT 12000 FT, RECEIVED (ENG 1 OIL FILTER CLOG) ECAM MESSAGE, THEN, THE NR 1 ENGINE BEGAN TO FLUCTUATE, VIBRATE AND SURGE UNTIL IT QUIT. CREW ACCOMPLISHED, THE SHUTDOWN PROCEDURES GIVEN BY ECAM ACTIONS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 18 MINUTES. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONALLY AND LEAK CHECKED OK. ENGINE VENDOR REPLACED NR 4 BEARING. 2L72 4F4 FRTA28NM E37NE 20041129000902004112900090NM 2004 11 29 USAA040783 120040829A5340 STRINGER CLIP BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT - Q5, TIE- .1250 INCH CRACK, RIVET, STR TO FRAME CLIP, STA 663.75-S10R. REMOVED AND REPLACED STRINGER CLIP (TIE) IAW 53-00-03. 2L72 4F4 FRTA16WE E2GL 20041129000932004112900093NM 2004 11 29 AMTA200401398 120041112A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211* 54555NE EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 L2 DOOR EGRESS LIGHTS INOPERATIVE AT ROW 9 R/SIDE (2 EA). RECONNECTED WIRING AT ROW 8 AND 9. OPS CHECK, OK. 2L72 4F4 FRTA2NM A12EU 20041129000952004112900095EA 2004 11 29 ASOA04799 120041015A5210601R319805 STEP CNDAIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27837AS 7271 7271 DURING A HANGAR INSPECTION, THE BOTTOM STEP AT THE ATTACH LINK ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050301000272005030100027SO 2005 3 1 UG8APA04005 120041118A1430GAF511BC FASTENER GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE MAIN ENTRY CORRODED E UG8AK NONE O OTHER ININSP/MAINT 1 GL23920DC 534 534 CORROSION FOUND ON FASTENERS UNDER MAIN ENTRANCE DOOR SEAL AT THE HINGE AREA. DISSIMILAR MATERIAL CORROSION BETWEEN THE HUCK FASTENERS AND THE SURROUNDING COMPOSITE STRUCTURE. REPLACED HUCK FASTENERS WITH RECOMMENDED FASTENERS FROM THE MANUFACTURE. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA12EA E00057EN 20041129000982004112900098GL 2004 11 29 ALG2004F00072 220041108A7320 B-NUT BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL PC LINE LOOSE E ALGAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW031075Y 45378 CAE860630 AIRCRAFT HAD COMPRESSOR STALL ON TAKE OFF. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST FOR EVIDENCE OF FOD, NO DAMAGE NOTED. PERFORMED AN ENGINE AIR LEAK CHECK AND FOUND THE PC LINE FROM THE GOVERNOR TO THE FUEL CONTROL WITH A LOOSE B-NUT. TORQUE CHECKED ALL AIR LINES AND APPLIED TORQUE STRIP. WHILE HEADING INBOUND PERFORMED ON ENGINE, POWER ASSURANCE CHECK WAS A +36. 1G71 3U3 U H2SW E1GL 20041129001002004112900100EA 2004 11 29 ASOA04795 120041013A3350GE1495X LAMP BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27902EV 7620 DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP NEAR THE SERVICE DOOR. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001012004112900101EA 2004 11 29 ASOA04792 120041012A5210601R319805 STEP CNDAIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27837AS 7271 7271 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001022004112900102NM 2004 11 29 ASAA0410406 120040928A5330654776531 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2L72 4F4 FRTA16WE E2EA 20041129001042004112900104EU 2004 11 29 COE2004F00001 120041103A2420N4063 ALTERNATOR FOKKERF27 F27MK600 4990706EU RROYCEDART DART5327R 54509NE RT ENG GEARBOX FAILED A COEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM13702FE 1289 10350 1472516014 ON CLIMB OUT, RT ALTERNATOR FAIL LIGHT CAME ON. AIRCRAFT RETURNED TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ALTERNATOR. AIRCRAFT WAS RETURNED TO SERIVCE. 2H72 4T4 T A817 E297 20041129001062004112900106WP 2004 11 29 EOO2004F00003 120040310A71206890530 SUPPORT HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL COMPRESSOR CRACKED B EOORO OTHER O OTHER NRNOT REPORTED 1 AL0390431112982094 1100833D CAE832750 FRONT SUPPORT ON COMPRESSOR FOUND CRACKED. REMOVED ENGINE FOR COMPRESSOR CASE HALF INSPECTION. FOUND FRONT SUPPORT CRACKED AT THE LT ANTI-ICE FITTING ABOUT 65 PERCENT AROUND THE CIRCUMFERENCE OF THE BRAZEO FLANGE JUST BEYOND THE BRAZE. REPLACED UNIT. 1G71 3U3 U H3WE E4CE 20041129001072004112900107NM 2004 11 29 USAA040745 120041011A5312 PRESSURE PANEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU52509 23856 PIT, C5; PRESSURE PANEL, 2 INCH CRACK. LT WHEEL WELL UPPER DECK, 30 INCH LT OF BL0. INSTALLED DOUBLER AND SHIMS IAW TYP REP 53-60-04A AND EA 79277. 2L72 4F4 FRTA16WE E21EU 20041129001082004112900108NM 2004 11 29 USAA040725 120040917A5320 FLOOR SUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B1US GL FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US 24554 FLOOR TRACK, ABOUT 3 INCHES LONG BY 1 INCH WIDE AREA, CORROSION; NO LEVEL OR TASK. FLOOR TRACK AT STA 500F + 16 INCHES RBL 17. FABRICATED BY MACHINE SHOP TO MATCH ORIGINAL IAW SRM 53-00-53-202. 2L72 4F4 FRTA16WE E2GL 20041129001092004112900109NM 2004 11 29 USAA040713 120040911A5230 TEE FITTING BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU AFT CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 TEE-CHORD, .2500 INCH LONG, AFT CARGO DOOR, 3RD LOCK FASTENER FROM AFT END OF LOWER TEE CHORD. REPLACED T-CORD ANGLE IAW SRM 52-30-02. 2L72 4F4 FRTA16WE E21EU 20041129001102004112900110EA 2004 11 29 A6WA200440153 120041017A2120 DUCT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT SEPARATED A A6WAO OTHER J WARNING INDICATION CLCLIMB 1 GL31410AW 7490 MESSAGE IN FLIGHT, QRH COMPLIED WITH. DISPLAY COOL MESSAGE INTERMITTENT IN FLIGHT. ALT POSITION WENT TO STANDBY POSITION THEN EXTINGUISHED THRU FL270 THEN WENT OFF (AIR RETURN). UPON INSPECTION FOUND DUCT ABOVE CAPTAINS RUDDER PEDAL OFF. RESECURED DUCT. OPS CHECK GOOD IAW AMM21-24-22. 2L72 4F4 FRTA21EA E15NE 20041129001122004112900112EA 2004 11 29 ASOA04804 120041007A5340 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING-FUSELAGE MIGRATED A ASOAO OTHER O OTHER DEDESCENT 1 SO27905EV 7632 DURING DESCENT, AT APPROX 24,000 FT THE CREW HEARD A LOUD (BANG) FROM UNDER THE RT WING ROOT. ALL INDICATIONS WERE NORMAL INCLUDING THE FLIGHT CONTROLS AND DOORS. AN EMERGENCY WAS DECLARED WITH A NORMAL APPROACH AND LANDING ACCOMPLISHED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE RT MLG. NO DEFECTS WERE NOTED. MAINT ALSO INSPECTED THE RT WING ROOT FOR POSSIBLE MIGRATION OF THE WING TO FUSELAGE FITTING BUSHINGS IAW REO601R-57-21-407. THE REO ALLOWS FOR BUSHING MIGRATION, WHICH IS TENTATIVELY SCHEDULED FOR FEB 2005. THIS MRR WILL REMAIN OPEN PENDING PERFORMANCE OF THAT INSPECTION. 2L72 4F4 FRTA21EA E15NE 20041129001132004112900113EA 2004 11 29 ASOA04813 120041023A5210601R3198067 STEP CNDAIR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27863AS 7488 7487 DURING A ROUTINE SERVICE CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AND THE STEP ACTUATING ROD WAS FOUND BENT. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ASSEMBLY AND REPAIRED THE STEP ACTUATING ROD ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001142004112900114EU 2004 11 29 A6WA200160048 120041007A5754 STRUCTURE BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE LT LE FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31179US E2041 WEAR DAMAGE TO THE LOWER L/E OF THE LT FLAP IN THE RECESSED AREA BETWEEN RIBS 25 AND 31. MAINTENANCE REPAIRED WEAR DAMAGE IAW BAE FAX BARA/AVR/6894/04-DC. 2H74 4F4 F A49EU E6NE 20041129001152004112900115EA 2004 11 29 REXA04028 120041105A2750 POTENTIOMETER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS OUT OF RIG A REXAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO258412F 7412 FLAP FAILURE ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. PERFORMED RIGGING OF FLAP POTENTIOMETERS AND BPSU IAW AMM 27. 2L72 4F4 FRTA21EA E15NE 20041129001162004112900116NM 2004 11 29 USAA040742 120041011A5311 FRAME BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT, Q4: FRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYPE REP 53-70-20A. 2L72 4F RTA16WE 20041129001192004112900119 2004 11 29 ALG2004F00073 420041029A3197 WIRE BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL INSTRUMENT PANELLOOSE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03182AL 52057 CAE895740 PUSHED THE STARTER BUTTON FOR THE FIRST FLIGHT AND THERE WAS A LOUD POP AND SPARKS FOR THE LT SIDE OF THE LOWER INSTRUMENT PANEL. MAINTENANCE FOUND THE BATTERY RELAY GROUND WIRE ON THE AIRFRAME SIDE LOOSE, REMOVED GROUND AND CLEANED TERMINAL AND REINASTALLED GROUND WIRE. THE AIRCRAFT WAS GROUND RUN AND OPS CHECKED GOOD. 1G71 3U3 UNCH2SW E1GL 20041129001202004112900120EA 2004 11 29 ASOA04774 120040930A5210601R383885 STOP FITTING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO27875AS 7563 7559 DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH FROM THE INSIDE. MAINTENANCE ADJUSTED THE LOWER FORWARD PIN STOP FITTING IAW THE AMM 52-11-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001212004112900121NM 2004 11 29 GAIA04103 120040910A5310 BEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE BULKHEAD CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FWD 1183 BULKHEAD VERTICAL BEAM RBL 36.8, CRACKED. REF FASI NR 86371, STOP DRILLED CRACKED HOLES AND REPAIRED 1183 BULKHEAD VERTICAL BEAM RBL 36.8, IAW SB 727-53-0192. 2L73 4F4 F A3WE E2EA 20041129001222004112900122NM 2004 11 29 ASAA0410403 120040929A53306545767541 LAP JOINT BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 SCRIBE MARK IN EXTERNAL SKIN LAP JOINT. REPAIRED SCRIBE MARK ON SKIN LAP. 2L72 4F4 FRTA16WE E2EA 20041129001272004112900127NM 2004 11 29 M562004F00004 120040704A5347 SEAT TRACK BOEING737 737400 138449ANM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED I M56BO OTHER O OTHER NRNOT REPORTED 1 EA0537NY 17852 23976 RT OB SEAT TRACK CORRODED FROM BS 635-645. REMOVED AND REPLACED SEAT TRACK. C1, C2, C3 INSP 8/4/04. 2L72 4F4 FRTA16WE E21EU 20041129001282004112900128NM 2004 11 29 GAIA04157 120040910A5312 PRESSURE PANEL BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 20041 DURING C-CHECK INSPECTION FOUND ELECT. COMPARTMENT BS 288, LBL24, PRESSURE WEB FOR NOSE WW CRACKED. REF FASI NR 86933, INSTALLED DOUBLER REPAIR IAW SRM 53-10-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041129001292004112900129NM 2004 11 29 GAIA04158 120040910A5313 STRINGER BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND STRINGER 21 RT AT BS 410, DENTED. REF FASI NR 86948, ACCOMPLISHED STRINGER REPAIR IAW SRM 53-10-2, FIG 2. 2L73 4F4 F A3WE E2EA 20041129001302004112900130NM 2004 11 29 GAIA04159 120040910A5230 SKIN BOEING BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE C2 DOOR BULGED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND C-2 DOOR SKIN BULGE IN LOWER SECTION. REF FASI NR 86950, INSTALLED SKIN REPAIR DOUBLER IAW SRM 52-00-3. 2L73 4F4 F A3WE E2EA 20041129001332004112900133NE 2004 11 29 ALG2004F00055 120041029A77200290697520 CIRCUIT BOARD SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE INSTRUMENT PANELCORRODED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03860AL1060 760527 20054 RECURRING INCIDENT, MORE THAN FOUR SEPARATE INCIDENTS SPANNING LESS THAN A FIVE MONTH PERIOD AND ON DIFFERENT AC. CIRCUIT BOARD CORROSION CAUSED DECU T4.5 TRIM FAULTS UPON SHUT DOWN, CONFORMATION BOX WIRES CORROSION RESULTED IN DECU T4.5 TRIM FAULT UPON SHUTDOWN AND CONFORMATION BOX WIRE CHAFED CAUSED FALSE T4.5 COCKPIT INDICATION. 1G72 3U3 UNCH1NE E19EU 20041129001342004112900134EA 2004 11 29 LAB2004F00000 220040325A8500 ENGINE PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA SHUTDOWN E LABAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION LDLANDING 1 AL053002T3151 643 287990320 L3711736A HAD INVOLUNTARY ENGINE SHUTDOWN DURING FLARE PORTION OF TOUCHDOWN ON RUNWAY. AFTER COASTING CLEAR OF ACTIVE RUNWAY, PILOT WAS ABLE TO RESTART ENGINE WITH EASE. AFTER DETERMINING ENGINE WAS OPERATING WITHIN NORMAL PARAMETERS, PILOT DELIVERED AC TO MAINT FOR FURTHER EXAMINATION. WEATHER CONDITIONS FAVORED RAINS WITH FREEZING TEMPERATURES. AC HAD 7 HOURS SINCE PHASE3, WITH ENGINE TBO OF 650.5. PERFORMED FUNCTIONAL CHECKS ON FUEL, IGNITION, CARB-HEAT, AND CHECKED ALL ENGINE RELATED FUNCTIONS DURING A DETAILED GROUND RUN. ALL SYS CHECKS GOOD, DETERMINATION THAT AC HAD DEVELOPED (CARB-ICE). AC WAS DETERMINED AIRWORTHY, RETURNED TO SERVICE. 1L71 3O3 O 2A13 E286 20041129001352004112900135 2004 11 29 526041 420040526A2312 RADIO CESSNA500 550 2076604CE PWA 530 PW530A NE NR 2 COMMS SMOKE E Z5FAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NE03306CS 5500881 DURING CRUISE, CREW REPORTED A BURNING SMELL AND SLIGHT AMOUNT OF SMOKE COMING FROM UNDER THE GLARE SHIELD. PROBLEM OCCURRED WHILE USING NR 2 COMM. CREW DETERMINED ODOR AND SMOKE COMING FROM RADIO. THE NR 2 COMM CIRCUIT BREAKER WAS PULLED, SMELL AND SMOKE CLEARED. CREW DETERMINED IT WOULD BE BEST TO LAND AIRCRAFT AND DETERMINE CAUSE. AIRCRAFT DIVERTED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT IS BEING INSPECTED BY MAINTENANCE. (NE03200410244) 1L72 4F4 F A22CE E00053EN 20041129001372004112900137EA 2004 11 29 ASOA04775 120041002A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27870AS 7520 7530 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001392004112900139 2004 11 29 KBM2004F00235 420040921A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH512 2884 DIRECTIONAL GYRO INOPERATIVE. REMOVED AND REPLACED WITH A RECONDITIONED GYRO. 1G71 3U3 U H9EU E19EU 20041129001402004112900140GL 2004 11 29 EOO2004F00002 220040720A7323 ADAPTER HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL DRIVE SPLINE WORN E EOORO OTHER O OTHER NRNOT REPORTED 1 AL035074R 362 1151D CAE832750 DURING TURBINE REMOVAL IT WAS DISCOVERED THAT THE EPOXY WAS MISSING FROM THE GOVERNOR DRIVE ADAPTOR AND THAT THERE IS EXCESSIVE SPLINE WEAR BETWEEN THE ADAPTOR AND THE GOVERNOR DRIVE SHAFT. THE EPOXY PIECE WAS RECOVERED FROM THE ENGINE GEARBOX GOVERNOR DRIVE GEAR. GOVERNOR WAS REPLACED. 1G71 3U3 U H3WE E4CE 20041129001422004112900142EU 2004 11 29 KBM2004F00236 120040818A5320FDT14194 STRUT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE A/C COMP PULLEY DAMAGED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH435 3787 IFS AIR CONDITIONING COMPRESSOR PULLEY CAME IN CONTACT WITH STRUT BAR. REPLACED STRUT BAR AND RESHIMMED PULLEY SO AS TO NOT MAKE CONTACT WITH STRUT. 1G71 3U3 U H9EU E19EU 20041129001432004112900143 2004 11 29 WIW2004F00001 420040927A611305522312 SPINNER CESSNA172 172S 2072439CE LYC IO360 IO360L2A EA PROPELLER CRACKED L WIWRK NONE O OTHER ININSP/MAINT 1 WP07121CW785 172S8975 DURING A 100 HOUR INSPECTION OF THE PROPELLER IT WAS NOTICED THAT THERE WERE CRACKS AROUND THREE OF THE BOLT HOLES OF THE FORWARD SPINNER BULKHEAD. THE PROBABLE CAUSE IS THAT DURING THE TORQUING PROCESS THE BULKHEAD IS BEING STRESSED AND BENT AS IT IS PULLED TIGHT TO THE PROP HUB. IT IS SUGGESTED THAT THE SPINNER BULKHEAD BE MADE OF THICKER MATERIAL. 1H71 3O3 ONT3A12 1E10 20041129001462004112900146NM 2004 11 29 GAIA04120 120040910A5710 PANEL BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE RT WING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND RT WING L/E STA 349 WEB PANEL CRACKED. REF FASI NR 86603, STOP DRILLED WEB AREA AND INSTALLED DOUBLER REPAIR IAW SRM 51-40-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041129001492004112900149NM 2004 11 29 GAIA04101 120040910A5320 WEB BOEING B727222 BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE AIRSTAIR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW27180AX 20041 20041 DURING C-CHECK INSPECTION FOUND AFT STAIR LT WEB LIGHTNING HOLES CRACKED BS 1243, WL172. REF FASI NR 86369, STOP DRILLED CRACK IAW SRM 51-10-1 AND INSTALLED DOUBLER REPAIR IAW SRM 51-40-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041129001512004112900151NM 2004 11 29 GAIA04119 120040910A5720 SUPPORT ANGLE BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE RTWING CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND PANEL SUPPORT ANGLE CRACK, RT WING L/E STA 130. REF FASI NR REMOVED, FABRICATED AND REINSTALLED PANEL SUPPORT ANGLE IAW SRM 57-20-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041129001572004112900157NM 2004 11 29 GAIA04155 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED, STA 1303, LT SIDE. REF FASI NR 86890 ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-30-3. 2L73 4F4 F A3WE E2EA 20041129001632004112900163EU 2004 11 29 PRI2004F00000 120040805A29134005303 PUMP AMD FALC10FALCON10 2730101EU GARRTTTFE731TFE731* 01518WP HYD SYSTEM INOPERATIVE E PRIAO OTHER O OTHER NRNOT REPORTED 1 GL03510LL 15 008 NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED IN FLIGHT. UPON REMOVAL OF FAILED PUMP. INSPECTION FOUND ONE PLUG O-RING HANGING OUT ALLOWING FLUID TO ESCAPE. (WP19200407082) 2L72 4F4 F A33EU E6WE 20041129001652004112900165EA 2004 11 29 ASOA04767 120040926A261324403615 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG WHEEL MALFUNCTIONED A ASOAO OTHER N FALSE WARNING DEDESCENT 1 SO27848AS 7339 DURING DESCENT TO 11,000 MSL, THE CREW RECEIVED AN OVERHEAT MLG FAIL MESSAGE WHICH EXTINGUISHED AFTER APPROX FIVE SECONDS. SUBSEQUENTLY THE CREW RECEIVED A MLG OVERHEAT WARNING MESSAGE WHICH CYCLED ON AND OFF FOR THE REMAINDER OF THE FLIGHT. THE QRH WAS COMPLIED WITH AND PRIORITY HANDLING REQUESTED DUE TO REOCCURRING MESSAGE. AN EMERGENCY WAS DECLARED WITH EMERGENCY VEHICLES ON STANDBY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT MAIN OVERHEAT WHEEL ASSY LOOP AND HARNESS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001662004112900166EU 2004 11 29 ASOA04769 120040927A3350 HOLDER AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT OUT OF ADJUST A ASOAK NONE O OTHER ININSP/MAINT 1 SO27631AS 362 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE ADJUSTED A FUSE HOLDER IN THE POWER SUPPLY UNIT IAW ATR-72, AMM33-55-00. OPS CHECKS GOOD. 2H72 4T4 TRT E20NE 20041129001672004112900167NM 2004 11 29 GAIA04100 120040910A5753 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE TE FLAP DEBONDED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND RT OB MID FLAP UPPER SKIN DISBONDED. REF FASI NR 86359, ACCOMPLISHED BONDED DOUBLER REPAIR IAW SRM 57-50-2, FIG 3. 2L73 4F4 F A3WE E2EA 20041129001682004112900168NM 2004 11 29 GAIA04105 120040910A5521 SPAR BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE LT ELEVATOR LOOSE A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND LT ELEVATOR REAR SPAR HAS 3 EA. LOOSE TAB HINGE FITTINGS. REF FASI NR 86375, REPLACED LT ELEVATOR REAR SPAR IAW SB 727-55-0089, REV 1. 2L73 4F4 F A3WE E2EA 20041129001692004112900169NM 2004 11 29 GAIA04106 120040910A5753 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE TE FLAPS DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND RT OB AFT FLAP TRAILING EDGE DENTED. REF FASI NR, ACCOMPLISHED BONDED DOUBLER REPAIR IAW SRM 57-50-3, FIG 4. 2L73 4F4 F A3WE E2EA 20041129001702004112900170NM 2004 11 29 GAIA04122 120040910A5754 RIB BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 6 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86613 REMOVED AND REPLACED NR 6 SLAT INTERIOR RIB IAW SRM 57-50-2. 2L73 4F4 F A3WE E2EA 20041129001722004112900172NM 2004 11 29 ASAA0410413 120040929A53306545777523 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE SCORED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02746AS 23123 LOWER SKIN OF LAP IS SCORED BETWEEN THE CENTER AND LOWER ROW. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20041123001652004112300165NM 2004 11 23 PCAA0407228 120040711A496063D49845521 CONTROL PANEL DHAV DHC8 DHC8102 2809003NM APU CONTROL STUCK A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA13840EX28682 327 APU FAILED DURING SHUTDOWN, C/B N-8 POPPED, ELECTRICAL ODOR IN CABIN. REMOVED AND REPLACED APU CONTROL PANEL WITH SERVICEABLE CONTROL PANEL FROM A/C 838, OPS CHECK GOOD. 2H72 4T RTA13NM 20041123001782004112300178NM 2004 11 23 SWAA043328 120041112A53116546554 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041123001882004112300188CE 2004 11 23 DXTA200400335 120040712A215011341041 MOTOR CESSNA500 560CESSNA 2076750CE AIR CONDITIONER BURNED OUT E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07318QS6839 5600418 DURING SHUT DOWN, VERY STRONG BURNING RUBBER ODOR DETECTED COMING FROM OVERHEAD VENTS. AFTER SHUTDOWN INSPECTED AFT EQUIPMENT BAY AND NOTED VERY STRONG BURNING SMELL BUT COULD NOT DETERMINE WHICH COMPONENT. FOUND AIR CONDITIONING DRIVE MOTOR TO BE AT FAULT. REMOVED DEFECTIVE DRIVE MOTOR, INSTALLED OVERHAULED DRIVE MOTOR. ALL WORK PERFORMED IAW THE CESSNA 560 MM CHAPTER 21-52-00, PERFORMED ENGINE RUN UP, NO BURNING SMELL DETECTED. 2L72 4F RTA22CE 20041123001912004112300191NM 2004 11 23 UPS04443381 120040924A571265B101425 RIB BOEING747 747121 1384871NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LEFT WING: CTR WING L/E SUPPORT RIB FOUND CRACKED AT ILES 964.55 AS MARKED. LEFT WING CTR WING L/E SUPPORT RIB AT ILES 964.55 REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20041123001992004112300199NM 2004 11 23 SWAA043281 120041109A3350100031 LIGHT BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29606SW 27926 DURING SPV, FOUND RT FWD GALLEY LOWER FACE EMERGENCY EXIT LIGHT MISSING. INSTALLED EMERGENCY EXIT LIGHT PER BAC DRAWING. 2L72 4F RTA16WE 20041123002012004112300201 2004 11 23 SWAA043269 420041109A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29615SW 27698 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041123002032004112300203NE 2004 11 23 DXTA200400377 220040831A720030J1272 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE LEFT BIRD INGESTION E DXTAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL07675QS1402 5605275 ON TAKEOFF ROLL INGESTED A BIRD IN LEFT ENGINE, ABORTED TAKEOFF AND RETURNED TO BLOCK. PRELIMINARY INSPECTION FOUND EVIDENCE OF INGESTION NOTED ON ENGINE INLET AND EXHAUST. INSPECTED LT ENGINE AS REQUIRED, CLEANED REMAINS OF BIRD FROM INTAKE. BORESCOPED ENGINE AS REQUIRED, BIRD WENT THROUGH BYPASS DUCT ONLY, NO DEFECTS NOTED. ALL WORK PERFORMED IAW CESSNA 560XL MM CHAPTER 5-50-00 SECTION E AND NJA AAIP. 2L72 4F4 FRTA22CE E00059EN 20041123002102004112300210NM 2004 11 23 UPS04243409 120041004A5313 STRINGER BOEING727 727185C 138406NNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE: C, SKIN BULGING AT BS 1307-1315 STR 8L. FOUND BULGING WAS CAUSED BY CORROSION ON STRINGER EXTRUSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIR DOUBLER INSTALLED IAW SRM 53-30-3. 2L73 4F A3WE 20041123002162004112300216NM 2004 11 23 UPS04243411 120041004A5312 BULKHEAD BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C, BS 178 BULKHEAD: EVIDENCE OF CRACK ON FWD FACE AT RBL 10 WL 235.1 EMANATING FROM FASTENER HOLE. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED AND ENDS MARKED. CUT OUT DAMAGED AREA IAW SRM 53-10-9. HFEC CARRIED OUT, NO DEFECTS FOUND. REPAIR DOUBLER INSTALLED IAW SRM 53-10-9. 2L73 4F A3WE 20041123002202004112300220NM 2004 11 23 UPS04M43283 120040812A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 16 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL BEARING SURFACE. CORROSION AT NR 16 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 16 RIGHT & INSTALLEDD SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT B/N HOLE NR 16 RIGHT PER EO MD11-5510-19409-H & EN 1299-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041123002222004112300222NM 2004 11 23 QXEA200400763 120041030A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 DELAMINATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - LEFT HAND OUTBOARD FLAP STARTING TO DELAMINATE AT THE INBOARD UPPER CORNER. REPAIRED IAW Q400 SRM TASK 51-22-20-340-801. 2H72 4T RTA13NM 20041123002262004112300226 2004 11 23 UPS04M43089 420040909A2565 LIGHT DOUG MD11 MD11F 3023600NM L1 DOOR SLIDE WILL NOT TEST A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP 48575 INSPECTION TYPE:N/A LEFT FORWARD CABIN DOOR SLIDE LIGHT WILL NOT TEST. REPLACED LIGHT BATTERIES IAW 25-61-04, OPS CHECK GOOD. 2L73 4F RTA22WE 20041124000012004112400001NM 2004 11 24 ASAA0410411 120040929A53306545777532 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON EXTERNAL SKIN. REPAIRED DAMAGE IAW EA. 2L72 4F4 FRTA16WE E2EA 20041124000042004112400004EA 2004 11 24 REXA04018 120040926A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAP MALFUNCTIONED A REXAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO258888D1735 7888 FLAPS FAILED AT 0 WHEN SELECTED TO 20. SYSTEM RESET IAW FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20041124000102004112400010NM 2004 11 24 GAIA04137 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME BS 640 ABOVE STR 17, STR 16, RT DENTED. REF FASI NR 86686 CUT OUT DAMAGED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000162004112400016NM 2004 11 24 GAIA04127 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 380 DENTED ABOVE STR 7 LT. REF FASI NR 86676, CUT OUT DAMAGED AREA, DIM 1.0 X 3.0 INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000202004112400020SO 2004 11 24 SIMA200427905 120040920A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21732DH 145358 CORROSION WAS FOUND ON A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20. REMOVED RPREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER, REINFORCEMENT PLATE AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142, CHAPTER 53, REV 27) 53-21-10 ITEM 2 FIGURE 201 AND STANDARD SRM PRACTICES. 2L72 4F4 FRTT00011ATTE6CH 20041124000222004112400022SO 2004 11 24 SIMA200428202 120041003A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21623AE11806 145109 RT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED ARA ON THE RT OMEGA BEAM. FABRICATED AN EXTERNAL DOUBLER. REPAIR DONE IAW EMB 145 SRM (SRM EMB 145/1142 REV 27) CHAPTERS 53-21-10, FIG 204. (SW21200500290) 2L72 4T4 FRTT00011ATTE6CH 20041124000232004112400023NM 2004 11 24 ASAA0410399 120040920A5330 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 FUSELAGE SKIN HAS DENT. CUT OUT DAMAGED AREA, AND INSTALLED EXTERNAL SKIN PATCH. 2L72 4F4 FRTA16WE E2EA 20041124000352004112400035SO 2004 11 24 SIMA200427902 120040924A532014521721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21624AE12051 145111 A PREVIOUS REPAIR OF THE FORWARD DIGITAL WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR OF THE FORWARD DIGITAL AND CLEANED ATHE AREA. PREPARED SECTION FROM A NEW DIGITAL. FABRICATED SHIMS AND 2 DOUBLERS. REPAIR DONE IAW SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-21-10. (SW21200500280) 2L72 4T4 FRTT00011ATTE6CH 20041124000422004112400042EA 2004 11 24 REXA04017 120040926A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A REXAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO258588D5984 7588 FLAPS FAILED AT 20 ON TAXI. SYSTEM RESET IAW FIM, FLAPS PLACED UNDER WATCH FOR 72 HOURS IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20041124000522004112400052NM 2004 11 24 GAIA04144 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE TORN A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND C1 DOOR CUT OUT AFT. FRAME STA 620 INNER SKIN TORN. REF FASI NR 86767 REMOVED DAMAGED AREA, INSTALLED REPAIR IAW SRM 51-40-2, FIG 1. 2L73 4F4 F A3WE E2EA 20041124000562004112400056EA 2004 11 24 A6WA200440151 120041017A5320601R3501252 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31437AW 7744 FS 621- FS 625-3 INTERCOSTAL, RT SIDE STR 14R, IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL (PN601R35012-52), IAW SRM 51-42-06. 2L72 4F4 FRTA21EA E15NE 20041124000602004112400060EA 2004 11 24 ASOA04777 120041006A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27829AS 7232 DURING AN A-CHECK, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041124000652004112400065 2004 11 24 A6WA200440167 420041025A3420 AHRS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT INOPERATIVE A A6WAO OTHER G MULTIPLE FAILURE CRCRUISE 1 GL31437AW 7744 AFTER SWITCHING ATT/HDG FROM NORM TO (2) AT 31000, BOTH CAPT AND F/O AHRS WENT BLANK. A/P KICKED OFF AND YAW NR 2 DISENGAGED SWITCHED TO NORM AND CAPT AHRS CAME BACK. THEN 5 SECS LATER F/O AHRS CAME BACK. REENGAGED A/P AND YAW DAMP, TO FURTHER PROBLEM. REMOVED AND REPLACED AHRS NR2 COMPUTER IAW 34-21-01, OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041124000682004112400068NM 2004 11 24 GAIA04115 120040910A5230 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE C3 DOOR SKIN DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION, FOUND CREASE IN C3 DOOR SKIN AFT EDGE AT STR 21 RT. REF FASI NR 86522, INSTALL DOUBLER REPAIR IAW B727 52-00-3, FIG 3. 2L73 4F4 F A3WE E2EA 20041124000782004112400078EA 2004 11 24 ASOA04682 120040910A5210601R319805 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27842AS 7305 7304 DURING HANGER MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. 2L72 4F4 FRTA21EA E15NE 20041124000792004112400079EU 2004 11 24 SDR2004068 120040823A3230D610361 UNIVERSAL JOINT MESSIER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT MLG ASSY LOOSE A TRBAO OTHER O OTHER NRNOT REPORTED 1 SO21448AM194165766 MN327 448 DISCREPANCY: LT MAIN GEAR SHOCK PIN OUT OF PLACE. IT WAS RUBBING WITH LT OB TIRE ASSEMBLY. REMOVED AND REPLACED LT LANDING GEAR UNIVERSAL JOINT AND PINS. 2H72 4T4 TRTA53EU E20NE 20041124000992004112400099 2004 11 24 KBM2004F00226 420040916A34215040032902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ARTIFICAL HORZ FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV182 3296 ARTIFICIAL HORIZON GYRO, UNIT WILL NOT CAGE. INSTALLED REPAIRED UNIT. 1G71 3U3 U H9EU E19EU 20041124001102004112400110NM 2004 11 24 USAA040814 120040829A5320 CLIP BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, CLIP EST. .125 INCH CRACK, STA 440S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40. 2L72 4F4 FRTA16WE E2GL 20041124001382004112400138NM 2004 11 24 AMTA200401360 120041102A5330 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 PERFORMED PERMANENT REPAIR TO DENT IN FUSELAGE SKIN FWD OF L-2 DOOR LEVEL WITH FLOOR (CABIN). FABRICATED AND INSTALLED DOUBLER, TRIPLER AND UPPER REPAIR P. LATE ON LT SIDE FUSELAGE FWD OF L-2 DOOR IAW REO L00814 REV IR DATED 10/05/04. 2L72 4F4 FRTA2NM E12EU 20041124001462004112400146EU 2004 11 24 KBM2004F00231 120040922A6720704A34130184 CABLE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE T/R CONTROL BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 2009 PILOT REPORTS BINDING T/R PEDALS. REMOVED AND REPLACED T/R FLEX CABLE WITH NEW. 1G71 3U3 U H9EU E19EU 20041124001612004112400161EU 2004 11 24 A6WA200460050 120041025A5310 FRAME BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 SUB FRAME CRACK ON ATTACH FLANGE FRAME 33BY BETWEEN STR 11 AND 12 LT. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 6008-2049004. 2H74 4F4 F A49EU E6NE 20041124001622004112400162 2004 11 24 REXA04026 420041104A2562 G SWITCH ARTEX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258710A4502 01465 7710 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2L72 4F4 FRTA21EA E15NE 20041124001642004112400164EA 2004 11 24 ASOA04787 120041009A5210601R31908059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27862AS 7476 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR BRACE WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129000012004112900001NM 2004 11 29 USAA040748 120041007A5312 BULKHEAD BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US53967 22958 PIT, C1; SKIN WITH .5 INCH LONG CRACK AT AFT PRESSURE BULKHEAD AT BL0 AND 10 INCHES ABOVE CENTER. INSTALLED DOUBLER IAW SRM 53-80-08. 2L72 4F4 FRTA16WE E2GL 20041129000022004112900002NM 2004 11 29 USAA040747 120041010A5312 BULKHEAD BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19504AU51904 23379 PIT, C1; WEB SKIN, .2500 INCH CRACK, FWD BULKHEAD, STA 178, WEB STA 212. INSTALLED DOUBLER REPAIR IAW EO 5300V153. 2L72 4F4 FRTA16WE E21EU 20041129000112004112900011NM 2004 11 29 USAA040741 120041015A53106545871523 DOOR FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE SERVICE DOOR CRACKED A K NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT, Q4, EDGE FRAME SERVICE DOOR, .5 INCH CRACK, EDGE FRAME CRACKED, FWD SERVICE DOOR AFT EDGE FRAME, MID STOP AREA. INSTALLED DOUBLER IAW TYPE REP 52-10-11. 2L72 4F4 FRTA16WE E2GL 20041129000142004112900014NM 2004 11 29 UIEA200400193 120041115A5411 FRAME BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 3 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD UPPER ASSY FRAMES CRACKED. STOPPED DRILLED THE CRACK ENDS IAW SRM 51-10-01. HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY PICKING UP ALL EXISTINGS FASTENERS AFFECTED BY THE REPAIR PARTS WITH HI-LOK FASTENERS. 2L74 4F4 F A20WE E23EA 20041129000152004112900015NM 2004 11 29 USAA040752 120041008A5314 KEELBEAM BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 PIT, C1, KEELBEAM, 1 INCH X 20 INCH AREA, CORROSION; NO LEVEL OR TASK, BS520-540 AT STR 26L. REMOVED CORROSION, INSTALED NESTED REPAIR ON ONE SIDE ONLY IAW SRM 51-70-12, DET III. 2L72 4F4 FRTA16WE E2GL 20041129000242004112900024EA 2004 11 29 ASOA04790 120041011A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING A C-CHECK, THE LT AND RT INTERCOSTALS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT INTERCOSTALS AT FS 625 IAW SRM 51-42-20. 2L72 4F4 FRTA21EA E15NE 20041129000262004112900026NM 2004 11 29 UIEA200400183 120041009A3020 ANTI-ICE VALVE BOEING747 74747UF 1384949NM GE CF6 CF680C2B6F 30025NE COCKPIT CONTAMINATED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15498MC 29259 GT9012 TLV/CAI: AUTO NACELLE ANTI-ICE. (ATB) APPROX 8,000 CLEAR, TEMP +27C, AUTO NACELLE ANTI-ICE COMMANDED ANTI-ICE ON. ICING WING ALSO DISPLAYED. WHEN NAC ANTI-ICE VALVE IN OFF, NAI VALVE 1,2,3 AND 4 CAME ON. ALL FOUR VALVES WERE STUCK OPEN BY CHECKLIST. CHECKED BOTH ICE DETECTORS, FOUND BOTH WITH EXCESSIVE AMOUNT OF ADHESIVE ON PROBES. CLEANED THOROUGHLY. PERFORMED ICE DETECTION SYSTEM, GROUND TEST IAW TASK 30-81-00/715-001 AND MM 30-81-00/PPG501-503, AND PERFORMED ICE DETECTION SYSTEM OPERATIONAL TEST IAW TASK 30-81-00/715-050 AND MM 30-81-00, PP503/506. ACCOMPLISHED CHECKS OK. RAN ENGINE AND CHECKED MANUAL. OPERATION OF ENGINE AND WING ANTI-ICE VALVES. OPS NORMAL. NOTE: NO FUEL DUMP. 2L74 4F4 FRT1384945 E13NE 20041129000272004112900027EA 2004 11 29 ASOA04827 120041024A5320601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A C-CHECK, THE IB AND OB CLIPS AT FS 484, RBL 27 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIP AT FS 484, RBL 27 AND REPAIRING THE OB CLIP AT FS 484, RBL 36 IAW EO600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041129000562004112900056CE 2004 11 29 GUU2004F00036 120041028A2120 UNKNOWN BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT & CABIN FUMES A GUUAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO1787554 UE227 DURING FLT, EXHAUST FUMES PRESENT IN CABIN AND COCKPIT. FUMES DISSIPATED WITH LT AND RT ENVIRONMENTAL VALVES SELECTED IN THE OFF POSITION. RAN NR 1 ENGINE WITH ENVIRONMENTAL ON FOR TEN MINUTES. COULD NO DUPLICATE. 2L72 4T4 TRTA24CE E26NE 20041129000722004112900072SO 2004 11 29 SIMA200428401 120041009A2150 A/C PACK EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 1 ODOR A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21705AE 145184 CREW REPORTED A HEAVY OIL SMELL COMING FROM THE NR 1 AIR CONDITIONING PACK. NR 1 PACK WAS PUT ON MEL AT THIS TIME. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERTATIONAL CHECK OF BOTH PACKS WAS COMPLIED WITH , NO SMELL NOTED. AIRCARFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20041129000942004112900094NM 2004 11 29 USAA040740 120040917A5210 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU AFT PAX DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT, Q4, Z-ANGLE, 26 INCHES, CORROSION; LEVEL 1; TASK NR C53-107-02, AFT ENTRY DOOR Z-ANGLE AROUND SCREW HOLES, STA 962-986. REPLACED Z-ANGLE, DRILLED HOLES IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20041129001052004112900105CE 2004 11 29 COE2004F00002 120041023A242026700481 RELAY CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE LT TOP FIREWALL BURNED A COEAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 NM13705FX3960 208B0425 19306 ENROUTE, PILOT REPORTED THE STANDBY ELECTRIC POWER (ON) AND (INOP) ANNUNCIATOR LIGHTS ILLUMINATED. STANDBY POWER SYSTEM WAS INOPERATIVE. PILOT REPORTED SMELLING SMOKE. NO EMERGENCY WAS DECLARED, HOWEVER, THE EMERGENCY EQUIPMENT RESPONDED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE STANDBY POWER RELAY AND ALTERNATOR CONTROL UNIT. REPAIRED SHORTED GENERATOR CONTACTOR SENSE WIRE AT GCU. AIRCRAFT WAS RETURNED TO SERVICE. NO CIRCUIT BREAKERS POPPED. 1H71 3T3 T A37CE E4EA 20041129001322004112900132EA 2004 11 29 A6WA200440171 120041028A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 FS280 UNDER FLOORBEAM AT LBL 12 AND WL 69 LOWER FLANGE IS CRACKED. CUT AWAY DAMAGED SECTION OF FLOOR ANGLE, PERFORMED LPI TO ENSURE NO CRACKS EXIST. FAB REPAIR ANGLE AND FILLER FROM S-6144-3, S-6144-13 AND INSTALLED WET USING SOLID RIVETS AND LOCK FASTENERS. IAW REO 601R-53-11-171 REV A AND BRAS EO 6012-53-5547. 2L72 4F4 FRTA21EA E15NE 20041129001362004112900136NM 2004 11 29 C7WA200400046 120040922A5320 SUPPORT ANGLE BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 SUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X .050 INCH. 2L73 4F4 F A3WE E2EA 20041129001472004112900147NM 2004 11 29 GAIA04121 120040910A5754 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 5 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NR 5 SLAT L/E LOWER TO OB END PREVIOUS REPAIR MISS MATCH. REF FASI NR 86609, REMOVED PREVIOUS REPAIR FROM NR 5 SLAT. INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1. 2L73 4F4 F A3WE E2EA 20041129001522004112900152EU 2004 11 29 ASOA04768 120040910A5347NTA44768 SEAT TRACK AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27631AS 362 DURING A C-CHECK, THE RT SEAT TRACK BETWEEN FR 39 AND 40 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT SEAT TRACK BETWEEN FR 39 AND 40 IAW SRM 51-25-04 AND 51-25-03. 2H72 4T4 TRT E20NE 20041129001592004112900159NM 2004 11 29 GAIA04160 120040910A5310 BEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE BULKHEAD CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND AFT CABIN VERTICAL BEAM BS 1183, LBL24 INCH, WL 269, CRACKED. REF FASI NR 86945 INSTALLED REPAIR KIT 65C33556-41 IAW SB 727-53-0182, REV 1. 2L73 4F4 F A3WE E2EA 20041129001612004112900161NM 2004 11 29 GAIA04107 120040910A5754 RIB BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 5 SLAT CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND NR 5 SLAT IB END RIB CRACKED. REF FASI NR, REMOVED, FABRICATED AND INSTALLED END RIB IAW SRM 57-50-2. 2L73 4F4 F A3WE E2EA 20041129001712004112900171NM 2004 11 29 USAA040732 120041011A5320 BRACKET BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19601AU 22193 BRACKET, 1 INCH SQUARE, CORROSION, STA 1376, STRINGER 26R AFT CARGO. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02. 2L72 4F4 FRTA2NM E12EU 20041129001732004112900173NM 2004 11 29 ASAA0410414 120040929A53306545777523 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE SCORED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 LOWER SKIN OF LAP IS SCORED BETWEEN THE CENTER AND LOWER ROW OF FASTNERS. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20041129001782004112900178EU 2004 11 29 ASOA03602S 120040102A2752FE231002 ACTUATOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE TE FLAP LEAKING A ASOAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27634AS198672476 370 FLAP ACTUATOR LEAKING. 2H72 4T4 TRTA53EU E20NE 20041129001812004112900181EU 2004 11 29 ASOA04679 120040908A3350LP1670 LAMP AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHT AT ROW 16 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 16. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20041129001822004112900182EU 2004 11 29 SIMA200426908 120040922A246031342003 GENERATOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE INOPERATIVE A SIMAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SW21235AE 340B235 AS AIRCRAFT WAS TAXIING IN MAINTENANCE PERSONNEL WHO WERE ON THE RAMP NOTED FLAME COMING OUT OF LT ENGINE GENERATOR VENT. CREW BLEW THE FIRE BOTTLES TO EXTINGUISH FLAME. CREW HAD REPORTED ON IB FLIGHT THE LT GENERATOR FAIL LIGHT WAS ON. MAINTENANCE FOUND THE LT GENERATOR TO BE THE PROBLEM. THE GENERATOR WAS REMOVED AND REPLACED IAW MM. OPERATIONAL AND LEAK CHECK WAS GOOD. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200500055WR) 2L72 4T4 TRTA52EU E8NE 20041129001832004112900183SW 2004 11 29 ALG2004F00057 120041007A1420 CONNECTOR BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANS PUMP DIRTY E ALGAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW03437AL 53141 CAE847048 ON TAKE OFF, RT FUEL TRANSFER LIGHT ILLUMINATED DURING TAKE OFF. MAINTENANCE FOUND MOISTURE ON TRANSFER PUMP CONNECTOR, CLEANED AND REINSTALLED, THE OPS CHECK WAS GOOD. 1G71 3U3 UO H2SW E1GL 20041129001872004112900187CE 2004 11 29 RG42004F00000 120040920A555107321014 ATTACH BRACKET CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA HORIZONTAL STAB CRACKED A RG4RO OTHER O OTHER NRNOT REPORTED 1 SO0363CE 1768 18280357 L2657048A PART FOUND CRACKED DURING 100 HR INSPECTION. CRACK LOCATED AT LOWER LT CORNER OF PART, LT BRACKET. RECOMMEND PART OF STRONGER MATERIAL OR DIFFERENT DESIGN. OBTAINING ENGINEERING APPROVAL FRO MFG TO INSTALL HEAVIER DESIGNED PART, VIA FIELD APPROVAL. (FIRST OCCURRENCE, 1600 TT) 1H71 3O3 ONT3A13 1E4 20041129001882004112900188NM 2004 11 29 USAA040715 120040910A5320 INTERCOSTAL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 INTERCOSTAL, .5 INCH CRACK IN RADIUS, BETWEEN STA 500E AND 500F, UNDER LT AFT CARGO PIT FLOOR ZEE ANGLE. FABRICATED REPLACEMENT PART IAW SRM 53-30-04, 51-10-02. 2L72 4F4 FRTA16WE E21EU 20041129001902004112900190CE 2004 11 29 TIM2004F00000 120040930A29101145800341 TUBE BEECH 1900 1900 1154160CE PWA PT6 PT6A65* EA LT IB WING PIN HOLE E TIMAK NONE K FLUID LOSS ININSP/MAINT 1 NM07192GA38469 UB17 WHILE DOING A ROUTINE INSPECTION, IT WAS NOTICED HYDRAULIC FLUID ON THE LOWER PORTION OF THE LT IB WING. AFTER CLEANING THE AREA AND PERFORMING A RETRACTION TEST, IT WAS DETERMINED THAT THE RETRACTION TUBE HAD A PIN HOLE IN IT. COULD NOT GUESS ON THE PROBABLE CAUSE. THE LINE WAS FOUND CORROSION FREE INSIDE AND OUT. THE HOLE WAS LOCATED IN A 90 DEGREE BEND. 2L72 4T4 TRTA24CE E4EA 20041129001972004112900197NE 2004 11 29 ALG2004F00052 120040925A32442070A900 TIRE SKRSKYS76 S76C 8143008NE NLG CUT E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03866AL65 760562 WHILE TAXING OUT THE NOSE WHEEL WHEN FLAT. MAINTENANCE REMOVED AND REPLACED NOSE TIRE ASSY, OLD TIRE HAD CUT ON THE TREAD AREA, ALL WORK DONE IAW S-76C+ MM. 1G72 3U NCH1NE 20041129001982004112900198GL 2004 11 29 ALG2004F00053 220040923A7261 CHIP DETECTOR BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL ENGINE ILLUMINATED E ALGAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW032619 51375 TAXING FOR TAKE OFF, ENGINE CHIP LIGHT CAME ON TAXING FOR TAKE OFF. MAINTENANCE REMOVED, INSPECTED AND CLEANED THE CHIP DETECTORS IAW MM. AIRCRAFT GROUND RAN FOR 30 MINUTES NO DEFECTS FOUND. 1G71 3U3 U H2SW E1GL 20041129002032004112900203NE 2004 11 29 ALG2004F00050 120040923A6320 TRANSMISSION SKRSKYS76 S76C 8143008NE MAIN ROTOR MAKING METAL E ALGAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW03864AL 760557 WHILE HOVERING TO REPOSITION FOR TAKEOFF MAIN GEAR BOX CHIP LIGHT ILLUMINATED. RETURNED TO PARKING, NOTIFIED CUSTOMER, BASE MANAGER AND MAINTENANCE. MAINTENANCE REMOVED BOTH CHIP PLUGS TO FIND 2 SMALL HAIR LIKE SLIVERS IN CHIP PLUG SCREEN, FOUND TO BE WITHIN LIMITS IAW S76C+ MM. REPLACED TRANSMISSION OIL AND FILTER, GROUND RAN LEAK CHECK GOOD. 1G72 3U NCH1NE 20041129002052004112900205NM 2004 11 29 USAA040709 120040914A5330 SKIN PANEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU KEELBEAM CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU* 23701 UNSCHEDULED MAINTENANCE, KEEL BEAM SKIN PANEL, 3 INCH CRACK, BS 690 KEEL BEAM PANEL. INSTALLED DOUBLER (TEMP REPAIR) IAW SRM 53-60-12, FIG 202. 2L72 4F4 FRTA16WE E21EU 20041129002092004112900209CE 2004 11 29 QFY2004F00000 120041008A5341258WS31051 LINK RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE731* 01518WP LT WING INADEQUATE B QFYRO OTHER O OTHER NRNOT REPORTED 1 NE03885M 1798 258410 LT FRONT WING LINK NOT SAFETYED FROM FACTORY. UPON PERFORMING WING LINK INSPECTION TO RID AIRCRAFT OF CLUNKING NOISE, FOUND LINK NOT SAFETYED. THE BOLT WAS STILL TIGHT AT THIS POINT, BUT THE WING LINK INSPECTION WAS BEING ACCOMPLISHED 3 YEARS EARLIER AS WELL. APPEARS THAT THE SAME POOR QUALITY OF WING LINK BUSHING FITS CARRIES OVER TO THE ENTIRE JOB PACKAGE. (NE03200501323) 2L72 4F4 FRTA3EU E6WE 20041129002102004112900210EA 2004 11 29 A6WA200440155 120041017A4990 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU OIL SYSTEM OVERSERVICED A A6WAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL31456ZW 7849 STRONG BURNED ELECTRICAL SMELL NOTED AFTER APU START, PRIOR TO SELECTING APU BLEEDS ON. SMELL DISAPPEARED AFTER APU BLEEDS SELECTED ON. APU OVERSERVICED, REMOVED OIL INTO SCREEN/ MARKINGS. OPS CHECK NORMAL. NO SMELLS NOTED AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20041129002122004112900212GL 2004 11 29 HXS2004F00003 220040801A72006887190 ENGINE HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL MAKING METAL B HXSDO OTHER O OTHER NRNOT REPORTED 1 AL051088N10124 300679D PILOT REPORTED ENGINE CHIP LIGHT. MECHANIC FOUND ENGINE MAGNETIC CHIP DETECTOR HAD METAL PARTICLES WHICH EXCEDED ALLOWABLE LIMIT IN SIZE. MECHANIC REMOVED ENGINE AND INSTALLED LIKE PN ENGINE, SN CAE834274. (AL05200402908) 1G71 3U3 U H3WE E4CE 20041130000012004113000001EA 2004 11 30 COMA0460632 120041118A3297601R572181PE WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01926CA 7027 FLIGHT 5481 RECEIVED A NLG DISAGREE CAUTION DURING APPROACH, WHEN GEAR WAS RETRACTED AND EXTENDED AGAIN, RECEIVED SAFE INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT NOSE GEAR DOOR WIRING HARNESS. 2L72 4F RTA21EA 20041130000022004113000002EA 2004 11 30 COMA0460633 120041118A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LT WING FAULTY A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01981CA25123 7163 FLIGHT 5304 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING TAXI OUT. AIRCRAFT RETURNED TO THE GATE. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20041130000062004113000006SO 2004 11 30 SWIA200414114 120041113A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM07189SW4326 1355 120048 AFTER TAKEOFF FLAPS OUTBOARD WOULD NOT RETRACT, RETURNED TO FIELD. REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-60. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041130000072004113000007SO 2004 11 30 RAIA00411007 120041107A291014531608401 LINE EMB 145 EMB145LR 3260212SO HYDRAULIC SYS FAILED A RAIAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CE03819HK 145062 STL- NR 1 HYDRAULIC PUMP FAILED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE LINE. 2L72 4T RTT00011AT 20041130000082004113000008NM 2004 11 30 SWAA043428 120041123A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 807 & BS 867, STR 9L. REPAIRED BOTH FRAMES PER SRM. 2L72 4F RTA16WE 20041130000092004113000009EA 2004 11 30 SWIA200414103 120041111A2750766389L CONTROLLER CNDAIRCL600 CL6002C10 1390015EA SLAT/FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07703SK 10139 SPLR/STAB FAULT, RUD LIMITER FAULT & PITCH FEEL FAULT DISPLAYED ON EICAS. REMOVED AND REPLACED SFECU NR 1 IAW CRJ MM 27-51-05. COMPLIED WITH SLAT/FLAP AUTO RIG AS REQUIRED. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130000102004113000010EA 2004 11 30 COMA0460626 120041114A3230555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926CA207565495 7027 FLIGHT 5605 GEAR DISAGREE WARNING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20041130000112004113000011NM 2004 11 30 AALA20041135 120041115A3350 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 DFW - EMERGENCY LIGHT ON FORWARD GALLEY WELL INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ON FORWARD GALLEY WELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20041130000122004113000012EU 2004 11 30 AWXA200401262 120041025A5347D53337111120202 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000162004113000016EU 2004 11 30 YENA200454 120041123A3240E21327003 CONTROL UNIT AIRBUS320 A320232 3930326EU BRAKES UNKNOWN A YENAO OTHER O OTHER LDLANDING 1 EA15593JB537 2280 BRAKES FAILED DURING ROLLOUT. REMOVED AND REPLACED BSCU, OPS CHECK AS PER 32-42-34-710. 2L72 4F RTA28NM 20041130000182004113000018EA 2004 11 30 SWIA200414099 120041116A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA RT SPOILERONS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07440SW4687 4687 7589 SPOILERON FAULT STATUS MESSAGE DURING TAXI OUT. REMOVED AND REPLACED THE RIGHT SPOILERON OUTBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130000192004113000019EA 2004 11 30 SWIA200414100 120041116A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07437SW 7564 FORWARD SECTION OF EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED FORWARD SECTION OF EMERGENCY LIGHTING ELECTRICAL STRIP IAW AMM 33-51-01 AND A WIRE MANUAL 33-51-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130000212004113000021EA 2004 11 30 SWIA200414062 120041104A3350 CONVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07592SW 7279 EMERGENCY TRACK LIGHTING AT SEAT 12AB IS NOT ILLUMINATING. REMOVED AND REPLACED CONVERTER IAW 33-00-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130000222004113000022NM 2004 11 30 AWXA200401288 120041116A7711UL16688 TUBE BOEING757 7572G7 1384963NM NR 1 ENGINE CHAFED A AWXAO OTHER J WARNING INDICATION CRCRUISE 1 WP28908AW 24233 PHX - EMERGENCY LANDING - FLT 0568 - EN ROUTE FROM MCO TO PHX LT ENGINE EPR INDICATED HIGH, DECLARED EMERGENCY, EPR APPEARED NORMAL ON APPROACH AND LANDING. MAINTENANCE PERFORMED BITE TEST OF ELECTRONIC ENGINE CONTROL AND FOUND CODE 47, FOLLOWED FIM 73-21-00 AND INSPECTED P1 SENSE LINE CONNECTIONS. FOUND UPPER P1 SENSE CHAFED WHERE IT PASSES THROUGH INLET COWL. REMOVED AND REPLACED P1 SENSE LINE AND PERFORMED PRESSURE CHECK. RAN ENGINE TO TAKEOFF POWER, ALL EPR INDICATIONS NORMAL. 2L72 4F RTA2NM 20041130000232004113000023NM 2004 11 30 AWXA200401289 120041101A521065458715 DOOR FRAME BOEING737 7373Y0 1384671NM R-1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 RT. MAINTENANCE STOP DRILLED CRACK IN AFT EDGE OF R-1 DOOR AT 3RD DOOR STOP FROM BOTTOM BS 312, STR 13 RT. PERFORMED HFEC INSPECTION OF STOP DRILL HOLE TO VERIFY CRACK CONTAINED, TREATED REPAIR AREA. 2L72 4F RTA16WE 20041130000252004113000025NM 2004 11 30 AWXA200401291 120041031A532065566551 REVEAL BOEING737 7373Y0 1384671NM DOOR FRAME CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 3 INCH CRACK WAS FOUND IN AFT CARGO DOOR CUTOUT AFT TORQUE BOX LOWER WEB AT BS 794, STR 25 RT. MAINTENANCE REMOVED CRACKED WEB AT BS 794, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-56655; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 10. 2L72 4F RTA16WE 20041130000272004113000027 2004 11 30 MASA200400268 420040517A34178220372154 ADC CNDAIRCL600 CL6002B19 1900309EA NR 2 FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0737218122342384 7218 AIRCRAFT RETURNED TO FIELD DUE TO THE ADC NR 2 FAIL IN FLIGHT. MX ARE IN THE PROCESS OF TROUBLESHOOTING THE PROBLEM. MX REPLACED THE NR 2 ADC, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041130000312004113000031EA 2004 11 30 COMA0460644 120041122A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01973CA 7146 SKIN BEHIND NOSE LANDING GEAR DOOR RIGHT HAND SIDE IS CRACKED. REPAIRED IAW REO 601R-53-11-048. 2L72 4F RTA21EA 20041130000332004113000033WP 2004 11 30 ABXA040381 120040923A53305750371501 SKIN DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 CORROSION FUSELAGE SKIN STA 1040, LONGERON 36. DEFERRED TIL 9-6-04 IAW REA D853-50415, IAW ABX GMM CHAPTER 1 07-04. FABRICATED DOUBLER AND FILLER IAW REA D853-50292MR. ALODINED AND PRIMED DOUBLER FILLER AND SKIN IAW DC-8 SRM 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC-8 SRM 51-1-20D. 2L74 4F 4A25 20041130000342004113000034WP 2004 11 30 ABXA040382 120041110A53155615364 FLOORBEAM DOUG DC8 DC863F 302198FWP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 FLOORBEAM AT STA 52, RIGHT BUTTLINE 51 HAD CORROSION ON BOTTOM CAP. REPAIRED AREA IAW REA D853-50309MR. 2L74 4F 4A25 20041130000352004113000035EU 2004 11 30 CX7A194J0457 120041102A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY FALSE ACTIVATIONA CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03315CE255446983 340B343 AVIONICS SMOKE LIGHT ON. 2L72 4T RTA52EU 20041130000362004113000036SO 2004 11 30 SWIA200414102 120041109A2797 WIRE EMB 120 EMB120ER 3260203SO TE FLAP ACTUATORBROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07291SW 120318 CONTROL FAULT ON FLAPS. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041130000372004113000037NE 2004 11 30 COMA0460615 220041112A72306018T30P14 FAN BLADE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LT ENGINE VIBRATES A COMAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01954CA5274 7100 FLIGHT 5037 LEFT ENGINE N2 VIBE INDICATION. REPLACED THE LEFT ENGINE FAN BLADES. 2L72 4F4 FRTA21EA E15NE 20041130000382004113000038WP 2004 11 30 ABXA040375 120041105A57535912168504 VANE DOUG DC9 DC941 302207NWP RT WING TE FLAP DAMAGED A ABXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL23971AX 47497 AIRFRAME RUMBLE/VIBRATION AT 285 KTS WITH AIRCRAFT CLEAN, VIBRATION CAN BE FELT THROUGH FLOOR AND RUDDER PEDALS. REPLACED RT FLAP FORWARD MOVABLE VANE IAW DC9 MM 27-51-02-4-0001. REPLACED BUSHING IN EYEBOLT ON RT WING T/E UPPER I/B PANEL SUPPORT. REPLACED STRAP, EYEBOLT & BUSHINGS ON LT WING T/E UPPER I/B PANEL. 2L72 4F A6WE 20041130000392004113000039NM 2004 11 30 ABXA040374 120041015A5754 STRUCTURE BOEING767 767281 1385109NM RT WING SLAT DAMAGED A ABXAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 GL23784AX 23017 EICAS MESSAGE, L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUMINATED. REPAIRED PER REA B657-50865 FOR NON-REV FERRY FLIGHT TO REPOSITION FOR PERMANENT REPAIRS IAW GMM CHAP 1, SECT 7.04. REPLACED NR 8 SLAT IAW B767 MM 27-81-02. 2L72 4F RTA1NM 20041130000402004113000040WP 2004 11 30 ABXA040376 120041107A5101 STRUCTURE DOUG DC9 DC941 302207NWP UNKNOWN VIBRATION A ABXAO OTHER E VIBRATION/BUFFET DEDESCENT 1 GL23971AX 47497 IN DESCENT, LEVELED OFF AT 300 KIAS, INCURRED VIBRATION, SLOWED TO 290 KIAS, VIBRATION WENT AWAY THEN CAME BACK AGAIN WHEN ACCELERATING THROUGH 295 KIAS. INSPECTED FOR GENERAL CONDITION & SECURITY OF THE FOLLOWING ITEMS: NOSE GEAR AREA, FUSELAGE, FLAPS, SLATS, AILERONS, SPOILER PANELS, RUDDER & TRIM, HORIZONTAL STABILIZER, VERTICAL STABILIZER AND ELEVATOR. FOUND NO DEFECTS. RAN BOTH ENGINES AT IDLE & POWER SETTINGS WITH CSD'S & GENERATOR ON & OFF. NO VIBRATION NOTED. 2L72 4F A6WE 20041130000422004113000042NM 2004 11 30 SWAA043410 120041120A3350101114 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED C3 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20041130000442004113000044NM 2004 11 30 SWAA043412 120041120A53306552988 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29357SW 26594 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 24L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041130000452004113000045NM 2004 11 30 SWAA043413 120041120A53116546532 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L TO STR 20 R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20041130000472004113000047EU 2004 11 30 AWXA200401338 120041124A2780830C000001 ACTUATOR AIRBUS320 A320232 3930326EU FLAP/SLATS MALFUNCTIONED A AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28662AW16397 1274 UPON PREPARING FOR LANDING PILOTS REPORTED SELECTING FLAP LEVER TO 1, WITH A SPEED OF 210 KTS AND RECEIVED A SLAT/FLAP ECAM FAULT. FLAPS OPERATED NORMAL, SLATS REMAINED AT ZERO. LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED 6079CM ROTARY ACTUATOR IAW AMM 27-84-49-04. OPERATIONAL TEST OF SYSTEM GOOD. BOTH FCC'S SELF TEST GOOD. WTB/POB TEST GOOD ON BOTH SIDES. VENDORS FUNCTIONAL TEST OF ROTARY ACTUATOR S/N 20852 CONFIRMED REASON FOR REMOVAL, UNIT FAILED LOW TEMPERATURE TEST. RESHIMMED UNIT AND REACCOMPLISHED FUNCTIONAL TEST IAW CMM 27-82-14, REV. 4. 2L72 4F RTA28NM 20041130000482004113000048EA 2004 11 30 SWIA200414085 120040910A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07908SW 7540 CRACKED ANGLES AT FS 280, LBL 9 AND EIE RBL 9.00. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE AT FS 280 LBL 9 UNDER FLOOR IAW SRM 51-42-06. 2L72 4F RTA21EA 20041130000512004113000051EU 2004 11 30 AWXA200401339 120041125A5270ABS012110 PROXIMITY SWITCH AIRBUS320 A320231 3930325EU CARGO DOOR MALFUNCTIONED A AWXAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP28621AW 053 ORD - ABORTED TAKEOFF - FLT 0010 - PILOT REJECTED TAKEOFF AT 60 KTS DUE TO FORWARD CARGO DOOR OPEN INDICATION. MAINTENANCE REMOVED AND REPLACED THE FORWARD CARGO DOOR PROX SWITCH 30WV IAW AMM 52-31-00-05. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE DOOR AND WAS FOUND GOOD. 2L72 4F RTA28NM 20041130000522004113000052EA 2004 11 30 MASA200400540 120040924A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX UNKNOWN A MASAK NONE O OTHER ININSP/MAINT 1 SW0777331 7331 DURING PREFLIGHT THE MAIN CABIN DOOR WOULD NOT CLOSE AND LOCK FROM THE INSIDE. MX OPERATIONALY CHECKED AND THE DOOR OPERATED NORMAL. 2L72 4F RTA21EA 20041130000542004113000054NM 2004 11 30 F3LA200400114 120041111A5330 SKIN BOEING737 7373M8 1384615NM FUSELAGE DAMAGED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03303FL 1637 25039 DURING C-6 CHECK, INSPECTION REPORTED FUSELAGE SKIN WORN UNDER DORSAL FIN AT STA 860 TO STA 887, LT AND RT. ABRASION RESISTANT COATING NOT CENTERED UNDER SEAL. FOUND DAMAGE AROUND AREA AT STA 870 TO STA 885, LBL 2.5 TO 4.5, TO BE OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED AREA PER EA B3-55R-10583. 2L72 4F RTA16WE 20041130000562004113000056WP 2004 11 30 ABXA040371 120041027A53119919619505N FRAME DOUG DC9 DC931 3022065WP CABIN CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 AFT LEFT MAIN FRAME, STA 737, REQUIRED REPLACEMENT DUE TO CRACKS. REMOVED AND REPLACED AFT LEFT MAIN FRAME STA 737 IAW JOB CARD EA 53400325-001-4. 2L72 4F A6WE 20041130000572004113000057WP 2004 11 30 ABXA040369 120041027A531159356507 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 FORWARD LEFT MAIN FRAME, STA 699 WAS CRACKED WITHIN REPAIRABLE LIMITS. REPAIRED MAIN FRAME, STA 699 LT IAW DC-9 SERVICE REWORK DRAWING 5933650 AND JOB CARD EA 63400110-001-1. 2L72 4F A6WE 20041130000592004113000059WP 2004 11 30 MWEA040208 120041116A533029129003 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 FUSELAGE SKIN DENTED AT FRAME STATION 209, LONGERON 15 RIGHT TO TWO INCHES 15 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041130000602004113000060SO 2004 11 30 MASA200400613 120041029A315080069425 WARNING SYSTEM EMB 145 EMB145LR 3260212SO COCKPIT FAULTY A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07827MJ3042 145217 THE CREW ABORTED TAKEOFF DUE TO TAKEOFF WARNING ANNUNCIATING DURING TAKEOFF ROLL FOR FLAPS AND SPOILERS. THE CREW REPORTED HAVING T/O OK DISPLAYED PRIOR TO INITIATING ROLL. MAINTENANCE REMOVED AND REPLACED THE AURAL WARNING UNIT AND PERFORMED A HI SPEED TAXI WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20041130000652004113000065EU 2004 11 30 AWXA200401274 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 DURING C-04 CHECK FRETTING CORROSION WAS FOUND ON RT INBOARD SEAT TRACK BETWEEN FR 46 AND FR 47. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 46 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000672004113000067EU 2004 11 30 AWXA200401293 120041023A5315D53472194200 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON FLOORBEAM Y20 LT AT FR 66+6 INCHES. MAINTENANCE REMOVED CORRODED FLOORBEAM Y20 LT AT FR 66+6 INCHES; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-00-14 FIG 207. 2L72 4F RTA28NM 20041130000702004113000070WP 2004 11 30 ABXA040380 120041116A3040 SWITCH DOUG DC9 DC931 3022065WP WINDSHIELD HEAT ARCED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23946AX 47003 CREW REPORTED ELECTRICAL ODOR COMING FROM OVERHEAD PANEL. FOUND WINDSHIELD HEAT SWITCH IN OVERHEAD PANEL ARCING AND WIRE H578B16 INSULATION MELTED. REPAIRED WIRE IAW WDM 30-41-00 AND REMOVED AND REPLACED WINDSHIELD HEAT SWITCH. WINDSHIELD HEAT OPS CHECKED GOOD. 2L72 4F A6WE 20041130000762004113000076EA 2004 11 30 COMA0460620 120041114A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AVIONICS UNRELIABLE A COMAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01916CA9848 1 7014 FLIGHT 5352 STAB CHANNEL NR 1 STATUS MESSAGE. REPLACED THE HSTCU. 2L72 4F RTA21EA 20041130000772004113000077 2004 11 30 AWXA200401307 420041120A2565D31354437 SLIDE BOEING737 737301 1384611NM R-2 DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28325AW321343960 23260 DURING INSPECTION FOUND R-2 DOOR SLIDE PRESSURE LOW. MX R/R R-2 DOOR SLIDE IAW T/C R1C25001. CONFIRMED REASON FOR REMOVAL FINDING RESERVOIR ASSEMBLY LEAKING AT THE RUPTURE DISC. REPLACED RUPTURE DISC AND RE-SERVICED RESERVOIR, LEAK CHECK GOOD PER CMM. 2L72 4F RTA16WE 20041130000792004113000079NM 2004 11 30 AWXA200401309 120041120A3397BMS13311122 WIRE BOEING737 7373B7 1384580NM SEAT ROW 2 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28328AW 23377 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL CHECK OF EMERGENCY LIGHTING FOUND THE EMERGENCY LIGHT AT SEAT ROW 2 LT INOPERATIVE, WIRES PULLED LOOSE FROM CONNECTORS. MAINTENANCE INSTALLED NEW WIRE HARNESS AT EMERGENCY LIGHT AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041130000802004113000080EU 2004 11 30 AWXA200401310 120041120A27804911710 COMPUTER AIRBUS320 A320231 3930325EU ZONE 120 MALFUNCTIONED A AWXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 WP28633AW473474148 082 ON APPROACH, AFTER SETTING FLAPS TO 1 THE SLATS LOCKED OUT. FOLLOWED ECAM INSTRUCTIONS AND ACCOMPLISHED FLAPS 3 APPROACH / LANDING. WHEN GEAR LOWERED AIRCRAFT WENT ALTERNATE LAW THEN DIRECT LAW, AUTO PILOT, FLT DIRECTOR 2, AND AUTO THROTTLES ALL FAILED. MX R / R SLAT FLAP CONTROL COMPUTERS 1 & 2 IAW T/C R2A27302, OPERATIONAL CHECKS WERE GOOD. BENCH TEST OF SLAT/FLAP CONTROL COMPUTER, NO FAULT FOUND, NO FAILURES STORED IN BITE READOUT, UNIT TESTED SEVERAL TIMES & RETURNED TO SERVICE IAW CMM 27-03-11. SLAT/FLAP CONTROL COMPUTER FAILED INCOMING TEST STEP 200500, UNIT DISASSEMBLED & A CRACKED SOLDER JOINT FOUND AT Q10 ON OUTPUT MODULE A9, CRACK RESOLDERED & UNIT TESTED SERVERAL TIMES PASSING ALL TESTS. 2L72 4F RTA28NM 20041130000812004113000081NM 2004 11 30 AWXA200401311 120041014A5320146N530011 CHANNEL BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR HAT CHANNEL SUPPORT BETWEEN BS 1690 AND BS 1716, AT LBL 7. MAINTENANCE REMOVED CORRODED HAT CHANNEL SUPPORT FROM BS 1690 TO BS 1716, LBL 7; FABRICATED A NEW REPLACEMENT HAT CHANNEL SUPPORT PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02. 2L72 4F RTA2NM 20041130000832004113000083EU 2004 11 30 AWXA200401264 120041025A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 42 AND FR 43. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 42 TO FR 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000852004113000085SO 2004 11 30 SWIA200414077 120041106A275012064207615CON SELECTOR EMB 120 EMB120ER 3260203SO FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM0758733224 224 120197 ON FINAL WHEN SELECTING FLAPS 25, CONTROL FAULT WITH ASSOCIATED LIGHTS. INSTALLED SERVICEABLE FLAP HANDLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041130000862004113000086GL 2004 11 30 RAIA00411013 220041110A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LEFT UNKNOWN A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03812HK 145373 PIT - ATTCS NO MARGIN, LEFT ENGINE. MAINTENANCE DID A GROUND POWER RUN ON BOTH ENGINES AND COULD NOT DUPLICATE. 2L72 4T4 FRTT00011ATTE6CH 20041130000872004113000087EA 2004 11 30 COMA0460619 120041113A27501104SD100301 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5606 FLAPS FAILED CAUTION MESSAGE. REPLACED THE NR 3 FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20041130000892004113000089NM 2004 11 30 CALA0400720 120041119A53436546830 FITTING BOEING737 7373T0 1384582NM LT MLG CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND LT MLG UPLOCK FORWARD SUPPORT FRAME FITTINGS (2 EACH) CORRODED WITH BUSHINGS WORN AT STA 685, S17L. THE LUG FITTING WAS REWORKED TO REMOVE THE CORROSION AND SLEEVE AND BUSHINGS WERE INSTALLED IAW SRM 53-60-14. 2L72 4F RTA16WE 20041130000902004113000090NM 2004 11 30 CALA0400721 120041119A5330148N32161 SKIN BOEING757 757224 1384958NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2741135 29284 INSPECTION FOUND FUSELAGE SKIN CORRODED BELOW APU BLEED DUCT BETWEEN BS 1825 AND 1844, S25L TO 27L. THE SKIN WAS REPAIRED IAW ERO 3432. 2L72 4F RTA2NM 20041130000942004113000094EA 2004 11 30 SWIA200414107 120041016A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07946SW 7776 LEFT FS 280 ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PER CRJ 200 SRM 51-42-06, 51-42-06. 2L72 4F RTA21EA 20041130000952004113000095EU 2004 11 30 AWXA200401272 120041026A5320D53480020342 WEB AIRBUS320 A320231 3930325EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK A 2 INCH CRACK WAS FOUND IN WEB TRAY LT SIDE OF FUSELAGE BETWEEN FR 68 AND FR 69, WL Z240. MAINTENANCE REMOVED CRACKED WEB TRAY ON LT SIDE FROM FR 68 TO FR 69. FABRICATED A NEW REPLACEMENT TRAY; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000962004113000096EA 2004 11 30 SWIA200414108 120041016A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07946SW 7776 STA 621 LOWER LEFT HAND CORNER AT WL 79.5 HAS A CRACK AT THE RADIUS. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOORBEAM ANGLE FS 621 LT IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041130000982004113000098SO 2004 11 30 SWIA200414110 120041118A2752 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07189SW 120048 ON DEPARTURE, FLAP RETRACTION, CONTROL FAULT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041129001752004112900175 2004 11 29 WIW2004F00002 420040928A6113055032111 BULKHEAD CESSNA172 172R 2072401CE LYC O360 IO360A1A 41514EA PROP SPINNER CRACKED L WIWRK NONE O OTHER ININSP/MAINT 1 WP079581G 17280530 DURING A 100 HOUR INSPECTION THE AFT SPINNER BULKHEAD WAS FOUND TO BE CRACKED ON THE CORNER BY NUTPLATE. 1H71 3O3 ONT3A12 1E10 20041129001762004112900176EU 2004 11 29 DAT2004F00003 120041023A6100B3339 BOLT STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA HARTZLHCB5M HCB5MP3 GL PROP ATTACH CRACKED E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13937MA390 SH3040 EVA2141 DURING SCHEDULED AINT AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE LT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND LOOSE AND ONE BROKEN. ALL EIGHT (8) PROP ATTACHMENT BOLTS (PN B3339) AND WASHERS (PNA20482) WERE REMOVED AND REPLACED WITH NEW ONES PURCHASED FROM MFG, PN NR 009048. AD WAS COMPLIED WITH IAW MFG SRM 140A AND IS NEXT DUE AT 19520.9 TAT. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 T A41EU E4EA 6 CP44GL 20041129001852004112900185EU 2004 11 29 SIMA200427202 120040927A3350MS274061 SWITCH SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21222NE 340B222 EMERGENCY LIGHT ON CENTRAL WARNING PANEL DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS SWITCH IS SELECTED OFF. REPLACED EMERGENCY LIGHT SWITCH IN COCKPIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200500059) 2L72 4T4 TRTA52EU E8NE 20041129001862004112900186SO 2004 11 29 SIMA200427903 120040924A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21624AE12051 145111 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING CENTER SILL AND CLEANED AREA. INSTALLED NEW CENTER SILL IAW SRM (SRM EMB-145/1142 REV 27) CHAPTER 51-20-01, 03,04 AND 51-40-06. (SW212005280) 2L72 4T4 FRTT00011ATTE6CH 20041129001922004112900192CE 2004 11 29 FFS2004F00002 120040929A561010138402521 WINDSHIELD BEECH 1900 1900C 1154161CE PWA PT6 PT6* 52043EA COCKPIT FAILED A FFSAA UNSCHED LANDING O OTHER CRCRUISE 1 AL01575G UC155 PILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED DURING CRUISE AT FL250, OUTSIDE AIR TEMPERATURE OF -35 DEGREES C. WITH THE WINDSHIELD HEAT ON. THE CRACKS APPEARED SUDDENLY AL OVER WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE UNKNOWN. (AL01200405421) (AL01200500999) NOTE: THIS IS THE 4TH SUCH FAILURE THIS OPERATOR HAS EXPERIENCED IN 14 MONTHS. 2L72 4T3 TRTA24CE E2NE 20041129002042004112900204NE 2004 11 29 ALG2004F00051 120040924A1420 CONNECTOR SKRSKYS76 S76C 8143008NE FIRE DETECTOR DIRTY E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03860AL1337 760527 ON RUN UP, THE NR 1 FIRE CAUTION LIGHT CAME ON. MAINTENANCE CLEANED THE NR1 FIRE DETECTOR CONNECTOR PLUG AND RESET MASTER CAUTION BREAKER, GROUND OPERATIONAL CHECK WAS GOOD. 1G72 3U NCH1NE 20041130000142004113000014 2004 11 30 MASA200400292 420040524A3460111711 DISPLAY EMB 145 EMB145LR 3260212SO FMS INOPERATIVE A MASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07836MJ160557812 145359 AIRCRAFT RETURNED TO THE GATE WITH THE PILOTS FMS BLANK. THE PILOT NOTICED THE FMS CB POPPED AND SAW SMOKE COMING FROM THE CB. MX PLACED THE FMS ON MEL AND THE AIRCRAFT DEPARTED WITH NO FURTHER DISCREPANCIES. MX REPLACED THE DISPLAY UNIT. 2L72 4T RTT00011AT 20041130000152004113000015SO 2004 11 30 MASA200400629 120041108A33507287580509 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07832MJ 145310 THE FLOOR EMERGENCY EXIT LIGHT AT ROW 12 INOP. MAINTENANCE REPLACED THE LIGHT ASSY AND IT OPERATED NORMALLY. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20041130000172004113000017 2004 11 30 MASA200400627 420041106A83006014T81G27 GEARBOX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE MAKING METAL A MASAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07759957551 7361 872633 AIRCRAFT RETURNED TO THE FIELD. CREW REPORTED A LEFT FUEL SCAVENGE EJECTOR CAUTION AND A LEFT FUEL MAIN SCAVENGE CAUTION MESSAGES, FOLLOWED BY A LOW OIL PRESSURE WARNING MESSAGE. OIL PRESSURE WAS FLUCTUATING BETWEEN 25 TO 28 PSI AND WITHIN A MINUTE DROPPED TO 1 PSI WHEN THE CREW SHUT DOWN THE NR 1 ENGINE AND RETURNED TO THE FIELD. MAINTENANCE CHECKED THE ACCESSORY GEARBOX AND FOUND IT FULL OF OIL WITH PIECES OF METAL IN THE OIL. PHX ENGINE TEAM TO TRAVEL TO CAE TO REPLACE THE ACCESSORY GEARBOX AND PART IS MOVING FROM CLT AT THIS TIME. 11/9/04 MAINTENANCE REPLACED THE GEARBOX, OPS AND LEAKED CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041130000322004113000032EA 2004 11 30 COMA0460638 120041122A2760 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA SPOILERS UNKNOWN A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01931CA 7037 FLIGHT 5054 ADVANCING THRUST LEVER FOR TAKEOFF RECEIVED A CONFIGURATION WARNING. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED FUNCTIONAL TEST OF THE SPOILER CONTROL SYSTEM, DISCREPANCY COULD NOT BE DUPLCIATED. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20041130000502004113000050NE 2004 11 30 MASA200400571 220041008A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 OVERTEMP A MASAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW071733713013 7337 872560 ABORTED TAKEOFF ON ROLLOUT. PILOT REPORTED NR 2 ENGINE OVERHEAT DURING ROLLOUT. MAINTENANCE RAN ENGINE 5 TIMES TO MAX THRUST AND FOUND ITT OUT OF LIMITS DURING 2 RUNS. THIS ENGINE HAD PREVIOUS FOD DAMAGE THAT WAS WITHIN LIMITS PER GE ENGINE MANUAL. SEVERE DAMAGE TO INLET STATOR VANES. ENGINE CHANGE REQUIRED. MAINTENANCE CHANGED THE NR 2 ENGINE AND RETURNED A/C TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041130000532004113000053WP 2004 11 30 MWEA040212 120041117A57535930496507 VANE DOUG DC9 DC982 3022082WP LT WING FLAP CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 LEFT WING FIXED VANE BELOW INBOARD FLIGHT SPOILER HAS A LARGE CHAFE. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041130000582004113000058WP 2004 11 30 MWEA040207 120041116A5313527779485 LONGERON DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48006 FORWARD CARGO BAY FRAME STATION 309 LONGERON 28 RIGHT NEEDS TO BE CUT AND SPLICED. FABRICATED AND INSTALLED NEW SPLICE. 2L72 4F A6WE 20041130000612004113000061WP 2004 11 30 AALA20041144 120041118A3260 SENSOR DOUG DC9 DC982 3022082WP OVERCENTER LOCK OUT OF ADJUST A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21574AA 53151 BWI - INFLIGHT T1576/18 NOSE LANDING GEAR RED LIGHT ILLUMINATED AFTER TAKEOFF. CREW DID NOT EXPERIENCE EXCESS DRAG. CONTINUED TO BWI. ON APPROACH RECEIVED GEAR UNSAFE LIGHT WARNING. LOWERED GEAR MANUALLY AND DID A FLYBY TO CONFIRM GEAR DOWN. LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR OVER CENTER LOCK SENSOR IN ACCORDANCE WITH AMM 32 60 05 2. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041130000712004113000071EU 2004 11 30 AWXA200401304 120041112A5320D53471124200 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LT AFT SHEAR PLATE BETWEEN FR 69 AND FR 70, OUTBOARD OF BEAM Y1292. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE FROM FR 69 TO FR 70, AT Y1292; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000722004113000072EU 2004 11 30 AWXA200401305 120041118A3350321454 EPSU AIRBUS320 A320231 3930325EU ZONE 242 FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW4380113515 055 LAS - EEL - DURING 8-DAY CHECK EMERGENCY EXIT LIGHT TEST FAULTED FOR RT EXTERNAL. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041130000742004113000074EU 2004 11 30 AWXA200401306 120041112A5321D5361040400000 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN DETERIORATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK FLOOR PANEL 231CF WAS FOUND DETERIORATED. MAINTENANCE REMOVED FLOOR PANEL 231CF, FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D53610404, AND INSTALLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20041130000752004113000075EA 2004 11 30 COMA0460618 120041113A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR ACTIVATED A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01956CA 7105 FLIGHT 5316 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS WERE NORMAL AND SATISFACTORY. 2L72 4F RTA21EA 20041130000782004113000078NM 2004 11 30 AWXA200401308 120041119A2560P4010021 BATTERY BOEING737 7373Q8 1384670NM ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28327AW 23507 PDX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS INOPERATIVE, RED LIGHT DID NOT FLASH. MAINTENANCE PLACED BATTERY IN FORWARD EMERGENCY FLASHLIGHT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041130000822004113000082EU 2004 11 30 AWXA200401263 120041025A5347 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 35 AND FR 36. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 35 TO FR 36; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041130000882004113000088EU 2004 11 30 AWXA200401271 120041021A5313D53230593202 STRINGER AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND ON STRINGER 41 LT IN FORWARD CARGO COMPARTMENT BETWEEN FR 33 AND FR 34. MAINTENANCE REMOVED CORROSION ON STRINGER 41 LT BETWEEN FR 33 AND FR 34. FABRICATED A REPAIR ANGLE AND SHIMS, AND INSTALLED REPAIR PARTS IAW A320 SRM 53-21-34 FIG 202. 2L72 4F RTA28NM 20041130000912004113000091NM 2004 11 30 CALA0400722 120041120A532065C807351 ANGLE BOEING737 7373T0 1384582NM R-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND R-2 DOOR ZEE ANGLE CORRODED AT STA 907-1006, RBL 0 TO RBL 45. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20041130000972004113000097EA 2004 11 30 SWIA200414109 120041016A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07946SW 7776 STA 621 LOWER RIGHT HAND CORNER AT WL 79.5 HAS CRACK AT RADIUS. ITEM FOUND AT C-CHECK INSPECTION. REPAIR ANGLES AND RADIUS STRAP, INSTALLED AS PER REO 601R-53-61-117 AND EO 601R-53-5514. 2L72 4F RTA21EA 20041130001052004113000105EU 2004 11 30 YENA200453 120041026A5347D5311278220000 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A YENAK NONE O OTHER ININSP/MAINT 1 EA15526JB12976 1546 CORROSION EXCEEDING SRM LIMIT WAS NOTED AT THE FOLLOWING LOCATIONS: LT & RT SEAT TRACKS Y-1292 & Y+1292 BETWEEN FRAMES 16 AND FRAME 20 IS CORRODED. LT & RT DUMMY RAILS AT Y-254 & Y+254 BETWEEN FRAMES 16 AND FRAME 20 IS CORRODED. AFFECTED SEAT TRACKS AND DUMMY RAILS WERE REPLACED IN ACCORDANCE WITH SRM 51-42-11. TRACK P/N D531127822000 (L/H) & D5311281520000 (R/H). 2L72 4F RTA28NM 20041130001092004113000109NM 2004 11 30 DLM88041033 120041113A2741279007350 MOTOR DOUG MD88 MD88 3023688NM TRIM SYSTEM UNKNOWN A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27961DL 49980 PRIMARY TRIM INTERMITTENT AT TIMES INOP. REPLACED TRIM MOTOR. 2L72 4F RTA6WE 20041130001152004113000115EA 2004 11 30 SWIA200414072 120041108A2741 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07903SW 7425 F/O'S TRIM SWITCH WILL NOT ADVANCE TRIM NOSE UP. REMOVED AND REPLACED F/O'S TRIM SWITCH, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130001272004113000127EA 2004 11 30 COMA0460635 120041117A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA LEFT DIRTY A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO01708CA 7235 FLIGHT 5250 ON APPROACH INTO PIT THE CREW WAS INFORMED OF SMOKE ODOR IN THE CABIN, AN EMERGENCY WAS DECLARED AND THE OXYGEN MASKS WERE DEPLOYED. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. THE ODOR DISSIPATED ONCE THE AIRCRAFT WAS ON THE GROUND. CLEANED THE LEFT WATER SEPARATOR COALESCER SOCK. 2L72 4F RTA21EA 20041130001502004113000150NM 2004 11 30 MWEA040187 120041015A1420 CONNECTOR BOEING717 717200 1383700NM ANTI-SKID SYS CONTAMINATED A MWEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL31909ME 0675 55173 ANTI-SKID RIGHT FAIL CAME ON. FOUND CONTAMINATED CONNECTOR. CLEANED AND RESEALED CONNECTOR FOR RIGHT INBOARD SERVO VALVE. 2L72 4F TRA6WE 20041130001512004113000151 2004 11 30 MASA200400600 420041025A3417 DCU CNDAIRCL600 CL6002B19 1900309EA NR 1 FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0717275 7275 ABORTED TAKEOFF DUE TO NR 1 ENGINE HOT ICON MESSAGE ON EICAS. MX VERIFIED THE NR 1 DCU WAS CAUSING THE PROBLEM, SO THE AIRCRAFT WAS FERRIED TO PHX. MX REPLACED THE NR 1 DCU, PART INFORMATION TO FOLLOW. 2L72 4F RTA21EA 20041130001522004113000152EA 2004 11 30 MASA200400603 120041026A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR HANDLE OUT OF RIG A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0777331 7331 PILOT REPORTED A PASSENGER DOOR HANDLE WARNING IN FLIGHT. MX RE-RIGGED THE HANDLE PROX SWITCH AND RETURNED AIRCRAFT TO SERVICE. NO PARTS USED. 2L72 4F RTA21EA 20041130001532004113000153EU 2004 11 30 MALA040704 120041028A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15420XJ 340B420 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2136 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/28/04. 2L72 4T RTA52EU 20041130001602004113000160EU 2004 11 30 MALA040679 120040929A5753 SPAR SAAB SF340 340B 7860101EU LT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, LT FLAP AFT SPAR CRACKED FOR WS 140.3 TO 142.3. MAINTENANCE REPAIRED IAW SAAB SRM 57-80-10. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041130001752004113000175NM 2004 11 30 2004UALA01057 120041113A5330 BEAR STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FUSELAGE SKIN AND BEAR STRAP WERE CORRODED. CORROSION WAS REMOVED AND EXTERNAL DOUBLER REPAIR WAS ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20041130001822004113000182EU 2004 11 30 MALA040703 120041027A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15420XJ 340B420 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 3301-51, S/N 2007 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-51 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/29/04. 2L72 4T RTA52EU 20041130001862004113000186SO 2004 11 30 SWIA200414123 120041121A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07563SW 120338 ONE FLOOR EMGERGENCY LIGHT INOPERATIVE. RELAMPED AFFECTED ASSEMBLY AS NEEDED, OPERATIONAL CHECK GOOD IAW EMB 120 MM 33-51-01. 2L72 4T RTA31SO 20041130002012004113000201EA 2004 11 30 MASA200400606 120041027A5240 MECHANISM CNDAIRCL600 CL6002D24 1390016EA SERVICE DOOR LACK OF LUBE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07904FJ 15004 SERVICE DOOR WAS DIFFICULT TO OPEN. MX LUBED SERVICE DOOR, NO FURTHER DISCREPANCIES. 2L72 4F RTA21EA 20041130002022004113000202EU 2004 11 30 AWXA200401281 120041022A5310D53475765204 BEAM AIRBUS320 A320231 3930325EU CARGO DOOR SILL CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK CORROSION WAS FOUND AT FASTENER HOLES ON LOWER SILL BEAM OF BULK CARGO DOOR BETWEEN FR 60 AND FR 62, STR 38 RT. MAINTENANCE CUT OUT DAMAGE IN SILL BEAM FROM FR 60 TO FR 62, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49, FIG 203. 2L72 4F RTA28NM 20041130002082004113000208SO 2004 11 30 SWIA200414131 120041123A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07189SW9031 9031 120048 WITH FLAPS SELECTED TO 15 DEGREES CONTROL FAULT OCCURRED DUE TO OUTBOARD FLAPS. REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. REPLACED RIGHT INBOARD FLAP CANNON PLUG IAW WMM 20-50-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041130002112004113000211EA 2004 11 30 SWIA200414088 120041108A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAILED A SWIAO OTHER O OTHER DEDESCENT 1 NM07959SW 7840 LEFT FRONT INBOARD PLY WINDSHIELD SHATTERED ON DESCENT THROUGH 26,000. INSTALLED NEW WINDSHIELD IN NR 1 POSITION IAW 56-12-01. P/N OFF 601R33033-17, S/N OFF 03122H3201. 2L72 4F RTA21EA 20041130002132004113000213EA 2004 11 30 SWIA200414090 120041112A2740DL2428M4 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA ELEVATOR MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07946SW 7776 ELEVATOR FEELS STIFF. REMOVED AND REPLACED LT ELEVATOR PITCH FEEL LINEAR ACTUATOR IAW AMM 27-31-00. OPERATIONAL CHECK GOOD. P/N DL2428M4, S/N ON 2437, S/N OFF 2160. 2L72 4F RTA21EA 20041130002152004113000215EA 2004 11 30 SWIA200414092 120041114A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07426SW3977 3977 7468 LEFT SPOILERON INBOARD PCU POSITION FAIL. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130002252004113000225NM 2004 11 30 AWXA200401330 120041123A2560P4010021 BATTERY BOEING737 7373U3 13844CCNM ZONE 900 DISCHARGED A AWXAO OTHER O OTHER NRNOT REPORTED 1 WP28335AW 28740 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041130002352004113000235SO 2004 11 30 SWIA200414147 120041005A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FUSELAGE; CORROSION FOUND ON SEAT TRACK (BROWN LINE) AND AROUND SCREW HEADS AS MARKED AT FR 15 - FR 31, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, AND AMM 20-00-00. 2L72 4T RTA31SO 20041130002372004113000237 2004 11 30 AWXA200401284 420041104A256565C318411 SLIDE BOEING737 7373Y0 1384671NM R-2 DOOR FRAYED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - EES - DURING C-15 CHECK THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING WAS FOUND FRAYED. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY ESCAPE SLIDE WEBBING IAW B737-300 SRM 51-40-02 FIG 3-4, & 6-8. 2L72 4F RTA16WE 20041130002452004113000245EU 2004 11 30 AWXA200401318 120041116A5321D5367160100000 FLOOR PANEL AIRBUS320 A320232 3930326EU CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK FOUND CABIN FLOOR PANEL 251FF DELAMINATED BETWEEN FR 58-62. MAINTENANCE CUT OUT DAMAGE IN CABIN FLOOR PANEL 251FF AND PERFORMED BOND REPAIR IAW A320 SRM 53-12-00 FIG 204. 2L72 4F RTA28NM 20041130002502004113000250EA 2004 11 30 SWIA200414104 120041111A2760 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILERS INOPERATIVE A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07706SK 10149 SSCU NR 2 INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED NR 2 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N:613645BA03, S/N OFF:735. 2L72 4F RTA21EA 20041201000042004120100004 2004 12 1 DL764041037 420041116A2330 VIDEO DISPLAY BOEING767 767432ER 1385134NM CABIN ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27831MH 29702 ATER T/O FLT ATTENDANT REPORTED NO VIDEO AVAILABLE. TRIED RESETTING THE SYSTEM A COUPLE OF TIMES AND NO HELP. ABOUT 3 HRS INTO FLIGHT THE FLT ATTENDANTS REPORTED A STRANGE ODOR POSSIBLE ELECTRICAL NEAR SEATS 6A/B, APPEARED TO COME FROM OVERHEAD AREA. POWER WAS REMOVED FROM PAX READING LIGHTS AT THE F/A VIDEO CONSOLE. ODOR DISSIPATED. POWER SWITCH LEFT OFF FOR REMAINDER OF FLIGHT. FWD TO MCO AND PLAC IFE ENT DUE TO BOOTUP PROBLEMS. NO SOURCE OF STRANGE ODOR NOTICED. INSPECTED OVERHEAD FLUORESENTS, INDIV SEAT PCUS, SIDEWALL LIGHTS, READING LIGHTS, O2 GEN IN FWD AREA 1-10. 2L72 4F RTA1NM 20041201000102004120100010EU 2004 12 1 AWXA200401321 120041025A5321D5348015800500 FLOOR PANEL AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR PANEL PLATE AT FR 66, -Y60 RT. MAINTENANCE REMOVED CORRODED PANEL PLATE AT FR 66, -Y60 RT; FABRICATED A NEW REPLACEMENT PANEL PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201000272004120100027NE 2004 12 1 SWIA200414078 220041008A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT FAILED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07416SW7813 7813 7089 873040 LT ENGINE CHANGE REQUIRED DUE TO FAILED BOROSCOPE INSPECTION. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041201000292004120100029EA 2004 12 1 SWIA200414080 120041030A2750 DRIVE ASSY CNDAIRCL600 CL6002B19 1900309EA TE FLAPS CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 LEFT WING NR 5 FLEX DRIVE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLEX DRIVE REMOVED, SURFACE CORROSION ON HEX END REMOVED, POWER CORE LUBRICATED, NEW END SEAL INSTALLED, FLEX SHAFT REINSTALLED IAW 27-53-10-400-805. 2L72 4F RTA21EA 20041201000382004120100038NE 2004 12 1 2004UALA01113 220041112A7230 BLADES BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 4 ENGINE FAILED A UALAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29174UA 24381 NR 4 ENGINE SHUT DOWN DUE TO HIGH EXHAUST GAS TEMPERATURE & LOSS OF POWER. ENGINE EXPERIENCED SURGE AFTER TAKEOFF. UPON INVESTIGATION FOUND MASSIVE HPC DAMAGE. ROOT CAUSE OF THE FAILURE WAS THE 6TH STAGE BLADE DETACHMENT THIS IS AN INDUSTRY ISSUE WITH THE FRONT END DURABILITY BEING WORKED BY THE OEM. 2L74 4F4 FRTA20WE E24NE 20041201000432004120100043EU 2004 12 1 YENA200455 120041123A25304110001137 COFFEEMAKER AIRBUS320 A320232 3930326EU GALLEY ODOR A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15504JB 1156 APPROX 25 MINS INTO FLT AT 370 NR 1 F/A CONTACTED FLT DECK REPORTING STRONG BURNING ODOR AROUND NR 1 GALLEY & GETTING STRONGER. ODOR SEEMED TO BE COMING FROM VENTS. PERFORMED SMOKE/AVIONICS SMOKE CHECKLIST IAW QRH 1.10, SMELL INTENSIFIED. PERFORMED SMOKE/TOXIC FUMES REMOVAL IAW QQRH 1.9, SMELL DISSIPATED. PERFORMED INSP OF FWD GALLEY, LAV A, AND PAX SEATS SEB & VDU'S AROUND ROWS 1, 2, 3. COULD NOT DUPLICATE OR FIND SOURCE OF ODOR, IAW INFO NOTICE 2004T023TR AND TSM 24-00-00-810-823. PERFORMED MX EVALUATION ON FERRY FLT FROM JAX TO FLL, NO DISCREPANCIES NOTED. REPLACED FWD GALLEY COFFEEMAKERS PRECAUTIONARY. 2L72 4F RTA28NM 20041201000452004120100045EU 2004 12 1 UPS04143496 120041115A5210 LEVER AIRBUSA300 A300F4622R 3930360EU PAX DOOR UNSECURE A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01147UP 0830 LEVER FOR MAIN ENTRANCE DOOR MOVED UP APPROX 2 INCHES DURING CLIMBOUT OF BQN. CABIN PRESS BUZZER CAME ON. ALL ECAM SYS NORMAL. PRESSURIZED A/C TO 8 PSI AND DOOR LEVEL STAYED IN PLACE OPEN AND CLOSED DOOR OPERATES NORMAL & CABIN PRESS LIGHT OPERATES NORMAL IAW MM 52-10-11-5. 2L72 4F RTA35EU 20041201000572004120100057NM 2004 12 1 SWAA043415 120041121A53306545773 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING WALKAROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 727D+6, STR 14R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20041201000592004120100059SO 2004 12 1 SWIA200414105 120041108A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07188SW 120039 BOTH OUTBOARD FLAPS WILL NOT MOVE. REMOVED AND REPLACED RIGHT OUTBOARD FLAP AND LEFT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-04. OPERATIONAL CHECK GOOD IAW 27-50-00. 2L72 4T RTA31SO 20041201000652004120100065NM 2004 12 1 MASA200400612 120041029A56108SC0043014 WINDSHIELD DHAV DHC8 DHC8202 2809007NM COCKPIT SPARKS A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07436YV2156 436 AIRCRAFT DIVERTED TO GJT DUE TO THE FIRST OFFICERS WINDSHIELD HEAT CAUSING SMOKE IN THE FLIGHT DECK. AIRCRAFT IS CURRENTLY AOG FOR A WINDSHIELD, SDR OPEN FOR FURTHER INVESTIGATION. 10/29 MX REPLACED WINDSHIELD. 2H72 4T RTA13NM 20041201000672004120100067SO 2004 12 1 RAIA00411004 120041105A213122250N030201 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03840HK8806 145341 BDL- RAPID DECOMPRESSION AT 30,000 FEET UNCOMMANDED. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER. 2L72 4T RTT00011AT 20041201000782004120100078EU 2004 12 1 MALA040697 120041013A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING CAPACITY INSPECTION IN MSP, EMERGENCY POWER SUPPLY P/N 61-0478-9, S/N 9710076 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/18/04. 2L72 4T RTA52EU 20041201000822004120100082NM 2004 12 1 DL73S041043 120041120A53106546877143 SHEAR BEAM BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 STRINGER 18A SHEAR BEAM WEB CRACKED AT STA 727 ON BOTH THE LT AND RT SIDES. REPAIRED IAW ERA 094822-14. 2L72 4F A16WE 20041201001062004120100106 2004 12 1 2004UALA00659 420040709A2565 BOTTLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE ESCAPE SLIDE MISPINNED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29120UA10413 GT1099 29166 DURING SLIDE OVERHAUL SAFETY PIN FOR BOTTLE FOUND INSTALLED IN REGULATOR. *S/D* PIN INCORRECTLY LEFT IN BOTTLE DURING PREVIOUS SLIDE OVERHAUL. AS SHOP AND PERSONNEL THAT OVERHAULED THIS SLIDE ARE NO LONGER BEING USED, NO CORRECTIVE ACTION NECESSARY. BOTTLE AND SLIDE RECEIVED ROUTINE CHECK AND WERE RETURNED TO SERVICE AFTER PIN REMOVAL. 2L74 4F4 FRTA20WE E24NE 20041201001162004120100116NM 2004 12 1 F3LA200400107 120041002A5320 WEB BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR WEBS AFT OF STA 1016 FLOORBEAM, CENTER OF FUSELAGE, CORRODED. REPLACED FLOOR WEB HAT CHANNEL, STA 1016, BL 0, PER DRAWING 69-77731, AND SRM 51-40-02 AND 53-60-51. 2L72 4F RTA16WE 20041201001222004120100122EA 2004 12 1 SWIA200414118 120041121A2701 NUT CNDAIRCL600 CL6002B19 1900309EA CONTROL YOKE LOOSE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07965SW 7871 F/O'S CONTROL YOKE CLICKS WHEN FULL DEFLECTION RIGHT OR LEFT AILERONS. RETORQUED NUT ON F/O'S YOKE AS REQUIRED, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20041201001252004120100125EA 2004 12 1 SWIA200414121 120041120A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07403SW 7028 WHEN SELECTING FLAPS 8 FLAPS FAIL CAUTION MESSAGE. REPLACED RIGHT INBOARD FLAP ACTUATOR; RIGHT INBOARD FLAP OUTBOARD ACTUATOR; LEFT WING INBOARD FLAP INBOARD ACTUATOR; LEFT WING INBOARD FLAP OUTBOARD ACTUATOR IAW SB 601R27-120 AND MM 27-53-01, 27-53-05. OPERATIONAL CHECK GOOD. P/N OFF 852D100-11, S/N OFF 1450AB, P/N OFF 852D100-9, S/N OFF 181, P/N OFF 852D100-11, S/N OFF 232AB, P/N OFF 852D100-9, S/N OFF 162. 2L72 4F RTA21EA 20041201001262004120100126EA 2004 12 1 SWIA200414122 120041117A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA UNIT-SKEW MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07973SW 7949 ON TAXI, FLAPS SELECTED TO 30, THE FLAP FAIL AMBER MESSAGE CAME ON. REPLACED NR 4 RIGHT AFT SKEW DETECTOR SENSOR AND SKEW DETECTION UNIT. OPERATIONAL CHECK GOOD IAW MM 27-51-15. P/N 601R59014-1, S/N OFF A317. 2L72 4F RTA21EA 20041201001282004120100128 2004 12 1 SWAA043417 420041122A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20041201001322004120100132NM 2004 12 1 SWAA043421 120041122A53306550570 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041201001332004120100133NM 2004 12 1 SWAA043422 120041122A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE KEELBEAM CORRODED AT STR 28L, BETWEEN BS 500D AND BS 520. REPAIRED KEEL BEAM SECTION PER SRM. 2L72 4F RTA16WE 20041201001342004120100134 2004 12 1 SWAA043423 420041122A256565C16820 CLIP BOEING737 7373H4 1384600NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK CLIPS LOOSE. SECURED STOW HOOK CLIPS PER MM. 2L72 4F RTA16WE 20041201001362004120100136NM 2004 12 1 MWEA040192 120041025A27315930497502 TAB DOUG MD88 MD88 3023688NM ELEVATOR NICKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 RIGHT ANTI-FLOAT TAB HAS TWO SMALL DINGS ON UPPER SURFACE. FABRICATED AND INSTALLED FILLERS AND REPAIR DOUBLER. 2L72 4F RTA6WE 20041201001372004120100137NM 2004 12 1 MWEA040193 120041025A532199366403 FLOORBOARD DOUG MD88 MD88 3023688NM FUSELAGE DELAMINATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 497601 CABIN FLOORBOARD FROM STATION 888 TO STATION 997, BETWEEN RIGHT SEAT TRACKS IS DELAMINATED. FABRICATED AND INSTALLED NEW FLOORBOARD. 2L72 4F RTA6WE 20041201001412004120100141WP 2004 12 1 ARWA20041005 120041024A2612D5020 FIRE LOOP DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE SHORTED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19441J 45988 669436 ON CLIMBOUT THROUGH 15,000 FT MASTER FIRE WARNING SOUNDED WITH LIGHT INDICATION ON NR 4 ENGINE. PERFORMED EMERGENCY CHECKLIST (RETARDED POWER LEVER, FIRE SHUTOFF LEVER FORWARD, LIGHT CONTINUED ON, FIRE EXT AGENT, LIGHT WENT OUT). COMPLETED CHECKLIST, ALL OTHER SYSTEMS NORMAL. RETURNED TO SBEG WITHOUT INCIDENT. PERFORMED ENGINE VISUAL INSPECTION FOR EVIDENCE OF FIRE; NO EVIDENCE OF FIRE NOTED; PERFORMED ENGINE RUN-UP AND FOUND NO REMOTE LEAKS. DURING ENGINE INSPECTION FOUND LOWER FIRE LOOP ELEMENT SHORTED OUT. REMOVED AND REPLACED LOWER ELEMENT IN ACCORDANCE WITH M/M 26-10-1. PERFORMED ENGINE RUN-UP AND OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH 71-00 AND 26-10-1. 2L74 4F4 F 4A25 1E8 20041201001432004120100143WP 2004 12 1 AALA20041145 120041119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217540A 49994 DEN - EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B528 FOR INOPERATIVE EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041201001442004120100144NM 2004 12 1 AWXA200401319 120041122A2560P2070001214 FLASHLIGHT BOEING737 73733A 1384673NM ZONE 900 INOPERATIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 LAS - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041201001462004120100146EA 2004 12 1 SWIA200414098 120041107A274170608 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07418SW 7746 STAB CHANNEL 1 WON`T ENGAGE. REMOVED AND REPLACED CB PANEL CB F5 AND HSTCU COMPUTER. OPERATIONAL CHECKS GOOD IAW 27-41-01. P/N OFF 7060-8, S/N OFF 959. 2L72 4F RTA21EA 20041201001472004120100147EA 2004 12 1 QXEA200040078 120041119A5230 DOOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY UNSECURE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09617QX2536 10130 ABQ - FLIGHT 4182 - FLIGHT RETURNED TO FIELD AFTER RECEIVING A CABIN ALTITUDE CAUTION MESSAGE. THE CABIN PRESSURE ADJUSTMENT WAS INOPERABLE IN BOTH THE AUTO AND MANUAL MODES. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR NOT PROPERLY SEATED. THE DOOR WAS CYCLED AND OPERATIONAL CHECKS PERFORMED. ALL CHECKS WERE NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041201001482004120100148EA 2004 12 1 QXEA200400782 120041119A5230 DOOR CNDAIRCL600 CL6002C10 1390015EA CARGO BAY UNSECURE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09617QX2536 10130 ABQ - FLIGHT 4182 - FLIGHT RETURNED TO FIELD AFTER RECEIVING A CABIN ALTITUDE CAUTION MESSAGE. THE CABIN PRESSURE ADJUSTMENT WAS INOPERABLE IN BOTH THE AUTO AND MANUAL MODES. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR NOT PROPERLY SEATED. THE DOOR WAS CYCLED AND OPERATIONAL CHECKS PERFORMED. ALL CHECKS WERE NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20041201001492004120100149NM 2004 12 1 F3LA200400109 120041004A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT CORRODED AT STA 1010, RBL 10. REPLACED FLOORBEAM SUPPORT PER SRM 51-40-02, 51-40-05 AND BAC DRAWING 65C33375. 2L72 4F RTA16WE 20041201001512004120100151EU 2004 12 1 AWXA200401261 120041025A5347D5337111120202 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 43 AND FR 44. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 43 TO FR 44; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201001532004120100153EU 2004 12 1 AWXA200401286 120041105A5210FE240004 DAMPER AIRBUS320 A320232 3930326EU R-1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW2448015901 543 MCN - MAJOR REPAIR - DURING C-06 CHECK A .375 INCH CRACK WAS FOUND IN THE R-1 DOOR STRIKER ASSEMBLY. MAINTENANCE REMOVED AND REPLACED R-1 DOOR DAMPER CYLINDER IAW AMM 52-11-14. 2L72 4F RTA28NM 20041201001572004120100157EU 2004 12 1 YENA200452 120041108A2121EVT3454H FAN AIRBUS320 A320232 3930326EU AVIONICS BAY FAILED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15522JB14299 1464 VENT EXTRACT FAN FAULT FOLLOWED BY ELECTRIC FUMES IN COCKPIT AND CABIN. PERFORMED INSPECTION OF COCKPIT AND CABIN PER TSM 24-22-810-823. FOUND EXTRACT FAN AT FAULT, PLACED ON MEL 21-26-02. AT THE COMPLETION OF FLT 28 REPLACED EXTRACT FAN PER 21-26-51-000-001, OPERATIONS CHECK GOOD PER 21-26-51-710-001. ALSO CONFIRMED UPON VISUAL INSPECTION THAT THE EXTRACT FAN FAILED INTERNALLY, POSSIBLE BEARING FAILURE. 2L72 4F RTA28NM 20041201001582004120100158NM 2004 12 1 AWXA200401257 120041111A2560P4010021 BATTERY BOEING757 7572G7 1384963NM ZONE 900 - DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK THE FORWARD EMERGENCY FLASHLIGHT DID NOT FLASH RED EVERY 10 SECONDS AS REQUIRED. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20041201001592004120100159NM 2004 12 1 AWXA200401258 120041110A2910NAS1611228 PACKING BOEING737 7373Q8 1384670NM HYD SYSTEM FAILED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28327AW 23507 ABQ - DIVERSION - FLT 0596 - EN ROUTE FROM PHX TO MCI LOST -A- HYDRAULIC SYSTEM PRESSURE, DIVERTED INTO ABQ AND LANDED WITHOUT EVENT. MAINTENANCE FOUND THE NR 4 GROUND SPOILER ACTUATOR UNION O-RING HAD BURST ON PRESSURE SIDE. REPLACED O-RING IAW AMM 20-10-17, LEAK CHECK WAS GOOD. 2L72 4F RTA16WE 20041201001602004120100160EU 2004 12 1 AWXA200401259 120041025A5347D5337111200400 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND RT INBOARD SEAT TRACK BETWEEN FR 44 AND FR 45. MAINTENANCE REMOVED CORRODED RT INBOARD SEAT TRACK FROM FR 44 TO FR 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201001612004120100161WP 2004 12 1 ABXA040379 120041102A5312995822125 ANGLE DOUG DC9 DC932 3022066WP MLG WW BULKHEAD CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 LEFT WHEEL WELL AFT BULKHEAD UPPER ANGLE CORRODED AT BUTTLINE 0. REPAIRED ANGLE IAW REA D953-51024-MR. 2L72 4F A6WE 20041201001622004120100162WP 2004 12 1 ABXA040378 120041101A531327779223 LONGERON DOUG DC9 DC932 3022066WP E & E BAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 LONGERON 23 LEFT CRACKED AT STA 200. REPAIRED LONGERON IAW DC-9 SRM 53-02. 2L72 4F A6WE 20041201001632004120100163EA 2004 12 1 COMA0460637 120041121A3260555406 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01914CA11362 7012 FLIGHT 5091 RECEIVED A LANDING GEAR DISAGREE CAUTION AND NOSE DOOR WARNING INBOUND TO CRW. CREW DECLARED AN EMERGENCY AND GEAR WAS EXTENDED MANAUALLY. REPLACED THE NOSE LANDING GEAR SELECTOR VALVE. 2L72 4F RTA21EA 20041201001652004120100165NM 2004 12 1 F3LA200400076 120040812A2700 SWITCH AIRBUSA319 A319111 3930336NM ELAC 2 MALFUNCTIONED A F3LAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 NM03921FR 2010 BLOCK TURNBACK. FLIGHT CREW REPORTED ELAC 2 ECAM MESSAGE. RESET ELAC 2 SWITCHES AND FAULT CLEARED. 2L72 4F RTA28NM 20041201001672004120100167SO 2004 12 1 RAIA00411005 120041107A5270 SWITCH EMB 145 EMB145 3260210SO GALLEY DOOR DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03801HK 145053 PIT- SERVICE DOOR OPEN EICAS MESSAGE IN FLIGHT. MAINTENANCE CLEANED GALLEY DOOR SWITCH. 2L72 4F RTT00011AT 20041201001722004120100172EU 2004 12 1 CX7A194J0437 120040704A261251533174 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE BROKEN A CX7AEB ENGINE SHUTDOWN EMER. DESCENT N FALSE WARNING CRCRUISE 1 GL03303CE 340B194 LEFT BLEED AIR LEAK. RAN CHECKLIST, LIGHT STAYED ON. SHUT DOWN LEFT ENGINE, DIVERTED TO SBN. 2L72 4T RTA52EU 20041201001732004120100173WP 2004 12 1 MWEA040215 120041124A533059360071 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 FUSELAGE SKIN DENT AT STATION 1305, LONGERON 19 RIGHT IS WITHIN 1 INCH OF LONGERON AND NO LONGER MEETS CONDITION PER STRUCTURAL REPAIR MANUAL. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041201001752004120100175EA 2004 12 1 COMA0460642 120041122A5310 DOUBLER CNDAIRCL600 CL6002B19 1900309EA CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01973CA 7146 LEFT HAND DOUBLER AT FS 559 IS CORRODED. REPAIRED IAW REO 601R-53-41-254 REV A. 2L72 4F RTA21EA 20041201001772004120100177WP 2004 12 1 AALA20041150 120041121A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217537A 49991 ORD - CEILING MOUNTED EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041201001782004120100178WP 2004 12 1 MWEA040211 120041118A5330591140733 SKIN DOUG DC9 DC981 3022081WP FUSLEAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 FUSELAGE SKIN DENTED AT STATION 212.5 LONGERON 17 RIGHT, DENT IS WITHIN 1 INCH OF LONGERON AND NO LONGER MEETS REQUIREMENTS OF CONDITION. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041201001792004120100179NM 2004 12 1 AALA20041153 120041122A3397 WIRE BOEING777 777223 1385213NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21772AN 29580 DFW - EMERGENCY SEAT LIGHTS IN AFT CABIN INOPERATIVE. REPAIRED SHORT IN WIRE AT ROW 36 FOR EMERGENCY SEAT LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041201001822004120100182WP 2004 12 1 AALA20041151 120041121A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217537A 49991 ORD - CEILING MOUNTED EMERGENCY LIGHTS BETWEEN SEAT ROWS 13 AND 16 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EMERGENCY LIGHTS BETWEEN SEAT ROWS 13 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041201001832004120100183WP 2004 12 1 ARWA20040701 120040714A3231 LINKAGE DOUG DC8 DC862 3021970WP NLG DOOR VIBRATION A ARWAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19810BN 45905 AFTER TAKEOFF HEAVY NOISE VIBRATION EXPERIENCE. CYCLE GEAR SEVERAL TIMES WITH NO CHANGE, RETURNED TO FIELD. FUEL DUMPED PER ABNORMAL CHECKLIST. CHECKED NOSE GEAR DOOR LINKAGE IN ACCORDANCE WITH MM 32-22-2; OPERATIONS AND TESTED IN ACCORDANCE WITH MM 32-21-1. CLEANED AND LUBED IAW MM 32-21-1. 2L74 4F 4A25 20041202000012004120200001NM 2004 12 2 DL738041050 120041122A2530MSC1151 CHILLER BOEING737 737832 13844CFNM FWD GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO273760C 30816 CREW REPORTED BURNING ODOR FROM FORWARD GALLEY CHILLER. TURNED CHILLER OFF AND SMELL WENT AWAY. REPLACED CHILLER. 2L72 4F RTA16WE 20041202000022004120200002EU 2004 12 2 MALA040689 120040922A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15366PX 340B267 DURING CAPACITY INSPECTION IN MSP, EMERGENCY LIGHT POWERED BY POWER SUPPLY P/N 60-1321-1, S/N 14587, SQUAWKED INOP. MAINTENANCE DEEP CYCLED & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/6/04. 2L72 4T RTA52EU 20041202000032004120200003NM 2004 12 2 MWEA040198 120041029A534523010431 MOUNT DOUG MD88 MD88 3023688NM GALLEY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 GALLEY ONE MOUNTING FEET HAVE MINOR CORROSION. REMOVED CORROSION. 2L72 4F RTA6WE 20041202000042004120200004WP 2004 12 2 ARWA20040703 120040715A5700 UNKNOWN DOUG DC8 DC863F 302198FWP LT WING UNKNOWN A ARWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO19441J 45988 AFTER APP TAKEOFF POWER HEARD BANG ON LEFT HAND SIDE WING. INSPECTED LEFT HAND WING IN ACCORDANCE WITH MM 57-00; NO OBVIOUS DEFECTS NOTED. ALSO INSPECTED LEFT HAND MAIN LANDING GEAR AND DOORS IN ACCORDANCE WITH MM 32-10-0, NO OBVIOUS DEFECTS NOTED. PERFORMED ENGINE RUN UP AND TAXI IN ACCORDANCE WITH MM 9-00 AND 71-00. ALL PARAMETERS NORMAL; PERFORMED FLIGHT CONTROL CHECK AND FOUND TO BE NORMAL IN ACCORDANCE WITH MM 27-00. COULD NOT DUPLICATE FAULT AT THIS TIME. 2L74 4F 4A25 20041202000052004120200005EA 2004 12 2 COMA0460624 120041115A275011045D100301 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA NR 3 MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5488 FLAPS FAIL CAUTION MESSAGE. REPLACED THE NR 3 FLEX DRIVE SHAFT. 2L72 4F RTA21EA 20041202000072004120200007EU 2004 12 2 YENA200458 120041126A3350 LIGHT AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A YENAO OTHER L NO TEST TXTAXI/GRND HDL 1 EA15526JB 1546 EMERGENCY EXIT LIGHTS INOP. RESET ACFT, PERFORMED OPS TEST. OK FOR SERVICE IAW 33-51-00, NO PRIOR HISTORY. 2L72 4F RTA28NM 20041202000082004120200008NM 2004 12 2 F3LA200400079 120040819A53126710282 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACKED WEB 178 BULKHEAD AT BL 19R, WL 195. REMOVED CRACKED WEB PER SRM 51-40-02. REMOVED DOUBLER PER SRM 51-40-02. PARTIALLY OPENED 178 BULKHEAD WEB TO GET ACCESS TO CRACKED WEB PER SRM 51-40-02. DRILLED NEW INTERCOSTAL PER BAC DWG 72038 AND SRM 51-40-05. INSTALLED FASTENERS THAT ATTACH WEB TO OUTER SKIN PER SRM 51-40-02. 2L72 4F RTA16WE 20041202000102004120200010EA 2004 12 2 SWIA200414134 120041024A5340 ATTACH BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 ATTACH BRACKETS CRACKED AT FS 280 INBOARD AND OUTBOARD OF LBL 9. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED (2) EACH 601R31113-57 ANGLES PER ENG DWG 601R31113 AND SRM 51-42-06 PAGES 5, 6, AND 7. 2L72 4F RTA21EA 20041202000112004120200011EA 2004 12 2 SWIA200414135 120041024A5340 ATTACH BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW ATTACH BRACKETS CRACKED AT FS 280 INBOARD AND OUTBOARD OF RBL 9. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED (2 EA) ATTACH BRACKETS AT FS 280 INBOARD AND OUTBOARD OF RBL 9 IAW CRJ 200 SRM 51-42-21 FIG 11 AND 51-42-06 FIG 8. 2L72 4F RTA21EA 20041202000122004120200012EA 2004 12 2 SWIA200414136 120041024A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 FS 589 LEFT ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE PER ENG DWG 601R35011 REV R. 2L72 4F RTA21EA 20041202000142004120200014NE 2004 12 2 MALA040655 220041012A7397230391202 WIRE HARNESS BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE HMU DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15536XJ E2372 NR 2 ENGINE EGT GAUGE ERRATIC. AIRCRAFT RETURNED TO MSP AFTER TAKEOFF DUE TO THE NR 2 ENGINE EGT FLUCTUATING -0- TO NORMAL. MAINTENANCE INSTALLED NR 2 ENGINE ECU-HMU HARNESS ASSEMBLY BY PIGGY BACKING IN SERVICEABLE HARNESS, OPS CHECKS GOOD. TEMPORARILY INSTALLED NR 2 ENGINE ECU/HMU HARNESS ASSY. PERMANENTLY INSTALL HARNESS P/N 2-303-912-02 AT NEXT MX CONVENIENCE OR NEXT NR 2 ENGINE CHANGE. 2H74 4F4 FRTA49EU E6NE 20041202000152004120200015WP 2004 12 2 0401989911 120041110A4930 FUEL FILTER HONEYWELL DOUG DC9 DC931 3022065WP APU LEAKING A NWAAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01961N P30719DCA 47405 PILOT REPORTED A STRONG OIL/FUEL ODOR IN THE AIRCRAFT FOR ENTIRE LENGTH OF THE FLIGHT. MAINTENANCE FOUND THE APU LOW PRESSURE FUEL FILTER LEAKING 72 DROPS PER MINUTE. MAINTENANCE REPLACED THE FUEL FILTER AND PACKING. ALSO REPLACED COALESCER BAGS. COMPLIED WITH PACK BURNOUT PROCEDURES. 2L72 4F A6WE 20041202000162004120200016 2004 12 2 SWAA043270 420041109A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29646SW 28331 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041202000182004120200018WP 2004 12 2 AALA20041119 120041111A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21510AM 49804 DEN - OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5102 FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202000192004120200019WP 2004 12 2 AALA20041115 120041110A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21244AA 49256 SFO - CEILING EMERGENCY LIGHTS BETWEEN ROWS 22 AND 26 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 22 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202000242004120200024EU 2004 12 2 AWXA200401325 120041112A5320D5347217320100 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BEAM -Y254 RT AT FR 68. MAINTENANCE REMOVED CORRODED BEAM -Y254 RT FROM FR 66 TO FR 68; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041202000272004120200027EU 2004 12 2 AWXA200401328 120041114A53212024T3071 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSLEAGE TORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK FOUND AFT CARGO COMPARTMENT ALUMINUM FLOOR PANEL PLATE TORN BETWEEN FR 49 AND FR 50. MAINTENANCE REMOVED CORRODED AFT CARGO COMPARTMENT FLOOR PANEL PLATE; FABRICATED A NEW REPLACEMENT PLATE FROM 2024T3.071; AND INSTALLED REPAIR PART IAW EO 5326-01007. 2L72 4F RTA28NM 20041202000312004120200031NM 2004 12 2 SWAA043356 120041116A55526959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RIGHT NR 1 TAB HINGE BOLT AND BUSHING PER MM. 2L72 4F RTA16WE 20041202000322004120200032WP 2004 12 2 AALA20041146 120041119A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21597AN 53287 ORD - FIRST CLASS GALLEY SIDEWALL MOUNTED EMERGENCY LIGHT FAILED TO TEST. REPLACED THE LIGHT ASSEMBLY FOR THE FIRST CLASS GALLEY SIDEWALL MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041202000342004120200034NE 2004 12 2 AALA20041154 220041121A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT FAILED A AALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SW21433AA 49451 725630 DFW - INFLIGHT T1166/21 LEFT ENGINE FAILED WITH VERY LOUD BANG THAT WAS FELT AND HEARD IN COCKPIT. ENGINE WAS PREVIOUSLY RUNNING SMOOTHLY AT 1.34. STABILIZED ENGINE PRESSURES RATIO. ENGINE APPEARED TO BE SEIZED. PRELIMINARY INSPECTION REVEALED METAL IN TAILPIPE. REPLACED DAMAGE IN TAILPIPE AREA. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20041202000382004120200038WP 2004 12 2 AALA20041143 120041119A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217531A 49923 TPA - COCKPIT AND FORWARD AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT POSITION B523 FOR EMERGENCY LIGHT AT COCKPIT AND FORWARD AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202000392004120200039NM 2004 12 2 2004UALA01140 120041118A2910 O-RING AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE YELLOW HYD SYS LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29813UA 858 YELLOW SYSTEM LOW LEVEL ECAM MESSAGE. CREW FOLLOWED ECAM, EDP SELECTED OFF. YELLOW SYSTEM PRESSURE ZERO, WITH QUANTITY IN AMBER ZONE. REPLACED O-RING ON YELLOW SYSTEM MANIFOLD. 2L72 4F4 FRTA28NM E40NE 20041202000402004120200040NM 2004 12 2 2004UALA01141 120041119A5412 FIREWALL BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 PYLON GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 NR 2 PYLON I/B FIREWALL BULKHEAD IS GOUGED. 2L72 4F4 FRTA2NM E17NE 20041202000412004120200041NM 2004 12 2 2004UALA01142 120041118A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 CABIN FLOORBEAM STA 324 AND RBL 53 HAS CORROSION. REMOVED DAMAGED T CAP SECTION AND INSTALLED NEW SECTION SPLICED WITH DOUBLERS. 2L72 4F4 FRTA2NM E17NE 20041202000422004120200042EA 2004 12 2 SWIA200414066 120041107A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07720SW 7297 THIRD EMERGENCY FLOOD LIGHT ON CEILING INOPERATIVE. RELAMPED 3RD EMERGENCY FLOOD LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041202000432004120200043EA 2004 12 2 MASA200400554 120041001A783032725706 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW072731818578 7318 THE CREW ABORTED THE TAKEOFF DUE TO THE RT THRUST REVERSER DISAGREE MESSAGE THAT CAME ON DURING TAKEOFF. MAINTENANCE PERFORMED MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 10/11/04 MAINTENANCE REPLACED RT INBOARD ACTUATOR, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041202000452004120200045NM 2004 12 2 DL764041019 120041106A3350 LAMP BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAO OTHER L NO TEST ININSP/MAINT 1 SO27837MH 29710 RIGHT AISLE EMERGENCY ESCAPE PATH OVERHEAD LAMP AT FORWARD BULKHEAD INOP. RELAMPED, OPS OK. 2L72 4F RTA1NM 20041202000462004120200046NM 2004 12 2 2004UALA01143 120041118A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 AFT PIT STA 1580 FRAME DENTED AT STR 25R. DAMAGED WAS CUTOUT AND FRAME J ANGLE REPAIR WAS ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20041202000482004120200048EU 2004 12 2 YENA200440 120040703A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT DISCHARGED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15519JB1386013860 1398 WHILE PERFORMING TEST OF THE EMERGENCY LIGHTS, L EPSU AND L EPSU BATTERY INOP. REPLACED EPSU BATTERY SUPPLY AFT LEFT PER AMM 33-51-38. OPS CHECK OK. 2L72 4F RTA28NM 20041202000512004120200051SO 2004 12 2 C2XA04SH546 120041102A531514525480003 FLOORBEAM EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711119 145677 DURING C-CHECK THE CARGO DOOR CUTOUT LOWER FLOORBEAM WAS FOUND TO BE CORRODED. REPLACE THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041202000522004120200052EU 2004 12 2 MALA040609 120041002A5220 WIRE SAAB SF340 340B 7860101EU SAFETY WIRE UNSECURE A MALAK NONE O OTHER NRNOT REPORTED 1 GL15453XJ 340B453 ONE C/D EMERGENCY EXIT SAFE WIRE NOT ATTACHED. MAINTENANCE RESECURED COVER WITH SAFETY WIRE. 2L72 4T RTA52EU 20041202000542004120200054NM 2004 12 2 F3LA200400103 120040928A5320 INTERCOSTAL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL FROM STA 947 - 986 LEFT OF CENTER CORRODED AT FLOOR PANEL NUT PLATES. REPLACED INTERCOSTAL PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375. 2L72 4F RTA16WE 20041202000552004120200055NM 2004 12 2 SWAA043405 120041120A53126546568 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT LBL 6, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041202000582004120200058NM 2004 12 2 2004UALA01118 120041113A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29574UA 26686 R-2 DOOR EMERGENCY LIGHTS INTERIOR AND EXTERIOR INOP. REPLACED BATTERY PACK AND OPS CHECKED REF MM 33-51-00. 2L72 4F4 FRTA2NM E17NE 20041202000592004120200059NM 2004 12 2 UPS04643360 120041018A2560MXP21000 SMOKE GOGGLES BOEING767 76734AF 1385212NM RT JUMPSEAT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01311UP 27741 INSPECTION TYPE:N/A, RIGHT JUMPSEAT SMOKE GOGGLES DAMAGED. REMOVED AND REPLACED RIGHT JUMPSEAT SMOKE GOGGLES. 2L72 4F RTA1NM 20041202000622004120200062SO 2004 12 2 C2XA04SH545 120041103A531514525480003 FLOORBEAM EMB 145 EMB145ER 3260211SO CARGO BAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK BAGGAGE DOOR LOWER BEAM FOUND CORRODED. REPLACED THE LOWER BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041202000652004120200065NM 2004 12 2 CALA0400713 120041109A53306545775 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2769348 23586 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BELOW FASTENER ROW BETWEEN STA 727E AND 747, S24R. A REPAIR DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 229. 2L72 4F RTA16WE 20041202000722004120200072 2004 12 2 SWAA043388 420041119A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29622SW 27932 R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20041202000732004120200073WP 2004 12 2 AALA20041098 120041107A3350 LIGHT DOUG DC9 DC982 3022082WP TAILCONE BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW2170404 49315 DFW - TAIL CONE JETTISON HANDLE EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED TAIL CONE JETTISON HANDLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202000742004120200074EU 2004 12 2 F3LA200400112 120041008A27003945128206 COMPUTER AIRBUSA318 A318111 3940019EU ELAC 2 INOPERATIVE A F3LAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM03804FR 2051 AIR TURNBACK. FLIGHT CREW REPORTED FLIGHT CONTROL RIGHT AILERON FAULT ON ECAM. PERFORMED OVERWEIGHT LANDING AND LANDED IN DEN WITHOUT INCIDENT. CABIN CREW REPORTED HYDRAULIC FLUID COMING FROM LT WING AND AN ELECTRICAL SMOKE ODOR WHEN LANDING GEAR WAS EXTENDED. REPLACED NR 1 ELAC AND CHECKED OKAY. COMPLIED WITH OVERWEIGHT INSPECTION PER ANM 05-51-11-991-016 FIG 602.1. REPLACED LEAKING NR 2 SPOILER SERVO PER AMN 27-64-51-400-004. PERFORMED ENGINE RUN. RAN PACKS OFF ENGINE BLEED. NO SMOKE ODOR NOTED. COULD NOT DUPLICATE REPORTED ODOR. 2L72 4F RT 20041130001032004113000103NM 2004 11 30 AALA20041157 120041122A3397 CONNECTOR DOUG MD80 MD83 3023681NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE O OTHER ININSP/MAINT 1 SW219413T 53188 STL - EMERGENCY PATH LIGHTS AT SEAT 14DEF INOPERATIVE. FOUND CONNECTOR DISCONNECED AT SIDEWALL SEAT 14DEF. RECONNECTED CONNECTOR FOR EMERGENCY PATH LIGHTS AT SEAT 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20041130001062004113000106WP 2004 11 30 MWEA040199 120041016A5210 SKIN DOUG DC9 DC981 3022081WP PAX DOOR DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31813ME 48007 PASSENGER DOOR DENTED AND CRACKED. REPAIRED LOWER FORWARD CORNER DAMAGE WITH REPAIR DOUBLER. 2L72 4F A6WE 20041130001072004113000107NM 2004 11 30 CALA0400725 120041119A53136545767 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND MULTIPLE CRACKS IN STRINGER 16L AND 16R AT STA 540. THE CRACKS WERE 0.025 INCH LONG. CHANNELS WERE INSTALLED IAW ECRA 5310-03418. 2L72 4F RTA16WE 20041130001102004113000110NM 2004 11 30 DLM88041034 120041114A3350 BATTERY PACK DOUG MD88 MD88 3023688NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27988DL 53339 FIVE OVERHEAD EMERGENCY LIGHTS INOP NEAR OVERWING EXIT. REPLACED BATTERIES ON B5-104 BATTERY PWR SUPPLY PACK. 2L72 4F RTA6WE 20041130001202004113000120EA 2004 11 30 SWIA200414076 120041107A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07430SW 7523 AFT MOST CEILING EMERGENCY LIGHT IS INOPERATIVE. RELAMPED AFT MOST CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130001242004113000124EU 2004 11 30 RAIA00411011 120041110A2432407817 BATTERY JETAIRJETSTMJETSTM4101 1500501EU NR 2 FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03564HK12547 41081 STL- NR 2 BATTERY SHOWED OFF LINE AFTER ENGINE STARTED. MAINTENANCE SWAPPED NR 1 AND NR 2 BATTERIES FOR TROUBLESHOOTING. REMOVED AND REPLACED NR 2 BATTERY. 2L72 4T RTA41NM 20041130001282004113000128EA 2004 11 30 COMA0460636 120041121A5610NP1393229 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01912CA3 7011 FLIGHT 5312 THE CAPTAINS SIDE WINDOW SHATTERED INBOUND TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE CAPTAINS SIDE WINDOW. 2L72 4F RTA21EA 20041130001292004113000129EA 2004 11 30 SWIA200414063 120041103A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07937SW 7735 AILERON TRIM WILL NOT RESPOND TO LEFT WING DOWN INPUT. REMOVED AND REPLACED AILERON/RUDDER CONTROL PANEL. OPERATIONAL CHECK GOOD IAW CRJ MM 200 27-12-01. 2L72 4F RTA21EA 20041130001322004113000132NM 2004 11 30 AWXA200401312 120041016A5315BAC1518827 FLOORBEAM BOEING757 757225 1384959NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28915AW 22209 LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 1680 FROM LBL 54 TO RBL 54. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CHORD AT BS 1681 FROM LBL 54 TO RBL 54; FABRICATED A NEW REPLACEMENT UPPER CHORD; INSTALLED REPAIR PART IAW ER 19-5365-00046-JS2A. 2L72 4F RTA2NM 20041130001352004113000135EA 2004 11 30 COMA0470080 120041118A3260533407 SELECTOR VALVE CNDAIRCL600 CL6002C10 1390015EA MLG FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01390CA3940 10106 FLIGHT 5286 DURING TAKEOFF ROLL RECEIVED A GEAR DISAGREE WARNING MESSAGE. AIRCRAFT RETURNED TO THE GATE. REPLACED THE MLG SELECTOR VALVE ASSEMBLY. 2L72 4F RTA21EA 20041130001372004113000137SO 2004 11 30 C2XA04BT118 120041117A2120 ODOR EMB 145 EMB145XR 3260214SO CABIN DETECTED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2711150 145756 DURING CRUISE CREW REPORTED STRONG ODOR IN THE CABIN. AIRCRAFT DIVERTED TO PHL AS PRECAUTION. INSPECTED AIRCRAFT, PERFORMED ENGINE AND APU WITH BLEEDS ON. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041130001382004113000138EU 2004 11 30 RAIA00411014 120041112A3060D45081B TIMER JETAIRJETSTMJETSTM4101 1500501EU PROP HEAT MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03558HK1814516031 41071 PIT - RIGHT PROP HEAT FAIL. MAINTENANCE REMOVED AND REPLACED DE-ICE TIMER. 2L72 4T RTA41NM 20041130001422004113000142EA 2004 11 30 SWIA200414113 120041114A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7701 FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED FORWARD CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD IAW CRJ MM CHAP 33-51-00. 2L72 4F RTA21EA 20041130001612004113000161EU 2004 11 30 MALA040680 120040929A5412 BULKHEAD SAAB SF340 340B 7860101EU RT NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, RT NACELLE INNER WALL CHAFED AT NS 205 O/B SIDE OF NACELLE REPAIRED IAW SAAB SRM 54-10-10. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041130001672004113000167NM 2004 11 30 AALA20041159 120041123A3350P4010051112 MODULE BOEING767 767223 1385123NM EMERGENCY LIGHTSINOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21339AA 22336 JFK - LEFT HAND EMERGENCY LIGHTS AT ROWS 31 TO 37 INOPERATIVE. REPLACED BATTERY PACK AND BATTERY CONTROL MODULE AT ROW 35AB FOR LEFT HAND EMERGENCY LIGHTS AT ROWS 31 TO 37. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041130001782004113000178EU 2004 11 30 2004UALA01125 120041116A3260 WARNING LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE MLG UPLOCK ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29485UA 1617 GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM. AFTER GEAR RETRACTION, RECEIVED A LANDING GEAR SHOCK ABSORBER FAULT ON UPPER ECAM.ACCOMPLISHED A COMPLETE NOSE GEAR STRUT SERVICE. CLEANED GREASE FROM NOSE PROX SENSORS. JACKED NOSE GEAR CLEAR OF GROUND AND GEAR CENTERED NORMALLY. 2L72 4F4 FRTA28NM E40NE 20041130001802004113000180NM 2004 11 30 2004UALA01127 120041116A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE. DAMAGED SKIN WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20041130001832004113000183 2004 11 30 2004UALA01133 420041111A2565 SLIDE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE L-1 DOOR DISLODGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29343UA 24247 DOOR 1L SLIDE HAS SLID DOWN FROM ITS MOUNT. UNIT WAS INSPECTED AND FOUND TO BE OK. SLIDE WAS REINSTALLED. 2L72 4F4 FRTA16WE E2GL 20041130001892004113000189NM 2004 11 30 2004UALA01061 120041115A5320 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 MAIN CABIN FLOOR SUPPORT CORRODED STA 1660 TO 1680 AT RBL 50 TO 55. TYPICAL FLOOR CORROSION. REMOVED DAMAGE AND REPLACED THE FLOOR SUPPORT. 2L72 4F4 FRTA2NM E17NE 20041130001992004113000199NM 2004 11 30 2004UALA01110 120041111A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 CABIN FLOORBEAM STA 1640 HAS CORROSION RBL 44 TO 52, UPPER CAP. CORRODED SECTION REMOVED AND A FLOORBEAM DOUBLER REPAIR WAS INSTALLED. 2L72 4F4 FRTA2NM E17NE 20041130002042004113000204EA 2004 11 30 COMA0460641 120041122A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01973CA 7146 FS 280 CENTER WEB CORRODED. REPAIRED IAW REO 601R-53-11-587. 2L72 4F RTA21EA 20041130002062004113000206EA 2004 11 30 SWIA200414129 120041123A5101 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA UNKNOWN UNKNOWN A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07463SW 7820 JUST AFTER TAKEOFF WITH FLAPS 20 AND TRIMS CENTERED THE AIRCRAFT ROLLS TO THE RIGHT. THIS HAPPENS IMMEDIATELY AFTER WEIGHT OFF WHEELS AND BECOMES LESS PRONOUNCED AFTER FLAP RETRACTION AND/OR INCREASE IN SPEED. SANDED ABRASION RESISTANT TEFLON FILM TO SPECIFIED LIMITS IAW CRJ MM 27-54-01-320-001. 2L72 4F RTA21EA 20041130002102004113000210NM 2004 11 30 MASA200400564 120041004A215078279018 ACM DHAV DHC8 DHC8202 2809007NM CABIN COOLING SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW07989HA7606 427 ON DESCENT AT 21,000 FEET PILOT REPORTED LITE SMOKE AND FUMES IN THE FLIGHT DECK AND CABIN. MAINTENANCE TROUBLESHOOTING. POSSIBLE ACM AND HEAT EXCHANGER REPLACEMENT. AIRCRAFT IS REQUESTED FOR TEST FLIGHT AFTERWARDS. 10/5/04 MAINTENANCE REMOVED AND REPLACED THE DUAL HEAT EXCHANGER AND THE AIR CYCLE MACHINE. HEAT EXCHANGER P/N 778683-2, S/N REMOVED 9802020. 2H72 4T RTA13NM 20041130002122004113000212EA 2004 11 30 SWIA200414089 120041112A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07590SW 7077 AFT MOST EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IN THE LIGHT ASSY, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130002142004113000214EA 2004 11 30 SWIA200414091 120041111A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07918SW 7645 RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EXIT DOOR LIGHT IAW CRJ MM 33-51-21. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041130002162004113000216NM 2004 11 30 AWXA200401275 120041112A3350900542 POWER SUPPLY BOEING737 737277 1384570NM EMERGENCY LIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FOUND THE LT EXTERIOR OVERWING EMERGENCY LIGHT AND LT LOWER AFT WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041130002182004113000218EU 2004 11 30 AWXA200401277 120041102A335032145410 POWER SUPPLY AIRBUS320 A320231 3930325EU ZONE 241 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW130806518 055 SAL - EEL - DURING C-04 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 LT, 17 LT, 19 LT, 24 LT AND 26 LT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041130002472004113000247NM 2004 11 30 AALA20041137 120041116A3350P2010031302 SIGN BOEING757 757223 1384957NM EMERGENCY EXIT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21612AA 24488 BOS - RIGHT 1 ENTRY EMERGENCY EXIT SIGN BROKEN. REPLACED RIGHT 1 EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041130002482004113000248WP 2004 11 30 AALA20041138 120041117A3350 WIRE HARNESS DOUG DC9 DC982 3022082WP CABIN DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21413AA 49324 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. FOUND EMERGENCY LIGHT SEAT HARNESS DAMAGED AT SEATS 9DEF. REPAIRED HARNESS FOR EMERGENCY LIGHT SEATS A 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041201000082004120100008SO 2004 12 1 SWIA200414115 120041117A3620 SENSOR EMB 120 EMB120ER 3260203SO DUCT LEAK MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07580SW 120348 RECEIVED ENGINE DUCT LEAK WARNING DURING FLIGHT. COMPLIED WITH QRH WARNING WOULD NOT EXTINGUISH; FOLLOWED QRH WHICH LED TO PRECAUTIONARY ENGINE SHUTDOWN. REPLACED THE SENSOR OVER THE PRESSURE REGULATOR ON THE LT SYSTEM. OPERATION CHECK GOOD. 2L72 4T RTA31SO 20041201000282004120100028EA 2004 12 1 SWIA200414079 120041030A2752 RECEPTACLE CNDAIRCL600 CL6002B19 1900309EA FLAP DRIVE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 LEFT WING NR 4 FLAP ACTUATOR FLAP DRIVE RECEPTICAL CORRODED. ITEM FOUND AT C-CHECK INSPECTION. LEFT NR 4 FLAP ACTUATOR REPLACED IAW CRJ AMM 27-53-05-000-801/27-53-05-400-801. 2L72 4F RTA21EA 20041201000332004120100033 2004 12 1 2004UALA01130 420041115A2565 SQUIB BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY EXIT WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29669UA 30025 CREW REPORTS BOTH EMERGENCY EXIT SQUIBS WON'T TEST. REPLACED DIODES K839 AND K838, BATTERY PACKS P/N 2013-1, AND CHARGERS P/N 2012-1. 2L72 4F4 FRTA1NM E24NE 20041201000372004120100037NM 2004 12 1 SWAA043429 120041123A53126545409 PRESSURE PANEL BOEING737 7373Y0 1384671NM MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND MAIN LANDING GEAR W/W BEADED PRESS WEB CRACKED AT BS 665, RBL 42. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041201000442004120100044EA 2004 12 1 COMA0460623 120041113A2720 RUDDER CNDAIRCL600 CL6002B19 1900309EA EMPENNAGE FLUCTUATES A COMAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO01783CA 7315 FLIGHT 5853 RUDDER FLUCTUATES LT AND RT DURING CRUISE. C/W YAW OSCILLATION TROUBLESHOOTING, NO DEFECTS FOUND. 2L72 4F RTA21EA 20041201000532004120100053WP 2004 12 1 AALA20041132 120041113A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21407AA 49318 DFW - CABIN CEILING EMERGENCY LIGHTS AT ROWS 7 TO 13 INOPERATIVE. REPLACED BATTERY PACK B5101 FOR CABIN CEILING EMERGENCY LIGHTS AT ROWS 7 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041201000622004120100062EA 2004 12 1 SWIA200414137 120041024A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07909SW 7558 FRAME 621 RIGHT SIDE CARGO BAY IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED -2, -4, -6 REPAIR PARTS IAW REO 601R-53-5542. 2L72 4F RTA21EA 20041201000692004120100069EA 2004 12 1 SWIA200414093 120041103A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB TRIM MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07932SW1867 1867 7714 STAB 1 CHANNEL 1 INOPERATIVE. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041201000802004120100080EU 2004 12 1 MALA040688 120040921A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15428XJ 340B428 DURING CAPACITY INSPECTION IN MSP, BATTERY SUPPLY P/N 3301-501, S/N 1458 REMOVED FOR FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY 3301-31 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 09/29/04. 2L72 4T RTA52EU 20041201000882004120100088 2004 12 1 159593 420041024A3417 AHRS SAAB SF340 SF340A 7850100EU COCKPIT FAILED A UHLAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 GL17123XS 123 ON 10-24-04 APPROX 2000 (UTC), FLT 7891 IAD-ORF. CREW RETURNED TO FIELD WHEN THE F/O'S AHRS FAILED IN FLIGHT. 2L72 4T RTA52EU 20041201000902004120100090EU 2004 12 1 MALA040698 120041013A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHTSFAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15366PX 340B267 DURING CAPACITY INSPECTION IN MSP, BATTERY SUPPLY P/N 61-0478-9, S/N ELB136 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 549-1324-06 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/16/04. 2L72 4T RTA52EU 20041201000932004120100093EA 2004 12 1 SWIA200414061 120041030A5320 SILL CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 CARGO BAY FLOOR SILL FS 574 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SILL IAW REO 601R-53-61-690 REV A. 2L72 4F RTA21EA 20041201001022004120100102EA 2004 12 1 COMA0460613 120041112A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR FALSE INDICATIONA COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01917CA 7017 FLIGHT 5425 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNTIONAL CHECKS OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM WERE NORMAL. 2L72 4F RTA21EA 20041201001092004120100109EA 2004 12 1 SWIA200414095 120041110A2797 WIRE CNDAIRCL600 CL6002B19 1900309EA TRIM SWITCH BROKEN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07932SW 7714 F/O TRIM SWITCH IS INTERMITTENT. RESOLDERED WIRES TO BACK OF SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041201001122004120100112EU 2004 12 1 F3LA200400070 120040719A3246D23355020 SLEEVE AIRBUSA318 A318111 3940019EU NLG WHEEL DAMAGED A F3LAO OTHER E VIBRATION/BUFFET CLCLIMB 1 NM03801FR 3317 1939 FLIGHT CREW REPORTED NOSE WHEEL VIBRATION ON GEAR RETRACTION. FOUND NOSE WHEEL LT BEARING AND SLEEVE DAMAGED. REMOVED SLEEVE AND INSPECTED AXLE FOR DAMAGE. NO DAMAGE NOTED. INSTALLED SERVICEABLE AXLE SLEEVE AT LT POSITION PER AMM 32-41-12-000-002 AND 32-41-12-400-002. REMOVED AND INSTALLED BOTH NOSE WHEEL ASSY'S FOR PRECAUTIONARY PER AMM 32-41-12-401 AND 32-41-12-401. TORQUE AND SPIN CHECK GOOD. NO DEFECTS NOTED. 2L72 4F RT 20041201001142004120100114NM 2004 12 1 F3LA200400106 120040930A5320 SILL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED L2 MOP SILL CORRODED. REPLACED L2 MOP SILL PER SRM 51-10-2 AND 51-40-02. 2L72 4F RTA16WE 20041201001192004120100119EA 2004 12 1 SWIA200414084 120040910A5315 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07908SW 7540 LEFT AND RIGHT ANGLES ON 625 BULKHEAD STRINGER 13L & 13R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLES PER CRJ 200 SRM 51-40-11 PG 1, 53-61-17 PG 2. 2L72 4F RTA21EA 20041201001232004120100123EA 2004 12 1 SWIA200414119 120041120A2750854D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07442SW7812 7812 7609 FLAPS FAIL CAUTION MESSAGE. REPLACED LEFT OUTBOARD FLAP OUTBOARD ACTUATOR IAW 27-53-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041201001452004120100145SO 2004 12 1 SWIA200414097 120041106A2460 RELAY EMB 120 EMB120ER 3260203SO APU FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07295UX 120295 SMOKE COMING FROM F/O'S SIDE PANEL. REPLACED OVERHEATED APU FEEDER PROTECTION RELAY. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041201001502004120100150EU 2004 12 1 AWXA200401260 120041025A5347D5337111120202 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT INBOARD SEAT TRACK BETWEEN FR 42 AND FR 43. MAINTENANCE REMOVED CORRODED LT INBOARD SEAT TRACK FROM FR 42 TO FR 43; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201001642004120100164 2004 12 1 RAIA00411003 420041103A34180861DT5 SENSOR EMB 145 EMB145ER 3260211SO AOA FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03827HK7687 145021 STL- AOA NR 1 INOP MESSAGE. MAINTENANCE REMOVED AND REPLACED AOA SENSOR SYSTEM. 2L72 4F RTT00011AT 20041201001662004120100166EU 2004 12 1 AWXA200401300 120041023A5320D5347209800000 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOORBEAM Y38 LT AT FR 66+6 INCH. MAINTENANCE REMOVED CORRODED FLOORBEAM Y38 LT FROM FR 65 TO FR 67; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201001692004120100169EU 2004 12 1 AWXA200401267 120041025A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 45 AND FR 46. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 45 TO FR 46; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041202000132004120200013EU 2004 12 2 MALA040654 120041006A2560P401004 POWER SUPPLY SAAB SF340 340B 7860101EU FLASHLIGHT INOPERATIVE A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15370PX 340B300 EMERGENCY FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED POWER UNIT IAW MM, ALL CHECKS GOOD. P/N ON & OFF P4-01-004. REMOVED FROM DMR, MAINTENANCE NOTIFIED. 2L72 4T RTA52EU 20041202000252004120200025EU 2004 12 2 AWXA200401326 120041111A5347D5337111200500 SEAT TRACK AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON 6 AREAS OF SEAT TRACK -Y1292 RT BETWEEN FR 43 AND FR 47. MAINTENANCE REMOVED CORRODED SEAT TRACK -Y1292 RT FROM FR 41 TO FR 47; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041202000282004120200028NM 2004 12 2 QXEA200400777 120041117A2731 SPRING DHAV DHC8 DHC8202 2809007NM ELEVATOR OUT OF RIG A QXEAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM09367PH8328 511 SEA - FLIGHT 2019 - ON ROTATION, THE ELEVATOR BACK PRESSURE WAS EXCESSIVELY HEAVY. ALL OTHER CONTROLS WERE NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT RE-RIGGED THE RIGHT ELEVATOR CONTROL SURFACE AND THE LEFT AND RIGHT ELEVATOR SPRING TABS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041202000332004120200033WP 2004 12 2 AALA20041148 120041120A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219405T 53141 DFW - FORWARD OVERWING EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041202000362004120200036WP 2004 12 2 AALA20041133 120041113A335060030451 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21470AA 49600 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 26 INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202000372004120200037EU 2004 12 2 AALA20041142 120041118A3350P4010049 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217055A 462 BOS - FIRST CLASS EMERGENCY LIGHTS ON RIGHT HAND SIDE INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS ON RIGHT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041202000492004120200049EU 2004 12 2 0401863354 120041004A1430STD142010 BOLT AIRBUS330 A330202 3930316EU PWA 4168 PW4168A NE NR 2 ENGINE MISSING A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING KA FLUID LOSS FLAME/FIRE CLCLIMB 1 GL01854NW 00620 733565 DURING CLIMB THE CREW OBSERVED DECREASING OIL QUANTITY AND PRESSURE ON THE NR 2 ENGINE. WHEN OIL PRESSURE DECREASED BELOW 70 PSI THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO NRT. AFTER LANDING HEAVY, A BRAKE FIRE OCCURRED ON THE LEFT MAIN LANDING GEAR. THE GEAR FIRE WAS EXTINGUISHED BY CFR PERSONNEL AND THE AIRCRAFT WAS TOWED TO THE GATE. THE NR 2 ENGINE AND ALL FOUR LEFT MAIN BRAKE AND TIRE ASSEMBLIES WERE REPLACED. 2L72 4F4 FRTA46NM 20041202000502004120200050EU 2004 12 2 MALA040604 120041002A3231 DOOR BAC 146 AVRO146RJ85A1500097EU MLG OUT OF ADJUST A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15504XJ E2311 AT ALTITUTE FL350 THE GEAR UNSAFE (LEFT MAIN) LIGHT CAME ON. THERE WAS NO AIRSPEED CHANGE OR YAW ON APPROACH. GEAR EXTENDED NORMALLY. MAINTENANCE ADJUSTED LT MAIN GEAR DOOR CLEARANCES IAW AMM 32-10-21. COMPLETED MULTIPLE SWINGS, OPS CHECKS GOOD. 2H74 4F RTA49EU 20041202000562004120200056NM 2004 12 2 SWAA043406 120041120A53116546532 FRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BS 482A FRAME CRACKED BETWEEN STR 20L & STR 21L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20041202000572004120200057NM 2004 12 2 SWAA043407 120041120A5311BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BS STR 4R CRACKED AT BS 908. REPAIRED STRINGER ASSY PER SRM. 2L72 4F RTA16WE 20041202000632004120200063 2004 12 2 ABXA040373 420041110A221025866865 COMPUTER DOUG DC9 DC931 3022065WP PITCH DEFECTIVE A ABXAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL23943AX6 47528 AUTOPILOT DID AN UNCOMMANDED 3000 FT MIN DESCENT WITH PITCH WHEEL IN ALTITUDE DETENT. FLIGHT 158, STA ALB. COULD NOT DUPLICATE. SUSPECT PITCH COMPUTER INSTALLED FOR TRIM PROBLEM CAUSING DIFFICULTIES WITH ALT HOLD. REMOVED AND REPLACED PITCH AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 22-10-00-5. 2L72 4F A6WE 20041202000682004120200068WP 2004 12 2 UPS04843454 120041010A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:C3, RIGHT WING CENTER L/E INTERNAL DOUBLER AND L/E SKIN IS CRACKED AT DRAIN HOLE XFS 335.250. REMOVED INTERNAL DOUBLER AND STOP DRILLED 2 CRACKS IAW DC-8 SRM 51-1-21 & 57-2-0 FIG 6. REMOVED, FABRICATED AND INSTALLED EXTERNAL IAW 51-1-20D, 51-1-21, DC8-5720-4087-B, SRM 57-2-0 & 51-1-20D. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DWG 5769589, SRM 51-1-21, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20041202000702004120200070EU 2004 12 2 CX7A194J0445 120040803A26121734362450 DETECTOR SAAB SF340 340B 7860101EU LT TAILPIPE SATURATED A CX7AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL03307CE 340B204 LT TAILPIPE LIGHT CAME ON WHEN SYSTEM WAS POWERED UP. ENGINES WERE NOT RUNNING. PERFORMED ENG RUN UP, LIGHT EXTINGUISHED. 2L72 4T RTA52EU 20041202000752004120200075 2004 12 2 MASA200400330 420040612A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPER FAULTY A MASAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SW07592ML210497288 7410 ABORTED T/O AND RETURNED TO GATE WHEN YAW DAMP 2 W/N STAY ENGAGED. FERRIED TO PHL. MX REPLACED THE NR 2 YAW DAMP ACTUATOR. 2L72 4F RTA21EA 20041202000772004120200077EA 2004 12 2 MASA200400469 120040821A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX OBSTRUCTED A MASAO OTHER C F.O.D. TXTAXI/GRND HDL 1 SW0737178 7178 PAX DOOR HANGS UP ON TOP CAMS. MAINTENANCE FOUND A BOTTLE CAP IN THE DOOR FRAME. REMOVED THE CAP AND PERFORMED THE OPERATIONAL CHECK ON THE DOOR. 2L72 4F RTA21EA 20041202000792004120200079NM 2004 12 2 SWAA043364 120041116A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29505SW 24182 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 932, STRINGER 23L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041202000802004120200080 2004 12 2 MASA200400607 420041028A3416 ALTIMETER EMB 145 EMB145LR 3260212SO COCKPIT FAILED A MASAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07849MJ 145534 AIRCRAFT RETURNED TO THE FIELD DUE TO THE F/O'S ALTIMETER FAILED. MX PERFORMED AN OPS CHECK AND PITOT STATIC CHECK, RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20041202000822004120200082CE 2004 12 2 DXTA200400339 120040713A7830 UNLOCK SWITCH CESSNA500 560CESSNA 2076750CE THRUST REVERSER OUT OF ADJUST E DXTAO OTHER N FALSE WARNING CRCRUISE 1 GL07334QS 5600434 LEFT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED DURING FLIGHT. ADJUSTED LT THRUST REVERSER UNLOCK SWITCHES, RAN ENGINE AND THE LT THRUST REVERSER OPS CHECKED GOOD. ALL WORK PERFORMED IAW CE560 MM 78-30-00. 2L72 4F RTA22CE 20041202000832004120200083EA 2004 12 2 MASA200400539 120040921A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX OUT OF ADJUST A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0777181 7181 UPON ARRIVAL IN CLT FLIGHT CREW COULD NOT OPEN PASSENGER DOOR. MAINTENANCE ADJUSTED PASSENGER DOOR AND PERFORMED OPERATIONAL TEST. NO FURTHER DEFECTS WERE NOTED AT THAT TIME. 2L72 4F RTA21EA 20041202000842004120200084EU 2004 12 2 MALA040678 120040929A3350 BULB SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY LIGHT AT SEAT 10C/D INOP. MAINTENANCE REPLACED BULB IAW SAAB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041202000852004120200085EU 2004 12 2 MALA040676 120040929A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, EMERGENCY POWER SUPPLY AT 21LN INOP. REPLACED IAW SAAB AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041202000872004120200087NM 2004 12 2 SWAA043361 120041116A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 760, STRINGER 19L AND BS 750, STRINGER 18R. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041202000912004120200091SO 2004 12 2 MASA200400608 120041028A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07846MJ 145507 THE EMERGENCY LIGHT ON THE AFT ROOF INOPERATIVE. MX CLEANED CONNECTIONS AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER PROBLEMS. 2L72 4T RTT00011AT 20041202000922004120200092SO 2004 12 2 MASA200400609 120041028A3350 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DIRTY A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 LEFT HAND WING EMERGENCY LIGHT INOPERATIVE. MX CLEANED THE CONNECTORS AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20041202000932004120200093WP 2004 12 2 MWEA040201 120041109A57535936824 PANEL DOUG DC9 DC981 3022081WP RT WING TE FLAP BULGED A MWEAO OTHER O OTHER NRNOT REPORTED 1 GL31803ME 48029 BULGE ON THE TOP SURFACE OF THE RIGHT WING. FABRICATED AND INSTALLED TRAILING EDGE PANEL AND INSTALLED NEW BRACKET AT STATION 118.147. 2L72 4F A6WE 20041202000952004120200095NM 2004 12 2 F3LA200400102 120040928A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM SUPPORT AT STA 947.5 - 967, LBL 14, CORRODED. REPLACED INTERCOSTAL AT STA 947.5 - 967, LBL 14, PER SRM 51-40-02, 51-30-01 AND DRAWING 65C33375. 2L72 4F RTA16WE 20041202000962004120200096EA 2004 12 2 MASA200400597 120041024A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775992 7401 CREW ABORTED TAKEOFF AND RETURNED TO THE GATE FOR SPOILER CONFIGURATION WARNING MESSAGE ON TAKEOFF ROLL. MX RESET SPOILER SYSTEM AND PERFORMED OPERATIONAL CHECKS WITHOUT FURTHER OCCURANCES. 2L72 4F RTA21EA 20041202000972004120200097EU 2004 12 2 MALA040562 120040903A79334053T73P01 DETECTOR SAAB SF340 SF340A 7850100EU ENGINE OIL MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL1527XJ 340A027 LT ENG OIL TEMP INCREASED TO 130 DEG C FOR MORE THAN 15 MIN. OIL PRESSURE STEADY AT 60 PSI. ALTITUDE 14,000 FT CRUISE FLT. AIR RETURN TO MSP. MX PERFORMED PRECAUTIONARY BOROSCOPE FOR INLET DAMAGE OR BLOCKAGE. REMOVED AND REPLACED LT ENG OIL TEMP DETECTOR AND LT ENG OIL PRESS AND TEMP INDICATOR. OIL TEMP OPS CHECK GOOD. REMOVED AND REPLACED LT ENG OIL TEMP DETECTOR AND REMOVED AND REPLACED LT ENG OIL PRESSURE AND TEMP INDICATOR. OPS CHECK GOOD. 2L72 4T RTA52EU 20041202001012004120200101NM 2004 12 2 UPS04443421 120041018A531565B381201 FLOORBEAM BOEING747 747123 1384873NM MAIN CABIN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38092, STA 1840 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.330 IN, AFT HOLE 0.390 IN. REAMED HOLES TO 0.389 AND 0.432. FABRICATED AND INSTALLED FREEZE PLUGS PER EO. REPLACED 65B38120-1 FITTING DUE TO OVERSIZED HOLES. FAB & INSTALLED 69B04576-5 & 69B04576-7 FITTINGS DUE TO EXCESSIVE GOUGES FOUND DURING DISASSMBLY. 2L74 4F A20WE 20041202001032004120200103NM 2004 12 2 UPS04443423 120041018A5315 FLOORBEAM BOEING747 747123 1384873NM MAIN CABIN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38093, STA 1860 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED. FWD HOLE 0.350, AFT HOLE 0.410. REMOVED AFT TRACK ATTACH ANGLE. REAMED BEAM HOLES TO 0.389 & 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH AND SRM 51-10-08. REAMED TRACK ATTACH FITTING O/B HOLES TO 0.341 & 0.400 PER EO. FAB & INSTALLED 1EA 69B04297-1 & 69B04576-7 PER EO C/W SK675-916. 2L74 4F A20WE 20041202001052004120200105NM 2004 12 2 UPS04443425 120041018A5315 FLOORBEAM BOEING747 747123 1384873NM MAIN CABIN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38095 STA 1900, LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED FWD HOLE 0.350, AFT HOLE 0.390. REMOVED AFT ATTACH ANGLE, REAMED BEAM HOLES FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED 2EA FREEZE PLUGS PER SKETCH & SRM 51-10-08. FWD ATTACH FITTING 69B04576-7 GOUGED BEYOND LIMITS. FAB & INSTALLED -7 PER DWG AND SK AFT FTG 69B04576-5. FAB & INSTALLED PER DWG & SK, C/W SAA SK675-619. 2L74 4F A20WE 20041202001062004120200106NM 2004 12 2 UPS04443426 120041019A5315 FLOORBEAM BOEING747 747123 1384873NM MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, SEAT TRACK SUPPORTS HAVE ELONGATED MOUNTS HOLES AT STA 1920, 1940, LBL 98.58. REMOVED 2EA DAMAGED SUPPORT ANGLES. FABBED ANGLE 69B04527 PER DWG STA 1920 ATTACH ANGLE CRACKED. FABBED AND INSTALLED REPAIR PER SRM 51-40-03. NDT VERIFIED DAMAGE REMOVAL. INSTALLED ALL REPAIRED AND/OR REM. PARTS REF SRM 51-10-02, 51-30-02, 51-40-03. 2L74 4F A20WE 20041202001092004120200109WP 2004 12 2 AALA20041140 120041117A3350 LIGHT DOUG DC9 DC982 3022082WP ROW 17 INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21574AA 53151 DFW - EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 17 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202001102004120200110WP 2004 12 2 AALA20041106 120041103A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW217517A 49894 DFW - EMERGENCY LIGHTS AT TAIL CONE SIDE WALL INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS AT TAIL CONE SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202001122004120200112EA 2004 12 2 MASA200400381 120040630A2711 WARNING SYSTEM CNDAIRCL600 CL6002D24 1390016EA AILERON TRIM ACTIVATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07923FJ 15023 ABORTED TAKEOFF DUE TO AN AILERON TRIM CONFIG WARNING. MAINTENANCE WAS ABLE TO RESET THE SYSTEM. 2L72 4F RTA21EA 20041202001132004120200113EA 2004 12 2 MASA200400410 120040717A2711 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA AILERON TRIM ACTIVATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW0777181 7181 CREW REPORTED THE AILERON TRIM AND TAKEOFF CONFIG MESSAGE. MX RESET THE SYSTEM AND OPS CHECK GOOD. 2L72 4F RTA21EA 20041202001162004120200116CE 2004 12 2 DXTA200400411 120041002A2810 VENT CESSNA750 750 2076810CE FUEL CELL MALFUNCTIONED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07907QS 7500201 AT FL280 APPROXIMATELY 25 MINUTES INTO FLIGHT LEFT WING BEGAN VENTING FUEL STARTING AT 2900 LBS IN WING (NO FUEL IN CENTER TANK), VENTING CONTINUED THROUGH DESCENT. OPENED LEFT WING FUEL BAY PANELS 552AB, 542DB, 541DB, 551AB, 511CB, & 511AB. INSPECTED SURGE TANK, VENT FLOAT VALVE, SURGE TANK FLAPPER VALVE AND CLIMB VENT LINE. FOUND LT VENT TUBE ASSY AT WS 54.85 1.0 INCH FROM TOP SKIN, REPOSITIONED VENT TUBE IAW CESSNA MM CHAPTER 28-12-00 AND 28-10-04, REFUELED LT WING. VENT AND LEAK CHECK NORMAL. 2L72 4J RTT00007WI 20041202001172004120200117WP 2004 12 2 UPS04843299 120040912A5310 BEAM DOUG DC8 DC871F 302199DWP PRESS BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD AFT SIDE 3RD J-BEAM UP FROM BOTTOM CRACKED AT BO BOTH UPPER & LOWER EXISTING DOUBLERS AT CENTERLINE WITH UPPER FLANGE HANS SHEARED & LOOSE FASTENERS. NDT VERIFIED CRACK IN BOTH UPPER & LOWER J-BEAM DOUBLERS IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VERIFIED CRACK IN J-BEAM IS TERMINATED AT EXISTING STOPDRILLS. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW EO DC8-5310-6598-C. 2L74 4F RT4A25 20041202001182004120200118WP 2004 12 2 UPS04843300 120040912A5310 BEAM DOUG DC8 DC871F 302199DWP PRESS BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 AFT SIDE OF AFT PRESSURE BULKHEAD 4TH J-BEAM UP FROM BOTTOM HAS LOWER EXISTING DOUBLER CRACKED AT CENTERLINE. NDT VERIFIED CRACK IN LOWER EXISTING DOUBLER IS 2 INCHES IN LENGTH. REMOVED EXISTING REPAIR DOUBLERS. NDT VERIFIED 2 INCH CRACK IN J-BEAM TERMINATES AT FASTENER HOLE AND STOPDRILL. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IAW EO DC8-5310-6598-C. 2L74 4F RT4A25 20041202001202004120200120WP 2004 12 2 UPS04843303 120040911A523037549301N FITTING DOUG DC8 DC871F 302199DWP CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, LOWER CARGO COMPARTMENT C-PIT DOOR (JAMB) FRAME AT APPROX STA 1165 LW LOWER LATCH BACK-UP FITTING HAS SEVER CORROSION ON FITTING & FASTENERS. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 20041202001212004120200121WP 2004 12 2 UPS04843310 120041007A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01705UP 45949 EMERGENCY LIGHTING WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK, GROUND OPS CHECK NORMAL. 2L74 4F RT4A25 20041202001222004120200122WP 2004 12 2 UPS04843311 120041006A33506012235 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01811UP 46089 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD PER REF DC-8 MM CH 33. 2L74 4F RT4A25 20041202001242004120200124SO 2004 12 2 SWIA200414138 120041005A5311 FRAME EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 CRACKED FRAME FOUND AT FRAME 47 RIGHT OUTBOARD SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW SRM 51-70-05 FIG 1. 2L72 4T RTA31SO 20041202001262004120200126EA 2004 12 2 MASA20040063 120040204A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A MASAB EMER. DESCENT O OTHER CRCRUISE 1 SW0717231 7231 CAPTAIN DECLARED AN EMERGENCY FOR CAPTAINS FRONT WINDSHIELD CRACKED. MX IS REPLACING THE WINDSHIELD. 2L72 4F RTA21EA 20041202001272004120200127SO 2004 12 2 SWIA200414140 120041005A5320 PLATE EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FS 13630.0 TO FS 15050.0 RIGHT INBOARD BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041202001282004120200128SO 2004 12 2 SWIA200414141 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 TWO CORNER ANGLE BRACKETS CRACKED AT ST 4121.5 BELOW FLOOR PANELS 221GF AND 222GF. ITEM FOUND AT C-CHECK INSPECTION. BRACKETS REPLACED IAW EMB 120 SRM 53-10-10 FIG 13, ITEM 10, 51-25-00, 51-30-01, 51-40-02, 51-22-00, AND 51-40-05. 2L72 4T RTA31SO 20041202001302004120200130NM 2004 12 2 F3LA200400091 120040820A5312 PRESSURE PANEL BOEING737 7373L9 1384470NM RT MLG WW CRACKED A F3LAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NM03313FL 26442 FLIGHT CREW REPORTED ALTITUDE CABIN CLIMBED AT 150 FPM WITH BOTH PACKS IN AUTO AT CRUISE ALTITUDE. PRESSURIZED AIRCRAFT ON THE GROUND AND FOUND AN 8-INCH CRACK AT TOP OF RT WHEEL WELL, STA 664, RBL 37. REPAIRED PER SRM 53-60-51, FIGURE 203, DETAIL IV AND EA B3-53R-10554. 2L72 4F RTA16WE 20041202001312004120200131NM 2004 12 2 UPS04243402 120041022A3350 BULB BOEING727 72731C 1384011NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01927UP 19232 INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH OFF IND BULB INOP. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH OFF IND BULB IAW 33-1000. 2L73 4F A3WE 20041202001372004120200137NM 2004 12 2 UPS04243196 120040831A5312 BULKHEAD BOEING727 727173C 1384059NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, BULGING CORROSION AND CRACKED SKIN FOUND ON BS 870 BULKHEAD RBL 43 APPROX HALF WAY DOWN ON BULKHEAD. DERIVETED REPAIR STRAP ON BULKHEAD IAW SRM 51-30-02. REPAIR FOUND OUT OF LIMITS. DAMAGED SECTION CUT OUT IAW SRM 53-10-09. HFEC CARRIED OUT ON AFFECTED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, NO DEFECTS FOUND. REPAIR FABRICATED AND INSTALLED IAW SRM 51-30-02. 2L73 4F A3WE 20041202001382004120200138NM 2004 12 2 UPS04243199 120040917A5712 RIB BOEING727 727173C 1384059NM LT WING L/E CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, EXFOLIATION CORROSION FOUND ON FIXED WING L/E RIB LOWER CHORDS AT LES 236.217 AND LES 243.977. REMOVED CHORDS ON ABOVE AREA IAW SRM 51-30-02. FABRICATED AND INSTALLED CHORDS ON ABOVE AREA IAW BOEING DRAWING NR 65-16269. 2L73 4F A3WE 20041202001402004120200140NM 2004 12 2 UPS04243204 120040913A5754 SKIN BOEING727 727173C 1384059NM NR4 KRUEGER FLAPCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, NR 4 KRUEGER FLAP HAS CORROSION ON INNER SURFACE BELOW ACTUATOR ATTACH AREA. CORROSION REMOVED AND FOUND TO BE BEYOND LIMITS IAW SRM 57-50-01. L/ED GE KRUEGER FLAP REMOVED IAW AMM 27-81-01 STEP 2. ACTUATOR ROD END BEARING FOUND TO BE WORN AND CORRODED. ACTUATOR REMOVED IAW AMM 27-81-22 FLAP ACTUATOR REPLACED IAW AMM 27-81-22. KRUEGER FLAP INSTALLED IAW AMM 27-81-01. ADJUSTMENT TEST CARRIED OUT IAW AMM 27-81-01. 2L73 4F A3WE 20041202001412004120200141NM 2004 12 2 UPS04243205 120040910A5754 SKIN BOEING727 727173C 1384059NM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK ON NR 7 SLAT OUTER SKIN AT O/B HOOK. HFEC CARRIED OUT ON SUSPECT CRACK IAW B727 NDTM 51-00-00 PT 6 FIG 4, 3 CRACKS NOTED AND MARKED ON SLAT. CRACKS FOUND TO BE CONTAINED WITHIN RIVET HOLES. 2L73 4F A3WE 20041202001442004120200144NE 2004 12 2 MASA200400572 220041010A72616087T04P05 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE UNSERVICEABLE A MASAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0717156 7156 872459 DIVERTED, AFTER SHUTTING DOWN NR 2 ENG. FLT CREW REPORTED LOW OIL PRESSURE IND. REDUCED THROTTLE TO IDLE & PRESSURE STABLIZED MOMENTARLY. OIL PRESSURE BEGAN TO FLUCTUATE ALONG WITH OIL TEMP. PILOT SHUTDOWN ENG BEFORE PRESSURE DROPPED BELOW 5 PSID. MX EXAMINED ENG & FOUND NO IMMEDIATE SIGNS OF LEAKAGE. OIL CHIP DETECTOR & FILTER PULLED AND EXAMINED FOR BEARING MATERIAL. NO MATERIAL FOUND. MX SERVICED ENG WITH 3 QUARTS OF OIL. ENGINES RAN WITH NO FURTHER DEFECTS NOTED. HOWEVER, WHEN PWR PULLED BACK TO IDLE THE OIL PRESS DROPPED AGAIN. 10/12 MAINTENANCE REMOVED AND REPLACED SCAVENGE PUMP. A/C RETURNED TO SERVICE. 10/12/04 MX REPLACED THE SCAVENGE PUMP. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041202001452004120200145NM 2004 12 2 AALA20041134 120041114A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21753AN 30261 EMERGENCY LIGHTS IN COACH RIGHT HAND SIDE OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENY LIGHTS IN COACH RIGHT HAND SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041202001462004120200146NM 2004 12 2 UPS04443459 120041028A531465B15085886 SUPPORT BOEING747 747200 1384847NM KEELBEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, FX - KEEL BEAM PANEL SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT STA 1480 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 3 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS. PANEL SUPPORT REPLACED AS PER SRM 51-10-01 FIG 8. CIC APPLIED IAW EO NR M-5100-2780-E. 2L74 4F RTA20WE 20041202001472004120200147NM 2004 12 2 UPS04443460 120041028A5315 FLOORBEAM BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE:C, LT BS 340 WL 280-320 UPPER DECK FLOORBEAM ONE EA FASTENER HOLE CRACK REVEALED AT FLOORBEAM UPPER CHORD AND STRAP LAYER. FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 23 PLUS SB 747-53A2459 REV 1 PART 3 MODIFICATION. 2L74 4F RTA20WE 20041202001492004120200149NM 2004 12 2 SWAA043352 120041116A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041202001502004120200150 2004 12 2 SWAA043353 420041116A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041202001522004120200152CE 2004 12 2 DXTA200400415 120041003A3260 WARNING LIGHT CESSNA750 750 2076810CE LANDING GEAR ILLUMINATED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07998QS 7500198 DURING DESCENT, PASSING THROUGH 14000 FT, AT 345 KIAS, AT 3000 FPM, GO TRANSIENT GEAR UNLOCK-FELT NOSE GEAR UNLOCK AND DROP MOMENTARILY BEFORE RE-LOCKING, THE REST OF FLIGHT NORMAL. JACKED AIRCRAFT AND PERFORMED GEAR SWING, CHECKED UPLOCK HOOK AND SWITCH RIGGINGS, CHECKED GOOD IAW CESSNA 750 MM CHAPTER 32-30-05. CHECKED THE BLEED RATE OF LANDING GEAR SYSTEM, SYSTEM OPS CHECKS GOOD IAW CESSNA 750 M/M CHAPTER 32-00-00. 2L72 4J RTT00007WI 20041202001532004120200153EA 2004 12 2 MASA200400563 120041004A2120 ODOR CNDAIRCL600 CL6002C10 1390015EA COCKPIT DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07512MJ 10109 CREW REPORTED A STRONG SMELL IN COCKPIT. MAINTENANCE CURRENTLY TROUBLESHOOTING. 10/4/04 MAINTENANCE PERFORMED OPS CHECKS, RAN THE PACKS AND NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20041202001542004120200154EA 2004 12 2 MASA200400584 120041017A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OVERSERVICED A MASAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SW0777331 7331 THE MAIN CABIN DOOR OUTER HANDLE WOULD NOT STOW. MAINTENANCE FOUND TOO MUCH GREASE ON THE OUTER HANDLE. MAINTENANCE CLEANED AND OPS CHECKS WERE NORMAL. 2L72 4F RTA21EA 20041202001552004120200155 2004 12 2 SWAA043431 420041123A2565D31354 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041202001572004120200157 2004 12 2 SWAA043432 420041123A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK LOOSE. SECURED GIRT BAR STOW HOOK PER MM. 2L72 4F RTA16WE 20041202001612004120200161NM 2004 12 2 QXEA200400759 120041028A5320 FLOOR SUPPORT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FUSELAGE INT FORWARD, X4, LEFT HAND Y11, Z100, FLOOR SUPPORT ANGLE IS CORRODED ON UPPER SURFACE. REPAIRED IAW HORIZON AIR EA 6-53-439 AND RD 8/4-53-1034. 2H72 4T RTA13NM 20041202001622004120200162NM 2004 12 2 QXEA200400760 120041031A5414 COWLING BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - RIGHT HAND ENGINE BOTTOM COWL 422AB INTERNAL WEB UPPER FLOWER ATTACH ANGLES ARE CRACKED. REPAIRED IAW HORIZON AIR EO 6-71-103 AND AMM TASK 71-10-16-400-801. 2H72 4T RTA13NM 20041202001642004120200164NE 2004 12 2 MASA200400476 220040826A7230 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 VIBRATION A MASAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 SW0777302 7302 872479 ABORTED TAKEOFF DUE TO NR 1 ENG N2 VIB. MAINTENANCE WAS ABLE TO DETERMINE THAT THE VIBRATION WAS TRANSIENT AND ALLOWABLE FOR 10 CYCLES PER GE MAINTENANCE MANUAL. 2L72 4F4 FRTA21EA E15NE 20041202001652004120200165EA 2004 12 2 COMA0460598 120041108A3220 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA NLG ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926CA 7027 FLIGHT 5044 GEAR DISAGREE WARNING. NLG UNSAFE. COULD NOT DUPLICATE GEAR SWINGS AND FUNCTION CHECKS OF HYDRAULIC SYSTEM COMPONENTS WERE SATISFACTORY. 2L72 4F RTA21EA 20041202001702004120200170NM 2004 12 2 UPS04243208 120040908A5710 STRUCTURE BOEING727 727173C 1384059NM LOWER LEFT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, LOWER LEFT WING, FIXED WING STRUCTURE WHICH SECURES NR 3 FLAP TRACK FAIRING IS CRACKED ON BOTH I/B AND O/B SIDES. HFEC CARRIED OUT ON SUSPECT CRACKS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONFIRMED ENDS MARKED. DAMAGED AREA REMOVES IAW SRM 51-10-01. REPAIR CARRIED OUT IAW SRM 51-40-03. 2L73 4F A3WE 20041202001722004120200172NM 2004 12 2 UPS04243209 120040909A5313 STRINGER BOEING727 727173C 1384059NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C CORROSION ON LOWER FLANGE OF STR 18A AT BS 850 RT VAPOR SEAL REMOVED FOR ACCESS IAW MM 51-30-00. CORROSION REMOVED ON LOWER FLANGE OF STR 18A IAW SRM 51-10-02. HFEC OF ABOVE AREA CARRIED OUT IAW B727-NDTM 51-00-00 PT6 FIG 4. ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. REPAIR STRAPS FABRICATED IAW DRWG 6 5C27166 AND EO 2004-083-008 (727-53-20165) CAD PLATING CARRIED OUT. 2L73 4F A3WE 20041202001742004120200174NM 2004 12 2 UPS04243211 120040910A5754 SKIN BOEING727 727173C 1384059NM NR3 KRUEGER FLAPCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, SUSPECT CRACK ON ANTI ICE SKIN AT I/B LOWER CORNER OF NR 3 KRUEGER FLAP. SKIN REPLACED IAW DRAWING 65-16225. 2L73 4F A3WE 20041202001772004120200177NM 2004 12 2 UPS04243216 120040910A5710 PLATE BOEING727 727173C 1384059NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, LIGHT SURFACE CORROSION AROUND FASTENER HEAD ON HORIZ FLANGE OF LT WING UPPER SPLICE PLATE AT BS 848. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-021. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4. ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. FASTENER INSTALLED IAW SRM 51-30-02. AREA SEALED IAW MM 28-11-00. 2L73 4F A3WE 20041202001792004120200179NM 2004 12 2 UPS04243220 120040908A5711 SPAR BOEING727 727173C 1384059NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD LEFT WING AT WBL 245. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. CORROSION MARKED ON AIRCRAFT. REPAIR OF AREA CARRIED OUT IAW EO B727-5710-17848 APPENDIX C AND AAAE EO 2004-083-004 (B727-57-20125). 2L73 4F A3WE 20041202001802004120200180EU 2004 12 2 CX7A194J0450 120040824A26131734362450 DETECTOR SAAB SF340 340B 7860101EU TAILPIPE CONTAMINATED A CX7AO OTHER N FALSE WARNING TOTAKEOFF 1 GL03307CE 340B204 TAIL PIPE ILLUMINATED DURING ROTATION. LIGHT SELF EXTINGUISHED AFTER A COUPLE SECONDS. 2L72 4T RTA52EU 20041202001822004120200182NM 2004 12 2 MWEA040184 120041014A523059101413 SKIN DOUG MD88 MD88 3023688NM CARGO DOOR DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FORWARD CARGO DOOR, FORWARD LOWER SKIN HAS A DENT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041202001832004120200183NM 2004 12 2 0401705803 120040923A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01583NW6367 32983 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041202001862004120200186NM 2004 12 2 0401695808 120040923A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01588NW5489 32988 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041202001872004120200187NM 2004 12 2 0401675815 120040923A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01595NW3576 32995 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE WAS WITHIN ALLOWABLE LIMITS. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041202001882004120200188NM 2004 12 2 MWEA040185 120041014A53115911448525 FRAME DOUG MD88 MD88 3023688NM FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 MID CARGO FRAME 598 HAS CORROSION AT LONGERON 30. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041202001912004120200191NM 2004 12 2 QXEA200400749 120041027A5320 SILL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FORWARD FUSELAGE, FORWARD PASSENGER DOOR LOWER DOOR SILL LOWER THRESHOLD MEMBER CORRODED UNDER A/NUT PLATES FSX1.00 TO 32.40 WLZ100.032. REPAIRED IAW RD 8/4-53-1033 HORIZON AIR EA 6-53-444. 2H72 4T RTA13NM 20041202001922004120200192NM 2004 12 2 QXEA200400750 120041101A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FUSELAGE INT FORWARD, X9.0 TO 71, RIGHT HAND Y9.250 INBOARD FORWARD SEAT RAIL IS CORRODED FROM X9.0 TO X71 ON TOP SURFACE AND INSIDE CLAW PORTION. REPAIRED IAW RD 8/4-53-1028 AND HORIZON AIR EA 6-53-438. 2H72 4T RTA13NM 20041201000352004120100035EU 2004 12 1 AWXA200401297 120041025A5320D53112091 FLOOR SUPPORT AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK GALVANIC CORROSION WAS FOUND ON LONGITUDINAL FLOORBEAM -Y765 RT BETWEEN FR 19 AND FR 20. MAINTENANCE REMOVED CORRODED LONGITUDINAL FLOORBEAM -Y765 RT FROM FR 19 TO FR 20; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-14 FIG 104. 2L72 4F RTA28NM 20041201000472004120100047NM 2004 12 1 DLM90041041 120041119A3222 STRUT DOUG MD90 MD9030 3023690NM NLG DISCHARGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27909DA 53389 ON LANDING GEAR RETRACTION THE RED NOSE GEAR LIGHT REMAINED ON. ACCOMPLISHED ABNORMAL CHECKLIST. RECYCLED LANDING GEAR AND NOSE GEAR LIGHT REMAINED ON, BUT WITH THE ADDITION OF LOUD AIR NOISE. LOWERED LANDING GEAR AND RETURNED TO DFW. CHECKED NOSE GEAR. SERVICED NOSE STRUT PER M/M 32-21-01-619-801. JACKED NOSE GEAR CYCLED NOSE GEAR ALL INDICIATIONS NORMAL. 2L72 4F RTA6WE 20041201000582004120100058NM 2004 12 1 SWAA043430 120041123A53306552880 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER FWD CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041201000662004120100066EU 2004 12 1 AWXA200401285 120041106A5320D53475765200 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW 543 MCN - MAJOR REPAIR - DURING C-06 CHECK CORROSION WAS FOUND ON BULK CARGO DOOR SILL WEB BETWEEN FR 60 AND FR 62, STR 38 RT. MAINTENANCE CUT OUT DAMAGE IN BULK CARGO DOOR SILL WEB FROM FR 60 TO FR 62, STR 38 RT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49, FIG 203. 2L72 4F RTA28NM 20041201000722004120100072SO 2004 12 1 MASA200400473 120040825A3350 SWITCH EMB 145 EMB145LR 3260212SO EMERGENCY EXIT MALFUNCTIONED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 A SIDEWALL EMERGENCY EXIT SIGN INOPERATIVE. THE CREW CYCLED THE LIGHT SWITCH AND CLEARED THE FAULT. 2L72 4T RTT00011AT 20041201000812004120100081NE 2004 12 1 DL757041042 220041119A7261 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 LEAKING A DALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27607DL42447 22814 ON T/O OUT OF ATL, F/C ALARM WENT OFF WITH BURNING ODOR OF RUBBER OR PLASTIC. REPLACED NR 1 ENGINE FOR INTERNAL OIL LEAK. 2L72 4F4 FRTA2NM E17NE 20041201001052004120100105EU 2004 12 1 159752 120041108A3260 UPLOCK SAAB SF340 SF340A 7850100EU MLG OUT OF ADJUST A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17123XS 123 AFTER TAKEOFF GEAR HANDLE WAS SELECTED UP AND YELLOW SAFE LIGHT STAYED ON. RECYCLED GEAR THREE TIMES WITHOUT GETTING THE YELLOW LIGHT TO EXTINGUISH. AIRCRAFT RETURNED TO FIELD. GEAR HANDLE YELLOW SAFE LIGHT STAYS ON WHEN GEAR UP. ADJUSTED RT UPLOCK STOP PAD IAW SAAB AMM 32-32-12-2. PERFORMED GEAR SWING IAW SAAB AMM 32-00-00. OPS CHECK GOOD. 2L72 4T RTA52EU 20041201001072004120100107EU 2004 12 1 154571 120041108A2910 SWIVEL SAAB SF340 SF340A 7850100EU DOWNLOCK ACT CRACKED A UHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL1719XS 019 AFTER TAKEOFF MAIN HYDRAULIC`S WENT TO 0, EMERGENCY 2800, PULLED EMERGENCY HANDLE PER QRH. INSPECTED & FOUND DOWNLOCK ACTUATOR SWIVEL TO BE CRACKED. REMOVED AND REPLACED SWIVEL IAW SAAB AMM 32-33-10-2. PERFORMED GEAR SWING, OPS CHECK GOOD IAW SAAB AMM 32-30-00-5. 2L72 4T RTA52EU 20041201001102004120100110SO 2004 12 1 SWIA200414096 120041112A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07226SW 120296 EMERGENCY ROW EXIT LIGHT ROW 9 NOT ILLUMINATED. REPAIRED BROKEN WIRE ON ROW 9 OVERHEAD BIN EMERGENCY EXIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041201001152004120100115EA 2004 12 1 SWIA200414082 120041111A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07459SW 7782 FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11. 2L72 4F RTA21EA 20041201001272004120100127NM 2004 12 1 SWAA043416 120041122A3350 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29429WN 33658 EEPLS INOP AT FWD END. RELAMPED EEPLS PER MM. 2L72 4F RTA16WE 20041201001312004120100131NM 2004 12 1 SWAA043420 120041122A57536546430122 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT MID SPAR AREA. REMOVED FORE FLAP ASSY PER MM. 2L72 4F RTA16WE 20041201001382004120100138EU 2004 12 1 AWXA200401268 120041025A5347D5337111200500 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK FRETTING CORROSION WAS FOUND LT OUTBOARD SEAT TRACK BETWEEN FR 38 AND FR 39. MAINTENANCE REMOVED CORRODED LT OUTBOARD SEAT TRACK FROM FR 38 TO FR 39; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041201001392004120100139EU 2004 12 1 AWXA200401269 120041027A5321D5361012600295 FLOOR PANEL AIRBUS320 A320231 3930325EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 055 SAL - MAJOR REPAIR - DURING C-04 CHECK A 2 X 7 INCH AREA OF DELAMINATION WAS FOUND ON FLOOR PANEL 222CF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 222CF IAW A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20041201001422004120100142NE 2004 12 1 ARWA20041006 220041026A7200 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 HUNG UP A ARWAO OTHER J WARNING INDICATION APAPPROACH 1 SO19661AV483251778 45969 671292 ON APPROACH, NR 4 ENGINE HUNG IN-FLIGHT; PERFORMED EMERGENCY ENGINE HUNG IN FLIGHT CHECKLIST. ENGINE ACCELERATED NORMAL. AFTER LANDING, NR 4 ENGINE SPOOLED DOWN TO 40 PERCENT N2 AND STAYED HUNG. PERFORMED ABNORMAL CHECKLIST TO NO AVAIL. SECURED NR 4 ENGINE. AFTER LANDING GROUND PROXIMITY WARNING SYSTEM FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED NR 4 ENGINE IN ACCORDANCE WITH DC-8 TASK CASD ARROW AIR M/M CARD DC8UN-003 OPERATIONAL CHECK ALL PARAMETERS ARE NORMAL IN ACCORDANCE WITH M/M 71-00. 2L74 4F4 F 4A25 1E8 20041201001562004120100156WP 2004 12 1 MWEA040203 120041112A53125910130394 BULKHEAD DOUG DC9 DC982 3022082WP AFT DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31810ME 48071 AFT PRESSURE BULKHEAD REQUIRES REPLACEMENT DUE TO BLENDING BETWEEN LONGERONS 19 AND 20 RIGHT. FABRICATED AND INSTALLED NEW SECTION. 2L72 4F A6WE 20041201001742004120100174EU 2004 12 1 YENA200457 120041124A3350 POWER SUPPLY AIRBUS320 A320232 3930326EU EMERGENCY LIGHT INOPERATIVE A YENAO OTHER O OTHER LDLANDING 1 EA15565JB 2031 REAR EXIT DOOR LIGHTS LT & RT INOP. RESET AFT LT EPSU, OPS CHECKS GOOD PER 25-60-00. 2L72 4F RTA28NM 20041201001762004120100176EU 2004 12 1 225622 120041123A3230 HANDLE SAAB SF340 SF340A 7850100EU MLG HAND PUMP BROKEN A UHLAB EMER. DESCENT J WARNING INDICATION LDLANDING 1 GL1735SZ 35 SELECTED GEAR DOWN & LT MLG DOWNLOCK LIGHT DID NOT ILLUMINATE. TRIED ACTUATING GEAR WITH EMERGENCY HAND PUMP, & PUMP HANDLE BROKE. PULLED EMERGENCY LANDING GEAR HANDLE & GEAR STILL SHOWED UNSAFE. PERFORMED LOW FLY-BY FOR THE TOWER TO VISUALLY CHECK IF THE GEAR WAS DOWN. AFTER LANDING, INSPECTED AND FOUND LT MLG DOWNLOCK ACTUATOR ATTACHING HARDWARE SHEARED IN HALF. ALSO FOUND HAND PUMP HANDLE INSERTION POINT TO BE BROKEN. 2L72 4T RTA52EU 20041201001812004120100181WP 2004 12 1 AALA20041149 120041120A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217520A 49897 SFO - CEILING EMERGENCY LIGHTS AT ROWS 17 TO 23 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 17 TO 23. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202000172004120200017 2004 12 2 SWAA043272 420041109A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29412WN 29818 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041202000202004120200020 2004 12 2 ARWA20041008 420041027A344220709620101 INDICATOR DOUG DC8 DC863F 302198FWP WX RADAR SYSTEM INOPERATIVE A ARWAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19784AL 46135 LOST WEATHER RADAR IN ROUTE TO GEG. REMOVED AND REPLACED RADAR INDICATOR AND RADAR R/T, OPERATIONS TESTED NORMAL IN ACCORDANCE WITH M/M 34-41-1. 2L74 4F 4A25 20041202000212004120200021 2004 12 2 UPS04143366 420041017A2565 LIMIT SWITCH AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE INTERMITTENT A IPXAK NONE O OTHER ININSP/MAINT 1 SO01156UP 0845 INSPECTION TYPE:N/A EVAC SLIDE WARNING LIGHTS FLASH IN FLIGHT WITH DOOR HANDLE CLOSED. ECAM INDICATIONS NORMAL. REF M289406. FOUND FWD LEFT DOOR ESCAPE SLIDE LIMIT SWITCH (13WN) INTERMITTENT. REMOVED AND REPLACED SWITCH & ADJUSTED PER MM 52-73-13-5, OPS CHECK GOOD. THIS CLEARS M289406. 2L72 4F RTA35EU 20041202000232004120200023EU 2004 12 2 MALA040670 120041101A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, I/B SEAT TRACK AT RBL 18.3 BETWEEN FS 236 & 276 IS CORRODED, OUT OF LIMITS. TRACK WAS REPLACED IAW SRM 51-40-21 AND 51-40-27. A/C WAS RELEASED 11/07/04. 2L72 4T RTA52EU 20041202000262004120200026EU 2004 12 2 AWXA200401327 120041111A5321D5367205000000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO FLOOR PANEL 151PF. MAINTENANCE REMOVED CORRODED AFT CARGO FLOOR PANEL 151PF, FABRICATED A NEW REPLACEMENT FLOOR PANEL; INSTALLED REPAIR PART IAW A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20041202000302004120200030NM 2004 12 2 SWAA043355 120041116A53126546547512 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD LOWER WEB AT BS 727, RBL 1, CRACKED. REPAIRED BULKHEAD WEB PER EA. 2L72 4F A16WE 20041202000442004120200044NM 2004 12 2 DLM88041018 120041107A3397 CONNECTOR DOUG MD88 MD88 3023688NM SEAT ROW 17-18 LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27990DL 53342 ON PREFLIGHT EMERGENCY LIGHTS AT SEAT ROWS 18 TO 23 INOP. RESEATED CONNECTOR BETWEEN SEATS 17 AND 18. NOW OPERATES NORM. 2L72 4F RTA6WE 20041202000472004120200047NM 2004 12 2 2004UALA01144 120041118A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 AFT PIT STA 1420 FRAME DENTED AT STR 25L. DENT CUTOUT AND J ANGLE REPAIR INSTALLED. 2L72 4F4 FRTA2NM E17NE 20041202000532004120200053WP 2004 12 2 UPS04843333 120041009A3350 LAMP DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01706UP 46056 INSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD. 2L74 4F RT4A25 20041202000612004120200061NE 2004 12 2 0401556308 220040916A7200 ENGINE BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 1 FLAMED OUT A NWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL01668US 24223 727973 DURING CLIMB AT 19,000 FT, THE NR 1 ENGINE FLAMED OUT. FLIGHT CREW DUMPED 180,000 LBS OF FUEL AND RETURNED TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONAL CHECK GOOD. 2L74 4F4 FRTA20WE E24NE 20041202000672004120200067SO 2004 12 2 C2XA04SH527 120041020A531114523119401 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK EDDY CURRENT INSPECTION OF MAIN PASSENGER DOORSTOP BOLT HOLE AT FRAME 18 AND STRINGER 14 REVEALED A CRACK. OVERSIZED HOLE REINSPECTED AND NO CRACKS NOTED IAW EC5310-01297. 2L72 4F RTT00011AT 20041202000712004120200071 2004 12 2 SWAA043387 420041119A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20041202000882004120200088NM 2004 12 2 SWAA043362 120041116A335010103113 LIGHT BOEING737 7373T5 1384608NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED C3 CHECK, FOUND RT AFT CABIN LOWER EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041202000892004120200089EU 2004 12 2 MALA040685 120040929A5320 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX DURING 4K INSPECTION IN LAN, BL 0 SEAT TRACK CORRODED FROM STA 291 TO STA 339. MAINTENANCE REPAIRED IAW MESABA EO 53060. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041202000982004120200098SO 2004 12 2 MASA200400605 120041027A3350744424 SIGN EMB 145 EMB145LR 3260212SO PASS ROW 12 LT INOPERATIVE A MASAK NONE O OTHER ININSP/MAINT 1 SW07828MJ 145218 THE AIRCRAFT WAS HAVING OVERNIGHT MAINTENANCE AND WAS SCHEDULED FOR A 2-DAY INSPECTION. DURING THE WALKAROUND IT WAS DISCOVERED THAT ROW 12 LT SIDE LIGHTED EMERGENCY EXIT SIGN WAS INOPERATIVE. MX REPLACED THE SIGN AND PERFORMED OPERATIONAL CHECKS. 2L72 4T RTT00011AT 20041202001082004120200108WP 2004 12 2 AALA20041139 120041117A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21487AA 49680 DFW - CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29 INOPERATIVE. REPLACED TWO BATTERY PACKS FOR CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041202001192004120200119WP 2004 12 2 UPS04843301 120040909A57545769857U613 RIB DOUG DC8 DC871F 302199DWP LT O/B SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 LEFT O/B SLOT UPPER DOOR CLOSE-OUT RIB AT I/B END BROKEN IN LOWER RADIUS. REMOVED AND REPLACED LEFT O/B SLOT CLOSE OUT RIB (PAN) IAW DC-8 SRM 51-1-21. REPAIRED LEFT O/B SLOT O/B END IAW SAA SK772-387. 2L74 4F RT4A25 20041202001232004120200123NM 2004 12 2 UPS04M43309 120040729A5311 WINDOW FRAME DOUG MD11 MD11F 3023600NM ZONE 210 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE: C, COCKPIT CORROSION ON BEARING SURFACE OF SUPPORT FRAME FOR LEFT NR 1 WINDSHIELD. COCKPIT BEARING SURFACE OF SUPPORT FRAME CORROSION REMOVED PER SRM 51-21-01 V.2R.35.V. INSPECTION CUT OUT ON TAE REWORK AREA FOUND CORROSION FREE. NEW FILLER FAB & INSTALLED PER EN1313-04. TASK ACCOMPLISHED OF REMOVING CORROSION AT COCKPIT BEARING SURFACE OF SUPPORT FRAME FOR LT NR 1 WINDSHIELD FOUND SATISFACTORY. 2L73 4F RTA22WE 20041202001252004120200125SO 2004 12 2 SWIA200414139 120041005A5320 SILL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FR 40 TO FR 44 LEFT SIDE SILL CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. INSTALL NEW CARGO DOOR SILL PLATE. 2L72 4T RTA31SO 20041202001582004120200158EA 2004 12 2 SWIA200414106 120041107A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM07973SW 7949 AFTER T/O FROM LAX, FLAPS FAIL CAUTION MSG. FLAPS FAILED AT 6 DEGREES. RETURNED TO LAX. REPLACED FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. P/N 860D100-18ABCD, S/N OFF 1413. 2L72 4F RTA21EA 20041202001592004120200159NM 2004 12 2 SWAA043433 120041123A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 767, STR 19L AND BS 727E, STR 18R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041202001672004120200167NM 2004 12 2 SWAA043263 120041108A53106546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500C, STRINGER 27R, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041202001692004120200169NM 2004 12 2 UPS04243207 120040906A3211 YOKE BOEING727 727173C 1384059NM LT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, ON REMOVAL OF LT MLG SWING LINK, YOKE OVER SWING LINK FOUND TO HAVE PITTING CORROSION. REPLACED YOKE ASSY IAW MM 32-32-00. 2L73 4F A3WE 20041202001732004120200173NM 2004 12 2 UPS04243210 120040910A5754 STRUCTURE BOEING727 727173C 1384059NM NR3 KRUEGER FLAPCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, PITTING CORROSION ON NR 3 KRUEGER FLAP BULLNOSE AT O/B LOWER MOUNT LUG. BULLNOSE REPLACED IAW OHM 57-51-21. 2L73 4F A3WE 20041202001842004120200184NM 2004 12 2 0401715655 120040923A2820316N310012 LINE BOEING757 757251 1384970NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01555NW7840 33391 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 12N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041202001852004120200185NM 2004 12 2 0401685802 120040923A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE FUEL SYSTEM CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01582NW6996 32981 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041202001892004120200189NM 2004 12 2 MWEA040186 120041014A5210591008111 SKIN DOUG MD88 MD88 3023688NM PASSENGER DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 PASSENGER DOOR LOWER, FORWARD CORNER INTERNAL SKIN IS CRACKED AND DEFORMED. FABRICATED AND INSTALLED ANGLE AND DOUBLER. 2L72 4F RTA6WE 20041202001942004120200194NM 2004 12 2 QXEA200400751 120041030A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - MIDDLE CENTER FUSELAGE DENTED AT FSX295.5 Z127.68, BEYOND LIMITS OF THE SRM 53-30-31. REPAIRED IAW HORIZON AIR EA 6-53-446 AND RD 8/4-53-1040. 2H72 4T RTA13NM 20041202001952004120200195NM 2004 12 2 QXEA200400754 120041028A5310 DOOR FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - AFT FUSELAGE RIGHT HAND AFT SERVICE DOOR SURROUND STRUCTURE FSX669.300 TO X697.000 WLZ100.032 EDGE CHANNEL HAS SURFACE CORROSION IN SEVERAL LOCATIONS. REPAIRED IAW HORIZON AIR EA 6-53-441, RD 8/4-53-1031 AND SRM 51-21-10-380-801. 2H72 4T RTA13NM 20041202001962004120200196NM 2004 12 2 UPS04443317 120040929A5711 SPAR BOEING747 747121 1384871NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, LEFT BS 1241 WL 180 UPPER WING REAR SPAR CHORD FOUND CRACK AT HOLE NR 10 RUNNING FORWARD APPROX .0625 INCH. CRACKED HOLE REWORKED AS PER EO 5740-17032. 2L74 4F A20WE 20041202001972004120200197NM 2004 12 2 SWAA043434 120041123A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C1 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 370, STR 26L, BS 377, STR 19R, AND BS 366, STR 15R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041202001992004120200199EA 2004 12 2 QXEA200400762 120041029A5420 INTERCOSTAL CNDAIRCL600 CL6002C10 1390015EA ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 PDX - RIGH HAND NACELLE, RIGHT HAND SIDE, ZONE 423 STATION XN198.00 ABOVE FLAP TRACK, INTERCOSTAL IS CRACKED. REPAIRED IAW SRM 51-42-05-330-001 AND SRM 51-40-15-400-001. 2L72 4F RTA21EA 20041202002012004120200201WP 2004 12 2 UPS04843200 120040927A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. ALL SWITCHES & BREAKERS WERE OFF PRIOR TO TEST. REPLACED BATTERY PACK, OPS CHECK OK. 2L74 4F RT4A25 20041202002022004120200202WP 2004 12 2 UPS04843201 120040924A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01-2. 2L74 4F RT4A25 20041202002102004120200210EU 2004 12 2 069071 120040716A2613 WARNING LIGHT SAAB SF340 340B 7860101EU TAILPIPE HOT ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17140CQ 12681 FLIGHT 7938 FROM BGM TO IAD. ON 7-16-2004 ON TAKEOFF AIRCREW NOTICED LT ENGINE TAILPIPE HOT LIGHT ILLUMINATING. AIRCREW RETURNED TO FIELD. 2L72 4T RTA52EU 20041202002132004120200213NE 2004 12 2 NACA20040048 220041023A8530356993 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 16 FAILED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA1514 1514 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING WHEN LEAN AND RUNNING ROUGH. NR 16 CYLINDER SHOWS LOW COMPRESSION. REPLACED NR 16 CYLINDER. OPS CHECKED GOOD. 2L74 4R4 R A781 5E8 20041202002142004120200214NM 2004 12 2 FE5F200400002 120040827A26131296825 SENSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE OVERTEMP FALSE ACTIVATIONW FE5FB EMER. DESCENT N FALSE WARNING CRCRUISE 1 WP03 39527 25044 P728717 A/C B27001 DURING CRUISE ON FL370(LOCAL TIME 19:45),"LEFT ENG BLEED OFF", "L PACK"AND L ENG ANTI ICE OFF" LIGHT ON, THEN CAPTAIN FOLLOW THE "QRH" ASKED DECEND TO FL330. ON DECENDING, "RIGHT ENG BLEED" AND "R PACK OFF" LIGHT ON, CAPTAIN ASKED DECEND TO FL290 AGAIN, AT THIS TIME "CABIN ALT INOP" LIGHT ON, THEN CAPTAIN PERFORM THE PROCEDURE OF "CABIN AUTOMATIC INOP" AND ASKED DESCEND TO FL210.ON LOCAL TIME 19:50, CABIN CHIEF REPORTED THAT PAX OXYGEN MASKS ARE DROPPED, THEN CAPTAIN ASKED DESCEND TO FL100. THE AIRPLANE ARE SAFELY LANDING ON KHH AT 20:30 LOCAL TIME. GROUND TEST FOR A/C B27001 AFTER LANDING: ENGINE IDLE: 1). NR 1 AND NR 2 ENGINE "BLEED AIR" NORMAL, (ENGINE BLEED VALVE LIGHT OFF) 2L72 4F4 FRTA2NM E17NE 20041203000022004120300002EU 2004 12 3 2004UALA01150 120041122A2121EVT3454H FAN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE E/E BAY DAMAGED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29454UA 1104 LAND ASAP ECAM DISPLAYED. FOUND FOD IN AVIONICS EXTRACT FAN (18HQ). REPLACED SAME. 2L72 4F4 FRTA28NM E40NE 20041203000052004120300005NM 2004 12 3 UPS04543536 120041119A5610141T480013 WINDSHIELD BOEING757 75724APF 1384969NM COCKPIT CRACKED A IPXAO OTHER O OTHER CRCRUISE 1 SO01415UP 23855 L1 FWD WINDSHIELD CRACKED OUTER PANE DURING CRUISE. REMOVED AND REPLACED LT FWD WINDSHIELD ASSY IAW AMM 56-11-01-4. ALL ACCOMPLISHED WITH NEW FASTENER KIT PH 654T0013-12 S/N TAG00724944. 2L72 4F RTA2NM 20041203000082004120300008NM 2004 12 3 04FDEA03221 120041125A5712 RIB DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING RIB 16 INBOARD FOUND CRACKED. REMOVED AND INSTALLED AS PER SRM 51-33-01 VOL II. REFER TO WORKCARD 27X8403 FOR CABLES ADJUSTMENT. 2L73 4F RTA22WE 20041203000092004120300009EU 2004 12 3 04FDEA03230 120041126A5313 STRINGER AIRBUS310 A310 EU FUSLEAGE DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25401FE 191 TWO HOLES HAVE DAMAGE, 1 GOUGED AND 1 MISDRILLED ON BACK SIDE, FS 54 LT SIDE STRINGERS 35 AND 37 AS MARKED. COMPLIED WITH EA 6-5310-84341. 2L72 4F RTA35EU 20041203000102004120300010NM 2004 12 3 USAA040756 120041015A5310 BEAM BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU PRESS BULKHEAD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19445US 24863 PIT, FPBH, VERTICAL CHORD, .750 INCH LONG, IB RADIUS OF VERTICAL CHORD LBL 5.7, WL 184. REPAIRED VERTICAL BEAM WITH REPAIR KIT IAW EO 5300V155 WITH EA 79303. 2L72 4F4 FRTA16WE E21EU 20041203000112004120300011WP 2004 12 3 ASAA0480525 120040928A5730593746815 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, LT WING L/E UPPER SURFACE CHAFED 25 INCHES OB OF L/E SLAT NR 0, OB TRACK REMOVED DAMAGE. HFEC, NO CRACKS NOTED, TREATED AND PRIMED IAW EA 5740-01411 AND EA 10592. 2L72 4F4 FRTA6WE E9NE 20041203000132004120300013SW 2004 12 3 24KM1 120041130A812037291001501 BRACKET GULSTM500 500B 0141106SW LYC O540 IO540E1A5 41532EA HARTZLHCC3Y HCC3YR GL TURBOCHARGER CRACKED E H3AAK NONE O OTHER ININSP/MAINT 1 SO3324KM 303 500B1296111 L18148 CK587 A CRACK APPROXIMATELY 2.5 INCHES LONG WAS NOTICED IN THE UPPER PORTION OF THE TURBO CHARGER ATTACH BRACKET. UPON REMOVAL OF FROM THE ENGINE MOUNT NUMEROUS CRACKS WERE NOTED RUNNING ALONG WELDS AND THROUGHOUT THE ENTIRE ASSEMBLY. SUBSEQUENT REMOVAL OF THE TURBO MOUNTING ASSEMBLY ON THE RIGHT ENGINE REVEALED CRACKS IN MANY OF THE SAME AREAS. THE CRACKS ARE DIFFICULT TO DETECT UNLESS THE ASSEMBLY IS REMOVED FROM THE ENGINE MOUNT. BOTH UNITS HAVE 303.5 HOURS SINCE NEW. PICTURES OF THESE UNITS ARE AVAILABLE AT YOUR REQUEST. 1H72 3O3 O 6A1 1E4 5 CP25EA 20041203000142004120300014WP 2004 12 3 UPS04843546 120041118A5712 RIB DOUG DC8 DC871 302199AWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 C3 RT WING CENTER L/E RIB CRACKED AT AFT END, STA XFS347. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6 .040 AND .032 AND INSTALLED SAME REF SRM 57-3-1, 57-2-0, 51-1-8, 2L74 4F 4A25 20041203000172004120300017NM 2004 12 3 SCNA04017 120041124A3350 BATTERY PACK BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT MALFUNCTIONED A SCNAO OTHER L NO TEST NRNOT REPORTED 1 GL15806SY 28215 CREW REPORTED AFT RIGHT OVERWING AND MID SECTION OVERHEAD BIN EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OK FOR SERVICE. 2L72 4F RTA16WE 20041203000202004120300020NM 2004 12 3 AWXA200401347 120041103A5320655287855 ANGLE BOEING737 7373Y0 1384671NM CREASE BEAM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-15 CHECK, CORROSION WAS FOUND ON ATTACH ANGLE AT BOTTOM OF L-2 CREASE BEAM INNER CHORD BETWEEN BS 969 AND BS 979, LBL 49. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ATTACH ANGLE BS 969 - 979, LBL 49; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12. 2L72 4F RTA16WE 20041203000212004120300021WP 2004 12 3 ASAA0480521 120040928A53113936607535 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK, AFT CARGO COMPARTMENT FRAME STA 1098 HAS CORROSION ON FORWARD SIDE AND TOP SIDE JUST ABOVE LONGERON 30. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, SPACER AND FILLER IAW SRM. 2L72 4F4 FRTA6WE E9NE 20041203000222004120300022NM 2004 12 3 ASAA0410473 120041104A53206567140148 FLOOR SUPPORT BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LONGITUDINAL BEAM HAS CORROSION. REMOVED DAMAGE, COMPLIED WITH HFEC, NO DEFECTS NOTED FLAP PEENED, TREATED, PRIMED, AND TOP-COATED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041203000232004120300023NM 2004 12 3 ASAA0410490 120041105A533065458001140 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LIGHTNING STRIKE DAMAGE OUT OF LIMITS ON SKIN IAW SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041203000252004120300025NM 2004 12 3 L0FR200400008 120041118A324626070812 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000302004120300030NM 2004 12 3 L0FR200400003 120041118A324626070812 WHEEL BOEING747 747200 1384847NM ZONE 700 CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000322004120300032NM 2004 12 3 L0FR200400002 120041118A324626070812 WHEEL BOEING747 747200 1384847NM ZONE 700 CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000332004120300033NM 2004 12 3 L0FR200400007 120041118A3246260356116 WHEEL BOEING747 747200 1384847NM ZONE 700 CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000342004120300034NM 2004 12 3 L0FR200400010 120041118A3246260356112 WHEEL BOEING747 747200 1384847NM ZONE 700 CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000352004120300035NM 2004 12 3 L0FR200400011 120041118A3246260356116 WHEEL BOEING747 747200 1384847NM ZONE 700 CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 FAILED BOLT HOLES ON OUTER RIM IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 EDDY CURRENT PROCEDURES. 2L74 4F RTA20WE 20041203000372004120300037WP 2004 12 3 ASAA0480483 120040825A33501001191 LIGHT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FWD ENTRY WAY INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02974AS3443 3443 53450 PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2L72 4F4 FRTA6WE E9NE 20041203000392004120300039NM 2004 12 3 2004UALA01151 120041123A2497 WIRE HARNESS BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN SPARKS A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29645UA 25280 WIRE BUNDLES UNDERNEATH PIT FLOOR FROM PDY 6R AREA TO PDU 6L AREA SPARKING AND POPPING CB'S. REPAIRED BY SPLICING IN NEW WIRING PER BOEING STANDARD PRACTICES. 2L72 4F4 FRTA1NM E24NE 20041203000402004120300040NM 2004 12 3 XNOA1213 120041124A2612 WARNING LIGHT BOEING727 727200 138407ENM CARGO FIRE FALSE ACTIVATIONA XN0AA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL2379754 21363 LOWER FORWARD CARGO FIRE LIGHT AND BELL ILLUMINATED IN FLIGHT DIVERTED TO BNA. PERFORMED OPS CHECK ON CDU, INDICATED FALSE ALARM S/N M13198. VISUALLY CHECKED LOWER BELLY. TRANSFER TO DMI 4771. MEL 26-19-1 CAT B. SWAPPED SENSOR FROM P-3 TO FWD CARGO FOR TROUBLE SHOOTING, R/R SMOKE DETECTOR IN FWD PIT, REPROGRAMMED CDU, OPS CK GOOD IAW B727 MM 26-17-00. THIS ACTION CLEARS DMI 4771. PLACARDS REMOVED. (STATUS:SUPP/CLOSED) 2L73 4F RTA3WE 20041203000412004120300041 2004 12 3 ASAA0480482 420040813A25653961896501 LANYARD AIRCRUISERS DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EMERGENCY SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 0928 53449 FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2L72 4F4 FRTA6WE E9NE 20041203000422004120300042 2004 12 3 ASAA0480487 420040903A25653961896501 LANYARD AIRCRUISERS DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02949AS 1878 53022 FORWARD PAX (L-1) DOOR EMERGENCY SLIDE RELEASE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2L72 4F4 FRTA6WE E9NE 20041203000452004120300045WP 2004 12 3 200411007 120041115A8012 START VALVE DOUG DC9 DC982 3022082WP ENGINE INOPERATIVE W ASMFK NONE O OTHER ININSP/MAINT 1 SW23501AM 49188 AIRCRAFT RETURNED TO PLATFORM DUE TO STARTER VALVE WAS NOT OPEN. SYSTEM WAS CHECKED AND LINE WAS FOUND BROKEN. LINE WAS REPLACED IAW MM 80-10-00, TEST CORRECT. 2L72 4F A6WE 20041203000462004120300046NM 2004 12 3 ASAA0410491 120041105A528065B281765 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE LT MLG DOOR DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LT MAIN LANDING GEAR, UPPER STRUT DOOR FWD AND AFT HINGE AREA DISBONDING. REMOVED DAMAGE, COMPLIED WITH COMPOSITE REPAIR IAW EA. 2L72 4F4 FRTA16WE E2EA 20041203000472004120300047 2004 12 3 ASAA0480269 420040407A2565 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ESCAPE SLIDE MISRIGGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02965AS26888105 53079 OKC C-CHECK, AFT SERVICE DOOR EMERGENCY SLIDE FAILED TO DEPLOY DURING DEPLOYMENT TEST. SUSPECT MIS-RIGGED LANYARD, BUT INVESTIGATION IS UNDERWAY TO MORE DEFINITIVELY DETERMINE CAUSE. MFG (ENG-G DOC 3053)- MIS-RIGGING APPEARS TO HAVE BEEN IMPROPER FOLDING OF THE HOSE ASSY CONNECTING THE ASPIRATOR TO THE INFLATION RESERVOIR. BUT, ACCORDING TO MFG, THIS KINKING OF THE HOSE WOULD NOT HAVE CAUSED THE FAILURE. ALTHOUGH NO FOREIGN MATERIAL WAS FOUND LODGED INSIDE THE ASPIRATOR, TEMPORARY INGESTION OF BUBBLE WRAP BY THE ASPIRATOR IS CONSIDERED THE MOST PROBABLE CAUSE OF FAILURE. THERE WAS SUBSTANTIAL AMOUNT OF THIS MATERIAL TAPED TO THE FUSELAGE NEAR THE ASPIRATOR. ENTIRE SLIDE WAS REPLACED. 2L72 4F4 FRTA6WE E9NE 20041203000492004120300049NM 2004 12 3 SPAA0400073 120041109A573065C171911 SKIN BOEING737 7372Y5 1384554NM LT WING CORRODED A SPAAK NONE O OTHER ININSP/MAINT 1 WP28712S 23038 CORROSION DAMAGE WAS FOUND ON THE LT UPPER WING SKIN P/N 65C17191-1 AT THE REAR SPAR AT APPROXIMATELY WS 442.0. THE CORROSION WAS REMOVED AND TRIMMED AND A REPAIR SCHEME WAS PROVIDED BY BOEING ENGINEERING. THE CORROSION AREA WAS REPAIRED PER BOEING INSTRUCTIONS AND A 8110-3 STRUCTURAL SUBSTANTIATION FOR WAS ISSUED. 2L72 4U RTA16WE 20041203000502004120300050NM 2004 12 3 HNAA0400168 120041130A533085320106155 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 DURING C CHECK, CORROSION WAS FOUND ON SKIN PANEL 85320106-155. TRIMMED OUT DAMAGED SKIN AND HFEC , BOND CHECK SKIN. FABRICATED PACKER AND REPAIR DOUBLER, INSTALLED REPAIR PARTS. 2H72 4T RTA13NM 20041203000522004120300052 2004 12 3 RAIR00411024 420041123A34257003110901 DISPLAY JETAIRJETSTMJETSTM4101 1500501EU EHSI MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03568HK165617435 41086 ERRONEOUS EHSI DISPLAY ON CO-PILOT SIDE AND CAPTAIN SIDE EHSI HAS NO DISPLAY. MAINTENANCE REMOVED AND REPLACED CAPTAIN EHSI DISPLAY. BOTH SIDES OPS CHECK GOOD. 2L72 4T RTA41NM 20041203000532004120300053CE 2004 12 3 2004F00430 120041115A81204066109025 TURBINE WHEEL CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO TURBOCHARGER EXCESS PLAY E EA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL27402SS 402B0562 826303R SHORTLY AFTER DEPARTURE FROM SIOUX, THE PILOT NOTICED THE LEFT ENGINE MANIFOLD PRESSURE DROPPING OFF AND THE ENGINE LOSING POWER. ALL OTHER ENGINE INDICATORS SHOWED NORMAL BUT, AS A PRECAUTION, THE LEFT ENGINE WAS SHUT DOWN AND SECURED. THE PILOT RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION BY MAINTENANCE PERSONNEL, IT APPEARED AS THOUGH THE TURBINE WHEEL OF THE TURBO CHARGER HAD RUBBED AGAINST THE HOUSING. THIS WAS A NEWLY INSTALLED TURBO CHARGER WITH ZERO HOURS ON IT. 1L72 3O3 O A7CE E8CE 20041203000552004120300055NM 2004 12 3 UPS04243508 120041118A3350 LIGHT BOEING727 72725C 138400HNM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01946UP 19721 COCKPIT EMERGENCY LIGHT WILL NOT CK ON PREFLT. RESET RELAY R-70 CKS OK. 2L73 4F A3WE 20041203000572004120300057NM 2004 12 3 UPS04443504 120041029A5712 RIB BOEING747 747200 1384847NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 L/E PNL SUPPORT RIB FOUND CRACKED AT WS 1420 JUST O/B OF NR 1 L/E FLAP PDU. L/E PNL SUPPORT RIB REPAIRED AS PER HX RS NR R57-41-35209 JUST AT WS 1420 O/B OF NR 1 L/E FLAP PDU. REFER UPS EO NR B747-5740-21328-A 2L74 4F RTA20WE 20041203000602004120300060NM 2004 12 3 NACA20040060 120041113A32607500355 ANNUNCIATOR BOEING727 72723 1384004NM MLG FAULTY A NACAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 AL03992AJ 19428 NOSE LANDING GEAR DID NOT RETRACT. MAIN LANDING GEAR ONLY PARTIAL RETRACTION. FOUND INDICATION TO BE FAULTY AND REPLACED GEAR POSITION ANNUNCIATOR PANEL. PERFORMED RETRACTION TEST WITH NO DISCREPANCIES IAW BMM 32-31-2. 2L73 4F A3WE 20041203000622004120300062WP 2004 12 3 IXXA04000121O 120041116A3210 LANDING GEAR DOUG DC8 DC871F 302199DWP MALFUNCTIONED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11821BX857662863 45811 AFTER TAKEOFF FROM KHRL TO KTOL, LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. UPLOCK CHECK UNSATISFACTORY, NOSE GEAR FALLS FREE. CREW LANDED IN KTOL WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2L74 4F RT4A25 20041203000632004120300063NM 2004 12 3 04FDEA03143 120041117A5347ACA7104511 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 MAIN DECK SEAT TRACK AT STA Y= 635, X= -8 FOUND WITH APPROXIMATELY FOUR (4) INCHES CRACKED AFTER FORWARD CARGO CEILING PANEL OPEN UP. MAIN DECK SEAT TRACK AT STA Y= 625 TO Y= 655, X= -8 CUT AND REMOVED PER SRM 51-31-01 VOLUME II. NEW SEAT TRACK FABRICATED AND INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1 AND SRM 51-31-01 VOLUME II. 2L73 4F RTA22WE 20041203000662004120300066NM 2004 12 3 04FDEA03146 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 20L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000682004120300068NM 2004 12 3 04FDEA03148 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 32L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000702004120300070CE 2004 12 3 GLBA20030758 120041111A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03118GL UE118 FOUR CRACKS EXTENDING FROM DEICE LINE HOLE IN HORIZ STABILIZER MAIN SPAR WEB. REPAIRED HORIZONTAL MAIN SPAR WEB IAW GLA EO 04-21 AND B1900SRM 55-91-02 2L72 4T RTA24CE 20041203000712004120300071NM 2004 12 3 04FDEA03149 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 1R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000722004120300072NM 2004 12 3 04FDEA03153 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 7R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000752004120300075NM 2004 12 3 L0FR200400005 120041118A324626070812 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000762004120300076WP 2004 12 3 0402039866 120041118A57545919526508 DUCT DOUG DC9 DC951 3022051WP RT WING SLAT LACK OF LUBE A NWAAF ACTIVATE FIRE EXT. KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01775NC 47785 WHEN SLATS WERE SELECTED TO EXTEND, THE AIRCRAFT ROLLED TO THE LEFT AND THE 'SLAT DISAGREE' LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURES AND THE SECOND ATTEMPT HAD THE SAME RESULTS. THE SLAT DISAGREE LIGHT DID NOT EXTINGUISH. FLIGHT LANDED UNEVENTFULLY AT GRR WITH THE SLATS RETRACTED. MAINTENANCE LUBRICATED THE RIGHT 'T' DUCT, EXERCISED THE SLAT EXTENSION SYSTEM, AND ALL CHECKED NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041203000782004120300078SO 2004 12 3 CHQA000581 120041106A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11283 145424 LT AND RT OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY ASSEMBLY. OPS CHECK GOOD PER EMB 145 MM 33-50-04-4. 2L72 4T RTT00011AT 20041203000792004120300079SO 2004 12 3 CHQA000582 120041108A3397 CONNECTOR EMB 145 EMB145LR 3260212SO WIRE HARNESS MISINSTALLED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260 145128 FORWARD OVERHEAD EXIT LOCATOR IS INOP. FOUND GALLEY LIGHT WIRING HARNESS CONNECTOR NOT CONNECTED PROPERLY. RESECURED EMERGENCY LIGHT WIRING HARNESS CONNECTOR IAW EMB 145 AMM 33-50-15. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041203000802004120300080SO 2004 12 3 CHQA000583 120041108A3397 CONNECTOR EMB 145 EMB145LR 3260212SO BATTERY HARNESS UNSECURE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265 145226 MULTIPLE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOP IN DCA. THE AIRCRAFT WAS FERRIED TO SDF FOR REPAIRS. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY AND RESECURED THE CONNECTOR ON THE NR 1 EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD PER EMB 145 AMM 33-50-00. 2L72 4T RTT00011AT 20041203000812004120300081WP 2004 12 3 0402049877 120041120A2730 SWITCH DOUG DC9 DC951 3022051WP ELEVATOR FAILED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL01786NC 48148 THE CREW REPORTED, THE AIRCRAFT FEELING VERY HEAVY ON THE CONTROLS THAT IT TOOK EXCESSIVE BACK PRESSURE TO CONTINUE TO CLIMB AFTER TAKEOFF. THE 'ELEVATOR POWER ON' LIGHT ILLUMINATED AT THE SAME TIME AND REMAINED ILLUMINATED UNTIL 10,000 FT. COMPLIED WITH COM PROCEDURES AND THE CREW RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT ATL. MAINTENANCE FOUND THE ELEVATOR POWER SWITCH BAD AND REPLACED IT. ALSO, CHECKED THE ELEVATOR, TAB, BOOST ACTUATOR SYSTEM, FOLLOW-UP MECHANISM, AND THE LOAD FEEL SPRING. ALL COMPONENTS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041203000822004120300082GL 2004 12 3 0402061223 220041123A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL NR 2 FIRE A NWAAE ENGINE SHUTDOWN A FLAME/FIRE TXTAXI/GRND HDL 1 GL01223NW 46580 528244 DURING NR 2 ENGINE START, GROUND CREW REPORTED A TAILPIPE FIRE. CFR WAS CALLED OUT AND SPRAYED FIRE EXTINGUISHING AGENT INTO THE TAILPIPE OF THE NR 2 ENGINE. THE ENGINE WILL BE REMOVED. 2L73 4F4 F A22WE A23EA 20041203000832004120300083NM 2004 12 3 0402053149 120041122A2121EVT3454H FAN AIRBUSA319 A319114 3930350NM E/E BAY SEIZED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01349NB6212 01815 DURING CRUISE, SMELLED ELECTRICAL FUMES, SMOKE, AND FELT VIBRATION. DIVERTED TO CMH AND LANDED UNEVENTFULLY. FOUND AVIONICS BLOWER FAN SEIZED. SWAPPED WITH EXTRACT FAN AND APPLIED MEL PROVISIONS FOR EXTRACT FAN. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20041203000842004120300084NM 2004 12 3 04FDEA03163 120041118A574465192596 ATTACH FITTING BOEING727 727100 1384036NM LT WING AILERON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 LT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING. 2L73 4F RTA3WE 20041203000852004120300085CE 2004 12 3 T2BA2 120041018A3297727022 CIRCUIT BREAKER BEECH 1900 1900C 1154161CE MLG TRIPPED E T2BAL ABORTED APPROACH S AFFECT SYSTEMS DEDESCENT 1 SO15172TE UB24 ON FINAL APPROACH TO ZQA, BAHAMAS, SELECTED GEAR DOWN, LANDING GEAR RELAY CIRCUIT BREAKER (2AMP) POPPED, SELECTED GEAR UP AND EXECUTED A MISS APPROACH AND WAITED 5 MINUTES TO RE-SET CIRCUIT BREAKER, UPON RE-SETTING C/B, NOTICE THE HYDRAULIC LOW ANNUNCIATOR ILLUMINATED FOR 3 SECONDS THEN EXTINGUISHED, SELECTED GEAR DOWN AND GOT THREE GREEN LIGHTS. UPON LANDING AT ZQA, MAINTENANCE PERSONNEL JACKED THE AIRCRAFT AND PERFORMED 6 GEAR SWINGS IN THE NORMAL MODE AND MANUAL EXTENSION, NO DEFECTS NOTED, WRITE UP WAS SIGNED OFF AND AIRWORTHINESS RELEASED ALSO SIGNED, AIRCRAFT DEPARTED ZQA TO DED AND LANDED WITH NO PROBLEMS. 2L72 4T RTA24CE 20041203000892004120300089NE 2004 12 3 NACA20040043 220041004A8500R2800 ENGINE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 3 OVERSPEED A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 AL034387214 14 533294 P54311 NR 3 ENGINE SHUT DOWN DUE TO OVERSPEED AND LOSS OF OIL. FOUND NR 3 ENGINE SEIZED AND OIL OVERBOARD. REPLACED NR 3 ENGINE. CHECKED GOOD. 2L74 4R4 R A781 5E8 20041203000912004120300091NE 2004 12 3 PNSA041001 220041004A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 MALFUNCTIONED A PNSALA ABORTED APPROACH UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 AL03665PA 340B181 ON A FLIGHT FROM ANC TO DUT, AT THE START OF THE DESCENT INTO DUT PILOT REDUCED POWER TO 60 PERCENT, AT WHICH TIME THEY HEARD A LOUD BOOM AND THE AIRCRAFT YAWED TO THE RIGHT. PILOTS NOTICED NR 2 ENGINE AT 20 PERCENT TORQUE AND TEMP RISING RAPIDLY, AFTER APPROX 3 SECONDS THE ENGINE RECOVERED AND BEGAN TO OPERATE NORMALLY. FLIGHT CREW ELECTED TO ABORT DESCENT AND DIVERTED TO CDB, ENGINE CONTINUED TO RUN PROPERLY. NO IMMEDIATE CAUSE WAS KNOWN FOR THE MALFUNCTION. 2L72 4T4 TRTA52EU E8NE 20041203000922004120300092WP 2004 12 3 LMAC 120040830A32331535927111 ACTUATOR LKHEED1011 10113853 5265020WP ZONE 700 CRACKED F ZJ4RL ABORTED APPROACH G MULTIPLE FAILURE DEDESCENT 1 SO13CS-TM 2046 1206 ON APPROACH LOUD NOISE HEARD THROUGHOUT A/C. L/G EXTENSION ACCOMPLISHED; AND ALTN EXTENSION UNSUCCESSFUL. WING MECHANICAL DOWNLOCK INDICATOR REMAINED FLUSH W/ WING SKIN. HYDRAULIC FLUID FROM SYSTEM 'C' COMPLETELY LOST. EMERGENCY DECLARED, UNEVENTFUL LANDING. INSPECTION REVEALED RT MLG RETRACT ACTUATOR CIRCUMFERENTIAL FRACTURE OF CYLINDER BODY LOCATED AT RETAINING RING GROOVE. END CAP SEPARATED FROM CYLINDER BODY. LONGITUDINAL CYLINDER CRACK STARTING FROM RETAINING RING GROOVE AREA ALSO FOUND. JURY BRACE FRACTURED AT THE UNIVERSAL ASSY. 2L73 4F A23WE 20041203000932004120300093NM 2004 12 3 MWEA040188 120041019A53305936434127 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 FUSELAGE SKIN DENT AT APPROXIMATELY STATION 351 FROM LONGERON 27 LEFT AND 28 LEFT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041203000942004120300094NM 2004 12 3 MWEA040189 120041019A53305924802519 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 BELLY SKIN DENTED BETWEEN LONGERON 29 AND 30 LEFT BETWEEN STATION 389 AND 370. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041203000952004120300095NM 2004 12 3 MWEA040190 120041019A53305924802519 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 BELLY SKIN DENTED BETWEEN STATION 389, 370 AND BETWEEN LONGERON 29 AND 30 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041203000972004120300097CE 2004 12 3 65453 120040930A323311238002223 ACTUATOR BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07190YV UE190 AFTER LOWERING THE LANDING GEAR HANDLE, CREW DID NOT HAVE A GOOD DOWN AND LOCKED INDICATION FOR THE NOSE LANDING GEAR . ACFT RETURNED TO PFN, LANDED WITH NO FURTHER INCIDENT. REMOVED INSTALLED OVERHAULED NOSE WHEEL ACT, P/N 11238002223 S/N 48. 2L72 4T RTA24CE 20041203000992004120300099NE 2004 12 3 ARWA20041003 220041013A732171128726 FUEL CONTROL DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE MALFUNCTIONED A ARWAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO19661AV 45969 671292 NR 4 ENGINE SLOW TO SPOOL AT MHLM AND DURING APPROACH ENGINE WOULD NOT ACCELERATE PAST IDLE. REMOVED AND REPLACED NR 4 ENGINE FUEL CONTROL UNIT IN ACCORDANCE WITH MM 73-20-1 AND SYSTEM OPERATIONAL CHECK NORMAL ON ENGINE RUN UP IN ACCORDANCE WITH MM 71-00. NO LEAKS NOTED, ALL PARAMETERS NORMAL. 2L74 4F4 F 4A25 1E8 20041203001032004120300103EU 2004 12 3 WRNA200400013 120041005A7830 WARNING LIGHT AIRBUS300 A300B4203 3930306EU THRUST REVERSER ILLUMINATED A WRNAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05504TA 216 ON TAKE OFF ROLL, NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT CAME ON. A/C RETURNED TO GATE. THRUST REVERSER LOCKED OUT. PLACED ON MEL 78-30-01, PLACARD INSTALLED. A/C RETURNED TO SERVICE 2L72 4F RTA35EU 20041203001042004120300104NE 2004 12 3 NACA20040046 220041016A8530356994 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 5 DAMAGED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03779TA1328 1328 45529 28737 NR 2 ENGINE SHUT DOWN DUE TO BACK FIRING. REPLACED NR 5 CYLINDER DUE TO LOW COMPRESSION. OPS CHECKED GOOD. 2L74 4R4 R A781 5E8 20041203001072004120300107NM 2004 12 3 SB04156 120041122A335020121 CHARGER BOEING737 737301 1384611NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 2 THRU 4, INCLUDING THE EMERGENCY EXIT SIGN, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041203001082004120300108NM 2004 12 3 F3LA200400113 120041015A3411 PITOT HEAD BOEING737 737317 138447PNM NR 2 OBSTRUCTED A F3LAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM03EICHH 23177 REJECTED TAKEOFF, FLIGHT CREW REPORTED NR 2 AIRSPEED INDICATOR WOULD NOT INDICATE AIRSPEED. FLUSHED FIRST OFFICER'S UPPER RIGHT PITOT PROBE FROM DISCONNECT AT NR 2 AIR DATA COMPUTER. NR 2 AIRSPEED INDICATOR, OPS CHECKED NORMAL PER MM 34-11-00. 2L72 4F RTA16WE 20041203001102004120300110SO 2004 12 3 CHQA000557 120040916A3350 BULB EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11379 145606 LEFT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB AMM 33-54-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041203001112004120300111NM 2004 12 3 HNAA0400093 120040929A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHK, FOUND CORROSION ON STR 31 STARBOARD, WHICH REQUIRED REMOVED AND REPLACED OF THE STRINGER. THIS EO8-53-04-0656 PERFORMS SPLICE OF X467 FRAME, WHICH HAD SECTIONS REMOVED FOR ACCESS FOR STR R/R`D. THIS EO IS A MAJOR REPAIR. 2H72 4T RTA13NM 20041203001122004120300112CE 2004 12 3 64051 120040819A6123 SWITCH BEECH 1900 1900D 1154162CE AUTOFEATHER SYS MALFUNCTIONED A AMWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07144ZV UE144 UPON TAKEOFF ROLL OUT, CREW OBSERVED RIGHT HAND ENGINE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATED. ABORTED TAKEOFF. RETURNED TO GATE WITH NO FURTHER INCIDENT. RESECURED SWITCH ASSY AND ADJUSTED SWITCH, OPS CK NORMAL. 2L72 4T RTA24CE 20041203001132004120300113CE 2004 12 3 DXTA200400403 120040921A291699144543 RESERVOIR CESSNA750 750 2076810CE A-HYD SYSTEM LEAKING E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07960QS2851 7500160 DURING FLIGHT, HYD PUMP FAIL A ILLUMINATED, FOLLOWED BY HYDRAULIC PTU FAIL. HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO ON "A" SIDE, AUX PUMP "A" DID NOT RESTORE QUANTITY OR PRESSURE. BLEW GEAR DOWN PER CHECKLIST AND USED EMERGENCY BRAKES FOR LANDING. INSPECTED "A" SIDE HYDRAULIC SYSTEM FOUND ACCUMULATOR HYDRAULIC BLOCK PLUG LEAKING, REMOVED AND REPLACED O-RING. SERVICED "A" SYSTEM, BLED BRAKES INSPECTED FILTERS NO DISCREPANCY NOTED. RAN AIRCRAFT AND CHECKED ALL FLIGHT CONTROLS, OPS CHECK GOOD AND BRAKES OPS CHECKED GOOD. REMOVED AND REPLACED "A" SYSTEM RESERVOIR ASSEMBLY IAW CESSNA 750 MM CHAPTER 29-10-01, OPERATIONAL AND LEAK CHECKS GOOD. 2L72 4J RTT00007WI 20041203001162004120300116EU 2004 12 3 YENA200447 120040929A2120 ODOR AIRBUS320 A320232 3930326EU CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15537JB 1785 ALL LIVE TV'S NOT WORKING. THERE WAS BURNING SMELL IN THE CABIN WHEN TURNING LTV'S TO STANDBY DURING RESET. PERFORMED LIVE TV INTEGRITY CHECK CONCERNING ELECTRICAL ODOR PER JETBLUE AIRWAYS INFORMATION NOTICE 2004-T023TR. FOUND NO EVIDENCE OF ELECTRICAL ODOR THROUGHOUT CABIN. LIVE TV SYSTEM, OPS CHECK NORMAL PER AMM 23-39-00. 2L72 4F RTA28NM 20041203001182004120300118NM 2004 12 3 F3LA200400108 120041001A5320 INTERCOSTAL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR PANEL SUPPORT CORRODED AT STA 986.5 - 1006, RBL 20. REPLACED FLOOR SUPPORT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51. 2L72 4F RTA16WE 20041206000012004120600001NE 2004 12 6 P9RA20040033 220040828A7200 ENGINE BOEING757 757236 1384971NM RROYCERB211 RB211535E4 54555NE RIGHT MALFUNCTIONED A P9RAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO11521NA 25592 AT FLIGHT LEVEL 360, POS-JFK, RIGHT ENGINE DECREASED TO PARTIAL THRUST WITH EPR INDICATING NORMAL CRUISE POWER, 1.6EPR. ALL OTHER INDICATIONS SHOWED PARTIAL THRUST. INITIATED ENGINE ANTI-ICE AND IGNITERS TO CONTINUOUS. CYCLED ENGINE LIMITER. NORMAL THRUST RETURNED AFTER 1 MINUTE. EEC BITE PRODUCED FAULT CODE 47. CHECKED P1 CONNECTIONS, NO LEAKS FOUND. CHECKED WIRING BETWEEN EPR TRANSMITTER AND EEC. CONTINUITY CHECKED GOOD. WORK PERFORMED IAW FIM 732100. ACCOMPLISHED ACCELERATION DECELERATION TEST. ENGINE TIME WITHIN LIMITS AND FREE OF SURGE PER MM 710000. 2L72 4F4 FRTA2NM E12EU 20041206000022004120600002CE 2004 12 6 DXTA200400375 120040828A3260 POSITION SWITCH RAYTHNDH125 HAWKER800XP 7150012CE MLG MALFUNCTIONED E DXTAO OTHER N FALSE WARNING DEDESCENT 1 GL07887QS 258387 WHILE DESCENDING INTO MDW ON ILS 4R, THE NOSE GEAR "GREEN" DOWN AND LOCK LIGHT WOULD NOT ILLUMINATE. CYCLED THE GEAR WITH NO LUCK, ALSO HAD THE PIN INDICATOR IN THE UP POSITION, FLEW BY THE TOWER AND CONFIRMED NOSE GEAR DOWN. PERFORM THE EMERGENCY GEAR EXTENSION PROCEDURE, LANDING WAS UNEVENTFUL. ADJUSTED NOSE GEAR LEG-LOCK SWITCH AND NOSE GEAR CHANGE-OVER SWITCH IAW HAWKER 800XP AMM CHAPTER 32-60-00. OPS CHECKED GOOD. 2L72 4F RTA3EU 20041206000032004120600003CE 2004 12 6 DXTA200400376 120040829A32416041H281A RELAY CESSNA500 560CESSNA 2076750CE ANTI SKID SYSTEMMALFUNCTIONED E DXTAA UNSCHED LANDING S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07339QS 5600339 POWER BRAKE LOW PRESS AND ANTI-SKID WENT INOP. ANNUNCIATORS ILLUMINATED DURING TAXI, FOLLOWED BY A LOSS OF BRAKE PRESSURE IN THE PILOT AND COPILOT BRAKE PEDALS. TROUBLESHOT SYSTEM REPLACED PUMP ELECTRICAL RELAY AND LOW PRESSURE SWITCH OPS CHECK AND LEAK CHECK SATISFACTORY. ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20041206000042004120600004CE 2004 12 6 65806 120041014A323011438800013 POWERPACK BEECH 1900 1900D 1154162CE MLG FAILED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07132YV UE132 GEAR WILL NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED POWER PACK P/N 114-388000-13 S/N MX 386539. 2L72 4T RTA24CE 20041201001242004120100124EA 2004 12 1 SWIA200414120 120041120A5350601R33038957 RADOME CNDAIRCL600 CL6002B19 1900309EA NOSE DAMAGED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07409SW5163 5163 7056 UPON ARRIVAL AT GATE, FIRST OFFICER NOTICED SMOKE COMING FROM NOSE (TRU) BAY. REPLACED RADOME ASSY. 2L72 4F RTA21EA 20041201001292004120100129 2004 12 1 SWAA043418 420041122A256565C19901 CABLE BOEING737 7373H4 1384600NM AFT DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29652SW 27722 DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE RELEASE CABLES MISROUTED. REROUTED CABLES PER MM. 2L72 4F RTA16WE 20041201001302004120100130NM 2004 12 1 SWAA043419 120041122A335065C27093 LIGHT BOEING737 7373G7 1384595NM FWD CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS HOLDER CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20041201001352004120100135WP 2004 12 1 MWEA040191 120040923A5320993061267 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31808ME 48070 LEFT FUSELAGE CUSP MEMBRANE AT FRAME STATION 1305 HAS A CRACK. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041201001402004120100140EA 2004 12 1 COMA0460631 120041121A291673031 RESERVOIR CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM FAULTY A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01914CA20942 7012 FLIGHT 5091 RECEIVED A LANDING GEAR DISGREE CAUTION AND NOSE DOOR WARNING INBOUND TO CRW. CREW DECLARED AN EMERGENCY AND GEAR WAS EXTENDED MANUALLY. REPLACED THE NR 3 HYDRAULIC RESERVOIR. 2L72 4F RTA21EA 20041201001542004120100154EU 2004 12 1 AWXA200401287 120041113A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU ZONE 242 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28605AW19035358 543 MCN - MAJOR REPAIR - DURING C-06 CHECK THE MID CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041201001682004120100168EU 2004 12 1 CX7A194J0438 120040712A21507769106 ACM SAAB SF340 340B 7860101EU CABIN COOLING SEIZED A CX7ABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL03315CE3982 3982 340B343 SHORTLY AFTER DEPARTURE THE FLIGHT CREW NOTICED A BURNING SMELL IN THE COCKPIT FOLLOWED BY THE FLIGHT ATTENDANT CALLING FORWARD TO REPORT SMOKE SMELL IN THE BACK AS WELL AS A WAILING/LOUD SOUND AND VIBRATION COMING FROM BETWEEN THE WINGS. A COUPLE OF MINUTES LATER THE SMELL OF SMOKE DISAPPEARED. FOUND LT PACK FAILED CAUSING SMELL AND SOUNDS. 2L72 4T RTA52EU 20041201001702004120100170NE 2004 12 1 079471 220040728A7200 UNKNOWN SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE UNKNOWN A UHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL17146SD N146SD 484 FLIGHT 7966 IAD-HPN. DURING TAKEOFF ROLL AT ABOUT 90 KNOTS THE CREW NOTICED THE LT TORQUE INDICATOR FLUCTUATING APPROXIMATELY 8-10 PERCENT. CTOT WAS ARMED. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE. A/C TAKEN OUT OF SERVICE 7-28-04 AT 2320 (LT). IAD MX RAN A/C WITH CTOT ON AND OFF IN MULTIPLE DIFFERENT POWER SETTINGS. NO DEFECTS NOTED AT THIS TIME. A/C RETURNED TO SERVICE 7-29-04 AT 0015 (LT). 2L72 4T4 TRTA52EU E8NE6 20041201001712004120100171EU 2004 12 1 CX7A194J0447 120040807A3260 SWITCH SAAB SF340 340B 7860101EU MLG WOW OUT OF POSITION A CX7AO OTHER N FALSE WARNING CLCLIMB 1 GL03309CE 340B201 AFTER TAKEOFF LANDING GEAR COULD NOT BE RETRACTED. SHIMMED NR 2 WOW SWITCH BRACKET. 2L72 4T RTA52EU 20041202000062004120200006EA 2004 12 2 COMA0460625 120041115A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CONTAMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01917CA 7017 FLIGHT 5888 CABIN DOOR WARNING MESSAGE. CLEANED EXCESSIVE GREASE FROM DOOR PROX SENSORS. 2L72 4F RTA21EA 20041202000092004120200009EU 2004 12 2 AWXA200401329 120041116A5347D53112782200 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28644AW 317 SAL - MAJOR REPAIR - DURING C-02 CHECK CORROSION WAS FOUND ON SEAT TRACK -Y765 AT FR 20. MAINTENANCE REMOVED CORRODED SEAT TRACK -Y765 FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 53-00-15 FIG 202. 2L72 4F RTA28NM 20041202000222004120200022EU 2004 12 2 CXA194J0436 120040701A33206500202 LAMP SAAB SF340 340B 7860101EU SEAT 14BC OUT OF ADJUST A CX7AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL03316CE 340B348 BURNING RUBBER (SMOKY) ODOR COMING FROM AFT CABIN ROWS 12-14. MAINTENANCE INSPECTED AIRCRAFT AND FOUND READING LIGHT ABOVE 14BC STUCK ON. READJUSTED READING LIGHT, OPERATIONAL CHECK GOOD. 2L72 4T RTA52EU 20041202000292004120200029EU 2004 12 2 MALA040673 120041103A14205GAJ1 CONNECTOR SAAB SF340 340B 7860101EU MLG WW DAMAGED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15438XJ 340B438 ON FINAL WITH GEAR DOWN AND 3 GREEN LT MAIN GEAR LIGHT FLICKERED, GEAR LIGHTS REMAINED STEADY. WENT BACK TO VIS APPROACH AND RECYCLED GEAR, 3 GREEN ALL STEADY, NO PROBLEMS. LANDED. INTRANSIT LIGHT FUNCTIONED NORMALLY BEFORE, DURING, AND AFTER GEAR CYCLES/SWINGS. CREW DID NOT REPORT EMERGENCY BUT THE TOWER REPORTED EMERGENCY. MAINTENANCE REPLACED CONNECTOR 5GA-J1 IN LT GEAR WELL. REPLACED LANDING GEAR CONTROL BOX. 2L72 4T RTA52EU 20041202000352004120200035WP 2004 12 2 AALA20041136 120041115A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW219304C 49530 DFW - INFLIGHT T560/15 SMOKE AND ELECTRICAL SMELL IN CABIN AT SEAT 13A. LANDED DFW WITHOUT INCIDENT. FOUND BURNED OUT LIGHT BULB AT ROW 12. REPLACED LIGHT BULB, RAN ENGINES AND PACKS. NO SMOKE OR FUMES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041202000602004120200060NM 2004 12 2 2004UALA01119 120041110A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE CARGO BAY BUCKLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 CARGO PIT FLOOR JUST IN FRONT OF DOORWAY IS SEVERELY BUCKLED. 2L72 4F4 FRTA2NM E17NE 20041202000642004120200064EA 2004 12 2 MASA200400569 120041007A2760 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA SPOILERONS ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0777302 7302 AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO SPOILERONS CAUTION MESSAGE DURING TAKEOFF ROLL. TESTED SYSTEM PER AMM AND FOUND NO FAULTS. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20041202000662004120200066NM 2004 12 2 SWAA043277 120041109A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29371SW BN961 26598 DURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT AFT FLAP PER MM. 2L72 4F RTA16WE 20041202000692004120200069EU 2004 12 2 CX7A194J0440 120040718A21507769106 ACM SAAB SF340 340B 7860101EU RIGHT SEIZED A CX7AO OTHER BS SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL03312CE19228421 340B334 AFTER NR 2 ENGINE START, HEARD A HIGH PITCHED NOISE AND A STRONG BURNING SMELL. NOTHING BUT HOT AIR BLOWING THROUGH THE CABIN. FOUND RT PACK SEIZED CAUSING SOUND AND SMELL. 2L72 4T RTA52EU 20041202000782004120200078NM 2004 12 2 SWAA043363 120041116A53306545774 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED A2 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 727E + 13 AND BS 790, STRINGER 18L. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041202000812004120200081EA 2004 12 2 MASA200400522 120040911A4900 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY FIRE A MASAF ACTIVATE FIRE EXT. AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 SW07591ML 7388 AFTER LANDING IN YUL AND SHUTTING DOWN THE APU FOR THE NIGHT THE GROUND CREW NOTICED FLAMES EMITTING FROM THE APU EXHAUST AREA. AS GROUND CREW WAS MOVING TO NOTIFY THE CREW, THE APU FIRE WARNING ALERTED IN THE COCKPIT AND SIMULTANEOUSLY DISCHARGED THE FIRE BOTTLE AUTOMATICALLY. MAINTENANCE IS IN THE PROCESS OF LOOKING FOR THE SOURCE OF THE FIRE. INDICATIONS ARE POINTING TO THE FIRE BOTTLE CONTAINED IN THE APU ENCLOSURE. 9/11 MX REPLACED FIRE DETECTION CONTROL P/N 472597-02, S/N 0434, AND APU FIREX CONTAINER. 2L72 4F RTA21EA 20041202000942004120200094WP 2004 12 2 MWEA040202 120041109A323359390745501 ACTUATOR DOUG DC9 DC982 3022082WP MLG OUT OF ADJUST A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31809ME 48071 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. FOUND RIGHT WEIGHT ON WHEELS CONDUIT HITTING ON BACK OF SHELL OF UP LATCH SENSOR. REPOSITIONED WEIGHT ON WHEEL CONDUIT & REPOSITIONED BACK SHELL OF UP LATCH SENSOR. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR AND RIGGED CONTROL CABLES. 2L72 4F A6WE 20041202001002004120200100NM 2004 12 2 UPS04243181 120040902A5730 PANEL BOEING727 727173C 1384059NM LT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, LEFT WING UPPER SURFACE T/E PANEL FWD OD MLG BEAM HAS DELAMINATION ON AFT END, ALSO HAS UPPER SURFACE DENTS. REPAIRED AND INSTALLED PANEL AS PER DRAWING 65-21655 IAW SRM 51-30-02. 2L73 4F A3WE 20041202001042004120200104NM 2004 12 2 UPS04443424 120041018A5315 FLOORBEAM BOEING747 747123 1384873NM MAIN CABIN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38096 STA 1920 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD & AFT HOLES 0.380. REAMED BEAM HOLES TO; FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH & SRM 51-10-08. FAB FWD FITTING 69B04238 & AFT FITTING 65B38747. INSTALLED FITTING PER EO C/W SK675-916. 2L74 4F A20WE 20041202001112004120200111EA 2004 12 2 MASA200400377 120040627A2711 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA AILERON TRIM ILLUMINATED A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07923FJ 15023 THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH AILERON MIS TRIM MESSAGE. MX PLACED THE AILERON TRIM SYSTEM ON MEL AND THE AIRCRAFT DEPARTED. MX TROUBLESHSOT PER FIM 27-12-00 AND PERFORMED POWER RUNS AND COULD NOT DUPLICATE THE PROBLEM. 2L72 4F RTA21EA 20041202001142004120200114WP 2004 12 2 ARWA20040604 120040625A2910 HYDRAULIC SYSTEM DOUG DC8 DC863 302198AWP NR 2 CONTAMINATED A ARWAO OTHER O OTHER DEDESCENT 1 SO19345JW 46042 PRIOR TO TOP OF DESCEND BOTH HYDRAULIC PUMPS OUTPUT PRESSURE ZERO. AILERON AND RUDDER REVERSION LIGHTS ON. COMPLETED EMERGENCY ABNORMAL HYDRAULIC CHECKLIST. CHECKED A/C FOR HYDRAULIC LEAK, NO LEAKS NOTED. INSPECTED MAIN HYDRAULIC CASE DRAIN FILTERS FOR CONTAMINATION, NO DEFECTS NOTED IN ACCORDANCE WITH DC8 MM 27-10-27 AND 29-10-17. CHECKED HYDRAULIC BYPASS LEVER FOR DETENT AND RIGGING PER MM 29-10-18, FOUND AIR IN HYDRAULIC SYSTEMS, BLED AIR FROM NR 2 ENGINE DRIVEN PUMP AND FLIGHT CONTROLS IN ACCORDANCE WITH MM 71-00 AND PERFORMED OPERATIONAL CHECK OF HYDRAULIC PUMPS PER MM 29-30-0; VERIFIED PROPER OPERATION OF INDICATION IAW MM 29-20-0; PUMPS OPERATIONAL CHECK GOOD. 2L74 4F 4A25 20041202001152004120200115EA 2004 12 2 SWIA200414058 120041030A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 621 LEFT HAND FLOOR SUPPORT ANGLE LBL 40 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20041202001342004120200134NM 2004 12 2 UPS04243182 120040909A5313 STRINGER BOEING727 727173C 1384059NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, CORROSION ON LOWER FLANGE OF STR 18A AT BS 850 LT SIDE CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IAW B727NDTM 51- 00-00 PT 6 FIG 4, ALL CORROSION REMOVED. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. 2L73 4F A3WE 20041202001392004120200139EA 2004 12 2 MASA200400474 120040824A5270 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT ILLUMINATED A MASAO OTHER N FALSE WARNING CRCRUISE 1 SW07909FJ 15009 RT FORWARD EMERGENCY EXIT CAUTION MESSAGE IN FLIGHT. MX MEL'ED. 8/25/04 MAINTENANCE RESEATED DOOR AND NO DEFECTS NOTED. 2L72 4F RTA21EA 20041202001512004120200151NM 2004 12 2 SWAA043354 120041116A2910651782121 MODULE BOEING737 7377H4 1384404NM B-HYD SYSTEM FAULTY A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29795SW 30606 AIR TURNBACK, FLAPS WOULD NOT RETRACT ABOVE POSITION 1. REMOVED AND REPLACED NR 2 HYDRAULIC B-SYSTEM MODULE PER MM. REMOVED AND REPLACED RIGHT W/W MAIN HYDRAULIC FILTER AND CASE DRAIN FILTERS PER MM. 2L72 4F RTA16WE 20041202001662004120200166NM 2004 12 2 SWAA043262 120041108A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME CHORD AT RIGHT BS 616, WL 201, CRACKED. REPAIRED FRAME CHORD SECTION PER ER. 2L72 4F RTA16WE 20041202001682004120200168NM 2004 12 2 UPS04243206 120040908A5730 PANEL BOEING727 727173C 1384059NM WING T/E PANEL DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C DELAM ON RT WING T/E PANEL LOWER SURFACE OF WING BELOW NR 13 SPOILER. REPAIRED DELAM ON PANEL IAW SRM 51-40-20. 2L73 4F A3WE 20041202001762004120200176NM 2004 12 2 UPS04243213 120040909A5730 STRINGER BOEING727 727173C 1384059NM WING CNTR SECT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN AT STR 10C RBL 65 BS 810. CLEANED CORROSION IAW SRM 51-10-01. HFEC CARRIED OUT IAW B727-NDTM -5 1-00-00 PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOP M 20-10-03. AREAS REPROTECTED. 2L73 4F A3WE 20041202001782004120200178NM 2004 12 2 UPS04243218 120040910A5730 SKIN BOEING727 727173C 1384059NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, AREA OF LITE SURFACE CORROSION AROUND FASTENER HEADS ON HORIZ FLANGE OF RT WING UPPER SPLICE PLATE AT BS 850. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IN ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. ALL CORROSION REMOVED. STRESS RELIEVED AREA, INSTALLED FASTENERS AND REPROTECTED AREA IAW SRM 51-10-02. 2L73 4F A3WE 20041202001902004120200190NM 2004 12 2 QXEA200400748 120041028A5320 SILL BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - FORWARD FUSELAGE, FORWARD PASSENGER DOOR LOWER DOOR SILL THRESHOLD MEMBER CORRODED AROUND A/NUT HOLES AND RIVET FASTENER HEAD FSX1.00 TO 32.40 WLZ100.032. 2H72 4T RTA13NM 20041202001932004120200193NM 2004 12 2 UPS04243222 120040901A5230 ANGLE BOEING727 727173C 1384059NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, SUSPECT CRACK ON INTERNAL STRUCTURE OF AFT LOWER CARGO DOOR. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED ENDS MARKED. REPLACED ANGLE IAW EO B727-5230-0032. 2L73 4F A3WE 20041202002032004120200203CE 2004 12 2 DXTA200400347 120040723A3260 UPLOCK SWITCH CESSNA750 750 2076810CE MLG DIRTY E DXTAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL07950QS 7500050 NOSE LANDING GEAR CYCLED IN FLIGHT AT FL430 & FL240, NOSE GEAR UNLOCK LIGHT ILLUMINATED FOR ABOUT 3 SECONDS. CLEANED NOSE GEAR AND MAIN GEAR UPLOCK SWITCHES CONNECTORS WITH CONTACT CLEANER, ADJUSTED NOSE GEAR UPLOCK SWITCHES, CYCLED LANDING GEAR SEVERAL TIMES, OPS CHECK WAS GOOD. WORK DONE IAW CESSNA 750 MM CHAPTER 32-30-05. 2L72 4J RTT00007WI 20041203000062004120300006EA 2004 12 3 04330643 120041125A3040 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDSHIELD HEAT FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27643BR 7363 WINDSHIELD HEAT FAILURE. MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER. 2L72 4F RTA21EA 20041203000072004120300007WP 2004 12 3 04FDEA03211 120041125A5751ARC1110501 SKIN DOUG DC10 DC1010 3022110WP AILERONS DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND LT OUTBD AILERON UPPER SKIN STA XOA 907 TO XOA 912. REPLACE SKIN PER SRM 51-35-01 PAG 1-12. REBALANCE AILERON WILL BE PERFORMED PER NRC NF10454. 2L73 4F A22WE 20041203000122004120300012SW 2004 12 3 H3AA1 120041130A812037291001501 BRACKET GULSTM500 500B 0141106SW LYC O540 IO540E1A5 41532EA HARTZLHCC3Y HCC3YR GL TURBOCHARGER CRACKED E H3AAK NONE O OTHER ININSP/MAINT 1 SO3324KM 303 500B129611 L18148 CK587 A CRACK APPROXIMATELY 2.5 INCHES LONG WAS NOTICED IN THE UPPER PORTION OF THE TURBO CHARGER ATTACH BRACKET. UPON REMOVAL OF FROM THE ENGINE MOUNT NUMEROUS CRACKS WERE NOTED RUNNING ALONG WELDS AND THROUGHOUT THE ENTIRE ASSEMBLY. SUBSEQUENT REMOVAL OF THE TURBO MOUNTING ASSEMBLY ON THE RIGHT ENGINE REVEALED CRACKS IN MANY OF THE SAME AREAS. THE CRACKS ARE DIFFICULT TO DETECT UNLESS THE ASSEMBLY IS REMOVED FROM THE ENGINE MOUNT. BOTH UNITS HAVE 303.5 HOURS SINCE NEW. PICTURES OF THESE UNITS ARE AVAILABLE AT YOUR REQUEST. 1H72 3O3 O 6A1 1E4 5 CP25EA 20041203000152004120300015NM 2004 12 3 04FDEA03151 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 17R EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000162004120300016NM 2004 12 3 ASAA0410423 120041003A531265465682 PRESSURE BLKHD BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE FUSLAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02742AS 23136 PAE - LFEC OF AFT PRESSURE BULKHEAD FOUND CRACK INDICATION AT STR 7 LT OB RIVET. REPAIRED AFT PRESSURE BULKHEAD IAW SRM. 2L72 4F4 F A16WE E2EA 20041203000262004120300026EU 2004 12 3 NA0207001 120041109A261267321000500 FIRE DETECTOR SUNDSTRANDEM BRAERODH125 HS125700A 4230170EU APU BAY FALSE INDICATIONE ERYAFH ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS N FALSE WARNING TXTAXI/GRND HDL 1 CE0770X 854008 NA0207 APU FIRE WARNING INDICATION AFTER APPROXIMATELY 15 MINUTES OF APU OPERATION ON GROUND. CREW DISCHARGED FIRE EXTINGUISHING SYSTEM AND SHUT DOWN APU. TROUBLESHOT PROBLEM TO A BAD BOTTOM APU HEAT DETECTOR. REPLACE HEAT DETECTOR WITH NEW UNIT. REPLACE FIRE BOTTLE/SQUIB ASSEMBLY WITH OVERHAULED UNIT. NO ACTUAL OVERHEAT/FIRE OCCURRED. 2L72 4F A3EU 20041203000282004120300028EU 2004 12 3 DJFA2004030 120041107A2130 CABIN PRESSURE AMD FALC50FALCON50MYST2730106EU FAILED E DJFAGBA O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23517CW 17 CREW REPORTED, WHILE CRUISING AT FL430 AIRCRAFT SUDDENLY LOST PRESSURIZATION. THE CABIN LIGHT AND CABIN HORN BOTH CAME ON SIMULTANEOUSLY. EMERGENCY DESCENT WAS PERFORMED IMMEDIATELY, AND OXYGEN MASKS WERE DONNED. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO KLWS. MANUAL PRESSURIZATION WOULD NOT OPERATE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A CABIN PRESSURIZATION CHECK IN ACCORDANCE WITH THE FALCON 50 MAINTENANCE MANUAL WITH NO DEFECTS NOTED. PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A46EU 20041203000362004120300036NE 2004 12 3 NACA20040059 220041109A8530 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 9 CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL0399330961 961 43576 P34459 NR 2 ENGINE SHUT DOWN DUE TO NR 9 CYLINDER DOUBLE SHORTED SECONDARY. INSPECTION OF NR 9 CYLINDER SHOWED CRACKED CYLINDER AND PLUGS OIL FOULED. PROP WOULD NOT TURN AND SCAVENGE SCREENS SHOWED EVIDENCE OF METAL. REPLACED NR 2 ENGINE. 2L74 4R4 R 6A3 5E8 20041203000482004120300048CE 2004 12 3 2004F00429 120041129A243499100944 SENSOR CESSNA404 404 2075901CE CONT O520 GTSIO520M 17032SO ALTERNATOR BURNED OUT E EA ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL2780BS 4040048 823572R WHILE IN CRUISE FLIGHT, THE PILOT NOTICED SPARKS COMING FROM THE LEFT ENGINE FORWARD COWL AREA. AS A PRECAUTION, THE ENGINE WAS SHUTDOWN AND SECURED. THE AIRCRAFT THEN MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, IT WAS DISCOVERED THAT THE ALTERNATOR OUT SENSOR SHORTED INTERNALLY AND HAD BURNED A HOLE THROUGH THE END OF IT'S CASE. THE SENSOR WAS REPLACED AND AN OPS CHECK PROVED SATISFACTORY. 1L72 3O3 ORTA25CE E7CE 20041203000512004120300051 2004 12 3 ASAA0480443 420040517A2565D29985107 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE L-2 DOOR FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02931AS483631618 49232 OKC - C-CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE FAILED TO INFLATE FULLY DURING DEPLOYMENT TEST IAW WK CARD 28525002. SLIDE ASSY WAS REPLACED INSP OF THE REMOVED ASSY REVEALED A DENTED ASPIRATOR. ASSY WAS OVERHAULED, INCLUDED REPLACEMENT OF ASPIRATOR, POWER UNIT, CYLINDER SLING, GIRT, AND GIRT ATTACHMENT. MOST PROBABLE CAUSE OF FAILURE WAS OBSTRUCTION OF THE ASPIRATOR PORT BY BUBBLEWRAP SECURED TO FUSELAGE TO PROTECT AC FROM IMPACT BY DEPLOYING SLIDE. MFG HAS DEVELOPED PROTECTIVE PADDING KIT: 1) CUSHIONED PAD TO PROTECT AC FROM IMPACT BY DEPLOYING SLIDE. 2) LARGE GROUND COVER TO PROTECT SLIDE FROM CONTAMINATION AND DAMAGE. SLIDE DEPLOYMENT TEST WK CARDS BEING REVISED TO SPECIFY USE OF KIT. (REV 3) 2L72 4F4 F A6WE E9NE 20041203000562004120300056NM 2004 12 3 UPS04243509 120041118A3350 SWITCH BOEING727 72725C 138400HNM EMERGENCY LIGHT WILL NOT TEST A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01946UP 19721 EMERGENCY EXIT LIGHTS WON'T TEST. FOUND 2 SCREWS LOOSE ON EMERGENCY LIGHT SWITCH. TIGHTENED SCREWS, CKS OK PER MM 33-50-01. 2L73 4F A3WE 20041203000582004120300058 2004 12 3 UPS04843540 420041123A2565 SLIDE DOUG DC8 DC873F 302199FWP COCKPIT DEPLOYED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01810UP 46001 MAIN CABIN EXIT EMERGENCY SLIDE DEPLOYED. REPLACED SLIDE IAW 25-60-00 SECURITY CK GOOD, THIS CLEARS M291801. 2L74 4F RT4A25 20041203000592004120300059WP 2004 12 3 UPS04843541 120041119A5720576598937 GUSSET DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 CRACKED GUSSET IN LT WING CENTER L/E NEAR XW371. REMOVED CRACKED GUSSET REF SRM 51-1-21. FAB REPLACEMENT FROM SHT 7075T6-.063 REF DWG5769589 AND SRM 51-1-8. INSTALLED GUSSET REF SRM 51-1-21. 2L74 4F RT4A25 20041203000642004120300064NM 2004 12 3 04FDEA03144 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 2L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000872004120300087EA 2004 12 3 HNAA0400151 120041004A2497 WIRE DHAV DHC8 DHC8311 1386006EA NR 1 GCU LOOSE A HNAAC ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 EA07335EN 375 AT 10,000 FT MASTER WARNING ILLUMINATED ASSOCIATED W/LOSS OF CABIN PRESS, DOOR WARNING LTS W/ AUX INVERT AND RUDDER FULL PRESS C/L AFTER CAPT'S G/S, SIDE PANEL AND FLIGHT INST WENT OUT, CAPTS 800 PANEL BLANK, A/P FAILED. NR 1 DC GEN C/L ILLUM SELF CORRECT. REMOVED AND REPLACED STARTER GEN AND GCU FOR NR 1 ENG OPS CHECK GOOD. THEN ON TAKEOFF ROLL AT V1 AUX INVERTER C/L ILLUMINATED ALONG WITH ALL EXTERIOR DOOR WARNING LTS CAPT FLT. INST LIGHTS WENT DARK ALONG WITH CAPT 800 PANEL AND RNAV. FOUND WIRE PULLING OUT OF PIN "LITTLE A" ON THE NR 1 DC GCU CONNECTOR. REPINED WIRE ,OPS CHECK GOOD. 2H72 4T RTA13NM 20041203000902004120300090CE 2004 12 3 T2BA1 120040930A3411 PITOT SYSTEM BEECH 1900 1900C 1154161CE PILOTS SIDE CONTAMINATED E T2BAO OTHER O OTHER CLCLIMB 1 SO15172TE UB24 WHILE EN ROUTE FROM AUA TO DED, PILOT REPORTED DURING CLIMB AND DESCENT, ALTIMETER AND VSI WAS ACTING ERRATIC. UPON ARRIVAL TO DED, THE PITOT STATIC SYSTEM WAS TESTED IAW MANUFACTURES RECOMMENDATIONS AND COULD NOT REPRODUCE PROBLEM ON THE GROUND. AIRCRAFT WAS RELEASE FOR TEST FLIGHT TO SEE IF PROBLEM PERSISTED AND WAS INSTRUCTED TO DEVIATE TO SFB TO CE AVIONICS OE4R411IF THE PROBLEM OCCURRED AGAIN. UPON FURTHER INVESTIGATION, CE FOUND MOISTURE IN THE PILOT PITOT STATIC SYSTEM. SYSTEM WAS CLEARED AND RECERTIFIED. 2L72 4T RTA24CE 20041203001172004120300117NE 2004 12 3 64468 220040831A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE MALFUNCTIONED A AMWAO OTHER O OTHER TOTAKEOFF 1 CE07131YV UE131 AFTER TAKEOFF CREW TURN ON BLEED MODE MAN COOL. CAPTAIN NOTED ITT WAS CLIMBING AT 780C. TORQUE HAD DROPPED TO 2500LB. TEMP STABILIZED BUT TORQUE CONTINUED TO DROP. THEN IT GOT TO 2000LB CREW DECLARED EMERGENCY AND RETURNED TO FIELD. LANDED SAFELY WITH NO FURTHER INCIDENT. NO DEFECTS NOTED, OPS CK NORMAL. 2L72 4T4 TRTA24CE E26NE 20041206000062004120600006NE 2004 12 6 NACA20040042 220041001A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 16 CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL036174C2112 2112 44075 56476 NR 2 ENGINE SHUT DOWN DUE TO BACKFIRING AND RUNNING ROUGH. REPLACED NR 16 CYLINDER DUE TO A CRACKED HEAD. CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20041206000072004120600007NE 2004 12 6 Z1RA097452 220040929A7200 SHIELD SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE LEFT ENGINE CRACKED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF2071 841PR 760523 20595 CONTAINMENT SHIELD CRACKED. REPLACED ITEM IAW TURBOMECA S/B 292722022 TU 22. 1G72 3U3 UNCH1NE E00054EN 20041206000082004120600008NE 2004 12 6 Z1RA097453 220040929A72000292817220 TURBINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE RT ENGINE CRACKED E Z1RAO OTHER O OTHER NRNOT REPORTED 1 SW11760AF2071 760523 20594 CONTAINMENT SHIELD CRACKED. REPLACED ITEM I/A/W TURBOMECA S/B 292722022 TU 22. 1G72 3U3 UNCH1NE E00054EN 20041206000092004120600009EU 2004 12 6 MHIA097614 120041005A5310350A36101502 SUPPORT BRACKET UROCOPEC130 EC130B4 8680989EU FUSELAGE CRACKED E MHIAK NONE O OTHER ININSP/MAINT 1 EA25454AE615 3490 DURING 100 HOUR INSPECTION, A HAIR LINE CRACK WAS NOTED ON THE LEFT HAND SIDE OF THE NR 2 TRDS BEARING SUPPORT (FROM FWD). ON REMOVAL THE CRACK WENT THROUGH THE SUPPORT ARM. CRACK LOCATED 32MM ABOVE THE CENTERLINE OF ATTACHMENT BOLT HOLE. THE SUPPORT IS STAINLESS AND THE CRACK IS DIFFICULT TO SEE. REMOVED SUPPORT AND REPLACED WITH NEW. 1G72 3U H9EU 20041206000122004120600012EU 2004 12 6 DHL2004365003 120040908A3260 CONNECTOR AIRBUS300 A300B4203 3930306EU PROXIMITY SWITCHCONTAMINATED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01365DH 149 AFTER DEPARTURE, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON THE CENTER PANEL AFTER GEAR RETRACTION. THE ASSOCIATED LIGHT WAS EXTINGUISHED ON THE SECOND OFFICERS PANEL. COMPLETED THE LANDING GEAR UNSAFE. FOUND OIL ON LT PROXIMITY SWITCH CONNECTORS, CLEANED AND RESECURED. SYSTEM OPERATES NORMALLY IAW 32-61-00. 2L72 4F RTA35EU 20041206000132004120600013 2004 12 6 P9RA20040034 420040830A2565767 BULB BOEING757 757236 1384971NM ESCAPE SLIDE INOPERATIVE A P9RAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO11522NA 25133 AIRCRAFT IN MAINTENANCE, ORD, 4R DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE WITH DOOR IN ARMED POSITION. REPLACED BULB FOR 4R DOOR SLIDE ARM LIGHT. 2L72 4F RTA2NM 20041206000142004120600014CE 2004 12 6 ACE09042004 120040904A5711118100021603 SPAR BEECH 1900 1900C 1154161CE RT WING CORRODED E YADAK NONE O OTHER ININSP/MAINT 1 AL03114AX28212 UC36 WHILE REPAIRING A FUEL LEAK IN THE RIGHT WING MAIN FUEL TANK, FOUND CORROSION ON THE MAIN SPAR LOWER CAP FORWARD FLANGE REQUIRING MAJOR REPAIR. THIS AREA WAS IDENTIFIED AS A SUSPECT CORROSION LOCATION IN RAYTHEON COMMUNIQUÉ NR 71. 2L72 4T RTA24CE 20041206000152004120600015EA 2004 12 6 HNAA0400157 120041028A5330 SKIN PANEL DHAV DHC8 DHC8311 1386006EA FUSELAGE DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07337EN 284 DURING C CHECK INSPECTION, NUMEROUS MINOR DENTS WERE FOUND IN THE SAME SKIN BAY. THIS WAS REPAIRED BY TRIMMING OUT THE DAMAGE AND INSTALLING AN EXTERNAL REPAIR DOUBLER. THIS IS A MAJOR REPAIR. 2H72 4T RTA13NM 20041206000162004120600016NM 2004 12 6 DHL2004753002 120040901A2781 POSITION SWITCH BOEING727 727223 1384074NM NR 2 & 3 SLAT FAILED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01753DH 22468 DURING FLAP RETRACTION FROM 5 DEG TO 2 DEG LE FLAP LIGHT REMAINED ILLUMINATED PERFORMED ABNORMAL PROCEDURE AND LIGHT REMAINED ILLUMINATED. POSITION TEST SHOWED 2, 3 SLATS 1 KUGGER AND 6, 7 WERE EXTENDED. REMOVED AND REPLACED NR 1 LEADING EDGE FLAP POSITION SWITCH, PERFORMED OPS CHECK, OPS CHECK GOOD IAW B727 M/M 27-82-01. 2L73 4F A3WE 20041206000172004120600017NM 2004 12 6 DHL2004754024 120041015A324226011825 BRAKE ASSY BOEING727 727223 1384074NM MLG MALFUNCTIONED A DHLAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01754DH 22008 WHEN BRAKES ARE APPLIED EVENLY, RIGHT BRAKE CHATTERS AND ACFT PULL TO THE RIGHT. REPLACED NR 3 BRAKE PER M/M 32-41-32. 2L73 4F A3WE 20041206000182004120600018NM 2004 12 6 0410002 120041026A5210 DOOR BOEING737 737230C 1384472NM L1 NOT CLOSED A MJYAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW07767TW 20258 AIRCRAFT FAILED TO PRESSURIZE ON CLIMB-OUT. 2L72 4F A16WE 20041206000202004120600020EU 2004 12 6 DHL2004363521 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3882, LBL 36 FS 18 TO FS 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FRAME 18 TO FRAME 26 1/2 LBL 36 MAIN CABIN REF: A-300 SRM 51-30-30. FOUND SEAT TRACK OUT OF LIMITS IAW A-300 SRM 53-10-00. INSTALLED NEW SEAT TRACK FROM FS 18 TO FS 30 AT LBL 36 IAW A-300 SRM 53-10-10 / 51-10-40. TREATED AND PRIMED AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 51-40-12. 2L72 4F RTA35EU 20041206000212004120600021CE 2004 12 6 091304A 120040910A3251 WHEEL LEAR 25 25B 5170511CE NLG OUT OF POSITION E ESUAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03425JL 127 THE CREW DID NOT NOTICE THAT THE NOSE WHEEL WAS TURNED 180 DEGREES, THEREFORE WHEN THE CREW RETRACTED THE LANDING GEAR THE NOSE GEAR COULD NOT LOCK IN THE UP POSITION, WHICH WOULD NOT ALLOW THE GEAR DOORS TO CLOSE. THEREFORE THE GEAR UNSAFE LIGHTS. 2L72 4J A10CE 20041206000232004120600023NE 2004 12 6 NACA20040038 220040918A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 4 CRACKED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL036174C515 515 44075 P33324 NR 1 ENGINE SHUT DOWN DUE TO RUNNING ROUGH. REPLACED NR 1 ENGINE NR 4 CYLINDER DUE TO A CRACKED HEAD. CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20041206000252004120600025NM 2004 12 6 DHL2004780505 120040909A5754 SKIN BOEING727 727223 1384074NM NR 1 SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, NR 1 SLAT L/E SURFACE, WS 720 HAS DENT WITH CREASE. CUT OUT DING AREA NR 1 SLAT L/E SKIN APPROX 3/4 BY 1 1/4 INCH AND FABRICATED ONE DOUBLER APPROX4 3/4" BY 4 3/4" USING 2024-T3 .080 PO 9001135 IAW B727 SRM 57-50-3 FIG 1 ALODINED AND PRIMED DOUBLER IAW B727 SRM 57-10-2. INSTALLED REPAIR IAW B727 SRM 57-50-3 FIG1. 2L73 4F A3WE 20041206000262004120600026NE 2004 12 6 ALGA097415 120040220A6320SB2559101 BEARING SKRSKYS76 S76A 8143006NE TRANSMISSION SPALLED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03PTHOR71 760003 TRANSMISSION DISASSEMBLED FOR METAL CONTAMINATION, FOUND ROLLER BEARING BREAKING DOWN. REMOVED AND REPLACED BEARING. 1G72 3U H1NE 20041206000332004120600033NM 2004 12 6 DHL2004780502 120040909A5313 LONGERON BOEING727 727223 1384074NM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, BULGE IN EXTERNAL SKIN WITH 2 POPPED RIVET HEAD AT STA 678 STR 28R. REMOVED OLD STRINGER SPLICE FROM STA 678, STR 28R IAW B727 SRM 51-30-2 FOUND CORROSION ON SPLICE TO BE CUT OUT OF LIMITS IAW B727 SRM 53-10-1. FAB NEW STR SPLICE FROM 7075 T6 063 PO NR 335792 P/N NR BAC 1498-125 IAW B727 SRM 51-10-2. INSTALLED PART IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041206000352004120600035EU 2004 12 6 DHL3004363518 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3889, FS 26.5 - FS 33.5 RBL 78 INCH MAIN CABIN SEAT TRACKS CORRODED BEYOND LIMITS PER A-300 SRM 51-40-11. REMOVED SECTION OF SEAT TRACK FROM FS 26 TO FS 33 RT BL 78" IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 26.5 TO FS 33.5 AT RBL IAW A-300 SRM 51-10-10 / 51-10-40. TREATED AND PRIME AND APPLY POLYWHITE AS REQUIRED REF: A-300 SRM 51-40-10 AND A-300 SRM 51-40-12. MATERIAL USED, 60-22457, PO 24302234. 2L72 4F RTA35EU 20041206000372004120600037 2004 12 6 P9RA20040041 420040918A2565D30654122 SLIDE BOEING757 757231 1384950NM L1 DOOR DEPLOYED A P9RAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO11708TW 28480 L1 DOOR SLIDE INADVERTENTLY BY CREW MEMBER. AIRCRAFT FERRIED TO DTW, SLIDE REPLACED PER MM. 2L72 4F RTA2NM 20041206000382004120600038NE 2004 12 6 NACA20040037 220040917A8530404481 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 8 FAILED A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL0343872437 437 533294 P33688 NR 3 ENGINE SHUT DOWN DUE TO NR 8 CYLINDER DOUBLE SHORTED SECONDARY. REPLACED NR 3 ENGINE DUE TO CYLINDER FAILURE AND METAL CONTAMINATION.. 2L74 4R4 R A781 5E8 20041206000412004120600041SO 2004 12 6 CHQA000553 120040904A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 LOWER FORWARD EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041206000432004120600043EU 2004 12 6 DHL2004363516 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 3874, FS 31-FS 35 RBL 36 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 31 - FS 35 AT RBL 36 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 31 - FS 35 AT RBL 36 IAW A-300 SRM 53-10-10 / 51-10-40. MATERIAL USED: 60-22457, PO NR 24302234. 2L72 4F RTA35EU 20041206000482004120600048NM 2004 12 6 DHL2004780509 120040910A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE BULGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, FWD CARGO COMP BULGE BS 600 STR 27 LT HAS BULGE IN CHANNEL AT FASTENER. REMOVED FASTENER FOR ACCESS STR 27LT BS 600 IAW B7272 SMR 51-30-2, CUT OUT DAMAGE SECTION OF STRINGER APPROX 13 FT AND FABRICATED ONE STR REPLACEMENT PART APPROX 13 INCH USING BACB 1498-142 PO NR 9001233 AND TWO SPLICES APPROX 10 INCH USING BACB 1498-131 PO NR 9001233 IAW B727 SRM 53-10-3 FIG 1 ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2 . INSTALLED REPAIR IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20041206000532004120600053WP 2004 12 6 WLDA200492 120040905A5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO1114075 46922 DURING "B4" CHECK IN BYH, FOUND LBL30 FS 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL LBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01. 2L73 4F4 F A22WE E23EA 20041206000542004120600054NE 2004 12 6 04053 220041024A7200 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 4 FAILED A KCSAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL23717CK59179 20325 685816 ON T/O FROM HNL, NR 4 ENGINE LOSS AT 200 FT WITH LOUD BANG AND BRIGHT FLASH. EGT WENT TO 1100 DEGREES, ENGINE OIL PRESSURE APPROX 10 PSI FOR 5 MIN, THEN WENT TO 5PSI. RETURNED TO HNL. BOROSCOPED NR 4 ENGINE LP AND HP COMP SECTIONS AND FOUND EVIDENCE OF BIRD STRIKE. 2L74 4F4 F A20WE E20EA 20041206000552004120600055CE 2004 12 6 66038 120041021A3210 LANDING GEAR BEECH 1900 1900D 1154162CE BOTH MALFUNCTIONED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07174YV UE174 BOTH MAIN GEARS WOULDN'T RETRACT AFTER TAKEOFF. RESET ALL C/B CLEANED ALL UPLOCK AND DOWNLOCK. 2L72 4T RTA24CE 20041206000562004120600056CE 2004 12 6 66145 120041026A3242 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07144ZV UE144 ON TAXI INTO CLT FROM DUJ ON REPO FLIGHT 9415, CREW REPORTED THE LEFT BRAKES FELT SPONGY. REMOVED AND REPLACED O/B BRAKE ASSY. 2L72 4T RTA24CE 20041206000592004120600059NM 2004 12 6 HNAA0400127 120041021A3222 STRUT DHAV DHC8 DHC8102 2809003NM NLG CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07809EX3282515364 L32091 302 DURING MAINTENANCE MIDDLETOWN, IT WAS DISCOVERED THAT AIRCRAFT 809EX HAD A 7 INCH CRACK FROM THE TOP AFT CENTER EDGE OF NOSE LANDING GEAR STRUT BODY DOWNWARD. MAINTENANCE REMOVED AND REPLACED THE STRUT ASSEMBLY. 2H72 4T RTA13NM 20041206000612004120600061NM 2004 12 6 DHL2004780510 120040910A5313 STRINGER BOEING727 727223 1384074NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, FWD CARGO COMP BILGE BS 480 STR 27 LT HAS BULGING AND CRACKS IN CHANNEL AT FASTENERS. REMOVED FASTENERS FOR ACCESS AT FWD CARGO COMP BILGE BS 480 STR 27L IAW B727 SRM 51-30-2. CUT OUT DAMAGE SECTION OF STRINGER APPROX 16 1/4". FABRICATED ONE STRINGER REPAIR APPROX 16 1/4 USING BACB 1498-142 PO NR 9001233 AND ONE SPLICE APPROX 10 1/4/ USING BACB 1498-131 PO NR 9001233 IAW B727 SRM 53-10-3 FIG 1 ALODINE AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED STRINGER REPAIR AND SPLICE IAW B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 20041206000632004120600063CE 2004 12 6 DXTA200400418 120041007A3246315371 WHEEL CESSNA750 750 2076810CE MLG WORN E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07960QS94 7500160 LT BRAKE NOISY AND GRABS AFTER LANDING, LT OUTER BRAKE ASSY SMOKES AFTER COOL DOWN. AFTER SHORT TAXI BRAKE CONTINUES TO SMOKE, INNER TIRE IS CONSIDERABLY COOLER THAN OUTER. INITIAL INSPECTION OF LT WHEELS AND BRAKES SHOWS LT OUTER TIRE TO HAVE 8 TO 10 INCH WEAR MARKS ON INBOARD AND OUTBOARD PERIMETER OF TIRE. TIRE PRESSURE ON LT OUTBOARD TIRE IS ALSO BELOW ACCEPTABLE LIMITS, TIRE PRESSURE WAS 158 PSI., LT INBOARD TIRE WAS ACCEPTABLE AT 183 PSI. INSPECTED LT O/B ANTI-SKID TRANSDUCER AND IT SPINS FREELY, ALL FITTING, LINES AND HOSES APPEAR NORMAL, NO LEAKS WERE NOTED. CHECKED LEFT AND RIGHT HYDRAULIC RESERVOIRS AND QUANTITY WAS GOOD ON BOTH. CHECKED LT/R HYDRAULIC ACCUMULATORS, BOTH WERE GOOD A 1300 PSI. 2L72 4J RTT00007WI 20041206000652004120600065CE 2004 12 6 65388 120040928A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS FAILED A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07131YV UE131 AFTER TAKE OFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO THE FIELD. MAINTENANCE WAS CALLED. REMOVED AND REPLACED FLAP SPLIT FLAP SWITCH. 2L72 4T RTA24CE 20041206000712004120600071EU 2004 12 6 DHL2004363007 120040911A3150 CONTROL BOX AIRBUS300 A300B4203 3930306EU AURAL WARNING MALFUNCTIONED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01363DH 85 TAKEOFF REJECTED DUE TO REPETITIVE AUDIO WARNINGS. NO WARNING LIGHTS ILLUMINATED. RESECURED AURAL WARNING CONTROL BOX. NO DEFECTS NOTED. OPS CK IS GOOD IAW 31-24-11. 2L72 4F RTA35EU 20041206000742004120600074CE 2004 12 6 GLBA20030739 120041021A212111438002811 BLOWER BEECH 1900 1900D 1154162CE AIR DISTRIBUTIONBINDING A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03253GL949 949 UE253 AIRCRAFT FLYING LEVEL AT 12,000 FT WHEN FLIGHT CREW NOTICED STRONG ODOR IN COCKPIT. CREW RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED THE FORWARD VENT BLOWER WAS DEFECTIVE, MAKING GRINDING NOISE AND THE CAUSE OF THE REPORTED ODOR. MAINTENANCE REPLACED DEFECTIVE VENT BLOWER AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTA24CE 20041206000762004120600076NM 2004 12 6 DHL2004753003 120040914A3260 SWITCH BOEING727 727223 1384074NM MLG DIRTY A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01753DH 22468 UPON RETRACTING, THE LANDING GEAR TAILSKID LIGHT REMAINED ILLUMINATED PERFORMED ABNORMAL PROCEDURE TAILSKID LIGHT EXTINGUISHED. CLEANED AND LUBED SWITCHES (UPLOCK AND DOWNLOCK). OPS CK NORMAL ON GROUND IAW MM 32-71-1. 2L73 4F A3WE 20041206000782004120600078NE 2004 12 6 C8GA20040020 220040917A7261 ENGINE BOEING727 727225 1384077NM PWA JT8 JT8D9A 52048NE NR 1 DEFECTIVE A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15808EA4123 22439 666344 FLT 1721 FROM FLL TO TOL, AT FL140, AT CLIMB POWER THE NR 1 ENG LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED. FOLLOWED AOM PROCEDURES A2-10 AND THE NR 1 ENG IN-FLIGHT SHUTDOWN AS A PRECAUTIONARY AND AIR TURN BACK TO FLL. A/C WAS INSPECTED AND THE LOW OIL PRESSURE SWITCH CONNECTOR WAS CLEAN AND THE MAIN OIL SCREEN ON THE NR 1 ENGINE WAS REPLACED AND THE SYSTEM OPS CHECKED GOOD PER B727 MM 72-61-8 AND 72-00, NO LEAKS NOTED DURING ENGINE RUN AND THE AIRCRAFT RETURNED TO SERVICE. THE AIRCRAFT THEN BLOCK OUT AND DURING TAXI, THE LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED AGAIN. AIRCRAFT THEN RETURNED TO BLOCK. REPLACED THE OIL PRESSURE RELIEF VALVE, THE MAIN ENGINE OIL SCREEN AND THE ENGINE OIL PUMP. 2L73 4F4 F A3WE E2EA 20041206000812004120600081NM 2004 12 6 DHL2004745023 120040911A3260 ACCESSORY UNIT BOEING727 727224 1384076NM MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 CENTER RED DOORS LIGHT AND S/O'S PANEL RT GEAR DOOR LIGHT CAME ON DURING CLIMB PERFORMED ABNORMAL PROCEDURE PER AOM 6.2.64 BOTH LIGHTS OFF WITH GEAR HANDLE UP. TRANSFERED TO DMI LOG PER MEL 32-1 CAT C CONTROL NR 17814 PLACARDS INSTALLED. REF DMI 17814 CENTER RED DOOR LIGHT AND RT GEAR DOOR LIGHT ON. ACCOMPLISHED POWER OFF RERACK OF LDG GEAR ACCY. OPERATED DOORS PER MM 32-12 AND 3262 ADJ AND TEST. OP NML PER MM . THIS CLEARS DMI 17814 PLACARDS REMOVED. 2L73 4F A3WE 20041206000822004120600082CE 2004 12 6 DXTA200400413 120041004A2450 CIRCUIT BOARD CESSNA750 750 2076810CE APU PANEL CONTAMINATED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07938QS 7500183 DURING FLIGHT, NOTICED ELECTRICAL BURN ODOR IN THE COCKPIT, FOLLOWED BY DISCOVERY OF WATER SEEPING OUT FROM BEHIND RT CIRCUIT BREAKER PANEL, BELOW THE 3 APU CIRCUIT BREAKERS. REMOVED AND INSPECTED CO-PILOT CIRCUIT BREAKER PANEL, CLEANED WITH CONTACT CLEANER, NO WATER NOTED BEHIND OR ON PANEL. INSTALLED CO-PILOT C/B PANEL, PERFORMED APU START. START WAS NORMAL. RAN BOTH ENGINES AND FOUND NO SMELL IN C/B PANEL AREA, RAN ENGINES FOR 5 MINUTES, NO FURTHER ACTION REQUIRED PER 750MM CHAPTER 24. 2L72 4J RTT00007WI 20041206000832004120600083NM 2004 12 6 0408001 120040805A535065465779 SKIN BOEING737 737230C 1384472NM DELAMINATED A MJYAK NONE O OTHER ININSP/MAINT 1 SW07767TW 20258 DURING A-CHECK INSPECTION, FOUND TAIL CONE WITH AN APPROXIMATELY 8 INCH BY 7 INCH SECTION OF DELAMINATION. 2L72 4F A16WE 20041206000842004120600084EU 2004 12 6 40004 120040906A3260C242450061 UPLOCK AMD FALC50FALCON900 2700160EU NLG INOPERATIVE E ERYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07369BG6698 040 UPON DEPARTURE FROM KIND, RETRACTED LANDING GEAR AND DETECTED INCOMPLETE RETRACTION CYCLE. PLACED LANDING GEAR HANDLE IN DOWN POSITION WITH SUCCESSFUL GEAR EXTENSION. RETURNED TO KIND WITH UNEVENTFUL ARRIVAL. TROUBLESHOT LANDING GEAR RETRACTION PROBLEM AND ISOLATED TO THE NOSE LANDING GEAR UPLOCK MECHANISM. REPLACED UPLOCK MECHANISM AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF SYSTEM. 2L73 4F RTA46EU 20041206000862004120600086NE 2004 12 6 N440SL2 220040908A7200 ENGINE BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE NR 1 MALFUNCTIONED E A1UAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE03440SL 7158 4573845234 APPROXIMATELY 2 TO 3 MINUTES INTO THE FLIGHT, MASTER CAUTION ILLUMINATED ALONG WITH ENG I LOW LIGHT. NOTICED THE TORQUE OF THE NR 1 ENGINE DROPPING ALL THE WAY TO ZERO. N1 OF THE NR 1 ENGINE WAS 75 PERCENT. N2 DROPPED TO APPROXIMATELY 97 PERCENT. BEEPED UP THE ENGINES TO GET APPROXIMATELY 99 PERCENT N2. PILOT THEN TRIED TO INCREASE THE TORQUE OF THE NR 1 ENGINE, HOWEVER HAD NO EFFECT OF ANY POWER CHANGE OR TORQUE INCREASE. PILOT PERFORMED RUN ON LANDING WITHOUT FURTHER PROBLEMS. MAINTENANCE PERFORMED NUMEROUS CHECKS TO DETERMINE CAUSE OF PROBLEM. ALL PARAMETERS WITHIN MANUFACTURERS LIMITS, NO DEFECTS FOUND. ALL COMPONENTS OPERATING NORMAL. 1G72 3U3 U H13EU E5NE 20041206000882004120600088EU 2004 12 6 DHL2004363526 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3888, FS 18 - FS 26.5 RBL 78 MAIN CABIN SEAT TRACK CORRODED BEYOND A-300 SRM 51-40-11. REMOVED CORROSION FROM AREA FRAME 18 - TO FRAME 26.5 RBL 78 FOUND OUT OF LIMITS IAW A-300 SRM 53-10-10. REMOVED SEAT TRACK FROM FS 18 TO 26.5 RBL 78 IAW A-300 SRM 53-10-10 AND 51-30-30. INSTALLED NEW SEAT TRACK FROM FS 18 - FS 26.5 AT RBL 78 IAW A-300 SRM 53-10-10. TREATED AND PRIMED AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 51-40-12. MATERIAL USED 60-22457, PO NR 24302234. 2L72 4F RTA35EU 20041206001022004120600102WP 2004 12 6 DHL2004801508 120040902A5511 FRAME DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT HORIZONTAL STABILIZER INBD L/E UPPER FORMER CRACKED 1.000, XFS 53.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. PERFORMED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW SRM 55-2-0 PG 7-8. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20041206001042004120600104NE 2004 12 6 NACA20040033 220040913A8530356994 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 17 CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA171 171 45529 P33192 NR 1 ENGINE SHUT DOWN DUE TO EXCESSIVE SMOKE AND RUNNING ROUGH. REPLACED NR 17 CYLINDER DUE TO A CRACKED HEAD. CHECKED GOOD. 2L74 4R4 R A781 5E8 20041206001062004120600106EU 2004 12 6 DHL2004363515 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3872 FS 30 - FS 38.2 BL 0 SEAT TRACK FLANGES CORRODED OUT OF LIMITS. CORRECTIVE ACTION AS FOLLOWS, REMOVED SEAT TRACK FROM FS 30 - FS 38.2 AT BL 0 IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 30 - 38.2 AT BL 0 IAW A-300 SRM 53-10-10 / 51-10-40. NOTE: MATERIAL USED 60-22457, PO NR 24302234. 2L72 4F RTA35EU 20041207000042004120700004NM 2004 12 7 AALA20041167 120041125A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21380AN 25449 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20B TO 24B INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 20B TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041207000052004120700005NM 2004 12 7 USAA040879 120041021A5313 STRINGER BOEING767 7672B7 1385107NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45788 24765 PIT - Q4, STRINGER, .5 INCH LONG CRACK, FRAME STA 887 AND STR 9R. INSTALLED REPAIR DOUBLERS IAW TYP REP 53-10-20A. 2L72 4F4 FRTA1NM E2GL 20041207000072004120700007EA 2004 12 7 COMA0460658 120041130A2610355523255 ELEMENT CNDAIRCL600 CL6002B19 1900309EA BLEED LEAK SYS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01914CA 7012 FLIGHT 5786 - ANTI-ICE DUCT WARNING MESSAGE. REPLACED THE LEFT FUSELAGE BLEED LEAK DETECTOR SENSE ELEMENT. 2L72 4F RTA21EA 20041207000082004120700008NM 2004 12 7 USAA040845 120041022A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME, .5 INCH CRACK, STR 9 LT AT FRAME, STA 767. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041207000092004120700009NM 2004 12 7 USAA040846 120041011A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041207000112004120700011WP 2004 12 7 AALA20041177 120041201A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21286AA 49298 SEA - CEILING EMERGENCY LIGHTS AT ROWS 4 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 4 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041207000122004120700012EA 2004 12 7 2004F00431 220041203A8500LW11187 RING GEAR BEECH 80 65B80 1152812CE LYC O540 IGSO540A1D 41532EA ENGINE CRACKED G A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW135376M LD301 6208650 OPERATOR REPORTED THAT THE LEFT ENGINE WAS SHUT DOWN AND THE PROPELLER FEATHERED DUE TO ROUGH RUNNING ENGINE SHORTLY AFTER TAKEOFF. MECHANIC INSPECTED ENGINE AFTER LANDING AND DISCOVERED CRACKED RING GEAR IN GEAR REDUCTION UNIT. 1L72 3O3 O 3A20 1E7 20041207000142004120700014NM 2004 12 7 USAA040873 120041020A5320 SKATE ANGLE BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 SKATE ANGLE, 10 INCHES OF CHAFING, 1006 TO 1016 BETWEEN STR 2R AND 3R. FABRICATED NEW ANGLE FROM ENG DWG 65548424. 2L72 4F4 FRTA16WE E2GL 20041207000152004120700015SO 2004 12 7 C2XA04CL119 120041120A2497464CC01 CONTACTOR EMB 145 EMB145LR 3260212SO APU LINE FAILED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2712567 145623 CREW REPORTED A BURNING ODOR AND CRACKING SOUND BEHIND THE CAPTAINS SEAT AFTER THE APU FAILED. REPLACED THE APU LINE CONTACTOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041207000162004120700016EU 2004 12 7 UPS04143563 120041203A2780 CONTROL SYSTEM AIRBUSA300 A300F4622R 3930360EU LE SLATS INOPERATIVE A IPXAO OTHER O OTHER APAPPROACH 1 SO01140UP 0823 ALL SLATS WILL NOT EXTEND ON APPROACH. LUBRICATED L/E SLATS AS REQUIRED PER A300 MM 12-22-27-0 SLATS SEEM TO OPERATE WITH LESS NOISE AND RESISTANCE. 2L72 4F RTA35EU 20041207000172004120700017 2004 12 7 UPS04543561 420041130A2320514013 CONTROL UNIT BOEING757 75724APF 1384969NM E/E BAY INOPERATIVE A IPXAA UNSCHED LANDING O OTHER DEDESCENT 1 SO01412UP 23852 PRIOR TO DAWNA, TRANSMITTED ON 2 FREQUENCIES WITH NO RESPONSE FROM ATC. AFTER DAWNA COULD NOT CONFIRM IF WE`RE TRANSMITTING OR RECEIVING. TRIED ALL MICS ON ALL COM AND NAV RADIOS. TRIED ALT POSITION, MASK , HAND MIC AND PTT SWITCH ON MIC SELECTOR PANEL. REMOVED AND REPLACED THE REMOTE ELECTRONICS CONTROL UNIT. ALL VHF'S OP S NORMAL CONTACTING OPS. 2L72 4F RTA2NM 20041207000182004120700018NM 2004 12 7 UPS04543564 120041203A2750 WARNING SYSTEM BOEING757 75724APF 1384969NM TE FLAPS LOCKED A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01417UP 23904 T/E FLAP ASSY EICAS MESSAGE; FLAPS LOCKED OUT. 2L72 4F RTA2NM 20041207000192004120700019WP 2004 12 7 UPS04843558 120041030A534036468742 FITTING DOUG DC8 DC871F 302199DWP RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 INSPECTION TYPE:C1 SHEAR WEB FITTING CRACKED IN RT MLG W/W AT STA 857 APPROX RBL12. REMOVED CRACKED FITTING REF SRM51-3-0. FABRICATED REPLACEMENT FITTING FROM PLATE7050T7 PER SAA SK798-657, BOEING SERVICE ID 1-48219038 AND DAC DWG3646874. INSTALLED FITTING REF SRM51-1-20D, 51-1-8, 51-1-11, 51-3-0. 2L74 4F RT4A25 20041207000232004120700023WP 2004 12 7 AALA20041180 120041202A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21582AA 53159 DTW - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT ROW 20 FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041207000262004120700026SO 2004 12 7 C2XA04BT117 120041117A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712957 145080 EWR- CO2355, CREW REPORTED THE FORWARD OVERHEAD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT SIGN INVERTER IAW EMB 145 MM NR 33-50-11. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041207000272004120700027NM 2004 12 7 USAA040833 120041008A5330 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US51981 23232 SKIN, 1.5 INCH CRACK, BS 727E, STR 22L. INSTALLED DOUBLER IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E2GL 20041207000302004120700030NM 2004 12 7 USAA040832 120041108A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU39875 27123 C4, FLOORBEAM CAP, .5000 INCH SQUARE, CORROSION, STA 365, RBL 62. ACCOMPLISHED TEE CAP REPAIR IAW TR 53-15-02, SRM 51-10-02, 53-00-51. 2L72 4F4 FRTA2NM E12EU 20041207000312004120700031EU 2004 12 7 SA04111 120041201A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING A FLAME/FIRE CRCRUISE 1 EA19763US12272 1360 CLT FLT 473 ENROUTE PIT TO TPA, DURING THE FLIGHT, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC, FOLLOWED BY THE OUTER PANE CRACKING. CREW ALSO RECEIVED ECAM WARNINGS "R WINDSHIELD" AND "R WINDOW". QRH PROCEDURES WERE FOLLOWED AND THE FLIGHT DIVERTED TO CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. 2L72 4F RTA28NM 20041207000322004120700032NM 2004 12 7 USAA040839 120041103A5312 BULKHEAD BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU39004 24934 PIT - C3, SKIN, 2 CRACKS, 1 INCH IN LENGTH TOTAL, FPBH WL 234, BL7R. DOUBLER REPAIR IAW SRM 53-10-08, FIG 209. 2L72 4F4 FRTA16WE E21EU 20041207000332004120700033NM 2004 12 7 USAA040825 120041008A5311 FRAME BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT - Q5, FRAME, CRACKED, (2EA) 2 INCHES AND 2.2500 INCH, 727D BETWEEN S-27L AND S-27R AT 1 RBBL AND LBBL. REPAIRED DOUBLER IAW SRM 51-70-11. 2L72 4F4 FRTA16WE E2GL 20041207000342004120700034WP 2004 12 7 UPS04843557 120041127A78303055866516 SUPPORT FITTING DOUG DC8 DC871F 302199DWP THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 INSPECTION TYPE: C1, UPPER FWD SUPPORT FITTING CRACKED INSIDE NR 1 IB TR CORE COWL. REMOVED NR 1 IB TR PER MM78-30-00-4. REMOVED AND REPLACED DISCREPANT FITTING REF SRM 51-3-0, 51-1-21. INSTALLED TR PER MM78-30-00-4. RIG, OPS, AND LEAK CHECK OF TR GOOD PER MM78-30-00-4. 2L74 4F RT4A25 20041207000362004120700036NM 2004 12 7 USAA040824 120040911A5314 KEELBEAM BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT - Q5, KEEL REPAIR ANGLE, .2500 INCH CRACK, FASTENER HOLE, STA 520 ON KEELBEAM REPAIR ANGLE RT. REPAIR ANGLES/DOUBLER INSTALLED IAW SRM 51-70-11. 2L72 4F4 FRTA16WE E2GL 20041207000372004120700037NM 2004 12 7 USAA040880 120041018A534065B57839430 FITTING BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 AREAS, 1 INCH BY 2 INCHES, CORRODED; LEVEL 1; TASK NR C53-107-02, LT AFT LAV STA 986.5. REMOVED AND REPLACED FITTING (2 EA) IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041207000392004120700039NM 2004 12 7 AALA20041172 120041127A3350 LIGHT BOEING757 7572Q8 1384972NM CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21703TW 27620 DFW - EMERGENCY ESCAPE PATH LIGHT AT ROWS 11 TO 14 INOPERATIVE. EMERGENCY TRACK LIGHT AT 24D MISSING END CAP AND BROKEN CABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT SEGMENTS AT ROWS 11 TO 14. REPLACED EMERGENCY TRACK LIGHT END CAP AT 24D AND REPLACED EMERGENCY LIGHT STRIP AT SEAT 24 TO LAVATORY D FOR BROKEN CABLE ON EMERGENCY TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041207000402004120700040EA 2004 12 7 COMA0460647 120041126A2750857D100504 DRIVE SHAFT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS WORN A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5584 - FLAPS FAILED CAUTION MESSAGE. COULD NOT DUPLICATE. REPLACED THE RT NR 5 FLEX SHAFT DRIVE. 2L72 4F RTA21EA 20041207000422004120700042EA 2004 12 7 COMA0460649 120041129A2910601R528639 LINE CNDAIRCL600 CL6002B19 1900309EA NR 1 HYD SYSTEM CRACKED A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01483CA 7689 FLIGHT 5204 - HYDRAULIC SYSTEM NR 1 LOW PRESSURE CAUTION, QUANTITY INDICATES ZERO. REPLACED CRACKED NR 1 SYSTEM HYDRAULIC LINE. 2L72 4F RTA21EA 20041207000442004120700044EA 2004 12 7 COMA0460645 120041127A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA 7315 FLIGHT 4958 - FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20041207000472004120700047SO 2004 12 7 C2XA04IA148 120041120A3350RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716911 145446 IAH- FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041207000482004120700048SO 2004 12 7 C2XA04SH538 120041026A532014532636403 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND CORRODED AROUND NUT PLATES AT FRAMES 29 AND 33. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTT00011AT 20041207000502004120700050SO 2004 12 7 C2XA04IA144 120041113A3350375901 SIGN EMB 135 EMB135LR 3260305SO EMERGENCY EXIT DISCONNECTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2727523 145389 CLE - FLIGHT 2948, DURING CREW INSPECTION, IT WAS REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 2 B/C WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE CONNECTOR ON THE SIGN. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCTAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041207000512004120700051GL 2004 12 7 C2XA04TY163 220040915A723023073717 BLADE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COMPRESSOR FAILED A C2XAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 SW27105751868 145640 CAE310005 DURING DESCENT INTO RDU, RIGHT ENGINE HAD A UNCOMMANDED SHUTDOWN AFTER A LOUD NOISE WAS HEARD. MAINTENANCE REMOVED AND REPLACED THE ENGINE. THE TEAR DOWN REPORT SHOWS THE CAUSE OF THE FAILURE TO BE A COMPRESSOR BLADE. 2L72 4T4 FRTT00011ATTE6CH 20041207000522004120700052NM 2004 12 7 USAA040857 120041030A5310 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT - Q4, FRAME, .1250 INCH CRACK, EMANATING FROM FASTENER, FRAME STA 847, STR 9L. INSTALLED DOUBLERS IAW TYPE REP 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041207000532004120700053NM 2004 12 7 USAA040859 120041021A5343 HANGER ASSY BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT MLG WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT - Q4, WALKING BEAM HANGAR, WORN BUSHINGS. RT MAIN LANDING SUPPORT BEAM. REPLACED WALKING BEAM HANGAR IAW AMM 57-15-00-434. 2L72 4F4 FRTA16WE E2GL 20041207000552004120700055NE 2004 12 7 COMA0470081 220041130A72304114T15P02 BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE COMPRESSOR FAN DIRTY A COMAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01368CA 10075 FLIGHT 4997 - N1 VIBE, BECAME UNCONTROLLABLE. REPLACED THE ENGINE FAN BLADES. 2L72 4F4 FRTA21EA EOOO63EN 20041202000762004120200076EA 2004 12 2 MASA200400411 120040718A2711 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA AILERON TRIM ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07923FJ 15023 ABORTED TAKEOFF DUE TO AILERON TRIM CONFIG WARNING. MX PERFORMED OPERATIONAL CHECK IAW MM 27-12-01, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041202000862004120200086EU 2004 12 2 MALA040681 120040929A5330 ICE SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15368PX 340B274 DURING 4K INSPECTION IN LAN, SEVERAL DENTS IN LT ICE SHIELD BETWEEN STRINGERS SL 1634 & SL 1636 REPAIRED IAW MESABA EO S530003. AIRCRAFT RETURNED TO SERVICE 9/29/04. 2L72 4T RTA52EU 20041202000902004120200090SO 2004 12 2 MASA200400556 120041001A3350744425 SIGN EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 LT EMERGENCY EXIT LIGHT FOR THE LEFT OVERWING EXIT INOP. MAINTENANCE REPLACED THE SIGN ASSEMBLY. 2L72 4T RTT00011AT 20041202001022004120200102NM 2004 12 2 UPS04443422 120041018A5315 FLOORBEAM BOEING747 747123 1384873NM MAIN CABIN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, FLOORBEAM 65B38094 STA 1880, LBL 98.58 SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.340, AFT HOLE 0.380. REMOVED AFT ATTACH ANGLE, REAMED HOLES IN BEAM TO 0.389 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH. REAMED OVERSIZED TRACK ATTACH FITTING HOLES TO 0.375 IN. FAB AND INSTALLED 1 EA 69B04297-3 & 1 EA 69B04576-5 PER EO TO C/W SAA SK675-916. 2L74 4F A20WE 20041202001072004120200107NM 2004 12 2 UPS04443428 120041018A5347 SEAT TRACK BOEING747 747123 1384873NM MAIN CABIN DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 INSPECTION TYPE: SPV, MAIN DECK SEAT TRACK REMOVED ALONG LBL 98.58 FROM STA 1840-1920. TRIMMED OUT DAMAGED SEAT TRACK & FABBED REPLACEMENT SECTION REF SRM 53-10-05 FIG 1A, DETAIL II. FABRICATED SPLICE FITTING 69B02537-15 PER DWG. FABRICATED 69B04238-1,-3 FITTINGS PER DWG'S, INSTALLED ALL PARTS PER SRM 53-10-05 FIG 1A DETAIL II, 51-10-2 & EO B747-5310-21190. 2L74 4F A20WE 20041202001292004120200129SO 2004 12 2 SWIA200414142 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 CORROSION AT FR 40 TO FR 44 RIGHT SIDE ANGLE ON INBOARD AND OUTBOARD SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIGHT SIDE ANGLE IAW SRM 51-40-02. 2L72 4T RTA31SO 20041202001322004120200132NM 2004 12 2 UPS04443384 120041021A215071923811 ACM BOEING747 747123F NM NR 3 DAMAGED A IPXAA UNSCHED LANDING BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET NRNOT REPORTED 1 SO01677UP 20391 ATB - SMOKE & FUMES FROM CASPER FOLLOWED BY VIBRATION WHICH CONTINUED AFTER PACKS SECURED UNTIL ACFT DEPRESSURATION. FOUND NR 3 ACM HEAVELY DAMAGED & CAUSE SMOKE. REMOVED AND REPLACED NR 3 ACM AND OPS CHECK OK IAW AMM 21-51-04 P401. 2L74 4F A20WE 20041202001332004120200133EA 2004 12 2 MASA200400466 120040820A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DIRTY A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0797325 7325 PAX DOOR CAUTION MESSAGE IN FLIGHT. MX CLEANED THE DOOR PROXIMITY SENSOR AND PERFORMED OPS CHECK. 2L72 4F RTA21EA 20041202001352004120200135NM 2004 12 2 UPS04243185 120040829A5320 ANGLE BOEING727 727173C 1384059NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, ANGLE BRACKET ON LOWER FWD BS 880 CORRODED RT MLG WW. INSTALLED NEW BRACKET IAW SRM 51-30-02. 2L73 4F A3WE 20041202001362004120200136NM 2004 12 2 UPS04243186 120040907A5320 INTERCOSTAL BOEING727 727173C 1384059NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, INTERCOSTAL CRACKED ON TOILET COMPARTMENT FLOOR BS 294.5-312. INTERCOSTAL REMOVED IAW SRM 51-30-02 AND DAMAGE REMOVED IAW SRM 51-40-03. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, NO DEFECTS FOUND. INSTALLED REPAIR AND INTERCOSTAL IAW SRM 51-30-02. 2L73 4F A3WE 20041202001422004120200142NM 2004 12 2 QXEA200400778 120041116A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR LEAKING A QXEAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 NM09400QX8318 4030 SEA - FLIGHT 2407 - THIRTY MINUTES INTO FLIGHT WHILE AT 25,000 FT, THE CABIN PRESSURE WARNING LIGHTS ILLUMINATED. THE CABIN ALTITUDE INDICATED 10,000 FT AND THE CABIN DIFFERENTIAL INDICATED 5.0 PSI. DURING DESCENT TO A LOWER ALTITUDE, THE PRESSURIZATION APPEARED TO BE NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AFT CARGO DOOR SEAL LEAKING. THE SEAL WAS REPLACED AND OPERATIONAL CHECKS WERE PERFORMED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041202001432004120200143NE 2004 12 2 MASA200400498 220040904A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BOTH OVERTEMP A MASAC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SW0717175 7175 THE AIRCRAFT ABORTED TAKEOFF FOR BOTH ENGINES APPROACHING AN OVERTEMP CONDITION SIMULTANEOUSLY. AFTER DISCUSSION WITH THE CAPTAIN OVER CONDITIONS AT THE TIME OF THE OCCURRENCE IT WAS DETERMINED ANOTHER AIRCRAFT WAS RUNNING UP ITS ENGINES IN THE DIRECTION OF THIS AIRCRAFT. MAINTENANCE PERFORMED RUNS AND FOUND NO DEFECTS. THE AIRCRAFT CONTINUED REVENUE SERVICE. 2L72 4F4 FRTA21EA E15NE 20041202001482004120200148NM 2004 12 2 SWAA043351 120041116A335090083 BATTERY BOEING737 7373Y0 1384671NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED THRU CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS WILL NOT SHUT OFF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041202001602004120200160NM 2004 12 2 QXEA200400757 120041030A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - LEFT HAND INBOARD FLAP YW STATION 60.90 THE UPPER FLAP SURFACE HAS A 1 INCH DIAMETER FOULING MARK INTO THE METAL FROM CHAFING WITH THE UPPER SHROUD. REPAIRED IAW HORIZON AIR EA 6-57-244 AND RD 8/4-57-375, STEPS 3-6. 2H72 4T RTA13NM 20041202001632004120200163NM 2004 12 2 QXEA200400761 120041028A5230 BELLCRANK BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - AFT BAGGAGE DOOR AFT LOWER BELLCRANK LEVER HAS MECHANICAL DAMAGE. REPAIRED IAW HORIZON AIR EA 6-52-350 AND RD8/4-52-710. 2H72 4T RTA13NM 20041202001712004120200171WP 2004 12 2 0401399907 120040822A278239200485511 CYLINDER DOUG DC9 DC932 3022066WP LT SLAT ACTUATORDAMAGED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01957N 47253 UPON CONFIGURING THE AIRCRAFT FOR LANDING, THE RIGHT SLAT DID NOT DEPLOY. THE AIRCRAFT DID ROLL UNCOMMANDED TO THE RIGHT. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT DTW. MAINTENANCE AT DTW FOUND THAT ALL OF THE BOLTS FOR THE RIGHT SLAT T-DUCT WERE LOOSE (AND ONE BACKED OUT) AND THE LEFT SLAT ACTUATOR EYE-BOLT WAS BROKEN. ALL LOOSE HARDWARE WAS SECURED, THE DAMAGED ACTUATOR WAS REPLACED, THE SLAT CONTROL VALVE WAS REPLACED, AND ALL DAMAGE TO SLAT DRIVE MECHANISM WAS BLENDED. OPERATIONAL CHECK GOOD. AIRCRAFT NOT YET BACK IN SERVICE. 2L72 4F A6WE 20041202001752004120200175NM 2004 12 2 UPS04243212 120040909A5730 SKIN BOEING727 727173C 1384059NM WING CNTR SECT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN BETWEEN STR 12-13C RBL 65 BS 795 IN THE AREA INTERFACING WITH Y FLANGE FITTING. CORROSION REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT ON BLENDED AREA IAW B727 NDTM 51-00-00PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOPM 20-10-03. REPAIRED IAW AAAE EO 2004-083-021 (B727-57-20125). 2L73 4F A3WE 20041202001812004120200181CE 2004 12 2 DXTA200400326 120040623A2821 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE NR 1 & 2 ENGINESMALFUNCTIONED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07836QS 258436 DURING TAKEOFF ROLL BOTH ENGINE FUEL ANNUNCIATOR LIGHTS ILLUMINATED, ABORTED TAKEOFF. DRAINED FUEL TANKS AND CHECKED FOR CONTAMINATION, NONE FOUND. REMOVED AND REPLACED NR 1 & NR 2 ENGINE FUEL FILTERS IAW TFE731BR MM CHAPTER 73-21-02. RAN ENGINES AND FILTERS LEAK, OPS CHECK GOOD. NO FUEL LOOK UP LIGHT ILLUMINATED AT THIS TIME. 2L72 4F RTA3EU 20041203000032004120300003CE 2004 12 3 66593 120041108A3242 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07139ZV UE139 CAPT REPORTS RT BRAKE SPONGY. BLED RT BRAKES. 2L72 4T RTA24CE 20041203000042004120300004EA 2004 12 3 QXEA200400784 120041020A3010 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA WING ANTI ICE FALSE ACTIVATIONA QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09609QX 10031 GOT AN ANTI-ICE DUCT MESSAGE ON APPROACH. RAN CHECKLIST (WING ANTI-ICE OFF-ON). WARNING MESSAGE DID NOT REAPPEAR. ON GROUND, RECEIVED SEVERAL ICE CAUTION MESSAGES. MAINTENANCE INTERROGATED MDC. FOUND NO CURRENT FAULTS. COMPLIED WITH OPERATIONAL TEST OF WING ANTI-ICE CONTROL AND INDICATING SYSTEM. NO DEFECTS NOTED. WING ANTI-ICE OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT OK FOR CONTINUED SERVICE. 2L72 4F RTA21EA 20041203000182004120300018EA 2004 12 3 04328703 120041123A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAULTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27703BR 7467 TOILET SMOKE IND ON CLIMB-OUT. ODOR BEGAN SHORTLY AFTER THROTTLES FORWARD FOR T/O NO VISIBLE SMOKE. ODOR WAS MORE OF A MUSTY SMELL, NOT OIL OR BURNING. MX FOUND FAULTY SMOKE DETECTOR. ALSO, REPLACED BOTH COALESCER SOCKS. PERFORMED ENGINE RUNS AT POWER WITH PACKS HOT FOR CONFIRMATION OF CORRECTIVE ACTION. OPS CHECK GOOD. 2L72 4F RTA21EA 20041203000192004120300019NM 2004 12 3 04FDEA03155 120041118A5510 STRUCTURE DOUG MD11 MD11 3023602NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 28L. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000312004120300031NM 2004 12 3 L0FR20040004 120041118A3246260356114 WHEEL BOEING747 747200 1384847NM ZONE 700 CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000672004120300067NM 2004 12 3 04FDEA03147 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 24L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000692004120300069CE 2004 12 3 32041 120041115A261213AT4S SWITCH BEECH 1900 1900C 1154161CE LT FIRE LOOP WILL NOT TEST A NSVAO OTHER L NO TEST NRNOT REPORTED 1 EA27119C UC19 LEFT FIRE LOOP WILL NOT TEST. 2L72 4T RTA24CE 20041203000962004120300096EU 2004 12 3 DJFA2004028 120041014A2120 SMOKE BRAERODH125 BAE125800A 1500285EU CABIN DETECTED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23824CW NA0417 CREW REPORTED THAT ON CLIMB-OUT FOR A TEST FLIGHT, SMOKE WAS NOTICED IN THE AVIONICS/LAV AREA, AND TRASH BIN UNDER THE SINK. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CREW ALSO REPORTED THAT AFTER LANDING THEY HAD OPENED THE REAR BAY DOOR AND THERE WAS SMOKE IN THERE AS WELL. MAINTENANCE INSPECTED THE AFT AVIONICS BAYS AND AREA BELOW SINK FOR SMOKE OR HEAT DAMAGE FROM RADIOS, RELAYS AND ELECTRICAL EQUIPMENT. ALSO, INSPECTED WAS THE AREA BELOW TRASH CONTAINER FOR ANY FOD THAT MAY HAVE CAUSED ARCING OR HEAT DAMAGE. INSPECTED REAR EQUIPMENT BAY ELECTRICAL EQUIPMENT AND BLEED AIR DUCTING FOR SMOKE OR HEAT DAMAGE. A GROUND RUN OF ENGINES, AND APU WAS PERFORMED. 2L72 4F RTA3EU 20041203001002004120300100NE 2004 12 3 ARWA20041002 220041012A7510 CLAMP DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE ANTI ICE DUCT OUT OF POSITION A ARWAEC ENGINE SHUTDOWN ABORTED TAKEOFF JR WARNING INDICATION PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO198969U 46070 671240 DURING TAKEOFF ROLL, NR 2 ENGINE EGT REACHED 580 DEGREES CELSIUS, PULLED POWER BACK OIL PRESS LIGHT ILLUMINATED, N1 AND EPR INDICATION ERRATIC. SHUTDOWN ENGINE NR 2; 200 PERCENT N1 5 PERCENT. OIL PRESSURE 10 PSI. FOUND ANTI-ICE DUCT CLAMP OUT OF POSITION, SECURED CLAMP AND OPERATIONAL CHECK OK IN ACCORDANCE WITH MM 75-10-4. NO LEAKS NOTED. REPAIRED WIRE AT OIL PRESSURE SWITCH IN ACCORDANCE WITH MM 20-50-1. PERFORMED ENGINE RUN UP IN ACCORDANCE WITH MM 71-00. ALL PARAMETERS WITHIN LIMITS AT ALL POWER SETTINGS; NO DEFECTS NOTED. 2L74 4F4 F 4A25 1E8 20041203001142004120300114CE 2004 12 3 64431 120040831A3246 WHEEL BEECH 1900 1900D 1154162CE NLG DAMAGED A AMWAO OTHER J WARNING INDICATION APAPPROACH 1 CE07142ZV UE142 UPON APPROACH HII, GEAR WOULD NOT EXTEND ON FIRST ATTEMPT. CREW RESET GEAR RELAY2 AMP C/B AND GEAR EXTENDED. AIRCRAFT LANDED AND TAXIED TO GATE WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY. 2L72 4T RTA24CE 20041203001152004120300115NM 2004 12 3 HNAA0400096 120040929A531385310984101 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHK, FOUND CORROSION UNDER COCKPIT FLOOR. THIS EO PERFORMS SPLICE REPAIR FOR STR 31 STARBOARD FOR CORROSION. THIS IS A MAJOR REPAIR. 2H72 4T RTA13NM 20041206000102004120600010NM 2004 12 6 TSAA0452074 120041011A5210 HANDLE BOEING737 73776N 13844CHNM PAX DOOR OUT OF POSITION A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13741AL 28641 ETOPS FLT 444, HNL-OAK, RT SERVICE DOOR EXTERIOR HANDLE IN VIEW OF WINDOW FROM INSIDE. NO PRESSURIZATION PROBLEM. RETURNED TO HNL. PERFORMED FIM TASK 52-10-00-810-808. VERIFIED FWD SERVICE DOOR IN LOCKED POSITION WITH HANDLE STOWED. PERFORMED VISUAL INSPECTION OF THE FORWARD SERVICE DOOR. NO DEFECTS NOTED. OVER GROSS WEIGHT LANDING <200 FT MIN DESCENT ON LANDING. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35-2, PHASE I INSPECTION DUE TO AIR RETURN. NO DEFECTS NOTED. 2L72 4F RTA16WE 20041206000112004120600011EU 2004 12 6 DHL2004363512 120041004A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3900 MAIN CABIN SEAT TRACK FLANGE OUT OF LIMITS BETWEEN FRAME 27 TO FRAME 33, LBL 57. REMOVED CORROSION FROM AREA MAIN CABIN SEAT TRACK BETWEEN FRAME 27 AND FRAME 33 LBL 57. FOUND OUT OF LIMITS PER A-300 S.R.M. 53-10-00. 2. FABRICATED NEW SEAT TRACK IAW A-300 SRM 53-10-10. INSTALLED NEW SEAT TRACK FROM FS 27 - FS 33 LBL 57 IAW A-300 SRM 51-10-40 AND 53-10-10. TREATED AND PRIME AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 51-40-12. 2L72 4F RTA35EU 20041206000272004120600027SW 2004 12 6 ALGA097360 120040920A6410206016201131 BLADE BELL 206 206L1 1182107SW TAIL ROTOR DEFECTIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032759N1886 45271 REMOVED DEFECTIVE BLADE FROM SERVICE AND INSTALLED NEW BLADE. 1G71 3U H2SW 20041206000292004120600029NE 2004 12 6 0410001 220041012A7261717000 GEARBOX BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE NR 1 ENGINE LEAKING A MJYAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07737TW 20257 DURING CRUISE ENGINE OIL QUANTITY DROPPED TO ZERO. 2L72 4F4 F A16WE E2EA 20041206000312004120600031EU 2004 12 6 DHL2004363528 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSLAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 3890 FS 18 - FS 26.5 RBL 58 MAIN CABIN SEAT TRACK CORRODED BEYOND A-300 SRM 51-40-11 LIMITS. REMOVED SEAT TRACK FROM FS 18 -26.5 AT RBL 58 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 18 - FS 26.5 RBL 58 IAW A-300 SRM 53-10-10/51-10-40. TREATED AND PRIME AREA AS REQUIRED REF: A-300 SRM 51-40-10 AND A-300 SRM 51-40-12. 2L72 4F RTA35EU 20041206000362004120600036WP 2004 12 6 2004000013 120041003A3610 DUCT DOUG DC10 DC1030 3023501WP BLEED AIR BLOWN A CNMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0717085 47957 AIRCRAFT DIVERTED TO BWI ,DUE TO BLEED AIR LEAK IN L2 DOOR AREA. NR 3 PNEUMATIC SYSTEM ALREADY DEFERRED. REPLACED BLOWN DUCT IN FWD CARGO AREA. 2L73 4F A22WE 20041206000392004120600039GL 2004 12 6 CHQA000558 220040918A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 UNSERVICEABLE A CHQAE ENGINE SHUTDOWN BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL11274 7997 3409 145344 CAE311802 DURING FLIGHT 6345 FROM MSP TO CVG, THERE WAS A BURNING SMELL IN THE COCKPIT DURING CRUISE FLIGHT FOLLOWED BY SMOKE. THE CREW SHUT THE PACKS OFF AND SMOKE BEGAN TO CLEAR WHEN AN E1 LOW OIL PRESSURE AND HIGH OIL TEMPERATURE MESSAGE APPEARED ON EICAS. THE CREW FOLLOWED THE QRH AND SHUTDOWN THE NR 1 ENGINE. THE AIRCRAFT MADE AN EMERGENCY LANDING INTO MSN. THE GROUND CREW NOTICED EXCESSIVE OIL ON THE NR 1 ENGINE COWLING. MAINTENANCE FOUND THE OIL QUANTITY AT 2 QUARTS AND MULTIPLE CMC MESSAGES. THE MAGNETIC CHIP DETECTOR WAS COVERED COMPLETELY WITH METAL CHIPS. R/R`D N1 ENGINE. ENGINE RUNS WERE PERFORMED AND THE ENGINE WAS LEAK CHECKED. THE ENGINE OPS CHECKED GOOD AND WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20041206000442004120600044EU 2004 12 6 254041 120040910A2697 WIRE SAAB SF340 340B 7860101EU LT FIRE WARNING BROKEN A NSVAK NONE P NO WARNING INDICATION ININSP/MAINT 1 EA27350CF 340B350 LEFT ENGINE FIRE TEST WILL NOT TEST PROPERLY NO CHIME. REPAIRED BROKEN WIRE AT LT FIRE WARNING CIRCUIT BREAKER IAW MM 31-50-05, OP CHECKED GOOD. 2L72 4T RTA52EU 20041206000452004120600045EU 2004 12 6 HE66097658 120041011A6700105860291 CONTROL UNIT BOLKMS105 BO105LSA1 5626021EU FLT CONTROLS UNSERVICEABLE E HEEAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 SW03202LF 2014 CAUSING UNCONTROLLED INPUT IN LATERAL AXIS OF FLIGHT CONTROLS. 1G72 3U H3AU 20041206000492004120600049NM 2004 12 6 HNAA0400124 120040928A6120 WARNING HORN DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF* NE BETA SYSTEM MALFUNCTIONED A HNAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 EA07809EX 302 FLIGHT NR 4082 REPORTED HAVING THEIR BETA WARNING HORN SOUND WITH LOSS OF NORMAL BRAKING WHEN POWER LEVERS WERE SELECTED BELOW FLIGHT IDLE DURING GROUND HANDLING. IT WAS DETERMINED THAT THE BETA WARNING HORN SYSTEM WAS AT FAULT, SYSTEM WAS MEL'D AND DEACTIVATED. ALL SYSTEMS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 6 CP7NE 20041206000582004120600058SW 2004 12 6 PNSA041003 120041016A2133 OUTFLOW VALVE SWRNGNSA227 SA227AC 8780603SW CABIN PRESSURE FAILED A PNSAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 AL032719H 713 CREW WAS STARTING CRUISE WHEN THEY LOST PRESSURIZATION, DECLARED EMERGENCY AND DID EMERGENCY DESCENT FROM 17000 FT TO 10000 FT FLIGHT WAS EN ROUTE FROM ANI TO ANC, FLIGHT CONTINUED TO ANC WITHOUT ANY DIFFICULTY. MX FOUND THAT OUTFLOW VALVE BAD, PART WAS REPLACED AND PRESSURIZATION CHECK WAS NORMAL. 2L72 4T RTA8SW 20041206000602004120600060NM 2004 12 6 DHL2004780507 120040909A5320 SPLICE BOEING727 727223 1384074NM STRINGER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, CORROSION ON STR SPLICE STA 1010 AND STR 30. STRINGER SPLICE FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED AND REPLACED STRINGER SPLICE FROM PART NR BAC1498-125 PO NR 335792 13 1/2" BY 3" IAW B727 SRM 51-40-3. ALODINED AND PRIMED PART IAW B727 SRM 51-10-2. INSTALLED NEW SPLICE A STR 30 STA 1010 IAW B727 SRM 51-40-3. 2L73 4F A3WE 20041206000622004120600062CE 2004 12 6 DXTA200400417 120041007A2820 WARNING LIGHT CESSNA750 750 2076810CE FUEL SYS ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07999QS 7500203 7500203 "WING O FILL R" AMBER LIGHT CAME ON IN FLIGHT, LOST ABOUT 400 LBS OF FUEL. INSPECTED RIGHT WING OUTBOARD TRANSFER VALVE. NO DEFECTS NOTED. PERFORMED FUEL TRANSFER SYSTEM SHUTOFF TEST. FOUND ALL OPERATION NORMAL. NO FURTHER ACTION TAKEN. WORK PERFORMED IAW CHAPTER 28-20-00 OF THE CITATION 750 MM. 2L72 4J RTT00007WI 20041206000642004120600064 2004 12 6 IXXA0400107O 420040921A22102588787904 COMPUTER DOUG DC8 DC862 3021970WP YAW DAMPER FAILED A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW11799AL748331598 45922335 AFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ONGOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE THAT THE YAW CHANNEL COMPUTER HAD FAILED THE SELF TEST. THE YCC WAS REMOVED AND REPLACED PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20041206000672004120600067NM 2004 12 6 DHL2004780511 120040912A5754 WEB BOEING727 727223 1384074NM NR 5 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, NR 5 SLAT OUTBOARD END WEB IS CRACKED NEAR LEADING EDGE. REMOVED WEB AT NR 5 SLAT OUTBD END NEAR LEADING EDGE TO BE FABRICATED IAW B727 SRM 51-30-2. FABRICATED NEW WEB MAT USED 2024T3 .032 PO NR 9001030 DIMENSIONS 5 X 4 1/2 IAW B727 SRM 57-50-2 FIG 2 ALODINED AND PRIMED IAW B727 SRM 57-10-2. INSTALLED NEW WEB IAW B727 SRM 57-50-2 FIG2 2L73 4F A3WE 20041206000892004120600089GL 2004 12 6 YTRR096995 220040611A73232549170 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL ENGINE FAILED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03239RA126 4039 THE GOVERNOR WAS INSTALLED AND AFTER 126.2 HRS N2 COULD NOT BE ADJUSTED ABOVE 97 PERCENT. 1G71 3U3 U H2SW E4CE 20041206000902004120600090GL 2004 12 6 YTRR096996 220040802A732323065121 GOVERNOR BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03913RL 2913 GOVERNOR WAS OVERHAULED AND AFTER 98.3 HRS TSO, THE ENGINE EXPERIENCE AN OVERSPEED THAT WAS CAUSED BY A HIGH SIDE FAILURE. 1G71 3U3 U H2SW E4CE 20041206000912004120600091GL 2004 12 6 YTRR096997 220040803A732323065121 GOVERNOR BELL 206 206B3 1181506SW ALLSN 250C 250C20 03013GL FAILED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03496RL 3496 GOVERNOR WAS OVERHAULED, AFTER 482.3 TSO, THE GOVERNOR EXPERIENCED A LOW SIDE FAILURE WHERE N2 COULD NOT BE SET ABOVE 92 PERCENT. 1G71 3U3 U H2SW E4CE 20041206000922004120600092SO 2004 12 6 CHQA000560 120040929A3350 LIGHT EMB 145 EMB145LR 3260212SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11261 145144 RIGHT SIDE AFT OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED AFT EXTERIOR EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD AT THIS TIME AND DATE. 2L72 4T RTT00011AT 20041206000932004120600093NM 2004 12 6 C8GA20040021 120040924A2910 O-RING BOEING727 7272J0 138407ENM HYD SYSTEM WORN A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15713AA 22469 FLT 712 FROM TOL TO ONT. AFTER TAKEOFF, THE "A" SYSTEM WHEN TO 1/2 GALLON, RETRACT THE FLAPS TO 5 DEGREES AND THE HYDRAULIC SYSTEM WENT TO ZERO. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST, AIR TURN BACK TO KTOL AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND REPLACED THE NR 1 HYDRAULIC PUMP RETURNED LINE O-RING. ALSO, REMOVED AND REPLACED THE NR 1 AND NR 2 "A" SYSTEM CASE DRAIN FILTERS, LEAK AND OPERATIONAL CHECKS GOOD DURING ENGINE RUN. SERVICED THE "A" SYSTEM HYDRAULIC RESERVOIR TO FULL, CYCLED ALL FLIGHT CONTROLS AND FLAPS AND SYSTEMS CHECKED GOOD IAW B727 MM 29-11-0 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20041206000942004120600094SO 2004 12 6 CHQA000561 120041003A3350 BULB EMB 145 EMB145MR 3260213SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11972 145440 OVERHEAD EMERGENCY LIGHT LOCATED IN THE AFT AISLE IS INOP. REMOVED AND REPLACED THE OVERHEAD EMERGENCY AISLE LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041206000952004120600095EU 2004 12 6 DHL2004363505 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3884, LBL 58 FS 18 TO FS 26 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM LBL 58" FS 18 TO 26 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK AS PER IAW A-300 SRM 51-10-40. TREAT AND PRIMED AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 18 TO FS 26 AT LBL 58 IAW A-300 SRM 53-10-10. 2L72 4F RTA35EU 20041206000962004120600096EU 2004 12 6 DHL2004363506 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING " C " CHECK IN MIAMI, FLORIDA AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3878 LBL 43 BETWEEN FS 19 SEAT TRACKS CORRODED OUT OF LIMITS PER A-300 PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 15 TO FS 19 AT LBL 43 IAW A-300 SRM 57-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT AND PRIMED AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 15 TO FS 19 AT LBL 43 IAW A-300 SRM 53-10-10. 2L72 4F RTA35EU 20041206000972004120600097NE 2004 12 6 DJFA2004025 220041009A7200 ENGINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE RIGHT POWER LOSS E DJFAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 EA23698TA3685 3685 RK298 PCEJA0301 CREW REPORTED NR 2 ENGINE WAS NOT MAKING TAKEOFF RATED THRUST. 98.7 NL REQUIRED, 98.4 NL ACHIEVED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED, AND NO FURTHER INCIDENTS HAD OCCURRED. MAINTENANCE ADJUSTED THE ENGINE HMU RIGGING. OPERATIONAL CHECK WAS SATISFACTORY. 98.7 NL REQUIRED AND ACHIEVED. AIRCRAFT RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20041206000982004120600098EU 2004 12 6 ALGA097671 120041007A6510C651A2001101 DISC PACK UROCOPEC120 EC120B 8680987EU TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03511AL 1252 FOUND CRACKED LAMINATES. REPLACED W/NEW PART. 1G72 3U NCR0001RD 20041206000992004120600099NM 2004 12 6 DHL2004751003 120041001A3350 BATTERY BOEING727 727264 138408MNM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01751DH 22982 BOTH EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING STANDBY POWER CHECK. REPLACED BATTERIES, BOTH EMERGENCY EXIT LAMPS CK NORMAL IAW B727 M/M 33-50-51. 2L73 4F A3WE 20041206001002004120600100EU 2004 12 6 379002 120040707A3310110VP01ABY1 CONTROL SWITCH AMD FALC20FALCON20F5 2730105EU OVERHEAD CONSOLEBURNED E ERYAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE07892SB 379 ON PREFLIGHT CHECK, MECHANIC IN THE COCKPIT OBSERVED SMOKE COMING FROM THE OVERHEAD PANEL. UPON FURTHER INSPECTION, MAINTENANCE PERSONNEL FOUND DAMAGED "NO SMOKING" AND "SEAT BELT" SWITCHES. THESE SWITCHES HAD BEEN PREVIOUSLY REPLACED AS A RESULT OF A NOISE DETECTED FROM THE OVERHEAD SPEAKER WHERE THE SWITCHES HAD BEEN DETERMINED AS THE CAUSE. THESE SWITCHES WERE REPLACED WITH COMPONENTS FROM A FALCON PARTS DISTRIBUTOR WHERE THE ORIGINAL P/N 110VP01ABO HAD BEEN SUPERSEDED BY P/N 110VP01ABY1. THIS PARTS SUPERSEDE INTRODUCED A REPLACEMENT SWITCH WHICH UTILIZES 28 VDC FOR ILLUMINATION OF THE INTERNAL LIGHTING VS. THE ORIGINALLY CONFIGURED 110 V/400HZ INTERNAL LIGHT. NO INFORMATION CONCERNING AN EXISTING REQ 2L72 4F RTA7EU 20041207000012004120700001NM 2004 12 7 AALA20041163 120041123A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21797AN 30012 DFW - OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT L1 FOR OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041207000032004120700003WP 2004 12 7 AALA20041165 120041124A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW219629H 53599 RDU - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT POSITION B5103 FOR FORWARD OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041207000132004120700013NM 2004 12 7 USAA040842 120041105A5330 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19353US 23556 SKIN, 2 INCH CRACK (SHEAR WRINKLE), STA 727D AT STR 23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229. 2L72 4F4 FRTA16WE E2GL 20041207000212004120700021WP 2004 12 7 UPS04843562 120041127A7830 DEFLECTOR DOUG DC8 DC871F 302199DWP THRUST REVERSER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 INSPECTION TYPE: C1, DEFLECTOR RING CRACKED INSIDE NR 1 T/R AT 7:00 POSITION. REMOVED TRANSLATING COWL PER MM78-30-03. STOP DRILLED CRACK AND VERIFIED SAME PER SPM06-10-01.001. FABRICATED AND INSTALLED REPAIR FROM AMS 5510/5515 PER SAA SK798-837, ESM78-31-41. INSTALLED TR PER MM78-30-03, OPS AND LEAK CHECK GOOD. 2L74 4F RT4A25 20041207000382004120700038NM 2004 12 7 USAA040872 120041020A5320 SKATE ANGLE BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - SKATE ANGLE, 10 INCHES, CHAFED, 1006 TO 1016 BETWEEN STR 2L AND 3L. FABRICATED NEW ANGLE IAW MFG ENG DWG 65-548423. 2L72 4F4 FRTA16WE E2GL 20041207000492004120700049SO 2004 12 7 C2XA04BT116 120041112A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711539 145536 EWR- CO2686, CREW REPORTED EMERGENCY EXIT SIGN BY THE MAIN CABIN DOOR IS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW EMB 145 AMM NR 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041207000562004120700056EA 2004 12 7 COMA0460650 120041124A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01962CA1628749 7123 FLIGHT 5815 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20041207000572004120700057EA 2004 12 7 COMA0460653 120041124A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA4752 7163 FLIGHT 5888 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT INBD FLAP ACTUATOR. 2L72 4F RTA21EA 20041207000582004120700058NM 2004 12 7 USAA040826 120041002A5553 ATTACH FITTING BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE VERT STAB CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT - Q5, FITTINGS, .1250, .5, .5, .5 INCH AREAS, HEAVY CHAFING (4 AREAS), ALL 4 AFT LUGS OF VERT STAB ATTACH FITTINGS. 2L72 4F4 FRTA16WE E2GL 20041207000592004120700059EA 2004 12 7 COMA0460651 120041125A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA LT TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01403CA128908441 7428 FLIGHT 5164, FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20041207000602004120700060EA 2004 12 7 COMA0460652 120041124A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA LT TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01471CA7087 2456 7655 FLIGHT 5841- FLAPS FAIL CAUTION MESSAGE DURING TAXI. REPLACED THE LEFT BPSU. 2L72 4F RTA21EA 20041207000612004120700061SO 2004 12 7 C2XA04CL118 120041118A335078241 INVERTER EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT INTERMITTENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 CLE - FLIGHT NR 2212, THE CREW REPORTED THE EMERGENCY CEILING LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20041207000622004120700062SO 2004 12 7 C2XA04IA149 120041121A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 MCI - FLIGHT 2034, DURING MAINTENANCE INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041207000652004120700065NM 2004 12 7 USAA040827 120041018A5312 PRESSURE BLKHD BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT - Q5, AFT PRESSURE BULKHEAD, NUMEROUS TENSION BOLTS LOOSE, STA 1016 AFT PRESSURE BULKHEAD. REPLACED TENSION BOLTS IAW EA 79074 AND SB 737-53-1229. 2L72 4F4 FRTA16WE E2GL 20041207000662004120700066EU 2004 12 7 UPS04143537 120041123A3150 WARNING LIGHT AIRBUS300 A300B4622R 3930312EU COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01133UP 0816 EVAC SLIDE WARNING LIGHTS ARE INOP. WARNING BUZZER IS OPERATIONAL OPERATED EVAC SLIDE WARNING IAW 52-73-11-4 LIGHT AND BUZZER, OPS CK GOOD. 2L72 4F RTA35EU 20041207000672004120700067EU 2004 12 7 UPS04143539 120041123A3510 OXYGEN MASK AIRBUS300 A300B4622R 3930312EU COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01129UP 0813 CAPTS 02 MASK WILL NOT TEST. JUMPSEAT 02 MASK WILL NOT TEST. REMOVED AND REPLACED CAPT 02 MASK PER MM 35-12-51-4. CHECK OK. CKS OK PER 35-12-51-5 CLEARED M291800 REMOVED PLACARD. 2L72 4F RTA35EU 20041207000692004120700069SO 2004 12 7 C2XA04IA159 120041120A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHTSINOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714974 145161 EWR - FLIGHT 3424, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE GALLEY DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041207000712004120700071NM 2004 12 7 UPS04443506 120041118A3350 LAMP BOEING747 747123F NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 CREW SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED AS NEEDED, OPS CK OK. 2L74 4F A20WE 20041207000722004120700072NM 2004 12 7 UPS04543534 120041119A5610 HANDLE BOEING757 75724APF 1384969NM CAPT L2 WINDOW STIFF A IPXAK NONE O OTHER ININSP/MAINT 1 SO01454UP 25475 AFTER LANDING ON FIRST LEG, CAPT WINDOW UNLOCK HANDLE BECAME HARD TO MOVE SMOOTHLY. AT THE END OF SECOND LEG, HANDLE REQUIRES EXCESSIVE PRESSURE TO COMPLETELY UNLOCK. IT APPEARS THAT WHEN AIRCRAFT IS PRESSURIZED, IT HELPS BIND THE HANDLE. DEF NR D291605 ASSIGNED. ADJUSTED WINDOW IAW AMM 56-11-02-5. PLACARD REMOVED. 2L72 4F RTA2NM 20041207000752004120700075EA 2004 12 7 COMA0460646 120041127A2120601R9521171 DUCT CNDAIRCL600 CL6002B19 1900309EA LT ACM CRACKED A COMAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SO01798CA 7348 FLIGHT 5910 - DISPLAY COOL AND CABIN ALTITUDE CAUTION MESSAGE. REPLACED CRACKED AIR DISTRIBUTION DUCT IN AIR CONDITIONING SYSTEM. 2L72 4F RTA21EA 20041207000772004120700077NM 2004 12 7 USAA040877 120041016A53151135085 FLOORBEAM BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4, BEAM, ABOUT .5 INCH, CRACKED, FLOOR SUPPORT BEAM, STA 540 AND LT OB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-46819-4. 2L72 4F4 FRTA16WE E2GL 20041207000782004120700078NM 2004 12 7 USAA040876 120041020A53131122424 STRINGER BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4, STRINGER, .1250 INCH CRACK, STA 907, STR4L, AROUND FASTENERS. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-52988. 2L72 4F4 FRTA16WE E2GL 20041207000802004120700080NM 2004 12 7 USAA040772 120041026A5412 PRESSURE PANEL BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE NACELLE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 PIT, C-4, WEB, .5 INCH BY .4 INCH BY .025 INCH DEEP, CHAFED PRESSURE PANEL STATION 145 TOP OF PYLON WEB. INSTALLED DOUBLER IAW EA 95897. 2L72 4F4 FRTA2NM E12EU 20041207000812004120700081NM 2004 12 7 SB04159 120041127A2150 ODOR BOEING737 7373B7 1384580NM LT A/C PACK DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19385US 22958 PHL - FLT1227, EN ROUTE FROM BTV TO PHL, CREW REPORTED A STRONG OIL SMELL IN CABIN. CREW WAS ABLE TO ISOLATE SOURCE TO LEFT PACK/LEFT ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FAULT ISOLATION STEPS FROM MM 21-00-01, PROCEDURE 2. NO FAULTS CONFIRMED. NO UNUSUAL ODORS OR FUMES NOTED WHEN OPERATING LEFT PACK FROM LT ENGINE. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20041207000822004120700082EA 2004 12 7 COMA0460654 120041125A2752852D10021 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA RT TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01981CA 7163 FLIGHT 5454 - FLAPS FAILED CAUTION MESSAGE. REPLACED THE RT INBD FLAP ACTUATORS. 2L72 4F RTA21EA 20041207000842004120700084NM 2004 12 7 LCQ10 120041006A5346 FITTING DOUG MD80 MD83 3023681NM LT ENGINE PYLON CRACKED B K NONE O OTHER ININSP/MAINT 1 SO15932AS 49233 LEFT ENGINE PYLON SUPPORT BULKHEAD UPPER AND LOWER FITTING HAS CRACKS IN HORIZ FLANGE STA 1307. 2L72 4F RT 20041207000862004120700086WP 2004 12 7 UPS04843547 120041119A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 C3 LT WING CENTER L/E RIB CRACKED AT UPPER AFT END STA XW398. STOP DRILLED CRACK NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG2, 57-3-1, FIG4, 57-3-1 FIG2, 51-1-8. 2L74 4F RT4A25 20041207000872004120700087WP 2004 12 7 UPS04843548 120041119A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LEFT WING CENTER L/E RIB CRACKED AT XW408. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG 1, 57-3-1 FIG 4, 51-1-8, 51-1-20D, 51-1-21. 2L74 4F RT4A25 20041207000912004120700091NM 2004 12 7 USAA040843 120041107A5754 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 SKIN, .1250 INCH CRACKS, LOWER SURFACE AFT ROW OF RIVET, NR 5 SLAT IB TRACK AREA. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2L72 4F4 FRTA16WE E21EU 20041207000932004120700093NM 2004 12 7 USAA040874 120041103A5320 STIFFENER BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 STIFFENER, .1250 INCH CRACK, LBL 5.7 IB AND OB SIDE 8 INCH IN FROM BOTTOM. STRAPS, ANGLES AND FILLERS INSTALLED ON BOTH SIDES OF VERT CORD IAW EO 5300V155 AND EA 79321. 2L72 4F4 FRTA16WE E2GL 20041207000942004120700094NM 2004 12 7 USAA040844 120041112A52406545871523 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FWD SERVICE DOOR SKIN, .1875 INCH CRACK, UPPER HINGE CUTOUT, LWR RADIUS TO DRAIN HOLE. INSTALLED DOUBLER IAW TYP REP 52-10-13. 2L72 4F4 FRTA16WE E2GL 20041207000952004120700095EU 2004 12 7 AALA20041175 120041201A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2190070 513 SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT ROWS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041207000962004120700096EU 2004 12 7 AALA20041174 120041201A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2190070 513 LEFT 3 DOOR LOWER FLOOD LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT 3 DOOR LOWER FLOOD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041207000972004120700097WP 2004 12 7 AALA20041176 120041201A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217540A 49994 CABIN OVERHEAD EMERGENCY LIGHTS FORWARD OF AFT CABIN VAULT DOOR INOPERATIVE. REPLACED BATTERY PACK IN RIGHT HAND AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041207001002004120700100NM 2004 12 7 USAA040838 120041030A5240 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU39004 24934 ANGLE, 3 INCHES, CRACK, ANGLE, FWD SVC DOOR, INTERIOR STRUCTURE JUST BELOW WINDOW. REPLACED L ANGLE IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20041207001012004120700101NM 2004 12 7 USAA040862 120041028A53201128783 ANGLE BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 ANGLE, 4, DEEP WEAR MARKS, VERT SUPPORT Z, VERT OB LEG AT AFT LEG GEAR WELL CUTOUT CORNER. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-48690. 2L72 4F4 FRTA16WE E2GL 20041207001022004120700102NM 2004 12 7 USAA040828 120041013A53126549914535 TEE FITTING BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE PRESSURE BLKHD DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 STRINGER T FITTING, NO EDGE DISTANCE. NO EDGE DISTANCE FOR FASTENERS, FWD SIDE AFT PRESSURE BULKHEAD AT S10L. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-49914, DASH NR 535, EA 79074. 2L72 4F4 FRTA16WE E2GL 20041207001042004120700104NM 2004 12 7 USAA040864 120041025A5320 SKATE ANGLE BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 SKATE ANGLE, 11 INCHES LONG, EXCESSIVELY DEEP CHAFE MARK, 1104 TO 1121, STR 2 L. 2L72 4F4 FRTA16WE E2GL 20041207001072004120700107NM 2004 12 7 AALA20041179 120041202A3350 LIGHT BOEING757 7572Q8 1384972NM ROW 2AB INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21706TW 28165 AFT PORTION OF EMERGENCY FLOOR TRACK LIGHT AT 2AB INOPERATIVE. REPLACED EMERGENCY FLOOR TRACK LIGHT ASSEMBLY AT ROW 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041207001082004120700108NM 2004 12 7 USAA040884 120041012A53151128907 FLOORBEAM BOEING737 737301 138447RNM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FLOORBEAM, 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 30.5 BETWEEN STA 947.5 AND 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041207001092004120700109NM 2004 12 7 USAA040885 120041012A53201123578 FLOOR SUPPORT BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 FLOOR SUPPORT, 4 INCHES BY 1 INCH, CORROSION; LEVEL 1; TASK NR C53-107-02, RBL 17.61, STA 986.5 TO 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041207001112004120700111WP 2004 12 7 UPS04843512 120041027A534037798741 FITTING DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 END FITTING CRACKED ON L13L STA 840. REMOVED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DWG 3779874 FROM 7075-T6 PLATE ON SAA TRAVELER NR 0072. NDT C/W ON FINISHED PART PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-20D. 2L74 4F RT4A25 20041207001142004120700114NM 2004 12 7 USAA040866 120041111A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55422 22956 SKIN, 1.75 INCHES CRACKED AT STA 927 AND 947.5 AT STR 25R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E2GL 20041207001152004120700115WP 2004 12 7 UPS04843552 120041115A532056434332 ANGLE DOUG DC8 DC871F 302199DWP RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 VERTICAL STIFFENER CORRODED BEYOND LIMITS ON AFT SIDE OF WING REAR SPAR, RT W/W, STA 857 BULKHEAD XCW46. FABRICATED REPLACEMENT ANGLE FROM ACA41283 7075T6 EXT REF DWG 5643433. NDT PER DPS4.707, NO CRACKS NOTED. REMOVED AND REPLACED ANGLE PER SRM 51-1-21, 51-1-8, 51-3-0, 51-1-20D. FUEL LEAK CHECK GOOD ON UPS TC8000. 2L74 4F RT4A25 20041207001182004120700118WP 2004 12 7 IXXA0400081S 120040608A5330 PLATE DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AFT CENTER SECTION LWR PLATING CRACKED 1 INCH BETWEEN STA 1555.00 AND SB 1560.00. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8-53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21, PAGE 1. REMOVED DAMAGED AREA AND FABRICATED DOUBLER FINGER DOUBLER & FILLER, IAW DC8 SRM 53-2-1 FIG 2. CLEANED, TREATED AND PRIMED AREA, FILLER AND FINGER DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PAGE 9. INSTALLED DOUBLER, FILLER AND FINGER. 2L74 4F RT4A25 20041207001212004120700121WP 2004 12 7 IXXA0400087S 120040526A5310 DOOR FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FWD ACCY COMPT FRAME CRACKED 1" AT STA 55.000, 1-24R. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PAGES 1, 2. REMOVED DAMAGED FRAME IAW DC8 SRM AND ANGLE DOUBLERS IAW DC8 SRM 53-2-0 FIG 2 PAGE 1 OF 3. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PAGES 1-13-17. CLEANED, TREATED AND PRIMED AREA AND FRAME SEGMENT AND ANGLES IAW DC9 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED FRAME SEGMENT AND ANGLE DOUBLERS WITH NEW FASTENERS IAW DC9 SRM 53-2-0 FIG 2, DC8 SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D, PAGE 9 DC8 SRM 51-1-15 PAGE 1. 2L74 4F RT4A25 20041207001222004120700122WP 2004 12 7 IXXA0400089S 120040522A5754 SKIN DOUG DC8 DC871F 302199DWP TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP L/E UPPER PART HAS INTERIM REPAIR AT XE 415.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4. REMOVED PLATING WITH INTERIM REPAIR IAW DC8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING IAW DC8 SRM 57-7-4 FIG 4. CLEANED, TREATED AND PRIMED AREA AND PLAYING INTERNAL PART IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20041207001232004120700123WP 2004 12 7 IXXA0400090S 120040518A5200 ACCESS DOOR DOUG DC8 DC871F 302199DWP ZONE 100 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE (02 EA) INTERIM REPAIRS ON EXHAUST DOOR SYSTEM CORNERS AT STA 40,000 L-31L. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 53-2-0 FIG 13. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1-20D PAGE 21. FABRICATED DOUBLER IAW DC8 SRM 53-2-0 PAGES 69 AND 70 FIG 13. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-15 PAGE 1. INSTALLED DOUBLER WITH NEW FASTENERS IAW DC8 SRM 53-2-0 PAGES 69 AND 70, DC8 SRM 51-1-20D PAGE 9. 2L74 4F RT4A25 20041207001252004120700125WP 2004 12 7 IXXA0400092S 120040526A5753 SKIN PANEL DOUG DC8 DC871F 302199DWP TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING ROUTINE C CHECK INSPECTION, FOUND LT INBD FLAP HAS INTERIM REPAIR ON UPPER PLATING, STA XW 89.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 1. REMOVED UPPER PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 1. CLEANED, TREATED AND PRIMED INNER FACE OF NEW PLATING IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20041207001262004120700126WP 2004 12 7 IXXA0400088S 120040603A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP LWR PART SKIN HAS INTERIM REPAIR AT XF 320.00. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4 PAGE 2 OF 2. REMOVED LOWER PLATING WITH INTERIM REPAIR IAW DC8 SRM 51-1-21 PAGE 1. FABRICATED NEW PLATING IAW DC8 SRM 57-7-1 PAGE 2 OF 2 FIG 4. CLEANED, TREATED AND PRIMED NEW PLATING AND AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20041207001272004120700127NM 2004 12 7 HNAA0400087 120040928A7600V319 SWITCH DHAV DHC8 DHC8201 2809001NM ENGINE INOPERATIVE A HNAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA07998HA 509 NR 2 ENG TQ SURGE AFTER T/O. REMOVED AND REPLACED SWITCH 6141-S4, OPS CHECK GOOD. REMOVED AND REPLACED SWITCH 6141-S4 OPS CHECK GOOD. 2H72 4T RTA13NM 20041207001302004120700130NE 2004 12 7 C8GA20040012 220040717A7261 O-RING BOEING727 727225 1384077NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE LEAKING A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO15808EA 22439 666344 DURING CRUISE, THE NR 1 ENGINE LOSS OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE. REFERENCE AOM CHECKLIST FOLLOWED BY NR 1 ENGINE IN-FLIGHT SHUTDOWN, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATION IN KTOL WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND OIL LEAKING FROM GEARBOX DRAIN ON STARTER PAD. REPLACED THE NR 1 ENGINE STARTER DRIVE OIL SEAL AND O-RING IAW P&W MM 72-61-00. OPERATIONAL AND LEAK CHECK NORMAL DURING ENGINE RUN AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041207001312004120700131SO 2004 12 7 C2XA04SH554 120041117A321014571035413 BEARING CAP EMB 145 EMB145ER 3260211SO LT MLG SCRATCHED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C-CHECK, THE LEFT MAIN GEAR BEARING CAP WAS FOUND SCRATCHED IN THE BEARING TRACK. REPLACED THE AFFECTED CAP IAW 32-10-01. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTT00011AT 20041207001332004120700133SO 2004 12 7 C2XA04CL115 120041116A335066367 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 CLE FLIGHT NR 2266, THE CREW REPORTED THE AISLE PATH LIGHT STRIP AT ROW 7/8 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20041207001342004120700134NM 2004 12 7 SB04160 120041130A2170V1211 COALESCER BAG BOEING737 737301 1384611NM L/R PACKS CONTAMINATED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19577US 23742 DFW - FLT 1227 - EN ROUTE, THE CABIN CREW NOTED A STRONG ODOR/FUMES WHICH RESULTED IN PASSENGER COMPALINTS OF BURNING EYES AND HEADACHES. MAINTENANCE FOUND THE WATER SEPARATOR BAGS CONTAMINATED AND REPLACED THEM. 2L72 4F RTA16WE 20041207001352004120700135SO 2004 12 7 C2XA04SH562 120041128A532014521712005 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712122 145684 DURING C-CHECK, THE RIGHT HAND OMEGA BEAM WAS FOUND CORRODED AT FRAME 23. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-02. AIRCRAFT RETURNED TO SERVICE 2L72 4F RT 20041207001372004120700137SO 2004 12 7 C2XA04SH556 120041118A531014525480003 BEAM EMB 145 EMB145ER 3260211SO CARGO DOORWAY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C-CHECK, THE LOWER CARGO DOOR CUTOUT BEAM WAS FOUND CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTT00011AT 20041207001382004120700138SO 2004 12 7 C2XA04IA156 120041129A3230 LANDING GEAR EMB 145 EMB145 3260210SO MAINS MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713964 145123 IAH - FLIGHT 2964, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY TESTED THE LANDING GEAR RETRACTION AND EXTENSION SYSTEM SEVERAL TIMES WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041207001392004120700139EU 2004 12 7 DHL2004363519 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 3889, FS 26.5 - FS 33.5 RBL 78" MAIN CABIN SEAT TRACKS CORRODED BEYOND LIMITS PER A-300 SRM 51-40-11. CORRECTIVE ACTIN AS FOLLOWS, REMOVED SECTION OF SEAT TRACK FROM FS 26 TO FS 33 RT BL 78" IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 26.5 TO FS 33.5 AT RBL IAW A-300 SRM 51-10-10 / 51-10-40. TREATED, PRIMED AND APPLY POLYWHITE AS REQUIRED REF: A-300 SRM 51-40-10 AND A-300 SRM 51-40-12 MATERIAL USED, 60-22457, PO NR 24302234. 2L72 4F RTA35EU 20041207001412004120700141SO 2004 12 7 C2XA04IA152 120041128A3260 WARNING SYSTEM EMB 145 EMB145XR 3260214SO MLG FALSE ACTIVATIONA C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2723139 145731 CREW REPORTED A LANDING GEAR DISAGREE AFTER TAKEOFF WITH THE GEAR UP. AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE PERFORMED MULTIPLE GEAR SWINGS WITH NO DISCREPANCEY NOTED. AIRCRAFT RETURNED TO SERVICE 2L72 4F RT 20041207001422004120700142NE 2004 12 7 NACA20040035 220040914A7421RHB32E SPARK PLUG DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 18 CYLINDER CRACKED A NACAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL03779TA44 44 45529 28737 ABORTED TAKEOFF DUE TO NR 2 ENGINE LOW FUEL FLOW AND LOW BMEP. REPLACED NR 18 CYLINDER FRONT PLUG (CRACKED CERAMIC), NR 8 CYLINDER REAR INTERMITTENT, BOTH PLUGS REPLACED. REPLACED NR 18 CYLINDER REAR PLUG. INSPECTED CARBURETOR AND FIRE WALL SHUT OFF FOR RIGGING. PERFORMED BARO RUN, ALL CHECKED GOOD. PERFORMED WET TAKEOFF RUN, DRY TAKEOFF RUN, ALL CHECKED GOOD. NEVER GOT LOW FUEL FLOW. 2L74 4R4 R A781 5E8 20041207001432004120700143CE 2004 12 7 62453 120040623A5220 HANDLE BEECH 1900 1900D 1154162CE EMERGENCY EXIT UNSECURE A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07173YV UE173 CREW NOTICED EMERGENGY EXIT HANDLE STICK OUT WAY FROM FUSELAGE MX RESEATED EXIT. REMOVED AND INSP LT EXIT DOOR REINSTALLED AND SECURED. 2L72 4T RTA24CE 20041207001442004120700144 2004 12 7 65497 420041001A3420 INDICATOR BEECH 1900 1900D 1154162CE COCKPIT MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07142ZV UE142 CAPT ADVISED FMN OPS THAT THE CAPT SIDE NAV WAS NOT DISPLAYING NAV DATA, CAPT ADVISED BY MX CTL TO RETURN TO FIELD FMN. A/C LANDED FMN WITH NO FURTHER INCIDENT. COULDN'T DUPLICATE DISCREPANCY, OPS CK NORMAL 2L72 4T RTA24CE 20041207001462004120700146WP 2004 12 7 USAA0480517 120040928A534059360281 FITTING DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, AFT BILLIE BATH TUB FITTING TO BULKHEAD STA 1003, LONG 30, HAS AREAS OF CORROSION ON FORWARD INSIDE OF FITTING. REMOVED DAMAGE, SPOT FACED FASTENER HOLES, TREATED AND PRIMED, SEALED AND APPLIED CORROSION INHIBITING COMPOUND IAW EA 5340-01132 AND EA 10588. 2L72 4F4 FRTA6WE E9NE 20041207001482004120700148NE 2004 12 7 NACA20040036 220040914A7322PR58E5 CARBURETOR DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE MALFUNCTIONED A NACAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL03779TA2672 2672 45529 28737 ABORTED TAKEOFF DUE TO LOW FUEL FLOW AND LOW BMEP. BARO ENGINE CHECK SHOWED NORMAL PARAMETERS. REPLACED NR 2 ENGINE CARBURETOR AND FUEL FEED VALVE. CHECKED GOOD. 2L74 4R4 R A781 5E8 20041207001502004120700150CE 2004 12 7 DXTA200400387 120040908A2121125027025 FAN CESSNA750 750 2076810CE CABIN FAILED E DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07903QS1211 7500162 DURING MAINTENENCE NOTICED A STRONG INSULATION BURNING ODOR IN THE CABIN, COMING FROM THE AFT CLOSET AREA. ACCESSED ELECTRICAL EQUIPMENT IN AFT CLOSET, PULLED BREAKERS FOR AIRSHOW, INVERTER, AUDIO AMP AND CABIN MODULE SMELL STILL THERE. ACCESSED BAGGAGE FAN FOUND NOT CAUSE OF SMELL, FOUND WEMAC BOOST FAN TO BE THE CAUSE OF THE ELECTRICAL SMELL, MOTOR OPERATING SLOW AND NOISY. REMOVED AND REPLACED FAN IAW CESSNA 750 MM CHAPTER 21-21-00. 2L72 4J RTT00007WI 20041207001522004120700152NM 2004 12 7 DHL2004780501 120040909A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK, COMPLIED WITH FCD03643 COOPER VEIN. REMOVE AFT AIRSTAIR IN FLIGHT LOCK ASSY IAW SRM 51-30-02. FABRICATE REPAIR DOUBLER IAW B727 SRM 53-30-3 USING 2024-T3 X .063 ALUMINUM. ALODINE IAW B727 SRM 51-10-2. PRIME IAW BOEING SOPM 20-41-2. INSTALL DOUBLER IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041207001532004120700153NE 2004 12 7 NACA20040040 220040927A7322891085 CARBURETOR DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE POWER LOSS A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL032907F2 2 533265 CP450668 NR 2 ENGINE SHUT DOWN DUE RUNNING ROUGH, HIGH FUEL FLOW, LOW BMEP AND COLD CHT. REMOVED AND REPLACED NR 2 ENGINE CARBURETOR. OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20041207001552004120700155SO 2004 12 7 GLBA20030673 120040713A2150 A/C PACK EMB 120 EMB120ER 3260203SO RIGHT FAILED A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM03293UX 120293 ON TAXI, CABIN FILLED WITH SMOKE AND RT PACK FAILED, PERFORMED GROUND CK OF PACK SYS, OPS CK GOOD. 2L72 4T RTA31SO 20041207001562004120700156WP 2004 12 7 UPS04843545 120041118A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING CENTER L/E LOWER RIB CRACKED AT AFT END, STA XW408. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR DOUBLERS FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-3-1 FIG 4, 57-2-0, 57-3-1, 51-1-21, 51-1-20D. 2L74 4F RT4A25 20041207001572004120700157SO 2004 12 7 C2XA04IA160 120041127A26123601133500230 FIRE LOOP EMB 135 EMB135LR 3260305SO NR 1 ENGINE DIRTY A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW27125281328513285 145504 IAH - FLIGHT 3439, MEM TO IAH, THE CREW REPORTED THAT THE ENGINE ONE FIRE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT AT LOW POWER SETTINGS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. DISCONNECTED, CLEANED AND RE-CONNECTED THE NUMBER ONE ENGINE FIRE LOOP. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041207001592004120700159WP 2004 12 7 DHL2004809007 120040921A292357155A PUMP DOUG DC8 DC873F 302199FWP AUX HYD SYSTEM FAILED A DHLAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01809DH 46047 HYD AUX PUMP QUIT DURING PREFLIGHT VAPOR AND SMOKE IN WHEEL WELL. REPLACED AUX HYD PUMP ASSY AS PER MM 29-20-2. 2L74 4F RT4A25 20041207001602004120700160EU 2004 12 7 SA04110 120041126A335032145410 EPSU AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19116US11354 1210 THE RIGHT SIDE MID-CABIN EMERGENCY POWER SUPPLY UNIT INDICATED INOP WHEN IT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE MID-CABIN, RIGHT SIDE, EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041207001612004120700161SO 2004 12 7 C2XA04CL116 120041116A3350B6245305 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716927 145006 DURING ROUTINE MAINTENANCE, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY. 2L72 4F RTT00011AT 20041202001982004120200198NM 2004 12 2 UPS04243231 120040929A5755651734863 PANEL BOEING727 72722C 138400FNM NR 8 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01930UP 19096 INSPECTION TYPE:N/A NR 8 GROUND SPOILER CENTER HINGE BOTTOM S/M PANEL DELAMINATED. REMOVED AND REPLACED NR 8 GROUND SPOILER PER MM 27-62-01. OPS CHECK NORMAL. 2L73 4F A3WE 20041202002002004120200200NM 2004 12 2 UPS04643214 120040925A2560 SMOKE GOGGLES BOEING767 76734AF 1385212NM COCKPIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01310UP 27762 INSPECTION TYPE:N/A, F/O SMOKE GOGGLES CRACKED. REMOVED & REPLACED F/O'S SMOKE GOGGLES. 2L72 4F RTA1NM 20041202002092004120200209CE 2004 12 2 60182102504 120041025A3231AN9014A WASHER LEAR 60 60LEAR 5170707CE SHUTTLE VALVE CRUSHED E J7SAA UNSCHED LANDING JKSWARNING INDICATION FLUID LOSS AFFECT SYSTEMS CLCLIMB 1 SW05245FX 182 "LOW HYD PRESS" WARNING MSG ILLUMINATED IN FLIGHT JUST AFTER TAKEOFF (FROM DEN) FOR BOTH 1/2 SYSTEMS. CREW DIVERTED TO ICT FOR RUNWAY LENGTH AND MX AVAILABILITY. EMERGENCY DECLARED AND PROCEDURES FOLLOWED FOR EMERGENCY GEAR EXTENSION AND BRAKE ACTIVATION. ON ROLLOUT, NR 1 AND NR 2 MAIN TIRES BLEW OUT. SUBSEQUENTLY FOUND NR 3 MAIN DEFLATED. A CRUSH WASHER P/N: AN901-4A ON THE LEFT HAND MAIN LANDING GEAR INBOARD DOOR ACTUATOR SHUTTLE VALVE WAS DISCOVERED TO BE BLOWN OUT. PICTURES OF THE WASHER HAVE BEEN REQUESTED. NO SIGNS OF METAL CONTAMINATION ARE PRESENT IN THE HYDRAULIC FLUID. TWO PUMPS HAVE BEEN PLACED ON ORDER, ALONG WITH NEW FILTERS. NO EVIDENCE OF METAL CONTAMINATION IN THE FILTERS. 2L72 4F RTA10CE 20041202002122004120200212NM 2004 12 2 UIA9315 120040913A5330 SKIN DOUG MD90 MD9030 3023690NM FUSELAGE CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017916 53539 DURING S90M C CHECK OF DATUM A/C 1. REPAIR ON THE RT FUSELAGE SKIN AT STA Y=484,L18R-L19R (526). CORROSION ON LE WING REAR SPAR LOWER CAP AT STA XRS510 AND XRS 550(527).3.A CRACK DAMAGE ON RT FUSELAGE SKIN (P/N:5910228-259) BETWEEN CANTED STA 1520-1531 (529).4.CORROSION ON FUSELAGE FRAME LOWER T-CHORD AT STA Y=1437,BETWEEN L-29R AND L-28R (530). 5.CORROSION ON RT OUTBD FLAP INBD VANE(P/N:5930496-510) TRAILING EDGE LOWER SURFACE (533). 6.TWO AREAS DAMAGE WITH CRACK AND OIL-CANNING ON LT FUSELAGE SKIN BETWEEN CANTED STA 1520-1531(537). 7.REPAIR ON FUSELAGE SKIN AT STA Y=434(538). 8.CRACKS ON DOUBLER AND CAP OF FUSELAGE BULKHEAD AT CANTED STA 1520L-3L(539).9.REPAIR ON FUSELAGE SKIN 2L72 4F RTA6WE 20041203000242004120300024NM 2004 12 3 HNAA0400167 120041130A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSLEAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 DURING C CHECK, FOUND WIDESPREAD CORROSION ON STR 31 STARBOARD. CUT STR 31 STARBOARD AND HFEC BOND CHECK STR 31. INSTALLED NEW STR 31 STARBOARD. 2H72 4T RTA13NM 20041203000272004120300027NM 2004 12 3 L0FR200400009 120041118A3246260356116 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041203000292004120300029NM 2004 12 3 L0FR200400001 120041117A3246260356116 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA 2L74 4F RTA20WE 20041203000382004120300038NM 2004 12 3 WLDA200499 120041103A5310 SHEAR TIE DOUG MD11 MD11 3023602NM FUSLEAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 DURING C2-CHECK INSPECTION, FOUND SHEAR TIE CORROSION AT STA 1741 BETWEEN L51L TO L51R. CUT OUT THE CORROSION AREA AND MADE REPAIR PARTS PER SRM 53-30-00 VOL 1 FIG 5. PERFORMED NDT INSP NO DEFECT FOUND. INSTALLED REPAIR PARTS PER MD11 SRM 51-33-01 VOL II REV35 AND APPLIED PROTECTION COATING. 2L73 4F RTA22WE 20041203000542004120300054CE 2004 12 3 GLBA20030756 120041106A5530 BRACKET BEECH 1900 1900D 1154162CE VERTICAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03122UX UE122 LT SIDE OF VERT STAB TO FUSELAGE L BRACKET CRACKED. REPAIRED CRACK IAW B1900 SRM 51-70 AND EO 04-UE122-01. 2L72 4T RTA24CE 20041203000612004120300061WP 2004 12 3 UPS04843507 120041118A3350 BATTERY DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 EMERGENCY BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW DC-8 AMM 30-50-01. OPS CK GOOD. 2L74 4F RT4A25 20041203000652004120300065NM 2004 12 3 04FDEA03145 120041117A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 16L EXCEEDED LIMITS. REPAIRED PER FEDEX EA 1-5510-79789, HORIZONTAL STABILIZERS BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000 2L73 4F RTA22WE 20041203000732004120300073NM 2004 12 3 04FDEA03154 120041118A5510 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 34R. EXCEEDED LIMITS AFTER CORROSION REMOVAL. REPAIRED PER FEDEX EA 1-5510-79789. 2L73 4F RTA22WE 20041203000742004120300074EU 2004 12 3 IXXA0400119O 220041107A72619026M70G01 ENGINE DOUG DC8 DC873F 302199FWP CFMINTCFM56 CFM562AFR 13802EU NR 4 MALFUNCTIONED A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW11603AL936871777 46003 692515 DURING TAKEOFF, NR 4 ENGINE OIL PRESSURE FLUXING 45-35PSI WITH OIL QUANTITY DROPPING SHUT DOWN ENGINE WINDMILLING OIL PRESSURE OPSI AT 1302 (LANDING WEIGHT 270.0) AN INSPECTION IS ON GOING. AS SOON AS INFORMATION BECOME AVAILABLE IT WILL BE PROVIDED. 2L74 4F4 FRT4A25 E21EU 20041203000862004120300086WP 2004 12 3 2004000012 120041004A5101 FLOOR PANEL DOUG DC10 DC1030 3023501WP CABIN OVERHEATED A CNMAJA DUMP FUEL UNSCHED LANDING M OVER TEMP CLCLIMB 1 SW0717085 47957 EXCESSIVE HEAT COMING FROM FLOOR AND WALL FORWARD AND AFT OF L-2 DOOR. TROUBLESHOOTING AS OF 10/5/04. 2L73 4F A22WE 20041203000882004120300088EU 2004 12 3 TXER097638 120040927A6710C761A2024104 COLL PITCH CNTR UROCOPEC120 EC120B 8680987EU COCKPIT BINDING B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09131MB524 1070 COLLECTIVE BINDING . 1G72 3U NCR0001RD 20041203000982004120300098EU 2004 12 3 226121 120040930A7931 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENG OIL ILLUMINATED A UHLAO OTHER J WARNING INDICATION APAPPROACH 1 GL1719XS 340A019 122 ON 09-30-04 APPROX 2105 (UTC), FLT 7891 IAD-ORF, DURING APPROACH, CREW OBSERVED RT ENGINE OIL LIGHT ON THE CWP AND NOTICED A OIL PRESSURE AROUND 30 PSI. FLIGHT LANDED WITHOUT INCIDENT. 2L72 4T4 TRTA52EU E8NE6 20041203001012004120300101EU 2004 12 3 CX7A194J0453 120041017A54157254501831 COWLING SAAB SF340 340B 7860101EU ENGINE DEPARTED A CX7AO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 GL03309CE 340B201 PORTION OF ENGINE COWLING DEPARTED A/C DURING FLIGHT. INSTALLED UPPER COWL FAIRING. 2L72 4T RTA52EU 20041203001022004120300102EU 2004 12 3 XNOA1202 120041016A2910 O-RING AIRBUS300 A300B4203 3930306EU HYD MANIFOLD LEAKING A XN0AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23370PC 134 DEPARTURE KSEA GREEN HYDRAULIC SYSTEM QUANTITY WENT TO "0" RETURN TO KSEA. REMOVED AND REPLACED O-RING ON PRESSURE PLUG OF GREEN HYDRAULIC MANIFOLD, OPS AND LEAK CHECK GOOD I/A/W A300 AMM 29-10-00 AND 20-23-16. 2L72 4F RTA35EU 20041203001052004120300105CE 2004 12 3 CWQR2004001 120040826A289765782323 WIRE HARNESS CESSNA CESSNA500 560CESSNA 2076750CE FUEL QTY TRANSM BURNED B DXTRK NONE O OTHER ININSP/MAINT 1 GL05340QS 1484A 5600514 DURING INSPECTION, FOUND LEFT WING OUTBOARD FUEL QUANTITY TRANSMITTER WIRING HARNESS INSOLATION BURNT BETWEEN WIRE SHIELDING AND TERMINAL. FILED SERVICE CONDITION REPORT NR 161570 WITH CESSNA/CITATION. COPY OF REPORTS, SUPPORTING DOCUMENTATION AND PICTURES SENT TO PMI AND OPERATOR. 2L72 4F RTA22CE 20041203001062004120300106NE 2004 12 3 NACA20040031 220040831A8510 CASE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE NOSE LEAKING A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03779TA108 108 45529 P33192 NR 1 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL LOSS. REPLACED NR 1 ENGINE NOSE CASE ASSEMBLY DUE TO A BLOWN ACCESSORY PLUG. 2L74 4R4 R A781 5E8 20041203001092004120300109SO 2004 12 3 CHQA000556 120040914A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11561 145447 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT HAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-54-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041206000192004120600019NE 2004 12 6 HNAA0400126 220041019A7320789846009 ECU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE FAULTY A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA07846EX9174 195 326 120585 FLIGHT NR 3937 OUT OF SWF REPORTED, THE NR 1 ENGINE CONTROL UNIT FAILING AND THE TORQUE DROPPING TO 49 PERCENT AS THEY WERE CLIMBING THROUGH 5000 FT. CREW BEGAN THE ABNORMAL CHECKLIST AS THE TORQUE CONTINUED TO DROP TO ZERO. THE NR 1 ENGINE WAS SHUTDOWN, AN EMERGENCY DECLARED, AND THE CABIN PREPPED FOR AN EMERGENCY. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ECU, FUEL PUMP, AND HYDRO MECHANICAL UNIT. AIRCRAFT WAS GROUND RUN. ALL SYSTEMS CHECK GOOD AT ALL POWER SETTINGS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20041206000222004120600022EU 2004 12 6 DHL2004363531 120040922A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3765, MAIN CABIN INTERIOR FLOOR SEAT TRACK HAS SEVERAL SPOTS OF CORROSION BETWEEN FS 40 AND FS 53 AND RBL 36 SEAT TRACK FLANGES. REMOVED ALL SURFACE CORROSION POINTS FROM SEAT TRACK FLANGES AT MAIN CARGO CABIN BETWEEN FS 41 AND FS 53 RBL 36 IAW A-300 SRM 51-40-11. MATERIAL LOSS .002 AREA WITHIN LIMITS IAW A-300 SRM 53-10-00. FOUND TRACK BETWEEN FS 46 AND FS 48 TO BE OUT LIMITS IAW A-300 SRM 53-10-00. REPAIRED DAMAGED SECTION FROM FS 44.5 TO FS 48.5 RBL 36 IAW A-300 SRM 53-10-10 FIG 721, MAT. USED 60-22457, PO NR 24302234, SEAT TRACK 2024-0, .080 INCH PO NR 2409. 2L72 4F RTA35EU 20041206000242004120600024NM 2004 12 6 DHL2004780504 120040909A5720 BRACKET BOEING727 727223 1384074NM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE FLORIDA, THE FOLLOWING DISCREPANIES WERE NOTED; LT WING L/E CAVITY WS 301 HAS NR 1 KRUGER FLAP ACT OB LOWER MOUNT BRACKET CORNER CRACKED. REMOVED BRACKET, FABRICATED NEW ONE (BRACKET) FROM 7075T6 .063 PO NR 900861 DIM 7' X 3 1/2" AND TREATED, PRIMED AND INSTALLED BRACKET IAW B727 SRM 51-40-3, 51-10-2 AND 51-30-2 2L73 4F A3WE 20041206000282004120600028 2004 12 6 2004000014 420041015A25655WD230102300 SLIDE DOUG DC10 DC1030 3023501WP L-3 DOOR FAILED A CNMAK NONE L NO TEST ININSP/MAINT 1 SW07720AX 48252 L-3 SLIDE/RAFT DID NOT FULLY DEPLOY DURING ACCOMPLISHMENT OF OMNI AIR WORKCARD 101C-744 (FUNCTIONAL CHECK OF SLIDE/RAFT FOR C-CHECK REQUIREMENTS) SLIDE/RAFT ASPIRATOR PART NUMBER 31002-201 SEPARATED FROM RAFT DUE TO IMPROPER INSTALLATION OF RETAINING RING. 2L73 4F A22WE 20041206000302004120600030NM 2004 12 6 HNAA0400156 120041025A3231 DOOR DHAV DHC8 DHC8102 2809003NM LT MLG OUT OF ADJUST A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07912HA 040 AFTER GEAR RETRACTION LEFT MAIN GEAR DOOR LT CAME ON AND VISUALLY CONFIRMED DOOR OPEN. DUE TO THE AIRSPEED RESTRICTION, A/C RETURNED TO PHL. A/C WILL FERRY TO SBY FOR REPAIRS. ADJUSTED LEFT FWD GEAR DOOR. GEAR SWINGS, OP'S CHECK GOOD. 2H72 4T RTA13NM 20041206000322004120600032NM 2004 12 6 F3LA200400095 120040916A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTED REPORTED FLOORBEAM AT STA 967, LBL 42, CORRODED AT FLOOR PANEL SCREW NUT PLATE. FOUND FLOORBEAM TO BE CORRODED BEYOND LIMITS PER SRM 53-60-51. REMOVED DAMAGED AREA, FABRICATED REPAIR SECTION AND REPAIR PARTS AND INSTALLED PER SRM 53-00-51, 51-20-01 AND 20-41-02. 2L72 4F RTA16WE 20041206000462004120600046CE 2004 12 6 66220 120041028A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07133YV UE133 ON TAXI RIGHT BRAKES FELT SPONGY. BLED BRAKES AND SERVICED FLUID. 2L72 4T RTA24CE 20041206000522004120600052WP 2004 12 6 WLDA200491 120040905A5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO1114075 46922 DURING "B4" CHECK IN BYH, FOUND RBL30 F/S 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL RBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01. 2L73 4F4 F A22WE E23EA 20041206000872004120600087EU 2004 12 6 DHL2004363522 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL, AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3881, LBL 18, FS18 TO FS 30 SEAT TRACK MAIN CABIN CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 18 TO FS 30 LBL 18 IAW A-300 SRM 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FS 18 TO FS 30 AT LBL 18 IAW A-300 SRM 53-10-10 / 51-10-40. TREAT / PRIME AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND A-300 SRM 51-40-12. 2L72 4F RTA35EU 20041206001032004120600103EU 2004 12 6 XN0A1198 120040911A3242 BRAKE AIRBUS300 A300B4203 3930306EU MLG LOCKED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23474AS 219 BRAKES LOCKED UP ON TAXI. 2L72 4F RTA35EU 20041206001072004120600107NM 2004 12 6 UIA9316 120040917A5730 SKIN DOUG MD90 MD9030 3023690NM RT WING CORRODED Z K NONE O OTHER ININSP/MAINT 1 TW0017911 53535 DURING C06 CHECK OF DATUM, A/C FOUND SEVERAL CORROSION ON UPPER SKIN (P/N:59305002-150) OF RT WING AT STA XRS=282. 2L72 4F RTA6WE 20041207000062004120700006EA 2004 12 7 COMA0460657 120041201A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ACTIVATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01977CA 7157 FLIGHT 5890 - FLAPS FAILED CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20041207000292004120700029NM 2004 12 7 USAA040840 120041104A5312 BULKHEAD BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU 24934 C3, BULKHEAD WEB, 3 CRACKS, .1250 INCH, FPBH BS 178, RBL 6, WL 210 AND 213. DOUBLER INSTALLED IAW EO 5300V153. 2L72 4F4 FRTA16WE E21EU 20041207000352004120700035NM 2004 12 7 USAA040837 120041019A5753 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE LT WING FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US54103 22958 PIT - C4, IB AFT FLAP SKIN, 3 INCHES X 2.5 INCHES AREA, DELAMINATION. IB AFT FLAP OB T/E LT WING. REMOVED DELAMINATION, INSTALLED REPAIR CORE, SKIN AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041207000462004120700046 2004 12 7 EM04023 420041127A2565 GIRT BAR EMB ERJ170ERJ170100 EU LT DOOR SLIDE DETACHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818MD 17000039 FLIGHT 1625, DFW TO PIT - LEFT PASSENGER DOOR GIRT BAR OUT OF CLIPS, UNABLE TO CLOSE DOOR. THE EMERGENCY SLIDE DID NOT DEPLOY. MAINTENANCE, REATTACHED GIRT BAR AND PERFORMED OPERATIONAL CHECK OF THE DOOR. 2L74 4F RTA56NM 20041207000642004120700064NM 2004 12 7 USAA040882 120041019A57431100302 FITTING BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT WING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4, FITTING, 1 INCH BY .5 INCH AREA, CORROSION; NO LEVEL OR TASK. RT WING AFT SPAR OB BUSHING BORE FTG WALKING BEAM HANGAR LUG AT STA 202. REMOVED AND REPLACED FITTING IAW MFG DWG 6545321 AND SRM 51-20-25. 2L72 4F4 FRTA16WE E2GL 20041207000702004120700070EU 2004 12 7 SA04109 120041125A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHTSFAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19717UW14594 1069 PHL - THE EMERGENCY LIGHT SYSTEM FAILED TEST WITH MESSAGE,"EPSU UNIT EMER L". MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BELOW THE LEFT EMERGENCY OVERWING DOOR. OPERATIONALLY TESTS OK. 2L72 4F RTA28NM 20041207000792004120700079NM 2004 12 7 USAA040770 120041026A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 CLT, C-4, FLOORBEAM, SEVERAL .5 INCH AREAS, CORROSION LEVEL 2, STA 365, BL0 TO RBL12. INSTALLED TEE CAP REPAIR IAW SRM 53-00-51. 2L72 4F4 FRTA2NM E12EU 20041207000882004120700088WP 2004 12 7 UPS04843549 120041027A532056423421 SUPPORT DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 RT FUSELAGE FLAP HINGE SUPPORT FITTING CRACKED. DISSASEMBLED FLAP BUSS DRUM ASSY TO FOM PER MM27-51-06. REMOVED AND REPLACED SUPPORT ASSEMBLY REF SRM 51-1-21, 51-1-20D, 51-3-0 51-1-8, 51-1-15. REASSEMBLED AND RIGGED FLAP BUS PER 27-51-06. OPS CHK GOOD. 2L74 4F RT4A25 20041207000982004120700098NM 2004 12 7 SB04157 120041123A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 7 INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19584US 23743 PHL - PILOT REPORTED THE SEAT LEVEL EMERGENCY LIGHT AT SEAT ROW 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 7. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041207000992004120700099NM 2004 12 7 USAA040831 120041001A57536546431279 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT OB FOREFLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19775AU38669 24933 TOP SKIN, CORE BOND, 2 INCH SQUARE AREA, DELAMINATION. LT OB FOREFLAP TOP SKIN SURFACE ON IB T/E. INSTALLED NEW CORE AND TOP DOUBLER, SEAL AND REFINISH IAW SRM. 2L72 4F4 FRTA16WE E21EU 20041207001052004120700105NM 2004 12 7 USAA040867 120041111A5330 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 SKIN, 1.5 INCH CRACK, STA 727D AT STR 23 RT. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E21EU 20041207001102004120700110NM 2004 12 7 USAA040883 120041018A53131710030 STRINGER BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 STRINGER, 6 INCHES FULL WIDTH AND SIDES, CORROSION; LEVEL 1; TASK NR C53-208-01, STR 27 R JUST FWD OF FRAME, STA 1006. CUT STR REPAIR SECTION TO FIT AND INSTALLED REPAIR IAW 53-00-03. 2L72 4F4 FRTA16WE E2GL 20041207001122004120700112NM 2004 12 7 USAA040886 120041012A5320 SUPPORT BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 SUPPORT, 5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 25 BETWEEN STA 947.5 AND 967. 2L72 4F4 FRTA16WE E2GL 20041207001172004120700117 2004 12 7 C8GA20040023 420041008A3414 PITOT HEAD BOEING727 727225 1384077NM FUSELAGE BIRD STRIKE A C8GAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SO15801EA 22432 FLT 717 FORM KELP TO KSTL, ABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON THE CAPTAIN AIRSPEED INDICATOR. AIRCRAFT RETURNED TO BLOCKS AND UPON INSPECTION FOUND A BIRD STRIKE ON THE CAPTAIN PITOT PROBE. REMOVED FEATHERS AND PERFORMED A BIRD STRIKE INSPECTION WITH NO DEFECTS NOTED AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20041207001202004120700120WP 2004 12 7 IXXA0400086S 120040513A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP UPPER SKIN HAS INTERIM REPAIR AT STA XF 282.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 51-1-0 PG 1 DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED RT OUTBD FLAP FWD UPPER PLATING WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-121 PG 1. FABRICATED NEW UPPER PLATING IAW DC8 SRM 57-7-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND PLATING INTERIOR IAW DC8 SRM 51-1-8B. INSTALLED NEW UPPER PLATING IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20041207001282004120700128CE 2004 12 7 DELA20040003 120040831A26974299100 CONNECTOR LEAR 55 55LEAR 5170702CE FIRE LOOP FAULTY E DELAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 CE03903JC 081 DURING TAXI, THE LEFT FIRE T- HANDLE AND MASTER WARNING LIGHTS BEGAN FLASHING. T/S REVEALED FAULTY (OPENS) IN 2 CONNECTORS IN THE FIRE DETECTION ELEMENT HARNESS. TWO EA CONNECTORS WERE REPLACED WITH NEW UNITS AND F/T SATISFACTORY. 2L72 4F A10CE 20041207001292004120700129CE 2004 12 7 62795 120040705A3297 WIRE BEECH 1900 1900D 1154162CE MLG HANDLE DAMAGED A AMWAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07155ZV UE155 AFTER TAKEOFF, GEAR HANDLE WAS PLACED IN UP POSITION. LANDING GEAR INTRANSIT LIGHTS AND AURAL HORN DID NOT EXTINGUISH AIRCRAFT RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. REPAIRED BROKEN WIRES AT TB152 AND REPAIRED BAD SPLICES AT A406 PCB. PERFORMED LANDING GEAR, OPS CK NORMAL. 2L72 4T RTA24CE 20041207001322004120700132EU 2004 12 7 XNOA1199 120040915A3242 SEAL AIRBUS300 A300B4203 3930306EU RT BRAKES DAMAGED A XN0AD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL23474AS 219 ON TAXI, RIGHT BRAKES GRABBED, PULLING PLANE TO RIGHT. REMOVED NR 3 MWA FOR INSP. FOUND SNAP RING SEAL, SEAL SPACER DAMAGED. REMOVED AND REPLACED SNAP RING SEAL, SPACER AND BEARINGS ASSY. ANTI-SKID TEST OK PER MM REF 32-42-00. 2L72 4F RTA35EU 20041207001362004120700136SO 2004 12 7 C2XA04TY176 120041122A531114523160409 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714933 145018 DURING C CHECK, THE FASTENER HOLES AT FRAME 61, STRINGER 11R WHERE FOUND DAMAGED. INSTALLED A REPAIR DOUBLER IAW 51-40-02 AND CMP 51-21-04/05. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTT00011AT 20041207001472004120700147CE 2004 12 7 DJFA2004018 120040811A3610 SEAL CESSNA650 650 2076802CE BLEED AIR LEAKING E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23311CW 6500011 DURING CLIMB, THE NR 1 ENGINE FIRE LIGHT CAME ON. THE CREW RETARDED THE THROTTLES AND THE LIGHT WENT OUT. THEY RETURNED TO THE DEPARTURE AIRPORT WITH NO PROBLEMS. THE FIRE LIGHT WAS CAUSED BY A BLEED AIR LEAK. THE SEALS WERE CHANGED AND GROUND RUNS WERE SATISFACTORY. 2L72 4F A9NM 20041207001492004120700149EA 2004 12 7 4025 220041022A7310 LINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MCAULY3DF36CB3DF36C526 GL FUEL INJECTION FAILED E BSYAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL073547C 318052018 L549661A 992255 ON TAKEOFF OUT OF TAMPA, ENGINE STARTED SURGING, RETURNED TO TPA. MAINTENANCE FOUND RUBBER PIECES IN FUEL INJECTION UPPER DECK LINE, CLEANED UPPER DECK AND CHANGED RUBBER HOSES, OPS CHECKS GOOD. 1L72 3O3 O A20SO E14EA 5 C 20041207001512004120700151SO 2004 12 7 C2XA04IA157 120041127A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714143 145739 IAH - DURING MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE CEILING EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20041207001622004120700162NM 2004 12 7 DHL2004743006 120040901A361024366100 SEAL BOEING727 727225 1384077NM BLEED AIR FAILED A DHLABEA EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01743DH 22438 LOWER AFT BODY OVERHEAT LIGHT ILLUM INFLIGHT. ABNORMAL PROCEDURE COMPLETED, DECLARED AN EMERGENCY AND DIVERTED TO MEM. REMOVED AND REPLACED SEALS P/N 24366-100 ON PURGE VALVE AIR SUPPLY TUBE AFT OF PRECOOLER VALVE ON RIGHT SIDE. RESECURED SLIPPED PNEUMATIC BOOT ON BLEED DUCT BELOW PRECOOLER VALVE. RAN NR 3 ENG IAW JRH 5.2. OPS CHECK. 2L73 4F A3WE 20041207001632004120700163SO 2004 12 7 C2XA04SH561 120041128A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712122 145684 DURING C CHECK, THE LEFT HAND OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041207001652004120700165WP 2004 12 7 DHL2004801535 120040904A5754 SKIN DOUG DC8 DC873F 302199FWP LE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT OUTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 CTR PART (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 4, TR NR 57-94. REMOVED WORN PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PLATING (AL 2024-T3 0.063) IAW SRM 57-7-1 PG 2 FIG 4. CLEANED, TREATED AND PRIMED AREA AND PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1, SRM 51-1-15 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20041207001662004120700166WP 2004 12 7 IXXA0400110O 120041001A2133 OUTFLOW VALVE DOUG DC8 DC862F 3021972WP CABIN PRESSURE MALFUNCTIONED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW1171CX 651141407 45961 AFTER TAKEOFF LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL250 AND RIGHT PACK OFF. RIGHT PACK CONTROL VALVE WILL NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL 250 AND LEFT PACK OFF. CREW RETURNED AIRCRAFT TO PHIK AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING AND INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. 2L74 4F 4A25 20041207001672004120700167NM 2004 12 7 DHL2004760008 120041002A2612 FIRE WARNING BOEING727 7272B7 138407LNM CARGO BAY FALSE ACTIVATIONA DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01760AT 21954 CARGO AFT FIRE WARNING LIGHT AND GLARE SHIELD CARGO FIRE LIGHT ILLUMINATED ON GROUND. TRANSFERRED TO DMI NR 18022 IAW B727MEL 26-19 CAT C PLACARDS INSTALLED. CHECKED LOWER CARGO FIRE DETECTOR SYSTEM IAW B 727 M/M 26-10-00. NO FAULTS FOUND. OKAY FOR CONTINUED SERVICE. DMI 18022 CLEARED. PLACARD REMOVED. 2L73 4F A3WE 20041207001682004120700168WP 2004 12 7 DHL2004801524 120040904A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 7 TRACK PLUG LUGS WORN, STA 210.000. REMOVED WORN PLUG IAW DC8 SRM 51-3-0 PG 1-2. FABRICATED NEW TRACK PLUG (S2772660) IAW DC8 SRM 53-2-3 PG. 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW DC8 SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW DC8 SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20041207001692004120700169WP 2004 12 7 DHL2004801547 120040914A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RUDDER RT SKIN DEFLECTED, ZR 150.000 TO ZR 178.719 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-OG7Z1, 1-OD780, SEMAN DRAWING NR 3714. REMOVED DAMAGED PLATING IAW DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL2024-T3 0.032) IAW BOEING MESSAGE NR 1-0G7Z1, 1-OD780. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW BOEING MESSAGE 1-OG7Z1, 1-OD780, SRM 51-1-21. THE RIBS BEHIND THE SKIN MUST BE X-RAY INSPECTED FOR ACOUSTIC FATIGUE CRACKS AT "C" CHECK INTERVALS, NOT TO EXCEED 24 MONTHS IAW BOEING MESSAGE NR 1-OD780. FOR REBALANCING SEE NR 0729. 2L74 4F RT4A25 20041207001702004120700170WP 2004 12 7 DHL2004801545 120040909A5553 ANGLE DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT VERTICAL STABILIZER LWR ATTACH ANGLE CRACKED 4.000, ZR 47.000 (FRONT SPAR PLANE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2 PG 44A, B, C, D. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2. FABRICATED SHIM (AL7075-T6 0.125) FILLER (AL7075-T6 0.160) ANGLE (STEEL 17.7 PH 0.079) IAW DC8 SRM 53-2-5 PG 44 A, B, C, D FIG 16A SHEET 1-2. HEAT TREATED STEEL ANGLE IAW DC8 SRM 51-1-6. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA, SHIM AND FILLER IAW DC8 SRM 51-1-8B. APPLIED PRC SELANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED SHIM, FILLER AND ANGLE IAW DC8. 2L74 4F RT4A25 20041207001722004120700172WP 2004 12 7 DHL2004801530 120040904A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT WING T/E PANEL INTERNAL SKIN DELAMINATED, XW 97.000 TO XRS 162.000 (LWR). REMOVED DELAMINATED RT WING T/E LWR PANEL (XW 97.000 - XRS 162.000) IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW RT WING T/E LWR PANEL IAW DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20041207001742004120700174EU 2004 12 7 TXER097010 120040622A5610366A25004204 WINDSHIELD UROCOPEC155 EC155B 8681000EU COCKPIT CRACKED B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09155EW242 6660 CRACKED WINDSHIELD. 1G72 3U H10EU 20041207001762004120700176NE 2004 12 7 N440SL1 220040901A7200 ENGINE BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101* NE NR 2 MALFUNCTIONED E A1UAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE03440SL 7158 4573845234 APPROXIMATELY 2 MINUTES INTO THE FLIGHT, MASTER CAUTION ILLUMINATED ALONG WITH ENG II LOW LIGHT, N1 OF NR 2 ENGINE OSCILLATED BETWEEN 60 PERCENT AND 70 PERCENT. TORQUE OF NR 2 ENGINE OSCILLATED BETWEEN 20 PERCENT AND 24 PERCENT. PILOT PERFORMED RUN ON LANDING WITHOUT FURTHER PROBLEMS. MAINTENANCE PERFORMED NUMEROUS CHECKS TO DETERMINE CAUSE OF PROBLEM. ALL PARAMETERS WITHIN MANUFACTURERS LIMITS, NO DEFECTS FOUND. ALL COMPONENTS OPERATING NORMAL. 1G72 3U3 U H13EU E5NE 20041207001792004120700179CE 2004 12 7 66058 120041022A3242 BRAKE BEECH 1900 1900D 1154162CE MLG WEAK A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07144ZV UE144 UPON TAXI IN TO PKB, CREW NOTICED LEFT BRAKING ACTION WEAK, TAXIED TO GATE AND PARKED. BLEED LT SIDE BRAKES, GROUND CK GOOD. 2L72 4T RTA24CE 20041207001812004120700181CE 2004 12 7 66078 120041023A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS LACK OF LUBE A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07132YV UE132 FLAPS WOULD NOT RETRACT AFTER TAKEOFF. A/C RETURNED TO THE FIELD. CLEANED AND LUBED FLAP SWITCH, REMOVED AND REPLACED RT SWITCH. 2L72 4T RTA24CE 20041207001822004120700182NM 2004 12 7 DHL2004748500 120041023A57406516201188 CLIP BOEING727 727225 1384077NM RT WING TE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01748DH44411 22440 FLIGHTSTAR NON-ROUTINE:CORROSION ON CLIP ON RIGHT WING TRAILING EDGE. REFER DMI NR 18019E. REMOVED AND REPLACED CLIP ON RT WING T/E WS 180. RESEALED FASTENERS AT CLIP ON RT WING WS 180 IAW B727 SRM 51-30-2 AND M/M 28-11-00. TEE CLIP P/N 65-16201-188 ATTACH CLIPS P/N 65-21656-170 2 EA. 2L73 4F A3WE 20041207001832004120700183NM 2004 12 7 2004UALA01044 120041111A3520 OXYGEN GEN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE PSU ACTIVATED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29903UA 25003 PSU LT NR 10 OXYGEN GENERATOR HEAT SENSITIVE BAND IS BLACK. RELEASE PIN INADVERTENTLY PULLED. REPLACED AND INSTALLED NEW OXYGEN GENERATOR. 2L72 4F4 FRTA16WE E2GL 20041207001842004120700184WP 2004 12 7 IXXA0400115O 120041028A2720 CONTROL VALVE DOUG DC8 DC871F 302199DWP RUDDER LEAKING A IXXAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SW11822BX890051995 45813 ON DESCENT FROM KPDX TO KBFI, RUDDER CONTROL LIGHT ILLUMINATED WITH HYDRAULIC SYSTEM PRESS READ ZERO AND HYDRAULIC QUANTITY DOWN TO 6 GALS. COMPLETED QR4 PROCEDURE (LOSS OF HYDRAULIC). CREW ABORTED DESCENT AND RETURNED TO KPDX. LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ON GOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE FOUND SLOT CONTROL VALVE LEAKING. REMOVED, REPACKED AND REINSTALLED VALVE. THE OPERATIONAL AND LEAK CHECK WAS GOOD ON THE ENGINE RUN PER ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20041207001852004120700185CE 2004 12 7 DXTA200400430 120041020A523099145531 DOOR SEAL CESSNA750 750 2076810CE CARGO DOOR LEAKING E DXTAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL07939QS 7500193 AFTER CRUISING AT FL 410 FOR APPROXIMATELY 1 HR, BAGGAGE DOOR SEAL CAS MESSAGE DISPLAYED. 15 MINUTES LATER, CABIN BEGAN TO CLIMB AT A RATE OF 1000' PER MIN WITH IN 1 MINUTE CABIN RATE INCREASED TO APPROX 6000' PER MINUTE. AMBER AND RED CABIN ALTITUDE CAS MESSAGE DISPLAYED THE AIRCRAFT WAS DECENDED IN AN EMERGENCY DESCENT TO 11000' WITHIN 3 OR 4 MINUTES OF WHEN THE CABIN BEGAN TO CLIMB. AT 11000' CABIN PRESS STABILIZED AND WAS NORMAL FOR THE REMAINDER OF FLIGHT. TROUBLESHOT AND FOUND TAIL BAGGAGE INFLATABLE SEAL FILLED WITH WATER. REMOVED AND REPLACED SEAL WITH NEW. ALSO C/W SB 750-52-29R1, TAIL BAGGAGE DOOR SEAL IMPROVEMENT PRESSURE CK GROUND LEAK OPS CHECKED GOOD. ALL WORK DONE IAW CE750 MM 52-30-00. 2L72 4J RTT00007WI 20041207001872004120700187NE 2004 12 7 200416 220040720A7261AS3209222 O-RING DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 2 ENGINE MISSING A KPVAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP13808WP 026 NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON. INSTALLED MISSING NR 2 ENGINE OIL FILLER CAP PACKING IAW P&W 72-00-00 PG 337. ENGINE RUN-UP IAW PSM 1-8-2 71-00-00 PG 529-534. 2H72 4T4 TRTA13NM E20NE 20041207001892004120700189 2004 12 7 HNAA0400152 420041012A3442 TRANSCEIVER DHAV DHC8 DHC8311 1386006EA WX RADAR INACCURATE A HNAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA07342EN 3099 395 WXR RADAR SPOKING CLT MNT COULD NOT DUPLICATE. CHANGING R/T AS A PRECAUTION. REMOVED AND REPLACED R/T, OPS CHECK GOOD. 2H72 4T RTA13NM 20041207001902004120700190EA 2004 12 7 HNAA0400153 120041013A5330 SKIN DHAV DHC8 DHC8311 1386006EA FUSELAGE DENTED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07331EN 279 DURING C CHECK, FOUND FUSELAGE SKIN WITH FIVE DENTS IN SMALL AREA REQUIRING A MAJOR REPAIR. REPAIRED PER EO8-53-04-0693. 2H72 4T RTA13NM 20041207001912004120700191NM 2004 12 7 USAA040863 120041022A5330 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 Q4, SKIN, 16 INCHES W BY 22 INCHES L, GOUGES, STA 887 BETWEEN S35R AND S27R. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E2GL 20041207001932004120700193WP 2004 12 7 DHL2004801531 120040906A1430 BOLT DOUG DC8 DC873F 302199FWP TORSION LINK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT MLG LWR AND UPPER TORSION LINK CTR BOLT CRACKED. REMOVED AND REPLACED CTR BOLT ON RT MLG LWR AND UPPER TORSION LINK IAW MM 32-11-4 PG 201 FOR OPS CHECK. 2L74 4F RT4A25 20041207001942004120700194NM 2004 12 7 F3LA200400094 120040916A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967, RBL 27.16, CORRODED AT FLOOR PANEL SCREW NUT PLATE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-51, FIG 202. 2L72 4F RTA16WE 20041207001952004120700195NM 2004 12 7 F3LA200400096 120040916A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 328 CRACKED 20 INCHES IN FROM FUSELAGE OUTER SKIN. VERTICAL ANGLE CRACKED ON LOWER END LT. REPLACED SHEAR TIE AT LBL 45 ON FWD SIDE OF STA 328 FLOORBEAM PER SRM 51-40-02, 51-40-05 AND SOPM 20-41-02. 2L72 4F RTA16WE 20041207001962004120700196EU 2004 12 7 DHL2004366006 120040929A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU CABIN ACTIVATED A DHLABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01366DH 249 ON DEPARTURE, SMOKE LIGHT ON MWP ALONG WITH CABIN SMOKE DETECTORS FWD L1, L2 AND R2. RAN BOTH PACKS AT DIFFERENT TEMP SETTINGS, COULD NOT DUPLICATE ON THE GROUND, OPS CKS GOOD IAW MM 26-14-00. 2L72 4F RTA35EU 20041208000032004120800003NM 2004 12 8 SWAA043452 120041126A531069353656 SHEAR TIE BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH SHEAR TIES CRACKED AT BS 360, BETWEEN STRINGERS 13L AND 15L. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20041208000042004120800004NM 2004 12 8 SWAA043512 120041203A53306545768 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29501SW 24178 FUSELAGE SKIN AT BS 517, STRINGER 17R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041208000052004120800005 2004 12 8 SWAA043519 420041203A2565D31354 SLIDE BOEING737 7373T0 1384582NM R1&R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C2 CHECK, FOUND R1 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R1 AND R2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20041208000062004120800006NM 2004 12 8 SWAA043526 120041204A57536546434301 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT INBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041208000072004120800007NE 2004 12 8 P5CA0401275 220041116A726180427 SEAL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE FAILED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23858FT 20109 662599 DURING CRUISE AT FL 36.0, NR 1 ENGINE OIL PRESSURE FLUCTUATING 40-35 PSI WITH OIL PRESSURE LIGHT DOING SAME. OIL PRESSURE WENT TO 25 PSI WITH STEADY LOW OIL PRESSURE LIGHT ON, ENGINE SHUTDOWN, WINDMILLING OIL PRESSURE 15-20 PSI. REPLACED STARTER SEAL PER AMM 80-11-02 & 80-11-00, PERFORMED ENGINE RUN UP, LEAK CHECK NORMAL PER AMM 71-00-00. 2L74 4F4 F A20WE E20EA 20041208000082004120800008NM 2004 12 8 04FDEA03317 120041201A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041208000092004120800009NM 2004 12 8 SWAA043481 120041130A33501619 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29479WN 33990 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR OUTSIDE EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM. 2L72 4F RTA16WE 20041208000122004120800012CE 2004 12 8 DXTA200400465 120041204A3240 BRAKE ASSY CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07912QS 7500012 RIGHT BRAKE PRESSURE IS LOCKED, RIGHT BRAKE PEDAL HAS NO PRESSURE. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20041208000132004120800013 2004 12 8 SWAA043508 420041202A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29787SA 29812 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208000142004120800014NM 2004 12 8 CALA0400734 120041203A53136545769 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717344 23582 INSPECTION FOUND STRINGER 27L CORRODED AT STA 385. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20041208000162004120800016NM 2004 12 8 SWAA043459 120041129A53106545833 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND 2 EACH CREASE BEAM CHORDS CRACKED AT RIGHT BS 188 AND LEFT BS 188. REMOVED AND REPLACED CREASE BEAM CHORD SECTIONS PER SRM. 2L72 4F RTA16WE 20041208000172004120800017NE 2004 12 8 DL757041073 220041201A7200PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27629DL44376 22919 716553 FLT 1723 LGA-CVG DIVERTED WITH REPORTS OF STRANGE ODOR IN CABIN AND FLIGHT DECK. INSPECTED AIRCRAFT AND RAN SYSTEMS. BOROSCOPED ENGINE FOR INTERNAL OIL LEAKS, NONE FOUND. 2L72 4F4 FRTA2NM E17NE 20041208000182004120800018NM 2004 12 8 DL73S041081 120041204A335020121 POWER SUPPLY BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27304DL 23076 ON L/O CHECK, FOUND FWD CABIN EMERGENCY PATH LIGHTS INOP. REPLACED FWD CABIN EMERGENCY LIGHTS POWER SUPPLY. CHECKS GOOD. 2L72 4F RTA16WE 20041208000192004120800019EU 2004 12 8 MALA040714 120040902A5343 ATTACH ANGLE BAC 146 AVRO146RJ85A1500097EU MLG WW CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, LT MLG WHEEL WELL BAFFLE ATTACH ANGLE HAS A 3 INCH CRACK LOCATED AT TOP CENTER. MAINTENANCE REPAIRED IAW SRM 51-71-11. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208000212004120800021NM 2004 12 8 DLM88041072 120041130A53305920323553 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27955DL 49886 THE FUSELAGE SKIN WAS BADLY CREASED BY CONTACT WITH GROUND EQUIPMENT BETWEEN FS 461 & 522 BELOW STRINGER 20R. THE DAMAGE WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND INTERNAL ALUMINUM FINGER DOUBLERS PER MD-88 SRM AND ER/A 095369-14, REV A. 2L72 4F RTA6WE 20041208000222004120800022NM 2004 12 8 DL777041079 120041204A2420 CASE BOEING777 777232 1385232NM NR 2 ENG IDG CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27865DA F559 29737 051201 ELEC GEN OFF RIGHT EICAS MESSAGE IN FLIGHT WITH GEN DRIVE RIGHT EICAS MESSAGE. FOUND RT IDG CASE SHATTERED AND ZERO OIL. REPLACED IDG AND RAN ENG PER PFHB TEST 1 AND 2. ALL NORMAL. 2L72 4F RTT00001SE 20041208000232004120800023NM 2004 12 8 DL76S041080 120041204A5410311T106577 DOOR BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 2 NACELLE MISSING A DALAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 SO27139DL 25984 580358 ON ARRIVAL FOUND MISSING BLOW OUT PANEL ON NR 2 ENGINE INBOARD PYLON. PANEL SIZE APPROX 9 INCHS DIAMETER. INSTALLED NEW ACCESS DOOR NR 2 PYLON INBOARD. 2L72 4F4 FRTA1NM E13NE 20041208000252004120800025WP 2004 12 8 04FDEA03240 120041128A5530AMC72791 ANGLE DOUG DC10 DC1010 3022110WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 COMPLY WITH EA 8-5530-82462 INSPECTION AND REPLACEMENT OF UPPER VERTICAL STABILIZER RESPAR BASE ANGLE SB DC10-55-019R3. CLOSING ACTION ON 11/15/04, ON N/R S00005. COMPLIED WITH EA 8-5530-82462. 2L73 4F A22WE 20041208000262004120800026WP 2004 12 8 04FDEA03241 120041129A5330 SKIN DOUG DC10 DC1010 3022110WP FUSLEAGE DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF FOUND IN LWR FUSELAGE DENT 1 X 1 INCH ON EXTERNAL SKIN STA 330 LT SIDE LONG 28. PERFORMED NDI, FOUND CRACK. INSTALLED EXTERNAL REPAIR DOUBLER X SRM 53-00-02 FIG 5 SHT 1. 2L73 4F A22WE 20041208000272004120800027SO 2004 12 8 MASA200400656 120041127A5220 DOOR EMB 145 EMB145LR 3260212SO EMERGENCY EXIT MISINSTALLED A MASAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW07827MJ 145217 ASH 2832 CLT, HAD AN EMERGENCY OVERWING EXIT THAT WAS SQUEALING DURING PRESSURIZATION IN THE AIR AND ON THE GROUND. MAINTENANCE REINSTALLED THE DOOR AND FOUND NO FURTHER LEAKS OR FAULTS. 2L72 4T RTT00011AT 20041208000292004120800029NM 2004 12 8 04FDEA03164 120041118A5330 SKIN BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION BS 480 STR 4R - STR 6R UNDER FWD SIDE OF THE SPLICE. FOUND VISUALLY, DURING DETAILED VISUAL INSPECTION. CORROSION NOT FOUND DURING LOW FREQUENCY INSPECTION. CORROSION BS 480 STR 4R TO 6R UNDER FWD SIDE OF SPLICE REPAIR ON W/C N01202 AND EO 7-5330-7-2319 PT 5. 2L73 4F RTA3WE 20041208000312004120800031WP 2004 12 8 04FDEA03166 120041118A3610350082 CONTROLLER DOUG MD10 MD1010F 3022112WP BLEED AIR FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO2568049 47803 DURING CLIMBOUT PASSING 1700 LEVEL ONE AIR SYS 3 OFF LEVEL ONE ALERT, FOLLOWED BY THE LEVEL 3 MANIF FAIL. NO FUEL DUMPED RETURN TO MEM. COMPLETED QRH. LEFT THROTTLE IN IDEL FOR REMAINDER OF TRIP. PERFORMED DECAY CHECK WITH AND WITHOUT ANTI-ICE. SYSTEM NR 3 HOLDS PRESSURE CONSISTENT WITH NR 1 AND NR 2. REMOVED AND REPLACED RELAY BR2-8998. NO FAULT BALLS IN CAC. TROUBLESHOOTING PER FIM36-23, NO DEFECTS. SHOT ALL WIRING PER AWM 36-23-02, ALL GOOD. PERFORMED HIGH POWER ENGINE RUNS AND EXERCISED PNEU SYSTEM. ALL PRESSURE AND TEMPS CHECK GOOD. CHANGED MANIFOLD FAIL CONTROLLER AS SUGGESTED BY FIM. RERAN CHECKS. ALL PNEU SYSTEMS MANIFOLD FAIL CHECK GOOD. DMI CLEARED AND PLACARD PULLED. 2L73 4F RTA22WE 20041208000322004120800032WP 2004 12 8 04FDEA03167 120041119A5753 ROLLER DOUG MD10 MD1010F 3022112WP ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 RIGHT WING INBOARD FLAP UPPER LOAD ROLLER HAS CHROME WORN AWAY ON BEARING SURFACE OF ROLLER. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK FORWARD UPPER LOAD ROLLER IAW FEDEX EA 8-5750-81513, WING - INBOARD ROLLER TORQUE REQUIREMENT - CLARIFICATION. REFERENCE NON-ROUTINE N00589. 2L73 4F RTA22WE 20041208000332004120800033WP 2004 12 8 04FDEA03099 120041112A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/CF IN AFT CARGO AT STA 1821-1841 FOUND STR 36 RT WITH EXISTING REPAIR. REPLACE LONGERON'S AND SPLICE PER SRM 51-33-01 PG 34-47. 2L73 4F A22WE 20041208000342004120800034NM 2004 12 8 TSAA0432078 120041129A3260 BULB BOEING737 737230 1384401NM MLG INDICATOR INOPERATIVE A TSAAO OTHER P NO WARNING INDICATION DEDESCENT 1 WP13823AL 23154 NON-ETOPS, FLT 90, HNL-KOA; LANDING GEAR INDICATOR LIGHTS WERE INOP WHEN THE LANDING GEAR EXTENDED. CONDUCTED A TOWER FLY BY TO CHECK FOR GEAR DOWN. UNEVENTFUL LANDING ACCOMPLISHED. FOUND SECTION 5 CIRCUIT BREAKERS POPPED. INSPECTED INDICATOR LIGHTS AND FOUND NR 1 ENGINE LOW OIL PRESSURE LIGHT BULB ARCING. REMOVED AND REPLACED BULB. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20041208000352004120800035NE 2004 12 8 DXTA200400460 220041129A731031J240401 FILTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE RT ENGINE WARNING LIGHT E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07621QS 5605280 PCEDB0574 DURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TRIGGERED BY RIGHT ENGINE FUEL FILTER BY-PASS ANNUNCIATOR. REMOVED AND REPLACED RT FUEL FILTER IAW P&W 545 MM CHAPTER 73-10-07. LEAK CHECK GOOD, FILTER INSTALLED IS NEW. OPERATIONAL CHECK SATISFACTORY. 2L72 4F4 FRTA22CE E00059EN 20041208000362004120800036NE 2004 12 8 DXTA200400461 220041130A731031J240401 FUEL FILTER CESSNA560 560XL 2076702CE PWA 545 PW545A NE ENGINE WARNING LIGHT E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07670QS 5605170 PCEDB0349 DURING TAKEOFF ROLL FUEL FILTER L-ANNUNCIATOR ILLUMINATED. TAKEOFF ABORTED, ANNUNCIATOR EXTINGUISHED DURING ABORT. REPLACED LEFT AND RIGHT ENGINE FUEL FILTER AND ASSOCIATED PACKING. PERFORMED SATISFACTORY ENGINE RUNS AND LEAK CHECKS. REFERENCE P + W 545 AMM 73-10-05. 2L72 4F4 FRTA22CE E00059EN 20041208000382004120800038CE 2004 12 8 DXTA200400462 120041130A3150 TRIM SCALE CESSNA750 750 2076810CE COCKPIT WARNING LIGHT E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07931QS 7500064 ON TAKEOFF ROLL JUST BELOW V1, RED MASTER WARNING ILLUMINATED WITH RED NO TAKEOFF EICAS MESSAGE. AFTER ABORTING T/O AND EXITING RUNWAY, NO ABNORMALITIES NOTED ON T/O PAGE, OR ANYWHERE ELSE. FOUND STAB TRIM OUT OF T/O ARC LIMITS. SET STAB TO WITHIN T/O LIMITS AND OP'S CHECK GOOD. CHECKED NO T/O SYSTEMS IAW 750 MM 31-52-00, OP'S CHECK GOOD. 2L72 4J RTT00007WI 20041208000392004120800039WP 2004 12 8 04FDEA03209 120041125A5730ARC05831 SKIN DOUG DC10 DC1010 3022110WP LT WING DELAMINATED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND LT WING INBOARD ISLAND UPPER SKIN WITH FINGER DOUBLER DELAMINATED. REPLACE UPPER SKIN PER SRM 51-35-01 PG 1-12 AND SRM 51-35-01 PG 34-47. 2L73 4F A22WE 20041208000412004120800041NM 2004 12 8 04FDEA03219 120041125A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT HAND WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II AND DWG ARC4125. 2L73 4F RTA22WE 20041208000422004120800042NM 2004 12 8 04FDEA03220 120041125A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. OUTBOARD FLAP REMOVED AND REPLACED AS PER ARM 51-33-01 VOL II AND DRAWING ARC4125. 2L73 4F RTA22WE 20041208000442004120800044EU 2004 12 8 04FDEA03327 120041202A5321 FLOOR PANEL AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 BULK CARGO COMPT FLOOR STRUCT FR 68 4 EA AREAS OF CORROSION TOP TO UNDERNEATH. REPLACED T PROFILE AND FITTING AT FR 66 TO 69 BL 0 AND RBL 20 FR 68 IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20041208000462004120800046WP 2004 12 8 04FDEA03329 120041202A5330NFA6013 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 AFT REPAIR AT STATION 966 TO 1001, LONGERON 37 RIGHT TO 42 RIGHT NEEDS EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED EXISTING DAMAGED PORTION OF SKIN IAW DC10 SRM 53-20-00 VOL 1. FABRICATED AND INSTALLED REPAIR IAW DC10 SRM 53-20-00 FIGURE 6. 2L73 4F RTA22WE 20041208000472004120800047EU 2004 12 8 04FDEA03330 120041202A5347 SEAT TRACK AIRBUS310 A310222 3930315EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 MDCC LEFT NR 5 SEAT TRACK HAS CORROSION AT FR C-54, 53, 52, 50.89, 48. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21 AND B/P 15 A 53811922 FROM FR 54 TO FR 45 LBL 77. 2L72 4F RTA35EU 20041208000502004120800050WP 2004 12 8 04FDEA03247 120041129A5712 RIB DOUG DC10 DC1010 3022110WP LT WING CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND 2 INCH LONGERON CRACK RIB 402 LT WING AFT OF FUEL TANK FLAPPER DOOR. INSTALL REPAIR DOUBLER -3 PER SRM 57-20-00 FIG 33. 2L73 4F A22WE 20041208000512004120800051WP 2004 12 8 04FDEA03248 120041129A5753 HINGE DOUG DC10 DC1010 3022110WP RT WING FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING OUTBD HINGE SECTION OF OUTBD FLAP STA XW 638 RUST NEAR HOLES FOR STUDBOLTS. ACCOMPLISH CORROSION REWORK OF ATTACH HOLES (NR 3) FWD/OUTB HINGE OUTBD FLAP IAW CMM 57-44-09 AT HOLES MARKED 7. ACCOMPLISH CORROSION REWORK IAW CMM 57-44-09 CONT PG 301 TO 414 AT HOLES MARKED 2 HOLES REMAIN AT ORIGINAL SIZE DIA. REPROTECT IAW CMM 57-44-09 REV 30. EVERY SINGLE REWORK AREA MUST BE PROTECTED AND PAINTED IAW CMM 57-44-09. 2L73 4F A22WE 20041208000522004120800052WP 2004 12 8 04FDEA03249 120041129A5315AEA03613 FLOORBEAM DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND CRACK ON FLOORBEAM DIM 3 INCH AT STA 1293 X= -107. REPLACE FLOORBEAM IAW DWG AEA 0361. 2L73 4F A22WE 20041208000532004120800053WP 2004 12 8 04FDEA03250 120041129A2760ARC310767 SEAL DOUG MD10 MD1010F 3022112WP ZONE 500 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LT HAND WING UPPER TRAILING EDGE HAS TORN SEAL AT OUTBOARD END OF NR 1 LEFT HAND SPOILER. REMOVED SEAL FROM SPOILER NR 1 LEFT WING IAW FEDES MD10-10 MM 20-50-02 PAGE 1. REPAIRED SEAL IAW FEDEX EA 8-2760-83941, REINSTALLED SEAL ON NR 1 LEFT WING SPOILER IAW FEDEX MD10-10 MM 20-50-02- 2 PAGE 1 AND FEDEX EA 8-2760-83941, FLIGHT CONTROL- NR 1 SPOILER, TRAILING EDGE WORN SEAL REPAIR. 2L73 4F RTA22WE 20041208000542004120800054WP 2004 12 8 04FDEA03251 120041129A5312NCA6044 BULKHEAD DOUG MD10 MD1010F 3022112WP ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR ON AFT SIDE OF PRESSURE BULKHEAD FORWARD WALL IN FORWARD CARGO COMPARTMENT FLOOR LEVEL ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR DATA ARE REPETITIVE INSPECTIONS REQUIREMENTS. EVALUATED REPAIR ON AFT SIDE OF PRESSURE BULKHEAD FORWARD WALL IN FORWARD CARGO COMPARTMENT FLOOR LEVEL AND ACCOMPLISHED FEDEX EA 8-5310-83845. 2L73 4F RTA22WE 20041208000552004120800055WP 2004 12 8 04FDEA03252 120041129A5330ABA7047 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 377 TO 413, LONGERON 50 RIGHT TO LONGERON 47 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR ID MAJOR OR MINOR AND IF REPORT IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. EVALUATED REPAIR AT STATION 377 TO 413 LONGERON 50 RIGHT TO LONGERON 47 LEFT AND ACCOMPLISHED FEDEX EA 8-5330-83846, FUSELAGE- REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STATION 377- 413 LONGERON 50 RIGHT TO LONGERON 47 LEFT. 2L73 4F RTA22WE 20041208000572004120800057WP 2004 12 8 04FDEA03261 120041129A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 1140 TO 1151 AT LONGERON 39 LEFT TO 41 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE MAJOR OR MINOR AND IF DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED PANEL 153AB AND REMOVED DOUBLER IAW DC10 SRM 51-31-01 VOL 2 AND 51-35-01 VOL 2. FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW DC10 SRM 53-20-01 VOL 2. REINSTALLED PANEL 153AB IAW DC10 SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20041208000592004120800059WP 2004 12 8 04FDEA03254 120041129A5753ARC0154 HINGE BRACKET DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT AND INBOARD FLAP OUTBOARD HINGE BOLT HOLE HAS AREA OF CORROSION. BOLT HOLE IS REPLACEMENT BOLT PART NUMBER 3D0031-8-90 STEP 23 OF FEDEX WIC E 8-5710-7-5005 PT1. REMOVED STOP FITTING IAW DAC DWG ARC0154, REMOVED OUTBOARD PANEL IAW MD10 SRM 51-31-01 VOL 2, REAMED HOLE TO .5273 INCH, OUT OF LIMITS IAW DAC DWG ARC0154 AND MD10 51-21-01 PAGE 1-8. ACCOMPLISHED FEDEX EA 8-5710-81535, WINGS- LEFT HAND, INBOARD FLAP, OUTBOARD HINGE BRACKET, UPSTOP MOUNTING HOLES- REPAIR. 2L73 4F RTA22WE 20041208000602004120800060WP 2004 12 8 04FDEA03255 120041129A2910 RESERVOIR DOUG DC10 DC1030 3023501WP NR 3 HYD SYSTEM LEAKING A FDEAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25309FE 48298 HYD SYS 3 ELEV OFF LT ILLUMINATED IN CRUISE AT FL 270 PERFORMED RED TAB PROCEDURES, DUMPED FUEL & RETURNED TO MEM. NR 3 HYD QUANT DROPPED TO 0. FOUND NR 3 HYD RESERVOIR LEAKING AT TOP ON INBOARD OF SIGHT EYE. SIGHT GLASS CRACKED. REMOVED AND REPLACED RELIEF AND SAMPLING VALVE, SIGHT GLASS ON RESERVOIR. SERVICED NR 3 SYSTEM HYDRAULICS. PERFORMED LEAK CK ON SYSTEM, NO LEAKS NOTED. RED TAB PROCEDURE MANUAL GEAR EXTEND HANDLE USED. RESTORED MANUAL GEAR HANDLE TO NORMAL CONFIGURATION. REMOVED AND REPLACED BOTH LT & RT NR 3 EDP'S CHECKED NR 3 HYDRAULIC MANIFOLD FILTERS, OK ALL OPS AND LEAK CHECK GOOD. 2L73 4F A22WE 20041208000612004120800061NM 2004 12 8 SWAA043485 120041130A52406969854 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME LOWER SECTION CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM AND BAC DRAWING. 2L72 4F RTA16WE 20041208000622004120800062NM 2004 12 8 SWAA043486 120041130A57536573732 STRUCTURE BOEING737 7373H4 1384600NM RT WING FLAP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E MID FLAP, CRACKED. REPAIRED RT WING MID FLAP PER SRM. 2L72 4F RTA16WE 20041208000632004120800063CE 2004 12 8 DXTA200400464 120041203A3234 CONTROL LEVER RAYTHNDH125 HAWKER800XP 7150012CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07817QS 258517 RIGHT RED GEAR INDICATION ILLUMINATED WITH GEAR SELECTED UP. JACKED AIRCRAFT AND USED EXTERNAL HYDRAULIC CART TO SUPPLY FLUID TO GEAR SYSTEM. CYCLED GEAR NUMEROUS TIMES AND COULD NOT DUPLICATE. CHECKED SIDE STAY CLEARANCES AND ADJUSTED TO MINIMUM ALLOWABLE CLEARANCE. FOUND CAM LEVER TO BE OUT OF ADJUSTMENT, SET CAM TO MINIMUM CLEARANCE OF .01 AND SWUNG GEAR NUMEROUS TIMES. ALL GEAR INDICATIONS IN COCKPIT ARE NORMAL. WORK IAW HAWKER 800 XP AMM 32-10-00/32-60-00. 2L72 4F RTA3EU 20041208000662004120800066NM 2004 12 8 SWAA043482 120041130A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED MV1 CHECK, AFT INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHTS BATTERY PER MM. 2L72 4F RTA16WE 20041208000672004120800067NM 2004 12 8 SWAA043483 120041130A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29751SW 29803 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20041208000712004120800071CE 2004 12 8 DXTA200400451 120041119A29103309A0113000E LINE CESSNA560 560XL 2076702CE HYDRAULIC SYS LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 GL07652QS3515 5605152 BRAKE PEDALS ARE SOFT AND GO TO THE FLOOR ON LANDING, ALSO ON POST AIRCRAFT INSPECTION THERE APPEARS TO BE A PUDDLE OF HYDRAULIC FLUID UNDER THE CO-PILOTS BRAKE PEDAL. FOUND CO-PILOTS LEFT BRAKE PEDAL VALVE HAS A BROKEN LINE AT TOP OF CYLINDER. REMOVED & REPLACED LINE. CLEANED AFFECTED AREA OF HYDRAULIC FLUID, BRAKE RESERVOIR SERVICED AND BRAKE BLED, NO OTHER DEFECTS NOTED. 2L72 4F RTA22CE 20041208000722004120800072NM 2004 12 8 CALA0400729 120041130A53306545775594 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717326 23456 INSPECTION FOUND TWO 2 INCH CRACKS IN FUSELAGE SKIN AT BS 727E, S22R AND S23R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01. 2L72 4F RTA16WE 20041208000742004120800074NM 2004 12 8 CALA0400731 120041029A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2776355 23593 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727D AND 727E AT S22L. REPAIRED IAW ECRA 5330-03388. 2L72 4F RTA16WE 20041208000772004120800077NM 2004 12 8 DL73S041051 120041122A261289638305 MODULE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 FIRE WARN MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27302DL 23047 709122 ON CLIMBOUT AT 14,000 FEET NR 1 ENG OVERHEAT LIGHT ILLUM. IAW CK LIST THRUST LEVER RETARDED. LIGHT WENT OUT. REPLACED ENG FIRE/OVERHEAT MODULE. RAN ENGS AT T/O AND CLIMB PWR, ALL TEST NORMAL. 2L72 4F4 FRTA16WE E2EA 20041206000052004120600005CE 2004 12 6 64378 120040829A3230571302 POWERPACK BEECH 1900 1900D 1154162CE MLG FAILED A AMWAO OTHER J WARNING INDICATION NRNOT REPORTED 1 CE07171ZV UE171 WHEN MAIN LANDING GEAR HANDLE WAS DOWN SELECTED, MAIN LANDING GEAR WOULD NOT EXTEND 2 AMP CB POPPED. CREW FOLLOWED PROCEDURES MANUALLY EXTENDED LANDING GEAR. GOT 3 GOOD DOWN AND LOCKED INDICATIONS. LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED MOTOR POWER PACK, OPS CHK NML P/N 571302 S/N 1320A. 2L72 4T RTA24CE 20041206000402004120600040SO 2004 12 6 CHQA000552 120040909A3350 LIGHT EMB 135 EMB135KL 3260302SO PAX DOOR INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11297 145522 EMERGENCY LIGHT AT MAIN CABIN DOOR HINGE IS INOP. INSPECTED AND FOUND THE LIGHT BASE ASSY HAD A BAD GROUND. CLEANED BONDING SURFACE AND REINSTALLED GROUND. OPS CHECK GOOD IAW EMB 140 AMM 33-50-00. 2L72 4F RTT00011AT 20041206000422004120600042WP 2004 12 6 ARWA20040906 120040928A5730 SKIN DOUG DC8 DC863F 302198FWP RT WING CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19906R 46087 DURING A "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND, RT WING INBOARD L/E LOWER SECTION STA XCW 69 OUTER PLATING AND INNER DOUBLER WITH 3 INCH CRACK. 2L74 4F 4A25 20041206000472004120600047WP 2004 12 6 WLDA200493 120040905A5321 FLOOR PANEL DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO1114075 46922 DURING "B4" CHECK IN BYH, FOUND FLOOR PANEL FWD OF LEFT FWD STORE CLOSET HAD EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR PANEL FWD OF LEFT STORE CLOSET IAW DC-10 MM 53-22-01. 2L73 4F4 F A22WE E23EA 20041206000502004120600050NM 2004 12 6 DHL2004764009 120040831A5750 CONNECTOR BOEING727 727264 138408MNM SLAT ACTUATOR MISPINNED A DHLAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01764AT 22984 NR 3 LED WOULD NOT RETRACT ON DEPARTURE ACCOMPLISHED ABNORMAL PROCEDURE LED WOULD NOT RETRACT ON SECOND ATTEMPT, NR 3 SLAT. SWAPPED PINS 1 AND 3, 2 AND 4 ON NR 3 SLAT ACTUATOR IAW B727 MM 27-82-11 PAGE 101. OPS CKS GOOD. 2L73 4F A3WE 20041206000512004120600051EU 2004 12 6 DHL2004363532 120041012A5330 SKIN AIRBUS300 A300B4203 3930306EU FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK AT AVBORNE HEAVY MAINTENACE IN MIAMI, FL DISCREPANCY AS FOLLOWS, N/R 3911, AFT FUSELAGE SKIN HAS DENT AT FS 65 AND STR 31R. BLENDED OUT AREA FOUND DENT BEYOND OF LIMITS IAW A-300 SRM 53-10-10. CUT-OUT DAMAGED AREA IAW A-300 SRM 53-10-10. PERFORMED HFEC OF CUT-OUT AREA AS PER A-300 NTM PT 1 51-31-05. NO DISCREPANCIES NOTED. INSTALLED DOUBLER REPAIR AS REQUIRED MATERIAL USED ALCLAD 2024 T-3 0.080 PO NR 240919001 LOT NR 2024 T-3 174861 IAW A-300 SRM 53-10-10, 7" X 11". TREATED, PRIMED, AND APPLIED PRC IAW A-300 SRM 51-40-10 / 51-40-20. 2L72 4F RTA35EU 20041206000572004120600057SO 2004 12 6 ESPA20040005 120041015A5230 DOOR GULSTMG159 G159 3952202SO CARGO BAY UNSECURE E ESPAA UNSCHED LANDING WE INADEQUATE Q C VIBRATION/BUFFET CLCLIMB 1 SO11190PA 195 CARGO DOOR CAME OPEN IN FLIGHT. CREW LANDED SAFELY. IT WAS DETERMINED THAT THE DOOR WAS NOT PROPERLY SECURED BEFORE TAKEOFF. 2L72 4T 1A17 20041206000662004120600066CE 2004 12 6 65848 120041015A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07144ZV UE144 CREW REPORTS BRAKES SPONGY. MX BLED BRAKES, A/C RETURNED TO SERVICE. 2L72 4T RTA24CE 20041206000682004120600068CE 2004 12 6 65672 120041008A5220 HANDLE BEECH 1900 1900D 1154162CE EMERGENCY EXIT UNSECURE A AMWAK NONE W INADEQUATE Q C ININSP/MAINT 1 CE07135YV UE135 PREFLIGHT INSPECTION REVEALED THAT EMERGENCY EXIT 6F OUTSIDE HANDLE NOT STOWED COMPLETELY. MX STOWED HANDLE A/C RETURNED TO SERVICE. CHECKED DOOR, STOWED LATCH, OPS CK NORMAL. 2L72 4T RTA24CE 20041206000692004120600069NE 2004 12 6 NACA20040032 220040803A8510NOSECASECB3 CASE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 4 ENGINE LEAKING A NACAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL03779TA1201 1201 45529 33325 NR 4 ENGINE SHUT DOWN DUE TO EXCESSIVE OIL LEAK. REPLACED NOSE CASE ASSEMBLY DUE TO A BLOWN ACCESSORY PLUG. 2L74 4R4 R A781 5E8 20041206000702004120600070EU 2004 12 6 WRNA200400010 120040904A2910AN6289D12 NUT AIRBUS300 A300B4203 3930306EU MANIFOLLD LOOSE A WRNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO05501TR 53 COMPLETE LOSS OF GREEN SYSTEM HYD QUANTITY. PERFORMED ABNORMAL CHECKLIST. RETURNED TO AIRPORT, PERFORMED MANUAL GEAR EXTENSION. LANDING NORMAL. MAINTENANCE FOUND JAMNUT LOOSE ON GREEN PRESSURE MANIFOLD. TORQUED NUT AND LEAK CHECK GOOD I/A/W A300 MM 20-21-12. SERVICED HYD SYSTEM IAW A300 MM 12-12-21. RESTORED LANDING GEAR ACTUATING SYSTEM TO NORMAL IAW A300 MM 32-30-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA35EU 20041206000732004120600073CE 2004 12 6 45120102004 120041020A2697 WIRE HARNESS LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP FIRE WARNING DAMAGED E J7SAO OTHER N FALSE WARNING APAPPROACH 1 SW05418FX 45120 PP116232C CREW REPORTED ON APPROACH, THE RT ENGINE FIRE WARNING CAME ON. THE FIRE ICON AND TRIPLE CHIME WENT OFF. CREW RETARDED THE RT THROTTLE TO IDLE AND THE FIRE WARNING WENT OUT AND THE AMBER ICAS MESSAGE OF (R ENG FIRE FAIL) CAME UP. DURING LANDING ROLL OUT, THE FIRE WARNING TRIPPED OFF AGAIN. CREW SHUTDOWN THE RT ENGINE AND THE MESSAGE WENT BACK TO THE AMBER ICAS. MAINTENANCE HAS FOUND THE WIRE BUNDLE AT P-133 CHAFED. APPROX 5 WIRES THAT THEY CAN TELL AT THIS POINT ARE CHAFED BADLY. WIRE NR'S RBA 0135B, RBA 0486C, RBA 2111, RBA 0295C, RBA 0061B. 2L72 4F3 TRTT00008WIAEXJ STC 20041206000752004120600075CE 2004 12 6 GLBA20030738 120041021A5313131686 STRINGER BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03261GL17674 UE261 INTERNAL LOWER SKIN TO STRINGER CORROSION FOUND DURING ROUTINE INSPECTION. CORROSION LOCATED BETWEEN BONDED STRINGER 16 AND FUSELAGE SKIN, BETWEEN FS 220 AND FS 236. CORROSION APPROX. 6 INCHES TO 8 INCHES IN LENGTH. 2L72 4T RTA24CE 20041206000772004120600077NM 2004 12 6 P9RA20040039 120040912A361032143042 PRESSURE VALVE BOEING757 757236 1384971NM RT ENGINE FAULTY A P9RAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11521NA 25592 RIGHT ENGINE HIGH STAGE BLEED MESSAGE ON EICAS AT 70 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED RIGHT HIGH STAGE VALVE IAW MM. 2L72 4F RTA2NM 20041206000792004120600079WP 2004 12 6 P9RA20040045 120040929A335041B004AD0763 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT WEAK A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1114816 49370 AIRCRAFT IN MAINTENANCE, SYR, 4 INTERIOR EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERIES IN 4 SEPARATE POWER SUPPLIES IAW MM. 2L72 4F A6WE 20041206001012004120600101CE 2004 12 6 DXTA200400410 120040929A2120 ODOR CESSNA750 750 2076810CE CABIN DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL07967QS 7500067 DURING DESCENT, STRONG SMOKE ODOR DETECTED AFTER REDUCING POWER, UNABLE TO DETERMINE CAUSE OR ISOLATE SOURCE. AFTER 3-4 MINUTES THE ODOR WENT AWAY. CHECKED NR 1 AND NR 2 ENGINE OIL LEVELS AND BOTH ACM OIL LEVELS, ALL LEVELS AT FULL. RAN BOTH ACM’S WITH APU AND BLEED AIR AND ENGINE BLEED AIR, NO ODORS NOTED, UNABLE TO DUPLICATE DISCREPANCY ON GROUND, MAINTENANCE PERFORMED IAW STANDARD PRACTICES. 2L72 4J RTT00007WI 20041207000022004120700002NM 2004 12 7 AALA20041162 120041123A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21797AN 30012 DFW - AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS AT R3 INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS AT R3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041207000102004120700010NM 2004 12 7 USAA040849 120041021A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME .2500 INCH CRACK, FRAME STA 787 AND STR 9R, CRACK EMANATING FROM FASTENER. INSTALLED REPAIR DOUBLER IAW TR 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041207000202004120700020WP 2004 12 7 UPS04843560 120041030A5711REFSRO8570009 SPAR DOUG DC8 DC871F 302199DWP WING CENTER SECTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 INSPECTION TYPE: C1, CENTER WING REAR SPAR LOWER CORD CRACKED IN RT W/W, STA 857, OB CORNER. NDT MAPPED CRACK REF SPMSPM06-10-01.001. STOP DRILLED AND VERIFIED BY NDT. FABRICATED AND INSTALLED REPAIR PARTS PER SRO8570009 2L74 4F RT4A25 20041207000222004120700022WP 2004 12 7 AALA20041181 120041202A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21245AA 49257 MSP - OVERHEAD EMERGENCY LIGHT AT ROW 9DEF INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041207000242004120700024NM 2004 12 7 AALA20041173 120041201A3350BPS73 BATTERY PACK BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21380AN 25449 LAX - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 24AB INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 20 THROUGH 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041207000252004120700025WP 2004 12 7 AALA20041182 120041202A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21552AA 53034 DFW - CEILING EMERGENCY PATH LIGHT AT ROWS 23, 24, AND 26 INOPERATIVE. RESEATED BATTERY IN BATTERY PACK FOR ROWS 23, 24 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041207000412004120700041EA 2004 12 7 COMA0460648 120041126A2120601R9521171 DUCT CNDAIRCL600 CL6002B19 1900309EA LT ACM CRACKED A COMAB EMER. DESCENT S AFFECT SYSTEMS CRCRUISE 1 SO01798CA 7348 FLIGHT 5364 - CABIN ALTITUDE CLIMBED TO 10,000 FT. REPLACED CRACKED AIR DISTRIBUTION DUCT IN AIR CONDITIONING SYSTEM. 2L72 4F RTA21EA 20041207000432004120700043EA 2004 12 7 COMA0460655 120041124A3010 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01914CA 7012 FLIGHT 5839 - ANTI-ICE DUCT WARNING MESSAGE. COULD NOT DUPLCATE. NO EVIDENCE OF LEAKS, ELECTRICAL AND OPERATIONAL CHECKS NORMAL. 2L72 4F RTA21EA 20041207000452004120700045NM 2004 12 7 UPS04M43505 120041118A3510801307 OXYGEN BOTTLE DOUG MD11 MD11F 3023600NM CREW SYSTEM LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01252UP NR 2 AND NR 4 O2 BOTTLES EMPTY. REMOVED AND REPLACED BOTTLES AND REPAIRED LEAK IN NR 4 SYSTEM. LEAK CHECK OK. 2L73 4F RTA22WE 20041207000632004120700063NM 2004 12 7 USAA040829 120041019A57536546434301MC SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE LT WING TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US54103 22958 PIT - C4, IB AFT FLAP SKIN, 3 INCHES BY 2.5 INCH AREA, DELAMINATION, IB AFT FLAP OB T/E LEFT WING. REMOVED SKIN AND CORE, INSTALLED REPAIR AND DOUBLER IAW TYP REP 57-53-04 AND SRM 51-70-10. 2L72 4F4 FRTA16WE E2GL 20041207000682004120700068EU 2004 12 7 UPS04143542 120041122A5730 SKIN PANEL AIRBUS300 A300B4622R 3930312EU RT WING TE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01140UP 0823 RT WING T/E OUTER SHROUD BOX INNER SKIN PANEL CRACKED. R & R PANEL ASSY IAW EO A300-5720-21353. DMI CLOSED. 2L72 4F RTA35EU 20041207000732004120700073WP 2004 12 7 UPS04843510 120041025A53204750422U1 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 C1 LONGERON 19 RT END FITTING CRACKED AT STA 860. REMOVED AND REPLACED L19R END FITTING REF SRM 51-1-20D. 2L74 4F RT4A25 20041207000832004120700083NE 2004 12 7 AALA20041178 220041126A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT STALLED A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW21592AA 53255 725975 LT ENGINE COMPRESSOR STALLS DURING CLIMB-OUT AT 11,000 FT. ENGINE ACCELERATED FOR CLIMB NORMALLY BUT STARTED STALLS WHILE AT FULL CLIMB THRUST. ENGINE ANTI-ICE ON. ENGINE FAIL CHECKLIST ACCOMPLISHED. ENGINE LEFT AT IDLE. FOUIND NUMEROUS LEFT ENGINE FAN BLADES DAMAGED. REPLACED LEFT HAND ENGINE PER CARD 71 91 99. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20041207000892004120700089WP 2004 12 7 UPS04843550 120041030A53403755822 FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 BATH-TUB FITTING CRACKED AT STA 320, LONG 27L. REMOVED CRACKED FITTING REF 51-3-0, 51-1-21. FABRICATED REPLACEMENT FITTING FROM PLT7075T6 PER DWG3755822. NDT FITTING REF DPS7.707 NO CRACKS NOTED. FABRICATE SPLICE ANGLES FROM BAC1503-100163 AND INSTALLED ALL PARTS REF SRM 53-2-0 FIG 2D, 51-1-8, 51-3-0, 51-1-20, 51-1-15. 2L74 4F RT4A25 20041207000902004120700090WP 2004 12 7 UPS04843551 120041101A53403652562 ATTACH FITTING DOUG DC8 DC871F 302199DWP TAILCONE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 TAILCONE ATTACH FITTING CRACKED AT CROWN (L1) ON FWD SIDE OF STA 1890 FRAME IN 62 COMP'T. REMOVED FITTING REF 51-1-20D. FABRICATED REPLACEMENT FITTING FROM PLATE 7075T6 REF DWG 3652562. NDT PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-8, 51-1-20D, 51-3-0, 51-1-21, 51-1-15. 2L74 4F RT4A25 20041207001062004120700106NM 2004 12 7 USAA040848 120041019A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME, .5 INCH CRACK, FRAME STA907,STR9L, CRACK EMANATING FROM FASTENER. CUTOUT CRACKED AREA AND INSTALLED REPAIR ANGLES IAW T.R. 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041207001132004120700113NM 2004 12 7 SB04158 120041125A27512061141 INDICATOR BOEING737 737301 1384611NM TE FLAPS FAULTY A USAAO OTHER O OTHER APAPPROACH 1 EA19563AU3681936819 23551 DURING APPROACH TO PHL FROM ORD, CREW EXPERIENCED A FLAP DISAGREEMENT WHEN FLAP HANDLE WAS PLACED BEYOND 15 UNITS. A FLAP SPLIT WAS CLEARLY INDICATED. NO ROLL FORCES WERE FELT. AN EMERGENCY WAS DECLARED AND EQUIPMENT WAS CALLED OUT. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND CLEANED THE RIGHT WING FLAP TRANSMITTER CONNECTOR. SYSTEM OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041207001192004120700119WP 2004 12 7 IXXA0400085S 120040515A5730 PLATE DOUG DC8 DC871F 302199DWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP L/E UPPER PLATING WEAR AT STA XF 211.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED WORN PLATING IAW DC8 SRM 51-1-21 PG 1 FABRICATED NEW PLATING IAW DC8 SRM 57-7-1PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PLATING IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-15 PG 1. 2L74 4F RT4A25 20041207001402004120700140CE 2004 12 7 66096 120041024A32439038000133 MASTER CYLINDER BEECH 1900 1900D 1154162CE BRAKES MALFUNCTIONED A AMWAO OTHER O OTHER LDLANDING 1 CE07144ZV UE144 LEFT BRAKE SPONGY AFTER LANDING. REMOVED AND REPLACED CAPTS LT PEDAL MASTER CYLINDER, P/N 9038000133 S/N 3152. 2L72 4T RTA24CE 20041207001452004120700145EU 2004 12 7 DJFA2004016 120040812A28218975131 FILTER BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP NR 2 FUEL SYSTEMBLOCKED E DJFAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA23845CW 258045 P91196 DURING TAKEOFF, THE NR 2 ENGINE FUEL BYPASS LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE FBO. FUEL FILTER WAS REPLACED, LEAK CHECKED AND FOUND TO BE OK. 2L72 4F4 FRTA3EU E6WE 20041207001582004120700158NE 2004 12 7 C8GA20040019 220040916A7200 ENGINE BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE NR 3 DAMAGED A C8GAEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO15708AA6865 22465 666251 FLT 727 FROM DFW TO TOL. ON TAKEOFF, THE NR 3 ENGINE HAD STRONG VIBRATION. IN-FLIGHT SHUTDOWN OF THE NR 3 ENGINE AS A PRECAUTIONARY ADVISED ATC DECLARED EMERGENCY AND AIR TURN BACK TO DFW. AIRCRAFT WAS INSPECTED AND FOUND FAILURE OF TURBINE SECTION PER EVIDENCE OF MISSING DAMAGE TURBINE BLADES. REPLACED THE NR 3 ENGINE PER B727 MM 71-00 AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20041207001752004120700175CE 2004 12 7 GLBA20030683 120040729A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03154GL UE154 CRACK IN FUSELAGE SKIN FWD AND LEFT OF LWR COMM ANTENNA, PERFORMED MAJOR REPAIR TO FUSELAGE SKIN. 2L72 4T RTA24CE 20041207001772004120700177NM 2004 12 7 USAA040759 120041019A5310 CREASE BEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 CLT, C-4, CREASE BEAM, .5 INCH AREA, LEVEL 2 CORROSION , STA 324, RBL 62. REPLACED WITH IDENTICAL PART IAW SRM. 2L72 4F4 FRTA2NM E12EU 20041207001782004120700178NM 2004 12 7 F3LA200400093 120040914A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED TOP OF FLOORBEAM AT STA 294.5 CORRODED IN SEVERAL SPOTS FROM 10 INCHES LEFT OF CENTER TO 40 INCHES RT OF CENTER. ALL SCREW HOLES IN THIS AREA CORRODED. SCRATCH ON TOP OF BEAM RT SIDE, 12 INCHES FROM CENTER TO WALL. REPAIRED FLOORBEAM AT STA 294.5 FROM LBL 20 TO RT BULKHEAD PER SRM 53-10-51, SECTION 41, FIG 205. 2L72 4F RTA16WE 20041207001862004120700186NE 2004 12 7 200415 220040719A7230 IMPELLER DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE RT ENGINE FOD A KPVAK NONE C F.O.D. ININSP/MAINT 1 WP13806WP 357 PCE120968 RT ENGINE PCE 120968 1ST STAGE IMPELLER FOD DAMAGE. REMOVED AND REPLACED NR 2 ENGINE PCE 120968 IAW FORM IA M-105. O DEFECTS NOTED. 2H72 4T4 TRTA13NM E20NE 20041207001882004120700188SO 2004 12 7 CHQA000572 120041023A2810 FLAPPER VALVE EMB 145 EMB145LR 3260212SO LT WING FUEL LEAKING A CHQAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL11275 145345 DURING CLIMB-OUT ON FLIGHT 3098 FROM PHL TO CMH, FUEL WAS SEEN LEAKING OUT OF THE LEFT WING. STREAM WAS APPROXIMATELY 8 INCHES WIDE AND IT WAS COMING OUT AT A STEADY RATE UNTIL THE AIRCRAFT LEVELED OFF. THE STREAM WAS LOCATED APPROXIMATELY 6 TO 8 FEET FROM THE WING TIP AND WAS VISIBLE TO THE PILOT FROM THE COCKPIT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO THE FIELD IN PHL WITHOUT INCIDENT. MAINTENANCE FOUND THE FLAPPER VALVE BETWEEN THE MAIN FUEL TANK AND THE FUEL VENT BOX TO BE BAD. REMOVED AND REPLACED FLAPPER VALVE ASSEMBLY P/N 2770138-101 IAW EMB 145 MM 28-11-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041207001922004120700192NM 2004 12 7 USAA040875 120041111A572065C27359 FLANGE BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUEL PANEL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FUEL PLATE FLANGE, (2 EA) .189 INCH IN LENGTH, CRACK (2) FUEL PANEL NR 881, 17R, 6 O`CLOCK AND 12 O`CLOCK POSITIONS. STOP DRILLED CRACKS, TRIMMED SKIN PANEL, INSTALLED FILLER AND DOUBLER IAW EA 79453. 2L72 4F4 FRTA16WE E2GL 20041207001982004120700198WP 2004 12 7 DHL2004801011 120041023A33505708458505 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01801DH 46033 EMERGENCY LIGHT ARE INOP IN TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-1. CHECKED OPERATION OK. 2L74 4F RT4A25 20041208000022004120800002NM 2004 12 8 SWAA043476 120041130A532065C27314 CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 3 EACH STRINGER CLIPS CRACKED AT BS 400, STRINGER 4R AND STRINGER 4L, BS 520, STRINGER 16L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20041208000102004120800010NM 2004 12 8 SWAA043460 120041129A3397 WIRE BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 FWD EMERGENCY EXIT LIGHT AND WIRING LOOSE. SECURED LIGHT AND WIRING PER MM. 2L72 4F RTA16WE 20041208000112004120800011WP 2004 12 8 04FDEA03338 120041203A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AT EXT LWR FUSELAGE RT SIDE - SKIN B/T STA 765 - 890 WITH SEVERAL DENT BEYOND LIMITS. NICKS, GAUGES AND EXISTING REPAIRS WITH PULLED HEAD FASTENERS B/T LONG 36-48. REPLACE SIDE SKIN ADA 3139-501 PER DWG NDA 6013 AND LONG 43. REPLACE SCUFF PLATE PER MM 20-50-02. REINSTALL DBLL RAM 1470-31 PER DWG RAM1470- 7009. WORK IN IAW NRC NF 10376. REPLACE P/N: ADA 3139-501 QTY:1 ADA 3483-1 QTY: 1 ADA 3968-29 QTY:1 ADA 3483-501 QTY 1. 2L73 4F A22WE 20041208000432004120800043WP 2004 12 8 04FDEA03326 120041202A5330 PANEL DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND, BY ULTRASONIC INSPECTION, EA 3 PANELS CRACKED (NR 14 POSITION) P/N ALC7436-1. REPLACE PANELS PER SB 55-16, FIG 15 GROUP I, EA-8-5510-70126 P/N: SB10550016-7 KIT, SB10550016-117 KIT, 62525-7-16-7, 113LH7940T070. (OPEN) 2L73 4F A22WE 20041208000642004120800064NM 2004 12 8 SWAA043477 120041130A53156546811 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 1016, LBL 6, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2L72 4F RTA16WE 20041208000692004120800069NM 2004 12 8 TSAA0471076 120041111A7600 LINE BOEING737 7372X6C 1384552NM PWA JT8 JT8D9A 52048NE PT2 SENSE OBSTRUCTED A TSAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP13816AL 23122 FLT 840, NR 2 ENGINE PUTTING OUT LESS POWER THAN THE NR 1 ENGINE AT 1.89 EPR. SUSPECT NR 2 PT2 PROBE. REMOVED DEBRIS FROM THE PT2 SENSE TUBE BETWEEN THE ENGINE AND TRANSDUCER. ENGINE RUN-UP AND EPR CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20041208000702004120800070NM 2004 12 8 TSAA0426075 120041109A2612 FIRE LOOP BOEING737 737800* NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE MALFUNCTIONED A TSAAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 WP13805AL 21809 P655014 FLT 922, (NON-ETOPS) HAD ENGINE NR 2 FIRE INDICATION ON CLIMBOUT. SHUTDOWN ENGINE NR 2 AND FIRED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. RETURNED TO HNL. REPLACED THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20041208000732004120800073NM 2004 12 8 CALA0400730 120041126A3397BR964411 WIRE BOEING737 7373T0 1384582NM EMERGENCY LIGHT BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW2714324 23375 INSPECTION FOUND THE AISLE PATH EMERGENCY LIGHT FIXTURE AT SEAT 21 ABC INOPERATIVE DUE TO A BROKEN WIRE. THE LIGHT FIXTURE WAS REMOVED AND REPLACED. 2L72 4F RTA16WE 20041208000752004120800075 2004 12 8 SWAA043507 420041202A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29428WN 29844 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208000782004120800078NM 2004 12 8 DL757041052 120041120A5330146N35319 SKIN BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27690DL 27585 CORROSION WAS FOUND AROUND TWO AIRPHONE ANTENNA CUTOUTS AT FS 150 BETWEEN STRINGERS 28L & 29L AND BETWEEN 28R & 29R. THE CUTOUTS WERE INCREASED TO REMOVE THE CORROSION DAMAGE AND EACH LOCATION WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 095227-14. 2L72 4F RTA2NM 20041208000802004120800080NM 2004 12 8 DL757041054 120041123A2420111101020714 INVERTER BOEING757 757232 1384965NM E/E BAY SMOKE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27629DL 22919 FLT 1870 ATL-GSP REPORTED SMOKE/HAZE IN THE CABIN AND AT THE SAME TIME THE STBY INVERTER STATUS MSG DISPLAYED ON THE EICAS SYSTEM. UPON ARRIVAL GSP THE CONTRACT MECH CONFIRMED A STRONG ODOR IN THE FWD E/E COMPARTMENT AND NOTED THAT THE STBY INVERTER WAS DEFINITELY THE SOURCE OF THE SMOKE/ODOR. REPLACED INVERTER. 2L72 4F RTA2NM 20041208000822004120800082NM 2004 12 8 SWAA043521 120041204A5313BSC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED A1 CHECK, FOUND STRINGER 23R AT BS 499, CRACKED. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20041208000842004120800084NM 2004 12 8 SWAA043511 120041203A256065564161 BUTTON BOEING737 7373H4 1384600NM ESCAPE ROPE STUCK A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 CAPTAIN'S EMERGENCY ESCAPE ROPE DOOR BUTTON STUCK. LUBED AND ADJUSTED BUTTON PER MM. 2L72 4F RTA16WE 20041208000892004120800089SO 2004 12 8 MASA200400642 120041116A21214611028900 GASPER FAN EMB 145 EMB145LR 3260212SO CABIN SMOKE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07826MJ6301 145214 ASH 2734 CLT. CREW REPORTED A STRONG SMELL OF SMOKE IN THE COCKPIT. MAINTENANCE FOUND THE RECIRCULATION FAN TO BE FAILING AND DEFERRED THE RECIRCULATION FAN. MAINTENANCE REPLACED THE RECIRCULATION GASPER FAN. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041208000902004120800090NM 2004 12 8 P5CA0401280 120041119A561060B100286 WINDOW BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE COCKPIT CRACKED A P5CAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 EA15858FT 20109 ON CLIMBOUT FROM ANCHORAGE THE R1 WINDOW STARTED ARCING & CRACKING. A 15 INCH CRACK DEVELOPED ON THE TOP EDGE OF THE WINDOW. FUEL WAS JETTISONED & A/C RETURNED TO ANCHORAGE. REMOVED & REPLACED R1 WINDOW. 2L74 4F4 F A20WE E20EA 20041208000912004120800091 2004 12 8 P5CA0401276 420041116A341737571832 CADC BOEING747 747341 13848AMNM GE CF6 CF650C2 30018NE NR 1 INGESTED A P5CAK NONE J WARNING INDICATION ININSP/MAINT 1 EA15355MC 23395 NR 1 CADC INOPERATIVE. REPLACED NR 1 CADC, OPS CHECK OK PER AMM 34-12-01. 2L74 4F4 FRTA20WE E23EA 20041208000922004120800092NM 2004 12 8 P5CA0401279 120041117A7711 INDICATOR BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 3 ENG EPR NO INDICATION A P5CAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 EA15921FT 21575 688856 NR 3 ENGINE HAS NO EPR INDICATION WHEN ACCELERATING. TRANSFERRED TO DMI 33386 PER MEL 77-04-1. 2L74 4F4 F A20WE E3NE 20041208000932004120800093NM 2004 12 8 SWAA043527 120041205A53306545776 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 747 + 14, STRINGER 19R, CRACKED. REPAIRED SKIN SECTION PER SRM. 2L72 4F A16WE 20041208000942004120800094NM 2004 12 8 SWAA043513 120041203A3350OL307IBPEGL LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29332SW 23696 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 6 DEF, INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20041208000952004120800095 2004 12 8 SWAA043514 420041203A256565C16820 HOOK BOEING737 7373H4 1384600NM GIRT BAR SHEARED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR HOOK RIVET SHEARED. REMOVED AND REPLACED L1 DOOR AFT GIRT BAR HOOK RIVET PER SRM. 2L72 4F RTA16WE 20041208000962004120800096NM 2004 12 8 DL738041074 120041201A2500 BATTERY BOEING737 737832 13844CFNM CABIN MISSING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27381DA 30350 CABIN ROGER UNIT SMOKED IN FLIGHT. BATTERIES REMOVED BY FLIGHT ATTENDANT. CABIN ROGER UNIT NR 1995 SER NUMBER 101433 REMOVED FROM A/C BY GATE GOURMET. 2L72 4F RTA16WE 20041208000972004120800097NM 2004 12 8 DL767041075 120041201A1430NAS6706D26 BOLT BOEING767 767232 1385132NM RT MLG MISINSTALLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27101DA 22213 FOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIMS ARE MISSING. INSTALLED NEW BOLT AND HARDWARE PER AMM 32-12-06 AND IPC32-12-01-05 RIGHT MLG WING DOOR LOWER AFT MOUNT INSTALLATIONS NOW CORRECT OK FOR SERVICE. 2L72 4F RTA1NM 20041208000982004120800098NM 2004 12 8 DL76L041076 120041202A3830734285E BPCU BOEING767 767332 1382001NM E/E BAY INOPERATIVE A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO27179DN 25144 ALL LAVS INOP, NO RINSE WATER, NO VACUUM. A/C DIVERTED TO JFK. REMOVED AND REPLACED RELAY K546 AND THE BPCU. ALL LAVS OPERATE NORMALLY. 2L72 4F RTA1NM 20041208000992004120800099EU 2004 12 8 MALA040709 120040902A5753 HINGE BAC 146 AVRO146RJ85A1500097EU FLAP TAB WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, RT WING FLAP TAB NR 1 HINGE HAS WEAR MARKS ON SKIN BY HINGE COVER. MAINTENANCE REPAIRED IAW EO NR A57073. AIRCRAFT RETURNED TO SERVICE 9/14/04. REFER TO 409 CARD NR 187019 FOR ADDITIONAL INFORMATION. 2H74 4F RTA49EU 20041208001012004120800101EU 2004 12 8 MALA040713 120040827A5330 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, 3 DENTS FOUND ON LT FUSELAGE SKIN AFT OF FRAME 20. MAINTENANCE REPAIRED IAW EO A53196. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208001052004120800105EU 2004 12 8 MALA040723 120040909A5414 COWLING BAC 146 AVRO146RJ85A1500097EU NR 4 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, NR 4 ENGINE RIGHT ZONE 2 COWL CHAFED IN PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041208001072004120800107NE 2004 12 8 TSAA0472079 220041127A7200 ENGINE BOEING737 73725A 1384481NM PWA JT8 JT8D9A 52048NE NR 2 FAILED A TSAAA UNSCHED LANDING EX VIBRATION/BUFFET ENGINE FLAMEOUT CLCLIMB 1 WP13819AL 23791 P674319 NON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGINE EPR DROPPED FROM 1.82 TO 1.76. REPORTED THAT A PASSENGER OBSERVED FLAMES EXITING THE NR 2 ENGINE EXHAUST. ALL OTHER ENGINE INDICATIONS WERE NORMAL. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 2 ENGINE IN ACCORDANCE WITH FORM M-212, M213, M215, AND M211. LEAK AND OPS CHECK GOOD. AIRPLANE RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20041208001082004120800108CE 2004 12 8 DXTA200400453 120041119A2750 WARNING SYSTEM CESSNA750 750 2076810CE TE FLAPS ACTIVATED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07960QS 7500160 AFTER TAKEOFF, SELECTED FLAPS UP, FLAPS WERE AT ZERO. THE AMBER YD FAIL A-B, CAS MESSAGE ILLUMINATED ON THE CONTROL PAGE. IT SHOWED THE UPPER FAILED TO THE RIGHT OF THE AVAILABLE GREEN LIMIT. SELECTED THE UPPER BUTTON AND THE CAS WENT OUT, UPON LANDING DID A GO-AROUND. SELECTED THE FLAPS BACK TO ZERO, THE "CYAN YD FAIL UPPER A" MESSAGE ILLUMINATED AND STAYED ON FOR LANDING. REMOVED AND REPLACED BOTTOM ("A") YSAS COMPUTER. SYS OPS CHECK GOOD IAW 750 MM CHP 27-24-01. 2L72 4J RTT00007WI 20041208001092004120800109NM 2004 12 8 CALA0400735 120041203A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND CABIN RIGHT O/B SEAT TRACK CORRODED AT STA 328-360, RBL 48 TO LBL 48. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52. 2L72 4F RTA16WE 20041208001132004120800113NM 2004 12 8 SWAA043463 120041129A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP AT BS 1016, RBL 1, CRACKED. REPAIRED BULKHEAD PER EA. 2L72 4F RTA16WE 20041208001142004120800114NM 2004 12 8 DL757041082 120041204A3350 WIRE BOEING757 757232 1384965NM EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27681DA 26957 ON CHECK FOUND EMERGENCY LIGHTS IN F/C AISLE INOP. REPAIRED BROKEN WIRE UNDER SEAT 1D AND REPLACED FUSE ON POWER SUPPLY. LIGHTS OP NORMAL. 2L72 4F RTA2NM 20041208001172004120800117SO 2004 12 8 MASA200400648 120041122A3397 CONNECTOR EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07852MJ 145567 ASH 2854 CLT-SDF. THE CREW REPORTED THE EMERGENCY EXIT SIGN AT THE EMERGENCY EXIT ROW INOPEATIVE. MAINTENANCE FOUND THE CONNECTOR FOR THE LIGHT ASSEMBLY DISCONNECTED. RECONNECTED THE CANNON PLUG AND THE SYSTEM CHECKED NORMALLY. 2L72 4T RTT00011AT 20041208001192004120800119NM 2004 12 8 DLM88041083 120041205A2150 ACM DOUG MD88 MD88 3023688NM RT ACM BAY ODOR A DALAB EMER. DESCENT BG SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CRCRUISE 1 SO27906DL 49537 AT FL310 RT PACK TRIPPED AFTER RUNNING FULL HOT. STARTED DESCENT AND LEFT PACK ALSO TRIPPED. CABIN APPROACHED 10,000. F/A'S NOTICED SMELL FROM PACKS IN CABIN. PACKS RECOVERED AFTER LEVEL AT 8000 FT. INSPECTED LT AND RT PACKS FOR BLOWN DUCTS AND ACM'S FOR ROTATION, ALL OK. CLEANED CABIN AND COCKPIT TEMP SENSORS. RAN PACKS IN AUTO AND MANUAL FULL COLD AND FULL HOT WITH APU AND ENGINES. ALL OPN IS NORMAL. PACKS CHECK OK. 2L72 4F RTA6WE 20041208001202004120800120NM 2004 12 8 DLM88041084 120041205A3510359701025 VALVE DOUG MD88 MD88 3023688NM OXYGEN MASK STICKING A DALAB EMER. DESCENT O OTHER CRCRUISE 1 SO27906DL 49537 CAPT'S O2 MASK HAS STICKING VALVE. FOUND KINK IN O2 MASK SUPPLY LINE. REPLACED MASK ENCLOSURE BOX PER M/M. LEAK AND OPERATIONAL CKECK GOOD. 2L72 4F RTA6WE 20041208001222004120800122NM 2004 12 8 SWAA043453 120041126A53306545767 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 445, STRINGER 10R, CRACKED. REPAIRED SKIN PER ACO. 2L72 4F RTA16WE 20041208001242004120800124NM 2004 12 8 SWAA043465 120041130A3350BR2013 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29793SA 27888 FWD EEPLS FLOOR TRACK LOOSE. REMOVED AND REPLACED EEPLS LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041208001262004120800126NM 2004 12 8 SWAA043467 120041130A575465C266022AA SKIN BOEING737 7373H4 1384600NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED LT NR 2 L/E SLAT PER MM. 2L72 4F RTA16WE 20041208001272004120800127NM 2004 12 8 SWAA043468 120041130A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 485, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041208001302004120800130 2004 12 8 SWAA043446 420041125A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR SLIDE MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20041208001342004120800134NM 2004 12 8 SWAA043450 120041126A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BUTT STRAP AT BS 908, STRINGER 11L, CRACKED. REPAIRED BUTT STRAP PER SRM. 2L72 4F RTA16WE 20041208001362004120800136EU 2004 12 8 MALA040716 120040903A5320HC255HY242000 PANEL BAC 146 AVRO146RJ85A1500097EU CARGO BAY DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, FWD CARGO PANEL DAMAGED. MAINTENANCE REPLACED WITH NEW PANEL. P/N HC255HU242-000. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208001372004120800137 2004 12 8 SWAA043454 420041126A256563550 SLIDE BOEING737 7377AD 1384502NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208001392004120800139NM 2004 12 8 SWAA043489 120041201A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 426, STRINGER 16R, CRACKED. REPAIRED SKIN SECTION PER EA. 2L72 4F RTA16WE 20041208001402004120800140SO 2004 12 8 MASA200400657 120041127A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07828MJ 145218 ASH 2693 CLT-LIT. ROW 1 AND 2 EMERGENCY LIGHT INOP. MAINTENANCE RESECURED THE CONNECTION AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20041208001412004120800141EU 2004 12 8 MALA040721 120040916A5320 BRACKET BAC 146 AVRO146RJ85A1500097EU MLG WW CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, GEAR BAY SEPARATOR LT FORWARD BRACKET CRACKED. MAINTENANCE MANUFACTURED NEW BRACKET & INSTALLED IAW SRM 53-20-16 FIG 3. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041208001422004120800142NM 2004 12 8 DL73S041058 120041124A555365468725 FITTING BOEING737 737247 138448DNM VERTICAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 VERTICAL STABILIZER ATTACH FITTINGS NR 3 AND NR 6 LUGS WORN ON THE AFT FACES DUE TO CORROSION. REPAIRED IAW ERA 095030-14. 2L72 4F A16WE 20041208001442004120800144NE 2004 12 8 DL76G041077 220041202A7200CF680C2B6 ENGINE BOEING767 7673P6 1385105NM GE CF6 CF680C2B6 30025NE NR 1 UNKNOWN A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO271501P366857253 24983 695438 SHORTLY AFTER T/O WITH ALL PARAMETERS NORMAL ON BOTH ENGINES THE LEFT ENGINE FIRE WARNING ANNUNCIATED. THE CREW PULLED BACK THE THROTTLE AND THE FIRE WARNING EXTINGUISHED. THE CREW ELECTED TO SHUT DOWN THE ENGINE. NO FIRE BOTTLES WERE BLOWN. A/C DID A ATB TO ATL. THE A/C ARRIVED WITH NO EVIDENCE OF FIRE DAMAGE. ENGINE REPLACED. 2L72 4F4 FRTA1NM E13NE 20041208001452004120800145EU 2004 12 8 MALA040708 120040911A5754 SKIN BAC 146 AVRO146RJ85A1500097EU LT WING LE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, LT WING FLAP INBOARD TAB LEADING EDGE CHAFED AT CENTER ATTACH POINT. MAINTENANCE REPAIRED IAW EO A57073. A/C RETURNED TO SERVICE 09/14/2004. 2H74 4F RTA49EU 20041208001462004120800146EU 2004 12 8 MALA040711 120040908A5755 SKIN BAC 146 AVRO146RJ85A1500097EU SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, RT WING CENTER LIFT SPOILER TRAILING EDGE CRACKED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208001472004120800147 2004 12 8 SWAA043515 420041203A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208001492004120800149EU 2004 12 8 MALA040726 120040909A5414 COWLING BAC 146 AVRO146RJ85A1500097EU NR 2 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, NR ENGINE LEFT ZONE 2 COWL CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041208001522004120800152NM 2004 12 8 P5CA0401281 120041205A2740 CHAIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE STAB TRIM WHEEL CONTAMINATED A P5CAO OTHER O OTHER NRNOT REPORTED 1 EA15858FT 20109 DURING STAB TRIM CHECK STAB TRIM BINDING IN BOTH ELECTRICAL & MANUAL. CLEANED DEBRIS ON STAB TRIM CONTROL WHEEL CHAIN, INDICATIONS CHECKED NORMAL. 2L74 4F4 F A20WE E20EA 20041208001542004120800154NM 2004 12 8 TSAA0426077 120041115A2697 CONNECTOR BOEING737 7372M6C 1384708NM PWA JT8 JT8D9A 52048NE FIRE LOOP DAMAGED A TSAAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 WP13805AL 21809 P655014 FLT 942, HNL-KOA: (NON-ETOPS) AFTER ENGINES WERE STARTED, THE NR 2 ENGINE FIRE WARNING SWITCH AND BELL CAME ON. FOLLOWED THE QRH AND SHUT DOWN THE ENGINE. REPLACED THE HERMETIC CONNECTORS ON THE NR 2 ENGINE LOWER FIRE DETECTION LOOP. ACCOMPLISHED HIGH POWER ENGINE RUN WITH NO FIRE WARNING INDICATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20041208001552004120800155NM 2004 12 8 SWAA043529 120041205A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041208001582004120800158NM 2004 12 8 SWAA043500 120041202A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29397SW 27691 BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 16 DEF, MISSING. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041208001592004120800159NM 2004 12 8 SWAA043501 120041202A3350604222 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29730SW 27862 DURING SCHEDULED MV1 CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041208001602004120800160NM 2004 12 8 SWAA043502 120041202A555265C263868 FITTING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29611SW 27697 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB INBOARD HINGE HAS PLAY. REMOVED AND REPLACED INBOARD ELEVATOR TAB HINGE FITTING PER MM. 2L72 4F RTA16WE 20041208001662004120800166NM 2004 12 8 MASA200400424 120040724A242131708001A GENERATOR DHAV DHC8 DHC8202 2809007NM NR 1 INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07455YV6130 2571 455 ASH 7035 RAP-DEN. THE CREW ABORTED TAKEOFF DUE TO A LEFT TRU FAIL FOLLOWED BY THE NR 1 A/C GENERATOR FAILING. MAINTENANCE IS WORKING PROBLEM 7/25. MX REPLACED AC GENERATOR AND THE GCU (GCU P/N 51608-001A). 2H72 4T RTA13NM 20041208001692004120800169EU 2004 12 8 RAIR00411021 120041120A7712 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU RT TORQUE INOPERATIVE A RAIAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 CE03552HK 41057 STL - RIGHT TORQUE GAUGE DASHED LINES. MAINTENANCE PERFORMED ENGINE GROUND RUNS. OPS CHECK OK, COULD NOT DUPLICATE. 2L72 4T RTA41NM 20041208001722004120800172SO 2004 12 8 RAIA00411018 120041119A2530LBG16707 CONNECTOR EMB 145 EMB145ER 3260211SO COFFEEMAKER BURNED A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03808HK 145157 RIC - SMELL IN CABIN. MAINTENANCE INSPECTED HOT JUGS AND FOUND BOTH CONNECTOR BURNED. REMOVED AND REPLACED HOT JUG CONNECTORS. 2L72 4F RTT00011AT 20041208001742004120800174SO 2004 12 8 SWIA200414150 120041125A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0758733 120197 EXIT SIGN FROM ROW 6A AT THE FLOOR FELL OFF. REPLACED LEFT OVERWING EMERGENCY EXIT IAW EMB 120 MM 33-00-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001752004120800175EU 2004 12 8 RAIA00412001 120041201A7933696230 INDICATOR JETAIRJETSTMJETSTM4101 1500501EU LT OIL TEMP MALFUNCTIONED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03573HK16017404 41092 STL - LEFT OIL TEMP SHOWING AT 45 DEGREES CELSIUS. MAINTENANCE REMOVED AND REPLACED LT OIL TEMP GAUGE. 2L72 4T RTA41NM 20041208001772004120800177SO 2004 12 8 SWIA200414152 120041124A2510 SEAT EMB 120 EMB120ER 3260203SO CABIN OUT OF POSITION A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07213SW 120277 FORWARD DOOR WILL NOT OPEN. FOUND FORWARD DOOR HANDLE HITTING F/A JUMPSEAT, REPOSITIONED F/A SEAT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001782004120800178EA 2004 12 8 SWIA200414153 120041128A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07962SW 7859 SPOILERON FAULT STATUS MESSAGE ON ED NR 2. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041208001802004120800180 2004 12 8 SWIA200414155 420041128A2340509612 HEADSET EMB 120 EMB120ER 3260203SO INTERPHONE SMOKE A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07236SW8281 8281 120312 F/A REPORTS SMOKE COMING FROM INTERPHONE IN AFT GALLEY. REPLACED AFT ATTENDANT HEADSET IAW MM 23-41-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001812004120800181NM 2004 12 8 DL73S041066 120041129A53136552988538 STRINGER BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 STRINGER 5L AND AFT ENTRY BEAR STRAP SUFFERED DAMAGE. REPAIRED IAW ERA 094945-14. 2L72 4F A16WE 20041208001822004120800182NM 2004 12 8 DL738041067 120041129A3246B73738N WHEEL BOEING737 737832 13844CFNM RT NLG SEPARATED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO2737700 29631 NOSE WHEEL TIRE PROBLEM ON TAKEOFF. REPLACED BOTH NOSE WHEELS. 2L72 4F RTA16WE 20041208001832004120800183NM 2004 12 8 DL73S041068 120041130A5551 FITTING BOEING737 737247 138448DNM HORIZONTAL STAB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 HORIZONTAL STABILIZER RT AND LT CENTER AND OUTBOARD SECTION LUG FITTINGS AT THE FRONT AND REAR SPAR CORRODED AND DAMAGE. REPAIRED IAW ER/A 094975-14AD & 094865-14AD. 2L72 4F A16WE 20041208001842004120800184NM 2004 12 8 DL733041069 120041130A3397 WIRE HARNESS BOEING737 737347 1384647NM COCKPIT BURNED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27313WA 23599 JUST PRIOR TO T/O WHEN LANDING LIGHTS TURNED ON, SPARKS CAME FROM OVERHEAD PANEL. TURNED OFF LIGHTS SPARKS STOPPED. REPAIRED WIRE BUNDLE IN OVERHEAD. 2L72 4F RTA16WE 20041208001852004120800185NM 2004 12 8 DL738041070 120041130A56102314M106 ARM BOEING737 737832 13844CFNM WINDSHIELD CRACKED A DALAO OTHER O OTHER LDLANDING 1 SO27379DA 30349 CAPTAINS WINDSHIELD WIPER ARM BROKE OFF .25 INCH ABOVE TENSIONING MECHANISM. 2L72 4F RTA16WE 20041208001862004120800186NM 2004 12 8 SWAA043473 120041130A53116554892 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 344, STRINGER 22L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041208001872004120800187NM 2004 12 8 SWAA043478 120041130A531365C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 482, STRINGER 14R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041208001892004120800189NM 2004 12 8 SWAA043455 120041126A53156546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 616, FLOORBEAM LT ATTACH POINT CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041208001902004120800190NM 2004 12 8 SWAA043456 120041128A335010107451 SIGN BOEING737 7377H4 1384404NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29717SA 27851 EMERGENCY EXIT SIGN AT AFT SERVICE DOOR BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2L72 4F RTA16WE 20041208001912004120800191NM 2004 12 8 SWAA043457 120041128A33507003661 BALLAST BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29776WN 30591 DURING SCHEDULED MV2 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20041208001942004120800194SO 2004 12 8 SWIA200414158 120041124A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07393SW1018510185 120330 LEFT INBOARD FLAP DROOPS. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001972004120800197EA 2004 12 8 SWIA200414161 120041119A2751601R590141 DETECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07955SW 7817 WHEN FLAPS 45 DEGREES SELECTED AIRPLANE ROLLS TO THE LEFT. FLAPS FAIL AND FLAPS DEGRADED MESSAGE. REMOVED AND REPLACED SKEW SENSOR ON RIGHT OUTBAORD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-51-15. OPERATIONAL CHECK GOOD. P/N 601R59014-1, S/N R431. 2L72 4F RTA21EA 20041208001992004120800199EA 2004 12 8 SWIA200414163 120041127A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07445SW 7651 FIRST GREEN SECTION OF THE EMERGENCY FLOOR PATH LIGHTS IS OUT. REPLACED FORWARD GREEN EMERGENCY FLOOR LIGHTING STRIP IAW CRJ MM 33-51-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041208002022004120800202NM 2004 12 8 SWAA043495 120041201A53306545773 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 797 AND BS 817, STRINGER 13L. REPAIRED SKIN SECTIONS PER ER. 2L72 4F RTA16WE 20041209000012004120900001 2004 12 9 SWAA043538 420041205A256565C16820 HOOK BOEING737 7375H4 138449DNM L1 GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE GIRT BAR AFT HOOK, CORRODED. REMOVED AND REPLACED GIRT BAR HOOK PER MM. 2L72 4F RTA16WE 20041209000032004120900003NM 2004 12 9 SWAA043534 120041205A53306545857 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY SERVICE DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041209000042004120900004NM 2004 12 9 SWAA043535 120041205A533066545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 875334 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FUSELAGE CUTOUT AT LOWER AFT CORNER, FUSELAGE CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041209000052004120900005NM 2004 12 9 SWAA043536 120041205A53306552880 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT, LOWER FWD CORNER, FUSELAGE SKIN, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041209000062004120900006EA 2004 12 9 04330649 120041125A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA ENGINE MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27649BR 7414 L 14TH STAGE DUCT WARNING. ENGINE AT IDLE. DIVERT TO NEAREST AIRPORT, LANDED SAFELY. MX REMOVED AND REPLACED DUCT LOOP. 2L72 4F RTA21EA 20041209000072004120900007 2004 12 9 SWAA043532 420041205A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041209000102004120900010NM 2004 12 9 SWAA043540 120041206A3350PH22300L LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29352SW 24888 FWD EEPLS STRIP LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20041209000112004120900011 2004 12 9 SWAA043541 420041206A2565D31354 SLIDE BOEING737 7373Y0 1384671NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 R1 DOOR EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041209000122004120900012 2004 12 9 C2XA04RI016 420041128A234054821MODD AMPLIFIER EMB 145 EMB145LR 3260212SO PA FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW27129961027610275 145296 ORF - FLT 2017, DURING PREFLIGHT CHECK THE CREW FOUND CABIN AND CABIN EMERGENCY LIGHTS IN OVERHEAD PANEL ILLUMINATED AND CABIN INTERPHONE AND PA INOP. MAINTENANCE REMOVED AND REPLACED PA AMP. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041209000132004120900013SO 2004 12 9 C2XA04BT119 120041123A33501317 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT BURNED OUT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713965 145125 DURING SERVICE AND ROUTINE CHECK, MAINTENANCE FOUND RIGHT HAND OVERWING EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACED RIGHT HAND EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041207000742004120700074WP 2004 12 7 UPS04843511 120041030A53403755822U515 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 C1 BATH-TUB FITTING CRACKED AT STA300 L27L-L28L. REMOVED CRACKED FITTING AND FABRICATED REPAIR PARTS REF SRM53-2-0 FIG 2D. INSTALLED REPLACEMENT FITTING AND SPLICE ANGLES REF SRM 53-2-0 FIG2D AND SRM 51-1-20D. 2L74 4F RT4A25 20041207000922004120700092NM 2004 12 7 USAA040878 120041014A5340 ATTACH BRACKET BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 ATTACH BRACKET, .5 INCH LONG CRACK, S10L, STA 360. MANUFACTURED ATTACH BRACKET IAW SRM 51-40-03. 2L72 4F4 FRTA16WE E2GL 20041207001162004120700116NM 2004 12 7 USAA040850 120041021A5313 STRINGER BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 STRINGER, .5 INCH LONG CRACK, STR 7L AT BS 1010. INSTALLED REPAIR ANGLE IAW 53-00-03. 2L72 4F4 FRTA16WE E2GL 20041207001242004120700124WP 2004 12 7 IXXA0400091S 120040521A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE EXTERNAL AC POWER RECEPTACLE EXTERNAL SKIN HAS INTERIM REPAIR AT FS 32.000, L-31R TO L-32R. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIR IAW DC8 SRM 51-1-21 PAGES 1, 2. REMOVED DAMAGED AREA IAW DC8 SRM 53-2-0 PAGES 2K FIG 10. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 53-2-0 PAGE 2K FIG 10. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 51-1-20D PAGE 9, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20041207001802004120700180CE 2004 12 7 66067 120041023A3242 BRAKE BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07144ZV UE144 UPON TAXI IN TO DUJ, CREW NOTICED LT BRAKING SPONGY. AIRCRAFT PARKED AND SHUT DOWN WITH NO FURTHER INCIDENT. BLEED BRAKES, OPS CK GOOD. 2L72 4T RTA24CE 20041207001972004120700197 2004 12 7 IXXA0400111O 420041004A34221428302001 FIBER OPTIC GYRO DOUG DC8 DC862 3021970WP COCKPIT FAULTY A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW1131CX 794273451 45911318 AFTER TAKEOFF FROM KCOF, CAPTAINS ADI GYRO "OFF FLAG" AND NR 1 COMPASS "OFF FLAG" APPEARED. CREW RETURNED AIRCRAFT TO KCOF AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FOG GYRO PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20041208000202004120800020NM 2004 12 8 DL73S041071 120041130A5330655298862 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27331DL 23103 A 1 INCH CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP AT THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER B737 SRM AND ER/A 095399-14, REV A. 2L72 4F RTA16WE 20041208000242004120800024SO 2004 12 8 RAIA00412002 120041201A801135059106 STARTER EMB 145 EMB145LR 3260212SO NR 1 ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03830HK2673 33 145313 STL - NR 1 ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 STARTER. 2L72 4T RTT00011AT 20041208000282004120800028NM 2004 12 8 CALA0400732 120041201A3350D71702030 CHARGER BOEING737 737724 13844BYNM EMERGENCY LIGHT INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2717719 28938 MAINTENANCE FOUND ALL THE EMERGENCY EXIT LIGHTS THAT RUN OFF OF BATTERY PACK M1670 INOPERATIVE. THE BATTERY CHARGER UNIT WAS REMOVED AND REPLACED IAW MM 33-51-06. 2L72 4F RTA16WE 20041208000402004120800040WP 2004 12 8 04FDEA03210 120041125A5730ARC11132 SKIN DOUG DC10 DC1010 3022110WP RT WING DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING OUTBD AILERON B/T STA XOA1006/1023 FOUND LOWER SIDE FASTENERS PULLED THROUGH IN THE SKIN AND 1EA WITH HEAD BROKEN. REPLACE SKIN PER SRM 51-35-01 PG 1-12 AND REBALANCE PER SRM 57-50-00. 2L73 4F A22WE 20041208000452004120800045EU 2004 12 8 04FDEA03328 120041202A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 MDCC RIGHT NR 2 SEAT TRACK HAS CORROSION AT FR 52.8, 51.2, 50.51, 49.5 AND 48.5. REMOVED AND REPLACED SEAT TRACK FROM FR STA 46 TO FR STA 54 RBL 15. 2L72 4F RTA35EU 20041208000482004120800048EU 2004 12 8 04FDEA03331 120041202A5321 FLOOR PANEL AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 BULK CARGO FLOOR STRUCTURE FR 69 FROM LT UP TO RT CORNER FLOOR STRUCT W/5 AREAS OF CORROSION TOP TO UNDERNEATH SURFACE. REMOVED AND REPLACED T-PROFILES AT FR 66-69 RBL 37 AND FR 66.5-69 LBL 27. 2L72 4F RTA35EU 20041208000492004120800049EU 2004 12 8 04FDEA03332 120041202A5310 STRUCTURE AIRBUS310 A310222 3930315EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 BULK CARGO FLOOR STRUCT RT SIDE FR 64 TO 67 FLOOR STRUCT W/MULTIPLE CORROSION FROM TOP TO UNDERNEATH SURFACE. REMOVED AND REPLACED T- PROFILE AT FR63 TO FR 67 RBL 37 RT IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20041208000682004120800068NM 2004 12 8 SWAA043472 120041130A53116546549 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041208000762004120800076NM 2004 12 8 CALA0400733 120041203A5347BAC1520792 GALLEY TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 275-294, RBL 43. A NEW FLOOR TRACK SECTION WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20041208000852004120800085 2004 12 8 SWAA043517 420041203A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208000862004120800086 2004 12 8 SWAA043518 420041203A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041208001002004120800100EU 2004 12 8 MALA040710 120040910A5755 SKIN BAC 146 AVRO146RJ85A1500097EU SPOILER TE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, LEFT WING OUTBOARD LIFT SPOILER TRAILING EDGE CRACKED NEAR INBOARD END. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208001022004120800102EU 2004 12 8 MALA040715 120040902A5280 DOOR BAC 146 AVRO146RJ85A1500097EU MLG CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, RT MLG DOOR AFT RECESS IS CRACKED AT FWD INBOARD CORNER. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041208001102004120800110NM 2004 12 8 CALA0400736 120041203A5347BAC1520792 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND CABIN RIGHT I/B SEAT TRACK CORRODED AT STA 328-355, BL 0 TO RBL 23. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 202. 2L72 4F RTA16WE 20041208001112004120800111NM 2004 12 8 SWAA043461 120041129A53156545410 FLOORBEAM BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH CRACKS ON FLOORBEAM WEB AND FLOORBEAM UPPER CAP AT CENTER FLOORBEAM, BS 663.75. REPAIRED FLOORBEAM CHORD AND UPPER CAP PER ER. 2L72 4F RTA16WE 20041208001282004120800128NM 2004 12 8 DL76G041064 120041127A2530828450407 OVEN BOEING767 767332 1382001NM FWD GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271607B 30388 STRANGE ELECTRICAL SMELL FROM FWD GALLEY. ALSO STRANGE VIBRATION NOISE LIKE A LOOSE FAN POSSIBLY. DEPOWERED FWD GALLEY, NOISE AND SMELL STOPPED. FOUND NR 1 OVEN IN FWD GALLEY C/B POPPED. REPLACED SAME. 2L72 4F RTA1NM 20041208001312004120800131NM 2004 12 8 SWAA043447 120041125A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 23R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041208001322004120800132NM 2004 12 8 SWAA043448 120041125A533065C38450 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29311SW 23333 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041208001332004120800133NM 2004 12 8 SWAA043449 120041125A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED C3 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 747 AND BS 867, BETWEEN STRINGERS 21L AND 24L. REPAIRED SKIN SECTIONS PER EA AND SRM. 2L72 4F RTA16WE 20041208001352004120800135NM 2004 12 8 SWAA043451 120041126A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS BETWEEN BS 767 AND BS 787, STRINGER 14R. REPAIRED SKIN SECTIONS PER SRM. 2L72 4F RTA16WE 20041208001432004120800143NM 2004 12 8 CALA0400737 120041204A53126546568519 STIFFENER BOEING737 7373T0 1384582NM BULKHEAD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND APB BOTTOM CENTER STIFFENER CORRODED ON LEFT HALF, BS 1016-1020. THE CORRODED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW ECRA 5311-01213. 2L72 4F RTA16WE 20041208001502004120800150NM 2004 12 8 SWAA043522 120041204A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29327SW 23691 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 400 + 4, STRINGER 16R, CRACKED. REPAIRED SKIN SECTION PER SRM. 2L72 4F RTA16WE 20041208001512004120800151NM 2004 12 8 SWAA043528 120041205A335065C34691 LIGHT BOEING737 7373H4 1384600NM ROW 21 ABC LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 21 ABC, LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20041208001532004120800153NM 2004 12 8 SWAA043523 120041204A575465C26686 SKIN BOEING737 7373H4 1384600NM NR 6 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RT WING NR 6 L/E SLAT SKIN PER SRM. 2L72 4F RTA16WE 20041208001572004120800157NM 2004 12 8 SWAA043531 120041205A53306545774 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 797, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041208001762004120800176SO 2004 12 8 SWIA200414151 120041125A2750 SELECTOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07189SW 120048 AFTER TAKEOFF UPON FLAP RETRACTION, FLAP CONTROL FAULT. REPLACED FLAP LEVER SELECTOR IAW MM 27-50-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001792004120800179SO 2004 12 8 SWIA200414154 120041121A27523430001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07561SW 120335 FLAP RETRACTION GENERATES A DISAGREEMENT ON TAXI. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. 2L72 4T RTA31SO 20041208001932004120800193SO 2004 12 8 SWIA200414157 120041120A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 NM07586SW3289 1411 120354 IN FLIGHT HAD CONTROL FAULT FLAP WARNING INDICATION. REMOVED AND REPLACED FLAP CONTROL COMPUTER IAW MM 27-50-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041208001952004120800195EA 2004 12 8 SWIA200414159 120041023A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07457SW 7773 AFT EQUIPMENT COMP, INTERCOSTAL CLIP IS CRACKED; FS 625.00; STR 14R. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16 AND 51-21-11. 2L72 4F RTA21EA 20041208001982004120800198 2004 12 8 SWIA200414162 420041125A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07215SW 120281 NR 1 STALL WARNING STAYS ON MAP AFTER TESTING. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 120-291. 2L72 4T RTA31SO 20041208002002004120800200EA 2004 12 8 SWIA200414164 120041122A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07595SW 7292 EMERGENCY EXIT FLOOD LIGHT BY PASSENGER DOOR BROKE. REMOVED AND REPLACED EMERGENCY EXIT FLOODLIGHT IAW MM 33-51-19, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041208002012004120800201SO 2004 12 8 SWIA200414165 120041129A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07563SW 120338 EMERGENCY LIGHT STRIP A BEAM MAIN CABIN DOOR IS INOPERATIVE. REPAIRED WIRE TO THE FORWARD RED LIGHT EMERGENCY LIGHT FLOOR STRIP. OPERATIONAL TEST GOOD. 2L72 4T RTA31SO 20041209000022004120900002NM 2004 12 9 SWAA043551 120041206A53116546593 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 500A, BETWEEN LBL 6 AND RBL 6, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041209000142004120900014EU 2004 12 9 SWAA043542 220041206A7261CFM567B22G2 ENGINE BOEING737 7377H4 1384404NM CFMINTCFM56 CFM562AFR 13802EU NR 2 MALFUNCTIONED A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW29757LV 29850 INFLIGHT SHUTDOWN, DIVERSION, DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT FL 410, FOLLOWED QRH, SHUT DOWN ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2L72 4F4 FRTA16WE E21EU 20041209000152004120900015NM 2004 12 9 SWAA043554 120041206A53206551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 907, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20041209000172004120900017SO 2004 12 9 C2XA04IA153 120041128A33503025101 LIGHT EMB 145 EMB145 3260210SO FUSELAGE INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 MCI - DURING ROUTINE INSPECTION THE FORWARD LEFT HAND OUTBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY IN ACCORDANCE WITH EMB-145 AMM 33-50-10 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041209000182004120900018SO 2004 12 9 C2XA04IA154 120041128A3350110049 POWER SUPPLY EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714959 145091 MCI - DURING ROUTINE INSPECTION THE REAR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY POWER SUPPLY IN ACCORDANCE WITH EMB-145 AMM 33-50-04 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041209000192004120900019NM 2004 12 9 SWAA043497 120041201A53126546568 BULKHEAD BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND AFT PRESSURE BULKHEAD AT BS 1016, BL 0, 4 INCHES ABOVE CENTER WEB, CRACKED. REPAIRED AFT BULKHEAD PER ER. 2L72 4F RTA16WE 20041209000202004120900020NM 2004 12 9 SWAA043498 120041201A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND BUTT STRAP AT BS 907, STRINGER 4R, CRACKED. REPAIRED BUTT STRAP PER SRM. 2L72 4F RTA16WE 20041209000212004120900021 2004 12 9 SWAA043499 420041201A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29434WN 32454 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041209000222004120900022 2004 12 9 SWAA043487 420041201A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 DURING SCHEDULED RON, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041209000232004120900023NM 2004 12 9 SWAA043488 120041201A2121215201 FAN BOEING737 7373T0 1384582NM E&E BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29684WN 23941 PAX AND F/A REPORT STRANGE SMELL IN CABIN. SMELL OF SULFUR, TURNED OFF RECIRC FAN, SMELL DISSIPATED. GASPER FAN C/B TRIPPED. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20041209000242004120900024EU 2004 12 9 MALA040720 120040916A5320 ANGLE BAC 146 AVRO146RJ85A1500097EU MLG WW CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, GEAR BAY SEPARATOR LT UPPER ANGLE CRACKED. MAINTENANCE REPAIRED BY MANUFACTURING NEW ANGLE & INSTALLING IAW SRM 51-42-00, 51-24-11, 51-25-00, 51-23-00, 51-31-00, 51-41-00, 51-43-00, & 53-20-16. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041209000272004120900027EU 2004 12 9 MALA040705 120040902A5755 SKIN BAC 146 AVRO146RJ85A1500097EU SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, LEFT WING ROLL SPOILER TRAILING EDGE CRACKED IN TWO LOCATIONS. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RELEASE DATE 9/14/04. 2H74 4F RTA49EU 20041209000302004120900030SO 2004 12 9 MASA200400638 120041115A7830 WARNING SYSTEM EMB 145 EMB145LR 3260212SO THRUST REVERSER ACTIVATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07831MJ 145273 ASH 2610 CAE-CLT. DURING TAKEOFF ROLL THE CREW ABORTED TAKEOFF DUE TO A NR 2 ENGINE REVERSER DISAGREE MESSAGE. THE AIRCRAFT WAS RETURNED TO THE GATE. THE SYSTEM WAS DEFERRED AND THE AIRCRAFT RETURNED TO SERVICE. 11/19 MAINTENANCE PERFORMED OPS CHECK AND ALL CHECKED GOOD. NO FURTHER ACTION WAS REQUIRED. NO PARTS USED. 2L72 4T RTT00011AT 20041209000322004120900032SO 2004 12 9 MASA200400668 120041129A5240 SEAL EMB 145 EMB145LR 3260212SO SERVICE DOOR LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07848MJ 145530 ASH 2665 CLT HAD A SERVICE DOOR THAT WAS DIFFICULT TO OPERATE. MAINTENANCE LUBED THE DOOR AND THE DOOR SEAL. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041209000332004120900033NM 2004 12 9 DL73S041059 120041124A5310654694630 SHEAR TIE BOEING737 737247 138448DNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27376DL 23603 STATION 927 WEB AND SHEAR TIE REPAIRED AT STRINGER 5L DUE TO TOOLING DAMAGE. REPAIRED IAW ERA 095091-143. 2L72 4F A16WE 20041209000342004120900034NM 2004 12 9 DL73S041060 120041123A52306547952524A FRAME BOEING737 737232 1384475NM C2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27332DL 23104 A 1 INCH CRACK WAS FOUND IN THE WEB OF THE UPPER FRAME EMANATING FROM A FASTENER HOLE COMMON TO THE UPPER AND LOWER FRAME LAP JOINT. THE CRACK WAS STOP DRILLED AND THE FRAME REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 095286-14. 2L72 4F RTA16WE 20041209000352004120900035NM 2004 12 9 DL75K041061 120041124A2120 UNKNOWN BOEING757 757232 1384965NM CABIN FUMES A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO276715C 30486 FUMES IN THE CABIN. THOROUGHLY CHECKED AIRCRAFT AND RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE. 2L72 4F RTA2NM 20041209000362004120900036NM 2004 12 9 DL76S041062 120041125A2910 CAP BOEING767 767332 1382001NM HYD MODULE CRACKED A DALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27119DL 23278 CENTER HYDRAULIC SYSTEM DUMPED ALL FLUID WHILE MOVING FLAPS TO 15 DEGREES ON TAXI OUT SLC. FOUND CAP CRACKED AND SEPARATED FROM MODULE ON UPPER PART ABOVE HANDLE ON RT GND CHECKOUT MODULE. REPLACED RT CHECKOUT MODULE. LK AND OP CK GOOD. REMOVED, INSPECTED AND REPLACED BOTH CTR ELEC PUMP CASE DRAIN AND SYSTEM FILTERS. NO METAL FOUND. 2L72 4F RTA1NM 20041209000382004120900038NM 2004 12 9 SWAA043494 120041201A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 380, STRINGER 20L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041209000392004120900039EU 2004 12 9 MALA040717 120040903A5320 PANEL BAC 146 AVRO146RJ85A1500097EU CARGO BAY PUNCTURED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, FWD CARGO PANEL ON 142CR IS PUNCTURED. MAINTENANCE REPAIRED PANEL IAW SRM 53-00-35-201. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041209000402004120900040EU 2004 12 9 MALA040718 120040911A5753 TAB BAC 146 AVRO146RJ85A1500097EU TE FLAPS CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, LEFT WING FLAP INBOARD TAB LEADING EDGE CHAFED AT INBOARD ATTACH POINT. MAINTENANCE REPAIRED IAW EO A57073. AIRCRAFT RETURNED TO SERVICE 9/14/04. 2H74 4F RTA49EU 20041209000412004120900041EU 2004 12 9 MALA040707 120040827A5414 COWLING BAC 146 AVRO146RJ85A1500097EU NR 3 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, NR 3 ENGINE RT ZONE 2 COWLING CHAFED IN FIRE SHIELD PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RELEASE DATE 9/14/04. 2H74 4F RTA49EU 20041209000432004120900043SO 2004 12 9 MASA200400671 120041201A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07840MJ 145429 ASH 2856 CLT-YYZ. DURING PREFLIGHT THE CREW FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 12. MAINTENANCE RELAMPED AND THE LIGHT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20041209000452004120900045SO 2004 12 9 MASA200400659 120041128A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07854MJ 145490 ASH 2941 PHL HAD AN EMERGENCY EXIT LIGHT AT SEAT 12A THAT WAS INOP. MAINTENANCE REPLACED THE LAMP. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041209000462004120900046EA 2004 12 9 MASA200400667 120041129A3350E520005704 CIRCUIT BOARD CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSINOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07908FJ 15008 ASH 6122 PHX. THE EMERGENCY LIGHTS WERE CYCLING ON AND OFF WITH NORMAL POWER AND SWITCH POSITION. MAINTENANCE STILL TROUBLESHOOTING. 11/29 MAINTENANCE REPLACED CIRCUIT BOARD CARD AND THE BATTERY PACKS (P/N 2013-1A). 2L72 4F RTA21EA 20041209000472004120900047NM 2004 12 9 CALA0400738 120041203A3350D71701100 BATTERY PACK BOEING767 767424ER 1385270NM EXIT SIGN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW2776055 29450 THE EMERGENCY EXIT SIGN AT L-1 AND R-1 DOORS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK IAW MM 33-51-07. 2L72 4F RTA1NM 20041209000482004120900048NM 2004 12 9 SWAA043490 120041201A57536546435277 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 DURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041209000492004120900049NM 2004 12 9 SWAA043491 120041201A53116546533 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500, STRINGER 26R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041209000502004120900050NM 2004 12 9 SWAA043492 120041201A53156546810 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, RBL 28, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM. 2L72 4F RTA16WE 20041209000522004120900052SO 2004 12 9 C2XA04CL120 120041128A27523632501003 MOTOR EMB 145 EMB145 3260210SO FLAP DRIVE FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715973 145159 CREW REPORTED FLAP FAILED IN FLIGHT. REPLACED THE NR 1 FLAP DRIVE MOTOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041209000542004120900054SO 2004 12 9 RAIA00411027 120041125A21208166101 CONTROL VALVE EMB 145 EMB145LR 3260212SO CABIN TEMP MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03837HK10019 145255 PVD - BLEED LEAK NUMBER 2 DURING NUMBER 1 ENGINE START. MAINTENANCE REMOVED AND REPLACED NUMBER 2 TEMP CONTROL VALVE. 2L72 4T RTT00011AT 20041209000562004120900056 2004 12 9 SWAA043543 420041206A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041209000582004120900058NM 2004 12 9 SWAA043545 120041206A57536546435270 SKIN BOEING737 737301 1384611NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041209000592004120900059NM 2004 12 9 SWAA043546 120041206A3350PH22300L LIGHT BOEING737 7377H4 1384404NM CABIN DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29718SW 27852 DURING SCHEDULED MV2 CHECK, FOUND 2 EACH SECTIONS OF EEPLS STRIPS BETWEEN ROWS 6 DEF AND 10 DEF, DELAMINATED. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20041209000622004120900062NM 2004 12 9 SWAA043556 120041206A57126545445 RIB BOEING737 7375H4 138449DNM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO. 2L72 4F RTA16WE 20041209000642004120900064NM 2004 12 9 SWAA043469 120041130A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, ABOVE STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041209000652004120900065NM 2004 12 9 SWAA043470 120041130A53306545877 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 271, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041209000672004120900067NM 2004 12 9 SWAA043475 120041130A5313BAC1498 STRINGER BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER 17L AT BS 195, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20041209000692004120900069NM 2004 12 9 SWAA043480 120041130A57536546435335 SKIN BOEING737 7375H4 138449DNM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041209000712004120900071NM 2004 12 9 SWAA043548 120041206A53156545810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 312, LBL 2, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. 2L72 4F RTA16WE 20041209000752004120900075NM 2004 12 9 F3LA200400090 120040823A21501303A000003 FLOW VALVE AIRBUSA319 A319111 3930336NM LT A/C PACK FAULTY A F3LAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03918FR5143 1242 1943 FLIGHT CREW REPORTED PASSENGERS IN AND AROUND ROWS 9, 10 AND 11 REPORTED ODOR WHICH SMELLED LIKE RUBBER. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. PRESSURIZED AIRCRAFT TO 4.5 DIFFERENTIAL PRESSURE, NO UNUSUAL ODORS NOTED. FOUND NR 1 (LT) PACK FLOW CONTROL VALVE FAULTY. REPLACED FCV AND CHECKED OKAY. PERFORMED VISUAL INSPECTION OF LIVE TV COMPONENTS BETWEEN ROWS 9 AND 13, FOUND ALL CONNECTORS SECURE AND NO SIGNS OF OVERHEATING/BURNING. SYSTEM OPS CHECKED GOOD PER MM 44-25-00. 2L72 4F RTA28NM 20041209000772004120900077EA 2004 12 9 SWIA200414112 120041117A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07406SW 7030 INBOARD GND SPLR FAULT AND SPOILERON FAULT STAUS MESSAGE UPON TAXI IN. REPLACED BOTH SECU'S IAW MM 27-61-05, OPERATIONAL CHECK GOOD. P/N 49-164-05, S/N OFF (LT) 01397, (RT) 01455. 2L72 4F RTA21EA 20041209000792004120900079NM 2004 12 9 SWAA043253 120041108A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STRINGER 21L REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20041209000812004120900081NM 2004 12 9 UPS04243080 120040822A5330 SKIN BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE:C, SUSPECT CORROSION BS 1340 BETWEEN STR 8L AND 9L DAMAGED SKIN REMOVED FROM BS 1323 TO BS 1342, FROM FIN TO STR 10L IAW SRM 51-10-6 AND REPAIRED IAW AAAE EO 2004-077-007. REF UPS FILE 727-53-20160. 2L73 4F A3WE 20041209000832004120900083NM 2004 12 9 QXEA200400781 120041117A3060 WIRE DHAV DHC8 DHC8202 2809007NM NT 2 PROP DEICE LOOSE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09379PH 530 BOI - ON FLT NR 2125, EMERGENCY LIGHTS FLICKERED IN FLIGHT WITH NR 2 PROP DE-ICE SELECTED ON. FOUND LOOSE DE-ICE BOOT LEAD ON NR 2 PROP. RESECURED LEAD. GROUND RUN OPERATIONAL CHECKS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041209000862004120900086SO 2004 12 9 SWIA200414143 120041005A5320 PLATE EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FS 13630.0 TO FS 15050.0 CENTER BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041209000872004120900087EA 2004 12 9 SWIA200414059 120041030A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 621 RIGHT HAND FLOOR SUPPORT ANGLE RBL 40 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV "B". 2L72 4F RTA21EA 20041209000892004120900089EU 2004 12 9 CX7A194J0455 120041028A3246 BEARING SAAB SF340 340B 7860101EU NR 4 MLG WHEEL FAILED A CX7AO OTHER O OTHER NRNOT REPORTED 1 GL03303CE 340B194 NR 4 MAIN WHEEL ASSY DEPARTED AIRCRAFT. FOUND OUTBOARD BEARING FAILURE. 2L72 4T RTA52EU 20041209000902004120900090EA 2004 12 9 MASA200400486 120040830A7830 WARNING LIGHT CNDAIRCL600 CL6002D24 1390016EA THRUST REVERSER ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07903FJ 15003 ABORTED T/O DUE TO LT THRUST REVERSER UNSAFE MESSAGE. MAINTENANCE PLACED THE THRUST REVERSER ON MEL. 2L72 4F RTA21EA 20041209000912004120900091EA 2004 12 9 MASA200400517 120040910A493038834491 TUBE CNDAIRCL600 CL6002B19 1900309EA APU BURST A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0787353 7353 THE PILOT REPORTED A STRONG SMELL OF FUEL IN THE CABIN. MAINTENANCE FOUND A LINE BURST IN THE APU FUEL SUPPLY SYSTEM IN THE AFT ACCESSORY COMPARTMENT. MAINTENANCE PLACED THE APU ON MEL AFTER CONFIRMIMG THE ABSENCE OF FUEL VAPOR. 9/10 MAINTENANCE REPLACED A FUEL LINE. OPS CHECK GOOD. 2L72 4F RTA21EA 20041209000922004120900092EA 2004 12 9 MASA200400525 120040912A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX OVERSERVICED A MASAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SW0737178 7178 MAIN CABIN DOOR WOULD NOT OPEN UPON ARRIVAL IN PHX. MAINTENANCE REMOVED EXCESS LUBRICANT, OPS CHECKED GOOD. 2L72 4F RTA21EA 20041209000942004120900094EA 2004 12 9 MASA200400493 120040903A2613 OVERHEAT LOOP CNDAIRCL600 CL6002B19 1900309EA NR 1 ENGINE DAMAGED A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0717358 7358 THE CREW ABORTED TAKEOFF FOR A NUMBER 1 JET PIPE OVERHEAT WARNING MESSAGE ON TAKEOFF ROLL. MAINTENANCE REPLACED THE LOOP-A TERMINAL ENDS AND THE SYSTEM CHECKED OK. 2L72 4F RTA21EA 20041209000962004120900096EA 2004 12 9 MASA200400536 120040918A3220 TORQUE LINK CNDAIRCL600 CL6002B19 1900309EA NLG OBSTRUCTED A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0787353 7353 DECLARED AN EMERGENCY, DIVERTED DUE TO LANDING GEAR DISAGREE AND NOT HAVING A NORMAL UPLOCK OR DOWNLOCK INDICATION. AFTER PERFORMING A FLYBY IN BOI IT WAS DETERMINED THAT THE GEAR WAS DOWN AND LOCKED. THE PLANE MADE AN UNEVENTFUL LANDING. MAINTENANCE WAS ABLE TO DETERMINE THAT THE RT NOSE LANDING GEAR TIRE SIDEWALL HAD DEPARTED UNLATCHING THE TORQUE LINK AND DAMAGING THE GEAR DOOR. MAINTENANCE HAS REPLACED BOTH NOSE GEAR TIRES AND ARE PREPARING TO FERRY TO PHX FOR GEAR DOOR REPLACEMENT AND SUBSEQUENT GEAR SWINGS. 9/18 MAINTENANCE REPLACED THE NLG DOORS AND RECONNECTED THE TORQUE LINKS, OPS CHECK GOOD. 2L72 4F RTA21EA 20041209000982004120900098NM 2004 12 9 UPS04243413 120041008A5320 WEB BOEING727 727185C 138406NNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C, BS 740 LOWER WEB RBL 35, WL 160 SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT IAW NDTM 51-00-00, CRACK CONFIRMED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 53-10-9 FIG 4. 2L73 4F A3WE 20041209000992004120900099NM 2004 12 9 MWEA040213 120041121A3810 SERVICE PANEL DOUG MD88 MD88 3023688NM POTABLE WATER INOPERATIVE A MWEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31601ME 49762 POTABLE WATER SYSTEM STOPPED WORKING. FOUND POTABLE WATER SERVICE PANEL GUARD BENT AND FILL/DRAIN/VENT TURN-TO-LOCK CAP IN INCORRECT POSITION. 2L72 4F RTA6WE 20041209001002004120900100WP 2004 12 9 MWEA040214 120041122A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31812ME 48006 DENT NUMBER 16 NO LONGER MEETS STRUCTURAL REPAIR MANUAL REQUIREMENTS AT STATION 343 LONGERON 27 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20041209001012004120900101NM 2004 12 9 UPS04443327 120040930A5740 FITTING BOEING747 747121 1384871NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, LEFT WING UPPER BS 1241 REAR SPAR SPLICE PLATE FASTENER HOLE (STR L28) FOUND CRACK AT HOLE NR 4 TERMINAL FITTING AT FWD POSITION APPROX 0.080 INCH LONG. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2L74 4F A20WE 20041209001022004120900102NM 2004 12 9 UPS04243277 120040912A5320 WEB BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C, SUSPECT CRACK ON RIGHT 950 FITTING HORIZONTAL WEB WL 202 APPROX. REPAIR CARRIED OUT IAW SRM 51-10-06, 51-10-02 & AAAE EO 2004-085-001. UPS ENGINEERING FILE 727-53-20166. 2L73 4F A3WE 20041209001042004120900104NM 2004 12 9 XNOA1215 120041207A2782 ACTUATOR BOEING727 727227 1384078NM NR 2 SLAT MALFUNCTIONED A XN0AA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL23793A 20774 ON CLIMB-OUT, LEADING EDGE DEVICES WOULD NOT INDICATE UP AND LOCKED. X-FERRED TO DMI 4798, MEL 27-6 CAT "C". PLACARDS INSTALLED AS REQUIRED. R/R NR 2 SLAT ACTUATOR, OPS CK GOOD ON GROUND IAW B727 MM 27-81-32. THIS ACTION CLEARS DMI 4798. PLACARDS REMOVED. (STATUS:SUPP/CLOSED) 2L73 4F A3WE 20041209001052004120900105SO 2004 12 9 C2XA04CL123 120041202A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2716999 145307 CREW REPORTED FUEL SMELL IN THE COCKPIT DURING FLIGHT. MAINTENANCE PERFORMED GROUND RUNS ON BOTH ENGINES AND APU WITH BLEEDS ON . NO DEFECTS NOTED. 2L72 4T RTT00011AT 20041209001062004120900106WP 2004 12 9 NACA20040063 120041207A7932381001E0024 PROBE DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 2 ENGINE DIRTY A NACAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 AL0343872192 192 533294 510118 NR 2 ENGINE SHUT DOWN DUE TO STEADY OIL LOSS INDICATION. CLEANED OIL QUANTITY CONNECTORS AT NR 2 OIL QUANTITY PROBE. OPS CHECKED GOOD. 2L74 4R4 R A781 5E8 20041209001072004120900107EA 2004 12 9 QXEA200400814 120041125A5210 STEP CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - MAIN CABIN DOOR STEP NR 6 AFT SIDE WALL HAS TWO EACH CRACKS AT AFT HANDRAIL. REPAIRED IAW HORIZON AIR EA R-52-198 AND REO 670-52-11-079. 2L72 4F RTA21EA 20041209001122004120900112EU 2004 12 9 ERAA098197 120040713A2841VT044 INDICATOR BOLKMS105 BO105S 5626006EU FUEL QTY CRACKED B ERAAO OTHER O OTHER NRNOT REPORTED 1 SW03149EH S705 FUEL QUANTITY READS LOWER THAN ACTUAL GALLONS. FOUND CASE CRACKED. REPLACED CASE ASSEMBLY. UNIT THEN FUNCTIONALLY TESTED GOOD. 1G72 3U H3EU 20041209001132004120900113SW 2004 12 9 ALGA098133 120040808A6320206040032001 BEARING BELL 206 206B3 1181506SW TRANSMISSION MAKING METAL B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0335WH 2937 2736 TRANSMISSION DISASSEMBLED FOR METAL, FOUND DUPLEX BRG BREAKING DOWN. REMOVED AND REPLACED BRG. 1G71 3U H2SW 20041209001182004120900118WP 2004 12 9 GTIA040805 120040910A5320 PAN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CARGO DOORWAY CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 FWD PIT, LOWER DOOR JAMB PAN NUMEROUS AREAS OF CORROSION. REMOVED LOWER SECTION OF DOOR JAMB PAN. DRILLED AND LOCATED NEW DOOR JAMB. INSTALLED DOOR JAMB SEC AND SPLICES. 2L72 4F4 FRTA6WE E9NE 20041209001222004120900122EU 2004 12 9 MALA040737 120041126A3060 WARNING LIGHT SAAB SF340 340B 7860101EU PROP HEAT ILLUMINATED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15361PX 340B249 RT PROP HEAT CAUTION LIGHT ON AFTER 36-40 SECONDS IN NORM, 6-8 SECONDS IN MAX. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED RT PROP PER JOB CARD 6110-303. P/N ON/OFF:R390/4-123-F/27. S/N ON:DAP 0204 S/N OFF: DAP 0117. OPS CHECK GOOD. 2L72 4T RTA52EU 20041209001252004120900125SO 2004 12 9 RAIA00412004 120041203A801232153581 START VALVE EMB 145 EMB145 3260210SO LT ENGINE MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03803HK15568 145077 LEFT ENGINE WON'T START. MAINTENANCE REMOVED AND REPLACED LEFT STARTER CONTROL VALVE. 2L72 4F RTT00011AT 20041209001312004120900131NM 2004 12 9 DHL2004762006 120041204A3150 WARNING HORN BOEING727 7272B7 138407LNM COCKPIT ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01762AT 22162 LOW SPEED RTO PERFORMED IMMEDIATELY AFTER BRAKE RELEASE AND THRUST LEVERS ADVANCED DUE TO T/O WARN HORN A/C WT 140000 SPEED APPROX 2 KNTS 7 C PA 1000 MSL RECYCLE SPD BRAKE, CHECKED TRIM FLAPS, SYS RETURNED TO NORMAL OPS. 2L73 4F A3WE 20041209001322004120900132NM 2004 12 9 ASA0440181 120041011A53304575094110 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU LT IB FORE FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02708AS 28895 OKC - FOUND HOLE IN THE LOWER SURFACE OF THE LT IB FORE FLAP, 3 INCH FROM THE T/E, 17 INCHES FROM THE IB EDGE. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E21EU 20041209001342004120900134NM 2004 12 9 ASA0440186 120041016A53106546548 SHEAR TIE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 PAE - CORROSION AFT CARGO BAY ON SHEAR TIE. REMOVED CORRODED SHEAR-TIE, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20041210000112004121000011WP 2004 12 10 UPS04843575 120041118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSLEAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LONGERON CRACKED AT STA 1742. CUT OUT CRACKED PORTION OF LONG AT SHEAR TIE. NDT VERIFIED ALL DAMAGE REMOVED REF SRM53-2-2 FIG 11 AND SPM06-10-01.001. FABRICATED FILLER AND REAPIR ANGLE FROM SHT7075T6/.063 AND S2645517 EXTRUSION AND INSTALLED SAME REF SRM 53-2-2 FIG11 51-1-20D. 2L74 4F RT4A25 20041210000152004121000015 2004 12 10 YENA200460 420041204A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU SEAT 4B UNKNOWN A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15544JB616 1835 AT 1952Z FA'S INFORMED US OF A STRONG SMELL OF SMOKE IN THE CABIN. FLT CREW ISOLATED GALLEY COMM AND AFT AVIONICS. SMELL WENT AWAY. INSPECTED IAW LIVE TV SYSTEM INTEGRITY CHECK CONCERNING ELECTRICAL ODOR AND FOUND SEB AT 4B WITH AN ELECTRICAL BURNING ODOR. REMOVED AND REPLACED SEB IAW LTV MM 23-39-00. OPS CHECK GOOD REF INFORMATION NOTICE 2004-T023TR. 2L72 4F RTA28NM 20041210000272004121000027NM 2004 12 10 ASA0440177 120041006A53476546815149 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - MECHANICAL DAMAGE TO TOP OF SEAT TRACK. REMOVED AND REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E21EU 20041210000292004121000029WP 2004 12 10 GTIA040793 120041002A5210 HANDLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE L1 DOOR LOOSE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23800NK 49144 L1 DOOR HANDLE LOOSE. SECURED HANDLE. 2L72 4F4 F A6WE E9NE 20041210000342004121000034WP 2004 12 10 ASAA0480501 120040924A575449374711 SLAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT WING WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 RT SLAT TRACK NR 3 AFT IB RUB BLOCK FAILS CLEARANCE CHECK AND WORN. REWORKED RUB BLOCK IAW EA 2780-01020. 2L72 4F4 FRTA6WE E9NE 20041210000392004121000039EA 2004 12 10 QXEA200400815 120041125A5210 STEP CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - MAIN CABIN DOOR STEP NR 6 FORWARD STEPWALL CRACKED AT BOTTOM UNDER WHERE FOLDING HANDRAIL BRACKET. REPAIRED IAW HORIZON AIR EA R-52-198 AND REO 670-52-11-079, NOTE 4. 2L72 4F RTA21EA 20041210000402004121000040EA 2004 12 10 QXEA200400820 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X459-X475, X481-X492, X504-X506, X520-X522, X534-X536. REPAIRED IAW CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041210000412004121000041EA 2004 12 10 QXEA200400821 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X428, X444-X446. REPAIRED IAW CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041210000422004121000042EA 2004 12 10 QXEA200400822 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT CORROSION AT STATION X409-X415 AND X399. REPAIRED IAW CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041210000432004121000043SO 2004 12 10 C2XA04SH567 120041202A532012004172001 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713978 145180 DURING C CHECK, THE LEFT OMEGA BEAM SPLICE WAS CORRODED AND CRACKED BETWEEN FRAMES 23 AND 24. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01179. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050210000572005021000057NM 2005 2 10 USAA040887 120041117A5320 SKIN BOEING767 767201 1385125NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND UNDOCUMENTED SKIN REPAIR, STATION 325, STRINGER 30R. REPAIR DOUBLER INSTALLED PER EA 85860B. (M) 2L72 4F RTA1NM 20041208000792004120800079NM 2004 12 8 DL73S041053 120041120A5330654577882 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27316DL 23088 THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 2.5 INCH CUTOUT IN THE SKIN AND BEARSTRAP. THE TRIMOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 397450-14, REV C. 2L72 4F RTA16WE 20041208000812004120800081NM 2004 12 8 SWAA043520 120041204A52406545871132 BEAM BOEING737 7373T0 1384582NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29684WN 23941 DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR NR 1 WEB BEAM, CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM. 2L72 4F RTA16WE 20041208000882004120800088NM 2004 12 8 SWAA043525 120041204A55526545166 ROD BOEING737 7373H4 1384600NM LT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR OUTBOARD FWD TAB ROD PER MM. 2L72 4F RTA16WE 20041208001032004120800103NM 2004 12 8 SWAA043509 120041202A53116546536 BELTFRAME BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND BELT FRAME AT BS 616, STRINGER 17R, CRACKED. REPAIRED BELT FRAME PER T1-153-018. 2L72 4F RTA16WE 20041208001062004120800106EU 2004 12 8 MALA040719 120040916A5240 SKIN BAC 146 AVRO146RJ85A1500097EU SERVICE DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, DAMAGE TO FUSELAGE SKIN AT FWD SERVICE DOOR HOLD OPEN LATCH. MAINTENANCE REPAIRED IAW EO A53172. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041208001122004120800112NM 2004 12 8 SWAA043462 120041129A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED AT BS 380 STRINGER 9L AND BS BS 500A, STRINGER 16R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20041208001162004120800116EA 2004 12 8 MASA200400645 120041120A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. 2L72 4F RTA21EA 20041208001232004120800123NM 2004 12 8 SWAA043464 120041130A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 10 DEF, LOOSE. SECURED STRIP PER MM. 2L72 4F RTA16WE 20041208001482004120800148EU 2004 12 8 MALA040725 120040909A5414 COWL DOOR BAC 146 AVRO146RJ85A1500097EU NR 2 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, NR 2 ENGINE INBOARD ZONE 2 COWL CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041208001562004120800156NM 2004 12 8 SWAA043530 120041205A53116546540 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 639, STRINGER 16R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041208001622004120800162 2004 12 8 SWAA043504 420041202A25656557463 FITTING BOEING737 7373Y0 1384671NM L1 GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM. 2L72 4F RTA16WE 20041208001632004120800163NM 2004 12 8 SWAA043505 120041202A53206545834 STRUCTURE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, FROM LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM. 2L72 4F RTA16WE 20041208001642004120800164NM 2004 12 8 SWAA043506 120041202A53306545766 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT WINDOW CUTOUT, BS 482A + 10, STRINGER 13R, CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20041208001732004120800173NM 2004 12 8 TSAA0421081 120041130A2120 CLAMP BOEING737 73725A 1384481NM CABIN AIR LOOSE A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13819AL 23791 PRESSURIZATION CHECKED BEFORE TAKEOFF, CABIN CLIMBED TO 1,000 FT BY THE TIME AIRCRAFT LEVELED AT 3,000 FT. RETURNED TO OGG. NOTE THAT THE RIGHT PACK WAS DEACTIVATED PRIOR TO THIS FLIGHT DUE TO REPORTS OF A WHOOSHING SOUND NEAR ROW 7 & 8. THE FIRST OFFICER FOUND THE MIX VALVE INOP AND ALL THE WAY COLD. THE RIGHT PACK WAS DEACTIVATED AND PUT ON MEL. CHECKED LT & RT PACK SYS; INSPECTED FWD ENTRY/SVC DOOR AND AFT SVC/ENTRY DOOR, PRESSURIZED A/C TO 3-4 INCHES, FOUND NO LEAKS. INSPECTED ALL DOORS & PANELS, NO LEAKS. INSPECTED LT PACK & FOUND AIR LEAKING FROM ACM EXHAUST DUCT. RESECURED CLAMP & SEAL. REPRESSURIZED A/C SYS 3-4 INCHES, ALL SYS CHECKS NORMAL. NO LEAKS, A/C OK FOR SERVICE. 2L72 4F RTA16WE 20041208002032004120800203NM 2004 12 8 SWAA043496 120041201A5313BAC1498 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10R AT BS 908, CRACKED. REPAIRED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20041209000082004120900008NM 2004 12 9 SWAA043533 120041205A53106517684 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29362SW 26573 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CUTOUT, LOWER FWD STOP FITTING, WEB DOUBLER CRACKED AT BS 303.9, STRINGER 16L. REMOVED AND REPLACED FRAME CUTOUT WEB DOUBLER PER SRM. 2L72 4F RTA16WE 20041209000092004120900009NM 2004 12 9 SWAA043539 120041206A2760654476118 PCU BOEING737 7373H4 1384600NM LT ELEVATOR LEAKING A SWAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW29347SW 24374 AIR TURNBACK, DECLARED EMERGENCY. A HYDRAULIC SYSTEM FAILURE AND FLUID LOSS IN FLIGHT. REMOVED AND REPLACED LT ELEVATOR PCU PER MM. 2L72 4F RTA16WE 20041209000162004120900016SO 2004 12 9 C2XA04BT120 120041123A335078241 INVERTER EMB 145 EMB145 3260210SO EMERGENCY LIGHT FAULTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714974 145161 CREW REPORTED EMERGENCY EXIT SIGN ABOVE GALLEY DOOR WILL NOT LIGHT UP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041209000252004120900025EU 2004 12 9 MALA040722 120040915A5753 TAB BAC 146 AVRO146RJ85A1500097EU TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15518XJ E2337 DURING C1 INSPECTION IN YYC, RIGHT IN BOARD FLAP TAB LEADING EDGE HAS CHAFING. MAINTENANCE REPAIRED IAW EO A57073. AIRCRAFT RETURNED TO SERVICE 9/25/04. 2H74 4F RTA49EU 20041209000262004120900026EU 2004 12 9 MALA040706 120040827A5414 COWLING BAC 146 AVRO146RJ85A1500097EU NR 4 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C1 INSPECTION IN YYC, NR 4 ENGINE LEFT ZONE 2 COWLING CHAFED IN FIRE SHIELD PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RELEASE DATE 9/14/04. 2H74 4F RTA49EU 20041209000512004120900051NM 2004 12 9 SWAA043493 120041201A53306545877 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR CUTOUT LOWER AFT CORNER SKIN CRACKED. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20041209000532004120900053SO 2004 12 9 RAIA00411026 120041125A3010 CLAMP EMB 145 EMB145 3260210SO ANTI ICE VALVE LOOSE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03805HK 145096 PIT - WING ANTI ICE FAULT/MULTIPLE POWER RELATED FAILURE MSGS. MAINTENANCE SECURED CLAMP AT ANTI ICE VALVE AND RESET POWER. 2L72 4F RTT00011AT 20041209000552004120900055SO 2004 12 9 RAIA00411029 120041128A4950 OIL CAP EMB 145 EMB145LR 3260212SO APU LOOSE A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03830HK 145313 SYR - SMOKE IN CABIN. MAINTENANCE INSPECTED AND FOUND APU OIL CAP LOOSE. RE-SECURED CAP. CLEANED APU COMPARTMENT OF OIL. 2L72 4T RTT00011AT 20041209000572004120900057NM 2004 12 9 SWAA043544 120041206A3350101073 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29608SW 27928 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041209000632004120900063NM 2004 12 9 SWAA043557 120041206A531565469563 CREASE BEAM BOEING737 7375H4 138449DNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM BETWEEN BS 400 AND BS 420, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTION PER EA. 2L72 4F RTA16WE 20041209000662004120900066NM 2004 12 9 SWAA043474 120041130A53206551698 SPLICE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER SPLICES CRACKED AT BS 907, STRINGER 4R AND STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM. 2L72 4F RTA16WE 20041209000682004120900068NM 2004 12 9 SWAA043479 120041130A57536546435278 SKIN BOEING737 7375H4 138449DNM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041209000702004120900070NM 2004 12 9 TSAA0452080 120041126A5270 WARNING LIGHT BOEING737 73776N 13844CHNM MASTER CAUTION ACTIVATED A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13750AL 32743 ETOPS FLT 477, OAK-HNL: CLIMBING OUT OF OAKLAND, THE MASTER CAUTION LIGHT ILLUMINATED, DOORS AND FORWARD CARGO WITH A LOSS OF PRESSURIZATION. RETURNED TO OAKLAND; UNEVENTFUL LANDING. ALL DOORS WERE VERIFIED CLOSED AND LOCKED; BIT CPC. NO DEFECTS NOTED. PERFORMED A CABIN PRESSURIZATION CHECK IN ACCORDANCE WITH MM 05-51-91-2. NO LEAKS NOTED. DECAY CHECK GOOD. FORWARD CARGO DOOR INDICATION INOP. DEFER PER MEL 52-3, CONTROL NUMBER 2611C06. DOOR IS VERIFIED CLOSED AND LOCKED BEFORE FLIGHT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20041209000722004120900072NM 2004 12 9 SWAA043558 120041206A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CUTOUT FWD CORNER, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041209001092004120900109 2004 12 9 GTIA040794 420041002A2565 SLIDE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE L1 DOOR UNSECURE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23801NK 48048 L1 SLIDE PACK CAME OFF DOOR. RESECURED SLIDE PACK. 2L72 4F4 F A6WE E9NE 20041209001142004120900114WP 2004 12 9 GTIA040819 120041018A2820 LINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE FUEL SYSTEM CHAFED A O OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23802NK 53168 STRONG FUEL SMELL IN CABIN WITH APU RUNNING. ITEM TRANSFERRED TO DMI 02911151 IAW MEL 49-1-0. CAT (C). PLACARD INSTALLED. FOUND FUEL LINE ON FUEL HEATER (APU) CHAFED THROUGH, REMOVED LINE AND ROUTED LINE SO IT DOES NOT CHAFE, LEAK CHECK GOOD. 2L72 4F4 FRTA6WE E9NE 20041209001162004120900116NM 2004 12 9 2004UALA01163 120041126A5315 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FLOORBEAM CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29670UA17696 29240 STATION 246 FLOORBEAM AT APPROX LBL 11, STIFFENER IS CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED STIFFENER. 2L72 4F4 FRTA1NM E24NE 20041209001202004120900120 2004 12 9 2004UALA01171 420041201A3418 SENSOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE AOA MALFUNCTIONED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29197UA 26901 ALTIMETER SPLIT 240-250 FT WITH RT SIDE READ LOW. THE RT AOA PROBE IS SUSPECTED TO BE PROVIDING ERRONEOUS INDICATIONS TO THE ADC AT HIGH SPEEDS (0.8 - 0.9 MACH). THE AIR DATA COMPUTER TAKES AOA INPUTS TO MAKE CORRECTIONS TO THE PITOT-STATIC PRESSURES. DURING HIGH SPEEDS, THE INCORRECT AOA INDICATIONS WERE CAUSING ERRONEOUS CORRECTIONS TO BE APPLIED BY THE AIR DATA COMPUTER, THEREBY RESULTING IN SPLIT ALTIMETER INDICATIONS BETWEEN THE CAPTAINS AND FIRST OFFICERS SIDE. REPLACEMENT OF THE FIRST OFFICERS ANGLE-OF-ATTACK PROBE RECTIFIED THE PROBLEM. 2L74 4F4 FRTA20WE E24NE 20041209001232004120900123EU 2004 12 9 MALA040734 120041123A5610NF20216402 WINDSCREEN BAC 146 AVRO146RJ85A1500097EU COCKPIT DELAMINATED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15503XJ E2310 FOB SCREEN DELAMINATED 100 PERCENT INFLIGHT. AIR RETURN TO MSP. MAINTENANCE REPLACED FOB SCREEN PN NF20216-402 SN OFF L292347 SN ON L310453. REF AMM 56-10-21 401. 2H74 4F RTA49EU 20041209001272004120900127EU 2004 12 9 RAIA00411031 120041109A79308582 PRESSURE SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE OIL MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03554HK67 41067 RIGHT ENGINE OIL CAP LIGHT ON. MAINTENANCE, DEFERRED AS PER MEL 79-4. SUBSEQUENTLY, REMOVED AND REPLACED RT OIL PRESSURE SWITCH. 2L72 4T RTA41NM 20041209001292004120900129NM 2004 12 9 USAA040852 120041014A5310 DOOR FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - DOOR EDGE FRAME, .5 INCH CRACK, FWD SERVICE DOOR AFT END FRAME AT MIDSTOP FITTING. ROUTED OUT CRACK, INSTALLED DOUBLER IAW TYP REP 52-10-11. 2L72 4F4 FRTA16WE E2GL 20041209001302004120900130NM 2004 12 9 SB04162 120041205A335020131A BATTERY PACK BOEING737 7373B7 1384580NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19376US 22955 ORD - MAINTENANCE REPORTED A FEW OF THE AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20041210000072004121000007 2004 12 10 2004UALA01182 420041202A2565 SLIDE BOEING747 747451 1384940NM PWA 4056 PW4056 NE CABIN TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 DEPLOYED SLIDE, FOUND TEAR IN FLOOR. SLIDE LEAKS IN INFLATABLE AND AT ASPIRATOR FLAPS. SLIDE SENT TO OEM (GOODRICH) FOR REPAIR. REPLACED GIRT AND ASPIRATOR. 2L74 4F4 FRTA20WE E24NE 20041210000172004121000017EA 2004 12 10 A6WA200440185 120041117A5310 DOUBLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31442AW 7778 AFTER REMOVING ACCESS PANEL 132AL, FOUND 4 HOLES IN FORWARD FUSELAGE ACCESS PANEL DOOR SURROUND DOUBLER FS 228, STR19R-20R. PERFORMED A MAJOR REPAIR BY OPENING UP HOLES TO REMOVE DAMAGE, FABRICATED AND INSTALLING FREEZE PLUGS. OPENED HOLES IN FREEZE PLUGS USING NR 10 DRILL BIT. ALL WORK DONE IAW REO 601R-53-11-162. 2L72 4F4 FRTA21EA E15NE 20041210000312004121000031 2004 12 10 GTIA040825 420041020A3422 GYRO DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE COCKPIT INACCURATE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23821NK 49508 HEADING LIGHT ON IN FLIGHT 6 FT-8 FT OFF. REPLACED NR 1 DG AND SWITCHING UNIT. 2L72 4F4 F A6WE E9NE 20041210000322004121000032NM 2004 12 10 UIEA200400198 120041116A276033205001 ACTUATOR BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 8 SPOILER LEAKING G UIEAHJA DEACTIVATE SYST/CIRCUITSDUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA15523MC 21782 DURING CLIMB-OUT, NR 4 HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON WITH A DROP OF SYSTEM QUANTITY OIL FROM 8.5 TO 2.5, SYSTEM WAS SHUTDOWN. QUANTITY REMAINED AT 2.5. TURNED ADP TO CONTINUOUS, QUANTITY STARTED DROPPING, SYSTEM SHUTDOWN. REF: LOG PAGE 537018, FUEL JETTISONED FROM 82.7 TO 47.1. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR IAW MM 27-61-04. OPS AND LEAK CHECK OK. REMOVED SPOILER ACTUATOR, PN 33205001, SN 452423. 2L74 4F4 FRTA20WE E23EA 20041210000332004121000033NM 2004 12 10 2004UALA01048 120041112A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 CABIN FLOORBEAM CAP AT BS 324 RBL 44, RBL 48, AND RBL 62 IS CORRODED. SUPPLEMENTAL DATA UPDATE, TYPICAL FLOORBEAM CORROSION. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES TO FLOORBEAMS. 2L72 4F4 FRTA2NM E17NE 20041210000512004121000051WP 2004 12 10 P9RA20040048 120041103A2760 WARNING SYSTEM DOUG DC9 DC983 3022083WP AUTO SPOILER ACTIVATED A P9RAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11960PG 49904 AUTO SPOILER WARNING DURING ENGINE RUN UP FOR TAKEOFF. PLACED ITEM ON MEL 271901. MAINTENANCE PROCEDURE COMPLIED WITH. MAINTENANCE ENTRY 11/8/04. REFERENCE MEL 271901. OPS CHECKED SPOILER SYSTEM IAW MM, COULD NOT DUPLICATE FAULT. MEL REMOVED. REVIEW OF LOG PAGES REVEAL NO FURTHER WRITE UPS. NO SPECIFIC PART INFORMATION TO ADD. 2L72 4F RTA6WE 20041210000562004121000056NM 2004 12 10 HNAA0400165 120041130A5313 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE DAMAGED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 MAJOR REPAIR DURING C CHECK WHILE WORKING REPAIRS FOR LIGHTNING STRIKE DAMAGE ELONGATED HOLES DRILLED IN STR 30P NECESSITATING REPAIR BY SPLICING REPLACEMENT SECTION. CUT STR30P, HFEC, FABRICATED REPLACEMENT SECTION, TRIMMED REPAIR ANGLES, INSTALLED PARTS 2H72 4T RTA13NM 20041210000572004121000057SO 2004 12 10 CHQA000579 120041104A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11264 145221 GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-09. RIGHT EMERGENCY OVERWING EXTERNAL LIGHT INOP. REMOVED AND REPLACED RIGHT WING EXTERNAL EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041210000582004121000058SO 2004 12 10 CHQA000578 120041102A3350 LIGHT EMB 135 EMB135LR 3260305SO GALLEY INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11841 145737 EMERGENCY EXIT LIGHT OVERHEAD THE GALLEY IS INOP. RELAMPED EMERGENCY EXIT LIGHT OVERHEAD THE GALLEY IAW EMB 135 MM 33-50-09. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041210000752004121000075EA 2004 12 10 SWIA200414186 120041118A5210 WEB CNDAIRCL600 CL6002B19 1900309EA PAX DOOR STEP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 PAX DOOR BOTTOM STEP LOWER WEB CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-71-59. 2L72 4F RTA21EA 20041210000812004121000081EU 2004 12 10 XNOA1210 120041029A3260 UPLOCK AIRBUS300 A300B4203 3930306EU NLG FAILED A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23373PC 218 ON TAKEOFF NOSE GEAR DOOR WOULD NOT CLOSE, COMPLETED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED DFW. REMOVED AND REPLACED LT NOSE GEAR DOOR UPLOCK ASSEMBLY IAW A300 AMM 32-31-14. OPS AND LEAK CHECK GOOD. 2L72 4F RTA35EU 20041210000852004121000085EA 2004 12 10 04323694 120041118A3260 SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27694BR 7768 EVENT SUMMARY STATES GEAR DISAGREE. REMOVED AND REPLACED SENSOR. ROUTED NLG SENSOR HARNESS. INSTALL SENSOR BRACKET. OPS CHECK GOOD. 2L72 4F RTA21EA 20041213000062004121300006NM 2004 12 13 SWAA043567 120041207A555265C25798 FITTING BOEING737 7375H4 138449DNM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C3 CHECK, LT ELEVATOR INBOARD TAB HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HINGE FITTING PER MM. 2L72 4F RTA16WE 20041213000122004121300012NM 2004 12 13 SWAA043573 120041207A3350311500 LENS BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 10 DEF, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041213000222004121300022NM 2004 12 13 SWAA043589 120041209A53156546811 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM SHEAR WEB FROM BS 947 TO BS 1006, RBL 45, CORRODED. REMOVED AND REPLACED WEB PER SRM. 2L72 4F RTA16WE 20041213000252004121300025NM 2004 12 13 F3LA200400116 120041206A2120 ODOR AIRBUSA319 A319111 3930336NM CABIN DETECTED A F3LAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03934FR 2287 AIR TURNBACK, FLT CREW REPORTED STRONG ODOR OF SMOKE IN CABIN, CONCENTRATED AT ROWS 17DEF & 18DEF. ODOR STRONGER AT EYE LEVEL AND STRONGEST AT WINDOW SEAT. NO SMOKE VISIBLE AT ANY TIME. INSPECTED AIRCRAFT, NO DEFECTS NOTED. COULD NOT DUPLICATE. INSPECTED E&E COMPARTMENT, NO DEFECTS OR ODORS NOTED. INSPECTED BEHIND PSU'S AT ROWS 16DEF THRU 19DEF. NO DEFECTS OR ODORS NOTED. PERFORMED TASK 24-00-00-810, NO FAULTS OR DEFECTS DETECTED. RAN NR 1 AND NR 2 ENGINES AND NR 1 AND NR 2 PACKS, NO DEFECTS OR ODORS NOTED. INSPECTED SEB'S, VOU'S AND SEAT TO SEAT CABLES FROM 15DEF TO 20DEF. NO ODOR NOTED. INSPECTED ALL CONNECTIONS, NO DISCOLORATION OF CONTACTS. ALL CONNECTORS SECURE. 2L72 4F RTA28NM 20041213000282004121300028NM 2004 12 13 SWAA043581 120041208A3350D71702001 BATTERY BOEING737 7372H4 138448CNM EMERGENCY LIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 AFT SERVICE DOOR EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F A16WE 20041213000322004121300032CE 2004 12 13 DXTA200400469 120041207A3240 BRAKE CESSNA500 560CESSNA 2076750CE BRAKE PEDAL MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07399QS 5600510 FIRST OFFICER RIGHT BRAKE PEDAL GOES TO FLOOR. NO FLUID VISIBLE OR UNDER PEDAL. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20041213000332004121300033CE 2004 12 13 DXTA200400470 120041207A3241 WARNING SYSTEM CESSNA560 560XL 2076702CE ANTI SKID SYS ACTIVATED E DXTAO OTHER J WARNING INDICATION LDLANDING 1 GL07635QS 5605358 LOW BRAKE PRESSURE/ANTISKID INOP (IN-FLIGHT) ANNUNCIATOR ILLUMINATED WITH RT GEAR LIGHT ILLUMINATED. CHECKLIST CONDUCTED EMERGENCY BRAKES USED. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20041213000512004121300051 2004 12 13 0402129760 420041125A2565 STRAP DOUG DC9 DC941 302207NWP TAILCONE SLIDE MISSING A NWAAO OTHER O OTHER NRNOT REPORTED 1 GL01760NW 47288 A LINE CHECK INSPECTION FOUND THE AFT EVACUATION SLIDE MISSING THE DEPLOYMENT STRAPS. MAINTENANCE INSTALLED THE STRAPS PER ROUTINE WORK CARD 2560-4064M, STEP 3G, RII INSPECTION REQUIRED AND COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041213000572004121300057WP 2004 12 13 AALA20041189 120041130A33506O030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21581AA 53158 LAX - CEILING EMERGENCY LIGHTS FROM STATION 301 TO STATION 414 ARE INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY AT B5100 FOR CEILING EMERGENCY LIGHTS FROM STATION 301 TO STATION 414. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000812004121300081NM 2004 12 13 WLDA2004104 120041103A5300 DRAIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE WASTE TANK CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 DURING C2 CHECK INSPECTION FOUND CORROSION IN WASTE TANK DRAIN PAN AT STA 1970 BETWEEN L50L AND L50R. REMOVED WASTE TANK DRAIN PAN AND INSTALLED NEW PART PER MD11 SRM 51-33-01 VOL II REV 36. APPLIED PROTECTION COATING. 2L73 4F4 FRTA22WE E24NE 20041213000832004121300083WP 2004 12 13 WLDA2004106 120041127A5101 STRUCTURE DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE FUSELAGE VIBRATION A WRLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO11304 47928 DAY/BRU ABORTED TAKEOFF AT 70 KTS DUE TO VIBRATION. INSPECTED ALL WHEELS AND BRAKES, FLAPS AND SPOILERS, NOSE GEAR AND NR 1 & 3 INLETS, NO DEFECTS NOTED. REVERIFIED ALL TIRE PRESSURE, ALL CHECKED NORMAL. 2L73 4F4 FRTA22WE E23EA 20041213000852004121300085EA 2004 12 13 04328636 120041123A3350 SIGN CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27636BR 7307 LEFT EMERGENCY EXIT SIGN INOP. MX FOUND WIRE DISCONNECTED AND RECONNECTED IT. OPS CHECK GOOD. 2L72 4F RTA21EA 20041213001082004121300108NM 2004 12 13 DHL2004755507 120041019A5753 SKIN BOEING727 727225 1384077NM LT WING TE FLAP DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, LEFT O/B MID FLAP UPPER T/E WBL 297 & 492 HAVE SKINS DELAMINATED. CUT OUT 2EA UPPER T/E DELAM AREAS APPROX 3 X 6.5 INCH & VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 30. FABRICATED 2EA REPLACEMENT SKINS APPROX 3 X 6.5 INCH & 3.5 X 16.5 INCH AND 2EA EXTERNAL DOUBLERS APPROX 3 X 3 INCH & 3.5 X 3 INCH FROM 2024-T3.016 PO 9001394 IAW B727 SRM 57-50-2 FIG 3. CLEARED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIR PARTS & SURFACES FOR BONDING. BONDED 2EA REPAIRS IAW B727 SRM 57-40-20 FIG 30. SANDED, CLEARED, TREATED, PRIMED & SEALED REPAIRS IAW B727 SRM 51-40-20 FIG 30. 2L73 4F A3WE 20041213001142004121300114 2004 12 13 DXTA200400450 420041118A22107022090901 COMPUTER CESSNA750 750 2076810CE RUDDER MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07953QS3520 7500153 IN FLIGHT AT 17,000 FT AND 320 KTS FELT A SHARP RUDDER KICK WITH THE AUTOPILOT ON, YD FAIL UPPER -B- AMBER CAS MESSAGE ILLUMINATED. REMOVED AND REPLACED -B- YSAC (UPPER) IAW 750 MM 27-24-01. OPS CHECKED GOOD. 2L72 4J RTT00007WI 20041213001242004121300124NM 2004 12 13 SWAA043391 120041119A53126545409 PRESSURE PANEL BOEING737 7373H4 1384600NM RT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 665 BEADED WEB CRACKED AT RBL 40. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041213001262004121300126NM 2004 12 13 SWAA043393 120041119A52106545871 DOOR FRAME BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR AFT FRAME CRACKED AROUND 4TH STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20041213001282004121300128 2004 12 13 SWAA043394 420041119A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29612SW 27930 R1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041213001302004121300130 2004 12 13 SWAA043396 420041119A2565D31354 SLIDE BOEING737 7377H4 1384404NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20041213001322004121300132 2004 12 13 SWAA043398 420041119A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20041214000052004121400005NM 2004 12 14 HL2004755516 120041024A5753 SKIN BOEING727 727225 1384077NM TE FLAP DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, RIGHT O/B AFT FLAP LOWER SURF WBL 475 HAS LARGE SMOOTH DENT. CUT OUT DENTED AREA OF AFT FLAP LWR SKIN APPROX 5 INCHES ROUND IAW B727 SRM 51-40-20 FIG 32. FABRICATED ONE FILLER APPROX 5 INCHES ROUND & ONE DOUBLER 8 INCHES ROUND FROM 2024 T3 .016 PO 9001394 IAW B727 SRM 51-40-20 FIG 32 & 57-50-2 FIG 4. SANDED, CLEANED, PREPPED, APPLIED ADHESIVE PRIMER & ADHESIVE TO ALL REPAIR PART SURFACES & BONDED REPAIR IAW B727 SRM 51-40-20 FIG 32. CURED REPAIR, SANDED SMOOTH, CLEANED & PERFORMED POST BOND INSP WITH NO DELAM NOTED. PRIMED & SEALED REPAIR. 2L73 4F A3WE 20041214000062004121400006NM 2004 12 14 DHL2004755517 120041121A5753 SKIN BOEING727 727225 1384077NM LT WING TE FLAP GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, LEFT WING I/B AFT FLAP - FORE FLAP HAS A GOUGE ON EXISTING EXTERNAL DOUBLER AT O/B END. CUT OUT EXISTING SKIN O/B FLAP IAW B727 SRM 51-10-1, FABRICATED SKIN 2020T3 .050 PO 9001425 7 X 12.5 INCH FILLER DOUBLER 2024T3.060 PO 9001387, 5.5 X 12.5 INCH IAW B727 SRM 57-50-4 FIG 4. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED REPAIR AT L/E IAW 727 SRM 51-30-2. 2L73 4F A3WE 20041214000072004121400007NM 2004 12 14 DHL2004755510 120041021A5330 SKIN BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, CORROSION FUSELAGE SKIN UNDER WING-TO-BODY FAIRING STA 720D + 14" STR 19R. REMOVED ANTI ICE DUCTS & HYD LINES HARDWARE. REMOVED RT WING ROOT WIRE HARNESSES AND SUPPORTS. CUT OUT DAMAGE UPPER SKIN 4.5 X 3 INCHES IAW B727 SRM 53-30-3 FIG 5. FABRICATED DOUBLER 9.5 X 12", 2024T3 .080 PO 9001245 SHIM 12 X 3" 2024T3 .071 PO 9001424 FILLER 2024.T3 .071 PO 9001424 IAW B727 SRM 53-30-3 FIG 6. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727 SRM, INSTALLED ANTI ICE DUCTS HYD LINES AND WING TO BODY FAIRING. INSTALLED R/W ROOT WIRE HARNESS & SUPPORTS. 2L73 4F A3WE 20041214000082004121400008NM 2004 12 14 DHL2004755513 120041021A5522 SKIN BOEING727 727225 1384077NM RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, RT ELEVATOR HAS A DENT ON BOTTOM INBOARD SKIN APPROX ELEV STA 50. CUT OUT DAMAGED AREA (1 X 1.25 INCH) AND FABRICATED REPAIR DOUBLER FROM 2024T3 PO 9001030 (2 X 2.5 INCH) .032 IAW 727 SRM 55-20-3 FIG 1. PARTS TREATED AND PRIMED IAW 727 SRM 51-10-2, PARTS INSTALLED IAW 727 SRM 55-20-3 FIG 1. REBALANCED RT ELEVATOR BY CALCULATION METHOD NEW BALANCE MOMENT IS +126.10 IN LBS NO ADDITIONAL BALANCE WEIGHTS REQUIRED WITH ALLOWABLE LIMITS IAW B727 SRM 51-80-7, NEW DATA PLATE INSTALLED. 2L73 4F A3WE 20041214000102004121400010NM 2004 12 14 DHL2004755515 120041022A5753 FAIRING BOEING727 727225 1384077NM FLAP TRACK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, NR 5 FLAP TRACK MID FAIRING T/E CRACK. REMOVED CRACK MEMBER FROM NR 5 FLAP TRACK MID FAIRING IAW B727 SRM 51-30-2, FABRICATED STRAP 2024-T3 .040 PO 9001298, 20 X 4 INCH IAW B727 SRM 51-20-2. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED STRAP IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041214000112004121400011CE 2004 12 14 DXTA200400476 120041209A5730 SKIN CESSNA500 560CESSNA 2076750CE LT WING CORRODED E DXTAK NONE O OTHER ININSP/MAINT 1 GL07339QS 5600339 DURING HEAVY MAINTENANCE FOUND CORROSION AT RIGHT WING TIP AND LEFT WING UPPER SKIN. ITEM IS BEING REPAIRED. 2L72 4F RTA22CE 20041214000142004121400014NE 2004 12 14 COMA0460669 220041208A7261 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF348C1 NE ENGINE OVERSERVICED A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 SO01918CA 7018 FLIGHT 5729 HIGH OIL TEMP CAUTION MESSAGE. FOUND ENGINE OIL SYSTEM OVERFILLED. DRAINED SYSTEM AND SERVICED TO PROPER LEVEL. 2L72 4F4 FRTA21EA EOOO63EN 20041214000152004121400015NE 2004 12 14 COMA0460670 220041207A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LEFT OVERTEMP A COMAO OTHER MJ OVER TEMP WARNING INDICATION LDLANDING 1 SO01494CA 7765 873681 FLIGHT 5559 LEFT ENGINE OVERTEMP DURING ABORTED LANDING. DOWNLOAD THE DFDR TO VERIFY ENGINE EXCEEDANCE OF 925 FOR 1 SEC. NO FURTHER ACTION REQUIRED. 2L72 4F4 FRTA21EA E15NE 20041214000162004121400016EA 2004 12 14 COMA0460671 120041207A30307858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA AOA HEAT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01821CA24495612 7420 FLIGHT 5217 LT PITOT, AOA HEAT AND 2T STATIC HEAT FAIL. REPLACED THE ADHSC. 2L72 4F RTA21EA 20041214000182004121400018NM 2004 12 14 CALA0400741 120041209A52306547952524B SKIN BOEING737 7373T0 1384582NM AFT CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (3RD FROM TOP AND 1 FROM AFT EDGE OF DOOR) IN AFT CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5230-01740. 2L72 4F RTA16WE 20041214000192004121400019EA 2004 12 14 COMA0460672 120041207A3260162253 TARGET CNDAIRCL600 CL6002B19 1900309EA NLG BENT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01999CA 7230 FLIGHT 5834 GEAR DISAGREE WARNING. FOUND NLG CENTERED, PROXIMITY TARGET BENT. STRAIGHTENED TARGET AND GEAR OPERATION NORMAL. 2L72 4F RTA21EA 20041214000202004121400020SO 2004 12 14 C2XA04BT122 120041203A33501317 LAMP EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 BTV- BTV2366, DURING 4A INSPECTION, MAINTENANCE FOUND THE EMERGENCY LIGHT OVER SEAT 12C IS NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT LAMP OVER SEAT 12C IAW EMB145 AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041214000212004121400021SO 2004 12 14 C2XA04SH565 120041130A3350375901 SIGN EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2727523 145389 SHV-FLIGHT 2478, THE EXIT SIGN AT ROW 2 DOES NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTORS ON THE SIGN AND VERIFIED NORMAL OPERATION IAW EMB 145 AMM 33-50-00. 2L72 4F RTT00011AT 20041214000232004121400023SO 2004 12 14 C2XA04CL113 120041103A1420 CONNECTOR EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT DIRTY A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2714943 145040 CLE THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHTS AT ROW 8 THRU 12 WERE INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE AISLE PATH EMERGENCY LIGHT CONNECTORS. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20041214000252004121400025EA 2004 12 14 COMA0460667 120041118A5210601R3199831 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01971CA20963 7145 7145 FLIGHT DURING HEAVY MAINTENANCE CHECK, (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH COMAIR ENGINEERING AUTHORIZATION EA 10-5210-00508A. OKAY FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20041214000262004121400026SO 2004 12 14 C2XA04IA164 120041203A335020131A BATTERY EMB 145 EMB145ER 3260211SO CABIN DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929115682141 145009 CRP - DURING MAINTENANCE INSPECTION THE NUMBER THREE EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041214000272004121400027SO 2004 12 14 C2XA04SH555 120041117A521014524061007 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C-CHECK EDDY CURRENT INSPECTION OF THE PASSENGER DOOR STOP ATTACHMENT AT STRING 14L HAD A CRACK INDICATION. REAMED HOLE TO OVERSIZED CONDITION INSTALLED BUSHING IAW EC5310-01307. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041214000282004121400028 2004 12 14 04343661 420041208A2210 COMPUTER CNDAIRCL600 CL6002B19 1900309EA NR 2 FCC INOPERATIVE A VTZAO OTHER O OTHER APAPPROACH 1 EA27661BR 7520 EVENT SUMMARY STATED PITCH AND ROLL CONTROLS EXTREMELY STIFF ON FINAL. AUTO PILOT WAS DISCONNECTED FLAPS AT 20. REMOVED AND REPLACED NR 2 FCC. 2L72 4F RTA21EA 20041214000292004121400029NM 2004 12 14 513NA0011 120041212A2760 WARNING LIGHT BOEING757 7572T7 1384914NM SPOILERS ILLUMINATED A PIDAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO05513NA 23895 ABORTED TAKEOFF DUE TO SPOILER MASTER CAUTION LIGHT. PERFORMED BITE PROCEDURE, RESET SYSTEM BY FIM 27-61-00. OPERATIONAL CHECK OK. NEXT FLIGHT: SPOILER OVERHEAD LIGHT AND EICAS MESSAGE CAME ON IN FLIGHT. NO ADVERSE FLIGHT CONTROLS NOTICED. ACCOMPLISHED BITE TEST AND FOUND NR 2 LT SPOILER CONTROL MODULE FAULT. REPLACED NR 2 LT SCM PER MM 27-09-00. SYSTEM TESTS GOOD. NO FURTHER FAULTS. 2L72 4F RTA2NM 20041214000312004121400031SO 2004 12 14 C2XA04BT121 120041203A2611FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO GALLEY FAULTY A C2XAO OTHER N FALSE WARNING LDLANDING 1 SW2726545 145558 EWR - CREW REPORTED LAV SMOKE WARNING WITH ELECTRICAL SMOKE SMELL IN THE GALLEY. PERFORMED 15 MINUTES OF GROUND RUNS, OPS CHECK OF BOTH ENGINE BLEEDS AND APU BLEED. NO ELECTRICAL SMOKE NOTED. REMOVED AND REPLACED GALLEY SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041214000322004121400032EA 2004 12 14 04344673 120041209A2720 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER INOPERATIVE A VTZAB EMER. DESCENT F FLT CONT AFFECTED CLCLIMB 1 EA27673BR 7599 EVENT SUMMARY STATED WHILE CLIMBING THROUGH 2500 FT THERE WAS A LARGE YAW. UPON INITIAL INSPECTION; FOUND RUDDER TRIM SWITCH TO BE BINDING AT FULL LEFT AND FULL RIGHT DEFLECTIONS. INSPECTED RUDDER TRIM SYSTEM WIRING FOR SHORTS REF WIRING MAN 27-22-00, NONE FOUND AT THIS TIME. REMOVED AND REPLACED RUDDER TRIM PANEL REF MM CH 27-12-10, PERFORMED OPS CHECK OF AILERON AND RUDDER TRIM SYSTEM REF MM CH 27-11-00 AND MM CH 27-21-00, NO DEFECTS NOTED. S/N ON MULT1073926, S/N OFF MULT2624116. 2L72 4F RTA21EA 20041214000342004121400034EU 2004 12 14 MALA040748 120040926A5320 ANGLE BAC 146 AVRO146RJ85A1500097EU LT MLG WW CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, LEFT GEAR BAY DIVIDER, LEFT UPPER ANGLE CRACKED. MAINTENANCE REPAIRED WITH MANUFACTURED PART IAW 53-42-00, 51-24-11, 51-25-00, 51-13-00, 53-20-16 OF SRM. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000352004121400035EU 2004 12 14 MALA040751 120040926A5710 SEAL BAC 146 AVRO146RJ85A1500097EU LT WING SHROUD WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, LEFT O/B WING SHROUD TRAILING EDGE SEAL WORN. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000392004121400039WP 2004 12 14 AALA20041195 120041202A3260833703 DOWNLOCK SENSOR DOUG DC9 DC983 3022083WP MLG INOPERATIVE A AALAO OTHER N FALSE WARNING APAPPROACH 1 SW219629H 53599 LAX - INFLIGHT ON APPROACH NOSE LANDING GEAR GREEN LIGHT DID NOT COME ON. ON SECOND APPROACH THE NOSE LANDING GEAR EXTENDED NORMALLY. NOSE LANDING LIGHT TESTED GOOD. NOSE LANDING LIGHT FLICKERED ON LANDING. REPLACED DOWNLOCK SENSOR FOR NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041214000402004121400040EU 2004 12 14 MALA040762 120040929A5320 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FLOOR SUPPORT STRUCTURE INTERCOSTAL BETWEEN FRAMES 41 & 43 HAS CORROSION. MAINTENANCE REPAIRED IAW EO A53202. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000412004121400041EU 2004 12 14 MALA040766 120040927A5320 STRAP BAC 146 AVRO146RJ85A1500097EU CARGO FLOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FWD CARGO PIT FLOOR STRAP CORRODED. MAINTENANCE REPAIRED IAW SRM 51-42-00. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000432004121400043NE 2004 12 14 MALA040746 220041206A7320216362038 MANIFOLD BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE FUEL SYSTEM LEAKING A MALAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL15530XJ E2364 DURING TAKEOFF ON FLIGHT 3669, NR 4 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE COMPLETED INSPECTION OF ENGINE NR 4, 1 & 2 FOR FIRE INDICATION. NO DEFECTS NOTED. INSPECTED NR 4 ENGINE FIRE LOOPS A & B. NO INDICATIONS NOTED. FIRE BOTTLE WAS NOT DISCHARGED. SUSPECT FUEL MAINFOLD LEAKING. COMPLETED TASK CARD 7310-501. REPLACED BOTH FUEL MANIFOLDS. LT FUEL MANIFOLD P/N 2-163-620-38, S/N OFF 13-714, RT FUEL MANIFOLD P/N 2-163-620-37, S/N OFF 1XM02556. LEAK AND OPS CHECK GOOD. 2H74 4F4 FRTA49EU E6NE 20041214000452004121400045EA 2004 12 14 04342673 120041207A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER INOPERATIVE A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27673BR 7599 CREW REPORT STATED PLANE BANKED HARD RIGHT WHEN A/P KICKED OFF. RESET SECU IAW 27-61-05. 2L72 4F RTA21EA 20041214000472004121400047NM 2004 12 14 DHL2004755509 120041022A5311 FRAME BOEING727 727225 1384077NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, STA 520 FRAME RT ABOVE STR 24 HAS A DENT IN RADIUS. CUT OUT DAMAGED SECTION OF FRAME AT STA 520 ABOVE STR 24 RT IAW B727 SRM 53-10-4 FIG 1. FABRICATED & INSTALLED REPAIR DOUBLER IAW B727 SRM 53-10-4 FIG 1. MAT USED .071 7075T-6 11 X 4.5 INCH PO 900606 ALL PARTS & AREA TREATED & PRIMED IAW B727 SRM 51-10-2. 2L73 4F A3WE 20041214000482004121400048WP 2004 12 14 AALA20041207 120041210A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW213507A 49801 LGA - TWO AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TWO AFT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041214000492004121400049EU 2004 12 14 MALA040750 120040926A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT WING SPOILER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, RT I/B WING LIFT SPOILER TRAILING EDGE SEAL STRIP DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000522004121400052EU 2004 12 14 MALA040769 120041202A3150 WEU SAAB SF340 340B 7860101EU RT GENERATOR MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15444XJ 340B444 RT GEN OVERTEMP ILLUMINATED IN CRUISE. COMPLETED QRH, CAUTION WAS INTERMITTENT THRU OUT FLIGHT. AFTER TURNING GEN OFF NOTED NO OVER OR UNDER VOLTAGE. AIR RETURN TO MEM. MAINTENANCE REPLACED WEU. 2L72 4T RTA52EU 20041214000532004121400053EU 2004 12 14 MALA040772 120041205A2613 SENSOR SAAB SF340 340B 7860101EU RT TAILPIPE CONTAMINATED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15412XJ 340B412 AFTER TAKEOFF THE RT TAIL PIPE HOT LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE APPLIED SEALENT TO TAIL PIPE SENSORS IAW SMM CHP 54-30-05-2 OPS CHECK GOOD IAW SMM CHP 26-11-00-5. 2L72 4T RTA52EU 20041214000542004121400054EU 2004 12 14 MALA040752 120040926A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT GRND SPOILER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, LT O/B GROUND SPOILER TRAILING EDGE SEAL DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000552004121400055EU 2004 12 14 MALA040758 120040926A5414 PANEL BAC 146 AVRO146RJ85A1500097EU NR 2 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, NR 2 ENGINE ZONE 2 COWL OUTBOARD DISHING PANEL CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000582004121400058EU 2004 12 14 MALA040765 120040927A5321 FLOOR PANEL BAC 146 AVRO146RJ85A1500097EU CARGO BAY CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ DURING C-CHECK INSPECTION IN YYC, FWD CARGO FLOOR PANEL 141EL HAS CORROSION. MAINTENANCE REPAIRED IAW SRM 51-42-00 & 51-20-11. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000602004121400060WP 2004 12 14 AALA20041194 120041206A56105887275505 WINDOW DOUG DC9 DC982 3022082WP COCKPIT CRACKED A AALAO OTHER O OTHER CRCRUISE 1 SW21458AA 49563 LAX - INFLIGHT CENTER WINDSHIELD ARCHED ON RIGHT SIDE AND WINDSHIELD CRACKED AT FL370. REPLACED WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041214000632004121400063EU 2004 12 14 MALA040754 120040926A5755 SEAL BAC 146 AVRO146RJ85A1500097EU GRND SPOILER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, LT I/B GROUND SPOILER TRAILING EDGE SEAL DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000652004121400065CE 2004 12 14 DXTA200400473 120041208A3240515712 BRAKE ASSY CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07996QS2125 7500196 RIGHT BRAKE VERY SOFT, BRAKE INDICTOR VERY LITTLE REMAINING. INSPECT THE RIGHT HAND SIDE BRAKE SYSTEM, 3 BRAKE INDICATOR HAD .075 INCH REMAINING AND NR 4 BRAKE INDICATOR HAS .068 REMAINING. REMOVED AND REPLACED BOTH NR 3 & NR 4 BRAKE ASSEMBLIES AND SHUTTLE VALVES, SYSTEM OPS CHECKED GOOD. 2L72 4J RTT00007WI 20041214000672004121400067NM 2004 12 14 DHL2004755512 120041021A5330 SKIN BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, CORROSION FUSELAGE SKIN UNDER WING-TO-BODY FAIRINGS STA 720 D +14 STR 10 LEFT. REMOVED ANTI ICE DUCTS, HYD LINES & HARDWARE. REMOVED LT WING ROOT HARNESSES, CUT OUT DAMAGED UPPER SKIN 4.5 X 3", FABRICATED DOUBLER REPAIR 9.5 X 12", SHIM 12 X 3", FILLER 14 X 7.5" 2024T3 .071 PO 9001424 IAW B727 SRM 53-30-3 FIG 6. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR, INSTALLED ANTI ICE DUCTS HYD LINES AND WING TO BODY FAIRING HARDWARE. INSTALLED LT WING ROOT WIRE HARNESS. 2L73 4F A3WE 20041214000702004121400070NM 2004 12 14 AALA20041199 120041206A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21954AN 30089 ORD - EMERGENCY LIGHTS THROUGHOUT CABIN FAILED TEST. REPLACED ALL NINE BATTERY PACKS FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20041214000712004121400071WP 2004 12 14 AALA20041202 120041208A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21110HM 49787 BOS - FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041214000762004121400076 2004 12 14 MWEA040196 420041028A3417102JD2FE PROBE BOEING717 717200 1383700NM RAM AIR TEMP INOPERATIVE A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31914ME 55177 RAM AIR TEMPERATURE PROBE FAIL. REMOVED AND REPLACED RAM AIR TEMPERATURE PROBE. 2L72 4F TRA6WE 20041214000772004121400077NM 2004 12 14 MWEA040197 120041029A531059568791 DOOR FRAME DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 PASSENGER DOOR JAMB WEB TANG IS CRACKED AT STATION 207 LONGERON 15 LEFT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F RTA6WE 20041214000792004121400079NM 2004 12 14 UPS04243272 120040920A5340 FITTING BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE:C, SUSPECT CRACK FROM RIGHT TERMINAL FITTING FOR STABILIZING LINK LWR IN TA TAIL SKID COMPARTMENT. INSTALLED NEW TERMINAL FITTING IAW SRM 51-30-02. 2L73 4F A3WE 20041214000832004121400083SO 2004 12 14 RAIA00411006 120041104A2760140197 TRANSDUCER EMB 145 EMB145LR 3260212SO SPOILERS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03818HK 145059 BDL- SPOILERS DEPLOY ON GROUND. REMOVED AND REPLACED NR 2 WHEEL SPEED TRANSDUCER. 2L72 4T RTT00011AT 20041214000862004121400086 2004 12 14 SWAA043289 420041110A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041214000872004121400087NM 2004 12 14 UPS04243374 120041020A2711 TAB BOEING727 727185C 138406NNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:C, I/B RIGHT AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REMOVED AILERON IAW AMM 27-10-00, REMOVED HINGES & SPAR IAW SRM 51-3 -30-02. SPAR REPAIRED IAW SRM 57-30-2 FIG 7 & SRM 51-40-02 FIG 1. NEW HINGES INSTALLED IAW SRM 51-30-2 AND DWG 65-21765. WEIGHT OF REPAIR .051LB ARM 20.75 INCHS. INSTALLED TAB HINGES IAW SRM 51-30-02 AND INSTALLED TAB IAW MM 27-10-05. 2L73 4F A3WE 20041214000882004121400088WP 2004 12 14 MWEA040210 120041111A3397 WIRE DOUG DC9 DC981 3022081WP ROW 1C BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31814ME 48010 FLOOR TRACK WIRING IS BROKEN & STICKING OUT OF FLOOR COVER. REPAIRED WIRE. 2L72 4F A6WE 20041214000892004121400089NM 2004 12 14 SWAA043282 120041110A32601899 DOWNLOCK SENSOR BOEING737 7373H4 1384600NM RT MLG OUT OF ADJUST A SWAAO OTHER J WARNING INDICATION LDLANDING 1 SW29372SW 26599 RT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR LOWERED FOR LANDING. RECYCLED GEAR, NO CHANGE. USED MANUAL GEAR EXTENSION, NORMAL LANDING. ADJUSTED RT MLG DOWNLOCK SENSOR PER MM. 2L72 4F RTA16WE 20041214000902004121400090NM 2004 12 14 UPS04243243 120040908A5753652163350 SKIN BOEING727 727173C 1384059NM RT MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, DELAM ON RIGHT O/B MIDFLAP T/E WEDGE FWD FACE I/B OF NR 2 AFT FLAP TRACK. DELAM OUT OF LIMITS. MIDFLAP REPLACED IAW MM 27-51-12. 2L73 4F A3WE 20041214000912004121400091WP 2004 12 14 UPS04843362 120041016A3350 LAMP DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 ENTRY DOOR EMERGENCY LIGHTS, 1 AFT INOP. RELAMPED EMERGENCY LIGHTS, OPS GOOD. 2L74 4F RT4A25 20041214000922004121400092NM 2004 12 14 DL73S040985 120041019A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27323DL 23095 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003- 08-15 REVEALED MULTIPLE CRACKS BETWEEN FS 560 & 620. THE CRACKS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 094301-14AD. 2L72 4F RTA16WE 20041214000932004121400093 2004 12 14 119522 420040727A34256226190113 AHRS SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE COCKPIT FAILED A UHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL1795 N95 FLIGHT 7941 IAD-BGM. DURING TAKEOFF ROLL THE FIRST OFFICER'S EADI SHOWED A 40 DEGREE TURN AND 10 DEGREES NOSE DOWN ATTITUDE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. A/C TAKEN OUT OF SERVICE 7-27-04 AT 1745 (LT). IAD MX REMOVED AND REPLACED THE NR 2 AHRS COMPUTER, SYSTEM OPERATIONAL TEST GOOD. A/C RETURNED TO SERVICE 7-27-04 AT 1845 (LT). 2L72 4T4 TRTA52EU E8NE6 20041214000942004121400094NM 2004 12 14 DL738040986 120041021A5210 DOOR BOEING737 737832 13844CFNM 1L UNSAFETIED A DALAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO27372DA 29620 FLT 473 SAN - JFK DIVERTED TO LAX, LOUD AIR LEAK NOISE FROM 1L DOOR AND NO PRESSURIZATION. FOUND 1L DOOR AFT EDGE NOT FULLY CLOSED. INSPECTED DOOR AND SEAL, CYCLE SEVERAL TIMES, PRESSURIZED ACFT, AND ALL CHECK NORMAL. NO PARTS REQUIRED. 2L72 4F RTA16WE 20041214000952004121400095NM 2004 12 14 DL76L040987 120041022A2750271003343 SHUTOFF VALVE BOEING767 767332 1382001NM TE FLAPS FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27189DN 25990 FLAPS FAILED TO RETRACT PAST 5 AFTER T/O. ALSO RECEIVED A TRAILING EDGE DISAGREE LIGHT. REPLACED RELAY K351 AND SHUTOFF VALVE SOLENOID V1. 2L72 4F RTA1NM 20041214000962004121400096NM 2004 12 14 DL757040988 120041022A5330141N33131 SKIN BOEING757 757232 1384965NM L1 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27615DL 22822 FUSELAGE SKIN AND BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. REPAIRED IAW ERA 094411-14AD. 2L72 4F RTA2NM 20041214000972004121400097NM 2004 12 14 DL757040989 120041025A2420 CHIP DETECTOR BOEING757 757232 1384965NM NR 1 IDG CRACKED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27607DL 22814 EICAS MSG LEFT GENERATOR DRIVE DISPLAYED. SERVICED OIL. REPLACED CRACKED CHIP DETECTOR. 2L72 4F RTA2NM 20041214000982004121400098NM 2004 12 14 F3LA200400080 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSELAGE SCRATCHED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK AT 178 BULKHEAD O/B OF RBL 5.7 AT WL 218. DETERMINED TO BE A SCRATCH, NOT A CRACK. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR PER EA B3-53R-10470 AND SRM 53-10-08 FIG 209 DETAIL 3. 2L72 4F RTA16WE 20041214001002004121400100SO 2004 12 14 MASA200400595 120041022A3243 CONNECTOR EMB 145 EMB145LR 3260212SO BRAKES LOOSE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07830MJ 145259 THE CREW ABORTED TAKEOFF DUE TO A BRAKE OUTBOARD INOP EICAS MESSAGE. CONTRACT MX FOUND LOOSE CONNECTORS ON BOTH OUTBOARD BRAKES. THE CONNECTORS WERE CHECKED FOR CONDITION AND CLEANED WITH NO DEFECTS NOTED. A TAXI AND OPERATIONAL CHECK WERE PERFORMED WITH NO FAULTS DISPLAYED. 2L72 4T RTT00011AT 20041214001012004121400101SO 2004 12 14 MASA200400042 120040123A2560P2070011100 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07855MJ 145614 AFT CABIN EMERGENCY FLASHLIGHT INOP. MX REPLACED THE FLASHLIGHT. OP CHECKS GOOD. 2L72 4T RTT00011AT 20041214001022004121400102EU 2004 12 14 MALA040658 120041021A2120 ODOR SAAB SF340 340B 7860101EU CABIN DETECTED A MALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL15443XJ 340B443 STRONG PLASTIC ODOR IN ENTIRE CABIN OF AIRCRAFT INFLIGHT. MAINTENANCE INSPECTED A/C INTERIOR, EXTERIOR, AND UNDER FLOORBOARDS FOR POSSIBLE SOUCE OR ODOR. NO DEFECTS NOTED. RAN A/C 20 MINUTES ON GROUND, NO UNUSUAL ODORS NOTED BY EITHER TECHNICIAN ON BOARD. SUSPECT ODOR MAY HAVE BEEN RTV, AS A/C RECETLY OUT OF C-CHECK. OPS CHECK OF ALL BLEED VALVES HP/LP BOTH ENGINE GOOD. 2L72 4T RTA52EU 20041209000282004120900028SO 2004 12 9 MASA200400625 120041105A7830 WARNING SYSTEM EMB 145 EMB145LR 3260212SO THRUST REVERSER ACTIVATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07837MJ 145367 ASH 2784 CLT. REJECTED TAKEOFF DUE TO AN E2 THRUST REVERSER DISAGREE. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE FAULT 11/05/04. MAINTENANCE SECURED CONNECTOR ON PDU AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041209000312004120900031SO 2004 12 9 MASA200400662 120041128A5210 SEAL EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07827MJ 145217 ASH 2665 CLT - ILM. MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED THE MAIN CABIN DOOR SEAL, OPS GOOD. 2L72 4T RTT00011AT 20041209000372004120900037NM 2004 12 9 DL73S041063 120041126A21337110033 OUTFLOW VALVE BOEING737 737232 1384475NM CABIN PRESSURE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27309DL 23081 ACFT UNABLE TO PRESSURIZE IN STBY MODE. REMOVED AFT OUTFLOW VALVE. INSTALLED NEW VALVE PER MAINTENANCE MANUAL. ALSO REPLACED CONTROLLER AND PANEL TEST SYS PER MAINTENANCE MANUAL. 2L72 4F RTA16WE 20041209000422004120900042NM 2004 12 9 DLM88041078 120041203A5330591140614 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27909DE 53418 FUSELAGE SKIN REPAIR DENTED AT STATION 229 AND LONGERON 17L. REPAIRED IAW ERA 385592-14 REV A. 2L72 4F RTA6WE 20041209000442004120900044SO 2004 12 9 MASA200400658 120041127A33501317 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07844MJ 145481 ASH 2986 CLT. EMERGENCY LIGHTS INOP. MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041209000732004120900073 2004 12 9 SWAA043389 420041119A3197RH5510 RELAY BOEING737 7373H4 1384600NM INSTRUMENT PANELFAULTY A SWAAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SW29607SW 27927 AIR TURNBACK, DURING ROTATION ACFT LOST ALL N1, EGT INDS, & ANNUNCIATOR LIGHTS. LANDING GEAR LEVER WOULD NOT MOVE UP. REMOVED AND REPLACED R1 RELAY, (BAT BUS AUTO RELAY) PER MM. 2L72 4F RTA16WE 20041209000782004120900078WP 2004 12 9 UPS04843304 120040912A534037558411 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, BS 1220.00 & L34R BATHTUB FITTING HAS CORROSION. REMOVED AND REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2G. 2L74 4F RT4A25 20041209000802004120900080NM 2004 12 9 UPS04243079 120040823A575365847812 CASTING BOEING727 727108C 1384039NM NR 7 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, CRACK ON NR 7 FLAP TRACK CASTING ON VERTICAL FLANGE SECOND FROM I/B. HFEC CARRIED OUT - CRACKS CONFIRMED AND ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-1. OUTSIDE LIMITS PER SRM 51-10-6. CASTING REPLACED AND INSTALLED IAW DRG 65-16201. 2L73 4F A3WE 20041209000822004120900082NM 2004 12 9 UPS04243081 120040817A5711 SPAR BOEING727 727108C 1384039NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 INSPECTION TYPE: C, CRACK INDICATION AT WS 205 ON LT UPPER CHORD REAR SPAR. REPAIR CARRIED OUT IAW AAAE EO 2004-077-005. REF UPS EO B727-5710-20995. 2L73 4F A3WE 20041209000842004120900084NM 2004 12 9 UPS04243082 120040903A33501000679 LIGHT BOEING727 72725C 138400HNM L1 EXIT DOOR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:N/A, EMERGENCY LIGHTING INOP AT L1 EXIT DOOR. REPLACED EMERGENCY EXIT LIGHT ASSY AT L1 DOOR PER MM 33-50-01, OPS CHECK GOOD. 2L73 4F A3WE 20041209000882004120900088WP 2004 12 9 UPS04843202 120040928A3397 PIN DOUG DC8 DC871F 302199DWP CONNECTOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:N/A BTB - EMERGENCY EXIT LIGHTS REMAINED ON DURING PUSHBACK SWITCH IN ARMED POSITION & GENERATOR NR 2 & NR 3 POWERING THE A/C. BLOCKED OUT AT 0221 BLOCKED IN 0232. FOUND PINS NR 9 & 10 PUSHED BACK ON CONNECTOR P1-1345. CLEANED AND RESET PINS. ALSO REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR PRECAUTIONARY. SYS OPS CHECKS NORMAL PER MM 33-50-01-2. 2L74 4F RT4A25 20041209000932004120900093EU 2004 12 9 MALA040694 120041005A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15367PX 340B271 DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-0478-9, S/N 9804449 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04. 2L72 4T RTA52EU 20041209000952004120900095EA 2004 12 9 MASA200400496 120040903A5610NP13932210 WINDSHIELD CNDAIRCL600 CL6002D24 1390016EA COCKPIT CRACKED A MASAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW07916FJ1412 15016 REJECTED TAKEOFF FOR A F/O WINDSHIELD SHATTERED ON TAKEOFF ROLL. AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. 9/4/04 MAINTENANCE REPLACED THE RT CO-PILOT WINDSHIELD. 2L72 4F RTA21EA 20041209000972004120900097NM 2004 12 9 UPS04443398 120040921A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, CRACK FOUND AT LEFT BS 488 AT NR 1 MED AT AFT FRAME WEB RUNNING DOWN FROM INNER CHORD .0625 INCH LONG (BS 488, STR L25 TO L25). CABIN LEFT BS 488 STR 23 TO STR 30 WEB REPAIRED AS PER SRM 53-10-04 FIG 92. 2L74 4F A20WE 20041209001032004120900103NM 2004 12 9 UPS04M43284 120040815A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 19 RIGHT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT NR 19 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 19 RIGHT INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 19 RIGHT PER EO MD11-5510-19409-H & EN 1295-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041209001152004120900115NM 2004 12 9 2004UALA01158 120041124A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT FRAME DENTED ON UPPER FLANGE STA 1400 AND STR 26L. INSTALLED NESTED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041209001172004120900117WP 2004 12 9 UPS04843576 120041122A5310975890715 GUSSET DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 GUSSET CRACKED AT STA 460 ABOVE LONG 31 R. REMOVED CRACKED GUSSET REF SRM 51-1-21. FABRICATED REPLACEMENT GUSSET FROM SHT7075T6/.080 REF DWG 9758907. INSTALLED SAME REF SRM 51-1-8, AND 51-1-20D 2L74 4F RT4A25 20041209001212004120900121EU 2004 12 9 A6WA200460058 120041116A3340 HOUSING BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE LIGHT CHAFED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31292UE E2087 CHAFING ON THE LT SIDE OF THE AFT NAVIGATION LIGHT HOUSING. MAINTENANCE REQUESTED REPAIR. 2H74 4F4 F A49EU E6NE 20041209001242004120900124EA 2004 12 9 SWIA200414166 120041129A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07416SW7105 7105 7089 ON DESCENT, RECEIVED STATUS "FLT SPOILER FAULT" MESSAGE ON THE RIGHT SIDE. REMOVED AND REPLACED RIGHT OUTBOARD FLIGHT SPOILER PCU IAW CRJ 200 MM 27-62-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041209001262004120900126SO 2004 12 9 RAIA00412005 120041205A3620S568230 SEAL EMB 145 EMB145LR 3260212SO BLEED AIR SYS FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03814HK 145046 NR 1 BLEED LEAK. MAINTENANCE, REMOVED AND REPLACED BLEED SEALS. 2L72 4T RTT00011AT 20041209001282004120900128 2004 12 9 RAIA00412003 420041205A3497 WIRE JETAIRJETSTMJETSTM4101 1500501EU STICK SHAKER DAMAGED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03569HK 41088 RIGHT STICKER SHAKER DID NOT WORK DURING FIRST FLIGHT CHECKS. MAINTENANCE, REPAIRED WIRING AT F/O STICK SHAKER. 2L72 4T RTA41NM 20041210000102004121000010WP 2004 12 10 UPS04843574 120041126A5320 WEB DOUG DC8 DC871F 302199DWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 TORQUE BOX WEB CORRODED BEYOND LIMITS AT STA 1200, LONG 36. REMOVED FASTENERS TO FOM REF SRM51-1-20D. REMOVED CORROSION REF SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL RANGE 0.125" - 0.088" REF NDT SPM 04-00-06. FABRICATED REPAIR DOUBLER FROM SHT7075T6-.160" REF SRM 53-2-0 FIG23, 53-2-0 FIG25 DWG9754945, 3753772. INSTALLED REPAIR REF SRM51-1-8, 51-1-21, 51-1-20D 2L74 4F RT4A25 20041210000282004121000028NM 2004 12 10 ASA0440185 120041016A53106546548 SHEAR TIE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU AFT CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 PAE - CORROSION AFT CARGO BAY ON SHEAR TIE. REMOVED CORRODED SHEAR-TIE, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20041210000372004121000037NM 2004 12 10 QXEA200400812 120041126A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - NR 2 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF RAILS AT X451-X453, X486 AND IN BOTTOM OF CHANNEL AT X439 AND X452. REPAIRED IAW RD 8-53-8209, PAGE 4, FIGURE 4. 2H72 4T RTA13NM 20041210000842004121000084EA 2004 12 10 04322652 120041117A2930 PUMP CNDAIRCL600 CL6002B19 1900309EA HYD SYSTEM INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27652BR 7429 CREW REPORT STATES RECEIVED CAUTION MSG HYD PUMP 3B INOP. OHM WIRING FOR THE 3B HYD PUMP TO CIRCUIT BREAKER A2 ON CB PNL 1. NO DEFECTS ARE NOTED IN WIRING REPLACE 3B HYD PUMP. THIS WO IS STILL IN APPR STAGE. 2L72 4F RTA21EA 20041213000022004121300002NM 2004 12 13 SWAA043585 120041208A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED RON, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041213000072004121300007NM 2004 12 13 SWAA043568 120041207A3350604222 BATTERY BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29523SW 26565 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041213000182004121300018NM 2004 12 13 AALA20041206 120041207A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21772AN 29580 DFW - EMERGENCY ESCAPE PATH LIGHT IN TOURIST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT IN TOURIST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041213000362004121300036WP 2004 12 13 AALA20041183 120041129A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21974TW 53624 SEA - EMERGENCY EXIT SIGNS ABOVE LEFT AND RIGHT FORWARD OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK AT B5103 FOR EMERGENCY EXIT SIGNS ABOVE LEFT AND RIGHT FORWARD OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041213000382004121300038WP 2004 12 13 AALA20041192 120041205A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT EXPOSED A AALAK NONE O OTHER ININSP/MAINT 1 SW21253AA 49286 SFO - EMERGENCY EXIT LIGHTS AT SEAT 7D INOPERATIVE. FOUND OPEN WIRE TO EMERGENCY SEAT HARNESS. REPAIRED WIRE FOR EMERGENCY EXIT LIGHTS AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000472004121300047NM 2004 12 13 UPS04543585 120041205A2120 ODOR BOEING757 75724APF 1384969NM COCKPIT DETECTED A IPXAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01465UP 28269 ATB - STRONG SMELL IN COCKPIT AFTER T/O. RAN LEFT AND RIGHT ENGS & PRESSURIZED A/C WITH BLEED AIR FROM ENGS. ALSO WITH APU BLEED & NO ODORS NOTED. INSP LT & RT A/C PACKS INLET PRIM & SEC HEAT EXCHANGERS INSP PNLS, ALL OK. INSPECTED BEHIND C/B PNLS IN C/P, E&E & ALL OK. UPON FURTHER INSP, FOUND CLEANING CREW LEFT SOILED CLEANING RAG CAUSED ODOR. AIRED OUT A/C OK FOR SERVICE. 2L72 4F RTA2NM 20041213000482004121300048WP 2004 12 13 UPS04843591 120041208A3260H141003 DOWNLOCK SWITCH DOUG DC8 DC873F 302199FWP RT MLG FAILED A IPXAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 SO01852UP 46052 RIGHT LANDING GEAR GREEN DOWN INDICATION FOR SAFE AND LOCKED INOP WITH FLAPS AT 35 DEGREES AND BEYOND NO UNSAFE WARNING HORN PRODUCED. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWN SNAP SWITCH IAW DC-8 M/M 32-60-00-2 AND CONNECTOR AS REFERENCED ON ITEM 3 THIS L/P OPS CHECKS GOOD AT THIS TIME. A/C OK FOR CONTINUED SERVICE. 2L74 4F RT4A25 20041213000562004121300056CE 2004 12 13 ACE120404 120041204A53471144301063 SEAT TRACK BEECH 1900 1900C 1154161CE FUSELAGE CORRODED E YADAK NONE O OTHER ININSP/MAINT 1 AL03114AX UC36 DURING CAMP INSPECTION, MAINTENANCE LOCATED CORROSION ON SEAT TRACK FLOOR PANEL FLANGES. SEAT TRACK AND ADJACENT LOCALIZED CORROSION SUSPECTED TO HAVE BEEN CAUSED BY CARGO SPILLAGE. SEAT TRACK REPLACED, OTHER AREAS REPAIRED. 2L72 4T RTA24CE 20041213000582004121300058 2004 12 13 04329710 420041124A3418 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27710BR 7852 STICKER SHAKER WENT OFF. MX REMOVED AND REPLACED STALL PROTECTION COMPUTER. 2L72 4F RTA21EA 20041213000592004121300059CE 2004 12 13 CWQR200400006 120041130A2820661645010 TUBE CESSNA560 560XL 2076702CE TAILCONE CRACKED B DXTAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 GL05603QS3190 5605203 AIRCRAFT WAS LEAKING FUEL. TECHNICIAN FOUND A 1.3 INCH CRACK IN -Y- TUBE IN PRESSURE REFUELING SYSTEM. NO EVIDENCE OF DAMAGE TO TUBE ASSY. REPLACED TUBE ASSY, AND LEAK CHECKED GOOD. 2L72 4F RTA22CE 20041213000622004121300062NM 2004 12 13 SWAA043591 120041209A534065C27314 STRINGER CLIP BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 277, STRINGER 15R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041213000792004121300079NM 2004 12 13 SWAA043584 120041208A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 786, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041213000822004121300082NM 2004 12 13 WLDA2004107 120041127A2750 CONTROLLER DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE TE FLAPS MALFUNCTIONED A WRLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11272 48437 FRA/KWI REJECTED TAKEOFF AT 40 KTS DUE TO FLAPS TAKEOFF WARNING. RECYCLED FLAPS, OPERATIONS CHECK ALL NORMAL. RESUMED NORMAL PROCEDURES. 2L73 4F4 FRTA22WE E24NE 20041213000892004121300089CE 2004 12 13 ACE110304 120041103A3260MS252531 SWITCH BEECH 1900 1900C 1154161CE COCKPIT LOOSE E YADAO OTHER J WARNING INDICATION APAPPROACH 1 AL03112AX UC45 PILOT REPORTED USING LANDING GEAR EMERGENCY PROCEDURE DUE CONTINUED GEAR UNSAFE WARNING EVEN WITH ALL GREEN DOWN AND LOCKED LIGHTS ON. UNEVENTFUL LANDING COMPLETED. MAINTENANCE LOCATED AND CORRECTED A LOOSE POWER LEVER POSITION SWITCH. 2L72 4T RTA24CE 20041213000902004121300090NM 2004 12 13 0402086312 120041125A3260856917 PSEU BOEING747 747451 1384940NM MLG FAILED A NWAAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01672US298017575 30267 DURING CLIMB, RECEIVED A GEAR DISAGREE AND GEAR DOOR EICAS MESSAGE ACCOMPANIED WITH VIBRATION AND NOISE. AIRCRAFT RETURNED TO DTW AND DUMPED 200,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. REPLACED THE PSEU. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20041213001012004121300101NM 2004 12 13 SWAA043561 120041207A3350PH22300L LIGHT BOEING737 737301 1384611NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 EEPLS STRIP FROM ROW 6 ABC TO ROW 8 ABC, LOOSE. SECURED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20041213001022004121300102CE 2004 12 13 DXTA200400456 120041122A282123061826 FUEL FILTER CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RT ENGINE CLOGGED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 GL07953QS 7500153 CAE330322 FUEL FILTER BYPASS-R CAS MESSAGE CAME ON DURING THE T/O ROLL. INSPECTED PER ROLLS ROYCE MM 73-30-00200-801 AND FOUND THAT FUEL FILTER NEEDED TO BE REPLACED. REMOVED & INSTALLED NEW FUEL FILTER AND O-RINGS WITH KIT P/N 23061826 RESET BYPASS INDICATOR PERFORMED MAINT GROUND RUNS AND NO LEAKS WERE FOUND. ALL WORK DONE IAW ROLLS-ROYCE MM 73-21-10-000-802, 73-21-10-400-802, 73-30-00-200-801. 2L72 4J4 FRTT00007WITE6CH 20041213001042004121300104EU 2004 12 13 DXTA200400457 120041122A2120 ODOR BRAERO1000 HAWKER1000 7450005EU COCKPIT DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07549QS 259049 AFTER TWO HOURS OF FLIGHT BOTH PILOTS SMELLED STRONG ELECTRICAL / BURNED OIL FUMES WHICH IRRITATED EYES. NO VISIBLE FUMES MAIN AIR VALVES SELECTED TO LOW PRESSURE FUMES DISAPPEARED. AIRCRAFT RUN UP SYSTEMS OPS CHECKED GOOD. DUCTS WORK INSPECTED (LOW PSI) NO DEFECTS. RT & LT ENG OIL SERVICING CHECKED, AGB OIL SERVICING NORMAL. NO DISCREPANCY FOUND. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA3EU 20041213001112004121300111NM 2004 12 13 DHL2004755505 120041018A5753 SKIN BOEING727 727225 1384077NM LT TE FLAPS GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 93 NEAR L/E HAS SKIN GOUGED. GOUGE IN SKIN FOUND TO BE OUT OF LIMITS NDT VERIFY NO FURTHER DAMAGE IAW B727 SRM 57-50-1. REMOVED DAMAGED AREA OF SKIN 1 X 1 INCH IAW B727 SRM 57-50-4. FABRICATED DOUBLER FROM 2024-T3, 4.8 X 4.8 INCH AND FILLER FROM 2024T3.063, .9 X .9 INCH IAW B727 SRM 57-50-4. ALODINED & PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR DOUBLER & FILLER IAW B727 SRM 57-50-4 FIG 10. 2L73 4F A3WE 20041214000022004121400002EU 2004 12 14 MALA040761 120040929A5311 FLOOR SUPPORT BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FLOOR SUPPORT STRUCTURE INTERCOSTAL LEFT INBOARD BETWEEN FRAMES 41 & 43 HAS CORROSION. MAINTENANCE MANUFACTURED NEW PART IAW SRM 51-42-00 & 51-43-00. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000032004121400003EU 2004 12 14 MALA040770 120041206A30206124100 DUCT SAAB SF340 340B 7860101EU RT INTAKE HEAT LEAKING A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15364PX 340B262 AFTER TAKEOFF THE RT INTAKE HEAT CAUTION LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED LOWER DUCT P/N 6124-100, S/N ON 292, S/N OFF 366. 2L72 4T RTA52EU 20041214000122004121400012 2004 12 14 04347634 420041212A3140 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA CONFIGURATION ACTIVATED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27634BR 7287 ABORTED TAKEOFF FOR WARNING MESSAGE, NO TAKEOFF CONFIGURATION TEST OK MESSAGE WILL POST. MX PERFORMED TAKEOFF CONFIGURATION CHECKS. OPS CHECK GOOD, ALL INDICATIONS NORMAL. 2L72 4F RTA21EA 20041214000222004121400022SO 2004 12 14 C2XA04RI014 120041109A1420 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 RIC - MX, DURING PREFLIGHT CHECK, MAINTENANCE FOUND FWD EMERGENCY EXIT LIGHT INOP. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND EMERGENCY LIGHT CONNECTOR LOOSE. MAINTENANCE SECURED LOOSE CONNECTOR. OPERATIONAL TESTS WERE PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATION. 2L72 4F RT 20041214000372004121400037EU 2004 12 14 MALA040747 120040926A5320 BRACKET BAC 146 AVRO146RJ85A1500097EU MLG WW CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, GEAR BAY DIVIDER, LEFT FORWARD LOWER BRACKET CRACKED. MAINTENANCE REPAIRED WITH MANUFACTURED PART IAW 53-20-16, 51-24-11, 51-43-00, 51-20-11 OF SRM. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000382004121400038EU 2004 12 14 MALA040757 120040926A7160 DUCT BAC 146 AVRO146RJ85A1500097EU NR 3 ENG FAN CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, NR 3 ENGINE LT AFT FAN DUCT COWLING CHAFED. MAINTENANCE MANUFACTURED AND INSTALLED PART IAW SRM 51-26-11, 51-42-00, 51-43-00. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000502004121400050EU 2004 12 14 MALA040764 120040928A5321HC252B1016223 STRIP BAC 146 AVRO146RJ85A1500097EU FLOOR PANEL CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, AFT CARGO PIT FLOOR PANEL JOINT STRIP IS EXFOLIATED. MAINTENANCE REPLACED STRIP P/N HC252B1016-223. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000622004121400062EU 2004 12 14 MALA040753 120040926A5755 SEAL BAC 146 AVRO146RJ85A1500097EU GRND SPOILER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, LT MID GROUND SPOILER TRAILING EDGE SEAL STRIP DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000642004121400064EU 2004 12 14 MALA040760 120040926A5230HC538J0026217 SCUFF PLATE BAC 146 AVRO146RJ85A1500097EU CARGO DOOR DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, DENT FOUND ON AFT CARGO DOOR SCUFF PLATE. MAINTENANCE REPLACED SCUFF PLATE P/N HC538J0026-217. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000742004121400074CE 2004 12 14 DXTA200400438 120041103A3222 STRUT CESSNA750 750 2076810CE NLG DAMAGED E DXTAO OTHER J WARNING INDICATION CLCLIMB 1 GL07943QS5657 7500043 AFTER GEAR RETRACTION, RED UNLOCK GEAR LIGHT REMAINED ILLUMINATED. AFTER TOUCHDOWN NOTICED MODERATE VIBRATION COMING FROM GEAR. PERFORMED GEAR SWING COULD NO DUPLICATE DISCREPANCY. MEASURED NOSE STRUT FOUND OVER EXTENDED. REMOVED LOWER BARREL ASSY AND REPACKED STRUT USING CPD750-5 KIT PER 750 CMM CHAPTER 32-20-62 AND SERVICED PER 750 M/M 12-10-38. GROUND OP'S CHECKED GOOD. 2L72 4J RTT00007WI 20041214000752004121400075WP 2004 12 14 MWEA040195 120041028A1430NAS11032 BOLT DOUG DC9 DC981 3022081WP RT MLG MISSING A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31813ME 48007 RIGHT MAIN GEAR UNSAFE AND AUTO SPOILER DO NOT USE LIGHT CAME ON. FOUND BOLT MISSING FROM RIGHT MAIN LANDING GEAR DOOR TARGET ALLOWING TARGET TO ROTATE AND PREVENTING DOOR LATCH FROM FULLY SEATING IN DOOR. REPLACED MISSING HARDWARE. 2L72 4F A6WE 20041214000822004121400082NM 2004 12 14 CALA0400714 120041111A2697UNK CONNECTOR BOEING737 7373T0 1384582NM APU FIRE LOOP SHORTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 THE APU DET INOP LIGHT CAME ON WHILE CLIMBING THROUGH FL 180. THE APU FIRE WARNING LIGHT WITH FIRE BELL ACTIVATED WHILE CLIMBING THROUGH FL 330. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND FIRELOOP CONNECTOR D984 SHORTED. THE CONNECTOR WAS REPLACED. THE APU AND PACKS WERE RUN AND OPERATIONAL CHECKS OF THE APU FIRE DETECTION SYSTEM WERE GOOD. THE APU FIRE BOTTLE WAS REPLACED IAW MM 26-22-11. 2L72 4F RTA16WE 20041214000852004121400085SO 2004 12 14 SWIA200414144 120041005A5315 PLATE EMB 120 EMB120ER 3260203SO FLOORBEAM CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FS 13630.0 TO FS 15050.0 LEFT INBOARD BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041214001042004121400104NM 2004 12 14 SWAA043271 120041109A335007912 COVER BOEING737 7375H4 138449DNM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29507SW 24184 EEPLS STRIP COVER FROM ROW 17 DEF TO ROW 19 DEF, LOOSE. REMOVED AND REPLACED EEPLS STRIP COVER PER MM. 2L72 4F RTA16WE 20041214001062004121400106NM 2004 12 14 UPS04243245 120040908A5711 SPAR BOEING727 727173C 1384059NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD, RIGHT WING BETWEEN WS 290-320 APPROX. REPAIR CARRIED OUT IAW UPS EO B727-5710-17848-B APPROX C AND AAAE EO 200 4-083-004 (727-5710-21057). 2L73 4F A3WE 20041214001072004121400107NM 2004 12 14 UPS04243251 120040913A5312 PANEL BOEING727 72722C 138400FNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE:C, HULL PRESSURE LEAK IN NLG WHEEL WELL CEILING PANEL (DUE TO CRACKING) AT BS 260 LBL 20. DAMAGED AREA REMOVED AS REQUIRED IAW SRM 51-40-2. HFEC CARRIED OUT - NO DEFECTS FOUND. REPAIR PARTS FABRICATED IAW SRM 51-40-2. REPAIR PARTS INSTALLED IAW SRM 51-40-2. 2L73 4F A3WE 20041214001092004121400109NM 2004 12 14 UPS04443233 120040928A5414 SKIN BOEING747 747200 1384847NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: AD, NR 2 PYLON UPPER LINK ATTACH LUG AREA, 1EA FASTENER HOLE CRACK FOUND ON NR 2ND LAYER, APPROX 0.060 INCH IN LENGTH, RUNNING O/B AS MARKED (BS 221 TO 221, WBL L470 TO L470). TEMPORARY REPAIR CARRIED OUT PER EO NR B747-5430-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE. 2L74 4F RTA20WE 20041214001142004121400114NM 2004 12 14 UPS04443269 120040924A5420 WEB BOEING747 747121 1384871NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE: C, ONE EACH FASTENER HOLE WAS CRACKED AT WEB AREA NAC STA 230 OF NR 1 PYLON. NR 1 PYLON NAC STA 230 AFT LOWER WEB I/B AREA WEB REPAIRED AS PER SRM 54-10-03 FIG 2 DETAIL 1. 2L74 4F A20WE 20041214001152004121400115NM 2004 12 14 UPS04443270 120040926A5310BAC1505100607 SHEAR TIE BOEING747 747121 1384871NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, FWD CARGO STA 840 S44L - S45L BILGE AREA SHEAR TIE CORROSION FOUND. NEW SHEAR TIE REPLACED & INSTALLED AT BS 840 STR 44L - 45L AS PER SRM 51-30-02, DUE TO BLEND OUT DEPTH 0.050 INCH, WIDTH 1 INCH & LENGTH 3 INCH OUT OF SRM 53-10-01 FIG 1 LIMITATION. 2L74 4F A20WE 20041214001162004121400116EA 2004 12 14 SWIA200414068 120041108A2731 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA ELEVATOR STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07412SW 7101 F/O'S ELEVATOR TRIM SWITCH IS STICKING. REMOVED AND REPLACED F/O'S PITCH TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECKS GOOD IAW MM 27-40-00. 2L72 4F RTA21EA 20041214001172004121400117EA 2004 12 14 SWIA200414069 120041108A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07403SW571 571 7028 INFLIGHT THE FLIGHT/GROUND SPOILERS FAULT AND THE INBOARD GROUND SPOILER FAULT MESSAGE CAME ON. REMOVED AND REPLACED NR 2 SECU PER CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041214001182004121400118CE 2004 12 14 DXTA200400434 120041029A3411 PITOT TUBE CESSNA750 750 2076810CE OBSTRUCTED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07953QS 7500153 ABORTED TAKEOFF AT LESS THAN 80 KTS DUE TO AMBER FADEC REV ADC R CAS MESSAGE. OPERATED AIRCRAFT & NOTED NO FAULTS FOR A OR B FADEC. ENTERED MAINT PAGE & CHECKED LOGGED FAULTS. ONE FAULT CODE OF 3106 LISTED, ADC SENSOR MISCOMPARE FOR 30 OCT 04. ACCOMPLISHED TASK 73-50-00-810-835 OF AE3007C PROCEDURE TO IDENTIFY P2.5 SENSOR DRIFT. BOTH P2.5 SENSORS CHECKED GOOD. INSPECTED PITOT TUBES & FOUND RT DRAIN HOLES PLUGGED, CLEARED OBSTRUCTION & WATER DRAINED FROM PITOT LINE. CYCLED PITOT/STATIC HEAT & DRIED TUBES COMPLETELY. OPERATED SYSTEM & AIRCRAFT IAW 750 MM CHAPTER 71-00-04. 2L72 4J RTT00007WI 20041214001202004121400120NM 2004 12 14 AALA20041113 120041011A5315141T5113 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21382AN 25451 AFW - UPPER SURFACE OF FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDS AT RBL 17, 22, 22.5, 26.5, 31, 35.5, 37.5, 40, 41.5, AND 47. THE CRITICAL BLEND IS AT RBL 17. IT IS 0.8 INCH DIAMETER WITH .048 INCH REMAINING FROM A THICKNESS OF .085 INCH. FABRICATED REPAIR STRAP OUT OF 301 1/2H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS5 95 SEALANT. FASTENERS TO BE INSTALLED WITH 4 6D SPACING. 2L72 4F RTA1NM 20041214001242004121400124EU 2004 12 14 MALA040648 120041006A21211250608 MOTOR SAAB SF340 340B 7860101EU FAN FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15423XJ 340B423 SUPP AC MOTOR SPARKING AND GIVING OFF A BURNING SMELL. INSPECTED AIRFRAME ENGINES AND SYSTEMS DETERMINED TO BE LIMITED TO SUPP AC SYS, VERIFIED. REMOVED CENTER FLOOR PANEL AND VISUALLY CONFIRMED ARCING INTERNALLY OF SUPP AC COMPRESSOR MOTOR REINSTALLED PANEL. FOUND IMPELLAR FOR SUPP AC MOTOR BLADES BROKEN OFF, USED TO HEAT FROM MOTOR. REMOVED AND REPLACED P/N 1250608 IAW CMM ARR 13RR MANUAL MOTOR IS DESIGNED TO SPARK INSIDE. REMOVED FROM DMR MXC NOTIFIED 8328 2L72 4T RTA52EU 20041214001262004121400126SO 2004 12 14 RAIA00411028 120041126A3397 CONNECTOR EMB 145 EMB145 3260210SO EMERGENCY LIGHT UNSECURE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03803HK 145077 PIT - EMERGENCY LIGHT INOP. MAINTENANCE RE-SECURED CONNECTOR ON EMERGENCY LIGHT. 2L72 4F RTT00011AT 20041214001272004121400127EU 2004 12 14 MALA040651 120041020A5347 GALLEY TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 DURING 4Y/2Y INSPECTION IN BNA, NOTED GALLEY FLOOR TRACK CORRODED. MAINTENANCE REPLACED TRACK. 2L72 4T RTA52EU 20041214001282004121400128WP 2004 12 14 UPS04843448 120041010A5712 RIB DOUG DC8 DC871F 302199DWP XFS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE TWO LOWER RIBS CRACKED AT XFS 622.500 AND XSF 616.250. INSTALLED REPAIR DOUBLERS ON TWO RIBS AT XFS 622.500 AND XSF 616.250 IAW SRM 57-3-2 FIG 6 SHEET 2. 2L74 4F RT4A25 20041214001302004121400130NM 2004 12 14 UPS04M43285 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 27 LT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION AT BARREL NUT HOLE NR 27 LT REMOVED, BLENDED & REAMED TO 1.162 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 27 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 27 LT PER EO MD11-5510-19409-H & EN 1251-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041214001342004121400134NM 2004 12 14 SWAA043425 120041123A57536546434 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20041214001362004121400136 2004 12 14 DXTA200400439 420041105A3414 INDICATOR CESSNA650 650 2076802CE AIRSPEED INOPERATIVE E DXTAC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 GL07797QS 6507097 RT AIRSPEED INDICATOR DID NOT OPERATE DURING TAKEOFF ROLL. INSPECTED LINES FOR CO-PILOTS PITOT SYSTEM & PERFORMED OPERATIONAL CHECK OF AIRSPEED SYSTEM SATISFACTORY IAW CE 650 MM 34-11-03. 2L72 4F A9NM 20041214001382004121400138NM 2004 12 14 SWAA043426 120041123A57536546435 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM. 2L72 4F RTA16WE 20041214001392004121400139NM 2004 12 14 SWAA043427 120041123A552365C26384 TAB BOEING737 7373H4 1384600NM RT ELEVATOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD HINGE CUTOUT. REMOVED AND REPLACED ELEV TAB PER MM. 2L72 4F RTA16WE 20041214001402004121400140WP 2004 12 14 UPS04843456 120041011A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE: C3, RIGHT CENTER L/E RIB (LOWER) CRACKED AT XFS 335. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-3-0 AND 51-1-20D. 2L74 4F RT4A25 20041214001412004121400141WP 2004 12 14 UPS04843219 120040929A29137802885502 PUMP DOUG DC8 DC873F 302199FWP HYD SYSTEM LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01880UP 46080 NR 3 ENGINE HYDRAULIC LEAK. TROUBLESHOT & FOUND PT LEAKING IN NR 3 ENG PYLON & LEAKING INTO DRAIN LINES, TO DRAIN MAST. REMOVED AND REPLACED PART. OPS CK'D GOOD, LEAK CK'D GOOD, PERFORMED ENG RUN, & HYD SYS OP'S OF FLIGHT CONTROLS. SVC'D HYD RES PER MM 12-00-00. 2L74 4F RT4A25 20041214001432004121400143WP 2004 12 14 UPS04843224 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 WING LT LEADING EDGE AT STA 735 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20041214001482004121400148EU 2004 12 14 222041 120040806A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A NSVAK NONE O OTHER ININSP/MAINT 1 EA27350CJ 350 AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY IAW MM 33-50-10, OP CHECKED GOOD. 2L72 4T RTA52EU 20041214001502004121400150NE 2004 12 14 AALA20041100 220041106A7510 DUCT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE RT RNGINE RUPTURED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21488AA 49681 DFW - DURING CLIMBOUT FIRE DETECTION LOOP -A- LIGHT ILLUMINATED THEN -B- ILLUMINATED. RETARDED THROTTLE AND LIGHTS EXTINGUISHED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE ANTI-ICE DUCT. LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20041214001512004121400151CE 2004 12 14 DXTA200400421 120041008A21305060001 SOLENOID CESSNA750 750 2076810CE ISOLATION VALVE FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07939QS2302 7500193 DURING INITIAL DESCENT WITH POWER REDUCTION, THE CABIN BEGAN TO CLIMB AT A RATE OF APPROX 2000 FPM. THE CABIN CONTINUED TO CLIMB AND CONTINUED TO DESCEND, THE CABIN ALT RED CAS ILLUMINATES, INITIATED EMERGENCY DESCENT FOR LOWER ALTITUDE. TROUBLESHOOT TO FAULTY ISOLATION VALVE SOLENOID. REMOVED AND REPLACED ISOLATION VALVE SOLENOID. PRESSURIZATION SYSTEM OPS CHECKED GOOD, ALL WORK DONE IAW CE750 MM CHAPTER 21-30-00 AND, 21-32-00. 2L72 4J RTT00007WI 20041214001572004121400157WP 2004 12 14 UPS04843401 120041024A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM 25-60. 2L74 4F RT4A25 20041214001582004121400158EU 2004 12 14 UPS04142785 120040727A2150 ODOR AIRBUS300 A300B4622R 3930312EU NR 2 A/C PACK DETECTED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01152UP 0834 VERY BAD SMELL IN COCKPIT FROM T/O THROUGH 20,000 FT & THEN AGAIN ON DESCENT THROUGH 20,000 FT. SUSPECT NR 2 PACK. OPERATED BOTH PACKS TOGETHER & INDIVIDUALLY FOR SEVERAL MINUTES & NO SMELL DETECTED AT THIS TIME. OKAY FOR SERVICE. 2L72 4F RTA35EU 20041214001602004121400160NM 2004 12 14 UPS04442781 120040706A532065B280813 ANGLE BOEING747 747200 1384847NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, NLG W/W LT UPPER CORNER AREA SUSPECT CRACKED AS MARKED AT STA 280. LT UPPER CORNER ANGLE REPLACED AS PER SB 747-53-2293. 2L74 4F RTA20WE 20041214001612004121400161NM 2004 12 14 UPS04442782 120040706A532065B280814 ANGLE BOEING747 747200 1384847NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, NLG W/W RIGHT UPPER CORNER AREA SUSPECT CRACKED MARKED AT STA 314. RIGHT UPPER CORNER ANGLE REPLACED AS PER SB 747-53-2293. 2L74 4F RTA20WE 20041214001622004121400162NM 2004 12 14 UPS04442783 120040712A531165B01716505 FRAME BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, M/D- BS 460 LT FRAME WEB & WEB STIFFENER FOUND CRACKED AS MARKED BETWEEN STR 13A & STR 14. FRAME REPAIRED AS PER SRM 51-30-02. 2L74 4F RTA20WE 20041214001632004121400163NM 2004 12 14 UPS04442784 120040713A5310BACB30NX8K11 SHEAR TIE BOEING747 747200 1384847NM BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, AFT CARGO COMPT - BS 1480 LT PRESSURE BULKHEAD LOWER CHORD ATTACH SHEAR TIE FOUND CRACKED AT STR 35L TO STR 36L. AFT CARGO COMPT BS 1480 LT BULKHEAD LOWER CHORD ATTACH SHEAR TIE AT S35L TO S36L AREA REPLACED AS PER SRM 51-10-01. 2L74 4F RTA20WE 20041214001642004121400164NM 2004 12 14 UPS04542779 120040717A5347 SEAT TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01412UP 23852 INSPECTION TYPE: C, CORROSION MAIN CARGO FLOOR TRACK, BS 440.5, RBL 46.5 WL 208. REPLACED SEAT TRACK PER SRM ADDENDUM B757-5340-20264A, ER04-3449 AND SRM 53-00-52. 2L72 4F RTA2NM 20041214001662004121400166NM 2004 12 14 UPS04442753 120040712A5320 FLOOR SUPPORT BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C U/D - BS 420 - 440 BL 0 LONGITUDINAL FLOOR SUPPORT LWR FACE FOUND CORRODED AROUND SCREW. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F RTA20WE 20041214001672004121400167NM 2004 12 14 UPS04442754 120040713A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, U/D - BS 420 - 440 LBL 43 SEAT TRACK CROWN AND LIP FOUND CORROSION. SEAT TRACK REPLACED AS PER SRM 51-10-01 PAGE 8. 2L74 4F RTA20WE 20041214001722004121400172NM 2004 12 14 UPS04442806 120040710A534065B0424699 FITTING BOEING747 747200 1384847NM STRINGER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, M/D- STRINGER END FITTING (TRIANGULAR SHAPE) FOUND CRACK AT BS 854 STR 25R. STRINGER END FITTING REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F RTA20WE 20041214001732004121400173WP 2004 12 14 UPS04843229 120040909A571257696001 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, WING LT LEADING EDGE AT STA XFS 672.500 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20041214001742004121400174NE 2004 12 14 UPS04542786 220040727A7200 TAILPIPE BOEING757 75724APF 1384969NM PWA 2037 PW2040 NE LT ENGINE FIRE A IPXAK NONE A FLAME/FIRE TXTAXI/GRND HDL 1 SO01405UP 23727 726691 DURING LT ENG START MX EXPERIENCED TAIL PIPE FIRE. REPLACED NR 1 FUEL CONTROL PER AMM 73-21-01. REPAIRED OUTBOARD FLAP TRACK FAIRING PER SRM 51-70-05. REPLACED NR 5 SPOILER, WIRE BUNDLES W3315 & W3319. REPAIRED AND REPLACED LT WING T/E PANELS, FLAPS, FLAP FAIRINGS, NR 1 ENG STRUT PANELS, MLG STRUT DOOR & MLG FAIRINGS. 2L72 4F4 FRTA2NM E17NE 20041214001752004121400175WP 2004 12 14 UPS04843305 120040913A5311 FRAME DOUG DC8 DC871F 302199DWP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE: C3, FS 1360 FRAME LWR FLANGE AT LONGERON 36 HAS EXFOLIATION CORROSION. REMOVED CORROSION & FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED TWO REPAIR ANGLES & INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20041214001762004121400176NM 2004 12 14 DHL2004755504 120041018A5753 SKIN BOEING727 727225 1384077NM LT WING FLAP CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING C-CHECK, LEFT I/B MID FLAP UPPER SURF WBL 124 HAS CORR BULGES AT SKIN BUTT JOINT, MARKED. CUT OUT CORROSION DAMAGED SECTION OF LEFT I/B MID FLAP UPPER SURFACE SKIN AT BUTT JOINT STA 124 SIZE 7.75 X 1.875 INCH IAW B727 SRM 51-10-1. REMOVED & REPLACED UPPER RIB CHORD AT STA 124 DUE TO CORROSION BEYOND LIMITS MATERIAL LOSS .031 IAW B727 SRM 57-50-1 FIG 3. FABRICATED REPAIR DOUBLER 13.5 X 5 INCH 2024-T3.071 PO 9001424 & FILLER FROM 2024T3.063 PO 9912380, 8 X 2 INCH IAW B727 SRM 57-50-4. ALODINED & PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 57-50-4 PO 4318177 P/N 69-20772-2. 2L73 4F A3WE 20041214001772004121400177CE 2004 12 14 DXTA200400330 120040705A2910 MANIFOLD CESSNA750 750 2076810CE HYD SYSTEM FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL07953QS 7500153 GEAR PARTIALLY DEPLOYED UNCOMMANDED DURING DESCENT AT 14,000 FT, GEAR UNLOCK LIGHT CAME ON, AIRCRAFT LANDED SAFELY AT FLL. REMOVED AND REPLACED LANDING GEAR CONTROL HYDRAULIC MANIFOLD, BLED ALL HYDRAULICS AND LEAK CHECKED MANIFOLD, LEAK CHECKED GOOD. SERVICED RESERVOIRS IAW MM CHAPTER 12-10-15, ALL WORK DONE IN ACCORDANCE WITH CESSNA 750 MM CHAPTER 32-30-02. GEAR OPS CHECK GOOD IAW CESSNA 750 MM CHAPTER 32-00-01. 2L72 4J RTT00007WI 20041214001792004121400179WP 2004 12 14 UPS04842788 120040729A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:N/A, NR 3 PIT DOOR CUTOUT AT LWR AFT CORNER HAS CRACK AT DOUBLER. REMOVED CRACKED FITTING & ATTACHING FITTINGS. DRILLED UP NEW FITTINGS, OK TO INSTALL. INSTALLED 80 PERCENT OF FASTENERS IN NEW FITTING. COMPLETED NEW INSTALLATION OF NEW FITTING & ATTACHING FITTINGS PER SRM 51-1-20D. 2L74 4F RT4A25 20041214001812004121400181NE 2004 12 14 DHL2004783016 220041209A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 1 FLAMED OUT A DHLAD RETURN TO BLOCK XJ ENGINE FLAMEOUT WARNING INDICATION TXTAXI/GRND HDL 1 SO01783DH 21999 ENGINE NUMBER 1 FLAMED-OUT AFTER START, ATTEMPTED SECOND START, NO LIGHT OFF, ON SECOND START. ACCOMPLISHED NO LIGHT OFF ABNORMAL PROCEDURE. REMOVED CONNECTOR, CLEANED CONNECTION FOR FUNCTIONAL CHECK OF VALVE, ALL INDICATION NORMAL IAW 28-22-01. ENGINE RUN PERFORMED FOR TWO MINUTES ALL INDICATIONS NORMAL. OK FOR CONTINUED SERVICE AT THIS TIME. 2L73 4F4 F A3WE E2EA 20041214001822004121400182NM 2004 12 14 SWAA043537 120041205A53136561777 STRINGER BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR FRAME STRINGER AT BS 360, STRINGER 14L, CRACKED. REMOVED AND REPLACED STRINGER PER SRM. 2L72 4F RTA16WE 20041214001842004121400184NM 2004 12 14 UPS04242705 120040618A5754 SKIN BOEING727 72725C 138400HNM NR 3 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, NR 3 LEADING EDGE FLAP ANTI ICE SKIN IS CRACKED IN TWO AREAS, ALSO LOOSE RIVETS IN ANTI ICE SKIN. REPAIRED CRACKS IAW EO B727-5750-3082. REPLACED LOOSE RIVETS IAW SRM 51-30-2. 2L73 4F A3WE 20041214001872004121400187NM 2004 12 14 UPS04242714 120040616A3270 YOKE BOEING727 72725C 138400HNM TAIL SKID CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C TAIL SKID UNIT FOUND CRACKED. TAIL SKID YOKE ASSY REPLACED IAW MM 32-71-41 & 31-71-22 FUNCTION CHECK. 2L73 4F A3WE 20041214001882004121400188NM 2004 12 14 UPS04242715 120040617A5755 SKIN BOEING727 72725C 138400HNM NR 2 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, NR 2 SPOILER HAS DELAMINATION ON UPPER & LWR SURFACES. REPAIRED IAW SRM 51-40-5. 2L73 4F A3WE 20041214001892004121400189NM 2004 12 14 UPS04242717 120040618A5330 SKIN BOEING727 72725C 138400HNM BS - BS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE: C, SUSPECT CORROSION AT BS 640-680 S1L TO S4L. ON INVESTIGATION CORROSION FOUND INTERNALLY ON SKIN PANEL AT BS 680 - 660 S4R, BS 620 S2L - 1L, BS 540 - 530 S2L REPAIR CARRIED OUT IAW SRM 51-30-2, 33-30-01 DRAWING 65-42370, AAAE EO 2004-61-006, UPS ENGINEERING FILE B727-5330-20718-A. 2L73 4F A3WE 20041214001922004121400192WP 2004 12 14 UPS04842718 120040713A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01718UP 46018 INSPECTION TYPE:N/A, COCKPIT AND ENTRY EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED GOOD PER MM 33-50-01-2. 2L74 4F RT4A25 20041214001932004121400193NM 2004 12 14 SWAA043550 120041206A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 360, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041214001942004121400194CE 2004 12 14 DXTA200400331 120040706A7603 ENGINE CESSNA560 560XL 2076702CE RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL07652QS 5605152 WITH POWER AT TAKEOFF THRUST AIRCRAFT YAWS SHARPLY LEFT, POWER ON BOTH ENGINES MATCHED. RAN AIRCRAFT TO TAKEOFF POWER, TAXI CHECKED BRAKES, TOP CHECKED RUDDER BIAS, COULD NOT DUPLICATE. FOUND RIGHT ENG ACCELERATING FASTER AND HIGHER THRUST THAN LEFT, COULD NOT DUPLICATE PROBLEM, SYSTEM OPS CHECKED SATISFACTORY. 2L72 4F RTA22CE 20041214001962004121400196CE 2004 12 14 DXTA200400333 120040706A3240 BRAKE RAYTHNDH125 HAWKER800XP 7150012CE MLG STICKING E DXTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL07875QS 258375 DURING TAXIING, NOTICED BRAKES WERE STICKING AND FADING, ALSO FELT LIKE BRAKES WERE OUT OF SYNC. GAINED ACCESS TO THE BRAKE CONTROL VALVE, BLED ALL FOUR MASTER CYLINDERS, TOP OFF ALL BRAKE MASTER CYLINDER UNITS. TAXIED AIRCRAFT AND CHECKED BRAKES FOR STICKING AND FADING, OPS CHECKED GOOD. ALL WORK DONE IAW HAWKER 800XP MM CHAPTER 32-40-00. 2L72 4F RTA3EU 20041214001992004121400199NM 2004 12 14 SWAA043576 120041207A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND 2 EACH CRACKS ON FRAME AT BS 616, BELOW STRINGERS 17R AND 17L. REPAIRED FRAME SECTIONS PER T1-153-018. 2L72 4F RTA16WE 20041214002002004121400200NM 2004 12 14 UPS04M42711 120040426A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C, MAIN DECK CABIN ALONG STA 1239, APPROX 7 INCHES LBL SEAT TRACK FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 REV 34 MAT'L THK 0.100 INCH THK REMOVED 0.023 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 VOL 1 REV 34. CORROSION SEAT TRACK CUT OUT AT STA 1229-1313 LBL 7 PER SRM 53-70-00 VOL 1. NEW SEAT TRACK SPLICE & SPLICE PLATE FABRICATED & INSTALLED PER SRM 53-70-0 0 VOL 1 REV 34. 2L73 4F RTA22WE 20041214002012004121400201WP 2004 12 14 ARWA20041101 120041105A2913 O-RING DOUG DC8 DC863 302198AWP HYD PUMP DAMAGED A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19345JW 46042 LOSS OF HYDRAULIC PRESSURE EN ROUTE HYDRAULIC QUANTITY NORMAL. FOUND O-RING DAMAGED AT NR 3 ENGINE HYDRAULIC DRIVEN PUMP PRESSURE PORT. REMOVED AND REPLACED O-RING AS REQUIRED IN ACCORDANCE WITH DC-8 M/M 22-60-0. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 29-10-12; NO LEAKS FOUND. 2L74 4F 4A25 20041214002022004121400202NM 2004 12 14 SWAA043265 120041108A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 991, BETWEEN LBL 37 AND LBL 41, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041214002032004121400203NM 2004 12 14 0401645811 120040922A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01591NW4457 32991 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041214002042004121400204NM 2004 12 14 0401665802 120040922A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01585NW6053 32985 THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041214002062004121400206NM 2004 12 14 UPS04M43430 120041031A2560 SEAL DOUG MD11 MD11F 3023600NM SMOKE DOOR TORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01251UP 48744 SEAL TORN IN HALF ON SMOKE DOOR UPPER DECK. REMOVED AND REPLACED TORN SEAL. FIT & FUNCTION CHECKED OK. 2L73 4F RTA22WE 20041214002072004121400207NM 2004 12 14 UPS04243134 120040920A33501000677 LIGHT BOEING727 727185C 138406NNM CREW ENTRY INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE:N/A, CREW ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM 33-50-67, OPS CHECK GOOD. 2L73 4F A3WE 20041215000012004121500001 2004 12 15 SWIA200414236 420041202A341835A573 STICK SHAKER CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 NM07923SW5905 5905 DURING STALL WARNING TEST, NO STICK SHAKER WARNING ON EITHER SIDE. REPLACED PILOTS CAPT'S SIDE SHAKER FOR YOKE, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041215000022004121500002EU 2004 12 15 AWXA200401372 120041114A5320D53475265200 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK, EXFOLIATION CORROSION WAS FOUND ON BULK CARGO DOOR SILL AT -Y1500, BETWEEN FS 60 AND FS 62. MAINTENANCE CUTOUT ALL CORRODED AREAS OF BULK CARGO DOOR SILL AT -Y1500, BETWEEN FS 60 AND FS 62; FABRICATED 5 EACH FILLERS AND DOUBLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-49. 2L72 4F RTA28NM 20041215000052004121500005WP 2004 12 15 COOSDR040021 120040823A5520 FITTING DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE HORIZONTAL STAB CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 LT HORIZONTAL STABILIZER ELEVATOR HINGE STA XE 140 SUPPORT HOLE CORRODED. 2L74 4F4 F 4A25 1E8 20041215000082004121500008NM 2004 12 15 COOSDR040036 120040816A5310 BEAM BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU MAIN CABIN CRACKED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23360UA 24453 MAIN CARGO, BS 685, LBL 45.5, WL 203.1, STUD BEAM CRACKED. 2L72 4F4 FRTA16WE E21EU 20041215000092004121500009NM 2004 12 15 COOSDR040024 120040817A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN BS 720A FLOORBEAM UPPER CHORD CORRODED. 2L73 4F4 FRTA3WE E2EA 20041215000102004121500010NM 2004 12 15 COOSDR040027 120040817A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE MAIN CABIN CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN, BS 1130 FLOORBEAM UPPER AND LOWER CHORD, CORRODED. 2L73 4F4 FRTA3WE E2EA 20041215000112004121500011 2004 12 15 FE62004F00000 420040727A3422 SOFTWARE AMD FALC50FALCON50MYST2730106EU GARRTTTFE731TFE731* 01518WP TAWS/RMI MALFUNCTIONED B FE6RO OTHER O OTHER NRNOT REPORTED 1 NM112FQ 1035 167 THE SANDEL TAWS/RMI SHOWS SIGNIFICANT BEARING ERRORS ON HEADINGS GREATER THAT 359 DEGREES OR LESS THAN 0 DEGREES. THIS PROBLEM WAS DISCOVERED IN FLIGHT AND VALIDATED THROUGH GROUND TEST OF NUMEROUS UNITS. PROBABLE CAUSE OF MALFUNCTION IS THE SOFTWARE. THE ST34 TAWS/RMI IS NOT RECOMMENDED FOR NAVIGATION AT THIS TIME. 2L73 4F4 F A46EU E6WE 20041215000132004121500013NM 2004 12 15 USAA040734 120041013A5320 ANGLE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19601AU 22193 TRANSITION ANGLE, 3 INCH SQUARE AREA, CORRODED STA 1380 TO 1440 ABOVE STRINGER 27R. REPLACED WITH IDENTICAL PART IAW SRM 51-10-02. 2L72 4F4 FRTA2NM E12EU 20041215000152004121500015NM 2004 12 15 USAA040757 120041018A5320 FLOOR SUPPORT BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 SUPPORT, 2 INCH BY 1 INCH, CORROSION, BL0 BETWEEN STATIONS 1661 AND 1681. REPLACED FLOOR SUPPORT IAW SRM 51-10-02. 2L72 4F4 FRTA2NM E12EU 20041215000162004121500016NM 2004 12 15 USAA040760 120041019A5320 CHANNEL BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU 27144 CLT, C-4, CHANNEL, 1 INCH AREA, LEVEL 2 CORROSION, BETWEEN STA 395, STA 377, BL0. REPLACED WITH IDENTICAL PART IWA SRM 51-10-02 AND SRM 51-40-02. 2L72 4F4 FRTA2NM E12EU 20041215000182004121500018NM 2004 12 15 USAA040765 120041017A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 FLOORBEAM, .5 INCH AREA, CORROSION LEVEL 2, STA 345, RBL 62. ACCOMPLISHED (T) CAP REPAIR IAW EA95913. 2L72 4F4 FRTA2NM E12EU 20041215000192004121500019NM 2004 12 15 USAA040768 120041026A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU63825 22193 CLT, C-3, STRINGER, 20 INCHES AREA, CORROSION, BETWEEN STA 1640, STA 1660, STR 29L. REPLACED STRINGER SECTION IAW EAS 95876, 95868. 2L72 4F4 FRTA2NM E12EU 20041215000202004121500020NM 2004 12 15 USAA040769 120041026A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 FLOORBEAM, 6 INCHES BY 2 INCHES, CORROSION LEVEL 2, STA 310, RBL 42. REPAIRED FLOORBEAM SECTION IAW EA 95898. 2L72 4F4 FRTA2NM E12EU 20041215000212004121500021NM 2004 12 15 USAA040771 120041026A5420 WEB BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE PYLON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 CLT, C-4, PYLON WEB, .310 INCH HOLE, PP STATION, 128 TOP WEB. INSTALLED DOUBLER IAW EA 95897. 2L72 4F4 FRTA2NM E12EU 20041210000732004121000073NM 2004 12 10 SWAA043578 120041207A53306545774 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 751, BELOW STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041210000742004121000074EU 2004 12 10 RAIA00412006 120041207A7930 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU OIL PRESSURE ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03552HK 41057 BNA - RIGHT OIL PRESSURE CAP LIGHT. MAINTENANCE DEFERRED AS PER MEL 79-4. 2L72 4T RTA41NM 20041210000762004121000076EA 2004 12 10 SWIA200414194 120041118A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 CARGO PIT FLOOR SUPPORT LBL 27.0 CRACKED AT 3 LOCATIONS INBOARD SIDE BETWEEN FS 574.0 TO 621.0, INBOARD WEB BUCKLED BETWEEN FS 574.0 TO FS 589.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-42-06, 51-42-10, 51-42-21. 2L72 4F RTA21EA 20041210000772004121000077SO 2004 12 10 SWIA200414208 120041101A5310 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 BUTT STRAP FROM FRAME 30-34 CENTER IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTT STRAP REPLACED IAW EMB 120 SRM 51-25-00, 51-40-00 2L72 4T RTA31SO 20041210000782004121000078SO 2004 12 10 SWIA200414215 120041101A5310 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 RIGHT BUTT STRAP AT Y479.00R FROM FRAME 21 TO FRAME 26 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION IAW EMB 120 SRM 53-20-10, FOUND TO BE WITHIN LIMITS. DEPTH .004. REPROTECTED IAW SRM 51-21-02 AND AMM 20-30-05. 2L72 4T RTA31SO 20041210000792004121000079SO 2004 12 10 SWIA200414222 120041101A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 FR38 - FR40 AT YR 479 OMEGA BEAM IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW EMB EO IC2004-120/5465. 2L72 4T RTA31SO 20041210000802004121000080NM 2004 12 10 DHL2004750045 120041209A3210 LANDING GEAR BOEING727 7272M7 138407SNM RIGHT COLLAPSED A DHLAO OTHER O OTHER LDLANDING 1 SO01750DH 21951 RIGHT MAIN LANDING GEAR DAMAGED AND WING DAMAGED DUE TO INCIDENT, AFTER TOUCHDOWN THE RIGHT HAND MAIN LANDING GEAR COLLAPSED. REPAIRED RT MLG & WING DAMAGE IAW JC NR000000001 WO 600012457 2L73 4F A3WE 20041210000822004121000082NM 2004 12 10 WLDA200498 120041107A5343 FITTING DOUG MD11 MD11 3023602NM MLG CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 DURING C2 CHECK FOUND CORROSION IN CENTER LANDING GEAR FITTING. CLEANED UP CORROSION BY MACHINING FAYING SURFACE, ENLARGED HOLE DIAMETER OF TURNION FITTING AND INSTALLED BUSHING. THE DIMENSIONS OF REWORK AREA ARE WITHIN LIMITS PER SRM 53-40-00 VOL 1 FIG 15. 2L73 4F RTA22WE 20041213000042004121300004NM 2004 12 13 SWAA043587 120041209A555218A80101 BOLT BOEING737 7373H4 1384600NM ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED C1 CHECK, LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT AND LT INBOARD NR 1 TAB BOLTS PER MM. 2L72 4F RTA16WE 20041213000052004121300005EA 2004 12 13 04328646 120041123A2760 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA SPOILERS FALSE ACTIVATIONA VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27646BR 7392 SPOILERON AND GROUND SPOILER FAULT CAUTION MESSAGE. ABORTED TAKEOFF. MX INTERROGATED SECU WITH NO FAULTS NOTED. RESET C/B. 2L72 4F RTA21EA 20041213000192004121300019WP 2004 12 13 AALA20041203 120041207A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21559AA 53089 LGA - FORWARD OVERWING EMERGENCY EXIT SIGN ON BOTH SIDES INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR FORWARD OVERWING EMERGENCY EXIT SIGN ON BOTH SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000202004121300020NM 2004 12 13 AALA20041204 120041207A3350 SOCKET BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21641AA 24599 DFW - DOOR FOUR LEFT EMERGENCY SLIDE LIGHT AT L56 INOPERATIVE. REPLACED THE SOCKET ASSEMBLY FOR THE L56 EMERGENCY SLIDE LIGHT AT DOOR FOUR LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041213000372004121300037WP 2004 12 13 AALA20041188 120041130A3397 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2170524 49916 DFW - EMERGENCY EXIT LIGHT ON FORWARD GALLEY AISLE INOPERATIVE. REPLACED THE QUICK DISCONNECT ON THE LIGHT ASSEMBLY WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041213000452004121300045 2004 12 13 WLDA200497 420041107A31604059011911 DISPLAY DOUG MD11 MD11F 3023600NM NR 1 DEU INOPERATIVE A WRLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11276 48632 LAX/ANC AIR TURNBACK DUE TO NR 1 DEU FAILED. DISPLAY UNITS WENT BLANK, SWITCHED TO AUX, RECOVERED DU'S. RESET C/B'S, SWITCHED BACK TO NORMAL, LOST DEU'S AGAIN. REMOVED AND REPLACED NR 1 DEU IAW MM 31-61-1, CHECKED EIS SOURCE SELECT AND OPS CHECKED ALL NORMAL. 2L73 4F RTA22WE 20041213000502004121300050WP 2004 12 13 0402119921 120041128A2130 CHECK VALVE DOUG DC9 DC932 3022066WP GROUND HEAT STICKING A NWAAB EMER. DESCENT S AFFECT SYSTEMS CLCLIMB 1 GL01943N 47647 AFTER DEPARTURE, THE CABIN BEGAN CLIMBING UNCONTROLLABLY. AT FL130, THE RED CABIN PRESSURE WARNING LIGHT ILLUMINATED WITH THE CABIN AT ABOUT 9,500 FT. FLIGHT CREW REQUESTED AN EMERGENCY LEVEL OFF AT FL140 AND THEN A DESCENT TO FL120 (THE MINIMUM ALTITUDE ALLOWED FOR TERRAIN CLEARANCE). THE RED BORDERED CHECKLIST WAS COMPLIED WITH BUT DID NOT HELP. OUTFLOW VALVE WAS INDICATING FULLY CLOSED. FLIGHT CONTINUED TO AN UNEVENTFUL LANDING AT GTF. MAINTENANCE COULD NOT DUPLICATE THE FAULT AND SUSPECTED THAT THE GROUND HEAT CART CONNECTION CHECK VALVE HAS BEEN STUCK OPEN. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041213000522004121300052 2004 12 13 04327685 420041122A3414607300001 TRANSDUCER CNDAIRCL600 CL6002B19 1900309EA NR 1 MACH INTERMITTENT A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27685BR 7712 ADC1 FAIL, MACH TRIM DISENGAGE INTERMITTENT ON CLIMBOUT. MX REMOVED & REPLACED NR 1 MACH TRANSDUCER. PERFORMED PITOT/STATIC CHECK. 2L72 4F RTA21EA 20041213000702004121300070NM 2004 12 13 AALA20041184 120041130A335060030451 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21185AN 32379 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041213000782004121300078NM 2004 12 13 SWAA043583 120041208A531165C2299 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500C, BETWEEN LBL 2 AND RBL 20, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041213000872004121300087WP 2004 12 13 0402079864 120041127A215020495055 ACM DOUG DC9 DC951 3022051WP LEFT SMOKE A NWAAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL01773NC 47775 DURING TAKEOFF ROLL, A STRONG ODOR AND VISIBLE SMOKE ENTERED THE FLIGHT DECK. SMOKE WAS ALSO REPORTED IN THE CAIBN COMING FROM THE GASPER VALVES. THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 120 KTS AND THE CREW PERFOMRED COM PROCEDURES FOR SMOKE REMOVAL PRIOR TO RETURNING TO THE GATE. MAINTENANCE REPLACED THE LEFT AIR CYCLE MACHINE, BOTH THE LEFT AND RIGHT COALESCER BAGS, AND THEN RAN THE ENGINE AT TAKEOFF POWER FOR FIVE MINUTES. NO SMOKE WAS GENERATED IN THE CABIN OR COCKPIT. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041213001122004121300112NM 2004 12 13 SWAA043575 120041207A53306545857 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT AFT SERVICE DOOR CUTOUT LOWER CORNER CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041213001182004121300118NM 2004 12 13 UPS04M43298 120040719A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 15 RIGHT BARREL NUT HOLE FOUND CORRODED ON SIDEWALL, BOTTOM AND BEARING SURFACE. CORROSION AT NR 15 RIGHT BARREL NUT HOLE REMOVED, BLENDED & REAMED TO 1.067 INCH FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 ON BLEND AREA AT BARREL NUT HOLE NR 15 RIGHT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 15 RIGHT PER EO MD11-5510-19409-H & EN 1249-04 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20041214000012004121400001EU 2004 12 14 MALA040759 120040926A5420 PAN BAC 146 AVRO146RJ85A1500097EU NR 1 NACELLE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, NR 1 ENGINE ZONE 2 COWL, INBOARD COWL DISHING PAN CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. REFER TO 409, 207841 & 207842 FOR FURTHER DETAIL. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000042004121400004NM 2004 12 14 DHL2004755511 120041021A5730 SKIN BOEING727 727225 1384077NM RT WING LE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, DENT RIGHT WING L/E WS 650. CUT OUT DAMAGED AREA SIZE 2 X 1 INCH ON RT WING L/E WS 650 IAW B727 SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 .063 SIZE 6 X 6 INCH PO 90024 IAW B727 SRM 57-30-4 FIG 1. TREATED, PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20041214000362004121400036EU 2004 12 14 MALA040749 120040926A5710 SHROUD BAC 146 AVRO146RJ85A1500097EU RT WING DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, RT O/B WING SHROUD TRAILING EDGE DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000422004121400042EU 2004 12 14 MALA040763 120040928A5321 FLOOR PANEL BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, AFT CARGO FLOOR PANEL 181 FL HAS CORROSION. MAINTENANCE MANUFACTURED NEW PANEL IAW SRM 51-42-00, 51-20-11, 51-31-00, 51-25-00. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000442004121400044EU 2004 12 14 MALA040771 120041206A2133 CONTROL SWITCH BAC 146 AVRO146RJ85A1500097EU OUTFLOW VALVE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15505XJ E2313 CREW STATED OUTFLOW VALVE WOULD NOT CLOSE. AIR RETURN TO MSP. MAINTENANCE FOUND OUTFLOW VALVE MODE SWITCH OUT OF DETENTS. REPOSITIONED SWITCH AS REQUIRED, PERFORMED CONTROLLER SELF TEST, ALL CHECKED GOOD. PERFORMED CONTROLLER FUNCTIONAL TEST AMM 21-30-00 501, ALL CHECKED GOOD. 2H74 4F RTA49EU 20041214000512004121400051NM 2004 12 14 CALA0400739 120041207A3233651781914 ACTUATOR BOEING737 7373T0 1384582NM NLG INOPERATIVE A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW2712327746 23457 THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS LOWERED ON APPROACH TO IAH. THE GEAR WAS CYCLED DURING A GO-AROUND AND THE GEAR EXTENDED NORMALLY WITH NORMAL INDICATIONS. MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-21. THE GEAR WAS CYCLED 10 TIMES AND ALL OPERATION CHECKED NORMAL. 2L72 4F RTA16WE 20041214000572004121400057EU 2004 12 14 MALA040773 120041205A3020NH24668165 DUCT SAAB SF340 340B 7860101EU LT NACELLE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15441XJ 340B441 AFTER TAKEOFF, THE LT INTAKE HEAT FAILED. AIR RETURN TO MSP. MAINTENANCE REPLACED LOWER INTAKE DUCT P/N OFF NH24668-169, S/N OFF L291010, P/N ON NH24668-165, S/N ON L155348, OPS CHECK GOOD IAW J/C 7160-301. 2L72 4T RTA52EU 20041214000592004121400059EU 2004 12 14 MALA040767 120040926A5321 FLOOR PANEL BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C-CHECK INSPECTION IN YYC, FLOOR PANEL 141DL DAMAGED. MAINTENANCE MANUFACTURED FLOOR PANEL IAW SRM 51-42-00, 51-32-00, 53-00-35 FIG 1. AIRCRAFT RELEASED 10/07/04. 2H74 4F RTA49EU 20041214000682004121400068NM 2004 12 14 DHL2004755508 120041020A5330 SKIN BOEING727 727225 1384077NM FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, FUSE BS 1108 STR 19 RT HAS SKIN CREASED AT STRINGER. CUT OUT DAMAGED SECTION OF SKIN AT STR 19R, STA 1108, DIMENSIONS ARE 3.25 X 2.375 INCH. FABRICATED REPAIR FILLER (DIMENSIONS ARE 3.25 X 1 INCH) FROM .050 2024-T3 PO 9001425, FABRICATED REPAIR DOUBLER (DIMENSIONS 12.5 X 8.3125 INCH) FROM .063 2024-T3 PO 9001387 IAW B727 SRM 53-30-3 FIG 3, TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 AND 51-30-2. 2L73 4F A3WE 20041214000722004121400072NM 2004 12 14 SWAA043399 120041119A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29635SW 27708 DURING SCHEDULED C4 CHECK, FOUND LT KEELBEAM WEB CRACKED BETWEEN BS 700 TO BS 710. REPAIRED KEELBEAM PER SRM. 2L72 4F RTA16WE 20041214000732004121400073NM 2004 12 14 AALA20041107 120041104A2121 FAN BOEING757 757223 1384957NM CABIN FAILED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21606AA 27057 MIA - INFLIGHT T922/04 AT ROW 12 SEAT-F SMOKE APPEARED TO COME FROM FLOOR VENT. ACRID BURNED WIRE ODOR ACCOMPANIED SMOKE. POWER PORT WAS NOT SOURCE OF SMOKE. TURNED OFF UTILITY BUSS AND RECIRCULATION FANS. SMOKE AND ODOR DISSIPATED. LANDED MIA WITHOUT INCIDENT. FOUND RIGHT RECIRCULATION FAN FAILURE. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041214000782004121400078EU 2004 12 14 MALA040669 120041101A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 DURING 6Y/4Y INSPECTION IN BNA, SEAT TRACK AT BL 0 IS CORRODED BETWEEN FS 294 AND 339. SEAT TRACK WAS REPLACED IN THIS AREA IAW MESABA EO S53060. A/C WAS RELEASED 11/07/04. 2L72 4T RTA52EU 20041214000992004121400099NM 2004 12 14 F3LA200400081 120040819A5312 BULKHEAD BOEING737 737317 138447PNM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03EICHH 1590 23177 DURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD ON O/B SIDE OF RBL 5.7 ABOVE WL 207. REMOVED DAMAGE, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED PER EA B3-53R-10470 AND SRM 53-10-08, FIG 210, DETAIL 3. 2L72 4F RTA16WE 20041214001032004121400103EU 2004 12 14 MALA040659 120041021A2121 BRUSHES SAAB SF340 340B 7860101EU FAN MOTOR FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15423XJ 340B423 SUPPLEMENTAL AC INOP. BURNING/SMOKE ODOR. MAINTENANCE REPLACED BELT & PULLEY. REMOVED FROM DMR, FOUND BELT SHROUD AND MOTOR IN BRUSH WORN. REMOVED AND REPLACED MOTOR, ALL THE ABOVE RAN, SUPP AC OPS CHECK GOOD. NO ODOR NOTED AT THIS TIME. S/N OFF 449, S/N ON 667, NOTIFIED MXC. 2L72 4T RTA52EU 20041214001112004121400111NM 2004 12 14 UPS04443235 120040927A5414 SKIN BOEING747 747200 1384847NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:AD, NR 3 PYLON UNDER THE PREVIOUS REPAIRED CAP SKIN, CRACKED I/B OF UPPER LINK ATTACHMENT LUG AREA AS RED MARKED, NSTA 221 TO 221, WBL R470-R470. SKIN CRACK ENG STOP HOLE DRILLED, NDT CONFIRM CRACK FREE AS PER CUSTOMER INFO NR 3 PYLON WAS PREVIOUSLY MODIFIED, NO FURTHER ACTION REQUIRED. 2L74 4F RTA20WE 20041214001122004121400112WP 2004 12 14 UPS04843247 120040918A53403779659U501 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 INSPECTION TYPE:C1, LONGERON 5R END FITTING CRACKED STA 850. REMOVED AND REPLACED FITTING IAW SRM 51-1-21-1-200. 2L74 4F RT4A25 20041214001212004121400121NM 2004 12 14 UPS04443438 120041029A5313 LONGERON BOEING747 747200 1384847NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, MAIN E/E COMPT LOWER FUSELAGE INTERIOR STRINGER FOUND CRACKED AT STA 440 TO STA 460 STR 37L. STA 440 TO STA 460 STR 37L REPAIRED AS PER SRM 53-10-03 FIG 3. 2L74 4F RTA20WE 20041214001252004121400125EU 2004 12 14 MALA040652 120041002A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON FRAME STA 258.0 FLANGE. REPAIRED PER SRM. 2L72 4T RTA52EU 20041214001462004121400146WP 2004 12 14 UPS04843228 120040908A57125769545506 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 CRACKED RIB AT APPROX STA XFS 728 RIGHT WING LEADING EDGE. REMOVED PREVIOUS REPAIR AND TRIMMED OUT CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. REINSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20041214001472004121400147NM 2004 12 14 MWEA040200 120041105A5313591143289 LONGERON DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 LONGERON TWO RIGHT IS CRACKED AT FRAME STATION 1418. FABRICATED AND INSTALLED LONGERON AND SPLICE. 2L72 4F RTA6WE 20041214001522004121400152CE 2004 12 14 DXTA200400422 120041011A28218975131 FILTER RAYTHNDH125 HAWKER800XP 7150012CE FUEL SYSTEM FAULTY E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07811QS 258614 ENGINE 1 FUEL LIGHT ILLUMINATED ON TAKEOFF AT 60KTS. REMOVED FILTER AND SHIPPED TO HONEYWELL FOR TEST. INSTALLED NEW FILTER, OPERATED ENGINE ON GROUND THROUGH VARIOUS POWER SETTINGS. LEAK CHECK AND OPERATIONS OK, REF 73-21-02. 2L72 4F RTA3EU 20041214001532004121400153CE 2004 12 14 DXTA200400423 120041011A323399144522 ACTUATOR CESSNA750 750 2076810CE NLG FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07983QS3659 7500083 UPON GEAR RETRACTION ALL GREEN LIGHTS OUT RED UNLOCK LIGHT ON. RECYCLED GEAR AND GOT THE SAME RESULT. A LOT OF AIR/WIND NOISE FROM NOSE OF PLANE, SOUNDED LIKE NOSE GEAR WAS EXTENDED. REMOVED & REPLACED NOSE GEAR ACTUATOR WITH RENTAL UNIT. SENT LINE NOSE GEAR BARREL ASSY TO CESSNA FOR REPAIR. REINSTALLED ORIGINAL REPAIRED UNIT. C/W CASTER ANGLE CK'S, GEAR SWINGS, LEAK CK'S, OPS CK'S & SPADE DOOR ADJUSTMENTS. ALL GEAR SYSTEMS OPS CK SATISFACTORY AT THIS TIME PER 750 M/M 32-20-02, 32-20-00, 32-30-03. 2L72 4J RTT00007WI 20041214001692004121400169NM 2004 12 14 UPS04442756 120040712A5320 FLOOR SUPPORT BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, U/D - BS 560 LBL 80 LONGITUDINAL FLOOR SUPPORT FOUND CORROSION. FLOOR SUPPORT REPAIRED PER SRM 51-40-04 FIG 2. 2L74 4F RTA20WE 20041214001702004121400170NM 2004 12 14 UPS04442791 120040710A5330 SKIN BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C M/D- BS 1140 - 1144 LBL 8-11, WING CENTER SECTION UPPER FACE FOUND CORROSION AS MARKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.094 X 4 X 4 INCH EXCEED SRM 57-30-01 LIMITS, WING CENTER SECTION SKIN BLENDING REPAIRED PER HXRS R57-14-35180 & UPS ENGINEERING FILE 747-57-20055. CIC APPLIED IAW EO M5100-2780-E. 2L74 4F RTA20WE 20041214001852004121400185NM 2004 12 14 UPS04242706 120040617A5542 SKIN BOEING727 72725C 138400HNM RUDDER WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 INSPECTION TYPE:C, SKIN ON LWR RUDDER L/E WORN IN SEVERAL PLACES ON LT & RT SIDES. LWR RUDDER REPLACED IAW MM 27-20-01, 27-20-11 & SRM 51-30-02. 2L73 4F A3WE 20041214001952004121400195CE 2004 12 14 DXTA200400332 120040706A2120 ODOR CESSNA750 750 2076810CE CABIN DETECTED E DXTAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07913QS 7500113 ALL WEMAC EMITTED A STRONG SULFUR SMELL INTERMITTENTLY IN DIFFERENT VALVE AND PAC POSITIONS, AS A RESULT CANNOT DETERMINE SOURCE. RAN ENGINES AND APU, USED BLEED AIR WITH NO ODOR FROM WEMACS. INSPECTED COALESCER SOCKS WITH NO DISCREPANCY OR ODORS NOTED. SYSTEM CHECKS GOOD IAW CESSNA 750 MM CHAPTER 21-21-00. 2L72 4J RTT00007WI 20041214001972004121400197CE 2004 12 14 DXTA200400342 120040717A291099146371 MANIFOLD CESSNA750 750 2076810CE HYD SYSTEM FAILED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07950QS1171 7500050 LANDING GEAR CYCLED IN FLIGHT AT FL 430 AND FL120 UNLOCK LIGHT ILLUMINATED THEN WENT OUT AFTER 1 MINUTE. TROUBLESHOT TO FAULTY LANDING GEAR HYDRAULIC MANIFOLD ASSEMBLY. REMOVED AND REPLACED HYDRAULIC MANIFOLD. BLED SYSTEM, OPS AND LEAK CHECKS GOOD, ALL WORK DONE IAW CESSNA750 MM CHAPTER 32-30-02. 2L72 4J RTT00007WI 20041215000072004121500007WP 2004 12 15 COOSDR040032 120040823A5315 FLOORBEAM DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE MAIN CABIN CRACKED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2341CX 46129 MAIN CARGO CABIN Y STA 360.0, FLOORBEAM UPPER CAP CRACKED AT +X 31.25. 2L74 4F4 F 4A25 1E8 20041215000142004121500014NM 2004 12 15 USAA040735 120041013A5340 STRINGER CLIP BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU63825 22193 STRINGER TIE CLIP, 2 INCH SQUARE, CORROSION, STA 1420 LOWER FLANGE OF FRAME ABOVE STR 28R. REPLACED WITH FABRICATED PARTS IAW SRM 51-10-02. 2L72 4F4 FRTA2NM E12EU 20041215000232004121500023EA 2004 12 15 A6WA200440182 120041108A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT IB FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31440AW 7766 RT IB FLAP BOTTOM SKIN IS DENTED APPROX .7500 INCH LONG X .6250 INCH WIDE AND .040 DEEP WITH GOUGES IN CENTER OF DENT. DENT IS 1.7500 INCH FORWARD OF AFT EDGE AND 8 INCH OB FROM IB ENGINE. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SKIN AND INSTALLING DOUBLER AND FILLER IAW REO 601R-57-52-058, REV A. 2L72 4F4 FRTA21EA E15NE 20041215000252004121500025EA 2004 12 15 A6WA200440187 120041117A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING TE STUCK A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31469AW 7917 FLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREES ON APPROACH. RESET FLAPS SYSTEM IAW SUPPLEMENT 98-18, NO FURTHER DISCREPANCIES. 2L72 4F4 FRTA21EA E15NE 20041215000262004121500026EA 2004 12 15 A6WA200440180 120041107A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31427ZW 7685 FUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. MAINTENANCE VERIFIED NO FUEL OR OIL LEAKS IN APU BAY. TROUBLESHOT APU FUEL SYSTEM. RAN APU AND AIR CYCLE MACHINE. NO FUEL SMELL DETECTED AND NO LEAKS. 2L72 4F4 FRTA21EA E15NE 20041215000272004121500027EA 2004 12 15 A6WA200440184 120041028A5320601R3895719 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SERVICE DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 SERVICE DOOR RAMP PLATE, PN 601R38957-19, CORRODED AROUND OPENINGS AND FASTENER HOLES. REPLACED RAMP PLATE WITH NEW RAMP PLATE IAW SRM 51-41-02. 2L72 4F4 FRTA21EA E15NE 20041215000282004121500028EA 2004 12 15 A6WA200440183 120041026A5740 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PUMP SUPPORT DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 LT BOOST PUMP CANISTER SATELLITE HOLE AFT SIDE LBL 11.18 FAILED EDDY CURRENT INSPECTION. INDICATION NOTED ON OB SIDE OF HOLE. REPAIRED SATELLITE HOLE BY REAMING THE HOLE TO .4150 AND INSTALLING A FREEZE PLUG. (OD EO 601R-57-21-526). 2L72 4F4 FRTA21EA E15NE 20041215000312004121500031EA 2004 12 15 A6WA200440179 120041107A3397787190 SPLICE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 FLOOR TRACK LIGHTING HAS A BROKEN SPLICE AT ROW NR 8. REMOVED AND REPLACED SPLICE AT ROW NR 8 IAW CRJ 200 WIRING MANUAL 20-17-10. 2L72 4F4 FRTA21EA E15NE 20041215000342004121500034EA 2004 12 15 ASOA04840 120041024A5320 BRACKET CL6002B19 CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 7579 DURING A C-CHECK, THE RT FS 484.00, RBL 36 AFT BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CRACKED BRACKET IAW EO 600-53-0194. 2L72 4F4 FRTA21EA E15NE 20041215000352004121500035EA 2004 12 15 ASOA04841 120041021A3350BR9279106 SIGN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING A C-CHECK, THE ENTRY WAY EMERGENCY EXIT LIGHT, JUST FORWARD OF THE PASSENGER DOOR, WAS FOUND TO HAVE THE COVERED CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20041215000362004121500036EA 2004 12 15 ASOA04842 120041027A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MACH TRIM JAMMED A ASOAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SO27856AS 7404 DURING CLIMB-OUT, EN ROUTE, AT APPROXIMATELY 7000 FT, THE CREW REPORTED STAB AND MACH TRIM FAILURE. AFTER COMPLYING WITH THE QRH THE TRIMS STILL COULD NOT BE ENGAGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AFTER RETURNING. MAINTENANCE INTERROGATED THE MDC AND FOUND THE FIRST OFFICERS STAB DISCONNECT SWITCH JAMMED. MAINTENANCE REMOVED AND REPLACED THE JAMMED DISCONNECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041215000382004121500038EU 2004 12 15 ASOA04844 120041027A3350 SOCKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27533AS 460 DURING A 3A-CHECK, THE FLOOR EMERGENCY LIGHT STRIP WAS FOUND MISSING A BULB HOLDER NEXT TO SEAT 17B. MAINTENANCE REPLACED THE MISSING EMERGENCY LIGHT BULB HOLDER. OPERATIONAL CHECKS GOOD. 2H72 4T4 TRTA53EU E20NE 20041215000392004121500039EA 2004 12 15 ASOA04845 120041028A5210601R317011 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MAIN PAX BINDING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27875AS7615 7559 DURING A GROUND INSPECTION, THE MAIN PASSENGER DOOR WAS HARD TO CLOSE USING THE HANDLE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041215000402004121500040EA 2004 12 15 ASOA04846 120041029A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27906EV 7642 DURING AN A-CHECK, THE ENGINE SUPPORT BEAM AT 36.20 ON THE LT AND RT SIDES WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM AT 36.20 ON THE LT AND RT SIDES LOWER WEB IAW EO 600-53-0071. THIS MRR WILL REMAIN OPEN PENDING THE PERMANENT REPAIR WHICH IS TO BE PERFORMED WITHIN 620 FLIGHTS. 2L72 4F4 FRTA21EA E15NE 20041215000412004121500041EA 2004 12 15 ASOA04847 120041029A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 DURING AN A-CHECK, THE LT FS 640 DOUBLER, LT FS 640 FRAME AND THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS 640, STRINGER 8-13 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT FS640 DOUBLER AND LT FS640 FRAME IAW SRM 53-00 AND REPAIRING THE SKIN BUTT JOINT STRAP ON THE LT SIDE AT FS640, STRINGER 8-13 IAW REO 601R-53-61-506. 2L72 4F4 FRTA21EA E15NE 20041215000422004121500042EA 2004 12 15 ASOA04848 120041029A5320601R3501153 SILL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE FLOOR SILL PLATE AT THE CARGO ENTRANCE TWO INTERCOSTAL ATTACH FASTENERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL PLATE AT THE CARGO ENTRANCE IAW EO 600-53-0117. 2L72 4F4 FRTA21EA E15NE 20041215000442004121500044EA 2004 12 15 ASOA04850 120041029A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO27852AS 7369 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED AT THE LIFT POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041215000452004121500045EA 2004 12 15 ASOA04851 120041030A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE GALLEY BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS 7579 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20041215000472004121500047NM 2004 12 15 ASAA0410419 120041003A53306548001183 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE- SKIN GOUGED UNDER LAP. BLENDED GOUGED SKIN AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2EA 20041215000482004121500048NM 2004 12 15 ASAA0410420 120041003A53306548001183 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS IN SKIN AT LAP. BLENDED SCRIBE MARKS AND INSTALLED REPAIR DOUBLERS. 2L72 4F4 FRTA16WE E2EA 20041215000492004121500049NM 2004 12 15 ASAA0410421 120041003A53306548001183 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE IN SKIN AT LAP. BLENDED DAMAGE AND INSTALLED REPAIR DOUBLERS. 2L72 4F4 FRTA16WE E2EA 20041215000542004121500054NM 2004 12 15 ASAA0410432 120041017A5340654585545 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE AFT GALLEY DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON THRESHOLD WEB AFT GALLEY DOOR CUT OUT. REMOVED AND REPLACED WEB. 2L72 4F4 FRTA16WE E2EA 20041215000552004121500055NM 2004 12 15 ASAA0410433 120041017A5313BAC1498158 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CRACKED STRINGER. REMOVED AND REPLACED STRINGER. 2L72 4F4 FRTA16WE E2EA 20041215000562004121500056NM 2004 12 15 ASAA0410454 120041028A5315654681136 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER SECTION, SUPPORT ANGLES, AND REPAIR STRAPS IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215000582004121500058NM 2004 12 15 ASAA0410469 120041104A53136545800122 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE E/E BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - E AND E BAY STRINGER EXFOLIATED. REMOVED DAMAGE, ORDERED AND INSTALLED NEW STRINGER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215000602004121500060NM 2004 12 15 ASAA0410471 120041104A5315654580863 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD SECTION AND REPAIR ANGLES IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215000612004121500061NM 2004 12 15 ASAA0410472 120041104A532065671406 FLOOR SUPPORT BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LONGITUDINAL FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR BEAM IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215000642004121500064WP 2004 12 15 ASAA0480490 120040924A533059114017 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK - FUSELAGE STATION 160 DENTED BETWEEN LONG 24L AND 25L X= .060 D .75 COLD WORKED SKIN BACK TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2L72 4F4 FRTA6WE E9NE 20041215000652004121500065WP 2004 12 15 ASAA0480491 120040924A53305936038501 BEAM DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK - AFT CARGO DOOR LOWER BEAM CORRODED ON LOWER HORIZONTAL FRAME UNDER REPAIR DOUBLER. REMOVED DAMAGED BEAM, ORDERED AND REPLACED BEAM IAW SRM 51-30-5. 2L72 4F4 FRTA6WE E9NE 20041215000662004121500066WP 2004 12 15 ASAA0480492 120040924A533059114053 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK - RT FUSELAGE SKIN DENTED AT STA 223 OVER LONG 4R (WITHIN 1 INCH OF LONG) COLD WORK TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04. 2L72 4F4 FRTA6WE E9NE 20041215000682004121500068WP 2004 12 15 ASAA0480494 120040924A531359360501 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK, LONGERON 30 CORRODED BETWEEN STA 1231 AND 1211 IN AFT PIT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02. 2L72 4F4 FRTA6WE E9NE 20041215000702004121500070WP 2004 12 15 ASAA0480496 120040924A5347593054790 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK- PAX CABIN GALLEY 2 IB FLOOR ATTACH TRACK HAS CORROSION AT STA 237. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 53-05, FIG 4. 2L72 4F4 FRTA6WE E9NE 20041215000732004121500073WP 2004 12 15 ASAA0480499 120040924A532199365851 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK - CABIN FLOOR PANEL AT STA 927 TO 1003 BROKEN AT FORWARD CORNER. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2L72 4F4 FRTA6WE E9NE 20041215000762004121500076WP 2004 12 15 ASAA0480518 120040928A21505910090137 FAIRING DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT ACM EXHAUST CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK, LT ACM EXHAUST FAIRING IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, WELDED CRACK IAW EA 2120-01087 AND EA 10573. 2L72 4F4 FRTA6WE E9NE 20041215000772004121500077WP 2004 12 15 ASAA0480519 120040928A53135936071503 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK, LONGERON 29L IS CORRODED FROM STA 1203 TO 1208 ON THE LOWER SURFACE OF THE OB FAIRING. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IAW SRM 53-02, FIG 18. 2L72 4F4 FRTA6WE E9NE 20041215000792004121500079WP 2004 12 15 ASAA0480523 120040928A575359100403 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT IB FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, RT IB FLAP VANE LOWER SKIN HAS DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2. 2L72 4F4 FRTA6WE E9NE 20041215000842004121500084WP 2004 12 15 ASAA0480529 120041002A531359364311 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19. 2L72 4F4 FRTA6WE E9NE 20041215000872004121500087WP 2004 12 15 ASAA0480532 120041010A561048951421 LATCH DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT WINDOW INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 SEA - PREFLIGHT CHECK - RT (F/O) SLIDING CLEARVIEW WINDOW WOULD NOT OPEN. REPLACED LATCH AND SPRING ASSY. WINDOW THEN OPERATED PROPERLY. 2L72 4F4 FRTA6WE E9NE 20041215000882004121500088 2004 12 15 ASAA0480533 420041011A25653961896501 LANYARD DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE L2 ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02979AS 53471 SJC, PRE-FLIGHT CHECK, AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2L72 4F4 FRT E9NE 20041215000902004121500090NM 2004 12 15 ASAA0480535 120041020A523059101413 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - C-CHECK, AFT PIT DOOR FORWARD MID SECTION 12 INCHES FROM TOP IS DENTED D=.920 X=.030. COLD WORKED DENT TO CONTOUR, HFEC COMPLIED WITH, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2L72 4F4 FRT E9NE 20041215000962004121500096NM 2004 12 15 ASAA0440165 120040929A53406935352U14 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 CRACKED STRINGER CLIP. REMOVED AND REPLACED CRACKED STRINGER CLIP. (REV 1) 2L72 4F4 FRTA16WE E21EU 20041215000972004121500097NM 2004 12 15 ASAA0440166 120040926A53406935352U14 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE WORN A K NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 LOOSE STRINGER CLIP. REMOVED AND REPLACED LOOSE STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041215000982004121500098WP 2004 12 15 ASAA0480503 120040924A53135936027515 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK, AFT PIT STA 1087-1098, LONG 29L, HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19. 2L72 4F4 FRTA6WE E9NE 20041215001012004121500101WP 2004 12 15 ASAA0480506 120040924A532199365477 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D17A 52049NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK, CABIN FLOORBOARD STA 180 TO 200 RBL 44 HAS DELAMINATION AND BROKEN EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2L72 4F4 FRTA6WE E2EA 20041215001042004121500104WP 2004 12 15 ASAA0480509 120040924A531359364311 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, AFT PIT LONGERON 28L AT STA 1098 TO 1110 CORRODED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19. 2L72 4F4 FRTA6WE E2EA 20041215001052004121500105NM 2004 12 15 ASA0440168 120041005A53406562208 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041215001072004121500107NM 2004 12 15 ASAA0410456 120041028A5330654576921 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC- EXTERIOR SKIN BLEND-OUT FOR LIGHTNING STRIKE IS OUT OF LIMITS. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLERS, DOUBLER, AND TRIPLER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001082004121500108NM 2004 12 15 ASAA0410463 120041103A52306547952511 STRUCTURE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE AFT CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC- AFT CARGO DOOR, CENTER SECTION, INTERNAL LIGHTING HOLE HAS .5 INCH CRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001102004121500110NM 2004 12 15 ASAA0410465 120041103A57536546431157 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FORE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LT WING T/E FORE FLAP HAS CHAFING AREA IN OB EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001122004121500112NM 2004 12 15 ASAA0410467 120041103A5313654577742 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - AFT CARGO PIT BILGE AREA CORROSION IN STRINGER FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRINGER SECTION IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001132004121500113NM 2004 12 15 ASAA0410452 120041026A5315654681136 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - CORROSION ON FLOORBEAM TOP FLANGE. REMOVED CORROSION, OUT OF LIMITS IAW SRM. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001142004121500114NM 2004 12 15 ASAA0410453 120041027A5315655491317 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - RT SIDE STA 948 FORWARD FLOORBOARD STRIP ANGLE RBL 44 FASTENER HOLES AND LOWER SIDE FLOORBEAM HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP, FILLER AND WASHERS IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001172004121500117NM 2004 12 15 ASAA0410474 120041104A71106585378340 CAP BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE ENGINE COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - CRACKS STOP DRILLED ON FWD CAP. PREVIOUS REPAIRS NOT ACCOMPLISHED IAW MFG SRM PROCEDURES. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001182004121500118NM 2004 12 15 ASAA0410475 120041104A71106585378339 CAP BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE ENGINE COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - CRACKS STOP DRILLED ON FWD CAP. PREVIOUS REPAIRS NOT ACCOMPLISHED IAW MFG SRM PROCEDURES. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001192004121500119NM 2004 12 15 ASAA0410476 120041104A71106585378333 WEB BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE ENGINE COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - WEB CRACKED AT 6 O`CLOCK POSITION. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001222004121500122NM 2004 12 15 ASAA0410479 120041104A71106585378358 WEB BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE ENGINE COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - WEB CRACKED. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001242004121500124NM 2004 12 15 ASAA0410481 120041104A541465856783 SKIN BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE LT COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - LT COWL OUTER SKIN CRACKED AT 4 O`CLOCK POSITION. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001252004121500125NM 2004 12 15 ASAA0410482 120041104A541465853786 SKIN BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE RT COWL DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - RT COWL OUTER SKIN CREASED AT 3:30 O`CLOCK POSITION. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001262004121500126NM 2004 12 15 ASAA0410483 120041105A53206551525 SPLICE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE STRINGER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - PRODUCTION SPLICE IS CRACKED. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2EA 20041215001282004121500128NM 2004 12 15 ASAA0410486 120041105A53207075T6040 SILL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON UPPER SILL WEB. REMOVED AND REPLACED SILL WEB. 2L72 4F4 FRTA16WE E2EA 20041215001292004121500129NM 2004 12 15 ASAA0410487 120041105A53206948948501 SPLICE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE STRINGER CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E2EA 20041215001312004121500131NM 2004 12 15 ASAA0410492 120041105A53306545768 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DENT IN SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001352004121500135NM 2004 12 15 ASAA0410460 120041028A5311654653980 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 PAE - CRACKED FRAME. REPAIRED. 2L72 4F4 FRTA16WE E2EA 20041215001412004121500141NM 2004 12 15 ASAA0410440 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001422004121500142NM 2004 12 15 ASAA0410441 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001442004121500144NM 2004 12 15 ASAA0410443 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE STA219,230 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001452004121500145NM 2004 12 15 ASAA0410444 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001532004121500153NM 2004 12 15 ASAA0410450 120041026A5313655291819 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CHAFED STRINGER. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001542004121500154NM 2004 12 15 ASAA0410451 120041026A531565549072 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON FLOORBEAM LWR CHORD. REPAIRED FLOORBEAM LWR CHORD IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001562004121500156WP 2004 12 15 ASAA0480511 120040924A52305910141 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, AFT CARGO DOOR SKIN DENTED UPPER AFT AREA X=.040, D=.60, FOUND TO BE CONDITION 1B IAW SRM 53-04, FIG 38, D/X=15. 2L72 4F4 FRTA6WE E9NE 20041215001582004121500158WP 2004 12 15 ASAA0480513 120040924A575359121687 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT IB FLAP PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, RT IB FLAP OB FLAPVANE HAS A PUNCTURE ON THE IB END. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2, PARA 18. 2L72 4F4 FRTA6WE E9NE 20041215001592004121500159WP 2004 12 15 ASAA0480514 120040924A53219936639413 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, FLOOR PANEL AT STA 826 TO 886 AFT IB CORNER ANGLE IS CRACKED. REMOVED, ORDERED AND REPLACED (W) ANGLE IAW SRM 51-30-8. 2L72 4F4 FRTA6WE E9NE 20041215001602004121500160WP 2004 12 15 ASAA0480515 120040924A5532591216610 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT VERT STAB CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, RT VERTICAL STAB LOWER SURFACE CHAFED IN 5 EA SPOTS INNER BANANA FAIRING PANEL 3802A, ATTACHMENT AREA. REMOVED DAMAGED SKINS, ORDERED AND INSTALLED NEW SKINS IAW SRM 51-30-2. 2L72 4F4 FRTA6WE E9NE 20041215001622004121500162NM 2004 12 15 ASA0440173 120041001A534069335352U14 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041215001632004121500163NM 2004 12 15 ASA0440174 120041001A53406935352U14 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041215001652004121500165NM 2004 12 15 ASA0440176 120041006A53476546815149 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - MECHANICAL DAMAGE TO TOP OF SEAT TRACK. REMOVED AND REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E21EU 20041220000022004122000002NM 2004 12 20 SWAA043616 120041213A53306545766 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041220000052004122000005NM 2004 12 20 SWAA043619 120041213A531165C25230 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPT FRAME AT BS 727E, BETWEEN RBL10 AND RBL 20, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041220000072004122000007NM 2004 12 20 SWAA043598 120041203A3350100031 SIGN BOEING737 7373A4 1384585NM EMERGENCY LIGHT DISCONNECTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29679AA 23291 DURING SPV, FOUND RT AFT EMERGENCY EXIT SIGN INOP. RECONNECTED EMERGENCY EXIT SIGN PER MM. 2L72 4F RTA16WE 20041220000092004122000009NM 2004 12 20 SWAA043611 120041213A5420311A1450 STRAP BOEING737 7375H4 138449DNM NR 2 NACELLE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 DURING SCHEDULED SERVICE CHECK, FOUND STRAP AT NAC STA 234, NR 2 ENGINE PYLON, CRACKED. REMOVED AND REPLACED STRAP PER SRM. 2L72 4F RTA16WE 20041220000102004122000010NM 2004 12 20 2004UALA01189 120041206A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29198UA29465 28716 AFT PIT FLOOR SUPPORT STRUCTURE AT STA 1800 HAS DENT AT RBL 22.0. CARGO OPERATIONS PERIODICALLY CAUSES STRUCTURAL DAMAGE IN THE SUPPORT FRAMES. STANDARD REPAIR. 2L74 4F4 FRTA20WE E24NE 20041213001232004121300123NM 2004 12 13 SWAA043390 120041119A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 2 O'CLOCK POSITION. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20041213001252004121300125NM 2004 12 13 UPS04443461 120041102A5312 SPLICE BOEING747 747200 1384847NM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01521UP 21944 INSPECTION TYPE: C, NWW BS 400 STR R44 RIGHT AFT CORNER INTERNAL CIRCUMFERENTIAL SKIN SPLICE FOUND CRACK APPROX .25 INCH LONG RUNNING AFT. THE CRACKED SPLICE REMOVED FOR STOP HOLE DRILLED. THE STOP CONFIRMED NIL CRACK BEYOND THE STOP HOLE. THE AREA REPAIRED PER SRM 53-30-03 FIG 35. 2L74 4F RTA20WE 20041213001272004121300127NM 2004 12 13 SWAA043392 120041119A52106545871 FRAME BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AROUND 3RD STOP FITTING. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20041213001292004121300129NM 2004 12 13 SWAA043395 120041119A3350PL2230LH00 LIGHT BOEING737 7377H4 1384404NM CABIN FLOOR MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29460WN 32464 EEPLS STRIP MISSING AT FWD END. INSTALLED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20041213001312004121300131NM 2004 12 13 SWAA043397 120041119A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED C1 CHECK, FOUND CORROSION BULGE AT FUSELAGE SKIN BS 440, STR 22R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041213001332004121300133WP 2004 12 13 UPS04843455 120041010A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 753.750. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-21 & 51-20D. 2L74 4F RT4A25 20041214000092004121400009NM 2004 12 14 DHL2004755514 120041021A5522 SKIN BOEING727 727225 1384077NM RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A C-CHECK, 2 DENTS SIDE BY SIDE ON LOWER MID SKIN OR RT ELEV APPROX ELEV STA 90. CUT OUT DAMAGED SECTION OF RT ELEV LOWER SKIN 2 X 2 INCH AT ELEV STA 90 & FABRICATED REPAIR DOUBLER 3 X 4 INCH FROM 2024-T3 .032 MAT PO 9001030 & INTERNAL BEADED DOUBLER 7.5 X 3.5 FROM 2024-T3 .032 FROM PO 9001030 IAW B727 SRM 55-20-3 FIG 1 & 55-20-3 FIG 3, TREATED /PRIMED PARTS AND INSTALLED PER B727 SRM 55-20-3 FIG 1, 55-20-3 FIG 3 & 51-10-2, REBALANCED RT ELEV BY CALCULATION METHOD IAW B727 SRM 51-80-7, NEW ELEV BALANCE MOMENT IS +126.65 IN LBS WITHIN ALLOWABLE LIMITS PER B727 SRM 51-80-7, NEW DATA PLATE INSTALLED. 2L73 4F A3WE 20041214000132004121400013NE 2004 12 14 COMA0460668 220041206A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE LEFT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01809CA 7366 807605 FLIGHT 5212 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20041214000172004121400017NM 2004 12 14 CALA0400740 120041209A52306546921530 SKIN BOEING737 7373T0 1384582NM C-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2719357 23841 INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE (2ND ROW FROM TOP) IN C-1 DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01053. 2L72 4F RTA16WE 20041214000242004121400024SO 2004 12 14 C2XA04IA163 120041203A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2734110 145658 EWR - FLIGHT 3332, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT AN EMERGENCY EXIT SIGN IN THE CABIN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20041214000302004121400030WP 2004 12 14 0402149989 120041207A291037723745503 SHUTOFF VALVE DOUG DC9 DC931 3022065WP HYD SYSTEM LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL018945E 47181 THE RIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT AND EXPERIENCED A COMPLETE LOSS OF FLUID. COMPLIED WITH COM PROCEDURES AND AIRCRAFT CONTINUED TO SCHEDULED DESTINATION. LANDING AT CMH WAS UNEVENTFUL AND MAINTENANCE REPLACED A LEAKING RUDDER HYDRAULIC POWER SHUTOFF VALVE. ALSO THE RIGHT SYSTEM FILTERS, ENGINE DRIVEN PUMP, AND ELECTRIC PUMP WERE ALL REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041214000332004121400033EU 2004 12 14 MALA040756 120040926A7160 DUCT BAC 146 AVRO146RJ85A1500097EU NR 4 ENG FAN CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, NR 4 ENGINE LT AFT FAN DUCT COWLING CHAFED. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000462004121400046 2004 12 14 MALA040768 420041202A34256226190113 AHRS SAAB SF340 340B 7860101EU COCKPIT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15361PX 340B249 AIR RETURN FOR YELLOW HEADING FLAGS. PUSHED BOTH CA/FO HEADING SLAVE DID NOT FIX FOLLOWED QRH TO COMPLETION DID NOT FIX AVIONCS HEADING FLAG INTERMITTENTLY ON IN FLIGHT BOTH SIDES APPEAR 3 DEGREES OFF FROM STANDBY HEADING INDICATOR. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS P/N 622-6190-113, S/N OFF 2179, S/N ON 3033. ALL CHECKS GOOD IAW SF340 CHAP 34. 2L72 4T RTA52EU 20041214000562004121400056EU 2004 12 14 MALA040755 120040926A7160 DUCT BAC 146 AVRO146RJ85A1500097EU NR 4 NACELLE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 DURING C1 INSPECTION IN YYC, NR 4 ENGINE RT AFT FAN DUCT COWLING CHAFED. MAINTENANCE MANUFACTURED PART AND INSTALLED IAW SRM 51-24-11, 51-42-00, 51-43-00. AIRCRAFT RETURNED TO SERVICE 10/7/04. 2H74 4F RTA49EU 20041214000612004121400061EU 2004 12 14 AALA20041197 120041206A3350 CONNECTOR AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2114077 612 MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10G INOPERATIVE. REPAIRED WIRING AT SEAT CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20041214000662004121400066CE 2004 12 14 DXTA200400471 120041208A3243991205017 MASTER CYLINDER CESSNA500 560CESSNA 2076750CE LT BRAKE FAILED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07373QS700 5600373 COPILOTS BRAKES SPONGY. LEFT PEDAL REQUIRES SIGNIFICANTLY MORE TRAVEL TO ENGAGE BRAKE (ABOUT 2 INCHES). TROUBLESHOT BRAKE SYSTEM A FAULTY CO-PILOT LT BRAKE MASTER CYLINDER. REMOVED AND REPLACED COPILOT'S LT BRAKE MASTER CYLINDER. BLED BRAKES LEAK & OPS CK WAS GOOD IAW CE560 MM CH 32-42-02. 2L72 4F RTA22CE 20041214000692004121400069WP 2004 12 14 AALA20041198 120041206A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21463AA 49593 SFO - EMERGENCY LIGHT AFT OF ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AFT OF ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041214000802004121400080WP 2004 12 14 ABXA040372 120041108A24322634006106 CHARGER DOUG DC9 DC931 3022065WP BATTERY DEFECTIVE A ABXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL23948AX184 47065 DIVERSION FOR A BATTERY CHARGER PROBLEM WHICH OCCURRED OUT OF ICT EN ROUTE TO ILN. AIRCRAFT DIVERTED TO MCI. BATTERY CHARGER INDICATED CONSTANT CHARGE IN CLIMB GREATER THAN 40 AMPS FOR MORE THAN 2 MINUTES. REMOVED AND REPLACED BATTERY CHARGER AND BOTH BATTERIES. CHECKED TEMP SENSOR 197 OHMS. FOUND TO BE GOOD IAW DC-9 AMM 24-30-02-2. 2L72 4F A6WE 20041214000812004121400081WP 2004 12 14 0401479907 120040831A2731 CONTROL CABLE DOUG DC9 DC931 3022065WP LT ELEVATOR OUT OF RIG A NWAAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL01957N 47253 AT ROTATION SPEED DURING TAKEOFF ROLL, THE AIRCRAFT PICKED UP AND TOOK OFF WITHOUT ANY PILOT INPUT ON THE CONTROLS. CREW ALSO MENTIONED FEELING A VIBRATION THROUGH THE YOKES DURING FLIGHT. AIRCRAFT WOULD PITCH UP NOTICEABLY DURING CLIMBOUT WITH AUTOPILOT DISCONNECTED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE AT DTW FOUND THE LEFT ELEVATOR AND CONTROL TAB CABLES OUT OF RIG. AFTER THE CABLES WERE RE-RIGGED, A FLIGHT TEST WAS PERFORMED AND THE AIRCRAFT CHECKED SATISFACTORY AND WAS RETURNED TO SERVICE. 2L72 4F A6WE 20041214000842004121400084NM 2004 12 14 F3LA200400104 120040928A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, FLOORBEAM GOUGED AND CORRODED AT STA 947.5 - 967, RBL 16. REPLACED DAMAGED INTERCOSTAL PER SRM 51-40-02 AND 53-60-51. 2L72 4F RTA16WE 20041214001052004121400105NM 2004 12 14 UPS04243244 120040829A5340 FITTING BOEING727 727173C 1384059NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, SUSPECT CRACK ON LEFT 950 O/B LUG AFT SIDE. FITTING REPLACED IAW SRM 51-30-02 AND AAAE EO 2004-083-001R1 (727-53- 20161). 2L73 4F A3WE 20041214001082004121400108NM 2004 12 14 UPS04443232 120040927A5414 SKIN BOEING747 747200 1384847NM NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE: AD, NR 1 PYLON UPPER LINK ATTACHMENT LUG AREA TOP 2ND LAYER SKIN CRACKED AS RED MARKED (BS 221, WBL L834 TO L834). TEMPORARY REPAIR CARRIED OUT PER EO B747-5430-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE. 2L74 4F RTA20WE 20041214001102004121400110NM 2004 12 14 UPS04443234 120040927A5414 SKIN BOEING747 747200 1384847NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01523UP 22381 INSPECTION TYPE:AD, NR 2 PYLON UPPER LINK ATTACHMENT LUG AREA TOP SKIN 1 OFF CRACK FROM RIVET HOLE TOWARDS REAR AS RED MARKED (BS 221-221, WBL L470-L470). TEMPORARY REPAIR CARRIED OUT PER EO B747-5430-21111-A. STOP HOLE DRILLED AND NDT CONFIRM CRACK FREE. THE ADDITION 2ND LAYER CRACK OF 0.06 INCH LENGTH. 2L74 4F RTA20WE 20041214001192004121400119SO 2004 12 14 SWIA200414070 120041108A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07295SW8330 8330 120322 FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-00. 2L72 4T RTA31SO 20041214001232004121400123NM 2004 12 14 SWAA043435 120041123A53306545772 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041214001332004121400133 2004 12 14 SWAA043424 420041123A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041214001352004121400135CE 2004 12 14 DXTA200400440 120041106A281099144751 FLAPPER VALVE CESSNA750 750 2076810CE FUEL CELL FAILED E DXTAO OTHER J WARNING INDICATION CRCRUISE 1 GL07990QS2576 7500190 INFLIGHT THE WING TANK OVERFILL L CAS MESSAGE CAME ON. THE LEFT WING TANK SHOWED 3200 LBS OF FUEL IN IT AND FUEL STARTED TO VENT OVERBOARD, VENTING STOPPED AT ABOUT 2970 LBS INDICATED IN L WING TANK. AFTER LANDING (20 MIN LATER) CREW NOTICED THE UNDERSIDE OF THE L WING WAS WET. DEFUELED & SUMPED LEFT WING TANK. GAINED ACCESS TO AND INSPECTED CLIMB VENT TUBE AT I/B END OF WING TANK & FOUND IT TO BE POSITIONED & SECURED PROPERLY. INSPECTED SURGE TANK DRAIN LINE FOR CLOGS WITH BOROSCOPE & FOUND NO DEBRIS. REPLACED SURGE TANK DRAIN FLAPPER VALVE P/N 9914475-1 WITH NEW FLAPPER. REPLACED VENT FLOAT VALVE AT O/B END OF WING TANK WITH A SERVICEABLE UNIT. REFUELED WING TANKS & FOUND NO LEAKS. 2L72 4J RTT00007WI 20041214001422004121400142WP 2004 12 14 UPS04843223 120040909A571257695891 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 UPPER RIB CRACKED IN LT CENTER L/E ABOVE OPENING FOR PANEL 520B. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20041214001562004121400156EA 2004 12 14 SWIA200414060 120041030A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20041214001782004121400178WP 2004 12 14 UPS04842787 120040729A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:N/A CIRCUMFERENTIAL TIE STRAP BELOW AFT DOOR FRAME AT LOWER DOOR CUTOUT HAS EXFOLIATION CORROSION. ACCOMPLISHED EO DC8-5310-20796 BLENDED OUT CORROSION. REPEAT INSP'S AT EVERY C-CHECK PERFORMED VLT THICKNESS CK & HFEC PER UPS EO DC8-5310-20796. NO CRACKS DETECTED. XFRD TO D284984. 2L74 4F RT4A25 20041214001902004121400190 2004 12 14 UPS04542700 420040709A2561350510141 LIFE VEST BOEING757 75724APF 1384969NM COCKPIT MISSING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01457UP 25478 INSPECTION TYPE:N/A, F/O'S LIFE VEST MISSING. REPLACED F/O'S LIFE VEST. 2L72 4F RTA2NM 20041215000172004121500017NM 2004 12 15 USAA040761 120041020A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 CLT, C-4, FLOORBEAM, .5 INCH AREAS SEVERAL SPOTS, LEVEL 1 CORROSION, STA 377.7 FROM LBL62 TO RBL12. ACCOMPLISHED (T) CAP REPAIR IAW TR 53-15-01 AND EA 95899. 2L72 4F4 FRTA2NM E12EU 20041215000242004121500024EA 2004 12 15 A6WA200440186 120041112A3213 STRUT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG DISCHARGED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31466AW 7899 GEAR DISAGREE AFTER TAKEOFF, COMPLIED WITH QRH LANDING WEIGHT 47,000 LBS. JACKED AIRCRAFT AND OBSERVED NLG NOT SELF-CENTERING SERVICED HYDRAULIC FLUID IN STRUT AND NITROGEN CHARGE IAW MM 12-1232. JACKED AIRCRAFT AGAIN, NLG CENTERS ON ITS OWN. SWUNG ALL 3 GEARS. OPS CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20041215000512004121500051NM 2004 12 15 ASAA0411428 120041012A53306545777 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - 50 HOLES HAVE CRACK INDICATIONS AT SKIN LAP. REPAIRED DISCREPANT HOLES IAW EA. OVERSIZED .0312 INCH. 2L72 4F4 FRTA16WE E2EA 20041215000622004121500062WP 2004 12 15 ASAA0480488 120040924A533059134213 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC C-CHECK - LT NOSE GEAR AFT HINGE CUT OUT IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05, FIG 63. 2L72 4F4 FRTA6WE E9NE 20041215000632004121500063WP 2004 12 15 ASAA0480489 120040924A533059114013 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK- LT FUSELAGE SKIN DENTED OVER FRAME AT STA 237, BETWEEN LONG 18L AND 19L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, FINGER DOUBLER, AND STRAP IAW SRM 53-04, FIG 12C. 2L72 4F4 FRTA6WE E9NE 20041215000672004121500067WP 2004 12 15 ASAA0480493 120040924A532099365473 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, CABIN FLOORBOARD AT STA 166 AND STA 152 AT RBL 7 HAS 2 EA CORRODED INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05 PAR 44. 2L72 4F4 FRTA6WE E9NE 20041215000752004121500075WP 2004 12 15 ASAA0480516 120040928A5250 STRAP DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE COCKPIT DOOR BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 137 53449 OKC - C-CHECK, COMPLY WITH JOB 062, LOG NR 5784357, COCKPIT DOOR CLOSING STRAP BROKEN OFF. FABRICATED AND INSTALLED PLATE IAW EA 5250-01191 AND EA 10559. 2L72 4F4 FRTA6WE E9NE 20041215000812004121500081WP 2004 12 15 ASAA0480526 120040928A55305912166259 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE VERTICAL STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK VERTICAL STAB UPPER SKIN GOUGED AROUND BANANA UPPER FAIRING PANEL 3705A ATTACHMENT AREA. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER/SKIN AND DOUBLER, IAW SRM 51-30-1 AND 51-30-2, EA 5530-01108 AND EA 10594. 2L72 4F4 FRTA6WE E9NE 20041215000822004121500082WP 2004 12 15 ASAA0480527 120041002A5530593602229 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, AFT BELLY SKIN CORRODED STA 1098 TO STA 1110 BETWEEN LONG 29L AND 27L. REMOVED DAMAGE, HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 5310-02398 AND EA 10582. 2L72 4F4 FRTA6WE E9NE 20041215000852004121500085WP 2004 12 15 ASAA0480530 120041002A5730ARB097517 ACCESS PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT WING LEAKING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS NR 5 AND NR 7 FROM IB. REMOVED PANEL, ORDERED AND INSTALLED NEW PANEL IAW MM 28-00-00. 2L72 4F4 FRTA6WE E9NE 20041215000922004121500092NM 2004 12 15 ASAA0480537 120041020A531059364423 DOOR FRAME DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - C-CHECK, AFT CARGO DOOR JAMB LOWER WEB IS CORRODED AT STA 1212 TO STA 1231. REMOVED DAMAGED SECTION OF WEB, ORDERED AND INSTALLED NEW WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-04 AND 51-30-5. 2L72 4F4 FRT E9NE 20041215001032004121500103WP 2004 12 15 ASAA0480508 120040924A532199366391 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, CABIN FLOOR PANEL, STA 826-STA 886 DAMAGED AT FWD IB CORNER. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM 53-05. 2L72 4F4 FRTA6WE E9NE 20041215001062004121500106NM 2004 12 15 ASAA0410455 120041028A5315654580863 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC- FLOORBEAM HAS CORROSION ON UPPER AND LOWER SURFACES OF TOP FLANGE. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER SHIM, AND REPAIR ANGLES IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001092004121500109NM 2004 12 15 ASAA0410464 120041103A575365464305 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FORE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC- RT WING IB FORE FLAP UPPER SURFACE HAS 6 AREAS THAT ARE CHAFED TO BARE METAL. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001112004121500111NM 2004 12 15 ASAA0410466 120041103A53156545812141 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - STA 328 FLOORBEAM CORRODED AT RBL 11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND ANGLES IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215001302004121500130NM 2004 12 15 ASAA0410488 120041105A5330654577465 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REMOVED DAMAGE AND INSTALLED REPAIR. 2L72 4F4 FRTA16WE E2EA 20041215001332004121500133NM 2004 12 15 ASAA0410458 120041028A531565549061 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON FLOORBEAM LOWER FLANGE, LOWER SURFACE. REPAIRED WITH DOUBLER. 2L72 4F4 FRTA16WE E2EA 20041215001402004121500140NM 2004 12 15 ASAA0410439 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001512004121500151NM 2004 12 15 ASAA0410448 120041022A531065454115 BEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON LONGITUDINAL BEAM. REMOVED AND REPLACED LONGITUDINAL BEAM. 2L72 4F4 FRTA16WE E2EA 20041215001522004121500152NM 2004 12 15 ASAA0410449 120041022A533065458001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE NICKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - EXTERIOR SKIN HAS NICKS. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20041220000082004122000008NM 2004 12 20 SWAA043607 120041212A53306545776 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29521SW 25320 FUSELAGE SKIN AT BS 931, ABOVE STRINGER 25L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041220000112004122000011NM 2004 12 20 2004UALA01199 120041208A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 STA 1460 FRAME HAS DENT IN THE UPPER FLANGE AT STR 26L. DAMAGE WAS CUTOUT AND A FRAME "J" ANGLE REPAIR ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20041220000152004122000015NM 2004 12 20 QXEA200400863 120041203A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT EXTERIOR SKIN PANEL HAS TWO NICKS AT STATION X58.5 BETWEEN STRINGERS 31X AND 32S. REPAIRED IAW HORIZON AIR EA 6-53-484 AND RD 8/4-53-1099. 2H72 4T RTA13NM 20041220000162004122000016NM 2004 12 20 AALA20041217 120041213A3350 CONNECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21373AA 25200 ORD - EMERGENCY LIGHTS AT SEAT 2H INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041220000192004122000019GL 2004 12 20 DL764041102 220041214A7200CF680C2B8F ENGINE BOEING767 767432ER 1385134NM GE CF6 CF680C2* GL NR 1 FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27844MH9070 29717 706431 ENGINE FAILED 5TH STAGE VANE INSP PER 48-78306-12, OVER 70 PERCENT LOOSE. REPLACED ENGINE. 2L72 4F4 FRTA1NM E23EA 20041220000202004122000020EU 2004 12 20 MALA040794 120041030A5755 SEAL BAC 146 AVRO146RJ85A1500097EU SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND RIGHT OUTBOARD LIFT SPOILER TRAILING EDGE SEAL CRACKED AND HAS PIECES MISSING. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20041220000222004122000022EU 2004 12 20 MALA040806 120041011A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND LT I/B SEAT TRACK 18.5R CORRODED. MAINTENANCE REPAIRED IAW MESABA EO S52060. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20041220000252004122000025NM 2004 12 20 SWAA043640 120041215A3350311500 LENS BOEING737 7373G7 1384595NM EMERGENCY LIGHT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 11 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041220000282004122000028NM 2004 12 20 04FDEA03436 120041217A5330 SKIN BOEING727 727100 1384036NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 EXTERNAL SKIN CRACKED AT AFT LWR CARGO DOOR CUTOUT 10 INCHES AFT OF THE FWD LWR CORNER 2 INCHES BELOW LWR EDGE. REPAIRED CRACKED SKIN, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA 7-5330-82517. 2L73 4F RTA3WE 20041220000322004122000032NM 2004 12 20 SWAA043641 120041215A5753 SKIN BOEING737 7373Q8 1384670NM RT WING FOREFLAPDELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29672SW 23406 DURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. 2L72 4F RTA16WE 20041220000342004122000034EA 2004 12 20 COMA0460692 120041216A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 LEFT HAND LOWER ENGINE SUPPORT BEAM HAS CRACK. REPAIRED IAW REO 601R-53-61-366. 2L72 4F RTA21EA 20041220000352004122000035NM 2004 12 20 04FDEA03424 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, FLOOR STRUCTURE HAT SECTION CORRODED AT STA 1821 TO STA 1887, LBL 36. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. DUPLICATE OF SNRM N3170. 2L73 4F RTA22WE 20041220000362004122000036EA 2004 12 20 COMA0460690 120041216A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 RIGHT LOWER ENGINE SUPPORT BEAM CRACK. REPAIRED IAW REO 601R-53-61-366. 2L72 4F RTA21EA 20041220000382004122000038NM 2004 12 20 04FDEA03431 120041217A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO - LONGERON SPLICE CRACKED AT L46R STA 1531, FOUND AFTER SPLICE REMOVAL. LONGERON SPLICE REMOVED, FABRICATED AND REPLACED AS PER DWG A5A7116 AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041220000392004122000039 2004 12 20 SWAA043639 420041215A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29670SW 23784 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041220000402004122000040EA 2004 12 20 04350668 120041215A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27668BR 7544 ODOR AND LITE FOGGY FILM IN CABIN AFTER TAKEOFF, ALSO ALARM WENT ON. MX INSPECTED CABIN AND LAV LIGHTING AND RAN ENGINE. NO DEFECT NOTED. POSSIBLE RESIDUE FROM DEICING FLUID. 2L72 4F RTA21EA 20041220000432004122000043 2004 12 20 RAIA00412018 420041213A3425 SYMBOL GENERATOR JETAIRJETSTMJETSTM4101 1500501EU NR 1 AHRS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03557HK 41074 RIC - NR 1 AHRS INTERMITTENT, BOTH ADI AND HSI INTERMITTENTLY LOOSING SYMBOLOGY DURING TAXI DISPLAYS WERE FLASHING. MAINTENANCE RESEATED NR 1 AHRS AND SYMBOL GENERATOR SYSTEM CHECK GOOD. 2L72 4T RTA41NM 20041220000452004122000045EA 2004 12 20 COMA0460689 120041216A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 RIGHT 640 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-487. 2L72 4F RTA21EA 20041220000462004122000046 2004 12 20 UPS04543592 420041209A3140 DISPLAY BOEING757 75724APF 1384969NM EICAS MALFUNCTIONED A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01446UP 27735 INCOMING RECEIVED EICAS MSG RT ELEVATOR PCU, LT ELEVATOR PCU, AFT EXHAUST FAN 1, AFT EXHAUST FAN 2. CREW UNABLE TO RESOLVE, DECLARED EMERGENCY. ALL STATUS LEVEL MSGS CLEARED THRU EICAS INTEROGATION REF CH AMM 31-41-00. PCU CHECKED, FOUND NO ERROR CODES, FLT CONTROL CHECKS PERFORMED A/C CLEARED WITH POWER TRANSFER CHECKS OK. 2L72 4F RTA2NM 20041220000482004122000048NM 2004 12 20 UPS04543595 120041208A3520 OXYGEN MASK BOEING757 75724APF 1384969NM F/O COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01414UP 23854 PILOT REPORT - FIRST OFFICERS 02 MASK INOP. REPLACED FIRST OFFICERS 02 BOX AND MASK WITH FIRST OBSERVERS 02 BOX AND MASK ASSY IAW MM REF 35-11-51-4. FIRST OFFICERS 02 MASK, NOW OK FOR SERVICE. 2L72 4F RTA2NM 20041220000492004122000049WP 2004 12 20 UPS04843594 120041209A3350 BULB DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:N/A EMERGENCY EXIT INDICATOR LIGHT BULB INOP. RELAMPED INTERIOR EMERGENCY EXIT LIGHT. OPS CK GOOD PER MM 33-11-0. 2L74 4F RT4A25 20041220000502004122000050NM 2004 12 20 SWAA043623 120041214A335007912 LIGHT BOEING737 7373H4 1384600NM ROWS 6 & 7 LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 EEPLS STRIP AT ROWS 6 AND 7 DEF, LOOSE. REPAIRED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20041220000512004122000051 2004 12 20 SWAA043624 420041214A25656557463 FITTING BOEING737 7375H4 138449DNM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29513SW 24190 AFT SERVICE DOOR EVAC SLIDE FWD GIRT BAR FITTING LOOSE. REINSTALLED SCREWS PER MM. 2L72 4F RTA16WE 20041220000542004122000054NM 2004 12 20 SWAA043627 120041214A53106545833 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 295 TO BS 299, RBL 55, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20041220000562004122000056NM 2004 12 20 SWAA043629 120041214A53306545778 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 885, ABOVE STRINGER 24R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041220000592004122000059EA 2004 12 20 COMA0460691 120041216A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 CARGO LANDING PLATE CRACKED AROUND LOCK FITTING HOLE ON FORWARD SCUFF PLATE FITTING AT 574.00. REPAIRED IAW REO 601R-53-61-1222. 2L72 4F RTA21EA 20041220000622004122000062EU 2004 12 20 AWXA200401404 120041209A5340D5323095720000 FITTING AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK A .5 INCH CRACK WAS FOUND IN FITTING IN FORWARD CARGO COMPARTMENT AT FR 28, STR 43 RT. MAINTENANCE REMOVED CRACKED FITTING AT FR 28, STR 43 RT; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2, 3, & 8. 2L72 4F RTA28NM 20041220000632004122000063NM 2004 12 20 AWXA200401405 120041129A5310654587113 DOOR FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-15 CHECK A .25 INCH CRACK WAS FOUND IN R-1 DOOR AFT FRAME AT 4TH DOOR STOP CUTOUT FROM THE BOTTOM BS 360, STR 11 RT. MAINTENANCE CUT OUT CRACKED AREA OF R-1 DOOR AFT FRAME AT DOOR STOP CUTOUT BS 360, STR 11 RT, WHILE PERFORMING REPAIR DISCOVERED CRACKED REPAIR ANGLE IN SAME LOCATION. REMOVED CRACKED ANGLE; FABRICATED A REPAIR DOUBLER AND NEW REPLACEMENT REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5200-04348-RC1. 2L72 4F RTA16WE 20041220000642004122000064NM 2004 12 20 SWAA043608 120041212A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 767, LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041220000652004122000065EU 2004 12 20 RAIA00412010 120041206A3250AIR860122 SELECTOR VALVE JETAIRJETSTMJETSTM4101 1500501EU NLG STEERING FAILED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03566HK17669 41084 STL - PULLS TO RIGHT DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED SELECTOR VALVE. 2L72 4T RTA41NM 20041220000672004122000067NM 2004 12 20 SWAA043599 120041114A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29747SA 29799 DURING SPV, FOUND 2 EACH BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 10 DEF AND ROW 19 ABC, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041220000692004122000069 2004 12 20 SWAA043601 420041211A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29767SW 29807 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041220000752004122000075NM 2004 12 20 2004UALA01201 120041120A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29574UA 26686 SMOKE ODOR IN CABIN AND FLT DECK. ON COFFEEMAKER PERFORMED VISUAL CHECK OF ALL INTERNAL AND EXTERNAL WIRING. NO DEFECTS FOUND. PERFORMED PERATIONAL TEST ON UNIT. UNIT PASSED BREW TEST. UNIT WAS MONITORED WITH POWER AND WATER ON FOR AN ADDITIONAL 30 MINUTES:NO ANOMALIES NOTED. ON COFFEEWARMER PERFORMED VISUAL CHECK OF ALL INTERNAL AND EXTERNAL WIRING. NO DEFECTS FOUND. NO PHYSICAL SIGNS OF DAMAGE OR DISTORTION TO UNIT. UNIT REMAINED POWERED-UP FOR 30 MINUTES: NO ANOMALIES NOTED. 2L72 4F4 FRTA2NM E17NE 20041220000772004122000077WP 2004 12 20 04FDEA03262 120041129A5753 ROLLER DOUG MD10 MD1010F 3022112WP ZONE 600 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 RIGHT WING LOWER AFT LOAD ROLLER HAS WORN BEARING SURFACE, CHROME WORN ON INBOARD FLAP TRACK ATTACHMENT AREA. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK AFT LARGE LOAD ROLLER IAW FEDEX EA 8- 5750-81513. 2L73 4F RTA22WE 20041220000782004122000078WP 2004 12 20 04FDEA03263 120041129A5753 ROLLER DOUG MD10 MD1010F 3022112WP ZONE 600 LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 RIGHT WING LOWER FORWARD INBOARD FLAP LOAD ROLLER HAS EXCESSIVE LATERAL PLAY. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK LOWER ROLLER IAW FEDEX EA 8-5750- 81513, WING- INBOARD FLAP- INBOARD ROLLER TORQUE REQUIREMENT- CLARIFICATION. 2L73 4F RTA22WE 20041220000792004122000079NE 2004 12 20 DL75K041087 220041206A7297 WIRE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE CHAFED A DALAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO276703D32613 30234 716583 NR 2 ENG ROLLED BACK TO APPROX 63 PERCENT N1 AT FL 410, WOULD NOT ACCELERATE NORMALLY AFTER THROTTLE RETARDED AND THE ADVANCED ENGINE STAYED ROLLED BACK UNTIL DESENDING BELOW 10,000 FT MSL AND THEN OPERATED NORMALLY FOR THE REST OF THE FLIGHT THROUGH LANDING. REPAIRED CHAFED WIRING AND REPLACED PDIU. 2L72 4F4 FRTA2NM E17NE 20041220000802004122000080EA 2004 12 20 COMA0460674 120041210A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01926CA 7027 FLIGHT 5274 RT REVERSER UNLOCK MESSAGE. SECURED T/R AND DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20041220000832004122000083NM 2004 12 20 SWAA043595 120041210A5753 SKIN BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29656SW BN1216 28401 DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20041220000852004122000085NM 2004 12 20 04FDEA03178 120041122A5510ALC8101503 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 3L EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 3L REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR. 2L73 4F RTA22WE 20041220000892004122000089EA 2004 12 20 COMA0460675 120041210A3240 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA BRAKE ACTIVATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01918CA 7018 FLIGHT 5144 ANTI SKID CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM AND OPERATIONAL CHECK, FOUND NO DEFECTS. 2L72 4F RTA21EA 20041220000912004122000091NM 2004 12 20 04FDEA03289 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220000922004122000092NM 2004 12 20 04FDEA03290 120041130A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09, PAGES 402-407. 2L73 4F RTA22WE 20041220000932004122000093NM 2004 12 20 DL764041094 120041212A3350 BULB BOEING767 767432ER 1385134NM EMERGENCY LIGHT FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO27825MH 29696 TWO OVERHEAD EXIT LIGHTS INOPERATIVE. RELAMPED SAME. 2L72 4F RTA1NM 20041220000942004122000094NM 2004 12 20 04FDEA03202 120041124A5410 LINER DOUG MD11 MD11 3023602NM NR 1 NACELLE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 POST FLIGHT WALK AROUND FOUND SEVERAL AFT LINER SEGMENTS WITH UPPER SKIN GONE AND HONEYCOMB MATERIAL DAMAGED. ALMOST EVERY SEGMENT DAMAGED ON NR 1 ENGINE. NR 3 ENGINE FOUND AFT LINER SEGMENT OUTER SKIN DELAMINATED AND HONEYCOMB MATERIAL DAMAGED ALMOST COMPLETED AROUND THE ENGINE. INSPECTED NR 2 ENGINE, FOUND 6 INCH SECTION OF SEGMENT AT THE 4 O'CLOCK POSITION DAMAGED. TRIPLE ENGINE CHANGE IN PROGRESS. 2L73 4F RTA22WE 20041220000952004122000095NM 2004 12 20 04FDEA03291 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09, PAGES 402-407. 2L73 4F RTA22WE 20041220000962004122000096NM 2004 12 20 DLM88041103 120041212A499038005041 APU DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE APU BAY LEAKING A DALAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27918DE14747 49959 P80295 ATB, SMOKE IN THE CABIN AFTER T/O AFT LAV SMOKE DETECTORS WENT OFF. NO SMOKE NOTED IN LAVS OR AFT CABIN. REPLACED APU AND PERFORMED DUCT BURNOUT. 2L72 4F4 FRTA6WE E2EA 20041220000972004122000097WP 2004 12 20 ABXA040392 120041111A53305911405503 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 MAIN ENTRY DOOR UPPER AFT STOP HAD CRACKED SURFACE SKIN. REPAIRED MAIN ENTRY DOOR UPPER AFT CORNER IAW JOB CARD EA 53100126-001, SERVICE REPAIR DRAWING SR09530252-7001 AND DC-9 SRM 53-05. 2L72 4F A6WE 20041220000992004122000099NM 2004 12 20 04FDEA03293 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09. REPAIRED AS PER EA 1-5750-78056. 2L73 4F RTA22WE 20041220001022004122000102WP 2004 12 20 ABXA040396 120041111A53305910228188 SKIN PANEL DOUG DC9 DC933F 302207AWP AFT FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 TWO CRACKS IN FUSELAGE SKIN FS 1143, APPROXIMATELY LONGERON 14 RIGHT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM 53-01. 2L72 4F A6WE 20041220001062004122000106WP 2004 12 20 04FDEA03258 120041129A5312NBA60543 PRESSURE BLKHD DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR UNDER RADAR ON PRESSURE BULKHEAD NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. PERFORMED FEDEX EA 8-5330-83949, FUSELAGE- REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STATION 275, FORWARD PRESSURE BULKHEAD. OPENED AND CLOSED RADOME IAW MD10-10 MM 53-51-00-2. 2L73 4F RTA22WE 20041220001072004122000107WP 2004 12 20 04FDEA03259 120041129A5246ARB1101503 DOOR DOUG MD10 MD1010F 3022112WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT WING REFUEL PANEL, DELAMINATED ON EDGES ADJACENT TO HINGE, AS MARKED. LOWER SKIN, CORE AND BLOCKS BONDED IAW TPS 1001 REV E, DAC DWG ARB1011 AND FEDEX EA 8- 5710-83944, AND DC10 SRM 51-70-00 VOL 2. 2L73 4F RTA22WE 20041220001152004122000115WP 2004 12 20 04FDEA03243 120041129A5313AGA3084507 LONGERON DOUG DC10 DC1010 3022110WP FUSELAGE MISMANUFACTURED A FDEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON STR 46 RT THE LONGERON SUPPLIED HAS BEEN FORMED INCORRECTLY. INSTALL A NEW LONGERON. 2L73 4F A22WE 20041220001172004122000117WP 2004 12 20 04FDEA03245 120041129A5753 HINGE DOUG DC10 DC1010 3022110WP RT TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT OUTBOARD FLAP FWD HINGE SECTION STA XW 638 WITH CORROSION IN THE BORE OF BUSHINGS ACTUATOR ATTACH POINTS. ACCOMPLISH CORROSION REWORK AT RT OUTBD FLAP OUTBD FWD HINGE HOLE BORES (5A), (5B) IAW CMM 57-44-09 REV 30. 2L73 4F A22WE 20041220001192004122000119WP 2004 12 20 04FDEA03264 120041129A78309077M51G02 MANIFOLD DOUG MD10 MD1010F 3022112WP ZONE 400 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 NR 1 ENGINE OUTBOARD THRUST REVERSER UPPER COOLING DUCT IS CHAFED IN SEVERAL AREAS. REMOVED COOLING DUCT IAW DC10 SRM 51-31-01 VOL 2. WELD REPAIRED COOLING MANIFOLD IAW FEDEX EA 8-7830-81526, EXHAUST SYSTEM NR 1 OUTBOARD THRUST REVERSER COOLING DUCT MANIFOLD REPAIR. REINSTALLED COOLING MANIFOLD DUCT IAW MD10 SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20041220001202004122000120NM 2004 12 20 04FDEA03273 120041130A5310652533855 BEAM BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25208FE 22930 MAIN CARGO DOOR LWR LONGITUDINAL FRAME / CAP IS CRACKED OUTSIDE PREVIOUS REPAIRED AREA AT NR 4 LATCH CAM. COMPLIED WITH EA 7-5230-55418, REF: WRI 52-30/8452. 2L73 4F RTA3WE 20041220001232004122000123NM 2004 12 20 04FDEA03320 120041202A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. 2L73 4F RTA22WE 20041220001252004122000125WP 2004 12 20 04FDEA03322 120041202A5313 LONGERON DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE CONVERSION FROM P-F/ACF FOUND RT LONGERON 33 CRACKED AT STA 555 / STA 575. P/N 3849-19. REPLACE LONGERON PER SRM 51-35-01 PAGE 1-13 P/N ACA 3849-19, REINSTALL SKIN PER SRM 51-33-01 PAGE 34-47, SRM 51-35-01 PAGE 1-13. 2L73 4F A22WE 20041220001272004122000127WP 2004 12 20 04FDEA03325 120041202A5410 BUSHING DOUG DC10 DC1010 3022110WP NR 3 PYLON WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON PYLON NR 3 BUSHING AFT WITH WEAR. REPLACE BUSHING PER MM 54-00-02-4, P/N AUB 7281-1. SPHERICAL BEARING PER MM 54-40-02. PERFORM DIMENSIONAL CHECK OF HOLE TO DETERTMINE WHICH O/S BEARING TO ORDERED. 2L73 4F A22WE 20041220001282004122000128NM 2004 12 20 04FDEA03420 120041215A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK - SEAT TRACK RBL 27 CORRODED AT STA 457 TO STA 467. 2L73 4F RTA22WE 20041220001312004122000131WP 2004 12 20 WX0400060 120041208A33501315 BULB DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19890GA 49371 LAS - MAINTENANCE REPORTED ROW 4 EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041220001322004122000132NM 2004 12 20 04FDEA03156 120041118A5510ALC8103503 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 30L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE NR 30L REPAIRED PER FEDEX EA 1-5510-79789, STABILIZERS - HORIZONTAL STABILIZERS - BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000. 2L73 4F RTA22WE 20041220001342004122000134NM 2004 12 20 04FDEA03158 120041118A5510ALC810Y1 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 26L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 26L, REMOVED AND REPLACED PER SRM 51-33-01 VOLUME 2. 2L73 4F RTA22WE 20041220001362004122000136EU 2004 12 20 MALA040795 120041028A5280 DOOR BAC 146 AVRO146RJ85A1500097EU NLG BENT A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT NOSE GEAR DOOR LOWER EDGE BENT. MAINTENANCE REPLACED RIVETS AND REPAIRED IAW SRM 51-42-00, 51-43-00 & 51-10-02. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20041220001382004122000138NM 2004 12 20 2004UALA00818 120040831A7120 HANGER ASSY BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 ENG MOUNT CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 3 ENGINE AFT MOUNT HANGER PITTED AROUND BOLT HOLE I/B SIDE & O/B SIDE. NR 3 ENGINE AFT MOUNT REPLACED. 2L74 4F4 FRTA20WE E24NE 20041220001412004122000141NM 2004 12 20 04FDEA03306 120041201A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 980 FOUND CORRODED. REPAIR CARRIED OUT AT RT WING REAR SPAR UPPER SKIN AT STA XORS 980 AS PER EA 1-5710-79795. 2L73 4F RTA22WE 20041220001422004122000142NM 2004 12 20 04FDEA03307 120041201A5730 SKIN DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 1042 FOUND CORRODED. REPAIR CARRIED OUT AT RIGHT HAND WING - REAR SPAR UPPER SKIN AT STA XORS 1042 AS PER EA 1-5710-79795. 2L73 4F RTA22WE 20041220001432004122000143NM 2004 12 20 04FDEA03308 120041201A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON 46 RT CORRODED AT STA 5-93. REPAIR CARRIED OUT AT LONGERON 46RH AT STA 5-93 AS PER SRM 53-10-00 VOL I. 2L73 4F RTA22WE 20041220001442004122000144NM 2004 12 20 QXEA200400876 120041211A5730 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT HAND WING BETWEEN STATION YW98.6-117.5. REPAIRED IAW RD 8/4-57-399 HORIZON AIR EA 6-57-268 AND SRM 51-21-10. 2H72 4T RTA13NM 20041220001452004122000145NM 2004 12 20 QXEA200400877 120041211A2810 LINE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - EJECTOR MOTIVE FLOW LINE INSIDE LEFT WING PANEL 523AT CHAFED BY FUEL FEED LINE. REPAIRED IAW HORIZON AIR EA 6-28-19 AND SRM TASK 28-21-06-000-801. 2H72 4T RTA13NM 20041220001502004122000150EU 2004 12 20 MALA040774 120041008A3210 ATTACH ANGLE BAC 146 AVRO146RJ85A1500097EU MLG BAFFLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, MLG CENTER SECTION BAFFLE ATTACHMENT TOP SIDE ANGLE CRACKED. MAINTENANCE REPAIRED IAW SRM 51-42-00, 51-18-00, 51-23-00, 51-24-11, 51-31-00, 53-20-16 FIG 3 SHEET 2. REFER TO 409, 187527 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20041220001512004122000151NM 2004 12 20 AALA20041218 120041214A3350 LIGHT BOEING767 767323 1385205NM SEAT 36H DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21357AA 24038 DFW - EMERGENCY EXIT LIGHT AT SEAT 36H DAMAGED. REPAIRED EMERGENCY LIGHT AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20041220001522004122000152NM 2004 12 20 2004UALA01190 120041207A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 25L & STR 26L. INSTALLED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041220001532004122000153WP 2004 12 20 UPS04843598 120041119A53403758497U1 ATTACH FITTING DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 INSPECTION TYPE: C3, INTERCOSTAL FRAME ATTACH FITTING CRACKED AT STA 1140 LONG 35L. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-1-20D, 51-1-8 NDT-SPM06-10-01.001. 2L74 4F RT4A25 20041220001562004122000156EA 2004 12 20 COMA0460676 120041209A2460TH04F60 DIODE CNDAIRCL600 CL6002B19 1900309EA DC BUSS FAILED A COMAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO01916CA 7014 FLIGHT 5754 DC BUSS 2 FAILURE IN FLIGHT. REPLACED DIODE CR 18PA, OPERATIONAL TEST SATISFACTORY. 2L72 4F RTA21EA 20041220001572004122000157NM 2004 12 20 2004UALA01191 120041207A2913 PUMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE HYD SYSTEM FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29902UA 25002 B-ELECTRIC PUMP OVERHEAT LIGHT ILLUMINATED. FUNCTIONAL BENCH TEST FAILED IN THE SHOP. NUMEROUS PARTS REPLACED DURING OVERHAUL OF UNIT (BEARINGS, CYLINDER BLOCK, MATING RING, ETC.). 2L72 4F4 FRTA16WE E2GL 20041220001602004122000160NM 2004 12 20 QXEA200400871 120041204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RT FUSELAGE SKIN AT STATION X322 AND STRINGER 14 RT HAS AREA OF SURFACE DAMAGE WITH TWO PITS. REPAIRED IAW RD 8/4-53-382, HORIZON AIR EA 6-53-480 AND SRM 51-25-15-370-801. 2H72 4T RTA13NM 20041220001632004122000163NM 2004 12 20 SWAA043613 120041120A3350311500 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29448WN 33721 DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041220001652004122000165EU 2004 12 20 DHL3622004500 120041202A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DURING C-CHECK, N/R 3194, FWD CABIN COURIER AREA - FR 19L - FR 15L, LBL 30 SEAT TRACK CORRODED. REMOVED CORROSION AT FWD CABIN AREA SEAT TRACK FOUND OUT OF LIMITS AT LBL 30 FR 19L - 15L AS PER A-300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK FROM FRAME 15 TO FRAME 19 LBL 38 REF: A-300 SRM 51-10-40 AND A-300 SRM 51-30-00. TREATED AND PRIMED NEW PART AS REQUIRED PER A-300 SRM 51-40-11 AND A-300 SRM 51-40-12. APPLY TOP COAT PAINT POLY WHITE AS REQUIRED PER A-300 SRM 51-10-40. 2L72 4F RTA35EU 20041220001662004122000166EU 2004 12 20 MALA040775 120041012A5755 STRUCTURE BAC 146 AVRO146RJ85A1500097EU SPOILER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, LEFT O/B LIFT SPOILER DAMAGED. MAINTENANCE REPAIRED IAW EO A57013, REFER TO 409, 187573 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20041220001672004122000167WP 2004 12 20 AALA20041219 120041209A3350 LIGHT DOUG DC9 DC982 3022082WP SEAT 30D INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21480AA 49655 DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 30D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041220001702004122000170NM 2004 12 20 DL75K041095 120041213A2560MV10 MEGAPHONE BOEING757 757232 1384965NM CABIN DEFECTIVE A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27644DL 23998 AT CRUISE LOUD SQUEAL REPORTED BY F/A IN AFT CABIN. NOISE DETERMINED TO BE COMING FROM MEGAPHONE. REPLACED MEGAPHONE. 2L72 4F RTA2NM 20041220001712004122000171NM 2004 12 20 DL76S041104 120041214A2121732591A FAN BOEING767 767332 1382001NM E/E BAY COOLING FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27127DL 24077 ON DESCENT PASSING THRU APPROX 15,000 FEET COCKPIT CREW SMELLED ELECTRICAL FUMES. SHORTLY AFTER THE FWD EXHAUST EQUIP COOLING FAN C/B POPPED. CREW RAN SMOKE, FUMES, FIRE, ELECTRICAL CHECKLIST. FUMES SUBSIDED AFTER C/B POPPED. C/B AND WIRING CHECK GOOD, FAN MAKING A LOT OF NOISE. REPLACED FWD EXHAUST EQUIP COOLING FAN PER M/M. OPERATION CHECKS GOOD. 2L72 4F RTA1NM 20041220001722004122000172EU 2004 12 20 MALA040800 120041011A5753 BULKHEAD SAAB SF340 340B 7860101EU RT BEAVERTAIL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND RT FLAP BEAVERTAIL BULKHEAD CRACKED AT REAR SPAR MOUNT. MAINTENANCE REPAIRED IAW SRM 57-20-10. AIRCRAFT RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20041220001732004122000173EU 2004 12 20 MALA040808 120041011A5347 GALLEY TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND GALLEY TRACK CORRODED AT STA 284.0. MAINTENANCE REPLACED IAW SAAB SRM 50-40-27. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20041214001132004121400113NM 2004 12 14 UPS04243278 120040916A5520 SKIN PANEL BOEING727 72722C 138400FNM LT ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 INSPECTION TYPE: C, SURFACE CORROSION ON LT ELEVATOR LOWER SKIN AT BUTT JOINT BETWEEN 5TH AND 6TH ACCESS PANELS FROM OUTBOARD. CORROSION REMOVED IAW SRM 51-10-1. BLEND OUT AREA FOUND TO BE WITHIN LIMITS IAW SRM 55-20-1. AREA REPROTECTED IAW SRM 51-10-2. 2L73 4F A3WE 20041214001222004121400122WP 2004 12 14 AALA20041112 120041109A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW2159523 49915 RDU - EMERGENCY LIGHTS AT FORWARD OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK AT BF103 FOR EMERGENCY LIGHTS AT FORWARD OVERWING ESCAPE HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041214001292004121400129 2004 12 14 UPS04843449 420041109A2565 SLIDE DOUG DC8 DC873F 302199FWP GIRT BAR INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:N/A, DEPARTURE - ESCAPE SLIDE GIRT BAR WOULD NOT ATTACH TO THE FLOOR MOUNTS. DEFERRED PER MEL M290986. REMOVED AND REPLACED CONTAINER FOR EVAC SLIDE, OPS CKS GOOD. M290986 CLOSED. 2L74 4F RT4A25 20041214001312004121400131EU 2004 12 14 RAIA00411025 120041124A7997 WIRE JETAIRJETSTMJETSTM4101 1500501EU TEMP SWITCH CHAFED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03572HK 41091 PIT - RIGHT ENGINE HIGH OIL TEMP LIGHT ILLUMINATED. MAINTENANCE REPAIRED CHAFED WIRING TO RIGHT TEMP SWITCH. OPS CHECK GOOD. 2L72 4T RTA41NM 20041214001322004121400132NM 2004 12 14 QXEA200400740 120041104A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY MALFUNCTIONED A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09366PH 510 PDX - FLIGHT 2297 - ON FINAL APPROACH, THE CREW RECEIVED A MASTER WARNING AND THE SMOKE LIGHT CAME ON FOR 3 SECONDS, THEN WENT OFF AND STAYED OFF. MAINTENANCE CHECKED THE SECURITY OF AFT BAGGAGE SMOKE DETECTORS AND THE CONDITION AND SECURITY OF THE CONNECTIONS. NO DEFECTS WERE NOTED. THERE WERE NO VISIBLE SIGNS OR REPORTS OF SMELL OF SMOKE. BOTH DETECTORS WERE TESTED SEVERAL TIMES AND THE OPERATIONAL CHECK WAS GOOD ON EVERY ATTEMPT. AIRCRAFT WAS OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20041214001372004121400137CE 2004 12 14 DXTA200400441 120041106A28218975131 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP ENGINE UNKNOWN E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07855QS 258355 P107495 NUMBER 1 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF, ABORTED TAKEOFF BELOW 80 KTS. ACCOMP ENGINE RUNS AT LOW PWR SETTING THRU CRUISE, NO DEFECTS NOTED. REMOVED FUEL FILTER & INSTALLED A NEW P/N 897513-1 FILTER & PACKINGS. ACCOMP ENGINE RUN AT T/O PWR, NO FUEL LIGHT AND/OR LEAKS NOTED. ALL WORK ACCOMP AS PER THE TFE731 EM/M CHAP 73-21-02. 2L72 4F4 FRTA3EU E6WE 20041214001442004121400144WP 2004 12 14 UPS04843225 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3, WING LT OUTBOARD LEADING EDGE AT STA 778.250 APROX RIB CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20041214001452004121400145WP 2004 12 14 UPS04843227 120040909A57125769545505 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3 WING LEFT L/E RIB IS CRACKED AT STA 785. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20041214001492004121400149EU 2004 12 14 314041 120041107A26117239203507 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY FALSE INDICATIONA NSVAO OTHER N FALSE WARNING CRCRUISE 1 EA27242CJ 340B242 AVIONIC SMOKE LIGHT ILLUMINATE IN FLIGHT. 2L72 4T RTA52EU 20041214001542004121400154 2004 12 14 DXTA200400419 420041007A34607007549905 COMPUTER BRAERO1000 BAE1251000A 1500104EU NR 2 FMS FAILED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07535QS6499 259035 NR 2 FMS WENT BLANK AND A ELECTRICAL BURNING ODOR WAS NOTICED SHORTLY AFTERWARDS IN COCKPIT. REPLACED NR 2 FMS IAW HAWKER 1000 AMM CHAPTER 34-61-00, OPS CHECK GOOD IAW HAWKER 1000 AMM CHAPTER 34-61-00. 2L72 4F RTA3EU 20041214001552004121400155CE 2004 12 14 DXTA200400420 120041007A3246315381 WHEEL CESSNA750 750 2076810CE NLG VIBRATION E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07937QS592 7500137 DURING TAKEOFF ROLL SEVERE NOSE GEAR SHIMMY / VIBRATION RESULTED IN ABORTED T/O AT 65 KTS. VIBRATION WAS REDUCED, NOT ELIMINATED, WITH APPLICATION OF ELEVATOR BACK PRESSURE. REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSY WITH OVERHAUL ASSY IAW 750 M/M 32-41-01. 2L72 4J RTT00007WI 20041214001592004121400159NM 2004 12 14 UPS04442780 120040712A5347BAC15201567 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE: C, U/D- BS 540-580 RBL 27 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.060 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, SEAT TRACK REPAIRED AT BS 540 - BS 620 RBL 27 PER SRM 53-10-05 FIG 6. CIC APPLIED IAW EO M5100-2780E. 2L74 4F RTA20WE 20041214001652004121400165 2004 12 14 UPS04142816 420040729A2565 SWITCH AIRBUSA300 A300F4622R 3930360EU DOOR SLIDE INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01121UP 0806 MAIN ENTRY DOOR SLIDE WILL NOT ARM, REF M384898. REMOVED AND REPLACED FWD CARGO COMPT ENTRY DOOR SLIDE ARM SWITCH. SYS OPS CK NORMAL. 2L72 4F RTA35EU 20041214001682004121400168NM 2004 12 14 UPS04442755 120040713A5347 SEAT TRACK BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C U/D - BS 420 - 460 LBL 60 - 64 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK SECTION REPLACED AND INSTALLED AS PER SRM 51-10-01 PAGE 8 A AND 51-30-02. 2L74 4F RTA20WE 20041214001712004121400171NM 2004 12 14 UPS04442803 120040729A2612 FIRE WARNING BOEING747 747212B 1384886NM NR 3 ENGINE FALSE INDICATIONA IPXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01520UP 21943 FIRE INDICATION ON NR 3 ENGINE. EXECUTED FIRE IN FLIGHT SHUTDOWN. BOTH FIRE BOTTLE DISCHARGED. INITIALLY OBTAINED FIRE DETECTION LIGHT ON FWD PANEL COUPLED W/FAULT LIGHT ON DET PANEL. ENG FIRE TEMP SENSOR IN ORANGE, INCREASING EMERGENCY RED FIRE HANDLE ILLUMINATED. T/S PER WDM 26-11-03 PG A1. CLEANED UP CONN DM219. NR 3 ENG FIRE INDICATION BACK TO NORMAL. REMOVED AND REPLACED NR 3 ENG BOTH FIRE BOTTLE & SQUIB PER MM 26-21-03. A/C OKAY FOR SERVICE. 2L74 4F A20WE 20041214001802004121400180SO 2004 12 14 SWIA200414145 120041005A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0715732 120195 FR 44 TO FR 47 RIGHT OUTBOARD SIDE ANGLE IS CORRODED ON INBOARD AND OUTBOARD SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20041214001832004121400183NM 2004 12 14 SWAA043549 120041206A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 480, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041214001862004121400186 2004 12 14 UPS04242710 420040712A344065249203 BRAKE ASSY BOEING727 72725C 138400HNM NR 2 INTERMITTENT A IPXAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01951UP 19850 AIR TURNBACK TO PHX DUE TO WHEEL WELL FIRE INDICATION. INSPECTED WHEEL WELL FIRE LOOPS AND WIRING, PERFORMED RESISTANCE CHECK OF FIRE LOOPS, ALL OK. FOUND NR 2 BRAKE GRABBING. REMOVED AND REPLACED BRAKE ASSY. REPLACED FIRE AND OVERHEAT CONTROL BOX PRECAUTIONARY. 2L73 4F A3WE 20041214001912004121400191WP 2004 12 14 UPS04842709 120040613A5313S2593956 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 INSPECTION TYPE: C-3, FWD PIT L31R HAS CORROSION AT STA 85 AROUND FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-9-0. FAB REPAIR ANGLE IAW DC8 SRM 51-2-1 TR51-130, REMOVED FASTENERS FOR ACCESS IAW DC8 SRM 51-1-2D & 51-1-21. ALODINED & PRIMED. INSTALLED REPAIR ANGLE & FASTENERS THAT WERE REMOVED FOR ACCESS IAW DC8 SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 20041214001982004121400198EU 2004 12 14 MALA040661 120041004A26117211121100 SMOKE DETECTOR SAAB SF340 340B 7860101EU E/E BAY MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15412XJ 340B412 AVIONICS RACK SMOKE DETECTION SYSTEM ON TAKEOFF ROLL AVIONICS SMOKE LIGHT ILLUMINATED. ABORTED TAKEOFF AT ABOUT 100 KTS, NO SMOKE NOTICED. MAINTENANCE INSPECTED TIRES AND BRAKES AFTER REJECTED TAKEOFF IAW FAXED AMM 05-50-00-6, NO SIDS NOTED. CONFIRMED AVIONICS RACK SMOKE DETECTOR LIGHT. MAINTENANCE REMOVED AND REPLACED DETECTOR. REMOVED FROM DMR, REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. TESTED SMOKE DETECTOR, OPS CKS GOOD. P/N 72-111211-00, S/N OFF-A5306, S/N ON-A3732. MXC NOTIFIED. 2L72 4T RTA52EU 20041214002052004121400205NM 2004 12 14 0401655809 120040922A2820316N310012 LINE BOEING757 757351 1384991NM PWA 2037 PW2037 NE RT WING CHAFED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01589NW5223 32989 THE SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA2NM E17NE 20041215000032004121500003WP 2004 12 15 04FDEA03386 120041207A5530AMC73051 HINGE BRACKET DOUG MD10 MD1010F 3022112WP ZONE 300 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 VERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE FITTING BENT AND GOUGED. REMOVED AND REPLACED UPPER RUDDER HINGE SUPPORT BRACKET IAW MD10-10 MM 55-53-01-2 AND EA 8- 5530-83844, STABILIZER- VERTICAL STABILIZER RUDDER HINGE BRACKET, REPAIR. REFERENCE NON-ROUTINE N01059. 2L73 4F RTA22WE 20041215000122004121500012NM 2004 12 15 USAA040731 120041011A5310 SHEAR TIE BOEING757 757225 1384959NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU63825 22193 SHEAR TIE, 1.5 INCHES SQUARE, CORROSION, STA 1300, STRINGER 27, 28L. FABRICATED NEW SHEAR TIE AND REMOVED LIGHT SURFACE CORROSION FROM ASSOCIATED PARTS IAW SRM 51-10-00. 2L72 4F4 FRTA2NM E21EU 20041215000332004121500033EU 2004 12 15 ASOA04839 120041005A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, SEVERAL AREAS OF THE LT SEAT TRACK BETWEEN FRAMES 36 AND 39 WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF THE LT SEAT TRACK IAW SRM 51-25-04. 2H72 4T4 TRTA53EU E20NE 20041215000372004121500037EU 2004 12 15 ASOA04843 120041027A2120 ODOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27632AS 338 ON APPROACH, THE CAPTAIN AND FIRST OFFICER NOTICED FUMES SIMILAR TO ELECTRICAL SMOKE OR BURNING PLASTIC. THERE WERE NO WARNINGS OR VISUAL INDICATIONS. THIS SMELL PERSISTED FOR ABOUT THIRTY SECONDS AND WAS NEVER NOTICED IN THE CABIN AREA. AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS OR EVIDENCE OF SMOKE OR FUMES. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA53EU E20NE 20041215000522004121500052NM 2004 12 15 ASAA0410429 120041016A531165622061 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE- CRACK IN FASTENER HOLE IN FRAME. REMOVED AND REPLACED FRAME. 2L72 4F4 FRTA16WE E2EA 20041215000712004121500071WP 2004 12 15 ASAA0480497 120040924A51015913528 SEALANT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE IDLER HINGE MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK-LOG PG 5784367, SEALANT MISSING LT IDLER HINGE. NO ROTATION NOTED, APPLIED SEALANT TO BOTH ENDS OF BOLT IAW EA 5750-01098. 2L72 4F4 FRTA6WE E9NE 20041215000742004121500074WP 2004 12 15 ASAA0480500 120040924A534799366401 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC- C-CHECK, CABIN FLOOR PANEL AT STA 886 TO 927 IS DAMAGED AT LOWER EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2L72 4F4 FRTA6WE E9NE 20041215000782004121500078WP 2004 12 15 ASAA0480520 120040928A57539935942502 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK, RT WING T/E IB FLAP DENTED AT LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-03, FIG 7. 2L72 4F4 FRTA6WE E9NE 20041215000802004121500080WP 2004 12 15 ASAA0480524 120040928A21005924037517 DIVERTER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE HEAT EXCHANGER CRAZED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, LT PRIMARY HEAT EXCHANGER RAM AIR DIVERTER WORN IN FORWARD LOWER CORNER STOP DRILLED CRACK, FPI FOR CRACK CONTAINMENT AND WELDED CRACK IAW EA 5300-01053 AND EA 10576. 2L72 4F4 FRTA6WE E9NE 20041215000832004121500083WP 2004 12 15 ASAA0480528 120041002A53135936027515 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, AFT PIT STA 1087-1098, LONG 29L HOLES HAVE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 53-02, FIG 19. 2L72 4F4 FRTA6WE E9NE 20041215000932004121500093NM 2004 12 15 ASAA0480538 120041020A523059101413 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE MID CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - C-CHECK, MID CARGO DOOR UPPER HAS NUMEROUS DENTS, FWD DENTS, X=.036, D=.800, 13 INCHES AFT OF FORWARD DENT X=.024, D=.800 AND IS OVER PREVIOUS REPAIR. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND STRAP DOUBLERS IAW SRM 53-04, FIG 12E. 2L72 4F4 FRT E9NE 20041215001002004121500100WP 2004 12 15 ASAA0480505 120040924A5531991196213 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D17A 52049NE VERTICAL STAB GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, VERTICAL STABILIZER PANEL 6308C, CUT OUT JAMB GOUGED AROUND LAND ORDERED AND INSTALLED NEW FRAME IAW SRM 51-30-2. 2L72 4F4 FRTA6WE E2EA 20041215001152004121500115NM 2004 12 15 ASAA0410435 120041019A523065479522 SKIN BOEING747 747200 1384847NM PWA JT8 JT8D17 52049NE AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - AFT CARGO PIT DOOR EDGE DENTED A=1.0, Y=0.120, A/Y=8.3. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM. 2L74 4F4 FRTA20WE E2EA 20041215001162004121500116NM 2004 12 15 ASAA0410462 120040922A571365671482 FITTING BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE STRINGER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02740AS 22578 ANC - FOUND .5 INCH CRACK IN THE NR 5 STRINGER FITTING AT WBL 71.24. CONFIRMED WITH NEGATIVE PRESSURE CHECK, BLOW BACK CHECK AND CRACK CONFIRMED WITH HFEC IAW AMM 51-00-00. FITTED AND DRILLED NEW FITTING, REAMED MOUNTING HOLES TO SIZE. INSTALLED RT WING SPLICE IAW EA 5710-01111 AND EA 5710-01110. 2L72 4F4 F A16WE E2EA 20041215001212004121500121NM 2004 12 15 ASAA0410478 120041104A5414658537816 SKIN BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE RT COWL WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - RT COWL INNER LIP SKIN WORN AT 8 O`CLOCK POSITION. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001272004121500127NM 2004 12 15 ASAA0410485 120041105A53106547956522 DOOR FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - AFT CARGO DOOR CUTOUT UPPER CHORD DENTED. REPLACED CHORD. 2L72 4F4 FRTA16WE E2EA 20041215001382004121500138NM 2004 12 15 ASAA0410437 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001472004121500147NM 2004 12 15 ASAA0410446 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001482004121500148NM 2004 12 15 ASAA0410447 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001492004121500149NM 2004 12 15 ASAA0410430 120041020A5330654577872 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001642004121500164NM 2004 12 15 ASA0440175 120041001A534065516989 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CRACKED STRINGER CLIP AT FASTENER. REMOVED AND REPLACED STRINGER SPLICE AND CLIP. 2L72 4F4 FRTA16WE E21EU 20041220000012004122000001NM 2004 12 20 SWAA043615 120041213A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 933, STRINGER 22L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041220000042004122000004NM 2004 12 20 SWAA043618 120041213A531165C22908 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPT FRAME AT BS 500B, BETWEEN LBL 6 AND RBL 6, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041220000062004122000006NM 2004 12 20 2004UALA00817 120040831A5744 FITTING BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 RT WING OUTBOARD AILERON 2ND FROM OUTBD HINGE FITTING CRACKED THRU LWR AFT FASTENER LOWER AREA. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FITTING. 2L74 4F4 FRTA20WE E24NE 20041220000132004122000013NM 2004 12 20 QXEA200400875 120041211A5710 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT WING, BETWEEN STATION YW117.5-136.3. REPAIRED IAW RD 8/4-57-399 AND HORIZON AIR EA 6-57-268. 2H72 4T RTA13NM 20041220000212004122000021EU 2004 12 20 MALA040798 120041030A2520 SUPPORT BAC 146 AVRO146RJ85A1500097EU SEAT BACK CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND PAX SEAT BACK SUPPORTS CRACKED ON SEATS 6B, 7B, 8B, 11A, B, 14A, B, 9F, 10F, 12F & 13A. MAINTENANCE REPLACED AFFECTED SEATS, REPAIRED IAW EO A25039, OR REPLACED WITH SERVICABLE. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20041220000532004122000053NM 2004 12 20 SWAA043626 120041214A57126545445 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND LT AND RT WINGS LOWER RIB CHORDS AT WBL 135.5, CRACKED. REPAIRED RIB CHORDS PER ER. 2L72 4F RTA16WE 20041220000552004122000055 2004 12 20 SWAA043628 420041214A25656949956 CABLE BOEING737 7373A4 1384585NM GIRT BAR MISROUTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C1 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE GIRT BAR CABLES MISROUTED. REROUTED R2 AND L2 DOOR EVAC SLIDE GIRT BAR CABLES PER MM. 2L72 4F RTA16WE 20041220000602004122000060EU 2004 12 20 MALA040804 120041011A5210 GUIDE SAAB SF340 340B 7860101EU PAX DOOR ROLLER CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PAX ENTRY DOOR I/B ROLLER GUIDE CORRODED. MAINTENANCE REPAIRED IAW SAAB AMM 52-60-05-2. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20041220000662004122000066SO 2004 12 20 RAIA00412011 120041209A7830 WARNING SYSTEM EMB 145 EMB145LR 3260212SO NR 1 TR FALSE ACTIVATIONA RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03816HK 145055 PHL - ENGINE NR 1 THRUST REVERSER DISAGREE EICAS MESSAGE (NR 2 T/R DEFERRED) AND SPOILER FAIL. MAINTENANCE PERFORMED OPS CHECK OF NR 2 THRUST REVERSER AND GROUND TESTED SPOILERS. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041220000732004122000073WP 2004 12 20 04FDEA03171 120041119A5753ARC0264502 SKIN DOUG DC10 DC1030 3023501WP RT INBD FLAP CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25320FE 47835 RIGHT INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE HAS A LARGE SKIN SECTION OIL CANNING. REPLACED SKIN PNL ASSY IAW DC-10 SRM 51-31-01 AT MAE ON N/R N01147. 2L73 4F A22WE 20041220000842004122000084NM 2004 12 20 SWAA043596 120041121A53306545774 SKIN BOEING737 7373A4 1384585NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SPV, FOUND FUSELAGE SKIN DOUBLER UNDER DORSAL FIN BETWEEN BS 860 AND BS 880, WORN. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041220000872004122000087NM 2004 12 20 04FDEA03287 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001002004122000100NM 2004 12 20 04FDEA03294 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-78056. 2L73 4F RTA22WE 20041220001012004122000101NM 2004 12 20 04FDEA03403 120041209A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-07 PAGES 403 TO 404. 2L73 4F RTA22WE 20041220001212004122000121NM 2004 12 20 04FDEA03318 120041202A5313 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER ACCESSORY COMPARTMENT FORWARD OF DOOR AT LONGERON R49 HARDWARE ON LONGERON SPLICE FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041220001302004122000130WP 2004 12 20 WX0400063 120041114A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19891GA 49423 LAS - MAINTENANCE REPORTED ONE AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041220001372004122000137EU 2004 12 20 MALA040799 120041011A5712 RIB SAAB SF340 340B 7860101EU WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND 611BR HAS 2 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. AIRCRAFT RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20041220001392004122000139NM 2004 12 20 04FDEA03304 120041201A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO COMPT - LONGERON 45 LT FOUND CRACKED AT STA 5-111 TO 5-121. REPAIR CARRIED OUT AT STA 5-111 TO 5-121 LONGERON 45 LT AS PER SRM 53-10-00 VOL I FIG 1. 2L73 4F RTA22WE 20041220001402004122000140NM 2004 12 20 04FDEA03305 120041201A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND INBOARD FLAP OUTBOARD FITTING OUTBOARD STRAP PIVOT HOLE SURROUNDING AREA OF HOLE SURFACES FOUND PITTING CORROSION OUT OF LIMIT. LEFT HAND INBOARD FLAP OUTBOARD FITTING OUTBOARD STRAP REPLACED BY NEW STRAP AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041220001472004122000147NM 2004 12 20 04FDEA03278 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001542004122000154WP 2004 12 20 ABXA040397 120041111A53119911839243 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 AFT ASSY CANTED FRAME 1121 CRACKED BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159. 2L72 4F A6WE 20041220001682004122000168EU 2004 12 20 MALA040784 120041024A5755 SEAL BAC 146 AVRO146RJ85A1500097EU SPOILER WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING MIDDLE LIFT SPOILER SEAL IS WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20041220001742004122000174EU 2004 12 20 RAIA00412012 120041210A3060 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU RT PROPELLER ILLUMINATED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03559HK 41075 RT PROP LIGHT COMES ON 70 SECONDS AFTER SWITCHING LONG CYCLE DURING FIRST FLIGHT CHECKS. MAINTENANCE DEFERRED PER J41 MEL 30-2 CAT C, RT PROP HEAT. SUBSEQUENTLY MAINTENANCE CLEARED DEFERRAL BY REMOVING AND REPLACING NR 2 PROP. 2L72 4T RTA41NM 20041220001752004122000175SO 2004 12 20 RAIA00412017 120041212A27607013348940 DAU EMB 145 EMB145LR 3260212SO E/E BAY MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03816HK110261002 145055 STL - SPOILER FAILED. MAINTENANCE REMOVED AND REPLACED DATA ACQUISITION UNIT. 2L72 4T RTT00011AT 20041220001762004122000176NM 2004 12 20 04FDEA03425 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, FLOOR STRUCTURE HAT SECTION CORRODED AT STA 1910 TO STA 2007, RBL 57. REMOVED FROM STA 1887 TO STA 2007, RBL 57 & REPLACED AS PER SRM 51-31-01 VOL II. FOR WORK DETAILS, REFER TO SNRM N3008. 2L73 4F RTA22WE 20041220001782004122000178SO 2004 12 20 WX0400062 120041211A3350 BULB PIPER PA22 PA22 7102202SO EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19945A 22254 LAS - MAINTENANCE REPORTED EMERGENCY FLOOR LIGHTS AT ROW 11 AND 17 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1H71 3O 1A6 20041220001802004122000180WP 2004 12 20 UPS04843596 120041118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 INSPECTION TYPE: C3, LONG 15R CRACKED AT FRAME ATTACHMENT, STA 1755. CUT OUT LONG SECTION FROM STA 1750-1760, REMOVED END FITTING AT STA 1760 & SHEAR TIE AT 1755. FAB LONG SECTION FROM S1616757 EXTRUSION, & TWO SPLICE STRAPS FROM SHT7075T6/.080 REF SRM 53-2-2 FIG 10, 51-1-8, 53-5-3 ASSEMBLED REPAIR & REINSTALLED PARTS & REPAIR SPLICE FITTING REF SRM 53-2-2 FIG 10, 51-1-20D, 51-1-8, DPS4.707, NDT-SPM06-10-01.001. 2L74 4F RT4A25 20041220001832004122000183SO 2004 12 20 SIMA200431509 120041102A532014525381033 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK 145371 DURING AN IMBV INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR PARTS AND CLEANED THE AREA. FABRICATED A REPAIR DOUBLER, FILLER, 2 SHIMS, AND PLATE. REPAIR DONE IAW SRM. (SW21200501189) 2L72 4F4 FRTT00011ATTE6CH 20041220001852004122000185NE 2004 12 20 A6WA200440193 220041123A7320 FUEL BOWL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE CONTAMINATED A A6WAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 GL31432AW 7257 ON APPROACH, RT ENG RED OIL PRESSURE WARNING MESSAGE. ENGINE FLAMED OUT C/W QRH, ENG WINDMILLED FOR 3 MINUTES. FOUND WATER IN RT ENG FUEL BOWL. ALL INSPECTION AND CHECKS GOOD EXCEPT FOR WATER IN BOWL IAW 769-10-00 AND 73-11-03. 2L72 4F4 FRTA21EA E15NE 20041220001862004122000186EA 2004 12 20 A6WA200440194 120041123A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31406AW 7402 ON APPROACH TO LANDING FLAPS FAILED AT 0 DEGREES UPON FLAP SELECTION TO 8 DEGREES. PLACED ON 72 FLAP WATCH C/W AWAC SUPPLEMENT 01-05. RESET FLAPS. NO DAMAGE NOTED. 2L72 4F4 FRTA21EA E15NE 20041220001952004122000195EA 2004 12 20 ASOA04898 120041113A5210601R3198057 STEP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27701EV 10020 DURING HANGER MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041220001972004122000197EA 2004 12 20 ASOA04910 120041117A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AVIONIC BAY DOORCRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7208 7207 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE BASE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20041220001982004122000198EA 2004 12 20 ASOA04912 120041117A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72-FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72- FS 589.00 IAW EO 600-53-0095. 2L72 4F4 FRTA21EA E15NE 20041220002022004122000202EA 2004 12 20 ASOA04944 120041126A14204871907191 CONNECTOR BRUCE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT DIRTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO27909EV 7658 DURING HANGAR MAINTENANCE, THE LT INTERIOR EMERGENCY EXIT LIGHT FORWARD OF THE WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE LT INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY FORWARD OF THE WING AND CLEANED THE CONNECTORS; THEN REINSTALLED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041220002042004122000204EU 2004 12 20 ASOA04868 120041018A5410 STRUCTURE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE LT AND RT UPPER EDGING ON THE LT LOWER NACELLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT UPPER EDGING ON THE LOWER NACELLE IAW SRM 51-25-03. 2H72 4T4 TRTA53EU E20NE 20041220002052004122000205EA 2004 12 20 ASOA04869 120041101A3350110049 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHTSINOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS5363 73 7421 DURING HANGAR MAINTENANCE, THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT FOR THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041220002082004122000208NM 2004 12 20 ASA0440200 120041029A53116546526 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041220002102004122000210WP 2004 12 20 GTIA040827 120041024A2910 LINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE HYD SYSTEM RUPTURED A GTIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23829NK 49931 DURING CLIMB, LT HYDRAULIC QTY WENT TO 3 PRESS 0, LT HYD PRESSURE LOW ANNUN, DID QRH CHK LIST. FOUND LT ELEVATOR POWER CONTROL HYDRAULIC LINE RUPTURED NEAR UNION AT THE CONTROL VALVE, REMOVED AND REPLACED RUPTURED LINE. AIRCARFT TAIL SWAP WITH N814NK. 2L72 4F4 F A6WE E2EA 20041220002112004122000211WP 2004 12 20 GTIA040845 120041112A3260 SENSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE MLG MALFUNCTIONED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23826NK 49391 LP NR 256794-1; AFTER TAKEOFF, LT GEAR UNSAFE LIGHT (RED) REMAINED ON, FOLLOWED QRH, WHEN RT ENGINE HYDRAULIC PUMP WAS TURNED OFF DOOR UNSAFE LIGHT CAME ON, TURNED PUMP BACK ON FOR DURATION OF FLIGHT. INSPECTED LT UP GEAR SENSOR AIR GAP, FOUND TO BE TOO MUCH, ADJUSTED SENSOR AIR GAP, CHECKED SENSOR PERF. PROX BITE CHECK NEAR/FAR SENSOR AND CARD OK, NO FAULTS NOTED. 2L72 4F4 FRTA6WE E9NE 20041220002132004122000213NM 2004 12 20 ASA0440206 120041029A53116546596 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041220002142004122000214NM 2004 12 20 ASA0440208 120041029A531165C25229 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041220002152004122000215NM 2004 12 20 ASA0440216 120041029A53116546558 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041220002162004122000216NM 2004 12 20 ASA0440220 120041029A5330 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 GOUGES IN SKIN. BLENDED GOUGED SKIN, AND INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E21EU 20041220002172004122000217NM 2004 12 20 ASA0440223 120041029A533065C3236511 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAO OTHER O OTHER NRNOT REPORTED 1 NM02762AS 25099 DOUBLE HOLE DRILLED IN SKIN AND BEARSTRAP. REAMED UP HOLE AND INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E21EU 20041220002192004122000219NE 2004 12 20 GTIA040840 220041103A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 2 BIRD INGESTION A GTIAO OTHER C F.O.D. NRNOT REPORTED 1 GL23821NK 49508 LP NR 0252843; MULTIPLE BIRD STRIKES ON APPROACH TO LGA, NR 2 LT EGT HIGH. REMOVED AND REPLACED NR 2 ENGINE. 2L72 4F4 F A6WE E9NE 20041220002202004122000220NM 2004 12 20 ASA0440203 120041029A53116546523 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000022004122100002SO 2004 12 21 SIMA200432208 120041107A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR8514 145368 IMBV - LT OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501181) 2L72 4F4 FRTT00011ATTE6CH 20041221000032004122100003SO 2004 12 21 SIMA200431505 120041106A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR 145368 DURING AN IMBV INSPECTION, A PREVIOUS AIR ON THE LT BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR AT FRAME 20. FABRICATED AN EXTERNAL ANGLE, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (SW21200501161) 2L72 4F4 FRTT00011ATTE6CH 20041221000062004122100006SO 2004 12 21 SIMA200430302 120040823A532014521718003 BRACKET EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FLOOR SUPPORT CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21830AE 145615 DURING AN MBV INSPECTION, THE FLOOR SUPPORT BRACKET AT FRAME 20 WAS FOUND CORRODED THROUGH THE AFT END. MAINTENANCE REPLACED FLOOR SUPPORT BRACKET IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159) 2L72 4F4 FRTT00011ATTE6CH 20041221000072004122100007SO 2004 12 21 SIMA200429814 120041008A532014525480003 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CARGO BAY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED CARGO DOOR CUTOUT LOWER SILL. INSTALLED NEW SILL IAW SRM. (SW2120050115500) 2L72 4F4 FRTT00011ATTE6CH 20041221000082004122100008EA 2004 12 21 A6WA200440207 120041214A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 RT FS 621 FLOOR SUPPORT ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20041221000102004122100010SO 2004 12 21 SIMA200429804 120041015A53201451721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21626AE 145117 DURING AN MBV INSPECTION, THE FORWARD DIGITAL AT FRAME 16 WAS FOUND CORRODED. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW21200501190) 2L72 4T4 FRTT00011ATTE6CH 20041221000112004122100011EU 2004 12 21 O3X004129241 120041202A3260622800200 DOWNLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP MCAULY4HFR344HFR34C653 NE NLG WW OUT OF RIG A O3XAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO03924AE 76 924 AIRCRAFT WAS ON APPROACH, THE GEAR WAS SELECTED DOWN. THE MAIN GEARS INDICATED DOWN AND LOCKED. NOSE LANDING GEAR INDICATE IN TRANSIT. THE GEAR WAS CYCLED AND THE NOSE LANDING GEAR TRANSIT LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO AIRPORT, DECLARED AN EMERGENCY. THE NOSE UNSAFE LIGHT REMAINED ON. DURING TOUCHDOWN THE NOSE (IN TRANSIT) LIGHT EXTINGUISHED AND THE GREEN (DOWN LOCKED) LIGHT ILLUMINATED. THE AIRCRAFT WAS FERRIED FOR INSPECTION. ADJUSTED AND RIGGED NOSE LANDING GEAR DOWNLOCK SWITCH ASSEMBLY. PERFORMED GEAR SWING AND NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20041221000132004122100013NM 2004 12 21 ASA0440207 120041029A53116546596 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000142004122100014WP 2004 12 21 GTIA040853 120041125A2611 SMOKE DETECTOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT LAVATORY INACTIVE A GTIAO OTHER P NO WARNING INDICATION CRCRUISE 1 GL23804NK 49104 LP NR 273191-1; RT LAV SMOKE DETECTOR DID NOT ACTIVATE WHEN PAX WAS SMOKING IN AIRCRAFT LAV. OPS TESTED SMOKE DETECTOR, NO FAULTS WERE NOTED. 2L72 4F4 F A6WE E9NE 20041221000152004122100015NM 2004 12 21 ASA0440213 120041029A53116546552 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000162004122100016NM 2004 12 21 ASA0440209 120041029A531165C3295 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A K NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000182004122100018WP 2004 12 21 GTIA040851 120041101A5330 SKIN DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE FUSELAGE CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23810NK 48015 2 INCH CRACK ABOVE FWD CARGO DOOR, CLASS II REPAIR. REMOVED EXISTING REPAIR DOUBLER, CUTOUT SKIN SECTION BETWEEN STA 351-389 AND BETWEEN L16R AND 18R (14 INCH BY 18 INCH), FABRICATED NEW SKIN FROM 2024T3-0.50, FABRICATED FINGER DOUBLER, LOCATED AND DRILLED DOUBLER, TREATED, PRIMED AND INSTALLED DOUBLER AND SKIN REPAIR. 2L72 4F4 F A6WE E9NE 20041221000202004122100020WP 2004 12 21 GTIA040847 120041116A5280 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE LT MLG DOOR CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23804NK 49104 LP NR 0167013; LT MAIN GEAR DOOR SKIN CRACKED ABOVE AND BELOW SKIN PLATE. UNSCHEDULED CHANGE OF AIRCRAFT EN ROUTE. PERFORMED REPAIR AND INSTALLED DOUBLER. 2L72 4F4 F A6WE E9NE 20041221000222004122100022NM 2004 12 21 ASA0440199 120041029A53116546526 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000242004122100024NM 2004 12 21 ASA0440204 120041029A53116546593 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000252004122100025NM 2004 12 21 ASA0440211 120041029A53116546548 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000262004122100026NE 2004 12 21 GTIA040852 220041112A7261 STUD DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE OIL FILTER CAP BACKED OUT A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 LP NR 0126074-1; LT OIL PRESSURE LOW LIGHT CAME ON WITH OIL QUANTITY DROPPING AND OIL PRESSURE DROPPING, SHUT DOWN NR 1 ENGINE. FOUND 2 FWD MOUNTING STUDS FOR OIL FILTER CAP LOOSE AND BACKED OUT, INSTALLED HELICOIL THREADED INSERTS AND RE-INSTALLED STUDS, NO LEAKS NOTED. 2L72 4F4 F A6WE E9NE 20041221000272004122100027NM 2004 12 21 ASA0440210 120041029A531165C32395 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000282004122100028WP 2004 12 21 GTIA040843 120041129A5310 DOOR FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT LOWER CARGO COMPARTMENT LOWER OB JAMB BEAM HAS CORROSION, STA 1155 TO STA 1211. REMOVED RIVNUTS TO CLEAN CORROSION ON JAMB BEAM, REMOVED FWD AND AFT SCUFF PLATES, REMOVED DOOR STOPS AT STA 1174 AND 1193, DOR JAMB BEAM WAS FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER AND TRIPLER, OK TO TREAT, PRIME AND TOPCOAT, INSTALLED REPAIR DOUBLER AND TRIPLER, INSTALLED FWD AND AFT DOOR STOPS AND SCUFF PLATES. 2L72 4F4 FRTA6WE E9NE 20041221000292004122100029EA 2004 12 21 A6WA200440212 120041214A5330 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 LT FS 484.00 AT LBL 36 ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20041221000302004122100030NM 2004 12 21 ASA0440214 120041029A53116546555 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000312004122100031NM 2004 12 21 ASAA0440218 120041029A531365622082 SPLICE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU STRINGER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 DAMAGED STRINGER SPLICE. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E21EU 20041221000342004122100034NM 2004 12 21 ASA0440221 120041029A533065C3236511 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 CORROSION ON INNER SKIN FORWARD OF AFT CARGO DOOR. REMOVED DAMAGE, INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E21EU 20041221000362004122100036NM 2004 12 21 USAA040891 120041110A5710 STIFFENER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT- Q6 - VERTICAL STIFFENER, 1.2500 INCH CRACK, AT RBBL 6.15, STA 663.75. REPLACED VERTICAL STIFFENER IAW EA 79313 AND EO 5704V245 (RAFT). 2L72 4F4 FRTA16WE E21EU 20041221000372004122100037WP 2004 12 21 AMTA200401439 120041124A5310 STRUCTURE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11161AT 1219 COMPLY WITH ERAL10-53R-5766, LBL16/RBL 16, LONGERON FS 1023 TO FS 1083, CORROSION REPAIR. COMPLIED WITH ERA L10-53R-5766 AS REQUIRED. 2L73 4F4 F A23WE E12EU 20041221000392004122100039NM 2004 12 21 USAA040939 120041119A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US 24557 PIT - Q1 -FRAME, 1 INCH CRACK, RT STA 601 BELOW S17R, FRAME TO FLOORBEAM ATTACH POINT. INSTALLLED REPAIR ANGLE IAW EA 79352. 2L72 4F4 FRTA16WE E21EU 20041221000452004122100045NM 2004 12 21 AMTA200401446 120041130A3397 WIRE HARNESS BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT FAILED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11526AT 30735 FOUND EGRESS LIGHT HARNESS TO BE BAD. REPLACED HARNESS, OPS CHECK NORMAL. 2L72 4F4 FRTA2NM E12EU 20041221000472004122100047WP 2004 12 21 AMTA200401464 120041202A3350 POWERPACK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE EMERGENCY LIGHT DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11162AT 1220 R3 AND R4 EXTERIOR EMERGENCY LIGHT SHUT OFF WITHIN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK. IAW MM 33-51-03. OK FOR SERVICE. 2L73 4F4 F A23WE E12EU 20041221000492004122100049CE 2004 12 21 1013041 120041013A2130241420027603 CONTROL MODULE LEAR 25 25B 5170511CE GE CJ610 CJ6101 30006NE CABIN PRESSURE MALFUNCTIONED E POSAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA0367HB 9188 189 ON A FLIGHT, THE FLIGHT CREW NOTICED THAT THE PRESSURIZATION SYSTEM WAS NOT INCREASING CABIN PRESSURE AT A RATE TYPICAL TO NORMAL AIRCRAFT OPERATION. AT 17,000 FT, WITH A CABIN ALTITUDE LOWER THAN THEY WERE USE TO SEEING, THE FLIGHT CREW DECIDED TO RETURN, LANDED WITHOUT INCIDENT. PRESSURIZATION CONTROL MODULE SUSPECTED TO BE FAULTY. 2L72 4J4 J A10CE 1E16 20041221000572004122100057EA 2004 12 21 A6WA200440200 120041209A2750 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT AND LT OUT OF RIG A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31414ZW 7586 FLAPS FAIL AT 20 DEGREES. 49700 LBS. LANDING WEIGHT LIGHT BREAKING. 5 MAX BTMS READING, LIGHT TOUCHDOWN. FOUND LT AND RT BRAKE POSITION SENSOR UNITS (BPSU) BOTH OUT OF RIG. RIGGED LT AND RT BPSU`S REF AMM, FLAPS OPS GOOD. 2L72 4F4 FRTA21EA E15NE 20041221000602004122100060WP 2004 12 21 GTIA040841 120041004A5347 SEAT TRACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 PASSENGER SEAT TRACK EXFOLIATED AT FS 1058, LT OB AND 1250 LT IB. CUT AND REMOVED DAMAGED SEAT TRACK, FABBED NEW SEAT TRACK AND SPLICE, TREAT, PRIME AND TOPCOAT SEAT TRACK AND INSTALLED. 2L72 4F4 F A6WE E9NE 20041221000612004122100061EU 2004 12 21 KBM2004F00237 120041009A5320 STUD SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL FUSELAGE BROKEN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 BROKEN ALUMEC CONNECTION STUD. REMOVED AND REPLACED. 1G71 3U3 U H9EU E4CE 20041221000622004122100062WP 2004 12 21 GTIA040839 120040930A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 EXTERNAL REPAIR AT STA 1165, LONGERON 18L TO 20L REQUIRES REPLACEMENT. REMOVED EXTERNAL REPAIR DOUBLER, STRIPPED SURROUNDING SKIN IAW SRM 51-10-3, FABRICATED EXTERNAL REPAIR DOUBLER FROM 2024-T3-0.025. OK TO TREAT AND PRIME REPAIR PARTS AND AREA, INSTALLED REPAIR DOUBLER AND FINGER DOUBLER. 2L72 4F4 F A6WE E9NE 20041221000632004122100063NM 2004 12 21 ASA0440222 120041029A533065C3236511 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 CORRODED INNER SKIN AFT OF AFT CARGO DOOR. REMOVED CORROSION AND INSTALLED DOUBLER. 2L72 4F4 FRTA16WE E21EU 20041221000642004122100064SO 2004 12 21 SIMA200432211 120041105A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK8574 145371 THE GALLEY AREA FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE GALLEY AREA FWD DIGITAL. INSTALLED THE NEW DIGITAL IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221000662004122100066NM 2004 12 21 ASA0440227 120041101A533065C3393239 SKIN BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU LT MLG CUTOUT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 CORROSION ON LOWER INNER CHORD OF LT MLG CUTOUT. REMOVED AND REPLACED LOWER CHORD. 2L72 4F4 FRTA16WE E21EU 20041221000672004122100067NM 2004 12 21 USAA040889 120041025A5315 FLOORBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE MISMANUFACTURED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19516AU52361 23702 PIT-Q5- FLOORBEAM, INCORRECT MATERIAL FROM MFG. FLOORBEAM UPPER CHORD REMOVED AND REPLACED IAW EA 68822A, FLOOR STA 328. 2L72 4F4 FRTA16WE E21EU 20041221000682004122100068EU 2004 12 21 ASOA04926 120041102A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE UPPER FLANGE OF FLOORBEAM 41 BETWEEN STRINGERS 17R AND 21R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORODED FLOORBEAM IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041215000222004121500022EU 2004 12 15 A6WA200460055 120041111A21501344D000002 ACM BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 2 MALFUNCTIONED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31606AW2628326283 E2033 NR PACK TEMP IS UNCONTROLLABLE IN EITHER MANUAL OR AUTO WHEN USING APU AIR. WILL RUN FULL HOT AND SMOKES CABIN. NOTE: CONTROLLABLE IN (MAN) MODE WITH ENGINE AIR, OTHERWISE SMOKES CABIN. PACK NR 2 HIGH TEMP LIGHT COMES ON. MAINTENANCE REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE THAT WOULD NOT TURN/ SEIZED. C/W WORK INSTRUCTIONS OF EO E04/022/621 REV C, NO DEFECTS NOTED. 2H74 4F4 FRTA49EU E6NE 20041215000292004121500029EA 2004 12 15 A6WA200440164 120041025A53405614414 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 INTERCOSTAL AT FS 484 LT SIDE IS CRACKED NEAR RADIUS OF ATTACHMENT FLANGE AT LBL36. CUT AWAY DAMAGED ATTACHMENT ANGLE. PERFORMED LPI TO ENSURE NO CRACKS EXIST, FAB REPLACEMENT ANGLE FROM 6144-14 AND INSTALLED USING SOLID RIVETS AND HI-LITE FASTENERS. ALL WORK DONE IAW REO 601R53-41-059, REV A AND BRAS. STANDARD REPAIR 601R5. 2L72 4F4 FRTA21EA E15NE 20041215000462004121500046NM 2004 12 15 ASAA0410418 120041006A53306548001183 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE- 5 HOLES WITH CRACK INDICATIONS. OVERSIZED HOLES AND INSTALLED REPAIR DOUBLERS. 2L72 4F4 FRTA16WE E2EA 20041215000592004121500059NM 2004 12 15 ASAA0410470 120041104A5320655054012 CHANNEL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - AFT CARGO BAY U CHANNEL IN HAT STRINGER IS CRACKED. REMOVED DAMAGED U CHANNEL, FABRICATED AND INSTALLED REPLACEMENT U CHANNEL IAW SRM. 2L72 4F4 FRTA16WE E2EA 20041215000722004121500072WP 2004 12 15 ASAA0480498 120040924A53219936640501 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK - CABIN FLOOR PANEL AT STA 864 TO 886 BROKEN AT FWD END. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2L72 4F4 FRTA6WE E9NE 20041215000892004121500089NM 2004 12 15 ASAA0480534 120041020A533059114015 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - C-CHECK, FUSELAGE SKIN, STA 218, BETWEEN LONGERON 18L AND 19L IS DENTED X=.042, D=2.20 WITHIN 1 INCH OF STRUCTURE. COLD WORKED SKIN TO CONTOUR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2L72 4F4 FRT E9NE 20041215000912004121500091NM 2004 12 15 ASAA0480536 120041020A523059101413 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - C-CHECK, AFT PIT DOOR, AFT MID SECTION 3 INCHES FROM EDGE DENTED X=1.10, D=.027, COLD WORKED TO CONTOUR, COMPLIED WITH HFEC. NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-04, FIG 38. 2L72 4F4 FRT E9NE 20041215000942004121500094NM 2004 12 15 ASAA0480539 120041020A53305924802509 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 OKC - C-CHECK, FUSELAGE SKIN, STA 237, LONGERON 17L HAS GOUGE WITH DENTS LESS THAN 1 INCH FROM STRUCTURE X=.034, D=1.11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLERS AND STRAPS IAW SRM 53-04, FIG 12C. 2L72 4F4 FRT E9NE 20041215000952004121500095NM 2004 12 15 ASAA0410425 120041012A53106546554 SHEAR TIE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 CORROSION ON SHEAR TIE. REMOVED SHEAR TIE FABRICATED NEW SHEAR TIE AND INSTALLED. 2L72 4F4 FRTA16WE E2EA 20041215000992004121500099WP 2004 12 15 ASAA0480504 120040924A531359364311 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, AFT PIT ON LONG 28L, OTBD LOWER LT SIDE AT STA 1098. REMOVED DAMAGE, FABRICATED REPAIR HAT SECTION IAW SRM 53-02, INSTALLATION TO BE COMPLIED WITH ON MIL-S 4788270. 2L72 4F4 FRTA6WE E9NE 20041215001232004121500123NM 2004 12 15 ASAA0410480 120041104A71106585378358 CAP BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE ENGINE COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - OTBD CAP CRACKED AT 6 O`CLOCK POSITION. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041215001322004121500132NM 2004 12 15 ASAA0410457 120041027A5330 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FUSELAGE SKIN DAMAGED FROM CHAFING. REMOVED DAMAGED SKIN, FABRICATED, NEW SKIN AND INSTALLED. 2L72 4F4 FRTA16WE E2EA 20041215001342004121500134NM 2004 12 15 ASAA0410459 120041028A5321656210042 FLOOR PANEL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE LAVATORY CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CRACKED FLOOR WEB IN FWD LAVATORY. REPAIRED WITH DOUBLER. 2L72 4F4 FRTA16WE E2EA 20041215001362004121500136NM 2004 12 15 ASAA0410461 120041028A5311654795965 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON FRAME STRAP AND FRAME. REMOVED AND REPLACED FRAME IB AND OB STRAP AND REMOVED AND REPLACED FRAME. 2L72 4F4 FRTA16WE E2EA 20041215001372004121500137NM 2004 12 15 ASAA0410436 120041022A5320654585554 SILL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON AFT GALLEY DOOR MOP SILL. REPLACED MOP SILL. 2L72 4F4 FRTA16WE E2EA 20041215001392004121500139NM 2004 12 15 ASAA0410438 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001432004121500143NM 2004 12 15 ASAA0410442 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001462004121500146NM 2004 12 15 ASAA0410445 120041022A5330654580001000 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001502004121500150NM 2004 12 15 ASAA0410434 120041020A5330654577872 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001552004121500155WP 2004 12 15 ASAA0480510 120040924A523059101413 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FWD CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, FORWARD CARGO DOOR SKIN ALONG FWD EDGE DINGED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-05, FIG 4. 2L72 4F4 FRTA6WE E9NE 20041215001572004121500157WP 2004 12 15 ASAA0480512 120040924A532199365831 FLOORBOARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE PAX CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, FLOORBOARD IN PASSENGER CABIN AT STA 826-864, BETWEEN 22R AND 44R DELAMINATD AND CRACKED. FABRICATED REPLACEMENT FLOORBOARD IAW SRM 53-05. 2L72 4F4 FRTA6WE E9NE 20041215001612004121500161NM 2004 12 15 ASA0440172 120041001A53406935352414 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE BENT A K NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - AFT CARGO BAY STRINGER CLIP BENT. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041220000032004122000003NM 2004 12 20 SWAA043617 120041213A533065C27257 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR CUTOUT AT LOWER FWD CORNER CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041220000122004122000012WP 2004 12 20 WX0400058 120041208A3350GE43 BULB DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19890GA 49371 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT INOPERATIVE AT L-1 DOOR. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041220000142004122000014NM 2004 12 20 04FDEA03357 120041206A5753 HINGE DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220000172004122000017NM 2004 12 20 DL733041086 120041207A2780 SWITCH BOEING737 737347 1384647NM NR 4 SLAT INTERMITTENT A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27311WA 23597 AFTER TAKEOFF AND FLAPS WERE RAISED PILOT HAD NR 4 SLAT INDICATION PROBLEM ON THE FWD PANEL AND ON THE OVERHEAD. REPLACED SWITCH ON NR 4 SLAT ROD END. 2L72 4F RTA16WE 20041220000182004122000018 2004 12 20 DL764041093 420041211A23108220987003 COUPLER BOEING767 767432ER 1385134NM NR 2 HF SYSTEM FAILED A DALAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO27825MH 29696 BOTH HF RADIOS UNABLE TO TRANSMIT, AUDIO OK. RESET C/B`S SEVERAL TIMES, NO HELP. REPLACED NR 2 HF COUPLER. 2L72 4F RTA1NM 20041220000242004122000024NM 2004 12 20 AWXA200401389 120041126A5330654577572 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN BETWEEN BS 727D AND BS 727E, STR 22 RT. MAINTENANCE CUT OUT DAMAGED AREA OF FUSELAGE SKIN BETWEEN BS 727D AND BS 727E, STR 22 RT; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20041220000272004122000027NM 2004 12 20 04FDEA03429 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1887 TO STA 2007, LBL 57. REMOVED AS PER SRM 51-31-01 VOL II. NEW HAT SECTION FABRICATED AS PER DWG AGA 7496 AND INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041220000332004122000033NM 2004 12 20 SWAA043642 120041215A55106551524 FITTING BOEING737 7373H4 1384600NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB FITTING RT AND LT FWD AND AFT CLEVIS LUGS CORRODED. REPAIRED HORIZONTAL STAB PER ER. 2L72 4F RTA16WE 20041220000412004122000041 2004 12 20 RAIA00412019 420041212A3444 ALTIMETER EMB 145 EMB145LR 3260212SO RADAR FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03831HK 145232 BUF - RADAR ALTIMETER NR 1 FAIL, GPWS FAILED, AND WIND SHEAR FAILED. MAINTENANCE DEFERRED RADAR ALTIMETER PER EMB 145 MEL 34-31-00. 2L72 4T RTT00011AT 20041220000522004122000052 2004 12 20 SWAA043625 420041214A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041220000612004122000061EU 2004 12 20 MALA040807 120041011A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND RT I/B SEAT TRACK BL 0 STA 300.0 CORRODED. MAINTENANCE REPAIRED IAW MESABA EO S53060. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20041220000702004122000070 2004 12 20 SWAA043612 420041120A256565C16820 HOOK BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29448WN 33721 DURING SPV, FOUND R1 DOOR EVAC SLIDE GIRT BAR AFT HOOK LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT HOOK FASTENER PER MM. 2L72 4F RTA16WE 20041220000712004122000071NM 2004 12 20 MWEA040220 120041213A5754993751219 DOUBLER DOUG MD88 MD88 3023688NM LT WING LE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 LEFT WING LEADING EDGE INTERNAL UPPER SURFACE DOUBLER HAS FOUR CRACKS AT THE EDGE OF THE STIFFENING INDENTATIONS, LOCATED APPROXIMATELY 5-14 INCHES INBOARD OF THE NUMBER TWO SLAT OUTBOARD TRACK. STOPPED DRILLED FOUR CRACKS. 2L72 4F RTA6WE 20041220000722004122000072EA 2004 12 20 COMA0460673 120041210A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01920CA 7022 FLIGHT 5808 FLAPS FAIL CAUTION MESSAGE. PERFORMED SYSTEM RESET AND OPERATIONAL CHECKS OF FLAP SYSTEM, FOUND NO DEFECTS. 2L72 4F RTA21EA 20041220000862004122000086NM 2004 12 20 04FDEA03286 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220000882004122000088NM 2004 12 20 04FDEA03396 120041209A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. BORE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057. 2L73 4F RTA22WE 20041220000982004122000098NM 2004 12 20 04FDEA03292 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. 2L73 4F RTA22WE 20041220001032004122000103NM 2004 12 20 04FDEA03355 120041206A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001052004122000105WP 2004 12 20 04FDEA03257 120041129A5730ARC0269503 PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT WING PANEL OVER AFT TRUNNION HAS MANY AREAS OF DELAMINATION. REPAIRED AFT TRUNNION PANEL ARC0269-503 BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC GWG ARC0269 AND FEDEX EA 8-5710-83945, WINGS- LEFT HAND MAIN LANDING GEAR FITTING TO FUSELAGE AFT, UPPER TRAILING EDGE PANEL- REPAIR. 2L73 4F RTA22WE 20041220001082004122000108WP 2004 12 20 04FDEA03260 120041129A5246ARB1101503 DOOR DOUG MD10 MD1010F 3022112WP ZONE 500 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT HAND WING REFUEL PANEL NEEDS REWORK DUE TO SHIFT OF INNER DOUBLER DURING AUTO-CLAVE CURE AND LACK OF TIMCO ROUTING SHEET BEING ASSIGNED. REPAIRED, REWORKED REFUEL PANEL PART NUMBER ARB1101-503 BY FABRICATING AND BONDING NEW OUTER SKIN AND INNER DOUBLER IAW TPS 10001 REV E AND DAC DWG ARB1101 AND FEDEX EA 8-5710-83944, WINGS- LEFT HAND WING, DOOR ASSEMBLY, REFUELING PANEL DISBOND- REPAIR. LOWER SKIN, CORE AND BLOCKS BONDED ON NON-ROUTINE N01203. 2L73 4F RTA22WE 20041220001112004122000111NM 2004 12 20 04FDEA03351 120041205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001132004122000113NM 2004 12 20 AWXA200401396 120041214A33501012721 LIGHT BOEING737 737301 1384611NM SEAT ROW 4 LT SHORTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28324AW 23261 PHX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT HAD SHORTED OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041220001142004122000114WP 2004 12 20 04FDEA03242 120041129A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT WING FWD INSIDE HINGE SECTION OF OUTBOARD FLAP STA XW 486 FOUND RUST NEAR HOLES FOR STUD BOLT AND IN THE HOLES OF THE LATERAL BRACE. ACCOMPLISH CORROSION REWORK OF RT FWD INBOARD HINGE OF RT OUTBOARD FLAP IAW CMM 57-44-08. 2L73 4F A22WE 20041220001222004122000122NM 2004 12 20 04FDEA03319 120041202A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407, 2L73 4F RTA22WE 20041220001242004122000124NM 2004 12 20 04FDEA03321 120041202A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. REPAIRED AS PER FEDEX EA 1-5750-77984. 2L73 4F RTA22WE 20041220001292004122000129WP 2004 12 20 WX0400059 120041208A33501315 BULB DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19890GA 49371 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 21. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041220001332004122000133NM 2004 12 20 04FDEA03157 120041118A5510ALC810Y1 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 14L EXCEEDED LIMITS AFTER CORROSION REMOVAL. BARREL NUT BORE FITTING NR 14L, REMOVED AND REPLACED PER SRM 51-33-01 VOLUME 2. 2L73 4F RTA22WE 20041220001492004122000149NM 2004 12 20 04FDEA03280 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001622004122000162NE 2004 12 20 SWAA043602 220041211A7230 BLADE BOEING737 7377H4 1384404NM GE CFM56 CFM56* 13802NE NR 2 COMPRESSOR TORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29767SW 29807 876349 DURING SCHEDULED HC2 CHECK, FOUND NR 2 ENGINE 8TH STAGE HPC ROTOR HAS 1 EACH BLADE TORN. REMOVED AND REPLACED NR 2 ENGINE PER MT 771-00-01. 2L72 4F4 FRTA16WE E2GL 20041220001792004122000179 2004 12 20 UPS04143603 420041212A2565 SLIDE AIRBUSA300 A300F4622R 3930360EU CABIN LOW A IPXAK NONE O OTHER ININSP/MAINT 1 SO01148UP 0831 DOOR SLIDE IS MARGINAL (LOW). REMOVED AND REPLACED DUAL ESCAPE SLIDE IAW MM 25-61-21-4. 2L72 4F RTA35EU 20041220001882004122000188NM 2004 12 20 USAA040940 120041111A5340113348 STRINGER CLIP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 STRINGER CLIP, .2500 INCH CRACK, BS 663.75, STRINGER 10 LT. DEFECTIVE PART REPLACED WITH IDENT PN. 2L72 4F4 FRTA16WE E21EU 20041220001892004122000189NM 2004 12 20 USAA040943 120041026A575435753 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 SKIN AND CORE, 4 INCH BY 4 INCH AREA, IB T/E NR 4 SLAT. REMOVED DELAMINATED SKIN AND CORE, INSTALLED DOUBLER, NEW CORE IAW 51-70-10. 2L72 4F4 FRTA16WE E21EU 20041220001942004122000194 2004 12 20 ASOA04892 420041108A3418C16258AA VANE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE AOA FALSE INDICATIONA ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27751EV201 10163 FOLLOWING TAKEOFF, CREW RECEIVED A STALL FAIL CAUTION MESSAGE. QRH WAS COMPLIED WITH AND APPROXIMATELY 250 KNOTS THE STICK SHAKER BEGAN TO SHAKE THE CONTROLS. THE AIRSPEED WAS INCREASED ABOVE 250 KNOTS AND PITCH LOWERED TO INCREASE ABOVE THE LOW SPEED CUE. UPON LOWERING THE PITCH AND INCREASING AIRCRAFT SPEED, THE SPEED CUE CONTINUED TO CLIMB, BEING UNABLE TO STOP THE STICK SHAKER. EMERGENCY WAS DECLARED WITH THE AIRCRAFT RETURNING, LANDING SAFELY. MAINTENANCE FOUND THE LEFT ANGLE OF ATTACK VANE (TRANSDUCER) COVERED WITH A PLASTIC BAG PREVENTING IT FROM MOVING. MAINTENANCE REMOVED AND REPLACED THE LT ANGLE-OF-ATTACK (AOA) VANE IAW VANE IAW AMM 27-35-05. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041220001962004122000196EA 2004 12 20 ASOA04902 120041115A3350 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING C-CHECK, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY NEAR THE SERVICE DOOR. 2L72 4F4 FRTA21EA E15NE 20041220001992004122000199EU 2004 12 20 ASOA04924 120041102A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, SEVERAL PLACES ON THE LT SEAT TRACK BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF SEAT TRACK IAW SRM 51-25-04. 2H72 4T4 TRTA53EU E20NE 20041220002002004122000200NM 2004 12 20 ASA0440198 120041029A53116546525 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041220002032004122000203NM 2004 12 20 USAA040914 120041022A53401133482 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1- CLIP, .2500 INCH CRACK AT STA 807, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20041220002092004122000209NM 2004 12 20 ASA0440215 120041029A53116546555 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041220002182004122000218NM 2004 12 20 ASA0440224 120041029A531065C25299 SHEAR TIE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 CORRODED SHEAR TIE. REPAIRED WITH DOUBLER. 2L72 4F4 FRTA16WE E21EU 20041221000042004122100004SO 2004 12 21 SIMA200431503 120041103A532014521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR 145368 DURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND CORRODED. REMOVED THE CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW SRM. (SW21200501161) 2L72 4F4 FRTT00011ATTE6CH 20041221000352004122100035NM 2004 12 21 ASA0440226 120041101A5311654655846 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 CORROSION FRAME BS 907 BETWEEN STR 27R-27L. REPAIRED CORRODED FRAME IAW SRM. 2L72 4F4 FRTA16WE E21EU 20041221000382004122100038NM 2004 12 21 USAA040898 120041019A5210 DOOR FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - FRAME, .5 INCH CRACK. FWD SERVICE DOOR SURROUND FRAME AT 294.5 AND S17R. FABRICATED DOUBLER IAW SRM 51-70-11. 2L72 4F4 FRTA16WE E21EU 20041221000412004122100041EU 2004 12 21 ASOA04886 120041105A33507012210 LAMP AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27533AS 460 DURING A GROUND INSPECTION, THE EXTERNAL RT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EXTERNAL RT FWD EMERGENCY LIGHT LAMP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041221000442004122100044EA 2004 12 21 A6WA200440198 120041129A4990 APU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE APU BAY LEAKING A A6WAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31402AW 7281 OIL SMELL COMING FROM BOTH PACKS. TROUBLESHOOTING AND FOUND APU LEAKING OIL. REPLACED BOTH COALESCER BAGS. RAN ENGINE. NO SMELL NOTED. 2L72 4F4 FRTA21EA E15NE 20041221000502004122100050NM 2004 12 21 AMTA200401449 120041125A3350 LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE SEAT18 DEF LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11528AT 30887 EMERGENCY EGRESS LIGHT AT SEAT 18 DEF UNDER BAGGAGE BIN, LOOSE. REATTACHED EMERGENCY EGRESS LIGHT AT SEAT 18 DEF, OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20041221000582004122100058EA 2004 12 21 A6WA200440211 120041214A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 RT FS 621 FLOOR SUPPORT ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20041221000592004122100059WP 2004 12 21 GTIA040842 120041112A5753 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE TE FLAPS DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 DENT ON LT OB FLAP LOWER SIDE, 19 INCH FROM T/E AND 8 INCHES FROM IB END OF T/E WEDGE, DEPTH 0.095 INCH, DIAM 2.0 INCH. REMOVED DAMAGED SKIN, FABRICATED SKIN AND DOUBLER TREATED AND PRIMED, INSTALLED SKIN AND DOUBLER, BONDED SKINS AND PAINTED. 2L72 4F4 F A6WE E9NE 20041221000692004122100069SO 2004 12 21 SIMA200431508 120041104A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK 145371 DURING AN IMBV INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW2120051190) 2L72 4F4 FRTT00011ATTE6CH 20041221000702004122100070EU 2004 12 21 ASOA04925 120041102A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON FLOORBEAM 39 IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041221000722004122100072EU 2004 12 21 ASOA04927 120041102A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE ZEE FLOOR SUPPORT BETWEEN FRAMES 39R AND 40R AT STRINGER 16R. MAINTENANCE REMOVED AND REPLACED THE CORRODED Z-ANGLE IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041221000742004122100074SO 2004 12 21 SIMA200429801 120041013A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21626AE 145117 DURING AN MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SERVICE DOOR SILL AND INSTALLED NEW SILL. REPAIR DONE IAW REPAIR STATMENT AND EM53-013. (SW21200501190) 2L72 4T4 FRTT00011ATTE6CH 20041221000762004122100076NM 2004 12 21 USAA040952 120041020A53131122424 STRINGER BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - STRINGER, .1250 INCH CRACKS, CRACKS IN STRING AROUND FASTENERS, STA 907, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-45772. 2L72 4F4 FRTA16WE E2GL 20041221000772004122100077SO 2004 12 21 SIMA200431502 120041104A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK 145371 DURING AN IMBV INSPECTION THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING CUTOUT. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221000792004122100079WP 2004 12 21 GTIA040836 120040930A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE DEFORMED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 WAVY SKIN 27 INCHES FROM LOWER EDGE OF AFT AIRSTAIRS RT SIDE, FABRICATED REPAIR PARTS (FILLER AND DOUBLER) FROM 2024T3-.032, OK TO TREAT AND PRIME FABBED FILLER AND DOUBLER, INSTALLED IAW SRM 52-01. 2L72 4F4 F A6WE E9NE 20041221000812004122100081NM 2004 12 21 USAA040755 120041012A5310 WINDOW FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU COCKPIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19521AU 23856 PIT, C5, WINDOW FRAME, .2500 INCH CRACK, CAPTAINS WINDOW POST BETWEEN NR 1 AND NR 2 WINDOWS TOP, FWD CORNER. INSTALLED DOUBLER IAW SRM, FIG 103. 2L72 4F4 FRTA16WE E21EU 20041221000822004122100082EA 2004 12 21 ASOA04875 120041103A3350 LENS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE SERVICE DOOR. 2L72 4F4 FRTA21EA E15NE 20041221000862004122100086WP 2004 12 21 GTIA040826 120041022A3150 SOLENOID DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE COCKPIT CHIME STUCK A GTIAK NONE P NO WARNING INDICATION ININSP/MAINT 1 GL23819NK 48016 LP 0264638; ON PRE-FLIGHT FOUND FLIGHT DECK AUDIO ALERTING CHIME INOPERATIVE. FOUND COCKPIT CHIME BELL SOLENOID STUCK AND SHORTING TO GROUND, REMOVED AND REPLACED COCKPIT CHIME BELL. AIRCRAFT TAIL SWAP WIGH N812NK. 2L72 4F4 F A6WE E2EA 20041221000882004122100088NM 2004 12 21 USAA040944 120041028A575465C26602257A SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - NR 2 SLAT SKIN, 3 INCH BY 4 INCH AREA, DELAMINATION, OB END T/E. REMOVED DAMAGE SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20041221000892004122100089WP 2004 12 21 GTIA040792 120041001A7540 DUCT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE TEMP VALVE LOOSE A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23800NK 49144 DURING CLIMB-OUT, TAIL COMPARTMENT HIGH LIGHT CAME ON 1 OR 3 TIMES SO RETURNED TO DEPARTURE AIRPORT. T/S FOUND RT TEMP CONTROL VALVE DUCT LOOSE. SECURED PRIMARY HEAT EXCHANGER EXHAUST DUCT. 2L72 4F4 F A6WE E9NE 20041221000902004122100090EA 2004 12 21 ASOA04914 120041119A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27886AS 7531 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221000922004122100092NM 2004 12 21 AMTA200401294 120041019A3397 CONNECTOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHTSLOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 FWD FLOOR TRACK LIGHTING HAS SEVERAL LIGHTS OUT. FOUND LOOSE CONNECTION AT FLOOR TRACK LIGHT INSPECTED AND SECURED. OPERATIONS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20041221000932004122100093NM 2004 12 21 USAA040900 120041027A5754 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - NR 4 SLAT SKIN, 6 FASTENER HOLES, .1250 INCH TO .2500 INCH CRACK. FASTENER HOLES, LOWER SKIN AREA BELOW ACTUATOR ATTACH POINT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER IAW SRM 57-43-01, FIG 206. 2L72 4F4 FRTA16WE E21EU 20041221000952004122100095EA 2004 12 21 ASOA04878 120041103A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041221000972004122100097NM 2004 12 21 AMTA200401296 120041020A3397 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT LOOSE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11518AT 27974 EMERGENCY LIGHTS NOT WORKING BEHIND ROW 9 F E D ON FLOOR PATH. FOUND 1 CONNECTION WIRE LOOSE ON LIGHT ASSEMBLY, RECONNECTED AND FOUND TO BE WORKING, OK. 2L72 4F4 FRTA2NM E12EU 20041221001002004122100100SO 2004 12 21 SIMA200432904 120041118A531514521713003 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21628AE 145124 DURING A MBV INSPECTION, CORROSION WAS FOUND ON THE GALLEY CENTER FLOORBEAM AT FRAME 20. REMOVED CORROSION BY CUTOUT. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW SRM. (SW21200501183) 2L72 4T4 FRTT00011ATTE6CH 20041221001012004122100101SO 2004 12 21 SIMA200429803 120041014A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21626AE 145117 DURING AN MBV INSPECTION, THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA OF THE LT OMEGA BEAM. FABRICATED A FILLER, EXTERNAL ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501190) 2L72 4T4 FRTT00011ATTE6CH 20041221001042004122100104EA 2004 12 21 A6WA200440188 120041118A30307858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AOA HEAT FAILED A A6WAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31405AW6738 4314 7362 RT AOA, RT TAT, RT STATIC, RT PITOT AFTER TAKEOFF RETURNED IAW DISPATCH. REMOVED AND REPLACED RT AIR DATA SENSOR HEAT CONTROLLER IAW MM 30-31-15, OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041221001082004122100108EA 2004 12 21 ASOA04876 120041103A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE CLIPS AT FS 280, LBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, LBL 9 IB AND OB. 2L72 4F4 FRTA21EA E15NE 20041221001112004122100111NM 2004 12 21 AMTA200401429 120041123A2120 ODOR BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE CABIN DETECTED A AMTAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL11552TZ 32586 WHEN ENTERING RUNWAY FOR TAKEOFF, NOTED PREVIOUSLY REPORTED ODOR AND RETURNED TO GATE. TAXIED AIRCRAFT AROUND AIRPORT 45-60 MINUTES. SAME AREA AS PREVIOUS CREW. NO UNUSUAL ODOR NOTED, CHECKED WHEELS, TIRES, BRAKES IAW MM 32-41-10-6. NO DEFECTS NOTED. OK FOR SERVICE. (GL11200505368) 2L72 4F4 FRTA2NM E12EU 20041221001122004122100112SO 2004 12 21 SIMA200429807 120041014A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE FORWARD DIGITAL ON LT FLOORBEAM WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED A SPLICE AND DOUBLER. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221001132004122100113NM 2004 12 21 USAA040947 120041103A5310 STRAP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU DOOR FRAME CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - STRAP, .2500 INCH BY .2500 INCH IN 66 AREAS, CORROSION; LEVEL 1; TASK NR-C53-107-02, AFT CARGO DOOR FRAME SECTION S25R, STA 807-848. REPLACED PART IAW SRM 53-00-07. 2L72 4F4 FRTA16WE E21EU 20041221001162004122100116SW 2004 12 21 KBM2004F00244 120041116A3246206321004N SKID BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MLG CORRODED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1973DP 2513 REMOVED LANDING GEAR ASSY DUE TO RT SKID FAILURE, JUST AFT OF AFT CROSS TUBE MOUTH, FOUND HEAVY CORROSION IN AREA OF FAILURE. APPEARED TO BE RELATED FILL LENGTH SKID SHOES. REPLACED SKID GEAR WITH AAI STC NR SH139250, THIS GEAR WAS REMOVED SERVICEABLE FROM ANOTHER AC. 1G71 3U3 U H2SW E4CE 20041221001172004122100117SO 2004 12 21 SIMA200429808 120041011A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE FORWARD DIGITAL WAS FOUND CORRODED AT CENTER BEAM. REMOVED CORROSION BY MAKING A CUT OUT OF THE FORWARD DIGITAL. CUTOUT A REPAIR PART FROM PN 145-21721-009. FABRICATED 2 DOUBLERS AND SHIM. REPAIR DONE IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001192004122100119EA 2004 12 21 ASOA04913 120041119A5320601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO BAY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7207 DURING A C-CHECK, THE CARGO DOOR FLOOR LANDING PLATE AT FS 589.00 AND FS 605.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR LANDING PLATE AT FS 589.00 AND FS 605.00 IAW EO 600-53-0117. 2L72 4F4 FRTA21EA E15NE 20041221001222004122100122NM 2004 12 21 USAA040945 120041027A57536546434302 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RT TE FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN TO CORE, 7 INCHES BY 2.5 INCH AREA DELAMINATED, IB RT AFT FLAP TOP SURFACE 34.5 INCHES- 42 INCHES FROM OB END. REMOVED UPPER SKIN AND CORE, INSTALLED NEW CORE AND TOP DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20041221001232004122100123EA 2004 12 21 ASOA04883 120041104A324450105711 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG BLOWN A ASOAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO27835AS 7258 DURING CRUISE, THE CREW WAS ADVISED BY TOWER THE AIRCRAFT MAY HAVE EXPERIENCED A TIRE BLOWING ON THE RT SIDE UPON TAKEOFF. AN EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT OB TIRE ASSY AS A RESULT OF THE BLOWN TIRE AND ALSO RT IB TIRE ASSY AS REQUIRED. IN ADDITION, MAINTENANCE REPLACED THE RT MAIN GEAR HARNESS ASSY AND SEVERAL RT ENGINE FAN BLADES WHICH WERE DAMAGED FROM TIRE FOD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221001242004122100124SO 2004 12 21 SIMA200429602 120041015A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21833AE 145629 DURING A MBV INSPECTION THE RT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A DOUBLER FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501186) 2L72 4F4 FRTT00011ATTE6CH 20041221001282004122100128SO 2004 12 21 SIMA200429810 120041014A532014522178005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 26 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001312004122100131WP 2004 12 21 GTIA040808 120040927A5240 RETAINER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE SERVICE DOOR CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 FWD SERVICE GALLEY DOOR LOWER PRESSURE SEAL RETAINER HAS CORROSION. REMOVED CORROSION, FABRICATED NEW RETAINER, INSTALLED NEW RETAINER. 2L72 4F4 F A6WE E9NE 20041221001322004122100132WP 2004 12 21 GTIA040807 120040913A5347 CARGO TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CARGO BAY CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 FWD PIT RT CARGO TRACK CORRODED IN NUMEROUS AREAS. CUT OUT DAMAGED CARGO TRACK. FABED NEW SPLICE REPAIR. DRILLED AND LOCATED NEW REPAIR. INSTALLED CARGO TRACK REPAIR. 2L72 4F4 FRTA6WE E9NE 20041221001332004122100133EU 2004 12 21 KBM2004F00240 120040922A6720704A34130184 CONTROL CABLE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE TAIL ROTOR BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 461 2009 PILOT REPORTS BINDING T/R PEDALS. REMOVED AND REPLACED T/R FLEX CABLE WITH NEW. 1G71 3U3 U H9EU E19EU 20041221001352004122100135SO 2004 12 21 SIMA200429806 120041012A532014522460013 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE CENTER BEAM WAS FOUND CORODED BETWEEN FRAMES 32-34. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001362004122100136EA 2004 12 21 ASOA04904 120041116A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105. 2L72 4F4 FRTA21EA E15NE 20041221001392004122100139WP 2004 12 21 GTIA040804 120041012A2697 CONNECTOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE LT FIRE LOOP BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23831NK 49617 LT ENGINE LOOP B ILLUMINATED AT CRUISE. FOUND CONNECTORS INNER INSULATOR BROKEN. REMOVED AND REPLACED B LOOP CONNECTOR, LOWER CENTER. 2L72 4F4 FRTA6WE E2EA 20041221001412004122100141SO 2004 12 21 SIMA200432905 120041118A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21628AE 145124 DURING AN MBV INSPECTION CORROSION WAS FOUND ON A PREVIOUS REPAIR TO THE LT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR AND INSPECTION THE UNDERLYING BEAM, NO DAMAGE NOTED. FABRICATED AN EXTERNAL ANGLE, FILLER, SHIMS ND PLATE. REPAIR DONE IAW SRM. (SW21200501183) 2L72 4T4 FRTT00011ATTE6CH 20041221001422004122100142 2004 12 21 GTIA040803 420041012A2565 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE L2 SLIDE DISCONNECTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 L2 DOOR SLIDE DEPLOY LANYARD CABLE DISCONNECTED. RECONNECTED DEPLOY LANYARD TO GIRT BAR RECEPTACLE. 2L72 4F4 FRTA6WE E9NE 20041221001432004122100143SO 2004 12 21 SIMA200429812 120041014A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA ON THE LT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001442004122100144EA 2004 12 21 ASOA04897 120041109A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27841AS9348 6262 7300 DURING CLIMB-OUT, AT APPROXIMATELY 18,000 FEET, THE CREW RECEIVED A (FLAP FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE POSITION SENSOR UNIT (BPSU) AND ALSO RIGGED THE LT AND RT FLAP SYSTEM TO ZERO. IN ADDITION, MAINTENANCE RIGGED THE RIGHT BPSU IAW THE MM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221001452004122100145WP 2004 12 21 GTIA040817 120041017A5210 HANDLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE L1 DOOR UNSECURE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23835NK 53044 L1 DOOR HANDLE LOOSE. SECURED DOOR HANDLE ON DOOR IAW MD-80, MM 52-61-00. OPS CHECK GOOD. 2L72 4F4 FRTA6WE E2EA 20041221001462004122100146WP 2004 12 21 GTIA040813 120041011A5397 CABLE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217A 52053NE TAILCONE MISINSTALLED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23815NK 49415 ONE TAILCONE CABLE NOT INSTALLED IN BLOCK. (TAILCONE LIGHT WAS ILLUMINATED). ROUTED AND INSTALLED CABLE IAW MM 53-53-02. 2L72 4F4 FRTA6WE E9NE 20041221001492004122100149SO 2004 12 21 SIMA200431003 120041027A532014521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21736DT 145388 DURING AN IMBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND CORRODED. REMOVED EXISTING CENTER HAT BEAM AND INSTALLED NEW BEAM. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221001512004122100151SO 2004 12 21 SIMA200432910 120041121A534314521680003 FITTING EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NLG CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 DURING AN MBV INSPECTION THE LT AND RT NOSE GEAR LEG BEARING TRACKS FOUND CORRODED. MAINTENANCE REMOVED CORROSION AND REINSTALLED BEARING CAPS IAW AMM, SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501182) 2L72 4T4 FRTT00011ATTE6CH 20041221001522004122100152NM 2004 12 21 ASAA0410426 120041012A53306545777 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20041221001532004122100153EA 2004 12 21 A6WA200440195 120041124A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31441ZW 7777 INTERCOSTAL CRACKED IN RADIUS APPROX 1.1 INCH LONG, FS 621- FS 625.1, STR 14R. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PN 601-35012-52 USING MS20470AS5 RIVETS IAW CRJ SRM 57-040-06. 2L72 4F4 FRTA21EA E15NE 20041221001542004122100154WP 2004 12 21 GTIA040814 120041019A3210 LANDING GEAR DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE LEFT UNKNOWN A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23829NK 49931 AFTER TAKEOFF, LT MAIN RED GEAR REMAINED ON WITH GEAR HANDLE UP. FOLLOW QRH PROCEDURE. ADVISED DISPATCH FOR FUEL BURN AND CONSULTED WITH MECHANIC CONTROL. CONTINUED TO ACY AT REDUCED SPEED AND ALT. CHECKED GEAR UP AND DOWN PROX SENSORS WIRING RESISTANCE IAW MM32-60-00. FOUND TO BE WITHIN RANGE. SHOT DOWN GEAR UP AND DOWN, SENSOR HARNESS FROM SENSORS TO FWD W/W CONNECTORS. WHILE MONITORING INDICATION LIGHTS, NO DEFECTS NOTED. ITEM REMAINS OPEN FOR FURTHER INVESTIGATION. 2L72 4F4 F A6WE E2EA 20041221001552004122100155EA 2004 12 21 A6WA200440197 120041123A2410755469E IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 DAMAGED A A6WAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL31444ZW3625 7788 IDG NR 2 AMGER CAS MESSAGE AT TAKEOFF. TAKEOFF ABORTED AT 60 KNOTS. FOUND IDG LEAKING OIL FROM DRAIN PLUG FOUND DRAIN PLUG DAMAGED/ REMOVED AND REPLACED DRAIN PLUG IAW AMM 24-31-00. REMOVED AND REPLACED IDG NR 2. OPS AND LEAK CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20041221001572004122100157EA 2004 12 21 A6WA200440196 120041126A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31441ZW 7777 PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 755, STRINGER 25L. REPAIRED DAMAGE BY ENLARGING FASTENER HOLE TO .1875 INCH AND INSTALLED RIVET MS2042AD6 IAW BRAS WO 601R-53-5674. 2L72 4F4 FRTA21EA E15NE 20041221001602004122100160NM 2004 12 21 ASAA0410427 120041012A53306545777 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20041221001612004122100161NM 2004 12 21 USAA040932 120041103A5320 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24577 PIT - Q1 - ZEE ANGLE, 2 INCH BY 3 INCH AREA, CORROSION LEVEL 1, TASK NR C53-100-1, BS 796, S25R IN AFT CARGO BIN. REMOVED ZEE ANGLE, AND INSTALLED NEW IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E21EU 20041221001622004122100162SO 2004 12 21 SIMA200432901 120041116A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21628AE 145124 DURING A MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM. 2L72 4T4 FRTT00011ATTE6CH 20041221001632004122100163NM 2004 12 21 USAA040893 120041015A5340 STRINGER CLIP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT- Q5- STRINGER TIE CLIP, .2500 INCH CRACK, BS 344, STR8, RT. FABRICATED IAW MFG DWG 66-244553 AND INSTALLED IAW SRM 51-40-01. 2L72 4F4 FRTA16WE E21EU 20041221001652004122100165NM 2004 12 21 USAA040933 120041022A53201136993 INTERCOSTAL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - INTERCOSTAL, .75 INCH BY 3 INCHES, CORROSION; LEVEL 1;TASK NR C53-107-02, FRAME 328, LBL 11. CHANGED INTERCOSTAL IAW SRM 51-10-02, 51-20-01, 51-40-01. 2L72 4F4 FRTA16WE E21EU 20041221001682004122100168EA 2004 12 21 A6WA200440006 120040113A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31404AW 7294 RIVET ON RT FUSELAGE SKIN AT FS 265.00 BETWEEN STRINGERS 22 AND 23 HAS LIGHTNING DAMAGE THAT EXTENDS BEYOND COUNTERSINK HOLE IN SKIN. (ADDTNL INFO-WO 59971 MWC 22) REMOVED FASTENER, ENLARGED FASTENER HOLE TO A NOMINAL .1875 DIAMETER, PERFORMED EDDY CURRENT TO ENSURE NO CRACKS EXISTED AND DAMAGE WAS REMOVED, INSTALLED FASTENER NAS1097AD6 WET USING PR1422B1/2 IAW WVAC EO 601R-53-4578. 2L72 4F4 FRTA21EA E15NE 20041221001692004122100169EA 2004 12 21 A6WA200440189 120041118A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE SPOILERS FAILED A A6WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL31416AW5982 194 7603 IN-FLIGHT RECEIVED SPOILERON CASS MESSAGE. REMOVED AND REPLACED NR 1 SECU, OPS CHECK GOOD IAW 27-61-00. 2L72 4F4 FRTA21EA E15NE 20041221001702004122100170SO 2004 12 21 SIMA200432909 120041124A321014524475003 CAP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NLG BEARING CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 DURING AN MBV INSPECTION THE RT NOSE GEAR LEG BEARING CAP WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED BEARING CAP IAW AMM. THE AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501182) 2L72 4T4 FRTT00011ATTE6CH 20041221001712004122100171EA 2004 12 21 A6WA200440177 120041107A3210601R572100323 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE MLG TRUNNION MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31440AW 7766 LT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED 0.005 INCH. REMOVED LT AFT MLG TRUNNION BUSHING IAW AMM 20-26-00-910-803. INSTALLED A NEW OVERSIZE (2ND) BUSHING PN 601R5721003-23. IAW REO 601R57-21-003B. REAMED INSIDE DIA TO 2.4384 IAW DWG 601R85007RWC. 2L72 4F4 FRTA21EA E15NE 20041221001772004122100177NM 2004 12 21 AMTA200401253 120041004A5313 STRINGER BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE FUSELAGE DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11553TZ 32587 STR 21L HAS (9) EA ELONGATED HOLES BETWEEN STA 511 AND STA 523. INSTALLED (9) EA FREEZE PLUGS IAW ERA 757-53R-5717. 2L72 4F4 FRTA2NM E12EU 20041221001832004122100183SO 2004 12 21 SIMA200432908 120041121A532014521725613 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21640AE 145183 DURING A CPCP INSPECTION, THE SILL OF THE FORWARD SERVICE DOOR FOUND SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE SILL IAW SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20041220000232004122000023EU 2004 12 20 AWXA200401403 120041214A3260848401 PROXIMITY SENSOR AIRBUS320 A320231 3930325EU NLG INTERMITTENT A AWXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP28625AW 064 DTW - EMERGENCY LANDING - FLT 0096 - WHILE PREPARING FOR LANDING AT DTW EN ROUTE FROM LAS AFTER LANDING GEAR WAS LOWERED RECEIVED A LANDING GEAR SYSTEM DISAGREE MESSAGE WITH LANDING GEAR CONTROL INTERFACE UNIT NR 2 INDICATING THE NOSE GEAR WAS UNSAFE. ABORTED APPROACH AND FLEW BY TOWER TO VERIFY GEAR WAS DOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR 19GA IAW AMM 32-31-73-04, OPERATIONAL TEST WAS GOOD. 2L72 4F RTA28NM 20041220000262004122000026EA 2004 12 20 COMA0460688 120041216A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 LEFT HAND INTERCOSTALS AT FS 484.00 OUTBOARD CRACKED. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20041220000292004122000029WP 2004 12 20 ABXA040390 120041206A3260 DOWNLOCK SWITCH DOUG DC9 DC941 302207NWP NLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING CRCRUISE 1 GL23955AX 47619 EN ROUTE, NOSE GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED NOSE GEAR DOWNLOCK SWITCH IAW DC9 MM 32-60-01. 2L72 4F A6WE 20041220000302004122000030NM 2004 12 20 MWEA040219 120041209A5244 LATCH BOEING717 717200 1383700NM ACCESS DOOR UNLATCHED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31912ME 55175 UPON ROTATION ACCESS COMPARTMENT DOOR ALERT ILLUMINATED. VERIFIED FORWARD ACCESSORY COMPARTMENT PROXIMITY TOO FAR FROM TARGET BECAUSE THE DOOR LATCH WAS OPEN, OPENED DOOR AND INSPECTED DOOR ASSEMBLY AND LATCHES. NO DEFECTS NOTED. CLOSED AND TESTED DOOR. OK FOR CONTINUED SERVICE. 2L72 4F TRA6WE 20041220000312004122000031EA 2004 12 20 COMA0460693 120041216A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 LEFT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041220000372004122000037NM 2004 12 20 04FDEA03430 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1821 TO STA 1887, LBL 36. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041220000422004122000042EU 2004 12 20 RAIA00412020 120041213A3350 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHT LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03561HK 41077 CID - ESCAPE PATH LIGHTING IN ROWS 1 AND 2 ARE OUT. MAINTENANCE RESECURED ESCAPE PATH LIGHTING CONNECTOR AT ROW 1 AND 2. 2L72 4T RTA41NM 20041220000442004122000044EU 2004 12 20 RAIA00412014 120041212A242051539019E GCU JETAIRJETSTMJETSTM4101 1500501EU RT GENERATOR MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03566HK173721392 41084 STL - RT GEN FELL OFF LINE. MAINTENANCE REMOVED AND REPLACED GENERATOR CONTROL UNIT. 2L72 4T RTA41NM 20041220000472004122000047NM 2004 12 20 UPS04543593 120041210A5610 WINDOW BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01441UP 27386 CREW PREFLIGHT F/O WINDOW WILL NOT OPEN OR CLOSE. GEARBOX IS BAD. REMOVED AND REPLACED FIRST OFFICER'S WINDOW CRANK GEARBOX PER AMM 56-11-04-4. 2L72 4F RTA2NM 20041220000572004122000057NM 2004 12 20 SWAA043630 120041214A53306545774 SKIN BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29696SW 23064 DURING SPV, FOUND FUSELAGE SKIN AT BS 727F + 15 BETWEEN STRINGER 18R AND STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041220000582004122000058NM 2004 12 20 SWAA043631 120041214A53206547953 TEE FITTING BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29506SW 24183 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR LOWER OUTBOARD TEE FITTING, CRACKED. REMOVED AND REPLACED TEE FITTING PER SRM. 2L72 4F RTA16WE 20041220000682004122000068NM 2004 12 20 SWAA043600 120041211A2560P2070001 FLASHLIGHT BOEING737 7373H4 1384600NM CABIN INGESTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 FWD OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2L72 4F RTA16WE 20041220000742004122000074NM 2004 12 20 2004UALA01200 120041208A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 EXTERNAL FUSELAGE SKIN CREASED AT BS 1705 BETWEEN STR 15L & 16L. INSTALLED FILLER, DOUBLER & TRIPLER. 2L72 4F4 FRTA2NM E17NE 20041220000762004122000076NM 2004 12 20 2004UALA01202 120041208A7931 TRANSMITTER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE OIL PRESSURE MALFUNCTIONED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29339UA 24243 RETURNED TO GATE AFTER 90 KNOT ABORTED TAKEOFF DUE TO OIL PRESSURE INDICATION. ENG 2 OIL PRESSURE WENT TO ZERO. REPLACED NR 2 OIL PRESSURE INDICATOR, OIL TEMPERATURE INDICATOR AND OIL PRESSURE TRANSMITTER. RAN ENGINE AND OPS CHECKED OK. THEN ON DEC 15, OIL PRESS INDICATION WAS INOP AGAIN AND THE OIL PRESSURE TRANSMITTER WAS REPLACED ONCE MORE. WIRING WAS CHECKED AND NO PROBLEMS WERE FOUND. 2L72 4F4 FRTA16WE E2GL 20041220000812004122000081NM 2004 12 20 SWAA043593 120041210A3350OL307IBPEGPL LAMP BOEING737 7372H4 138448CNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LIGHT AT ROW 10 DEF INOP. RELAMPED PER MM. 2L72 4F A16WE 20041220000822004122000082NM 2004 12 20 SWAA043594 120041210A3350BCREF4146 LIGHT BOEING737 7372H4 138448CNM EMERGENCY EXIT MALFUNCTIONED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY DIM. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20041220000902004122000090NM 2004 12 20 04FDEA03288 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001042004122000104NM 2004 12 20 04FDEA03356 120041206A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001092004122000109NM 2004 12 20 04FDEA03358 120041206A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001102004122000110WP 2004 12 20 04FDEA03368 120041206A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND PITTING CORROSION ON SIDE SKIN BETWEEN LONG 48 RT - 41 RT, STA 1531 - 1754. EXISTING REPAIR WITH BULGING AND CRACK AROUND JAMB DOOR. REPLACE PANEL PER SRM 51-33-02 PAGE 34-47, SRM 51-35-01 PAGE 1-12 AND DWG NFA 6013. P/N AFA 3076-501, AFA 6014-5. 2L73 4F A22WE 20041220001122004122000112NM 2004 12 20 04FDEA03352 120041205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001162004122000116WP 2004 12 20 04FDEA03244 120041129A5340 FITTING DOUG DC10 DC1010 3022110WP LONGERON CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND, AFTER REMOVAL BELLY SKIN, END FITTING WITH CORROSION AND REPAIR NOT CONFORMED TO SRM, BETWEEN STA 1521 TO STA 1581 LONGERON 52. REPLACE LONGERON 52 PER SRM 51-33-01 PAGE 34-47 MM 20-50-02. 2L73 4F A22WE 20041220001182004122000118WP 2004 12 20 04FDEA03246 120041129A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND RT OUTBOARD FLAP, FWD HINGE SECTION, STA XW 486 WITH CORROSION IN THE BORE OF BUSHINGS ACTUATOR ATTACH POINTS. ACCOMPLISH CORROSION REWORK AT RT OUTBOARD FLAP INBOARD FWD HINGE HOLES BORES (5A), (5B) IAW CMM 57-44-08 REV 30. 2L73 4F A22WE 20041220001262004122000126WP 2004 12 20 04FDEA03324 120041202A7160 ANGLE DOUG DC10 DC1010 3022110WP NR 2 INLET DUCT CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ON NR 2 ENGINE INLET DUCT, INBOARD PANEL 361 HL, ANGLE BROKEN. REMOVE NOSE COWL PER MM 20-50-02, REPLACE CRACKED SHIELDS PER DWG AJC7151, P/N AJC 7151-27, AJC 7151-29, INSTALL NOSE COWL PER MM 20-50-02. 2L73 4F A22WE 20041220001352004122000135WP 2004 12 20 04FDEA03159 120041118A5753ARC25121 HINGE DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 LEFT WING INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE, FOUND TO BE OUT OF LIMITS, FABRICATED OVERSIZED REPAIR BUSHING, INSTALLED AND HONED BUSHING IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81528, WINGS - LEFT HAND INBOARD FLAP, OUTBOARD HINGE BRACKET OVERSIZE PIVOT BORE AND STRAP. 2L73 4F RTA22WE 20041220001462004122000146NM 2004 12 20 QXEA200400870 120041204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - FUSELAGE SKIN AT STATION X245.5 AND STRINGER 17 RT HAS AREA OF SURFACE DAMAGE WITH ONE PIT. REPAIRED IAW RD 8/4-53-382, HORIZON AIR EA 6-53-479 AND SRM 51-25-15-370-801. 2H72 4T RTA13NM 20041220001482004122000148NM 2004 12 20 04FDEA03279 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041220001552004122000155WP 2004 12 20 ABXA040393 120041111A53305911412157 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 LOWER AFT CORNER OF FORWARD LOWER CARGO DOOR CUTOUT HAD 2 EACH CRACKS. REPAIRED IAW DC-9 SRM 53-05 AND REA D953-51052MR. 2L72 4F A6WE 20041220001582004122000158 2004 12 20 2004UALA01203 420041209A2565 SLIDE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE R1 DOOR DEPLOYED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29378UA 24653 DURING SERVICING, CATERERS REPORTED THAT THE DOOR 1R WAS OPEN AND HAD THE SLIDE PARTIALLY DEPLOYED. THE DOOR WAS NOT DISARMED. CAUSE IS UNKNOWN. A SLIDE COMPARTMENT (CLAMSHELL) LATCH WAS FOUND OPENED DURING INSPECTION. WHETHER THE LATCH WAS OPENED WHILE IT WAS INSTALLED ON THE DOOR CANNOT BE CONFIRMED. SLIDE UNIT WAS INSPECTED, REPACKED AND RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20041220001592004122000159WP 2004 12 20 WX0400061 120041208A33501315 BULB DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19890GA 49371 LAS - MAINTENANCE REPORTED EMERGENCY LIGHTS IN AFT INTERIOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041220001612004122000161NM 2004 12 20 04FDEA03414 120041214A5313 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON 52 SPLICE, AT STA 5-123 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041220001642004122000164NM 2004 12 20 AWXA200401397 120041214A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28818AW 1375 DURING THRU FLIGHT CHECK THE FORWARD LT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN FORWARD LT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041220001692004122000169NM 2004 12 20 DL73S041088 120041206A5330 SKIN BOEING737 737247 138448DNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27243WA 23517 FOUND ON S2 LETTER CK, CORROSION ON LOWER FUSELAGE SKIN STA 727A BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. REPAIRED PER SRM 53-30-3 FIG 1. 2L72 4F A16WE 20041220001772004122000177NM 2004 12 20 04FDEA03426 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1887 TO STA 2007, RBL 24. REMOVED AS PER SRM 51-31-01 VOL II. NEW HAT SECTION FABRICATED AS PER DWG AGA7497 & INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041220001812004122000181WP 2004 12 20 UPS04843597 120041118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 INSPECTION TYPE: C3, LONGERON 16R CRACKED AT STA 1750 FRAME ATTACH FASTENERS. REMOVED END FITTING, ATTACH CLIP, AND LONGERON SECTION FROM STA 1750-1 TO 1760. FAB REPLACEMENT LONG SECTION FROM S1616757 EXTRUSION & 2 SPLICE STRAPS FROM SHT7075T6/.080 INSTALLED ALL PARTS & REPAIR SPLICE FITTING. ALL MAINT PER SRM 53-2-2 FIG 10, 53-5-3, 51-1-8, 51-1-20D, DWG 5644130, DPS4.707, NDT-SPM06-10-01.001. 2L74 4F RT4A25 20041220001872004122000187NM 2004 12 20 USAA040931 120041028A5340 ATTACH ANGLE BOEING737 737500* NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - ATTACH ANGLE, .5 INCH LONG CRACK, FRAME 706, STR S-11L. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02, 51-40-03. 2L72 4F4 FRTA16WE E21EU 20041220002012004122000201NM 2004 12 20 USAA040890 120041019A5320 STIFFENER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LBB6.15 TO663.45CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU 23702 PIT- Q5 - VERTICAL STIFFENER, .7500 INCH CRACK, VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERTICAL STIFFENER OF LBBL 6.15 TO 663.45. REPLACED VERT STIFFENER IAW EA 79313/ EO5704V245 (DRAFT). 2L72 4F4 FRTA16WE E21EU 20041220002062004122000206 2004 12 20 RU3A0421 420041208A344110090910101 COOLING FAN BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE INERTIAL REF UNTBURNED E RU3AAGHIUNSCHED LANDING O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITSCABIN DEPRESSURIZATION BGJSMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE WARNING INDICATION APAPPROACH 1 SW1576 FF11 WHILE SETTING UP FOR FLIGHT INSPECTION MANEUVER, GOT A RED MASTER CAUTION LIGHT WITH AN AP TRIM DISC LIGHT. TEMPORARILY LOST TCAS, PILOTS FLIGHT DIRECTOR, AND THE PILOTS NCU. AT THE SAME TIME HEARD ELECTRICAL SHORTING SOUND. STRONG ELECTRICAL FUMES WERE DETECTED AND THE CREW DONNED O2 MASK. COPILOT INFORMED APPROACH OF THEIR STATUS AND REQUESTED A FULL STOP LANDING. SHORTLY AFTER THE POWER INTERRUPTION, PILOTS NCU CAME BACK UP. COPILOT TURNED OFF THE MISSION EQUIPMENT AND THE MSU TO REDUCE CHANCES OF ELECTRICAL FIRE AND THE AIRCRAFT WAS DEPRESSURIZED ON FINAL IN AN ATTEMPT TO REDUCE FUMES. THE CREW MADE AN UNEVENTFUL LANDING. FOUND LASER REFERENCE COOLING FAN SHORTED. 2L72 4T4 T A24CE E4EA 20041220002122004122000212NM 2004 12 20 ASA0440205 120041029A531165C22909 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000012004122100001SO 2004 12 21 SIMA200431006 120041101A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAO OTHER O OTHER NRNOT REPORTED 1 SW21733KR 145368 DURING AN IMBV INSPECTION THE FORWARD DIGITAL CENTER SECTION WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED 2 REPAIR DOUBLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200501161) 2L72 4F4 FRTT00011ATTE6CH 20041221000092004122100009EA 2004 12 21 A6WA200440208 120041213A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A K NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 LT WING LOWER PANEL FUEL TANK ACCESS DOOR CUT-OUT AT WS 12.245 HAS NUMEROUS AREAS OF PITTING/ FRETTING LOCATED ON FAYING SURFACE AND RADIUS AREAS. DEPTH LESS THAN .015 INCH. REPAIRED ACCESS DOOR CUTOUT AT WS 12/245 IAW BOMBARDIER REO 601R-57-21-030 REV C. (M) 2L72 4F4 FRTA21EA E15NE 20041221000192004122100019NM 2004 12 21 USAA040888 120041021A5320 PAN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT, Q5, FLOOR PAN, .5 INCH TEAR, LBL 18 INCH AT STA 986.5. INSTALLED FILLER/DOUBLER IAW SRM 51-70-13, FIG 1. 2L72 4F4 FRTA16WE E21EU 20041221000322004122100032NM 2004 12 21 ASA0440225 120041029A53156546808 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OVERSIZED HOLES IN LOWER FLANGE OF FLOORBEAM. REPAIRED FLOORBEAM. 2L72 4F4 FRTA16WE E21EU 20041221000422004122100042EA 2004 12 21 ASOA04895 120041111A2610356024310 LOOP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE MALFUNCTIONED A ASOAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27852AS 7369 DURING CLIMB-OUT, AT APPROXIMATELY 9,500 FEET, THE CREW RECEIVED A TRIPLE CHIME RT 14TH DUCT MESSAGE AND AURAL WARNING. THE CREW LEVELED THE AIRCRAFT TO 12,000 FEET AND COMPLIED WITH THE QRH. THE RT ENGINE WAS PULLED TO FLIGHT IDLE AND THE MESSAGE EXTINGUISHED. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT RETURNING, MAKING A SINGLE ENGINE LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE 14TH BLEED DUCT LEAK DETECTION LOOP A46WK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221000522004122100052WP 2004 12 21 GTIA040846 120041112A3234 SELECTOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE MLG DIRTY A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23830NK 49932 LP NR 3022501; DEPARTING DCA AFTER GEAR RETRACTION, ALL 3 RED UNSAFE LIGHTS REMAINED ILLUMINATED, GEAR DOOR LIGHT EXTINGUISHED. ACCOMPLISHED QRH PROCEDURE WITH NO CHANGE IN INDICATIONS. ACP BITE CHECK OF PSEU, CLEANED LANDING GEAR HANDLE SWITCH S1-89 AND THROTTLE GEAR SWITCHES. OPS CHECK GOOD. 2L72 4F4 F A6WE E2EA 20041221000532004122100053NM 2004 12 21 ASA0440179 120041008A53406940367 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 OKC - CRACKED STRINGER CLIP. REMOVED AND REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E21EU 20041221000652004122100065SO 2004 12 21 SIMA200432903 120041118A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21627AE 145121 DURING AN MBV INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER SHIMS. REPAIR DONE IAW SRM. 2L72 4T4 FRTT00011ATTE6CH 20041221000782004122100078SO 2004 12 21 SIMA200432204 120041106A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK 145371 THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AND INSTALLED AN EXTERNAL DOUBLER. REPAIR DONE IAW SRM. (SW21200501189) 2L72 4F4 FRTT00011ATTE6CH 20041221000802004122100080 2004 12 21 GTIA040848 420041116A2565 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE ESCAPE SLIDE MISROUTED A GTIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL23836NK 53045 R1 SLIDE GIRT BAR SLIDE PACK LANYARD NOT ROUTED PROPERLY. RE-ROUTED R1 SLIDE GIRT BAR LANYARD. 2L72 4F4 FRTA6WE E2EA 20041221000872004122100087NM 2004 12 21 USAA040892 120041015A53401133422 STRINGER CLIP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT- Q5- STRINGER TIE CLIP, 1.25 INCH CRACK, BS 360, STR 4, RT. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20041221001032004122100103EU 2004 12 21 A6WA200460056 120041116A5755 LONGERON BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE RT AIRBRAKE CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31292UE E2087 CHAFING ON THE RT AIRBRAKE UPPER HINGE CUTOUT UPPER LONGERON. MAINTENANCE REQUESTED REPAIR. 2H74 4F4 F A49EU E6NE 20041221001072004122100107NM 2004 12 21 AMTA200401424 120041120A2410 LINE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE IDG OIL LEAKING A AMTAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 GL11516AT 27972 ON POSTFLIGHT WALKAROUND, FOUND OIL LEAK ON NR 2 IDG. REMOVED AND REPLACED IDG OIL FEED LINE IAW MM. OPS CHECKED NORMAL, NO LEAKS NOTED. 2L72 4F4 FRTA2NM E12EU 20041221001102004122100110SO 2004 12 21 SIMA200429603 120041015A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21833AE 145629 DURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, PLATE AND 2 SHIMS FOR REPAIR. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221001202004122100120EA 2004 12 21 ASOA04899 120041113A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7515 7513 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221001262004122100126NM 2004 12 21 USAA040856 120041030A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT - Q4 - FRAME, .2500 INCH CRACK. CRACK EMANATING FROM FASTENER, FRAME STA 867 AND STR 9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041221001272004122100127SO 2004 12 21 SIMA200429811 120041014A532014522461003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE LT OMEGA BEAM BETWEEN FRAMES 33 AND 34 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE DAMAGED AREA OF THE LT OMEGA BEAM. FABRICATED AN EXTERNAL ANGLE FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001342004122100134SO 2004 12 21 SIMA200431507 120041104A532014525381 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR 145368 DURING AN IMBV INSPECTION THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 32 AND 43. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND AN EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW21200501161) 2L72 4F4 FRTT00011ATTE6CH 20041221001372004122100137EA 2004 12 21 A6WA200440199 120041202A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31443AW 7781 THE LT AND RT SIDE UNDER FLOORBEAM STRUCTURE IS CRACKED AT FSL73, LBL40 AND RBL40. REMOVED CRACKED AREA AND INSTALLED REPAIR PARTS IAW REO. 2L72 4F4 FRTA21EA E15NE 20041221001402004122100140WP 2004 12 21 GTIA040818 120041017A3230 RETRACT CYLINDER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT MLG OUT OF ADJUST A GTIAO OTHER J WARNING INDICATION CLCLIMB 1 GL23817NK 49141 AFTER TAKEOFF, RT MAIN GEAR RED LIGHT REMAINED ON WITH GEAR HANDLE UP. FOLLOWED PROCEDURE IN QRH AND CONSULTED WITH MECHANIC CONTROL. CONTINUED TO DESTINATION AT REDUCED SPEED IAW QRH. ON DESCENT IN TPA AT 10,000 PRIOR TO EXTENDING LANDING GEAR, RED LIGHT WENT OUT. ALL OTHER INDICATIONS WERE NORMAL DURING FLIGHT. FOUND RT MAIN GEAR RETRACT CYLINDER OUT OF ADJUSTMENT. ADJUSTED AND SECURED IAW MM 32-32-04. OPS CHECK GOOD. PERFORMED BITE CHECK OF PSEU IAW MM 32-60-00. BITE CHECK TESTS GOOD. 2L72 4F4 F A6WE E9NE 20041221001562004122100156NM 2004 12 21 ASA0440191 120041026A531565C339482 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED UPPER FLANGE OF FLOORBEAM, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20041221001662004122100166 2004 12 21 KBM2004F00238 420041008A34242202403 INDICATOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TURN & BANK INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH828 2337 TURN AND BANK INOPERATIVE, REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20041221001672004122100167WP 2004 12 21 GTIA040816 120041017A5240 SPRING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE SERVICE DOOR BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23820NK 49126 R1 SVC, DOOR BAYONET ROLLER HELICAL TORSION SPRING BROKEN. REMOVED AND REPLACED R1 DOOR BAYONET ROLLER HELICAL TORSION SPRING. OPS CHECK GOOD IAW 52-41-00. 2L72 4F4 F A6WE E9NE 20041221001822004122100182EU 2004 12 21 ASOA04871 120041102A3350 POWERPACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT MALFUNCTIONED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27637AS 383 DURING A GROUND INSPECTION, THE FORWARD HALF OF EMERGENCY FLOOR LIGHTING ON THE RT SIDE WOULD NOT EXTINGUISH. MAINTENANCE RESET THE EMERGENCY LIGHT POWER PACK SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041221001852004122100185NM 2004 12 21 USAA040922 120041031A2120 DUCT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RAM AIR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US 24557 PIT - Q1 - AIR DUCT, .5 INCH CRACK, LT RAM AIR DUCT UPPER SIDEWALL AT STA 540 AND S-22L. INSTALLED DOUBLER IAW TYP REP 53-50-03. 2L72 4F4 FRTA16WE E21EU 20041221001862004122100186NM 2004 12 21 USAA040851 120041021A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME, .1250 INCH CRACK, CRACKED AROUND RIVET AT FRAME AT STA 827, STR 9L. REMOVED CRACK AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20041221001872004122100187CE 2004 12 21 GUU2004F00041 120041119A55201016200111 BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO178154619047 UE187 AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20041221001892004122100189SO 2004 12 21 SIMA200431004 120041028A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21736DT 145388 DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT SECTION OF THE DAMAGED BEAM. FRABRICATED EXTERNAL ANGLE, FILLER AND SHIMS. REPAIR DONE IAW SRM. (SW21200501158) 2L72 4F4 FRTT00011ATTE6CH 20041221001902004122100190CE 2004 12 21 UG8AGM0418 120041208A36201103P0912 SWITCH CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL HP BLEED AIR SYSSTICKING E UG8AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL235113 7500013 TAKEOFF ABORTED, DURING TAKEOFF ROLL DUE TO HP DUCT O PRESSURE CAS (AMBER) MESSAGE ILLUMINATING. CREW COULD NOT DETERMINE WHICH ENGINE PROBLEM OCCURRED ON. THROTTLE WAS PULLED BACK IMMEDIATELY. TRIP WAS PUT ON ANOTHER AIRCRAFT. SB COMPLIED WITH. MAINT GROUND RUN OF LT AND RT ENGINES AT FULL TAKEOFF POWER WITH ANTI-ICE ON. CYCLED ANTI-ICE ON AND OFF AT FULL POWER SETTINGS. COULD NOT DUPLICATE PROBLEM. DOWNLOADED CAS MESS FROM IMT, DETERMINED THAT DUCT O PRESSURE INDICATION WAS ON LT ENGINE. INSP AND FUNCTIONALLY CHECKED CKD LT, RT DUCT O PRESS SWITCHES. LT SWITCH WAS FOUND, NORMAL. RT SWITCH WAS FOUND TO HAVE STICKY CONTACT. REPLACED RT O PRESS SWITCH. OPS CKD GOOD, AC WAS RETURNED TO SERVICE. 2L72 4J4 FRTT00007WITE6CH 20041221001912004122100191EU 2004 12 21 ASOA04921 120041102A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE TOP FLANGES OF FLOORBEAMS 38 AND 40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM TOP FLANGES IAW 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041221001942004122100194SO 2004 12 21 SIMA200431002 120041030A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21736DT 145388 DURING AN IMBV INSPECTION THE GALLEY FLOOR AREA FORWARD DIGITAL WAS FOUND CORRODED. REMOVED THE EXISTING FORWARD DIGITAL. INSTALLED NEW DIGITAL. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221001952004122100195NM 2004 12 21 AMTA200401383 120041107A335020131A BATTERY PACK BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 ALL EMERGENCY LIGHT THAT OPERATES OFF OF POWER SUPPLY/ BATTERY PACK M731, INOPERATIVE. REMOVED AND REPLACED M731 BATTERY PACK IAW AMM 33-51-07-2, OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20041221001962004122100196SO 2004 12 21 SIMA200432207 120041103A532014525480003 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CARGO FLOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR8514 145368 IMBV - CARGO DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. INSTALLED NEW CARGO DOOR CUT OUT LOWER SILL IAW SRM AND CPM. (SW21200501181) 2L72 4F4 FRTT00011ATTE6CH 20041221001972004122100197NM 2004 12 21 UIEA200400201 120041209A78101313M56G01 STRUCTURE BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE NR 4 ENGINE MISSING A UIEAK NONE O OTHER ININSP/MAINT 1 EA15526MC 22337 POST FLIGHT INSPECTION, FLT EK4979, 07/DEC/2004. DURING INSPECTION, FOUND NR 4 ENGINE AFT CENTER BODY CRACKED OFF. MISSING, LAST 20 INCHES FROM T/E. REMOVED AND REPLACED NR 4 ENGINE AFT CTR BODY IAW MM 78-11-02. INSPECTED AREA AFT OF NR 4 ENGINE FLAPS, WING AND TAIL SECTION. NO DAMAGE FOUND. 2L74 4F4 FRTA20WE E23EA 20041221001982004122100198CE 2004 12 21 O2G2004F00009 120040611A2613355843255 OVERHEAT LOOP LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE TAIL COMPT MALFUNCTIONED E O2GAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE0314TU 3714 026 DURING DEPARTURE, BOTH RED BLEED AIR LIGHTS ILLUMINATED. TURNED RT BLEED AIR SWITCH OFF, LIGHTS STAYED ON. TURNED RT BLEED AIR SWITCH ON, TURNED 1 BLEED AIR SWITCH OFF, LIGHTS STAYED ON. WITH RT BLEED AIR SWITCH ON AND RT ENGINE TO IDLE AND LEFT BLEED AIR SWITCH OFF, THERE WAS NO CHANGE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. DURING DESCENT THRU 8000 FT, SHUT OFF BOTH LEFT AND RT BLEED AIR SWITCHES. MET CABIN AT 4000 FT BOTH LT AND RT BLEED AIR LIGHTS EXTINGUISHED AT ABOUT 2000 FT ON APPROACH. DURING TROUBLESHOOTING FOUND TAIL COMPARTMENT OVERHEAT DETECTION LOOP CONTACTING DUCT CAUSING A FAULT INDICATION. REPOSITION OVERHEAT DETECTOR LOOP IAW MFG MM. 2L72 4F4 FRTA10CE E35NE 20041221002002004122100200SO 2004 12 21 SIMA200432210 120041103A532014522178 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR 145368 THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED CORRODED CENTER DOOR SILL. INSTALLED NEW SILL IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221002032004122100203NM 2004 12 21 USAA040928 120041030A5340 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - ATTACH CLIP, .5 INCH CRACK, STA 706, STR 1. REMOVED AND REPLACED WITH INDENT PART IAW SRM 51-40-02 AND 51-40-03. 2L72 4F4 FRTA16WE E21EU 20041221002042004122100204NE 2004 12 21 B2O2004F00000 220040826A8530 CYLINDER DOUG DC4 C54G 3021536WP PWA R2000 R2000* 52023NE HAMSTD23E 23E50 NE NR 6 CRACKED I B2OBO OTHER O OTHER NRNOT REPORTED 1 AL0151802 650 35930 106102 NR 6 CRACKED CYLINDER AND TRIANGLER PIECE CAME OUT, MELTED OIL CROSSOVER TUBE CAUSING SMALL OIL FIRE. FIRE WARNING ZONE 1 WENT ON, SHUT ENGINE DOWN, FIRE WENT OUT. 2L74 4R4 R A762 5E5 6 CP603 20041222000012004122200001WP 2004 12 22 GTIA040830 120041102A3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE MLG DIRTY A GTIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23826NK 49391 LP NR 281684-1; QRH PROCEDURE; AFTER TAKEOFF, LT GEAR RED LIGHT WAS ON, FOLLOWED QRH PROCEDURE. CLEANED DIRTY PROX SENSOR FOR LT LANDING GEAR AND CHECKED GENERAL CONDITION OF UP LOCK PROX SENSOR AND FOUND TO BE OK. PERFORMED PSEU TEST. OPS CHECK NORMAL. CHECKED GAP LIMITS AND FOUND WITHIN LIMITS. 2L72 4F4 FRTA6WE E9NE 20041222000022004122200002CE 2004 12 22 DXTA200400482 120041218A2913 PUMP CESSNA750 750 2076810CE A-HYD SYSTEM FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07966QS 7500166 DURING FLIGHT HYDRAULIC A-PUMP FAILED, HYDRAULIC -B- OVERTEMP BLEW GEAR DOWN AND USED MANUAL BRAKES ON LANDING. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20041222000032004122200003CE 2004 12 22 DXTA200400486 120041219A3260 INDICATOR CESSNA500 560CESSNA 2076750CE MLG INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07806QS 5600614 NO GREEN LIGHT ON LEFT MAIN LANDING GEAR WHEN SELECTED DOWN. INTRANSIT LIGHT ON, HYD PRESS LIGHT OFF, GEAR UNSAFE WARNING HORN ON. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20041222000052004122200005 2004 12 22 SWAA043654 420041217A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20041222000092004122200009NM 2004 12 22 AWXA200401413 120041129A5210654587113 SKIN BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .0312 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN AT UPPER HINGE CUTOUT BS 310, STR 10 RT. MAINTENANCE TRIMMED OUT CRACK, FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-04350-HF1. 2L72 4F RTA16WE 20041222000102004122200010WP 2004 12 22 WX0400064 120041218A3350 BULB DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19862GA 49556 LAS - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS AT ROW 8 AND ROWS 23 THROUGH 32 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULBS IAW 33-51-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041222000112004122200011NM 2004 12 22 SWAA043667 120041217A3350D71701100 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED 5Y CHECK, FOUND LT AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041222000132004122200013NM 2004 12 22 04FDEA03444 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 832 TO 899 RT NR 2 SEAT TRACK AREAS FOUND WITH CORROSION. REMOVED SEAT TRACK FASTENERS AT MAIN DECK: STA Y = 810 TO STA 910 AS PER SRM 51-31-01 VOL II. SEAT TRACK AT RT NR 2 STA 810 AND STA 910 CUT OUT AS PER SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 VOL II. INSTALLED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041222000142004122200014NM 2004 12 22 04FDEA03440 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 859 TO 879 LT MOST OUTBOARD SEAT TRACK FOUND WITH EVIDENCE OF CORROSION. TRIMMED OFF AS PER SRM 53-70-00 FIG 1 VOL I. SEAT TRACK AND SPLICES FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I AND INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041222000162004122200016NM 2004 12 22 04FDEA03450 120041220A5510 STRUCTURE BOEING727 727100 1384036NM HORIZONTAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 N01259 RT HAND HORIZONTAL STAB L/E UPPER CHORD CRACKED ON LWR SURFACE BETWEEN L/E STAB STA 1.0 TO L/E STAB STA 72.0. FOUND RT HORIZ STAB L/E UPR CHORD OUT OF LIMITS. TRIMMED OUT SEGMENT OF CHORD, FABRICATED NEW CHORD FROM REF. PO 179160, SPLICE FROM BAC1490-2811 & 7075T6, 586206, 7075T6 .071 514703. ALODINE, PRIMED AND INSTALLED UPR CHORD AND SPLICE REPAIR PER SRM 55-10-5, 51-30-5, 51-30-2. 2L73 4F RTA3WE 20041222000172004122200017NM 2004 12 22 SWAA043673 120041219A53106546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, STRINGER 27L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041222000182004122200018NM 2004 12 22 CALA0400749 120041218A5414301A3109 PANEL BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2761304 23355 INSPECTION FOUND TWO 1 INCH CRACKS IN NR 2 PYLON PANEL CUTOUT 5824R. THE CRACKS WERE LOCATED AT UPPER FORWARD CORNER OF PANEL. ONE CRACK ORIGINATED FROM RIVET HOLE FOR RUB STRIP AND THE OTHER WAS ON FAYING SURFACE FOR ACCESS PANEL. 2L72 4F RTA16WE 20041222000192004122200019NM 2004 12 22 2004UALA01206 120041211A5310 STRUCTURE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 MAIN CABIN AT STA 1640 & RBL 8 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED "J" ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041222000202004122200020NM 2004 12 22 2004UALA01212 120041214A5320 SILL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT CARGO DOOR SILL FS 1380 TO 1440 IS CORRODED. 2L72 4F4 FRTA2NM E17NE 20041222000212004122200021 2004 12 22 2004UALA01217 420041214A2565 GIRT BAR BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29509UA 24763 SLIDE WOULD NOT ARM BY GIRT. INSPECTION SHOWS GIRT WAS OPERATIONAL. THE PACKBOARD CAME IN WITH MAJOR DAMAGE. GIRT WAS CHECKED FOR CORRECT POSITIONING AND LENGTH PER P-11886 PACKING MANUAL. SLIDE HAS NO RECENT HISTORY OF GIRT REPAIR. NO CAUSE FOR REPORTED DISCREPANT SLIDE ARMING WAS FOUND. SLIDE APPEARS TO HAVE BEEN DROPPED DURING HANDLING, CAUSING DAMAGE TO PACKBOARD CORNER. PACKBOARD WAS REPLACED AND SLIDE MADE SERVICEABLE. 2L72 4F4 FRTA2NM E17NE 20041222000222004122200022NM 2004 12 22 2004UALA01222 120041215A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 SHEAR TIE CORRODED BEYOND LIMITS AT STA 1400. INSTALLED NEW SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20041222000232004122200023 2004 12 22 2004UALA01226 420041216A2565 ASPIRATOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE MISINSTALLED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29197UA 26901 CRACKED UPPER TUBE ASPIRATOR. ASPIRATOR DAMAGED DUE TO IMPROPER PACKING DURING PREVIOUS OVERHAUL. REPLACED ASPIRATOR. 2L74 4F4 FRTA20WE E24NE 20041222000242004122200024NM 2004 12 22 QXEA200400885 120041213A5710 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT HAND WING, BETWEEN STATION YW 155.2-173.2. REPAIRED IAW HORIZON AIR EA 6-57-268 AND RD 8/4-57-399. 2H72 4T RTA13NM 20041222000282004122200028EA 2004 12 22 MASA200400702 120041217A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW0775987 7405 N75987 WAS ON RON LAST NIGHT AND SCHEDULED FOR A SERVICE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THAT THE RIGHT SIDE OVERWING EXTERIOR EMERGRNCY LIGHT WAS NOT ILLUMINATING. REPLACED THE LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222000292004122200029SO 2004 12 22 1398121804 120041218A56101159SCB310213 WINDSCREEN GULSTMG1159 GIV 3980115SO COCKPIT CRACKED E N93AO OTHER O OTHER DEDESCENT 1 SO13498QS 1398 WINDSHIELD OUTER PANE SHATTERED ON DESCENT. 2L72 4F RTA12EA 20041222000302004122200030NM 2004 12 22 04FDEA03439 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK - SEAT TRACK RBL 27 CORRODED AT STA 1831 TO STA 1887. SEAT TRACK CUT AND REMOVED AS PER SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 VOL II. INSTALLED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II.. 2L73 4F RTA22WE 20041222000342004122200034NM 2004 12 22 2004UALA01221 120041215A5310 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 SHEAR TIE IS CORRODED BEYOND LIMITS AT STA 1400 BETWEEN STR 30 AND 29R. REPLACED SHEAR TIE. 2L72 4F4 FRTA2NM E17NE 20041222000352004122200035NM 2004 12 22 DL75A041107 120041216A5330146N35317 SKIN BOEING757 757212 1384951NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27751AT 23125 FUSELAGE SKIN DENTED AND REPAIR REPLACEMENT AT STATION 1505 AND STR 28L. REPAIRED IAW ERA 095225-14. 2L72 4F RTA2NM 20041222000362004122200036NM 2004 12 22 DL767041108 120041216A2612261780107 CIRCUIT CARD BOEING767 767232 1385132NM FIRE WARNING INTERMITTENT A DALAO OTHER N FALSE WARNING APAPPROACH 1 SO27106DA 22218 INTERMITTENT FWD CARGO FIRE LIGHT PLUS BELL CAME ON DURING TAXI IN. REPLACED FIRE CARD M10427 IN P-54 PANEL. SYSTEM CHECKS NORMAL PER M/M. PER CVG FIRE DEPT, NO EVIDENCE OF SMOKE, ODOR, OR FIRE FOUND. 2L72 4F RTA1NM 20041222000372004122200037NE 2004 12 22 DL777041109 220041214A7320TRENT892 ENGINE BOEING777 777232 1385232NM RROYCERB211 RB211TRENT89 NE NR 1 MALFUNCTIONED A DALAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO27861DA17568 29952 051175 ON TAXI OUT ENG CONTROL L EICAS MSG THEN EXTINGUISHED. AFTER CLEARED FOR T/O ENG CONTROL EICAS MSG RETURNED. LEFT ENGINE DID NOT ACCELERATE NORMALLY. T/O DISCONTINUED AT 17.5 KTS. RETURNED TO GATE. CHECKED VSV FOR FREEDOM OF MOVEMENT. CKS GOOD PER M/M 75-33-00. CORE COWLS REMOVED. REMOVED AND REPLACED ENGINE ON TRANS 11T003. ENGINE CHANGE COMPLETED PER TRANS 11T003. 2L72 4F4 FRTT00001SEE00050EN 20041222000382004122200038NM 2004 12 22 DL73S041110 120041216A3397 WIRE BOEING737 737232 1384475NM EMERGENCY LIGHT PULLED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27334DL 23105 SEAT ROW EMERGENCY LIGHT AT 18DEF INOP, HAS WIRED PULLED OUT OF CONNECTOR. REPLACED EMERGENCY LIGHT ON 18DEF SEAT ROW. 2L72 4F RTA16WE 20041222000392004122200039NM 2004 12 22 DL73S041111 120041216A3350 BULB BOEING737 737232 1384475NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27334DL 23105 EMERGENCY LIGHT BELOW OVERHEAD BIN AT ROW 1 ABC INOP. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA16WE 20041222000402004122200040NM 2004 12 22 DLM88041112 120041217A3610 DUCT DOUG MD88 MD88 3023688NM APU CONTAMINATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27918DE 49959 SMOKE ALARM AND ODOR IN RIGHT AFT LAV AFTER T/O RETURNED TO ATL. PERFORMED DUCT BURNOUT. 2L72 4F RTA6WE 20041222000442004122200044NM 2004 12 22 04FDEA03443 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA 840 TO 879 RT NR 1 SEAT TRACK & FLANGE AREAS FOUND WITH CORROSION. CORRODED SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR SEAT TRACK PARTS AS PER SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20041222000452004122200045 2004 12 22 2004F00433 420041221A34604010455000101 DISPLAY DHAV DHC2 DHC2* 2800108EA COCKPIT MALFUNCTIONED B O OTHER O OTHER NRNOT REPORTED 1 AL0547AK 726 DISPLAY HAS AN INTERMITTENT LINE ACROSS MIDDLE OF SCREEN. 1H71 3R A806 20041222000462004122200046NM 2004 12 22 QXEA200400897 120041216A3297471515 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09407QX1749 1749 4049 PDX - FLIGHT 2416 - FLIGHT RETURNED TO FIELD WHEN DURING THE CLIMB, THE GEAR FAILED TO RETRACT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NOSE LANDING GEAR WOW 2 CENTERING HARNESS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222000472004122200047NM 2004 12 22 AWXA200401410 120041202A5330654577678 SKIN BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 767 AND BS 787, WHERE FORWARD FLIGHT PHONE ANTENNA WAS LOCATED. MAINTENANCE CUT OUT CORRODED FUSELAGE SKIN FROM BS 767 TO BS 787; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20041222000482004122200048 2004 12 22 2004F00434 420041221A34614010455000101 DISPLAY DHAV DHC2 DHC2* 2800108EA COCKPIT INOPERATIVE B O OTHER O OTHER NRNOT REPORTED 1 AL0547AK 726 ATTEMPTED TO INSTALL 5.0 SOFTWARE, SCREEN WENT BLANK HALFWAY THROUGH UPGRADE. 1H71 3R A806 20041222000502004122200050NM 2004 12 22 AWXA200401408 120041112A5330654577572 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 PERFORM PERMANENT REPAIR ON CRACKED SKIN BS 787, STR 22 RT. MAINTENANCE REMOVED TEMPORARY REPAIR ON CRACKED FUSELAGE SKIN AT BS 787, STR 22 RT; FABRICATED A REPAIR DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01 FIG 229. 2L72 4F RTA16WE 20041222000512004122200051NM 2004 12 22 AWXA200401409 120041207A5310141N516078 SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SUPPORT STRUCTURE AT RBL 60 BETWEEN BS 350 AND BS 365.25. MAINTENANCE REMOVED CORRODED SUPPORT STRUCTURE AT RBL 60 FROM BS 350 TO BS 365.25; INSTALLED NEW REPLACEMENT SUPPORT STRUCTURE IAW B757-200 SRM 51-10-02. 2L72 4F RTA2NM 20041222000532004122200053NM 2004 12 22 QXEA200400895 120041217A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNSECURE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09404QX8342 4046 GEG - FLIGHT 2322 - THE FLIGHT DIVERTED TO GEG AFTER RECEIVING A FORWARD CARGO DOOR WARNING. MAINTENANCE INSPECTED THE DOOR AND FOUND THE DOOR HANDLE PROTRUDING .25 INCH. THE HANDLE WAS SECURED AND OPERATIONAL CHECKS WERE PERFORMED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222000592004122200059NM 2004 12 22 04FDEA03438 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 SEAT TRACK RBL 107 CORRODED AT STA 1929 TO STA 2000. REMOVED AND REPLACED WITH NEW SEAT TRACK AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041222000602004122200060CE 2004 12 22 DXTA200400484 120041218A3220 LANDING GEAR CESSNA750 750 2076810CE NOSE MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07938QS 7500183 DURING CRUISE FLIGHT AT FL390, THE NOSE WHEEL PARTIALLY EXTENDED AT MACH .90, RED UNLOCK LIGHT ILLUMINATED. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20041222000632004122200063CE 2004 12 22 DXTA200400485 120041218A2910 LINE CESSNA500 560CESSNA 2076750CE HYDRAULIC SYS FAILED E DXTAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL07810QS 5600625 RIGHT BRAKE PEDAL ON PILOTS SIDE WENT TO THE FLOOR AND RIGHT BRAKE WOULD NOT HOLD AIRCRAFT WHILE TRYING TO DO BRAKE BURN IN. INSPECTED RIGHT BRAKE ASSY, NO DEFECTS NOTED. BLED ANTI SKID BRAKING SYSTEM. NOTED SOME AIR IN SYSTEM. BLED RT SYSTEM AGAIN. SYSTEM BLED CHECKS GOOD. ANTI SKID FUNCTION CHECKS GOOD. BRAKE SYSTEM OPS CHECKS GOOD. WORK PERFORMED IAW CHAPTER 32-42-00 OF THE CE 560 MM. 2L72 4F RTA22CE 20041222000652004122200065EA 2004 12 22 QXEA200400888 120041213A5510 BUSHING CNDAIRCL600 CL6002C10 1390015EA ZONE 300 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - HORIZONTAL STAB RIGHT HINGE BUSHING CHAFED INTO ANTI ROTATION LUG ON STABILIZER FITTING. REPAIRED IAW HORIZON AIR EA R-55-27 AND REO 670-55-11-016. 2L72 4F RTA21EA 20041222000672004122200067NM 2004 12 22 DL73S041119 120041218A2913623337 PUMP BOEING737 737247 138448DNM A-HYD SYSTEM FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27373DL 23520 LOSS OF A-SYSTEM HYDRAULIC PRESSURE IN FLIGHT. REPLACED BOTH ENGINE PUMPS DUE A-SYSTEM CONTAMINATION. 2L72 4F A16WE 20041222000692004122200069WP 2004 12 22 WX0400065 120041218A33506011779 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19864GA 49912 LAS - MAINTENANCE REPORTED OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PACK IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041222000712004122200071EA 2004 12 22 SWIA200414273 120040924A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 FLOORBOARD MOUNT BRACKET COMMON TO THE AFT PRESSURE BULKHEAD AT FS 621, LBL 41 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE BRACKET AND SPLICE IAW EO 601R-53-5479. 2L72 4F RTA21EA 20041222000732004122200073SO 2004 12 22 SWIA200414275 120041215A2121AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203SO CABIN COOLING FAILED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07587335978 2753 120197 AFTER APU START, AND START UP OF PACKS NOTED A SMOKE ODOR. REMOVED AND REPLACED LEFT GROUND COOLING FAN IAW MM REF 21-20-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222000742004122200074SO 2004 12 22 SWIA200414276 120041215A27503075001017 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM0758733340 340 120197 WHEN SELECTING FLAPS 25 ON FINAL, RECEIVED A FLAP CONTROL FAULT. REMOVED AND REPLACED FCU. OPERATIONAL CHECK GOOD, REF 27-50-06. 2L72 4T RTA31SO 20041222000752004122200075EA 2004 12 22 04352629 120041217A3241 TIRE CNDAIRCL600 CL6002B19 1900309EA MLG FAILED A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27629BR 7251 BLOWN TIRE ON TAKEOFF. PAX DEPLANED ON TAXIWAY. MX CHANGED TIRE. THEN CHANGED AGAIN, DUE TO SKYDROL CONTAMINATION. 2L72 4F RTA21EA 20041222000762004122200076CE 2004 12 22 DXTA200400480 120041214A3240CV02259 CHECK VALVE CESSNA500 560CESSNA 2076750CE BRAKES FAILED E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07324QS 5600423 RIGHT BRAKE PEDAL ON CO-PILOT SIDE WAS MUSHY AND THEN WENT COMPLETELY TO THE FLOOR DURING TAXI. REMOVED AND REPLACED CHECK VALVE. BLED BRAKES IN ACCORDANCE WITH CE560 MM 32-42-00. OPERATIONAL CHECK GOOD. 2L72 4F RTA22CE 20041222000772004122200077NM 2004 12 22 BB04094 120041219A2121 COOLING FAN BOEING757 7572B7 1384964NM E/E BAY FAILED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19611AU 27123 CLT FLT 979 SHORTLY AFTER DEPARTURE, THE CREW NOTICED AN ELECTRICAL ODOR FOLLOWED BY A EQUIPMENT OVERHEAT WARNING ON THE EICAS DISPLAY. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DID NOT FIND A DEFINITIVE SOURCE OF THE PROBLEM AND REPLACED THE NR 1 EQUIPMENT COOLING FAN, THE OVERBOARD EXHAUST VALVE, EQUIPMENT COOLING LOW FLOW SENSORS AND THE SMOKE DETECTOR. ALL PARTS WERE CHANGED AS A PRECAUTION. 2L72 4F RTA2NM 20041222000812004122200081EU 2004 12 22 0402183265 120041214A5320 FLOOR SUPPORT AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01365NW 0964 DURING H-CHECK FOUND CORROSION ON THE RT OUTBOARD FLOOR SUPPORT AT FR 66. REPAIRED PER EA 32-201979. 2L72 4F RTA28NM 20041222000822004122200082NM 2004 12 22 SWAA043660 120041217A33501010731 LENS BOEING737 7373K2 13844BANM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2L72 4F RTA16WE 20041222000852004122200085NM 2004 12 22 SWAA043671 120041217A52106552873 SKIN BOEING737 7373H4 1384600NM DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR SKIN AT LOWER FWD RADIUS CRACKED. REPAIRED DOOR SKIN PER SRM. 2L72 4F RTA16WE 20041222000862004122200086NM 2004 12 22 SWAA043672 120041219A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, FROM LBL 12 TO RBL 14, CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20041222000892004122200089NM 2004 12 22 DL764041123 120041219A3350 BULB BOEING767 767432ER 1385134NM EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27834MH 29707 ON TRANSIT CHECK FOUND 3 EACH OVERHEAD EMERENGCY EXIT LIGHTS INOP. RELAMPED EMERGENCY EXIT LIGHTS, OPERATION OK. 2L72 4F RTA1NM 20041222000902004122200090EA 2004 12 22 SWIA200414282 120041211A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07703SK 10139 OUTBOARD SPOILERONS & OUTBOARD GROUND SPOILERS CAUTION MESSAGE. REMOVED AND REPLACED NR 2 SSCU IAW CRJ MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222000922004122200092 2004 12 22 UPS04143612 420041218A2565 SWITCH AIRBUSA300 A300F4622R 3930360EU ESCAPE SLIDE DIRTY A IPXAK NONE O OTHER ININSP/MAINT 1 SO01133UP 0816 HAD TO CYCLE THE ESCAPE SLIDE ARMING LEVER SEVERAL TIMES TO INDICATED PROPER SLIDE, ARMED AND DISARM ON ECAM DOOR GAGE. ITEM DEFERRED ON M293373 PER MEL 52-30-04 PLACARD INSTALLED. T/S FOUND ESCAPE SLIDE SWITCH 13WN STICKING. CLEANED SWITCH. SYSTEM OPS CK GOOD. PER MM 52-73-13-5 PLACARD REMOVED. 2L72 4F RTA35EU 20041222000942004122200094NM 2004 12 22 UPS04643614 120041219A4910 APU BOEING767 76734AF 1385212NM APU BAY INOPERATIVE A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01305UP 27243 LT GEN DRIVE LIGHT IN FLIGHT. APU FAULTED TWICE IN FLIGHT, DID NOT START. CREW DIVERTED TO NEAREST SUITABLE AIRPORT (DNA). DECLARED EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. LT IDG DEFRD DMI 293462. PER FIM 24-11-00 REPLACED LH IDG & OPS CHECKED NORMAL AS PER MM 24-11-00-5. A/C OK FOR SERVICE CLEARD DMI 293462 AND REMOVED PLACARD. 2L72 4F RTA1NM 20041220001822004122000182SO 2004 12 20 RAIA00412013 120041211A2910156221 PRESSURE SWITCH EMB 145 EMB145LR 3260212SO NR HYD SYSTEM MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03818HK14659 145059 STL - NR 1 HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 1 PRESSURE SWITCH. 2L72 4T RTT00011AT 20041220001902004122000190NM 2004 12 20 ASA0440219 120041029A533065C3236511 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 NUMEROUS GOUGES ON SKIN BELOW AFT CARGO THRESHOLD. BLENDED GOUGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20041220001912004122000191NM 2004 12 20 AMTA200401435 120041124A3350 CONNECTOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT UNSECURE A K NONE L NO TEST ININSP/MAINT 1 GL11522AT 29330 EGRESS LIGHTS INOPERATIVE FROM ROW 5 THRU ROW 9. FLOOR ESCAPE PATH. SECURED CONNECTOR AT ROW 5 EGRESS LAMP. EGRESS PATH LIGHTING OPS CHECKS GOOD. 2L72 4F4 FRTA2NM E12EU 20041220001922004122000192NM 2004 12 20 USAA040906 120041122A5320 INTERCOSTAL BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU 27123 CLT - C-4 - INTERCOSTAL, 1 INCH BY 1 INCH, CORROSION STA 1640 TO 1660, RBL 57. REPLACED INTERCOSTAL. 2L72 4F4 FRTA2NM E12EU 20041220001932004122000193NM 2004 12 20 USAA040903 120041103A5551 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU HORIZONTAL STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 HORIZ STAB CENTER SECTION THRUST BEAM ATTACH ANGLE RT SIDE. REMOVED AND REPLACED ANGLE IAW TYP REP REMOVED AND REPLACED SRM 51-00-30. 2L72 4F4 FRTA16WE E21EU 20041220002072004122000207NM 2004 12 20 ASA0440171 120041001A53306545775 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - LIGHTNING STRIKE ON FUSELAGE SKIN. REPAIRED LIGHTNING STRIKE. 2L72 4F4 FRTA16WE E21EU 20041220002212004122000221 2004 12 20 GTIA040844 420041110A2565 GIRT BAR DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE L2 DOOR SHORT A GTIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL23810NK 48015 SAS NR B00182-05N-11136; L2 DOOR EMERGENCY SLIDE DID NOT DEPLOY PROPERLY. FOUND L2 DOOR SLIDE GIRT BAR TOO SHORT, REMOVED AND REPLACED GIRT BAR. 2L72 4F4 F A6WE E9NE 20041221000052004122100005SO 2004 12 21 SIMA200430304 120040823A532014521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21830AE 145615 DURING AN MBV INSPECTION, THE OMEGA BEAM WAS FOUND CORRODED THROUGH AT FRAME 20 WHERE CROSSBEAM CONNECTS. REPAIRED OMEGA BEAM AT FRAME 20 IAW SRM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159) 2L72 4F4 FRTT00011ATTE6CH 20041221000232004122100023NM 2004 12 21 ASA0440202 120041029A53116546529 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT RT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20041221000402004122100040WP 2004 12 21 GTIA040838 120040929A5730 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT WING CHAFED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 LT WING L/E CHAFED ON EXTERNAL SURFACE AT STA XRS 240, XRS 164, XRS 137. BLENDED OUT CHAFED AREAS IAW SRM 57-01, FIG 1, MATERIAL LOSS AT XRS 137 AND 240 OUT OF LIMITS, FABRICATED 2EA REPAIR DOUBLERS FROM 7075-T6-.063, LOCATED DRILLED REPAIR DOUBLERS, TREATED, PRIMED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-06B, FIG 14 AND 51-30-5. 2L72 4F4 F A6WE E9NE 20041221000462004122100046WP 2004 12 21 AMTA200401463 120041202A3350 POWERPACK LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE EMERGENCY LIGHT DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11162AT 1220 DURING WALK AROUND, L3 AND L3A DOOR LIGHTS TURN OFF IN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK FOR L3 AND L3A DOOR LIGHTS (EXTERIOR). IAW MM 33-51-03. OK FOR SERVICE. 2L73 4F4 F A23WE E12EU 20041221000512004122100051NM 2004 12 21 USAA040896 120041014A5320 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - ANGLE, .5 INCH CRACK, STA 380 AT STR 15R. FABRICATED REPAIR ANGLE IAW SRM 51-70-11. 2L72 4F4 FRTA16WE E21EU 20041221000942004122100094NM 2004 12 21 USAA040912 120041029A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1- FRAME, 1 INCH CRACK AND .7500 INCH CRACK (2 CRACKS) BS 616 AT S17L AND BS 616 AT S17R. CUT OUT DAMAGE, INSTALLED FILLERS AND NESTED ANGLES IAW TYP REP 53-62-01. 2L72 4F4 FRTA16WE E21EU 20041221000962004122100096EA 2004 12 21 ASOA04911 120041117A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLOOR SUPPORT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7207 DURING C-CHECK, THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT SIDE FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600-53-0105. 2L72 4F4 FRTA21EA E15NE 20041221000982004122100098NM 2004 12 21 USAA040946 120041021A5321 FLOOR PANEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - FLOOR PANEL, 1 INCH BY 5 INCH AREA CORROSION, LEVEL 1; TASK NR C53-107-02, PANEL NR 99, STA 1016. REPLACED FLOOR PANEL NR 99 IAW SRM 51-70-12. 2L72 4F4 FRTA16WE E21EU 20041221000992004122100099EA 2004 12 21 A6WA200440203 120041211A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH LACK OF LUBE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 CREW ESCAPE HATCH, OUTER HANDLE FROZE IN POSITION, WILL NOT DEPLOY. LUBRICATED OUTER HANDLE ASSEMBLY ON CREW ESCAPE HATCH. FOUND TO BE IN GOOD WORKING ORDER IAW CRJ AMM 12-20-52-640-803. (M) 2L72 4F4 FRTA21EA E15NE 20041221001022004122100102NM 2004 12 21 USAA040913 120041022A53201123372 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1- CLIP, .1250 INCH CRACK AT STA 663.75 AND STR S-10R. REMOVED AND REPLACED CLIP IAW SRM 51-40-03. 2L72 4F4 FRTA16WE E21EU 20041221001092004122100109SO 2004 12 21 SIMA200432212 120041109A491012036982501 MOUNT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL APU COWLING DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21734EK8574 145371 IMBV- THE APU COWLING LT LOWER MOUNT FRAME WAS FOUND TO BE CRACKED. REMOVED DAMAGED MOUNT FRAME. INSTALLED NEW MOUNT IAW SRM. (SW21200501189) 2L72 4F4 FRTT00011ATTE6CH 20041221001212004122100121EU 2004 12 21 ASOA04900 120041114A33503011162 COVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EMERGENCY LIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING A GROUND INSPECTION, THE RT FWD FLOOR LEVEL EMERGENCY EXIT LIGHT COVER WAS FOUND MISSING. MAINTENANCE REPLACED THE RT FORWARD FLOOR LEVEL EMERGENCY EXIT LIGHT COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20041221001292004122100129SO 2004 12 21 SIMA200429809 120041009A532014521713003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION THE GALLEY AREA CENTER HAT BEAM WAS FOUND CORRODED. REMOVED GALLEY AREA CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20041221001302004122100130 2004 12 21 GTIA040811 420041011A2565 CABLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE SLIDE MISROUTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 R1 SLIDE INFLATION CABLE NOT ROUTED THROUGH GROMMET TAB. RE-ROUTED CABLE. 2L72 4F4 F A6WE E9NE 20041221001472004122100147SO 2004 12 21 SIMA200431504 120041105A532014521721009 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR 145368 DURING AN IMBV INSPECTION THE LT SIDE OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY CUTTING OUT A SECTION OF THE FORWARD DIDITAL. FABRICATED A DOUBLE. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20041221001482004122100148SO 2004 12 21 SIMA200430303 120040823A534713500439007 SEAT TRACK EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21830AE 145615 DURING AN MBV INSPECTION, THE LT FORWARD IB SEAT TRACK WAS FOUND WITH NUMEROUS AREAS OF CORROSION AROUND SCREW HOLES. MAINTENANCE INSTALLED NEW SEAT TRACK IAW MM. AIRCRAFT RETURNED TO SERVICE. (SW21200501159) 2L72 4F4 FRTT00011ATTE6CH 20041221001752004122100175EU 2004 12 21 A6WA200460057 120041116A5310 BEAM BAC 146 146200A 1500266EU LYC ALF502ALF502R5 41580NE FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31292UE E2087 (3) BOLT HOLES ARE ELONGATED ON THE BEAM AT FRAME 45 RT MAINTENANCE REQUESTED REPAIR. 2H74 4F4 F A49EU E6NE 20041221001782004122100178NM 2004 12 21 AMTA200401288 120041016A335020131A BATTERY BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT MALFUNCTIONED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 EMERGENCY LIGHTS FROM ROW 5 TO 15 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AS REQUIRED. OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20041221001812004122100181EU 2004 12 21 KBM2004F00243 120041015A6400355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19313LV978 3296 HALF SHELLS, WORN BEYOND LIMITS, REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20041221001842004122100184SO 2004 12 21 SIMA200431506 120041107A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR 145368 DURING AN IMBV INSPECTION THE LT OMEGA BEAM BETWEEN FRAME 20 AND 22 WAS FOUND CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW21200501161) 2L72 4F4 FRTT00011ATTE6CH 20041221001922004122100192NM 2004 12 21 USAA040923 120041021A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US 24557 PIT - Q1 - FRAME, .2500 INCH CRACK, STA 867 BETWEEN STR 8L AND STR 9L. INSTALLED DOUBLER IAW TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E21EU 20041221001932004122100193NM 2004 12 21 BJNA041004 120041012A3350762624 LIGHT BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE CABIN INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11233TM 23043 AFT EMERGENCY TRACK LIGHT AND BOTTOM AFT EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT STRIP IAW CMM 33-50-01. OPERATIONAL CHECK OK. 2L72 4F4 FRTA16WE E2EA 20041222000062004122200006NM 2004 12 22 CALA0400751 120041219A53206552878U124 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND L-2 DOOR THRESHOLD ZEE ANGLE CORRODED AT STA 907-1006, LBL 58. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20041222000272004122200027EA 2004 12 22 MASA200400696 120041213A335020131A BATTERY PACK CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSDISCHARGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07923FJ 15023 ASH - CABIN EMERGENCY LIGHTS INOP DUE TO BEING LEFT ON BY CREW. AIRCRAFT WAS FERRIED TO PHX WHERE MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD. 2L72 4F RTA21EA 20041222000312004122200031NM 2004 12 22 QXEA200400896 120041219A5100 UNKNOWN BOMBDRDHC8 DHC8401 1390041NM UNKNOWN UNKNOWN A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09413QX 4060 SEA - FLIGHT 2413 - THE FLIGHT RETURNED TO THE GATE AFTER THE PUSHER SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND RESET THE CIRCUIT BREAKERS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222000412004122200041NM 2004 12 22 DL73S041113 120041215A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED CRACKS AT FS 470. THE CRACKS WERE REMOVED WITH A 17 INCH LONG SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095528-14AD. 2L72 4F RTA16WE 20041222000522004122200052NM 2004 12 22 QXEA200400898 120041216A3297471525 WIRE HARNESS BOMBDRDHC8 DHC8401 1390041NM NLG STEERING FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09410QX7434 4053 SMF - FLIGHT 2302 - THE CREW COMPLIED WITH THE CHECKLIST WHEN AFTER GEAR EXTENSION THE NOSE STEERING CAUTION LIGHT ILLUMINATED. MAINTENANCE REPLACED THE NOSE LANDING GEAR STEERING HARNESS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222000722004122200072EA 2004 12 22 SWIA200414274 120040924A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 MAIN CABIN FLOORBEAM ATTACH ANGLE AT FS 461 RBL IS CRACKED AT RADIUS LOCATION. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE BRACKET AND SPLICE IAW REO 601R-53-61-004. 2L72 4F RTA21EA 20041222000782004122200078EA 2004 12 22 04354679 120041219A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAILED A VTZAO OTHER S AFFECT SYSTEMS APAPPROACH 1 EA27679BR 7662 FLAPS FAIL AT ZERO DEGREES ON APPROACH. EMERGENCY DECLARED. FLIGHT LANDED WITH NO FURTHER INCIDENT. A/C STILL IN MX. 2L72 4F RTA21EA 20041222000842004122200084NM 2004 12 22 SWAA043670 120041219A53306545766 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 978, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA. 2L72 4F RTA16WE 20041222000872004122200087 2004 12 22 2004UALA01227 420041215A2565 BOTTLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE ESCAPE SLIDE DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29562UA 26664 ESCAPE SLIDE HAS A LOW BOTTLE. CYLINDER ASSEMBLY GAUGE ADAPTER FITTING O-RING LEAKING. REPLACED O-RING. 2L72 4F4 FRTA2NM E17NE 20041222000882004122200088 2004 12 22 2004UALA01228 420041215A2565 ASPIRATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLIDE BOTTLE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29524UA 24977 LOW BOTTLE PRESSURE. FOUND DURING ASPIRATOR INSPECTION THAT BOTH ASPIRATORS HAD DENTED BARRELS. LOW BOTTLE PRESSURE: CYLINDER ASSEMBLY TEMPERATURE WAS STABILIZED AND GAGE NEEDLE WAS OBSERVED IN CENTER OF GREEN BAND. CYLINDER ASSEMBLY WAS LEAK CHECKED. NO LEAKS DETECTED. ASPIRATORS BARRELS DENTED. NO EXTERNAL SLIDE DAMAGE OBSERVED. SLIDE FOLDING PROCEDURE OBSERVED TO HAVE BEEN CORRECTLY PERFORMED PER AIR CRUISER CMM 25-66-02. IT IS ASSUMED SLIDE PACK WAS OVER-COMPRESSED DURING PACKING PROCEDURE. 2L72 4F4 FRTA2NM E17NE 20041222000912004122200091NM 2004 12 22 QXEA200400894 120041217A5210 SCREW DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR OUT OF ADJUST A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09369PH14267 513 SEA - MAINTENANCE REPORTS THAT THE MAIN CABIN DOOR WILL NOT OPEN. UPON INSPECTION, MAINTENANCE FOUND THE AFT HANDRAIL SCREW TO BE TOO LONG AND DIGGING INTO THE ENTRY DRAFT BULKHEAD PARTITION. THE HANDRAIL SCREW WAS ADJUSTED TO THE PROPER LENGTH AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222000952004122200095EA 2004 12 22 VNAA0411003 120041115A3250530133 TILLER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NLG STEERING FAILED A VNAAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL05705PS1178 10144 THE CREW OF FLIGHT 2239 RECEIVED A STEERING INOP CAUTION MESSAGE ON ROLLOUT AFTER LANDING AT DAY. USING DIFFERENTIAL THRUST & BRAKING THE AIRCRAFT WAS TAXIED OFF OF RUNWAY 24L ONTO THE PARALLEL TAXIWAY AND STOPPED. THE AIRCRAFT WAS THEN TOWED TO THE GATE WHERE PSA MECHANICS TROUBLESHOT AND REPAIRED THE SYSTEM BY REPLACING THE NOSE WHEEL STEERING HAND CONTROL ASSEMBLY IAW CRJ700 AMM 32-51-01-000-801-A01. THE NOSE WHEEL STEERING OPS CHECKED GOOD IAW CRJ 700 AMM 32-51-00-710-A01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041222000962004122200096EA 2004 12 22 VNAA0412002 120041214A5220 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ESCAPE HATCH DIRTY A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05237PS 7906 DURING CLIMBOUT AFTER TAKEOFF FROM PIT THE CREW OF FLIGHT 2377 NOTED THE CABIN ALTITUDE READING 11,000FT, IT THEN WENT TO 7000 FT AND THE CABIN ALTITUDE WAS CLIMBING WITH THE AIRCRAFT. THE CREW HEARD A LOUD NOISE AND FELT AIR ESCAPING FROM THE COCKPIT ESCAPE HATCH. THE AIRCRAFT RETURNED TO PIT AND MADE AN UNEVENTFUL LANDING. MAINTENANCE AT PIT CLEANED AND INSPECTED THE CREW HATCH SEAL AND FOUND NO DEFECTS. THE AIRCRAFT WAS PRESSURIZED IAW CRJ 200 AMM 21-31-10-710-801. THE PRESSURIZATION SYSTEM OPS CHECKED GOOD AND NO LEAKS WERE FOUND. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041222001112004122200111EU 2004 12 22 04FDEA03348 120041205A5753 SKIN AIRBUS310 A310 EU TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 REPAIR RT OUTBOARD TE FLAP LOWER SURFACE OUTBOARD OF NR 2 CANOE FAIRING. REPAIRED IAW EA 6-2750-50362, DATED JUNE/16/2000. 2L72 4F RTA35EU 20041222001132004122200113SO 2004 12 22 C2XA04BT127 120041206A21214611028900 FAN EMB 145 EMB145LR 3260212SO CABIN FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2711536 145520 CREW REPORTED FOUL ODOR COMING IN THE CABIN AND THE RECIRCULATION FAN APPEARS TO HAVE NO EFFECT. MAINTENANCE REPLACED THE RECIRCULATION FAN OPERATIONALLY CHECK GOOD NO ODORS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041222001152004122200115EA 2004 12 22 SWIA200414235 120041204A274170609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07923SW922 922 7664 ON TAXI, MACH TRIM CAUTION MESSAGE WITH STAB TRIM CH 2 STATUS MESSAGE, HAPPENED 3 TIMES ON TAXI FROM HANGAR TO GATE. REMOVED AND REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222001172004122200117SO 2004 12 22 RAIA00412022 120041215A3000 WARNING LIGHT EMB 145 EMB145LR 3260212SO ICE DETECTION ILLUMINATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03837HK 145255 ICE DETECTION NR 1 AND NR 2 FAILED MESSAGES. MAINTENANCE CYCLED ICE DETECTION NR 1 AND NR 2 ANTI-ICING C/B. 2L72 4T RTT00011AT 20041222001192004122200119NE 2004 12 22 04FDEA03389 220041207A7310 FILTER DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE FUEL SYSTEM CLOGGED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25306FE 48287 AFTER T/O DURING LANDING GEAR RETRACTION, OBSERVED BOTH NR 1 AND 3 ENG FUEL FILTER PRESSURE DROP LIGHTS WERE ILLUMINATED. AFTER SELECTING CLIMB POWER. THE NR 3 LIGHT EXTINGUISHED AND NR 1 REMAINED ILLUMINATED. LEVELED OFF AT 5000 FT AND WHEN THE POWER WAS REDUCED, THE NR 1 LIGHT EXTINGUISHED. COMPLIED WITH QRH. LIGHT REMAINED EXTINGUISHED. R AND R NR 2 ENGINE FUEL FILTER. R AND R NR 1 AND 3 FUEL FILTERS AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. RAN ALL THREE ENGINES LEAK CK NORMAL. RAN AT HIGH POWER PER MAX POWER ASSURANCE CHECK. NO FUEL FILTER PRESS LIGHT ON AT ANY TIME. A/C OKAY FOR FLIGHT. 2L73 4F4 FRTA22WE E23EA 20041222001212004122200121WP 2004 12 22 04FDEA03390 120041207A3610 SEAL DOUG DC10 DC1030 3023501WP ANTI ICE DUCT FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25323FE 47811 NR 3 PNEU MANIFOLD FAILURE LIGHT ILLUMINATED INTERMITTENTLY SHORTLY AFTER T/O (NR 3 PNEU SUPPLY ON DUE TO WING ANTI-ICE REQUIRED FOR T/O). PHASE IS ACCOMPLISHED. QRH PROCEDURES COMPLETED. LIGHT WENT OUT IMMEDIATELY AS NR 3 PNEU SUPPLY SELECTOR WAS TURNED OFF. NR 3 PNEUMATIC PRESSURE DROPPED TO 5 PSI. FOUND TELESCOPING DUCT SEALS BLOWN. REMOVED AND REPLACED SEALS PER SMP. ALSO, REMOVED AND REPLACED ANTI- ICE SHUTOFF VALVE AND PNEU MANIFOLD FAULT COMP AS PRECAUTIONARY. TOOK ACFT TO HIGH POWER AND RAN ACFT PER JRH TO TAKEOFF POWER WHILE TESTING ANTI-ICE SYSTEM. NO FAULTS NOTED. POST RUN, NO FAULT BALLS TRIPPED ON MANIFOLD FAULT COMP. ALL WORK DONE IAW DC-10-30 TAFI 36-23-00. 2L73 4F A22WE 20041222001222004122200122NM 2004 12 22 A4JA12100401 120041126A2612TFC1300242 CONNECTOR DOUG MD88 MD88 3023688NM FIRE DETECTION LOOSE A A4JAO OTHER J WARNING INDICATION CRCRUISE 1 SO3512FQ 49766 AT CRUISE ALTITUDE, THE AFT CARGO B FAIL LIGHT ILLUMINATED ON THE CARGO FIRE DETECTION PANEL. FOUND CONNECTOR LOOSE, RESECURED IAW MM 20-50-04. OPS CHECK OK. 2L72 4F RTA6WE 20041222001232004122200123EU 2004 12 22 MALA040829 120041116A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 14 GALLEY SEAT TRACK PROFILE CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-23. REFER TO NRC NR 219214 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20041222001242004122200124EA 2004 12 22 SWIA200414185 120041118A5210 FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW PAX DOOR 7 INCHES ABOVE DATUM 1 AT FS 320.1 AND 338.9 FORMERS ARE CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPAIRED IAW CRJ REO 601R-52-11-609. 2L72 4F RTA21EA 20041222001262004122200126WP 2004 12 22 0402159943 120041213A5311 FRAME DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011308T 47315 DURING "M" CHECK, FOUND CRACK IN FUSELAGE FRAME AT FS 408 L16R TO L18R. REPAIRED PER EA 99-201809. 2L72 4F A6WE 20041222001272004122200127CE 2004 12 22 Z4TA200400003 120041213A3610442CW12 PUMP BEECH 58 58 1152740CE PNEUMATIC SYSTEMBROKEN D Z4TAO OTHER J WARNING INDICATION CRCRUISE 1 SO0595KM 568 TH1315 IN FLIGHT, NOTICED RIGHT PNEUMATIC PRESSURE PUMP INOP FLAGGED. CONTINUED FLIGHT ON LEFT PUMP SYSTEM. SENT ACFT TO MAINTENANCE. REPLACED PUMP WITH OVERHAULED PART. REPLACED RIGHT INSTRUMENT FILTER. OPS CK OK. 1L72 3O 3A16 20041222001282004122200128NM 2004 12 22 QXEA200400851 120041211A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH11445600 486 EMERGENCY LIGHTS FAIL OPERATIONAL CHECK. LIGHTS POWERED BY BATTERY PACK 3351 PS2 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK AT PS2. OPERATIONAL TEST OF EMERGENCY LIGHTS SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222001292004122200129EA 2004 12 22 SWIA200414268 120041214A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07445SW4196 4196 7651 INBOARD GROUND SPOILERS STATUS ON AFTER 2ND ENGINE START. REMOVED AND REPLACED NR 1 SECU IAW MM CH 27-61-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222001302004122200130EU 2004 12 22 MALA040813 120041019A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ DURING 4K INSPECTION IN LAN, GALLEY SEAT TRACK CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-27. REFER TO NRC NR 196554 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04 2L72 4T RTA52EU 20041222001312004122200131EU 2004 12 22 MALA040817 120041102A5313 RIB SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 611BR HAS 4 CRACKED RIBS. REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 126856 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2L72 4T RTA52EU 20041222001322004122200132EU 2004 12 22 MALA040820 120041102A5313 RIB SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 512AL 2 CRACKED RIBS, REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 126860 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2L72 4T RTA52EU 20041222001332004122200133CE 2004 12 22 DELA20040004 120041202A2130 CONTROL VALVE LEAR 35 35A 5170602CE CABIN PRESSURE FAILED E DELAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03360LJ 360 FLT CREW REPORTED DURING CLIMB TO 12,000 FT, CABIN ALTITUDE WARNING AND EMERGENCY PRESSURIZATION SYSTEM ACTIVATED. FLT CREW FOLLOWED THE "LOSS OF PRESSURIZATION AT ALTITUDE" CHECKLIST AND DESCENDED TO 10,000 FT. CABIN ALTITUDE CONTROL REGAINED WITH PRESS SYS SELECTED TO MANUAL MODE. THE FLT CONTINUED UNEVENTFULLY BELOW 10,000 FT TO LANDING. A/C WAS DELIVERED TO MX. MX PERFORMED OPS CHECK OF NORMAL AND EMERG PRESS SYS IAW THE LR 35 MM 21-30-00. VISUAL INSPECTION OF THE FLOW CONTROL VALVES, PRESS SYS COMPONENTS AND EXTERIOR OF PRESSURE VESSEL REVEALED NO DEFECTS. THE A/C WAS RETURNED TO SERVICE AND A FUNCTIONAL FLIGHT CHECK OF THE PRESS SYS WAS CONDUCTED. OP OF THE PRESS SYS WAS FOUND TO BE SATISFACTORY. 2L72 4F A10CE 20041222001352004122200135SO 2004 12 22 C2XA04BT124 120041203A335078241 INVERTER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW2734110 145658 EWR- CO3332, CREW REPORTED THAT THE EMERGENCY EXIT SIGN OVER THE WING IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER, OPS CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20041222001362004122200136NM 2004 12 22 QXEA200400873 120041213A243051539008D GCU DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09355PH114824784 500 NR 1 DC CAUTION LIGHT ILLUMINATED, WOULD NOT RESET PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 DC GCU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222001372004122200137NM 2004 12 22 QXEA200400874 120041213A243023088008 GENERATOR DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NM09355PH9853 3 500 NR 1 DC GENERATOR FAILED AND WOULD NOT RESET PER CHECKLIST. MAINTENANCE REMOVED AND REPLACED NR 1 DC STARTER GENERATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222001432004122200143NM 2004 12 22 QXEA200400880 120041216A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09363PH16828454 520 EMERGENCY LIGHTING INOPERATIVE ON FLOOR TRACK FORWARD EMERGENCY EXIT. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY LIGHT STRIP AND POWER SUPPLY 3352 PG 2 BATTERY PACK 3. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222001482004122200148SO 2004 12 22 SWIA200414250 120041212A2720 RUDDER PEDAL EMB 120 EMB120ER 3260203SO COCKPIT MISINSTALLED A SWIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM07580SW 120348 FO'S LEFT RUDDER PEDAL STUCK ON PEDESTAL TRIM PANEL. REINSTALLED RUDDER PEDALS CORRECTLY IAW MM 27-21-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222001532004122200153CE 2004 12 22 DELA20040005 120041203A5610PAS66004047 WINDSCREEN LEAR 55 55LEAR 5170702CE COCKPIT FAILED E DELAK NONE O OTHER ININSP/MAINT 1 CE03903JC1167 081 DURING A ROUTINE SCHEDULED PRISM INSPECTION OF THE LEFT PILOTS WINDSHIELD, A DEFECT WAS NOTED IN THE DEFOG NOZZLE AREA. THE DEFOG NOZZLE ASSY WAS REMOVED AND FURTHER EXAMINATION REVEALED A 2.8 INCH L BY .8 INCH W V-GROOVE WITH A VARYING DEPTH OF LESS THAN 4" LOCATED ON THE OUTER STRUCTURAL LAYER. NO OTHER DEFECTS WERE NOTED IN THE WINDSHIELD ASSY, DEFOG NOZZLE, OR RELATED PLUMBING OR SEALS. THE WINDSHIELD ASSY WAS REPLACED WITH A NEW UNIT OF SAME PART NUMBER. 2L72 4F A10CE 20041222001552004122200155EA 2004 12 22 SWIA200414256 120040924A5321 FLOOR PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 MAIN AVIONICS COMPARTMENT APPROX STA 280 RT AFT ANGLE UNDER COCKPIT FLOOR PANEL CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW REPAIR ANGLE IAW REO 601R-53-11-034. 2L72 4F RTA21EA 20041222001562004122200156EA 2004 12 22 SWIA200414257 120040924A5340 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 MAIN CABIN FLOORBEAM ATTACH ANGLE AT FS 461 RBL 10 IS CRACKED AT RADIUS LOCATION. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE IAW CRJ 200 SRM 51-42-21 AND EO NR 601R-53-5459. 2L72 4F RTA21EA 20041222001572004122200157EA 2004 12 22 SWIA200414258 120041203A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 CRACK IN RIGHT SIDE ADG VIEWING LIGHTENING HOLE ON FS 169.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW CRJ REO 601R-53-11-834 REV "NC". 2L72 4F RTA21EA 20041222001582004122200158EA 2004 12 22 SWIA200414259 120041203A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07435SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11. 2L72 4F RTA21EA 20041222001592004122200159EA 2004 12 22 SWIA200414260 120041203A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED INBOARD, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11, 51-42-13. 2L72 4F RTA21EA 20041222001602004122200160NM 2004 12 22 AWXA200401383 120041209A2560P4010021 BATTERY BOEING737 7373S3 1384711NM ZONE 900 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28312AW 24060 PHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE FORWARD BULKHEAD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD BULKHEAD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041222001632004122200163SO 2004 12 22 C2XA04IA161 120041203A3260852701 PROXIMITY SWITCH EMB 145 EMB145 3260210SO NLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716963 145116 CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR PROXIMITY SWITCH. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041222001682004122200168EU 2004 12 22 MALA040810 120041019A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 DURING 4K INSPECTION IN LAN, CENTER CARGO COMPARTMENT SEAT TRACK CORRODED FS 621.138 TO 686.888. MAINTENANCE REMOVED AND REPLACED CENTER CARGO COMPARTMENT SEAT TRACK IAW SAAB SRM 53-70-60-2. REFER TO NRC NR 196536 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2L72 4T RTA52EU 20041222001832004122200183NM 2004 12 22 AWXA200401362 120041122A33973404302 CONNECTOR BOEING737 73733A 1384673NM SEAT ROW 19 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 DURING 8-DAY CHECK, THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT WAS FOUND INOPERATIVE. MAINTENANCE REPINNED WIRING IN CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041222001842004122200184NM 2004 12 22 AWXA200401363 120041128A57536546486129 WEDGE BOEING737 73733A 1384673NM TE FLAPS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE 26" FROM OUTBOARD END, BETWEEN WBL 153 AND WBL 157. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20041222001852004122200185NM 2004 12 22 AWXA200401364 120041128A57536546486129 WEDGE BOEING737 73733A 1384673NM TE FLAPS DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK ,THE LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED 14" FROM OUTBOARD END, BETWEEN WBL 169 AND WBL 176. MAINTENANCE CUTOUT DAMAGED AREA OF LOWER SURFACE OF LT WING INBOARD MID FLAP TRAILING EDGE WEDGE; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20041222001862004122200186NM 2004 12 22 AWXA200401365 120041122A52306546921528 DOOR FRAME BOEING737 73733A 1384673NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW19206 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, A 1 1/2" CRACK WAS FOUND IN FORWARD EDGE OF FORWARD CARGO DOOR FRAME JUST BELOW CEILING HOOK, BS 460, STR 20 RT. MAINTENANCE REMOVED AND REPLACED FORWARD CARGO DOOR ASSEMBLY IAW T/C R8M52001. 2L72 4F RTA16WE 20041222001872004122200187NM 2004 12 22 AWXA200401366 120041122A531465458682 KEELBEAM BOEING737 73733A 1384673NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 MCN - MAJOR REPAIR - DURING 8-DAY CHECK CORROSION WAS FOUND ON RT KEEL BEAM AT BS 540, STR 27 RT. MAINTENANCE CUTOUT DAMAGED AREA OF KEEL BEAM LOWER CHORD FROM BS 500A TO BS 540; FABRICATED A NEW REPLACEMENT SECTION OF KEEL BEAM CHORD, 3 EACH FILLERS, AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-12, FIG 203. 2L72 4F RTA16WE 20041223000042004122300004EU 2004 12 23 MALA040825 120041116A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, SEAT TRACK LBL18.5 CORRODED AT STA 302. MAINTENANCE REPLACED SEAT TRACK FROM STA 297 TO STA 330 IAW MESABA EO NR S53060. REFER TO NRC NR 127285 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20041223000062004122300006NM 2004 12 23 UPS04243611 120041216A3350 LIGHT BOEING727 72725C 138400HNM EMERGENCY EXIT MALFUNCTIONED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 EMERGENCY EXIT LIGHT IN COCKPIT FLICKERS VERY DIM WHEN SWITCH PLACED TO ON. REMOVED AND REPLACED EMERGENCY LIGHT PER 33-50-1, TEST OK. 2L73 4F A3WE 20041223000142004122300014NM 2004 12 23 DHL2004755500 120041013A5330 SKIN BOEING727 727225 1384077NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A "C" CHECK, RT FUSE HAS A GOUGE AFT BS 1133 BELOW STR 24R. CUT-OUT DAMAGED SKIN 2 1/2" BY 1" AT STA 1133 BELOW STR 24R IAW B727 SRM 53-30-3. FABRICATED DOUBLER 10" X 7" P/N 2024 T3.071 PO NR 9001189 IAW B727 SRM 53-30-3,TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 20041223000152004122300015NM 2004 12 23 AWXA200401382 120041129A53306552873158 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-15 CHECK A .1875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT L-2 DOOR LOWER HINGE CUTOUT BS 955, STR 15 LT. MAINTENANCE BLENDED OUT CRACK, MATERIAL LOSS WITHIN LIMITS IAW B737-300 SRM 53-00-01, FIG 101. PERFORMED HFEC INSPECTION OF BLEND OUT TO ENSURE NO CRACKS EXIST, TREATED AREA. 2L72 4F RTA16WE 20041223000162004122300016NE 2004 12 23 PG9R097903 220041021A7261900D3409526105 LINE DOUG MD900 MD900 3027375NM PWC PW207 PW207E NE ENGINE OIL LEAKING B PG9RK NONE K FLUID LOSS ININSP/MAINT 1 WP19368PA 90000012 FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/REPLACED OIL HOSE ASSY. 1G72 3U3 UNCH19NM E42NE 20041223000182004122300018SO 2004 12 23 LR7A04199 120041110A24243S2060DR113A1 VOLT REGULATOR LKHEED382 382G 526414USO NR 4 OVERHEATED A LR7AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 AL03401LC 1347 4606 FLIGHT CREW REPORTED BURNING RESISTOR SMELL IN THE COCKPIT DURING ENGINE SHUTDOWN. FOUND NR 4 VOLTAGE REGULATOR OVERHEATED. REPLACED VOLTAGE REGULATOR IAW MM SMP 581 24-20, PG 226. OPS CKS NORMAL. LP 18065, ITEM 1. 2H74 4T A1SO 20041223000222004122300022WP 2004 12 23 ABXA040377 120041112A5312 PRESSURE PANEL DOUG DC9 DC941 302207NWP MAIN CABIN LEAKING A ABXAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL23962AX 47768 DESCENDING, PASSING FL 180, AUTOPILOT WITH HEADING MODE ENGAGED, NOTICED A/C DRIFTED 20 DEGREES LT OF COURSE WITH NOSE DOWN, SWITCHED TO TURN KNOB, A/C WOULD NOT RESPOND. DISENGAGED AUTOPILOT, YOKE STILL IN LT/FWD POSITION. WENT TO ROLL WINGS LEVEL BUT YOKE JAMMED. USED FORCE & YOKE BROKE FREE THEN JAMMED IN RT ROLL. YOKE THEN FREED UP. LATER IN DESCENT, ENGAGING SPEED BRAKES CAUSED SEVERE ROLL TO RT. FOUND OUTBD PULLEY CLUSTER FROZEN, INSPECT FLT CONTROL CABLES & THAWED OUT PULLEYS. PERFORMED LEAK CHK OF SLANT PRESS PNL IAW JC 9079020. FOUND SLANT PNL SPRAYING WATER DIRECTLY ON PULLEY CLUSTER. REMOVED CABIN FLOORBOARD PNL & SEALED LT SLANT PRESS PNL. PERFORMED LEAK TEST, NO WATER SPRAYING ON PULLEY CLUSTER. 2L72 4F A6WE 20041223000282004122300028CE 2004 12 23 091304 120040910A3220 WHEEL LEAR 25 25B 5170511CE NLG OUT OF POSITION E ESUAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03425JL 127 THE CREW DID NOT NOTICE THAT THE NOSE WHEEL WAS TURNED 180 DEGREES, THEREFORE WHEN THE CREW RETRACTED THE LANDING GEAR THE NOSE GEAR COULD NOT LOCK IN THE UP POSITION, WHICH WOULD NOT ALLOW THE GEAR DOORS TO CLOSE. THEREFORE THE GEAR UNSAFE LIGHTS. 2L72 4J A10CE 20041223000312004122300031NM 2004 12 23 372PA0079 120041109A3350 BULB BOEING737 737306 13844BGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 L2 DOOR EMERGENCY LIGHT INOP AND LENS CRACKED. REPLACED BULB AND LENS. OPS CHECKS NORMAL. 2L72 4F RTA16NE 20041223000372004122300037EU 2004 12 23 MALA040832 120041123A5320 PLATE BAC 146 AVRO146RJ85A1500097EU FUSELAGE OUT OF ADJUST A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, THERE IS INSUFFICIENT CLEARANCE BETWEEN THE FLANGED PLATE ON THE FIN STRUCTURE OF LT SIDE. MAINTENANCE REPAIRED IAW PER EO NR A27004. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041223000382004122300038 2004 12 23 VW3R200400004 420041210A2565D29601103 GIRT BAR AIRCRUISERS AIRBUS310 A310 EU ESCAPE SLIDE MISLOCATED B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0153 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PAD RIDES UP ON CAVITY RIDGE OF GIRT BAR. 2L72 4F RTA35EU 20041223000392004122300039EU 2004 12 23 MALA040833 120041123A5720 INTERCOSTAL BAC 146 AVRO146RJ85A1500097EU AILERON QUADRANTCHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, INTERCOSTAL UNDER RT AILERON QUADRANT CHAFED. MAINTENANCE REPAIRED INTERCOSTAL IAW EO NR A53206. REFER TO 409 NR 224428 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041223000432004122300043SO 2004 12 23 SWIA200414269 120041208A5210 STRUT EMB 120 EMB120ER 3260203SO F/A JUMP SEAT SEPARATED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07213SW 120277 MAIN CABIN DOOR WOULD NOT OPEN. REATTACHED F/A JUMP SEAT STRUT. DOOR OPERATES NORMAL. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041223000482004122300048EA 2004 12 23 QXEA200400728 120041028A29136619002 PUMP CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 HYD SYS LEAKING A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09615QX 10065 FLIGHT RETURNED TO FIELD AFTER THE NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 ENGINE DRIVEN PUMP LEAKING. A NEW PUMP WAS INSTALLED, OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20041223000492004122300049NE 2004 12 23 EM04024 220041207A73204120T01P02 FMU EMB ERJ170ERJ170100 EU GE CF34 CF348E5 30015NE NR 1 ENGINE MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19804MD 000016 193137 REMOVED NR 1 ENGINE FADEC FOR TROUBLESHOOTING, NO HELP. REINSTALLED FADEC ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE FUEL METERING UNIT. FAULT CLEARED, GROUND POWER ASSURANCE RUN CHECK IS NORMAL. 2L74 4F4 FRTA56NM E00063EN 20041227000022004122700002EU 2004 12 27 AWXA200401110 120041005A2421728843H IDG AIRBUS320 A320232 3930326EU NR 2 ENGINE MALFUNCTIONED A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28652AW 953 ON TAKEOFF AT LAS, RECEIVED ECAM WARNING NR 2 ENG IDG LOW OIL PRESSURE, REJECTED TAKEOFF AT 80 KTS. MX ISSUED MEL 24-20-01, COND. 2 "NR 2 IDG INOP". PERFORMED FAULT ISOLATION PER TSM, ITEM 4 - 4A2, NO WIRING FAULTS NOTED. REMOVED AND REPLACED NR 2 ENG IDG IAW T/C R5M24301, OPS CHECK OF IDG GOOD. VENDOR INCOMING FUNCTIONAL TEST OF IDG COULD NOT DUPLICATE LOW OIL PRESSURE FAULT THAT WAS INDICATED ON ECAM; ALL STATIC TESTS WERE WITHIN ACCEPTABLE LIMITS. BUT DISASSEMBLY FOUND OUTBOARD BEARING INNER RACE ON FIXED HYD INPUT SPLINE WORN CAUSING SPLINE TO WOBBLE AND WEAR AGAINST FIXED CYLINDER INPUT GEAR SHAFT. IT IS BELIEVED THE WOBBLING LINKAGE CAUSED THE HYD BLOCK TO LIFT OFF AND LEAK OIL, CONSISTENT WITH REASON FOR2L72 4F RTA28NM 20041227000032004122700003NM 2004 12 27 SB04164 120041210A4960655280131 CONTROL UNIT BOEING737 7373B7 1384580NM E3-3 RACK FAULTY A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19391US4616646166 23313 ATL - FLT1203 - FLIGHT DEPARTED CLT, EN ROUTE TO IAH, WITH THE NR 2 CSD/GENERATOR ON MEL 24-1 FOR LEAKING OIL. AT FL350, JUST PASSING ATL, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU SHUTDOWN. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU CONTROL UNIT (M280). INSPECTED APU FOR OIL LEAKS AND PROPER OIL LEVEL. ALL CHECK NORMAL. RAN APU SEVERAL TIMES WITH NO DEFECTS NOTED. CLEARED MEL 24-1 ON NR 2 CSD/GENERATOR WITH THE REPLACEMENT OF A LEAKING PACKING FOR THE NR 2 CSD OIL CHARGE FILTER HOUSING. RAN ENGINE. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20041227000042004122700004NM 2004 12 27 SB04167 120041213A2424915F2124 CONTROL UNIT BOEING737 737301 1384611NM P6 PANEL UNRELIABLE A USAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19576US787874754 23741 PIT FLT414 FLIGHT DEPARTED ORD, EN ROUTE TO PHL, WITH THE NR 2 GENERATOR ON MEL 24-1. DURING CRUISE, THE APU GENERATOR DROPPED OFF LINE, LEAVING ONLY THE NR 1 GENERATOR. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED APU PERFORMANCE CHECK CARD J3-049. ALL PARAMETERS WITHIN MAINTENANCE MANUAL LIMITS. REMOVED AND REPLACED APU GENERATOR CONTROL UNIT (GCU), AS PRECAUTIONARY, PER MM 24-21-81-4. GENERATOR NR 2 REMAINS ON MEL 24-1. 2L72 4F RTA16WE 20041227000052004122700005EU 2004 12 27 SA04089 120040920A3350321431 BATTERY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19701UW 0890 CLT - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST WITH MESSAGE "EPSU UNIT EMER L". MAINTENANCE REPLACED THE BATTERY PACK THE LEFT, OVERWING EXIT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041227000072004122700007EU 2004 12 27 SA04108 120041123A335032145410 EPSU AIRBUSA319 A319112 3930323EU LEFT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19756US7705 1340 DURING TEST, THE EMERGENCY LIGHTS GIVE THE BITE FAULT: "FWD LEFT EPSU INT OVERLOAD". MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041227000122004122700012NM 2004 12 27 2004UALA01168 120041125A5210 GIRT BAR BOEING757 757222 1384956NM PWA 2037 PW2037 NE R1 DOOR DIRTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 DOOR 1R DIFFICULT TO ARM. GALLEY DEBRIS IN GIRT AREA. GIRT BAR ATTACHMENT SYSTEM WAS CLEANED AND LUBED. 2L72 4F4 FRTA2NM E17NE 20041227000132004122700013NE 2004 12 27 P5CA0401274 220041114A7200 ENGINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 1 FAILED A P5CAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 EA15920FT 22237 702192 ON TAKEOFF TOWER REPORTED SPARKS FROM NR 1 ENGINE DURING CLIMB.EGT HIGH (600 DEGREE) AS COMPARED TO OTHER ENGINES.N1 90% N2 94%, EXPERIENCED COMPRESSOR STALL AT FL 250 WHILE CDLIMBING TO FL 350. ENGINE REPLACED PER POLAR WORK CARD M71-00-02. 2L74 4F4 F A20WE E3NE 20041227000142004122700014NM 2004 12 27 2004UALA01002 120041029A5313 STRINGER BOEING757 757222 1384956NM PWA 2037 PW2037 NE STA STR GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 CABIN STRINGER GOUGED ON LWR SIDE AT STA 620 STR 16L. DAMAGED DURING REPAIR TO SURROUNDING STRUCTURE. BLENDED OUT DAMAGE, FABRICATED HAT CHANNEL REPAIR. 2L72 4F4 FRTA2NM E17NE 20041227000172004122700017NM 2004 12 27 04FDEA02955 120041020A7830683L218G07 COWLING DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 ENG NR 2 LT HAND T/R COWL AT UPPER SLIDER TRACK END CRACKED. ENG NR 2 LEFT HAND T/R COWL UPPER SLIDER TRACK REPAIRED IAW ROHR AERO SERVICES - ASIA ENGINEERING REPAIR NR 'RASA-040560'. (WITH FAA FORM 8130-3, TRACKING 5586, J009768-000). 2L73 4F RTA22WE 20041227000192004122700019NM 2004 12 27 2004UALA01156 120041124A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT FRAME DENTED UPPER FLANGE AT STA 1420, STR 26L. 2L72 4F4 FRTA2NM E17NE 20041227000232004122700023NM 2004 12 27 SB04161 120041205A2120 DUCT BOEING737 737301 1384611NM A/C DISTR BAY DISCONNECTED A USAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19592US 23937 MCO FLT1222 EN ROUTE FROM PBI TO DCA, AT FL370, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW COULD NOT CONTROL CABIN ALTITUDE AND BOTH PACKS WERE ACTING ABNORMAL. THEY ALSO RECEIVED A DUCT OVERHEAT. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO REGAIN CONTROL OF CABIN. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CONTROL CABIN DUCTING DISCONNECTED AT DISTRIBUTION PLENUM AREA, AFT OF FORWARD CARGO BAY. RECONNECTED AND SECURED WITH CLAMPS. OPERATED PACKS. OPERATIONAL CHECK AND LEAK CHECK GOOD. ALSO, REMOVED AND REPLACED THE LEFT AND RIGHT AIR CYCLE MACHINES DUE TO COOLING PROBLEMS AND PERFORMANCE DURING PRESSURIZATION CONFIDENCE CHECK. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20041227000242004122700024NM 2004 12 27 04FDEA02976 120041022A5753ARC7482501 SUPPORT DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD HOLES FWD AND CENTER ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801. 2L73 4F RTA22WE 20041227000262004122700026EU 2004 12 27 04FDEA03024 120041107A5730 SKIN AIRBUS310 A310 EU LT WING DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25456FE 318 LT WING OUTBOARD TE PANEL (BOTTOM SKIN - FOUND 6 LOCATIONS WITH DELAMINATION. AREAS OF DELAMINATION ARE AS FOLLOW (INBD TO OUBD): 1: 36.5 X 12, 2: 14 X 14, 3: 4 X 3, 4: 2.5 X 2.5, 5: 2 X 0.5, 6: 1.5 X 0.5 ......NOTED 2EA EXISTING REPAIRS ON UPPER SKIN, ADJA CENT TO ABOVE AREAS NR 1 AND 2. 2L72 4F RTA35EU 20041227000292004122700029NM 2004 12 27 2004UALA01166 120041130A5210 DOOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE R 2 LEAKING A UALAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP29549UA 25397 FLIGHT DIVERTED DUE TO A DOOR SQUEAL. INTERIM REPAIR WAS ACCOMPLISHED WITH THE USE OF ALUMINUM SPEED TAPE FOR LEAKAGE NOTED AT UPPER PART OF DOOR 2R. PERMANENT FIX INCLUDED FIT AND FAIR ADJUSTMENT OF DOOR 2R STOP PINS AND/OR PAD FOLLOWED BY PRESSURIZING AIRCRAFT. 2L72 4F4 FRTA2NM E17NE 20041227000312004122700031SO 2004 12 27 CHQA000547 120040901A3350 LIGHT EMB 145 EMB145LR 3260212SO FUSELAGE INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270 145304 FLOOR EMERGENCY PROXIMITY LIGHT IS INOP. INSTALLED NEW FLOOR PROXIMITY EMERGENCY LIGHT AT FLOORBOARD LOCATION 261BF IAW EMB 145 AMM 33-50-12. 2L72 4T RTT00011AT 20041227000332004122700033NM 2004 12 27 2004UALA01195 120041208A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 AFT PIT FUSELAGE FRAME INBOARD FLANGE DENTED AT BS 1420 STR 25L TO STR 26L. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041227000342004122700034NM 2004 12 27 04FDEA02975 120041022A5753ARC7480501 SUPPORT FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LT WING INBOARD FLAP VANE INBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED AND OUTBOARD AFT HOLE IS CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801. 2L73 4F RTA22WE 20041227000352004122700035NM 2004 12 27 04FDEA03025 120041108A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK - LBL 47 STA 965 FOUND WORN BEYOND LIMITS. CABIN SEAT TRACK - LBL 47 STA 965 AREA REPAIR CARRIED OUT AS PER SRM 53- 70-00 FIG.1 VOL I AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041227000362004122700036NM 2004 12 27 BB04091 120041123A335020131A BATTERY BOEING767 7672B7 1385107NM CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652US 24765 FOUND LEFT AISLE EMERGENCY LIGHTS INOPERATIVE FROM ROW 9 THROUGH 13. MAINTENANCE REPLACED THE BATTERY PACK AT POWER SUPPLY M1209. 2L72 4F RTA1NM 20041227000372004122700037EU 2004 12 27 SA04112 120041203A3350 WIRE AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT DISCONNECTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19722US 1097 THE EMERGENCY EXIT LIGHT WIRING WAS FOUND DISCONNECTED AND THE MAIN ENTRANCE DOOR SLIDE COVER LOOSE. MAINTENANCE INSTALLED THE LOOSE SLIDE COVER AND CONNECTED THE EMERGENCY LIGHT WIRING. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041227000382004122700038EU 2004 12 27 SA04091 120040928A335032145510 EPSU AIRBUSA321 A321211 3930370EU EMERGENCY LIGHT FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19178US11728 1519 RECEIVED LEFT FWD MID EXT SLIDE LIGHTS FAULT. MAINTENANCE REPLACED THE LEFT MID CABIN EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041227000402004122700040EU 2004 12 27 SA04102 120041104A5210FE240221001 DIAPHRAGM AIRBUS320 A320214 3930316EU PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW 1065 THE AFT LEFT PASSENGER DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. MAINTENANCE FOUND THE DOOR ASSIST DAMPER PRESSURIZED BY A CRACKED SEAL. MAINTENANCE REPLACED THE CRACKED SEAL. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041221001992004122100199NM 2004 12 21 USAA040915 120041022A53401133482 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - CLIP, .1250 INCH CRACK, STA 807 AND STR 10R. REMOVED AND REPLACED CLIP IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20041222000082004122200008NM 2004 12 22 DL76G041121 120041219A5246145T861612 ACCESS DOOR BOEING767 7673P6 1385105NM FUSELAGE MISSING A DALAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO27154DL 25241 ON ARRIVAL ACCESS DOOR FOR HYD HIGH PRESSURE CONNECT MISSING REPAIRED PER ERA 095866-14, INSTALLED PANEL, TIME LIMITED TO ONE FLIGHT. NDS PANEL P/N 145T8616-12 AND RELATED HARDWARE REF IPC 53-52-54-01 SHT 4 ITEM 100. 2L72 4F RTA1NM 20041222000152004122200015NM 2004 12 22 04FDEA03449 120041219A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25577FE 48469 STA 836 LT NR 3 SEAT TRACK EXISTING FLANGE REPAIR FOUND NOT CONFORMING TO SRM STANDARD. REPAIRED SEAT TRACK & SPLICE FABRICATED AS PER SRM 53-70-00. 2L73 4F RTA22WE 20041222000252004122200025EA 2004 12 22 QXEA200400890 120041209A5210 STEP CNDAIRCL600 CL6002C10 1390015EA ZONE 800 DELAMINATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - MAIN CABIN DOOR TOP STEP ASSEMBLY IS DELAMINATED AT TOP RIGHT HAND CORNER. REPLACED MAIN CABIN DOOR TOP STEP ASSEMBLY PANEL. 2L72 4F RTA21EA 20041222000422004122200042NM 2004 12 22 04FDEA03441 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25577FE 48469 STA 836 LT NR 1 SEAT TRACK EXISTING FLANGE REPAIR FOUND NOT CONFORMING TO SRM STANDARD. REMOVED AS PER SRM 53-70-00 FIG 1 VOL I. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL I AND REPROTECTED AS PER SRM 51-21-01 VOL II. REPAIR SEAT TRACK AND SPLICE INSTALLED AS PER 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20041222000432004122200043NM 2004 12 22 04FDEA03442 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25577FE 48469 STA 840 RT NR 1 SEAT TRACK EXISTING FLANGE EXISTING REPAIR FOUND NOT CONFORMING TO SRM STANDARD. 2L73 4F RTA22WE 20041222000492004122200049NE 2004 12 22 0402179750 220041214A7200 ENGINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 1 FLAMED OUT A NWAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL01750NW 47114 676199 AFTER TAKEOFF, THE NR 1 ENGINE FLAMED OUT AT 3,300 FT, RELIGHT ATTEMPT WAS UNSUCCESSFUL. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE DUE TO LOW OIL PRESSURE DURING ENGINE WINDMILLING. 2L72 4F4 F A6WE E2EA 20041222000562004122200056NM 2004 12 22 2004UALA01139 120041117A52106F16655501 HANDLE BOEING747 747422 1384935NM PWA 4056 PW4056 NE DOOR ASSIST MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29181UA 25278 UPPER DECK DOOR LEFTSIDE ASSIST STRAP NEEDS TO BE ON FORWARD HANDLE NOT AFT. PREVIOUS MAINTENANCE WORK PERFORMED WAS NOT IN ACCORDANCE WITH INSTRUCTIONS IN 747 AIRCRAFT MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG, CAUSING DISCREPANT CONFIGURATION. MIS-LOCATED STRAP WAS REMOVED AND INSTALLED IN PROPER LOCATION. 2L74 4F4 FRTA20WE E24NE 20041222000572004122200057NM 2004 12 22 AWXA200401414 120041129A5210654587113 SKIN BOEING737 7373G7 1384595NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .0312 INCH CRACK WAS FOUND IN R-1 DOOR EXTERNAL SKIN AT LOWER HINGE CUTOUT BS 310, STR 13 RT. MAINTENANCE TRIMMED OUT CRACK, FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW ER 03-5200-04350-HF1. 2L72 4F RTA16WE 20041222000582004122200058NM 2004 12 22 04FDEA03437 120041217A5311 FRAME BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25151FE 19147 FLT CREW COMPARTMENT LEFT SIDE AT FS 227.8 FRAME HAS 2 EACH AREAS OF CORROSION ABOVE AND BELOW OXYGEN PANEL. REMOVED DAMAGE AREA IAW SRM 51-40-2, MADE NEW WEB FROM 7075-T6 .125C BATCH 0000828965 & DOUBLER MADE FROM 7075-T6 .160C BATCH 0000687676 IAW SRM 51-40-2. INSTALLED NEW WEB & DOUBLER IAW SRM 51-30-2. 2L73 4F RTA3WE 20041222000612004122200061SO 2004 12 22 CHQA000594 120041217A33503025103 LIGHT EMB 145 EMB145MP 3260216SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11975 145337 EMERGENCY EXIT LIGHT ABOVE RIGHT HAND HINGE IS INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT ABOVE THE RIGHT HAND WING IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041222000642004122200064EA 2004 12 22 04349627 120041214A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA PAX DOOR FALSE INDICATIONA VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27627BR 7233 PAX DOOR LATCH LIGHT CAME ON IN CLIMBOUT. RTF. MX PERFORMED OPS CHECK IAW FIM 52-70-04, NO DEFECT NOTED. 2L72 4F RTA21EA 20041222000662004122200066EA 2004 12 22 04353650 120041218A5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27650BR 7418 CA'S WINDSHIELD OUTER PANE CRACKED. NO PRESSURIZATION ISSUES. MX REMOVED AND REPLACED WINDSHIELD. 2L72 4F RTA21EA 20041222000702004122200070EA 2004 12 22 SWIA200414272 120040924A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07587SW 7062 FLOORBOARD FRAME CRACKED AT STA 621 LEFT SIDE. ITEM FOUND AT C-CHECK INSPECTION. INSTALL REPAIR ANGLES IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20041222000832004122200083 2004 12 22 SWAA043661 420041217A2565D31354 SLIDE BOEING737 7373K2 13844BANM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041222000932004122200093NM 2004 12 22 UPS04243613 120041220A33501000677 LIGHT BOEING727 72722C 138400FNM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01944UP 19103 FWD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 33-50-01. F/C OK. 2L73 4F A3WE 20041222000972004122200097EU 2004 12 22 EM04025 120041217A32349037B000103 LEVER EMB ERJ170ERJ170100 EU MLG INOPERATIVE A USAAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 EA19812MD1151 000030 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, THE HANDLE WOULD NOT MOVE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. 2L74 4F RTA56NM 20041222001002004122200100SO 2004 12 22 RAIA00412024 120041215A7830 WARNING SYSTEM EMB 145 EMB145LR 3260212SO THRUST REVERSER ACTIVATED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03816HK 145055 THRUST REVERSER NR 2 DISAGREE MESSAGE ON EICAS. MAINTENANCE, DEFERRED NR 2 TRUST REVERSER PER MEL 78-30-00 CAT C. 2L72 4T RTT00011AT 20041222001022004122200102EA 2004 12 22 QXEA200400829 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 LT OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AT FS 364-379, FS 423-430 AND FS 445. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20041222001042004122200104WP 2004 12 22 WX0400040 120041001A3397 WIRE DOUG DC9 DC987 3022087WP EMERGENCY LIGHT LOOSE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19945MA 49725 IFP - POST FLIGHT WALK AROUND, CREW REPORTED LOOSE WIRES EMERGENCY LIGHT IN TAIL CONE. MAINTENANCE SECURED WIRES IAW 20-50-04. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041222001062004122200106WP 2004 12 22 ABXA040391 120041130A5310J06011940 SHEAR TIE DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23964AX 47781 UPPER END OF SHEAR TIE CRACKED AT LONGERON 14 RIGHT, AFT OF FRAME 1056. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20041222001082004122200108NM 2004 12 22 QXEA200400853 120041201A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND INBOARD FORWARD SEAT RAIL HAS PITTING CORROSION ON TOP INBOARD FLANGE AT FUSELAGE STATION X66.0. REPAIRED IAW RD 8/4/53/884-1551 AND SRM SUB TASK 51-40-15-400-001. 2H72 4T RTA13NM 20041222001092004122200109EU 2004 12 22 04FDEA03345 120041205A7830 STRUCTURE AIRBUS310 A310 EU THRUST REVERSER GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 040 313 NR 1 ENGINE, THRUST REVERSER RT FOUND WITH WEAR CLOSE TO BREATHER. ACCOMPLISHED IAW EA 6-7830-81809. 2L72 4F RTA35EU 20041222001102004122200110NM 2004 12 22 DHL2004760014 120041214A3350 BATTERY BOEING727 7272B7 138407LNM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01760AT 21954 EMERGENCY EXIT LIGHTS WON'T ILLUMINATE DURING STANDBY POWER CHECK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW B727 MM 33-10-0 LIGHTS OPS CHECKED GOOD. 2L73 4F A3WE 20041222001342004122200134SO 2004 12 22 C2XA04IA166 120041209A3350110049 CHARGER EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712528 145504 IAH- DURING MAINTENANCE INSPECTION, THE NUMBER TWO CEILING EMERGENCY LIGHT AND EXTERIOR RIGHT HAND FORWARD EMERGENCY LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20041222001402004122200140WP 2004 12 22 A4JA12100403 120041127A2611 SMOKE DETECTOR DOUG DC9 DC931 3022065WP LAVATORY CONTAMINATED A A4JAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO35935DS 48158 AFTER LANDING IN SWF, BOTH LAV SMOKE DETECTORS SOUNDED. NO INDICATION OF SMOKE. CLEANED DEBRIS FROM LAV SMOKE DETECTOR. GROUND OPS CHECK NORMAL IAW DC9 MM 26-10-0. 2L72 4F A6WE 20041222001412004122200141SO 2004 12 22 C2XA04IA162 120041203A32347455503 CONTROL LEVER EMB 145 EMB145 3260210SO MLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716963 145116 CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20041222001422004122200142NM 2004 12 22 UPS04243607 120041215A324221147 METERING VALVE BOEING727 727173C 1384059NM LEFT MLG BRAKE MALFUNCTIONED A IPXAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 SO01938UP 19506 BRAKES DO NOT SEEM TO RELEASE AFTER BRAKE APPLICATION A/C COMES TO COMPLETE STOP AND HAVE TO ADD POWER TO TAXI A/C. ALSO, SEE L/P 694861 ITEM 2 ADJUSTED LT MLG BRAKE METERING VALVE WRT 32-41-11 SYSTEM OPS CK GOOD. 2L73 4F A3WE 20041222001442004122200144NM 2004 12 22 QXEA200400850 120041207A5210 BUSHING DHAV DHC8 DHC8202 2809007NM MAIN CABIN DOOR WORN A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09368PH14693 512 UPON ARRIVAL, THE CREW COULD NOT OPEN THE MAIN CABIN DOOR. MAINTENANCE INSPECTED THE DOOR FOR RIG AND FOUND THE RIGGING OF THE DOOR TO BE GOOD. UPON FURTHER INSPECTION, MAINTENANCE FOUND THE AFT DOOR RAIL ARM PIVOT EMBEDDING ITSELF INTO THE FALSE BULKHEAD LOCATED IN FRONT OF ROW 1A. THE BUSHINGS LOCATED AT THE TOP AND BOTTOM OF THE BULKHEAD WERE REPLACED GIVING CLEARANCE TO THE HANDRAIL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041222001452004122200145SO 2004 12 22 SWIA200414247 120041206A3350 LAMP EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07227SW EMERGENCY LIGHT OVER MAIN CABIN DOOR IS INOPERATIVE. RELAMPED EMERGENCY LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222001462004122200146SO 2004 12 22 SWIA200414248 120041209A2721 WHEEL EMB 120 EMB120ER 3260203SO RUDDER TRIM WORN A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07227SW RUDDER TRIM WHEEL DOES NOT TURN. REPLACED RUDDER TRIM WHEEL SPLICED SHAFT AND BEARING IN CENTER CONSOLE PER EMB 120 MM 27-23-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222001472004122200147 2004 12 22 SWIA200414249 420041210A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL PROTECTIONMALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07418SW5050 5050 SHORTLY AFTER ROTATION, RECIEVED "WINDSHEAR FAIL" AND "CONT IGNITION" STATUS MESSAGES, ALSO HAD INTERMITTENT STICK SHAKER. REPLACED STALL PROTECTIVE COMPUTER. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222001492004122200149EA 2004 12 22 SWIA200414251 120041208A2751855D10011 POSITION SENSOR CNDAIRCL600 CL6002B19 1900309EA RT WING TE FLAPSMALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07448SW 7678 FLAP FAIL CAUTION MESSAGE DURING LANDING APPROACH. REMOVED AND REPLACED RIGHT WING FLAP BPSU IAW AMM 27-51-10. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041222001502004122200150SO 2004 12 22 SWIA200414252 120041208A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07569SW 120344 EXIT LIGHT ON OVERHEAD BIN-ROW 9 IS INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222001512004122200151SO 2004 12 22 SWIA200414253 120041210A5753 FLAP TRACK EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07189SW 120048 ON TAKE OFF AFTER SELECTING FLAPS UP, RECEIVED "FLAP" AND "ADVANCED SWS" LIGHTS ON THE MAP. REMOVED AND REPLACED ALL MOVEABLE AND STATIONARY FLAP TRACKS, GUIDES AND ROLLER WITH SERVICEABLE UNITS IAW MM 57-53-04 AND 57-53-06. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222001522004122200152SO 2004 12 22 SWIA200414254 120041208A27523430001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07215SW1103211032 120281 FLAP DISAGREEMENT WHILE EXTENDING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT INBOARD FLAP ACTUATOR IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041222001622004122200162NM 2004 12 22 AWXA200401385 120041129A5320654583475 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 DURING C-15 CHECK A 1/2 INCH CRACK WAS FOUND IN UPPER ATTACH CHORD OF CABIN FLOOR INTERCOSTAL AT FORWARD END BS 345, LBL 17, WL 207.9. MAINTENANCE REMOVED CRACKED UPPER CHORD OFF CABIN FLOOR INTERCOSTAL FROM BS 344 TO BS 360, LBL 17. RECEIVED AND INSTALLED A NEW REPLACEMENT INTERCOSTAL UPPER CHORD IAW B737-300 SRM 51-40-02, FIG 3, 4, 8, & 12. 2L72 4F RTA16WE 20041222001652004122200165EU 2004 12 22 MALA040858 120041118A2612472326 FIRE LOOP SAAB SF340 340B 7860101EU NACELLE MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15447XJ 340B447 FIRE DETECT WARNING ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED NACELLE SENSING FIRE LOOP (AFT) PN 472326 IAW SAAB AMM 26-11-05-2, OP CHECK GOOD. 2L72 4T RTA52EU 20041223000082004122300008WP 2004 12 23 UPS04843609 120041215A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 EMERGENCY EXIT LIGHTS FAIL PRELIGHT TEST. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50, OPS CK GOOD. 2L74 4F RT4A25 20041223000132004122300013NM 2004 12 23 251TR0012 120041207A335020131A BATTERY PACK BOEING737 737228 13844AGNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05251TR 23792 EMERGENCY EXIT LIGHTS OUTSIDE OF L1 DOOR AND ABOVE L2 DOOR INOP. REPLACED BATTERY PACK AND OPS CHECKED GOOD PER MM 33-51-81. 2L72 4F RTA16WE 20041223000332004122300033SO 2004 12 23 CHQA000585 120041120A3350 BATTERY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT MALFUNCTIONED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11382 145624 WITH BATTERY AND EMERGENCY SWITCHES SET TO THE OFF POSITION, THE OVER WING EXIT LIGHTS ARE ILLUMINATING. REMOVED AND REPLACED THE NR 3 EMERGENCY BATTERY. OPS CHECK GOOD IAW EMB 140 MM 33-50-04. 2L72 4F RTT00011AT 20041223000452004122300045NM 2004 12 23 DHL2004783015 120041120A3297 CONNECTOR BOEING727 727227 1384078NM MLG DOOR DETACHED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01783DH 21999 R GEAR DOOR LIGHT ILLUMINATED WHEN HANDLE SELECTED OFF. PER ABNORMAL, RECYCLE HANDLE LIGHT OFF. CLEANED AND RESECURED CONNECTOR ON RT MLG DOOR SWITCH, TESTED RT MLG DOOR SWITCH IAW B-727 MM 32-62-11, NO DEFECTS NOTED. 2L73 4F A3WE 20041223000462004122300046SO 2004 12 23 SWIA200414270 120041211A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07562SW9563 9563 THE FIRST EMERGENCY EXIT LIGHT ABOVE CENTER AISLE IN PASSENGER CABIN WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041227000092004122700009 2004 12 27 DXTA200400447 420041110A2210H517A POSITION SENSOR CESSNA750 750 2076810CE RUDDER INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07953QS3515 7500153 YD FAIL UPPER A CAS MESSAGE DURING CLIMB. DETERMINED UPPER RUDDER POSITION SENSOR -A- WITH FAULT. REPLACED SENSOR -A-, DUE TO CAS MESSAGE DURING CLIMB, WITH FAULT. INSTALLED NEW SENSOR UNIT INTO -A- POSITION. DETERMINED UPPER RUDDER POSITION SENSOR "A" WITH FAULT. REPLACED SENSOR "A", DUE TO CAS MESSAGE DURING CLIMB, WITH FAULT. INSTALLED NEW SENSOR UNIT INTO "A" POSITION. DONE IAW CHAPTER 27-24-01 OF THE CESSNA 750 MAINT MANUAL. LEAK CHECK, OPS CHECK OK. CNQ2918C 2L72 4J RTT00007WI 20041227000102004122700010 2004 12 27 2004UALA01000 420041102A2565D30665105 CABLE AIRCRUISERS AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29411UA A5730 464 DOOR 2R WILL NOT ARM. THE CABLE AT BOTTOM OF SLIDE/RAFT ASSY WAS FOUND BROKEN WHICH DISRUPTED THE NORMAL FUNCTION OF EMERGENCY SELECTOR MECHANISM. THE SLIDE RAFT CABLE SYSTEM IN THE SLIDE LOWER LACING COVER IS A SENSITIVE DESIGN. RELEASING THE CABLE SYSTEM WOULD DROP THE SLIDE PACK FOR DEPLOYMENT. IN-SERVICE ABUSE, SUCH AS INADVERTENT IMPACT BY FOOD CARTS, ETC OR BY SOMEONE SITTING ON THE SLIDE BUSTLE COULD TRIGGER THIS UNWANTED RESULT. REPLACED 2R DOOR SLIDE. 2L72 4F4 FRTA28NM E40NE 20041227000112004122700011NM 2004 12 27 04FDEA03223 120041125A5310A5A7114519 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO - LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 37L. CENTER CARGO BETWEEN STA 5-123 TO STA 1531 LONGERON 37L CRACK LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II WITH NEW SPLICE FABRICATED AS PER DRAWING A5A7114 P/N FXA5A7114-519. 2L73 4F RTA22WE 20041227000222004122700022EU 2004 12 27 BA04030 120041214A3350321431 BATTERY AIRBUS330 A330323 3930335EU R1 DOOR DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19673UW 337 PHL ON TEST, FOUND R1 DOOR BATTERY PACK FAULTED. MAINTENANCE REPLACED THE BATTERY. 2L72 4F RTA46NM 20041227000302004122700030NM 2004 12 27 2004UALA01011 120041102A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 STRINGER 13L HAS 2 DENTS AT BS 1025 AND 1030. REMOVED DAMAGED SECTION OF THE STRINGER AND FABRICATED AND INSTALLED STRINGER AND SKIN DOUBLER. 2L72 4F4 FRTA16WE E2GL 20041227000322004122700032NM 2004 12 27 04FDEA03411 120041214A5511 SPAR BOEING727 727100 1384036NM LT HOR. STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 WHILE ACCESSING FRONT SPAR WEB FOR UPR SPAR REPAIR, LWR FRONT SPAR VERTICAL FLANGE CRACKED BETWEEN LT L/E STA 109 & 119. REPAIRED IAW SRM 55-10-5. 2L73 4F RTA3WE 20041227000392004122700039EU 2004 12 27 SA04094 120041006A335032145410 EPSU AIRBUSA319 A319112 3930323EU EMERGENCY LIGHTSFAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19706UW13586 946 THE EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041227000412004122700041 2004 12 27 SA04103 420041105A2565D30665105 SLIDE AIRBUS320 A320214 3930316EU PAX DOOR WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19109UW131194524 1065 DURING TROUBLESHOOTING, MAINTENANCE FOUND THE AFT LEFT PASSENGER DOOR SLIDE LACING WORN ALMOST ALL THE WAY THROUGH. MAINTENANCE REPLACED THE AFT LEFT DOOR SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20041227000472004122700047NM 2004 12 27 AWXA200401348 120041104A5755654645262A PANEL BOEING737 7373Y0 1384671NM SPOILER CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW19588 23684 MCN - FLIGHT CONTROL - DURING C-15 CHECK A .50 CRACK WAS FOUND ON NR 4 SPOILER CENTER OUTBOARD HINGE. MAINTENANCE REMOVED AND REPLACED NR 4 SPOILER PANEL ASSEMBLY IAW AMM 27-62-12. 2L72 4F RTA16WE 20041227000552004122700055NM 2004 12 27 2004UALA01196 120041208A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 AFT PIT FRAME UPPER FLANGE HAS ELONGATED HOLE AT BS 1620 BETWEEN STR 29L & STR 30L. INSTALLED REPAIR DOUBLER & FILLER. 2L72 4F4 FRTA2NM E17NE 20041228000292004122800029EU 2004 12 28 MALA040852 120041211A3020 CONNECTOR SAAB SF340 340B 7860101EU ANTI ICE CONTROLLOOSE A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15408XJ 340B408 LEFT INTAKE CYCLES ON/OFF. AIR RETURN TO DTW. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURES IAW SF340 MM 30-20-00. ALL CHECKS GOOD. DID FIND ONE CONNECTOR LOOSE ON CONTROLLER TIGHTEN AS REQUIRED. GROUND RAN FOR 30 MINUTES, ALL CHECKS GOOD. 2L72 4T RTA52EU 20041228000312004122800031NM 2004 12 28 MWEA040222 120041219A2420800027119 PCDU BOEING717 717200 1383700NM ENGINE INOPERATIVE A MWEAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 GL31919ME 55181 AFTER BOTH ENGINES WERE STARTED AND AUXILIARY POWER UNIT WAS SHUT DOWN BOTH GENERATORS CAME OFF LINE. REMOVED AND REPLACED LEFT AND RIGHT POWER CONVERSION AND DISTRIBUTION UNIT. 2L72 4F TRA6WE 20041228001012004122800101NM 2004 12 28 C1HA200493019 120041130A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 CABIN FLOORBEAM STA 1160 LBL 20 TO RBL 20 CORRODED TOP SIDE EA-10698, MAJOR. 2L73 4F A3WE 20041228001042004122800104NM 2004 12 28 QXEA200400901 120041220A6120 POTENTIOMETER DHAV DHC8 DHC8202 2809007NM NR 1 & 2 OUT OF RIG A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09357PH 504 SEA FLIGHT 2185 AUTOFEATHER FAILED TO ARM ON TAKEOFF. MAINTENANCE RIGGED NR 1 AND NR 2 POWER LEVER AUTOFEATHER ARMING POTENTIOMETERS IAW TEMP REVISION OF ENG RIG MAN PART 7, PARAGRAPH 5 AND 5-1. GROUND RAN AIRCRAFT AND FUNCTIONAL CHECK OF AUTOFEATHER SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041228001062004122800106NM 2004 12 28 SWAA043692 120041221A53106546529 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 460, STRINGER 13L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041228001122004122800112EU 2004 12 28 MALA040845 120041123A5280 DOOR BAC 146 AVRO146RJ85A1500097EU MLG CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT I/B MLG DOOR INNER SKIN FWD CUTOUT FWD RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001172004122800117EU 2004 12 28 DHL2004363014 120041218A3240 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01363DH 85 BRAKES GRAB ON RT SIDE. PERFORMED OPERATIONAL CHECK OF NORMAL, ALT, AND ANTI-SKID SYSTEMS. NO DEFECTS NOTED IAW MM 32-42-00. 2L72 4F RTA35EU 20041228001212004122800121NM 2004 12 28 QXEA200400886 120041214A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - PANEL 522CT HAS CORROSION IN NUMEROUS BOLT HOLES AND ON PANEL MATING SURFACE. REPLACED LEFT HAND WING FUEL PANEL 522 IAW Q400 WC 500ME28 60266. 2H72 4T RTA13NM 20041228001232004122800123WP 2004 12 28 UPS04843616 120041220A2150 A/C PACK DOUG DC8 DC871F 302199DWP BOTH ODOR A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01706UP 46056 ON TOP OF DESCENT STRONG DIESEL FUEL JET FUEL ODOR WAS PRESENT AND SMELLED. ODOR WAS VERY STRONG. PRESSURIZED A/C, RAN BOTH PACKS FOR 30 MIN. NO ODOR NOTED. INSPECTED A/C FOR SPILLED FLUIDS IN CARGO AREA AND LOWER PITS. NONE FOUND. A/C OK FOR SERVICE. 2L74 4F RT4A25 20041228001282004122800128EU 2004 12 28 MALA040839 120041123A5340 SUPPORT BRACKET BAC 146 AVRO146RJ85A1500097EU GIRT BAR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD ENTRY DOOR GIRT BAR FLOOR SUPPORT PLATE FROM FRAME 15-18 HAS POCKETS OF CORROSION. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001302004122800130EU 2004 12 28 MALA040843 120041123A5280 DOOR BAC 146 AVRO146RJ85A1500097EU MLG CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN AFT CUTOUT I/B FWD RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001332004122800133WP 2004 12 28 WX0400067 120041220A213139271411 REGULATOR VALVE DOUG DC9 DC983 3022083WP RT A/C PACK MALFUNCTIONED A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19891GA 49423 LAS TO OKC - DURING CLIMBOUT CREW REPORTED, UNABLE TO CONTROL TEMP IN AUTO OR MANUAL BOTH PACKS. OVERHEAT TRIPPED OFF RIGHT PACK. BOTH VALVES SHOW FULL COLD, CABIN SUPPLY TEMP 60 DEGREES CELSIUS. HP BLEED OFF, NO CHANGE. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WATER SEPARATOR FORWARD CLAMP AND REPLACED LEFT PRESSURE REGULATOR VALVE. SYSTEM OPERATIONALLY CHECKED GOOD ON GROUND. TEST FLIGHT COMPLETED SUCCESSFULLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041228001352004122800135EU 2004 12 28 AWXA200401417 120041220A3350321430 BATTERY AIRBUS320 A320232 3930326EU ZONE 221 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28602AW 565 PHX - EEL - DURING 4-DAY CHECK THE LT FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED BATTERY AT LEFT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041228001362004122800136EA 2004 12 28 COMA0460696 120041219A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA9794 7315 FLIGHT 5794 FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20041228001372004122800137WP 2004 12 28 04FDEA03423 120041216A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF DURING REMOVAL INLET DUCT IS NOTED EXFOLATION ON EXTERNAL SKIN STA 2160 RT SIDE B/T LONG 10-12 AND CRACK ON DOUBLER AJC7057-5. REPLACE INTERNAL DOUBLER P/N AJC7057-5 PER SRM 53-00-01 FIG 4 SHEET 2. 2L73 4F A22WE 20041228001392004122800139NM 2004 12 28 2004UALA01225 120041216A335020131A POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29120UA 29166 AFT EMERGENCY EXIT SIGN INOP. REPLACED CHARGER AND BATTERY PACK TO DM5934 CONNECTOR. 2L74 4F4 FRTA20WE E24NE 20041228001412004122800141NM 2004 12 28 SWAA043674 120041219A53106545569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 907, BETWEEN STRINGER 25R AND STRINGER 26R, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20041228001432004122800143NM 2004 12 28 SWAA043676 120041219A531065C25722 BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND STUB BEAM AT BS 616, RBL 64, CRACKED. REPAIRED STUB BEAM PER ER. 2L72 4F RTA16WE 20041228001442004122800144NM 2004 12 28 2004UALA01223 120041216A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 FWD PIT STA 580 AND BETWEEN STR 24L AND 25L, FRAME HAS DENT. INSTALLED "J" ANGLE REPAIR ON TOP OF FRAME. 2L72 4F4 FRTA2NM E17NE 20041228001482004122800148EA 2004 12 28 SWIA200414279 120041215A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 NM07588SW6902 6902 7069 ON TAXI OUT, SPOILERON CAUTION MESSAGE. INSTALLED SERVICEABLE SECU IN NR 1 POSITION. OPERATIONAL CHECK GOOD IAW 27-60-00. 2L72 4F RTA21EA 20041228001502004122800150NM 2004 12 28 04FDEA03445 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK: STA Y = 859 RT NR 2 SEAT TRACK FLANGE EXISTING DOUBLER REPAIR FOUND WITH CORROSION. DOUBLER EVALUATED & FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.1 VOL I. EXISTING DOUBLER AT MAIN DECK STA Y = 859 RT NR 2 SEAT TRACK FLANGE REMOVED & REPAIRED AS PER SRM 53-70-00 FIG.1 VOL I. 2L73 4F RTA22WE 20041228001522004122800152NM 2004 12 28 04FDEA03447 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK: STA Y = 859 LT NR 2 SEAT TRACK FLANGE EXISTING REPAIR DOUBLER FOUND WITH KNIFE EDGE. REPAIRED AS PER 53-70-00. 2L73 4F RTA22WE 20041228001532004122800153 2004 12 28 04FDEA03448 420041218A3420 DISPLAY AIRBUS310 A310322 3930334EU COCKPIT INTERMITTENT A FDEAC ABORTED TAKEOFF I FLT. ATTITUDE INST. TOTAKEOFF 1 SO25447FE 251 REJECTED TAKEOFF IND DUE TO F/O PFD & ND BLANKING AT ABOUT 95 KTS. DISPLAYS RETURNED BY THE TIME THE A/C STARTED SLOWING. BACK TO RAMP TO ALLOW BRAKES TEMPS TO COOL NO OTHER PROBLEM DEVELOPED WITH PFD/ND APPEARED NORMAL. SECOND TAKEOFF NORMAL. MALFUNCTION NOT VERIFIED ON GRD. F/O'S PFD & ND CK GOOD PER A310 AMM 34-71-00-5. 2L72 4F RTA35EU 20041228001542004122800154NM 2004 12 28 SWAA043668 120041218A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29367SW 26578 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E, STRINGER 25L, CRACKED. REPAIRED SKIN SECTION PER SRM. 2L72 4F RTA16WE 20041228001552004122800155NM 2004 12 28 SWAA043669 120041219A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 947.5, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA. 2L72 4F RTA16WE 20041228001562004122800156 2004 12 28 SWAA043643 420041216A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29639SW 27712 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041228001572004122800157NM 2004 12 28 SWAA043644 120041216A52306516352 STOP FITTING BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR AFT FRAME, LOWER STOP FITTING, CRACKED. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20041228001582004122800158NM 2004 12 28 SWAA043645 120041216A53106546550 DOOR FRAME BOEING737 7373H4 1384600NM CARGO BAY CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT FRAME AT BS 787, RBL 10, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041228001592004122800159NM 2004 12 28 SWAA043646 120041216A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED BETWEEN BS 827 AND BS 867, STRINGER 9R. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041228001602004122800160NM 2004 12 28 SWAA043647 120041216A55316546872 SPAR BOEING737 7373Y0 1384671NM VERTICAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR LT AND RT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED STAB PER ER. 2L72 4F RTA16WE 20041228001612004122800161NM 2004 12 28 SWAA043648 120041216A33503051F LAMP BOEING737 7373TO 138447GNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20041228001622004122800162NM 2004 12 28 SWAA043649 120041216A335007912 COVER BOEING737 7377H4 1384404NM EMERGENCY LIGHT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29414WN 29820 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 13 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM. 2L72 4F RTA16WE 20041228001632004122800163NM 2004 12 28 SWAA043650 120041216A33506104789 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29468WN 33858 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20041228001642004122800164NM 2004 12 28 SWAA043651 120041216A5753656546434 SKIN BOEING737 7373H4 1384600NM RT WING TE FLAP SEPARATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP, SKIN SEPARATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20041228001662004122800166EA 2004 12 28 COMA0460698 120041219A5610601R330332 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01918CA119942941 7018 FLIGHT 5435 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20041228001672004122800167EA 2004 12 28 VNAA0411005 120041127A5200 ACCESS DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE OPEN A VNAAA UNSCHED LANDING EW VIBRATION/BUFFET INADEQUATE Q C CLCLIMB 1 GL05223JS 7892 AFTER TAKEOFF THE CREW OF FLIGHT 2302 NOTICED A LOUD WHINE FROM THE FIRST OFFICERS SIDE PANEL AREA. THE AIRCRAFT RETURNED TO CLT WHERE MAINTENANCE FOUND THE AC ELECTRICAL-GROUND POWER ACCESS DOOR OPEN. THE DOOR WAS INSPECTED IAW CRJ 200 AMM 52-45-00-210-801 AND FOUND TO BE IN SERVICABLE CONDITION. THE DOOR WAS SECURED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041228001692004122800169EA 2004 12 28 COMA0460694 120041215A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA2043310814 7315 FLIGHT 5108 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20041228001702004122800170EA 2004 12 28 COMA0460695 120041217A5210601R3199831 ANGLE CNDAIR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01975CA21069 7150 7150 FLIGHT DURING HEAVY MAINTENANCE CHECK, (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH SRM STANDARD PROCEDURES. 2L72 4F RTA21EA 20041228001712004122800171EA 2004 12 28 COMA0470084 120041218A2780 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SLATS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01371CA 10082 FLIGHT 5866 SLAT FAIL CAUTION MESSAGE. RESET THE SFECU, SYSTEM OPERATIONAL CHECK SATISFACTORY. 2L72 4F RTA21EA 20041228001722004122800172NM 2004 12 28 SWAA043655 120041217A3350OL307IBPEGL LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29401WN 29813 FWD MOST LT EEPLS INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20041228001732004122800173 2004 12 28 SWAA043656 420041218A256563550 SLIDE BOEING737 7377H4 1384404NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29745SW 29491 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041228001742004122800174NM 2004 12 28 SWAA043657 120041218A2560P4010021 BATTERY BOEING737 7377H4 1384404NM FLASHLIGHT FAULTY A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 AFT EMERGENCY FLASHLIGHT WILL NOT SHUT OFF. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2L72 4F RTA16WE 20041228001752004122800175 2004 12 28 SWAA043658 420041219A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29329SW 23693 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20041228001762004122800176NM 2004 12 28 SWAA043659 120041219A3260 WARNING HORN BOEING737 7373T5 1384608NM MLG MALFUNCTIONED A SWAAO OTHER N FALSE WARNING APAPPROACH 1 SW29667SW 23063 COULD NOT SILENCE LANDING GEAR WARNING HORN ON APPROACH WITH FLAPS 30, 3 GREEN LANDING GEAR LIGHTS SHOWING. CYCLED ALL SYSTEMS, COULD NOT SILENCE HORN. INSPECTED LANDING GEAR AND FLAPS, NO DISCREPANCIES NOTED. C/W FLAP POSITION AND LANDING GEAR WARNING TEST PER MM, NO DEFECTS NOTED. 2L72 4F RTA16WE 20041228001772004122800177NM 2004 12 28 QXEA200400899 120041220A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09365PH32276581 526 BOI - DURING THE DAILY SYSTEMS CHECK, MAINTENANCE WAS UNABLE TO GET THE BAGGAGE SMOKE WARNING TEST 1 OR TEST 2 TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BAGGAGE SMOKE DETECTOR AND RELAMPED THE NR 1 SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041228001782004122800178EA 2004 12 28 COMA0460699 120041220A7931 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 1900309EA LT ENGINE OIL TRIPPED A COMAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO01798CA 7348 FLIGHT 5512 LEFT ENGINE OIL PRESSURE INDICATES ZERO. RESET TRIPPED CIRCUIT BREAKER. OIL PRESSURE INDICATES NORMAL. 2L72 4F RTA21EA 20041228001812004122800181EA 2004 12 28 SWIA200414284 120041005A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07588SW 7069 RIGHT SIDE SEAT RAILS CORRODED FROM FS 364 - 559+79. ITEM FOUND AT C-CHECK INSPECTION. SEAT RAILS REPLACED IAW CRJ SRM 51-41-02, 51-41-04, 51-23-00, REO 601R-53-00-055 REV NC. 2L72 4F RTA21EA 20041228001822004122800182NM 2004 12 28 2004UALA01214 120041214A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29323UA 23955 EMERGENCY EXIT FLOOR LIGHTS AT ROW 12 HAVE BEEN PULLED UP. REPLACED DAMAGED EEL STRIP. 2L72 4F4 FRTA16WE E2GL 20041228001832004122800183NM 2004 12 28 2004UALA01216 120041214A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29347UA 24251 AFT EMERGENCY FLOOR EEL LIGHTS INOP FROM MID TO AFT OF AIRCRAFT. REPLACED EEL LIGHTS MID TO AFT GALLEY. 2L72 4F4 FRTA16WE E2GL 20041228001842004122800184NM 2004 12 28 2004UALA01218 120041215A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 FRAME WEB CORRODED OUT OF LIMITS AT STA 1400 RT BETWEEN STR 28R AND 29R. REPLACED FRAME SECTION. 2L72 4F4 FRTA2NM E17NE 20041228001862004122800186NM 2004 12 28 2004UALA01220 120041215A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT PIT FRAME DENTED AT STA 1320 NEAR STR 26L AT INBOARD FLANGE. REPAIRED FRAME WITH INNER NESTED J-ANGLE. 2L72 4F4 FRTA2NM E17NE 20041228001872004122800187EU 2004 12 28 YENA200461 120041218A25304110001137 COFFEEMAKER AIRBUS320 A320232 3930326EU GALLEY ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15544JB9004 1835 ODOR IN THE REAR GALLEY OF BURNED ELECTRICAL SMELL. F/A CHECKED AREA AND FOUND SMELL IS COMING FROM ONE OF THE REAR COFFEEMAKERS. UNITS WERE SHUTOFF & SMELL WENT AWAY. REPLACED NR 2 AFT GALLEY COFFEEMAKER PER 25-35-15. OPERTIONS CHECK GOOD. 2L72 4F RTA28NM 20041228001912004122800191WP 2004 12 28 NACA20040064 120041220A7930220012C12 TRANSMITTER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE OIL PRESS INOPERATIVE A NACAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 AL0343872 533294 33553 PRECAUTIONARY ENGINE SHUTDOWN, DUE TO LOSS OF OIL PRESSURE ON NR 4 ENGINE, OIL PRESSURE LIGHT STAYS OFF. REPAIRED ELECT CONNECTIONS IN OIL TRANSMITTER CANNON PLUG. REPLACED NR 4 OIL PRESSURE TRANSMITTER. OPS AND LEAK CHECKS GOOD. 2L74 4R4 R A781 5E8 20041228001932004122800193 2004 12 28 YENA200462 420041219A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ROW 17 ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA15534JB728 1705 ELECTRICAL ODOR FROM ROW 17E ON SHORT FINAL TO LAS. SECURED LTV AND SMELL WENT AWAY. INSPECTED CABIN IAW TSM 24-00-00-810-823 AND NO DISCREPANCIES NOTED. ITEM WAS DEFERRED PER MEL 25-22-03 CONDITION 2. ON 12/20/04 REMOVED AND REPLACED SEB AT 17E DUE ELECTRICAL ODOR IN THAT AREA. 2L72 4F RTA28NM 20041228001942004122800194EA 2004 12 28 QXEA200400893 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - LEFT OUTBOARD SEAT RAIL CORROSION AT X738.00 AND X754. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041228001952004122800195NM 2004 12 28 CALA0400743 120041217A52306547952537 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND A 0.3 INCH CRACK AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01057. 2L72 4F RTA16WE 20041228001962004122800196NM 2004 12 28 CALA0400744 120041217A52306547952537 SKIN BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND TWO 0.3 INCH CRACKS AT LIGHTENING HOLE IN AFT CARGO DOOR INNER SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01056. 2L72 4F RTA16WE 20041228001972004122800197NM 2004 12 28 CALA0400745 120041217A534765458341 SEAT TRACK BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND SEAT TRACK BELOW G-1 GALLEY CORRODED AT STA 290. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02 AND BOEING DRAWING 69-45834. 2L72 4F RTA16WE 20041228001982004122800198NM 2004 12 28 CALA0400746 120041203A532065C807351 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED AT STA 991.5, RBL 46 TO LBL 46. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20041228001992004122800199NM 2004 12 28 CALA0400747 120041218A531365516989 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND A .5 INCH CRACK AT FASTENER OF STRINGER 4L SPLICE, STA 907. REPLACED STRINGER SPLICE IAW SRM 51-10-02. 2L72 4F RTA16WE 20041228002002004122800200NM 2004 12 28 CALA0400748 120041218A5314656215U25 KEELBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2761304 23355 INSPECTION FOUND LT SIDE KEELBEAM CORRODED BETWEEN STA 520 AND 540, LBL 10. A KEEL BEAM SPLICE REPAIR WAS INSTALLED IAW SRM 53-60-12, FIGURE 203. 2L72 4F RTA16WE 20041228002012004122800201NM 2004 12 28 DL73S041114 120041215A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 432. THE CRACK WAS REMOVED WITH A SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND ER/A 095531-14AD. 2L72 4F RTA16WE 20041228002022004122800202NM 2004 12 28 DL73S041115 120041215A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 512. THE CRACK WAS REMOVED WITH A 14 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095529-14AD. 2L72 4F RTA16WE 20041228002032004122800203SO 2004 12 28 CHQA000444 120040214A3350 SIGN EMB 145 EMB145MP 3260216SO CABIN INOPERATIVE A CHQAK NONE O OTHER ININSP/MAINT 1 GL11976 145322 EMERGENCY EXIT SIGN OVER AISLE IN GALLEY ARE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN OVER AISLE IN GALLEY AREA IAW EMB 145 MM 33-50-15. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041229000012004122900001 2004 12 29 04FDEA03469 420041222A2230 CONNECTOR DOUG MD10 MD1010F 3022112WP FLAP TRANSMITTERFROZEN A FDEAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 SO25360FE 46636 AFTER T/O THE UPPER FOOT CAME DOWN AND A/T'S WENT TO IDLE, THEN BTM FOOT CAME UP AND THROTTLES CLAMPED AND WENT TO MAX. DISC THROTTLES AND THEN FOOT CAME UP AND THROTTLES CAME TO MAX, CLAMP AGAIN. UPPER AND LOWER FOOT CYCLED INTO THE AIRSP CAUSING THROTTLES TO ALTERNATLEY GO FROM MAX TO IDLE. IT APPEARED THAT ACFT ONLY THOUGHT IT WAS TOO FAST. AIRSPEED WAS NEVER TOO FAST OR TOO SLOW FOR THE CONFIG. CHKD WIRING TO ROB FLAP TRANSMITTER FROM NR 1 FCC, NO FAULTS NOTED. FOUND CONNECTOR AT ROB TRANSMITTER ICED UP. REMOVED ICE AND DRIED PLUG REFER TO WRI 27- 50/2130 FOR CURRENT DEFERRAL PROCEDURE. USED ALTERNATE PROCEDURE FOR DEFERRAL WHICH REMOVES WIRE B502-1231 -22 FROM S3625. 2L73 4F RTA22WE 20041229000022004122900002NM 2004 12 29 249TR0050 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BS 1016 FLOORBEAM HAS CORROSION AT FLOORBOARD HOLES BL 0 TO LBL 20. REPAIRED PER EA 53-346. 2L72 4F RTA16WE 20041229000032004122900003NM 2004 12 29 249TR0074 120041222A5320 CHANNEL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON HAT SECTION AT FLOOR FOR LEFT COCKPIT DOOR WALL. REPLACED HAT SECTION PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000042004122900004NM 2004 12 29 249TR0089 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT RBL 8 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592 AND SRM 51-40-0. 2L72 4F RTA16WE 20041229000052004122900005NM 2004 12 29 249TR0042 120041222A5311 FRAME BOEING737 7372K5 138448XNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 AFT CARGO FRAME DAMAGED ON UPPER FLANGE AT BS 787 ABOVE STRINGER 26RT. REPAIRED PER SRM 51-70-11. 2L72 4F RTA16WE 20041229000072004122900007NM 2004 12 29 249TR0049 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BS 947 FLOORBEAM UPPER SURFACE AND FLOORBOARD ATTACH HOLES HAVE CORROSION. REPAIRED PER EA 53-340. 2L72 4F RTA16WE 20041229000082004122900008EA 2004 12 29 COMA0460700 120041220A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA4212 7132 FLIGHT 5316 FLAPS FAILED CAUTION MESSAGE. REPLACED THE LEFT SIDE NR 2 FLAP ACTUATOR. 2L72 4F RTA21EA 20041229000152004122900015EA 2004 12 29 SWIA200414300 120041223A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07919SW 7657 ON TAXI OUT FLIGHT SPOILER STATUS MESSAGE. REPLACED NR 1 AND NR 2 SECU IAW AMM 27-60-00, REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-61-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 01533, P/N 49-164-06, S/N OFF 01598, P/N 27000-7, S/N OFF 5494. 2L72 4F RTA21EA 20041229000162004122900016EA 2004 12 29 04359664 120041224A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 FRONT EMERGENCY FLOOR LIGHTING NOT WORKING AT OUTSTATION. FERRIED AIRCRAFT. MX REMOVED AND REPLACED FORWARD SECTION OF EMERGENCY LIGHTING. 2L72 4F RTA21EA 20041229000172004122900017NM 2004 12 29 249TR0068 120041222A5247 HINGE BOEING737 7372K5 138448XNM APU DOORS CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 ATTACH ANGLE AT FORWARD HINGE OF APU DOOR CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000182004122900018NM 2004 12 29 249TR0069 120041222A5324 CHANNEL BOEING737 7372K5 138448XNM FWD LAVATORY CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 AFT LAVATORY FORWARD PARTITION BOTTOM CHANNEL HAS CORROSION. REPLACED CHANNEL PER SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20041229000202004122900020EA 2004 12 29 SWIA200414294 120041218A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07587SW 7062 ON TAXI-OUT, GOT SPOILERON FAULT MESSAGE. REMOVED AND REPLACED LEFT SPOILERON OUTBOARD PCU IAW CRJ MM 27-62-09, OPERATIONAL CHECK GOOD. S/N OFF 3342. 2L72 4F RTA21EA 20041229000212004122900021EA 2004 12 29 COMA0470085 120041220A2150 ACM CNDAIRCL600 CL6002C10 1390015EA RIGHT FAILED A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01658CA 10148 FLIGHT 5835 SMOKE IN CABIN AND RT PACK HIGH TEMP. DEFERRED MAINT ON RT AC SYSTEM PER MEL. 2L72 4F RTA21EA 20041229000242004122900024NM 2004 12 29 249TR0086 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 967 TO BS 986 AT LBL 18 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0. 2L72 4F RTA16WE 20041222000992004122200099WP 2004 12 22 04FDEA03402 120041209A5230 VENT DOUG MD10 MD1010F 3022112WP CARGO DOOR LOOSE A FDEAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO25390FE 46624 UNABLE TO PRESSURIZE A/C. RETURNED TO PDX. FOUND HARDWARE DAMAGED AND LOOSE ON MAIN CARGO VENT DOOR. INSPECTED DOOR NO DAMAGED. REPLACED HARDWARE PER SMP. PERFORMED PRESSURIZATION CHECK. OPS CHECK NORMAL. 2L73 4F RTA22WE 20041222001012004122200101SO 2004 12 22 SWIA200414246 120041212A27503430001001 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07227SW7985 7985 120304 NACELLE FLAP DISAGREE ON RETRACTION. REPLACED RIGHT NACELLE FLAP ACTUATOR. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041222001032004122200103EA 2004 12 22 QXEA200400833 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL, TOP SURFACE AND LUG HOLE AREAS AT FS 702-708, FS 709-724 AND FS 736-452. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20041222001052004122200105WP 2004 12 22 WX0400050 120041108A5710 STRUCTURE DOUG DC9 DC983 3022083WP LT WING BIRD STRIKE A WX0AA UNSCHED LANDING O OTHER CLCLIMB 1 WP19865GA 49998 LAS - CREW REPORTED BIRD STRIKE LEFT WING TRAILING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-08. NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041222001072004122200107NM 2004 12 22 AWXA200401390 120041129A532069564081 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A 1 INCH CRACK WAS FOUND IN FORWARD UPPER CORNER OF INTERCOSTAL (WEB) ON AFT SIDE OF E/E COMPARTMENT DOOR CUTOUT BS 355, LBL 3, WL 156. MAINTENANCE CUTOUT DAMAGED FORWARD UPPER CORNER OF INTERCOSTAL AT BS 355, LBL 3; FABRICATED A FILLER AND ANGLE REPAIR; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-70-11, FIG. 1. 2L72 4F RTA16WE 20041222001122004122200112EU 2004 12 22 04FDEA03374 120041206A5530 STRUCTURE AIRBUS310 A310 EU VERTICAL STAB MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25452FE 313 VERTICAL STAB TOO LARGE COMPOSITE REPAIR ON LT SIDE L/E. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50375, DATED 06/23/2000. DAMAGED STEEL COVER WAS REPAIRED BY NEW ONE, IAW EA 6-5500-50375. 2L72 4F RTA35EU 20041222001612004122200161 2004 12 22 AWXA200401384 420041209A3414 INDICATOR BOEING737 7373G7 1384595NM AIRSPEED MALFUNCTIONED A AWXAC ABORTED TAKEOFF I FLT. ATTITUDE INST. TOTAKEOFF 1 WP28155AW 23777 ON TAKEOFF AT ABQ EN ROUTE TO PHX DURING 80 KT CROSS CHECK, THE FIRST OFFICERS AIRSPEED INDICATOR INDICATED 250 KTS AND INCREASING WITH RED FLAGS, REJECTED TAKEOFF AT 80 KTS AND RETURNED TO GATE ISSUED MEL 34-1 COND. 1 "F/O MACH INDICATOR INOP". MX R/R MACH AIRSPEED INDICATOR IAW BMM, OPS CHECK GOOD. VENDORS FUNCTIONAL TEST OF MACH AIRSPEED INDICATOR S/N 681 WAS NO FAULT FOUND, UNIT WAS INSPECTED AND TESTED IAW CMM. MX TROUBLESHOT WIRING AND FOUND PIN 44A OF THE NR 2 ADC PUSHED IN, REPLACED CONNECTOR D311A AT NR 2 ADC IAW BWDM 34-11-11. 2L72 4F RTA16WE 20041222001642004122200164NM 2004 12 22 200421 120041208A73328G1295 PRESSURE SWITCH DHAV DHC8 DHC8103 1386005NM LEFT ENGINE LEAKING A KPVAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13806WP 357 (PIREP) FUEL SMELL INTO CABIN AND COCKPIT WITH AIR CONDITIONING, ON GROUND ONLY. (MX) FOUND NR 1 ENGINE LOW FUEL PRESSURE SWITCH FAULTY. REPLACED NR 1 ENGINE FUEL PRESSURE SWITCH IAW, 8 MM, CHAP. 71-00-02 PG. 78-79. LEAK CHECK GOOD. (NOTE) PRESSURE SWITCH IS TO BE INSTALLED WITH SNUBBER ASSY P/N 8280191-001 OR LEAKAGE MAY OCCUR PER NOTE IN PW INSTALLATION MANUAL. ENGINE WAS RECEIVED ON AIRCRAFT (NEW TO FLEET) WITHOUT SNUBBER ASSY INSTALLED. 2H72 4T RTA13NM 20041222001662004122200166EU 2004 12 22 MALA040814 120041019A5210 ROLLER SAAB SF340 340B 7860101EU PAX DOOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED IB PAX DOOR ROLLER TRACK CORRODED. REPLACED IAW SAAB SRM 51-40-27. REFER TO NRC NR 196555 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2L72 4T RTA52EU 20041222001782004122200178 2004 12 22 P9RA20040049 420041105A2565100502115 SLIDE DOUG DC9 DC982 3022082WP L2 DOOR DEPLOYED A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO1110801941 49127 THE L2 DOOR WAS PARTIALLY OPEN WHEN A GUST OF WIND FORCED THE DOOR TO THE FULL OPEN POSITION CAUSING THE SLIDE BOTTLE TO DEFLATE AND PARTIALLY DEPLOY THE SLIDE. 2L72 4F A6WE 20041222001802004122200180EU 2004 12 22 NACA20040062 120041124A3234F96GA0102 CONTROL LEVER AEROSPATR42 ATR42* 8680900EU MLG SHORTED A NACAO OTHER O OTHER LDLANDING 1 AL0342NC 067 LANDING GEAR WOULD NOT EXTEND NORMALLY. HAD TO USE MANUAL EXTENSION CONTROL. REPLACED LANDING GEAR CONTROL LEVER. OP CHECKED GOOD. 2H72 4T RTA53EU 20041222001812004122200181 2004 12 22 IXXA0400120O 420041107A23115221501041 TRANSCEIVER DOUG DC8 DC862F 3021972WP COCKPIT BROKEN A IXXAA UNSCHED LANDING O OTHER CRCRUISE 1 SW1141CX 7648828 46129523 DURING FLIGHT FROM KSUU TO PHIK, HF NR 1 AND NR 2 RADIO REPORTED TO HAVE LOUD BACKGROUND SQUEAL AND IS UNREADABLE. CREW RETURNED AIRCRAFT TO KSUU AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 HF ACCESSORY COUPLER AND NR 2 HF R/T. OPERATIONAL CHECKS WERE GOOD PER ALL APPLICABLE MANUALS. 2L74 4F 4A25 20041222001822004122200182NM 2004 12 22 AWXA200401361 120041207A2560P4010021 BATTERY BOEING737 737301 1384611NM ZONE 900 DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28324AW 23261 LAS - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK, THE AFT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041223000052004122300005EU 2004 12 23 MALA040830 120041123A5347 SKIN BAC 146 AVRO146RJ85A1500097EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, A DENT WAS FOUND IN THE FUSELAGE SKIN BELOW THE AFT CARGO DOOR. MAINTENANCE REPAIRED FUSELAGE SKIN IAW EO A53098. COMPLY WITH EO A53098. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041223000072004122300007WP 2004 12 23 UPS04843608 120041213A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 EMERGENCY LIGHTS NO ILLUMINATION. REMOVED AND REPLACED BATTERY PACK, OPS GOOD MM 33-50-00. 2L74 4F RT4A25 20041223000322004122300032SO 2004 12 23 CHQA000587 120041121A2121 FAN EMB 145 EMB145LR 3260212SO E/E BAY OBSTRUCTED A CHQAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL11272 145306 CREW REPORTED THEY FAINTLY DETECTED A BURNING RUBBER AND ELECTRICAL ODOR DURING LANDING. AT THE GATE WITH THE PASSENGERS OFF THE AIRCRAFT THE ODOR BECAME VERY STRONG AND WAS LOCATED NEAR THE FORWARD COAT CLOSET. MAINTENANCE FOUND INSULATION IN THE LT AVIONICS FAN. REMOVED INSULATION FROM FAN IAW EMB 145 AMM 21-21-04. NO ODOR NOTED AT THIS TIME. 2L72 4T RTT00011AT 20041223000442004122300044NM 2004 12 23 DHL2004783014 120041119A335010604503 RELAY BOEING727 727227 1384078NM EMERGENCY LIGHT FAILED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01783DH 21999 EMERGENCY EXIT LIGHTS ILLUMINATED AFTER GOING TO SHIPS POWER. DEFER APU DUE TO EXTERNAL PWR RELAY STICKING AND GEN RELAY PER MEL REF 49-1, CONTROL NR 18533 , PLACARD INSTALLED. DEFER APU DUE TO EXTERNAL PWR RELAY STICKING AND GEN RELAY PER MEL REF 49-1, CONTROL NR 18533, PLACARD INSTALLED. FOUND EMERGENCY LIGHT RELAY TO BE BAD. REMOVED AND REPLACED RELAY, SYS OPS CK NORMAL IAW BMM CH 33-50-00, THIS CLEARS DMI NR 18533, PLACARD REMOVED, P/N INSTALLED, 10-60450-3 NO S/N. 2L73 4F A3WE 20041227000152004122700015NE 2004 12 27 P5CA0401277 220041106A7200 ENGINE BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE NR 1 MALFUNCTIONED A P5CAJA DUMP FUEL UNSCHED LANDING MAXOVER TEMP FLAME/FIRE ENGINE FLAMEOUT CLCLIMB 1 EA15920FT 22237 702192 IN CLIMB AT 9200 FT NR 1 ENGINE EGT WENT TO 771 FOR 18 SECOND, FOLLOWED BY A LOUD BLAST & BRIGHT FLASH OF LIGHT FROM LEFT SIDE OF A/C, WINDMILL TIME 50 MINUTES,MINIMUM OIL PRESSURE 5 PSI. REVIEWED EXCEDANCE,FOUND WITH IN LIMITS.VISUAL INSPECTION ACCOMPLISHED,FOUND FUEL CONDITION MOTOR C/B POPPED,REPLACED CONTINOUS ACTUATOR,PERFORMED ENGINE RUN. 2L74 4F4 F A20WE E3NE 20041227000162004122700016NM 2004 12 27 2004UALA01010 120041101A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 PUNCTURED HOLE IN FUSELAGE AT STA 1862 UPPER LT SIDE. PUNCTURE DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA2NM E17NE 20041227000182004122700018EU 2004 12 27 0402163235 120041214A2121 FAN AIRBUS320 A320212 3930322EU CABIN FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01335NW 340 DURING CRUISE, PILOTS EXPERIENCED SLIGHT SMOKE AND BURNING ODOR. DIVERTED TO DES MOINES AND LANDED UNEVENTFULLY. INSPECTED CABIN, AVIONICS BAY, AND CARGO BAYS AND FOUND NO DEFECTS. FOUND LEFT CABIN FAN SUPPLY CIRCUIT BREAKER POPPED AND LEFT FAN INDICATION IN THE COND PAGE. APPLIED MEL PROVISIONS FOR LEFT CABIN FAN. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20041227000202004122700020NM 2004 12 27 2004UALA01157 120041124A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 AFT PIT FRAME DENTED UPPER FLANGE AT STA 1500 AND STR 26L. INSTALLED J ANGLE REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20041227000252004122700025NM 2004 12 27 04FDEA02978 120041022A5753ARC7482501 SUPPORT FITTING DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RT WING - INBOARD FLAP VANE, OUTBOARD SUPPORT FITTING INBOARD HOLES (03 OFF) ARE CORRODED. ALL BORES ARE NOT WITHIN EO LIMITS. SUPPORT FITTING REPLACED AS PER AMM27-50-24 AND FUNCTIONAL TEST CARRIED OUT AS PER AMM 27-50-00-860-801. 2L73 4F RTA22WE 20041227000272004122700027EU 2004 12 27 SA04115 120041210A3397D9299200900000 WIRE HARNESS AIRBUSA319 A319112 3930323EU PASSENGER CABIN SHORTED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19718UW 1077 TPA - THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 19, LEFT SIDE, WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT HARNESS. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20041227000512004122700051EU 2004 12 27 2004UALA01047 120041111A5610NP1653016 WINDSHIELD AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29408UA 457 FIRST OFFICER'S WINDSHIELD CRACKED. CRACK APPEARS TO HAVE INITIATED FROM A BUBBLE AT THE TOP CENTER OF THE WINDOW WHICH DID NOT IMPAIR VISIBILITY. 2L72 4F4 FRTA28NM E40NE 20041227000522004122700052NM 2004 12 27 04FDEA03026 120041108A5320ACA71501 SPLICE DOUG MD11 MD11F 3023600NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 FORWARD CARGO COMPARTMENT - STA 755 TO 775 STR 43L SPLICE FOUND CRACKED. FORWARD CARGO COMPARTMENT - STA 755 TO 775 STR 43L AREA SPLICE REMOVED AND REPLACED AS PER SRM 51-31-01 & 51-33-01 VOL II. 2L73 4F RTA22WE 20041228000012004122800001GL 2004 12 28 EOO2004FAA 220040802A732123070606 FUEL CONTROL HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENGINE INOPERATIVE E EOOAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 AL03CFASX 588 1150D CAE833881 PILOT COMPLAINED IDLE WAS AT 55 PERCENT, AND IT WAS. WHEN ADJUSTMENT WAS ATTEMPTED IT WAS DISCOVERED THAT THERE WAS NO DRAG TORQUE ON THE IDLE SCREW. THE SCREW WAS ADJUSTED UNTIL DRAG WAS ENCOUNTERED (THIS HAD TO BE DONE WHILE THE ENGINE WAS NOT RUNNING). STARTED THE ENGINE AND IT IDLED AT 76 PERCENT, ONE FLAT BACK BROUGHT IT TO 74 PERCENT N, AND THEN THERE WAS NO DRAG TORQUE AND IT WOULD VIBRATE DOWN TO 55 PERCENT N, AGAIN. READJUSTED THE SCREW TO WHERE THE DRAG OCCURRED AND ADDED 1 FLAT. REMOVED THE UNIT AND WHEN IT COOLED, IT TOOK OVER 1.5 TURNS TO LOOSEN DRAG TORQUE. REPLACED UNIT. 1G71 3U3 U H3WE E4CE 20041228000042004122800004EU 2004 12 28 AWXA200401226 120041102A4930 FUEL CONTROL AIRBUS320 A320232 3930326EU APU FAILED A AWXAFD ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 WP28650AW 856 DURING TAXI, FLAMES REPORTED AT APU BY ANOTHER ACRFT, FIRE CHIEF CONFIRMED SMALL FLAME IN TAILPIPE, DISCHARGED APU FIRE BOTTLE PER FIRE CHIEFS RECOMMENDATION. NO INDICATIONS NOTED IN COCKPIT, APU HAD BEEN SHUTDOWN LESS THAN TWO MINUTES FOLLOWING NR 2 ENG START. MX INSPECTED APU IAW AMM; NO DAMAGE NOTED. ISSUED MEL. A FOLLOW UP WRITTEN TO REPLACED APU FUEL FLOW DIVIDER AND FUEL CONTROL UNIT. MAX R/R APU FCU IAW AMM, & FUEL DIVIDER IAW AMM, LEAK & OPS CHKS GOOD.FUEL CONTROL UNIT FAILED FOR LOW PUMP PERFORMANCE. DISASSEMBLY OF UNIT FOUND THE GEAR SHAFT AND ALL FOUR BEARINGS ERODED, REPLACED SHAFT AND BEARINGS. UNIT CALIBRATED, TESTED, & RETURNED TO SERVICE IAW CMM 49-30-97. 2L72 4F RTA28NM 20041228000082004122800008EU 2004 12 28 MALA040849 120041107A2520 HEADREST BAC 146 AVRO146RJ85A1500097EU CABIN SEAT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FROM 409, 224359 TEN SEAT HEAD RESTS CRACKED. MAINTENANCE REPAIRED IAW EO A25041. REFER TO 409, 224375 FOR ADDITIONAL DETAIL. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228000102004122800010NM 2004 12 28 C1HA200493018 120041121A5320 WEB BOEING727 727212 138407GNM FUSELAGE CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 WEB AT BS 825.95 RBL 62 WL 208 IS CRACKED, VIEWED FROM BELOW. REPLACED WEB, MINOR. 2L73 4F A3WE 20041228000172004122800017NM 2004 12 28 C1HA200493021 120041126A5320 CLIP BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 FRAME TO CUSP WEB CLIP IS CORRODED ON STA 1166 FRAME AT STR 17L. INSTALLED NEW CLIP, MINOR. 2L73 4F A3WE 20041228000382004122800038NM 2004 12 28 AALA20041234 120041218A3350 BALLAST BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21773AN 29583 SIDEWALL EMERGENCY LIGHT ABOVE SEAT 10A INOPERATIVE. REPLACED BALLAST ASSEMBLY FOR SIDEWALL EMERGENCY LIGHT ABOVE SEAT 10A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041228000402004122800040NM 2004 12 28 SWAA043683 120041220A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND 3 EACH FUSELAGE FRAMES CRACKED BETWEEN BS 867 AND BS 787, STRINGER 9L AND BS 787, STRINGER 9R. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20041228000432004122800043NM 2004 12 28 SWAA043689 120041220A53156546811 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, BETWEEN LBL 47 AND RBL 47, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER EA. 2L72 4F RTA16WE 20041228000452004122800045NM 2004 12 28 C1HA200493003 120041122A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 FS 1090 FLOORBEAM IS CORRODED FROM LBL 35 TO LBL 63. SRM REPAIR MAJOR. 2L73 4F A3WE 20041228000472004122800047NM 2004 12 28 C1HA200493009 120041119A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 SEAT TRACK LBL 45 STA 1130-1090 CORRODED SEVERAL AREAS. 2L73 4F A3WE 20041228000482004122800048NM 2004 12 28 SWAA043704 120041221A53116558280 FRAME BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 360, BETWEEN STRINGER 14R AND STRINGER 15R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20041228000522004122800052EU 2004 12 28 MALA040838 120041123A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD CABIN FLOORBEAM AT FRAME 18 AND SEAT TRACK 3 (RT IB) UPPER FLANGE EDGE AND GUSSET PLATE CORRODED. MAINTENANCE REPAIRED IAW EO A53224. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228000552004122800055NM 2004 12 28 QXEA200400902 120041220A2611PU90461S SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY FAILED A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09368PH14773 512 SEA - FLIGHT 2051 - THE CREW REPORTED THE LAVATORY SMOKE DETECTOR SOUNDED DURING THE CLIMBOUT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041228000572004122800057NM 2004 12 28 C1HA200493013 120041126A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 CABIN SEAT TRACK HAS CORROSION AND BARE METAL LBL 45 FS 852-868. REPLACED SEAT TRACK. 2L73 4F A3WE 20041228000592004122800059 2004 12 28 P9RA20040056 420041218A2565BACB30LT4U14 BOLT BOEING757 757231 1384950NM BACKED OUT A P9RAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO11708TW 28480 MAINTENANCE ENTRY L4 DOOR ARMED CONDITION INDICATOR INOPERATIVE. PLACED ON MEL 25-66-4. MAINTENANCE ENTRY 12/19/2004. REFERENCE MEL 25-66-4. REINSTALLED BOLT IN CONTROL ROD MECHANISM. BOLT HAD BACKED OUT OF NUTPLATE. OPS CHECKED NORMAL AND REMOVED MEL. 2L72 4F RTA2NM 20041228000612004122800061NM 2004 12 28 AWXA200401425 120041202A534069353509 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT STRINGER TIE CLIP AT BS 500, STR 28 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500, STR 28 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 65-46533; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4 & 8. 2L72 4F RTA16WE 20041228000632004122800063NM 2004 12 28 AWXA200401427 120041202A5755654645165A PANEL BOEING737 7373G7 1384595NM NR 9 SPOILER DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK THE UPPER SURFACE OF THE NR 9 SPOILER WAS FOUND DELAMINATED AT THE INBOARD END BETWEEN WBL 290.07 RT AND WBL 293.07 RT. MAINTENANCE CUT OUT DAMAGED AREA OF NR 9 SPOILER SKIN; FABRICATED A FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20041228000672004122800067WP 2004 12 28 AALA20041236 120041220A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21415AA 49326 SFO - OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR ALL OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041228001452004122800145NM 2004 12 28 AWXA200401411 120041219A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM ZONE 900 DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28819AW 1395 DURING 4-DAY CHECK THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20041228001802004122800180NM 2004 12 28 2004UALA01207 120041212A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 MAIN CABIN AT BS 1661 FLOORBEAM CORRODED BETWEEN BL 0 AND LBL 1. FABRICATED & INSTALLED STRAP REPAIR TO UPPER CHORD. 2L72 4F4 FRTA2NM E17NE 20041229000062004122900006NM 2004 12 29 249TR0043 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON BS 344 FLOORBEAM. REPAIRED PER SRM 53-10-9. 2L72 4F RTA16WE 20041229000102004122900010EA 2004 12 29 04359646 120041224A2430 GENERATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 FAILED A VTZAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA27646BR 7392 NR 2 GENERATOR FAIL, APU INTAKE DOOR CLOSED. RTF. GEN AND APU WERE DEFERRED. WORK STILL WAITING TO BE SCHEDULED AT THAT TIME, A/C BEING AT REPAIR STATION FOR DAMAGE NOT RELATED TO THIS EVENT. 2L72 4F RTA21EA 20041229000112004122900011NM 2004 12 29 249TR0041 120041222A5240 ANGLE BOEING737 7372K5 138448XNM R-2 DOOR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 R-2 DOOR Z-ANGLE CORRODED. REPLACED Z-ANGLE PER SRM 51-30-2 AND SRM 51-10-1. 2L72 4F RTA16WE 20041229000132004122900013EU 2004 12 29 MALA040888 120041106A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15408XJ 340B408 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY 3301-51, S/N 1353 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31, UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/12/04. 2L72 4T RTA52EU 20041229000192004122900019NM 2004 12 29 249TR0087 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL AT BS 947+14 FROM RBL 17 TO RBL 44 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000232004122900023SO 2004 12 29 LR7A04200 120041110A5512 SKIN LKHEED382 382G 526414USO HORIZONTAL STAB CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 484 4590 DURING SCHEDULED A CHECK PER JOB CARD HA1200 FOUND FS 1078 HORIZONTAL STAB LOWER SKIN CRACKED 1.5 INCH SPANWISE AT RBL 46, WL 223. REPAIRED IAW SRM SMP 583 55-20-06. LP 15658, GMM133 ITEM M3. 2H74 4T A1SO 20041229000262004122900026NM 2004 12 29 249TR0051 120041222A5313 STRINGER BOEING737 7372K5 138448XNM FUSELAGE MISREPAIRED A PIDAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO05249TR 22598 STRINGER REPAIR NOT PER SRM AT STR 13LT. REPAIRED STRINGER PER SRM 53-10-3. 2L72 4F RTA16WE 20041229000272004122900027NM 2004 12 29 249TR0058 120041222A5347 SEAT TRACK BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON SEAT TRACK FROM BS 344 TO BS 366 AT LBL 22. REPAIRED PER SRM 53-10-5. 2L72 4F RTA16WE 20041229000302004122900030NM 2004 12 29 249TR0065 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL CORRODED BETWEEN BS 927 AND BS 907 AT RBL 8. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000312004122900031 2004 12 29 249TR0100 420041222A2210158000104 ACTUATOR BOEING737 7372K5 138448XNM ELE SERVO ACT LEAKING A PIDAK NONE K FLUID LOSS ININSP/MAINT 1 SO05249TR 22598 EVIDENCE OF FLUID LEAK FROM -A- SYSTEM AUTO PILOT ELEVATOR SERVO ACTUATOR. FOUND -B- SYSTEM AUTO PILOT ACTUATOR LEAKING DOWN ONTO -A- SYSTEM ACTUATOR. REPLACED -B- SYSTEM ACTUATOR PER MM 22-11-261. 2L72 4F RTA16WE 20041229000322004122900032NM 2004 12 29 QXEA200400915 120041223A335061047811 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAO OTHER O OTHER TXTAXI/GRND HDL 1 NM09369PH1439 270 513 SEA - ON FLIGHT NUMBER 2155, TOP EMERGENCY EXIT SIGN AT DOOR 1E ILLUMINATED DURING TAXI, ALL OTHERS WERE DARK. ON TAKEOFF SIGN GOT BRIGHT THEN WENT DIM, THEN DARK. MAINTENANCE INSPECTED AND FOUND BATTERY PACK AT CONNECTOR 3351-P TO BE DEAD. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229000332004122900033NM 2004 12 29 QXEA200400916 120041224A33506104781 BATTERY PACK DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09369PH505 513 SEA - EMERGENCY EXIT SIGN ABOVE GALLEY, AT RIGHT FORWARD EXIT DOOR, RIGHT FORWARD EXTERIOR EGRESS LIGHT, AND SECOND AFT CEILING LIGHT ARE ALL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY AND POWER SUPPLY 3351 PS 2, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229000352004122900035EA 2004 12 29 QXEA200400905 120041217A5311 STRAP CNDAIRCL600 CL6002C10 1390015EA ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - GOUGE IN INNER, UPPER FRAME STRAP ON UPPER AFT CORNER OF MAIN CABIN DOOR FRAME STRUCTURE AT FS 349.00. REPAIRED IAW HORIZON AIR EA R-53-247. 2L72 4F RTA21EA 20041229000362004122900036EA 2004 12 29 QXEA200400906 120041215A2910 LINE CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - RIGHT HAND SIDE PYLON PRESSURE PAN HAS CRACK AT AFT EDGE OF CUTOUT FOR THE NR 2 PRESSURE LINE. REPAIRED IAW CRJ SRM 51-42-06. 2L72 4F RTA21EA 20041229000412004122900041NM 2004 12 29 AALA20041238 120041221A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21175AN 32394 DFW - SEAT MOUNTED LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041229000442004122900044NM 2004 12 29 AALA20041237 120041222A3350D71702001 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21905AN 29507 RNO - CABIN EMERGENCY LIGHTS AT RIGHT SIDE SEAT ROWS 12 TO 14, 21 TO 27 AND LEFT SIDE SEAT ROWS 12 TO 20 FAILED TEST. REPLACED BATTERY PACK FOR CABIN EMERGENCY LIGHTS AT RIGHT SIDE SEAT ROWS 12 TO 14 AND 21 TO 27 AND LEFT SIDE ROWS 12 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20041229000462004122900046EU 2004 12 29 MALA040877 120041122A5246 DOME SAAB SF340 340B 7860101EU LAV SERVICE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, LAV SERVICE DOME IS CORRODED OUT OF LIMITS AND IS BEING REPLACED IAW SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229000472004122900047EU 2004 12 29 MALA040870 120041118A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15367PX 340B271 DURING 4Y/2Y INSPECTION IN BNA, FRAME CHAFED ON RT SIDE AT FS 686.888 WAS REPAIRED IAW EO S53261. AIRCRAFT RETURNED TO 11/23/04. 2L72 4T RTA52EU 20041229000482004122900048EU 2004 12 29 MALA040871 120041118A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15367PX 340B271 DURING 4Y/2Y INSPECTION IN BNA, GALLEY SEAT TRACK P/N 7253721-459 CORRODED. MAINTENANCE REMOVED AND REPLACED. AIRCRAFT RETURNED TO 11/23/04. 2L72 4T RTA52EU 20041229000502004122900050EU 2004 12 29 MALA040866 120041216A2910 HYDRAULIC SYSTEM SAAB SF340 340B 7860101EU YELLOW SYSTEM LOW A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15413XJ 340B413 AT CRUISE AT FL18,0 HYD QTY BEGAN TO DROP INTO THE YELLOW QTY CONTINUED TO DROP UNTIL IT REACHED JUST ABOVE RED LINE. PER QRH TURN PUMP OFF. EXTENDED GEAR AND FLAPS NORMALLY USING PUMP. WHEN PUTTING GEAR DOWN QTY WENT BACK TO BOTTOM OF THE GREEN ARC. WHEN USING FLAPS QTY DROPPED AGAIN INTO TO YELLOW. AFTER LANDING QTY WENT BACK INTO THE GREEN. MAINTENANCE SERVICED AND REPLENISHED PER AAM 12-10-29. PRESSURIZED ALL HYDRAULIC SYSTEMS. NO LEAKS NOTED AND PRESSURES CHECKED GOOD. AIRCRAFT OK FOR RETURNED TO SERVICE. 2L72 4T RTA52EU 20041229000542004122900054EU 2004 12 29 MALA040880 120041125A3350549132406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15407XJ 340B407 EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N 1639 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. REPLACED CELL PACKS P/N 549-1324-06 UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 11/28/04. 2L72 4T RTA52EU 20041229000562004122900056NM 2004 12 29 249TR0046 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BS 1016 FLOORBEAM LOWER -T- HAS CORROSION AT LBL 13. REPAIRED PER EA 53-342. 2L72 4F RTA16WE 20041229000602004122900060EA 2004 12 29 SWIA200414298 120041221A2752 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07448SW FLAPS FAIL AT 0 DEGREES. REPLACED NR 1 AND NR 3 ACTUATORS, OPERATIONAL CHECK GOOD. P/N (NR 1RT) 852D100-19, S/N OFF 3947, P/N (NR 3RT) 853D100-20, S/N OFF 1912. 2L72 4F RTA21EA 20041229000612004122900061NM 2004 12 29 AALA20041245 120041215A5312 BULKHEAD BOEING767 767223 1385123NM FUSELAGE CUT A AALAK NONE O OTHER ININSP/MAINT 1 SW21323AA 22324 MCI - RIGHT HAND BULKHEAD WEB OUTER EDGE CUT DURING CHORD ANGLE REMOVAL. ONE HALF INCH CUT AT STATION 1809.5. REPAIRED CUT WITH TRIM OUT AND FILLER PER MRB 767 2640. 2L72 4F RTA1NM 20041229000622004122900062WP 2004 12 29 AALA200411242 120041223A3350P4010049 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21481AA 49656 RDU - AFT SECTION SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT SECTION SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041229000642004122900064 2004 12 29 AALA20041244 420041222A2565 GIRT BAR BOEING777 777223 1385213NM ESCAPE SLIDE MISINSTALLED A AALAK NONE O OTHER ININSP/MAINT 1 SW21793AN 30255 DFW - FOUND RIGHT NR 2 SLIDE GIRT BAR INSTALLED UPSIDE DOWN. REPLACED SLIDE FOR RIGHT NUMBER 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041229000652004122900065SO 2004 12 29 C2XA04BT129 120041211A3397 CONNECTOR EMB 145 EMB145LR 3260212SO BATTERY CHARGER FAULTY A C2XAO OTHER O OTHER CRCRUISE 1 SW2716981 145208 EWR - CREW REPORTED, EMERGENCY LIGHTS STAYED ON IN FORWARD SECTION OF THE CABIN FOR TWO MINUTES WHILE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED CONNECTOR ON NR 2 BATTERY CHARGER P8501 IAW EMB 145 AMM 25-23-09. OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20041229000682004122900068NM 2004 12 29 249TR0047 120041222A5340 ATTACH ANGLE BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BS 947 FRAME TO SKIN ATTACH ANGLE CRACKED AT STR 17RT. REPLACED ATTACH ANGLE PER SRM 51-30-2. 2L72 4F RTA16WE 20041229000712004122900071NM 2004 12 29 249TR0093 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON INTERCOSTAL AT LAV DOOR FROM BS 294 TO BS 312. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-2. 2L72 4F RTA16WE 20041229000722004122900072EA 2004 12 29 QXEA200400909 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 695.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND SRM TASK 51-21-16. 2L72 4F RTA21EA 20041229000742004122900074EA 2004 12 29 QXEA200400912 120041012A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 508.00, FS 540.00, FS 553.00 AND FS 572.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041229000752004122900075EA 2004 12 29 QXEA200400913 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 490.00, FS 508.00, FS 522.00, FS 540.00, FS 552.00 AND FS 572.00. REPAIRED IAW AMM 53-00-49-400-801. 2L72 4F RTA21EA 20041229000762004122900076EA 2004 12 29 QXEA200400910 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 582.00 AND FS 665.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND SRM 51-21-16. 2L72 4F RTA21EA 20041229000792004122900079EU 2004 12 29 MALA040876 120041116A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, FUSELAGE IS DENTED AT LOWER FUSELAGE, BELOW CARGO DOOR AND WAS REPAIRED IAW MESABA EO S53253. AIRCRAFT WAS RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229000812004122900081EU 2004 12 29 MALA040872 120041122A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, UPPER FUSELAGE IS DENTED FWD OF FRAME 560 AT 12 O'CLOCK POSITION AND WAS REPAIRED IAW MESABA EO S53035. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229000822004122900082EU 2004 12 29 MALA040886 120041113A3350549123406 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15418XJ 340B418 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY P/N 501-1712-02, S/N OFF 2003 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY PACKS P/N 549-1234-06, UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/17/04. 2L72 4T RTA52EU 20041229000852004122900085EU 2004 12 29 MALA040878 120041123A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 IS CORRODED BETWEEN FS 608 AND 640 AND IS BEING REPAIRED IAW MESABA EO S53079. AIRCRAFT WAS RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229000872004122900087SO 2004 12 29 CHQA000598 120041224A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11836 145713 EMERGENCY FLOOR PROXIMITY STRIP IS INOP. INSTALLED NEW FLOOR PROXIMITY LIGHT STRIP IAW EMB 135 AMM 33-50-12. 2L72 4F RTT00011AT 20041229000882004122900088NM 2004 12 29 249TR0078 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSLEAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 FORWARD SIDE OF LOWER TEE AT LEFT SIDE OF BS 1006 FLOORBEAM OUTBOARD ATTACH ANGLE HAS CORROSION. REPLACED ATTACH ANGLE PER SRM 51-10-1 AND 51-10-2 AND 51-30-0. 2L72 4F RTA16WE 20041229000912004122900091SO 2004 12 29 CHQA000600 120041224A3350 LIGHT EMB 135 EMB135KL 3260302SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11372 145538 LEFT OVERWING EMERGENCY LIGHT IS INOP. RELAMPED LEFT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD PER EMB 140 MM 33-50-10. 2L72 4F RTT00011AT 20041229000942004122900094NM 2004 12 29 249TR0077 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT LBL 41 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592. 2L72 4F RTA16WE 20041229000952004122900095NM 2004 12 29 249TR0082 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 DIAGONAL INTERCOSTAL FROM BS 1006 TO BS 1016 AT AFT LAV THRESHOLD HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000962004122900096NM 2004 12 29 249TR0038 120041222A5310 SHEAR TIE BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 SHEAR TIE AT STRINGER 22RT AT BS 1016 CORRODED. REPLACED SHEAR TIE PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000972004122900097NM 2004 12 29 249TR0095 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON TWO INTERCOSTALS AT BS 320 RBL 12 AND RBL 56. REPLACED INTERCOSTALS PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000982004122900098NM 2004 12 29 249TR0096 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 EDGE OF INTERCOSTAL BETWEEN BS 328 AND BS 340 AT LBL 12 DAMAGED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001012004122900101EA 2004 12 29 SWIA200414303 120041219A2720DL2428M9 ACTUATOR CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07710SK 10170 RUDDER LIMIT FAULT STATUS MESSAGE. REMOVED AND REPLACED RUDDER TRAVEL LIMITER ACTUATOR IAW CRJ700 MM 27-25-03. OPERATIONAL CHECK GOOD. P/N DL2428M9, S/N OFF 0477. 2L72 4F RTA21EA 20041229001022004122900102SO 2004 12 29 SWIA200414304 120041217A2720 ACTUATOR EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07234SW 120308 DURING TAKEOFF ROLL, EXPERIENCED CONTINUOUS RAPID STIFFENING/RESISTANCE IN RUDDER PEDALS. REPLACED BLUE SYSTEM RUDDER ACTUATOR WITH A SERVICEABLE UNIT IAW EMB M/M 27-22-02. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041229001052004122900105NM 2004 12 29 249TR0090 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL AT BS 947+14 FROM RBL 8 TO RBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001082004122900108NM 2004 12 29 249TR0055 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL HAS CORROSION FROM BS 967 TO BS 986.5 AT RBL 18. REPLACED INTERCOSTAL PER SRM 53-10-2. 2L72 4F RTA16WE 20041229001092004122900109NM 2004 12 29 249TR0059 120041222A5320 THRESHOLD BOEING737 7372K5 138448XNM R-2 DOOR CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 R-2 DOOR THRESHOLD CLOSE OUT WEB HAS CORROSION AT FORWARD DRAIN FITTING HOLE. REPAIRED PER SRM 51-40-2. 2L72 4F RTA16WE 20041229001142004122900114NM 2004 12 29 249TR0056 120041222A5320 WEB BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 WEB AT BS 1016 AT RBL 3 IS CORRODED AND MISDRILLED. REPLACED WEB PER SRM 51-10-1 AND BOEING DRAWING 65C10592. 2L72 4F RTA16WE 20041229001162004122900116NM 2004 12 29 249TR0062 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL CORRODED BETWEEN BS 947.5 AND BS 927 AT LBL 8. REPLACED INTERCOSTAL PER SRM 53-10-2 AND SRM 51-30-0. 2L72 4F RTA16WE 20041229001192004122900119NM 2004 12 29 249TR0099 120041222A5313 STRINGER BOEING737 7372K5 138448XNM FUSELAGE MISREPAIRED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 STRINGER REPAIRS NOT PER THE SRM AT STR 15LT. REPAIRED PER SRM 53-10-3. 2L72 4F RTA16WE 20041229001202004122900120NM 2004 12 29 QXEA200400904 120041222A323185424002003 DOOR BOMBDRDHC8 DHC8401 1390041NM MLG OUT OF RIG A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09408QX8055 4050 BIL - FLIGHT 2416 - WHILE EN ROUTE AT FL250, THE GEAR DOORS CYCLED OPEN AND CLOSED. THE GEAR DOOR LIGHT, THE RED UNLOCK LIGHT AND THE LIGHT IN THE GEAR HANDLE WAS ILLUMINATED. MAINTENANCE INTERROGATED PSEU HISTORY. NO FAULTS WERE FOUND. THE GEAR WAS RETRACTED AND IT WAS NOTED THAT THE LEFT MAIN LANDING GEAR DOOR WAS NOT FAIRED. ADJUSTMENTS TO THE DOOR WERE MADE AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229001212004122900121SO 2004 12 29 SWIA200414290 120041219A26126468 CONTROL MODULE EMB 120 EMB120ER 3260203SO FIRE DETECTION MALFUNCTIONED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM07220SW1063310633 120288 LEFT FIRE PIPE ZONE LIGHT FLICKERED AFTER GEAR EXTENSION. REPLACED LEFT WHEEL WELL ENGINE DETECTION CONTROL MODULE. OPERATIONAL CHECKS GOOD. 2L72 4T RTA31SO 20041229001232004122900123SO 2004 12 29 SWIA200414292 120041220A5210 ROLLER EMB 120 EMB120ER 3260203SO PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07250YV 120250 MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. REPLACED FORWARD AND AFT TRANSLATION BELL CRANK ROLLERS AND TORQUED AFT TRANSLATION CAM MOUNT BASE BOLT. LUBED CAM'S AND ROLLERS. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041229001262004122900126WP 2004 12 29 0402209926 120041109A5312 DOUBLER DOUG DC9 DC932 3022066WP BULKHEAD CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING M-CHECK FOUND CORROSION ON CANTED BULKHEAD DOUBLER AT BS 1211 STR 16L. REPAIRED PER EA 99-200911. 2L72 4F A6WE 20041229001292004122900129NM 2004 12 29 249TR0061 120041222A3610 DUCT BOEING737 7372K5 138448XNM BLEED AIR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BLEED AIR DUCT HOUSING CRACKED ON LEFT ENGINE PYLON. WELDED CRACK PER BOEING REPAIR SPEC BAC 5975. 2L72 4F RTA16WE 20041229001312004122900131NM 2004 12 29 249TR0070 120041222A5320 ANGLE BOEING737 7372K5 138448XNM LAV BULKHEAD CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON OUTBOARD ANGLE FOR FORWARD LAV AFT BULKHEAD WALL. REPLACED WALL SUPPORT ANGLE PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001332004122900133 2004 12 29 SWAA043711 420041223A2565D31354 SLIDE BOEING737 7375H4 138449DNM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29504SW 24181 L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041229001352004122900135EU 2004 12 29 MALA040879 120041124A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BL 0 CORRODED FROM FS 294-363. DAMAGED TRACK WAS REMOVED AND REPLACED IAW MESABA EO S53060. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229001372004122900137EU 2004 12 29 MALA040881 120041118A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15370PX 340B300 BATTERY PACK P/N 61-0478-9, S/N 70 WILL NOT LIGHT REQUIRED EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY CELL PACK P/N 55-2198-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/26/04. 2L72 4T RTA52EU 20041229001402004122900140 2004 12 29 SWAA043713 420041224A256565C16820 HOOK BOEING737 7377H4 1384404NM L1 DOOR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29790SW 30604 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR AFT STOW CLIP HOOK LOOSE. INSTALLED CLIP HOOK FASTENER PER MM. 2L72 4F RTA16WE 20041229001412004122900141NM 2004 12 29 SWAA043714 120041225A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29305SW 22945 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 454, STR 16L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20041229001422004122900142NM 2004 12 29 SWAA043705 120041222A53126545819 PRESSURE PANEL BOEING737 7375H4 138449DNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29503SW 24180 DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CRACKS AT NLG W/W CEILING WEB, BS 259.5, LT & RT SIDES OF ACCESS PANEL. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041229001502004122900150NM 2004 12 29 UPS04M43587 120041206A5753 SKIN DOUG MD11 MD11F 3023600NM LT OB FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01270UP LEFT OUTBOARD FLAP DELAMINATED. 2L73 4F RTA22WE 20041229001582004122900158WP 2004 12 29 2004000015 120041124A5410NSL6316519 COWLING DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 ENGINE DEPARTED A CNMAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SW0759083 47926 455127 AT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF. 2L73 4F4 F A22WE E23EA 20041229001602004122900160NM 2004 12 29 QXEA200400846 120041208A5100 UNKNOWN DHAV DHC8 DHC8202 2809007NM UNKNOWN UNKNOWN A QXEAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM09355PH 500 THE TAKEOFF WAS ABORTED WHEN AFTER REACHING 102KTS, THE AIRCRAFT DID NOT ROTATE WHEN THE CONTROL YOKE WAS PULLED BACK. THE AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE BEGAN WORKING ON THE AIRCRAFT TO DETERMINE THE CAUSE. THE AIRCRAFT IS DOWN FOR MAINTENANCE AND THIS SDR WILL REMAIN IN AN OPEN STATUS PENDING FURTHER INFORMATION. CAUSE WAS DETERMINED TO BE AN EXCESSIVE AMOUNT OF TYPE 4 DE-ICE FLUID ON THE FLIGHT CONTROLS. 2H72 4T RTA13NM 20041229001642004122900164NE 2004 12 29 DHL2004803001 220041119A7200CFM562C1QEC ENGINE DOUG DC8 DC873 302199CWP GE CFM56 CFM562C1 13802NE NR 4 MALFUNCTIONED A DHLAEBA ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01803DH 46123 SHUTDOWN NR 4 ENG DUE TO LOSS OF OIL QUANTITY NOTE PSI WAS 28 OIL QUANTITY WAS .5 QUART ENG OIL TEMP WAS 85 ENG WINDMILLED FOR APPROX 25 MINS COMPLETED ABNORMAL PROCEDURES NOTE AFTER ENG WAS SHUT DOWN OIL QUANTITY. REMOVED AND REPLACED NR 4 ENG PER DC-8 TASK MANUAL 71. OPS CHECK AND LEAK CHECK GOOD IAW CFM 71-00-00, JRH CHAPTER 13.1- 13.5. 2L74 4F4 FRT4A25 E2GL 20041229001672004122900167NM 2004 12 29 QXEA200400881 120041216A33506038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09345PH1582411487 476 PSC - FLOOR TRACK RED LIGHTS DS3 AND DS4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED PS6 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229001702004122900170 2004 12 29 BB04092 420041207A23304953200002 VIDEO UNIT BOEING757 7572B7 1384964NM CABIN BURNED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19626AU 27303 FLIGHT CREW REPORTED THAT THE VIDEO SYSTEM HAD A BURNING ODOR. MAINTENANCE REPLACED THE VIDEO PLAYER. 2L72 4F RTA2NM 20041229001712004122900171SO 2004 12 29 SWIA200414267 120041213A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07293SW1075510755 120320 ON THE GROUND, RECEIVED FLAP LIGHT ON THE MAP WITH THE INBOARD FLAPS. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD IAW 27-50-02, P/N 343000-1005 S/N ON 0349 S/N OFF 0523. 2L72 4T RTA31SO 20041229001722004122900172NM 2004 12 29 DHL2004782013 120041207A3350MIOSCO62 BATTERY BOEING727 727227 1384078NM EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 BOTH EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES IAW MM 33-50-71, OPS CK NORMAL P/N MIOSC062 (4 EA). 2L73 4F A3WE 20041229001742004122900174NM 2004 12 29 04FDEA03170 120041119A5230B275307019 HINGE BOEING727 72722 1384002NM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25186FE 18872 DOOR MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19. ENT BY: 497207 RPT BY: 497207 FACT 20 NOV 04 00:49 BFM U COMPLIED WITH EA NR 7-5210-82074 DOOR, MAIN CARGO DOOR UPPER HINGE LOBE GOUGE REPAIR P/N B27-53-070-19 ENT BY: 497212 RPT BY: 497212. 2L73 4F A3WE 20041229001772004122900177EU 2004 12 29 04FDEA03172 120041120A5730 SKIN AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 RIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650 HB HAS 6 EA ELONGATED SCREW HOLES AS MARKED AREA RIB 21 AND 22. COMPLIED WITH FEDEX ENGINEERING AUTHORIZATION 6-5710-83632. 2L72 4F RTA35EU 20041229001852004122900185EU 2004 12 29 MALA040822 120041116A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, RT FRAME AT STA 686.388 HAS CHAFING. MAINTENANCE REPAIRED IAW MESABA EO NR S53260. REFER TO NRC NR 127285 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20041227000562004122700056NM 2004 12 27 2004UALA01174 120041202A5230135W13212 TORQUE TUBE BOEING777 777222 1385219NM PWA PW4077PW4077 NE CARGO DOOR SHEARED A UALAK NONE O OTHER ININSP/MAINT 1 WP29778UA34441 26940 FORWARD CARGO DOOR, AFT TORQUE TUBE CRACKED. SUPPLEMENTAL DATA UPDATE THE FAILURE IS PROBABLY DUE TO FATIGUE LOADING IN THE TORQUE TUBE SKIN. AFTER REPEATED OPENING AND CLOSING, A CRACK APPEARED IN THE SKIN AT THE END ATTACHING FASTENER. REPLACED THE TORQUE TUBE. 2L72 4F4 FRTT0001SE E46NE 20041228000212004122800021EA 2004 12 28 04356647 120041221A3320 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN LIGHT WRONG PART A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27647BR 7399 SMOKE TOILET WARNING AFTER TAKEOFF. MX REMOVED AND REPLACED LAV RETURN TO SEAT LT BULBS DUE TO WRONG LIGHT BULBS FOUND. 2L72 4F RTA21EA 20041228000232004122800023NM 2004 12 28 SCNA04019 120041219A3350 COVER BOEING737 737800* NM EMERGENCY LIGHT BROKEN A SCNAK NONE O OTHER ININSP/MAINT 1 GL15PHHZJ 30389 MAINTENANCE DISCOVERED FWD EMERGENCY LIGHT COVER AT BULKHEAD POSITION BROKEN. PLACED ITEM ON MEL 33-19-1. ON 12/22, INSTALLED NEW TRACK COVER. 2L72 4F RTA16WE 20041228000282004122800028EU 2004 12 28 MALA040854 120041212A3020 DUCT SAAB SF340 340B 7860101EU RT INTAKE DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15411XJ 340B411 RIGHT INTAKE HEAT OVERTEMPING EVERY 25 SECONDS. AIR RETURN TO MSP. MAINTENANCE REPAIRED SURFACE DAMAGE TO LOWER DUCT IAW ACT CMM 30-21-00, OPS CHECK GOOD. 2L72 4T RTA52EU 20041228000302004122800030EU 2004 12 28 MALA040853 120041211A3020 MODULE SAAB SF340 340B 7860101EU ANTI ICE SYSTEM MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15453XJ 340B453 RIGHT INTAKE LIGHT ILLUMINATED IN FLIGHT. FAILED QRH AND LIGHT RE-ILLUMINATED. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED RIGHT DEICE MODULE, RAN HALF HOUR, OPS CHECK IAW SAAB MM30. 2L72 4T RTA52EU 20041228000322004122800032NM 2004 12 28 P5CA0401289 120041220A3260160805 PROXIMITY SWITCH BOEING747 747283B 1384867NM NLG DAMAGED A P5CAO OTHER J WARNING INDICATION ININSP/MAINT 1 EA15921FT 21575 NOSE LANDING GEAR ALT SQUAT SWITCH FOUND DAMAGED. REPLACED NLG ALT SQUAT SWITCH PER MM 32-60-00. 2L74 4F A20WE 20041228000372004122800037NM 2004 12 28 SWAA043681 120041220A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STRINGER 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20041228000392004122800039NM 2004 12 28 SWAA043682 120041220A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 907, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION SRM. 2L72 4F RTA16WE 20041228000512004122800051NM 2004 12 28 MWEA040223 120041219A2730 CONTROL CABLE BOEING717 717200 1383700NM ELEVATOR BINDING A MWEAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31920ME 55182 FOUND ELEVATOR BINDING DURING FLIGHT CONTROL CHECK. PERFORMED ADJUSTMENT TEST ELEVATOR CONTROL SYSTEM IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL 27-30-0. 2L72 4F TRA6WE 20041228000532004122800053NM 2004 12 28 C1HA200493002 120041121A5315 FLOORBEAM BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 CORROSION ON MAIN CABIN FLOORBEAM T-CAP AT STA 1030, LBL 12 TO RBL 12. SRM REPAIR MAJOR. 2L73 4F A3WE 20041228000642004122800064WP 2004 12 28 DHL2004807014 120041219A324426014112 TIRE DOUG DC8 DC873F 302199FWP MLG DAMAGED A DHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO01807DH 45990 DURING TAKEOFF ROLL BRAKES SEEMED TO BE LOCKING UP, REJECTED TAKEOFF AT SPEED AT 40 KTS. NR 5 MAIN TIRE FLAT SPOTTED. INSPECTED ALL EIGHT MAIN ASSY'S, CYCLED BRAKES SEVERAL TIMES, NO DRAGGING BRAKE'S NOTED PER DC-8 MM 32-42-1. REMOVED AND REPLACED NR 5 MAIN WHEEL AND TIRE ASSY PER M/M 32-40-0. 2L74 4F RT4A25 20041228000662004122800066SO 2004 12 28 C2XA04TY182 120041222A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2716541157 145542 IN SDF, FLIGHT 2068, THE PILOT WROTE UP THAT THE EMERGENCY LIGHTS ARE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 LIGHT STRIP IAW EMB 145 AMM-33-50-12 AND THE NR 3 EMERGENCY BATTERY IAW EMB-145 AMM-43-50-04, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20041228000682004122800068NM 2004 12 28 C1HA200493006 120041119A5347 SEAT TRACK BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 SEAT TRACK RBL 55 STA 344-380 IS CORRODED SEVERAL AREAS. REPLACED SEAT TRACK. 2L73 4F A3WE 20041228000812004122800081EA 2004 12 28 QXEA200400889 120041213A5510 FITTING CNDAIRCL600 CL6002C10 1390015EA ZONE 300 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - HORIZONTAL STAB LEFT HINGE BUSHING CHAFED INTO ANTI ROTATION LUG ON STABILIZER FITTING. REPAIRED IAW HORIZON AIR EA R-55-27 AND REO 670-55-11-013. 2L72 4F RTA21EA 20041228000832004122800083NM 2004 12 28 DHL2004747011 120041218A5270 SWITCH BOEING727 727224 1384076NM MLG DOOR DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01747DH 22253 LEFT MAIN GEAR DOOR LIGHT ILLUM DURING TAKEOFF ROLL EXTINGUISHED DURING CLIMBOUT (RED LIGHT ON F/O PANEL). FOUND LEFT MAIN GEAR DOOR SWITCH CONTAMINATED. CLEANED SWITCH, CYCLED SEVERAL TIMES, FOUND TO BE MOVING FREELY. OPS CHECKS GOOD ON GROUND IAW MM 32-62-00. NO FURTHER DEFECTS NOTED. 2L73 4F A3WE 20041228000852004122800085NM 2004 12 28 AALA20041227 120041216A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21752AN 30260 EMERGENCY LIGHTS AT FIRST SECTION OF TOURIST CLASS INOPERATIVE. REPLACED BATTERY PACK AT 3R FOR EMERGENCY LIGHTS AT FIRST SECTION OF TOURIST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20041228000892004122800089WP 2004 12 28 DHL2004801015 120041220A3260 UPLOCK SWITCH DOUG DC8 DC873F 302199FWP MLG DOOR DIRTY A DHLAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO01801DH 46033 AFTER T/O WITH GEAR HANDLE DOORS NOT LATCHED AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY. UP LATCH CHECK OK AND LIGHTS REMAINED OUT. CLEANED AND RESEATED RIGHT GEAR DOOR UP LIMIT SWITCH, PERFORMED SYS ADJ/TEST PER MM 32-60-00, SYS OK FOR SERVICE. 2L74 4F RT4A25 20041228000912004122800091NM 2004 12 28 DHL2004748008 120041217A3350 SOCKET BOEING727 727225 1384077NM EMERGENCY LIGHT DIRTY A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR DID NOT ILLUMINATE DURING EMERGENCY POWER TEST. CLEANED CONTACT ON LIGHT & SOCKET OPS CHECKS NORMAL IAW 33-50-10. 2L73 4F A3WE 20041228000932004122800093NM 2004 12 28 P5CA0401290 120041220A3244260356112 TIRE BOEING747 747123 1384873NM NR 4 LEAKING A P5CAK NONE O OTHER ININSP/MAINT 1 EA15858FT 20109 NR 4 TIRE FOUND WITH SCREW IMBEDDED AND LEAKING AIR. REPLACED WHEEL ASSY PER MM 32-45-01. SPIN & LEAK CHECK OK. 2L74 4F A20WE 20041228000952004122800095NM 2004 12 28 C1HA200493016 120041123A5313 STRINGER SPLICE BOEING727 727212 138407GNM FUSELAGE CORRODED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 FWD PIT FWD SIDE OF STA 480 FRAME STRINGER 27L STRINGER SPLICE IS EXFOLIATED 100 PERCENT THROUGH TO THE SKIN. INSTALLED STRINGER SPLICE, MINOR. 2L73 4F A3WE 20041228000972004122800097NM 2004 12 28 AWXA200401423 120041204A534069389396 STRINGER CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 DURING C-18 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AFT OF THE R-1 DOOR ENTRANCE AT BS 344, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 344, STR 10 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-38939; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8, 12 & 14. 2L72 4F RTA16WE 20041228000992004122800099NM 2004 12 28 SWAA043685 120041220A53306545765 SKIN BOEING737 737317 138447PNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29693SW 23174 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20041228001272004122800127EU 2004 12 28 MALA040837 120041123A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, FWD CABIN FLOORBEAM AT FRAME 18 AND SEAT TRACK 4 (RT O/B) UPPER FLANGE EDGE AND GUSSET PLATE CORRODED. MAINTENANCE REPAIRED IAW EO A53224. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001292004122800129EU 2004 12 28 MALA040842 120041123A5280 DOOR BAC 146 AVRO146RJ85A1500097EU MLG CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN AFT CUTOUT INBOARD AFT RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001312004122800131EU 2004 12 28 MALA040844 120041123A5280 DOOR BAC 146 AVRO146RJ85A1500097EU MLG CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT MLG DOOR INNER SKIN FWD CUTOUT I/B AFT RADIUS IS CRACKED. MAINTENANCE REPAIRED IAW EO A52033. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20041228001322004122800132EA 2004 12 28 COMA0460697 120041219A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NR 2 FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01966CA4210 7132 FLIGHT 5316 FLAPS FAIL CAUTION. REPLACED THE LEFT NR 2 FLAP ACTUATOR. 2L72 4F RTA21EA 20041228001342004122800134WP 2004 12 28 WX0400066 120041220A2131 CONTROLLER DOUG DC9 DC983 3022083WP CABIN PRESSURE MALFUNCTIONED A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19891GA 49423 MSN TO LAS - DURING CLIMBOUT AT 9000 FT CREW REPORTED FLOW LIGHT ILLUMINATED. CABIN CLIMBED 500 FT PER MINUTE WHILE LEVEL. COULD NOT MAINTAIN CABIN IN AUTO. CREW COMPLETED FLOW LIGHT ILLUMINATED CHECKLIST. AIRCRAFT RETURNED TO MSN AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED AUTOMATIC PRESSURE CONTROL IAW MEL 21-24. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041228001382004122800138SO 2004 12 28 C2XA04SH551 120041109A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715912 145439 DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 20. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20041228001402004122800140SO 2004 12 28 C2XA04IA167 120041211A32347455503 CONTROL LEVER EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2716987 145261 DURING CLIMB THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CHECK GOOD. 2L72 4T RTT00011AT 20041228001422004122800142NM 2004 12 28 SWAA043675 120041219A52406969854 FRAME BOEING737 7373H4 1384600NM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME AT LOWER CORNER CRACKED. REPAIRED DOOR FRAME PER BAC DRAWING. 2L72 4F RTA16WE 20041228001472004122800147EU 2004 12 28 AWXA200401416 120041114A5230D534755212000 SEAL AIRBUS320 A320232 3930326EU CARGO DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT ON UPPER INBOARD SURFACE FR 53. MAINTENANCE REMOVED CORRODED LOWER FORWARD CORNER SEALING ASSEMBLY AT FR 53; FABRICATED A NEW REPLACEMENT CORNER SEALING ASSEMBLY; INSTALLED REPAIR PART IAW A320 SRM 53-41-49. 2L72 4F RTA28NM 20041228001492004122800149EA 2004 12 28 SWIA200414280 120041215A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07957SW 7829 CEILING EMERGENCY FLOODLIGHT AT ROW 10 IS INOPERATIVE. RELAMPED EMERGENCY FLOODLIGHT AT ROW 10 . OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041228001512004122800151NM 2004 12 28 04FDEA03446 120041217A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA Y = 840 TO 899 LT NR 2 SEAT TRACK & FLANGE AREAS FOUND WITH CORROSION. REPAIRED IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20041228001652004122800165EA 2004 12 28 COMA0470083 120041215A3010GG670800031 SHUTOFF VALVE CNDAIRCL600 CL6002C10 1390015EA RT WING ANTI ICEMALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01668CA848 10162 FLIGHT 4975 RIGHT ENGINE BLEED CAUTION MESSAGE. REPLACED THE RIGHT WING ANTI-ICE SOV. 2L72 4F RTA21EA 20041228001682004122800168NM 2004 12 28 2004UALA01224 120041216A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE BULGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT LAV SERVICE AREA STA 1700 HAS BULGING SKIN. CORROSION DAMAGE AT THE AFT LAV SERVICE DOOR DUE TO FLUID LEAKAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041228001852004122800185NM 2004 12 28 2004UALA01219 120041215A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT PIT FRAME DENTED STA 1420 BY STR 26L. REPAIRED FRAME WITH NESTED "J" ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041228001882004122800188NM 2004 12 28 SWAA043698 120041220A2121215201 FAN BOEING737 7373H4 1384600NM E&E BAY FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29373SW 26581 DECLARED EMERGENCY, 25 MINUTES OUT OF AUS, F/A'S NOTICED AND SMELLED SMOKE IN CABIN. COULD NOT DETERMINE IF SMOKE WAS ELECTRICAL OR FROM PACKS. REMOVED AND REPLACED GASPER FAN PER MM. 2L72 4F RTA16WE 20041228001892004122800189NM 2004 12 28 SWAA043652 120041216A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 616, STRINGER 17R, CRACKED. REPAIRED FRAME SECTION PER EA. 2L72 4F RTA16WE 20041229000122004122900012EU 2004 12 29 MALA040887 120041111A33505521981 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15367PX 340B271 DURING CAPACITY CHECK, BATTERY PACK P/N 61-0478-9, S/N ELB502 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 55-2198-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/13/04. 2L72 4T RTA52EU 20041229000252004122900025 2004 12 29 237TR0008 420041204A2210 SWITCH BOEING737 737228 13844AGNM THROTTLE MALFUNCTIONED A PIDAK NONE O OTHER NRNOT REPORTED 1 SO05237TR 23007 FLIGHT DIRECTOR BAR GOES AWAY WHEN TOGA IS PRESSED. PLACED ON MEL 22-17. 12/08/2004: REPLACED SWITCH IN RIGHT HAND THROTTLE. FLIGHT DIRECTOR OPS CHECKS GOOD PER MM 22-11-01. 2L72 4F RTA16WE 20041229000282004122900028NM 2004 12 29 249TR0075 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON INTERCOSTAL AT LAV DOOR FORWARD OF BS 294 FLOORBEAM. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000372004122900037EA 2004 12 29 QXEA200400907 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - LEFT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 728.00. REPAIRED IAW CRJ SRM 51-21-16 AND HORIZON AIR EA R-53-240. 2L72 4F RTA21EA 20041229000392004122900039SO 2004 12 29 C2XA04CL125 120041208A3397 WIRE EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715941 145035 CLE FLIGHT 2481 THE CREW REPORTED THE EMERGENCY LIGHTS AT THE CENTER OF THE AIRCRAFT WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRES IN THE CEILING AT ROW 12. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20041229000532004122900053EU 2004 12 29 MALA040869 120041119A3350 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 DURING TASKJ CARD 335993 FUNCTIONAL TEST OF EMERGENCY BATTERY CAPACITY CHECK, BATTERY 20LN FAILED. 2L72 4T RTA52EU 20041229000552004122900055NM 2004 12 29 249TR0045 120041222A5320 ANGLE BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON R-1 DOOR Z-ANGLE FORWARD OF THE DOOR. REPLACED Z-ANGLE PER SRM 51-30-2 AND SRM 51-10-1. 2L72 4F RTA16WE 20041229000572004122900057SO 2004 12 29 SWIA200414295 120041216A2750 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07189SW 120048 AFTER LANDING WHEN FLAPS SELECTED UP, FLAP CONTROL FAULT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06 AND CLEANED CANNON PLUGS OF GLYCOL. OPERATIONAL CHECK GOOD. P/N OFF 300500-1007, S/N OFF 0009. 2L72 4T RTA31SO 20041229000582004122900058EA 2004 12 29 SWIA200414296 120041211A2751 INDICATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CLCLIMB 1 NM07710BR 7852 WHILE CLIMBING THROUGH FL260 THE GEAR AND FLAP DISPLAYS APPEARED ON ED-1. FLAPS DEGRADED STATUS MESSAGE. REPLACED LEFT FLAP POSITION INDICATOR. OPERATIONAL CHECK GOOD IAW 27-55-01. 2L72 4F RTA21EA 20041229000632004122900063WP 2004 12 29 AALA20041243 120041223A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21441AA 49460 DFW - EMERGENCY EXIT LIGHTS AT FORWARD ENTRY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY CEILING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041229000662004122900066NM 2004 12 29 249TR0091 120041222A5347 SEAT TRACK BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 SEAT TRACK AT RBL 38 HAS CORROSION AT BS 986 + 4. REPLACED SECTION OF TRACK PER SRM 51-10-1 AND 53-10-2. 2L72 4F RTA16WE 20041229000672004122900067NM 2004 12 29 249TR0094 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON INTERCOSTAL BETWEEN BS 312 AND BS 328 AT RBL 12. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000692004122900069NM 2004 12 29 249TR0083 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 DIAGONAL INTERCOSTAL FROM BS 986 TO BS 1006 AT AFT LAV THRESHOLD HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0. 2L72 4F RTA16WE 20041229000732004122900073EA 2004 12 29 QXEA200400911 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 583.00, FS 665.00 AND FS 677.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND SRM 51-21-16. 2L72 4F RTA21EA 20041229000832004122900083EU 2004 12 29 MALA040873 120041122A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, UPPER FUSELAGE IS DENTED FWD OF STA 487.0 AT 11:00 POSITION AND WAS REPAIRED IAW MESABA EO S53035. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229000862004122900086SO 2004 12 29 CHQA000597 120041228A3350RPS1B BATTERY PACK EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT FALSE ACTIVATIONA CHQAK NONE L NO TEST ININSP/MAINT 1 GL11834 145696 FOUND EMERGENCY LIGHT SWITCHES IN THE ARM POSITION AND EMERGENCY LIGHTS CYCLING ON AND OFF. FERRIED AIRCRAFT FROM GSP TO MCO. REMOVED AND REPLACED ALL FOUR EMERGENCY BATTERY POWER SUPPLIES IAW EMB 135 AMM 33-50-04. OPS CHECK GOOD. EMERGENCY LIGHT STRIP ON FLOOR BESIDE EMERGENCY EXIT ROW WILL NOT ILLUMINATE. REMOVED AND REPLACED FLOOR STRIP BESIDE EMERGENCY EXIT ROW IAW EMB 135 AMM 30-50-08. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041229000902004122900090SO 2004 12 29 CHQA000596 120041227A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11833 145687 RIGHT REAR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT REAR EMERGENCY EXIT LIGHT IAW EMB 135 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041229001002004122900100SO 2004 12 29 SWIA200414302 120041218A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07288SW 120316 EMERGENCY EXIT SIGN IN SEAT 6A BROKEN. REPAIRED EMERGENCY EXIT SIGN AT 6A. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041229001032004122900103SO 2004 12 29 SWIA200414305 120041221A27523082001005 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07190SW 120050 RECEIVED CONTROL FAULT ON APPROACH WHEN SELECTING FLAPS 25 DEGREES. REMOVED AND REPLACED RIGHT INBOARD, RIGHT NACELLE, AND RIGHT OUTBOARD FLAP ACTUATORS IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1005, S/N 0091 AND S/N 0834, P/N 320300-1007, S/N 0036. 2L72 4T RTA31SO 20041229001042004122900104NM 2004 12 29 249TR0080 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 1006 TO BS 1016 AT RBL 3 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001062004122900106NM 2004 12 29 249TR0079 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT LBL 8 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592. 2L72 4F RTA16WE 20041229001132004122900113NM 2004 12 29 249TR0052 120041222A5313 STRINGER BOEING737 7372K5 138448XNM FUSELAGE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 STRINGER CRACKED AT BS 1032 STR 14LT. REPAIRED PER SRM 53-10-3. 2L72 4F RTA16WE 20041229001172004122900117NM 2004 12 29 249TR0084 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL AT BS 947+9 FROM LBL 17 TO LBL 41 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592. 2L72 4F RTA16WE 20041229001182004122900118NM 2004 12 29 249TR0085 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 947 TO BS 967 AT LBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001342004122900134NM 2004 12 29 QXEA200400919 120041224A27207G7921 SWITCH DHAV DHC8 DHC8202 2809007NM RUDDER FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM09355PH16578 500 THE FLIGHT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDDER PRESS CATUION LIGHT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE NR 1 PRESSURE REGULATOR SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229001442004122900144NM 2004 12 29 SWAA043707 120041222A5315BAC1505 FLOORBEAM BOEING737 7373K2 13844BANM AFT CARGO CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT FLOORBEAM CORRODED AT BS 767, LBL 3. REPAIRED BEAM PER SRM & SWA EA. 2L72 4F RTA16WE 20041229001592004122900159EU 2004 12 29 MALA040827 120041116A5313 RIB SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 611BR 4 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 127444 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20041229001622004122900162NM 2004 12 29 SCNA04018 120041124A3350 BATTERY PACK BOEING737 7378Q8 13844BXNM EMERGENCY LIGHT INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15806SY 28215 CREW REPORTED R2 INTERIOR AND EXTERIOR EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. 2L72 4F RTA16WE 20041229001732004122900173 2004 12 29 2004UALA01181 420041202A2565 BULB AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE BURNED OUT A UALAK NONE O OTHER ININSP/MAINT 1 WP29433UA 589 6 BULBS BURNED OUT. MOORING LINE NOT IN POCKET, PLACED IN BETWEEN GIRT HALVES. HOSE WAS TAPED OVER SWIVEL 6 INCES FROM MAT DOWN HOSE. INFLATION CABLE NOT RUN IN CABLE GUIDE AND RAN THROUGH LACING GROMMET, THEREFORE SLIDE WOULD NOT HAVE FIRED, WAS 10 INCHES OR LARGER-RECOMMENDED 4 INCH WALL. SLIDE FOLDED NOT ROLLED AND PACKED OVER BOTTLE AND ASPIRATOR. 2L72 4F4 FRTA28NM E40NE 20041229001832004122900183NM 2004 12 29 QXEA200400842 120041201A2612473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM CARGO BAY MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09355PH16445 500 THE CREW REPORTED THE SMOKE WARNING LIGHT CAME ON INTERMITTENTLY DURING CLIMB AND STAYED ON FOR APPROXIMATELY 5 MINUTES DURING CRUISE. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETECTORS, AND NOTED NO DEFECTS. THE DETECTORS WERE CLEANED AS A PRECAUTIONARY MEASURE AND OPERATIONAL CHECKS WERE PERFORMED. THE CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229001872004122900187EU 2004 12 29 MALA040823 120041116A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, BLO SEAT TRACK CORRODED FROM STA 297 TO 330. MAINTENANCE REPAIRED IAW MESABA EO NR S53060. REFER TO NRC NR 1272865 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20041229001922004122900192EU 2004 12 29 MALA040740 120041124A3020NH24668169 DUCT SAAB SF340 340B 7860101EU INTAKE HEAT CRACKED A MALAK NONE J WARNING INDICATION CRCRUISE 1 GL15449XJ 340B449 DURING FLIGHT INTAKE HEAT LIGHT ILLUMINATED INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED FWD INLET IAW 71-60-05-4 PN NH24668-169 SN/OFF L198028, SN/ON L291011. RAN A/C FOR 20 MINUTES. REINSTALLED SHOEBOXES BACK TO ORIGINAL POSITIONS, OPS CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20041229001932004122900193EU 2004 12 29 MALA040741 120041124A30202351A000003 VALVE BAC 146 AVRO146RJ85A1500097EU NR 3 ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15524XJ E2349 NR 3 ENGINE INTAKE LOW PSI LIGHT ILLUMINATED IN LIGHT GRADUALLY WAS ABLE TO GET IT EXTINGUISHED 80-89 PERCENT. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 ENGINE INTAKE ANTI-ICE VALVE. PN OFF/2351A000, SN/OFF 899351-2, PN/ON 2351A000-003, SN/ON 899352-8. REF AMM 30-21-17. OPS AND LEAK CHECK GOOD. 2H74 4F RTA49EU 20041229001942004122900194 2004 12 29 MALA040744 420041130A34406227337001 TRANSCEIVER SAAB SF340 340B 7860101EU WX RADAR SYS FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15360PX 340B220 WEATHER RADAR FAILED INFLIGHT. AIR RETURN TO MEM. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WEATHER RADAR R/T. PERFORMED AMM CHECK PER34-47-00-5. OPS CHECK GOOD. STABILIZATION IS GOOD. OK FOR SERVICE PN ON/OFF622-7337-001, SN ON 4501, SN OFF 1596. 2L72 4T RTA52EU 20041229001972004122900197EU 2004 12 29 MALA040727 120041110A27508519M3 CONTROLLER SAAB SF340 340B 7860101EU TE FLAP MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15449XJ 340B449 FLAP FAULT CWP ILLUMINATES WHEN EXTENDING FLAPS UNTIL FLAPS REACH SELECTED POSITION. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED FLAP CONTROLLER PN 8519M3, SN/OFF 555, SN/ON 057, IAW SMM CHAP 27-51-1. 2L72 4T RTA52EU 20041229001982004122900198WP 2004 12 29 04FDEA03200 120041124A32444081580902 CONNECTOR DOUG MD10 MD1010F 3022112WP COCKPIT MISPINNED A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25390FE 46624 ON ARRIVAL AT KMEM SELECTED GEAR DOWN, GOT LEVEL 2 ANTI-SKID FAIL ALERT. MISSED APPROACH, RAN CHECKLIST, STILL GOT SAME ALERT. LANDED UNEVENTFULLY WITH ANTI-SKID FAIL LIGHT ILLUMINATED. SELECTED ANTI-SKID OFF CLEARING RUNWAY IAW CHECKLIST. T/S FOUND A "G" ON INSERT B PIN F8 ON ALL 3 VIA'S PER TSM THIS SHOULD BE A "O". INTERMITTENT "G" ON PIN 8G OF INSERT B. ONLY ON VIA-1. VIA'S 2&3 INDICATE NORMAL. THIS FAULT INDICATES A WIRE FROM TERM BLOCK S3-90 IS BAD OR A BAD VIA-1. R/R'D VIA 1 & VIA 2 IAW MD10-10 M/M. ALL CHECKS NORMAL IAW RTS. RETESTED ANTI SKID PER FIM. ALL TEST PASSED AS REQUIRED IN FIM. OK FOR SVC AT THIS TIME. 2L73 4F RTA22WE 20041229001992004122900199WP 2004 12 29 04FDEA03201 120041124A4930 FUEL FILTER DOUG DC10 DC1010 3022110WP APU FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25385FE 46619 "ENG 1 FUEL FILTER" LEVEL 1 ALERT ILLUMINATED APPROX 1 30 AFTER TAKEOFF. APPROX 40 MIN AFTER "1 ENG FUEL FILTER LIGHT CAME ON, THE LEVEL 2," FUEL CONTAMINATED" ALERT CAME ON , DIVERTED TO STL. REMOVED ALL THREE ENGINE FUEL FILTERS. FOUND ALL CONTAMINATED. REPLACED ALL 3 ENGINE FUEL FILTERS, MEC'S, ENGINE FUEL PUMPS, FUEL DIFFERENTIAL PRESSURE SWITCHES. REPLACED APU FUEL FILTER. DEFUELED AND ENTERED ALL 3 FUEL TANKS. CLEANED SAME. ALL COMPONENTS RIGGED, ADJUSTED AND LEAK CHECKED PER APPROPRIATE MAINTENANCE MANUAL. PERFORMED SATISFACTORY TEST FLIGHT DUE TO ALL THREE ENGINE WORK. RETURNED AIRCRAFT TO SERVICE. 2L73 4F A22WE 20041229002042004122900204SO 2004 12 29 SWIA200414216 120041101A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 FS 13 TO 21 RIGHT AT STR 15 FLOOR SUPPORT ANGLE IS CORRODED, (ITEM FOUND AT C-CHECK INSPECTION.) FLOOR SUPPORT ANGLE BLENDED AND ASSESSED TO BE WITHIN LIMITS IAW EMB 120 SRM 5320-10 MAX MAT'L LOSS .004. AREA REPROTECTED IAW MB 120 SRM 51-21-02 AND AMM 20-30-05. 2L72 4T RTA31SO 20041229002052004122900205NE 2004 12 29 NACA20040061 220040927A7322PR58E5 CARBURETOR DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE POWER LOSS A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL032907F2 2 533265 CP450668 NR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH, HIGH FUEL FLOW AND LOW BMEP CHT COLD. REMOVED AND REPLACED CARBURETOR. LEAK AND OP CHECK GOOD. 2L74 4R4 R A781 5E8 20041230000012004123000001 2004 12 30 LAB2004F00002 420040921A34258350006220 AHRS PIPER PA32 PA32300 7103212SO LYC O540 IO540K1G5 41532EA COCKPIT MALFUNCTIONED E LABAO OTHER O OTHER NRNOT REPORTED 1 AL0554KA 327840197 AHRS (ALTITUDE HEADING REF SYSTEM) INSTALLED IAW EFIS-SV SYSTEM UNDER STC NR SA02203AK FAILED TO REPORT HEADING INDICATION. 1L71 3O3 O A3SO 1E4 20041230000022004123000002NM 2004 12 30 L0FR200400006 120041118A324626070812 WHEEL BOEING747 747200 1384847NM MLG CRACKED B Q2SAK NONE O OTHER ININSP/MAINT 1 AL03 CRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA. 2L74 4F RTA20WE 20041230000062004123000006SO 2004 12 30 SWIA200414223 120041101A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 CRACK ON OMEGA BEAM LOCATED 3 INCHES AFT OF FRAME 30 CENTER BUTT STRAP. (ITEM FOUND AT C-CHECK INSPECTION.) CRACKED AREA, REPAIRED IAW EMB 120 SRM 51-70-05, FIG 1. 2L72 4T RTA31SO 20041230000072004123000007SO 2004 12 30 SWIA200414224 120041101A5712 RIB EMB 120 EMB120ER 3260203SO WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 RIB 19 LEFT SIDE MOST FORWARD LOWER CLEAT IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SHEAR CLIP IAW SRM 51-22-00, 51-25-00, 51-40-02, 51-30-01, 51-21-02, 57-20-07, 51-40-02 AND MM 20-30-05. 2L72 4T RTA31SO 20041230000082004123000008SO 2004 12 30 SWIA200414225 120041101A5712 RIB EMB 120 EMB120ER 3260203SO WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 RIB 19 LEFT SIDE MOST FWD UPPER CLEAT IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SHEAR CLIP IAW SRM 51-22-00, 51-25-00, 51-40-02, 51-30-01, 51-21-02, 57-20-07, 51-40-02 AND MM 20-30-05. 2L72 4T RTA31SO 20041230000092004123000009GL 2004 12 30 SAAIEN440786 220041201A723023073717 BLADE RROYCE EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL STAGE 1 HPC FRACTURED B C2XAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 SO03105751869 1869 A17436 145640 CAE310005 1ST STAGE HPC BLADE FOR NR 2 ENGINE FRACTURED DURING OPERATION, RESULTING IN UNCOMMANDED IN-FLIGHT SHUTDOWN. ONCE ENGINE DISASSEMBLED, BLADE REMNANT RETURNED TO ROLLS-ROYCE FOR ANALYSIS. 2L72 4F4 FRTT00011ATTE6CH 20041230000182004123000018NE 2004 12 30 NAFA20040005 320041117A6140B8A RELAY DOUG DC6 DC6A 3021706WP HAMSTD43E 43E60 NE PROP WARNING MALFUNCTIONED C N32BC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AL017780B8255 8255 45372 TAKEOFF WARNING HORN INTERMITTENT ON TAKEOFF. REPLACED NR 4 PROPELLER TAKEOFF WARNING RELAY. OP CHECKED GOOD. 2L74 4R 6A3 6 CP871 20041230000192004123000019WP 2004 12 30 04FDEA03256 120041129A5730ARC0263503 PANEL DOUG MD10 MD1010F 3022112WP ZONE 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT HAND WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF MAIN LANDING GEAR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED PANEL PART NUMBER ARC0263, BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, DOUBLER AND CORE IAW RPS 1001 REV E, DAC PRINT ARC0263 AND FEDEX EA 8-5710-81525, WINGS- LEFT HAND UPPER WING PANEL ASSEMBLY AILERON TO MAIN LANDING GEAR REPAIR. REMOVED AND REINSTALLED SEALS, RETAINERS AND PANEL IAW DC10 SRM 51-31-01 VOL 2. REFERENCE NON-ROUTINE N00895. 2L73 4F RTA22WE 20041230000212004123000021WP 2004 12 30 DHL2004801013 120041111A3260 UPLOCK SWITCH DOUG DC8 DC873F 302199FWP MLG DOOR DIRTY A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 AFTER TAKEOFF, RIGHT DOOR UNSAFE LIGHT ILLUMINATED PERFORMED ABNORMAL PROCEDURE LIGHT EXTINGUISHED BUT NOISE CAME FROM UNDERSIDE OF A/C. CLEANED UPLATCH SWITCHES AND ADJUSTED MAIN GEAR DOOR UPLATCH MECH IAW 32-31-3. PERFORMED MAIN GEAR DOOR UPLATCH TEST, OPS CHECK GOOD IAW MM 32-31-4. 2L74 4F RT4A25 20041230000242004123000024EA 2004 12 30 SWIA200414168 120041130A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07908SW 7540 CENTER CEILING EMERGENCY LIGHT OUT IN CABIN NEAR ROW 5. RELAMPED CENTER CEILING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041230000252004123000025SO 2004 12 30 SWIA200414169 120041202A3397 WIRE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07569SW OVERHEAD EMERGENCY LIGHT AT ROW 9 INOPERATIVE. REPAIRED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041230000262004123000026WP 2004 12 30 WX0400041 120041001A3397 CONNECTOR DOUG DC9 DC987 3022087WP EMERGENCY LIGHT LOOSE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19945MA 49725 MAINTENANCE REPORTED AFT STAIR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE SECURED CONNECTOR TO LIGHT ASSEMBLIES IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041230000272004123000027WP 2004 12 30 WX0400048 120041102A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCONNECTED A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 LAS-MAINTENANCE REPORTED EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE, DISCONNECTED AT ROWS 6 TO 9, ROWS 12 TO 16 AND ROW 19. MAINTENANCE RECONNECTED FLOOR TRACK LIGHTING AT ROW 6, ROW 13 AND ROW 19. EMERGENCY FLOOR TRACK LIGHTING SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041230000292004123000029WP 2004 12 30 WX0400057 120041130A335060030451 POWER SUPPLY DOUG DC9 DC987 3022087WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19945MA 49725 LAS-MAINTENANCE REPORTED SEVERAL CEILING EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 11 AND 17. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY AT STATION 693R. SYSTEM OPERATIONALLY CHECKED GOOD IAW 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041230000302004123000030EA 2004 12 30 SWIA200414195 120041118A5320 PLATE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 CARGO PIT; CARGO DOOR ENTRY LANDING PLATE HAS CORROSION AROUND A/NUT LOCATIONS, UPPER AND LOWER SURFACES AT FS 574.0 TO 621.0 LBL 42, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 53-61-23 & 53-00-00. 2L72 4F RTA21EA 20041230000342004123000034SO 2004 12 30 RAIR04412025 120041217A3260 CONNECTOR EMB 145 EMB145LR 3260212SO WOW DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03813HK 145044 5657- STL- LANDING GEAR AIR/GROUND FAILED EICAS MESSAGE. MAINTENANCE INSPECTED AND FOUND DAMAGED CONNECTOR ON NOSE LANDING GEAR ON WEIGHT ON WHEEL SWITCH. REMOVED AND REPLACED CONNECTOR. 2L72 4T RTT00011AT 20041230000382004123000038NM 2004 12 30 QXEA200400793 120041113A5420 INTERCOSTAL BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - LEFT HAND NACELLE OUTBOARD SIDE OF ZONE 413 INTERCOSTAL ATTACHING TO UPPER SKIN IS CRACKED AT STATION XN210.0. REPAIRED IAW RD 8/4-54-155 AND SRM 51-42-05-800-801 AND SRM 51-40-15, PAGE 210. 2H72 4T RTA13NM 20041230000402004123000040NE 2004 12 30 DHL2004782012 220041113A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D15 52051NE NR 3 LEAKING A DHLAC ABORTED TAKEOFF GKJMULTIPLE FAILURE FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO01782DH 21998 AT 10 KTS ON THE TAKEOFF ROLL RWY 35L WINDS CALM TEMP +1C A LOUD BOOM WAS HEARD THE AUTOPACK TRIP TRIPPED AND THE TAKEOFF REJECTED. THE A/C WAS TAXIED OFF THE RUNWAY AND THE NR 3 ENGINE OIL WAS DECREASING THE NR 3 ENGINE WAS SHUT DOWN RETURNED TO THE BLOCKS REJECTED TAKEOFF SPEED APPROXIMATELY 10 KTS. REMOVED AND REPLACED NR 3 ENGINE ASSY REF MTM 71.1. 2L73 4F4 F A3WE E2EA 20041230000412004123000041NM 2004 12 30 QXEA200400790 120041118A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND OUTBOARD FLAP HAS A SIX FOOT LONG BY 2 INCH WIDE CHAFING MARK ON THE UPPER SURFACE STARTING AT THE INBOARD EDGE WHERE THE FLAP SITS BETWEEN 0 AND 5 DEGREES. REPAIRED IAW RD 8/4-57-106, ISS 7. 2H72 4T RTA13NM 20041230000422004123000042NM 2004 12 30 QXEA200400792 120041117A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - LEFT HAND INBOARD FLAP HAS A DEEP WEAR MARK ON THE UPPER SURFACE WHERE THE UPPER SHROUD INBOARD RUB BUTTON SITS. REPAIRED IAW HORIZON AIR EA 6-57-253. 2H72 4T RTA13NM 20041230000432004123000043NM 2004 12 30 QXEA200400794 120041113A5414 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 400 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - LEFT HAND NACELLE OUTBOARD SIDE ZONE 413 THREE RIVETS PULLED THROUGH SIDE SKIN IMMEDIATELY AFT OF CRACKED INTERCOSTAL. REPAIRED IAW SRM 51-42-05-800-801. 2H72 4T RTA13NM 20041230000442004123000044CE 2004 12 30 66793 120041115A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07139ZV UE139 CREW REPORTED CAPT'S RIGHT BRAKE SPONGY ON LANDING. PRESSURE RT BLEED RT BRAKES. 2L72 4T RTA24CE 20041230000452004123000045EA 2004 12 30 SWIA200414187 120041118A5411 RIB CNDAIRCL600 CL6002B19 1900309EA LT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 LEFT PYLON AFT RIB IS CRACKED; FS 605.00, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED RIB IAW SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00. 2L72 4F RTA21EA 20041230000472004123000047EU 2004 12 30 04FDEA03375 120041206A5330 SKIN AIRBUS310 A310 EU FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK NR 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. FUSELAGE, WEAR AT EXTERIOR FUSELAGE SKIN SURFACE ON FWD SURROUNDED OF FWD CARGO DOOR BETWEEN STRG 36 RT AND 39 RT. REPAIRED IAW EA 6-5310-81816. 2L72 4F RTA35EU 20041230000502004123000050NM 2004 12 30 DHL2004782011 120041028A8011 PRESSURE SWITCH BOEING727 727227 1384078NM START VALVE MALFUNCTIONED A DHLAEB ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION DEDESCENT 1 SO01782DH 21998 NR 2 START VALVE ILLUMINATED IN FLIGHT SHUT DOWN NR 2 ENGINE AS PRECAUTION. TRANSFERED NR 2 START VALVE OPEN LIGHTS TO DMI NR 18276 PER MEL 80-1-1B PLACARD INSTALLED. REMOVED AND REPLACED START VALVE PRESSURE SWITCH PER 80-11-11. GROUND CHECKS GOOD CLEAR DMI18276 PLACARD REMOVED. 2L73 4F A3WE 20041230000522004123000052WP 2004 12 30 04FDEA03185 120041123A5100 UNKNOWN DOUG MD10 MD1010F 3022112WP UNKNOWN UNKNOWN A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25372FE 46610 ON DEPARTURE OUT OF ONT AT APPROX 1000 AGL GOT A TAIL WINDSHEAR ALERT. WENT TO FIREWALL. NO OVERSPEED. DUMPED FUEL. DIVERT TO LAX. NO ENGINE EXCEEDANCE'S REPORT ON ACARS NOR AIU'S PERFORMED POSSIBLE TAIL STRIKE INSPECTION AND FLIGHT CONTROL INSPECTION. PULLED FLIGHT RECORDER AND VOICE RECORDER PER FLIGHT SAFETY. PERFORMED INSPECTION 05-51-12-6 PART 2 A-CHECK AND HARD LANDING SECTION A AND B WITH NO DEFECTS NOTED. FLIGHT CONTROL CHECK PER MM 27-00-0-2. ALL CHECK PASSED AS REQUIRED. REMOVED AND REPLACED FLIGHT DATA RECORDER PER FLT SAFETY. SYSTEM OPS CHECK GOOD. RETURNED TO SERVICE. 2L73 4F RTA22WE 20041230000532004123000053WP 2004 12 30 DHL2004802007 120041112A3260H2024B UPLOCK SWITCH DOUG DC8 DC873 302199CWP LT MLG DOOR MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01802DH 46076 DURING LEVEL OFF AND FL 250 DOOR NOT LATCHED LIGHT ILLUMINATED RAN ABNORMAL PROCEDURES DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED. RESTRICTED TO 230 KTS S/O PANEL RT GEAR DOOR UNSAFE LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED LT MLG DOOR UPLATCH SWITCH PER MM 20 50-0, OPS CK GOOD PER MM 32-60-0 PN: H20-24B. 2L74 4F RT4A25 20041230000562004123000056CE 2004 12 30 66896 120041119A24001013645801 CIRCUIT BOARD BEECH 1900 1900D 1154162CE UNKNOWN BURNED OUT A AMWAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 CE07144ZV UE144 ON TAKEOFF ROLL, CREW SMELLED ELECTRICAL FUMES IN COCKPIT, ABORTED TAKEOFF, RETURNED TO GATE WITH NO FURTHER INCIDENT. REMOVED 11/21/04-REPLACED A127 PCB GOOD P/N 101-364580-1. 2L72 4T RTA24CE 20041230000592004123000059SW 2004 12 30 ALGA098105 120041123A6410206016201131 BLADE BELL 206 206L3 1182108SW TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03362AL1306 51471 INSPECTION FOR SKIN ON THE AREA OF TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3. 1G71 3U H2SW 20041230000602004123000060NM 2004 12 30 2004UALA01164 120041124A3260 PROXIMITY SENSOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29318UA 23950 RETURNED TO DEN, DUE TO A GEAR IN TRANSIT LIGHT PROBLEM. INDICATION WAS CAUSED BY FAULTY GEAR DOWN LOCK PROXIMITY SWITCH. REPLACED GEAR DOWN LOCK SWITCH. PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE SYSTEM. GEAR OPEARTION AND INDICATION FOUND NORMAL. 2L72 4F4 FRTA16WE E2GL 20041230000622004123000062EU 2004 12 30 DHL200436310 120041205A2613 INDICATOR AIRBUS300 A300B4203 3930306EU NR 8 BRAKE TEMP INOPERATIVE A DHLAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO01363DH 85 APPROXIMATELY 15 MINUTES AFTER TAKEOFF AT FLIGHT LEVEL 290, THE BRAKE TEMP ON WHEEL NR 8 INDICATED 700 DEGREES AND BRAKES HOT ILLUMINATED ON MASTER WARNING PANEL. ABNORMAL PROCEDURE COMPLETED ON LANDING APR BRAKE. T/S, SUSPECT F/E NR 8 BRAKE TEMP INDICATION FAULTY. DEACTIVATED NR 8 MAIN WHEEL BRAKE IAW AMM 32-00-00. NR 8 BRAKE TEMP IND PLACARD INOPERATIVE. TRANSFERED TO DMI 18694 PER MEL 32-42-09-1. 2L72 4F RTA35EU 20041230000652004123000065 2004 12 30 IXXA0400117O 420041031A22102588787904 COMPUTER DOUG DC8 DC862F 3021972WP RUDDER WEAK A IXXAA UNSCHED LANDING O OTHER CRCRUISE 1 SW11799AL750721836 45922 DURING CRUISE FROM RJTY AIRCRAFT YAWS TO THE RIGHT WHEN YAW DAMPER IS TURNED ON. THE AUTOPILOT RUDDER IS OFF SCALE RIGHT INDICE AUTOPILOT RUDDER OFF SCALE RIGHT. MAINTENANCE TROUBLESHOT AUTOPILOT SYSTEM AND FOUND YAW AND ROLL CHANNEL COMPUTERS WEAK. REMOVED AND REPLACED YAW CHANNEL AND ROLL COMPUTERS PER ALL APPLICABLE MANUALS AND THE OPERATIONAL CHECK WAS GOOD ON THE GROUND. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20041230000672004123000067WP 2004 12 30 UPS04843565 120041120A53103750891520 SHEAR TIE DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 SHEAR TIE CRACKED AT STA 440 LONG 21L. REMOVED, FABRICATED, AND INSTALLED. REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-9-0 FIG 88A, 51-1-20D DWG3750891, AND DPS7.00-1. 2L74 4F RT4A25 20041230000692004123000069WP 2004 12 30 UPS04843567 120041118A5313 LONGERON DOUG DC8 DC871F 302199DWP MAIN CABIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LONG 15L CRACKED AT STA 1702. REMOVED LONG 15L FROM STA 1695-1707 REF SRM53-2-0FIG10. FAB LONG SECTION FROM S1616757 EXTRUSION AND 4 SPLICE STRAPS FROM SHT7075T6 .080" REF SRM 53-2-2 FIG10 AND 53-5-3. INSTALLED PARTS AND TWO REPAIR SPLICES PER SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 20041230000712004123000071EU 2004 12 30 DHL2004363012 120041205A3150354001056 WARNING SYSTEM AIRBUS300 A300B4203 3930306EU MALFUNCTIONED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01363DH 85 RTO DUE TO CONTINUES CHIME. NO ANNUNCIATORS ILLUMINATED. REPLACE MWC PER MM 33-15-11. AURAL WARNING CHECKS OK PER MM 31-24-00. 2L72 4F RTA35EU 20041230000722004123000072EU 2004 12 30 04FDEA03333 120041202A5315 FLOORBEAM AIRBUS310 A310 EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 BULK CARGO FLOOR STRUCT RT SIDE FS 64 TO 67 FLOOR STRUCTURE W/MULTIPLE CORRODED FROM TOP TO UNDERNEATH SURFACE. REMOVED AND REPLACED TEE PROFILE AT FS 63 TO FS 67 RBL 37 RT IAW A310 SRM 51-40-21. 2L72 4F RTA35EU 20041230000742004123000074NM 2004 12 30 UPS04243588 120041204A3350 BATTERY PACK BOEING727 727185C 138406NNM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2L73 4F A3WE 20041230000752004123000075NM 2004 12 30 UPS04443589 120041205A3350M335 MODULE BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 AFT 2 EMERGENCY LIGHT IN CEILING PASSENGER SEAT AREA COMES ON MOMENTARILY THEN GO OUT WHEN SWITCH PLACED IN ON POSITION. REMOVED AND REPLACED POWER SUPPLY MODULE IAW MM 33-51-00 AND MM 33-57-04. OPS CHECK GOOD. EMERGENCY POWER SUPPLY INSTALLED STA 650. 2L74 4F A20WE 20041230000762004123000076NM 2004 12 30 HNAA0400163 120041130A533085320106 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSELAGE LIGHTNING STRIKEA HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 THIS EO PERFORMS REPAIR FOR FUSELAGE SKIN DAMAGED BY LIGHTNING STRIKE BY TRIMMING OUT DAMAGED SKIN ONLY AND INSTALLING EXTERNAL REPAIR DOUBLER. DMT FOR MANUFACTURERS DT REVIEW ALSO CREATED. REV A. ADDRESSES CHANGE DUE TO DAMAGE INCURRED DURING REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGE HFEC AND BOND TESTED. FABRICATED REPAIR DOUBLER AND REPAIR PACKERS INSTALLED REPAIR PARTS. 2H72 4T RTA13NM 20041230000802004123000080SO 2004 12 30 4028 220041119A8520 PISTON BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO HARTZLHCJ3Y PHCJ3YF2 GL NR 2 CYLINDER DAMAGED E BSYAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 GL07400RP TH319 299439R ED4456B ON APPROACH INTO CMH, RIGHT ENGINE LOST ALL OIL PRESSURE, PROPELLER FEATHERED AND ENGINE SHUT DOWN. FOUND NR 2 CYLINDER PISTON WITH SIGNS OF DESTINATION, FUEL NOZZLE OK. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20041230000812004123000081NM 2004 12 30 04FDEA03284 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230000822004123000082NM 2004 12 30 DHL2004760012 120041105A2613 CONTROL PANEL BOEING727 7272B7 138407LNM OVERHEAT SYSTEM MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01760AT 21954 OVERHEAT DETECTION SYSTEM STRUT AND LOWER AFT BODY LIGHTS ALL ILLUMINATED. WOULD NOT EXTINGUISH. FOUND TEST SWITCH FOR OVHT DETECTION SYSTEM FOR STRUTS AND LOWER AFT BODY LIGHTS INOP. DEFFERED TEST FUNCTION PER ASTAR MEL 26-10-2. CAT C CONTROL NR 18357. PLACARD INSTALLED. REF DMI 18357 OVERHEAT DETECTION SYS STRUT AND LOWER AFT BODY LIGHTS ARE ILLUMINATED, WOULD NOT EXTINGUISH. REMOVED AND REPLACED STRUT AND LOWER AFT BODY OVERHEAT DETECTION PANEL IAW B727 M/M 26-14-00. OPS CHECKED GOOD. THIS CLEARS DMI NR 18357 PLACARD REMOVED. 2L73 4F A3WE 20041230000872004123000087WP 2004 12 30 04FDEA03266 120041130A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 1942 LONGERON 50 RIGHT TO 51 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MINOR OR MAJOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENT. REMOVED OLD REPAIR IAW DC10 SRM 51-35-01 VOL 2, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC10 SRM 53-20-00 VOL 1, 51-21-01 VOL 2 AND 51-35-01 VOL 2. REFERENCE NON-ROUTINE N01182 2L73 4F RTA22WE 20041230000892004123000089WP 2004 12 30 04FDEA03268 120041130A5320 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 EXTERNAL DOUBLER ON LEFT HAND LOWER FUSELAGE SKIN STATION 470 TO 475 BETWEEN LONGERON 30 LEFT AND 31 LEFT APPEARS NOT TO BE PER THE SRM. REMOVED OLD REPAIR IAW DC10 SRM 51-33-01 VOL 2. FABRICATED AND INSTALLED NEW DOUBLERS IAW DC10 SRM 53-20-00 VOL 1, FIGURE 6, 51-35-01 AND 51-33-01 V0L 2. REFERENCE NON-ROUTINE N01093. 2L73 4F RTA22WE 20041230000912004123000091GL 2004 12 30 110404N103CS1 120041104A3260MS25237327 BULB CIRRUSSR SR22 2130001GL MLG INDICATOR BURNED OUT E Z5FALA ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION LDLANDING 1 NE03103C 5250438 UNSAFE GEAR INDICATION ON APPROACH TO KSFB. CREW FOLLOWED CHECKLIST AND DECIDED TO DIVERT TO KMCO AND DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. FAULT DETERMINED TO BE A FAILED LIGHT BULB. 1L71 3O NTA00009CH 20041230000922004123000092WP 2004 12 30 ASMF200412001 120041202A8010 COUPLER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE START VALVE BROKEN W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23205AM 49405 718411 DURING ENGINES START, LEFT ENGINE WAS NOT STARTED, START VALVE WAS OPENED MANUALLY AND FAIL CONTINUE. AIRCRAFT RETURNED TO PLATFORM AND DURING MAINTENANCE REVISION, ENGINE START COUPLER WAS DETECTED BROKEN. ENGINE START COUPLER WAS REPLACED IAW MM 72-61-00, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20041230000952004123000095WP 2004 12 30 UPS04843577 120041116A575346495971 FITTING DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING STA 419 T/E FLAP CANOE SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-3-0, 51-1-20D, 51-1-8. 2L74 4F RT4A25 20041230000962004123000096WP 2004 12 30 UPS04843578 120041119A5754576958927 DOUBLER DOUG DC8 DC871F 302199DWP RT WING L/E CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 RT WING L/E INTERNAL DOUBLER CRACKED AT DRAN HOLE, STA XFS329. FABRICATED REPLACEMENT DOUBLER FROM SHT7075T6/.090 PER SRM 57-3-0 FIG 12. TREATED AND PRIMED REF SRM 51-1-8. REMOVED AND REPLACED PART PER SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 20041230000992004123000099EU 2004 12 30 04FDEA03346 120041205A5330 SKIN AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 24 NOV0 16:00 MC1 R. DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC ENT BY: 067708. REPAIR APPROX FS 59 FWD OF RT AFT CARGO DOOR (LWR) NOT LISTED ON FEDEX MAJOR REPAIR REPORT. REPAIR PERFORMED IAW EA 6-5317-40001, DATED FROM 09/22/98. 2L72 4F RTA35EU 20041230001002004123000100NM 2004 12 30 QXEA200400786 120041128A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR UNLOCKED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09406QX8181 4048 SEA - FLIGHT 2322 - DURING DESCENT THROUGH 10,000 FEET, THE CREW RECEIVED A FUSELAGE DOOR WARNING FOR THE AFT BAGGAGE DOOR. THE AIRCRAFT ALSO LOST PRESSURIZATION. AFTER LANDING, THE DOOR WAS INSPECTED AND MAINTENANCE FOUND THE AFT DOOR HANDLE IN THE OUT POSITION. MAINTENANCE INSPECTED THE DOOR AND WAS UNABLE TO DISLODGE THE HANDLE. SEVERAL OPERATIONAL CHECKS WERE PERFORMED WITH THE AIRCRAFT PRESSURIZED AND UNPRESSURIZED. THE DOOR HANDLE STAYED IN THE LOCKED POSITION. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041228001792004122800179EU 2004 12 28 2004UALA01208 120041210A3010 O-RING AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DE ICE SYSTEM LEAKING A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29464UA 1290 FLIGHT DIVERTED WITH A WING LEAK, RESTRICTED TO NO ICING. FOUND FAN AIR VALVE THERMOSTAT LEAKING ONTO OVERHEAT LOOP - REPLACED SENSOR AND O-RING. 2L72 4F4 FRTA28NM E40NE 20041228001902004122800190EA 2004 12 28 MASA200400703 120041217A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 ASH 2799 IN PHL PILOT REPORTED A SECTION OF THE EMERGENCY EXIT PATH LIGHTING WAS INOP. MAINTENANCE RESECURED THE LIGHTING CONNECTOR. 2L72 4F RTA21EA 20041228001922004122800192NM 2004 12 28 2004UALA01204 120041210A3350BPS73 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29119UA 28812 FLASHING EMERGENCY EXIT LIGHTS UPPER DECK FWD OF EXIT DOORS INOP. REPLACED BATTERY PACK FOR LIGHTS. 2L74 4F4 FRTA20WE E24NE 20041229000092004122900009EA 2004 12 29 04361708 120041226A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA TE FROZEN A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27708BR 7575 FLAPS FAILED AT 0. DIVERSION DUE TO SNOW CONTAMINATION. MX RETRIEVED FAULT CODES, RESET SYSTEM. OPS CHECK GOOD AT THAT TIME. 2L72 4F RTA21EA 20041229000142004122900014EA 2004 12 29 SWIA200414299 120041222A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07952SW 7805 FLAP FAIL INBOUND. REPLACED RIGHT NR 1 FLAP ACTUATOR AND FECU IAW AMM 27-53-05, 27-53-10, 27-52-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041229000222004122900022NM 2004 12 29 0402195520 120041222A5320 FLOOR SUPPORT BOEING757 757251 1384970NM GALLEY CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01520US 23208 DURING H-CHECK FOUND CORROSION ON GALLEY FLOOR SUPPORT AT BS 365 RBL 24. REPAIRED PER EA 55-201148. 2L72 4F RTA2NM 20041229000342004122900034SO 2004 12 29 C2XA04BT128 120041211A335074441 LIGHT EMB 145 EMB145LR 3260212SO FUSELAGE INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712569 145630 BNA - CREW REPORTED, DURING PREFLIGHT FOUND EXIT ROW 12 OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT ROW EMERGENCY LIGHT IAW EMB 145 AMM 33-50-00. OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20041229000402004122900040EA 2004 12 29 04356649 120041221A4900 APU CNDAIRCL600 CL6002B19 1900309EA ODOR A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27649BR 7414 AFTER GEAR UP, INDICATION OF SMOKE IN THE BACK. NO SMOKE VISIBLE BUT STRONG SMELL. MX INSPECTED AC DUCTS AND CLEANED. PERFORMED ENGINE RUNS. APU STARTED AND OIL SMELL CAME BACK. APU BEING WORKED ON. MX WILL ALSO INSPECT LAV, RETURNED TO SEAT LIGHTED PLACARD, BECAUSE OF OTHER SIMILAR EVENTS ON FLEET. 2L72 4F RTA21EA 20041229000432004122900043WP 2004 12 29 AALA20041241 120041222A322039567851 LINKAGE DOUG DC9 DC982 3022082WP NLG SHEARED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21501AA 49738 RDU - INFLIGHT T583/22 STRONG VIBRATION FROM NOSE GEAR ON TAKEOFF JUST AFTER GEAR RETRACTION. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. FOUND SHEARED BOLT ON UNLOCK HANDLE ON GEAR DOOR. REPLACED LEFT GEAR DOOR LINKAGE AND ADJUSTED LEFT AND RIGHT LINKAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20041229000512004122900051EU 2004 12 29 MALA040867 120041118A5512 SKIN SAAB SF340 340B 7860101EU HORIZONTAL STAB DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 DURING LC2 INSPECTION, NOTED STABILIZER L/E, FOUND DENT ON UPPER SKIN OF RT HORIZONTAL STAB. DIAMETER OF DENT IS 1.875 INCH DEPTH IS .057. DENT IS 3.875 INCH AFT OF SKIN PANEL LEADING EDGE, 72 INCHES O/B FROM FUSELAGE. 2L72 4T RTA52EU 20041229000522004122900052EU 2004 12 29 MALA040868 120041118A3350 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15370PX 340B300 DURING TAWS INSPECTION, FOUND EMERGENCY LIGHT ASSOCIATED WITH POWER SUPPLY 24LN INOP. BATTERY PACK IN POWER SUPPLY 24LN INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY. OPS CHECK GOOD. 2L72 4T RTA52EU 20041229000802004122900080EU 2004 12 29 MALA040884 120041116A3350 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15421XJ 340B421 DURING CAPACITY CHECK, EMERGENCY POWER SUPPLY 3301-51 S/N 1438 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 3301-31 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/17/04. 2L72 4T RTA52EU 20041229000892004122900089SO 2004 12 29 CHQA000599 120041221A3350 BULB EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11841 145737 RIGHT TOP EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041229000992004122900099EA 2004 12 29 SWIA200414301 120041224A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07924SW 7681 FLAPS FAIL MESSAGE WHEN FLAPS SELECTED. REMOVED AND REPLACED FECU PER CRJ 200 MM 27-51-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041229001112004122900111NM 2004 12 29 249TR0066 120041222A5247 ATTACH ANGLE BOEING737 7372K5 138448XNM APU DOOR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 ATTACH ANGLE AT AFT HINGE OF APU DOOR CRACKED. REPLACED ATTACH ANGLE PER SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20041229001152004122900115NM 2004 12 29 249TR0060 120041222A5320 CLOSEOUT PANEL BOEING737 7372K5 138448XNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CLOSE OUT FLOOR WEB AT BS 1006 AT APPROX RBL 45 IS DAMAGED. REPLACED WEB PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001242004122900124SO 2004 12 29 SWIA200414293 120041220A3350D36604001 BATTERY PACK EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07564SW476 476 120339 FOUR FLOOR LEVEL EMERGENCY LIGHTS AND BOTH PAIRS OF OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041229001252004122900125NM 2004 12 29 QXEA200400917 120041222A2910 LINE BOMBDRDHC8 DHC8401 1390041NM NR 1 BRAKE RUPTURED A QXEAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM09401QX8597 4031 SEA - FLIGHT 2372 - FLIGHT RETURNED TO GATE AFTER RECEIVING A NR 2 HYDRAULIC CAUTION WITH ASSOCIATED LOSS OF NR 2 HYDRAULIC QUANTITY. USERS OF NR 2 HYDRAULICS BECAME INOPERATIVE. HYDRAULIC PRESSURE FLUCTUATED BETWEEN 150 AND 2000 PSI. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 MAIN LANDING BRAKE LINE RUPTURED. THE LINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041229001362004122900136EU 2004 12 29 MALA040874 120041122A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, UPPER FUSELAGE IS DENTED FWD OF STA 487 AT 11 O'CLOCK POSITION AND WAS REPAIRED IAW MESABA EO S53035. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229001392004122900139 2004 12 29 SWAA043712 420041224A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29643SW 27716 R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041229001572004122900157NM 2004 12 29 QXEA200400845 120041205A2810 PACKING DHAV DHC8 DHC8202 2809007NM RT WING LEAKING A QXEAO OTHER K FLUID LOSS NRNOT REPORTED 1 NM09357PH15793 504 FUEL WAS NOTED LEAKING FROM THE NR 2 ENGINE COWLING BEHIND THE ENGINE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PACKING FOR THE RIGHT WING SPAR CONNECTOR RECEPTACLE. THE LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20041230000122004123000012WP 2004 12 30 WX0400049 120041106A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19861GA 49557 MAINTENANCE REPORTED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT BATTERY PACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041230000162004123000016GL 2004 12 30 CHQA000584 220041112A739723062387 WIRE HARNESS EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE CHAFED A CHQAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL11280 145381 CAE312346 DURING CLIMB OUT ON FLIGHT 3441 FROM LGA TO IND, "RUD HDOV PROT FAIL", "BLD VLV 2 FAIL", AND "BLEED 2 VLV CLOSED" MESSAGES APPEARED ON EICAS. WITHIN TEN SECONDS THE NR 2 ENGINE SHUTDOWN AND "ENG 2 OUT" MESSAGE APPEARED ON EICAS. THE CREW ATTEMPTED AN APU ASSISTED AIR RESTART, BUT THE ENGINE HUNG AT 36.5%. AN EMERGENCY WAS DECLARED AND THE CREW RETURNED TO LGA. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO VISUAL DAMAGE TO THE INLET, FAN, OR EXHAUST AREAS. FADEC'S 2A AND 2B WERE REMOVED AND REPLACED. UPON FURTHER INSPECTION, MAINTENANCE FOUND THE YELLOW FACEC HARNESS CHAFFED AT THE CONNECTION TO THE PYLON. REMOVED AND REPLACED E2 YELLOW FADEC HARNESS AND PMA ASSEMBLY. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20041230000172004123000017NE 2004 12 30 DJFA2004032 220041112A7200 ENGINE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343A 30015NE NR 1 MALFUNCTIONED E DJFAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA23699CW 5009 350205 CREW REPORTED, THAT DURING CLIMB WHILE EN ROUTE FROM KBRO TO KATL CLIMB POWER WAS NOT ACHIEVED. THE NR 1 ENGINE POWER WAS 2 PERCENT LOWER THAN REQUIRED. AIRCRAFT DIVERTED TO KDAL. MAINTENANCE SWAPPED THE P2 AND T2 PROBES BETWEEN THE LEFT AND RIGHT ENGINES AND SWAPPED N1 AMPLIFIERS BETWEEN LEFT AND RIGHT ENGINES. DURING GROUND RUN MAINTENANCE FOUND ENGINE ABLE TO MAKE TAKEOFF POWER AND N1 INDICATION TO BE WITHIN LIMITS. ENGINE TROUBLESHOT WITH REFERENCE TO GENERAL ELECTRIC FAULT ISOLATION TABLE 114 WITH NO DEFECTS NOTED. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20041230000282004123000028SW 2004 12 30 ALGA097958 120040905A6300406310405101 BEARING BELL 407 407 1182206SW M/R DRIVE BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03XAJMB95 53274 AXIAL WEAR AND BINDING, REPLACED W/NEW. 1G71 3U O H2SW 20041230000372004123000037 2004 12 30 DHL2004743007 420041113A3414 INDICATOR BOEING727 727225 1384077NM COCKPIT INOPERATIVE A DHLAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01743DH 22438 RTO F/O'S AIRSPEED DID NOT WORK ON T/O RUN. REMOVED AND REPLACED F/O'S AIRSPEED INDICATOR. OPS CKS GOOD IAW MM 34-12-0. PITOT STATIC CKS GOOD IAW MM 34-11-0. 2L73 4F A3WE 20041230000462004123000046 2004 12 30 P9RA20040052 420041212A2565387 BULB BOEING757 757231 1384950NM SLIDE LIGHT INOPERATIVE A P9RAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO11708TW 28480 DTW GATE, L2 SLIDE ARM LIGHT FAILS TO ILLUMINATE WHEN DOOR ARMED. RELAMPED L2 SLIDE ARM LIGHT IAW MM. 2L72 4F RTA2NM 20041230000662004123000066 2004 12 30 DHL2004806004 420041105A2561P0723E105P LIFE VEST DOUG DC8 DC873F 302199FWP CABIN MISSING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH 46002 AFT COURIER SEAT AT CABIN ENTRY AREA MISSING LIFE PRESERVER. INSTALLED SERVICABLE VEST IN AFT COURIER SEAT IAW M/M 25-60-0 DATE CHECKED 10/4 RE-CHECK DUE 10/6. 2L74 4F RT4A25 20041230000682004123000068WP 2004 12 30 UPS04843566 120041120A53103750891520 SHEAR TIE DOUG DC8 DC871F 302199DWP CARGO BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 CRACKED SHEAR TIE AT LONG 21L STA 460. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE REF SRM 51-1-21, 51-1-8, 51-1-20D, 51-9-0 FIG 68A, DWG3750891, AND DPS7.00-1. 2L74 4F RT4A25 20041230000772004123000077NM 2004 12 30 04FDEA03281 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT HAND WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230000792004123000079NM 2004 12 30 04FDEA03283 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230000832004123000083SO 2004 12 30 SWIA200414237 120041204A2752 ACTUATOR EMB 120 EMB120ER 3260203SO NACELLE FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM0758733 120197 CONTROL FAULT AFTER SELECTING FLAPS 45. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR AND RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-00. REMOVED AND REPLACED ANNUNCIATOR ASSY IAW 27-50-08; REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD IAW 27-50-00 PN OFF 308200-1007, SN OFF 0353 PN OFF 306900-1005, SN OFF 0108, PN OFF 307500-1001, SN OFF 0215. 2L72 4T RTA31SO 20041230000842004123000084 2004 12 30 750WL0011 420041126A2230 SERVO BOEING757 757200 1384950NM AUTO THROTTLE MALFUNCTIONED A PIDAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO05750WL 23928 ON TAKEOFF ROLL AND ALL PHASES OF FLIGHT, THE AUTO THROTTLE SYSTEM COMMANDED ERRATIC THROTTLE MOVEMENT. PLACED ON MEL 22-30-1. REPLACED AUTO THROTTLE SERVO MOTOR GENERATOR PER MM 22-32-01. 2L72 4F RTA2NM 20041230000942004123000094EA 2004 12 30 HNAA0400172 120041205A5270 PROXIMITY SENSOR DHAV DHC8 DHC8311 1386006EA EMERGENCY EXIT OUT OF ADJUST A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07343EN 340 PASSING THROUGH 7,700 FT, RT FORWARD EMERGENCY EXIT WARNING LT ILLUMINATED. LT EXTINGUISHED AFTER DUMPING PRESSURE PER EMERGENCY CHECK LIST. ADJUSTED DOOR PROXIMITY SENOR RAN A/C PRESSURIZED TO MAX DIFFERENTIAL. OPS CHECK GOOD. NO DEFECTS NOTED. 2H72 4T RTA13NM 20041230001022004123000102NM 2004 12 30 HNAA0400164 120041130A5330 SKIN PANEL DHAV DHC8 DHC8102 2809003NM FUSLEAGE LIGHTNING STRIKEA HNAAK NONE O OTHER ININSP/MAINT 1 EA07937HA 148 THIS EO PERFORMS REPAIR FOR FUSELAGE SKIN DAMAGED BY LIGHTNING STRIKE BY TRIMMING OUT DAMAGED SKIN ONLY AND INSTALLING EXTERNAL REPAIR DOUBLER. TRIMMED OUT DAMAGE SKIN AND WAFFLE. HFEC AND BOND TESTED. FABRICATED REPAIR DOUBLER AND PACKER. INSTALLED PARTS 2H72 4T RTA13NM 20041230001042004123000104EU 2004 12 30 DHL2004366007 120041109A3240C200601004 BRAKE ASSY AIRBUS300 A300B4203 3930306EU NR 1 DAMAGED A DHLAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01366DH 249 BRAKE TEMP INDICATOR FLUCTUATED +/- 30 DEGREES ON TAXI IN. NR 1 WHEEL ASSY DAMAGED FROM NR 1 BRAKE. FOUND NR 1 BRAKE TEMP SENSOR DAMAGED BECAUSE NR 1 BRAKE ASSY. ALSO, DAMAGED REPLACED NR 1 BRAKE ASSY IAW M/M 32-42-27. OPS CK AND LEAK CK GOOD. REPLACED NR 1 MLG WHEEL ASSY IAW M/M 12-37-32. OPS CK GOOD. 2L72 4F RTA35EU 20041230001052004123000105CE 2004 12 30 GLBA20030753 120041105A5514 WEB BEECH 1900 1900D 1154162CE HORZONATAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03122UX UE122 IN PANEL 332 ATC WHERE DE-ICE LINE GOES THROUGH METAL CRACKED AROUND GROMMET ( FWD WEB). REPAIRED HORIZ MAIN SPAR WEB. 2L72 4T RTA24CE 20041230001082004123000108NM 2004 12 30 04FDEA03276 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CONTAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230001092004123000109NM 2004 12 30 QXEA200400854 120041129A5753 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND INBOARD FLAP HAS CHAFING DAMAGE FROM CONTACT WITH WING UPPER TRAILING EDGE ALONG THE ENTIRE FLAP LENGTH. REPAIRED IAW SRM 57-51-30-992-001. 2H72 4T RTA13NM 20041230001132004123000113 2004 12 30 2004UALA01169 420041130A2565 FITTING AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GIRT BAR STUCK A UALAK NONE O OTHER ININSP/MAINT 1 WP29449UA 851 DOOR 1L AFT GIRT BAR ATTACH FITTING IS STUCK OPEN AND WILL NOT SPRING BACK TO CLOSED OR LOCKED POSITION. REMOVED DEBRIS TRAPPED IN THE INTERFACE AND LUBED GIRT BAR. 2L72 4F4 FRTA28NM E40NE 20041230001142004123000114 2004 12 30 2004UALA01170 420041201A2200 AUTOPILOT SYS BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE MALFUNCTIONED A UALAO OTHER O OTHER CRCRUISE 1 WP29676UA 30028 CREW REPORTS TWO UNCOMMANDED YAW EVENTS EN ROUTE. LT AND RT YAW DAMPENER MODULES WERE CHECKED FOR RECORDED FLT FAULTS AND NONE WERE FOUND. MCDP CHECKS 1, 9, 40, AND 69, RELATING TO THE AUTOPILOT DIRECTIONAL SERVOS, WERE PERFORMED AND ALL CHECKED OK. CENTER FCC WAS REPLACED AS A PRECAUTION. AUTOPILOT DOES NOT INTERFACE WITH RUDDER SERVOS DURING CRUISE. FLIGHT RECORDER DATA DID NOT INDICATE ANY ENGINE ANOMALIES TO ACCOUNT FOR THE EVENT. THERE IS NO CLEAR EXPLANATION FOR THE UNCOMMANDED YAW. 2L72 4F4 FRTA1NM E24NE 20041230001162004123000116SO 2004 12 30 CHQA000591 120041204A33503025103 LIGHT EMB 145 EMB145ER 3260211SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11977 1230312303 145185 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT LIGHT ASSY PER EMB 145 AMM 33-50-07. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041230001172004123000117SO 2004 12 30 CHQA000590 120041203A3350 LIGHT EMB 135 EMB135KL 3260302SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11375 145569 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT OVERWING EMERGENCY EXIT LIGHT IAW EMB 140 MM 25-50-00. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041230001202004123000120NM 2004 12 30 04FDEA03285 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230001232004123000123NM 2004 12 30 P9RA20040053 120041212A335020121 CHARGER BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11720TW 30319 MIAMI MAINTENANCE, DURING EMERGENCY LIGHT TEST, FOUND LEFT AFT LIGHT INOPERATIVE. REPLACED BOTH BATTERY PACK AND CHARGER UNIT IAW MM. BATTERY OFF PN 20131A SERIAL NUMBER OFF 70171. 2L72 4F RTA2NM 20041230001242004123000124EU 2004 12 30 AWXA200401373 120041112A5347D53112830200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK, CORROSION WAS FOUND ON DUMMY RAIL -Y81, BETWEEN FS 13 AND FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL -Y81, FROM FS 13 TO FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20041230001262004123000126CE 2004 12 30 112204N336CS1 120041122A3220 LANDING GEAR CESSNA500 550 2076604CE NOSE MALFUNCTIONED E Z5FAO OTHER J WARNING INDICATION LDLANDING 1 NE03336CS 5501095 UNSAFE NOSE GEAR INDICATION, GEAR MANUALLY DROPPED. CAUSE TO BE DETERMINED AT SERVICE CENTER. 1L72 4F A22CE 20041230001272004123000127NM 2004 12 30 AWXA200401340 120041126A335020121 CHARGER BOEING757 7572S7 1384962NM EMERGENCY LIGHT FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - EEL - DURING 4-DAY CHECK, EMERGENCY ESCAPE PATH LIGHTS BETWEEN SEAT ROWS 27 AND 35 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AND BATTERY AT BS 1650, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20041230001282004123000128 2004 12 30 AWXA200401341 420041126A2565D30665105 SLIDE AIRBUS320 A320231 3930325EU L-2 DOOR FAULTY A AWXAO OTHER PS NO WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 WP28624AW7704 1282 055 PHX - EEL / EES - FLT 0005 - DURING FLIGHT, EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13, 17, 19, AND 24 ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY IAW T/C R1C25304, OPERATIONAL CHECK OF EMERGENCY LIGHTING AND SLIDE WAS GOOD. 2L72 4F RTA28NM 20041230001342004123000134NM 2004 12 30 AWXA200401349 120041031A52305917001053 FRAME BOEING737 7373Y0 1384671NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK A 2 INCH CRACK WAS FOUND ON FRAME AT FORWARD UPPER EDGE OF AFT CARGO DOOR BS 442.55, STR 21 RT. AFTER REMOVAL OF PRESSURE SEAL AND CABLE DRUM ASSEMBLY A CRACK WAS FOUND IN LOWER FRAME CORNER. MAINTENANCE OPENED INNER SKIN ON AFT CARGO DOOR AND REMOVED BOTH FORWARD UPPER AND LOWER CORNER FRAMES; FABRICATED NEW REPLACEMENT UPPER AND LOWER CORNER FRAMES; INSTALLED REPAIR PARTS IAW E.O. 52-33-02, FIG 1-7. 2L72 4F RTA16WE 20041230001352004123000135NM 2004 12 30 AWXA200401350 120041031A33973404302 CONNECTOR BOEING737 7373Y0 1384671NM ZONE 200 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 DURING C-15 CHECK, NUMEROUS EMERGENCY ESCAPE PATH LIGHT HARNESS SPLICES AND CONNECTORS WERE FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED DAMAGED SPLICES AND CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT HARNESS, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20041230001392004123000139NM 2004 12 30 04FDEA03297 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. 2L73 4F RTA22WE 20041230001422004123000142WP 2004 12 30 04FDEA03212 120041125A5313AGA3082505 LONGERON DOUG MD10 MD1010F 3022112WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AFT CARGO AT STA 187. FOUND STR 44 RT WITH CORROSION. REPLACE LONG 44 PER SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAGE 1-12. 2L73 4F RTA22WE 20041230001432004123000143WP 2004 12 30 04FDEA03213 120041125A5311AGA31833 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT FUSELAGE COMPT STA 1975 FOUND FRAME P/N AGA 3183-3 WITH CORROSION. REPLACE FRAME PER SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34-47. 2L73 4F A22WE 20041230001442004123000144WP 2004 12 30 04FDEA03214 120041125A5330AFA30931 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT CARGO LOWER BELLY SKIN B/L LONG 48 RT - 48 LT STA 1531-1741 WITH CORROSION INTERNAL AND EXTERNAL SIDE. REPLACE SKIN PER SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34- 47 (REF DWG NFA 6014) 2L73 4F A22WE 20041230001452004123000145WP 2004 12 30 04FDEA03215 120041125A5311AGA37873 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT FUS VAST COMP STA 1986 FOUND EXISTING REPAIRED AND CORROSION ON FRAME P/N AGA3787-3. REPLACE FRAME PER SRM 51-35-01 PAGE 1-12 AND SRM 51-33-01 PAGE 34-47. 2L73 4F A22WE 20041230001482004123000148CE 2004 12 30 66603 120041108A32429038000133 MASTER CYLINDER BEECH 1900 1900D 1154162CE BRAKES FAILED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07139ZV UE139 UPON TAXI IN, CAPT EXPERIENCED RT BRAKE PERFORMANCE SPONGY, A/C CONTINUED TO GATE/HANGAR WITH NO FURTHER INCIDENT. REMOVED AND REPLACED CAPT'S RT BRAKE MASTER CYLINDER AND BLED BRAKES. OPS CK NORMAL P/N 90-380001-33 S/N 3273 P/N 90-380001-33 (OFF) S/N 3123 (OFF) 2L72 4T RTA24CE 20041230001492004123000149NM 2004 12 30 QXEA200400813 120041122A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - NR 1 SEAT TRACK HAS LIGHT SURFACE CORROSION ON TOP OF RAILS AT STATIONS X295-297, X330-X332, X363-X366, X376-X379, X393, X406-X409 AMD X425. REPAIRED IAW RD 8-53-1342, SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20041230001502004123000150EA 2004 12 30 QXEA200400817 120041124A7130 SEAL CNDAIRCL600 CL6002C10 1390015EA ZONE 400 TORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND AFT CORE-COWL P-SEAL IS TORN AT OUTBOARD SIDE. REPAIRED IAW SRM 51-42-06-001-001-401, PAGE 1-16. 2L72 4F RTA21EA 20041230001512004123000151EU 2004 12 30 MALA040728 120041111A33507339410005 CAP SAAB SF340 340B 7860101EU EMERGENCY LIGHT MISSING A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15418XJ 340B418 FLOOR EMERGENCY LIGHTING IS MISSING END CAP IN FRONT. PLACED ON 100 FLIGHT HOURS PWI TO INSTALL END CAP PN 7339410-005 AND SCREW PN NAS1102-06-10. REPLACED MISSING END CAP IN EMERGENCY FLOOR LIGHTING. ALL CHECKS GOOD. 2L72 4T RTA52EU 20041230001522004123000152WP 2004 12 30 04FDEA03339 120041203A5754 SLAT TRACK DOUG DC10 DC1010 3022110WP LT WING WORN A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT LT WING FIX L/E NR 6 SLAT TRACK RIB WITH SEVERAL WEAR. REPLACE RIB PER SRM 51-33-01 PAGE 34/47. REPLACED P/N: ARB 1188-1 QTY: 8 ARB 1141-1 QTY: 1 ARB 1143-503 QTY:1 ARB 1147-503 QTY:1. 2L73 4F A22WE 20041230001542004123000154EA 2004 12 30 QXEA200400818 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION AT STATION X691, X713-X719. REPAIRED IAW CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20041230001582004123000158NM 2004 12 30 04FDEA03222 120041125A5320 SPLICE DOUG MD11 MD11 3023602NM ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 38R. REMOVED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20041230001612004123000161SO 2004 12 30 2004F00432 120041106A3010 BOOT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2A GL LT WING DEBONDED G A UNSCHED LANDING PDENO WARNING INDICATION INFLIGHT SEPARATION VIBRATION/BUFFET NRNOT REPORTED 1 AL053590N 318052148 DURING FLIGHT, LEFT WING DE-ICE BOOT OUTBOARD OF LEFT ENGINE ONE FOOT OF DE-ICE BOOT DEBONDED FROM WING SURFACE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20041230001632004123000163SO 2004 12 30 CHQA000592 120041211A3350 LIGHT EMB 145 EMB145MP 3260216SO OVERWING EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11975 145337 LEFT HAND EMERGENCY OVERWING EXIT LIGHT IS INOP. RELAMPED LEFT EXTERNAL OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050103000032005010300003WP 2005 1 3 ABXA040394 120041110A5313592599225 LONGERON DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 LONGERON 30 CRACKED FORWARD AND AFT AT SPLICE FS 380. REMOVED AND REPLACED LONGERON 30 FROM STA 355 TO 415. 2L72 4F A6WE 20050103000062005010300006WP 2005 1 3 ABXA040398 120041112A53119923409502N FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 RIGHT FORWARD MAIN FRAME FS 699 CRACKED AT FORWARD FLANGE POINTS F & E AND AFT FLANGE POINTS H & I. REMOVED AND REPLACED FRAME AT STA 699 IAW EA 53400322-001-3. 2L72 4F A6WE 20050103000082005010300008WP 2005 1 3 ABXA040401 120041220A3040 ODOR DOUG DC9 DC932 3022066WP COCKPIT DETECTED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23903AX 47427 WHILE EN ROUTE TO FSD, FLIGHT 140 HAD A SLIGHT ODOR IN THE COCKPIT. ISOLATED TO AROUND FIRST OFFICER'S MAP LIGHT. PULLED MAP LIGHT CIRCUIT BREAKER, ODOR APPEARED TO GO AWAY. DURING DESCENT, AROUND 8000 FT, ODOR RE-APPEARED. NO OTHER INDICATIONS, (I.E. SMOKE, ETC.). VERIFIED MAP LIGHT OKAY FOR SERVICE. ISOLATED SMELL TO FIRST OFFICER'S CLEARVIEW WINDOW ANTI-FOG WINDOW HEAT. WORK IN PROGRESS. 2L72 4F A6WE 20050103000102005010300010WP 2005 1 3 ABXA040403 120041226A2740920710296 RELAY DOUG DC9 DC932F 3022067WP PRIMARY TRIM FAILED A ABXAO OTHER FB FLT CONT AFFECTED SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23905AX2383 47147 DURING INITIAL CLIMB, PRIMARY TRIM C/B 0A TRIPPED, ALTERNATE TRIM WORKED FINE. ELECTED TO PULL PRIMARY TRIM C/B'S 0B AND 0C. CONTINUED FLIGHT USING AUTOPILOT. WHEN REMOVING CREW BAGS, NOTICED STRONG ELECTRICAL SMELL (BURNT ODOR) IN BELLY'S 1 AND 2. FOUND UPPER PRIMARY LONG TRIM RELAY BURNT. REMOVED AND REPLACED RELAY IAW DC-9 MM 27-40-04 AND WORK PACK WO 2004905. 2L72 4F A6WE 20050103000112005010300011EU 2005 1 3 AWXA200401434 120041227A3350321454 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28644AW129 317 PHX - EEL - FLIGHT CREW REPORTED THE RT CENTER EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050103000122005010300012NM 2005 1 3 AWXA200401435 120041207A5320BAC1498217 SUPPORT BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON PASSENGER CABIN SUPPORT SECTION AT BS 365.25, RBL 55. MAINTENANCE REMOVED CORRODED SUPPORT SECTION AT BS 365.25, RBL 55; FABRICATED A NEW SUPPORT SECTION PER DWG 141N5186; INSTALLED REPAIR PART IAW B757-200 SRM 51-10-02. 2L72 4F RTA2NM 20050103000162005010300016NM 2005 1 3 AWXA200401439 120041208A575369372099 SUPPORT BOEING737 7373G7 1384595NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTER GIMBLE INDEXING PLATE SUPPORT AT WBL 173.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTER GIMBLE INDEXING PLATE SUPPORT IAW B737-300 SOPM 20-50-01 FIG 1. 2L72 4F RTA16WE 20050103000222005010300022EU 2005 1 3 AWXA200401455 120041212A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28619AW119624587 527 MCN - EEL - DURING C-08 CHECK FOUND THE EMERGENCY EXIT LIGHTS AT SEAT ROW 1 LT, FORWARD CLASS DIVIDER, R-1 DOOR, AND L-1 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT FORWARD EMERGENCY POWER SUPPLY UNIT (10WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050103000242005010300024NM 2005 1 3 AWXA200401457 120041207A5320694122615 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INNER CHORD SPLICE (ANGLE) BETWEEN BS 998 AND BS 1003, RBL 43, WL 208.5. MAINTENANCE REMOVED CORRODED ANGLE AT RBL 43 FROM BS 998 TO BS 1003; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-41226-15; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050103000252005010300025NM 2005 1 3 AWXA200401446 120041207A53206546812186 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 991, RBL 14, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 991, RBL 14, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 1 & 12. 2L72 4F RTA16WE 20050103000262005010300026NM 2005 1 3 AWXA200401458 120041205A5320654587512 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON R-1 ENTRY WAY UPPER CHORD (ANGLE) BETWEEN BS 298 AND BS 328, RBL 60, WL 209. MAINTENANCE REMOVED CORRODED ANGLE AT RBL 60 FROM BS 298 TO BS 328; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-45875-12; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 8. 2L72 4F RTA16WE 20050103000282005010300028NM 2005 1 3 AWXA200401447 120041207A53206546812185 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 999, LBL 11, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 999, LBL 11, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1 & 12. 2L72 4F RTA16WE 20050103000302005010300030NM 2005 1 3 AWXA200401449 120041205A5320654580863 BEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON BEAM AT BS 294, BETWEEN RBL 24 AND RBL 59, WL 208. MAINTENANCE REMOVED CORRODED BEAM AT BS 294, FROM RBL 24 TO RBL 59; FABRICATED A NEW REPLACEMENT BEAM PER DWG 65-45808; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8. 2L72 4F RTA16WE 20050103000322005010300032NM 2005 1 3 AWXA200401451 120041211A532065C334192 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON RT AFT LAVATORY SUBFLOOR (SHEAR WEB) AT BS 1018 RBL 2 AND RBL 34, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB AT BS 1018 FROM RBL 2 TO RBL 34; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C33419; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9 & 10. 2L72 4F RTA16WE 20050103000342005010300034NM 2005 1 3 AWXA200401453 120041208A5753693720910 SUPPORT BOEING737 7373G7 1384595NM RT MID FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBLE, OUTBOARD BEARING SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBLE, OUTBOARD BEARING SUPPORT IAW B737-300 SOPM 20-50-01 FIG 1. 2L72 4F RTA16WE 20050103000352005010300035NM 2005 1 3 AWXA200401429 120041207A532065C3267723 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON RT OUTBOARD HORIZONTAL WEB BETWEEN BS 995 AND BS 1014, AT RBL 41. MAINTENANCE REMOVED CORRODED RT OUTBOARD HORIZONTAL WEB AT RBL 41 FROM BS 995 TO BS 1014; FABRICATED A NEW REPLACEMENT WEB PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050103000372005010300037EU 2005 1 3 AWXA200401431 120041110A5320D53230585200 WEB AIRBUS320 A320232 3930326EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT SILL WEB AT -Y607 BETWEEN FR 24 AND FR 29. MAINTENANCE REMOVED CORRODED SILL WEB AT -Y607 FROM FR 24 TO FR 29; FABRICATED A NEW REPLACEMENT SILL WEB; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 FIG 2-3, 8, 12-13 & 18. 2L72 4F RTA28NM 20050103000402005010300040NM 2005 1 3 AWXA200401445 120041207A532065C320747 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 990, RBL 33, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 990, RBL 33, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1 & 12. 2L72 4F RTA16WE 20050103000442005010300044NM 2005 1 3 AWXA200401406 120041216A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28827AW 1547 PHX - EMERGENCY EQUIPMENT - DURING THROUGH FLIGHT INSPECTION THE FORWARD INBOARD EMERGENCY FLASHLIGHT WAS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050103000452005010300045NM 2005 1 3 AWXA200401398 120041203A53206545834107 STRAP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON LOWER FLOORBEAM STRAP AT BS 330.5, LBL 44, WL 201. MAINTENANCE REMOVED FASTENERS IN REPAIR AREA AND DRILLED A STOP DRILL HOLE AT END OF CRACK BS 330.5, LBL 44; FABRICATED A REPAIR PLATE PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FIG 204. 2L72 4F RTA16WE 20050103000472005010300047NM 2005 1 3 AWXA200401442 120041208A53116545855101 FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND AT FASTENER HOLES ON INNER CHORD BETWEEN BS 967 AND BS 986, RBL 60, WL 208. MAINTENANCE REMOVED CORRODED INNER CHORD FROM BS 967 TO BS 986, RBL 60; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050103000492005010300049EU 2005 1 3 AWXA200401386 120041112A5320D5311278520100 WEB AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT OUTBOARD WEB -Y1672 AT FR 20. MAINTENANCE REMOVED CORRODED RT OUTBOARD WEB -Y1672 FROM FR 20 TO FR 24; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050103000512005010300051NM 2005 1 3 AWXA200401388 120041129A5320693535011 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .3125 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT FORWARD SIDE OF BS 500D, STR 26 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500D, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050103000542005010300054EU 2005 1 3 AWXA200401392 120041112A5320D5311282720100 DUMMY RAIL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL Y503 AT FR 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL Y503 FROM FR 12 TO FR 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050103000562005010300056NM 2005 1 3 AWXA200401394 120041209A532065479573 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK GALVANIC CORROSION WAS FOUND ON AFT CARGO DOOR SILL WEB BETWEEN BS 807 AND BS 837, STR 25 RT. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL WEB FROM BS 807 AND BS 837, STR 25 RT; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1, 8, 9, & 10. 2L72 4F RTA16WE 20050103000582005010300058EU 2005 1 3 AWXA200401399 120041113A5321D5361033200800 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND IN SEVERAL LOCATIONS ON L-1 DOORWAY FLOOR PANEL 221FF. MAINTENANCE REMOVED CORRODED FLOOR PANEL 221FF, INSTALLED NEW REPLACEMENT FLOOR PANEL IAW AWA T/C C1D25306. 2L72 4F RTA28NM 20050103000592005010300059EU 2005 1 3 AWXA200401400 120041114A5320D53475575258 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR THRESHOLD COVERSHEET (SILL) BETWEEN FR 52 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FROM FR 52 TO FR 56; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050103000632005010300063SO 2005 1 3 C2XA04SH563 120041202A532014523171003 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C-CHECK THE LEFT OMEGA BEAM HAT SECTION WAS CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW EC5320-01177. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050103000642005010300064SO 2005 1 3 C2XA04TY179 120041209A335066369 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711526 145410 A/C 526 WAS IN FOR A MOD, FOUND BOTH FWD EMERGENCY FLOOR PROX LIGHT STRIPS TO BE INOP. MAINTENANCE REPLACED BOTH LIGHT STRIPS IAW EMB 135 AMM 33-50-08 AND OPS CHECK WAS GOOD. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF SCHEDULED MODIFICATIONS. 2L72 4F RTT00011AT 20050103000652005010300065SO 2005 1 3 C2XA04SH570 120041206A532014521713005 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715932 145015 DURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION WAS FOUND TO BE CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050103000672005010300067SO 2005 1 3 C2XA04RI017 120041208A33501317 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711536 145520 RIC - MX DURING ROUTINE INSPECTION, MAINTENANCE FOUND RIGHT WING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECKS PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050103000682005010300068SO 2005 1 3 C2XA04IA158 120041124A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716559 145603 IAH - FLIGHT 2018, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE ONE CEILING EMERGENCY LIGHT AND THREE LOWER LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050103000732005010300073NM 2005 1 3 C7WA200400065 120041103A3610BACC10DU350T CLAMP BOEING737 737231 1384079NM PWA JT8 JT8D219 52053NE CABIN PRESSURE LOOSE A C7WAA UNSCHED LANDING O OTHER CRCRUISE 1 SO1724343 21630 AIR RETURN, UNABLE TO PRESSURIZE IN FLIGHT. ATTEMPTED TO CONTROL CABIN MANUALLY WITH FULL INCREASE PRESSURE, NO HELP. RESECURED LOOSE DUCT AT LT MIX VALVE. OPS CHECK GOOD ON THE GROUND IAW MM 21-10-05. 2L72 4F4 FRTA16WE E9NE 20050103000742005010300074NM 2005 1 3 C8GA20040025 120041201A3250BACC13AP3C177 CONTROL CABLE BOEING727 7272A1 138407FNM NLG STEERING OUT OF ADJUST A C8GAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO15287SC 21345 FLT 717 FROM ELP TO STL. NO RUDDER PEDAL STEERING DURING TAKEOFF. TAKEOFF ABORTED. AIRCRAFT RETURNED TO BLOCKS WITH NO FURTHER INCIDENT. PLACED RUDDER PEDAL STEERING ON MEL 32-14, CONTROL NUMBER 12-01-01-C-11. AIRCRAFT RETURNED TO SERVICE. ON 12/02/04, ADJUSTED CABLE TENSION ON THE RUDDER PEDAL STEERING ARM AND RIGGED SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050103000792005010300079EA 2005 1 3 COMA0470082 120041212A3620 OVERHEAT LOOP CNDAIRCL600 CL6002C10 1390015EA RT ENGINE OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01367CA 10069 FLIGHT 5474 RT ENGINE BLEED CAUTION. COULD NOT DUPLICATE. ADJUSTED BLEED SENSOR LOOPS. 2L72 4F RTA21EA 20050103000802005010300080EA 2005 1 3 COMA0460679 120041213A33501308 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01712CA 7244 FLIGHT 5309 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB. 2L72 4F RTA21EA 20050103000822005010300082EA 2005 1 3 COMA0460686 120041215A5311 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01442CA 7483 RIGHT HAND 640 FRAME DOUBLER CRACKED. REPAIRED IAW SRM 51-44-06 AND 51-42-21. 2L72 4F RTA21EA 20050103000842005010300084EA 2005 1 3 COMA0460683 120041215A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01988CA 7204 RIGHT HAND NLG AFT FUSELAGE SKIN CRACKED AT RADIUS. REPAIRED IAW REO 601R-53-11-048. 2L72 4F RTA21EA 20050103000852005010300085 2005 1 3 COMA0460682 420041214A3425 FLIGHT DIR CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01936CA 7043 FLIGHT 5303 FLIGHT DIRECTOR WOULD NOT FOLLOW THE ILS. COULD NOT DUPLICATE. CYCLED AIRCRAFT POWER, ALL OPERATIONAL CHECKS WERE SATISFACTORY. 2L72 4F RTA21EA 20050103000892005010300089EA 2005 1 3 COMA0460678 120041213A2750 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT ACTIVATED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01783CA 7315 FLIGHT 5028 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD98-20-01. 2L72 4F RTA21EA 20050103000902005010300090NM 2005 1 3 DL73G041085 120041203A3246B737300MAIN BOLT BOEING737 7373L9 1384470NM NR 1 WHEEL SHEARED A DALAO OTHER O OTHER LDLANDING 1 SO27232DZ 24220 UPON LANDING TOWER REPORTED PUFF OF SMOKE FROM GEAR AND UPON PARKING AT GATE FOUND NUMBER 1 TIRE FLAT AND 5 RIM BOLTS SHEARED. REPLACED BOTH NUMBER 1 AND NUMBER 2 WHEELS ASSY'S. INSPECTED A/C, NO EVIDENCE OF ANY OTHER DAMAGE. 2L72 4F RTA16WE 20050103000922005010300092NM 2005 1 3 DL764041090 120041208A3350 CONNECTOR BOEING767 767432ER 1385134NM CABIN DISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27842MH 29715 ON TRANSIT CHECK FOUND EMERGENCY PATH LIGHT INOP AT SEAT 42F. FOUND QUICK DISCONNECT UNHOOKED UNDER SEAT. RECONNECTED, OPS OK. 2L72 4F RTA1NM 20050103000932005010300093NM 2005 1 3 DL73S041091 120041209A3243 SHUTTLE VALVE BOEING737 737232 1384475NM MLG BRAKE LEAKING A DALAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO27313DL 23085 B-SYSTEM HYD LEAK FOUND AT PUSHBACK. REPLACED BRAKE SHUTTLE VLV IAW M/M. 2L72 4F RTA16WE 20050103000982005010300098NM 2005 1 3 DLM88041089 120041208A71105930639531 ACCESS DOOR DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE MISSING A DALAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SO27932DL 49719 718223 N 2 ENGINE MANUAL START ACCESS DOOR MISSING. REPLACED SAME. 2L72 4F4 FRTA6WE E9NE 20050103000992005010300099NE 2005 1 3 DL76S041096 220041213A7200CF680A2 ENGINE BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 MAKING METAL A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27126DL38876 24076 580394 LEFT ENG OIL FILTER MESSAGE. DID NOT EXT WITH THROTTLE REDUCTION. OIL PRESS AND TEMP NORMAL. PERFORMED ENG SHUTDOWN PER QRH. DIVERTED TO JAX. DEBRIS FOUND ON CHIP DETECTORS. REPLACED ENGINE. 2L72 4F4 FRTA1NM E13NE 20050103001022005010300102NM 2005 1 3 DLM88041101 120041214A3222 STRUT DOUG MD88 MD88 3023688NM NLG LOW A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27913DL 49544 NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. SERVICED NOSE STRUT AND CYCLED GEAR. 2L72 4F RTA6WE 20050103001052005010300105NM 2005 1 3 DL73S041118 120041216A5312 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 INSPECTION OF THE FS 1016 P-DOME BULKHEAD WEB PER AD 99-08- 23 REVEALED 3 CRACKED CHORD ATTACH FASTENER HOLES BETWEEN STRINGERS 5L & 7L. THE CRACKS WERE REMOVED BY TRIMMING THE WEB. THE WEB WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 095482-14AD. 2L72 4F RTA16WE 20050103001072005010300107NM 2005 1 3 DHL2004746009 120041216A3200 LANDING GEAR BOEING727 727224 1384076NM MLG VIBRATION A DHLAO OTHER E VIBRATION/BUFFET LDLANDING 1 SO01746DH 22252 ON LANDING AIRCRAFT HAD SHAKING FEELING WHEN MAINS TOUCHED DOWN. INSPECTED MLG BRAKES, TIRES, TIRE PRESS, MLG ATTACH POINTS AND PERFORMED TAXI CHECK, NO DEFECTS NOTED AT THIS TIME IAW B727 MM 32-45-00 AND JRH 9.1. 2L73 4F A3WE 20050103001082005010300108CE 2005 1 3 DJFA2004041 120041216A3610 DUCT BEECH MU300 400A 1155402CE BLEED AIR SYS LEAKING E DJFAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23753TA RK230 CLIMBING TO 10,000 FT, LT BLEED AIR DUCT FAIL ANNUNCIATOR HAD ILLUMINATED. ENG THRUST REDUCED, AND CABIN PRESSURIZATION SOURCE TURNED OFF. TWO MINS LATER COCKPIT & CABIN HAD FILLED WITH SMOKE FOLLOWED BY EMERGENCY PRESSURIZATION VALVE OPENING. CREW DONNED OXYGEN MASKS & GOGGLES AS SMOKE HAD BECOME FAIRLY THICK. AN EMERGENCY WAS DECLARED & AIRCRAFT MADE AN UNEVENTFUL LANDING. MX FOUND A Y-DUCT ON LEFT SIDE TO BE MISALIGNED AND LEAKING. A NEW SEAL WAS INSTALLED ON THE OUTBOARD DUCT AT THE TOP OF THE FUSELAGE ABOVE THE PYLONS. THE EMERGENCY PRESSURIZATION VALVE WAS FOUND TO BE STUCK IN THE OPEN POSITION. A NEW VALVE WAS INSTALLED. OPERATIONAL CHECKS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050103001102005010300110CE 2005 1 3 DXTA200400494 120041224A323099146371 MANIFOLD CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07952QS2452 7500200 NOSE GEAR BUMP DURING DESCENT. REPLACED LANDING GEAR MANIFOLD ASSEMBLY AS PER THE CE750 MM CHAPTER 32-30-02. GROUND OPS AND LEAK CHECKS WERE SATISFACTORY. 2L72 4J RTT00007WI 20050103001122005010300112EU 2005 1 3 ESPA20040006 220041105A72005298Z ENGINE GULSTMG159 G159 3952202SO RROYCEDART DART5298Z 54507EU ROTOL R4304 R1844304 EU ENGINE MAKING METAL E ESPAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SO11190PA20602250 195 16121 DRG42267 ENGINE FLAMED OUT IN FLIGHT WITH NO WARNING OR INDICATION. METAL WAS FOUND IN THE OIL SCREEN. ENGINE WILL BE SENT BACK TO OVERHAUL FACILITY FOR EVALUATION AND WARRANTY CONSIDERATION. 2L72 4T4 T 1A17 E297 6 CP899 20050103001132005010300113 2005 1 3 F3LA200400101 420040926A2565 SLIDE AIRBUSA319 A319112 3930323EU L1 DOOR OUT OF ADJUST A F3LAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM03907FR 1743 BLOCK TURNBACK. FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT ARM. REMOVED, ADJUSTED AND REINSTALLED L1 DOOR SLIDE. OPS CHECK GOOD PER MM 25-62-44-000-062. 2L72 4F RTA28NM 20050103001142005010300114NM 2005 1 3 04FDEA03427 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1887 TO STA 1921, RBL 57. REMOVED AS IAW SRM 51-31-01 VOL II. NEW HAT SECTION FABRICATED AS PER DWG AGA 7496 AND INSTALLED IAW SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050103001152005010300115NM 2005 1 3 04FDEA03434 120041217A3221 TRUNNION DOUG MD11 MD11 3023602NM NLG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 UPON REMOVAL OF NOSE LANDING GEAR FOR BULKHEAD 595 REPAIR FOUND LEFT HAND TRUNNION FITTING (LOWER INBOARD-FORWARD OF BUSHING AREA) WITH A HAIR LINE CRACK. CRACKED AREA REPAIRED AS PER SRM 53-40-00 VOL I FIG 22. 2L73 4F RTA22WE 20050103001162005010300116NM 2005 1 3 04FDEA03435 120041217A3221 TRUNNION DOUG MD11 MD11 3023602NM NLG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 UPON REMOVAL OF NOSE LANDING GEAR FOR BULKHEAD 595 REPAIR FOUND RIGHT HAND TRUNNION FITTING (LOWER INBOARD-FORWARD OF BUSHING AREA) WITH A HAIR LINE CRACK. REMOVED AS PER SRM 51-33-01 VOL II AND NEW TRUNNION FITTING INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050103001192005010300119NM 2005 1 3 04FDEA03312 120041201A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. 2L73 4F RTA22WE 20050103001202005010300120NM 2005 1 3 04FDEA03181 120041122A5330 SKIN BOEING727 727100 1384036NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 UPPER EXTERNAL SKIN BS 761, 2 INCHES ABOVE STR 4 LT IS GOUGED. BLENDED GOUGE ON SKIN BS 761, 2 INCHES ABOVE STR 4 LT, OUT OF LIMITS. REPAIRED DAMAGE SKIN AT BS 761 STR 4 LT PER SRM 53-30-3 FIG 5. 2L73 4F RTA3WE 20050103001222005010300122WP 2005 1 3 04FDEA03188 120041123A7160 NOSE COWL DOUG DC10 DC1010 3022110WP NR 3 ENGINE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND ENG NR 3 NOSE COWL BORDER ENTRY, WITH NR 6 HOLE APPROX .125 INCH PLUS NICK. REPLACE ENG NR 3 NOSE COWL IAW MM 71-11-00-2: P/N NSL 6051-511. 2L73 4F A22WE 20041229000292004122900029NM 2004 12 29 249TR0064 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL CORRODED AT BS 907 + 8 BETWEEN RBL 8 AND RBL 23. REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 53-10-2. 2L72 4F RTA16WE 20041229000382004122900038EA 2004 12 29 QXEA200400908 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - RIGHT HAND INBOARD SEAT RAIL CORROSION APPROXIMATELY FS 728.00, FS 756.00 AND FS 828.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ SRM 51-21-16. 2L72 4F RTA21EA 20041229000422004122900042NM 2004 12 29 AALA20041239 120041221A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21693AA 26973 SAN - SEAT MOUNTED AISLE EMERGENCY LIGHTS IN COACH INOPERATIVE. REPLACED THREE BATTERY PACKS IN COACH CABIN FOR SEAT MOUNTED AISLE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20041229000452004122900045WP 2004 12 29 AALA20041240 120041222A3260 WARNING LIGHT DOUG DC9 DC983 3022083WP NLG ILLUMINATED A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21982TW 53632 ORD - INFLIGHT T1335/22 NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED FULL SERVICE ON NOSE LANDING GEAR STRUT AND GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20041229000492004122900049EU 2004 12 29 MALA040875 120041123A5310 DOOR FRAME SAAB SF340 340B 7860101EU CARGO DOOR CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15404XJ 340B404 DURING 4K INSPECTION IN BNA, CARGO DOOR CABLE HAS CHAFED INNER FLANGE OF FRAME AT FS 686.996. DAMAGE IS ACCEPTABLE AND WAS REPAIRED IAW MESABA EO 53213 AND SAAB DOCUMENT 340SDS007917. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2L72 4T RTA52EU 20041229000592004122900059EA 2004 12 29 SWIA200414297 120041219A27505332D1007 MOTOR-BRAKE UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 NM07934SW 7722 FLAPS HALFSPEED STATUS MESSAGE WHEN FLAPS SELECTED ON APPROACH. REMOVED AND REPLACED LEFT MOTOR/BRAKE ASSY IAW AMM TASK 27-52-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041229000702004122900070NM 2004 12 29 249TR0092 120041222A5340 ATTACH ANGLE BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON ATTACH ANGLE FOR AFT WALL OF FORWARD LAV. REPLACED HAT CHANNEL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229000772004122900077EU 2004 12 29 MALA040885 120041116A3350330151 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15421XJ 340B421 DURING CAPACITY CHECK, BATTERY PACK P/N 3301-51, S/N 2004 FAILED. REPLACED BATTERY ASSEMBLY P/N 3301-31 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/17/04. 2L72 4T RTA52EU 20041229000782004122900078NM 2004 12 29 249TR0098 120041222A53506548607181 SUPPORT ANGLE BOEING737 7372K5 138448XNM WING/BODY FAIR CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 LEFT INBOARD SUPPORT ANGLE CRACKED UNDER FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-341. 2L72 4F RTA16WE 20041229000842004122900084EU 2004 12 29 MALA040883 120041119A3350 POWER SUPPLY SAAB SF340 340B 7860101EU EMERGENCY LIGHTSINOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15445XJ 340B445 EMERGENCY POWER SUPPLY P/N 3301-51, S/N 1457 UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/26/04. 2L72 4T RTA52EU 20041229000922004122900092SO 2004 12 29 CHQA000601 120041222A3350 CONTROL PANEL EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11279 145379 UPON ENTERING THE AIRCRAFT THE EMERGENCY LIGHTS WERE COMING ON AND OFF ON THEIR OWN. TROUBLESHOT TO FLIGHT ATTENDANT CONTROL PANEL. REMOVED AND REPLACED FLIGHT ATTENDANT CONTROL PANEL IAW EMB 145 MM 25-27-09. OPS CHECK GOOD. 2L72 4T RTT00011AT 20041229000932004122900093NM 2004 12 29 249TR0076 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL CORRODED AT BS 947+9 AT FROM LBL 17 TO LBL 8. REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 53-10-2. 2L72 4F RTA16WE 20041229001072004122900107NM 2004 12 29 249TR0081 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL FROM BS 1006 TO BS 1016 AT BL 0 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-0. 2L72 4F RTA16WE 20041229001102004122900110NM 2004 12 29 249TR006512 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL CORRODED BETWEEN BS 927 AND BS 907 AT RBL 8. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001122004122900112NE 2004 12 29 249TR0067 220041222A7270 FLANGE BOEING737 7372K5 138448XNM PWA JT8 JT8D15A 52051NE ENGINE CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 719084 LEFT ENGINE FLANGE CRACKED OUTBOARD MOUNT FLANGE FOR THE PRECOOLER. REPAIRED PER JT8D MM 72-00. 2L72 4F4 FRTA16WE E2EA 20041229001222004122900122SO 2004 12 29 SWIA200414291 120041218A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07197SW 120186 EMERGENCY EXIT LIGHT (OVERHEAD) AT ROW 6C INOPERATIVE. RELAMPED BULB, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20041229001272004122900127EA 2004 12 29 04361624 120041226A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27624BR 7211 CA'S WINDOW CRACKED. RTF. MX REMOVED AND REPLACED LT FRONT WINDSHIELD. DID PRESSURIZATION CHECK. 2L72 4F RTA21EA 20041229001282004122900128EA 2004 12 29 04358708 120041223A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS FAULTY A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27708BR 7575 FLAP FAILURE AT 0 ON APPROACH. RUNWAY TOO SHORT DUE TO CONTAMINATION. DIVERSION. MX INTERROGATED FECU. CLEARED FAULTS, CHECKS FLAPS, OPS CHECK GOOD AT THIS TIME. 2L72 4F RTA21EA 20041229001302004122900130NM 2004 12 29 249TR00642 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL CORRODED AT BS 907 + 8 BETWEEN RBL 8 AND RBL 23. REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 53-10-2. 2L72 4F RTA16WE 20041229001322004122900132NM 2004 12 29 249TR0073 120041222A5347 GALLEY TRACK BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON INBOARD TRACK FOR G-1 GALLEY. REPLACED SECTION OF TRACK PER SRM 51-10-1. 2L72 4F RTA16WE 20041229001382004122900138EU 2004 12 29 MALA040882 120041125A3350 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15519XJ E2344 BATTERY PACK P/N 61-2275-1, S/N 0010437 WILL NOT LIGHT REQUIRED EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY CELL PACK P/N 61-2275-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/26/04. 2H74 4F RTA49EU 20041229001432004122900143 2004 12 29 SWAA043706 420041221A2565416A2200 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29735SA 27867 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM. 2L72 4F RTA16WE 20041229001452004122900145NM 2004 12 29 SWAA043708 120041222A53126545409 PRESSURE PANEL BOEING737 7373K2 13844BANM MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND MLG W/W CEILING BEADED WEB CRACKED AT BS 663, LBL 32 & RBL 43. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20041229001462004122900146NM 2004 12 29 SWAA043709 120041222A53126546547246 BULKHEAD BOEING737 7373Y0 1384671NM RT MLG WW PUNCTURED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BULKHEAD WEB PUNCTURED AT BS 727, RBL 24, WL 178. REPAIRED WEB PER SWA EA. 2L72 4F RTA16WE 20041229001472004122900147NM 2004 12 29 SWAA043710 120041222A5340907822 HINGE FITTING BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR UPPER AND LOWER HINGE BOX FITTINGS CRACKED. REMOVED AND REPLACED BOTH HINGE BOX FITTINGS PER MM & SRM. 2L72 4F RTA16WE 20041229001612004122900161EU 2004 12 29 MALA040828 120041116A5712 RIB SAAB SF340 340B 7860101EU WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 512AL 5 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 218746 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20041229001782004122900178NM 2004 12 29 04FDEA03177 120041122A5510ALC8103504 FITTING DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 BARREL NUT BORE NR 35R EXCEEDED LIMITS AFTER CORROSION REMOVAL. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 35R, REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR. 2L73 4F RTA22WE 20041229001842004122900184NM 2004 12 29 DHL2004755518 120041108A5753 SKIN BOEING727 727225 1384077NM TE FLAPS DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01755DH 21857 DURING A "C" CHECK, REPLACE INTERIM REPAIR ON RT WING I/B MID FLAP UPPER SKIN I/B END WITH A PERMANENT REPAIR. REMOVED INTERIM REPAIR FROM RT I/B MID FLAP UPPER I/B T/E TRIMMED OUT DELAMINATED AREA APPROX 1INCH BY 12 INCHES. FABRICATED FILLER APPROX 1 X 12 AND DOUBLER APPROX 2.5 X 13.5 FROM 2024.T3.016 PO NR 9001394 CLEANED, PREPPED, APPLIED ADHESIVE PRIMER, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES IAW B727 SRM 57-50-2 FIG 3 AND 51-40-20 FIG 30. 2L73 4F A3WE 20041229002002004122900200CE 2004 12 29 GLBA20030757 120041106A5320 BRACKET BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03122UX UE122 LT SIDE OF VERT STAB TO FUSELAGE L BRKT CRACK AT APPROX FS 70.107. REPAIRED CRACK IAW EO 04-122UE-01 AND B1900 SRM 51-70 MLS52057 ITEM 1. 2L72 4T RTA24CE 20041230000132004123000013WP 2004 12 30 WX0400046 120041013A5320 FRAME DOUG DC9 DC983 3022083WP CARGO DOOR DAMAGED A WX0AK NONE O OTHER ININSP/MAINT 1 WP19861GA 49557 MAINTENANCE REPORTED AFT CARGO PIT DOOR FRAME DAMAGED AT AFT LOWER CORNER. AIRCRAFT WAS FERRIED TO GYR FOR REPAIR. TIMCO ACCOMPLISHED EXTERNAL DOUBLER REPAIRS APPROVED BY SRM 53-05 FIG. 106 AND 117 PER REPAIR SCHEME PROVIDED VIA TIMCO REO-A00288 REV. IR DATED 10 OCT 04. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20041230000152004123000015WP 2004 12 30 WX0400045 120041028A323310281375001 ACTUATOR DOUG DC9 DC982 3022082WP NLG FAILED A WX0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP19864GA 49912 AFTER TAKEOFF FROM PIA EN ROUTE TO LAS, CREW REPORTED NOSE GEAR WOULD NOT RETRACT PROPERLY. AIRCRAFT RETURNED TO PIA , CREW PERFORMED NORMAL OVERWEIGHT LANDING UNDER THE FOLLOWING CONDITIONS; SINK RATE 256 TO 300 FEET PER MINUTE, NO SIDE LOADS, LANDING WEIGHT 144,800 LBS. CONTRACT MX ACCOMPLISHED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-04 WITH NO DEFECTS FOUND. MX REMOVED NOSE GEAR HYDRAULIC RESTRICTORS, CLEANED, INSPECTED AND FLOW CHECKED FOR TROUBLESHOOTING. RESTRICTORS OPERATIONALLY GOOD IAW MM 32-60-00. RESTRICTORS REINSTALLED. AIRCRAFT FERRIED TO GYR. MX REMOVED AND REPLACED NLG ACTUATOR IAW MM 32-32-06. UNIT LEAK CHECKED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20041230000222004123000022NM 2004 12 30 2004UALA01152 120041124A1430D62562 BOLT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NLG MISALIGNED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29806UA 788 AFTER DIFFICULTY RAISING GEAR HANDLE, GEAR DID NOT INDICATE RETRACTED. LOUD AIR NOISE FURTHER INDICATED THAT GEAR WAS NOT UP. MLG SHOCK ABSORBER MESSAGE DISPLAYED. AIRCRAFT ARRIVED WITH LARGE AMOUNT OF ICE ON NLG AND SENSORS. CFDS SHOWS NLG FAULTS. CLEANED LARGE AMOUNT OF ICE AND SNOW OFF SENSOR AREA. LOOSENED AND REALIGNED BOLT D62562 TO REALIGN SENSOR TARGET LEVERS. 2L72 4F4 FRTA28NM E40NE 20041230000232004123000023SO 2004 12 30 SWIA200414167 120041201A3350D36604001 BATTERY EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT DISCHARGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07188SW464 464 120039 FORWARD PORTION OF EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. REPLACED FORWARD EMERGENCY LIGHT BATTERY, OPERAIONAL CHECK GOOD. 2L72 4T RTA31SO 20041230000312004123000031CE 2004 12 30 GLBA20030759 120041115A2120 ODOR BEECH 1900 1900D 1154162CE CABIN DETECTED A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM03245GL UE245 CREW DETECTED STRONG ODOR IN CABIN AND PACK REPORTED SMOKE IN SEAT 2A. REMOVED FLOOR BOARDS INSP PCD'S, FWD VENT BLOWER AND RUN A/C, NO DEFECTS NOTED. 2L72 4T RTA24CE 20041230000352004123000035SO 2004 12 30 RAIA00410027 120041029A26130132AFU2 SENSOR EMB 145 EMB145LR 3260212SO NR 3 TEMP MALFUNCTIONED A RAIAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE03847HK199 14500857 8052 - IAD - BRAKE TEMP NR 3 OVERHEAT INDICATION. MAINTENANCE DEFERRED NR 3 BRAKE TEMP SYSTEM AND SUBSEQUENTLY CLEARED THE DEFERRAL BY REMOVING AND REPLACING THE NR 3 TEMP SENSOR. 2L72 4T RTT00011AT 20041230000392004123000039NM 2004 12 30 QXEA200400791 120041118A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - LEFT HAND OUTBOARD FLAP HAS A SIX FOOT LONG BY TWO INCH WIDE CHAFING MARK ON THE UPPER SURFACE STARTING AT THE INBOARD EDGE WHERE THE FLAP SITS BETWEEN 0 AND 5 DEGREES. REPAIRED IAW RD 8/4-57-016, ISS 7. 2H72 4T RTA13NM 20041230000482004123000048EU 2004 12 30 04FDEA03376 120041206A5410 FAIRING AIRBUS310 A310 EU NR 2 PYLON DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK, 003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. PYLON NR 2, LOWER AFTER FAIRING WITH INTERIM REPAIR ON OUTER SKIN SURFACE LT AT AFT AREA. REPAIRED IAW EA 6-5480-81814. 2L72 4F RTA35EU 20041230000492004123000049EU 2004 12 30 04FDEA03377 120041206A5754 SKIN AIRBUS310 A310 EU KRUEGER FLAP DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK, NR 003 ENT BY: 067708, PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. LEFT WING, KRUEGER FLAP OUTER SURFACE FOUND DENTED. REPAIRED IAW EA 6-5750-81817. 2L72 4F RTA35EU 20041230000542004123000054EA 2004 12 30 QXEA200400834 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL, TOP SURFACE AND LUG HOLE AREAS AT FS 752-761, FS 785-797, FS 803-828. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20041230000632004123000063EU 2004 12 30 DHL200436311 120041205A3240 BRAKE AIRBUS300 A300B4203 3930306EU AUTO BRAKE SYS MALFUNCTIONED A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01363DH 85 ON REJECT, AUTO BRAKES DIDN'T ENGAGE UNTIL BRAKES APPLIED WITH PEDALS. ALSO, DID NOT DISENGAGE WITH PEDAL PRESSURE. DEFERRED AUTO BRAKES AS PER MEL 32-42-07. CAT "C". TRANSFERED TO DMI LOG. CONTROL NR 18696 EMP 8662. 2L72 4F RTA35EU 20041230000782004123000078NM 2004 12 30 04FDEA03282 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230000862004123000086WP 2004 12 30 04FDEA03265 120041129A5753ARC0613502 PANEL DOUG MD10 MD1010F 3022112WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 RIGHT WING PANEL ARC0613-502, UPPER TRAILING EDGE PANEL AT INBOARD END OF OUTBOARD FLAP DELAMINATED. RIGHT WING PANEL ARC0613-502 REPAIRED BY FABRICATING AND BONDING NEW OUTER SKINS, DOUBLER AND CORE IAW TPS 1001 REV E, DAC DWG ARC0613 AND FEDEX EA 8-5710-81523, WINGS, RIGHT HAND UPPER WING PANEL ASSEMBLY. REPAIR, INSTALLED PANEL IAW DC10 SRM 51-31-01 VOL 2. REFERENCE NON-ROUTINE N00723. 2L73 4F RTA22WE 20041230000882004123000088WP 2004 12 30 04FDEA03267 120041130A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 470-475 LONGERON 30 RIGHT TO 30 LEFT, NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE INSPECTION REQUIREMENTS. REMOVED EXISTING REPAIR. REPLACED DOUBLER PER DC10 SRM 53-20-00 VOL 1, FIGURE 6, SHEET 15. REFERENCE NON-ROUTINE N01169. 2L73 4F RTA22WE 20041230000902004123000090WP 2004 12 30 ASMF200411012 120041129A29107912643570 PIPE DOUG DC9 DC987 3022087WP HYD SYSTEM DAMAGED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23216AM 49586 DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN RIGHT FLIGHT INTERIOR SPOILER. HYDRAULIC PRESSURE LINE WAS DETECTED WITH DAMAGES AND WAS REPLACED IAW MM 27-62-02, TEST CORRECT. 2L72 4F RTA6WE 20041230000972004123000097WP 2004 12 30 DHL2004804005 120041105A2611327 BULB DOUG DC8 DC873F 302199FWP SMOKE DETECTOR INOPERATIVE A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01804DH 46124 NR 8 SMOKE DETECTER INOP. DEF PER MEL 26-6-1 PLACARD INSTALLED DMI NR 18370. REFER TO DMI 18370. NR 8 POSITITON SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 8 SMOKE DETECTOR AND OPS CHECKED GOOD AS PER MM 26-10-5. THIS CLEARS DMI 18370. (BULB P/N 327). 2L74 4F RT4A25 20041230000982004123000098EA 2004 12 30 SWIA200414229 120041206A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07912SW 7595 EMERGENCY EXIT LIGHT BULBS OUT ON GALLEY DOOR. REPLACED LIGHT BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041230001032004123000103NM 2004 12 30 2004UALA01162 120041126A5315 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29670UA17696 29240 STATION 246 FLOORBEAM AT APPROX LBL 2, STIFFENER IS CRACKED. REPLACED STIFFENER. 2L72 4F4 FRTA1NM E24NE 20041230001112004123000111CE 2004 12 30 4029 120041201A3233232710021 ACTUATOR LEAR 35 35LEAR 5170600CE GARRTTTFE731TFE73122B 01518WP MLG LEAKING E BSYAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL07130F 978 044 P74101 ON APPROACH INTO MKC, SELECTED GEAR DOWN ONLY, THE TWO MAINS CAME DOWN AND LOCKED, DIVERTED TO MCI AIRPORT USED EMERGENCY AIR TO BLOW GEAR DOWN LANDED NO PROBLEMS. MAINTENANCE SERVICED HYD RESERVOIR AND BLED SYSTEM. FERRIED A/C TO MKC MAINTENANCE FOUND LEFT GEAR ACTUATOR LEAKING, REMOVED AND REPLACED ACTUATOR OPS. CHECKS GOOD, CYCLED GEAR SIX TIMES RELEASED FOR SERVICE 2L72 4F4 F A10CE E6WE 20041230001122004123000112NM 2004 12 30 QXEA200400858 120041201A5321 FLOORBOARD BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - CARGO TRACK HAS ONE SPOT OF CORROSION ON OUTBOARD FLOOR BOARD FLANGE AROUND THE SCREW HOLE AT STATION X776. REPAIRED IAW HORIZON AIR EA 6-53-478 AND RD 8/4-53-1091. 2H72 4T RTA13NM 20041230001212004123000121WP 2004 12 30 DHL2004809011 120041204A335023661001 BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH 46047 DURING PREFLIGHT DURING BATTERY TEST, BATTERY AT 10 VOLTS AND EMERG LIGHTS DID NOT ILLUMINATE. REMOVE AND REPLACE MAIN SHIPS BATTERY. OPS CK GOOD IAW M/M 33-50-2, EMERG LIGHTS CK GOOD AND M/M 24-30-1. 2L74 4F RT4A25 20041230001252004123000125EU 2004 12 30 AWXA200401374 120041112A5320D5311209120300 FLOOR SUPPORT AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK EXFOLIATION, CORROSION WAS FOUND ON BEAM -Y765, FORWARD SIDE OF FS 18 TO FS 20. MAINTENANCE REMOVED CORRODED BEAM -Y765, FROM FS 12 TO FS 24; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A320 SRM 53-11-15, FIG 203. 2L72 4F RTA28NM 20041230001382004123000138NM 2004 12 30 04FDEA03296 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77986. 2L73 4F RTA22WE 20041230001532004123000153WP 2004 12 30 04FDEA03340 120041203A5312 BULKHEAD DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT STA 1701 X = 32.0 EXISTING REPAIR ON BULKHEAD AND DAMAGED CAUSE CHAIN. REMOVE EXISTING REPAIRS AT X=30 AND DISCART THEN. PERFORM VISUAL INSP FOR CRACKS AND DAMAGED AREA. IF GAUGES ARE FOUND, BLEND OUT AREAS IAW SRM 53-00-01 FIG 18. REPORT BACK WITH FINDING. REPLACE P/N: AFA0043-3 QTY:1. 2L73 4F A22WE 20041230001602004123000160EU 2004 12 30 04FDEA03349 120041205A5753 SKIN AIRBUS310 A310 EU RT WING TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. RT WING REPAIR RT INBD FLAP LWR SURFACE. REPAIRED IAW EA 6-5750-81812. 2L72 4F RTA35EU 20041230001642004123000164WP 2004 12 30 04FDEA03231 120041126A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND CORROSION ON LWR SKIN BTW FRAMES 1168/1334 AND STRG 46L/49R. REMOVE CORROSION PER SRM 52-21-01 PAGE 28. CHECK LIMIT PER SRM 53-40-00 FIG 14 (OUT LIMITS). REPLACE SKIN PER DWG NYB 6008 P/N 6008-27. 2L73 4F A22WE 20050103000012005010300001WP 2005 1 3 AALA20041246 120041225A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21403A 49314 DEN - AFT ACCY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT ACCY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050103000072005010300007NM 2005 1 3 ABXA040400 120041205A3213161T11383 BEARING BOEING767 767281 1385109NM RT MLG SEIZED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23773AX 22788 RIGHT MAIN LANDING GEAR INNER BEARING RACE SEIZED TO AXLE. AXLE CHROME MISSING. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR FORWARD AXLE BEARING ASSEMBLY IAW DC-9 MM. 2L72 4F RTA1NM 20050103000092005010300009NM 2005 1 3 ABXA040402 120041222A2150 A/C PACK BOEING767 767231 1385131NM A/C BAY MALFUNCTIONED A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23702AX 22566 EMERGENCY DECLARED. AIR DIVERSION FROM ILN TO ORD, FLIGHT 1408. RIGHT PACK INOP AND PACK OFF LIGHT ILLUMINATED. EICAS MESSAGE'S RIGHT PACK OFF AND RIGHT PACK TEMP DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN STANDBY SELECTED OR WHEN PACK SELECTED OFF. INSPECTED RIGHT PACK FLOW CONTROL AND SHUT-OFF VALVE. INSPECTED AND CLEARED CANNON PLUG FOR SHUT-OFF VALVE. NO DEFECTS NOTED. PERFORMED OPS CHECK OF RIGHT PACK SYSTEM. OPS CHECKED GOOD. SUSPECT ICE IN INLET DOOR. NO FAULTS. PLACARD REMOVED. 2L72 4F RTA1NM 20050103000142005010300014NM 2005 1 3 AWXA200401437 120041205A534769403522 GALLEY TRACK BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY OUTBOARD TRACK AT BS 294, RBL 42, WL 208.5. MAINTENANCE REMOVED CORRODED FORWARD GALLEY OUTBOARD TRACK AT BS 294, RBL 42; FABRICATED A NEW REPLACEMENT TRACK PER DWG 69-40352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-04 FIG 1. 2L72 4F RTA16WE 20050103000232005010300023NM 2005 1 3 AWXA200401456 120041211A532065C105924 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER OUTBOARD LEG BETWEEN BS 950 AND BS 960, RBL 46, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT RBL 46, FROM BS 950 TO BS 960; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050103000392005010300039NM 2005 1 3 AWXA200401433 120041223A3097 WIRE BOEING737 7373G7 1384595NM COCKPIT PINCHED A AWXAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28309AW 24711 ONT - DIVERSION / SMOKE - FLT 0282 - EN ROUTE FROM PHX TO SJC THE CAPTAINS SLIDING WINDOW OVERHEATED AND BEGAN TO ARC AND SMOKE. THE CREW DISCONNECTED THE WINDOW HEAT CONNECTOR AND DIVERTED INTO ONT. ISSUED MEL 30-11 LT SIDE WINDOW HEAT INOP. WHEN AIRCRAFT ARRIVED IN LAS MAINTENANCE REPAIRED PINCHED WIRE AND RE-PINNED WINDOW HEAT CONNECTOR AT LT SLIDING WINDOW IAW SPM 20-00, OPERATIONAL TEST WAS GOOD IAW T/C A1B30003. 2L72 4F RTA16WE 20050103000422005010300042EU 2005 1 3 AWXA200401428 120041222A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28656AW19978 1079 PHX - EEL - DURING 4-DAY CHECK, FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM FOUND THE AFT SECTION EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT AFT EMERGENCY POWER SUPPLY UNIT (13WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050103000502005010300050NM 2005 1 3 AWXA200401387 120041129A5320693535011 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT FORWARD SIDE OF BS 500C, STR 26 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500C, STR 26 RT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35350; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 & 12. 2L72 4F RTA16WE 20050103000662005010300066SO 2005 1 3 C2XA04SH571 120041208A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713124 145689 DURING C-CHECK THE LEFT HAND OMEGA SHAPE WAS FOUND TO BE CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20050103000692005010300069SO 2005 1 3 C2XA04IA165 120041213A335074441 LIGHT EMB 145 EMB145ER 3260211SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713936 145025 IAH - FLIGHT 2474, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE ROW THREE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050103000752005010300075 2005 1 3 CALA0400703 420041105A2330RDAA201304 ENTERTAIN SYS BOEING767 767224 1385170NM CABIN MALFUNCTIONED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2776151 30430 STRONG FUMES WITH A BURNING WIRE-LIKE ODOR WERE NOTED IN THE FIRST CLASS CABIN (FORWARD IN AREA OF ENTERTAINMENT SECTION) AFTER APPROXIMATELY 3 HOURS OF FLIGHT WHILE EN ROUTE TO EWR. THE ENTERTAINMENT SYSTEMS WERE SECURED AND THE ODOR CLEARED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE NOTED THAT THE NR 1 EADB (ENHANCED AREA DISTRIBUTION BOX) SMELLED BURNT. THE NR 1 EADB WAS REMOVED AND REPLACED. THE IFE FILTER WAS CHECKED AND IT WAS NOT CLOGGED. OPERATIONAL CHECKS WERE GOOD. THE IFE SYSTEM WAS RUN FOR 30 MINUTES AND OPERATION CHECKED GOOD. 2L72 4F RTA1NM 20050103000772005010300077EA 2005 1 3 COMA0460596 120041104A5210601R31998312 SKIN PANEL CNDAIR CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA26218 7031 7031 DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH BOMBARDIER REO 601R-52-11-578. OK FOR RETURN TO SERVICE. 2L72 4F RTA21EA 20050103000812005010300081EA 2005 1 3 COMA0460680 120041212A323210811003 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA NLG DOOR MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01966CA21344 7132 FLIGHT 5527 NOSE LANDING GEAR DOORS OPEN MESSAGE. REPLACED THE NLG DOORS ACTUATOR. 2L72 4F RTA21EA 20050103000832005010300083EA 2005 1 3 COMA0460685 120041215A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01988CA 7204 LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 11 AND 12. REPAIRED IAW EO 53-027. 2L72 4F RTA21EA 20050103000882005010300088EA 2005 1 3 COMA0460677 120041213A2750855D1009 BPSU CNDAIRCL600 CL6002B19 1900309EA FLAP MALFUNCTIONED A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01735CA137618993 7267 FLIGHT 4964 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20050103000912005010300091NM 2005 1 3 DL738041092 120041209A3350D71701100 FUSE BOEING737 737832 13844CFNM BATTERY CHARGER BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO273749D 30490 ON L/O FOUND EMERGENCY LIGHTS AT SEAT ROW 22D AFT INOP. SWAPPED BATTERY PACK, NO HELP. FOUND AFT RT POWER SUPPLY BAD. REMOVED POWER SUPPLY AND BATTERY PACK. BATTERY CHARGER HAS A BAD FUSE. REPLACED FUSE REF M/M. REPLACED BATTERY AND REINSTALLED CHARGER. TEST GOOD. 2L72 4F RTA16WE 20050103001032005010300103NM 2005 1 3 DL73S041116 120041215A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 INSPECTION OF THE STRINGER 4L SKIN LAP JOINT REVEALED A CRACK AT FS 411. THE CRACK WAS REMOVED WITH A 7 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095530-14AD. 2L72 4F RTA16WE 20050103001112005010300111NM 2005 1 3 DXTA200400495 120041225A3240 WARNING LIGHT AMD FALC50FALCON2000 2730170NM COCKPIT ILLUMINATED E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07222QS 122 AFTER LOWERING GEAR A -BRAKE- YELLOW LIGHT WAS SEEN. PERFORMED CHECKLIST, LANDED WITH -BRAKE- YELLOW LIGHT ON. AFTER LOWERING GEAR A -BRAKE PRESS- YELLOW LIGHT WAS NOTICED. IN THE COURSE OF A FEW MINUTES LIGHT EXTINGUISHED BY ITSELF. ITEM IS UNDER INVESTIGATION. 2K73 4F RTA50NM 20050103001212005010300121WP 2005 1 3 04FDEA03183 120041123A5420 ADAPTER DOUG DC10 DC1010 3022110WP NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND NR 2 PYLON JOINT PANEL INTERAL SIDE WITH CRACK. REPLACED ADAPTER RING: ATL7029-91, ATL7029-87, ATL7029-89. 2L73 4F A22WE 20050103001232005010300123WP 2005 1 3 04FDEA03184 120041123A5500 PANEL DOUG DC10 DC1010 3022110WP EMPENNAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND BY ULTRASONIC INSPECTION 1 PANEL P/N ALC7438-2 (19 POSITION) CRACKED. REPLACED PANEL PER SB 55-16 FIG 20 GROUP 1 (KIT SB10550016-57). 2L73 4F A22WE 20050103001242005010300124NM 2005 1 3 04FDEA03228 120041125A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 45L. REMOVED AS PER SRM 51-33-01 VOL II. FABRICATED NEW SPLICE AS PER DWG A5A7116 AND INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050103001252005010300125WP 2005 1 3 04FDEA03421 120041216A5754ARB1766501 RIB DOUG DC10 DC1010 3022110WP L/E SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND AT LT SLAT NR 5 OUTBOARD SIDE, RIB WITH HOLES IN RADIUS ANGLE. REPLACE RIB ASSY PER SRM 51-35-01 PAGE 1-12 SRM 51-35-02 PAGE 3-9. P/N ARB1766-501. 2L73 4F A22WE 20050103001262005010300126NM 2005 1 3 04FDEA03428 120041216A5320 CHANNEL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, HAT SECTION CORRODED AT STA 1875 TO STA 1887, RBL 36. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050103001272005010300127NM 2005 1 3 04FDEA03400 120041209A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), STOP BOLT ATTACHMENT, BARREL NUT BORE FOUND CORRODED. CORROSION REMOVED BY HAND-CLEAN AS PER CMM 20-11- 01. 2L73 4F RTA22WE 20050103001282005010300128NM 2005 1 3 04FDEA03401 120041209A5330 SKIN BOEING727 727100 1384036NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 COMPLY WITH EO 7-5330-7-2319 PART 5 BS 441 AT STR 19-20 RT AND STR 20-21 RT. *S/D* REPAIRED FUSE SKIN BS 441 STR 19-21 RT IAW EO 7-5330-7-2319 AND EA 7-5330-82513. 2L73 4F RTA3WE 20050103001312005010300131NM 2005 1 3 04FDEA03451 120041220A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 CTR CARGO - STA Y1806 STR34L LONGERON CRACKED. CRACKED LONGERON CUT AND REMOVED BETWEEN STA Y= 1791 TO Y= 1810 PER SRM 53-10-00 VOLUME I, FIGURE 1. LONGERON SPLICE FABRICATED PER DWG AFA7736. SPLICE FITTING AND NEW LONGERON INSTALLED PER SRM 53-10-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050103001322005010300132EU 2005 1 3 04FDEA03468 120041222A3340 CIRCUIT BREAKER AIRBUS310 A310203 3930313EU LIGHT MALFUNCTIONED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO25402FE 201 DURING FLT, HEARD CRACKING & ARCING SOUND COMING FROM REAR OF COCKPIT (CB PANEL), FOLLOWED BY ACRID ELECTRICAL ODOR. DONNED O2 & DIVERTED INTO MCO. NO APPARENT EQUIP PROBLEMS DURING APPROACH & LANDING. LANDED 18R MCO UNEVENTFULLY. FOUND LANDING GEAR AND AIR COND COMPARTMENT DOME LIGHT C/B POPPED AND WOULD NOT RESET. CYCLED A/C COMPARTMENT DOME SWITCH TO OFF AND THEN C/B RESET. PULLED AND COLLARED C/B. MEL 33-45-01. ALL WHEEL WELL DOME LIGHT(S) INOP. REMOVED AND REPLACED CIRCUIT BREAKER 4LM, AND SWITCH 33LS PER AWM 33-37-01 AND AWM 33-35-01 RESPECTIVLEY. PERFORMED SATISFACTORY OPERATIONAL CHECK OF A/C BAY AND LANDING GEAR BAY LIGHTING PER AMM 33-32-00-5. 2L72 4F RTA35EU 20050103001332005010300133NM 2005 1 3 04FDEA03494 120041228A5320 STRUCTURE DOUG MD11 MD11 3023602NM CENTER CARGO BAYBROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO FLOOR STRUCTURE BROKEN AT STA 1701 LBL 32. REPAIRED AS PER SRM 53-00-01 VOL I FIG 7 SHEET 7, REPAIR ANGLE AND FILLER FABRICATED AS PER SRM 53-00-01 FIG 7 SHEET 7 VOL I AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050103001362005010300136WP 2005 1 3 04FDEA03483 120041225A3234 SWITCH DOUG MD10 MD1010F 3022112WP COCKPIT FAULTY A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25385FE 46619 ON APPROACH TO LAND, LOWERED LANDING GEAR AND DID NOT GET DOWN AND LOCKED ON ANY GEAR JUST 3 RED INDICATIONS. GRABBED GEAR HANDLE AND CHECKED FOR LOCKED DOWN HANDLE, THEN JIGGLE HANDLE, NO HELP. CYCLED LANDING GEAR AND AGAIN GOT 3 RED INDICATIONS. HYDRAULICS WERE GOOD, CHECKED HANDLE FOR SECURITY AND STILL NO GREEN LIGHTS (EITHER SD OR LIGHTS). HIT THE HANDLE HARD WITH FIST AND INSTANTLY GOT 3 GREEN INDICATION. REMOVED AND REPLACED S1-431 LANDING GEAR HANDLE SWITCH, OPS CHECKS OK PER MM 32-31-02-2 AND SUPP 32-60-00-0 PAR 11. 2L73 4F RTA22WE 20050103001372005010300137EU 2005 1 3 04FDEA03484 120041224A7830 THRUST REVERSER AIRBUS300 A300F4605R 3930327EU NR 2 MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25684FE 802 REJECTED TAKEOFF AT 80 KIAS AFTER RECEIVING AMBER ECAM REV 2 PRESS MEL 24DEC04. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. R&R DPV AND PRESS SW LEAK AND OP CHKS GOOD PER E.O. 7830-7-3316B. 2L72 4F RTA35EU 20050103001382005010300138NM 2005 1 3 04FDEA03470 120041222A783049B1613000069 TRACK DOUG MD11 MD11 3023602NM NR 2 T/R CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 ENGINE NR 2 RIGHT HAND THRUST REVERSER UPPER SLIDER TRACK AFT EDGE FOUND CRACKED AND WORN. THRUST REVERSER REPLACED AS PER WORK CARD NR 78T3902-R. 2L73 4F RTA22WE 20050103001402005010300140WP 2005 1 3 04FDEA03472 120041219A5320AEA00246 INTERCOSTAL DOUG DC10 DC1030 3023501WP RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25309FE 48298 EXCESSIVE CORROSION ON INTERCOSTAL IN RIGHT WHEEL WELL, AFT BULKHEAD AT LONGERON 36. REMOVED AND REPLACED INTERCOSTAL. 2L73 4F A22WE 20050103001412005010300141WP 2005 1 3 04FDEA03473 120041219A5320AEA00256 INTERCOSTAL DOUG DC10 DC1030 3023501WP RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25309FE 48298 CORROSION ON INTERCOSTAL IN RIGHT WHEEL WELL AT AFT BULKHEAD. REMOVED AND REPLACED INTERCOSTAL. 2L73 4F A22WE 20050103001432005010300143WP 2005 1 3 04FDEA03410 120041214A3234 SELECTOR VALVE DOUG DC10 DC1030F 3023504WP LANDING GEAR LEAKING A FDEAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25316FE 48314 SHORTLY AFTER LEVEL OFF GOT LEVEL 1 ALERT HYD 3 ELEV OFF, NOTED THAT HYD 3 QUANTITY WAS DECREASING AT 2.5 GALS. HSC SHUTOFF NR 3 HYD. HYD 3 OFF LEVEL 1 ALERT. AFTER SLATS EXTENDED ON APPROACH, HYD 3 RESTORED. REMAINING FLUID LEAKED OUT, HYD 3 FAILED. GEAR EXTENDED MANUALLY. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE GEAR UP PRESSURE PORT O-RING, PER STD MAINT PRACTICE. NO LEAKS NOTED WITH GEAR HANDLE UP OR DOWN. SERVICED NR 3 HYD SYS TO 7.5 GALS. OK FOR SERVICE. 2L73 4F RTA22WE 20050103001472005010300147NM 2005 1 3 04FDEA03478 120041223A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1544 TO STA 5-93. 2L73 4F RTA22WE 20050103001482005010300148NM 2005 1 3 04FDEA03479 120041223A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 77 CORRODED AT STA 1841 TO STA 1887. CORRODED SEAT TRACK REMOVED AS PER SRM 53-70-00. FABRICATED REPAIR SEAT TRACK AND SPLICE AS PER FIG 1 & FIG 7 OF SRM 53-70-00 AND INSTALLED AS PER SRM 51-31-01& 53-70-00. 2L73 4F RTA22WE 20050103001492005010300149NM 2005 1 3 04FDEA03480 120041223A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 1310 TO STA 1361. REMOVED AS PER SRM 51-31-01. 2L73 4F RTA22WE 20050103001502005010300150NM 2005 1 3 04FDEA03485 120041226A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 STA Y=832 TO 919 RIGHT HAND NR 3 SEAT TRACK AREAS FOUND WITH CORROSION. REPIARED IAW SRM 53-70-00 FIG 1 VOL I. 2L73 4F RTA22WE 20050103001512005010300151NM 2005 1 3 04FDEA03486 120041227A5511 SPAR CAP DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 HORIZONTAL STABILIZER RIGHT HAND UPPER FORWARD SPAR CAP NR 1R BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2L73 4F RTA22WE 20050103001542005010300154NM 2005 1 3 04FDEA03452 120041220A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 CTR CARGO - STA Y1541 STR36L LONGERON SPLICE CRACKED. SPLICE REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED PER DWG A5A7114 AND PART MARKED PER GMM 7-0-1001. NEW LONGERON SPLICE INSTALLED PER SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050103001562005010300156WP 2005 1 3 04FDEA03454 120041221A3240 VALVE DOUG MD10 MD1010F 3022112WP LT PARKING BRAKEMALFUNCTIONED A FDEAO OTHER J WARNING INDICATION DEDESCENT 1 SO25377FE 47965 AFTER GEAR EXTENSION, RECEIVED LVL 2 LT ANTI SKID FAIL. EXECUTED GO-AROUND, FOLLOWED QRH PROCEDURES. ALERT MOMENTARILY EXTINGUISHED AFTER CYCLING ANTI SKID SWITCH, BUT RE-APPEARED ON NEXT GEAR EXTENSION. HISTORY OF SAME PROBLEM. T/S PER FIM 32-40-08 & M/M 32-45-01-5. REMOVED AND REPLACED LEFT PARKING BRAKE VALVE ACTUATOR PER M/M 32-45-05-2. 2L73 4F RTA22WE 20050103001572005010300157WP 2005 1 3 04FDEA03455 120041221A3260 PROXIMITY SENSOR DOUG DC10 DC1010 3022110WP RT MLG CONTAMINATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25366FE 46602 UNSAFE INDICATION IN RIGHT MAIN LANDING GEAR LIGHT AFTER RAISING GEAR HANDLE ON TAKEOFF. MAINTAINED AIRSPEED, RAN QRH PROCEDURE, LIGHT WENT OUT AFTER CYCLING THE GEAR HANDLE. AIRCRAFT HAD REQUIRED DE-ICING AT MHT DUE TO SNOW STORM OVER THE PREVIOUS 24 HOUR. INSPECTED RT MLG PROXIMITY SENSORS AND FOUND TO BE COATED WITH DE-ICE FLUID. CLEANED PROX SENSORS ON RT MLG IAW SMP. PERFORMED BITE CHECK ON PROXIMITY ELECTRONICS UNIT IAW MM 32-61-01 WITH NO FAULTS NOTED, OK FOR SERVICE. 2L73 4F A22WE 20050103001592005010300159NM 2005 1 3 04FDEA03457 120041221A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 CENTER CARGO - BILGE AREA AT STA Y=1711 - 49L LONGERON AT SPLICE AREA FOUND CRACKED. CRACKED LONGERON SPLICED AND REMOVED PER 53-10-00 VOLUME I, FIGURE 1. NEW LONGERON FABRICATED SRM 51-33-01 VOLUME II AND INSTALLED PER SRM 53-10-00 VOLUME I, FIGURE 1. 2L73 4F RTA22WE 20050103001612005010300161NM 2005 1 3 SB04165 120041212A33503114981 REFLECTOR BOEING737 7374B7 1384702NM EXTERIOR FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19430US 24552 PIT - MAINTENANCE REPORTED THE AFT SERVICE DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050103001692005010300169NM 2005 1 3 USAA040895 120041011A5320 TIE CLIP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 663 STRINGER 2 RT. FABRICATED NEW CLIP IAW DWG 69-45156 IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20050103001702005010300170NM 2005 1 3 USAA040858 120041019A5720 BRACKET BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 BRACKET, 1 INCH CRACK, LT WING SPAR (AFT) STA 218, MFG NEW BRACKET IAW J020-37-20. 2L72 4F4 FRTA16WE E2GL 20050103001722005010300172NM 2005 1 3 USAA040916 120041029A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - FRAME, .2500 INCH CRACK, BS 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR IAW TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E21EU 20050103001742005010300174NM 2005 1 3 USAA040924 120041103A5347 TRACK BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - TIE DOWN TRACK, CORROSION AND CRACK, 2 INCH BY 4 INCH AREA AND 1 INCH CRACK. CORROSION; LEVEL 1: TASK NR C 53-208-01, BS 727F, S 26L. CUT OUT DAMAGED SECTION AND SPLICED IN NEW IAW SRM 53-00-53, FIG 202. 2L72 4F4 FRTA16WE E21EU 20050103001752005010300175NM 2005 1 3 USAA040894 120041215A5320 TIE CLIP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 500B, STR 13,LT. FABRICATED IAW MFG DWG 69-45156 AND INSTALLED IAW SRM 51-40-02. 2L72 4F4 FRTA16WE E21EU 20050103001762005010300176NM 2005 1 3 USAA040901 120041026A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN, 1.5 INCH CRACK, FWD SERVICE DOOR CUTOUT AFT LOWER CORNER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-01. 2L72 4F4 FRTA16WE E21EU 20050103001772005010300177NM 2005 1 3 USAA040907 120041021A5320 TIE CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 -CLIP, .1250 INCH CRACK FROM RIVET AT FRAME STA 663.75, STR S10L. REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-10-2, 51-40-03 AND MFG DWG 65-46541. 2L72 4F4 FRTA16WE E21EU 20050103001832005010300183EU 2005 1 3 SA04113 120041207A5610NP1653116 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAO OTHER O OTHER DEDESCENT 1 EA19738US13687 1254 PUJ FLT 799 EN ROUTE CLT TO PUJ, THE F/O'S WINDSHIELD CRACKED ON DESCENT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CRACKED WINDSHIELD. OK FOR SERVICE. 2L72 4F RTA28NM 20050104000012005010400001EU 2005 1 4 ASOA04881 120041104A5330 SKIN AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27635AS 372 DURING HANGAR MAINTENANCE, THE FUSELAGE SKIN AT THE T/E OF THE AFT EQUIPMENT COMPARTMENT ACCESS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE FUSELAGE SKIN AT THE T/E OF THE AFT EQUIPMENT COMPARTMENT ACCESS BY STOP DRILLING THE CRACKS IAW SRM 51-25-06. THE PERMANENT REPAIR IS TO BE PERFORMED WITHIN 50 FLIGHTS, IAW SRM 53-81-04, FIG 301, ZONE D. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO72-53-0159. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000022005010400002EU 2005 1 4 ASOA04935 120041110A5320 ANGLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE ANGLE AT FS 28 WING TO FUSELAGE ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE AT FS 28 WING TO FUSELAGE ON THE RT SIDE IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20050104000072005010400007EU 2005 1 4 ASOA04934 120041104A5753 BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE T/E FLAP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE BRACKET AT THE LEFT FLAP BEAM ACTUATOR (IB FLAP) WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE BRACKET AT THE LT FLAP BEAM ACTUATOR (IB FLAP) IAW SRM 51-25-02 AND 51-25-01. 2H72 4T4 TRTA53EU E20NE 20050104000082005010400008EA 2005 1 4 ASOA04938 120041116A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27825AS 7207 DURING A C-CHECK, THE PASSENGER DOOR TOP STEP FORWARD IB CORNER WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP IAW MM 52-11. 2L72 4F4 FRTA21EA E15NE 20050104000092005010400009EU 2005 1 4 ASOA04928 120041102A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE RT SEAT TRACK BETWEEN FRAMES 39 AND 40 WERE FOUND TO BE CORRODED BEYOND LIMITS IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT IAW SRM 51-25-04. 2H72 4T4 TRTA53EU E20NE 20050104000132005010400013EA 2005 1 4 ASOA04942 120041124A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000152005010400015EA 2005 1 4 ASOA04896 120041112A36107C14 CLAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE BLEED AIR SYS LOOSE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27852AS 7369 DURING CLIMB-OUT, AT APPROXIMATELY 25,000 FT, THE CREW RECEIVED AT RIGHT 14TH DUCT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND THE RT ENGINE THRUST LEVER BROUGHT BACK TO IDLE FOLLOWED BY THE WARNING MESSAGE EXTINGUISHING. AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT DIVERTING, MAKING A SINGLE ENGINE LANDING SAFELY. MAINTENANCE FOUND SEVERAL CLAMPS LOOSE ON THE AFT RT 14TH STAGE DUCT FUSELAGE BLEED LOOP AND RESECURED THE LOOPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000162005010400016EA 2005 1 4 ASOA04939 120041123A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27867AS 7463 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000182005010400018EU 2005 1 4 ASOA04930 120041102A5720 HOUSING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT WING CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE FLANGE HOUSING AT 522CT. MAINTENANCE REPAIRED THE CORRODED FLANGE HOUSING ON THE RT WING IAW SRM 57-14-12. 2H72 4T4 TRTA53EU E20NE 20050104000202005010400020EU 2005 1 4 ASOA04879 120041103A33503012000 BATTERY PACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS163503065 383 DURING A GROUND INSPECTION, THE FORWARD HALF OF THE EMERGENCY FLOOR STRIP LIGHTING WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT 61WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000212005010400021EU 2005 1 4 ASOA04917 120041119A33503011052 COVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE EXIT SIGN CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27534AS 463 DURING A GROUNG INSPECTION, THE EMERGENCY EXIT SIGN AT ROW 1-C/D WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN COVER AT ROW 1-C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000252005010400025EA 2005 1 4 ASOA04887 120041106A5260601R31980 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27916EV 7757 DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000262005010400026EA 2005 1 4 ASOA04885 120041105A3350100865 CHARGER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27859AS23 23 7421 DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS BATTERY PACK CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000302005010400030EU 2005 1 4 ASOA04866 120041005A5420 STRUCTURE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE LT ENGINE LOWER NACELLE, FORWARD UPPER RT EDGING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE LOWER NACELLE, UPPER EDGING ON THE RT SIDE IAW SRM 51-25-03. 2H72 4T4 TRTA53EU E20NE 20050104000332005010400033EA 2005 1 4 ASOA04915 120041119A335058728 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN FAULTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHTS WERE FOUND FLICKERING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT TRACK BETWEEN ROWS 2 TO 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000342005010400034EU 2005 1 4 ASOA04931 120041102A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 338 DURING C-CHECK INSPECTION, ON THE RT SEAT TRACK BETWEEN FRAMES 38 AND 39 CORROSION WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-25-04. 2H72 4T4 TRTA53EU E20NE 20050104000372005010400037NE 2005 1 4 ASOA04908 220041117A72616087T04P06 SCAVENGE PUMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE COKED A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27824AS114455 7203 872517 DURING CLIMB-OUT, AT APPROXIMATELY 31,800 FT, THE CREW RECEIVED AN ENGINE OIL PRESSURE MASTER WARNING AND AURAL. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE LUBE SCAVENGE PUMP AND ALSO THE OIL PRESSURE TRANSDUCER IAW AMM 79-20-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000392005010400039EA 2005 1 4 ASOA04891 120041108A215078279015 ACM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE A/C BAY MALFUNCTIONED A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27909EV6325 7658 DURING DESCENT, AT APPROXIMATELY 11,000 FEET, THE CREW NOTICED A STRONG BURNING SMELL IN THE COCKPIT AND CABIN WITH THE LT PACK GOING TO FULL HOT WHICH BECAME UNCONTROLLABLE IN EITHER AUTOMATIC OR MANUAL MODES. AN AUTOMATIC SHUTDOWN OF THE PACK OCCURRED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AIR CYCLE MACHINE AND ALSO THE COMPRESSOR DISCHARGE OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000402005010400040EU 2005 1 4 ASOA04919 120041102A5320 FLOOR SUPPORT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE T-FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 WAS FOUND TO BE CORRODED BEYOND LIMITS AT THE LT STR 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED T-FLOOR SUPPORT IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041229001952004122900195WP 2004 12 29 04FDEA03180 120041122A5754 SLAT TRACK DOUG DC10 DC1010 3022110WP LT WING WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO2510060 46970 LT WING FIXED L/E WORN FROM NR 1 SLAT TRACK INBD TO FUSELAGE IN SEVERAL PLACES, CAUSED FROM NR 1 SLAT LWR LIP. CUT OUT DAMAGED AREA FAB REPAIR DOUBLER PER SRM 57-10-00 FIG 40. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 PAGE 129 FIG 40. N/R 64 GENERATED TO SUPPLEMENT ORIGINAL N/R 47. DISCREPANCY REPAIR ACCOMPLISHED ON LT FIXED L/E EXCEEDS SRM 57-10-00 FIG 40 LIMITS IN AREA ADJACENT TO NR 1 SLAT TRACK CUT OUT ON INBD SIDE. FABRICATED (1) REPAIR SKIN FROM .040 CLAD 7075-T6; AND FABRICATED(1) REPAIR DOUBLER FROM .025 301 1/2 HD S.S. INSTALLED REPAIR IN REF TO SRM 57-10-00 VOL1 FIG 39 REPAIR 4 AND REF SRM 57-10-00 VOL 1 FIG 40. 2L73 4F A22WE 20041230000032004123000003NE 2004 12 30 NACA20040055 220041102A8530356993 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 2 BURNED A NACAE ENGINE SHUTDOWN KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL036174C3 3 44075 P33708 NR 4 ENGINE SHUT DOWN DUE TO LOSS OF OIL AND DOUBLE SHORTED SECONDARY NR 2 CYLINDER. TEMPORARY INSTALLED NEW NR 2 CYLINDER ON NR 4 ENGINE FOR FERRY FLIGHT. 2L74 4R4 R 6A3 5E8 20041230000322004123000032SO 2004 12 30 SWIA200414196 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 CORROSION DETECTED BY PILOT AND COPILOT SEAT RAILS, FRAME 13 AND FWD, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT CORROSION AND ASSESSED IAW EMB 120 SRM 53-00-00 AND 53-10-10; MATERIAL LOSS = .003 WITHIN LIMITS IAW EMB SRM. 2L72 4T RTA31SO 20041230000332004123000033SO 2004 12 30 SWIA200414197 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO COCKPIT CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 EVIDENCE OF CORROSION UNDERNEATH PILOT'S INBOARD TRACK, ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION AND FOUND IT TO BE WITHIN LIMITS WITH A MAX MATL. LOSS OF 0.003" IAW EMB 120 SRM 53-20-10. 2L72 4T RTA31SO 20041230000362004123000036WP 2004 12 30 04FDEA03272 120041130A5330AGA31081 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 1957 TO 1993 LONGERON 49 LEFT TO 49 RIGHT NEED ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVE DATA AND REPETITIVE INSPECTION REQUIREMENT. CUT AND REMOVE SKIN IAW EA8-5330-83838. REMOVED CORROSION FROM LONGERON AND FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-10-01 VOL 1. FABRICATED AND INSTALLED SKIN, SPLICE, 2 EACH DOUBLERS, AND LONGERON SPLICE REPAIR FITTINGS IAW DC10 SRM 53-20-00 VOL 1, 51-31-01VOL 2, 51-35-01 VOL 2, AND FEDEX EA 8-5330-83838, FUSELAGE, SKIN SPLICE IN AREA OF ART LAV PAN, REPAIR. REFERENCE NON-ROUTINE N01183. 2L73 4F RTA22WE 20041230000512004123000051NM 2004 12 30 04FDEA03405 120041211A2170 COALESCER BAG DOUG MD11 MD11 3023602NM A/C PACK DIRTY A FDEAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO25583FE 48421 DURING CRUISE FLT AT FL300 250KTS, HAD WHITE SMOKE OMITTING FROM TOP OF GLARESHIELD. REF QRH SMOKE FUMES OF ELECT, AIR COND OR UNKNOWN REASONS, DECLARED EMERG WITH VHHH AND EXPEDITED TO A LANDING AT VHHH. SMOKE DISSIPATED BY LANDING CREW VERBAL NOT ELECT BURN, JUST SMELL OILY AND ACFT ALL SYSTEM WORK NORM. INSP AV COMPT & ALL DU'S INST PNL AREA, ALL WIRING NO DISCREPANCY. INSP ALL 3 PACK'S COALESCER BAG FOUND NR 3 HAS SLIGHT OILY SMELL. PERF AIR COND ODOR DIST DUCT CLEANING PER MM 21-53-00-7.RR ALL 3 COALESCER BAG'S PER 21-54-05-2.C/W THE MTSI INSP ALL 3 ENG 8TH STAGE CHECK VALVE & APU LBV DUCTING NO WET SIGN PER 36-11-01-4 & 36- 16-02. PRECAUTIONARY DEF NR 3 PACK PER MEL 21-51-01-A. ACFT OK FOR SERVICE. 2L73 4F RTA22WE 20041230000582004123000058SW 2004 12 30 ALGA098103 120040216A6410206016201131 BLADE BELL 206 206B3 1181506SW TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032201W675 3477 INSPECTED FOR SKIN CRACKS AND TRAILING EDGE OF BALANCE WEIGHT C/W ASB206L-04-127 REVB PT3. 1G71 3U H2SW 20041230000612004123000061SO 2004 12 30 SWIA200414209 120041101A5310 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 BUTT STRAP AT Y479.00L FROM FRAME 30-34 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB SRM 120 51-40-02, 51-25-00. 2L72 4T RTA31SO 20041230000702004123000070WP 2004 12 30 UPS04843570 120041124A5730575178439 DOUBLER DOUG DC8 DC871F 302199DWP RT LE AUX TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 RT WING L/E INTERNAL DOUBLER (AUX TANK) CRACKED AT STA.182.502. FABRICATED REPAIR DOUBLER FROM SHT7075T6/0.125 AND INSTALLED SAME PER SAA SK744-520, SRM 51-1-8, 51-1-26, 51-1-20D. 2L74 4F RT4A25 20041230000732004123000073CE 2004 12 30 DJFA2004035 120041122A1420 PIN CESSNA500 560CESSNA 2076750CE CONNECTOR LOOSE E DJFAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 EA23525CW 5600225 AFTER T/O AT 10,000 FT & CLIMBING AT 2,000 FT/MIN, NOTICED FLT MGMT SYS DID NOT RECORD T/O TIME & FELT A CABIN PRESS BUMP AROUND 22,000 FT. N1 RECOMENDATION WINDOW NOT WORKING. CABIN BEGAN TO RISE RAPIDLY WHEN 10,000 FT LIGHT CAME ON. DONNED O2 MASK & EMERG DESCENT BEGAN. GEAR EXTENDED FOR LANDING CLOCKS BEGAN TO WORK NORMALLY. A/C RETURNED TO PBI W/O FURTHER INCIDENT. MX REPLACED & ADJUSTED LT SQUAT SWITCH. SQUAT SWITCH WIRING & PRINTED CIRCUIT BOARD CHECKED, NO DEFECTS NOTED. GEAR SWING CHECK GOOD. PROBLEM REOCCURED ALONG WITH MLG HANDLE BEING LOCKED IN DOWN POSITION. SOCKET PIN ON CONNECTOR BACK SHELL FOUND LOOSE. LOOSE SOCKET PIN RESECURED. MLG OPS CHECK GOOD. A/C RETURNED TO SERVICE. 2L72 4F RTA22CE 20041230000852004123000085WP 2004 12 30 ABXA040385 120041126A3260 WARNING LIGHT DOUG DC9 DC932 3022066WP MLG ILLUMINATED A ABXAO OTHER J WARNING INDICATION DEDESCENT 1 GL23982AX 47317 NOSE LANDING GEAR LIGHT WAS NOT ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR, LIGHT CAME ON. INSPECTED NOSE LANDING GEAR WIRING FOR CONTINUITY & PIN ENGAGEMENT AT SWITCH CONNECTORS. INSPECTED SWITCHES FOR SECURITY AND OPERATION. CYCLED NOSE LANDING GEAR 10 TIMES, ALL POSITION & WARNING INDICATIONS WERE IMMEDIATE & NORMAL PER DC9 MM 32-60-00. 2L72 4F A6WE 20041230001062004123000106NM 2004 12 30 04FDEA03274 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230001102004123000110NM 2004 12 30 04FDEA03277 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230001152004123000115SO 2004 12 30 CHQA000589 120041202A3350 LIGHT EMB 135 EMB135LR 3260305SO EMERGENCY EXIT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11843 145599 RIGHT HAND EMERGENCY OVERWING EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT HAND OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20041230001192004123000119EU 2004 12 30 DHL2004363013 120041205A3150 WARNING SYSTEM AIRBUS300 A300B4203 3930306EU COCKPIT ACTIVATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01363DH 85 T/O REJECTED DUE TO CONTINUOUS CHIME. NOTED CAB PRESSURE LIGHT FLICKER. REPLACED SEQUENCE BOX . SYS TESTS OK PER 21-31-00. 2L72 4F RTA35EU 20041230001302004123000130 2004 12 30 66269 420041029A2210 YAW DAMPER BEECH 1900 1900D 1154162CE RUDDER MALFUNCTIONED A AMWAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE07126YV UE126 YAW DAMPER ENGAGED ON TAKEOFF ROLL, CREW ABORTED TAKEOFF GOT AND YAW DAMPER/RUDDER BOOST FAIL ANNUN WHEN TAXIING. RETURNED TO GATE AND THE SYSTEM WAS DEFERRED WITH NO FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND YAW DAMPER OPS CK NORMAL. 2L72 4T RTA24CE 20041230001362004123000136NM 2004 12 30 AWXA200401351 120041103A5310 SHEAR TIE BOEING737 7373Y0 1384671NM CORRODED CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AND BEAR STRAP IN AFT BILGE AREA BS 967, BL "0". MAINTENANCE REMOVED SHEAR TIE AND AFTER CLEANING OFF CORROSION FOUND NO MATERIAL LOSS. TRIMMED OUT CORRODED AREA OF BEAR STRAP AT BS 967, BL "0"; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW E.R. 03-5300-04328-SS1. 2L72 4F RTA16WE 20041230001402004123000140NM 2004 12 30 04FDEA03298 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230001462004123000146NM 2004 12 30 DHL2004780007 120041118A5250 HANDLE BOEING727 727223 1384074NM COCKPIT DOOR SEPARATED A DHLAO OTHER O OTHER CRCRUISE 1 SO01780DH 22006 COCKPIT DOOR HANDLE FELL OFF. REINSTALLED COCKPIT DOOR HANDLE IAW B727 MM 52-50-0, OPS CHECKS GOOD. 2L73 4F A3WE 20041230001552004123000155WP 2004 12 30 04FDEA03341 120041203A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DENTED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND DENT ON EXTERNAL SKIN BETWEEN STA 304 TO STA 330 RT SIDE LONG 33 TO LONG 36. REPLACE PANEL SKIN ABA 7049U4 PER DWG ABA7049/SRM 51-35-01 GAG 1/13 51-33-01 PAGE 34/47. REPLACE P/N: ABA 7049U4 , BN 330-428-4. 2L73 4F A22WE 20041230001572004123000157NE 2004 12 30 COMA0460662 220041204A75329799982 BLEED VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01506CA1990 7793 FLIGHT 5861- RT 10TH STAGE BLEED VALVE FAILED IN THE OPEN POSITION. REPLACED THE 10TH STAGE VALVE. 2L72 4F4 FRTA21EA E15NE 20041230001622004123000162 2004 12 30 P9RA20040054 420041211A2565387 BULB BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11521NA 25592 IN MAINTENANCE LAS, SLIDE ARM LIGHTS AT R2 AND R3 DOORS INOPERATIVE. RELAMPED EMERGENCY SLIDE ARM LIGHTS IAW MM. 2L72 4F RTA2NM 20050103000182005010300018NM 2005 1 3 AWXA200401418 120041215A531465621257 KEELBEAM BOEING737 737301 1384611NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28324AW 23261 MCN - MAJOR REPAIR - DURING INSPECTION PHX MAINTENANCE FOUND A 3 INCH CRACK IN LT PACK BAY FORWARD END KEEL BEAM AT BS 540, CRACK RUNS HORIZONTALLY THROUGH MACHINED STEP. AIRCRAFT WAS MAINTENANCE FERRIED TO MCN FOR REPAIR. CUTOUT DAMAGED SECTION OF KEEL BEAM AT LBL 6 FROM BS 500A TO BS 540.6. PERFORMED AN HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST. FABRICATED A NEW REPLACEMENT SECTION OF KEEL BEAM, 2 EACH ANGLES, AND 3 EACH FILLERS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-12, FIG 203. 2L72 4F RTA16WE 20050103000192005010300019EU 2005 1 3 AWXA200401419 120041221A3250664700500A4D CONTROL UNIT AIRBUS320 A320231 3930325EU NR 1 FAULTY A AWXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP28628AW11371 67 ON SHORT FINAL AFTER MLG SELECTED DOWN, RECEIVED NLG STEERING FAULT, ABORTED APPROACH & FLEW BY TOWER. CYCLED ANTI-SKID & NLG STEERING SWITCH & FAULT CLEARED, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT SYS, BITE CODES INDICATED INTERNAL FAULT IN MLG CONTROL INTERFACE UNIT NR 1. R/R LGCIU NR 1 (D197) IAW AMM, OPS CHECK GOOD. FUNCTIONAL TEST OF LGCIU COULD NOT DUPLICATE REASON FOR REMOVAL, UNIT WAS INSPECTED AND SUBJECTED TO EXTENSIVE TESTING PER CMM, RETURNED TO SERVICE AS NFF. 2L72 4F RTA28NM 20050103000202005010300020NM 2005 1 3 AWXA200401415 120041209A53206547955533 DOUBLER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW 24711 MCN - MAJOR REPAIR - DURING C-15 CHECK EXFOLIATION CORROSION WAS FOUND ON INNER DOUBLER AT BS 807 BETWEEN STR 26 RT AND STR 27 RT. MAINTENANCE CUTOUT LOWER ANGLE AND BEAR STRAP ON FRAME AT BS 807 BETWEEN STR 26 RT AND STR 27 RT, FABRICATED A FRAME FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW ER 03-5300-04353-HF1. 2L72 4F RTA16WE 20050103000212005010300021NM 2005 1 3 AWXA200401454 120041228A3350110049 CHARGER BOEING757 757225 1384959NM CABIN FAULTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28914AW 22208 PHX - EEL - DURING A-06 CHECK THE L-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY CHARGER (M733) AT BS 705, LBL 46, AND EMERGENCY EXIT SIGN AT L-2 DOOR; OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050103000272005010300027NM 2005 1 3 AWXA200401459 120041208A5315654681192 FLOORBEAM BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND AT FASTENER HOLES ON FLOORBEAM AT BS 986 BETWEEN RBL 25 AND RBL 60. MAINTENANCE REMOVED CORRODED FLOORBEAM AT BS 986 FROM RBL 25 TO RBL 60; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW B7373-300 SRM 51-40-02, FIG 1 & 12. 2L72 4F RTA16WE 20050103000312005010300031NM 2005 1 3 AWXA200401450 120041211A532065C334191 SHEAR WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON LT AFT LAVATORY SUBFLOOR (SHEAR WEB), BETWEEN BS 1018 AND BS 1029, LBL 1 AND LBL 37, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 1018 TO BS 1029, LBL 1 TO LBL 37; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65C33419; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 9 & 10. 2L72 4F RTA16WE 20050103000432005010300043NM 2005 1 3 AWXA200401461 120041227A532069353526 TIE CLIP BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN AFT GALLEY STRINGER TIE CLIP AT BS 907, STR 2 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 907, STR 2 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B7373-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050103000482005010300048NM 2005 1 3 AWXA200401443 120041207A5311655287864 FRAME BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON L-2 DOOR ENTRY WAY INNER CHORD BETWEEN BS 963 AND BS 991, LBL 52, WL 209. MAINTENANCE REMOVED CORRODED INNER CHORD FROM BS 963 TO BS 991, LBL 52; FABRICATED A NEW REPLACEMENT INNER CHORD PER DWG 65-52878; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050103000532005010300053EU 2005 1 3 AWXA200401391 120041213A7920MS9388143 SEAL AIRBUS320 A320232 3930326EU NR 2 ENGINE LEAKING A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28649AW 803 ON CLIMBOUT OF PHX EN ROUTE TO DTW THE NR 2 ENGINE OIL QUANTITY INDICATED ZERO, OIL PRESSURE AND OIL TEMERATURE INDICATED NORMAL, TURNED BACK TO PHX FOR REPAIR, SHUTDOWN ENGINE DURING TAXI BACK TO GATE. MAINTENANCE INSPECTED NR 2 ENGINE AND FOUND DE-OILER LEAKING FROM SEALS, REPLACED DE-OILER SEALS AND RAN ENGINE, NO LEAKS WERE NOTED. OIL QUANTITY AFTER LANDING WAS 5 QUARTS, SERVICED 18 QUARTS OF OIL. 2L72 4F RTA28NM 20050103000572005010300057EU 2005 1 3 AWXA200401395 120041213A561066642870 WINDSHIELD AIRBUS320 A320232 3930326EU COCKPIT CRACKED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28603AW206732007 661 AFTER DEPARTING PHX EN ROUTE TO SEA THE CAPTAINS WINDSHIELD SHATTERED, DIVERTED INTO LAS FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW AMM 56-11-11, AND WINDOW HEAT COMPUTER NR 1 IAW AMM , OPS CHECK GOOD. TEST OF WINDOW HEAT COMPUTER COULD NOT VERIFY REASON FOR REMOVAL. MEMORY ALARM "561000 WINDSHIELD" CLEARED AND A FULL FUNCTIONAL TEST WAS PERFORMED WITH NO FAULTS NOTED, UNIT RETURNED TO SERVICE IAW CMM. VENDOR WAS NOT ASKED TO PERFORM A FAILURE ANALYSIS OF WINDSHIELD DUE TO AGE AND FLT HOURS ACCRUED. WINDSHIELD FAILURE APPEARS TO BE SIMILAR TO OTHER RECENT FAILURES THAT EXHIBITED SIGNS OF WATER INGRESSION. 2L72 4F RTA28NM 20050103000612005010300061NM 2005 1 3 AWXA200401444 120041205A53205093266 FITTING BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON L-1 DOOR OPENING ON THE FUSELAGE TORQUE TUBES LOWER FITTING UPPER SURFACE AT BOLT HOLE BS 294, STR 13 LT. MAINTENANCE REMOVED CORRODED FUSELAGE TORQUE TUBES LOWER FITTING AT BS 294, STR 13 LT; FABRICATED A NEW REPLACEMENT FITTING PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 8 & 12. 2L72 4F RTA16WE 20050103000702005010300070NM 2005 1 3 C7WA200400051 120040922A5313 STRINGER BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO178887Z 21856 STR 27 RT CORRODED STA 620. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED STRINGER REPAIR IAW SRM 53-10-4 FIG 1, DETAIL 2. 2L73 4F4 F A3WE E2EA 20050103000712005010300071NM 2005 1 3 C7WA200400064 120041102A3230 LANDING GEAR BOEING737 737231 1384079NM PWA JT8 JT8D* NE NLG LACK OF LUBE A C7WAO OTHER J WARNING INDICATION APAPPROACH 1 SO1724343 21630 NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. RED NOSE GEAR UNSAFE LIGHT ON. MANUALLY LOWERED NOSE LANDING GEAR IAW AOM VOL 1. INSPECTED NOSE GEAR ACTUATOR, LOCKING ACTUATOR AND LINKAGE NO DAMAGE NOTED. LUBRICATED NOSE GEAR TRUNNIONS, ACTUATOR AND DRAG BRACE AS NEEDED. PERFORMED EXTENSION AND RETRACTION CHECK OF NOSE LANDING GEAR INCLUDING EMERGENCY EXTENSION IAW MM 32-33-00 AND 32-33-11. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA16WE E2EA 20050103000722005010300072NE 2005 1 3 C7WA200400040 220041007A7510652673831 DUCT BOEING727 727200 138407ENM PWA JT8 JT8D7B 52053NE NR 2 ENGINE BROKEN A C7WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17902PG 20725 AIR RETURN, INTERMITTENT FIRE WARNING LIGHT ON NR 2 ENGINE AFTER TAKEOFF. FOUND NR 2 ENGINE Y-DUCT BROKEN. REMOVED AND REPLACED NR 2 ENGINE ANTI-ICE DUCT. 2L73 4F4 FRTA3WE E2EA 20050103000782005010300078EA 2005 1 3 COMA0460681 120041211A30106243843 SENSOR CNDAIRCL600 CL6002B19 1900309EA LT WING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01977CA4777 7157 FLIGHT 5097 LEFT WING ANTI-ICE CAUTION MESSAGE DURING T/O. REPLACED THE OVERHEAT SENSOR. 2L72 4F RTA21EA 20050103000862005010300086EA 2005 1 3 COMA0460684 120041215A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01988CA 7204 RIGHT HAND FUSELAGE 718.00 CRACKED AT 2 LOCATIONS BETWEEN STRINGERS 10 AND 12. REPAIRED IAW EO 53-027. 2L72 4F RTA21EA 20050103000872005010300087EA 2005 1 3 COMA0460687 120041216A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01431CA 7472 RIGHT HAND 621.00 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050103000942005010300094NM 2005 1 3 DL76L041097 120041214A2530251050045 CHILLER BOEING767 767332 1382001NM FWD GALLEY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27195DN 28452 STRONG ELECTRICAL ODOR IN FWD CABIN AREA. ISOLATED COMPONENTS AND FOUND FWD GALLEY CHILLER TO BE THE CAUSE. REPLACED SAME. 2L72 4F RTA1NM 20050103001002005010300100NM 2005 1 3 DL73S041105 120041215A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 NUMEROUS SKIN CRACKS FOUND ALONG STRINGER 4L BETWEEN STATION 540 AND 727. REPAIRED IAW ERA 095481-14AD. 2L72 4F RTA16WE 20050103001012005010300101NM 2005 1 3 DLM88041106 120041215A3320F30T12SP41RS LIGHT DOUG MD88 MD88 3023688NM CABIN DAMAGED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27968DL 53161 AS PAX DEPLANED AN ELECTRICAL ODOR WAS NOTICED IN CABIN. FOUND BURNED FLUORESCENT TUBE HOLDER AT 11DE. REPLACED SAME. 2L72 4F RTA6WE 20050103001042005010300104NM 2005 1 3 DL73S041117 120041215A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 INSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK AT FS 380. THE CRACK WAS REMOVED WITH A 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095527-14AD. 2L72 4F RTA16WE 20050103001182005010300118WP 2005 1 3 04FDEA03364 120041206A5240 ACCESS PANEL DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND EXISTING REPAIR FWD OF MID LAVATORY ACCESS PANEL AT 6 O'CLOCK APPROX STA 770. STRAP INSTALLED PER SRM 53-00-01 FIG 4 SHEET 2. 2L73 4F A22WE 20050103001342005010300134NM 2005 1 3 04FDEA02979 120041022A5753ARC7490501 TEE FITTING DOUG MD11 MD11 3023602NM FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING BORES FOUND CORROSION ARE NOT WITHIN EO LIMITS. TEE FITTING REPLACED AS PER AMM27-50-22 AND OPERATIONAL TEST CARRIED OUT AS PER AMM 27-50-00. 2L73 4F RTA22WE 20050103001352005010300135WP 2005 1 3 04FDEA03482 120041224A3260 PROXIMITY SENSOR DOUG MD10 MD1010F 3022112WP LT MLG OUT OF ADJUST A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25391FE 46625 AFTER T/O RAISED LANDING GEAR, BOTH PRI AND SEC IND SHOWED LT GEAR NOT UP AND LOCKED. NOTED NO UNUSUAL VIB OR CONT INPUT. C/W QRH AND LOWERED THEN RAISED LANDING GEAR. ALL IND WERE LEFT MAIN GEAR NOT UP AND LOCKED. DECIDED TO RETURN TO RAMP. CTR GAVE US A RT TURN AND ALL IND SHOWED UP AND LOCKED. JACKED A/C IN REF TO MD10-10 M/M 07-10-00-0. FOUND GAP AT LT MLG UPLOCK LATCH PROX TO TARGET NOT WITHIN LIMITS. ADJ SHIMS AS REQ TO OBTAIN GAP REF MD-10-10 AMM 32-61-15-4. AS PRECAUTION REMOVED AND REPLACED PSEU IN REF MD-10-10 AMM 31-71-01-2. PERF ADJ TEST OF PROX TARGETS AND TARGETS REF MM 32-61-15-5. ALL TEST PASSED. COMPLETED SEVERAL NORMAL GEAR RETRACTIONS WITH NO DEFECTS NOTED. 2L73 4F RTA22WE 20050103001452005010300145NM 2005 1 3 04FDEA03476 120041223A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1391 TO STA 1471. REPAIRED SEAT TRACK & SPLICE FABRICATED AS PER SRM 53-70-00. 2L73 4F RTA22WE 20050103001532005010300153NM 2005 1 3 04FDEA03488 120041227A5320 CLIP DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 AFT FUSELAGE COMPARTMENT - DOG HOUSE CANT STA Y=2092.88 FRAME CLIP P/N AJC7028-11, CRACKED. REPLACED AS PER SRM 51-35-01 VOL2. 2L73 4F RTA22WE 20050103001632005010300163NM 2005 1 3 USAA040919 120041105A5320 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - T-ANGLE, 3 INCH BY 4 INCH AREA CRACKED AND PULLED. OUTBD SLING ATTACH POINT. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20050103001662005010300166NM 2005 1 3 USAA040854 120041030A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME, .3750 INCH CRACK, STA 540 BETWEEN RT IB SEAT TRACK, RBL 24.75 AND CRT FLOOR SUPPORT BEAM BL 0. DEFECTIVE PART, REPLACED WITH IDENT PN IAW MFG DWG 65-46819. 2L72 4F4 FRTA16WE E2GL 20050103001712005010300171NM 2005 1 3 USAA040917 120041029A5320 INTERCOSTAL BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - MOUNT/INTERCOSTAL WITH 2 INCH CRACK AND 2 INCH BY 4 INCH CORRODED AREA, BS 727D TO BS 727E AT S 28L. REMOVED CORROSION, TREATED AND PRIMED. REPLACED INTERCOSTAL MOUNT IAW SRM 51-10-2. 2L72 4F4 FRTA16WE E21EU 20050103001732005010300173NM 2005 1 3 USAA040918 120041022A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - FRAME, 2 INCH BY 1.5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-101-01, FRAME OUTER CHORD BS 227.8, WL 208.1 AND 2 INCH. REMOVED CORROSION, TREATED AND PRIMED, REINSTALLED FASTENERS IAW SRM 51-40-03. 2L72 4F4 FRTA16WE E21EU 20050103001792005010300179NM 2005 1 3 USAA040951 120041123A5755654645170A SPOILER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SPOILER, 4 BY 6 INCH AREA, DELAMINATION. REMOVED AND REPLACED SPOILER IAW MM 27-62-91. 2L72 4F4 FRTA16WE E21EU 20050103001812005010300181NM 2005 1 3 USAA040950 120041025A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN, .025 INCH DEEP AND AT 10 INCHES LONG, GOUGED, STA 887-867, STR 1. CUT OUT DAMAGE INSTALLED SHIMS, FILLERS, STRAPS, DOUBLER AND TRIPLER IAW EA 79291. 2L72 4F4 FRTA16WE E21EU 20050104000042005010400004EA 2005 1 4 ASOA04872 120041102A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT LB0 WAS FOUND TO BE CRACKED UNDER THE FIRE LOOP BRACKET BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 600-53-0072. 2L72 4F4 FRTA21EA E15NE 20050104000102005010400010EU 2005 1 4 ASOA04933 120041104A5753 BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE T/E FLAP CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE OMEGA BRACKET ON THE RT IB FLAP, OB ARM WAS FOUND TO BE CRACKED BEYOND LIMITS. 2H72 4T4 TRTA53EU E20NE 20050104000172005010400017EA 2005 1 4 ASOA04937 120041121A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR STUCK A ASOAK NONE O OTHER ININSP/MAINT 1 SO27855AS 7395 DURING A GROUND INSPECTION, THE OUTSIDE HANDLE TO THE PASSENGER DOOR WOULD NOT COME OUT MAKING IT DIFFICULT TO OPEN THE DOOR. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON THE PASSENGER DOOR. NO DEFECTS WERE NOTED. 2L72 4F4 FRTA21EA E15NE 20050104000292005010400029EA 2005 1 4 ASOA04874 120041103A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105. 2L72 4F4 FRTA21EA E15NE 20050104000312005010400031EU 2005 1 4 ASOA04918 120041102A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING A C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON A FLOORBEAM 36. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20050104000322005010400032EU 2005 1 4 ASOA04923 120041102A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE LT IB SEAT TRACK, CROWN AND FLANGE, BETWEEN FRAMES 38 AND 39 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACK IAW SRM 51-25-04 AND 51-21-42. 2H72 4T4 TRTA53EU E20NE 20050104000362005010400036EA 2005 1 4 ASOA04916 120041119A33508GH00247308 LIGHT CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF343B1 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27703EV 10038 DURING AN A-CHECK, THE RT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT AFT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000412005010400041EU 2005 1 4 ASOA04888 120041107A3350NSA936501TA2004 TERMINAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27533AS 460 DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY IN THE ARMED POSITION. MAINTENANCE RESECURED A LOOSE TERMINAL ON THE TWO MINUTE SWITCH AT THE AFT PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000442005010400044EA 2005 1 4 ASOA04905 120041116A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING C-CHECK, THE LT AND RT FS 625 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT FS625 CLIP. 2L72 4F4 FRTA21EA E15NE 20050104000452005010400045EU 2005 1 4 ASOA04889 120041107A33503012000 BATTERY PACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27640AS 53 405 DURING HANGAR MAINTENANCE, VARIOUS LIGHTS WERE FOUND INOPERATIVE ON THE EMERGENCY FLOOR LIGHT STRIP. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000462005010400046EU 2005 1 4 ASOA04894 120041110A3350E0029387 LIGHT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27532AS 458 DURING HANGER MAINTENANCE, THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE UPON DEPRESSING THE TWO MINUTE SWITCH BUTTON. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000482005010400048EA 2005 1 4 ASOA04870 120041101A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. 2L72 4F4 FRTA21EA E15NE 20050104000492005010400049EA 2005 1 4 ASOA04877 120041103A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE CLIPS AT FS280, RBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, RBL 9 IB AND OB. 2L72 4F4 FRTA21EA E15NE 20050104000522005010400052NM 2005 1 4 04FDEA03300 120041201A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PAGES 402-407, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.229, MAXIMUM ALLOWABLE DIAMETER=1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77985. 2L73 4F RTA22WE 20050104000582005010400058NM 2005 1 4 04FDEA03381 120041207A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA1-5750-78058, 2L73 4F RTA22WE 20050104000602005010400060NM 2005 1 4 04FDEA03383 120041207A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 FWD CARGO AT STA 979 LONGERON 51 IS CRACKED 2 INCHES. TRIMMED OUT AS PER SRM 53-10-00 VOL I. REWORKED NEW LONGERON AS PER DWG ADA8091 AND MACHINED REPAIR SPLICES AS PER SRM 53-10-00 VOL I. REPAIR PARTS INSTALLED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050104000612005010400061NM 2005 1 4 04FDEA03384 120041207A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON SPLICE FOUND CORRODED AT STA 1711 L49R. REMOVED AND REPLACED NEW SPLICE AS PER DWG AFA7102 AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050104000632005010400063NM 2005 1 4 04FDEA03391 120041207A5711 SPAR CAP DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, REAR SPAR AT APPROX XORS 1042 UPP CAP FOUND CORROSION. REPAIRED AS PER FEDEX EA 1-5710-81640. 2L73 4F RTA22WE 20050104000652005010400065WP 2005 1 4 04FDEA03216 120041125A5311 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND FWD AVIONIC COMPT AT STA 401 FRAME P/N ABA7104-67 AND ANGLE P/N 7104-69 WITH CORROSION. REPLACE FRAME AND ANGLE PER SRM 51-35-01 PAGE 1-12 AND SRM 51- 33-01 PAGE 33-47. 2L73 4F A22WE 20050104000682005010400068WP 2005 1 4 04FDEA03336 120041202A5753NRC6068513 SUPPORT DOUG DC10 DC1010 3022110WP LT FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 WING D-LT OUTBD FLAP-FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-55416. 2L73 4F A22WE 20050104000702005010400070WP 2005 1 4 04FDEA03193 120041123A5753ARC19842 HINGE DOUG MD10 MD1010F 3022112WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25388FE 46622 RIGHT WING OUTBOARD FLAP, INBOARD SUPPORT PIVOT ATTACH POINT INBOARD BUSHING CORRODED. FABRICATED OVERSIZE REPAIR BUSHING, FOUND OUT OF LIMITS. INSTALLED AND FINAL HONED OVERSIZE BUSHING IAW DAC CMM 57-52-02 AND FEDEX EA NR 8-5750-83939, WING-RIGHT HAND OUTBOARD FLAP, INBOARD HINGE BRACKET, OVERSIZE PIVOT BORES REPAIR. 2L73 4F RTA22WE 20050104000712005010400071NM 2005 1 4 04FDEA03234 120041126A5743 ATTACH FITTING BOEING727 72722 1384002NM WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25186FE 18872 MAIN FRAME MLG FWD TRUNNION ATTACH FITTING OVERSIZE HOLE REWORK C/W EA 7-5710-55408 ENT BY: 497236 RPT BY: 497236 FACT 26NOV04 15:03 COMPLIED WITH EA 7-5710-55408 HOLES OVERSIZED TO .875 AND REPAIR BUSHINGS INSTALLED RII:497228 ENT BY: 497236 RPT BY: 497236. 2L73 4F A3WE 20050104000722005010400072NM 2005 1 4 04FDEA03342 120041203A2612 CONTROL UNIT BOEING727 7272S2F 1384O81NM FIRE DETECTION MALFUNCTIONED A FDEAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SO25212FE 22934 IN DESCENT THROUGH FL200, THE NR 1 FIRE HANDLE LIGHT CAME ON INTERMITTENTLY. IN CONJUNCTION WITH THE FIRE HANDLE AND BELL, THE NR 1 ENGINE DETECTOR INOP LIGHT ILLUMINATED. RAN QRH FOR ENGINE FIRE AND SHUT THE NR 1 ENGINE DOWN. INSTALLED A NEW FIRE CONTROL UNIT PER AMM 26-11-000-4. TESTED PER AMM 26-11-000-1, OPS CHECK GOOD. INSTALLED A NEW MAIN OIL FILTER, NO METAL FOUND IN THE OLD FILTER. RAN THE ENGINE PER B-727-200 JRH, OPS AND LEAK CHECK GOOD. 2L73 4F A3WE 20050104000732005010400073NM 2005 1 4 04FDEA03150 120041117A5514ALC8104502 FITTING DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 15R EXCEEDED LIMITS. REFERENCE TO EO 1-5510-7-5000 C4 PT1, BARREL NUT NR 15R REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE REWORK/REPAIR - 1-5510-7-5000. 2L73 4F RTA22WE 20050104000742005010400074NM 2005 1 4 04FDEA03353 120041205A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050104000752005010400075NM 2005 1 4 04FDEA03359 120041206A5313 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON CORRODED 47L STA 1562. CARRIED OUT REPAIR AS PER SRM 53-10-00 VOL I FIG 1 AT CENTER CARGO LONGERON 47L AT STA 1562. 2L73 4F RTA22WE 20050104000792005010400079WP 2005 1 4 04FDEA03160 120041118A5753 ROLLER DOUG MD10 MD1010F 3022112WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT HAND INBOARD FLAP INBOARD FLAP TRACK AREA, LOWER FORWARD SMALL ROLLER PLATING WORN. REMOVED AND REPLACED LEFT HAND INBOARD FLAP INBOARD TRACK LOWER FORWARD SMALL ROLLER IAW FEDEX EA 8-5750-8513, WING INBOARD FLAP INBOARD ROLLER TORQUE REQUIREMENT, CLARIFICATION. REFERENCE NON-ROUTINE N00605. 2L73 4F RTA22WE 20050104000802005010400080WP 2005 1 4 04FDEA03270 120041130A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 REPAIR AT STATION 304 TO 328 LONGERON 26 LEFT AND 38 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIRS IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND REPETITIVE REQUIREMENTS. EVALUATED REPAIR IAW FEDEX EA 8-5330-83848, FUSELAGE, REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STATION 304-328 LONGERON 26L-38L- REPAIR. REPAIR IS MAJOR AND REPLACEMENT IS REQUIRED AT NEXT "C" CHECK IAW FEDEX EA 8-5330-83848. REFERENCE NON-ROUTINE N01166. 2L73 4F RTA22WE 20050104000812005010400081EU 2005 1 4 04FDEA03173 120041120A5730 SKIN AIRBUS310 A310 EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 RIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650KB HAS 1 EA ELONGATED SCREW HOLE AS MARKED AREA RIB 23 TO 24. COMPLIED WITH FED EX ENGINEERING AUTHORIZATION 6-5710-83632 (NOTE: MAJOR REPAIR PER EA ). 2L72 4F RTA35EU 20050104000822005010400082EU 2005 1 4 04FDEA03175 120041121A5347 SEAT TRACK AIRBUS310 A310 EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 LEFT SEAT TRACK NR 5 FROM FS 18 TO 21 BETWEEN FS 20 AND 21 HAS MATERIAL REMOVED OUT OF LIMITS, LOCATION B(65 INCHES) OTBD. REPAIRED BY REMOVING DAMAGED SECTION AND SPLICING IN A NEW SECTION IAW A310/200 SRM 53-10-16 FIG 208. 2L72 4F RTA35EU 20050104000842005010400084WP 2005 1 4 04FDEA03365 120041206A5330 SKIN DOUG DC10 DC1010 3022110WP FUSELAGE DAMAGED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND EXISTING REPAIR BTW STA 959-STA 979 ON BOTTOM SKIN AT 6 O' CLOCK FOR SUMP DRAIN VALVE. NO ACTION REQUIRED, THE DOUBLER IS INSTALLED PER SB 53-86. 2L73 4F A22WE 20050104000862005010400086NM 2005 1 4 04FDEA03362 120041206A5753 SKIN DOUG MD11 MD11 3023602NM FLAP VANE DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX EA 1575079794. 2L73 4F RTA22WE 20050104000872005010400087EU 2005 1 4 04FDEA03347 120041205A5753 SKIN AIRBUS310 A310 EU T/E FLAP ACTIVATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R. DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708. REPAIR RT INBD FLAP UPPER SURFACE ON INBD SIDE. INBOARD, REPAIRED IAW SRM 57--, FIG 202. OUTB, REPAIRED IAW EA 6-5750-81811. 2L72 4F RTA35EU 20050104000882005010400088EU 2005 1 4 04FDEA03344 120041205A54142210081152 SKIN AIRBUS310 A310 EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 PYLON LOWER SPAR, INSP FOR COMPLY WITH E.O. 6-5450-7-3302 REV NO. B3 POS PT3 ENT BY: 067708. NR 1 PYLON, LOWER AFT FAIRING WITH LOOSE RVTS, CRK'D AND PAINT IN BAD CONDITION. LOWER FAIRING REPAIRED IAW EA 6-5480-81814. REINSTALLED IAW AMM 54-55-00. PAINTED IAW SRM 51-75-10. 2L72 4F RTA35EU 20050104000892005010400089NM 2005 1 4 04FDEA03354 120041206A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050104000922005010400092WP 2005 1 4 04FDEA03370 120041206A5720 STRUCTURE DOUG DC10 DC1010 3022110WP RT WING BROKEN A FDEAK NONE O OTHER UKUNKNOWN 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON RT WING LWR SIDE XORS 309, B/T REAR SPAR AND HINGE FLAP, 5 EA TL WITH HEAD BROKEN AND 1 EA WITH HIGH SUSPECT CORROSION BELOW SKIN. REMOVE EAS TL WITH HEAD BROKEN PER SRM 51-34-01 PAG 1-7. PERFORM ULTRASONIC INSPECTION PER DPS 4.713 ON BELOW SKIN. REPAIR WING LWR SKIN PER EA 8-5710-701131, REPLACE SUPPORT ARB 2259-2 ARB 2259-502. INSTALLED HINGE FLAP PER MM 57-41-01 P/N: ARB 2259-2, ARB 2259-502, TLV110-5-24. 2L73 4F A22WE 20050104000932005010400093EU 2005 1 4 04FDEA03371 120041206A5753 STRUCTURE AIRBUS310 A310 EU T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R, DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708 LT WING, REPAIRS (2 EA) LT INBD FLAP T/E LOCATED ON EITHER SIDE OF INBD CANNOE. EXISTING COMPOSITE REPAIRS PERFORMED IAW EA 6-5500-50325, DATED 06/23/2000. REPAIRED IAW EA 6-5750-81810. 2L72 4F RTA35EU 20050104000942005010400094NM 2005 1 4 04FDEA03407 120041213A5320 ANGLE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, TEE ANGLE ON BULKHEAD STA 2007 CORRODED AT RBL 8. 2L73 4F RTA22WE 20050104000962005010400096WP 2005 1 4 04FDEA03412 120041214A5320 FITTING DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 CENTER ACCESSORY COMPARTMENT FUSELAGE STATION 1156 RIGHT HAND WING BOX FITTING IS CRACKED AT APPROX LONGERON 27 RIGHT. REMOVED INNER ATTACHED ANGLE IAW DC10 SRM 51-33-01 VOL 2, FABRICATED AND INSTALLED SPLICED ANLES AND FILLERS IAW DC10 SRM 53-30-00 VOL 1 FIGURE 7. REINSTALLED INNER ATTACH ANGLE IAW DC10 SRM 51- 33-01 VOL 2. REFERENCE NON-ROUTINE N00185. 2L73 4F A22WE 20050104000972005010400097NM 2005 1 4 04FDEA03413 120041214A5320 FITTING DOUG DC10 DC10 N/A-SDRNM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25395FE 46629 CENTER ACCESSORY COMPARTMENT AT FUSELAGE STATION 1156 LT WING BOX FITTING IS CRACKED. REMOVED INNER ATTACHED ANGLE IAW DC10 SRM 51-33-01 VIL 2, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW DC10 SRM 51-21-01 VOL 2 AND 53-30-00 VOL 1. REINSTALLED INNER ATTACH ANGLE IAW D10 SRM 51-33-01 VOL 2. REFERENCE NON-ROUTINE N00184 2L73 4F RTA22WE 20050104000982005010400098WP 2005 1 4 04FDEA03195 120041123A3260894601 PSEU DOUG MD10 MD1010F 3022112WP E/E BAY FAULTY A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 THE PSEU FAIL FAULT CODE INDICATES AN INTERNAL FAILURE WITHIN THE PSEU BOX BUT THE OEM COULD NOT LOCATE CAUSES OF THIS FAULT CODE. THIS EA WILL CAP AND STOW THE UNUSED PINS AT THE RACK, THUS COMPLETELY ELIMINATING THE WIRE AS AN EMT SOURCE. COMPLIED WITH EA NR 8-3260-81418, MD10 LANDING GEAR - LANDING GEAR POSITION INDICATION SYSTEM, ALTERATION REFERENCE NO - WRI - 32602959. 2L73 4F RTA22WE 20050104001042005010400104NM 2005 1 4 04FDEA03343 120041204A3411 LINE BOEING727 7272S2F 1384O81NM PITOT/STATIC SYSMISALIGNED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25210FE 22932 F/O'S A/S AND ALT LAG BEHIND CAPT'S. CAPT'S A/S AND ALT MATCH W/ STBY. ENT BY: 220542 FACT 05DEC04 08:44 MEM T/S AND FOUND SPARE STATIC FLEX LINE QUICK DISC BEHIND F/O'S INST PNL LEAKING. LINE IS LOOSE AND NOT CONNECTED TO ANY INSTRS. THE QUICK DISC WAS MISALIGNED, REF IPC 34-10-00 62A ITEM 15. EA TO CAP AND STOW THE PITOT AND STATIC LINES WHICH USED TO RUN TO THE MACH AIRSPEED IND ON THE F/O'S SIDE. C/W EA 7-3410- 84482. VERIFIED NO UNCONNECTED LINES ON THE CAPTS SIDE. PERFORMED A FULL RANGE PITOT STATIC LEAK TEST TO 22,500 FEET LEFT AT ALT FOR 20 MINUTES NO LEAKAGE NOTED. A/S WAS 350 KTS, REF B727-200 AMM 34-11-000-5. CK F/O'S INST'S ALL OK. 2L73 4F A3WE 20050104001052005010400105NM 2005 1 4 04FDEA03217 120041125A5280 STRUCTURE DOUG MD11 MD11 3023602NM LT MLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA OF STRUT FITTING. CRACK REPAIRED AS PER SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I. 2L73 4F RTA22WE 20050104001062005010400106NM 2005 1 4 04FDEA03218 120041125A5280 STRUCTURE DOUG MD11 MD11 3023602NM LT MLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT FORWARD OF STRUT FITTING NEAR HINGE AREA. CRACK REPAIRED AND REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I. 2L73 4F RTA22WE 20050104001072005010400107WP 2005 1 4 04FDEA03168 120041118A5280 DOOR DOUG MD10 MD1010F 3022112WP NLG VIBRATES A FDEAK NONE E VIBRATION/BUFFET CRCRUISE 1 SO25362FE 48261 14000 FT HEAVY VIBRATION SLOWED AND LANDED WITH NO PROBLEM, EVEN WITH GEAR DOWN HAD VIBRATION. "DECLARED EMERGENCY" HAD FIRE TRUCKS STANDING BY. REMOVED AND REPLACED LT NOSE GEAR DOOR PER MM 32-23-01-2. ACCOMLISHED GEAR SWING AND DOOR FIT CHECK PER EA 8-3220-84377 REV POS2 BY EMP NR EJO 476920 AND SOLD TO QA 275049, 11/20/04, JTK183086 RII:275049. 2L73 4F RTA22WE 20050104001082005010400108WP 2005 1 4 04FDEA03196 120041123A5320SR105300483 SILL DOUG MD10 MD1010F 3022112WP FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 FORWARD CARGO DOOR, DOOR SILL FORWARD STATION 899, LONGERON 42 R, SMALL TOP LIGHTNING HOLE, CORROSION INSIDE. FABRICATED AND INSTALLED -7 CHORD SECTION AND -7, -17, -19 INTERNAL AND EXTERNAL DOUBLERS IAW FEDEX DC10 SRM 51-31-01 VOL II, 51-21-01 VOL II, 53-00-01 VOL I, 53-50-00 VOL I AND FEDEX EA 8-5330-81532 FUSELAGE, FORWARD CARGO DOORWAY JAMB, SKIN DOUBLER, REPAIR. REFERENCE, NON-ROUTINE NO. N00318. 2L73 4F RTA22WE 20050104001112005010400111NM 2005 1 4 04FDEA03225 120041125A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 39L. REMOVED AS PER SRM 51-33-01 VOLUME II AND NEW LONGERON SPLICE INSTALLED AS PER SRM 51-33-01 VOLUME II, NEW LONGERON SPLICE MACHINED AS PER DWG A5A7114. FPI CARRIED OUT ON NEW LONGERON SPLICE AS PER DPS 4.707 AND FOUND NO CRACK EVIDENT. 2L73 4F RTA22WE 20050104001132005010400113NM 2005 1 4 04FDEA03227 120041125A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 45R. REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED NEW LONGERON SPLICE AS PER DRAWING A5A7116. FPI CARRIED OUT AS PER DPS 4.707 ON NEW LONGERON SPLICE AND FOUND NO CRACK EVIDENT. INSTALLED NEW LONGERON SPLICE AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050104001142005010400114NM 2005 1 4 04FDEA03236 120041127A79201800M18G01 TUBE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE NR 2 ENGINE BROKEN A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25609FE 48549 702750 DURING CRUISE AT F330 LEVEL 2, ALERT"ENG 2 OIL PRESS LOW" OBSERVED OIL PRESS READING 4 IN RED. ALSO, OBSERVED OIL QTY ZERO (0) ON ENG 2. COMPLIED WITH APPROPRIATE QRH PROCEDURES. AFTER SHUT DOWN N1 26.1 EGT 7 N2 22 .1 ENG SHUT DOWN AT 1350Z, LANDED AT 1601Z. FOUND PUMP DISCHARGE PRESSURE TUBE BROKEN OFF. REFER IPC 79-22-05-01. REPLACED NEW TUBE AND FILTERS. 2L73 4F4 FRTA22WE E13NE 20050104001162005010400116NM 2005 1 4 04FDEA03461 120041222A5330 SKIN PANEL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 AFT ACCESSORY COMPT: STA Y=2157 TO 2163, X50, 2 NUT PLATE ATTACHMENT FUSELAGE SKIN PANELS FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-78102. 2L73 4F RTA22WE 20050104001172005010400117NM 2005 1 4 04FDEA03462 120041222A5330 SKIN PANEL DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 AFT ACCESSORY COMPT: STA Y=2140 TO 2158, X50, 6 EACH NUT PLATES ATTACHMENT FUSELAGE SKIN PANELS FOUND WITH CORROSION. CORROSION ON SKIN PANEL BLENDED THRU AS PER SRM 51-21-01, VOL II AND FOUND EXCEEDED LIMIT AS PER SRM 53-00- 01 FIG 1A VOL I. 2L73 4F RTA22WE 20050104001182005010400118NM 2005 1 4 04FDEA03463 120041222A5511 SPAR CAP DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 EMPENNAGE: HORIZONTAL STABILIZER RIGHT HAND UPPER SPAR CAP NR 36R BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2L73 4F RTA22WE 20050104001222005010400122WP 2005 1 4 AALA20041248 120041225A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21253AA 49286 BDL - CEILING MOUNTED EMERGENCY LIGHTS AT ROWS 19 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING MOUNTED EMERGENCY LIGHTS AT ROWS 19 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001232005010400123WP 2005 1 4 AALA20041249 120041225A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219306T 49567 DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 9, 10 AND 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050104001242005010400124WP 2005 1 4 AALA20041250 120041226A3222 STRUT DOUG DC9 DC982 3022082WP NLG LOW A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21574AA 53151 YUL - EN ROUTE ORD GEAR WOULD NOT RETRACT. RETURNED YUL AND LANDED UNEVENTFULLY. ACCOMPLISHED SERVICING OF NOSE STRUT WITH NITROGEN ONLY PER MAINTENANCE MANUAL/TECH SERVICES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001252005010400125NM 2005 1 4 AALA20041251 120041227A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 PHX - COCKPIT ENTRY WAY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT ENTRY WAY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050104001262005010400126NM 2005 1 4 AALA20041252 120041227A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 PHX - SECOND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR SECOND OVERWING EXIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050104001282005010400128NM 2005 1 4 AALA20041254 120041227A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 PHX - EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31 INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050104001312005010400131WP 2005 1 4 AALA20041231 120041218A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21226AA 49176 DTW - OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY CHARGER FOR OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001332005010400133WP 2005 1 4 AALA20041233 120041218A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21483A 49676 DFW - TWO EACH OVERHEAD EMERGENCY LIGHTS AT AIRSTAIRS CATWALK AND ONE TAIL CONE EMERGENCY LIGHT INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR TWO EACH OVERHEAD EMERGENCY LIGHTS AT AIRSTAIRS CATWALK AND FOR ONE TAIL CONE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001362005010400136NM 2005 1 4 AALA20041224 120041215A3350 BATTERY BOEING737 737823 13844BZNM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21975AN 29549 ORD - EMERGENCY LIGHTS IN CABIN FAILED TEST. CHARGED BATTERIES FOR 1.5 HOURS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050104001372005010400137NM 2005 1 4 AALA20041220 120041214A3350 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21631AA 24589 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT ROW 9 INOPERATIVE. FOUND LOOSE CONNECTION. RECONNECTED LOOSE PLUG FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050104001382005010400138WP 2005 1 4 AALA20041221 120041213A3260 SENSOR DOUG DC9 DC982 3022082WP NLG FAULTY A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21574AA 53151 ORD - AFTER TAKEOFF RED NOSE GEAR LIGHT ILLUMINATED AND REMAINED ON. FOLLOWED CHECKLIST AND RECYCLED GEAR. RED NOSE GEAR LIGHT AGAIN ILLUMINATED. NO VIBRATION WAS FELT OR HEARD. LANDED ORD WITHOUT INCIDENT. REMOVED FROM AIRCRAFT FROM SERVICE FOR REPAIR. REPLACED UPLOCK SENSOR D132. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001392005010400139NE 2005 1 4 AALA20041222 220041214A7314GP202MK1 PUMP BOEING757 757223 1384957NM RROYCERB211 RB211535E4B3 NE LT ENGINE FAILED A AALAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SW21661AA 25295 31340 SJU - LEFT HAND ENGINE FAILED AT 800 FEET ON FINAL. LEFT ENGINE LOW PRESSURE PUMP ANNUNCIATED ON EICAS. ALL OTHER INDICATIONS NORMAL. REPLACED ROTOR AND DRIVE ASSEMBLY (UL39542 MFG ROLLS ROYCE) AND STATOR (450401 MFG UNISON INDUSTRIES) AND HIGH PRESSURE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA2NM E12EU 20050104001402005010400140WP 2005 1 4 AALA20041223 120041215A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21232AA 49179 DFW - EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY FOR EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001412005010400141EU 2005 1 4 AALA20041225 120041215A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2177080 626 MIA - EMERGENCY LIGHTS AT SEATS 19C TO 25C AND AT 3L DOOR AND 27C TO 28C INOPERATIVE. REPLACED BATTERY PACK 110WL5 FOR EMERGENCY LIGHTS AT SEATS 19C TO 28C AND AT 3L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050104001422005010400142WP 2005 1 4 AALA20041226 120041215A2910 HYDRAULIC SYSTEM DOUG DC9 DC982 3022082WP RIGHT LOW A AALAK NONE O OTHER CRCRUISE 1 SW21242AA 49255 PHX - RIGHT HYDRAULIC PRESSURE DROPPED TO 0 AND HYDRAULIC QUANTITY DROPPED TO 4 QUARTS. EMERGENCY GEAR EXTENSION PROCEDURES USED. LANDED PHX WITHOUT INCIDENT. SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. INSPECTED ALL RIGHT SYSTEM HYDRAULIC COMPONENTS AND OPERATED ALL RIGHT HYDRAULIC SYSTEMS. NO LEAKS NOTED. RELEASED AIRCRAFT FOR FLIGHT CHECK PER SPOTTING MESSAGE 12 044. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001432005010400143WP 2005 1 4 AALA20041212 120041210A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21417AA 49328 MSP - OVERHEAD EMERGENCY LIGHTS AT AFT ROW 18 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FOR AFT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001442005010400144WP 2005 1 4 AALA20041210 120041210A1430 FASTENER DOUG DC9 DC982 3022082WP FUEL BOOST PUMP LOOSE A AALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW21266AA 49291 SLC - INFLIGHT FUEL LEAKING FROM BOOST PUMP COVER ON RIGHT WING. FOUND FASTENERS LOOSE ON RIGHT FORWARD AND AFT OF BOOST PUMP COVER. RETORQUED LOOSE FASTENERS ON RIGHT FORWARD AND AFT OF BOOST PUMP COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001462005010400146NM 2005 1 4 AALA20041211 120041210A2120 SMOKE BOEING737 737823 13844BZNM COCKPIT DETECTED A AALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW21967AN 29545 ORD - TAKEOFF ABORTED AT 100 TO 110 KNOTS DUE TO SMOKE IN COCKPIT AND SMOKE REPORTED IN CABIN OF MODERATE INTENSITY. AIRCRAFT TAKEN OUT OF SERVICE. RIGHT HAND ENGINE WAS BORESCOPED PREVIOUS NIGHT. SP40 WAS USED TO LOOSEN BORESCOPE PLUGS. SUSPECT INGESTION INTO ENGINE WAS PATH. PERFORMED HIGH POWER RUN. NO SMOKE NOTED AND SMELL DISSIPATED. REMOVED AND REPLACED RIGHT HAND RECIRCULATION FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050104001472005010400147NM 2005 1 4 AALA20041215 120041212A3397 WIRE BOEING757 7572Q8 1384972NM CABIN BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21710TW 28169 DFW - EMERGENCY LIGHTS IN FRONT OF R3 LAVATORY TRACK STRIP BROKEN. REPLACED BROKEN TRACK CABLE FROM ROW 18 TO LAVATORY D FOR EMERGENCY LIGHTS IN FRONT OF R3 LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050104001492005010400149NM 2005 1 4 AALA20041214 120041212A3350 LIGHT BOEING757 7572Q8 1384972NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21710TW 28169 DFW - EMERGENCY ESCAPE PATH LIGHT BETWEEN ROW 21 AND 22 INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP BETWEEN ROWS 21 AND 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050104001512005010400151NM 2005 1 4 AALA20041209 120041206A3350D71702001 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21795AN 30257 MIA - AFT CABIN SEAT MOUNTED EMERGENCY LIGHT FROM CENTER ROW SEATS 30 TO 44 INOPERATIVE. REPLACED BATTERY PACK FOR AFT CABIN SEAT MOUNTED EMERGENCY LIGHT FROM CENTER ROW SEATS 30 TO 44. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050104001522005010400152NM 2005 1 4 SWAA043722 120041227A53106546550 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 787, RBL 8. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050104001532005010400153NM 2005 1 4 SWAA043715 120041224A5610141A48103 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW29725SW 27857 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW PER MM. 2L72 4F RTA16WE 20050104001552005010400155NM 2005 1 4 SWAA043717 120041227A53106520722 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT FUSELAGE FRAME CRACKED AT BS 440, NR 5 DOOR STOP FITTING. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20041230001012004123000101NM 2004 12 30 2004UALA01161 120041124A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 STATION 1380 LBL 19, INTERNAL SKIN DOUBLER CORRODED BEYOND LIMITS IN AFT PIT. 2L72 4F4 FRTA2NM E17NE 20041230001072004123000107NM 2004 12 30 04FDEA03275 120041130A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20041230001292004123000129 2004 12 30 2004UALA01180 420041202A2565 LINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE ESCAPE SLIDE OUT OF POSITION A UALAK NONE O OTHER ININSP/MAINT 1 WP29414UA 472 MOORING LINE LOOP UNDER LOWER LACING COVER. SLIDE REPACKED WITH MOORING LINE LOOP INSTALLED ON TOP OF LACING. 2L72 4F4 FRTA28NM E40NE 20041230001372004123000137NM 2004 12 30 04FDEA03295 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77986. 2L73 4F RTA22WE 20041230001412004123000141NM 2004 12 30 04FDEA03299 120041201A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PAGES 402-407, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.232, MAXIMUM ALLOWABLE DIAMETER=1.190. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77985. 2L73 4F RTA22WE 20041230001472004123000147EA 2004 12 30 QXEA200400830 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREA AT FS 453-475, FS 487-505 AND FS 506-517. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20041230001562004123000156EA 2004 12 30 COMA0460661 120041203A3230750006000 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01929CA7453 7035 FLIGHT 4962, LOUD CLUNKING NOISE FROM NLG. REPLACED THE NLG DOORS SELECTOR VALVE. 2L72 4F RTA21EA 20041230001592004123000159EU 2004 12 30 DHL2004365006 120041105A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 2 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01367DH 265 ENG NR 2 LOOP B ILLUMINATED ON CLIMB-OUT. PERFORMED LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURE AND PLACED LOOPS SWITCH ON OPPOSITE SYSTEM. DEFERRED ENG NR 2 LOOP B PER MEL 26-12-01-1, ASSIGNED CONTROL NR 18361. PLACARD INSTALLED. 2L72 4F RTA35EU 20041230001652004123000165WP 2004 12 30 04FDEA03233 120041126A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAPS CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND ON LT OUTBOARD FLAP HINGE SECTION STA XW 638 WITH OXIDATION WHERE CONTACT STUD BOLTS. ACCOMPLISH CORROSION REWORK AT LT OUTBOARD FLAP FWD OUTB'D HINGE SECTION IAW CMM 51-44-09. 2L73 4F A22WE 20050103000022005010300002WP 2005 1 3 AALA20041247 120041225A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21494AA 49732 DEN - OVERHEAD EMERGENCY LIGHTS AT AFT SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR OVERHEAD EMERGENCY LIGHTS AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050103000042005010300004WP 2005 1 3 ABXA040395 120041110A53115911448501 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 FRAME CRACKED FS 357 AT LONGERON 30. REPAIRED FRAME STA 357 AT LONGERON 30 IAW DC-9 SRM 53-03. 2L72 4F A6WE 20050103000052005010300005WP 2005 1 3 ABXA040399 120041116A5510ASSB2215 BEARING DOUG DC9 DC933F 302207AWP HORIZONTAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 RIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM. 2L72 4F A6WE 20050103000132005010300013NM 2005 1 3 AWXA200401436 120041208A5753655058517 PLATE BOEING737 7373G7 1384595NM LT MID FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTER INDEXING PLATE AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTER INDEXING PLATE IAW B737-300 OHM 57-53-22 FIG 1101. 2L72 4F RTA16WE 20050103000152005010300015NM 2005 1 3 AWXA200401438 120041208A575369431205 RETAINER BOEING737 7373G7 1384595NM LT MID FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBLE ASSEMBLY RETAINER AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBLE ASSEMBLY RETAINER IAW B737-300 OHM 57-53-22 FIG 1101. 2L72 4F RTA16WE 20050103000172005010300017NM 2005 1 3 AWXA200401440 120041208A5753694065710 SUPPORT BOEING737 7373G7 1384595NM RT MID FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP INBOARD GIMBLE OUTER BEARING SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP INBOARD GIMBLE OUTER BEARING SUPPORT ASSEMBLY IAW B737-300 SOPM 20-50-01 FIG 1. 2L72 4F RTA16WE 20050103000292005010300029NM 2005 1 3 AWXA200401448 120041207A532065C326778 FLOOR SUPPORT BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 991, LBL 17, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 991, LBL 17, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C32677; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 1 & 12. 2L72 4F RTA16WE 20050103000332005010300033NM 2005 1 3 AWXA200401452 120041208A575369406575 SUPPORT BOEING737 7373G7 1384595NM LT MID FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBLE SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBLE SUPPORT IAW B737-300 SOPM 20-50-01 FIG 1. 2L72 4F RTA16WE 20050103000362005010300036EU 2005 1 3 AWXA200401430 120041210A5321D5367201200000 FLOOR PANEL AIRBUS320 A320232 3930326EU CARGO BAY CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LOWER SKIN OF FORWARD CARGO COMPARTMENT FLOOR PANEL 132FF. MAINTENANCE REMOVED CORRODED FLOOR PANEL 132FF FROM FR 28 TO FR 30, STR 36 RT TO STR 38 RT; FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR PANEL IAW A320 SRM 53-02-00 FIG 209. 2L72 4F RTA28NM 20050103000382005010300038NM 2005 1 3 AWXA200401432 120041221A5753113N260311 WEDGE BOEING757 757225 1384959NM RT FLAP SEPARATED A AWXAO OTHER DF INFLIGHT SEPARATION FLT CONT AFFECTED DEDESCENT 1 WP28913AW 22207 ON DESCENT A PASSENGER REPORTED THAT A 3FT X 6FT SECTION OF RT WING INBOARD TRAILING EDGE FLAP HAD BROKEN OFF AND SEPARATED FROM THE AIRCRAFT, A ROLL WAS FELT WITH FLAPS AT 25, SELECTED FLAPS 20 AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE EVALUATED DAMAGE AFTER THE AIRCRAFT HAD LANDED AND FOUND A 3FT X 6FT SECTION OF TRAILING EDGE FLAP WEDGE WAS MISSING OFF THE RT WING INBOARD FLAP AT THE OUTBOARD END. PERFORMED INSPECTION OF MID FLAP AND HORIZONTAL STABILIZER FOR SECONDARY DAMAGE, NO DAMAGE WAS NOTED. REMOVED REMAINING PIECES OF TRAILING EDGE FLAP WEDGE FROM RT INBOARD FLAP, INSTALLED NEW REPLACEMENT TRAILING EDGE FLAP WEDGE IAW B757-200 SRM 51-30-2. 2L72 4F RTA2NM 20050103000412005010300041NM 2005 1 3 AWXA200401460 120041202A575465C26603100 SKIN BOEING737 7373G7 1384595NM L/E SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE UPPER SURFACE OF THE NR 4 SLAT DELAMINATED AT THE INBOARD CORNER BETWEEN WS 521.30 AND WS 531.25. MAINTENANCE CUTOUT DAMAGED SKIN ON UPPER SURFACE OF NR 4 SLAT; FABRICATED AN INTERNAL & EXTERNAL DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5741-04358-ES3. 2L72 4F RTA16WE 20050103000462005010300046NM 2005 1 3 AWXA200401441 120041211A5320654585546 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON LOWER SURFACE OF R-2 DOOR ENTRY WAY INNER CHORD (CREASE STIFFENER) BETWEEN BS 972 AND BS 984, RBL 51, WL 207.5. MAINTENANCE REMOVED CORRODED INNER CHORD CREASE STIFFENER FROM BS 972 TO BS 984, RBL 51; FABRICATED A NEW REPLACEMENT CREASE STIFFENER PER DWG 65-45855; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3 & 8. 2L72 4F RTA16WE 20050103000522005010300052NM 2005 1 3 AWXA200401402 120041215A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW12990109 1049 PHX - EEL - DURING E-04 CHECK THE LT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND TO HAVE AN INTERNAL FAILURE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050103000552005010300055EU 2005 1 3 AWXA200401393 120041111A5321D5361033200900 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FORWARD GALLEY FLOOR PANEL 222FF (R-1 DOOR SILL). MAINTENANCE REMOVED AND REPLACED CORRODED FORWARD GALLEY FLOOR PANEL 222FF IAW T/C C1C25306. 2L72 4F RTA28NM 20050103000602005010300060EU 2005 1 3 AWXA200401401 120041114A5320D53475565210 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON AFT CARGO DOOR THRESHOLD OUTBOARD COVERSHEET (SILL) BETWEEN FR 52 AND FR 56. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR OUTBOARD SILL FROM FR 52 TO FR 56; FABRICATED A NEW REPLACEMENT SILL; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050103000762005010300076NM 2005 1 3 CALA0400708 120041109A3350D71701100 BATTERY PACK BOEING777 777224 1385225NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW2779011 29859 THE EMERGENCY LIGHTS AT SEATS 1-5 FAILED FUNCTIONAL TEST. THE BATTERY PACK AT M33094 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-06-960-802. 2L72 4F RTT00001SE 20050103000952005010300095NE 2005 1 3 DL76S041098 220041213A7200CF680A2 ENGINE BOEING767 767332 1382001NM GE CF680 CF680A2 NE NR 1 MAKING METAL A DALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO27126DL38876 24076 580394 LT ENGINE OIL FILTER MSG IN FLIGHT RETARDED LT ENGINE TO IDLE WITH MSG STILL THERE SHUTDOWN LT ENG IN FLIGHT. CHECKED SCAVENGE FILTERS AND ALL CHIP DETS FOUND HEAVY FUZZON MASTER CHIP DET LARGE AMOUNT OF SHINY FLAKES ON AFT B-SUMP DET FOUND TWO OR THREE SHINY CHIPS ON FWD B-SUMP DET, ALL OTHER DETECTORS OK. REPLACED NR 1 ENGINE. 2L72 4F4 FRTA1NM E13NE 20050103000962005010300096NM 2005 1 3 DL75A041099 120041214A5330141N33131 SKIN BOEING757 757212 1384951NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27751AT 23125 FUSELAGE SKIN CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. REPAIRED IAW ERA 095131-14AD. 2L72 4F RTA2NM 20050103000972005010300097NM 2005 1 3 DL73S041100 120041214A5330 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27310DA 23082 FUSELAGE SKIN CRACKED AT MULTIPLE LOCATIONS ALONG STRINGER 4R BETWEEN STA 540 AND 727. REPAIR IAW ER/A 095480-14AD. 2L72 4F RTA16WE 20050103001062005010300106EU 2005 1 3 DHL2004364018 120041218A53132024T3 STRINGER AIRBUS300 A300B4203 3930306EU FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING A-CHECK IN MIAMI, FLORIDA AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 4418 CRACK AT FR 21 STR 9R INTERNAL. REMOVED FASTENERS OUT OF DAMAGE AREA AS PER A-300 SRM 51-30-30. REMOVED DAMAGE AT FRAME 21 STR 9R AS PER A-300 SRM 53-10-10 (2 INCHES LONG). HEAT TREATMENT MATERIAL 2024 0.063 AS REQUIRED AS PER A-300 SRM 51-40-30. INSTALLED FRAME REPAIR AT FR NR 21, STG 9R MAT USED 2024 T3 .063 PO 3797 AS PER A-300 SRM 53-10-10 FIG 715 SIZE OF REPAIR 17 INCHES LONG BY 6 INCHES WIDE. 2L72 4F RTA35EU 20050103001092005010300109CE 2005 1 3 DXTA200400493 120041223A2740 PITCH CONTROL CESSNA500 560CESSNA 2076750CE COCKPIT FROZEN E DXTAO OTHER J WARNING INDICATION DEDESCENT 1 GL07366QS 5600466 DESCENDING THROUGH 18,000 FT, RECEIVED A PITCH MIS TRIM ANNUNCIATOR. ATTEMPTED TO HELP THE AUTOPILOT BY TRYING TO TRIM THE NOSE UP. DISCOVERED THAT THE PITCH WHEEL WAS FROZEN IN A VERY NOSE DOWN POSITION. AT 13,000 FT USED EXTREME FORCE TO MOVE THE PITCH WHEEL ENOUGH TO LAND. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050103001172005010300117EU 2005 1 3 04FDEA03363 120041204A2930353152003 CONTROL UNIT AIRBUS310 A310222 3930315EU HYDRAULIC SYS MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25450FE7798 7798 162 DURING CLIMBOUT YELLOW HYDRO SERVO SYSTEM JAMMED. JAM LIGHT ILLUMINATED ON OVERHEAD PANEL. NO ECAM WARNING. FOLLOWED CHECKLIST. JAM DETECTION CONTROL UNIT REPLACED. 2L72 4F RTA35EU 20050103001302005010300130NM 2005 1 3 04FDEA02969 120041022A5320A5A7112501 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 MAIN DECK - ATTIC AREA STA 5-116 LONGERON 9R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG A5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20050103001392005010300139WP 2005 1 3 04FDEA03471 120041219A5320AEA002618 INTERCOSTAL DOUG DC10 DC1030 3023501WP RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25309FE 48298 EXCESSIVE CORROSION ON INTERCOSTAL IN RIGHT WHEEL, AFT BULKHEAD AT LONGERON 30. REMOVED AND REPLACED INTERCOSTAL. 2L73 4F A22WE 20050103001622005010300162NM 2005 1 3 SB04166 120041213A335020131A BATTERY PACK BOEING737 737401 1384701NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19425US 23992 CLT - MAINTENANCE REPORTED THE MAIN ENTRY DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY LIGHT BATTERY PACK FOR THE MAIN ENTRY DOOR OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050103001672005010300167NM 2005 1 3 USAA040841 120041105A5753 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT FOREFLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19776AU39004 24934 SKIN, 4 INCH BY 14 INCH AREA DELAMINATION, LT OB FOREFLAP T/E IB END. DEFECTIVE PART REPLACED WITH IDENT PN. 2L72 4F4 FRTA16WE E21EU 20050103001782005010300178NM 2005 1 3 USAA040909 120041020A53201133482 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 -CLIP, .5 INCH CRACK AT BS578, S8L. DEFECTIVE PART REPLACED WITH IDENT PART IAW IDENT PART IAW SRM 51-40. 2L72 4F4 FRTA16WE E21EU 20050103001842005010300184EU 2005 1 3 SA04114 120041208A261273040102 FIRE DETECTOR AIRBUSA319 A319112 3930323EU APU BAY FAULTY A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19724UW13156 1122 PHL FLT 1280 EN ROUTE CLT TO MHT, WHILE IN CRUISE FLIGHT, A "LAND ASAP" MESSAGE APPEARED ON THE ENGINE/WARNING DISPLAY UNIT, WITH NO OTHER INDICATIONS. THE ECAM RECALL FUNCTION DISPLAYED AN "APU FIRE" MESSAGE. THE FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU FIRE DETECTION UNIT. SYSTEM CHECKS OK. 2L72 4F RTA28NM 20050104000032005010400003EA 2005 1 4 ASOA04941 120041123A30207C14 CLAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT COWLING LOOSE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27852AS 7369 873088 AFTER TAKEOFF, WHEN CLIMBING THROUGH 12,000 FT, THE CREW RECEIVED A MASTER WARNING, 14TH STAGE DUCT ON EICAS AND DUCT FAIL OF 14TH STAGE PANEL. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFELY. MAINTENANCE GROUND RAN THE RT ENGINE AND FOUND A BLEED LEAK ON THE COWL ANIT-ICE DUCTING. MAINTENANCE RESECURED A CLAMP ON THE DUCTING IN THE PYLON. NO FURTHER LEAKS WERE NOTED, ALSO CHECKED FOR SECURITY OF BOTH PYLON LOOPS, REPOSITIONED AND SECURED BOTH LOOPS; AND THEN GROUND RAN THE RT ENGINE AGAIN. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000272005010400027EU 2005 1 4 ASOA04929 120041102A5320 INTERCOSTAL AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON THE RT INTERCOSTAL BETWEEN FRAMES 36 AND 38 AT STRINGER 16R AND ALSO ON THE LT INTERCOSTAL BETWEEN FRAMES 38 AND 39 AT STRINGER 16L. MAINTENANCE REMOVED AND REPLACED THE CORRODED INTERCOSTALS IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20050104000282005010400028EU 2005 1 4 ASOA04936 120041120A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27632AS 338 DURING AN A-CHECK, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000352005010400035EU 2005 1 4 ASOA04932 120041102A5320 ANGLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, THE LT END OF THE FAIL SAFE ANGLE ON FR 36 WAS FOUND TO BE CORRODED AND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT OF THE FAIL SAFE ANGLE ON FR 36 IAW SRM 53-00-00, FIG 417. 2H72 4T4 TRTA53EU E20NE 20050104000532005010400053NM 2005 1 4 04FDEA03301 120041201A243231432001 BATTERY DOUG MD11 MD11 3023602NM NR 1 & 2 FAILED A FDEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION ININSP/MAINT 1 SO25618FE 48754 "EMERGENCY POWER TEST FAIL" ALERT DISPLAY. TWO (2) EACH MAIN BATTERY (P/N: 31433-001) REMOVED AND REPLACED PER AMM 24-34-02-4. OPERATIONAL TEST OF THE MAIN BATTERY CARRIED OUT PER AMM 24-34-02-5. FOUND SATISFACTORY. POSITION 1, S/N OFF: 10101125, S/N ON:10201519, SERVICEABLE TAG NO.: 684804 POSITION 2, S/N OFF: 10201514, S/N ON:10200188, SERVICEABLE TAG NO.: 684803. 2L73 4F RTA22WE 20050104000622005010400062NM 2005 1 4 04FDEA03385 120041207A2781 SWITCH BOEING727 72722 1384002NM L/E SLAT MALFUNCTIONED A FDEAB EMER. DESCENT N FALSE WARNING CRCRUISE 1 SO25168FE 18865 AT FL280, LE AMBER LIGHT ILLUMINATED (WING ANTI-ICE ON). NO ROLL OR DIRECTIONAL CENTRAL PROBLEM NOTED. NR 2 FLAP ON FE PNL L AMBER. SLOWED DOWN TO 230 KTS, CLOSED WING ANTI-ICE. LIGHT STAYED ON, RECEIVED QRH. DID NOT CHANGE CONFIG. DESCENDED T0 200 DECLARED EMERG. AFTER REDUCED PWR AND 240 FL LIGHT WON`T GO OUT KEPT POWER REDUCED. SUSPECT BLEED AIR LEAK. WING ANTI-ICE DUCTING ON THE LT SIDE LEAK CHECKED AS PER B727-100 AMM 30-13- 000-5 AND NO LEAKS FOUND. L/E POSITION INDICATING HARNESS INSPECTED AND NO DEFECTS FOUND. L/E FLAP POSITION INDICATING SWITCH REMOVED AND REPLACED PER B727-100 AMM 27-82-001-4 - PRECAUTIONARY. COULD NOT DUPLICATE THE FAULT, CHECKS SERVICEABLE. 2L73 4F A3WE 20050104000642005010400064NM 2005 1 4 04FDEA03204 120041124A3150 WARNING SYSTEM BOEING727 72722 1384002NM COCKPIT ACTIVATED A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25151FE 19147 RECEIVED GND PROX WARNING ON TAKEOFF. PERFORMED ESCAPE MANEUVER USING FIREWALL POWER. FUEL WAS DUMPED TO MAX LDG WT. NO EMERGENCY WAS DECLARED. OTHER FLIGHT INFO AS FOLLOWS: 1000' AGL 10"C OAT 180 KIAS AIRSPEED BLEEDS 1 & 3 OPEN NR 2 CLOSED EGT APPROX 540"C ALL ENGINES ALL GEN ON LINE TOTAL FUEL DUMPED 2500 LBS. ENT BY: 031478 RPT BY: 223437. PERFORMED ENGINE RUNS PER JRH AND FEDEX FORM M-3423, FAXED INFO TO MOCC POWER PLANT. ENT BY: 354144 RPT BY: 354144 FACT 24NOV04 21:29 DAY U ALL 3 ENGINES OK FOR SERVICE PER EA 7-7100-84408 GPWS TESTED PER TSI 34-52-5677 AND MM 34-52-000-5 RII:354144 ENT BY: 031478 RPT BY: 031478. 2L73 4F A3WE 20050104000662005010400066NM 2005 1 4 04FDEA03406 120041213A5320 ANGLE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, TEE ANGLE ON BULKHEAD STA 2007 CORRODED AT LBL 75. REPLACEMENT OF TEE ANGLE AT STA 2007. 2L73 4F RTA22WE 20050104000762005010400076WP 2005 1 4 04FDEA03369 120041206A5743 FITTING DOUG DC10 DC1010 3022110WP LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF REF NRC NF 11565, FOUND AFTER NUT REMOVAL, CORROSION AROUND FASTENERS HOLES ON MLG TRUNNION FITTING LT WING AND ON SPLICE ANGLE P/N ARB 0634-1. REPLACE SPLICE ANGLE PER SRM 51-34-01, P/N ARB0634-1, TLU 980-9-47, TLN 1000L9, ARB 1997-501, 2431218-9C18E, AN960C916L. REMOVE FASTENERS PER SRM 51-34-01, REMOVE CORROSION PER SRM 51-21-01, REWORKED AREA PER EA 8-55710-70140. 2L73 4F A22WE 20050104000782005010400078EU 2005 1 4 04FDEA03379 120041206A5245 FITTING AIRBUS310 A310 EU A/C ACCESS DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 ACCOMPLISH MAINTENANCE "C" CHECK #003 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 29SEP04 14:53:57:6 BY:067708 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 162248 ON: 29OCT04 12:31:08:0 S=M. AIR COND, SEVERAL HOLES OF FITTINGS AT ACCESS DOORS (148 CZ) TO AIR COND COMPT DAMAGED. REPAIRED IAW EA 6-5315-82534. 2L72 4F RTA35EU 20050104000902005010400090EU 2005 1 4 04FDEA03372 120041206A5753 FAIRING AIRBUS310 A310 EU T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 REPAIR, NR 2 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49992 REV NO POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:56:3 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:45:04:9 S=M. COMPLIED WITH EA 6-5720-49992. 2L72 4F RTA35EU 20050104000912005010400091EU 2005 1 4 04FDEA03373 120041206A5753 FAIRING AIRBUS310 A310 EU T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25452FE 313 REPAIR, NR 4 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49991 REV NO. POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:48:9 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:44:51:3 S=M. COMPLIED EA 6-5720-49991. 2L72 4F RTA35EU 20050104001092005010400109WP 2005 1 4 04FDEA03197 120041123A5330 SKIN DOUG MD10 MD1010F 3022112WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 REPAIR DOUBLER AND TRIPLER AT FUSELAGE STATION 577-591, LONGERON 42L-44L NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA AND IF REPETITIVE INSPECTION ARE REQUIRED. COMPLIED WITH FEDEX EA 8-5330-83947, FUSELAGE, SKIN CRACK REPAIR AT EXHAUST, RAM AIR- EVALUATION. REPAIR IS MINOR PER GMM 4-1-975 FIGURE 5 AND EA 8-5330- 83947. 2L73 4F RTA22WE 20050104001122005010400112NM 2005 1 4 04FDEA03226 120041125A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 44R. REMOVED AND REPLACED WITH NEW SPLICE AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050104001152005010400115EU 2005 1 4 04FDEA03237 120041126A7830 THRUST REVERSER AIRBUS300 A300B4605R 3930308EU NR 2 ENGINE OUT OF RIG A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25665FE 769 DURING T/O, NR 2 ENGINE ECAM "THRUST REVERSER UNLOCKED" RTO POWER SETTING 70 PERCENT N1 AIRSPEED 30 KTS. ENT BY: 299976 RPT BY: 096807 FACT 26NOV04 23:59 EWR R RE-RIGGED NR 2 ENGINE THRUST REVERSER PER AMM 78-31-00-5-F. RE-RIGGED NR 2 ENGINE THRUST REVERSER RT RVDT PER AMM 78-31-07-4-F. NR 2 ENGINE THRUST REVERSER OPS CHECKED OK PER AMM 78-31-00-5-F. RII:099732 ENT BY: 299976 RPT BY: 299976. 2L72 4F RTA35EU 20050104001192005010400119NM 2005 1 4 04FDEA03464 120041222A5511 SPAR CAP DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 EMPENNAGE: HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SPAR CAP NR 1L BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIMIT. 2L73 4F RTA22WE 20050104001292005010400129NM 2005 1 4 AALA20041255 120041227A3350 POWER SUPPLY BOEING767 767323 1385205NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21380AN 25449 JFK - EMERGENCY PROXIMITY LIGHTS AT ROWS 20A TO 24B ARE INOPERATIVE. REPLACED POWER SUPPLY M737 FOR EMERGENCY PROXIMITY LIGHTS AT ROWS 20A TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050104001322005010400132WP 2005 1 4 AALA20041232 120041218A3350 CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21226AA 49176 DTW - OVERHEAD EMERGENCY EXIT LIGHTS AT AFT GALLEY INOPERATIVE. REPLACED BATTERY CHARGER FOR OVERHEAD EMERGENCY EXIT LIGHTS AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001342005010400134NM 2005 1 4 AALA20041228 120041217A3397 WIRE BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139365 24046 SFO - EMERGENCY ESCAPE PATH LIGHT IN FIRST CLASS GALLEY INOPERATIVE. FOUND WIRING FOR LIGHT WRAPPED AND STOWED BEHIND RIGHT SIDE FLOOR GRILL. ROUTED AND CONNECTED WIRING TO EMERGENCY LIGHT AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050104001352005010400135WP 2005 1 4 AALA20041229 120041217A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21498AA 49736 AUS - EMERGENCY LIGHT AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050104001502005010400150EU 2005 1 4 AALA20041213 120041210A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2114056 463 JFK - EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT DOOR 1L. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050104001562005010400156NM 2005 1 4 SWAA043718 120041227A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, RBL 39 TO RBL 45, WL 208. REPAIRED FLOORBEAM PER SRM. 2L72 4F RTA16WE 20050104001582005010400158NM 2005 1 4 SWAA043720 120041227A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, WL 201, RT SIDE. REPAIRED FRAME PER T1-153-018. 2L72 4F RTA16WE 20050104001612005010400161 2005 1 4 SWAA043633 420041215A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29092SW 22964 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20050104001632005010400163NM 2005 1 4 SWAA043604 120041212A53156545833 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 270 FROM LBL 7 TO RBL 7, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM. 2L72 4F RTA16WE 20050104001642005010400164NM 2005 1 4 SWAA043614 120041120A3350101114 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29448WN 33721 DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050104001662005010400166 2005 1 4 SWAA043700 420041221A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 & R2 DOORS OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED C2CHECK, FOUND R2 AND L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED R2 AND L2 DOOR EVAC SLIDES PER MM. 2L72 4F RTA16WE 20050104001672005010400167NM 2005 1 4 SWAA043597 120041201A5313BAC1498 STRINGER BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29679AA 23291 DURING SPV, FOUND STRINGER AT BS 867, STRINGER 1, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2L72 4F RTA16WE 20050104001682005010400168NM 2005 1 4 SWAA043605 120041212A532065C27314 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SPV, FOUND 2 EACH STRINGER CLIPS AT BS 620, BS 616, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050104001692005010400169NM 2005 1 4 SWAA043606 120041212A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 520, STRINGER 12L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050104001702005010400170NM 2005 1 4 SWAA043620 120041213A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050104001732005010400173NM 2005 1 4 SWAA043635 120041215A53116546552 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 827, STRINGER 8L, CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050104001742005010400174NM 2005 1 4 SWAA043636 120041215A575365C357030 STRUCTURE BOEING737 7373H4 1384600NM RT FORE FLAP WARPED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND RT WING OUTBOARD T/E FORE FLAP, WARPED. REMOVED AND REPLACED RT WING OUTBOARD T/E FORE FLAP PER MM. 2L72 4F RTA16WE 20050104001752005010400175NM 2005 1 4 SWAA043637 120041215A5320907822 FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR UPPER HINGE BOX PER SRM. 2L72 4F RTA16WE 20050104001762005010400176 2005 1 4 SWAA043638 420041215A25656949956 CABLE BOEING737 7373H4 1384600NM L2 DOOR FRAYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29629SW 27704 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2L72 4F RTA16WE 20050104001772005010400177NM 2005 1 4 SWAA043610 120041213A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29628SW 27703 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN FROM BS 860 TO BS 1006, UNDER DORSAL FIN, WORN. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20050104001782005010400178NM 2005 1 4 SWAA043621 120041213A53116546549 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPT FRAME AT BS 767, RBL 12, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20050104001802005010400180NM 2005 1 4 SWAA043609 120041213A53146545866 PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29620SW 28036 DURING SCHEDULED C3 CHECK, FOUND KEEL BEAM LOWER PANEL BETWEEN MLG W/W CUTOUTS, CRACKED. REPAIRED PANEL PER SRM. 2L72 4F RTA16WE 20050105000032005010500003NM 2005 1 5 DL767041130 120041222A2120 ODOR BOEING767 767232 1385132NM CABIN DETECTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27113DA 22225 DURING CLIMBOUT, SMELL NOTICED IN COCKPIT, LIKE BURNING PLASTIC. RAN ENGINES AND PACKS, UNABLE TO DUPLICATE. SUSPECT RECENT FAN LUBE. 2L72 4F RTA1NM 20050105000042005010500004 2005 1 5 DLM88041131 420041223A3417349001222 ADC DOUG MD88 MD88 3023688NM E/E BAY FAILED A DALAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 SO27953DL 49884 AFTER TAKEOFF, CAPT AIRSPEED WAS DECREASING, CAPT ALTIMETER STUCK AT FIELD ELEVATION. F/O AIRSPEED INDICATING ZERO, GPWS ALERT SOUNDING CONSTANTLY. REPLACED CADC. 2L72 4F RTA6WE 20050105000112005010500011NM 2005 1 5 DL767041140 120041225A2121732591 COOLING FAN BOEING767 767232 1385132NM E/E BAY MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27106DA 22218 FWD EQUIPMENT COOLING FAN MESSAGE WITH SMELL. REPLACED SAME. 2L72 4F RTA1NM 20050105000182005010500018NM 2005 1 5 DL75K041145 120041228A2560P4010021SM BATTERY BOEING757 757232 1384965NM FLASHLIGHT DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27684DA 27104 THE 4R FLASHLIGHT BATTERY NOT BLINKING. REPLACED BATTERY. 2L72 4F RTA2NM 20050105000192005010500019NM 2005 1 5 DL757041146 120041228A2997 WIRE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO27631DL45027 23612 716548 AFTER ENGINE START {BOTH} HAD EICAS MESSAGE.LT HYD ENGINE PRESSURE AND DISCREET LIGHT AS WELL AS A STATUS MESSAGE. POWER XFER UNIT. FOUND DAMAGED WIRING IN NR 1 ENGINE PYLON. REPAIRED SAME. 2L72 4F4 FRTA2NM E17NE 20050105000222005010500022NM 2005 1 5 DL757041149 120041229A3810BAC60B50064 ELEMENT BOEING757 757232 1384965NM WATER HEATER BURNED A DALAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27660DL 24422 FIRST CLASS LAV HOT WATER HEATER HAS A BURNED ELEMENT. REPLACED SAME. 2L72 4F RTA2NM 20050105000242005010500024CE 2005 1 5 DXTA200400488 120041221A2810 FUEL SYS CESSNA750 750 2076810CE RT WING MALFUNCTIONED E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07997QS 7500208 REPEAT - AMBER WING TANK -O FULL R- CAS ON IN FLIGHT. FUEL SPILLING FROM RIGHT WING WITH ONLY 3000 LBS IN WING TANK, SPILLING STOPPED THEN STARTED AGAIN WITH 2700 LBS IN WING TANK AND SAME CAS MESSAGE. ITEM IS UNDER INVESTIGATION. 2L72 4J RTT00007WI 20050105000252005010500025CE 2005 1 5 DXTA200400496 120041225A2740 PITCH CONTROL RAYTHNDH125 HAWKER800XP 7150012CE COCKPIT FROZEN E DXTAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 GL07842QS 258542 PITCH TRIM FROZEN IN FLIGHT. ON CLIMBOUT FROM MINNEAPOLIS 10 DEG CELSIUS APPROX AUTOPILOT BEGAN 300-500 FT +- PITCH EXCURSIONS. UPON DESCENT, PITCH TRIM BEGAN WORKING WHEN IOAT ABOVE 0 DEGREE. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA3EU 20050105000262005010500026 2005 1 5 DXTA200400498 420041226A31607007549905 CDU BRAERO1000 BAE1251000A 1500104EU COCKPIT FAULTY E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07523QS NA1010 BURING ELECTRICAL SMELL IN COCKPIT, NO OTHER INDICATIONS. GEN 1 AMPS 80/ GEN 2 AMPS 120. REMOVED NR 1 FMS CDU DUE TO NO DISPLAY AND FAINT BURNING ELECTRICAL SMELL. REPLACED WITH SERVICEABLE FMS CDU OPS CHECK GOOD IAW HAWKER 1000 MM CH 34-61-00 REV 27 10/04. OPS CHECKED NR 1 AND NR 2 GENERATORS AMP SPLIT WITHIN LIMITS PER HAWKER 1000 MM CH 24-30-07. 2L72 4F RTA3EU 20050105000272005010500027CE 2005 1 5 DXTA200400499 120041226A3230 LANDING GEAR CESSNA560 560XL 2076702CE NLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07603QS 5605203 AFTER TAKEOFF NOSE GEAR WOULD NOT GET INTO UPLOCK AND CONTINUED TO CLUNK IN WHEEL WELL. HYDRAULIC PRESSURE LIGHT WOULD NOT GO OUT. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20050105000282005010500028CE 2005 1 5 DXTA200400481 120041217A322267421602 STRUT CESSNA750 750 2076810CE NLG LOW E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07932QS 7500032 AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE OUT OF THE DOWN POSITION. JACKED A/C FOUND NOSE STRUT SERVICE LOW. SERVICED NOSE STRUT AS REQUIRED. PERFORMED GEAR SWING SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE750 M/M 12-10-38. 2L72 4J RTT00007WI 20050105000312005010500031CE 2005 1 5 DXTA200400474 120041208A3240681330 O-RING CESSNA500 560CESSNA 2076750CE LT BLEED PORT LEAKING E DXTAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 GL07324QS 5600423 CREW REPORTED RIGHT BRAKE PEDAL LOSES PRESSURE DURING TAXI. PRESSURE BLEEDS OFF CREATING A SOFT PEDAL. REPLACED O-RINGS ON LEFT BRAKE BLEEDER PORT, BLEED BRAKES, CHECKED BRAKE RESERVOIR AND LINES FOR LEAKS. CHECKED GOOD. PERFORMED CO-PILOTS SPONGY BRAKE CHECKLIST. EVERYTHING CHECKED GOOD IAW CESSNA MM 32-42-00. 2L72 4F RTA22CE 20050105000322005010500032EU 2005 1 5 DXTA200400472 120041208A2120 ODOR BRAERO1000 BAE1251000 1500287EU CABIN DETECTED E DXTAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07505QS 259005 AT FL370 A BURNING ODOR WAS DETECTED, LASTING ABOUT 3-5 MINUTES. ANOTHER DIFFERENT BURNING ODOR WAS DETECTED PASSING 15,000 FEET IN THE DESCENT, IT LASTED UNTIL THE BLEED AIR WAS TURNED OFF PASSING 10,000 FEET. RAN ENGINES AND CHECKED OIL LEVEL. NR 2 ENGINE WAS .25 INCH FROM THE TOP. NR 1 ENGINE .75 INCH FROM THE TOP. RAN ENGINES AGAIN AT ALL POWER LEVELS AND INDIVIDUALLY ONE AT A TIME FOR AN HOUR. CONSECUTIVELY RAN ALL AVIONICS AND BLEED AIR ITEMS. NO ODOR. SHUT DOWN AND DESERVICED APPROX 1 PINT ENGINE OIL FROM NR 2 ENGINE. RAN AGAIN FOR 30 MINUTES. NO ODOR AT THIS TIME. 2L72 4F RTA3EU 20050105000332005010500033CE 2005 1 5 DXTA200400475 120041209A3246315381 WHEEL CESSNA750 750 2076810CE NLG VIBRATION E DXTAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL07910QS246 7500110 VIOLENT SHAKING IN NOSE GEAR ON TAKEOFF ROLL, ABORTED AROUND 30-40 KTS. REMOVED & REPLACED LT & RT NOSE TIRES, AND WHEEL ASSEMBLIES, WORK DONE IAW CITATION 750 M/M 32-41-01. 2L72 4J RTT00007WI 20050105000342005010500034 2005 1 5 DXTA200400329 420040630A31607014300901 DISPLAY CESSNA500 560CESSNA 2076750CE COCKPIT FAILED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07382QS2343 5600382 AFTER TAKEOFF CLIMBING THROUGH 31,000 FT, THE AOA AND WINDSHEAR FAIL ANNUNCIATOR COME ON AND GO BACK OUT TWICE. AFTER LEVELING AT 39,000 FT SMELLED SMOKE AND PDF NR 1 WENT BLANK. CONFIRMED DISCREPANCY, REMOVED AND REPLACED NR 1 DISPLAY UNIT WITH NEW UNIT IAW CESSNA 560 MM CHAPTER 34-23-02, OPERATIONAL CHECK GOOD. 2L72 4F RTA22CE 20050105000362005010500036CE 2005 1 5 DXTA200400408 120040928A3240 PEDAL CESSNA500 560CESSNA 2076750CE COCKPIT STIFF E DXTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07361QS 5600361 BRAKES ARE VERY HARD TO PUSH, THE TOPS OF BRAKE PEDALS SEEM TO BE TOO FAR FORWARD IN THE FRAME. TESTED LT AND RT BRAKES ON PILOT & CO-PILOT SIDES, OPS CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20050105000432005010500043NM 2005 1 5 UPS04443605 120041212A3350 BATTERY PACK BOEING747 747200 1384847NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:N/A EXIT SIGN AT UPPER DECK EMERGENCY EXIT IS INOP AND MARKED AS DEACTIVATED. REMOVED DEACTIVATED LABEL, NO POWER AT EXIT SIGN REQUIRES FURTHER T/S. REPLACED BATTERY PACK IAW B747 MM 33-51-04, OPS CHECK GOOD. 2L74 4F RTA20WE 20050105000442005010500044WP 2005 1 5 UPS04843599 120041117A5220DWG5758037 DOOR FRAME DOUG DC8 DC871F 302199DWP PLUG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 INSPECTION TYPE:C3 RIGHT FWD OVERWING PLUG DOOR FRAME CRACKED AT FWD UPPER CORNER. STOP DRILLED CRACK, NDT VERIFIED PER NDT-SPM06-10-01.001. REMOVED ADJACENT DOUBLER PER SRM 51-1-20B. WELDED CRACK PER DPS10.225. NDT WELD PER DPS4.707, NO DEFECTS. TREAT AND PRIME PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 20050105000462005010500046NM 2005 1 5 UPS04M43188 120040801A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 14 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM SIDEWALL & BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 0.988 INCH AT BARREL NUT HOLE NR 14 RT, FOUND OUT OF LIMIT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 14 RT PER EO MD11-5510-19409-H. REPAIR CUTOUT AT BARREL NUT HOLE NR 14 RT PER EO MD11-5510-19409-H & EN:1283-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050105000472005010500047NM 2005 1 5 UPS04M43189 120040804A5514 STRUCTURE DOUG MD11 MD11F 3023600NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01277UP 48578 INSPECTION TYPE:C, HORIZONTAL STAB NR 32 RT BARREL NUT HOLE FOUND CORRODED ON BOTTOM, SIDEWALL AND BEARING SURFACE. CORROSION REMOVED, BLEND & REAMED TO 1.178 INCH FOUND OUT OF LIMIT AT BARREL NUT HOLE NR 32 RT. FAB SLEEVE & BUSHING PER EO MD11-5510-19409-H. APPLIED SEALANT PR1422B1/2 AT BLEND AREA & INSTALLED SLEEVE BUSHING AT BARREL NUT HOLE NR 32 RT PER EO MD11-5510-19409-H. REPAIR C/O AT BARREL NUT HOLE NR 32 RT PER EO MD11-5510-19409-H & EN: 1294-04, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050105000482005010500048NM 2005 1 5 UPS04442807 120040712A5313 RIB BOEING747 747200 1384847NM APU BAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, APU COMPT FUSELAGE RIB CRACKED AT LEFT STA 2669.52 AS MARK. APU COMPT FUSELAGE RIB AT STA 2669.52 CRACK REPAIRED AS PER SRM 51-40-03 FIG 1. 2L74 4F RTA20WE 20050105000492005010500049NM 2005 1 5 UPS04442808 120040712A5720 FITTING BOEING747 747200 1384847NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C, LEFT WING - BS 1241 LONGERON FITTING ATTACH BOLT HOLE NR 6 FOUND CORRODED. FX - LEFT BS 1241 AREA BETWEEN EXTERNAL & INTERNAL LONGERON FITTING ATTACH NR 6 BOLT HOLE CORROSION CLEANED BY OVERSIZE .0156 INCH AND NR 6 ATTACH BOLT. ALSO REPLACED AS PER MM 20-51-01 AND SRM 51-30-05 PG 13. 2L74 4F RTA20WE 20050105000522005010500052NM 2005 1 5 UPS04243150 120040922A323365178197 ACTUATOR BOEING727 72731C 1384011NM RT MLG BROKEN A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01926UP 19233 INSPECTION TYPE:N/A ON APPROACH RIGHT MAIN UPLOCKED LIGHT GEAR DOOR LIGHT REMAINED ON. RECYCLED ONCE, LIGHTS STILL ON, MANUALLY CRANKED RIGHT GEAR DOWN. REPLACED RIGHT MLG LOCK ACTUATOR, PERFORMED MAIN GEAR EXTENSION AND RETRACTION ADJ/TEST W/R/T MM 32-32-00. 2L73 4F A3WE 20050105000532005010500053NM 2005 1 5 UPS04243172 120040914A5730 PANEL BOEING727 727173C 1384059NM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, RIGHT WING UPPER SURFACE T/E PANEL DELAM ON UPPER SURFACE AT I/B AFT CORNER. PANEL REPLACED IAW MM 20-80-01. 2L73 4F A3WE 20050105000572005010500057NM 2005 1 5 UPS04243177 120040909A5523 TAB BOEING727 727173C 1384059NM RT ELEVATOR DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, DELAMINATION FOUND ON RIGHT ELEVATOR TAB. REPLACED RIGHT ELEVATOR TAB. 2L73 4F A3WE 20050105000612005010500061NM 2005 1 5 UPS04443320 120040930A5730 SKIN BOEING747 747121 1384871NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, RIGHT BS 1241 WL 178 WING REAR SPAR UPPER SPLICE FITTING AREA FOUND HOLE NR 11 CRACKED AT WING UPPER SKIN. CRACKED HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2L74 4F A20WE 20050105000622005010500062 2005 1 5 UPS04M43431 420041101A2565 WARNING LIGHT DOUG MD11 MD11F 3023600NM R1 SLIDE ILLUMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01271UP 48572 INSPECTION TYPE:N/A, R1 SLIDE LOW PRESS LIGHT INOP. VERIFIED SYS PRESS, OK FOR SERVICE PER DMP 25-61-2. 2L73 4F RTA22WE 20050105000642005010500064 2005 1 5 UPS04M43432 420041031A2565 LIGHT DOUG MD11 MD11F 3023600NM L1 EVAC SLIDE INCORRECT A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01274UP 48575 INSPECTION TYPE:N/A, L1 DOOR SLIDE PRESS TO TEST INDICATION SYSTEM INOP. CHECKED CONTINUITY OF PRESS SWITCH. NO CONTINUITY ON SWITCH. PRESS SWITCH & BOTTLE PRESS OK PER WDM 25-61-01. FOUND WRONG BULBS INSTALLED IN REMOTE PRESS INDICATOR & HIGH RESISTANT SHORT ON JACK CAUSING LIGHT TO ILLUM VERY DIM SHORTENING BATTERY LIFE. REPLACED L1 EVAC SLIDE. 2L73 4F RTA22WE 20050105000652005010500065WP 2005 1 5 UPS04843137 120040914A57209890103502 DOUBLER DOUG DC8 DC871F 302199DWP STUB WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 INSPECTION TYPE:C3, UPON REMOVAL OF STUB WING NR 4 FOUND AT TRAILING EDGE OF STUB WING INTERNAL DOUBLER CRACKED AT STA XW406 RIGHT WING. REPAIRED NR 4 STUB WING INTERNAL DOUBLER IAW DC-8 SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20050105000662005010500066EU 2005 1 5 MALA040785 120041024A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING OUTBOARD LIFT SPOILER SEAL IS WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000672005010500067EU 2005 1 5 MALA040790 120041027A7130 FIRESHIELD BAC 146 AVRO146RJ85A1500097EU NR 2 ENGINE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND CHAFING ON NR 2 ENGINE LEFT ZONE 2 COWLING IN FIRE SHIELD PANNED AREA. MAINTENANCE REPAIRED IAW SRM 51-71-12. AIRCRAFT WAS RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20050105000682005010500068EU 2005 1 5 MALA040786 120041020A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING LIFT SPOILERS (3X) ROLL SPOILER & WING TO FLAP TAB TRAILING EDGE SEALS CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000692005010500069EU 2005 1 5 MALA040803 120041011A5320 BEAM SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND O/B BEAM BETWEEN STA 258.0 AND 272.0 CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20050105000712005010500071EU 2005 1 5 MALA040791 120041030A5315 FLOORBEAM BAC 146 AVRO146RJ85A1500097EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK INSPECTION, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT FRAME 18. REPAIRED IAW EO A53026. AIRCRAFT RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20050105000722005010500072EU 2005 1 5 MALA040776 120041008A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT SPOILER DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, LEFT MID GROUND SPOILER SEAL STRIP DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20050105000742005010500074EU 2005 1 5 MALA040782 120041024A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING INBOARD LIFT SPOILER SEAL IS WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000762005010500076EU 2005 1 5 MALA040783 120041024A5755 SEAL BAC 146 AVRO146RJ85A1500097EU LT SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT WING TRAILING EDGE SEAL IS WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000772005010500077EU 2005 1 5 MALA040788 120041013A7130 FIRESHIELD BAC 146 AVRO146RJ85A1500097EU NR 2 ENGINE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND NR 2 ENGINE ZONE 2 OUTBOARD COWL HAS A CHAFE IN THE FIRE PAN. REPAIRED IAW SRM 51-71-12. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000802005010500080EU 2005 1 5 MALA040787 120041020A5311 FRAME BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND CRACK ON DIAGONAL FRAME IN AIRBRAKE COMPARTMENT FWD OF AIRBRAKE AND AFT OF FRAME 50 LOWER CROSS MEMBER 5 INCHES FROM BOTTOM CORNER OF FRAME. REPAIRED IAW SRM 51-71-11. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000812005010500081EU 2005 1 5 MALA040789 120041017A2710 ACTUATOR BAC 146 AVRO146RJ85A1500097EU LT & RT AILERON CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND LEFT & RIGHT AILERON QUADRANT LINEAR ACTUATOR RUBBING AGAINST FLOOR INTERCOSTAL. REPAIRED IAW EO A53206. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000832005010500083EU 2005 1 5 MALA040779 120041007A5753 SKIN BAC 146 AVRO146RJ85A1500097EU T/E FLAP DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, LT FLAP TOP SKIN FOUND DAMAGED. MAINTENANCE REPAIRED IAW EO A57079. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20050105000842005010500084EU 2005 1 5 MALA040801 120041011A5720 RIB SAAB SF340 340B 7860101EU PANEL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PANEL 612AR 4 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. AIRCRAFT RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20050106000022005010600002EU 2005 1 6 MALA040891 120041124A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, SEAT TRACK I/B FLANGE AT FS 294 AND LBL 18.3 IS CORRODED OUT OF LIMITS AND WAS REPAIRED IAW SRM 53-70-60 AND MESABA 30 53079. ANGLE ATTACHED TO FWS END OF TRACK WAS REPLACED DUE TO HEAVY CORROSION DAMAGE. AIRCRAFT RETURNED TO SERVICE 11/28/04. 2L72 4T RTA52EU 20050106000042005010600004EU 2005 1 6 MALA040890 120041124A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, SEAT TRACK FLANGE AT FS 294, AT BL 0 IS CORRODED. CORROSION ON SEAT TRACK IS WITHIN LIMITS IAW SRM 53-70-60 AFTER REMOVED. ANGLE ON FWD END F/O SEAT TRACK WAS REPLACED DUE TO HEAVY CORROSION DAMAGE. AIRCRAFT RETURNED TO SERVICE 11/28/04. 2L72 4T RTA52EU 20050106000052005010600005EU 2005 1 6 MALA040892 120041124A53207259721389 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, FLOOR WEB P/N 7253721-389 CORRODED OUT OF LIMITS AT FS 294 AT BL 0 & LBL 10.0. DAMAGE WAS REPAIRED IAW SRM 53-70-30. 2L72 4T RTA52EU 20050106000062005010600006EU 2005 1 6 MALA040894 120041129A5320 ANGLE BAC 146 AVRO146RJ85A1500097EU AFT CARGO BAY CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15515XJ E2333 DURING C-CHECK INSPECTION IN YYC, AFT CARGO PIT GILLINER ATTACH ANGLE AT FRAME 35 RT STRINGER 34 IS CRACKED. MAINTENANCE REPAIRED IAW EO A53235. AIRCRAFT RETURNED TO SERVICE 12/5/04. 2H74 4F RTA49EU 20050106000072005010600007EU 2005 1 6 MALA040835 120041123A5755 STRUCTURE BAC 146 AVRO146RJ85A1500097EU LT SPOILER WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, LT I/B LEADING EDGE SPOILER SCREW HOLES WORN. MAINTENANCE REPAIRED IAW EO A57084. AIRCRAFT RETURNED TO SERVICE 11/23/2004. 2H74 4F RTA49EU 20050106000082005010600008EU 2005 1 6 MALA040847 120041123A5321 FLOORBOARD BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, PASSENGER COMPARTMENT FLOORBOARD, P/N HC532H0192-002 HAS CORRODED INSERTS AND EDGE DAMAGE (FLOORBOARD 231AF). MAINTENANCE REPAIRED IAW BAE 146 SRM 51-46-00. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20050106000092005010600009EU 2005 1 6 MALA040780 120041011A5320 INTERCOSTAL BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, FLOOR INTERCOSTAL AT AILERON BELLCRANK DAMAGED. MAINTENANCE FERRIED AIRCRAFT TO MSP FOR REPAIR. DURING MAINTENANCE FOUND FLOOR STIFFENER UNDER COCKPIT FLOOR AT AILERON BELLCRANK (LEFT) DAMAGED DUE TO INTERFERENCE WITH AILERON BELLCRANK PUSH-PULL ROD CONNECTING BOLT FOR AILERON POSITION TRANSMITTER. REPAIRED STIFFENER IAW EO A53204, DURING MAINT REMOVED AND REINSTALLED LT CONTROL COLUMN PUSH PULL AND AILERON POSITION SENSOR REF 409 204217 FOR DETAIL. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20050106000112005010600011NM 2005 1 6 0412001 120041215A2612 FIRE WARNING BOEING737 737230C 1384472NM PWA JT8 JT8D15 52051NE COCKPIT ACTIVATED A MJYAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07737TW 20257 FLIGHT 9604 - WHILE EN ROUTE (CRUISE) FROM ATL TO ADS AN UNSCHEDULED LANDING IN SHV WAS ENCOUNTERED DUE TO NR 1 ENGINE FIRE LIGHT ILLUMINATION AND THE FIRE BELL RINGING. FOLLOWED THE AAC QRH MEMORY ITEMS AND UPON PULLING FIRE HANDLE THE LIGHT EXTINGUISHED. DECLARED EMERGENCY AND DIVERTED TO SHV. UPON LANDING FIRE AND RESCUE DID NOT OBSERVE ANY FIRE OR SMOKE. 2L72 4F4 F A16WE E2EA 20050106000122005010600012WP 2005 1 6 MWEA040221 120041218A3610 CLAMP DOUG DC9 DC981 3022081WP RT ENGINE DEFECTIVE A MWEAO OTHER J WARNING INDICATION DEDESCENT 1 GL31807ME 48033 DURING LEVEL OFF, RIGHT ENGINE FIRE WARNING SOUNDED. REMOVED AND REPLACED 13TH STAGE SADDLE DUCT END CAP CLAMP. 2L72 4F A6WE 20050106000152005010600015NM 2005 1 6 MWEA040224 120041223A2720 WARNING SYSTEM BOEING717 717200 1383700NM COCKPIT FALSE ACTIVATIONA MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31914ME 55177 RUDDER LIMITER FAULT ILLUMINATED. COMPLIED WITH QUICK REFERENCE HANDBOOK (QRH) AND MANUAL OPERATION NORMAL. PERFORMED FAULT ISOLATION MANUAL (FIM) TASK 27-20-804-805 AND NO FAULT FOUND. PERFORMED FIM 27-20-811, AMM TASK 27-26-01-820-802 AND 27-26-03-820-801 AND NO FAULT OR ADJUSTMENTS MADE. 2L72 4F TRA6WE 20050106000162005010600016NM 2005 1 6 MWEA040225 120041223A2730 CLEVIS BOEING717 717200 1383700NM ELEVATOR BINDING A MWEAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL31912ME 55175 CREW NOTED BINDING IN THE ELEVATOR CONTROLS. FOUND MINOR CONTACT ON ELEVATOR STANDBY LOOP CLEVIS AND TENSION CLEVIS LINKS AT CABLE RUNS 5B AND 6B. PERFORMED ENGINEERING TECHNICAL ACTION (ETA) 0318; REFERENCE BOEING COMMUNICATION 1-56549321. 2L72 4F TRA6WE 20050106000202005010600020NM 2005 1 6 P5CA0401285 120041212A3241 MODULE BOEING747 747123 1384873NM ANTI-SKID SYS MALFUNCTIONED A P5CAK NONE O OTHER LDLANDING 1 EA15858FT 20109 AFTER LANDING TOWER REPORTED SUSPECTED BLOWN TIRES. AT BLOCKS, FOUND NR 10 & 12 TIRES BLOWN. ON CONDITIONAL INSPECTION FOUND DAMAGE TO RT UPPER AFT WING/BODY FAIRING BETWEEN STA 1540 AND 1580. ALSO FOUND DAMAGE TO RT INBD TRAILING EDGE MID FLAP. REPLACED NR 10 & 12 TIRES. REPLACED NR 9 & 11 TIRES DUE ON SAME AXLES AS FAILED TIRES. REPAIRED RT UPPER AFT WING/BODY FAIRING PANEL PER SRM 53-40-12. REPAIRED RT INBD MID FLAP PER 51-40-12. REPLACED ANTI-SKID CONTROL MODULE PER MM 32-42-02. OPS & LEAK CHECK OK. 2L74 4F A20WE 20050106000222005010600022NM 2005 1 6 P5CA0401282 120041207A80117755507 STARTER BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 2 ENGINE FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15451PA 30809 706214 NR 2 ENGINE NO ROTATION ON START. REPLACED STARTER MOTOR PER MM 80-11-02. 2L74 4F4 FRTA20WE E23EA 20050106000232005010600023NM 2005 1 6 P5CA0401284 120041210A7830 THRUST REVERSER BOEING747 747283B 1384867NM NR 4 ENGINE MALFUNCTIONED A P5CAK NONE J WARNING INDICATION CRCRUISE 1 EA15921FT 21575 NR 4 ENGINE THRUST REVERSER OPERATING LIGHT CAME ON IN FLIGHT. NO ADVERSE INDICATIONS. REPLACED PDU, NO HELP REV INOP. TRANSFERRED TO DMI 33496 PER MEL 78-2A. PLACARD INSTALLED. 2L74 4F A20WE 20050106000272005010600027NM 2005 1 6 P5CA0401295 120041228A2913 PUMP BOEING747 747123 1384873NM NR 4 ENGINE LEAKING A P5CAK NONE K FLUID LOSS CLCLIMB 1 EA15858FT 20109 NR 4 HYDRAULIC QUANTITY WENT TO ZERO IN CLIMB. FOUND HYDRAULIC LEAK ON NR 4 ENG EDP. REMOVED EDP AND INSTALLED HYDRAULIC PUMP FROM THE NR 3 ADP POSITION. OPS AND LEAK CHECK OK. NR 3 ADP DEACTIVATED PER MEL 29-2A. 2L74 4F A20WE 20050106000282005010600028WP 2005 1 6 P9RA20040058 120041223A3350101191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1114816 49370 A/C IN SYR, PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. 2L72 4F A6WE 20050103001442005010300144NM 2005 1 3 04FDEA03475 120041223A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 1421. REPAIRED AS PER SRM 53-70-00 FIG I & SRM 51-31-01 VOL II. REFER TO SNRM N2547 FOR WORK DETAILS. 2L73 4F RTA22WE 20050103001462005010300146NM 2005 1 3 04FDEA03477 120041223A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE SCRATCHED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1541 TO STA 5-73. REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SEAT TRACK FABRICATED AS PER DRAWING A5A7084 & INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I & SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050103001522005010300152NM 2005 1 3 04FDEA03487 120041227A5320 CLIP DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 AFT FUSELAGE COMPARTMENT - DOG HOUSE CANT STA Y=2046 FRAME CLIP P/N AJC7021-11, CRACKED. 2L73 4F RTA22WE 20050103001552005010300155NE 2005 1 3 04FDEA03453 220041220A7200 ENGINE AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 2 MALFUNCTIONED A FDEAF ACTIVATE FIRE EXT. RAJPARTIAL RPM/PWR LOSS FLAME/FIRE WARNING INDICATION TOTAKEOFF 1 SO25801FD 539 AT 1200 FT ON T/O, NR 2 ENGINE SEVERE COMPRESSOR STALLS. TOWER REPORTED FLAME FROM RIGHT ENGINE IN FLIGHT. PERFORMED ENGINE FIRE CHECKLIST NR 2. RETURNED TO LAND, IND WEIGHT 216.0. FIRE HANDLE PULLED, 1ST AGENT DISCHARGED. EPR/EGT EXCEEDENCE MESSAGES ON ECAM. IT WAS DETERMINED THAT THE ENGINE NEEDS TO BE REPLACED DUE TO EPR AT 1.37 WHEN THE SURGE HAPPENNED. 2L72 4F RTA35EU E24NE 20050103001582005010300158NM 2005 1 3 04FDEA03456 120041221A7830 TRACK DOUG MD11 MD11 3023602NM THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 ENGINE NR 2 LEFT HAND THRUST REVERSER UPPER SLIDER TRACK AFT EDGE FOUND WITH SUSPECT CRACK. CRACK REPAIRED REF FAA FORM 8130-3. 2L73 4F RTA22WE 20050103001602005010300160NM 2005 1 3 04FDEA03460 120041222A5310 DOOR FRAME DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 AFT CARGO DOOR AFT JAMB CORRODED AROUND FASTENERS 5 PLACES. AFT CARGO DOOR AFT JAMB CORRODED AREA REPAIR CARRIED OUT AS PER SRM 53-00-01 VOL I. 2L73 4F RTA22WE 20050103001642005010300164NM 2005 1 3 USAA040921 120041027A532069771901 BRACKET BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - BRACKET, 1 INCH CRACK, STA 927 AT 24.7L SUPPORT BRACKET. MANUFACTURED PART AND INSTALLED IAW SRM 51-41 AND MFG DWG 69771901. 2L72 4F4 FRTA16WE E21EU 20050103001652005010300165NM 2005 1 3 USAA040853 120041021A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 FRAME .2500 INCH LONG CRACK BS 360 ON FRAME BETWEEN S8L AND S9L. INSTALLED REPAIR ANGLES IAE TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E2GL 20050103001682005010300168NM 2005 1 3 USAA040930 120041112A5320 GUSSET BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - GUSSET, .7500 INCH CRACK, BS 927 UNDER RT IB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20050103001822005010300182NM 2005 1 3 SB04124 120040916A33501012721 LIGHT BOEING737 7373B7 1384580NM CABIN UNSECURE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19518AU 23704 PHL - PILOT REPORTED THE EMERGENCY EXIT LIGHTS ON SEAT 10A INOPERATIVE. MAINTENANCE SECURED THE EMERGENCY EXIT LIGHTS ON SEAT 10A. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050104000052005010400005EA 2005 1 4 ASOA04873 120041102A5260601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27853AS12486 7374 DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW AMM 52-11. 2L72 4F4 FRTA21EA E15NE 20050104000112005010400011EU 2005 1 4 ASOA04922 120041102A5320 DOUBLER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING C-CHECK INSPECTION, CORROSION BEYOND LIMITS WAS FOUND ON PL DOUBLER (GUSSET) BETWEEN LT HAND STRINGER 20 AND 21 AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE CORRODED DOUBLER (SUSSET) IAW SRM 51-21-42 AND 51-25-01. 2H72 4T4 TRTA53EU E20NE 20050104000122005010400012EA 2005 1 4 ASOA04940 120041123A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE COCKPIT CRACKED A ASOAK NONE O OTHER CRCRUISE 1 SO27850AS12648 7355 DURING CRUISE, THE RT FWD WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND THE CREW INITIATED A DESCENT TO 10,000 FT AND REDUCED AIRSPEED TO 250 KNOTS. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT FWD WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000222005010400022EA 2005 1 4 ASOA04906 120041116A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING A C-CHECK, THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 IAW EO 600-53-0070. 2L72 4F4 FRTA21EA E15NE 20050104000232005010400023EU 2005 1 4 ASOA04890 120041108A3397M22759 WIRE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27533AS 460 AFTER LANDING, THE EMERGENCY LIGHTS OVER BOTH FLIGHT ATTENDANT`S JUMP SEATS ILLUMINATED UNCOMMANDED. MAINTENANCE RESECURED THE WIRES TO CONNECTOR PLUG P.8 ON THE FLIGHT ATTENDANT`S PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050104000242005010400024EA 2005 1 4 ASOA04907 120041116A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO 600-53-0072. 2L72 4F4 FRTA21EA E15NE 20050104000382005010400038EA 2005 1 4 ASOA04909 120041117A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27866AS 7517 DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20050104000422005010400042EA 2005 1 4 ASOA04943 120041126A5260601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27884AS 7513 DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. 2L72 4F4 FRTA21EA E15NE 20050104000502005010400050WP 2005 1 4 04FDEA03334 120041202A2450 CIRCUIT BREAKER DOUG DC10 DC1010 3022110WP COCKPIT FAILED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO2568060 46970 ON CLIMB-OUT PASSING 15,000, NR 1 CADC FAILED FOLLOWED BY L EMER A/C BUS OFF. FOLLOWED RED TABS L EMER A/C BUS CIRCUIT BREAKER POPPED. RETURNED TO FLL. CADC SWITCH WOULD NOT PICK UP CAPT'S INSTURMENTS WHEN BOTH ON 2 SELECTED. REMOVED AND REPLACED L EMER AC BUS RCCB R1-136 IAW MM 24-50-01-2. REMOVED AND REPLACED L EMER AC BUS CIRCUIT BREAKER PRECAUTIONARY IAW SMP, ALL ASSOCIATED INSTRUMENTS AND CADC SWITCHING. OPS CK'D NORMAL AIRCRAFT OK FOR SERVICE. 2L73 4F A22WE 20050104000552005010400055NM 2005 1 4 04FDEA03303 120041201A5744 HINGE DOUG MD11 MD11 3023602NM LT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. 2L73 4F RTA22WE 20050104000562005010400056NM 2005 1 4 04FDEA03316 120041201A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. 2L73 4F RTA22WE 20050104000572005010400057NM 2005 1 4 04FDEA03380 120041207A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 PAGES 442-443. 2L73 4F RTA22WE 20050104000672005010400067NM 2005 1 4 04FDEA03224 120041125A5320 SPLICE DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO, LONGERON SPLICE CRACKED AT STA 1531/5-123 LONGERON 38L. REMOVED AS PER SRM 51-31-01 VOL II. FABRICATED NEW LONGERON SPLICE AS PER DRAWING A5A7114. FPI CARRIED OUT AS PER DPS 4.707 ON NEW LONGERON SPLICE AND FOUND NO CRACK EVIDENT. INSTALLED NEW LONGERON SPLICE AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050104000832005010400083EU 2005 1 4 04FDEA03176 120041121A5313A5398541521000 STRINGER AIRBUS310 A310 EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 THS BAY PROFIL STRINGER HAS 4" OF CORROSION FS 90 RT OVER TORQUE BOX. REMOVED T-PROFILE AT FS 90 ON UPPER RT EDGE BEAM THAT WAS CORRODED OUT OF LIMITS AND REPLACED IAW A310/200 SRM 51-72-10. 2L72 4F RTA35EU 20050104000952005010400095NM 2005 1 4 04FDEA03409 120041214A5514 STRUCTURE DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 EMPENNAGE, HORIZONTAL STAB LEFT HAND UPPER FORWARD PLANK NR 5L, BARREL NUT BORE CORROSION REWORKED. FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2L73 4F RTA22WE 20050104001002005010400100NM 2005 1 4 04FDEA03199 120041124A2611473925 CONTROL UNIT BOEING727 72722 1384002NM AFT CARGO BAY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25185FE 18871 LOWER AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. RAN QRH. DISCHARGED BOTTLE-1, LANDED IN LCK IN 20 MIN. SECOND BOTTLE DID NOT AUTO-FIRE AS PER 25 MIN REQUIREMENT. CFR CREWS DETERMINED NO FIRE PRESENT. FOUND ALL TEST LIGHTS ON AFT LOWER CARGO COMPARTMENT CEU, COULD NOT GET THEM TO GO OUT UNLESS C/B'S WERE PULLED, SUSPECT BAD AFT LOWER CARGO CEU. REMOVED AND REPLACED AFT LOWER CARGO CEU REF BOEING AMM CP 26-16-012-2. TESTS GOOD. REMOVED AND REPLACED NR 1 FIRE BOTTLE AND AFT PIT SQUIB REF BOEING AMM CP 26-16-014-2. OK FOR SERVICE. 2L73 4F A3WE 20050104001012005010400101WP 2005 1 4 04FDEA03186 120041123A5330 SKIN DOUG DC10 DC1010F 3022111WP FUSELAGE DAMAGED A FDEAO OTHER O OTHER UKUNKNOWN 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND DURING INSP, LWR FUS EXT STRUC EXISTING REPAIR (40 INCHES X 19 INCHES) STA 1781 TO STA 1821 RT SIDE BETWEEN L34 TO L38. SCRAP EXISTING REPAIR, DUE TO REPLACEMENT OF SKIN BELOW LONG 36, PERFORM A NEW REPAIR ON SKIN OVER LONG 36 PER SRM 53-20-00 FIG 6 SH 5, 6. 2L73 4F A22WE 20050104001022005010400102WP 2005 1 4 04FDEA03187 120041123A5313 LONGERON DOUG DC10 DC1010F 3022111WP FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT STA 959, FWD CARGO COMPT, STR 40 LT WITH DENT. CUT DAMAGED LONGERON BETWEEN STA 939/959 - 959/979 AND INSTALL TWO LONGERON SPLICE PER SRM 53-10-10 FIG 1, 2 VOL I (TYPE I), P/N S2929835, S2613996. 2L73 4F A22WE 20050104001102005010400110WP 2005 1 4 04FDEA03198 120041123A5413ASL0046 LONGERON DOUG MD10 MD1010F 3022112WP NR 3 COWLING CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25393FE 46627 NR 3 INBOARD COWLING UPPER LONGERON CHAFED UNDER RUB STRIP. FABRICATED AND INSTALLED DOUBLER IAW FEDEX EA 8-5410-81527, NACELLES/PYLON, NR 3 ENGINE INBOARD CORE COWL UPPER LONGERON, REPAIR. REFERENCE NON-ROUTINE N00471. 2L73 4F RTA22WE 20050104001272005010400127NM 2005 1 4 AALA20041253 120041227A335060030451 BATTERY PACK DOUG MD80 MD83 3023681NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219414W 53189 PHX - EMERGENCY LIGHTS AT ROWS 24, 25 AND 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR EMERGENCY LIGHTS AT ROWS 24, 25 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RT 20050104001482005010400148WP 2005 1 4 AALA20041256 120041224A3230 LANDING GEAR DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21968TW 53618 ORD - EN ROUTE PSP AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT COMPLETELY. RED NOSE GEAR LIGHT REMAINED ON AND GREEN NOSE GEAR WENT OUT. RETURNED ORD AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT PER MM 7-12-00-2, PERFORMED INSPECTION OF NOSE GEAR. NO FAULTS NOTED. DROP CHECKED NOSE GEAR THREE TIMES, NO FAULTS. GREASED NOSE GEAR WITH WTR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050104001592005010400159NM 2005 1 4 SWAA043721 120041227A532065C27314 STRINGER CLIP BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20050104001652005010400165NM 2005 1 4 SWAA043699 120041221A3350PH22300L COVER BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29655WN 28400 EEPLS PHOTOLUMINESCENT STRIP FROM ROW 6 DEF TO ROW 10 DEF, COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20050104001792005010400179NM 2005 1 4 SWAA043622 120041213A53106545833 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB FROM BS 330 TO BS 335, RBL 55, CORRODED. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050105000062005010500006NM 2005 1 5 DL764041134 120041223A21508252092 ACM BOEING767 767432ER 1385134NM A/C BAY SEIZED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27839MH 29712 UPON DESCENT AT APPROXIMATELY 27,000 FT, ADVISED BY THE CABIN CREW OF A SMOKEY HAZE IN THE CABIN, REPORTED TO SMELL ELECTRICAL. SMOKE AND FUMES PROCEDURES WERE APPLIED BUT SMOKE NEVER TOTALLY DISSIPATED. STATUS MSGS - LT PACK ACM AND FWD IFE COOLING. FOUND LEFT ACM SEIZED. REPLACED ACM AND RAN PACKS AND ENGINES. ALL CHECKS OK. 2L72 4F RTA1NM 20050105000132005010500013NM 2005 1 5 DLM88041127 120041221A2910AE7055381 HYDRAULIC LINE DOUG MD88 MD88 3023688NM LT ENGINE CRACKED A DALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO27911DL 49542 DURING CLIMBOUT LT HYD QTY DECREASED TO 1 QUART. REPLACED NUMBER 1 ENGINE HYD PUMP SUPPLY LINE. 2L72 4F RTA6WE 20050105000162005010500016NM 2005 1 5 DL75K041125 120041221A2120 BRACKET BOEING757 757232 1384965NM CABIN DISLODGED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27684DA 27104 AIR TURNBACK, A/C REPORTED SMOKE IN CABIN. SHUT DOWN RT PACK AND SMOKE AND SMELL DISSIPATED. MTC FOUND BRACKET DISLODGED FROM MAIN DISTRIBUTION DUCT ABOVE SEAT ROW 12. INSTALLED INTERN REPAIR PER ERA 095909-14. 2L72 4F RTA2NM 20050105000232005010500023NE 2005 1 5 DL73S041144 220041227A7321 FUEL CONTROL BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO27239WA47789 23187 709185 AT APPROX 9800 FT DURING MANUAL POWER ADVANCE NR 2 ENGINE COMPRESSOR STALLED. REPLACED FUEL CONTROL. 2L72 4F4 F A16WE E2EA 20050105000372005010500037NM 2005 1 5 04FDEA03432 120041217A5754 WEB BOEING727 727100 1384036NM L/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25151FE 19147 LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BATCH 0792675 (FILLERS) IAW SRM 57-30-4 FIG 5. REMOVED & REINSTALLED ANTI-ICE DUCT IAW MM 27-81-001-4. 2L73 4F RTA3WE 20050105000382005010500038NM 2005 1 5 04FDEA03433 120041217A5754 WEB BOEING727 727100 1384036NM L/E FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25151FE 19147 LT WING NR 3 L/E FLAP INBD ANTI-ICE DUCT CHAFING FLAP. REMOVED & REPLACED WEB IAW SRM 51-30-2, NEW WEB FABBED FROM 2024-T3 .050, BATCH 814135, FOUND INNER SKIN DAMAGED, CUT OUT AREA IAW SRM 57-30-4 FIG 5. FABBED & INSTALLED COVER & FILLER FROM 2024-T3 .016 BATCH 0792675 (FILLERS) IAW SRM 57-30-4 FIG 5. REMOVED & REINSTALLED ANTI-ICE DUCT IAW MM 27-81-001-4. 2L73 4F RTA3WE 20050105000402005010500040NM 2005 1 5 FX7A2004XXXX2 120041213A2781 POSITION SWITCH BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE L/E FLAP MISRIGGED A FX7AD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO1979749 22451 DURING TAXI OUT NR 4 LEADING EDGE FLAPS RIGHT DOES NOT HAVE A GREEN LIGHT ON THE F/E PANEL POSITION TEST, RETURNED TO THE GATE. TROUBLESHOT AND FOUND NR 4 LEADING EDGE FLAP POSITION SWITCH LEVER ARM MISALIGNED. ADJUSTED THE POSITION SWITCH LEVER ARM IAW MM REF 27-82-0, NOW OPERATES NORMALLY. 2L73 4F4 F A3WE E2EA 20050105000452005010500045EU 2005 1 5 UPS04143138 120040922A3350 SWITCH AIRBUSA300 A300F4622R 3930360EU CABIN DEFECTIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01127UP 0811 INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT DISARM WILL NOT COME ON, LIGHT TEST OK. REMOVED PANEL 436 VU, REPLACED EMERGENCY EXIT LIGHT SWITCH, INSTALLED PANEL 436 VU. OPS CHECK OF ALL SWITCHES AND LIGHTS ON PANEL 436 VU OK. 2L72 4F RTA35EU 20050105000512005010500051NM 2005 1 5 UPS04442810 120040714A5320 FITTING BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING NR 11 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 11 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE BOLT HOLE .0156 INCH AS PER SRM 51-30-05 AND MOUNT BOLT, ALSO REPLACED AS PER MM 20-51-01. 2L74 4F RTA20WE 20050105000542005010500054NM 2005 1 5 UPS04243173 120040914A5730 ACCESS PANEL BOEING727 727173C 1384059NM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, RIGHT WING ACCESS PANEL NR 8640 DELAM ALONG EDGE AND SUSPECT CRACK ON LWR SURFACE. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 51-40-20. 2L73 4F A3WE 20050105000592005010500059NM 2005 1 5 UPS04443318 120040929A5711 SPAR BOEING747 747121 1384871NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 INSPECTION TYPE:C, CRACK FOUND ON LT BS 1241 WL 170 TO 180 WING REAR SPAR WEB AT KICK FITTING AREA AT HOLE NR 2 BY APPROX .0625 INCH RUNNING O/B & DOWN. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032. 2L74 4F A20WE 20050105000702005010500070EU 2005 1 5 MALA040802 120041011A5320 RIB SAAB SF340 340B 7860101EU PANEL CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND PANEL 511BL HAD 9 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20050105000752005010500075EU 2005 1 5 MALA040781 120041020A5755 SEAL BAC 146 AVRO146RJ85A1500097EU RT SPOILER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND RIGHT WING CENTER LIFT SPOILER TRAILING EDGE SEAL WORN & CRACKED. REPAIRED IAW EO A57013. AIRCRAFT WAS RETURNED TO SERVICE 10/27/04. 2H74 4F RTA49EU 20050105000782005010500078EU 2005 1 5 MALA040805 120041011A5320 BEAM SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND I/B BEAM BETWEEN STA 258.0 AND 272.0 CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20050105000822005010500082EU 2005 1 5 MALA040809 120041011A5320 WEB SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15449XJ 340B449 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND WEB BETWEEN FRAMES 288.0 AND 299.0 CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-21. AIRCRAFT WAS RETURNED TO SERVICE 10/12/04. 2L72 4T RTA52EU 20050106000102005010600010EU 2005 1 6 MALA040778 120041008A5743 ANGLE BAC 146 AVRO146RJ85A1500097EU MLG CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, MLG CENTER SECTION BAFFLE ATTACHMENT TOP SIDE ANGLE CRACKED. MAINTENANCE REPAIRED IAW SRM 51-42-00, 51-18-00, 51-23-00, 51-24-11, 51-31-00, 53-20-16 FIG 3 SHEET 2. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20050106000142005010600014WP 2005 1 6 MWEA040226 120041224A3397 WIRE DOUG DC9 DC981 3022081WP CABIN DAMAGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31803ME 48029 FLOOR LIGHTING ACROSS FROM FORWARD LAVATORY IS INOPERATIVE. REPAIRED WIRE. 2L72 4F A6WE 20050106000192005010600019WP 2005 1 6 0401579915 120040803A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01965N 47417 DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 20. REPAIRED PER EA 99-200164. 2L72 4F A6WE 20050106000242005010600024NM 2005 1 6 P5CA0401293 120041224A2910 HYDRAULIC LINE BOEING747 747283B 1384867NM HYDRAULIC SYS LEAKING A P5CAK NONE K FLUID LOSS UKUNKNOWN 1 EA15921FT 21575 NR 3 HYD SYS LOST 2 GALS IN THIS FLIGHT FROM UAM-HIK. FOUND LINE LEAKING FROM CASE DRAIN FOR NR 3 EDP. REMOVED EDP DUE TO LEAK. ITEM TRANSFERRED TO DMI 33554 PER MEL 29-1A. 2L74 4F A20WE 20050106000252005010600025NM 2005 1 6 P5CA0401292 120041226A2820 VALVE BOEING747 74746NF 13848BTNM GE CF6 CF650C2 30018NE NR 2 DIRTY A P5CAK NONE J WARNING INDICATION NRNOT REPORTED 1 EA15452PA 30810 706220 ENGINE NR 2 FUEL VALVE MSG FUEL SPAR VLV 2 STATUS MSG. REMOVED NR 2 FUEL SPAR VALVE. CLEANED SHAFT AND REINSTALLED SPAR VALVE. OPERATION CHECKS OK PER MM 28-22-01. 2L74 4F4 FRTA20WE E23EA 20050106000292005010600029WP 2005 1 6 P9RA 120041223A3350101191 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1114816 49370 A/C IN SYR. PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. 2L72 4F A6WE 20050106000302005010600030NM 2005 1 6 P9RA20040055 120041212A25606500994001 CAP BOEING757 757236 1384971NM R1 DOOR INOPERATIVE A P9RAK NONE O OTHER NRNOT REPORTED 1 SO11522NA 25133 CLE PIREP, GIRT BAR CIRCUIT BREAKER POPPED AND WOULD NOT RESET. MAINTENANCE ASSIGNED TO MEL 25-66-5 FOR R1 SLIDE GIRT BAR LIGHT. MAINTENANCE ACTION ON 12-14-2004 REF MEL 25-66-5. REMOVED AND REPLACED R1 SLIDE LIGHT CAP ASSEMBLY PER MM. CLEARED MEL. 2L72 4F RTA2NM 20050106000322005010600032NM 2005 1 6 249TR0097 120041222A5347 GALLEY TRACK BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 RIGHT OUTBOARD GALLEY TRACK CORRODED FOR G-2 GALLEY. REPLACED SECTION OF TRACK PER BOEING DRAWING 65-45834 AND SRM 53-10-2 AND 51-10-2. 2L72 4F RTA16WE 20050106000332005010600033 2005 1 6 249TR0101 420041222A2230734SUE23 COMPUTER BOEING737 7372K5 138448XNM AUTOTHROTTLE SYSFAULTY A PIDAK NONE J WARNING INDICATION ININSP/MAINT 1 SO05249TR 22598 AUTO THROTTLE FAILS STEP A; SHOWS AF6 FAULT CODE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101. 2L72 4F RTA16WE 20050106000362005010600036NM 2005 1 6 249TR0039 120041222A5315 FLOORBEAM BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 BS 986 FLOORBEAM HAS CORROSION AT SEVERAL FLOORBOARD ATTACH HOLES ON UPPER AND LOWER SURFACE OF FLANGE. REPAIRED PER EA 53-343. 2L72 4F RTA16WE 20050106000392005010600039NM 2005 1 6 249TR0063 120041222A5320 CHANNEL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 HAT CHANNEL FOR AFT LAVATORY FORWARD WALL IS CORRODED. REPLACED HAT CHANNEL PER SRM 51-10-1 AND SRM 51-30-0. 2L72 4F RTA16WE 20050106000412005010600041NM 2005 1 6 249TR0072 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION ON INTERCOSTAL AT RIGHT COCKPIT DOOR POST. REPLACED INTERCOSTAL PER SRM 51-10-1. 2L72 4F RTA16WE 20050106000422005010600042NM 2005 1 6 750WL0012 120041215A335020131A BATTERY PACK BOEING757 757200 1384950NM CABIN DISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 EMERGENCY EXIT FLOOR LIGHTING NEXT TO L3 DOOR IS INOP. REPLACED BATTERY FOR INOP SECTION. OPS CHECKS GOOD PER MM 33-50. 2L72 4F RTA2NM 20050106000442005010600044NM 2005 1 6 249TR0088 120041222A5320 INTERCOSTAL BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 INTERCOSTAL AT RBL 8, BETWEEN BS 947.5 AND BS 927 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-0 AND 53-10-2. 2L72 4F RTA16WE 20050106000452005010600045SW 2005 1 6 PNSA041203 120041215A7603 POWER LEVER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP COCKPIT SEPARATED A PNSAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 AL03650PA AC775B DURING INTIAL TAKEOFF ROLL LEFT POWER LEVER REVERSE TRIGGER CAME LOOSE AND FELL IN QUANDRANT. FLIGHT CREW ABORTED TAKEOFF AND RETURNED TO GATE. 2L72 4T3 TRTA8SW E2WE 20050106000482005010600048NM 2005 1 6 QXEA200400884 120041214A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - COUNTER SINKS CHAFED AT LEFT WING FUEL PANEL 523AT. HEAVIEST AT INBOARD AND OUTBOARD ENDS. REPLACED IAW Q400 WC 500ME28 60266. 2H72 4T RTA13NM 20050106000502005010600050NM 2005 1 6 QXEA200400882 120041213A2820 FUEL LINE BOMBDRDHC8 DHC8401 1390041NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - FUEL FEED LINE INSIDE LEFT WING PANEL 523AT IS CHAFED BY EJECTOR MOTIVE FLOW LINE. REPAIRED IAW HORIZON AIR EA 6-28-14. 2H72 4T RTA13NM 20050106000512005010600051NM 2005 1 6 QXEA200400922 120041227A2450 ELECTRICAL SYS BOMBDRDHC8 DHC8401 1390041NM COCKPIT MALFUNCTIONED A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09406QX 4048 SEA - LEFT MAIN BUS FAILED WHILE ON GROUND. RESET BUS FAULT PER EMERGENCY CHECKLIST, EVERTHING NORMAL. MAINTENANCE PERFORMED OPERATIONAL TEST OF THE MAIN 28V DC GENERATION SYSTEM. NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST AND DATA RETRIVAL FROM EPCU. NO DEFECTS OR FAULTS NOTED. OPERATIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050106000532005010600053NM 2005 1 6 QXEA200400921 120041223A6123YD4N SENSOR DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS INOPERATIVE A QXEAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM09358PH 506 SEA - ON FLIGHT NUMBER 2212, ABORTED TAKEOFF DUE TO AUTOFEATHER ARM FAILURE PRIOR TO ROTATION. MAINTENANCE REMOVED AND REPLACD RELAYS 6121-K2 AND 6121-K5 AND NR 1 ENGINE TSCU. ALL AUTOFEATHER OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050106000542005010600054EA 2005 1 6 QXEA200400920 120041223A4970 WARNING SYSTEM CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 NM09606QX 10023 DEN - ON FLIGHT NUMBER 4321, UPON APU STARTUP RECEIVED APU OVERTEMP WARNING. COMPLETED CHECKLIST. MAINTENANCE PERFORMED APU STARTUP ON RAMP, APU STARTED NORMALLY. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050106000562005010600056NM 2005 1 6 QXEA200400864 120041127A5330 DOUBLER BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND EXTERIOR LAVATORY SOURCE DOOR EXTERNAL DOUBLER HAS CORROSION IN PAINT CHIP AT STATION X-5 AND STRINGER 26S. REPAIRED IAW SRM 51-14-00-100-001. 2H72 4T RTA13NM 20050106000592005010600059NM 2005 1 6 QXEA200400878 120041214A33506104781 POWER SUPPLY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09359PH18371301 514 SEA - VARIOUS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY NR 4. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050106000612005010600061NM 2005 1 6 QXEA200400879 120041215A3411 LINE BOMBDRDHC8 DHC8401 1390041NM PITOT/STATIC SYSDIRTY A QXEAO OTHER GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 NM09404QX 4046 GEG - ON FLIGHT NUMBER 2395, WHILE IN CRUISE, IAS MISMATCH APPEARED ON BOTH PFD'S. NR 2 IAS STUCK ON 250 KTS WHILE NR 1 IAS AND STANDBY IAS WERE IN AGREEMENT. YD THEN QUIT AND AP DISENGAGED. THEN GOT PITCH TRIM, ELEVATOR FEEL, SPOILER OUTBOARD, ROLL SPOILER OUTBOARD AND RUD CAUTION LIGHTS. PERFORMED EMERGENCY CHECKLIST AND SLOWED AIRCRAFT TO 200 KTS, ALL CAUTION LIGHTS STAYED ON UNITL OAT REACHED -9 DEG, THEN ALL WENT OUT. MAINTENANCE C/W NR 1 AND NR 2 PITOT STATIC LINE CLEANING. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050106000622005010600062NM 2005 1 6 QXEA200400867 120041204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND FUSELAGE SKIN HAS TWO PITS LOCATED AT FUSELAGE STATION X233 BETWEEN STRINGERS 16R AND 17R. REPAIRED IAW SRM TASK 51-25-15-370-801 AND RD 8/4-53-1074. 2H72 4T RTA13NM 20050106000632005010600063NM 2005 1 6 QXEA200400868 120041204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND FUSELAGE SKIN AT STATION 237 AND STRINGER 16R HAS AREA OF SURFACE DAMAGE WITH ONE PIT. REPAIRED IAW SRM 51-26-10-150-801 AND RD 8/4-53-1074. 2H72 4T RTA13NM 20050106000642005010600064NM 2005 1 6 QXEA200400869 120041204A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND FUSELAGE SKIN AT STATION X239 AT STRINGER 16R HAS AREA OF SURFACE DAMAGE WITH ONE PIT. REPAIRED IAW SRM TASK 51-25-15-370-801, RD 8/4-53-1074 AND HORIZON AIR EA 6-53-479. 2H72 4T RTA13NM 20050106000652005010600065SO 2005 1 6 RAIA00412016 120041212A3080 DETECTOR EMB 145 EMB145LR 3260212SO ANTI-ICE SYS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03814HK 145046 STL - ICE DETECTORS 1 AND 2 FAILED DURING TAXI OUT. MAINTENANCE OPS CHECK ICE DETECTORS, OPS CHECK GOOD. 2L72 4T RTT00011AT 20050106000662005010600066SO 2005 1 6 RAIR00412021 120041213A801135059105 STARTER EMB 145 EMB145LR 3260212SO NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03814HK547 145046 STL - NR 1 ENGINE NO ROTATION ON START ATTEMPT. MAINTENANCE REMOVED AND REPLACED AIR TURBINE STARTER. 2L72 4T RTT00011AT 20050106000682005010600068NM 2005 1 6 SCNA04014 120041105A3350 LIGHT BOEING737 737800* NM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15PHHZX 28248 DURING FAA CONFORMITY, SECTION OF EMERGENCY FLOOR TRACK OUT AT ROW 19. REMOVED AND REPLACED FLEX LAMP IAW AMM 33-51-13. CHECKS GOOD. 2L72 4F RTA16WE 20050106000712005010600071NM 2005 1 6 AT0400026 120041213A324426130411 TIRE BOEING717 717200 1383700NM NR 3 MLG SEPARATED A ZZDAO OTHER O OTHER TOTAKEOFF 1 SO15945AT 55008 BLOWN RETREAD OFF NR 3 MLG TIRE ON TAKEOFF, FOD DAMAGE. REMOVED AND REPLACED NR 3 TIRE AND WHEEL ASSEMBLY. 2L72 4F TRA6WE 20050106000722005010600072 2005 1 6 YENA200463 420041222A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU ENTRTAINMENT SYSFAULTY A YENAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15519JB6852 5067 1398 ELECTRICAL SMOKE SMELL DETECTED BY F/A'S AND PAX IN ROW 26 SEAT C. RETURNED TO SJU. DURING RETURN LIVE TV MASTER SWITCH WAS TURNED OFF ALONG WITH CABIN CAMERA & WADL SYSTEMS. ELECTRICAL SMOKE SMELL SEEM TO DISAPPEAR AFTER THESE ACTIONS. AIRCRAFT WAS RELEASED PER MEL 25-22-03 CAT D, CONTROL L07467. UPON ARRIVAL AT JFK REACTIVTED LIVE TV SYSTEM AS PER INFO NOTICE 2004-T023TR SUB B, REMOVED AND REPLACED LTV SEB AT 26C AND REMOVED AND REPLACED LTV SEAT TO SEAT CABLE FROM 26C TO 25B AS PRECAUTIONARY. 2L72 4F RTA28NM 20050106000732005010600073EU 2005 1 6 YENA200464 120041225A25304110001137 PIN AIRBUS320 A320232 3930326EU COFFEE MAKER BURNED A YENAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15542JB9010 3225 1802 SMOKE SMELL REPORTED AROUND COFFEEMAKERS IN FWD GALLEY. FOUND BURNT PIN ON NR 2 COFFEEMAKER. AIRCRAFT RELEASED UNDER MEL 25-22-03 CONTROL L03922. UPON ARRIVAL AT JFK FIXED TRAY TO NR 2 COFFEEMAKER. REMOVED AND REPLACED NR 2 COFFEEMAKER AND OPS CHECK NORMAL. 2L72 4F RTA28NM 20050106000742005010600074EA 2005 1 6 04362679 120041227A2750 SEAL CNDAIRCL600 CL6002B19 1900309EA T/E FLAP LACK OF LUBE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED APAPPROACH 1 EA27679BR 7662 FLAP FAILURE AT 0. AIRCRAFT DIVERTED BECAUSE OF SNOW CONTAMINATION IN BOS. A/C FERRIED TO MX BASE. MX RETRIEVED CODES, CHECKED TORQUES ON FLAP DRIVE SYSTEM (GOOD), DETAILED INSPECTION OF FLEXIBLE DRIVE SHAFTS. REMOVED AND REPLACED TEFLON SEALS, CLEANED AND LUBED. SAFETIED FLEX SHAFTS AND RIGGED INBOARD FLAP. 2L72 4F RTA21EA 20050106000752005010600075EA 2005 1 6 04348632 120041213A3260 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA RIGHT OUT OF ADJUST A VTZAK NONE N FALSE WARNING CRCRUISE 1 EA27632BR 7268 WOW INPUT AND OUTPUT MESSAGE IN FLIGHT. MX ADJUSTED RT PROX SENSOR. 2L72 4F RTA21EA 20050106000762005010600076EA 2005 1 6 04350690 120041215A27409960013 SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT DEFECTIVE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA27690BR 7739 STAB TRIM FAILURE ON CLIMBOUT. MX REMOVED AND REPLACED PILOT'S PITCH TRIM DISCONNECT SWITCH. 2L72 4F RTA21EA 20050106000782005010600078EA 2005 1 6 04348706 120041213A3260 TARGET CNDAIRCL600 CL6002B19 1900309EA MLG LOOSE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27706BR 7553 GEAR UP DISAGREE MESSAGE ON TAKEOFF. LT MAIN GEAR DID NOT SHOW UP. MX ADJUSTED THE LOOSE MLG UPLOCK TARGET FOR PROX SENSOR AND PERFORMED NUMEROUS GEAR SWINGS. 2L72 4F RTA21EA 20050106000812005010600081NM 2005 1 6 2004UALA00816 120040831A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT WING SPINNING A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 RT WING UPPER SURFACE ENG NR 4 NACELLE UPPER LINK WING FITTING HAS 1 SPINNING FASTENER WS 1168. FASTENER REMOVED. HFEC OF HOLE, NO DEFECTS NOTED. INSPECTION OF STACK UP ACCOMPLISHED WITH NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NEW NUT. 2L74 4F4 FRTA20WE E24NE 20050106000822005010600082NM 2005 1 6 2004UALA01194 120041207A2751 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP29527UA 24995 UNPLANNED STOP DUE TO FLAP INDICATION. 2L72 4F4 FRTA2NM E17NE 20050106000832005010600083 2005 1 6 2004UALA01179 420041201A2565D3104220501 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN OVERSIZED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29537UA 25157 SLIDE TOO LARGE, AS MEASURED WITH TEMPLATE. SLIDE WAS PACKED INCORRECTLY AT OVERHAUL. WHEN SLIDE INSTALLATION WAS ATTEMPTED, IT WAS REJECTED DUE TO BEING OVERSIZE. SLIDE WAS NOT INSTALLED ON A/C. SLIDE WAS REPACKED PER AIR CRUISER CMM 25-66-01 AND MADE SERVICEABLE. 2L72 4F4 FRTA2NM E17NE 20050106000852005010600085NM 2005 1 6 2004UALA01264 120041229A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CREASE BEAM WEB CORRODED UPPER SURFACE STA 1385 TO 1397, RBL 68-71. 2L72 4F4 FRTA2NM E17NE 20050106000862005010600086 2005 1 6 2004UALA01265 420041229A2565 SLIDE BOEING777 777222 1385219NM PWA PW4077PW4077 NE R1 DOOR READS LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29773UA 26929 DOOR 1R SLIDE PRESSURE GAUGE IS 3 NEEDLE WIDTHS BELOW THE GREEN BAND. BOTTLE PRESSURE WAS OBSERVED WITHIN GREEN BAND. SLIDE/RAFT WAS DETERMINED TO BE SERVICEABLE AND WAS RETURNED TO SERVICE. 2L72 4F4 FRTT0001SE E46NE 20050106000872005010600087NM 2005 1 6 2004UALA01184 120041204A2933 WARNING LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT ACTIVATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29371UA 24540 FLIGHT RETURNED TO DEN DUE TO B-SYSTEM HYDRAULIC PRESSURE LIGHT. PROBLEM COULD NOT BE REPEATED ON GROUND. OPS CHECKED OK. NO UNITS REPLACED. 2L72 4F4 FRTA16WE E2GL 20050106000882005010600088NM 2005 1 6 2004UALA00811 120040803A5315 FLOORBEAM BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29781UA 26945 09MAY OAK CF -9 :FWD PIT FLOORBEAM UPPER AFT FLANGE CRACKED IN RADIUS APPROX BS 15 RBL 29. REPAIR INSTALLED PER 53-00-53, (INTERIM REPAIR) AND MUST BE REPLACED WITH A CAT-A OR CAT-B BEFORE 4000 FLIGHT CYCLES. MAJOR REPAIR ACCOMPLISHED. PERMANENT REPAIR ACCOMPLISHED THIS VISIT. 2L72 4F4 FRTT0001SE E46NE 20050106000902005010600090NM 2005 1 6 2004UALA00813 120040831A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 1 PYLON ROTATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 1 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING INBOARD & OUTBOARD ROW UPPER HORIZONTAL FASTENERS HAVE ROTATED (2 TTL FASTENERS). FASTENER REMOVED, HFEC ON HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NUT. 2L74 4F4 FRTA20WE E24NE 20050106000942005010600094NM 2005 1 6 2004UALA01229 120041219A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE BS680 TO BS740 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CABIN FLOOR, RT CREASE BEAM I/B CHORD ANGLE CORRODED AT BS 680 TO BS 740 BL 66R. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED CREASE BEAM I/B CHORD ANGLE AND REINSTALLED WITH NEW PART. 2L72 4F4 FRTA2NM E17NE 20050106000962005010600096NM 2005 1 6 2004UALA01231 120041219A2121 FAN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP29324UA 23956 LANDED UNDER AMBER ALERT DUE TO REPORTED SMOKE IN CABIN. FOUND EQUIPMENT COOLING NORMAL FAN FAILED. REPLACED NORMAL FAN. 2L72 4F4 FRTA16WE E2GL 20050106000982005010600098 2005 1 6 2004UALA01242 420041220A2213 COMPUTER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE AUTOPILOT SYS MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29815UA 867 ALL FMGC 1 FUNCTIONS LOST. AUTOPILOTS DISENGAGED. SUPPLEMENTAL DATA UPDATE FMGC 1 WAS FAULTED BY THE CFDS TEST. REPLACED THE NR 1 FMGC. SHOP TEST FOUND SOLDER CRACKS ON THE U10 OF A51 CARD. 2L72 4F4 FRTA28NM E40NE 20050106000992005010600099NM 2005 1 6 2004UALA01251 120041226A5610 WINDSHIELD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE COCKPIT CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29311UA 23672 DIVERTED DUE TO FIRST OFFICER'S WINDSHIELD CRACKED. WINDOW HEATING ELEMENT ARCED. REPLACED WINDOW. 2L72 4F4 FRTA16WE E2GL 20050106001022005010600102NM 2005 1 6 2004UALA01254 120041227A3397 CONNECTOR BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT FAILED A UALAO OTHER O OTHER CLCLIMB 1 WP29673UA 29241 EMERGENCY EXIT LIGHTS AT ALL SEATS AND WALL EXITS FLICKERED ON AND OFF DURING CLIMB. REPLACED 9 EA SPADE CONNECTORS AND AFT LT CONTROL SWITCH. 2L72 4F4 FRTA1NM E24NE 20050106001032005010600103NM 2005 1 6 2004UALA01255 120041228A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CREASE BEAM WEB CORRODED STA 1406-1411, RBL 69-70 UPPER SURFACE. 2L72 4F4 FRTA2NM E17NE 20050106001052005010600105NM 2005 1 6 2004UALA00989 120041029A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 AFT PIT BODY FRAME DENTED AT STA 1340 BETWEEN STRINGERS 25R & 26R. MAJOR REPAIR ACCOMPLISHED. TYPICAL CARGO PIT DENT DAMAGE FROM CARGO LOADING. TRIMMED OUT DAMAGE & FABRICATED J-ANGLE REINFORCEMENT REPAIR. 2L72 4F4 FRTA2NM E17NE 20050106001062005010600106NM 2005 1 6 2004UALA01233 120041218A2913 PUMP AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE HYD SYSTEM LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29817UA 873 GREEN SYSTEM LOW LEVEL ECAM MSG AND ECAM SHOWING LOW LEVEL. AMBER ALERT DECLARED. FOUND NR 1 ENG EDP HYD PUMP LEAKING, REPLACED EDP PUMP AND REPLACED CASE DRAIN FILTER. 2L72 4F4 FRTA28NM E40NE 20050106001072005010600107EU 2005 1 6 2004UALA01234 120041218A3220 PROXIMITY SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NLG MALFUNCTIONED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29494UA 1840 LANDED UNDER AMBER ALERT DUE TO NOSE GEAR INDICATION. NORMAL LANDING BUT NO NOSE WHEEL STEERING AND HAD TO BE TOWED IN. MLG UNSAFE INDICATION ON FWD PANEL WITH ECAM DOOR NOT CLOSED AND NW STEERING FAULT PER POST FLIGHT REPORT, FOUND NLG DOWNLOCK PROX SENSOR 18GA FAULTING. REPLACED NOSE SERVO CONTROL & SERVO VALVE. REPLACED NLG DOWN LOCK PROX SENSOR 18GA. 2L72 4F4 FRTA28NM E40NE 20050106001082005010600108EU 2005 1 6 2004UALA01235 120041219A2150 CONTROLLER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE A/C PACK FAULTY A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 WP29445UA 826 FLIGHT DIVERTED DUE TO NR 2 PACK SLOWLY OVERHEATING AND NR 1 PACK PREVIOUSLY DEFERRED. REPLACED FAULTY CONTROLLER 2L72 4F4 FRTA28NM E40NE 20050106001102005010600110NM 2005 1 6 2004UALA01237 120041218A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 FUSELAGE EXTERNAL SKIN HAS CORROSION AROUND FASTENER HOLES TO RIGHT FWD UPPER WING TO BODY FAIRING ATTACH PT. 2L72 4F4 FRTA2NM E17NE 20050106001112005010600111 2005 1 6 2004UALA01238 420041220A2565 ASPIRATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29411UA 464 LOWER CHAMBER ASPIRATOR (60322-105) CRUSHED AND RENDERED UNREPAIRABLE. PACKBOARD DAMAGED AT BOTH OUTBOARD CORNERS AND BOTTOM SHAFT SUPPORTS DAMAGED FROM SERVICE HANDLING. ASPIRATORS APPEAR DAMAGED FROM LAST PACKING. REPLACED THE ASPIRATORS AND PACKBOARD. 2L72 4F4 FRTA28NM E40NE 20050106001122005010600112NM 2005 1 6 2004UALA01239 120041220A5270 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29572UA 26682 AFT DOOR OPEN EICAS MESSAGE LIGHT. 2L72 4F4 FRTA2NM E17NE 20050106001152005010600115NM 2005 1 6 2004UALA01243 120041221A5270 WARNING SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29572UA 26682 ABORTED TAKEOFF DUE TO DOOR 3L INDICATION. 2L72 4F4 FRTA2NM E17NE 20050106001182005010600118NM 2005 1 6 2004UALA00990 120041028A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 AFT MAIN CABIN FLOORBEAM CORRODED BS 1640 JUST FWD OF R-2 DOOR LOWER SILL. MAJOR REPAIR ACCOMPLISHED. TYPICAL CORROSION DAMAGE. FABRICATED & INSTALLED T-CAP SPLICE SECTION AND REPAIR ANGLES. 2L72 4F4 FRTA2NM E17NE 20050106001252005010600125NM 2005 1 6 2004UALA01258 120041229A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CABIN FLOORBEAM T-CAP AT BS 365 CORRODED FROM BL 0 TO RBL 62, NUMEROUS AREAS. 2L72 4F4 FRTA2NM E17NE 20050106001272005010600127NM 2005 1 6 2004UALA01260 120041229A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CABIN FLOORBEAM CAP AT BS 311 CORRODED AT RBL 41. 2L72 4F4 FRTA2NM E17NE 20050106001282005010600128NM 2005 1 6 2004UALA01261 120041229A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CREASE BEAM WEB UPPER SURFACE CORRODED FROM STA 1422 TO 1434, RBL 69-71. 2L72 4F4 FRTA2NM E17NE 20050106001302005010600130 2005 1 6 SWIA200414277 420041215A3418C818061MODA COMPUTER EMB 120 EMB120ER 3260203SO STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07587335913 5913 120197 IN CRUISE, RECEIVED A STALL WARNING MAP LIGHT, WITH NO ASSOCIATED LIGHTS ON THE STALL CONTROL PANEL. REMOVED AND REPLACED STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD. REF 27-34-04. 2L72 4T RTA31SO 20050106001322005010600132EA 2005 1 6 SWIA200414286 120041217A2711 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA LT AILERON DEFECTIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07457SW 7773 LEFT WING DOWN AILERON TRIM INOPERATIVE. REMOVED AND REPLACED AILERON TRIM PANEL, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050106001332005010600133 2005 1 6 SWIA200414287 420041215A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING MALFUNCTIONED A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07429SW 7518 STALL FAIL CAUTION MESSAGE. REPLACED STALL COMPUTER IAW 27-35-00. OPERATIONAL CHECK GOOD. S/N OFF 589. 2L72 4F RTA21EA 20050106001362005010600136SO 2005 1 6 SWIA200413992 120041021A3397 WIRE EMB 120 EMB120ER 3260203SO CABIN CHAFED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07393SW 120330 EMERGENCY LIGHT C/B POPS WHEN TESTED. REPAIRED CHAFED WIRE AT EMERGENCY LIGHT BATTERY PACK NR 2. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050106001372005010600137 2005 1 6 SWAA043559 420041206A25656949956 CABLE BOEING737 7373H4 1384600NM R2 DOOR MISROUTED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2L72 4F RTA16WE 20050106001382005010600138NM 2005 1 6 SWAA043560 120041206A5752654645528C TAB BOEING737 7373H4 1384600NM RT AILERON DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29648SW 27718 DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT WING AILERON TAB PER MM. 2L72 4F RTA16WE 20050106001392005010600139NM 2005 1 6 SWAA043563 120041207A335065C27093 LIGHT BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29096SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2L72 4F A16WE 20050106001402005010600140NM 2005 1 6 SWAA043564 120041207A3350101114 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS AT ROW 22, LOOSE. SECURED LIGHT LENS PER MM. 2L72 4F RTA16WE 20050106001422005010600142NM 2005 1 6 SWAA043566 120041207A57536546434370 STRUCTURE BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050106001442005010600144NM 2005 1 6 SWAA043257 120041108A53106546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1006, LBL 4 TO RBL 4, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050106001462005010600146 2005 1 6 SWAA043663 420041217A2565D31354 SLIDE BOEING737 7373A4 1384585NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29676SW 23288 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050106001482005010600148NM 2005 1 6 SWAA043665 120041217A335007912 STRIP BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29719SW 27853 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP AT ROW 1 ABC, BROKEN. REMOVED AND REPLACED EEPLS STRIP PER MM. 2L72 4F RTA16WE 20050106001492005010600149NM 2005 1 6 SWAA043666 120041217A1430 FASTENER BOEING737 7377H4 1384404NM CABIN FLOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED 5Y CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOLD DOWN BRACKET FASTENER BROKEN. REPLACED FASTENER PER MM. 2L72 4F RTA16WE 20050106001522005010600152NM 2005 1 6 AALA20041168 120041125A3397 WIRE HARNESS BOEING767 767323 1385205NM CABIN FAULTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21373AA 25200 EMERGENCY LIGHTS AT SEATS 26AB INOPERATIVE. REPLACED HARNESS AT 26AB FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050106001532005010600153WP 2005 1 6 AALA20041169 120041126A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW219302B 49528 FORWARD CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD CABIN OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20050106001552005010600155NM 2005 1 6 AALA20041171 120041126A3397 WIRE BOEING767 767323 1385205NM CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21389AA 27449 SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23B INOPERATIVE. REPAIRED SEAT WIRING AT SEAT 23B FOR SEAT MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050106001582005010600158WP 2005 1 6 WX0400042 120041004A3350 LIGHT DOUG DC9 DC987 3022087WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19945MA 49725 IFP-MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-LAMPED BURNT OUT BULBS IAW 33-53-00. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001602005010600160WP 2005 1 6 WX0400023 120040808A3350 TRACK DOUG DC9 DC987 3022087WP CABIN BROKEN A WX0AK NONE O OTHER LDLANDING 1 WP19945MA 49725 UPON LANDING IN IFP, THE CREW REPORTED EMERGENCY LIGHT FLOOR TRACK BROKEN WITH WIRES EXPOSED IN TWO LOCATIONS. MAINTENANCE SECURED EMERGENCY FLOOR LIGHTING AT ROWS 15 AND 19. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001622005010600162 2005 1 6 WX0400055 420041111A2230 AUTOTHROTTLE SYS DOUG DC9 DC982 3022082WP COCKPIT MALFUNCTIONED A WX0AC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP19864GA 49912 SCHEDULED FLIGHT MSN TO LAS, CREW ABORTED TAKEOFF AFTER BRAKE RELEASE ON TAKEOFF ROLL AT ABOUT 60 KNOTS DUE TO AUTO THROTTLES CLICKING OFF. CREW REPORTED THE AUTO THROTTLES KICKED OFF AS SOON AS POWER WAS SET FOLLOWED BY A POWER LOSS TO THE NR 1 FMA, NR 1 FD FAILURE AND DFGS FAILURE. AIRCRAFT CLEARED THE RUNWAY WITH VERY LIGHT BRAKING. MAINTENANCE CONTROL ADVISED CREW TO DE-POWER THE AIRCRAFT TO RESET THE SYSTEM. AFTER POWER WAS RESTORED ALL SYSTEMS FUNCTIONED PROPERLY AND AIRCRAFT CONTINUED THE SCHEDULED FLIGHT. 2L72 4F A6WE 20050106001632005010600163WP 2005 1 6 WX0400043 120041007A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19865GA 49998 LAS-MAINTENANCE REPORTED EMERGENCY LIGHT INOPERATIVE AT ROW 15 CEILING. MAINTENANCE RE-LAMPED BURNT OUT BULB IAW 33-52-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001642005010600164WP 2005 1 6 WX040026 120040823A792005630602 OIL FILTER DOUG DC9 DC983 3022083WP OIL SYSTEM CLOGGED A WX0AC ABORTED TAKEOFF J WARNING INDICATION TXTAXI/GRND HDL 1 WP19891GA 49423 AFTER RECEIVING TAKEOFF CLEARANCE, THROTTLES FORWARD TO 1.4 EPR, ENGINES SPOOLED, WITHIN 2 SECONDS AFTER THE AUTO THROTTLES HAD MOVED FORWARD FOR THE FLIGHT LAS TO LAN THE CREW REPORTED MASTER CAUTION LIGHT AND RIGHT OIL STRAINER CLOG LIGHT. CREW DISCONNECTED AUTO THROTTLES, AND BROUGHT THROTTLES TO IDLE, MASTER CAUTION AND CLOG LIGHT EXTINGUISHED. CREW EXITED THE RUNWAY AND CONTACTED MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED TO RETURN TO GATE. MAINTENANCE REMOVED AND REPLACED MAIN OIL FILTER IAW MM 79-00-00, LEAK CHECKED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001652005010600165WP 2005 1 6 WX0400051 120041108A3350 TRACK DOUG DC9 DC983 3022083WP CABIN UNSECURE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19860GA 49786 LAS-CREW REPORTED EMERGENCY TRACK LIGHTING COMING UP AT ROW 5. MAINTENANCE RE-SECURED TRACK LIGHTING AT ROW 5 IAW MM 33-50-00. EMERGENCY LIGHTING OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001662005010600166WP 2005 1 6 WX0400054 120041110A33503115 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19863GA 49911 DEN - MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 3 AND 22. MAINTENANCE RE-LAMPED EMERGENCY LIGHTS AT ROWS 3 AND 22. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050104001572005010400157NM 2005 1 4 SWAA043719 120041227A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 15L TO STR 16L. REPAIRED FRAME PER BOEING SB. 2L72 4F RTA16WE 20050104001712005010400171 2005 1 4 SWAA043701 420041221A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20050105000022005010500002 2005 1 5 DLM88041129 420041222A2340 SWITCH DOUG MD88 MD88 3023688NM COCKPIT SHORTED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27910DL 49541 WHEN ATTENDANT CALL RESET WAS PUSHED IN, LIGHT FIZZLED FOLLOWED BY SMOKE COMING FROM BEHIND SWITCH. REPLACED ATTENDANT CALL RESET SWITCH. SYSTEM NOW CHECKS NORMALLY. 2L72 4F RTA6WE 20050105000082005010500008NM 2005 1 5 DL76G041137 120041225A361079275515 FITTING BOEING767 767332 1382001NM NR 2 ENGINE DAMAGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2716065 DL5 30199 RIGHT ENGINE BLEED OFF LIGHT WITH LOSS OF RIGHT PACK, ALSO RECEIVED EICAS MSG RIGHT ENGINE PRV AFTER T/O. A/C RETURNED TO ATL FOR REPAIRS. BITE OF AIR SUPPLY MODULE REVEALED NO FAULTS. INSPECTION OF PRV AND PRSOV NO DEFECTS NOTED. FOUND FITTING ON PRV CONTROL DAMAGED. REPLACED LINE AND PRV CONTROLLER. 2L72 4F RTA1NM 20050105000102005010500010 2005 1 5 DL757041139 420041226A2230226080004 COMPUTER BOEING757 757232 1384965NM PWA 2037 PW2037 NE E/E BAY MALFUNCTIONED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27613DL 22820 716330 AS TAKEOFF POWER WAS APPLIED THE LEFT EPR ADVANCED THEN THE LEFT COMMAND SECTOR RETREATED. REPLACED TMC. 2L72 4F4 FRTA2NM E17NE 20050105000122005010500012NE 2005 1 5 DLM88041141 220041224A7321 FUEL CONTROL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE MALFUNCTIONED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER CLCLIMB 1 SO27912DL34858 49543 725775 SHUT DOWN RT ENGINE IN FLIGHT AFTER T/O AND CLEANUP. THE RT ENG STARTED SURGING, RT GEN DROP OFF AND ON. SHUT DOWN RT ENG IAW MANUAL. ENGINE WINDMILL FOR APPROX 10-12 MIN, TOTAL TIME FROM OFF TO ON WAS 20 MIN. WINDMILL OIL PRESS >10 PSI. PERFORMED WINDMILL INSP AND REPLACED ENG OIL FILTER PER M/M. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL. PERFORMED IDLE CHECK, PART PWR CHECK, AND T/O POWER CHECK PER PFHB. ALL TEST ARE GOOD. 2L72 4F4 FRTA6WE E9NE 20050105000172005010500017NM 2005 1 5 DL76G041126 120041221A3230 BUTTON BOEING767 7673P6 1385105NM COCKPIT LACK OF LUBE A DALAK NONE O OTHER TOTAKEOFF 1 SO27152DL 24984 AFTER T/O GEAR HANDLE WOULD NOT MOVE TO UP. IAW QRH USED LOCK OVERRIDE SWITCH TO RAISE HANDLE. GEAR HANDLE FELT STIFF WHILE RAISING IT. GEAR HANDLE CAME DOWN NORMALLY. PERFORMED BITE CHECK ON PSEU, NO FAULTS. FOUND MANUAL OVERRIDE BUTTON STUCK IN LUBED SHAFT ASSEMBLY AND PERFORMED GEAR HANDLE CHECK PER MM, OPS CHECK OK. 2L72 4F RTA1NM 20050105000202005010500020NE 2005 1 5 DL75K041147 220041227A7321 FUEL CONTROL BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO276703D32761 30234 716583 AT FL 370 ENG INSTRUMENTS APPEARED FROZEN ENG WOULD NOT ACCELERATE ABOVE 65 PERCENT, N1 ENG WOULD IDLE DOWN. DIVERTED TO CVG. REPLACED FUEL CONTROL AND FUEL PUMP. LEAK CKS OK, ENG TEST OK PER PFHB AND M/M. 2L72 4F4 FRTA2NM E17NE 20050105000292005010500029CE 2005 1 5 DXTA200400477 120041211A3243MS905804 O-RING CESSNA500 560CESSNA 2076750CE MASTER CYLINDER LEAKING E DXTAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 GL07324QS 5600423 CO-PILOT RIGHT BRAKE PEDAL LOST PRESSURE DURING TAXI. BLEED OFF CAUSED A SOFT PEDAL. INSPECTED SYSTEM FOUND, CO-PILOTS RT MASTER CYLINDER LEAKING FLUID. REMOVED AND REPLACED O-RINGS. BLED BRAKE SYSTEM. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. MAINT PERFORMED IAW CC560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20050105000352005010500035CE 2005 1 5 DXTA200400409 120040929A3241429271 COMPUTER CESSNA500 560CESSNA 2076750CE ANTI-SKID SYS FAULTY E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07312QS7247 5600312 BOTH CAPTAIN'S BRAKES INTERMITTENTLY REQUIRE UNEVEN APPLICATION CAUSING PLANE TO SLOW/STOP UNEVENLY OR GRAB. APPEARS LEFT BRAKE INTERMITTENTLY TRAVELS FURTHER BEFORE ENGAGING. FOUND ANTISKID CONTROL SERVO OPENING AND PORTING FLUID DUE TO FAILED ANTISKID COMPUTER SENDING FAULTY OUTPUT SIGNAL. REMOVED AND REPLACED ANTISKID CONTROL BOX, OPS CHECKED AND LEAK CHECKED GOOD, ALL WORK DONE IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20050105000392005010500039NM 2005 1 5 FX7A2004XXXX3 120041213A7910MS938812A PACKING BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE OIL TANK CAP PINCHED A FX7AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO1979749 22452 AFTER ENGINE START ON THE NR 3 NOTICED THE LOW OIL QUANTITY INDICATION. RETURNED TO THE GATE. REPLACED THE DEFECTIVE PACKING ON THE OIL TANK CAP AND TIGHTENED OIL PRESSURE SWITCH LINE B-NUT, IAW MM REF 79-20-11 AND 79-11-0. SERVICED THE NR 3 ENGINE FOUR QUARTS OF OIL AND PERFORMED AN ENGINE GROUND RUN, NO LEAKS NOTED. 2L73 4F4 F A3WE E2EA 20050105000502005010500050NM 2005 1 5 UPS04442809 120040714A5320 FITTING BOEING747 747200 1384847NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:C FX- LEFT BS 1241 AREA EXTERNAL LONGERON FITTING NR 12 MOUNT BOLT HOLE FOUND CORROSION AT FX SIDE. FX - LEFT BS 1241 AREA EXTERNAL LONGERON FITTING ATTACH NR 12 MOUNT BOLT HOLE CORROSION CLEANED BY OVERSIZE .0156 INCH AS PER SRM 51-30-05 PG 13 AND MOUNT BOLT, ALSO REPLACED AS PER MM 20-51-01. 2L74 4F RTA20WE 20050105000562005010500056NM 2005 1 5 UPS04243175 120040908A5330 PANEL BOEING727 727173C 1384059NM FUSELAGE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, PANEL NR 3512 LT REQUIRES COMPOSITE REPAIR. PANEL REPAIRED IAW SRM 51-40-9. 2L73 4F A3WE 20050105000582005010500058NM 2005 1 5 UPS04243180 120040906A7120 BUSHING BOEING727 727173C 1384059NM ENGINE MOUNT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 INSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING, REPAIR BUSHINGS IN BOTH O/B HOLES HAVE MIGRATED. REPAIRED IAW UPS EO B727-5440-11592-A. 2L73 4F A3WE 20050105000732005010500073EU 2005 1 5 MALA040792 120041028A5720 INTERCOSTAL BAC 146 AVRO146RJ85A1500097EU LT WING DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK IN YYC, MAINTENANCE FOUND INTERCOSTAL ABOVE LEFT AILERON CABLE COMPENSATOR DAMAGED. MAINTENANCE REPAIRED IAW EO A53206. AIRCRAFT RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20050105000792005010500079EU 2005 1 5 MALA040793 120041029A5320HC252BU896000U PANEL BAC 146 AVRO146RJ85A1500097EU FUSELAGE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15521XJ E2346 DURING C-CHECK INSPECTION IN YYC, MAINTENANCE FOUND FWD CARGO BAY AFT ENTRANCE GALLEY PANEL HAS HOLES/DAMAGE. MAINTENANCE REPLACED PANEL P/N HC252BU896-000U. AIRCRAFT RETURNED TO SERVICE 11/08/04. 2H74 4F RTA49EU 20050106000032005010600003EU 2005 1 6 MALA040893 120041124A5320 FLANGE SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426XJ 340B426 DURING 4Y/2Y INSPECTION IN BNA, FLOOR FLANGE IS CORRODED OUT OF LIMITS BETWEEN FS 272 & FS 288 AT LBL 30. FLANGE WAS REMOVED AND REPLACED. 2L72 4T RTA52EU 20050106000172005010600017WP 2005 1 6 MWEA040228 120041227A213039271411 REGULATOR DOUG DC9 DC982 3022082WP AIR CONDITIONINGMALFUNCTIONED A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31808ME 48070 AT LEVEL OF AT FL250, FLOW METER CAME ON. REMOVED AND REPLACED AIR CONDITIONING PRESSURE REGULATOR. 2L72 4F A6WE 20050106000182005010600018EU 2005 1 6 3611204 120041223A26121734362450 FIRE DETECTOR SAAB SF340 340B 7860101EU COCKPIT ACTIVATED A NSVAB EMER. DESCENT J WARNING INDICATION TOTAKEOFF 1 EA27339CJ 340B339 AFTER T/O, RT ENGINE TAILPIPE HOT LIGHT ILLUMINATED. ENGINE SHUT DOWN. 2L72 4T RTA52EU 20050106000372005010600037NM 2005 1 6 249TR0057 120041222A7830 FAIRING BOEING737 7372K5 138448XNM THRUST REVERSER CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 NR 1 ENGINE THRUST REVERSER INBOARD FAIRING CRACKED AT AFT END. WELDED PER BOEING REPAIR SPEC BAC5975. 2L72 4F RTA16WE 20050106000382005010600038NM 2005 1 6 249TR0048 120041222A5320 ANGLE BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 Z-ANGLE AT AFT ENTRY DOOR HAS CORROSION. REPLACED Z-ANGLE PER SRM 51-30-2. 2L72 4F RTA16WE 20050106000402005010600040NM 2005 1 6 249TR0071 120041222A5347 GALLEY TRACK BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 CORROSION IN OUTBOARD TRACK FOR G-1 GALLEY. REPLACED TRACK PER SRM 51-40-2. 2L72 4F RTA16WE 20050106000462005010600046NM 2005 1 6 QXEA200400883 120041214A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM LT WING CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09408QX 4050 PDX - COUNTER SINKS CHAFED LEFT WING FUEL PANEL 522CT, HEAVIEST AT INBOARD AND OUTBOARD ENDS. REPLACED IAW Q400 WC 500ME28 60266. 2H72 4T RTA13NM 20050106000552005010600055NM 2005 1 6 QXEA200400923 120041226A21617548902 CONTROLLER DHAV DHC8 DHC8202 2809007NM COCKPIT FAILED A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09348PH17336 484 EUG - FLIGHT 2195 - WHILE ON DESCENT, THE CREW RECEIVED A FLIGHT COMPARTMENT DUCT HOT CAUTION LIGHT. THE CREW COMPLETED THE CHECKLIST. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLIGHT COMPARTMENT TEMPERATURE CONTROLLER. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050106000572005010600057NM 2005 1 6 QXEA200400872 120041205A1430 BOLT BOMBDRDHC8 DHC8401 1390041NM STOP FITTING BACKED OUT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - AFT BAGGAGE DOOR FORWARD BOTTOM STOP FITTING HAS ONE BOLT THAT WILL NOT GRIP AND HAS BACKED OUT. REPAIRED IAW HORIZON EA 6-52-360, RD 8/4-52-178 AND SRM 52-31-23-400-801. 2H72 4T RTA13NM 20050106000602005010600060NM 2005 1 6 QXEA200400866 120041125A5420 INTERCOSTAL BOMBDRDHC8 DHC8401 1390041NM LT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - LEFT HAND NACELLE UPPER AREA OF ZONE 413 FRAME XN210 OUTBOARD INTERCOSTAL IS CRACKED. REPAIRED IAW Q400 SRM 51-40-15 AND RD 8/4-54-155. 2H72 4T RTA13NM 20050106000672005010600067EU 2005 1 6 RAIA00412015 120041212A7930 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ACTIVATED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03560HK 41076 STL - LEFT ENGINE OIL CONTAMINATION LIGHT CAME ON. MAINTENANCE PERFORMED LEFT CHIP DETECTOR INSPECTION, FOUND TO BE IN LIMITS. 2L72 4T RTA41NM 20050106000792005010600079EA 2005 1 6 04349636 120041214A2132 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT FALSE ACTIVATIONA VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27636BR 7307 LEFT PACK HIGH PRESSURE MESSAGE ON CLIMBOUT. OPS CHECK OF LT PACK, NO DEFECT NOTED. 2L72 4F RTA21EA 20050106000912005010600091NM 2005 1 6 2004UALA00814 120040831A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 PYLON ROTATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 2 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING, ONE FASTENER HAS ROTATED AT INBD ROW UPPER HORIZONTAL FASTENER. FASTENER REMOVED, HFEC OF HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NUT. 2L74 4F4 FRTA20WE E24NE 20050106000922005010600092NM 2005 1 6 2004UALA00815 120040831A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 PYLON ROTATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 3 PYLON UPPER LINK TO WING ATTACH FITTING HAS ONE FASTENER THAT HAS ROTATED INBD VERTICAL FASTENER MOST AFT. FASTENER REMOVED, HFEC OF HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NEW NUT. 2L74 4F4 FRTA20WE E24NE 20050106000932005010600093NM 2005 1 6 2004UALA01210 120041217A2751 WARNING SYSTEM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT ACTIVATED A UALAK NONE J WARNING INDICATION LDLANDING 1 WP29653UA 25391 ASYMMETRICAL FLAP WARNING. PERFORMED PSEU BITE TEST. FAULTED SWITCH S303. REPLACED SWITCH, SYSTEM OPS CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20050106000972005010600097NM 2005 1 6 2004UALA01232 120041219A2450 GCU BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT GENERATOR MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29348UA 24252 DIVERTED TO TWF (TWIN FALLS, ID) DUE TO LEFT GENERATOR BUSS FAILURE. AIRCRAFT EXPERIENCED ELECTRICAL FAILURE WHILE CLIMBING. NR 1 GEN OFF BUS LIGHT WITH ASSOCIATED "BUSS OFF" LIGHT ILLUMINATED. TRANSFER BUS LIGHT DID NOT ILLUMINATE BUT HAD BOTH LT TANK FUEL PUMP INOP LIGHTS ON. FOUND SEVERAL CB'S POPPED. APPEARS TO BE VOLTAGE SPIKE. PERFORMED CHECK OF SYSTEM WITH NR 2 ENG GEN AND APU SUPPLYING POWER AFTER CB RESET AND ALL SYSTEMS OPS CHK NORMAL. DISCONNECTED NR 1 CSD, OIL LEVEL NORMAL AIRCRAFT REQUIRED TROUBLE SHOOTING FOR NR 1 ENG GENERATOR SYSTEM. REPLACED THE NR 1 ENG GENERATOR CONTROL UNIT AS A PRECAUTION. 2L72 4F4 FRTA16WE E2GL 20050106001142005010600114 2005 1 6 2004UALA01241 420041220A2565D31096201 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 ON LOWER TUBE, BOTH SUPPORT LEGS AT THE FRONT END ON UPPER SIDE, OPPOSITE ASPIRATOR, LEAKING. LEAKING ON MITERED CORNER AT BUMPER TUBE ON ASPIRATOR SIDE IN FRONT. SLIDE FAILED AIR RETENTION TEST. LEAKAGE WAS FOUND AT SEAMS. POROSITY WAS FOUND NEAR SEAMS. ABRASION ON ONE SEAM CONTRIBUTED TO LEAKAGE. 2L72 4F4 FRTA2NM E17NE 20050106001162005010600116NM 2005 1 6 2004UALA01244 120041220A3230 SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NLG & MLG MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29304UA 23665 GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT DIVERTED. A FAILED S106 LANDING GEAR SAFETY SWITCH CAUSED THE AIRCRAFT TO REMAIN IN THE GROUND MODE, RESULTING IN THE GEAR FAILING TO RETRACT. THE S106 LANDING GEAR SAFETY SWITCH WAS REPLACED AND THE LANDING GEAR EXTENDED AND RETRACTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20050106001242005010600124NM 2005 1 6 2004UALA01257 120041228A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN MALFUNCTIONED A UALAK NONE O OTHER NRNOT REPORTED 1 WP29661UA 27158 EMERGENCY EXIT FLOOR LIGHTS FWD CABIN COME ON, GO OFF, AND FLASH INFLIGHT FOR NO REASON. REPLACED EEL LIGHT BATTERY PACK BEHIND KICK PANEL AT SEAT GROUP 1AB. 2L72 4F4 FRTA1NM E24NE 20050106001352005010600135SO 2005 1 6 SWIA200413991 120041020A275012064207611 CONTROL LEVER EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07188SW30 30 120039 FLAP CONTROL FAULT WITH OUTBOARD FLAPS STUCK AT 7 DEGREES. REMOVED AND REPLACED FLAP SELECTOR LEVER AND CLEANED OUTBOARD FLAP CANNON PLUGS IAW 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050106001432005010600143NM 2005 1 6 SWAA043256 120041108A532065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 11R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20050106001452005010600145NM 2005 1 6 SWAA043702 120041221A33503051F LIGHT BOEING737 7373Y0 1384671NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29682SW 23496 DURING SCHEDULED D-CHECK, FOUND FWD RT EMERGENCY EXIT DOOR SLIDE LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050106001472005010600147NM 2005 1 6 SWAA043664 120041217A53306545776 SKIN BOEING737 7373TO 138447GNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN SECTION PER EA. 2L72 4F RTA16WE 20050106001592005010600159WP 2005 1 6 WX0400022 120040806A3350 CONNECTOR DOUG DC9 DC983 3022083WP CABIN UNSECURE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19860GA 49786 AFTER SCHEDULED LANDING IN LAS, MAINTENANCE REPORTED EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE RE-SECURED LIGHT CONNECTORS AT SEVERAL LOCATIONS AND REINSTALLED FLOOR TRACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001672005010600167WP 2005 1 6 WX0400053 120041110A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19860GA 49786 LAS - MAINTENANCE REPORTED FLOOR EVACUATION EMERGENCY LIGHTS INOPERATIVE AT ROWS12/14. MAINTENANCE RE-LAMPED EMERGENCY LIGHTS AT ROW 12/14. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD IAW MM 33-53-01. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001792005010600179WP 2005 1 6 UPS04843573 120041119A532037592221 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 SPLICE FITTING CRACKED AT STA 1270, LONG 34L. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-8, 51-3-2, 51-1-20D. 2L74 4F RT4A25 20050106001852005010600185WP 2005 1 6 UPS04843555 120041129A33505708458503 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 EMER LIGHTS STAY ON FOR LESS THAN A SECOND. REMOVED AND REPLACED EMER LIGHTS BATT PACK. OPS CK GOOD. 2L74 4F RT4A25 20050106001922005010600192WP 2005 1 6 UPS04843519 120041028A575356423422 SUPPORT FITTING DOUG DC8 DC871F 302199DWP T/E FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 RT FUSELAGE FLAP HINGE STA 3 SUPPORT FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ASSY REF SRM 51-1-20D, 51-1-21, UPS EO DC8-5740-21256A. 2L74 4F RT4A25 20050106002182005010600218NM 2005 1 6 ASA0440195 120041029A531565468118 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 CORROSION ON FLOORBEAM. REMOVED CORRODED UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050107000052005010700005NM 2005 1 7 QXEA200400924 120041228A5270 WARNING SYSTEM DHAV DHC8 DHC8202 2809007NM COCKPIT ACTIVATED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09348PH 484 YKM - FLIGHT 2015 - THE TAKEOFF WAS ABORTED AFTER THE CREW RECEIVED A BAGGAGE DOOR WARNING DURING THE ROLL. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE DOOR HANDLE PROPERLY SECURED. THE DOOR WAS PLACED ON MEL. SDR TO REMAIN OPEN PENDING FURTHER INFORMATION. 2H72 4T RTA13NM 20050107000112005010700011EU 2005 1 7 MALA040895 120041123A5730 SKIN BAC 146 AVRO146RJ85A1500097EU RT WING DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, A DENT WAS FOUND ON RT WING LEADING EDGE. MAINTENANCE REPAIRED LEADING EDGE IAW EO NR A57080. AIRCRAFT RETURNED TO SERVICE 11/23/2004. 2H74 4F RTA49EU 20050107000162005010700016EU 2005 1 7 MALA040900 120041214A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 BETWEEN FS 294-339 IS CORRODED AND PREVIOUS SPLICE REPAIR IS NON STANDARD. DAMAGED TRACK HAS BEEN REMOVED AND REPLACED IAW MESABA EO NR S53060 BETWEEN FS 294 AND FS 350. REFER EAMS WORK ORDER NR 211236/TASK 1526 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000212005010700021NM 2005 1 7 AWXA200401356 120041202A5270 TARGET BOEING757 757225 1384959NM R2 DOOR LOOSE A AWXAK NONE O OTHER NRNOT REPORTED 1 WP28915AW 22209 PHX - EES - FLIGHT CREW REPORTED THE R-2 DOOR SLIDE LIGHT WAS INOPERATIVE WITH THE SLIDE IN ARMED POSITION. MAINTENANCE RE-SECURED LOOSE R-2 DOOR ARMED LIGHT SENSOR TARGET AT FORWARD END OF GIRT BAR, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050107000222005010700022NM 2005 1 7 AWXA200401342 120041128A3397BMS13311122 WIRE BOEING757 7572G7 1384963NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20050107000302005010700030 2005 1 7 AWXA200401353 420041130A2565D31865110 SLIDE AIRBUS320 A320231 3930325EU CABIN DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28646AW304721064 271 PHX - EES - DURING 4-DAY CHECK THE LOWER AFT CORNER OF THE RT OVERWING SLIDE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C R1A25301. 2L72 4F RTA28NM 20050107000382005010700038EU 2005 1 7 AWXA200401229 120041026A5320D53475575232 PLATE AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 DURING C-04 CHECK, EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR SILL FORWARD PLATE, AT FORWARD INBOARD EDGE FS 53. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FORWARD PLATE AT FS 53; FABRICATED A NEW REPLACEMENT PLATE; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, FIG. 2, 3, 8, & 12. 2L72 4F RTA28NM 20050107000432005010700043EU 2005 1 7 AWXA200401380 120041114A5313D53470422204 STRINGER AIRBUS320 A320232 3930326EU FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 43 LT AT FS 55 IN AFT CARGO COMPARTMENT. MAINTENANCE BLENDED OUT CORROSION ON STRINGER 43 LT AT FS 55 AND REMOVED STRINGER TIE CLIP; FABRICATED A REPAIR ANGLE AND SHIM FOR BLEND OUT, AND FABRICATED A NEW REPLACEMENT TIE CLIP DUE TO NEW THICKNESS OF REPAIR AREA; INSTALLED REPAIR PARTS IAW A320 SRM 53-00-13, FIG. 202. 2L72 4F RTA28NM 20050107000452005010700045NM 2005 1 7 AWXA200401345 120041126A2910AE7079101 HYDRAULIC LINE AIRBUSA319 A319132 3930340NM NR 2 ENGINE BLOWN A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28804AW 1043 PHX - DIVERSION - FLT 0361 - EN ROUTE FROM LAX TO IAD RECEIVED ECAM MESSAGE HYDRAULIC RESERVOIR LOW LEVEL, YELLOW QUANTITY INDICATOR ALSO SHOWED LOW, DIVERTED INTO PHX FOR REPAIR. MAINTENANCE FOUND A BLOWN FLEX LINE FOR NR 2 ENGINE HYDRAULIC PUMP PRESSURE SWITCH. REMOVED AND REPLACED FLEX LINE, OPERATIONAL AND LEAK CHECKS WERE GOOD. 2L72 4F RTA28NM 20050107000502005010700050EU 2005 1 7 AWXA200401107 120040925A5321D5367320100000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, A 4 INCH CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT FLOOR PANEL 131DF BETWEEN FS 24 AND FS 28. MAINTENANCE REMOVED FLOOR PANEL 131DF; CUTOUT DAMAGED AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000542005010700054NM 2005 1 7 AWXA200401368 120041116A53306545772213 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28334AW 23747 MCN - MAJOR REPAIR - DURING 8-DAY CHECK FUSELAGE SKIN WAS FOUND CHAFED AT DORSAL FIN AREA BETWEEN BS 908 AND BS 927, STR 2 RT. MAINTENANCE BLENDED OUT DAMAGE IN FUSELAGE SKIN FROM BS 908 TO BS 931, STR 2 RT, THICKNESS MEASUREMENT OF SKIN FOUND MATERIAL LOSS TO BE OUT OF LIMITS; FABRICATED A DOUBLER, TRIPLER, AND 4 EACH WEAR STRAP LEVELING SHIMS; INSTALLED REPAIR PARTS IAW ER 03-5361-04326-SS1. 2L72 4F RTA16WE 20050107000712005010700071CE 2005 1 7 65790 120041014A561010138402521 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A AMWAO OTHER O OTHER UKUNKNOWN 1 CE07159YV UE159 CAPT'S WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD P/N 10138402521 S/N 98161H7878. 2L72 4T RTA24CE 20050107000892005010700089SO 2005 1 7 C2XA04CL134 120041205A2120 ODOR EMB 145 EMB145XR 3260214SO COCKPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2713132 145708 CREW REPORTED STRONG BURNING SMELL AFTER ANTI-ICE WAS TURNED OFF. MAINTENANCE PERFORMED GROUND RUNS OF BOTH ENGINES WITH BLEEDS AND PACKS ON AND OFF. NO DEFECTS NOTED. 2L72 4F RT 20050107000902005010700090SO 2005 1 7 C2XA04BT126 120041205A2120BWT138005 DUCT EMB 145 EMB145LR 3260212SO A/C SYSTEM ODOR A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2711536 145520 CREW REPORTED FOUL SMELL FROM PACK SYSTEM. MAINTENANCE REPLACED THE RECIRCULATING DUCT. OPERATIONALLY CHECK SYSTEM NO SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050107000922005010700092 2005 1 7 SB04143 420041011A3425DG1035AB03 CONVERTER BOEING737 737301 1384611NM E/E BAY DEFECTIVE A USAAA UNSCHED LANDING IJ FLT. ATTITUDE INST. WARNING INDICATION CRCRUISE 1 EA19589US5190351903 23934 CLT - FLT528 - THIRTY MINUTES AFTER TAKEOFF FROM CLT, EN ROUTE TO MCI, THE FIRST OFFICERS ADI FAILED WITH INTERMITTENT FLAGS IN VIEW. CREW DECIDED TO RETURN TO FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 2 DIGITAL TO ANALOG CONVERTER (DAA) DEFECTIVE. REMOVED AND REPLACED THE DAA. ALSO, REMOVED AND REPLACED FIRST OFFICERS ADI. FUNCTIONAL TESTS GOOD. 2L72 4F RTA16WE 20050107000992005010700099NM 2005 1 7 USAA040953 120041123A532065C80736 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SUPPORT ANGLE, .1250 INCH CRACK, STA 260 C/L. REPAIRED WITH NEW PART IAW MFG DWG 65-45833. REPAIRED WITH NEW PART IAW MFG DWG 65-45833. 2L72 4F4 FRTA16WE E21EU 20050107001032005010700103NM 2005 1 7 USAA040948 120041021A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - ANTENNA MOUNT FRAME, 3 INCHES L BY 1 INCH W, CORROSION; LEVEL 1; TASK NR C53-107-01, VHF ANTENNA NR 2 MOUNT. REPAIRED IAW SM 51-10-2 AND 51-40-00. 2L72 4F4 FRTA16WE E21EU 20050107001072005010700107NM 2005 1 7 USAA040935 120041105A575365C26602224 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU T/E FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - FLAP, 4.5 INCHES BY 5 INCHES DELAMINATION, IB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20050107001092005010700109NM 2005 1 7 USAA040830 120041014A57536546435274 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE T/E FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19504AU51924 23379 PIT - C2, UPPER AND LOWER SKIN, .5 INCH BY 2.5 ALONG T/E, DELAMINATED, IB T/E OF RT OB AFT FLAP. FABRICATED REPAIR SKIN AND DOUBLER AND NEW IAW TR 57-50-39A AND EO 5796X105. 2L72 4F4 FRTA16WE E2GL 20050107001112005010700111NM 2005 1 7 SB04153 120041107A335020121 CHARGER BOEING737 7374B7 1384702NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19432US 24554 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 15 THROUGH 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001122005010700112NM 2005 1 7 USAA040934 120041105A575365C26602224 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU T/E FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - FLAP, 3.5 INCH BY 5 INCH AREA, DELAMINATED, OB T/E. REMOVED TOP SKIN, CORE, INSTALLED INTERNAL DOUBLER, NEW CORE, EXT DBLR IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20050107001132005010700113NM 2005 1 7 USAA040936 120041110A554265C25841 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - SKIN, 1 INCH BY 1.5 INCHES WEAR, KNIFE EDGE WEAR, 1 INCH AFT OF FWD CORNER AT RUDDER STA. INSTALLED REPAIR PLIES IAW EA 79467, SRM 51-70-17. 2L72 4F4 FRTA16WE E21EU 20050107001152005010700115NM 2005 1 7 USAA040937 120041105A575465C26603 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 3 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - SLAT 15 INCH BY 6 INCH DELAMINATION. NR 3 SLAT IB END. REMOVED TOP SKIN AND CORE, INSTALLED INTERNAL DOUBLER, CORE, TOP SKIN TYP REP 57-42-03, SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20050107001202005010700120EU 2005 1 7 SA04104 120041104A2560 GIRT BAR AIRBUSA319 A319112 3930323EU CABIN OUT OF POSITION A USAAK NONE O OTHER TXTAXI/GRND HDL 1 EA19760US 1354 CLT - THE SLIDE GIRT BAR FELL FROM THE FORWARD ENTRY DOOR DURING PUSHBACK. AIRCRAFT RETURNED TO GATE. MAINTENANCE RE-ATTACHED THE GIRT BAR TO THE FORWARD ENTRY DOOR SLIDE. OK FOR SERVICE. 2L72 4F RTA28NM 20050107001222005010700122NM 2005 1 7 SB04145 120041016A5610PPG5893543109 WINDSHIELD BOEING737 7373B7 1384580NM COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19384US3534935349 22957 PHL - FLT 1447 - EN ROUTE FROM PHL TO ATL, AT FL270, CAPTAIN REPORTED VIA ACARS THE L1 WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO PRESSURIZATION PROBLEMS WERE ENCOUNTERED AND NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE L1 WINDSHIELD. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F RTA16WE 20050107001232005010700123EU 2005 1 7 BA04023 120040923A3350321431 BATTERY AIRBUS330 A330323 3930335EU R3 & R4 DOOR DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19678US 388 PHL - EPSU'S AT DOORS 4R AND 3R FAILED THE CAPACITY TEST. MAINTENANCE REPLACED THE BATTERIES. 2L72 4F RTA46NM 20050107001262005010700126NM 2005 1 7 QXEA200400809 120041123A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - FORWARD RIGHT HAND INBOARD SEAT TRACK TOP SURFACE HAS CORROSION AT APPROXIMATELY STATION X215.500. REPAIRED IAW RD 8-53-1102. 2H72 4T RTA13NM 20050107001272005010700127NM 2005 1 7 QXEA200400810 120041120A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AT CENTER CHANNEL AND CHANNEL RADIUS AT APPROXIMATELY STATION X451.000. REPAIRED IAW DHCC8-200 SRM 51-40-00 AND SRM 51-40-11. 2H72 4T RTA13NM 20050107001282005010700128NM 2005 1 7 QXEA200400799 120041108A5320 SILL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - FORWARD FUSELAGE, FORWARD RIGHT HAND EMERGENCY EXIT, LOWER HINGED DOOR, DOOR LOWER SILL SHOWS SIGNS OF CORROSION AROUND LOWER STOP FITTING. REPAIRED IAW Q400 SRM SUBTASK 51-41-00-800-801 AND 51-41-05-800-801. 2H72 4T RTA13NM 20050107001292005010700129NM 2005 1 7 QXEA200400841 120041202A3240FE279000 BRAKE BOMBDRDHC8 DHC8401 1390041NM PARKING BRAKE MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09417QX1135 4086 SEA - ON FLIGHT NUMBER 2385, TAKEOFF WARNING DURING POWER UP FOR TAKEOFF. TAKEOFF ABORTED. TAKEOFF WARNING WAS CHECKED AFTER BRAKE RELEASE PRIOR TO TAXI AND NO TONE WAS HEARD. ALL TAKEOFF CONFIGURATION ITEMS WERE RECHECKED FOLLOWING ABORTED TAKEOFF AND NO DEVIATIONS OR ABNORMALITIES FOUND. TAKEOFF WARNING WAS RECHECKED AFTER CLEARING RUNWAY AND WARNING TONE DID NOT SOUND AGAIN. REMOVED AND REPLACED PARK BRAKE QUADRANT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107001302005010700130NM 2005 1 7 QXEA200400843 120041204A243523088008 STARTER GEN DHAV DHC8 DHC8202 2809007NM NR 2 ENGINE MALFUNCTIONED A QXEAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 NM09348PH10638621 484 SEA-DURING PUSHBACK, THE NR 2 STARTER BEGAN TO SMOKE. RAMPER SAW SMALL FIRE DEVELOPE ON NUMBER TWO ENGINE. CAPT INSTRUCTED PASSENGER AND CREW TO EVACUATE. EVERYBODY DEPLANED THROUGH PAX DOOR. MAINTENANCE REPLACED NR 2 ENGINE STARTER GENERATOR AND DC GCU. O PERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107001322005010700132NM 2005 1 7 QXEA200400789 120041117A5753 SKIN BOMBDRDHC8 DHC8401 1390041NM T/E FLAP WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND INBOARD FLAP HAS A DEEP WEAR MARK ON THE UPPER SURFACE WHERE THE UPPER SHROUD INBOARD RUB BUTTON SITS. REPAIRED IAW HORIZON AIR EA 6-57-252. 2H72 4T RTA13NM 20050107001332005010700133NM 2005 1 7 QXEA200400798 120041113A5320 SILL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - PASSENGER DOOR SURROUND STRUCTURE LOWER DOOR SILL PLATE HAS CORROSION UNDER "A" NUTS. REPAIRED IAW Q400 SRM SUBTASK 51-21-00-350-001. 2H72 4T RTA13NM 20050107001372005010700137EA 2005 1 7 QXEA200400835 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE EXPOSED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS BARE METAL EXPOSED AT FS 855.00. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001382005010700138NM 2005 1 7 QXEA200400857 120041129A5753 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - LEFT HAND INBOARD FLAP HAS CHAFE DAMAGE FROM CONTACT WITH WING UPPER TRAILING EDGE ALONG THE ENTIRE FLAP LENGTH. REPAIRED IAW SRM 57-51-30-320-001. 2H72 4T RTA13NM 20050107001392005010700139NM 2005 1 7 QXEA200400855 120041201A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - LEFT HAND INBOARD SEAT RAIL HAS CORROSION ON THE TOP FLAT AREA FROM STATION X2.070 TO 32. REPAIRED IAW RD 8/4-53-884 ISSUE 1. 2H72 4T RTA13NM 20050107001402005010700140NM 2005 1 7 QXEA200400788 120041129A5210 DOOR BOMBDRDHC8 DHC8401 1390041NM AFT PAX DOOR STUCK A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09415QX2507 4081 SEA - FLIGHT 2315 - CREW REPORTS THE AFT PASSENGER DOOR IS STUCK. MAINTENANCE INSPECTED THE AFT PASSENGER DOOR AND UNSTUCK THE SAME. THE DOOR WAS CYCLED SEVERAL TIMES AND ALL OF THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107001412005010700141NM 2005 1 7 QXEA200400844 120041130A324221599 BRAKE DHAV DHC8 DHC8202 2809007NM RT BRAKES OVERTEMP A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09379PH10160802 530 YVR - FLIGHT 2151 - WITH THE PARKING BRAKE HANDLE RELEASED, THE CREW WAS UNABLE TO MOVE THE AIRCRAFT. THE BRAKE WAS OBSERVED TO BE EXTREMELY HOT AND GLOWING. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH THE NR 3 AND NR 4 BRAKE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107001422005010700142EA 2005 1 7 QXEA200400819 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION STATION X562-X566, X554-X542 WITH GOUGES AT STATION X629, X614 AND X553-X554. REPAIRED IAW CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001432005010700143NM 2005 1 7 QXEA200400785 120041122A5210 DOOR DHAV DHC8 DHC8202 2809007NM PAX DOOR OUT OF RIG A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09375PH12171 529 SEA - FLIGHT 2062 - THE FLIGHT ATTENDANT REPORTS THE MAIN CABIN DOOR IS DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND FOUND IT OUT OF RIG. THE DOOR WAS RIGGED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107001452005010700145NM 2005 1 7 QXEA200400802 120041116A5320 FITTING BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - AFT BAGGAGE DOOR SURROUND LOWER SILL MACHINE RIB FITTING, TOP SURFACE HAS CORROSION AT "A" NUT. REPAIRED IAW SUBTASK 51-21-00-500-801, RD 8/4-53-1070 AND HORIZON AIR EA 6-53-472. 2H72 4T RTA13NM 20050107001472005010700147NM 2005 1 7 QXEA200400803 120041117A5753 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM T/E FLAP CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - LEFT HAND OUTBOARD FLAP HAS A CHAFING MARK 8 INCH LONG AND .500 INCH WIDE WHICH IS THROUGH THE PAINT AND METAL IS EXPOSED AT FLAP STATION 191 TO 227. REPAIRED IAW RD 8/4-57-388 AND HORIZON AIR EA 6-57-256. 2H72 4T RTA13NM 20050107001482005010700148NM 2005 1 7 QXEA200400800 120041116A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND INBOARD SEAT RAIL AT STATION X-39 TO STATION X 3.0 HAS PITTING CORROSION. REPAIRED IAW RD 8/4-53-884 AND SRM SUBTASK. 51-40-15-400-001 AND 51-42-05-330-001, PARAGRAPH E. 2H72 4T RTA13NM 20050107001512005010700151NM 2005 1 7 QXEA200400805 120041109A5420 SUPPORT CHANNEL BOMBDRDHC8 DHC8401 1390041NM NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - SUPPORT CHANNEL FOR NACELLE AFT DECK AT THE FINGERNAIL ATTACH POINT IS CRACKED. REPAIRED IAW Q400 SUBTASK 51-40-07-320-801 AND 51-42-05-330-801. 2H72 4T RTA13NM 20050107001522005010700152EA 2005 1 7 QXEA200400826 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 383, FS 420, FS 448. REPAIRED IAW CRJ 700 SRM 51-21-16. AND HORIZON AIR EA R-53-233. 2L72 4F RTA21EA 20050107001532005010700153NM 2005 1 7 QXEA200400787 120041127A27207G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007NM RUDDER FAILED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09356PH18018 502 RDM - FLIGHT 2199 - THE CREW REPORTED RUDDER PRESSURE CAUTION LIGHTS ON APPROACH. THE CHECKLIST WAS COMPLETED ON THE GROUND. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED BOTH RUDDER PRESSURE SWITCHES. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107001542005010700154EA 2005 1 7 QXEA200400823 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION AT FS 727. REPAIRED IAW CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001552005010700155EA 2005 1 7 QXEA200400839 120041119A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT HAND LOWER BULKHEAD AT FS 280 FLOOR LEVEL HAS CORROSION AT FIVE LOCATIONS ALONG 27 INCH AREA STARTING AT RIGHT HAND SIDE OF COCKPIT DOORWAY. REPAIRED IAW CRJ SRM 51-42-06 AND REO 670-53-11-052. 2L72 4F RTA21EA 20050107001562005010700156EA 2005 1 7 QXEA200400824 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 714 AND FS 702. REPAIRED IAW CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001572005010700157EA 2005 1 7 QXEA200400840 120041129A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INTERMITTENT A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - EMERGENCY FLOOR PATH LIGHTS STRIP SECOND STRIP AFT OF FORWARD STRIP HAS INTERMITTENT RED LIGHTS. REPAIRED IAW W/C 200ME3320667. 2L72 4F RTA21EA 20050107001582005010700158EA 2005 1 7 QXEA200400837 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREAS AT FS 884-890 AND FS 936-953. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001602005010700160EA 2005 1 7 QXEA200400825 120041128A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - RIGHT INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 667, FS 599, FS 536, FS 507 AND FS 479. REPAIRED IAW HORIZON AIR EA R-53-233 AND REO 670-53-00-054. 2L72 4F RTA21EA 20050107001642005010700164NM 2005 1 7 QXEA200400859 120041203A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND EXTERIOR SKIN PANEL 85327151 HAS FIVE NICKS AT STATION X21, BETWEEN STRINGERS 31 AND 32. REPAIRED IAW HORIZON AIR EA 6-53-483 AND RD 8/4-53-1096. 2H72 4T RTA13NM 20050107001672005010700167EA 2005 1 7 QXEA200400831 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREAS AT FS 517-541, FS 543-565 AND FS 566. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001682005010700168EA 2005 1 7 QXEA200400832 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS LIGHT SURFACE CORROSION INSIDE CHANNEL AND LUG HOLE AREAS AT FS 580-587, FS 629 AND FS 645-661. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001692005010700169EA 2005 1 7 A6WA200440215 120041114A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 LT FS 625.00 OBLIQUE ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20050107001732005010700173NM 2005 1 7 SWAA043738 120041229A324626066712 WHEEL BOEING737 7373A4 1384585NM NR 3 MLG MISSING A SWAAK NONE O OTHER TXTAXI/GRND HDL 1 SW29677AA 23289 UPON ARRIVAL TO GATE NR 3 MLG TIRE/WHEEL ASSY NOTED MISSING FROM ACFT. REMOVED AND REPLACED NR 3 MLG INNER STRUT ASSY AND NR 3 MLG TIRE/WHEEL ASSY PER MM. 2L72 4F RTA16WE 20050107001822005010700182NM 2005 1 7 SWAA050004 120041231A523065647952 SKIN BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT, LT UPPER CORNER SKIN, CRACKED. REPAIRED DOOR SKIN PER EA. 2L72 4F RTA16WE 20050107001832005010700183NM 2005 1 7 SWAA043732 120041229A5753654643089 SKIN BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM. 2L72 4F RTA16WE 20050107001882005010700188NM 2005 1 7 SWAA043733 120041229A3350PH22300L STRIP BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29613SW 27931 DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP WORN AT ROWS 1 ABC & 3 ABC. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20050107001912005010700191NM 2005 1 7 SWAA043723 120041227A5753113A3700 SKIN BOEING737 7377H4 1384404NM T/E FLAP PUNCTURED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29718SW 27852 DURING SCHEDULED MV1 CHECK, FOUND LT WING T/E INBD AFT FLAP SKIN PUNCTURED NEAR INBOARD END. REPAIRED AFT FLAP PER SWA EA. 2L72 4F RTA16WE 20050107001932005010700193NM 2005 1 7 SWAA043725 120041228A53106546548 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FRAME SHEAR TIE CORRODED AT BS 747, RBL 7 TO RBL 13. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050107001942005010700194NM 2005 1 7 SWAA043726 120041228A52406545871 DOOR FRAME BOEING737 7373K2 13844BANM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT NR 3 & NR 4 STOP FITTINGS. REMOVED AND REPLACED R1 DOOR PER MM. 2L72 4F RTA16WE 20050107001952005010700195NM 2005 1 7 SWAA043727 120041227A3350100031 LIGHT BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29368SW 26579 LT OVERWING EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050107001982005010700198NM 2005 1 7 SWAA043730 120041229A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE TORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD SHEAR WEB TORN AT BL 0 TO LBL 25. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050107002102005010700210NM 2005 1 7 SWAA043736 120041228A32407816903 VALVE BOEING737 7372H4 138448CNM MLG W/W LEAKING A SWAAK NONE O OTHER APAPPROACH 1 SW29083SW 22732 DURING APPROACH WITH LANDING GEARS DOWN, LOST HYD A-SYS. REMOVED AND REPLACED HYD A-B SYS AUTO BRAKE VALVE PER MM. 2L72 4F A16WE 20050107002112005010700211NM 2005 1 7 SWAA043737 120041229A324226010425 BRAKE ASSY BOEING737 7372H4 138448CNM MLG FAULTY A SWAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW29083SW 22732 DURING TAXI OUT, BRAKES WERE INTERMITTENT AND FELT LIKE SKIPPING. REMOVED AND REPLACED NR 2 & NR 4 MLG BRAKE ASSY'S PER MM. 2L72 4F A16WE 20050110000012005011000001SO 2005 1 10 SWIA200414198 120041101A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 INTERCOSTAL ATTACHING RIGHT 479.00 FLOORBEAM TO RIGHT STR 15 FLOOR SUPPORT ANGLE FRAME 40 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) UPON FURTHER INSPECTION, NO CORROSION FOUND ITEM NOT REPLACED, NO FURTHER ACTION REQUIRED. 2L72 4T RTA31SO 20050110000032005011000003SO 2005 1 10 SWIA200414217 120041101A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 FS 16 TO 21 RIGHT AT STR 15 FLOOR SUPPORT ANGLE IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE BLENDED AND ASSESSED TO BE WITHIN LIMITS EMB 120 SRM 53-20-10 MAX MAT'L LOSS .004. AREA REPROTECTED IAW EMB 120 SRM 51-21-02 AND AMM 20-30-05. 2L72 4T RTA31SO 20050110000042005011000004SO 2005 1 10 SWIA200414226 120041101A5712 RIB EMB 120 EMB120ER 3260203SO RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 RIGHT WING, RIB 17 FORWARD OF AUX SPAR, CLEAT IS CRACKED, IN WET BAY AREA, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED RIB IAW EMB 120 SRM 57-20-07 FIG 203 SHEET 1,2,3. 2L72 4T RTA31SO 20050110000072005011000007EA 2005 1 10 SWIA200414238 120041204A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07463SW 7820 2ND OVERHEAD EMERGENCY FLOOD LIGHT AND AFT OF PAX DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000092005011000009EA 2005 1 10 SWIA200414262 120041203A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 AFT EQUIP COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06 & 51-25-16. 2L72 4F RTA21EA 20050110000112005011000011SO 2005 1 10 SWIA200414264 120041215A2752 ACTUATOR EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07268UE 120207 FLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT OUTBOARD FLAP ACTUATOR, FLAP SELECTOR LEVER AND FLAP CONTROL UNIT IAW EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD. PN 320300-1007 SN OFF 1113PN 120-64207-615 SN OFF 280040-316 PN OFF 307500-1017 SN OFF 0216. 2L72 4T RTA31SO 20050106000432005010600043NM 2005 1 6 249TR0053 120041222A5310 SHEAR TIE BOEING737 7372K5 138448XNM FUSELAGE CORRODED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05249TR 22598 SHEAR TIE CORRODED IN AFT CARGO AT BS 986 AT STR 24RT. REPLACED SHEAR TIE PER SRM 51-10-1 AND SRM 51-30-2. 2L72 4F RTA16WE 20050106000472005010600047EA 2005 1 6 QXEA200400892 120041214A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09602QX 10010 PDX - RIGHT OUTBOARD SEAT RAIL CORROSION AT X738.00 AND X754.00. REPAIRED IAW HORIZON AIR EA R-53-240 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20050106000522005010600052NM 2005 1 6 QXEA200400918 120041225A5230 HANDLE BOMBDRDHC8 DHC8401 1390041NM AFT CARGO DOOR UNLATCHED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09408QX8079 4050 BOI - FLIGHT 2364 - THE FLIGHT RETURNED TO FIELD WHEN DURING THE CLIMB, THE CREW RECEIVED A FUSELAGE DOOR WARNING FOR THE REAR CARGO DOOR. MAINTENANCE INSPECTED THE DOOR AND FOUND THE HANDLE IN THE UNLATCHED POSITION. THE HANDLE WAS SECURED AND OPERATIONAL CHECKS WERE PERFORMED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050106000692005010600069NM 2005 1 6 SCNA04020 120041217A3350 SPRING BOEING737 737800* NM CABIN BROKEN A SCNAK NONE O OTHER CRCRUISE 1 GL15PHHZX 28248 FLIGHT CREW DISCOVERED EMERGENCY LIGHT COVER SPRING BROKEN, PLACED ON DMI 465. ON 12/23, INSTALLED NEW COVER. 2L72 4F RTA16WE 20050106000772005010600077EA 2005 1 6 04351669 120041216A3320BF0010005 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INCORRECT A VTZAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA27669BR 7545 ATO FOR SMOKE IN LAV. RETURN SEAT LAV ASSY INSTALLED WITH INCORRECT BULBS, CAUSING ASSY TO OVERHEAT AND SMOKE. 2L72 4F RTA21EA 20050106000842005010600084NM 2005 1 6 2004UALA01263 120041229A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 FWD PIT LT TUNNEL, LAV SERVICE AREA, SKIN CORRODED AT BS 705-715, STR 21L-22L. 2L72 4F4 FRTA2NM E17NE 20050106000892005010600089NM 2005 1 6 2004UALA00812 120040831A5751 HINGE FITTING BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT AILERON CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 LT WING OUTBOARD AILERON NR 2 HINGE FITTING CRACKED AT AFT LOWER AREA THROUGH LWR AFT FASTENER. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FITTING. 2L74 4F4 FRTA20WE E24NE 20050106000952005010600095 2005 1 6 2004UALA01230 420041215A2565XD4L015 RELAY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 1 EVAC SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29648UA 25285 LEFT SQUIB ON NR 1 ESCAPE SLIDE WILL NOT TEST. REPLACED RELAYS K3, K4, K5, & K6 ON M1135 MODULE ABOVE LEFT AFT OVERWING DOOR PER WIRING DIAGRAM 25-65-11 AND PERFORMED REPETITIVE ITERATIONS OF SQUIB TEST. ALL CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20050106001042005010600104NM 2005 1 6 2004UALA00987 120041027A5312 PRESSURE PANEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29572UA 26682 MAIN CABIN STA 1700 AFT PRESSURE DECK CORRODED. MAJOR REPAIR ACCOMPLISHED. TYPICAL CORROSION DAMAGE. FABRICATED & INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050106001172005010600117 2005 1 6 2004UALA01246 420041222A2565520S0020 O-RING AIRCRUISERS BOEING757 757222 1384956NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29584UA 0554 26706 LOW BOTTLE PRESSURE. PRESSURE LEAKING AT SHAFT O-RING. REPLACED SHAFT O-RING, BACK-UP O-RING, BALL SEAT, GAGE ADPATER O-RING. 2L72 4F4 FRTA2NM E17NE 20050106001192005010600119NM 2005 1 6 2004UALA01247 120041223A5315 FLOORBEAM BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29178UA 24385 UPPER T-CHORD FWD FLANGE OF AFT CARGO COMPARTMENT FLOORBEAM AT STA 1760, LBL 51 WAS FOUND DENTED. REPAIR ACCOMPLISHED. 2L74 4F4 FRTA20WE E24NE 20050106001232005010600123NM 2005 1 6 2004UALA01256 120041227A5532 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE VERTICAL STAB DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29306UA 23667 VERTICAL FIN L/E SKIN HAS A DENT AT LES 132. DENT IS 1.55 BY 0.046 INCH DEEP. DENT IS A ZONE 3 DENT. INSTALLED FLUSH REPAIR. 2L72 4F4 FRTA16WE E2GL 20050106001262005010600126NM 2005 1 6 2004UALA01259 120041229A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE BULGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 STATION 1681 RT AFT DECK PLATE (FLOORBEAM) BULGED AROUND FASTENER HOLE RBL 39.5 TO RBL 40. 2L72 4F4 FRTA2NM E17NE 20050106001292005010600129NM 2005 1 6 2004UALA01262 120041229A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CABIN FLOORBEAM UPPER CAP CORRODED STA 1639 TO 1641, RBL 48 TO RBL 56. 2L72 4F4 FRTA2NM E17NE 20050106001312005010600131SO 2005 1 6 SWIA200414278 120041210A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0758733 120197 EMERGENCY EXIT OVERHEAD LIGHT NOT ILLUMINATED. RELAMPED OVERHEAD EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050106001412005010600141NM 2005 1 6 SWAA043565 120041207A57536546435335 STRUCTURE BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29638SW 27711 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM. 2L72 4F RTA16WE 20050106001512005010600151WP 2005 1 6 AALA20041166 120041125A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21286AA 49298 FORWARD OVERWING ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERWING ESCAPE PATH EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050106001542005010600154NM 2005 1 6 AALA20041170 120041126A3350P4010049 BATTERY PACK BOEING757 757223 1384957NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21602AN 27053 EMERGENCY LIGHTS ON SEATS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON SEATS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050106001612005010600161NE 2005 1 6 WX0400025 220040815A7320 SENSE LINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT ENGINE DISCONNECTED A WX0AA UNSCHED LANDING O OTHER CLCLIMB 1 WP19862GA 49556 AFTER TAKEOFF EN ROUTE FROM LAS TO BLI, CREW REPORTED ABNORMAL EPR SPLIT AT 11,000 FT, APPROXIMATELY 20 DEGREES C, 210 KNOTS WITH THE FOLLOWING ENGINE INDICATIONS. LEFT ENGINE AT 1.08 EPR, 49 PERCENT N1, 392 EGT, 75 PERCENT N2, 16.8 FF RIGHT ENGINE AT 1.12 EPR, 31 PERCENT N1, 317 EGT, 57 PERCENT N2, 7.0 FF. CREW REPORTS THIS OCCURS AT CLIMB-OUT AND DESCENT. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PT2 LINE FROM ENGINE TO PYLON DISCONNECTED ON RIGHT ENGINE. MAINTENANCE CONNECTED THE LINE AND PERFORMED TAKEOFF POWER ASSURANCE RUNS IAW 71-00-00. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E9NE 20050106001692005010600169WP 2005 1 6 WX0400037 120040928A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A WX0AK NONE L NO TEST ININSP/MAINT 1 WP19862GA 49556 DEN - MAINTENANCE REPORTED RIGHT/LEFT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. RIGHT/LEFT OVERWING EMERGENCY EXIT LIGHTS OPERATIONALLY CHECKED GOOD.AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050106001892005010600189WP 2005 1 6 UPS04843516 120041029A53203644359503 FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 INTERCOSTAL ATTACH FITTING CRACKED ON FWD SIDE OF STA 1000 FRAME AT L30L. REMOVED 2 GUSSETS AT STA 1000 AND REMOVED CRACKED FITTING REF SRM 51-1-21, 51-1-20D, 51-3-0. INSTALLED REPLACEMENT FITTING AND 2 GUSSETS REF SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 20050106002052005010600205NM 2005 1 6 ASA0440197 120041029A531365516989 STRINGER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 STRINGER 4L CRACKED AT FASTENER. REPLACED STRINGER SPLICE AND CLIP. 2L72 4F4 FRTA16WE E21EU 20050106002062005010600206NM 2005 1 6 ASA0440190 120041021A532065458550103 SILL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CORROSION ON MOP SILL. REPLACED MOP SILL. 2L72 4F4 FRTA16WE E21EU 20050107000142005010700014EU 2005 1 7 MALA040898 120041215A38307253680117 DOME SAAB SF340 340B 7860101EU LAVATORY CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, LAVATORY DUMP DOME IS CORRODED OUT OF LIMITS PN 7253680117. DOME HAS BEEN REMOVED AND REPLACED IAW SRM 51-40-21 AND SRM 51-40-22. REFER EAMS WO NR 211236/TASK1534 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000192005010700019EU 2005 1 7 MALA040897 120041218A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15410XJ 340B410 DURING 4K INSPECTION IN BNA, INNER FLANGE OF FRAME AT FS 686.888 HAS BEEN CHAFFED OUT OF LIMITS BY CARGO DOOR CABLE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO NR S53275. REFER EAMS WORK ORDER NR 211236/TASK 2584 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/24/04. 2L72 4T RTA52EU 20050107000312005010700031EU 2005 1 7 AWXA200401354 120041201A5210 FITTING AIRBUS320 A320231 3930325EU R1 DOOR OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 PHX - EES - DURING 4-DAY CHECK AND SCHEDULED SLIDE DEPLOYMENT, THE R-1 DOOR SLIDE DID NOT DEPLOY UPON INITIAL OPENING OF DOOR, DOOR REQUIRED SLIGHT ADDITIONAL PRESSURE TO DEPLOY SLIDE. WHEN SLIDE FINALLY DID DEPLOY, IT DID SO NORMALLY. MAINTENANCE FOUND R-1 DOOR ROLLERS WERE NOT ADJUSTED PROPERLY. ADJUSTED R-1 DOOR GUIDE FITTINGS IAW AMM 52-11-00-05, SUBTASK 52-11-00-820-053, OPERATIONAL CHECK OF DOOR WAS GOOD. 2L72 4F RTA28NM 20050107000342005010700034NM 2005 1 7 AWXA200401344 120041128A2560P4010021 BATTERY BOEING737 73733A 1384673NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE RED TEST LIGHT WAS NOT WORKING ON AFT CABIN EMERGENCY FLASHLIGHT, FLASHLIGHT WORKS BUT RED LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050107000622005010700062CE 2005 1 7 62227 120040614A71101189100283 COWLING BEECH 1900 1900D 1154162CE LT ENGINE SEPARATED A AMWAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 CE07133YV UE133 PILOT RECEIVED REPORT FROM PASSENGER THAT PART OF THE LT ENG COWL MAY HAVE BLOWN OFF. PILOT CONTINUED TO DESTINATION AND LANDED WITH NO FURTHER INCIDENT. UPON IMMEDIATE WALK AROUND FOUND THAT LT ENG OB COWLING PANEL WAS MISSING AND HAD DEPARTED AIRCRAFT IN FLIGHT. INSTALLED NEW TOP CENTER COWL/FABRICATED P/N 118-910028-3 AND 129-910043-601. 2L72 4T RTA24CE 20050107000632005010700063CE 2005 1 7 62001 120040604A2612 FIRE LOOP BEECH 1900 1900D 1154162CE RIGHT FAULTY A AMWAO OTHER N FALSE WARNING UKUNKNOWN 1 CE07173YV UE173 RT FIRE LOOP ANNUNCIATOR ILLUMINATED IN FLIGHT AND REMAINED ON. FLIGHT CREW LANDED AND TAXIED TO THE GATE WITH NO FURTHER INCIDENT. NO EMERGENCY DECLARED. NO EQUIPMENT INVOLVED OR REQUIRED. T/S RT ENG FIRELOOP. REMOVED AND REPLACED FIRELOOP. 2L72 4T RTA24CE 20050107000692005010700069CE 2005 1 7 62912 120040708A3520 OXYGEN MASK BEECH 1900 1900D 1154162CE CABIN DEPLOYED A AMWAO OTHER O OTHER CLCLIMB 1 CE07127ZV UE127 PAX O2 MASKS DEPLOYING UPON AIRCRAFT CLIMB. FLIGHT CREW UNAWARE IF MASK DEPLOYMENT UNTIL LANDING IN ABQ. RESECURED PAX O2 MASK 2L72 4T RTA24CE 20050107000882005010700088SO 2005 1 7 C2XA04BT125 120041205A335074441 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2711536 145520 EWR-CO2146, CREW REPORTED EMERGENCY LIGHT OVER SERVICE DOOR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT OVER SERVICE DOOR IAW EMB145 AMM NR 33-50-09. OPS CHECKED SYSTEM GOOD. 2L72 4T RTT00011AT 20050107000962005010700096NM 2005 1 7 USAA040942 120041002A575465C26602257A SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 2 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - NR 2 SLAT, 2 SQ INCH AREA, DELAMINATION, IB T/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20050107000972005010700097NM 2005 1 7 USAA040897 120041018A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT- Q5 - FRAME, 2 INCH CRACK, STA 440 S9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A. 2L72 4F4 FRTA16WE E21EU 20050107001022005010700102NM 2005 1 7 USAA040929 120041111A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US 24557 PIT - Q1 - FRAME, .2500 INCH CRACK, FRAME 727F BETWEEN S8L AND S9L. CUT OUT CRACKED SECTION AND INSTALLED REPAIR ANGLES IAW TYP REP 53-10-20A AND EA 79502. 2L72 4F4 FRTA16WE E21EU 20050107001102005010700110EU 2005 1 7 BA04022 120040919A2530112251 COFFEEMAKER AIRBUS330 A330323 3930335EU FWD GALLEY MALFUNCTIONED A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19674UW9222 9222 342 PIT - FL 781 - APPROXIMATELY FIVE MINUTES PRIOR TO LANDING, A STRONG ELETRICAL SMELL WAS NOTED IN THE FORWARD GALLEY. AFTER THE CIRCUIT BREAKER WAS PULLED, THE SMELL SUBSIDED. MAINTENANCE REPLACED THE FORWARD GALLEY COFFEE MAKER. 2L72 4F RTA46NM 20050107001142005010700114NM 2005 1 7 BB04088 120041009A335020121 CHARGER BOEING767 7672B7 1385107NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19651US 24764 CDG - FOUND FLOOR PROXIMITY LIGHTING INOPERATIVE IN THE LEFT AISLE, FORWARD BULKHEAD AFT TO ROW 7. MAINTENANCE REPLACED THE BATTERY CHARGER (M735) AND BATTERY. 2L72 4F RTA1NM 20050107001172005010700117NM 2005 1 7 SB04151 120041029A335020121 CHARGER BOEING737 7374B7 1384702NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19777AU 24979 PIT - MAINTENANCE REPORTED THE MID-CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND THE BATTERY PACK AT SEAT ROW 21 OVERHEAD. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001362005010700136NM 2005 1 7 QXEA200400796 120041116A5230 SUPPORT FITTING BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - CARGO DOOR BOTTOM FORWARD LOCKING ROLLER SUPPORT FITTING IS GOUGED IN RADIUS AREA APPROXIMATELY .040 INCH DEEP, MATERIAL LOSS. REPAIRED IAW SRM 51-41-00 AND SUBTASK 51-40-15-400-001, PARAGRAPH M. 2H72 4T RTA13NM 20050107001972005010700197NM 2005 1 7 SWAA043729 120041229A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND BS 947, BS 967 & BS 987 AFT CABIN FLOORBEAMS UPPER CHORDS CORRODED. REPAIRED FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20050107002002005010700200NM 2005 1 7 SWAA043735 120041229A29106590737329 HYDRAULIC LINE BOEING737 7373K2 13844BANM L MLG WW LEAKING A SWAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW29340LV 23738 AIR TURNBACK / DECLARED EMERGENCY. HYD A-SYS FAILURE DURING FLIGHT. REMOVED AND REPLACED LT MLG RETRACT ACTUATOR HYD HOSE PER MM. 2L72 4F RTA16WE 20050107002012005010700201NM 2005 1 7 SWAA050007 120041231A335065C34691 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29369SW 26580 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 8 DEF, LOOSE. SECURED LIGHT ASSEMBLY PER MM. 2L72 4F RTA16WE 20050110000052005011000005EA 2005 1 10 SWIA200414230 120041206A3350 PIN CNDAIRCL600 CL6002B19 1900309EA TERMINAL BLOCK LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07912SW 7595 EMERGENCY EXIT SIGN AT SERVICE DOOR DOES NOT ILLUMINATE. RESECURED LOOSE PIN IN TERMINAL BLOCK ADJACENT TO BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000102005011000010EA 2005 1 10 SWIA200414263 120041203A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 CARGO COMPARTMENT FLOOR SUPPORT ANGLE IS CRACKED; FS 621.00 RBL 38.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" . 2L72 4F RTA21EA 20050110000122005011000012SO 2005 1 10 SWIA200414265 120041207A2120 SMOKE EMB 120 EMB120ER 3260203SO A/C PACK DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07560SW 120334 ON GROUND WITH APU, RIGHT PACK PRODUCES ON HIGH OR NORM, BURNING SMELL AND FAINT SMOKE IN COCKPIT. OPERATED RIGHT PACK IN HIGH AND NORMAL FOR 1/2 HOURS, INSPECTED GROUND COOLING FAN AND TURBINE FOUND NO DEFECTS, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050110000132005011000013SO 2005 1 10 SWIA200414239 120041206A5210 SWITCH EMB 120 EMB120ER 3260203SO PAX DOOR FAULTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07270YV 120270 FORWARD DOOR ACTUATOR LIGHT ILLUMINATED ON/OFF, UNABLE TO OPEN FORWARD DOOR. INSTALLED NEW DOOR SWITCH AT F/A STATION, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050110000152005011000015SO 2005 1 10 SWIA200414227 120041101A5534 ANGLE EMB 120 EMB120ER 3260203SO VERTICAL STAB CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LEFT FUSELAGE VERTICAL STAB CLOSING ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. LEFT FUSELAGE TO VERTICAL STAB CLOSING ANGLE REPAIRED IAW EMB E.O. 2L72 4T RTA31SO 20050110000202005011000020SO 2005 1 10 SWIA200414199 120041101A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 FLOOR SUPPORT ANGLE, STR 15, RIGHT FRAME 44-47 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPLACED IAW EMB 120 SRM 51-25-00, 51-40-02. 2L72 4T RTA31SO 20050110000222005011000022SO 2005 1 10 SWIA200414201 120041101A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 INTERCOSTAL CONNECTING CENTER FLOORBEAM TO RIGHT FLOORBEAM 479.00 AT FRAME 40 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW SRM 51-25-00, 51-40-06 AND 51-40-02. 2L72 4T RTA31SO 20050110000282005011000028EA 2005 1 10 SWIA200414180 120041118A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 VERTICAL BEAM AT FS 409+128 LBL 27 INBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV "C. 2L72 4F RTA21EA 20050110000292005011000029SO 2005 1 10 SWIA200414211 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LEFT BUTT STRAP AT Y479.00L FROM FRM 26 TO FRM 30 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION IAW 53-20-10, FOUND TO BE WITHIN LIMITS, DEPTH .004. REPROTECTED AREA IAW SRM 51-21-02 AND AMM 20-30-05. 2L72 4T RTA31SO 20050110000342005011000034EA 2005 1 10 SWIA200414173 120041204A2730 LINKAGE CNDAIRCL600 CL6002B19 1900309EA LT ELEVATOR DEFECTIVE A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07416SW 7089 UNUSUAL FLUTTERING EXPERIENCED INFLIGHT, REDUCED SPEED, FLUTTER STOPPED. REPLACED LEFT ELEVATOR NR 1-3 PCU BOLTS AND BUSHINGS, NR 2, NR 3 LINKAGE. REPLACED RIGHT PCU LINKAGE AND HARDWARE FOR SYSTEMS 1-3 IAW MM CH 27-33-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000362005011000036EA 2005 1 10 SWIA200414190 120041118A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW AFT EQUIPMENT COMPARTMENT FRAME IS CRACKED; FS 640.00 STR 9L, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-557 REV "NC" 2L72 4F RTA21EA 20050110000432005011000043SO 2005 1 10 SWIA200414234 120041205A275012064207615 CONTROL HANDLE EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07189SW 120048 WITH FLAPS SELECTED TO 25 DEGRESS AND BOTH INDICATORS AGREEING. GPWS GAVE "TOO LOW FLAPS" BETWEEN 500 FT AND 100 FT AGL. REMOVED AND REPLACED FLAP CONTROL HANDLE IAW MM 27-50-01. OPERATIONAL CHECK GOOD, PN 120-64207-615 OFF 120040. 2L72 4T RTA31SO 20050110000442005011000044EA 2005 1 10 SWIA200414240 120041204A2751 TRANSMITTER CNDAIRCL600 CL6002B19 1900309EA T/E FLAP INTERMITTENT A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07412SW 7101 INTERMITTENT (STALL FAIL), (WINDSHEAR FAIL) MESSAGES WITH FLAPS AT 30 DEGREES AND AT 8 DEGREES. REMOVED AND REPLACED LEFT AND RIGHT FLAP POSITION TRANSMITTERS IAW MM 27-55-01, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000462005011000046EA 2005 1 10 SWIA200414182 120041118A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 CORROSION ON FRAME 349.0 STR 26L AND ON FRAME 364.0 STR 26L IN AVIONICS CRAWL WAY. (ITEM FOUND AT C-CHECK INSPECTION.) AFFECTED AREAS REPAIRED IAW CRJ SRM 53-21-15. 2L72 4F RTA21EA 20050110000482005011000048EA 2005 1 10 SWIA200414184 120041118A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 MAIN AVIONICS COMPARTMENT INTERCOSTAL STR 26L BETWEEN FS 349 AND FS 364 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) CORRODED SECTION OF INTERCOSTAL BLENDED OUT IAW CRJ SRM 53-00-00 MATERIAL LOSS OF .004' WITHIN LIMITS. REINSTALLED INTERCOSTAL IAW CRJ SRM 51-42-21, 51-42-06, 51-23-00, 51-25-06, 51-25-16. 2L72 4F RTA21EA 20050110000522005011000052SO 2005 1 10 SWIA200414205 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 BUTT STRAP AT Y479.00R FROM FRAME 34-39 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02 & 51-25-00. 2L72 4T RTA31SO 20050110000542005011000054SO 2005 1 10 SWIA200414221 120041101A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 INTERCOSTAL FLOORBEAM JUST AFT OF FRAME 15 FROM Y479.00L TO EDGE OF DOOR IS CORRODED. FLOORBEAM REPLACED IAW SRM 51-40-02 & 51-22-00. 2L72 4T RTA31SO 20050110000562005011000056EA 2005 1 10 SWIA200414266 120041215A2781 SENSOR CNDAIRCL600 CL6002C10 1390015EA L/E SLAT FAULTY A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07712SK 10172 SLAT FAULT STATUS MESSAGE CLIMBING OUT OF FL250. REPLACED INBOARD LEFT SLAT DISCONNECT SENSOR IAW MM 27-81-39. OPERATIONAL CHECK GOOD IAW MM 27-81-39. 2L72 4F RTA21EA 20050110000572005011000057EA 2005 1 10 SWIA200414174 120041129A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07916SW 7634 CABIN EMERGENCY FLOODLIGHT AT ROW 10 IS INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW CRJ 200 MM 33-51-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000612005011000061 2005 1 10 SWIA200414243 420041211A22136229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT SYS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07932SW408 408 7714 STAB CH 1 INOPERATIVE. STATUS AP PITCH TRIM CAUTION, STAB TRIM/MACH TRIM CAUTION. REMOVED AND REPLACED HSTCU AND FCC. OPERATIONAL CHECK GOOD PN 7060-9, SN OFF 1057. 2L72 4F RTA21EA 20050110000642005011000064EA 2005 1 10 ZJW2004F00002 220040913A8530 CYLINDER GULSTM500 500B 0141106SW LYC O540 IO540E1A5 41532EA NR 1 BROKEN E ZJWAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 CE056154X1426832 500B98324 NR 1 CYLINDER BARREL BROKE CAUSING PISTON TO BE CAUGHT ON THE DOWN STROKE. THEN ROD BOLTS BROKE AND ROD CAP CAME OFF. ENGINE LOST MUCH OF OIL AND WAS FEATHERED AND LANDED SAFELY. 1H72 3O3 O 6A1 1E4 20050110000682005011000068EU 2005 1 10 USAA041009 120041111A5320D5347217320100 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 2.5 INCH X 1 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500-010; MAIN CABIN FLOOR AT FR 67, BL - Y170. INSTALLED NEW BEAM IAW SRM 53-00-14, 51-74-00, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110000692005011000069NM 2005 1 10 USAA040982 120041113A53206935352414 TIE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - STRINGER TIE, 1 INCH CRACK AT STA 827, S4L. DEFECTIVE PART REPLACED WITH IDENT PART. 2L72 4F4 FRTA16WE E21EU 20050110000722005011000072EU 2005 1 10 USAA040997 120041112A5321D5367180500400 FLOOR PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A K NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - FLOOR PANEL, 0.017 INCH X 1.3 INCH X 1.1 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53100, R-2 DOOR- Y1732- Z240, FR 66-FR68. INSTALLED NEW PANEL IAW SRM 53-12-12, 53-12-00. 2L72 4F4 FRTA28NM E37NE 20050110000782005011000078NM 2005 1 10 USAA041043 120041102A575465C26603102 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - TOP SKIN, 3 INCH X 3 INCH AREA AND LOWER SKIN DAMAGE 1 INCH SQUARE, DELAMINATION AND SKIN DAMAGE, NR 4 SLAT TOP SURFACE T/E. INSTALLED FILLER AND INTERNAL DOUBLER, NEW CORE AND TOP DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050110000802005011000080EU 2005 1 10 USAA041015 120041201A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - SILL, 1.5 INCH X 1.5 INCH X .060 INCH DEEP; CORROSION; LEVEL 2; TASK JA-260-53500-010, MAIN CABIN FLOOR, FR C66, Y1732. REMOVED AND REPLACED SILL IAW SRM 53-41-14. 2L72 4F4 FRTA28NM E37NE 20050110000832005011000083NM 2005 1 10 USAA041061 120041123A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN SURFACE, 5 INCH LONG GOUGE, RUDDER LT SIDE STA 186, NEAR T/E. INSTALLED REPAIR PLYS IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050110000842005011000084EU 2005 1 10 USAA041000 120041111A5320D5367009923600 STRAP AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - STRAP, 9 INCHES X 2 INCHES X .020 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53100, FRAME 68Y=1490. REMOVED AND REPLACED IAW SRM 51-42-11, 53-02-00. 2L72 4F4 FRTA28NM E37NE 20050110000932005011000093EU 2005 1 10 USAA040996 120041112A5320D5367009200300 STRAP AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - STRAP, 0.38 INCH X 1.3 INCH X 1 INCH AREA, CORROSION; LEVEL; TASK NR JA-260-53100-002; R-2 DOOR - Y1732 FR 66 AND 68 - Z240. INSTALLED NEW STRAP IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110000992005011000099NM 2005 1 10 USAA041034 120041111A552265C25746154 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - LOWER SKIN SURFACE, 2 INCH SQ DELAMINATION, RT LELVATOR 41 INCH FROM IB END AND 13 INCH AFT OF L/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED SER COR, REPLACEMENT SKIN PANEL IAW SRM, EA. 2L72 4F4 FRTA16WE E2GL 20050110001012005011000101EU 2005 1 10 USAA041002 120041112A5321 FLOOR PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - FLOOR PANEL, .04 INCH X .5 INCH X 3.2 INCH AREA, L1 ENTRY DOOR FLOOR PANEL NR 221FF, +Y1732, FR 16420. INSTALLED NEW PANEL IAW SMM 53-12-12, 53-12-00. 2L72 4F4 FRTA28NM E37NE 20050110001022005011000102EU 2005 1 10 USAA041003 120041115A5315D5347219021100 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 1.5 INCH X 1 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FLOORBEAM AT FR 66, BL-Y1292. REMOVED AND REPLACED BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001042005011000104EU 2005 1 10 USAA040990 120041117A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - SILL, BLENDED AREA 2.0 INCH X 1.5 INCH X .07 INCH DEEP. CORROSION; LEVEL 2 TASK NR JA-260-53500-004; L-2 DOOR SILL, FWD FLANGE FR 66,Y 1482. REPLACED SILL IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001092005011000109EU 2005 1 10 USAA040956 120041031A5320D5311281400200 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - FLOOR SUPPORT, 2 INCHES X 12 INCHES X 0.020 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR BET FR 16, 20, BL-Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110001102005011000110EU 2005 1 10 USAA040957 120041102A5320D53112571001 WEB AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - FLOOR WEB, 1.5 INCH X 2 INCHES X 0.50 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR; Y1584, BET FR14 AND 16. REMOVED AND REPLACED IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050110001112005011000111EU 2005 1 10 USAA040959 120041101A5320D53111414202 SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - SUPPORT, 2 INCH X 5 INCHES X .025 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FL -Y189, FR 20. REMOVED AND REPLACED IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050110001122005011000112NM 2005 1 10 USAA040981 120041121A5313 STRINGER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - STRINGER, .25 INCH LONG CRACK AT STA 887 S-9L. INSTALLED (2) REPAIR ANGLES IAW TR 53-10-20A, 51-30-02, 51-40-09, 51-30-01. 2L72 4F4 FRTA16WE E21EU 20050110001132005011000113NM 2005 1 10 USAA040980 120041115A531365C35945 STRINGER BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 PIT - Q5 - STRINGER, .75 INCH CRACK, S-5A, BS 1138, INSTALLED DOUBLER IAW T/R 53-80-04 AND 53-00-01, FIG 221. 2L72 4F4 FRTA16WE E21EU 20050110001142005011000114NM 2005 1 10 USAA040974 120041116A5311 FAILSAFE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - FAIL SAFE CHORD, .75 INCH CRACK, STA 380 AT STR 15R. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM 51-70-11, FIG 1. 2L72 4F4 FRTA16WE E21EU 20050110001152005011000115EU 2005 1 10 USAA040964 120041029A5320D5347112420100 SHEAR PLATE AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US 0861 BFM - S2 - SHEAR PLATE, 1 INCH X 1 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW 69 AND 70, BL - Y1292. REMOVED AND REPLACED SHEAR PLATE (WEB) IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050110001172005011000117EU 2005 1 10 USAA041023 120041201A5320D5347217220400 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1 INCH X .050 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500-006, MAIN CABIN FLOOR, FR C68, Y1292. REMOVED AND REPLACED BEAM. 2L72 4F4 FRTA28NM E37NE 20050110001182005011000118NM 2005 1 10 USAA041033 120041124A575165C2591111A SPAR BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT AILERON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19541AU53047 23700 PIT - Q2 - SPAR, .50 INCH X .25 INCH AREA COMPOSITE DAMAGE/ DELAMINATION. LT AILERON L/E SPAR 26 INCHES FROM OB END UPPER FLANGE. REMOVED DAMAGED AREA AND TAPER SANDED FLANGE, INSTALLED REPAIR PLYS IAW EA, SRM. 2L72 4F4 FRTA16WE E21EU 20050110001212005011000121EU 2005 1 10 USAA041018 120041126A5315D5347209000200 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - FLOORBEAM, 3 INCH X 2 INCH X .040 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500 FR 66, Y765 CABIN FLOOR STRUCTURE. REMOVED AND REPLACED BEAM IAW SRM 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001262005011000126EU 2005 1 10 USAA040962 120041031A5320D5311281300251 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - FLOOR SUPPORT, 1.5 INCH X 2 INCHES X .040 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-200-53500, BTW FR 16 AND 20, Y1292, FLOOR SUPPORT. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110001282005011000128NM 2005 1 10 USAA040968 120041026A5310 CREASE BEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - CREASE BEAM WEB, .75 INCH (6 AREAS), CORROSION; NO LEVEL OR TASK, BETWEEN STA 420 AND STA 440, RT SIDES. CREASE BEAM WEB MFG IAW DWG 65-96956 AND BACD2003. 2L72 4F4 FRTA16WE E21EU 20050110001292005011000129EU 2005 1 10 USAA041027 120041130A5320D5347209001100 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR AT FR 66, BL Y1292. REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001312005011000131EU 2005 1 10 USAA041016 120041127A5320D5311281520200 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - FLOOR SUPPORT, 2.5 INCH X 2.5 INCH X .069 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-22053500, FLOOR SUPPORT AT FRAME 16 AT Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001342005011000134NM 2005 1 10 USAA041030 120041206A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US 23742 PIT - B CK - SKIN, 3 INCH CRACK, SKIN AT STA 740, STR 18R. INSTALLED DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050110001422005011000142EU 2005 1 10 USAA041022 120041201A5320D5347209001000 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - BEAM, 2 INCH X 2 INCH X .045 INCH DEEP CORROSION; LEVEL 2; TASK NR JA-260-53500-002, MAIN CABIN FLOOR, FR C66, Y1292. REMOVED AND REPLACED BEAM IAW SRM 53-00-14. 2L72 4F4 FRTA28NM E37NE 20050110001432005011000143EU 2005 1 10 USAA041025 120041130A5320D5347217220390 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1 INCH X .030 INCH AREA CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR AT FR 68, BL - Y1292. REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001442005011000144EU 2005 1 10 USAA040958 120041102A5320D5311281700400 TRACK AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - TRACK ASSEMBLY, 2 INCH X 2 INCH X 0.50 INCH AREA, CORROSION LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR- Y254 BET FR16 AND 23. REMOVED AND REPLACED IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050110001482005011000148NM 2005 1 10 USAA041055 120041123A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN SURFACE, 1.5 INCH LONG, TAPERING DEPTH, DEEP CHAFE WEAR, RUDDER LOWER RT L/E CORNER. INSTALLED REPAIR PLYS IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001552005011000155NM 2005 1 10 USAA040988 120041202A5320 ANGLE BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU39875 27123 CLT - C-4 - Z-ANGLE, 6 INCH SQUARE CORROSION AT STATION 324-318, RBL 66. INSTALLED ANGLE DOUBLER IAW EA. 2L72 4F4 FRTA2NM E12EU 20050110001562005011000156NM 2005 1 10 USAA040973 120041111A5343 FITTING BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE LT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT- Q4 - MLG SUPPORT BEAM AFT FITTING, .0625 INCH CRACK (2) HOLES ON MLG SUPPORT AFT BEAM FITTING, 12 O`CLOCK AND 9 O`CLOCK. REPLACED LT MGL SUPPORT BEAM AFT FITTING IAW EO 5702V054. 2L72 4F4 FRTA16WE E2GL 20050110001572005011000157NM 2005 1 10 USAA041040 120041111A552265C25746154 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .75 INCH GOUGE, RT ELEVATOR AT 84.5 AND 4 - 5 INCH IN FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050110001612005011000161EU 2005 1 10 USAA041028 120041127A5320D53471124200 SHEAR WEB AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - SHEAR WEB, 1 INCH X .5 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR, BETWEEN FR 69-70, Y1292. REPLACED WEB IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001632005011000163NM 2005 1 10 USAA041060 120041123A554165C2584151 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER SEPARATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - CONDUCTIVITY FRAME, 15 INCHES X 12 INCHES, SEPARATION, RUDDER TOP LT SURFACE, UPPER LT CONDUCTIVITY FRAME SEPARATING FROM RUDDER. INSTALLED NEW CONDUCTIVITY FRAME IAW MM AND BAC 5010 AND DWG 65C25841. 2L72 4F4 FRTA16WE E21EU 20050110001642005011000164NM 2005 1 10 USAA040986 120041130A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU39875 27123 CLT - C-4 - FLOORBEAM, 9 INCH AREA, CORROSION AT STA 324, RBL 43-49. REPLACED T-CAP SECTION IAW EA. 2L72 4F4 FRTA2NM E12EU 20050110001672005011000167NM 2005 1 10 USAA041045 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA, SINGLE LAYER DAMAGE. RUDDER LT SIDE 105./5 INCHES FROM BOTTOM AND .3750 FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI PLY REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001682005011000168EU 2005 1 10 USAA041005 120041115A5315D5347218920200 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 2.5 INCH X 1.25 INCH X 0.06 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FLOORBEAM BTW FR 68-69 AT BL-Y1162. REMOVED AND REPLACED BEAM PER SRM 51-74-00, 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001692005011000169NM 2005 1 10 USAA040860 120041021A5743 FITTING BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT MLG WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT - Q4, STAB BEAM FITTING, WORN BUSHING. STAB BEAM LUG, RT MLG SUPPORT BEAM. REPLACED STAB BEAM FITTING IAW AMM 57-15-00-434. 2L72 4F4 FRTA16WE E2GL 20050110001732005011000173NM 2005 1 10 USAA041039 120041111A552265C25746154 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 -LOWER SKIN SURFACE, SINGLER LAYER COMPOSITE DAMAGE .50 INCH GOUGE. RT ELEVATOR AT STA 62 AND 15 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050110001752005011000175NM 2005 1 10 USAA041047 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DAMAGE, 37 INCH FWD OF T/E, 48 INCH UP FROM BOTTOM. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI-LAYERED REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001772005011000177NM 2005 1 10 UIEA200400190 120041112A2780126344171 PDU BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE L/E SLAT FAILED A UIEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA15526MC 22337 DURING CLIMB-OUT, NR 3 LEADING EDGE FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 3 LE PDU. OPS CHECK OK IAW MM 27-81-03. PDU OFF PN 126344-17-1, SN 22337, TOTAL MAINT DELAY, 3 HRS, 17 MIN. NOTE: NO FUEL WAS DUMPED. 2L74 4F4 FRTA20WE E23EA 20050110001782005011000178CE 2005 1 10 UG8AGM0417 120041112A27413G5212C SENSOR CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL STAB TRIM FAILED E UG8AK NONE O OTHER ININSP/MAINT 1 GL235113 7500013 STAB TRIM FAILED ON PREFLIGHT INSPECTION. REPLACED STAB TRIM POSITION SENSOR. 2L72 4J4 FRTT00007WITE6CH 20050110001802005011000180EU 2005 1 10 SIMA3453001S 120041026A33202LA005932 CIRCUIT BOARD SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN FAILED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21345SB 340B345 DISPATCH REPORT AC DIVERTED DUE TO SMOKE SMELL IN CABIN. CAPT REPORTS THAT THE SMELL CAME FROM THE AREA OF ROW 12 BC. C/A RAI 12A-12BC PSU IAW MM 25-20 OPS CK GOOD, ALL LITES AND EMERGENCY LIGHTING B. (SW21200501237) 2L72 4T4 TRTA52EU E8NE 20050110001852005011000185SO 2005 1 10 SIMA200432702 120041117A2611FD5765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LAVATORY MALFUNCTIONED A SIMAB EMER. DESCENT N FALSE WARNING CLCLIMB 1 SW21691AE 14500860 EICAS LAVATORY SMOKE INDICATION DURING CLIMB OUT. INSPECTED LAVATORY FOUND NO EVIDENCE OF SMOKE. REPLACED LAVATORY SMOKE DETECTOR IAW AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501195) 2L72 4T4 FRTT00011ATTE6CH 20050110001862005011000186SO 2005 1 10 SIMA200431701 120041109A27503635001001 BRAKE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL LT & RT FLAPS MALFUNCTIONED A SIMAK NONE F FLT CONT AFFECTED APAPPROACH 1 SW21726AE 145314 DURING APPROACH TO LGA WHEN CREW SELECTED FLAPS THE FLAPS FROZE WOULD NOT MOVE FROM 0 DEGREES. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FLAP TRANSMISSION BRAKES IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050111000032005011100003GL 2005 1 11 ERAA098179 220040811A7323252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE SPLIT B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH5177 598 10 PERCENT TORQUE SPLIT WHEN ADJUSTED ALL THE WAY UP, LADDER GOVERNOR DROPS OUT OF SERVICE LIMITS. OVERHAULED IAW HONEYWELL OHM FORM 15 1095A. 1G72 3U3 U H3EU E4CE 20050111000042005011100004WP 2005 1 11 ABXA040389 120041203A32607000010101 SWITCH DOUG DC9 DC941 302207NWP RT MLG DEFECTIVE A ABXAO OTHER O OTHER NRNOT REPORTED 1 GL23968AX 47499 RT MLG DOWN (GREEN) LIGHT DID NOT ILLUMINATE (ALTERNATE DOWN LIGHTS INDICATED DOWN), RECYCLED GEAR. ALL 3 DOWN LIGHTS CAME ON. REPLACED RIGHT MAIN LANDING GEAR DOWN LOCK SWITCH IAW PARA 3 OF DC9 AMM 32-60-01-2-0101, PARA 1D APPLIED, NO GEAR SWING REQUIRED. 2L72 4F A6WE 20050111000052005011100005GL 2005 1 11 ERAA098180 220040418A7321252464431N FUEL CONTROL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE STALLED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03125EH10372 S562 HAS COMPRESSOR STALL OFF IDLE WHILE ADVANCING THROTTLE TO FULL FCU TESTED WITHIN SERVICE LIMITS. FCU TESTED IAW HONEYWELL OHM FORM 15-602E AND RESET TO NOMINAL LIMITS. 1G72 3U3 U H3EU E4CE 20050111000132005011100013WP 2005 1 11 AALA20041258 120041230A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21451AA 49477 DEN - OVERHEAD EMERGENCY LIGHTS BETWEEN AFT LAVS INOPERATIVE. REPLACED BATTERY PACK B5-27 FOR OVERHEAD EMERGENCY LIGHTS BETWEEN AFT LAVS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000152005011100015WP 2005 1 11 AALA20041260 120041231A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217506 49800 STL - RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000192005011100019WP 2005 1 11 AALA20041263 120041229A2910 FITTING DOUG DC9 DC982 3022082WP THRUST REVERSER LOOSE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21471AA 49601 DFW - EN ROUTE DFW-PHL SMOKE IN CABIN. RETURNED DFW AND LANDED WITHOUT INCIDENT. FOUND LOOSE HYDRAULIC LIGHT TEE FITTING ABOVE LEFT HAND THRUST REVERSER CONTROL VALVE. TIGHTENED HYDRAULIC LIGHT TEE FITTING ABOVE LEFT HAND THRUST REVERSER CONTROL VALVE. ACCOMPLISHED PACK BURNOUT PER CARD 21 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000202005011100020WP 2005 1 11 AALA20041264 120041225A3230 LANDING GEAR DOUG DC9 DC982 3022082WP NLG MALFUNCTIONED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21413AA 49324 DTW - EN ROUTE DTW-DFW COULD NOT RETRACT LANDING GEAR. HANDLE STOPPED HALF-WAY UP. RETURNED DTW AND LANDED WITHOUT INCIDENT. OPERATED GEAR HANDLE SEVERAL TIMES AND SWUNG NOSE GEAR SEVERAL TIMES. SERVICED NOSE GEAR WITH 5606 AND NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000212005011100021NM 2005 1 11 AALA20050005 120041208A2740 MODULE BOEING757 757223 1384957NM STABILIZER TRIM MALFUNCTIONED A AALAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 SW21669AA 25334 JFK - DURING TAKEOFF ROLL VERTICLE STABILIZER TRIM WENT FROM 4.6 TO 7.5 UNCOMMANDED RESULTING IN RED STABILIZER MESSAGE AND TAKEOFF WARNING HORN. ABORTED TAKEOFF. REPLACED LEFT AND RIGHT STABILIZER TRIM POSITION MODULES AND LEFT STABILIZER TRIM AND ELEVATOR ASYMMETRY LIMIT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. AWAITING TEAR DOWN REPORT FROM BOEING ON LEFT STABILIZER TRIM AND ELEVATOR ASYMMETRY LIMIT MODULE. 2L72 4F RTA2NM 20050111000232005011100023NM 2005 1 11 AALA20050008 120041226A2421 IDG BOEING757 757223 1384957NM RT ENGINE LEAKING A AALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21188AN 32382 LAX - RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED DURING CRUISE. DISCONNECTED IDG. REPLACED RIGHT HAND IDG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050111000282005011100028NM 2005 1 11 AWXA200401462 120041205A53206545812521 ANGLE BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON BEAM (ANGLE) AT BS 328 BETWEEN RBL 15 AND RBL 50, WL 208. MAINTENANCE REMOVED CORRODED ANGLE AT BS 328 FROM RBL 15 TO RBL 50; FABRICATED A NEW REPLACEMENT BEAM PER DWG 65-45812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02 FIG 1, 3, 8 & 12. 2L72 4F RTA16WE 20050111000332005011100033EU 2005 1 11 AWXA200401466 120041215A2597 WIRE AIRCRUISERS AIRBUS320 A320232 3930326EU EVAC SLIDE FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW407385313 C0061 527 MCN - EEL - DURING C-08 CHECK THE EMERGENCY LIGHT TEST FROM THE PROGRAMMING AND TEST PANEL INDICATED EXTERNAL LOADS FAILURE. MAINTENANCE TROUBLESHOT WIRING AND FOUND L-1 DOOR SLIDE CIRCUIT OPEN, REMOVED AND REPLACED L-1 DOOR SLIDE IAW T/C R1C25305, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050111000402005011100040EU 2005 1 11 AWXA200500012 120041110A5314D53371827208 ATTACH ANGLE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK A .75 INCH CRACK WAS FOUND IN KEELBEAM LT ATTACH ANGLE, AFT OF MAIN LANDING GEAR DOOR BETWEEN FR 46 AND FR 47, STR 43 LT. MAINTENANCE REMOVED DAMAGED KEELBEAM LT ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER ER 26-5335-04355-SS2, PER ER 26-5335-04355-SS2 A ITEM IS TO BE INSPECTED EVERY 3500 FLIGHT CYCLES OR EVERY C-CHECK NOT TO EXCEED 15 MONTHS OR UNTIL PART HAS BEEN REPLACED WITH ORIGINAL MATERIAL, OR MATERIAL CALLED FOR IN A320 SRM 53-35-11 FIG 229. 2L72 4F RTA28NM 20050106001762005010600176WP 2005 1 6 UPS04843582 120041121A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 STA 70 FRAME CORRODED BEYOND LIMITS ABOVE LONG 21R. REMOVED CORROSION, TREATED AND PRIMED SITE PER SRM51-1-8. FABRICATED REPAIR DOUBLER FROM SHT7075O-.080 PER EO DC8- 5310-11728/DWGDC8-53A-011. HEAT TREAT TO T6 PER DPS7.00 INSTALLED REF SRM 51-1-20D, 51-1-8, EOD C8-5310-11728. 2L74 4F RT4A25 20050106001802005010600180WP 2005 1 6 UPS04843580 120041118A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LONG 9R CRACKED AT STA 1735 FRAME ATTACH. CUT OUT DAMAGE, NDT VERIFIED PER SPM 06-10-01.001. FABRICATED FILLER FROM SHT7075T6/.063 AND DOUBLER FROM S2645716 EXTRUSION PER SRM 53-2-2 FIG 11. INSTALLED PARTS REF SRM 51-1-8, 51-1-20D, 51-3-0. 2L74 4F RT4A25 20050106001812005010600181WP 2005 1 6 UPS04843581 120041119A53203750257U1 SPLICE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LONG 31R SPLICE FITTING CRACKED AT STA 1050. REMOVED AND REPLACED SPLICE FITTING REF SRM 51-1-20D, 51-1-8, 51-1-22, 51-3-2. 2L74 4F RT4A25 20050106001832005010600183NM 2005 1 6 UPS04243559 120041130A3510 VALVE BOEING727 727185C 138406NNM O2 MASK STUCK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 CAPT O2 MASK HAS STUCK VALVE. REPLACED MASK ASSY, OPS CK NORMAL. 2L73 4F A3WE 20050106001912005010600191WP 2005 1 6 UPS04843518 120041030A531337585931 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 LONGERON 34L CRACKED AT STA 1260-1280. REMOVED LONG SPLICES AT STA 1270 STA 1350 PER SRM 51-1-20D OPENED SKIN FROM STA 1250-1350 FOR ACCESS REF SRM 51-1-21, 51-1-20D. REMOVED, FABRICATED, AND REPLACED LONG 34L FROM STA 1270-1350 REF DWG3758593, AND CLOSED SKIN PER SRM 51-1-21 AND 51-1-20D. REINSTALLED SPLICE FITTINGS REF SRM 51-1-20D. 2L74 4F RT4A25 20050106001952005010600195WP 2005 1 6 UPS04843524 120041103A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 RT WING UPPER SKIN CORRODED AROUND HILOCK AT XRS554, ABOVE S54. NDT VERIFIED MATERIAL THICKNESS AT CORROSION REMOVAL SITE RANGED FROM .090-0.125. CUT OUT CORROSION SITE REF SRM 57-2-1 FIG28. FABRICATED DOUBLER AND FILLER FROM SHT7075T6-.190, MACHINED FILLER TO MATCH THICKNESS, INSTALLED AND SEALED CONICAL WASHERS AND REPAIR PARTS REF SRM 57-2-1 FIG 28, 51-1-20D, 51-1-8, 51-1-20B, 51-1-15. 2L74 4F RT4A25 20050106001982005010600198WP 2005 1 6 UPS04843528 120041117A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING L/E LOWER RIB CRACKED AT END, STA 753.75. STOP DRILLED CRACK, NDT VERIFIED PER SPM06-10-01.001. FABRICATED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050106002012005010600201WP 2005 1 6 UPS04843531 120041117A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING L/E RIB CRACKED AT LOWER AND UPPER ENDS, STA835. STOP DRILLED CRACKS. NDT VERIFIED BOTH REF SPM 06-10-01.001. FABRICATED UPPER REPAIR FROM 7075T6-.050 AND FABRICATED LOWER REPAIR FROM S25972423 EXTRUSION REF SRM57-3-1, 57-2-0. INSTALLED REPAIRS REF SRM 57-2-0, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050106002022005010600202WP 2005 1 6 UPS04843532 120041117A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 LT WING L/E RIB CRACKED AT STA 728 UPPER AFT END. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D. 2L74 4F RT4A25 20050106002042005010600204WP 2005 1 6 UPS04843544 120041119A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 RT WING O/B L/E RIB CRACKED NEAR XFS722.50. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE REPAIR ANGLE FROM SHT7075T6-.063 AND INSTALLED SAME REF SRM 57-3-3, 57-2-0 FIG2, 51-1-8, 51-1-21. 2L74 4F RT4A25 20050106002152005010600215NM 2005 1 6 ASA0440184 120041016A5310654797387 CREASE BEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 PAE - CORROSION ON CREASE BEAM WEB AT NUT-PLATE HOLES. REMOVED FABRICATED AND INSTALLED NEW WEB. 2L72 4F4 FRTA16WE E21EU 20050107000072005010700007 2005 1 7 QXEA200400927 420041228A2210 AUTOPILOT SYS CNDAIRCL600 CL6002C10 1390015EA COCKPIT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING UKUNKNOWN 1 NM09616QX 10128 CREW FOLLOWED ABNORMAL CHECKLIST AND TURNED OFF AUTOPILOT WHEN THEY RECEIVED A MASTER CAUTION "AUTOPILOT RIGHT TRIM" MESSAGE. MAINTENANCE PERFORMED FUNCTIONAL TEST OF AILERON TRIM SYSTEM. THE FUNCTIONAL AND OPERATIONAL TESTS WERE GOOD. THE OPERATIONAL CHECK FLIGHT WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050107000082005010700008NM 2005 1 7 QXEA200400928 120041228A33506038443 BATTERY DHAV DHC8 DHC8202 2809007NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09345PH1582073 476 SEA - UPON INSPECTION MAINTENANCE FOUND FORWARD EXIT EMERGENCY LIGHTING FLOOR TRACK STRIP RED LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK LIGHTING STRIP AND BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050107000122005010700012EU 2005 1 7 MALA040896 120041201A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 DURING 4K INSPECTION IN BNA, SEAT TRACK AT BLO, BETWEEN FS 294 AND 363 IS CORRODED OUT OF LIMITS AT 3 LOCATIONS, 294, 318, 340. THE DAMAGED AREAS WERE REPAIRED IAW MESABA EO #S53079. REFER EAMS NR 211114, TASK 1524 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/2/2004. 2L72 4T RTA52EU 20050107000292005010700029NM 2005 1 7 AWXA200401358 120041206A3350BR964411 LIGHT BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 DFW - EEL - DURING A-01 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050107000332005010700033NM 2005 1 7 AWXA200401359 120041206A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28805AW3081 338 1049 LAX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050107000352005010700035EU 2005 1 7 AWXA200401378 120041111A5320 DUMMY RAIL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON DUMMY RAIL -Y1379 AT FS 16. MAINTENANCE REMOVED CORRODED DUMMY RAIL -Y1379, FROM FS 12 TO FS 16; FABRICATED A NEW REPLACEMENT RAIL; INSTALLED REPAIR PARTS IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050107000422005010700042EU 2005 1 7 AWXA200401379 120041116A1430D5755103920051 BOLT AIRBUS320 A320232 3930326EU NR 1 SPOILER CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 DURING C-08 CHECK LEVEL II EXFOLIATION CORROSION WAS FOUND ON LT NR 1 SPOILER HINGE BOLTS. MAINTENANCE REMOVED AND REPLACED CORRODED NR 1 SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-41-020-050-B, AND SUBTASK 27-64-41-420-050-B. 2L72 4F RTA28NM 20050107000472005010700047EU 2005 1 7 AWXA200401104 120040925A5321D5367205400000 FLOOR PANEL AIRBUS320 A320232 3930326EU FUSELAGE DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28658AW 1110 DURING BC-4 CHECK, AFT CARGO COMPARTMENT FLOOR PANEL 151LF WAS FOUND DISBONDED BETWEEN FS 56 AND FS 58. MAINTENANCE REMOVED FLOOR PANEL 151LF; CUTOUT DISBOND AREA; PERFORMED EDGE FILLING PROCEDURE (DOUBLER) IAW A320 SRM 53-02-00, FIG 209. 2L72 4F RTA28NM 20050107000522005010700052NM 2005 1 7 AWXA200401236 120041106A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN FAULTY A AWXAK NONE O OTHER ININSP/MAINT 1 WP28805AW21725 1049 DURING 4-DAY CHECK, OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM FOUND THE LT OVERWING EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20050107000702005010700070CE 2005 1 7 65218 120040923A5210 ROD END BEECH 1900 1900D 1154162CE PAX DOOR OUT OF ADJUST A AMWAO OTHER O OTHER UKUNKNOWN 1 CE07139ZV UE139 WHEN CREW WENT TO CLOSE AIRSTAIR DOOR, DOOR WOULD NOT CLOSE PROPERLY PASSENGERS WHERE DEPLANED AND MAINTENANCE CALLED. ADJUSTED ASD COUNTER BALANCE RODENDS, CK GOOD. 2L72 4T RTA24CE 20050107000792005010700079SO 2005 1 7 C2XA04IA147 120041120A3350RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716911 145446 IAH - FLIGHT 2680, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW SEVEN (7) WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY. OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050107000802005010700080SO 2005 1 7 C2XA04IA143 120041117A521014525311403 SEAL EMB 145 EMB145XR 3260214SO PAX DOOR LACK OF LUBE A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW2717115 145666 DURING PREFLIGHT, THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. MAINTENACE LUBED THE SEAL AND OPERATIONALLY CHECKED THE DOOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20050107000862005010700086SO 2005 1 7 C2XA04TY177 120041201A33502013A BATTERY EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27145436769 145553 AIRCRAFT 543 WAS IN FOR A SERVICE/ROUTINE INSPECTION WHEN MAINTENANCE FOUND THE AFT OVERWING RT AND LT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AND OPS CHECK WAS GOOD IAW EMB 145 AMM 33-50-04. AIRCRAFT WAS RELEASED UPON COMPLETION OF THE SERVICE/ROUTINE INSPECTION. 2L72 4T RTT00011AT 20050107000912005010700091NM 2005 1 7 USAA040861 120041021A5755 ATTACH BRACKET BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT SPOILER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT - Q4, ATTACH BRACKET, MIGRATING AND MISSING BUSHINGS. RT MLG SUPPORT BEAM, SPOILER ACT ATTACH BRACKET. REPLACED SPOILER ACTUATOR ATTACH BRACKET IAW MFG DWG 63895. 2L72 4F4 FRTA16WE E2GL 20050107000932005010700093NM 2005 1 7 SB04141 120041009A361046638 CHECK VALVE BOEING737 737401 1384701NM RT A/C BAY BROKEN A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19423US1429914299 23990 MCO - FLT 1276, AFTER DEPARTURE FROM RSW, EN ROUTE TO PHL, CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE NORMALLY. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE PNEUMATIC GROUND SERVICE CONNECTION CHECK VALVE STUCK OVER CENTER IN THE OPEN POSITION. THE MECHANICAL STOP HAD DEPARTED THE DUCT ALLOWING THE CHECK VALVE TO OVER CENTER IN THE OPEN POSITION. REPLACED MECHANICAL STOP AND REPLACED BROKEN FASTENERS ON HINGE HALVES FOR CHECK VALVE. PRESSURIZED AIRCRAFT. PRESSURIZATION CHECK GOOD. 2L72 4F RTA16WE 20050107000982005010700098NM 2005 1 7 USAA040899 120041026A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SUPPORT ANGLE, 1 INCH LONG, CRACKED. SUPPORT DOWNLOCK VIEWER LT FWD CORNER, STA 259.5. REPLACED PART IAW DWG 65-45833. 2L72 4F4 FRTA16WE E21EU 20050107001002005010700100NM 2005 1 7 USAA040941 120041021A53201132009 CHANNEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - CHANNEL, .5 INCH CRACK, STA 540 LBBL 0, RBBL U CHANNEL. REPLACED CHANNEL IAW SRM 53-00-03. 2L72 4F4 FRTA16WE E21EU 20050107001082005010700108NM 2005 1 7 USAA040910 120041021A5320653535214 STRINGER CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - CLIP, .2500 INCH CRACK, RIVET OF STRINGER CLIP, STA 767 S4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-01 AND 51-40-03. 2L72 4F4 FRTA16WE E21EU 20050107001182005010700118NM 2005 1 7 SB04139 120041005A495036052392 CONTROL VALVE BOEING737 737401 1384701NM APU FAULTY A USAAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19420US12096882 23987 RSW - FLT 1179 - EN ROUTE FROM PIT TO RSW, THE NR 2 ENGINE GENERATOR TRIPPED OFF LINE AND WOULD NOT RESET. CREW STARTED THE APU. THE APU OPERATED NORMALLY UNTIL FINAL APPROACH WHEN THE APU GENERATOR DROPPED OFF LINE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU PROPORTIONAL CONTROL VALVE. OPERATIONAL CHECK GOOD, OR THE NR 2 GENERATOR DROPPING OFF LINE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIREWALL CONNECTOR D3026 AND FEEDER HARNESS DUE TO BURNT CONTACTS. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001312005010700131EA 2005 1 7 QXEA200400836 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE EXPOSED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS BARE METAL EXPOSED AT FS 916.00. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001352005010700135NM 2005 1 7 QXEA200400797 120041113A5230 BEAM BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR SCORED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - AFT BAGGAGE DOOR STRUCTURAL BEAM FOUND SCORED BY HI-LITE STEM OF ROD ASSEMBLY. REPAIRED IAW MM TASK 52-31-11-000-801, PARAGRAPH 4(L) AND HORIZON AIR EA 6-52-355. 2H72 4T RTA13NM 20050107001442005010700144EA 2005 1 7 QXEA200400838 120041120A5312 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND LOWER BULKHEAD AT FS 280 FLOOR LEVEL HAS CORROSION AT SEVERAL AREAS ALONG 26 INCH AREA STARTING AT LEFT HAND SIDE OF COCKPIT DOORWAY. REPAIRED IAW CRJ SRM 51-42-06 AND REO 670-53-11-052. 2L72 4F RTA21EA 20050107001502005010700150NM 2005 1 7 QXEA200400806 120041116A5420 SUPPORT BEAM BOMBDRDHC8 DHC8401 1390041NM RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND ENGINE OUTBOARD PEC SUPPORT BEAM, FORWARD END, AFT SIDE OF HORSE COLLAR 90 DEGREE ANGLE IS CRACKED. REPAIRED IAW SRM SUBTASK 51-42-05-330-001, PAGE 206, PARAGRAPH E AND SUBTASK 51-40-800-801. 2H72 4T RTA13NM 20050107001592005010700159EA 2005 1 7 QXEA200400827 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND INBOARD SEAT TRACK HAS CORROSION AT THE FOLLOWING LOCATIONS, FS 505, FS 537, FS 549, FS 569, FS 600 AND FS 663. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001622005010700162NM 2005 1 7 QXEA200400862 120041203A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND EXTERIOR SKIN PANEL HAS TWO NICKS AT STATION X53.5, 2 INCH OUTBOARD OF STRINGER 32S. REPAIRED IAW HORIZON AIRE A 6-53-484 AND RD 8/4-53-1099. 2H72 4T RTA13NM 20050107001632005010700163NM 2005 1 7 QXEA200400856 120041129A5320 THRESHOLD BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - FORWARD PASSENGER DOOR THRESHOLD MEMBER IS CORRODED ON TOP SURFACE. REPAIRED IAW SRM SUBTASK 51-25-10-370-001. 2H72 4T RTA13NM 20050107001652005010700165NM 2005 1 7 QXEA200400860 120041203A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT HAND EXTERIOR SKIN PANEL HAS TWO NICKS AT STATION X23, OUTBOARD OF STRINGER 32X. REPAIRED IAW HORIZON AIR EA 6-53-483 AND RD 8/4-53-1096. 2H72 4T RTA13NM 20050107001662005010700166EA 2005 1 7 QXEA200400828 120041121A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09601QX 10009 PDX - LEFT HAND INBOARD SEAT TRACK HAS GOUGE AND CORROSION AT THE FOLLOWING LOCATIONS: FS 697, FS 729, FS 797, FS 830, FS 596 AND FS 893. REPAIRED IAW HORIZON AIR EA R-53-233 AND CRJ 700 SRM 51-21-16. 2L72 4F RTA21EA 20050107001742005010700174 2005 1 7 SWAA050001 420041230A2565D31354 SLIDE BOEING737 7372H4 138448CNM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29083SW 22732 L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F A16WE 20050107001922005010700192NM 2005 1 7 SWAA043724 120041228A53106546551 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29330SW 23694 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPT FRAME SHEAR TIE CORRODED AT BS 807, LBL 5 TO RBL 5. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050107001962005010700196NM 2005 1 7 SWAA043728 120041229A53106546550 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 9, WL 148. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20050107001992005010700199NM 2005 1 7 SWAA043731 120041229A53116516301 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188 LT SIDE, WL 192. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20050110000022005011000002SO 2005 1 10 SWIA200414210 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 BUTT STRAP AT Y479.00R FROM FRAME 30-34 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW SRM 51-40-02 AND SRM 51-25-00. 2L72 4T RTA31SO 20050110000062005011000006SO 2005 1 10 SWIA200414170 120041204A27523203001007 ACTUATOR EMB 120 EMB120ER 3260203SO T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07268UE9363 7933 120207 WHEN FLAPS ARE RETRACTED INTERMITTENT CONTROL FAULT. REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050110000082005011000008EA 2005 1 10 SWIA200414261 120041203A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07435SW 7555 AFT EQUIP COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16. 2L72 4F RTA21EA 20050110000232005011000023SO 2005 1 10 SWIA200414202 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 479.00 LEFT BUTT STRAP FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-25-00, 51-40-06, AND 51-40-02. 2L72 4T RTA31SO 20050110000242005011000024SO 2005 1 10 SWIA200414203 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 479.00 RIGHT BUTT STRAP FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-25-00, 51-40-06 & 51-40-02. 2L72 4T RTA31SO 20050110000302005011000030SO 2005 1 10 SWIA200414212 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 RIGHT BUTT STRAP AT Y479.00R FROM FRM 26 TO FRM 30 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) BLENDED & ASSESSED CORROSION IAW SRM 53-20-10, FOUND TO BE WITHIN LIMITS, DEPTH .004. REPROTECTED AREA IAW SRM 51-21-62 AND AMM 20-30-05. 2L72 4T RTA31SO 20050110000332005011000033EA 2005 1 10 SWIA200414233 120041202A27505913163 DETECTOR CNDAIRCL600 CL6002C10 1390015EA T/E FLAP MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07705SK1732 1732 10145 FLAP HALFSPEED MESSAGE. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD SKEW DETECTOR AS PER FIM 27-52-45. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000652005011000065 2005 1 10 YAX2004F00000 420040713A3417962830A1S8 ADC PIPER PA32 PA32301 7103207SO LYC O540 IO540K1G5 41532EA COCKPIT MALFUNCTIONED E YAXAO OTHER O OTHER NRNOT REPORTED 1 AL058200M162 328006048 ADC REPORTING TO IDU VARIED ALTITUDE OF +800 FEET. CROSSWIND COMPONENT ERRONEOUS AT TIMES. UNIT INSTALLED AS PART OF EFIS-SV SYSTEM. 1L71 3O3 O A3SO 1E4 20050110000672005011000067NE 2005 1 10 VIB2004F00001 220040326A7260 GEARBOX BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE LT ENGINE SEPARATED E VIBAA UNSCHED LANDING X ENGINE FLAMEOUT DEDESCENT 1 SO13825JG FA196 DURING DESCENT THE LT ENGINE SUFFERED A FLAME OUT. THE CREW DIVERTED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE DETERMINED THA THE ACCESSORY GEARBOX HAD BECOME DECOUPLED FROM THE COMPRESSOR. IAW MM, THE ENGINE IS BEING REMOVED AND SENT TO OVERHAUL FACILITY. 2L72 4T4 T A24CE E4EA 20050110000712005011000071NM 2005 1 10 USAA041032 120041124A575165C2591111A SKIN PANEL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT AILERON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU53047 23700 PIT - Q2 - TOP SKIN PANEL, 2 INCH SQ SINGLE LAYER, COMPOSITE DAMAGE, LT AILERON TOP SKIN PANEL AT TAB CONTROL ROD FAIRING MOUNT SURFACE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, RESTORES FINISH IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050110000902005011000090EU 2005 1 10 USAA040994 120041117A5320D5367095100100 STRUCTURE AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - PANEL BASE SECT. ASSY, L 1 INCH X W .50 INCH X D .020 INCH; CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y 1584. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM 53-11-14. 2L72 4F4 FRTA28NM E37NE 20050110000962005011000096EU 2005 1 10 USAA040989 120041116A5315D5347209001000 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 2.5 INCH X 2.0 INCH X .03 INCH DEEP; CORROSION; LEVEL 1; TASK NR JA-260-53500, LONGERON FLOORBEAM AT FR 66; Y1292 (LT). REMOVED AND REPLACED AT FR 66; Y 1292 (LT). REMOVED AND REPLACED BEAM ASSY IAW SRM 51-74-00, SRM 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110000972005011000097EU 2005 1 10 USAA040995 120041117A5320D53112785201 WEB AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - FLOOR WEB, 1 INCH X 2 INCH X .055 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-220-53500; STA Y 1584, FR 20. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001052005011000105EU 2005 1 10 USAA040999 120041111A5320D5348015900400 PLATE AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - PLATE ASSEMBLY; LONG 4 INCH EDGE, CORROSION/ DELAMINATION; FRAME 68Y=-1502. REMOVED AND REPLACED PART ASSY IAW SRM 51-42-11, 53-02-00. 2L72 4F4 FRTA28NM E37NE 20050110001062005011000106EU 2005 1 10 USAA040954 120041031A5320D53610188200 SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US 0861 BFM - S1- SEAL SUPPORT, .5 INCH X .5 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500-015, MAIN CABIN FLOORBOARD SEAL SUPPORT AT Y1584 BETWEEN 14 AND 16. REMOVED AND REPLACED FLOORBOARD SEAL SUPPORT IAW SRM 51-74-00, SRM 53-11-14, SRM 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110001332005011000133EU 2005 1 10 USAA041026 120041130A5320D5347218820400 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BTW FR 66 AND FR 68, BL Y1292. REPLACED BEAM IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001402005011000140NM 2005 1 10 USAA040977 120041117A575465C26601180 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - NR 6 SLAT SKIN, .1250 TO 4 INCH CRACKS- NUMEROUS; LOWER SURFACE AFT ROW RIVETS - NUMEROUS AREAS ENTIRE LENGTH. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2L72 4F4 FRTA16WE E21EU 20050110001602005011000160NM 2005 1 10 USAA040984 120041105A5312 BULKHEAD BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - WEB, 1 INCH CRACK, AT BS179, WL233.5, RBBL5.7 (178 BULKHEAD) WEB. INSTALLED DOUBLER IAW SRM 53-10-08, FIG 209 DETAIL II. 2L72 4F4 FRTA16WE E21EU 20050110001662005011000166NM 2005 1 10 USAA041056 120041123A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN SURFACE, SEVERAL AREAS OF 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. INSTALLED REPAIR PLYS IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001822005011000182EU 2005 1 10 SIMA200432907 120041122A2170QB0443 FILTER SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN DIRTY A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21376AE 340B376 AFTER TAKEOFF, CREW NOTICED A STRONG DETERGENT SMELL IN THE COCKPIT AND IN THE CABIN. SMELL FELT STRONGER IN THE COCKPIT. MAINTENANCE REPORTED A COMPRESSOR WASH HAD BEEN ACCOMPLISHED THE NIGHT BEFORE. MAINTENANCE REMOVED AND REPLACED THE CABIN AIR FILTERS. A GROUND RUN WAS COMPLIED WITH AND NO ORDERS DETECTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 20050110001832005011000183EU 2005 1 10 SIMA200433605 120041130A3350 LIGHT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN MALFUNCTIONED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21305AE 340B305 DURING PREFLIGHT CREW REPORTED THE AFT EMERGENCY PROXIMITY LIGHT WENT OUT AFTER 10 SECONDS. COULD NOT DUPLICATE DISCREPANCY. PERFORMED EMERGENCY LIGHTS SYSTEM OPERATIONAL TEST IAW MM. NO DEFECTS NOTED AT THIS TIME. (SW21200501343) 2L72 4T4 TRTA52EU E8NE 20050111000392005011100039EU 2005 1 11 AWXA200500011 120041110A5314D53371827209 ATTACH ANGLE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28619AW 527 MCN - MAJOR REPAIR - DURING C-08 CHECK A 1 INCH CRACK WAS FOUND IN KEEL BEAM RT ATTACH ANGLE, AFT OF MAIN LANDING GEAR DOOR BETWEEN FR 46 AND FR 47, STR 43 RT. MAINTENANCE REMOVED DAMAGED KEEL BEAM RT ATTACH ANGLE; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER ER 26-5335-04355-SS1 PER ER 26-5335-04355-SS1A ITEM IS TO BE INSPECTED EVERY 3500 FLIGHT CYCLES OR EVERY C-CHECK NOT TO EXCEED 15 MONTHS OR UNTIL PART HAS BEEN REPLACED WITH ORIGINAL MATERIAL, OR MATERIAL CALLED FOR IN A320 SRM 53-35-11 FIG 229. 2L72 4F RTA28NM 20050111000502005011100050NM 2005 1 11 CALA0400752 120041229A53136946579619 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714358 23943 INSPECTION FOUND RT APU TORQUE BOX CORRODED ON TOP STRINGER 14R AT AIR INLET CUTOUT, STA 1121-1156. THE UPPER APU TORQUE BOX STRINGER WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050111000512005011100051NM 2005 1 11 CALA0400753 120041230A5320143A948535 FLOOR SUPPORT BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2724202 30429 INSPECTION FOUND CENTER FLOOR SUPPORT BEAM CORRODED AT STA 500I, LBL 30 TO RBL 30. SUPPORT IS LOCATED DIRECTLY BELOW BULKHEAD PANEL AT STA 500I, FORWARD BAGGAGE BIN. THE CENTER FLOOR SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20050111000612005011100061EA 2005 1 11 COMA0570004 120041228A2780766359B PDU CNDAIRCL600 CL6002C10 1390015EA L/E SLAT FAILED A COMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 SO01398CA3932 10112 FLIGHT 9495 SLAT FAIL MESSAGE. REPLACED THE POWER DRIVE UNIT. 2L72 4F RTA21EA 20050111000652005011100065EA 2005 1 11 COMA0570005 120041224A2781895304 PSEU CNDAIRCL600 CL6002C10 1390015EA E/E BAY MALFUNCTIONED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01398CA3931 10112 FLIGHT 5071 SLAT FAIL CAUTION. REPLACED THE PSEU. 2L72 4F RTA21EA 20050111000702005011100070EA 2005 1 11 COMA0560018 120041231A3150 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01716CA 7250 FLIGHT 5715 DISPLAY COOL MESSAGE. COULD NOT DUPLICATE. INSPECTED SYSTEM, FOUND NO DEFECTS. 2L72 4F RTA21EA 20050111000722005011100072EA 2005 1 11 COMA0560014 120041230A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 LEFT HAND INTERCOSTAL AT FS 484 CRACKED. REPAIRED IAW REO 601R-53-059. 2L72 4F RTA21EA 20050111000742005011100074EA 2005 1 11 COMA0560013 120041230A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 FS 280 AFT ANGLE IS CORRODED UPPER SURFACE UNDER FLOORBOARD 213 ALF. REPAIRED IAW REO 601R-53-11-136. 2L72 4F RTA21EA 20050111000772005011100077EA 2005 1 11 COMA0560010 120041227A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA LT & RT ACM DIRTY A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01937CA 7044 FLIGHT 5244, SMOKE IN COCKPIT AND CABIN AFTER T/O. REPLACED THE LT AND RT ACM COALESCERS. 2L72 4F RTA21EA 20050111000782005011100078EA 2005 1 11 COMA0560011 120041225A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01507CA 7796 FLAPS FAIL CAUTION. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM PER AD 98-20-01, NO DEFECTS FOUND. 2L72 4F RTA21EA 20050111000812005011100081EA 2005 1 11 COMA0560005 120041223A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA 7326 LOWER LEFT HAND WING PLANK CRACK INBOARD OF WS 149.85. REPAIRED IAW REO 601R-57-21-539. 2L72 4F RTA21EA 20050111000842005011100084EA 2005 1 11 COMA0560003 120041222A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA 7326 RIGHT HAND 718 FRAME CRACKED. REPAIRED IAW EO 53-027. 2L72 4F RTA21EA 20050111000862005011100086EA 2005 1 11 COMA0560006 120041223A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA 7326 LOWER NOSE SKIN DAMAGED FORWARD OF FS 280 BETWEEN STRINGERS 25R AND 26R. REPAIRED IAW EA 10-5310-00515. 2L72 4F RTA21EA 20050111000882005011100088NM 2005 1 11 DLM88041150 120041228A5330593666751 SKIN DOUG MD88 MD88 3023688NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27910DE 53419 THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 1271 & 1287 AND BETWEEN LONGERONS 26R & 30. THE DENT DAMAGE WAS REMOVED WITH A 25 X 18.5 INCHES CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 095859-14. 2L72 4F RTA6WE 20050111000892005011100089NM 2005 1 11 DL777041151 120041229A3350528740294 BATTERY BOEING777 777232 1385232NM CABIN UNSERVICEABLE A DALAK NONE O OTHER ININSP/MAINT 1 SO27861DA 29952 EMPASS BATTERY ARM SWITCH FAULTY. REMOVED AND REPLACED EMPASS BATTERY WITH SERVICEABLE. OPS CHECK OK. 2L72 4F RTT00001SE 20050111000912005011100091NM 2005 1 11 DL76G041154 120041230A3350 FUSE BOEING767 767332 1382001NM POWER SUPPLY BLOWN A DALAK NONE L NO TEST ININSP/MAINT 1 SO271607B 49245 30388 DURING SVC FOUND SEATS 1AB TO 3AB AND L1 CLOSET E-PATH LIGHTS INOP. REPLACED FUSE ON M730 AND REPLACED M736 AND BATTERY PACK OPS OK. 2L72 4F RTA1NM 20050111000932005011100093NM 2005 1 11 DLM88041156 120041231A323139567851 LINK DOUG MD88 MD88 3023688NM NLG DOOR DEFECTIVE A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27905DL 49536 AFTER GEAR RETRACTION LOUD NOISE AND VIBRATION IN COCKPIT. REPLACED RIGHT NOSE GEAR DOOR LINK. 2L72 4F RTA6WE 20050111001082005011100108EA 2005 1 11 SWIA200414350 120041120A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 AFT OF FRAME 280 LEFT SIDE 2 ANGLE CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ 200 SRM 51-42-06, FIG 8, 51-42-21. 2L72 4F RTA21EA 20050111001092005011100109EA 2005 1 11 SWIA200414351 120041120A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 CRACKED SUPPORT ANGLE AT FS 625 NEAR STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ SRM 200 51-42-06 PG 11 & 51-77-00 PG 1. 2L72 4F RTA21EA 20050111001122005011100112 2005 1 11 SWIA200414335 420041227A22166225734002 SERVO EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM07291SW 120318 ON FINAL APPROACH RUDDER REQUIRED INCREASED PRESSURE TO OPERATE. REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001182005011100118EA 2005 1 11 SWIA200414329 120041229A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT DEFECTIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07433SW 7550 RUDDER TRIM WON’T GO NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001222005011100122EA 2005 1 11 SWIA200414333 120041230A2721 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07413SW 7102 RUDDER TRIM FFOD TEST. REMOVED AND REPLACED RUDDER TRIM PANEL IAW CRJ MM 27-12-6, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001242005011100124EA 2005 1 11 SWIA200414307 120041213A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07460SW 7803 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED; FS 280.00, LBL 9.0 OUTBOARD CLIP. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, AND 51-21-11. 2L72 4F RTA21EA 20050111001262005011100126EA 2005 1 11 SWIA200414309 120041226A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07928SW 7701 THE SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS NOT WORKING. RELAMPED LIGHT BULB FOR CEILING FLOOD LIGHT IAW 33-51-00 CRJ AMM. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001392005011100139EA 2005 1 11 A6WA200440205 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 RT FS 625.00 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-12 IAW CRJ SRM 51-42-06. (M) 2L72 4F4 FRTA21EA E15NE 20050111001492005011100149NM 2005 1 11 ASA0440231 120041109A5311BAC15171470 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 FRAME CRACKED BELOW STRINGER FOR BIN RAIL. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050111001532005011100153NM 2005 1 11 ASAA0410530 120041112A53506545775 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FAIRING DAMAGED A K NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, AT WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001552005011100155NM 2005 1 11 ASAA0410517 120041110A53506545771 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FAIRING DAMAGED A K NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001702005011100170NM 2005 1 11 ASAA0410518 120041110A53506545771 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001712005011100171NM 2005 1 11 ASAA0410531 120041112A533065458001138 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING VISUAL INSPECTION OF LAP JOINT AT STRINGER 24L IAW ER 04-3622, SEC 1 FOUND ADDITIONAL SCRIBE MARKS FROM BS 259-360. 2L72 4F4 FRTA16WE E2EA 20050111001732005011100173NM 2005 1 11 ASAA0410516 120041110A53506545771 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001752005011100175NM 2005 1 11 ASAA0410528 120041112A53306545774 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT AFT WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001772005011100177NM 2005 1 11 ASAA0410576 120041122A5320654656847 SUPPORT ANGLE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SUPPORT ANGLE CRACKED. REMOVED, FABRICATED NEW ANGLE AND INSTALLED. 2L72 4F4 FRTA16WE E2EA 20050111001792005011100179NM 2005 1 11 ASAA0410573 120041122A5313BAC1493522 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON STRINGER. REPLACED STRINGER. 2L72 4F4 FRTA16WE E2EA 20050111001812005011100181NM 2005 1 11 ASAA0410494 120041109A52306545775558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE AFT CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARK IN EXTERNAL SKIN AT AFT CARGO DOOR UPPER AFT CORNER. REPAIRED AFT CARGO DOOR IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001832005011100183NM 2005 1 11 ASA0440232 120041109A5311BAC15171470 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 FRAME CRACKED BELOW STRINGER FOR BIN RAIL. REMOVED CRACK IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050111001852005011100185NM 2005 1 11 ASA0440196 120041029A5310654796039 DOOR FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 AFT CARGO DOOR CUT OUT, AFT FRAME WEB BENT. ACCOMPLISHED REPAIR IAW EA ON AFT FRAME. 2L72 4F4 FRTA16WE E21EU 20050107000952005010700095NM 2005 1 7 USAA040926 120041102A5311 FRAME BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - FRAME, .1250 INCH CRACK, BS787 AT S9L-S8L. CUT OUT DAMAGE AND INSTALLED NESTED REPAIR ANGLES IAW TYP REP 53-10-02A. 2L72 4F4 FRTA16WE E21EU 20050107001012005010700101NM 2005 1 7 SB04142 120041010A33501619 LIGHT BOEING737 7373B7 1384580NM EXTERIOR LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19392US 23314 CLT - MAINTENANCE REPORTED THE EXTERIOR EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. MAINTENANCE FOUND THE BULB LOOSE IN SOCKET. SECURED BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001042005010700104NM 2005 1 7 SB04140 120041007A335020131A BATTERY PACK BOEING737 7374B7 1384702NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19434US 24556 PIT - MAINTENANCE REPORTED THE FLOOR PATH EMERGENCY LIGHTING AT SEAT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001052005010700105NM 2005 1 7 SB04128 120040920A33501012721 SOCKET BOEING737 737301 1384611NM CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19352US 23555 BDL - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EVACUATION LIGHT, AT SEAT ROW 18ABC, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT/SOCKET ASSEMBLY AND RELAMPED THE BULB. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001062005010700106NM 2005 1 7 USAA040927 120041029A53201123371 CLIP BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - ATTACH CLIP, BROKEN, FRAME 706, STR S1. REMOVED BROKEN TIE CLIP AND REPLACED WITH SAME IAW SRM 51-40-02 AND 51-40-03. 2L72 4F4 FRTA16WE E21EU 20050107001192005010700119NM 2005 1 7 SB04137 120041002A2781189929 PROXIMITY SENSOR BOEING737 7373B7 1384580NM L/E FLAP FAULTY A USAAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 EA19385US 22958 EWR - FLT 2164 - ON DESCENT INTO LGA FROM DCA, CREW RECEIVED A NR 4 LEADING EDGE KRUGER FLAP AMBER LIGHT ALONG WITH A LEADING EDGE TRANSIT AMBER LIGHT DURING SLAT EXTENSION. CREW RECYCLED FLAPS IN HOPES OF CLEARING THE PROBLEM WITH NO HELP. CREW DECIDED TO DIVERT FLIGHT TO EWR DUE TO THE LONGER RUNWAYS. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED, REPLACED AND RIGGED THE NR 4 LEADING EDGE KRUGER FLAP UP PROXIMITY SENSOR IN ASSOCIATION WITH MM 27-88-11. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050107001212005010700121EU 2005 1 7 EM04020 120041027A32608001901 PROXIMITY SENSOR EMB ERJ170ERJ170100 EU NLG DEFECTIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19808MD 17000021 FLIGHT 1639, IAH TO PHL - THE CAPTAIN RETURNED TO IAH DUE TO LANDING GEAR HANDLE WOULD NOT RAISE AND THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE TROUBLESHOT PROBLEM TO THE NOSE LANDING GEAR WEIGHT ON WHEELS SENSOR NUMBER ONE. REMOVED AND REPLACED SENSOR AND PERFORMED GEAR SWING OPERATIONAL CHECK. 2L74 4F RTA56NM 20050107001242005010700124NM 2005 1 7 QXEA200400807 120041123A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - NR 4 SEAT TRACK OUTBOARD FLANGE HAS CORROSION ON TOP SURFACE FROM X201 TO X228. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20050107001252005010700125NM 2005 1 7 QXEA200400808 120041120A5531 FRAME DHAV DHC8 DHC8102 2809003NM VERTICAL STAB CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH 512 PDX - VERTICAL STABILIZER FRAME 4 IS CRACKED AT STRINGER RT 4 IN AFT FUSELAGE SECTION. REPAIRED IAW RD 8-55-199. 2H72 4T RTA13NM 20050107001342005010700134NM 2005 1 7 QXEA200400795 120041112A5420 INTERCOSTAL BOMBDRDHC8 DHC8401 1390041NM RT NACELLE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND NACELLE OUTBOARD SIDE, ZONE 623, INTERCOSTAL ATTACHING TO UPPER SKIN IS CRACKED AT STATION XN 210.0. REPAIRED IAW SRM 51-40-15, PAGE 201 AND Q400 SRM 51-25-05-370-801. 2H72 4T RTA13NM 20050107001462005010700146NM 2005 1 7 QXEA200400801 120041116A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND INBOARD SEAT RAIL AT STATION X11 TO X70 HAS PITTING CORROSION ON INSIDE AND TOP SURFACE. REPAIRED IAW SRM SUBTASK 51-42-05-330-001, PARAGRAPH E AND 51-40-15-400-00, PARAGRPHA G-I. 2H72 4T RTA13NM 20050107001492005010700149NM 2005 1 7 QXEA200400804 120041116A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09406QX 4048 PDX - RIGHT HAND INBOARD SEAT RAIL AT STATION X664 HAS DEEP PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW RD 8/4-53-1059 AND HORIZON AIR EA 6-53-463. 2H72 4T RTA13NM 20050107001612005010700161NM 2005 1 7 QXEA200400861 120041203A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 YYC - RIGHT EXTERIOR SKIN PANEL HAS ONE NICK AT STATION 23, 1.5 INCH INBOARD OF STRINGER 32X. REPAIRED IAW RD 8/4-53-1096 AND CRJ SRM 51-14-00-800-801. 2H72 4T RTA13NM 20050107001702005010700170NM 2005 1 7 SWAA050002 120041231A2560PH22300L GLOWSTRIP BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29333SW 23697 EMERGENCY EXIT PHOTOLUMINESCENT STRIP AT ROW 8 ABC, LOOSE. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM. 2L72 4F RTA16WE 20050107001812005010700181NM 2005 1 7 SWAA050003 120041231A3350101073 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29711HK 27845 FWD GALLEY SERVICE DOOR LOWER EMERGENCY EXIT LIGHT COVER, LOOSE. REINSTALLED COVER PER MM. 2L72 4F RTA16WE 20050107001892005010700189NM 2005 1 7 SWAA043734 120041229A3350PH22300L STRIP BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29707SA 27841 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIPS WORN AT ROWS 1 DEF & 3 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM. 2L72 4F RTA16WE 20050107001902005010700190NM 2005 1 7 SWAA050006 120041231A57536546435282 STRUCTURE BOEING737 7373H4 1384600NM T/E FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C4 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20050107002182005010700218EA 2005 1 7 SWIA200414255 120041204A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA CABIN PULLED A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07983SW 7961 FIRST OVERHEAD EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE #LY3D22 PULLED FROM TB1101A. REINSERTED PIN IAW WM 33-51-00. OPERATIONAL CHECK GOOD IAW MM 33-51-00. 2L72 4F RTA21EA 20050107002192005010700219EA 2005 1 7 SWIA200414188 120041118A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14L, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2L72 4F RTA21EA 20050112000292005011200029EU 2005 1 12 MALA040913 120041223A3260 SQUAT SWITCH BAC 146 AVRO146RJ85A1500097EU MLG FROZEN A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15530XJ E2364 DURING TAKEOFF, LANDING GEAR WOULD NOT RETRACT. ALONG WITH AUTO THROTTLE FAILING TO ENGAGE AND MANUAL SPOILER FAULT. AIR RETURN TO DTW. MAINTENANCE CLEANED SNOW AND ICE FROM MLG SQUAT SWITCHES. PERFORMED SEVERAL NORMAL GEAR SWINGS, ALL CHECKS GOOD OF ALL ASSOCIATED SYSTEMS. 2H74 4F RTA49EU 20050112000302005011200030GL 2005 1 12 C2XA04RI018 220041219A7200 ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW271417477 14500876 CAE312707 DURING FLIGHT AFTER ENGINE BLEEDS WERE SELECTED THE LAV SMOKE ALARM CAME ON ALONG WITH THE LAV SMOKE INDICATION ON THE EICAS. REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRT TE6CH 20050112000312005011200031SO 2005 1 12 MASA200400647 120041121A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07837MJ 145367 ASH FLT 2875 CAE-CLT. ABORTED TAKEOFF DUE TO THE E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 11/23/04 MAINTENANCE RESET SYSTEM AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050112000322005011200032SO 2005 1 12 MASA200400654 120041126A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07837MJ 145367 ASH 2812 CAE-CLT ABORTED TAKEOFF DUE TO THE E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES AND RETURNED THE AIRCRAFT TO SERVICE. 11/30 MAINTENANCE CLEANED THE LOCK PIN AND SYSTEM OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050112000332005011200033SO 2005 1 12 MASA200400675 120041202A2731 CONTROLLER EMB 145 EMB145LR 3260212SO PITCH TRIM MALFUNCTIONED A MASAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW07838MJ 145384 ASH 2861 CLT. AIRCRAFT RETURNED TO THE FIELD. MX REPORTED THE CREW REPORTED A MAIN PITCH TRIM AND BACKUP PITCH TRIM FAIL OCCURRED AND WOULD NOT RESET. MAINTENANCE PERFORMED AN ELECTRICAL TEST OF THE HORIZONTAL STABILIZER CONTROLLER AND OPS CHECKED THE TRIM SYSTEM. ALL OPS CHECKS WERE GOOD. 2L72 4T RTT00011AT 20050112000342005011200034SO 2005 1 12 MASA200400676 120041203A4990 OIL CAP EMB 145 EMB145LR 3260212SO APU LOOSE A MASAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW07828MJ 145218 ASH 2610 FROM CLT TO CLE RETURNED TO THE FIELD DUE TO A LAV SMOKE WARNING MSG AND VISIBLE SMOKE IN THE FLIGHT DECK. MAINTENANCE PLACED THE APU BLEED SYSTEM ON MEL AND THE A/C DEPARTED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE APU OIL CAP OFF, SECURED CAP AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050112000352005011200035SO 2005 1 12 MASA200400692 120041211A4920 APU EMB 145 EMB145LR 3260212SO APU BAY SEIZED A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07832MJ 145310 ASH FLT 2784 CLT - GSO RETURNED TO THE FIELD DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND THE APU SIEZED. RAN THE ENGINES TO CLEAR THE CABIN. MX DEFERRED THE APU. 12/15 MAINTENANCE INSPECTED AND FOUND THE APU NOT SIEZED AND WAS FOUND TO BE GYLCOL. 2L72 4T RTT00011AT 20050112000362005011200036SO 2005 1 12 MASA200400695 120041213A532014522178005 CHANNEL EMB 145 EMB145LR 3260212SO DOOR THRESHOLD CORRODED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07845MJ 145502 SERVICE DOOR THRESHOLD SUPPORT STRUCTURE, IS BEING REPLACED DUE TO HEAVY CORROSION. REF EAMS WORK ORDER 211203 TASK 1514. 2L72 4T RTT00011AT 20050112000372005011200037SO 2005 1 12 MASA200400706 120041219A21408152892 SENSOR EMB 145 EMB145LR 3260212SO NR 2 PACK HEAT INOPERATIVE A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07836MJ 145359 ASH 2693 FROM CLT TO LIT THE CREW WROTE UP THE NR 2 PACK HEAT WAS UNCONTROLLABLE AND PRODUCED A SMOKE SMELL IN THE A/C. MAINTENANCE FOUND THE CONDENSER/MIXER CRACKED CAUSING HEAT FROM THE BLEED AIR SYSTEM TO MELT THE GROUND AIR T-DUCT AND A HEAT SENSOR. 12/19 MAINTENANCE REPLACED GROUND AIR T-DUCT AND TEMP SENSOR. DUCT P/N 145-22277-403 AND 145-22285-401. 2L72 4T RTT00011AT 20050112000382005011200038SO 2005 1 12 MASA200400707 120041219A2820 WARNING LIGHT EMB 145 EMB145LR 3260212SO FUEL SYSTEM ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07860MJ 145773 ASH 2827 FROM ROC TO CLT ABORTED TAKEOFF DUE TO A FUEL IMBALANCE CAUTION MESSAGE. CONTRACT MAINTENANCE TRANSFERRED FUEL AND OPS CHECKED THE FUEL TRANSFER SYSTEM OPS GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050112000392005011200039SO 2005 1 12 MASA200400712 120041220A4900 ODOR EMB 145 EMB145LR 3260212SO APU DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07827MJ 145217 ASH 2801 STL TO CLT. APU OIL SMELL IN BLEED AIR. MAINTENANCE COMPLIED WITH MEL PROCEDURES FOR APU AIR. 12/22 MAINTENANCE CLEANED APU. 2L72 4T RTT00011AT 20050112000432005011200043EU 2005 1 12 MALA040926 120041209A5320 INTERCOSTAL SAAB SF340 340B 7860101EU FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4K INSPECTION IN BNA, INTERCOSTAL LOCATED AT RBL 18.0 IS GOUGED BETWEEN FS 272 AND FS 288. THE INBOARD FLANGE IS OUT OF LIMITS AND WILL BE REMOVED AND REPLACED FOLLOWING APPLICABLE SRM PROCEDURES. REFER EAMS WORK ORDER 211207 TASK 1529. AIRCRAFT RETURN TO SERVICE 12/17/04. 2L72 4T RTA52EU 20050112000442005011200044EU 2005 1 12 MALA040922 120041208A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4K INSPECTION IN BNA, RT FUSELAGE IS DENTED JUST AFT OF FS 339, BETWEEN SL 1617 & 1620. DAMAGE WILL BE REPAIRED IAW MESABA EO S53005, REFER TO EAMS WO 211207, TASK 2523. AIRCRAFT RETURNED TO SERVICE 12/17/04. 2L72 4T RTA52EU 20050112000452005011200045EU 2005 1 12 MALA040924 120041209A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4K INSPECTION IN BNA, CENTER AISLE SEAT TRACK FLANGE AT BL 0 IS CORRODED. DAMAGE WILL BE REPAIRED IAW MESABA EO S53060. REFER TO EAMS WO 211207, TASK 1524. AIRCRAFT RETURNED TO SERVICE 12/17/04. 2L72 4T RTA52EU 20050112000462005011200046EU 2005 1 12 MALA040923 120041208A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4K INSPECTION IN BNA, LT FUSELAGE IS DENTED BETWEEN FS 339 & FS 363, AND BETWEEN SL 1516, & 1519 OUT OF LIMITS. AREAS WILL BE REPAIRED IAW MESABA EO S53009, REFER TO EAMS WO 211207, TASK 2502. AIRCRAFT RETURNED TO SERVICE 12/17/04. 2L72 4T RTA52EU 20050112000472005011200047EU 2005 1 12 MALA040925 120041209A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 BETWEEN FS 483 AND FS 630 IS CORRODED ON O/B FLOOR PANEL FLANGE. DAMAGE WILL BE REPAIRED IAW MESABA EO S53078, REFER EAMS WORK ORDER 211207, TASK 1538 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURN TO SERVICE 12/17/04. 2L72 4T RTA52EU 20050112000482005011200048EU 2005 1 12 MALA040927 120041209A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15413XJ 340B413 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 INBOARD FLANGE IS CORRODED BETWEEN FS 319 AND 339. DAMAGE WILL BE REPAIRED IAW MESABA EO S53060. REFER EAMS WORK ORDER 211207 TASK 1533. AIRCRAFT RETURN TO SERVICE 12/17/04. 2L72 4T RTA52EU 20050112000522005011200052WP 2005 1 12 05FDEA00014 120040610A5712ARB70601 RIB DOUG MD10 MD1010F 3022112WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25565FE 46996 WING - LT WING RIB XORS 372 UPPER CAP CRACKED. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-78165. 2L73 4F RTA22WE 20050112000552005011200055SO 2005 1 12 C2XA04IA117 120040905A33502013BR BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711165614 614 14500819 MCI - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AND THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK WAS WEAK. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050112000572005011200057WP 2005 1 12 05FDEA00010 120040221A5512 SKIN PANEL DOUG MD10 MD1010F 3022112WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568050 47804 HORIZONTAL STABILIZER - CONSTANT SECTION, UPPER AND LOWER SKIN CRACKS WITHIN FLYABLE LIMITS. PANELS REPLACEMENT PER SB 55-16 IAW FEDEX EA 8-5510-73237. 2L73 4F RTA22WE 20050112000582005011200058NM 2005 1 12 05FDEA00015 120041231A2780 WARNING LIGHT BOEING727 727200 138407ENM COCKPIT ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25488FE 21491 AFTER DEPARTURE MEM NR 4 SLAT INDICATED EXTENDED WITH FLAPS SELECTED TO 2 DEGREES. AMBER L/E FLAPS LIGHT ILLUMINATED ON FOWARD PANEL. GREEN NR 4 SLAT ANNUNCIATOR LIGHT ILLUMINATED DN F/E AUX PANEL. COMPLIED WITH CHECKLIST PROBLEM. RETURNED FOR LANDING. CYCLED LEADING EDGE SLAT & OVERIDE SWITCHES S1010 & S1011, CYCLED SLATS SEVERAL TIMES NR 4 SLAT AMBER & GREEN LIGHTS OPS CHECK SATISFACTORY ON FWD & AFT PANELS. A/C OK FOR SERVICE. ALSO VISUAL CHECK OF SLATS OPS CHECK NORMAL. 2L73 4F RTA3WE 20050112000592005011200059NM 2005 1 12 05FDEA00016 120041231A2780 WARNING LIGHT BOEING727 727200 138407ENM SLATS ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25488FE 21491 AFTER DEPARTURE MEM NR 4 SLAT INDICATED EXTENDED WITH FLAPS SELECTED TO 2 DEGREES. AMBER L/E FLAPS LIGHT ILLUMINATED ON FORWARD PANEL. GREEN NR 4 SLAT ANNUNCIATOR LIGHT ILLUMINATED DN F/E AUX PANEL. COMPLIED WITH CHECKLIST PROBLEM. RETURNED FOR LANDING. CYCLED LEADING EDGE SLAT & OVERIDE SWITCHES S1010 & S1011, CYCLED SLATS SEVERAL TIMES NR 4 SLAT AMBER & GREEN LIGHTS OPS CHECK SATISFACTORY ON FWD & AFT PANELS. A/C OK FOR SERVICE. ALSO VISUAL CHECK OF SLATS OPS CHECK NORMAL. 2L73 4F RTA3WE 20050112000602005011200060EU 2005 1 12 MALA040920 120041230A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 DURING 4K INSPECTION IN BNA, LT FUSELAGE HAS OUT OF LIMITS DENTS BETWEEN FS 350 AND FS 363, AND BETWEEN SL 1515 TO SL 1517. DAMAGE WILL BE REPAIRED IAW MESABA EO S53009. REFER TO EAMS WORK ORDER 211273, TASK 2504 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1/7/05. 2L72 4T RTA52EU 20050112000622005011200062WP 2005 1 12 05FDEA00011 120040426A5712ARB70601 RIB DOUG MD10 MD1010F 3022112WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568050 47804 WINGS - LT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-571-75732. 2L73 4F RTA22WE 20050112000642005011200064WP 2005 1 12 05FDEA00013 120040512A5320AFA32451 SILL DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25565FE 46996 FUSELAGE - RT CENTRAL CARGO DOOR SILL RAIL CORROSION AT STA 1681, LONGERON 43. CORROSION REMOVAL AND REPAIR ANGLE INSTALLATION IAW FEDEX EA 8-5315-75701. 2L73 4F RTA22WE 20050112000652005011200065WP 2005 1 12 UPS04843620 120041224A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP EMERGENCY LIGHTSINOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 NO EMERGENCY EVAC LIGHTS DURING BISE CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-01-2, OPS CHECK GOOD. 2L74 4F RT4A25 20050113000012005011300001EA 2005 1 13 UIA9317 120041008A75001611301 TUBE DHAV DHC8 DHC8311 1386006EA LYC O540 O540* 41532EA APU BLEED AIR DEFORMED Z A UNSCHED LANDING O OTHER CLCLIMB 1 TW001521919019 381 NO.2 BLEED HOT CAUTION LIGHT ON (IN FLIGHT),AFTER LANDING IAW AMM21-11-00 AND AMM 49-10-00 CHECK FOUND ENG BLEED HEATSHIELD DEFORM.REPLACED HEATSHIELD PIPE AND ENG RUN-UP CHECK CONDCTION BACK NORMAL. 2H72 4T3 ORTA13NM E295 20050113000022005011300002NE 2005 1 13 BDCA2104 220041015A7200 ENGINE BOEING767 767300 1385204NM GE CF6 CF680C2B7 NE NR 1 VIBRATION H EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW99VPBAZ 30111 704956 NR 1 ENGINE INFLIGHT SHUT DOWN DUE TO VIBRATION. 2L72 4F4 FRTA1NM E13NE 20050113000062005011300006NM 2005 1 13 UPS04M43407 120041026A3411 PITOT TUBE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE COCKPIT PLUGGED A IPXAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 SO01253UP 48439 ON T/O AIRSPEED WENT BLANK. F/O SIDE APPEARED NORMAL. THIS WAS ACCOMPANIED BY SEL FLAP LIM OVRD AND SEL ELEV FEEL MAN. NUMEROUS OTHER LIGHTS WERE ILLUMINATED. ACCOMPLISHED CHECKLIST. CAPT'S PITOT PROBE CLOGGED WITH DEBRIS. REMOVED AND REPLACED CAPTS PITOT TUBE DUE TO OBSTRUCTION. REF MM 34-11-01. LEAK CKS GOOD. PITOT/STATIC SYSTEM CKD BOTH CAPTS AND FO'S USING RESPECTIVE CADC SYS. NO LESS OR SPLIT OF AIRSPEED NOTED. 2L73 4F4 FRTA22WE E31N3 20050113000422005011300042NM 2005 1 13 QXEA200400930 120041229A5100 STRUCTURE DHAV DHC8 DHC8202 2809007NM CONTAMINATED A QXEAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM09345PH 476 TAKE-OFF WAS ABORTED WHEN THE AIRCRAFT FAILED TO ROTATE AT VR. THE TAKE-OFF WAS ABORTED AT 102KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND CLEANED RESIDUAL TYPE IV DEICE FLUID FROM AIRCRAFT. THE AIRSPEED INDICATORS AND THE ELEVATOR CONTROL SYSTEM SYSTEM WERE CHECKED FOR PROPER OPERATION. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050113000482005011300048NM 2005 1 13 DXTA200400497 120041226A3220D233320004 LEG ASSY AMD FALC50FALCON2000 2730170NM NLG VIBRATION E DXTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL07290QS1922 190 NOSE GEAR SCISSORS NOT PINNED PRIOR TO TAKE OFF, NLG WOULD NOT RETRACT INTO WHEEL-WELL, SEVERE VIBRATION FROM NOSE WHEEL WAS NOTED ON TOUCHDOWN. REMOVED NOSE LANDING GEAR LEG ASSY PN- D23332000-4 SN- B147. INSTALLED AN OVERHAULED NOSE GEAR LEG ASSY PN D233320004, SN B2. WORK DONE PER THE FOLLOWING F2000 WORK PROCEDURES : 32-203, 32-213, 32-201, 32-214, 32-401, 32-200, 32-300, AND 32-501. 2K73 4F RTA50NM 20050113000492005011300049NM 2005 1 13 2004UALA01173 120041202A2613355574255 OVERHEAT LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29308UA 23669 DIVERTED TO SLC DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY . 2L72 4F4 FRTA16WE E2GL 20050113000502005011300050CE 2005 1 13 DXTA200400489 120041221A3230 MODULE CESSNA560 560XL 2076702CE MLG LOGIC CONTROFAILED E DXTAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL07635QS 5605358 RIGHT GEAR LIGHT CAME ON DURING FLIGHT (GEAR HANDLE UP) FOLLOWED BY LOW BRAKE PRESS & ANTI SKID INOP CAUTION LIGHT ON. AFTER 20 MIN ALL 3 LIGHTS EXTINGUISHED, DURING DESCENT (10,000 FT) OPERATION OF GEAR AND BRAKES DURING LANDING WAS NORMAL. REPLACED LANDING GEAR CONTROL LOGIC MODULE IAW 560XL 24-51-02 OPS CHECK GOOD 2L72 4F RTA22CE 20050113000512005011300051CE 2005 1 13 DXTA200400490 120041222A2750 CONTROL CABLE CESSNA750 750 2076810CE TE FLAPS OUT OF RIG E DXTAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL07900QS 7500123 FLAPS FAIL EICAS MESSAGE SLATS DEPLOYED, BUT NO FLAPS. COULD NOT DUPLICATE SQK. C/W MECHANICAL RIG AND ELECTRICAL RIG IAW 750 M/M 27-50-00. FOUND LT INBD FLAP BINDING, RE-RIGGED FLAPS AND OPS CHECKED GOOD. 2L72 4J RTT00007WI 20050113000522005011300052CE 2005 1 13 DXTA200400491 120041222A275099146153 PDU CESSNA750 750 2076810CE TE FLAPS MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07918QS 7500223 FLAPS FAILED WHILE APPROACHING DESTINATION, TRIED TO RESET WITH NO CHANGE. LANDED WITH SLATS EXTENDED AND NO FLAPS. REMOVED & REPLACED FLAP MOTOR (PDU) IAW: CE750 M/M 27-52-00. RIGGED FLAP SYSTEM IAW: CE750 M/M 27-50-00. FLAP SYSTEM OPERATIONALY CHECK'S GOOD. 2L72 4J RTT00007WI 20050113000532005011300053CE 2005 1 13 DXTA200400492 120041223A561099143794 WINDOW CESSNA750 750 2076810CE COCKPIT FAILED E DXTAB EMER. DESCENT D INFLIGHT SEPARATION CLCLIMB 1 GL07926QS6681 7500026 WHILE CLIMBING THRU FL300 THE OUTER PORTION OF COPILOTS SIDE COCKPIT WINDOW COMPLETELY SHATTERED. INNER PLASTIC PANEL REMAINED INTACT. REPLACED CO-PILOT'S SIDE, ELEC. HEATED COCKPIT WINDOW WITH A NEW WINDOW PER CE 750 MM 56-12-00. OPS CHECK GOOD. NO LEAKS NOTED DURING PRESSURIZATION CHECKS. 2L72 4J RTT00007WI 20050113000542005011300054CE 2005 1 13 DXTA200400487 120041221A1420 CONNECTOR CESSNA560 560XL 2076702CE MLG DIRTY E DXTAO OTHER J WARNING INDICATION APAPPROACH 1 GL07652QS 5605152 WHEN GEAR WAS SELECTED DOWN, RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE AND GEAR UNLOCKED LIGHT REMAINED ON. AFTER RECYCLING THE GEAR, THE GEAR LOCKED WITH RECEIVED THREE GREEN LIGHTS. JACKED AIRCRAFT CLEANED/RESEATED ALL GEAR WIRING CONNECTORS COMPLIED WITH (25) GEAR SWINGS NO FAULTS FOUND ALL INDICATIONS NORMAL DOWNJACKED AIRCRAFT. SERVICED MAIN HYDRAULIC RESERVOIR WITH SKYDROL MX IAW THE CE560XL MM CHAPTER 32-30-00 2L72 4F RTA22CE 20050113000592005011300059NM 2005 1 13 C7WA2004000AA 120040825A80121G386 SWITCH BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE START VALVE INOPERATIVE A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177640U 19913 654447 ENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ASSOCIATED EMERGENCY PROCEDURE IAW AOM. LIGHTS STAYED ON UNTIL ENGINE SHUTDOWN ON THE GROUND. REMOVED AND REPLACED NR 3 ENGINE START VALVE LIGHT PRESSURE SWITCH OPS CHECKED GOOD IAW MM. FOUND DUCT AIR TEMP INDICATOR OPS CHECKED OK IAW MM. 2L73 4F4 F A3WE E2EA 20050113000602005011300060NM 2005 1 13 C7WA2004000BB 120040831A3260656021132 ACCESSORY UNIT BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE ELECTRONIC BAY INOPERATIVE A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177644U 20038 RED LT GEAR, RT GEAR, NOSE GEAR AND AMBER TAIL SKID LIGHTS ON PILOTS FRONT PANEL REMAINED ILLUMINATED AFTER GEAR HANDLE WAS RAISED ON TAKEOFF. FLIGHT ENGINEERS ANNUNCIATOR LIGHTS REMAINED OUT. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX IAW MM. OPS CHECK NORMAL IAW MM. 2L73 4F4 F A3WE E2EA 20050113000612005011300061NE 2005 1 13 C7WA2004000CC 220040828A7510652673822 DUCT BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE BROKEN A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177638U 19911 AFTER TAKEOFF NR 3 ENGINE FIRE WARNING WENT OFF. EMERGENCY CHECK LIST ACCOMPLISHED. WHEN NR 3 THROTTLE WAS RETARDED FIRE WARNING LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND NR 3 ENGINE ANTI-ICE DUCT BROKEN. REMOVED AND REPLACED NR3 ENGINE ANTI-ICE DUCT IAW MM. OPS CHECKED GOOD. 2L73 4F4 F A3WE E2EA 20050113000652005011300065NE 2005 1 13 04FDEA03084 220041111A7320441790 HYDROMECH UNIT DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE FUEL SYSTEM FAILED A FDEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO25595FE223556956 48553 "ENG 3 RPM LOW" ALERT RECEIVED AT START OF DESCENT FROM FL330. EGY NR 3 APPROX 50, FUEL FLOW APPROX 700. NO INDICATEIONS OF ENGINE DAMAGED. COMPLIED WITH QRH PROCEDURES FOR ENG RPM LOW AND ENG RESTART INFLIGHT. ENGINE RESTARTED NORMALLY AND OPERATED NORMALLY FOR REMAINDER FO FLIGHT. (OPEN) 2L73 4F4 FRTA22WE E31N3 20050113000662005011300066NM 2005 1 13 2004UALA00980 120041026A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE STA 360-380 AND DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 SKIN AT STA 360-380 AND STR 16L-17L IS DAMAGED. INSTALLED DOUBLER AND TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050114000082005011400008WP 2005 1 14 ARWA20041203 120041217A2612390D AMPLIFIER DOUG DC8 DC863F 302198FWP FIRE DETECTION MALFUNCTIONED A ARWAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19441J 45988 AFTER TAKEOFF NR 4 ENGINE FIRE WARNING ILLUMINATED INTERMITTENTLY, SHUT DOWN ENGINE AND RETURNED TO KMIA AFTER FUEL DUMPING. OVERWEIGHT LANDING IN KMIA, SMOOTH LANDING. REMOVED AND REPLACED AMPLIFIER (POSITION NR 4) IN ACCORDANCE WITH MM 26-10-4 AND REMOVED & REPLACED FIRE LOOP AFT LOOP POSITION IN ACCORDANCE WITH MM 26-10-0 CHECKED SYSTEM OK IN ACCORDANCE WITH MM 26-10-0 AND MM 71-00. 2L74 4F 4A25 20050114000092005011400009NM 2005 1 14 2004UALA01121 120041112A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 AFT CARGO DOOR BEAR STRAP REPAIR NEEDS TO BE REPLACED AT BS 847 STR. 23R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050114000122005011400012NM 2005 1 14 04FDEA03076 120041111A55116520656 SPAR BOEING727 727100 1384036NM HORIZONTAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 N01167 CORROSION ON LT. HORIZ. STAB UPPER SPAR AT STAB STA. 198. REPAIRED PER SRM 55-10-5 FIG 1 2L73 4F RTA3WE 20050114000142005011400014 2005 1 14 SB04130 420040921A22104051601932 CONTROL PANEL BOEING737 737301 1384611NM FLIGHT DECK FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19353US4156641566 23556 DURING CRUISE, EN ROUTE FROM PHL TO DFW, CREW REPORTED THE CHANNEL A AUTOPILOT DROPPED OFF FOLLOWED BY THE AUTOPILOT MODE CONTROL WINDOW DISPLAYING 50,000 FEET. THE LEFT NAV THEN DROPPED OFF LINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE MODE CONTROL PANEL AND PERFORMED FUNCTIONAL CHECK PER R5 CARD. ALSO, REMOVED AND REPLACED FMC AND LOADED NAV DATA. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050114000152005011400015WP 2005 1 14 AALA20041155 120041121A3242910352 CONDUIT DOUG DC9 DC982 3022082WP FUSELAGE DAMAGED A AALAO OTHER O OTHER LDLANDING 1 SW21234AA 49181 DEN - INFLIGHT T1115/21 ON LANDING AIRCRAFT RAN OFF RUNWAY AND MADE CONTACT WITH APPROACH LIGHTS. DAMAGE TO LEFT MAIN LANDING GEAR AND ENGINE COWL. FOUND HYDRAULIC LEAK AT LEFT MAIN LANDING GEAR. REPLACED NUMBER 1 AND 2 FORWARD HYDRAULIC LINES AND SERVICED HYDRAULIC RESERVOIR. ACCOMPLISHED TEMPORARY REPAIRS TO COWLING ON LEFT HAND ENGINE. FERRIED AIRCRAFT TO ORD FOR REPAIR TO DAMAGED LEFT ENGINE NOSE COWL AND LEFT FORWARD LOWER COWL. AIRCRAFT TO FERRY TO TUL FOR REPAIR OF NUMBER 1 BRAKE TEMPERATURE SENSOR CONDUIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (SUPP CLOSED) 2L72 4F A6WE 20050114000172005011400017SO 2005 1 14 CHQA000548 120040903A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11269SK 145293 CENTER AISLE SECOND CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050114000222005011400022NM 2005 1 14 2004UALA01132 120041110A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29932UA 26658 AFT SERVICE DOOR OPENING HAS CRACK AT FWD LOWER CORNER. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED SCUFF PLATE AND TAPERED SHIM. 2L72 4F4 FRTA16WE E2GL 20050114000232005011400023 2005 1 14 2004UALA01175 420041201A256562510101 ASPIRATOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE ESCAPE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29210UA 30216 ASPIRATOR HAS DAMAGED FLAPPER VALVE. FAILED AIR RETENTION TEST DUE TO LEAKING OF VALVE. SUPPLEMENTAL DATA UPDATE SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. DISCREPANT ASPIRATOR WAS OBSERVED DURING SLIDE/RAFT OVERHAUL AIR RETENTION TEST. FAILED AIR RETENTION TEST DUE TO DAMAGED ASPIRATOR FLAPPER VALVE LEAKING. CAUSE OF FLAPPER VALVE DAMAGE HAS NOT BEEN DETERMINED. ASPIRATOR WAS REPLACED PER AIR CRUISERS CMM 25-61-32. 2L72 4F4 FRTT0001SE E46NE 20050114000242005011400024 2005 1 14 2004UALA01176 420041201A256561949108 PACKBOARD AIRCRUISERS BOEING777 777222 1385219NM ESCAPE SLIDE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29227UA 1008 30555 PACKBOARD CRACKED IN 2 PLACES. SLIDE/RAFT WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. PACKBOARD CRACKS WERE OBSERVED DURING SLIDE/RAFT OVERHAUL. CRACKS WERE MINOR AND WOULD NOT HAVE AFFECTED PERFORMANCE OF THE SLIDE/RAFT. IT IS POSSIBLE CRACKS WERE CAUSED BY REMOVAL FROM AIRCRAFT OR SUBSEQUENT HANDLING. CRACKS WERE REPAIRED PER AIR CRUISERS CMM 25-61-31. 2L72 4F RTT0001SE 20050114000252005011400025NM 2005 1 14 AWXA200401233 120041104A2120M204JJJX5011 BEARING HONEYWELL BOEING737 737375 13844BNNM ZONE 213 DISINTEGRATED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28336AW 212085 23707 PHX - AIR TURN BACK - FLT 0158 - ON CLIMB OUT OF PHX EN ROUTE TO STL NOTICED A MODERATE AIRFRAME VIBRATION LEAVING FL 180, TURNED BACK TO PHX, VIBRATION CONTINUED THROUGH DESCENT AT FL 10 VIBRATION CEASED. MAINTENANCE REMOVED AND REPLACED R/H TURBINE FAN ASSEMBLY IAW T/C R2C21002, OPERATIONAL CHECK WAS GOOD. **SUPP** REPAIR VENDORS INCOMING INSPECTION OF TURBO FAN S/N 212085 FOUND FAN SEIZED, OPERATIONAL TEST COULD NOT BE PERFORMED. DISASSEMBLY OF UNIT FOUND CATASTROPHIC DAMAGE CAUSED BY BEARING FAILURE IN TURBINE SECTION, UNIT BEYOND ECONOMICAL REPAIR, SCRAPPED AT VENDOR. 2L72 4F RTA16WE 20050114000262005011400026 2005 1 14 2004UALA00997 420041031A256520131 BATTERY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29671UA 30026 RIGHT OVERWING SLIDE SQUIB DOES NOT TEST IN POSITION 1. DEFECT CAUSED BY LOW BATTERY. REPLACED RIGHT HAND BATTERY. 2L72 4F4 FRTA1NM E24NE 20050118000012005011800001 2005 1 18 249TR0102 420041222A2230MS245471 SWITCH BOEING737 7372K5 138448XNM COCKPIT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05249TR 22598 RIGHT TO/GA SWITCH IS INOP. REPLACED SWITCH S787B IN RIGHT THROTTLE PER MM 34-22-0 AND MM 22-31-01. 2L72 4F RTA16WE 20050118000022005011800002WP 2005 1 18 04FDEA03388 120041207A5210 CONNECTOR DOUG DC10 DC1010 3022110WP R1 DOOR DIRTY A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2568058 46705 AFTER TAKEOFF R1 DOOR LIGHT CAME ON AND WOULD NOT PRESSURIZE. ATB TO MEM. MEL 52-04-02: FWD CABIN DOOR CAUTION LIGHT INOPERATIVE. CHECKED WIRING ON R-1 DOOR, CLEANED CONNECTOR TO ACTUATOR. PRECAUTIONARY, ACTUATED DOOR MULTIPLE TIMES INSIDE AND OUT, CLEANED OUT SIDE SWITCH. DOOR OPS CHECKED NORMALLY AS PER M/M 52-10-01-2, OK TO CONTINUE. 2L73 4F A22WE 20050118000032005011800003WP 2005 1 18 0400349860 120040228A2782 ACTUATOR DOUG DC9 DC951 3022051WP SLATS MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01769NC 47757 DURING APPROACH FOR LANDING, THE RIGHT LEADING EDGE SLAT DID NOT COME FULLY OUT ON EXTENSION. THE AIRCRAFT DID EXPERIENCE AN UNCOMMANDED ROLL TO THE RIGHT. THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT DID ILLUMINATE AND THE BLUE SLAT EXTEND INDICATOR DID NOT. AS THE AIRCRAFT SLOWED TO 210 KTS BOTH SLATS EXTENDED. ALL INDICATIONS WERE NORMAL AND THE LANDING WAS UNEVENTFUL. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND FOUND NO DISCREPANCIES IN THE SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 20050118000042005011800004WP 2005 1 18 05FDEA00044 120040610A5310AFA32491 RAIL DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25374FE 46612 BULK CARGO DOOR JAMB RAIL P/N AFA3249-1 CORRODED APPROX AT STA 1755-1764. FILLER, CAP AND REPAIR ANGLE INSTALLED AFTER CORROSION REMOVAL IAW FEDEX EA 8-5310- 79980. 2L73 4F RTA22WE 20050118000112005011800011WP 2005 1 18 0402219926 120041227A2170 COALESCER BAG DOUG DC9 DC932 3022066WP BOTH CONTAMINATED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01926NW 47425 IMMEDIATELY AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN THE CABIN AND THE LAVATORY SMOKE DETECTORS IN ALARM. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO AN UNEVENTFUL LANDING BACK AT FLL. NO MENTION OF COM OR APU/PACK CONFIGURATION. PASSENGERS DEPLANED NORMALLY THROUGH MAIN CABIN DOOR AND CFR FOUND NO EVIDENCE OF FIRE. MAINTENANCE COULD NOT FIND ANY FAULTS EXCEPT FOR A PUDDLE OF DE-ICING FLUID IN THE TAIL CONE AND EXTERIOR. THE DE-ICE FLUID WAS CLEANED UP, BOTH WATER SEPARATORS BAGS WERE REPLACED, AND PACK BURNOUT PROCEDURES WERE COMPLIED WITH. NO SMOKE OR SMELL PRESENT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 20050118000172005011800017NM 2005 1 18 UPS05M43627 120041211A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 290 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C, CABIN CORROSION ON SEAT TRACK FLANGE AT STA 1900-2007 X =107.0. CORROSION REMOVE AT STA1995 X=107, FOUND EXCEED LIMIT. MATERIAL REMOVED 0.060 IN & ORIGINAL MATERIAL THICKNESS 0.080 IN, OUT OF LIMIT. TRIMMED AT & NDT PERFORMED, FOUND NO CRACK EVIDENT. REPAIR PARTS FAB USING 7075-T6 0.080 IN & 707 5-T6 0.125 IN AS PER SRM 53-70-00 F-5.V-1.R.35. REPAIR PTS FR PRIME AS PER 51-21-01-V-2.R-35 & INSTALLED PER SRM 53-70-00F-5.V.1.R.35. 2L73 4F RTA22WE 20050118000222005011800022NM 2005 1 18 AWXA200500027 120041222A575465C26602212 SKIN BOEING737 7373Q8 1384670NM NR 5 SLAT DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE ON UPPER AND LOWER SURFACE AT OUTBOARD END BETWEEN SS 248.87 AND SS 254.27. MAINTENANCE REMOVED DAMAGE IN NR 5 SLAT WEDGE ON UPPER AND LOWER SURFACE AT OUTBOARD END; FABRICATED NEW HONEYCOMB CORES AND DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 16. 2L72 4F RTA16WE 20050328000852005032800085EA 2005 3 28 YAX2005F00000 220040606A7314RG17980DM PUMP PIPER PA32 PA32300 7103212SO LYC O540 TIO540* 41532EA HARTZLHCC2Y HCC2YK1 GL FUEL SYSTEM FAILED E YAXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AL0515950 587 327340075 L1819548A CH35455B UPON TAKE-OFF, THE ENGINE FALTURED AND STUTTERED, THE PILOT EXITED THE RUNWAY AND UNLOADED PASSENGERS AND FREIGHT. THE AIRCRAFT WAS BROUGHT TO THE SHOP WHERE IT WAS DISCOVERED THAT THE FUEL PRESSURE WAS LOW. THE MECHANICS REPLACED THE ENGINE DRIVEN FULE PUMP, AIRCRAFT WAS TEST FLOWN AND THEN RETURNED TO SERVICE. (AL05200402659) (K) 1L71 3O3 O A3SO E14EA 5 CP920 20050329000222005032900022WP 2005 3 29 ASAA0480603 120041214A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL IS DENTED AND RIPPED AT AFT SIDE. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050329001062005032900106WP 2005 3 29 ASAA0480617 120041216A53115912995504 FRAME DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, MOUNTING HOLES GOUGED AT BOTTOM FRAME OF RIGHT OVERWING EXIT. INSTALLED DOUBLER PER EA 5320-01680. (M) 2L72 4F RTA6WE 20050329001472005032900147SO 2005 3 29 MASA200400665 120041129A3260852701 SENSOR EMB 145 EMB145LR 3260212SO NLG INOPERATIVE A MASAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07836MJ9428 145359 RETURNED TO THE FIELD DUE TO THE LANDING GEAR AIR TO GROUND MESSAGE ILLUMINATED. MAINTENANCE FOUND NOSE PROX SENSOR WOW CANNON PLUG LOOSE. RESECURED CANNON PLUG, FOUND RT FWD WOW SENSOR CRACKED AND FOUND LT AFT SENSOR INOP. MX REMOVED AND REPLACED LT AFT AND RT FWD SENSOR OPS CHECKED GOOD. P/N 8-527-01, LT S/N A-16169, RT S/N A-16161 BOTH TT 9428 AND 8737 TC. 2L72 4T RTT00011AT 20050329002012005032900201NM 2005 3 29 EIA2004154 120041203A5311 FRAME BOEING747 747132 1384882NM FUSLEAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D FRAME FOUND CRACKED AT BS 2180 ST25L. FRAME REPAIRED PER SRM 53-10-04 FIG 1. 2L74 4F A20WE 20050329002022005032900202NM 2005 3 29 EIA2004155 120041203A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D FRAME FOUND CRACKED AT BS 2220 ST23L. FRAME REPAIRED PER SRM 53-10-04 FIG 1. 2L74 4F A20WE 20050329002132005032900213NM 2005 3 29 EIA2004156 120041203A5313 STRINGER BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 1470-1475 S15R STRINGER END CRACKED. STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050328000842005032800084EU 2005 3 28 IJA2005F00000 120041210A2435800350 STARTER GEN AEROSPAS355 AS355N 8680818EU TMECA ARRIUSARRIUS1A NE LT ENGINE VIBRATION G IJAAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 CE07912EM 5560 STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND THE STARTER GEN ADAPTER WAS FOUND TO HAVE 2 MOUNTING FLANGES BROKEN OFF AND ONE CRACKED. THINK THAT THE STARTER GEN VIBRATION SHOULD BE CHECKED EVERY 25 HOURS EVEN IF THE NEW EXHAUST PIPE HAS THE RETAINING STRAPS IAW TU106. (K) 1G72 3U3 URTH11GU E34NE 20050328000922005032800092CE 2005 3 28 CVU2005F00000 120041123A3710442CW6 PUMP BEECH 80 65B80 1152812CE LYC O720 IO720A1B 41546EA HARTZLHCA3V HCA3VK2 GL RT ENGINE FAILED E CVUAK NONE O OTHER ININSP/MAINT 1 WP1346MA 371 LD413 PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR, DAY) (K) 1L72 3O3 O 3A20 1E15 5 CP6EA 20050328001042005032800104CE 2005 3 28 LJJ2005F00000 120041231A5310 STRAP BEECH 100 A100 1152915CE PWA PT6 PT6A27 52043EA LT SPAR CORRODED E LJJAK NONE O OTHER ININSP/MAINT 1 EA23601LM B116 CORROSION FOUND AT HOLE B, LWS 90.35, DURING INSPECTION OF LT S AND K SPAR STRAP. DER WAS CONSULTED FOR REPAIR. RECOMMEND CLOSE INSPECTION OF HOLES DURING REPETITIVE INSPECTIONS. ALSO RECOMMEND THE USE OF AN ANTI-CORROSION LUBRICANT DURING BOLT INSTALLATION. (K) 1L72 3T4 T A14CE E4EA 20050329000132005032900013WP 2005 3 29 ASAA0480618 120041216A5330591140733 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK, FUSELAGE SKIN DENTED AT R1 DOOR CUTOUT. REPAIRED DENT PER EA 5330-01864. (M) 2L72 4F RTA6WE 20050329000302005032900030WP 2005 3 29 ASAA0480612 120041216A57303912757503 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, LEFT WING FUEL PANEL 1303 CHAFED AND PITTED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050329000312005032900031WP 2005 3 29 ASAA0480614 120041216A531359644461 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, FOUND LONGERON 30 IS CORRODED. REMOVED DAMAGED SECTION. INSTALLED U-CHANNEL AND FILLER. (M) 2L72 4F RTA6WE 20050329000322005032900032WP 2005 3 29 ASAA0480615 120041216A53135936053501 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, LONGERON 29L IS CORRODED. APPLIED SEALANT PER EA 5310-02430. (M) 2L72 4F RTA6WE 20050329000352005032900035WP 2005 3 29 ASAA0480600 120041214A532199365391 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD, CRACKED. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M) 2L72 4F RTA6WE 20050329001052005032900105WP 2005 3 29 ASAA0480608 120041216A57535935907 BRACKET DOUG DC9 DC983 3022083WP FLAP TRACK CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, LEFT WING INBOARD FLAP TRACK MOUNTING BRACKET BOLT HOLES ARE PITTED. REAMED HOLES AND INSERTED BUSHINGS PER EA 5750-01160. (M) 2L72 4F RTA6WE 20050329002162005032900216NM 2005 3 29 04FDEA03408 120041213A5320NJC6040U175 ANGLE DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, TEE ANGLE ON BULKHEAD STA 2007 CORRODED AT LBL 36. MAIN DECK, CORRODED TEE ANGLE ON BULKHEAD AT STA 2007 LBL 36. REMOVED AND NEW TEE ANGLE INSTALLED AS PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050330000522005033000052 2005 3 30 KBM2005F00035 420040209A3422 POWER SUPPLY SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE DIRECTIONAL GYROBURNED OUT E KBMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP1953SH 23010 2009 SMOKED POWER SUPPLY INTERNAL INPUT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050330000562005033000056GL 2005 3 30 UIEA200400208 220041228A75309125M65G13 ARM BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 1 ENGINE VSV BROKEN A UIEAK NONE O OTHER ININSP/MAINT 1 EA15409MC 30558 DURING ACCOMPLISHMENT OF ENGINE CONDITION MONITORING ALERT ITEM NR 2004P093. ENGINE NR 1 VISUAL INSPECTION OF STG 5 ACTUATION HARDWEAR, FOUND ONE VSV LEVER ARM MISSING AT 11 OCLOCK POSITION AMM. REPLACED ENGINE NR 1 IAW WORK CARD NR A717101GT1 AND MM. PERFORMED OPS CHECK AND LEAD CHECK, ALL OK. (K) 2L74 4F4 FRT1384945 E23EA 20050330000572005033000057NM 2005 3 30 RYN2005F00001 120041224A213111211997110AC CONTROLLER BOEING737 737800* NM CABIN PRESSURE INOPERATIVE A RYNAO OTHER J WARNING INDICATION CRCRUISE 1 CE07ELDGZ 28718 UNABLE TO CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER. (K) 2L72 4F RTA16WE 20050330000582005033000058SO 2005 3 30 N382005F00000 120041209A5310 DOOR FRAME GULSTMG1159 G1159B 3953535SO FUSELAGE CRACKED A N38RO OTHER O OTHER NRNOT REPORTED 1 EA05211SJ 75 DURING AC 4000 LANDING INSPECTION, FOUND APPROX 1INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRACK AND REPAIRED WITH AN OVERLAY DOUBLER IAW THE SRM. OVERLAY INSTALLED WET WITH PRC 1440. (K) 2L72 4F RTA12EA 20050330000592005033000059NE 2005 3 30 ASAA0480481 220040805A7200 RELIEF VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE RT ENGINE FAILED A ASAAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM02968AS 53016 6720 CLIMB, OIL PRESSURE AND QUANTITY INDICATIONS DROPPED BELOW ACCEPTABLE LEVELS. ENGINE WAS SHUTDOWN IN FLIGHT, AND ATB TO LAX WAS EXCUTED. REMOVED AND REPLACED ENGINE DUE INDICATION OF INTERNAL FAILURE. REPLACED OIL PRESSURE RELIEF VALVE. OP AND LEAK CHECKED OK. NO INTERNAL FAILURE FOUND. (K) 2L72 4F4 FRTA6WE E9NE 20050330000612005033000061WP 2005 3 30 WPA2005F00000 120041128A3260 INDICATOR CVAC 640 640340D 2422814WP RROYCEDART DART54210 54522EU MLG MALFUNCTIONED I WPABO OTHER N FALSE WARNING DEDESCENT 1 SW013417 48 DURING DECENT, UPON SELECTING GEAR DOWN. ALL 3 GREEN GEAR DOWN AND LOCKED LIGHTS ILLUMINATED. THE RED GEAR UNSAFE LIGHT ALSO REMAINED ILLUMINATED. AFTER LANDING THE RED UNSAFE LIGHT EXTINGUISHED AFTER SEVERAL MINUTES. CURRENTLY WE HAVE BEEN UNABLE TO DUPLICATE SQUAWK. AFTER 2 DAYS OF TROUBLESHOOTING, STILL UNABLE TO DUPLICATE. REPLACED GEARDOWN RELAY WITH NEW (PN 237- EAU) AND ALL 3 (MAIN AND NOSE) LANDING GEAR DOWNLOCK SWITCHES WITH NEW. ALL GROUND OPS CHECKS AND FLIGHT TEST NORMAL. (SW01200501233) (K) 2L72 4T4 TRTA793 E5EU 20050330000622005033000062EU 2005 3 30 KC82005F00000 120041209A215014640113A0101 VALVE AMD FALCONFALCON20 2730103EU GE CF700 CF7002D 30010NE AIR CONDITIONINGSTUCK E KC8AK NONE O OTHER ININSP/MAINT 1 GL2370CK 128 AIR CONDITIONING VALVE STUCK PARTIALLY OPEN NOT ALLOWING ENOUGH AIR INTO THE CABIN TO PRESSURIZE. REPLACED VALVE WITH SERVICEABLE VALVE. PERFORED OPS CHECK IAW MM. 2L72 4F4 FRTA7EU E7EA 20050330000632005033000063CE 2005 3 30 JX62005F00000 120041130A326041EN16 SQUAT SWITCH BEECH MU300 400BEECH CE MLG MALADJUSTMENT E JX6AO OTHER O OTHER NRNOT REPORTED 1 CE09599JL RJ14 FOLLOWING MAJOR MAINTENANCE AIRCRAFT DEPARTED AIRPORT. UPON GEAR RETRACTION THRUST REVERSER UNLOCKED LIGHTS ILLUMINATED. EMERGENCY STOW SWITCHES WERE DEPRESSED AND AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. INVESTIGATION REVEALED MLG SQUAT SWITCHES WERE ADJUSTED IMPROPERLY DURING MAINTENANCE EVENT. AIRLOAD ON LANDING GEAR CAUSED MALFUCTION IN FLIGHT. SWITCHES WERE READJUSTED PROPERLY. UNEVENTFUL FLIGHT WAS CONDUCTED FOLLOWING ADJUSTMENT. TO PREVENT RECURRENCE MAINTENANCE PERSONNEL SHOULD FOLLOW FULLY THE SWITCH ADJUSTMENT INSTRUCTIONS IN THE AC MM. (NM03200504817) 2H72 4F RTA16SW 20050330000852005033000085 2005 3 30 S2YA04008 420040322A34141303800057 INDICATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE AIRSPEED ERRATIC A S2YAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL1391SK 16115258 UE91 DURING TAKEOFF ROLL, THE CREW NOTICED THE FO`S AIRSPEED INDICATOR WENT FROM INDICATING 0 KNOTS TO 55 KNOTS WHEN THE PILOT`S GAUGE INDICATED 75 KNOTS. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE FO`S AIRSPEED INDICATOR AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2L72 4T4 TRTA24CE E26NE 20050330000862005033000086NE 2005 3 30 S2YA04009 220040326A7261310047001 ELBOW BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE CRACKED A S2YAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL13881SK UE88 DURING FLIGHT, MASTER WARNING ILLUMINATED FOR THE RT ENGINE OIL PRESSURE INDICATION. THE RT ENGINE AUTO-FEATHERED AND THE CREW IAW QRH SHUTDOWN THE ENGINE IN FLIGHT. THE AC THEN MADE AN AIR-TURN-BACK AND DECLARED AN EMERGENCY. THE CREW MADE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM AND FOUND THE OIL PRESSURE ELBOW HAD CRACKED AS A RESULT THE PROP LOST OIL PRESSURE AND WENT INTO A FEATHERED POSITION. MX REPLACED THE ELBOW AND SERVICED, INSPECTED AND RAN THE ENGINE. THE AC WAS FERRIED BACK, AND THE RT ENGINE WAS REPLACED. (K) 2L72 4T4 TRTA24CE E26NE 20050330000892005033000089NM 2005 3 30 S2YA04014 120040507A2120 SMOKE DORNERDO32 DO328300 NM PWA 306 PW306B NE COCKPIT DETECTED A S2YAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL13351SK 3108 DURING FLIGHT, THE CREW REPORTED SMOKE IN THE COCKPIT, DIVERTED AND PERFORMED AN EMERGENCY LANDNG. THE CREW MADE AN UNEVENTFUL LANDING AND EVACUATED ON THE RUNWAY. THE AC WAS INSPECTED AND OPERATED IN SEVERAL DIFFERENT ENGINE, APU AND EVIRONMENTAL PACKS CONFIGURATIONS BUT COULD NOT PRODUCE ANY SMOKE. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330000902005033000090 2005 3 30 S2YA04016 420040522A3417 COMPUTER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13801SK UE80 DURING FLIGHT, THE CREW NOTED SEVERAL ELECTRICALLY RELATED ANNUNCIATORS ILLUMINATED INCLUDING THE FLIGHT DIRECTOR AND YAW DAMP. THE CREW MADE A PRECAUTIONARY AIR-TURN-BACK. MX INSPECTED THE SYSTEM INCLUDING REMOVAL, INSPECTION AND REINSTALL OF BOTH FYD-65 YAW DAMP COMPUTERS. MX WAS NOT ABLE TO DUPLICATE THE PROBLEM OR FIND ANY DISCREPANCIES. AFTER A DELAY THE AC CONTINUED ON FLIGHT, WITH NO FURTHER DEFECTS. (K) 2L72 4T4 TRTA24CE E26NE 20050330000922005033000092CE 2005 3 30 S2YA04018 120040601A2422SPC10 INVERTER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT AC ERRATIC A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL1392SK 10632 UE92 BEFORE FLIGHT, THE CREW NOTED SEVERAL ELECTRICALLY RELATED PROBLEMS, INCLUDING LT AC ANNUNCIATOR ILLUMINATED AND THE VOLT METER BEING ERRATIC. THE CREW RETURNED TO THE GATE AND AFTER CONSULTING WITH MX, MEL`D THE SYSTEM. MX INSPECTED THE SYSTEM INCLUDING SWAPPING THE INVERTERS AND THE PROBLEM SWITCHED SIDES. MX RETURNED THE GOOD INVERTER BACK AND REPLACED THE OTHER INVERTER. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2L72 4T4 TRTA24CE E26NE 20050330000942005033000094CE 2005 3 30 S2YA04024 120040706A3213114810021607 AXLE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT MLG BROKEN A S2YAO OTHER O OTHER LDLANDING 1 GL1387SK UE87 DURING LANDING, CREW NOTED A PROBLEM WITH GEAR. IT STARTED AS A VIBRATION/SHIMMY AFTER TOUCHDOWN, THEN LT LOWER LANDING GEAR TO ROTATED CAUSING AC TO VEER TO LT AT END OF ROLLOUT. PAX DEBARKED ONTO RUNWAY AND WERE SHUTTLED TO TERMINAL. MX INSPECTED AC AND FOUND LT MLG LOWER TORQUE KNEE ATTACH POINT HAD BROKEN OFF FROM REST OF LOWER CASTING (KNUCKLE CASTING). WHEN CASTING BROKE, LOWER ASSY OF LANDING GEAR WAS NO LONGER ATTACHED TO TORQUE KNEE ENABLING LOWER ASSY TO ROTATE. MX REPLACED LT MLG AXEL AND PISTON ASSY AND OTHER DAMAGE PARTS INCLUDING TORQUE KNEE, SQUAT SWITCH AND WHEEL ASSY. MX OPS CHECKED SYS, FOUND NO FURTHER DISCREPANCIES. 2L72 4T4 TRTA24CE E26NE 20050330000972005033000097NM 2005 3 30 S2YA04031 120040908A2421ALT3524 ALTERNATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE RT INTERMITTENT A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13358SK7825 14 3188 DURING TAKEOFF OF FLIGHT, THE CREW REPORTED THE RT ALTERNATOR FAIL CAS MESSAGE. THE CREW DID A LOW SPEED ABORTED TAKEOFF. THE MESSAGE CLEAR ITSELF AND AFTER CONSULTING WITH MX A SECOND ATTEMPT WAS MADE. DURING THE SECOND TAKEOFF, THE CREW REPORTED THE RT ALTERNATOR FAILED CAS MESSAGE. THE CREW DID A LOW SPEED ABORTED TAKEOFF. THE CREW CONSULTED WITH MX AND THE AC HAD TO FERRIED BACK TO DEPARTURE. MX INSPECTED THE SYSTEM AND REPLACED THE RT ALTERNATOR MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. NOTE: THIS SN ALTERNATOR HAD BEEN SWAPPED FROM LT TO RT FOR TROUBLESHOOTING OF 2 CAS MESSAGES (L ALT FAIL) AND (L A/C VOLT FAIL) BUT THE PROBLEM DID NOT SEEM TO FOLLOW. (K) 2H72 4T4 FRTA55NM E35NE 20050330001002005033000100CE 2005 3 30 S2YA04036 120041004A33501013810087 BATTERY BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE EMERGENCY LIGHT DISCHARGED A S2YAA UNSCHED LANDING O OTHER CRCRUISE 1 GL1385SK 7941 1086 UE85 DURING FLIGHT, THE CREW NOTED THE BATTERY WAS NOT CHARGING SINCE THE BATTERY CHANGE LIGHT HAD STAYED ON SINCE START UP AND WAS STILL DRAWING 10-20 AMPS. INSTEAD STRANDING THE AC, THE DECISION WAS MADE TO PERFORMED AN AIR-TURN-BACK. MX CHARGED THE BATTERY AND INSPECTED THE SYSTEM AND FOUND NO DISCREPANCIES. MX REPLACED THE BATTERY AND RETURNED AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2L72 4T4 TRTA24CE E26NE 20050330001012005033000101NM 2005 3 30 S2YA04037 120041014A52970010908A506000 WIRE HARNESS DORNERDO32 DO328300 NM PWA 306 PW306B NE AIRSTAIR INOPERATIVE A S2YAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL13360SK 3136 DURING FLIGHT, JUST AFTER LEVELING OFF AT FL280, THE CREW NOTED MULTIPLE CHIME AND MESSAGES FOR THE MAIN DOOR BEING OPEN. THERE WAS NO CHANGE IN PRESSURE SO IT WAS A SUSPECTED SENSOR PROBLEM SO THEY MADE AN AIR-TURN-BACK. THE MX INSPECTED THE AC AND REPLACE THE AIR STAIR DOOR PROXIMITY SENSOR HARNESS. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330001032005033000103NM 2005 3 30 S2YA04040 120041002A21504068B000002 CONTROL VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE RT A/C PACK INOPERATIVE A S2YAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL13360SK101652209 3136 BEFORE FLIGHT, A PASSENGER NOTICED SMOKE COMING FROM THE FLIGHT DECK. THE CREW DEPLANED THE PAX. MX INSPECTED THE AC INCLUDING RUNNING THE ENGINES BUT COULD NOT DUPLICATE THE SMOKE. THE AC WAS RETURNED TO SERVICE. THE RT PACK OVERHEATED AND WAS FOLLOWED BY SMOKE IN THE CABIN. MX REPLACED THE RT PACK FLOW CONTROL VALVE. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330001042005033000104NM 2005 3 30 S2YA04042 120041123A2131 CONTROLLER DORNERDO32 DO328300 NM PWA 306 PW306B NE CABIN PRESSURE MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13352SK 3111 DURING CLIMB OUT, THE CREW WAS UNABLE TO PRESSURIZE THE AC AND RECEIVED INTERMITTENT DOOR OPEN INDICATION. THE CREW PERFORMED AND AIR-TURN-BACK. MX INSPECTED THE AC INCLUDING PRESSURIZATION AND DOOR INDICATION. THE AC WAS PRESSURIZED TO MAXIMUM PRESSURE DIFFERENTIAL WITH NO DEFECTS NOTED. THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330001062005033000106NM 2005 3 30 S2YA04047 120041213A7700 WARNING LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE ILLUMINATED A S2YAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL13354SK 82 3126 SHORTLY AFTER TAKEOFF, THE CREW NOTICED A LT ENGINE FADEC FAULT. THE CREW PERFORMED AN AIR-TURN-BACK. AFTER MX CONSULTATION THE ANNUNCIATOR WAS MEL`D AND THE AC RETURNED TO SERVICE. MX TROUBLESHOT THE SYSTEM INCLUDING INSPECTION OF THE WIRING. WITH NO DEFECTS NOTED THE LT ELECTRONIC ENGINE CONTROL (EEC) FOR TROUBLESHOOTING. WITH NO FURTHER DISCREPANCIES THE MEL WAS CLEARED AND THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330001072005033000107NM 2005 3 30 S2YA04048 120041215A7500 CONNECTOR DORNERDO32 DO328300 NM PWA 306 PW306B NE BLEED SYSTEM DIRTY A S2YAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL13351SK 3108 BEFORE FLIGHT, DURING TAXI OUT THE CREW GOT A RT BLEED SOV CAS MESSAGE, THEY CONSULTED WITH MX BUT WERE UNABLE TO GET IT TO CLEAR. THE AC RETURNED TO THE GATE. MX CLEANED THE RT LOW PRESSURE AND HIGH PRESSURE VALVE CONNECTORS. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330001082005033000108NE 2005 3 30 ALG2005F00010 120041208A3260 PROXIMITY SWITCH SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG OUT OF ADJUST E ALGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW03518AL 760134 CAE890798S ON TAKE OFF, AFTER RAISING GEAR HANDLE, THE RED LIGHT WOULD NOT GO OUT. RECYCLED GEAR NO CHANGE, RETURNED TO GET FIXED. MAINTENANCE ADJUSTED PROXIMITY SWITCH TO PROPER POSITION, HAD PILOT PULL TO A HOVER AND CYCLE THE LANDING GEAR ALL LIGHTS WENT OUT, RETURNED AIRCRAFT TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20050330001122005033000112EA 2005 3 30 REXA04054 120041228A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258611A 7611 FLAPS FAILED AT ZERO, WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY. DIVERTED, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED, LUBED AND REINSTALLED FLEX SHAFTS. PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K) 2L72 4F4 FRTA21EA E15NE 20050330001172005033000117SO 2005 3 30 GUU2005F00003 120041226A3397 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT CHAFED A GUUAK NONE O OTHER ININSP/MAINT 1 SO17282AS 120226 DURING MAINTNANCE DAILY CHECK, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED CHAFED RT EMERGENCY LIGHT WIRE AND FUSE. OPERATIONAL CHECK NORMAL. (K) 2L72 4T4 TRTA31SO E20NE 20050330001182005033000118NM 2005 3 30 HALA0500119 120041227A7714889313 PROBE BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE NR 2 ENGINE SHEARED A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13481HA 55126 ON DEPARTURE AT 4500 FT, RT ENGINE BEGAN OSCILLATING- AUTO IGNITION ON ENGINE OUT PAGE CAME UP. REDUCED POWER/ RETURED TO DEPARTURE. NO LIMITS EXCEEDED. TROUBLESHOT IAW FIM, TASK 803. REPLACED NR 2 ENGINE NR 2 SPEED PROBE SHEARED IAW MM. OPS AND LEAK CHECK PENDING. OPS AND LEAK CHECK GOOD IAW MM. NO FAULTS NOTED. 2L72 4F4 FTRA6WE E00061EN 20050330001272005033000127EU 2005 3 30 BAQ2005F00000 120041110A641010981320H11 BLADE AGUSTAA109 A109E 0260119EU TMECA ARRIELARRIEL1C 60030NE TAIL ROTOR CRACKED E BAQAK NONE O OTHER ININSP/MAINT 1 EA03911UF176 11604 FOUND CRACK ON 1 SIDE OF T/R BLADE AT STA 540.00, CRACK EXTEND FROM DOUBLER BACK 4 INCHES ALONG STA 540. CORDWISE REF FIG. 1 OF AD 2002-25-51 AIRCRAFT WAS POST MOD. (K) 1G72 3U3 URTH7EU E19EU 20050330001312005033000131CE 2005 3 30 TIM2005F00001 120041018A5512115620010121 SHEAR PLATE BEECH 99 B99 1154004CE PWA PT6 PT6A27 52043EA HORIZONTAL STAB CRACKED E TIMAK NONE O OTHER ININSP/MAINT 1 NM07950AA U159 WHILE INSPECTING THE HORIZONTAL STABILIZER, THE LT SHEAR PLATE WAS FOUND TO HAVE A CRACK RUNNING ACROSS IT. THE ELEVATOR CONTROL HORN IS ATTACHED TO THE SHEAR PLATE WHICH IS ATTACHED TO THE HORIZONTAL STABILATOR. THE CRACK MUST HAVE DEVELOPED UNDER NORMAL CIRCUMSTANCES. DO NOT HAVE AN IDEA FOR THE PROBABLE CAUSE OR RECOMMENDATION FOR PREVENTING RECURRENCE. THE AGE AND AMOUNT OF FLIGHT HOURS MAY HAVE BEEN A CONTRIBUTING FACTOR. 1L72 3T4 T A14CE E4EA 20050330001402005033000140NM 2005 3 30 ASA0440375 120041227A53116546595260 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - DENT IN TOP OF FRAME FLANGE. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050330001412005033000141NM 2005 3 30 ASA0440354 120041218A532069434771 SUPPORT ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FLOOR TO WALL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CORROSION ON FLOOR TO WALL SUPPORT. REPLACED WALL SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050330001422005033000142NM 2005 3 30 ASA0440353 120041218A534069353527 STRINGER CLIP BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - STRINGER CLIP CRACKED. REPLACED STRINGER CLIP. (K) 2L72 4F4 FRTA16WE E21EU 20050330001552005033000155CE 2005 3 30 XIR2005F00000 120041102A321059420011 BELLCRANK CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MLG CORRODED E XIRAK NONE O OTHER ININSP/MAINT 1 WP09101G 310R0017 PART SHOWED SIGNS OF INTERGRANULAR CORROSION AT BRAKE. (K) 1L72 3O3 O 3A10 E5CE 20050330001592005033000159EU 2005 3 30 IJA2005F00001 120041026A78100319778440 EXHAUST PIPE AEROSPAS355 AS355N 8680818EU TMECA ARRIUSARRIUS1A NE LT ENGINE FAILED E IJAAK NONE O OTHER ININSP/MAINT 1 CE07912EM 5560 (3) OUT OF (4) STRUTS THAT HOLD THE OUTSIDE PART OF THE EXHAUST ON FAILED. TT OF THE PART IS UNKNOWN. MFG THINKS THE PROBLEM IS RELATED TO A HIGH VIBRATION IN THE STARTER GEN. THE VIBRATION LEVEL WAS .04 WHICH IS WELL BELOW THE LIMIT. (CE07200502200) (K) 1G72 3U3 URTH11GU E34NE 20050329000152005032900015WP 2005 3 29 ASAA0480611 120041216A53105936070 SPACER DOUG DC9 DC983 3022083WP DOOR FRAME CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, AFT CARGO BAY DOOR JAMB BEAM SPACER IS CORRODED. REPLACED SPACER. (M) 2L72 4F RTA6WE 20050329000192005032900019WP 2005 3 29 ASAA0480605 120041216A575359359153 JOINT DOUG DC9 DC983 3022083WP LT WING TE FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - DURING HV-CHECK, LT WING FLAP FLEX JOINT UPPER BAR 6TH HOLE FROM T/E DAMAGED. REPAIRED WITH WASHER PER EA 5750-02019. (M) 2L72 4F RTA6WE 20050329000202005032900020WP 2005 3 29 ASAA0480601 120041214A53219936537 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL, IN COCKPIT, HAS EDGE DAMAGE. REPAIRED DAMAGED AREA WITH FIBERGLASS. (M) 2L72 4F RTA6WE 20050329000232005032900023WP 2005 3 29 ASAA0480604 120041214A53219957918 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV -CHECK FLOOR PANEL HAS ONE REINFORCEMENT HAT SECTION CRACKED, ANOTHER BUCKLED. REPLACED DAMGED HAT SECTIONS. (M) 2L72 4F RTA6WE 20050329000332005032900033WP 2005 3 29 ASAA0480599 120041214A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 OKC - HV-CHECK, CABIN FLOOR PANEL, FLOORBOARD DELAMINATED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050330000462005033000046WP 2005 3 30 XV62005F00001 220040905A72618941172 ADAPTER DORNERDO228 DO228202 2992030EU GARRTTTPE331TPE33110T WP OIL FILTER CRACKED E XV6AK NONE O OTHER ININSP/MAINT 1 WP19405VA 1962 8144 OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200501116) 2H72 4T4 TRTA16EU E4WE 20050330000502005033000050EU 2005 3 30 KBM2005F00020 120040218A6720704A34130184 CONTROL CABLE SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR FAILED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19215LA 2143 TAIL ROTOR CONTROL CABLE, BLACK GREASE COMING FROM BOTH ENDS. (OLD STYLE) REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050330001052005033000105NM 2005 3 30 S2YA04045 120041201A5270 PROXIMITY SWITCH DORNERDO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR DIRTY A S2YAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL13354SK 3126 SHORTLY AFTER TAKEOFF, THE CREW NOTICED A CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. MX CLEANED THE POXI SWITCHES OF ICE AND SNOW, OPENED AND CLOSED THE CARGO DOOR. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330001112005033000111EA 2005 3 30 REXA04053 120041228A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER J WARNING INDICATION APAPPROACH 1 SO258505Q 7505 FLAPS FAILED AT ZERO WHEN SELECTD TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K) 2L72 4F4 FRTA21EA E15NE 20050330001292005033000129NE 2005 3 30 KC82005F00001 220041208A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D 30010NE RIGHT SHUTDOWN E KC8AO OTHER RYJPARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TXTAXI/GRND HDL 1 GL23227CK 227 245399 RT ENGINE ROLLED BACK AND SHUTDOWN WHEN CAPTAIN ADVANCED THE POWER LEVERS. PILOT TAXIED BACK TO HANGAR. PERFORMED ENGINE RUNS AND PERFORMANCE CHECKS IAW GE MANUAL SEI-187. COULD NOT DUPLICATE PROBLEM. CHECKED ENGINE FUEL FILTERS AND CLEANED, PERFORMED OVERSPEED GOVERNOR BYPASS CHECK. PERFOMRED GENERAL INSPECTION OF ENGINE, FUEL SYSTEM AND CONTROLS. PERFORMED HIGH SPEED TAXI CHECKS. NO DEFECTS NOTED. AIRCRAFT TEST FLIGHT WAS PERFORMED WITH NO DEFECTS OR ABNORMAL OPERATIONS NOTED. (K) 2L72 4F4 F A7EU E7EA 20050330001302005033000130CE 2005 3 30 GNB2005F00000 120041018A5100S10011171 LINE CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO CRACKED E GNBAK NONE O OTHER ININSP/MAINT 1 SW01402MQ 402C0095 CRACKED PRESSURE LINE AT THE BEND. (SW01200502449) (K) 1L72 3O3 O A7CE E8CE 20050330001392005033000139NM 2005 3 30 ASA044403 120041229A5347 CARGO TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO COMPARTMENT TIE DOWN FITTINGS HAVE LIGHT CORROSION. RBL 13.80, STA 947.5 TO 727 RBL 13.8. (K) 2L72 4F4 FRTA16WE E21EU 20050330001472005033000147SO 2005 3 30 UQM2005F00002 220041118A7414BL500556103 MAGNETO PIPER PA28 PA28R201T 7102813SO CONT O360 TSIO360FB 17025SO ENGINE FAILED E UQMAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CE013856735 28R7703243 PILOT WAS FLYING AT 7000 FT AND LOST POWER. HE SAID ENGINE WENT TO IDLE. HE MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGINE WAS NOT RUNNING. FOUND THE MAGS BOTH LT AND RT HAVE NO SPARK. REMOVED P LEADS AND STILL NO SPARK. REPLACED CONDENSERS AND STILL NO SPARK. REMOVED MAGS FROM ENGINE AND BENCH CHECKED AND NO SPARK. THE LT MAG HAS SN LISTED ABOVE AND RT MAGS SN D04DA208R. AFTER TALKING WITH MFG AND IS WARRANTY ISSUE, CANNOT FIND CAUSE OF PROBLEM. ENGINE WAS FROM FACTORY AND INSTALLED AT 6/23/2004, AND THE MAG FAILED ON 11/13/2004 WITH 35.14 HOURS SINCE OVERHAUL. (K) 1L71 3O3 O 2A13 E9CE 20050330001602005033000160EU 2005 3 30 IJA2005F00002 120041210A78100319778440 EXHAUST PIPE AEROSPAS355 AS355N 8680818EU TMECA ARRIUSARRIUS1A NE LT ENGINE VIBRATION E IJAAK NONE O OTHER ININSP/MAINT 1 CE07912EM 5560 STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. SERVICEABLE EXHAUST PIPE WAS INSTALLED. (CE07200506287) (K) 1G72 3U3 URTH11GU E34NE 20050330001612005033000161EU 2005 3 30 IJA2005F00003 120041210A2435524061 STARTER GEN AEROSPAS355 AS355F2 8680812EU TMECA ARRIUSARRIUS1A NE LT ENGINE VIBRATION E IJAAK NONE O OTHER ININSP/MAINT 1 CE07912EM 5560 STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. (K) 1G72 3U3 U H11EU E34NE 20050330001652005033000165WP 2005 3 30 KC82005F00002 220041117A731430708507 PUMP LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP FUEL SYS FAILED E KC8AO OTHER J WARNING INDICATION CLCLIMB 1 GL2372CK 11134 165 P73250 PILOT ADVANCED THE POWER LEVER ON THE START OF HIS TAKEOFF ROLL AND THE LT ENGINE ROLLED BACK AND SHUT DOWN. FUEL PUMP FAILED FUEL DISCHARGE PRESSURE TEST DURING OUR TROUBLESHOOTING IAW MM. REPLACED FUEL PUMP WITH SERVICEABLE PUMP. PERFORMED REQUIRED ENGINE PERFORMANCE CHECKS, EEC ADJUSTMENT, MANUAL MODE ADJUSTMENT, MANUAL MODE TRANSFER, OVERSPEED SOLENOID, AND LEAK CHECKS IAW GARRETT LIGHT MAINTENANCE. (K) 2L72 4F4 F A10CE E6WE 20050330001722005033000172NM 2005 3 30 CSJ2005F00000 120041119A5210250002505 DOOR PIPER PA60 PA60600 7106001NM LYC O540 IO540* 41532EA MAIN PAX DEPARTED A CSJAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 GL2549MG 4763 600634796120 PILOT REPORTED THAT IN LEVEL CRUISE FLIGHT AFTER ENCOUTERING TURBULENCE THE CABIN DOOR OPEN LIGHT ILLUMINATED. IMMEDIATELY FOLLOWING THE LIGHT THE UPPER CABIN DOOR OPENED AND DEPARTED THE AIRCRAFT. THE PILOT EXECUTED AN EMERGENCY LANDING WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND THE FORWARD AND AFT DOOR LATCH MICROSWITCHES AND THE DOOR OPEN LIGHT WERE FOUND TO BE OPERATIONAL. THE DOOR WAS RETREIVED AND THE LATCHING MECHANISM WAS FOUND INTACT AND OPERATIONAL. (EA13200501883) (EA13200501865) 1M72 3O3 ORTA17WE 1E4 20050331000022005033100002WP 2005 3 31 ASAA0480623 120041227A53305936021505 SKIN DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, FUSELAGE GOUGED ON LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050331000032005033100003WP 2005 3 31 ASAA0580024 120040123A57303912757503 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT WING FUEL PANEL 1303, CORRODED ON LANDING. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050331000052005033100005WP 2005 3 31 ASAA0580038 120040123A532199365811 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, CABIN FLOORBOARD PANEL HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M) 2L72 4F RTA6WE 20050331000062005033100006WP 2005 3 31 ASAA0580009 120040122A5310593644315 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - FOUND HV-CHECK, MID CARGO BAY DOOR FRAME LIP SEAL WAS FOUND BENT AND DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR SPLICE AND DOUBLER. (M) 2L72 4F RTA6WE 20050331000092005033100009WP 2005 3 31 ASAA0580030 120040123A53475930566115 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, SEAT TRACK CORRODED. REPLACED SEAT TRACK. (M) 2L72 4F RTA6WE 20050331000102005033100010WP 2005 3 31 ASAA0580031 120040123A532059360717 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LONGERON 29L INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050331000122005033100012WP 2005 3 31 ASAA0580032 120040123A531199360734 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, FRAME LOWER FLANGE IS CORRODED. REPLACED FRAME. (M) 2L72 4F RTA6WE 20050331000132005033100013WP 2005 3 31 ASAA0580025 120040123A575359100433 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RIGHT OUTBOARD FLAP INBOARD VANE L/E IS CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050331000142005033100014WP 2005 3 31 ASAA0580026 120040123A5730ARB0872515 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV CHECK, RIGHT WING FUEL ACCESS PANEL, FOR BOOST PUMP, IS CORRODED AROUND FASTENERS. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050331000152005033100015WP 2005 3 31 ASAA0580019 120040123A55435940508 TAB DOUG DC9 DC983 3022083WP RUDDER DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RUDDER TAB IS DELAMINATED AT BASE WEDGE. BOND REPAIRED. (M) 2L72 4F RTA6WE 20050331000172005033100017WP 2005 3 31 ASAA0580004 120040122A53219936581 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, TWO CABIN FLOORBOARDS WERE FOUND TO HAVE CORRODED AND INSERTS FROM FS 541-617 AND BUTTOCK LINES L22 TO R22. BOTH PANELS WERE REPLACED. (M) 2L72 4F RTA6WE 20050331000182005033100018WP 2005 3 31 ASAA0580018 120040123A55235910414 TAB DOUG DC9 DC983 3022083WP RT ELEVATOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RIGHT ELEVATOR GEAR TAB UPPER SURFACE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050331000192005033100019WP 2005 3 31 ASAA050027 120040123A523059364351 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR DENTED JUST BELOW TOP EDGE. RECONTOURED DOOR SKIN AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050331000202005033100020WP 2005 3 31 ASAA0580037 120040123A53219936651515 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, CABIN FLOORBOARD HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M) 2L72 4F RTA6WE 20050331000212005033100021WP 2005 3 31 ASAA0580001 120040121A5321 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, FOUND CABIN FLOORBOARDS WERE FOUND DELAMINATED AT 25 DIFFERENT LOCATIONS FROM FUSELAGE STATION 148 TO 1250 AND BUTTOCK LINES L45 TO R50. DAMAGED FLOORBOARDS WERE REMOVED AND REPLACED IN ALL CASES. 2L72 4F RTA6WE 20050331000252005033100025WP 2005 3 31 ASAA0480626 120041227A523059101413 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. RECONTOURED DOOR SKIN AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050331000262005033100026WP 2005 3 31 ASAA0580005 120040122A532199366391 FLOORBOARD DOUG DC9 DC983 3022083WP CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - FOUND HV-CHECK, CABIN FLOORBOARD WAS FOUND TO BE DELAMINATED, WITH CRACKED 'W' CHANNEL. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050331000272005033100027WP 2005 3 31 ASAA0580013 120040123A5230591014125 STRUCTURE DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY DOOR CORRODED AT SEVERAL SLEEVE AND EXPANDER POINTS. REMOVED DAMAGED SECTIONS. INSTALLED REPAIR DOUBLERS. (M) 2L72 4F RTA6WE 20050331000292005033100029WP 2005 3 31 ASAA0580035 120040123A5330591140659 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FUSELAGE SKIN DENTED. RECONTOURED SKIN WITH REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050331000312005033100031WP 2005 3 31 ASAA0580020 120040123A575499359405 SKIN DOUG DC9 DC983 3022083WP TE FLAP GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT INBOARD FLAP LOWER SURFACE GOUGED. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329001772005032900177NE 2005 3 29 AWXA200400970 220040902A73205009392 SPUR GEAR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 ENGINE GALLED A AWXACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP28620AW 052 0288 ABORT T/O, NR 1 ENG ROLLED BACK TO IDLE WHEN BRAKES RELEASED. PRIOR, NR 1 ENG SHUTDOWN WHEN THROTTLES ADV & BRAKES RELEASED. INSP INLET & EXHAUST, BITE TEST OF CFDS & FADEC 1A&1B, HI PWR ENG RUN GOOD. *S/D* 10TH STG SOLENOID VLV INPUT LINE HAND TIGHT, TORQUED LINE. REPLACED NR 1 ENG DEDICATED ALTERNATOR, FMU, LO/HI PRESS FUEL PUMP & FUEL FILTER. *S/D* VENDORS TEST OF FUEL PUMP CONFIRMED FAILURE OF UNIT FOR FUEL FLOW ERODED BEYOND LIMITS. BEARINGS WORN & PUMP CAVITATED. REPLACED CARBON FACE SEALS, 3 BEARINGS & GEAR ASSY. TEST OF FMU FAILED SET POINTS OF CALIBRATION CURVE DUE TO LOSS OF METERING VLV SPILL PRESS. MV MOTOR FILTER BLOCKED & RECEPTACLES CONTAM BY FUEL, REPLACED FILTER & RECEPTACLES. 2L72 4F4 FRTA28NM E311NE 20050330000542005033000054SW 2005 3 30 ALG2005F00005 120041129A6320406040058109 MANIFOLD BELL 407 407 1182206SW ALLSN 250C 250C47B GL XMSN OIL FILTER DAMAGED E ALGAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW03587AL 53248 AFTER LANDING AT SS69 PASSENGER INFORMED THE PILOT THERE WAS OIL ALL ALONG THE SIDE OF THE AIRCRAFT. SHUTDOWN AND CHECKED THE TRANSMISSION OIL LEVEL AND THE SIGHT GLASS WAS EMPTY. MAINTENANCE REMOVED AND REPLACED THE MAIN TRANSMISSION EXTERNAL OIL FILTER MANIFOLD ASSEMBLY BECAUSE TEMPERATURE BULB INSERT WAS DAMAGED CAUSING LEAK. GROUND RUN AND LEAK CHECK WAS GOOD, AIRCAFT RETURNED TO SERVICE. (K) 1G71 3U3 UO H2SW E1GL 20050330000552005033000055EU 2005 3 30 KBM2005F00005 120041201A7931704A37642043 TRANSDUCER SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE ENGINE OIL FAILED E KBMAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP1953SH 73 2009 TRANSDUCER, NO INDACATED OIL PRESSURE AT START-UP. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050330000602005033000060WP 2005 3 30 ASAA0480485 120040825A3244 TIRE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE MLG FAILED A ASAAK NONE O OTHER ININSP/MAINT 1 SO27931AS 49232 DURING LANDING ROLL, BOTH LT MLG TIRES RUPTURED. THE MLG STRUT DID NOT COLLAPSE, BUT SOME FUSELAGE DAMAGE WAS CAUSED BY FLYING PIECES OF TIRE MATERIAL. (AN O-53 FLIGHT IRREGULARITY/HAZARD REPORT HAS BEEN FILED AS HAS A PRELIMINARY ENGINEERING REPORT). THE POS-1 TIRE HAD BEN RETREAD 3 TIMES, POS-2 TIRE, 1 TIME. AIRCRAFT DAMAGE WAS REPAIRED AS REQUIRED. PIECES HAVE BEEN SENT TO MFG FOR ANALYSIS. (K) 2L72 4F4 F A6WE E9NE 20050330000832005033000083WP 2005 3 30 O3X04129212 220041213A72618650954 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C653 NE LT ENGINE LEAKING A O3XAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO03921AE2973 2973 921 P66262C AIRCRAFT WAS ENROUTE, WHEN THE LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED, THE OIL PRESSURE STARTED TO DROP AND THE OIL TEMPERATURE INCREASED. THE ENGINE WAS SHUT DOWN AND THE AC RETURNED WITHOUT FURTHER PROBLEMS. OIL WAS LEAKING FROM THE REAR TURBINE BEARING AND SCAVENGE PUMP SEAL. ENGINE CHANGE IN PROGRESS. ENGINE WILL BE SHIPPED TO MFG FOR EVALUATION AND REPAIR. (K) 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20050330000882005033000088 2005 3 30 S2YA04011 420040428A3417D60286 MODULE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE ADC FAILED A S2YAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL1385SK 14435 UE85 BEFORE FLIGHT, THE CREW NOTED THE TAWS FAILED RIGHT AFTER REACHING TAKE-OFF POWER. THE CREW ABORTED THE TAKE-OFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND COULD NOT CLEAR AN (ADC 1 INVALID) MESSAGE ON THE TAWS. MX REPLACED THE AIR DATA MODULE AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (D) 2L72 4T4 TRTA24CE E26NE 20050330000932005033000093NM 2005 3 30 S2YA04022 120040620A2421230GC02Y03 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE LT GENERATOR INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13356SK 837 3163 DURING TAKEOFF FLIGHT, THE CREW NOTED A CAS MESSAGE FOR LT GENERATOR FAIL. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE 1VE PANEL. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050330000962005033000096CE 2005 3 30 S2YA04028 120040830A79311013890235 TRANSDUCER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT OIL PRESS MALFUNCTIONED A S2YAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1387SK 21443 UE87 AFTER TAKEOFF OF FLIGHT, THE LT ENGINE`S OIL PRESSURE GAUGE PEGGED OUT AT MAX PSI (ABOUT 200 PSI). THE CREW MADE AN AIR-TURN-BACK. MX INSPECTED THE AC AND REPLACED THE LT OIL PRESSURE TRANSDUCER. MX OPS CHECK THE SYSTEM FOUND NO FURTHER DISCREPANCIES AND RETURN THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050331000282005033100028WP 2005 3 31 ASAA0580033 120040123A53219957826503 FLOOR PANEL DOUG DC9 DC983 3022083WP CABIN PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, COCKPIT FLOOR PANEL PUNCTURED. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050331000752005033100075EA 2005 3 31 COMA0560204 120040328A304016591 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA WINDOW HEAT FAULTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01812CA13101 7381 FLIGHT 5480 RECEIVED A LEFT WINDOW HEAT CAUTION DURING CLIMBOUT OF GSO, AIRCRAFT RETURNED TO THE FIELD. FERRIED THE AIRCRAFT TO MCO, REPLACED THE WINDOW HEAT CONTROLLER. 2L72 4F RTA21EA 20050401000182005040100018EU 2005 4 1 KBM2005F00015 120040216A2150050143 MOTOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE EVAPORATOR INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19230SH3691 2337 5 INCH AFT EVAP MOTOR, INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050401000192005040100019EU 2005 4 1 KBM2005F00016 120040218A6510350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR TORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19230SH728 2337 T/R LAMINATED BEARING, TORN, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050401000292005040100029EU 2005 4 1 KBM2005F00017 120040227A21500500844 BLOWER SNIAS 350 AS350B2 8680813EU AIR CONDITIONER INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19751H 3403 AIR CONDITIONER BLOWING AMBIENT TEMP, AIR ONLY, REMOVED AND REPLACED.(K) 1G71 3U H9EU 20050401000412005040100041EU 2005 4 1 KBM2005F00026 120040222A6510350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE TAIL ROTOR CRACKED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM7967 2167 CRACKED .6666 THE WAY DOWN THE NUT SIDE OF FORK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050401000472005040100047EU 2005 4 1 KBM2005F00024 120040220A6720350A33214501 PITCH LINK SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19115SH 3141 TAIL ROTOR PITCH LINK ROD HAS SILENT BLOCK HAS V-CRACK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050401000542005040100054EU 2005 4 1 KBM2005F00031 120040115A6510350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR FAILED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19884SH 2884 LAMINATE BEARINGS, VIBRATION FELT IN TAILROTOR AT NG 65->70 PERCENT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050401000822005040100082EU 2005 4 1 KC82005F00005 120041112A2711 CONTROL PANEL AMD FALCONFALCON20 2730103EU GE CF700 CF700* 30010NE AILERON TRIM STUCK E KC8AK NONE O OTHER ININSP/MAINT 1 GL23192CK 192 WHEN PILOT ACTIVATED THE AILERON TRIM, THE TRIM CONTROL STUCK AND RAN TOWARDS FULL TRAVEL AND POPED CIRCUIT BREAKER. FOUND AILERON TRIM CONTROL STUCK ON IN THE TRIM CONTROL PANEL. REPLACED TRIM CONTROL PANEL WITH SERVICEABLE TRIM CONTROL PANEL. ALL WORK PERFORMED IAW MM. 2L72 4F4 FRTA7EU E7EA 20050110000142005011000014SO 2005 1 10 SWIA200414218 120041101A5320 BUTTPLATE EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 FS 13 TO 21 AT YN479 BUTT PLATE IS CORRODED ON UPPER SURFACE, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-25-00, 51-40-02. 2L72 4T RTA31SO 20050110000162005011000016SO 2005 1 10 SWIA200414228 120041101A5534 ANGLE EMB 120 EMB120ER 3260203SO VERTICAL STAB CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 RIGHT FUSELAGE VERTICAL STAB CLOSING ANGLE IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. RT FUSELAGE TO VERTICAL STAB CLOSING ANGLE REPAIRED IAW EMB EO SST128099 2L72 4T RTA31SO 20050110000172005011000017EA 2005 1 10 SWIA200414171 120041201A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07432SW 7548 EMERGENCY EXIT CEILING POD LIGHT BURNED OUT. RELAMPED , OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000182005011000018EA 2005 1 10 SWIA200414172 120041205A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07929SW 7703 FLAPS FAIL CAUTION MESSAGE SELECTING FLAPS 0 TO 8. REPLACED NR 1 AND NR 4 ACTUATORS. RIGGED FLAPS IAW AMM 27-51-10, OPERATIONAL CHECK GOOD. PN 852D100-19 SN OFF 4187 PN 854D100-20 SN OFF 2195. 2L72 4F RTA21EA 20050110000192005011000019EA 2005 1 10 SWIA200414189 120041118A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16. 2L72 4F RTA21EA 20050110000212005011000021SO 2005 1 10 SWIA200414200 120041101A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 FLOOR SUPPORT ANGLE, STR 15, RT FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FLOOR SUPPORT IAW EMB 120 SRM 51-25-00, 51-40-02. 2L72 4T RTA31SO 20050110000252005011000025EA 2005 1 10 SWIA200414177 120041118A5320 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FUSELAGE UPPER FLANGE ON TRANSVERSE BEAM IS CRACKED; FS 280.00, RBL 9.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 60R53-11-13 REV "NC" RII 53-401. 2L72 4F RTA21EA 20050110000262005011000026EA 2005 1 10 SWIA200414178 120041118A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 PAX DOOR FORWARD AND AFT LOWER CORNERS FRAMES CORRODED, ITEM FOUND AT C-CHECK INSPECTION. CORNER FITTINGS REPLACED IAW CRJ REO 601R52-11-0600, REO 601R-52-11-583. 2L72 4F RTA21EA 20050110000272005011000027EA 2005 1 10 SWIA200414179 120041118A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 FUSELAGE; PULLEY INTERTCOSTAL HAS A CRACKED REMOTE ANGLE FS 484.00; LBL-27.0, ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ REO 601R53-41-059 REV "A" . 2L72 4F RTA21EA 20050110000312005011000031EA 2005 1 10 SWIA200414231 120041207A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07595SW3960 3960 7292 SPOILERONS FAULT STATUS MESSAGE JUST AFTER TAKEOFF. REMOVE AND REPLACE NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000322005011000032EA 2005 1 10 SWIA200414232 120041203A2720C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA RUDDER MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07710SK 10170 RUDDER LIMIT FAULT STATUS MESSAGE. REMOVED AND REPLACED SSCU IAW AMM 27-61-05. TESTED IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000352005011000035EA 2005 1 10 SWIA200414181 120041118A5320 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 VERTICAL BEAM AT FS 409+128 RBL 27 INBOARD SIDE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV. "C". 2L72 4F RTA21EA 20050110000372005011000037SO 2005 1 10 SWIA200414204 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 CENTER BUTTSTRAP FROM FRAME 39-44 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02 AND 51-25-00. 2L72 4T RTA31SO 20050110000382005011000038SO 2005 1 10 SWIA200414213 120041101A5753 STRINGER EMB 120 EMB120ER 3260203SO LT FLAP CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LEFT NACELLE FLAP, UPPER SURFACE, INTERNAL STRINGER CRACKED, ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW EMB 120 SRM 51-25-00, 51-12-02, 51-30-01, 51-40-02, 57-50-02. 2L72 4T RTA31SO 20050110000392005011000039SO 2005 1 10 SWIA200414219 120041101A5320 BUTTPLATE EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 FS 13 TO 21 AT YN479 BUTT PLATE IS CORRODED AT SEVERAL LOCATIONS ON TOP SURFACE, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTPLATE IAW EMB 120 SRM 51-25-00, 51-40-02. 2L72 4T RTA31SO 20050110000402005011000040SO 2005 1 10 SWIA200414220 120041101A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 INTERCOSTAL BETWEEN CENTER FLOORBEAM AND RIGHT FLOORBEAM 479.00 AT FRAME 38 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW EMB 120 SRM 51-40-02, 51-40-04 AND 51-25-00. 2L72 4T RTA31SO 20050110000412005011000041SO 2005 1 10 SWIA200414214 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LEFT BUTT STRAP AT Y479.00L FROM FS 21 TO FS 26 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) BLENDED AND ASSESSED CORROSION IAW EMB 120 SRM 53-20-10, FOUND TO BE WITHIN LIMITS. DEPTH, .004. REPROTECTED AREA IAW SRM 51-21-02 AND AMM 20-30-05. 2L72 4T RTA31SO 20050110000422005011000042EA 2005 1 10 SWIA200414193 120041118A5514 WEB CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 LEFT HORIZONTAL STAB WEB CRACKED FROM LIGHTNING HOLE AT LBL 58.92 AND STRINGER NR 2, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT HORIZONTAL STAB, WEB AT LBL 58.92 AND STRINGER NR 2, IAW CRJ REO 601R-55-11-136. 2L72 4F RTA21EA 20050110000452005011000045EA 2005 1 10 SWIA200414241 120041206A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA LT SPOILERON MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07924SW7092 7092 7681 "SPOILERONS FAULT" STATUS MESSAGE ON TAXI. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000472005011000047EA 2005 1 10 SWIA200414183 120041118A5210 RISER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 PAX DOOR SILL RISER CORRODED IN SEVERAL LOCATIONS. (ITEM FOUND AT C-CHECK INSPECTION.) AFFECTED AREAS REPAIRED IAW CRJ SRM 53-21-23 2L72 4F RTA21EA 20050110000492005011000049SO 2005 1 10 SWIA200414207 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 BUTT STRAP AT Y479.00 FROM FRAME 34-39 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02, 51-25-00. 2L72 4T RTA31SO 20050110000502005011000050EA 2005 1 10 SWIA200414191 120041118A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 AFT EQUIPMENT COMPARTMENT FRAME IS CRACKED; FS 640.00 STR 9R, ITEM FOUND AT C-CHECK INSPECTION. FRAME REPAIRED IAW REO 601R-53-61-557 REV NC. 2L72 4F RTA21EA 20050110000512005011000051EA 2005 1 10 SWIA200414192 120041118A5514 FITTING CNDAIRCL600 CL6002B19 1900309EA HORIZ STAB CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07410SW 7066 HORIZONTAL STAB ANTI-ROTATION FITTING CORRODED, ITEM FOUND AT C-CHECK INSPECTION. HORIZONTAL STAB ANTI-ROTATION FITTING REPLACED IAW SB 601R-55-007. 2L72 4F RTA21EA 20050110000532005011000053SO 2005 1 10 SWIA200414206 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 BUTT STRAP CENTER FROM FRAME 34-39 IS CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-25-00 & 51-40-02. 2L72 4T RTA31SO 20050110000552005011000055EA 2005 1 10 SWIA200414245 120041211A5610 WINDOW CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07416SW 7089 PILOTS SIDE WINDOW CRACKED IN LOWER AFT CORNER. REPLACED LEFT SIDE WINDOW IAW 56-12-01, PN OFF 601R3033-3, SN OFF 9517349897. 2L72 4F RTA21EA 20050110000582005011000058EA 2005 1 10 SWIA200414175 120041126A2752853D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA T/E FLAP FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07442SW 7609 FLAP FAIL MESSAGE INTO SLC. REPLACED L3, L2, R3 FLAP ACTUATOR IAW 27-53-01 AND 27-53-05. PN 853D100-19 SN OFF 1847: PN 853D100-20 SN OFF 1828: PN 852D100-19 SN OFF 3182AB. 2L72 4F RTA21EA 20050110000592005011000059EA 2005 1 10 SWIA200414176 120041130A7120 YOKE CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 LEFT ENGINE FORWARD MOUNT YOKE CORROSION FOUND ON BEARING SURFACES. REMOVED AND REPLACED FORWARD LEFT ENGINE YOKE MOUNT ASSEMBLY REF 71-21-01. 2L72 4F RTA21EA 20050110000602005011000060EA 2005 1 10 SWIA200414242 120041212A2740 TRIM SWITCH CNDAIRCL600 CL6002B19 1900309EA COCKPIT INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07426SW 7468 FO'S STAB TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050110000622005011000062EA 2005 1 10 SWIA200414244 120041212A27604916406 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA RT SPOILERON MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07403SW713 713 7028 SPOILERONS FAULT STATUS MESSAGE. REPLACED RIGHT INBOARD SPOILERON PCU IAW MM 27-62-01. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD, PN 27000-7, SN OFF 3779. 2L72 4F RTA21EA 20050110000632005011000063EA 2005 1 10 ZJW2004F00001 220040914A853060828 CAP IO540E1A5 GULSTM500 500B 0141106SW LYC O540 IO540E1A5 41532EA NR 5 CYLINDER OUT OF POSITION E ZJWAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 CE05127KH L2706A8 102738 L2706A8 NR 5 CYLINDER WRIST PIN CAP ROLLED UP IN PISTON. CAUSE METAL FRAGMENTS IN OIL SCREEN. RESTRICTED OIL FLOW TO GOVERNOR. CAUSED DROP IN RPM. ENGINE WAS FEATHERED AND LANDED SAFETY. 1H72 3O3 O 6A1 1E4 20050110000662005011000066NE 2005 1 10 Y2PA04032 220041208A7200CF7002D ENGINE AMD FALCONFALCON20 2730103EU GE CF700 CF7002D2 30010NE NR 1 FLAMED OUT E Y2PAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 GL23826AA8276 4821 67 NR 1 ENG FAILED (FLAMED OUT) AT 36,300 FT IN CLIMB TO 36,500 FT. CREW ATTEMPTED RE-LIGHTS AT 29,000, 24,000, AND 19,000 TO NO AVAIL. CREW DECLARED EMER, RETURNED TO DEPART, LANDED WITHOUT INCIDENT. AC WAS IN EXPERIMENTAL CONFIGURATION FOR RVSM TESTING. MAINT INSPECTED THE NR 1 ENG FOR FOD, WITH NO DEFECTS NOTED. FLAMEOUT INSP WAS PERFORMED IAW MM. OVERSPEED GOVERNOR WAS REPLACED DUE TO LEAKING. T2 SENSE LINE WAS REPLACED DUE TO BEING CRUSHED. LEAK AT THE FUEL FLOW TRANSMITTER WAS REPAIRED BY RESEALING. ENGINE WAS RUN, LEAK AND OPERATIONAL CHECKS SHOWED NO DEFECTS. NR 1 ENG FLAMED OUT DURING TEST. RETURNED, LANDED WITHOUT INCIDENT. ENGINE WAS REPLACED, RUN UP WITH NO DEFECTS, AC RETURNED TO SERVICE.2L72 4F4 FRTA7EU E7EA 20050110000702005011000070NM 2005 1 10 USAA041031 120041124A575165C2591111A SPAR BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT AILERON DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU53047 23700 PIT - Q2 - SPAR, 2 INCHES X 1 INCH AREA, COMPOSITE DAMAGE/ DELAMINATION, LT AILERON, LEADING EDGE SPAR 34 INCH FROM OB END, UPPER FLANGE. INSTALLED REPAIR PLYS AND EXTRA IAW EA AND SRM. 2L72 4F4 FRTA16WE E21EU 20050110000742005011000074EU 2005 1 10 USAA041013 120041111A5320 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 2 INCHES X 2 INCHES X .050 INCH AREA, CORROSION; LEVEL 1; TASK NR JA-220-53500; MAIN CABIN FLOOR AT FR 16, BL-Y765. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-14, 51-42-11, 53-11-14. 2L72 4F4 FRTA28NM E37NE 20050110000752005011000075EU 2005 1 10 USAA041014 120041201A5320D5348004320501 SILL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - SILL, 1.5 INCH X 1 INCH X .070 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-001, MAIN CABIN FLOOR, FR 67, Y1732. REMOVED AND REPLACED SILL IAW SRM 53-41-14. 2L72 4F4 FRTA28NM E37NE 20050110000762005011000076EU 2005 1 10 USAA040991 120041117A5320D5348004320401 SILL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - SILL, BLENDED AREA 3 INCHES X 1.25 INCH X .06 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-001; R-2 DOOR SILL FORWARD FLANGE FR66, Y1482. REPLACED SILL IAW SRM 51-42-00, 51-74-00, 53-41-14. 2L72 4F4 FRTA28NM E37NE 20050110000772005011000077EU 2005 1 10 USAA041011 120041110A5347D5311282600101 DUMMY RAIL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - DUMMY RAIL, 6 INCH X 1.250 INCH X .070 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN FLOOR Y 503.2, BTW FR 12 AND FR 16. 2L72 4F4 FRTA28NM E37NE 20050110000792005011000079EU 2005 1 10 USAA040998 120041113A5320D5361019720140 STRAP AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - STRAP, .012 INCH X 1.19 INCH X 1.9 INCH AREA, CORROSION; MAIN CABIN FLOOR PANEL; DEFECTIVE PART REPLACED WITH IDENT PART IAW AMM. 2L72 4F4 FRTA28NM E37NE 20050110000812005011000081NM 2005 1 10 USAA041044 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 2 INCH AREA OF DAMAGE, RUDDER LT SIDE 98.5 INCH FROM BOTTOM AND 9.25 INCHES FROM L/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110000822005011000082EU 2005 1 10 USAA041019 120041124A5347D5311282600101 DUMMY RAIL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - DUMMY RAIL, 2 INCHES X 2 INCHES X .125 INCH AREA; CORROSION; LEVEL 2; NR JA-220-53500, MAIN CABIN FLOOR AT FR 16, BL 503.2. REMOVED AND INSTALLED NEW DUMMY RAIL IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110000862005011000086EU 2005 1 10 USAA041006 120041112A5321D5361060500100 FLOOR PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - FLOOR PANEL, .017 INCH X 1.3 INCH X 1.2 INCH AREA; CORROSION; R1 DOOR Y1732 - Z240, FR 16 AND FR 20. INSTALLED NEW PART IAW AMM 53-74-00, 53-12-00. 2L72 4F4 FRTA28NM E37NE 20050110000872005011000087NM 2005 1 10 USAA040979 120041118A575465C226603157 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU L/E SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - NR 3 SLAT, 6 INCH X 6 INCH AREA, CRACKED AND DISBONDED AT IB LOWER T/E. REMOVED SKIN AND CORE, REPLACED CORE AND REPAIR PLYS IAW SRM 51-70-10 AND EA 70537. 2L72 4F4 FRTA16WE E21EU 20050110000882005011000088NM 2005 1 10 USAA041046 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - TOP COMPOSITE LAYER, 2 INCHES X 1 INCH AREA DAMAGE, RUDDER LT SIDE 95.5 INCHES FROM BOTTOM AND 20 INCHES FWD OF T/E. PREPARED AREA, LIGHT SANDING, INSTALLED MULTI LAYER REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110000892005011000089EU 2005 1 10 USAA040993 120041117A5320D5361019900142 SUPPORT ANGLE AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - SUPPORT ANGLE, 3 INCHES X 2 INCHES X .020 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 20, Y1584. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 53-11-14. 2L72 4F4 FRTA28NM E37NE 20050110000922005011000092EU 2005 1 10 USAA040965 120041030A5315D5347217220400 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - FLOORBEAM- 2 INCHES X 1.5 INCHES X .04 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500-012, Y1292, BTW C68 AND C69 MAIN CABIN FLOOR. REMOVED AND REPLACED FLOOR BEAM IAW SRM 53-00-14, SRM 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110000942005011000094EU 2005 1 10 USAA040969 120041103A5320D5348004320501 SILL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 PIT - S1 - SILL, 1 INCH X 1 INCH X .07 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-006; CABIN FLOOR, R-2 DOOR SEAL ASSY ON CROSSBEAM C66 AND AFT ENDI OF FRAME - Y1732. REPLACED DOOR SEAL IAW SRM 51-74-00, 53-41-14, 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110000952005011000095EU 2005 1 10 USAA040985 120041112A5321D5367180500500 FLOOR PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - PANEL, 0.020 INCH X 2.8 INCH X 1.7 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53100; L2 ENTRY DOOR, FLOOR PANEL NR 261FF, +Y1732, Z240 FR 66-68. INSTALLED NEW PANEL IAW SRM 53-12-12, 53-12-00. 2L72 4F4 FRTA28NM E37NE 20050110000982005011000098EU 2005 1 10 USAA041004 120041115A5315D5347217220390 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 2 INCHES X 1 INCH X .035 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FLOORBEAM BTW FR 66-68, BTW BL Y-1162 AND Y-1292. REMOVED AND REPLACED BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2L72 4F RTA28NM 20050110001002005011000100EU 2005 1 10 USAA041008 120041111A5320D53471124200 SHEAR WEB AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - SHEAR WEB, 7 INCHES X 3 INCHES X .02 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 BTW FR 69 AND FR 70, BTW BL +Y1162 AND Y1262. INSTALLED NEW SHEAR WEB IAW SRM 51-74-00, 53-41-17, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001032005011000103EU 2005 1 10 USAA041007 120041111A5320D5347219320000 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 1 INCH X .075 INCH X 08 INCH AREA, CORROSION; LEVEL 2; TASK NR FA-260-53500, MAIN CABIN FLOOR BTW FR 67 AND FR 68, BL Y765. INSTALLED NEW BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001072005011000107EU 2005 1 10 USAA040955 120041103A5320 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - FLOOR SUPPORT, 2 INCH X 3 INCH X 0.075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR - Y254 BET FR 16 AND 20. FABRICATED PARTS IAW SRM 53-00-14 FIG 206 PR SRM 53-11-14, 51-74-00, 53-14-00, 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110001082005011000108NM 2005 1 10 USAA040976 120041116A53206548607181 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19515AU52779 23701 PIT - C5 - SUPPORT ANGLE, 1 INCH LONG CRACK AT STA 540 S - 22L. SPLICE ANGLE IAW TYP REP 53-50-03. 2L72 4F4 FRTA16WE E21EU 20050110001162005011000116EU 2005 1 10 USAA041021 120041127A5320D5367180500400 PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - PANEL, 1.250 IN X .750 INCH X .005 INCH AREA. CORROSION; LEVEL 1, TASK NR JA-260-53100; L2 ENTRY PNL NR 261 FF - NUMEROUS AREAS. REMOVED AND REPLACED WITH NEW PANEL IAW SRM 51-74-00, 53-12-00. 2L72 4F4 FRTA28NM E37NE 20050110001192005011000119EU 2005 1 10 USAA041017 120041126A5320D5311278220201 FLOOR SUPPORT AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - CABIN FLOOR SUPPORT, 3 INCH X 1 INCH X .040 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y1292, MAIN CABIN FLOOR SUPPORT. INSTALLED DOUBLER AND FILLER REPAIR IAW SRM 53-11-15, FIG 203. 2L72 4F4 FRTA28NM E37NE 20050110001202005011000120EU 2005 1 10 USAA041010 120041110A5315D5347209200000 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - FLOORBEAM, 2 INCH X 1 INCH X .024 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, AFT CABIN AREA Y765, FR68. REMOVED AND REPLACED IAW SRM 51-42-11, 51-74-00, 53-00-14. 2L72 4F4 FRTA28NM E37NE 20050110001222005011000122EU 2005 1 10 USAA041020 120041127A5320D5367180500500 PANEL AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - PANEL, .375 INCH X .750 INCH X .12 INCH AREA; CORROSION; LEVEL 1; TASK NR JA-260-53100, R2 ENTRY PANEL NR 262FF - NUMEROUS AREAS. REMOVED AND REPLACED WITH NEW PANEL IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050110001232005011000123NM 2005 1 10 USAA040987 120041201A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19590US51084 23935 CLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01. 2L72 4F4 FRTA16WE E21EU 20050110001242005011000124NM 2005 1 10 USAA040971 120041111A5730 DOUBLER BOEING737 737301 1384611NM CFMINTCFM56 CFM563B1US GL RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - DOUBLER, .25 INCH LONG CRACKS (2 EA), RT WING FUEL PANEL REBATE PANEL NR 8817R. INSTALLED EXT DOUBLER .125 THICK IAW EA 79453. 2L72 4F4 FRTA16WE E2GL 20050110001252005011000125NM 2005 1 10 USAA040978 120041118A575465C26603157 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 3 SLAT BULGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - NR 3 SLAT, 1 INCH X 2 INCH BUBBLE IN SKIN, T/E AT SKIN JOINT 12 INCHES FROM IB END. REMOVED DAMAGE, INSTALLED FILLER AND REPAIR PLYS IAW SRM 51-70-10, EA 79537. 2L72 4F4 FRTA16WE E21EU 20050110001272005011000127EU 2005 1 10 USAA040992 120041119A5315D5347217220400 FLOORBEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW 1033 BFM - S1 - BEAM, 2 INCH X 2 INCH X 0.02 INCH CORRODED AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BEAM BTW, FR 66-68, BL Y 1162-Y1292. REMOVED AND REPLACED BEAM IAW SRM 51-74-00, 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20050110001302005011000130NM 2005 1 10 USAA041029 120041205A575365C263201 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE T/E MID FLAP CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US50264 23237 PIT - RON - L/E SKIN, .5 INCH X 4 INCH CHAFE MARK, LT OB MID FLAP L/E APPROX WBL 204 LT. INSTALLED REPAIR DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E2GL 20050110001352005011000135EU 2005 1 10 USAA040961 120041028A5315D5347219320000 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - BEAM, 3 INCHES X 2 INCHES X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN DECK FLOOR RAIL, FRAME 68, -Y765. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110001362005011000136EU 2005 1 10 USAA040966 120041031A5347D53112830202 DUMMY RAIL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - DUMMY RAIL, 2 INCHES X 1 INCH X .050 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500. MAIN CABIN FLOOR @ FR 16, LB -Y81. REPLACED DUMMY RAIL IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050110001372005011000137NM 2005 1 10 USAA040967 120041109A5730 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RT WING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q6 - WING SKIN CUT OUT, 1.2500 INCH X .2500 INCH AT 4 LOCATIONS, CORROSION; NO LEVEL OR TASK, RT WING BOOST PUMP CUT OUT. REMOVED CORROSION AND INSTALLED REPAIR IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050110001382005011000138NM 2005 1 10 USAA040975 120041116A5730 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT WING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q6 - WING SKIN CUTOUT, .5 INCH X .75 INCH AT (4) LOCATIONS, CORROSION; NO LEVEL OR TASK; LT WING 7403L PANEL FUEL BOOST PUMP ACCESS AREA. REMOVED CORROSION AND REPAIRED IAW DRAFT EA 79514. 2L72 4F4 FRTA16WE E21EU 20050110001452005011000145EU 2005 1 10 USAA040960 120041030A5315D534721882 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US12260 0861 BFM - S1 - BEAM, 18 INCHES X 2 INCHES X .03 INCH AREA, CORROSION; LEVEL 2; TSK NR JA 260-53500-004, MAINT CABIN FLOOR Y1292 BET C66 AND C68. REMOVED AND REPLACED FLOORBEAM IAW SRM. 2L72 4F4 FRTA28NM E38NE 20050110001462005011000146NM 2005 1 10 USAA041052 120041123A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001472005011000147NM 2005 1 10 USAA041051 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 -RUDDER TOP LAYER, .1250 INCH X .1250 INCH X .005 INCH DEEP PIT, 8.25 INCH FWD OF T/E, 72 INCHES DOWN FROM TIP. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001492005011000149NM 2005 1 10 USAA041057 120041111A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - TOP COMPOSITE LAYER, SEVERAL AREAS 2 INCH SQUARE, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE BETWEEN STA 96 AND 121. APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001502005011000150NM 2005 1 10 USAA041038 120041111A552265C25746154 SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .50 INCH GOUGE, RT ELEVATOR AT STA 71 AND 10 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050110001512005011000151NM 2005 1 10 USAA041053 120041123A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN SURFACE, 1 INCH CHAFE WEAR, RUDDER RT SIDE L/E AT STA 170. INSTALLED REPAIR PLYS IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001522005011000152NM 2005 1 10 USAA041054 120041123A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SKIN SURFACE, 3 INCH LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178 AND 13 INCHES FROM FWD SPAR. INSTALLED REPAIR PLYS IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001532005011000153NM 2005 1 10 USAA041059 120041111A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - TOP COMPOSITE LAYER, 1 INCH X .2500 INCH AREA, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE STA 0 L/E. APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001542005011000154NM 2005 1 10 USAA041041 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION 28 INCH FWD OF T/E, 39 INCH UP FROM BOTTOM. PREPARED DAMAGED AIR, INSTALLED REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001582005011000158EU 2005 1 10 USAA040963 120041030A5347D5311282600200 DUMMY RAIL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4P NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19103US 0861 PIT - S1 - DUMMY RAIL, 2.5 INCHES X 2 INCHES X .075 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-220-53500; MAIN CABIN FLOOR FR 16, Y503.2. REPLACED DUMMY RAIL (BEAM) ALT PN INSTALLED IAW SRM 51-74-00, 53-11-14, 51-42-11. 2L72 4F4 FRTA28NM E38NE 20050110001622005011000162NM 2005 1 10 USAA041050 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - RUDDER TOP LAYER, .3750 INCH X .1875 INCH AREA, DELAMINATION, 3 INCH AFT OF NR 6 HINGE CUTOUT. INSTALLED MULTI LAYER REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001652005011000165NM 2005 1 10 USAA041042 120041115A5753654643489 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU T/E FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - UPPER AND LOWER SKIN, 3.5 INCH X 2 INCH AREA, DELAMINATION, LT IB AFT FLAP OB END UPPER AND LOWER SURFACE. REMOVED DISBONDED SKIN AND CORE MATERIAL, INSTALLED NEW CORE AND TOP SKIN DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050110001712005011000171NM 2005 1 10 USAA041037 120041111A552265C25746154A SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE, 2 GOUGES 1.25 INCHES, COMPOSITE DAMAGE, 2 GOUGES, RT ELEVATOR AT STA 70 AND 8 TO 9 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, SUPPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050110001722005011000172NM 2005 1 10 USAA041058 120041111A554265C2584151 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - TOP COMPOSITE LAYER, 3 INCHES LONG, SINGLE LAYER COMPOSITE DAMAGE, RUDDER LT SIDE AT STA 178, 13 INCHES FROM FWD SPAR. APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050110001742005011000174NM 2005 1 10 USAA041036 120041111A5522655C25746154A SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US 23555 PIT - Q4 - LOWER SKIN SURFACE, COMPOSITE DAMAGE, .3750 INCH GOUGE, COMPOSITE DAMAGE - SINGLE LAYER, RT ELEVATOR AT STA 64 + 7 INCH FROM FWD SPAR. REPAIRED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050110001792005011000179SO 2005 1 10 SIMA200432801 120041120A27403621001013 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL E/E BAY FAILED A SIMAK NONE FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW21816AE 145552 DURING CRUISE FLIGHT THE CREW REPORTED PITCH TRIM .5 INOPERATIVE. MASTER WARNING WHEN A/P DISCONNECTED MOMENTARILLY. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501202) 2L72 4F4 FRTT00011ATTE6CH 20050110001812005011000181SO 2005 1 10 SIMA200429805 120041010A532014522178005 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21730KW 145346 DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE SERVICE DOOR SILL AND INSTALLED NEW SILL IAW SRM. (SW21200501155) 2L72 4F4 FRTT00011ATTE6CH 20050110001842005011000184SO 2005 1 10 SIMA200430801 120041030A2740362100101J CONTROL UNIT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL E/E BAY MALFUNCTIONED A SIMAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SW21673AE 145797 DURING DESCENT, CREW REPORTED FAILURE OF BOTH PITCH TRIM SYSTEMS. AUTO-PILOT DID NOT DISCONNECT. CREW FOLLOWED AOM PROCEDURES AND RECOVERED BACK UP TRIM. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETUREND TO SERVICE. (SW21200501219) 2L72 4T4 FRTT00011ATTE6CH 20050110001872005011000187SO 2005 1 10 SIMA200430301 120041025A3350110049 CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21800AE 145425 MAINTENANCE REPORTED THE NR 2 AND 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK AND CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204) 2L72 4F4 FRTT00011ATTE6CH 20050110001882005011000188EU 2005 1 10 SIMA200433602 120041128A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21222NE 340B222 DURING PREFLIGHT, THE FLIGHT ATTENDENT REPORTED THE FORWARD EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 20050111000012005011100001EU 2005 1 11 ERAA098191 120040924A63204638001007 TRANSMISSION BOLKMS105 BO105S 5626006EU MAIN ROTOR MAKING METAL B ERAAO OTHER O OTHER NRNOT REPORTED 1 SW03293EH6524 559 TRANSMISSION MAKING METAL. LT PINION BREAKING DOWN, SPACER MECHANICAL DAMAGED RT PINION BREAKING DOWN, INT SHAFT ROLLER BEARING MECH DAMAGED ON INNER RACE, LT BEVEL GEAR, BREAKING DOWN. INT SHAFT BALL BEARING SCORED, ROTOR MAS BUSHING LINER DAMAGED, 5 EAQ PLANETARY AXLE BREAKING DOWN, 4 EA PLANETARY GEAR INNER RACE DAMAGED FROM METAL CONTAMINATION, 4 EA. ACTION TAKEN: DISASSEMBLED AS FAR AS NECESSARY; FOR REPAIR;. VISUALLY INSPECTED PARTS. REPLACED PARTS WORN CORRODED OR MECH DAMAGED BEYOND LIMITS. ADJUSTED ALL BACKLASHES, DISTANCES AND PATTERNS. REASSEMBLED WITH NEW O-RINGS, PROSEALED AND PAINTED. C/W 600 HOUR CLUTCH INSPECTION ON BOTH CLUTCHES. REPAIRED IAW REM 109 AND MM CHAPTER. 1G72 3U H3EU 20050111000022005011100002WP 2005 1 11 NACA20040054 120041102A7933122803 THERMOSTAT PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 1 ENGINE SHORTED A NACAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 AL03779TA358 358 P33192 45529 P33192 NR 1 ENGINE OIL TEMPERATURE CIRCUIT BREAKER POPPED, COULD NOT BE RESET. REPLACED NR 1 ENGINE OIL THERMOSTAT. LEAK AND OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20050111000062005011100006NE 2005 1 11 ERAA098181 120040726A62206515500017106 TRANSDUCER SKRSKYS61 S61N 8142104NE ENGINE INOPERATIVE B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03562EH 61257 BIM COMES ON WHEN NR IS 80 PERCENT AND GOES OUT WHEN NR IS 80 PERCENT ALL BLADE SPAR PRESSURE GOOD. CONTACTS WERE CLEANED AND ADJUSTED, CONNECTOR V/S ACTION TAKEN: INSPECTED REPAIRED ADJUSTED CONNECTOR AND O-RINGS REPLACED POST REPAIR FUNCTION TEST. 2G72 4U 1H15 20050111000072005011100007NE 2005 1 11 ERAA098182 120040715A6320A15008 BLOWER SKRSKYS61 S61N 8142104NE MAIN ROTOR BROKEN B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03564EH BLOWER SHAFT KEY BROKEN. LOOSE PULLEY ACTION TAKEN: WE HAVE SEEN THIS ON SEVERAL ERA BLOWERS YOU SHOULD POSSIBLY INITIATE AN TORQUE CHECK ON MAIN NUT OF BLOWER. 2G72 4U 1H15 20050111000122005011100012WP 2005 1 11 AALA20041257 120041229A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217528A 49920 STL - LEFT AND RIGHT AFT EMERGENCY ESCAPE HATCH LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT AFT EMERGENCY ESCAPE HATCH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000142005011100014WP 2005 1 11 AALA20041259 120041230A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW217542A 49996 DEN - OVERHEAD EMERGENCY LIGHTS AT ROW 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR OVERHEAD EMERGENCY LIGHTS AT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000162005011100016NM 2005 1 11 AALA20041261 120041226A2931 O-RING BOEING767 767323 1385205NM HYD INDICATOR BLOWN A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21378AN 25447 LAS - EN ROUTE LAX-ORD RIGHT HAND HYDRAULIC SYSTEM QUANTITY LOSS. CONFIRMED CONTINUING LOSS OF FLUID FROM .48 TO .11 INDICATED. LANDED LAS WITHOUT INCIDENT. REPLACED BLOWN OUT O-RING ON THE HYDRAULIC DIFFERENTIAL PRESSURE INDICATOR LOCATED ON THE RIGHT ENGINE HYDRAULIC SYSTEM MODULE. SERVICED HYDRAULICS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050111000172005011100017WP 2005 1 11 AALA20041262 120041228A2170 COALESCER BAG DOUG DC9 DC982 3022082WP A/C BAY DIRTY A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21471AA 49601 MCI - EN ROUTE MCI-DFW SMOKE IN CABIN. RETURNED MCI AND LANDED WITHOUT INCIDENT. CHECKED FOR HYDRAULIC AND OIL LEAKS. CHANGED COALESCER BAGS AND PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050111000252005011100025NM 2005 1 11 AALA20050007 120041226A2421 IDG BOEING757 757223 1384957NM RT ENGINE LOW A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW21188AN 32382 KOA - RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED. DISCONNECTED RIGHT GENERATOR DRIVE. SERVICED ENGINE IDG OIL TO FULL CHECKED FOR LEAKS. NONE FOUND. RAN ENGINE, NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050111000272005011100027NM 2005 1 11 AWXA200500015 120041207A57536546431280 SKIN BOEING737 7373G7 1384595NM RT FORE FLAP DEBONDED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF RT OUTBOARD FORE FLAP AFT OF A REPAIR AT INBOARD END BETWEEN WBL 212.5 LT AND WBL 217.5 LT. MAINTENANCE REMOVED DAMAGE ON UPPER SURFACE OF RT OUTBOARD FORE FLAP; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737-300 SRM 51-70-10 FIG 31. 2L72 4F RTA16WE 20050111000292005011100029NM 2005 1 11 AWXA200401463 120041207A53306545778518 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER R-2 DOOR HINGE CUTOUT IN LOWER FORWARD CORNER BS 951, LBL 66, WL 227. MAINTENANCE CUTOUT DAMAGE IN FUSELAGE SKIN AT LOWER R-2 DOOR HINGE CUTOUT BS 951, LBL 66; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH FILLERS, A DOUBLER & TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 208. 2L72 4F RTA16WE 20050111000302005011100030NM 2005 1 11 AWXA200401464 120041205A575365C263204 SKIN BOEING737 7373G7 1384595NM RT MID FLAP CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK 1 INCH CRACK WAS FOUND IN RT WING OUTBOARD MID FLAP SKIN AT LEADING EDGE, NR 8 FLAP CARRIAGE CUTOUT WBL 363.60. MAINTENANCE CUTOUT DAMAGE IN RT WING OUTBOARD MID FLAP SKIN AT WBL 363.60; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW ER 03-5754-04357-ES4. 2L72 4F RTA16WE 20050111000312005011100031NM 2005 1 11 AWXA200401465 120041215A532065458661050 WEB BOEING737 7373G7 1384595NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 MCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON MARKER BEACON ANTENNA COVER PLATE (WEB ASSEMBLY) BS 629, BL-0, 148. MAINTENANCE REMOVED CORRODED WEB ASSEMBLY AT BS 629, BL -0, 148; FABRICATED A NEW REPLACEMENT WEB ASSEMBLY PER DWG 65-45866; INSTALLED REPAIR PART IAW ER 03-5300-04364-SS2. 2L72 4F RTA16WE 20050111000372005011100037NM 2005 1 11 AWXA200500009 120041220A52106545871528 DOOR FRAME BOEING737 7373Q8 1384670NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND IN THE R-1 DOOR FRAME AT 4TH AFT DOOR STOP FROM BOTTOM BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK IN FRAME AT R-1 DOOR CUTOUT 4TH AFT DOOR STOP FROM BOTTOM; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; TREATED AREA, REPAIR ACCOMPLISHED IAW B737-300 SRM 52-10-02 FIG 101. 2L72 4F RTA16WE 20050111000382005011100038NM 2005 1 11 AWXA200500010 120041207A5315141N29321 FLOORBEAM BOEING757 7572S7 1384962NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 324, RBL 50. MAINTENANCE CUT OUT CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 324, RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM UPPER CHORD, 2 EACH SPLICE STRAPS, AND 2 EACH SPLICE REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 19-5310-04365-RC3. 2L72 4F RTA2NM 20050111000462005011100046NM 2005 1 11 AWXA200500006 120041220A2560P4010021 BATTERY BOEING737 7373Q8 1384670NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28327AW 23507 MCN - EMERGENCY EQUIPMENT - DURING C-17 CHECK THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS FOUND LOW. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20050111000582005011100058EA 2005 1 11 COMA0560001 120041222A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA 7326 LEFT HAND FS FRAME 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117. 2L72 4F RTA21EA 20050111000592005011100059EA 2005 1 11 COMA0570002 120041221A2780 SLAT CNDAIRCL600 CL6002C10 1390015EA WING MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01398CA 10112 FLIGHT 5454, SLAT FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, FOUND NO DEFECTS. REMOVED AND REPLACED DCU'S AND SLAT ACTUATORS FOR TROUBLESHOOTING. 2L72 4F RTA21EA 20050111000602005011100060EA 2005 1 11 COMA0570003 120041220A2920MM67075294001 HYDRAULIC LINE CNDAIRCL600 CL6002C10 1390015EA HYDRAULIC SYS CHAFED A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01340CA 10062 FLIGHT 5048, EDP 2A FAILED AND LOSS OF FLUID QUANTITY. REPLACED SECTION OF HYDRAULIC TUBING WHICH HAD CHAFED THRU IN THE AFT EQUIPMENT BAY. 2L72 4F RTA21EA 20050111000692005011100069EA 2005 1 11 COMA0560015 120041230A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 RIGHT HAND INTERCOSTAL AT FS 484 CRACKED. REPAIRED IAW REO 601R-53-41-059. 2L72 4F RTA21EA 20050111000712005011100071EA 2005 1 11 COMA0560012 120041229A2421 IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 LACK OF LUBE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01957CA 7109 FLIGHT 5884, NR 1 IDG CAUTION DURING T/O. SERVICED THE IDG OIL SYSTEM, OPERATIONAL CHECKS WERE SATISFACTORY. 2L72 4F RTA21EA 20050111000732005011100073EA 2005 1 11 COMA0570006 120041230A5610 WINDSHIELD CNDAIRCL600 CL6002C10 1390015EA COCKPIT LEAKING A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SO01331CA 10061 FLIGHT 5538, COPILOTS FLOOD LIGHT IS SMOKING. FOUND WATER LEAKING ONTO FLOOD LIGHT. REPLACED LIGHT AND RETORQUED WINDOW I STRAP SCREWS. 2L72 4F RTA21EA 20050111000762005011100076EA 2005 1 11 COMA0560009 120041219A5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01938CA101136348 7046 FLIGHT 5251, CO-PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20050111000792005011100079EA 2005 1 11 COMA0570001 120041221A3520 OXYGEN BOTTLE CNDAIRCL600 CL6002C10 1390015EA CABIN DISCHARGED A COMAO OTHER O OTHER CRCRUISE 1 SO01655CA 10134 FLIGHT 5113, BOTH CABIN 02 BOTTLES ARE DEPLETED. SERVICED 02 BOTTLES. 2L72 4F RTA21EA 20050111000802005011100080EA 2005 1 11 COMA0560008 120041221A5245 DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SERVICE OPEN A COMAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SO01956CA 7105 FLIGHT 5315, 02 SERVICE DOOR LEFT OPEN. INSPECTED FOR DAMAGE AND SECURED DOOR IN CLOSED POSITION. 2L72 4F RTA21EA 20050111000832005011100083EA 2005 1 11 COMA0560002 120041222A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA 7326 FS 280 IS CORRODED ON FORWARD AFT ANGLES AFT OF CREW ENTRY WAY. REPAIRED IAW REO 601R-53-11-584. 2L72 4F RTA21EA 20050111000852005011100085EA 2005 1 11 COMA0560004 120041222A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01785CA 7326 LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 10 AND 12. REPAIRED IAW EO 53-027. 2L72 4F RTA21EA 20050111000872005011100087EA 2005 1 11 COMA0560007 120041221A2751 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01409CA 7441 FLIGHT 4958, FLAPS FAIL CAUTION. COULD NOT DUPLICATE. C/W ALL REQUIRED MAINTENANCE PER AD 98-20-01. NO DEFECTS FOUND. 2L72 4F RTA21EA 20050111000902005011100090NM 2005 1 11 DL76G041153 120041229A2130 CONTROL PANEL BOEING767 7673P6 1385105NM COCKPIT FAILED A DALAO OTHER ZJ SIGNIFICANT FAILURE REPORTWARNING INDICATION CRCRUISE 1 SO27155DL 25269 CABIN AUTO INOP EICAS MSG CAME ON AS A/C WAS LEVELING OFF AT FL 370. CABIN ALT AUTO 2 AND CABIN ALT AUTO 2 STATUS MSG, AUTO INOP LIGHT ILLUMINATED ON PRESS CONTROL PANEL. REPLACED CABIN PRESSURE CONTROL PANEL. 2L72 4F RTA1NM 20050111000922005011100092 2005 1 11 DLM88041155 420041231A2210 ANNUNCIATOR DOUG MD88 MD88 3023688NM COCKPIT FAULTY A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27930DL 49717 F/O REPORTS SMOKE COMING FROM AROUND F/O FMA. REPLACED FMA. 2L72 4F RTA6WE 20050111000942005011100094NM 2005 1 11 DLM88041143 120041227A2130 WARNING SYSTEM DOUG MD88 MD88 3023688NM COCKPIT ACTIVATED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27961DL 49980 ON CLIMBOUT, THE A/C DID NOT PRESSURIZE AND CREW HAD A FLOW LIGHT. PERFORMED VISUAL INSPECTION OF THE A/C NO DEFECTS NOTED. CHECK OPERATION OF THE OUTFLOW VLV, OPS NORM. PERFORMED BITE OF THE AUTO PRESS CONTROLLER CHECK GOOD. PRESSURIZED A/C FROM APU AND ENGINE PNEUMATICS. ELECTED TO INOP THE A/C, AUTO SHUT-DOWN SYSTEM AS A PRECAUTION. 2L72 4F RTA6WE 20050111000992005011100099 2005 1 11 DL76G050003 420041229A3160341002572 CDU BOEING767 767332 1382001NM COCKPIT FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO2716065 30199 RIGHT FMS CDU FAILED IN FLIGHT AND WOULD NOT RESET. DIVERTED TO JFK. REPLACED CDU. 2L72 4F RTA1NM 20050111001002005011100100NM 2005 1 11 DLM88050004 120041230A533029525581 SKIN DOUG MD88 MD88 3023688NM FUSELAGE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27910DE 53419 FUSELAGE SKIN GOUGED ADJACENT TO A PREVIOUS REPAIR AT STATION 617 AND LONGERON 29L. REPAIRED IAW ERA 095589-14. 2L72 4F RTA6WE 20050111001132005011100113SO 2005 1 11 SWIA200414336 120041231A2731 ACTUATOR EMB 120 EMB120ER 3260203SO ELEVATOR CONTAMINATED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07299SW 120329 UPON LEVEL OFF AT 270 ELEVATOR TRIM WHEEL SPRANG FORWARD ABOUT 1/2 TURN AND AUTOPILOT KICKED OFF. INSPECTED TRIM ACTUATORS FOR BOTH ELEVATOR AND AILERON TRIM AND FOUND MOISTURE ON ALL ACTUATOR SHAFTS. CLEANED RESIDUAL MOISTURE FROM ALL ACTUATORS AND LUBRICATED AS NECESSARY. ALL CHECKS GOOD, ALL WORK PERFORMED IAW EMB MM CH 27. 2L72 4T RTA31SO 20050111001152005011100115EA 2005 1 11 SWIA200414326 120041231A2711 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA COCKPIT FAULTY A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07967SW 7872 AILERON TRIM STICKS. REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001172005011100117SO 2005 1 11 SWIA200414328 120041231A27203211001003 PCU EMB 120 EMB120ER 3260203SO RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM07212SW9036 9036 120276 RIGHT RUDDER JAMMED AFTER TAKEOFF. REMOVED AND REPLACED RUDDER PCU IAW 27-22-01. 2L72 4T RTA31SO 20050111001232005011100123EA 2005 1 11 SWIA200414306 120041213A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07460SW 7803 FUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIPS ARE CRACKED; FS 280.00, RBL 9.0 INBOARD AND OUTBOARD CLIPS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, 51-21-11. 2L72 4F RTA21EA 20050111001252005011100125EA 2005 1 11 SWIA200414308 120041222A5210 MECHANISM CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BINDING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07406SW 7030 DOOR HARD TO OPEN AND CLOSE. REMOVED AND REPLACED PAX DOOR FORWARD COUNTERBALANCE CABLES, PULLEY ASSY, TENSION STRAP, CABLE STANDOFFS, AND CABLE GUARD IN ACCORDANCE WITH CRJ AMM 52-11-17. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001272005011100127SO 2005 1 11 SWIA200414310 120041224A275012064207611 SELECTOR EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07190SW3748 3748 120050 WHEN FLAP LEVER WAS MOVED, CONTROL FAULT MESSAGE. REMOVED AND REPLACED FLAP SELECTOR IAW EMB MM 22-50-01. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001282005011100128EA 2005 1 11 SWIA200414311 120041227A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAD RETURN TO BLOCK O OTHER TOTAKEOFF 1 NM07588SW 7069 AT TAKEOFF, HEARD LOUD CRACK, RIGHT WINDSHIELD OUTER PANES BROKEN. REMOVED AND REPLACED RIGHT WINDSHIELD IAW CRJ 200 MM 56-00-00, 56-11-01, 56-12-01. OPERATIONAL CHECK GOOD. P/N: NP139321-12, S/N: 03175R71B7. 2L72 4F RTA21EA 20050111001292005011100129SO 2005 1 11 SWIA200414312 120041225A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY INTERMITTENT A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07235SW 120310 LAV SMOKE DETECTOR GOING OFF INTERMITTENTLY. REPLACED SMOKE DETECTOR. OPERATIONAL CHECKED GOOD. 2L72 4T RTA31SO 20050111001302005011100130SO 2005 1 11 SWIA200414313 120041216A492038003761 APU EMB 120 EMB120ER 3260203SO APU BAY MALFUNCTIONED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07580SW 120348 APU BLEED AIR CAUSING SMOKE IN CABIN WITH PACKS ON. REPLACED APU ASSEMBLY IAW EMB 120 MM 49-00-01 OPERATIONAL CHECK GOOD. P/N 3800376-1, S/N P-449. 2L72 4T RTA31SO 20050111001312005011100131SO 2005 1 11 SWIA200414314 120041222A2450 RCCB EMB 120 EMB120ER 3260203SO COCKPIT FAULTY A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 NM07299SW 120329 DURING INITIAL POWER UP, AN ELECTRICAL ODOR AND SMOKE DEVELOPED IN THE COCKPIT. REPLACED RCCB FOR GREEN HYDRAULIC AUX PUMP. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001322005011100132EA 2005 1 11 SWIA200414315 120041223A2760 ECU CNDAIRCL600 CL6002B19 1900309EA SPOILERON MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 NM07919SW 7657 SPOILERON FAULT STATUS MSG ON ED2 DURING TAXI OUT. REPLACED SECU NR 2 IAW 27-60-00. REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-61-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001332005011100133SO 2005 1 11 SWIA200414316 120041223A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN LOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07236SW 120312 ONE EMERGENCY LIGHT ROW 9 CAME LOOSE. REPLACED DAMAGED RED EMERGENCY FLOOR LAMP IN ROW 9 IAW 33-50-00. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001342005011100134SO 2005 1 11 SWIA200414317 120041226A27523203001005 ACTUATOR EMB 120 EMB120ER 3260203SO T/E FLAP FAILED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 NM07268UE445 445 120207 INBOARD CONTROL FAULT, ASYMMETRY FLAPS SETTING 25. REMOVED AND REPLACED RT INBOARD FLAP ACTUATOR ASSY WITH SERVICEABLE UNIT IAW 27-50-00, OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001352005011100135SO 2005 1 11 SWIA200414318 120041221A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN UNSECURE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07564SW 120339 ROW 6 EXIT PLACARD FELL OFF. INSTALLED NEW EMERGENCY LIGHT FIXTURE. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001362005011100136EA 2005 1 11 SWIA200414320 120041228A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA SPOILERON MALFUNCTIONED A SWIAC ABORTED TAKEOFF FJ FLT CONT AFFECTED WARNING INDICATION TOTAKEOFF 1 NM07925SW 7682 CONFIG SPOILERS WARNING ON T/O ROLL. ABORTED TAKEOFF. REPLACED RIGHT SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050111001382005011100138 2005 1 11 SWIA200414337 420041228A3418C818171 SENSOR EMB 120 EMB120ER 3260203SO STALL WARNING FAULTY A SWIAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM07299SW6891 5094 120329 STALL WARNING SYSTEM ALARM ON F/O SIDE ILLUMINATES WITH ASSOCIATED AURAL WARNING. REMOVED AND REPLACED SIDE SLIP SENSOR. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050111001402005011100140EA 2005 1 11 A6WA200440214 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 RT FS 625.00 OBLIQUE ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20050111001412005011100141EA 2005 1 11 A6WA200440229 120041211A2550 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CARGO BAY DETECTED A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31447AW 7812 RAMPER SMELLED BURNED PLASTIC WHEN OPENING CARGO DOOR. VISUALLY INSPECTED CARGO BAY, COULD NOT SMELL ANY PLASTIC SMELL. CARGO FAN OPS TESTED GOOD AND PERFORMED OPS TEST OF SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20050111001422005011100142EA 2005 1 11 A6WA200440231 120041221A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RIGHT FROZEN A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31433AW 7289 AFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSER, AIRCRAFT FERRIED AND PLACED ON MEL. 2L72 4F4 FRTA21EA E15NE 20050111001432005011100143EA 2005 1 11 A6WA200440225 120041219A3222 STRUT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG LACK OF LUBE A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31402AW 7281 GEAR DISAGREE UPON GEAR RETRACTION COMPLIED WITH. SERVICED NOSE STRUT WITH OIL AND NITROGEN IAW AMM. IAW AMM GEAR SWING, OPS CHECK GOOD IAW 32-30-00. 2L72 4F4 FRTA21EA E15NE 20050111001442005011100144NM 2005 1 11 ASAA0410511 120041106A53136545800197 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. 2L72 4F4 FRTA16WE E2EA 20050111001462005011100146NM 2005 1 11 ASAA0410495 120041109A53306545775558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE NICKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - NICK IN SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001472005011100147NM 2005 1 11 ASAA0410497 120041109A53306545775558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - MECHANICAL DAMAGE, 8 AREAS. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001482005011100148NM 2005 1 11 ASAA0410493 120041109A52306545775558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE AFT CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARK IN EXTERNAL SKIN AT AFT CARGO DOOR. REPAIRED AFT CARGO DOOR IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001502005011100150NM 2005 1 11 ASA0440233 120041109A5313BAC1498157 STRINGER BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 STRINGER IS GOUGED. REPAIRED STRINGER IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050111001522005011100152NM 2005 1 11 ASA0440230 120041109A5311BAC15171470 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 CRACK IN FRAME AT FASTENER FOR BIN HANGAR. REMOVED CRACK, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E21EU 20050111001542005011100154NM 2005 1 11 ASAA0410499 120041109A5320656212230 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON WEB. REPLACED WEB. 2L72 4F4 FRTA16WE E2EA 20050111001562005011100156NM 2005 1 11 ASAA0410564 120041119A53506545768233 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS AT RT FWD UPPER AND LOWER WING TO BODY FAIRING. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001572005011100157NM 2005 1 11 ASAA0410572 120041122A531165465692 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FRAME DAMAGED. REPAIRED FRAME BY INSTALLING DOUBLER. 2L72 4F4 FRTA16WE E2EA 20050111001582005011100158NM 2005 1 11 ASAA0410561 120041118A532065496096 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON AFT CARGO DOOR CUT OUT UPPER FRAME CLOSURE WEB. REPLACED UPPER FRAME CLOSURE WEB. 2L72 4F4 FRTA16WE E2EA 20050111001592005011100159NM 2005 1 11 ASAA0410571 120041122A531565549063 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON FLOORBEAM ON TOP OF LWR FLANGE LWR SURFACE. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001602005011100160NM 2005 1 11 ASAA0410554 120041116A533065458001126 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS AT SKIN LAP. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001612005011100161NM 2005 1 11 ASAA0410557 120041116A53306545800 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARK IN SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001622005011100162NM 2005 1 11 ASAA0410570 120041122A531565549062 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON FLOORBEAM ON TOP OF LWR FLANGE AROUND NUTPLATE. REMOVED CORROSION AND REPAIRED FLOORBEAM. 2L72 4F4 FRTA16WE E2EA 20050111001632005011100163NM 2005 1 11 ASAA0410529 120041112A53306545768 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT FWD WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001642005011100164NM 2005 1 11 ASAA0410555 120041116A533065458001126 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS AROUND DOUBLER, LWR FWD CORNER OF FWD ENTRY DOOR CUTOUT. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001652005011100165NM 2005 1 11 ASAA0410527 120041112A53306545774 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS IN EXTERNAL SKIN, ALONG RT AFT WING TO BODY FAIRING. REPAIRED SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001662005011100166NM 2005 1 11 ASAA0410512 120041108A53206545800197 STRINGER CLIP BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23124 PAE - CORROSION ON INTERCOSTAL AND STRINGER CLIP. REMOVED AND REPLACED INTERCOSTAL AND STRINGER CLIP. 2L72 4F4 FRTA16WE E2EA 20050111001672005011100167NM 2005 1 11 ASA0440229 120041109A5311654655846 FRAME BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02788AS 28885 CORROSION ON FRAME. REPAIRED CORRODED FRAME IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050111001682005011100168NM 2005 1 11 ASA0440234 120041110A533065C2653825 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 LT WING LOWER EXTERIOR SKIN IS DENTED. REPLACED LOWER EXTERNAL SKIN IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050111001722005011100172NM 2005 1 11 ASAA0410515 120041110A53506545771 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARKS ON EXTERNAL SKIN AT WING TO BODY FAIRING. REPAIRED EXTERNAL SKIN IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001742005011100174NM 2005 1 11 ASAA0410514 120041108A53206545800197 STRINGER SPLICE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED AND STRINGER SPLICE. 2L72 4F4 FRTA16WE E2EA 20050111001762005011100176NM 2005 1 11 ASAA0410574 120041122A53306545772155 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARK IN SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001782005011100178NM 2005 1 11 ASAA0410532 120041112A533065458001138 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - SCRIBE MARK IN EXTERNAL SKIN LAP JOINT STA 359, STRINGER 24L, 2 INCHES LONG. REPAIRED SCRIBE MARK. 2L72 4F4 FRTA16WE E2EA 20050111001802005011100180NM 2005 1 11 ASAA0410569 120041122A5313BAC14936597075T6STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - STRINGER CHAFED AT WIRE BUNDLE STANDOFF. REPAIRED STRINGER IAW SRM. 2L72 4F4 FRTA16WE E2EA 20050111001822005011100182NM 2005 1 11 ASAA0410496 120041109A53306545775558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON SKIN, 3 INCHES BELOW AFT CARGO DOOR CUTOUT, UPPER AFT CORNER. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050111001842005011100184NM 2005 1 11 ASAA0410671 120041130A5320656211310 FLOOR SUPPORT BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050111001862005011100186NM 2005 1 11 ASAA0410632 120041120A533065549352 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, SCRIBE MARK ON SKIN LAP AT STRINGER 14L. REPAIRED PER EA 5230-01250. (M) 2L72 4F RTA16WE 20050112000242005011200024EU 2005 1 12 MALA040919 120041230A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 DURING 4K INSPECTION IN BNA, RT FUSELAGE HAS NUMEROUS DENTS BETWEEN FS 339 AND FS 363, AND BETWEEN STR 1615 TO SL 1617. DAMAGE WILL BE REPAIRED IAW MESABA EO S53009. REFER TO EAMS WORK ORDER 211273, TASK 2514 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1/7/05. 2L72 4T RTA52EU 20050112000262005011200026EU 2005 1 12 MALA040914 120041223A5610NF20216525 WINDSCREEN BAC 146 AVRO146RJ85A1500097EU COCKPIT DELAMINATED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15523XJ E2348 PILOT REPORTED CAPT A SCREEN WAS DELAMINATED AND ARCING AND POPPING. SHORTLY AFTER THAT THE OUT PLY STARTED TO COME AWAY FROM THE WINDOW INFLIGHT. AIRCRAFT DIVERTED TO CVG AND DECLARED AN EMERGENCY. MAINTENANCE REMOVED AND REPLACED CAPT -A- SCREEN, P/N NF20216-525, SN/OFF L315445, PN/ON SPSBAE146-2-2-1 SN/ON 37, ALL CHECKS GOOD. 2H74 4F RTA49EU 20050112000282005011200028EU 2005 1 12 MALA040912 120041222A3260 UPLOCK BAC 146 AVRO146RJ85A1500097EU MLG FROZEN A MALAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15534XJ E2370 DURING FLIGHT, LT GEAR NOT INDICATING UP AND LOCKED. RED LIGHT ILLUMINATED AND GEAR HANDLE LIGHT ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE FOUND ICE COMPLETELY AROUND DOOR UPLOCK LATCH AND SURROUND DOOR WAS UNABLE TO LATCH CLOSED. REMOVED ICE, NO DAMAGE NOTED AT DOOR OR LATCH NOTED. 2H74 4F RTA49EU 20050112000672005011200067SO 2005 1 12 C2XA04IA168 120041224A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716541 145542 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLOOR EMERGENCY LIGHT STRIP, OPERATIONALLY CHECKED THE LIGHT STRIP AND CLEARED THE DISCREPANCY. SEE SDR CONTROL NUMBER C2XA04IA169 FOR DOCUMENTATION OF THE NR 3 EMERGENCY LIGHT BATTERY PACK REPLACEMENT FOR THIS SAME OCCURRENCE. 2L72 4T RTT00011AT 20050112000712005011200071SO 2005 1 12 C2XA04IA155 120041129A3350110049 CHARGER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713992 145284 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT AN EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND MEL'D THE EXTERIOR EMERGENCY LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/29/04, IN IAH, MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR BATTERY EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE - THIS PART IS NOT TRACKED FOR TIMES & CYCLES. 2L72 4T RTT00011AT 20050112000732005011200073NM 2005 1 12 04FDEA03501 120041228A5312 BULKHEAD DOUG MD11 MD11 3023602NM ZONE 200 MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, BULKHEAD HEAD'S WEB AT STA 2007 FOUND WITH EXISTING HOLES AT LBL 27.5 AFTER TEE CHORD REMOVED FOR REPLACEMENT. EXISTING DOUBLE HOLES AT LBL 20 AFTER TEE CHORD EVALUATED AND FOUND NOT IN ACCORDANCE WITH SRM CHAPTER 53. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-78099. 2L73 4F RTA22WE 20050112000742005011200074NM 2005 1 12 04FDEA03502 120041229A5310 STRUCTURE DOUG MD11 MD11 3023602NM ZONE 700 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER LANDING GEAR WORK PLATFORM AFT CENTER JOINT PIECE (UPPER) FOUND DELAMINATED. REPAIRED AS PER SRM 51-43-01 VOL II AND PAINTED AS PER SRM 51-21-02 VOL II. INSTALLED AS PER AMM 32-17-06. 2L73 4F RTA22WE 20050112000752005011200075NM 2005 1 12 04FDEA03503 120041229A5330 SKIN DOUG MD11 MD11 3023602NM ZONE 100 MISREPAIRED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25577FE 48469 FORWARD CARGO RT APPROX STA 620, A REPAIR THAT GOES FROM LONGERON 49R TO 40R NEEDS INVESTIGATION. EVALUATED AND FOUND NOT CONFORMING TO SRM CHAPTER 53. REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-77979, 2L73 4F RTA22WE 20050112000762005011200076NM 2005 1 12 04FDEA03504 120041229A5522 SKIN DOUG MD11 MD11 3023602NM ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND INBOARD ELEVATOR OUTBOARD UPPER AND LOWER SURFACES (TRAILING EDGE) FOUND DELAMINATED. REMOVED AND RE-INSTALLED AFTER REPAIR AS PER AMM 27-30-20. ELEVATOR RANGE OF MOVEMENT TEST CARRIED OUT AS PER AMM 27-30-00 FOUND SATISFACTORY. 2L73 4F RTA22WE 20050113000032005011300003NE 2005 1 13 MOR2104 220041015A7200 ENGINE BOEING767 767300 1385204NM GE CF6 CF680C2B7 NE NR 1 VIBRATION G EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO01VPBAZ 30111 704956 NR 1 ENGINE INFLIGHT SHUT DOWN DUE TO VIBRATION. 2L72 4F4 FRTA1NM E13NE 20050113000052005011300005 2005 1 13 ASMF200410014 420041019A34449650476088 COMPUTER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE GPWS FAILED W ASMFD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW23838AM5952 49397 DURING LT ENGINE STARTING, STRONG NOISE WAS HEARD. CAPTAIN SHUTOFF ENGINE AND RETURNED TO PLATFORM. DURING CHECK, WAS DETECTED THAT THE NOISE WAS PRODUCED BY THE GPWS. IT WAS DEFERRED IAW MEL 34-29. DURING TRANSIT CHECK AT MEX, GPWS COMPUTER WAS REPLACED IAW MM 34-45-01. DURING OVERNIGHT SERVICE, GPWS WAS TESTED IAW MM 34-45-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050113000402005011300040EU 2005 1 13 ASAA0340346S 220041128A7200 ENGINE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU NR 1 FLAMED OUT A ASAAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 NM02713AS 30161 860139 DURING CRUISE NR 1 ENGINE EXPERIENCE ELECTRICAL POWER DISCREPANCIES AND SUBSEQUENT FLAME OUT. AIRCRAFT DIVERTED AND LANDED WITH OUT INCIDENT. WHILE PERFORMING ENGINE FUEL FEED LINES/COUPLING VACUUM TEST IAW TECH SERVICE REQUEST AND IAW AMM, FOUND THE THERMAL RELIEF VALVE ON PORT ADAPTER ASSY ON ENGINE FUEL SHUT OFF VALVE LEAKING AIR. REMOVED AND REPLACED ENGINE FUEL SHUT OFF VALVE. OPERATIONAL CHECKED GOOD. 2L72 4F4 FRTA16WE E21EU 20050113000442005011300044NM 2005 1 13 2004UALA01198 120041208A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 FUSELAGE SKIN AND STRINGER BELOW THE AFT ENTRY DOOR IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIRED SKIN DOUBLER , TRIPLER, & FILLER. SPLICED IN NEW STRINGER SECTION. 2L72 4F4 FRTA2NM E17NE 20050113000552005011300055SO 2005 1 13 CHQA000515 120040714A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265 145226 WHILE PERFORMING JOB CARD 33-50-04-720-001, THE NR 1 POSITION CHASSIS WAS UNABLE TO POWER THE EMERGENCY LIGHTS. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050113000562005011300056SO 2005 1 13 CHQA000523 120040727A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11278 145370 DURING CRUISE FLIGHT A BURNING ODOR OCCURRED WHEN THE ANTI ICE SYSTEM WAS ACTIVATED IN ICING CONDITIONS. PERFORMED OPERATIONAL CHECK OF THE PNEUMATIC SYSTEM AND FOUND NO SMELL OR DEFECTS IN THE SYSTEM AT THIS TIME AND DATE. INSPECTED IAW EMB 145 AMM 36-00-00. 2L72 4T RTT00011AT 20050113000572005011300057EU 2005 1 13 XN0A1216 120041214A2797 WIRE AIRBUS300 A300B4203 3930306EU NR 3 SLAT CHAFED A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23472AS 125 NR 3 WITH SLAT RETRACTION LOW SPEED AILERONS (RED LIGHT) & CONFIG LIGHT ON FWD PANEL ILLUMINATED. TRANFERED TO DMI LIST IAW ENA A300 MEL 27-11-01, CAT "B" DMI 4824 S.P. 27-11-01 C/W. REPAIRED CHAFED WIRE ON HARNESS TO LSA SERVO OF THE LT WING, SYSTEM OPS CK NORMAL I/A/W A300 AMM 27-11-00. THIS ACTION CLEARS DMI 4824. PLACARDS REMOVED. (STATUS:SUPP/CLOSED) 2L72 4F RTA35EU 20050113000582005011300058NM 2005 1 13 P9RA20040059 120041224A3397 WIRE BOEING757 757231 1384950NM EMERGENCY LIGHT LOOSE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11962 24119 A/C IN ORD, EMERGENCY FLOOR AISLE LIGHTS OUT 3 EACH FWD MOST. RESECURED WIRING AFT FLOOR LIGHT LENS ASSEMBLY. OP'S OK PER MM 33-51-05. NO PART CHANGED. 2L72 4F RTA2NM 20050113000632005011300063 2005 1 13 P9RA20040060 420041224A2565767 BULB BOEING757 757236 1384971NM ESCAPE SLIDE INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11522NA 25133 A/C IN LAS. R1 & R3 EMERGENCY SLIDE LIGHT INOP. RELAMPED R1 & R3 2L72 4F RTA2NM 20050113000642005011300064NM 2005 1 13 04FDEA03051 120041108A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 1090 LBL 47. REPAIRED AS PER SRM 53-70-00 FIG 1, VOL I & SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050114000012005011400001NM 2005 1 14 04FDEA03493 120041228A5310707500125 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 MAIN DECK, LT TRANSVERSE FRAME AT STA 535 FOUND DAMAGED IN TWO PLACES. MAIN DECK, LT TRANSVERSE FRAME AT STA 535 DAMAGE REPAIRED AS PER SRZ-53-503. 2L73 4F RTA22WE 20050114000112005011400011NM 2005 1 14 SB04155 120041117A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19777AU 24979 MAINTENANCE REPORTED AN EMERGENCY LIGHT IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050114000132005011400013NM 2005 1 14 QXEA200400780 120041118A243051539008D GCU DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER J WARNING INDICATION CRCRUISE 1 NM09357PH1657310029 504 ON FLIGHT NUMBER 2174, NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED IN FLIGHT, RESET PER CHECKLIST. NR 1 DC GENERATOR LIGHT WENT OUT BUT REILLUMINATED SHORTLY THEREAFTER. REMOVED AND REPLACED NR 1 GCU.OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2H72 4T RTA13NM 20050114000162005011400016SO 2005 1 14 CHQA000546 120040831A3350 BULB EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11377SK 145579 LEFT SIDE EXTERNAL EMERGENCY OVERWING LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 140 MM. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050114000182005011400018SO 2005 1 14 CHQA000549 120040903A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11264SK 145221 LEFT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050118000282005011800028NM 2005 1 18 04FDEA03505 120041229A552165174286 RIB BOEING727 727100 1384036NM ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25151FE 19147 RIGHT HORIZONTAL STAB ELEVATOR STATION 17.20, INBOARD RIB CRACK RUNS FROM RIVET ON UPPER. REMOVED RIB IAW SRM 51-30-2 & SB 727-55A0091. INSTALLED NEW RIB WITH P/N 65-17428-6 IAW SRM 51-30-2 & SB 727-55A0091. 2L73 4F RTA3WE 20050118000322005011800032NM 2005 1 18 0402236719 120041223A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01619US 21321 DURING L-CHECK FOUND CRACK IN FRAME AT BS 400 S23L. REPAIRED PER EA 67-165182. 2L74 4F A20WE 20050118000392005011800039SO 2005 1 18 C2XA04IA170 120041224A335020131A BATTERY EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27175139874 895 145292 DURING SCHEDULED MAINTENANCE THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4F RTT00011AT 20050118000442005011800044SO 2005 1 18 C2XA04IA175 120041228A335020131A BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCHARGED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713969611 611 145141 IAH - THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050118000472005011800047SO 2005 1 18 MASA200400710 120041220A783083990137 SWITCH EMB EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07828MJ9368 TR0374 145218 ASH 2624 CAE TO DCA. ABORTED TAKEOFF DUE TO E2 REVERSER DISAGREE MESSAGE. MAINTENANCE COMPLIED WITH MEL PROCEDURES. MAINTENANCE R2 THE STOW/TRANSIT SWITCH, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050118000482005011800048SO 2005 1 18 MASA200400717 120041221A7830M8353610024M RELAY EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07831MJ 145273 ENGINE 2 THRUST REVERSER DISAGREE MESSAGE. MAINTENANCE PLACED THE T/R ON MEL. 12/21 MAINTENANCE REMOVED AND REPLACED RELAYS P/N M83536-10-024M AND M83536/2-024M. 2L72 4T RTT00011AT 20050118000492005011800049SO 2005 1 18 MASA200400723 120041223A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07847MJ 145517 ABORTED TAKEOFF DUE TO E2 REVERSER DISAGREE ON TAKEOFF. MESSAGE WENT AWAY, AN ON-CALL MAINTENANCE PERFORMED OPERATIONAL CHECK AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTT00011AT 20050118000502005011800050SO 2005 1 18 MASA200400725 120041224A7830 ROD EMB 145 EMB145LR 3260212SO THRUST REVERSER OUT OF ADJUST A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07847MJ 145517 AIRCRAFT ABORTED TAKEOFF DUE TO AN E2 REV DISAGREE MESSAGE DURING TAKEOFF ROLL. CONTRACT MX PLACED THE NR 2 THRUST REVERSER ON MEL. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. OPEN PENDING RESOLUTION OF MEL. 12/29 MAINTENANCE ADJUSTED LOWER ACTUATOR ROD AND RIGGED ALL SWITCHES. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050118000572005011800057NM 2005 1 18 MASA200400684 120041207A3350OL4009BPE LAMP DHAV DHC8 DHC8202 2809007NM CABIN LIGHTS BURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 ASH 6259 PHX. ROW 3 OVERHEAD LIGHT IS SMOKING. MAINTENANCE IS TROUBLESHOOTING. 12/9 MAINTENANCE REPLACED LAMP ASSY. 2H72 4T RTA13NM 20050118000622005011800062EA 2005 1 18 MASA200400720 120041222A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INTERMITTENT A MASAO OTHER L NO TEST ININSP/MAINT 1 SW0737178 7178 ASH 6389 PHX-MFR. DURING PREFLIGHT THE CREW REPORTED THE AFT SECTIONS OF THE FLOOR PATH EMERGENCY LIGHTS INOP. MAINTENANCE FOUND THE LIGHTS TO WORK NORMALLY. 2L72 4F RTA21EA 20050118000632005011800063EA 2005 1 18 MASA200400724 120041223A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0737178 7178 ASH 6271 ICT. AIRCRAFT HAD 4 SECTIONS OF EMERGENCY EXIT PATH WAY LIGHTING INOP. MX SECURED THE ELECTRICAL CONNECTION UNDER THE LAV FLOOR TO CLEAR FAULT. 2L72 4F RTA21EA 20050607000782005060700078EU 2005 6 7 TXER100924 120040824A6410C642A0300102 TAIL ROTOR UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE WORN B TXERK NONE O OTHER ININSP/MAINT 1 SW09690WR 1059 TAIL ROTOR, OUT OF LIMITS IAW 64-21-00,6-9 PG. 602 ZONE E. 1G72 3U3 UNCR0001RD E34NE 20050608001332005060800133SW 2005 6 8 GJD2005F00000 120041118A641047642117105 BLADE BELL 47 47G3B2 1181029SW TAIL ROTOR FRACTURED G GJDAO OTHER O OTHER NRNOT REPORTED 1 NM097825S1723 6688 DURING ACCIDENT INVESTIGATION, FOUND EVIDENCE OF FATIGUE FRACTURE ON TAIL ROTOR BLADE. OPPOSING BLADE WAS FRACTURED DUE TO APPARENT OVERLOAD. BOTH BLADES SENT TO MFG LABS UNDER NTSB ESCORT. TEARDOWN REPORT INDICATES BOTH BLADES HAD PROGRESSIVE FATIGUE EMANATING FROM PITTING OF INTERNAL BLADE SKINS. PITTING TRACED TO PREBONDING ETCHING PROCESS DURING MFG. MFG LABS REPORT THIS CONDITION BEING INVESTIGATED FOR OTHER BLADES MANUFACTURED AROUND THE SAME DATES. NO FINAL ANALYSIS AVAILABLE. (K) 1G71 3O 2H3 20050608001362005060800136NM 2005 6 8 QXEA200500955 120040523A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM CARGO DOOR OUT OF SEQUENCE A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09414QX 4061 EUG - ON CLIMBOUT, THE AFT BAGGAGE DOOR LIGHT ILLUMINATED SETTING OFF THE MASTER WARNING AND FUSELAGE DOOR LIGHT. NO LOSS OF PRESSURE, CONTINUED TO EUG. ON APPROACH THE AIRCRAFT DEPRESSURIZED. MAINTENANCE FOUND DOOR HANDLE OUT OF SEQUENCE. RESET HANDLE AND WARNING EXTINGUSHED. CYCLED DOOR THREE MORE TIMES. WARNING OPERATED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE AND NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20050607000792005060700079EU 2005 6 7 TXER100925 120040830A6400C642A0300102 TAIL ROTOR UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE WORN B TXERK NONE O OTHER ININSP/MAINT 1 SW09588SC 1130 TAIL ROTOR, OUT OF LIMITS PER 64-21-00,6-9 ZONE D. 1G72 3U3 UNCR0001RD E34NE 20050613000852005061300085CE 2005 6 13 ENHA0501 120040910A242010300B ALTERNATOR CESSNA207 207A 2073604CE ENGINE FAILED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL039651M 107 20700715 FIELD OPEN. UNIT FAILED. 1H71 3O A16CE 20050118000062005011800006WP 2005 1 18 MWEA040229 120041229A533059101413 DOUBLER DOUG DC9 DC981 3022081WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31803ME 48029 ELECTRICAL DISCHARGE AT APPROXIMATELY STATION 668 LONGERON 21 RIGHT. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20050118000212005011800021NM 2005 1 18 AWXA200500026 120041220A57536546486129 WEDGE BOEING737 7373Q8 1384670NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK THE LT INBOARD MID FLAP WEDGE WAS FOUND DELAMINATED ON LOWER SURFACE 36 INCHES FROM THE INBOARD END BEWTEEN WBL 104 AND WBL 115. MAINTENANCE CUT OUT DAMAGE IN LT INBOARD MID FLAP WEDGE ON LOWER SURFACE 36 INCHES FROM INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO MID FLAP IAW B737-300 SRM 51-70-10, FIG 30. 2L72 4F RTA16WE 20050118000302005011800030GL 2005 1 18 MASA200400713 220041220A72614252070 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE WORN A MASAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW07832MJ5859 145310 CAE311836 ASH 2760 CAE TO CLT. SHUT DOWN NR 1 ENGINE DUE TO LOSS OF OIL PRESSURE. MAINTENANCE TROUBLESHOT AND REPLACED MAGNETIC CARBON SEAL ON THE NR 1 ENGINE. OPS CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050118000372005011800037SO 2005 1 18 C2XA04IA169 120041224A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW271654110298170 145542 DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2L72 4T RTT00011AT 20050118000452005011800045SO 2005 1 18 C2XA04BT131 120041224A3350 BULB EMB 145 EMB145 3260210SO EMERGENCY LIGHT LOOSE A C2XAO OTHER O OTHER UKUNKNOWN 1 SW2714959 145091 EWR LOG SQUAWK EMERGENCY EXIT LIGHT ABOVE ROW 1C WILL NOT ILLUMINATE. RESET EMERGENCY LIGHT ABOVE ROW 1C IAW EMB MM 33-50-00. 2L72 4F RTT00011AT 20050118000612005011800061EA 2005 1 18 MASA200400718 120041221A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0747239 7239 ASH 6239 PHX - SBP FLOOR LEVEL EMERGENCY FLOOD LIGHTS HAVE ONE BULB OUT AT THE PAX DOOR. MAINTENANCE REMOVED AND REPLACED THE BULB. 2L72 4F RTA21EA 20050118000712005011800071CE 2005 1 18 DXTA200400502 120041228A3220 UPLOCK CESSNA560 560XL 2076702CE NLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07603QS 5605203 AFTER TAKEOFF NOSE GEAR WOULD NOT FULLY RETRACT. CYCLED ON UPLOCK ON & OFF (UNLOCK LIGHT). ADJUSTED NOSE GEAR UPLOCK. OPS CHECK GOOD. WORK DONE IAW CESSNA 560XL MAINTENANCE MANUAL 32-30-05. 2L72 4F RTA22CE 20050118000752005011800075SO 2005 1 18 SWIA200414321 120041228A3350 SIGN EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07298SW 120328 EXIT SIGN TO LOWER RIGHT OF F/A SEAT BROKEN. REPLACED LIGHT RECEPTACLE FOR EMERGENCY LIGHT AT F/A SEAT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050118000772005011800077SO 2005 1 18 SWIA200414322 120041228A5210 SWITCH EMB 120 EMB120ER 3260203SO PAX DOOR INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07235SW 120310 AFTER SHUTDOWN, FORWARD CABIN DOOR WOULD NOT OPEN. FORWARD ACTUATOR LIGHT ON. REPLACED FORWARD CABIN DOOR F/A'S SWITCH. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050118000792005011800079NM 2005 1 18 04FDEA03490 120041227A5260 WARNING LIGHT BOEING727 727200 138407ENM AFT AIRSTAIR ILLUMINATED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25209FE 22931 AFT STAIR LIGHT ILLUMINATE. OAK-LINE ENT BY: 390984 ON: 27DEC04 23:46:58:3 S=M MEL 27DEC04. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 06JAN05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. 2L73 4F RTA3WE 20050118000882005011800088NM 2005 1 18 04FDEA03495 120041228A5320AFJ70411 INTERCOSTAL DOUG MD11 MD11 3023602NM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25599FE 48598 CENTER CARGO, INTERCOSTAL AT STA Y= 1710 FOUND CRACKED. 2L73 4F RTA22WE 20050118000902005011800090SO 2005 1 18 MASA200400728 120041226A3397 WIRE EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BROKEN A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07836MJ 145359 ASH 2859 CAE TO CLT. AIRCRAFT HAD A FLOOR EMERGENCY LIGHTING STRIP INOP. MX REPAIRED A BROKEN WIRE AT THE CONNECTOR AND THE LIGHT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050118000922005011800092SO 2005 1 18 C2XA04SH573 120041219A532014521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713913 145438 DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050118000952005011800095SO 2005 1 18 C2XA04SH574 120041230A532014530642401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714937 145026 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050118000962005011800096SO 2005 1 18 C2XA04SH575 120041230A531514530643403 FLOORBEAM EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714937 145026 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01185. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050118000982005011800098SO 2005 1 18 C2XA04SH572 120041217A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711127 145697 DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED AND REPLACED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RT 20050118001022005011800102NM 2005 1 18 UPS04443622 120041228A3350 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE:N/A, EMERGENCY EXIT SIGN ABOVE UPPER DECK EMERGENCY EXIT DOOR INOP. REMOVED AND REPLACED BATTERY PACK (M312), OPS CHECK GOOD, MM 33-51-04. 2L74 4F A20WE 20050118001032005011800103NM 2005 1 18 UPS05443623 120041231A3350 BATTERY PACK BOEING747 747200 1384847NM R1 EMER EXIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01522UP 21936 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER R1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK ASSY AS PER AMM 33-51-04. OPS CHECK GOOD. 2L74 4F RTA20WE 20050118001042005011800104EU 2005 1 18 MALA040777 120041013A5320 MOUNT BAC 146 AVRO146RJ85A1500097EU AIRBRAKE SPIGOT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING C-CHECK INSPECTION IN YYC, RT AIRBRAKE SPIGOT RECEPTICLE MOUNTING STRUCTURE CRACKED. MAINTENANCE REPAIRED IAW SRM 51-20-11, 51-23-00, 51-24-11, 51-25-00, 51-41-00, 51-42-00, 51-43-00, 53-50-11 FIG 1, 22. AIRCRAFT RETURNED TO SERVICE 10/17/04. 2H74 4F RTA49EU 20050118001092005011800109NM 2005 1 18 04FDEA03492 120041228A5720 RUB STRIP DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING - NR 2 TANK NR 531 AT CUTOUT RUB STRIP FOUND CORRODED. REMOVED DAMAGED RUB-STRIP AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RUB-STRIP AS PER SRM 51-42-04 VOL II AND SRM 51-35-01 VOL II AT LT WING NR 2 TANK 531AT CUT-OUT. 2L73 4F RTA22WE 20050118001102005011800110EU 2005 1 18 04FDEA03496 120041228A5315 FLOORBEAM AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 BULK CARGO COMPT FLOOR STRUCT FR 67 LEFT TO MID RIGHT SIDE HAS MULTIPLE AREAS OF CORROSION FROM TOP SKIN TO UNDERNEATH SURFACE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED BEAM IAW SRM 51-40-21 AT FR 67. 2L72 4F RTA35EU 20050118001112005011800111EU 2005 1 18 04FDEA03497 120041228A5315 FLOORBEAM AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 BULK CARGO COMPT FLOOR STRUCTURE FR 67 LT TO MID RT SIDE HAS MULTIPLE AREAS OF CORROSION FROM TOP SKIN TO UNDERNEATH SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED BEAM IAW SRM 51-40-21 AT FR 67. 2L72 4F RTA35EU 20050118001132005011800113EU 2005 1 18 04FDEA03499 120041228A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 MCD FR 47 TO FR 53 LT NR 1 SEAT TRACK HAS 4 AREAS OF CORROSION REF N-CARD N00473. REPAIRED TRACK AT FR 46.5 TO FR 47.5 AND FR 52.5 TO FR 54 IAW SRM 53-10-16. 2L72 4F RTA35EU 20050118001142005011800114EU 2005 1 18 04FDEA03500 120041228A5313 STRINGER AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 FR 38 TO FR 38.1 BILGE AREA HAS 2EA AREAS OF CORROSION ON STR 43L AND IN BETWEEN STR 44 AND 45, 48 SQ INCH REF N-CARD N00882. CLEANED AREA BETWEEN STR 44 AND 45 FOUND TO BE DIRTY, NO CORROSION EXIST IAW SRM 51-74-10. REPAIRED STR 43L FROM FR 38 TO FR 38.1 IAW SRM 53-10-14 FIG 201 & 51-40-21. 2L72 4F RTA35EU 20050118001182005011800118SO 2005 1 18 C2XA04IA132 120041017A3234 CONTROL LEVER EMB 145 EMB145 3260210SO MLG INOPERATIVE A C2XAO OTHER J WARNING INDICATION APAPPROACH 1 SW27139587354 0486 145085 CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND NORMALLY. AIRCRAFT LANDED AT OKC WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRIED TO IAH AND LANDING WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER AND OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050118001192005011800119SO 2005 1 18 C2XA04IA133 120041006A33507287100507 CONTROL PANEL EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW2741104 145646 CREW REPORTED EMERGENCY EXIT LIGHTS CAME ON AFTER LANDING WITH AN EMERGENCY LIGHT NOT ARMED WARNING. REMOVED AND REPLACED THE FLIGHT ATTENDANTS CONTROL PANEL. 2L72 4F RT 20050118001212005011800121SO 2005 1 18 C2XA04IA141 120041104A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO MLG INOPERATIVE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2716981 145208 DURING CLIMB THE LANDING GEAR LEVER WOULD NOT GO TO THE UP POSITION. USING THE DOWNLOCK RELEASE BUTTON THE GEAR RETRACTED SUCCESSFULLY BUT THE NOSE GEAR DOORS REMAINED OPENED. AIRCRAFT RETURNED TO IAH LANDED WITHOUT INCIDENT. REPLACED THE NLG DOOR SEQUENCE SWITCH AND OPERATIONALLY CHECK GOOD. AIRCRAFT APPROVED FOR SERVICE. 2L72 4T RTT00011AT 20050118001222005011800122GL 2005 1 18 C2XA04BT123 220041203A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 SMOKE A C2XAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2726545 145558 CAE311419 CREW REPORTED LAV SMOKE WARNING AFTER TAKEOFF. THIS OCCURRED 60 SECONDS AFTER TRANSITION FROM APU BLEED TO ENGINE BLEEDS. AIRCRAFT RETURNED TO NEWARK AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SMOKE SMELL WITH BLEEDS ON AFTER TAKEOFF POWER OBTAINED. APPEARS TO BE STRONG OIL SMELL FROM NR 2 ENGINE. AIRCRAFT FERRIED TO TYS FOR FURTHER TROUBLESHOOTING. ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20050118001242005011800124SO 2005 1 18 C2XA04BT130 120041211A4920 ODOR EMB 145 EMB145LR 3260212SO APU DETECTED A C2XAD RETURN TO BLOCK BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW2713994 145291 DURING TAXI CREW REPORTED VERY STRONG BURNING SMELL FOLLOWED BY GRINDING NOISE AND VIBRATION. SHUTDOWN APU AND INDICATIONS WENT AWAY. INSPECTED APU, ENGINES AND AIR CONDITIONING PACKS IN VARIOUS CONDITIONS OF POWER AND BLEED SETTINGS. NO DEFECTS NOTED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050118001252005011800125SO 2005 1 18 MASA200400714 120041220A5220 SEAL EMB 145 EMB145LR 3260212SO EMERGENCY EXIT LEAKING A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW07826MJ 145214 CREW REPORTED A LOUD SQUEAL FROM THE RT OVERWING EMERGENCY EXIT WHEN THE PAX DOOR WAS SHUT. MAINTENANCE REMOVED THE OVERWING HATCH INSPECTED THE SEAL AND REINSTALLED THE DOOR AND PERFORMED A PRESSURIZATION CHECK WITH NO LEAKS OR SQUEALS NOTED. 2L72 4T RTT00011AT 20050118001272005011800127SO 2005 1 18 C2XA04CL132 120041229A3350BA50933901 CHARGER EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER O OTHER TXTAXI/GRND HDL 1 SW2713123 145688 CLE - THE CREW TURNED OFF THE CABIN LIGHTS AND THE EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND ELECTRICAL CONNECTOR P8500. 2L72 4F RT 20050118001282005011800128SO 2005 1 18 C2XA04IA177 120041228A3350AD20131A BATTERY PACK EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCHARGED A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW27139695 5 145141 THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20050118001302005011800130SO 2005 1 18 MASA200400700 120041216A7830M83536 RELAY EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07828MJ 145218 ASH 2819 CRW TO CLT. ABORTED TAKEOFF DUE TO AN E2 REV DISAGREE MESSAGE. MAINTENANCE PLACED THE NR 2 ENGINE THRUST REVERSER ON MEL. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 12/19 MAINTENANCE REPLACED RELAYS. 2L72 4T RTT00011AT 20050118001312005011800131SO 2005 1 18 MASA200400705 120041217A783083990168 SWITCH EMB EMB 145 EMB145LR 3260212SO THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07842MJ2806 TR0770 145457 ASH 2765 FROM BTV TO PHL ABORTED TAKEOFF DUE TO AN E1 REV DISAGREE MESSAGE DURING TAKEOFF ROLL. MAINTENANCE PLACED THE NR 1 THRUST REVERSER ON MEL. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 12/23 MAINTENANCE REPLACED LT 3 & 4 STOW/TRANSIT SWITCH. 2L72 4T RTT00011AT 20050118001332005011800133NE 2005 1 18 04FDEA03481 220041224A7200PW44623 ENGINE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 2 FAILED A FDEAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO25580FE1085910859 48471 NR 2 ENGINE VIBRATION AT TAKEOFF ROTATION FOLLOWED BY A BANG AT ROTATION. COMPRESSOR STALL REPORTED BY ANOTHER AIRCRAFT. EXCEEDENCE WENT AMBER TO 5.3 ON CLIMB & 4.4 IN CRUISE AT 10K FT, VIBRATION NOTICABLE IN CRUISE WITH ENGINE & WING ANTI-ICE ON & IGNITION OVERRIDE, ENGINES WERE DE-ICE & ANTI-ICE IN GATE FOLLOWED 30 SECOND RUN UP ON RUNWAY. DUE TO TAKEOFF COMPRESSOR STALL ABOVE 1.25 EPR THIS ENGINE IS APPROVED FOR REMOVAL PER PP/ENGINEERING. COMPLETED ENGINE CHANGE 1/1/05. 2L73 4F4 FRTA22WE E24NE 20050118001432005011800143NM 2005 1 18 UPS05543625 120041231A3350 LAMP BOEING757 75724APF 1384969NM EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01457UP 25478 INSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER AMM 33-51-06-2. OPS NORMAL. 2L72 4F RTA2NM 20050118001462005011800146SO 2005 1 18 C2XA04CL130 120041222A335020131A BATTERY EMB 145 EMB145 3260210SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW27139694898 145141 CLE - THE CREW REPORTED THE EMERGENCY EXIT LIGHT OUT AT 3B. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND CHARGER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050118001472005011800147SO 2005 1 18 C2XA04SD013 120041227A3260 TARGET EMB 145 EMB145LR 3260212SO MLG OUT OF ALIGNMENTA C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2712921 145354 SDF - AIR GROUND FAIL ON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. REPOSITIONED GROUND PROX SWITCH TARGET ON NOSE LANDING GEAR, JACKED AIRCRAFT AND CYCLED LANDING GEAR IAW EMB AMM 32-63-05. OPS CHECKED GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050118001482005011800148NE 2005 1 18 DXTA200400503 220041230A7261 OIL SYSTEM BRAERO1000 HAWKER1000 7450005EU PWA 305 PW305 NE NR 1 ENGINE OVERSERVICED E DXTAA UNSCHED LANDING WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07544QS 259044 IMMEDIATELY AFTER AIRBORNE & SELECTING MAIN AIR VALVE TO ON, SMOKE BEGAN TO BELLOW THROUGHOUT THE COCKPIT AND CABIN AREAS. MAIN AIR VALVES WERE IMMEDIATELY SELECTED OFF AND RAM AIR SELECTED TO FULL ON, TO HELP CLEAR THE COCKPIT. ON THE GROUND, ON REINSPECTION OF THE NR 1 ENGINE, OIL WAS FOUND ALL OVER THE NI INLET FAN. FOUND NR 1 ENGINE OIL SERVICED TOO HIGH. REMOVED EXCESS OIL. PERFORMED COMPRESSOR WASH, OPS CHECKED ENGINE. ALL SATISFACTORY IAW P&W 305B MM CH 71-00-00 AND HAWKER 1000 MM CH 12-10-00. 2L72 4F4 FRTA3EU E35NE 20050118001502005011800150CE 2005 1 18 DXTA200400504 120041230A214073838433 ACM CESSNA750 750 2076810CE ODOR E DXTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07918QS1593 7500223 AT FL 410, CREW AND PAX SMELLED FUMES IN THE GALLEY AREA AND COCKPIT. SMELL DIMINISHED IN CABIN AREA. SMELL WAS INTERMITTANT FOR 30 MINUTES DURING DESCENT. SMELL WENT AWAY WHEN COCKPIT PAC WAS TURNED OFF. COCKPIT PAC WAS TURNED OFF DUE TO LOSS OF TEMPERATURE CONTROL. DURING DESCENT, TEMP IN DUCT REMAINED AT 110 DEGREES AND WOULD NOT COOL DOWN. REMOVED AFT ACM AND INSTALLED AN OVERHAULED UNIT IAW CH 21-11-00 OF THE CE750 MM LEAK CHECK AND OPS CHECK GOOD. 2L72 4J RTT00007WI 20050118001742005011800174EA 2005 1 18 SWIA200414349 120041120A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 AFT OF FRAME 280 RIGHT SIDE 2 ANGLE CLIPS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ 200 SRM 51-42-06 FIG 8 AND 51-42-21. 2L72 4F RTA21EA 20050118001752005011800175EA 2005 1 18 SWIA200414352 120041120A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07910SW 7566 CRACKED SUPPORT ANGLE AT FS 625 NEAR STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ 200 SRM 51-42-06 PG 11 & 51-77-00 PG 1. 2L72 4F RTA21EA 20050118002012005011800201SO 2005 1 18 LR7A04203 120041231A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 648 5025 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND RIGHT AFT FUSELAGE BULKHEAD WEB CRACKED AT SCREW HOLE 2.2 INCH AT FS 924, WL 270, RBL 62-64. WEB REPAIRED IAW SMP583 CHP 51-10. 2H74 4T A1SO 20050118002022005011800202SO 2005 1 18 LR7A04204 120041231A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 648 5025 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND RIGHT AFT FUSELAGE BULKHEAD WEB CRACKED THROUGH RIVET EDGE 3 INCHES AT FS 924, WL 267, RBL 62-65. WEB REPAIRED IAW SMP583 CHP 51-10. 2H74 4T A1SO 20050119000012005011900001NM 2005 1 19 2004UALA00988 120041027A5312 PRESSURE PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 STA 664 PRESSURE WEB IS CRACKED AT LBL 31 JUST FWD OF AIL TOWER SHAFT. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA16WE E2GL 20050119000022005011900002NM 2005 1 19 2004UALA01159 120041124A5330143N31514 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29575UA 26689 RT EXT FUSELAGE AT STA 595 AND STR 8R, REPAIR DOUBLER AREA DAMAGED, CUTOUT CORNERS HAVE INSUFFICIENT RADII. *S/D* REMOVED EXISTING REPAIR DOUBLER, ENLARGED CUTOUT TO PROPER CUTOUT SPECIFICATIONS, AND INSTALLED REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20050119000132005011900013NM 2005 1 19 2005UALA00001 120041231A5313 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 AFT CARGO PIT, SHEAR TIE CORRODED BETWEEN STR 29R AND 28R. 2L72 4F4 FRTA2NM E17NE 20050119000142005011900014NM 2005 1 19 2005UALA00002 120040101A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 27L. 2L72 4F4 FRTA2NM E17NE 20050119000152005011900015NM 2005 1 19 2005UALA00003 120040101A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 CABIN FLOORBEAM CAP AT STA 324 CORRODED FROM RBL 30 TO RBL 63. 2L72 4F4 FRTA2NM E17NE 20050119000162005011900016NM 2005 1 19 2005UALA00004 120040101A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 AFT PIT STA 1560 STR 25L FRAME IS DAMAGED. 2L72 4F4 FRTA2NM E17NE 20050119000222005011900022NM 2005 1 19 2005UALA00011 120040103A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 AFT CARGO PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED. 2L72 4F4 FRTA2NM E17NE 20050119000242005011900024NM 2005 1 19 2005UALA00014 120041231A5270 WARNING LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE DOOR WARNING ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29576UA 26690 ABORTED TAKEOFF AT 110 KTS DUE TO A DOOR EICAS INDICATION. 2L72 4F4 FRTA2NM E17NE 20050119000282005011900028NM 2005 1 19 2005UALA00018 120040104A5340 ATTACH ANGLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 ATTACH ANGLE FOR BS 940 FRAME BELOW LEFT FWD OVERWING DOOR CUTOUT CORRODED BETWEEN STR 16L. 2L72 4F4 FRTA2NM E17NE 20050119000292005011900029NM 2005 1 19 2005UALA00019 120040104A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 FLOORBEAM HAS AREAS OF CORROSION FROM BL 0 TO RBL 60 AT BS 365. 2L72 4F4 FRTA2NM E17NE 20050119000312005011900031NM 2005 1 19 2005UALA00022 120040104A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 CABIN FLOORBEAM T-CAP CORRODED ON PREVIOUS REPAIR DOUBLER AT BS 1640, RBL 48-56. 2L72 4F4 FRTA2NM E17NE 20050119000342005011900034NM 2005 1 19 2005UALA00028 120040105A5230 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE CARGO DOOR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29776UA 26937 LOWER FWD CORNER OF AFT PIT DOOR HAS TEMP REPAIR INSTALLED. AFT CARGO DOOR HAD A PREVIOUSLY INSTALLED TEMPORARY REPAIR. THE TEMPORARY REPAIR WAS REMOVED AND REPLACED WITH A PERMANENT REPAIR. 2L72 4F4 FRTT0001SE E46NE 20050119000382005011900038 2005 1 19 MALA040911 420041221A34206226190113 COMPUTER SAAB SF340 340B 7860101EU NR 1 AHRS INOPERATIVE A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15447XJ 340B447 A/P DISCONNECTED, A/C 10 DEG ROLL TO LEFT WITH A/P ENGAGED WITH NO TURN INTIATED, ROLL FLAG ON EADI, CAPTAINS EADI ROLLS CONTINOUSLY TO LEFT, HEADING ON CAPT'S SIDE DOES NOT MATCH MAG COMPASS OF F/O'S EHSI. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER P/N 622-6190-113, S/N OFF 2817, S/N ON 241. OPS CHECK GOOD. 2L72 4T RTA52EU 20050119000392005011900039NE 2005 1 19 MALA040916 220041224A7320 HMU BAC 146 AVRO146RJ85A1500097EU GE CT7TP CT79B 30030NE NR 2 ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL15504XJ E2311 CLIMBING THROUGH FL 280, A THUMP WAS FELT THROUGH AIRFRAME AND THE MWS LIGHT FAULT LIGHT ILLUMINATED BRIEFLY. AIR RETURN TO MSP. MAINTENANCE COMPLETED 409 204198 DOWNLOAD OF FDAMS SHOWED NR 2 ENGINE COMPRESSOR STALL, NR 2 ENGINE BLEED BAND ACTUATOR AND HMU WERE REPLACED WITH SERVICEABLE PARTS. BOTH OPS CHECKED GOOD REFER TO WORK CARD FOR DETAILS. 2H74 4F4 TRTA49EU E8NE 20050119000412005011900041EU 2005 1 19 MALA040918 120041226A3260 PROXIMITY SWITCH BAC 146 AVRO146RJ85A1500097EU MLG MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15520XJ E2345 RT GEAR INTRANSIT LIGHT REMAINS ON WITH GEAR HANDLE UP. RETURN TO DTW. AC TO BE FERRIED FROM DTW TO MEM GEAR DOWN UNPINNED FOR FURTHER TROUBLESHOOTING / REPAIR FOR RT GEAR INTRANSIT LIGHT. MAINTENANCE CLEANED AND CHECKED ALL PROX SWITCHES. PERFORMED ADJUSTMENT TEST IAW 32-30-00-501 USING DEATUTER (TARGETS) AT GEAR DOOR, UPLOCK WHEELS AND DOWNLOCK SENSORS. WHEN GEAR SELECTED UP RED TRANSIT LIGHT GOES OUT. HANDLE SEL LIGHT ON. AC RELEASED FOR TEST FLIGHT TO PERFORM GEAR UP/DOWN, NO JACKS. A/C REQUIRES TEST FLIGHT TO PERFORM FUNCTIONAL TEST OF LANDING GEAR UP/DOWN FOR RT RED TRANSIT LIGHT. TEST FLT SATISFACTORY. LANDING GEAR TRANSIENT, UP & LOCKED, DOWN AND LOCK ALL NORMAL. A/C GOOD FOR CONT SERVICE. 2H74 4F RTA49EU 20050119000452005011900045EA 2005 1 19 ASOA04947 120041129A5210601R3807413 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050119000462005011900046EU 2005 1 19 ASOA04976 120041206A33507012210 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27642AS 395 FLT 4308 - DURING A GROUND INSPECTION IN ATL, THE RIGHT FRONT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENACNE REMOVED AND REPLACED THE RIGHT FRONT EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050119000472005011900047EA 2005 1 19 A6WA200440221 120041215A3230 BUSHING CNDAIRCL600 CL6002B19 1900309EA LT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 LEFT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. (M) 2L72 4F RTA21EA 20050119000482005011900048EA 2005 1 19 A6WA200440239 120041229A2721 CONTROL PANEL CNDAIRCL600 CL6002B19 1900309EA RUDDER TRIM MALFUNCTIONED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31420AW 7640 ABORTED TAKEOFF DUE TO CONFIG TRIM WARNING. ABORTED AT 60 KNOTS, RUDDER IN GREEN BAND, WILL TRAVEL TO LEFT BUT NOT TO THE RIGHT. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL, IAW AMM 27-10-01, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050119000512005011900051NM 2005 1 19 ASAA0410688 120041129A2560 GLOWSTRIP BOEING737 737210C 1384459NM CABIN FLOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 ANC - LUMINESCENT FLOOR TRACK STRIP DAMAGED BY AFT COAT CLOSET. APPROX 24 INCH SECTION. REPLACED STRIP SECTION. (M) 2L72 4F A16WE 20050119000522005011900052NM 2005 1 19 ASAA0410508 120041108A531165465321 FRAME BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND FRAME GOUGED ON UPPER FLANGE AFT RADIUS BETWEEN STRINGERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND ANGLES IAW SRM. (M) 2L72 4F RTA16WE 20050119000532005011900053NM 2005 1 19 ASAA0410566 120041119A521065C161481 FITTING BOEING737 7372X6C 1384552NM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 AFT CARGO COMPARTMENT MOST LOWER FORWARD DOOR STOP FITTING CHAFED/WORN. REMOVED DAMAGED FITTINGS, ORDERED AND INSTALLED NEW FITTINGS IAW EA. (M) 2L72 4F RTA16WE 20050119000542005011900054NM 2005 1 19 ASAA0410503 120041109A5310652072328 SHEAR TIE BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01747AS 23124 OKC - FOUND FRAME GOUGED ON UPPER FLANGE AFT RADIUS BETWEEN STRINGERS. REMOVED DAMAGED SHEAR-TIE, FABRICATED AND INSTALLED REPAIR FILLERS AND ANGLES PER SRM. (M) 2L72 4F RTA16WE 20050119000552005011900055NM 2005 1 19 ASAA0410507 120041108A57536547928 SKIN BOEING737 7372X6C 1384552NM TE FLAPS CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND RIGHT OUTBOARD MID FLAP CHAFED AT INBOARD LEADING EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOULER IAW SRM. (M) 2L72 4F RTA16WE 20050119000562005011900056NM 2005 1 19 ASAA0410509 120041108A524265458304 DOOR BOEING737 7372X6C 1384552NM E/E BAY DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND E/E DOOR DENTED TWO PLACES ALONG OUTER EDGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW SRM. (M) 2L72 4F RTA16WE 20050119000582005011900058NM 2005 1 19 ASAA0410565 120041119A531065C2518021 DOOR FRAME BOEING737 7372X6C 1384552NM CARGO DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - AFT CARGO DOOR FRAME CRACKED AT FORWARD LOWER CORNER. REMOVED DAMAGED FORWARD LOWER DOOR FRAME CORNER, ORDERED AND INSTALLED A NEW FRAME CORNER IAW SRM. (M) 2L72 4F RTA16WE 20050119000592005011900059EA 2005 1 19 ASOA04998 120041209A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING A-CHECK IN BTR, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119000622005011900062NM 2005 1 19 ASAA0410672 120041130A5347655496921 SEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE MISINSTALLED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: SEAT TRACK REQUIRES REPLACEMENT DUE TO FASTENER EDGE MARGIN. REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E2EA 20050119000642005011900064EA 2005 1 19 ASOA04972 120041205A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27853AS 7374 DURING A GROUND INSPECTION IN ELP, THE BOTTOM STEP SUPPORT FITTING ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119000672005011900067EA 2005 1 19 A6WA200540002 120041229A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31464AW 7890 AIRCRAFT HAS EXTERNAL SKIN DAMAGE AROUND A/C POWER RECEPTACLE. (M) 2L72 4F RTA21EA 20050119000712005011900071NM 2005 1 19 ASAA0410568 120041123A57536571909127 SKIN BOEING737 7372X6C 1384552NM TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND LEFT WING TRAILING EDGE OUTBOARD MID FLAP HAS TWO CHAFED AREAS IN SKIN, LOWER SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS EA AND AAR EA. (M) 2L72 4F RTA16WE 20050119000722005011900072EA 2005 1 19 ASOA04950 120041130A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 625 LEFT PRESSURE BULKHEAD IAW SRM 51-41-06. (M) 2L72 4F RTA21EA 20050118000202005011800020NM 2005 1 18 AWXA200500025 120041229A534069353642 STRINGER CLIP BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT AFT SIDE OF BS 1006, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 1006, STR 14 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35364; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050118000252005011800025NE 2005 1 18 05FDEA00001 220041231A7261 ENGINE DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE NR 3 LEAKING A FDEAO OTHER K FLUID LOSS NRNOT REPORTED 1 SO25583FE346539910 48421 702730 ENGINE 3 OIL QTY DECREASED TO 8 GALLONS AT 4 HOURS AFTER TAKEOFF. QUANTITY DECREASED TO 4 GALLONS EVEN WHILE USING REDUCED POWER ON THAT ENGINE. DIVERTED THE FLIGHT TO EGSS AND QUANTITY WAS AS LOW AS 1 GALLON ON APPROACH. TEMPERATURE AND PRESSURE WERE NORMAL. AFTER LANDING THE ENGINE WAS SHUTDOWN AND QUANTITY INCREASED TO 7 GALLONS. 2L73 4F4 FRTA22WE E31N3 20050118000292005011800029SO 2005 1 18 MASA200400701 120041216A2120 ODOR EMB 145 EMB145LR 3260212SO CABIN DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW07832MJ 145310 ASH 2965 FROM CLT TO GSP REPORTED SMOKE IN THE FLIGHT DECK AND CABIN AND NR 1 ENGINE HAD EVIDENCE OF AN OIL LEAK. MAINTENANCE RAN ENGINE AND FOUND THE NR 1 PACK CAUSING THE SMOKE AND WAS PLACED ON MEL. MAINTENANCE FOUND NO ENGINE OIL LEAKS DURING ENGINE RUN. 12/17 REPLACED CARBON SEAL. 2L72 4T RTT00011AT 20050118000512005011800051EU 2005 1 18 MALA040921 120041230A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 DURING 4K INSPECTION IN BNA, RT FUSELAGE HAS OUT OF LIMIT DENTS BETWEEN FS 307 AND FS 319, AND BETWEEN SL 1616 TO SL 1618. DAMAGE WILL BE REPAIRED IAW MESABA EO S53035. REFER TO EAMS WORK ORDER 211273, TASK 2513 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 1/7/05. 2L72 4T RTA52EU 20050118000582005011800058EA 2005 1 18 MASA200400711 120041220A3350 COVER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 ASH 6389 PHX TO MFR. EMERGENCY LIGHT FLOOR STRIP DAMAGED. MAINTENANCE REPLACED STRIP COVER. 2L72 4F RTA21EA 20050118000722005011800072CE 2005 1 18 DXTA200400500 120041227A3230D45C24 SWITCH CESSNA560 560XL 2076702CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07617QS163 5605509 AFTER GEAR UP/FLAPS UP HAD HYD PRESS, STAB MISCOMPARE ANNUNCIATORS AND UNLOCK GEAR LIGHT. PULL HYD C/B, AND LOUD THUMP HEARD AND FELT IN NOSE GEAR AREA. PUSH HYD C/B IN GET SAME NOISE. ALL LIGHTS OUT AND SYSTEMS WORKED FINE WITH GEAR DOWN AND FLAPS FULL AT LANDING. AFTER T/S VIA CE-560XL MM FOUND HORIZONTAL STAB COMPARE AIRSPEED SWITCH TO FAIL. REPLACED FAILED SWITCH WITH NEW SWITCH IA CE-560XL MM CHAP 27-40-00. CARRIED OUT OPS CHECK STANDBY PITOT/STATIC SYSTEM IAW CE560XL MM CHAP 34-11-08. CARRIED OUT STAB OPS CHECK IAW CE-560XL MM CHAP 27-40-00. ALL CHECK WERE GOOD. JACKED A/C AS REQUIRED. PERFORMED LANDING GEAR FUNCTIONAL TEST. RETRACTED AND EXTENDED LANDING GEAR 30 TIMES, NO DEFECTS NOTED. 2L72 4F RTA22CE 20050118000852005011800085SO 2005 1 18 C2XA05SH002 120041230A532014521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2731131 145705 DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVE THE DAMAGED AREA AND PERFORMED A REPAIR IAW 145XR SRM 53-21-10 FIGURE 201 SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050118000942005011800094SO 2005 1 18 C2XA04IA174 120041227A534014552422401 SUPPORT BRACKET EMB 145 EMB145XR 3260214SO FUSELAGE BROKEN A C2XAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 SW2714116 145672 THE CREW REPORTED AN EXPLOSION SOUND WITH A RUSH OF AIR AND SLIGHT SMOKE ODOR WITH A BLEED LEAK 1 MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE BLEED DUCT BRACKET BETWEEN ROW 19 A&B TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050118001072005011800107NM 2005 1 18 04FDEA03467 120041222A3230656021132 ACCESSORY UNIT BOEING727 727200 138407ENM MLG MALFUNCTIONED A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25469FE 21581 ON GEAR RETRACTION RED GEAR UNSAFE & DOOR LIGHTS ON FRONT PANEL, AND MAIN GEAR DOOR LIGHTS ON S/O PANEL GEAR WAS RECYCLED AND GEAR LIGHTS NOT OUT, WOULD NOT RETRACT. ALL QRH PROCDURES WERE ACCOMPLISHED 7000LBS OF FUEL DUMPED AND AIRCRAFT LANDED AT MEM. JACKED AIRCRAFT AND PERFORMED NORMAL GEAR SWING SEVERAL TIMES IN REFERENCE TO 727-200 AMM 32-32-000-5, GEAR WORKED NORMALLY. AS PRECAUTIONARY REMOVED AND REPLACED LANDING GEAR ACCESORY UNIT IN REFERENCE TO 727-200 AMM 32-09-121-4. PERFORMED LANDING GEAR ELECTRONIC MODULE ADJUSTMENT/TEST IN REFERENCE TO 727-200 AMM 32-09-121-5. ALL TESTS PASSED. AGAIN CYCLED GEAR SEVERAL TIMES AND ALL INDICATIONS AND SWINGS CHECKED GOOD. 2L73 4F RTA3WE 20050118001152005011800115 2005 1 18 0402225516 420041229A22116224591512 COMPUTER BOEING757 757251 1384970NM FLT CONTROL BURNED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL01516US577247188 23204 DURING DESCENT FLIGHT CREW REPORTED ELECTRICAL SMELL IN COCKPIT. FLIGHT ATTENDANT INDICATED FUMES/SMOKE COMING OUT OF OVERHEAD VENTS AND SOME FLOOR VENTS IN CABIN. DECLARED EMERGENCY AND DID AIR CONDITIONING SMOKE/FUME CHECK LIST. SMOKE LESSENED AFTER PACKS/UTILITY BUSSES OFF. AIRCRAFT LANDED UNEVENTFULLY IN MSP. REPLACED FLIGHT CONTROL COMPUTER AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA2NM 20050118001262005011800126SO 2005 1 18 C2XA04IA172 120041227A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716981 145208 DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE RESET THE AIRCRAFT ELECTRICAL SYSTEM, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO PARTS WERE CHANGED. 2L72 4T RTT00011AT 20050118001292005011800129SO 2005 1 18 C2XA04IA176 120041228A3350110049 CHARGER EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2713969 145141 LFT - THE CREW REPORTED, THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. THE AIRCRAFT FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: TIMES/CYCLES NOT TRACKED ON THIS PART. 2L72 4F RTT00011AT 20050119000172005011900017NM 2005 1 19 2005UALA00006 120040101A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 FRAME AT STA 1500 AND STR 26L-25L IS DENTED. 2L72 4F4 FRTA2NM E17NE 20050119000202005011900020NM 2005 1 19 2005UALA00009 120040101A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1460 STR 25L. 2L72 4F4 FRTA2NM E17NE 20050119000262005011900026NM 2005 1 19 2005UALA00016 120041231A2910 HYDRAULIC SYSTEM BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 2 LEAKING A UALAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP29105UA 26473 FLIGHT LOST ALL QUANTITY IN THE NR 2 HYD SYS. LOSS OF FLUID DUE TO CHAFED THRUST REVERSER RETURN HYDRAULIC LINE. MAINTENANCE ALSO NOTED LEAK AT PUMP FLANGE. LEAK AT PUMP FLANGE POSSIBLY DUE TO PUMP FAILURE DUE TO SUBSEQUENT FLUID STARVATION. SYDMM ACCOMPLISHED PERMASWAGE REPAIR OF DAMAGED LINE. NO ADDITIONAL HYD PUMP INFORMATION AVAILABLE FROM OSV AT THIS TIME. 2L74 4F4 FRTA20WE E24NE 20050119000272005011900027NM 2005 1 19 2005UALA00017 120040104A5320 SHEAR WEB BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 CABIN AFT FLOOR SHEAR WEB HAS UPPER SURFACE CORROSION IN AREAS FROM BS 1680-1720 FROM LBL 62 TO RBL 56. 2L72 4F4 FRTA2NM E17NE 20050119000402005011900040EU 2005 1 19 MALA090917 120041224A79334053T73P01 SENSOR SAAB SF340 340B 7860101EU OIL TEMP MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL15424XJ 340B424 LEFT ENGINE OIL TEMP IS HIGH, BORDERING RED LINE. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LT OIL TEMP SENSOR P/N 4053T73P01, S/N ON EGNAN921, S/N OFF LWE79565, ALSO REPLACED LT OIL PRESS & TEMP INDICATOR P/N 522794, S/N ON 230, S/N OFF 9706634A. OPS CHECK GOOD. 2L72 4T RTA52EU 20050119000502005011900050EA 2005 1 19 ASOA04978 120041206A3250481051 SWITCH CNDAIRCL600 CL6002C10 1390015EA NLG STEERING INOPERATIVE A ASOAK NONE J WARNING INDICATION CLCLIMB 1 SO27713EV 10081 DURING CLIMB-OUT FROM BTR-ATL, THE CREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND THE NWS WAS TURNED OFF. THE CREW REQUESTED EMERGENCY VEHICLES BE PUT ON STANDBY AS A PRECAUTION. THE TOWER DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NWS PRESSURE SWITCH. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119000602005011900060NM 2005 1 19 ASAA 120041130A53206546812109 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE LAVATORY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB. 2L72 4F4 FRTA16WE E2EA 20050119000652005011900065EA 2005 1 19 ASOA04971 120041205A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR SILL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE CLIP AT FS 589 LEFT OUTBOARD BY THE CARGO DOOR SILL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 589 LEFT OUTBOARD BY THE CARGO DOOR SILL. (M) 2L72 4F RTA21EA 20050119000692005011900069NM 2005 1 19 ASAA0410558 120041116A53156554907501 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FLOORBEAM CORROSION AT FASTENER HOLES UPPER FLANGE, UPPER AND LOWER SURFACES. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119000742005011900074NM 2005 1 19 ASAA0410502 120041109A53106546595194 SHEAR TIE BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - SHEAR TIE GOUGED IN RADIUS. REMOVED DAMAGED SHEAR TIE, FABRICATED REPLACEMENT SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20050119000752005011900075NM 2005 1 19 ASAA0410522 120041112A53306545800594 SKIN BOEING737 7372X6C 1384552NM FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND LIGHTNING STRIKES OUT OF LIMITS. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLER, AND PLATES IAW EA. (M) 2L72 4F RTA16WE 20050119000762005011900076NM 2005 1 19 ASAA0410520 120041110A53306545768 SKIN BOEING737 7372X6C 1384552NM FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LIGHTNING STRIKES OUT OF LIMITS PER SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER PER SRM. (M) 2L72 4F RTA16WE 20050119000792005011900079NM 2005 1 19 ASAA0410651 120041130A532069428001 SUPPORT FITTING BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, WHILE WORKING LAP REPAIR AT BS 951, STRINGER 10R FOUND SUPPORT FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED SUPPORT FITTING. (M) 2L72 4F RTA16WE 20050119000802005011900080NM 2005 1 19 ASAA0410652 120041130A53206941473 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. (M) 2L72 4F RTA16WE 20050119000812005011900081NM 2005 1 19 ASAA0410653 120041130A5320654585649 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION INTERCOSTAL AND ATTACHMENTS. REPLACED INTERCOSTAL AND ATTACH ANGLES. (M) 2L72 4F RTA16WE 20050119000822005011900082NM 2005 1 19 ASAA0410655 120041130A53206545876501 WEB BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON WEB. REPLACED WEB. (M) 2L72 4F RTA16WE 20050119000832005011900083NM 2005 1 19 ASAA0410656 120041130A5320 WEB BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON WEB. REPLACED WEB. (M) 2L72 4F RTA16WE 20050119000842005011900084EA 2005 1 19 ASOA04974 120041206A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT & RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE LOWER WING PLANKS AT WS 148.019 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANKS AT WS 148.019 LHS/RHS IAW ASA EO 600-57-0134A. (M) 2L72 4F RTA21EA 20050119000862005011900086EA 2005 1 19 A6WA200440236 120041221A7830 THRUST REVERSER CNDAIRCL600 CL6002B19 1900309EA RT ENGINE OBSTRUCTED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31433AW 7289 AFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSER AIRCRAFT FERRIED TO ORD AND PLACED ON MEL. REACTIVATED THRUST REVERSER SYSTEM, OPS CHECK NORMAL. CLEARED MEL. (M) 2L72 4F RTA21EA 20050119000882005011900088EA 2005 1 19 A6WA200540006 120041226A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31449AW 7818 FOUND RIGHT SIDE FS 621-625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED IN RADIUS .6 INCH LONG. REMOVED CRACKED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL IAW CRJ200 SRM 51-42-06. (M) 2L72 4F RTA21EA 20050119000892005011900089EA 2005 1 19 ASOA04986 120041207A2760 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A ASOAO OTHER J WARNING INDICATION CLCLIMB 1 SO27913EV 7731 DURING CLIMB-OUT FROM PHX-DFW, AT APPROXIMATELY 24,000 FT THE CREW RECEIVED 'FLT SPLRS' AND 'SPOILERS' CAUTION MESSAGES AND AN 'IB GRD SPOILERS FAULT' ON THE EICAS. THE QRH WAS COMPLIED AND THE CREW REQUESTED EMERGENCY VEHICLES BE ON STANDBY AS A PRECAUTION. AIR TRAFFIC CONTROL DECLARED AND EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE FOUND SPOILER ELECTRONIC CONTROL UNIT 2B FAIL BITS POSTED AND SECU 2 FAILED A1 POSTED, AND REMOVED AND REPLACED THE RIGHT SECU. MAINTENANCE ALSO PERFORMED A SYSTEM BITE TEST. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119000902005011900090NM 2005 1 19 ASAA0410667 120041130A532065458856 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON UNDERSIDE AT WEB. REPLACED WEB. 2L72 4F4 FRTA16WE E2EA 20050119000912005011900091EA 2005 1 19 ASOA04991 120041209A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, LBL 36, RBL 36 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, LBL 36, RBL 36 AND RBL 27 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050119000922005011900092EA 2005 1 19 ASOA04990 120041209A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY CLIP AT FS 625 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIP AT FS 625 LEFT. (M) 2L72 4F RTA21EA 20050119000932005011900093EA 2005 1 19 ASOA04994 120041209A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 UNDER THE FIRE LOOP CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20050119000942005011900094EA 2005 1 19 ASOA04985 120041207A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE FLOORBEAM AT FS 574-621 WERE FOUND TO BE CORRODED BEYOND LIMIT. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOORBEAMS AT FS 574-621. (M) 2L72 4F RTA21EA 20050119000952005011900095EA 2005 1 19 ASOA04981 120041206A3210HB12TF200BS CLAMP CNDAIRCL600 CL6002B19 1900309EA LANDING GEAR DAMAGED A ASOAO OTHER O OTHER CLCLIMB 1 SO27915EV 7754 FLT 4773 - DURING TAKEOFF ROLL FROM FNT-CVG, AT APPROXIMATELY 130 KNOTS THE RIGHT MAIN LANDING GEAR MLG STRUCK A COYOTE. GEAR RETRACTION AND SUBSEQUENT TAKEOFF WERE NORMAL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE FOUND ANIMAL REMAINS AND DAMAGE TO TWO BAND CLAMPS ON THE RIGHT MLG WHICH WERE REPLACED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001012005011900101NM 2005 1 19 ASAA0410629 120041130A534765549688 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001022005011900102NM 2005 1 19 ASAA0410638 120041130A53206505693 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON INTERCOSTAL AT BS 953. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20050119001032005011900103NM 2005 1 19 ASAA0410646 120041130A532069414737 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20050119001042005011900104EA 2005 1 19 ASOA04979 120041206A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27907EV 7648 DURING HANGAR MAINTENANCE IN BTR, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS PERFORMING A TEMPORARY REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW BOMBARDIER RO NR 601R-53-61-361. (M) 2L72 4F RTA21EA 20050119001062005011900106EA 2005 1 19 A6WA200440235 120041223A2150 ODOR CNDAIRCL600 CL6002B19 1900309EA RT A/C PACK DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31413AW 7585 AFTER TURNING ON RT PACK, CABIN FILLED WITH SMOKE AND SMELLED LIKE OIL. INSPECTED SYSTEM AND RT PACK FOUND NO DEFECTS. PERFORMED OPS OF SYSTEM. SYSTEM OPS NORMAL. (M) 2L72 4F RTA21EA 20050119001082005011900108EA 2005 1 19 ASOA04982 120041206A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FLOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AREA AT FS 484 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE PRESSURE FLOOR AREA AT FS 484 LEFT. (M) 2L72 4F RTA21EA 20050119001092005011900109EA 2005 1 19 ASOA04948 120041129A2560111RJ7001 GLOWSTRIP CNDAIRCL600 CL6002C10 1390015EA CABIN TORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27718EV 10095 FLT 4535 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY PHOTOLUMINESCENT FLOOR STRIP WAS FOUND TORN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY PHOTOLUMINESCENT FLOOR STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001102005011900110SO 2005 1 19 SIMA200434215 120041201A532014521719003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21634AE 145150 DURING CPCP INSPECTION, FOUND OMEGA BEAM FRAME 20 LT, ABOVE STRINGERS 18-19L IS CORRODED AT CARBON CROSSBEAM. REPAIRED OMEGA BEAM IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050119001112005011900111EA 2005 1 19 ASOA04980 120041206A2840 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA FUEL SYSTEM FALSE ACTIVATIONA ASOAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27867AS 7463 FLT 4722 - DURING CLIMB-OUT FROM ATW-ATL, THE CREW NOTICED A FUEL DISCREPANCY AND LOSS OF 1,800 LBS WITH A CONINUING LOSS OF 10 LBS PER SECOND ACCOMPANIED BY SPORADIC FUEL TOTALIZER READINGS. AN EMERGENCY WAS DECLARED. FUEL LOSS READINGS CONTINUED TO FLUCTUATE BETWEEN 10 LBS PER SECOND TO 500 LBS PER MINUTE. THE AIRCRAFT DIVERTED TO ORD AND LANDED SAFELY. MX CHECKED FOR LOGGED FAULTS. NO FAULTS WERE FOUND AND THEN RESET THE FUEL COMPUTER. ALL READINGS WERE NORMAL. MAINTENANCE ALSO SUMPED THE FUEL TANKS FOR WATER. NO FAULT CODES WERE FOUND ON THE FUEL QUANTITY GAUGING COMPUTER OR THE MX DIAGONISTIC COMPUTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001132005011900113NM 2005 1 19 ASAA0410639 120041124A53306545829505 BEAR STRAP BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON BEAR STRAP AT BS 348. REPAIRED PER EA 5310-02415. (M) 2L72 4F RTA16WE 20050119001142005011900114NM 2005 1 19 ASAA0410643 120041126A532065528792 WEB BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND WEB CRACKED AT LOWER END. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20050119001152005011900115EA 2005 1 19 ASOA04975 120041206A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20050119001162005011900116 2005 1 19 A6WA200440238 420041227A34206229336400 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AVIONICS BAY MALFUNCTIONED A A6WAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31403AW5121 1758 7288 CAPTAINS SIDE 'RED MAG' INDICATION ON PFD1 PRIOR TO TAKEOFF. TAKEOFF ABORTED, AIRSPEED LESS THAN 40 KNOTS. REMOVED AND REPLACED AHRS NR 1 UNIT IAW/AMM 34-21-01, OPS CHECK GOOD. (M) 2L72 4F RTA21EA 20050119001192005011900119NM 2005 1 19 ASAA0410663 120041130A53306546558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050119001202005011900120EA 2005 1 19 ASOA04951 120041130A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE LEFT FS 280 INBOARD CLIP AND THE RIGHT FS 280 INBOARD AND OUTBOARD CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT FS 280 INBOARD CLIP AND THE RIGHT FS 280 INBOARD AND OUTBOARD CLIPS. (M) 2L72 4F RTA21EA 20050119001222005011900122EA 2005 1 19 ASOA04996 120041209A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DIRTY A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 FLT 4316 - DURING A GROUND INSPECTION IN DFW, THE FIRST SECTION OF EMERGENCY FLOOR LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE FIRST SECTION OF EMERGENCY FLOOR LIGHTS CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001242005011900124NM 2005 1 19 ASAA0410593 120041121A53306545767506 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001252005011900125NE 2005 1 19 ASOA04965 220041203A7200 ENGINE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LEFT ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27632AS 338 FLT 4131 - DURING DESCENT INTO ATL FROM PFN, THE CREW NOTICED A SMELL SIMILAR TO DIRTY SOCKS WHEN ENGINE POWER WAS INCREASED. NO SMOKE OR BURNING ODOR OCCURRED. THE DIRTY SOCK SMELL DISSIPATED SHORTLY AFTERWARDS AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPS AND LEAK CHECKS GOOD DURING ENGINE RUNS. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20050119001272005011900127NM 2005 1 19 ASAA0410552 120041116A53206517684654 ANGLE BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - L-ANGLE CRACKED BS 292, 11 INCHES BELOW STRINGER 15L. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001292005011900129NM 2005 1 19 ASAA0410525 120041112A531065671407 BEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LONGITUDINAL BEAM HAS CORROSION. REMOVED DAMAGE, COMPLIED WITH HFEC INSPECTION AND NO DEFECTS NOTED. FLAP PEENED AFFECTED AREA. FABRICATED AND INSTALLED REPAIR FILLERS, STRAPS, AND WASHERS IAW EA. (M) 2L72 4F RTA16WE 20050119001302005011900130NM 2005 1 19 ASAA0410612 120041124A53406552928592 STRINGER CLIP BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP PER SRM. (M) 2L72 4F RTA16WE 20050119001312005011900131NM 2005 1 19 ASAA0410614 120041130A534765549696 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001322005011900132NM 2005 1 19 ASAA0410607 120041123A57536571909107 SKIN BOEING737 7372X6C 1384552NM MID FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - DURING C-CHECK, LEFT OUTBOARD MID FLAP UPPER SURFACE HAS A DENT INBOARD OF NR 1 FLAP SPINDLE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-20. (M) 2L72 4F RTA16WE 20050119001332005011900133NM 2005 1 19 ASAA0410613 120041124A53116546550 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FRAME DOUBLER AT BS 787, STRINGER 23R, WL 156. REMOVED, FABRICATED AND INSTALLED FRAME DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20050119001342005011900134NM 2005 1 19 ASAA0410665 120041130A5347BAC152014347178TSEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON LWR SURFACE OF SEAT TRACK. REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E2EA 20050119001362005011900136NM 2005 1 19 ASAA0410661 120041130A53306548600 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON EXTERNAL SKIN AT WING-TO-BODY FAIRING. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001372005011900137NM 2005 1 19 ASAA0410526 120041112A5311654655045 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND FRAME CORRODED BETWEEN 26 AND 20L AROUND NUMEROUS NUTPLATES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. (M) 2L72 4F RTA16WE 20050119001382005011900138NM 2005 1 19 ASAA0410611 120041124A53406552928593 STRINGER CLIP BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON STRINGER CLIP. REMOVED, FABRICATED AND INSTALLED STRINGER CLIP PER SRM. (M) 2L72 4F RTA16WE 20050119001392005011900139NM 2005 1 19 ASAA0410500 120041109A5315655490510 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FLOORBEAM HAS CORROSION. REMOVED DAMAGE, REMOVED PRE-EXISTING REPAIRS, FLAT PEENED, TREATED, PRIMED, TOPCOATED, AND REINSTALLED PRE-EXISTING REPAIRS IAW EA. (M) 2L72 4F RTA16WE 20050119001412005011900141NM 2005 1 19 ASAA0410549 120041116A533065458001126 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CRACK INDICATIONS AT SKIN LAP. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001432005011900143NM 2005 1 19 ASAA0410535 120041116A27506571909128 JACKSCREW BOEING737 7372X6C 1384552NM RT WING TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND RIGHT WING OUTBOARD MID FLAP BEHIND OUTBOARD JACKSCREW IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLED BLENDED AREA IAW AS AND AAR EA. (M) 2L72 4F RTA16WE 20050119001442005011900144NM 2005 1 19 ASAA0410559 120041116A53306545477761 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE AT STRINGER 14L, BS 907-947. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001452005011900145EA 2005 1 19 A6WA200440234 120041222A32306229820008 DCU CNDAIRCL600 CL6002B19 1900309EA NR 2 MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31408AW 7568 AFTER ROTATION AND GEAR UP RECEIVED SEVERAL M/C'S AND WINDSHEAR NOSE GEAR DOOR, DISAGREE AND STEERING INOPERATIVE FOLLOWED QRH RETURNED TO CKB WITHOUT INCIDENT. POWERED DOWN AC REMOVED AND RERACKED NR 2 DCU, OPS IAW CRJ AMM 31-41-04. OPS GOOD, NOTE GROSS AT LOG 36200, NO OVERWEIGHT INSPECTION REQUIRED. (M) 2L72 4F RTA21EA 20050119001462005011900146NM 2005 1 19 ASAA0410545 120041117A531065549307 DOOR FRAME BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - MAIN CARGO DOOR FRAME CRACKED. REPLACED FRAME PER SRM. (M) 2L72 4F RTA16WE 20050119001482005011900148NM 2005 1 19 ASAA0410560 120041116A5330654577761 SKIN BOEING737 7372X6C 1384552NM FS DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DAMAGE AT STRINGER 14L, BS 986-1016. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001492005011900149NM 2005 1 19 ASAA0410550 120041116A533065458001126 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE APPROX 2 INCHES LONG. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001502005011900150EA 2005 1 19 ASOA04983 120041206A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FLOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15 LT/RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOOR PRESSURE FLOOR BETWEEN FS 449.85-473.15 LEFT AND RIGHT. (M) 2L72 4F RTA21EA 20050119001512005011900151EA 2005 1 19 ASOA04984 120041207A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FLOOR CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AREA AT FS 484-559, BL 36 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE FLOOR PRESSURE FLOOR AT FS 484-559, BL 36 LEFT. (M) 2L72 4F RTA21EA 20050119001522005011900152NM 2005 1 19 ASAA0410551 120041116A533065458001126 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DAMAGE APPROX 21 INCHES LONG. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001532005011900153NM 2005 1 19 ASAA0410553 120041116A533065458001126 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE AT SKIN LAP. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001542005011900154NM 2005 1 19 ASAA0410547 120041117A533065458001126 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001562005011900156NM 2005 1 19 ASAA0410536 120041116A531065671408 BEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - LONGITUDINAL BEAM BETWEEN STATION 540-727B BL 0, HAS CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRAP AND FILLERS BLENDED AREA IAW AS AND AAR EA. (M) 2L72 4F RTA16WE 20050119001572005011900157NM 2005 1 19 ASAA0410654 120041130A5247655090426 FRAME BOEING737 7372X6C 1384552NM APU DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CHAFED FRAME ON APU ACCESS DOOR. REPLACED FRAME. (M) 2L72 4F RTA16WE 20050119001582005011900158NM 2005 1 19 ASAA0410689 120041129A33508731002142 LIGHT BOEING737 737210C 1384459NM EMERGENCY EXIT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 ANC - SMOKE BARRIER EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M) 2L72 4F A16WE 20050119001592005011900159NM 2005 1 19 ASAA0410563 120041119A53206545812501 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - INTERCOSTAL CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM. (M) 2L72 4F RTA16WE 20050119001602005011900160NM 2005 1 19 ASAA0410649 120041130A5330654577872 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON SKIN. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001612005011900161NM 2005 1 19 ASAA0410650 120041130A5320694147301 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, REJECTION INTERCOSTAL IS STILL CRACKED, FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL. (M) 2L72 4F RTA16WE 20050119001622005011900162NM 2005 1 19 ASAA0410660 120041130A5510654684511 HOUSING BOEING737 7372X6C 1384552NM LT STAB HINGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND LEFT CENTER SECTION HINGE DAMAGED AT CENTER SECTION ATTACH POINT. REPLACED LT STAB HINGE HOUSING. (M) 2L72 4F RTA16WE 20050119001632005011900163NM 2005 1 19 ASAA0410537 120041116A5330654577656 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FUSELAGE EXTERIOR LOWER SKIN CORRODED FROM STATION 927 TO 947 BETWEEN 26L AND 27L. REMOVED DAMAGE, AND EXISTING DOUBLER, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW AS AND AAR EA. (M) 2L72 4F RTA16WE 20050119001652005011900165NM 2005 1 19 ASAA0410504 120041107A53156546568519 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND FLOORBEAM HAS CORROSION AT TOP FLANGE. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM T-CAP IAW EA. (M) 2L72 4F RTA16WE 20050119001662005011900166EA 2005 1 19 ASOA04993 120041209A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLES AT FS 621 LT/RT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 LEFT/RIGHT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050119001672005011900167NM 2005 1 19 ASAA0410642 120041130A5320654795617 BRACKET BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON BRACKET. REMOVED AND REPLACED BRACKET PER SRM. (M) 2L72 4F RTA16WE 20050119001682005011900168NM 2005 1 19 ASAA0410647 120041130A532069414736 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND FORWARD CARGO BAY INTERCOSTAL IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20050119001702005011900170NM 2005 1 19 ASAA0410594 120041121A53306545767592 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DAMAGED ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001712005011900171EU 2005 1 19 ASOA04969 120041205A3397MS22759 WIRE AEROSPATR72 ATR72 EU EMERGENCY LIGHT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27643AS 413 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE TO THE EMERGENCY LIGHT ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050119001732005011900173EU 2005 1 19 ASOA04963 120041202A3350LP1670 LAMP AEROSPATR72 ATR72 EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27630AS 336 DURING AN A-CHECK IN MCN, THE EMERGENCY FLOOR LIGHT TRACK AT ROW 15B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 15B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RT 20050119001752005011900175EA 2005 1 19 ASOA04995 120041209A335061000976 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27717EV 10088 DURING AN A-CHECK IN BTR, THE SECOND FROM AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001762005011900176EA 2005 1 19 ASOA04952 120041130A5340601R3117117 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050119001772005011900177EA 2005 1 19 ASOA04961 120041202A5210601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27889AS 7538 DURING AN A-CHECK IN MCN, THE PASSENGER DOOR TOP STEP AT THE RIGHT REAR SECTION WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP. (M) 2L72 4F RTA21EA 20050119001812005011900181NM 2005 1 19 ASAA0410666 120041130A5347BAC15201432 SEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 SW15746AS 23123 PAE, D-CHECK: CROWN TOOTH DAMAGED ON SEAT TRACK. REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E2EA 20050119001822005011900182NM 2005 1 19 ASAA0410644 120041126A53206547955500 ANGLE BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE IN FASTENER HOLE ON L ANGLE. REMOVED AND REPLACED L ANGLE PER SRM. (M) 2L72 4F RTA16WE 20050119001832005011900183NM 2005 1 19 ASAA0410645 120041130A532065528772 WEB BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, WEB AT STATION 980 HAS A CRACK. REMOVED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20050119001842005011900184NM 2005 1 19 ASAA0410673 120041130A534765549892 SEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E2EA 20050119001852005011900185NM 2005 1 19 ASAA0410624 120041130A534765549721 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK AT BS 947. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001872005011900187NM 2005 1 19 ASAA0410634 120041130A532069530062 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON FLOORBEAM INTERCOSTAL AT FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20050119001922005011900192NM 2005 1 19 ASAA0410605 120041122A53306545772155 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DAMAGED ON SKIN. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001942005011900194EA 2005 1 19 ASOA04956 120041130A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 LT/RT IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20050119001952005011900195EA 2005 1 19 ASOA04955 120041130A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA CENTER ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M) 2L72 4F RTA21EA 20050119001962005011900196EU 2005 1 19 ASOA04954 120041130A2150 A/C PACK AEROSPATR72 ATR72212 8680945EU LEFT ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27632AS 338 FLT 4374 - DURING DESCENT INTO ATL FROM AGS, THE CREW NOTICED A MUSTY ODOR IN THE COCKPIT WHEN AIRCRAFT POWER WAS REDUCED FROM THE CRUISE POWER SETTING. NO FUMES OR SMOKE WAS OBSERVED. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE DEFERRED THE LEFT PACK IAW MEL NR 21-50-1. CAT C EXPIRING ON 12/10/04. AIRCRAFT OK FOR SREVICE. (M) 2H72 4T RTA53EU 20050119001972005011900197EA 2005 1 19 ASOA04968 120041204A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SUPPORT ANGLE AT FS 621 RT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050119001982005011900198NM 2005 1 19 ASAA0410616 120041130A5347655496816 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FLOOR SEAT TRACK FLANGE. REMOVED AND REPLACED SEAT TRACK. (M) 2L72 4F RTA16WE 20050119002002005011900200NM 2005 1 19 ASAA0410505 120041107A53156546811510 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND FLOORBEAM HAS CORROSION AT TOP FLANGE. REMOVED DAMAGED REPAIR, FABRICATED AND INSTALLED REPAIR TEE CHORD, TRIPLER ANGLE, SPLICE ANGLE, REPAIR STRAP, TRIPLER STRAP, AND FILLER IAW EA. (M) 2L72 4F RTA16WE 20050119002012005011900201NM 2005 1 19 ASAA0410628 120041130A534765549685 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119002022005011900202NM 2005 1 19 ASAA0410630 120041130A53206554829501 WEB BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON WEB. REMOVED, FABRICATED AND REPLACED WEB PER SRM. (M) 2L72 4F RTA16WE 20050119002032005011900203NM 2005 1 19 ASAA0410631 120041129A5330654577259 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE ON EXTERNAL SKIN AT BS 908-913. REPAIRED PER EA 5330-01841. (M) 2L72 4F RTA16WE 20050119002042005011900204NM 2005 1 19 ASAA0410590 120041122A53306545767541 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DENT IN EXTERNAL SKIN UNDER PREVIOUSLY INSTALLED REPAIR. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119002062005011900206NM 2005 1 19 ASAA0410668 120041130A53206546812109 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE LAVATORY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON LAV WEB. REPLACED WEB. 2L72 4F4 FRTA16WE E2EA 20050119002072005011900207NM 2005 1 19 ASAA0410601 120041122A53306546776531 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119002082005011900208NM 2005 1 19 ASAA0410636 120041130A5320694147315 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND INTERCOSTAL IS CRACKED AT BS 400-420. REMOVED AND REPLACED INTERCOSTAL PER SRM. (M) 2L72 4F RTA16WE 20050119002102005011900210NM 2005 1 19 ASAA0410596 120041122A5313169875ASA SPLICE BOEING737 7372X6C 1384552NM STRINGER CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION ON STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE AND CLIP. (M) 2L72 4F RTA16WE 20050119002122005011900212EA 2005 1 19 ASOA04953 120041130A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050119002142005011900214EA 2005 1 19 ASOA04970 120041205A5340601R311719 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE CLIPS AT FS 484, LBL 27 AND RBL 27 INBOARD AND THE CLIPS AT FS 484, LBL 36 AND RBL 36 OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS AT FS 484, LBL 27 AND RBL 27 INBOARD AND REPAIRING THE CLIPS AT FS 484, LBL 36 AND RBL 36 OUTBOARD IAW ASA EO 600-53-0098. (M) 2L72 4F RTA21EA 20050118000402005011800040SO 2005 1 18 C2XA04IA171 120041224A335020131A BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27115486778 1553 145565 DURING SCHEDULED MAINTENANCE THE NR 2 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO HAVE LOW VOLTAGE. THE AFFECTED BATTERY WAS REMOVED AND REPLACED, THE LIGHTING SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. 2L72 4T RTT00011AT 20050118000592005011800059NM 2005 1 18 MASA200400715 120041220A3397 WIRE HARNESS DHAV DHC8 DHC8202 2809007NM EMERGENCY SIGN DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07448YV 448 EMERGENCY EXIT SIGN OVER CABIN DOOR INOP. MAINTENANCE RECONNECTED THE HARNESS. OPS CHECKED GOOD. 2H72 4T RTA13NM 20050118000602005011800060EA 2005 1 18 MASA200400716 120041221A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAO OTHER L NO TEST NRNOT REPORTED 1 SW0717231 7231 ASH 6152 PHX-SBA. CREW REPORTED AN OVERHEAD EMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE BULB, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050118000642005011800064EA 2005 1 18 MASA200400727 120041226A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0777302 7302 ASH 6336 PHX. PILOT REPORTED THE EXIT PATH LIGHTING STRIP WAS INOP. MX RECONNECTED THE LIGHT STRIP PLUG. 2L72 4F RTA21EA 20050118000732005011800073CE 2005 1 18 DXTA200400501 120041227A3240216011 BRAKE CESSNA560 560XL 2076702CE MLG FIRE E DXTAO OTHER A FLAME/FIRE TXTAXI/GRND HDL 1 GL07626QS1115 5605126 ON TAXI IN, GROUND PERSONNEL NOTICED THE LT WHEEL WELL HAD A FIRE, FLIGHT CREW DID NOT NOTICE ANY GRINDING, PULLING, OR VIBRATION INDICATING A PROBLEM. INSPECTED LT MAIN LANDING GEAR AND SURROUNDING WING AREA FOR DAMAGE, NONE NOTED. REMOVED LT MAIN WHEEL ASSY P/N 9912487-1, S/N 0410, TIRE P/N M13701, S/N 3296A051, LT MAIN BRAKE ASSY REMOVED P/N 2-1601-1, S/N 0532. INSTALLED OVERHAULED BRAKE ASSY. INSTALLED REPAIRED WHEEL ASSY P/N 3-1571-2, S/N 0987. WORK DONE IAW CESSNA 560XL MM 32-42-00, 32-42-01, 32-42-02. 2L72 4F RTA22CE 20050118000742005011800074SO 2005 1 18 LR7A04201 120041229A335044910 LIGHT LKHEED382 382G 526414USO CABIN INOPERATIVE A LR7AK NONE L NO TEST ININSP/MAINT 1 AL03402LC 40 4698 DURING SCHEDULED A CHECK PER JOB CARD HA1200 FLIGHT DECK LOWER EMERGENCY LIGHT FAILED FUNCTIONAL CHECK. REPLACED LIGHT ASSY. OPS CHECK GOOD IAW SMP 581 33-50. 2H74 4T A1SO 20050118000782005011800078NM 2005 1 18 04FDEA03459 120041221A32103914016 UNLOCK CYLINDER DOUG MD11 MD11 3023602NM ZONE 700 INOPERATIVE A FDEAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO25579FE 48470 ON TAKEOFF RIGHT MAIN GEAR UNSAFE INDICATION BOTH SYSTEM, COULD FEEL DRAG. CYCLED GEAR OPERATED NORMALLY. T/S RIGHT MLG RETRACT FUNCTION AS PER FIM 32-30-00 FIG 103, WITH A/C ON JACKS AND LANDING GEAR SWING TEST AS PER MM 32-31-00-5 & 07-11-00. PHYSICAL CHECK RIGHT GEAR DOOR LATCH, GEAR POSITION FOLLOW-UP CABLES AND PUSH RODS ALL CONDITION NORMAL PER 32-34-05-5 AND 32-31-00-5. TEST LANDING GEAR RETRACT TIME PASSED AS PER TASK 32-31-00-700-804. CONTINUE OPS LANDING GEARS FOR TWO HOURS MORE THAN FORTY TIMES, STILL UNABLE TO DUPLICATE PROBLEM. REMOVED AND REPLACED RT MLG UNLOCK CYLINDER PER MM 32-33-02-4. LUBRICATED RT LANDING GEAR/DOOR PER MM 12-21-00. A/C OK FOR SERVICE. 2L73 4F RTA22WE 20050118000802005011800080SO 2005 1 18 SWIA200414323 120041228A3350 BULB EMB 120 EMB120ER 3260203SO EMERGENCY LIGHT BURNED OUT A SWIAO OTHER L NO TEST NRNOT REPORTED 1 NM07580SW 120348 FLOOR EMERGENCY LIGHTING, FIRST WHITE LIGHT INOPERATIVE. REPLACED LAMP FIRST WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050118000812005011800081EA 2005 1 18 SWIA200414324 120041226A5610 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07408SW 7055 DURING PREFLIGHT FOUND LARGE CRACK IN RIGHT WINDSHIELD. REPLACED RIGHT WINDSHIELD IAW CRJ MM 56-00-00, 56-11-01, 56-12-01. 2L72 4F RTA21EA 20050118000912005011800091SO 2005 1 18 C2XA04TY180 120041212A531014525175001 SHEAR TIE EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714939 145030 DURING C-CHECK THE LEFT AND RIGHT FRAME 65 AND FRAME 68 SHEAR CLIPS WERE FOUND CORRODED. REPAIRED IAW SRM 51-30-01 AND IC2004-145/5946. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050118000932005011800093SO 2005 1 18 C2XA04IA173 120041227A2913971808MODA PUMP EMB 145 EMB145LR 3260212SO NR 2 ENGINE LEAKING A C2XAH DEACTIVATE SYST/CIRCUITS KSJFLUID LOSS AFFECT SYSTEMS WARNING INDICATION CRCRUISE 1 SW27169769873 9873 145171 THE CREW REPORTED THAT IN CRUISE, THE NR 2 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONAL AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20050118000992005011800099SO 2005 1 18 C2XA04CL117 120041116A2612 CONNECTOR SUNDSTRANDEM EMB 145 EMB145LR 3260212SO APU LOOSE A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW2713997 SPE0114169 145298 IN CRUISE CREW REPORTED APU FIRE MESSAGE DURING APU START. MESSAGE WENT AWAY AFTER APU GOT TO FULL SPEED. CREW SHUT DOWN APU AND CONTINUED FLIGHT. INSPECTED APU, NO SIGN OF FIRE AND CLEANED THE APU FIRE LOOP CONNECTOR AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050118001002005011800100SO 2005 1 18 C2XA04CL122 120041201A2121BWT138005 NOISE ATTENUATOR EMB 145 EMB145ER 3260211SO RECIRC FAN RUPTURED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW2717928 145007 DURING APPROACH THE CREW REPORTED A BURNING PLASTIC SMELL. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RUPTURED NR 2 RECIRCULATION FAN NOISE ATTENUATOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050118001062005011800106NM 2005 1 18 04FDEA03466 120041222A5347 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK, SEAT TRACK RBL 107 FOUND WITH SCRATCHES AT STA 1665 TO STA 1721. REPLACEMENT CARRIED OUT AT MAIN DECK RBL 107 STA 1531 TO STA 2007 2L73 4F RTA22WE 20050118001162005011800116SO 2005 1 18 C2XA04IA116 120040906A33502013BR BATTERY PACK EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711165614 614 14500819 DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AND THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK WAS WEAK. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050118001172005011800117SO 2005 1 18 C2XA04IA130 120041016A261247359713 SMOKE DETECTOR EMB 145 EMB145 3260210SO CARGO BAY INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW27139706936 145146 DURING CRUISE, CREW REPORTED A CARGO COMPARTMENT FIRE WARNING. BOTH FIRE BOTTLES WERE DISCHARGED AND AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. REMOVED AND REPLACED DEFECTIVE CARGO COMPARTMENT SMOKE DETECTOR AND FIRE BOTTLES. OPERATIONALLY CHECK OK. 2L72 4F RTT00011AT 20050118001202005011800120SO 2005 1 18 C2XA04IA131 120041017A27503631001007 CONTROL UNIT EMB 145 EMB145LR 3260212SO TE FLAP MALFUNCTIONED A C2XAO OTHER J WARNING INDICATION APAPPROACH 1 SW27139559661 145075 DURING FINAL APPROACH CREW REPORTED FLAP FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED AT JAX WITH INCIDENT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT, OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050118001232005011800123SO 2005 1 18 C2XA04SH522 120041021A323414532170401 CONTROL LEVER EMB 145 EMB145LR 3260212SO MLG DEFECTIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713955 145075 DURING CLIMBOUT OF BNA GEAR SELECT UP AND GEAR DID NOT RETRACT. AIRCRAFT DIVERTED TO SHV AND LANDED WITH OUT INCIDENT. REPLACED THE LANDING GEAR CONTROL LEVER AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050118001322005011800132SO 2005 1 18 C2XA05SH001 120041230A533012022656048 SKIN EMB 145 EMB145XR 3260214SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2731131 145705 DURING C-CHECK THE FUSELAGE EXTERNALLY HAS 2 GOUGES BETWEEN FR 2 AND 3 STR 17 R. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EMB 145XR SRM 53-11-01 FIG 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050118001392005011800139SO 2005 1 18 C2XA04CL131 120041226A335020131A BATTERY EMB 145 EMB145 3260210SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27149724986 145151 THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050118001452005011800145SO 2005 1 18 C2XA04CL129 120041222A21508152914 SWITCH EMB 145 EMB145ER 3260211SO NR 2 PACK FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2717928 145007 CLE - THE CREW REPORTED IN FLIGHT, IN ICING HAD A VERY HOT RUBBER SMELL AND PACK 2 AIR WAS VERY HOT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PACK DUCT OVERTEMP SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20050118001792005011800179WP 2005 1 18 05FDEA00043 120040814A5330NYB60083 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25374FE 46612 NOT APPROVED FUSELAGE SKIN REPAIR AT LT AND RT LONG 44-47, STA 1526. SUBJECT REPAIRS WERE INSPECTED FOR COMPLIANCE WITH 14CFR 121.368, THE REPAIRS WERE EVALUATED TO BE ACCEPTABLE AS PERMANENT, PROVIDED REPAIRS ARE MODIFIED BY FEDEX EA 8-5310-84848. 2L73 4F RTA22WE 20050118002002005011800200SO 2005 1 18 LR7A04202 120041231A5340 ATTACH FITTING LKHEED382 382G 526414USO BULKHEAD CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03405LC 648 5025 DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND RT AFT FUSELAGE BULKHEAD STRUT LOWER ATTACH FITTING CRACKED AT FS 858, WL 202.0, RBL 62. ATTACH FITTING REPLACED IAW SMP583 CHP 51-10. 2H74 4T A1SO 20050119000182005011900018NM 2005 1 19 2005UALA00007 120040101A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L. 2L72 4F4 FRTA2NM E17NE 20050119000492005011900049SO 2005 1 19 SIMA200434214 120041201A532014521725613 WEB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21634AE 145150 DURING CPCP INSPECTION, FOUND WEB AT FRAME 17 TO 20R FORWARD OF SERVICE DOOR HAS SPOTS OF CORROSION ON UPPER SURFACE. INSTALLED NEW WEB IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050119000572005011900057NM 2005 1 19 ASAA0410510 120041106A5330654580027 SKIN BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 FOUND R1 DOOR CUTOUT FUSELAGE SKIN CRACKED TWO PLACES LOWER AFT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLER, AND TRIPLER IAW SRM. (M) 2L72 4F RTA16WE 20050119000612005011900061EA 2005 1 19 ASOA04989 120041208A5310601R3501153 PLATE CNDAIRCL600 CL6002B19 1900309EA CARGO DOOR SILL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO DOOR FLOOR SILL PLATE IAW ASA EO 600-53-0117. (M) 2L72 4F RTA21EA 20050119000632005011900063NM 2005 1 19 ASAA0410591 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGEON EXTERNAL SKIN. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119000732005011900073EA 2005 1 19 ASOA04988 120041208A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE PRESSURE FLOOR AT FS 473-559 RT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS SUBMITTING A REPAIR REQUEST TO BOMBARDIER FOR AN REO TO REPAIR THE PRESSURE FLOOR AT FS 473-559 RT. (M) 2L72 4F RTA21EA 20050119000852005011900085SO 2005 1 19 SIMA200434213 120041201A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21634AE 145150 DURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED ON TOP SURFACE AROUND NUT PLATES. REPLACED SERVICE DOOR SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.(K) 2L72 4T4 FRTT00011ATTE6CH 20050119001002005011900100NM 2005 1 19 ASAA0410625 120041130A5347655496810 SEAT TRACK BOEING737 7372X6C 1384552NM CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK FLANGE AT STATION 480. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001052005011900105EA 2005 1 19 A6WA200440233 120041222A3213 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG DISCHARGED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31408AW 7568 AFTER ROTATION AND GEAR UP RECEIVED SEVERAL MESSAGES NOSE DOOR, GEAR DISAGREE, WOW INPUT AND STEERING INOP. FOLLOWED QRH PROCEDURES LANDED WITH NOSE STEERING INOPERATIVE. SERVICED NLG STRUT IAW CRJ AMM 12-12-32B REFERENCE AWAC W/O NR 77064 FOR DETAILS OF WORK PERFORMED KMCBICK 6735 CRSWVER835K. (M) 2L72 4F RTA21EA 20050119001122005011900112EA 2005 1 19 ASOA04949 120041130A7120 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE RT ENGINE SUPPORT BEAM AT BL 36.20 INBOARD FORWARD CORNER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M) 2L72 4F RTA21EA 20050119001182005011900118EA 2005 1 19 ASOA04999 120041209A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 IAW ASA EO 600-57-039A. (M) 2L72 4F RTA21EA 20050119001402005011900140NM 2005 1 19 ASAA0410615 120041125A551165499256 SPAR BOEING737 7372X6C 1384552NM HORIZONTAL STAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND HORIZ STAB CENTER SECTION, UPPER AFT SPAR CHORD IS CRACKED. REPAIRED PER EA 5210-01203. (M) 2L72 4F RTA16WE 20050119001552005011900155NM 2005 1 19 ASAA0410548 120041117A533065458001126 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119001782005011900178EU 2005 1 19 ASOA04959 120041201A3350E0029387 LAMP AEROSPATR72 ATR72212 8680945EU EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27637AS 383 DURING HANGAR MAINTENANCE IN MCN, THE FORWARD TWO MINUTE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD TWO MINUTE EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20050119001862005011900186NM 2005 1 19 ASAA0410648 120041130A53206547655522 SUPPORT ANGLE BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM. (M) 2L72 4F RTA16WE 20050119001892005011900189NM 2005 1 19 ASAA0410622 120041126A5310654581231 SHEAR TIE BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND SHEAR TIE ANGLE CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20050119001912005011900191NM 2005 1 19 ASAA0410627 120041130A534765549695 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001992005011900199NM 2005 1 19 ASAA0410521 120041110A5320654587546 ANGLE BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND ZEE ANGLE CORRODED UNDER R1 DOOR THRESHOLD. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM. (M) 2L72 4F RTA16WE 20050119002092005011900209NM 2005 1 19 ASAA0410595 120041122A53136545800197 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. (M) 2L72 4F RTA16WE 20050119002132005011900213NM 2005 1 19 ASAA0410592 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN AT LAP JOINT. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050120000012005012000001EU 2005 1 20 2005F00002 120041206A3230F96GA0102A SELECTOR VALVE AEROSPATR72 ATR72212 8680945EU MLG BROKEN A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21417AT 417 DURING CLIMB, UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE UP POSITION. REPLACED LANDING GEAR SELECTOR DUE TO BROKEN HANDLE. (M) 2H72 4T RTA53EU 20050120000072005012000007EA 2005 1 20 SWIA200414382 120041220A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 CORROSION FOUND BETWEEN FS 364 AND FS 349, STR 25R TO STRINGER 25L. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 51-21-06 & 53-00-00 MAT. LOSS MEASURED .002". REPROTECTED AREA IAW CRJ SRM 51-21-11, 51-25-06, 51-25-16. 2L72 4F RTA21EA 20050120000122005012000012EA 2005 1 20 SWIA200414383 120041220A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 484 LEFT INTERCOSTAL INBOARD ANGLE LBL 27 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050120000142005012000014EA 2005 1 20 SWIA200414385 120041220A5320 POST CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 559 VERTICAL POST LBL 9.0 INBOARD LOWER FLANGE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. VERTICAL POST REPAIRED IAW CRJ REO 601R-53-41-057. 2L72 4F RTA21EA 20050120000152005012000015EA 2005 1 20 SWIA200414386 120041220A5210 BRACKET CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 PAX DOOR FLOOR BRACKET FS 343 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-23-00. 2L72 4F RTA21EA 20050120000222005012000022NM 2005 1 20 2005UALA00058 120040113A5310 DOOR FRAME BOEING747 747422 1384935NM PWA 4056 PW4056 NE POWER RECEPTICLEDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29199UA 28717 EXTERNAL POWER RECEPTACLE PANEL DOOR FRAME IS DENTED. FABRICATED & INSTALLED INTERNAL DOUBLER PER EA. INSTALLED SHIMS & FILLERS AS REQUIRED 2L74 4F4 FRTA20WE E24NE 20050120000342005012000034NM 2005 1 20 AWXA200500033 120041220A575465C2679310 SKIN BOEING737 7373Q8 1384670NM NR 3 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK 6 CRACKS WERE FOUND EMANATING FROM FASTENER HOLES ON LOWER SURFACE OF NR 3 SLAT BETWEEN OUTBOARD AUXILIARY TRACK AND TELESCOPING DUCT WBL 36.50 - 100.27 LT. MAINTENANCE CUT OUT DAMAGE IN LOWER SURFACE OF NR 3 SLAT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIG 206. 2L72 4F RTA16WE 20050120000402005012000040EA 2005 1 20 SWIA200414380 120041220A5210 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 PAX DOOR FORWARD AND AFT BOTTOM DOOR CORNERS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DOOR IAW REO 601R-52-11-632. 2L72 4F RTA21EA 20050120000452005012000045NM 2005 1 20 AWXA200500031 120041223A555169736972 BOLT BOEING737 7373Q8 1384670NM CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOLT BS 1096.428, LBL 35.50. MAINTENANCE REMOVED AND REPLACED CORRODED LT HORIZONTAL STABILIZER LOWER FORWARD ATTACH BOLT IAW BMM 27-41-11. 2L72 4F RTA16WE 20050120000832005012000083EA 2005 1 20 VNAA0412003 120041215A21331037708 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL05206PS2084 7860 AFTER TAKEOFF THE CREW OF FLIGHT 2401 NOTED THAT THE AIRCRAFT WAS NOT PRESSURIZING. THE AIRCRAFT RETURNED TO PHL AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT PHL MEL'D THE PRESSURIZATION SYSTEM. THE AIRCRAFT FLEW TO CAK WHERE PSA MAINTENANCE FOUND THE PRIMARY OUTFLOW VALVE FAILED IN THE OPEN POSITION. THE VALVE WAS REMOVED AND REPLACED IAW CRJ 200 AMM 21-32-01-000-801 AND AMM 21-32-01-400-801. THE PRESSURIZATION SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20050120000842005012000084EA 2005 1 20 VNAA0412004 120041224A5270 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE PAX DOOR ILLUMINATED A VNAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL05220PS 7887 THE PILOTS OF FLIGHT 2434, DCA TO YYZ, REPORTED A PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON THE EICAS PRIMARY DISPLAY. THE AIRCRAFT DIVERTED TO PIT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE TROUBLESHOT THE PASSENGER DOOR SYSTEM IAW CRJ200 FIM 52-70-04. NO DEFECTS WERE FOUND. THE DOOR OPERATIONALLY TESTED GOOD IAW CRJ200 AMM 52-70-04-710-801. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20050120001132005012000113EA 2005 1 20 SWIA200414390 120041220A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 RIGHT SIDE SEAT RAIL FROM FS 544.00 TO 559+96 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SEAT RAIL IAW CRJ SRM 51-41-02 AT FS 544 TO 559+96 RBL 27.0. 2L72 4F RTA21EA 20050428000012005042800001EA 2005 4 28 SWIA200414392 120041220A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSLEAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW LEFT SIDE SEAT RAIL FROM FS 409+16 TO 409+112 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT RAIL REPLACED IAW CRJ SRM 51-41-02 AT FS 409+16 TO 409+112. 2L72 4F RTA21EA 20050120001152005012000115EA 2005 1 20 SWIA200414394 120041220A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FLOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FUSELAGE PRESSURE FLOOR HAS SURFACE CORROSION FS 409+128 TO FS 559.0 LBL 36-43. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 51-21-06. MAPPED DAMAGED AREA IAW CRJ SRM 51-13-01. REF REO 601R-53-41-272 REV A. 2L72 4F RTA21EA 20050120001272005012000127NM 2005 1 20 AWXA200500024 120041222A575465C26602212 WEDGE BOEING737 7373Q8 1384670NM SLAT ASSY DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A DISBOND AREA WAS FOUND IN NR 5 SLAT WEDGE AT LOWER INBOARD END BETWEEN SS 124.53 AND SS 128.03. MAINTENANCE CUT OUT DAMAGE IN NR 5 SLAT WEDGE AT LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SLAT IAW B737-300 SRM 51-70-10 FIG 16. 2L72 4F RTA16WE 20050118000672005011800067SO 2005 1 18 SWIA200414319 120041226A2120 ODOR EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM07579SW 120347 AFTER SHUTDOWN, VISIBLE SMOKE COMING FROM F/O'S CONSOLE AREA. OPERATED APU AS REQUIRED WITH ALL ELECTRICAL SYSTEMS AVAILABLE ON APU GENERATOR AND FOUND NO EVIDENCE OF SMOKE. OPERATED BOTH ENGINES AS REQUIRED WITH ALL ELECTRICAL SYSTEMS AVAILABLE WITH MAIN GEN'S ONLINE. FOUND NO EVIDENCE OF SMOKE. INSPECTED F/O'S CONSOLE AREA FOR SIGNS OF BURNING OR OVERHEATING. NO EVIDENCE FOUND. COULD NOT DUPLICATE AT THIS TIME. 2L72 4T RTA31SO 20050118000822005011800082SO 2005 1 18 C2XA05BT001 120041231A3260 WARNING LIGHT EMB 145 EMB145LR 3260212SO MLG ILLUMINATED A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2713553 145585 GSO - PILOT REPORTED AIR/GROUND FAIL INDICATION MESSAGE ILLUMINATED CAUSING THE LANDING GEAR NOT TO RETRACT. THE AIRCRAFT RETURNED TO GSO AND LANDED WITHOUT INCIDENT. UPON LANDING THE AIR/GROUND FAIL MESSAGE CLEARED ITSELF. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAIL MESSAGE AND PERFORMED A PRECAUTIONARY SYSTEM RESET WITHOUT FURTHER FAILURE INDICATIONS BEING NOTED. 2L72 4T RTT00011AT 20050118000892005011800089NM 2005 1 18 0402246627 120041231A3320 BALLAST BOEING747 747251B 1384892NM CABIN ODOR A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01627US 21709 WHILE IN FLIGHT, GALLEY G3B HAD BURNING SMELL FOLLOWED BY SMOKE AND THEN LIGHT WENT OUT. POWER WAS TURNED OFF. REPLACED THE FLUORESCENT LIGHT SOCKET AND BALLAST. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20050118001012005011800101EU 2005 1 18 UPS04143619 120041229A5100 UNKNOWN AIRBUSA300 A300F4622R 3930360EU FUSELAGE UNKNOWN A IPXAB EMER. DESCENT F FLT CONT AFFECTED DEDESCENT 1 SO01159UP 0848 CAPTAIN REPORTED A LOUD THUNK 5 TIMES IN FLIGHT. THE NOISE BECAME LOUDER AND EFFECTED THE AIRPLANE AND FLIGHT CONTROLS. AT THIS TIME AN INFLIGHT EMERGENCY WAS DECLARED. PERFORMED BOW TS 1883 REV 0098 WITH NO FAULTS NOTED. 2L72 4F RTA35EU 20050118001082005011800108NM 2005 1 18 04FDEA03491 120041228A5720 CHANNEL DOUG MD11 MD11 3023602NM ZONE 500 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT HAND WING NR 2 TANK NR 531 AT CUTOUT GANG CHANNEL FOUND DAMAGED. REMOVED DAMAGED GANG CHANNEL AS PER SRM 51-31-01 VOL II. FABRICATED BUSHING AS PER SRM 51-73-00 VOL II AND INSTALLED AS PER SRM 51-73-00 VOL II. INSTALLED NEW GANG CHANNEL AS PER SRM 51-42-04. 2L73 4F RTA22WE 20050118001402005011800140SO 2005 1 18 C2XA04CL128 120041220A3350SG9632 LIGHT EMB 145 EMB145XR 3260214SO CABIN MISSING A C2XAO OTHER O OTHER NRNOT REPORTED 1 SW2711113 145662 CLE - THE CREW REPORTED THE AISLE PATH LIGHTING STRIP WAS MISSING. MAINTENANCE INSPECTED AND INSTALLED THE AISLE PATH LIGHTING STRIP COVER. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050118001412005011800141SO 2005 1 18 C2XA04CL127 120041217A33502013BR BATTERY EMB 145 EMB145XR 3260214SO EMERGENCY LIGHT DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27121661095 43 14500831 THE CREW REPORTED THE CABIN OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20050118001442005011800144WP 2005 1 18 UPS05843626 120041230A3350 LAMP DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. RELAMPED PER M/M 30-50-02-2 AS NEEDED. OPS CHECK GOOD. 2L74 4F RT4A25 20050118001732005011800173EA 2005 1 18 SWIA200414348 120041030A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07432SW 7548 FS 625 LT INTERCOSTAL STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050119000302005011900030NM 2005 1 19 2005UALA00020 120040104A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 CABIN FLOORBEAM AT STA 324 RBL 40 IS CORRODED BEYOND LIMITS. 2L72 4F4 FRTA2NM E17NE 20050119000662005011900066NM 2005 1 19 ASAA0410538 120041116A531565549065 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FLOORBEAM STATION 500A RBL 24 TO 63 IC CORRODED. REMOVED EXISTING REPAIR STRAPS, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAPS IAW AS AND AAR EA. (M) 2L72 4F RTA16WE 20050119000682005011900068NM 2005 1 19 ASAA0410556 120041116A53156554979501 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050119000702005011900070EA 2005 1 19 ASOA04977 120041206A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27843AS 7310 DURING HANGAR MAINTENANCE IN BTR, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119000962005011900096NM 2005 1 19 ASAA0410562 120041119A5320654795939 INTERCOSTAL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND INTERCOSTAL CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM. (M) 2L72 4F RTA16WE 20050119000992005011900099NM 2005 1 19 ASAA0410621 120041130A534765549711 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001212005011900121EA 2005 1 19 ASOA04997 120041209A3350487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27859AS 7421 DURING AN A-CHECK IN BTR, THE EMERGENCY FLOOR LIGHTS AT ROWS 9 C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT CONNECTORS AT ROW 9/CD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001262005011900126EA 2005 1 19 ASOA04966 120041204A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 DURING A GROUND INSPECTION IN DFW, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001282005011900128NM 2005 1 19 ASAA0410606 120041123A575365464305 SKIN BOEING737 7372X6C 1384552NM FORE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - C-CHECK DENT WITH CREASE, CENTER OF LEFT INBOARD FORE FLAP, UPPER SURFACE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-20. (M) 2L72 4F RTA16WE 20050119001352005011900135NM 2005 1 19 ASAA0410669 120041130A523069539711 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE DOOR UPLATCH CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: AFT CARGO DOOR UPLATCH WEB IS CRACKED. REPLACED. 2L72 4F4 FRTA16WE E2EA 20050119001472005011900147EA 2005 1 19 A6WA200540003 120041228A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 LEFT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. (M) 2L72 4F RTA21EA 20050119001642005011900164NM 2005 1 19 ASAA0410546 120041117A53156554908501 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION LOWER FLOORBEAM BS 787 STRINGER 18R WL 201. REPAIRED TRANSVERSE BEAM PER EA 5310-02402 AND EO 04-3651. (M) 2L72 4F RTA16WE 20050119001722005011900172EA 2005 1 19 ASOA04964 120041202A335058728 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27861AS 7445 DURING OVERNIGHT MAINTENANCE IN SHV, THE FIRST SECTION OF THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR LIGHT TRACK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001882005011900188NM 2005 1 19 ASAA0410623 120041130A532065549721 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SEAT TRACK AT BS 727B. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119001932005011900193EA 2005 1 19 ASOA04962 120041202A3397487190 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT LOOSE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27848AS 7339 FLT 4589 - DURING A GROUND INSPECTION IN CAE, THE FIRST SECTION OF THE EMERGENCY FLOOR LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE FOUND A LOOSE CONNECTOR ON THE SECOND EMERGENCY FLOOR LIGHT STRIP AND RECONNECTED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119002112005011900211NM 2005 1 19 ASAA0410597 120041122A53156567140508 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION ON FLOORBEAM AT FASTENER HOLE UPPER AND LOWER SURFACE OF UPPER FLANGE. REPLACED STUB BEAM. (M) 2L72 4F RTA16WE 20050120000132005012000013EA 2005 1 20 SWIA200414384 120041220A5320 POST CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 409+128 VERTICAL POST OUTBOARD LOWER FLANGE RBL 18 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED VERTICAL POST IAW CRJ REO 60R-53-41-056 REV "NC". 2L72 4F RTA21EA 20050120000162005012000016EA 2005 1 20 SWIA200414387 120041220A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 MAIN CABIN SEAT TRACK HAS NUMEROUS AREAS OF CORROSION; FS 559.0 TO FS 559.0+80 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SEAT TRACK IAW CRJ SRM 51-40-11, 51-23-00, 51-41-04 AT F.S 559.0 TO 559.01-80, RBL 9.0. 2L72 4F RTA21EA 20050120000172005012000017EA 2005 1 20 SWIA200414388 120041220A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 MAIN CABIN SEAT TRACK HAS NUMEROUS AREAS OF CORROSION; FS 559.0 TO FS 559.0+80 LBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION AND TREATED IAW CRJ SRM 51-21-06 & 51-21-11 AREAS BLENDED WITHIN LIMITS IAW CRJ SRM 53-51-49 & 53-21-49. 2L72 4F RTA21EA 20050120000352005012000035NM 2005 1 20 AWXA200500034 120041222A53306545778532 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT R-2 DOOR UPPER HINGE CUTOUT BS 956, STR 11 RT. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT R-2 DOOR UPPER HINGE CUTOUT BS 956, STR 11 RT; FABRICATED A FILLER AND REPAIR PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01 FIG 205. 2L72 4F RTA16WE 20050120001142005012000114EA 2005 1 20 SWIA200414391 120041220A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 LEFT SIDE SEAT RAIL FROM FS 449+85 TO 499.00 CORRODED. SEAT RAIL INSTALLED IAW CRJ SRM 51-41-02 AT 449+85 TO 499.00. 2L72 4F RTA21EA 20050428000022005042800002EA 2005 4 28 SWIA200414393 120041220A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW LT SEAT RAIL FROM FS 364.00 TO 409+16 CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT REPAIRED IAW CRJ SRM 51-41-02 AT FS364.0 TO 409+16. 2L72 4F RTA21EA 20050120001182005012000118EA 2005 1 20 SWIA200414395 120041220A5321 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE FLOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FUSELAGE PRESSURE FLOOR HAS SURFACE CORROSION FS 409+128 TO FS 559.0 RBL 36-43. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW CRJ SRM 51-21-06 REO 601R-53-41-272. MAP DAMAGE IAW CRJ SRM 51-13-01. 2L72 4F RTA21EA 20050121000292005012100029EA 2005 1 21 SWIA200414396 120041220A5210 TORQUE TUBE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 PAX DOOR PULL-IN LEVER TORQUE TUBE IS CORRODED AND INNER SHAFTS ARE SEIZED. ITEM FOUND AT C-CHECK INSPECTION. PULL IN LEVER TORQUE TUBE FWD AND AFT SECTIONS, FWD INNER SHAFT, AFT PULL IN LEVER AND HARDWARE REPLACED IAW CRJ MM 52-11-01-400-819. 2L72 4F RTA21EA 20050121000312005012100031EA 2005 1 21 SWIA200414398 120041220A5414 SKIN CNDAIRCL600 CL6002B19 1900309EA NACELLE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 TWO METAL PLATES CORRODED ON TOP SKIN OF THE LEFT NACELLE/PYLON FS 736 AND 7 INCHES FWD OF T/E OF THE NACELLE/PYLON. ITEM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51-22-46. 2L72 4F RTA21EA 20050121000342005012100034EA 2005 1 21 SWIA200414401 120041220A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06. 2L72 4F RTA21EA 20050121000692005012100069EA 2005 1 21 QXEA200500084 120041211A3230 SKIN CNDAIRCL600 CL6002C10 1390015EA FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 PDX - DAMAGE TO AC SKIN FORWARD OF RT RECEPTACLE DOOR. TEAR AT BOTH EXTERNAL SKIN AND ACCESS DOOR FLANGE. FABRICATED AND INSTALLED PARTS IAW EA 53-239. 2L72 4F RTA21EA 20050119000772005011900077NM 2005 1 19 ASAA0410567 120041119A534765671406 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 LONGITUDINAL BEAM TRACK HAS CORROSION IN THE INBOARD FLANGE BOTTOM SIDE AROUND SCREW HOLES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, STRAPS, AND TRIPPER STRAP IAW AS EA AND AAR EA. (M) 2L72 4F RTA16WE 20050119000782005011900078NM 2005 1 19 ASAA0410501 120041109A57536571909127 SKIN BOEING737 7372X6C 1384552NM TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND LEFT WING T/E OUTBOARD MID FLAP HAS TWO CHAFING AREAS IN SKIN, LOWR SURFACE, AREA AT SECOND TRACK FAIRING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW EA. (M) 2L72 4F RTA16WE 20050119000972005011900097NM 2005 1 19 ASAA0410506 120041109A5313655162829 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - AFT PIT BILGE AREA HAS CORROSION IN STRINGER, AND EXTERIOR SIDES AT FRAME. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION OF STRINGER IAW SRM. (M) 2L72 4F RTA16WE 20050119000982005011900098NM 2005 1 19 ASAA0410617 120041130A53306545765723 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE AT SKIN LAP, STRINGER 4L. REPAIRED PER EA 5330-01845. (M) 2L72 4F RTA16WE 20050119001072005011900107EA 2005 1 19 A6WA200440237 120041224A3220 PIN CNDAIRCL600 CL6002B19 1900309EA NLG CAM LOCK DAMAGED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31425AW 7663 AIR RETURN GEAR DISAGREE MASTER WARNING, PERFORMED QRH LIFT OFF POSITIVE CLIMB AT 160 KNOTS 0004Z NOSE GEAR DID NOT RETRACT, IT REMAINED DOWN ENTIRE TIME. REPACKED NOSE GEAR AND INSTALLED NEW CAM LOCKING PINS. OPS AND LEAK CHECK GOOD AND SWING SATISFACTORY. ALL OK FOR SERVICE. REF CRJ MM 32-20-04 AND 32-33-00. (M) 2L72 4F RTA21EA 20050119001172005011900117SO 2005 1 19 SIMA200434212 120041201A531514522461011 GUSSET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FLOORBEAM CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21634AE 145150 DURING CPCP INSPECTION, FOUND GUSSET ON FLOORBEAM AT FRAME 20, ABOVE STRINGER 18L, HAS CORROSION. REPLACED GUSSET AT FR 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE.(K) 2L72 4T4 FRTT00011ATTE6CH 20050119001232005011900123NM 2005 1 19 ASAA0410599 120041122A531365516983 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - ELONGATED FASTENER HOLE IN STRINGER. REMOVED DISCREPANT AREA, INSTALLED REPAIR STRINGER SPLICE. (M) 2L72 4F RTA16WE 20050119001422005011900142NM 2005 1 19 ASAA0410534 120041116A534069353644 STRINGER CLIP BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND AFT PIT, LEFT HAND SIDE STATION 927 AND 947 AT 24L STRINGER CLIPS ARE CORRODED. REMOVED DAMAGED STRINGER CLIPS, FABRICATED AND INSTALLED REPLACEMENT STRINGER CLIPS IAW DRAWING 69-35364 AND SRM. (M) 2L72 4F RTA16WE 20050119001692005011900169NM 2005 1 19 ASAA0410604 120041122A53156554908501 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION LOWER FLOORBEAM. REPAIRED TRANSVERSE BEAM PER EA. (M) 2L72 4F RTA16WE 20050119001742005011900174EA 2005 1 19 ASOA04958 120041129A5210601R3807423 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M) 2L72 4F RTA21EA 20050119001792005011900179NM 2005 1 19 ASAA0410670 120041130A532065479575 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION IN AFT CARGO WEB. REPLACED WEB 2L72 4F4 FRTA16WE E2EA 20050119001802005011900180EA 2005 1 19 ASOA04987 120041208A339759465 WIRE HARNESS CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27923EV 7826 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS AT ROWS 5 THROUGH 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT CONNECTOR CABLE AT ROWS 5 THROUGH 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050119001902005011900190NM 2005 1 19 ASAA0410626 120041130A534765549693 SEAT TRACK BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON SEAT TRACK AT STATION 727. REMOVED AND REPLACED SEAT TRACK PER SRM. (M) 2L72 4F RTA16WE 20050119002052005011900205EA 2005 1 19 ASOA04992 120041209A5340 CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING A C-CHECK IN MCN, THE LEFT AND RIGHT INBOARD AND OUTBOARD CLIPS AT FS 280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT INBOARD AND OUTBOARD CLIPS AT FS 280. (M) 2L72 4F RTA21EA 20050120000442005012000044NM 2005 1 20 AWXA200500030 120041224A53206517688165 SILL BOEING737 7373Q8 1384670NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON L-1 DOOR SILL INNER CHORD (CREASE BEAM) BETWEEN BS 300 AND BS 349, LBL 60, WL 208. MAINTENANCE REMOVED CORRODED L-1 DOOR SILL CREASE BEAM FROM BS 300 TO BS 349, LBL 60; FABRICATED A NEW REPLACEMENT CREASE BEAM PER DWG 65-17688; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 8 & 12. 2L72 4F RTA16WE 20050120000982005012000098EA 2005 1 20 SWIA200414389 120041220A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 LEFT FUSELAGE INTERCOSTAL FS 349-364 STR 11L DAMAGED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL. 2L72 4F RTA21EA 20050121000322005012100032EA 2005 1 21 SWIA200414399 120041220A5411 RIB CNDAIRCL600 CL6002B19 1900309EA RT PYLON CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 RIGHT PYLON RIB FS 605 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00. 2L72 4F RTA21EA 20050121000332005012100033EA 2005 1 21 SWIA200414400 120041220A5414 SKIN CNDAIRCL600 CL6002B19 1900309EA RT NACELLE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 TWO METAL PLATES CORRODED ON TOP SKIN OF THE RIGHT NACELLE FS 736 AND 7 INCHES FWD OF T/E OF NACELLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED METAL PLATES IAW CRJ SRM 51-31-00, 51-21-11, 51-24-36, 51-25-06, 51-25-01, 51-40-11, 51-42-13 & 51-22-46. 2L72 4F RTA21EA 20050121000772005012100077NM 2005 1 21 SWAA050073 120041228A33507003665 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29789SW 29816 DURING SCHEDULED SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050121001192005012100119SO 2005 1 21 SWIA200414371 120041230A3350 FUSE EMB 120 EMB120ER 3260203SO EMERGENCY LIGHTSLOOSE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07585SW 120353 FIRST 2 RED EMERGENCY FLOOR LIGHTS AND FIRST 2 WHITE EMERGENCY LIGHTS ARE NOT WORKING. RESEATED FUSE, EMERGENCY FLOOR LIGHT OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 20050121001472005012100147EU 2005 1 21 2005UALA00050 120040111A7830 SENSOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE THRUST REVERSER MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29410UA 463 NR 2 ENGINE REVERSER FAULT LIGHT ILLUMINATED. THE CAUSE WAS THE MAIN LANDING GEAR SENSOR 22GA. SENSOR 22GA WAS REPLACED. THE FLIGHT MANUAL PROCEDURES FOR ABNORMAL AND EMERGENCY SECTION 3.03.70 PG 1 SEQ 035 REV 24 WAS REVIEWED AND IT WAS FOUND THAT THE REVERSER FAULT LIGHT ALONE IS NOT CAUSE FOR DIVERSION. 2L72 4F4 FRTA28NM E40NE 20050121001592005012100159WP 2005 1 21 ASMF200411006 120041112A3250 CONTROL VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NLG STEERING FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23205AM1388 49405 CAPTAIN REPORTED THAT DURING TAXING AND TAKE OFF, AIRCRAFT TURNED TO THE RT SIDE. STEERING WAS CHECKED AND WHEELS WERE TURNED .5000 INCH TO THE RT SIDE OF STEERING INDICATOR CENTER. CABLES, PULLEYS, PRESSURE TIRES AND STEERING CONTROL VALVE TRIMMING PIN, WERE CHECKED, BEING ALL CORRECT. AIRCRAFT WAS SENT TO THE HANGAR AND STEERING CONTROL VALVE WAS REPLACED, DIRECTIONAL CONTROL SYSTEM TRIM WAS PERFORMED AND NOSE LANDING GEAR RT WHEEL WAS REPLACED, IAW MM 32-52-01, 32-51-00 AND 32-40-02, RESPECTIVELY, TESTS WERE CORRECT. 2L72 4F4 FRTA6WE E9NE 20050121001762005012100176SO 2005 1 21 SIMA200434206 120041119A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21627AE12114 145121 CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 24. REMOVED CORROSION BY PERFORMING A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM.(K) 2L72 4T4 FRTT00011ATTE6CH 20050124000092005012400009NM 2005 1 24 ASMF200410021 120041028A2821AC9608F65 FILTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE RT ENGINE CLOGGED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23158PL 49761 718082 AIRCRAFT RETURNED TO PLATFORM, "RT ENGINE STRAINER CLOGGED" LIGHT TURNED ON. DIFFERENTIAL PRESSURE ALARM LINES LP5 AND LP6 WERE CLEANED AND OIL FILTER WAS REPLACED IAW MM 79-20-06, TEST CORRECT. DURING OVERNIGHT SERVICE, OIL AND OIL FILTER WERE REPLACED IAW MM 79-20-06 AND DIFFERENTIAL PRESSURE SWITCH WAS REPLACED IAW MM 79-35-01, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20050124000502005012400050NM 2005 1 24 HNAA0400169 120041130A3010HA1398 WIRE HARNESS DHAV DHC8 DHC8201 2809001NM HORN HEATER INOPERATIVE A HNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA07998HA 509 LT ELEVATOR HORN HEAT C/L ILLUMINATED INFLIGHT DUE TO BAD WEATHER A/C RETURNED TO BLOCK. REMOVED AND REPLACED ELEV HORN L/E NO FIX. REMOVED AND REPLACED ELEVATOR HORN WIRE HARNESS, OPS CHECK GOOD. 2H72 4T RTA13NM 20050124000512005012400051NM 2005 1 24 ASAA0410662 120041122A53306546558 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE- D-CHECK, DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050124000522005012400052NM 2005 1 24 ASMF2004012 120041228A2421947F9453 GENERATOR DOUG MD88 MD88 3023688NM APU FAILED W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23158PL 49761 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CROSS FEED TEST WAS NOT CORRECT AND APU GENERATOR LOST FREQUENCY AND VOLTAGE. APU GENERATOR WAS RESEATED AND BCU WAS REPLACED IAW MM 24-20-04 AND FAIL CONTINUED. GCU OF APU WAS REPLACED IAW MM 24-20-05 AND ENGINES WERE SHUTDOWN. CIRCUIT BREAKER B1-686 AND RELAY R2-45 WERE REPLACED AND TESTED IAW MM 24-23-03, ALL CORRECT. 2L72 4F RTA6WE 20050124000542005012400054NM 2005 1 24 SB04163 120041209A335020121 CHARGER BOEING737 7374B7 1384702NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19781AU 25020 PHL - MAINTENANCE REPORTED THE RIGHT EMERGENCY EXIT HATCH LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK AT STA 598R. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050124000612005012400061NM 2005 1 24 QXEA200400926 120041226A30405YLZ50970 CONTROLLER DHAV DHC8 DHC8202 2809007NM WINDSHIELD HEAT FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09368PH180 180 512 SEA - FLIGHT 2004 - DURING THE CLIMB-OUT, THE CREW RECEIVED A RIGHT WINDSHIELD HOT CAUTION LIGHT. PER THE CHECKLIST, THE CREW WENT TO WARM-UP AND THE CAUTION LIGHT WENT OUT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE WINDOW TEMPERATURE CONTROL. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050124000622005012400062NM 2005 1 24 2005UALA00005 120040101A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 FRAME AT STA 1520 AND STR 26L AND 25L IS DENTED. 2L72 4F4 FRTA2NM E17NE 20050124000672005012400067GL 2005 1 24 DJFA2004043 220041224A7261 CARBON SEAL CESSNA525 525 2076601CE WILINTFJ44 FJ441A GL RT ENGINE FAILED E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA23288CW589 589 5250218 1952 CREW REPORTED THAT 10 MINUTES AFTER TAKE OFF, DURING CLIMB TO ALTITUDE, THE RT ENGINE OIL PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE WAS READING APPROXIMATELY 50 PSI AND DECREASING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO KBGM. MAINTENANCE INSTALLED A NEW CARBON SEAL IN THE RIGHT STARTER/GENERATOR GEARBOX ADAPTER. AIRCRAFT WAS GROUND RUN AT 90 PERCENT N1 FOR 15 MINUTES. NO LEAKS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4F4 FRTA1WI E3GL 20050124000682005012400068SO 2005 1 24 CV2XA04SH533 120041026A531514530645401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713935 145022 DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 53-21-10 AND EC 5320-01168. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050124000732005012400073WP 2005 1 24 ARWA20041204 120041228A275057511525 DRIVE LINK DOUG DC8 DC863 302198AWP LT WING TE FLAPSBROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 DURING SERVICE CHECK, FOUND LEFT WING INBOARD FLAP DRIVE LINK BROKEN. REMOVED AND REPLACED LEFT WING INBOARD FLAP DRIVE LINK IN ACCORDANCE WITH DC8-MM 27-51-4. OPERATIONAL CHECK NORMAL IAW DC8-MM 27-51-4. 2L74 4F 4A25 20050124000742005012400074NM 2005 1 24 ASAA0410589 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON EXTERNAL SKIN LAP. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050124000832005012400083NM 2005 1 24 QXEA200500032 120041215A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN PANEL AT STATION 281.00 TO 301.00 BETWEEN STRINGER 9 PORT AND 10 PORT HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2H72 4T RTA13NM 20050120000372005012000037NM 2005 1 20 AWXA200500036 120041220A57536546431279 SKIN BOEING737 7373Q8 1384670NM FORE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 10 INCHES FROM INBOARD END, WBL 208.69 - 210.69 LT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A HONEYCOMB CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PARTS TO FORE FLAP IAW B737-300 SRM 57-70-10 FIG 18. 2L72 4F RTA16WE 20050120000412005012000041EA 2005 1 20 SWIA200414381 120041220A5315 ATTACH ANGLE CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-23-00, 51-21-11 & 51-42-21. 2L72 4F RTA21EA 20050121000712005012100071EA 2005 1 21 QXEA200500085 120041211A5310 FRAME CNDAIRCL600 CL6002C10 1390015EA RECEPTICAL BOX DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 PDX - FRAME FOR AC RECEPTACLE BOX BENT AT FLANGE. REMOVED DAMAGED FRAME AND INSTALLED A NEW FRAME PER SRM 51-42-06. 2L72 4F RTA21EA 20050124000572005012400057NM 2005 1 24 WLDA2004118 120041014A5340AEA7131501 SUPPORT FITTING DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE MLG WW CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND CORROSION IN CENTER WING W/W RT/LT SUPPORT FITTING AT STA Y=1481 X=-31.5 AND X=31.5. REPAIRED CORROSION ON LT/RT FWD TRUNNION FITTING BOOT STRAP OF CENTER MLG PER EGAT EI W2004A53B-590 REV.00 (FAA 8110-3 FORM DATED OCT/04/2004). CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124000642005012400064NM 2005 1 24 2005UALA00021 120040104A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 FWD PIT FUSELAGE FRAME PRODUCTION SPLICE HAS A DENT ON INNER FLANGE AT STA 580 ABOVE STR 26L. 2L72 4F4 FRTA2NM E17NE 20050124000692005012400069EU 2005 1 24 SA04099 120041025A3350321431 BATTERY PACK AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19721UW 1095 BOS - THE FORWARD EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE FORWARD EMERGENCY POWER SUPPLY UNIT BATTERY. 2L72 4F RTA28NM 20050124000772005012400077SO 2005 1 24 RAIA00411030 120041128A7830 WARNING LIGHT EMB 145 EMB145LR 3260212SO THRUST REVERSER FALSE INDICATIONA RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03816HK 145055 5657- STL- NR 2 THRUST REVERSER DISAGREE ON EICAS. MAINTENANCE DEFERRED NR 2 THRUST REVERSER PER MEL 78-34-00 CAT C. SUBSEQUENTLY, DID GROUND TEST OF NR 2 THRUST REVERSER: NO DEFECT NOTED. 2L72 4T RTT00011AT 20050124000892005012400089EA 2005 1 24 04362677 120041227A2750 FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27677BR 7652 FLAP FAILURE. MX RETRIEVED CODES FROM FECU. INSPECTED AND RESET FLAPS. OPS CHECK GOOD. 2L72 4F RTA21EA 20050124000952005012400095EA 2005 1 24 04361687 120041226A3030 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA AOA HEAT LOOSE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27687BR 7720 AOA HEAT FAILURE. MX RESEATED CONNECTOR ON RT DE-ICE CONTROLLER. PERFORMED OPS CHECK. GOOD AT THIS TIME 2L72 4F RTA21EA 20050124000962005012400096NM 2005 1 24 WLDA2004119 120041014A5754ARC2369504 SKIN PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT INBRD FLAP NICKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING C2+12A CHECK, FOUND NICK ON RT WING INBOARD FLAP ON STA XIFH 152WITH D=0.039" AND L=3/8". REPAIRED NICK ON RT WING INBOARD FLAP UPPER SKIN AT XIFH 152 PER EGAT EI W2004A57B-585 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 34 SHEET 3). CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124000982005012400098WP 2005 1 24 ASMF200412006 120041217A741010353875 IGNITION UNIT DOUG DC9 DC987 3022087WP RIGHT FAILED W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW23214AM26038331 49585 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES STARTING, IGNITION SYSTEM FAILED IN BOTH ENGINES. DURING MAINTENANCE REVISION WAS DETECTED THAT 115VAC WAS NOT AVAILABLE AND SWITCH FASTENERS LOOSEN IN TWO LINES. FASTENERS WERE TIGHTENED AND ENGINES STARTING WAS CORRECT. DURING TRANSIT AT MEX, IGNITION BOX WAS REPLACED IAW MM 74-10-01, TESTED CORRECT. 2L72 4F RTA6WE 20050124001032005012400103NM 2005 1 24 WLDA2004115 120041014A5512ALC84005 SKIN PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB SCRATCHED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 ITEM: DURING 2C+12A CHECK, FOUND 3 EA SCRATCH ON EXTERNAL SKIN ON LT HST L/E BETWEEN XFS 275.410 AND XFS 263.762. BLENDED REPAIR PER EGAT EI W2004A 55B-575 REV 00 (1-PGVIM WITH FAA 811-3 FORM DATED SEP/23/2004). CONDITION CHECK FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124001072005012400107NM 2005 1 24 WLDA2004116 120041014A5347S4929147 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND CABIN SEAT TRACK CORRODED AT STA Y=959 X=-8.5. REPAIRED DAMAGED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00, CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124001102005012400110CE 2005 1 24 DJFA2004042 120041224A2910 B-NUT CESSNA500 560CESSNA 2076750CE OIL SYSTEM LEAKING E DJFAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23501CW 5600050 CREW REPORTED THAT AFTER APPROXIMATELY 15 MINUTES INTO FLIGHT THEY NOTICED A BURNING OIL SMELL COMING FROM THE OVERHEAD VENTS. ACTIONS WERE TAKEN TO ISOLATE THE SMELL BY TURNING OFF FANS AND ISOLATING BLEED AIR SOURCES. A/C DIVERTED TO KCRG WHERE A NORMAL DESCENT AND LANDING WERE ACCOMPLISHED. MAINTENANCE RAN THE AIRCRAFT AND CONFIRMED THE PROBLEM. IT WAS DISCOVERED THAT OIL WAS DRIPPING ONTO A HOT BLEED DUCT IN THE AFT EQUIPMENT BAY. A B-NUT WAS TIGHTENED THAT RAN FROM A FILTER TO THE FLOW SWITCH. AIRCRAFT WAS RAN FOR 30 MINUTES WITH NO EVIDENCE OF THE OIL SMELL. B-NUT WAS RECHECKED AND NO LEAKS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA22CE 20050124001112005012400111 2005 1 24 AMTA200401484 420041209A2565 PROXIMITY SENSOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE R1 DOOR SLIDE MALFUNCTIONED A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11526AT 30735 1R SLIDE LIGHT DOES NOT EXTINGUISH WHEN DOOR IS DISARMED. REMOVED AND REPLACED 1R DOOR FWD SLIDE ARM PROX SENSOR IAW AMM. OPS CHECKED GOOD. OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20050124001202005012400120NM 2005 1 24 SB04170 120041222A2120 ODOR BOEING737 7374B7 1384702NM COCKPIT DETECTED A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19437US 24559 JAX - FLT783 - JUST AFTER TAKEOFF FROM PHL, EN ROUTE TO JAX, CREW REPORTED A BURNING RUBBER ODOR IN THE COCKPIT THAT LASTED FOR 10 TO 15 SECONDS. CREW SUSPECTED A TIRE PROBLEM BUT NO ABNORMAL LANDING GEAR OR ENGINE INDICATIONS WERE NOTED. TOWER IN PHL REQUESTED A RUNWAY SWEEP WHICH REVEALED NEGATIVE RESULTS AS NO TIRE DEBRIS WAS FOUND. FLIGHT PROCEEDED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSPECTED ALL GEAR AND TIRES, INCLUDING TIRE PRESSURE. NO DEFECTS FOUND. INSPECTED ENGINES AND RAM AIR INTAKES. NO DEFECTS FOUND. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050124001252005012400125NM 2005 1 24 WLDA2004111 120041014A5713ARB2890502ARB2 STRINGER DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE RT WING FIXED LECRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND RT WING FIXED L/E SKIN CRACK ABOUT 10" AND STRINGER DOUBLER CRACK AT STA XOS 906. REPAIRED CRACK ON RT WING FIXED L/E SKIN PANEL AND STRINGER DOUBLER AT STA XOS 906 PER EGAT EI W2004A57B-558 REV 00. (MD-11 SRM VOL.I 57-10-00 FIG 18 AND FIG 37). SLAT OPERATION AND CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124001372005012400137NM 2005 1 24 04FDEA03314 120041201A5710ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMATER=1.191, FINAL DIAMETER=1.219, AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-77983. 2L73 4F RTA22WE 20050124001442005012400144GL 2005 1 24 CHQA000593 220041211A723023073567 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ENGINE LEAKING A CHQAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11275 115577819 145345 CAE311337 FLIGHT 3192 DEPARTING SDF, DURING TAKEOFF ROLL, THE CREW HAD SMOKE IN THE COCKPIT AND ABORTED THE TAKEOFF. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE LEFT ENGINE "0" CARBON SEAL LEAKING. REMOVED AND REPLACED E1 0 CARBON SEAL. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050125000162005012500016EU 2005 1 25 MALA050136 120040115A3230 CONTROL VALVE SAAB SF340 340B 7860101EU MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15363PX 340B260 GEAR UNSAFE INDICATION DURING NORMAL APPROACH TO LANDING FOLLOWED GEAR DOWN UNSAFE CONDITION QRH. EMERGENCY GEAR EXTENSION GEAR SAFE ON LANDING NO NOSE GEAR STEERING. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL VALVE IAW SF340 AMM CHAP 32-31-15-4. SECURITY/LEAK AND OPS CHECK GOOD. 2L72 4T RTA52EU 20050125000362005012500036GL 2005 1 25 C2XA04CL126 220041215A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 LEAKING A C2XAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW27139037759 7759 145479 CAE311902 CREW REPORTED A LAV SMOKE WARNING AFTER TAKEOFF. AIRCRAFT RETURNED TO EWR WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20050121000302005012100030EA 2005 1 21 SWIA200414397 120041220A5340 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 PAX DOOR SILL CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SILL IAW CRJ SRM 51-40-11. 2L72 4F RTA21EA 20050121000362005012100036EA 2005 1 21 SWIA200414402 120041220A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 RIGHT FUSELAGE SKIN BETWEEN FS 559+80 AND 559+96 STR 22, 23, 24 CORRODED. ITEM FOUND AT C-CHECK INSPECTION. DAMAGE REPAIRED, BLENDED AND ASSESSED, FOUND TO BE W/IN LIMITS IAW CRJ SRM 53-51-31, 53-00-31. 2L72 4F RTA21EA 20050124000142005012400014SO 2005 1 24 SIMA200430802 120041031A33307281000501 MODULE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21728AE 145328 CREW REPORTED A SMOKE SMELL IN COCKPIT AND GALLEY AREA, AIRCRAFT WAS DIVERTED AND SAFELY WITH NO INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE SIDE WALL LIGHT CONTROL MODULE IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050124000782005012400078SO 2005 1 24 C2XA04CL110 120041025A49204504113 APU EMB 135 EMB135LR 3260305SO APU BAY FIRE A C2XAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW27285183486 145334 CREW REPORTED AN APU FIRE WARNING INDICATION DURING AIRBORNE START. APU SHUTDOWN AND AIRCRAFT LANDED WITH OUT INCIDENT. APU REPLACED AND OPERATIONALLY CHECKED GOOD. 2L72 4F RTT00011AT 20050124000822005012400082 2005 1 24 VW3R200400005 420041228A2565D29601103 GIRT BAR AIRCRUISERS AIRBUS330 A300* EU ESCAPE SLIDE MISLOCATED B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL 0153 ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. 2L72 4F RTA26NM 20050124000862005012400086EU 2005 1 24 SA04107 120041120A3350 CONTACTOR AIRBUSA319 A319112 3930323EU LT WING OUT OF ADJUST A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19722US 1097 THE CABIN CREW REPORTED THAT THE LEFT OVERWING EXIT LIGHT DOES NOT ILLUMINATE WHEN NO PED SWITCH IS TURNED ON. MAINTENANCE ADJUSTED A CONTACT. OPERATIONALLY CHECKS OK. 2L72 4F RTA28NM 20050124000912005012400091NM 2005 1 24 P5CA0501304 120041227A323365B825582 ACTUATOR BOEING747 747249F 1384849NM NR 1 HYD SYSTEM FAILED A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 EA15920FT 22237 WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND DOWN LOCK ACTUATOR FAILED. REPLACED ACTUATOR PER MM 32-33-15. 2L74 4F A20WE 20050124000942005012400094NM 2005 1 24 AMTA200401471 120041204A3350 WIRE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHTSDISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11515AT 27598 ROWS 10-12 EGRESS PATH ILLUMINATED LIGHTS, INOPERATIVE. FOUND LIGHT ASSY DISCONNECTED. RE-CONNECTED AS REQUIRED. OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20050125001102005012500110NM 2005 1 25 SWAA050141 120041208A3350101114 LAMP BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29773SA 27881 DURING SPV, FOUND EMERGENCY EXIT LIGHT ABOVE ROWS 18 AND 19 INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20050126000052005012600005NM 2005 1 26 2004UALA01213 120041211A2130806002 SWITCH BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29917UA 25384 DIVERTED TO LAS DUE TO A CABIN PRESSURE PROBLEM OUT OF LAX. WHEN TROUBLE SHOOTING INTERFACING SYSTEM ON E11 "LANDING GEAR LOGIC SHELF", M1110 "NOSE GEAR GROUND SENSING PROXIMITY SWITCH" FAILED. IN ADDITION, MAIN LANDING GEAR GROUND SAFETY SENSOR FOUND OUT OF LIMITS. REPLACED M1110 AND ADJUSTED MAIN LANDING GEAR GROUND SAFETY SENSORS. SYSTEM OPERATIONAL CHECKED GOOD. 2L72 4F4 FRTA16WE E2GL 20050126000072005012600007SO 2005 1 26 CHQA200500010 120040121A3350RPS1B BATTERY PACK EMB 135 EMB135KL 3260302SO EMERGENCY LIGHTSDISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11295SK 145513 LEFT HAND OVERWING FORWARD EMERGENCY LIGHT IS INOP. AISLE EGRESS LIGHT AND CABIN FLOOD LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EGRESS BATTERY PACK PER EMB 140 MM 33-50-04-5. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050126000162005012600016NM 2005 1 26 SB04171 120041225A3397 WIRE BOEING737 7373B7 1384580NM EMERGENCY LIGHT BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU 23380 MAINTENANCE FOUND A BROKEN WIRE FOR THE EMERGENCY LIGHT AT SEAT 8ABC. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050126000182005012600018NM 2005 1 26 SB04174 120041229A335020121 CHARGER BOEING737 7373B7 1384580NM EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU 23381 PHL - MAINTENANCE REPORTED THE RIGHT-HAND CENTER EMERGENCY EXIT SIGN AND THE LEFT-HAND OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND BATTERY M1160. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050126000332005012600033WP 2005 1 26 ASMF200412011 120041225A2840 CONNECTOR DOUG DC9 DC982 3022082WP FUEL INDICATION FAILED W ASMFD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SW231003Y 48O68 AIRCRAFT RETURNED TO PLATFORM DUE TO NO FUEL INDICATION IN BOTH CHANNELS. SEM CONNECTORS WERE CHECKED DETECTING ONE CHANNEL LOOSEN, THE FOUR CHANNELS WERE DISCONNECTED AND CHECKED. THE FOUR CONNECTORS WERE INSTALLED AND TESTED IAW MM 28-40-05, ALL CORRECT. 2L72 4F A6WE 20050126000362005012600036SO 2005 1 26 RAIA00412031 120041222A3250852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212SO NLG MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03833HK10901 145240 8003- ORD- NOSE WHEEL STEERING PULLED HARD RIGHT. REMOVED AND REPLACED 7 DEGREE PROX SWITCH. 2L72 4T RTT00011AT 20050126000372005012600037SO 2005 1 26 RAIA00412033 120041222A3010 WARNING LIGHT EMB 145 EMB145LR 3260212SO WINGS FALSE INDICATIONA RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03818HK 145059 5609- STL- WING ANTI-ICE FAIL MESSAGE IN FLIGHT. MAINTENANCE TEST ANTI-ICE SYSTEM. NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050126000462005012600046EU 2005 1 26 RAIA00412029 120041223A243051539019E GCU JETAIRJETSTMJETSTM4101 1500501EU NR 2 FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03551HK15371 41040 5539- STL- RT GENERATOR WILL NOT COME ON LINE. MAINTENANCE REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT. 2L72 4T RTA41NM 20050126000482005012600048EU 2005 1 26 MALA050105 120040104A3260 UPLOCK SWITCH SAAB SF340 340B 7860101EU MLG FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15360PX 340B220 AFTER TAKEOFF, THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIR RETURN TO MSP. MAINTENANCE REPLACED UPLOCK SWITCH PER 32-61-15-2. 2L72 4T RTA52EU 20050126000542005012600054WP 2005 1 26 ABXA050002 120041229A33105956888503 CONTROL PANEL DOUG DC9 DC941 302207NWP COCKPIT PEDESTALDEFECTIVE A ABXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23977AX 47513 ON CLIMB-OUT FROM RIC, SMOKE OBSERVED COMING FROM CENTER CONSOLE. AIRCRAFT DIVERTED TO ROA. ISOLATED SMOKE TO PEDESTAL RED FILL LIGHT RHEOSTAT KNOB. DISCONNECTED PLUG TO PEDESTAL LIGHT CONTROL. REMOVED AND REPLACED PEDESTAL INSTRUMENT PANEL LIGHT CONTROL ASSEMBLY IAW DC-9 AMM 33-00-00. 2L72 4F A6WE 20050126000562005012600056EA 2005 1 26 04366667 120041231A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA LAV SMOKE FALSE INDICATIONA VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27667BR 7535 TOILET SMOKE MESSAGE POSTED ON TAKEOFF. PERFORMED INSPECTION OF LAV FOR ABNORMALITIES, PERFORMED OPS CK'S OF PAX AT FULL POWER INSP'D APU BAY, AND CARGO BAY REF CRJ MM 26-10-00, 36-10-00. NO DEFECTS NOTED COULD, NOT DUPLICATE. AIRCRAFT OK TO CONT SERVICE AT THIS TIME. 2L72 4F RTA21EA 20050126000582005012600058NM 2005 1 26 QXEA200500002 120041230A5230502213 SEAL BOMBDRDHC8 DHC8401 1390041NM CARGO DOOR DAMAGED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09405QX8102 4047 BOI - FLIGHT 2344 - THE FLIGHT DIVERTED TO BOI AFTER THE AIRCRAFT FAILED TO PRESSURIZE ABOVE 1 TO 1.2 PSI DIFFERENTIAL. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AFT CARGO DOOR SEAL. OPERATIONAL CHECKS WERE PERFORMED AND WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126000592005012600059NM 2005 1 26 DHL2004784007 120041231A5270 SWITCH BOEING727 727227 1384078NM PAX DOOR DIRTY A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01784DH 22001 ON TAKEOFF, WHEN LANDING GEAR HANDLE RAISED THE FWD ENTRY DOOR LIGHT ILLUMINATED RETURNED FOR LANDING. PERFORMED FWD DOOR ENTRY INDICATOR SWITCH CLEANED AND TIGHTENED SAME TEST OK LT OFF IN CLOSED POS IAW AMM 52-11-01. 2L73 4F A3WE 20050126000602005012600060EU 2005 1 26 RAIA00412034 120041223A3241 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU ANTI SKID SYSTEMILLUMINATED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03572HK 41091 3659- BWI- CONFIG RED CAP BETWEEN 90-100 KNOTS AND ANTI-SKID FAILED. MAINTENANCE PERFORMED TAKEOFF CONFIG, OPS TEST AND ANTI-SKID OPS CHECK. NO DEFECTS NOTED. 2L72 4T RTA41NM 20050126000612005012600061EU 2005 1 26 RAIA00412035 120041228A3230 MECHANISM JETAIRJETSTMJETSTM4101 1500501EU MLG LACK OF LUBE A RAIAL ABORTED APPROACH WJ INADEQUATE Q C WARNING INDICATION LDLANDING 1 CE03557HK 41074 3663-GSO- NOSE GEAR WILL NOT EXTEND. MAINTENANCE INSPECTED NOSE LANDING GEAR AND UPLOCK MECHANISM AND LUBRICATED UP LOCK AND NOSE LANDING GEAR SHORTING MECHANISM. PERFORMED GEAR SWING. 2L72 4T RTA41NM 20050126000622005012600062EU 2005 1 26 RAIA00412036 120041223A2424243211 GCU AEROSPATR42 ATR42300 8680920EU NR 1 FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03426TE 228 5511- STL- ACW BUS 1 OFF WILL NOT RESET. MAINTENANCE REMOVED AND REPLACED NR 1 ACW GENERATOR CONTROL UNIT. 2H72 4T RTA53EU 20050126000652005012600065EU 2005 1 26 SA04117 120041227A5610NP1653118 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19768US12266 1389 PHL - FLT 107 - EN ROUTE PHL - SEA, DURING CLIMB-OUT FROM PHL, THE FIRST OFFICER'S WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD IN PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. ALSO, REPLACED THE NR 2 WINDSHIELD HEAT COMPUTER. 2L72 4F RTA28NM 20050126000672005012600067 2005 1 26 ASMF200412008 420041220A34224055900906 GENERATOR DOUG MD88 MD88 3023688NM RIGHT EFIS FAILED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23162PL6556 6556 49765 AIRCRAFT PERFORMED A REJECTED TAKEOFF AS A CONSEQUENCE OF EFIS DISPLAY WITHOUT INFORMATION, SEVERAL LIGHTS ON FMA AND PANEL SELECTOR MODES OUT OF SERVICE. DFGC NR 2 CIRCUIT BREAKER WAS RESEATED, RTS WAS TESTED IAW MM 22-01-05 AND FMS WAS CHECKED AND TESTED IAW MM 34-63-00, ALL CORRECT. DURING OVERNIGHT SERVICE, BREAKERS B10-408 AND B10-409 WERE CHECKED AND EFIS SYMBOL GENERATOR NR 2 WAS REPLACED AND TESTED IAW MM 34-22-00. REJECTED TAKEOFF INSPECTION WAS PERFORMED IAW MM 05-56-00, ALL CORRECT. 2L72 4F RTA6WE 20050126000692005012600069NM 2005 1 26 BB04095 120041220A793121SN04334 PRESSURE SWITCH BOEING767 7672B7 1385107NM GE CF6 CF680C2B2 30025NE LT ENGINE FAULTY A USAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA19651US 24764 690177 SJU - FL 1268 - EN ROUTE, THE CREW RECEIVED THE EICAS MESSAGE 'L OIL FILTER.' THE OIL PRESSURE AND QUANTITY WERE NORMAL. CREW REDUCED THRUST TO IDLE, BUT THE MESSAGE REMAINED. THE LEFT ENGINE WAS SECURED. FLIGHT CONTINUED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE OIL FILTER AND FOUND ONLY MINOR CARBON PARTICLES. THE SCAVENGE FILTER DIFFERENTIAL PRESSURE SWITCH WAS REPLACED. ENGINE RUN WAS PERFORMED. NO PROBLEMS NOTED. AIRCRAFT MADE READY FOR FERRY FLIGHT TO PHL. 2L72 4F4 FRTA1NM E13NE 20050126000722005012600072NM 2005 1 26 P5CA0501297 120041229A2711680000152769 PULLEY BOEING747 747283B 1384867NM FLT CONTROLS WORN A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA15921FT 21575 ON TAXI OUT, FLIGHT CONTROL CHECK REVEALED WHEN CONTROL WHEEL TURNED TO LEFT, NORMAL MOVEMENT OBSERVED. WHEN CONTROL WHEEL TURNED TO RIGHT IT STOPPED AT 10 DEGREES FOR 4-6 SECONDS THEN RETURNS SLOWLY TO NEUTRAL. FOUND CABLE PULLEY IN LT WHEEL WELL WORN. REPLACED PULLEY, PERFORMED AILERON AND AILERON TRIM SYSTEM TEST PER MM 27-11-00. ALL OPS NORMAL. 2L74 4F A20WE 20050126000732005012600073NE 2005 1 26 ASMF200412013 220041228A732076960615 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LEFT FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23205AM386906034 49405 718411 CAPTAIN REPORTED LEFT ENGINE WITH N2 47 PERCENT IN IDLE POSITION. DURING MAINTENANCE REVISION WAS DETECTED LEFT ENGINE WITH N2 52 PERCENT, EPR 1.03; ENGINE STABILIZED AT N2 50 PERCENT, EPR 1.03. WHEN LEFT AIR CONDITIONING SWITCH WAS OPERATED N2 48 PERCENT, EPR 1.02 AND WITH ELECTRICAL CHARGES N2 TREND TO LET OUT OF SERVICE LEFT GENERATOR. ENGINES WERE SHUTDOWN AND AIRCRAFT WAS SENT TO THE HANGAR, FCU WAS REPLACED IAW MM 73-20-01, TRIMMING AND ADJUSTMENT WERE PERFORMED IAW MM 71-00-00, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050126000782005012600078EU 2005 1 26 225922 120041229A3234 CONTROL PANEL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MLG SELECTOR INOPERATIVE A UHLAO OTHER J WARNING INDICATION LDLANDING 1 GL1735SZ 035 RT MLG, GREEN GEAR LIGHT INOP. WILL NOT TEST, CHANGED BULBS STILL NO FIX, LANDED PER QRH. INSPECTED AND FOUND LANDING GEAR HANDLE CONTROL PANEL TO BE INOP. REMOVED AND REPLACED LANDING GEAR HANDLE CONTROL PANEL IAW SAAB AMM 32-31-05-2, OPS CHECK AND GEAR SWINGS GOOD, IAW SAAB AMM 32-30-00-5, NO DEFECTS NOTED. 2L72 4T4 TRTA52EU E8NE6 20050126000842005012600084EA 2005 1 26 QXEA200500047 120041226A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - LEFT HAND LOWER WEB OF BULKHEAD AT STATION 280 HAS CORROSION. REPLACED IAW CRJ SRM 51-42-06 AND SRM 51-42-13. 2L72 4F RTA21EA 20050126000942005012600094CE 2005 1 26 DJFA2004044 120041230A32601EN115BN111 SWITCH RAYTHNDH125 HAWKER800XP 7150012CE NOSE GEAR INTERMITTENT E DJFAO OTHER N FALSE WARNING APAPPROACH 1 EA23781TA 258281 CREW REPORTED THAT WHILE ON APPROACH AND GEAR SELECTED DOWN THAT THE NOSE WHEEL DOWN INDICATOR HAD FAILED TO ILLUMINATE. TOWER VERIFIED GEAR POSITION TO BE DOWN AND LOCKED. CREW REQUESTED PRIORITY, AND DECLARED AN EMERGENCY. A NORMAL LANDING WAS MADE. MAINTENANCE FOUND THE NOSE GEAR LEG LOCK MICROSWITCH TO BE INTERMITTENT. A NEW MICROSWITCH WAS INSTALLED, AND SEVERAL SATISFACTORY GEAR SWINGS WERE PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA3EU 20050121000722005012100072EA 2005 1 21 QXEA200500086 120041211A5310 STRUCTURE CNDAIRCL600 CL6002C10 1390015EA RECEPTICAL BOX DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09611QX 10041 PDX - AC RECEPTACLE BASE DAMAGED. REMOVED DAMAGED RECEPTACLE BASE. INSTALLED NEW BASE PER SRM 51-42-06. FABRICATED AND INSTALLED NEW PARTS IAW EA R-53-239. 2L72 4F RTA21EA 20050121000732005012100073EA 2005 1 21 QXEA200500087 120041225A5720 PAN CNDAIRCL600 CL6002C10 1390015EA RT WING CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09613QX 10045 PDX - THE RIGHT STUB WING PRESSURE PAN HAS A CRACK IN IT. REO 670-53-61-060. 2L72 4F RTA21EA 20050121001462005012100146EA 2005 1 21 SWIA200414379 120041220A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 FS 202 LBL 23 PRESSURE BULKHEAD WL 59 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED BULKHEAD IAW CRJ REO 601R-53-11-563. 2L72 4F RTA21EA 20050121001572005012100157NM 2005 1 21 XNOA1207 120041103A2131 CONTROLLER BOEING727 72722C 138400FNM GARRTTTFE731TFE731* 01518WP CABIN PRESSURE UNCONTROLLABLE A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23792A 19195 NR 2 AIRCRAFT PRESSURIZATION SYSTEM IS UNCONTROLABLE BOTH AUTO AND MANUAL MODE. (STATUS:ORIG/OPEN) 2L73 4F4 F A3WE E6WE 20050124000012005012400001NM 2005 1 24 ASMF200410020 120041026A71105930645505 COWLING DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE LEFT DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23161PL10952 49764 718075 CAPTAIN REPORTED THAT AIRCRAFT WAS STRUCK BY FOD ON ENGINE NR 1. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DENT WAS DETECTED ON LT ENGINE NOSE COWLING TRAILING EDGE WITH 4 X 1.750 INCHES AND 0.197 AT 12 OCLOCK POSITION IAW SRM 54-04. DURING OVERNIGHT SERVICE LT ENGINE NOSE COWLING WAS REPLACED IAW MM 71-10-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050124000022005012400002NM 2005 1 24 UIA9321 120041218A3260833703 PROXIMITY SENSOR DOUG MD90 MD9030 3023690NM NLG MALFUNCTIONED Z A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 TW0017913 53537 AFTER AIRBONE, RAISE GEAR HANDLE UP, NOSE GEAR RED LIGHT ILLUMINATE. A/C AIR TURN BACK, A/C LANDING. PERFORMED TROUBLESHOOTING, FOUND NOSE GEAR PROXIMITY SENSOR FUNCTION NO GOOD IAW AMM 32-60-02. REPLACED NOSE LANDING GEAR DOWN AND LOCKED PROXIMITY SENSOR AND ADJ. GAP TO 0..75IN , OPERATIONAL CHECK CONDITION BACK TO NORMAL. 2L72 4F RTA6WE 20050124000112005012400011SW 2005 1 24 FVY2004F00000 120041129A27301094082 CONTROL CABLE GULSTMG73 G73 3951802SW PWA PT6 PT6A60A 52043NE ELEVATOR FAILED A FVYAO OTHER O OTHER NRNOT REPORTED 1 SO17142PA J42 PILOT REPORTS THAT ELEVATOR CONTROL WAS UNAVAILABLE IN FLIGHT AND UNABLE TO ACHIEVE NOSE DOWN POSITION WITHOUT TRIM. MAINTENANCE INSPECTED ELEVATOR CABLES. REMOVED AND REPLACED ELEVATOR DOWN CABLE FROM TORQUE TUBE TO AFT. BAGGAGE COMPONENT TENSION AND RIGGED ELEVATOR CABLES IAW MM. (SO17200504411) 1H72 3R4 T A783 E4EA 20050124000602005012400060EU 2005 1 24 SA04090 120040920A3350321431 BATTERY PACK AIRBUSA319 A319112 3930323EU EMERGENCY LIGHTSDISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19701UW 0890 CLT - THE EMERGENCY LIGHTS TEST FAILED WITH MESSAGE "EPSU UNIT AFT L". MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT BATTERY PACK. 2L72 4F RTA28NM 20050124000852005012400085NM 2005 1 24 WLDA2004114 120041014A5754ARB1668501 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE LT WING NR3 SLATDENTED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND SHARP DENT ON LT WING NR 3 SLAT UPPER SKIN AND INNER RIB AT STA XOS 414. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-581 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33). PERFORMED SLAT OPERATION AND CONDITION CHECK, FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124000922005012400092NM 2005 1 24 WLDA2004112 120041014A5754ARB1568503 SKIN PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE LT WING NR1 SLATPUNCTURED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND LT WING NR 1 SLAT L/E AREA HOLE DAMAGE AT STA XIS 186. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-560 REV 00 (MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). PERFORMED SLAT OPERATION CHECK, FOUND NORMAL. 2L73 4F4 FRTA22WE E24NE 20050124000972005012400097NM 2005 1 24 WLDA2004117 120041014A5320AGA717041 WEB DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE CARGO BAY CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND CRACK AT CENTER CARGO COMPARTMENT STA 1841 L-50 RT WEB. REPAIRED CRACK ON FUSELAGE FRAME WEB STA 1841 L-50 RT PER EGAT EI W2004A53B-559 REV.00 (FAA 8110-3 FORM DATED SEP/23/2004). CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124001182005012400118EU 2005 1 24 YENA200465 120041227A2752793C000001 ACTUATOR AIRBUS320 A320232 3930326EU TE FLAPS WORN A YENAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA15592JB1247 2259 FLAP SYS JAM IN CONF 3. TROUBLESHOOT PER TSM 27-51-00. FOUND NR 3 LT FLAP TRACK ACTUATOR TORQUE LIMITER POPPED. REMOVED AND REPLACED NR 3 LT FLAP ACTUATOR PER MM 27-54-49. ALL CHECKED OK FOR SERVICE. 2L72 4F RTA28NM 20050124001192005012400119 2005 1 24 YENA200466 420041228A23303042865102 ELECTRICAL BOX AIRBUS320 A320232 3930326EU CABIN ODOR A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15523JB5409 1506 CABIN CREW REPORTED ELECTRIC SMELL IN AFT HALF OF CABIN. NO SPECIFIC LOCATION, LTV TAKEN OFF LINE BY CREW AS PRECAUTION. ACCOMPLISHED INFORMATION NOTICE 2004-T023TR (ATA 23-39)LIVE TV SYSTEM INTEGRITY CHECK FOR WIRING ELECTRICAL ODOR. ACCOMPLISHED TSM 24-00-00-810-823. FOUND SEB AT 25G WITH ELECTRIC ORDER, REMOVED AND REPLACED IAW LTV MM 23-39-00, OPS CHECK GOOD. 2L72 4F RTA28NM 20050125000122005012500012EU 2005 1 25 MALA050135 120040114A3260 PROXIMITY SWITCH BAC 146 AVRO146RJ85A1500097EU MLG FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15509XJ E2321 AFTER TAKEOFF LEFT GEAR DIDN'T INDICATE UP AND LOCKED. RED LEFT GEAR AND GEAR SELECTOR LIGHT ON. GEAR LOWERED NORMALLY. AIR RETURN TO MEM. MAINTENANCE FOUND GEAR PROXIMITY SWITCHES DIRTY. CLEANED AND PERFORMED OPS TEST OF LANDING GEAR. LEFT TRANSITENT LIGHT AND GEAR HANDLE LIGHT EXTINGUISHED. 2H74 4F RTA49EU 20050125000882005012500088NM 2005 1 25 SWAA050133 120041207A53216545834 FLOOR PANEL BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SPV, FOUND 3 EACH CRACKS ON FLOOR PANEL WEB AT BS 178, RBL 17.1. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050126000172005012600017WP 2005 1 26 DHL2004802008 120041229A3260H2024B UPLOCK SWITCH DOUG DC8 DC873 302199CWP MLG DOOR FAILED A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01802DH 46076 "DOORS NOT LATCHED" AND "RIGHT DOOR UNSAFE" LIGHTS ILLUMINATED EN ROUTE. ABNORMAL PROCEDURE COMPLETED. REMOVED AND REPLACED LEFT GEAR DOOR UPLATCH SWITCH AND CLEANED AND RESEATED RT SIDE SWITCH IAW DC-8 M/M 32-31-4 AND 32-10-0. CK'S NORMAL. P/N: H20-24B. 2L74 4F RT4A25 20050126000202005012600020NM 2005 1 26 SB04172 120041229A33501012721 LIGHT BOEING737 737301 1384611NM SEAT 10C INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU 23512 CLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C WAS INOPERATIVE. MAINTENANCE INSTALLED A NEW LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. 2L72 4F RTA16WE 20050126000212005012600021NM 2005 1 26 SB04173 120041229A3397 WIRE BOEING737 7373B7 1384580NM SEAT ROW 19 BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE SEAT. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050126000382005012600038EU 2005 1 26 RAIA00412030 120041223A2421200322 GENERATOR AEROSPATR42 ATR42300 8680920EU NR 1 ENGINE FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03426TE21930 228 5727- STL- ACW BUSS INOP. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ACW GENERATOR. 2H72 4T RTA53EU 20050126000402005012600040NM 2005 1 26 P5CA0501300 120041230A2612 WARNING LIGHT BOEING747 747123 1384873NM PWA JT9 JT9D7 52054NE NR 4 ENG FIRE ILLUMINATED A P5CAEFJAENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15858FT 20109 662473 DURING FULL THRUST T/O AT 650', NR4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED LEFT AND RIGHT FIRE BOTTLES PER MM 26-21-03. ALL TESTS OK. 2L74 4F4 F A20WE E20EA 20050126000702005012600070NM 2005 1 26 P5CA0501302 120041227A323365B0150415 ACTUATOR BOEING747 747249F 1384849NM MLG LEAKING A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 EA15920FT 22237 WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYD SYSTEM. LANDING WAS NORMAL. FOUND LEFT BODY GEAR LEVELING CYLINDER FAILED. REPLACED PER MM-13-15. 2L74 4F A20WE 20050126000712005012600071NM 2005 1 26 QXEA200500019 120041216A5347 CARGO TRACK BOMBDRDHC8 DHC8401 1390041NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE INT AFT, X683, RIGHT HAND INBOARD CARGO TRACK IS CORRODED ON UPPER SURFACE OF OUTBOARD FLANGE. REPAIRED IAW HORIZON AIR EA 6-53-498 AND RD 8/4-53-116. 2H72 4T RTA13NM 20050126000802005012600080NM 2005 1 26 QXEA200500025 120041219A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM ZONE 100 LIGHTNING STRIKEA QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE EXTERIOR LEFT HAND SIDE THERE ARE TEMPORARY LIGHTNING STRIKE REPAIRED AT FUSELAGE STATION X296, X301.85, X321.55, X541 AND X753. MADE PERMANENT REPAIRS IAW HORIZON AIR EA 6-53-503 AND RD 8/4-53-1108, ISSUE 1. 2H72 4T RTA13NM 20050126000922005012600092NM 2005 1 26 AMTA200401481 120041209A3350 HOUSING BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE EMERGENCY LIGHT DIRTY A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11552TZ 32586 THE OUTSIDE 1R EMERGENCY DOOR LIGHT IS INOPERATIVE. CLEANED CONTACT OF LIGHT AND HOUSING. OPS CHECK NORMAL. OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20050126001042005012600104NM 2005 1 26 P5CA0401296 120041229A2741 SWITCH BOEING747 747283B 1384867NM STAB TRIM IND MALFUNCTIONED A P5CAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA15921FT 21575 AT APPROXIMATELY 80 KNOTS TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AT OKO. STAB TRIM WAS AT THE EDGE OF THE GREEN BAN. CAPTAINS TRIM INDICATOR HAS NO CENTER INDEX. MAX THRUST WAS SET PRIOR TO BRAKE RELEASE AT TAKEOFF OKO. RESET GREEN BAND SWITCH PER MM 31-26-00. 2L74 4F A20WE 20050126001052005012600105EA 2005 1 26 04363708 120041228A2750853D10018 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS INADEQUATE A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27708BR 7575 FLAP FAILURE AT 0. FERRIED A/C TO MAINTENANCE BASE. MX FOUND WATER INTO THE FLAP FLEX SHAFTS, WHICH IS FREEZING AT ALTITUDE. UPGRADED FLAPS ACTUATORS. ALL FLEX SHAFTS WERE CLEANED AND LUBE, AND ALL FLEX SHAFT SEALS WERE REPLACED. 2L72 4F RTA21EA 20050126001142005012600114NM 2005 1 26 SB04168 120041220A56105893543109 WINDSHIELD BOEING737 737301 1384611NM COCKPIT ARCED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19591US1251112511 23936 PHL - FLT1027 - ON CLIMB-OUT FROM PHL, AT 3,000 FEET, THE CAPTAIN'S L1 WINDSHIELD BEGAN TO ARC. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S L1 WINDSHIELD PER JOB CARD J356-11-01. ALSO, REMOVED AND REPLACED THE WINDOW HEAT CONTROL UNIT FOR THE L1 WINDSHIELD. OPERATIONAL CHECK GOOD. 2L72 4F RTA16WE 20050126001292005012600129NM 2005 1 26 2005UALA00067 120040116A5310 WINDOW FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 RT CABIN WINDOW FRAME NR 4 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME. 2L72 4F4 FRTA2NM E17NE 20050126001382005012600138NM 2005 1 26 QXEA200400932 120041228A6120 CONNECTOR DHAV DHC8 DHC8202 2809007NM AUTOFEATHER SYS DIRTY A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM09357PH 504 SEA ABORTED TAKEOFF AT 70 KTS DUE TO AUTOFEATHER FAILING TO ARM. INSPECTED AND CLEANED CONNECTORS ON BOTH NR 1 AND NR 2 TSCU'S/ COMPLIED WITH AUTOFEATHER AND POWER UPTRIM TEST. CHECKED GOOD SEVERAL TIMES. NO OTHER DEFECTS NOTED. NO PARTS REPLACED AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126001412005012600141NM 2005 1 26 ASAA0410600 120041122A533065516983 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE -DAMAGE ON SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050126001552005012600155EA 2005 1 26 QXEA200500049 120041227A5210 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 800 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - MAIN CABIN DOOR, AFT ATTACHMENT ANGLE STEP ASSEMBLY TO INNER DOOR SKIN HAS CRACK NEXT TO PULLEY ASSEMBLY. REPAIED IAW REO 670-52-11-072, SHEET 2, NOTE 5 AND CRJ 700 AMM TASK 52-11-08-400-801-A01. 2L72 4F RTA21EA 20050126001582005012600158EA 2005 1 26 COMA0460663 120041206A5230 DOOR CNDAIRCL600 CL6002B19 1900309EA CARGO BAY OPEN A COMAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 SO01924CA 7026 CARGO DOOR CAUTION MESSAGE, ABNORMAL CABIN ALTITUDE CLIMB RATE. CARGO DOOR FOUND PARTIALLY OPEN. NO DEFECTS FOUND, CLOSED DOOR AND A/C PRESSURIZE NORMAL. 2L72 4F RTA21EA 20050126001612005012600161SO 2005 1 26 148011142004 120041114A56101159SCB310211 WINDSHIELD GULSTMG1159 GIV 3980115SO COCKPIT BROKEN E N93AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO13480QS 1380 LIGHT ILLUMINATED FROM LOWER WINDSHIELD AREA ABOVE GLARESHIELD, PILOTS SIDE. 2L72 4F RTA12EA 20050126001652005012600165CE 2005 1 26 8445185 120041020A1430AN17517A BOLT BEECH 1900 1900D 1154162CE RUDDER BENT A JJBAK NONE O OTHER ININSP/MAINT 1 EA01844CA6048 UE410 DURING INSPECTION, FOUND RUDDER CONTROL HORN CENTER PIVOT BOLT BENT. APPARENT CAUSE IS SHEAR STRESS. TOTAL OF 10 SIMILAR PROBLEMS DISCOVERED IN FLEET OF 26 AIRCRAFT SINCE 5/26/2002. 2L72 4T RTA24CE 20050126001682005012600168CE 2005 1 26 DJFA2004031 120041109A750045A40301021 BELLOWS BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE BLEED AIR CRACKED E DJFAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 EA23898TA RK295 PCEJA0364 CREW REPORTED AIRCRAFT WOULD NOT INCREASE SPEED WITH INCREASED POWER AND AT 190 KTS STICK SHAKER WAS ENCOUNTERED. ABQ CENTER WAS ADVISED THAT AIRCRAFT HAD TO DESCEND. ENGINES WOULD NOT DEVELOP PUBLISHED TAKEOFF POWER. MAINTENANCE FOUND 2 BLEED AIR BELLOWS CRACKED AT ATTACH TUBE WELDS ON RIGHT ENGINE. FUNCTION CHECK AND SYSTEM OPERATIONAL CHECK WAS GOOD FOR DISCREPANCY OF STICK SHAKER BEING ENCOUNTERED WHILE AT INDICATED AIRSPEED OF 190 KNOTS. BLEED AIR DUCT TUBES/BELLOWS WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20050126001712005012600171SW 2005 1 26 51011082004 120041108A7603 THROTTLE CABLE FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE33111U 01514WP FROZEN E STZAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 AL03510FS CC842B P44709C DURING DESCENT INTO FAIRBANKS AK, PILOT REPORTED "A STUCK LT POWER LEVER" PILOT PERFORMED A PRECAUTIONARY ENGINE SHUT DOWN PER THE CHECKLIST AND CONTINUED HIS DESCENT. APPROX 8 MILES FROM THE AIRPORT THE PILOT "BUMPED" THE POWER LEVER AND FOUND IT TO BE "FREE" THE PILOT THEN PERFORMED AN AIRSTART AND LANDED W/O INCIDENT. POST FLT INVESTIGATION AND INSPECTION BY MX PERSONNEL FOUND THE CONTROL SYSTEM TO BE PROPERLY RIGGED AND FUNCTIONING NORMALLY. A/C DEPARTED FAIRBANKS AND RETURNED TO ANCHORAGE WITH NO FURTHER PROBLEMS. 2L72 4T4 TRTA18SW E4WE 20050126001732005012600173EU 2005 1 26 MHIA098086 120041119A6310365A32653000 COUPLING AEROSPAS365 AS365N2 8680815EU M/R GEARBOX CRACKED B MHIAK NONE O OTHER ININSP/MAINT 1 EA25886TW 6413 DURING INSPECTION, FOUND RT FORWARD ENGINE/MGB DRIVE FLEX COUPLING CRACKED. REPLACED WITH NEW. 1G72 3U RTH10EU 20050126001762005012600176WP 2005 1 26 ARWA20041202 120041211A3610 DUCT DOUG DC10 DC1030 3023501WP PNEUMATIC SYSTEMDEFECTIVE A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19526MD 46998 AFTER TAKEOFF AND ENGINE IN CLIMB POWER TURNED NR 2 PNEUMATIC SUPPLY SWITCH TO AUTO NR MANIFOLD LIGHT CAME ON. REMOVED DEFECTIVE PNEUMATIC DUCT (LT) BETWEEN FUSELAGE STATION 1239 AND STA 1361 IN ACCORDANCE WITH DC-10-30 MM 36-14-02. INSTALLED NEW PNEUMATIC DUCT (LT) IN ACCORDANCE WITH DC-10-30 MM 36-14-02. LEAK CHECK IS SATISFACTORY. 2L73 4F A22WE 20050126001822005012600182EU 2005 1 26 MALA040907 120041203A5330 PANEL SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 DURING 4K INSPECTION IN BNA, FORWARD CLOSEOUT PANEL AT FS 294, BETWEEN LBL 18.3 AND LBL33 IS CORRODED AND PANEL WAS REMOVED AND REPAIRED. REFER EAMS WORK ORDER NR 211114/TASK 1526 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050126001842005012600184EU 2005 1 26 MALA040910 120041229A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15444XJ 340B444 DURING 4K INSPECTION IN BNA, RT FUSELAGE FRAME AT FS 686.888 IS CHAFED BY CARGO DOOR CABLE. DAMAGE WILL BE REPAIRED IAW MESABA EO S53277 AND SAAB DOCUMENT NR 340SDS007917. REFER EAMS WORK ORDER 211273/TASK 2520. 2L72 4T RTA52EU 20050126001862005012600186SW 2005 1 26 ALGA097870 120040810A6520 BEARING BELL 206 206B3 1181506SW T/R GEARBOX FAILED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0335WH 1552 2736 TAILROTOR GEARBOX DISASSEMBLED FOR CHIP LIGHT, FOUND DUPLEX BRG BREAKING DOWN. REPLACED WITH NEW. 1G71 3U H2SW 20050126001892005012600189EU 2005 1 26 MALA040733 120041125A3020HTE690041 SWITCH BAC 146 AVRO146RJ85A1500097EU ANTI ICE SYSTEM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15533XJ E2367 NR 3 INTAKE LOW PRESS LIGHT ILLUMINATED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE DEFERRED NR 3 ENG INTAKE LOW PRESS INDICATION PER MEL 30-20-2-2-C ENTERED INTO DMR MXC NOTIFIED. REPLACED NR 3 ENG ANTI-ICE LOW PSI SWITCH, P/N HTE690041, S/N OFF FR074BA, S/N ON FR102BA IAW AMM 30-21-14. OPS CHECK GOOD. REMOVED FROM DMR. MXC NOTIFIED NR 4632. 2H74 4F RTA49EU 20050126001912005012600191 2005 1 26 VW3R200400003 420041126A2562P3030029 ELT DOUG MD11 MD11F 3023600NM CABIN INOPERATIVE B VW3RK NONE L NO TEST ININSP/MAINT 1 WP09ALL ALL ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2L73 4F RTA22WE 20050126001962005012600196EU 2005 1 26 MALA040860 120041210A243523080031 STARTER GEN SAAB SF340 340B 7860101EU LT ENGINE FAILED A MALAB EMER. DESCENT A FLAME/FIRE TXTAXI/GRND HDL 1 GL15433XJ 340B433 ENGINE FIRE LEFT ENGINE (NR1) ENGINE STOPPED AROUND 18 PERCENT ITT RISE TO 600 DEG C PERFORMED MEMORY ITEMS + REF QRH. FOUND LT STARTER GEN FAILED AND SMELLED BURNED. NO EVIDENCE OF ENGINE FIRE. COMPLETED TASK CARD 243103 FOR STARTER GEN CHANGE. P/N ON AND OFF 23080-031, S/N OFF 3974, S/N ON 99523, OPS AND LEAK CHECKS GOOD. REMOVED LT FIRE BOTTLE P/N 404028, S/N 24736EL. INSTALLED SERVICEABLE ONE. BOTTLE P/N 404028 S/N 97957EJ, REPLACED LT SQUIB WITH SERVICEABLE. 2L72 4T RTA52EU 20050126002002005012600200EU 2005 1 26 MALA040826 120041116A5313 RIB SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, 612AR 4 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 218750 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20050126002052005012600205SO 2005 1 26 GLBA20030762 120041106A2810 PANEL EMB 120 EMB120ER 3260203SO FUSELAGE LEAKING A GLBAK NONE K FLUID LOSS ININSP/MAINT 1 NM0371GL 120071 FUEL SEEP RT LOWER I/B PANEL. REPAIRED FUEL LEAK IAW EO 04-71GL-02. 2L72 4T RTA31SO 20050126002082005012600208NM 2005 1 26 QXEA200500020 120041217A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM ZONE 400 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND ENGINE FORWARD FRAME INTAKE COWL ATTACHMENT LUGS, INBOARD HAS BEEN GOUGED ON INBOARD FACE, ABOVE PIN HOLE. REPAIRED IAW HORIZON AIR EA 6-54-325 AND RD 8/4-54-219. 2H72 4T RTA13NM 20050127000062005012700006 2005 1 27 VW3R200400001 420041126A2562P3030029 ELT BFGOODRICH DOUG MD11 MD11F 3023600NM CABIN INOPERATIVE B VW3RK NONE LP NO TEST NO WARNING INDICATION ININSP/MAINT 1 WP09ALL 10R418 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2L73 4F RTA22WE 20050127000072005012700007 2005 1 27 VW3R200400006 420041228A2565 PAD AIRCRUISERS AIRBUS330 A300* EU GIRT BAR DEFECTIVE B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. 2L72 4F RTA26NM 20050127000422005012700042 2005 1 27 P9RA20040050 420041123A2565D30654122 SLIDE BOEING757 757231 1384950NM R1 DOOR DEPLOYED A P9RAK NONE W INADEQUATE Q C NRNOT REPORTED 1 SO11720TW 30319 AFTER PUSH BACK IN CCS. GROUND CREW REPORTED DEBRIS UNDER R1 DOOR AND REQUESTED CREW TO OPEN THE DOOR. CREW MEMBER FAILED TO DISARM THE DOOR CAUSING THE SLIDE TO INFLATE. SLIDE REPLACED PER MM. 2L72 4F RTA2NM 20050127000442005012700044WP 2005 1 27 ASMF200412005 120041217A3260 WARNING LIGHT DOUG DC9 DC987 3022087WP MLG FALSE ACTIVATIONW ASMFK NONE N FALSE WARNING ININSP/MAINT 1 SW231075T 49724 AIRCRAFT ARRIVED WITH CAPTAIN REPORT AFTER TAKEOFF THE THREE LANDING GEAR RED LIGHTS AND AUDIBLE ALARM TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHTS AND ALARM TURNED OFF. AIRCRAFT WAS SENT TO THE HANGAR, SWITCHES S-319 AND S1-89 WERE REPLACED IAW MM 32-61-00 AND TESTED IAW MM 32-30-00, ALL CORRECT. 2L72 4F RTA6WE 20050127000472005012700047EU 2005 1 27 MALA040818 120041102A5313 RIB SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 612AR 2 CRACKED RIBS, REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 126857 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2L72 4T RTA52EU 20050124000882005012400088NM 2005 1 24 SB04169 120041221A3260806007 LOGIC CARD BOEING737 7373B7 1384580NM RT MLG DIRTY A USAAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA19383US 22956 ALB - FLT1231 - ON APPROACH TO ALB FROM CLT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. CREW PERFORMED MANUAL GEAR EXTENSION PROCEDURE AND RECEIVED ALL THREE GREEN GEAR LIGHTS. CREW REPORTED LIGHTS TESTED OK. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED, CLEANED AND REINSTALLED M981 LOGIC CARD. INSPECTED RIGHT MAIN LANDING GEAR. NO DEFECTS NOTED. OPERATIONALLY CHECKED M981 CARD PER MM 32-09-20-724-015. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA16WE 20050124000932005012400093NM 2005 1 24 WLDA2004113 120041014A5754ARB1568503 SKIN PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE LT WING NR1SLAT DENTED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND 2EA SHARP DENT ON LT WING NR 1 SLAT UPPER SKIN PANEL LOCATED AT STA XIS 240. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-564 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). SLAT OPERATION AND CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20050124001062005012400106 2005 1 24 ASMF200412007 420041219A23124034240906 CONTROL PANEL DOUG MD88 MD88 3023688NM LT VHF FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23160PL2065020650 49763 CAPT REPORTED VHF-NAV NR 1 FAILED. DURING MX REVISION, FIVE REPORTS WERE DETECTED ON MX LOGBOOK. 1. VHF NAV 1 WITH OSCILLATIONS DURING FLIGHT AND TAXING. VHF COMPUTER WAS RESEATED AND TESTED IAW MM 34-50-00, ALL CORRECT. 2. DURING FLIGHT AUTO THROTTLE ACCELERATOR WAS OUT OF SERVICE. IN GROUND TEST WAS PERFORMED IAW MM 22-31-00, ALL CORRECT. 3. VHF NAV 2 WITH INDICATION AND SPEED MACH INFO DAMAGED. VHF NAV PANEL WAS REPLACED AND TESTED IAW MM 34-51-00, ALL CORRECT. 4. DURING LANDING GPWS FAILED. GPWS GROUND TEST WAS PERFORMED IAW MM 34-43-2, ALL CORRECT. 5. ILS DID NOT ENGAGE TO THE AUTO PILOT AND FREQUENCY WAS NOT RECEIVED. VHF NAV 1 WAS REPLACED IAW MM 34-51-00, TESTED CORRECT. 2L72 4F RTA6WE 20050124001082005012400108NM 2005 1 24 HNAA0400173 120041220A3397817142AA1 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003NM EMERGENCY LIGHTSINOPERATIVE A HNAAO OTHER O OTHER CRCRUISE 1 EA07908HA 015 EMERGENCY LIGHTS FLICKERED ON AND OFF SEVERAL TIMES IN FLIGHT. REMOVED AND REPLACED 9811-TB14 MODULES 4 AND 7. 2H72 4T RTA13NM 20050124001092005012400109NM 2005 1 24 WLDA2004121 120041226A5210 SOLENOID DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE PAX DOOR OVERHEATED A WRLAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11271 48518 SMOKE IN COCKPIT WHEN TAXI FOR TAKEOFF, RETURNED TO BLOCKS. FOUND DOOR SOLENOID VERY HOT AND SMOKING. DISCONNECTED AND TAPED WIRES BACK. C/B PULLED AND TRANSFERRED TO DMI M52DE2604-134 PER MEL 52-54-2 CAT "A". 2L73 4F4 FRTA22WE E24NE 20050126000532005012600053EA 2005 1 26 04366639 120041231A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA AIR CONDITIONINGNOISY A VTZAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 EA27639BR 7313 LOUD NOISE ON TAKEOFF ROLL COMING FROM AC PACK. PERFORMED ENGINE RUNS AND OP CHECKED PACKS IAW 72-00. 2L72 4F RTA21EA 20050126000762005012600076EA 2005 1 26 04365647 120041230A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY MALFUNCTIONED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27647BR 7399 SMOKE TOILET CAUTION MSG AFTER TAKEOFF. REMOVED AND REPLACED RETURN TO SEAT BULBS DUE TO WRONG PART NUMBER. ALSO, REPLACING LAV SMOKE DETECTOR (EICAS MESG BUT NO AUDIBLE WARNING). 2L72 4F RTA21EA 20050126000772005012600077NM 2005 1 26 HNAA0400174 120041223A2913570347 PUMP DHAV DHC8 DHC8102 2809003NM NR 2 HYD SYSTEM SHEARED A HNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 EA07937HA 148 NR 2 MAIN HYD PRESSURE WENT TO ZERO, WITH STANDBY PUMP PRESSURE. REMOVED AND REPLACED NR 2 HYD ENGINE DRIVEN PUMP AND CASE FILTER. OPS AND LEAK CHECK GOOD. FOUND HYD PUMP SHAFT SHEARED. 2H72 4T RTA13NM 20050126001012005012600101CE 2005 1 26 GLBA20030776 120041230A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM0396UX UE96 FOUR CRACKS .4 INCHES LONG EXTENDING FROM DEICE LINE HOLE IN HORIZ STAB MAIN SPAR CENTER WEB, REPAIRED PER EO 04/21 BEECH 1900 SRM 55-91-02 2L72 4T RTA24CE 20050126001182005012600118 2005 1 26 224873 420041228A3430 RECEIVER SAAB SF340 SF340A 7850100EU NAVIGATION INOPERATIVE A UHLAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL17121CQ 121 NR 1 AND NR 2 NAV RECEIVERS INOPERATIVE WITH MULTIPLE NAV FREQUENCIES SELECTED. NO CDI DISPLAY, NO DME, RMI'S SHOWED CORRECTLY. AIRCRAFT RETURNED TO MAINTENANCE HANGAR. 2L72 4T RTA52EU 20050126001192005012600119NM 2005 1 26 ASMF200412009 120041222A2913622532 PUMP BOEING757 7572Q8 1384972NM HYD SYSTEM DAMAGED W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23804AM4591 26271 CAPT REPORTED LT HYD SYSTEM LOST, LT HYD QTY AT EICAS FAULT CODE 291106-01, LT HYD ELECTRIC PUMP FAULT CODE 291133-01, PTU FAULT CODE 292201-00 AND RT ELECTRIC PUMP OVERHEAT AT EICAS FAULT CODE 291113-02; THEREFORE LANDING GEAR WAS OPERATED IN ALTERNATE MODE. WHEN A/C WAS IN RUNWAY, IT WAS TOWED TO PLATFORM BY TOWING TRUCK DUE TO THE STEERING WAS OUT OF SERVICE. DURING MX REVISION, A LEAK WAS DETECTED ON LANDING ACTUATION HYD LINE AND THE HYD TANK WAS EMPTY. THE HYD LINE WAS REPLACED IAW MM 32-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, LOW LT HYD QTY AND HYD LEAK ON PTU WERE DETECTED. PTU WAS REPLACED IAW MM 29-22-01, TESTED CORRECT. 2L72 4F RTA2NM 20050126001282005012600128NM 2005 1 26 2005UALA00066 120040116A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 RT CABIN WINDOW FRAME NR 6 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME. 2L72 4F4 FRTA2NM E17NE 20050126001782005012600178WP 2005 1 26 WLDA2004110 120041213A2530 OVEN DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE GALLEY CONTAMINATED A WRLAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11352 47838 CENTER GALLEY OVERHEAD LIGHT EMITTED ELECTRICAL SMELL. INVESTIGATED ELECTRICAL SMELL IN MID GALLEY AREA. CHECKED OVERHEAD LIGHTS AND ELECTRICAL CONNECTIONS, NO EVIDENCE OF ARCING OR BURNT CONNECTIONS, CHECKED ELECTRICAL CABLES FOR SIGNS OF DAMAGE, NONE EVIDENT. CHECKED OVENS, BURNED FOOD FOUND IN NR 5 OVEN. CLEANED SAME, NO OTHER FAULTS FOUND, OK TO CONTINUE. 2L73 4F4 F A22WE E23EA 20050126001792005012600179NE 2005 1 26 ERAA098184 120040908A6210 PAD SKRSKYS61 S61N 8142104NE MAIN ROTOR MISSING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03564EH4539 WEAR PAD MISSING. DEFORMING SHOULDER. RESULT, CRACKED. RECOMMEND ASSEMBLY PRACTICES DEVELOPED. VISUAL INSPECTION AND NDT CONFIRMATION. SCRAP AND RETURN TO ERA. 2G72 4U 1H15 20050126001852005012600185EU 2005 1 26 MALA040908 120041208A5320 BRACKET BAC 146 AVRO146RJ85A1500097EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15516XJ E2334 DURING C-CHECK INSPECTION IN YYC, BRACKET CRACKED BETWEEN FRAME 24 AND FRAME 25, NEXT TO LT WING FUSELAGE PANEL. (281BT)MAINTENANCE REPAIRED IAW SRM 51-71-11, FIG 2. REFER TO 409 NR 224597 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/13/2004. 2H74 4F RTA49EU 20050126001882005012600188 2005 1 26 MALA040729 420041113A22106227491210 COMPUTER SAAB SF340 SF340A 7850100EU E/E BAY MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15106XJ 340A106 AFTER TAKEOFF, YAW DAMPER WOULD NOT ENGAGE. NOTED BREAKERS N10 AND N11C/B POPPED, RESET BREAKERS, RECEIVED AUTOPILOT DISCONNECT TONE, ENGAGE YAW DAMPER AND RECEIVED AUTO TRIM MASTER WARNING. PERFORMED QRH MEMORY ITEMS RUDDER KICKED LEFT, DURING YAW DAMPER APPLICATION. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED FGC PN 622-7491-210, SN/ON 2029, SN/OFF 2364, CHECKS GOOD INSPECTED RUDDER AND SERVO LINKAGE FOR CONDITION. PERFORMED AILERON CONTROL FORCE CHECK, INSPECTED AND LUBED AILERON BELL CRANKS, AND ROD ENDS. AVIONICS TESTED YAW DAMPER SYSTEM ALL CHECKS GOOD. 2L72 4T RTA52EU 20050126001902005012600190NM 2005 1 26 CALA0400742 120041210A531165C229101 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717329 23459 INSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN FORWARD CARGO PIT AT STA 500D BETWEEN S27L AND S28L. INSTALLED REPAIR IAW SRM 53-00-07, FIGURE 205. 2L72 4F RTA16WE 20050126001942005012600194EU 2005 1 26 MALA040859 120041119A30202351A000 VALVE BAC 146 AVRO146RJ85A1500097EU ANTI ICE SYS MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15524XJ E2349 ENG NR 3 INTAKE LO PSI LIGHT ILLUMINATED IN FLIGHT GRADUALY WAS ABLE TO GET IT EXTINGUISHED 80-89 PERCENT. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 ENG INTAKE ANTI-ICE VALVE PN OFF 2351A000 SN OFF 899351-2 PN ON 2351A000-003 SN ON 899352-8 REF AMM 30-21-17. OPS AND LEAK CHECKS GOOD. 2H74 4F RTA49EU 20050126001982005012600198EU 2005 1 26 MALA040824 120041116A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15453XJ 340B453 DURING 6Y/4Y INSPECTION IN LAN, GALLEY SEAT TRACK CORRODED. MAINTENANCE REPLACED IAW SAAB SRM 51-40-27. REFER TO NRC NR 127281 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04. 2L72 4T RTA52EU 20050126002022005012600202EU 2005 1 26 MALA040831 120041123A5230 SKIN BAC 146 AVRO146RJ85A1500097EU CARGO DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15502XJ E2307 DURING C-CHECK INSPECTION IN YYC, AFT CARGO DOOR SKIN DAMAGED DURING OPERATIONS IN MSP. MAINTENANCE RESKINNED AFT CARGO DOOR IAW EO NR A52062. COMPLY WITH EO NR A62062. AIRCRAFT RETURNED TO SERVICE 11/23/04. 2H74 4F RTA49EU 20050126002032005012600203CE 2005 1 26 1663 120041130A21405543622155 CONTROL CABLE BEECH 58 58 1152740CE CABIN HEATER WORN E Z4TAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO0595KM TH1315 CABIN HEATER BECAME INOPERATIVE. FOUND BAD IRIS CONTROL CABLE SWITCH INOP. REPLACED AND OPS CK OK. 1L72 3O 3A16 20050126002072005012600207NM 2005 1 26 250TR0059 120041201A3350 LAMP BOEING737 7372K5 138448XNM EMERGENCY LIGHT INOPERATIVE A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 L-1, R-1, R-2 EXTERNAL EMERGENCY EXIT LIGHTS INOP. REPLACED LAMPS. OPS CHECKS GOOD PER MM 33-40-1. 2L72 4F RTA16WE 20050127000512005012700051NE 2005 1 27 HNAA0400160 220040722A7250311560101 TURBINE BLADES DHAV DHC8 DHC8201 2809001NM PWA PW120 PW123 NE NR 2 ENGINE CRACKED A HNAAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA07969HA12321 468 AG0080 ON TAKEOFF FROM HHH, AT 1000 FT, HEARD LOUD BANG FROM NR 2 ENGINE. ENGINE AUTO FEATHERED AND TQ WENT 0 PERCENT. COMPLETED SHUT-DOWN PER CHECKLIST AND DIVERTED TO MCAS BEAUFORT. LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION REVEALED HPT BLADE FAILURE. THERE WAS NO ENGINE CASE PENETRATION. 2H72 4T4 TRTA13NM E20NE 20050127000572005012700057NM 2005 1 27 ASAA0410582 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE LAP JOINT DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON EXTERNAL SKIN LAP JOINT, 2 INCH LONG. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050127000612005012700061WP 2005 1 27 AMTA200401474 120041206A3350 LIGHT LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4 54555NE EMERGENCY EXIT INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11161AT 1219 EGRESS TRACK LIGHT INOPERATIVE FROM SEAT 29ABC AFT, PAST GALLEY. REMOVED AND REPLACED (EXIT) LIGHT ASSY AT L3 DOOR. OPS CHECK GOOD. OK FOR SERVICE. 2L73 4F4 F A23WE E12EU 20050127000632005012700063WP 2005 1 27 GTIA040831 120041107A2913AS66411LS666 SHAFT DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE HYDRAULIC PUMP SHEARED A GTIAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23834NK 49847 AIR RETURN DUE TO LOSS OF LT SYSTEM HYDRAULIC PRESSURE. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP, NOTED SHEARED SHAFT. LEAK AND OPS CHECK GOOD. 2L72 4F4 FRTA6WE E2EA 20050127000662005012700066EA 2005 1 27 QXEA200400933 120041226A5320 WEB CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX RIGHT HAND LOWER WEB AT STATION 280 HAS CORROSION. REPLACED IAW SRM 51-42-06, 51-42-13. 2L72 4F RTA21EA 20050127000692005012700069NM 2005 1 27 HNAA0400159 120041030A2914570347 PUMP DHAV DHC8 DHC8102 2809003NM NR 1 HYD SYSTEM FAILED A HNAAO OTHER S AFFECT SYSTEMS CLCLIMB 1 EA07937HA 148 NR 1 EDP HYD PUMP FAILED AFTER T/O 20 MILES NORTH OF SBY, EXPERIENCED NR 1 HYD SYSTEM QUANTITY AND PRESS LOSS. REMOVED AND REPLACED R HYD PUMP AND HYDRAULIC LINE P/N 82970010-477. 2H72 4T RTA13NM 20050127000702005012700070NE 2005 1 27 GTIA040854 220041124A7230 FAN BLADE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE NR 2 ENGINE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23831NK 49617 LP NR 281042-3; UPON INSPECTION, AFTER AIRCRAFT RETURNED TO THE GATE, FOUND NR 2 ENGINE C-1 (6 EA) FAN BLADES CURLED. REMOVED AND REPLACED NR 2 ENGINE. 2L72 4F4 FRTA6WE E2EA 20050127000712005012700071WP 2005 1 27 GTIA040802 120041006A7933 BULB DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE OIL TEMP FAILED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23810NK 48015 RT ENGINE OIL TEMP HIGH 145 IN CLIMB, 12 MINUTES STABILIZED IN CRUISE, HIGH ON APPROACH 150, 5 MIN. REMOVED AND REPLACED NR 2 ENGINE OIL TEMP BULB. ENGINE OPS CHECK, OK. MM 79-32-01. 2L72 4F4 F A6WE E9NE 20050127000722005012700072NM 2005 1 27 SCNA04016 120041122A3350 LIGHT BOEING737 737800* NM CABIN LOOSE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15PHHZJ 30389 CREW REPORTED ROW 12 RT SIDE, EMERGENCY LIGHTING COMING UP. MAINTENANCE RESECURED TRACK LIGHTING, OK FOR SERVICE. 2L72 4F RTA16WE 20050127000742005012700074NM 2005 1 27 DHL2004747009 120041130A2782 ACTUATOR BOEING727 727224 1384076NM NR 1 SLAT INOPERATIVE A DHLAB EMER. DESCENT S AFFECT SYSTEMS DEDESCENT 1 SO01747DH 22253 "A" SYSTEM FAILED DURING LDG GEAR EXTENSION. PERFORMED ABNORMAL PROCEDURE AND LANDED. A/C TOWED IN. REMOVED AND REPLACED NR 1 SLAT ACTUATOR IAW M/M 27-81-31, NO LEAKS NOTED. 2L73 4F A3WE 20050127000752005012700075NM 2005 1 27 DHL2004747010 120041201A3260 WARNING LIGHT BOEING727 727224 1384076NM MLG ILLUMINATED A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01747DH 22253 AFTER T/O FROM IAH, GEAR HANDLE PLACED TO OFF THE RED DOORS LIGHT AND RT DOOR LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES LIGHTS WENT OUT. WHEN GEAR HANDLE PLACED TO UP APPROACHING CVG PLACED GEAR HANDLE TEE. CYCLED RIGHT HAND GEAR DOOR SEVERAL TIMES AND LUBED SWITCH, OPS CK GOOD IAW MM 32-12-1. 2L73 4F A3WE 20050127000772005012700077NE 2005 1 27 AMTA200401466 220041202A7261 LINE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT ENGINE LEAKING A AMTAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11523AT 30232 31672 RT ENGINE OIL QUANTY ZERO, OIL PRESSURE LOW (24-28 PSI). ENGINE WAS SHUT DOWN. ENGINE WINDMILLED 63 MIN W/ APPROX 12 PSI. OIL TEMP 100 DEGREES AT SHUTDOWN. REPLACED CRACKED OIL LINE. LEAK CHECKS GOOD. 2L72 4F4 FRTA2NM E12EU 20050127000782005012700078WP 2005 1 27 GTIA040834 120041005A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT - CORRODED INTERCOSTAL AND FRAME AT FS 1326, LONG 28L - 27L. REMOVED CORROSION ON FRAME, REMOVED CARGO TRACK FROM STA 1320-1271 (FOM), REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-5, 51-30-2. 2L72 4F4 F A6WE E9NE 20050127000792005012700079NM 2005 1 27 PCS2004F00000 120040811A2751 WARNING LIGHT BOEING727 7272F9 138407DNM PWA JT8 JT8D17 52049NE TE FLAPS ILLUMINATED A PCSAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO17199AJ 21426 AFTER DEPARTING, IB FLAPS WENT ASYMMETRIC FROM POSITION 5 DEGREES TO 2 DEGREES COMPLETED ABNORMAL CHECKLIST. JETTISONED FUEL DOWN TO MAX LANDING WEIGHT. AIRCRAFT DIVERTED BACK AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET AND RAN FLAPS 3 TIMES, OPERATION CHECK NORMAL. LUBRICATED ALL POSITION INDICATOR TRANSMITTERS PULLEYS AND CABLES. RAN FLAPS SEVERAL TIMES, CHECK NORMAL OPERATION. NO ASYMMETRY IAW MM27-51-0. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20050127000812005012700081NM 2005 1 27 ABXA040384 120041113A3397 WIRE BOEING767 767281 1385109NM EMERGENCY LIGHT LOOSE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23775AX 22790 CABIN ENTRY LIGHTS FLICKERED ACCOMPANIED BY ARCING IN THE AREA OF SWITCH. INSPECTED WIRE ON BACK SIDE OF SWITCH, FOUND LOOSE WIRE. REINSTALLED WIRE ON SWITCH, OPS CHECKED GOOD. 2L72 4F RTA1NM 20050127000832005012700083 2005 1 27 AMTA200401476 420041207A2565 GIRT BAR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE L1 DOOR OUT OF POSITION A AMTAK NONE O OTHER ININSP/MAINT 1 GL11528AT 30887 UNABLE TO ARM L -1 DOOR. REPOSITIONED GIRT BAR AFTER REMOVING DEBRIS. OPS CHECK NORMALLY. ARMED SEVERAL TIMES. OK FOR SERVICE IAW MM 52-11-25/501. 2L72 4F4 FRTA2NM E12EU 20050127000892005012700089WP 2005 1 27 WX0400068 120041222A3250 STEERING SYS DOUG DC9 DC983 3022083WP NLG MALFUNCTIONED A WX0AO OTHER O OTHER TXTAXI/GRND HDL 1 WP19865GA 49998 FNL TO LAS - CREW CONTACTED MAINTENANCE CONTROL TO REPORT AIRCRAFT NOSE WHEELS DROVE OFF TAXIWAY INTO DIRT AT FNL. MAINTENANCE POSITIONED AIRCRAFT BACK ONTO TAXIWAY AND INSPECTED NOSE LANDING GEAR IAW 05-51-03 A-CHECK. NO DAMAGE NOTED, OKAY FOR CONTINUED SERVICE. AIRCRAFT RETURNED TO SERVICE . 2L72 4F RTA6WE 20050127000902005012700090EA 2005 1 27 COMA0460660 120041203A2621346000371 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CARGO BAY DISCHARGED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01811CA13514 7380 FLIGHT 5217 - CARGO FIRE BOTTLE LOW PRESSURE MESSAGE. REPLACED THE CARGO FIRE BOTTLE. 2L72 4F RTA21EA 20050127000922005012700092NM 2005 1 27 DHL2004752010 120040928A2740657278419 STABILIZER BOEING727 727223 1384074NM TAIL DAMAGED A DHLAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO01752DH 22466 LEFT HORIZONTAL STAB AND ELEVATOR DAMAGED FROM TAXIING A/C TURNING INTO SPOT. A/C WAS PARKED. REPLACED LEFT ELEVATOR ASSY IAW BMM 27-30-01. RIG AND OPS CHECKED IAW BMM 27-30-01. REPLACED LT HORIZ STAB TIP ASSY IAW 55-10-11. NO FURTHER NOTED. OPS OK. 2L73 4F A3WE 20050127000932005012700093NM 2005 1 27 NACA20040041 120040928A52305216838 DEPRESSOR BOEING727 72723 1384004NM CARGO DOOR SEAL BENT A NACAA UNSCHED LANDING O OTHER CRCRUISE 1 AL03992AJ 19428 RETURNED TO ANCHORAGE DUE TO LOW CABIN PRESSURE. FOUND MCD SEAL DEPRESSOR AT FORWARD LOWER CORNER BENT. RECONTOURED DEPRESSOR. DOOR FUNCTIONED GOOD. 2L73 4F A3WE 20050127000952005012700095 2005 1 27 GTIA040822 420041025A2565 LANYARD DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE L1 DOOR SLIDE LOOSE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23800NK 49144 L1 DOOR GIRT BAR WAS DIFFICULT TO UNLATCH. FOUND LANYARD LOOSE, RESECURED LANYARD AND CLEANED GIRT BAR LATCH, OPS CHECK GOOD. 2L72 4F4 F A6WE E9NE 20050127000972005012700097WP 2005 1 27 IXXA0400108O 120040929A2697 WIRE DOUG DC8 DC871F 302199DWP FIRE LOOP CHAFED A IXXAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SW11823BX86760732 46064 ON APPROACH TO KRFD, THE NR 1 SHORT LIGHT AND NR 1 FIRE LIGHT ILLUMINATED INTERMITTENTLY THEN CAME ON STEADY, NR 1 ENGINE SHUTDOWN. DURING ENGINE SHUTDOWN, THE ENGINE DID NOT SHUTDOWN WITH THE FIRE HANDLE. ENGINE DID NOT SHUT DOWN UNTIL FUEL SHUTOFF LEVER WAS PLACED TO OFF. THE CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. THE ENGINE SHORT LIGHT REMAINED ILLUMINATED AND FIRE TEST NR 1 ENGINE INOP. AN INVESTIGATION IS ON GOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE FOUND CHAFFED AND SHORTED WIRES IN J BOX AFT AREA UNDER T/R. THE WIRE WAS REPAIRED PER ALL APPLICABLE MANUALS, RAN ENGINES PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050127000982005012700098CE 2005 1 27 0034 120040622A2134E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE OUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESSURIZATION CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050127001002005012700100CE 2005 1 27 0036 120040622A2134E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE CABIN PRESSURE OUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050127001022005012700102CE 2005 1 27 0038 120040622A2134E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE CABIN PRESSURE OUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050127001072005012700107EA 2005 1 27 COMA0460665 120041202A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA AVIONICS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01868CA5091 7427 FLIGHT 9463 - FLAPS FAIL CAUTION. REPLACED THE FECU. 2L72 4F RTA21EA 20050127001242005012700124CE 2005 1 27 67554 120041212A2720 YAW DAMPER BEECH 1900 1900D 1154162CE RUDDER PEDALS MALFUNCTIONED A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07146ZV UE146 WHEN YAW DAMPER SYS ON, CREW EXPERIENCED A MOMENTARY STIFFNESS IN THE RUDDER PEDALS. CREW SHUT OFF THE YAW DAMPER AND CONTINUED FLIGHT WITH NO FURTHER INCIDENT. PERFORMED TAXI TEST. INSPECTED, OPS CHECK NORMAL AT THIS TIME. 2L72 4T RTA24CE 20050127001252005012700125CE 2005 1 27 67556 120041212A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE MLG WEAK A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07163YV UE163 CREW EXPERIENCED WEAK BRAKING ACTION ON RIGHT SIDE ON TAXI IN WITH NO FURTHER INCIDENT. BLED BRAKES. 2L72 4T RTA24CE 20050127001262005012700126CE 2005 1 27 67819 120041221A3242 BRAKE ASSY BEECH 1900 1900D 1154162CE LT MLG SMOKE A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE07176YV UE176 AFTER LANDING IN MIA CREW NOTICED LEFT BRAKES SMOKING. CLEANED LEFT MAIN GEAR BRAKE ASSY. CHECK OK AT THIS TIME. 2L72 4T RTA24CE 20050127001272005012700127CE 2005 1 27 67971 120041226A32601293840091 ANNUNCIATOR BEECH 1900 1900D 1154162CE MLG FAILED A AMWAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE07182YV UE182 TAIL DE-ICE ANNUNCIATOR FAILED IN FLIGHT DURING ICING CONDITIONS, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED TAIL DE-ICE SENSOR AND SERVICED TUBES, OPS CHECK GOOD. 2L72 4T RTA24CE 20050127001282005012700128CE 2005 1 27 67974 120041226A3231 WIRE BEECH 1900 1900D 1154162CE MLG CHAFED A AMWAO OTHER J WARNING INDICATION CLCLIMB 1 CE07146ZV UE146 DEPARTING OMA RETRACTED GEAR, C/B TRIPPED. RESET C/B, GEAR THEN RETRACTED, C/B TRIPPED AGAIN. DID NOT RESET 2ND TIME PER CHECK LIST. DIVERTED TO HON MANUAL EXTENSION. MX THEN SECURED LANDING GEAR AND TOWED A/C TO GATE. REPAIRED CHAFED WIRE ON HYDRO GROUND. 2L72 4T RTA24CE 20050127001292005012700129CE 2005 1 27 68027 120041229A3220 WHEEL BEECH 1900 1900D 1154162CE NLG DAMAGED A AMWAO OTHER O OTHER LDLANDING 1 CE07126YV UE126 UPON LANDING ROLLOUT, A COYOTE RAN INFRONT OF THE AIRCRAFT AND WAS STRUCK BY THE NOSE LANDING GEAR. CREW SLOWED AND STOPPED THE AIRCRAFT ON THE APRON WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NOSE WHEEL ASSY, NOSE GEAR ASSY, DRAG LEG ASSY. VISUALLY INSPECTED ATTACH POINTS AND GEAR ACTUATOR. OPS CHECK NORMAL. 2L72 4T RTA24CE 20050127001662005012700166NM 2005 1 27 0402256719 120041224A5311 FRAME BOEING747 747251F 1384898NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01619US 21321 DURING L-CHECK, FOUND CRACK IN FRAME AT BS 380 S24R. REPAIRED PER EA 67-165180. 2L74 4F A20WE 20050126000192005012600019WP 2005 1 26 DHL2004807015 120041230A3297 WIRE DOUG DC8 DC873F 302199FWP DOWNLOCK SWITCH BROKEN A DHLAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO01807DH 45990 DURING APPROACH, NOSE GEAR LIGHT DID NOT ILLUMINATE. WENT AROUND AND ACCOMPLISHED ABNORMAL PROCEDURE. NO LIGHT. DURING RETURN TO AIRPORT LIGHT ILLUMINATED AT 50' AGL LIGHT EXTINGUISHED LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE AT NOSE DOWN LOCK SWITCH REPLACED PIN NR 6 ON CONNECTOR CLEANED PLUG. OPS CKS GOOD IAW DC8 MM 32-60-0. 2L74 4F RT4A25 20050126000352005012600035EU 2005 1 26 RAIA00412028 120041223A30103D354701 PRESSURE SWITCH JETAIRJETSTMJETSTM4101 1500501EU DE ICE SYSTEM FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03557HK15349 41074 3648- ABE- AIRFRAME DE-ICE BOOTS CCT2 AND CCT3 FAULTS. REMOVED AND REPLACED PRESSURE SWITCH. 2L72 4T RTA41NM 20050126000392005012600039NM 2005 1 26 P5CA0501299 120041230A7100 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 4 FAILED A P5CAEFJAENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15858FT 20109 662473 DURING FULL THRUST T/O 650' NR 4 ENGINE FAILED WITH FIRE INDICATION. SHUT DOWN ENGINE AND FIRED BOTTLES. REPLACED NR 4 ENG PER WC 7100-002. RUN UP OK. 2L74 4F4 F A20WE E20EA 20050126000442005012600044NM 2005 1 26 ASMF200412003 120041215A215032144884 SHUTOFF VALVE BOEING757 7572Q8 1384972NM LT PACK FAILED W ASMFE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM1760 1760 26273 CAPTAIN REPORTED THAT WHEN LEFT THRUST LEVER WAS LOCATED IN IDLE POSITION THE AIR-CONDITIONING PACK WAS SHUTDOWN AND "HI STAGE" LIGHT TURNED ON. DUAL VALVE WAS REPLACED IAW MM 36-11-08, ALL CORRECT. DURING ENGINE STARTING, "HI STAGE" LIGHT DID NOT TURNED OFF, ENGINES WERE SHUTDOWN AND PILOT REGULATOR WAS RESEATED, LIGHT TURNED OFF. LEFT ENGINE WAS STARTED AND FAIL CONTINUE. AIRCRAFT WAS SENT TO THE HANGAR, LEFT HIGH PRESSURE SHUTOFF VALVE WAS REPLACED IAW MM 36-11-07, TESTED CORRECT. 2L72 4F RTA2NM 20050126000632005012600063SO 2005 1 26 RAIA00412032 120041222A361014541376401 EXHAUST DUCT EMB 145 EMB145ER 3260211SO NR 1 PRECOOLER DAMAGED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03808HK 145157 3566- PIT- NR 1 BLEED OVERTEMP. MAINTENANCE REMOVED AND REPLACED NR 1 PRECOOLER EXHAUST DUCT ASSY. 2L72 4F RTT00011AT 20050126000832005012600083EA 2005 1 26 QXEA200500048 120041228A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - LEFT HAND OUTBOARD SEAT TRACK HAS CORROSION AT STATION 738 TO 756. REPLACED IAW CRJ AMM 53-00-49. 2L72 4F RTA21EA 20050126001372005012600137NM 2005 1 26 HNAA0400175 120041228A5610NP1579014 WINDSCREEN DHAV DHC8 DHC8102 2809003NM COCKPIT CRACKED A HNAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA07815EX 321 FO'S WINDSCREEN SPIDERWEBBED. REMOVED AND REPLACED FO'S WINDSCREEN OPS CHECK GOOD. 2H72 4T RTA13NM 20050126001502005012600150EU 2005 1 26 DHL2005362501 120041206A5414 SKIN AIRBUS300 A300B4203 3930306EU NR 2 PYLON CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DURING "C" CHECK, FOUND RT WING IB SIDE PYLON NR 2 WING T/E LWR SIDE ACCESS PANEL, CLOSE PYLON RIB 22 PANEL CUT OUT HAS CORROSION. REMOVED PREVIOUS REPAIR FOR ACCESS TO REMOVE CORROSION AREA RT WING I/B SIDE PYLON NR 2 T/E LWR SIDE. CLEANED & REMOVED CORROSION AREA FOUND BEYOND LIMITS IAW A-300 SRM 57-33-11. ACCOMP VISUAL INSPECTION OF REPAIR AREA IAW ASTAR EVA 5724-043, STEP 1, PAGE 2. FOUND CORROSION ON SKIN LWR SURFACE OF PNL EXTENDING BEYOND FASTENER HOLE FOR NEW REPAIR DOUBLER; I/B EDGE. 2L72 4F RTA35EU 20050126001512005012600151WP 2005 1 26 DHL2004809010 120041203A3350CA101N BATTERY DOUG DC8 DC873F 302199FWP EMERGENCY LIGHT INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH 46047 ON PREFLIGHT WHILE DOING BATTERY TEST, EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE. DURING SUBSEQUENT TESTS, EMERGENCY EXIT LIGHT DID ILLUMINATED, BUT FAILED WHEN IGNITION POWER WAS PLACED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND A/C MAIN BATTERY, OPS CHECK GOOD, PER MM 33-50-2 AND MM 24-30-1. 2L74 4F RT4A25 20050126001562005012600156EU 2005 1 26 MALA050124 120040108A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425XJ 340B425 DURING 4Y/2Y CHECK IN BNA, SEAT TRACK AT BLO BETWEEN FS 294-319 IS CORRODED OUT OF LIMITS AND DAMAGED SECTION WILL BE REMOVED AND REPLACED AS NEEDED IAW MESABA EO NR S53060. REFER EAMS WO NR 211363, TASK 1512 FOR ADDITIONAL INFORMATION. AIRCRAFT WAS RELEASED 1/11/05. 2L72 4T RTA52EU 20050126001642005012600164NM 2005 1 26 QXEA200500008 120041231A2810DSC33816D FITTING DHAV DHC8 DHC8202 2809007NM FUEL SYSTEM LEAKING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09368PH14842 512 PDX - A FUEL LEAK WAS NOTED BY MAINTENANCE AFT OF THE NR 2 WHEEL WELL. THE SYSTEM WAS INSPECTED AND THE WIGGINS FITTING OF THE MASTER REFUEL VALVE WAS REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050126001802005012600180EU 2005 1 26 ERAA098192 120040910A3212D24762101 FLOAT BOLKMS105 BO105S 5626006EU MLG LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH S675 HOLES IN AFT COMPARTMENT OF FLOAT BAG. FLOAT WAS INSPECTED AND REPAIRED IAW OHSS-100-1. C/W INSPECTION IAW BO105-25-60-95. 1G72 3U H3EU 20050126001932005012600193SO 2005 1 26 623 120041130A27521159SCC5005 ACTUATOR GULSTMGV GULFSTREAMGV3980116SO ZONE 300 MALFUNCTIONED E N93AO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO13506QS3812 623 AFTER LANDING, SELECTED FLAPS TO UP BUT DID NOT MOVE. FLAP/STAB FAIL MESSAGE, FLAP/STAB IND INOP MESSAGE. 2L72 4F RTA12EA 20050126001972005012600197NM 2005 1 26 DHL2004754025 120041103A3241 METERING VALVE BOEING727 727223 1384074NM RT MLG BRAKE FAILED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01754DH 22008 NR 3 AND NR 4 MLG BRAKES DRAGGING. REMOVED AND REPLACED RMLG BRAKE METERING VALVE, RT BRAKE SPRING CARTRIDGE, AND RIGGED RT AND LT BRAKE CONTROL LINKAGE PER B727 M/M 32-41-11 AND 32-41-01. LEAK, FUNCTIONAL, AND OPS CHECKS GOOD PER B727 M/M 32-41. 2L73 4F A3WE 20050126001992005012600199NM 2005 1 26 DHL2004746008 120041104A2510 MECHANISM BOEING727 727224 1384076NM 1ST OFFICER SEATLACK OF LUBE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01746DH 22252 FIRST OFFICERS SEAT HEIGHT ADJUSTMENT CANNOT BE USED. CLEANED AND LUBRICATED MECHANISM, OPS CHECK GOOD PER MM 25-10-40. 2L73 4F A3WE 20050126002012005012600201NM 2005 1 26 DHL2004745024 120041127A5270 CONNECTOR BOEING727 727224 1384076NM MLG DOOR CONTAMINATED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01745DH 20665 DURING GR RETRACTION "DOORS" LIGHT ILLUMINATED WHEN HANDLE WAS RETURNED TO "OFF" POSITION. LIGHTS STAY OFF IF GEAR HANDLE IS LEFT IN THE 'OFF' POSITION. RIGHT GEAR DOOR LIGHT ON S/O PANEL WAS OBSERVED TO FLI. REMOVED RTV FROM CONNECTOR, REMOVED CONNECTOR AND FOUND CONNECTOR FULL OF WATER. DRIED AND CLEANED CONNECTOR AND CONDUIT OF ALL WATER. CHECKED RIGGING AND OPERATION OF DOOR LOCK ACTUATOR AND SWITCH. NO DEFECT. 2L73 4F A3WE 20050126002042005012600204 2005 1 26 DHL2004764010 420041124A344064021101101SC DISPLAY BOEING727 727264 138408MNM TAWS FAILED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO01764AT 22984 WX RADAR MADE GRINDING NOISE WX RADAR C/B THEN POPPED SMELLED ELECTRICAL SMOKE. REMOVED AND REPLACED TWAS DISPLAY (MFD 640) IAW MMS 34-20-02, OPS CK NORMAL PER CM 34-20-02-01. 2L73 4F A3WE 20050126002062005012600206EU 2005 1 26 YENA200459 120041127A3242 STEERING SYS AIRBUS320 A320232 3930326EU NLG MALFUNCTIONED A YENAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 EA15558JB 1915 STEERING AND BRAKES FAILED ON TAKEOFF ROLL. PERFORMED BITE TEST OF BSCU PER AMM 32-46-00, NO FAULTS NOTED, PERFORMED OPERATION CHECK OF NOSE GEAR STEERING PER AMM 32-51-00. ALL CHECKS NORMAL. NO FAULT NOTED AIRCRAFT CLEARED FOR SERVICE. OPS CHECK NORMAL BRAKE SYSTEM AMM 32-42-00. ALL CHECKS NORMAL. 2L72 4F RTA28NM 20050127000342005012700034 2005 1 27 VW3R200400007 420041228A2565 PAD AIRCRUISERS AIRBUS330 A300* EU GIRT BAR MISINSTALLED B VW3RK NONE W INADEQUATE Q C ININSP/MAINT 1 WP09ALL ALL GIRT EXTENSION DOES NOT FIT PROPERLY ON GIRT BAR. GIRT EXTENSION PADS RIDE UP ON CAVITY RIDGE OF GIRT BAR. 2L72 4F RTA26NM 20050127000382005012700038 2005 1 27 HNAA0400155 420041019A2565 BOTTLE DHAV DHC8 DHC8311 1386006EA SLIDE/RAFT LEAKING A HNAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA07333EN 221 DURING LAYOVER DITCHING DAM RT EMERGENCY EXIT DOOR WATER DAM WAS ACTIVATED BUT DID NOT DEPLOY. DURING LAYOVER F/A ATTEMPTED TO OPEN EXIT DOOR TO VENT A/C. F/A HERD A HISSING NOISE AND STOPPED REMOVING DOOR. FOUND HISSING NOISE TO BE NITROGEN FROM DITCHING DAM BOTTLE. SERVICED BOTTLE, OPS CHECKED DITCHING DAM SYSTEM NO DISCREPANCY NOTED AND THEN SERVICED AND REACTIVATED SYSTEM. 2H72 4T RTA13NM 20050127000452005012700045WP 2005 1 27 GTIA040837 120041110A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FLOORBEAM CRACKED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 AFT PIT OVERHEAD FLOORBEAM INTERCOSTAL CRACKED AT (4 EA) PLACES ALONG FASTENER HOLES, FS 1287-1309. REMOVED FLOORBEAM INTERCOSTAL AT FS 1287-1309, FABRICATED NEW INTERCOSTAL SRM 51-10-2 FROM 7075-T6-.063. HEAT TREATED NEW INTERCOSTAL, LOCATED AND DRILLED HOLES FOR NEW INTERCOSTAL, TREATED, PRIMED, TOP COATED, INSTALLED NUT PLATES AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-5, 51-30-2. 2L72 4F4 F A6WE E9NE 20050127000482005012700048NM 2005 1 27 AMTA200401384 120041107A7500 WARNING LIGHT BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT ENG BLEED SYSILLUMINATED A AMTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL11517AT 27973 LT BLEED (ENGINE) LIGHT CAME ON AT 80 KIAS ALSO ON EICAS ABORTED AC TAKEOFF. DEFERRED. 2L72 4F4 FRTA2NM E12EU 20050127000502005012700050NM 2005 1 27 QXEA200500071 120041215A5230 RETAINER DHAV DHC8 DHC8202 2809007NM CARGO DOOR SEAL DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09346PH 477 CARGO DOOR SEAL RETAINER DAMAGED. REPAIRED IN ACCORDANCE WITH RD8-52-086. 2H72 4T RTA13NM 20050127000562005012700056NE 2005 1 27 GTIA040829 220041101A7230 COMPRESSOR AIRBUSA321 A321211 3930370EU IAE V2533 V2533A5 NE RT ENGINE STALLED A GTIAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL23584NK 1408 V10417 LP NR 2907041; SHUTDOWN RT ENGINE, AIR RETURN. RT ENGINE COMPRESSOR STALL ON T/O AFTER V1, PULLED THROTTLE TO IDLE. TRIED ADVANCING POWER AGAIN ANOTER COMPRESSOR STALL AT ABOUT 1.3 EPR, FLEW SINGLE ENGINE APPROACH AND LANDING. REMOVED AND REPLACED RT ENGINE. 2L72 4F4 FRTA28NM E40NE 20050127000602005012700060WP 2005 1 27 GTIA040800 120041005A2612 FIRE LOOP DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE NR 2 B-LOOP INTERMITTENT A GTIAO OTHER N FALSE WARNING CLCLIMB 1 GL23810NK 48015 ON TAKEOFF, AFTER ROTATION, WITH FLEX POWER 1.86, THE NR 2 B-LOOP FIRE LIGHT BEGAN TO FLICKER UNTIL GEAR RETRACTION. ALL OTHER ENGINE INDICATIONS NORMAL. NOTE: NOSE WHEEL VIBRATION AFTER T/O UNTIL RETRACTION SEEMS TO COINCIDE WITH THE LIGHT FLICKER. 2L72 4F4 F A6WE E9NE 20050127000622005012700062WP 2005 1 27 GTIA040833 120040929A5720MS21063L314 CHANNEL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT WING CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 LT WING L/E STA XRS 240 AFT L/E FLANGE ACCESS PANEL ATTACHED HAS CORROSION AT GANG CHANNEL. REMOVED CORRODED GANG CHANNEL, INSTALLED NEW GANG CHANNEL IAW SRM 51-30-2. 2L72 4F4 F A6WE E9NE 20050127000732005012700073WP 2005 1 27 ASMF200411011 120041120A3260 SENSOR DOUG DC9 DC987 3022087WP NLG DAMAGED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23205AM 49405 A/C RETURNED, DUE TO "UNSAFE NLG" LIGHT TURNED ON & STRONG NOISE DETECTED. A/C SENT TO HANGAR & NOSE L/G DOORS INSPECT, DOORS TEST & EXTENSION/RETRACTION TEST WERE PERFORMED IAW MM 32-20-00, 32-22-01, 32-30-00, RESPECTIVELY, ALL CORRECT. DURING CLIMB IN NEXT FLT, A/C RETURNED OF FLT BY SAME FAILURE & A/C SENT TO HANGAR AGAIN. DURING OVERNIGHT SERVICE, NLG STRUT SERVICED, NLG DOORS PRECHARGE CHECKED, GEAR UP & LOCKED SENSOR & NLG ACTUATOR REPLACED, EXTENSION/RETRACTION TEST PERFORMED IAW MM 32-21-02, 32-22-01, 32-60-05, 32-32-06 AND 32-30-00, RESPECTIVELY. SENSORS D1-31 AND D1-32 WERE CHECKED & SENSOR D1-31 WAS REPLACED IAW MM 32-60-00, ALL CORRECT. O/W INSPECT PERFORMED IAW MM 05-51-04 AND TEST FLT WAS PERFO2L72 4F RTA6WE 20050127000992005012700099CE 2005 1 27 0035 120040622A2134E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE CABIN PRESSURE OUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050127001012005012700101CE 2005 1 27 0037 120040622A2134E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE CABIN PRESSURE OUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050127001702005012700170NE 2005 1 27 3641204 220041229A7261 CHIP DETECTOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE COCKPIT ILLUMINATED A NSVAO OTHER J WARNING INDICATION CRCRUISE 1 EA27347CJ 340B347 RIGHT CHIP DETECTOR LIGHT ILLUMINATED IN FLIGHT. 2L72 4T4 TRTA52EU E8NE 20050127001782005012700178NM 2005 1 27 234TR0024 120041030A5330 SKIN BOEING737 737228 13844AGNM FUSELAGE DAMAGED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05234TR 23004 REMOVED FUSELAGE SKIN FROM BS 1016 TO 1033 FROM STR 26 RT TO 26 LT FOR ACCESS TO BS 1016 BULKHEAD REPAIRS. REPAIRED FUSELAGE SKIN PER SB 737-53A1075. REPAIRS TO THE BS 1016 BULKHEAD THAT REQUIRED REMOVAL OF FUSELAGE SKIN ARE REPORTED ON UNIQUE CONTROL NR 234TR0022 AND 234TR0023. 2L72 4F RTA16WE 20050127001792005012700179WP 2005 1 27 UPS05843750 120041230A5712 RIB DOUG DC8 DC873F 302199FWP RT WING L/E CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 847. STOP DRILLED CRACK, VERIFIED STOP DRILL REF NDTSPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT7075T6-.050. INSTALLED REPAIR REF SRM 51-1-21, 51-1-20D, 51-1-8, 57-2-0 FIG 6, 57-3-3, 57-2-0 FIG 2. 2L74 4F RT4A25 20050202000252005020200025WP 2005 2 2 DHL2004801504 120040901A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT WING CTR L/E UPPER FORMER CRACKED 1.000, STA XFS 354.000. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050126001392005012600139NM 2005 1 26 QXEA200500004 120041229A2160 BAFFLE DHAV DHC8 DHC8202 2809007NM ZONE 100 INOPERATIVE A QXEAO OTHER J WARNING INDICATION DEDESCENT 1 NM09348PH17366 484 EUG - FLIGHT 2081 - THE CREW RAN THE CHECKLIST WHEN THE FLIGHT COMPARTMENT DUCT HOT CAUTION LIGHT ILLUMINATED ON DESCENT. MAINTENANCE INSPECTED THE SYSTEM AND PERFORMED MEGGERING AND INTEGRITY CHECKS OF THE WIRES AND SWITCHES. THE CHECKS WERE GOOD. MAINTENANCE REPLACED THE BAFFLE LOCATED IN THE ECS SPLITTER DUCT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVCICE. 2H72 4T RTA13NM 20050126001462005012600146CE 2005 1 26 GLBA20030763 120041116A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM0394GL UE94 .5 IN CRACKS EXTENDING FROM DE-ICE LINE HOLE AT MAIN SPAR WEB OF HORIZONTAL STABILIZER. REPAIRED CRACKS (4) .5 IN LONG IN WEB HOLE IAW EO 04-21 WHICH FOLLOWS BEECH SPM 55-91-02. 2L72 4T RTA24CE 20050126001692005012600169EU 2005 1 26 DHL2004367008 120041105A5270 WARNING LIGHT AIRBUS300 A300B4203 3930306EU DOOR WARNING FALSE INDICATIONA DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01367DH 265 DOORS LIGHT ILLUMINATED ON MWP WITH NO LIGHT ON S/O PANEL. TWO OCCURANCES. CYCLED EACH DOOR AND VISUALLY INSPECTED. NO FAULTS NOTED. DOOR WARNING SYSTEM, OPS CHECKED GOOD AS PER MM 52-71-11. 2L72 4F RTA35EU 20050126001722005012600172EU 2005 1 26 MHIA098050 120041113A5610350A25900400 WINDSHIELD UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE COCKPIT CRACKED B MHIAO OTHER O OTHER LDLANDING 1 EA25456AE 3492 23012 DURING DESCENT TO LANDING, PILOT NOTED CENTER WINDSHIELD CRACKED FROM JOGGLE POINT ACROSS LOWER WINDSCREEN. REPAIRED WINDSCREEN IN ACCORDANCE WITH EUROCOPTER STANDARD PRACTICE MANUAL SECTION 20.00.05.401 FOR FLIGHT TO MAINTENANCE. REPLACED WINDSCREEN WITH NEW. 1G72 3U3 U H9EU E00054EN 20050126001772005012600177NM 2005 1 26 WRNA200400016 120041114A5220 NUT BOEING747 747200 1384847NM HATCH HANDLE MISSING A WRNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05524UP 21446 AFTER TAKEOFF, CREW HEARD LOUD NOISE. DISCOVERED OVERHEAD EMERGENCY EXIT HATCH LEAKING EXCESSIVELY. RETURNED TO AIRFIELD, LANDING NORMAL. MAINTENANCE FOUND NUT MISSING FROM EMERGENCY ESCAPE HATCH LATCH HANDLE AND BOLT LOOSE. REINSTALLED BOLT AND NUT IAW B747 STD. PRACTICES. PERFORMED CHECK OF PRESSURIZATION SYSTEM IAW B747 MM 21-31-00. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 20050126001812005012600181EU 2005 1 26 MALA040906 120041203A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 DURING 4K INSPECTION IN BNA, SEAT TRACK AT LBL 18.3 IS CORRODED ON INBOARD FLANGE, BETWEEN FS 294 AND FS 319. THE OUT OF LIMITS AREAS WERE REPAIRED IAW MESABA EO NR S53079. REFER EAMS WORK ORDER NR 211114/TASK 1523 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050126001832005012600183EU 2005 1 26 MALA040909 120041220A5330 ICE SHIELD SAAB SF340 SF340A 7850100EU FUSELAGE DENTED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15110XJ 340A110 DENTS DISCOVERED ON RT ICE SHIELD. MAINTENANCE CARRIED OUT REPAIR IAW MESABA EO NR S53276. REFER TO LOG PAGE 1335862 FOR ADDITIONAL INFORMATION. 2L72 4T RTA52EU 20050127000432005012700043WP 2005 1 27 ASMF200412004 120041217A2131 CONTROLLER DOUG DC9 DC982 3022082WP NR 2 MALFUNCTIONED W ASMFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW23501AM 49188 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AS A CONSEQUENCE OF PRESSURIZATION FAILED. CAPTAIN REPORTED THAT DURING FLIGHT AT 35000 FEET, CABIN PRESSURE INCREASED AND DECREASED 500 FEET, AFTER THAT CONDITION WAS SELECTED PRIMARY AND SECONDARY SYSTEM AND AFTER 10 MINUTES PRESSURE WAS LOST AND "CABIN ALT" LIGHT TURNED ON. CONTROLLERS WERE CHECKED AND FAIL WAS DETECTED ON CONTROLLER NR 2 AND PRESSURE VALVES WERE DETECTED DIRTY. PRESSURE VALVES WERE CLEANED AND TESTED IAW MM 21-32-5, ALL CORRECT. DURING OVERNIGHT SERVICE, CABIN PRESSURE CONTROLLERS NO. 1 AND 2, AND PRESSURE VALVES, WERE TESTED IAW MM 21-32-00, ALL CORRECT. 2L72 4F A6WE 20050127000462005012700046NE 2005 1 27 MALA040816 320041019A6110 BLADE SAAB SF340 340B 7860101EU ROTOL R390 R3904123F27 NE PROPELLER DEBONDED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED 1,2,3 BLADES HAVE DISBONDS IN NICKEL LEADING EDGE. MAINTENANCE REPLACED RT PROPELLER, IAW MESABA JOB CARD 6110-303. REFER TO NRC NR 196549 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2L72 4T RTA52EU 6 CP31NE 20050127000492005012700049NE 2005 1 27 GTIA040799 220040921A7250 TURBINE BLADES DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 1 ENGINE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23801NK5981 48048 725446 DURING NOTCH CK IW SB A6224, TABLE 3, FOUND MORE THAN ONE - 4TH STAGE BLADES WITH LESS THAN OR EQUAL TO 5 IN LBS (6 BLADES LOOSE). REPLACED WITHIN 20 HOURS OR CYCLES. REMOVED AND REPLACED ENGINE. 2L72 4F4 F A6WE E9NE 20050127000552005012700055NM 2005 1 27 ASAA0410581 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE LAP JOINT DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN LAP JOINT, 18 INCHES LONG. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050127000642005012700064NE 2005 1 27 GTIA040828 220041027A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 1 MALFUNCTIONED A GTIAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 GL23820NK 49126 716757 LT 283881; INFLIGHT SHUTDOWN - DIVERSION, SHUTDOWN LT ENGINE DUE TO LOW OIL PRESSURE, LOW OIL QTY. REMOVED AND REPLACED NR 1 ENGINE. 2L72 4F4 F A6WE E9NE 20050127001042005012700104EU 2005 1 27 DJFA2004008 120040526A5730 SKIN BRAERODH125 BAE125800A 1500285EU WING CORRODED E DJFAK NONE O OTHER ININSP/MAINT 1 EA23867CW 258067 DURING INSPECTION OF THE WING, AFTER LEADING EDGES WERE REMOVED, CORROSION WAS FOUND ON THE WING SKIN SURFACES WHERE THE LEADING EDGES FIT ON. RAYTHEON AIRCRAFT WAS NOTIFIED AND A FIELD REPAIR FOR REMOVING THE CORROSION WAS APPROVED. ALL CORROSION WAS CLEANED AND SURFACES INSPECTED AND PRIMED. 2L72 4F RTA3EU 20050127001062005012700106CE 2005 1 27 GLBA20030750 120041029A52201294300433 PAN BEECH 1900 1900D 1154162CE EXIT WINDOW CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03257GL UE257 SEAT 4C, 6C, 6A, EMERG EXIT WINDOWS PAN CRACKED. REMOVED AND REPLACED WINDOW PANS. 2L72 4T RTA24CE 20050127001092005012700109 2005 1 27 DHL2004801014 420041119A221075130 TRANSFER VALVE DOUG DC8 DC873F 302199FWP RUDDER FAILED A DHLABA EMER. DESCENT UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO01801DH 46033 RUDDER INDICATOR WAS FULL LEFT. IT TOOK 5 1/2 UNITS TO MAINTAIN STRAIGHT AND LEVEL. WHEN THE RUDDER TRIM WAS MOVED TOWARD ZERO THE AIRCRAFT MADE AN AGGRESSIVE ROLL TO THE LEFT. DID NOT TRY TO FLY AIRCRAFT WITH YAW. REMOVED AND REPLACED ROLL SERVO DRIVE IAW DC-8 M/M 22-10-4, NO HELP. REMOVED AND REPLACED RUDDER TRANSFER VALVE IAW DC-8 M/M 27-21-6, OPS CHECKS SERVICEABLE. 2L74 4F RT4A25 20050131000212005013100021EA 2005 1 31 SWIA200414421 120040901A5315 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07454SW 7749 CORROSION FOUND ON LONGITUDINAL FLOOR SUPPORT AT RBL 27 APPROX FS 559 + 110 IN AFT BAGGAGE COMPARTMENT AT FLOORBOARD LOCATIONS 282 FRF AND 282 HRF. ITEM FOUND AT C-CHECK INSPECTION. REMOVED CORROSION IAW SRM 51-21-06 PG 1 & PG 2. CORROSION DID NOT PENETRATE PROTECTIVE LAYER. 2L72 4F RTA21EA 20050131000222005013100022EA 2005 1 31 SWIA200414422 120040901A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07454SW 7749 ON 625 BULKHEAD STRINGER 13L AND 13R CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED 2 REPLACEMENT BRACKETS PER RJ200 SRM 51-42-21 PG 13. 2L72 4F RTA21EA 20050131000232005013100023EA 2005 1 31 SWIA200414423 120040901A5312 ANGLE CNDAIRCL600 CL6002B19 1900309EA BULKHEAD CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07454SW 7749 AT 280 BULKHEAD, BL 9.00 & BR 9.00 2 ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED THE NEW ANGLES AT FS 280 L & R BL 9 UNDER FLOORBEAMS IAW EO 601R-53-11-136. 2L72 4F RTA21EA 20050127000582005012700058 2005 1 27 VW3R200400002 420041126A2564P3030029 ELT BFGOODRICH DOUG MD11 MD11F 3023600NM LIFE RAFT INOPERATIVE B VW3RK NONE L NO TEST ININSP/MAINT 1 WP23 10R418 ELT DOES NOT TRANSMIT ANY SIGNAL AND NEEDS TO BE REPLACED. 2L73 4F RTA22WE 20050127000802005012700080NE 2005 1 27 746002 220041121A7200 ENGINE BOEING747 747206B 1384856NM GE CF6 CF650E2 30018NE NR 4 FAILED A Q2SAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NE03746SA 21111 517136 ON TAKEOFF, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL. CREW SHUT DOWN ENGINE, DUMPED FUEL AND RETURNED TO BASE. ENGINE BOROSCOPED WITH NO DEFECTS NOTED. FOUND METAL IN TAILPIPE. ENGINE IS BEING REPLACED AT THIS TIME. 2L74 4F4 FRTA20WE E23EA 20050127000822005012700082WP 2005 1 27 GTIA0408806 120040914A5330 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23814NK 49619 RADIO ALTIMETER ANTENNA HAS CORROSION AT SKIN. REMOVED ANTENNA DOUBLER. LOCATED AND DRILLED NEW DOUBLER. INSTALLED DOUBLER ANTENNA. 2L72 4F4 FRTA6WE E9NE 20050127000862005012700086SO 2005 1 27 CHQA200500004 120040112A2611 WARNING SYSTEM EMB 145 EMB145LR 3260212SO LAV SMOKE FALSE ACTIVATIONA CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11971RP 145426 FLIGHT 901 ORD TO YIP - PILOT RETURNED TO FIELD DUE TO LAV SMOKE INDICATION ON CLIMB-OUT. PILOT RPTS RECEIVED TRIPLE CHIME, MASTER CAUTION AND LAV SMOKE. FLT ATTENDANT DID NOT SEE OR SMELL SMOKE. MX PERFORMED LAV SMOKE INSPECTIONS AND PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. 2L72 4T RTT00011AT 20050127000912005012700091 2005 1 27 GTIA040823 420041026A2565 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE R1 DOOR SLIDE DISCONNECTED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23831NK 49617 R1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. SECURED R1 DOOR EMERGENCY SLIDE LANYARD, OK FOR SERVICE. 2L72 4F4 FRTA6WE E2EA 20050127000962005012700096EU 2005 1 27 ALGA096919 120040814A6300C622A1003103 SCISSORS UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL1175 1263 FOUND WEAR PLATE DEBONDED. REPLACED WITH NEW PART IN FIELD. 1G72 3U NCR0001RD 20050127001052005012700105CE 2005 1 27 4023 120040917A7603 THROTTLE ARM BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO THROTTLE BODY BROKEN E BSYAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 GL07696BD TH352 827264R AIRCRAFT WAS ON APPROACH AND ENGINE WOULD NOT RESPOND TO POWER LEVER ADJUSTMENTS. ENGINE WAS SHUT DOWN AND LANDING WAS MADE. VISUAL INSPECTION REVEALED THROTTLE ARM BROKEN AT THROTTLE BODY. REPLACED WITH NEW. 1L72 3O3 O 3A16 E5CE 20050127001082005012700108NE 2005 1 27 EIA2004136 220041105A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 2 FAILED A EIAAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 NM09482EV 20713 701664 EN ROUTE FRA/HKG, CRUISE CONFIGURATION AT FLT LEVEL 37K, CREW NOTICED MOMENTARY VIBRATION/RUMBLE, AND OBSERVED LOSS OF NR 2 ENGINE POWER (ROLL BACK). ENGINE INSTRUMENTS AT IDLE VALUES WITH N1 RPM ZERO. REPEATED THROTTLE CYCLING PRODUCED NO ENGINE RESPONSE. PERFORMED IFSD, ENGINE WINDMILLED WITH POSITIVE OIL PRESS (+ 5 PSI) FOR APPROX 3 MINUTES. ENGINE SUCCESSFULLY RE-STARTED AND OPS CHECK OK. NORMAL ENGINE OPERATION FOR DURATION OF FLIGHT TO ORIGINAL DESTINATION. UNSUCCESSFUL SPOOL UP AFTER MAINTENANCE AND RESTART ON GROUND, REMOVED AND REPLACED NR 2 ENGINE. 2L74 4F4 F A20WE E20EA 20050127001102005012700110WP 2005 1 27 DHL2004801529 120040907A5347 CARGO TRACK DOUG DC8 DC873F 302199FWP CARGO BAY WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 MAIN CARGO COMPT NR 2 TRACK LUGS WORN, STA 319.000. CUT OUT DAMAGED SECTION AND FABRICATED NEW TRACK PLUG (S2772660) IAW DC8 SRM 53-2-3 PG 17-19. CLEANED, TREATED AND PRIMED AREA AND NEW TRACK PLUG IAW DC8 SRM 51-1-8B. INSTALLED NEW CHANNEL AND TRACK PLUG IAW DC8 SRM 53-2-3 PG 17-19, DC8 SRM 51-3-0 PG 1-2. 2L74 4F RT4A25 20050127001882005012700188 2005 1 27 3651204 420041228A61228210410 GOVERNOR BEECH 1900 1900D 1154162CE LT PROPELLER MALFUNCTIONED A NSVAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27171CJ UE71 LEFT AUTOFEATHER DID NOT ARM ON TAKEOFF. 2L72 4T RTA24CE 20050127001992005012700199NM 2005 1 27 AWXA200500059 120041224A5320654681282 WEB BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF LT AFT OUTBOARD SHEAR WEB BETWEEN BS 996 AND BS 1005, LBL 39 TO LBL 42, WL 208. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 996 TO BS 1005, LBL 39 TO LBL 42; FABRICATED A NEW REPLACEMENT SHEAR WEB PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4 & 8. 2L72 4F RTA16WE 20050128001002005012800100CE 2005 1 28 ACE122404 120041224A52101013840961 SHAFT BEECH 1900 1900C 1154161CE DOOR HANDLE SHEARED E YADAO OTHER O OTHER NRNOT REPORTED 1 AL03112AX UC45 PILOT REPORTED THAT INSIDE DOOR HANDLE ON AIRSTAIR DOOR WAS SHEARED. MAINTENANCE REPLACED HANDLE ASSY. 2L72 4T RTA24CE 20050201000502005020100050EA 2005 2 1 NAH2005F00000 220041123A853010532 CYLINDER PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA RT ENG NR 5 CRACKED E NAHAE ENGINE SHUTDOWN A FLAME/FIRE TXTAXI/GRND HDL 1 EA1720AN 964 274693 L2001248A WHILE PERFORMING AN ENGINE RUN-UP/MAG CHECK, NR 5 CYLINDER ON THE RT ENGINE CRACKED/DISLOCATED AT THE INTERFACE AREA OF THE STEEL BARREL TOP AND ALUMINUM HEAD. THE ENGINE WAS SHUT DOWN AND RESULTANT LOCALIZED FIRE WAS CONTAINED TO THE IMMEDIATE AREA BY THE USE OF THE FIRE EXTINGUISHER. THE CYLINDER PRESENTED NO OBVIOUS FLAWS AT THE MOST RECENT INSPECTION. A POST INCIDENT INSPECTION OF THE AREA FOUND ENGINE BAFFLING INTACT AND CORRECTLY POSITIONED. IT IS SUSPECTED THAT A DEFECT IN THE CYLINDER REPAIR PROCESS (IE: WELDING) ALLOWED AN ABNORMAL STRESS CONCENTRATION TO CAUSE A FAILURE. THE CYLINDER WAS SENT BACK TO THE ENGINE REBUILDER FOR ANALYSIS. (K) 1L72 3O3 O 1A10 1E4 20050201001192005020100119EU 2005 2 1 W9YA200400001 120041124A27429787314203 ACTUATOR PILATSPC12 PC1245 7090551EU HORIZONTAL STAB INOPERATIVE E W9YAO OTHER F FLT CONT AFFECTED CRCRUISE 1 CE09276CN1019 138 276 DURING A 14 CFR 91 REPOSITIONING FLIGHT, THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR FAILED IN THE MAIN AND STAND-BY MODES DURING CRUISE FLIGHT. THE PILOT REPORTED DIFFICULTY MAINTAINING LEVEL FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE DEFECTIVE ACTUATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1L71 3T RTA78EU 20050127002002005012700200NM 2005 1 27 AWXA200500060 120041228A532069353654 ANGLE BOEING737 7373Q8 1384670NM CABIN FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH CRACKS WERE FOUND IN CABIN FLOOR STIFFENER ANGLE BETWEEN BS 380 AND BS 400, AT BL 0. MAINTENANCE REMOVED CRACKED STIFFENER ANGLE FROM BS 380 TO BS 400, AT BL 0; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-35365; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 3 & 8. 2L72 4F RTA16WE 20050127002022005012700202EU 2005 1 27 AWXA200500062 120040112A5347D53371112000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 SAL - MAJOR REPAIR - DURING C-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT OUTBOARD SEAT TRACK BETWEEN FR 42 AND FR 44. MAINTENANCE REMOVED CORRODED SECTION OF LT OUTBOARD SEAT TRACK FROM FR 42 TO FR 44; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK; INSTALLED REPAIR PART IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20050128000042005012800004NM 2005 1 28 04FDEA03404 120041210A55106516880 WEB BOEING727 727100 1384036NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 CORROSION LT HORIZONTAL STAB FIXED L/E INTERNAL VERTICAL WEB L/E STA 29. *S/D* REPAIRED PER SRM 55-10-1 FIG 1, 51-30-2, 51-10-1, 55-10-4, 51-30-5. 2L73 4F RTA3WE 20050128000852005012800085NM 2005 1 28 AWXA200500068 120041228A53156545815108 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 344 BETWEEN LBL 15 AND RBL 10. MAINTENANCE REMOVED CORRODED UPPER CHORD AT BS 344 FROM LBL 15 TO RBL 40; FABRICATED A NEW REPLACEMENT UPPER CHORD AND 2 EACH ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-10-51, FIG 205. 2L72 4F RTA16WE 20050128000882005012800088NM 2005 1 28 AWXA200500070 120041228A5320654681282 WEB BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON LT AFT OUTBOARD SHEAR WEB, ADJACENT TO WATER LINE FITTING BETWEEN BS 996 AND BS 1005, LBL 39 AND LBL 42, WL 208. MAINTENANCE REMOVED DAMAGED AREA OF LT AFT OUTBOARD SHEAR WEB FROM BS 996 TO BS 1005, LBL 39 TO LBL 42; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-46812-82; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 FIG 3, 4, 6, 7, 8 & 12. 2L72 4F RTA16WE 20050128000892005012800089NM 2005 1 28 AWXA200500071 120041220A53106545871523 DOOR FRAME BOEING737 7373Q8 1384670NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND IN R-1 DOOR FRAME ON AFT SIDE AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK IN R-1 DOOR FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 328, STR 14 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND SHIM; INSTALLED REPAIR PARTS IAW ER 035200-05014-ES2. 2L72 4F RTA16WE 20050201001682005020100168EA 2005 2 1 SIMA200432701 120041117A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21523AE 10152 CREW REPORTS ON PRE-FLIGHT EMERGENCY LIGHTS WILL NOT TEST. FOUND EMERGENCY LIGHT SWITCH LEFT IN THE ON POSITION. REPLACED BATTERY PACK NR 1,2,3, AND 4, IAW CRJ700 MM 33-50-17. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. SN 1) 85317 2) 85318 3) 85593 4) 85640. (SW21200501047) 2L72 4F4 FRTA21EA EOOO63EN 20050202000082005020200008 2005 2 2 AALA20050043 420041230A3460 COMPUTER AIRBUS300 A300B4605R 3930308EU FLT CONTROL INOPERATIVE A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW2125071 514 EN ROUTE MIA-MEX, AFTER TAKEOFF RECEIVED AN ECAM CAUTION WITH A PITCH FEEL FAULT. PITCH FEEL WAS NOTICEABLE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FCC, DIODE 156VD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20050202000272005020200027WP 2005 2 2 DHL2004801539 120040923A57403645612U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT WING NR 4 ALT TANK BOOSTER PUMP BRACKET CRACKED (AFT) REF 505B ACCESS DOOR. REMOVED AND REPLACED CRACKED BRACKET ON RT WING NR 4 ALT TANK BOOSTER PUMP REF 505B ACCESS DOOR IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050202000292005020200029WP 2005 2 2 DHL2004801542 120040918A53204612650A FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 FWD ACCY COMPT END FITTING CORRODED AT STA 8.000, L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17,18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED END FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW END FITTING IAW SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050202000312005020200031EU 2005 2 2 DHL2004364015 120041029A3260 PROXIMITY SENSOR AIRBUS300 A300B4203 3930306EU LT MLG MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01364DH 141 FRONT PANEL LEFT MAIN LANDING GEAR RED UNSAFE MOMENTARILY ILLUMINATED ON APP TO CVG. 2ND OFFICER LEFT MAIN LANDING GEAR INDICATED GREEN AT ALL TIMES WITH LANDING GEAR EXTENDED. PERFORMED OPS CHECK OF PROXIMITY DETECTOR MODULE UNIT IAW M/M 32-61-12, OPS GOOD, NO DEFECTS NOTED. 2L72 4F RTA35EU 20050202000322005020200032 2005 2 2 GLBA20030701 420040823A341657024929412 ALTIMETER BEECH 1900 1900D 1154162CE COCKPIT FAILED A GLBAO OTHER P NO WARNING INDICATION CLCLIMB 1 NM03210GL6919 UE210 FO'S ALTIMETER SMOKED INSIDE OF GLASS AND CB POPPED. REMOVED AND REPLACED FO'S ALTIMETER PN 570-24929-412. 2L72 4T RTA24CE 20050202000352005020200035WP 2005 2 2 DHL2004801012 120041105A2612 FIRE LOOP DOUG DC8 DC873F 302199FWP NR 2 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01801DH 46033 ENG NR 2 FIRE LOOP B SHORT CIRCUIT LIGHT ILLUMINATED ON TAXI OUT. DEFERRED NR 2 ENG "B" FIRE LOOP PER MEL 26-2-3 CAT C DMI 18369 PLACARD INSTALLED. 2L74 4F RT4A25 20050202000362005020200036WP 2005 2 2 DHL2004806003 120041105A2560P0723E105P LIFE VEST DOUG DC8 DC873F 302199FWP CABIN MISSING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH 46002 FWD COURIER SEAT AT CABIN ENTRY AREA MISSING LIFE PRESERVER. INSTALLED SERVICEABLE VEST IN FWD COURIER IN SEAT IAW M/M 25-60-0 DATE CHECKED 6/4 RE-CHECK DUE 6/9. 2L74 4F RT4A25 20050202000432005020200043NE 2005 2 2 DJFA2004006 220040622A7261 O-RING BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE OIL FILTER CHIPPED E DJFAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA23427CW RK27 PCEJA0146 DURING FLIGHT, THE LEFT OIL PRESSURE ANNUNCIATORS WAS DROPPING. THE ENGINE WAS SHUT DOWN IN FLIGHT. THE CAUSE WAS FOUND THAT THE OIL FILTER WAS LEAKING THIS WAS CAUSED BY A CHIPPED O-RING ON THE OIL FILTER HOUSING. 2H72 4F4 FRTA16SW E25EA 20050202000442005020200044WP 2005 2 2 DHL2004801541 120040924A53404750422U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 UPPER CUSP EXTRUSION FITTING CRACKED 1.000, STA 857.000 L-19R. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050202000452005020200045WP 2005 2 2 NACA20040052 120041029A792131354 ACTUATOR DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE OILCOOLER DOOR INOPERATIVE A NACAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 AL039933098 98 31613 43576 31613 NR 1 ENGINE SHUT DOWN DUE TO HIGH AND UNCONTROLABLE OIL TEMPERATURE. REPLACED NR 1 ENGINE OIL COOLER DOOR ACTUATOR. OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20050202000472005020200047WP 2005 2 2 NACA20040057 120041106A3297 WIRE DOUG DC6 DC6A 3021706WP LT MLG SHORTED A NACALA ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION LDLANDING 1 AL036174C 44075 LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE, NO GEAR WARNING HORN. FOUND LEFT HAND MAIN LANDING GEAR DOWN AND LOCKED SWITCH WIRES SHORTING AGAINST NR 1 MAIN WHEEL. REPAIRED AND SECURED WIRES. OP CHECKED GOOD. 2L74 4R 6A3 20050202000632005020200063WP 2005 2 2 ABXA040387 120041201A5610 WINDOW DOUG DC9 DC933F 302207AWP COCKPIT STUCK A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. OPENED WINDOW AND APPLIED LUBRICANT TO WINDOW MECHANISM, WINDOW OPERATES NORMAL. 2L72 4F A6WE 20050202000672005020200067NM 2005 2 2 2004000008 120040627A2910 HYDRAULIC SYSTEM BOEING757 75728A 1384976NM LEFT LOW A CNMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07369AX 28161 LEFT HYDRAULIC SYSTEM QUANTITY LOW. SERVICED LEFT HYDRAULIC SYSTEM. 2L72 4F RTA2NM 20050202000742005020200074NM 2005 2 2 ANCF200400036 120041127A52805930583290 DOOR DOUG MD80 MD83 3023681NM MLG DAMAGED W ANCFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO23583AN 53183 AFTER TAKEOFF AND AFTER LANDING GEAR RETRACTION THE RED GEAR LIGHT REMAIN ON ALONG WITH THE GEAR DOOR OPEN LIGHT. CHECKIST WAS PERFORMED AND THE GEAR WAS CYCLED WITH NO HELP. RETURNED WAS MADE THE GEAR WHEN DONE OK, AND THE GEAR DOOR OPEN LIGHT WHEN OFF NORMALLY. RIGHT INBOARD DOOR WAS REPLACED IN ACCORDANCE WITH AMM 32-12-01 PAGES 201 TO 208 AND TEST WAS PERFORMED IN ACCORDANCE WITH AMM 32-31-04 PAGES 203 TO 207 P/N 5930583-290 S/N WITHOUT. 2L72 4F RT 20050202000812005020200081NM 2005 2 2 EIA2004040 120040604A3350S1356B37 LIGHT BOEING747 747121 1384871NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 EMERGENCY LIGHT AT STATION 2200 LS INOP. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL MM REF 33-51-07. 2L74 4F A20WE 20050202000832005020200083WP 2005 2 2 EIA2004042 120040611A3350 BATTERY DOUG DC9 DC915F 3022037WP EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09916F 47044 EMERGENCY LIGHTS IN COCKPIT EXTREMELY DIM WHEN TURNED ON. REPLACED COCKPIT EMERGENCY LIGHT BATTERY PER DC9 MM 33-53-0, OPS CHECKED GOOD. 2L72 4F A6WE 20050202000882005020200088WP 2005 2 2 31177050304 220040503A7314307085048 PUMP LEAR 35 31A 5170531CE ALIDSGTFE731TFE7313AR WP RT ENGINE FAILED E J7SAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SW05132FX3051 31177 P99480 DURING DESCENT FROM CRUISE, RIGHT ENGINE FLAMED OUT. ENGINE WAS SUCCESSFULLY RESTARTED. DIVERTED TO KBDL. REPLACED RIGHT ENGINE FUEL PUMP DUE TO LOW PRESSURE. REPLACED RIGHT ENGINE FUEL CONTROL DUE TO METAL CONTAMINATION IN STRAINER BETWEEN FUEL PUMP AND FUEL CONTROL. PERFORMED FUEL SAMPLING ANALYSIS BY HONEYWELL FOR CONTAMINATION, NO DEFECTS NOTED. ENGINE GROUND RUNS PERFORMED SATISFACTORY. 2L72 4F4 FRTA10CE E6WE 20050202001272005020200127CE 2005 2 2 GLBA20030704 120040826A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE DAMAGED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03118GL UE118 EO 03-17 REV 1 DUE FUSELAGE REPAIR ON ANT, REPAIRED PER EO 03-17. 2L72 4T RTA24CE 20050202001322005020200132WP 2005 2 2 200411008 120041115A2761 LINE DOUG DC9 DC987 3022087WP SPOILER ACTUATORLEAKING W ASMFK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SW23755RA 49727 AIRCRAFT ARRIVED WITH CAPTAIN REPORT THAT HYDRAULIC LEAK FROM OUTBOARD SPOILER SYSTEM IN RIGHT WING. BOTH LINES SPOILER IN RIGHT WING WERE REPLACED IAW MM 27-60-00, ALL CORRECT. 2L72 4F RTA6WE 20050202001332005020200133NE 2005 2 2 ERAA097087 120040820A7603 THROTTLE SKRSKYS61 S61N 8142104NE GE CT58 CT581402 30011NE EMERGENCY SYS CONTAMINATED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03562EH19355 61257 295043C WATER CONTAMINATED, EMERGENCY THROTTLE LOCKED UP. DUE L/O IN 96 HOURS. ECU SHAFT AND THROTTLE VALVE STIFF 6O ROTATE, FUEL PUMP DRIVE SHAFT VERY STIFF. INTERNAL CORROSION TO FUEL SYSTEM DUE 6O WATER CONTAMINATION. INHIBIT AND PRESERVE ENGINE FUEL SYSTEM IAW SEI-182 SECT 72-00 PG 303-309. ENGINE ASSY LIGHT OVERHAULED IAW SE--1-183 REV 21. 2G72 4U4 U 1H15 1E3 20050202001352005020200135WP 2005 2 2 04FDEA03232 120041126A5310 STRUCTURE DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT AFT CARGO AT STA 1801 STR 45 RT EXFOLIATION. REMOVED CORROSION PER SRM 51-21-01 PAGE 28. CHECK LIMIT PER SRM 53-00-01. REPLACED LONGERON 45 RT PER SRM 51-33-01, P/N AGA 3083-505. 2L73 4F A22WE 20050202001372005020200137WP 2005 2 2 04FDEA03239 120041128A5753 VANE DOUG DC10 DC1010 3022110WP ZONE 500 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 WINGS, LT INBD FLAP REWORK OF CHAFED AREA ON VANE TE EXTRUSION. CLOSING ACTION ON 11/26/04, ON N/R S00022. COMPLIED WITH EA 8-5710-55415. 2L73 4F A22WE 20050202001382005020200138NE 2005 2 2 HNAA0400125 220041011A7260 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE OIL ILLUMINATED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07846EX 326 FLIGHT NR 3842 REPORTED THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATING ON TAKEOFF CLIMB. THE NR 2 OIL OIL PRESSURE ALSO FLUCTUATED WITHIN THE SAFE ZONE AND STABILIZED WHEN POWER WAS REDUCED. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE FOR LEAKS, NONE FOUND. OIL WAS SERVICED WITH 2 QUARTS OIL, AND GROUND RUN FOR 10 MINUTES, NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050202001402005020200140WP 2005 2 2 04FDEA03206 120041125A5340AJC72481 FITTING DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AFT FUSELAGE VAST COMPT STA 1986-2007 3EA END FITTING LONGERON CORRODED. REPLACED END FITTING PER SRM 51-33-01 PAGE 34-47. 2L73 4F A22WE 20050202001422005020200142WP 2005 2 2 04FDEA03208 120041125A5311ABA7348U3 FRAME DOUG DC10 DC1010 3022110WP FUSELAGE CRACKED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND FWD ACC COMP AT STA 469 RT SIDE. FOUND 1 CRACK OF 5 INCHES ON FRAME AND 1 CRACK ON LWR FLANGE OF 0.90 INCHES. REPLACED FRAME PER SRM 51-33-01 PAGE 34-47 AND SRM 51-35-01 PAGE 1- 12. 2L73 4F A22WE 20050202001462005020200146EA 2005 2 2 HNAA0400098 120040929A215078279018 ACM DHAV DHC8 DHC8311 1386006EA CABIN COOLING FAILED A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA07331EN5881 163 279 AFTER TAKEOFF, CREW NOTED HOT BURNING SMELL IN ACFT, RET TO FIELD. INSPECTED AND GROUND RAN ACFT, NO BURNING SMELL OR DEFECT NOTED. INSPECTED FOR SECONDARY DAMAGE, NONE NOTED, SUSPECT ODOR FROM ACM PACK HOT CAUTION LIGHT AND NOISY ACM NOTED DURING TAXI IN ON PREVIOUS FLIGHT. ACM WAS MEL'D FOR THAT DISCREPANCY. 2H72 4T RTA13NM 20050202001502005020200150CE 2005 2 2 0041 120040622A2131E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE PRESS CONTROLLEROUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050202001522005020200152NM 2005 2 2 TSAA0479053 120040707A793039101201001 TRANSMITTER BOEING737 737230 1384401NM NR 2 ENGINE FAILED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13821AL 23155 ON TAKEOFF ROLL, THE NR 2 ENGINE OIL QUANTITY INDICATOR DROPPED TO ZERO. REJECTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE NR 2 ENGINE OIL QUANTITY INDICATOR IAW MEL 79-1, CONTROL NR 0778B-10. SERVICED THE NR 2 ENGINE TO FULL AND INSTALLED PLACARDS ON AIRCRAFT AND LOG-BOOK. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE OIL QUANTITY TRANSMITTER IAW AMM 79-31-11. OPS AND LEAK CHECK OK, PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050202001562005020200156CE 2005 2 2 45162081504 120040815A5246 SKIN LEAR 45 45LEAR 5170805CE DOOR FATIGUED E J7SAO OTHER O OTHER NRNOT REPORTED 1 SW05426FX 45162 AFTER LANDING, CREW FOUND RT SIDE FUEL SUMP SERVICE DOOR OPEN. MAINTENANCE FOUND LATCH HAD FATIGUED THE DOOR SKIN WHICH ALLOWED THE DOOR TO COME OPEN. DOOR ASSEMBLY WAS REPLACED. 2L72 4F RTT00008WI 20050202001572005020200157NE 2005 2 2 ZWOA0400401 220040629A72613938314501 LINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE NR 1 ENGINE OIL CRACKED A TWAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE13957U 49702 1449 THE NR 1 ENGINE WAS SHUT DOWN IN FLIGHT DUE TO LOW ENGINE OIL PRESSURE AND QUANTITY GOING TO ZERO. REPLACED THE OIL LINE TO THE DIFFERENTIAL PRESSURE SWITCH. CHECK-C 10-25-2003 STL. 2L72 4F4 F A6WE E9NE 20050203000452005020300045SO 2005 2 3 SWIA200414446 120041101A5340 BRACKET EMB 120 EMB120ER 3260203SO CENTER WING BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 WING CENTER SECTION RIGHT SIDE LOWER FUSELAGE BRACKET IS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BRACKET IAW SRM 51-40-02 & 51-22-00. 2L72 4T RTA31SO 20050203000492005020300049WP 2005 2 3 DHL2004873507 120041103A53404641324U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000-1700.000, L-28L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203000512005020300051WP 2005 2 3 DHL2004873509 120041103A53404641324U501 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000 - 1700.000, L-32R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED AFT SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203000542005020300054WP 2005 2 3 DHL2004873534 120041129A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LEFT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 98.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM LEFT VERTICAL STABILIZER, L/E STA ZFS 98.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 1. REMOVED CORRODED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL7075-T6 0.050) IAW SRM 55-5-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW SKIN IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050128000842005012800084NM 2005 1 28 AWXA200500067 120041221A53306545774105 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-17 CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727D, STR 21 LT. MAINTENANCE CUT OUT DAMAGED AREA OF FUELAGE SKIN AT BS 727D, STR 21 LT; FABRICATED A DOUBLER AND TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-01, FIG 229. 2L72 4F RTA16WE 20050202000182005020200018NM 2005 2 2 AALA20050058 120041216A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 FLOORBEAM AT RIGHT BUTTLINE 49 AT STATION 325 HAS CORROSION 1.0 INCH BY 1.0 INCH WITH DEPTH OF .069. MATERIAL REMAINING IS BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 AND ONE HALF HARD STAINLESS STEEL 0.050 THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTNERS TO BE INSTALLED WITH 4 6D SPACING. 2L72 4F RTA1NM 20050202000222005020200022CE 2005 2 2 0039 120040622A2134E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE CABIN PRESSURE OUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. THEY SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FT. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050202000232005020200023NM 2005 2 2 200417 120040727A2150782790XX ACM DHAV DHC8 DHC8103 1386005NM CABIN COOLING FROZEN A KPVAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 WP13808WP 118 026 SMOKE SMELL IN COCKPIT AND ROW 1. COULD NOT DETERMINE SOURCE. COMPLIED WITH A WALK AROUND INSPECTION AND HAVE DETERMINED THIS AIRCRAFT TO BE IN A SAFE CONDITION FOR A FERRY FLIGHT FROM JHM-HNL ONLY. SOURCE DETERMINED TO BE FROM ACM. ACM FOUND FROZEN. REMOVED AND REPLACED ACM IAW DHC MM 21-50-11 PG 206-210. LEAK AND OPS CHECK GOOD. 2H72 4T RTA13NM 20050202000242005020200024WP 2005 2 2 DHL2004801502 120040901A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT WING CTR L/E UPPER FORMER CRACKED 0.500, STA. XFS 435.789. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW DC8 SRM 57-2-0 PG 10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050202000262005020200026WP 2005 2 2 DHL2004801538 120040923A7830 DOUBLER DOUG DC8 DC873F 302199FWP THRUST REVERSER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 NR 4 ENGINE LT SIDE T/R INTERNAL STRUCTURE DOUBLER CRACKED 10.000 AT 3 O'CLOCK POSITION, STA 202.000. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (AL2024-T3 0.050) IAW MM 78-30-00 PG 836 FIG 812. CLEANED, TREATED AND PRIMED IAW MM 78-30-0 PG 834. INSTALLED DOUBLER IAW MM 78-30-00 PG 833/837 FIG 812. 2L74 4F RT4A25 20050202000342005020200034NM 2005 2 2 ASMF200412002 120041207A2780 WARNING LIGHT DOUG MD88 MD88 3023688NM SLAT FAIL ILLUMINATED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23158PL 49761 AIRCRAFT PERFORMED A REJECTED TAKEOFF AT 110 KNOTS AS A CONSEQUENCE OF "AUTO SLAT FAIL" LIGHT TURNED ON. BITE AND RESEAT WERE PERFORMED TO STALL WARNING COMPUTERS IAW MM 34-19-00, AUTO SLATS SYSTEM WAS CHECKED IAW MM 27-80-00 AND INSPECTION BY REJECTED TAKEOFF WAS PERFORMED IAW MM 05-56-00, ALL CORRECT. 2L72 4F RTA6WE 20050202000522005020200052WP 2005 2 2 LATA02010501 220040715A7200 ENGINE CESSNA441 441 2076020CE GARRTTTPE331TPE33110 01514WP RIGHT POWER LOSS E LATAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL05441SA3575 4410172 77493 UPON DEPARTURE AT APPROX 1000 FEET AGL, WHILE STILL IN THE TRAFFIC PATTERN, THE RIGHT SIDE ENGINE TORQUE ROLLED BACK TO LESS THAN 200LBS. THE PILOT ELECTED NOT TO TROUBLESHOOT THE LOSS OF TORQUE AND SECURED THE ENGINE AND RETURNED TO THE AIRPORT. SUBSEQUENT INSPECTION OF THE ENGINE AND FUEL SYSTEM REVEALED NO PROBLEMS. THE AIRCRAFT WAS THEN GROUND RUN FOR FIFTEEN MINUTES AT TAKEOFF AND CLIMB POWER WITH NO ANOMALIES NOTED. THE AIRCRAFT WAS THEN FLOWN TO BASE WITH NO INFLIGHT DISCREPANCIES. PROBABLE CAUSE OF POWER REDUCTION IS THE ELECTRONIC ENGINE CONTROL SYSTEM. TO HELP REDUCE RECURRENCES, A ROUTINE CLEANING OF ELECTRICAL CONNECTIONS BETWEEN THE EEC, FCU AND RELATED COMPONENTS DURING PHASE INSPECTIONS. 1L72 3T4 TRTA28CE E4WE 20050202000642005020200064CE 2005 2 2 66839 120041117A5220 DOOR BEECH 1900 1900D 1154162CE EMERGENCY EXIT OPEN A AMWAO OTHER O OTHER NRNOT REPORTED 1 CE07190YV UE190 PAX PULLED EMERGENCY EXIT 4F. MAINTENANCE REINSTALLED AND AIRCRAFT RETURNED TO SERVICE. INSTALLED RT FWD EMERG HATCH EXIT. 2L72 4T RTA24CE 20050202000902005020200090WP 2005 2 2 04FDEA03190 120041123A3150 WARNING LIGHT DOUG MD10 MD1010F 3022112WP WINDSHEAR ILLUMINATED A FDEAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25385FE 46619 ON DEPARTURE OUT OF ONT AT APPROX 1000 AGL, GOT A TAIL WINDSHEAR ALERT. WENT TO FIREWALL. NO OVERSPEED. DUMPED FUEL. DIVERTED TO LAX. NO ENGINE EXCEEDANCE'S REPORT ON ACARS NOR AIU'S. PERFORMED POSSIBLE TAIL STRIKE INSPECTION AND FLIGHT CONTROL INSPECTION. PULLED FIGHT RECORDER AND VOICE RECORDER PER FLIGHT SAFTEY. PERFORMED INSPECTION 05-51-12-6 PART 2 A CK AND HARD LANDING SECTION A AND B WITH NO DEFECTS NOTED. FLIGHT CONTROL CK PER MM 27-00-0-2, ALL CK PASSED AS REQUIRED. REMOVED AND REPLACED FLIGHT DATA RECORDER PER FLIGHT SAFETY. SYSTEM OPS CHECK GOOD IAW MD10 MM 31-31-01-2. RETURNED TO SERVICE. 2L73 4F RTA22WE 20050202000922005020200092WP 2005 2 2 P9RA20040020 120040715A335060030451 CHARGER DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO1114816 49370 IN INSPECTION, VARIOUS EMERGENCY EXIT LIGHTS OUT OVERHEAD. REMOVED AND REPLACED 3 BATTERY CHARGERS SERIAL NUMBERS 5227 15955 21872 AND AND 4 EMERGENCY BATTERIES PART NUMBER 5014. 2L72 4F A6WE 20050202000952005020200095NM 2005 2 2 ANCF200400035 120041122A32604062575 TRANSDUCER DOUG MD80 MD83 3023681NM MLG MALFUNCTIONED W ANCFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO23632CT 49632 TWO REJECTED TAKEOFF WAS PERFORMED DUE WHEEL NOT TURNING COMES ON APPROX 90 KNOTS. REPLACED TRANSDUCER IN MLG RT POSITION NR 3 AND NR 4 IAW AMM:32-43-02 PAG 201 PN OFF:4062575, S/N:OFF:627, S/N ON:5325A POS NR 3. 2L72 4F RT 20050202000972005020200097NM 2005 2 2 0704026 120040727A2611 SMOKE DETECTOR BOEING737 737242 1384477NM LAVATORY MALFUNCTIONED A MJYAO OTHER N FALSE WARNING LDLANDING 1 SW07742TW 21186 FORWARD LAVATORY SMOKE DETECTOR WENT OFF ON LANDING NO SIGN OF SMOKE OR FIRE IN FORWARD LAVATORY. 2L72 4F A16WE 20050202001012005020200101NE 2005 2 2 GTIA040801 220041006A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217A 52053NE NR 2 SHUTDOWN A GTIAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23810NK 48015 708145 INFLIGHT SHUTDOWN, EMERGENCY AIR RETURN. RT OIL TEMP HIGH IN CLIMB, SHUTDOWN ENGINE AT 165 DEGREES. REMOVED AND REPLACED NR 2 ENGINE IAW MM. LEAK CHECK OK. 2L72 4F4 F A6WE E9NE 20050202001032005020200103WP 2005 2 2 P9RA20040028 120040808A3830835880403 WASTE TANK DOUG DC9 DC983 3022083WP FUSELAGE OVERSERVICED A P9RAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11960PG 49904 FLT NUMBER 315, SLC-AMA, AT APPROXIMATELY 15,000 FEET, 280 KTS, SMOKE WAS REPORTED IN AFT CABIN BY AFT FLIGHT ATTENDANT STATION. SOURCE AND TYPE UNKNOWN AT THAT TIME. EMERGENCY DECLARED. RETURNED TO SLC. AIRCRAFT INSPECTED AND DETERMINED SAFE TO TAXI TO GATE. ALL OTHER ASPECTS OF FLIGHT WERE ROUTINE, 161 PAX ON BOARD. SLC, MAINTENANCE REPORT. INSPECTED AFT CABIN AREA AND FOUND LAVATORIES OVERSERVICED AND LEAKING FLUID. DRAINED ALL LAVATORIES AND AIRCRAFT FERRIED TO DFW FOR FURTHER MAINTENANCE. DFW MAINTENANCE ENTRY, CLEANED TOWELS FROM ALL LAVATORY TANKS, CLEANED BOX FROM LEFT AFT LAV DUMP VALVE. FILLED LAVS WITH SANI CLEAN. DUMPED AND RESERVICED. GROUND PRESSURIZED THE AIRCRAFT AND INS 2L72 4F RTA6WE 20050202001052005020200105SW 2005 2 2 PNSA041002 120041016A2133 OUTFLOW VALVE SWRNGNSA227 SA227AC 8780603SW CABIN PRESSURE MALFUNCTIONED A PNSAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 AL032719H 713 CREW WAS STARTING CRUISE WHEN THEY LOST PRESSURIZATION, DECLARED EMERGENCY AND DID EMERGENCY DESCENT FROM 17000FT TO 10000FT FLIGHT WAS ENROUTE FROM ANI TO ANC, FLIGHT CONTINUED TO ANC WITHOUT ANY DIFFICULTY. MX FOUND THAT MASS FLOW VALVE BAD, PART WAS REPLACED AND PRESSURIZATION CHECK WAS NORMAL. 2L72 4T RTA8SW 20050202001092005020200109EA 2005 2 2 DJFA2004036 120041124A56106003303025 WINDSHIELD CNDAIRCL600 CL6002B16 1900305EA LEFT BURNED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23699CW2945 5009 CREW REPORTED WHILE AT CRUISE FL370 APPROXIMATELY 35 MINUTES AFTER TAKEOFF, NOTED AN ELECTRICAL HOT/BURNING ODOR. OXYGEN MASKS WERE DONNED AND AIRCRAFT DIVERTED TO KSFB. MAINTENANCE FOUND THE INSULATION MELTED AND NR 2 POWER LUG SHORTED ON THE LEFT WINDSHIELD. ALSO, FOUND WAS A DEFECTIVE POWER SUPPLY FOR THE OVERHEAD LIGHTING. LEFT WINDSHIELD AND POWER SUPPLY PART NUMBER 449-2 WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20050202001182005020200118WP 2005 2 2 DHL2004805012 120041201A5250AR25291GRY1 LATCH DOUG DC8 DC873F 302199FWP COCKPIT DOOR BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH 46125 COCKPIT DOOR LATCH BROKEN DOOR WILL NOT LATCH CLOSED. REMOVED AND REPLACED LATCH ASSY WITH SERVICEABLE LATCH ASSY. OPS CHECKS GOOD PER 52-51-1 P/N AR2529-1GRY1. 2L74 4F RT4A25 20050202001222005020200122CE 2005 2 2 100704 120041007A2435300SGL138Q43 STARTER GEN CESSNA560 560XL 2076702CE PWA 545 PW545A NE LT ENGINE MELTED E W9FAO OTHER M OVER TEMP TXTAXI/GRND HDL 1 EA073 564 5605341 DB069 ENGINE WOULDN'T START. BRUSHS HOUSING ON STARTER GENERATOR MELTED. 2L72 4F4 FRTA22CE E00059EN 20050202001252005020200125CE 2005 2 2 452004090204 120040902A261274412135 FIRE LOOP LEAR 45 45LEAR 5170805CE RT ENGINE DEFECTIVE E J7SAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05605FX495 452004 RT ENGINE "FIRE" AURAL WARNING AND ENGINE FIRE CAS/CWP MSG DURING CLIMB-OUT. WARNING INDICATIONS EXTINGUISHED WHEN POWER PULLED BACK AND DID NOT RETURN. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. ITT RANGE WAS NORMAL. MX REPLACED TAIL PIPE FIRE LOOP. OPS CHECK NORMAL. 2L72 4F RTT00008WI 20050202001262005020200126WP 2005 2 2 45111080804 220040808A729730707227 MONOPOLE LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP LT ENGINE FAILED E J7SAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW05414FX 4511 P116213 LEFT ENGINE COMPUTER CAS MSG LIGHT ILLUMINATED, ENGINE TRIP TO MANUAL MODE. AIRCRAFT DIVERTED TO GRR. MAINTENANCE REPLACED N2 MONOPOLE. NO FURTHER DEFECTS NOTED. 2L72 4F3 TRTT00008WIAEXJ STC 20050202001282005020200128SW 2005 2 2 ERAA098188 120041026A3246412050015110R SKID BELL 412 412 1182202SW MLG CRACKED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH3395 FLOAT/SKID ASSY HAS CRACKED SADDLE. AFT SADDLE ON SKID TUBE CRACKED IAW RING HAS DAMAGED THREADS. REMOVED ALL FLOAT/COVER ASSEMBLIES, HOSES, PASSENGER STEP, SKID SHOES AND HARDWARE FROM UNSERVICEABLE SKID TUBE AND RE-INSTALLED EVERYTHING (SAME AS REMOVED) ONTO 1 EA SERVICEABLE SKID TUBE. INSTALLED NEW TOW RING 1 EA PN 204-050-104-001. ALL WORK DONE IAW BHT 412 MM 5 AND BHT 412-SI-2. 1G72 4U H4SW 20050202001302005020200130EU 2005 2 2 ERAA098189 120040730A642010531714 ROTOR HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR CRACKED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03149EH11080 S705 TAIL ROTOR CRACKED INNER SLEEVE BUSHING. TEFLON BUSHINGS WORN, INNER SLEEVE STEEL BUSHINGS WORN, GASKETS ROTTEN, 2 SLEEVES CORRODED, 1 RING CORRODED. COMPLETELY DISASSEMBLED FOR INSPECTION. REPLACED UNSERVICEABLE PARTS. C/W 1200 HR AND 2400 HR INSPECTIONS ON T/R HUB. C/W 300 HR AND 2400 HR BLADE INSPECTIONS. REASSEMBLED WITH NEW NUTS WASHERS, TORQUED AND SAFTIED AS REQUIRED. REINSTALLED 2 SERVICEABLE BLADES AND STATIC BALANCED. INSPECTED AND REPAIRED IAW BO105 REM 301, MM 33,34,101 AND 107 TT 11,0749.4 TSI -0-. 1G72 3U H3EU 20050203000712005020300071WP 2005 2 3 DHL2004873529 120041116A5512 SKIN DOUG DC8 DC873F 302199FWP HORIZONTAL STAB ELONGATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RT HORIZONTAL STABILIZER L/E ELONGATED HOLES IN UPPER SKIN (STA XFS 60.000-116.250) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3475. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CUT OUT DAMAGED SKIN SEGMENT IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3475. FABRICATED REPAIR DOUBLER (AL7075-T6 0.050) IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG ED-3745. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED EXTERNAL REPAIR DOUBLER AND NEW FASTENERS IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3745, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050203000722005020300072WP 2005 2 3 DHL2004873526 120041201A53215892159 FLOOR PANEL DOUG DC8 DC873F 302199FWP FUSELAGE DEFORMED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FLOOR PANEL NR 1D SKIN DEFORMED AND CRACKED 40.000 (STA 879.000-1000.000). REMOVED DEFORMED AND CRACKED FLOOR PANEL NR 1D (STA 879.000-1000.000) IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SRM 51-1-8B. INSTALLED NEW FLOOR PANEL IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050203000732005020300073WP 2005 2 3 DHL2004873527 120041130A5321 FLOOR PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT NR 3C FLOOR PANEL SKIN CORRODED AND CRACKED 1.000 (STA 1560.000-1580.000). REMOVED CORROSION FROM NR 3C FLOOR PANEL SKIN (STA 1560.000-1580.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLER (7075-T6 0.080) IAW SRM 53-2-3 PG 39-40. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 PG 39-40, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050203000782005020300078WP 2005 2 3 DHL2004873511 120041111A57403645611U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 NR 1 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2L74 4F RT4A25 20050203000892005020300089SO 2005 2 3 SWIA200414448 120041101A5341 BRACKET EMB 120 EMB120ER 3260203SO WING TO BODY CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 WING CENTER SECTION LEFT SIDE LOWER FUSELAGE BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. BRACKET REPLACED IAW EMB SRM 51-25-00, 51-30-01, 51-40-02. 2L72 4T RTA31SO 20050203000912005020300091SO 2005 2 3 SWIA200414449 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 RIGHT INBOARD SEAT TRACK FROM FR34-FR38 TO BE REMOVED FOR ACCESS TO BUTT STRAP. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. SEAT TRACK INSTALLED AS PER AMM 53-01-05. 2L72 4T RTA31SO 20050203000922005020300092SO 2005 2 3 SWIA200414450 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 RIGHT INBOARD SEAT TRACK FROM FR15-FR32 TO BE REMOVED FOR ACCESS TO BUTT STRAP, AND ASSESS FOR CORROSION. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. SEAT TRACK INSTALLED IAW AMM 53-01-05. 2L72 4T RTA31SO 20050203000952005020300095SO 2005 2 3 SWIA200414453 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LITE CORROSION AROUND SCREW LEADS ON OUTBOARD SEAT TRACK RIGHT SIDE FROM FRAME 14 TO FRAME 25. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. RIGHT OUTBOARD SEAT TRACK INSTALLED IAW AMM 53-01-05. 2L72 4T RTA31SO 20050203001002005020300100WP 2005 2 3 DHL2004809508 120041228A5320577327557 CHANNEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 MAIN CARGO COMPT CHANNEL CRACKED 1.000 STA 680.000 RBL 24. REMOVED CRACKED CHANNEL IAW SRM 51-1-20D PG 1. FABRICATED NEW CHANNEL (AL7075-0-0.100) IAW DWG 5773275. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW CHANNEL IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW CHANNEL IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050616000022005061600002CE 2005 6 16 ENHA0502 120041022A242010300BR ALTERNATOR CESSNA207 207A 2073604CE ENGINE FAILED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL03207DF 349 20700728 LOW VOLTAGE LIGHT ON. NO AMP OUTPUT. 1H71 3O A16CE 20050616000042005061600004CE 2005 6 16 ENHA0503 120041031A242010300JR ALTERNATOR CESSNA172 172L 2072432CE ENGINE DAMAGED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL034265Q 223 17260165 COOLING FINS LOOSE. 1H71 3O NT3A12 20050616000062005061600006SO 2005 6 16 ENHA0504 120041101A2420ALU8521RS ALTERNATOR PIPER PA31 PA31350 7103110SO ENGINE DAMAGED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL03417PM 281 318052051 ALTERNATOR HAS WEAK OUTPUT. 1L72 3O A20SO 20050616000082005061600008CE 2005 6 16 ENHA0505 120041227A2420DOFF10300JR ALTERNATOR CESSNA172 172L 2072432CE ENGINE DAMAGED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL034265Q 230 17260165 AMMETER SHOWS DISCHARGE, ALT INOP. 1H71 3O NT3A12 20050623001362005062300136NM 2005 6 23 72300195 120041012A5320 FLANGE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 INCH CRACK IN UPPER FLANGE. 2L73 4F4 FRTA3WE E2EA 20050623001372005062300137NM 2005 6 23 72300196 120041020A5340 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION OF FITTING. 2L73 4F4 FRTA3WE E2EA 20050623001382005062300138NM 2005 6 23 72300197 120041020A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 5 INCH AREA OF CORROSION ON SKIN. 2L73 4F4 FRTA3WE E2EA 20050623001392005062300139NM 2005 6 23 72300198 120041118A5320 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 1 INCH AREA OF CORROSION ON FITTING. 2L73 4F4 FRTA3WE E2EA 20050623001412005062300141NM 2005 6 23 72300200 120041122A5320 STIFFENER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAEG CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 2 X 3 INCH AREA OF CORROSION ON STIFFENER. 2L73 4F4 FRTA3WE E2EA 20050201000462005020100046NE 2005 2 1 ALG2005F00006 120041214A32307665009801107 MODULE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MLG INOPERATIVE E ALGAO OTHER J WARNING INDICATION CLCLIMB 1 SW03522AL18383388 760236 AFTER TAKE OFF, GEAR DID NOT RAISE NORMALLY- RED LIGHT ON 3 GREENS OFF. VISUAL CONFIRMATION 3 GEAR HANGING DOWN. RECYCLED SEVERAL TIMES DECREASED AIRSPEED AT 20 KNOTS GEAR FINALLY RETRACTED, ALL LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED HYDRAULIC MODULE IAW MM. 1G72 3U3 U H1NE E1GL 20050201000632005020100063CE 2005 2 1 HYTA2M5004 120041223A321326430161 STRUT CESSNA208 208B 2073701CE NLG DEBONDED E HYTAK NONE O OTHER ININSP/MAINT 1 AL0132WA 11946 208B0234 TUBE OF NOSE GEAR STRUT TUBE ASSY PN 26430161, CAME LOOSE FROM UPPER END CAP ALLOWING TUBE TO FLOAT WITH NOSE GEAR STRUT MOVEMENT. VENT TUBE INSIDE STRUT TUBE WAS CRUSHED AND SHOVED TO UPPER END OF TUBE. EXAMINATION OF TUBE AND END CAP REVEALED THAT END CAP WAS ONLY ABOUT 60 PERCENT BONDED TO TUBE. NEW ASSEMBLY FROM MFG HAS GAPS IN BONDING AGENT AND IS LESS THAN 100 PERCENT BONDED. (AL01200501892) 1H71 3T A37CE 20050201001312005020100131WP 2005 2 1 ASMF200411003 120041104A32443910097543 TIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NLG DAMAGED W ASMFA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW23838AM5849 49397 AIRCRAFT PERFORMED AN AIR TURNBACK, STRONG NOISE AND VIBRATION ON NOSE LANDING GEAR. DURING MAINTENANCE REVISION, FOUND THE WATER DEFLECTOR BROKEN, THE TIRES DAMAGED, A HYDRAULIC LEAK ON STEERING BYPASS VALVE, BOTH NOSE LIGHTS BROKEN, DENTS ON LOWER FUSELAGE AND A CRACK ON METALLIC SEAL OF SLAT ZERO IN LT WING. TIRES 1 AND 2, WATER DEFLECTOR, STEERING BYPASS VALVE FITTING AND NOSE LIGHTS WERE REPLACED IAW MM 32-40-02, 32-20-01, 20-12-02 AND 33-41-01, RESPECTIVELY, TEST CORRECT. DENTS AN CRACK WERE WITHIN LIMITS. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM 05-51-04, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050201001582005020100158SO 2005 2 1 SIMA200430804 120041030A361014536587401 TUBE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL BLEED TUBE SEPARATED A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21621AE 145105 AFTER TAKEOFF, CREW REPORTED LOUD BANG FOLLOWED BY A BLEED 1 LEAK MESSAGE, CREW FOLLOWED AOM PROCEDURE AND MESSAGE DID NOT EXTINGUISH FOLLOWED AOM FOR A PRECAUTIONARY ENGINE SHUTDOWN. FA REPORTED VIBRATION IN THE CABIN NOT FELT BY THE CREW. INSPECTED AND FOUND BLEED TUBE ASSY JOINT BLOWN OPEN AND SEPARATED REMOVED AND REPLACED BLEED TUBE IAW AMM. OPS CHECK AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050201001692005020100169WP 2005 2 1 ASMF200411002 120041104A29107936907665 LINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE HYDRAULIC SYS CRACKED W ASMFA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW23751RA 49779 AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, HYDRAULIC LEAK ON RT SYSTEM. DURING MAINTENANCE REVISION, HYDRAULIC LEAK WAS DETECTED ON REAR CARGO COMPARTMENT AND HYDRAULIC FLEXIBLE LINE WAS INSTALLED TO THE RUDDER CONTROL SHUTOFF VALVE IAW MM 20-12-04, TEST CORRECT. DURING OVERNIGHT SERVICE, HYDRAULIC FLEXIBLE LINE WAS REPLACED AND SYSTEM WAS TESTED IAW MM 27-20-09, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050201001742005020100174WP 2005 2 1 ASMF200411005 120041109A7410103538754 IGNITION UNIT DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23214AM15598 49585 725948 DURING ENGINES STARTING, LT ENGINE DID NOT START. CIRCUIT BREAKER WAS CHECKED AND EDP TEST WAS PERFORMED IAW MM 72-21-01, ALL CORRECT. LT ENGINE START WAS PERFORMED AND FAIL CONTINUE, EGT AND RPM INDICATIONS WERE NOT SHOWN. IGNITION BOX AND EXCITER PLUG CABLE WERE REPLACED IAW MM 74-10-01 AND 74-20-01, RESPECTIVELY, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20050202000302005020200030NM 2005 2 2 HNAA040008 120040929A531385320056107 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDESPREAD NATURE OF DAMAGE, DECISION MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO FS PAR FR.(387) FOR CONVENIENCE IN LIEU OF REPEATED BLENDING AND MEASURING WITH SAME POTENTIAL RESULTS(SPLICE). THIS EO ACCOMPLISHES R/R`D BY PERFOMING SPLICES PER RD8-53-2499. THIS REPAIR IS A MAJOR REPAIR. 2H72 4T RTA13NM 20050202000332005020200033NE 2005 2 2 301041 220041026A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT SHUTDOWN A NSVAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA27239CJ 340B239 785311 AT 8000, RT IGNITION LIGHT ILLUMINATED THE THE ITT SPIKED, THEN THERE WAS A LOUD BANG THE RT ENGINE SHUT DOWN. 2L72 4T4 TRTA52EU E8NE 20050202000372005020200037EU 2005 2 2 XNOA1203 120041020A2710 ACTUATOR AIRBUS300 A300B4203 3930306EU AILERONS FAILED A XN0AA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL23370PC 134 LOW SPEED AIL FAILED TO DISCONNECT AT FLAPS RET/OVERWEIGHT LANDING BELOW 360' PM. REMOVED AND REPLACED LOW SPEED AILERON LOCKOUT ACTUATOR I/A/W A300 AMM 27-11-48, OPS CK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION I/A/W A300 AMM 5-51-11, NO DEFECTS NOTED. 2L72 4F RTA35EU 20050202000382005020200038NM 2005 2 2 TSAA0475073 120040929A7500 LINE BOEING737 7372X6C 1384552NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE LOOSE A TSAAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP13817AL 23292 P702685 NR 1 ENGINE WILL NOT REACH TAKEOFF POWER; REPORTED BY CREW. MAINTENANCE TROUBLE SHOOTING FOUND THE AFT PT7 LINE LOOSE. SECURED THE LINE; RAN ENGINE TO POWER. ALL PARAMETERS, OPS AND LEAK CHECK GOOD. SYSTEM CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20050202000392005020200039NE 2005 2 2 XNOA1195 220040810A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 2 MALFUNCTIONED A XN0AC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23793A 20774 NR 2 ENG EPR DIDN'T REACH T/O THRUST INDICATIONS. ALL OTHER INDICATIONS NORMAL. TRANSFERRED TO DMI NR 4469 IAW MEL77-1. PLACARDS INSTALLED. 2L73 4F4 F A3WE E2EA 20050202000402005020200040NM 2005 2 2 C8GA20040007 120040617A275065413321 TOGGLE BOEING727 727223 1384074NM TE FLAPS BENT A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15708AA 22465 AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO KBOS. NO EMERGENCY ACTION WAS TAKEN AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND CLEANED THE OUTBOARD FLAP POSITION INDICATOR CONNECTOR. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 27-51-11 AND THE AIRCRAFT RETURNED TO SERVICE. FLT 723 DEPARTED AGAIN FROM KBOS TO ROC. AFTER TAKEOFF, THE OUTBOARD FLAP INDICATED ASYMMETRY AND THE AIRCRAFT RETURNED TO KBOS AND LANDED WITHOUT INCIDENT. THE OUTBOARD FLAP POSITION INDICATOR WAS REPLACED AND ALL SYSTEM CHECKED GOOD IAW MM 27-51-11. 2L73 4F A3WE 20050202000412005020200041NE 2005 2 2 ASMF200411004 220041105A7250815431 BLADE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE RT ENGINE NICKED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23803AM 26268 727138 DURING OVERNIGHT SERVICE, BOROSCOPE INSPECTION WAS PERFORMED ON RIGHT ENGINE AND NICKS WERE DETECTED ON ONE BLADE OF 11TH STAGE, OUT OF LIMITS IAW MM 72-00-00. RIGHT ENGINE WAS REPLACED IAW MM 71-00-00, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20050202000482005020200048NM 2005 2 2 TSAA0449051 120040701A49302118966222 ECU BOEING737 73776N 13844CHNM CARGO BAY FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13743AL 28654 AFTER T/O, APU FAULT LIGHT CAUSED APU AUTO SHUTDOWN. LANDING GW 142.3 K, SINK RATE AT TOUCHDOWN LESS THAN 300 FPM. DIVERTED TO HNL, UNEVENTFUL LANDING. PERFORMED APU BITE CHECK, ECU INTERNAL FAULT SHOWN. REPLACED APU ELECTRONIC CONTROL UNIT PER AMM 49-61-12-00-801. STARTED APU AND PERFORMED APU BITE TEST, OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35-2, PAGES 1-13. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050202000492005020200049NM 2005 2 2 HNAA0400092 120040929A531385530150103 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHK, FOUND CORROSION UNDER CABIN FLOOR. THIS EO8-53-04-0655 PERFORMD REPLACEMENT OR STR 31 STARBOARD FR X424 TO SECTION END AT X531 FOR CONVENIENCE OF CORROSION REPAIRS. NOTE THAT THE REPLACEMENT SECTION OF STR31 IS CUT AS ALLOWED BY RD. 2H72 4T RTA13NM 20050202000502005020200050CE 2005 2 2 GLBA20030710 120040831A5210 SKIN BEECH 1900 1900D 1154162CE PAX DOOR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03201GL UE201 PAX DOOR HAS CORROSION AROUND DOOR HANDLE, REPAIRED PER EO 04-14. 2L72 4T RTA24CE 20050202000512005020200051NE 2005 2 2 197041 220040714A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A11 52043NE NR 2 SHUTDOWN A NSVAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 EA27191CJ UE19 32347 NR 2 ENGINE FAILED IN CLIMB, ENGINE SHUT DOWN EMERGENCY DECLARED AND RETURNED TO BLOCK (REASON FOR FAILURE STILL TO BE DETERMINED). 2L72 4T3 TRTA24CE E4EA 20050202000622005020200062WP 2005 2 2 ABXA040386 120041124A5310 STRUCTURE DOUG DC8 DC841 3021914WP VIBRATION A ABXAO OTHER E VIBRATION/BUFFET DEDESCENT 1 GL23971AX 47497 IN DESCENT THROUGH APPROX 16,000 FEET AND AROUND 300 KTS, THERE WAS A NOTICABLE AIRFRAME VIBRATION THAT LASTED UNTIL WE SLOWED THROUGH ABOUT 270 KTS. ENGINE/POWER CHANGES HAD NOT NOTICABLE EFFECT ON THE VIBRATION. NO INDICATION OF ANY ENGINES PROBLEMS WERE NOTED. SEE LINE MAINTENANCE WORK ORDER NR 600213176 AND NR 2004971 FOR WORK ACCOMPLISHED. A FUNCTIONALY CHECK FLIGHT WAS PERFORMED WITH NO VIBRATION NOTED. 2L74 4J 4A25 20050202000682005020200068WP 2005 2 2 2004000009 120040805A2612 FIRE WARNING DOUG DC10 DC1030 3023501WP NR 1 ENGINE ACTIVATED A CNMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07810AX 48265 ON CLIMB-OUT, ENGINE FIRE INDICATION NR 1 ENGINE, AIR TURN BACK. 2L73 4F A22WE 20050202001022005020200102WP 2005 2 2 GTIA040798 120041002A2410947F9453 GCU DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT GENERATOR MALFUNCTIONED A GTIAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL23826NK 49391 AIR RETURN , RT GEN TRIPPED OFF ON ROTATION. RAN AC CROSSTIE LOCKOUT CHECKLIST RESET. RT GEN TRANSFERRED DFGS TO AP NR 1. TURNED A/T AND A/P ON. RT GEN TRIPPED OFF AGAIN WITHIN 30 SECONDS. APU PICKED UP RT SIDE LOAD. 2L72 4F4 FRTA6WE E9NE 20050202001042005020200104NM 2005 2 2 P9RA20040031 120040808A335020121 POWER SUPPLY BOEING757 757236 1384971NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11958PG 24118 AIRCRAFT IN MAINTENANCE, FORWARD FIRST CLASS PROXIMITY LIGHTS AND DOOR 1R EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED M730 POWER SUPPLY AND BATTERY PER MM 335107. BATTERY PART NUMBER IS AD2013A AND SERIAL NUMBER OFF IS 46863. 2L72 4F RTA2NM 20050202001062005020200106 2005 2 2 IXXA0400106O9 420040921A2210 YAW DAMPER DOUG DC8 DC862 3021970WP AUTOFLIGHT MALFUNCTIONED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11799AL74833 45922335 AFTER TAKEOFF FROM WSAP, YAW DAMPER ENGAGED, RUDDER KICKED TO THE LEFT. DISENGAGED YAW DAMPER. CREW TRIED TO RE-ENGAGE YAW DAMPER AND RUDDER KICKED LEFT AGAIN, TURNED OFF YAW DAMPER. CREW RETURNED AIRCRAFT TO WSAP AND LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ONGOING. AS SOON AS INFORMATION IS AVAILABLE IT WILL BE PROVIDED. 2L74 4F 4A25 20050201000212005020100021EA 2005 2 1 2004F00438 120041221A5320612826 TRACK DHAV DHC2 DHC2* 2800108EA PWA R985 R985* 52008NE ADC MOUNT CRACKED B HJBRK NONE E VIBRATION/BUFFET ININSP/MAINT 1 AL0537756700 1456 DURING A SCHEDULED INSPECTION, FOUND THE AIR DATA COMPUTER (ADC) BROKE LOOSE FROM ITS MOUNT. UPON FURTHER INVESTIGATION FOUND THE MOUNTING BRACKET FLANGE CRACKED COMPLETELY OFF THE AIRFRAME STRUCTURE IT WAS RIVETED TO. AFTER REMOVAL OF THE BRACKET, AND FURTHER INSPECTION, IT IS BELIEVED THAT THE FLANGE WAS NOT MANUFACTURED WITH THE PROPER RADIUSES IN THE CUTOUT FOR THE THUMBNAIL SCREW CAUSING IT TO CRACK. VIBRATION FROM GENERAL AIRCRAFT OPERATION CONTRIBUTED TO THE ISSUE. THIS ADC WAS INSTALLED AS PART OF THE STC NR SA02203AK EFIS-SV SYSTEM IN APRIL OF 2004. 1H71 3R3 R A806 5E1 20050201000342005020100034EU 2005 2 1 KBM2005F00006 120041120A6420355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19966SH 3787 TAIL ROTOR HALF SHELLS, BEARINGS WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050201000492005020100049 2005 2 1 ANCF200400038 420041218A2312G631704 RADIO BOEING757 757236 1384971NM RROYCERB211 RB211* 54555NE VHF COMM INOPERATIVE W ANCFB EMER. DESCENT O OTHER CRCRUISE 1 SO23506NA 24771 RECEPTION ON L VHF COMM INOPERATIVE, TRANSMISSION O.K. AND R VHF INOPERATIVE AND DEFERRED. AFTER LANDING 2 VHF COMM BECOME NORMAL. IAW WDM 23-12-02 AND 23-12-02 VHF COMM CONTROL PANEL WIRING WAS CHECKED AND OPERATIONAL TEST WAS PERFORMED IAW AMM 23-12-00 PAGE BLOCK 501. TEST SATISFACTORY. 2L72 4F4 FRTA2NM A12EU 20050201000922005020100092CE 2005 2 1 2004F00439 120041221A323311538000254 MOTOR BEECH 100 B100 1152919CE GARRTTTPE331TPE3315 01514WP MLG DAMAGED E DRUAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2588FA 78 BE74 DURING TAKEOFF, LANDING GEAR FAILED TO RETRACT, THEN FAILED TO EXTEND, WAS MANUALLY EXTENDED VIA EMERGENCY PROCEDURES. MAINTENANCE DISCOVERED LANDING GEAR MOTOR CIRCUIT BREAKER TRIPPED, MOTOR ITSELF SUFFERED INTERNAL HEAT DAMAGE. TIME IN SERVICE SINCE OVERHAUL, 78 HOURS. 1L72 4T4 T A14CE E4WE 20050201001202005020100120NM 2005 2 1 HALA0401045 120041101A2997 RELAY BOEING767 76733A 1385209NM PWA 4060 PW4060 52119NE HYD SYSTEM BURNED W HALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO23587HA 33421 APPROX HALF WAY THROUGH FLIGHT, ELECTRICAL BURNING SMELL APPEARED IN COCKPIT. AS A PRECAUTION TURNED C-1 HYD PUMP. SMELLED DISAPATED. FOUND RELAY M303 LEAKING EXTERNALLY. TIME DELAY FOR CI PUMP. NO STOCK HNL, AOC FOR CCN-2903041. 348 TO MOC. RM5273. REPLACED ECCR IAE AMM 29-11-14. OPS CHECK OK NO BURNING SMELL NOTED. REMOVED AND REPLACED RELAY M303. OPS CHECK OK IAW FIM 29-11-00-1. 2L72 4F4 FRTA1NM E24NE 20050202000172005020200017NM 2005 2 2 AALA20050057 120041206A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21384AA 26996 AFW - FLOORBEAM SECTION 41 AT STATION 347 HAS CORROSION. MATERIAL REMAINING IS BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 AND ONE HALF HARD STAINLESS STEEL 0.050 THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS WITH 2 COATS BMS10 11 PRIMER. FILL BLENDS WITH BMS 5 95 SEALANT. INSTALL REPAIR STRAP WET WITH BMS 5 95 SEALANT. FASTNERS TO BE INSTALLED WITH 4 6D SPACING. 2L72 4F RTA1NM 20050202000282005020200028WP 2005 2 2 DHL2004801540 120040923A5730 ACCESS DOOR DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT WING ACCESS DOOR NR 583F HOLES ELONGATED. REMOVED ACCESS DOOR NR 583F IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW ACCESS DOOR (7075T6 0.080) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED INNER SIDE OF ACCESS DOOR IAW DC8 SRM 51-1-8B. INSTALLED NEW ACCESS DOOR IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050202000652005020200065EU 2005 2 2 DHL2004363500 120040922A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 3767 MAIN CABIN INTERIOR FLOOR SEAT TRACK FLANGES HAS SPOTS OF CORROSION BETWEEN FS 44 AND FS 45 AND RBL 15. REMOVED SURFACE CORROSION SPOTS FROM SEAT TRACK FLANGES AT MAIN CARGO CABIN BETWEEN FS 44 AND FS 45 RBL 15 IAW A-300 SRM 51-40-11. FOUND SPLICE AREA OUT OF LIMITS IAW A-300 SRM 53-10-00. REMOVED SEAT TRACK FROM FRAME 40 AND FS 44 RBL 15 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK AS PER EXAMPLE IAW A-300 SRM 51-10-40. TREATED, ALODINED, AND PRIMED AND PAINTED IAW A-300 SRM 51-40-10. INSTALLED NEW SEAT TRACK FROM FS 40 TO FS 45 AT RBL 15 IAW. 2L72 4F RTA35EU 20050202000662005020200066EA 2005 2 2 COMA0460659 120041203A5210 SEAL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR BROKEN A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01436CA 7482 FLT 5135 - HIGH SQUEAL FROM CABIN DOOR, A/C WOULD NOT PRESSURIZE. FORWARD AND AFT DOOR SEAL NIBS BROKEN, REPAIRED IAW SRM. 2L72 4F RTA21EA 20050202000692005020200069EU 2005 2 2 222042 120040809A3350 BULB SAAB SF340 340B 7860101EU EMERGENCY LIGHT LOOSE A NSVAO OTHER O OTHER NRNOT REPORTED 1 EA27239CJ 340B239 F/A EMERGENCY LIGHT INOP, RE-SEAT BULBS, OP CHECKED GOOD. 2L72 4T RTA52EU 20050202000732005020200073NM 2005 2 2 P9RA20040051 120041127A335020121 CHARGER BOEING757 757231 1384950NM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11720TW 30319 LEFT AFT AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER IAW MM. 2L72 4F RTA2NM 20050202000782005020200078NM 2005 2 2 EIA2004037 120040522A3350 LIGHT BOEING747 747132 1384882NM EMERGENCY EXIT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 EMERGENCY EXIT LIGHT IN CEILING ABOVE STAIRS INOP. FOUND PIN 2 PUSHED BACK. INSTALLED PUSH BACK PIN AT PIN 2 EMERGENCY LIGHT IN CEILING PANEL ABOVE STAIRS, OPS CHECKED NORMAL PER MM 33-51-00 PAGE 501. 2L74 4F A20WE 20050202000792005020200079NM 2005 2 2 EIA2004038 120040522A3350 LAMP BOEING747 747132 1384882NM EMERGENCY LIGHT BURNED OUT A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 R5 EMERGENCY EXIT LIGHT SIGN LIGHTS FORWARD AND AFT INOP. RELAMPED R5 EMERGENCY EXIT LIGHT ASSEMBLY. R5 EMERGENCY LIGHT OPS CHECK NORMAL PER MM 33-51-00 PAGE 501. 2L74 4F A20WE 20050202000802005020200080NM 2005 2 2 EIA2004039 120040522A3350 LAMP BOEING747 747132 1384882NM EMERGENCY LIGHT BURNED OUT A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 L5 EMERGENCY EXIT LIGHT SIGN LIGHT FWD AND AFT INOP. RELAMPED L5 EMERGENCY EXIT LIGHT ASSEMBLY. EMERGENCY LIGHT OPS CHECKED NORMAL PER MM 33-57-00 PAGE 501. 2L74 4F A20WE 20050202000822005020200082NM 2005 2 2 EIA2004041 120040604A3350S12356B37 LIGHT BOEING747 747121 1384871NM CABIN INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09480EV 20348 EMERGENCY LIGHT IN CEILING, AFT LEFT SIDE COMES ON AND GOES OUT. REPLACED EMERGENCY LIGHT ASSY. OPS CHECK NORMAL REF MM 33-51-07. 2L74 4F A20WE 20050202000842005020200084NM 2005 2 2 EIA2004043 120040623A3350 CHARGER BOEING747 747132 1384882NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 CREW DOOR SLIDE LIGHT COMES ON FOR TWO SECONDS THEN GOES OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER PER MM 33-51-04. ALSO, REMOVED AND REPLACED BATTERY CARTRIDGE PER MM 33-51-50 PG 201, OPS CHECKED NORMAL PER MM 34-51-00 PG 501. 2L74 4F A20WE 20050202000852005020200085NE 2005 2 2 200412 220040625A7200 ENGINE DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE NR 1 FOD A KPVAO OTHER C F.O.D. NRNOT REPORTED 1 WP13805WP162857747 353 PCE120692 NR 1 ENGINE PCE 120692, LP IMPELLER FOD DAMAGED BEYOND LIMITS (ENGINE CHANGE). REMOVED AND REPLACED NR 1 ENGINE WITH PCE 120107 IAW FORM AIAM-105. PERFORMANCE ENGINE RUN UP IAW DHC 8 PSM 1-8-2, 71-00-00 MM PG 529-544 SEC 3 TABLE 505. 2H72 4T4 TRTA13NM E20NE 20050202000862005020200086NM 2005 2 2 P9RA20040025 120040731A3350MS1557081 BULB BOEING727 7272J0 138407ENM EMERGENCY LIGHT INOPERATIVE A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11906PG 20728 AIRCRAFT IN MAINTENANCE, R2 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED R2 DOOR EXTERIOR LIGHT IAW MM 335001. 2L73 4F RTA3WE 20050202000872005020200087CE 2005 2 2 31201052404 120040524A21302618466006 VALVE LEAR 35 31A 5170531CE CABIN PRESSURE INOPERATIVE E J7SAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 SW05137FX 201 AIRCRAFT WENT TO EMERGENCY PRESSURIZATION DURING CLIMB-OUT, WOULD NOT PRESSURIZE AT 8000 FT. PERFORMED UNSCHEDULED LANDING. MX REPLACED RT 3-WAY VALVE, BOTH MOD VALVES AND MOD CONTROL BOX. CABIN PRESSURIZING ON GROUND, APPROX 2000 FPM WHEN ADVANCED THROTTLES. WOULD RETURN TO NORMAL WHEN RETRACTED. CREW TURNED OFF BLEED SWITCHES WITH NO EFFECT. MAINTENANCE REPLACED RT 3 WAY VALVE, RT MODULATING VALVE AND RT VALVE CONTROL BOX. OPS CHECKS NORMAL. 2L72 4F RTA10CE 20050202000892005020200089GL 2005 2 2 04FDEA03189 220041123A7532 BLEED VALVE DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL ENGINE INOPERATIVE A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25372FE 46610 ON TAKEOFF AT1000' AGL GOT LEVEL 3"AIR MANF 1 FAIL. COMPLIED WITH QRH, RETURNED TO AN UNEVENTFUL LANDING. PERFORMED DECAY CHECK FOR PNEUMATIC SYS 1 PER MM. CHECKED NORMAL. WHILE T/S FOUND AIU 3 INTERNAL FAULT FAILED TEST. REMOVED AND REPLACED AIU. NO FAULT LIGHTS ON MANIFOLD FAULT INDICATOR. R/R`D MANIFOLD RELAY R2-8962. R/R`D MANIFOLD FAILURE DETECTION PRESSURE SWITCH PER MM 36-23-03-4. R/R`D MANIFOLD FAILURE DETECT CONTROLLER. HIGH PRESSURE VALVE ON NR 1 ENG NEVER MOVES STAYS IN THE CLOSED POSITION THROUGHOUT ENGINE RUN. INSTALLED SERVICABLE HIGH PRESSURE BLEED VALVE. RAN NR 1 ENGINE I/A/W JRH. HP VALVE OPERATED NORMALLY. PERFORMED HIGH POWER RUN WITH WING ANTI-ICE SELECTED. 2L73 4F4 FRTA22WE E23EA 20050202000912005020200091EU 2005 2 2 04FDEA03192 120041118A3260 UPLOCK AIRBUS310 A310 EU MLG FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25408FE 257 AFTER TAKEOFF, NOSE GEAR AMBER "DOOR" WARNING LIGHTS (FWD AND OVERHEAD) REMAINED ON FOLLOWING GEAR RETRACTION. NO EXCESSIVE NOISE OR VIBRATION OBSERVED. WHEN GEAR WAS EXTENDED AGAIN, "DOOR" LIGHT REMAINED ON (BOTH FORWARD AND OVERHEAD INDICATIONS) RETURNED TO IND. REMOVED AND REPLACED RT NLG DOOR UPLOCK ASSY IAW A310-200 MM 32-31-14, SYS OPS OK, A/C OK 4 FLT RII:377762. PREMATURE REMOVAL/INSTALLATION OFF MFG A25431001POS RT SRL M579, ON MFG A25431001-2, SRL U1606 TAG 609521. 2L72 4F RTA35EU 20050202000982005020200098WP 2005 2 2 GTIA040812 120041010A2612 FIRE LOOP DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE NR 2 ENGINE MALFUNCTIONED A GTIAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL23810NK 48015 NR 2 ENGINE (B) LOOP FLICKERS ON T/O AND DURING FLT. NR 2 ENGINE CHANGED WITH LOOP ON IT. NOTE: ENGINE CHANGE ACCOMPLISHED ON 10/10/04, OCCURRENCE DATE CHANGED TO REFLECT CLOSURE OF REPORT. 2L72 4F4 F A6WE E9NE 20050202001192005020200119NM 2005 2 2 P5CA0501303 120041227A323365B0155212 ACTUATOR BOEING747 747249F 1384849NM MLG FAILED A P5CAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 EA15920FT 22237 WHEN GEAR WAS EXTENDED A LOUD NOISE WAS HEARD AND HAD LOSS OF NR 1 HYDRAULIC SYSTEM. LANDING WAS NORMAL. FOUND EXTEND/RETRACT ACTUATOR FAILED. REPLACED EXTERNAL/RETRACT ACTUATOR PER MM 32-33-01. 2L74 4F A20WE 20050202001292005020200129CE 2005 2 2 45135081104 120040811A27406627401000007 ACTUATOR LEAR 45 45LEAR 5170805CE PITCH TRIM FAILED E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05422FX3200 45135 PRIMARY PITCH TRIM FAIL CAS MSG AFTER TAKEOFF, DURING NOSE DOWN TRIM ACTUATION. MAINTENANCE REPLACED PITCH TRIM ACTUATOR AND PILOT TRIM BARRELL SWITCH. FUNCTION CHECK GOOD, NO FURTHER DEFECTS NOTED. 2L72 4F RTT00008WI 20050202001342005020200134WP 2005 2 2 04FDEA03235 120041126A3610831651 PRESSURE SWITCH DOUG DC10 DC1010 3022110WP ANTI ICE SYSTEM FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO25373FE 46611 NR 3 MANIFOLD FAIL LIGHT ILLUMINATED SHORTLY AFTER TURNING ON WING ANTI ICE. RAN RED TABS; FAULT LIGHT WENT OUT IMMEDIATELY. AFTER TURNING OFF NR 3 ENG PNEU SUPPLY SELECTOR. CHECK RT WING ANTI-ICE DUCTING FOR LEAKS NO LEAKS NOTED. CHECKED MANIFOLD FAIL DETECTOR CONTROLLER FOR FAULTS. FOUND FAULT BALL FOR RT WING PRESSURE SWITCH. REPLACED PRESSURE SWITCH IAW AMM 36-23-03-4. RAN ENGINE AGAIN WITH WING ANTI-ICE. NO LEAKS NOTED AND FAULT DID NOT RETURN. OPS CHECK GOOD. 2L73 4F A22WE 20050202001362005020200136WP 2005 2 2 04FDEA03238 120041128A5753ARC2761 BRACKET DOUG DC10 DC1010F 3022111WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 WINGS, RT INBD FLAP REWORK OF TRACK/DRIVER BRACKET P/N ARC2761. CLOSING ACTION ON 11/27/04 ON N/R S00018. COMPLIED WITH EA 8-5754-55412. 2L73 4F A22WE 20050202001392005020200139NM 2005 2 2 04FDEA03205 120041125A7932ST104Z TRANSMITTER BOEING727 727227 1384078NM OIL PRESSURE FAILED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25478FE 21395 DURING CLIMB THROUGH 17,000 FT, NOTICED NR 1 ENG OIL PRESS AT 27 PSI. SHUT ENG DOWN IAW RED TABS LANDED IN MEM. ENT BY: 206208 RPT BY: 111069, SWAPED NR 1 AND NR 2 OIL PRES IND, RAN NR 1 ENG OIL PRES IND STUCK AT 27PSI, LOP LIGHT WAS OUT ALL OTHER IND WERE NORMAL, POSSIBLE OIL PRESS TRANSMITTER. REMOVED AND REPLACED PRESSURE TX REF PER MM 79-33-001-4. OPS CK AND LEAK CK NORMAL REF PER 79-32-000-5. RAN ENG PER JRH CH 5, ALL IND NORMAL. 2L73 4F A3WE 20050202001412005020200141WP 2005 2 2 04FDEA03207 120041125A1430 FASTENER DOUG DC10 DC1010 3022110WP FUSELAGE WRONG PART A FDEAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SO25559FE 46930 DURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT INSP HEAD MARKINGS OF FASTENERS ON THE VERTICAL TAIL IS INSTALLED FASTENER P/N HL221-8. REMOVE EXISTING FASTNERS AND REPAIR BY SB 55-023 GROUP 1. 2L73 4F A22WE 20050202001442005020200144WP 2005 2 2 0411001 120041111A7711 SENSE LINE DOUG DC9 DC915F 3022037WP ENGINE LOOSE A MJYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07785TW 47015 DURING CLIMB ABOVE 20,000 FT, THE NR 2 ENGINE DID NOT INDICATE CLIMB THRUST (EPR). 2L72 4F A6WE 20050202001452005020200145NM 2005 2 2 0411002 120041118A2420 CSD BOEING737 737230C 1384472NM NR 1 ENGINE OVERTEMP A MJYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07737TW 20257 DURING CLIMB, THE NR 1 CSD HIGH OIL TEMP LIGHT ILLUMINATED. 2L72 4F A16WE 20050202001472005020200147CE 2005 2 2 GLAB20030698 120040802A2400 RECEPTACLE BEECH 1900 1900D 1154162CE MLG WW DAMAGED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03184UX UE184 RT NACELLE POWER CABLE OPENING AT WHEEL WELL IS DAMAGED, REPAIRED. 2L72 4T RTA24CE 20050202001482005020200148CE 2005 2 2 0033 120040622A2131E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE PRESS CONTROLLERDEFECTIVE E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FT + OR - 250 FT. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050202001492005020200149CE 2005 2 2 0040 120040622A2131E45C49 PRESSURE SWITCH LEAR 35 35A 5170602CE PRESS CONTROLLEROUT OF LIMITS E CIEAK NONE O OTHER ININSP/MAINT 1 NM03222BE 35A0489 DURING A 2400 HOUR INSPECTION, THE ABSOLUTE PRESSURE WARNING SWITCH FOR THE PRESS CONTROLLER WAS FOUND TO BE DEFECTIVE. A REPLACEMENT UNIT WAS PURCHASED FROM THE AIRFRAME MANUFACTURER AND WAS ALSO FOUND TO BE OUT OF TOLERANCE. A TOTAL OF 9 UNITS WERE PURCHASED AND ALL WERE FOUND TO BE OUT OF TOLERANCE. THE AIRFRAME MANUFACTURER WAS CONTACTED TO ASSIST IN RESOLUTION OF THIS ISSUE. SENT SEVERAL UNITS TO THEIR LAB AND WERE ABLE TO SHIP US A TOTAL OF TWO UNITS WITHIN ALLOWED LIMITS. THESE UNITS ARE TO CLOSE THE SWITCH DURING CLIMB AT 8,750 FEET + OR - 250 FEET. THE SWITCH IS TO REOPEN PRIOR TO 7,200 FEET DURING THE DESCENT. SUSPECT THERE ARE SEVERAL UNITS REPLACED AFTER JANUARY 1, 2001. 2L72 4F A10CE 20050202001512005020200151WP 2005 2 2 2004000011 120040929A2120AAM7101509 DUCT DOUG DC10 DC1030 3023501WP CABIN AIR RUPTURED A CNMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07630AX 46596 THICK SMOKE IN AFT LAV'S ALONG WITH A HOT FLOOR. AFTER PACKS 2 AND 3 TURNED OFF SMOKE SEEMED TO DISSIPATE. REMOVED AND REPLACED RUPTURED DUCT IN CENTER CARGO PIT LEFT SIDE. 2L73 4F A22WE 20050202001532005020200153GL 2005 2 2 ERAA097088 220040514A7320252464430N FUEL CONTROL BELL 412 412 1182202SW ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03423EH6302 ON START WOULD ACELERATE TO 62 TO 65 THEN ADVANCING THROTTLE WOULD STILL BLEED OFF. OVERHAULED IAW HONEYWELL OHM FORM 15-6026. 1G72 4U3 U H4SW E4CE 20050202001552005020200155EU 2005 2 2 ERAA097091 120040719A32306864027600 CIRCUIT BOARD SNIAS AS332 AS332L 8680809EU MLG MALFUNCTIONED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03170EH LANDING GEAR CONTROL HAS NO CONTROL POWER, SHOWING MANUAL EXTENSION LIGHT ACTION TAKEN: UNIT INSPECTED, CAPACITOR C68 UNSERVICEABLE, HEAT DAMAGE EVIDENT ON PCB. TEMPORARY CAPACITOR FITTED IN PLACE OF C68 TO ENABLE TESTING OF UNIT. UNIT TESTED, RELAY K7 AND INTEGRATED CIRCUIT MN22 RENEWED, DRY JOINT LOCATED ON TRACK SIDE OF RESISTOR R119, DRY JOINT REMOVED AND R119 CLEANED AND RESOLDERED. HEAT DAMAGE AND FLUX CLEANED FROM BOARD AS BEST AS POSSIBLE. CAPACITOR C68 RENEWED. UNIT TESTED, SEVERAL TIMES, AFTER BEING SUBJECTED TO HEAT SOAK AND COLD SOAK. UNIT PASSED TEST SATISFACTORILY. 2G72 4U H4EU 20050203000462005020300046SO 2005 2 3 SWIA200414447 120041101A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 CORROSION FOUND OUT OF ALLOWABLE LIMITS ON CO-PILOT OUTBOARD BUTT STRAP (UNDER SEAT TRACK). ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-25-00, 51-22-00 & 51-40-02. 2L72 4T RTA31SO 20050203000502005020300050WP 2005 2 3 DHL2004873508 120041106A53403750257U503 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 1.000, STA 1050.000 L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203000522005020300052WP 2005 2 3 DHL2004873506 120041110A5542 DOUBLER DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RUDDER ACCESS DOOR NR 61A DOUBLER CRACKED 0.500. REMOVED CRACKED DOUBLER IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (AL2024-T3 0.032) IAW DC8 SRM 55-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED NEW DOUBLER IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050203000532005020300053WP 2005 2 3 DHL2004873525 120041201A53215892159 FLOOR PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FLOOR PANEL NR 1E SKIN DEFORMED AND CRACKED 20.000 (STA 688.000-729.000). REMOVED CRACKED AND DEFORMED FLOOR PANEL NR 1E (STA 688.000-729.000) IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SRM 51-1-8B. INSTALLED NEW FLOOR PANEL IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050203000662005020300066WP 2005 2 3 DHL2004873514 120041108A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RUDDER LT SIDE SKIN CORRODED BETWEEN ZR 253.000 AND ZR 271.000 NEXT FRONT SPAR (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE NR 1-RROU7 FAA FORM 8110-3 DATED 10-26-04. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED RUDDER LT SKIN (CORRODED) IAW BOEING MESSAGE NR 1-RROU7, SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL2024-Y3 0.032) IAW BOEING MESSAGE NR 1-RROU7. CLEANED TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW BOEING MESSAGE NR 1-RROU7, SRM 51-1-21 PG 1. PERFORMED X-RAY INSPECTION FOR CRACK AT INTERVALS TO EXCEED 24 MONTHS. 2L74 4F RT4A25 20050203000672005020300067WP 2005 2 3 DHL2004873510 120041103A53404641324501N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT AFT SPLICE FITTING CRACKED 0.500 (STA 1690.000 - 1700.000, L-28R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED AFT SPLICE FITTING IAW DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203000702005020300070WP 2005 2 3 DHL2004873512 120041113A57403645611U BRACKET DOUG DC8 DC873F 302199FWP NR 4 ALT TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 NR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2L74 4F RT4A25 20050203000752005020300075WP 2005 2 3 DHL2004873528 120041130A5280 ANGLE DOUG DC8 DC873F 302199FWP MLG DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RIGHT WING T/E MLG DOOR JAMB ZEE ANGLE CRACKED 2.000, STA XW 3.125. REMOVED CRACKED ZEE ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ZEE ANGLE (AL2024 -0- 0.050) IAW DWG 5651221. HEAT TREATED IAW DADO DPS 7.00. CLEANED, TREATED AND PRIMED AREA AND ZEE ANGLE IAW SRM 51-1-8B. INSTALLED NEW ZEE ANGLE IAW DWG 5651221, SRM 5-1-21. 2L74 4F RT4A25 20050203000932005020300093SO 2005 2 3 SWIA200414451 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LEFT INBOARD SEAT TRACK FROM FR16A-FR32 TO BE REMOVED FOR ACCESS TO BUTT STRAP AND ASSESS CORROSION ON SEAT TRACK. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. SEAT TRACK INSTALLED IAW MM 53-01-05. 2L72 4T RTA31SO 20050203000942005020300094SO 2005 2 3 SWIA200414452 120041101A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0757734 120199 LEFT INBOARD SEAT TRACK FROM FR32-39 TO BE REMOVED FOR ACCESS TO BUTT STRAP AND ASSESS FOR CORROSION. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. INSTALLED SEAT TRACK FROM FR32-39 IAW AMM 53-01-05. 2L72 4T RTA31SO 20050203001122005020300112EA 2005 2 3 SWIA200414464 120041210A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07698BR 7799 ANGLE 621 AT CARGO FLOOR LEVEL, RIGHT SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117. 2L72 4F RTA21EA 20050203001242005020300124WP 2005 2 3 DHL2004809509 120041227A5320577327557 CHANNEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 MAIN CARGO COMPT CHANNEL CRACKED 1.000 STA 680.000 RBL 46. REMOVED CRACKED CHANNEL IAW SRM 51-1-20D PG 21. FABRICATED NEW CHANNEL (AL7075-0-0.100) IAW DWG 5773275. HEAT TREATED IAW DACO DPS 7.00. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW CHANNEL IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW CHANNEL IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203001262005020300126WP 2005 2 3 DHL2004809506 120041227A5753 STRUCTURE DOUG DC8 DC873F 302199FWP TE FLAPS WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 RIGHT WING OUTBOARD FLAP UPPER AFT PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED WORN PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL2024T3 0.063) IAW SRM 57-7-1 FIG 4 TR 57-94. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING WITH NEW FASTENERS IAW SRM 51-1-21. 2L74 4F RT4A25 20050203001312005020300131WP 2005 2 3 DHL2004873531 120041110A5320 STIFFENER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT STIFFENER CORRODED AT FS 980.000, L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1, TR 51-130, SRM 53-4-1 FIG 51 PG 183-184. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED CHANNEL REPAIR (7075-T6 51 0.125) IAW SRM 51-2-1 FIG 1 SHEET 1, 2 DWG ED SEMAN 37-65. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED CHANNEL REPAIR ON STIFFENER IAW SRM 51-2-1 FIG 1 SHEET 1, 2, 12, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050203001342005020300134WP 2005 2 3 DHL2004873561 120041126A531597540241 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT FLOORBEAM CRACKED 0.500, STA 1160.000 L-26R TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FLOORBEAM IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FLOORBEAM IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203001362005020300136WP 2005 2 3 DHL2004873562 120041130A53205640916501 STIFFENER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT STIFFENER CORRODED, STA 980.000 L-27L. REMOVED CORROSION FROM STIFFENER STA 980.000 L-27L IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED STIFFENER IAW SRM 53-1-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED STIFFENER (AL7075T651) IAW DWG 5640916. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000102005020800010NM 2005 2 8 CALA0500033 120041106A7603 THROTTLE CABLE BOEING737 737524 1384721NM ENGINES STIFF A CALAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 SW2714605 27318 THE THROTTLES WOULD NOT REDUCE TO CLIMB POWER IN VNAV CAPTAIN SIDE THROTTLES WERE VERY STIFF. TROUBLESHOOTING FOUND BOTH NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES AT FAULT. THE NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES WERE REMOVED AND REPLACED IAW MM 76-11-07, PAGE 408. BOTH PUSH-PULL CABLES WERE ADJUSTED IAW MM 76-11-01. 2L72 4F RTA16WE 20050208000112005020800011NM 2005 2 8 CALA0500034 120041126A7603 THROTTLE CABLE BOEING737 737524 1384721NM NR 1 ENGINE JAMMED A CALAE ENGINE SHUTDOWN F FLT CONT AFFECTED CRCRUISE 1 SW2716607 27320 THE NR 1 THROTTLE JAMMED AND DID NOT RETARD (STUCK AT 83 PERCENT N1) ON INITIAL LEVEL OFF. THE NR 1 ENGINE WAS SHUTDOWN FOLLOWING QRH. THROTTLES SPLIT. TRIED TURNING OFF AUTOTHROTTLE TO NO AVAIL. THE NR 1 THRUST CONTROL PUSH-PULL CABLE WAS REMOVED AND REPLACED IAW MM 76-11-00, PAGE 501. OPERATIONAL CHECKS WERE GOOD. THE ENGINE WAS RUN TO 86 PERCENT N1 WITH NO DISCREPANCIES NOTED. 2L72 4F RTA16WE 20050208000392005020800039WP 2005 2 8 DHL2004873517 120041106A53405640915177 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FITTING ATTACHING BEAM TO PRESSURE BULKHEAD CRACKED 0.500, STA 980.000 BL 0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1-2, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG 1-2, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000402005020800040WP 2005 2 8 DHL2004873557 120041203A53113755820 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME HAS 3 MISDRILLED HOLES STA 1300.000, L-10R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12/02/04, DWG W90-R18 REV IR DATED 11/22/04. REMOVED 2 FITTINGS IAW DWG W90-R18, SRM 51-1-21 PG 1, SRM 51-1-20C. CUT OUT MISDRILLED HOLES AREA IAW DW W90-R18. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T60.090) FILLER (AL7075T6 0.080) AND 2 FRAME FITTINGS (AL7075T651) IAW DWG W90-R18, DWG 3755820 (FITTING). NDT INSPECTED NEW FITTINGS IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND EXTERNAL REPAIR DOUBLER, FILLER AND FITTINGS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DWG W90-R18, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000422005020800042WP 2005 2 8 DHL2004873518 120041117A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT UPPER FLOORBEAM FLANGE CORRODED, STA 1300.000 RBL 8 TO RBL 16 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1G, TR 53-124. REMOVED CORROSION FROM UPPER FLOORBEAM FLANGE AT STA 1300.000 RBL 8 TO RBL 16 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 1F NOTE 7. APPLIED PRC SEALANT TO BLENDOUT AREA IAW SRM 53-2-0 FIG 1G PAR C. FABRICATED REPAIR ANGLE (EXTRUSION 7075-T6 0.100) AND STEEL STRAP (301 1/4H 0.020) IAW SRM 53-2-0 FIG 1G, SRM 53-7-3 FIG 10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REPAIR ANGLE AND STEEL STRAP IAW SRM 53-2-0 FIG 1G, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000442005020800044WP 2005 2 8 DHL2004873533 120041128A5313S2641455 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT ACCY COMPT L-34R INTERNAL PART CORRODED AT FS 1660.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 43A. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED LONGERON IAW SRM 51-1-20D PG 21. FABRICATED NEW LONGERON (EXTRUSION S264155-12000). CLEANED, TREATED AND PRIMED AREA AND NEW EXTRUSION IAW SRM 51-1-8B. INSTALLED NEW LONGERON IAW SRM 51-1-20D PG 9, SRM 51-1-11 PG 1. 2L74 4F RT4A25 20050208000632005020800063WP 2005 2 8 DHL2004873550 120041203A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME HAS 3EA MISDRILLED HOLES AT STA 1400.000 L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R17, REV IR DATED 11-22-04, FAA FORM 8110-3 DATED 12-02-04. CUT OUT MISDRILLED HOLE AREA IAW DWG W90-R17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED REPAIR ANGLE (AL7075-T6 0.094) AND FILLERS (AL7075-T6 0.080) (AL7075-T6 0.125) IAW DWG W90-R17. CLEANED, TREATED AND PRIMED REPAIR ANGLE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED FILLERS AND REPAIR ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1, DWG W90-R17. 2L74 4F RT4A25 20050208000652005020800065WP 2005 2 8 DHL2004873530 120041129A5753 SKIN DOUG DC8 DC873F 302199FWP RT WING TE FLAPSDAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RIGHT WING OUTBOARD FLAP LWR FWD SKIN DAMAGED (BROKEN 1.000) AT XF 203.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG 1 PG 3/4, 5/6. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-5 FIG 1 PG 5-6. FABRICATED PLATING SEGMENT (AL2024-T3 0.032) SPLICE (AL2024-T3 0.063) FILLET (AL2024-T3 0.020) IAW SRM 57-2-5 PG 5-6. CLEANED, TREATED AND PRIMED NEW PLATING INTERIOR, SPLICE AND FILLET IAW SRM 51-1-8B. INSTALLED NEW FILLER, PLATING SEGMENT AND SPLICE IAW SRM 57-2-5 FIG 1 PG 3/4, 5/6, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050208000662005020800066WP 2005 2 8 DHL2004873500 120041027A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LT WING CTR L/E FORMER CRACKED 0.500 AT XFS 447.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLERS (AL 2024-T3 0.040) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050208000672005020800067WP 2005 2 8 DHL2004873501 120041104A57403645612U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 NR 1 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2L74 4F RT4A25 20050208000682005020800068WP 2005 2 8 DHL2004873535 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1000.000 L-14R TO L-15R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20 FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208000812005020800081WP 2005 2 8 DHL2004873555 120041203A53113755820 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLES AT STA 1300.000, L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-02-04, DWG W90-R18 DATED 11-22-04. REMOVED 2EA FITTINGS IAW DWG W90-R18, SRM 51-1-21 PG 1, SRM 51-1-20C. TRIMMED OUT MISDRILLED HOLES AREA IAW DWG W90-R18. FABRICATED EXT REPAIR DOUBLER (L7075-T6 0.090) AND FILLER (AL7075-T6 0.080) AND 2EA FRAME FITTING (AL7075T651) IAW DWG W90-R18, DWG 3755820 (FITTINGS). NDT INSPECTED NEW FITTINGS IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED EXT REPAIR DOUBLER, FILLER AND FRAME FITTINGS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS IAW DWG W90-R18, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000832005020800083WP 2005 2 8 DHL2004873540 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1560.000 L-20R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20 FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1 DWG W90-R20. 2L74 4F RT4A25 20050208000842005020800084WP 2005 2 8 DHL2004873536 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1540.000 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208000862005020800086WP 2005 2 8 DHL2004873559 120041203A53105651221 FAIRING DOUG DC8 DC873F 302199FWP MLG DOOR FRAME CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RT MLG DOOR JAMB FAIRING CRACKED 0.875, XW 3.125 AFTER EXISTING REPAIR (MAJOR REPAIR). REMOVED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-02-04, DWG W90-R12 REV IR DATED 11-18-04 DWG BOEING 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2024-0-0.040) IAW DWG W90-R12 DWG BOEING 5651221. HEAT TREATED IAW DACO DPS. 7.00. PERFORMED ND INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FAIRING IAW SRM 51-1-8B. INSTALLED NEW FAIRING IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 1-4. 2L74 4F RT4A25 20050208000902005020800090WP 2005 2 8 DHL2004873543 120041202A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-20R. PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208000912005020800091WP 2005 2 8 DHL2004873549 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1200.000, L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R19, REV:IR DATED 11-22-04 FAA FORM 8110-3 DATED 11-29-04. REMOVED EXISTING DAMAGED FRAME SPLICE PLATE AND FASTENERS IAW DWG W90-R19, SRM 51-1-21 PG 1, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER STRAP (AL7075-T6 0.090) AND FRAME SPLICE PLATE (7075T6 0.063) IAW DWG W90-R19. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PLUGGED MISDRILLED HOLES WITH RIVETS (NAS1097AD5) IAW SRM 51-1-21 PG 1, DWG W90-R19. INSTALLED EXTERNAL REPAIR DOUBLER STRAP AND FRAME SPLICE PLATE WITH NEW FASTENERS IAW DWG W90-R19, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050208001222005020800122GL 2005 2 8 CHQA200500018 220040125A72612307356 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A CHQAO OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL11268SK 145270 CAE311482 FLIGHT 3063 - LGA-SYR - EN ROUTE TO SYR A SMELL OF BURNING PLASTIC OR AN ELECTRICAL FIRE WAS NOTED IN THE COCKPIT AND CABIN. THE ODOR MADE EYES WATER AND THROAT SORE. LANDED IN SYR WITHOUT EVENT. MAINTENANCE FOUND NR 0 CARBON SEAL LEAKING ON THE LEFT HAND ENGINE. REMOVED AND REPLACED NR 0 CARBON SEAL ASSEMBLY. OPS AND LEAK CHECK GOOD IAW EMB 145 AMM 72-25-25. 2L72 4T4 FRTT00011ATTE6CH 20050203001372005020300137WP 2005 2 3 DHL2004873560 120041128A5311 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE FRAME CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT ACCY COMPT FRAME SPLICE ANGLE CRACKED 4.000 STA 1640.000 BETWEEN L-25 AND L-26R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 51. REMOVED CRACKED FRAME SPLICE ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FRAME SPLICE ANGLE (AL70750 0.071) IAW SRM 53-4-1 FIG 51, SRM 51-1-4 PG 1, DPS 3.69-4 REV-AM. PERFORMED HEAT TREATMENT IAW DPS 7.00-1 REV-BJ, SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FRAME SPLICE ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203001712005020300171NM 2005 2 3 CALA0500029 120041217A5313654988625 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2761304 23355 INSPECTION FOUND STRINGER 26L CORRODED BETWEEN STA 440 AND 500D. THE STRINGER WAS REPAIRED USING A SPLICE IAW ECRA 5311-01215. 2L72 4F RTA16WE 20050208000352005020800035WP 2005 2 8 DHL2004873565 120041124A53403754025 FITTING DOUG DC8 DC873F 302199FWP FUSLAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT FITTING CRACKED 1.500 STA 1160.000 L-26R TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1, DWG 3754025. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW FITTING (7075T651) IAW DWG 3754025. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D PG 9, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050208000362005020800036WP 2005 2 8 DHL2004873566 120041204A534037592221 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 7.000, FS 1275.000, L-36 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000622005020800062WP 2005 2 8 DHL2004873546 120041201A5753 SKIN DOUG DC8 DC873F 302199FWP LE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LT WING OUTBOARD FLAP L/E UPPER PART SKIN WORN BETWEEN XF 200.000 AND XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R03 REV: TR DATE 11/08/04 FAA FORM 8110-3 DATED 11-30-04. TRIMMED OUT PLATING SEGMENT (DAMAGED) IAW DWG W90-R03. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW PLATING SEGMENT (AL2024-T3 0.040) INTERNAL SPLICE DOUBLER (AL2024-T3 0.050) IAW DWG W90-R03. CLEANED, TREATED AND PRIMED AREA, NEW PLATING INTERIOR, INTERNAL SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED INTERNAL SPLICE DOUBLER AND PLATING SEGMENT (NEW) WITH NEW FASTENERS IAW DWG W90-R03, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050208000642005020800064WP 2005 2 8 DHL2004873503 120041104A534037799191N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 0.250, FS 1345.000, L-35R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208000692005020800069WP 2005 2 8 DHL2004873541 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1080.000, L-15R TO L-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208001412005020800141WP 2005 2 8 DHL2004873551 120041201A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 140.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R16, REV IR DATED 11-18-04 FAA FORM 8110-3 DATED 11-30-04. REMOVED L/E SKIN PANEL AND REPAIR PARTS FROM INTERNAL STRUCTURE IAW DWG W90-R16, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. FABRICATED 2EA SKIN PANEL (AL7075-T6 0.050) AND INTERNAL DOUBLER (AL7075-T6 0.063) AND 2EA REPAIR DOUBLER (AL7075-T6 0.063) IAW DWG W90-R16. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIR PARTS AND L/E SKIN PANELS IAW DWG W90-R16, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050208001592005020800159WP 2005 2 8 DHL2004873554 120041203A534037552222 FITTING DOUG DC8 DC873F 302199FWP FLOORBEAM CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FITTING ATTACHING TRACK NR 3 TO FLOORBEAM CRACKED 1.000 STA 798.000. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208001632005020800163WP 2005 2 8 DHL2004873556 120041203A53205651221 FAIRING DOUG DC8 DC873F 302199FWP MLG DOOR FRAME CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LT MLG DOOR JAMB FAIRING CRACKED 1.500 AT XW 3.125 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-02-04 DWG W90-R12 REV IR DATED 11-18-04 DWG BOEING 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2024 0 0.040) IAW DWG W90-R12, DWG BOEING 5651221. HEAT TREATED IAW DACO DPS 7.000. PERFORMED NDT INSP IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FAIRING IAW SRM 51-1-8B. INSTALLED FAIRING IAW SRM 51-1-21 PG 1. SRM 51-1-21A PG 1-4. 2L74 4F RT4A25 20050208001762005020800176WP 2005 2 8 DHL2004873545 120041201A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LT WING INBOARD L/E CRACKED 3.000 IN LWR SKIN SURFACE (STA XFS 622.500 - 628.725) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R14, REV: IR DATED 11-22-04, FAA FORM 8110-3 DATE 11-29-2004. REMOVED EXISTING REPAIR DOUBLER IAW DWG W90-R14, SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DWG W90-R14. PERFORMED NDT INSP IAW NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T6 0.063) AND FILLER (AL7075-T6 0.050) IAW DWG W90-R14. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF DOUBLER AND FILLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW DWG W90-R14, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208001792005020800179WP 2005 2 8 DHL2004809501 120041222A5720 INTERCOSTAL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LT WING CTR L/E INTERCOSTAL CRACKED 1.000, XFS 410.250 (UPPER PART). REMOVED CRACKED INTERCOSTAL IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERCOSTAL (AL2024-T3 0.063) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW INTERCOSTAL IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050208001812005020800181WP 2005 2 8 DHL2004809500 120041222A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 RIGHT WING CTR L/E FORMER CRACKED 0.250, STA XFS 291.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050209000192005020900019EA 2005 2 9 SWIA200414503 120041213A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 RIGHT SIDE FS 621 FLOORBEAM BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLES IAW REO 601R-53-61-117 AND REO 601R-53-5750. 2L72 4F RTA21EA 20050209000572005020900057WP 2005 2 9 UPS05843853 120041231A574037701441 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01868UP 45968 INSPECTION TYPE: C3, INBOARD END FITTING CRACKED AT RIGHT OUTBOARD SLOT UPPER DOOR. REMOVED AND REPLACED FITTING REF SRM 51-1-21, 51-3-0, DWG 3770144. OPS CHECK SLOT PER AMM27-80-05-4, 27-80-00. CHECK GOOD. 2L74 4F RT4A25 20050209001022005020900102EA 2005 2 9 SWIA200414500 120041213A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 FS 280 BL 9 LEFT INBOARD AND OUTBOARD ANGLE BRACKETS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. INSTALL NEW ANGLES PER REO 601R-53-11-137 AND CRJ 200, SRM 51-42-00, PG 1. 2L72 4F RTA21EA 20050209001222005020900122NM 2005 2 9 DHL2005743506 120041217A5315150510061 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3843038340 22438 MAIN PASSENGER CABIN STA 380 RBL 20 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6 FOUND OUT OF LIMITS. REMOVED FLOORBOARD TO GAIN ACCESS. REMOVED UPPER CHORD FROM STA 380 BL 0 TO RBL 33. MAT ID FOR UPPER CHORD BAC 1505-10061 PO 33-41778 IAW B727 SRM 53-10-2 FIG 7 SH 2. CUT AND TRIMMED UPPER CHORD, DRILL, DEBURRED, MATERIAL. FABRICATED -2 SUPPORT ANGLE AN 2 REINFORCEMENT STRAPS IAW B727 SRM 53-10-8. ALODINED AND PRIMED ALL MATERIAL IAW B727 51-10-2. INSTALLED ALL NEW MATERIAL IAW B727 SRM 53-10-8 PG 19. 2L73 4F A3WE 20050209001232005020900123NM 2005 2 9 DHL2005743505 120041217A5347606549 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3843038340 22438 MAIN PASSENGER CABIN STA 344 TO 380 RBL 44 SEAT TRACK HAS CORROSION. REMOVED, FAB, TRIMMED, DRILLED, DEBURRED, INSTALLED SEAT TRACK FS 344-380 RBL 44 IAW B727 SRM 53-10-5, 51-10-2, 53-10-2 FIG 7 51-30-2, 53-10-1 FIG 3. 2L73 4F A3WE 20050203001292005020300129WP 2005 2 3 DHL2004873558 120041130A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME FLANGE CRACKED 2.000 AND DENTED, STA 1580.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-110. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2. FABRICATED NEW FRAME SEGMENT (7075"0" 0.080) AND 2EA SPLICES (7075"0"0.071) IAW SRM 53-2-0 FIG 2, DACO DPS 3.69-4, SRM 51-1-4 PG 1. HEAT TREATED FRAME SEGMENT AND SPLICES IAW DACO DPS 7.00 RV -BJ-, SRM 51-1-1 PG 1, 13, 17. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 2, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050203001322005020300132WP 2005 2 3 DHL2004809505 120041227A5200 DOOR DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 EXTERNAL FUSELAGE D-BELLY DOOR FWD UPPER CORNER JAMB CRACKED 0.750, STA 1400.000 L-26.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2004-06-06, SB DC8-53-078 REV-1, DWG SRO8530019 CONFIGURATION G, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW DWG SRO8530019. FABRICATED FILLER (AL7075-T6 0.080), DOUBLER (AL7075-T6 0.070), TRIPLER (AL7075-T6 0.125) IAW DWG SRO8530019. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26. INSTALLED REPAIRED PARTS IAW DWG SR08530019, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. PERFORMED REPETITIVE INSPECTIONS IAW AD2004-06-06 PARAGRAPH A)3) AT INTERVALS NOT TO EXCEED 4400 LANDINGS. 2L74 4F RT4A25 20050208000342005020800034WP 2005 2 8 DHL2004873564 120041204A53132753715 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT L-34R CRACKED 5.000 AT FS 1270.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 PG 1, 2, 4, 6, 9, 13, SRM 53-2-0 PG 1, SRM 53-4-1 FIG 43A. TRIMMED OUT CRACKED LONGERON IAW SRM 53-2-2 FIG 4A. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED SPLICE FITTING (7075T6AL 0.250) SRM 53-2-2 TR 53-153 FIG 10. FABRICATED NEW LONGERON SEGMENT (EXTRUSION 2753715) IAW SRM 53-4-1 FIG 43A. CLEANED, TREATED AND PRIMED AREA NEW LONGERON SEGMENT AND SPLICE FITTING IAW SRM 51-1-8B. INSTALLED REPAIRED PARTS IAW SRM 53-2-2 PG 1, 2, 4, 6, 13, SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050208000432005020800043WP 2005 2 8 DHL2004873515 120041104A5542 SKIN DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RT RUDDER SKIN CRACKED 0.250, STA ZR 161.000 (HOIST POINT) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU. REMOVED CRACKED SKIN IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU, SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-T3AL 0.032) IAW BOEING MSG 1-RJ0SG AND MSG 1-RL7IU. PERFORMED DIMPLING TO NEW SOLID SHEET SKIN IAW DC8 SRM 51-1-22. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED NEW SKIN IAW BOEING MSG 1-RJ0SG AND BOEING MSG 1-RL7IU, DC8 SRM 51-1-21. AT C-CHECK INTERVALS A VISUAL AND X-RAY INSP IS ACCOMPLISHED TO INSPECT FOR CRACKS IN THE SKIN AND RADIUS OF THE INTERNAL RIBS. 2L74 4F RT4A25 20050208000612005020800061WP 2005 2 8 DHL2004873537 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED AT STA 1020.000, L-14R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208000702005020800070WP 2005 2 8 DHL2004873544 120041202A5310 BEAM DOUG DC8 DC873F 302199FWP BULKHEAD DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT AFT PRESSURE BULKHEAD VERTICAL BEAM HOLES MISDRILLED AT STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R15 AND FAA FORM 8110-3 NOV 30,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470DD) IAW SRM 561-1-21 PG 1, DWG W90-R15. 2L74 4F RT4A25 20050208000712005020800071WP 2005 2 8 DHL2004873553 120041201A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LT WING INBOARD L/E LWR SKIN CRACKED 0.500 AT XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R01, REV IR DATED 11-08-04 FAA FOMR 8110-3 DATED 11-30-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAGED SECTION IAW DWG W90-R01. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T6 0.071) AND FILLER (AL7075-T6 0.063) IAW DWG W90-R01. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED FILLER AND DOUBLER WITH NEW FASTENERS IAW DWG W90-R01, SRM 51-1-20D PG 9, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050208000872005020800087WP 2005 2 8 DHL2004873547 120041203A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME HAS 2EA MISDRILLED HOLES AT STA 1380.000, L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R17, REV IR DATED 11-22-04, FAA FORM 8110-3 DATED 12-2-04. CUT OUT MISDRILLED HOLE AREA IAW DWG W90-R17. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED REPAIR ANGLE (AL7075-T6 0.094) AND FILLERS (AL7075-T6 0.080_ (AL7075-T6 0.125) IAW DWG W90-R17. CLEANED, TREATED AND PRIMED REPAIR ANGLE AND FILLERS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED FILLERS AND REPAIR ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9, DWG W90-R17. 2L74 4F RT4A25 20050208000882005020800088WP 2005 2 8 DHL2004873548 120041201A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 UPPER FUSELAGE SKIN DENTED BETWEEN STA 210.000 AND 220.000 (4.000 BELOW MAIN CARGO DOOR LWR JAMB) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R09, REV:IR DATED 11-22-04, FAA FORM 8110-3 DATED 11-29-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. SMOOTHED BLENDED DAMAGE TWO PLCS WITH R1.0 MIN IAW DWG W90-R09. FABRICATED REPAIR DOUBLER (AL7075-T6 0.090) IAW DWG W90-R09. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACE IAW SRM 51-1-11 PG 1. INSTALLED REPAIR DOUBLER WITH NEW FASTENERS IAW DWG W90-R09, SRM 51-1-20D PG 9, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050208000952005020800095NM 2005 2 8 UPS05M43859 120041215A5320 STIFFENER DOUG MD11 MD11F 3023600NM LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C, LEFT MLG WHEEL WELL TORQUE BOX INTERIOR SIDE FOUND T-STIFFENER CRACKED AS MARKED. T-STIFFENER & ATTACHED BRACKET REMOVED AS PER SRM 51-35-01 & 5133-01 V.2 REV 35. NEW T-STIFFENER FAB AS PER DWG AEA7031.FPI CUTOUT ON FAB STIFFENER, NO CRACK FOUND. NEW STIFFENER HOLES TRANSFERED AS PER SRM 51-3 1-01 V.2R.36. NEW T-STIFFENER SURFACE PROTECTION CUTOUT AS PER SRM 51-2 1-01V.2.R36 & ATTACHED BRACKET INSTALLED AS SRM 51-33 (& 35) -01.V2.R36. 2L73 4F RTA22WE 20050208001652005020800165WP 2005 2 8 DHL2004809507 120041227A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 EXTERNAL FUSELAGE - EXTERNAL SKIN CRACKED 0.500 AT STA 194.000 L-30L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5. FABRICATED FILLER (AL7075-T6 0.071) FINGER DOUBLER (AL7075T6 0.050) DOUBLER (AL7075T6 0.080) IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5 SRM 53-4-1 PG 7 FIG 4. CLEANED TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW SRM 53-2-1 FIG 7 SHEET 1, 3, 5 SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208001682005020800168WP 2005 2 8 DHL2004873502 120041104A534037799191N FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT SPLICE FITTING CRACKED 0.250, FS 1345.00, L-34R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050208001802005020800180WP 2005 2 8 DHL2004873519 120041114A571297532973 RIB DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 NR 1 LEFT STUB WING RIB HOLES ELONGATED, STA XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED NR 1 LEFT STUB WING RIB IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW RIB IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050209001412005020900141WP 2005 2 9 DHL2004873552 120041130A5342 ANGLE DOUG DC8 DC873F 302199FWP VERTICAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT FUSELAGE ATTACH ANGLE WITH VERTICAL STABILIZER CORRODED (BETWEEN FRONT SPAR AND CTR SPAR RT SIDE). PERFORMED MAJOR REPAIR. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. TRIMMED OUT CORRODED AREA IAW SRM 53-2-5 FIG 16A, SHEET 1. FABRICATED FILLER (AL7075-T6 0.160) SHIM (AL7075-T6 0.125) ANGLE DOUBLER (STEEL 17.7 PH 0.079) IAW SRM 53-2-5 FIG 16A SHEET 1-2. PERFORMED HEAT TREATMENT TO STEEL 17.7 PH IAW DPS 5.00R. PERFORMED NDT INSPECTION TO ANGLE DOUBLER IAW NDT SPM PART 08-00-02107, SRM 53-2-5 FIG 16A SHEET 2. CLEANED,TREATED AND PRIMED AREA, FILLER, SHIM IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER, SHIM & ANGLE DOUBLER. 2L74 4F RT4A25 20050209001562005020900156WP 2005 2 9 DHL2004809510 120041230A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 EXTERNAL FUSELAGE - EXTERNAL SKIN CORRODED STA 857.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (AL7075-T6 0.100) INTERNAL FINGER DOUBLERS (2EA) (AL7075-T6 0.050) IAW DWG X32-R02. CLEANED, TREATED AND PRIMED REPAIRED PARTS IAW SRM 51-1-8B. FILLED VOID IN BLENDOUT WITH HYSOL IAW SRM 51-1-9. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS. 2L74 4F RT4A25 20050209001622005020900162NM 2005 2 9 DHL2005743508 120041217A5347 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 MAIN PASSENGER CABIN STA 360 LBL 20 FLOORBEAM HAS CORROSION. CUT OUT DAMAGE AREA, FAB NEW UPPER CHORD, 2 EA REPAIR ANGLES, AND 2 EA REINFORCEMENT STRAPS. DRILLED AND DEBURRED, ALODINED AND PRIMED AND INSTALLED IAW BOEING 727 SRM 51-30-2, 53-10-8, 51-10-2 AND 53-10-1. 2L73 4F A3WE 20050209001762005020900176NM 2005 2 9 DHL2005743507 120041217A5347 FLOORBEAM BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 MAIN PASSENGER CABIN STA 344 RBL 47 FLOORBEAM HAS CORROSION. CORROSION AT RBL 47 UPPER CHORD FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B727 SRM 53-10-1 FIG 4. REMOVED FASTENERS AND CUT AND REMOVED UPPER TEE CAP FROM LBL 20 TO RBL 66 IAW B727 SRM 53-10-8 FIG 9. FABBED, POSITIONED, DRILLED, DEBURRED, ALODINED AND PRIMED (1) NEW UPPER TEE CAP AND (2), -2, -3 REPAIR ANGLES IAW B727 SRM 53-10-8 FIG 9. 2L73 4F A3WE 20050209001852005020900185EA 2005 2 9 SWIA200414501 120041213A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 FS 280 BL 9 RIGHT INBOARD AND OUTBOARD ANGLE BRACKETS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INBOARD AND OUTBOARD BRACKET IAW SRM 51-42-06. 2L72 4F RTA21EA 20050209001862005020900186EA 2005 2 9 SWIA200414502 120041213A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07437SW 7564 RIGHT AND LEFT FS 625.00 BRACKETS ARE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INTERCOSTALS FS 625.00 STR 14 RIGHT AND LEFT PER CRJ 200 SRM 51-42-06. 2L72 4F RTA21EA 20050209002032005020900203NM 2005 2 9 SWAA050165 120041215A3350D71702001 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29764SW 27878 DURING SPV, FOUND L1 DOOR EMERGENCY EXIT INTERIOR AND EXTERIOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20050210000022005021000002EU 2005 2 10 USAA041125 120041217A5315F53478214200300EFLOORBEAM AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND FLOORBEAM CORRODED .6 INCH BY .6 INCH BY .045 INCH DEEP, MAIN CABIN FLOORBEAM 74, -Y 1202 CM. CORROSION LEVEL 2, TASK NR J7-270-53500. REMOVED AND REPLACED BEAM PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050210000032005021000003WP 2005 2 10 GTIA040871 120041223A5280 DOOR DOUG DC9 DC981 3022081WP MLG DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 MCO - FLT 138 - RIGHT HYDRAULIC LEAK, NO QTY OR PRESSURE, FURTHER INSPECTION REVEALED DAMAGE TO LOWER SECTION OF MAIN LANDING GEAR DOORS. AIRCRAFT SWAP. REPAIRED RT MLG AND LT MLG DOORS IAW MD80 SRM 52-05, INSTALLED TEMP REPAIR. (M) 2L72 4F A6WE 20050210000062005021000006NM 2005 2 10 GTIA040862 120041202A5330 SKIN DOUG MD80 MD83 3023681NM FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND FUSELAGE SKIN CUTOUT FOR L1 DOOR HOLD OPEN HOOK CRACKED AND GOUGED OUT. BLENDED GOUGE AND REMOVED CRACKED EDGE AT L1 DOOR CUTOUT, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RT 20050210000082005021000008 2005 2 10 GTIA040873 420041225A2310 RADIO DOUG DC9 DC982 3022082WP HF SYSTEM WILL NOT TEST A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23829NK 49931 MCO - FLT 1865 - UNILINK FAILED AND HF RADIO WILL NOT TEST, UNABLE TO ESTABLISH COMMUNICATION DURING PREFLIGHT, AIRCRAFT SWAPPED. RESEATED UNILINK BOX AND C/B'S, PERFORMED OPS CHECK, OPS CHECK OK. REMOVED AND REPLACED HF TRANSCEIVER, OPS TEST OK. (M) 2L72 4F A6WE 20050210000102005021000010WP 2005 2 10 GTIA040876 120041228A215020495054 ACM DOUG DC9 DC982 3022082WP RIGHT LEAKING A GTIAA UNSCHED LANDING KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL23829NK 49931 EWR - FLT 861 - SMOKE IN CABIN, INCREASING VISIBLE IN COCKPIT, SET OFF DETECTOR IN AFT LAV'S, APU WAS OFF, CLIMB POWER, LANDED IN EWR. SMOKE DISSIPATED ON LANDING. FOUND RIGHT ACM LEAKING OIL INTO AIR CONDITION SYSTEM. REMOVED AND REPLACED RIGHT AC AND RIGHT TEMP CONTROL VALVE, LEAK CHECKS GOOD. (M) 2L72 4F A6WE 20050210000152005021000015NM 2005 2 10 HALA0401181 120041215A3230 BOLT BOEING717 717200 1383700NM DRIVE ARM BENT A HALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 WP13478HA 55123 ATB - MAIN LANDING GEAR DOORS WOULD NOT RETRACT AFTER LANDING GEAR EXTENDED. AIRCRAFT RETURNED TO HNL WHERE AN UNEVENTFUL LANDING WAS MADE. RIGHT MAIN LANDING GEAR FOUND DOOR SEQUENCE DRIVE ARM BOLT BENT. REPAIR ARM AND BOLT, PERFORMED GEAR SW PER AMM 32-33-00, OPS CHECK GEAR SW GOOD, RESTOWED EMERGENCY EXT HANDLE REP BOTH MLG SKIN PADS PER DAC DWG NR 5910783 SECURITY CHECK OK. (M) 2L72 4F TRA6WE 20050210000162005021000016NM 2005 2 10 USAA041063 120041215A5330 SKIN BOEING757 7572B7 1384964NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU39875 27123 CLT - FOUND SKIN CRACKED, LOWER FORWARD CORNER OF FORWARD PRESSURE RELIEF DOOR CUTOUT. INSTALLED DOUBLER IAW EA 96083. (M) 2L72 4F RTA2NM 20050210000172005021000017EU 2005 2 10 USAA041113 120041210A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - SEAT TRACK CORRODED .479 INCH WIDE BY .125 INCH DEEP BY .125 INCH LENGTH AREA, FRAME 43, Y PLUS -450 SCALLOP OF SEAT TRACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SH 8, 51-42-11. (M) 2L72 4F RTA46NM 20050210000182005021000018EU 2005 2 10 USAA041109 120041209A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 FOUND SEAT TRACK CORRODED .024 INCH DEEP BY .50 INCH WIDE BY .075 INCH LONG AREA, BETWEEN FRAME 46-47, Y+-450 SEAT TRACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2L72 4F RTA46NM 20050210000192005021000019NM 2005 2 10 USAA040871 120041115A5315 FLOORBEAM BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND FLOORBEAM CORRODED 2 SQUARE INCHES, STATION 347 RBL 48. ACCOMPLISHED T-CAP REPAIR IAW SRM 53-00-01. (M) 2L72 4F RTA1NM 20050210000212005021000021NM 2005 2 10 USAA040869 120041115A5330 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND SEAT TRACK CORRODED .5 INCH BY .5 INCH, STATION 347, RBL 88. REPLACED SEAT TRACK SECTION IAW SRM 51-40-2. (M) 2L72 4F RTA1NM 20050210000222005021000022NM 2005 2 10 USAA040904 120041118A5330 SKIN BOEING767 767201 1385125NM FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND SKIN WITH UNDOCUMENTED REPAIR, STATION 347 STRINGER 31R. DOUBLER INSTALLED IAW EA 85680. (M) 2L72 4F RTA1NM 20050210000232005021000023EU 2005 2 10 USAA041126 120041216A5347F53275665200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED 1 INCH WIDE BY 1 LENGTH BY .039 INCH DEEP, Y1959 FROM FRAME 32-33. CORROSION LEVEL 2, TASK NR J7-230-53500. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 53-21-15, 51-44-11. (M) 2L72 4F RTA46NM 20050210000242005021000024EU 2005 2 10 USAA041127 120041218A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK ASSEMBLY CORRODED .075 INCH LENGTH BY 050 INCH WIDE BY .040 INCH DEEP, AFT CABIN SEAT TRACK AT Y-1207, FRAME 73. CORROSION LEVEL 2, TASK NR J7-200-53500. REMOVED AND REPLACED PER SRM 53-00-15, 51-74-00, 51-42-11, 51-44-11. 2L72 4F RTA46NM 20050210000262005021000026EU 2005 2 10 USAA041131 120041213A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED, .055 INCH DEEP BY 5 INCH LENGTH BY 2 INCHES WIDE, FRAME 44, Y=-450. REMOVED AND REPLACED PER SRM 53-31-15. CORROSION LEVEL 2, TASK NR J7-200-2578C-003. (M) 2L72 4F RTA46NM 20050210000272005021000027NM 2005 2 10 USAA041062 120041213A5200 SKIN BOEING767 767201 1385125NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US70070 23901 CLT - FOUND SKIN CRACKED .375 INCH, LOWER FORWARD CORNER OF AFT CARGO DOOR, 2ND HOLE FROM LEFT. INSTALLED DOUBLER IAW EA 96069. (M) 2L72 4F RTA1NM 20050210000312005021000031EU 2005 2 10 USAA041128 120041211A5310F5347901100100 STRUCTURE AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND PROFILE Z-ASSY CORRODED .781 INCH LONG BY .843 INC WIDE BY .054 INCH DEEP, CABIN MAIN, Y-1805, FRAME 76-77. REMOVED AND REPLACED PROFILE Z-ASSY PER SRM 53-41-14, 51-74-00, 51-42-11. (M) 2L72 4F RTA46NM 20050210000322005021000032NM 2005 2 10 USAA041111 120041228A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU53844 23228 CLT - FOUND SKIN CRACKED 1.5 INCH, S-23R AT STATION 727D. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050210000332005021000033NM 2005 2 10 USAA041080 120041220A5315 FLOORBEAM BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US70070 23901 CLT - FOUND FLOORBEAM CORRODED 12 INCHES, STATION 347 FROM FROM 32 TO 44 RBL . REPLACED TEE CAP SECTION PER SRM 53-00-51. (M) 2L72 4F RTA1NM 20050210000342005021000034EU 2005 2 10 USAA041104 120041211A5321F5367141400000 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND PANEL FLOOR DELAMINATED, MAIN CABIN FLOOR PANEL 261BF. FABRICATED NEW PANEL PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050210000362005021000036 2005 2 10 GTIA040870 420041221A3454 RECEIVER DOUG DC9 DC982 3022082WP NR 2 VOR SYS INOPERATIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23829NK 49931 DTW - NR 2 VOR INOPERATIVE, NO RECEPTION, AIRCRAFT SWAP. REMOVED AND REPLACED NR 2 VOR/IIS RECEIVER, OPS CHECK GOOD. (M) 2L72 4F A6WE 20050210000372005021000037NM 2005 2 10 GTIA040865 120041202A5730 ACCESS PANEL DOUG MD80 MD83 3023681NM LT WING DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND LEFT WING INBOARD BUTTE DOOR INBOARD EDGE, BOTTOM SIDE IS DAMAGED. BLENDED OUT DAMAGE MATERIAL LOSS OUT OF LIMITS, FABRICATED NEW DOUBLER, DRILLED AND LOCATED HOLES. OK TO TREAT, PRIME AND INSTALLED DOUBLER. (M) 2L72 4F RT 20050210000382005021000038NM 2005 2 10 GTIA040864 120041203A5320 FLOOR SUPPORT DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND FORWARD CABIN STATION 207, RBL 11 INCH FLOOR SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT AT STATION 207, RBL 11, FABRICATED NEW FLOOR SUPPORT, TREATED, PRIMED, TOPCOATED AND INSTALLED FLOOR SUPPORT. (M) 2L72 4F RT 20050210000402005021000040 2005 2 10 2005F00003 420041015A34147002860909 INDICATOR AEROSPATR72 ATR72 EU CAPT. AIRSPEED FAILED A TRBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO21417AT 417 DURING TAKEOFF ROLL, CAPTAIN AIRSPEED INDICATOR FAILED AT 100 KTS, FLUCTUATED BETWEEN 80 KTS AND 120 KTS WITH RED FLAP. REPLACED AIRSPEED INDICATOR. (M) 2H72 4T RT 20050210000412005021000041 2005 2 10 2005F00004 420041028A34177000700951 ADC AEROSPATR72 ATR72212 8680945EU NR 1 FAILED A TRBAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO21417AT10475 417 DURING TAKEOFF ROLL, CAPTAIN SIDE AIRSPEED FAIL FLAP CAME OUT, THE TRUE AIRSPEED SHOWED ONLY DASHES AND THE STANDBY ALTIMETER STUCK MOMENTARILY. TAKEOFF ABORTED. REPLACED NR 1 AIR DATA COMPUTER. (M) 2H72 4T RTA53EU 20050210000422005021000042WP 2005 2 10 GTIA040872 120041224A7711 LINE DOUG DC9 DC982 3022082WP LT ENGINE PT2 LOOSE A GTIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL23821NK 49508 DTW - FLT 689 - ON TAKEOFF ROLL, AUTO THROTTLES ON SETTING NORMAL POWER LEFT ENGINE EPR 1.70 ONLY WHILE N1 WENT OT 103 PERCENT, EGT WAS 500 DEGREES, ABORTED TAKEOFF, AIRCRAFT SWAP. FOUND PT2 LINE IN NOSE BULLET CONNECTIONS ON BOTH ENDS LOOSE, TIGHTENED LINES, OPS CHECK GOOD. (M) 2L72 4F A6WE 20050210000452005021000045NM 2005 2 10 USAA041079 120041220A5347 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US 23901 CLT - FOUND SEAT TRACK CORRODED 3 INCH BY 1 INCH, STATION 713.5 TO 716 LBL 88.5. INSTALLED NEW SECTION OF SEAT TRACK PER SRM 53-00-52. (M) 2L72 4F RTA1NM 20050210000462005021000046EU 2005 2 10 USAA041105 120041210A5347F3311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED, .038 INCH DEEP BY 1 INCH WIDE BY 1 INCH LENGTH, FRAME 47, Y+450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578C-025. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101, SHT 8, SRM 51-42-11. (M) 2L72 4F RTA46NM 20050210000472005021000047EU 2005 2 10 USAA041106 120041209A5320F5347821620600 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND FLOOR SUPPORT CORRODED, 2 INCH BY 1 INCH BY .045 INCH DEEP CORRODED AT LOCK FASTENER, Y 0 AT FRAME 78. CORROSION LEVEL 2, TASK NR J7-270-53500-017. REMOVED AND REPLACED SUPPORT PER SRM 53-00-15, 51-42-11, 51-44-11. (M) 2L72 4F RTA46NM 20050210000482005021000048EU 2005 2 10 USAA041107 120041210A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .022 INCH DEEP BY .35 INCH WIDE BY .075 INCH LONG AREA, BETWEEN FRAME 41-42, Y= -450, SEAT TRACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SH 8, 51-42-11. (M) 2L72 4F RTA46NM 20050210000492005021000049EU 2005 2 10 USAA041108 120041210A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED, .019 INCH DEEP Y .25 INCH WIDE BY .5 INCH LONG AREA, BETWEEN FRAME 44-45, Y=-450 SEAT TRACK. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2L72 4F RTA46NM 20050210000502005021000050NM 2005 2 10 USAA040868 120041115A5347 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND SEAT TRACK CORRODED 3 SQUARE INCHES, STATION 347 RBL 52. REPLACED SEAT TRACK SECTION. (M) 2L72 4F RTA1NM 20050210000512005021000051NM 2005 2 10 USAA040865 120041110A5347 SEAT TRACK BOEING767 767201 1385125NM FS CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND SEAT TRACK CORRODED 1 INCH BY 14 INCHES, STATION 347 LBL 88. FABRICATED SEAT TRACK FROM NEW EXTRUSION IAW DRAWING NR 141T5121-25. (M) 2L72 4F RTA1NM 20050210000532005021000053EU 2005 2 10 USAA041119 120041211A5320F5347823420000 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND FLOORBOARD SUPPORT CORRODED 2 INCHES WIDE BY 1.3750 INCH LENGTH BY .035 INCH DEEP, Y308 AT FRAME 75. CORROSION LEVEL 2, TASK NR J7-270-53500-015. REMOVED AND REPLACED SUPPORT PER SRM 51-74-00, 53-41-14, 51-42-11, 51-44-11. (M) 2L72 4F RTA46NM 20050203001302005020300130WP 2005 2 3 DHL2004873513 120041108A5542 STRUCTURE DOUG DC8 DC873F 302199FWP RUDDER CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RUDDER RIGHT L/E CRACKED 3.000M ZR 172.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-6-1 FIG 1. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (ALCLAD 2024-T3 0.040) IAW SRM 55-6-1 PG 2 FIG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED NEW PLATING IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050207000132005020700013NM 2005 2 7 2005UALA00088 120040123A3350 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETERIORATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29597UA 28750 EMERGENCY EQUIPMENT LIGHT (EEL) STRIPS DETERIORATED THROUGHOUT THE CABIN. REPLACED EEL LIGHT STRIPS. 2L72 4F4 FRTA2NM E17NE 20050208000852005020800085WP 2005 2 8 DHL2004873538 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT MISDRILLED HOLES AT STA 1311.000 L-11 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED 29-11,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGINS MISDRILLED HOLES WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208000892005020800089WP 2005 2 8 DHL2004873539 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-17R. PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050208001662005020800166WP 2005 2 8 DHL2004873563 120041204A531327S3715 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT L-36 CRACKED 6.000 AT FS 1270.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-2 PG 1, 2, 4, 6, 9, 13, SRM 53-2-0 PG 1, SRM 53-4-1 FIG 43A. TRIMMED OUT CRACKED LONGERON SEGMENT IAW SRM 55-2-2 FIG 4A. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. FABRICATED SPLICE FITTING (7075T6AL 0.250) IAW SRM 53-2-2 TR 53-153 FIG 10. FABRICATED NEW LONGERON SEGMENT (EXTRUSION 2753715) IAW SRM 53-4-1 FIG 43A. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON SEGMENT, SPLICE FITTING IAW SRM 51-1-8B. INSTALLED REPAIRED PARTS IAW SRM 53-2-2 PG 1, 2, 4, 6, 9, 13 SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20050208001692005020800169WP 2005 2 8 DHL2004873542 120041201A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-20L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470ADG) IAW SRM 51-1-21 PG 1, DWG W90-R20. 2L74 4F RT4A25 20050209001512005020900151NM 2005 2 9 DHL2005743503 120041222A5320 FLOOR SUPPORT BOEING727 727225 1384077NM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3843038340 22438 AFT CARGO COMPT STA 1183 RBL 7, LONGITUDINAL FLOOR SUPPORT CRACKED AT END, .375 INCH. CUT OUT DAMAGED SECTION IAW B727 SRM 51-40-3. FABBED REPAIR ANGLE IAW B727 SRM 51-40-3 FROM 7075-0 .071 PO 044327, HEAT TREATED TO T-6 ON PEMCO TRAVELER 76314000863. DRILLED, TRIMMED, DEBURRED, ALODINED AND PRIMED IAW B727 SRM 51-10-2. FABBED REPAIR FILLER FROM 7075T-6 .050 PO 0441816, TRIMMED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW B727 SRM 51-10-2, 51-10-2. 2L73 4F A3WE 20050209001592005020900159WP 2005 2 9 DHL2004809511 120041227A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 EXTERNAL FUSELAGE - CORROSION BETWEEN SKIN AND L-30L, STA 1263.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 FIG 7 SHEET 4, 5. FABRICATED FINGER DOUBLER (AL7075-T6 0.050), FILLER (AL7075-T6 0.100), DOUBLER (AL7075-T6 0.125) IAW SRM 53-2-1 FIG 7 SHEET 1, 4, 5 SRM 53-4-1 FIG 17A. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS AND FASTENERS (NEW) IAW SRM 53-2-1 FIG 7 (SHEET 1, 4, 5) SRM 51-1-21 PG 1, SRM 51-1-20D PG 9 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050209001652005020900165WP 2005 2 9 DHL2004873521 120041123A5320 CUSP WEB DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT CUSP EXTRUSION CRACKED 2.000, STA 1080.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 15, TR 53-179. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CUT OUT CUSP EXTRUSION DAMAGED SEGMENT IAW SRM 53-2-5 FIG 15 PG 35-38. FABRICATED 4EA SPLICES (7075"0"0.160) AND 1EA EXTERNAL DOUBLER (7075 "0" 0.071) IAW SRM 53-2-5 FIG 15 SHEET 2, 4, 5. HEAT, TREATED SPLICES AND EXTERNAL DOUBLER IAW DACO DPS 7.00. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 1. INSTALLED NEW CUSP EXTRUSION SEGMENT (EXTRUSION S2757602) EXTERNAL DOUBLER, SPLICES AND NEW FASTENERS. 2L74 4F RT4A25 20050210000042005021000004NM 2005 2 10 GTIA040866 120041201A5753 WEDGE DOUG MD80 MD83 3023681NM TE FLAPS DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD WEDGE BOTTOM SIDE HAS DENT WITH FILLER COMPOUND. STRIPPED FILLER COMPOUND DENT OUT OF LIMITS, CUT OUT DAMAGE 1.5 INCH BY 2.5 INCH, FABRICATED FILLER AND DOUBLER, DRILLED HOLES. OK TO TREAT AND PRIME AND INSTALLED REPAIR. (M) 2L72 4F RT 20050210000072005021000007NM 2005 2 10 GTIA040857 120041206A2150 GASKET DOUG MD80 MD83 3023681NM A/C PACK DAMAGED A GTIAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL23822NK 49392 FLL - FLT 758 - AFTER TAKEOFF AT 800 FEET, THE TAIL COMPARTMENT OVERTEMP LIGHT CAME ON, FOLLOWED QRH PROCEDURES THE LIGHT WENT OUT WHEN THE LEFT THROTTLE WAS PLACED IN IDLE. THE LIGHT CAME BACK ON WHEN THE THROTTLE WAS RETURNED ABOVE 1.5 EPR, THE LIGHT WENT OUT WHEN THROTTLE WAS REDUCED BELOW 1.4 EPR, RETURNED TO FLL ON REDUCED POWER. INSPECTED THE PNEUMATIC DUCTING ON THE LEFT SIDE TAIL COMPARTMENT AND DETERMINED THE PACK INLET HIGH TEMP SENSOR GASKET WAS DAMAGED. REMOVED AND REPLACED SENSOR GASKET, OPS CHECK GOOD. (M) 2L72 4F RT 20050210000202005021000020NM 2005 2 10 USAA040870 120041115A5330 SKIN BOEING767 767201 1385125NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US69337 23902 CLT - FOUND SKIN CRACKED 4 INCHES, FORWARD OF RIGHT HORIZ STAB LE STATION 1637 S-14R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA1NM 20050210000282005021000028EU 2005 2 10 USAA041129 120041219A5347F5347621120100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH LENGTH BY 1.250 INCH WIDE BY .129 INCH DEEP, Y 1959 BETWEEN FRAME 57.4-58 - Z240. REMOVED AND REPLACED WITH NEW SEAT TRACK PER SRM 53-00-15 AND 51-42-11. (M) 2L72 4F RTA46NM 20050210000522005021000052EU 2005 2 10 USAA041123 120041216A5347F5347821720100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED 1.5 INCH LONG BY .68 INCH WIDE BY .060 INCH DEEP, -Y406, AT FRAME 73. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 51-44-11, 51-21-11. CORROSION LEVEL 2, TASK NR J7-270-53500. (M) 2L72 4F RTA46NM 20050210000592005021000059EU 2005 2 10 USAA041103 120041211A5321 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND FLOOR PANEL DELAMINATED, GREATER THAN 10 PERCENT OF PANEL AREA, F5367284300200. FABRICATED NEW PANEL PER SAMPLE PER SRM 53-02-00. (M) 2L72 4F RTA46NM 20050210000632005021000063WP 2005 2 10 GTIA040874 120041226A3241426071 CONTROL BOX DOUG DC9 DC983 3022083WP ANTI SKID SYSTEMFAULTY A GTIAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL23826NK 49391 DTW - BRAKES FAILED ON TAXI OUT TO RUNWAY 25R, ANTI-SKID TEST SHOWED 3 ANTI-SKID FAIL. FOUND ANTI-SKID CONTROL BOX AT FAULT, REPLACED ANTI-SKID CONTROL UNIT. OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 20050210000652005021000065EU 2005 2 10 USAA041116 120041211A5347F5711056820400 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED 1.2 INCHES LONG BY .700 INCHES WIDE BY .030 INCHES DEEP, CABIN FLOOR, Y450, FRAME 41, FRAME 42. CORROSION LEVEL 2, TASK NR J7-200-2578C. REMOVED AND REPLACED SEAT TRACK ASSY PER SRM 53-31-15, 51-42-11. (M) 2L72 4F RTA46NM 20050210000662005021000066EA 2005 2 10 A6WA200440217 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 FOUND LEFT FS 484 AT LBL 36 ANGLE CRACKED. REPAIRED LEFT FS 484 AT LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A. (M) 2L72 4F RTA21EA 20050210000682005021000068EU 2005 2 10 USAA041115 120041210A5347F5327584620000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA1967OUW 315 BFM - FOUND SEAT TRACK CORRODED, 2 INCHES BY .5 INCH BY .070 INCH AREA, Y 1456 BETWEEN FRAME 32 AND 33. CORROSION LEVEL 2, TASK NR J7-230-53500-001. REMOVED AND REPLACED TRACK PER SRM 53-00-15. (M) 2L72 4F RTA46NM 20050210000712005021000071NM 2005 2 10 ASAA0410542 120041116A5313655292833 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - AFT CARGO PIT BILGE AREA AT STRINGER 27R HAS BLOWN OUT CORROSION BETWEEN STATION 947 AND 967. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICED IAW SRM. (M) 2L72 4F RTA16WE 20050210000722005021000072NM 2005 2 10 ASAA0410541 120041116A53116547955508 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FRAME STATION 767 CORRODED BETWEEN STRINGER 26L AND 26R. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR SHEAR TIE, DOUBLERS, RADIUS FILLERS AND SHIMS, IAW SRM. (M) 2L72 4F RTA16WE 20050210000742005021000074WP 2005 2 10 GTIA040859 120041210A2730 PRESSURE SWITCH DOUG DC9 DC982 3022082WP ELEVATOR CONTROLINTERMITTENT A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23829NK 49931 MCO - FLT 1912 - LEVELING AT 3,000 FEET ELEVATOR POWER LIGHT CAME ON, NO ABNORMAL ELEVATOR CONTROL FELT, RETURNED TO MCO. PERFORMED INSPECTION ON ELEVATOR POWER PACK, PLUS CHECKED ACCUMULATOR. NO FAULT FOUND, SUSPECT BAD CONTACT SWITCH, INTERMITTENT. REMOVED AND REPLACED ELEVATOR POWER CONTROL PRESSURE SWITCH, OPS CHECK GOOD. (M) 2L72 4F A6WE 20050210000752005021000075NE 2005 2 10 GTIA040858 220041207A7261 FILTER DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE RT ENGINE CLOGGED A GTIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23835NK 53044 ORF - FLT 379 - RIGHT OIL STRAINER CLOGGING LIGHT CAME ON DURING TAKEOFF, DIVERTED TO ORF. REMOVED OIL FILTER AND FOUND CLOGGED FILTER, INSTALLED NEW OIL FILTER AND SECURED. PERFORMED ENGINE RUN UP WITH CREW. REMOVED OIL FILTER AND INSPECTED FOR CONTAMINENTS. NONE FOUND, REINSTALLED FILTER AND PERFORMED SECOND ENGINE RUN UP. LEAK CHECK GOOD. (M) 2L72 4F4 FRTA6WE E2EA 20050210000772005021000077WP 2005 2 10 GTIA040856 120041201A5311 FRAME DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23811NK 48017 DTW - FOUND 7 INCH CRACK ON STATION 1463 AT 8:00 POSITION A/C LEFT. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW SRM. (M) 2L72 4F A6WE 20050210000792005021000079EA 2005 2 10 A6WA200440216 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 FOUND RIGHT FS 484 AT RBL 36 ANGLE CRACKED. REPAIRED RIGHT FS 484 AT RBL 36 ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A. (M) 2L72 4F RTA21EA 20050210000802005021000080EU 2005 2 10 2005F00008 120041009A324020125112Y00 METERING VALVE AEROSPATR72 ATR72 EU BRAKE SYSTEM INOPERATIVE A TRBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO21545AT 545 DURING TAXI, CAPTAIN RIGHT BRAKE PEDAL INOPERATIVE. REPLACED BRAKE METERING VALVE. (M) 2H72 4T RT 20050210000812005021000081EU 2005 2 10 USAA041117 120041211A5347F5711056820400 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED .700 INCH LENGTH BY .650 INCH WIDE BY .033 INCH DEEP, CABIN FLOOR, Y450, FRAME 40.1 AND FRAME 40.2 CORROSION LEVEL 2, TASK NR J7-20-2578C. REMOVED AND REPLACED SEAT TRACK ASSY PER SRM 53-31-15, 51-42-11. (M) 2L72 4F RTA46NM 20050210000822005021000082NM 2005 2 10 GTIA040875 120041130A5230 SKIN DOUG MD80 MD83 3023681NM FUSELAGE DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND FORWARD CARGO DOOR HAS DENT ON LOWER EDGE OF SKIN APPROX .098 INCH DEEP 1.0 INCH DIAMETER. CUT OUT DAMAGED, DENTED SKIN. FABRICATED REPAIR DOUBLER AND FILLER, TREATED AND PRIMED FABRICATED PARTS AND INSTALLED REPAIR. (M) 2L72 4F RT 20050210000862005021000086NM 2005 2 10 ASAA0410635 120041130A5320656361512 CHANNEL BOEING737 7372X6C 1384552NM FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CHANNEL AND ANGLE (P/N 656361514) SUPPORT END IS BROKEN OFF AT RIVET HOLE. REMOVED, FABRICATED AND REPLACED CHANNEL AND ANGLE SUPPORT PER SRM. (M) 2L72 4F RTA16WE 20050210000892005021000089EA 2005 2 10 ASOA04957 120041130A5320601R3114525 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27879AS 7600 DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, RBL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 484, RBL 36 IAW ASA EO 600-53-0202. (M) 2L72 4F RTA21EA 20050210000902005021000090EA 2005 2 10 ASOA04973 120041206A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 NM02827AS 7212 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 LEFT IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20050210000912005021000091NM 2005 2 10 ASAA0410641 120041126A52306554935506 SKIN BOEING737 7372X6C 1384552NM CARGO DOOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE ON SKIN LAP, MAIN CARGO DOOR. REPAIRED PER EA 5230-01250. (M) 2L72 4F RTA16WE 20050210000922005021000092NM 2005 2 10 ASAA0410610 120041124A53306545767541 SKIN BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BTM OF MAIN CARGO DOOR CUTOUT, FUSELAGE STATION 398. REPAIRED PER EA 5330-01861. (M) 2L72 4F RTA16WE 20050210000932005021000093NM 2005 2 10 ASAA0410619 120041129A5311654531234 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FRAME. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050210000942005021000094NM 2005 2 10 ASAA0410620 120041130A532065479564 SILL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON UPPER SILL WEB AT STATION 794-847, INBOARD OF STRINGER 18R. REMOVED AND REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050210000972005021000097NM 2005 2 10 ASAA0410598 120041122A5330654577872 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DAMAGE ON SKIN. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050210000982005021000098EA 2005 2 10 ASOA04960 120041201A5210601R3198059 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27838AS 7276 DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M) 2L72 4F RTA21EA 20050210000992005021000099EA 2005 2 10 A6WA200440228 120041220A57307075T6 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 FOUND SCREW HOLE NEAR NACA SCOOP AT LT WS 148 ELONGATED TO .300 INCH. REPAIRED BY INSTALLING COUNTERSUNK FREEZE PLUG IN SKIN PANEL AND INNER STRINGER EO NR 601R-57-5753 REV A. (M) 2L72 4F RTA21EA 20050210001032005021000103NM 2005 2 10 ASAA0410640 120041126A52306554935506 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON SKIN LAP, MAIN CARGO DOOR. REPAIRED PER EA 5230-01250. (M) 2L72 4F RTA16WE 20050210001042005021000104NM 2005 2 10 ASAA0410602 120041122A53206550568503 SILL BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON MOPSILL, REPLACED. (M) 2L72 4F RTA16WE 20050210001052005021000105NM 2005 2 10 ASAA0410544 120041116A53106546595194 SHEAR TIE BOEING737 7372X6C 1384552NM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - SHEAR TIE AT STATION 727B AND STRINGER 18 GOUGED IN RADIUS. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT IAW SRM. (M) 2L72 4F RTA16WE 20050210001082005021000108NM 2005 2 10 ASAA040533 120041114A5313655162816 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND AFT PIT LEFT SIDE AT LBL 24 FROM BS 907-947 STRINGER IS CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM. (M) 2L72 4F RTA16WE 20050210001112005021000111EA 2005 2 10 A6WA200440230 120041221A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA LT WING DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 WHILE ACCOMPLISHING SB 601R-57-037, THE NR 18 HOLE AT WS 148 LT WAS FOUND TO BE ELONGATED TO .280 INCH. REPAIRED ELONGATED HOLE AT LT WS 148 BY INSTALLING FREEZE PLUG IAW BRAS REO 601R-57-5757. (M) 2L72 4F RTA21EA 20050210001122005021000112EU 2005 2 10 USAA041118 120041210A5347F5331140220001 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22412 0315 BFM - FOUND SEAT TRACK CORRODED, 1 INCH BY 1 INCH BY .026 INCH AREA, Y450 BETWEEN FRAME 48 AND 49. CORROSION LEVEL 2, TASK NR J7-200-2578C-023. REMOVED AND REPLACED SET TRACK PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050210001132005021000113EU 2005 2 10 USAA041120 120041210A5347F5711056820501 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK ASSY CORRODED .500 INCH LONG BY 1 INCH WIDE BY .037 INCH DEEP, CABIN FLOOR, Y-450 BETWEEN FRAME 40.1 AND 40.2. CORROSION LEVEL 2, TASK NR J7-200-2578C-013. REMOVED AND REPLACED SEAT TRACK PER SRM 53-31-15, FIG 101, SH 8, SRM 51-42-11. (M) 2L72 4F RTA46NM 20050210001142005021000114EU 2005 2 10 USAA041121 120041210A5347F5327584520000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .750 INCH LENGTH BY .500 INCH WIDE BY .051 INCH DEEP, CABIN FLOOR, Y-450, BETWEEN FRAME 36/37, TWO PLACES. CORROSION LEVEL 2, TASK JA-260-53500-001. REMOVED AND REPLACED PER SRM 53-00-15, FIG 101, SRM 51-74-00, 51-42-11. (M) 2L72 4F RTA46NM 20050210001162005021000116NM 2005 2 10 ASAA0410659 120041130A5320655496042 WEB BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, WEB CRACKED. REPLACED WEB. (M) 2L72 4F RTA16WE 20050210001172005021000117EU 2005 2 10 2005F00009 120041015A324310025111Y00 MASTER CYLINDER AEROSPATR72 ATR72 EU BRAKES INOPERATIVE A TRBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO21545AT 545 DURING TAXI, NO BRAKE PRESSURE ON CAPTAIN'S RIGHT BRAKE PEDAL. REPLACED BRAKE MASTER CYLINDER. (M) 2H72 4T RT 20050210001182005021000118 2005 2 10 GTIA040861 420041201A2565D29982113 SLIDE DOUG MD80 MD83 3023681NM L1 DOOR FAILED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND L1 DOOR SLIDE FAILED TO DEPLOY. REPLACED L1 DOOR SLIDE. (M) 2L72 4F RT 20050210001192005021000119 2005 2 10 GTIA040860 420041213A2565 LANYARD DOUG DC9 DC982 3022082WP ESCAPE SLIDE DISCONNECTED A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23820NK 0290 49126 DTW - FOUND L1 DOOR EVAC SLIDE DEPLOYMENT LANYARD DISCONNECTED FROM SLIDE ASSY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE. (M) 2L72 4F A6WE 20050210001212005021000121EA 2005 2 10 ASOA04946 120041129A5712 RIB CNDAIRCL600 CL6002B19 1900309EA RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING AN A-CHECK IN MCN, THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-195. THIS IS A TEMPORARY REPAIR IS VALID FOR 500 FLIGHT HOURS FROM THE TIME OF INCORPORATION AND IS TO BE INSPECTED AT EVERY SERVICE CHECK. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050210001292005021000129NM 2005 2 10 AMTA200401470 120041203A5330 SKIN BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE FUSELAGE DENTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11554TZ 32588 DENT RT FUSELAGE FS 661 AND S19R REQUIRES PERMANENT REPAIR (REF ERA). REPAIRED AREA IAW ERA. 2L72 4F4 FRTA2NM E12EU 20050210001312005021000131NM 2005 2 10 AWXA200500156 120041224A532065524572 PAN BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT LAVATORY SUB-FLOOR PAN BETWEEN BS 1016 AND BS 1031, LBL 2 AND LBL 17, WL 208. MAINTENANCE REMOVED CORRODED LT AFT LAVATORY SUB-FLOOR WEB AND STRAP; FABRICATED A NEW REPLACEMENT WEB AND STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050208001672005020800167WP 2005 2 8 DHL2004809504 120041227A5310 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 LT ACCESS DOOR JAMB NR 91B UPPER INTERNAL DOUBLER BROKEN 0.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-1 FIG 1. REMOVED BROKEN INTERNAL DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (AL2024-T3 0.063) IAW SRM 53-3-1 FIG 1 (SHEET 1, 5, 8). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW INTERNAL DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050208001822005020800182WP 2005 2 8 DHL2004873516 120041103A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LEFT OUTBOARD SLOT DOOR SKIN CRACKED 0.500, STA XS 478.897 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 21. REMOVED LEFT OUTBOARD SLOT DOOR SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (AL2024-T6 0.050) IAW SRM 57-3-3 FIG 21. CLEANED, TREATED AND PRIMED AREA AND SKIN INNER FACE IAW SRM 51-1-8B. INSTALLED NEW SKIN TO LEFT OUTBOARD SLOT DOOR IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050209000212005020900021NM 2005 2 9 2004UALA01209 120041212A2497 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT IDG DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29569UA C1377 26677 DIVERTED DUE TO LEFT 115V AC BUS VOLTAGE PULSATING. *S/D* REPLACED LEFT INTEGRATED DRIVE GENERATOR (IDG). SHOP FINDINGS: DAMAGED IDG CONNECTOR AND DAMAGED TERMINAL T2. 2L72 4F4 FRTA2NM E17NE 20050209000262005020900026WP 2005 2 9 DHL2004809512 120041230A5720 FAIRING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 RIGHT WING T/E FAIRING CRACKED 2.000 (STA XW -5.000 TO 5.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-22-04, DWG X32-R01, REV IR DATED 12-20-04, DWG 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2024-0-0.40) IAW DWG X32-R01 REV IR, DWG 5651221, SRM 51-1-4 PG 1, DACO DPS 3.69.4. HEAT TREATED IAW DACO DPS 7.00-1 REV -BJ-, SRM 51-1-1 PG 1-13-17. NDT INSPECTED IAW DC8 NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA AND NEW FAIRING IAW SRM 51-1-8B. INSTALLED NEW FAIRING IAW DWG X32-R01 REV IR, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050209000272005020900027WP 2005 2 9 DHL2004809502 120041221A57403645611U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 NR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED FWD BOOSTER PUMP BRACKET (NR 4 ALT TANK) IAW DC8 SRM 51-1-20D PG 21-9. 2L74 4F RT4A25 20050209000282005020900028WP 2005 2 9 DHL2004873532 120041129A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 RIGHT VERTICAL STABILIZER L/E LWR SKIN CORRODED, STA ZFS 80.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM RIGHT VERTICAL STABILIZER L/E LWR SKIN STA ZFS 80.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN 7075-T6 0.050 IAW SRM 55-5-1 PG 2. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF NEW SKIN IAW SRM 51-1-8B. INSTALLED NEW SKIN IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050209000292005020900029WP 2005 2 9 DHL2004873522 120041122A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 AFT CARGO COMPT FLOORBEAM FLANGE CORRODED AT STA FS 1360.000 LBL 47 TO LBL 50 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1G TR 53-124. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED REPAIR ANGLE (EXTRUSION 7075-T6511 0.120) IAW SRM 53-2-0 FIG 1G SHEET 1-2, SRM 53-7-3 FIG 10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1G SHEET 1-2, SRM 51-1-20D PG 9, SRM 51-1-15 PG 1. 2L74 4F RT4A25 20050209000302005020900030WP 2005 2 9 DHL2004873504 120041103A57403645612U BRACKET DOUG DC8 DC873F 302199FWP BOOST PUMP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 NR 4 ALT TANK AFT BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED CRACKED BRACKET ON NR 4 ALT TANK AFT BOOSTER PUMP IAW SRM 51-1-20D PG 9-21. 2L74 4F RT4A25 20050209000322005020900032WP 2005 2 9 DHL2004873505 120041101A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LT OUTER OUTBOARD WING L/E FORMER CRACKED 0.500 AT XFS 885.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050209000332005020900033WP 2005 2 9 DHL2004873520 120041126A57545769960501N DOOR DOUG DC8 DC873F 302199FWP LT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 LEFT INBOARD SLOT UPPER DOOR CRACKED 1.000. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050209000342005020900034WP 2005 2 9 DHL2004809503 120041227A5310 DOUBLER DOUG DC8 DC873F 302199FWP DOOR FRAME BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 RIGHT ACCESS DOOR JAMB NR 91D AFT INTERNAL DOUBLER BROKEN 0.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-3-1 FIG 1. REMOVED INTERNAL DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (AL2024-T3 0.063) IAW SRM 53-3-1 FIG 1 (SHEET 2, 5, 8). CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED INTERNAL DOUBLER IAW SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050209000352005020900035WP 2005 2 9 DHL2004873524 120041201A53215892159 FLOOR PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 MAIN CARGO COMPT FLOOR PANEL NR 3E CRACKED 10.000 AND CORRODED ON SEVERAL AREAS OF SKIN SURFACE (STA 1300.000-1582.000). REMOVED CRACKED FLOOR PANEL NR 3E IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SRM 51-1-8B. INSTALLED NEW FLOOR PANEL IAW SRM 51-3-0 PG 1. 2L74 4F RT4A25 20050210000092005021000009EU 2005 2 10 USAA041122 120041210A5320F5347823420100 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA1967OUW22412 315 BFM - FOUND FLOOR SUPPORT CORRODED .74 INCH BY .49 INCH BY .37 INCH AREA, -Y401 AT FRAME 75. REMOVED AND REPLACED SUPPORT PER SRM 53-41-14. CORROSION LEVEL 2, TASK NR J7-270-53500-013. (M) 2L72 4F RTA46NM 20050210000132005021000013EU 2005 2 10 A6WA200460066 120041230A21501344D000002 ACM BAG BAE146BAE146300A 1500267EU RIGHT ODOR A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31616AW E3145 NR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF VENT IN COCKPIT THEN SMOKE ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND AIR CYCLE MACHINE. (M) 2H74 4F RTA49EU 20050210000302005021000030EU 2005 2 10 USAA041130 120041213A5347F3311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED .031 INCH DEEP BY 4 INCH LENGTH BY 2 INCHES WIDE, FRAME 51, Y=450. REMOVED AND REPLACED PER SRM 53-31-15. CORROSION LEVEL 2, TASK NR J7-200-2578C-020. (M) 2L72 4F RTA46NM 20050210000352005021000035EU 2005 2 10 USAA041112 120041210A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 FOUND SEAT TRACK CORRODED .020 INCH DEEP BY 2 INCH WIDE BY .5 INCH LENGTH AREA, FRAME 41, Y=-450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578C-011. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2L72 4F RTA46NM 20050210000392005021000039NM 2005 2 10 ASAA0410539 120041116A53116549886173 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND CORROSION STATION 500 UNDER NUTPLATE AT STRINGER 27R INSIDE LONGERON CHANNEL. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A REPLACEMENT SECTION, ANGLE, AND CHANNEL IAW SRM. (M) 2L72 4F RTA16WE 20050210000432005021000043WP 2005 2 10 GTIA040869 120041221A2822 PUMP DOUG DC9 DC983 3022083WP FUEL BOOST INOPERATIVE A GTIAK NONE L NO TEST ININSP/MAINT 1 GL23826NK 49391 FLT 478 - DURING TEST ON RIGHT AFT BOOST PUMP B-TEST IS INOPERATIVE, AIRCRAFT SWAP. REMOVED AND REPLACED AFT FUEL TANK B-BOOST PUMP. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 20050210000562005021000056NM 2005 2 10 USAA040835 120041109A5347 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19650US 23902 CLT - FOUND SEAT TRACK CORRODED .5 INCH, STATION 808-816 RBL 88. REPLACED SEAT TRACK SECTION IAW SRM 53-50-52. (M) 2L72 4F RTA1NM 20050210000602005021000060EU 2005 2 10 2005F00005 120041016A7712311649902 TORQUE SENSOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE INOPERATIVE A TRBAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SO21348AE 349 127113 DURING TAKEOFF, LEFT ENGINE TORQUE INDICATOR NOT INCREASING. ABORTED TAKEOFF. REPLACED ENGINE TORQUE SENSOR. (M) 2H72 4T4 TRTA53EU E20NE 20050210000612005021000061EA 2005 2 10 A6WA200540004 120041229A5246 ACCESS DOOR CNDAIRCL600 CL6002B19 1900309EA LT WING FUEL CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .010 INCH DEEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M) 2L72 4F RTA21EA 20050210000622005021000062EU 2005 2 10 USAA041114 120041210A5347F57110568203 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .055 INCH DEEP BY .75 INCH WIDE BY .5 INCH LENGTH AREA, BETWEEN FRAME 42-43, Y=-450 SEAT TRACK. CORROSION LEVEL 2, TASK NR J7-200-2578C-001. BLENDED CORROSION, REPLACED SEAT TRACK PER SRM 51-74-00, 53-31-15 FIG 101 SHT 8, 51-42-11. (M) 2L72 4F RTA46NM 20050210000692005021000069EU 2005 2 10 2005F00006 120041016A215038650 HOSE AEROSPATR72 ATR72202 8680940EU HEAT EXCHANGER DAMAGED A TRBAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO21252AM 253 DURING LANDING, CAPTAIN REPORT SMOKE ON CABIN. REPLACED HEAT EXCHANGER HOSE. (M) 2H72 4T RTA53EU 20050210000832005021000083NM 2005 2 10 ASAA0410657 120041130A53106546948503 FAILSAFE BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND CORROSION ON FAIL/SAFE CHORD. REPLACED FAIL/SAFE CHORD. (M) 2L72 4F RTA16WE 20050210000842005021000084NM 2005 2 10 ASAA0410524 120041112A5313654688318 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01747AS 23124 OKC - FOUND AFT PIT STATION STRINGER RT IS CORRODED. REMOVED DAMAGED SECTION FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM. (M) 2L72 4F RTA16WE 20050210000852005021000085NM 2005 2 10 ASAA0410523 120041112A531565549055 FLOORBEAM BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01747AS 23124 OKC - FLOORBEAM HAS CORROSION ON TOP. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR T-CHORD, ANGLES, STRAPS AND FILLERS IAW EA. (M) 2L72 4F RTA16WE 20050210000882005021000088EA 2005 2 10 ASOA0467 120041204A5320601R3501163 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27827AS 7212 DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT SILL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT SILL PLATE. (M) 2L72 4F RTA21EA 20050210001072005021000107NM 2005 2 10 ASAA0410519 120041110A531165465461 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND FRAME CORRODED ALL AROUND NUTPLATES IN INTERIOR CAVITY. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM. (M) 2L72 4F RTA16WE 20050210001202005021000120EA 2005 2 10 ASOA04945 120041128A5210601R3198067 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27881AS 7496 DURING AN A CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050210001552005021000155WP 2005 2 10 DHL2004873523 120041122A5330 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ85619 46091 EXT FUSELAGE FWD CARGO COMPT FWD DOOR JAMB DOUBLER REPAIR INTERNAL PART CORRODED AT STA 320.000 L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-SHTHH FAA FORM 8110-3 DATED 11-11-2004 SB DC8 53078 REV 1 SR08530019 AD2004-06-06 DWG SEMAN ED3447-1. REMOVED CORRODED DOUBLER REPAIR, REPAIR AREA, FASTENERS IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (AL7075-T6 0.080) DOUBLER(AL7075-T6 0.090) TRIPLER (AL7075-T6 0.125) IAW DWG SEMAN ED3447-1, DWG SR08530019. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED CONICAL WASHERS IAW SRM 51-1-26. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG.1. INSTALLED FILLER, DOUBLER AND TRIPLER IAW DWG 2L74 4F RT4A25 20050210001582005021000158NE 2005 2 10 C8GA20040029 220041228A7261 ENGINE BOEING727 727223 1384074NM PWA JT8 JT8D15 52051NE NR 2 LEAKING A C8GAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO15715AA 22470 687453 FLT 202 FROM SVMI TO KMIA - ON CLIMB-OUT, NR 2 ENGINE OIL QUANTITY DECREASED. AT 1.8 GALLONS INDICATED, NOTICEABLE DECREASING INDICATION. RETURNED TO SVMI AND LANDED WITHOUT INCIDENT. FERRIED AIRCRAFT TO JAX AND CHANGED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050210001612005021000161NM 2005 2 10 WLDA2004100 120041103A5310AGA713317 SHEAR TIE DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 ITEM: DURING "C2" CHECK INSPECTION, FOUND SHEAR CLIP CORROSION AT STA 1953, STA 1959 AND STA 1975 BETWEEN L48L AND L52R. REMOVED THE CORROSION SHEAR CLIP AND INSTALLED NEW PARTS PER MD11 SRM VOL II 51-35-01. APLIED PROTECTION COATING. 2L73 4F RTA22WE 20050210001662005021000166NM 2005 2 10 AWXA200500099 120041228A5315654581292 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 328, FROM BL "0" TO RBL 53. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 328, FROM BL "0" TO RBL 53; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD PER DWG 65-45812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2L72 4F RTA16WE 20050210001722005021000172NM 2005 2 10 AWXA200500148 120041223A5240655287846 STRUCTURE BOEING737 7373Q8 1384670NM L2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION FOUND ON L-2 DOOR INNER CHORD (CREASE BEAM) AT LBL 48, BETWEEN BS 940 AND 996, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED INNER CHORD AT LBL 48, FROM BS 940 TO 996, WL 208 TO WL 209; FABRICATED A NEW REPLACEMENT INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050210001732005021000173NM 2005 2 10 AWXA200500149 120041224A5320654587545 SILL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHEC, EXFOLIATION CORROSION FOUND ON R-1 DOOR SILL INNER CHORD (CREASE BEAM) AT RBL 58, BETWEEN BS 298 AND 360, WL 208 AND WL 209. MAINTENANCE REMOVED DAMAGED INNER CHORD AT RBL 58, FROM BS 298 TO 360, WL 208 TO WL 209; FABRICATED A NEW REPLACEMENT INNER CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050210001742005021000174NM 2005 2 10 AWXA200500150 120041220A57536546434301 SKIN BOEING737 7373Q8 1384670NM TE FLAP DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, FOUND THE LT INBOARD FLAP DELAMINATED AT THE AFT OUTBOARD CORNER. MAINTENANCE REMOVED AND REPLACED THE LT INBOARD FLAP IAW T/C R3M27007. 2L72 4F RTA16WE 20050210001782005021000178NM 2005 2 10 DHL2005743504 120041216A5347606549 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3843038340 22438 MAIN CABIN RT SIDE LUGS OF I/B SEAT TRACK CORROSION BS 380-460. REMOVED CORROSION IAW B727 SRM 51-10-2. REMOVED .120 FROM ORIGINAL0.270 THICKNESS OF MATERIAL LEFT .150 FOUND OUT OF LIMITS IAW B727 SRM 51-10-01 FIG 3 SHEET 3. CALIPERS WJ-6181 DEC. 15,05. FAB NEW SEAT TRACK PO NR 0331976 P/N 60-6549 7178T6511 IAW B727 SRM 51-20-02. ALODINED AND PRIMED IAW B727 SRM 51-10-02. INSTALLED SEAT TRACK RBL 24.50 SAT. 340-440 IAW B727 SRM 51-30-02. 2L73 4F A3WE 20050211000012005021100001NM 2005 2 11 WLDA2004101 120041103A5313AGA7044508 LONGERON DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11279 48756 IDURING "C2" CHECK INSPECTION, FOUND CORROSION AT LONGERON 50R FROM STA 1884 TO STA 1975. REMOVED THE CORRODED LONGERON AND INSTALLED NEW PART PER MD11 SRM VOL II 51-33-01. APPLIED PROTECTIVE COATING. 2L73 4F RTA22WE 20050211000312005021100031NM 2005 2 11 AWXA200500131 120041222A53306545800 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, 2 EACH CRACKS WERE FOUND IN FUSELAGE SKIN AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT. MAINTENANCE CUTOUT DAMAGE IN OUTER FUSELAGE SKIN AND BEAR STRAP AT L-1 DOOR LOWER AFT CORNER CUTOUT BS 339, STR 17 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5311-05021-RC1. 2L72 4F RTA16WE 20050211000332005021100033NM 2005 2 11 AWXA200500133 120041227A53206548948501 CHANNEL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER 28 RT BETWEEN BS 353 AND BS 363. MAINTENANCE REMOVED STRINGER TIE CLIP AND CORRODED SECTION OF STRINGER 28 RT FROM BS 353 TO BS 363; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER AND TIE CLIP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000352005021100035NM 2005 2 11 AWXA200500135 120041221A53136546877136 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, A 1 INCH CRACK WAS FOUND IN RT WHEEL WELL STRINGER 18A AT BS 727. MAINTENANCE CUTOUT CRACK IN STRINGER 18A AT BS 727, FABRICATED 2 EACH FILLERS AND A GUSSET, INSTALLED REPAIR PARTS IAW ER 03-5300-05026-ES1. 2L72 4F RTA16WE 20050211000422005021100042NM 2005 2 11 AWXA200500105 120041227A531065465677 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 1006, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 1006, FROM STR 27 LT TO STR 27 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 65-46567; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000432005021100043NM 2005 2 11 AWXA200500106 120041224A53206546812175 FLOOR SUPPORT BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 38, BETWEEN BS 1007 AND BS 1014, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT LBL 38, FROM BS 1007 TO BS 1014; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050209001392005020900139NM 2005 2 9 DHL2005743509 120041229A5347606549 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH 22438 MAIN CABIN STA 360 BL 0 SEAT TRACK CORRODED (SEAT TRACK SECTION 360-500). REMOVED CORROSION IAW B727 SRM 53-10-1. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW B727 SRM 51-30-2. OBTAINED NEW SEAT TRACK PO 60-6549-0331976. LOCATE, DRILL, DEBURRED TRACK IAW B727 SRM 51-30-5. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050209001662005020900166WP 2005 2 9 DHL2004809513 120041230A5753 SKIN DOUG DC8 DC873F 302199FWP RT WING TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01809DH91189 46047 RT WING OUTBOARD FLAP FWD UPPER PLATING HAS INTERIM REPAIR, XF 211.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 12-28-04, DWG X32-R03 REV IR DATE 12-21-04. REMOVED PLATING WITH INTERIM REPAIR AND EXISTING INTERNAL SPLICE IAW DWG X32-R03, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01.001. FABRICATED NEW PLATING SEGMENT (AL2024-T3 0.040) INTERNAL SPLICE (AL2024-T3 0.050) IAW DWG X32-R03. CLEANED, TREATED AND PRIMED AREA AND INTERNAL SPLICE AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED INTERNAL SPLICE AND NEW PLATING SEGMENT. 2L74 4F RT4A25 20050210000052005021000005NM 2005 2 10 GTIA040863 120041202A5347 SEAT TRACK DOUG MD80 MD83 3023681NM FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23828NK 49823 FTW - FOUND CABIN FLOOR SEAT TRACK CORRODED AT STATION 200-237, RBL 22. REMOVED CORROSION AND SECTION OF TRACK AT STATION 200-237, FABRICATED SECTION OF SEAT TRACK, TREATED, PRIMED AND TOPCOATED, OK TO INSTALL. (M) 2L72 4F RT 20050210000122005021000012EA 2005 2 10 A6WA200540005 120041229A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 FOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 163 HAS MINOR FRETTING ON FAYING SURFACE. LESS THAN .008 INCH DEEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M) 2L72 4F RTA21EA 20050210000252005021000025NM 2005 2 10 USAA041110 120041228A5330 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19300AU53844 23228 CLT - FOUND SKIN CRACKED 3 INCHES, S-19R AT STATION 767. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050210000292005021000029NM 2005 2 10 USAA041078 120041220A5230 SKIN BOEING767 767201 1385125NM CARGO DOOR GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19649US70070 23901 CLT - FOUND CARGO DOOR SKIN GOUGED .250 INCH, LOWER INNER LIP OF FORWARD CARGO DOOR SKIN, 16 INCHES FROM AFT EDGE. ACCOMPLISHED DOUBLER REPAIR PER EA 96113. (M) 2L72 4F RTA1NM 20050210000552005021000055NM 2005 2 10 USAA041064 120041215A5230 SKIN BOEING757 7572B7 1384964NM CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19611AU39875 27123 CLT - FOUND INNER SKIN CRACKED .250 INCH, AFT CARGO DOOR 6 INCHES FROM FORWARD EDGE. INSTALLED DOUBLER. (M) 2L72 4F RTA2NM 20050210000672005021000067EA 2005 2 10 A6WA200440218 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 FOUND LEFT FS 625 OBLIQUE ANGLE CRACKED. REPLACED ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-06. (M) 2L72 4F RTA21EA 20050210000782005021000078NM 2005 2 10 ASAA0410543 120041116A533065458001 SKIN BOEING737 7372X6C 1384552NM FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND STATION 188 STRINGER 17L HAS LIGHTING STRIKE DAMAGE THAT IS OUT OF LIMITS IAW SRM. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLERS AND TRIPLER IAW SRM. (M) 2L72 4F RTA16WE 20050210001002005021000100NM 2005 2 10 ASAA0410637 120041130A53206545815513 BRACKET BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND T-BRACKET HAS ELONGATED HOLES AT STATION 344. REMOVED, FABRICATED AND INSTALLED T-BRACKET PER SRM. (M) 2L72 4F RTA16WE 20050210001022005021000102NM 2005 2 10 ASAA0410609 120041124A5330 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, DAMAGE ON SKIN A LAP. REPAIRED PER EA 5330-01835. (M) 2L72 4F RTA16WE 20050210001152005021000115NM 2005 2 10 ASAA0410658 120041130A53106550568 DOOR FRAME BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, ELONGATED HOLES IN WEB. REPLACED WEB. (M) 2L72 4F RTA16WE 20050210001522005021000152NM 2005 2 10 C8GA20040027 120041222A7921749965 OIL COOLER BOEING727 727200 138407ENM NR 2 ENGINE INOPERATIVE A C8GAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO15713AA22649 22469 FLT 707 FROM MCI TO TOL, IN CRUISE, NR 2 ENGINE OIL TEMPERATURE INCREASED TO 150 DEG C FOR 14 MINUTES. OIL PRESSURE AT 42 PSI AND FLUCTUATED. SHUT DOWN NR 2 ENGINE AS A PRECAUTION. AIRCRAFT CONTINUED TO TOL AND LANDED WITHOUT INCIDENT. FOUND NR 2 FUEL/OIL COOLER INOPERATIVE. REPLACED FUEL/OIL COOLER. ALSO CHANGED MAIN OIL FILTER AS A PRECAUTION. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F RTA3WE 20050210001672005021000167NM 2005 2 10 AWXA200500100 120041228A53206545805121 INTERCOSTAL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF INTERCOSTAL UPPER LEG AT BS 270, BETWEEN LBL 7 AND RBL 1. MAINTENANCE CUTOUT DAMAGE IN INTERCOSTAL UPPER LEG AT BS 270, FROM LBL 7 TO RBL 1; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050211000372005021100037NM 2005 2 11 AWXA200500137 120041224A532065479577 WEB BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND IN 3 PLACES ON INBOARD SIDE OF WEB BETWEEN BS 847 AND BS 867, RBL 17.50. MAINTENANCE REMOVED CORRODED SECTION OF WEB FROM BS 847 TO BS 867, RBL 17.50; FABRICATED A NEW REPLACEMENT SECTION OF WEB PER DWG 65-47957; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000412005021100041NM 2005 2 11 AWXA200500104 120041223A531565C10592160 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 956, BETWEEN RBL 26 AND RBL 40, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 956, FROM RBL 26 TO RBL 40; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65C10592; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000722005021100072NM 2005 2 11 AWXA200500107 120041223A531565498842 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 967, BETWEEN LBL 50 AND RBL 38, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 967, FROM LBL 50 TO RBL 38; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW ER 03-5310-05007-RC1. 2L72 4F RTA16WE 20050211000732005021100073NM 2005 2 11 AWXA200500108 120041224A53206546812189 FLOOR SUPPORT BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT AT RBL 38, BETWEEN BS 997 AND BS 1004, WL 208. MAINTENANCE CUTOUT DAMAGE ON FLOOR SUPPORT AT RBL 38, FROM BS 997 TO BS 1004; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-12. 2L72 4F RTA16WE 20050211000752005021100075NM 2005 2 11 AWXA200500110 120041224A5320654681282 WEB BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT OUTBOARD WEB, BETWEEN BS 995 AND BS 1012, RBL 39 AND RBL 44, WL 208. MAINTENANCE REMOVED CORRODED RT AFT OUTBOARD WEB, FROM BS 995 TO BS 1012, RBL 39 TO RBL 44; FABRICATED A NEW REPLACEMENT WEB PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000762005021100076NM 2005 2 11 AWXA200500111 120041223A53206546812198 FLOOR SUPPORT BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT LBL 18, BETWEEN BS 979 AND BS 983, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT LBL 18, FROM BS 979 TO BS 983; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000772005021100077NM 2005 2 11 AWXA200500112 120041223A53206546812169 FLOOR SUPPORT BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT RBL 18, BETWEEN BS 969 AND BS 984, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT RBL 18, FROM BS 969 TO BS 984; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-46812; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000812005021100081NM 2005 2 11 AWXA200500116 120041228A53206545834256 FLOOR SUPPORT BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 324, RBL 10, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT BS 324, RBL 10; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 12. 2L72 4F RTA16WE 20050211000822005021100082NM 2005 2 11 AWXA200500117 120041228A53206546568519 STIFFENER BOEING737 7373Q8 1384670NM BULKHEAD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL REPAIR ANGLE AT BS 1022, LBL 0.5, WL 195. MAINTENANCE REMOVED CORRODED PREVIOUS REPAIR ON AFT PRESSURE BULKEAD FORWARD FACE STIFFENER CHANNEL AT BS 1022, LBL 0.5; FABRICATED 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11. 2L72 4F RTA16WE 20050211000872005021100087 2005 2 11 AWXA200500119 420041228A256565C1612162 ATTACH BRACKET BOEING737 7373Q8 1384670NM GIRT BAR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58. MAINTENANCE REMOVED CORRODED L-1 DOOR AFT GIRT BAR ATTACH BRACKET AT BS 344 LBL 58; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000882005021100088NM 2005 2 11 AWXA200500120 120041224A5320654681233 STRAP BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CENTER FLOOR STRAP BETWEEN BS 1012 AND BS 1027, LBL 6 AND RBL 6. MAINTENANCE REMOVED CORRODED AFT CENTER FLOOR STRAP FROM BS 1012 TO BS 1027, LBL 6 TO RBL 6; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050211000922005021100092NM 2005 2 11 AWXA200500124 120041224A532065524571 PAN BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT LAVATORY SUB-FLOOR PAN BETWEEN BS 1017 AND BS 1025, RBL 1 AND RBL 35, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY SUB-FLOOR WEB AND STRAP; FABRICATED A NEW REPLACEMENT WEB AND STRAP; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050214000102005021400010EA 2005 2 14 MASA200400738 120041231A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A MASAK NONE O OTHER ININSP/MAINT 1 SW07650ML 7137 THE CREW REPORTED A CEILING EMERGENCY LIGHT INOPERATIVE. THE ITEM WAS PLACED ON MEL. 1/3/05 MAINTENANCE RELAMPED, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050214000292005021400029CE 2005 2 14 MALA040932 120041123A5311 FRAME BEECH 95 B95 1153404CE FUSELAGE GOUGED A MALAK NONE O OTHER ININSP/MAINT 1 GL155320 TD452 DURING INSPECTION, LT SIDE FUSELAGE GOUGED BETWEEN FRAMES 18 & 19 ON LAP -C-, STRINGER 24. MAINTENANCE REPAIRED REFER TO 409 CARD 226160, AND EO A53234 FOR ADDITONAL INFORMATION. 1L72 3O 3A16 20050214000312005021400031EU 2005 2 14 MALA040934 120040804A3350549132106 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15424XJ 340B424 EMERGENCY POWER SUPPLY P/N 601-1713-02, S/N 1603 PAPS CIRCUIT BREAKER. MAINTENANCE REPLACED BOTH BATTERY PACKS P/N 549-1321-06 AND PCB P/N 542-2616-06. UNIT PASSES CMM CHECKS RETURNED TO SERVICE 12/9/04. 2L72 4T RTA52EU 20050214000322005021400032EU 2005 2 14 MALA040935 120041110A33506013211 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT SMOKE A MALAK NONE O OTHER ININSP/MAINT 1 GL15363PX 340B260 BATTERY ASSEMBLY 60-1321-1 S/N 19113 STARTED SMOKING UPON INSTALLATION BATTERY FOUND AT FAULT. CLEANED & BENCH CHECKED GOOD IAW CMM. RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050214000332005021400033EU 2005 2 14 MALA040937 120041201A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 BATTERY POWER SUPPLY P/N 330151, S/N 1318 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSY. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 12/2/04. 2L72 4T RTA52EU 20050427000012005042700001EU 2005 4 27 AC2A099711 120041101A641010515150 BLADE BOLKMS105 BO105S 5626006EU TAIL ROTOR CRACKED E AC2AO OTHER O OTHER CRCRUISE 1 SO078776 7431 776 THE PILOT REPORTED PICKING UP A MAIN ROTOR VIBRATION IN FLIGHT AND WAS INSTRUCTED BY FIELD BASE MAINTENANCE PERSONNEL TO RETURN TO BASE. MAIN ROTOR BLADE WAS FOUND TO BE CRACKED NEAR CUFF ON LOWER SIDE. BLADE WAS REPLACED. 1G72 3U H3EU 20050214000532005021400053EU 2005 2 14 MALA040939 120041209A3350 FUSE SAAB SF340 340B 7860101EU POWER SUPPLY BLOWN A MALAK NONE L NO TEST ININSP/MAINT 1 GL15445XJ 340B445 DURING SCHEDULED CAPACITY CHECK, BATTERY POWER SUPPLY P/N 3301-51, S/N 2170 HAS BLOWN FUSE. MAINTENANCE REPLACED FUSE P/N 779 -435-72, UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 12/23/04. 2L72 4T RTA52EU 20050214000552005021400055EU 2005 2 14 MALA040930 120041102A5712 RIB SAAB SF340 340B 7860101EU LT WING LE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15454XJ 340B454 LEFT O/B LEADING EDGE HAS 2 CRACKED RIBS. RIBS WERE REPAIRED IAW MESABA EO S57026. 2L72 4T RTA52EU 20050214000562005021400056EU 2005 2 14 MALA040931 120041119A3350 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445XJ 340B445 DURING FUNCTIONAL TEST OF EMERGENCY BATTERY CAPACITY CHECK, BATTERY 20LN FAILED. 2L72 4T RTA52EU 20050214000572005021400057EU 2005 2 14 MALA040936 120041201A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15411XJ 340B411 DURING CAPACITY CHECK BATTERY POWER SUPPLY P/N 3301-51, S/N 1357 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-51 & UNIT PASSES CAPACITY CHECKS. A/C RETURNED TO SERVICE 12/2/04. 2L72 4T RTA52EU 20050214000582005021400058EU 2005 2 14 MALA040947 120041211A33506113211 RELAY SAAB SF340 340B 7860101EU EMERGNECY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15365PX 340B265 BATTERY POWER SUPPLY P/N 61-1321-1, S/N OFF 18522 REPORTED TO NEED BENCH CHECK. MAINTENANCE FOUND WHITE ARM SWITCH ON LIGHT DOES NOT LIGHT. MAINTENANCE REPLACED C4, C5, Q1, Q5 AND SCR1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 1/21/04. 2L72 4T RTA52EU 20050214000592005021400059EU 2005 2 14 MALA040940 120041209A33506104789 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15360PX 340B220 BATTERY PACK P/N 61-0478-9, S/N 010 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050214000612005021400061EU 2005 2 14 MALA040941 120041207A3350 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15434XJ 340B434 BATTERY PACK P/N 3301-51, S/N 2088 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 3301-31 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/9/04. 2L72 4T RTA52EU 20050214000632005021400063EU 2005 2 14 MALA040943 120041209A33506104789 BATTERY SAAB SF340 SF340A 7850100EU FUSELAGE FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 BATTERY POWER SUPPLY P/N 61-0478-9, S/N ELB150 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 55-2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/20/04. 2L72 4T RTA52EU 20050214000652005021400065EU 2005 2 14 MALA040946 120041211A33506104789 BATTERY PACK SAAB SF340 SF340A 7850100EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15106XJ 340A106 BATTERY PACK P/N 61-0478-9, S/N ELB149 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED & PASSES CMM CHECKS, RETURNED TO SERVICE 12/20/2004. 2L72 4T RTA52EU 20050210000542005021000054EU 2005 2 10 USAA041124 120041216A5320F5347824120000 FLOOR SUPPORT AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 FOUND FLOOR SUPPORT CORRODED 1 INCH LONG BY 1 INCH WIDE BY .040 INCH DEEP, Y1107 AT FRAME 74. CORROSION LEVEL 2, TASK NR J7-270-53500. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-74-00, 51-42-11, 51-21-11. (M) 2L72 4F RTA46NM 20050210000582005021000058EU 2005 2 10 USAA041102 120041211A5321F5367273600600 FLOOR PANEL AIRBUS330 A330323 3930335EU FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND FLOOR PANEL DELAMINATED, SEVERAL AREAS GREATER THAN 10 PERCENT OF PANEL, MAIN CABIN FLOOR PANEL 241BF. FABRICATED NEW PANEL PER SAMPLE, AND SRM 53-002-00. (M) 2L72 4F RTA46NM 20050210000702005021000070WP 2005 2 10 GTIA040868 120041220A3213 PACKING DOUG DC9 DC983 3022083WP RT MLG STRUT LEAKING A GTIAK NONE K FLUID LOSS ININSP/MAINT 1 GL23832NK 49618 DTW - FLT 503 - DURING PREFLIGHT, FOUND HYDRAULIC FLUID ON RT MLG, AIRCRAFT SWAP. RE-PACKED RT MAIN GEAR STRUT, LEAK CHECK GOOD. (M) 2L72 4F RTA6WE 20050210000732005021000073 2005 2 10 2005F00007 420041215A2565 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE MISROUTED A GTIAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23808NK 49504 DTW - FOUND R1 DOOR SLIDE PULL HANDLE, INSPECT PULL HANDLE ROUTING. INSPECTED AND CORRECTED PULL LANYARD ON R1 DOOR SLIDE. NO OTHER DEFECTS NOTED. (M) 2L72 4F RTA6WE 20050210000872005021000087NM 2005 2 10 ASAA0410618 120041126A5330655258814 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, FOUND DAMAGE ON EXTERNAL SKIN AT BS 907, STRINGER 14L. REPAIRED PER EA 5330-01846. (M) 2L72 4F RTA16WE 20050210000952005021000095NM 2005 2 10 ASAA0410633 120041129A5310654581234 SHEAR TIE BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND DURING D-CHECK, CORROSION ON SHEAR TIE AT STATION 328. REPAIRED SHEAR TIE PER SRM. (M) 2L72 4F RTA16WE 20050210000962005021000096NM 2005 2 10 ASAA0410603 120041122A532065565551 WEB BOEING737 7372X6C 1384552NM DOOR FRAME CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FOUND CORROSION AT AFT CARGO DOOR CUTOUT FOWARD FRAME CLOSEOUT PANEL FASTENER HOLES. REPLACED AFT CARGO DOOR CLOSEOUT WEB. (M) 2L72 4F RTA16WE 20050210001012005021000101NM 2005 2 10 ASAA0410608 120041124A53306545772155 SKIN BOEING737 7372X6C 1384552NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DURING D-CHECK, DAMAGE ON SKIN AT LAP. REPAIRED PER EA 5330-01835. (M) 2L72 4F RTA16WE 20050210001062005021000106NM 2005 2 10 ASAA0410540 120041116A53136549886148 STRINGER BOEING737 7372X6C 1384552NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC - FOUND CORROSION UNDER AND AROUND NUTPLATES, STRINGER 27L INSIDE STRINGER CHANNEL STATION 500. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION, REPAIR ANGLE AND INSTALLED A REPLACEMENT STRINGER CLIP IAW DRAWING 69-35352. (M) 2L72 4F RTA16WE 20050210001602005021000160NE 2005 2 10 C8GA20040028 220041223A7200 ENGINE BOEING727 7272A1 138407FNM PWA JT8 JT8D17 52049NE NR 3 FLAMED OUT A C8GAK NONE X ENGINE FLAMEOUT LDLANDING 1 SO15287SC 21345 707922 FLT 725 FROM PHL TO TOL, AFTER LANDING, WHILE ON ROLL-OUT, NR 3 ENGINE FLAME OUT OCCURRED. AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION. ICING CONDITIONS WERE NOTED BUT NO ICE INGESTION WAS EVIDENT. NO DAMAGE WAS NOTED IN ENGINE INTAKE OR EXHAUST. PERFORMED ENGINE RUN TO TAKEOFF POWER AND DRAINED P4 MOISTURE TRAP AS A PRECAUTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050210001792005021000179NM 2005 2 10 DHL2005743502 120041215A5347606549 SEAT TRACK BOEING727 727225 1384077NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01743DH3843038430 22438 MAIN CABIN LEFT SIDE, CENTER OF I/B SEAT TRACK CORROSION BS 720E. REMOVED CORROSION. REMOVED .065 ORIG THICKNESS .485 REMAINING MAT`L. FOUND OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK MAT`L. ID 60-6549 7128T6511 PO NR 0331976 IAW SRM B727 53-10-2. FAB MAT`L, HOLES DRILLED, COUNTERSUNK, DEBURRED IAW B727 SRM 51-20-2 FIG 1. ALODINED AND PRIMED IAW B727 SRM 51-10-2. SEAT TRACK INSTALLED IAW B727 SRM 53-10-2. 2L73 4F A3WE 20050211000322005021100032NM 2005 2 11 AWXA200500132 120041227A53306545800219 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF LOWER SKIN AT BS 358, ON INBOARD AND OUTBOARD SIDE OF STR 27 LT. MAINTENANCE CUTOUT CORRODED SECTION OF SKIN AT BS 358, STR 27 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER, INSTALLED REPAIR PARTS IAW ER 03-5300-05022-ES1. 2L72 4F RTA16WE 20050211000362005021100036NM 2005 2 11 AWXA200500136 120041220A3397BR96359007 WIRE HARNESS BOEING737 7373Q8 1384670NM ZONE 200 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - EEL - DURING C-17 CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT HARNESS DAMAGED. MAINTENANCE REPLACED NUMEROUS SPLICES IN THE EMERGENCY ESCAPE PATH LIGHT HARNESS, OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD. 2L72 4F RTA16WE 20050211000402005021100040NM 2005 2 11 AWXA200500103 120041224A53156546568121 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN LBL 4 AND LBL 34, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 1016, FROM LBL 4 TO LBL 34; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG 202. 2L72 4F RTA16WE 20050211000742005021100074NM 2005 2 11 AWXA200500109 120041223A5315654681138 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 986, BETWEEN LBL 45 AND RBL 45, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD AT BS 986, FROM LBL 45 TO RBL 45; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW E.R. 03-5310-05007-RC2. 2L72 4F RTA16WE 20050211000792005021100079NM 2005 2 11 AWXA200500114 120041224A53156546811 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 1016, BETWEEN RBL 4 AND RBL 34, WL 208. MAINTENANCE CUTOUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 1016, FROM RBL 4 TO RBL 34; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD, 2 EACH SUPPORT ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-51, FIG 203. 2L72 4F RTA16WE 20050211000892005021100089NM 2005 2 11 AWXA200500121 120041221A5313654577627 STRINGER BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT BETWEEN BS 1006 AND BS 1009. MAINTENANCE REMOVED CORRODED STRINGER 27 LT FROM BS 978 TO BS 1016; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, A REPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201. 2L72 4F RTA16WE 20050211000902005021100090NM 2005 2 11 AWXA200500122 120041227A532069489551 ANGLE BOEING737 7373Q8 1384670NM FUSLEAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON INTERCOSTAL ATTACH ANGLE AT BS 357, OUTBOARD OF STRINGER 28 LT. MAINTENANCE REMOVED CORRODED INTERCOSTAL ATTACH ANGLE AT BS 357, STR 28 LT; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2L72 4F RTA16WE 20050214000452005021400045EU 2005 2 14 MALA040938 120041203A3350330151 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 BATTERY POWER SUPPLY P/N 3301-51, S/N 2208 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31, A/C WAS RETURNED TO SERVICE 12/3/04. 2L72 4T RTA52EU 20050214000622005021400062EU 2005 2 14 MALA040942 120041209A33506122751 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15517XJ E2335 BATTERY PACK P/N 61-2275-1, S/N 9908129 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 61-2274-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2H74 4F RTA49EU 20050214000642005021400064EU 2005 2 14 MALA040944 120041210A33505521981 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15369PX 340B295 BATTERY PACK P/N 61-0478-9, S/N 1929 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 55-2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050215000122005021500012NE 2005 2 15 S2YA04039 220041015A7230 COMPRESSOR DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ENGINE DAMAGED A S2YAB EMER. DESCENT E VIBRATION/BUFFET CRCRUISE 1 GL13359SK8588 2261 3202 PCECD0018 DURING FLIGHT, CREW REPORTED A LOAD BANG FROM AFT OF THE FLIGHT DECK FOLLOWED BY A FAINT SMELL OF SMOKE. THEY DONNED OXYGEN MASKS AND REQUESTED PRIORITY, BUT DID NOT SHUTDOWN THE ENGINE OR DECLARE AN EMERGENCY. THE CREW PERFORMED AN UNEVENTFUL LANDING. MX INSPECTED THE ENGINE AND FOUND THE NR 2 COMPRESSOR FAN HAD ONE BLADE THAT APPEARED TO HAVE LOST AND SECTION OF ITS LEADING EDGE AND 3 OTHER BLADES WERE DAMAGED. FANS AFT OF THE NR 2 COMPRESSOR HAD SEVERAL DAMAGED BLADES MOSTLY LIKELY FROM THOSE PIECES GOING THROUGH THE ENGINE. THE ENGINE WAS REMOVED AND SENT TO MFG FOR SERVICE.(K) 2H72 4T4 FRTA55NM E35NE 20050215000132005021500013NM 2005 2 15 USAA041069 120041202A5320 INTERCOSTAL BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 PIT- Q5- INTERCOSTAL, 2 INCH CRACK, IN RADIUS- FLOOR INTERCOSTAL, STA 380, BBL 0. REPLACED SUPPORT ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050215000142005021500014EU 2005 2 15 USAA041086 120041212A5310D5347217220390 BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 CHECK - BEAM, 2.0 INCH X 1.2 INCH X 0.049 INCH AREA, CORROSION; LEVEL 2; TASK NR JA 260-53500, MAIN CABIN FLOOR BTW FR 66-68, BI - Y1292. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215000202005021500020CE 2005 2 15 UG82005F00000 120041224A32336600264003 ACTUATOR LEAR 60 60LEAR 5170707CE NLG DEFECTIVE E UG8AO OTHER J WARNING INDICATION APAPPROACH 1 GL23699DA129 237 237 LT MAIN UNSAFE INDICATION, RAN ALT GEAR EXT CHECKLIST. ENDED UP WITH LT MAIN AND NOSE GEAR UNSAFE INDICATION ADN FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. FLIGHT CREW DID A BLOW DOWN CYCLE OF THE LANDING GEAR TO SEE IF THAT WOULD CLEAR THE INDICATION. IT DID NOT. LT MAIN GEAR ACTUATOR AND DOWN AND LOCKED SWITCH (PN P624007) WERE REPLACED IAW MFG. MAINT CHECKS WERE CARRIED OUT IAW MM, NO FURTHER DEFECTS NOTED. AC WAS RETURNED TO SERVICE. (PA-04-004 CNTRL NR) (K) 2L72 4F RTA10CE 20050215000232005021500023SO 2005 2 15 SIMA200435815 120041218A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 DURING INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200501979) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000292005021500029SO 2005 2 15 SIMA200435811 120041219A532114522461011 DOUBLER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN FLOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR DOUBLERS HAVE CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR DOUBLERS IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000302005021500030SO 2005 2 15 SIMA200435813 120041218A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21739AE 145402 DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT BELLEY FAIRING CUTOUT. BLENDED THE CHAFED AREA. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DONE IAW SRM. (SW21200501981) (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000312005021500031NM 2005 2 15 S2YA04006 120040303A3231001A322A1500 ROD DORNERDO32 DO328300 NM PWA 306 PW306B NE NLG DOOR BROKEN A S2YAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL13353SK 3122 SHORTLY AFTER TAKEOFF, THE CREW REPORTED A LOUD THUMPING FROM BELOW THE COCKPIT. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MX FOUND THE LT FORWARD NOSE LANDING GEAR DOOR HANGING LOOSE. THE SHEAR ROD HAD BROKEN. MX REPLACED THE ROD ASSEMBLY AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS.(K) 2H72 4T4 FRTA55NM E35NE 20050215000332005021500033SO 2005 2 15 SIMA200434202 120041205A2612K0323 RELAY EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 2 FIRE DETECTINOPERATIVE A SIMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW21803AE 145483 ICE CONDITION ANTI-ICE WARNING. ENGINE 2, FIRE DETECTION FAIL EICAS MESSAGE. REPLACED AIR GROUND RELAY AT LT RELAY SUPPORT B14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.(K) 2L72 4F4 FRTT00011ATTE6CH 20050215000342005021500034EA 2005 2 15 SIMA200433601 120041127A335020131A BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21519AE 10131 DURING PREFLIGHT CHECK SOME OF THE EMERGENCY LIGHTS WOULD NOT COME ON. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY POWER SUPPLY BATTERY PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501341) 2L72 4F4 FRTA21EA EOOO63EN 20050215000362005021500036EA 2005 2 15 GIC2005F00000 220041018A74144370 MAGNETO PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA RIGHT BROKEN D GICSA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 NM01535971284 2842166 L1967139A ACFT WAS BEING USED FOR TRAINING, THE PILOT STATED THAT (SUDDENLY THE ENG LOST 3500 RPM. THE PILOT TRIED CARBURETOR HEAT AND CHANGED THE FUEL SELECTOR TO THE OPPOSITE TANK. BOTH OF THESE PRODUCED NO CHANGE. THE PILOT THEN MADE A PRECAUTIONARY LANDING. AFTER LANDING, HE TRIED PERFORMING A MAGNETO CHECK. WHEN MAG SWITCH WAS PLACED IN RT POSITION, ENGINE DIED. MAINT TROUBLESHOT, REMOVED RT MAG. UPON DISASSEMBLY OF MAG, ROTOR ASSY (M3548) WAS FOUND BROKEN OFF AT THE BASE OF MACHINED FORK (INTERNAL TO MAG), PLASTIC DISTRIBUTOR DRIVE GEAR (M3827) WITH BOTH PIECES OF FORK WERE FLOATING AROUND INSIDE THE MAGNETO. NO OTHER DISCREPANCIES WERE NOTED WITH MAGNETO. NO VISIBLE CLUES WHICH LEAD TO FAILURE. (K) 1L71 3O3 O 2A13 E274 20050215000422005021500042NM 2005 2 15 USAA041068 120041202A5330 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU STA500C+19IB STRCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5- SKIN, 1.25 INCH, CORROSION, LEVEL 1; TASK NR C53-208-01, STA 500C + 19 INCH IB OF STR 28L. REMOVED CORROSION IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050215000462005021500046EU 2005 2 15 USAA041081 120041213A5321D5361060500100 FLOOR PANEL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - Q1 - PANEL, 0.500 INCH X 2.0 INCH X 0.060 INCH AREA, CORROSION; NO LEVEL OR TASK; MAIN CABIN FLOOR PANEL 222FF. REMOVED AND REPLACED PANEL IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215000482005021500048NM 2005 2 15 S2YA04012 120040430A261244TS08Y01 CONTROL PANEL DORNERDO32 DO328300 NM PWA 306 PW306B NE RT FIRE DETECT FALSE INDICATIONA S2YAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL13352SK 3111 DURING FLIGHT, THE CREW NOTED A FIRE INDICATION FOR THE RT ENGINE. THE CREW SHUT THE RT ENGINE DOWN IN FLIGHT AND MADE AN SUCCESSFUL SINGLE ENGINE LANDING. MX INSPECTED THE AC AND FOUND NO INIDCATION OF FIRE. MX SWAPPED FIRE EXTINGUISHER/APU PANELS. MX RETURNED BOTH AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050211000302005021100030NM 2005 2 11 AWXA200500130 120041221A53306573736518 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF BELLY SKIN BETWEEN BS 1001 AND BS 1011, STR 26 LT AND STR 27 RT. MAINTENANCE REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS FROM BS 1004 TO BS 1011. REMOVED CORRODED SECTION OF SKIN FROM FROM BS 1004 TO BS 1011, STR 26 LT TO STR 27 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIR PARTS IAW ER 03-5300-05022-ES2. 2L72 4F RTA16WE 20050211000782005021100078NM 2005 2 11 AWXA200500113 120041227A5311694820417 FRAME BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SIDE OF FRAME AT BS 360, BETWEEN STR 27 LT AND STR 28 LT. MAINTENANCE REMOVED SHEAR TIE AND CUTOUT DAMAGE IN FRAME FOOT AT BS 360, BETWEEN STR 27 LT AND STR 28 LT; FABRICATED A NEW REPLACEMENT SHEAR TIE AND FRAME FOOT PER DWG 69-58280; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG. 210. 2L72 4F RTA16WE 20050211001012005021100101NM 2005 2 11 AWXA200500125 120041224A533065457721044 PANEL BOEING737 7373Q8 1384670NM FUSELAGE CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK FOUND THE DORSAL FIN DOUBLER ON TOP OF FUSELAGE CHAFED IN 2 PLACES BETWEEN BS 857 AND BS 907, STR 2 LT AND STR 2 RT. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN ON TOP OF FUSELAGE FROM BS 857 TO BS 907, STR 2 LT TO STR 2 RT; FABRICATED 3 FILLERS, A STRAP, A DOUBLER, AND A TRIPLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-01, FIG 209. 2L72 4F RTA16WE 20050214000272005021400027NE 2005 2 14 IXXA0400122O 220041221A7320 GASKET DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ENGINE LEAKING A IXXAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW11828BX311842600 45993 692264 DURING TAKEOFF ROLL NR 2 ENGINE GOT TO ABOUT 78 PERCENT N1 AND BEGAN TO ROLL BACK. AFTER THE TAKEOFF WAS ABORTED THE ENGINE CONTINUED TO ROLLBACK BELOW IDLE RPM. ENGINE WAS SHUTDOWN AT THAT POINT. EGT WAS NORMAL, FUEL FLOW WAS FLUCUATING BETWEEN -0- AND -1000- PPH. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED FUEL FLOW TRANSMITTER GASKET. OPERATIONAL AND LEAK CHECK WERE GOOD PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20050214000302005021400030EU 2005 2 14 MALA040933 120040508A33506104789 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT SMOKE A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL15367PX 340B271 BATTERY PACK P/N 61-0478-9, S/N 19881 STARTED SMOKING WHEN INSTALLED INTO POWER SUPPLY. MAINTENANCE REPLACED BATTERY PACK P/N 55-2198-1. UNIT PASSED CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050214000432005021400043EU 2005 2 14 PNSA041204 120041230A5100 UNKNOWN SAAB SF340 340B 7860101EU COCKPIT UNKNOWN A PNSAC ABORTED TAKEOFF W INADEQUATE Q C TOTAKEOFF 1 AL03676PA 316 CAPT MISTAKENLY HEARD AUTOCOARSEN FAIL CALLOUT BY SECOND IN COMMAND ON INITIAL TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AFTER TURNING OFF RUNWAY FAILURE LIGHT WAS CONFIRMED NOT TO BE ON. MAINTENANCE WAS CALLED BUT NO ACTION TAKEN. AIRCRAFT TAXIED BACK TO RUNWAY AND A NORMAL TAKEOFF WAS PERFORMED. 2L72 4T RTA52EU 20050214000602005021400060EU 2005 2 14 MALA040945 120041210A33506104789 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 BATTERY PACK P/N 61-0478-9, S/N ELB307 FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT P/N 51-2198-1 UNIT PASSES CMM CHECKS, RETURNED TO SERVICE 12/12/04. 2L72 4T RTA52EU 20050215000212005021500021GL 2005 2 15 SIMA200500101 220041229A7200AE3007A12 ENGINE EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL RIGHT FAILED A SIMAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW21737MW 145396 DURING CLIMB THE CREW REPORTED HEARING A LOUD BANG FROM ENGINE TWO. THEN ENGINE 2 SHUTDOWN UNCOMMANDED. NO WARNINGS JUST SEEMED TO SPOOL DOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502367) (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000442005021500044NM 2005 2 15 S2YA04013 120040506A3000 WARNING LIGHT DORNERDO32 DO328300 NM PWA 306 PW306B NE HORN HEAT FALSE INDICATIONA S2YAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL13352SK 3111 DURING FLIGHT, WHILE ENCOUNTERING SOME LIGHT TURBULANCE THE CREW NOTED A (L/R ELEVATOR HORN HEAT FAIL). THE CREW PERFORMED AN AIR-TURN-BACK AND MADE AN UNEVENTFUL LANDING. MX INSPECTED THE SYSTEM, REMOVED THE LT AND RT RUDDER HORNS BUT DID NOT FIND ANY DISCREPANCIES. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050215000472005021500047NE 2005 2 15 S2YA04023 220040701A7297P610149 WIRE HARNESS DORNERDO32 DO328300 NM PWA 306 PW306B NE RT ENGINE INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13360SK 2400 DURING TAKEOFF FOR FLIGHT, THE CREW NOTED A CAS MESSAGE FOR RT GENERATOR FAIL. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. AFTER CONSULTATION WITH MX THE SYSTEM WAS PLACED ON MEL. ON 7/05/04 MX INSPECTED THE SYSTEM AND REPLACED THE RT ENGINE DC CONTROL HARNESS. MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050215000512005021500051NM 2005 2 15 S2YA04021 120040610A3260 BULB DORNERDO32 DO328300 NM PWA 306 PW306B NE MLG INDICATOR FAILED A S2YAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL13357SK 3164 SHORTLY AFTER TAKEOFF, THE CREW REPORTED AN INCORRECT GEAR INDICATION. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MX REPLACED THE LIGHT BULBS IN THE RT MAIN GREEN DOWN ARROW AND RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050215000542005021500054EU 2005 2 15 BMAC040014 120041216A6120 BETA TUBE BAG JETSTMJETSTM3101 1500215EU NR 1 ENGINE LEAKING A B16AO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NE05525PA 666 PILOT REPORTED: SMOKE AND FUMES PRESENT IN COCKPIT, PROBLEM WENT AWAY WITH BOTH FLOWS OFF. NR 1 PROP HUB LEAKING LARGE AMOUNT OF OIL. FOUND SMOKE AND FUMES IN COCKPIT TO BE FROM LEAKING BETA TUBE ON NR 1 ENGINE. FOUND NR 1 ENGINE BETA TUBE LEAKING OIL. REPLACED O-RINGS AND REINSTALLED BETA TUBE IAW AMM. OPS CHECKED GOOD. NO LEAKS FOUND. SERVICED NR 1 ENGINE OIL IAW AMM.(K) 2L72 4T RTA21EU 20050215000552005021500055 2005 2 15 DAT2005F00000 420041215A61228210209F GOVERNOR STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA PROPELLER FAILED E DATAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL13167RC 151 SH3038 WHILE ON THE RETURN FLIGHT, CREW EXPERIENCED RT ENGINE ABNORMALITIES. THE TORQUE INDICATION EXCEEDED THE RED LINE LIMITATION AND BECAME UNCONTROLLABLE. AT THE SAME TIME, A DRASTIC DECLINE IN PROP RPM (BELOW 900 RPM) WAS NOTED. BOTH INDICATIONS WERE NOT ADJUSTABLE TO A STABLE CONDITION, THUS THE NECESSITY TO EXECUTE PRECAUTIONARY RT ENGINE SHUTDOWN. AN EMERGENCY WAS ALSO DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC REPLACED PROP GOVERNOR WITH A SERVICEABLE ONE IAW MM. OPS CHECK GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2H72 4T4 T A41EU E4EA 20050215000562005021500056SO 2005 2 15 SIMA200436602 120041228A32504PB717T2 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CAPTAIN'S YOKE SHORTED A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21653AE 145433 CREW REPORTED THE CAPTAINS YOKE NEAR EMITTING SMOKE NEAR THE STEERING DISCONNECT SWITCH WHEN AIRCRAFT IS ON GROUND. MAINTENANCE REPLACED THE CAPTAIN AUTOPILOT DISCONNECT SWITCH AND CHART HOLDER. IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW200502010) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000572005021500057NM 2005 2 15 USAA041077 120041210A5730 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE RT WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19392US53307 23314 PIT - WALKAROUND- WING T/E, 8 INCH X 12 INCH AREA, DELAMINATION, UPPER PANEL OB RT FIXED T/E OF WING. REPLACED PANEL IAW SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050215000612005021500061SO 2005 2 15 SIMA200432201 120041114A33502013R BATTERY EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21800AE 145425 EMERGENCY FLOOR LIGHT ON LT SIDE (FIRST 6 ROWS) DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY POWER SUPPLY 2 IAW AMM. OPERATIONAL CHECK GOOD. (SW21200502112) (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000622005021500062EA 2005 2 15 REXA04042 120041212A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS MALFUNCTIONED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258718E 7718 FLAPS FAILED ON APPROACH, EMERGENCY DECLARED, QRH FOLLOWED, UNEVENTFUL LANDING. SYSTEM RESET PLACED FLAP ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20050215000642005021500064NM 2005 2 15 ASA0440218 120041029A532065622082 SPLICE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU STRINGER MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02762AS 25099 MISDRILLED STRINGER SPLICE. REPLACED STRINGER SPLICE. 2L72 4F4 FRTA16WE E21EU 20050215000692005021500069CE 2005 2 15 FFS2005F00000 120040929A561010138402521 WINDSHIELD BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL MLG BROKEN A FFSAO OTHER O OTHER NRNOT REPORTED 1 AL01575G UC155 PILOTS INNER WINDSHIELD PANE SHATTERED. FAILURE OCCURRED DURING CRUISE AT FL250, OUTSIDE AIR TEMPERATURE OF -35 DEGREES C WITH THE WINDSHIELD HEAT ON. THE CRACKS APPEARED SUDDENLY ALL OVER WITH A LOUD BANG. WINDSHIELD TIME IN SERVICE UNKNOWN. (AL01200405421) 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20050215000702005021500070SO 2005 2 15 SIMA200434203 120041126A5320145425391003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21839AE4948 145653 DURING MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000712005021500071SO 2005 2 15 SIMA200434204 120041130A531514521721009 FLOORBEAM EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21737MW8469 145396 DURING AN IMBV INSPECTION FOUND THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED A SECTION OF GALLEY AREA FORWARD DIGITAL. FABRICATED 2 REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050215000722005021500072EU 2005 2 15 USAA041083 120041209A5315D53472090000200 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 CHECK, FLOORBEAM, 2.4 INCH L X 1.81 INCH X .066 INCH D, CORROSION; LEVEL 2; TASK NR JA260-53500-007, FR 66,Y765, Z240. REMOVED AND REPLACED WITH NEW FLOORBEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215000752005021500075EA 2005 2 15 REXA04041 120041204A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258674A 7674 FLAPS FAILED AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD98-20-01. 2L72 4F4 FRTA21EA E15NE 20050215000822005021500082SO 2005 2 15 SIMA200434102 120041203A27503631001005 CONTROL UNIT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL TE FLAPS INOPERATIVE A SIMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW21726AE 145314 ON APPROACH, RECEIVED (FLAP FAIL) ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBRICATED THE LT AND RT FLAP FLEX SHAFTS AND REPLACED NR 2 AND NR 3 FLAP ACTUATORS AND THE FLAP ELECTRONIC CONTROL UNIT IAW MM. OPS CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE.(K) 2L72 4F4 FRTT00011ATTE6CH 20050215000842005021500084EU 2005 2 15 BMAC040015 120041220A3200 WARNING LIGHT BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP MLG ILLUMINATED A B16AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05536PA 681 LANDING GEAR INDICATE DOWN AFTER THE LANDING GEAR HANDLE GOES UP- LT SIDE. PERFORMED LANDING GEAR EXTENSION AND RETRACTION FUNCTION CHECK IAW MM. OPS CHECKED OK. (K) 2L72 4T4 TRTA21EU E4WE 20050215000862005021500086NM 2005 2 15 C7WA200400061 120041011A575365192493 FLAP TRACK BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE RT WING TE FLAP CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177635U 19908 RT WING IB FLAP OB TRACK AFT MOUNT PAD HAS CORROSION. RT WING IB FLAP OB. TRACK NR 6 PN 65192493, CORROSION ON AFT MOUNT PAD REMOVED. MATERIAL REMOVED WAS 0.020. REPAIR ACOMPLISHED IAW EO. 2L73 4F4 F A3WE E2EA 20050215000902005021500090EA 2005 2 15 REXA04044 120041213A2750 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA PWA 305 PW305 NE TE FLAPS INOPERATIVE A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258505Q8575 7505 FLAPS FAILED AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAP ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F4 FRTA21EA E35NE 20050215000912005021500091CE 2005 2 15 POSA1204041 120041204A3260 INDICATOR BEECH 100 100BEECH 1152916CE PWA PT6 PT6A60A 52043NE MLG FALSE INDICATIONE POSAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA03100KA B11 ON FLIGHT, THE FLIGHT CREW TOOK OFF, RETRACTED LANDING GEAR AND NOTICED GEAR HANDLE STAYED RED INDICATING. LANDING GEAR WAS NOT FULLY UP AND STOWED. FLIGHT CREW LOWERED LANDING GEAR AND LANDED WITHOUT INCIDENT. ONLY FLIGHT CREW WAS ON BOARD. THERE WAS NO SPECIFIC PART CAUSING PROBLEM. INSPECTING LANDING GEAR AND ADJUST UPLIMIT SWITCH IAW MM. 1L72 3T4 T A14CE E4EA 20050215000922005021500092EA 2005 2 15 REXA04037 120041124A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS FAILED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258674A5158 7674 FLAPS FAILED ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20050215000952005021500095NM 2005 2 15 C7WA200400060 120041011A5314 KEELBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177635U 19908 AFT CARGO COMPARTMENT, STA 1007 RT KEELBEAM CHORD HAS CORROSION. INSTALLED INTERNAL SPLICE REPAIR ON RT HEELBEAM CHORD SECTION BETWEEN BS 980 AND BS 1007. DAMAGED KEELBEAM CHORD SECTION REMOVED. NEW KEELBEAM CHORD SECTION FABRICATED IAW SAMPLE AND MFG DWG 65-56441. MATERIAL USED TO FABRICATE THE KEELBEAM SECTION WAS 7075-T6511 ALUMINUM BAR 3.00 INCH X 4.00 INCH X 28.00 INCH. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. RPAIR ACCOMPLISHED IAW EO. 2L73 4F4 F A3WE E2EA 20050215000962005021500096EU 2005 2 15 USAA041093 120041213A5310D5347218820400 SUPPORT BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1-CHECK - SUPPORT BEAM, 2.15 X 1.0 X .036 INCH AND 1.73 X 1.70 X .052 INCH. CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN Y1292, FR 66-68. (K) 2L72 4F4 FRTA28NM E38NE 20050215000982005021500098EA 2005 2 15 REXA04043 120041212A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO258891A 7891 FLAPS FAILED ON TAXI OUT. SYSTEM RESET, PLACED FLAP ON 72 HOUR WATCH IAW AD98-20-01. 2L72 4F RTA21EA 20050215000992005021500099SO 2005 2 15 LAB2004F00001 120040929A3412681201 PROBE PIPER PA32 PA32300 7103212SO LYC O540 IO540K1G5 41532EA OAT INOPERATIVE E LABAO OTHER O OTHER NRNOT REPORTED 1 AL05666EB2 327940115 OAT (OUTSIDE AIR TEMPERATURE) PROBE INSTALLED IN CONJUNCTION WITH EFIS-SV SYSTEM FAILED. REPLACED PROBE WITH NEW AND CORRECTED PROBLEM. 1L71 3O3 O A3SO 1E4 20050215001032005021500103SO 2005 2 15 UQM2005F00001 220041118A7414BL500556103 MAGNETO PIPER PA28 PA28R201T 7102813SO CONT O360 TSIO360FB 17025SO ENGINE FAILED E UQMAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 CE013856735 28R7703243 PILOT WAS FLYING AT 7000 FT AND LOST POWER. ENGINE WENT TO IDLE. MADE A SAFE LANDING. AFTER COMING TO A STOP THE ENGINE WS NOT RUNNING. FOUND THE MAGS BOTH LT AND RT HAVE NO SPARK. REMOVED P LEADS AND STILL NO SPARK. REPLACED CONDENSORS AND STILL NO SPARK. REMOVED MAGS FROM ENGINE AND BENCH CHECKED AND NO SPARK. THE LT MAG HAS SN LISTED ABOVE AND RT MAG SN DO4DA208R. AFTER TALKING WITH MFG CAN NOT FIND CAUSE OF THE PROBLEM. ENGINE WAS FROM FACTORY AND INSTALLED AT 6/23/04, AND THE MAGS FAILED ON 11-13-04 WITH 35.14 HOURS SINCE OVERHAUL. (CE01200502044) 1L71 3O3 O 2A13 E9CE 20050215001132005021500113SO 2005 2 15 SIMA200435818 120041221A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 DURING AN MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED DOOR SILL TO REMOVE CORROSION. FABRICATED AN INTERNAL DOUBLER. REPAIR DONE IAW AEA. (SW21200501984) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001172005021500117 2005 2 15 REXA04035 420041109A2562 G SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ELT FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258869B2512 69322 7869 ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2L72 4F4 FRTA21EA E15NE 20050215001192005021500119EU 2005 2 15 KBM2005F00000 120041128A6410355A09103601 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP191188P977 2347 HALF SHELLS CRACKED. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050215001212005021500121SO 2005 2 15 SIMA200500902 120041231A532014521725615 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21632AE 145143 DURING CPCP INSPECTION MAINTENANCE FOUND THE SERVICE DOOR, AFT SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502484) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001222005021500122GL 2005 2 15 LC12005F00000 120041111A7921654585 OIL COOLER CIRRUSSR SR22 2130001GL CONT O550 IO550N 17042SO FUSLEAGE CRACKED B LC1RO OTHER O OTHER NRNOT REPORTED 1 EA07956C 308 0387 OIL COOLER IS CRACKED AT THE LOWER LT FLANGE AREA. 1L71 3O3 ONTA00009CHE3SO 20050215001242005021500124SO 2005 2 15 SIMA200434504 120041210A335020131A POWER SUPPLY EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21709GB 145211 DURING PRE-FLIGHT THE EMERGENCY LIGHTS FROM ROW NINE BACK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050215001302005021500130CE 2005 2 15 S2YA04019 120040607A32601003810061 UPLOCK SWITCH BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NLG INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1387SK UE87 AFTER TAKEOFF, THE GEAR IN TRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER THE GEAR SHOULD HAFE RETRACTED. THE CREW MADE AN AIR-TURN-BACK. MX INSPECTED THE AC AND REPLACED THE NOSE UPLOCK SWITCH. MX OPS CHECK THE SYSTEM, FOUND NO DISCREPANCIES AND RETURNED THE AC TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050215001432005021500143EU 2005 2 15 USAA041085 120041221A5315D2127698925000 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 CHECK- BEAM, 3.1 INCH X 1.5 INCH X 0.043 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500-005, FLOOR SUPPORT BEAM AT Y765, FR 66. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215001462005021500146NM 2005 2 15 PCS2005F00000 120040716A3610 BALL JOINT BOEING727 727212 138407GNM PWA JT8 JT8D15A 52051NE ENGINE LOOSE A PCSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17598AJ 21947 DURING CLIMBOUT NR 3 ENGINE FIRE WARNING BELL AND LIGHT WHEN OFF. DISCHARGED LT FIRE EXTINGUISHER IAW EMERGENCY PROCEDURES AND ABNORMAL CHECK LIST. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT FIRE EXTINGUISHER IAW MM. IN ADDITION, MAINTENANCE INSPECTED NR 3 ENGINE, FOUND 13TH STAGE AIR HIGH PRESSURE SADDLE DUCT BALL JOINT LOOSE, INSTALLED LAMINATED SHIMS AND RESECURED BALL JOINT, NO JET BLAST WAS OBSERVED, RAN ENGINE AT TAKE OFF POWER 2.07 EPR, 94 PERCENT N2. NO LEAKS NOTED IAW MM. ACCOMPLISHED GMM AND MM NO DEFECTS NOTED. AIRCRAFT WAS RETURNED BACK TO SERVICE. (K) 2L73 4F4 F A3WE E2EA 20050215001512005021500151NM 2005 2 15 C7WA200400068 120041111A80121G386 PRESSURE SWITCH BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE INOPERATIVE A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177638U 19911 653889 NR 3 ENGINE START VALVE LIGHT CAME ON DURING FLIGHT. FOUND NR 3 ENGINE START VALVE PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED PRESSURE SWITCH IAW MM. 2L73 4F4 F A3WE E2EA 20050215001522005021500152WP 2005 2 15 ASAA0480547 120041030A5730993749819 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK- LT WING L/E SURFACE HAS 7 CHAFED AREAS 5 INCHES FROM L/E AND I/B OF NR 5 L/E SLAT TRACK. REMOVED DAMAGED AREAS, THEN HFEC TREATED, PRIMED AND TOPCOATED THOSE AREAS IAW EA. 2L72 4F4 FRTA6WE E9NE 20050215001542005021500154NM 2005 2 15 C7WA200400085 120041103A3610BACC10DU350T CLAMP BOEING737 737231 1384079NM PWA JT8 JT8D219 52053NE LT MIX VALVE LOOSE A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO1724343 21630 AIR RETURN: UNABLE TO PRESSURE IN FLIGHT. ATTEMPIED TO CONTROL CABIN MANUALLY WITH FULL INCREASE PRESSURE NO HELP. RESECURED LOOSE DUCT AT LT MIX VALVE. OPS CHECK GOOD ON THE GROUND IAW MM. 2L72 4F4 FRTA16WE E9NE 20050215001622005021500162SO 2005 2 15 SIMA200434218 120041202A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21651AE8477 145422 THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED ATHE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001632005021500163NM 2005 2 15 RYN2005F00002 120041224A213340631997201AB OUTFLOW VALVE BOEING737 737800* NM CABIN PRESSURE INOPERATIVE A RYNAO OTHER J WARNING INDICATION CRCRUISE 1 CE07ELDGZ 28718 UNABLE TO CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED OUTFLOW VALVE. (K) 2L72 4F RTA16WE 20050215001652005021500165SO 2005 2 15 SIMA200434210 120041130A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21651AE 145422 DURING AN IMBV INSPECTION, STRINGER 19L WAS FOUND GOUGED FORWARD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001662005021500166SO 2005 2 15 SIMA200435820 120041220A532014521713005 BEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 DURING AN MBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER HAT BEAM. INSTALLED SERVICEABLE HAD BEAM IAW SRM. (SW21200501979) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001742005021500174SO 2005 2 15 SIMA200435816 120041220A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 DURING AN MBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED DIGITAL TO REMOVED CORROSION. FABRICATED A DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200501984) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001752005021500175SO 2005 2 15 SIMA200435817 120041221A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21638AE 145172 DURING AN MBV INSPECTION, A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR FROME THE LT OMEGA BEAM. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DOEN IAW SRM. (SW21200501984) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001762005021500176EA 2005 2 15 A6WA200540015 120041228A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31411ZW 7569 LT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. REPAIRED LT SIDE 484 ANGLE AT LBL 36 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050215001792005021500179CE 2005 2 15 S2YA04046 120041207A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE AIR STAIR FALSE ACTIVATIONA S2YAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1385SK UE85 SHORTLY AFTER TAKEOFF, THE CREW NOTICED AN AIR STAIR DOOR ANNUNCIATOR ILLUMINATED. THE CREW PERFORMED AN AIR-TURN-BACK. THE DOOR WAS FOUND TO BE SECURE. AFTER MX CONSULTATION, THE ANNUNCIATOR WAS MEL`D AND THE AC RETURNED TO SERVICE. MX CLEANED AND INSPECTED THE DOOR SWITCHES. WITH NO FURTHER DISCREPANCIES, THE MEL WAS CLEARED AND THE AC WAS RETURNED TO SERVICE. (K) 2L72 4T4 TRTA24CE E26NE 20050217000022005021700002SW 2005 2 17 JJWA0059046 120041015A6410206016201133 BLADE BELL 206 206B 1181511SW TAIL ROTOR FAILED E JJWAK NONE O OTHER ININSP/MAINT 1 SO1725PM 267 1839 TAIL ROTOR BLADE, SENT TR BLADES INSPECTION, BLADE FAILED SKIN THICKNESS TEST WAS .0064 ON UPPER SURFACE, NOT REPAIRABLE. WARRANTY CLAIM. 1G71 3U H2SW 20050211000912005021100091NM 2005 2 11 AWXA200500123 120041227A532065596644 CHANNEL BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER SPLICE BETWEEN BS 355 AND BS 363, STR 27 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE FROM BS 355 TO BS 363, 27 LT; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER SPLICE CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2L72 4F RTA16WE 20050214000282005021400028EU 2005 2 14 MALA040928 120041007A261172111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU E/E BAY MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15106XJ 340A106 PERSISTENT AVIONICS SMOKE INDICATION IN FLIGHT. CONTINUED TO REPEAT UNTIL SHUTDOWN, NO VISUAL OR SMELL IND OF SMOKE. MAINTENANCE REMOVED AND REPLACED AVIONICS SMOKE DETECTOR P/N ON & OFF 72-111211-000, PERFORMED REQUIRED OPS CHECKS ALL CHECKS ARE GOOD AT THIS TIME. 2L72 4T RTA52EU 20050214000542005021400054EU 2005 2 14 MALA040929 120041017A2710 BELLCRANK BAC 146 AVRO146RJ85A1500097EU AILERONS BINDING A MALAK NONE O OTHER ININSP/MAINT 1 GL15513XJ E2329 DURING FREEDOM OF MOVEMENT CHECK ON AILERON SYSTEM BINDING WAS FELT IN THE CONTROLS ACCOMPANIED BY NOISE AT THE BINDING POINTS. FURTHER INVESTIGATION REVEALED THAT THE HEAD OF THE BOLT WHICH CONNECTS THE INPUT ROD TO THE AILERON CABLE COMPENSATOR BELLCRANK WAS INTERFERING WITH THE INTERCOSTAL ABOVE IT. THIS CONDITION WAS NOTED ON BOTH THE CAPT & F/O'S SIDES. CAPT SIDE WAS CRACKED, F/O'S SIDE CHAFED. 2H74 4F RTA49EU 20050215000392005021500039EA 2005 2 15 SIMA200434901 120041212A3350110049 CHARGER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE EMERGENCY LIGHT INOPERATIVE A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21502AE 10018 EMERGENCY EXIT LOCATOR LIGHTS ABOVE THE GALLEY FOR THE PASSENGER DOOR AND SERVICE DOOR DO NOT ILLUMINATE. REPLACED NR 1 EMERGENCY LIGHT BATTERY AND CHARGER IAW AMM. OPERATIONAL CHECK GOOD IAW AMM. AC RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050215000432005021500043NM 2005 2 15 USAA041071 120041202A53306545772 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - SKIN, 9 INCHES X .5 INCH X .0075 INCH DEEP, CHAFED, RT OF S1 AT STA 867 TO 887. DOUBLER AND TRIPLER REPAIR SCHEME IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050215000452005021500045NM 2005 2 15 USAA041076 120041206A5330 SKIN BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19577US 23742 PIT - B-CHECK - SKIN, 3 INCH CRACK, STA 740, STR 18R. INSTALLED DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050215000492005021500049NM 2005 2 15 S2YA04020 120040609A3040 SENSOR DORNERDO32 DO328300 NM PWA 306 PW306B NE WINDSHIELD INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13352SK7528 3111 DURING TAKEOFF, THE CREW NOTED A WINDSHIELD HEAT FAIL CAS MESSAGE. THE CREW RETURNED TO THE GATE AND CONSULTED WITH MX. SINCE THE SPARE WINDSHIELD SENSOR WAS ALREADY ON MCO, MX REPLACEDTHE WINDSHIELD AND RETURNED THE AC TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050215000972005021500097SO 2005 2 15 UQM2005F00000 220041208A8520 CRANKSHAFT PIPER PA28 PA28R201T 7102813SO CONT O360 TSIO360FB 17025SO ENGINE BROKEN E UQMAO OTHER O OTHER NRNOT REPORTED 1 CE013856735 28R7703243 299928R AFTER INSTALLING REBUILT MAGS, TEST RAN AND WAS KNOCKING. REMOVED NR 1 CYLINDER AND FOUND CRANKSHAFT BROKEN AT THE JOURNAL. I FEEL THE CRANK MAY BE BROKEN IN ANOTHER SPOT. MFG IS AWARE OF THIS AND A REPLACEMENT ENGINE HAS BEEN SENT. PILOT WAS FLYING AT 7000 FT AND THE ENGINE QUIT. MADE A SAFE LANDING. (CE01200502280) 1L71 3O3 O 2A13 E9CE 20050215001092005021500109NM 2005 2 15 C7WA200400063 120041025A273069201841 SEAL PLATE BOEING727 727231 1384079NM PWA JT8 JT8D219 52053NE LT ELEVATOR DAMAGED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO1724343 21630 LOSS OF SYSTEM A HYDRAULIC PRESSURE AND QUANITY IN FLIGHT. FOUND DAMAGED PLATE SEAL AT LT ELEVATOR POWER PACKAGE. REMOVED AND REPLACED SEAL PLATE. 2L73 4F4 F A3WE E9NE 20050215001102005021500110SO 2005 2 15 SIMA200434208 120041130A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSLEAGE GOUGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21651AE8477 145422 DURING AN IMBV INSPECTION STRINGER 19R WAS FOUND GOUGED FWD OF FRAME 53. BLENDED THE GOUGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FAB 2 SHIMS AND REPAIR ANGLE. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001152005021500115CE 2005 2 15 FPI2005F00001 120041126A3240RA16402706 ROTOR BEECH 58 58 1152740CE BRAKE ASSY CRACKED E FPIAK NONE O OTHER ININSP/MAINT 1 SO15752P 370 TH422 RADIAL CRACK FOUND ON WEAR SURFACE ON INSIDE OF ROTOR. THIS WAS A REPLACEMENT PART NR RA-164-02706. SUSPECT MFG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETECTED. LT ROTOR, TT 370 HOURS 1L72 3O 3A16 20050215001582005021500158EA 2005 2 15 ASOA05004 120041228A3350BR9279106 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY EXIT BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27823AS 7196 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER AND TRIM AT THE SERVICE DOOR WERE FOUND BROKEN. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (K) 2L72 4F4 FRTA21EA E15NE 20050215001702005021500170NM 2005 2 15 ASAA0480555 120041102A533059114004 SKIN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 C-CHECK- NLG RT DOOR AFT HINGE COUTOUT IS CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR DOUBLER IAW SRM. 2L72 4F4 FRT E9NE 20050217000102005021700010NM 2005 2 17 ASA0440330 120041214A532065C3397047 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DOUBLE HOLE IN FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000112005021700011NM 2005 2 17 ASAA0470046 120041117A5320111A100046 WEB BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02618AS 30543 PAE - FOUND DURING MAINTNANCE CHECK, 8 INCH CRACK IN WEB AT BS 663, LB 13 AND WL 140. REPAIR IAW SRM 57-10-10. (M) 2L72 4F RTA16WE 20050217000152005021700015NM 2005 2 17 ASAA0470044 120041115A532015201397 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STATION 792. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050217000172005021700017NM 2005 2 17 ASA0440299 120041214A534069353521 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND STRINGER TIE CRACKED. REPLACED STRINGER TIE. (M) 2L72 4F RTA16WE 20050217000212005021700021NM 2005 2 17 ASA0440328 120041214A53406936656U9 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - INTERCOSTAL ANGLE IS CRACKED. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217000222005021700022NM 2005 2 17 ASA0440338 120041215A534765C3148354 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND SEAT TRACK DAMAGED. REPLACED SEAT TRACK. (M) 2L72 4F RTA16WE 20050217000232005021700023NM 2005 2 17 ASA0440337 120041215A53306545776 SKIN BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 PAE - FOUND EXTERNAL FUSELAGE SKIN GOUGE. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050217000242005021700024NM 2005 2 17 ASA0440336 120041214A531069353552 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON SHEAR TIE. REPLACED SHEAR TIE. (M) 2L72 4F RTA16WE 20050217000252005021700025NM 2005 2 17 ASA0440320 120041212A57536546435159 SKIN BOEING737 7374Q8 138447QNM TE FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02754AS 25095 OKC - FOUND RIGHT OUTBOARD FLAP INBOARD CORNER IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM. (M) 2L72 4F RTA16WE 20050217000262005021700026NM 2005 2 17 ASA0440294 120041211A5320654659247 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK. REPAIRED FLOOR TRACK. (M) 2L72 4F RTA16WE 20050217000282005021700028NM 2005 2 17 ASA0440276 120041208A532065C3184764 STRIP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR STRIP. REPLACED FLOOR STRIP. (M) 2L72 4F RTA16WE 20050217000292005021700029NM 2005 2 17 ASA0440291 120041210A53476546815148 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND DAMAGED SEAT TRACK. REPLACED SEAT TRACK. (M) 2L72 4F RTA16WE 20050217000322005021700032NM 2005 2 17 ASA0440267 120041208A53206545834525 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND FLOOR INTERCOSTAL CRACKED. REPLACED CRACKED INTERCOSTAL. (M) 2L72 4F RTA16WE 20050217000332005021700033NM 2005 2 17 ASA0440266 120041208A5320652072631 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND FORWARD CARGO BAY, SCRATCHES ON WEB UNDER FLOOR TO SIDEWALL SUPPORT. REPLACED WEB. (M) 2L72 4F RTA16WE 20050217000352005021700035NM 2005 2 17 ASA0440285 120041212A531065C329621 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000362005021700036NM 2005 2 17 ASA0440284 120041207A53106552878U102 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CREASE BEAM CHORD CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000372005021700037NM 2005 2 17 ASA0440283 120041207A5320654769015 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND AFT LOWER CARGO COMPARTMENT LEFT SIDEWALL/FLOOR SUPPORT CORRODED. REPAIRED FLOOR TO SIDEWALL SUPPORT PER SRM. (M) 2L72 4F RTA16WE 20050217000392005021700039NM 2005 2 17 ASA0440278 120041208A53476546815148 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND SEAT TRACK IS DAMAGED. REPLACED SEAT TRACK. (M) 2L72 4F RTA16WE 20050217000402005021700040NM 2005 2 17 ASA0440275 120041208A534065C340275 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON GALLEY SUPPORT HAT CHANNEL. REMOVED, FABRICATED AND INSTALLED HAT CHANNEL. (M) 2L72 4F RTA16WE 20050217000412005021700041NM 2005 2 17 ASA0440263 120041207A53206545834260 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000442005021700044NM 2005 2 17 ASA0440249 120041202A532069353591 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND INTERCOSTAL CRACKED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000452005021700045NM 2005 2 17 ASA0440264 120041204A53206545834256 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000462005021700046NM 2005 2 17 ASA0440261 120041207A575465C26687 WEDGE BOEING737 7374Q8 138447QNM NR 1 SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M) 2L72 4F RTA16WE 20050217000502005021700050NM 2005 2 17 ASA0440323 120041214A5755 STRUCTURE BOEING737 7374Q8 138447QNM NR 4 SPOILER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02754AS 25095 OKC - FOUND NR 4 SPOILER LOWER SEAL INSERTS IS CORRODED AND BROKEN SCREW STUDS. REMOVED DAMAGED SPOILER, ORDERED AND INSTALLED NEW SPOILER PER AMM. (M) 2L72 4F RTA16WE 20050217000512005021700051NM 2005 2 17 ASA0440318 120041213A532069374024 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CRACKED ANGLE. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217000522005021700052NM 2005 2 17 ASA0440335 120041214A53206546579531 STIFFENER BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND STIFFENER CORRODED AT APU INTAKE OPENING. REPLACED CORRODED STIFFENER PER SRM. (M) 2L72 4F RTA16WE 20050217000532005021700053NM 2005 2 17 ASA0440334 120041214A5347655384410 CARGO TRACK BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO TIE DOWN FITTINGS ARE CORRODED. REPAIRED TRACK TIE DOWN FITTING PER SRM. (M) 2L72 4F RTA16WE 20050217000552005021700055NM 2005 2 17 ASA0440258 120041205A53116546593 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND MECHANICAL DAMAGE ON FRAME. REPAIRED FRAME. (M) 2L72 4F RTA16WE 20050217000562005021700056NM 2005 2 17 ASA0440257 120041205A53116546567 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON AFT CARGO BAY, FRAME, FORWARD LOWER ANGLE. REPAIRED DAMAGED FAIL/SAFE L-ANGLE, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050217000592005021700059NM 2005 2 17 ASA0440280 120041209A531165450807 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FRAME CRACKED. REPLACED FRAME PER EA. (M) 2L72 4F RTA16WE 20050217000602005021700060NM 2005 2 17 ASA0440279 120041209A53206520726 WEB BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND GOUGES IN VERTICAL WEB. REPLACED WEB. (M) 2L72 4F RTA16WE 20050217000612005021700061NM 2005 2 17 ASA0440277 120041208A53476546813 SEAT TRACK BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REMOVED DAMAGED TRACK AND SPLICED IN NEW TRACK. (M) 2L72 4F RTA16WE 20050217000652005021700065NM 2005 2 17 ASA0440288 120041213A531065C25229 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FRAME TO SKIN ANGLE. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000672005021700067NM 2005 2 17 ASA0440273 120041208A531565C3394116 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM UPPER FLANGE. (M) 2L72 4F RTA16WE 20050217000702005021700070NM 2005 2 17 ASA0440270 120041208A534765C3184764 STRAP BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR STRAP. REPLACED FLOOR STRAP. (M) 2L72 4F RTA16WE 20050217000712005021700071NM 2005 2 17 ASA0440269 120041208A53206547690 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - ELONGATED HOLES AND DRILL STARTS. REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 20050217000722005021700072NM 2005 2 17 ASA0440268 120041208A53206545834259 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000742005021700074NM 2005 2 17 ASA0440262 120041207A575465C26687 WEDGE BOEING737 7374Q8 138447QNM NR 1 SLAT DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - NR 1 SLAT T/E WEDGE UPPER SURFACE HAS TWO DENTS. REPAIRED DENTS PER SRM. (M) 2L72 4F RTA16WE 20050217000772005021700077NM 2005 2 17 ASA0440317 120041213A53116546595260 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT ON TOP OF FRAME. REPAIRED FRAME PER SRM. (M) 2L72 4F RTA16WE 20050217000792005021700079NM 2005 2 17 ASAA0410690 120041220A57546545320147 RIB BOEING737 737298C 1384490NM NR 5 SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02745AS 20794 ANC - NR 5 LEADING EDGE SLAT OUTBOARD MAIN TRACK RIB ATTACH ANGLE CRACKED. REPLACED STIFFENER. (M) 2L72 4F RTA16WE 20050217000802005021700080NM 2005 2 17 ASA0440300 120041214A53206552878U102 SILL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND FUSELAGE UPPER LOBE, AFT ENTRY DOOR MOP SILL CORRODED. REPLACED MOP SILL. (M) 2L72 4F RTA16WE 20050217000812005021700081NM 2005 2 17 ASA0440298 120041214A5310654659249 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 FOUND CORROSION ON SHEAR TIE UPPER SURFACE. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000882005021700088NM 2005 2 17 ASA0440352 120041221A532069366791 STOP FITTING BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO BAY FORWARD INBOARD DOOR STOP FITTING GOUGED. REPLACED AFT CARGO BAY FORWARD INBOARD DOOR STOP FITTING. (M) 2L72 4F RTA16WE 20050217000902005021700090NM 2005 2 17 ASA0440350 120041220A531165C32396 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FRAME DAMAGED. REMOVED DAMAGED FRAME, FABRICATED REPAIR, INSTALLED FRAME. (M) 2L72 4F RTA16WE 20050217000912005021700091NM 2005 2 17 ASA0440349 120041220A5340655572746 SUPPORT ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO BAY FLOOR TO SIDEWALL ANGLE CRACKED. REPLACED CRACKED FLOOR TO SIDEWALL ANGLE. (M) 2L72 4F RTA16WE 20050217000932005021700093NM 2005 2 17 ASA0440343 120041216A53106546555 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON SHEAR TIE. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217000942005021700094NM 2005 2 17 ASA0440342 120041216A53106545855103 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01765AS 25102 PAE - FOUND CORROSION ON CREASE BEAM CHORD, MOPSILL. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217000952005021700095NM 2005 2 17 ASAA0440341 120041215A532069366569 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND INTERCOSTAL IS CRACKED. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM. (M) 2L72 4F RTA16WE 20050217000982005021700098NM 2005 2 17 ASA0440348 120041220A532065465981 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M) 2L72 4F RTA16WE 20050217001022005021700102NM 2005 2 17 ASAA0440313 120041211A53116546596163 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT ON TOP OF FRAME FLANGES. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217001032005021700103NM 2005 2 17 ASA0440306 120041210A53106552878U102 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CREASE BEAM CHORD CORRODED. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217001072005021700107NM 2005 2 17 ASAA0470047 120041228A5210147A61532 STRUCTURE BOEING737 737790 13844CNNM PAX DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02619AS 30164 PAE - DURING SI CHECK, FOUND DENT AND CRACK ON AFT ENTRY DOOR LOWER FORWARD EDGE AT BS 960. REPAIRED IAW SRM 52-00-01. (M) 2L72 4F RTA16WE 20050217001092005021700109NM 2005 2 17 ASA044031 120041211A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED FLOORBEAM UPPER CHORD PER SRM. (M) 2L72 4F RTA16WE 20050217001102005021700110NM 2005 2 17 ASA0440308 120041210A531065468172 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON UPPER LOBE INTERIOR CORROSION ON CREASE BEAM WEB. REPLACED CREASE BEAM WEB. (M) 2L72 4F RTA16WE 20050217001132005021700113NM 2005 2 17 ASA0440302 120041213A532065C80736749 SUPPORT CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - GALLEY SUPPORT CHANNEL IS CORRODED. REMOVED AND REPLACED CHANNEL. (M) 2L72 4F RTA16WE 20050217001142005021700114NM 2005 2 17 ASA0440301 120041213A532065C3184778 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND FLOOR SUPPORT IS CORRODED. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217001152005021700115NM 2005 2 17 ASA0440347 120041218A532065465981 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M) 2L72 4F RTA16WE 20050217001162005021700116NM 2005 2 17 ASA0440346 120041217A532065465981 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR. REPLACED DAMAGED SECTION OF FLOOR TRACK. (M) 2L72 4F RTA16WE 20050217001172005021700117NM 2005 2 17 ASA0440345 120041216A5340697599628 SUPPORT FITTING BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON GALLEY SUPPORT FITTING. REPLACED FITTING. (M) 2L72 4F RTA16WE 20050217001182005021700118NM 2005 2 17 ASA0440340 120041215A5753657193069 SKIN BOEING737 7374Q8 138447QNM TE FLAPS DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02754AS 25095 OKC - FOUND LEFT OUTBOARD FLAP HAS A DENT ON THE LOWER SURFACE SKIN, A=.5, Y=.55, AY=9. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (M) 2L72 4F RTA16WE 20050217001192005021700119NM 2005 2 17 ASA0440339 120041215A5320657374637 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION AFT CARGO BAY ON FLOOR SUPPORTS AT PREVIOUS REPAIR. BLENDED CORROSION ON FLOOR SUPPORTS, FOUND SEVERAL LOCATIONS OUT OF LIMITS, GENERATED MIG-5'S TO DOCUMENT INDIVIDUAL REPAIRS. (M) 2L72 4F RTA16WE 20050217001202005021700120NM 2005 2 17 ASA0440329 120041214A532065C33268 ANGLE BOEING737 7374Q8 138447QNM INTERCOSTAL CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - INTERCOSTAL ANGLE IS CRACKED. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217001212005021700121NM 2005 2 17 ASA0440327 120041214A532065C2730887 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON SIDEWALL SUPPORT. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050217001232005021700123NM 2005 2 17 ASA0440297 120041214A5320654659249 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK. REMOVED DAMAGE/CORROSION FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050217001242005021700124NM 2005 2 17 ASA0440296 120041210A534069353521 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND STRINGER TIE CRACKED. REPLACED STRINGER TIE. (M) 2L72 4F RTA16WE 20050217001262005021700126EU 2005 2 17 TXER097637 120041005A6520350A33020005 GEARBOX AEROSPAS355 AS355N 8680818EU TAIL ROTOR MAKING METAL B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588BP1898 5688 GEARBOX MAKING METAL. 1G72 3U RTH11GU 20050217001332005021700133EU 2005 2 17 MALA040953 120041220A33506122741 BATTERY PACK BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15531XJ E2365 BATTERY PACK FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED CELL PACK ASSEMBLY, P/N 61-2274-1. UNIT PASSES ALL CMM CHECKS. A/C RETURNED TO SERVICE 1/5/05. 2H74 4F RTA49EU 20050217001342005021700134EU 2005 2 17 MALA040951 120041223A3350549132406 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15365PX 340B265 BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/26/04. 2L72 4T RTA52EU 20050217001352005021700135NM 2005 2 17 XN0A1227 120041224A3050 WARNING LIGHT BOEING727 727227 1384078NM NR 3 CSD ILLUMINATED A XN0AO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL2376752 21248 NR 3 ENGINE CSD LOW PRESSURE WARNING LIGHT ON WITH NO FREG. DISCONNECTED NR 3 CSD DEFERRED NR 3 GENERATOR INOP IAW ENA B727 MEL 24-1 PROCEDURES DMI 4858 CAT-B ITEM. PLACARDS INSTALLED. 2L73 4F A3WE 20050217001362005021700136SW 2005 2 17 47504123104 120041231A2900222382001103 SERVO BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE HYD SYSTEM FAILED E A1UAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 CE03431MA 47504 47209 SCENE FLIGHT FROM BASE 7 LAS VEGAS, NV TO JEAN, NV TO UNIVERSITY MEDICAL CENTER (UMC), LAS VEGAS, NV. APPROXIMATELY 1 MILE SOUTH OF UMC, NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIENT WAS TRANSPORTED VIA AMBULANCE ACROSS THE STREET TO UMC. RT DUAL ACTUATOR SERVO LEAKING AT PISTON. REMOVED AND REPLACED SERVO. 1G72 3U3 U H9SW E5NE 20050215000262005021500026NE 2005 2 15 S2YA04015 220040514A75324067B000004 SHUTOFF VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE LT BLEED SYS MALFUNCTIONED A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13359SK 3202 BEFORE FLIGHT, THE CREW NOTED A CAS MESSAGE FOR LT BLEED SOV FAIL AND LT PACK FAIL. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED AND OPERATED THE SYSTEM BUT COULD NOT DUPLICATE THE DISCREPANCIES. MX REPLACED THE LT PRESSURE REDUCING VALVE (BOV) FOR TROUBLESHOOTING AND RETURNE THE AIRCRAFT TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050215000352005021500035SO 2005 2 15 SIMA200434211 120041201A532014521725615 WEB EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21634AE 145150 FOUND WEB AFT OF SERVICE DOOR AT RIB 22 AND 23, STR 15 HAS SMALL SPOTS OF CORROSION. REPLACED RIGHT AFT SERVICE DOOR WEB IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050215000382005021500038EA 2005 2 15 RU3A0419 120041129A2810 SEAL CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343A1 30015NE FUEL CAP DETERIORATED A RU3AAB UNSCHED LANDING EMER. DESCENT K FLUID LOSS CLCLIMB 1 SW1587 5190 AFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP. 2L72 4F4 FRTA21EA E15NE 20050215000602005021500060EU 2005 2 15 USAA041088 120041212A5315D5347218920200 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1-CHECK - BEAM, 2.0 INCH X .75 INCH X 0.052 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN FLOOR BETWEEN FR 68-69, BL Y1292. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215000732005021500073NE 2005 2 15 15HA0424011 220041211A8530327626 CYLINDER CVAC 240 T29B 2422644WP PWA R2800 CA18 52026NE RT ENG, CYL 18 CRACKED A I5HAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER CRCRUISE 1 GL23150PA 278 WHILE ENROUTE, CREW OBSERVED THE RT ENGINE WAS RUNNING ROUGH. THE CREW PERFORMED A PRECAUTIONARY IN-FLIGHT ENGINE SHUT-DOWN AND DIVERTED. INSPECTION OF THE RT ENGINE REVEALED THAT THE NUMBER EIGHTEEN CYLINDER WAS CRACKED. THE CYLINDER WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4R4 R 6A6 E231 20050215000852005021500085CE 2005 2 15 K5L2005F00000 120041227A3260BZ2RQ181A2 UPLOCK SWITCH BEECH 200 A200 1152921CE PWA PT6 PT6A41 52043EA LT MLG FAILED E K5LAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA05636B BC61 ON TAKEOFF, RETRACTED GEAR AND IN TURBULENCE, GEAR HANDLE LIGHTS FLICKERED ON AND OFF. PULLED BACK ON YOKE AND LIGHTS STAY ON, PUSH FWD AND LIGHTS GO OFF. REMOVED GEAR UP LIMIT SWITCH AND FOUND IT WAS GOING OFF BEHIND AUDIAL CLICK OFF SWITCH. REPLACED SWITCH AND RIGGED GEAR AND LANDING GEAR HANDLE LIGHTS STAY OFF. (K) 1L72 4T4 T A24CE E4EA 20050215001062005021500106NM 2005 2 15 UIEA200400203 120041221A2780 CONNECTOR BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE NR 4 SLAT LOOSE A UIEAJA DUMP FUEL UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 EA15536MC 21576 NR 4 LEADING EDGE FLAP WOULD NOT RETRACT OR EXTEND NORMALLY OR ELECTRICALLY. JETTISONED 60.0 K FUEL. FOUND FORWARD CONNECTOR LOOSE ON L/E DRIVE UNIT. RESECURED CONNECTOR IAW MM. OPS CHECK OK, NORMAL. (K) 2L74 4F4 F A20WE E23EA 20050215001472005021500147SO 2005 2 15 SIMA200434207 120041127A532014522178005 SILL EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL SERVICE DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21737MW8469 145396 DURING AN IMBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SERVICE DOOR CENTER AND INSTALLED NEW SERVICEABLE SILL IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050215001502005021500150NE 2005 2 15 C7WA200400067 220041111A7261652186717 LINE BOEING727 7272M7 138407SNM PWA JT8 JT8D219 52053NE NR 3 ENG OIL LOOSE A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO17721RW 21200 ON CLIMB OUT THROUGH 16,000, NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE WAS 35 PSI AND DECREASING. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW AOM. FOUND NR 3 ENGINE LOW OIL PRESSURE SWITCH OIL LINE LEAKING. REMOVED AND REINSTALLED LINE OPERATIONAL CHECK GOOD, NO LEAKS NOTED. 2L73 4F4 F A3WE E9NE 20050215001552005021500155NM 2005 2 15 S2YA04043 120041123A2420ALT3524 ALTERNATOR DORNERDO32 DO328300 NM PWA 306 PW306B NE ENGINE INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13356SK8219 391 3163 DURING CLIMB OUT, THE CREW RECEIVED A LT ALTERNATOR FAIL CAS MESSAGE. THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED THE LT AC ALTERNATOR. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050215001562005021500156 2005 2 15 A6WA200440220 420041214A2210 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE AILERONS BINDING A A6WAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL31410AW 7490 FIRST OFFICER REPORTED RT AILERON BINDING ON APPROACH WITH AUTO PILOT SELECTED OFF. INSPECTED AILERON CONTROL SYSTEM IAW SL. FOUND NO EVIDENCE OF MOISTURE OR PULLEY BINDING. NO FAULTS IN MDC. PERFORMED OPS CHECK OF AUTOPILOT, OPS CHECK GOOD IAW 27-11-00. 2L72 4F4 FRTA21EA E15NE 20050215001672005021500167SO 2005 2 15 SIMA200436301 120041226A2120 SMOKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21716AE 145264 AIRCRAFT RETURNED TO FIELD AND DECLARED AN EMERGENCY FOR SMOKE IN THE COCKPIT. PERFORMED OPERATIONAL CHECK OF THE AIR CONDITIONING PACKS AND BLEED AIR SYSTEMS WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (SW21200502002) (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001782005021500178GL 2005 2 15 ALG2005F00002 220041204A7300 FILTER BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL AIR SYSTEM DIRTY E ALGAC ABORTED TAKEOFF G MULTIPLE FAILURE TOTAKEOFF 1 SW03269AL 52284 WHILE LIFTING UP TO A HOVER TO DEPART, N2 RPM BLED OFF TO BELOW 90 PERCENT AND WOULD RECOVER, THROTTLE WAS FULL OPEN AND MAX BEEP WOULD NOT INCREASE THE RPM. MAINTENANCE REMOVED THE P/C, CLEANED AND DID A SYSTEM AIR LEAK CHECK. REINSTALLED SAME P/C FILTER AND DID OPS CHECK FLIGHT, CHECK FLIGHT WAS GOOD. (K) 1G71 3U3 UNCH2SW E1GL 20050217000162005021700016NM 2005 2 17 ASAA0470042 120041115A5320143A948535 FLOOR SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE - FOUND DURING MAINTENANCE CHECK, CORRODED FLOOR SUPPORT ANGLE. REPAIRED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 20050217000202005021700020NM 2005 2 17 ASAB0440333 120041214A53206546567 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - LT VERTICAL STAB SKATE (FWD) ANGLE IS CHAFFED. REPLACED LEFT VERTICAL STAB FORWARD SKATE ANGLE. (M) 2L72 4F RTA16WE 20050217000272005021700027NM 2005 2 17 ASA0440293 120041211A532069407124 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND INTERCOSTAL IN AFT CARGO BAY MISDRILLED. REPLACED INTERCOSTAL. (M) 2L72 4F RTA16WE 20050217000342005021700034NM 2005 2 17 ASA0440286 120041212A532065C329621 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000622005021700062NM 2005 2 17 ASA0440274 120041208A53116546566 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION UPPER LOBE ON FRAME. FABRICATED AND INSTALLED FRAME. (M) 2L72 4F RTA16WE 20050217000632005021700063NM 2005 2 17 ASA0440290 120041212A551465C274942 SKIN BOEING737 7374Q8 138447QNM HORIZONTAL STAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED. CUT OUT DAMAGED SKIN, FABRICATED REPAIR FILLER AND DOUBLER PER SRM AND EA, INSTALLED REPAIR DOUBLER TO LOWER SKIN OF RIGHT HORIZONTAL STABILIZER. (M) 2L72 4F RTA16WE 20050217000642005021700064NM 2005 2 17 ASA0440289 120041212A532065C807351 SILL BOEING737 7374Q8 138447QNM GALLEY DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON AFT GALLEY DOOR MOP SILL. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000662005021700066NM 2005 2 17 ASA0440287 120041212A531065C32396 SHEAR TIE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND SHEAR TIE UPPER SURFACE CORRODED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000752005021700075NM 2005 2 17 ASA0440246 120041202A53156545808260 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000782005021700078NM 2005 2 17 ASA0440310 120041210A53156545810110 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON FLOORBEAM. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000832005021700083NM 2005 2 17 ASA0440254 120041205A53116546596141 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT ON TOP OF FRAME. FABRICATED REPAIR PART AND INSTALLED. (M) 2L72 4F RTA16WE 20050217000892005021700089NM 2005 2 17 ASA0440351 120041218A532065C2730892 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON SUPPORT CHANNEL UPPER SURFACE. REMOVED AND INSTALLED NEW SUPPORT CHANNEL. (M) 2L72 4F RTA16WE 20050217000922005021700092NM 2005 2 17 ASA440344 120041216A5315654681179 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM. REPLACED PER EA. (M) 2L72 4F RTA16WE 20050217001312005021700131EU 2005 2 17 MALA040949 120041218A33506104789 BATTERY PACK SAAB SF340 340B 7860101EU EMERGECNY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15365PX 340B265 BATTERY PACK FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/23/2004. 2L72 4T RTA52EU 20050217001322005021700132EU 2005 2 17 MALA040952 120041220A33506122741 BATTERY BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15508XJ E2318 BATTERY POWER SUPPLY REMOVED FOR SCHEDULED CAPACITY CHECK. FAILED FINAL TEST MAINTENANCE REPLACED BATTERY ASSEMBLY UNIT PASSES ALL CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/23/04. 2H74 4F RTA49EU 20050218000192005021800019NM 2005 2 18 04FDEA03360 120041206A5313AFA7772501 LONGERON DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 CENTER CARGO LONGERON CORRODED - 50L AT STA 1681. CENTER CARGO LONGERON 50L AT STA 1681 REPAIR CARRIED OUT AS PER SRM 53-10-00 VOL I. 2L73 4F RTA22WE 20050218000202005021800020CE 2005 2 18 4015 120040618A3230583800901 MOTOR BEECH 58 58 1152740CE CONT O550 IO550C SO HARTZLHCJ3Y PHCJ3YF2 GL MLG INOPERATIVE E BSYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07140S TH1155 299231R ED3660A AIRCRAFT DEPARTED CLT, WHEN PILOT SELECTED GEAR UP NOTHING HAPPENED, PILOT RETURNED TO CLT. MAINTENANCE FOUND LANDING GEAR MOTOR BAD, REMOVED AND REPLACED MOTOR, OPS CHECKS GOOD. 1L72 3O3 O 3A16 E3SO 5 CP36EA 20050218000322005021800032NM 2005 2 18 USAA050218A 120041231A5330 SKIN BOEING737 7373B7 1384580NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU53288 23700 CLT - FOUND SKIN CRACKED 1.375 INCH, FS 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050218000372005021800037SO 2005 2 18 CHQA000565 120041007A3350 BATTERY EMB 135 EMB135KL 3260302SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11295SK 145513 EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW EMB 140 AMM 33-50-09. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050222000032005022200003SO 2005 2 22 SWIA200413330 120040414A5411 FRAME EMB 120 EMB120ER 3260203SO RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07271YV 120271 RT NACELLE FRAME NR 1 CRACKED INBOARD AND OUTBOARD AT TORSION BAR MOUNTS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME IAW 120 SB 120-54-0036 AND RII. PART II COMPLIED WITH. 2L72 4T RTA31SO 20050222000042005022200004GL 2005 2 22 AC2A094952 220040430A732323065123 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL LOOSE B AC2AK NONE O OTHER ININSP/MAINT 1 SO075058810600 780 POTTING COMPOUND IS BROKEN LOOSE AT SHAFT. REPLACED WITH SERVICEABLE GOVERNOR. 1G72 3U3 U H3EU E4CE 20050222000052005022200005SW 2005 2 22 AC2A094953 120040506A3213206323021 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07537023032 51249 DEEP CORROSION PITS AROUND SADDLE AND CLAMPS. 1G71 3U H2SW 20050222000062005022200006SW 2005 2 22 AC2A094954 120040506A3213206323022 CROSSTUBE BELL 206 206L3 1182108SW MLG CORRODED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07537023032 51249 DEEP CORROSION PITS AROUND SADDLES AND CLAMPS. 1G71 3U H2SW 20050222000072005022200007 2005 2 22 AC2A094956 420040517A34205040028903 GYRO BOLKMS105 BO105S 5626006EU ATTITUDE MALFUNCTIONED B AC2AK NONE O OTHER ININSP/MAINT 1 SO078775 775 ATTITUDE GYRO S/N 9257B WAS INSTALLED WHICH IT BEGAN TO PROCESS AFTER ABOUT 5 MINUTES NOSE HIGH. REINSTALLED ORIGINAL GYRO, ORDERED ANOTHER REPLACEMENT. 1G72 3U H3EU 20050222000092005022200009WP 2005 2 22 JRAA0520041 120040520A5315 FLOORBEAM CVAC 440 440 2422902WP RROYCEDART DART54210 54522EU FUSELAGE CORRODED E JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 DURING A SCID INSPECTION 53-20, A MISSING RIVET HEAD WAS FOUND AT STA 712.0. RT SIDE AT THE FLOORBEAM TO BELTFRAME ATTACH POINT. CORROSION WAS FOUND UNDER RIVET HEAD. NO OTHER RIVETS WERE FOUND TO BE CORRODED AT THIS TIME. RIVET REPLACEMENT IN PROGRESS AT THIS TIME. 2L72 4R4 T 6A6 E5EU 20050222000112005022200011NE 2005 2 22 ERAA095249 120040201A62107615009100051 BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR CORRODED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 9880 THIS INFO FOR FAA SDR. BLADE ASSY HAS CORROSION AT C BLOCK TO SPAR BOUND LINE. ACTION TAKEN: SENT TO CTI FOR REPAIR. INSPECTED, PERFORMED X- RAY FOR MOISTURE (FOUND APPROX 50-60 CELLS IN VIEW, E-9) REPLACED C BLOCK PER RS-008G-11, REPLACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9; REPLACED 4 EA ROOT END THROUGH BUSHINGS PER RS-004N-VII; REPAIRED SHEATH TANGS PER CTI-96-02; REPAIRED LEADING EDGE DAMAGE PE SA4047-76-5 PROCEDURE #6, REPAIRED SKIN DAMAGE ON LOWER SURFACE AT STA 122.875 PER SA4047-76-5 PROCEDURE #3; REINSTALLED TIP CAP SN A175-00295; REFINISHED WITH HIGH VIS SCHEME 2 PER SA 4047-76-5 DRWG 76150-090000 AND 76150-09100, STATIC BALANCED PER CTI-DAL-DA-026 @ TT 9880.1 1G72 3U H1NE 20050222000192005022200019NE 2005 2 22 HEEA095228 120040526A76007630103901102 ACTUATOR SKRSKYS76 S76A 8143006NE NR 2 ENGINE MALFUNCTIONED E HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW03776P 760275 DURING CRUISE FLIGHT NR 2 ENGINE BEEPED TO MINIMUM BY ITSELF. BEEPED ENGINE BACK UP BUT ENGINE AUTO BEEPED TO MINIMUM. COMPLIED WITH EMERGENCY CHECK LIST AND LANDED AT NEW ORLEANS. 1G72 3U H1NE 20050222000202005022200020SW 2005 2 22 HEEA095229 120040506A5610407030115125 WINDSHIELD BELL 407 407 1182206SW COCKPIT BIRD STRIKE E HEEAO OTHER O OTHER LDLANDING 1 SW03723PH 53283 BIRD STRIKE WHILE LANDING AT VEN NOBLE. MAINTENANCE REPLACED RT WINDSHIELD. NO OTHER DAMAGE TO AIRCRAFT. 1G71 3U O H2SW 20050222000212005022200021SW 2005 2 22 ALGA095231 120040610A632023071895 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03487AL134 53204 CAE847302 SPALLING ON GEAR TEETH, THIS IS A RECURRING EVENT ON C-47 GEARBOXES. REPLACED GEAR W/NEW PART. 1G71 3U3 UO H2SW E1GL 20050222000222005022200022SW 2005 2 22 ALGA095232 120040610A632023077527 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03487AL134 53204 CAE847302 SPALLING ON GEAR TEETH. THIS IS A NEW STYLE GEAR AND THIS GEARBOX WAS REMOVED FOR HIGH VIBES. THIS IS A RECURRING EVENT ON C-47 GEARBOXES. REPLACED GEAR W/NEW PART. 1G71 3U3 UO H2SW E1GL 20050222000232005022200023EU 2005 2 22 ALGA095233 120040610A6220C622A0101056 HUB UROCOPEC120 EC120B 8680987EU MAIN ROTOR DAMAGED E ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03512AL2141 1148 LIGHTNING STRIKE INSPECTION, FOUND ARCING ON YELLOW PITCH CHANGE ROD AND ON HUB SPLINE. ALSO, FOUND VARIOUS LOCATIONS ON HUB ASSY WITH HIGH MAGNETISM. 1G72 3U NCR0001RD 20050222000242005022200024 2005 2 22 AC2A095321 420040603A3425430375002109 DISPLAY BELL 430 430 1182150SW ALLSN 250B 250B* GL EFIS DAMAGED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 DISPLAY I S UNREADABLE. REPLACED EFIS TUBE. 1G72 3U3 TRTH9SW E10CE 20050222000262005022200026EU 2005 2 22 DHL2004362005 120040615A26123500813 CONTROLLER AIRBUS300 A300B4203 3930306EU FIRE LOOP MALFUNCTIONED A DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01362DH 84 LEFT WING MANIFOLD FAULT DETECTOR LOOP B INOP IN TEST. FOUND EITHER LOOP FIN NR 145HF OR FIN NR 147 HAS ONLY 2M OHMS TO GROUND. ON ORDER REQ NR 300109474. DMI NR 16915 STILL OPEN. REF DMI 16915, LT WING MANIFOLD FAULT DETECTOR LOOP B INOP IN TEST. C/W S/P. C/W S/P OF LT WING MANIFOLD FAULT DETECTOR LOOP A IAW MEL 36-12-03. DMI REMAINS IN EFFECT. LT WING MANIFOLD FAULT DETECTION LOOP B INOP IN TEST. REPLACED CFD CONT UNIT SYSTEM, OPS NORMAL AS PER 26-16-00 THIS CLEARS DMI NR 16915. 2L72 4F RTA35EU 20050222000282005022200028CE 2005 2 22 GLBA20030647 120040607A5210 DOOR BEECH 1900 1900D 1154162CE MAIN PAX CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03220GL UE220 CABIN DOOR HAS CORROSION AROUND BUTTON, REPAIRED CORROSION. 2L72 4T RTA24CE 20050222000302005022200030NE 2005 2 22 TSAA0436050 220040620A75321074925 BLEED VALVE BOEING737 73776N 13844CHNM CFMINTCFM567CFM567B2US 13802NE NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13742AL5894 30830 THE NUMBER TWO ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS CHECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK OK. REMOVED AND REPLACED 390 TEMP SENSOR (PRE-COOLER CONTROL VALVE SENSOR) IAW AMM 36-12-03-04, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20050222000312005022200031NM 2005 2 22 TSAA0436048 120040620A36001296662 SENSOR BOEING737 73776N 13844CHNM NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13742AL11315 30830 THE NR 2 ENGINE BLEED TRIPPED IN FLIGHT, DIVERTED TO HNL. PERFORMED ENGINE GROUND RUN-UP TO VERIFY BLEED TRIP AND OPS CHECK, RUN-UP OK. REMOVED AND REPLACED THE NR 2 ENGINE BLEED AIR REGULATOR FOR TROUBLESHOOTING IAW AMM 36-11-03-4, LEAK AND OPS CHECK OK. REMOVED AND REPLACED 390 TEMP SENSOR (PRE-COOLER CONTROL VALVE SENSOR) IAW AMM 36-12-03-04, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050222000342005022200034NM 2005 2 22 C8GA20040009 120040622A2913371380 PUMP BOEING727 727223 1384074NM HYD SYSTEM FAILED A C8GAO OTHER J WARNING INDICATION DEDESCENT 1 SO15899AA1762 22015 UPON DESCENT INTO KTOL, THE NR 2 ENGINE HYDRAULIC PUMP LOW-PRESSURE WARNING LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-05-2, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATION IN TOL WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NR 2 HYDRAULIC PUMP, THE HYD MODULAR PACK AND ALL FILTERS WERE REPLACED IAW MM B727 29-11-32, 29-11-61 AND 29-11-10. ALL SYSTEMS OPERATIONAL AND LEAK CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. FLT 502 FROM KTOL TO KMCI. DURING FLIGHT, THE NR 2 HYD PUMP PRESSURE WARNING LIGHT ILLUMINATED. AFTER NR 2 PUMP FAILURE FLUID LEVEL DROPPED TO ZERO ACCOMPANIED BY THE NR 1 LOW PRESSURE LIGHT ILLUMINATED. 2L73 4F A3WE 20050222000362005022200036EU 2005 2 22 DHL2004362006 120040624A3240 BRAKE AIRBUS300 A300B4203 3930306EU AUTOBRAKES SYS MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01362DH 84 PRIOR TO TAKEOFF, WHEN SELECTING AUTO BRAKES TO MAX, NORMAL BRAKING WAS LOST, THEN AUTO BRAKES OFF LIGHT WENT AMBER AND NORMAL BRAKING RETURNED AUTOBRAKES COULD NOT BE SELECTED WITH BRAKES APPLIED. PERFORMED OPS CHECK OF AUTOBRAKES SYSTEM IAW M/M 32-42-54. OPS GOOD, NO DEFECTS NOTED. 2L72 4F RTA35EU 20050222000392005022200039EU 2005 2 22 BAQA095539 120040623A14301051410110 BOLT BOLKMS117 BK117A4 5626017EU M/R BLADE UNSERVICEABLE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03587MC 7086 MAIN ROTOR BLADE BOLT WERE MANUFACTURED WITH THE CENTER HOLE TO SMALL TO ACCEPT WASHER P/N 117-181001.02. 1G72 3U H13EU 20050215001072005021500107NM 2005 2 15 C7WA200400084 120041102A3220 LANDING GEAR BOEING737 737231 1384079NM PWA JT8 JT8D219 52053NE NOSE MALFUNCTIONED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO1724343 21630 NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. RED NOSE GEAR UNSAFE LIGHT ON MANUALLY LOWERED NOSE LANDING GEAR IAW AOM. INSPECTED NOSE GEAR ACTUATOR, LOCKING ACTUATOR AND LINKAGE NO DAMAGE NOTED. LUBRICATED NOSE GEAR TRUNIONS, ACTUATOR AND DRAGBRACE AS NEEDED. PERFORMED EXTENSION AND RETRACTION CHECK OF NOSE LANDING GEAR INCLUDING EMERGENCY EXTENSION IAW MM. OPERATIONAL CHECKS GOOD. 2L72 4F4 FRTA16WE E9NE 20050215001202005021500120SO 2005 2 15 SIMA200434501 120041207A33501683 BULB EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMABA EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21826AE 145592 FA REPORTED A BURNING SMELL AT 16000 FT. DECLARED EMERGENCY AND RETURNED TO FIELD. THE FLIGHT ATTENDANT NOTICED AFTER LANDING THAT THE FORWARD OVERHEAD ENTRY LIGHT ABOVE HIS SEAT WAS BURNED OUT. CONTACTED MAINTENANCE, VERIFIED THAT THE BULBS WERE BURNED AND REPLACED THEM. OPS CHECK WAS GOOD AND NO SMELL WAS REPORTED. (K) 2L72 4F4 FRTT00011ATTE6CH 20050215001312005021500131NM 2005 2 15 S2YA04026 120040729A3246AHA2225 WHEEL DORNERDO32 DO328300 NM PWA 306 PW306B NE NR 2 INOPERATIVE A S2YAC ABORTED TAKEOFF EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL13355SK7517 416 3124 DURING TAKEOFF FOR FLIGHT, THE CREW NOTED AN ABNORMAL SHUDDER AND THEN ALINGERING BURNED RUBBER SMELL. THE CREW CONSULTED WITH MX AND PERFORMED AN AIR-TURN-BACK. MX INSPECTED THE AC AND FOUND THE LT NOSE FELT ROUGH CAUSING A VIBRATION WHEN SPUN. MX REPLACED THE BOTH NOSE WHEEL ASSEMBLIES AND RETURNED THE AC TO SERIVCE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050215001342005021500134EA 2005 2 15 REXA04033 120041105A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE TE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258943A997 7943 FLAPS FAIL AT 32 DEGREES ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT BPSU (BRAKE POSITION SENSING UNIT) IAW 27 AMM. OPERATIONALLY TESTED GOOD. 2L72 4F4 FRTA21EA E15NE 20050215001382005021500138EU 2005 2 15 KBM2005F00004 120041204A6420355A09103601 BEARING SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1D NE TAIL ROTOR WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1953SH 680 2009 HALF SHELLS WORN, REMOVED AND REPLACED.(K) 1G71 3U3 U H9EU E19EU 20050215001442005021500144EU 2005 2 15 USAA041092 120041213A5321D5367180500200 FLOOR PANEL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1-CHECK - FLOOR PANEL, .300 INCH X .200 INCH X 0.032 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53100, FLOOR PANEL NR 261 FF, Y1292, FR 66-68. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215001452005021500145EU 2005 2 15 USAA041095 120041221A5315D5347209001000 FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW 0863 BFM - S1-CHECK - SUPPORT BEAM - 1.5 X 1.2 X 0.035 INCH AND 1.5 X 1.5 X 0.040 INCH, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN Y1292, FR 66. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050215001482005021500148SO 2005 2 15 SIMA200434221 120041204A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21651AE8477 145422 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (K) 2L72 4T4 FRTT00011ATTE6CH 20050215001492005021500149WP 2005 2 15 ASAA0480545 120041030A575399359543 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 24 INCHES FROM THE T/E AND 17.5 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM. 2L72 4F4 FRTA6WE E9NE 20050215001602005021500160EA 2005 2 15 A6WA200440209 120041210A5753 VANE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 LT OB FLAP - VANE FITTING AT WS 296.073 IS WORN BEYOND LIMITS. COMPLY WITH MFG REO. 2L72 4F4 FRTA21EA E15NE 20050215001722005021500172EA 2005 2 15 O2G2005F00000 120041218A5610 WINDSHIELD CNDAIRCL601 CL6013A 8070802EA GE CF34 CF34* NE COCKPIT CRACKED E O2GAB EMER. DESCENT O OTHER CRCRUISE 1 NE03604GR 5478 THE OUTER PLY OF THE PILOTS WINDSHIED CRACKED AT APPROX 35,000 FT. CHANGED PILOTS NR 1 WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20050215001732005021500173NM 2005 2 15 BJNA041201 120041215A33506104789 BATTERY PACK BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE EMERGENCY LIGHT DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 DURING A PREFLIGHT WALK AROUND INSPECTION THE NR 1 OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY EXIT BATTERY PACK IAW MM. EMERGENCY EXIT LIGHTS NO OPERATE NORMALLY. (K) 2L72 4F4 FRTA16WE E2EA 20050215001772005021500177SO 2005 2 15 SIMA200435819 120041218A531314533888001 STRINGER EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21739AE 145402 DURING AN IMBV INSPECTION STRINGER 19R WAS FOUND TO BE CHAFED AT AFT BELLY FAIRING CUT OUT. BLENDED THE CHAFED AREA. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE, 2 SHIMS. REPAIR DOEN IAW SRM. (SW21200501981) (K) 2L72 4F4 FRTT00011ATTE6CH 20050217000302005021700030NM 2005 2 17 ASA0440295 120041211A5320654659247 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR TRACK. REPAIRED FLOOR TRACK. (M) 2L72 4F RTA16WE 20050217000472005021700047NM 2005 2 17 ASA0440260 120041207A5320654654712 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO BAY FLOOR SUPPORT IS DAMAGED. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000482005021700048NM 2005 2 17 ASA0440319 120041213A53116552255511 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FRAME DAMAGED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000542005021700054NM 2005 2 17 ASA0440259 120041209A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM PER SRM. (M) 2L72 4F RTA16WE 20050217000572005021700057NM 2005 2 17 ASA0440256 120041205A5320654587547 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON WEB. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050217000582005021700058NM 2005 2 17 ASA0440281 120041208A523065C362151 WEB BOEING737 7374Q8 138447QNM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT AT LIGHTING HOLE FORWARD CARGO DOOR INNER WEB. REMOVED DAMAGED AREA, FABRICATED TWO REPAIR PARTS, AND REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000692005021700069NM 2005 2 17 ASA0440271 120041208A53476546813106 SEAT TRACK BOEING737 7374Q8 138447QNM FUSLEAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. (M) 2L72 4F RTA16WE 20050217000822005021700082NM 2005 2 17 ASA0440316 120041213A53116546596163 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - DENT AFT CARGO BAY FRAME. REPAIRED FRAME PER SRM. (M) 2L72 4F RTA16WE 20050217000842005021700084NM 2005 2 17 ASA0440253 120041205A5320657374637 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORRODED FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000862005021700086NM 2005 2 17 ASA0440248 120041202A53156546811 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 FOUND CORROSION FUSELAGE UPPER LOBE, FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED FLOORBEAM. (M) 2L72 4F RTA16WE 20050217001002005021700100NM 2005 2 17 ASA0440315 120041212A534065C161219 ATTACH FITTING BOEING737 7374Q8 138447QNM GIRT BAR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON GIRT BAR MOUNT. REPLACED GIRT BAR MOUNT. (M) 2L72 4F RTA16WE 20050217001052005021700105NM 2005 2 17 ASAA0470043 120041115A5321146A75068 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE - DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOOR PANEL. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20050217001112005021700111NM 2005 2 17 ASA0440307 120041210A53206531787U6 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON U-ANGLE. REPLACED U-ANGLE. (M) 2L72 4F RTA16WE 20050218000102005021800010SO 2005 2 18 CHQA000575 120041028A3350 BULB EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11571RP 14500827 COCKPIT EMERGENCY OVERHEAD LIGHT IS INOP. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT BULB PER EMB 145 MM 33-50-05. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050218000122005021800012NE 2005 2 18 2004UALA01148 220041121A72306A5942 BLADE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE COMPRESSOR CRACKED A UALAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION DEDESCENT 1 WP29804UA 759 V10289 NR 2 ENGINE COMPRESSOR STALL AND SHUTDOWN ON DECENT. THIRD STAGE COMPRESSOR BLADE FAILED. BLADE RE-DESIGN IS IN PROCESS TO ADDRESS THIS PROBLEM. 2L72 4F4 FRTA28NM E40NE 20050222000142005022200014EU 2005 2 22 HE66095157 120040526A6330L633M2010104 MOUNT UROCOPEC135 EC135T1 5620026EU M/R GEARBOX WORN B HEEAO OTHER O OTHER NRNOT REPORTED 1 SW03135CR 0164 MAIN ROTOR GEARBOX MOUNT WORN BEYOND LIMITS 1G72 3U H88EU 20050222000322005022200032NM 2005 2 22 TSAA0452047 120040619A5210 DOOR BOEING737 73776N 13844CHNM MAIN PAX LACK OF LUBE A TSAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 WP13748AL 30050 FORWARD ENTRY DOOR DID NOT SEAL AFTER TAKEOFF, NO DOOR WARNING LIGHT. RETURNED TO PHX. LUBED DOOR HINGES AND ROLLERS, DOOR OPENS AND CLOSES OK. SEALS ARE OK, NO DEFECTS NOTED. OPS CHECK GOOD IAW AMM 52-11-00-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050222000372005022200037NM 2005 2 22 XNOA1189 120040611A2150 A/C PACK BOEING727 727227 1384078NM LEFT DAMAGED A XN0AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23371PC 157 LEFT PACK PRODUCES TOXIC FUMES WHEN USED. PERFORMED ADJUSTMENT/TEST OF THE NR 1 PACK SYSTEM IAW A300 AMM 21-51-00. NO DEFECTS NOTED. 2L73 4F A3WE 20050222000442005022200044EU 2005 2 22 04FDEA01866 120040627A2910 FITTING AIRBUS300 A300B4605R 3930308EU HYD SYSTEM LEAKING A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25663FE 766 IN LEVEL FLIGHT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNED OFF AT 3250 PSI. FOUND LEFT NOTCH FLAP ACTUATOR TEE FITTING LEAKING AT PACKING ON AFT TEE. REPLACED PACKING ON AFT LEFT NOTCH FLAP TEE PER SMP. LEAK CHECK IS GOOD. RESET LANDING GEAR FREE FALL EXTENSION PER 32-33-00-2. SECURED ALL PANELS, GEAR DOORS. 2L72 4F RTA35EU 20050222000452005022200045EU 2005 2 22 04FDEA01869 120040628A2910 FITTING AIRBUS300 A300F4605R 3930327EU HYD SYSTEM LEAKING A FDEAH DEACTIVATE SYST/CIRCUITS WKJINADEQUATE Q C FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25663FE 766 IN LEVEL FLT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNED OFF AT 3250 PSI. FOUND LEFT NOTCH FLAP ACT T-FITTING LEAKING AT PACKING ON AFT TEE. REPLACED PACKING ON AFT L/NOTCH FLAP TEE PER SMP. LEAK CHECK GOOD. RESET LANDING GEAR FREE FALL EXTENSION PER 32-33-00-2. SECURED ALL PANELS, GEAR DOORS. 2L72 4F RTA35EU 20050222000462005022200046CE 2005 2 22 GLBA20030658 120040626A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03240GL UE240 FUSELAGE SKIN AT NR 1 TRANSPONDER AND ATTACH POINT IS CORRODED. REMOVED CORROSION AND REPAIRED. 2L72 4T RTA24CE 20050222000472005022200047WP 2005 2 22 IXXA0400094S 120040430A5711 SPAR DOUG DC8 DC871F 302199DWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING REAR SPAR DOUBLER UPPER SIDE HAS CRACK DAMAGE AT STA XCW 69.500. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS, ALONG WITH THE DAMAGED AREA IAW DC8 SRM 51-1-20D PG 21 AND DC8 SRM 57-2-6 FIG 15. FABRICATED FILLER AND DOUBLER IAW DC8 SRM 57-2-6 FIG 15 PAGES 67 AND 68. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER AREA. APPLIED SEALANT ON FAYING SURFACES, INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS PER ALL APPLICABLE MANUALS. 2L74 4F RT4A25 20050222000482005022200048WP 2005 2 22 IXXA0400095S 120040505A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR SKIN BELOW ADF LOOP ANTENNA CORRODED, STA 115.000 TO 160.000, L-35R TO L-35L. REPAIR WAS ACCOMPLISHED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW 51-1-8 PG 17-18, AND 53-20 PG 24. REMOVED CORRODED SKIN AND INTERNAL DOUBLER IAW DC8 SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED DOUBLER AND SKIN PER ALL APPLICABLE MANUALS. 2L74 4F RT4A25 20050222000502005022200050EU 2005 2 22 DHL2004362007 120040627A3240 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01362DH 84 PRIOR TO TAKEOFF, WHEN SELECTING AUTO BRAKES TO MAX, NORMAL BRAKING WAS LOST, THEN AUTOBRAKES OFF LIGHT WENT AMBER AND NORMAL BRAKING RETURNED. AUTOBRAKES COULD NOT BE SELECTED WITH BRAKES APPLIED. AFTER LANDING AUTOBRAKES DISENGAGE WHEN MANUALLY APPLYING BRAKES AUTOBRAKES THEN RE-ENGAGE WHEN MANUAL BRAKES ARE NO LONGER APPLIED. DEFER FURTHER T/S AND REPAIR REF MEL 32.42.07. AUTOBRAKE SYS DMI17037 PLACARD INSTALLED. 2L72 4F RTA35EU 20050222000522005022200052NM 2005 2 22 ASA0440243 120041201A5320693535214 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CRACKED STRINGER CLIP. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050222000552005022200055NM 2005 2 22 ASA0440238 120041203A532065596593 WEB BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FORWARD CARGO DOOR CUTOUT, LOWER FORWARD CLOSE OUT WEB DENTED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050222000622005022200062EU 2005 2 22 XNOA1191 120040629A2150 A/C PACK AIRBUS300 A300B4203 3930306EU NR 1 SHUTDOWN A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23472AS 125 ON TAXI, NR 1 PACK SHUT-OFF. RE-SEATED CIRCUIT BREAKER AND OPS CHECK GOOD IAW A300 AMM CHAPTER 21-51-00. 2L72 4F RTA35EU 20050222000642005022200064NM 2005 2 22 04FDEA01709 120040614A5744ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 2.252 INCH, FINAL DIAMETER = 2.323 INCH. COMPLIED WITH FEDEX EA NR 1-5740-76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222000662005022200066NM 2005 2 22 04FDEA01724 120040614A5753ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIA 1.187 INCH, FINAL DIA 1.282 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76743, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20050222000672005022200067NM 2005 2 22 04FDEA01725 120040614A5753ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL THICKNESS=0.652 INCH, REMAINING THICKNESS=0.585 INCH, MATERIAL REMOVED=0.067 INCH, AND FOUND WITHIN LIMIT AS PER CMM 57-52-03. 2L73 4F RTA22WE 20050222000682005022200068NM 2005 2 22 04FDEA01726 120040614A5744ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORROSION. REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.006 INCH, REMAINING THICKNESS = 0.421 INCH FOUND WITHIN TOLERANCE OF DWG ARC0502. 2L73 4F RTA22WE 20050222000692005022200069NM 2005 2 22 04FDEA01727 120040614A5744ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER=0.641 INCH, FINAL DIAMETER 0.711 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5740-76742, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222000752005022200075NM 2005 2 22 04FDEA01872 120040628A5753ARC2518U502 STRAP DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP P/N ARC2518U502, REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050222000772005022200077WP 2005 2 22 04FDEA01901 120040701A5753 HINGE DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25559FE 46930 DURING P TO F MODIFICATION AND TRANSATION CHECK FOUND LEFT OUTBOARD FLAP HINGE FWD SECTION STA XW 486 WITH OXIDATION WHERE CONTACT STUD BOLTS. REMOVED CORROSION AT BARREL NUT CORRESPONDING SIDE LOAD FITTING BOLT HOLE IAW CMM 57-44-08, INSTALLED BUSHING IAW CMM 57-44-08FIG 404. 2L73 4F A22WE 20050222000802005022200080SW 2005 2 22 ALGA095923 120040630A6230406310406101 BEARING BELL 407 407 1182206SW M/R GEARBOX OUT OF TOLERANCEE ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03647AL383 53357 MAIN ROTOR GEARBOX BEARING HAS RADIAL PLAY BEYOND MAX LIMITS. REPLACED WITH 4EA NEW PARTS. 1G71 3U O H2SW 20050222000862005022200086WP 2005 2 22 04FDEA01921 120040703A5320 ANGLE DOUG DC10 DC1030 3023501WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 ZONE 316 FORWARD UPPER BULKHEAD ANGLE IS CRACKED AT STATION 2164 BULKHEAD TO FUSELAGE SKIN ATTACH ANGLE AT RBL 8. PERFORMED DYE PEN CHECK, FOUND 1 INCH CRACK, REMOVED DAMAGED ANGLE AND INTERCOSTAL CLIPS IAW DC10 SRM 51-35-01 VOL II. FABRICATED AND INSTALLED REPAIR COMPONENTS (FILLER AND ANGLE) AND REINSTALLED INTERCOSTAL CLIPS IAW DC10 SRM 53-00-01 VOL I, DC 10 SRM 51-31-01 VOL II AND DAC DWG AJC7615. REFERENCE N/R N00348. 2L73 4F A22WE 20050222000882005022200088NM 2005 2 22 DHL2004784003 120040707A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE GROUNDED A DHLAO OTHER J WARNING INDICATION CRCRUISE 1 SO01784DH 22001 NR 3 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT IS ILLUMINATED. REPOSITIONED NR 3 ENGINE GROUND FAULT FIRE DETECTOR LOOP. CLOSED AND RESECURRED NR 3 ENGINE COWL. TESTED ENGINE FIRE DETECTION IAW B727 M/M 26-11-001. NO DEFECTS NOTED. 2L73 4F A3WE 20050222000902005022200090NM 2005 2 22 ASA0440242 120041201A532065453132 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CRACKED STRINGER CLIP. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050222000932005022200093CE 2005 2 22 GLBA20030649 120040620A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03192GL UE192 LT FUSELAGE BELLY SKIN CORROSION STRINGER 16, REPAIRED. 2L72 4T RTA24CE 20050222000982005022200098CE 2005 2 22 GLBA20030641 120040613A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03254GL UE254 FUSELAGE SKIN CORRODED AND CRACKED AT STRINGERS 15 AND 16 APPEX FUSELAGE STATIONS 243.0 AND 258.0, REPAIRED. 2L72 4T RTA24CE 20050222000992005022200099CE 2005 2 22 GLBA20030640 120040614A5260 DOOR BEECH 1900 1900D 1154162CE AIRSTAIR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03257GL UE257 AIRSTAIR DOOR HAS CORROSION, REPAIRED. 2L72 4T RTA24CE 20050222001002005022200100NM 2005 2 22 C8GA20040010 120040708A793142D107A2 SWITCH BOEING727 727223 1384074NM NR 1 ENGINE DEFECTIVE A C8GAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO15715AA 22470 DURING TAKEOFF ROLL, THE NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON AT 80 KNOTS. ABORTED TAKEOFF AND RETURNED TO RAMP WITH NO FURTHER INCIDENT. DMI THE NR 1 ENGINE LOW OIL PRESSURE LIGHT UNDER MEL 79-4. AIRCRAFT RETURNED TO SERVICE. CLEARED MEL 79-4 ON 7/8/2004 UPON ARRIVING IN KFLL BY REPLACING THE LOW OIL PRESSURE LIGHT SWITCH IAW B727 MM 79-33-0. OPERATIONAL SYSTEM CHECKED GOOD IAW B727 MM 79-32-0 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050222001012005022200101 2005 2 22 HAEA00135 420040331A342225883023 GYRO AMD FALC20FALCON 2720302EU COCKPIT ACTIVE E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05165TW1334013340 65 PILOT REPORTED CAPT'S DG STUCK ON RUNWAY HEADING, RETURN TO DEPARTURE AIRPORT. MAINTENANCE COULD NOT DULICATE. CK GOOD ON ALL HEADINGS IAW WITH FALCON 20 M/M. 2L72 4F A7EU 20050222001032005022200103EU 2005 2 22 HAEA00154 120040712A2197 CIRCUIT BREAKER AMD FALC20FALCON 2720302EU AIR CON TRIPPED E HAEAA UNSCHED LANDING O OTHER CLCLIMB 1 SW05158TW 158 AIRCRAFT DEPARTED GSO, ON CLIMB-OUT CABIN FAILED TO PRESSURIZE. CREW NOTICED A/C VALVE C/B POPPED. AIRCRAFT RETURNED GSO. MORE INFORMATION TO BE ADDED WHEN AVAILABLE. 2L72 4F A7EU 20050222001042005022200104NM 2005 2 22 ASA0440236 120041203A5320654659247 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND AFT CARGO FLOOR SUPPORT CORRODED. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050222001052005022200105WP 2005 2 22 04FDEA02031 120040708A3620 CONTROL UNIT DOUG MD10 MD1010F 3022112WP NR 2 MANIFOLD MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25550FE 46521 NR 2 MANIFOLD FAIL ALERT ILLUMINATED IN FLIGHT. DIVERTED TO STL PER THE QRH, ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 CATEGORY: C EXPIRATION: 18JUL04. NR 2 MANIFOLD FAIL DETECTION LOOP INOP. MX MUST CLEAR ALERT PRIOR TO EACH DISPATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. REMOVED AND REPLACED MANIFOLD FAILURE DETECTION CONTROL UNIT PER M/M 36-23-01-4, ALL SYSTEM TESTS PASS. 2L73 4F RTA22WE 20050222001072005022200107NE 2005 2 22 00133 220040320A7200CJ6106 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LEFT FLAMED OUT E HAEAB EMER. DESCENT XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW05888TW9885 9885 292 249SC104A PILOT REPORTED, LT ENGINE FLAMED OUT CLIMBING THRU FL38.5, ENGINE RELET AT FL25. CONTINUED FLIGHT WITH NO FURTHER PROBLEM, PILOT INSPECTED ENGINE AT DESTINATION NO FOD DAMAGE OR LEAKS, AIRCRAFT ROUTED TO MAINTENANCE BASE. YIP, MAINTENANCE PERFORMED FLAMEOUT INSPECTION, GROUND RUNS AND LEAK CHECKS, NO DEFECTS NOTED, AIRCRAFT RETURN TO SERVICE. 2L72 4J4 J A10CE 1E16 20050222001112005022200111NM 2005 2 22 C8GA20040013 120040720A3230H1010153 SWITCH BOEING727 727227 1384078NM NLG DEFECTIVE A C8GAO OTHER J WARNING INDICATION APAPPROACH 1 SO15894276047 21365 ON APPROACH INTO KMIA, THE NOSE GEAR DID NOT EXTEND WHEN THE GEAR WAS LOWERED. GEAR WAS RECYCLED PER CCIA AOM AND THE RED LIGHT STAY ON, NO GREEN LIGHT. EXECUTED A GO AROUND AND MANUALLY LOWERED THE NOSE GEAR, CONFIRMED GEAR DOWN AN ADVISED ATC, DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE NOSE LANDING GEAR DOWN LOCK SWITCH WAS REPLACED. ALSO, LUBED THE NOSE LANDING GEAR AND PERFORMED GEAR EXTENSION AND RETRACTION TEST. OBSERVED NORMAL OPERATIONS FOR ALL TEST AND NO DEFECTS NOTED IAW B727 MM 32-31-15, 12-00-0 AND 32-33-0 PAGE 502 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050222001132005022200113NM 2005 2 22 04FDEA01942 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, SIDE LINK MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.495 INCH, MATERIAL REMOVED=0.003 INCH, REMAINING THICKNESS=0.492 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222001142005022200114NM 2005 2 22 04FDEA01943 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.248 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222001192005022200119SW 2005 2 22 AC2A096517 120040714A243239563001 BATTERY PACK BELL 430 430 1182150SW MASTER FAILED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CV 49072 BATTERY PACK FAILED CAPACITY TEST. REPLACED BATTERY. 1G72 3U RTH9SW 20050222001202005022200120SW 2005 2 22 AC2A096518 120040722A243239563001 BATTERY PACK BELL 430 430 1182150SW MASTER FAILED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CH 49037 BATTERY PACK FAILED CAPACITY TEST. EPLACED PART WITH A NEW UNIT. 1G72 3U RTH9SW 20050222001262005022200126NE 2005 2 22 ALGA096398 120040720A65107636104008103 COUPLING SKRSKYS76 S76C 8143008NE TAIL ROTOR DISC CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03861AL1286 760529 FOUND 1 CRACKED DISC. REPLACED ASSY W/NEW BY FIELD MAINTENANCE. 1G72 3U NCH1NE 20050222001302005022200130NM 2005 2 22 ASA0440237 120041203A5320654659247 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FLOOR SUPPORT CORRODED. REPAIRED PER EA. (M) 2L72 4F RTA16WE 20050222001532005022200153NE 2005 2 22 NACA20040053 220041030A7421 SPARK PLUG PWA CB3 DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE NR 16 CYLINDER CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03779TA88 88 P34011 45529 P34011 NR 3 ENGINE SHUT DOWN DUE TO NR 10 CYLINDER DOUBLE SHORTED SECONDARY. REMOVED AND INSPECTED NR 10 CYLINDER SPARK PLUGS, FOUND NO DEFECTS. SHORTED NR 10 CYLINDER TO VERIFY TIMING. FOUND TO BE OFF 6 PATTERNS. REMOVED AND REPLACED NR 16 CYLINDER FRONT SPARK PLUG FOR CRACKED CERAMIC AND NR 16 CYLINDER REAR PLUG AND SHORT LEAD. OP CHECKED GOOD. 2L74 4R4 R A781 5E8 20050222001542005022200154NM 2005 2 22 04FDEA01903 120040701A5753ARC40082 FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING, THREE (3) HOLES FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING CORROSION REMOVED AS PER SRM 51-21-00 VOLUME II. (1) OUTBOARD MIDDLE HOLE: ORIGINAL DIAMETER = 0.583 INCH, FINAL DIAMETER = 0.653 INCH, (2) INBOARD FORWARD HOLE: ORIGINAL DIAMETER = 0.567 INCH, FINAL DIAMETER = 0.630 INCH (3) OUTBOARD FORWARD HOLE: ORIGINAL DIAMETER = 0.630 INCH, FINAL DIAMETER = 0.699 INCH COMPLIED WITH FEDEX EA NR 1-5750-76755, WINGS, RIGHT OUTBOARD FLAP, SUPPORTS CORRODED. 2L73 4F RTA22WE 20050222001552005022200155NM 2005 2 22 04FDEA01940 120040706A5320A5A71241 SPLICE DOUG MD11 MD11F 3023600NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R. REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PART MARKED FX A5A7124-1 PER GMM 7-0-1001. 2L73 4F RTA22WE 20050222001562005022200156NM 2005 2 22 04FDEA01946 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001582005022200158NM 2005 2 22 04FDEA01948 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.404 INCH, MATERIAL REMOVED = 0.002 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001602005022200160NM 2005 2 22 04FDEA01950 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 INCH, MATERIAL REMOVED = 0.010 INCH, REMAINING THICKNESS = 0.487 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001612005022200161NM 2005 2 22 04FDEA01951 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.505 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.502 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001622005022200162NM 2005 2 22 04FDEA01952 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 INCH, FINAL DIAMETER = 1.127 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001642005022200164NM 2005 2 22 04FDEA01954 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.093 INCH; FINAL DIAMETER: 1.147 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001662005022200166NM 2005 2 22 04FDEA01956 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.514 INCH; MATERIAL REMOVED 0.004 INCH; REMAINING THICKNESS: 0.510" AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001672005022200167NM 2005 2 22 04FDEA01957 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.482 INCH; MATERIAL REMOVED 0.006 INCH; REMAINING THICKNESS: 0.476 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001682005022200168NM 2005 2 22 DHL2004765006 120040728A7711 INDICATOR BOEING727 727264 138408MNM NR 1 EPR MALFUNCTIONED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01765AT 23014 RTO FOR NR 1 ENGINE EPR GAUGE WOULD NOT ADVANCE PAST 1.6 EPR AND FLUCTUATED WILDLY. WEIGHT 180.0 IAS, 70 KTS OAT, 14 DEGREES C PA, 897 FT. DEFERRED NR 1 ENGINE EPR PER 77-1-1 CONTROL NR 17349 PLACARD INSTALLED DEFERRED BY 35840. 2L73 4F A3WE 20050222001712005022200171CE 2005 2 22 GLBA20030682 120040727A52101292140591 CABLE BEECH 1900 1900D 1154162CE DOOR LATCH INOPERATIVE A GLBAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM03219GL UE219 CABIN DOOR WOULD NOT OPEN, REPLACED DOOR CABLE. 2L72 4T RTA24CE 20050222001722005022200172NM 2005 2 22 04FDEA01902 120040701A5753ARC40092 SUPPORT FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE REPAIRED PER FEDEX EA NR 1-5750-76755, WINGS, RIGHT OUTBOARD FLAP, SUPPORTS CORRODED. 2L73 4F RTA22WE 20050222001732005022200173NM 2005 2 22 DHL2004745510 120040702A5330 SKIN BOEING727 727224 1384076NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, LT FUSE HAS A DENT AFT BS 560 ABOVE STR 27L. DAMAGE FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 57/8 X 21/4 AND FABBED FILLER FROM 2024 T3 .040 PO NR 9001030 DIM 57/8 X 1 AND DOUBLER FROM 2024 T3 .063 PO NR 9001061 DIM 281/4"X91/4" IAW 727 SRM 53-30-3 FIG3. PARTS TREATED, PRIMED AND INSTALLED IAW 727 SRM 51-10-2 AND 53-30-3 FIG 3. 2L73 4F A3WE 20050222001782005022200178WP 2005 2 22 04FDEA02318 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AT APPROXIMATELY 11 0`CLOCK POSITION 14 4/5 INCHED FROM RIGHT HAND PRIMARY STATIC PORT, THE SKIN IS DIMPLED APPROXIMATELY .022 INCHES. REWORKED DENT IAW MD10 SRM 53-20-00 VOL I, PERFORMED HFEC IAW NDT MANUAL SPM 06-10-10 .001. NO CRACKS FOUND. DENT WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. PERFORMED RVSM INSPECTION OF THE NOTED DISCREPANT AREA, MEASUREMENT -0.001, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2. REF. N/R N00228. 2L73 4F RTA22WE 20050222001792005022200179 2005 2 22 IXXA0400100O 420040731A3497 WIRE DOUG DC8 DC871F 302199DWP RADAR BROKEN A IXXAA UNSCHED LANDING O OTHER CRCRUISE 1 SW11830BX7593416 45973 DURING CRUISE FROM KTOL, RADAR HAD A TENUATION NOISE BAND AT 20 MILE MARKER RUNNING COMPLETELY ACROSS DISPLAY IN ANY RANGE SELECTED. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED DEFECTIVE SPLICES BEHIND PLUG D10-61 IN RADIO RACK AND RADAR OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050222001802005022200180EU 2005 2 22 109080304 120040803A14201090130201 CONNECTOR AGUSTAA109 A109 0260109EU COCKPIT DAMAGED B JBZRO OTHER O OTHER NRNOT REPORTED 1 WP2721RX 7131 PILOT REPORTED MILD CASE OF TAIL ROTOR AUTHORITY LOSS AT GROSS WEIGHT AND WITH ABOVE NORMAL AMBIENT TEMPERATURES, AND REQUESTED MECHANIC TO CHECK OUT TAIL ROTOR SYSTEM. MECHANIC NOTICED TAIL ROTOR PITCH/PULL ROD HAD A GREATER AMOUNT OF THREAD SHOWING THAN ON OTHER A109A HELICOPTERS IN OUR FLEET. ADDITIONALLY, THE SPACE BETWEEN THE BELLCRANK AND TAIL ROTOR GEARBOX WAS LESS THAN SIMILAR AIRCRAFT IN FLEET. AFTER MUCH INVESTIGATION IT WAS FOUND THAT A SET OF RIGID CONNECTOR LINKS WERE LONGER THAN THOSE ON OUR FLEET. THE AGUSTA IPB FOR THE A MODEL AIRCRAFT SPECIFIES P/N 109-0130-20-1. THE SUSPECT LINKS ARE APPROXIMATELY 1/2 INCH LONGER THAN P/N 109-0130-20-1. OUR ONLY SOURCE FOR THESE PARTS IS AGUSTA. OUR PAR1G72 3U H7EU 20050222001832005022200183 2005 2 22 P9RA20040027 420040807A256560B4001842 PROXIMITY SENSOR BOEING757 757236 1384971NM 1L DOOR SLIDE OUT OF ADJUST A P9RAO OTHER O OTHER NRNOT REPORTED 1 SO11521NA39533 25592 1L DOOR "ARMED" LIGHT NOT ON WITH DOOR IN ARMED POSITION. CLEANED AND ADJUSTED PROXIMITY SWITCHS FOR 1L DOOR SLIDE LIGHT IAW MM 256611. INDICATION WORKING NORMALLY. 2L72 4F RTA2NM 20050222001872005022200187NE 2005 2 22 ERAA096622 120040409A62107615009100052A BLADE SKRSKYS76 S76A 8143006NE MAIN ROTOR PEELING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03576EH 760212 TRIM TAD PEALING/SEPARATED. INSPECTED, PERFORMED X RAY ULTRASONIC INSPECTIONS PER QATI 3048, 3016, SS8806 & 3095, PERFORMED ALL INSPECTIONS UP TO AND INCLUDING 900 HOUR INSPECTIONS, COMPLIED WITH AD 884-10-02 & ASB 76-65-18C; REPLACED TRIM TAB 1 ER PER RS-006K-III; REPLACED NICKEL STRIP PER RS-007J-1; REPLACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9; REPLACED 4 EA ROOT END THROUGH BUSHINGS PER RS-004N-VII; REINSTALLED TIP CAP SN A175-03282; REFINISHED WITH HIGH VIS SCHEME 2 PER SA 4047-76-5 DRWG 76150-09000 AND 76150-09100; STATIC BALANCED PER CTI-DAL-DA-026 @ TT 9172.0 1G72 3U H1NE 20050222001912005022200191SW 2005 2 22 ERAA096627 120040504A6410212010750105FM BLADE BELL 412 412 1182202SW TAIL ROTOR DAMAGED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03168EH2695 T/R BLADE HAS VOID AT OUTBOARD TIP, SKIN LIFTING. SENT TO CTI FOR REPAIR. INSPECTED PER 204-099-223 VOLUME X SECTION 1.1 AND 1.2 REV 1; COMPLIED WITH ASB 412-00-106; REPAIRED SKIN DAMAGE AT TIP FWD EDGE ON BOTH SURFACES PER 212-64-10-002 AND 8110-38497; REPLACED BUFFER PADS 4 EA PER 212 CR&O 64-35; REFINISHED PER BPS 4488 AND FED-STD-595 STATIC BALANCED PER DPS 17M PARAGRAPH 3.6 AT TT 2695.4 1G72 4U H4SW 20050222001922005022200192SW 2005 2 22 ERAA096628 120040324A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR CRACKED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03417EH10351 33031 M/R BLADE HAS CRACKS, VOIDS AT STA 90. SENT TO CTI FOR REPAIR INSPECTED, PERFORMED 2500 HOUR INSPECTIONS AND REPAIRED. 1G72 4U H4SW 20050217000092005021700009WP 2005 2 17 ASAA0480627 120041229A33506011779 POWER SUPPLY DOUG DC9 DC983 3022083WP EMERGENCY LIGHT DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS16495118 53076 DURING LINE CHECK, FOUND OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050217000122005021700012NM 2005 2 17 ASA0440304 120041213A532065C335821 WEB BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON HORIZONTAL WEB. REMOVED WEB, FABRICATED NEW WEB, AND INSTALLED. (M) 2L72 4F RTA16WE 20050217000132005021700013NM 2005 2 17 ASAA0470048 120041228A5210147A61861 STRUCTURE BOEING737 737790 13844CNNM L1 DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02619AS 30164 PAE - FOUND DURING SI C-CHECK, DENT ON L1 DOOR UPPER RIGHT CORNER AT BS 344. REPAIRED IAW SRM 52-00-01. (M) 2L72 4F RTA16WE 20050217000142005021700014NM 2005 2 17 ASAA0470045 120041115A5320146A7502 SUPPORT BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE - FOUND DURING MAINTENANCE CHECK, CORROSION ON SIDEWALL SUPPORT AT STATION 727. REPAIRED IAW SRM 53-00-53. (M) 2L72 4F RTA16WE 20050217000182005021700018NM 2005 2 17 ASA0440322 120041214A5330 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01754AS 25095 OKC - FOUND FUSELAGE SKIN HAS 2 EACH DENTS WITHIN 10 INCHES OF E/E BAY DOOR CUTOUT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER AS EA AND AAR EA. P/N'S 6545800-1, 6545815-65. (M) 2L72 4F RTA16WE 20050217000192005021700019NM 2005 2 17 ASA0440321 120041212A5754 SKIN BOEING737 7374Q8 138447QNM TE FLAP SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02754AS 25095 OKC - FOUND RIGHT OUTBOARD FLAP UPPER SURFACE IS SCRATCHED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CORE PLUG AND DOUBLER IAW SRM. (M) 2L72 4F RTA16WE 20050217000312005021700031NM 2005 2 17 ASA0440292 120041210A531565C3394311 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOORBEAM UPPER FLANGE. CORROSION FOUND OUT OF LIMITS, REPAIRED FLOORBEAM. (M) 2L72 4F RTA16WE 20050217000382005021700038NM 2005 2 17 ASA0440282 120041207A5310654587512 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON L-ANGLE OF RIGHT CREASE BEAM. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000422005021700042NM 2005 2 17 ASA0440251 120041202A532065C362151 WEB BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01765AS 25102 PAE - FOUND DENT IN FORWARD CARGO INNER WEB. FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050217000432005021700043NM 2005 2 17 ASA0440250 120041202A523065C362151 STRUCTURE BOEING737 7374Q8 138447QNM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT IN EDGE OF LIGHTING HOLE, FORWARD CARGO DOOR INNER SURFACE AT UPPER FORWARD CORNER. CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20050217000492005021700049NM 2005 2 17 ASA0440324 120041214A533065464861 SKIN PANEL BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02754AS 25095 OKC - FOUND PANEL 7420 HAS DENT AFT SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER PER SRM. (M) 2L72 4F RTA16WE 20050217000682005021700068NM 2005 2 17 ASA0440272 120041208A53206555726U86 SUPPORT ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO BAY SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE. (M) 2L72 4F RTA16WE 20050217000732005021700073NM 2005 2 17 ASAA0440265 120041208A532065C3184778 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (M) 2L72 4F RTA16WE 20050217000762005021700076NM 2005 2 17 ASA0440255 120041205A53206545807U30 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND UPPER LOBE ANGLE CRACKED. REPLACED UPPER LOBE ANGLE. (M) 2L72 4F RTA16WE 20050217000852005021700085NM 2005 2 17 ASA0440252 120041205A532065C2730887 SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FORWARD CARGO SIDEWALL SUPPORT IS GOUGED. INSTALLED NEW SIDEWALL SUPPORT. (M) 2L72 4F RTA16WE 20050217000872005021700087NM 2005 2 17 ASA0440247 120041202A53156546811 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 FOUND CORROSION FUSELAGE UPPER LOBE, FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED FLOORBEAM. (M) 2L72 4F RTA16WE 20050217000962005021700096NM 2005 2 17 ASA0440332 120041215A53206545834260 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 FOUND CORROSION ON FLOOR SUPPORT. REPLACED PER AMM. (M) 2L72 4F RTA16WE 20050217000972005021700097NM 2005 2 17 ASA0440331 120041215A53116552255511 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FRAME DAMAGED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217000992005021700099NM 2005 2 17 ASA0440325 120041214A53106545875070 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON INBOARD CHORD OF RT CREASE BEAM, MOPSILL. REPLACED MOPSILL, CREASE BEAM. (M) 2L72 4F RTA16WE 20050217001012005021700101NM 2005 2 17 ASA0440314 120041212A53106517688165 CREASE BEAM BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON INBOARD CREASE BEAM CHORD, MOPSILL. REPLACED CREASE BEAM CHORD. (M) 2L72 4F RTA16WE 20050217001042005021700104NM 2005 2 17 ASA0440305 120041210A53116545807 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND FRAME CRACKED. REPLACED PER EA. (M) 2L72 4F RTA16WE 20050217001062005021700106NM 2005 2 17 ASA0440309 120041210A5320692471 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON Z-ANGLE. REPLACED Z-ANGLE. REPLACED Z-ANGLE PER SRM. (M) 2L72 4F RTA16WE 20050217001082005021700108NM 2005 2 17 ASA0440312 120041211A53116546595260 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT ON TOP OF FRAME FLANGES. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050217001122005021700112NM 2005 2 17 ASA0440303 120041213A532069331354 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND DRILL START IN U-CHANNEL ON INTERCOSTAL. REPLACED U-CHANNEL ON INTERCOSTAL. (M) 2L72 4F RTA16WE 20050217001222005021700122NM 2005 2 17 ASA0440326 120041214A53116546596163 FRAME BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND DENT ON TOP OF FRAME FLANGE. REPLACED FLANGE. (M) 2L72 4F RTA16WE 20050217001292005021700129EU 2005 2 17 MALA040948 120041216A3350330131 BATTERY SAAB SF340 340B 7860101EU EMERGENCY LIGHT FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15447XJ 340B447 BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS, A/C RETURNED TO SERVICE 12/23/04. 2L72 4T RTA52EU 20050217001302005021700130EU 2005 2 17 MALA040950 120041218A33506122741 BATTERY BAC 146 AVRO146RJ85A1500097EU EMERGENCY LIGHT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15526XJ E2351 BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/23/2004. 2H74 4F RTA49EU 20050218000302005021800030NM 2005 2 18 04FDEA03315 120041201A5740ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. 2L73 4F RTA22WE 20050218000382005021800038NM 2005 2 18 04FDEA03399 120041209A5753ARC0154501 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-07 PAGES 403- 404. 2L73 4F RTA22WE 20050222000082005022200008SW 2005 2 22 AC2A094947 120040207A6510430010105105 PLATE BELL 430 430 1182150SW TAIL ROTOR WORN B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CH6588 49037 PLATE IS WORN. CONTACT WEAR BY RESTRAINT. REPLACED CLAMP SET. 1G72 3U RTH9SW 20050222000122005022200012SW 2005 2 22 ERAA095244 120040416A6310212040176007 BOOT BELL 412 412 1182202SW TRANSMISSION DAMAGED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH91 33064 BOOT HAS ONLY 91.4 HOURS AND WAS INSTALLED 2/2004 AND IS ALREADY DEBONDING ON TORE INBOARD AREA. RETURNING TO BELL ON ERA PACK SLIP 5944 REQUESTING CREDIT. 1G72 4U H4SW 20050222000182005022200018SW 2005 2 22 HEEA095227 120040505A2612872203 FIRE LOOP BELL 212 212 1181420SW NR 2 ENGINE FALSE INDICATIONE HEEAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SW033131S 30953 AIRCRAFT WAS INBOUND FROM MALONGO WHEN THE NR 2 ENGINE FIRE LIGHT CAME ON. PULLED TEE HANDLE AND FIRE BOTTLE FIRED, BUT LIGHT STAYED ON. FIRED THE RESERVE BOTTLE AND THE LIGHT WENT OUT. 1G71 4U H4SW 20050222000272005022200027CE 2005 2 22 GLBA20030645 120040620A329711436406811 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE MLG TRIPPED A GLBAO OTHER J WARNING INDICATION CRCRUISE 1 NM03253GL UE253 LANDING GEAR RELAY CB POPS IN CRUISE, RESEATED P552 ON PCB A316. 2L72 4T RTA24CE 20050222000332005022200033 2005 2 22 TSAA0434049 420040621A34132074021 INDICATOR BOEING737 7372X6C 1384552NM VERT SPEED FAILED A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13817AL 23292 CAPTAINS VERTICAL SPEED INDICATOR INOPERATIVE. RETURN TO HNL. REPLACED VERTICAL SPEED INDICATOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050222000352005022200035NM 2005 2 22 DHL2004760006 120040624A2612 WARNING LIGHT BOEING727 7272B7 138407LNM CARGO BAY FIRE FALSE ACTIVATIONA DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01760AT 21954 ON PREFLIGHT, FOUND LOWER AFT CARGO FIRE LIGHT ILLUMINATED. TRANSFERED TO DMI NR 17008 PER ASTAR MEL 26-19 CAT C SEE SP 26-19. PLACARD INSTALLED EMP NR 35944. 2L73 4F A3WE 20050222000382005022200038NM 2005 2 22 XNOA1190 120040624A3260 WARNING LIGHT BOEING727 727227 1384078NM NLG FALSE INDICATIONA XN0AO OTHER N FALSE WARNING DEDESCENT 1 GL2376753 21249 NOSE LANDING GEAR WARNING LIGHT REMAINS ILLUMINATED WITH NO GEAR EXTENSION, DURING GEAR EXTENSION. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST. LUBED NOSE LANDING GEAR PER B727 M/M CHAPTER 12-12-11. PERFORMED L/G CONTROL SYSTEM ADJUSTMENT AND TEST PER B727 M/M CHAPTER 32-31-0. NO DEFECTS NOTED. EXERCISED NOSE GEAR LOCK SWITCH. OPS CK NORMAL. INSPECTED CABLES AND GEAR SELECTOR VALVE. NO DEFECTS NOTED. 2L73 4F A3WE 20050222000422005022200042WP 2005 2 22 04FDEA01852 120040624A3260 MECHANISM DOUG DC10 DC1010F 3022111WP MLG HANDLE DIRTY A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO2568059 46907 GEAR HANDLE DOWN AND IN RED LIGHTS AT BOTH PANELS. UNABLE TO CHECK ANTI-SKID TEST. QRH COMPLETED. RECYCLED GEAR ALL LIGHTS GREEN ANTI-SKID TEST NORMAL. TWR VISUAL CK GEAR DOWN. PER CAPTAIN DEBRIEF, WHEN RED LIGHTS WERE ILLUMINATED, THE HANDLE WAS SLIGHTLY JIGGLED AND ALL SAFE LIGHTS ILLUMINATED. THE CREW THEN CYCLED THE GEAR AND ALL INDICATIONS WERE NORMAL. PERFORMED THE LANDING GEAR CONTROL MECHANISM CLEANING AND LUBE PER M/M 32-31-02-7. INDICATIONS NORMAL. ANTI-SKID TEST NORMAL PER M/M 32-45-01-2. A/C OKAY FOR SERVICE. 2L73 4F A22WE 20050222000432005022200043NM 2005 2 22 04FDEA01865 120040626A7700 WARNING LIGHT BOEING727 727227 1384078NM COCKPIT ILLUMINATED A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO25483FE 21465 WENT TO FIREWALL POWER ON TCAS ALERT AT 5000 FT, FIREWALL POWER LESS THAN 10 SECS. IN WORK ADDITIONAL TSI 34-55-6491 ISSUED TO REMOVE TCAS PROCESSOR FOR BENCH DOWNLOAD/READOUT. ADDITIONAL TSI 23-70-6490 ISSUED TO REMOVE CVR FOR BENCH READOUT. PER VERBAL INFO A/C WAS AT 5000 LEVEL. INTRUDER SINGLE ENG WAS AT 4000 AND CLIMBING. TYS TOWER CONFIRMED. 99 DAY HISTORY SHOWS NO TCAS RA PROBLEMS. COMPLETED INLET/EXHAUST INSPECTION AND FIREWALL AND/OR EMERGENCY ESCAPE CHECK PER JRH 6-38. ALL CHECKS OK, RETURNED TO SERVICE PER EA 7-7200-78554. 2L73 4F A3WE 20050222000492005022200049WP 2005 2 22 IXXA0400096S 120040525A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11830BX759182677 45973 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FORWARD CENTER SECTION INTERIM REPAIR AROUND STA FS 356.00, L-25L. REPAIR WAS ACCOMPLISHED. REMOVED EXTERNAL CIRCULAR DOUBLER IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7. CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FINGER DOUBLER WITH NEW FASTENERS IAW ALL APPLICABLE MANUALS. 2L74 4F RT4A25 20050222000532005022200053NM 2005 2 22 ASA0440245 120041202A53306545807U30 SKIN BOEING737 7374Q8 138447QNM FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND SKIN DENTED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050222000562005022200056NM 2005 2 22 ASA0440239 120041130A53206545834259 FLOOR SUPPORT BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND CORROSION ON FLOOR SUPPORT. REPAIRED AND REPLACED PART PER SRM. (M) 2L72 4F RTA16WE 20050222000592005022200059NM 2005 2 22 TSAA0475050 120040628A7500655812310 DUCT BOEING737 7372X6C 1384552NM NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13817AL 23292 DURING CLIMB-OUT, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. RETURNED TO HNL. REMOVED AND REPLACED THE NR 2 ENGINE NOSE-COWL ANTI-ICE DUCT DUE TO LEAK AT THE BELLOWS. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050222000632005022200063WP 2005 2 22 DHL2004807011 120040701A2612 WARNING LIGHT DOUG DC8 DC873F 302199FWP CARGO FIRE DET ILLUMINATED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01807DH 45990 DURING CRUISE FLIGHT, LOWER CARGO FIRE "MX" LIGHT ILLUMINATED "SYS OK" LIGHT REMAINED ILLUMINATED. NO DEFECT NOTED, PERFORMED SYSTEM OPS CHECK IAW MM SUPP 26-15-00, OK FOR SERVICE. 2L74 4F RT4A25 20050222000702005022200070NM 2005 2 22 ASA0440241 120041201A532065622445 FITTING BOEING737 7374Q8 138447QNM FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND LOWER AFT LATCH FITTING FOR ASD GOUGED. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050222000852005022200085WP 2005 2 22 04FDEA01925 120040703A5751 SKIN DOUG DC10 DC1030 3023501WP ZONE 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RIGHT HAND WING INBOARD AILERON UPPER SKIN SURFACE HAS NUMEROUSE DENTS. CHECKED LIMITS ON 58 DENTS, 54 DENTS WITHIN LIMITS, 4 DENTS EXCEEDED SRM LIMITS IAW DC10 SRM 51-30-01 VOLUME II. TWO DENTS ON FORWARD UPPER SURFACE AND TWO DENTS ON AFT UPPER SURFACE DAMGE REMOVED AND FABRICATED REPAIRS FOR FOUR REPAIRS IAW 57-00-01 VOLUME I. INSTALLED REPAIRS IAW DC10 SRM 51-35-01 VOLUME II, SRM 51-33-01 VOLUME II AND SRM 51-35-02 VOLUME II. REFERANCE NR N00193. 2L73 4F A22WE 20050222000972005022200097CE 2005 2 22 GLBA20030642 120040616A6120 VALVE BEECH 1900 1900D 1154162CE NR 1 PROPELLER OUT OF ADJUST A GLBAO OTHER S AFFECT SYSTEMS APAPPROACH 1 NM03202GL UE202 NR 1 PROP FEATHERED ON FINAL, ADJ NR 2 FEATHER VALVE, OPS CK GOOD. 2L72 4T RTA24CE 20050222001082005022200108NE 2005 2 22 DJFA2004009 220040712A7200 ENGINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE NR 1 & 2 SHUTDOWN E DJFAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 EA23455CW RK365 PCEJA0511 AFTER STARTING THEIR DESCENT, THE PILOTS NOTICED THAT BOTH ENGINES WERE OUT. DURING DESCENT, THE CREW TRIED STARTING THE NR 2 ENGINE, IT DID NOT START. TRIED THE NR 1 ENGINE IT WOULD NOT START. TRIED THE NR 2 ENGINE AGAIN AND IT STARTED AT ABOUT FL170. DID NOT TRY THE NR 1 ENGINE AGAIN. THE CREW THEN DIVERTED TO KSRQ. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. THIS INCIDENT IS BEING INVESTIGATED BY THE NTSB AND AT THIS POINT THERE HAS BEEN NO CONCLUSION OF THE CAUSE OF THE FAILURE. 2H72 4F4 FRTA16SW E25EA 20050222001092005022200109EU 2005 2 22 203041 120040717A3320 SIGN SAAB SF340 340B 7860101EU CABIN INOPERATIVE A NSVAO OTHER O OTHER NRNOT REPORTED 1 EA27339CJ 340B339 FASTEN SEAT BELT SIGN ON RIGHT SIDE OF CABIN NOT ILLUMINATED. DEFERRED IN ACCORDANCE WITH MEL 33-20-2. 2L72 4T RTA52EU 20050222001162005022200116EU 2005 2 22 XN0A1193 120040727A3150 FUSE AIRBUS300 A300B4203 3930306EU WARNING COMPUTERBLOWN A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL23373PC 218 CONFIG LIGHT ON MWP CAME ON DURING TAXI OUT. RETURNED TO RAMP. REMOVED AND REPLACED FUSE ON MASTER WARNING COMPUTER IAW A-300 STANDARD PRACTICES, OPS CHECKS GOOD IAW A-300 MM 33-15-00. 2L72 4F RTA35EU 20050222001482005022200148NM 2005 2 22 ASA0440240 120041201A532065453136 STRINGER CLIP BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FOUND STRINGER CLIP CRACKED. REPAIRED PER SRM. (M) 2L72 4F RTA16WE 20050222001742005022200174NM 2005 2 22 04FDEA02314 120040730A5730 SKIN DOUG MD11 MD11F 3023600NM ZONE 600 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 RIGHT HAND WING LEADING EDGE SKIN HAS CHAFFING MARKS FROM NR 4, 5, 6 & 7 LEADING EDGE SLATS, ALSO TEFLON PAINT MISSING IN SOME AREAS. CHAFFING AREA IS BETWEEN STATION XOS 660 AND XOS 1005. BLENDED LEADING EDGE BEHIND SLAT NR 4 AND 7, FOUND TO BE OUT OF LIMITS AT XOS 600 AND XOS 594, IAW DC10 SRM 57-10-00 VOL I. FABRICATED DOUBLERS (2 EACH) IAW DC10 SRM 57-10-00 VOL I. ALODINED AND PRIMED DOUBLERS IAW DC10 SRM 51-21-01 VOL II. INSTALLED DOUBLERS IAW DC10 SRM 57-10-00 VOL I; DC10 SRM 51-33-01 VOL II AND DC10 SRM 51-35-01 VOL II. LEADING EDGE BEHIND SLATS 5 AND 6 WAS FOUND TO BE WITHIN LIMITS IAW DC10 SRM 57-10-00 VOL I. 2L73 4F RTA22WE 20050222001762005022200176WP 2005 2 22 04FDEA02316 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AT APPROXIMATELY 8 O’CLOCK POSITION 17 1/2 INCHES FROM CENTER OF RIGHT HAND PRIMARY STATIC PORT, NEAR CARGO DOOR EDGE, THE SKIN IS DIMPLED OUT OF LIMITS. CHECKED LIMITS, LIMITS DEPTH WAS .012 INCHES, BLENDED GOUGE IAW DC10 SRM 53-00-01 VOL I. INSTALLED RIVET IAW DC10 SRM 53-20-00 VIL I, ALODINED AND PRIMED AREA OF SKIN IAW DC10 SRM 51-21- 01 VOL II. PERFORMED RVSM INSPECTION OF NOTED DISCREPANT AREA, MEASUREMENT IS -.001, FOUND TO BE WITHIN LIMITS IAW MD10 MM 34-11-01-2. DAMAGE LOCATED AT FS 880 AT LONGERON 42R. REF N/R N00226. 2L73 4F RTA22WE 20050222001772005022200177WP 2005 2 22 04FDEA02317 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 AT APPROXIMATE 9 O’CLOCK POSITION 16 1/2 INCHES FROM RIGHT HAND PRIMARY STATIC, AT CARGO DOOR EDGE THE SKIN IS DAMAGED OUT OF LIMITS. POLISHED AREA, CHECKED LIMITS, FOUND TO BE WITHIN LIMITS .0042 IAW MD10 AMM 34-11-01-2. PERFORMED RVSM INSPECTION ON NOTED DISCREPANT AREA, MEASUREMENT IS .004, FOUND TO BE WITHIN LIMITS IAW MD10-10 MM 34-11-01-2, REF N/R N00227. 2L73 4F RTA22WE 20050222001862005022200186GL 2005 2 22 ERAA096620 220040502A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 2 ENGINE SPLIT B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH11629 S675 TORQUE SPLITS GOVERNOR READS VERY FAST NR 2 ENGINE GOVERNOR COULDN'T KEEP UP. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20050222001892005022200189SW 2005 2 22 ERAA096625 120040520A79218537651 OIL COOLER BELL 412 412 1182202SW ENGINE DIRTY B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH 33004 HIGH OIL TEMP. TOO MUCH PAINT ON FIN; TOO LITTLE AIR FLOW. DIRTY AND BLOCKED CORE. UNIT WAS CLEANED, FLUSHED, OVERHAULED, TESTED AND INSPECTED. 1G72 4U H4SW 20050222001902005022200190SW 2005 2 22 ERAA096626 120040509A7921209062502101 BLOWER BELL 412 412 1182202SW OIL COOLER DAMAGED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03167EH15277 33089 OIL COOLER BLOWER DUE OVERHAUL. IMPELLER HAS TWO CRACKED BLADES. SPACER BETWEEN BRGS MECHANICALLY DAMAGED. KEY MECHANICALLY DAMAGED. JC/W PRELIMINARY INSPECTION. DISASSEMBLED, STRIPPED PRIMER, SCRAPPED IMPELLER, BRG SPACER AND KEY. FPI AND MPI'D PARTS AS REQUIRED. PRIMED PARTS AS REQUIRED. REPLACED CRACKED, WORN AND DAMAGED PARTS. REASSEMBLED, REPAIRED IAW BELL 412 CR&O CH 79. OVERHAUL IAW ERA 412-CAMP. 1G72 4U H4SW 20050222001942005022200194EU 2005 2 22 ERAA096630 120040527A3212D24873101 FLOAT BOLKMS105 BO105S 5626006EU MLG DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03152EH16701 S701 6 MONTH INSPECTION DUE, NITROGEN CYLINDER SN 812 DUE HYDROTEST 5-04. FLOAT BAG FOUND TO HAVE HOLE IN ONE COMPARTMENT. FLOAT COVER AND FWD END CAP WORN AND TORN. REMOVED NITROGEN CYLINDER SN 812 AND SENT OUT FOR TESTING. INSTALLED 1 EA SERVICEABLE CYLINDER SN 221. REPAIRED HOLE IN FLOAT BAG WITH PATCH USING PROCEDURE IN AIR CRUISERS MM 25-60-95. REMOVED AND REPLACED FLOAT COVER AND FWD END CAP. PERFORM 18 MONTH INSPECTION. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-2. 1G72 3U H3EU 20050222001952005022200195EU 2005 2 22 ERAA096631 120040605A3212D24873102 FLOAT BOLKMS105 BO105A EU MLG LEAKING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH10770 S675 CYLINDER FOUND TO BE LEAKING NITROGEN FROM SQUIB VALVE. PERFORMED 6 MONTH FLOAT INSPECTION AND REPACK. REPAIRED LEAKING SQUIB VALVE BY REPLACING O-RING AND LEATHER BACK UP RING AT VALVE TO MANIFOLD JUNCTION. VERIFIED COMPLIANCE WITH SB NUMBERS 102-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1G72 3U H3EU 20050222001962005022200196EU 2005 2 22 ERAA096632 120040429A63203701020000 OIL COOLER BOLKMS105 BO105A EU M/R GEARBOX MAKING METAL B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH S675 OIL COOLER HAD METAL IN TRANSMISSION OIL FILTER CHANGE IAW BO105 MM. LEAKING IN CORE THE UNIT WAS CLEANED, FLUSHED, OVERHAULED, TESTED AND INSPECTED. UNIT PASSED X RAY INSPETION, NO METAL. 1G72 3U H3EU 20050222001972005022200197NE 2005 2 22 ERAA096633 120040618A63206107435000058 FREEWHEEL UNIT SKRSKYS61 S61A 814210CNE M/R GEARBOX CORRODED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03SPARE SERVICE CORROSION ON TEETH. HAS EXTERNAL CORROSION, PITTING, BEYOND LIMITS ON SPUR GEAR ACTION TAKEN: REPACK UNITS BEING STORED FOR EXTENDED PERIODS. SPUR GEAR CHANGED. 2G72 4U H2EA 20050222001992005022200199 2005 2 22 ERAA096636 420040515A2562453015002 ELT SKRSKYS76 S76 8143010NE CABIN DEFECTIVE B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03574EH 760369 ELT DEFECTIVE INERTIA, G SWITCH TOO SENSITIVE. SENT TO ARTEX FOR REPAIR. FOUND ELT MOUNTED AT 45 DEGREES, SHOULD BE HORIZONTAL. TESTED IAW ARTEX PROCEDURES, REINSTALLED BATTERY PACK. 1G72 3U H1NE 20050222002032005022200203WP 2005 2 22 IXXA0400103O 120040808A2910 B-NUT DOUG DC8 DC862 3021970WP HYD SYSTEM LOOSE A IXXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW11799AL745111276 45922335 DURING TAKEOFF FROM PGUA, HYDRAULIC FLUID DROPPED TO STAND PIPE LEVEL. HYDRAULIC FLUID WAS LEAKING FROM NR 2 ENGINE. AIRCRAFT RETURNED TO PGUA AND LANDED WITH INCIDENT. AN INSPECTION IS ON GOING. INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. MAINTENANCE FOUND HYDRAULIC FLUID DRIPPING FROM NR 2 ENGINE COWL. THE COWL WAS OPENED AND BOTH ENGINE AND COWL WERE CLEANED. DRY MOTORED NR 2 ENGINE AND FOUND HYDRAULIC LEAK AT NR 10 B-NUT BY THE HYDRAULIC FILTER. MAINTENANCE TIGHTENED B-NUT, DRY MOTORED ENGINE AND PERFORMED LEAK CHECK. ALL CHECKS ARE NORMAL PER ALL APPLICABLE MANUALS. NR 2 ENGINE COWL WAS CLOSED AND HYDRAULIC RESEVIOR WAS SERVICED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20050222002042005022200204GL 2005 2 22 HDNR200400001 220040704A7250E23062750 SHIELD BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NOZZLE SEPARATED B HDNAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW03911EB 199 S812 CAE834470 THE NR 1 NOZZLE SHIELD DOME SEPARATED CAUSING THE TURBINE NR 8 BEARING SCAVENGE STRUT TO CLOG WITH CARBON INDUCED BY THE EXCESS HEAT ALLOWED IN THE AREA BY THE MISSING DOME. WHEN THE SCAVENGE FLOW WAS COMPLETELY LOST, THE OIL WAS FORCED THROUGH THE NR 8 LABYRINTH SEAL CAUSING SMOKING AND AN EXTREMELY HIGH RATE OF OIL CONSUMPTION. INSPECTION OF THE NOZZLE SHIELD BRAZE JOINT REVEALS, WHAT APPEARS TO BE, A LACK OF 100 PERCENT BRAZE COVERAGE IN THE JOINT. PART WAS SENT TO EXTEX FOR INVESTIGATION. NOTE THAT THIS APPEARS TO HAVE BEEN CAUSED BY A LACK OF BRAZE MATERIAL AND DIFFERS FROM THE BRAZE CRACKING PROBLEM THAT IS COVERED BY CEB 1370. 1G72 3U3 U H3EU E4CE 20050222002062005022200206EU 2005 2 22 U30A200400010 120040814A2120 ODOR AIRBUS320 A320214 3930316EU COCKPIT/CABIN DETECTED A U30AO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA17260AV 1564 ON INITIAL DESCENT, THE LEAD FLIGHT ATTENDANT ADVISED THE CAPTAIN OF A STRONG SMELL OF BURNING RUBBER AROUND ROW 7. THE FO WENT TO THE CABIN AND CONFIRMED THE SMELL. THERE WAS NO SMOKE AND NO HEAT RADIATING FROM THE FLOOR OR OVERHEAD BINS. THE LEAD FA WAS INSTRUCTED TO MONITOR THE SMELL AND AFTER A FEW MINUTES THE LEAD FA ADVISED THE SMELL WAS INCREASING. THE CAPT DECIDED TO DECLARE AN EMERGENCY TO GET PRIORITY HANDLING INTO DTW. THE SMELL ENTERED THE COCKPIT AND THE CREW DONNED THEIR O2 MASKS. LANDING AT DTW WAS UNEVENTFUL. THE FIRE MARSHALL MET THE FLIGHT AND CONFIRMED NO FIRE IN CARGO. SMELL SEEMED TO DISSIPATE ON LANDING. SMELL WAS NOT PRESENT WHEN MAINTENANCE BOARDED THE AIRCRAFT. 2L72 4F RTA28NM 20050222002082005022200208SO 2005 2 22 ESPA200400004 120040821A5310 STRUCTURE GULSTMG159 G159 3952202SO FUSELAGE BIRD STRIKE E ESPAO OTHER O OTHER APAPPROACH 1 SO11197PA 93 WHILE ON APPROACH AIRCRAFT WAS STRUCK BY A BIRD ON THE LEFT SIDE OF THE FORWARD FUSELAGE. 2L72 4T 1A17 20050222002092005022200209 2005 2 22 U30A200400011 420040820A2565DHE1141 DETECTOR AIRBUS320 A320214 3930316EU PAX DOOR SLIDE INTERMITTENT A U30AK NONE O OTHER ININSP/MAINT 1 EA17261AV 1615 PRIOR TO FLT 105 PHL-FLL, THE 2L PAX/CREW DOOR "ARMED" INDICATION WAS INTERMITTENT. MAINTENANCE INSPECTED AND CONFIRMED INTERMITTENT CONDITION. MAINTENANCE DEFERRED PER MEL 25-60-04-1 AND RETURNED THE AIRCRAFT TO SERVICE. ON 8/21/04, MAINTENANCE REPLACED THE 2L POX/CREW DOOR PROXIMITY DETECTOR 7WN1 PER AMM 52-73-11 PG 401 AND OPS CK'D OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA28NM 20050222002122005022200212CE 2005 2 22 421C083004 120040830A32431036 MASTER CYLINDER CESSNA421 421C 2076016CE BRAKES MALFUNCTIONED B JBZRO OTHER O OTHER TXTAXI/GRND HDL 1 WP27321FL 421C0207 PILOT REPORTED THAT WHILE PERFORMING A SLOW TIGHT LEFT HAND TURN WHILE TAXIING, THE RIGHT HAND PEDAL APPEARED TO DEPRESS BEYOND ITS NORMAL RANGE, RESULTING IN LESS THAN PROPER STOPPING ABILITY. THE PILOT WAS ABLE TO STOP THE AIRCRAFT WITHOUT INCIDENT. SUBSEQUENT BRAKE CHECKS RESULTED IN NO FURTHER DISCREPANCIES. BUT WHEN THE AIRCRAFT WAS PUT IN MX HANGAR AND THE NOSE TURNED TO SIMULATE A TIGHT LEFT HAND TURN, THE BRAKE MASTER CYLINDER ONCE AGAIN APPEARED TO DEPRESS WELL BEYOND ITS NORMAL OPERATIONAL RANGE. UNABLE TO DETERMINE ACTUAL CAUSE OF MASTER CYLINDER FADE/FAILURE. PROCESS INITIATED TO REPLACE CYLINDER. 1L72 3O A7CE 20050222002132005022200213CE 2005 2 22 GLBA20030707 120040830A5320 BRACKET BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03192GL UE192 RT FUSELAGE TO DORSAL FIN L BRACKET PATCH CRACKED AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACED RT FUSELAGE TO DORSAL FIN BRACKET PATCH REF EO 04-VE192-02. 2L72 4T RTA24CE 20050222002192005022200219 2005 2 22 ERAA097081 420040307A25624530190 ELT BOLKMS105 BO105S 5626006EU CABIN CRACKED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03128EH 572 ELT DUE 1 YEAR INSPECTION, CRACKED SUB ASSSEMBLY AND TOP COVE. TESTED IAW ARTEX PROCEDURE 4128, 412*9. REPLACED SUB ASSEMBLY AND TOP COVER. NEW PRODUCT LABEL. 1G72 3U H3EU 20050222002212005022200221EU 2005 2 22 ERAA097085 120040429A63204638001004 TRANSMISSION BOLKMS105 BO105C 5626005EU MAIN ROTOR MAKING METAL E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 10580 FOUND UNACCEPTABLE AMOUNTS OF ALUMINUM, BRONZE AND METAL FLAKES IN OIL FILTER. BUSHINGS MISSING IN INTERMEDIATE SHAFT BOLT HOLE BORES. NO DRY LUBE ON BEVEL GEARS, BEVEL GEARS SWITCHED SIDES ON LAST O/H, LT PINION AND BEVEL GEAR SCRAPPED (TEETH BREAKING DOWN), LOWER HOUSING, INTERMEDIATE SHAFT BORES WORN AND WEAR STRIPPED, OIL PUMP HAD FOD DAMAGE, T/R OUTPUT SEAL LEAKING, RT OUTSIDE INT SHAFT BOLTS NOT SAFTIED. SLIPPING AND WEAR IN LOWER HOUSING CAUSED BY BUSHINGS MISSING IN INTERMEDIATE SHAFT BOLT HOLE BORES. REMOVED TOP CASE, CENTER CASE AND DISASSEMBLED LOWER CASE. BUILT UP NEW LOWER CASE ASSY. INSTALLING ONE EA NEW PINION AND BEVEL GEAR, REPAIRED, INS 1G72 3U H3EU 20050222002292005022200229NM 2005 2 22 EIA2004118 120040930A5330 SKIN BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 FOUND CORROSION ON UPPER CENTER SKIN SECTION AT STA 1140, RBL 100, MAIN DECK. CORROSION BLENDED FROM SKIN PAD ON UPPER SURFACE OF UPPER SKIN PANEL NR 2 AT S-14, JUST O/B RBL 98.58 FLOORBEAM. INSPECTED AREA AND DETERMINED CORROSION AND CRACK FREE. SHOT PEENED AND REFINISHED PER EN EA 57-0427, BOEING MESSAGE 1-OWPN9, 1-P23XO, AND 1-PCW1X. 2L74 4F RTA20WE 20050222002302005022200230GL 2005 2 22 ERAA097093 220040714A7200 ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL FOD E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH20764 598 CAE835276 ENGINE HAS HARD CLUTCH ENGAGEMENT. GEARBOX PILOT BORE DELAMINATED, COMPRESSOR FOD. INSPECTED ENGINE ASSY IAW RR OMM CH 72-00-00 PARA I.D. (4). INSTALLED SERVICEABLE COMPRESSOR AND GEARBOX. 1G72 3U3 U H3EU E4CE 20050222002312005022200231NM 2005 2 22 EIA2004123 120040922A5320 WEB BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CRACK IN STA 40 RT SUPPORT WEB, STA 2220-2240, BULK CARGO DISCHARGE COMPARTMENT. WEB REPLACED PER SRM 51-30-02, AND 51-10-01. 2L74 4F RTA20WE 20050222002352005022200235NM 2005 2 22 EIA2004117 120040930A5280 SKIN BOEING747 747SR46 1384816NM RT BLG DOOR CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 RT BLG I/B STRUT DOOR FOUND CORROSION AND CRACK ON EXT FACE OF OUTER DOOR-SKIN AT AFT EDGE. TRIM CORROSION AND CRACK IN 0.040 OUTER SKIN AT BS 1483.7, RBL 55.6, AND INSTALLED REPAIR DOUBLER BONDED TO FILLER. INSTALLED THREE (3) ROWS OF BLIND RIVETS AROUND THE EDGE OF DOUBLER AND FILLER PER EN 52-0048. BOEING MESSAGE 1-OJH2M, 1-OX3YA, 1-POV53, 1-P3J9Q, AND 1-P8ZP5. 2L74 4F RTA20WE 20050222002362005022200236SW 2005 2 22 ERAA097096 120040520A6210412015300109 BLADE BELL 412 412 1182202SW MAIN ROTOR DEBONDED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH7649 33064 MID LEADING EDGE SCARF JOINT DEBONDED, LEADING EDGE BOND LINE VOIDED NEAR TIP AND UNDER SIDE OF BLADE DETERIORATED. SENT TO CTI FOR REPAIR. INSPECTED PERFORMED 2500 HOUR INSPECTION AND REPAIRED. 1G72 4U H4SW 20050222002382005022200238SW 2005 2 22 ERAA097097 120040607A6220 BEARING BELL 412 412 1182202SW SPINDLE DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH322 DN741 33004 PIVOT BEARING BROKEN IN HALF. CAME IN CONTACT WITH M/R FITTING WHEN PIVOT BEARING BROKE. NO DEFECTS NOTED ON SPINDLE. PIVOT BEARING BROKEN. REMOVED PITCH HORN FROM SPINDLES BROKEN PIVOT BEARING, CLEANED AND INSPECTED PARTS. C/W NDT OF SPINDLE AND REASSEMBLED IAW BHT 412 CR&O CH 62 WITH PITCH HORN A-4296. 1G72 4U H4SW 20050222002402005022200240NM 2005 2 22 EIA2004122 120040922A5720 STRUCTURE BOEING747 747SR46 1384816NM LT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 BULGING CORROSION LEFT WING JUST AFT NR 12 K-FLAP, LOWER LEADING EDGE AT FIXED COMPOSITE FAIRING. SUSPECT INT METAL STRAP CORROSION. REMOVED CORROSION PER SRM 51-10-01, REWORK AREA 3 IN LONG BY .5 IN WIDE, BY 0.04 IN DEEP IS OUT OF SRM 57-20-01, FIG 1 LIMIT. REPLACED STRAP PER SRM 51-10-01. 2L74 4F RTA20WE 20050222002412005022200241EU 2005 2 22 ERAA097099 120040507A672010545361 CONTROL ROD BOLKMS105 BO105S 5626006EU DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03154EH 704 WATER DRIPPING FROM INSIDE NORMAL WEAR, FOUND EVIDENCE OF WATER IN ONE OF CONTROL TUBES. C/W PRELIMINARY INSPECTION, DISASSEMBLED. STRIPPED PAINT FROM TUBES. VISUALLY INSPECTED. PRIMED INSIDE OF TUBES. PRIMED AND PAINTED OUTSIDE OF TUBES. REASSEMBLED AND SET TO NOMINAL LENGTH. INSPECTED AND REASSEMBLED IAW BO-105 MM CH 41. 1G72 3U H3EU 20050222002432005022200243SW 2005 2 22 ERAA097100 120040629A2435 BEARING BELL 412 412 1182202SW STARTER-GEN FAILED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH10399 7315 33064 STARTER GEN HAS BEARING FAILURE. OVERHAULED AND TESTED. 1G72 4U H4SW 20050222002442005022200244NM 2005 2 22 EIA2004111 120040930A5330 SKIN BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 FUSELAGE SKIN BULGED AT SB/T STA 2180 TO STA 2200, STR 44R. CORRODED SKIN TRIMMED OUT. REMOVE AND DISCARD EXISTING DOUBLER OVERLAPPING STR 46R LAP JOINT. TRIM OUT CORRODED OVERLAPPING SKIN. INTL REPAIR DOUBLER PER EN AND EA53-0825. BOEING MESSAGE I-PC15E, I-PTIVO, & PVHU4. REPETITIVE INSPECTION PER ECRA 477-51-098-1, WITH FAA 8110-3. 2L74 4F RTA20WE 20050222002452005022200245EU 2005 2 22 ERAA097101 120040331A642010531714 ROTOR HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR BINDING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03293EH13353 559 BINDING TAIL ROTOR BLADE. NORMAL WEAR ON BUSHINGS AND SLEEVES ACTION TAKEN: DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS. C/W 300 HR / 2400 HR BLADE INSPECTION ON BLADES SN 658 AND 663. INSTALLED NEW INNER SLEEVE BUSHING AND NEW GRIP BUSHING. NEW SEALS AND NEW SPACER RINGS. REASSEMBLED AND INSPECTED IAW BO105 REM 301, COMPLIED WITH BO105 MM CH 34 AND INSTALLED SERVICEABLE BLADES AND MARVEL BALANCED IAW BO105 MM CHAPTER 107. 1G72 3U H3EU 20050222002462005022200246NM 2005 2 22 EIA2004112 120040930A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 MULTIPLE DEFECTS (CRACKS) ON LT AND RT SIDE BS 2231 FRAME ASSY AT MED NR 5L/R FWD EDGE CUTOUT AREA. TRIM OUT DAMAGED PORTION, SPLICE REPLACEMENT SECTION OF FRAME STRAP AND REVEAL PANEL ON RHS AND5. BOEING MESSAGE: I-OJHBI, I-P3MEM, AND I-P8ZPI. REPETITIVE INSPECTION MONITORED BY ECRA 477-53-102-1. 2L74 4F RTA20WE 20050222002472005022200247EU 2005 2 22 ERAA097102 120040428A621010515141 BLADE BOLKMS105 BO105S 5626006EU MAIN ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03134EH13067 635 M/R BLADE REJECTED FOR FLIGHT DUE TO LOOP A AREA BEING TOO THIN ON INNER RADIUS. BLADE SCRAPPED. 1G72 3U H3EU 20050222002482005022200248EU 2005 2 22 ERAA097103 120040428A621010515141 BLADE BOLKMS105 BO105S 5626006EU MAIN ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03134EH1304 635 M/R BLADE REJECTED FOR FLIGHT DUE TO LOOP A AREA BEING TOO THIN ON INNER RADIUS. BLADE SCRAPPED. 1G72 3U H3EU 20050222002502005022200250EU 2005 2 22 ERAA097105 120040524A6220105141081 ROTOR HEAD BOLKMS105 BO105S 5626006EU MAIN ROTOR LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH6645 598 LEAKING INBOARD SEAL. SEALS WORN, WEAR RINGS GROOVED, FLAT WASHERS WARPED. DISASSEMBLED TO FACILITATE INBOARD SEAL REPLACEMENT. VISUALLY INSPECTED AND FOUND SLIGHT CORROSION, REPAIRED. 1G72 3U H3EU 20050222002512005022200251EU 2005 2 22 ERAA097106 120040820A63204638001007 TRANSMISSION BOLKMS105 BO105S 5626006EU MAIN ROTOR LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03292EH 562 LT INPUT SEAL LEAKS. NORMAL WEAR ACTION TAKEN. REMOVED LT FW SHAFT AND SEAL HOUSING. INSTALLED SERVICEABLE HOUSING WITH A NEW SEAL AND O-RING. RE INSTALLED FW SHAFT WITH NEW O-RING ON CAP. ALL WORK DONE IAW REM 103 TT 14439.0 TSO 1995.3. 1G72 3U H3EU 20050222002522005022200252NM 2005 2 22 EIA2004115 120040922A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CRACKS IN TENSION TIE TO FRAME JOINTS AT LOCATION BS 840 FRAME, LEFT SIDE S-10L. HOLE IN FRAME OVERSIZED TO REMOVE CRACKS AND FREEZE PLUGS INSTALLED. REPAIR DOUBLER INSTALLED INCORPORATING EXISTING PRODUCTION DOUBLER PER EN 53-084 BOEING MESSAGE NR 1-OUMRW, 1-OOHR4, AND 1-P8ZM7 WITH FAA 8110-3. 2L74 4F RTA20WE 20050222002552005022200255EU 2005 2 22 ERAA097110 120040714A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU MLG DISCHARGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03125EH11348 S562 FLOAT BOTTLE PRESSURE LOW FLOAT BOTTLE SQUIB VALVE FOUND TO BE LEAKING AT VALVE/MANIFOLD JUNCTION (4) GROMMETS ON SUPPORT TUBE WORN AND CRACKED. FLOAT COVER FOUND TO BE WORN AND TORN. 18 MONTH INSPECTION DUE IN ONLY ABOUT 4 MONTHS. PERFORMED 18 MONTH INSPECTION ON FLOAT ASSY. REPAIRED LEAK AT SQUIB VALVE/MANIFOLD JUNCTION. SERVICED CYLINDER AND CHECKED FOR LEAKS, NO LEAKS FOUND. REMOVED AND REPLACED (4) GROMMETS (P/N MS35489-27) ON SUPPORT TUBE. REMOVED AND REPLACED FLOAT COVER. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-2,. 1G72 3U H3EU 20050222002562005022200256NM 2005 2 22 EIA2004116 120040922A5320 TIE BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CRACKS IN TENSION TIE TO FRAME JOINTS AT LOCATION BS 800 TENSION TIE, LEFT AND RT S-11L. BOTH ENDS OF TENSION TIE CHANNELS WERE TRIMMED AND NEW SEGMENTS AND SPLICE PARTS INSTALLED PER EN 53-0824. BOEING MESSAGE NR 1-OUMRW, 1-OOHR4, AND 1-P8ZM7 WITH FAA 8110-3. 2L74 4F RTA20WE 20050222002592005022200259NM 2005 2 22 EIA2004121 120040922A5411 SPAR BOEING747 747SR46 1384816NM NR 1 PYLON CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CRACK AT NAC STA 210, LOWER SPAR WEB, CENTER AREA, NR 1 PYLON. REPAIR LWR SPAR WEB PER SRM 54-10-03, FIG 2, SPAR WEB FABRICATED IAW SRM 54-10-03, FIG 2. 2L74 4F RTA20WE 20050222002602005022200260NM 2005 2 22 EIA2004125 120040930A5313 STRINGER BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 UPPER DECK STRINGER CRACKED AT BS 746, STR L3. REPAIRED STRINGER PER SRM 53-10-03, FIG 10. 2L74 4F RTA20WE 20050222002622005022200262NM 2005 2 22 04FDEA02927 120041012A5320AEA0526U1 DOUBLER DOUG MD11 MD11 3023602NM CENTER LG WW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 CENTER LANDING GEAR WHEEL WELL LEFT HAND STA 1381 DOUBLER SUSPECT CRACKED. CENTER LANDING GEAR WHEEL WELL LEFT HAND STA 1381 DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. LEFT HAND SPOILER CONTROL PUSHROD "DU" AND "MO" ADJUSTED AS PER AMM 27-61-00-830-006 AND AMM 27-61-00-830-017. OPERATION CHECK CARRIED OUT FOUND 'SATIS' AS PER AMM 27-61-00-730-801. 2L73 4F RTA22WE 20050222002642005022200264NM 2005 2 22 04FDEA02954 120041019A5311AFA0020 FRAME DOUG MD11 MD11F 3023600NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25595FE 48553 MAIN CARGO DECK LT STA 1701 TRANSVERSE FRAME DAMAGED BETWEEN LONGERON 11 AND LONGERON 12. MAIN CARGO DECK LT STA 1701 TRANSVERSE FRAME BETWEEN LONGERON 11 AND LONGERON 12, DAMAGED AREA TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG 1 VOLUME I. REFER TO FEDEX EA 1-5310-79787, TITLE: FUSELAGE, MAIN FRAME TRACKING SRM REPAIR ON FRAME AT STATION 1701. 2L73 4F RTA22WE 20050222002652005022200265EU 2005 2 22 ERAA097116 120040624A79213701020000 OIL COOLER BOLKMS105 BO105C 5626005EU ENGINE CONTAMINATED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 OIL COOLER RETURNED FROM OVERHAUL AT DRAKE AIR WITH DEBRIS AND FOREIGN OBJECTS (GRASS) IN BETWEEN COOLING FINS AND CASE. RETURNING ON ERA REPAIR ORDER RW-900233 REQUESTING WARRANTY REPAIR. 1G72 3U H3EU 20050222002682005022200268EU 2005 2 22 ERAA097079 120040817A64201053172904 BUSHING BOLKMS105 BO105A EU T/R HEAD ROUGH E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03SPARE NEW BUSHING THAT IS ROUGH AND UNFINISHED. ID IS TOO LARGE. WHEN INSTALLED ON INNER SLEEVE, BUSHING SPINS LOOSE. SUSPECT IMPROPER MANUFACTURE OF BUSHING. RETURNING ON ERA PACK SLIP NR 5956 REQUESTING CREDIT FOR REPLACEMENT PART. 1G72 3U H3EU 20050222002702005022200270 2005 2 22 AC2A097162 420040818A3197209075323001 RELAY BELL 206 206B3 1181506SW WARNING SYSTEM OPEN E AC2AK NONE O OTHER ININSP/MAINT 1 SO0721460 4075 RELAY HAS A CIRCUIT OPEN. NORMALLY CLOSED CONTACTS REMAIN OPEN, HIGH RESISTANCE. REPLACED RELAY. 1G71 3U H2SW 20050222002712005022200271SW 2005 2 22 AC2A097164 120040404A6220430010122101 STUD BELL 430 430 1182150SW M/R HEAD CRACKED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CT2442 49089 PART IS CRACKED WHERE THREADED AREA ATTACHES TO FLANGE. REPLACED STUD ASSEMBLY. 1G72 3U RTH9SW 20050222002722005022200272SW 2005 2 22 AC2A097165 120040818A6320222040111101 SHAFT BELL 430 430 1182150SW TRANSMISSION DAMAGED E AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CT2873 A97 49089 METAL TRANSFER FROM SUN GEAR. REPLACED SHAFT. REQUEST WARRANTY. 1G72 3U RTH9SW 20050222002732005022200273SW 2005 2 22 AC2A097166 120040818A6320430040112103 SUN GEAR BELL 430 430 1182150SW TRANSMISSION DAMAGED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CT2873 A97 49089 SUN GEAR WORN BEYOND LIMIT AT 3000 HOUR INSPECTION. METAL TRANSFERRED TO SHAFT. REPLACED SUN GEAR. REQUEST WARRANTY. 1G72 3U RTH9SW 20050222002742005022200274EU 2005 2 22 TXER097126 120040728A212112002601 BLOWER UROCOPEC120 EC120B 8680987EU CABIN AIR INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09116KG 1152 BLOWER INOP. 1G72 3U NCR0001RD 20050222002752005022200275EU 2005 2 22 TXER097127 120040817A212112002601 BLOWER UROCOPEC120 EC120B 8680987EU CABIN AIR INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09517SS 1080 BLOWER INOP. 1G72 3U NCR0001RD 20050222002762005022200276EU 2005 2 22 TXER097141 120040618A2120SE08626 CIRCUIT BOARD UROCOPEC155 EC155B 8681000EU A/C COMPRESSOR INOPERATIVE B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09155EW218 6660 CIRCUIT BOARD INOPERATIVE, SHUTTING A/C COMPRESSOR DOWN. 1G72 3U H10EU 20050222002772005022200277CE 2005 2 22 110404 120041023A3610 BLEED AIR SYS LEAR 25 25B 5170511CE LEAKING E ESUAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 CE0365WH 086 THE AIRCREW EXPERIENCED ELECTRICAL POWER FAILURE. IT WAS FOUND THAT A BLEED AIR LEAK WAS OVERHEATING THE GENERATOR CONTROL PANEL, CAUSING THE GENERATORS TO GO OFF LINE. 2L72 4J A10CE 20050222002782005022200278CE 2005 2 22 4026 120041104A3230 LANDING GEAR BEECH 58 58 1152740CE CONT O520 IO520CB 17032SO HARTZLHCJ3Y PHCJ3YF2 GL NLG & MLG MALFUNCTIONED E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL071847F TH1291 830925R ED3111 ON DEPARTURE OUT OF IND, SELECTED GEAR UP NOTHING HAPPENED, RETURNED TO IND. MAINTENANCE COULD NOT DUPLICATE GEAR UP PROBLEM, CHANGED DYNAMIC BREAK RELAY AND LANDING GEAR MOTOR AS PRECAUTIONARY MEASURE, CYCLED GEAR SIX TIMES OPS CHECKS GOOD. 1L72 3O3 O 3A16 E5CE 5 CP36EA 20050222002822005022200282EU 2005 2 22 DHL2004362012 120040922A3240 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG CHATTERING A DHLAK NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01362DH 84 BRAKES CHATTERING WHILE APPLING EVEN BRAKE, ALSO VIBRATING. PERFORMED VISUAL INSPECTION OF BRAKES IAW M/M 32-40-00, WITH NO DEFECTS NOTED. ALSO PERFORMED NORMAL BRAKING, OPS CHECK IAW M/M 32-42-00, WITH NO DEFECTS NOTED. ALSO, PERFORMED PEDAL POSITION TRANSMITTER BRAKE AS REQUIRED. 2L72 4F RTA35EU 20050222002832005022200283EU 2005 2 22 DHL2004362014 120041009A3240 LINE AIRBUS300 A300B4203 3930306EU NR 5 & 6 BRAKES CONTAMINATED A DHLAK NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01362DH 84 DURING TAXI, THERE WAS A NOTICEABLE BRAKE SHUDDER, ESPECIALLY AT LOW SPEEDS. BLEEDS NR 5 AND NR 6 BRAKES IAW MM 32-42-00. OPS CHECK GOOD. 2L72 4F RTA35EU 20050222002842005022200284NM 2005 2 22 DHL2004780515 120040930A5532 SKIN BOEING727 727223 1384074NM VERTICAL STAB DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A "C" CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER FIN STA 157.5 (LT SIDE RUDDER). DENT FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-40-1. FABRICATED DOUBLER 2024T-3 .040 PO NR 9001359 4 1/2/ X 2 1/2 IAW B727 SRM 55-40-2 AND 55-20-3, TREATED AND PRIME IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050218000112005021800011SO 2005 2 18 CHQA000576 120041031A3350 LIGHT EMB 145 EMB145LR 3260212SO RT OVERWING INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11291SK 145486 AFT RIGHT OVERWING EXIT LIGHT IS INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050218000182005021800018 2005 2 18 2004UALA01177 420041201A2565P2010035012 LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29852UA A8115 1671 DURING OVERHAUL EMERGENCY EXIT SLIDE LIGHT WERE FOUND TO BE DAMAGED. SUPPLEMENTAL DATA UPDATE THE LIGHT ASSEMBLY WAS REPLACED. 2L72 4F4 FRTA28NM E40NE 20050218000432005021800043 2005 2 18 CHQA000566 420041007A25654A40302 SLIDE EMB ERJ170ERJ170100LR EU CABIN UNSERVICEABLE A CHQAK NONE O OTHER ININSP/MAINT 1 GL11632RW33 33 17000050 DURING FAA EMERGENCY EVACUATION DEMONSTRATION, THE FORWARD RIGHT EMERGENCY EXIT SLIDE DEPLOYED PRIOR TO THE EXIT DOOR FULLY OPENING. THE SLIDE DEPLOYED SIDEWAYS AND LODGED BETWEEN THE EXIT DOOR AND THE FUSELAGE BELOW THE FIRST OFFICER'S SIDE WINDOW RENDERING IT UNUSABLE. REMOVED AND REPLACED EMERGENCY EVACUATION SLIDE ASSY IAW EMB 170MM 25-65-07. 2L74 4F RTA56NM 20050222000292005022200029CE 2005 2 22 GLBA20030648 120040619A5210 DOOR BEECH 1900 1900D 1154162CE MAIN PAX CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03211GL UE211 CABIN DOOR IS CORRODED AROUND BUTTON, REPAIRED CORROSION. 2L72 4T RTA24CE 20050222000512005022200051WP 2005 2 22 IXXA04000930 120040622A2611 WARNING LIGHT DOUG DC8 DC873F 302199FWP CFMINTCFM56 CFM563C1 13802EU WILL NOT TEST A IXXAK NONE N FALSE WARNING ININSP/MAINT 1 SW11606AL911272880 46044 693534 DURING DESCENT, NR 1 ENG FIRE WARNING SYSTEM SHORT LIGHT ILLUMINATED AND FIRE WARNING WOULD NOT TEST. NR 1 ENGINE SHUT DOWN IN FLIGHT. MAINTENANCE NOTED ENGINE IS WITHIN LIMITS PER ALL APPLICABLE MANUALS. MAINTENANCE CLEANED AND RESECURED WIRING CONNECTORS ON UPPER ENGINE HOT SECTION FIRE LOOP. OPS CHECK GOOD IAW DACO 70 SERIES MM CHAPTER 26-10-1. 2L74 4F4 FRT4A25 E21EU 20050222000652005022200065NM 2005 2 22 04FDEA01710 120040614A5744ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750- 76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222000712005022200071NM 2005 2 22 04FDEA01728 120040614A5744ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORROSION REMOVED AND EXCEED LIMITS PER CMM 57-44-08, ORIGINAL THICKNESS = 0.500 INCH, MATERIAL REMOVED = 0.012 INCH, REMAINING THICKNESS = 0.488 INCH FOUND WITHIN TOLERANCE OF DWG ARC0502. 2L73 4F RTA22WE 20050222000722005022200072NM 2005 2 22 04FDEA01729 120040614A5744ARC0502 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.224". COMPLIED WITH FEDEX EA NR 1-5740-76742, WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222000812005022200081EU 2005 2 22 04FDEA01937 120040705A27504907903 CONTROLLER AIRBUS310 A310203 3930313EU TE FLAPS MALFUNCTIONED A FDEAB EMER. DESCENT J WARNING INDICATION DEDESCENT 1 SO25427FE7204 7204 362 ON TAKEOFF DURING SLAT FLAP RETRACTION SYSTEM 2 FLAP FAULT LIGHT ON OVERHEAD PANEL CAME ON WITH ACCOMPANIED ECAM WARNING. ALSO, SPEED LIMIT WARNING (LOCATED AT THE BASE OF THE FIRST OFFICERS PFD CAME ON). SELECTED ADC INST ON FO'S SIDE SWITCHING PANEL AND SPEED LIMIT WARNING WENT OUT. ON APPROACH TO MEM AT FLAPS EXTENSION GOT THE SECOND SYSTEM 1 FLAP FAULT LIGHT AND DUAL ECAM WARNING, FLAPS WOULD NOT MOVE. FLEW A NO FLAP (SLAT ONLY) APPROACH TO RUNWAY 18L MEM. NO PROBLEM. TRIED TO RESET SFCC NR'S 1 AND 2, NR 1 RESET AND BITE TESTED GOOD, NR 2 WOULD NOT RESET. REMOVED AND REPLACED NR 2 SFCC, PERFORMED BITE AND OPS CHECKS, CHECKED GOOD. 2L72 4F RTA35EU 20050222000832005022200083WP 2005 2 22 04FDEA01935 120040703A5711 SPAR DOUG DC10 DC1030F 3023504WP ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 RT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPECTION OF BUSHING IAW DAC SPM 20-30-02 AND EA 8-5710-77571. NO DEFECTS NOTED. CAD PLATING ACCOMPLISHED BY OUTSIDE VENDOR ON PO NR 448912. INSTALLED RIGHT HAND WING BUSHING STATION XW 255.000 LOWER SPAR BEAM OUTBOARD HOLE, HOLE "C", PER PAGE 9 OF 18 OF EO 8- 5750-7-5000 PART 2 IAW EA 8-5710-77571. REFERENCE N/R N01153. 2L73 4F RTA22WE 20050222000912005022200091NE 2005 2 22 GLBA20030652 220040622A7200 COMPRESSOR BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE NR 1 ENGINE STALLED A GLBAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM03154GL1895511254 UE154 114179 NR 1 ENG COMPRESSOR STALLS, SHUT DOWN ENG IN FLT RETURNED TO DEN. REMOVED AND REPLACED ENG PN PT6A-67D. 2L72 4T4 TRTA24CE E26NE 20050222001152005022200115NM 2005 2 22 04FDEA01944 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL THICKNESS=0.343 INCH, MATERIAL REMOVED=0.038 INCH, REMAINING THICKNESS=0.305 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222001182005022200118SW 2005 2 22 AC2A096516 120040714A33501000553 HOUSING BELL 430 430 1182150SW EMERGENCY LIGHT BROKEN B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CV 49072 HOUSING IS BROKEN. AUTOMATIC ON FUNCTION IS INOPERATIVE. ONE CELL IS DEAD. REPLACED ASSEMBLY WITH A NEW PART. TOO EXPENSIVE TO REPAIR OLD UNIT. 1G72 3U RTH9SW 20050222001292005022200129SW 2005 2 22 ALGA096400 120040720A632023071895 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL M/R GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03417AL595 53054 CAE847532 FOUND SPALLED GEAR TEETH ON GEAR. REPLACED W/NEW PART. 1G71 3U3 UO H2SW E1GL 20050222001572005022200157NM 2005 2 22 04FDEA01947 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001592005022200159NM 2005 2 22 04FDEA01949 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.003 INCH, REMAINING THICKNESS = 0.402 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001632005022200163NM 2005 2 22 04FDEA01953 120040706A5753ARC1991 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.130 INCH. COMPLIED WITH FEDEX EA NR 1-5750-76784, WINGS, LEFT AND RIGHT OUTBOARD FLAP, HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050222001752005022200175WP 2005 2 22 04FDEA02315 120040730A5330 SKIN DOUG MD10 MD1010F 3022112WP ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25396FE 26456 LOWER FORWARD CARGO DOOR CUTOUT AFT LOWER CORNER REPAIR TRIPLER DAMAGED. REMOVED TRIPLER REPAIR IAW MD10 SRM 51-33-01 PAGE 1 VOL I, FABRICATED NEW REPAIR TRIPLER IAW MD10 SRM 53-20-00 VOL I FIG 6 SHEET 5, ALODINE AND PRIMED IAW MD10 SRM 51-21-01 VOL II, PAGE 32. INSTALLED NEW TRIPLER IAW MD10 SRM 51-35-01 VOL II AND 51-33-01 VOL II. DAMAGE REPAIRED AT FS 959-990, LONGERON 38R TO 43R. REF N/R N00020. 2L73 4F RTA22WE 20050222002012005022200201SW 2005 2 22 ALGA096731 120040804A6210206015001115 BLADE BELL 206 206L3 1182108SW MAIN ROTOR CORRODED B ALGAO OTHER O OTHER NRNOT REPORTED 1 AL03343AL2361 51372 TRAILING EDGE EXTRUSION EXFOLIATED, LOWER O/B GRIP FINGER DOUBLER SEPARATED AND CORRODED, ALSO CORROSION BETWEEN SKIN AND SPAR. SCRAPPED BLADE, AND INSTALLED A NEW BLADE. 1G71 3U H2SW 20050222002152005022200215NM 2005 2 22 04FDEA02487 120040817A5320AEA7621 WEB DOUG MD11 MD11F 3023600NM ZONE 100 CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER LANDING GEAR WHEEL WELL, RT VERTICAL WEB FOUND WITH OIL CANNING CONDITION. CENTER LANDING GEAR WHEEL WELL, RT VERTICAL WEB INSPECTION CARRIED OUT AND FOUND WITHIN SRM 53-00-01 VOLUME I LIMITS. STA Y= 1394-1401, Z= 100-115, 0.067" STA Y= 1401-1411, Z= 100-115, 0.085" STA Y= 1411-1421, Z= 100-115, 0.075" STA Y= 1421-1431, Z= 100-115, 0.090" STA Y= 1431-1441, Z= 80-100, 0.160" STA Y= 1461-1471, Z= 100-115, 0.071" COMPLIED WITH FEDEX EA NR 1-5330-76819, FUSELAGE - PLATES AND SKIN, KEEL WEB IN THE CENTER LANDING GEAR WHEEL WELL. 2L73 4F RTA22WE 20050222002172005022200217GL 2005 2 22 ERAA097078 220040804A725023004513 CARBON SEAL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03125EH S562 NEW CARBON SEAL ISSUED TO AIRCRAFT BUT COULD NOT BE USED DUE TO LEAKING, UNEVEN SURFACE ON CARBON FACE. RETURNING TO AVIALL ON ERA PACK SLIP NR 5955 REQUESTING CREDIT. 1G72 3U3 U H3EU E4CE 20050222002342005022200234SW 2005 2 22 ERAA097095 120040712A6210412015300101 BLADE BELL 412 412 1182202SW MAIN ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03417EH7057 33031 SET SCREW MISSING IN TIP CAP SUSPECT FACTORY BALANCE WEIGHTS MISSING. INSPECTED, PERFORMED 2500 HOUR INSPECTIONS PER BHT-412-MM CHAPTER 5; REPLACED INBOARD AND CENTER TRIM TABS PER 204-099-223 APPENDIX B SECTION 2 PARAGRAPH 2.7REV L; REPAIRED SKIN ON UPPER SURFACE AT STA 155 TO STA 160 PER 204-099-223 APPENDIX B SECTION 1.4.1; REPLACED ROOT TAPE PER TB 412-02-182; REFINISHED PER 4488D AND 412-947-015 REV F; APPLIED HIGH VIS PER CUSTOMER REQUIREMENT; STATIC BALANCED PER 204-099-223 VOL XVII SECTION 2.8.1 REV L AT TT 7412.5. BLADE IS 55.6 GRAMS TIP HEAVY TO MASTER.. 1G72 4U H4SW 20050222002422005022200242NM 2005 2 22 EIA2004110 120040923A573065B080609 FAIRING BOEING747 747SR46 1384816NM LT WING CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 LT WING LEADING EDGE WING ROOT ALUMINUM NOSE CAP (D-FAIRING) AT LALDG LIGHT LWR AREA FOUND CORROSION. CORROSION REMOVED, HFEC INSP TO INSURE CORROSION CRACK FREE. APPLIED FINISH PER BOEING MESSAGE NR I-OYSCJ, I-OW4AE, TEC-XMN-04-01388C. EN EA-57-0428, REPETITIVE INSP MONITORED PER ECRA 477-51-098-1 (24 MONTH). 2L74 4F RTA20WE 20050222002492005022200249EU 2005 2 22 ERAA097104 120040524A62201051410110 BOLT BOLKMS105 BO105A EU MAIN ROTOR GALLED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH S675 BLADE BOLT GALLED SLIGHT GALLING ON BOTH BOLTS ACTION TAKEN. SCRAPPED BOTH PRIMARY BLADE BOLTS DUE TO GALLING BEYOND LIMITS IAW BO-105 MM CH 13. 1G72 3U H3EU 20050222002572005022200257 2005 2 22 ERAA097111 420040628A341661031004 ALTIMETER BOLKMS105 BO105S 5626006EU COCKPIT FAILED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03296EH S849 ALTIMETER BENCH CHECKED. UNIT FAILED SCALE ERROR TEST AT 3000 FEET ACTION TAKEN, UNIT FAILED SCALE ERROR TEST. SEND TO ANCHORAGE FOR REPAIR. 1G72 3U H3EU 20050222002692005022200269SW 2005 2 22 AC2A097170 120040822A33501104611 HOUSING BELL 430 430 1182150SW LIGHT DETERIORATED E AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07430CT 49089 PART HOUSING IS DETERIORATED. ORDERED REPLACEMENT PART. 1G72 3U RTH9SW 20050222002792005022200279NM 2005 2 22 DHL2004760011 120041104A3260 PIN BOEING727 7272B7 138407LNM NLG NOT SEATED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01760AT 21954 ON DEPARTURE OUT OF SLW, RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUM. FOUND PIN "A" AT CONNECTOR D298 UNSEATED ON NOSE GEAR LOCKED SWITCH. RESEATED PIN "A" NOSE GEAR LOCKED SWITCH. INDICATION LIGHT TEST NORMAL IAW ASTAR M/M 32-61-71. 2L73 4F A3WE 20050222002812005022200281EU 2005 2 22 DHL2004363523 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3873, FS 30 - FS 38.2 RBL - 18 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 30 - FS 38.2 AT RBL 18 IAW A-300 SRM 53-10-10 AND 51-30-30. FABRICATED NEW SEAT TRACK FROM FS 30 - FS 38.2 IAW A-300 SRM 53-10-10. INSTALLED NEW SEAT TRACK FROM FS 30 - FS 38.2 AT RBL 18 IAW A-300 SRM 51-10-40 AND 53-10-10. TREATED AND PRIMED AND APPLY POLY WHITE PER A-300 SRM 51-40-10 AND 51-40-12. 2L72 4F RTA35EU 20050223000042005022300004NM 2005 2 23 DHL2004784006 120040904A2612 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01784DH 22001 ENGINE NR 3 DETECTOR CIRCUIT GRD LIGHT ILLUMINATED ON P-6-5 PANEL. COULD NOT DUPLICATE. RE-POSITIONED NR 3 ENG FIRE LOOP IN 2 LOCATIONS AS PRECAUTIONARY AND OP'S CHECKED IAW MM 26-11-0. SYSTEM CHECKS GOOD. 2L73 4F A3WE 20050223000052005022300005NM 2005 2 23 DHL2004752007 120040904A3150 WARNING HORN BOEING727 727223 1384074NM COCKPIT ACTIVATED A DHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01752DH 22466 TAKEOFF WARNING HORN SOUNDED WHEN T/O POWER WAS APPLIED FLAPS 15 DEG TRIM AT 5.0 ABORTED T/O AT LESS THAN 5 KNOTS GROUND SPEED. PERFORMED T/O WARNING SYSTEM TEST IAW B-727 M/M 31-26-1. NO DEFECTS FOUND. OK FOR FURTHER SERVICE. 2L73 4F A3WE 20050223000072005022300007CE 2005 2 23 HAEA200400160 120040726A261224417585 FIRE LOOP LEAR 24 24F 5170317CE NR 1 ENGINE FALSE INDICATIONE HAEAO OTHER N FALSE WARNING CLCLIMB 1 SW05444TW1426214262 348 ENGINE NR 1 FIRE DETECTION WARNING ILLUMINATES AT EXHAUST TEMPS OF EXCEEDING 600 DEGREES CELSIUS IN CLIMB-OUT OR IN WARM AMBIENT TEMPS. REPLACED UPPER COWLING SENSOR. OPS CHECK GOOD. 2L72 4J A10CE 20050223000092005022300009NM 2005 2 23 04FDEA02486 120040817A5320AEA7621 WEB DOUG MD11 MD11F 3023600NM ZONE 100 CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER LANDING GEAR WHEEL WELL, LEFT VERTICAL WEB FOUND WITH OIL CANNING CONDITION. CENTER LANDING GEAR WHEEL WELL, LEFT VERTICAL WEB INSPECTION CARRIED OUT AND FOUND WITHIN SRM 53-00-01 VOLUME I LIMITS. STA Y= 1394-1401, Z= 100-115, 0.087" STA Y= 1401-1411, Z= 100-115, 0.091" STA Y= 1411-1421, Z= 100-115, 0.082" STA Y= 1421-1431, Z= 100-115, 0.093" STA Y= 1431-1441, Z= 80-100, 0.146" STA Y= 1441-1451, Z= 80-100, 0.115" STA Y= 1471-1481, Z= 100-115, 0.064" COMPLIED WITH FEDEX EA NR 1-5330-76819, FUSELAGE, PLATES AND SKIN, KEEL WEB IN THE CENTER LANDING GEAR WHEEL WELL. 2L73 4F RTA22WE 20050223000102005022300010NM 2005 2 23 04FDEA02511 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, XORS= 620 TO XORS= 633, UPPER AND LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 620 TO XORS= 633 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000112005022300011NM 2005 2 23 04FDEA02512 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, XORS= 613 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 613 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000152005022300015NM 2005 2 23 04FDEA02485 120040817A5730APB74411 SKIN DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER WING TANK, STA 1219 - STA 1239, LBL 27 - LBL 47 HORIZONTAL PRESSURE PANEL TOP SURFACE CORRODED. CORROSION REMOVED, MATERIAL ORIGINAL THICKNESS = 0.175 INCH, MATERIAL REMOVED = 0.017 INCH, REMAINING MATERIAL = 0.158 INCH AND FOUND WITHIN LIMITS AS PER FEDEX EA NR 1-5710-76817, WINGS, CENTER WING UPPER PANEL, SKIN CORROSION. 2L73 4F RTA22WE 20050223000162005022300016WP 2005 2 23 04FDEA02646 120040904A5730ARC2008508 PANEL DOUG DC10 DC1030F 3023504WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 RIGHT WING PANEL 635 GL DELAMINATED AND ONE GOUGE. REPAIRED PANEL 635 GL BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2008 AND FEDEX EA 8-5750-81442. REFERENCE N/R N00239. 2L73 4F RTA22WE 20050223000202005022300020WP 2005 2 23 04FDEA02650 120040904A5753ARC25122 HINGE FITTING DOUG DC10 DC1030F 3023504WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 RIGHT WING INBOARD FLAP OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.1885 FINAL DIAMETER 1.3817, FOUND TO BE OUT OF LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF .9997 INCHES, WITHIN LIMITS IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81452, LISTED ON N/R N00371 FOR CORRECTIVE ACTION. REFERENCE N/R N00371. 2L73 4F RTA22WE 20050223000212005022300021WP 2005 2 23 04FDEA02651 120040904A5753ARC25121 HINGE FITTING DOUG DC10 DC1030F 3023504WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 LEFT WING INBOARD FLAP, OUTBOARD HINGE SUPPORT, PIVOT ATTACH POINT, INBOARD BORE PITTED AND CORRODED. REMOVED CORROSION, ORIGINAL DIAMETER 1.240, FINAL DIAMETER 1.2819, MATERIAL REMOVED .0419 IS BEYOND LIMITS. FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL DIAMETER OF 1.0001, WITHIN LIMITS IAW DAC CMM 57-52-01 AND FEDEX EA 8-5750-81451. REFERENCE N/R N00367. 2L73 4F RTA22WE 20050223000262005022300026EU 2005 2 23 04FDEA02664 120040907A5310R538D104820200 ADAPTER AIRBUS310 A310203 3930313EU FUSLAGE BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 MAIN CABIN FS 44 FLOOR LEVEL BETWEEN SEAT TRACK R1 AND R2 SEAT TRACK (CLS ADAPTER) IS BROKEN. REMOVED AND REPLACED CLS ADAPTOR IAW A310/200 SRM 51-40-21. 2L72 4F RTA35EU 20050223000272005022300027EU 2005 2 23 04FDEA02665 120040907A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 MAIN DECK SEAT TRACK R4 HAS A 2 INCH CRACK IN VERTICAL LEG BETWEEN FS 21 AND 22. REPAIRED AREA IAW EA6-5310-81919. 2L72 4F RTA35EU 20050223000322005022300032NM 2005 2 23 04FDEA02520 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 598 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 598 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000352005022300035NM 2005 2 23 04FDEA02523 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT XORS= 585 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 585 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000382005022300038WP 2005 2 23 04FDEA02605 120040902A2997 CONNECTOR DOUG DC10 DC1030F 3023504WP NR 3 ELEVATOR MISWIRED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25312FE 48300 AT C-CHECK, NR HYD SYS SHUTOFF VALVE FAILED THE OP'S CK. THE ELECTRIC ELEVATOR SHOV FAILED TO MOVE TO THE CLOSED POSITION. NR 3 ELEVATOR OFF ALERT SHOWS. T/S AND FOUND CONNECTOR P10- 548B MISPINNED. WIRE E204-125-20 WAS IN HOLE NR 9 AND NOT NR 2 AS CALLED OUT IN THE WIRE HOOK UP LIST AND WDM. REPINNED CONNECTER IAW WIRE HOOKUP LIST. VOLTAGE CHECK THROUGH THE 19 QT LEVEL SWITCH (S1- 1402) TO GROUND GOOD. 2L73 4F RTA22WE 20050223000392005022300039CE 2005 2 23 0042 120040910A554396630000335 TRIM TAB BEECH 90 E90 1152914CE RUDDER WRONG PART E CIEAK NONE O OTHER ININSP/MAINT 1 NM0363BV LW256 DURING A DETAILED INSPECTION OF THE AIRCRAFT THE RUDDER TRIM TAB HORN BUSHING WAS FOUND TO BE WORN BEYOND ALLOWED LIMITS. REPLACEMENT OF THE HORN IN THE TRIM TAB IS NOT A GOOD OPTION, DUE TO THE AMOUNT OF DISASSEMBLY OF THE TAB IN ORDER TO ACCOMPLISH THE TASK. A REPLACEMENT TRIM TAB WAS PURCHASED. DURING THE INSPECTION OF THE NEW TRIM TAB IT WAS NOTED THAT THE WATER DRAIN HOLE REQUIRED BY AD 91-12-12, AMENDMENT 39-7023 WHICH HAS BEEN SUPERSEDED BY AD 92-07-05 AMENDMENT 39-8201, WHICH WAS EFFECTIVE APRIL 30, 1992, WAS NOT INSTALLED ON THE NEW TAB. THESE AIRWORTHINESS DIRECTIVES REFER TO BEECHCRAFT SERVICE BULLETIN 2365 DATED JANUARY 1991. THE REPLACEMENT TRIM TAB RECEIVED WAS MANUFACTURED ON 03-05-2002. 1L72 3T 3A20 20050223000402005022300040CE 2005 2 23 31201081704 120040817A2430 GCU LEAR 35 31 5170530CE RIGHT OUT OF TOLERANCEE J7SAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW05137FX 31201 CLIMBING THRU FL220, YELLOW ELEC PWR MONITOR LIGHT FLASHING AND VDC READ 29.6. PERFORMED EMERGENCY CHECKLIST AND WHEN LT GEN SHUT OFF, VDC READ 30.0. RETURNED TO DEPARTURE AIRPORT WITH RT GEN OFF. MAINTENANCE FOUND RT GCU NOT WITHIN ADJUSTED TOLERANCE. ADJUSTED RT GCU. NO DEFECTS NOTED 2L72 4F RTA10CE 20050223000422005022300042NM 2005 2 23 DHL2004765007 120040918A291017583141 FILTER BOEING727 727264 138408MNM HYD SYSTEM DIRTY A DHLAK NONE O OTHER TXTAXI/GRND HDL 1 SO01765AT 23014 RIGHT MAIN GEAR BRAKES ARE CHATTERING WITH BRAKE APPLICATIONS WHEN RELEASE BRAKE APPLICATION NOTICE BRAKES STICKING. CHECK FOR FREE WHEEL ROTATION IS GOOD SERVICED BRAKE SYSTEM. REMOVED AND REPLACED RETURN "B" SYSTEM FILTER, NO LEAKS NOTED, OPS GOOD PER MM 32 41 0, FILTER P/N 17583141. 2L73 4F A3WE 20050223000442005022300044WP 2005 2 23 04FDEA02649 120040904A5415AUB702533 FITTING DOUG DC10 DC1030F 3023504WP NR 1 PYLON MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 NUMBER 1 ENGINE PYLON AFT SPHERICAL ATTACH BOLT TORQUE STRIPE BROKEN AND THE BEARING IS MIGRATING. REMOVED BEARING IAW DC10MM 54-40-02, REMOVED CORROSION IAW DC10 MM 54-40-02. REMOVED AFT BULKHEAD FITTING AUB 7025-33 IAW DC10-30 SRM 51-31-01 VOL II, LOCATED, DRILLED NEW AFT BULKHEAD FITTING IAW DAC DWG AUB 7025 AND DC 10-30 SRM 51-31-01 VOL II, PIN AUB 7025-33 INSTALLED IAW DAC DWG AUB 7025 AND DC10 SRM 51-31-01 VOL II. REFERENCE N/R N00494. 2L73 4F RTA22WE 20050223000452005022300045NM 2005 2 23 04FDEA02661 120040907A5512ARC81042 PANEL DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 RIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE CORROSION EXCEEDED CONDITION 3 LIMITS. RIGHT HAND HORIZONTAL STABILIZER NR 22 BARREL NUT BORE REPAIRED AS PER EA NR 1-5510-80309 TITLE: HORIZONTAL STABILIZER, BARREL NUT BORE 22R. REWORKED BEYOND S/B MD11-55-023 REV 2 LIMITS. 2L73 4F RTA22WE 20050223000462005022300046EU 2005 2 23 IXXA0400105O 120040828A5270 STRIKER ISRAEL1124 1124 4500102EU MLG DOOR OUT OF ADJUST A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW11830 76120202 406 AFTER TAKEOFF FROM PDX, DOOR LIGHT CAME ON DURING GEAR UPLATCH CHECK, GEAR AND DOOR LIGHT REMAINS ON WITH GEAR UP AND LOCKED. CREW RECYCLE GEAR AND NO CHANGE, AND RETURNED BACK TO PDX. MX INSPECTED MAIN GEAR AND FOUND RT GEAR DOOR STRIKER MISSING DOOR SWITCH. REPOSITION AND TEST PER APPLICABLE MANUALS AND RETURNED AIRCRAFT TO SERVICE. 2M72 4F A2SW 20050223000472005022300047NM 2005 2 23 04FDEA02655 120040905A5753ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 RT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050223000502005022300050SO 2005 2 23 GLBA20030726 120040927A3260 WARNING LIGHT EMB 120 EMB120ER 3260203SO MLG FALSE INDICATIONA GLBAO OTHER N FALSE WARNING APAPPROACH 1 NM03299UX 120299 LANDING GEAR GIVES FALSE INDICATION, PERFORMED LANDING GEAR EXTENSION COULD NOT DUPLICATE 2L72 4T RTA31SO 20050223000512005022300051NM 2005 2 23 DHL2004763006 120040925A3260 UPLOCK SENSOR BOEING727 727264 138408MNM MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01763AT 22983 AT FL 290, RT MAIN GEAR RED WARNING LIGHT ILLUMINATED THEN LATER EXTINGUISHED. PERFORMED TEST OPERATION OF UPLOCK SENSOR, OPS TEST GOOD PER MM 32-61-81, P403. 2L73 4F A3WE 20050223000542005022300054NM 2005 2 23 04FDEA02653 120040905A5753ARC2512504 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.227 INCH, AND REPAIRED AS PER EA NR 1-5750-80343, TITLE: WINGS TRAILING EDGE FLAPS, RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20050223000552005022300055NM 2005 2 23 04FDEA02654 120040905A5753ARC2512504 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442 TO 443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.285 INCH, AND REPAIRED AS PER EA NR 1-5750-80343, TITLE: WINGS TRAILING EDGE FLAPS, RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR. 2L73 4F RTA22WE 20050223000582005022300058NM 2005 2 23 F3LA200400098 120040927A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986.5 CORRODED AT FLOOR PANEL NUT PLATES. REPLACED FLOORBEAM UPPER CHORD AT STA 986.5 PER SRM 53-60-51, 53-00-51, FIG 202, AND MM 51-20-01. 2L72 4F RTA16WE 20050223000592005022300059NM 2005 2 23 F3LA200400099 120040927A5315 FLOORBEAM BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 947.5 CORRODED AT FLOOR PANEL NUT PLATES. REPAIRED FLOORBEAM UPPER CHORD PER SRM 53-00-51, 51-40-02, 51-20-01 AND MM 51-21-01. 2L72 4F RTA16WE 20050223000602005022300060NM 2005 2 23 F3LA200400100 120040927A5315 FLOOR SUPPORT BOEING737 7373L9 1384470NM FUSELAGE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03310FL 3661 26440 DURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CRACKED AT STA 927 - 947.5, RBL 16. REMOVED FLOOR SUPPORT TO REPLACE CRACKED FLANGE. REPAIRED CRACKED FLANGE AND REINSTALLED FLOOR SUPPORT PER BOEING DRAWING 65-36656, 737-300 SRM 51-40-02 AND 51-10-02, AND SOPM 20-41-02. 2L72 4F RTA16WE 20050223000612005022300061NE 2005 2 23 CX7A194J0452 220040926A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT OVERHEATED A CX7AC ABORTED TAKEOFF MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 GL03314CE 340B335 GEE785532 RT ENGINE OVER TEMPED ON TAKEOFF AFTER CTOT ENGAGED. RT ENGINE SURGED 3 TIMES IN 2 SECONDS THEN TEMP WENT TO 1135. 2L72 4T4 TRTA52EU E8NE 20050223000642005022300064NE 2005 2 23 TSAA0473068 220040914A73217436025 FCU BOEING737 73725A 1384481NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A TSAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP13819AL 23791 P707365 ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MAX-POWER OBTAINED WAS 1.97 EPR WITH N1 AT 94 PERCENT; FURTHER THRUST LEVER MOVEMENT HAD NO EFFECT. REMOVED AND REPLACED THE NR 1 ENGINE FCU IAW PRATT MM 79-21-01. PERFORMED LEAK VERIFICATION IAW AQ FORM M-215. OPS AND LEAK CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20050223000652005022300065NM 2005 2 23 TSAA0436069 120040917A3600 BLEED AIR SYS BOEING737 737282 13844ATNM RIGHT MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13824AL 23045 FLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE ISOLATION VALVE CLOSED AND THE RT BLEED & RT PACK OFF. THE PRESSURE THEN DECREASED TO 14 PSIG, AND THEN DECREASED FURTHER WHEN POWER WAS REDUCED. RETURNED TO HNL. OPS AND LEAK CHECKED THE ISOLATION VALVE AND NR 2 ENGINE BLEED VALVE, CLEARED PRESSURE REGULATOR VENT HOLE. RAN ENGINES IAW AMM 71-00, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050223000672005022300067NM 2005 2 23 TSAA0427065 120040907A27512061141 INDICATOR BOEING737 7372T4 1384492NM TE FLAPS FAILED A TSAAA UNSCHED LANDING P NO WARNING INDICATION DEDESCENT 1 WP13808AL 23445 NON-ETOPS FLIGHT 110, HNL-OGG: FLAPS DID NOT DEPLOY DURING NORMAL FLAP EXTENSION, USED ALTERNATE MODE TO DEPLOY LEADING EDGE FLAPS. THE TRAILING EDGE FLAPS WERE ASYMMETRICALLY SPLIT AT LESS THAN ONE UNIT. RETURNED TO HNL. REMOVED AND REPLACED THE FLAP POSITION INDICATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050223000682005022300068 2005 2 23 TSAA0431067 420040912A3414 INDICATOR BOEING737 73725A 1384481NM AIRSPEED SLOW A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13819AL 23791 NON-ETOPS FLIGHT 62, HNL-OGG: ON TAKEOFF 80KTS CROSS-CHECK WAS OK, AFTER LIFTOFF THE FIRST-OFFICERS AIRSPEED INDICATOR READ 50KTS SLOWER THAN CAPTAIN’S STANDBY INDICATOR. RETURNED TO HNL. CLEARED FIRST-OFFICERS PITOT TUBE OF DEBRIS IAW AMM 34-11-0, LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050223000692005022300069NM 2005 2 23 TSAA0429071 120040920A2910 HYDRAULIC SYSTEM BOEING737 7372M6C 1384708NM B SYSTEM CONTAMINATED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13805AL 21809 NON-ETOPS CARGO FLIGHT 909, HNL-LIH: ON CLIMB-OUT PASSING 1500 FT THE FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. RETURNED TO HNL. REPLACED THE B HYDRAULIC SYSTEM RETURN FILTER AND CASE DRAIN FILTERS DUE TO CONTAMINATION, OPS CHECK GOOD. REPLACED THE A SYSTEM RETURN FILTER AND DRAINED/RE-SERVICED THE A SYSTEM HYDRAULIC RESERVOIR, OPS CHECK GOOD. CHECKED ELEVATOR PITOT SYSTEM FOR LEAKS IAW AMM 27-31-22, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE 2L72 4F RTA16WE 20050223000702005022300070NM 2005 2 23 TSAA0424070 120040920A2497 BUSS BOEING737 73776N 13844CHNM GALLEY INOPERATIVE A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13750AL 32743 ETOPS FLIGHT 473, OAK-OGG - GALLEY POWER BECAME INOP, RETURNED TO OAK. LOW TO MODERATE SINK-RATE COMPLIED WITH, SMOOTH TOUCH-DOWN. RESET AIRCRAFT GROUND SERVICE BUSS 1 AND 2, GALLEY POWER VERIFIED. OPS CHECK OK. CONFORMED WITH HEAVY LANDING PHASE I INSPECTION IAW AMM 05-51-01-2, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050223000712005022300071NM 2005 2 23 TSAA0427072 120040920A3150 WARNING LIGHT BOEING737 7372M6C 1384708NM COCKPIT ILLUMINATED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13805AL 21809 NON-ETOPS CARGO FLIGHT 909, HNL-LIH, ON CLIMB-OUT PASSING 2000-3000 FT, THE FEEL DIFFERENTIAL PRESSURE LIGHT CAME ON. RETURNED TO HNL. BLEW OUT ELEVATOR PITOT TUBES, PITOT TUBES CLEAR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050223000722005022300072NM 2005 2 23 04FDEA02660 120040907A5311AFA00193 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 MAIN DECK, RT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1721, L-12R. FRAME AT STA 1721 RT SIDEWALL L-12R DENTED AREA REPAIRED AS PER SRM 53-30-00 VOL I FIG 1. REPAIR IS CAT B INITIAL INSPECTION AT 14,500 AND REPETITIVE INSPECTION REQUIRED AT 9,500 LANDINGS. REFER TO EA NR 1-5310-76835, TITLE:FUSELAGE MAIN FRAME, TRACKING SRM REPAIR ON FRAME AT STATION 1721, LONGERON 12R. 2L73 4F RTA22WE 20050223000732005022300073NM 2005 2 23 DHL2004747006 120040929A2910AE2460010H0360 LINE BOEING727 727224 1384076NM HYD SYSTEM LEAKING A DHLAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01747DH 22253 BEFORE LANDING CVG B HYD SYSTEM QUANTITY WENT TO ZERO QUANTITY HYD SYSTEM B FAILED ABNORMAL PROCEDURE C/W. INSTALLED FLEX LINE BETWEEN B HYD SYSTEM AND FILTER PER GMM CHP 20.1 LEAK CK OK P/N AE 2460010H0360 AND P/N BACH8CO8NN0290. 2L73 4F A3WE 20050223000752005022300075CE 2005 2 23 4024 120040923A2120 ODOR CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL COCKPIT DETECTED E BSYAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL07103AN 208B0928 PCEPC0928 022293 AIRCRAFT WAS IN CRUISE, PILOT THOUGHT HE SAW AND SMELLED SMOKE, ARM REST FELT WARM, LANDED A/C SAFELY. AIRCRAFT WAS INSPECTED, NO PROBLEM COULD BE FOUND, TEST FLEW A/C ALL SYSTEMS NORMAL, COULD NOT DUPLICATE PROBLEM. 1H71 3T3 T A37CE E4EA 5 CP60GL 20050223000762005022300076WP 2005 2 23 IXXA0400109O 120040930A2150P51351 FLOW VALVE DOUG DC8 DC862F 3021972WP LT A/C PACK FAILED A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW1171CX 651131406 45961 AFTER TAKEOFF, LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 1000 FEET WITH AIRCRAFT AT FL 250 AND RIGHT PACK OFF. CREW RETURNED TO PHIK AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED SECURTIY OF LEFT PACK/FLOW CONTROL SYSTEM, DUCTS AND COMPONENTS. NO DEFECTS WERE NOTED. VERIFIED SECURITY AND FREEDOM OF OPERATION OF LEFT CONDITIONED AIR, CHECK VAVLE AND RAM AIR(COLD) CHECK VALVE, NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED LEFT FLOW CONTROL VALVE PER ALL APPLICABLE MANUALS. 2L74 4F 4A25 20050223000772005022300077NM 2005 2 23 DHL2004780506 120040909A5320 WEB BOEING727 727223 1384074NM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A C-CHECK, CORROSION ON WEB BETWEEN FRAMES 950D AND 950E WHERE IT ATTACHES TO STR 30 IN THE AFT BAG BIN. ON AFT PIT BETWEEN STA 950D AND 950E STR 30, REMOVED WEB IAW B727 SRM 51-30-2 FAB NEW IAW B727 SRM 51-20-1 FIG 7 MAT USE 7075T6 .040, 19 1/2" X 8 1/4", PO NR 9001068 IAW B727 SRM 53-10-2 FIG 5. TREATED AND PRIMED WEB IAW B727 SRM 51-10-2 INST WEB IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050223000782005022300078NM 2005 2 23 04FDEA02602 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B HOLE SPOTFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL THICKNESS=0.502 INCH, MATERIAL REMOVED=0.002INCH, REMAINING THICKNESS=0.500 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20050223000792005022300079NM 2005 2 23 04FDEA02603 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, I/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.093 INCH, FINAL DIAMETER=1.125 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20050223000802005022300080NM 2005 2 23 04FDEA02604 120040902A5753ARC199114 BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4, ORIGINAL DIAMETER=1.062 INCH, FINAL DIAMETER=1.094 INCH AND REPAIRED AS PER EA NR 1-5750-80339, TITLE: WINGS, RIGHT HAND OUTBOARD FLAP, OUTBOARD HINGE AFT BRACKET (FLAP SIDE) PIVOT AND ACTUATOR BORES, CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20050223000812005022300081NM 2005 2 23 DHL2004780508 120040910A5330 SKIN BOEING727 727223 1384074NM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A C-CHECK, DENT IN SKIN AT STA 1400 BETWEEN STR 4L AND STR 5L. REMOVED FASTENERS AS REQ FOR REPAIR AT STA 1400 ATR 4L & STR 5L IAW B727 SRM 51-30-2. CUT OUT AREA DAMAGE, FOUND OUT OF LIMITS. DIMENSION 2 1/2 X 3. FABRICATED REPAIR DOUBLER MATERIAL USED 2024T3 .063 PO NR 90024 DIMENSIONS 11 1/2 X 9 1/2 IAW B727 SRM 53-30-3 FIG 1 ALODINED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER AT STA 1400 BETWEEN STR 4L AND STR 5L IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050223000822005022300082NM 2005 2 23 DHL2004780512 120040912A5754 DOUBLER BOEING727 727223 1384074NM NR 6 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A C-CHECK, NR 6 SLAT RIB REPAIR DOUBLER IS CRACKED AT NUT PLATE, INBD OF ACTUATOR. REMOVED ACCESS PNL AT SLAT NR 6 ROUTED OUT CRACK AREA, FABRICATED DOUBLER FROM 0.032 CRES AISI 321 PO NR 900878 DIM 6 1/2 X 3 3/4 AND TREATED PRIMED AND INSTALLED DOUBLER AND REINSTALLED ACCESS PNL AND ACTUATOR BOLT IAW B727 SRM 57-50-3 FIG 9 51-10-2 AND 51-30-2. 2L73 4F A3WE 20050223000832005022300083GL 2005 2 23 ERAA097497 220040914A725023037447 COVER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL SUMP MISOVERHAULED B ERAAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 AL03124EH S559 SUMP COVER AIR HOLE IS BLOCKED. RETURNING ON ERA REPAIR ORDER NR RW-900461 REQUESTING WARRANTY REPAIR. 1G72 3U3 U H3EU E4CE 20050223000862005022300086 2005 2 23 ERAA097500 420040617A2562 G SWITCH BELL 412 412 1182202SW ELT INOPERATIVE E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH 67843 33064 FOUND G SWITCH INOPERABLE. FOUND G SWITCH INOP. SENT UNIT TO ARTEX FOR REPAIR. 1G72 4U H4SW 20050223000882005022300088 2005 2 23 ERAA097502 420040913A2562 G SWITCH SNIAS AS332 AS332L 8680809EU ELT INOPERATIVE E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03170EH 68128 THIS INFO FOR FAA SDR. FOUND G SWITCH TO BE NOPERABLE. CORROSION ON FRONT SIDE OF UNIT. ACTION TAKEN: SENT UNIT TO MANUFACTURER FOR REPAIR. 2G72 4U H4EU 20050223000922005022300092EU 2005 2 23 ERAA097506 120040625A63206894171 GEARBOX BOLKMS105 BO105S 5626006EU MAIN ROTOR SPLIT E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH16819 S675 BLACK FLAKES IN OIL. TORQUE SPLITS. FLAKES FROM OIL PUMP BODY SEPARATOR. WORN POCKET ON OIL PUMP PRESSURE BODY. COMPLIED WITH CEB-1135 GEARBOX COVER REPLACED, INCREASED RIGIDITY AT TORQUE METER SUPER SHAFT BOSS. OVERHAULED GEARBOX. 1G72 3U H3EU 20050223000962005022300096NE 2005 2 23 ERAA097510 120040711A64107610105101041 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR ERODED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 5720 T/R BLADE HAS EROSION. SENT TO CTI FOR REPAIR. UNIT X-RAYED, ULTRASONIC INSPECTED PER QATI3016.3261 AND 3098 PERFORMED ALL SCHEDULED INSPECTIONS UP TO AND INCLUDING 1500 HOUR INSPECTION IN ACCORDANCE WITH COMPOSITE MM 4047-76-5 TABLE 3-2 AND MM 4047-76-2, 65-21-00 AND 65-21-01 INSPECTED, ELLIPTICAL PLUG FOR DEBONDING X-RAY REVEALS 50 TO 75 CELLS H20 IN PADDLE B. REMOVED MOISTURE, REPLACED BOTH PRIMARY POLYURETHANE STRIPS. REPLACED BOTH SUPPLEMENTAL POLYURETHANE STRIPS. ADHESIVE INJECTION REPAIR ON PADDLE, REPLACED PYLON SIDE LAMINAR PAD ON PADDLE B AND REMOVED AND REPLACED PADDLE B. REPAIRED TRAILING EDGE ON PADDLE B AND REASSEMBLED CENTER HARDWARE . 1G72 3U H1NE 20050223000972005022300097NE 2005 2 23 ERAA097511 120040721A64107610105101042 BLADE SKRSKYS76 S76A 8143006NE TAIL ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 2168 VOIDED AT TIP BLOCK AREA. X-RAYED, ULTRASONIC, INSPECTED, PERFORMED ALL SCHEDULED INSPECTIONS UP TO AND INCLUDING 1500 HR INSPECTION. REPLACED BOTH PRIMARY POLYURETHANE STRIPS. REPLACED BOTH SUPPLEMENTAL POLYURETHANE STRIPS AND REPAIRED TIP WEIGHT COVER ON PADDLE A. REPLACED PITCH HORN BUSHINGS ON BOTH PADDLES. REPLACED PIVOT RETAINERS, REPLACED TIP CAP ON PADDLE B REPLACED SPAR PLUG REPLACED AND REASSEMBLED CENTER HARDWARE. REFINISHED PAINT STATIC BALANCED. 1G72 3U H1NE 20050223000982005022300098NE 2005 2 23 ERAA097512 120040711A32127625101102102 FLOAT SKRSKYS76 S76A 8143006NE MLG LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03577EH 760222 FLOAT LEAKING. SENT TO OFFSHORE HELICOPTER FOR REPAIR. REPAIRED IAW OHSS 100-1 AND C/W INSPECTION IAW 32-70-03. 1G72 3U H1NE 20050223000992005022300099SW 2005 2 23 ERAA097513 120040125A6410 BLADE BELL 412 412 1182202SW T/R HEAD ERODED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03169EH1392 HB747 33064 TIP RIVETS ERRODED. TIP RIVETS OF BLADE A11405 ERRODED, TRUNNION ROUGH, FEATHER BEARINGS HAVE PLAY ONE BEARING GALLED, T/R BLADES. REMOVED TO F.O.M. REMOVED YOKE BEARINGS, TRUNNION ASSY, NDT INSPECTED, BEARING BORES, INSTALLED NEW BEARINGS, STAKED IAW 412 CR&O, INSTALLED SERVICEABLE TRUNNION, BEARINGS AND SEALS. ASSEMBLED HUB ASSY IAW TB 412-95-134 & 412 CR&O INSTALLED SERVICEABLE T/R BLADES, MARVEL BALANCED, TORQUED AND SAFETIED IAW 412 CR&O., COMPLIED WITH ASB412-00-106 PART B T.B. 412-95-134. 1G72 4U H4SW 20050223001012005022300101SW 2005 2 23 ERAA097517 120040831A3246 SADDLE BELL 412 412 1182202SW SKID TUBE BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 1082L FORWARD SADDLE ON SKID TUBE BROKEN. FWD SADDLE ON SKID TUBE BROKEN. PERFORMED INSPECTION OF ALL FLOATS, COVERS AND HOSES IAW ERA 412 CAMP-1, INSPECTION GUIDE AND BHT-412-SI-2. ALL COMPONENTS FOUND TO BE IN SERVICEABLE CONDITION. REMOVED ALL COMPONENTS FROM UNSERVICEABLE SKID TUBE AND REINSTALLED THEM ONTO SERVICEABLE SKID TUBE, VERIFIED COMPLIANCE WITH ABS 412-93-78. 1G72 4U H4SW 20050223001042005022300104EU 2005 2 23 ERAA097521 120040804A642010531714 ROTOR HEAD BOLKMS105 BO105S 5626006EU TAIL ROTOR DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03149EH9013 S705 INNER SLEEVE HAT BUSHING DIMENSION TOO LARGE. COULD NOT INSTALL. REMOVED MOUNTING FORK AND BLADE ASSEMBLIES. REMOVED AND REPLACED 2 EA INNER SLEEVE HAT BUSHINGS. MILLED TO PROPER DIMENSIONS AND LINE REAMED BORGS AS REQUIRED. VISUALLY INSPECTED AND FOUND NO OTHER DEFECTS. REATTACHED FORKS AND BLADES WITH ORIGINAL HARDWARE. TORQUED NUTS AND SAFETIED. STATIC BALANCED HUB AND BLADE ASSY. REPAIRED IAW BO-105 REM 301-AND MM CHAPTER 33, 34 AND 107. 1G72 3U H3EU 20050223001052005022300105EU 2005 2 23 ERAA097522 120040624A63204619005001 BLOWER BOLKMS105 BO105S 5626006EU OIL COOLER CHAFED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03S769 CUSTOMER OWNED AIRCRAFT. BLOWER FAN WHERE RUBS. FOUND INBOARD BEARING ROUGH. SCRAPPED BEARING, HOUSING DUE TO EXCESSIVE PITTING. FOD HAS BEEN BETWEEN WHEEL AND HOUSING, NO DAMAGE TO FAN WHEEL, SLIGHT RUB MARKS IN PAINT ON HOUSING, PROBABLY SOMETHING LIKE GRASS WAS CAUGHT BUT WAS LOST DURING REMOVAL FROM A/C. ALSO, FEELS LIKE ONE BEARING IS ROUGH. DISASSEMBLED BLOWER ASSY, INSPECTED, REPAIRED IAW REM 104-7. INSTALLED NEW HOUSING, INBOARD BEARING, SEAL AND PACKINGS. SANDED AND REPAINTED HOUSING. REASSEMBLED IAW REM 104-7. 1G72 3U H3EU 20050223001062005022300106EU 2005 2 23 ERAA097523 120040823A63203701020000 OIL COOLER BOLKMS105 BO105S 5626006EU M/R GEARBOX DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03152EH S701 AIRCRAFT IN MAJOR INSPECTION AND OIL COOLER SENT OFF FOR INSPECTION AND REPAIR. OIL COOLER OVERHAULED. 1G72 3U H3EU 20050223001082005022300108EU 2005 2 23 ERAA097525 120040724A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU MLG TORN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH S675 INSPECTION DUE ON FLOAT ASSY. FLOAT COVER AND FWD END CAP WORN AND TORN. SQUIB CHARGE (1) P/N 94455 (SN 1709) EXPIRES 12-04. ELBOW ON SQUIB VALVE CORRODED. BAD CHECK VALVE ON AFT COMPARTMENT OF FLOAT BAG. REMOVED AND REPLACED FWD END CAP AND FLOAT COVER. REMOVED SQUIB CHARGE (SN 1709) AND INSTALLED CHARGE (SN 3341). REMOVED AND REPLACED 1 EA SQUIB VALVE ELBOW (PN B17794-1). REMOVED AND REPLACED 1 EA CHECK VALVE PN B17573-5 ON FLOAT BAG. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1G72 3U H3EU 20050223001092005022300109EU 2005 2 23 ERAA097526 120040809A3212D24873102 FLOAT BOLKMS105 BO105S 5626006EU MLG LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH 598 CYLINDER LEAKING. CYLINDER SQUIB VALVE ASSY TO BE LEAKING. REMOVED SQUIB VALVE/MANIFOLD ASSY FROM CYLINDER. REMOVED AND REPLACED O-RING AND BACK UP RING. VALVE TO MANIFOLD JUNCTION AND RE-INSTALLED VALVE/MANIFOLD ASSY ONTO CYLINDER. RE-CHARGED CYLINDER AND LEAK CHECKED. NO LEAKS FOUND. PERFORMED 6 MONTH INSPECTION ON REMAINDER OF FLOAT ASSY. VERIFIED COMPLIANCE WITH SB NUMBERS 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1G72 3U H3EU 20050223001102005022300110EU 2005 2 23 ERAA097527 120040904A3212D24873101 FLOAT BOLKMS105 BO105S 5626006EU MLG LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH S675 FLOAT ASSY DUE 6 MONTH ASSY. SQUIB ALE LEAKING AT VALVE/MANIFOLD JUNCTION FWD CHECK VALVE ON BAG NOT OPENING PROPERLY. FLOAT BAG HAS EXCESSIVE NUMBER OF HOLES AT AFT COMPARTMENT. FWD END CAP WORN AND TORN. REMOVED AND REPLACED 1 EA O-RING AND 1 EA BACK UP RING AT VALVE TO MANIFOLD JUNCTION. REPLACED 1 EA CHECK VALVE ON BAG. REMOVED FLOAT BAG SN 0808, AND INSTALLED FLOAT BAG (SN -0705). REMOVED AND REPLACED 1 EA FWD END CAP. VERIFIED COMPLIANCE WITH S'S NR'S 120-81-3, 120-81-4, 120-82-4, 120-84-1, 802-25-1, 802-25-2. 1G72 3U H3EU 20050223001112005022300111EU 2005 2 23 ERAA097528 120040121A2435 ARMATURE BOLKMS105 BO105S 5626006EU STARTER GEN ARCED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03153EH8332 22090 702 STARTER GEN INTERMITTENT. ARMATURE AND STATOR DAMAGED. SIGNS OF ARCHING ON ARMATURE. OVERHAULED AND TESTED. 1G72 3U H3EU 20050223001132005022300113EU 2005 2 23 ERAA097530 120040428A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03293EH 559 GUIDE ASSY INOPERABLE FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO-105 REM 405. 1G72 3U H3EU 20050223001142005022300114EU 2005 2 23 ERAA097531 120040527A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03293EH 559 GUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 REM 405. 1G72 3U H3EU 20050223001152005022300115EU 2005 2 23 ERAA097532 120040610A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03129EH 580 GUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, SPRING, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105- REM 405. 1G72 3U H3EU 20050223001162005022300116EU 2005 2 23 ERAA097533 120040627A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM BROKEN E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03423EH GUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED, NEW SOCKET, SPRING, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 - REM 405. 1G72 3U H3EU 20050223001212005022300121 2005 2 23 ERAA097539 420040810A2562 G SWITCH SNIAS AS332 AS332L 8680809EU ELT DEFECTIVE E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03170EH 68911 THIS INFO FOR FAA SDR. ELT SENT TO ARTEX FOR INSPECTION BATTERY HAS LOW VOLTAGE G SWITCH IS STUCK ACTION TAKEN: REPLACED G SWITCH, SUB ASSY INCORRECT PART INSTALLED DURING ASSY 452-0181-01, TESTED IAW ARTEX PROCEDURES, REPLACED BATTERY PACK AND ELT MEETS ALL SPECIFICATIONS. 2G72 4U H4EU 20050223001522005022300152EU 2005 2 23 DHL2004362013 120041007A3240 BRAKE AIRBUS300 A300B4203 3930306EU MLG MALFUNCTIONED A DHLAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01362DH 84 BOTH BRAKES GRABBY AND CHATTERY. BLED AND INSPECTED BRAKES. NO DEFECTS NOTED. PERFORMED NORMAL BRAKING TEST. NO DEFECTS NOTED, ALL IAW M/M 32-42-00. OPS CK GOOD AT THIS TIME. 2L72 4F RTA35EU 20050222000542005022200054NM 2005 2 22 ASA0440244 120041201A53206545807U30 ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FOUND UPPER LOBE, ANGLE CRACKED. REPLACED PER SRM. (M) 2L72 4F RTA16WE 20050222000572005022200057WP 2005 2 22 04FDEA01871 120040628A3241 WARNING LIGHT DOUG DC10 DC1030F 3023504WP ANTI-SKID SYSTEMILLUMINATED A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25301FE 46800 UPON LOWERING GEAR FOR LANDING, GOT "ANTI SKID L FAIL" ALERT, WENT MISSED APPROACH AND RAISED GEAR. LOWERED GEAR A SECOND TIME AND GOT SAME ALERT. FOLLOWED CHECKLIST BY TURNING ANTI-SKID OFF, THEN BACK TO ARM. ALERT WENT OUT. TESTED ANTI-SKID AND ALERT STAYED OFF. RETESTED ANTI-SKID ON GROUND AND TESTED OK. PERFORMED PHYSICAL INSPECTION ON MLG, NO DEFECTS NOTED, TIRE PRESSURES NORMAL PER SERVICE CHECK WORK CARDS. PERFORMED ANTI-SKID SYSTEM OPS TEST PER MM 32-45-00-2 WITH PASSING RESULTS. NO DEFECTS NOTED. 2L73 4F RTA22WE 20050222000612005022200061EU 2005 2 22 DHL2004364010 120040629A3230 LANDING GEAR AIRBUS300 A300B4203 3930306EU NR 1 SYSTEM MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01364DH 141 UNABLE TO RAISE THE LANDING GEAR HANDLE AFTER TAKEOFF. SYSTEM 1 INOPERATIVE. COMPLIED WITH ABNORMAL PROCEDURES. DEFERRED NR 1 LEVER LOCK AND WARNING SYSTEM IAW MEL 32-31-02A, DMI NR 17050 PLACARD INSTALLED, SYS NR 2, OPS NORMAL. 2L72 4F RTA35EU 20050222000732005022200073NM 2005 2 22 04FDEA01770 120040617A5753ARC2512 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE CORRODED. RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGIGINAL DIAMETER=1.187 INCH, FINAL DIA 1.283 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76743, TITLE: WINGS, LEFT AND RIGHT INBOARD TRAILING EDGE FLAP, HINGE BRACKETS CORRODED. 2L73 4F RTA22WE 20050222000762005022200076NM 2005 2 22 USAA041137 120041229A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19384US53622 22957 CLT - FOUND SKIN CRACKED 10 INCHES AFT OF STATION 727E BELOW STRINGER 18R AND STATION 749 S19R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050222000782005022200078WP 2005 2 22 04FDEA01939 120040705A5347S4929311 SEAT TRACK DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25398FE 46634 AFT LWR CARGO COMPT, RT CARGO TRACK HAS SEVERAL NICKS AND DINGS ON UPPER SURFACE AND CORROSION INSIDE TRACK LOBES. REMOVED CORROSION IAW SRM 51-21-01 VOL 1 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW SRM 53-70-00 FIG 1 VOL 1. 2L73 4F RTA22WE 20050222000822005022200082EU 2005 2 22 04FDEA01936 120040705A2910 HOSE AIRBUS300 A300B4605R 3930308EU HYD SYSTEM LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25664FE 768 ON T/O OUT OF MEM , GOT YELLOW HYD RES: LOW AND HYD YELLOW PRESS LOW WARNINGS. COMPLIED WITH ECAM , REVIEWED QRH, AND RETURNED TO MEM. UPON INSPECTION FOUND RT WING AILERON INB MOSTACTUATOR HYD HOSE RUPTURED. ORDERED HOSES AND PLACED IN A/C FOR TURN OVER. REMOVED AND REPLACED AILERON HYD HOSE PER AIRBUS SMP ITEM STILL NEEDS LEAK CK AND HYD SYTEMS NEEDS SERVICING. SERVICED YELLOW HYD SYSTEM AND OPS CHECKED AILERONS. OPS CHECK GOOD. 2L72 4F RTA35EU 20050222000842005022200084WP 2005 2 22 04FDEA01933 120040703A5315 FLOORBEAM DOUG DC10 DC1030 3023501WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25323FE 47811 FORWARD CARGO PIT FLOORBEAM AT FUSELAGE STATION 775 IS CRACKED. REMOVED CENTER ROLLER TRAY FOR ACCESS. FABRICATED REPAIR FILLER ANGLE, REPAIR ANGLE AND CUT OUT DAMAGED AREA IAW DC10 SRM 53-00-01 VOL I. INSTALLED REPAIR PARTS AT STATION 775 FLOORBEAM IAW DC10 SRM 53-00-01 VOL I. REINSTALLED CENTER ROLLER TRAY AT STATION 606-879 IAW DC10 SRM 51-31-01 VOL II. REFERENCE N/R N00368. 2L73 4F A22WE 20050222000872005022200087NM 2005 2 22 C1HA200483010 120040702A2121 FAN BOEING727 7272S7 138407ZNM LT A/C PACK INOPERATIVE A C1HAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL15683CA 22490 DURING PS CK FOUND LT PACK GRD COOLING FAN INOP AND POPPED CB, FWD DRAIN MAST INOP & POPPED CB FOUND WIRING CHAFFING BEHIND GILL LINER IN FWD PIT AFT LT CORNER REPAIRED WIRING PER BOEING SP 20-10-11 & OPS CK GOOD MM 38-33-21. GASPER FAN INOP & POPPED CB FOUND WIRING CHAFFING BEHIND GILL LINER IN FWD PIT AFT LT CORNER REPAIRED WIRING BOEING STANDARD WIRING PRACTICES 20-10-11 & OPS CKD GOOD MM 21-23-00 LT PACK FAN INLET DOOR INOP & POPPED CB. FOUND WIRING CHAFFING BEHIND GILL LINER IN FWD PIT AFT LT CORNER REPAIRED WIRING BOEING STANDARD PRACTICES 20-10-11 & OPS CK GOOD MM 21-56-71 GASPER FAN DUCTING DAMAGED JUST FWD OF FAN R/R DUCT ASSY & Y DUCT ASSY MM 21-20-04 COMPLY WITH E/C E99683-3 HFEC INSPECTION COMPLIED 2L73 4F A3WE 20050222001102005022200110NM 2005 2 22 TSAA0429054 120040716A29136507506 PUMP BOEING737 7372X6C 1384552NM NR 2 ENGINE FAILED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13816AL4849 23122 HYDRAULIC SYSTEM FAILED. TURNED TO HNL. REMOVE AND REPLACE NR 2 ENGINE HYDRAULIC PUMP IAW AMM 29-11-32. LEAK AND OPS CHECK GOOD. REMOVE AND REPLACE NR 1 AND NR 2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTERS. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050222001122005022200112NM 2005 2 22 04FDEA01941 120040706A5753ARC0503 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE, UPPER SIDE LINK HOLE CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER= 0.323 INCH, FINAL DIAMETER= 0.409 INCH, AND REPAIRED AS PER EA NR 1-5740-76785, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20050222001842005022200184EU 2005 2 22 ERAA096616 120040608A25604530190 ELT BOLKMS105 BO105A EU CABIN CRACKED A ERAAO OTHER O OTHER NRNOT REPORTED 1 SO03135EH2054 S675 FOUND CRACKED ELT ASSY. SENT UNIT TO MANUFACTURER FOR REPAIR. 1G72 3U H3EU 20050222001882005022200188NE 2005 2 22 ERAA096623 120040524A62107615009043054 TIP CAP SKRSKYS76 S76A 8143006NE M/R BLADE DEBONDED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03575EH 760366 TIP CAP ASSY BOTTOM DISBONDED. SENT TO CTI FOR REPAIR. INSPECTED PER SA4047-76-5 REV11; REPAIRED KEVLAR PER PROCEDURE NR 2 AND NR 18 1 PLY; REFINISHED PER DRWG NO 76150-09043; STATIC BALANCE PER RS-005N-VI. 1G72 3U H1NE 20050222002232005022200223NM 2005 2 22 200419 120041030A3231 DOOR DHAV DHC8 DHC8103 1386005NM MLG MALFUNCTIONED A KPVAO OTHER O OTHER CLCLIMB 1 WP13807WP 023 (PIREP) LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. PERFORMED ALT GEAR EXT PROCEDURE, OVERHEAD DOOR WAS FOUND OPEN. (MX) CONSULTED W/FLT CREW AND DETERMINED FAILURE TO RETRACT DUE TO OPEN EMERGENCY MLG RELEASE DOOR. PERFORMED EXPANDED PSEU BITE DIAGNOSTIC TEST AND RECOVERED CORROBATIVE FAULT CODES IAW DHC MM 32-61-50 PG 202-204 PARA 2A. NO FURTHER DEFECTS NOTED. 2H72 4T RTA13NM 20050222002242005022200224WP 2005 2 22 DHL2004809009 120041030A5210 MECHANISM DOUG DC8 DC873F 302199FWP PAX DOOR LACK OF LUBE A DHLAK NONE O OTHER CRCRUISE 1 SO01809DH 46047 CABIN ENTRY DOOR STICKS SHUT INFLIGHT VERY HARD TO RE-ENTER COCKPIT. LUBED DOOR PER NAS INC MM 52-10-0 PG 301, OPS CHK'S GOOD. 2L74 4F RT4A25 20050222002322005022200232NM 2005 2 22 EIA2004124 120040930A5311 FRAME BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CRACK AT END OF MAIN DECK FRAME AT FASTENER HOLE, BS 340, S-16L. REPAIRED FRAME PER SRM 53-10-04, FIG 85. 2L74 4F RTA20WE 20050222002582005022200258 2005 2 22 ERAA097112 420040601A341661031004 ALTIMETER BELL 412 412 1182202SW COCKPIT FAILED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03423EH 200 FT DIFFERENCE ON MODE C. UNIT FAILED SCALE ERROR TEST. TESTED UNIT. FAILED SEND TO ANCHORAGE FOR REPAIR. 1G72 4U H4SW 20050222002612005022200261EU 2005 2 22 ERAA097113 120040627A6320AHA1121MOD12345 CALIPER BOLKMS105 BO105A EU M/R GEARBOX DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03135EH S675 DISC RUBBING CALIPER ASSY. CLEANED, INSPECTED, AND REPAIRED. TESTED. 1G72 3U H3EU 20050222002662005022200266 2005 2 22 HNAA0400158 420041028A34257003360941 AHRS DHAV DHC8 DHC8311 1386006EA NR 2 FAILED A HNAAO OTHER I FLT. ATTITUDE INST. CRCRUISE 1 EA07336EN 336 NR 2 AHRS FAILED IN FLIGHT, DETECTED BAD WEATHER. REMOVED AND REPLACED NR 2 AHRS, OPS CHECK GOOD. 2H72 4T RTA13NM 20050223000082005022300008NM 2005 2 23 DHL2004762003 120040908A2150 WARNING LIGHT BOEING727 7272B7 138407LNM A/C PACK ILLUMINATED A DHLAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01762AT 22162 AUTO PACK TRIP LIGHT ILLUMINATED ON START OF TAKEOFF ROLL. DEFERRED CONTROL NR 17783 MEL 21-4, OK FOR SERVICE. 2L73 4F A3WE 20050223000142005022300014NM 2005 2 23 04FDEA02515 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, XORS= 1020 FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 1020 AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000182005022300018WP 2005 2 23 04FDEA02643 120040904A5410ATL005511 PAN DOUG DC10 DC1010F 3022111WP ZONE 400 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 NR 2 ENGINE RIGHT HAND FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER "U" BOLT. REMOVED CENTER "U" BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW DC10 SRM 51-35-01 VOL II. WELD REPAIRED IAW FEDEX EA 8-5410-81450. INSTALLED PAN IAW DC10 SRM 51-31-01 VOL II. INSTALLED CENTER "U" BOLT AND FITTING IAW DC10 SRM 51-31-01 VOL II, REFERENCE N/R N00899. 2L73 4F A22WE 20050223000342005022300034NM 2005 2 23 04FDEA02522 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX E NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000432005022300043WP 2005 2 23 04FDEA02648 120040904A5415AUB702533 FITTING DOUG DC10 DC1030F 3023504WP NR 3 PYLON MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25321FE 47836 NUMBER 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATING. REMOVED SPHERICAL BEARING HONED HOLE REMOVED AFT BULKHEAD FITTING, LOCATED AND DRILLED NEW FITTING IAW DAC DWG AUB 7025, INSTALLED NEW FITTING P/N AUB 7025-33 IAW DAC DWG AUB 7025 IAW FEDEX DC10 SRM 51-38-01 VOL II, REAMED 2 EACH HOLES IAW FEDEX DC10 SRM 51-31-01 VOL II. INSTALLED DRAIN LINE PREVIOUSLY REMOVED IAW DC10-30 SRM 54-10-00. 2L73 4F RTA22WE 20050223000482005022300048NM 2005 2 23 04FDEA02656 120040905A5753ARC4125501 STOP FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25593FE 48551 LT WING OUTBOARD FLAP INBOARD STOP FITTING FOUND CRACKED. REMOVED CRACKED FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LEFT HAND WING OUTBOARD FLAP INBOARD AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050223000572005022300057CE 2005 2 23 GLBA20030723 120040920A29101013880167 LINE BEECH 1900 1900D 1154162CE HYD SYSTEM LEAKING A GLBAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM03169GL UE169 LANDING GEAR WILL NOT EXTEND, MANUALLY EXTENDED, FOUND BAD HYD LINE. REMOVED AND REPLACED, OPS CK GOOD. 2L72 4T RTA24CE 20050223000622005022300062CE 2005 2 23 ACE09242004 120040924A2120 DUCT BEECH 1900 1900C 1154161CE HEATER CONTAMINATED E YADAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL03114AX UC36 UNUSUAL ODOR EMANATING FROM AIR DUCTS WHEN BLEED AIR SYSTEM TURNED ON. RETURNED TO AIRPORT FOR INVESTIGATION, MAINTENANCE RECONNECTED MAIN HEATER DUCT IN BELLY (BELLY HAD CARGO SPILL RESIDUE IN AREA). 2L72 4T RTA24CE 20050223000892005022300089 2005 2 23 ERAA097503 420040409A2562 G SWITCH BELL 412 412 1182202SW ELT FAILED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03422EH 64818 33068 FAILED G SWITCH TEST. DAMAGED MOUNTING TRAY AND END CAP. REPLACED G SWITCH, MOUNTING TRAY AND END CAP. TESTED AS NECESSARY. 1G72 4U H4SW 20050223000932005022300093GL 2005 2 23 ERAA097507 220040714A72306890550 COMPRESSOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE CRACKED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH10849 598 CRACKED AND FOD ON IMPELLER VANES. OVERHAULED COMPRESSOR, COMPLIED WITH CEB A-1392 ADAPTER COUPLING. 1G72 3U3 U H3EU E4CE 20050223001022005022300102SW 2005 2 23 ERAA097518 120040729A3246420500015110R SKID BELL 412 412 1182202SW MLG CORRODED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH SKID TUBE SEVERELY CORRODED. SKID TUBE CORRODED BEYOND LIMITS. ALL FLOAT AG COVERS WORN AND TORN. AFT FLOAT BAG HAS EXCESSIVE NUMBERS OF HOLES. FWD FLOAT BAG AS 2 HOLES. ALL RUBBER BANDS AND RETAINERS ON FLOAT COVES IN NEED OF REPLACEMENT. ALL 8 BUSHINGS ON PASSENGER STEP WORN. 1 EA RIV NUT ON SKID TUBE SPINNING. DISASSEMBLED FLOAT ASSY AND REPLACED SKID TUBE. UPON REASSEMBLY, CHANGED ALL FLOAT COVERS ALONG WITH ATTACHED RUBBER BANDS AND RETAINERS, REPLACED AFT FLOAT BAG AND REPAIRED HOLES IN FWD BAG. REPLACED SPINNING RIV NUTS AND BUSHINGS. REPLACED AFT FLOAT BAG AND REPAIRED HOLES IN FWD BAG. REPLACED SPINNING RIV NUTS AND BUSHINGS ON STEP ASSY. VERIFIED TIME REM 1G72 4U H4SW 20050223001072005022300107EU 2005 2 23 ERAA097524 120040609A3213D24762102 FLOAT BOLKMS105 BO105S 5626006EU MLG DELAMINATED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 1280 DELAMINATED AT TOPPING OFF VALVE ON NR 2 COMPARTMENT. SENT IN FOR REPAIR. FLOAT WAS REPAIRED AND TESTED GOOD IAW 25-60-95. 1G72 3U H3EU 20050223001532005022300153NE 2005 2 23 NACA20040044 220040930A8530356996 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 R2800CB3 52026NE ENGINE CRACKED A NACAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL03779TA2106 2106 45529 P34011 NR 3 ENGINE, NR 18 CYLINDER RIGHT AND LEFT LOW COMPRESSION. CHECKED NR 18 CYLINDER AND SYNC GENERATOR, BOTH CHECKED GOOD. FOUND NR 11 CYLINDER WITH A CRACKED HEAD, REPLACED CYLINDER. CHECKED GOOD. 2L74 4R4 R A781 5E8 20050223001542005022300154WP 2005 2 23 04FDEA02883 120041007A5512ALC74291 PANEL DOUG DC10 DC1010F 3022111WP ZONE 300 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LEFT HORIZONTAL STABILIZER 1 EACH PANEL AT STATION XE122 COMPOSITE PANEL AT AFT SPAR TOP SIDE IS DELAMINATED. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKIN, INNER DOUBLER AND CORE IAW DWG ALC7429 AND EA 8-5510-81439 AND TPS 1001 REV E. REFERENCE NON-ROUTINE N01578. 2L73 4F A22WE 20050223001552005022300155WP 2005 2 23 04FDEA02884 120041007A5510ALC7084 FITTING DOUG DC10 DC1010F 3022111WP ZONE 300 MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE, STABILIZER TO STABILIZER BOX SAFETY LINK, OUTBOARD ATTACH CLEVIS BUSHING WORN AND MIGRATED THROUGH STABILIZER LOWER INBOARD ACCESS PANEL 334MB. REMOVED FITTING FOR INSTALLATION OF REPAIR BUSHING IAW FEDEX DC10 SRM 55-10-00 VOL 1. REMOVED AND REINSTALLED BEARING, HAND STAKED IAW FEDEX EA 8-5510-81489, HORIZONTAL STABILIZER SIDE LOAD SUPPORT FITTING. REINSTALLED FITTING IAW FEDEX DC10 SRM 51-31-01 VOL II, REMOVED AND REINSTALLED FORWARD BULKHEAD ACCESS PANEL AND HORIZONTAL STABILIZER LEADING EDGE IAW FEDEX DC10 SRM 51-31-01 VOL II AND DC10 MM 55-30-01-2. REFERENCE NONROUTINE N02092. 2L73 4F A22WE 20050223001562005022300156WP 2005 2 23 04FDEA02885 120041007A5313 LONGERON DOUG DC10 DC1010F 3022111WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LOWER FUSELAGE UNDERWING LONGERON 49R IS CORRODED FROM STATION 1368 TO 1521. REMOVED CORROSION LONGERON 49R, FOUND TO BE OUT OF LIMITS. REMOVED LONGERON 49R FROM STATION 1330 TO 1521. FABRICATED LONGERON 49R IAW DAC DWG 7013 AND SPLICE REPAIR IAW DC10 SRM 53-00-01 VOL 1 PAGE 30. INSTALLED NEW END FITTING LONGERON AND REPAIR SPLICES IAW DAC DWG AYB 7020, 7013 AND DC10 SRM 53-00-01 VOL II, REFERENCE NON-ROUTINE N00937. 2L73 4F A22WE 20050223001592005022300159NE 2005 2 23 DHL2004809008 220041008A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 4 FLAMED OUT A DHLAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01809DH 46047 ENGINE NR 4 FLAMED OUT AT FL 370, RAN ENGINE FAILURE EMERGENCY. CHECK LIST FOLLOWED BY THE ENGINE INFLIGHT START, BUT NO LIGHT OFF DESCENDED TO FL250 TRIED ANOTHER ATTEMPT TO START WITH NO LIGHT OFF. STILL NO LIGHT OFF. TROUBLESHOT PER CFM 71-00-00. PERFORMED VISUAL INSP INLET AND EXHAUST ENG FOR SERVICEABILITY. NO DEFECTS NOTED, PERFORMED DC-8 POWER ASSURANCE CHECK PER JRH 13.3, SYS CK GOOD PERFORMED ACCELERATION. 2L74 4F4 FRT4A25 E2GL 20050223001652005022300165EU 2005 2 23 DHL2004363507 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 3877 FS 34-FS 38.2 RBL 98 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FS 34 TO FS 38.2 AT RBL 98 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT, PRIMED AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 34 TO FS 38.2 AT RBL 98 IAW A-300 SRM 51-30-30 AND 53-10-10. 2L72 4F RTA35EU 20050223001662005022300166EU 2005 2 23 DHL2004363508 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 3879, LBL 20 BETWEEN FS 15 AND FS 19 SEAT TRACKS CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVE SEAT TRACK FROM FS 15 TO FS 19 LBL 20 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT, PRIMED, AND PAINTED IAW A-300 SRM 51-40-10 AND 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 15 TO FS 19 AT LBL 20 IAW A-300 SRM 53-10-10. NOTE: MATERIAL USED P/N 60-22457, PO NR 24302234. 2L72 4F RTA35EU 20050223001712005022300171WP 2005 2 23 04FDEA02907 120041011A5753ARC25122 HINGE FITTING DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 RIGHT HAND INBOARD FLAP PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION BEGINNING BORE 1.1875 INCH FINAL 1.2583 INCH MATERIAL REMOVED .0708 INCH IAW DACCMM 57-52-01. FABBED REPAIR BUSHING IAW DACCMM 57-52-01 AND EA8-5750-81475. PERFORMED MPI IAW DPS 4.704. CAD PLATED, INSTALLED AND HONED REPAIR IAW DACCMM 57-52-01. 2L73 4F RTA22WE 20050223001802005022300180NM 2005 2 23 DHL2004745019 120040828A3260 WARNING LIGHT BOEING727 727224 1384076NM MLG ILLUMINATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01745DH 20665 RIGHT MAIN GEAR DOOR ILLUMINATED AFTER GEAR SELECTED UP THEN OFF. PERFORMED MAIN GEAR DOORS EXTENSION AND RETRACTION TEST, 7 CYCLES AND IN OFF POSITION IAW B-727 MM 32-12-0. OPS CHECK GOOD, FOUND NORMAL. 2L73 4F A3WE 20050223001812005022300181WP 2005 2 23 DHL2004801532 120040908A5720 CLIP DOUG DC8 DC873F 302199FWP RT WING BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT WING NR 4 ALT TANK CLIP BROKEN REF 505B ACCESS DOOR. REMOVED BROKEN CLIP IAW SRM 51-1-20D PG 21. FABRICATED NEW CLIP (AL2024-T3 0.050) IAW SRM 57-2-0 PG 1. CLEANED, TREATED AND APPLIED FUEL TANK COATING MATERIAL IAW SRM 51-1-12 PG 7 TO 12. INSTALLED NEW CLIP ON RT WING NR 4 ALT TANK REF 505B ACCESS DOOR IAW SRM 51-1-20D PG 9. FOR FUEL LEAK CHECK SEE NR 1981. 2L74 4F RT4A25 20050223001822005022300182WP 2005 2 23 DHL2004801543 120040927A53205711283515J FITTING DOUG DC8 DC873F 302199FWP FLOOR SUPPORT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 AFT CARGO COMPT FLOOR SUPPORT FITTING CORRODED, STA 1260.000, L-34R TO L-35R. REMOVED CORROSION FROM FLOOR SUPPORT FITTING IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED FLOOR SUPPORT FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FLOOR SUPPORT FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9, DC8 SRM 53-1-0 PG 1. 2L74 4F RT4A25 20050223001852005022300185WP 2005 2 23 DHL2004801534 120040910A551037014272 FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 EMPENNAGE, LT HORIZONTAL STABILIZER LWR FITTING CRACKED 1.000 AT XFS 60.000. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1. PERFORMED ANTI-CORROSIVE TREATMENT AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON LT HORIZONTAL STABILIZER, XFS 60.000 WITH HI-LOKS IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050223001882005022300188WP 2005 2 23 DHL2004801555 120040929A5753 PLATE DOUG DC8 DC873F 302199FWP TE FLAPS WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT OTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R05 FAA FORM 8110-3 DATED 09-28-04. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.071) INTERNAL SPLICE DOUBLER (2024-T3AL 0.080) IAW DWG W51-R05. CLEANED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN SEGMENT INTERIOR, INTERNAL SPLICE IAW SRM 51-1-8B. APPLIED SEALANT IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT AND INTERNAL SPLICE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, DWG W51-R05. 2L74 4F RT4A25 20050223001902005022300190WP 2005 2 23 DHL2004801548 120040909A5530 ANGLE DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LEFT VERTICAL STABILIZER LWR ATTACH ANGLE CRACKED 4.000, ZR 47.000 (FRONT SPAR PLANE) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2 PG 44A,B,C,D. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. CUT OUT DAMAGED SECTION IAW DC8 SRM 53-2-5 FIG 16A SHEET 1-2. FABRICATED SHIM (AL7075T6 0.125), FILLER (AL7075-T6 0.160) AND ANGLE (STEEL 17.7 PH 0.079) IAW DC8 SRM 53-2-5 PG 44A, B, C, D FIG 16A SHEET 1-2. HEAT TREATED STEEL ANGLE IAW DC8 SRM 51-1-6. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02/07. CLEANED, TREATED AND PRIMED AREA, SHIM AND FILLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED SHIM, FILLER AND ANGLE. 2L74 4F RT4A25 20050223001922005022300192WP 2005 2 23 DHL2004801505 120040831A5730 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LEFT INNER WING OUTBOARD L/E SECTION INTERNAL DOUBLER CRACKED 0.250, STA XW 485.000. REMOVED CRACKED INTERNAL DOUBLER IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW INTERNAL DOUBLER (ALCLAD 7075-T6 0.050) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INTALLED INTERNAL DOUBLER WITH NEW FASTENERS IAW DC8 SRM 57-2-0 PG 1, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050223001942005022300194 2005 2 23 ALGA097672 420040508A83006893672 GEAR SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL RGB SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03707AL1037 760189 CAE890734S FOUND SPALLING ON GEAR TEETH. RETURNED TO VENDOR FOR WARRANTY CREDIT. 1G72 3U3 U H1NE E1GL 20050223001952005022300195WP 2005 2 23 04FDEA02949 120041018A27302594366904 ACTUATOR DOUG DC10 DC1010 3022110WP ELEVATOR MALFUNCTIONED A FDEAJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25369FE 46607 BEFORE TAKEOFF FLIGHT, CONTROL CHECKS WERE NORMAL. ROTATION FELT SLIGHTLY HEAVIER THAN NORMAL. DURING ACCELERATION AND CLEAN UP, ELEVATOR BECAME VERY DIFFICULT TO MOVE. ACTED AS IF AUTOPILOT MIGHT BE ON, BUT NO CB'S POPPED. DUMPED 5000 LBS AND RETURNED TO MEM. PERFORMED ELEVATOR MOVEMENT TEST WITH NO NOTICEABLE STIFFNESS. FOUND FAULT BALLS ON ELF/FL PROGRAMMER FOR FL ACTUATOR FOR NR 2 PROGRAMMER. FOUND FAULT BALLS ON BOTH PITCH COMP FOR COMPUTER, ACTR A, AND ACTR B. PERFORMED BI TE CK ON BOTH CONTROLLERS BOTH PASSED. REMOVED AND REPLACED ELEVATOR LOAD FEEL DUPLEX ACT. IN REFERENCE TO DC-10-10 M/M 27-32-01-2, OPS CHECKED GOOD. 2L73 4F A22WE 20050223001962005022300196NE 2005 2 23 WLDA200494 220041007A7230 COMPRESSOR DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 2 ENGINE STALLED A WRLAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SO11275 48631 P723914 AIR TURNBACK DUE TO NR 2 ENGINE COMPRESSOR STALLED WITH ANTI-ICE ON THROUGH 11000 FEET. TEMPERATURE APPROX 620 DEG. BROUGHT THROTTLE TO IDLE, NR 2 EGT WAS APPROX 70 DEG HOTTER THAN NR 1 AND NR 3, FF 900LBS HIGHER THAN NR 1 AND NR 3. ADVANCED THROTTLE WITH ANTI-ICE OFF AND ENGINE STALLED AGAIN. PERFORMED BORESCOPE INSPECTION IAW MM 72-00-00, FOUND EXTENSIVE DAMAGE TO HIGH PRESSURE COMPRESSOR. REMOVED AND REPLACED NR 2 ENGINE IAW MM PROCEDURES. ENGINE RUN CHECK NORMAL. 2L73 4F4 FRTA22WE E24NE 20050223001972005022300197EU 2005 2 23 DHL2004363525 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK IN MIAMI, FL. AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3880, RBL 78 BETWEEN FS 15 AND FS 19 SEAT TRACKS CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVE SEAT TRACK FROM FS 15 TO FS 19 AT RBL 78 IAW A-300 SRM 51-30-30. FABRICATED NEW SEAT TRACK IAW A-300 SRM 51-10-40. TREAT /PRIMED AND PAINTED IAW A-300 SRM 51-40-10 / 51-40-12. INSTALLED NEW SEAT TRACK FROM FS 15 TO FRAME 19, RBL 78 REF: IAW A-300 SRM 53-10-10 / 51-10-40. MATERIAL USED, 60-22457, PO NR 24302234. 2L72 4F RTA35EU 20050223001992005022300199NM 2005 2 23 04FDEA02895 120041008A5510ALC8107Y2 FITTING DOUG MD11 MD11F 3023600NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25612FE 48605 NR 26 RIGHT HAND BARREL NUT BORE FOUND CRACKED AT BOTTOM INBOARD SIDE AREA. NR 26 RIGHT HAND BARREL NUT BORE SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. 2L73 4F RTA22WE 20050223002012005022300201NM 2005 2 23 04FDEA03398 120041209A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. SPOT FACE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057. 2L73 4F RTA22WE 20050223002022005022300202NM 2005 2 23 04FDEA03361 120041206A5280 STRUCTURE DOUG MD11 MD11 3023602NM RT MLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RIGHT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA. CRACK REPAIRED AS PER SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I. 2L73 4F RTA22WE 20050223002032005022300203WP 2005 2 23 04FDEA03161 120041118A5753 ROLLER DOUG MD10 MD1010F 3022112WP T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT INBOARD FLAP INBOARD FLAP TRACK AREA, LOWER FORWARD LARGE ROLLER CORRODED ON OUTBOARD SIDE. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TRACK LOWER FORWARD LARGE ROLLER IAW FEDEX EA 8-5750-81513. REFERENCE NON-ROUTINE N00604. 2L73 4F RTA22WE 20050223002042005022300204WP 2005 2 23 04FDEA03162 120041118A5753 ROLLER DOUG MD10 MD1010F 3022112WP T/E FLAP WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25377FE 47965 LEFT WING INBOARD FLAP INBOARD FLAP ROLLERS MOST FORWARD UPPER LARGE ROLLER WORN. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TRACK FORWARD UPPER LARGE ROLLER IAW FEDEX EA 8- 5750-81513, WINGS, INBOARD FLAP, INBOARD ROLLER TORQUE REQUIREMENTS, CLARIFICATION. REFERENCE NON-ROUTINE N00603. 2L73 4F RTA22WE 20050223002052005022300205NM 2005 2 23 04FDEA03392 120041207A5730 SKIN DOUG MD11 MD11 3023602NM LT WING BULGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LEFT WING, UPPER SURFACE AT APPROX STA 980 XORS FORWARD OF OUTBOARD AILERON TOP SURFACE FIXED PANEL BULGING. REPAIR CARRIED AT LT WING FORWARD UPPER SURFACE OF OUTBOARD AILERON AT APPROX. STA 980 XORS AS PER SRM 57-20-00 FIG 16 VOL I. 2L73 4F RTA22WE 20050223002072005022300207WP 2005 2 23 04FDEA03395 120041208A5340 ATTACH FITTING DOUG DC10 DC1010F 3022111WP FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568059 46907 FUSELAGE, ATTACH FITTINGS INBD FLAP SUPPORT STRUCTURE FITTING CRACK REPAIR. COMPLIED WITH EA 8-5310-55417. 2L73 4F A22WE 20050223002092005022300209NM 2005 2 23 04FDEA03415 120041214A5312 BULKHEAD DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 FUSELAGE MAIN FRAME BODY STATION 595.00 BULKHEAD REPAIR. REPAIR CARRIED OUT TO COMPLY WITH FEDEX EA 1-5310-77978. 2L73 4F RTA22WE 20050223002112005022300211NM 2005 2 23 04FDEA03152 120041117A5514ALC8104502 FITTING DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25618FE 48754 CORROSION REMOVED ON BARREL NUT BORE NR 21R EXCEEDED LIMITS. REF TO EO 1-5510-7-5000 C4 PT1, BARREL NUT BORE NR 21R. REPAIRED PER FEDEX EA NR 1-5510-79789, STABILIZERS, HORIZONTAL STABILIZERS, BARREL NUT BORE, REWORK/REPAIR, 1-5510-7-5000. 2L73 4F RTA22WE 20050223002122005022300212EU 2005 2 23 04FDEA03417 120041215A2750 CONTROL HANDLE AIRBUS310 A310 EU COCKPIT OBSTRUCTED A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25425FE 264 SLATS WOULD NOT RETRACT AFTER TAKEOFF. SLAT/FLAP HANDLE WOULD ONLY OPERATE BETWEEN 15/0 AND 20/20 POSITIONS. RETURNED TO MEM AND MADE 20/20 LANDING. NO OTHER INDICATIONS OF MALFUNCTION ON SFPI OR FLAPS/SLATS SYS 1/2 INDICATIONS. FOUND DEBRIS IN FLAP HANDLE. REMOVED AND OPERATED. OPS CHECKS AS PER AIRBUS M/M 27-50-00. 2L72 4F RTA35EU 20050223002132005022300213NM 2005 2 23 04FDEA03028 120041108A5311 FRAME BOEING727 72722 1384002NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 AFT CARGO FRAME DENTED AT BS 990 STR 26 LT. REPAIRED PER SRM 51-40-3, 51-10-2 AND 51-30-2. 2L73 4F A3WE 20050223002142005022300214NM 2005 2 23 04FDEA03029 120041108A5311 FRAME BOEING727 72722 1384002NM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 AFT CARGO FRAME DENTED AT BS 1030, STR 26R. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 20050223002512005022300251NM 2005 2 23 UPS05M43893 120041213A5754ARB2850505 RIB DOUG MD11 MD11F 3023600NM L/E SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 NR 16 LEADING EDGE SLAT TRACK INBOARD FITTING FOUND WITH SIGN OF CRACK AS MARKED. HFEC C/O IAW DAC NDT SPM R.11 PART 06-10-01.001 AND CRACK CONFIRM APPROX 1/2 INCH LONG. LT NR 16 L/E SLAT TRACK AND DOOR REMOVED PER 57-40-01 REV 47 CRACKED. RIB REMOVED PER SRM 51-35-01 AND 51-33-01 V.2R.35. NEW RIB HOLES TRANSFER PER SRM 51-31-01V.2R.35 AND DWG ARB2873. NEW RIB INSTALLED PER SRM 51-35-0 1 AND 51-33-01 V.2R.35. LHW NR 16 SLAT TRACK AND DOOR REINSTALLED PER 57-40-01R.45. 2L73 4F RTA22WE 20050223002522005022300252NM 2005 2 23 UPS05M43894 120041211A5754ARB2850506 RIB DOUG MD11 MD11F 3023600NM L/E SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 RT WING NR 16 LEADING EDGE SLAT TRACK SUPPORT BRACKET FOUND WITH SIGN OF CRACK AS MARKED. HFEC C/O IAW DAC SPM R.11 PT.06-10-01.001 AND CRACK CONFIRM APPROX 5/8 INCH LONG. RT NR 16 SEAT TRACK AND DOOR REMOVED PER AMM 57-40-01 R.47. CRACKED RIB REMOVED AS PER SRM 51-35-01 AND 51-33-01 V.2 R.35. NEW RIB HOLES TRANSFERED PER SRM 51-31-01 V.2 R.35 AND DWG ARB2873. NEW RIB INSTALLED PER SRM 51-35-01 AND 51-33-01 V.2 R.36. RT NR 16 SEAT TRACK AND DOOR REINSTALLED PER AMM 57-40-01 R.45. 2L73 4F RTA22WE 20050223002572005022300257NM 2005 2 23 QXEA200500007 120041229A2760KX511 SWITCH DHAV DHC8 DHC8202 2809007NM LT SPOILER FAILED A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09356PH16613 502 PDX - FLIGHT 2186 - THE CHECKLIST WAS COMPLIED WITH WHEN DURING THE CLIMB, THE CREW NOTICED SOME UNUSUAL CONTROL FORCES. THE SPOILER 2 LIGHT ON THE GLARESHIELD ILLUMINATED. THE LIGHT WAS PUSHED AS PER THE CHECKLIST AND THE CAUTION LIGHT FOR THE ROLL SPOILER OUTBOARD HYDRAULICS THEN CAME ON. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE LOWER MICROSWITCH ON THE LEFT SPOILER CLUTCH. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20050223002612005022300261NM 2005 2 23 QXEA200500034 120041215A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN AT STATION 301.0 TO 321.0, BETWEEN STRINGERS 10P AND 11P HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073. 2H72 4T RTA13NM 20050223002642005022300264NM 2005 2 23 QXEA200500021 120041217A5411 FRAME BOMBDRDHC8 DHC8401 1390041NM RT NACELLE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - RIGHT HAND ENGINE FORWARD FRAME, INTAKE COWL ATTACHMENT LUG, OUTBOARD HAS BEEN GOUGED ON THE OUTBOARD FACE. REPAIRED IAW HORIZON AIR EA 6-54-325 AND RD 8/4-54-219. 2H72 4T RTA13NM 20050223002652005022300265NM 2005 2 23 QXEA200500023 120041218A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE EXTERIOR, FUSELAGE SKIN PANELS REQUIRED PERMANENT REPAIRS AT STATION X216 AND STRINGER 29P, X236 BETWEEN STRINGER 29P AND 30P, X361 BETWEEN STRINGER 29P AND 30P. REPAIRED IAW HORIZON AIR EA 6-53-370B, RD 8/4-53-1106 AND RD 8/4-53-1109, ISSUE 1. 2H72 4T RTA13NM 20050223002702005022300270NM 2005 2 23 QXEA200500037 120041215A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN PANEL STATION 281.00 TO 301.00 BETWEEN STRINGER 8P AND 9P HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2H72 4T RTA13NM 20050223002722005022300272NM 2005 2 23 QXEA200500041 120041218A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - PREVIOUS DAMAGE ON FUSELAGE SKIN AT STATION X428 TO 440 BETWEEN STRINGER 31P AND 30P. REPAIRED IAW HORIZON AIR EA 6-53-503, RD 8/4-53-1108, ISSUE 1 AND SRM 51-25-15-370-801. 2H72 4T RTA13NM 20050223002732005022300273NM 2005 2 23 QXEA200500042 120041219A5420 STIFFENER BOMBDRDHC8 DHC8401 1390041NM LT NACELLE BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND NACELLE AFT FAIRING PANEL 414AL INTERNAL STIFFENER IS BROKEN AT ONE END. REPAIRED IAW HORIZON AIR EA 6-54-324 AND RD 8/4-54-218, ISSUE 1. 2H72 4T RTA13NM 20050223002742005022300274NM 2005 2 23 QXEA200500043 120041219A5420 STIFFENER BOMBDRDHC8 DHC8401 1390041NM RT NACELLE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - RIGHT HAND NACELLE AFT FAIRING PANEL 424AL INTERNAL STIFFENER IS WORN ON ONE END. REPAIRED IAW RD 8/4-54-218, ISSUE 1 AND HORIZON AIR EA 6-54-324. 2H72 4T RTA13NM 20050223002792005022300279EA 2005 2 23 QXEA200500046 120041227A5320 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09608QX 10026 PDX - BEAM 280 IS CRACKED AND CORRODED. REPAIRED IAW REO 670-53-11-045. 2L72 4F RTA21EA 20050223002822005022300282NM 2005 2 23 QXEA200500073 120041227A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM FUSELAGE STRIPPED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09349PH 486 PDX - FUSELAGE PANEL HAS FOUR STRIPPED OUT NUTPLATES. REPLACED OLD NUTPLATES WITH NEW NUTPLATES. 2H72 4T RTA13NM 20050223002852005022300285NM 2005 2 23 QXEA200500076 120041204A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PANEL SPINNING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - PANEL 121AR HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS. 2H72 4T RTA13NM 20050223002862005022300286NM 2005 2 23 QXEA200500077 120041221A5720 FLANGE DHAV DHC8 DHC8202 2809007NM WING CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09357PH 504 PDX - PITTING ON THE UPPER SURFACE OF THE LOWER INBOARD FLANGE. COMPLETED BLENDING OF PITTING IN ACCORDANCE WITH EA2-57-151A. 2H72 4T RTA13NM 20050223002872005022300287NM 2005 2 23 QXEA200500078 120041229A5544 STRUCTURE DHAV DHC8 DHC8202 2809007NM RUDDER CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09359PH 514 PDX - TOP OF FORE RUDDER HAS A CRACK NEAR A RIVET. INSTALLED THE REPAIRED PARTS AND SEALED IAW RD 8-55-335. 2H72 4T RTA13NM 20050224000012005022400001CE 2005 2 24 ENHA200420001 120041019A2133 LINE BEECH 200 200BEECH 1152920CE OUTFLOW VALVE SPLIT E ENHAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL0390PB BB125 ON TAKEOFF, PILOT UNABLE TO CONTROL CABIN PRESSURIZATION, RETURN TO AIRPORT OF DEPARTURE. FOUND SPLIT PRESSURIZATION LINE AT OUTFLOW VALVE, REPAIRED IAW BEECH 200 MM20-06-00 PG 201. AIRCRAFT TEST FLOWN. PRESSURIZATION SYSTEM FUNCTION NORMAL. 1L72 4T A24CE 20050224000022005022400002WP 2005 2 24 NACA20040049 120041002A5313 STRINGER DOUG DC6 DC6 3021702WP FUSELAGE CORRODED A NACAK NONE O OTHER ININSP/MAINT 1 AL03779TA 45529 RIGHT FUSELAGE HAS SURFACE CORROSION AT STA 926 STRINGER 25. CUT OUT CORROSION. DAMAGE CUTOUT 3/4 INCH. FABRICATED AND INSTALLED DOUBLER. .040 7075-T6, DIMPLED ORIGINAL HOLES REF DOUGLAS OHM 12-36 FIG 12-22. 2L74 4R A781 20050224000032005022400003 2005 2 24 HNAA0400128 420041025A3417 ADIRU DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07810EX 308 FLIGHT NR 3933 REPORTED HAVING A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT SHORTLY AFTER CAPTAIN'S ADI FAILED. MAINTENANCE COULD NOT DUPLICATE. ADI OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050224000042005022400004NM 2005 2 24 WLDA200495 120041009A5310 STRUCTURE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE TAIL DAMAGED A WRLAO OTHER O OTHER TOTAKEOFF 1 SO11275 48631 IMMEDIATELY UPON BRAKE RELEASE DURING TAKEOFF, NOSE RAPIDLY BEGAN TO RISE, RESULTING IN TAIL STRIKE. REPAIRED THE DAMAGE PER DELTA ERA 094364-14 AND 094561-14. PERFORMED AIRCRAFT WEIGHT, ALL CHECKED NORMAL. 2L73 4F4 FRTA22WE E24NE 20050224000062005022400006EU 2005 2 24 BAQA097863 120041027A2435 BRUSHES AGUSTAA109 A109E 0260119EU STARTER GEN WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109UP 11061 BRUSHESWORNOUT ON STARTER GENERATOR 1G72 3U RTH7EU 20050224000262005022400026CE 2005 2 24 Z4TA200400002 120041202A2823HE1431590 CONTROL CABLE BEECH 58 58 1152740CE FUEL SELECTOR BROKEN D Z4TAK NONE O OTHER ININSP/MAINT 1 SO0595KM 3904 20 TH1315 FOUND LEFT FUEL SELECTOR CABLE FROZEN. REPLACED WITH NEW HOUSING AND CABLE CORE. OPS CK OK. 1L72 3O 3A16 20050224000392005022400039WP 2005 2 24 WX0400069 120041231A56105912290505 WINDSHIELD DOUG DC9 DC983 3022083WP COCKPIT CRACKED A WX0AA UNSCHED LANDING O OTHER CLCLIMB 1 WP19862GA 49556 LAS - AIR TURN BACK DUE TO CAPTAIN’S WINDSHIELD CRACKED ON CLIMB-OUT PASSING 9000 FEET. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN’S WINDSHIELD AND INSTALLED ANTI-ICE/ANTI-FOG TERMINAL BLOCKS IAW AMM 56-10-02. AIRCRAFT RETURNED TO SERVICE . 2L72 4F RTA6WE 20050222001932005022200193EU 2005 2 22 ERAA096629 120040525A63213701020000 OIL COOLER BOLKMS105 BO105S 5626006EU ENGINE LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03129EH 580 LEAK AT TOP OF NR 2 COOLING AREA. SENT TO DRAKE AIR FOR REPAIR. CLEANED, FLUSHED, REPAIRED/OVERHAULED, TESTED AND INSPECTED. 1G72 3U H3EU 20050222002002005022200200GL 2005 2 22 ERAA096641 220040714A7323 SHIM BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL GOVERNOR MISSING B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH7603 86220670 598 GOVERNOR HAS ONLY 178.4 HOURS SINCE OVERHAUL AT ACRO. SHIMS ARE MISSING ON DRIVESHAFT. RETURNING ON ERA REPAIR ORDER RW-899866 REQUESTING WARRANTY REPAIR. 1G72 3U3 U H3EU E4CE 20050222002022005022200202WP 2005 2 22 IXXA0400102O 120040807A7932 ENGINE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D3 52039NE NR 4 FAILED A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW1171CX 6824 1117 45961 671365 DURING CRUISE FROM KSUU TO PHIK, NR 4 ENGINE LOSS OF ALL OIL QUANTITY AND OIL PRESSURE OF 12PSI. ENGINE NR 4 OIL LIGHT CAME ON. CREW SHUT DOWN NR 4 ENGINE AND AFTER SHUT DOWN NR 4 ENGINE WINDMILLING OIL PRESSURE AT 5PSI. AIRCRAFT ARRIVED IN PHIK AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING AND INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. MAINTENANCE FOUND EVIDENCE OF OIL IN GAS PATH. MAINTENANCE REMOVED NR 4 ENGINE AND INSTALLED REPLACEMENT. OPERATIONAL CHECK GOOD ON GROUND AND ENGINE RUN GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20050222002102005022200210EU 2005 2 22 XNOA1196 120040826A2450 CIRCUIT BREAKER AIRBUS300 A300B4203 3930306EU NR 2 DUAL SHUTOFTRIPPED A XN0AO OTHER O OTHER NRNOT REPORTED 1 GL23224KW 073 NR 2 ENG NO LIGHT OFF. RESET CIRCUIT BREAKERS ON NR 2 DUEL SHUT OFF CIRCUIT, OPS CHECKED FUEL SHUT OFF SYSTEM. PERFORMED ENGINE OPS RUN, OPS CHECKED GOOD PER 28-10-00 AND 71-00-00. 2L72 4F RTA35EU 20050222002142005022200214CE 2005 2 22 GLBA20030708 120040830A5320 BRACKET BEECH 1900 1900D 1154162CE FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03192GL UE192 LEFT FUSELAGE TO VERT STAB L BRACKET PATCH CRACKED AT CANTED BULKHEAD. REMOVED AND REPLACED LEFT FUSELAGE TO VERT STAB L BRACKET AT CANTED BULKHEAD REF EO 04-VE192-02. 2L72 4T RTA24CE 20050222002162005022200216CE 2005 2 22 60196050804 120040508A2740MS3456L2027S CONNECTOR LEAR LEAR 60 60LEAR 5170707CE ACTUATOR DAMAGED E J7SAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW05252FX 60196 PRIMARY PITCH TRIM INOPERATIVE DURING FLIGHT. AIRCRAFT DIVERTED TO MAINTENANCE BASE AT TEB. REPLACED CONNECTOR ON STAB ACT. 2 SPEED CONTROL BOX. OPS CHECK NORMAL. 2L72 4F RTA10CE 20050222002252005022200225NE 2005 2 22 ERAA097092 120040506A741037D400347P101 EXCITER SKRSKYS61 S61N 8142104NE IGNITION SYS SHORTED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03563EH26740 61808 EXCITER IGNITION REMOVED FOR POPPING NR 1 STARTER CIRCUIT BREAKER ON START. CLEANED HOUSING AND COVER, REPLACED BUSH HANGER ASSY UNIT, TESTED, UNIT TESTED SERVICEABLE. 2G72 4U 1H15 20050222002272005022200227NM 2005 2 22 EIA2004090 120040526A5330 SKIN BOEING747 747273C 1384896NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09470EV 20653 STR 43L FUS STA 1900, EXISTING REPAIR CORRODED, SKIN OUTBD AND FWD OF REPAIR CORRODED AND BULGING. REPAIRED CORRODED AND BULGING SKIN. REMOVED AND REPLACED CORRODED DOUBLER, PER B747 SRM 53-30-03, FIG 36, PAGES 99-100B, AT FS 1820 STR 48L. 2L74 4F A20WE 20050222002282005022200228NM 2005 2 22 EIA2004114 120040922A5320 TIE BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 CRACK FOUND IN TENSION TIE TO FRAME JOINTS AT LOCATION B880 FRAME, LT SIDE, S-9L. FRAME HOLE OVERSIZED TO REMOVE CRACKS AND FREEZE PLUGS INSTALLED. REPAIR DOUBLER INSTALLED INCORPORATING EXISTING PRODUCTION DOUBLER PER EN 53-084 BOEING MESSAGE NR 1-OUMRW, 1-OOHR4, AND 1-P8ZM7 WITH FAA 8110-3. 2L74 4F RTA20WE 20050222002332005022200233SW 2005 2 22 ERAA097094 120040722A6420212011701121 ROTOR HEAD BELL 412 412 1182202SW TAIL ROTOR OUT OF BALANCE E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH3203 33004 UNABLE TO BALANCE HIGH FREQ, TRUNNION HAS PLAY. PITCH HORN BUSHINGS MISSING, NO PLAY IN YOKE BRHS, TRUNNION FEELS GOOD, NO DETECTABLE PLAY. TRUNNION SPLINES ARE WEAR STEPPED. SCRAPPED TRUNNION. DISASSEMBLED T/R ASSY, REPAIRED T/R BLADE A-10206, INSTALLED NEW TRUNNION ASSY, THRUST PLUGS, TRUNNION BEARINGS AND SEALS. REASSEMBLED T/R HUB, COMPLIED WITH TB-412-95-134. REASSEMBLED T/R ASSY AND MARVEL BALANCED, TORQUED AND SAFTIED IAW 412 CR&O, COMPLIED WITH TB 412-95-134. 1G72 4U H4SW 20050222002372005022200237NM 2005 2 22 EIA2004119 120040930A5230 SKIN BOEING747 747SR46 1384816NM CARGO DOOR CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 BULGE FROM CORROSION ON SKIN AT AFT LWR CORNER OF AFT CARGO DOOR. TRIM OUT CORROSION PER SRM 51-10-01. HFEC INSPECTED. REINFORCE ENTIRE DAMAGED AREA WITH TWO OUTER DOUBLERS PER EN EA 52-0048. BOEING MESSAGE, 1-P48WC, 1-PBPA2, AND 1-P1QFU. TIME LIMITED REPAIR MONITORED PER ECRA 477-51-098-1. 2L74 4F RTA20WE 20050222002392005022200239SW 2005 2 22 ERAA097098 120040730A3246412050015109 SKID BELL 412 412 1182202SW MLG CORRODED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH 33004 SKID TUBE CORRODED AND AFT SADDLE CRACKED. FORWARD, MIDDLE AND AFT FLOAT COVERS AND END CAPS WORN AND TORN SKID TUBE CORRODED BEYOND LIMITS. AFT FLOAT BAG (SN 0372) HAS AN EXCESSIVE NUMBER OF HOLES. MIDDLE FLOAT BAG (SN 0628) HAS ONE HOLE. PASSENGER STEP ASSY HAS 2 BOLTS SEIZED IN BUSHINGS DUE TO CORROSION. 6 YEAR LIFE ON SERIALIZED HOSES NEEDS TO BE VERIFIED (SEE HOW MUCH TIME IS LEFT UNTIL RETIREMENT). ALL RUBBER BANDS ON COVERS NEED REPLACEMENT. PERFORMED FLOAT INSPECTION AS PER ERA CAMP INSPECTION FORM AND BHT 412-SI-2. REMOVED AND REPLACED AFT FLOAT BAG AND REPAIRED MIDDLE FLOAT BAG. REMOVED AND REPLACED ALL RUBBER BANDS AND FLOAT COVERS. 1G72 4U H4SW 20050222002532005022200253EU 2005 2 22 ERAA097108 120040723A63204638001007 TRANSMISSION BOLKMS105 BO105S 5626006EU MAIN ROTOR LEAKING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03292EH14435 562 LEFT INPUT SEAL LEAKS. REMOVED SMALL OIL SEAL AND LEFT PINION ASSY. DISASSEMBLED PINION ASSY, INSTALLED NEW SEAL AND SERVICEABLE FW SHAFT. REASSEMBLED AND REINSTALLED PINION AND OIL JET WITH NEW O-RINGS AND ORIGINAL HARDWARE. ALL WORK DONE IAW 105 REM 103 TT 14435.3, TSO 1991.6. 1G72 3U H3EU 20050222002852005022200285WP 2005 2 22 DHL2004801500 120040823A3213 TORQUE LINK DOUG DC8 DC873F 302199FWP RT MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 PERFORM NDT OF RT MLG UPPER TORQUE LINK AND ATTACH BOLT. PERFORMED MAGNETIC PARTICLES METHOD NDT OF RT MLG UPPER TORQUE LINK AND ATTACH BOLT IAW DC8 NDT SPM PART 07-00-01/08. REFER TO NR 1481 FOR DISCREPANCY FOUND CRACK IN RT TORQUE LINK ATTACH BOLT THREAD, ENCLOSED SMN-FORM 242-5. 2L74 4F RT4A25 20050222003092005022200309WP 2005 2 22 04FDEA02877 120041005A5230NDA6066543 SKIN DOUG MD10 MD1010F 3022112WP CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 FORWARD PIT DOOR, LOWER AFT CORNER OF DOOR IS DENTED AND GOUGED. ACCOMPLISHED EA 8-5230-81484, TO FORWARD CARGO DOOR SKIN BLEND OUT ON LOWER AFT CORNER. REFERENCE NON-ROUTINE NR N00253 2L73 4F RTA22WE 20050223000132005022300013NM 2005 2 23 04FDEA02514 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, XORS= 540 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 540 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000192005022300019NM 2005 2 23 04FDEA02647 120040904A5730ARC05841 PANEL DOUG DC10 DC10 N/A-SDRNM ZONE 500 DEBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25058FE 46705 FINGER DOUBLERS DISBONDED INSIDE LEFT WING TRAILING EDGE FAIRING BETWEEN XW 373 AND XORS 486, ACCESS THROUGH 641 MB. REMOVED ARC0584-1 SKIN FOR REPLACEMENT IAW DC10 SRM 51-35-01, 51-33-01 VOL II. FABRICATED NEW ARC0584-1 SKIN ASSEMBLY IAW DAC DWG 0584. INSTALLED NEW ARC0584 IAW DC10 SRM 51-33-24, 51-35-01 AND 51-38-01 VOL II AND EA 8-5710-77629. REMOVED PANEL P/N ARC0810-503 AND ARC0810-184 FOR ACCESS. REINSTALLED BOTH PANELS IAW DC10 SRM 51-31-01 VOL II. REFERENCE N/R N00544. 2L73 4F RTA22WE 20050223000232005022300023NM 2005 2 23 04FDEA02658 120040904A2613 DETECTOR DOUG MD11 MD11F 3023600NM NR 2 ENGINE BURST A FDEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO25621FE 48792 ON T/O, PRIOR TO FLAP RET, A/C DISPLAYED A MOMENTARY LVL 3 ENG 2 A-ICE DUCT ALERT. AS THROTTLE WAS BEING MOVED TO IDLE ALERT WENT AWAY. CLIMB TO FL 290 WAS UNEVENTFUL UNTIL 30 MIN INTO FLT WHEN A/C DISP LVL-1 ENG 2 A-ICE OFF ALERT, WITH A CONS OF ENG 2 A-ICE DUCT HAS FAILED. ENG SHUT DOWN IN FLT (QRH) WAS PERF AND APPROX 50K FUEL WAS DUMPED. INSPECTED ANTI-ICE DUCT FROM NR 2 ENG FIREWALL AFT R/R`D SENSING ELEMENTS D89, D90, D91 IAW MD-11 MM 30-22-11-4. REPLACED BURST DETECTION UNIT PER MD11 MM 30-22-10-4. PERF MAX POWER ASSURANCE ON NR 2 ENG AND RAN FOR APPROX 5 MIN WITH NO FAULTS OR ALERTS. NR 2 NOSE COWL ANTI-ICE OPS CHECK NORMAL PER JRH 4-28. A/C OK FOR SVC. 2L73 4F RTA22WE 20050223000242005022300024EU 2005 2 23 04FDEA02662 120040907A5347 SEAT TRACK AIRBUS310 A310203 3930313EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 MAIN CABIN SEAT TRACK 4R AT STA 1315 (FR 17) HAS 1 EA FASTENER HOLE WITH CORROSION. REPAIRED IAW EA 6-5310-81944. 2L72 4F RTA35EU 20050223000252005022300025EU 2005 2 23 04FDEA02663 120040907A5315 FLOORBEAM AIRBUS310 A310203 3930313EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25414FE 400 FOUND UPPER DECK FLOORBEAM CRACKED .020 INCH LONG ON THE FWD FACE AFT OF FS 36, 8 INCHES OTBD FROM 1L SEAT TRACK. REMOVED DAMAGE IAW A310/200 SRM SUPP. 53-10-15 FIG 201, NDT AREA, IAW NTM 51-10-08, CRACKED REMOVED, REPAIRED AREA IAW A310/200 SRM SUPP 53-10-15 FIG 201. 2L72 4F RTA35EU 20050223000292005022300029NM 2005 2 23 04FDEA02517 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT XORS= 633 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 633 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000302005022300030NM 2005 2 23 04FDEA02518 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000312005022300031NM 2005 2 23 04FDEA02519 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 720 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 720 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000362005022300036NM 2005 2 23 04FDEA02524 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 CORROSION REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000492005022300049 2005 2 23 P9RA20040042 420040924A2565D30665122 SLIDE BOEING757 757231 1384950NM R1 DOOR DEPLOYED A P9RAO OTHER W INADEQUATE Q C TXTAXI/GRND HDL 1 SO11715TW 28483 AT GATE IN TOL, R1 DOOR SLIDE DEPLOYED BY GROUND SERVICE PERSONNEL INADVERTENTLY. REMOVED AND REPLACED R1 SLIDE PER MM. 2L72 4F RTA2NM 20050223000842005022300084 2005 2 23 ERAA097498 420040916A2562 G SWITCH BELL 412 412 1182202SW ELT INTERMITTENT B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03412EH 58646 33001 G SWITCH IS TOO SENSITIVE AND IT WORKS INTERMITTENTLY SUB ASSEMBLY AND TOP COVER CRACKED/BROKEN. REPLACED SUB ASSEMBLY AND TOP COVE, G SWITCH. REPLACED AS PART OF SUBASSEMBLY. 1G72 4U H4SW 20050223000852005022300085 2005 2 23 ERAA097499 420040831A2562 FWC SKRSKYS61 S61N 8142104NE ELT FAULTY E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03562EH 42015 61257 FAULTY G SWITCH. SWITCH BECAME OPERABLE AFTER GENTLY TAPPING THE REAR END OF UNIT, BUT UNIT WAS SENT OUT FOR REPAIR AS PER MANUFACTURER'S RECOMMENDATION. 2G72 4U 1H15 20050223001002005022300100SW 2005 2 23 ERAA097514 120040824A6520209062501005 OIL COOLER BELL 412 412 1182202SW T/R GEARBOX DAMAGED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03421EH 33067 OIL COOLER CORE LEAKING EXCESSIVE OIL. UNIT EXHIBITED EXCESSIVE CORE DAMAGE, DIRTY CORE, DAMAGED FINE, EXCESSIVE CARBON AND DIRT AND WORN SEALS. A MATRIX CORE WAS INSTALLED, CLEANED, FLUSHED, OVERHAULED, WORN SEALS REPLACED, TESTED AND INSPECTED IAW DAR-8500. 1G72 4U H4SW 20050223001202005022300120GL 2005 2 23 ERAA097537 220040805A72306890550 COMPRESSOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE FAILED E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03426EH5528 552 COMPRESSOR BLADE AND VANE FAILED 2-3 STAGE COMP BLADES CAME OFF, HEAVY DAMAGE ON 1, 2, AND 3 STAGE VANES. CHANGED MODULE ON ENGINE ASSY. 1G72 3U3 U H3EU E4CE 20050223001232005022300123EA 2005 2 23 HNAA0400099 120040930A36101612481 LINE DHAV DHC8 DHC8311 1386006EA BLEED SYSTEM LEAKING A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA07328EN 281 BURNING SMELL IN CABIN AREA, STRONGER AT ROW 12 AND 13 WITH NO BLEEDS SELECTED. FOUND BLEED, ROW 6, REPLACED LINE. 2H72 4T RTA13NM 20050223001682005022300168NM 2005 2 23 04FDEA02659 120040907A5311AFA00203 FRAME DOUG MD11 MD11F 3023600NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 MAIN DECK, LT SIDEWALL STRUCTURE FRAME'S INNER CHORD DENT AT STA 1701, L-12L. FRAME AT STA 1701 L-12L DAMAGED DOUBLER REMOVED AND REPLACED AS PER SRM 53-00-00 VOL I FIG 1. 2L73 4F RTA22WE 20050223001722005022300172WP 2005 2 23 04FDEA02908 120041011A5753ARC01541 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 LEFT WING INBOARD FLAP OUTBOARD HINGE AT LOCATION NR 1 INBOARD AND OUTBOARD LUGS HAVE CORROSION. REMOVED CORROSION FROM LOCATION NR 1 MOUNTING SURFACE IAW DACCMM 57-44-07 AND FEDEX EA8-5750- 81473. PRIMED LUGS IAW DC10 SRM 57-21-01 VOLUME I, BEGINNING BORE 1.255 INCH REMOVED .0200 INCH FINAL 1.2360 INCH FOUND TO BE WITHIN LIMITS IAW DACCMM 57-44-07. 2L73 4F RTA22WE 20050223001742005022300174CE 2005 2 23 DJFA2004023 120041007A3213 STRUT BEECH MU300 400A 1155402CE MLG OVERSERVICED E DJFAO OTHER WG INADEQUATE Q C MULTIPLE FAILURE LDLANDING 1 EA23476LX RK376 CREW REPORTED THAT DURING LANDING ROLL, THRUST REVERSERS WOULD NOT DEPLOY, SPEED BRAKES WOULD NOT EXTEND AND ANTI-SKID WAS INTERMITTENT. WHEN BRAKES FINALLY ENGAGED RIGHT TIRE GRABBED FIRST AND CAUSED FLAT SPOT. MAINTENANCE FOUND SHOCK STRUTS TO BE TOO HIGH. LEFT AND RIGHT STRUTS WERE SERVICED TO PRESSURE AS PLACARDED ON STRUTS, LEFT AND RIGHT MAIN GEAR WHEEL ASSEMBLIES WERE REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050223001772005022300177WP 2005 2 23 IXXA0400112O 120041008A7331 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FAILED A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW11823BX86803775 46064 692325 ON CLIMB-OUT AT 30,000 CLIMB POWER SETTING, NR 4 ENGINE FUEL FLOW STATED FLUX AND ENGINE LOST POWER. ROLLED BACK TO FLIGHT IDLE AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. OTHER ENGINE INDICATIONS WERE NORMAL ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ON GOING AND AS SOON AS MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MX FOUND N1 AND N2 ROTORS LOCKED TO EACH OTHER. DEFFERED NR 4 ENGINE, COMPLIED WITH CFM MM 71-00-00 SECURED NI AND N2 ROTOR FOR A NO WINDMILL FERRY. AIRCRAFT WAS FERRIED FROM KIAH TO KTOL WERE MAINTENANCE REMOVED AND REPLACED THE NR 4 ENGINE. ENGINE WAS RUN PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 FRT4A25 E2GL 20050223001842005022300184WP 2005 2 23 DHL2004801533 120040910A5510SE085500094 FITTING DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 EMPENNAGE, RT HORIZONTAL STABILIZER LWR FITTING CRACKED 1.000, XFS 60.000. REMOVED CRACKED LWR FITTING IAW SRM 51-1-21 PG 1. PERFORMED ANTI-CORROSIVE TREATMENT AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ON RT HORIZONTAL STABILIZER, XFS 60.000 IAW SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050223002062005022300206NM 2005 2 23 04FDEA03394 120041208A5313BAC1489147 STRINGER BOEING727 727277 138408SNM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE42487 21394 DURING "B" CHECK VISIT, LOWER AFT FUSELAGE FWD OF STATION 1183 HAS HI LOCK AND RIVETS MISSING. FURTHER INVESTIGATION REVEALED STRINGER 28R, STA 1166 HAD EXFOLIATION CORROSION OUT OF SRM LIMITS. SPLICED IN NEW SECTION OF STRINGER PER B727 SRM 53-10-3, FIG 1, SHEET 4, DETAIL 1. 2L73 4F RTA3WE 20050223002172005022300217EU 2005 2 23 04FDEA03418 120041215A3260BDM3003 PROXIMITY SENSOR AIRBUS310 A310 EU MLG MALFUNCTIONED A FDEAH DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE CLCLIMB 1 SO25435FE 369 NR 1 AUTOPILOT, FLIGHT DIRECTOR AND PITCH TRIM INOP. REMOVED AND REPLACED FCC NR 1 IAW A310 MM 22-18-34-4. AFS LAND TEST WILL NOT PASS, FAILS TEST AT DIFFERENT PHASES. AUTO PILOTS ENGAGE INTERMEDIATELY. AUTO THROTTLE WOULD DISENGAGE AT RANDOM. PITCH TRIM AND YAW DAMP ALSO ENGAGE INTERMEDIATELY. AUTOPILOT TRANSFERRED TO WRI 22-10-0479. PITCH TRIM TRANSFERRED TO WRI 22-23-0477. FLT DIRECTOR TRANSFERRED TO WRI 34-62-0475. REMOVED AND REPLACED PROX DETECTION SYSTEM MM 32-31-71-4. 2L72 4F RTA35EU 20050223002602005022300260NM 2005 2 23 QXEA200500033 120041215A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN PANEL, STATION 281 TO STATION 301.0 BETWEEN STRINGERS 10P AND 11P HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2H72 4T RTA13NM 20050223002772005022300277NM 2005 2 23 QXEA200500040 120041217A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE NICKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE SKIN PANEL HAS TWO NICKS AT STATION 58 BETWEEN STRINGER 32P AND 32S. REPAIRED IAW HORIZON AIR EA 6-53-501 AND RD 8/4-53-1120, ISSUE 1. 2H72 4T RTA13NM 20050223002782005022300278NM 2005 2 23 QXEA200500045 120041215A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE INT AFT, LEFT HAND OUTBOARD SEAT RAIL HAS CORROSION ON UPPER SURFACE AT STATION 664. REPAIRED IAW RD 8/4-53-1112, ISSUE 1 AND HORIZON AIR EA 6-53-497. 2H72 4T RTA13NM 20050223002892005022300289NM 2005 2 23 QXEA200500080 120041220A5751 HINGE DHAV DHC8 DHC8202 2809007NM RT AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - RIGHT AILERON INBOARD HINGE CHAFED. PRIMED AND BLENDED AREA IAW EA 2-57-298. 2H72 4T RTA13NM 20050224000082005022400008WP 2005 2 24 IXXA0400116O 120041029A32204647409 LINK ASSY DOUG DC8 DC871F 302199DWP NLG BINDING A IXXAA UNSCHED LANDING O OTHER CLCLIMB 1 SW11830BX76567648 45973 WHEN THE GEAR UPLATCH CHECK WAS ACCOMP WITH THE HANDLE IN THE UPLATCH CHECK POSITION. AT THE SAME TIME THE NOSE GEAR SEEMED TO FALL HARD ONTO THE NOSE DOORS CAUSING INCREASED NOISE. THE GEAR WAS CYCLED DOWN AND UP. THE UPLATCH CHECK REPEATED AND THE NOISE FROM THE NOSE GEAR WAS LOUDER AND THE "GEAR UNSAFE" LIGHT CAME BACK ON. NO LIGHTS ARE ON WITH THE GEAR HANDLE UP. AN INVESTIGATION IS ON GOING. WHEN MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MX FOUND RIGHT UPPER UPATCH LINK BINDING. REMOVED AND REPLACED LINK ASSEMBLY AND THE OPS CHECK WAS GOOD PER ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20050224000232005022400023CE 2005 2 24 111904N336CS1 120041119A3230 PIN CESSNA500 550 2076604CE CONNECTOR BACKED OUT E Z5FAO OTHER J WARNING INDICATION APAPPROACH 1 NE03336C 5501095 UNSAFE GEAR INDICATION ON APPROACH, GEAR WAS MANUALLY LOCKED DOWN USING EMERGENCY BLOWDOWN BOTTLE. RESET PUSHED BACK PIN AND ALL FUNCTIONAL CHECKS GOOD 1L72 4F A22CE 20050224000582005022400058EA 2005 2 24 04365651 120041230A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A VTZAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA27651BR 7426 FLAPS FAIL AT ZERO. RETRIEVED FAULT CODES 1 JAM 2. PDU DIFF 3 UNSPECIFIED, CLEARED FAULTS OPS CHECKS GOOD AT THIS TIME REF 27-51-00. 2L72 4F RTA21EA 20050224000982005022400098NM 2005 2 24 UIEA200400196 120041115A575465B392502 SPAR BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE KRUEGER FLAP CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 D-CHECK, DURING SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE FOUND AT ENDS OF THE NR 15 KRUEGER FLAP FRONT SPAR. TRIMMED OUT CRACKED REGION OF SPAR ATTACHED FLANGES. NDT INSPECTED TRIMMED EDGES TO ENSURE CRACK AND DEFECT FREE CONDITION. INSTALLED REPAIR FILLERS AND REPAIR CHANNELS. REFINISHED SPARS TO DESIGN STANDARD. DETAIL VISUALLY INSPECTION TO BE ACCOMPLISHED OF THE REPAIR AREA AT C-CHECK INTERVALS, NOT TO EXCEED 18 MONTHS, FOR SIGNS OF DEGRADATION INCLUDING CRACKS, CORROSION AND LOOSE FASTENERS. TO ISSUE EO TO ACCOMPLISH INSPECTION AT C-CHECK OR 18 MONTHS, WHICHEVER COMES FIRST. 2L74 4F4 F A20WE E23EA 20050224001012005022400101NM 2005 2 24 2004UALA01122 120041113A5320 STRUCTURE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO PIT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29924UA 26645 FWD CARGO PIT HAS DAMAGE JUST AFT OF EXISTING REPAIR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR TO INCLUDE NEW REPAIR. REMOVED DAMAGE AS NEEDED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050224001082005022400108NM 2005 2 24 2004UALA01009 120041030A5320 ANGLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29653UA 25391 IN E/E COMPARTMENT, CRACK ON UPPER ANGLE OF STATION 246 FLOORBEAM, LBL 10, AFT SIDE. SUBJECT OF OEM SERVICE BULLETIN AND INCORPORATED INTO ROUTINE INSPECTION PROGRAM. 2L72 4F4 FRTA1NM E24NE 20050224001132005022400113EA 2005 2 24 REXA04030 120041109A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING MALFUNCTIONED A REXAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO258674A 7674 FLAPS FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (NE02200500600) 2L72 4F4 FRTA21EA E15NE 20050224001142005022400114EA 2005 2 24 REXA04029 120041108A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING MALFUNCTIONED A REXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO258673D 7673 RECEIVED (FLAPS HALF-SPEED) MESSAGE ON BLOCK OUT. FLAP SYSTEM INSPECTED FECU CHECKED FOR CODES, NO CODES FOUND. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20050224001222005022400122EU 2005 2 24 RAIA00412042 120041230A3060D45081B TIMER JETAIRJETSTMJETSTM4101 1500501EU PROP DEICE SYS MALFUNCTIONED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03556HK7931 41073 5534 - STL - RIGHT PROP HEAT STAYS ON IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED NR 2 PROP DE-ICE TIMER. 2L72 4T RTA41NM 20050224001232005022400123SO 2005 2 24 RAIA00412037 120041230A2913PV303211 PUMP EMB 145 EMB145 3260210SO NR 1 ENGINE FAILED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03801HK13360 145053 3510- RIC- NR 1 ENGINE HYD PUMP FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 HYD PUMP. 2L72 4F RTT00011AT 20050224001252005022400125SO 2005 2 24 RAIA00412038 120041229A3610AS568226 SEAL EMB 145 EMB145LR 3260212SO BLEED AIR SYS LEAKING A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03816HK 145055 5673- STL- NR 2 BLEED LEAK INDICATION IN FLIGHT. MAINTENANCE REMOVED AND REPLACED BLEED SEALS. 2L72 4T RTT00011AT 20050224001262005022400126SO 2005 2 24 RAIA00412039 120041229A361033020 CLAMP EMB 145 EMB145 3260210SO BLEED AIR SYS LEAKING A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03801HK 145053 3517- BDL- NR 1 AND NR 2 BLEED LEAK, SMOKE IN COCKPIT. MAINTENANCE REMOVED AND REPLACED GAMMA DUCT CLAMP AND SEALS AT BLEED NR 1 PNEUMATIC LINE. 2L72 4F RTT00011AT 20050224001372005022400137NM 2005 2 24 QXEA200500083 120041213A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09412QX 4059 PDX - FUSELAGE DENT ON LEFT HAND SIDE. INSPECTED DENT FOR CRACKS. NO CRACKS NOTED. REF EA 6-53-492. 2H72 4T RTA13NM 20050224001382005022400138NM 2005 2 24 750WL0010 120041101A3350 CONTACTOR BOEING757 757200 1384950NM EXTERIOR DIRTY A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05750WL 23928 R1 EXTERIOR, L2 EXTERIOR, AND INTERIOR EMERGENCY LIGHTS INOP. CLEANED LAMP CONTACTS AT R1 EXTERIOR LIGHT AND RELAMPED L2 EXTERIOR AND INTERIOR LIGHTS. ALL OPS CHECK GOOD PER MM 33-51-06. 2L72 4F RTA2NM 20050224001392005022400139NM 2005 2 24 PCS2004F00001 120040924A2740 STABILIZER BOEING727 727225 1384077NM TAIL OUT OF ADJUST A PCSAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO17604AJ 21453 CREW REPORTED, THROUGH FL 270 AIRCRAFT STARTED PORPOISING, TURNED AUTOPILOT OFF, PORPOISE CONTINUED SLOWED TO .76 MACH, THEN DISAPPEARED. AIRCRAFT DIVERTED BACK AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED HORIZONTAL STABILIZER ADJUSTMENT/TEST AND TRIM CONTROL SYSTEM IAW MM 27-40-0 AND VISUAL INSPECTION OF THE HORIZONTAL STABILIZER JACKSCREW FOR FREE PLAY CHECK OK, IN CONDITION AND SECURITY. PERFORMED A VERTICAL STABILIZER HINGE BEARING AND JACKSCREW FOR FREE PLAY CHECK OK, IAW WORK CARD 4618 IAW MM 55-30-81. TEST FLIGHT FLOWN AND DISCREPANCY DID NOT REPEAT. (SO19200506574) 2L73 4F A3WE 20050224001512005022400151NM 2005 2 24 P5CA0501301 120041231A2121 COOLING FAN BOEING747 74746NF 13848BTNM CARGO BAY FAULTY A P5CAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15453PA 30811 AFTER BLOCK IN ON THE GROUND IN HKG, STRONG SMELL OF TOXIC FUMES WERE PRESENT IN THE COCKPIT AND UPPER DECK. THE FUMES HAD THE SMELL OF ELECTRIC WIRING OVERHEAT OR BURNING AND CAUSED EYE AND SINUS IRRITATION. THE FUMES PERSISTED AFTER VENTILATION. FOUND LEFT SIDE WALL FWD CARGO COMPT STA 550 DRIVEBAY NR 1 E/E COOLING FAN EMITTING AN ODOR. LOCKED OUT FAN AND DEFERRED PER 21-58-6. 2L74 4F RTA20WE 20050224001612005022400161SO 2005 2 24 SWIA200414580 120041201A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 INTERCOSTAL IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050224001622005022400162SO 2005 2 24 SWIA200414581 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 RIGHT OUTBOARD COCKPIT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050224001712005022400171EA 2005 2 24 MASA2004663 120041129A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA EXTERIOR INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW0775999 7471 ASH 7104 BNA, PILOT REPORTED THE AFT EXTERIOR EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING A SYSTEM TEST. THE LIGHT WAS PLAC EXIT LIGHTED OF MEL 33-51-02. 11/29 REPLACED LT EMERGENCY LIGHT. 2L72 4F RTA21EA 20050224001772005022400177EA 2005 2 24 MASA200400685 120041208A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAK NONE L NO TEST NRNOT REPORTED 1 SW0727318 7318 ASH 6156 PHX. CABIN CEILING EMERGENCY LIGHT ABOVE ROW 11 IS INOPERATIVE. MAINTENANCE RELAMPED THE CELING LIGHT. 2L72 4F RTA21EA 20050224001832005022400183EA 2005 2 24 MASA200400688 120041210A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA CABIN DETACHED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07906FJ 15006 ASH 6127 PHX - YEG, EXIT LIGHT ON SIDEWALL BY ROW-1 DOOR NOT ATTACHED TO AIRCRAFT. MAINTENANCE RE-ATTACHED THE EXIT LIGHT. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20050222003082005022200308WP 2005 2 22 04FDEA02876 120041005A5320AFA7395 COVER DOUG MD10 MD1010F 3022112WP FUSELAGE PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 PUNCTURE/GOUGES ON AFT PIT LOWER AFT TORQUE BOX COVER. WELD REPAIRED IAW FEDEX EA 8-5320-81483. REFERENCE NON-ROUTINE NR N00990. 2L73 4F RTA22WE 20050223000062005022300006EU 2005 2 23 DHL2004362011 120040905A2120 ODOR AIRBUS300 A300B4203 3930306EU COCKPIT DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01362DH 84 DETECTED ODOR OF BURNING RUBBER DURING DESCENT. ODOR IN CABIN, NOT IN COURIER AREA. NO SMOKE LIGHTS OR ABNORMAL TEMPS. SECURED LEFT PACK AS A PRECAUTION AND ODOR SEEMED TO DISIPATE. INSPECTED LEFT PACK AIR INLET AND PERFORMED OPERATIONAL TEST IAW AMM 21-51-00. NO DEFECTS NOTED. SYSTEM OPS CHECKS NORMAL. 2L72 4F RTA35EU 20050223000122005022300012NM 2005 2 23 04FDEA02513 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LEFT WING, REAR SPAR, XORS= 585 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 585 LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000172005022300017WP 2005 2 23 04FDEA02642 120040904A5730ARC05662 PANEL DOUG DC10 DC1010F 3022111WP ZONE 600 DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 PANEL 636 DL HAS SEVERAL AREA OF DELAMINATION. REPAIRED PANEL P/N ARC0566-2 BY FABRICATING AND BONDING NEW SKIN, DOUBLERS AND CORE IAW FEDEX EA 8-5710-77513, DAC DWG ARC0566 AND TPS 1001 REV E, REFERENCE N/R N00321. 2L73 4F A22WE 20050223000222005022300022NE 2005 2 23 04FDEA02657 220040906A7261 ENGINE DOUG MD11 MD11F 3023600NM GE CF6 CF680 30025NE NR 2 LEAKING A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25609FE36034 48549 702750 AFTER START NR 2 ENG OIL WAS APPROX 15 QTYS. AFTER 1 37 OIL QTY DECREASED TO 10 QTYS. MONITORED AND SLOW LEAK OVER THE NEXT 45 MIN DOWN TO 4 QTYS. NR 2 ENG SHUT DOWN AT 6 QTYS. OIL TEMP AND PRESS NORMAL DURING THE LEAK. FND OIL TUBE ASSY P/N 1800M14G01 BROKEN. ALSO, OIL PRES S/W MOUNT BROKEN. R/R'D LOW OIL PRESS SW S1-8121 PER 79-33-02-4-1 DUE ITS MOUNTING FLANGE BROKEN. R/R'D OIL PRESS TXMTR PER 79-33-01-4-1 DUE POSSIBLE INTERNAL LEAK. R/R`D GASKET SEAL AT CONNECTION OF OIL SUPPLY LINE REF GE IPC79-00-00 FIG25 ITEM75 FOR PRECAUTIONARY MEASURE DUE ONLY LOWER PORTION OF FAN COWL GETTING OIL ON IT. INSTALLED TUBE, NR 2 ENG PER MD11JRH CHPT-5, NO LEAKAGE NOTED AND ALL PARAMETERS ARE NORMAL. 2L73 4F4 FRTA22WE E13NE 20050223000282005022300028NM 2005 2 23 04FDEA02516 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000332005022300033NM 2005 2 23 04FDEA02521 120040819A5711ARB7411 SPAR DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 RT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACK REPAIR. 2L73 4F RTA22WE 20050223000372005022300037NM 2005 2 23 04FDEA02488 120040817A5313AFA7098501 LONGERON DOUG MD11 MD11F 3023600NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 CENTER CARGO, CORROSION OBSERVED ON LONGERON 46R BETWEEN STA 1701 AND STA 1721. CENTER CARGO, STA 1671 TO STA 1811 LONGERON 46R REMOVED AND NEW LONGERON P/N AFA7098-501, INSTALLED PER DWG AFA7098, SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II. 2L73 4F RTA22WE 20050223000412005022300041CE 2005 2 23 45111081504 120040815A740030707227 MONOPOLE LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP IGNITION SYS MISINSTALLED E J7SAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW05414FX 45111 P116213 LEFT ENGINE BEGAN TO SURGE WHEN PWR BROUGHT BACK FROM T/O TO MCT PWR SETTING. CONTINUED TO SURGE WITH POWER DROPPING TO APPROX 58 PERCENT. AUTO-IGNITION WOULD COME ON AND ENGINE WOULD RESTART. RETURNED TO DEPARTURE POINT. MAINTENANCE FOUND BOTH MONOPOLES TO BE SHIMMED TO THE HIGH LIMITS. SWAPPED N2 MONOPOLES AND PERFORMED GROUND RUNS. CND PROBLEM. PERFORMED MAINTENANCE CHECK FLIGHT WITH NO DEFECTS NOTED. 2L72 4F3 TRTT00008WIAEXJ STC 20050223000522005022300052NM 2005 2 23 DHL2004782010 120040925A3240 BRAKE ASSY BOEING727 727227 1384078NM MLG MALFUNCTIONED A DHLAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01782DH 21998 LEFT BRAKE SQUEALS, SHUDDERS AND GRABS ON APPLICATION. INSPECTED LT BRAKES, NO DEFECTS NOTED. BLED LEFT BRAKES AS A PRECAUTIONARY. WORK DONE IAW B-727 MM 32-41-0. TAXIED AIRCARFT, BRAKES OPS CHECKED GOOD. 2L73 4F A3WE 20050223000532005022300053NM 2005 2 23 04FDEA02652 120040905A5753ARC2512503 BRACKET DOUG MD11 MD11F 3023600NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE FOUND CORRODED. LEFT WING, I/B FLAP O/B HINGE (FLAP SIDE), PIVOT ATTACH LUG, O/B BORE CORROSION. REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-52-03 PAGES 442-443, ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.256 INCH AND REPAIRED AS EA NR 1-5750-80342, TITLE: WINGS, TRAILING EDGE FLAPS, LEFT HAND INBOARD FLAP (FLAP SIDE), PIVOT BORE REPAIR. 2L73 4F RTA22WE 20050223000632005022300063NE 2005 2 23 TSAA0477066 220040911A7200 ENGINE BOEING737 73725A 1384481NM PWA JT8 JT8D9A 52048NE NR 1 MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13819AL 23791 ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR LINES. PERFORMED ENGINE RUN FOR TAKEOFF POWER VERIFICATION, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 20050223000662005022300066 2005 2 23 TSAA0423064 420040907A256211032801 ANTENNA BOEING737 73776N 13844CHNM ELT FAILED A TSAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13745AL 29904 LAS-HNL: DURING CLIMB-OUT, A LOUD NOISE WAS HEARD FROM THE CEILING NEAR ROW 17. RETURNED TO LAS FOR OVER-WEIGHT LANDING AT 147K LBS, SMOOTH TOUCHDOWN. FOUND ELT ANTENNA DELAMINATED/DAMAGED. REMOVED DAMAGED ANTENNA AND INSTALLED BLANKING PLATE IAW AQ ECO 7-0223. DEFERRED ELT SYSTEM IAW MEL 23-12, PLACARDS INSTALLED. PERFORMED OVER-WEIGHT LANDING INSPECTION IAW AQ M-121-PART 1, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.INSTALLED ELT ANTENNA IAW AQ ECO 7-0223-PART II; OPS CHECK OK. PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050223000742005022300074CE 2005 2 23 GLBA20030732 120040928A29101013880083 VALVE BEECH 1900 1900D 1154162CE HYD SYSTEM FAILED A GLBAO OTHER S AFFECT SYSTEMS APAPPROACH 1 NM03219GL5347 UE219 GEAR WILL NOT EXTEND, MANUALLY EXTENDED. REMOVED AND REPLACED HYD SERVICE VALVE, OPS CK GOOD. 2L72 4T RTA24CE 20050223000872005022300087 2005 2 23 ERAA097501 420040623A2562 G SWITCH AMTR BELNCABELLANCAREP 0566041GL ELT INOPERATIVE E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03164EH 64653 FOUND G SWITCH TO BE INOPERABLE. G-SWITCH WAS INOPERABLE, BUT IT BECAME OPERABLE AFTER GENTLY TAPPING UNIT'S REAR END. SENT OUT FOR REPAIR AS PER MANUFACTURER RECOMMENDATION. 1H71 3O NCEXPA1H71 20050223000902005022300090GL 2005 2 23 ERAA097504 220040711A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 1 ENGINE WEAK E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03125EH7187 S562 WEAK AT HOVER, NR ROTOR 100 PERCENT. TORQUE NR 1 ENGINE 80 PERCENT. NR 2 ENGINE 50 PERCENT WHEN TORQUE IS MATCHED NR DROPS TO 98 PERCENT. 1G72 3U3 U H3EU E4CE 20050223000912005022300091GL 2005 2 23 ERAA097505 220040330A7323252466715H GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE BINDING E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03133EH7289 598 GOVERNOR HAS BINDING ARM. UNABLE TO TEST AS RECEIVED DUE TO SEIZED THROTTLE. BUSHING SEIZED, INTERNAL BEARINGS FOUND ROUGH/DRY. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20050223001222005022300122WP 2005 2 23 2004000010 120040814A2120 UNKNOWN DOUG DC10 DC1030 3023501WP MID-GALLEY FUMES A CNMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0749082 47927 FLIGHT CREW REPORTED FUMES IN MID-GALLEY AREA AFTER TAKEOFF. AIRCRAFT DIVERTED TO MILDENHALL, ENGLAND AS A PRECAUTION. COULD NOT DUPLICATE ON THE GROUND. NO SMOKE WAS REPORTED OR SEEN. ACCOMPLISHED OPERATIONAL CHECKS OF ENTERTAINMENT SYSTEM, LIGHTS, GALLEY EQUIPMENT AND PNEUMATIC SYSTEM WITH ENGINES RUNNING. NO DEFECTS NOTED. FLIGHT CONTINUED TO ATL WITH NO FURTHER INCIDENT. 2L73 4F A22WE 20050223001512005022300151WP 2005 2 23 04FDEA02878 120041005A5410AUB7054501 VENTILATOR PANEL DOUG MD10 MD1010F 3022112WP ZONE 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 NUMBER 3 PYLON PRECOOLER PANEL CRACKED AT WELD CORNER. WELD REPAIRED IN NEW PIECE OF MATERIAL IAW FEDEX EA 8-5480-81477 NACELLE/PYLONS NR 3 ENGINE VENTILATOR PANELS REPAIR. REFERENCE NON-ROUTINE NR N00798. 2L73 4F RTA22WE 20050223001572005022300157WP 2005 2 23 04FDEA02886 120041007A5313AYB70162 LONGERON DOUG DC10 DC1010F 3022111WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568058 46705 LOWER FUSELAGE UNDERWING LONGERON 48R IS CORRODED FROM STATION 1368 TO STATION 1521. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I PAGE 8, FIGURE 1B. REMOVED DAMAGE SECTION OF LONGERON 48R FROM STATION 1330 TO 1521. INSTALLED LONGERON 48R PART NUMBER AYB 7016-2 IAW DAC DWG 7020 AND SPLICE FITTING IAW DC10 SRM 53-00-01 VOL 1. REFERENCE NON-ROUTINE N00938. 2L73 4F A22WE 20050223001582005022300158NE 2005 2 23 DJFA2004024 220040929A7261310261402 PUMP CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENGINE MALFUNCTIONED E DJFAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 EA23583CW 5600123 PCE108513 DURING TEST FLIGHT FROM CGF, LEFT ENGINE OIL PRESSURE DECREASED INTO THE RED ARC, LEFT ENGINE WAS SECURED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED OIL PUMP PART NUMBER 3102614-02 SERIAL NUMBER 1GAT57 IN ACCORDANCE WITH MAINTENANCE MANUAL AND INSTALLED OIL PUMP PART NUMBER 3104289-01 SERIAL NUMBER 8W081. OIL WAS SERVICED. FUNCTION AND LEAK CHECK WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA22CE E25EA 20050223001612005022300161NM 2005 2 23 DHL2004760009 120041006A2910269002910M ACTUATOR BOEING727 7272B7 138407LNM NR 2 SLAT FAILED A DHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01760AT 21954 DURING CLIMB, HYDRAULIC "A" SYSTEM FAILED, QTY ZERO PRESSURE ZERO. COMPLETED ABNORMAL PROCEDURE. FOUND NR 2 SLAT ACTUATOR HOUSING BROKEN. REMOVED AND REPLACED ACTUATOR IAW B727 MM 27-81-32. OPS CKS GOOD. NO LEAKS NOTED. (SEE ITEM NR 2). 2L73 4F A3WE 20050223001732005022300173NE 2005 2 23 DJFA2004026 220041006A7200 ENGINE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE LEFT OVERHEATED E DJFAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA23283CW5985 1992 5500713 PCE71777 CREW REPORTED, THAT THE LEFT ENGINE WENT OVER TEMPERATURE LIMITS AFTER ROTATION. THE TEMPERATURE WAS UP TO APPROXIMATELY 710 WHEN THE POWER WAS PULLED BACK. IT WAS OVER 700 FOR ABOUT 5 SEC. AIRCRAFT RETURNED BACK TO KTRM. THE ENGINE IS UNDERGOING A HOT SECTION INSPECTION. 1L72 4F4 F A22CE E1NE 20050223001762005022300176WP 2005 2 23 WLDA200496 120041009A3234 LEVER DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE COCKPIT STUCK A WRLAO OTHER O OTHER LDLANDING 1 SO1114075 46922 ON APPROACH, LANDING GEAR HANDLE WOULD NOT RELEASE. COMPLIED WITH ALTERNATE GEAR EXTENSION PROCEDURE AND COMPLETED NORMAL LANDING. CLEANED AND LUBED CABLES, CLEANED CANNON PLUG ON HOLDING COIL AND CHECKED FOR BINDING ON GROUND. NO BINDING OR BROKEN CABLES, GEAR HANDLE OPERATION NORMAL IAW MM PROCEDURES. 2L73 4F4 F A22WE E23EA 20050223001832005022300183WP 2005 2 23 DHL2004801501 120040828A5712 RIB DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LEFT INNER WING OUTBOARD L/E FORMER CRACKED 0.750, STA XFS 703.750. PERFORMED STOP HOLE AND FABRICATED (2EA) REINFORCING ANGLES (AL2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLES IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050223001872005022300187WP 2005 2 23 DHL2004801554 120040927A5753 PLATE DOUG DC8 DC873F 302199FWP TE FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 RT OTBD FLAP L/E UPPER PLATING WORN, XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R03, FAA FORM 8110-3 DATED 09-24-2004. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, DWG W51-R03. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.040), INTERNAL SPLICE DOUBLER (2024-T3AL 0.050) IAW DWG W51-R03. CLEANED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN SEGMENT INTERIOR, INTERNAL SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED SEALANT TO ALL FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT INTERNAL SPLICE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, DWG W51-R03. 2L74 4F RT4A25 20050223001892005022300189WP 2005 2 23 DHL2004801544 120040927A53403755854U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 AFT CARGO COMPT STOP FITTING CRACKED 1.000, STA 1240.000, L-24L TO L-27L. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9, DC8 SRM 53-1-0 PG 1. 2L74 4F RT4A25 20050223001932005022300193WP 2005 2 23 DHL2004801512 120040902A5531 RIB DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 VERTICAL STABILIZER L/E FORMER CRACKED 0.500 AT ZRS 104.000 (LT). MED STOP DRILL AND FABRICATED ANGLE DOUBLER (AL- 2024-T3, 0.032") IAW SRM 55-2-0 PAGE 7,8.CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PAGE 1, SRM 51-1-20D PAGE 9. 2L74 4F RT4A25 20050223002002005022300200NE 2005 2 23 SPAA0400071 220040531A7200 ENGINE BOEING737 7372T4 1384492NM PWA JT8 JT8D17 52049NE NR 1 STALLED A SPAAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28703S 367777406 22529 P700543 NR 1 ENGINE S/N COMPRESSOR STALLS AT TOP OF CLIMB FL 37. 2L72 4F4 F A16WE E2EA 20050223002082005022300208EU 2005 2 23 04FDEA03271 120041130A1430 SCREW AIRBUS310 A310 EU FLAP HANDLE BROKEN A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO25425FE 264 AFTER TAKEOFF, THE FLAP HANDLE COULD NOT BE MOVED PAST THE FLAPS 0 DEGREES, NOR COULD MOVE IT PAST THE FLAPS 20 DEGREE POSTION. THE FLAPS DID MOVE FROM THE 20 DEGEES TO 15 AND BACK. FOUND SPECIAL-SCREW ITEM 161 REF A310-200 IPC 53-11-31-13 BROKEN. PARTS NEEDED. ADDED MPN A2791261920000, CPN 5310684 QTY 1 SCREW MSN 908160. INSTALLED FLAP HANDLE AND DETENT SCREW PER AMM 27-51-11-4. OPS CK NORMAL. RII:292460 ENT BY: 014582 RPT BY: 014582. 2L72 4F RTA35EU 20050223002152005022300215NM 2005 2 23 04FDEA03077 120041111A5313 STRINGER BOEING727 72722 1384002NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25166FE 18863 MAIN CARGO BAY HAS 2 GOUGES ON STR 16R AT BS 554 AND BS 557. GOUGES ON STR 16R BS 554 AND BS 557 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED STR 16R IAW SRM 53-10-3. 2L73 4F A3WE 20050223002622005022300262NM 2005 2 23 QXEA200500035 120041215A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND FORWARD FUSELAGE UPPER SKIN AT STATION 301.00 TO STATION 321.00 BETWEEN STRINGER 11P AND 12P HAS DENTS. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073. 2H72 4T RTA13NM 20050223002692005022300269NM 2005 2 23 QXEA200500036 120041215A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FORWARD FUSELAGE LEFT HAND UPPER SKIN PANEL AT STATION 301.00 TO 321.00 BETWEEN STRINGER 12P AND 13P HAS DENT. REPAIRED IAW HORIZON AIR EA 6-53-496 AND RD 8/4-53-1073, ISSUE 1. 2H72 4T RTA13NM 20050223002712005022300271NM 2005 2 23 QXEA200500039 120041215A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE INTERIOR RIGHT HAND FORWARD SEAT RAIL FROM X105 TO 102.5 HAS PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 6-53-495 AND SRM TASK 51-42-05-330-001. 2H72 4T RTA13NM 20050223002762005022300276NM 2005 2 23 QXEA200500038 120041214A5330 SKIN PANEL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - RIGHT HAND FORWARD FUSELAGE LOWER SKIN PANEL STATION 211.00S BETWEEN STRINGER 20S AND 21S DENTED. REPAIRED IAW RD 8/4-53-66, ISSUE 1. 2H72 4T RTA13NM 20050223002882005022300288NM 2005 2 23 QXEA200500079 120041220A5420 STRUCTURE DHAV DHC8 DHC8202 2809007NM NR 2 NACELLE DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09366PH 510 PDX - COUPON CUTOUT ON NR 2 NACELLE. INSTALLED REPAIR DOUBLER IAW EA 2-54-213. 2H72 4T RTA13NM 20050224000372005022400037SO 2005 2 24 SWIA200414597 120041201A5310 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 34-38, YL479.00, LEFT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00. 2L72 4T RTA31SO 20050224000402005022400040SO 2005 2 24 SWIA200414606 120041201A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 OMEGA BEAM DAMAGED AND CORRODED AT FRAME 38 CENTER BUTTSTRAP. ITEM FOUND AT C-CHECK INSPECTION. OMEGA BEAM REPAIRED IAW EMB 120 SRM 51-40-02 AND 51-70-05. 2L72 4T RTA31SO 20050224001062005022400106NM 2005 2 24 2004UALA00999 120041028A5320 SUPPORT ANGLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29653UA 25391 E/E COMPARTMENT CRACK IN SUPPORT ANGLE STATION 246 FLOORBEAM AT RBL 5. MAJOR REPAIR ACCOMPLISHED. CRACK DUE TO BODY FLEXING/LOADING. CRACKED ANGLE WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 20050224001242005022400124EU 2005 2 24 RAIA00411032 120041117A3234AIR860122 SELECTOR VALVE JETAIRJETSTMJETSTM4101 1500501EU NLG MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03550HK16139 41039 5543- STL- STEERING PULLING HARD TO THE LEFT. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL SELECTOR VALVE. 2L72 4T RTA41NM 20050224001352005022400135NM 2005 2 24 QXEA200500081 120041220A5751 HINGE DHAV DHC8 DHC8202 2809007NM RT AILERON CHAFED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09367PH 511 PDX - RIGHT AILERON INBOARD HINGE CHAFFED AGAINST TRIM ACTUATOR HARNESS. PRIMED AND BLENDED AREAS IAW EA 2-57-298. 2H72 4T RTA13NM 20050224002062005022400206SO 2005 2 24 LR7A04198 120041108A52203629833 DOOR LKHEED382 382G 526414USO EMERGENCY EXIT DETACHED A LR7AJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 AL03404LC 6 4763 FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO YFB. AT YFB FOUND RT SIDE EMERGENCY EXIT LAYING ON FREIGHT. INSPECTED DOOR ASSY, AIRCRAFT FRAME AND LATCHING MECHANISM. NO DEFECTS NOTED PER MM SMP 581 52-20. REINSTALLED DOOR. OPS CHECK NORMAL. 2H74 4T A1SO 20050224002172005022400217SO 2005 2 24 SWIA200414582 120041201A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 RIGHT INBOARD MOST FORWARD SEAT RAIL IS CORRODED IN SEVERAL LOCATIONS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT RAIL IAW SRM 51-25-00, 51-40-06, 51-40-02, AND MM 20-10-01. 2L72 4T RTA31SO 20050224002322005022400232SO 2005 2 24 SWIA200414583 120041201A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CHAFED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 LEFT FLOORBEAM BUTTSTRAP HAS CHAFING MARKS AT FRAME 16. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050224002372005022400237SO 2005 2 24 SWIA200414585 120041201A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FUSELAGE FR38 BETWEEN CENTER AND T-PROFLIE IS DAMAGED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED T-PROFILE IAW EMB SRM 51-22-00, 51-40-02. 2L72 4T RTA31SO 20050224002392005022400239SO 2005 2 24 SWIA200414587 120041201A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FR 34 TO FR 38 SEAT TRACK IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT TRACK IAW EMB SRM 51-25-00, 51-40-06, 51-21-02, 51-40-02, AMM 20-10-01. 2L72 4T RTA31SO 20050224002552005022400255NM 2005 2 24 HNAA0400170 120041201A3230CSP3259 DIODE DHAV DHC8 DHC8102 2809003NM LANDING GEAR SHORTED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07930HA 126 ON APPROACH TO DCA, ALL THREE LANDING GEAR DOORS OPENED AND CLOSED THEN OPENED AGAIN. FERRIED A/C TO SBY FOUND 2 BAD DIODES 3261-CR1 AND 3261-CR2 REMOVED AND REPLACED DIODES, OPS CHECK GOOD. 2H72 4T RTA13NM 20050224002582005022400258NM 2005 2 24 HNAA0400162 120041128A3297 WIRE HARNESS DHAV DHC8 DHC8201 2809001NM NLG MISROUTED A HNAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA07966HA 452 NOSE GEAR WOULD NOT RETRACT ON TAKEOFF. REROUTED WIRE HARNESS SUPPORT ASSY BLEED NR 2 HYDRAULIC SYSTEM AS REQUIRED. SWUNG GEAR, OPS CHECK GOOD. 2H72 4T RTA13NM 20050224002602005022400260NM 2005 2 24 HNAA0400088 120040929A531385320056107 STRINGER DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07911HA 034 DURING C-CHK, FOUND WIDESPREAD CORROSION ON STR 31S. DUE TO WIDESPREAD NATURE OF DAMAGE, DECISION MADE TO REMOVE ENTIRE STR SECTION FROM X182 TO FR (387) FOR CONVENIENCE IN LIEU OF REPEATED BLENDING AND MEASURING WITH SAME POTENTIAL RESULTS (SPLICE). THIS EO ACCOMPLISHES REMOVED AND REPLACED BY PERFUMING SPLICES PER RD8-53-2499. THIS REPAIR IS A MAJOR REPAIR. 2H72 4T RTA13NM 20050224002622005022400262 2005 2 24 GTIA040810 420041011A2565 HANDLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE SLIDE DEFECTIVE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23817NK 49141 AIL SLIDE MANUAL DEPLOY HANDLE (RED STRAP) NOT ROUTED THROUGH DEPLOYMENT LANYARD RELEASE. UPON ATTEMPTING TO REROUTE TAIL SLIDE MANUAL DEPLOY HANDLE FOUND SLIDE COMING APART. REMOVED AND REPLACED SLIDE PACK. 2L72 4F4 F A6WE E9NE 20050224002662005022400266WP 2005 2 24 GTIA040797 120041002A1430 BOLT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EVAC SLIDE LOOSE A GTIAK NONE O OTHER ININSP/MAINT 1 GL23827NK 49793 RT FWD HOLD DOWN STRAP CLIP FOR AFT EVAC SLIDE HAS A LOOSE IB MOUNTING BOLT. TIGHTENED MOUNTING BOLT. 2L72 4F4 FRTA6WE E9NE 20050224002702005022400270WP 2005 2 24 GTIA040835 120040930A5532 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE VERTICAL STAB DAMAGED A GTIAK NONE O OTHER NRNOT REPORTED 1 GL23823NK 48020 SAS B0017605R00118; VERTICAL STABILIZER UPPER (VOR) L/E LOWER MOUNT HOLES, COUNTERSINKS BEYOND SKIN, OFF CENTER HOLES ELONGATED, INTERIOR SURFACE CHAFED. INSTALLED REPAIR DOUBLER IAW SRM 51-30-5, TOPCOATED IAW SRM 51-10-3, BLENDED OUT CHAFED AREA IAW SRM 55-01, TREATED PRIMED AND PAINTED. 2L72 4F4 F A6WE E9NE 20050223001602005022300160 2005 2 23 DJFA2004022 420041007A2210 CONTACT BEECH 200 B200 1152922CE DAMPER SENSOR DIRTY E DJFAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 EA23619TA BB1758 CREW REPORTED THAT AFTER NORMAL TAKEOFF, THE YAW DAMPER AND AUTOPILOT FAILED TO ENGAGE ON SEVERAL ATTEMPTS. AIRCRAFT THEN DIVERTED TO DAL. MAINTENANCE CLEANED THE CONTACTS AT THE YAW RATE SENSOR AND APS-65. GROUND CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A24CE 20050223001622005022300162CE 2005 2 23 45120100604 120041006A2612 FIRE LOOP LEAR 45 45LEAR 5170805CE ALIDSGTPE331TPE331201A 0517 WP RT ENGINE MALFUNCTIONED E J7SAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW05418FX 45120 P116232C RT ENGINE FIRE WARNING INDICATIONS AFTER TAKEOFF. TRIPLE CHIME WARNING "RIGHT ENGINE FIRE" AND RED "FIRE" IN ITT GAUGE. DID NOT SEE RED CAS OR PEDESTAL LIGHTS. AIRCRAFT RETURNED TO DEPARTURE POINT AFTER DECLARATION OF EMERG TOWER DID NOT REPORT SMOKE OR FIRE. NO EXTERNAL INDICATION OF ANY FIRE. MAINTENANCE SUSPECTS BAD FIRE LOOP. 2L72 4F3 TRTT00008WIAEXJ STC 20050223001632005022300163EU 2005 2 23 DHL2004363503 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSLEAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING "C" CHECK, N/R 5712, CABIN SEAT TRACK HAS CORROSION ON THE FLANGE AT FS 62 RBL 78". REMOVED FASTENERS IAW A-300 SRM 51-30-30 AT CABIN SEAT TRACK AT FS 67 RBL 78". INSTALLED NEW PART IAW SRM 51-10-40 AT CABIN SEAT TRACK AT FS 62 RBL 78" AND SRM 53-10-10. 2L72 4F RTA35EU 20050223001642005022300164EU 2005 2 23 DHL2004363504 120040928A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, N/R 3875, FS 34-FS 38.2 RBL 58 SEAT TRACK FLANGES CORRODED OUT OF LIMITS PER A-300 SRM 51-40-11. REMOVED SEAT TRACK FS 34-38.2 RBL 58 IAW A-300 SRM 51-30-27. FABRICATED NEW SEAT TRACK AS PER EXAMPLE IAW A-300 SRM 51-10-40. TREAT, PRIMED, AND PAINTED IAW A-300 SRM 51-40-10, 51-40-12. INSTALLED SEAT TRACK FROM FS 34 TO FS 38.2 AT RBL 58 IAW A-300 SRM 53-10-10. 2L72 4F RTA35EU 20050223001692005022300169WP 2005 2 23 04FDEA02905 120041011A5720ARC01542 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 RIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA8-8750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME II. BEGINNING SURFACE 1.255 INCH INBOARD FINAL 1.2400 INCH OUTBOARD 1.2360 INCH. MATERIAL REMOVED INBOARD .015 INCH OUTBOARD .019 INCH FOUND OUT OF LIMITS IAW DACCMM 57-44-07. 2L73 4F RTA22WE 20050223001752005022300175NM 2005 2 23 DHL2004780513 120040923A5511 FRAME BOEING727 727223 1384074NM HORIZONTAL STAB CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01780DH 22006 DURING A C-CHECK, RT STAB AT STA 190 HAS CORROSION ON REAR 75 PERCENT CHORD. MOVED AND REPLACED RIGHT HAND STAB REAR BEAM UPPER 75 PERCENT CHORD PN-65-24571-2 IAW B727 SRM 51-30-2. 2L73 4F A3WE 20050223001862005022300186WP 2005 2 23 DHL2004801549 120040920A5730 DOUBLER DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 LT WING TOP PANEL PLATING INNER DOUBLER 505F ACCESS DOOR CRACKED 1.500 BETWEEN XRS 8.000 AND XRS 22.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW MESSAGE BOEING NUMBER 1-NRSB2, ROD SKETCH 04-08-25-001, FAA FORM 8110-3 DATED 09-01-04. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21, SRM 51-1-20D. TRIMMED OUT DAMAGED AREA IAW ROD SKETCH 04-08-25-001. FABRICATED INTERNAL REPAIR DOUBLER (7075-T6AL 0.063) EXTERNAL REPAIR DOUBLER (7075-T6AL 0.160) AND FILLER (7075-T6AL 0.385) IAW ROD SKETCH 04-08-25-001. CLEANED, AND APPLIED FUEL TANK COATING MATERIAL TO INTERNAL AREA, FILLER, INTERNAL REPAIR DOUBLER IAW SRM 51-1-12. CLEANED, TREATED AND PRIMED EXTERNAL AREA AND EXTERNAL REPAIR DOUBLE. 2L74 4F RT4A25 20050223001912005022300191WP 2005 2 23 DHL2004801551 120040929A5730 SKIN DOUG DC8 DC873F 302199FWP WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 CRT L/E HAS INTERIM REPAIR AT XFS 347.750 RT (LWR PART). PERFORMED MAJOR REPAIR IAW DWG W51-R09, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DWG W51-R09. CUT OUT DAMAGED SECTION IAW DWG W51-R09. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01.001. FABRICATED REPAIR DOUBLER (7075-T6AL 0.071) AND FILLER (7075-T6AL 0.063) IAW DWG W51-R09. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF FILLER AND REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED FILLER AND REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9, DC8 SRM 51-3-0 PG 1, DWG W51-R09. 2L74 4F RT4A25 20050223002102005022300210NM 2005 2 23 04FDEA03416 120041214A5330 SKIN DOUG MD11 MD11 3023602NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 FUSELAGE PLATES AND SKIN, BS 595.000 THROUGH 623.000. LONGERONS 36 THROUGH 48 LT AND RT, SKIN SPLICE REPAIR. 2L73 4F RTA22WE 20050223002162005022300216NM 2005 2 23 04FDEA03052 120041108A5347S4929147 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 CABIN SEAT TRACK FOUND WORN BEYOND LIMITS AT STA 998 AND 1026 RBL 47. SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIG1 VOL 1 AND SRM 51-33-01 VOL 2. 2L73 4F RTA22WE 20050223002632005022300263NM 2005 2 23 QXEA200500017 120041217A5320 SILL BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FORWARD PASSENGER DOOR SILL MEMBER HAS CORROSION AROUND SCREW HOLES ON UPPER AND LOWER SURFACES. REPAIRED IAW HORIZON AIR EA 6-53-500, R/C 4-53-118 AND SRM 51-21-0-800-801. 2H72 4T RTA13NM 20050223002672005022300267NM 2005 2 23 QXEA200500016 120041217A5347 SEAT TRACK BOMBDRDHC8 DHC8401 1390041NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - FUSELAGE INT FORWARD, LEFT INBOARD SEAT RAIL HAS CORROSION ON TOP SURFACE AT OUTBOARD SIDE AND AROUND RIVET HEADS AT STATION X-18 TO STATION X32. REPAIRED IAW SEM SUBTASKS 51-42-05-330-001, 51-40-15-400-001 AND 51-41-00-800-801. 2H72 4T RTA13NM 20050223002682005022300268NM 2005 2 23 QXEA200500022 120041220A5280 STRUCTURE BOMBDRDHC8 DHC8401 1390041NM RT MLG DOOR CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - RIGHT HAND MAIN LANDING GEAR RIGHT HAND AFT DOOR LOWER EDGE ADJACENT TO DOOR DRAIN IS CRACKED AND CRUSHED. REPAIRED IAW HORIZON AIR EA 6-54-326 AND RD 8/4-54-220, ISSUE 1. 2H72 4T RTA13NM 20050223002752005022300275NM 2005 2 23 QXEA200500044 120041219A5420 STIFFENER BOMBDRDHC8 DHC8401 1390041NM LT NACELLE WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09411QX 4055 YYC - LEFT HAND NACELLE AFT ACCESS PANEL 414AR INTERNAL STIFFENER IS WORN AWAY. REPAIRED IAW RD 8/4-54-218, ISSUE 1 AND HORIZON AIR EA 6-54-324. 2H72 4T RTA13NM 20050223002812005022300281NM 2005 2 23 QXEA200500072 120041225A5330 SKIN DHAV DHC8 DHC8202 2809007NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09347PH 480 PDX - GOUGE FOUND ON RIGHT FUSELAGE BEHIND ICE SHIELD. DAMAGE WAS REPAIRED IN ACCORDANCE WITH RD8-53-2181. 2H72 4T RTA13NM 20050223002842005022300284NM 2005 2 23 QXEA200500075 120041204A1430 NUT PLATE DHAV DHC8 DHC8202 2809007NM PANEL SPINNING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09354PH 498 PDX - PANEL 122BL HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS. 2H72 4T RTA13NM 20050224000052005022400005EU 2005 2 24 BAQA097859 120041026A1430 NUT BOLKMS117 BK117A1 5626010EU FUEL CELL BROKEN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03118NC 150 7067 ANCHOR NUT BROKEN/ REPLACED CELL 1G72 3U H13EU 20050224000072005022400007 2005 2 24 Z1RA097890 420041026A22107015480903 AUTOPILOT SYS SKRSKYS76 S76C 8143008NE NR 2 INTERMITTENT B Z1RAO OTHER S AFFECT SYSTEMS NRNOT REPORTED 1 SW11760AF2122 760523 NR 2 ROLL CHANNEL ROCKING BACK AND FORTH ON AUTOPILOT SYSTEM 1G72 3U NCH1NE 20050224000292005022400029CE 2005 2 24 Z4TA200400001 120041125A21405543622155 CONTROL CABLE BEECH 58 58 1152740CE CABIN HEAT BROKEN D Z4TAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO0595KM TH1315 CABIN HEATER BECAME INOPERATIVE. FOUND BAD IRIS CONTROL CABLE. REPLACED CABLE AND OPS CK OK. 1L72 3O 3A16 20050224000322005022400032CE 2005 2 24 Z4TA20040003 120041213A3710442CW12 PUMP BEECH 58 58 1152740CE RT ENGINE FAILED D Z4TAK NONE J WARNING INDICATION CRCRUISE 1 SO0595KM 568 TH1315 IN FLIGHT, NOTICED RIGHT PNEUMATIC PRESSURE PUMP INOP FLAGGED. CONTINUED FLIGHT ON LEFT PUMP SYSTEM. SENT ACFT TO MAINTENANCE. REPLACED PUMP WITH OVERHAULED PART. REPLACED RIGHT INSTRUMENT FILTER. OPS CK OK. 1L72 3O 3A16 20050224001272005022400127EU 2005 2 24 RAIA00412041 120041230A3150 WARNING SYSTEM JETAIRJETSTMJETSTM4101 1500501EU COCKPIT MALFUNCTIONED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03567HK 41085 5474 - STL - CONFIG WARNING INDICATION DURING TAKEOFF ROLL. MAINTENANCE PERFORMED OPS CHECK OF TAKEOFF CONFIG-WARNING WITH NO DEFECTS NOTED. 2L72 4T RTA41NM 20050224001312005022400131NE 2005 2 24 RAIA00412040 220041230A7200 ENGINE AEROSPATR72 ATR72202 8680940EU PWA PW120 PW124B NE RIGHT OUT OF TRIM A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03723TE 283 5512 - STL - RIGHT ENGINE TORQUE INDICATION HIGH. MAINTENANCE ADJUSTED TRIM FOR BOTH ENGINES AND OPS CK GOOD. 2H72 4T4 TRTA53EU E2ONE 20050224001362005022400136NM 2005 2 24 QXEA200500082 120041209A3220 ARM BOMBDRDHC8 DHC8401 1390041NM NLG DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09405QX 4047 PDX - RIGHT SIDE OF NOSE LANDING GEAR TRAILING ARM DAMAGED. REPAIRED DAMAGED AREAS IAW RD 8/4-32-026. 2H72 4T RTA13NM 20050224001572005022400157SO 2005 2 24 1386531 120041207A3260103219351 DOWNLOCK SWITCH GULSTMG1159 GIV 3980115SO LANDING GEAR FAULTY E N93AK NONE N FALSE WARNING TXTAXI/GRND HDL 1 SO13486QS4705 1386 RED LIGHT IN LANDING GEAR HANDLE WITH HANDLE IN DOWN POSITION AND 3 GREEN DOWN AND LOCKED ILLUMINATED. 2L72 4F RTA12EA 20050224001652005022400165SO 2005 2 24 1408121004 120041210A24221159SCAV373509 CONVERTER GULSTMG1159 GIV 3980115SO AC SYSTEM FAILED E N93AA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO13401QS4121 1408 1.5 HOURS INTO FLT LEFT AC POWER AND LT DC POWER FAILED. 2L72 4F RTA12EA 20050224001812005022400181SO 2005 2 24 MASA200400687 120041209A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST NRNOT REPORTED 1 SW07828MJ 145218 ASH 2851 FROM CLT TO HSV, THE FORWARD FLOOR EMERGENCY EXIT LIGHT STRIP INOP. MAINTENANCE REPLACED THE LIGHT STRIP AND AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050224002332005022400233SO 2005 2 24 SWIA200414584 120041201A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 LEFT FLOOR SUPPORT IS CORRODED AT FRAME 16, STR 15. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FLOOR SUPPORT IAW SRM 51-25-00, 51-40-06, AND 51-40-02. 2L72 4T RTA31SO 20050224002382005022400238SO 2005 2 24 SWIA200414586 120041201A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FR 32 TO FR 39 SEAT TRACK IS CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, 51-22-00, 51-40-020 AMM 21-10-01. 2L72 4T RTA31SO 20050224002812005022400281SO 2005 2 24 GLBA20030768 120041116A4960M835362024M RELAY EMB 120 EMB120ER 3260203SO COCKPIT MALFUNCTIONED A GLBAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 NM03293UX 120293 BURNING SMELL IN COCKPIT FO SIDE PANEL TOO HOT TO TOUCH. REMOVED AND REPLACED RELAY K0238. 2L72 4T RTA31SO 20050224002822005022400282NM 2005 2 24 F3LA200400117 120041212A3260106122615 PROXIMITY SENSOR BOEING737 7373L9 1384470NM LANDING GEAR FAULTY A F3LAK NONE N FALSE WARNING LDLANDING 1 NM03312FL 1720 24569 FLIGHT CREW REPORTED LANDING GEAR WARNING HORN STUCK ON WHEN FULLY CONFIGURED ON FINAL AND WOULD NOT SILENCE UNTIL FLAPS RETURNED TO UP POSITION AFTER LANDING. REPLACED PROXIMITY SENSOR 5853. OPS CHECKED GOOD. 2L72 4F RTA16WE 20050225000302005022500030SO 2005 2 25 SWIA200414596 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 34-38, CENTER BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED BUTTSTRAP IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050225000402005022500040SO 2005 2 25 SWIA200414608 120041201A2731 CONTROL ROD EMB 120 EMB120ER 3260203SO RT ELEVATOR TRIMCORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 RIGHT ELEVATOR TRIM CONTROL RODS, ROD ENDS AT TAB CONNECTION ARE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. RT ELEVATOR TRIM CONTROL ROD ENDS AT TAB CONNECTION REPLACED IAW AMM 27-32-00. 2L72 4T RTA31SO 20050225000412005022500041SO 2005 2 25 SWIA200414609 120041201A5534 ANGLE EMB 120 EMB120ER 3260203SO VERTICAL STAB CRACKED A SWIAO OTHER O OTHER ININSP/MAINT 1 NM0716731 120190 VERTICAL STAB LOWER RIGHT CLOSING ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLOSING ANGLE REPAIRED IAW EMB 120 SST-1280/99 REF SB 120-53-0074. 2L72 4T RTA31SO 20050228000312005022800031SO 2005 2 28 SWIA200414599 120041201A5315 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 34-38, STR 15R, RIGHT FLOOR SUPPORT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050224001532005022400153NM 2005 2 24 P5CA0401278 120041117A7830 THRUST REVERSER BOEING747 747283B 1384867NM NR 1 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 ON POST FLIGHT, MAINTENANCE WALK AROUND, FOUND NR 1 RT REVERSER HALF HAS DAMAGE TO PREVIOUSLY REPAIRED AREA AT FWD EDGE BETWEEN 4 O'CLOCK AND 6 O'CLOCK. REPAIRED CARRIED OUT PER SRM 54-30-03 AND 54-03. 2L74 4F A20WE 20050224001792005022400179SO 2005 2 24 MASA200400686 120041209A3350 SIGN EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A MASAK NONE L NO TEST NRNOT REPORTED 1 SW07836MJ 145359 ASH 2714 FROM MEM TO CLT, HAD THE LT OVERWING INTERIOR EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REINSTALLED THE SIGN AND IT OPERATED NORMALLY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4T RTT00011AT 20050224002832005022400283SW 2005 2 24 ERAA098196 120040723A2842VT044 TRANSMITTER BELL 412 412 1182202SW FUEL SYS CRACKED B ERAAK NONE O OTHER NRNOT REPORTED 1 SW99423EH FUEL QUANTITY FLUCTUATES. FOUND CASE CRACKED. REPLACED CASE ASSEMBLY. UNIT THEN FUNCTIONALLY TESTED GOOD. 1G72 4U H4SW 20050228000392005022800039SO 2005 2 28 SWIA200414590 120041201A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 SIDEWALL SEAT TRACK CORRODED AT STA X5533.0-10870.0 STR 12L. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00. 2L72 4T RTA31SO 20050228000542005022800054SO 2005 2 28 SWIA200414600 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 30-34, YR479.00, RIGHT BUTTSTRAP CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REMOVED AND REPLACED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050228001262005022800126WP 2005 2 28 ARWA20050202 120040203A2910 LINE DOUG DC8 DC862F 3021972WP HYDRAULIC SYS LEAKING A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19791AL 46150 DURING CRUISE LOST HYDRAULIC QUANTITY TO STAND PIPE. PERFORMED EMERGENCY/ABNORMAL CHECK LIST. FOUND ONE HYDRAULIC LINE, ENGINE NR 3, TO ENGINE LINE OPERATIONAL CHECK AND LEAK CHECK OK IN ACCORDANCE WITH MM 29-00-00. 2L74 4F 4A25 20050224002542005022400254NM 2005 2 24 HNAA0400130 120041108A2910 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003NM NR 2 CONTAMINATED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07839EX 226 NR 2 HYD CAUTION LIGHT ILLUMINATING DURING GEAR RETRACTION. FLIGHT RETURNED. MAINTENANCE JACKED AIRCRAFT AND SWUNG THE LANDING GEAR SEVERAL TIMES. BLED THE NR 2 HYDRAULIC SYSTEM AND SERVICED AS NEEDED. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050228001842005022800184SO 2005 2 28 SWIA200414601 120041201A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 30-34 STR 15R, FLOOR SUPPORT CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050228001952005022800195SO 2005 2 28 SWIA200414592 120041201A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 40 BETWEEN CENTER AND RIGHT FLOORBEAMS, INTERCOSTAL IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL PROFILE -T- IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050228002702005022800270SO 2005 2 28 SIMA200436302 120041227A2510 MECHANISM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT DIRTY A SIMAO OTHER O OTHER TOTAKEOFF 1 SW21621AE 145105 ON TAKEOFF THE FO SEAT SLID BACK UNCOMMANDED. INSPECTED CLEANED AND LUBED SEAT LOCKING MECHANISM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200502003) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002752005022800275SO 2005 2 28 SIMA200434219 120041202A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21737MW8469 145396 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20050228002772005022800277SO 2005 2 28 SIMA200434904 120041213A5330 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE LIGHTNING STRIKEA SIMAK NONE O OTHER ININSP/MAINT 1 SW21635AE 145158 LIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 20 BETWEEN STRINGERS 3L AND 4L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501814) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002802005022800280SO 2005 2 28 SIMA200434209 120041201A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21737MW 145396 DURING AN IMBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED CORROSION, FABRICATED A PLATE, FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002912005022800291SO 2005 2 28 SIMA200434205 120041126A532014525391003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21839AE4948 145653 DURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, FILLER, SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002922005022800292SO 2005 2 28 SIMA200429601 120041019A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL E/E BAY FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21840AE 145656 DURING CRUISE FLIGHT, CREW REPORTED A MAIN AND BACK UP PITCH TRIM MASTER WARNING MESSAGE WITH THE AUTO PILOT STILL CONNECTED AND AN AUTO TRIM CAUTION MESSAGE, AIRCRAFT WAS DIVERTED TO FSM. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND C/W ETN. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501218) 2L72 4F4 FRTT00011ATTE6CH 20050228002932005022800293SO 2005 2 28 SIMA200435201 120041209A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21842AE 145673 DURING AN MBV INSPECTION OF AIRCRAFT. THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMAGED OMEGA BEAM AND TREATED THE BARE METAL EDGES. FABRICATED A REPAIR ANGLE .050 IN, REPAIR PLATE .125 IN, SHIMS AND A FILLER. REPAIR DONE IAW SRM. (SW21200501808) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228002952005022800295SO 2005 2 28 SIMA200435204 120041215A272015793101 PRESSURE SWITCH EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL NR 2 FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21738NR 145401 DURING CLIMB, THE YAW DAMP FAILED FOLLOWED BY RUDDER SYS-1 INOPERATIVE. FOLLOWED BY THE RUDDER SYS-2 INOPERATIVE. AIRCRAFT WAS CONTROLLABLE AND RETURNED AS A PRECAUTION . MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER PRESSURE SWITCH IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501805) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003012005022800301SO 2005 2 28 SIMA200434502 120041206A3350110049 CHARGER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21630AE 145132 CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIPS FROM ROW 8 THRU 12 DO NOT STAY ON WHEN TESTED THEY COME ON THEN IMMEDIATELY GO OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050228003062005022800306SO 2005 2 28 SIMA200435807 120041219A532014524131007005 ANGLE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION, FOUND THE MAIN DOOR SILL ANGLES ARE CORRODED. REMOVED AND REPLACED MAIN DOOR SILL ANGLES IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003072005022800307SO 2005 2 28 SIMA200433603 120041129A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMAK NONE L NO TEST CRCRUISE 1 SW21800AE 145425 DURING PRE-FLIGHT, THE EMERGENCY LIGHTS DID NOT WORK DURING TEST FROM FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK AND POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502113) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003082005022800308EA 2005 2 28 SIMA200425901 120040912A2920MM67075293001 HYDRAULIC LINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE NR 2 SYSTEM LEAKING A SIMAHBA DEACTIVATE SYST/CIRCUITSEMER. DESCENT UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21503AE 10021 IN CRUISE, HYDRAULIC SYS, 2 FAIL. QUANTITY WENT TO 10 PERCENT. CREW FOLLOWED AOM AND SHUT NR 2 SYS DOWN, DIVERTED/LANDED AT NEAREST SUITABLE AIRPORT, AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT AND DID NOT LAND OVERWEIGHT. HYDR TEMP REMAINED AT 48 DEGREES FOR REMAINDER OF FLIGHT. RT HYD SHUT OFF VALVE MESSAGE REMAINED ON FOR APPROXIMATELY 13 MIN. FOUND PRESS LINE ON NR 2 SYS LEAKING. REPLACED IAW CRJ700 AMM 20-30-00, ALSO REPLACED SLEEVE PN B03D2136J08 AND NUT PN B03D2136J08 AND SWEDGE PN B0301010-08. PRESSURE CHECK OK, OPS CHECK GOOD. AC RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050228003092005022800309EA 2005 2 28 SIMA200432911 120041122A2432100021102 CHARGER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE E/E BAY SHORTED A SIMAK NONE A FLAME/FIRE ININSP/MAINT 1 SW21503AE 10021 APU BATTERY CHARGER SHORTED INTERNALLY AND CAUGHT FIRE WHILE AIRCRAFT POWER WAS ON. POWER WAS REMOVED AND FIRE WAS PUT OUT. FIRE WAS NOT SEVERE AND NO DAMAGE WAS NOTED TO THE AREA. BATTERY CHARGER WAS CONTAMINATED WITH SKYDROL FROM ECOLOGY BOTTLE THAT WAS NOT INSTALLED CORRECTLY. BOTTLE WAS INSTALLED CORRECTLY AND BATTERY CHARGER WAS REPLACED IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501060) 2L72 4F4 FRTA21EA EOOO63EN 20050228003102005022800310SO 2005 2 28 SIMA200435812 120041220A533014530203002 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING MBV INSPECTION, A DENT WAS FOUND AFT OF RADOME FRAME 1 AND STRINGER 13 R. REPLACED DAMAGED SECTION OF SKIN IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003312005022800331EA 2005 2 28 SIMA200435701 120041220A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE CABIN BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21506AE 10056 DURING CREW PREFLIGHT 4 FLOOR PROXIMITY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE FOR THE LIGHTS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 4 BATTERY PACKS WERE ALSO CHANGED DURING TROUBLESHOOTING. (SW21200502057) (K) 2L72 4F4 FRTA21EA EOOO63EN 20050228003322005022800332SO 2005 2 28 SIMA200435802 120041220A532014521718003 ANGLE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION FOUND ANGLE CORRODED THROUGH AFT END. REMOVED AND REPLACED FORWARD CABIN FLOOR ANGLE WITH A NEW ANGLE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003382005022800338NM 2005 2 28 ASA0440368 120041227A531165C252286 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET. REPAIRED CRACKED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050301000682005030100068EA 2005 3 1 A6WA200440201 120041126A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE LIGHTNING STRIKEA A6WAK NONE O OTHER ININSP/MAINT 1 GL31441ZW 7777 PERFORMED PERMANENT REPAIR TO LIGHTNING STRIKE DAMAGE AT FS 280 TO FS 349 ALONG STRINGER L26 (5) LOCATIONS. PERFORMED PERMANENT REPAIR TO FUSELAGE AT FS 280 TO FS 349 ALONG STRINGER 26L IAW EO 601R-53-5672. 2L72 4F4 FRTA21EA E15NE 20050301000802005030100080EA 2005 3 1 A6WA200440140 120040930A2700 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING MALFUNCTIONED A A6WAK NONE F FLT CONT AFFECTED APAPPROACH 1 GL31434AW 7322 AFTER GEAR SELECTED DOWN, AIRCRAFT STARTED UNCONTROLLED ROLL LT (AUTO-PILOT OFF), STOPPED AFTER 5 SECONDS. THEN HAPPENED SECOND AND THIRD TIME 3 MILE END-TO-END TRAILING B737. ALL ROLLS TO LT. M/C (FIRST TIME FLAPS AT 0. SECOND FLAPS AT 20, THIRD FLAPS. PERFORMED VISUAL INSPECTION OF EXTERIOR OF AIRCRAFT INCLUDING FLIGHT CONTROL SURFACES. NO DEFECTS FOUND. PERFORMED SYSTEM SECU BITE CHECK IAW MM AND CHECKED MOVEMENT OF FLAPS AND AILERONS ALL SYSTEMS CHECKS GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050301000912005030100091EA 2005 3 1 A6WA200440192 120041117A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING MALFUNCTIONED A A6WAK NONE FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL31469AW 7917 FLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREE ON APPROACH. RESET FLAP SYSTEM IAW AWAC SUPPLEMENT 98-18. NO FURTHER DISCREPANCIES. 2L72 4F4 FRTA21EA E15NE 20050301000932005030100093EA 2005 3 1 A6WA200440190 120041122A21331037708 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE STUCK A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31459AW2365 7863 REF LOG PG 124783, BLOCK 1, ON CLIMB-OUT, RECEIVED (CABIN ALT) MESSAGE AT 10K FEET. COMPLIED WITH QRH. FOUND PRIMARY OUTFLOW VALVE STUCK IN OPEN POSITION. REPLACED PRIMARY VALVE IAW AMM 21-32-01. OPS CHECK COMPLIED WITH. AUTO OK, MANUAL FAILED. 2L72 4F4 FRTA21EA E15NE 20050301000992005030100099EA 2005 3 1 A6WA200440224 120041219A7710 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE DIRTY A A6WAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31405AW 7362 ENGINE NR 1 READS 0 PERCENT IN FLIGHT, ALL OTHER PARAMETERS NORMAL. CLEANED ALL CONNECTOR PLUGS, NR 1 ALTERNATOR AND SOCKET GROUND RAN TO TAKEOFF POWER, OPS CHECK GOOD. NO DEFECTS NOTED IAW AMM. 2L72 4F4 FRTA21EA E15NE 20050301001052005030100105EA 2005 3 1 A6WA200440227 120041219A3230 LANDING GEAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG MALFUNCTIONED A A6WAK NONE J WARNING INDICATION LDLANDING 1 GL31423AW6186 7636 NOSE GEAR WOULD NOT EXTEND. MANUAL EXTENSION OK. COMPLIED WITH GEAR SWING 8 TIMES. (5 TIMES REGULAR/ 3 TIMES ON EMERGENCY) OPS CHECK GOOD. (K) 2L72 4F4 FRTA21EA E15NE 20050224002802005022400280SO 2005 2 24 SWIA200414588 120041201A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 SIDEWALL SEAT TRACK CORRODED AT STA X4600.0-10870.0 STR 12R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050225000292005022500029SO 2005 2 25 SWIA200414595 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 CENTER BUTTSTRAP AT FRAME 39-44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. STRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00 NW740S. 2L72 4T RTA31SO 20050225000392005022500039SO 2005 2 25 SWIA200414607 120041201A2731 ROD EMB 120 EMB120ER 3260203SO LT ELEVATOR TRIMCORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 LEFT ELEVATOR TRIM TAB ACTAUTOR ROD ARMS, THE TAB ATTACH, TERMINALS ARE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED OUTBOARD ROD END ON LEFT ELEVATOR TRIM TAB ACTUATOR ROD ARM. ROD ENDS REPLACED IAW AMM 27-32-02. 2L72 4T RTA31SO 20050225000482005022500048NM 2005 2 25 04FDEA02968 120041022A5340A5A71121 SPLICE DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 MAIN DECK - ATTIC AREA STA 1538 LONGERON 6R LONGERON SPLICE FOUND CRACK. NEW LONGERON SPLICE FABRICATED AS PER DWG NR A5A7112. CRACKED LONGERON SPLICE REMOVED & REPLACED AS PER SRM51-33-01 VOL 2. 2L73 4F RTA22WE 20050228000532005022800053SO 2005 2 28 SWIA200414591 120041201A5320 INTERCOSTAL EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 40, BETWEEN CENTER AND LEFT FLOORBEAMS INTERCOSTAL IS CORRODED ON THE UNDERSIDE. ITEM FOUND AT C-CHECK INSPECTION. T-PROFILE REPLACED IAW EMB 120 SRM 51-40-02 NW740S. 2L72 4T RTA31SO 20050228002812005022800281SO 2005 2 28 SIMA200431008 120041105A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21636AE 145160 DURING PREFLIGHT, CREW FOUND THE EMERGENCY LIGHTS AFT OF ROW 12 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER PACK IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20050228002852005022800285SO 2005 2 28 SIMA200431702 120041111A2120 SMOKE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DETECTED A SIMAO OTHER BP SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION DEDESCENT 1 SW21635AE 145158 DURING DECENT, CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT FOR ABOUT 30 SECONDS WITH PAINT SMOKE BEING SEEN FOLLOWED QRH PROCEDURES. THERE WERE NO ALARMS, WARNING MESSAGES OR SMOKE IN CABIN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS INSPECTED FOR SMOKE IN COCKPIT. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501211) 2L72 4T4 FRTT00011ATTE6CH 20050228002962005022800296SO 2005 2 28 SIMA200434902 120041212A27403621005009 CONTROL UNIT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL E/E BAY FAILED A SIMAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW21739AE 145402 DUAL PITCH TRIM FAIL ON CLIMBOUT. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501813) (K) 2L72 4F4 FRTT00011ATTE6CH 20050228003042005022800304SO 2005 2 28 SIMA200435203 120041208A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21631AE 145139 DURING AN MBV INSPECTION THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED, REMOVED EXISTING CENTER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM AND CORROSION PREVENTATIVE MANUAL. 2L72 4T4 FRTT00011ATTE6CH 20050228003162005022800316SO 2005 2 28 SIMA200435804 120041220A531514521721009 FLOORBEAM EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION, FOUND THE FLOOR DIGITAL CORRODED IN SEVERAL AREAS REMOVED AND REPLACED FLOOR DIGITAL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003172005022800317SO 2005 2 28 SIMA200435810 120041217A532014522460013 GUSSET EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR GUSSET HAS CORROSION ON UPPER SURFACE. INSTALLED NEW GUSSET IAW SRM. AC RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003182005022800318SO 2005 2 28 SIMA200435207 120041217A494023080013A STARTER GEN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL APU MALFUNCTIONED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21619AE 145101 CREW REPORTED ELECTRICAL SMELL IN COCKPIT AFTER ATTEMPTED APU START WHICH FAILED. INSPECTED APU AND FOUND STARTER GENERATOR TO BE MAKING LOUD NOISES AND SPARKING ON START UP. MAINTENANCE REMOVED AND REPLACED THE STARTER/GENERATOR IAW MM. GROUND RUN WAS COMPLIED WITH AND NO SMELL NOTED. (SW21200501803) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003262005022800326SO 2005 2 28 SIMA200435202 120041210A5330AL2024T3 SKIN EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21840AE 145656 DURING AN MBV INSPECTION AND REPAIR OF A DENT DEFERRED UNDER TDMI NR 84053525 BETWEEN FRAMES 21 AND 22 AND BETWEEN STRINGERS 12L AND 13L. PERFORMED A CUTOUT OF THE DAMAGED SKIN AND TREATED THE BARE METAL EDGES. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20050301001022005030100102EA 2005 3 1 A6WA200440176 120041107A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DETECTED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31427ZW 7685 FUEL SMELL UPON START UP OF APU ON GROUND BEFORE BLEEDS ARE TRANSFERRED. COMPLIED WITH (CM) ACTION PLACARDED AND PLACED ON MEL. TROUBLESHOT APU FUEL SYSTEM RAN APU AND ACM NO FUEL ODOR DETECTED. NO LEAKS DETECTED. RETURN TO SERVICE. REMOVED OFF MEL. (K) 2L72 4F4 FRTA21EA E15NE 20050301001072005030100107EU 2005 3 1 AJC2005F00000 120041229A3260M8805100018 UPLOCK SWITCH ISRAEL1125 ASTRASPX 4500205EU GARRTTTFE731TFE731* 01518WP NLG OUT OF ADJUST A AJCAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25387PA655 145 AC DEPARTED, ENROUTE. AFTER RETRACTING THE GEAR ON CLIMB OUT, THE CREW NOTED THE RED UNSAFE LIGHT IN THE LANDING GEAR HANDLE WAS ILLUMINATED. THE CREW EXTENDED THE GEAR AND GOT THREE GREEN DOWN AND LOCKED LIGHTS. THE AIRCRAFT RETURNED AND LANDED SAFELY WITHOUT INCIDENT. CREW DID NOT DECLARE AN EMERGENCY. THE AIRCRAFT WAS FERRIED FOR REPAIRS. TROUBLESHOT SYSTEM AND FOUND THE NOSE LANDING GEAR UPLOCK SWITCH WAS OUT OF ADJUSTMENT. ADJUSTED NLG UPLOCK SWITCH IAW MM. ALL SYSTEM AND OPERATIONAL CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16NM E6WE 20050301001132005030100113NM 2005 3 1 AMTA200401546 120041229A3350 LIGHT BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE EXTERIOR INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11556TZ 32590 R-1 EMERGENCY DOOR LIGHT INOPERATIVE (EXTERIOR). REMOVED AND REPLACED R-1 DOOR SLIDE, LT IAW MM. OPS CHECK NORMAL. (K) 2L72 4F4 FRTA2NM E12EU 20050301001142005030100114NM 2005 3 1 AMTA200401493 120041213A2613 WARNING SYSTEM BOEING757 75733N 1384931NM RROYCERB211 RB211535E4 54555NE COCKPIT MALFUNCTIONED A AMTAK NONE N FALSE WARNING CRCRUISE 1 GL11559TZ 32593 LT ENG OH DET 1 LOOP STATUS MSG FOLLOWED BY LT ENG OVHT EICAS. WAS ABLE TO GET OVHT LIGHT TO EXTINGUISH AFTER COMPLETING QRH PROCEDURES NNC 7.21. PERFORMED FIM PROCEDURE 26-12-00, NO DEFECTS NOTED. (K) 2L72 4F4 FRTA2NM E12EU 20050301001152005030100115NM 2005 3 1 AMTA200401328 120041027A5730 SKIN BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT WING CHAFED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11522AT 29330 RT WING LWR SKIN, 2 INCHES AFT OF FUEL ACCESS PANEL 641DB, SKIN CHAFED. REWORKED LOWER SKIN AT FUEL ACCESS PANEL 641DB, SKIN CHAFED WAS REPAIRED IAW SRM 57-20-01 AND ER 04-3910. 2L72 4F4 FRTA2NM E12EU 20050301001172005030100117NM 2005 3 1 AMTA200401414 120041116A2611 SMOKE DETECTOR BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LAVATORY ACTIVATED A K NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 GL11516AT 27972 FWD LAV SMOKE ALARM ACTIVATED BY SMOKE. EXTINGUISHER DID NOT DISCHARGE AND TEMP INDICATOR STILL IN GRAY. CHECKED LAV FLUSH MOTOR, UNDER SINK AREA AND ALSO CHECKED NAPKIN HOLDER BY SIDEWALL LIGHT, NO BURNT WIRES OR SMOKE SMELL. AC OK FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 20050302000072005030200007NM 2005 3 2 ASA0440366 120041217A5347654681513 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K) 2L72 4F4 FRTA16WE E21EU 20050302000122005030200012NM 2005 3 2 ASA0440369 120041227A531165465252 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050302000202005030200020NM 2005 3 2 ASA0440374 120041227A53154654681179 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM09765AS 25102 PAE - CORROSION ON FLOORBEAM. REPAIRED CORRODED FLOORBEAM. (K) 2L72 4F4 FRTA16WE E21EU 20050302000302005030200030SO 2005 3 2 SIM2005F00004 120041117A5240 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL ACCESS DOOR DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21627AE 145121 DURING A MBV INSPECTION, ACCESS DOOR 123BL WAS FOUND DENTED. PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER AND INSTALLED. REPAIR DONE IAW SRM. (SW21200501184) 2L72 4T4 FRTT00011ATTE6CH 20050302000332005030200033NM 2005 3 2 ASA0440387 120041226A53476546815 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - DAMAGED SEAT TRACK AT BS 927. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050302000342005030200034NM 2005 3 2 ASA0440385 120041227A532065C332685 ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - SHEAR WEB UPPER ANGLE DAMAGED AT THE EDGE AT BS 946, WL 208. REPLACED ANGLE. (K) 2L72 4F4 FRTA16WE E21EU 20050302000392005030200039SO 2005 3 2 SIM2005F00002 120041025A33502013BR CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21800AE 145425 MAINTENANCE REPORTED THE NR 2 AND NR 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204) 2L72 4F4 FRTT00011ATTE6CH 20050302000432005030200043SO 2005 3 2 SIM2005F00005 120041202A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21737MW8469 145396 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND DOUBLER. REPAIR DONE IAW SRM. 2L72 4F4 FRTT00011ATTE6CH 20050302000482005030200048NM 2005 3 2 ASA0440392 120041229A531165465558 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET STA 867 LT. REPAIRED FRAME IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050302000512005030200051NM 2005 3 2 ASA0440372 120041227A531165582802 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050302000572005030200057SO 2005 3 2 SIM2005F00006 120041025A33502013BR CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21800AE 145425 MAINTENANCE REPORTED THE NR 2 AND NR 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204) 2L72 4F4 FRTT00011ATTE6CH 20050302000602005030200060NM 2005 3 2 ASA0440383 120041227A53206546809129 STIFFENER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - VERTICAL STIFFENER CRACKED AT BS 947. REPLACED STIFFENER ANGLE. (K) 2L72 4F4 FRTA16WE E21EU 20050302000622005030200062NM 2005 3 2 ASA0440381 120041227A534765465588 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - SEAT TRACK CORRODED AT STA 370. REPAIRED SEAT TRACK. (K) 2L72 4F4 FRTA16WE E21EU 20050302000632005030200063NM 2005 3 2 ASA0440380 120041227A531165465588 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FRAME CRACKED AT PSU SUPPORT BRACKET. REPAIRED FRAME IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050302000662005030200066CE 2005 3 2 M2L2005F00000 120040915A3210121160134 FITTING CESSNA206 TU206G 2073357CE CONT O520 TSIO520M 17040SO MLG CRACKED E M2LAK NONE O OTHER ININSP/MAINT 1 NM117520N9965 U20603663 825640R THIS IS A RESULT OF HARD USE FOR MANY YEAR IN BACK COUNTRY. THE CRACKS WERE FOUND AT A PHASE II INSPECTION. THESE PARTS HAVE SERVED THEIR USEFUL LIFE AND SHOULD BE CHANGED WITH THIS MUCH TIME AND HARD USE. LANDING GEAR FITTINGS, LT AND RT, OB. (NM11200403612) (K) 1H71 3O3 O A4CE E8CE 20050302000672005030200067NM 2005 3 2 ASA0440359 120041220A53206546812169 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION FOUND ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050302000692005030200069CE 2005 3 2 N382005F00002 120041126A29102607003453 HYDRAULIC SYSTEM LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP HYDRAULIC SYS LOW E N38AO OTHER O OTHER DEDESCENT 1 EA05825LJ 496 WHILE ARRIVING, NOTICED LOW HYDRAULIC QUANTITY. CREW DIVERTED, DUE TO INCREASED RUNWAY LENGTH. (EA25200504599) 2L72 4F4 F A10CE E6WE 20050330001792005033000179EA 2005 3 30 MASA200400640 120041116A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT OUT OF ADJUST A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW07922FJ 15022 REPORTED THE RIGHT FORWARD EMERGENCY EXIT MESSAGE IN FLIGHT. MAINTENANCE ADJUSTED THE DOOR PROX SENSOR. 2L72 4F RTA21EA 20050331000072005033100007WP 2005 3 31 ASAA0580011 120040123A53119919605501 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY FRAME CORRODED. REMOVED AND REPLACED DAMAGED SECTION. INSTALLED REPAIR SPLICE. (M) 2L72 4F RTA6WE 20050331000222005033100022WP 2005 3 31 ASAA0580003 120040122A5730ARB0975 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, NINE RIGHT WING FUEL PANELS, FROM XRS TO XRS 477, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M) 2L72 4F RTA6WE 20050331000242005033100024WP 2005 3 31 ASAA0480625 120041227A531059568791 DOOR FRAME DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, FORWARD ENTRY DOOR JAMB WEB CRACKED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER. (M) 2L72 4F RTA6WE 20050331000302005033100030WP 2005 3 31 ASAA0580034 120040123A533059114073 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED SKIN WITH REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050401000532005040100053 2005 4 1 KBM2005F00028 420040109A34225050010902 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE DIRECTIONAL MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM 2167 DG ROTATES 180 DEGREES IN STRAIGHT AND LEVEL FLT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404001872005040400187NM 2005 4 4 EIA2004157 120041203A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 960 S24L FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050405000182005040500018WP 2005 4 5 ASAA0580012 120040123A532099305387 CUSP WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, MID CARGO BAY CUSP WEB/MEMBRANE CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000312005040500031WP 2005 4 5 ASAA0580006 120040122A532199365441 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, CABIN FLOORBOARD PANEL HAS CORRODED INSERTS. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050405000322005040500032WP 2005 4 5 ASAA0580002 120040122A5730ARB0975 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, SEVEN LEFT WING FUEL PANELS, FROM XRS 189 TO XRS 445, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M) 2L72 4F RTA6WE 20050405000332005040500033WP 2005 4 5 ASAA0580007 120040122A53219936651515 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, CABIN FLOORBOARD PANEL HAS INSERTED PULLED THROUGH. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050405000342005040500034WP 2005 4 5 ASAA0580008 120040122A53219936531 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHK, CABIN FLOORBOARD PANEL WAS FOUND DELAMINATED WITH CORRODED INSERTS. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050405000352005040500035WP 2005 4 5 ASAA0580010 120040122A5311993607331 FRAME DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY FRAME LOWER FLANGE WAS FOUND CORRODED ABOVE LONGERON 30. REMOVED AND REPLACED DAMAGED SECTION. (M) 2L72 4F RTA6WE 20050405000462005040500046WP 2005 4 5 ASAA0580036 120040123A532199391951 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD PANEL HAS PULLED FIBERGLASS STRANDS. APPLIED FIBERGLASS OVERLAY. (M) 2L72 4F RTA6WE 20050405000532005040500053 2005 4 5 ASAA0480622 420041225A25653961896501 LANYARD DOUG DC9 DC983 3022083WP L1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 SEA - PREFLIGHT CHECK, FORWARD PASSENGER L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20050405000542005040500054 2005 4 5 ASAA0480597 420041213A25653961896501 LANYARD DOUG DC9 DC983 3022083WP R1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 SEA - PREFLIGHT CHECK, AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20050405000622005040500062WP 2005 4 5 ASAA0580043 120040124A5730ARB0975535 ACCESS PANEL DOUG DC9 DC983 3022083WP RT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RIGHT WING FUEL PANEL AT HEAT BLANKET IS CORRODED. REPLACED PANEL. (M) 2L72 4F RTA6WE 20050405000632005040500063 2005 4 5 ASAA0480598 420041213A25653961896501 LANYARD DOUG DC9 DC983 3022083WP R1 DOOR SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 LAX - PREFLIGHT CHECK, AFT SERVICE L-2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20050401000272005040100027NE 2005 4 1 KBM2005F00019 220040216A74149560137520 SEAL SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE MAGNETO LEAKING E KBMAK NONE K FLUID LOSS ININSP/MAINT 1 WP19884SH 2884 MAG SEAL, LEAKING, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404000182005040400018SO 2005 4 4 DD52005F00000 220041112A8550 GEAR PIPER PA32 PA32R300 7103213SO LYC 0540 IO540K1G5D 41532SO OIL PUMP BROKEN E DD5AK NONE O OTHER ININSP/MAINT 1 CE056249J 1747 32R7680340 RL1842248A THE DRIVEN OIL PUMP GEAR (PN 61298) WHICH WAS ALUMINUM AND WAS NOT CHANGED AT OVERHAUL LOST A TOOTH. THE BROKEN TOOTH JAMED INTO THE DRIVE GEAR (PN 61297) WHICH BROKE 2 TEETH OFF THE OIL PUMP DRIVE (PN LW 10318) THIS IS THE ONLY PART INVOLVED THAT WAS REPLACED AT OVERHAUL. THE IDLER GEAR (PN LW 10284) HAD ONE BROKEN TOOTH AND THE CRACKSHAFT GEAR (PN LW 10297) HAD ONE TOOTH BROKEN AS WELL. DO NOT KNOW WHY THIS ENGINE IS EXEMPT FROM AD. THE ENGINE IS JUNK NOW. 1L71 3O3 O A3SO 1E4 20050404000332005040400033NM 2005 4 4 AMTA200401475 120041207A7603 LEVER BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE LT ENGINE STUCK A AMTAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 GL11528AT 30887 31398 UPON LEAVING CRUISE AT FL 410 LT ENGINE THROTTLE LEVER STUCK AT 1.5 EPR AND 85 PERCENT N1 IT UNSTUCK AT FL 240 AND WAS THEN NORMAL. PERFORMED FIM 76-11-00, FIG 103, STEPS 1, 1A, 2, 11, 22. SYSTEM OK. ALL OPS NORMAL. (GL11200508816) (K) 2L72 4F4 FRTA2NM E12EU 20050404000492005040400049EA 2005 4 4 HQ82005F00000 320041015A6114 HUB PIPER PA28 PA28161 7102803SO LYC O320 O320* 41508EA SNSNCH76E 76E* EA PROPELLER CORRODED D HQ8SK NONE O OTHER ININSP/MAINT 1 WP07616MA2200 2842116 A58490 DURING THE REMOVAL FOR PROP/ENG TBO, DISSIMILAR METAL CORROSION WAS NOTICED IN THE HUB, TN THE BOLT HOLES. THIS AC IS APPROX THREE YEARS OLD WITH 2000 HOURS. RECOMMEND: LUBE BOLT SHANKS PRIOR TO ASSEMBLY; BETTER PRIMING INSIDE THE BOLT HOLES BY MFG. (WP07200505591)(K) 1L71 3O3 O 2A13 E274 5 NP4EA4 20050404001512005040400151NM 2005 4 4 2005UALA00260 120040324A3097 WIRE BOEING757 757222 1384956NM PWA 2037 PW2037 NE WINDOW HEAT BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29525UA 24978 WINDOW HEAT RT 1 INOP, FOUND WIRES ON TB5070 TERMINALS 4, 5 & 6 SEVERELY BURNED. ELECTRICAL POWER PANEL WIRES AT P-37 OVERHEATED AND BECAME LOOSE AT TERMINALS 4, 5, AND 6. REPLACED TERMINAL STRIP. REPAIRED AND RE-TERMINATED WIRES. 2L72 4F4 FRTA2NM E17NE 20050405000162005040500016WP 2005 4 5 ASAA0580015 120040123A5540DAT4864A1503 BEARING DOUG DC9 DC983 3022083WP RUDDER WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RUDDER TORQUE TUBE BEARING IS WORN. REPLACED TORQUE TUBE ASSEMBLY. (M) 2L72 4F RTA6WE 20050405000202005040500020WP 2005 4 5 ASAA0580017 120040123A53135936037 LONGERON DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, AFT CARGO BAY LONGERON 29R CORRODED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLE. (M) 2L72 4F RTA6WE 20050405000302005040500030WP 2005 4 5 ASAA0580028 120040123A5753591004241 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT OUTBOARD FLAP INBOARD VANE CHAFED. REMOVED DAMAGE. INSTALLED REPAIR FILLER AND DOUBLER. (M) 2L72 4F RTA6WE 20050405000812005040500081WP 2005 4 5 ASAA0580040 120040124A5730ARB0975517 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT WING FUEL PANELS 1307, 13333, AND 1379 ARE WORN AND CHAFED AT EDGE. REPLACED PANELS AT XFS 70-196, XCW58-70, AND XRS 445-447 RESECTIVELY. (M) 2L72 4F RTA6WE 20050405000952005040500095WP 2005 4 5 ASAA0580041 120040124A5730ARB0975517 ACCESS PANEL DOUG DC9 DC983 3022083WP LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT WING FUEL PANELS 1363 AND 1367 ARE CORRODED ON LANDINGS. REPLACED PANELS, AT XRS 267-295 AND XRS 295-353 RESPECTIVELY. (M) 2L72 4F RTA6WE 20050405001102005040500110NM 2005 4 5 72300038 120041016A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050405001152005040500115WP 2005 4 5 IXXA0500038S 120040924A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND TH FUSELAGE FORWARD CENTER SECTION FLOORBEAM CAP UPPER CORROSION DAMAGE STA 857.000, LBL 32 INCH. REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED AREA AND FABRICATED FILLER AND REPAIR ANGLE. CLEANED, TREATED, PRIMED AND APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050405001162005040500116WP 2005 4 5 IXXA0500039S 120040924A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE AFT CENTER SECTION FLOORBEAM INTERIM REPAIR STA 1560.000, LBL 45 INCH. REPAIR ACCOMPLISHED, REMOVED INTERIM REPAIR. PERFORMED BLEND OUT ON DAMAGE AREA, FOUND OUT OF LIMITS. FABRICATED FILLER AND REPAIR ANGLE, CLEANED, TREATED AND PRIMED AREA + FILLER + REPAIR ANGLE. APPLIED PRC SEALANT ON FAYING SURFACES, INSTALLED FILLER, REPAIR ANGLE AND NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050405001182005040500118WP 2005 4 5 IXXA0500041S 120040807A5320 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE STRUCTURE FOWARD CENTER SECTION PRESSURE ATTACH ANGLE HAS CORROSION DAMAGE AT STA Y=857.125(XCW 44). REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED ANGLE, CLEANED TREATED AND PRIMED AREA. INSTALLED NEW ANGLE WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050405001602005040500160NM 2005 4 5 72300042 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 13 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2L73 4F4 FRTA3WE E2EA 20050405001612005040500161NM 2005 4 5 72300043 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 15 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2L73 4F4 FRTA3WE E2EA 20050405001622005040500162NM 2005 4 5 72300044 120041024A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 10 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2L73 4F4 FRTA3WE E2EA 20050405001762005040500176NM 2005 4 5 72300046 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2.5 INCH BY 5 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050405001792005040500179NM 2005 4 5 72300049 120041025A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .5 INCH BY 1 INCH AREA OF CORROSION IN CENTER OF S-26R. 2L73 4F4 FRTA3WE E2EA 20050405001852005040500185EA 2005 4 5 MASA200400697 120041213A215032156222 PRESSURE VALVE CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW077264V10182 7264 ASH 6517 LAX - DIVERTED TO LAX BECAUSE THE RIGHT PACK TRIPPED OFFLINE AND THE LEFT PACK IS ALREADY ON MEL. AFTER LANDING CREW SUCCESSFULLY STARTED RIGHT PACK. CONTRACT MAINTENANCE FOUND A LOOSE SENSE LINE ON THE PACK AND TIGHTENED IT. A/C WAS FERRIED TO PHX. 12/14 MAINTENANCE OPS CHECKED, TESTED GOOD THE LEFT PRSOV WAS CHANGED TO CLEAR THE LEFT PACK MEL. 2L72 4F RTA21EA 20050228000302005022800030SO 2005 2 28 SWIA200414598 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FRAME 34-38, YR479.00, RIGHT BUTTSTRAP IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP BETWEEN FRAMES 34-38 RT FIT, DRILLED AND INSTALLED IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050228002332005022800233SO 2005 2 28 SWIA200414593 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 BUTTSTRAP AT YR 479.00 FRAME 39-114 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00, 51-25-00 NW740S. 2L72 4T RTA31SO 20050228002782005022800278SO 2005 2 28 SIMA200435801 120041220A532014521725001 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION FOUND FORWARD CABIN LT SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228002842005022800284SO 2005 2 28 SIMA200433401 120041127A27403621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL HORIZ STAB FAILED A SIMAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SW21853AE3321 145742 CREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200501201) 2L72 4F4 FRTT00011ATTE6CH 20050228002872005022800287SO 2005 2 28 SIMA200432209 120041106A532014525381003 FLOOR SUPPORT EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21733KR8514 145368 IMBV - RT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND EXTERNAL ANGLE. REPAIR DONE IAW SRM. (SW 21200501181) 2L72 4F4 FRTT00011ATTE6CH 20050228003272005022800327SO 2005 2 28 SIMA200435205 120041213A27223833001009 ACTUATOR EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL RUDDER INOPERATIVE A SIMAB EMER. DESCENT F FLT CONT AFFECTED CLCLIMB 1 SW21710TB 145224 CREW REPORTED DURING CLIMB, THE RUDDER TRIM JAMMED RT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE YAW TRIM ACTUATOR IAW MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050228003362005022800336NM 2005 2 28 ASA0440373 120041229A53156573741179 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON FLOORBEAM. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050301000822005030100082EA 2005 3 1 A6WA200440219 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 RT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE AT FS 625 RT SIDE AND REPLACED WITH NEW SERVICEABLE ANGLE PN 601-35012-52 IAW SRM. 2L72 4F4 FRTA21EA E15NE 20050301001162005030100116NE 2005 3 1 AMTA200401158 220040919A7532AC69841 BLEED VALVE LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122* 54555NE NR 3 ENGINE MALFUNCTIONED A AMTAE ENGINE SHUTDOWN J WARNING INDICATION LDLANDING 1 GL11194AT 193B1230 ON FINAL, A FIRE DET LIGHT ILLUM WITH FIRE DET LOOP LIGHT. IAW PROCEDURES GOOD (B) LOOP WAS SELECTED AND TESTED GOOD. ON SHORT FINAL (B) LOOP ILLUMINATED WITH FULL FIRE INDICATIONS. BELL WAS SILENCED, ENGINE SHUT DOWN ON TAXI IN. REMOVED AND REPLACED NR 3 HP COMPRESSOR BLEED VALVE IAW 75-32-01. 2L73 4F4 F A23WE A12EU 20050302000082005030200008SO 2005 3 2 SIM2005F00003 120041116A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21627AE 145121 DURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR CENTER SILL AND INSTALLED NEW SILL. REPAIR DONE IAW SRM. (SW21200501184) 2L72 4T4 FRTT00011ATTE6CH 20050302000142005030200014NM 2005 3 2 ASA0440361 120041220A532065C3397257 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON GALLEY FLOOR SUPPORT. REPAIRED FLOOR SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050302000272005030200027EA 2005 3 2 A6W2005F00002 120041214A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 RT FS 621.00, FLOOR SUPPORT ANGLE CRACKED. REMOVED DAMAGED PORTION OF ANGLE AND INSTALLED REPAIR ANGLE IAW REO. 2L72 4F4 FRTA21EA E15NE 20050302000522005030200052NM 2005 3 2 ASA0440371 120041227A531165C252298 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050302000642005030200064NM 2005 3 2 ASA0440379 120041227A5311653239531 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FRAME CRACKED. REPAIRED FRAME IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050302000722005030200072NM 2005 3 2 ASA0440376 120041227A5313655054038 STRINGER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - STRINGER 20R CRACKED. REPLACED STRINGER. (K) 2L72 4F4 FRTA16WE E21EU 20050302000812005030200081NM 2005 3 2 USAA041101 120041214A53306516635227 STRAP BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - STRAP, WEB, SKIN, 3 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BTW, 26R, 27R SKIN SECTION. REMOVED CORROSION, INSTALLED FILLER, STRAPS AND DOUBLER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050302000932005030200093NM 2005 3 2 USAA041100 120041208A53201136020 SUPPORT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU CARGO BAY CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q05 - SUPPORT, .075 INCH CRACK, AFT CARGO DOOR UPLOCK SUPPORT. REMOVED AND REPLACED SUPPORT IAW SRM. 2L72 4F4 FRTA16WE E21EU 20050302000972005030200097NM 2005 3 2 USAA041065 120041203A534565B5783913 MOUNT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU 23704 PIT-Q5-LAV MOUNTS (2), 2 INCHES X 2 INCHES (2 EA), CORROSION; LEVEL 1; TASK NR C53-107-02, STA 994, RBL 21 AND RBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K) 2L72 4F4 FRTA16WE E21EU 20050302000982005030200098NM 2005 3 2 USAA041066 120041203A534565B5783913 MOUNT BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT-Q5-LAV MOUNTS, 2 INCHES X 2 INCHES (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-02, STA 913, LBL 21 AND LBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K) 2L72 4F4 FRTA16WE E21EU 20050302000992005030200099EU 2005 3 2 USAA041084 120041221A5320D53112818200 FLOOR SUPPORT AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1-CHECK - SUPPORT BEAM, 40 INCHES X 2 INCHES X .045 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-220-53500-003, FLOOR SUPPORT BEAM FR16 - FR21, Y254. FAB PARTS IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050302001002005030200100NM 2005 3 2 USAA041070 120041201A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - FRAME, 1.5 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK C53-107-02, FRAME AT STA 993.5, RBL 46. REMOVED CORROSION, PRIMED AND PAINTED ISW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001262005030200126EU 2005 3 2 USAA041087 120041212A5320D53472197200 BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW 0863 BFM - S1 CHECK- BEAM, 2.1 INCH X 1.0 INCH X .0200 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500-006, MAIN CABIN FLOOR AT FR 68, BL-Y254. REMOVED AND REPLACED BEAM ASSY IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050302001312005030200131NM 2005 3 2 USAA041074 120041124A5315 FLOORBEAM BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - BEAM, 10 INCH L X 1 INCH WIDE, CORROSION; LEVEL 1; TASK NR C53-107-01, FLOORBEAM SCREW HOLES, STA 312, LBBL 13 TO RBBL13. 22 INCH REPAIR ANGLE WITH 10 INCH X 1 INCH W FILLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001332005030200133EU 2005 3 2 USAA041090 120041211A5347 SEAT TRACK AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 CHECK - SEAT TRACK, 5.3 INCH X 1.0 X 0.030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500-007, SEAT TRACK AT Y1292, APPROX FR 21. INSTALLED NEW SEAT TRACK SEGMENT AND REPAIR ANGLES IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050302001352005030200135NM 2005 3 2 USAA041073 120041122A57536546434302 SKIN BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU T/E FLAP DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - SKIN, 4 INCH X 4 INCH AREA, DELAMINATION, AT IB AFT FLAP BOTTOM. REMOVED BOTTOM SKIN, CORE, INSTALLED BOTTOM REPAIR DOUBLER IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050302001372005030200137EU 2005 3 2 USAA041096 120041213A5320D53112815200202 SUPPORT BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1-CHECK - SUPPORT BEAM - SEAT TRACK; 1 INCH X 2 INCH X 0.060 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, MAIN CABIN Y765, FR 16. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050228000382005022800038SO 2005 2 28 SWIA200414589 120041201A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 SIDEWALL SEAT TRACK CORRODED AT STA X11430.0-12860.0 STR 12R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB SRM 51-40-02, 51-22-00, 51-25-00. 2L72 4T RTA31SO 20050228000622005022800062SO 2005 2 28 MASA200400736 120041230A4930 LINE EMB 145 EMB145LR 3260212SO APU LEAKING A MASAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 SW07832MJ 145310 ASH - CLT AIRCRAFT EXPERIENCED SMOKE IN THE CABIN WHILE PASSENGERS WERE BOARDING. MAINTENANCE SECURED A FUEL LEAK AT THE APU. 2L72 4T RTT00011AT 20050228000632005022800063 2005 2 28 MASA200400737 420041231A34180020BN4MOD3A COMPUTER EMB 145 EMB145LR 3260212SO STALL WARNING FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07851MJ6916 145572 CLT TO LIT ABORTED TAKEOFF DUE TO SPS2 INOP MESSAGE AND SPS ADVANCED. MAINTENANCE REPLACED THE SPS COMPUTER AND THE NR 2 AOA VANE. (AOA VANE P/N 0861DT5 MOD 2, S/N OFF 1317 WITH 6916 TT AND 6343 TC). 2L72 4T RTT00011AT 20050228002792005022800279EU 2005 2 28 SIMA200436601 120041228A33506013211 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21235AE 340B235 CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE AT ROWS 8,9, AND 10. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY POWER SUPPLY UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502058) (K) 2L72 4T4 TRTA52EU E8NE 20050228002942005022800294EA 2005 2 28 SIMA200431703 120041107A2824T99A38603 EJECTOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT WING CRACKED A SIMAK NONE O OTHER CRCRUISE 1 SW21517AE 10124 DURING CRUISE FLIGHT, CREW REPORTED FUEL TRANSFERRED FROM THE RT WING TO THE CENTER TANK WITH BOOST PUMPS OFF. MAINTENANCE FOUND THE RT PRIMARY EJECTOR CRACKED. THE EJECTOR WAS REPLACED WITH A NEW TYPE EJECTOR IAW EO CR-2800-019. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20050228002972005022800297EU 2005 2 28 SIMA200435206 120041217A3350330151 POWER SUPPLY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21386AE 340B386 DURING PRE-FLIGHT CREW FOUND THE EMERGENCY LIGHT AT 4A TO BE INOPERATIVE. MAINTENANCE REPLACED THE DOME LIGHT AT 4A AND AN EMERGENCY POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501824) (K) 2L72 4T4 TRTA52EU E8NE 20050228003032005022800303SO 2005 2 28 SIMA200432703 120041118A2910156221 SWITCH EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL HYDRAULIC SYS LEAKING A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21613AE 145081 CREW REPORTED AIRCRAFT HAD HYDRAULIC SYSTEM 2 FAIL IN FLIGHT. THEY FOLLOWED THE AOM AND CONTINUED AND PERFORMED AN EMERGENCY LANDING. AIRCRAFT LANDED SAFELY WITH NO OTHER INCIDENTS. FOUND NR 2 HYDRAULIC SYSTEM SWITCH LEAKING REPLACED SWITCH. FOUND NR 2 EDMP PRESSURE LINE LEAKING REPLACED LINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PARTS REPLACED SWITCH 156221 AND LINE 15622101. (SW21200501199) 2L72 4F4 FRTT00011ATTE6CH 20050228003112005022800311SO 2005 2 28 SIMA200434903 120041213A33502013BR BATTERY EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN DISCHARGED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21688AE 14500849 DURING EMERGENCY LIGHT TEST ALL LIGHTS ILLUMINATE MOMENTARILY THEN ALL LIGHTS AFT OF ROW 7 DIM AND GO OUT. REPLACED NR1, NR2, NR3 AND NR4 BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. BATTERY PN 2013BR SN OFF NR1-B2425/ NR2-B2430 / NR3-B2433 / NR4-B2434. (SW21200501809) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003132005022800313SO 2005 2 28 SIMA200435809 120041217A532014521725651 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR SILL ASSEMBLY HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FORWARD SILL ASSEMBLY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003302005022800330SO 2005 2 28 SIMA200434905 120041213A53302024T3 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE LIGHTNING STRIKEA SIMAK NONE O OTHER ININSP/MAINT 1 SW21635AE 145158 LIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 16788.5 STRINGER 6L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501815) (K) 2L72 4T RTT00011AT 20050228003342005022800334SO 2005 2 28 SIMA200435806 120041219A532014522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION, FOUND THE SUPPORT CORRODED UPPER AFT END. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN FRAME 19 AND FRAME 20 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20050228003352005022800335NM 2005 2 28 ASA0440394 120041227A531165465262 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CRACKED FRAME. TRIMMED OUT CRACK AND INSTALLED DOUBLER. (K) 2L72 4F4 FRTA16WE E21EU 20050228003392005022800339NM 2005 2 28 ASA044400 120041229A5320652072631 WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE SCRATCHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - FWD CARGO BAY BS 429, RBL 22.5, SCRATCHES ON WEB UNDER FLOOR TO SIDEWALL SUPPORT. BLENDED SCRATCHES, FOUND OUT OF LIMITS, REMOVED AND REPLACED WEB. (K) 2L72 4F4 FRTA16WE E21EU 20050228003402005022800340NM 2005 2 28 ASA0440391 120041229A5230654795145 SCUFF PLATE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - AFT LOWER CARGO DOOR CTR SCUFF PLATE GOUGED. REPLACED SCUFF PLATE. (K) 2L72 4F4 FRTA16WE E21EU 20050301000922005030100092EA 2005 3 1 A6WA200440226 120041217A5753 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT T/E FLAP DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 FLAP LOWER SKIN DENTED AT WS NEAR T/E. DENT MEASURES 2 INCHES ROUND BY .085 INCH DEEP. INSTALLED EXTERNAL REPAIR TO LT IB FLAP LOWER SKIN AT WS 106, 5 INCHES FROM T/E IAW REO. 2L72 4F4 FRTA21EA E15NE 20050301001002005030100100EA 2005 3 1 A6WA200440210 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 LT FS 621.00 FLOOR SUPPORT ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20050301001392005030100139EU 2005 3 1 USAA041094 120041213A5320D5347217220290 SUPPORT BEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 CHECK - SUPPORT BEAM, 3.33 INCHES X 1.25 INCH X 0.060 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, MAIN CABIN Y1292, FR 68. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050302000092005030200009NM 2005 3 2 ASA0440396 120041229A53206545807U30 ANGLE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - UPPER LOBE, ANGLE CRACKED, BS 292, WL 240, RBL 53. REMOVED AND REPLACED ANGLE. (K) 2L72 4F4 FRTA16WE E21EU 20050302000112005030200011NM 2005 3 2 ASA0440386 120041226A53136550540502 STRINGER BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE IMPROPER A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - STR 19R HAS SHORT EDGE DISTANCE AT FACTORY TERMINATION BS 927. REPLACED STRINGER. (K) 2L72 4F4 FRTA16WE E21EU 20050302000132005030200013NM 2005 3 2 ASA0440367 120041227A531165465587 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FRAME IS CRACKED AT PSU SUPPORT MOUNTING BRACKET. REPAIRED CRACKED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050302000162005030200016NM 2005 3 2 ASA0440398 120041229A523069366791 STOP FITTING BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - AFT CARGO BAY FWD IB DOOR STOP FITTING IS GOUGED. REPLACED AFT CARGO BAY FWD IB DOOR STOP FITTING. (K) 2L72 4F4 FRTA16WE E21EU 20050302000212005030200021NM 2005 3 2 ASA0440397 120041229A5210694122810 STOP FITTING BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CORRODED STOP FITTING. REPLACED STOP FITTING. (K) 2L72 4F4 FRTA16WE E21EU 20050302000352005030200035EA 2005 3 2 A6W2005F00000 120041115A3211 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 LT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .025 INCH. REMOVED MIGRATED BUSHING AND INSTALLED 2ND OVERSIZED BUSHING IAW REO. 2L72 4F4 FRTA21EA E15NE 20050302000702005030200070NM 2005 3 2 ASA0440378 120041227A531165465558 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FRAME CRACKED. REPAIRED FRAME IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050302001302005030200130EU 2005 3 2 USAA041089 120041208A5320D5311282600101 DUMMY RAIL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW 0863 BFM - S1 - DUMMY RAIL, 18 INCHES X 2.5 INCHES X 0.070 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, DUMMY RAIL AT Y503.2 BTW FR 12-16. REPLACED DUMMY RAIL IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050302001342005030200134NM 2005 3 2 USAA041072 120041201A5311 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - FRAME, 3 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BETWEEN STR 27R AND 28R FRAME. INSTALLED DOUBLERS IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050303000252005030300025WP 2005 3 3 NACA20040065 120041224A14302356375225 BOLT DOUG DC6 DC6 3021702WP TE FLAPS SHEARED A NACAO OTHER F FLT CONT AFFECTED APAPPROACH 1 AL03779TA 45529 RIGHT FLAP OUTBOARD ACTUATOR BOLT SHEARED. REPLACED BOLT AND INSPECTED FLAP AND CARRIAGE SYSTEM, OK FOR SERVICE. INSTALLED NEW NUT AND WASHER. OP CHECKED GOOD. 2L74 4R A781 20050228002342005022800234SO 2005 2 28 SWIA200414602 120041201A5320 BUTTSTRAP EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 FR 13-21, YR 479.00, RIGHT BUTTSTRAP CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED STRAP IAW EMB 120 SRM 51-40-02. 2L72 4T RTA31SO 20050228002832005022800283GL 2005 2 28 SIMA200432101 220041113A7200AE30071 ENGINE EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 SW21850AE3750 145722 UNCOMMANDED SHUTDOWN ON ENGINE NR 1 ON CLIMBOUT. REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20050228003052005022800305SO 2005 2 28 SIMA200435805 120041220A532014521725015 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION, FOUND THE FORWARD CABIN FLOOR RT SILL HAS CORROSION AROUND NUTPLATE. REMOVED AND REPLACED SILL ASSY IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003192005022800319SO 2005 2 28 SIMA200435808 120041219A532014522178005 SILL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION, FOUND THE SERVICE DOOR SILL CORRODED AROUND NUTPLATES UPPER SURFACE. REMOVED AND REPLACED SERVICE DOOR SILL PLATE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050228003332005022800333SO 2005 2 28 SIMA200435803 120041219A532014521713003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21650AE 145417 DURING CPCP INSPECTION FOUND THE FORWARD CABIN FLOOR OMEGA SHAPE CORRODED. REPAIRED FORWARD LT CABIN OMEGA SHAPE AT FRAME 20 CROSSBEAM ATTACH JUNCTION IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501985) (K) 2L72 4T4 FRTT00011ATTE6CH 20050301000832005030100083EA 2005 3 1 A6WA200440206 120041214A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31408AW 7568 LT FS 621 FLOOR SUPPORT ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20050301000852005030100085EA 2005 3 1 A6WA200440202 120041126A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31441ZW 7568 RT FS 484.00 AT RBL 36 ANGLE CRACKED. 2L72 4F4 FRTA21EA E15NE 20050301000862005030100086EA 2005 3 1 A6WA200440223 120041219A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY MALFUNCTIONED A A6WAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL31439AW2895 7753 MACH TRIM CAUTION MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE RE-OCCURRED. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20050301000902005030100090EA 2005 3 1 A6WA20040191 120041121A21331037729 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN PRESSURE FAILED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31459AW2365 7863 REF LOG 124783, BLOCK 1, ON CLIMB-OUT, RECEIVED (CABIN ALT) MESSAGE. COMPLIED WITH QRH. REPLACED SECONDARY OUTFLOW VALVE IAW AMM 21-32-01. OPS CHECK COMPLIED WITH, AUTO AND MANUAL CHECK GOOD AT THIS TIME. 2L72 4F4 FRTA21EA E15NE 20050405000802005040500080 2005 4 5 ASAA0480628 420041230A25653961896501 LANYARD DOUG DC9 DC983 3022083WP ESCAPE SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 SEA - PREFLIGHT CHECK, AFT SERVICE L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M) 2L72 4F RTA6WE 20050302000102005030200010NM 2005 3 2 ASA0440390 120041227A534765C3148354 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - MECHANICAL DAMAGE SEAT TRACK AT BS 727B TO 927. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050302000172005030200017NM 2005 3 2 ASA0440384 120041227A53476546813114 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE MISMANUFACTURED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02765AS 25102 PAE - OB FLANGE OF SEAT TRACK IS MISSING FLOOR PANEL ATTACHMENT HOLES AT BS 360-480. LOCATED AND DRILLED HOLES. (K) 2L72 4F4 FRTA16WE E21EU 20050302000492005030200049NM 2005 3 2 ASA0440389 120041226A534765C3148354 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - DAMAGED SEAT TRACK AT BS 727B. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050302000502005030200050NM 2005 3 2 ASA0440388 120041226A53476546813123 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - DAMAGED SEAT TRACK AT BS 480. REMOVED DAMAGED SEAT TRACK AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050302000682005030200068SO 2005 3 2 SIM2005F00007 120041221A532014521713005 CHANNEL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 DURING AN MBV INSPECTION, THE RT HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 23. BLENDED THE RT HAT BEAM TO REMOVE CORROSION. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER. REPAIR DONE IAW SRM. 2L72 4T4 FRTT00011ATTE6CH 20050302000792005030200079EA 2005 3 2 REXA04034 120041118A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING OUT OF RIG A REXAO OTHER F FLT CONT AFFECTED LDLANDING 1 SO258412F10011 7412 FLAPS FAIL ON LANDING. SYSTEM RE-RIGGED IAW AMM 27-54-00, OPERATIONALLY CHECKED GOOD. 2L72 4F4 FRTA21EA E15NE 20050302000802005030200080EU 2005 3 2 USAA041097 120041214A5315D531128152020080FLOORBEAM AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1-CHECK - FLOOR BEAM, 16 INCHES L X 2 INCHES X .027 INCH D, CORROSION; LEVEL 2; TASK JA-220-53500-001, BEAM Y1292, FR 16-20. REMOVED AND REPLACED WITH NEW BEAM IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050302000962005030200096NM 2005 3 2 USAA041067 120041203A53116973057 FRAME BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT- Q5- FRAME, 1.5 INCH, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 500D, STR 28L FRAME. MANUFACTURED ANGLE IAW MFG DWG 65C22910. (K) 2L72 4F4 FRTA16WE E21EU 20050302001322005030200132EU 2005 3 2 USAA041091 120041213A5321D5367180500300 FLOOR PANEL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 CHECK - FLOOR PANEL, .500 INCH X .300 INCH X 0.032 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-250-53100-002. FLOOR PANEL NR 262FF, Y1292, FR 66-68. REMOVED AND REPLACED WITH NEW PART IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050303001142005030300114NM 2005 3 3 AWXA200500242 120040215A5230654795217 SKIN BOEING737 7373G7 1384595NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 DURING C-16 CHECK A .25 INCH CRACK WAS FOUND IN AFT CARGO DOOR INNER SKIN AT LIGHTENING HOLE IN LOWER FORWARD CORNER BS 807, RBL 42, WL 163. MAINTENANCE CUTOUT CRACK IN AFT CARGO DOOR INNER SKIN AT LOWER FORWARD CORNER; FABRICATED A FILLER AND 2 EACH REPAIR PLATES; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13 FIG 1. 2L72 4F RTA16WE 20050302000712005030200071NM 2005 3 2 ASA0440377 120041227A53116517684 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED FWD SIDE UNDER STOP FITTING SUPPORT. REPAIRED FRAME WEB. (K) 2L72 4F4 FRTA16WE E21EU 20050302001362005030200136NM 2005 3 2 USAA041075 120041212A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US54497 22958 PIT - A-CHECK - SKIN, 2 INCH CRACK, STA 760, STR 19R, INSTALLED DOUBLER IAW SRM. 2L72 4F4 FRTA16WE E2GL 20050307000662005030700066GL 2005 3 7 CHQA200400562 220041006A7261 CARBON SEAL EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A CHQAC ABORTED TAKEOFF KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11280SK 145381 CAE312123 FLIGHT 3115 FROM ROC TO DCA - WHEN TAKEOFF POWER WAS ADDED THE FLIGHT DECK AND CABIN INSTANTLY FILLED UP WITH SMOKE. THE TAKEOFF WAS ABORTED AND THE PLANE WAS EVACUATED ON THE TAXIWAY. MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SMOKE TO COMING FROM THE LT ENGINE WITH THE PACKS SELECTED AT A HIGH POWER SETTING. THE AIRCRAFT WAS FERRIED WITH THE LT PACK OFF TO IND FOR A POSSIBLE ENGINE CHANGE. MAINTENACNE BOROSCOPED THE ENGINE AND FOUND THE LT ENGINE 0 CARBON SEAL LEAKING. REMOVED AND REPLACED 0 CARBON SEAL. ENGINE RUNS WERE PERFORMED AND THE ENGINE OPS CNA LEAK CHECKED GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050307000672005030700067GL 2005 3 7 CHQA200400563 220041009A7200AE3007A1P ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQAC ABORTED TAKEOFF KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11280SK9105 820 145381 CAE312123 DURING FLIGHT 3089 FROM CVG TO PHL, DURING TAKEOFF ROLL AT AROUND 85 KNOTS SMOKE BEGAN TO ACCUMULATE IN THE CABIN ALONG WITH A BURNING SMELL. THE TAKEOFF WAS ABORTED AND THE SMOKE DISSIPATED RAPIDLY AND CLEARED AFTER POWER REDUCTION. ALL TEMPERATURES WERE NORMAL AND THERE WERE NO FIRE INDICATIONS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND IT TO BE SAFE FOR FERRY TO CMH WITH THE BLEEDS SELECTED OFF. IN CMH MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW ROLLS ROYCE JOBCARD CE72-00-01. OPS AND LEAK CHECKED GOOD. NO SMOKE OR BURNING SMELL WAS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050307000682005030700068SO 2005 3 7 CHQA200400564 120041011A335078241 STATIC INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT FAULTY A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11260SK 145128 WHILE PERFORMING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM THE EMERGENCY LIGHTS ON THE FLOOR AFT OF THE EMERGENCY EXIT DOORS DID NOT ILLUMINATE ALONG WITH THE EXIT DOOR LOCATOR LIGHTS. REMOVED AND REPLACED STATIC INVERTER NR 5 AND NR 6 IAW EMB 145 MM 33-50-50. OPS CHECK GOOD AT THIS TIME AND DATE. 2L72 4T RTT00011AT 20050307000692005030700069SO 2005 3 7 CHQA200400573 120041026A335078812 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11266SK 145241 EMERGENCY EXIT DOOR FLOOR PROXIMITY LIGHT IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-50-02. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307000802005030700080EU 2005 3 7 AALA20050147 120041222A5340 ANGLE AIRBUS300 A300B4605R 3930308EU WING ROOT CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW217062A 474 TUL - LEFTHAND WING ROOT PICK UP ANGLE HAS CORROSION AT RIB NR 1, FRAME 41 LEFT TO F2L. CORROSION AREA IS 1 INCH BY 12 INCHES LONG WITH A DEPTH OF .064. COMPLETED REPAIR PER ESO 30595 DATED 1/21/05. 2L72 4F RTA35EU 20050307000812005030700081SO 2005 3 7 CHQA200400551 120040904A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11287SK 145460 BOTH OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. 2L72 4T RTT00011AT 20050307000832005030700083GL 2005 3 7 CHQA200400577 220041030A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL MAKING METAL A CHQABA EMER. DESCENT UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 GL11279SK11745781 145379 CAE311220 DURING CRUISE ON FLIGHT 3103 FROM LGA TO SDF, THE FLIGHT CREW HEARD A LOUD BANG. THE ITT DROPPED TO THE AMBER RANGE, AN EICAS E2 OUT MESSAGE APPEARED, AND THE ENGINE SHUTDOWN. THE QRH WAS RAN AND ABOUT 35 MINUTES OUT FROM SDF, AN EMERGENCY WAS DECLARED. DURING LANDING AN EICAS E2 EXCEEDED MESSAGE AND AN E2 SHORT DISPATCH MESSAGE APPEARED. MAINTENANCE INSPECTED THE ENGINE AND FOUND METAL SHAVINGS IN THE EXHAUST SECTION. REMOVED AND REPLACED NR 2 ENGINE. MAINTENANCE PERFORMED GROUND RUNS OF NR 2 ENGINES WITH NO LEAKS NOTED. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050307000852005030700085 2005 3 7 CHQA200400580 420041104A25654A40302 SLIDE EMB ERJ170ERJ170100LR EU CABIN DEPLOYED A CHQAO OTHER O OTHER TXTAXI/GRND HDL 1 GL11633RW59 59 17000054 AFTER ARRIVING AT THE GATE ON FLIGHT 7702 FROM IAH TO IAD, THE FLIGHT ATTENDANT COULD NOT OPEN THE EXIT DOOR. THE GIRT BAR WOULD NOT FULLY DISENGAGE FROM THE ACTIVATED POSITION. WHEN THE DOOR WAS OPENED FROM THE OUTSIDE, THE SLIDE DID NOT DISCONNECT FROM THE AIRCRAFT AND THE SLIDE PULLED OUT OF THE CONTAINER AT THE BASE OF THE DOOR. THE DOOR SLIDE ASSEMBLY DEPLOYED UPON ARRIVAL AT THE GATE BY THE MECHANICS. MAINTENANCE PERFORMED AND INSPECTION OF THE FORWARD PASSENGER DOOR EMERGENCY MECHANISM IAW EMB 170 AMM 52-11-40. REMOVED AND REPLACED EMERGENCY SLIDE ON FORWARD PASSENGER DOOR IAW WMB 170 AMM 52-11-40. 2L74 4F RTA56NM 20050307000842005030700084SO 2005 3 7 CHQA200400579 120041104A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11264SK 145221 GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED GALLEY OVERHEAD EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-09. RIGHT EMERGENCY OVERWING EXTERNAL LIGHT INOP. REMOVED AND REPLACED RIGHT WING EXTERNAL EMERGENCY EXIT LIGHT PER EMB 145 MM 33-50-10. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307002132005030700213EA 2005 3 7 SWIA200414526 120041202A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 LEFT INBOARD FS 280 BRACKET IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW ANGLE PER CRJ 200 SRM 51-42-06 AND 51-42-20. 2L72 4F RTA21EA 20050307002142005030700214EA 2005 3 7 SWIA200414527 120041202A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 FLOORBEAM AT STA 280 RBL 9.1 CRACKED ON INBOARD AND OUTBOARD SIDES OF FLOORBEAM WEB, AND AT LEFT OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLES IAW CRJ 200 SRM 51-42-06 FIG 8, 51-42-21 FIG 10. 2L72 4F RTA21EA 20050307002152005030700215EA 2005 3 7 SWIA200414528 120041202A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07433SW 7550 RIGHT SIDE FS 621.00 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED -2 ANGLE, -6 ANGLE, -6 STRAP AND -302 ANGLE PER CRJ 200 REO 601R35-61-117. 2L72 4F RTA21EA 20050307002192005030700219SO 2005 3 7 SWIA200414604 120041201A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 OMEGA BEAM FROM FRAME 40 TO 38 YL479.00 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW 1C 2004-120/5994. 2L72 4T RTA31SO 20050307002202005030700220SO 2005 3 7 SWIA200414605 120041201A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 OMEGA BEAM CORRODED AT STA X13056.0 YR479.00. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED OMEGA BEAM IAW EMB 120 SRM 51-70-05 FIG 1. 2L72 4T RTA31SO 20050307003012005030700301SO 2005 3 7 SIMA200432202 120041115A3350110049 CHARGER EMB 135 EMB135KL 3260302SO CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21800AE 145425 EMERGENCY FLOOR LIGHTING ROWS 1-6 FAIL TO LIGHT DURING TEST. REPLACED BATTERY AND BATTERY CHARGER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050307003102005030700310EU 2005 3 7 ASA0440194 220041028A72611663M91G03 SEAL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU NR 2 ENGINE OUT OF POSITION A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM02774AS2498824988 25107 PDX - AFTER TAKEOFF F/A'S REPORTED FOG IN THE CABIN. REMOVED AND REPLACED THE NR 2 ENGINE IAW ASA T/C 48571015. REF ASA LOG PAGE AVAILABLE UPON REQUEST. THIS REPORT IS BEING FILED AS CLOSED AS CONFIRMED BY THE TEARDOWN REPORT FINDING THAT THE SMOKE EVENT WAS INDEED A RESULT OF THE FOLLOWING: NR 3 AFT AIR/OIL SEAL SEPARATED AND MOVED AFT AND CONTACTED THE HPS 1-2 SPOOL AND FORWARD SHAFT, FORWARD HALF OF SEAL REMAINED BOLTED TO FAN FRAME. THE ORIGINAL COPY OF THE TEARDOWN REPORT IS AVAILABLE AT THE RELIABILITY DEPARTMENT. (M) 2L72 4F4 FRTA16WE E21EU 20050307003112005030700311NM 2005 3 7 ASAA0410686 120041130A5320654655110 INTERCOSTAL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON WEB INTERCOSTAL. REPLACED INTERCOSTAL. (K) 2L72 4F4 FRTA16WE E2EA 20050307003122005030700312NM 2005 3 7 ASAA0410674 120041130A5347655498614 SEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE MISDRILLED A ASAAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: SEAT TRACK HAS MISDRILLED HOLES. REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E2EA 20050307003132005030700313NM 2005 3 7 ASAA0410675 120041130A5320654796010 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: AFT CARGO DOOR AFT CUTOUT CLOSURE WEB BETWEEN STRINGERS IS GOUGED. REPLACED WEB. 2L72 4F4 FRTA16WE E2EA 20050307003142005030700314NM 2005 3 7 ASAA0410687 120041130A532069353521 INTERCOSTAL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON WEB INTERCOSTAL. REPLACED INTERCOSTAL.(K) 2L72 4F4 FRTA16WE E2EA 20050307003152005030700315NM 2005 3 7 ASAA0470033S 120041104A53451496377 SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND CORROSION ON SIDE WALL SUPPORT FRM BS727 TO BS767. REPAIRED IAW SRM 51-40-05. (K) 2L72 4F4 FRTA16WE E00055EN 20050307003162005030700316NM 2005 3 7 ASAA0470034S 120041104A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE CARGO BAY DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND NR 3 FLOOR PANEL DAMAGED IN FWD CARGO BAY. REPAIRED IAW SRM 53-30-53. (K) 2L72 4F4 FRTA16WE E00055EN 20050307003192005030700319NM 2005 3 7 ASAA0470039S 120041104A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND AFT BAY NR 2 FLOOR PANEL DAMAGED. REPAIRED IAW SRM 51-20-01. (K) 2L72 4F4 FRTA16WE E00055EN 20050307003212005030700321NM 2005 3 7 ASAA0470037S 120041104A5320HFAB53FS011 FLOOR SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 775, LBL4 IN AFT CARGO BAY. REPAIRED IAW SRM 51-40-02.(K) 2L72 4F4 FRTA16WE E00055EN 20050307003232005030700323NM 2005 3 7 ASAA0470036S 120041104A53201496444 SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT IN FWD CARGO BAY. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E00055EN 20050307003242005030700324NM 2005 3 7 ASAA0410676 120041130A53476554968 SEAT TRACK BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON SEAT TRACK. REPLACED SEAT TRACK. 2L72 4F4 FRTA16WE E2EA 20050307003262005030700326WP 2005 3 7 ASAA0480571 120041118A575359304963 VANE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE T/E FLAP DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - RT IB FLAP HAS DAMAGED OB VANE. INSTALLED REPAIR FILLER AND DOUBLER.(K) 2L72 4F4 F A6WE E9NE 20050307003282005030700328WP 2005 3 7 ASAA0480569 120041118A5310995773991 SHEAR TIE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - SHEAR TIE IS CORRODED. REPLACED SHEAR TIE.(K) 2L72 4F4 F A6WE E9NE 20050307003292005030700329WP 2005 3 7 ASAA0480565 120041118A53305911410531 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - FWD LAV SERVICE DOOR CUTOUT IN LOWER AREA. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR DOUBLER IAW EA.(K) 2L72 4F4 F A6WE E9NE 20050307003312005030700331WP 2005 3 7 ASAA0480559 120041118A533059114011 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK- FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK. 2L72 4F4 F A6WE E9NE 20050307003322005030700332WP 2005 3 7 ASAA0480563 120041118A531159128525 FRAME DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM03934AS 49235 C-CHECK - NLG LT TUNNEL FORWARD CUTOUT FRAME, CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR ANGLE.(K) 2L72 4F4 F A6WE E9NE 20050307003342005030700334NM 2005 3 7 ASAA0470031 120041026A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK, FOUND FWD CARGO COMP NR 1 FLOOR PANEL CORRODED AT BS 596. FABRICATED IAW SRM.(K) 2L72 4F RTA16WE 20050307003382005030700338WP 2005 3 7 ASAA0480541 120041028A33506011779 BATTERY PACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02969AS259949394 53063 OKC C-CHECK, OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLY (BATTERY PACK). LIGHTS THEN OPERATED PROPERLY.(K) 2L72 4F4 FRTA6WE E9NE 20050307003392005030700339WP 2005 3 7 ASAA0480549 120041030A21205910090289 RETAINER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE HEAT EXCHANGER CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK-HEAT EXCHANGER RAM AIR (Y) DUCT HAS BROKEN RETAINER ON LT SIDE. REMOVED DAMAGE, WELDED IN REPAIR TAB IAW EA. 2L72 4F4 FRTA6WE E9NE 20050307003402005030700340NM 2005 3 7 ASAA0410679 120041130A532065330183001 ANGLE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON WEB IB ANGLE BELOW CAPT NR 2 WINDOW. REPLACED WEB IB ANGLE. 2L72 4F4 FRTA16WE E2EA 20050307003412005030700341NM 2005 3 7 ASAA0410680 120041130A532065330183001 ANGLE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON WEB ANGLE. FABRICATED AND REPLACED WEB IB ANGLE. 2L72 4F4 FRTA16WE E2EA 20050307003432005030700343NM 2005 3 7 ASAA0410677 120041130A532069353592 INTERCOSTAL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON INTERCOSTAL. REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2EA 20050307003442005030700344NM 2005 3 7 ASAA0410678 120041130A531065558852 CREASE BEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CREASE BEAM WEB IS CRACKED. REPLACED CREASE BEAM WEB. 2L72 4F4 FRTA16WE E2EA 20050307003482005030700348NM 2005 3 7 ASAA0410681 120041130A53306545800 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: SCRIBE MARK IN SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050307003492005030700349NM 2005 3 7 ASAA0410684 120041130A53206546530 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: FRAME/FLOOR WEB CRACKED. REPAIRED CRACKED FRAME/FLOOR WEB. 2L72 4F4 FRTA16WE E2EA 20050307003502005030700350NM 2005 3 7 ASA0440362 120041220A532065C3397255 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON GALLEY FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050308000522005030800052NM 2005 3 8 EIA2004113 120040930A5320 FLOOR SUPPORT BOEING747 747SR46 1384816NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 UPPER DECK, FLOOR SUPPORT UPPER CHORD OPEN HOLES CRACKED AT BS380, 400, 420, 520, 540, 600, 660, AND 720. REPAIR OPEN HOLES PER SB 747-53A2452. REPETITIVE INSPECTION ECRA 477-53-105-1. 2L74 4F RTA20WE 20050308000612005030800061NM 2005 3 8 200411010 120041116A2910 LINE DOUG MD88 MD88 3023688NM HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23161PL 49764 DURING TRANSIT, CHECK WAS DETECTED LEAK IN LINE HYD BRAKE NR 1. THE PROCEDURE MAINTENANCE AND DEFERRED IAW MEL 32-10 CAT. C WAS PERFORMED. DURING OVERNIGHT SERVICE, CHECK VALVE BRAKE NR 1 WAS REPLACED IAW MM 32-42-00, ALL CORRECT. 2L72 4F RTA6WE 20050308000642005030800064EU 2005 3 8 DHL2004363009 120041120A3243 B-NUT AIRBUS300 A300B4203 3930306EU MASTER CYLINDER LOOSE A DHLAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO01363DH 85 AFTER LANDING AND WHILE APPLYING BRAKES, AIRCRAFT PULLS NOTICABLY TO THE RIGHT. ALSO, RIGHT BRAKE PEDAL FEELS "SOFT". FOUND LOOSE B-NUT ON MASTER CYLINDER LOCATED UNDER F/O'S FLOOR PANEL. RESECURED B-NUT, LEAK CHECKS OK. NO FURTHER DEFECTS NOTED IAW 32-43-60. 2L72 4F RTA35EU 20050308000652005030800065CE 2005 3 8 DJFA2004034 120041119A29104AS65020001 PUMP BEECH MU300 400A 1155402CE HYD SYSTEM OUT OF LIMITS E DJFAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA23709TA RK180 CREW REPORTED, IN CLIMB, NOTICED HYD PRESS FLUCTUATING ABOVE NORM. AFTER FL390, PRESS STABLE FOR 5 TO 10 MINS THEN INCREASED TO 2000 PSI AND HELD. EMERG DECLARED. A/C LANDED USING ALT GEAR EXTENSION, WITH A NO FLAPS APPROACH. PWR BRAKE FAILURE CHECKLIST USED. NO FURTHER PROBLEMS DURING LANDING. MX FOUND LOOSE WIRE SPLICE FOR NR 4 WIRE OF HYD PRESS XMITTER CANNON PLUG. NEW SPLICE INSTALLED, OPS CHECK OF HYD PRESS IND WAS PERFORMED. SPEED BRAKES, FLAPS, L/G, THRUST REVERSERS, AND BRAKE SYSTEMS WERE BLED. THE N2 BLOW DOWN BOTTLE WAS SERVICED. OP`S CHECK WAS GOOD. PROBLEM REOCCURED DURING TEST FLT LT/RT ENG DRIVEN HYD PUMPS AND RT HYD PUMP DRAIN LINE REPLACED. TEST FLT COMPLETED. A/C RETURNED TO SERV. 2H72 4F RTA16SW 20050308000672005030800067WP 2005 3 8 ABXA040388 120041118A3230 PIN DOUG DC8 DC863F 302198FWP MLG SHEARED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23819AX 45927 UPON GEAR RETRACTION, "LNDG GEAR UNSAFE' LIGHT REMAINED ILLUMINATED, FAILED UPLATCH CHECK. LEFT GEAR AND LEFT DOOR LATCH LIGHT ILLUMINATED DURING ALT UPLATCH CHECK. MAINTENANCE AT FLL, FOUND LEFT MAIN GEAR RETRACT ACTUATOR ATTACH PIN SHEARED. REPLACED LEFT HAND GEAR RETRACT ACTUATOR ATTACH PIN IAW OVERHAUL MANUAL 32-1-1B. WORK PERFORMED BY AAR LANDING GEAR SERVICES. LANDING GEAR RETRACTION CHECK DEFERRED PER FERRY PERMIT NR 017-04. AIRCRAFT FERRIED TO ILN. AT ILN PERFORMED ADJUSTMENT TEST OF EXTENSION AND RETRACTION SYSTEM IAW DC8 MM 32-30-00-2-0001. AT ILN, REPLACED LEFT HAND MAIN LANDING GEAR RETRACT SWIVEL GLAND LOWER 90 DEGREE FITTING DUE TO LEAKING IAW DC8 MM 20-13-00-2-0001, LEAK CHECKED GOOD. 2L74 4F 4A25 20050308000682005030800068NM 2005 3 8 DHL2004760013 120041202A3260 WARNING LIGHT BOEING727 7272B7 138407LNM MLG ILLUMINATED A DHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01760AT 21954 RED NOSE GEAR LIGHT ILLUMINATED UPON GEAR RETRACTION AFTER TAKEOFF. RECYCLED LANDING GEAR DOWN THEN UP, AND ALL LIGHTS EXTINGUISHED. PERFORMED NOSE GEAR EXTENSION AND RETRACTION SEVERAL TIMES, NOSE GEAR INDICATION CK NORMAL IAW M/M 32-33-00. NO DEFECTS NOTED. 2L73 4F A3WE 20050308000692005030800069NM 2005 3 8 DHL2004781005 120041202A3350 LIGHT BOEING727 727227 1384078NM COCKPIT LOOSE A DHLAO OTHER O OTHER CRCRUISE 1 SO01781DH 21996 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR FLASHES INTERMITTENTLY. RESECURED ASSY, OPS CK GOOD IAW 33-50-101. ` 2L73 4F A3WE 20050307002982005030700298SO 2005 3 7 SIMA200435601 120041219A3350201314 BATTERY PACK EMB 135 EMB135LR 3260305SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21709GB 145211 RDU - FLT 4707 - EMERGENCY EXIT SIGN AND FLOOR LIGHTS INOPERATIVE. REPLACED NR 4 BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050307003252005030700325WP 2005 3 7 ASAA0480564 120041118A5310991960493 SHEAR TIE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - SHEAR TIE CORRODED ON AFT SIDE. REPLACED SHEAR TIE.(K) 2L72 4F4 F A6WE E9NE 20050307003472005030700347NM 2005 3 7 ASAA0410682 120041130A532065C27771 INTERCOSTAL BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON AFT CARGO INTERCOSTAL. REPLACED INTERCOSTAL. 2L72 4F4 FRTA16WE E2EA 20050308000602005030800060NM 2005 3 8 04FDEA02971 120041022A5753ARC74901 BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 RIGHT WING INBOARD FLAP VANE, INBOARD TEE FITTING HOLES HAVE CORROSION AND FORWARD HOLE BORE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL 2 AND REPAIRED AS PER FEDEX EA 1-5750-81569 TITLE: WINGS TRAILING EDGE FLAPS, RIGHT HAND I/B FLAP VANE, I/B TEE FITTING BORES, CORROSION REPAIR. 2L73 4F RTA22WE 20050308000662005030800066EA 2005 3 8 HNAA0400161 120041124A6120 BETA SWITCH DHAV DHC8 DHC8311 1386006EA NR 2 OUT OF RIG A HNAAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 EA07337EN 284 AFTER TAKEOFF, NR 2 ENGINE HAD BATE LOCKOUT FAILURE ASSOCIATED WITH THE NR 2 ENGINE TORQUE FLUX MAX TORQUE AT 100 PERCENT RETARDED NR 2 POWER LEVER TO 900 RPM SYSTEM RETURNED TO NORMAL. PHL MNT IS GOING OUT TO A/C TO DEACTIVATE BETA LOCKOUT SYSTEM. CAPT DID NOT DECLARE AN EMERGENCY. A/C NOT BACK TO GATE UNTIL 11:05 CHECKED RIGGING AND OPERATION OF NR 2 BETA BACK UP SWITCH 6141-S4 THROUGH PIN P AND Y AT 9811 P38, NO DEFECT NOTED FOUND SWITCH 6141 S4 DUSTY AND STICKY CLEANED SWITCH REACTIVATED BETA LOCKOUT PERFORMED BETA LOCKOUT GROUND LOGIC OPS CHECK W/C 61-20-10. 2H72 4T RTA13NM 20050308000982005030800098WP 2005 3 8 ASAA0480586 120041207A53305936003501 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-SKIN IS GOUGED. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.(K) 2L72 4F4 FRTA6WE E9NE 20050308000992005030800099WP 2005 3 8 ASAA0480587 120041207A53219957918501 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-OVERWING FLOOR PANEL SCREW HOLE TORN. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER.(K) 2L72 4F4 FRTA6WE E9NE 20050308001012005030800101WP 2005 3 8 ASAA0480574 120041126A25603961896501 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE R1 DOOR DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02947AS 53020 PRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K) 2L72 4F4 FRTA6WE E9NE 20050308001022005030800102NM 2005 3 8 ASA0440360 120041220A53206546812169 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION FOUND ON FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050308001032005030800103NM 2005 3 8 ASAA0470029 120041026A53207075T6 SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 SW15626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION FWD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT AT BS 500B TO 500D. REPAIRED IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050308001152005030800115NM 2005 3 8 ASAA0470018 120041009A5330143A32521 SKIN BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE DAMAGED A ASAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM02623AS 30166 OKC - TOW BAR SNAPPED CAUSING RT FUSELAGE DAMAGE FORWARD OF FORWARD CARGO DOOR AT STA 375 TO 410 BETWEEN STR 18R AND 20R. REPAIR IAW EA 5330-01838. 2L72 4F4 FRTA16WE E00055EN 20050308001172005030800117NE 2005 3 8 GUU2004F00040 220041009A72503044700 TURBINE BLADES BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUAO OTHER S AFFECT SYSTEMS ININSP/MAINT 1 SO17815351735110071 UE147 PS114375 DURING POST FLIGHT WALK-AROUND, FOUND A HOLE IN NR 2 ENGINE IB EXHAUST STACK. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS INTERNAL DAMAGE. REPLACED RT POWER SECTION MODULE. POWER ASSURANCE RUN AND LEAK CHECK COMPLIED WITH. ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: SUSPECT NR 2 PT BLADE FAILURE. 2L72 4T4 TRTA24CE E26NE 20050308001182005030800118CE 2005 3 8 EHA2004F00006 120040726A2110 UNKNOWN BEECH 200 B200C 1152924CE PWA PT6 PT642A NE CABIN PRESSURE MALFUNCTIONED P EHAAO OTHER J WARNING INDICATION TOTAKEOFF 1 AL03134WJ BL134 PRELIMINARY - AIRCRAFT DEPARTED ON MEDICAL EVACUATION TRIP. AIRCRAFT DID NOT PRESSURIZE. PIC NOTED LACK OF PRESSURIZATION BY THE EMERGENCY OXYGEN MASK AUTOMATIC DEPLOYMENT. AIRCRAFT AIR TURNED BACK. AIRCRAFT REMOVED FROM SERVICE. PERFORMED MM 21-30-00, PREFLIGHT TEST SATISFACTORY. AIRCRAFT REMAINS OUT OF SERVICE PENDING FURTHER TROUBLESHOOTING. 1L72 4T4 T A24CE E4EA 20050308001192005030800119NM 2005 3 8 AMTA200401415 120041117A2424 GCU BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE UPPER MALFUNCTIONED A AMTAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11525AT 30548 AFTER TAKEOFF, LT ENG LIMITER LIGHT CAME ON AND LT EEC LIGHT CAME ON ABOUT 15 MINUTES LATER. LOST THE LT GEN, OIL PRESSURE DROPPED TO 18 AND ENGINE WAS FAILING SO WE SHUT IT DOWN. RAN ALL CHECK LISTS. REPLACED UPPER DEDICATED GENERATOR CONTROL UNIT IAW MM. PERFORMED TEST 2 AND 3 OF MM 71-00-00-5. OPS CHECK NORMAL. 2L72 4F4 FRTA2NM E12EU 20050308001212005030800121EA 2005 3 8 DAT2004F00008 220041110A7200PT6A45R ENGINE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA RIGHT FAILED E DATACE ABORTED TAKEOFF ENGINE SHUTDOWN O OTHER TOTAKEOFF 1 GL13390GA SH3077 DURING THE TAKEOFF ROLL, A LOUD BANG AND HIGH PITCH WHINE COULD BE HEARD FROM THE RT ENGINE. AC SURGED AND YAWED AND THE POWER LEVERS WERE RETARDED IMMEDIATELY. THE TAKEOFF WAS ABORTED AND THE RT ENGINE WAS SHUTDOWN. THE AC WAS RETURNED TO THE RAMP AT APPROXIMATELY 0205Z. MAINT REMOVED THE GAS GENERATOR(PCE 84180), POWER SECTION(PS84232) AND PROP( EVA2175) FROM THE RT SIDE OF AC. GAS GENERATOR (PCE 84221) AND POWER SECTION (PS 84003) WERE INSTALLED AS A COMPLETE ENG MODULE ASSY WITH THE ACCESSORIES INSTALLED AS REMOVED. IAW PT6A-45 MM. THE ORIGINAL PROPELLER (EVA2175) WAS REINSTALLED ON RT SIDE IAW MM, INCLUDING COMPLIANCE OFAD IAW SB A203A AND IS NEXT DUE AT 18574.6. OPS CK GOOD, RETURNED TO SERVICE. 2H72 4T4 T A41EU E4EA 20050308001252005030800125CE 2005 3 8 DJFA2004037 120041124A561010138402523 WINDSHIELD BEECH 200 B200 1152922CE COCKPIT CRACKED E DJFAA UNSCHED LANDING O OTHER CRCRUISE 1 EA23615TA BB1745 CREW REPORTED, THE PILOTS SIDE WINDSHIELD SHATTERED AT FL250. NORMAL LANDING WAS PERFORMED AT KBED. MAINTENANCE REMOVED AND REPLACED THE PILOTS SIDE WINDSHIELD. WINDSHIELD LEAK CHECK AND HEATING CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T A24CE 20050308001262005030800126EA 2005 3 8 COMA0460656 120041201A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01918CA 7018 FLIGHT 5173 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050308001272005030800127 2005 3 8 ERAA098185 420040921A34165035P2P25 WIRE SKRSKYS76 S76A 8143006NE ALTIMETER BROKEN A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03577EH 760222 INDICATES 200 FEET OFF. CONFIRMED ENCODING OUTPUT OFF. REPLACED BROKEN WIRE SHROUD AND STEM SEAL. RESET GEAR MESH, CLEANED AND CALIBRATED. UNIT THEN FUNCTIONALLY TESTED GOOD TO 20,000 FEET PER FAR 43E (B). 1G72 3U H1NE 20050308001302005030800130SW 2005 3 8 ERAA098187 120040331A6321412010123101 BUSHING BELL 412 412 1182202SW ROTOR BRAKE VIBRATION B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03167EH5890 33089 ROTOR BRAKE QUILL HAS VIBRATION AND BEARING PLAY. BEARINGS SPINNING IN SLEEVE LINER, SPACER SET DAMAGED, BEARING RETAINER PLATE SCRAPPED. DISASSEMBLED, CLEANED AND VISUALLY INSPECTED ALL PARTS. INSPECTED, REPAIRED AND REASSEMBLED IAW BHT 412 CR/O CH 63. INSTALLING NEW SLEEVE, NEW RETAINER PLATE, NEW SEAL NEW O-RINGS AND NEW SPACER SET. TORQUED AND SAFTIED AS REQUIRED. 1G72 4U H4SW 20050308001312005030800131EU 2005 3 8 ERAA098194 120040917A3212D24762101 FLOAT BOLKMS105 BO105S 5626006EU MLG DELAMINATED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03129EH 580 DELAMINATION AT AFT COMPARTMENT TOPPING OFF VALVE FOUND LEAKING VALVE AND 2 HOLES. REPAIRED IN A/W AC 25-60-95. FOUND BAG TO BE SERVICEABLE. 1G72 3U H3EU 20050308001322005030800132EU 2005 3 8 ERAA098195 120040622A2842VT044 TRANSMITTER BOLKMS105 BO105S 5626006EU FUEL QUANTITY CRACKED B ERAAO OTHER N FALSE WARNING NRNOT REPORTED 1 AL03133EH 598 FUEL PROBE FLOAT STICKS. FOUND CASE CRACKED. REPLACED CASE ASSY. UNIT THEN FUNCTIONALLY TESTED GOOD. 1G72 3U H3EU 20050308001342005030800134SW 2005 3 8 ALGA098163 120041118A6320406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03937AL702 53383 BINDING AND AXIAL PLAY BEYOND MAX. REPLACED W/NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050308001362005030800136SW 2005 3 8 ALGA098167 120041123A6230406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03457AL393 53151 EXCESSIVE AXIAL PLAY AND BINDING. REPLACED W/NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050308001372005030800137SW 2005 3 8 ALGA098168 120041027A6230406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBEO744 23190 BINDING AND AXIAL PLAY BEYOND MAX. REPLACED W/NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050308001402005030800140EU 2005 3 8 DHL2004364017 120041119A3240C200601004 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG BINDING A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01364DH 141 EXCESSIVE BREAKAWAY THRUST REQUIRED TO MOVE AIRCRAFT NR 3 BRAKE ASSY, REMOVED. FOUND NR 3 BRAKE BOUND. REMOVED NR 3 BRAKE ASSY PER MM 32-00-00 AND 32-42-27 XFER TO DMI 18528 PER MEL 32-42-09-1, CAT C. NR 3B RAKE ASSY REMOVED. INSTALL SERVICEABLE BRAKE ASSY AS PER MM 32-42-27. 2L72 4F RTA35EU 20050308001412005030800141NM 2005 3 8 HALA0401073 120041118A2711 TRIM SYSTEM BOEING767 76733A 1385209NM PWA 4060 PW4060 52119NE AILERON BINDING A HALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 WP13581HA 28141 AILERONS ARE VERY HEAVY. AILERON TRIM IS ERRATIC, FEELS LIKE SYSTEM IS BINDING. REPAIR IN WORK. (WP09200500753) AIRCRAFT OUT OF SERVICE. 2L72 4F4 FRTA1NM E24NE 20050308001422005030800142CE 2005 3 8 DJFA2004039 120041205A2120 ODOR BEECH MU300 400A 1155402CE CABIN DETECTED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA23799TA RK209 CREW REPORTED THAT THE CABIN HAD FILLED WITH AN ELECTRICAL OR ENVIRONMENTAL SMELLING SMOKE. AIRCRAFT HAD DIVERTED TO KSAV. MAINTENANCE RAN BOTH ENGINES AND OPERATED THE ENVIRONMENTAL CONTROL SYSTEM. THE FREON AIR CONDITIONING SYSTEM WAS ALSO RAN. NO SMOKE NOR ELECTRICAL SMELL COULD BE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050308001432005030800143NE 2005 3 8 ALG2004F00074 120041030A5302 PYLON SKRSKYS76 S76C 8143008NE TAILBOOM CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03864AL 760557 ON A DAILY SERVICE CHECK, FOUND 4 INCH CRACK ON LT SIDE FOR VERTICAL PYLON, UPPER FORWARD CORNER OF THE INSPECTION PANEL AT VS STATION 123.071. MAINTENANCE REPAIRED THE CRACK IAW S76 SRM. 1G72 3U NCH1NE 20050308001462005030800146EU 2005 3 8 MALA040732 120041118A2612472326 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL15447XJ 340B447 LT FIRE DETECT FAIL LIGHT ON CWP ILLUMINATED SEVERAL TIMES THEN WENT OUT. MAINTENANCE REPLACED NACELLE SENSING FIRE LOOP (AFT) PN 472326 IAW SAAB AMM 26-11-05-2. OPS CHECK GOOD. 2L72 4T RTA52EU 20050308001472005030800147EU 2005 3 8 MALA040736 120041126A3097660714263 LEAD SAAB SF340 340B 7860101EU PROP DEICE SYS OPEN A MALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL15402XJ 340B402 RT PROP HEAT CAUTION LIGHT ILLUMINATES 40 SECONDS IN NORMAL AND 10 SECONDS IN MAX. AIR RETURN TO MSP. MAINTENANCE CLEANED BRUSH BLOCK, RAN AC OPS CK GOOD. MAINTENANCE FOUND PROP DE-ICE LEADS AT PROP BLADES 1 AND 3 TO HAVE OPEN LEADS. REPLACED DE-ICE LEADS PN 660714263 AS PER SAAB AMM RAN AC FOR 15 MIN, OPS CHECKS GOOD. 2L72 4T RTA52EU 20050308001492005030800149EU 2005 3 8 MALA040743 120041130A21507769106 ACM SAAB SF340 340B 7860101EU LEFT MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15442XJ 340B442 LEFT TEMP UNCONTROLABLE IN AUTO OR MANUAL. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED LEFT ACM IAW J/C 215181, OPS CHECK GOOD PN 776910-6 SN ON 911231 OFF 9803193. 2L72 4T RTA52EU 20050308001502005030800150GL 2005 3 8 UIEA200400199 220041207A7261 B-NUT BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 1 ENGINE LOOSE A UIEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15412MC 30559 EICAS MESG; ENGINE NR 1 OIL PRESSURE. CONFIRMED OIL PRESSURE BELOW 10 PSI. SHUTDOWN NR 1 ENGINE. CONFIRMED NR 1 ENGINE OIL QTY LOW, AND ON INSPECTION FOUND B-NUT LOOSE FROM OIL TUBE CONNECTED TO FRONT OF MAIN GEAR BOX AT 6 O’CLOCK POSITION. SERVICED ENGINE OIL TO FULL AND SECURED B-NUT IAW MM 79-10-00. PERFORMED INSPECTION ON MAIN OIL SCREEN, CHIP DETECTOR AND SCAVENGE SCREEN IAW MM 79-21-06 AND MM 79-21-04 NO CONTAMINATION FOUND. PERFORMED WINDMILL INSPECTION IAW MM 72-00-00, PAGE 206. NO DEFECTS NOTED. PERFORMED HIGH POWER RUN UP, ALL INDICATIONS NORMAL. REINSPECTED ALL SCREENS, ALL NORMAL. 2L74 4F4 FRT1384945 E23EA 20050308001512005030800151EU 2005 3 8 MALA040739 120041124A2750 CONTROL SYSTEM SAAB SF340 340B 7860101EU TE FLAPS MALFUNCTIONED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15417XJ 340B417 INFLIGHT FLAPS SELECTED TO 15 DEGREES. FLAPS REMAINED AT ZERO. PER QRH LANDED HIGHSPEED ZERO FLAPS ON GROUND. FLAPS DID MOVE AS COMMANDED. MAINTENANCE PERFORMED FLAP OPERATIONAL TEST AND FOUND NO FAULT AT THIS TIME. 2L72 4T RTA52EU 20050308001522005030800152NM 2005 3 8 GAIA04174AOP 120041129A5330 SKIN BOEING727 727223 1384074NM PWA JT8 JT8D9A 52048NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07856AA 20997 NO FLIGHT: DURING WALK AROUND, A LARGE DENT WAS FOUND ON THE LT SIDE OF THE NOSE OF THE AIRCRAFT BELOW THE L2 WINDOW. THE AIRCRAFT WAS FERRIED FOR REPAIR. 2L73 4F4 F A3WE E2EA 20050308001532005030800153EU 2005 3 8 MALA040731 120041114A3230 UPLOCK TARGET BAC 146 AVRO146RJ85A1500097EU MLG LOOSE A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15504XJ E2311 LEFT MAIN GEAR INTRANSIT LIGHT ILLUMINATED ALONG WITH GEAR INTRANSIT LIGHT. A/C DIVERTED TO MSP AND CONTINUED TO MEM IN A/C 516. A/C DIVERTED TO MSP. MAINTENANCE FOUND TARGET LOOSE ON LT MAIN GEAR UPLOCK SWITCH. RESECURED TARGET PERFORMED OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION IAW AMM 32-30-00. OPS CHECK GOOD. 2H74 4F RTA49EU 20050308001542005030800154NM 2005 3 8 DHL2004753004 120041208A33501000677 LIGHT BOEING727 727223 1384074NM CABIN INOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01753DH 22468 EMERGENCY LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CK NORMAL IAW MM 33-50-11. 2L73 4F A3WE 20050308001552005030800155EA 2005 3 8 COMA0460664 120041206A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG UNRELIABLE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01959CA4818 7116 FLIGHT 5107 - STEERING INOP CAUTION DURING T/O. REPLACED THE NLG PRIORITY VALVE. 2L72 4F RTA21EA 20050308001562005030800156EA 2005 3 8 COMA0460666 120041202A2750860D10018ABCD CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01977CA15961184 7157 FLIGHT 5028 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20050308001592005030800159NM 2005 3 8 GAIA04177OP 120041207A3610 CLAMP BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 ENGINE BROKEN A GAIAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW07279US 21158 DURING CLIMB, NR 2 ENGINE FIRE WARNING AFTER TAKEOFF. SHUT DOWN NR 2 ENGINE. RETURNED TO AIRPORT. DECLARED EMERGENCY. LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN CLAMP ON 8TH STAGE SADDLE DUCT AT THE ANTI-ICE CONNECTION. REPLACED CLAMP. LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20050308001602005030800160NM 2005 3 8 GAIA04176OP 120041207A2424902F2425 GCU BOEING727 727251 138408HNM PWA JT8 JT8D7B 52053NE NR 3 MALFUNCTIONED A GAIAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC APAPPROACH 1 SW07252US 19971 DURING APPROACH, LOST ALL (REMAINING, NR 2 AND NR 3) GENERATORS IN FLIGHT DURING APPROACH. RESET NR 2 GEN. NO VOLTAGE OR FREQS. ON NR 3, UNABLE TO RESET. FAULT PANEL INDICATED NR 3 SYSTEM UNDER VOLTAGE. LANDING WAS MADE WITHOUT INCIDENT. SWAPPED NR 3 GCU AND APU GCU. OPS CHECK OF BOTH SYSTEMS SATISFACTORY IAW MM. AIRCRAFT WAS RETURNED TO SERVICE. (NOTE: NR1 PREVIOUSLY DEFERRED). 2L73 4F4 F A3WE E2EA 20050308001612005030800161CE 2005 3 8 RU3A0420 120041203A5714602240111 SPLICE PLATE LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE CENTER WING LEAKING E RU3AO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW1555 4619 013 CREW REPORTED SMELL OF FUEL IN AFT CABIN AT ALTITUDES OF 2500 FT AND BELOW IN LEVEL FLIGHT. IT WAS ALSO NOTICEABLE ON GROUND. IT WAS LESS NOTICEABLE AT HIGHER ALTITUDES AND UNDER PRESSURIZATION. MAINT LOCATED SOURCE OF SMELL. FWD WING CENTERLINE SPLICE PLATE (PN 602240111) WAS SEEPING FUEL PAST RIVETS. SPLICE IS LOCATED JUST AFT OF CABIN PRESS POPPET VALVES, WHICH ARE FOUND AT END OF CABIN AISLE WALKWAY. WHEN AC WAS AT ALTITUDE, POPPET VALVES WERE HELD CLOSED BY CABIN PRESSURE, BUT AS AC DESCENDED (2500 FT AND BELOW) CABIN PRESSURE DECREASED ALLOWING POPPET VALVES TO OPEN AND PERMIT JET FUEL FUMES TO ENTER CABIN. TECH RECOMMENDS TO DEMATE WING FROM FUSELAGE, REPAIR LEAKS AND REMATE WING. AC IN REPAIR. 2L72 4F4 FRTA10CE E35NE 20050308001622005030800162NM 2005 3 8 C8GA20040026 120041214A2420SCN001 CONNECTOR BOEING727 7272A1 138407FNM NR 2 GENERATOR LOOSE A C8GAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO15286SC52070 21601 FLT 737 FROM GDL TO MTY, ON TAKEOFF ROLL, NR 2 GENERATOR SHOWED UNDERVOLTAGE WITH ASSOCIATED THREE LIGHT TRIP. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. DEFERRED NR 2 GENERATOR UNDER MEL 24-1. AIRCRAFT RETURNED TO SERVICE. TWO LEGS LATER IN TOL, CLEANED AND RESECURED CONNECTORS ON NR 2 LOAD CONTROLLER AND GENERATOR PROTECTION PANEL. OPS CHECK GOOD. MEL CLEARED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20050308001632005030800163CE 2005 3 8 RK267001 120041213A282345AS480025 FLOW VALVE BEECH MU300 400A 1155402CE FUEL SYSTEM INOPERATIVE E ERYAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE074467X1135 RK267 DURING CRUISE, RT JET PUMP LIGHT ON CROSSFEED PANEL ILLUMINATED. DIVERTED, AND LANDED UNEVENTFULLY AT APA. 2H72 4F RTA16SW 20050308001642005030800164EU 2005 3 8 MALA040819 120041102A5313 RIB SAAB SF340 340B 7860101EU FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED 612BR 1 CRACKED RIB, REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 126346 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2L72 4T RTA52EU 20050308001652005030800165EU 2005 3 8 MALA040812 120041019A5320 FLOOR SUPPORT SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 DURING 4K INSPECTION IN LAN, MAINTENANCE NOTED FLOOR BOARD SUPPORT ANGLE CORRODED BEWEEN STA 236.5 & 258.0. REPLACED IAW SAAB SRM 51-40-21. REFER TO NRC NR 196553 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2L72 4T RTA52EU 20050308001662005030800166EU 2005 3 8 MALA040821 120041102A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15450XJ 340B450 DURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE NOTED LT AISLE FWD SEAT TRACK CORRODED LBL18.5 STA 294-326, REPAIRED IAW SAAB SRM 53-70-62. REFER TO NRC NR 126704 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/03/04. 2L72 4T RTA52EU 20050308001692005030800169SW 2005 3 8 ALGA098476 120041210A6510407340339107 BEARING BELL 407 407 1182206SW TAIL ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL1134 53240 FAILED VIBRATION CHECK. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050308001702005030800170EA 2005 3 8 REXA04038 120041124A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING MALFUNCTIONED A REXAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SO258908D5157 7908 FLAPS FAILED ON CLIMB OUT FROM DSM QRH FOLLOWED CONTINUED WITH UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD98-20-01. 2L72 4F4 FRTA21EA E15NE 20050308001722005030800172 2005 3 8 REXA04039 420041202A2562C4062 ELT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258877A2419 7877 ELT FAILS G-SWITCH TEST DURING 12-MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2L72 4F4 FRTA21EA E15NE 20050308001732005030800173SW 2005 3 8 ALGA098480 120041210A6510407340339107 BEARING BELL 407 407 1182206SW TAIL ROTOR VIBRATION B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL824 53240 FAILED VIBRATION CHECK. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050308001742005030800174 2005 3 8 REXA04040 420041202A2562C4062 ELT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258886A2252 7886 ELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2L72 4F4 FRTA21EA E15NE 20050308001762005030800176SW 2005 3 8 ALGA098355 120041210A6410206016201131 BLADE BELL 206 206L1 1182107SW TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW038WH 459 45318 REPORTS OF CRACKS AND DEFORMATION IN SKIN AND WEIGHTS, SENT TO RBI TO CW AD 2004-24-08. 1G71 3U H2SW 20050308001772005030800177 2005 3 8 UIEA200400200 420041207A34182566A30A SENSOR BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE STALL WARNING FAILED A UIEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15540MC 22508 IMMEDIATELY AFT T/O, STALL WARNING, STICK SHAKER ACTIVATED ASSOCIATED WITH STALL WARNING. (POWER OFF) LIGHT ILLUMINATION ON PILOTS OVERHEAD PANEL. REMOVED AND REPLACED LT ANGLE OF ATTACK SENSOR. OPS CHECK NORMAL IAW MM. 2L74 4F4 F A20WE E23EA 20050308001782005030800178NM 2005 3 8 LCQ200503 120041221A5330 DOUBLER BOEING737 737522 138449FNM FUSLEAGE DAMAGED B K NONE O OTHER ININSP/MAINT 1 SW15945UA 26684 DOUBLER HAS OVERSIZED FASTENERS AND BLIND RIVETS AFT RT FUSELAGE APPROX STA 1121 S-17 AND S-18R. REF NR 23679 2L72 4F RTA16WE 20050308001812005030800181NM 2005 3 8 LCQ20053 120041221A5510 SKIN BOEING737 737 UTILSYSNM FUSELAGE DENTED B K NONE O OTHER ININSP/MAINT 1 SW15945UA 26684 DENTS IN LT HORIZ STAB L/E SKIN HS 110. REF NR 23435, S/O 269001. 2L72 4F RTA16WE 20050308001822005030800182NM 2005 3 8 2004UALA01187 120041209A5210131W1151 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE R4 DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29209UA 30215 DOOR 4R HAS 2 EA DENTS ON EXT SKIN AT BOTTOM EDGE. DOOR SKIN ON PASSENGER ENTRY DOOR (PED) WAS FOUND DAMAGED. THE DAMAGE CONSISTED OF TWO DENTS AT THE LOWER DOOR EDGE. THE DAMAGE WAS REPAIRED PER SRM. MAJOR REPAIR ACCOMPLISHED. 2L72 4F4 FRTT0001SE E46NE 20050308001852005030800185 2005 3 8 TSAA0425082 420041217A2565D31355427 SLIDE BOEING737 7372T4 1384492NM FWD SVC DOOR DEPLOYED A TSAAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP13807AL 23443 DURING GROUND MAINTENANCE, GROUND CREW INADVERTENTLY DEPLOYED THE FORWARD SERVICE DOOR ESCAPE SLIDE. NO INJURIES. REMOVED AND REPLACED THE FORWARD SERVICE DOOR SLIDE IN ACCORDANCE WITH MM 25-61-200. 2L72 4F A16WE 20050308001862005030800186NM 2005 3 8 C7WA200400039 120040211A291010605634 HYDRAULIC LINE BOEING727 7272J0 138407ENM PWA JT8 JT8D7B 52053NE HYDRAULIC SYS CHAFED A C7WAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO17902PG 20725 AT FLIGHT LEVEL 20.0 A-SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. REPLACED CHAFED HYDRAULIC HOSE AT NR 2 ENGINE DRIVEN HYDRAULIC PUMP OPERATIONAL AND LEAK CHECK NORMAL. 2L73 4F4 FRTA3WE E2EA 20050308001882005030800188CE 2005 3 8 122304N338CS1 120041222A3260 SENSOR CESSNA500 550 2076604CE MLG CONTAMINATED E Z5FAO OTHER J WARNING INDICATION LDLANDING 1 NE03338CS 5501084 DURING APPROACH GEAR WAS SELECTED DOWN AND THERE WAS NO DOWN AND LOCKED INDICATION FOR RT MAIN GEAR. CREW DECLARED AN EMERGENCY AND BLEW THE GEAR DOWN AS A SAFETY PRECAUTION. LANDING WAS NORMAL BUT THERE NEVER WAS A GREEN INDICATION FOR THE RT GEAR. SUSPECT ICE AND SNOW BUILD UP PRIOR TO DEPARTURE CAUSED PROBLEM. GROUND TROUBLESHOOTING FOUND NO FAULT WITH INDICATING SYSTEM. 1L72 4F A22CE 20050308001902005030800190 2005 3 8 TSAA0434084 420041222A34142083081 INDICATOR BOEING737 737282 13844ATNM AIRSPEED INOPERATIVE A TSAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP13824AL 23045 FLT 220, HNL-OGG: FIRST OFFICE AIRSPEED INDICATOR INOP. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MACH AIR SPEED INDICATOR. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050308001952005030800195SW 2005 3 8 HEEA098567 120041204A7931222375077113 TRANSMITTER BELL 430 430 1182150SW NR 2 ENG OIL FLUCTUATES B HEEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW03430XM 49073 INFLIGHT THE NR 2 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 131-132 PSI. RETURNED TO GRAND AISLE. MAINTENANCE REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER. 1G72 3U RTH9SW 20050308001972005030800197NE 2005 3 8 HEEA098568 120041130A6340 TRANSMITTER SKRSKYS76 S76C 8143008NE M/R GEARBOX FLUCTUATES B HEEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW03478X 760493 DURING CLIMB-OUT, MAIN GEARBOX PRESSURE FLUCTUATED FROM GREEN TO YELLOW RANGE THEN DROPPED TO ZERO. MAINTENANCE CLEANED THE CANNON PLUG CONNECTING TO THE TRANSMISSION OIL PRESSURE TRANSMITTER. 1G72 3U NCH1NE 20050308001982005030800198NM 2005 3 8 C7WA200400053 120041011A5315 FLOORBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO177635U 19908 FLOORBEAM AT BS 660 RBL 45.50 HAS LIGHT CORROSION. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 660, RBL 45.50. REMOVED DAMAGED CHORD PORTION, FINAL TRIM OUT WAS 2.00 INCH. FABRICATED REPAIR SECTION FROM ALUM 7075-0 X 0.090 INCH X 16 INCHES. HEAT TREATED TO T6 IAW BAC5602. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. FLOORBEAM REPAIR ACCOMPLISHED IAW SRM. 2L73 4F4 F A3WE E2EA 20050308001992005030800199NM 2005 3 8 TSAA0429085 120041228A7830 LINE BOEING737 737230 1384401NM THRUST REVERSER LEAKING A TSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13821AL 23155 FLT 46, HNL-ITO: HYDRAULIC FLUID QUANTITY DECREASING DURING GEAR RETRACTION. RETURNED TO HNL. UNEVENTFUL LANDING. WHILE ON GROUND, HYDRAULIC FLUID QUANTITY CONTINUED TO DECREASE SLOWLY. MAINTENANCE FOUND LEAKS AT THE NR 2 THRUST REVERSER LINE AND NR 4 SPOILER OUTBOARD ACTUATOR LINE AND B-NUT. REMOVED AND REPLACE THE NR 2 TR HYDRAULIC LINE. OPS AND LEAK CHECK OK. REMOVED AND REPLACED THE HYDRAULIC LINE AND B-NUT ON THE NR 4 SPOILER OUTBOARD ACTUATOR. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050307000702005030700070SO 2005 3 7 CHQA200400574 120041027A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11265SK 145226 EMERGENCY EXIT LIGHT OVER LT WING IS INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10-4. OPS CHECK GOOD. 2L72 4T RTT00011AT 20050307000712005030700071SO 2005 3 7 CHQA200400550 120040903A33501317 LAMP EMB 135 EMB135LR 3260305SO EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11845RP 145551 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050307002972005030700297SO 2005 3 7 SIMA200432203 120041116A33207281000501 CONTROLLER EMB 135 EMB135LR 3260305SO CABIN MALFUNCTIONED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21718AE 145275 CAPTAIN REPORTED STRONG ODOR OF BURNED PLASTIC FROM FLIGHT ATTENDANT GASPER AND FROM CABIN LIGHTS CONTROL MODULE. ALSO, LIGHTS FLICKERING THROUGHOUT THE CABIN. REPLACED CABIN LIGHT CONTROLLER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050307003332005030700333NM 2005 3 7 ASAA0470041S 120041105A5320146A75068 FLOOR SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON FLOOR SUPPORT AT STA 775. REPAIRED IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050307003352005030700335NM 2005 3 7 ASAA0470032 120041104A5330147A310019 SKIN BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND GOUGES IN FUSELAGE APPROX 4 FT FWD OF R-2 DOOR 1.75, 1.25. REPAIRED IAW SRM 53-00-01. (K) 2L72 4F4 FRTA16WE E00055EN 20050307003372005030700337WP 2005 3 7 ASAA0480548 120041030A21505924037513 DIVERTER DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ACM CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK- RT ACM(AIR CYCLE MOTOR) DIVERTER IS CHAFED AND CRACKED. REMOVED DAMAGE, WELDED IN FILLER REPAIR IAW EA. 2L72 4F4 FRTA6WE E9NE 20050307003422005030700342WP 2005 3 7 ASAA0480554 120041101A25603753213143 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE L2 DOOR DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 PRE-FLIGHT CHECK- AFT SERVICE (L-2) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2L72 4F4 FRTA6WE E9NE 20050307003462005030700346NM 2005 3 7 ASAA0410685 120041130A53206546570 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON AFT LAV FLOOR WEB. REPAIRED WEB (K) 2L72 4F4 FRTA16WE E2EA 20050307003512005030700351WP 2005 3 7 ASAA0480580 120041130A531359360481 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-LONGERON 28R IN AFT CARGO BAY AREA IS CORRODED. REPLACED DAMAGED SECTION.(K) 2L72 4F4 FRTA6WE E9NE 20050308000972005030800097NM 2005 3 8 ASAA0410580 120041122A53306545767541 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - GOUGES IN SKIN AT BOTTOM OF MAIN CARGO DOOR CUTOUT. REPAIRED IAE EA.(K) 2L72 4F4 FRTA16WE E2EA 20050308001082005030800108WP 2005 3 8 ASAA0480570 120041118A5320591479243 PAN DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE AFT FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - AFT LAV SERVICING PAN IS CORRODED. REPLACED SERVICING PAN.(K) 2L72 4F4 F A6WE E9NE 20050308001232005030800123SO 2005 3 8 OIK2004F00000 120041018A52804665300 HINGE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2A GL RT MLG DOOR BROKEN E OIKAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP13500SA 317552056 RL199568A DJ11173A ON 10/17/04, APPROXIMATELY 12:30 PM, DURING CRUISE, PILOT NOTICED THE LANDING GEAR UNLOCK LIGHT ILLUMINATED. PILOT RETURNED TO AIRPORT. UPON POST FLIGHT INSPECTION, THE RT MAIN GEAR IB DOOR HINGES WERE FOUND BROKEN. (WP13200505092) 1L72 3O3 O A20SO E14EA 5 CP33EA 20050308001442005030800144EU 2005 3 8 MALA040730 120041114A3233SIT864102 ACTUATOR SAAB SF340 340B 7860101EU MLG FAILED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15411XJ 340B411 RT MAIN LANDING GEAR TAKES A VERY LONG TIME TO SHOW A DOWN LOCKED INDICATION AFTER LANDING DEPLOYMENT. MAINTENANCE REMOVED AND REPLACED RT MLG ACTUATOR PN AIR86410-2, SN/OFF LK9601076, SN/ON LK9701575 IAW SF3 AMM 32-21-20-4. 2L72 4T RTA52EU 20050308001482005030800148EU 2005 3 8 MALA040745 120041129A214013051002 HEATER SAAB SF340 340B 7860101EU CABIN ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15429XJ 340B429 AUX HEAT HAS BURNING SMELL COMING FROM FWD HEATER BOX. DEFERRED AUX HEATERS PER MEL 21-40-1 (D). MAINTENANCE REPLACED AUX HEATER PN 1305100-2, SN/OFF 533, SN/ON 518. IAW MM CHAP 21. REMOVED FROM DMR, MXC NOTIFIED. 2L72 4T RTA52EU 20050308001682005030800168 2005 3 8 REXA04036 420041105A2562C4062 ELT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO258709A4625 7709 ELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207. 2L72 4F4 FRTA21EA E15NE 20050308001962005030800196NM 2005 3 8 C7WA200400052 120041011A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO177635U 19908 NR 3 RT COCKPIT WINDOW UPPER SKIN (EXTERIOR) HAS AN APPROXIMATELY 1 INCH CRACK. INSTALLED EXTERNAL SKIN REPAIR ON RT NR 3 WINDOW UPPER SKIN. REMOVED DAMAGED SKIN PORTION. SKIN TRIM OUT 4.00 X 5.00. FABRICATED AND INSTALLED REPAIR FILLER PLATE FROM 2024-T3 X .040 X 4.00 X 5.00. FABRICATED AND INSTALLED DOUBLER FROM 2024-T3 X .080 X 15 INCH X 15 INCH. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. REPAIR ACCOMPLISHED IAW SRM. 2L73 4F4 F A3WE E2EA 20050308002012005030800201NM 2005 3 8 C7WA200400055 120041011A5310 SHEAR TIE BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A C7WAK NONE O OTHER ININSP/MAINT 1 SO177635U 19908 SHEAR TIE CRACKED AT FRAME STA 930 BETWEEN STRINGER 13 RT AND STRINGER 14 RT. INSTALLED INTERNAL REPAIR ON SHEAR TIE AT BS 930 BETWEEN STRINGER 13 RT AND 14 RT. DAMAGED SHEAR TIE REMOVED. REPAIR PART FABRICATED FROM 7075-T6, X .063. REPAIR PARTS AND BARE EDGED TREATED IAW SRM. REPAIR ACCOMPLISHED IAW SB. 2L73 4F4 F A3WE E2EA 20050308002022005030800202NM 2005 3 8 C7WA200400056 120041011A5315 FLOORBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO177635U 19908 TRAVERSE FLOORBEAM STA 720 HAS CORROSION BETWEEN BL0 AND LBL 24.5. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 720A, BETWEEN BL0.0 AND LBL 24.5. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIMENSION WAS 6.00 INCH X 2.00 INCH. REPAIR SECTION FABRICATED FROM BAC 1505-100617 X 7075-T73. REINFORCEMENT ANGLE FABRICATED FROM ALUM. 7075-0 X 0.090 X 14 INCH X 4 INCH, AND ALUM 7075-0 X 0.050 INCH X 21 INCH X 4 INCH, HEAT TREATMENT TO T6 IAW BAC 5602. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. FLOORBEAM REPAIR ACCOMPLISHED IAW SRM. 2L73 4F4 F A3WE E2EA 20050308002032005030800203NM 2005 3 8 C7WA200400057 120041011A5315 FLOORBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO177635U 19908 FLOOR TRAVERSE BEAM AT STA 600 HAS LIGHT CORROSION BETWEEN BL0 AND RBL 24.5 AND BETWEEN LBL 45.5 AND LBL50. INSTALLED INTERNAL FLOORBEAM REPAIR ON DAMAGE LOCATED AT BS 600 BETWEEN BL0 AND LBL 24.50. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIMENSION WAS 1.50 X 1.00. REINFORCEMENT ANGLE FABRICATED FROM ALUM. 7075-0 X 0.090 INCH X 14 INCH X 7 INCH, AND ALUM 7075-0 X 0.090 X 18 INCH X 7 INCH, HEAT TREATMENT TO T-6 IAW BAC 5602. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. FLOORBEAM REPAIR ACCOMPLISHED IAW SRM. 2L73 4F4 F A3WE E2EA 20050308002082005030800208WP 2005 3 8 ASAA0480544 120041030A575399359543 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE T/E FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK- RT IB FLAP LOWER SURFACE IS DENTED 11.5 INCHES FROM T/E AND 19.25 INCHES FROM IB FAIRING SEAL. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER IAW SRM. 2L72 4F4 FRTA6WE E9NE 20050308002112005030800211WP 2005 3 8 ASAA0480546 120041030A575359100403 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE T/E FLAP VANE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK- RT IB FLAP VANE HAS DELAMINATION ON LOWER SURFACE. REMOVED DAMAGED SECTION, AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM. 2L72 4F4 FRTA6WE E9NE 20050308002122005030800212GL 2005 3 8 ALG2005F00000 220041202A7200 ENGINE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 1 MAKING METAL E ALGAO OTHER J WARNING INDICATION CRCRUISE 1 SW03522AL 760236 NR 1 ENGINE CHIP LIGHT ILLUMINATED IN CRUISE FLIGHT, COMPLIED WITH CHECKLIST PROCEDURES AND CONTINUED TO AIRPORT. MAINTENANCE REMOVED 2 EA CHIP PLUGS FOUND ONE TINY SLIVER ON FORWARD PLUG AND SMALL CARBON ON AFT PLUG. DRAINED AND RESERVICED OIL SYSTEM, CHECKED BOTH CHIP PLUGS AFTER 30 MINUTE GROUND RUN , NO DEFECTS NOTED. (K) 1G72 3U3 U H1NE E1GL 20050308002162005030800216NM 2005 3 8 UIEA200400205 120041227A551265B0352133 FAIRING BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE LT HORIZ STAB MISSING A UIEAK NONE O OTHER ININSP/MAINT 1 EA15536MC 21576 ON WALK AROUND CHECK, FOUND LT AFT TIP FAIRING OF HORIZONTAL STABILIZER MISSING. EO ISSUED TO ACCOMPLISH TIME-LIMITED REPAIR WORK TO BE DONE PRIOR TO FURTHER FLIGHT. FABRICATED A TIME LIMITED REPLACEMENT FAIRING FROM 0.040 INCH THICK 2024-T3 CLAD SHEET. PERMANENT REPAIR TO BE ACCOMPLISHED IAW EO WITH IN 25 FLIGHT CYCLES. (K) 2L74 4F4 F A20WE E23EA 20050308002172005030800217NM 2005 3 8 UIEA200400206 120041227A521065B100034 MECHANISM BOEING747 7472D7B 1384803NM GE CF6 CF650E2 30018NE L1 DOOR BROKEN A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15522MC 21783 AFTER TAKEOFF AT APPROX 2,500 FT, THE LT ENTRY DOOR (L1) DOOR LIGHT CAME ON. ACCOMPLISHED CHECK LIST. THEN HEARD A LOAD NOISE WITH AIRCRAFT PRESS CLIMBING. RETURNED TO SFO. AFTER LANDING, FOUND DOOR LOCKING LUG BROKEN OFF. ACCOMPLISHED DETAILED INSPECTION OFF L1 DOOR MM. REPLACED UPPER AND LOWER AFT LATCH ROLLER CRANKS. ACCOMPLISHED ADJUSTMENT CHECK AND LEAK CHECK OF L1 DOOR. PERFORMED PRESSURE CHECK OF L1 DOOR. PRESSURE CHECK GOOD. 2L74 4F4 FRTA20WE E23EA 20050308002182005030800218EU 2005 3 8 KBM2005F00001 120041205A74109550178290 SOLENOID VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE UNSERVICEABLE E KBMAO OTHER X ENGINE FLAMEOUT ININSP/MAINT 1 WP19313LV 3696 FLAMED OUT DURING VIBRATION TEST. REPLACED IGNITION SOLENOID WITH SERVICEABLE UNIT AS NEEDED. 1G71 3U3 U H9EU E19EU 20050308002192005030800219NM 2005 3 8 C7WA200400071 120041210A278226900297L ACTUATOR BOEING727 7272Q6 138407VNM PWA JT8 JT8D17R 52049NE L/E SLAT LEAKING A C7WAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO171279E 21971 AIR RETURN; AFTER TAKEOFF AND FLAP RETRACTION SYSTEM (A) HYDRAULIC QUANTITY WAS DROPPING RAPIDLY. ACCOMPLISHED ABNORMAL PROCEDURE FOR LOSS OF SYSTEM (A) QUANTITY. FOUND NR 1 SLAT ACTUATOR LEAKING. REMOVED AND REPLACED SLAT ACTUATOR IAW MM. (K) 2L73 4F4 FRTA3WE E2EA 20050308002212005030800221NM 2005 3 8 UIEA200400202 120041217A2720AV16E12154 SHUTOFF VALVE BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE RUDDER LEAKING A UIEAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA15516MC 22507 DURING CRUISE, LOSS OF FLUID NR 4 HYD SYSTEM. SYSTEM DEPRESSURIZED AT 2.0 GALS QUALITY. EDP TO SUPPLY OFF. FOUND NR 4 RUDDER CONTROL SHUTOFF VALVE FAILED. (LEAKED) REMOVED AND REPLACED NR 4 RUDDER SHUTOFF VALVE. OPS AND LEAD CHECK GOOD IAW MM. (K) 2L74 4F4 F A20WE E23EA 20050307002992005030700299SO 2005 3 7 SIMA200434201 120041205A335020131A BATTERY EMB 135 EMB135LR 3260305SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21709GB 145211 RDU - FLT 4673 - AFT EMERGENCY LIGHTS DIM OUT DURING TEST. REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW 33-50-04. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20050307003202005030700320NM 2005 3 7 ASAA0470035S 120041104A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE CARGO BAY DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND NR 2 FLOOR PANEL DAMAGED IN FWD CARGO BAY. REPAIRED IAW SRM 51-30-01.(K) 2L72 4F4 FRTA16WE E00055EN 20050307003222005030700322NM 2005 3 7 ASAA0470038 120041104A5320149A811829 SUPPORT ANGLE BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK FOUND CORROSION ON AFT CARGO PIT BULKHEAD LWR SUPPORT ANGLE AT BS 947. REPAIRED IAW SRM 51-20-02. 2L72 4F4 FRTA16WE E00055EN 20050307003302005030700330WP 2005 3 7 ASAA0480567 120041118A532059360715 INTERCOSTAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - LONGERON 29L INTERCOSTAL IS CORRODED. REPLACED INTERCOSTAL.(K) 2L72 4F4 F A6WE E9NE 20050307003362005030700336WP 2005 3 7 ASAA0480542 120041028A33501001191 LIGHT DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02974AS38650619 53450 LINE CHECK- PORTABLE EMERGENCY LIGHT, SITUATED NEAR THE FORWARD PASSENGER DOOR, IS OPERATIVE. REPLACED LIGHT ASSEMBLY. 2L72 4F4 FRTA6WE E9NE 20050308001162005030800116EA 2005 3 8 HYTA2005003 220041119A7220 SEAL CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA ENGINE INLET LOOSE D HYTAK NONE O OTHER ININSP/MAINT 1 AL01976E 208B0976 FELT SEALING STRIP APPROXIMATELY .5 INCH X 7 INCHES WAS COMING LOOSE FROM INSIDE THE ENGINE INDUCTION AIR PLENUM. OFFENDING FELT STRIP WAS REMOVED AS IT SERVES NO PURPOSE. THIS STRIP WAS LOCATED AT ABOUT 4 O’CLOCK ON THE INSIDE SURFACE ACROSS THE RT END OF THE LOWER PLENUM PANEL PN 2658039-19. LOCATION OF STRIP COINCIDES WITH LOWER END OF ACCESS PANEL PN 2658039-1 WHICH HAS PROPERLY POSITIONED FELT SEALING STRIPS. 1H71 3T3 T A37CE E2NE 20050308001292005030800129WP 2005 3 8 G1I2004F00003 220041114A72618955081 SEAL MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE331* 01514WP LT ENGINE LEAKING G G1IAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL01438663668 757SA SMOKE APPEARED IN CABIN AFTER ROTATION. RETURNED TO SAME AIRPORT. IT APPEARS A COMPRESSOR SEAL LEAK IN THE LT ENGINE ALLOWED TURBINE OIL TO ENTER THE POWER SECTION, BURN AND CREATE ENVIRONMENTAL SMOKE. OIL LEAK WAS DETERMINED TO BE WITHIN ALLOWABLE LIMITS. (AL01200501682) 1H72 3T3 TRTA10SW E2WE 20050308001392005030800139EU 2005 3 8 ALGA098149 120041202A6230C622A1003102 SCISSORS UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03516AL475 1157 PLATE DEBONDED. REPLACED WITH SERVICEABLE SCISSOR. 1G72 3U NCR0001RD 20050308001672005030800167EU 2005 3 8 MALA040811 120041019A5311 FRAME SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15408XJ 340B408 DURING 4K INSPECTION IN LAN, FRAME AT STA 258.0 CORRODED ON LT SIDE. MAINTENANCE REPAIRED IAW SAAB SRM 53-70-30-2. REFER TO NRC NR 196552 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04. 2L72 4T RTA52EU 20050308001752005030800175SW 2005 3 8 ALGA098250 120041125A6220406310405101 BEARING BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03437AL465 53141 BINDING, ROUGH, AND AXIAL PLAY BEYOND MAX. REPLACED W/NEW BY FLT MAINTENANCE. 1G71 3U O H2SW 20050308001912005030800191 2005 3 8 C7WA200400038 420040914A2210GM10323 TRANSDUCER BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE YAW DAMPER INOPERATIVE A C7WAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO178887Z 21856 AIR RETURN: DURING CLIMBOUT UPPER RUDDER DEFLECTED TO FULL RT YAW DAMPER POSITION THEN BEGAN OSCILLATING LT TO RT CONTINUOUSLY. REMOVED AND REPLACED UPPER YAW DAMPER TRANSDUCER. SYSTEM OPERATIONAL CHECKS NORMAL. 2L73 4F4 F A3WE E2EA 20050308001942005030800194NM 2005 3 8 C7WA200400041 120040907A27519660021002 TRANSMITTER BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE T/E FLAP FROZEN A C7WAO OTHER N FALSE WARNING APAPPROACH 1 SO177640U 19913 EXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSMITTER FROZEN. REMOVED AND REPLACED TRANSMITTER AND REPAIRED WIRES AT D224 IB FLAP INDICATOR CONNECTOR OPERATIONAL CHECK GOOD IAW MM. 2L73 4F4 F A3WE E2EA 20050308002002005030800200NM 2005 3 8 C7WA200400054 120041011A5312 BEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CORRODED A C7WAK NONE O OTHER ININSP/MAINT 1 SO177635U 19908 BULKHEAD STA 1183 HAS A 6 INCH CRACK IN THE VERTICAL BEAM AT LBL 24.5, WL 250. INSTALLED INTERNAL REPAIR ON DAMAGED VERTICAL BEAM AT BS 1183 AT LBL 24.50, WL 250. DRILLED STOP HOLE .250. REPAIR CHANNEL 65C33556-45 AND SHIMS INSTALLED IAW SB. REPAIR PARTS AND BARE EDGES TREATED IAW SRM. VERTICAL BEAM REPAIRED IAW SB. 2L73 4F4 F A3WE E2EA 20050308002062005030800206WP 2005 3 8 ASAA0480543 120041030A2497BXS70188 WIRE HARNESS DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CABIN MISROUTED A ASAAK NONE WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM02969AS 53063 SEA BTB NON-ROUTINE LINE CHECK-SPARKS AND SMOKE NOTED COMING FROM OVERHEAD GRILL BETWEEN L1 DOOR AND FORWARD GALLEY. INSP REVEALED THAT A WIRE BUNDLE WAS CHAFING ON A PLENUM DUCT CLAMP, SOME OF THE WIRING WAS SHORTING ON CLAMP, AND HAD BURNED THROUGH 1 FOOT FORWARD OF S3-25 TERMINAL STRIP. IT WAS FURTHER DETERMINED THAT THE WIRING BUNDLE HAD BEEN MIS-ROUTED, AND DUCT CLAMP HAD BEEN IMPROPERLY INSTALLED. REPAIRED DAMAGED WIRING. REROUTED WIRING BUNDLE, ALSO REPLACED PLENUM DUCT AND CLAMP. OPS CHECKED OK. 2L72 4F4 FRTA6WE E9NE 20050308002132005030800213SW 2005 3 8 ALG2005F00001 120041206A2497 WIRE BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL COCKPIT BURNED E ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW033179S 45781 DURING RUN UP, SMOKE OBSERVED COMING FROM UP CIRCUIT BREAKER PANEL, AIRCRAFT SHUT DOWN AND MAINTENANCE WAS NOTIFIED. MAINTENANCE INSPECTED AND FOUND THE DIODE ON THE BATTERY RELAY, SEVERAL WIRES ON BATTERY RELAY BURNED. FURTHER INSPECTION FOUND WIRES GOING UP THE CENTER POST OF WINDSHIELDS WERE ALSO BURNED AND THE BATTERY SWITCH AND GENERATOR SWITCH ARE BURNED. MAINTENANCE IN PROCESS OF REPLACEMENT OF THE WIRES AND SWITCHES. (K) 1G71 3U3 U H2SW E1GL 20050308002402005030800240NM 2005 3 8 UIEA200400207 120041227A561060B100285 WINDSHIELD BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL COCKPIT CRACKED A UIEAO OTHER O OTHER ININSP/MAINT 1 EA15497MC 29258 MAINTENANCE PICKED UP ITEM. CAPTAINS WINDSHIELD CRACKED (L1). REPLACED L1 WINDSHIELD MM. CHECKS OK. (K) 2L74 4F4 FRT1384945 E23EA 20050308002832005030800283NM 2005 3 8 ASA0440365 120041217A5347654681513 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE TORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K) 2L72 4F4 FRTA16WE E21EU 20050308002852005030800285NM 2005 3 8 ASA044402 120041229A5320654587514 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CORROSION FWD GALLEY DOOR CUTOUT (4 EA) THRESHOLD PLATE SUPPORTS. REMOVED AND REPLACED (4 EA) THRESHOLD PLATE SUPPORTS. 2L72 4F4 FRTA16WE E21EU 20050308002892005030800289NM 2005 3 8 ASA0440395 120041228A5210654795978 DOOR FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CORROSION ON DOORSILL FWD FRAME. REPLACED FRAME IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050308002902005030800290NM 2005 3 8 ASA0440357 120041218A532065C35582 WEB BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CANNING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - OIL CANNED WEB. REMOVED FABRICATION AND INSTALLED NEW WEB. (K) 2L72 4F4 FRTA16WE E21EU 20050309000842005030900084WP 2005 3 9 05FDEA00379 120041001A5710ARB07601 CAP DOUG MD10 MD1010F 3022112WP ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25562FE 46947 LEFT WING RIB UPPER CUP CRACK AT XORS 372. TRIMMED OUT CRACKED PORTION AND SPLICE REPAIRED IAW FEDEX EA 8-571-80005. 2L73 4F RTA22WE 20050309000852005030900085WP 2005 3 9 05FDEA00380 120041118A5730ARB08661 DOUBLER DOUG MD10 MD1010F 3022112WP ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25562FE 46947 LEFT WING UPPER GEAR DOUBLER CORRODED. CORROSION WAS BLENDED OUT AND REPAIRED WITH FILLER AND DOUBLER IAW FEDEX EA 8-571-84840. 2L73 4F RTA22WE 20050309000862005030900086WP 2005 3 9 05FDEA00381 120041206A5312AYB70151 BULKHEAD DOUG MD10 MD1010F 3022112WP ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25562FE 46947 FUSELAGE - LEFT AND RIGHT TEE CAPS, STA 1156, CRACKED. LEFT AND RIGHT TEE CAPS REPLACED OVERSIZING AND BUSHING HOLES AND INSTALLING REPAIR DOUBLERS IAW FEDEX EA 8-5310-84882. 2L73 4F RTA22WE 20050309000872005030900087WP 2005 3 9 05FDEA00382 120041208A5311ACA00293 FRAME DOUG MD10 MD1010F 3022112WP ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25562FE 46947 FUSELAGE - FRAME SPLICE CORROSION AT STA 475 BETWEEN LONGERONS 23 & 24, LEFT SIDE. TRIMMED FRAME BETWEEN LONG 23 & 24 AND REMOVED FRAME LOWER SECTION THAT TERMINATES AT HORIZONTAL PRESSURE WEB AROUND Z= -37. INSTALLED NEW FRAME SECTION USING ANGLE DOUBLER IAW FEDEX EA 8-5310-84845. 2L73 4F RTA22WE 20050309001372005030900137WP 2005 3 9 05FDEA00378 120040914A5512ALC7204 SKIN PANEL DOUG MD10 MD1010F 3022112WP ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25562FE 46947 DURING MAINTENANCE INSPECTIONS, FOUND CRACKS ON LOWER CONSTANT SECTION SKINS OF THE HORIZONTAL STABILIZER. THE CRACKS WERE WITHIN FLYABLE LIMITS. P/N: ALC7204-1, ALC7205-1, ALC7206-1. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, FED EX EA 8-5510-80003. 2L73 4F RTA22WE 20050308001002005030800100NM 2005 3 8 ASAA0480573 120041120A25603961896501 LANYARD DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE R1 DOOR DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 PRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K) 2L72 4F4 FRT E9NE 20050308001042005030800104NM 2005 3 8 ASAA0470027 120041026A53207075T6 SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK, CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727 TO 849 RBL 25. FABRICATED NEW IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050308001112005030800111SO 2005 3 8 N3B2004F00000 120040716A3244348F332 TIRE GULSTMG1159 G1159B 3953535SO RROYCESPEY SPEY5118 54523EU LT MLG BLOWN E N3BAK NONE O OTHER TOTAKEOFF 1 SW01510SR 070 LT MAIN GEAR TIRE BLEW OUT ON TAKEOFF. DAMAGE TO LT WING, LT GEAR HARNESS, BRAKE LINES, AND A DENT IN THE LT LOWER ENGINE COWL. 2L72 4F4 FRTA12EA E2EU 20050308001202005030800120NM 2005 3 8 AMTA200401396 120041110A335020121 CHARGER BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE CABIN FAILED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11515AT 27598 EMERGENCY FLOOR LIGHTS FROM ROW 6 TO R-2 DOOR FADE OUT AS LIGHTS ARE TURNED ON. REMOVED AND REPLACED BATTERY CHARGER IAW MM, OPS CHECK GOOD. 2L72 4F4 FRTA2NM E12EU 20050308001282005030800128SW 2005 3 8 ERAA098186 120041009A6410 BLADE BELL 412 412 1182202SW TAIL ROTOR VIBRATION B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03421EH 33067 VIBRATION AFTER 3 DAYS OF HEAVY RAIN. NO BALANCE WEIGHTS ON BALANCE BRACKETS. REMOVED T/R BLADE A-10206 AND SENT TO CTI FOR EVALUATION. REMOVED T/R BLADES, VISUALLY INSPECTED ALL COMPONENTS, INSTALLED SERVICEABLE T/R BLADES, LUBED TRUNNION, MARVEL BALANCED, TORQUED AND SAFTIED IAW 412 CR/O. 1G72 4U H4SW 20050308001332005030800133CE 2005 3 8 GUU2004F00042 120041119A55241016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO1781546* UE187 AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20050308001382005030800138 2005 3 8 JX62004F00000 420040803A2210512211002 COMPUTER BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112NE AFT TAIL CONE MALFUNCTIONED E JX6AA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CE09598JL RJ19 (LG NR 000173) AIRCRAFT DEPARTED, CLIMBING THROUGH FL370 AT M.58, THE YAW DAMPER BEGAN A SERIES OF LT TO RT INPUTS INCREASING TO FULL SCALE DEFLECTION AT A RATE OF APPROXIMATELY ONE PER SECOND. THE AUTOPILOT WAS TURNED OFF, AND THE MALFUNCTION CONTINUED. TURNED YAW DAMP OFF, AND THE MALFUNCTION CEASED. CREW NOTIFIED ATC AND RETURNED TO AIRPORT. PHYSICAL LOCATION OF FAILED PART IS IN THE AFT TAIL CONE COMPARTMENT. (CE09200404353) 2H72 4F4 FRTA16SW E25EA 20050308001452005030800145EU 2005 3 8 MALA040742 120041128A3040 GROUND WIRE SAAB SF340 340B 7860101EU WINDSHIELD HEAT ARCED A MALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 GL15448XJ 340B448 CREW SMELLED SOMETHING BURNING THEN NOTICED A SMALL PLUME OF SMOKE FROM LOWER LT SIDE OF LT WINDSHIELD. SELECTED LT FRONT HEAT OFF AND SMOKE AND SMELL WENT AWAY. MAINTENANCE FOUND GROUND CONNECTION FOR LT WINDSCREEN VERY LOOSE AND SIGNS OF ARCING. RESECURED GROUND NO DAMAGE NOTED, VERIFIED WINDSCREEN, OPS CHECKS GOOD. 2L72 4T RTA52EU 20050308001712005030800171SW 2005 3 8 ALGA098477 120041210A6510407340339107 BEARING BELL 407 407 1182206SW TAIL ROTOR VIBRATION B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03547AL584 53240 FAILED VIBRATION CHECK. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050308001792005030800179NM 2005 3 8 LCQ2005031 120041221A5300 SKIN BOEING737 737522 138449FNM CARGO DOOR DENTED B K NONE O OTHER ININSP/MAINT 1 SW15945UA 26684 C-2 DOOR HAS NUMEROUS DENTS, CUSTOMER REQUESTS DOOR TO BE RESKINNED. REF NR 23419 S/O 269001. 2L72 4F RTA16WE 20050308001832005030800183WP 2005 3 8 I5HA03580009 120041209A326009588738 BUSHING CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL RT MLG BACKED OUT A I5HAO OTHER J WARNING INDICATION CRCRUISE 1 GL23584E 24 ENROUTE, CREW OBSERVED LANDING GEAR (UNSAFE LIGHT) REMAINED ON AFTER LANDING GEAR WAS RAISED AND AFTER HYDRAULIC BYPASS HANDLE WAS PUT IN (BYPASS) POSITION. MECHANICS WERE UNABLE TO DUPLICATE THIS DISCREPANCY WITH AC ON JACKS BUT DETERMINED THAT NLG ACTUATOR WAS BYPASSING INTERNALLY. THE ACTUATOR WAS REMOVED AND REPLACED, AC RETURNED TO SERVICE. CREW AGAIN EXPERIENCED DISCREPANCY. MECH STILL UNABLE TO DUPLICATE. FURTHER INSP REVEALED BUSHING (ITEM 20 ON ATTACHED FIG) IN RT MLG UPLOCK SWITCH ASSY THAT HAD BACKED OUT OF HSG. THIS ALLOWED LG TO DROP ENOUGH TO ILLUMINATE (UNSAFE LIGHT). OCCURRED INTERMITTENTLY, ONLY INFLIGHT. BUSHING WAS REPLACED AND AC RETURNED TO SERVICE. 2L72 4R4 T 6A6 E282 20050308001842005030800184NM 2005 3 8 TSAA0432083 120041217A3260189929 DOWNLOCK SENSOR BOEING737 7372T4 1384492NM LT MLG DEFECTIVE A TSAAO OTHER N FALSE WARNING DEDESCENT 1 WP13808AL 23445 NON-ETOPS FLT. 82, HNL-KOA - DURING DESCENT, LEFT GEAR RED LIGHT WAS ON WITH THE LANDING GEAR HANDLE IN THE DOWN POSITION. FLEW BY TOWER TO VERIFY GEAR DOWN. UNEVENTFUL LANDING AT KOA. VERIFIED LEFT DOWNLOCK SENSOR BAD. REPLACED PROXIMITY SENSOR PER AMM 32-61-31. OPS CHECK OK. OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050308001922005030800192EU 2005 3 8 HEEA098565 120041103A2697B232M CONNECTOR BOLKMS105 BO105S 5626006EU FIRE DETECTOR CONTAMINATED B HEEAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 SW036607K S841 EN ROUTE OFFSHORE, FLIGHT PILOT DIVERTED TO HI-264 TO CHECK NR 1 ENGINE FIRE LIGHT ILLUMINATION. MAINTENANCE CLEANED CONNECTORS AT FIRE DETECTORS. 1G72 3U H3EU 20050308001932005030800193EU 2005 3 8 HEEA098566 120041104A2910D1331454E GUIDE BOLKMS105 BO105S 5626006EU HYD SYSTEM MALFUNCTIONED B HEEAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW03800PH S800 HYDRAULIC LIGHT CAME ON IN FLIGHT. RETURNED TO HOUMA. MAINTENANCE REPLACED GUIDE ASSY. 1G72 3U H3EU 20050308002862005030800286 2005 3 8 ASA044404 420041228A256561621469 SLIDE BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU R1 DOOR FAILED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS9478 25103 PAE - R1 ESCAPE SLIDE TEST FAILED. (SLIDE DEPLOYED, COCKED AT 90 DEGREES) REMOVED AND REPLACED SLIDE IAW AMM. THIS SLIDE WAS USED AS PART OF A F/A TRAINING EXERCISE. PRIOR TO DEPLOYING SLIDE A "TARP" WAS INGESTED INTO THE ASPIRATOR OF THE SLIDE BOTTLE AND ENTANGLED WITH THE SLIDE DURING DEPLOYMENT. THE OVERHAUL OF THE SLIDE WAS DONE IAW MANUFACTURES INSTRUCTIONS, CMM 26-66-07 AND EO 2560-01148, AND NO DEFECT WAS FOUND WITH THE SLIDE OR ANY ASSOCIATED SUBSYSTEMS. THIS SLIDE WAS RETURNED TO SERVICE. (M) 2L72 4F4 FRTA16WE E21EU 20050308002872005030800287NM 2005 3 8 ASA044401 120041229A5311655828056 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CRACK ON FRAME AT FASTENER BS 359, STR 2L. REPAIRED CRACK IN FRAME AT FASTENER IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050309001342005030900134NM 2005 3 9 UPS05M43955 120041226A54102215105501 FITTING DOUG MD11 MD11F 3023600NM NR 2 BELLMOUTH CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 2 ENG BELL MOUTH AFT LWR BRACE LINK SUPPORT AT 6 O'CLOCK POSN FOUND WITH SURFACE CORROSION AS MARKED. CORROSION REMOVED & SURFACE REPROTECTED AS PER SRM 51-21-01, ORIG THK 0.2 5 INCH & MAT REMOVED 0.043 INCH, FOUND EXCEEDED LIMIT AS SRM 54-00-01 FIG 1A V1 REV 36. NEW FITTING HOLE TRANSFERRED AS PER SRM 51-31-01, V2 R36. BELLMOUTH LWR BRACE LINK SUPPORT FITTING INSTALLED AS PER MM 70-10-03 R45. 2L73 4F RTA22WE 20050310000012005031000001 2005 3 10 04FDEA02983 420041023A2230B415ABM1 COMPUTER AIRBUS300 A300B4605R 3930308EU AUTOTHROTTLE MALFUNCTIONED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25680FE 794 REJECTED TAKEOFF - AIRCRAFT NI WENT TO MAX POWER (TOGA) THOUGH FLEX POWER SELECTED ENT BY: 097576 RPT BY: 097023 THIS ITEM WAS CLEARED WITH THE R&R OF THE T.C.C. PER A-300-600 M/M 22-36-34-4-01, AND OPS CHECK OF THE AUTOTHROTTLE SYSTEM PER A-300-600 M/M 22-30-00-5 -01. SEE PREVIOUS UPDATE FOR ORIGINAL SIGNOFF OF THE DEFERAL AND THE PART CHANGED. 2L72 4F RTA35EU 20050310000032005031000003GL 2005 3 10 Y3AR097979 220041020A725023031938 TURBINE NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C28B 03013GL ENGINE DESTROYED B Y3ARA UNSCHED LANDING O OTHER CRCRUISE 1 SW03 791 CAT30378F DURING DISASSEMBLY FOUND NR 2 TURBINE NOZZLE DIAPHRAM TO BE DETACHED FROM THE NOZZLE ASSEMBLY. THIS CAUSED THE DIAPHRAM TO RUB ON BOTH THE 1ST & 2ND STAGE TURBINE WHEELS CAUSING SEVER DAMAGE TO BOTH WHEELS 1Q71 3R3 U 2A6 E1GL 20050310000042005031000004EA 2005 3 10 UIA9319 120041120A7932AS3209113 PACKING DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE BROKEN Z A UNSCHED LANDING O OTHER CLCLIMB 1 SW9915223 404 123206 IN FLIGHT NR1 OIL PRESS DROP TO ZERO. AFTER LANDING CHECK FOUND NR1 DC/STARTER PACKING CHAFING IAW AMM 80-10-11 REPLACED NEW PACKING AND ENG RUN-UP CHECK NO LEAKING FIND,A/C RETURN TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20050310000202005031000020GL 2005 3 10 ERAA098178 220040819A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03124EH12815 S559 GOVERNOR DROPS OUT OF SERVICE LIMITS. COMPONENTS WORN INTERNALLY. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20050310000212005031000021 2005 3 10 ERAA098198 420040914A2562 BATTERY SNIAS AS332 AS332L 8680809EU ELT LEAKING A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03170EH 68128 THIS INFO FOR FAA SDR. BATTERY LEAKED, MOISTURE DAMAGE, G SWITCH STICKS. ACTION TAKEN: PERFORMED PRELIMINARY INSPECTION AT ARTEX 9/27/2004 AND REPAIRES. 2G72 4U H4EU 20050310000452005031000045EU 2005 3 10 TXER098345 120041029A6220704A33633208 SPHERICAL STOP AEROSPAS355 AS355* EU MAIN ROTOR WORN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09151TA 2601 SHERICAL STOPS WORN 1G72 3U H11EU 20050310000482005031000048NM 2005 3 10 LCQ050310 120041221A5330 SKIN BOEING737 737 UTILSYSNM FUSELAGE DENTED B K NONE O OTHER ININSP/MAINT 1 SW15945UA 26684 DENT ON AFT LT SIDE OF FUSELAGE AT APPROX. STATION 1029 APPROX. STRINGER 13. REF NR 23463 S/O 269001 2L72 4F RTA16WE 20050310000502005031000050EA 2005 3 10 2004F00437 120041221A5340612826 MOUNT DHAV DHC2 DHC2MK1 2800102EA ADC CRACKED B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL0594DC 600 238 DURING A SCHEDULED INSPECTION, FOUND THE AIR DATA COMPUTER (ADC) BROKE LOOSE FROM ITS MOUNT. UPON FURTHER INVESTIGATION FOUND THE MOUNTING BRAKET FLANGE CRACKED COMPLETELY OFF THE AIRFRAME STRUCTURE IT WAS RIVETED TO. AFTER REMOVAL OF THE BRAKET, AND FUTHER INSPECTION, IT IS BELIVED HTAT THE FLANGE WAS NOT MANUFACTURED WITH THE PROPER RADIUSES IN THE CUTOUT FOR THE THUMBNAIL SCREW CAUSING IT TO CRACK. VIBRATION FROM GENERAL AIRCRAFT OPERATION CONTRIBUTED TO THE ISSUE. THIS ADC WAS INSTALLED AS PART OF THE CHELTON FLIGHT SYSTEMS STC#SA02203AK EFIS-SV SYSTEM IN JUNE OF 2004. 1H71 3R A806 20050310000552005031000055SO 2005 3 10 1322122304 120041223A3233115941000145 ACTUATOR GULSTMG1159 GIV 3980115SO MLG LEAKING E N93AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO13422QS 1322 DURING FLIGHT LOSS OF HYDRAULIC FLUID OCCURRED "QUANTITY LOW" MESSAGE ILLUMINATED 2L72 4F RTA12EA 20050310000622005031000062CE 2005 3 10 20030778 120041230A3213114810000656 AXLE BEECH 1900 1900D 1154162CE RT MLG CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03253GL2461 2461 UE253 RT MAIN GEAR LOWER STRUT AXLE ASSY LUG HAS (2) CRACKS APPROX .05 AND .06 LONG WHERE LOWER TORQUE KNEE ATTACHES TO LUG. 2L72 4T RTA24CE 20050310001082005031000108SW 2005 3 10 ALGA098819 120041228A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03627AL647 53284 ROUGH, BINDING, AXIAL PLAY BEYOND MAX. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050310001212005031000121NM 2005 3 10 ASAA0410578 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN LAP 6 INCHES LONG. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001232005031000123NM 2005 3 10 USAA0410583 120041122A5330654576795 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001242005031000124NM 2005 3 10 ASAA0410584 120041122A53106545829502 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE EE DOOR CUTOUT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON WEB RT SIDE OF E AND E DOOR CUTOUT. REMOVED AND REPLACED. 2L72 4F4 FRTA16WE E2EA 20050310001252005031000125NM 2005 3 10 ASAA0410585 120041122A53306545800220 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE SKIN LAP DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001262005031000126NM 2005 3 10 ASAA0410586 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001282005031000128NM 2005 3 10 ASAA0410588 120041122A53306545767541 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE LIGHTNING STRIKEA ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - LIGHTING STRIKE HOLE IN EXTERNAL SKIN. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001292005031000129NM 2005 3 10 F3LA200400118 120041210A2710 CONTROL CABLE BOEING737 73736Q 1384409NM RT AILERON OUT OF ADJUST A F3LAO OTHER F FLT CONT AFFECTED LDLANDING 1 NM03307FL 28760 FLIGHT CREW REPORTED ON SHORT FINAL APPROACH, FULLY CONFIGURED AILERON ROLL FELT TO BIND. ALL OTHER PHASES OF FLIGHT NORMAL. ADJUSTED LT AND RT AILERON BOS CABLES TO BRING LT AILERON WITHIN LIMITS. 2L72 4F RTA16WE 20050310001312005031000131NM 2005 3 10 ASAA0470028 120041026A53001434948535 SUPPORT ANGLE BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK FOUND CORROSION FWD CARGO BAY AFT CTR BULKHEAD SUPPORT ANGLE UPPER SIDE AT BS 500 D. REPAIRED IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050310001322005031000132NM 2005 3 10 ASAA0470026 120041026A53202024T3 SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE SIDEWALL CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727 TO 849 LBL 25 WL 154. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E00055EN 20050310001352005031000135NM 2005 3 10 ASAA0470024 120041026A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION ON NR 3 FLOOR PANEL IN AFT CARGO BAY. FABRICATED IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050310001372005031000137WP 2005 3 10 ASAA0480540 120041024A3350 BATTERY PACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE EMERGENCY LIGHT INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 PDX LINE CHK - EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE FROM ROW 2 TO 7. REPLACED ASSOCIATED BATTERY PACK (POWER SUPPLY). LIGHTS THEN OPERATED PROPERLY. 2L72 4F4 FRTA6WE E9NE 20050310001382005031000138WP 2005 3 10 ASAA0480552 120041030A53115913596503 FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK - AFT ACCESSORY COMPARTMENT FRAME CHAFED AT LONGERON 20R. REMOVED DAMAGED SECTION AND INSTALLED REPAIR ANGLE IAW SRM.(K) 2L72 4F4 FRTA6WE E9NE 20050310001392005031000139NM 2005 3 10 ASAA0480553 120041104A335060030451 POWER SUPPLY DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE OVERWING EXIT DISCHARGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 SERVICE CHECK- EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE AT OVERWING EXIT ON BOTH SIDES. REPLACED ASSOCIATED BATTERY PACKS (POWER SUPPLYS). LIGHT THEN OPERATED PROPERLY.(K) 2L72 4F4 FRT E9NE 20050310001402005031000140WP 2005 3 10 ASAA0480551 120041030A53219936651509 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02969AS 53063 C-CHECK-MAIN CABIN FLOOR PANEL IS DELAMINATED AT CORNER. REPLACED FLOOR PANEL IAW SRM.(K) 2L72 4F4 FRTA6WE E9NE 20050310001422005031000142WP 2005 3 10 ASAA0480560 120041118A53305911410531 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK. (K) 2L72 4F4 F A6WE E9NE 20050310001432005031000143WP 2005 3 10 USAA0480560 120041118A53305911410531 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 SW15934AS 49235 C-CHECK - FUSELAGE SKIN DENTED. HFEC INSPECTION IAW EA REVEALED NO DAMAGE REQUIRING REPAIR. BUT REPETITIVE INSPECTIONS ARE REQUIRED UNTIL NEXT HEAVY MAINTENANCE CHECK.(K) 2L72 4F4 F A6WE E9NE 20050310001472005031000147NM 2005 3 10 ASAA048558 120041102A532199365391 FLOOR PANEL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE FLIGHT DECK CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 C-CHECK - FLIGHT DECK FLOOR PANEL IS CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM.(K) 2L72 4F4 FRT E9NE 20050308002052005030800205NM 2005 3 8 ASAA0410498 120041109A5311654681542 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE MISDRILLED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - UPPER FRAME SECTION HAS MISDRILLED PILOT HOLES UNDER FRAME CAP. REPAIRED IAW SRM. 2L72 4F4 FRTA16WE E2EA 20050308002152005030800215NM 2005 3 8 UIEA200400204 120041223A3260 SWITCH BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE RT WING GEAR DIRTY A UIEAO OTHER J WARNING INDICATION CLCLIMB 1 EA15534MC 21832 ON TAKEOFF, WHEN GEAR RETRACTED, RED GEAR WARNING LIGHT CAME ON. F/E PANEL RT WING DOOR OPEN LIGHT WAS ON, BOTH PRIMARY AND ALT POSITIONS. DID FHB CHAPTER 3, GEAR HANDLE UP, LIGHT WHEN OUT. GEAR HANDLE OFF, LIGHTS ON AGAIN. LT HANDLE UP. INSPECTED AND FOUND ABNORMAL AMOUNT OF DIRT AND GRIT IN RT WING GEAR ROLLER AND UPLOCK ROLLER INTERFACE. ALSO, FOUND DIRT AND GRIT AT DOOR INDICATOR MAG SWITCHES. CLEANED ALL AFFECTED AREAS AND CYCLED WING GEAR DOOR FOLLOW UP DOOR. OPS CHECK GOOD IAW MM. NO DEFECTS NOTED. 2L74 4F4 F A20WE E23EA 20050308002822005030800282NM 2005 3 8 ASA0440364 120041217A53476546815526 SEAT TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - MECHANICAL DAMAGE ON SEAT TRACK. REPLACED SEAT TRACK. (K) 2L72 4F4 FRTA16WE E21EU 20050308002842005030800284NM 2005 3 8 ASA0440363 120041220A532065C3397254 FLOOR SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE- CORROSION ON GALLEY FLOOR SUPPORT. REPLACED FLOOR SUPPORT. (K) 2L72 4F4 FRTA16WE E21EU 20050308002922005030800292NM 2005 3 8 ASA0440358 120041220A53206545834525 INTERCOSTAL BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL. (K) 2L72 4F4 FRTA16WE E21EU 20050310000442005031000044NE 2005 3 10 UPS04443610 220041215A73147479995 PUMP BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE INOPERATIVE A IPXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO01676UP 20101 CREW SHUTDOWN NR 2 ENGINE IN FLIGHT DUE TO ENGINE NOT RESPONDING. CREW RESTARTED AND ENGINE PERFORMED NORMALLY. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-21-01 AND 73-11-01. PERFORMED ADJ AND TEST PER MM 71-00-00 OPS CK LEAK CK GOOD. 2L74 4F4 F A20WE E20EA 20050310000492005031000049 2005 3 10 2004F00436 420041221A3417962830A1S8 ADC DHAV DHC2 DHC2MK1 2800102EA COCKPIT INACCURATE B HJBRO OTHER O OTHER NRNOT REPORTED 1 AL0594DC 518 238 AIR DATA COMPUTER (ADC) INSTALLED AS PART OF THE CHELTON FLIGHT SYSTEMS EFIS-SV SYSTEM UNDER STC SA02203AK REPORTING 500' ALTITUDE ERROR. 1H71 3R A806 20050310000632005031000063CE 2005 3 10 5285001 120041227A783064ND780024 THRUST REVERSER CESSNA560 560XL 2076702CE LT ENGINE LACK OF LUBE E ERYAO OTHER WJ INADEQUATE Q C WARNING INDICATION LDLANDING 1 CE07422AB929 5605285 LT THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. OCCURRED AFTER A FLIGHT 2 HOURS IN CLEAR AIR AND DESCENT INTO HAZY BELOW FREEZING MOISTURE CONDITIONS. MAINTENANCE FOUND LUBRICATION NEEDED. LUBRICATED AND F/C SATISFACTORY. 2L72 4F RTA22CE 20050310001002005031000100SW 2005 3 10 47567122504 120041225A6330222031613103 LINK BELL BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE M/R GEARBOX FAILED E A1UAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 CE03220LN A125 47567 47208 WHILE IN CRUISE FLIGHT WITH PATIENT ABOARD. TWO LOAD BANGS WERE HEARD. A PRECAUTIONARY LANDING WAS MADE AT DCU. LANDED AIRCRAFT AND INSPECTED DOORS. NOTHING WAS FOUND. RESUMED THE FLIGHT AND APPROXIMATELY 2 MIN LATER A LOUD BANG BEGAN ACCOMPANIED BY VIBRATION AIRCRAFT WAS HALF MILE NORTH OF HUNTSVILLE INTERNATIONAL AIRPORT. AIRCRAFT WAS LANDED AT HSV. PATIENT WAS TRANSPORTED BY GROUND. FOUND LOWER ELASTOMERIC BEARING OF RIGHT HAND FORWARD TRANSMISSION LIFT LINK FAILED. REPLACED WITH SERVICEABLE LIFT LINK AND AIRCRAFT RETURNED TO SERVICE. 1G72 3U3 U H9SW E5NE 20050310001062005031000106GL 2005 3 10 ALGA098856 220041113A72006895007 METER BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL TORQUE SPALLED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW035NBFH1907 52275 CAE895961 METAL ON BOTH PLUGS, FOUND TORQUE METER AFT BEARING BREAKING DOWN, HEAVY SPALLING OUTER EDGES OF ROLLERS AND INNER RACE. REPLACED BEARING AND REPAIRED GEAR BOX. 1G71 3U3 UNCH2SW E1GL 20050310001172005031000117NM 2005 3 10 TSAA0427086 120041231A27512061141 INDICATOR BOEING737 737230 1384401NM TE FLAPS DEFECTIVE A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13823AL 23154 RIGHT TRAILING EDGE FLAP INDICATED AT 1 DEGREE WHEN FLAPS WERE PUT UP. INDICATOR THEN WENT UP 5 MINUTES IN THE FLIGHT. UNABLE TO DUPLICATE THE DISCREPANCY ON GROUND. REPLACED TRAILING EDGE POSITION INDICATOR FOR TROUBLESHOOTING PURPOSE. OPS CHECK OKAY, OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 20050310001412005031000141NM 2005 3 10 ASAA0480556 120041102A5230591014167 PAN DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE CARGO DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02982AS 53473 C-CHECK - AFT CARGO DOOR LOWER FRAME AND INNER PAN ARE GOUGED ALONG EDGE ADJACENT TO RUB BLOCK. REMOVED DAMAGED AREA. REPAIRED IAW EA.(K) 2L72 4F4 FRT E9NE 20050310001442005031000144WP 2005 3 10 ASAA0480561 120041118A5320991555416 INTERCOSTAL DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - INTERCOSTAL CORRODED UNDER FLOOR TRACK. REPLACED INTERCOSTAL. (K) 2L72 4F4 F A6WE E9NE 20050310001452005031000145WP 2005 3 10 ASAA0480566 120041118A5340593606441 TEE FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FRAME CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - FRAME TEE FITTING CORRODED BELOW CARGO TRACK. REPLACED TEE FITTING.(K) 2L72 4F4 F A6WE E9NE 20050310001482005031000148WP 2005 3 10 ASAA0480576 120041130A533059114003 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECKED- LT NLG DOOR AFT HINGE CUTOUT IS CRACKED. STOP-DRILLED CRACK, INSTALLED DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050310001502005031000150WP 2005 3 10 ASAA0480575 120041130A523059101413 BRACKET DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CARGO DOOR CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK - MID CARGO BAY DOOR UPPER AFT LATCH BRACKET CHAFED. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER.(K) 2L72 4F4 FRTA6WE E9NE 20050310001512005031000151WP 2005 3 10 ASAA0480578 120041130A5313593071503 LONGERON DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE AFT CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK - LONGERON 29L IS CORRODED IN AFT CARGO BAY AREA. REMOVED DAMAGED SECTION AND REPAIR SPLICES.(K) 2L72 4F4 FRTA6WE E9NE 20050310001522005031000152WP 2005 3 10 ASAA0480579 120041130A534759305487 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK - SEAT TRACK CORRODED. REPLACED DAMAGED SECTION.(K) 2L72 4F4 FRTA6WE E9NE 20050310001542005031000154SO 2005 3 10 SIMA200430803 120041031A3350110049 CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21833AE 145629 CREW REPORTED THE THIRD EMERGENCY LIGHT TO BE INOPERATIVE DURING PREFLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050310001552005031000155WP 2005 3 10 ASAA0480588 120041207A53219936582505 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-CENTER FLOOR PANEL IS PUNCTURED AND DELAMINATED. REPLACED PANEL. (K) 2L72 4F4 FRTA6WE E9NE 20050310001572005031000157WP 2005 3 10 ASAA0480590 120041207A575359357706 FLAP TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TE FLAPS CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 CHECK-RT IB FLAP TRACK MOUNTING BRACKETS BOLT HOLES PITTED. REAMED PITTED HOLES AND INSTALLED BUSHINGS IAW EA. (K) 2L72 4F4 FRTA6WE E9NE 20050310001582005031000158SO 2005 3 10 SIMA200431001 120041020A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21837AE 145647 DURING AN MBV INSPECTION THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050310001592005031000159SO 2005 3 10 SIMA200432206 120041113A5330 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 DAMAGE ON THE AFT LOWER FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 211. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM. 2L72 4T4 FRTT00011ATTE6CH 20050310001602005031000160SO 2005 3 10 SIMA200433604 120041126A27303621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL PITCH TRIM FAILED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21853AE 145742 CREW REPORTED MAIN AND BACKUP PITCH TRIM FAILURE. MAINTENANCE COMPLIED WITH ENT AND FAULT ISOLATION MANUAL AND REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F4 FRTT00011ATTE6CH 20050310001612005031000161WP 2005 3 10 ASAA0480595 120041207A531059568791 DOOR FRAME DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-FORWARD ENTRY DOOR JAMB WEB AFT SIDE AT CRACKED. REMOVED DAMAGE, INSTALLED REPAIR FILLER AND DOUBLER.(K) 2L72 4F4 FRTA6WE E9NE 20050310001632005031000163WP 2005 3 10 ASAA0480582 120041130A575259104133 TAB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ELEVATOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK- LT ELEVATOR CONTROL TAB LOWER SURFACE IS DENTED. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050310001652005031000165WP 2005 3 10 ASAA0480596 120041207A523059101419 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE CARGO BAY DOOR GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-FORWARD CARGO BAY DOOR FORWARD LOCK AREA IS GOUGED ABOVE LOCK. INSTALLED REPAIR DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050310001662005031000166WP 2005 3 10 ASAA0480583 120041130A5752591041417 TAB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ELEVATOR DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK, RT ELEVATOR GEARED TAB LOWER SURFACE DELAMINATED AND DENTED, BETWEEN NR 2 AND NR 3 HINGE POINTS. REMOVED DAMAGED AREAS AND INSTALLED FILLERS AND DOUBLERS. 2L72 4F4 FRTA6WE E9NE 20050310001692005031000169SO 2005 3 10 SIMA200431007 120041101A3610CA33010 CLAMP EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL RT ENGINE SEPARATED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21621AE 145105 DURING CLIMB FROM ORD ENTERED ICING CONDITIONS. HEARD A LOUD (POP) NOISE FROM BACK. BLD (2) LK ON EICAS. NOISE WAS LOUDEST OVER WING AND PASSENGERS SEAT AT WING REPORTED FEELING VERY HOT RUSH OF AIR FROM ABOVE. INSPECTED AND FOUND BAD BLEED LINE CLAMP AND SLEEVE. REPLACED BOTH CLAMP AND SLEEVE AS WELL AS PANEL DAMAGED WHEN CLAMP SEPARATED. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4T4 FRTT00011ATTE6CH 20050310001702005031000170SO 2005 3 10 SIMA200434216 120041201A5210 SKIN EMB 135 EMB135LR 3260305SO ALLSN AE300 AE3007A GL PAX DOOR CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21737MW 145396 A DENT 18 INCHES AFT OF THE PASSENGER DOOR WAS FOUND. REMOVED THE DAMAGED SKIN BY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) 2L72 4F4 FRTT00011ATTE6CH 20050311000532005031100053EU 2005 3 11 BUE2005F00000 220041101A720018355515P ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515P 54521EU NR 1 VIBRATION E BUEAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 GL23159AD38297 11227 9616 NR 1 ENGINE VIBRATION THEN EGT STARTED RAISING TOWARD UPPER LIMITS, ENGINE DID NOT RESPOND TO ENGINE EGT CHECK LIST, SO THE ENGINE WAS SHUT DOWN. 2L72 4F4 FRTA20EU E2EU 20050311000552005031100055EA 2005 3 11 ASOA041005 120041218A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO27856AS 7404 DURING HANGAR MAINTENANCE, THE RT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2L72 4F4 FRTA21EA E15NE 20050311000622005031100062EU 2005 3 11 KBM2005F00002 120041215A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE HALF SHELLS WORN A KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH755 3345 HALF SHELLS WORN. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20050311000642005031100064GL 2005 3 11 ALG2005F00003 220041108A7321 B-NUT BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL FUEL CONTROL LOOSE E ALGAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW031075Y 45378 DURING TAKEOFF, AIRCRAFT HAD A COMPRESSOR STALL. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST FOR EVIDENCE OF FOD NO DAMAGE NOTED. PERFORMED AN ENGINE AIR LINE LEAK CHECK AND FOUND THE P/C LINE FROM THE GOVERNOR TO THE FUEL CONTROL WITH A LOOSE B-NUT. TORQUE CHECKED ALL AIRLINES AND APPLIED TORQUE STRIP. WHILE HEADING INBOUND PERFORMED ON ENGINE, POWER ASSURANCE CHECK WAS A +36. (K) 1G71 3U3 U H2SW E1GL 20050311000722005031100072NM 2005 3 11 S2YA04029 120040902A291342152 PUMP DORNERDO32 DO328300 NM PWA 306 PW306B NE RT HYD SYS INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13360SK2953 3136 DURING FLIGHT, THE CREW REPORTED SYSTEM B HYDRAULIC PUMP FAILURE. THE CREW MADE AN AIR-TURN-BACK, AFTER CONSULTING WITH MECHANIC. THE AC WAS INSPECTED BY MECHANIC WHO CHECKED THE SYSTEM AND REPLACED THE B SIDE HYDRAULIC AC MOTOR PUMP. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050311000882005031100088NM 2005 3 11 S2YA04032 120040909A2150GB2001AA1 VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE LT PACK BROKEN A S2YAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 GL13352SK 3111 DURING FLIGHT, THE CREW REPORTED LOAD VIBRATION THAT SOUNDED LIKE IT WAS OUTSIDE OF THE AC. THE CREW MADE AN AIR-TURN-BACK. THE AC WAS INSPECTED BY MX WHO FOUND THE LT PACK VALVE WAS BROKEN. MX REPLACED THE LT PACK VALVE. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050311000982005031100098EU 2005 3 11 BMAC040013 120041208A2160 CONNECTOR BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP OVERTEMP SWITCH LOOSE A B16AK NONE O OTHER ININSP/MAINT 1 NE05529PA 771 SMOKE PRESENT IN COCKPIT WITH FLOWS ON. FOUND CONNECTOR ON LT OVERTEMP SWITCH TO BE LOOSE. RECONNECTED AND SECURED IAW MM. FUNCTIONAL CHECK GOOD. 2L72 4T4 TRTA21EU E4WE 20050314000032005031400003CE 2005 3 14 761003 120040708A32112643030200 SUPPORT CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE NLG DAMAGED E HSYAK NONE O OTHER ININSP/MAINT 1 NM07748FX4564 208B0503 NLG DRAG LINK SUPPORT DAMAGED. (K) 1H71 3T3 T A37CE E4EA 20050308002882005030800288NM 2005 3 8 ASA0440399 120041229A5347655384426 CARGO TRACK BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02769AS 25103 PAE - CORROSION ON FLOOR TRACK AT PREVIOUS REPAIR BS772, RBL 13.80, WL 153. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS ORIGINAL .070 INCH REMAINING .31 INCH X 1 INCH X 2.5 INCHES. REMOVED AND REPLACED CARGO TRACK FROM BS 727 TO 947.5, RBL 13.8, WL 153. (K) 2L72 4F4 FRTA16WE E21EU 20050308002912005030800291NM 2005 3 8 ASA0440356 120041217A53106545875 CREASE BEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FWD SERVICE DOOR, DAMAGE ON WEB. REMOVED DAMAGE ON CREASE BEAM WEB, FABRICATED REPAIR PARTS AND INSTALLED. (K) 2L72 4F4 FRTA16WE E21EU 20050310000022005031000002NE 2005 3 10 EGRR097941 120041104A6397 WIRE SKRSKYS76 S76C 8143008NE CHIP LIGHT MISINSTALLED B EGRRO OTHER N FALSE WARNING NRNOT REPORTED 1 EA1776AF 760533 MAIN GEAR BOX CHIP DETECTORS FAILED OPERATIONAL CHECK DURING THE FIRST TWELVE MONTH CALENDAR INSPECTION SINCE DELIVERY. TROUBLESHOT AND FOUND MISWIRED AT NR 1 RELAY PANEL. 1G72 3U NCH1NE 20050310000222005031000022EA 2005 3 10 UIA9320 120041205A326085860 PSEU DHAV DHC8 DHC8311 1386006EA NLG DOOR FAULTY Z A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW991523116410 414 IN FLIGHT NOSE GEAR DOOR RED LIGHT ON A/C AIR TURN BACK, AFTER LANDING CHECK FOUND PSEU FAULT.IAW AMM32-61-50 REPLACED PSEU AND FUNCTION TEST CONDITION BACK NORMAL. 2H72 4T RTA13NM 20050310000512005031000051NM 2005 3 10 2004UALA01193 120041208A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 CABIN CREASE BEAM ANGLE CORRODED AT FS 1410 LBL 68. DAMAGED CAUSED BY TYPICAL CABIN CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE AND FILLER. 2L72 4F4 FRTA2NM E17NE 20050310000562005031000056NM 2005 3 10 XNOA1219 120041229A3150 WARNING LIGHT BOEING727 727200 138407ENM CSD TEMP ILLUMINATED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2376753 21249 NR 3 CSD OIL TEMP GANGE INDICATE 160 DEGREE FOR CSD "IN" INDICATION. TRANFERRED TO DMI 4874 IAW MEL 24-3 (STATUS:ORIG/OPEN). 2L73 4F RTA3WE 20050310001072005031000107SW 2005 3 10 ALGA098818 120041228A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR BINDING B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL498 53265 SEVERE BINDING AND RATCHETING. REPLACED WITH NEW BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050310001092005031000109SW 2005 3 10 ALGA098887 120041208A6400206016201131 BEARING BELL 206 206L1 1182107SW TAIL ROTOR BENT B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031067D763 45435 BENT EXCESSIVLY, UNABLE TO SHIM NEW BEARINGS / REPLACED BLADE 1G71 3U H2SW 20050310001202005031000120NM 2005 3 10 ASAA0410577 120041122A55404554B94008 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE RUDDER DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02746AS 23123 PAE - MULTIPLE OUTER PLY DAMAGE ON RUDDER L/E. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001222005031000122NM 2005 3 10 ASAA0410579 120041122A53306545767506 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON EXTERNAL SKIN LAP 4 INCHES LONG. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001332005031000133NM 2005 3 10 ASAA0470022 120041026A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 SW15626AS 30793 PAE: DURING C-CHECK FOUND AFT CARGO BAY NR 2 FLOOR PANEL REQUIRES REPLACEMENT DUE TO DENT. FABRICATED IAW SRM. (K) 2L72 4F4 FRTA16WE E00055EN 20050310001362005031000136NM 2005 3 10 ASAA0470025 120041026A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED C ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK, FOUND AFT CARGO BAY NR 1 FLOOR PANEL CORRODED. FABRICATED IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050310001562005031000156WP 2005 3 10 ASAA0480589 120041207A532199366401 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-CABIN FLOOR PANEL AFT CORNER IS DEBONDED. REPLACED PANEL.(K) 2L72 4F4 FRTA6WE E9NE 20050310001622005031000162WP 2005 3 10 ASAA0480581 120041130A5752591004713 CAP DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE AILERON DEBONDED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV- CHECK-LT IB AILERON CONTROL TAB END CAP IS SEPARATING FROM SKIN. BOND-REPAIRED SEPARATING SECTION. (K) 2L72 4F4 FRTA6WE E9NE 20050311000482005031100048NM 2005 3 11 UIEA200400209 120041229A3310245904 RHEOSTAT BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE LIGHTS BURNED A UIEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15505MC 21251 HOT SMELL (ELECTRICAL) DETECTED IN CRUSE. C/B PILOT PANEL ENDER FLIGHT DECK LIGHTS WAS PULLED ON P6 PANEL. SMELL STOPPED, SHORTLY AFTER. PANEL BELOW CAPTAIN CUP HOLDER FELT HOT. ON T/S FOUND T77 DIMMER BURNED. REMOVED AND REPLACED DIMMER. OPS CHECK NORMAL. (K) 2L74 4F4 FRTA20WE E23EA 20050311000502005031100050WP 2005 3 11 VGC2005F00000 120041222A2612355909575 ELEMENT CVAC 340 340CVAC 242270AWP ALLSN 501D 501D13 03004GL ALLSN A6441 A6441FN606 GL RT ENGINE CHAFED A VGCAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23131FL 155 501597 HC2464 AFTER DEPARTING SDF CLIMBING THROUGH 8500 FT, NR 2 ENGINE ZONE 2, FIRE INDICATION LIGHT ILLUMINATED. CREW PERFORMED CHECKLISTS (IE PERFORMED ENGINE SHUTDOWN) AS REQUIRED AND RETURNED TO SDF. CREW REPORTED THAT NO VISUAL INDICATIONS OF FIRE, AND AFTER ENGINE COOLED DOWN, FIRE WARNING TEST STILL FAILED. FALSE FIRE WARNING INDICATION SUSPECTED. 2L72 4R4 T 6A6 E282 6 CP898 20050311000512005031100051EA 2005 3 11 TIM2005F00000 220041228A723031019012 BLADE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE BROKEN E TIMAE ENGINE SHUTDOWN C F.O.D. CRCRUISE 1 NM07153GA 973 UB34 PCE32475 AIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K) 2L72 4T4 TRTA24CE E4EA 20050311000962005031100096CE 2005 3 11 GUU2005F00000 120041208A2620 WARNING LIGHT BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE INTERMITTENT A GUUAO OTHER N FALSE WARNING CRCRUISE 1 SO1781536 UE152 DURING FLIGHT, LT ENGINE FIRE BOTTLE DISCHARGE LIGHT FLICKERS ON AND OFF. CHECKED SYSTEM AND PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE. OPS CHECK NORMAL. (K) 2L72 4T4 TRTA24CE E26NE 20050314000132005031400013CE 2005 3 14 YDA2005F00000 120041018A528099820043 HINGE BEECH 99 99A 1154003CE PWA PT6 PT6A27 52043EA LT NLG DOOR DAMAGED E YDACK NONE O OTHER ININSP/MAINT 1 AL0399GH U112 THE LT NOSE GEAR DOOR CENTER HINGE AND NOSE GEAR DOOR ACTUATOR LINK QUIDE, BENT. THE NOSE GEAR DOORS WERE DISCONNECTED FOR AN INSPECTION. THE LT MAIN GEAR DOORS WERE RIGGED AND A RETRACTION TEST WAS PERFORMED. A LOAD POPPING NOISE WAS HEARD. UPON INSPECTION THE DAMAGE TO THE NOSE DOOR CENTER HINGE AND THE GUIDE WAS DISCOVERED. THE DAMAGE WAS PROBABLY CAUSED BY IMPROPER NOSE GEAR DOOR RIGGING. (K) 1L72 3T4 T A14CE E4EA 20050314000242005031400024EU 2005 3 14 TXER099450 120041217A6420C642A0100103 HUB UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE TAIL ROTOR WORN B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09120TX3121 1029 WEAR LIMITS EXCEEDED ON TAIL ROTOR HUB. 1G72 3U3 UNCR0001RD E34NE 20050310000242005031000024NE 2005 3 10 ANCF200400037 220041210A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT MALFUNCTIONED W ANCFE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO23190AN218981082 53190 P725925D DURING CLIMB AT 15000 FEET, SEVERE DAMAGE OCCURRED IN THE LT ENGINE, EMERGENCY PROCEDURE WERE PERFORMED. LT ENGINE WAS CHANGED IAW AMM 71-00-00 PAGE 401. TEST WITH ENGINE RUN UP WERE PERFORMED IAW AMM 71-00-00 PAGE BLOCK 501 WITH SATISFACTORY RESULTS. BOROSCOPE WAS PERFORMED WITH THE FOLLOWING RESULTS: T1 BLADES: NORMAL, T2 BLADES: SOME MINOR DAMAGES, T3 / T4 BLADES: MISSING, PRELIMINARY CONCLUSION : T3 / T4 BLADE FAILURE. 2L72 4F4 FRTA6WE E9NE 20050310000462005031000046EU 2005 3 10 TXER098386 120041206A6520350A33020005 GEARBOX AEROSPAS355 AS355N 8680818EU TAIL ROTOR MAKING METAL B TXERO OTHER O OTHER NRNOT REPORTED 1 SW09588BP 5688 GEARBOX MAKING METAL 1G72 3U RTH11GU 20050310000992005031000099CE 2005 3 10 4508912172004 120041217A32206632302001003 VALVE LEAR 45 45LEAR 5170805CE NLG FAULTY E J7SAO OTHER J WARNING INDICATION APAPPROACH 1 SW05406FX3910 089 NOSE GEAR REMAINED UP ON FIRST 4 CYCLES OF THE GEAR HANDLE THEN LOWERED NORMALLY ON 5TH ATTEMPT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL VALVE. OPS CHECK NORMAL. NO DEFECTS NOTED AND NO RE-OCCURRENCE 2L72 4F RTT00008WI 20050310001012005031000101SW 2005 3 10 047504123104 120041231A2910222382001103 SERVO BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE HYD SYSTEM MALFUNCTIONED E A1UAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 CE03431MA 47504 47209 NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIENT WAS TRANSPORTED VIA AMBULANCE ACROSS THE STREET TO UMC. RT DUAL ACTUATOR SERVO LEAKING AT PISTON. REMOVED AND REPLACED SERVO. 1G72 3U3 U H9SW E5NE 20050310001052005031000105EU 2005 3 10 MHIA098772 120041227A5610350KA25900400 WINDSHIELD UROCOPEC130 EC130B4 8680989EU COCKPIT CRACKED B MHIAO OTHER O OTHER APAPPROACH 1 EA25454AE 3490 AIRCRAFT WAS ON APPROACH AND THE LOWER PORTION OF THE WINDSCREEN CRACKED THROUGH, THE LOWER PORTION OF THE WINDSCREEN FROM THE JOGGLE POINTS IN LOWERED INTO THE CABIN. DID NOT COME LOOSE FROM THE BONDING MATERIEL. REPAIRED I/A/W EUROCOPTER STANDARD PRACTICE MANUAL SECTION 20.03.05.401. REPLACED WINDSCREEN WITH NEW. WEATHER COLD UNDER 20 DG F. 1G72 3U H9EU 20050310001272005031000127NM 2005 3 10 ASAA0410587 120041122A53306545767541 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - DAMAGE ON SKIN LAP. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20050310001462005031000146WP 2005 3 10 ASAA0480572 120041118A575359304963 VANE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RT IB FLAP DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - RT IB FLAP HAS DAMAGED OB VANE DELAMINATED. INSTALLED REPAIR FILLER AND DOUBLER. (K) 2L72 4F4 F A6WE E9NE 20050311000462005031100046EU 2005 3 11 BMAC040017 120041229A2750 SELECTOR VALVE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP TE FLAPS INOPERATIVE E B16AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE05531PA 748 UNCOMMANDED FLAP DEPLOYMENT IN FLIGHT VERIFIED VISUALLY TO APPROXIMATELY 20 DEGREES. FLAPS CONTINUED TO DEPLOY TOWARD 35. UPON LANDING FLAPS RETURNED TO ZERO VERIFIED VISUALLY UNCOMMANDED. NO HORN WAS HEARD WITH FLAPS DEPLOYED AND POWER LEVER BELOW 20 PERCENT. REPLACED FLAP SELECTOR VALVE. OPS CHECKED GOOD. TEST FLIGHT FAILED. FOUND BROKEN WIRE IN CENTER CONSOLE. REPAIRED WIRE AND PERFORMED FUNCTIONAL CHECKS OF FLAP SYSTEM IAW AMM. FUNCTIONAL TEST GOOD. PERFORMED IN-FLIGHT FUNCTIONAL CHECK OF FLAPS, FOUND OPERATION NORMAL. 2L72 4T4 TRTA21EU E4WE 20050311000492005031100049NM 2005 3 11 RYN2005F00000 120041224A213011231997303AB CONTROL MODULE BOEING737 737800* NM CABIN PRESSURE INOPERATIVE A RYNAO OTHER O OTHER CRCRUISE 1 CE07ELDGZ 28718 UNABLE TO CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED PRESSURE CONTROL MODULE. (K) 2L72 4F RTA16WE 20050311000672005031100067NM 2005 3 11 S2YA04007 120040307A3241AE208741 CONTROL UNIT DORNERDO32 DO328300 NM PWA 306 PW306B NE ANTI-SKID SYS INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13354SK 3126 DURING TAKEOFF, THE CREW NOTED A CAS MESSAGE FOR ALTERNATE ANTI-SKID DEGRADE. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX INSPECTED THE SYSTEM AND REPLACED THE ANTI SKID CONTROL UNIT (ASCU). MX RETURNED THE AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050311000702005031100070NM 2005 3 11 S2YA04030 120040902A3260OL3092 BULB DORNERDO32 DO328300 NM PWA 306 PW306B NE NLG INDICATOR INOPERATIVE A S2YAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL13356SK 3163 DURING APPROACH OF FLIGHT, THE CREW REPORTED THERE WAS NO GREEN DOWN AND LOCK INDICATION FOR THE NOSE GEAR. THE CREW EXECUTED A MISSED APPROACH AND MANUALLY EXTENDED THE GEAR BUT STILL DID NOT ACHIEVE THREE GREEN BUT PROCEEDED TO LAND WITHOUT INCIDENT. THE LIGHT BULBS FOR THE INDICATOR WERE REPLACED BY THE CREW AFTER MECHANIC CONSULTATION. THE AC HAD TO BE FERRIED BACK BECAUSE OF THE MANUAL EXTENSION. MECHANIC PERFORMED NECESSARY CHECKS AND SERVICE AND RETURNED AC TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050311000752005031100075NM 2005 3 11 S2YA04041 120041103A35003283074 SHUTOFF VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE OXYGEN SYS INOPERATIVE A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13358SK7290 3051 3188 BEFORE FLIGHT, DURING TAXI OUT THE RT LOW PRESSURE REDUCING VALVE (PRSOV) CYCLED ON AND OFF. THE CREW RETURNED TO THE GATE AND MECHANIC INSPECTED THE AC. THE HIGH AND LOW PRSOV WHERE SWAPPED FOR TROUBLESHOOTING WITH THE OPERATION CHECKS BEING BAD. MECHANIC REPLACED THE OXYGEN/ECS PANEL AND THE SYSTEM OPS CHECKED GOOD. THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050311000932005031100093NE 2005 3 11 RG82005F00000 120041107A14309550158060 FASTENER SKRSKYS76 S76 8143010NE TMECA ARRIELARRIEL1S1 60030NE LT DUCT PANEL LOOSE D RG8AK NONE O OTHER ININSP/MAINT 1 CE09370GS 760370 15532 AFTER LANDING, PILOT PERFORMING POST-FLIGHT CHECK NOTICED LARGE AMOUNT OF OIL ON GROUND. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT A FASTENER, PN 9550158060 ON LT SIDE OF OIL COOLER DUCTING PANEL PN 0401272790 HAD COME LOOSE AND WORN A HOLE ON THE IB SIDE OF OIL SUPPLY LINE PN 0401274100. RECOMMEND DAILY INSPECTION OF FASTENER PN 9550158060. (K) 1G72 3U3 U H1NE E19EU 20050314000062005031400006GL 2005 3 14 YTRR099306 220041116A732123070606 FUEL CONTROL BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILED B YTRAO OTHER R PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW0337AJ 327 1877 FUEL CONTROL PURCHASED NEW. ENGINE DEACCELERATED TO 88 PERCENT AND WAS NOT ABLE TO RECOVER. 1G71 3U3 U H2SW E4CE 20050314000802005031400080SW 2005 3 14 ALG2005F00007 120041129A6340214040806003 PRESSURE SWITCH BELL 407 407 1182206SW ALLSN 250C 250C47B GL TRANSMISSION INOPERATIVE E ALGAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW03457AL 53151 DURING BEFORE TAKEOFF CHECK, THE TRANSMISSION OIL PRESSURE LIGHT CAME ON, BUT THE GAUGE WAS READING AT A NORMAL LEVEL. LANDED AND CALLED MAINTENANCE, SHUTDOWN AND CHECK THE MEL BOOK AND THE CONNECTOR PLUGS. MAINTENANCE FLYING PART OUT. MAINTENANCE REMOVED TRANSMISSION PRESSURE SWITCH AND INSTALLED SERVICEABLE PRESSURE SWITCH IAW MM. (K) 1G71 3U3 UO H2SW E1GL 20050315000052005031500005NM 2005 3 15 EIA2004162 120041203A5347 SEAT TRACK BOEING747 747132 1384882NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D 1880-1920 LBL 75 SEAT TRACK FOUND CRACKED. M/D BS 1880-1920 LBL 75 SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050315000082005031500008NM 2005 3 15 EIA2004165 120041117A5712 RIB BOEING747 747132 1384882NM RT WING CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 RIGHT WING L/E CAVITY RIB UPPER CORD FWD END FOUND CRACKED AT ILES 1056. L/E RIB REPLACED PER SRM 51-30-02. 2L74 4F A20WE 20050315000092005031500009NM 2005 3 15 EIA2004166 120041116A5330 SKIN BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 NLG W/W CUTOUT RIGHT FWD CORNER SKIN AT STA 250 RBL 36 FOUND CRACKED. RIGHT FWD CORNER SKIN REPAIRED PER SB 747-53-2304. 2L74 4F A20WE 20050315000102005031500010NM 2005 3 15 EIA2004167 120041121A5313 STRINGER BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 MD AT BS 1470-1475 STRINGER 15R, STRINGER END FOUND CRACKED. DEFECTIVE STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050310001672005031000167SO 2005 3 10 SIMA200432205 120041113A5330 SKIN EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21633AE 145148 DAMAGE ON AFT LOWER FUSELAGE AT FRAME 68 AND STRINGER 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.(K) 2L72 4T4 FRTT00011ATTE6CH 20050310001682005031000168WP 2005 3 10 ASAA0480585 120041207A575259304973 TAB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT ELEVATOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-RT ELEVATOR ANTI-FLOAT TAB IS DENTED 4 INCHES FROM RIG LINE. REMOVED DAMAGE, AND INSTALLED FILLER AND DOUBLER. (K) 2L72 4F4 FRTA6WE E9NE 20050310001712005031000171SO 2005 3 10 SIMA200434217 120041204A532014525381003 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL FR 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21651AE 145422 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER, 2 SHIMS AND PLATE. REPAIR DONE IAW SRM.(K) 2L72 4T4 FRTT00011ATTE6CH 20050311000042005031100004NE 2005 3 11 CED2005F00000 220041109A7200PHC112C31680 HOSE AMD FALC20FALCOND 2720304EU GE CF700 CF7002D2 30010NE NR 1 ENGINE LEAKING E CEDAO OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW05219CA 193 WHILE PASSING THROUGH FL320 ON CLIMB TO FL350, THE NR 1 ENGINE ROLLED BACK TO 25 PERCENT. THE CREW REGAINED POWER AND CLIMBED TO FL350 AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE ENGINE TO INCLUDE BORESCOPE, AND REPLACED T2 HOSE. ENGINE FLIGHT TESTED GOOD. 2L72 4F4 F A7EU E7EA 20050311000542005031100054EU 2005 3 11 KBM2005F00007 120041128A2560504305401 SHOULDER BELT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT STUCK E KBMAK NONE O OTHER ININSP/MAINT 1 WP19966SH884 3787 PILOT SEAT SHOULDER HARNESS STUCK. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050311000892005031100089NE 2005 3 11 S2YA04035 220041001A73208224963003 CONTROL UNIT DORNERDO32 DO328300 NM PWA 306 PW306B NE LT ENGINE INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13351SK 1053 3108 DURING CLIMBOUT, THE CREW NOTED A LT FADEC FAULT AND NO ITT INDICATION ON THE RT ENGINE, AFTER CONSULTING MECHANIC, THEY MADE AN AIR-TURN-BACK. THE MECHANIC INSPECTED THE AC AND REPLACED THE RT EDU. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050314000022005031400002CE 2005 3 14 761187 120040721A32112643030200 SUPPORT CESSNA208 208 2073702CE PWA PT6 PT6A114 52043NE MLG DAMAGED E HSYAK NONE O OTHER ININSP/MAINT 1 NM07800FE 20800007 NLG SUPPORT DAMAGED. (K) 1H71 3T3 TNTA37CE E4EA 20050314000282005031400028 2005 3 14 ALG2005F00009 420041223A2213 AMPLIFIER SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL AFCS SMOKE E ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW03518AL 760134 LANDING, ON DOWN WIND APPROACH SMELLED ODOR, ON FINAL THE ODOR BECAME STRONGER, ON LANDING SMOKE CAME FROM OVERHEAD CIRCUIT BREAKER PANEL AREA. THE NR 2 PITCH AMP BREAKER POPPED. MAINTENANCE PULLED OVERHEAD AND AFCS CIRCUIT BREAKER PANEL, FOUND NO EVIDENCE OF FIRE. TRACED WIRE BACK TO THE NR 2 AFCS AMP ASSY. REMOVED NR 2 AFCS AMP AND FOUND EVIDENCE OF THE NR 2 AMP HAD SMOKED. REINSTALLED CABIN AND PILOT OVERHEAD TRIM AND THE AFCS CIRCUIT BREAKER PANEL, CARRIED THE NR 2 PITCH AMP TO HARDCOVER (MEL) AND RETURNED AIRCRAFT TO SERVICE. (K) 1G72 3U3 U H1NE E1GL 20050315000122005031500012NM 2005 3 15 EIA2004151 120041121A5313 STRINGER BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 MD AT BS 1470-1475 STRINGER 15R STRINGER END FOUND CRACKED. DEFECTIVE STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050315000892005031500089EU 2005 3 15 SIMA200429201 120041013A3350330151 BATTERY PACK SAAB SF340 340B 7860101EU EMERGENCY LIGHT INOPERATIVE A SIMAK NONE O OTHER TXTAXI/GRND HDL 1 SW21370AM 340B370 DFW - FLT 3302 - CREW REPORTED ALL EMERGENCY LIGHTS AFT OF ROW 9 TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20050315001342005031500134SO 2005 3 15 SWIA200414603 120041201A5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 OMEGA BEAM AT YL479.0 FROM FRAME 40 TO 44 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. OMEGA BEAM REPLACED IAW EMB 120 SRM 51-40-02, 51-22-00 AND 51-25-00. 2L72 4T RTA31SO 20050314000432005031400043NE 2005 3 14 ALG2005F00012 120041030A5302 STRUCTURE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL2B NE VERTICAL STAB CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03864AL 760557 ON DAILY SERVICE CHECK FOUND 4 INCH CRACK ON LT SIDE FOR VERTICAL PYLON, UPPER FORWARD CORNER OF THE INSPECTION PANEL AT VS STATION 123.071. MAINTENANCE REPAIRED THE CRACK IAW WITH SRM. (K) 1G72 3U3 UNCH1NE E00054EN 20050315000062005031500006NM 2005 3 15 EIA2004163 120041203A5347 SEAT TRACK BOEING747 747132 1384882NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 1655-1660 LBL 95 SEAT TRACK CRACKED. M/D BS 1655 - 1660 LBL 95 SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050315001422005031500142SO 2005 3 15 SWIA200414621 120041121A5320 SUPPORT ANGLE EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07562SW 120336 CRACKED SUPPORT ANGLE, FORWARD OF PAX DOOR AFT HINGE ARM, UNDER FLOOR (MARKED). ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE ON FORWARD OF PAX DOOR AFT HINGE ARM UNDER FLOOR. 2L72 4T RTA31SO 20050315002842005031500284NM 2005 3 15 BJNA041102 120041128A5313BAC1498124 STRINGER BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 26L STATION 950 BL 10L. REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER 26L AT STATION 950 BL 10L IAW BOEING SRM 53-10-3. (M) 2L72 4F RTA16WE 20050315003442005031500344NM 2005 3 15 BJNA041104 120041128A5313BAC1498124 STRINGER BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM49031 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER 27L AT STATION 950 LBL 5. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 27L AT STATION 950 LBL 5 IAW BOEING SRM CHAPTER 53-10-3. (M) 2L72 4F RTA16WE 20050316000522005031600052NM 2005 3 16 UPS05M44046 120041210A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE: C, NR 1 LT CORROSION ON WALL BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION AT BEARING S/W REMOVED PER SRM 51-21-01V.2R.35, FOUND OUT OF LIMIT PER EO MD11-5510-14909-I. REWORKED BARREL NUT HOLE NR 1 LT PER SRM 51-21-01 V.2.R35. FAB REPAIR SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT NR 1 LT BARREL NUT HOLE & INSTALLED FAB BUSHING PER EO MD11- 5510-14909-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 1 LT FOUND IAW EN 1116-05. 2L73 4F RTA22WE 20050316000532005031600053NM 2005 3 16 UPS05M44047 120041226A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 17 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT. CORROSION REMOVED AT BARREL NUT HOLE NR 17 LT FOUND OUT OF LIMIT PER EO MD11-55 10-19409-I. REWORKED BARREL NUT HOLE NR 17 LT PER EO MD11-5510-19409-I. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 17 LT & INSTALLED FAB SLEEVE. REPAIR COMPLETED AT BARREL NUT HOLE NR 17 LT PER EO MD11-5510-14909-I & EN 1126-05 FOUND SATISFACTORY. 2L73 4F RTA22WE 20050315000012005031500001NM 2005 3 15 EIA2004160 120041203A5313 STRINGER BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 990 S13L STRINGER END FOUND CRACKED. STRINGER END REPLACED PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 20050315000042005031500004NM 2005 3 15 EIA2004161 120041203A5320 STIFFENER BOEING747 747132 1384882NM PRESSURE PANEL CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D PRESSURE DECK STIFFENER CRACKED AT BS 1436 LBL 70. REPLACED STIFFENER PER SRM 51-10-01. 2L74 4F A20WE 20050315000072005031500007NM 2005 3 15 EIA2004164 120041203A5310 TIE BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 920 LEFT O/B TENSION TIE AFT SIDE CRACKED. TENSION TIE REPAIRED PER SRM 51-30-02 AND SB 747-53-2371 FIG 3. 2L74 4F A20WE 20050316000572005031600057NM 2005 3 16 UPS05M44048 120041227A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE: C, NR 11 LT CORROSION ON WALL BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 11 LT PER EO MD11-5510-19409-I, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 11 LT SRM 51-21-01 V.2.R.36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 11 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 11 LT PER EN1123-05 FOUND SATISFACTORY. 2L73 4F RTA22WE 20050316000592005031600059NM 2005 3 16 2004UALA00673 120040716A575165B0813044 RIB BOEING747 747422 1384935NM PWA 4056 PW4056 NE AILERON CRACKED A UALAO OTHER E VIBRATION/BUFFET CLCLIMB 1 WP29187UA45701 26876 SIGNIFICANT SHUDDER ON CLIMBOUT WITH RIGHT O/B AIL. *S/D* THE NR 2 RIGHT OUTBOARD AILERON HINGE FITTING WAS FOUND CRACKED DUE TO FATIGUE. THE CRACKED FITTING WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 20050316000602005031600060NM 2005 3 16 2004UALA00819 120040811A5330 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29905UA 25005 AIRCRAFT DAMAGE ON LEFT AFT SIDE UNDER DOOR 2L APPROXIMATELY 3 FT DOWN. *S/D* ACCOMPLISHED STRINGER SPLICE REPAIR ON STR 20L AND SKIN REPAIR FROM STA 847 TO 867 AND ENCOMPASSES LAP JOINT. 2L72 4F4 FRTA16WE E2GL 20050316000612005031600061NM 2005 3 16 2004UALA00831 120040821A335058781 WIRE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29935UA 26663 EEL LIGHTS INOP IN AFT CABIN FROM ROWS 15 TO AFT GALLEY. *S/D* REPLACED EEL TRACK FEEDER CABLE AND POWER LEAD CABLE FROM SIDEWALL. 2L72 4F4 FRTA16WE E2GL 20050316000662005031600066NM 2005 3 16 UPS05M44050 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 9 LT CORROSION ON WALL BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL HOLE NR 9 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1V.2.R35. REWORKED BARREL NUT HOLE NR 9 LT PER SRM 51-21-01V.2.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 9 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 9 LT PER EN 1121-05 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050316000672005031600067NM 2005 3 16 UPS05M44051 120041230A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 8 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 8 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1V.2 R36. REWORKED BARREL NUT HOLE NR 8 LT PER SRM 51-21-01 V.2 R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 8 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 8 LT PER EN 1120-05 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050316000682005031600068NM 2005 3 16 UPS05M44052 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 7 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 7 LT FOUND OUT OF LIMIT PER SRM 51-21-0 1V.2 R35. REWORKED BARREL NUT HOLE NR 7 LT PER SRM 51-21-01V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 7 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 7 LT PER EN 1119-05, FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050316000762005031600076NM 2005 3 16 UPS05M44054 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 17 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION AT BARREL NUT HOLE NR 17 RT REMOVED PER SRM 51-21-01 V2.R35, FOUND OUT LIMIT. REWORKED NR 17 BARREL NUT RT PER SRM 51-21-01. V.2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I.PR1422B1/2. APPLIED ON BARREL NUT HOLE NR 17 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE 17 RT FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000412005031700041NM 2005 3 17 UPS05M44057 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C, NR 20 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 20 RT PER SRM 51-21-01.V2.R.35, FOUND OUT LIMIT. REWORKED BARREL NUT HOLE NR 20 RT PER SRM 51-21-01.V2.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 20 RT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 20 RT FOUND WITHIN LIMIT PER EN1159-05 & SATISFACTORY. 2L73 4F RTA22WE 20050317000432005031700043NM 2005 3 17 UPS05M44059 120041222A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 36 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 36 LT FOUND OUT OF LIMIT PER SRM 51-21- 01 V.2R.35. REWORKED BARREL NUT HOLE NR 36 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 36 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 36 LT PER EN 1142-05, FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050317000442005031700044NM 2005 3 17 UPS05M44060 120041222A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 1 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 1 RT PER SRM 51-21-01.V2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 1 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 1 RT & INSTALLED PER EOMD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 1 RT PER EN1143-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000452005031700045NM 2005 3 17 UPS05M44061 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 33 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 33 RT PER SRM 51-21-01V.2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 33 RT PER SRM 51-21-01.V.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BAREL NUT HOLE NR 33 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1170-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000462005031700046NM 2005 3 17 UPS05M44062 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 2 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 2 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 2 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 2 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1144-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000472005031700047NM 2005 3 17 UPS05M44063 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 27 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 27 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 27 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 27 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-1. REPAIR COMPLETED AT BARREL NUT HOLE NR 27 RT FOUND WITHIN LIMIT PER EN1164-05 & SATISACTORY. 2L73 4F RTA22WE 20050317000522005031700052NM 2005 3 17 UPS05M44070 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 15 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 15 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 15 RT PER SRM 51-21-01. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT ON BARREL NUT HOLE NR 15 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19049-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 15 RT PER EN1155-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000672005031700067NM 2005 3 17 UPS05M44071 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 6 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 6 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 6 RT PER SRM 51-21-01V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 6 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 6 RT PER EN1147-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000682005031700068NM 2005 3 17 UPS05M44072 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 36 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 36 RT PER SRM 51-21-01V.2R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 36 RT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 39 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 36 RT PER EN 1173-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000692005031700069NM 2005 3 17 UPS05M44073 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 24 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 24 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 24 RT PER SRM 51-21-01V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 24 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 24 RT PER EN1161-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000702005031700070NM 2005 3 17 UPS05M44074 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 21 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 21 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 21 RT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 21 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 21 RT PER EN1160-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000712005031700071NM 2005 3 17 UPS05M44075 120041222A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 32 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 32 LT PER SRM 51-21-01.V2.R5, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE PER SRM 51-21-01.V2.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 32 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-1. REPAIR COMPLETED ON BARREL NUT HOLE NR 32 LT FOUND WITHIN LIMIT PER EN1139-05 & SATISFACTORY. 2L73 4F RTA22WE 20050317000722005031700072NM 2005 3 17 UPS05M44076 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 9 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 9 RT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 9 RT PER SRM 51-21-01-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 9 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 9 RT PER EN 1149-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050315001332005031500133SO 2005 3 15 SWIA200414594 120041201A5320 BUTTSTRAP EMB 120 EMB120 3260201SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0716731 120190 BUTTSTRAP AT YL479.00 FRAME 39-44 IS CORRODED ON THE UNDERSIDE. ITEM FOUND AT C-CHECK INSPECTION. BUTTSTRAP REPLACED IAW EMB 120 SRM 51-40-02, 51-25-00, 51-22-00. 2L72 4T RTA31SO 20050315002322005031500232WP 2005 3 15 2005F00031 120041215A2120 ODOR DOUG DC9 DC982 3022082WP CABIN DETECTED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23829NK 49931 MYR - FLT 1581 - F/A REPORTED LIGHT TO MODERATE SMOKE IN FORWARD CABIN. INSPECTED ALL BALLASTS AND LIGHTING AND GALLEY EQUIPMENT, INSPECTED WIRING AND C/'B'S IN FORWARD CABIN, CHECKED E/E FORWARD ACCY COMPT NO EVIDENCE OF OVERHEAT, SMOKE OR FIRE FOUND, RUN A/C PACKS WITH ENGINES AND APU NO SMOKE, COULDN'T DUPLICATE. REMOVED SOCKS AND FOUND EVIDENCE OF SMOKE AND LIGHT OILY ODOR ON THE RIGHT SOCK, REMOVED AND REPLACED BOTH SOCKS. (M) 2L72 4F A6WE 20050315003072005031500307NM 2005 3 15 BJNA041103 120041128A5311 FRAME BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 DURING A SCHEDULED C CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A FRAME RIB AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. CUTOUT CORRODED AREA OF FRAME AT STATION 285 FROM STRINGER 24L TO STRINGER 28L. FABRICATED FILLER AND DOUBLER USING 7075-T6 .040. INSTALLED FASTENERS AND REPAIR PARTS IAW BOEING SRM CHAPTER 51-40-2. TREATED AND PRIMED FABRICATED PARTS AND SURROUNDING STRUCTURE IAW BOEING SRM CHAPTER 51-30-2. (M) 2L72 4F RTA16WE 20050315003132005031500313NM 2005 3 15 BJNA041101 120041128A575469406121 SUPPORT BRACKET BOEING737 737282 13844ATNM SLAT ACTUATOR CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A LEADING EDGE SLAT ACTUATOR SUPPORT BRACKET ON THE LEFT WING SPAR AT WING STATION 421. REMOVED AND REPLACED THE SUPPORT BRACKET AT THE CENTER OF THE NUMBER TWO LEADING EDGE SLAT ACTUATOR ATTACHMENT LOCATED ON THE LEFT HAND WING SPAR AT STATION 421 IAW BOEING SRM CHAPTER 51-30-2. (M) 2L72 4F RTA16WE 20050316000652005031600065NM 2005 3 16 UPS05M44049 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 10 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 10 LT PER SRM 51-21-01V.2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE 10 LT PER SRM 51-21-01V.2R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 10 LT & INSTALLED SLEEVE BUSHING PER MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 10 LT FOUND PER EN1122-05 & WITHIN LIMIT. 2L73 4F RTA22WE 20050316000802005031600080NM 2005 3 16 UPS05M44055 120041223A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE: C, NR 11 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION AT NR 11 RT BARREL NUT HOLE REMOVED PER SRM 51-21-01.V2.R35, OUT OF LIMIT. REWORKED NR 11 RT BARREL NUT HOLE PER EN1151-05. FAB SLEEVE BUSHING PER EO MD1 1-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE 11 RT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 11 RT PER EN1151-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317000362005031700036NM 2005 3 17 UPS05M44056 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 4 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 4 LT FOUND OUT OF LIMIT PER SRM 51-21-01 V.2 R.35. REWORKED BARREL NUT HOLE NR 4 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 4 LT & INSTALLED SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 4 LT PER EN 1117-05 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050317000422005031700042NM 2005 3 17 UPS05M44058 120041223A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 14 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION ON BARREL NUT NR 14 RT REMOVED PER SRM 51-21-01.V2.R35, FOUND OUT LIMIT. REWORKED BARREL NUT HOLE NR 14 RT PER SRM 51-21-01.V2.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 14 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 14 RT FOUND WITHIN LIMIT EN1154-05 & SATISFACTORY. 2L73 4F RTA22WE 20050317000492005031700049NM 2005 3 17 UPS05M44067 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 30 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 30 LT PER SRM 51-21-01.V2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 30 LT PER SRM 51-21-01.V2.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2OB BARREL NUT HOLE NR 30 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 30 LT PER EN1138-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001332005031700133NM 2005 3 17 UPS05M44079 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 12 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 12 RT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 12 RT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 12 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 12 RT PER EN 1152-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001352005031700135NM 2005 3 17 UPS05M44081 120041223A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 34 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 34 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 34 RT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 34 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409I. REPAIR COMPLETED ON BARREL NUT HOLE NR 34 RT PER EN1171-05 FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001752005031700175NM 2005 3 17 UPS05M44085 120041226A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 31 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED BARREL NUT HOLE NR 31 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 31 RT PER SRM 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 31 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1168-05 ON BARREL NUT HOLE NR 31 RT FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001762005031700176NM 2005 3 17 UPS05M44086 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 21 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 21 LT PER SRM 51-21-01 V.2R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 21 LT PER SRM 51-21-01 V.R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 21 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 21 LT PER EN 1130-5, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001782005031700178NM 2005 3 17 UPS05M44088 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 27 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 27 LT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 27 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 27 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 27 LT PER EN 1135-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001952005031700195NM 2005 3 17 UPS05M44091 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 30 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 30 RT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 30 RT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 30 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 30 RT PER EN1167-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20081231 NM 2008 12 31 DLM88081759 120041009A5312 PRESSURE PANEL DOUG MD88 MD88 3023688NM MLG WW DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27976DL 53257 FUSELAGE - MLG WHEEL WELL - SLANT PRESSURE PANEL REPAIR IAW 09-085387-12. C/W 09-085387-12 ME01. 2L72 4F RTA6WE 20050315003452005031500345NM 2005 3 15 BJNA041107 120041128A5340 STRINGER CLIP BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON TWO STRINGER TIE OF STRINGER 26L LOCATED AT STATION 947. REMOVED AND REPLACED CORRODED STRINGER TIE OF STRINGERS 26L AT STATION 947. STRINGER TIES WERE FABRICATED FROM 7075-T6 .063. WORK DONE IAW BOEING SRM 51-30-2. (M) 2L72 4F RTA16WE 20050317000792005031700079NM 2005 3 17 UPS05M44077 120041222A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 29 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 29 LT PER SRM 51-21-01.V2.R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 29 LT PER SRM 51-21-01.V2.R36 & EN1137-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 29 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409 -I. REPAIR COMPLETED PER EN1137-05 ON BARREL NUT HOLE NR 29 LT FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050317001342005031700134NM 2005 3 17 UPS05M44080 120041230A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 19 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 19 RT PER SRM 51-21-01.V2.R36, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 19 RT PER SRM 51-21-01.V2.R.36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 19 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1158-05, FOUND WITHIN LIMIT & SATISFACTORY ON BARREL NUT HOLE NR 19 RT. 2L73 4F RTA22WE 20050317001362005031700136NM 2005 3 17 UPS05M44082 120041211A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 18 LT CORROSION ON WALL, BASE AND BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 18 LT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 18 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 18 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED AT BARREL NUT HOLE NR 18 LT PER EN 1127-05, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001372005031700137NM 2005 3 17 UPS05M44083 120041226A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 5 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 5 RT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 5 RT PER SRM 51-21-01.V2.R36 & EN1146-05. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE ON NR 5 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 5 RT FOUND WITHIN PER EN1146-05 & SATISFACTORY. 2L73 4F RTA22WE 20050317002232005031700223NM 2005 3 17 UPS05M44092 120041223A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C, NR 26 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED AT BARREL NUT HOLE NR 26 LT PER SRM 51-21-01 V.2 R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 26 LT PER SRM 51-21-01 V.2 R.35. FAB SLEEVE BUSHING AS PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 AT BARREL NUT HOLE NR 26 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409 -I. REPAIR COMPLETED AT BARREL NUT HOLE NR 26 LT PER EN1134-05, FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050317002242005031700224NM 2005 3 17 UPS05M44093 120041226A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 20 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 20 LT PER SRM 51-21-01.V2.R35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 20 LT PER SRM 51-21-01.V2.R35. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 20 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED ON BARREL NUT HOLE NR 20 LT PER EN1129-05 FOUND WITHIN LIMIT. 2L73 4F RTA22WE 20050317002252005031700225NM 2005 3 17 UPS05M44094 120041220A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 23 LT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED & REWORKED CUTOUT ON BARREL NUT HOLE NR 23 LT PER SRM 51-21-01.V 2.R35, FOUND OUT OF LIMIT. FAB SLEEVE BUSHING PER EOMD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 23 LT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED PER EN1132-05 ON BARREL NUT HOLE NR 23 LT, FOUND WITHIN LIMIT & SATISFACTORY. 2L73 4F RTA22WE 20050317001562005031700156NM 2005 3 17 UPS05M44084 120041226A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01278UP 48577 INSPECTION TYPE:C NR 26 RT CORROSION ON WALL, BASE & BEARING SURFACE OF BARREL NUT HOLE. CORROSION REMOVED ON BARREL NUT HOLE NR 26 RT PER SRM 51-21-01.V2R.35, FOUND OUT OF LIMIT. REWORKED BARREL NUT HOLE NR 26 RT PER 51-21-01.V2.R36. FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. APPLIED SEALANT PR1422B1/2 ON BARREL NUT HOLE NR 26 RT & INSTALLED FAB SLEEVE BUSHING PER EO MD11-5510-19409-I. REPAIR COMPLETED BARREL NUT HOLE NR 26 RT FOUND WITHIN LIMIT PER EN1163-05 & SATISFACTORY. 2L73 4F RTA22WE 20050321000752005032100075WP 2005 3 21 IXXA0500004S 120040822A5720 DOUBLER DOUG DC8 DC873F 302199FWP WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING ROUTINE C-CHECK INSPECTION PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 36 PG 133-134. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, PERFORMED STOP HOLE ON CRACK END IAW DC8 SRM 57-2-1 PAGES 133, 134 FIG 36. FABRICATED EXTERNAL DOUBLER (AL 707576 0-160) INTERNAL DOUBLER (AL 7075 160. 063) IAW DC8 SRM 57-2-1 PAGES 133, 134 FIG 36. CLEANED, TREATED AND PRIMED AREA AND INTERNAL AND EXTERNAL DOUBLER IAW DCI SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED EXTERNAL AND INTERNAL DOUBLER WITH NEW FASTENERS IAW DC8 SRM 1-1-21 PG 1, SRM 51-1-29 PAGE 1, DC8 SRM 57-1-1 PG 133, 134, FIG 36. 2L74 4F RT4A25 20050321000762005032100076WP 2005 3 21 IXXA0500005S 120040817A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING CORROSION DAMAGE AROUND STA 1340.000, L-31 RT. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1 DC8, SRM 51-1-20D PG 21. REMOVED CORROSION IAW DC8 51-1-8 PAGES 17 & 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2. REMOVED CORRODED AREA IAW DC8 SRM 53-2-1 FIG 7 SHEET 3. CLEANED, TREATED & PRIMED. FABRICATED FINGER DOULBER, FILLER DOUBLER. CLEANED, TREATED AND PRIMED FINGER DOULBER, FILLER AND DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED SPACER IAW DC8 SRM 51-1-26. INSTALLED FILLER FINGER DOUBLER, DOUBLER WITH NEW FASTENERS. 2L74 4F RT4A25 20050321000792005032100079WP 2005 3 21 IXXA0500008S 120040818A5753 SKIN DOUG DC8 DC873F 302199FWP RT WING TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK MAINTENANCE FOUND RT OUTBOARD FLAP L/E HAS INTERIM REPAIR ON UPPER SKIN, STA XF 418.000. PERFORMED MAJOR REPAIR IAW DCI SRM 57-1-0 PG 1 DC8, SRM 57-7-1 FIG 4 (TR 5794). REMOVED PLATING WITH INTERIM REPAIR ON IT, IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW PLATING ( 2024T3 0.32) IAW DC8 SRM 57-7-1 FIG 4 (TR 57-94). CLEANED, TREATED AND PRIMED AREA + INNER FACE OF NEW PLATNG IAW DC8 SRM 51-1-8B. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21 PG 1 DC8, SRM 51-1-185 PG 1. 2L74 4F RT4A25 20050321000842005032100084WP 2005 3 21 IXXA0500011S 120040822A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION RT FUSELAGE AFT CENTER SECTION FLOORBEAM CORROSION DAMAGE STA 1480.000, RBL 47. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED AREA IAW DC8 SRM 51-2-7 FIG 1 PAGES 8-14 (SHEET 7). FABRICATED FILLER (AL 7075 T6 599-0.150) IAW DC8 SRM 51-2-1 FIG 1 (SHEET 1). CLEANED, TREATED AND PRIMED AREA FILLER AND REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SC8 SRM 51-1-11 PAGE 9. INSTALLED FILLER REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 1 PAGE 8-14 (SHEET 7-12), DC8 SRM 51-1-21 PAGE 1 DC9 SR, 51-1-20D PAGE 9. 2L74 4F RT4A25 20050321001292005032100129NM 2005 3 21 EIA2004147 120041203A3350 BULB BOEING747 747SR46 1384816NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09477EV 20784 AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK INOP. RELAMPED AFT EMERGENCY LIGHT BULB AT L1 DOOR MAIN CARGO DECK. GRN CHECKED NORMAL IAW MM 33-51-00. 2L74 4F RTA20WE 20050321001312005032100131NM 2005 3 21 EIA2004149 120041216A3350 BATTERY PACK BOEING747 747SR46 1384816NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09477EV 20784 U/D SILL LIGHT ON CREW EXIT DOOR INOP. REPLACED UPPER DECK BATTERY PACK ASSY IAW MM 33-51-04. 2L74 4F RTA20WE 20050321001322005032100132 2005 3 21 EIA2004150 420041219A3421TSG420101 INVERTER BOEING747 747132 1384882NM COCKPIT FAILED A EIAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09479EV 19898 STANDBY ATTITUDE TUMBLED; NO FLAG IN VIEW; INDICATOR WOULD NOT ERECT; STRONG ELEC SMELL IN COCKPIT; DECLARED EMERGENCY AND DIVERTED TO KJFK. REMOVED AND REPLACED INDICATOR AND INVERTER. INSPECT COCKPIT AREA FOR EVIDENCE OF ELECTRICAL SMELL. NO SUCH SMELL NOTED; SUSPECT SMELL FROM FAILED STANDBY INDICATOR. 2L74 4F A20WE 20050321001492005032100149EA 2005 3 21 SWIA200414705 120041220A5210 DOOR FRAME CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07591SW 7079 PAX DOOR FRAMES P/N 601R31902-5, -25, -26 TO -455 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FRAMES PART IAW REO 601R52-11-402, REV B. 2L72 4F RTA21EA 20050321001932005032100193NM 2005 3 21 EIA2004159 120041203A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 1520 S25L FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050321002342005032100234EA 2005 3 21 ASOA04800S 120041015A5320 SUPPORT ANGLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27900EV 7608 DURING C-CHECK, THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050321002502005032100250EU 2005 3 21 ASOA04954S 120041130A2120 ODOR AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN DETECTED A ASOAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO27632AS 338 DURING DESCENT, THE CREW NOTICED A MUSTY ODOR IN THE COCKPIT WHEN AIRCRAFT POWER WAS REDUCED FROM THE CRUISE POWER SETTING. NO FUMES OR SMOKE WAS OBSERVED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE LT PACK AND NO DEFECTS WERE NOTED. OPS CHECK GOOD. AC OK FOR SERVICE. (K) 2H72 4T4 TRTA53EU E20NE 20050321000802005032100080WP 2005 3 21 IXXA0500009S 120040818A5532 SKIN DOUG DC8 DC873F 302199FWP VERTICAL STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION MAINTENANCE PERFORMED A MAJOR REPAIR ON VERTICAL STABILIZER L/E UPPER SKIN. FOUND CORROSION AT STA ZFS 179.000. REMOVED CORROSION FROM VERTICAL STABILIZER L/E UPPER SKIN STA ZFS 179.000 IAW DC8 SRM 51-1-8 PGS 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-1 FIG 3 PGS 15, 16. REMOVED DAMAGED AREA IAW DC8 SRM 55-2-1 FIG 4 PAGE 17. FABRICATED FILLER (AL 7075 T6- 0.050) + DOUBLER (AL 707516 0.050) IAW DC8 SRM 55-2-1 FIG 4 PAGE 17. CLEANED, TREATED AND PRIMED FILLER AND DOUBLER INTERNAL PART IAW DC8 SRM 51-1-8B. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 55-2-1, SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D PAGE 9, DC8 SRM 51-1-11 PAGE 1. 2L74 4F RT4A25 20050321001282005032100128NM 2005 3 21 EIA2004146 120041122A3350 BATTERY PACK BOEING747 747212B 1384886NM EMERGENCY LIGHT INOPERATIVE A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 FOUND CREW DOOR SILL EMERGENCY LIGHT INOP DURING SERVICE CHECK. REMOVED AND REPLACED BATTERY PACK CARTRIDGE AND BATTERY PACK PER MM 33-51-00, OP'S CHECK OK. 2L74 4F A20WE 20050321001332005032100133NM 2005 3 21 EIA2004152 120041202A5313 STRINGER BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 FWD CARGO FS 983 S38L STRINGER END CRACKED AT BATHTUB 26 ATTACH. FWD CARGO STRINGER S38L AT FS 983 REPAIRED IAW SRM 53-10-03 FIG 1. 2L74 4F A20WE 20050322000312005032200031NM 2005 3 22 BJNA041105 120041128A5340 STRINGER CLIP BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON STRINGER TIES AT STATION 967 STRINGER 26L AND STRINGER 27L. REMOVED AND REPLACED CORRODED STRINGER TIES OF STRINGER 26L AND STRINGER 27L AT STATION 967. STRINGER TIES WERE FABRICATED FROM 7075-T6 .063. WORK DONE IAW BOEING SRM CHAPTER 51-30-2. (M) 2L72 4F RTA16WE 20050322000322005032200032NM 2005 3 22 BJNA041106 120041128A5320 BRACKET BOEING737 737282 13844ATNM FUSELAGE CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11233TM49031 23043 DURING A SCHEDULED C-CHECK INSPECTION, LEVEL TWO CORROSION WAS DISCOVERED ON A BRACKET LOCATED AT STATION 950 LBL 15. REMOVED AND REPLACED CORRODED BRACKET LOCATED AT STATION 950 LBL 15. BRACKET WAS FABRICATED FROM 7075-T6 .050. WORK DONE IAW BOEING SRM 51-30-2. (M) 2L72 4F RTA16WE 20050322000502005032200050WP 2005 3 22 2005F00034 120041215A7910 OIL SYSTEM DOUG DC9 DC982 3022082WP NR 2 ENGINE OVERSERVICED A GTIAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23829NK 49931 F/A REPORTED LIGHT TO MODERATE SMOKE IN FORWARD CABIN. UPON ARRIVAL FOUND NR 2 ENGINE OVERSERVICED, SERVICED OIL. REMOVED AND REPLACED BOTH COALESCER BAGS. NO EVIDENCE OF SMOKE WITH ENGINE/PACK OPERATION. (M) 2L72 4F A6WE 20050321000772005032100077WP 2005 3 21 IXXA0500006S 120040822A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE AFT PASSENGER DOOR UPPER CORNER DOOR JAMB CRACKED .5 INCH AT STA 1660.000 L-9 TO L-101. PERFORMED MAJOR REPAIR. REMOVED FASTENER, DAMAGED AREA AND FABRICATED FILLER, DOUBLER, AND TRIPLER. CLEANED, TREATED AND PRIMED AREA + FILLER + DOUBLER + TRIPLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED FILLER, DOULBER AND TRIPLER WITH NEW FASTENERS PER ALL APPLICABLE MANUALS. 2L74 4F RT4A25 20050321000782005032100078WP 2005 3 21 IXXA0500007S 120040817A5300 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION, EXTERNAL FUSELAGE CRACKED .75 INCH FROM STA 1718.000 TO STA 1719.000. MAINTENANCE PERFORMED MAJOR REPAIR IAW DC8 DRM 53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. REMOVED CRACKED AREA IAW DC8 SRM 51-1-21 PG 1. REMOVED CRACKED AREA IAW DC8 SRM 53-2-1 (SHEET3, 5). FABRICATED DOUBLER (AL 707576 0.63), FINGER DOUBLER (AL 707516 0.32), FILLER (AL 707516 0.050) IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3, 5). CLEANED, TREATED AND PRIMED AREA, FINGER DOUBLER FILLER AND DOUBLER IAW DC8 SRM 51-1-8B, INSTALLED DOUBLER, FINGER DOUBLER AND FILLER WITH NEW FASTENERS IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 3, 5) DC8 SRM 51-1-1 PG 1, DC8 SRM 51-1-200 PG 9, DC8 SRM 51-1-11 PAGE 9. 2L74 4F RT4A25 20050321000832005032100083WP 2005 3 21 IXXA0500010S 120040822A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING ROUTINE C-CHECK INSPECTION RT FUSELAGE AFT CENTER SECTION FLOORBEAM CORRSION DAMAGE STA 1460.000, RBL 48 WAS FOUND. REMOVED CORROSION IAW DC8 SRM 51-1-1 PAGES 17, 18, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PGS 20. REMOVED CORRODED AREA IAW DC8 SRM 51-2-1 FIG 1, PAGES 8-14 (SHEET 3). FABRICATED FILLER (AL 7075 T6 0.125) + REPAIR ANGLE (EXTRUSION 7075T6 0.150) IAW DC8 SRM 51-2-18 FIG 1 (SHEET 7). CLEANED, TREATED AND PRIMED AREA AND FILLER AND REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW DC8 SRM 51-1-11 PG 9. INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 1 (SHEET 7, 12) DC8 SRM 51-1-21 PAGE 1, DC8 SRM 51-1-20D PAGE 9. 2L74 4F RT4A25 20050321001302005032100130NM 2005 3 21 EIA2004148 120041214A7160 FAIRING BOEING747 747132 1384882NM NR 2 ENGINE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09479EV 19898 FOLDING FAIRING (BULL NOSE) NR 20, 2ND INBOARD OF NR 4 ENGINE DAMAGED. REMOVED NR 20 BULLNOSE IAW CDL 27-81-0 DMI 339 ENTERED. 2L74 4F A20WE 20050324000192005032400019NE 2005 3 24 ASMF200502014 220040226A7412103538754 EXCITER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23754RA312 49641 696354 WITH LEFT IGNITION SYSTEM IN OVERRIDE, THE LEFT ENGINE DID NOT START. THE CIRCUIT BREAKER C/B U42 WAS REESTABLISHED BUT FAILURE CONTINUED. THE LEFT IGNITION C/B WAS DEFERRED IAW MEL 74-A BUT DURING PUSH BACK, THE LEFT ENGINE IGNITION WAS OUT SERVICE AGAIN. THE LEFT SIDE EXCITER IGNITION WAS REPLACED IAW MM 74-10-01, TESTED CORRECT. DURING OVERNIGHT SERVICE, IGNITION SYSTEM WAS TESTED IAW MM 74-10-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050324000862005032400086NM 2005 3 24 2005UALA00099 120040126A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29597UA 28750 LT EXT FUSELAGE SKIN AT BS 620 AND STR 16L IS DENTED. INSTALLED PARTIAL SKIN REPLACEMENT USING DOUBLERS AND TRIPLERS. 2L72 4F4 FRTA2NM E17NE 20050325001192005032500119NM 2005 3 25 EIA2004153 120041203A5311 FRAME BOEING747 747132 1384882NM FUSELAGE DEFORMED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 2020 BETWEEN ST 13-14 RT FRAME 1/3 CHORD FOUND DEFORMED. FRAME REPAIRED PER SRM 53-10-04 FIG 1. 2L74 4F A20WE 20050328000422005032800042 2005 3 28 KBM2005F00014 420040414A34215040032902 INDICATOR SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1C 60030NE ATTITUDE INTERMITTENT E KBMAK NONE O OTHER ININSP/MAINT 1 WP1953SH 2009 ATTITUDE INDICATOR, WILL NOT HOLD ATT, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050405000172005040500017WP 2005 4 5 ASAA0580022 120040123A575359100433 VANE DOUG DC9 DC983 3022083WP TE FLAP CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT OUTBOARD FLAP VANE CHAFED INBOARD EDGE. REMOVED DAMAGE. INSTALLED FILLER AND REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000292005040500029WP 2005 4 5 ASAA0580023 120040123A531159135963 FRAME DOUG DC9 DC983 3022083WP FUSELAGE GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, RIGHT TAIL COMPARTMENT FRAME IS GOUGED. REMOVED DAMAGE. INSTALLED REPAIR PLATE AND ANGLE. (M) 2L72 4F RTA6WE 20050405001172005040500117WP 2005 4 5 IXXA0500040S 120041011A5513 PLATE DOUG DC8 DC873F 302199FWP HORIZONTAL STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, RT HORIZONTAL STAILIZER OUTBOARD LEADING EDGE UPPER PLATING CORROSION DAMAGE BETWEEN STA XFS 172.000 AND XFS 335.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS AND CORROSION. FOUND OUT OF LIMITS, REMOVED CORROSION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPLACEMENT, AN EXTERNAL REPAIR DOUBLER AND TWO FILLERS. CLEANED, TREATED AND PRIMED THE REPLACED SECTION OF SKIN DOUBLER INTERIOR SURFACE AND FILLERS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PART ON RT HORIZ STAB O/B L/E UPPER PLATING USING NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL, BOEING ROD SKETCH 04-9-23-004 AND BOEING MESSAGE 1-PPR41, 1-Q821M A1-PPR43H, 2L74 4F RT4A25 20050405001772005040500177NM 2005 4 5 72300047 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 INCH BY 16 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050405001782005040500178NM 2005 4 5 72300048 120041026A5313 STRINGER BOEING727 7272H3 138368NNM ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 8 INCH AREA OF CORROSION ON STRINGER. 2L73 4F RTA3WE 20050406000182005040600018WP 2005 4 6 IXXA0500021S 120040827A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, THE RT FUSELAGE AFT CENTER SECTION FLOORBEAM HAS CORROSION DAMAGE AT STA 1300.000 RBL 48 INCH. MAJOR REPAIR WAS ACCOMPLISHED. REMOVED CORROSION IAW DC8 SRM 51-1-8 PGS 17-18. FOUND OUT OF LIMITS IAW EC8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED AREA IAW DC8 SRM 51-2-1 FIG 1 PAGES 8-14 (SHEET 7). FABRICATED FILLER (AL 7075 76. 0.125"0 )+ REPAIR ANGLE (EXTRUSION 7075.TG 5110.0150") IAW DC8 SRM 51-2-1 FIG 1 (SHEET 7). CLEANED TREATED AND PRIMED AREA, FILLER & REPAIR ANGLE IAW DC8 SRM 51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PAGE 9. INSTALLED FILLER AND REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-2-1 FIG 1(SHEET 7,12) DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050406000192005040600019WP 2005 4 6 IXXA0500020S 120040830A5754 SKIN DOUG DC8 DC873F 302199FWP LT WING TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER PLATING HAS INTERIM REPAIR AT STA XF 1340.000. MAJOR REPAIR ACCOMPLISHED. REMOVED SKIN WITH INTERIM REPAIR ON IT IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-3-0 PG1. FABRICATED NEW SKIN (AL2024130.050") IAW DC8 SRM 57-7-1 PG 2 FIG 4 TR NR 57-94. CLEANED, TREATED AND PRIMED AREA + INNER FACE OF SKIN IAW DC8 SRM 51-1-8B. INSTALLED NEW SKIN AND FASTENERS IAW EC8 SRM 51-1-21 PG1 DC8 SRM 51-3-0 PG1. 2L74 4F RT4A25 20050406000372005040600037WP 2005 4 6 IXXA0500033S 120040811A5310 DOOR FRAME DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE FORWARD PASSENGER DOOR UPPER FORWARD JAMB CORNER INTERIM REPAIR AROUND STA 25.000, L-8L TO L-10L. REPAIR ACCOMPLISHED, REMOVED INTERIM REPAIR, FABRICATED DOUBLER AND TRIPLER. CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED DOUBLER AND TRIPLER WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWINGS DACO SR 08530021 AND 5750776. 2L74 4F RT4A25 20050406000872005040600087EA 2005 4 6 MASA200400581 120041016A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ENGINE ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07652ML 7036 ASH 2870 TRI-CLT, ABORTED TAKEOFF DUE TO MULTIPLE MASTER WARNINGS DURING TAKEOFF ROLL. DEPOWERED AND REPOWERED AIRCRAFT. OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20050406001082005040600108EA 2005 4 6 MASA200400637 120041114A3230864808 PSEU CNDAIRCL600 CL6002B19 1900309EA MLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07372288804 7228 ASH 6424 FROM PHX TO DSM, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A GEAR DISAGREE MESSAGE AFTER TAKEOFF. THE GEAR HANDLE WAS SELECTED DOWN AND THE GEAR EXTENDED NORMALLY. THE AIRCRAFT THEN LANDED UNEVENTFULLY. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. 11/14/04 MAINTENANCE REMOVED AND REPLACED PSEU. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050406001542005040600154NM 2005 4 6 ASA0440410 120041231A5315654681025 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON FLOORBEAM, STA 967 LBL 14-48, WL 208. REPAIRED 967 FLOORBEAM UPPER FLANGE IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050406001642005040600164NM 2005 4 6 ASA044408 120041231A57206550820223 ANGLE BOEING737 7374Q8 138447QNM LT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - LT WING T/E LWR ANGLE CRACK ON UPPER T/E PANEL. REMOVED, FABRICATED AND REPLACED ANGLE. (K) 2L72 4F RTA16WE 20050407000492005040700049NM 2005 4 7 72300147 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050407000502005040700050NM 2005 4 7 72300148 120041028A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 1 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050407000512005040700051NM 2005 4 7 72300149 120041102A5315 FLOORBEAM BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 TWO 1 X 1 INCH AREAS OF CORROSION ON FLOORBEAM CHORD. 2L73 4F4 FRTA3WE E2EA 20050405001142005040500114WP 2005 4 5 IXXA0500037S 120040927A5712 RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT STUB WING NR 1 STRUCTURE RIB WITH CRACK DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED CRACKED RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW RIB ON LT WING NR 1 STUB WING PER DOUGLAS STRUCTURAL MANUAL, REPAIR SPEC NR 2003-05 AND DRAWING NR 9753297. 2L74 4F RT4A25 20050405001592005040500159NM 2005 4 5 72300041 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 16 INCH AREA OF CORROSION ON BOTTOM OF STRINGER 2L73 4F4 FRTA3WE E2EA 20050405001742005040500174NM 2005 4 5 72300045 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH AREA OF CORROSION ON S-26R. 2L73 4F4 FRTA3WE E2EA 20050405001992005040500199NM 2005 4 5 72300056 120041028A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 INCH BY 5 INCH AREA OF CORROSION ON FRAME WEB. 2L73 4F4 FRTA3WE E2EA 20050406000092005040600009EA 2005 4 6 MASA200400679 120041203A32204622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07593ML1663 7465 ASH 2789 FROM MCI-DCA RETURNED TO THE FIELD DUE TO A GEAR DISAGREE MESSAGE AND NOSE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT WAS FERRIED TO OKC,AAR FOR TROUBLESHOOTING AND REPAIR 12/3/04 MAINTENANCE REPLACED PRIORITY VALVE, ADJUSTED PROX SWITCH AND PSEU. OPS CHK GOOD. 2L72 4F RTA21EA 20050406000202005040600020WP 2005 4 6 IXXA0500022S 120040827A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND FLOORBEAM CORROSION ON RT FUSELAGE AFT CENTER SECTION AT STA 15000.000 RBL 48 INCH. MAJOR REPAIR ACCOMPLISHED IAW DC8 SRM 51-2-1 FIG 1 PAGES 8-14 (SHEET 7,12) TR NR 51-1-30. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PG 2P. REMOVED CORRODED AREA IAW DC8 SRM 51-2-1 FIG 1 PG 8-14 (SHEET 7). FABRICATED FILLER (AL 7075.+6 0.125") + REPAIR ANGLE (EXTRUSION 7075-T.6 0.150") IAW DC8 SRM 51-2-1 FIG PAGES 8-14 (SHEET 7). CLEANED, TREATED AND PRIMED AREA + FILLER + REPAIR ANGLE IAW DC8 SRM 51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9 INSTALLED FILLER + REPAIR ANGLE WITH NEW FASTENERS IAW DC8 SRM 51-1-1 F2L74 4F RT4A25 20050406000402005040600040WP 2005 4 6 IXXA0500036S 120040927A5343 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR FRAME FITTING CRACK DAMAGE AT STA 98.000, BETWEEN L-19R AND L-24. REPAIR ACCOMPLISHED. REMOVED THE CRACKED FITTING, CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050407001402005040700140NM 2005 4 7 ASA044407 120041231A53306545770 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON UPPER FUSELAGE SKIN AROUND ANTENNA CUTOUT STA 620 BETWEEN STRINGER 1 AND 2R. REPAIRED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050406000102005040600010EA 2005 4 6 MASA200400691 120041211A2612355924400 ELEMENT CNDAIRCL600 CL6002B19 1900309EA FIRE DETECTOR BROKEN A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07715SF 7115 CLOSED 2748 FROM PHL TO DTW, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A COWL ANTI-ICE FAIL AND 14TH STAGE BLEED FAIL. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING. 12/11/04, MAINTENANCE REPLACE PYLON LOOP A OPS CHECKED GOOD. 2L72 4F RTA21EA 20050406000262005040600026NM 2005 4 6 72300067 120041021A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050407002822005040700282NM 2005 4 7 AWXA200500045 120041228A53206545834552 INTERCOSTAL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 326, RBL 34, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 326, RBL 34; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2L72 4F RTA16WE 20050406001632005040600163NM 2005 4 6 ASA044406 120041231A532065C1730887 SUPPORT BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON SIDEWALL SUPPORT. REPLACED IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050408000492005040800049EA 2005 4 8 MASA200400683 120041205A5210 HANDLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR MALFUNCTIONED A MASAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0727191 7191 ASH 2606 PHL - BGR - PAX DOOR HANDLE WILL NOT STOW FROM INSIDE OF AIRCRAFT. MAINTENANCE TROUBLESHOT AND FOUND NO FAULTS. 2L72 4F RTA21EA 20050408000632005040800063NE 2005 4 8 MASA200400689 220041211A72006087T15G01 GEARBOX CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENG 2 DAMAGED A MASAK NONE O OTHER ININSP/MAINT 1 SW0737342 7342 872622 ASH N37342, E2 WEAR TO THE AXIS BB GEARSHAFT CONTACT SURFACES WAS FOUND DURING A SCHEDULED BORESCOPE INSPECTION OF THE GEAR BOX ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20050408000932005040800093NM 2005 4 8 72300004 120041023A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .75 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050408000942005040800094NM 2005 4 8 72300005 120041025A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 2.5 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050408000952005040800095NM 2005 4 8 72300006 120041024A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050408001072005040800107EA 2005 4 8 MASA200400672 120041201A21507546911 SENSOR CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK INOPERATIVE A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07401MJ 7316 ASH 2770 PHL - BNA - CREW REPORTED SMOKE IN THE CABIN AREA AND THE LEFT PACK OVERHEATED AND DIVERTED TO IAD. MAINTENANCE FOUND THE LEFT HAND PACK FAIL. DEFERRED THE LEFT PACK AND CLEARED SMOKE FROM THE CABIN. 12/7/04 MAINTENANCE REPLACED DUCT TEMP SENSOR. 2L72 4F RTA21EA 20050407002392005040700239SO 2005 4 7 CHQA00050 120040903A3350 LIGHT EMB 135 EMB135LR 3260305SO CABIN INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11845RP 145551 LEFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 135 AMM 33-50-10. OPS CHECK GOOD. 2L72 4F RTT00011AT 20050408000482005040800048EA 2005 4 8 MASA200400664 120041129A2150 A/C PACK CNDAIRCL600 CL6002B19 1900309EA CONTAMINATED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW0777195 7195 ASH 6605 DTW - THE PILOT REPORTED AN UNUSUAL BURNING SMELL WITH THE BLEED ON. ON CALL MAINTENANCE WAS DISPATCHED AND TROUBLESHOT THE PROBLEM TO BE DE-ICE FLUID ON THE PACK DUCTS. MAINTENANCE CLEANED THE FLUID, RAN THE SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT CONTINUED REVENUE SERVICE. 2L72 4F RTA21EA 20050407002842005040700284NM 2005 4 7 AWXA200500046 120041228A53206545834551 INTERCOSTAL BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 342, LBL 46, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL FROM BS 328 TO BS 344, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG 8 AND 12. 2L72 4F RTA16WE 20050407003272005040700327NM 2005 4 7 72300131 120041024A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 5 X 2 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050411001152005041100115NM 2005 4 11 2004UALA00132 120040216A3397W2070W2072W23 WIRE HARNESS BOEING757 757222 1384956NM PWA 2037 PW2037 NE P34 PANEL DAMAGED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29556UA 26650 EQUIPMENT CTR LIGHT, DRAIN MAST HTR GND, SEAT BELT SIGNS, RT FWD ENTRY AND ATTENDANT LIGHTS, FUEL VALVE QTY CTL LIGHT, SIDEWALL LIGHT, RT SIDEWALL LIGHT, CONT SIDEWALL LIGHT, ENTRY GALLEY LIGHTS, RT CEILING LIGHT AND CTL CEILING CIRCUIT BREAKERS FOUND POPPED. *S/D* WIRES BELONGING TO BUNDLES: W2070, W2072, W2356, W3576 AND W3614 WERE FOUND WITH EXTENSIVE OVERHEAT DAMAGE NEAR THE P34 ELECTRICAL PANEL. THERE IS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE OVERHEAT DAMAGE, POSSIBLE EXISTING DEGRADATION TO THE WIRE INSULATION, TYPICAL TO THE WIRE TYPE BMS13-51 - PLAIN KAPTON. WIRE BUNDLES WERE REPAIRED USING ENVIRONMENTAL SPLICES PER BSWM 20-10-13. 2L72 4F4 FRTA2NM E17NE 20050411001772005041100177EA 2005 4 11 MASA200400732 120041229A3150 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA COCKPIT ILLUMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0717175 7175 OPEN - ASH 9710 DTW-PIT PILOT DIVERTED DUE TO NO STARTER CUTOUT CAUTION IN FLT AND STALL FAIL IN FLIGHT. AIRCRAFT FERRIED TO CLT WHERE MAINTENANCE IS TROUBLESHOOTING. 2L72 4F RTA21EA 20050411001852005041100185NM 2005 4 11 72300008 120041020A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050411001862005041100186NM 2005 4 11 72300009 120041025A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH CRACK IN SHEAR TIE RADIUS. 2L73 4F4 FRTA3WE E2EA 20050411001882005041100188NM 2005 4 11 72300011 120041026A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050411001892005041100189NM 2005 4 11 72300012 120041020A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050411001912005041100191WP 2005 4 11 IXXA0500023S 120040829A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, RT WING TOP PANEL PLATING HAS CRACK DAMAGE STA XRS 74.000, S-9. MAJOR REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1 FIG 17 PG 87, 88 1. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-1 PAGES 87, 88 FIG 17. FABRICATED DOUBLER (AL 7075 T6 0.160") IAW SRM 57-2-1 PGS 87, 88 FIG 17. CLEANED, TREATED AND PRIMED DOUBLER, FILLER AREA IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SUFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED DOUBLER AND FILLER WITH NEW FASTENERS IAW DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20050411001932005041100193WP 2005 4 11 IXXA0500026S 120040823A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND FLOORBEAM CORRODED AT STA 1400.00 RBL 45". REPAIR WAS ACCOMPLISHED, CORROSION WAS REMOVED. FABRICATED FILLER & REPAIR ANGLE. CLEANED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED FILLER & ANGLE DOUBLER PER THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050411001752005041100175NM 2005 4 11 72300007 120041024A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH CRACK IN PREVIOUS SHEAR TIE REPAIR ANGLE RADIUS. 2L73 4F4 FRTA3WE E2EA 20050412002972005041200297WP 2005 4 12 ASAA0580021 120040123A552359304971 TAB DOUG DC9 DC983 3022083WP LT ELEVATOR DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, LEFT ELEVATOR ANTI-FLOAT TAB MISSING COMPOUND. REPLACED MISSING COMPOUND. (M) 2L72 4F RTA6WE 20050414000542005041400054SO 2005 4 14 CHQA000551 120040904A3350 BATTERY EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11287 145460 BOTH OVERWING EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY IAW EMB 145 AMM 33-50-04. 2L72 4T RTT00011AT 20050414000612005041400061GL 2005 4 14 CHQA000577 220041030A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 MAKING METAL A CHQABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL11279 11745781 145379 CAE311220 DURING CRUISE ON FLT 3103 FROM LGA TO SDF, THE FLIGHT CREW HEARD A LOUD BANG. THE ITT DROPPED TO THE AMBER RANGE, AN EICAS E2 OUT MESSAGE APPEARED, AND THE ENGINE SHUTDOWN. THE QRH WAS RAN AND ABOUT 35 MINUTES OUT FROM SDF, AN EMERGENCY WAS DECLARED. DURING LANDING AN EICAS E2 EXCEEDED MESSAGE AND AN E2 SHORT DISPATCH MESSAGE APPEARED. MAINTENANCE INSPECTED THE ENGINE AND FOUND METAL SHAVINGS IN THE EXHAUST SECTION. REMOVED AND REPLACED NR 2 ENGINE. MAINTENANCE PERFORMED GROUND RUNS OF NR 2 ENGINES WITH NO LEAKS NOTED. OPS CHECK GOOD. 2L72 4T4 FRTT00011ATTE6CH 20050414000642005041400064NE 2005 4 14 VIBA20040916 220040916A73213036359 FUEL CONTROL BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE LT ENGINE FAILED E VIBAO OTHER O OTHER NRNOT REPORTED 1 SO13771MG BB1636 PCEPJ0228 THE FUEL PUMP DRIVE SHAFT BEARING ASSEMBLY APPARENTLY FAILED OVER AN UUNDETERMINED PERIOD OF TIME, LEADING TO SHAFT LOCK UP AND SHEARED THE DRIVE COUPLING. BLACK RESIDUE FROM THE BEARING FAILURE WAS FOUND TO BE EMITTING FROM THE GANG DRAIN AND STREAKING BACK ON THE LT OB MAIN GEAR DOOR OF THE AIRCRAFT. THE LT ENGINE WAS SHUTDOWN DUE TO UNCONTROLLED ENGINE TEMPERATURE AND TORQUE RISE RESULTING FROM THE FUEL CONTROL FAILURE. AC LANDED WITHOUT INCIDENT. PROBABLE CAUSE WAS THAT THE FC SHAFT BEARING ASSEMBLY SEAL FAILED. WASHING OUT THE GREASE IN THE BEARING CAGE LEADING TO THE FAILURE OF THE FUEL CONTROL. FUEL PUMP WAS ALSO REPLACED AS PRECAUTIONARY MEASURE. 1L72 4T4 T A24CE E4EA 20050414000652005041400065NM 2005 4 14 C7WA20040922 120040922A5322 SHEAR TIE BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 SHEAR TIE CORRODED AT STA 950A BETWEEN STR 28 AND STR 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11 MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES. 2L73 4F4 F A3WE E2EA 20050414000672005041400067NE 2005 4 14 SOKF20041118 220041118A7200 ENGINE AIRBUS320 A320233 3930329EU IAE V2527 V2527EA5 NE NR 2 FOD W SOKFA UNSCHED LANDING C F.O.D. LDLANDING 1 SO23465TA 1374 V10828 DURING LANDING, CAPTAIN REPORTED (FOD ON ENGINE NR 2, NO ABNORMAL INDICATION DURING TAXI). MAINT PERFORMED INSPECTION OF ENGINE NR 2 IAW MM AND FOUND SOME DAMAGES LOCATED ON ATTRITION LININGS AT 5 OCLOCK, ACOUSTIC PANEL AT 4:30, (ENGINE, FROM THE FRONT), SOME SCORES ON INNER BARREL OF INTAKE COWL: ALL OF THEM ACCEPTABLE IAW MM. ALSO FOUND DAMAGES OUT OF LIMITS ON FAN BLADES, POSITIONS: 9,13,14,15,16,17,18,20, WHICH WERE REMOVED AND REPLACED IAW AMM. A FRONT LINER PANEL AT 4 OCLOCK IAW AMM, ADDITIONALLY WAS REPLACED THE RUBBER SEAL AT 5 OCLOCK DUE TO DAMAGES, PERFORMED TEST NR 8 VIBRATION SURVEY IAW AMM AND TEST NR 9. FAN TRIM BALANCE IAW AMM WITH SATISFACTORY RESULTS AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E40NE 20050414000692005041400069NM 2005 4 14 04FDEA03311 120041201A5720ARC199114 SUPPORT BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL THICKNESS=0.505, REMAINING THICKNESS=0.495, MATERIAL REMOVED=0.010 AND REPAIRED AS PER FEDEX EA 1-5750-77983. 2L73 4F RTA22WE 20050414000712005041400071NM 2005 4 14 04FDEA03393 120041208A5711ARB7411 SPAR DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 LT WING OUTBOARD AILERON OUTBOARD SIDE AT APPROX XORS 1048 FOUND CORROSION AT LOWER CHORD REAR SPAR CAVITY. REPAIR CARRIED OUT IAW FEDEX EA 1571081640. 2L73 4F RTA22WE 20050414001212005041400121NM 2005 4 14 AWXA200500126 120041227A553465537448 CHANNEL BOEING737 7373Q8 1384670NM VERTICAL STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A 1/2" CRACK WAS FOUND IN VERTICAL STABILIZER LOWER ANGLE (CHANNEL) ON AFT SIDE OF RT AFT LUGS BS 1016, STR 2 RT. MAINTENANCE REMOVED CRACKED VERTICAL STABILIZER LOWER CHANNEL AT BS 1016, STR 2 RT; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-53744; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050414000622005041400062EU 2005 4 14 HXSD2004517 120040507A6410355A12005004 BLADE SNIAS 350 AS350B3 8680954EU TMECA ARRIELARRIEL2B NE TAIL ROTOR CRACKED B HXSDO OTHER O OTHER NRNOT REPORTED 1 AL05405AE 3286 INSPECTOR FOUND CRACK IN TAIL ROTOR PROTRUDING OUT OF RIVET LOCATION ON TRIM TAB. CRACK WAS FOUND DURING INSPECTION IAW AD 2001-26-55. (AL05200402466) 1G71 3U3 U H9EU E00054EN 20050414000832005041400083NM 2005 4 14 2005UALA00059 120040116A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29580UA 26698 AFT PIT STA 1460 FRAME DENTED STR 26 LT ON INNER FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050414001222005041400122NM 2005 4 14 AWXA200500127 120041222A5330 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28327AW 23507 MCN - MAJOR REPAIR - DURING C-17 CHECK A TWO 1 INCH CRACKS WERE FOUND IN FUSELAGE SKIN EMANATING FROM FASTENER HOLES AT R-1 DOOR UPPER FORWARD CORNER CUTOUT BS 300-305, STR 7-8 RT. MAINTENANCE REMOVED CRACKED VERTICAL STABILIZER LOWER CHANNEL AT BS 1016, STR 2 RT; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 65-53744; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02. 2L72 4F RTA16WE 20050415001072005041500107SW 2005 4 15 YTRR099230 120040909A7712222375077119 TRANSDUCER BELL 407 407 1182206SW ENGINE TORQUE FAILED B YTRAO OTHER O OTHER NRNOT REPORTED 1 SW03594RL545 53594 ENGINE TORQUE TRANSDUCER FAILED. 1G71 3U O H2SW 20050418001632005041800163EU 2005 4 18 USAA041133 120041213A5347F53311325200 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .031 INCH DEEP BY 4 INCH LONG BY 2 INCHES WIDE. REMOVED AND REPLACED PER SRM 53-31-15. (M) 2L72 4F RTA46NM 20050418001652005041800165EU 2005 4 18 USAA041136 120041215A5347J727053500006 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED .100 INCH LONG BY 1.5 INCH WIDE BY .050 INCH DEEP, FS 72, Y-1202. REMOVED AND REPLACED PER SRM 53-00-15-101, 53-41-15-101, 51-42-11, 51-44-11. CORROSION LEVEL 2, TASK NR J7-270-53500. (M) 2L72 4F RTA46NM 20050418001872005041800187EU 2005 4 18 USAA041134 120041216A5347F5347721420100 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED VARIOUS LENGTHS, WIDTHS AND DEPTHS, -Y450 FROM FRAME 59-68, 8 AREAS. CORROSION LEVEL 2, TASK NR J7-200-2580C-004. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 51-42-11, 51-72-11, 51-43-11. (M) 2L72 4F RTA46NM 20050418001882005041800188EU 2005 4 18 USAA041135 120041215A5347F5347821720000 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW22421 0315 BFM - FOUND SEAT TRACK CORRODED 2 INCHES BY .250 INCH BY .032 INCH, 1 INCH BY .250 INCH BY .034 INCH, Y 460, FRAME 72-73, 73-74, 74-75, 1.5 INCH BY .500 INCH BY .060 INCH. REMOVED AND REPLACED PER SRM 51-72-11, 51-42-11, 53-00-15 FIG 101. (M) 2L72 4F RTA46NM 20050415001872005041500187NM 2005 4 15 P9RA20040056A 120041222A3397 CONNECTOR BOEING757 757231 1384950NM EMERGENCY LIGHT LOOSE A P9RAK NONE O OTHER ININSP/MAINT 1 SO11720TW 30319 A/C IN CCS, AFT CABIN EMERGENCY LIGHTS INOP. T/S AFT CABIN EMERGENCY LIGHTS FOUND CANNON PLUG NR D80 LOOSE, TIGHTEND CANNON PLUG NR 80 IAW WD 33-51-15 TEST LIGHT OK. NO PARTS CHANGED. 2L72 4F RTA2NM 20050420000682005042000068NM 2005 4 20 FRISBY05001 120040603A292041022021 HOUSING DOUG MD80 MD83 3023681NM DRAIN PORT CRACKED B O OTHER O OTHER NRNOT REPORTED 1 SO05 16764 461C PTU, P/N 4100310-6, S/N 461 WAS REMOVED FROM JAPAN AIRLINES MD-80 AIRPLANE DUE TO NOISY OPERATION AND HOT TEMPERATURE OF THE PTU BODY. THE PTU WAS DISASSEMBLED IN THE SHOP, WHICH REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1 HAD CRACKED COMPLETELY AROUND THE CIRCUMFERENCE. SUBJECT HOUSING HAD ACCUMULATED 16,764 HOURS SINCE INSTALLATION IN ACCORDANCE WITH SB 4100310-29-0031 (AD 94-22-03). THE FAILED DRAIN PORT HOUSING WAS FORWARDED TO FRISBY AEROSPACE FOR A FAILURE INVESTIGATION. 2L72 4F RT 20050422000062005042200006 2005 4 22 04UALA01181 420041202A2565D31517113 SLIDE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE DOOR 2 LT UNSERVICEABLE A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29433UA 7391 589 DURING OVERHAUL OF DOOR TWO LEFT SLIDE THE MOORING LINE WAS FOUND TO BE PACKED IN BETWEEN GIRT HALVES. THE INFLATION CABLE WAS NOT RUN IN CABLE GUIDE BUT RUN THROUGH LACING GROMMET INSTEAD, THE SLIDE WAS FOLDED INSTEAD OF ROLLED AND WAS PACKED OVER BOTTLE AND ASPIRATOR. SUPPLEMENTAL DATA UPDATE OVERHAULED SLIDE AND REPACKED CORRECTLY. 2L72 4F4 FRTA28NM E40NE 20050422000622005042200062NM 2005 4 22 EIA2004158 120041003A5311 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09481EV 19896 M/D BS 1500 S24L FRAME FOUND CRACKED. FRAME REPAIRED PER SRM 53-10-04 FIG 4. 2L74 4F A20WE 20050420000692005042000069NM 2005 4 20 FRISBY05002 120040628A292041022021 HOUSING DOUG MD80 MD83 3023681NM DRAIN PORT CRACKED B D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO05 18504 945C 1584 ON JUNE 28, 2004, ALITALIA MD-80 FUSELAGE 1584 HAD A PILOT REPORT OF RETURN TO PARKING BECAUSE LT HYDRAULIC TEMPERATURE HI LIGHT ON. GROUND MAINTENANCE CHECK REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1, INSTALLED ON PTU, P/N 4100310-6, S/N 945C HAD CRACKED COMPLETELY AROUND THE CIRCUMFERENCE. THE SUBJECT HOUSING HAD ACCUMULATED 18,504 HOURS SINCE INSTALLATION IN ACCORDANCE WITH SB 4100310-29-0031 (AD 94-22-03). THE FAILED DRAIN PORT HOUSING WAS FORWARDED TO FRISBY AEROSPACE FOR A FAILURE INVESTIGATION. 2L72 4F RT 20050420000702005042000070NM 2005 4 20 FRISBY05003 120041225A292041022021 HOUSING DOUG MD80 MD83 3023681NM DRAIN PORT CRACKED B O OTHER J WARNING INDICATION LDLANDING 1 SO05 20765 915C AFTER LANDING ON DECEMBER 25, 2004, THE FLIGHT CREW OF AN ALITALIA MD-80 REPORTED THE HYDRAULIC PRESSURE OF BOTH HYDRAULIC SYSTEMS WENT TO ZERO, BUT THE HYDRAULIC PRESSURE RETURNED TO NORMAL VALUE WITH THE AUXILIARY AND TRANSFER PUMP OFF. GROUND MAINTENANCE CHECK REVEALED THE DRAIN PORT HOUSING, P/N 4102202-1, INSTALLED ON PTU, P/N 4100310-6, S/N 915C, HAD CRACKED COMPLETELY AROUND THE CIRCUMFERENCE. THE PTU HAD ACCUMULATED 29,686 TSN AND 32,667 CSN, AND THE SUBJECT HOUSING HAD ACCUMULATED 20,765 HOURS AND 22,664 CYCLES SINCE INSTALLATION IN ACCORDANCE WITH SB 4100310-29-0031 (AD 94-22-03). THE FAILED DRAIN PORT HOUSING WAS FORWARDED TO FRISBY AEROSPACE FOR A FAILURE INVESTIGATION. 2L72 4F RT 20050425001692005042500169WP 2005 4 25 COOSDR040043 120041015A5532 PANEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE VERTICAL STAB CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23825BX 45978 VERTICAL STABILIZER, LT SIDE PANEL CORRODED AND DELAMINATED, LOCATED FROM STA ZR 253.000 TO STA ZV 299.125. (K) 2L74 4F4 FRT4A25 E2GL 20050425001722005042500172 2005 4 25 2004UALA01215 420041214A2565300267105 FITTING BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE BOTTLE LEAKING A UALAK NONE O OTHER ININSP/MAINT 1 WP29122UA 29168 LOW BOTTLE PRESSURE. CHARGE FILL FITTING LEAKING. REPLACED BOTTLE AND VALVE. 2L74 4F4 FRTA20WE E24NE 20050426001042005042600104NE 2005 4 26 AC2A099708 120041024A5280 HINGE SKRSKYS76 S76A 8143006NE NLG DOOR CORRODED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO077266F 760273 NOSE GEAR DOOR WAS FOUND HANGING DOWN BY PILOT AS AIRCRAFT WAS SITTING ON THE PAD. ONE HINGE WAS CORRODED AND HAD BROKEN ALLOWING THE DOOR TO BECOME PARTIALLY DETACHED FROM AIRCRAFT. NOSE WHEEL HAD ROLLED OVER DOOR AND CAUSED DAMAGE TO THE DOOR. 1G72 3U H1NE 20050426001062005042600106SW 2005 4 26 AC2R099710 120041030A2432RG407A1 BATTERY BELL 430 430 1182150SW MASTER FAILED B AC2RO OTHER O OTHER NRNOT REPORTED 1 SO07430CT114 49089 PART FAILED TEST TWO CHARGE AND CAPACITY CHECKS. REPLACED BATTERY AND BOOSTED GENERATOR OUTPUT TO 28.5. 1G72 3U RTH9SW 20050426001082005042600108SW 2005 4 26 AC2A099714 120041208A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO077159H349 51397 BATTERY IS WEAK. UNIT FAILED FIRST CAPACITY TEST AFTER 25 MINUTES. PERFORMED A 16 HOUR CONDITIONING CHARGE AT C 1/10TH RATE AND RETESTED. BATTERY FAILED AFTER 44 MINUTES. REPLACED BATTERY. 1G71 3U H2SW 20050426001102005042600110SW 2005 4 26 AC2A099718 120041211A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO0731079564 51526 BATTERY IS WEAK. BATTERY FAILED 1ST CAPACITY CHECK AFTER 28 MINUTES. CHARGED BATTERY WITH C 1/10 CONDITIONING CHARGE. BATTERY FAILED 2ND CHECK AFTER 33 MINUTES. SUBMITTED FOR WARRANTY CONSIDERATION. 1G71 3U H2SW 20050426001142005042600114SW 2005 4 26 AC2A099719 120041223A6410206016201131 BLADE BELL 206 206L3 1182108SW TAIL ROTOR DAMAGED B AC2AK NONE O OTHER ININSP/MAINT 1 SO07310791574 51526 AVERAGE SKIN THICKNESS .00673 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPPED BLADE. REQUEST WARRANTY. 1G71 3U H2SW 20050427000042005042700004EU 2005 4 27 TXER099765 120041106A6730SC50911 SERVO UROCOPEC120 EC120B 8680987EU CYCLIC LEAKING B TXERO OTHER K FLUID LOSS NRNOT REPORTED 1 SW03120GB 1063 CYCLIC SERVO LEAKING. 1G72 3U NCR0001RD 20050427000182005042700018CE 2005 4 27 FPI2005F00004 120041126A3240RA16402706 ROTOR BEECH 58 58 1152740CE CONT O520 IO520* 17032SO BRAKE CRACKED E FPIAK NONE O OTHER ININSP/MAINT 1 SO159098Q402 TH109 RADIAL CRACK FOUND ON WEAR SURFACE ON INSIDE OF ROTOR. THIS WAS A REPLACEMENT MFG PART (PN RA-164-02706). SUSPECT MFG DEFECT. NO EVIDENCE OF OVERHEAT CONDITION DETECTED. (LEFT ROTOR) 1L72 3O3 O 3A16 E5CE 20050427000262005042700026EU 2005 4 27 I262005F00000 120041105A28222C402 PUMP BRAERODH125 HS125700A 4230170EU FUEL BOOST WEAK E I26AO OTHER J WARNING INDICATION NRNOT REPORTED 1 NE05125SJ NA0275 LT (FUEL LOW PRESSURE) LIGHT ILLUMINATED, CREW ELECTED TO LAND. FOUND LT FUEL BOOST PUMP WEAK. PUMP REPLACED WITH OVERHAULED PUMP. AWAITING TEARDOWN REPORT ON REMOVED PUMP. (NE05200503254) (K) 2L72 4F A3EU 20050427000862005042700086NM 2005 4 27 2004UALA00832 120040830A5512 SKIN AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE HORIZONTAL STAB PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29847UA 1627 PUNCTURE IN LOWER SURFACE OF HORIZ STAB SKIN RT. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA28NM E40NE 20050427000952005042700095NM 2005 4 27 72300027 120041021A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON BOTTOM OF S-24 LT. 2L73 4F4 FRTA3WE E2EA 20050427000962005042700096NM 2005 4 27 72300028 120041026A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSLEAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON STRINGER BETWEEM BS 670 AND 720. 2L73 4F4 FRTA3WE E2EA 20050427000972005042700097NM 2005 4 27 72300029 120041016A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427000982005042700098NM 2005 4 27 72300030 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 STRINGER FLANGE CORRODED 20 INCH IN LENGTH. 2L73 4F4 FRTA3WE E2EA 20050427000992005042700099NM 2005 4 27 72300031 120041102A5310 DOOR FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 INCH BY 5 INCH AREA OF CORROSION ON FUSELAGE DOOR FRAME. 2L73 4F4 FRTA3WE E2EA 20050427001002005042700100NM 2005 4 27 72300032 120041024A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050427001012005042700101NM 2005 4 27 72300033 120041113A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON STRINGER BETWEEN BS 600-660. 2L73 4F4 FRTA3WE E2EA 20050427001022005042700102NM 2005 4 27 72300034 120041109A5312 BULKHEAD BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1.5 INCH BY 1.5 INCH AREA OF CORROSION ON WEB. 2L73 4F4 FRTA3WE E2EA 20050427001032005042700103NM 2005 4 27 72300035 120041018A5320 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 1.5 INCH AREA OF CORROSION ON CHORD. 2L73 4F4 FRTA3WE E2EA 20050427001042005042700104NM 2005 4 27 72300036 120041102A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCY BY 3 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050427001052005042700105NM 2005 4 27 72300037 120041016A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001062005042700106NM 2005 4 27 72300014 120041017A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001072005042700107NM 2005 4 27 72300015 120041019A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050427001172005042700117NM 2005 4 27 72300081 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSLEAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050427001192005042700119NM 2005 4 27 72300083 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050427001542005042700154EA 2005 4 27 MASA200400521 120040911A2420755469D IDG CNDAIRCL600 CL6002B19 1900309EA NR 1 GENERATOR LEAKING A MASAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW0737228399 7228 ASH 6311 SBP-PHX - ABORTED TAKEOFF DUE TO GEN 1 OFF LINE AND IDG CAUTION MESSAGE. MX FOUND THE IDG LOW ON OIL AND DISCONNECTED IT AND PLACED IT ON MEL. 9/13/04 MAINTENANCE REMOVED AND REPLACED THE IDG. 2L72 4F RTA21EA 20050427000792005042700079NM 2005 4 27 2004UALA00809 120040830A5315 FLOORBEAM BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29642UA 25092 CABIN FLOORBEAM UPPER SURFACE CORRODED, STA 808-813, RBL 57. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SPLICE. 2L72 4F4 FRTA1NM E24NE 20050427000812005042700081NM 2005 4 27 2004UALA00824 120040830A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 CABIN DOORS 2R AND 2L EXTERIOR EMERGENCY LIGHTS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M734 IN RT AFT CABIN. 2L72 4F4 FRTA1NM E24NE 20050427000832005042700083NM 2005 4 27 2004UALA00826 120040830A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 DOOR 2L UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK M739. 2L72 4F4 FRTA1NM E24NE 20050427000852005042700085NM 2005 4 27 2004UALA00828 120040830A5744 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT WING BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 LT WING, REAR SPAR, OUTBOARD FLAP OUTBOARD HINGE FITTING BROKEN IN HALF. FLAP TRANSMISSION OVER TORQUE LIMIT INDICATOR ALSO POPPED. SUPPLEMENTAL DATA UPDATE, REAR SPAR RIB POST PART NR 113T1369-1 REPLACED. FLAP TRANSMISSION OVERTORQUE LIMIT INDICATOR RESET. 2L72 4F4 FRTA1NM E24NE 20050427000872005042700087NM 2005 4 27 2004UALA00851 120040925A4900 APU BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE MALFUNCTIONED A UALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 WP29673UA 29241 60165 RETURNED TO HNL DUE TO FAILED EN ROUTE ETOPS VERIFICATION, APU ALTITUDE START. SUPPLEMENTAL DATA UPDATE, THE CAUSE OF THE FAILED ALTITUDE START WAS NOT CONFIRMED. TEST CELL FINDINGS COULD NOT REPEAT NO START EVENT. THE FOLLOWING LRU WERE ROUTED-GENERATOR OIL SWITCH, P2 SENSOR, LOT SWITCH, EXCITER, DE-OIL SOLENOID VALVE, FUEL FLOW DIVIDER, AND FUEL CONTROL UNIT RELATED TO ALTITUDE STARTING WERE REPLACED AS PRECAUTIONARY. APU PASSED THE AS-RECEIVED DIAGNOSTIC TEST. APU WAS TREATED AS A CONVENIENCE SHOP VISIT AND MADE SERVICEABLE. SUBSEQUENT, THE APU AND A/C COMBINATION EXHIBITED SAME EVENT. THE APU CONTROLLER AND APU START SWITCH WAS REPLACED. NO OTHER EVENTS HAVE OCCURRED. 2L72 4F4 FRTA1NM E24NE 20050426001052005042600105SW 2005 4 26 AC2R099709 120041030A2432RG407A1 BATTERY BELL 430 430 1182150SW MASTER FAILED B AC2RO OTHER O OTHER NRNOT REPORTED 1 SO07430CV247 49072 PART FAILED TEST TWO CHARGE AND CAPACITY TESTS. (LESS THAN 25 MINIUTES). REPLACED BATTERY AND BOOSTED GENERATOR VOLTAGE TO 28.5 VDC. 1G72 3U RTH9SW 20050426001072005042600107SW 2005 4 26 AC2A099712 120041111A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO03715CC179 51380 PART IS WEAK. THE BATTERY FAILED A CAPACITY CHECK. REPLACED BATTERY. 1G71 3U H2SW 20050426001092005042600109SW 2005 4 26 AC2A099717 120041217A2432RG222 BATTERY BELL 206 206L3 1182108SW MASTER WEAK B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO036533U438 51439 BATTERY IS WEAK. CHARGED BATTERY, PERFORMED FIRST CAPACITY CHECK, FAILED AFTER 26 MINUTES. RECHARGED WITH CONDITIONING CHARGE OF C1/10. BATTERY FAILED SECOND CAPACITY CHECK AFTER 48 MINUTES. REPLACED BATTERY WITH NEW PART. RETURNED FOR WARRANTY CONSIDERATION. 1G71 3U H2SW 20050426001152005042600115SW 2005 4 26 AC2A099720 120041223A6410206016201131 BLADE BELL 206 206L3 1182108SW TAIL ROTOR DAMAGED B AC2AO OTHER O OTHER NRNOT REPORTED 1 SO07310791574 51526 AVERAGE SKIN THICKNESS .00684 LOWER SURFACE NOT REPAIRABLE AS PER ASB 206L-04-127 AND 206-04-100 REV B PART III. SCRAPPED BLADE. REQUEST WARRANTY. 1G71 3U H2SW 20050816000842005081600084NM 2005 8 16 SWAA040804 120040315A534065C27314 CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND 3 EA STRINGER CLIPS CRACKED AT BS 727C, STR 22R, STR 21R, & BS 727D, STR 23R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001092005081600109NM 2005 8 16 SWAA040876 120040323A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9R, BS 380, BS 480, BS 747, BS 807, BS 827, BS 887, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20050816001122005081600112NM 2005 8 16 SWAA040892 120040325A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D-CHECK, FOUND 3 EA FUSELAGE FRAMES CRACKED AT STRINGER 9R, BS 807, BS 867, BS 827. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20050816001132005081600113NM 2005 8 16 SWAA040932 120040329A53116546520 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9R, BS 380, BS 480, BS 767, BS 787, BS 887, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20050816001152005081600115NM 2005 8 16 SWAA041044 120040412A53116546520 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 380, AND BS 400, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001162005081600116NM 2005 8 16 SWAA041001 120040406A531169353656 TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SPV, FOUND SHEAR TIES AT BS 360, STRINGER 14L AND STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001172005081600117NM 2005 8 16 SWAA041765 120040623A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND CREASE BEAMS AT BS 360 TO BS 380, RBL 70.5, BS 500 TO BS 500A, RBL 70.5, CORRODED. REMOVED AND REPLACED CREASE BEAM SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001192005081600119NM 2005 8 16 SWAA041177 120040426A53156545815 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 328, RBL 42, BS 344, LBL 50 TO RBL 0, CORRODED. REPAIRED FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20050816001222005081600122 2005 8 16 SWAA040033 420040105A2565D31354 SLIDE BOEING737 7373G7 1384595NM L1 DOOR DEPLOYED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29671SW 23785 UPON OPENING L1 DOOR, EVACUATION SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVACUATION SLIDE PER MM. 2L72 4F RTA16WE 20050816001282005081600128NM 2005 8 16 SWAA040501 120040217A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 480, BS 827, BETWEEN STRINGER 8R AND STRINGER 9R, AND BS 807, BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20050816001292005081600129NM 2005 8 16 SWAA040659 120040301A5315BAC1515 FLOORBEAM BOEING737 7373A4 1384585NM MID CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D-CHECK, FOUND 3 EA LONGITUDINAL FLOORBEAMS CRACKED AT LBL 26, BS 708, BL 0, BS 710, AND RBL 25, BS 712. REPAIRED BEAMS PER ER. 2L72 4F RTA16WE 20050816001302005081600130NM 2005 8 16 SWAA040584 120040225A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS BS 460, STRINGER 14L AND BS 887, STRINGER 9L. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20050816001312005081600131NM 2005 8 16 SWAA040585 120040225A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS STRINGER 9R, BS 837, BS 807, BS 787, BS 907. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20050816001322005081600132NM 2005 8 16 SWAA040586 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727E, STRINGERS 7L, 5L, 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001342005081600134NM 2005 8 16 SWAA040588 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727C, STRINGERS 5L, 6L, 7L, 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001352005081600135NM 2005 8 16 SWAA040593 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727D, STRINGERS 7R, 3R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001362005081600136NM 2005 8 16 SWAA040594 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, STRINGERS 5R, 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001372005081600137NM 2005 8 16 SWAA040595 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747, STRINGERS 10R, 5R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001412005081600141NM 2005 8 16 SWAA041693 120040615A53406551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED AT BS 538, STR 10R, AND BS 908, STR 4R. REMOVED AND REPLACED BOTH STR SPLICES PER SRM. 2L72 4F RTA16WE 20050816001422005081600142NM 2005 8 16 SWAA041180 120040426A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 747, STR 9L, BS 767 STR 9R AND 9L, BS 807, STR 9R, BS 827, STR 9L AND 9R, BS 887, STR 9R AND 8L, CRACKED. REPAIRED FRAMES PER SRM. 2L72 4F RTA16WE 20050816001432005081600143NM 2005 8 16 SWAA041184 120040426A53226546529 TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 440, BETWEEN STR 26L AND STR 27L, BS 500A, BETWEEN STR 28L AND STR 28R, CORRODED. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001452005081600145NM 2005 8 16 SWAA041357 120040512A53156545810 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 312, LBL 26 TO RBL 7, BS 328, RBL 42, BS 344, LBL 42.5, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001462005081600146NM 2005 8 16 SWAA041372 120040513A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 867, BS 907, STRINGER 8L, AND BS 867, BS 907, STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001472005081600147NM 2005 8 16 SWAA041461 120040523A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29642WN 27715 DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM SUPPORTS AT BS 859, LBL 3, BS 794, LBL 3, CORRODED. REPAIRED FLOORBEAMS PER EA. 2L72 4F RTA16WE 20050816001482005081600148NM 2005 8 16 SWAA041474 120040524A53106519603 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CHORDS AT BS 360 TO BS 380, LBL 65, BS 375 TO BS 380, LBL 70, CRACKED. REMOVED AND REPLACED CREASE BEAM CHORDS PER SRM. 2L72 4F RTA16WE 20050816001492005081600149NM 2005 8 16 SWAA041601 120040606A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10L, BS 707, STRINGER 11L, BS 663, STRINGER 10R CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001502005081600150NM 2005 8 16 SWAA041613 120040607A53306545770 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D + 6, STRINGER 20R, BS 727E - 3, STRINGER 23L, BS 750, STRINGER 19L, BS 942.5, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050816001512005081600151NM 2005 8 16 SWAA041181 120040426A53226546546 TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 747, STR 27R, BS 867, BL 0, BS 807, LBL 18 AND LBL 9, CORRODED. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001522005081600152NM 2005 8 16 SWAA041370 120040513A531165C25200 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 727 D, STRINGER 8L, AND BS 747, STRINGER 8R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001532005081600153NM 2005 8 16 SWAA041477 120040524A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 9007, BS 867, BS 827, 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001622005081600162NM 2005 8 16 SWAA040883 120040324A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 827, STRINGER 9L AND BS 867, STRINGER 9R, CRACKED. REPAIRED FRAMES PER ER AND SRM. 2L72 4F RTA16WE 20050816001692005081600169NM 2005 8 16 SWAA041037 120040410A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES AT BS 727D, BS 787, BS 907, BETWEEN STRINGERS 8R AND 9R, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001742005081600174NM 2005 8 16 SWAA041003 120040407A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS AT BS 727B, STRINGER 25R, BS 727B, STRINGER 25L, BS 727D, STRINGER 23L, BS 727E, STRINGER 23L, BS 747, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001782005081600178NM 2005 8 16 SWAA041159 120040425A53226546569 TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29322SW 23343 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 967 AND BS 989, STRINGER 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001792005081600179NM 2005 8 16 SWAA041214 120040429A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS AT BS 360, STRINGER 8R, BS 420, STRINGER 3L, BS 420, STRINGER 9R, BS 420, STRINGER 1R, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001802005081600180NM 2005 8 16 SWAA040613 120040226A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 480, BS 787, 907, STRINGER 9L ALSO AT BS 867, STRINGER 9R. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20050816001862005081600186NM 2005 8 16 SWAA040633 120040227A53156546957 SHEAR WEB BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND SHEAR WEB CORRODED BETWEEN RT BS 400 AND RT BS 420, ABOVE AND BELOW FLOOR LEVEL. REPAIRED SHEAR WEB PER SRM. 2L72 4F RTA16WE 20050816001892005081600189NM 2005 8 16 SWAA040690 120040304A53406551698 SPLICE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER SPLICES CRACKED AT BS 540, STR 10L, AND BS 360, STR 6L. REPAIRED STR SPLICES PER SRM AND ERO. 2L72 4F RTA16WE 20050816001922005081600192NM 2005 8 16 SWAA040757 120040308A534065C27314 CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIPS CRACKED AT STRINGER 4L AND BS 706, BS 639, BS 616. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001932005081600193NM 2005 8 16 SWAA040799 120040315A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 380, STR 26L & STR 26R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001962005081600196NM 2005 8 16 SWAA040776 120040313A53156547973 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEBS CRACKED AT BS 576, LBL 71, WL 208 AND BS 637, LBL 71, WL 208. REMOVED AND REPLACED CREASE BEAM WEBS PER SRM. 2L72 4F RTA16WE 20050816001972005081600197NM 2005 8 16 SWAA040787 120040312A534065C27314 CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 639, STRINGER 8L, BS 706, STRINGER 2L AND BS 616, STRINGER 4R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001982005081600198NM 2005 8 16 SWAA040801 120040315A53306552988 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29669SW 23752 DURING SCHEDULED C1 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 929, STR 22R & BS 935, STR 23R.. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050816001992005081600199NM 2005 8 16 SWAA040911 120040327A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 312, BS 344, BS BS 986, LBL 65 TO RBL 42 CORRODED. REPAIRED FLOORBEAM SECTIONS PER SRM AND ER. 2L72 4F RTA16WE 20050816002002005081600200NM 2005 8 16 SWAA040915 120040328A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29320SW 23341 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS AT BS 767, STRINGER 25L, BS 907, STRINGER 25R AND BS 727B, STRINGER 25R, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816002112005081600211NM 2005 8 16 MZZA0400003 120041006A5210 ROD END BOEING737 737823 13844BZNM PAX DOOR JAMMED A MZZAO OTHER K FLUID LOSS ININSP/MAINT 1 WP1335236 28801 THE L1 DOOR JAMMED WHILE ATTEMPTING TO OPEN AT GATE IN MNL. THE DOOR SHROUD WAS REMOVED. MX FOUND THE UPPER GATE FWD GUIDE RODEND JAMMED. THE ROD END WAS SECURED, SAFETIED, AND ADJUSTED. THE DOOR SHROUD WAS REINSTALLED. AN OPS CHECK OF THE DOOR WAS NORMAL IAW MM 52-11-00. 2L72 4F RTA16WE 20050817000042005081700004NM 2005 8 17 MZZA0400002 120040807A3350D71701100 BATTERY BOEING737 737823 13844BZNM MID CABIN INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1335236 28801 ALL MID-SECTION EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE LT AND RT MID EMERGENCY EXIT LIGHT BATTERY PACKS WERE REMOVED AND REPLACED IAW MM. (K) 2L72 4F RTA16WE 20050817000052005081700005NM 2005 8 17 MZZA0400001 120040320A5210BACR15BA5B RIVET BOEING737 737823 13844BZNM DOOR GUIDE TRACKSHEARED A MZZAK NONE O OTHER TXTAXI/GRND HDL 1 WP1314235 28947 FORWARD ENTRY DOOR WOULD NOT OPEN UPON ARRIVAL. MAINTENANCE FOUND A RIVET SHEARED ON LOWER GUIDE TRACK ASSY. GUIDE TRACK ASSY WAS REPAIRED IAW ECRA. OPERATIONAL CHECK OF THE DOOR WAS GOOD. (K) 2L72 4F RTA16WE 20050427000272005042700027EU 2005 4 27 KBM2005F00030 120040111A3340DHS7751604 LIGHT SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE EXTERIOR INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19351WM 2167 EXTERIOR LIGHT INOPERATIVE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050427000802005042700080NM 2005 4 27 2004UALA00810 120040830A5753 HINGE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE RT TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29642UA 25092 RT INBD AFT FLAP EXTERNAL HINGE IS CRACKED AT THE MID FLAP AFT SPAR. REPAIRED FITTING WITH ANGLE REPAIR. 2L72 4F4 FRTA1NM E24NE 20050427000822005042700082NM 2005 4 27 2004UALA00825 120040830A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 DOOR 2R UPPER INTERIOR EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED BATTERY PACK AT AFT RT ATTENDANTS SEAT. 2L72 4F4 FRTA1NM E24NE 20050427000842005042700084NM 2005 4 27 2004UALA00827 120040830A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29650UA 25287 CENTER LT OVERWING EMERGENCY LIGHT HAS ONE INOP LAMP. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED BATTERY PACK M738 AND RELAMPED LT CENTER OVERWING LIGHT ASSEMBLY. 2L72 4F4 FRTA1NM E24NE 20050427001102005042700110NM 2005 4 27 72300019 120041016A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .5 INCH BY 1 INCH AREA OF CORROSION ON SHEAR TIE 2L73 4F4 FRTA3WE E2EA 20050427001182005042700118NM 2005 4 27 72300082 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050427001552005042700155 2005 4 27 MASA200400590 420041019A22006229968001 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA YAW DAMPENER INOPERATIVE A MASAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW07571ML669 7209 ASH 2924- GRR-PHL - DURING CRUISE, THE RUDDER MOVED UNCOMMANDED. MAINTENANCE REPLACED THE YAW DAMP ACTUATORS, P/N 622-9968-001 S/N 3178 AND P/N DL2233M1-1 S/N 777. 2L72 4F RTA21EA 20050427002452005042700245EA 2005 4 27 MASA200400636 120041113A5246 DOOR CNDAIRCL600 CL6002B19 1900309EA OXYGEN SERVICE OPEN A MASAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 SW07400MJ 7309 ASH 2846 PHL-PHL - AIRCRAFT RETURNED TO FIELD DUE TO LOUD NOISE AT RIGHT SIDE OF FUSELAGE. MAINTENANCE FOUND THE OXYGEN SERVICE DOOR OPEN. SECURED OXYGEN SERVICE DOOR CLOSED. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. 2L72 4F RTA21EA 20050427002472005042700247EA 2005 4 27 200400652 120041124A3260864202 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA NLG FAULTY A MASABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07593ML3624 7465 ASH 2600 GRR - THE PILOT REPORTED A NOSE GEAR DISAGREE MSG AFTER GEAR SELECTED UP. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AFTER THE GEAR WAS SUCCESSFULLY PLACED DOWN AND LOCKED UTILIZING THE NORMAL DOWN SELECTION. ON CALL MX WAS UNABLE TO FIND ANY OBVIOUS DEFECTS WITH THE RETRACTION SYSTEM SO THE A/C WAS PREPPED FOR A FERRY. A/C IS CURRENTLY BELOW WEATHER MINIMUMS TO FERRY. 11/25 MAINTENANCE REPLACED NOSE UP LOCK PROXIMITY SWITCH. OPS GOOD. 2L72 4F RTA21EA 20050427000232005042700023WP 2005 4 27 XV62005F00000 220041205A72618941172 ADAPTER DORNERDO228 DO228202 2992030EU GARRTTTPE331TPE3315 01514WP NR 1 ENG OIL FILCRACKED E XV6AK NONE O OTHER ININSP/MAINT 1 WP19403VA 2316 8171 OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200407922) 2H72 4T4 TRTA16EU E4WE 20050427002442005042700244EA 2005 4 27 MASA200400635 120041112A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA COCKPIT CRACKED A MASAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07771811831 7181 ASH 2912 PHL -PHL - AIRCRAFT RETURNED TO FIELD DUE TO A CRACKED PILOTS WINDSHIELD ON CLIMB-OUT. MAINTENANCE CHANGED THE PILOTS WINDSHIELD. 2L72 4F RTA21EA 20050427002462005042700246EA 2005 4 27 MASA200400643 120041117A2760 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA SPOILERS MALFUNCTIONED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0775994 7367 ASH 7194 FROM IAD TO PHL, ABORTED TAKEOFF WHEN RECEIVED A TAKEOFF CONFIG SPOILER CAUTION MESSAGE. MAINTENANCE RESET SPOILER CONTROL SYSTEM AND SYSTEM, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050427002482005042700248 2005 4 27 MASA200400660 420041128A3418 WARNING SYSTEM CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FALSE ACTIVATIONA MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW07592ML 7410 ASH 2708 ERI - PHL - AIRCRAFT ABORTED TAKEOFF DUE TO A STALL FAIL WARNING. AIRCRAFT IS BEING FERRIED TO PHL FOR TROUBLESHOOTING. 11/28/04 MAINTENANCE COULD NOT DUPLICATE THE PROBLEM, NO PROBLEMS NOTED. 2L72 4F RTA21EA 20050427002552005042700255EA 2005 4 27 MASA200400674 120041202A8097 WIRE CNDAIRCL600 CL6002B19 1900309EA VALVE DAMAGED A MASAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0717175 7175 ASH 7177 FROM IAD - DTW - DIVERTED TO PIT DUE TO A NR 1 ENGINE NO STARTER CUT-OUT EICAS MESSAGE. FLIGHT CREW COULD ONLY CLEAR FAULT AFTER PULLING NR 1 10TH STAGE VALVE C/B. MAINTENANCE REPAIRED DAMAGED WIRE TO 10TH STAGE VALVE AND SECURED ELECTRICAL CONNECTORS ON 10TH STAGE VALVE, AIR TURBINE STARTER AND AIR START VALVE. ENGINES WERE RUN AND NO FURTHER DEFECTS WERE NOTED. 2L72 4F RTA21EA 20050427002562005042700256EA 2005 4 27 MASA200400677 120041203A7830 SWITCH CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF ADJUST A MASAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW0737178 7178 ASH 6491 FROM PHX TO ICT ABORTED TAKEOFF DUE TO A RIGHT ENGINE THRUST REVERSER UNLOCK WARNING. MAINTENANCE COMPLIED WITH MEL MAINTENANCE ACTION. 12/04/04 MAINTENANCE ADJUSTED SWITCH. OPS CHK GOOD. 2L72 4F RTA21EA 20050427002572005042700257EA 2005 4 27 MASA200400680 120041204A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG INOPERATIVE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07593ML1663 7465 ASH 2992 PHL - AIRCRAFT RETURNED TO FIELD DUE TO THE NOSE GEAR NOT RETRACTING. MAINTENANCE ARE IN THE PROCESS OF SWINGING THE GEAR IN THE HANGER. 12/4 MAINTENANCE REPLACED PRIORITY VALVE. 2L72 4F RTA21EA 20050427002592005042700259EA 2005 4 27 MASA200400699 120041215A21331037729 OUTFLOW VALVE CNDAIRCL600 CL6002B19 1900309EA NR 2 STUCK A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07172179787 7217 ASH 7138 ORD TO RDU-AIRCRAFT RETURNED TO FIELD BECAUSE THE AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT WAS FERRIED TO IAD. MAINTENANCE REPLACED THE SECONDARY OUTFLOW VALVE AND SYSTEM OPS CHECKED GOOD. 2L72 4F RTA21EA 20050427002602005042700260EA 2005 4 27 MASA200400719 120041222A78301267587 PDU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER FAILED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW073721810259 7218 ASH 6159 COS-PHX ABORTED TAKEOFF DUE TO RT REVERSE UNLOCK CAUTION MESSAGE. MAINTENANCE PLACED THE T/R ON MEL. 12/22 MAINTENANCE REPLACED THE POWER DRIVE UNIT (PDU), OPS CHECK GOOD. 2L72 4F RTA21EA 20050427002612005042700261NE 2005 4 27 MASA200400729 220041227A7261 PLUG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EDP DISLODGED A MASAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0717231 7231 ASH 6381 PHX TO EUG - SHUTDOWN NR 1 ENGINE AND DIVERTED TO SMF DUE TO A OIL PRESSURE FLUCTUATION. MX IS IN THE PROCESS OF TROUBLE SHOOTING. OPEN PENDING RESOLUTION. RECOMPLIED WITH MEL FOR EDP. UPON INSPECTION FOUND EDP SPLINE PLUG HAD FALLEN OUT. INSTALLED NEW O-RING AND SPLINE PLUG SERVICED AND PERFORMED OIL CONSUMPTION TEST. NO DEFECTS NOTED ENG DID NOT CONSUME ANY OIL. 2L72 4F4 FRTA21EA E15NE 20050503002642005050300264EU 2005 5 3 ERAA100058 120041221A2435230322111 ARMATURE BOLKMS105 BO105S 5626006EU STARTER GEN DAMAGED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03154EH 704 STARTER GEN ARMATURE SENT IN FOR EXCHANGE HAS EXCESSIVE SPARKING. 1G72 3U H3EU 20050504000472005050400047WP 2005 5 4 IXXA0500042S 120040807A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE LONGERON 24 FITTING FRAME CRACK DAMAGE AT STA 879.000. REPAIR ACCOMPLISHED. REMOVED FITTING. FABRICATED SHIMS, DOUBLER AND SPLICES. HEAT TREATED SHIMS AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND SHIMS, DOUBLER AND SPLICES. APPLIED PRC SEALANT TO FAYING SURFACES INSTALLED SPLICES, DOUBLER, SHIM AND NEW FITTING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050504000482005050400048WP 2005 5 4 IXXA0500043S 120040831A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, REMOVED MAIN CARGO COMPT FRAME FITTING AT STA920.00 L-23L TO L24L IN ORDER TO COMPLY WITH N/R 3484. REPAIR ACCOMPLISHED. REMOVED FITTING TO GAIN ACCESS TO STRUCTURAL REPAIR. FRABRICATED SPLICES, DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED SPLICES, DOUBLER AND FILLERS AND FITTING. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PART TO FITTING. REINSTALLED FITTING PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050504000492005050400049WP 2005 5 4 IXXA0500044S 120040809A5730 SKIN DOUG DC8 DC873F 302199FWP TE FLAPS DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR AROUND STA XF. 226.000. REPAIR ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREA. REMOVED THE DAMAGED AREA. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SKIN SEGMENT AND INTERNAL SPLICE. CLEANED, TREATED AND PRIMED THE NEW SKIN SEGMENT INTERIOR SURFACE AND INTERNAL SPLICE. APPLIED REC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON RT O/B FLAP STA XF. 226.000 USING NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL, FAA FORM 8110-3 AND EO NR 2004414 AND DRAWING W43-R10. 2L74 4F RT4A25 20050504000502005050400050WP 2005 5 4 IXXA0500048S 120040825A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION, LT FUSELAGE LONGERON 24 FITTING FRAME WAS REMOVED AND INSTALLED TO COMPLY WITH N/R 3484 SID 960.000L-24 TO L-23L. REPAIR ACCOMPLISHED, REMOVED FRAME FITTING, CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICES AND DOUBLER AND FILLERS. PERFORMED HEAT TREATMENT TO FILLERS AND DOUBLER. CLEANED TREATED AND PRIMED. REPAIRED PARTS. INSTALLED FRAME FITTING REPAIR PARTS WITH NEW FASTENERS AFTER COMPLIED WITH N/R 3484 PER THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050505000162005050500016WP 2005 5 5 IXXA0500046S 120041011A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE NOSE SECTION PRESSURE PANEL CORROSION DAMAGE BETWEEN STA FS 8.00 AND STA FS -67.00 LBL 40.30 TO LBL 56.00. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA. REMOVED THE CORROSION AND FOUND OUT OF LIMITS. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A NEW SEGMENT PANEL, FIVE EXTERNAL REPAIR DOUBLER, TWO INTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED THE REPAIR PARTS. APPLIED PRC SEALANT TO FAYING SURFACES, INSTALLED THE REPAIR PARTS ON THE NOSE SECTION PRESSURE PANEL USING NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL, FAA FORM 8110-3 DWG W43-R20 AND EO NR 2004484. 2L74 4F RT4A25 20050505000172005050500017WP 2005 5 5 IXXA0500047S 120041011A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION, FOUND RT FUSELAGE NOSE SECTION STRUCTURE FLIGHT COMPARTMENT HAS DAMAGE FROM CORROSION AT STA -67.000. REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED THE CORRODED FRAME SEGMENT AND FABRICATED A NEW FRAME SEGMENT. HEAT TREATED NEW FRAME, CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT. INSTALLED NEW FRAME SEGMENT PER DOUGLAS STRUCTURAL REPAIR MANUAL, DPS 3.69-4 REV "AM", DPS 7.00-1 REV. "BJ" 2L74 4F RT4A25 20050505000182005050500018WP 2005 5 5 IXXA0500049S 120041011A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD VANE SLOT HAS INTERIM REPAIR AT STA XILD 7095.00. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL REPAIR DOUBLER, FILLER, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED INNER FACE OF DOUBLER-INTERNAL/EXTERNAL, FILLER. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER AND INTERNAL DOUBLER PER DOUGLAS STRUCTURAL REPAIR MANUAL AND DWG W43-R04. 2L74 4F RT4A25 20050505000232005050500023WP 2005 5 5 IXXA0500054S 120041011A5753 SKIN PANEL DOUG DC8 DC873F 302199FWP TE FLAP CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR FOUND ON LOWER SURFACE OF LT OUTBOARD FLAP STA XF 420.000. REPAIR ACCOMPLISHED REMOVAL OF SKIN WITH THE INTERIM REPAIR ON IT. FABRICATED NEW SKIN PLUS FINGER DOUBLER. BONDED FINGER DOUBLER ON SKIN. CLEANED, TREATED AND PRIMED INNER FACE OF NEW SKIN PANEL. INSTALLED NEW SKIN PANEL PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050505000252005050500025WP 2005 5 5 IXXA0500056S 120041011A5312 PRESSURE PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION DAMAGE ON RT FUSELAGE NOSE SECTION PRESSURE PANEL BETWEEN STA FS 8.00 AND STA FS -67.00, RBL 28.78 TO RBL 56. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CORROSION. FOUND OUT OF LIMITS, REMOVED DAMAGED SEGMENT. PERFORMED NDT INSPECTION. FABRICATED NEW PRESSURE PANEL SEGMENT, EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA AND NEW PRESSURE PANEL SEGMENT. APPLIED RC SEALANT TO FAYING SURFACE. INSTALLED NEW PRESSURE PANEL SEGMENT AND INTERNAL/EXTERNAL REPAIR DOUBLERS WITH NEW FASTENERS PER ALL APPLICABLE MANUALS AND DRAWINGS. 2L74 4F RT4A25 20050505000262005050500026WP 2005 5 5 IXXA0500057S 120041011A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, LT FUSELAGE LONGERON 24 FITTINGS FRAME REMOVED AND INSTALLED FOR NR 3484 AT STA 940.000. REPAIR ACCOMPLISHED REMOVAL OF FITTING IN ORDER TO GAIN ACCESS FOR REPAIR. FABRICATED SPLICES, DOUBLER AND FILLERS. HEAT TREATED DOUBLER AND FILLER, CLEANED, TREATED AND PRIMED AREA AND SPLICES, DOUBLER , FILLER AND FITTING. APPLIED SEALANT TO FAYING SURFACES AND INSTALLED FILLERS, DOUBLER AND SPLICES ON FITTING. REINSTALLED IN ACCORDANCE WITH DOUGLAS STRUCTURAL MANUAL. 2L74 4F RT4A25 20050505000272005050500027WP 2005 5 5 IXXA0500058S 120041011A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND CRACKED L-34 RT AFT CARGO COMPARTMENT STA FS1400.00 TO FS 1420.000. REPAIR ACCOMPLISHED REMOVAL OF CRACKED LONGERON SEGMENT. CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICE FILLING LONGERON. PERFORMED HEAT TREATMENT TO LONGERON AND SPLICES. CLEANED TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS IAW DOUGLAS SRMS AND ATI REPAIR SPECIFICATION 2003-05. 2L74 4F RT4A25 20050505000282005050500028WP 2005 5 5 IXXA0500059S 120041011A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, INTERIM REPAIR ON FUSELAGE EXTERIOR SKIN FROM FS 685.000 - 779.000 L-35 LT TO L-34 RT AND CORROSION DAMAGE. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA. REMOVED CORROSION AND FOUND OUT OF LIMITS. PERFORMED NDT INSPECTION, CLEANED, TREATED, AND PRIMED AREA. FABRICATED A NEW SEGMENT PANEL, A REPAIR DOUBLER, AND A REPAIR TRIPLER. CLEANED, TREATED AND PRIMED THE NEW SEGMENT PANEL AND REPAIR DOUBLER AND TRIPLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON FUSELAGE EXTERIOR SKIN USING NEW FASTENERS IAW DOUGLAS SRM, ATI DWG W43-R21 AND FAA FORM 8110-3. 2L74 4F RT4A25 20050505000292005050500029WP 2005 5 5 IXXA0500060S 120041011A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT ZEE FRAME CRACK DAMAGE AROUND STA FS 260.000, L-20 RT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FRAME SEGMENT. CLEANED, TREATED AND PRIMED AREA. FABRICATED FRAME SEGMENT AND SPLICES. PERFORMED HEAT TREATMENT TO FRAME SEGMENT AND SPLICES. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS IAW DOUGLAS SRM, DPS 3.69-4 REV 'AM' DPS 7.00 1 REV BJ. 2L74 4F RT4A25 20050505000302005050500030WP 2005 5 5 IXXA0500064S 120041011A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION FOUND TAIL SECTION FUSELAGE EXTERNAL SKIN CRACKED .75 INCH STA 1755.000-L-13 TO L14. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS WITH THE REPAIR AREA AND EXISTING REPAIR DOUBLER. REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, SHINS AND TWO INTERNAL FINGER DOUBLER. CLEANED TREATED AND PRIMED THE REPAIR PARTS. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON TAIL SECTION EXTERNAL SKIN USING NEW FASTENERS PER DOUGLAS STRUCTURAL MANUAL, ATI DWG W43-R13 AND FAA FORM 8110-3. 2L74 4F RT4A25 20050505000432005050500043NM 2005 5 5 72300156 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1.5 X 5 INCH AREA OF CORROSION ON STRINGER BOTTOM. 2L73 4F4 FRTA3WE E2EA 20050505000452005050500045NM 2005 5 5 72300158 120041020A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON STRINGER BOTTOM. 2L73 4F4 FRTA3WE E2EA 20050505000472005050500047NM 2005 5 5 72300160 120041019A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 6 INCH AREA OF CORROSION ON FRAME WEB. 2L73 4F4 FRTA3WE E2EA 20050503002632005050300263EU 2005 5 3 ERAA100057 120041221A2435230322111 ARMATURE BOLKMS105 BO105S 5626006EU STATER GEN FAILED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03134EH 635 STARTER GENERATOR ARMATURE SENT IN FOR EXCHANGE HAS EXCESSIVE SPARKING. 1G72 3U H3EU 20050505000152005050500015WP 2005 5 5 IXXA0500045S 120040810A5330 SKIN PANEL DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION, FOUND LT FUSELAGE FORWARD AND AFT CENTER SECTION PRESSURE PANEL CORROSION DAMAGE BETWEEN STA FS 980.000 AND FS 857.000. REPAIR ACCOMPLISHED. REMOVED FASTENERS, AND REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSPECTION. FABRICATED NEW PANEL SEGMENT, EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLERS. CLEANED, TREATED AND PRIMED AREA, NEW PANEL SEGMENT, EXTERNAL REAPIR DOUBLER AND INTERNAL REPAIR DOUBLER. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED NEW PANEL SEGMENT, EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER WITH NEW FASTENERS PER DOUGLAS SRM, DRWG W43-R12, AND EO 2004423 2L74 4F RT4A25 20050505000192005050500019WP 2005 5 5 IXXA0500050S 120041011A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION MAIN CARGO COMP BEAM WEB CORROSION & 2 INCH CRACK STA 920.000 LBL 64-69". REPAIR ACCOMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGED AREA ON BEAM. FABRICATED FILLER REPAIR AND REPAIR ANGLES. CLEANED, TREATED AND PRIMED AREA. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIRED PARTS PER DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050505000202005050500020WP 2005 5 5 IXXA0500051S 120041011A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION DAMAGE ON RT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT ZEE FRAME AROUND STATION 240.000, L-33R AND L-34R. REPAIR ACCOMPLISHED THE REMOVAL OF THE CORRODED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT AND SPLICES. HEAT TREATED SPLICES, CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT AND SPLICES. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED NEW FRAME SEGMENT AND SPLICES PER DOUGLAS STRUCTURAL REPAIR MANUAL, DPS 3.69-4 REV "AM", DPS 7.00-1 REV "BJ". 2L74 4F RT4A25 20050505000212005050500021WP 2005 5 5 IXXA0500052S 120041011A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, CRACK DAMAGE WAS FOUND AT LT FUSELAGE STRUCTURE MAIN CARGO COMPARTMENT FLOORBEAM LOWER SIDE CRACK DAMAGE AT STA FS 980.000 LBL 40. REPAIR ACCOMPLISHED REMOVED OF "T" ANGLE SEGMENT, CLEANED, TREATED AND PRIMED AREA. FABRICATED "T" ANGLE SEGMENT AND SPLICES. PERFORMED HEAT TREATMENT, CLEANED, TREATED AND PRIMED "T" ANGLE SEGMENT AND SPLICES. APPLIED PRC SEALANT ON FAYING SUFACES. INSTALLED NEW "T" ANGLE SEGMENT AND SPLICES PER DOUGLAS STRUCTURAL REPAIR MANUAL, 2L74 4F RT4A25 20050505000222005050500022WP 2005 5 5 IXXA0500053S 120041011A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, TEE CRACK DAMAGE WAS FOUND RT FUSELAGE STRUCTURE MLG COMPARTMENT AROUND STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. FABRICATED TEE ANGLE, HEAT TREATED AND PERFORMED NDT INSPECTION. FABRICATED SPLICES. APPLIED PRC SEALANT TO FAYING SURFACES. CLEANED, TREATED AND PRIMED SPLICE AND TEE ANGLE. INSTALLED SPLICES AND TEE ANGLE PER DOUGLAS STRUCTURAL REPAIR AND ATI REPAIR SPECIFICATION NR 2003-05, DPS 7.00-1. 2L74 4F RT4A25 20050505000342005050500034WP 2005 5 5 IXXA0500068S 120041011A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSLEAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 CORROSION DAMAGE BETWEEN STA 920.00 AND STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF CORROSION. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED. FABRICATED ANGLES. CLEANED, TREATED AND PRIMED. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED ANGLES IAW DOUGLAS SRM AND BOEING MESSAGE 1-M3W2D. 2L74 4F RT4A25 20050505000242005050500024WP 2005 5 5 IXXA0500055S 120041011A5320 WEB DOUG DC8 DC873F 302199FWP FUSLAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK, RT FUSELAGE WELL MLG WEB CRACK DAMAGE BETWEEN STA Y=857.125 AND XCW=25.000. REPAIR ACCOMPLISHED, REMOVED FASTENERS, REMOVED WEB DAMAGED SEGMENT. PERFORMED NDT INSPECTION. FABRICATED NEW WEB SEGEMENT AND EXTERNAL REPAIR DOUBLER AND INTERNAL REPAIR DOUBLER. CLEANED, TREATED AND PRIMED REPAIR PARTS. APPLIED PRC SEALANT TO FAYING SURFACES INSTALLED NEW WEB SEGMENT AND INTERNAL/EXTERNAL REPAIR DOUBLER WITH NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWING W43-R01 2L74 4F RT4A25 20050505000312005050500031WP 2005 5 5 IXXA0500065S 120041011A5730 PLATE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING OUTBOARD EXTENDED LEADING EDGE PLATING WITH INTERIM REPAIR AT STA XFS 710.000. REPAIR ACCOMPLISHED REMOVAL OF ALL FASTENERS WITHIN THE REPAIR AREA AND THE EXISTION INTERIM REPAIR. REMOVED THE DAMAGED SKIN AREA AND PERFORMED A NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED THE REPAIR DOUBLER INTERIOR SURFACE AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON LT OUTER WING OUTBOARD LEADING EDGE STA XFS 710.000 USING NEW FASTENERS PER DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DRAWING W43-R14, AND FAA FORM 8110-3. 2L74 4F RT4A25 20050505000322005050500032WP 2005 5 5 IXXA0500066S 120041011A5730 PLATE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C CHECK INSPECTION, FOUND LT WING EXTENDED LEADING EDGE OUTBOARD VANE PLATING INTERIM REPAIR STA XOLDO 67.000. REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SKIN AREA AND PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR DOUBLER, A FILLER AND AN INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE, INTERNAL DOUBLER AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS WITH NEW FASTENERS IAW DOUGLAS SRM, ATI DWG W43-R06 AND FAA FORM 8110-3. 2L74 4F RT4A25 20050505000332005050500033WP 2005 5 5 IXXA0500067S 120041011A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 FITTING FRAME HAS CORROSION DAMAGE ON LOWER SIDE AT STA 960.000. REPAIR ACCOMPLISHED REMOVAL OF THE CORRODED AREA AND FOUND OUT OF LIMITS. FABRICATED NEW FITTING. FABRICATED SPLICES, DOUBLER AND FILLERS. HEAT TREATED DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED AREA AND SPLICES DOUBLER AND FILLERS. APPLIED SEALANT TO FAYING SURFACES, INSTALLED SPLICES AND FILLER AND DOUBLER ON FITTING. INSTALLED NEW FITTING IAW DOUGLAS SRM AND REPAIR SPECIFICATION 2003-05 AND DWG 3647117. 2L74 4F RT4A25 20050511001102005051100110NM 2005 5 11 72300163 120041012A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 SEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER. 2L73 4F4 FRTA3WE E2EA 20050511001122005051100112NM 2005 5 11 72300165 120041018A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 3 INCH BY 12 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050511001162005051100116NM 2005 5 11 72300169 120041028A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME WEB. 2L73 4F4 FRTA3WE E2EA 20050510001012005051000101NM 2005 5 10 20057 120041229A2611 WARNING LIGHT DHAV DHC8 DHC8103 1386005NM PWA PW121 PW121 52124NE HAMSTD14SF 14SF7 NE CARGO SMOKE MALFUNCTIONED A KPVAK NONE J WARNING INDICATION CRCRUISE 1 WP13808WP 026 SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AFFECTED SYSTEM WITH NO FAULTS FOUND. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20050816001102005081600110NM 2005 8 16 SWAA040891 120040325A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D-CHECK, FOUND 5 EA FUSELAGE FRAMES CRACKED AT STRINGER 9L, BS 887, BS 847, BS 827, BS 787, BS 727E. REPAIRED FRAMES PER ER. 2L72 4F RTA16WE 20050816001182005081600118NM 2005 8 16 SWAA041111 120040419A532265C27314 TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 706, STRINGER 1R, BS 787, STRINGER 10L, BS 847, STRINGER 14L, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001332005081600133NM 2005 8 16 SWAA040587 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727D, STRINGERS 8L, 7L, 6L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001382005081600138NM 2005 8 16 SWAA040596 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 878, STRINGER 10R, BS727E, STRINGER 5R, BS 578, STRINGER 8R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001442005081600144NM 2005 8 16 SWAA041335 120040511A53116546520 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29389SW 26592 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 380, STRINGER 8L AND BS 440, STRINGER 8L, CRACKED. REPAIRED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001562005081600156NM 2005 8 16 SWAA040612 120040226A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, STRINGER 10L, BS 277, WL 25, RBL 60 AND BS 727C, STRINGER 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001572005081600157NM 2005 8 16 SWAA040860 120040322A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 500C, BL 0, STRINGER 28L AND BS 500, BETWEEN STRINGERS 26L AND 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001652005081600165NM 2005 8 16 SWAA040931 120040329A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9L, BS 400, BS 787, BS 807, BS 847, BS 887, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20050816001772005081600177NM 2005 8 16 SWAA041122 120040420A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29347SW 24374 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIPS CRACKED AT BS 727D, STRINGER 23L AND STRINGER 25R, BS 500B, STRINGER 26R AND STRINGER 25L, BS 767, STRINGER 23L AND STRINGER 22L, BS 847, STRINGER 20L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001842005081600184NM 2005 8 16 SWAA040616 120040226A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL FLOORBEAMS UPPER CHORD CRACKED AT BS 664, BL 0, WL 208, BS 727A, RBL 45.5, WL 208. REPAIRED CHORDS PER ER. 2L72 4F RTA16WE 20050816001872005081600187NM 2005 8 16 SWAA040646 120040228A53146545866 KEELBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29319SW 23340 DURING SCHEDULED 1/4D CHECK, FOUND RT KEEL BEAM WEB CORRODED AT BS 727 + 11, STRINGER 27R, BS 727 + 14, STRINGER 27R. REPAIRED WEB SECTION PER ER. 2L72 4F RTA16WE 20050816001912005081600191NM 2005 8 16 SWAA040763 120040310A53156546812 FLOORBEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED SPV, FOUND FLOORBEAMS CORRODED AT BS 1006, LBL 14 TO LBL 38, WL 208 AND BS 1016, LBL 3 TO LBL 8, WL 208. REPAIRED FLOORBEAMS PER ER. 2L72 4F A16WE 20050816002092005081600209NM 2005 8 16 MZZA0400004 120041026A3350 BATTERY PACK BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A MZZAO OTHER K FLUID LOSS ININSP/MAINT 1 WP1313227 28788 INSPECTION FOUND RT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK ADN CHARGER ASSY WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2L72 4F RTA16WE 20060117000782006011700078WP 2006 1 17 IAAX0500218S 120041003A5230 SKIN DOUG DC8 DC871F 302199DWP ZONE 800 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND SKIN CRACKED AT AFT CARGO BASKET DOOR AFT RIGHT UPPER CORNER APPROXIMATELY STATION 1200. REMOVED CARGO DOOR. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS. INSTALLED AND ADJUSTED CARGO DOOR IAW SC8 SRM 52-2-0, 52-4-0, AND 51-1-8, DC8 MM 52-31-1. 2L74 4F RT4A25 20060117000802006011700080WP 2006 1 17 IXXA0500227S 120041006A5320 ANGLE DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND RIGHT HAND CUSP CRACKED AT STATION 1050 LONGERON 21 RIGHT. CLEANED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-21-1, 51-2-1, 51-1-5 AND 51-1-8. 2L74 4F RT4A25 20060117000822006011700082WP 2006 1 17 IXXA0500228S 120041011A5300 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING DOUBLER AT STATION 1544 LONGERON 35 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 1537 TO STATION 1551 BETWEEN LONGERON 34 LEFT TO LONGERON 34 RIGHT IAW DC8 SRM 53-21-2, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060117000842006011700084WP 2006 1 17 IXXA0500231S 120041005A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 280 LONGERON 7 RIGHT. CLEANED DAMAGE FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, AND 51-1-8. 2L74 4F RT4A25 20060117000862006011700086WP 2006 1 17 IXXA0500233S 120041005A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 100 LONGERON 7 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, 51-1-5 AND 51-1-8. 2L74 4F RT4A25 20060117000882006011700088WP 2006 1 17 IXXA0500235S 120041003A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CRACKED AT STATION 17 BETWEEN LONGERONS 14 LEFT ANF 17 LEFT, FORWARD ENTRANCE HOLD OPEN PAN AREA. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW COOPESA EO COO-8-53-376-04. 2L74 4F RT4A25 20060117000902006011700090WP 2006 1 17 IXXA0500237S 120041109A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LOWER CHORD AT STATION 70 BETWEEN LONGERONS 35 RIGHT AND 34 LEFT CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW COOPESA EO COO-8-53-440-04. 2L74 4F RT4A25 20060117000922006011700092WP 2006 1 17 IXXA0500239S 120041022A5330 SKIN DOUG DC8 DC871F 302199DWP BS 620-630 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN FROM STATION 620 TO 630 AT LONGERONS 29 LEFT AND 30 LEFT. REMOVED DAMAGED SKIN AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW COOPESA EO COO-8-53-407-4. 2L74 4F RT4A25 20060117001072006011700107WP 2006 1 17 IXXA0500225S 120041002A5230 SKIN DOUG DC8 DC871F 302199DWP ZONE 800 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND FORWARD CARGO DOOR DENTED AT STATION 523 BETWEEN LONGERON 31 RIGHT AND 32 LEFT. REMOVED DOOR. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, PRIMED AND INSTALLED REPAIR PARTS. INSTALLED AND ADJUSTED DOOR IAW DC8 MM 52-30-02, DC8 SRM 52-2-3, 52-4-1, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060117001172006011700117WP 2006 1 17 IXXA0500220S 120041003A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND CORROSION AT FORWARD CARGO COMPARTMENT INNER SKIN STATION 280. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 276.5 TO 280 BETWEEN LONGERON 35 RIGHT AND 35 LEFT IAW DC8 SRM 53-2-0, 51-1-4, 51-3-0, 53-4-1 AND 51-1-8. 2L74 4F RT4A25 20060117000672006011700067WP 2006 1 17 IXXA0500206S 120041110A5300 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS REMOVE EXISTING FASTENERS AND EXISTING FUSELAGE DOUBLER AT STATION 107 LONGERON 35 RIGHT. INSTALL REPAIR AT FUSELAGE SKIN SECTION FROM STATION 98.5 TO STATION 114.5 BETWEEN LONGERON 34 LEFT TO LONGERON 35 RIGHT. FABRICATE REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND FASTENERS IAW COOPESA EO COO-8-53-408-04 DATED 10/23/04. 2L74 4F RT4A25 20060117000712006011700071WP 2006 1 17 IXXA0500210S 120041011A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STATION 680, LONGERON 33 LEFT AND 34 LEFT. REMOVED DAMAGE, FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AT STATION 674 TO STATION 696 BETWEEN LONGERON 31 RIGHT AND 34 RIGHT IAW COOPESA EO COO-8-53-385-04. 2L74 4F RT4A25 20060117000732006011700073WP 2006 1 17 IXXA0500212S 120041008A5310 DOUBLER DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND CENTER FUEL TANK LOWER DOUBLER SKIN BETWEEN FRONT SPAR STATION 683.055 AND STRINGER 65 CORRODED. REMOVED CORROSION, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS. IAW COOPESA EO COO-8-57-388-04. 2L74 4F RT4A25 20060117000752006011700075WP 2006 1 17 IXXA0500214S 120041004A573057103692 CLOSEOUT PANEL DOUG DC8 DC871F 302199DWP WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND AFT WING FILLET PANEL NUMBER 161X SKIN DISBONDED AND CORRODED. FABRICATED NEW PANEL, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FILLET PANEL IAW COOPESA EO COO-8-53-431-04. 2L74 4F RT4A25 20060117000772006011700077WP 2006 1 17 IXXA0500217S 120041003A53134711412501 LONGERON DOUG DC8 DC871F 302199DWP ZONE 100 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND A FITTING WITH A DOUBLE HOLE AT STATION 580 OVER LONGERON 33 RIGHT. FABRICATED NEW FITTING. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 53-2-0, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060117000792006011700079WP 2006 1 17 IXXA0500219S 120041003A5320 ANGLE DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND ANGLE CORRODED AT STATION 297 LONGERON 29 LEFT. REMOVED ANGLE, FABRICATED NEW ANGLE, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW ANGLE WITH NEW HI-LOKS AND RIVETS IAW DC8 SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060117001182006011700118WP 2006 1 17 IXXA0500221S 120041002A53203750257U1 SPLICE DOUG DC8 DC871F 302199DWP BS 440-460 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON SPLICE BROKEN AT STATION 440 TO STATION 460 LONGERON 31 RIGHT. FABRICATED NEW SPLICE, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED, NEW SPLICE AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-20, AND 51-1-8. 2L74 4F RT4A25 20060117001202006011700120WP 2006 1 17 IXXA0500223S 120041003A5230 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND AFT CARGO DOOR SKIN DENTED AT STATION 1402 TO 1407.7 NUMBER 4 BEAM AND LOWER FRAME. REMOVED AFT CARGO DOOR. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS. INSTALLED AND ADJUSTED DOOR IAW DC8 MM 52-32-1, DC8 SRM 52-2-3, 52-4-1, AND 51-1-8. 2L74 4F RT4A25 20050511000032005051100003NM 2005 5 11 USAASB04024 120040302A3230654610912 ARM BOEING737 737301 1384611NM LT MLG FRACTURED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19355US63243 23558 CLT - FLT 240 - UPON GEAR RETRACTION, CREW HEARD A LOUD THUMP. THE LEFT MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BOTH LUGS OF THE LEFT MAIN GEAR ACTUATOR BEAM ARM ASSY HAD FRACTURED, ALLOWING THE RETRACT ACTUATOR BEAM, (WALKING BEAM) AND ACTUATOR TO MOVE OUTBOARD. AT THE OUTBOARD END OF THE ACTUATOR BEAM, THE SUPPORT LINK ASSEMBLY WAS ALSO FRACTURED. REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR BEAM ARM ASSEMBLY, SUPPORT LINK ASSEMBLY AND MAIN LANDING GEAR BEAM ASSEMBLY. REPAIRED IMPACT DAMAGE TO AFT FACE OF LEFT WING REAR SPAR WEB AND FRACTURE DAMAGE TO TWO NEARBY VERTICAL STIFFENERS OF THE REAR SPAR ASSEMBLY. 2L72 4F RTA16WE 20050511001152005051100115NM 2005 5 11 72300168 120041020A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 2 INCH BY 2 INCH AREA OF CORROSION ON FRAME WEB. 2L73 4F4 FRTA3WE E2EA 20050516001252005051600125NM 2005 5 16 2005UALA00364 120040416A4900 APU BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE MALFUNCTIONED A UALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 WP29665UA 29237 RETURNED TO SFO DUE TO AN AUXILIARY POWER UNIT PROBLEM. P2 SENSOR REPLACED. P2 SENSOR CONFIRMED SHIFTED. SHIFT IN FUEL FLOW SCHEDULE CAUSED APU NO START. 2L72 4F4 FRTA1NM E24NE 20050517001102005051700110NM 2005 5 17 72300173 120041017A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 2 INCH AREA OF CORROSION ON BOTTOM OF STRINGER END FITTING. 2L73 4F4 FRTA3WE E2EA 20050523002102005052300210WP 2005 5 23 05FDEA01203 120041202A5754ARB1766501 RIB DOUG MD10 MD1010F 3022112WP LT L/E SLAT DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25559FE 46930 DURING AIRPLANE`S CONVERSION FROM P-F/ACF FOUND AT LT SLAT NR 5 OUTBOARD SIDE RIB WITH HOLE IN RADIUS ANGLE. REPLACE RIB ASSY PER SRM 51-35-01 PG 1-12 SRM 51-35-02 PG 3-9. P/N ARB1766-501. 2L73 4F RTA22WE 20050524001302005052400130WP 2005 5 24 IXXA0500070S 120041011A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLAT DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT OUTER WING INBOARD EXTENDED LEADING EDGE OUTER LOWER PLATING WITH INTERIM REPAIR AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR. THE DAMAGED SECTION WAS REMOVED AND A NDT INSPECTION WAS PERFORMED. FABRICATED REPAIR DOUBLER AND FILLERS. CLEANED, TREATED AND PRIMED INNER FACE OF DOUBLER AND FILLERS. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED NEW DOUBLER AND FILLERS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050524001572005052400157WP 2005 5 24 IXXA0500076S 120041011A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND LOWER EXTERNAL FUSELAGE SKIN CORRODED AT STA 1410.000 L-35. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE CORROSION. FOUND OUT OF LIMITS AND REMOVED THE DAMAGED PLATING. CLEANED, TREATED AND PRIMED AREA. APPLIED THE PRC SEALANT TO FAYING SURFACES AND INSTALLED NEW PLATING IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050524001602005052400160WP 2005 5 24 IXXA0500077S 120040819A5753 SKIN DOUG DC8 DC873F 302199FWP T/E FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND LT INBOARD FLAP WITH TEMP REPAIR ON UPPER SURFACE STA XW 90.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH THE TEMP REPAIR ON IT. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREA AND THE INNER FACE OF THE NEW PLATING. INSTALLED THE NEW PLATING IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050523003742005052300374WP 2005 5 23 IXXA0500069S 120041011A5320 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE LONGERON 24 FITTING FRAME HAS CORROSION DAMAGE AT STATION 940.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FITTING. CLEANED, TREATED AND PRIMED AREA. FABRICATED SPLICES, DOUBLER AND FILLER. PERFORMED HEAT TREATMENT TO DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS WITH NEW FASTENERS AND INSTALLED NEW FITTING IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050524001322005052400132WP 2005 5 24 IXXA0500071S 120041011A5754 SKIN DOUG DC8 DC873F 302199FWP L/E SLAT CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENED LEADING EDGE OUTBOARD VANE PLATING REPAIR DOUBLER WITH ELONGATED HOLES AND CRACK DAMAGE BETWEEN STA XOLDO 67.000 AND XS 497.491. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR DOUBLER AND REMOVAL OF THE DAMAGED AREA. PERFORMED A NDT INSPECTION AND FABRICATED NEW SKIN SEGMENT, INTERNAL DOUBLER AND EXTERNAL SPLICE. CLEANED, TREATED AND PRIMED NEW SKIN SEGMENT, INTERNAL PART AND INTERNAL DOUBLER ALONG WITH THE EXTERNAL SPLICE. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PART WITH NEW FASTENERS IN ACCORDANCE WITH ATI DWG W43-R08 AND DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050524001382005052400138WP 2005 5 24 IXXA0500073S 120041012A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND CRACK ON MAIN CARGO COMPARTMENT FRAME FLANGE 1 INCH AT STA 340.000 L-20L. MAJOR REPAIR ACCOMPLISHED BY REMOVAL OF CRACKED FRAME SEGMENT. FABRICATED NEW FRAME SEGMENT AND SPLICES. HEAT TREATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND NEW FRAME SEGMENT AND SPLICES. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW FRAME SEGMENT AND SPLICES IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL. 2L74 4F RT4A25 20050524003212005052400321NM 2005 5 24 2005UALA00406 120041112A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 FLOORBEAM AT STA 324 RBL 60 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FLOORBEAM CHORD SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20050524001402005052400140WP 2005 5 24 IXXA0500074S 120041011A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL912462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND DAMAGE ON THE FUSELAGE EXTERNAL SKIN AT STA 125.000 - 275.000 L-21L. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SECTION. PERFORMED AN NDT INSPECTION, FABRICATED EXTERNAL REPAIR DOUBLER, FILLERS, FINGER DOUBLERS AND REPAIR TRIPLER. CLEANED, TREATED, PRIMED AREA, DOUBLERS, FILLERS, FINGER DOUBLER AND TRIPLERS. APPLIED PRC SEALANT TO FAYING SURFACES. INSTALLED THE DOUBLERS, FILLERS, FINGER DOUBLER AND TRIPLERS PER THE DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DWG W43-R15, REV IR DATED 10/6/04 AND FAA FORM 8110-3. 2L74 4F RT4A25 20050524001562005052400156WP 2005 5 24 IXXA0500075S 120041011A5754 VANE DOUG DC8 DC873F 302199FWP L/E SLAT DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL921462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND LT WING EXTENDED LEADING EDGE O/B VANE PLATING HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA. AN NDT INSPECTION WAS PERFORMED. FABRICATED REPAIR DOUBELR, FILLER INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED REPAIR DOUBLER, INTERNAL PART, FILLER INTERNAL DOUBLER. APPLIED PRC SEALANT TO FAYING SURFACES AND INSTALLED REPAIR PARTS WITH NEW FASTENERS IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DWG W43-R05. 2L74 4F RT4A25 20050524001352005052400135WP 2005 5 24 IXXA0500072S 120041011A5754 VANE DOUG DC8 DC873F 302199FWP L/E SLAT DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11606AL921462999 46044 DURING A ROUTINE C-CHECK INSPECTION FOUND RT WING EXTENDED LEADING EDGE INBOARD VANE PLATING INTERIM REPAIR AROUND STA XS 247.000. MAJOR REPAIR ACCOMPLISHED BY REMOVAL OF THE FASTENERS WITHIN REPAIR AREA AND THE EXISTING INTERIM REPAIR. REMOVED THE DAMAGED SKIN AREA AND PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AND EXTERNAL REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED THE EXTERNAL REPAIR DOUBLER INTERIOR SURFACE, INTERNAL DOUBLER AND FILLER. APPLIED PRC SEALANT ON FAYING SURFACES. INSTALLED THE REPAIR PARTS ON RT WING EXTENDED L/E INBOARD VANE SLOT USING NEW FASTENERS IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL, ATI DWG W43-R07, FAA FORM 8110-3. 2L74 4F RT4A25 20050526001502005052600150NM 2005 5 26 72300180 120041102A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 1 INCH AREA OF CORROSION ON LOWER CHORD. 2L73 4F4 FRTA3WE E2EA 20050608000662005060800066NE 2005 6 8 GUU2005F00017 220040827A7250 BLADE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GUUAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION APAPPROACH 1 SO294954315662 UE181 DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR2 ENGINE ASSY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K) 2L72 4T4 TRTA24CE E26NE 20050526000802005052600080CE 2005 5 26 CYW2005F00000 120041230A2841 TRANSMITTER BEECH 60 B60 1153605CE LYC O541 TIO541* 41536EA FUEL QTY INOPERATIVE E CYWAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SW13217RB3198 P487 FUEL QUANTITY INDICATORS WOULD ONLY SHOW APPROX 35 GALS MAX EVEN WITH FULL FUEL. FOUND IB AND OB LEADING EDGE CELL TRANSMITTERS GROUNDED TO AIRFRAME. REMOVAL REVEALED GROMMETS DETERIORATED ALLOWING TRANSMITTER CASE TO TOUCH AIRFRAME. RECOMMEND REPLACING GROMMETS WITH FUEL CELLS, ALSO USING MFG RUBBER GASKETS AND TRANSMITTERS. PARTS CATALOG DOES NOT SHOW GROMMETS AT TRANSMITTER INSTALLATION. (K) 1L72 3O3 O A12CE E10EA 20050526001512005052600151NM 2005 5 26 72300181 120041102A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 9 INCH AREA OF CORROSION ON LOWER CHORD. 2L73 4F4 FRTA3WE E2EA 20050606000552005060600055EU 2005 6 6 MAC4801 120040802A3610AC64208 SELECTOR VALVE FOKKERF27 F27MK500 4990629EU PNEUMATIC SYS LEAKING A MTNAO OTHER O OTHER TXTAXI/GRND HDL 1 SO33718FE 10470 DURING TAXI, PNEUMATIC PRESSURE WENT TO 200 PSI RESULTING IN LOSS OF BRAKES AND STEERING. THE LANDING GEAR SELECTOR VALVE WAS DETERMINED TO HAVE CAUSED THE LOSS OF PNEUMATIC PRESSURE. THE VALVE WAS REPLACED AND THE A/C RETURNED TO SERVICE. 2H72 4T A817 20050616000092005061600009SO 2005 6 16 ENHA0506 120041230A2420ALU8521RS ALTERNATOR PIPER PA31 PA31350 7103110SO ENGINE FAILED E ENHAO OTHER O OTHER NRNOT REPORTED 1 AL0378GA 117 318352030 ALTERNATOR FAILED. 1L72 3O A20SO 20050616001512005061600151NM 2005 6 16 72300190 120041026A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 TWO 3 X 3 INCH AREAS OF CORROSION. 2L73 4F4 FRTA3WE E2EA 20050621001962005062100196NM 2005 6 21 2005UALA00528 120041204A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 TWO DENTS LT FUSELAGE AT STA 606, STR 15L AND 16L. REMOVED 4 EA EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR PER EVA IMC-30171. 2L72 4F4 FRTA2NM E17NE 20050628001112005062800111NM 2005 6 28 ASAA0410416 120041001A2611 WIRE BOEING737 7372Q8C 138448SNM PWA JT8 JT8D17 52049NE CARGO SMOKE SHORTED A ASAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM02741AS 21959 AT CRUISE ALT (30,000 FT) GOT FIRE BELL AND CARGO SMOKE LIGHT. THE CARGO SMOKE PANEL HAD (SMOKE) AND (ARMED) ANNUNCIATIONS. CREW FIRED HALON AND DECLARED EMERGENCY. RETURNED TO DEPARTURE WITH NO FURTHER EVENTS. REPLACED BOTH AFT CARGO FIRE BOTTLES AND SQUIBS. FOUND 14VDC AT PIN 9 OF D9503P OF CEU NR 2, FOUND INTERMITTENT SHORT. FOUND WIRES BARE DUE TO RUBBING ON APU BLEED AIR DUCT AT UPPER LT FWD BAG PIT. REPAIRED ALL AFFECTED WIRES (8 EA) IAW AMM. OPS TEST OF CARGO SMOKE DETECTORS AND FIRE SUPPRESSION SYSTEM GOOD REF AMM. (REF SDR ASAA0410410, SUBM 9/29/04 SAME EVENT AWAITING TEARDOWN REPORT. (K) 2L72 4F4 F A16WE E2EA 20050627000652005062700065SO 2005 6 27 C2XA05IA074 120040527A3350 LIGHT EMB 145 EMB145 3260210SO EMERGENCY LIGHTSINTERMITTENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712957 145080 PREFLIGHT INSP FOUND EXIT LIGHTS WERE INOP. MX RESET SYSTEM. OPS CHECKED EXIT LIGHTS WITH NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20050629000532005062900053EA 2005 6 29 ASOA04979S 120041206A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE ENGINE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27907EV 7648 DURING HANGAR MAINTENANCE, THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE WAS FOND TO BE CRACKED BEYOND LIMITS. (S) MAINTENANCE PERFORMED THE PERMANENT REPAIR TO THE ENGINE SUPPORT BEAM LOWER WEB, BL 36.20 RT AND LT SIDE IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050705000772005070500077NM 2005 7 5 BB04014 120040124A4920380029812 APU BOEING767 7672B7 1385107NM APU BAY FAULTY A USAAK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 EA19653US4927549275 24894 WITH LT IDG ON MEL, APU WAS OPERATING ON THE GROUND. APU PERFORMED AN AUTO SHUTDOWN. APU WAS RESTARTED AND SHUTDOWN AGAIN. AFTER SEVERAL ATTEMPTS AT REPLACING COMPONENTS (SURGE VALVE, ECU, LCIT SENSOR), APU REPLACED (11FEB04). VERIFICATION FLIGHT WAS PERFORMED SUCCESSFULLY ON 12FEB04. 2L72 4F RTA1NM 20050707000612005070700061WP 2005 7 7 05FDEA01771 120041119A5512ALC72071 SKIN PANEL DOUG MD10 MD1010F 3022112WP GE CF6 CF66D 30020GL HORIZONTAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25368FE 46606 DURING MAINTENANCE INSPECTION, FOUND CRACK IN THE UPPER CONSTANT SECTION OF THE HORIZONTAL STABILIZER. THE CRACK WAS IN THE FLYABLE LIMITS. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, IAW EA 8-5510-84843 (REF. NRC N0464). 2L73 4F4 FRTA22WE E23EA 20050718001382005071800138 2005 7 18 ASAA044404 420041228A2565 SLIDE BOEING737 7374Q8 138447QNM R1 DOOR FAILED A ASAAO OTHER L NO TEST NRNOT REPORTED 1 NM02769AS 25103 FOUND R1 ESCAPE SLIDE TEST FAILED. REMOVED AND REPLACED SLIDE PER AMM 25-61-35. THIS SLIDE WAS USED AS PART OF A F/A TRAINING EXERCISE. PRIOR TO DEPLOYING SLIDE A `TARP` WAS AFFIXED TO THE FUSELAGE WITH TAPE TO PROTECT THE PAIN FROM INADVERTENT DAMAGE. THE `TARP` WAS INGESTED INTO THE ASPIRATOR OF THE SLIDE BOTTLE AND ENTANGLED WITH THE SLIDE DURING DEPLOYMENT. THE OVERHAUL OF THE SLIDE WS DONE IAW MANUFACTURES INSTRUCTIONS (CMM 25-66-07 AND EO 2560-00148) AND NO DEFECT WAS FOUND WITH THE SLIDE OR AY ASSOCIATED SUBSYSTEM. THIS SLIDE WAS RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 20050720000242005072000024SO 2005 7 20 W9F2005F00000 120041108A329737S3J1 CONNECTOR GULSTMG1159 GIV 3980115SO RROYCETAY TAY6108 NE DOWNLOCK SWITCH DISCONNECTED E W9FAO OTHER N FALSE WARNING DEDESCENT 1 EA071 1071 AFTER SELECTING GEAR DOWN, THE AIRCRAFT EXPERIENCED AN UNSAFE GEAR DOWNLOCK INDICATION ON THE LT MLG. (NO GREEN LIGHT). AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CONNECTOR PLUG DISCONNECTED. CONNECTOR PLUG RECONNECTED, SYS FUNCTIONED NORMALLY. (K) 2L72 4F4 FRTA12EA E25NE 20050719001862005071900186NM 2005 7 19 72300216 120041016A5200 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE DOOR CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON INTERIOR DOOR SKIN. 2L73 4F4 FRTA3WE E2EA 20050719001872005071900187NM 2005 7 19 72300217 120041019A5340 THRESHOLD BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON DOOR THRESHOLD ATTACHMENT ANGLES, WEB STIFFENERS, WEB REPLACEMENT. 2L73 4F4 FRTA3WE E2EA 20050726001662005072600166NM 2005 7 26 72300222 120041025A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CRACKED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CRACK IN SHEAR TIE RADIUS. 2L73 4F4 FRTA3WE E2EA 20050727001502005072700150 2005 7 27 USAABB04027 420040224A2565 SLIDE BOEING757 7572B7 1384964NM R1 DOOR DEPLOYED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19619AU 27198 PIT - DURING AN ANNUAL SLIDE OPERATIONAL CHECK, THE R1 DOOR SLIDE DEPLOYED PROPERLY, BUT FAILED TO HOLD PRESSURE. MAINTENANCE REPLACED THE SLIDE. THE SLIDE WAS FOUND TO HAVE NUMEROUS HOLES. THE HOLES WERE REPAIRED AND THE SLIDE RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 20050727001522005072700152EU 2005 7 27 USAABA04012 220040531A7261 SEAL AIRBUS330 A330323 3930335EU RROYCETAY TAY6118 EU DEOILER LEAKING A USAAA UNSCHED LANDING WK INADEQUATE Q C FLUID LOSS CRCRUISE 1 EA19677UW 0380 MCO - FLT 1470 - THIS FLIGHT WAS A VERIFICATION FLIGHT FOR RIGHT ENGINE OIL LOSS. CREW NOTED THAT THE RIGHT ENGINE WAS AGAIN LOSING OIL. FLIGHT DIVERTED TO MCO. AFTER THE PREVIOUS FLIGHT, EIGHT QUARTS OF OIL HAD BEEN ADDED TO THE ENGINE. MAINTENANCE PERFORMED TSM TASK 79-00-00-810-813 AND COMPLETED THE NR 3 BEARING COMPARTMET BREATHER CHECK. NO DISCREPANCIES WERE FOUND. THE ENGINE WAS OPERATED FOR APPROXIMATELY 45 MINUTES WITH NO OIL LOSS. THE AIRCRAFT WAS RELEASED FOR THIS FLIGHT. MAINTENANCE REPLACED THE DEOILER DRIVE SEAL. ENGINE CONTINUED TO LOSE OIL. THE RIGHT ENGINE WAS REPLACED. TEARDOWN REVEALED THAT THE NR 3 BEARING STACK WAS NOT PROPERLY TORQUED. (M) 2L72 4F4 FRTA46NM E25NE 20050729000912005072900091GL 2005 7 29 ALGA096920 220040819A725023008593 NOZZLE CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C28B 03013GL ENGINE OUT OF TOLERANCEB ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 CAE860266 NOZZLE HEIGHT WAS MEASURED AT .620 1Q71 3R3 U 2A6 E1GL 20050729000922005072900092 2005 7 29 ALGA095538 420040623A8300E6893673 GEAR CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE NICKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 ON INSTALLATION OF T/M GEAR FOUND NICKS ON EDGE OF GEAR TEETH CAUSING ABNORMAL NOISE WHEN SPINNING WITH PINION GEAR. SENT TO VENDOR FOR WARRANTY. 1Q71 3R3 U 2A6 E1GL 20050802000842005080200084NM 2005 8 2 AALA20050474 120041011A5315 FLOORBEAM BOEING767 767323 1385205NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21382AN 25451 AFW - UPPER SURFACE OF FLOORBEAM AT STATION 325 HAD CORROSION BLENDED BEYOND LIMITS. BLENDS AT RIGHT BUTTLINES 17, 22, 22.5, 26.5, 31, 37.5, 40, 41.5, AND 47. CRITICAL BLENDS AT RIGHT BUTTLINE 17 IS 0.8 INCH IN DIAMETER WITH .048 REMAINING FROM A PARENT THICKNESS OF .085. FABRICATED REPAIR STRAP OUT OF 301 AND ONE HALF H STAINLESS STEEL 0.050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH TWO COATS BMS10 11 PRIMER. FILLED BLENDS WITH BMS595 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS595 SEALANT. INSTALLED FASTENERS WITH 46D SPACING. 2L72 4F RTA1NM 20050729000932005072900093GL 2005 7 29 ALGA094257 220040426A725023053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30 03013GL ENGINE OUT OF TOLERANCEB ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03 FLOW AREA ON THIS PART IS BELOW MIN. FLOW OF 5.770. ACTUAL: 5.74 RETURNED PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20050809000072005080900007WP 2005 8 9 IXXA0500080S 120041209A5730 SKIN DOUG DC8 DC873F 302199FWP ZONE 500 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A C-CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN WITH INTERIM REPAIR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED PLATING PANEL. FABRICACTED NEW PLATING PANEL. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING PANEL INTERNAL PART. APPLIED PRC SEALANT TO FAYING SERVICES. INSTALLED NEW PLATING PANEL IAW DC8 SRM 51-1-21, 51-3-0, 51-1-8B 51-1-11 AND FAA FORM 8110-3 DWG SEMAN ED 3774. 2L74 4F RT4A25 20050816001112005081600111NM 2005 8 16 SWAA040875 120040323A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9L, BS 360, BS 400, BS 440, BS 480, BS 727E, BS 747, BS 807, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER. 2L72 4F RTA16WE 20050816001142005081600114NM 2005 8 16 SWAA040964 120040401A53226546569 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 927, AND BS 887, BETWEEN STRINGERS 26L AND 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001552005081600155NM 2005 8 16 SWAA041603 120040606A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 787, BS 827, BS 867,BS 907, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001592005081600159NM 2005 8 16 SWAA040889 120040325A53116546500 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 492, STR 24R-STR 25R, AND BS 616, RBL 65, WL 202. REPAIRED FRAMES PER ER AND SRM. 2L72 4F RTA16WE 20050816001672005081600167NM 2005 8 16 SWAA040940 120040330A53156545410 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29304SW 22944 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM WEBS AT BS 709, RBL 25, BS 706, BL 0, CRACKED. REMOVED AND REPLACED WEB SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001702005081600170NM 2005 8 16 SWAA041040 120040411A53116546546 TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES IN AFT CARGO COMPARTMENT AT BS 747, LBL 9, AND BS 787, BL 0, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001752005081600175NM 2005 8 16 SWAA041096 120040418A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAMS AT BS 727D + 5, LBL 13, AND BS 774 TO BS 777, LBL 8, CORRODED. REPAIRED FLOORBEAMS PER EA. 2L72 4F RTA16WE 20050816001822005081600182NM 2005 8 16 SWAA040615 120040226A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, LBL 25, WL 203, BS 947, LBL 52, WL 208. REPAIRED WEB PER ER. 2L72 4F RTA16WE 20050816001882005081600188NM 2005 8 16 SWAA040561 120040223A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND BS 500 + 17, STRINGER 28L AND BS 493, STRINGER 28R, CORRODED. REPAIRED STRINGERS PER SRM. 2L72 4F RTA16WE 20050816001902005081600190NM 2005 8 16 SWAA040694 120040304A53156546804 FLOORBEAM BOEING737 7373A4 1384585NM CABIN FLOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER SURFACES CORRODED AT BS 344, LBL 10 TO LBL 65, BS 328, RBL 15 TO RBL 50, AND BS 312, LBL 8 TO RBL 49. REPAIRED FLOORBEAMS PER SRM. 2L72 4F RTA16WE 20050816001952005081600195NM 2005 8 16 SWAA040722 120040307A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29348SW 24375 DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 787, STR 25L AND BS 807, STR 25L. REMOVED AND REPLACED STR CLIPS PER SRM. 2L72 4F RTA16WE 20050818000332005081800033NM 2005 8 18 SWAA041829 120040629A53226546529 SHEAR TIE BOEING737 7373T5 1384608NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES AT BS 500B, LBL 18, BS 500C, LBL 18, BS 500D, LBL 16 TO LBL 19, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050816001262005081600126NM 2005 8 16 SWAA040269 120040127A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT THE FOLLOWING BS 500D, STRINGER 8R, BS 520, STRINGER 8R, BS 578, STRINGER 8R, BS 597, STRINGERS 8R AND 7R, BS 616, STRINGERS 8R AND 8L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001272005081600127NM 2005 8 16 SWAA040496 120040217A53306545700 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29689SW 23387 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT FOLLOWING LOCATIONS, BS 740, STRINGER 18R, BS 740, STRINGER 24L, BS 920, STRINGER 23R AND BS 930, STRINGER 25L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050816001392005081600139NM 2005 8 16 SWAA040597 120040225A534065C27314 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 460, STRINGER 14L, BS 595, STRINGER 7L, BS 597, STRINGER 8L, BS 706, STRINGER 11L, BS 616, STRINGER 2L. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20050816001402005081600140NM 2005 8 16 SWAA041739 120040621A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 907, BS 867, BS 827, BS, 787, STRINGER 8L, BS 907, BS 867, BS 787, STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001542005081600154NM 2005 8 16 SWAA041479 120040524A53116546550 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED D-CHECK, FOUND FRAMES AT BS 907, BS 787, STRINGER 9R, CRACKED. REMOVED AND REPLACED FRAME SECTIONS PER SRM. 2L72 4F RTA16WE 20050816001722005081600172NM 2005 8 16 SWAA041015 120040408A53106547978 CREASE BEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB AT RT BS 360 TO RT BS 380, LT BS 400 TO LT BS 420, CORRODED. REMOVED AND REPLACED CREASE BEAM WEB PER EA. 2L72 4F RTA16WE 20050816001762005081600176NM 2005 8 16 SWAA041103 120040418A2612 WARNING LIGHT BOEING737 7372H4 138448CNM CARGO BAY FIRE ILLUMINATED A SWAAO OTHER N FALSE WARNING DEDESCENT 1 SW29091SW 22963 DECLARED EMERGENCY, AT FL 22.0 FWD CARGO BAY FIRE DETECTION LIGHT ILLUMINATED AND BELL CAME ON. DISCHARGED BOTTLES. AFTER 2 MINUTES FWD CARGO BAY FIRE LIGHT WENT OUT. REMOVED AND REPLACED NR 1 AND NR 2 FIRE BOTTLES, CARGO FIRE SYSTEM METERING VALVE, DIVERTER VALVE, PER MM. 2L72 4F A16WE 20050816001852005081600185NM 2005 8 16 SWAA040617 120040226A53116546500 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 706, STRINGER 11R, BS 616, STRINGER 7L. REPAIRED FRAMES SECTION PER SRM. 2L72 4F RTA16WE 20050816001942005081600194NM 2005 8 16 SWAA040695 120040304A53226546508 SHEAR TIE BOEING737 7373A4 1384585NM LOWER FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D-CHECK, FOUND 2 EA LOWER FUSELAGE SHEAR TIES CORRODED AT BS 500D, LBL 6 TO LBL 10, AND BS 847, RBL 5. REPAIRED SHEAR TIES PER SRM. 2L72 4F RTA16WE 20050817001652005081700165NM 2005 8 17 SWAA040817 120040316A534065C27314 CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29699SW 23826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 520, STRINGER 4R AND BS 867, STRINGER 9R. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20060227002892006022700289WP 2006 2 27 IXXA060151S 120040610A5414 SKIN DOUG DC8 DC873F 302199FWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT INBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR ATTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED REPAIR DOUBLERS AND NEW FASTENERS IAW DC8 SERVICE BULLETIN 54-93. 2L74 4F RT4A25 20060227002922006022700292WP 2006 2 27 IXXA060154S 120040617A5420 ANGLE DOUG DC8 DC873F 302199FWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON LOWER AFT SECTION HAS CRACKED RIB ANGLE VERY AFT RIB. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB ANGLE. FABRICATED NEW RIB ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, PRIMED. INSTALLED NEW RIB ANGLE AND NEW FASTENERS IAW DC8 SRM 51-1-4, 54-2-0 AND 51-1-8. 2L74 4F RT4A25 20050822000862005082200086EA 2005 8 22 BCF2005F00000 220040922A855006B23072 GASKET PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA OIL FILTER FAILED E BCFAO OTHER O OTHER NRNOT REPORTED 1 EA0327956196 317952064 PILOT REPORTED SEEING FIRE ON RT ENGINE, SHUTDOWN ENGINE, LANDED, AFTER INSPECTION FOUND OIL LEAKING AROUND OIL CONVERTER GASKET. THE GASKET WAS INSTALLED NEW IAW SB AND AD AND GASKET WAS FOUND TO BE SOFT AND EDGES WERE PRETRUDING OUT, ALSO FOUND A PIECE OF GASKET BLOWED OUT. POSSIBLY COULD BE SOME GASKETS MARKED WRONG FROM MFG. (K) 1L72 3O3 O A20SO E14EA 20050822000792005082200079CE 2005 8 22 EEJ2005F00000 120041012A2510MS203922C11 CLEVIS CESSNA CESSNA172 172N 2072434CE LYC O320 O320* 41508EA SEAT PIN WORN E EEJAK NONE O OTHER ININSP/MAINT 1 NM079390E 17272243 FIELD EXP HAS SHOWN DURING COMPLIANCE WITH AD IS NOT JUST FOR THE RAILS INSP THE ENTIRE SEAT TOO! HAVE SEEN MS203922C11 CLEVIS PINS WORN TO .030. IF BOTH PINS FAIL, THE SEAT BACK WILL RECLINE ANOTHER 60 DEGREES OR GO FLAT RESULTING IN LOSS OF AIRCRAFT. (K) 1H71 3O3 ONT3A12 E274 20050830000682005083000068WP 2005 8 30 ASAA0580394 120041228A3350L201919 LIGHT DOUG DC9 DC983 3022083WP COCKPIT LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM02944AS 53019 SEA - PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING DID NOT ILLUMINATE DURING SYSTEM TEST. RESECURED LOOSE CONNECTOR AT L2-550. LIGHTS THEN OPERATED PROPERLY. (M) 2L72 4F RTA6WE 20050901001152005090100115EU 2005 9 1 MHI2005F00001 120041227A5610350KA25900400 WINDSHIELD UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE COCKPIT CRACKED E MHIAO OTHER O OTHER APAPPROACH 1 EA25454AE 3490 23011 AIRCRAFT WAS ON APPROACH AND THE LOWER PORTION OF THE WINDSCREEN CRACKED THROUGH, THE LOWER POTION OF THE WINDSCREEN FROM THE JOGGLE POINTS IN LOWERED INTO THE CABIN. DID NOT COME LOOSE FROM THE BONDING MATERIAL. REPAIRED IAW MM, REPLACED WINDSCREEN WITH NEW. WEATHER COLD UNDER 20 DEGREES F. THIS IS SECOND WINDSCREEN TO CRACK IN FLIGHT IN COLD WEATHER. (K) 1G72 3U3 U H9EU E00054EN 20050920001312005092000131EU 2005 9 20 MTNA20043 120040427A5100 FIRE FOKKERF27 F27MK500 4990629EU AFT DETECTED A MTNAFBA ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CRCRUISE 1 SO33715FE 10468 DURING FLIGHT FDX7145 EZE-POA THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE THIRD CREW MEMBER OCCUPYING THE JUMP SEAT CHECKED THE CARGO COMPARTMENT AND OBSERVED FLAMES IN THE REAR OF THE AIRCRAFT. THE CREW DECLARED AN EMERGENCY AND THE JUMPSEAT CREW MEMBER USED 2 HAND HELD EXTINGUISHERS ON THE CARGO TO SUPPRESS THE FLAMES. THE AIRCRAFT MADE A SUCCESSFUL LANDING IN MELO, URUGUAY. AFTER LANDING FIRE CREWS ARRIVED AND FINISHED EXTINGUISHING THE FIRE WHICH WAS STILL SMOLDERING. 2H72 4T A817 20050926000012005092600001EA 2005 9 26 200400653 120041125A5210 HANDLE CNDAIRCL600 CL6002C10 1390015EA PAX DOOR LOOSE A MASAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07506MJ 10073 ASH 7204 ORD TO ATL - A/C DIVERTED TO BNA DUE TO A MAIN CABIN DOOR WARNING MESSAGE. MX FOUND THE DOOR OUTER HANDLE OPEN WHEN PLANE ROLLED UP, AND BY CLOSING THE OUTER HANDLE THE MESSAGE WENT AWAY. AFTER NUMEROUS OPS CHECKS, THE PROBLEM COULD NOT BE DUPLICATED. 2L72 4F RTA21EA 20050926000022005092600002EA 2005 9 26 MASA200400644 120041119A2700 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA CONFIGURATION ILLUMINATED A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07507MJ 10077 ASH 7230 DEN - ABORTED TAKEOFF FOR TAKEOFF CONFIG MESSAGE AT 80 KNOTS. MAINTENANCE CURRENTLY TROUBLESHOOTING. 11/19/2004 MAINTENANCE PERFORMED CONFIGURATION OPS CHECK AND ALL CHECKS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20050922000402005092200040EA 2005 9 22 MASA200500586 120040723A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER NRNOT REPORTED 1 SW0717231 7231 ASH 6713 PHX. FLOOR ELECTROLUMINESCENT PROXIMITY EMERGENCY ESCAPE PATH LIGHT WITHOUT ORANGE OVERLAY WAS FOUND TO BE INOP. MX PLACED THAT SECTION OF LIGHTS ON MEL. ACFT CONTINUED OPERATIONS. 2L72 4F RTA21EA 20050926001452005092600145EA 2005 9 26 MASA200400673 120041202A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW07506MJ 10073 ASH 7262 TUS, THE FLIGHT CREW REPORTED THE LAVATORY SMOKE DETECTOR ALARM SOUNDED UPON POWER UP. MAINTENANCE RESET THE SYSTEM AND THE SYSTEM TESTED NORMALLY. 2L72 4F RTA21EA 20050926001472005092600147 2005 9 26 MASA200400698 420041214A31008221310101 DCU CNDAIRCL600 CL6002C10 1390015EA COCKPIT NO INDICATION A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07507MJ946 10077 ASH 7251 AT 125 KNOTS, ON TAKEOFF ROLL RECEIVED CONFIG AILERON WARNING AT HIGH SPEED. CREW ABORTED TAKEOFF AND AIRCRAFT WAS FERRIED TO PHL FOR REPAIRS. MAINTENANCE REPLACED NR 1 DCU BUT IN THE PROCESS FOUND 2 CHAFED HYD LINES AND ARE NOW AOG FOR PARTS. MAINTENANCE REPLACED HYD LINES. 2L72 4F RTA21EA 20050926001622005092600162EA 2005 9 26 MASA200400670 120041130A2711 TRIM SWITCH CNDAIRCL600 CL6002C10 1390015EA AILERONS DIRTY A MASAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW07507MJ 10077 ASH 7246 DEN, WITH TAKEOFF CONFIG OK RECEIVED AILERON CONFIG WARNING AND AILERON TRIM WARNING. MAINTENANCE CLEANED TRIM SWITCH, OPS CHECKED GOOD. 2L72 4F RTA21EA 20050926001652005092600165EA 2005 9 26 MASA200400721 120041222A2611 SMOKE DETECTOR CNDAIRCL600 CL6002C10 1390015EA LAVATORY MALFUNCTIONED A MASAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW07502MJ 10050 ASH 7217 ATL - MASTER WARNING FOR SMOKE IN AFT LAVATORY. CONTRACT MAINTENANCE PLACED LAV ON MEL. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND OPS CHECKED GOOD. 2L72 4F RTA21EA 20050926000902005092600090EA 2005 9 26 MASA200400655 120041126A2131GG670980025 CONTROLLER CNDAIRCL600 CL6002D24 1390016EA CABIN PRESSURE UNCONTROLLABLE A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07902FJ1889 15002 ASH 6931 MZT-LAX, THE CREW RETURNED THE AIRCRAFT TO THE FIELD DUE TO LOSS OF CABIN PRESSURIZATION CONTROL. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. 11/27/04 MAINTENANCE REPLACED NR 1 CABIN PRESSURE CONTROLLER. OPS CHECKED GOOD. 2L72 4F RTA21EA 20050926001462005092600146EA 2005 9 26 MASA200400731 120041229A2150GG670950091 ACM CNDAIRCL600 CL6002C10 1390015EA ODOR A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW07506MJ1158 10073 ASH 7210 AUS, RETURNED TO FIELD WITH SMELL AND VISIBLE SMOKE AFT LAV SMOKE DETECTOR ALARMED. PILOT DECLARED AN EMERGENCY AND EMERGENCY ESCAPE PROCEDURES WERE PERFORMED. AIRCRAFT WAS PREPPED FOR FERRY TO TUS FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED BOTH ACM'S. 2L72 4F RTA21EA 20050926001492005092600149EA 2005 9 26 MASA200400681 120041204A2710 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA AILERONS FALSE INDICATIONA MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07507MJ 10077 ASH 7240 LAX-TUS - CAPTAIN ABORTED TAKEOFF AND RETURNED TO GATE. REPORTED THAT PRIOR TO TAKEOFF ROLL, THE AIRCRAFT HAD TAKEOFF CONFIG OK AND ALL TRIMS GREEN. THEN ON TAKEOFF ROLL, RECEIVED CONFIG AILERON WARNING AND AILERON TRIM AURALS. MAINTENANCE CHECKED AILERON TRIM SWITCH CONNECTIONS, PERFORMED SYSTEMS OPS CHECKS, OPS CHECKED NORMAL. MAINTENANCE WENT WITH FLIGHT CREW FOR OPS CHECK ON RUNWAY, SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20060425001052006042500105SO 2006 4 25 SIMA200534701 120041208A5330AL2024T3 SKIN EMB 135 EMB135LR 3260305SO MAIN DOOR DENTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE11722 145301 A DENT WITH GOUGES WAS FOUND ON THE OUTER SKIN OF THE MAIN DOOR. REMOVED THE PAINT FROM AREA AND BLENDED OUT GOUGES. PERFORMED NDT INSP OF AREA WITH NO INDICATIONS NOTED. FABRICATED A DOUBLER, REPAIR DONE IAW REPAIR STATEMENT AND SRM. (K) 2L72 4F RTT00011AT 20060425001062006042500106EU 2006 4 25 SIMA200536101 120041222A33506013211 BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAO OTHER L NO TEST TXTAXI/GRND HDL 1 SW21301AE 340B301 EMERGENCY LIGHTS AT ROW 9 AND 10 WILL NOT ILLUMINATE DURING TEST. EXIT SIGN OVER SEAT 8A DOES NOT ILLUMINATE. REPLACED BATTERY PACK. IAW MM OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K) 2L72 4T RTA52EU 20060425001252006042500125EA 2006 4 25 SIM2006F00001 120041208A2133 OUTFLOW VALVE CNDAIRCL600 CL6002C10 1390015EA CABIN PRESS SYS MALFUNCTIONED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21511AE 10107 CONTACTED BY THE CREW VIA TELESIS, AIRCRAFT WILL NOT PRESSURIZE IN AUTO MODE, SELECTED TO MANUAL MODE AND PRESSURIZATION WORKS OK. CREW ELECTED TO RETURN TO BLOCK. LT AND RT PRSOV. PERFORMED PRESSURIZATION OPS CHECK, OPS CHECK GOOD LT PRSOV, PN OFF GG670800025, SN OF 00455, RT PRSOV PN OFF GG670800025 SH OFF 00453. (K) 2L72 4F RTA21EA 20060425000932006042500093SO 2006 4 25 SIMA200534706 120041211A532014522461011 GUSSET EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21723AE 145288 FOUND GUSSETS ABOVE RT OMEGA BVEAM ARE CORRODED AT FRAME. REPLACED GUSSET DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20060425000942006042500094SO 2006 4 25 SIMA200534704 120041206A532014525381003 BEAM EMB 135 EMB135LR 3260305SO GALLEY CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE11722 145301 THE LT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING CUTOUT. FABRICATED A DOUBLER, FILLER, AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F RTT00011AT 20060425000922006042500092SO 2006 4 25 SIMA200534703 120041208A532014525381003 BEAM EMB 135 EMB135LR 3260305SO FRAME 25 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE 145301 THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKEING A CUT OUT. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F RTT00011AT 20060425001102006042500110SO 2006 4 25 SIMA200534702 120041203A532014525381003 BEAM EMB 135 EMB135LR 3260305SO FRAME 20 CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21724AE 145301 A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K) 2L72 4F RTT00011AT 20060425001202006042500120SO 2006 4 25 SIMA200534801 120041211A335020131A BATTERY PACK EMB 135 EMB135KL 3260302SO CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21828AE 145604 CREW NOTED WHEN ACTIVATING EMERGENCY LIGHTS FOR TEST, LIGHTS WOULD ILLUMINATE THEN FADE OUT FAST. CA REPLACED ALL 4 EMERGENCY LIGHT BATTERIES. OPERATONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K) 2L72 4F RTT00011AT 20050926001242005092600124 2005 9 26 MASA200400669 420041130A3416 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA ALTIMETER FALSE INDICATIONA MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07504MJ 10066 ASH 7248 DEN-DSM, AIRCRAFT RETURNED TO GATE WITH GLD UNSAFE CAUTION MESSAGE. MAINTENANCE CLEANED THE RADIO ALTIMETER ANTENNA AND IT OPS CHECKED GOOD. 2L72 4F RTA21EA 20050926001412005092600141EA 2005 9 26 MASA200400708 120041219A7830TY214810A ISOLATION VALVE CNDAIRCL600 CL6002C10 1390015EA THRUST REVERSER INOPERATIVE A MASAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW07502MJ3913 10050 ASH 7256 RDU-IAD, THE CREW ABORTED TAKEOFF DUE TO A LEFT REVERSER UNSAFE MESSAGE. THE AIRCRAFT RETURNED TO THE GATE AND THE REVERSER WAS PLACED ON DEFERRAL. MAINTENANCE REMOVED AND REPLACED ISOLATION VALVE. 2L72 4F RTA21EA 20051017000132005101700013WP 2005 10 17 IXXA0500087S 120041108A5744 HINGE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C-CHECK INSPECTION FOUND LT OB FLAP HINGE CRACKED AT STATION XC 337.000. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED SUPPORT FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SUPPORT FITTING IAW SRM 51-1-21 SRM 51-20D AND 51-3-0. 2L74 4F4 FRT4A25 E2GL 20051017000142005101700014WP 2005 10 17 IXXA0500099S 120041211A5315 FLOOR PANEL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BS 759 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM CORROSION DAMAGE IN CARGO COMPARTMENT AT STA FS 759.000 LBL 10. REPAIR ACCOMPLISHED BY REMOVING THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-32-0 PG 2P. FABRICATED REAPRI ANGLE IAW DC8 SRM 53-2-0 FIG 1 SHEET 1, 2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 P 9. INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1G. SHEET 1, 2 SRM 51-1-21 PG 1, SRN 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20051017000212005101700021CE 2005 10 17 UAT2005F00008 120041129A2421DOFF10300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520* 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL039736M 20700722 ALTERNATOR FAILED AT 233.0 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051017000122005101700012WP 2005 10 17 IXXA0500102S 120041214A5210 DOOR DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 200 MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C-CHECK INSPECTION FOUND PASSENGER DOOR FORWARD UPPER CORNER HAS A TEMPORARY REPAIR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF REPAIR. FABRICATED DOUBLER, TRIPLER, & FILLER. CLEANED, TREATED AND PRIMED AREA, REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 15 SHEET 4,5,8, SRM 51-1-20A SRM 51-1-20D PG 9 AND SRM 51-1-21 PG 1, DWG 5750776. 2L74 4F4 FRT4A25 E2GL 20051017001252005101700125WP 2005 10 17 IXXA0500084S 120041208A5753 SKIN DOUG DC8 DC873F 302199FWP TE FLAP DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS INTERIM REPAIR BETWEEN STATION XW63.00-XW91.000. MAJOR REPAIR WAS ACCOMPLISHED BY REMOVED THE UPPER PLATING WITH INTERIM REPAIR. FABRICATED NEW PLATING PANEL, CLEANED, TREATED AND PRIMED AREA + NEW PLATING PANEL INTERNAL PART APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW PLATING PANEL IN ACCORDANCE WITH DC8 SRM 51-1-8B, FAA FORM 8110 NR 04571, DWG SEMAN EO 3375-1, SRM 51-1-11 AND 51-1-21 AND 51-3-0. 2L74 4F RT4A25 20051017001282005101700128WP 2005 10 17 IXXA0500085S 120041111A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD L/E INTERIM REPAIR AT STA XFS 710.000. ACCOMPLISHED MAJOR REPAIR BY REMOVING EXISTING REPAIR AND THE DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOULBER AND FILLER IN ACCORDANCE WITH FAA FORM 8110-3 NR 04589, SEMAN DWG EO 3788, DC8 SRM 51-1-21, 51-3-0, 51-1-20D. CLEANED, TREATED AND PRIMED AREA + FILLER + DOUBLER INTERNAL PART IN ACCORDANCE WITH DC9 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 INSTALLED FILLER + DOUBLER WITH NEW FASTENERS IAW DWG SEMON EO 3788, DC8 SRM 51-1-20D AND DC8 SRM 51-3-0 DC8 SRM 51-1-21. 2L74 4F RT4A25 20051017001302005101700130WP 2005 10 17 IXXA0500088S 120041111A5754 VANE DOUG DC8 DC873F 302199FWP XOLDO DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C-CHECK INSPECTION, FOUND LEADING WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STATION XOLDO 67.000. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR, REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION AND FABRICATED PLATING SEGMENT, REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA. REPAIRED PARTS INTERNAL PARTS. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW DWG SEMAN EO 3785, SRM 51-1-21, 51-1-20D, 51-3-0, DWG SEMON EO NR 3785, SRM 51-1-21A. 2L74 4F RT4A25 20051017001312005101700131WP 2005 10 17 IXXA0500100S 120041110A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP BS 560 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND FOWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 560.000 RBL 60. MAJOR REPAIR ACCOMPLISHED BLEND OUT OF DAMAGED AREA. FOUND OUT OF LIMITS IAW DC8 SRM 53.2.0 FIG 1F. FABRICATED REPAIR ANGLE IAW EC8 SRM 53-2-0 FIG 1G SHEET 1-2. CLEANED, TREATED AND PRIMED AREA, REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-0 FIG 16, DC8 SRM 51-1-20 D PG 9 SRM 51-.-0 PG 1. 2L74 4F RT4A25 20051017001292005101700129WP 2005 10 17 IXXA0500086S 120041208A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION FOUND LT L/E WING INBOARD EXTENDED L/E OUTER PLATING INTERIM REPAIR AROUND STA XSF 710.000. MAJOR REPAIR ACCOMP IAW FAA FORM 8110-3 NR 04592, DWG SEMON EO 3787. REMOVED FASTENERS IAW DC8 SRM 51-1-21 AND SRM 51-1-20D. REMOVED DAMAGED AREA IAW DWG SEMON EO 3787. PERFORMED NDT INSPECTION IAW DWG EO 3787, DC8 NDT SRM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER + FILLER IAW DWG SEMON EO 3787. CLEANED, TREATED AND PRIMED AREA + REPAIRED PARTS INTERNAL PART IAW DC9 SRM 51-1-8B APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW DWG SEMAN EO 3787 DC8 SRM 51-1-21 AND 51-1-20D 2L74 4F RT4A25 20051017001322005101700132WP 2005 10 17 IXXA0500101S 120041214A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING NR 4 STUB WING INTERNAL RIB CRACKED 3" XS 520.468. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED RIB IAW DC8 SRM 51-1-20D PAGE 21 DC8 SRM 51-3-0 PG 1. FABRICATED NEW RIB IAW REPAIR SPEC NR 2003-05 DWG 9753297 DC8 SRM 51-1-1 PG 1. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PG 1, 13, 17 DPS7.00-1 REV. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 00-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW RIB IAW DC8 SRM 51-1-8B. INSTALLED NEW RIB WITH FASTENERS IAW DC8 SRM 51-3-0 PG 1 DC8 SRM 51-1-21 PG1 DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20051020001682005102000168SO 2005 10 20 MASA200400308 120040604A2611 FIRE WARNING EMB 145 EMB145LR 3260212SO CARGO BAY FALSE ACTIVATIONA MASAK NONE N FALSE WARNING ININSP/MAINT 1 SW07841MJ7091 145448 ASH 2758 CLT. BAG FIRE EXTINGUISHER LIGHT W/N ILLUMINATE DURING FIRE TEST. FOUND BOTH BAG COMPARTMENTS FIRE EXTINGUISHERS EXPENDED. REPLACED BOTH EXTINGUISHERS. 224 CU IN P/N 33700027-1, S/N 39422D1, 360 CU IN P/N 34600073-1, S/N 19779F1. 2L72 4T RTT00011AT 20060224000882006022400088WP 2006 2 24 IXXA060048S 120041009A5320 SUPPORT BEAM DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EMERGENCY EXIT DOOR BEAM INBOARD CHORD CRACKED AT CENTER SECTION FROM STATION 1110.000 TO STATION 1140.000 AT STOP FITTING 7. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED CHORD. FAB`D NEW CHORD, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW CHORD AND FASTENERS FROM STATION 1110.000 TO STATION 1140.000 AT STOP FITTING 7 IAW DC8 SRM 52-1-0, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060224000932006022400093WP 2006 2 24 IXXA060056S 120041016A5720 STRAP DOUG DC8 DC871F 302199DWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 347.750. REMOVE DAMAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEFT WING CENTER LEADING EDGE STATION XFS 347.750. IAW DC8 SRM 57-1-0, AND 51-1-20. 2L74 4F RT4A25 20060224000952006022400095WP 2006 2 24 IXXA060058S 120041017A5712 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 464.000. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT LEFT WING LEADING EDGE UPPER RIB AT STATION XFS464.000. IAW DC8 SRM 57-3-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224000982006022400098WP 2006 2 24 IXXA060060S 120041002A5320 SUPPORT ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND A CRACKED SUPPORT ANGLE AT EXTERNAL FUSELAGE STATION 781.5, +X65. REMOVED DAMAGE. FAB`D REPAIR ANGLE, LOCATED, DRILLED, TRIMMED TREATED, PRIMED, INSTALLED REPAIR ANGLE AND NEW FASTENERS AT EXTERNAL FUSELAGE STATION 781.5, +X65. IAW DC8 SRM 53-2-0, 51-1-20, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001002006022400100WP 2006 2 24 IXXA060061S 120041002A5320 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LOWER FUSELAGE DOUBLER CORRODED FROM STATION 690 TO 778. REMOVED FASTENERS AS NEEDED TO REMOVE EXISTING DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER, AND FASTENERS WET WITH SEALANT FROM STATION 690 TO 778. IAW DC8 SRM 53-2-0, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001012006022400101WP 2006 2 24 IXXA060062S 120041002A5320 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX8582334028 45978 DURING ROUTINE C CHECK, FOUND A CRACKED WEB AT EXTERNAL FUSELAGE STATION 778.5 BETWEEN LONGERON 33 RIGHT AND 35 RIGHT. REMOVED HYDRAULIC LINES FOR ACCESS. REMOVED ACCESS PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 786.5 BETWEEN +X6 AND +X44. INSTALLED ACCESS PANEL, AND HYDRAULIC LINES, AND LEAK CHECKED IAW DC8 MM 20-12-0, 20-16-0, 29-00-00 DC8 SRM 53-2-0, 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001062006022400106WP 2006 2 24 IXXA060065S 120041003A5320 SUPPORT ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED IN THE FORWARD CARGO COMPARTMENT BETWEEN STATION 580 AND 637 AT LONGERON 33 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPROT ANGLE. FABRICATED NEW ANGLE. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW FLOOR SUPPORT ANGLE AND FASTENERS FROM STATION 580 TO STATION 637 AT LONGERON 33 RIGHT IAW DC8 SRM 53-2-0, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001072006022400107WP 2006 2 24 IXXA060066S 120041003A5320 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 980 BETWEEN +X65 TO -Z54. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW EXTERNAL FUSELAGE ANGLE AND FASTENERS AT STATION 980 BETWEEN +X65 AND -Z54 IAW 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001092006022400109WP 2006 2 24 IXXA060067S 120041003A5330 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE DOUBLER WORN AT STATION 980 BETWEEN +X65 TO -Z54. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW EXTERNAL FUSELAGE DOUBLER AND FASTENERS AT STATION 980 BETWEEN +X65 AND -Z54. IAW 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001132006022400113WP 2006 2 24 IXXA060053S 120041007A5514 ANGLE DOUG DC8 DC871F 302199DWP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE LOWER ANGLE CRACKED AT STATION XE 29.77. REMOVED DAMAGE, FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND FASTENERS IN LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER ANGLE AT STATION XE 29.77 IAW DC8 SRM 51-2-1, 51-1-4, 51-1-5 AND 51-1-8. 2L74 4F RT4A25 20060224001162006022400116WP 2006 2 24 IXXA060052S 120040930A5511 RIB DOUG DC8 DC871F 302199DWP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE INBOARD RIB CRACKED AT STATION XFS 141.250. REMOVED DAMAGE. FAB`D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PART AT STATION XFS 141.250 IN RIGHT HORIZONTAL STABILIZER LEADING EDGE IAW DC8 SRM 55-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001202006022400120WP 2006 2 24 IXXA060055S 120041012A575357511521 FITTING DOUG DC8 DC871F 302199DWP T/E FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE FLAP DRIVE LINK FITTING CRACKED AT STATION XW 97.906. REMOVED DRIVE LINK. REMOVED DAMAGED DRIVE LINK FITTING. RECEIVED NEW DRIVE LINK FITTING AND INSTALLED NEW FITTING AT STATION 97.906. INSTALLED DRIVE LINK FORWARD ATTACH POINT IAW DC8 MM 27-21-4. 2L74 4F RT4A25 20060224001222006022400122WP 2006 2 24 IXXA060057S 120041016A5720 STRAP DOUG DC8 DC871F 302199DWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 366.500. REMOVE DAMAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEFT WING CENTER LEADING EDGE STATION XFS 366.500 IAW DC8 SRM 57-1-0, AND 51-1-20. 2L74 4F RT4A25 20060224001242006022400124WP 2006 2 24 IXXA060068S 120041003A5320 SUPPORT ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SUPPORT ANGLE CRACKED AT STATION 640 BETWEEN +X70 AND -Z35. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED SUPPORT ANGLE. FABRICATED NEW SUPPROT ANGLE, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW SUPPORT ANGLE AND FASTENERS AT STATION 640 BETWEEN +X70 AND -Z35. IAW DC8 SRM 53-2-1, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001312006022400131WP 2006 2 24 IXXA060073S 120041005A5320 RIB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIB CRACKED AT STATION -175 FORWARD BULKHEAD RIGHT LOWER SECTION. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FASTENERS AT STATION -175 FORWARD BULKHEAD RIGHT LOWER SECTION IAW DC8 SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001332006022400133WP 2006 2 24 IXXA060074S 120041005A5312 BULKHEAD DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND WEB CRACKED AT STATION -175 FORWARD BULKHEAD LOWER SECTION. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED WEB. FABRICATED WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND FASTENERS AT STATION -175 FORWARD BULKHEAD LOWER SECTION. IAW DC8 SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001342006022400134WP 2006 2 24 IXXA060079S 120041009A532026641324501N ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND AFT FUSELAGE LONGERON ATTACH FITTING CRACKED AT STATION 1690 LONGERON 28 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW FITTING, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW LONGERON ATTACH FITTING AND FASTENERS AT STATION 1690 LONGERON 28 LEFT IAW DC8 MM 20-16-0, DC8 SRM 53-2-0, 51-3-1, AND 51-1-8. 2L74 4F RT4A25 20060224001382006022400138WP 2006 2 24 IXXA060081S 120041009A5320 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858132773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 810 AT +X18. REMOVED DAMAGE. FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR ANGLE AND FASTENERS AT STATION 810 BETWEEN +X17.5 AND +X31 IAW DC8 SRM 53-2-0, 51-1-20, 51-1-21, 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001442006022400144WP 2006 2 24 IXXA060083S 120041007A5320 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND WEB CRACKED FROM STATION 920 TO 940 AT -X25, Z0. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER AND REPAIR DOUBLER AND FASTENERS FROM STATION 935.250 TO STATION 938.750 BETWEEN -X23.250 AND -X26.750, Z0 IAW DC8 SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001472006022400147WP 2006 2 24 IXXA060031S 120041003A5532 SKIN DOUG DC8 DC871F 302199DWP VERTICAL STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND VERTICAL STABILIZER LEFT SIDE PANEL INTERNAL SKIN CORRODED BETWEEN STATION ZR253 AND STATION ZR299.125. REMOVED EXISTING STRUCTURE FROM DAMAGED PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED STRUCTURE, NEW STIFFENERS, AND FASTENERS WET WITH SEALANT. YAW COPES EGO. COO-8-55-382-04 DATED 10/12/2004. 2L74 4F RT4A25 20060224001492006022400149WP 2006 2 24 IXXA060032S 120041002A5311 FRAME DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION 1978 -X2. FABRICATED NEW FRAME, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS AT STATION 1798 IAW DC8 SRM 53-2-0, 51-1-21, 53-5-1, 51-1-4, 51-1-5, AND 51-1-8. SEE SDR IXXA060030S. 2L74 4F RT4A25 20060224001512006022400151WP 2006 2 24 IXXA060033S 120041002A5522 SKIN DOUG DC8 DC871F 302199DWP RT ELEVATOR DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR UPPER SKIN DENTED OUT OF LIMITS AT STATION XE 111.006. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS WET WITH SEALANT FROM STATION XE 106 TO STATION 117 IAW DC8 SRM 55-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001592006022400159WP 2006 2 24 IXXA060084S 120041020A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE CHECK, FOUND A CRACKED INTERCOSTAL FROM STATION 1140 TO STATION 1160 AT LONGERON 14 RT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED INTERCOSTAL. FABRICATED NEW INTERCOSTAL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW INTERCOSTAL AND FASTENERS FROM STATION 1140 TO STATION 1160 AT LONGERON 14 RT IAW SRM 53-2-0, 51-1-20, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060224000972006022400097WP 2006 2 24 IXXA060059S 120041002A5320 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND A CRACKED WEB AT EXTERNAL FUSELAGE STATION 781.5 +X18. REMOVED HYDRAULIC LINES FOR ACCESS. REMOVED ACCESS PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 781.5 BETWEEN +X6 AND +X44. INSTALLED ACCESS PANEL, AND HYDRAULIC LINES, AND LEAK CHECKED IAW DC8 MM 20-12-0, 20-16-0, 29-00-00 DC8 SRM 53-2-0, 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001392006022400139WP 2006 2 24 IXXA060082S 120041028A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING RIB WEB CRACKED AT STATION XRS6. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER, AND FASTENERS AT RIGHT HAND WING STATION XRS6 IAW DC8 SRM 57-2-0, 51-1-21, 57-5-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001732006022400173WP 2006 2 24 IXXA060086S 120041007A5320 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXISTING DOUBLER CRACKED AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER AND FASTENERS AT STATION 1620 BETWEEN LONGERON 17 LEFT NAD 24 LEFT IAW DC8 SRM 53-2-0, 51-1-21, 51-3-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224002012006022400201WP 2006 2 24 IXXA060092S 120041004A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, FOUND RIGHT WING INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS BETWEEN STATION XW15 AND XW45. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. PERFORMED HOT BOND TO DAMAGED AREA IAW DC8 SRM 57-1-0, 51-1-9, 51-1-5 AND 51-1-8. 2L74 4F RT4A25 20060224002352006022400235WP 2006 2 24 IXXA060035S 120040920A5512 SKIN DOUG DC8 DC871F 302199DWP HORIZ STAB DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER L/E DENTED AT STATION XFS 188.750. REMOVED DAMAGE. FAB`D REPAIR PARTS. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS WET WITH SEALANT FROM STATION XFS 185.5 TO STATION 199.5 IAW DC8 SRM 55-2-1, 55-3-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227000022006022700002WP 2006 2 27 IXXA060090S 120041005A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 397.75. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT STATION XFS 397.75 IAW DC8 SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227000032006022700003WP 2006 2 27 IXXA060091S 120041005A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 404. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT STATION XFS 404 IAW DC8 SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227000242006022700024WP 2006 2 27 IXXA060117S 120040614A5313 LONGERON DOUG DC8 DC873F 302199FWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND CORROSION AROUND DOME NUTS AT STATION 44 LONGERON 27 RIGHT. REMOVED CORROSION, OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE SECTION OF LONGERON. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS IAW DC8 SRM 53-2-2, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060227000262006022700026WP 2006 2 27 IXXA060119S 120040622A5311 FRAME DOUG DC8 DC873F 302199FWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 1580 LONGERON 21 LEFT. REMOVED FASTENER AS NEEDED TO REMOVE DAMAGED FRAME SECTION. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 1580 LONGERON 21 LEFT IAW DC8 SRM 53-2-0, 51-1-20D, 51-1-8 AND 51-1-21. 2L74 4F RT4A25 20060227000282006022700028WP 2006 2 27 IXXA060121S 120040711A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND CAPTAIN'S OUTBOARD SEAT TRACK HAS EXCESSIVE WEAR AROUND LOCKPIN HOLES. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED SEAT TRACK SECTION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT CAPTAIN'S OUTBOARD SEAT TRACK IAW DC8 SRM 53-2-3, 51-1-8, AND 51-1-20D. 2L74 4F RT4A25 20060227000302006022700030WP 2006 2 27 IXXA060123S 120040615A5740 ATTACH ANGLE DOUG DC8 DC873F 302199FWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND RIGHT WING INTERIOR OF PANEL NUMBER 546 FORWARD INBOARD VERTICAL ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSTALLED NEW ANGLE AND NEW FASTENERS RIGHT WING INTERIOR OF PANEL NUMBER 546 FORWARD INBOARD VERTICAL ANGLE IAW DC8 SRM 53-2-0, 51-1-20D, AND 51-1-8. 2L74 4F RT4A25 20060227000522006022700052WP 2006 2 27 IXXA060075S 120041005A5320 SUPPORT CHANNEL DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND FLOOR SUPPORT CHANNEL CRACKED IN THE AFT CARGO COMPARTMENT AT STATION 1263 BETWEEN LONGERON 33 LEFT AND 34 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPORT CHANNEL, FABRICATED NEW FLOOR SUPPORT CHANNEL, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW FLOOR SUPPORT CHANNEL, AND FASTENERS AT STATION 1263 BETWEEN LONGERON 33 LEFT AND 34 LEFT. IAW DC8 SRM 51-2-0, 51-1-21, 51-1-4, 51-1-5 AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060227000962006022700096WP 2006 2 27 IXXA060125S 120040618A57535652287506 VANE DOUG DC8 DC873F 302199FWP RT TE FLAPS DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782553 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING FLAP NUMBER 1 VANE LOWER INBOARD SECTION DELAMINATED. REPLACED RIGHT WING FLAP NUMBER 1 VANE WITH OVERHAULED UNIT. 2L74 4F RT4A25 20060224000922006022400092WP 2006 2 24 IXXA060049S 120041008A5240 BEAM DOUG DC8 DC871F 302199DWP SERVICE DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR BEAM NUMBER 1 CRACKED AT AFT SECTION. REMOVED SERVICE DOOR. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED BEAM. FAB`D NEW BEAM. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW BEAM NUMBER 1 AND FASTENERS IN AFT SERVICE DOOR. INSTALLED AFT SERVICE DOOR, RIGGED, AND LEAK CHECKED IAW DC8 MM 52-10-12, 52-10-16, 52-10-05, 21-30-05, DC8 SRM 52-1-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001032006022400103WP 2006 2 24 IXXA060063S 120041003A5320 SUPPORT DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND A CRACKED LATERAL SUPPORT IN THE AFT CARGO COMPARTMENT AT STATION 1140 LONGERON 27 LEFT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 1138 AND 1142 BETWEEN +X50 AND +X54 IAW DC8 SRM 53-2-0, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001122006022400112WP 2006 2 24 IXXA060051S 120040930A5511 RIB DOUG DC8 DC871F 302199DWP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE INBOARD RIB CRACKED AT STATION XFS 53.500. REMOVED DAMAGE. FAB`D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PART AT STATION XFS 53.500 IN RIGHT HORIZONTAL STABILIZER LEADING EDGE IAW DC8 SRM 55-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001142006022400114WP 2006 2 24 IXXA060050S 120040930A5511 RIB DOUG DC8 DC871F 302199DWP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER LEADING EDGE INBOARD RIB CRACKED AT STATION XFS 116.250. REMOVED DAMAGE. FAB`D REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PART AT STATION XFS 116.250 IN LEFT HORIZONTAL STABILIZER LEADING EDGE IAW DC8 SRM 55-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001182006022400118WP 2006 2 24 IXXA060054S 120041004A5720 SUPPORT FITTING DOUG DC8 DC871F 302199DWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING FLAP CANOE FITTING UPPER SUPPORT CRACKED AT STATION XRS 235. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW SUPPORT, LOCATED, DRILLED, TRIMMED, TEREATED, PRIMED, INSTALLED NEW SUPPORT AND FASTWENERS ON LEFT HAND WING FLAP CANOE AT STATION XRS 235. IAW SRM 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001362006022400136WP 2006 2 24 IXXA060080S 120041009A5320 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 810 AT +X2. REMOVED DAMAGE. FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR ANGLE AND FASTENERS AT STATION 810 BETWEEN +X2 AND +X12. IAW DC8 SRM 53-2-0, 51-1-20, 51-1-21, 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001532006022400153WP 2006 2 24 IXXA060070S 120041003A5320 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 857 AND +X16. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLERS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER, FILLERS AND FASTENERS AT STATION 857 FROM +X11 TO +X19.5. IAW DC8 SRM 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227000042006022700004WP 2006 2 27 IXXA060137S 120040614A5320 PAN DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND AFT CARGO COMPARTMENT STATION 1120 AND 1160 PAN ABOVE NUMBER 3 CARGO DOOR IS CRACKED AT BOTH ENDS. REMOVED FASTENERS AS NEEDED TO REMOVE PAN. REMOVED DAMAGE. FABRICATED DOUBLERS, LOCATED DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLERS AND NEW FASTENERS. INSTALLED PAN ABOVE NUMBER 3 CARGO DOOR IAW DC8 SRM 55-2-0, 51-3-0, 53-11-2, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060227000272006022700027WP 2006 2 27 IXXA060120S 120040622A5320 SUPPORT CHANNEL DOUG DC8 DC873F 302199FWP ZONE 200 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND HAT CHANNEL BROKEN AT STATION 1586 LONGERON 21 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED HAT CHANNEL SECTION. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 1586 LONGERON 21 RIGHT IAW DC 8 SRM 51-3-0, 53-2-0, 51-1-8 AND 51-1-21. 2L74 4F RT4A25 20060227001502006022700150WP 2006 2 27 IXXA060140S 120040609A5320 CUSP WEB DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND A CRACKED CUSP BETWEEN STATION 980 AND 1000 AT LONGERON 21 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AT STATION 980 AND 1000 AT LONGERON 21 RIGHT IAW DC8 SRM 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20060227001522006022700152WP 2006 2 27 IXXA060141S 120040610A5320 FLOOR SUPPORT DOUG DC8 DC873F 302199FWP ZONE 100 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND LEFT FLOOR TRACK FLANGE GOUGED AT STATION 1080. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED NEW FLANGE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW FLANGE AND NEW FASTENERS AT LEFT HAND FLOOR TRACK FLANGE AT STATION 1080 IAW DC8 SRM 53-2-0, 51-4-0, 51-3-0, 51-1-4, AND 51-1-8. 2L74 4F RT4A25 20060227001532006022700153WP 2006 2 27 IXXA060142S 120040610A5320 FLOOR SUPPORT DOUG DC8 DC873F 302199FWP ZONE 100 CORRUPTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORT FLANGE CRACKED AT STATION 1160 LONGERON 31 RIGHT. REMOVED DAMAGE, FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED FILLER AND DOUBLER AND NEW FASTENERS AT AT STATION 1160 LONGERON 31 RIGHT IAW DC8 SRM 54-4-1, 53-4-1, 53-2-0, 51-1-20D, 51-1-20A, AND 51-1-8. 2L74 4F RT4A25 20060227001542006022700154WP 2006 2 27 IXXA060143S 120040610A5320 FLOOR SUPPORT DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL9357825654 46106 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORT FLANGE HAS 5 EACH CRACKS AT STATION 1280 LONGERON 31 RIGHT AND 29 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPORT FLANGE. WELDED CRACKS IAW DC8 DPS 10.225. INSTALLED REPAIRED FLANGE AT AT STATION 1280 LONGERON 31 RIGHT AND 29 LEFT, IAW DC8 SRM 51-1-21, 51-1-8, AND 51-20D. 2L74 4F RT4A25 20060227001562006022700156WP 2006 2 27 IXXA060145S 120040614A5320 STIFFENER DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND HORIZONTAL STIFFENER CRACKED APPROXIMATELY 1 INCH AT STATION 1956 LEFT SIDE. REMOVED FASTENERS AS NEEDED TO REMOVE STIFFENER. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS, REINSTALLED STIFFENER AT STATION 1956 IAW DC8 SRM 53-2-0, 51-1-21, 53-5-3, 51-1-20D, AND 51-1-8. 2L74 4F RT4A25 20060227001572006022700157WP 2006 2 27 IXXA060148S 120040616A5414 ACCESS PANEL DOUG DC8 DC873F 302199FWP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 3 PYLON FOOTSTOOL ACCESS PANEL HAS SEVERAL AREAS WITH DEEP FRETTING WEAR. FABRICATED NEW FOOTSTOOL ACCESS PANEL, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, AND PRIMED NEW FOOTSTOOL ACCESS PANEL IAW DC8 SRM 53-2-0, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060227001592006022700159WP 2006 2 27 IXXA060150S 120040610A5312 PANEL DOUG DC8 DC873F 302199FWP MLG WW CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT PYLON ADAPTER PANEL CRACKED APPROXIMATELY 2 1/2 INCHES AT FORWARD ACCESS PANEL. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS IAW DC8 SRM 54-2-0, 51-1-26, AND 51-1-8. 2L74 4F RT4A25 20060227001882006022700188WP 2006 2 27 IXXA060126S 120040618A5753 VANE DOUG DC8 DC873F 302199FWP ZONE 600 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING FLAP NUMBER 2 FIXED VANE OUTBOARD UPPER EDGE GOUGED. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, ALODINED, INSTALLED AND CURED ALL REPAIR PARTS ON RIGHT WING FLAP NUMBER 2 FIXED VANE, PRIMED AND SEALED IAW DC8 SRM 51-1-9A, 57-7-0,51-1-15, AND 51-1-8. 2L74 4F RT4A25 20060227001892006022700189WP 2006 2 27 IXXA060127S 120040618A5753 SUPPORT ANGLE DOUG DC8 DC873F 302199FWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING RIGHT OUTBOARD FLAP INBOARD TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT RIGHT HAND WING RIGHT HAND OUTBOARD FLAP INBOARD TRAILING EDGE IAW DC8 SRM 57-2-0, 51-1-21 AND 51-1-8. 2L74 4F RT4A25 20060227001902006022700190WP 2006 2 27 IXXA060128S 120040618A5753 FLAP TRACK DOUG DC8 DC873F 302199FWP ZONE 600 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP LEADING EDGE INBOARD HINGE AT FLAP STATION XRS-230.000 ICE DOOR INBOARD TRACK GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED TRACK. FABRICATED NEW TRACK, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW TRACK AND FASTENERS AT RIGHT HAND OUTBOARD FLAP LEADING EDGE INBOARD HINGE AT FLAP STATION XRS-230.000 ICE DOOR INBOARD TRACK IAW DC8 SRM 51-1-21, 51-1-8, 51-1-8B, 51-3-0, 51-1-4 AND 57-2-0. 2L74 4F RT4A25 20060227001912006022700191WP 2006 2 27 IXXA060129S 120040618A5753 FLAP TRACK DOUG DC8 DC873F 302199FWP ZONE 600 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT OUTBOARD FLAP OUTBOARD HINGE ICE DOOR TRACK GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED TRACK. FABRICATED NEW TRACK, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED INSTALLED NEW TRACK AND FASTENERS AT RIGHT HAND OUTBOARD FLAP OUTBOARD HINGE ICE DOOR TRACK. IAW 51-3-0, 51-1-4, 57-2-0, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060227001962006022700196WP 2006 2 27 IXXA060134S 120040508A5753 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 TORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP OUTBOARD TRAILING EDGE WEDGE LOWER SKIN GOUGED AND TORN. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS WET WITH SEALANT AT RIGHT WING OUTBOARD FLAP OUTBOARD TRAILING EDGE WEDGE LOWER SKIN. SEALED AREA. IAW 57-2-5, 51-1-15, 51-3-0 AND 51-1-8. 2L74 4F RT4A25 20060227001972006022700197WP 2006 2 27 IXXA060135S 120040814A575157630901 HINGE FITTING DOUG DC8 DC873F 302199FWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND LEFT WING INBOARD AILERON UPPER INBOARD HINGE FITTING CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED HINGE FITTING. RECEIVED NEW PART, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED NEW FITTING AND NEW FASTENERS. RIGGED AILERON IAW DC8 MM 27-11-1, 20-16-0, 27-11-2, 27-10-0, DC8 SRM 51-1-20D, 51-3-0, AND 51-1-21A 2L74 4F RT4A25 20060227001982006022700198WP 2006 2 27 IXXA060136S 120040809A5755 ANGLE DOUG DC8 DC873F 302199FWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING LOWER SURFACE INBOARD OF NUMBER 1 SPOILER PANEL ATTACH ANGLE CRACKED. REMOVED DAMAGE. FABRICATED REPAIR ANGLES, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR ANGLES AND NEW FASTENERS AT RIGHT WING LOWER SURFACE INBOARD OF NUMBER 1 SPOILER PANEL ATTACH ANGLE IAW 57-2-0, 51-1-20D, 51-9-0, 51-3-2, 51-1-8, AND 57-5-2. 2L74 4F RT4A25 20060227002042006022700204WP 2006 2 27 IXXA060023S 120041006A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND THE LT WING UPPER SURFACE CORRODED AT STATION XFS304. REMOVED LEFT WING CENTER SECTION LEADING EDGE TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLED FILLER, DOUBLER AND FASTENERS WET WITH SEALANT FROM STATION XFS304 TO XFS344. INSTALLED LEFT WING CENTER SECTION LEADING EDGE IAW DC8 SRM 57-2-1, 57-20-2, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001042006022400104WP 2006 2 24 IXXA060064S 120041003A5320 SUPPORT DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND A CRACKED LATERAL SUPPORT IN THE AFT CARGO COMPARTMENT AT STATION 1160 LONGERON 27 LEFT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 1155 AND 1160 BETWEEN +X50 AND +X54. IAW DC8 SRM 53-2-0, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001262006022400126WP 2006 2 24 IXXA060071S 120041003A5320 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 810 AT -X68. REMOVED DAMAGED. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS AT STATION 810 BETWEEN -X50 AND -X70 IAW DC8 SRM 53-2-0, 53-8-1, 51-1-4, 561-1-5 AND 51-1-8. 2L74 4F RT4A25 20060224001282006022400128WP 2006 2 24 IXXA060072S 120041003A5320 WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 857 AT -X16. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS AT STATION 857 FROM -X11 TO -X21 IAW DC8 SRM 53-2-0, 53-8-1, 51-1-4, 561-1-5 AND 51-1-8. 2L74 4F RT4A25 20060224001462006022400146WP 2006 2 24 XXA060086S 120041007A5320 DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, FOUND EXISTING DOUBLER CRACKED AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER AND FASTENERS AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT IAW DC8 SRM 53-2-0, 51-1-21, 51-3-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060224001552006022400155WP 2006 2 24 IXXA060069S 120041003A5320 ANGLE DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 857 AND +X16. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW ANGLE AND FASTENERS AT STATION 857 FROM +X13 TO +X22.5 IAW DC8 SRM 53-8-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227000052006022700005WP 2006 2 27 IXXA060138S 120040714A5330 SKIN DOUG DC8 DC873F 302199FWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND INTERNAL SKIN CORROSION AT STATION 610 BETWEEN LONGERON 33 RIGHT AND 34 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 620 TO 640 BETWEEN LONGERON 35 LEFT TO 33 RIGHT IAW DC8 SRM 51-1-21, 51-1-20D, 53-2-1, 51-1-4, AND 51-1-8. 2L74 4F RT4A25 20060227000092006022700009WP 2006 2 27 IXXA060147S 120040614A5320 WEB DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND WEB CRACKED APPROXIMATELY .5 INCH AT STATION 1910 LONGERON 30 RIGHT. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 1910 LONGERON 30 RIGHT IAW DC8 SRM 53-5-0, 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20060227000292006022700029WP 2006 2 27 IXXA060122S 120040611A5751 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND RIGHT WING OUTBOARD AILERON UPPER SURFACE DENTED. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT WING OUTBOARD AILERON UPPER SURFACE IAW DC8 SRM 53-3-0, 87-2-3, 51-1-9, 51-1-231, 51-3-0, AND 51-1-8. 2L74 4F RT4A25 20060227000432006022700043WP 2006 2 27 IXXA060124S 120040617A5751 WEDGE DOUG DC8 DC873F 302199FWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND RT WING OUTBOARD AILERON OUTBOARD WEDGE TRAILING EDGE GOUGED. PERFORMED HFEC, FOUND WEDGE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT WING OUTBOARD AILERON OUTBOARD WEDGE TRAILING EDGE IAW DC8 SRM 57-2-1. 2L74 4F RT4A25 20060227000532006022700053WP 2006 2 27 IXXA060076S 120041005A5320 WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, FOUND WEB CRACKED IN THE AFT CARGO COMPARTMENT STATION 1267 BETWEEN +X40 AND -Z8. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER AND FASTENERS FROM STATION 1265 TO 1269 BETWEEN +X40 AND -Z8. IAW DC8 SRM 53-2-0, 51-4-5, 51-1-4, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060227001482006022700148WP 2006 2 27 IXXA060139S 120040609A5320 SUPPORT DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT AFT LOWER CARGO TUNNEL; STATION 1000 RIGHT UPPER HORIZONTAL SIDE WALL SUPPORT CRACKED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT RIGHT AFT LOWER CARGO TUNNEL; STATION 1000 RIGHT UPPER HORIZONTAL SIDE WALL SUPPORT IAW DC8 SRM 51-1-4, 53-2-0, 51-1-21, 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20060227001552006022700155WP 2006 2 27 IXXA060144S 120040617A5230 SKIN DOUG DC8 DC873F 302199FWP ZONE 800 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND AFT CARGO DOOR INTERIOR SKIN AT UPPER FORWARD STOP CORRODED. REMOVED FASTENERS AS NEEDED TO REMOVE EXISTING DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT AFT CARGO DOOR INTERIOR SKIN AT UPPER FORWARD STOP IAW DC8 SRM 51-1-21, 52-2-0, 51-3-0, 52-2-3, AND 51-1-8. 2L74 4F RT4A25 20060227001922006022700192WP 2006 2 27 IXXA060130S 120040626A5751 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935783554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD AILERON TP SIDE ABOVE AILERON TRIM LINKAGE SKIN CORRODED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED. TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 57-2-0, 57-8-0, 51-1-4, 51-1-21, AND 51-1-8. 2L74 4F RT4A25 20060227001932006022700193WP 2006 2 27 IXXA060131S 120040626A5753 ANGLE DOUG DC8 DC873F 302199FWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGLE, AND FASTENERS AT RIGHT WING INBOARD FLAP OUTBOARD ANGLE. IAW DC8 SRM 51-1-21, 51-2-0, AND 51-1-8. 2L74 4F RT4A25 20060227001942006022700194WP 2006 2 27 IXXA060132S 120040629A5730 SKIN DOUG DC8 DC873F 302199FWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING DENTED AT STATION XFS-45 OUTBOARD OF LIFT ATTACH POINT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS WET WITH SEALANT AT RIGHT WING STATION XFS-45. SEALED REPAIR IAW 57-2-1, AND 51-1-8. 2L74 4F RT4A25 20060227002702006022700270WP 2006 2 27 IXXA060043S 120041007A5320 WEB DOUG DC8 DC871F 302199DWP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND FLOOR PANEL CORRODED FROM STATION 40 TO STATION 55 BETWEEN +X60 AND -X60.7=0. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED FLOOR PANEL WEB. FAB`D NEW WEB, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FLOOR PANEL WEB FROM STATION 40 TO STATION 55 BETWEEN +X60 AND -X60.7=0 IAW DC8 SRM 51-1-21, 53-7-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227002732006022700273WP 2006 2 27 IXXA060155S 120040608A27525751152503 DRIVE LINK DOUG DC8 DC873F 302199FWP T/E FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FORWARD FLAP DRIVE LINK ASSEMBLY CRACKED AT ACTUATOR ATTACH POINT -J-, AT WING STATION XW-97.906. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLAP LINK ASSEMBLY. RECEIVED NEW FLAP DRIVE LINK ASSEMBLY, AND INSTALLED NEW FLAP DRIVE LINK ASSEMBLY AND FASTENERS IAE DC8 MM27-51-4, AND 27-27-4. 2L74 4F RT4A25 20060227002822006022700282WP 2006 2 27 IXXA060095S 120041004A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XW65. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB. LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FASTENERS AT RIGHT WING TRAILING EDGE STATION XW65. IAW DC8 SRM 57-1-0, 51-1-20, 51-1-21, 51-3-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227002902006022700290WP 2006 2 27 IXXA060152S 120040612A5414 PANEL DOUG DC8 DC873F 302199FWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND NUMBER 1 ENGINE PYLON AFT OUTBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR ATTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED REPAIR DOUBLERS AND NEW FASTENERS IAW DC8 SERVICE BULLETIN 54-93. 2L74 4F RT4A25 20060227002912006022700291WP 2006 2 27 IXXA060153S 120040614A5420 ANGLE DOUG DC8 DC873F 302199FWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON LOWER AFT SECTION HAS CRACKED RIB ANGLE EIGHTH FROM FRONT AT SPLICE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB ANGLE. WELDED RIB ANGLE. INSTALLED RIB ANGLE AND NEW FASTENERS, IAW DC8 SRM 51-1-21, AND DC8 DPS 10.255. 2L74 4F RT4A25 20060227003162006022700316WP 2006 2 27 IXXA060157S 120040611A5720 ANGLE DOUG DC8 DC873F 302199FWP LT WING GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING ROOT XFS-970, XW-0 ANGLE GOUGED AT AFT END, NUMBER 1 FLAP ROLLER TRACK. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED. INSTALLED NEW ANGLE AND NEW FASTENERS IAW DC8 SRM 51-3-0, 51-1-4, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060224002252006022400225WP 2006 2 24 IXXA060034S 120041001A5511 STRINGER DOUG DC8 DC871F 302199DWP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER INNER SPAR BOX UPPER SECTION STRINGER NUMBER 1 CRACKED AT STATION XFS 47.500. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS WITH SEALANT BETWEEN THE FAYING SURFACES, AND FASTENERS IAW COOPESA E.O. COO-8-55-390-04 DATED 10/14/2004. 2L74 4F RT4A25 20060227000082006022700008WP 2006 2 27 IXXA060146S 120040614A5320 WEB DOUG DC8 DC873F 302199FWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND WEB CRACKED APPROXIMATELY .5 INCH AT STATION 1906 LONGERON 30 LEFT. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 1906 LONGERON 30 LEFT IAW DC8 SRM 53-5-0, 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20060227000252006022700025WP 2006 2 27 IXXA060118S 120040622A5311 FRAME DOUG DC8 DC873F 302199FWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 1580 LONGERON 21 RIGHT. REMOVED FASTENER AS NEEDED TO REMOVE DAMAGED FRAME SECTION. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 1580 LONGERON 21 RIGHT IAW DC8 SRM 53-2-0, 51-1-20D, AND 51-1-21. 2L74 4F RT4A25 20060227000542006022700054WP 2006 2 27 IXXA060077S 120041006A5320 WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND WEB CRACKED IN THE AFT CARGO COMPARTMENT, AFT DOOR JAMB FROM STATION 1440 TO STATION 1446 BETWEEN LONGERON 32 RT AND LONGERON 34 RT. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER AND FASTENERS FROM STATION 1440 TO STATION 1446 BETWEEN LONGERON 32 RIGHT AND LONGERON 34 RT IAW SRM 53-2-0, 51-4-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060227001582006022700158WP 2006 2 27 IXXA060149S 120040906A5312 PANEL DOUG DC8 DC873F 302199FWP MLG WW DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND LEFT AFT WHEEL WELL PANEL 161X DENTED ON OUTER SKIN. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, TREATED, APPLIED ADHESIVE, CURED, AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-9A, 53-8-3, 51-1-15, AND 51-1-8. 2L74 4F RT4A25 20060227001952006022700195WP 2006 2 27 IXXA060133S 120040714A5753 ANGLE DOUG DC8 DC873F 302199FWP ZONE 600 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK, FOUND RIGHT WING JOINT AREA BETWEEN INBOARD AND OUTBOARD FLAPS, AREA ON UPPER OUTBOARD FLAP ANGLE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PART. LOCATED, DRILLED TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING JOINT AREA BETWEEN INBOARD AND OUTBOARD FLAPS, AREA ON UPPER OUTBOARD FLAP ANGLE IAW DC8 SRM 57-2-0, 51-9-0, AND 51-1-20D. 2L74 4F RT4A25 20060227002152006022700215WP 2006 2 27 IXXA060024S 120041005A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANT FROM STATION XW39 TO STATION XW45 IAW DC8 SRM 57-2-5, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227002802006022700280WP 2006 2 27 IXXA060094S 120041004A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP TRAILING EDGE HAS SEVERAL DENTS BETWEEN STATIONS XW64 AND XW101. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS. IAW DC8 SRM 57-1-0, 51-1-21, 51-1-9, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060227003182006022700318WP 2006 2 27 IXXA060166S 120040707A5311561194334 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND CORRODED FRAME AT STATION 70 BETWEEN LONGERON 31 RIGHT AND 32 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE ATTACHING FRAME STRUCTURE. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FRAME. RECEIVED NEW FRAME, FABRICATED FRAME SPLICE REPAIR PARTS. LOCATED NEW FRAME AND FRAME SPLICE REPAIR PARTS LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED NEW FRAME AND FRAME SPLICE REPAIR PARTS, AND NEW FASTENERS. RE-ATTACHED FRAME STRUCTURE IAW DC8 SRM 53-2-5, 51-1-21, 51-3-0, 51-1-20D, 53-2-0, AND 51-1-8. 2L74 4F RT4A25 20051028001012005102800101NM 2005 10 28 USAA200510004 120041024A5330 SKIN BOEING737 7374B7 1384702NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19782AU 25021 A 1.5 INCH CRACK AT STA 727 BELOW ST 23 RT. REPAIRED IAW T/R 53-60-03. 2L72 4F RTA16WE 20051031001322005103100132CE 2005 10 31 UAT2005F00009 120041129A2421DOFF10300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL039736M 179 20700722 ALTERNATOR FAILED AT 170.6 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051031001352005103100135CE 2005 10 31 UAT2005F00006 120041129A242110300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL039475M 393 20700695 ALTERNATOR FAILED AT 393.0 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051031001362005103100136CE 2005 10 31 UAT2005F00007 120041129A242110300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL039475M 107 20700695 ALTERNATOR FAILED AT 107.7 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051031001332005103100133CE 2005 10 31 UAT2005F00005 120041129A242110300B ALTERNATOR CESSNA207 T207A 2073614CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL0373789 225 20700629 ALTERNATOR FAILED AT 225.2 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051109000192005110900019CE 2005 11 9 UAT2005F00000 120041129A2434DOFF10300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL037605U 10 20700443 ALTERNATOR FAILED AT 10.6 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051109001112005110900111EU 2005 11 9 KBM2005F00319 120041228A6720704A34130184 CONTROL CABLE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE T/ROTOR CONTROL BINDING E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 3403 T/R CONTROL CABLE BINDING IN FLIGHT. REPLACED WITH SERVICEABLE CABLE. (K) 1G71 3U3 U H9EU E19EU 20051109000202005110900020CE 2005 11 9 UAT2005F00001 120041129A2434DOFF10300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL037605U 20700443 ALTERNATOR FAILED AT 55.1 TSO. REPLACE WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051109000212005110900021CE 2005 11 9 UAT2005F00003 120041129A2434DOFF10300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL0373503 92 20700599 ALTERNATOR FAILED AT 92.5 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051109000222005110900022CE 2005 11 9 UAT2005F00004 120041129A2434DOFF10300B ALTERNATOR CESSNA207 T207A 2073614CE CONT O520 IO520F 17032SO ENGINE FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL0373789 57 20700629 ALTERNATOR FAILED AT 57.4 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20051110000622005111000062EU 2005 11 10 071794 120040910A61208205271 ARM HAMSTD AEROSPATR42 ATR42* 8680900EU HAMSTD14SF 14SF* NE ACTUATOR CORRODED B EY2RK NONE O OTHER ININSP/MAINT 1 GL03 880806 CORROSION ON ARM OF ACTUATOR. 2H72 4T RTA53EU 6 CP7NE 20051121000062005112100006WP 2005 11 21 IXXA0500108S 120041208A5730 SKIN DOUG DC8 DC873F 302199FWP WS 7095 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A C CHECK INSPECTION, FOUND RT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AROUND STA XILD 7095. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS IAW DC8 SRM 51-1-21 PG 1,DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW SEMAN DWG EO 3792 DC8 NDT SPM PART 06-10-01 001. FAB`D EXTERNAL DOULBLER, FILLERS AND INTERNAL DOUBLER AS REQUIRED IAW SEMAN DWG EO 3792. CLEANED, TREATED AND PRIMED AREA AND INTERNAL DOUBLER, FILLER AND EXTERNAL DOUBLER AND INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED INTERNAL DOUBLER, FILLER, EXTERNAL DOUBLER WITH NEW FASTENERS IAW SEMON DWG EO 3792 IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9 AND 51-3-0 PG 1. 2L74 4F RT4A25 20051121000092005112100009WP 2005 11 21 IXXA0500111S 120041208A5522 SKIN DOUG DC8 DC873F 302199FWP WS74.469-123.187CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT ELEVATOR LOWER PLATING INBOARD SECTION CORROSION DAMAGE BETWEEN STA XE 74.469 AND XE 123.187. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. CORROSION WAS REMOVED IAW DC8 SRM 55-2-1 FIG B PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PG 12. REMOVED THE DAMAGED SECTION IAW DC8 SRM 55-2-1 FIG 8. FABRICATED FILLER & REPAIR SPLICE IAW DC8 SRM 55-2-1 FIG 8 DC8 55-4-1 FIG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B BONDED FILLER + REPAIR SPLICE WITH HYSOL IAW DC8 SRM 51-1-9A. INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20051121000122005112100012WP 2005 11 21 IXXA0500112S 120041209A5753 VANE DOUG DC8 DC873F 302199FWP WS 6.224 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD PLATING A STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL FASTENERS IAW DC8 SRM 51-1-21 PGG1, DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW DWG SEMON EO 3780 PERFORMED NDT INSPECTION IAW NOTE NR 3 DWG SEMON EO 3780, NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER IAW DWG SEMAN EO 3780. CLEANED, TREATED AND PRIMED AREA, REPAIRED PARTS. INTERNAL PORT IAW DC8 SRM 51-1-8B APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS IAW DWG SEMON EO 3780 SR, 51-1-21 PG1 SRM 51-1-20D PG9 DC8 SRM 51-3-0. 2L74 4F RT4A25 20051121000132005112100013WP 2005 11 21 IXXA0500109S 120041208A5754 REPAIR DOUG DC8 DC873F 302199FWP WS 6.224 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A C CHECK INSPECTION, FOUND LT WING EXTENDED L/E OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR IAW DWG SEMON EO 3784, DC8 SRM 51-1-21 PG 1, DC7 SNR 51-1-20D PG 21, AND 51-3-0 PG1. REMOVED DAMAGED AREA IAW DEG SEMON EO 3784. PERFORMED NDT INSPECTION IAW DWG SEMON EO 3784 NOTE 3 DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, INTERNAL DOUBLER AS REQUIRED. FILLER IAW DWG SEMON EO 3784. CLEANED, TREATED AND PRIMED AREA REPAIRED PARTS INTERNAL PARTS IAW DC8 SRM 51-1-8D. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS WITH NEW FASTNERS IAW DC8 SRM 51-3-0 PG 1. 2L74 4F RT4A25 20051121000212005112100021WP 2005 11 21 IXXA0500114S 120041210A5730 PLATE DOUG DC8 DC873F 302199FWP WS 726.000 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD AILERON UPPER OUTBOARD PLATING DENT DAMAGE AT STA XA 726.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN IAW DC8 SRM 51-1-21 PG1. FABRICATED NEW SKIN + FINGER DOUBLER IAW DC8 SRM 57-8-1 PG 9 FIG 4. BONDED SKIN AND FINGER DOUBLER IAW DC8 SRM 51-1-9 PGS 1/3. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED SKIN AND FINGER DOUBLERS IAW DC8 SRM 51-1-21 PG 1. INSTALLED NEW SKIN AND FINGER DOUBLER IAW DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20051121000222005112100022WP 2005 11 21 IXXA0500115S 120041209A5522 PLATE DOUG DC8 DC873F 302199FWP RT ELEVATOR DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, RT ELEVATOR UPPER PLATING INBOARD SECTION SEVERAL DAMAGES BETWEEN STA XAR O AND XE 132.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED UPPER PLATING IAW DC8 SRM 51-1-11 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 5-1-8B. INSTALLED NEW PLATING DC8 SRM 51-1-21 PG 1, DC8 SRM 5-1-21A PGS 1-4. 2L74 4F RT4A25 20051121000072005112100007WP 2005 11 21 IXXA0500110S 120041110A5730 SKIN PANEL DOUG DC8 DC873F 302199FWP WS 63.50-107.50 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP CORROSION DAMAGE BETWEEN STA XFS 63.500 AND XFS 107.500. MAJOR REPAIR ACCOMPLISHED BLEND OUT ON CORRODED AREA REMAINING OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 37 PGS 135 AND 136. FAB`D EXTERNAL DOUBLER IAW DC8 SRM 57-2-1 FIG 37 PGS 135 AND 136. CLEANED, TREATED, AND PRIMED AREA AND EXTERNAL DOUBLER INTERIOR IAW DC8 SRM 51-1-8 B. PRIMED AREA AND EXTERNAL DOUBLER INTERIOR IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON INDICATED AREA IAW DC8 SRM 51-1-12, INSTALLED EXTERNAL DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9. 2L74 4F RT4A25 20051121000202005112100020WP 2005 11 21 IXXA0500113S 120041209A5730 PLATE DOUG DC8 DC873F 302199FWP WS 716.000 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A C CHECK INSPECTION, RT OUTER WING OUTBOARD EXTENDED LEADING EDGE OUTER PLAING UPPER SIDE CORROSION DAMAGE AROUND STA XFS 716.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION FROM RT WING OUTBD L/E UPPER SKIN AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED DAMAGE SECTION IAW DC8 SRM 57-2-1 FIG 38. FABRICATED FILLER + DOUBLER IAW DC8 SRM 57-2-1 FG 38. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER + DOUBLER IAW DC8 SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-15 PG 1. INSTALLED FILLER + DOUBLER IAW DC8 SRM 57-2-1FG 38,TR NR 57-85, DC8 SRM 51-1-20D PG 7 DC8 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20051202000772005120200077CE 2005 12 2 FAAJIKA81204 120040812A521052113306 BELLCRANK CESSNA402 402B 207590PCE PAX DOOR WORN G JIKAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 NM095550K14958 402B1226 AT 13000 FT PIC GOT DOOR OPEN IND LITE, WHEN HE WHEN TO CLOSE DOOR CAME OPEN IN FLIGHT. INVESTIGATION REVEAL BELLCRANK ASSY WORN. MM DOES NOT REQUIRE PULL TEST OF THE BREAK OVER PRESS OF THE HANDLE. LATER MODEL HAS DIFFERENT CONFIG HANDLE ASSY. 1L72 3O A7CE 20051208001572005120800157SO 2005 12 8 RAIA00512004 120041203A3610 FILTER EMB 145 EMB145LR 3260212SO DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03838HK 145321 FLT 7970 - ORD - ON CLIMB-OUT, BLEED NR 1 OVER-TEMP INDICATION APPEARED ON THE EICAS. MAINTENANCE CLEANED THE FAN AIR VALVE FILTER AND PERFORMED A SYSTEM TEST. 2L72 4T RTT00011AT 20060105002572006010500257SO 2006 1 5 623456 120041130A27421159SCC5005 ACTUATOR GULSTMGV GULFSTREAMGV3980116SO RROYCEBR700 BR700710A110 NE HORIZ STAB FAILED E N93AK NONE FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO13506QS3812 623 AFTER LANDING, SELECTED FLAPS TO UP BUT DID NOT MOVE. FLAP / STAB FAIL MESSAGE, FLAP / STAB IND INOP MESSAGE. 2L72 4F4 FRTA12EA E00057EN 20060117000682006011700068WP 2006 1 17 IXXA0500207S 120041011A5300 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENT REMOVED EXISTING DOUBLER AT STATION 74 LONGERON 35 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS AT STATION 70 TO 78.5, LONGERONS 34 LEFT TO LONGERON 35 RIGHT IAW COPESA EO COO-8-53-404-04. 2L74 4F RT4A25 20060117000702006011700070WP 2006 1 17 IXXA0500209S 120041018A5300 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 TEMPORARY A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING EXTERNAL DOUBLER AT STATION 1702 LONGERON 26 LEFT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER AT STATION 1690 TO 1713 LONGERON 24 LEFT TO LONGERON 30 LEFT IAW COOPWSA EO COO-8-53-409-04. 2L74 4F RT4A25 20060117000722006011700072WP 2006 1 17 IXXA0500211S 120041009A534047731561N ATTACH FITTING DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON ATTACH FITTING CRACKED AT STATION 1690 LONGERON 23 RIGHT. REMOVED DAMAGED FITTING, FABRICATED NEW FITTING. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW LONGERON ATTACH FITTING IAW DC8 MM 20-16-0, DC8 SRM 51-3-1, 51-1-8, MDC 93K-393 NDT SPM, DPS 4-999, AND DPS 7-05-3. 2L74 4F RT4A25 20060117000762006011700076WP 2006 1 17 IXXA0500216S 120041004A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON 28 RIGHT CORRODED AT STATION 330 TO 370. REMOVED DAMAGED LONGERON SECTION. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW COOPESA EO COO-8-53-377-04. 2L74 4F RT4A25 20060117000832006011700083WP 2006 1 17 IXXA0500230S 120041005A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND A CRACKED LONGERON AT STATION 1747 LONGERON 15 RIGHT. CLEANED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 52-1-5, AND 51-1-8. 2L74 4F RT4A25 20060117000852006011700085WP 2006 1 17 IXXA0500232S 120041005A5313 LONGERON DOUG DC8 DC871F 302199DWP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 100 LONGERON 9 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, 51-1-5 AND 51-1-8. 2L74 4F RT4A25 20060117000872006011700087WP 2006 1 17 IXXA0500234S 120041003A5210 BEAM DOUG DC8 DC871F 302199DWP ZONE 800 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND FORWARD ENTRY DOOR NR 1 BEAM CRACKED. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 52-2-0, 52-3-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060117000892006011700089WP 2006 1 17 IXXA0500236S 120040927A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK UPON FLIGHT READINESS FOUND SKIN DAMAGED ADJACENT TO GROUND POWER DOOR AREA, UPPER LEFT CORNER, STOP DRILLED. REPAIRED EXTERNAL FUSELAGE SKIN BY REMOVING DAMAGED SKIN, FABRICATED NEW SKIN SECTION AND DOUBLERS, LOCATED REPAIR PARTS, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS AT STATION -22 TO STATION -48 BETWEEN LONGERONS 30 RIGHT AND 33 RIGHT IAW COOPESA EO COO-8-53-378-04. 2L74 4F RT4A25 20060117000932006011700093WP 2006 1 17 IXXA0500240S 120041022A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CORRODED FROM STATION 660 TO STATION 662 AT LONGERON 33 LEFT. REMOVED DAMAGED SKIN. FABRICATED FILLER, DOUBLER, AND TRIPLER. LOCATED DRILLED TRIMMED TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW COOPESA EO COO-8-53-410-04. 2L74 4F RT4A25 20060117000972006011700097WP 2006 1 17 IXXA0500241S 120041020A5311 FRAME DOUG DC8 DC871F 302199DWP ZONE100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 420 LONGERON 35 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 420 BETWEEN LONGERONS 33 LEFT AND 35 LEFT IAW DC8 SRM 51-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060117001062006011700106WP 2006 1 17 IXXA0500224S 120041003A5320 STRAP DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND CORROSION ON WING FILLET STRAPS AT STATION 980 TO 1160. REMOVED DAMAGED STRAPS. FABRICATED NEW STRAPS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW STRAPS AND FASTENERS IAW DC8 SRM 53-2-0, 51-1-8, 51-1-4, AND 51-1-5. 2L74 4F RT4A25 20060117001082006011700108WP 2006 1 17 IXXA0500226S 120041001A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND CORROSION AND EXISTING BLEND OUTS AT STATION 980 TO 1040 BETWEEN 35 LEFT AND 35 RIGHT. REMOVED CORROSION, MANUFACTURED REPAIR PARTS, LOCATED DRILLED, PRIMES AND INSTALLED REPAIR PARTS AND FASTENERS IAW COOPESA EO COO-8-53-401-04. 2L74 4F RT4A25 20060201001962006020100196WP 2006 2 1 IXXA060045S 120041007A534045976431 ATTACH FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND MAIN CARGO CABIN SUPPORT END FITTING CORRODED AT STATION Y55 -X65 Z0. REMOVED FASTENERS AS NEEDED TO REMOVE END FITTING. MANUFACTURED NEW END FITTING, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW END FITTING AND FASTENERS AT STATION Y55 -X65 Z0. IAW SRM 51-3-0, 51-1-20, 51-3-1, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060130001262006013000126NM 2006 1 30 SWAA042621 120040909A53116546520 FRAME BOEING737 737301 1384611NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 8L & STRINGER 8R CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001272006013000127NM 2006 1 30 SWAA042623 120040909A53116546550 FRAME BOEING737 737301 1384611NM BS 807 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 807, STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001312006013000131NM 2006 1 30 SWAA043217 120041104A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 480 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 480, BL 0 TO RBL 3, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001332006013000133NM 2006 1 30 SWAA043254 120041108A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN LBL 18 TO RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001402006013000140NM 2006 1 30 SWAA042624 120040909A53116546540 FRAME BOEING737 737301 1384611NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, STRINGER 8L & STRINGER 8R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001422006013000142NM 2006 1 30 SWAA042666 120040914A53116546550 FRAME BOEING737 737301 1384611NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 8R CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001302006013000130NM 2006 1 30 SWAA043186 120041102A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500C CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 500C, BETWEEN STR 26L TO STR 28L, CORRODED. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001432006013000143NM 2006 1 30 SWAA042805 120040927A53156546811 FLOORBEAM BOEING737 737301 1384611NM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS BS 1016, LBL 9 TO LBL 17, CORRODED. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20060130001982006013000198NM 2006 1 30 SWAA041934 120040708A53116546550 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907 STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001992006013000199NM 2006 1 30 SWAA041968 120040712A53156545833 FLOORBEAM BOEING737 7373H4 1384600NM 188 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29390SW 26593 DURING SCHEDULED D CHECK, FOUND FLOORBEAMS AT BS 188 TO BS 198, STRINGER 17R TO STRINGER 17L CRACKED. REMOVED AND REPLACED FLOORBEAM SECTION PER BAC DRAWING AND SRM. 2L72 4F RTA16WE 20060130002012006013000201NM 2006 1 30 SWAA042060 120040720A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8R TO STRINGER 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002032006013000203NM 2006 1 30 SWAA042082 120040722A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 21 TO RBL 1. REPAIRED FLOOR BEAM PER SRM. 2L72 4F RTA16WE 20060130002062006013000206NM 2006 1 30 SWAA042136 120040727A532269353656 SHEAR TIE BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14R CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130002072006013000207NM 2006 1 30 SWAA042155 120040728A53116546550 FRAME BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 907, STRINGER 9L AND STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002082006013000208NM 2006 1 30 SWAA042168 120040729A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 460 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 460, STRINGER 16R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002092006013000209NM 2006 1 30 SWAA042191 120040801A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM BS 772 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 772, BETWEEN RBL 8 TO LBL 8 CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20060130002112006013000211NM 2006 1 30 SWAA041830 120040629A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D CHECK, FOUND FRAME BS 787, BETWEEN STRINGER 8R AND STRINGER 8L, CRACKED. REMOVED AND REPLACED SECTION PER SRM. 2L72 4F RTA16WE 20060130002212006013000221NM 2006 1 30 SWAA042270 120040808A53116546569 SHEAR TIE BOEING737 7373Y0 1384671NM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 947, STR 26L CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130002222006013000222NM 2006 1 30 SWAA042272 120040808A53116546550 FRAME BOEING737 7373Y0 1384671NM BS 847 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 847 TO BS 867, STR 8L CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002232006013000223 2006 1 30 SWAA042275 420040808A25656557463 FITTING BOEING737 7373Y0 1384671NM GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D CHECK, FOUND FWD ENTRY EVAC SLIDE GIRT BAR FITTING AT BS 312, LBL 53 CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2L72 4F RTA16WE 20060130002242006013000224NM 2006 1 30 SWAA042293 120040810A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED STR CLIP PER SRM. 2L72 4F RTA16WE 20060130002252006013000225NM 2006 1 30 SWAA042337 120040814A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 727B CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29351SW 24572 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 727B, STRINGER 22L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002262006013000226NM 2006 1 30 SWAA042346 120040815A534065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727C, STR 4R TO STR 7R CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20060130002552006013000255NM 2006 1 30 SWAA042349 120040815A531165C25220 FRAME BOEING737 7373A4 1384585NM BS 727C CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727C TO BS 727D, STR 9L CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002572006013000257NM 2006 1 30 SWAA042416 120040821A53116546520 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 400 , STRINGER 8L AND STRINGER 8R, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002582006013000258NM 2006 1 30 SWAA042460 120040825A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 400 TO BS 420, STRINGER 16L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20060130002592006013000259NM 2006 1 30 SWAA042469 120040825A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29394SW 27380 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 787, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130002602006013000260NM 2006 1 30 SWAA042521 120040829A53116546529 SHEAR TIE BOEING737 7373A4 1384585NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500 RBL 1, WL 148, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001322006013000132NM 2006 1 30 SWAA043243 120041106A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM BS 500A CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, FROM LBL 4 TO LBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20060130001412006013000141NM 2006 1 30 SWAA042626 120040909A5315BAC1509100146 FLOORBEAM BOEING737 7373H4 1384600NM BS 727E CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29358SW 26595 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727E, BETWEEN LBL 3 TO RBL 8 CORRODED. REPAIRED FLOORBEAM PER EA. 2L72 4F RTA16WE 20060130002002006013000200NM 2006 1 30 SWAA042003 120040715A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 706 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 706, STRINGER 13R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002272006013000227NM 2006 1 30 SWAA042347 120040815A53116546540 FRAME BOEING737 7373A4 1384585NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND FRAME AT BS 747 TO BS 767, STR 9R TO STR 13R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001282006013000128NM 2006 1 30 SWAA043141 120041028A5311BAC1490 FRAME BOEING737 7373H4 1384600NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29601WN 27695 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20060130001292006013000129NM 2006 1 30 SWAA043183 120041102A53116546550 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 DURING SCHEDULED D-CHECK, FOUND FRAME AT BS BS 787, STR 8R & STR 8L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001342006013000134NM 2006 1 30 SWAA043255 120041108A53116546526 FRAME BOEING737 7373H4 1384600NM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001352006013000135NM 2006 1 30 SWAA043299 120041110A5311654659 FRAME BOEING737 7373H4 1384600NM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 8R AND STRINGER 8L. REMOVED AND REPLACED FRAME SECTION PER SRM. 2L72 4F RTA16WE 20060130001362006013000136NM 2006 1 30 SWAA043552 120041206A53106546550 STRUCTURE BOEING737 7373H4 1384600NM BS 787-867 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND STRUCTURE CRACKED BETWEEN BS 787 AND BS 867, STRINGER 8L. REMOVED AND REPLACED STRUCTURE SECTION PER SRM. 2L72 4F RTA16WE 20060130001372006013000137NM 2006 1 30 SWAA043553 120041206A53106546525 STRUCTURE BOEING737 7373H4 1384600NM BS 380-440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED BETWEEN BS 380 AND BS 440, STRINGER 8L. REMOVED AND REPLACED STRUCTURE SECTION PER SRM. 2L72 4F RTA16WE 20060130002022006013000202NM 2006 1 30 SWAA042064 120040720A53106546520 STRUCTURE BOEING737 7373H4 1384600NM BS 400-440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29392SW 27379 DURING SCHEDULED D CHECK, FOUND STRUCTURE AT BS 400 TO BS 440, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRUCTURE SECTION PER SRM. 2L72 4F RTA16WE 20060130002052006013000205NM 2006 1 30 SWAA042135 120040727A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29339SW 24090 DURING SPV, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060130002102006013000210NM 2006 1 30 SWAA042200 120040802A53156920158 FLOORBEAM BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29391SW 27378 DURING SCHEDULED D CHECK, FOUND FLOORBEAM WEB AT BS 178 TO BS 182, LBL 24 TO LBL 37, CRACKED. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER SRM. 2L72 4F RTA16WE 20060130002202006013000220NM 2006 1 30 SWAA042269 120040808A534065C27314 STRINGER CLIP BOEING737 7373Y0 1384671NM BS 177 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29308SA 23498 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 177, STR 10R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002042006013000204NM 2006 1 30 SWAA042093 120040723A531365C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663, STRINGER 10L CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060130002122006013000212NM 2006 1 30 SWAA041833 120040629A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT BS 663, STRINGER 10R AND STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20060130002192006013000219NM 2006 1 30 SWAA041915 120040707A53206551698 SPLICE BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29341SW 24091 DURING SPV, FOUND STRINGER SPLICE AT BS 360, BETWEEN STRINGER 4L AND 4R CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2L72 4F RTA16WE 20060130002562006013000256NM 2006 1 30 SWAA042385 120040818A534065C27314 STRINGER CLIP BOEING737 7373A4 1384585NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 7R CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2L72 4F RTA16WE 20060201000812006020100081WP 2006 2 1 IXXA060099S 120041002A5712 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS722.500. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS722.500. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201000822006020100082WP 2006 2 1 IXXA060110S 120040730A5311 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND CORRODED FRAME AT STATION 220 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS .100 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT STATION 220 LONGERON 36. IAW SRM 51-1-8, AND 53-2-0. 2L74 4F4 FRT4A25 E2GL 20060201000852006020100085WP 2006 2 1 IXXA060102S 120041002A5712 WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND RT WING LEADING EDGE UPPER WEB CRACKED AT STATION XFS610. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED WEB. FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS610. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201000862006020100086WP 2006 2 1 IXXA060103S 120040609A5320 CUSP WEB DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND FORWARD CARGO COMPARTMENT BETWEEN STATION 80 AND STATION 100 LONGERON 21 RT 10 INCHES FROM OB CUSP WEB CRACKED. REMOVED DAMAGE. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, DEBURED, PRIMED, INSTALLED REPAIR DOUBLER AND NEW FASTENERES AT FORWARD CARGO COMPARTMENT BETWEEN STATION 80 AND STATION 100 LONGERON 21 RT 10 INCHES FROM OB CUSP WEB. IAW SRM 53-4-1, 53-2-0, 51-3-0, 51-1-8, 51-1-21, AND 51-1-20. 2L74 4F4 FRT4A25 E2GL 20060201000872006020100087WP 2006 2 1 IXXA060106S 120040611A5311 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED OUT OF LIMITS AT STATION 280 BETWEEN LONGERON 32 RT AND LONGERON 34 RT. REMOVED FASTENERS AS NEEDED TO REPLACE FRAME SEGMENTS. FABRICATED NEW FRAME SEGMENTS, AND REPAIR ANGLES. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT STATION 280 BETWEEN LONGERON 32 RT AND 34 RT. IAW SRM 53-2-0, 51-1-8, 51-1-20D, 53-4-1, 51-1-21, AND 51-3-1. 2L74 4F4 FRT4A25 E2GL 20060201000882006020100088WP 2006 2 1 IXXA060107S 120040611A5320 SPLICE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782553 46106 DURING ROUTINE C CHECK FOUND LONGERON 31 RIGHT OUTBOARD SIDE CENTER SPLICE CRACKED FROM STATION 460 TO STATION 476. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED SPLICE. FABRICATED NEW SPLICE, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW SPLICE AND NEW FASTENERS AT LONGERON 31 RIGHT BETWEEN STATION 460 TO STATION 476. IAW DC8 SRM 51-1-8, 53-2-0, 51-1-20D, AND 51-1-21. 2L74 4F4 FRT4A25 E2GL 20060201001052006020100105WP 2006 2 1 IXXA060028S 120041009A5532 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 300 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED OUT OF LIMITS AT STATION ZFS149. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER, AND FASTENERS WET WITH SEALANT FROM STATION ZFS 133.5 TO STATION ZFS149. IAW SRM 55-2-1, 55/5/1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001162006020100116WP 2006 2 1 IXXA060108S 120040611A5313 LONGERON DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782553 46106 DURING ROUTINE C-CHECK FOUND STATION 120 TO 140 LONGERON 35 LT CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVED DAMAGED LONGERON SECTION. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS WET WITH SEALANT AT LONGERON 35 LT FROM STATION 120 TO STATION 140. IAW SRM 53-2-0, 53-2-2, 53-4-1, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001202006020100120WP 2006 2 1 IXXA060113S 120040610A5320 SILL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 200 MISDRILLED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND RT SERVICE DOOR SILL (FRAME, WEB AND ANGLE) AT STATION 196 LONGERON 11 RT HAS A FASTENER HOLE DOUBLE DRILLED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS FROM STATION 176 TO STATION 205 BETWEEN LONGERON 8 RT AND LONGERON 12 RT IAW SRM 53-2-0, 51-1-4, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001482006020100148WP 2006 2 1 IXXA060029S 120041006A5311 FRAME DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT FRAME CRACKED AT STATION 1978. REMOVED EXISTING FASTENERS, AND FRAME. FABRICATED FRAME, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS WET WITH SEALANT. IAW SRM 53-2-051-1-21, 53-5-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001492006020100149WP 2006 2 1 IXXA060030S 120041005A5311 FRAME DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND RT FRAME CRACKED AT STATION 1978. REMOVED EXISTING FASTENERS, AND FRAME. FABRICATED FRAME, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS WET WITH SEALANT. IAW DC8 SRM 53-2-051-1-21, 53-5-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001092006020100109WP 2006 2 1 IXXA060115S 120040616A5320 WEB DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BS 1164 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND A CRACKED WEB AT LIGHTNING HOLE AT STATION 1164 LBL 68 LONGERON 21 LT. REMOVED DAMAGED. FABRICATED DOUBLER, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED DOUBLER AND NEW FASTENERS AT STATION 1164 LBL 68. IAW SRM 51-1-21, 53-4-1, AND 51-1-3. 2L74 4F4 FRT4A25 E2GL 20060201001172006020100117WP 2006 2 1 IXXA060109S 120040730A5311 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND CORRODED FRAME AT STATION 180 LONGERON 36. REMOVED CORROSION, ORIGINAL THICKNESS .100 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS. IAW SRM 51-1-8, AND 53-2-0. 2L74 4F4 FRT4A25 E2GL 20060201001802006020100180WP 2006 2 1 IAAX060114S 120040611A5320 SILL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND AFT ENTRANCE DOOR SILL HAS TOOLING DAMAGE AT STATION 1620 LONGERON 20 LT. REMOVED DAMAGE. FABRICATED REPAIR PART. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT STA 1620 LONGERON 20 LT IAW SRM 53-2-0, 51-1-21, 51-1-4, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001892006020100189WP 2006 2 1 IXXA060088S 120041007A5753 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 600 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND RT WING IB FLAP OB VANE UPPER SKIN DELAMINATED. REMOVED FLAP VANE. REMOVED DELAMINATED SKIN, PERFORMED HOT BOND TO DAMAGED AREA. INSTALLED VANE. IAW MM 27-51-14, SRM 51-1-9A. 2L74 4F4 FRT4A25 E2GL 20060201001912006020100191WP 2006 2 1 IXXA060040S 120041016A5330 REPAIR DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE BS 1360 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REPLACED EXISTING FUSELAGE SKIN REPAIR DUE TO DTA REQUIREMENTS AT STATION 1360 LONGERON 16 LT SIDE. REMOVED NECESSARY FASTENERS AND EXISTING REPAIR. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER, FILLER, AND FASTENERS WET WITH SEALANT FROM STATION 1358 TO STATION 1378 BETWEEN LONGERON 14 LT AND LONGERON 16 LT. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001922006020100192WP 2006 2 1 IXXA060041S 120041016A5330 REPAIR DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE BS 1735-1750 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REPLACED EXISTING FUSELAGE SKIN REPAIR FROM STATION 1735 TO STATION 1750 BETWEEN LONGERON 14 RT AND 17 RT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS AS NEEDED, AND EXISTING REPAIR. FABRICATED DOUBLER AND FILLERS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLERS, DOUBLER, AND FASTENERS WET WITH SEALANT FROM STATION 1735 TO STATION 1750 BETWEEN LONGERON 14 RT AND LONGERON 17 RT IAW SRM 53-2-1, 53-5-1, 51-1-5 AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201000802006020100080WP 2006 2 1 IXXA060098S 120041002A5712 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS672. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LOWER LEADING EDGE STATION XFS672. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201000842006020100084WP 2006 2 1 IXXA060101S 120041003A5300 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND FORWARD ENTRY DOOR CUT OUT, AFT RIB CRACKED BETWEEN LONGERON 19 LT AND 20 LT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED,TREATED, PRIMED, INSTALLED NEW RIB AND NEW FASTENERS. IAW SRM 53-2-0, 51-1-20, 51-1-21, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001472006020100147WP 2006 2 1 IXXA060025S 120041005A5753 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39 AFT AREA. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANT FROM STATION XW34 TO STATION XW44. IAW SRM 57-2-5, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001942006020100194WP 2006 2 1 IXXA060042S 120041007A534037796571 FITTING DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 200 CRACKED A IXXAO OTHER O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND LONGERON 1 FITTING CRACKED AT STATION 650. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. MANUFACTURED NEW FITTING, LOCATED DRILLED TREATED, PRIMED, INSTALLED FITTING AND FASTENERS WET WITH SEALANT AT LONGERON 1 STATION 650 IAW SRM 51-1-20, 51-1-21, 53-2-0 AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201000702006020100070WP 2006 2 1 IXXA060096S 120041003A5712 RIB DOUG DC8 DC871F 302199DWP GE CFM CFM562 GL ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS360. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS360. IAW SRM 57-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001182006020100118WP 2006 2 1 IXXA060111S 120040730A5311 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND CORRODED FRAME AT STATION 140 LONGERON 36. REMOVED CORROSION,. ORIGINAL THICKNESS, .080 REMOVED .040 MATERIAL, OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS AT STATION 140 LONGERON 36 . IAW SRM 51-1-8, AND 53-2-0 2L74 4F4 FRT4A25 E2GL 20060201001192006020100119WP 2006 2 1 IXXA060112S 120040616A5420 PANEL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 600 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND NR 4 PYLON WRAP AROUND PANEL HAS 2 EACH DEEP GOUGES. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS ON NR 4 PYLON WRAP AROUND PANEL. IAW SRM 54-2-0, 54-3-1, 54-2-1, 51-1-21, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001902006020100190WP 2006 2 1 IXXA060039S 120040930A5532 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE VERTICAL STAB DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED AT STATION ZFS 121. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS WET WITH SEALANT FROM STATION ZFS 114.5 TO STATION ZFS 126. IAW SRM 55-2-1, 55-5-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001952006020100195WP 2006 2 1 IXXA060044S 120041007A5320 CUSP WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND RT CUSP HORIZONTAL FLANGE CORRODED AT STATION 30 LONGERON 21 RT. REMOVED AIR CONDITIONING DUCTS. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND FASTENERS AT STATION 30 LONGERON 21 RT. INSTALLED AIR CONDITIONING DUCTS IAW SRM 53-2-0, 51-3-0, 51-3-1, 51-1-4, 51-1-5, AND 51-1-8, MM 20-11-0. 2L74 4F4 FRT4A25 E2GL 20060201001972006020100197WP 2006 2 1 IXXA060046S 120041022A5340 WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATRED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 AND 33.5 AT -X48. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001982006020100198WP 2006 2 1 IXXA060026S 120041005A5753 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP UPPER SURFACE DENTED OUT OF LIMITS AT STATION XW35. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANT FROM STATION XW32 TO STATION XW39. IAW SRM 57-2-5, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060201001932006020100193WP 2006 2 1 IXXA060036S 120040930A5512 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE XFS 307.750 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT HORIZONTAL STABILIZER LEADING EDGE DENTED AT STATION XFS 307.750. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS, WET WITH SEALANT FROM STATION XFS 300 TO STATION XFS 312 IAW SRM 55-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060209001332006020900133WP 2006 2 9 IXXA060159S 120040611A5730 PANEL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE WING DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND LT WING LOWER TRAILING IB FIXED PANEL HAS DENT AFT OF MAIN LANDING GEAR STRUT. REMOVED FASTENERS AS NEEDED TO REMOVE PANEL. REMOVED DAMAGE. FABRICATED REPAIR PARTS, TRIMMED, TREATED, APPLIED ADHESIVE, PERFORMED HOT BOND, INSTALLED PANEL WITH NEW FASTENERS. IAW SRM 20-16-0, 51-3-0, 51-1-9A, 57-31-1, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060209001352006020900135WP 2006 2 9 IXXA060161S 120040611A5755 SPOILER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND LT WING NR 3 SPOILER PANEL IB TRAILING EDGE GOUGED IN TWO PLACES. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, TRIMMED, AND TREATED. APPLIED ADHEASIVE, AND CURED. SEALED EDGES AND PRIMED. IAW SRM 57-7-0, 51-1-8, 51-1-15, AND 51-1-9A. 2L74 4F4 FRT4A25 E2GL 20060210000032006021000003WP 2006 2 10 IXXA060021S 120041010A5753 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT IB FLAP DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB FLAP TRAILING EDGE PANEL UPPER SKIN DELAMINATED. REMOVED FASTENEERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN SECTION. FABRICATED FINGER DOUBLERS AND NEW UPPER SKIN SECTION. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW UPPER SKIN SECTION AND NEW FASTENERS FROM STATION XW91 TO STATION XW104. IAW SRM 57-2-1, 51-1-21, 51-1-9A, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060210000042006021000004WP 2006 2 10 IXXA060022S 120041006A5730 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT WING UPPER SURFACE CORRODED BEOND LIMITS AT STATION XRS111.000 AT FORWARD SPAR. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER AND FASTENERS WET WITH SEALANT FROM STATION XRS100.5 TO STATION 120.0 AT FRONT SPAR IAW EO COO-8-57-380-04 DATED 10/12/2004. 2L74 4F4 FRT4A25 E2GL 20060209001342006020900134WP 2006 2 9 IXXA060160S 120040611A5755 SPOILER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE LT WING GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND LT WING NR 2 SPOILER PANEL LOWER OB TRAILING EDGE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, TRIMMED, AND TREATED. APPLIED ADHESIVE, AND CURED. SEALED EDGES AND PRIMED. IAW SRM 57-7-0, 51-1-8, 51-1-15, AND 51-1-9A. 2L74 4F4 FRT4A25 E2GL 20060210000102006021000010WP 2006 2 10 IXXA060093S 120041004A5753 SKIN DOUG DC8 DC871F 302199DWP ALLSN AE300 AE3007A GL RT OB FLAP DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND RT WING OB FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XF 418. REMOVED DAMAGED. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING OB FLAP UPPER LEADING EDGE AT STATION XF 418. IAW SRM 57-2-0, 51-1-21, 51-3-0, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 TE6CH 20060210000112006021000011WP 2006 2 10 IXXA0600001S 120041011A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROURINE C-CHECK REPLACE EXTERNAL FUSELAGE SKIN AT STATION 1695 LONGERON 36 REPAIR DUE TO DTA REQUIREMENTS. REMOVED EXISTING REPAIR. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED AND INSTALLED REPAIR PARTS AND INSTALLED NEW FASTENERS. IAW EO COO-8-53-423-04. 2L74 4F4 FRT4A25 E2GL 20060210000122006021000012WP 2006 2 10 IXXA060002S 120041011A5300 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK, REPLACE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 1686 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND FASTENERS. IAW EO COO-8-53-423-4. 2L74 4F4 FRT4A25 E2GL 20060210000132006021000013WP 2006 2 10 IXXA060003S 120041011A5300 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK REPLACE EXTERNAL FUSELAGE SKIN REPAIR AT STATION 1795 LONGERON 35 LT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR, AND EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED TREATED, PRIMED, INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 1258 TO STATION 1277 BETWEEN LONGERON 35 RT TO LONGERON 34 LT. IAW SRM 53-2-1, 51-1-4, 51-1-5 AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060210000142006021000014WP 2006 2 10 IXXA060004S 120041011A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX828232773 45978 DURING ROUTINE C-CHECK REPLACE EXISTING FUSELAGE SKIN REPAIR AT STATION 1144 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED AFFECTED FASTENERS AND EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED TREATED, PRIMED INSTALLED REPAIR PARTS, AND NEW FASTENERS FROM STATION 1137.5 TO STATION 1151 BETWEEN LONGERON 34 RT TO LONGERON 35 LT IAW COOPESA EO COO -8-53-411-04. 2L74 4F4 FRT4A25 E2GL 20060210000152006021000015WP 2006 2 10 IXXA060005S 120041011A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 543 LONGERON 35 RT DUE TP DTA REQUIREMENTS. REMOVED AFFECTED FASTENERS AND EXISTING SKIN REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED,REMOVED, TREATED, PRIMED, INSTALLED REPAIR PARES, AND NEW FASTENERS FROM STATION 525 TO STATION 552.5 BETWEEN LONGERON 34 RT TO LONGERON 35 LT. IAW EO COO-8-53-400-04. 2L74 4F4 FRT4A25 E2GL 20060210000172006021000017WP 2006 2 10 IXXA06007S 120041011A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 550, LONGERON 35 RT. REMOVED NECESSARY FASTENERS AND EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED REMOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS, AND FASTENERS, AT STATION 525 TO STATION 552.5 LONGERON 34 RT TO LONGERON 35 LT. IAW EO COO-8-53-400-04. 2L74 4F4 FRT4A25 E2GL 20060210000182006021000018WP 2006 2 10 IXXA060008S 120041110A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR DT STATION 410 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED AFFECTED FASTENERS AND DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS FROM STATION 397 TO STATION 422 BETWEEN LONGERON 34 RT TO 34 LT IAW SRM 53-2-1, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060210000212006021000021WP 2006 2 10 IXXA060047S 120041022A5300 WEB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND WEB CRACKED ST STATION 30 -X48. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER AND FASTENERS AT STATION 30 TO 33.5 AT -X48. IAW SRM 53-2-0, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060214000942006021400094WP 2006 2 14 IXXA060009S 120041110A5101 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 SCHEDULED MAINT A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REMOVE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 220 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. REMOVED NECESSARY FASTENERS, AND EXISTING DOUBLER, REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TERATED, PRIMED, INSTALLED NEW REPAIR PARTS ANS FASTENERS FROM STATION 211 TO STATION 236, BETWEEN LONGERON 34 RIGHT AND 33 LEFT IAW COOPESA EO COO -8-53-405-4 2L74 4F RT4A25 20060214000952006021400095WP 2006 2 14 IXXA0060010S 120041011A5101 REPAIR DOUG DC8 DC871F 302199DWP ZONE 100 SCHEDULED MAINT A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK REMOVE EXISTING EXTERNAL SKIN REPAIR AT STATION 172 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS AS NEEDED AND EXISTING DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND NEW FASTENERS AT STATION 169.5 TO STATION 182.5 BETWEEN LONGERON 34 RIGHT AND 34 LEFT IAW COOPESA E.O. COO-8-53-406-04. 2L74 4F RT4A25 20060214000962006021400096WP 2006 2 14 IXXA060011S 120041025A5522 SKIN DOUG DC8 DC871F 302199DWP ZONE 300 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND EMPENNAGE RIGHT HAND ELEVATOR UPPER AND LOWER SKIN DENTED IN SEVERAL AREAS. REMOVED RIGHT HAND ELEVATOR. REMOVED RIGHT HAND ELEVATOR UPPER AND LOWER SKIN SECTION FROM STATION XE 132.531 TO XE251.562. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW SKIN SECTION AND NEW FASTENERS. INSTALLED RIGHT HAND ELEVATOR ON EMPENNAGE IAW DC8 MM 27-30-1, 27-31-01, DC8 SRM 51-1-9, 55-4-1, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060214000972006021400097WP 2006 2 14 IXXA060012S 120041003A5712 RIB DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HAND WING LEADING EDGE CAVITY AT STATION XFS410.25 AND 416.500 UPPER RIBS CRACKED. REMOVED NEEDED FASTENERS. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC87 SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060214000982006021400098WP 2006 2 14 IXXA060013S 120041011A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HAND WING SKIN CRACKED AT STATION 143.000. REMOVED FUEL DUCTS. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS WET WITH SEALANT FROM STATION XRS 60-300 TO 88.050 BETWEEN CENTER SPAR AND STRINGER NUMBER 10 IAW DC8 MM 28-25-16, DC8 SRM 57-2-1, 51-1-12, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060214000992006021400099WP 2006 2 14 IXXA060015S 120041011A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XFS 132.250. REMOVED FASTENERS AS NEEDED TO PERFORMED REPAIR. REMOVED DAMAGE. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER, FILLER AND NEW FASTENERS WET WITH SEALANT FROM STATION XFS 116.250 TO 132.250 AT FRONT SPAR IAW COOPESA E.O. COO-8-57-384-04 DATED 10/12/2004. 2L74 4F RT4A25 20060214001002006021400100WP 2006 2 14 IXXA060016S 120041005A575556551671 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT HAND WING SPOILER NUMBER 3 DELAMINATED AT STATION XRS 218. REMOVED RIGHT HAND NUMBER 3 SPOILER. REMOVED UPPER, LOWER SKIN AND HONEYCOMB CORE. FABRICATED NEW REPAIR PARTS. INSTALLED AND BONDED REPAIR PARTS IN NUMBER 3 RIGHT HAND SPOILER. INSTALLED NUMBER 3 RIGHT HAND SPOILER, RIGGED AND OPERATIONAL CHECK GOOD IAW DC8 MM27-61-1, AND COOPESA EO COO-CMP-8-57-412-04 DATED10/28/2004. 2L74 4F RT4A25 20060214001012006021400101WP 2006 2 14 IXXA060017S 120041004A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING OUT BOARD FLAP DENTED AT STATION XW384. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND NEW FASTENESR WET WITH SEALANT FROM STATION WX382 TO STATION XW385 IAW DC8 SRM 57-2-5, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060214001022006021400102WP 2006 2 14 IXXA060018S 120041004A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED BETWEEN STATION XF309 AND XF333. REMOVED FASTENERS AS NEEDED. REMOVED LOWER SKIN SECTION. FABRICATED NEW SKIN SECTION AND FILLERS. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW SKIN AND NEW FASTENERS WET WITH SEALANT FROM STATION XF309 TO STATION XF333 IAW DC8 SRM 57-2-0, 51-1-21, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060214001032006021400103WP 2006 2 14 IXXA060019S 120041005A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REMOVED FASTENERS AS NEEDED TO REMOVE RIGHT WING OUTBOARD FLAP LOWER SKIN FROM STATION XF169 TO STATION XF213. FABRICATED, NEW SKIN AND FINGER DOUBLERS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW SKIN AND FINGER DOUBLERS FROM STATION XF169 TO STATION XF213. IAW DC8 SRM 57-2-0, 51-1-21, 51-1-9, 57-7-1, 51-1-5, AND 51-1-8. 2L74 4F RT4A25 20060214001042006021400104WP 2006 2 14 IXXA060020S 120041010A5730 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND LEFT HAND WING UPPER SKIN CRACKED AT STATION XRS 22.7 AT CENTER SPAR. REMOVED ALL FASTENERS COMMON TO REPAIR AREA. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS WET WITH SEALANT FROM STATION XRS 27.750 TO STATION XRS 6.750 BETWEEN STRINGER 9 AND STRINGER 10 IAW COOPESA EO COO-8-57-381-04. 2L74 4F RT4A25 20060209001322006020900132WP 2006 2 9 IXXA060158S 120040611A5720 ANGLE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND LT WING AFT WING ROOT, AT STATION XFS-950,AND XW-0, ANGLE PLATE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGLE AND NEW FASTENERS. IAW SRM 51-1-21, 51-1-4, 51-1-24, 51-1-8, AND 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20060210000022006021000002WP 2006 2 10 IXXA060027S 120041005A5753 SKIN DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE LT IB FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK FOUND LT WING IB FLAP LEADING EDGE UPPER SKIN CRACKED AT STATION XW84. REMOVED FLAP VANE, AND NOSE PANEL TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER, FILLER, AND FASTENERS WET WITH SEALANT FROM STATION XW 81.5 TO STATION 86.5. INSTALLED FLAP VANE AND NOSE PANEL. IAW MM 27-51-14, OHM 27-27-1, SRM 57-2-1,57-7-1, 51-1-5 AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060210000162006021000016WP 2006 2 10 IXXA060006S 120041011A5330 DOUBLER DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C-CHECK REMOVED EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STATION 543 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED NECESSARY FASTENERS AND EXISTING SKIN REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS, FROM STATION 525 TO STATION 552.5 BETWEEN LONGERON 34 RT AND LONGERON 35 LT. IAW EO COO-8-53-400-4 2L74 4F4 FRT4A25 E2GL 20060216002102006021600210WP 2006 2 16 IXXA060163S 120040611A5720 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE DOUBLER CRACKED AND MISSING FASTENERS. REMOVED DOUBLER. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SC8 SRM 57-2-0, 57-5-0, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20060216002112006021600211WP 2006 2 16 IXXA060164S 120040612A5730 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT WING GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C CHECK FOUND LT WING NR 1 MAIN-TANK-VENT FLOAT VALVE JUST OB OF XRS-358 HAS GOUGED UPPER SKIN. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, NEW FASTENERS AND SEALED REPAIR. IAW SRM 51-10-0, 57-3-0, AND DRAWING W20-R02 REVISION IR DATED 7/2/04. 2L74 4F4 FRT4A25 E2GL 20060216003892006021600389WP 2006 2 16 IXXA060089S 120041007A5753 SKIN DOUG DC8 DC871F 302199DWP T/E FLAP VANE PUNCTURED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND RIGHT HAND WING INBOARD FLAP OUTBOARD VANE UPPER SIDE SKIN PUNCTURED. REMOVED VANE. REMOVED DAMAGED. MANUFACTURED REPAIR PARTS, PERFORMED HOT BOND. INSTALLED VANE. IAW DC8 MM 27-51-14, DC8 SRM 51-1-9A. 2L74 4F RT4A25 20060227002762006022700276WP 2006 2 27 IXXA060156S 120040610A5720 MEMBRANE DOUG DC8 DC873F 302199FWP LT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING LEADING EDGE 522A BAY INBOARD AND FORWARD OF PANEL CUT OUT ANTI-ICE DISCHARGE MEMBRANE CRACKED AT HOLES 3 PLACES .5 INCH EACH XFS395. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED REPAIR PART AND NEW FASTENERS IAW DC8 SRM 51-1-21, 57-2-1, AND 51-1-8. 2L74 4F RT4A25 20060227003172006022700317WP 2006 2 27 IXXA060165S 120040615A5753 DOUBLER DOUG DC8 DC873F 302199FWP T/E FLAP GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FLAP UPPER OUTBOARD REPAIR DOUBLER GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED NEW DOUBLER AND NEW FASTENERS IAW DC8 SRM 57-2-1, 51-1-21, 57-7-0, 51-1-20A AND 51-1-8. 2L74 4F RT4A25 20060327001102006032700110 2006 3 27 MASA200400734 420041230A3416HG2010AC02 INDICATOR EMB 145 EMB145LR 3260212SO COCKPIT FAILED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07849MJ7248 145534 OPEN -ASH 2731 CLT TO JAN RETURNED TO THE FIELD DUE TO LOSS OF FIRST OFFICERS HEADING AND ALTITUDE INFORMATION AND AN IC600 FAIL ON THE FMS. MAINTENANCE IS TROUBLESHOOTING. MAINTENANCE R2 NR 2 AHRS. 2L72 4T RTT00011AT 20060327001092006032700109 2006 3 27 MASA200400709 420041220A3160 DISPLAY EMB 145 EMB145LR 3260212SO COCKPIT INOPERATIVE A MASAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW07827MJ 145217 ASH 2930 TRI-CLT - ABORTED TAKOFF DUE TO THE CAPTAINS PFD GOING BLANK AND THEN COMING BACK ON LINE. ON CALL MAINTENANCE RERACKED THE PFD AND PERFORMED THE OPERATIONAL CHECK. 2L72 4T RTT00011AT 20060328002042006032800204SO 2006 3 28 MASA200400052 120040128A2560P2070011100 FLASHLIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A MASAK NONE L NO TEST ININSP/MAINT 1 SW07827MJ 145217 ASH 2719 CLT - CREW REPORTED THE FLIGHT DECK EMERGENCY FLASHLIGHT WAS INOP. MX REPLACED THE FLASHLIGHT. 2L72 4T RTT00011AT 20060328002052006032800205 2006 3 28 MASA200400561 420041004A2250 YAW DAMPER EMB 145 EMB145LR 3260212SO WARNING LIGHT A MASAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW07855MJ 145614 ASH 2607 CLT - RETURNED TO THE GATE FOR A YAW DAMPER FAILED AFTER PUSHBACK. MAINTENANCE RESET THE YAW DAMP SYSTEM. 2L72 4T RTT00011AT 20060328002072006032800207 2006 3 28 MASA200400661 420041128A2210HG2010AC02 AHRS EMB 145 EMB145LR 3260212SO NR 2 MALFUNCTIONED A MASAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW07827MJ9099 145217 ASH 2665 CLT - AUTO PILOT FAILED IN FLIGHT. MAINTENANCE REPLACED THE NR 2 AHRS. 2L72 4T RTT00011AT 20060327001082006032700108 2006 3 27 MASA200400693 420041213A3160 DISPLAY EMB 145 EMB145LR 3260212SO COCKPIT FAILED A MASAC ABORTED TAKEOFF P NO WARNING INDICATION TOTAKEOFF 1 SW07827MJ 145217 ASH 2722 PWM TO CLT - ABORTED TAKEOFF DUE TO CAPTAINS PFD GOING BLANK AND THEN COMING BACK ON LINE. ON CALL MAINTENANCE RERACKED THE PFD AND PERFORMED THE OPERATIONAL CHECK. 2L72 4T RTT00011AT 20060328002062006032800206 2006 3 28 MASA200400562 420041004A2200 UNKNOWN EMB 145 EMB145LR 3260212SO UNKNOWN A MASAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 SW07835MJ 145353 ASH 2792 DCA - HAD AN AUTO PILOT DISENGAGE IN FLIGHT AT FL 210. THE AIRCRAFT ROLLED UNCOMMANDED TO THE RIGHT, THEN ABRUPTLY TO THE LEFT. MAINTENANCE INSPECTED AND TESTED AUTO PILOT SYSTEM AND COULD NOT DUPLICATE FAULT. 2L72 4T RTT00011AT 20060404000192006040400019EA 2006 4 4 MASA200400722 120041223A29169604501 RESERVOIR CNDAIRCL600 CL6002C10 1390015EA HYD SYSTEM LEAKING A MASAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07501MJ4979 10047 ASH 7276 TUS-DEN - RETURNED TO FIELD DUE TO HYD 3 LOSS OF FLUID. MAINTENANCE REMOVED AND REPLACED NR 3 HYD RESERVOIR AND REPLACED CRACKED HYD LINE IN THE RT WING. 2L72 4F RTA21EA 20060626001942006062600194WP 2006 6 26 IXXA060189S 120041004A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND SKIN BULGING AT STATION 1582 BETWEEN LONGERONS 27 LEFT AND 28 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060522002462006052200246SW 2006 5 22 HEEA108771 120041208A5630205032669233 WINDOW BELL 212 212 1181420SW CARGO BAY DEPARTED E HEEAK NONE D INFLIGHT SEPARATION CRCRUISE 1 SW035736J 31140 LH CARGO DOOR FWD WINDOW DEPARTED IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE AND INSTALLED A NEW WINDOW. 1G71 4U H4SW 20060524002192006052400219 2006 5 24 CLC2006F00006 420040728A25655WD230100201 WINDOW FRAME DOUG DC10 DC1040F 3023507NM PWA JT9 JT9D* NE R1 DOOR OUT OF ADJUST A CLCAK NONE O OTHER ININSP/MAINT 1 SO29140WE 3061 46920 R1 DOOR WILL NOT DISARM, WHILE TROUBLESHOOTING THE DOOR THE SLIDE DEPLOYED. FOUND VIEW WINDOW FRAME FOR THE ARMED LEVER BINDING. REPOSITIONED VIEW WINDOW FRAME, REPLACED SLIDE, FUNCTIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO REVENUE SERVICE. (K) 2L73 4F4 FRTA22WE E20EA 20060526000202006052600020SO 2006 5 26 4011 120040321A3260487862 DOWNLOCK SWITCH PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA LT MLG INTERMITTENT E BSYAK NONE N FALSE WARNING LDLANDING 1 GL07711LH 318152174 L173868A FH848 INTERMITTENT LEFT GEAR DOWN AND LOCK LIGHT. FOUND DOWN AND LOCK SWITCH BAD. REMOVED AND REPLACED SWITCH OPS, CHECKS GOOD. 1L72 3O3 O A20SO E14EA 20060526000252006052600025NE 2006 5 26 4022 220040914A8520 CRANKSHAFT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2B NE LT ENGINE FAILED E BSYAA UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CRCRUISE 1 GL07525AA 318052111 L867361A PILOT WAS IN CRUISE, LEFT ENGINE HAD VIBRATION AND UNCOMMANDED SHUT DOWN. PILOT LANDED AT PHD. VISUAL INSPECTION REVEALED CRANKCASE DAMAGE / CRANKSHAFT HAD FAILED. REASON UNKNOWN AT THIS TIME. REPLACED ENGINE WITH NEW. 1L72 3O3 O A20SO E14EA 20060612002032006061200203SO 2006 6 12 XGN2006F00027 220041221A8530ECI712BCA CYLINDER CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW054165G885 402B1212 502537R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060609002402006060900240SO 2006 6 9 XGN2006F00031 220041101A8530ECI712BCA CYLINDER CONT CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE CRACKED E XGNAK NONE O OTHER ININSP/MAINT 1 SW055421M595 503049R 402B0021 503049R CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) 1L72 3O3 O A7CE E8CE 20060614000382006061400038WP 2006 6 14 IXXA060230S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C-CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1000 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060614000352006061400035WP 2006 6 14 IXXA060219S 120040609A535056544372 PANEL DOUG DC8 DC862F 3021972WP FUSELAGE DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C-CHECK FOUND WING FILLET PANEL NUMBER 162C DENTED. REPLACED OUTER SKIN AND HONEYCOMB SECTION PER COOPESA EO COO-CMP-8-53-260-04 DATED 07/14/2004. 2L74 4F 4A25 20060801001452006080100145WP 2006 8 1 IXXA060588S 120040910A5753 SKIN DOUG DC8 DC871F 302199DWP ZONE 500 GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11829BX868322840 45994 DURING ROUTINE C CHECK, FOUND LEFT INBOARD FLAP TOP SKIN GOUGED AT STATION XF 90. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-21. 2L74 4F RT4A25 20060621001852006062100185NM 2006 6 21 2006UALA01154 120040829A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 RIGHT OVERWING DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REMOVE AND REPLACE LATCHES IAW 767 MM 25-65-98 2L72 4F4 FRTA1NM E24NE 20060621001832006062100183NM 2006 6 21 2006UALA01153 120040829A2560 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 LT O/W COMPT DOOR LATCH NR 3 PINHOLE EDGE MARGIN WORN BEYOND LIMITS, LATCH REPLACED. 2L72 4F4 FRTA1NM E24NE 20060622000602006062200060WP 2006 6 22 IXXA060183S 120040607A5313 FITTING DOUG DC8 DC862 3021970WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 23 RIGHT. REPLACED DAMAGED END FITTING, AND FASTENERS AT STATION Y1530 LONGERON 23 RIGHT IAW DC8 SRM 53-2-0, AND 51-1-20D. 2L74 4F 4A25 20060622001492006062200149WP 2006 6 22 IXXA060272S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y902 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001512006062200151WP 2006 6 22 IXXA060274S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1280 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001542006062200154WP 2006 6 22 IXXA060277S 120040625A5320 ANGLE DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION Y110, +Z3, +X48. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001552006062200155WP 2006 6 22 IXXA060278S 120040629A5315 FLOORBEAM DOUG DC8 DC862 3021970WP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT STATION Y1542, -X37 TO -X43. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001592006062200159WP 2006 6 22 IXXA060282S 120040701A5310 WINDOW FRAME DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1240 TO 1260 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001612006062200161WP 2006 6 22 IXXA060289S 120040713A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP ZONE 200 DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND SEAT TRACK AND FLOOR PANEL WITH A HOLE AT STATION Y1500 +X45. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001622006062200162WP 2006 6 22 IXXA060200S 120040608A5347 CARGO TRACK DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CARGO TRACK AND SUPORT CHANNEL CORRODED FROM STATION 990 TO STATION 1120 - X 17 AT LONGERON 33 RIGHT HAND. REMOVED CORROSION ON CARGO TRACK, WITH IN LIMITS. REPLACED CARGO TRACK SUPPORT CHANNEL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001642006062200164WP 2006 6 22 IXXA060206S 120040608A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND SEAT TRACK CORRODED AT STATION 1150 Z0 X0. REPLACED SEAT TRACK FROM STATION 1120 TO 1197 Z0 X0 PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001562006062200156WP 2006 6 22 IXXA060279S 120040630A5330 DOUBLER DOUG DC8 DC862 3021970WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND DOUBLER CORRODED FROM STATION 188 TO 208 AT Z=0 BETWEEN -X45 AND -X62. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001572006062200157WP 2006 6 22 IXXA060280S 120040701A5310 WINDOW FRAME DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1320 TO 1340 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001602006062200160WP 2006 6 22 IXXA060283S 120040701A5310 WINDOW FRAME DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1240 TO 1260 RIGHT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002782006062200278WP 2006 6 22 IXXA060293S 120040715A5340 FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602990 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION Y798, -Z1, +X25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002792006062200279WP 2006 6 22 IXXA060294S 120040725A5313 LONGERON DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CRACKED LONGERON AT STATION Y1500 LONGERON 24 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002802006062200280WP 2006 6 22 IXXA060295S 120040721A5340 FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CORRODED FITTING FROM STATION Y960 TO Y980, -Z10, +X25. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002822006062200282WP 2006 6 22 IXXA060297S 120040715A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y1480 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002832006062200283WP 2006 6 22 IXXA060298S 120040725A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME SPLICE WITH A DOUBLE DRILLED HOLE AT STATION Y1500 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002892006062200289WP 2006 6 22 IXXA060236S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1080 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002902006062200290WP 2006 6 22 IXXA060237S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1120 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002912006062200291WP 2006 6 22 IXXA060238S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1140 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002922006062200292WP 2006 6 22 IXXA060239S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME WORN IN SEVERAL PLACED AT STATION 480 BETWEEN LONGERONS 20 LEFT AND 21 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002932006062200293WP 2006 6 22 IXXA060240S 120040607A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1240 BETWEEN LONGERONS 10 LEFT AND 11 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002942006062200294WP 2006 6 22 IXXA060241S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 100 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A FRAME RADIUS WITH A HOLE AT STATION 1400 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002962006062200296WP 2006 6 22 IXXA060244S 120040607A5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORTS CORRODED BETWEEN STATION 1540 AND STATION 1620 FROM X40 AND -X4, Z0. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002972006062200297WP 2006 6 22 IXXA060245S 120040607A5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FLOOR SUPPORTS CORRODED AT STATION 1580 BETWEEN X35 AND -X35, Z0. REPLACED FLOOR SUPPORTS PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002982006062200298WP 2006 6 22 IXXA060284S 120040702A5330 DOUBLER DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND DOUBLER CORRODED AT STATION 198, -X61, -Z10. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060622003002006062200300WP 2006 6 22 IXXA060286S 120040709A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1000 AT LONGERON 13 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003022006062200302WP 2006 6 22 IXXA060287S 120040710A5340 SUPPORT DOUG DC8 DC862F 3021972WP ZONE 200 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT AFT ENTRY DOOR UPPER HINGE SUPPORT WORN. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003142006062200314WP 2006 6 22 IXXA060304S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003172006062200317WP 2006 6 22 IXXA060195S 120041004A5330 SKIN DOUG DC8 DC862F 3021972WP ZONE 100 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND SKIN DENTED AT STATION Y1190 BETWEEN LONGERONS 31 LEFT AND 33 LEFT. REPAIRED SKIN PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003182006062200318WP 2006 6 22 IXXA060307S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003192006062200319WP 2006 6 22 IXXA060308 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003222006062200322WP 2006 6 22 IXXA060309S 120040605A5512 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX * 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN FROM FRONT SPAR TO REAR SPAR AT STATION XE28.843 CORRODED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003242006062200324WP 2006 6 22 IXXA060311S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003262006062200326WP 2006 6 22 IXXA060319S 120040608A5512 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED AT STATION XFS239. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003272006062200327WP 2006 6 22 IXXA060321S 120040610A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RUDDER LEFT SIDE AFT SKIN PANEL BULGED FROM STATION ZR100 TO ZR110. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003282006062200328WP 2006 6 22 IXXA060335S 120040613A5320 SUPPORT DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CEILING SUPPORT CORRODED AT STATION Y101, +X45. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003402006062200340WP 2006 6 22 IXXA060341S 120040615A5343 BOSS DOUG DC8 DC862F 3021972WP ZONE 700 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT MAIN LANDING GEAR SHOCK STRUT RETRACT PIN BOSS INNER SURFACE CORRODED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003442006062200344WP 2006 6 22 IXXA060345S 120040615A5315 SUPPORT FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y253, +X45, -Z1. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003452006062200345WP 2006 6 22 IXXA060346S 120040625A5315 SUPPORT FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y267, -X45. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003472006062200347WP 2006 6 22 IXXA060348S 120040803A5313 LONGERON DOUG DC8 DC862F 3021972WP ZONE100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 25 RIGHT CRACKED AT STATION Y390. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003482006062200348WP 2006 6 22 IXXA060336S 120040613A5320 WEB DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y169, -X52 AND -X58, -Z11. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003492006062200349WP 2006 6 22 IXXA060337S 120040614A5320 WEB DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y169, +X52, -Z11. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003502006062200350WP 2006 6 22 IXXA060338S 120040614A5320 WEB DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WEB CORRODED AT STATION Y148, +X52, -Z11. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003512006062200351WP 2006 6 22 IXXA060199S 120040608A5347 CARGO TRACK DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND TRACK CORRODED FROM STATION 990 TO STATION 1380 + X17 AT LONGERON 33 LEFT HAND. REPLACED CARGO TRACK SECTION FROM STATION 1140 TO STATION 1380 + X17 PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003572006062200357WP 2006 6 22 IXXA060203S 120040608A5330 SKIN DOUG DC8 DC862F 3021972WP ZONE 100 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FUSELAGE SKIN EXISTING DOUBLER BULGED AT STATION Y1530 BETWEEN LONGERONS 29 LEFT AND 32 LEFT. REMOVED CORROSION, MANUFACTURED AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003582006062200358WP 2006 6 22 IXXA060205S 120040608A5330 SKIN DOUG DC8 DC862F 3021972WP ZONE 100 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN BULGED AT STATION 522 AT LONGERON 34 RIGHT HAND. REPAIRED PER COTNEY DRAWING W08-R08 DATED 7/22/04. 2L74 4F 4A25 20060622001482006062200148WP 2006 6 22 IXXA060271S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y860 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001522006062200152WP 2006 6 22 IXXA060275S 120040618A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION 188 BETWEEN LONGERONS 3 RIGHT AND 11 RIGHT, ALSO 3 LEFT AND 11 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001672006062200167WP 2006 6 22 IXXA060290S 120040715A5340 FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A CRACKED FITTING AT STATION 759, +X25, -Z1. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002762006062200276WP 2006 6 22 IXXA060291S 120040715A5340 FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION 781, -Z1, +X25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002772006062200277WP 2006 6 22 IXXA060292S 120040715A5340 FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION 781, -Z1, -X25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002872006062200287WP 2006 6 22 IXXA060302S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003152006062200315WP 2006 6 22 IXXA060305S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003162006062200316WP 2006 6 22 IXXA060306S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE221 BULGED AND DENTED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003232006062200323WP 2006 6 22 IXXA060310S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE SECTION BETWEEN STATION XE272 TO XE312 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003252006062200325WP 2006 6 22 IXXA060312S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE149 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003292006062200329WP 2006 6 22 IXXA060339S 120040615A531057585422N BEAM DOUG DC8 DC862F 3021972WP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND UPPER TRANSVERSAL BEAM CRACKED AT STATION Y260 +X45. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003302006062200330WP 2006 6 22 IXXA060340S 120040615A531057585422N BEAM DOUG DC8 DC862F 3021972WP ZONE 200 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND UPPER TRANSVERSAL BEAM CRACKED AT STATION Y260 -X45. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003312006062200331WP 2006 6 22 IXXA060350S 120040606A5311 DOUBLER DOUG DC8 DC862F 3021972WP ZONE100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND DOUBLER ATTACH FRAME CORRODED AT STATION Y255. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003322006062200332WP 2006 6 22 IXXA060349S 120040808A5340 FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FITTING CORRODED AT STATION Y1280 LONGERON 33 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003412006062200341WP 2006 6 22 IXXA060342S 120040611A53405753113U509 FITTING DOUG DC8 DC862 3021970WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT FITTING CORRODED AT STATION Y910, -Z10. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003432006062200343WP 2006 6 22 IXXA060344S 120040625A5315 SUPPORT FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND AIR CONDITIONING FLOORBEAM SUPPORT FITTING CRACKED AT STATION Y253, +X45. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003532006062200353WP 2006 6 22 IXXA060194S 120041004A5244 DOUBLER DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND AIR START ACCESS DOOR CUTOUT DOUBLER CRACKED. REPLACED DOUBLER PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001502006062200150WP 2006 6 22 IXXA060273S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1120 AT LONGERON 14 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001532006062200153WP 2006 6 22 IXXA060276S 120040616A5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOOR SUPPORTS CORRODED FROM STATION YT200 TO Y240, Z=0 BETWEEN +X40 AND -X40. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001582006062200158WP 2006 6 22 IXXA060281S 120040701A5310 WINDOW FRAME DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1280 TO 1300 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622001632006062200163WP 2006 6 22 IXXA060204S 120040608A5330 SKIN DOUG DC8 DC862F 3021972WP ZONE 200 SCRATCHED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AT STATION 268.5 AT LONGERON 24 LEFT HAND. REPAIRED PER COTNEY DRAWING WO8-R14 DATED 7-20-04. 2L74 4F 4A25 20060622002842006062200284WP 2006 6 22 IXXA060299S 120040725A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1340 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002862006062200286WP 2006 6 22 IXXA060301S 120040725A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y1060 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002882006062200288WP 2006 6 22 IXXA060235S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 960 LONGERON 14 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003032006062200303WP 2006 6 22 IXXA060288S 120040710A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP ZONE 200 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND SEAT TRACK CORRODED FROM STATION Y420 TO Y560, -X25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003462006062200346WP 2006 6 22 IXXA060347S 120040719A5320 INTERCOSTAL DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CORRODED INTERCOSTAL FROM STATION Y460 TO Y480, BETWEEN LONGERONS 34 LEFT AND 35 LEFT REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003522006062200352WP 2006 6 22 IXXA060193S 120041004A5313 LONGERON DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT CORRODED FROM STATION Y879.375 TO STATION Y402.000. REPAIRED LONGERON PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003542006062200354WP 2006 6 22 IXXA060201S 120040608A5320 CHANNEL DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FLOOR CHANNELS CORRODED AND CRACKED FROM STATION 990 TO STATION 1120 -X7, AND +X7. REPLACED FLOOR CHANNELS FROM STATION 990 TO STATION 1120 -X7 AND+X7, PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003562006062200356WP 2006 6 22 IXXA060196S 120041004A5313 LONGERON DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND LONGERON 23 RIGHT CORRODED BETWEEN STATION Y1000 AND STATION Y1020. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003592006062200359WP 2006 6 22 IXXA060190S 120041004A5313 LONGERON DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND LONGERON 29 LEFT CORRODED FROM STATION Y510 TO STATION Y490. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623000882006062300088WP 2006 6 23 IXXA060351S 120040606A5313 LONGERON DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LONGERON 8 RIGHT CORRODED BETWEEN STATIONS Y300 TO Y348. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623000892006062300089WP 2006 6 23 IXXA060352S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y742 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623000922006062300092WP 2006 6 23 IXXA060355S 120040606A5320 INTERCOSTAL DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND INTERCOSTAL CORRODED FROM STATION Y270 TO Y255 BETWEEN LONGERONS 6 LEFT AND 7 LEFT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060623000952006062300095WP 2006 6 23 IXXA060356S 120040607A5313 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LONGERON 20 LEFT END FITTING CRACKED AT STATION Y1530. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060623001052006062300105WP 2006 6 23 IXXA060359S 120040715A5320 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FITTING CRACKED AT STATION 798, -Z1, -X25. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001082006062300108WP 2006 6 23 IXXA060325S 120040611A5320 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND CRACKED FITTING ST STATION Y101, +X20. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001092006062300109WP 2006 6 23 IXXA060326S 120040615A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND SKIN DENTED AT STATION Y1287 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001112006062300111WP 2006 6 23 IXXA060328S 120040615A5313 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT END FITTING CORRODED AT STATION Y212. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001132006062300113WP 2006 6 23 IXXA060330S 120040612A5313 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 23 LEFT END FITTING CRACKED AT STATION Y990. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001142006062300114WP 2006 6 23 IXXA060331S 120040612A5313 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT LONGERON 22 RIGHT STATION Y990. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001152006062300115WP 2006 6 23 IXXA060332S 120040612A5321 FLOOR PANEL DOUG DC8 DC862F 3021972WP CARGO BAY CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR PANEL CRACKED FROM STATION Y480 TO Y500. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001232006062300123WP 2006 6 23 IXXA060188S 120041004A5730 FILLET DOUG DC8 DC862F 3021972WP LT WING DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING FILLET PANEL (NUMBER 1612) DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001302006062300130WP 2006 6 23 IXXA060191S 120041004A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION Y181, -X35, BETWEEN LONGERONS 21 RIGHT AND 32 RIGHT. REPLACED FRAME SECTION PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001452006062300145WP 2006 6 23 IXXA060184S 120040607A5320 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 46129523 DURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 21 RIGHT. REMOVED DAMAGED END FITTING. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW END FITTING AT STATION Y1530 LONGERON 21 RIGHT IAW DC8 SRM 51-1-20D, AND 53-2-0. 2L74 4F 4A25 20060623001622006062300162WP 2006 6 23 IXXA060366S 120040617A5514565208689 HOUSING DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LINKAGE HOUSING CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS136. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001742006062300174WP 2006 6 23 IXXA060369S 120040617A5511 STRAP DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER CLOSING SPAR STRAP SCRATCHED AND CRACKED BETWEEN STATION XRS176 TO XRS215. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001752006062300175WP 2006 6 23 IXXA060370S 120040617A5511 STRINGER DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER STRINGER CRACKED AT STATION XFS47. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002812006062200281WP 2006 6 22 IXXA060296S 120040723A5320 ANGLE DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A CORRODED ANGLE AT STATION 1500 LONGERON 23 LEFT STRUCTURE BOX. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002852006062200285WP 2006 6 22 IXXA060300S 120040725A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y640 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002952006062200295WP 2006 6 22 IXXA060242S 120040607A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 200 TOOL DAMAGE A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION 1460 LONGERON 9 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622002992006062200299WP 2006 6 22 IXXA060285S 120040702A53404641324501W ATTACH FITTING DOUG DC8 DC862F 3021972WP ZONE 100 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON FITTING CRACKED AT STATION 1530 LONGERON 34 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003042006062200304WP 2006 6 22 IXXA060303S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003422006062200342WP 2006 6 22 IXXA060343S 120040616A5313 LONGERON SPLICE DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT SPLICE CORRODED AT STATION Y406. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003552006062200355WP 2006 6 22 IXXA060202S 120040608A5311 FRAME DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FRAME CORRODED ON UPPER CHORD LOWER FACE AT STATION 1100 BETWEEN LONGERON 33 LEFT AND 33 RIGHT. REMOVED CORROSION, MANUFACTURED AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001042006062300104WP 2006 6 23 IXXA060358S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y600 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001122006062300112WP 2006 6 23 IXXA060329S 120040611A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND TRACK CORRODED FROM STATION Y1000 TO Y1100, Z0, -X60. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001282006062300128WP 2006 6 23 IXXA060187S 120041004A5313 LONGERON SPLICE DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON SPLICE CRACKED BETWEEN STATIONS 600, AND STATION 620 LONGERON 31 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623002332006062300233WP 2006 6 23 IXXA060362S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623002362006062300236WP 2006 6 23 IXXA060372S 120040617A5511 SUPPORT DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER SPAR CAP SUPPORT CRACKED AT STATION XFS62. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000262006062600026WP 2006 6 26 IXXA060374S 120040617A5511 SPAR DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER LOWER REAR SPAR CRACKED AT STATION XE40. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626000272006062600027WP 2006 6 26 IXXA060375S 120040617A5511 FITTING DOUG DC8 DC862F 3021972WP HORIZ STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER FRONT SPAR SUPPORT FITTING CORRODED AT STATION XFS72. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000292006062600029WP 2006 6 26 IXXA060377S 120040618A5522 SKIN DOUG DC8 DC862F 3021972WP RT ELEVATOR CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT ELEVATOR LOWER SURFACE SKIN CORRODED AT STATION XE246. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000302006062600030WP 2006 6 26 IXXA060197S 120040607A5320 FITTING DOUG DC8 DC862 3021970WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 26 LEFT. REPLACED DAMAGED END FITTING WITH NEW PER APPLICABLE DATA. 2L74 4F 4A25 20060626000552006062600055WP 2006 6 26 IXXA060207S 120040608A5320 SUPPORT DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND CEILING SUPPORTS CORRODED IN SEVERAL PLACES FROM STATION 1380 -28 BETWEEN -X41 AND +X41. REMOVED CORROSION AND REPLACED SUPPORTS AS NEEDED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000852006062600085WP 2006 6 26 IXXA060208S 120040608A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE SCRATCHED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AT STATION 557.5 BETWEEN LONGERONS 29 RIGHT HAND AND 30 RIGHT HAND. REPAIRED PER COTNEY DRAWING W08-R12 DATED 7-22-04 2L74 4F 4A25 20060626001012006062600101WP 2006 6 26 IXXA060213S 120040609A5315 FLOORBEAM DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOOR BEAM CRACKED AT STATION 1420, Z0, -X45. REPAIRED PER COOPESA EO COO-8-53-243-04 DATED 7/7/04. 2L74 4F 4A25 20060626001032006062600103WP 2006 6 26 IXXA060211S 120040609A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FORMER CRACKED AT STATION 380 BETWEEN LONGERONS 31 RIGHT HAND AND 32 RIGHT HAND. REMOVED DAMAGE, MANUFACTURED, AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001052006062600105WP 2006 6 26 IXXA060215S 120040609A5315 FLOORBEAM DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOORBEAM UPPER FLANGE CORRODED AT STATION 420 BETWEEN -X29 AND -X42. REPAIRED FLOORBEAM PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001102006062600110WP 2006 6 26 IXXA060217S 120040610A5313 LONGERON SPLICE DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A CRACKED LONGERON SPLICE BETWEEN STATION 600 AND 620 AT LONGERON 31 LEFT. REPLACED LONGERON SPLICE PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001212006062600121WP 2006 6 26 IXXA060221S 120040611A57305656352504 FILLET DOUG DC8 DC862F 3021972WP WING DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 162V DELAMINATED. REPAIRED PANEL PER COOPESA EO COO-CMP-8-53-273-04 DATED 07/15/2004. 2L74 4F 4A25 20060626001252006062600125WP 2006 6 26 IXXA060222S 120040606A5320 INTERCOSTAL DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND CORRODED INTERCOSTAL FROM STATION Y702.75 TO Y717.75 AT LONGERON 20 LEFT. REPLACED INTERCOSTAL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001272006062600127WP 2006 6 26 IXXA060223S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLE AT STATION 822.5 LONGERON 14 LEFT. REPAIRED FRAME PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001342006062600134WP 2006 6 26 IXXA060224S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION 864.5 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001402006062600140WP 2006 6 26 IXXA060226S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 880 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001442006062600144WP 2006 6 26 IXXA060243S 120040607A5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOOR SUPPORTS CORRODED AT STATION Y1540, X40 AND -X40 AT Z0. REPLACED FLOOR SUPPORTS PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001482006062600148WP 2006 6 26 IXXA060246S 120040608A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A FRAME WITH A DOUBLE DRILLED HOLE AT STATION 460 LONGERON 21 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001512006062600151WP 2006 6 26 IXXA060247S 120040608A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND SEAT TRACK CORRODED FROM STATION 1270 TO STATION 1420 AT +X40, Z=0. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001662006062600166WP 2006 6 26 IXXA060231S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1060 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001702006062600170WP 2006 6 26 IXXA060248S 120040609A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP FUSELAGE DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A SEAT TRACK WITH AN ELONGATED HOLE AT STATION 827.5 X=0, Z=0. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001712006062600171WP 2006 6 26 IXXA060249S 120040609A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP FUSELAGE WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND SEAT TRACK WORN OUT OF LIMITS BETWEEN STATION Y717 TO Y742 AT -X25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001722006062600172WP 2006 6 26 IXXA060250S 120040610A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND SKIN CRACKED AND SHEARED FASTENERS AT STATION Y1589 BETWEEN LONGERONS 15 LEFT AND 17 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001732006062600173WP 2006 6 26 IXXA060251S 120040609A5347 SEAT TRACK DOUG DC8 DC862F 3021972WP FUSELAGE WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 76460 DURING ROUTINE C CHECK FOUND A SEAT TRACK WORN OUT OF LIMITS BETWEEN STATIONS Y400 AND Y420 AT -X45. REPLACED SEAT TRACK PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001752006062600175WP 2006 6 26 IXXA060253S 120040611A5321 FLOOR PANEL DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED, WITH LOOSE RIVETS AND A DOUBLE HOLE. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001762006062600176WP 2006 6 26 IXXA060254S 120040611A5321 FLOOR PANEL DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED AND LOOSE FASTENERS BETWEEN STATION Y1520 AND Y1542 AND BETWEEN -X40 AND +X40. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001772006062600177WP 2006 6 26 IXXA060255S 120040611A5321 FLOOR PANEL DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOOR PANEL CORRODED BETWEEN STATIONS Y1542 AND Y1580 AT -X40 AND +X40. REPLACED FLOOR PANEL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001792006062600179WP 2006 6 26 IXXA060314S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE272 TO XE312.5 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001812006062600181WP 2006 6 26 IXXA060316S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE221 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001822006062600182WP 2006 6 26 IXXA060317S 120040605A5312 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE149 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001832006062600183WP 2006 6 26 IXXA060318S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE28.843 TO XE77 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001842006062600184WP 2006 6 26 IXXA060320S 120040608A5512 SKIN DOUG DC8 DC862F 3021972WP HORIZ STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE CORRODED FROM STATION XFS60 TO XFS142. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001862006062600186WP 2006 6 26 IXXA060263S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y420 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626001882006062600188WP 2006 6 26 IXXA060265S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y560 AT LONGERON 14 RIGHT. REPAIRED PER ALL PPLICABLE DATA 2L74 4F 4A25 20060626001892006062600189WP 2006 6 26 IXXA060266S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y600 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626001902006062600190WP 2006 6 26 IXXA060267S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y660 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001912006062600191WP 2006 6 26 IXXA060268S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y500 AT LONGERON 14 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626001922006062600192WP 2006 6 26 IXXA060269S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y781 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626001932006062600193WP 2006 6 26 IXXA060270S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y834 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060622003602006062200360WP 2006 6 22 IXXA060324S 120040611A5320 ANGLE DOUG DC8 DC862F 3021972WP ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED IN THE LEFT SIDE NOSE LANDING GEAR TUNNEL AT STATION Y102. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060622003622006062200362WP 2006 6 22 IXXA060323S 120040617A5530 ANGLE DOUG DC8 DC862F 3021972WP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT SIDE VERTICAL STABILIZER TO FUSELAGE SKIN ATTACH ANGLE CORRODED AT STATION Y1606. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623000902006062300090WP 2006 6 23 IXXA060353S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y759 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623000912006062300091WP 2006 6 23 IXXA060354S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW115311 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y789 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001062006062300106WP 2006 6 23 IXXA060360S 120040605A5514 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001102006062300110WP 2006 6 23 IXXA060327S 120040615A5313 LONGERON DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A CORRODED LONGERON AT STATION Y267 LONGERON 22 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001162006062300116WP 2006 6 23 IXXA060333S 120040614A5320 ANGLE DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND ANGLE CORRODED AT STATION Y190 LONGERON 33 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001172006062300117WP 2006 6 23 IXXA060334S 120040613A5313 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LONGERON 27 RIGHT END FITTING CORRODED AT STATION Y270. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001612006062300161WP 2006 6 23 IXXA060365S 120040616A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED AND RIVET SHEARED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623002372006062300237WP 2006 6 23 IXXA060373S 120040617A5514 HOUSING DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER LINKAGE HOUSING CRACKED AT STATION XRS218. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000312006062600031WP 2006 6 26 IXXA060198S 120040608A5347 CARGO TRACK DOUG DC8 DC862F 3021972WP CARGO BAY CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND TRACK CORRODED FROM STATION Y990 TO Y1020 AT TX45 TO Z 0. REPLACED DAMAGED TRACK PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000952006062600095WP 2006 6 26 IXXA060210S 120040609A5315 FLOORBEAM DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FLOORBEAM UPPER FLANGE CRACKED AT STATION 380, +X32. REPAIRED PER COOPESA EO COO-8-53-245-04 DATED 6/10/04. 2L74 4F 4A25 20060626000982006062600098WP 2006 6 26 IXXA060212S 120040608A5312 SUPPORT DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT WHEEL WELL FORWARD BULKHEAD SUPPORT CORRODED AT STATION 857, +X56 AND -Z25. REPLACED SUPPORT PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001602006062600160WP 2006 6 26 IXXA060228S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 940 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001672006062600167WP 2006 6 26 IXXA060232S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 1120 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001682006062600168WP 2006 6 26 IXXA060233S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 822.5 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001742006062600174WP 2006 6 26 IXXA060252S 120040610A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND SKIN CRACKED AT STATION 215 BETWEEN LONGERONS 15 LEFT AND 16 LEFT, (FORWARD ENTRANCE DOOR HOLD OPEN PIN CUTOUT). REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001852006062600185WP 2006 6 26 IXXA060322S 120040610A5531 SPAR DOUG DC8 DC862F 3021972WP VERTICAL STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND VERTICAL STABILIZER RIGHT SIDE REAR SPAR INTERNAL AREA CORRODED AT STATION ZV299. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001972006062600197WP 2006 6 26 IXXA060256S 120040611A5320 FITTING DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A FITTING WITH A DOUBLE HOLE AT STATION 1740 BETWEEN LONGERONS 10 LEFT AND 11 LEFT. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001982006062600198WP 2006 6 26 IXXA060257S 120040613A5313 LONGERON DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A CRACKED LONGERON FROM STATION Y1580 TO Y1586 AT LONGERON 15 LEFT. REPAIRED LONGERON PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626002032006062600203WP 2006 6 26 IXXA060259S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLES AT STATION 600 AT LONGERONS 7 LEFT AND 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626002062006062600206WP 2006 6 26 IXXA060260S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND DOUBLE DRILLED HOLE IN FRAME FLANGE AT STATION 640, LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626002072006062600207WP 2006 6 26 IXXA060261S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y834 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626002082006062600208WP 2006 6 26 IXXA060262S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1120 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623000982006062300098WP 2006 6 23 IXXA060357S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y380 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001072006062300107WP 2006 6 23 IXXA060361S 120040605A5514 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE149 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001312006062300131WP 2006 6 23 IXXA060192S 120041004A5320 GUIDE DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129523 DURING ROUTINE C CHECK, FOUND ROLLER GUIDE DOOR ANGLE CRACKED AT STATION Y500, LONGERON 29 RIGHT. REPLACED ROLLER GUIDE PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001662006062300166WP 2006 6 23 IXXA060367S 120040616A5514 DOUBLER DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND DOUBLER BULGING AND CRACKED ON LEFT HAND HORIZONTAL STABILIZER AT STATION XRS250. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001722006062300172WP 2006 6 23 IXXA060368S 120040616A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE221 TO XE149 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623001792006062300179WP 2006 6 23 IXXA060371S 120040617A5514 SUPPORT DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LOWER SECTION SUPPORT CRACKED AT STATION XFS47. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623002342006062300234WP 2006 6 23 IXXA060363S 120040610A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANELS AT STATIONS ZR267.218, ZR276.531, AND ZR284.75 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060623002352006062300235WP 2006 6 23 IXXA060364S 120040616A5514 CAP DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER STATION XRS54 TEE CAP CRACKED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001072006062600107WP 2006 6 26 IXXA060216S 120040610A5310 DOOR FRAME DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FORWARD CARGO COMPARTMENT DOOR FRAME CRACKED AT THE UPPER AFT CORNER. REPAIRED DOOR FRAME PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001162006062600116WP 2006 6 26 IXXA060218S 120040609A5730 FILLET DOUG DC8 DC862F 3021972WP WING DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262F DELAMINATED AND CORRODED AT AFT FACE. REPLACED PANEL PER COOPESA EO NUMBER COO-8-53-304-04 DATED 08/06/2004. 2L74 4F 4A25 20060626001532006062600153WP 2006 6 26 IXXA060214S 120040609A5330 SKIN DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND SKIN BULGED AND CRACKED FROM STATION 1460 TO STATION 1480 BETWEEN LONGERONS 31 RIGHT AND 33 RIGHT. REPAIRED PER COOPESA EO COO-8-53-244-04 DATED 6/8/04. 2L74 4F 4A25 20060626001582006062600158WP 2006 6 26 IXXA060227S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 900 TO 902 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001652006062600165WP 2006 6 26 IXXA060229S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 960 LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001692006062600169WP 2006 6 26 IXXA060234S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 920 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001782006062600178WP 2006 6 26 IXXA060313S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE LOWER PANEL BETWEEN STATION XE77 TO XE28.843 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001802006062600180WP 2006 6 26 IXXA060315S 120040605A5512 PANEL DOUG DC8 DC862F 3021972WP HORIZ STAB BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER PANEL BETWEEN STATION XE221 TO XE272 BULGED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001872006062600187WP 2006 6 26 IXXA060264S 120040616A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y500 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060626000282006062600028WP 2006 6 26 IXXA060376S 120040617A5514 SUPPORT FITTING DOUG DC8 DC862F 3021972WP HORIZ STAB CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT HAND HORIZONTAL STABILIZER SUPPORT FITTING CRACKED AT STATION XFS72 BETWEEN STRINGERS 6 AND 7. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626000872006062600087WP 2006 6 26 IXXA060209S 120040609A5315 FLOORBEAM DOUG DC8 DC862F 3021972WP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND CRACKED FLOORBEAM AT STATION Y360 AT +X28 AND +X32. REPAIRED PER COOPESA EO COO-8-53-264-04 DATED 6/15/04. 2L74 4F 4A25 20060626001202006062600120WP 2006 6 26 IXXA060220S 120040609A57305710369 FILLET DOUG DC8 DC862F 3021972WP WING DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262K DELAMINATED AND CORRODED. REPLACED PANEL PER COOPESA EO COO-8-53-304-04. 2L74 4F 4A25 20060626001372006062600137WP 2006 6 26 IXXA060225S 120040606A5311 FRAME DOUG DC8 DC862F 3021972WP FUSELAGE MISDRILLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 857.1 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060626001992006062600199WP 2006 6 26 IXXA060258S 120040701A5310 WINDOW FRAME DOUG DC8 DC862F 3021972WP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND WINDOW CUT OUT FRAME CORRODED FROM STATION Y1400 TO STATION Y1420 RIGHT HAND SIDE. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000752006071300075WP 2006 7 13 IXXA060379S 120040618A5522 SKIN DOUG DC8 DC862 3021970WP LT ELEVATOR BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN TRAILING EDGE BULGED FROM STATION XE246 TO XE318. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000762006071300076WP 2006 7 13 IXXA060381S 120040618A5522 SKIN DOUG DC8 DC862 3021970WP LT ELEVATOR CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN INTERNAL "TEE" AND SKIN CORRODED AT STATION XE40. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000862006071300086WP 2006 7 13 IXXA060432S 120040609A5730 SKIN DOUG DC8 DC862 3021970WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD SLOT AREA UPPER SURFACE SKIN CORRODED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000872006071300087WP 2006 7 13 IXXA060433S 120040611A5712 RIB DOUG DC8 DC862 3021970WP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE RIB CRACKED AT STATION XW36. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000882006071300088WP 2006 7 13 IXXA060434S 120040611A5730 PANEL DOUG DC8 DC862 3021970WP ZONE 600 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE FIXED PANEL DELAMINATED AND NICKED AT STATIONS XW10, XW40, AND XW75. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000892006071300089WP 2006 7 13 IXXA060435S 120040824A5753 ANGLE DOUG DC8 DC862 3021970WP TE FLAP WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING ANGLE WORN AT STATION XF218. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000902006071300090WP 2006 7 13 IXXA060437S 120040611A5753 SKIN DOUG DC8 DC862 3021970WP TE FLAP DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000912006071300091WP 2006 7 13 IXXA060438S 120040615A5740 FITTING DOUG DC8 DC862 3021970WP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND NUMBER 4 MAIN FUEL TANK FITTING CRACKED AT STATION 239.793 BETWEEN FRONT SPAR AND STRINGER 18. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000922006071300092WP 2006 7 13 IXXA060439S 120040617A5753 STRAP DOUG DC8 DC862 3021970WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LEADING EDGE STRAP CORRODED AND WORN. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000952006071300095WP 2006 7 13 IXXA060443S 120040702A5753 FITTING DOUG DC8 DC862 3021970WP TE FLAP CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING FLAP HINGE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000962006071300096WP 2006 7 13 IXXA060444S 120040705A5700 FITTING DOUG DC8 DC862 3021970WP TE FLAPS CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000972006071300097WP 2006 7 13 IXXA060445S 120040605A5753 FITTING DOUG DC8 DC862 3021970WP TE FLAPS CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602944 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF340. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060714000112006071400011WP 2006 7 14 IXXA060418S 120040820A5753 FITTING DOUG DC8 DC862 3021970WP TE FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING IN BOARD FLAP FITTING CRACKED AT STATION XW97. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000132006071400013WP 2006 7 14 IXXA060420S 120040901A5751 DOUBLER DOUG DC8 DC862 3021970WP XONE 500 MISINSTALLED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON REPAIR SHORT ONE RIVET FROM STATION XA661 TO XA671. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000162006071400016WP 2006 7 14 IXXA060423S 120040607A5740 ANGLE DOUG DC8 DC862 3021970WP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TEE ANGLE CRACKED AT STATION XRS162. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000192006071400019WP 2006 7 14 IXXA060426S 120040608A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATION XW250. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000302006071400030WP 2006 7 14 IXXA060429S 120040609A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING UPPER IN BOARD PANEL (DIHEDRAL) SKIN, CORRODED. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000362006071400036WP 2006 7 14 IXXA060430S 120040609A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED FROM STATION XW257 TO XW260. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000412006071400041WP 2006 7 14 IXXA060448S 120040629A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 600 WORN A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING SKIN WORN AT STATION XOLDO67. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000422006071400042WP 2006 7 14 IXXA060449S 120040604A5512 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 SCRATCHED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SKIN SCRATCHED AT STATION XFS139.250. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000742006071300074WP 2006 7 13 IXXA060378S 120040618A5522 SKIN DOUG DC8 DC862 3021970WP RT ELEVATOR DEBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SKIN SURFACE CORRODED AND DEBONDED AT STATION XE205.687. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000932006071300093WP 2006 7 13 IXXA060440S 120040629A5730 SKIN DOUG DC8 DC862 3021970WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 76460 DURING ROUTINE C CHECK, FOUND RIGHT WING SKIN CORRODED AT STATION XOLDI6.224. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000122006071400012WP 2006 7 14 IXXA060419S 120040916A5730 PANEL DOUG DC8 DC862 3021970WP ZONE 500 DELAMINATED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE DIHEDRAL PANEL DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000172006071400017WP 2006 7 14 IXXA060424S 120040607A5730 SKIN DOUG DC8 DC862 3021970WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE LOWER SKIN CORRODED FROM STATION XFS735 TO XFS885. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000202006071400020WP 2006 7 14 IXXA060427S 120040608A5712 RIB DOUG DC8 DC862F 3021972WP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE CAVITY LOWER RIB CORRODED AND CRACKED AT STATION XFS360.25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000392006071400039WP 2006 7 14 IXXA060446S 120040705A5753 FITTING DOUG DC8 DC862F 3021972WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATA 2L74 4F 4A25 20060714000932006071400093WP 2006 7 14 IXXA060392S 120040726A5522 WEB DOUG DC8 DC862F 3021972WP ZONE 300 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR WEB CRACKED AT STATION XE77. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000942006071400094WP 2006 7 14 IXXA060395S 120040610A5753 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP UPPER SKIN DENTED AT STATION XF440. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000952006071400095WP 2006 7 14 IXXA060401S 120040611A5753 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XW58. REPAIRED SKIN PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000962006071400096WP 2006 7 14 IXXA060403S 120040628A5754 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW454 AND XW485. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000972006071400097WP 2006 7 14 IXXA060404S 120040628A5754 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW257 AND XW408. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000982006071400098WP 2006 7 14 IXXA060408S 120040702A5740 FITTING DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 7660 2994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING FLAP HINGE BASE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000992006071400099WP 2006 7 14 IXXA060409S 120040703A5712 RIB DOUG DC8 DC862F 3021972WP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS384. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714001052006071400105WP 2006 7 14 IXXA060396S 120040610A5712 RIB DOUG DC8 DC862F 3021972WP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS780. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714001062006071400106WP 2006 7 14 IXXA060397S 120040610A5712 RIB DOUG DC8 DC862F 3021972WP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS842. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714001092006071400109WP 2006 7 14 IXXA060400S 120040611A5753 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP TRAILING EDGE SKIN DENTED FROM STATION XRS172 TO XRS220. REPLACED SKIN PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000282006071300028WP 2006 7 13 IXXA060417S 120040730A5730 SKIN DOUG DC8 DC862 3021970WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED AT STATION XFS61. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000852006071300085WP 2006 7 13 IXXA060431S 120040609A5730 SKIN DOUG DC8 DC862 3021970WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS335.25. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060713000942006071300094WP 2006 7 13 IXXA060441S 120040702A5753 SKIN DOUG DC8 DC862 3021970WP TE FLAPS CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP TRAILING EDGE SKIN CRACKED AT STATION XF300. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000212006071400021WP 2006 7 14 IXXA060428S 120040609A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATIONS XFS -11.250 THRU XFS63.750. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000402006071400040WP 2006 7 14 IXXA060447S 120040715A5712 RIB DOUG DC8 DC862F 3021972WP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING AUXILIARY TANK RIB CRACKED AT STATION XFS20. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714001082006071400108WP 2006 7 14 IXXA060399S 120040611A5751 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON UPPER SKIN DENTED AT STATION XW671. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001562006071700156WP 2006 7 17 IXXA060380S 120040618A5522 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR LOWER SKIN CRACKED AND CORRODED FROM STATION XE137 TO XE181. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001572006071700157WP 2006 7 17 IXXA060405S 120040628A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING UPPER SKIN CORRODED BETWEEN STATION XW0 AND XRS74. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001582006071700158WP 2006 7 17 IXXA060406S 120040629A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATION XW257 AND XW223. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001592006071700159WP 2006 7 17 IXXA060407S 120040629A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE LOWER SKIN CORRODED BETWEEN STATION XFS710 AND XFS635. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717002002006071700200WP 2006 7 17 IXXA060410S 120040705A5740 FITTING DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUT BOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717002012006071700201WP 2006 7 17 IXXA060411S 120040705A5753 FITTING DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XT340. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717002022006071700202WP 2006 7 17 IXXA060412S 120040705A5753 FITTING DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000142006071400014WP 2006 7 14 IXXA060421S 120040605A5730 PANEL DOUG DC8 DC862 3021970WP ZONE 600 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE LOWER PANEL CORRODED AROUND SCREWS AT STATION XRS169. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000152006071400015WP 2006 7 14 IXXA060422S 120040605A5751 SKIN DOUG DC8 DC862 3021970WP ZONE 600 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD AILERON LOWER SKIN DENTED AND SCRATCHED AT STATION XA524. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000182006071400018WP 2006 7 14 IXXA060425S 120040607A5712 RIB DOUG DC8 DC862F 3021972WP ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS773. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714000922006071400092WP 2006 7 14 IXXA060390S 120040704A5542 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 BENT A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT SIDE RUDDER SKIN BENT FROM STATION ZR208 TO ZR239. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714001102006071400110WP 2006 7 14 IXXA060402S 120040618A5740 FITTING DOUG DC8 DC862F 3021972WP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING RIGHT CENTER FUEL TANK FITTING PLATE CRACKED AT STATION XWC23 BETWEEN STRINGERS 1 AND 2. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001642006071700164WP 2006 7 17 IXXA060383S 120040619A5522 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 BULGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR TRAILING EDGE UPPER AND LOWER SKIN BULGED FROM STATION XE263 TO XE280. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001652006071700165WP 2006 7 17 IXXA060384S 120040621A5514 FITTING DOUG DC8 DC862F 3021972WP ZONE 300 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER SUPPORT FITTING CRACKED AT STATION XFS72 BETWEEN STRINGER 2 AND FRONT SPAR. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001662006071700166WP 2006 7 17 IXXA060385S 120040622A5514 BUSHING DOUG DC8 DC862F 3021972WP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR SUPPORT BUSHING CORRODED AT STATION XE 140. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001672006071700167WP 2006 7 17 IXXA060386S 120040624A5522 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SURFACE SKIN CORRODED AT STATION XE32.398. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001682006071700168WP 2006 7 17 IXXA060387S 120040616A5521 SPAR CAP DOUG DC8 DC862F 3021972WP ZONE 300 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RIGHT ELEVATOR LOWER SPAR CAP CORRODED FROM STATION XE32 TO XE285. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060714001072006071400107WP 2006 7 14 IXXA060398S 120040611A5751 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 TOOL DAMAGE A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND A DOUBLE HOLE IN THE LEFT WING OUTBOARD AILERON AT STATION XW698. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001272006071700127WP 2006 7 17 IXXA060413S 120040705A5753 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 DEBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP SKIN DEBONDED AT STATION XW115. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001282006071700128WP 2006 7 17 IXXA060414S 120040710A5751 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 DENTED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON SKIN DENTED FROM STATION XA646 TO XA674. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001292006071700129WP 2006 7 17 IXXA060415S 120040721A5753 FITTING DOUG DC8 DC862F 3021972WP ZONE 500 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP TRAILING EDGE PANEL FITTING CRACKED AT STATION XW375. REPLACED FITTING PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001302006071700130WP 2006 7 17 IXXA060416S 120040721A5730 SKIN DOUG DC8 DC862F 3021972WP ZONE 500 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATIONS XRS710 TO XRS761. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001692006071700169WP 2006 7 17 IXXA060388S 120040704A5542 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 DEBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RUDDER SKIN DEBONDED AND CORRODED FROM STATION ZR150 TO ZR115. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001702006071700170WP 2006 7 17 IXXA060389S 120040702A5542 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 DEBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RUDDER SKIN DEBONDED AND CORRODED FROM STATION ZR59 TO ZR115. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001712006071700171WP 2006 7 17 IXXA060391S 120040707A5542 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 DEBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND RUDDER RIGHT SIDE SKIN DEBONDED AND A LOOSE RIVET FROM STATION ZR59 TO ZR87. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001722006071700172WP 2006 7 17 IXXA060393S 120040721A5551 FITTING DOUG DC8 DC862F 3021972WP ZONE 300 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER FITTING CRACKED AT STATION XFS47 BETWEEN STRINGERS 1 AND 2. REPLACED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060717001732006071700173WP 2006 7 17 IXXA060394S 120040802A5522 SKIN DOUG DC8 DC862F 3021972WP ZONE 300 DEBONDED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK, FOUND LEFT ELEVATOR UPPER SKIN TRAILING EDGE DEBONDED AND CORRODED FROM STATION XE260 TO XE280. REPAIRED PER ALL APPLICABLE DATA. 2L74 4F 4A25 20060724000142006072400014WP 2006 7 24 IXXA0400040S 120040316A5312 BULKHEAD DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11603AL919102910 46003 DURING ROUTINE C-CHECK INSPECTION, LT FUSELAGE AFT PRESSURE BULKHEAD STRUCTURE HAS CRACK. REPAIR ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW SRM 53-2-5 FIG 9, AT STA. XW 130.00, IAW SRM 51-1-20D PAGE 21 PERFORMED CRACK END, SRM 53-2-5 PAGE 15-16 AND PERFORMED HEAT TREATMENT 53-2-5 FIG. 9 SRM 51-1-1 PAGE 1, 13, 17, CLEANED, TREATED, AND PRIMED AREA AND DOUBLER, INSTALLED DOUBLER IAW SRM 51-1-8B, IAW SRM 53-2-5 PAGES 15, 16 SRM 51-2-20. 2L74 4F RT4A25 20060724002032006072400203WP 2006 7 24 IXXA060382S 120040619A5522 SKIN DOUG DC8 DC862F 3021972WP LT ELEVATOR CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW1141CX 764602994 46129 DURING ROUTINE C CHECK FOUND LEFT ELEVATOR INTERNAL FINGER DOUBLER AND SKIN CORRODED AT STATION XE38. REPAIRED PER ALL APPROVED DATA. 2L74 4F 4A25 20070328001792007032800179NM 2007 3 28 AT0700072 120040627A5753 SKIN BOEING717 717200 1383700NM T/E FLAP DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15717JL 55042 LEFT FLAP DAMAGE DUE TO FOD. INSTALLED TWO DOUBLER REPAIR AT LEFT INBOARD AREA IAW AIRTRAN RES 06-05-19. MATERIAL USED 0.063 7075T6. SIZE 7" X 7.5" AND 6" X 8". 2L72 4F TRA6WE 20070330001262007033000126NM 2007 3 30 QXEA200700367 120040312A5100 UNKNOWN BOMBDRDHC8 DHC8402 1390042NM CONTROL WHEEL UNKNOWN A QXEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM09424QX 4006 PDX FLIGHT NR 2325: AFTER CONTROL WHEEL CHECK, WHEEL TILTED 25 DEGREES TO THE RIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED LEFT AND RIGHT AILERONS. NO DEFECTS NOTED. C/W TRAVEL OPS CHECK OF AILERON TRIM. CHECKS GOOD. C/W OPS TEST OF AILERON CONTROL SYSTEM IAW TASK 27-10-00-710-801. NO DEFECTS NOTED. CONTROL WHEEL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20070406001152007040600115NM 2007 4 6 AT0700086 120040606A5330 SKIN BOEING717 717200 1383700NM BS 229 S18L DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15963AT 55024 DENT FOUND AT FS 229 AND STRINGER L-18 ON LT SIDE OF FUSELAGE JUST AFT OF L-1 DOOR - 2 INCH WIDE BY 4.35 INCHES LONG MAX DEPTH OF DENT .091. INSTALLED DOUBLER REPAIR AT STA 229 TO STA 245.5 BETWEEN L-16 TO L-18 IAW B717 STM 53-00-01 REPAIR 6. MATERIAL USED FILLER 2024 T3 .050 SIZE 16.75" X 14.125". DOULBER 2024 T3.063, 23.5" X 4", FINGER DOUBLER 2024T3.063 32.5" X 5.75". 2L72 4F TRA6WE 20070406001102007040600110NM 2007 4 6 AT0700031 120040327A5101 STRUCTURE BOEING717 717200 1383700NM FS 207 GROUND DAMAGE A ZZDAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO15980AT 55039 CATERING TRUCK STRUCK AIRCRAFT ON RIGHT SIDE NEAR R-1 DOOR. INSTALLED REPAIR CLASS 3 PAGE 219-226 LONGERON 19R-20R STA 210-200 AS PER B717 SRM 53-00-01 AND RES 04-0289 WO 24177 AND N/R 3052 AVBORNE. 2L72 4F TRA6WE 20070412001252007041200125NM 2007 4 12 AT0700032 120041110A5330 SKIN BOEING717 717200 1383700NM BS 329 - 342 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15966AT 55027 ON POST FLIGHT FOUND SMALL DENT ON RIGHT SIDE OF A/C FWD OF FWD CARGO PIT. INSTALLED PERMANENT REPAIR ON RIGHT FUSELAGE AT STA 329 TO 342.5 BETWEEN L-19R TO 21R PER B717 SRM 53-00-01. 2L72 4F TRA6WE 20070412001662007041200166NM 2007 4 12 AT0700139 120040901A5330 SKIN BOEING717 717200 1383700NM FS 408 DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15943AT 55006 DENT LOCATED FS 408 AND RT L16 MEASURES A 1.5 INCH IN DIA BY .045 DEEP, PER SRM 53-00-01 COND 3 MUST BE REPAIRED WITHIN 4500 FLT HOURS. INSTALLED DOUBLER REPAIR ON FUSELAGE SKIN RT BETWEEN STA 414.5 TO 422 AND BETWEEN L-16R TO 18R IAW B717 SRM 53-00-01 FIG 201. SIZE OF REPAIR 7.5 X 8.0 INCHES. 2L72 4F TRA6WE 20070417002842007041700284NM 2007 4 17 AT0700073 120040606A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15963AT 55024 DENT FOUND AT FS 229 AND STRINGER L-18 ON LT SIDE OF FUSELAGE JUST AFT OF L-1 DOOR - 2 INCH WIDE BY 4.35 INCHES LONG MAX DEPTH OF DENT .091. INSTALLED DOUBLER REPAIR AT STA 229 TO STA 245.5 BETWEEN L-16 TO L-18 IAW B717 SRM 53-00-01 REP 6. MATERIAL USED FILLER 2024 T3 .050 SIZE 16.75" X 14.125". DOUBLER 2024 T3.063 23.5" X 4", FINGER DOUBLER 2024T3.063 32.5" X 5.75". 2L72 4F TRA6WE 20070426000822007042600082NM 2007 4 26 AT0700037 120041026A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15961AT 55023 A/C HAS DENT ON AFT SIDE OF L1 DOOR DUE TO HARD CONTACT JET WAY DRIVER. INSTALLED FLUSH REPAIR AT STA 229 TO STA 244 BETWEEN LONG 16 TO 18L IAW B717 SRM 53-00-01 FIG 201. MATERIAL USED FINGERS DOUBLERS 2024T3.025, DOUBLERS 2024T3 .063 FILLER 2024T3.050 AND STRAP 2024T3.63. 2L72 4F TRA6WE 20070426000842007042600084NM 2007 4 26 AT0700053 120040823A5330 SKIN BOEING717 717200 1383700NM FUSELAGE DENTED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15994AT 55138 A/C HAS DENT LOCATED AFT OF L-1 DOOR AT APPROX STA 235, 8 INCHES ABOVE CUSP LINE .5 L X .75 W X .018 DEEP. INSTALLED DOUBLER REPAIR AT AFT OF L-1 DOOR STA 235 AS PER B717 SRM 53-00-01. MATERIAL USED 2024 T3.032, 6.25 X 5.75 INCHES. 2L72 4F TRA6WE 20090202 NM 2009 2 2 DLM88090079 120040911A5330 SKIN DOUG MD88 MD88 3023688NM BS 474 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27966DL 53115 LIGHTNING STRIKE DAMAGE JUST FORWARD OF THE RIGHT ALTERNATE STATIC PORT. REPAIRED IAW ERA 093374-14, C/W ERA 093374-14. 2L72 4F RTA6WE 20040419001862004041900186 2004 4 19 SWAA041017 420040408A25656557463 FITTING GIRT BAR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29 DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE FWD GIRT BAR FLOOR FITTING CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE FWD FITTING PER MM. 20050822000892005082200089 2005 8 22 GYN2005F00000 120041104A51002J47 AIR FILTER MISMANUFACTURED E GYNAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 SW13 MFG SWITCHED FROM PN 1J47 TO PN 2J47. THE PROBLEM IS THAT THE NEW STYLE FILTER IS SMALLER IN DIAMETER THAN THE OLD STYLE FILTER, AND WE HAVE NOT BEEN ABLE TO PURCHASE A (DG-47) ADEL CLAMP FROM ANY OF OUR SUPPLIERS. AS NOW, WE HAVE TO RESORT TO REDRILLING THE SCREW HOLE AND TRIMMING THE END OFF. (K) 20040521001322004052100132 2004 5 21 BI0001 420040504A2565C19347101 LINK ESCAPE SLIDE DEPLOYED B O OTHER O OTHER NRNOT REPORTED 1 WP05 UPON OPENING SLIDE FOR RECEIVING INSPECTION, IT WAS DISCOVERED THAT ALL THE FRANGIBLE LINKS HAD BEEN DEPLOYED PREVIOUSLY, THEN TIED TOGETHER WITH BREAK AWAY THREAD. THERE IS NO PROCEDURE IN THE CMM FOR THIS TYPE OF REPAIR. THE FRANGIBLE LINKS SHOULD HAVE BEEN REPLACED. 20041129002002004112900200WP 2004 11 29 OEJ2004F00001 220040610A7200TFE7315 ENGINE GARRTTTFE731TFE7315BR WP NR 1 SHUTDOWN E OEJAO OTHER YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 SW15632FW 258294 P107139 AIRCRAFT DEPARTED, ON INBOUND, NR 1 SHUT DOWN. AIRRAFT LANDED WITHOUT ANY INCIDENTS. THE NR 1 ENGINE IS BEING REMOVED AND SENT TO MFG FOR EVALUATION. (SW15200410963) 4 F E6WE 20050202001542005020200154GL 2005 2 2 ERAA097089 220040726A7200 ENGINE ALLSN 250C 250C20B 03013GL MAKING METAL B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 8874 CAE833014 ENGINE MAKING METAL. REPAIRED ENGINE, CHANGED BEARING AND INNER RACE. 3 U E4CE 20050223000942005022300094GL 2005 2 23 ERAA097508 220040724A7200 ENGINE ALLSN 250C 250C20B 03013GL MAKING METAL E ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03 8653 CAE835475 ENGINE MAKING METAL. INSTALLED SERVICEABLE GEARBOX AND COMPRESSOR, C/W CEB-A-1392, C/W E CHECK INSPECTION. 3 U E4CE 20040227000812004022700081 2004 2 27 9999V012604 420040125A34147002860903 INDICATOR AIRSPEED FAILED E UVCAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE039999V 22 CO-PILOTS AIRSPEED/ MACH INDICATOR FAILED AND FLAGGED PRIOR TO TAKEOFF. FLIGHT WAS CANCELLED. 20050107001162005010700116 2005 1 7 BB04090 420041119A2565101630305 SLIDE CABIN LEAKING A USAAK NONE O OTHER ININSP/MAINT 1 EA19 A LEFT OVERWING SLIDE FOR A 767 WAS GIVEN A RETENTION TEST. THE TEST FAILED. THE SLIDE WAS RETURNED TO THE VENDOR. FURTHER ACTION PENDING. 20041119000912004111900091GL 2004 11 19 ALG2004F00049 220040819A7314 PUMP ALLSN 250C 250C28B 03013GL FUEL SYSTEM FAILED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW031075Y 45378 CAE860763 WHILE AT A HOVER, MANEUVERING FOR TAKE OFF, NOTICED N2 DROPPED AND STABILIZED BELOW THE RED LINE AND DID NOT RECOVER UNTIL LANDED. REMOVED AND REPLACED STARTER GENERATOR, DID NOT FIX THE PROBLEM. REMOVED ALL ENGINE AIR LINES AND INSPECTED FOR CRACKS AND LEAKS, REINSTALLED AIRLINES AND COMPLIED WITH A PNEUMATIC LEAK CHECK, NO DEFECTS NOTED. REMOVED AND REPLACED ACCUMULATOR DOUBLE CHECK VALVE, REMOVED AND REPLACED FUEL PUMP AND COMPLIED WITH A COMPENSATOR RIGGING CHECK, RIGGED TO A NORMAL SETTING IAW MM. AIRCRAFT GROUND RAN, LEAK AND OPS CHECKED GOOD. FLIGHT CHECK PERFORMED AND CHECKED GOOD. 3 U E1GL 20040223001912004022300191 2004 2 23 ANCF200400001 420040109A344320412170415 TRANSCEIVER RADAR FAILED W ANCFA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO23506NA WXR FAIL DISPLAYED ON HSI WXR TEST DISPLAY WXR FAIL RT. THE TRANSCEIVER RADAR WAS CHANGED IAW-AMM 34-43-01 PAG 401, TEST OK. P/N-OFF/ON-2041217-0415,S/N-OFF-2274, S/N-ON-6464. 20040401001312004040100131NE 2004 4 1 RYN2004F00001 220040221A7200V2527EA5 ENGINE IAE V2527 V2527EA5 NE RIGHT MALFUNCTIONED A RYNAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 CE07951LF 460 ON TAKEOFF, THERE WAS A LOUD BANG AND ECAM WARNING INDICATED EGT OVERTEMP ON NR 2 ENGINE. ECAM PROCEDURES FOLLOWED AND EMERGENCY DECLARED. AIRCAFT RETURNED, AND LANDED WITHOUT INCIDENT. 4 F E40NE 20050422000252005042200025NE 2005 4 22 2005UALA00159 220040211A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 FLUCTUATES A UALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29547UA 25368 726527 DIVERTED TO HNL DUE TO NR 2 ENGINE POWER FLUCTUATION. AS A PRECAUTIONARY MEASURE BOROSCOPED ENGINE TO CHECK COMPRESSOR HEALTH, RECHECKED CHIP DETECTORS AND OIL FILTER. ALSO REPLACED 10TH STAGE CHECK VALVE. 2L72 4F4 FRTA2NM E17NE 20040122000142004012200014WP 2004 1 22 DHL2004802001 120040104A2821ACB006F2474Y3 FUEL FILTER DOUG DC8 DC873 302199CWP GE CFM56 CFM562C1 13802NE NR 4 ENGINE CONTAMINATED A DHLAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO01802DH 46076 692512 DURING CRUISE FLIGHT AT FL 350, NR 4 ENGINE FLAMED OUT. SEVERAL ATTEMPTS TO RESTART, THE LAST AT FL 250 AT 300 KIAS WERE UNSUCCESSFUL. REMOVED AND REPLACED NR 4 ENGINE FUEL FILTER DUE TO CONTAMINATION IAW DC-8 M/M 73-11-10. PERFORMED VISUAL INSPECTION OF BOOST PUMP AREA, NO DEBRIS. OPS AND LEAK CHECKED OK. ENGINE RUN PERFORMED IAW JRH. 2L74 4F4 FRT4A25 E2GL 20040202003452004020200345NM 2004 2 2 2004UALA00033 120040113A5753 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT WING TE FLAP GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 LEFT WING INBOARD TRAILING EDGE AFT FLAP IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED AFT FLAP PER SRM 57-53-01 AND TIMCO REO (EVA) G-09637. 2L72 4F4 FRTA2NM E17NE 20040227000742004022700074CE 2004 2 27 BAQA091783 120040122A324050030967 BRAKE ASSY LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP WORN B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 253 092 BRAKE ASSY WORN. REPLACED WITH SERVICABLE UNIT. 01/27/2004 2L72 4F4 F A10CE E6WE 20040301001202004030100120CE 2004 3 1 XVQ2004F00000 120040119A3230131378252899 CHAIN BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA NLG RETRACT SYS MISROUTED E XVQAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO17512KA BB512 LANDING GEAR WOULD NOT EXTEND WHEN LANDING HANDLE SELECTED FOR DOWN. PILOT SUCCESSFULLY EXTENDED GEAR RECEIVING THREE DOWN AND LOCKED INDICATION. UNEVENTFUL LANDING PERFORMED. INSPECTION OF SYSTEM REVEALED THAT THE NLG RETRACT CHAIN WAS IMPROPERLY ROUTED OVER THE IDLER SPROCKET LOCATED FORWARD OF THE CHAIN TENSIONING SPROCKET AND BINDING AGAINST SUPPORT STRINGER. INSPECTED ENTIRE RETRACT SYSTEM, REROUTED AND RIGGED NLG CHAIN. REPLACED NLG ACTUATOR AS PRECAUTION. PERFORMED MLG GEAR RIGGING. OPERATIONAL CHECK FOUND TO BE GOOD. NLG CHAIN INSPECTION AND LUBRICATION HAD BEEN ACCOMPLISHED 200 HOURS PRIOR. RECOMMEND MORE DETAILED DRAWINGS IN MM SHOWING PROPER ROUTING OF NLG RETRACT CHAIN. 1L72 4T3 T A24CE E2NE 20040303001982004030300198EU 2004 3 3 2004UALA00149 120040220A5320 SUPPORT BEAM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29410UA 463 AFT CABIN STRUCTURE SUPPORT BEAM AT FRAME 67 RBL 50 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOOR SUPPORT. 2L72 4F4 FRTA28NM E40NE 20040301001392004030100139WP 2004 3 1 DHL2004806575 120040129A5522 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01806DH84257 46002 LT ELEVATOR UPPER SKIN SURFACE WITH 3.000 CRACK IN STA XE 39.188 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED FASTENERS, TRIMMED OUT CRACKED SKIN, PERFORMED NDT INSPECTION. FABRICATED FILLER AND DOUBLER (2024-T3AL 0.032) CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. REFER TO NR 2429 FOR WEIGHT AND BALANCE. 2L74 4F4 FRT4A25 E2GL 20040301001732004030100173NM 2004 3 1 2004UALA00114 120040210A5315 FLOORBEAM BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 AFT CARGO COMPARTMENT FLOORBEAM AT STA 1820 BL0 DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CHORD REPAIR. 2L74 4F4 FRTA20WE E24NE 20040303002332004030300233NM 2004 3 3 DHL2004783003 120040227A8010 SWITCH BOEING727 727227 1384078NM PWA JT8 JT8D17 52049NE NR 3 FAULTY A DHLAO OTHER X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 SO01783DH 21999 708917 DURING START OF ENGINE NR 3 ENGINE ROLLED BACK AT APPROXIMATELY 40 PERCENT N2. ALL INDICATIONS WERE NORMAL DURING THE FIRST START. ATTEMPTED RESTART, AFTER CONFERRING WITH MAINTENANCE CONTROL (MXC), AND ADVISED TO RESTART. START WAS SUCCESSFUL WITH NO ANOMALIES NOTED. CLEANED PEDESTAL SWITCHES AND FUEL VALVE CONTROL. CYCLED FUEL VALVE APPROXIMATELY 20 TIMES IN 4 HOUR PERIOD, AND 3 ENGINE STARTS AT 2 HOUR INTERVALS. FOUND ALL NORMAL STARTS AND NORMAL SHUTDOWNS PER JRH. REFER TO LOG PAGE 372802 ITEM 1P DURING ENGINE START ENGINE NR 3 ROLL BACK TO APPROXIMATELY 40 PERCENT N2. REMOVED AND REPLACE NR 3 START SWITCH IAW ASTAR B-727 M/M 20-1-0, OPS CHECKED IAW ASTAR JRH 5.1.2. 2L73 4F4 F A3WE E2EA 20040401001452004040100145EU 2004 4 1 TRB2004F00006 120040113A6123 AUTOFEATHER SYS AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE NR 2 MALFUNCTIONED A TRBACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO21429AT 429 MM1388 AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) SYSTEM DID NOT ARM DURING TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 AUTOFEATHERING UNIT. 2H72 4T4 TRTA53EU E20NE 20040407000432004040700043NE 2004 4 7 USAABB04021 220040212A731021SN04223 PRESSURE SWITCH BOEING767 767201 1385125NM GE CF6 CF680C2B2 30025NE LEFT ENG FUEL FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA19649US 23901 SJU - FLT 134, EN ROUTE STT TO PHL, CREW RECEIVED THE EICAS MESSAGE 'L ENG FUEL FILT.' FLIGHT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE FILTER AND FOUND IT SATISFACTORY. THE FUEL DIFFERENTIAL PRESSURE SWITCH WAS REPLACED, AS WELL AS THE FILTER. (M) 2L72 4F4 FRTA1NM E13NE 20040409000512004040900051GL 2004 4 9 MASA200400113 220040226A7200 ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 2 FLAMED OUT A MASAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 SW07860MJ 145773 CAE312515 CREW REPORTED NR 2 ENGINE FLAMED OUT DURING LANDING ROLL-OUT. MX PERFORMED ENGINE RUNS. MX FOUND NO DEFECTS. NO PARTS USED. 2L72 4T4 FRTT00011ATTE6CH 20040409000722004040900072NM 2004 4 9 2004UALA00295 120040330A5311 FRAME BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29904UA 25004 INTERNAL FUSELAGE BS 616R FRAME WEB FORWARD FACE BELOW FLOOR LINE S16R LOCATED UNDER OVERWING EXIT RIGHT SIDE HAS CRACK APPROX 1 INCH LENGTH COMING FROM FASTENER HOLE, FRAME INNER CORD. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F4 FRTA16WE E2GL 20040426002032004042600203NM 2004 4 26 2004UALA00350 120040413A5313 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 HOLES ON STRINGER ELONGATED AT STA 767 & 768 STR 23R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040428001722004042800172NM 2004 4 28 DL76L040348 120040417A80107755386 START VALVE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27196DN 890730 28453 727830 LEFT STARTER CUTOUT EICAS MSG AND VALVE LIGHT ILLUMINATED ON TAKEOFF. FOLLOWED QRH. START VALVE REPLACED. 2L72 4F4 FRTA1NM E24NE 20040429000382004042900038EU 2004 4 29 HCM2004F00000 120040309A772064660251 SENSOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE ENGINE FAILED E HCMAO OTHER O OTHER NRNOT REPORTED 1 WP13995BH 2987 ON MARCH 9, 2004 WHILE ON A SIGHT SEEING TRIP, THE PILOT NOTICED A HIGH ENGINE OIL TEMPERATURE INDICATION. HE MADE A PRECAUTIONARY LANDING. A MECHANIC WAS FLOWN TO THE SCENE AND REPLACED THE ENGINE OIL TEMPERATURE SENSOR. THE AIRCRAFT WAS FLOWN BACK TO BASE WITHOUT FURTHER INCIDENT. 1G71 3U3 U H9EU E19EU 20040428000382004042800038SW 2004 4 28 BAQA093856 120040227A2422MD2628 INVERTER BELL 407 407 1182206SW ALLSN 250C 250C47B GL AC SYSTEM INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03302LE49 53572 WARRANTY. UNIT IS NOT GIVING A/C OUTPUT VOLTAGE. REPLACED WITH SERVICABLE UNIT. 03/18/2004 1G71 3U3 UO H2SW E1GL 20040429000472004042900047GL 2004 4 29 ALGA093962 220040326A72606893672 GEAR BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL GEARBOX SPALLED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032618 1081 45503 CAE895112 FOUND HEAVY SPALLING ON GEAR TEETH. 1G71 3U3 U H2SW E1GL 20040430000912004043000091EA 2004 4 30 VNAA0403010 120040315A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DETECTED A VNAAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 GL07218PS 7885 THE CREW REPORTED A CARGO OVERHEAT MESSAGE AND A STRONG ELECTRICAL ODOR IN THE CABIN. OUSTATION MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DISCREPENCIES. THE AIRCRAFT WAS THEN FERRIED TO DAY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 21-50-00-863-801 AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040504000562004050400056EU 2004 5 4 PG92004F001 120040302A6510 SPAR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19911KR819 9289 2094 TAIL ROTOR BLADE HAS SPAR CRACKED UNIT. 1G71 3U3 UNCH9EU E19EU 20040505001702004050500170SW 2004 5 5 EAT2004F00003 120040325A5311263106510 FRAME SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP FUSELAGE CRACKED B EATRK NONE O OTHER ININSP/MAINT 1 GL09220AM32313 TC234 DURING INSPECTION FRAME (PN 262106510) WAS FOUND CRACKED AT THE CONTROL COLUMN BEARING MOUNT ON THE RT SIDE. THIS WAS THE IMPROVED BEARING MOUNT SETUP AS CALLED OUT BY AD AND SB TO PREVENT CRACKING. THE CRACKS ARE OCCURRING RIGHT AT THE TOP OF THE IMPROVED (PN 2621352-001/005) DOUBLER ASSY. BELOW THE RADIUS ON THE 26-21065-10 FRAME. THIS APPEARS NOT TO BE A FLUKE. THIS IS THE SECOND AIRCRAFT FOUND WITH THIS PROBLEM. MFG HAD ANOTHER SB CONCERNING THIS AREA THAT CHANGES THE MOUNTING AGAIN AND MAKING THE DOUBLER LONGER TO SPREAD OUT THE LOAD BETTER TO THE FRAME. 2L72 4T3 TRTA8SW E2WE 20040510002512004051000251NM 2004 5 10 2004UALA00369 120040417A5330 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE LIGHTNING STRIKEA UALAK NONE O OTHER ININSP/MAINT 1 WP29388UA 24663 UPPER NR 1 VHF ANTENNA LT AFT MOUNTING HOLE HAS LIGHTNING STRIKE DAMAGE. FOUND WHEN ANTENNA REMOVED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TRIPLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040514000882004051400088SO 2004 5 14 BNG2004F00000 120040420A32207642603 LINK PIPER PA28 PA28R201T 7102813SO CONT O360 TSIO360* 17025SO NOSE GEAR BRACE CRACKED B BNGRO OTHER O OTHER NRNOT REPORTED 1 GL19476813012 28R7703421 NOSE GEAR LINK PN 76426-03, CRACKED TOP RT SIDE. 1L71 3O3 O 2A13 E9CE 20040518001172004051800117SO 2004 5 18 421C032204DG 220040308A8500 ENGINE CESSNA421 421C 2076016CE CONT O520 GTSIO520L 17032SO NR 1 MALFUNCTIONED B JBZRO OTHER O OTHER NRNOT REPORTED 1 WP27321FL 421C0207 292378R DURING A ROUTINE PREFLIGHT INSPECTION, PILOT NOTICED PULL THROUGH OF NR 1 ENGINE WAS MORE DIFFICULT THAN NORMAL FOR THAT ENGINE MAKE AND MODEL. A ENGINE START AND RUN-UP WAS PERFORMED TO NORMAL OPERATING TEMPERATURES; WITH NO ABNORMAL CONDITIONS NOTED OTHER THAN AN EVEN MORE DIFFICULT HAND PULL THROUGH. SPARKPLUGS, ALTERNATOR AND STARTER ADAPTER WERE REMOVED IN ATTEMPT TO ISOLETTE CAUSE OF STIFF ROTATION, RESULTING IN NO CHANGE OF CONDITION. DECISION WAS MADE TO REPLACE ENGINE. 1L72 3O3 O A7CE E7CE 20040520002802004052000280EU 2004 5 20 CX7A194J0422 120040427A750012J63125 COUPLING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE BLEED AIR BUCKLED A CX7AB EMER. DESCENT MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL03312CE 340B334 785273 AFTER TAKEOFF NOTED L/H ENGINE OVERTEMP LIGHT ON. ITT OF 985 – REDUCED POWER TO 80%, ITT WENT TO 878. UNCOMMANDED ENGINE SHUTDOWN DURING CLIME OUT. L/H HP LINE BECAME DISCONNECTED DAMAGING INTERNAL STRUCTURE OF L/H ENGINE COWLING. 2L72 4T4 TRTA52EU E8NE 20040528000362004052800036WP 2004 5 28 UPS04842412 120040508A5313 LONGERON DOUG DC8 DC871F 302199DWP GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 INSPECTION TYPE: C1 STATION 1730 LONGERON 14R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 1720 TO 1740 AND INSTALLED SPLICES AND STRAPS IAW SRM. 53-2-2 FIG. 10. 2L74 4F4 FRT4A25 E2GL 20040528000432004052800043CE 2004 5 28 3117705162004 120040516A213026195009 VALVE LEAR 35 31 5170530CE GARRTTTFE731TFE7312B WP CABIN PRESSURE FAILED E J7SAB EMER. DESCENT O OTHER CRCRUISE 1 SW05132FX3205 31177 AT FL390, CABIN DOOR BEGAN TO SQUEAL. AT FL405, CABIN BEGAN TO CLIMB 1,500 TO 2,000 FPM. CREW REQUESTED LOWER ALTITUDE FROM LAX ATC BUT WERE DENIED. AT THAT POINT, CREW DECLARED AN EMERGENCY DUE TO INABILITY TO CONTROL CABIN PRESSURE. AIRCRAFT LANDED WITHOUT INCIDENT. CURRENTLY IN MX. DOOR SEAL FOUND TO HAVE SEVERE TEAR AND THE MOD VALVES HAVE A HIGH LEAK RATE. REPLACED THE FOLLOWING PARTS DUE TO SUSPECTED FAILURE: CABIN DOOR SEAL, LT 3 WAY VALVE, LT AND RT MIXING VALVE. F/T OF PRESSURIZATION SYSTEM NORMAL. 2L72 4F4 FRTA10CE E6WE 20040614003272004061400327WP 2004 6 14 GTIA040460 120040308A5330 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE FUSELAGE DAMAGED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 12 INCH X 10 INCH CLASS II EXTERNAL REPAIR AT FS 249 BETWEEN LONGERON 17C AND 18L. REMOVED EXISTING EXTERNAL REPAIR. CUT OUT DAMAGED AREA 13.5 INCHES X 14 INCHES. FABRICATED NEW REPAIR PARTS EXTERNAL SKIN, FINGER DOUBLER, 03 EA DOUBLERS. INSTALLED NEW REPAIR PARTS. 2L72 4F4 F A6WE E2EA 20040616001172004061600117 2004 6 16 2004UALA00539 420040514A2565 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DEPLOYED A UALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29193UA 26890 FORWARD BOTTLE DISCHARGED WHEN PINS WERE PULLED RESULTING IN SLIDE DEPLOYMENT. UNABLE TO DEFINITIVELY DETERMINE CAUSE OF FAILURE DUE TO PARTIAL DEPLOYMENT OF SLIDE. SUSPECT THAT INFLATION CABLE WAS MISROUTED, RESULTING IN TENSION WHICH DEPLOYED SLIDE WHEN BOTTLE PINS WERE PULLED. SLIDE RECEIVED MINOR DAMAGE DURING DEPLOYMENT DUE TO IMPACT WITH DOCK STRUCTURE. SLIDE RETURNED TO SHOP FOR ROUTINE CHECK, REPAIR, REPACKING, AND RETURN TO SERVICE. 2L74 4F4 FRTA20WE E24NE 20040616001672004061600167NM 2004 6 16 2004UALA00562 120040607A2721 TRIM SYSTEM BOEING757 757222 1384956NM PWA 2037 PW2037 NE RUDDER MALFUNCTIONED A UALAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 WP29520UA 24890 PLANE HAD RIGHT RUDDER TRIM PROBLEM. ADDITIONAL PROBLEMS WITH SPOILERS. FAILED RUDDER TRIM ACTUATOR INHIBITED ABILITY TO TRIM RUDDER. REMOVED AND REPLACED SUBJECT RUDDER TRIM ACTUATOR WITH NEW SERVICABLE ACTUATOR. THE NR 9 SPOILER ACTUATOR WAS REPLACED TO ADDRESS ASSOCIATED SPOILER PROBLEMS. 2L72 4F4 FRTA2NM E17NE 20040618001032004061800103EU 2004 6 18 ASOA04389 120040528A3350NSA931320075 CIRCUIT BREAKER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE TRIPPED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27535AS 464 DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS CAME ON IN THE ARMED POSITION AFTER ENGINE START. MAINTENANDE RESET THE EMERGENCY LIGHTS CIRCUIT BREAKER AND NSPECTED THE WIRE ON THE SWITCH PANEL WHICH CHECKED GOOD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20040623000892004062300089WP 2004 6 23 GTIA040507 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT IB SEAT TRACK FS 1022-1309 CORRODED AND GOUGED. SEAT TRACK REMOVED FROM 1032-1309. LOCATED AND DRILLED SEAT TRACK AND SPLICES. INSTALLED RT IB SEAT TRACK AND SPLICES. 2L72 4F4 FRTA6WE E2EA 20040628000312004062800031EA 2004 6 28 SWIA200413473 120040617A3350 LENS CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT MISSING A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07964SW 7868 MISSING RED LENS ON AFT EMERGENCY EXIT SIGN OF ROW 8. INSTALLED NEW RED LENS ON AFT EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040628000502004062800050 2004 6 28 SWIA200413409 420040615A22156225734002 SERVO EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE ELEVATOR CONTROLMALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07579SW39 39 120347 CREW REPORTED ROUGH FEEL IN ELEVATOR CONTROL. REMOVED AND REPLACED ELEVATOR SERVO REF AMM 22-10-05. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040630000212004063000021EU 2004 6 30 USAA040310 120040608A5321D5367175309800 FLOOR PANEL AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19709UW16153 0997 FLOOR PANEL, 10 PERCENT OF TOTAL AREA, MAIN DECK FLOOR PANEL 262HG, DELAMINATION. FABRICATED NEW PANEL IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630000472004063000047SO 2004 6 30 SIMA200412501 120040501A27313621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL PITCH TRIM INOPERATIVE A SIMAO OTHER J WARNING INDICATION APAPPROACH 1 SW21802AE 145471 PITCH TRIM 1-2 INOPERATIVE ON EICAS AT 520 FT SHORTLY AFTER DISCONNECTING AUTO PILOT. REPLACED HSCU. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406976) 2L72 4F4 FRTT00011ATTE6CH 20040624000042004062400004GL 2004 6 24 P5CA0401098 220040528A7261 ENGINE BOEING747 74746NF 13848BTNM GE CF6 CF680C2* GL NR 2 LEAKING A P5CAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP23454PA 30812 706483 NR 2 ENGINE OIL FILTER BYPASS WARNING IN CRUISE RAPID LOSS OF OIL QUANTITY FROM 14 QUARTS TO 3 QUARTS. AS PER QUICK REF HANDBOOK NR 2 ENGINE SHUTDOWN PROCEDURES. 2L74 4F4 FRTA20WE E23EA 20040622002132004062200213NM 2004 6 22 GTIA040542 120040511A5347 SEAT TRACK DOUG MD80 MD83 3023681NM PWA JT8 JT8D* NE FUSELAGE WORN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23822NK 49392 CABIN LT IB SEAT TRACK WORN AND CORRODED STA 200-1307. STA 935 TO 1117 AND STA 1200 OUT OF LIMITS. REMOVED SEAT TRACK AND SPLICES STA 915-1090 AND 1184-1221. INSTALLED SEAT TRACK AND SPLICES STA 1184-1221. INSTALLED SEAT TRACK AND SPLICES STA 915-1090. 2L72 4F4 FRT E2EA 20040630001072004063000107EU 2004 6 30 USAA040255 120040528A5320D5348004320501 SILL AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19102UW13221 0844 DOOR SILL, 1.0 INCH X 1.5 INCH X 0.07 INCH DEEP, CORROSION; LEVEL 2; FR 66 TO 68, -Y 1524, Z-240. REPLACED DOOR SILL IWA SRM. 2L72 4F4 FRTA28NM E2GL 20040722000352004072200035CE 2004 7 22 G1I2004F00000 120040616A5210MS203922C31 CLEVIS PIN BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA PAX DOOR LATCH SHEARED E G1IAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL0125KA BB783 DURING CLIMB OUT, THROUGH APPROX 1800 FEET EXPERIENCED RAPID LOSS OF CABIN PRESSURE. DESCENDED AND RETURNED TO DEPARTURE AIRPORT. AFTER EXTENSIVE TROUBLESHOOTING IT WAS DETERMINED THAT THE UPPER FORWARD LATCH HAD A BROKEN CLEVIS PIN AT THE LATCH PIVOT POINT. PRESSURIZATION AND FLIGHT CHECK SATISFACTORY. 1L72 4T3 T A24CE E2NE 20040811000612004081100061NM 2004 8 11 VNAA0408002 120040802A3350501122803 POWER SUPPLY DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE EMERGENCY LIGHT FAILED A VNAAO OTHER L NO TEST TXTAXI/GRND HDL 1 GL07425JS216321531 3037 THE CREW REPORTED THAT THE EMERGENCY POWER SUPPLY WAS DEAD. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY POWER SUPPLY IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040913001712004091300171NM 2004 9 13 P5CA0401117 120040709A361073836219 VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 1 PYLON MALFUNCTIONED A P5CAK NONE J WARNING INDICATION ININSP/MAINT 1 WP23505MC 21251 DMI NR 32768, NR 1 PYLON VALVE INOPERATIVE, ALSO HIGH PRESSURE BLEED VALVE ON ENGINE NR 1. REMOVAL AND REPLACEMENT. REMOVED AND REPLACED PYLON VALVE DUE TO NOT CLOSING COMPLETELY , OPS CHECK AND LEAK CHECKS GOOD IAW MM 36-11-04. 2L74 4F4 FRTA20WE E23EA 20040823001052004082300105SO 2004 8 23 LR7A04068 120040716A5330330421756 DOUBLER LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND BELLY ANTENNA FLANGE WITH DENTS AND DEEP SCRATCHES AT FS 265 - 278 BL18 L/R, WL126. RADIO ALTIMETER ANTENNA DOUBLERS FABRICATED AND INSTALLED IAW DWG 3304217. DRC 2034. 2H74 4T4 T A1SO E282 20040831000562004083100056EA 2004 8 31 SWIA200413668 120040807A2760270007 PCU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLIGHT SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07435SW2704 2704 7555 LT SPOILERON NR 1 PCU STATUS MESSAGE ON EICAS. REMOVED AND REPLACED LT IB SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040907001652004090700165NM 2004 9 7 2004UALA00758 120040810A1430 FASTENER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 1 PYLON LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29107UA 26900 NR 1 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING INBOARD & OUTBOARD ROW UPPER HORIZONTAL FASTENERS HAVE ROTATED, 2 TTL FASTENERS. 2L74 4F4 FRTA20WE E24NE 20040928000342004092800034EU 2004 9 28 04FDEA02783 120040920A5315TSDSQ007778 FLOORBEAM AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E1 52054NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25421FE 342 MDIS 421 53-10 0009108 21SEP04 SIN CLOSE U- QA PICKUP FLOORBEAM AT FWD FACE OF FR 33, BETWEEN -Y450 AND -Y953 WITH HAIR LINE CRACK. ENT BY: 275296 RPT BY: 275296 FACT 21SEP04 02:26 SIN U FLOORBEAM REPAIR C/O IAW SRM 53-10-15 FIG 201 SH 4A. RII BY L1160. ENT BY: 275296 RPT BY: 275296. 2L72 4F4 FRTA35EU E3NE 20040928000922004092800092NE 2004 9 28 DLM88040892 220040916A7200 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 BIRD INGESTION A DALAA UNSCHED LANDING CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27943DL33351 49816 726051 ACRID SMELL IN COCKPIT AND CABIN SHORTLY AFTER TAKEOFF IN DCA. SMELL WORSENED ACCORDING TO FLT ATTENDANTS. DIVERTED TO IAD. FLT CREW DISCOVERED BIRD REMAINS ON STATOR BLADES OF LEFT ENGINE INTAKE ABOUT 6 ABOVE BULLET NOSE. NO APPARENT DAMAGE TO FN BLADES. SMELL HAD BEGUN TO DISSIPATE DURING DESCENT. PERFORMED BIRD STRIKE INSP. 05-51-08 NO DEFECTS NOTED. CLEAN STATOR VANE AND INSPECTED ENG, RAN ENGINE AND A/C PACKS, NO ODORS OR SMELLS PRESENT, ENGINE RUN NORMAL. 2L72 4F4 FRTA6WE E9NE 20040917000162004091700016GL 2004 9 17 2004F00379 220040803A732323065125 GOVERNOR BELL 206 206L4 1182110SW ALLSN 250C 250C30P 03013GL ENGINE MALFUNCTIONED E ALGAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SW03414LV12758 52006 IN A HOVER READY FOR TAKEOFF, TOOK OFF INTO A HOVER AND THE N2 DROPPED TO 95 PERCENT AND WOULD NOT RECOVER OR RESPOND TO INCREASE OR DECREASE TO BEEP SWITCH. MAINTENANCE FOUND BEEP MOTOR INTERMITTENT, REMOVED AND REPLACED, ALSO FOUND THAT THE GOVERNOR WAS DROPPING, REMOVED AND REPLACED GOVERNOR. COMPLIED WITH GROUND CHECKS AND OPS CHECK FLIGHT ALL CHECKS GOOD. (M) 1G71 3U3 UNCH2SW E1GL 20040923000242004092300024NE 2004 9 23 AALA20040964 220040916A7200JT8D217C ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LEFT BIRD INGESTION A AALAFA ACTIVATE FIRE EXT. UNSCHED LANDING CYAF.O.D. ENGINE STOPPAGE FLAME/FIRE CLCLIMB 1 SW21253AA 49286 718490 ENROUTE, MULTIPLE BIRDSTRIKES TO LT ENGINE. FIRE LIGHT ILLUMINATED AND BOTH BOTTLES DISCHARGED. RETURNED AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME FOUR MINUTES. AIRCRAFT OUT OF SERVICE FOR REPAIRS. OPEN. 2L72 4F4 F A6WE E9NE 20041008000412004100800041NM 2004 10 8 P5CA0401233 120041001A5330 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 APU EXHAUST AREA SKIN CRACKED BS 2742. CUT OUT DAMAGED AREA, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 53-30-03. 2L74 4F4 F A20WE E20EA 20041013000092004101300009NM 2004 10 13 2004UALA00875 120040918A5310 STRUCTURE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 LT EXTERNAL FUSELAGE RIVET HOLE AT STA 520 AND STR 19L HAS EGG SHAPED HOLE. CUTOUT DAMAGE AND INSTALLED STRUCTURAL FILLER AND DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20041018000132004101800013WP 2004 10 18 DHL2004801550 120040930A5730 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 2127: RT CTR L/E HAS INTERIM REPAIR AT XFS 304.000 (LWR. PART). PERFORMED MAJOR REPAIR IAW DWG W51-R10, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1-21 PG.1, SRM 51-1-20D PG.21, DC8 SRM 51-3-0 PG.1, DWG W51-R10. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED NEW REPAIR DOUBLER (7075-T6AL 0.071) IAW DWG W51-R10. CLEANED, TREATED AND PRIMED AREA AND INNER SIDE OF REPAIR DOUBLER IAW DC8 SRM 51-1-8B. APPLIED PRC SELANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG.9. INSTALLED NEW REPAIR DOUBLER IAW DC8 SRM 51-1-21 PG.1, DC8 SRM 51-1-20D PG.9, DC8 SRM 51-3-0 PG.1, DWG W51-R10. 2L74 4F4 FRT4A25 E2GL 20041020001942004102000194CE 2004 10 20 ZFD2004F00000 120040916A3220584200021 TRUNNION CESSNA310 310R 2074245CE CONT O520 IO520* 17032SO RT NLG BROKEN E ZFDAO OTHER O OTHER NRNOT REPORTED 1 GL25623687750 310R0131 AC WAS BEING TAXIED WHEN A SNAP WAS HEARD AND THE AIRCRAFT STARTED AN UNCOMMANDED TURN. THE PILOT IMMEDIATELY PULLED BOTH MIXTURES SHUTTING DOWN THE ENGINES. UPON EXITING THE AIRCRAFT, THE PILOT FOUND THE NLG LEANING AND TURNED SIDEWAYS. THE AIRCRAFT WAS INSPECTED BY A LOCAL MECH WHO FOUND THE NLG TRUNNION LUG HAD FAILED, ALLOWING THE NLG TO TWIST OUT OF ITS MOUNT. WILL SUBMIT A MORE COMPLETE REPORT WHEN ALL FACTS ARE FOUND. 1L72 3O3 O 3A10 E5CE 20041026001452004102600145NM 2004 10 26 UPS04243392 120041006A5751652176618 SKIN BOEING727 727185C 138406NNM RROYCETAY TAY65154 EU RT OB AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 INSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14. 2L73 4F4 F A3WE E25NE 20041108001512004110800151CE 2004 11 8 4020 120040813A2612 WARNING LIGHT LEAR 25 25D 5170514CE GE CJ610 CJ6108 30006NE ENGINE FIRE ILLUMINATED E BSYAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION APAPPROACH 1 GL07228SW 228 251800 ON APPROACH INTO CLT RIGHT ENGINE FIRE LIGHT CAME ON, FIRST STARTED FLICKERING THEN CAME ON STEADY. REDUCED POWER LIGHT WENT OUT, THEN CAME BACK ON AND STAYED ON. SHUT DOWN ENGINE AND BLEW BOTH BOTTLES. 2L72 4J4 J A10CE 1E16 20041122000692004112200069NM 2004 11 22 2004UALA01022 120041107A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 FRAME WEB IS CRACKED AT STA 194 AT LBL 16 AND WL 208. FABRICATED AND REPLACED SHEAR WEB. 2L72 4F4 FRTA16WE E2GL 20041026001242004102600124NM 2004 10 26 DLM88040959 120041009A53305936004503 SKIN DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE FS L-30 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27924DL 49711 FUSELAGE SKIN FS 630 LONGERON 29-30 RT : THE FUSELAGE SKIN AND UNDERLYING DOUBLER WERE FOUND CORRODED AT FS 630 BETWEEN LONGERON 29R AND 30. THE CORROSION WAS REMOVED WITH A 9 INCH X 5 INCH CUTOUT IN THE SKIN AND A 7 INCH X 5 INCH CUTOUT IN THE DOUBLER. THE CUTOUTS WERE REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS IAW ER/A 094196-14. 2L72 4F4 FRTA6WE E9NE 20041102000272004110200027NM 2004 11 2 2004UALA00866 120040908A5414 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE PYLON DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 EXISTING FASTENER HOLES IN THE NR 1 RT AND LT FWD PYLON SIDE SKINS ARE LARGER THAN ALLOWABLE LIMITS. REPAIRED OVERSIZED HOLES WITH FREEZE PLUG REPAIRS. 2L72 4F4 FRTA2NM E17NE 20041102001102004110200110SO 2004 11 2 SWIA200414000 120041022A27523430001005 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAP MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07565SW1048610486 120340 AFTER ENGINE START, RECEIVED A FLAP ASYMMETRY WITH THE IB PAIR. REPLACED LT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20041108000152004110800015NE 2004 11 8 COMA0470078 220041031A7200 ENGINE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LEFT FLAMED OUT A COMAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO01354CA 10064 965381 FLIGHT 5655 LT ENGINE FLAMED OUT DURING DESCENT FROM FL 410. NO FAULTS IN MDC, RAN ENGINE, NO DEFECTED NOTED. 2L72 4F4 FRTA21EA EOOO63EN 20041118001902004111800190NM 2004 11 18 USAA040751 120041015A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 FLOORBEAM, SEVERAL .5 INCH AREAS, CORROSION LEVEL 2, STA 365 BL0 TO RBL12. INSTALLED TEE CAP REPAIR IAW SRM 53-00-51. 2L72 4F4 FRTA2NM E12EU 20041129000342004112900034EA 2004 11 29 ASOA04791 120041012A3350100865 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27877AS7323 7579 DURING A GROUND INSPECTION, THE LOWER EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129000742004112900074NM 2004 11 29 C7WA200400048 120040922A5310 SHEAR TIE BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO178887Z 21856 SHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 LT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11, MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES. 2L73 4F4 F A3WE E2EA 20041129000132004112900013NM 2004 11 29 UIEA200400187 120041031A750019099262 PRECOOLER BOEING747 7472F6B 1384807NM GE CF6 CF650E2 30018NE NR 4 ENGINE CRACKED A UIEAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CRCRUISE 1 EA15534MC 21832 EK9971 ICN/ANC (ATB) FIRE WARNING: NR 4 ENGINE FIRE LIGHT CAME ON IN-FLIGHT NACELLE INDICATOR WAS ABOUT 3 TO 3.5 EGT APPROX 900 DEGREE HIGH STAGE BLEED LIGHT CAME ON JUST BEFORE FIRE LIGHT AND BELL. FIRE LIGHT CAME ON ABOUT FL 24.2 ENGINE S/D A/WITH FHB. INSPECTION FOUND NR 4 ENGINE PRECOOLER HAS CIRCUMFERENTIAL CRACK ON INLET FLANGE APPROX FROM 5 OCLOCK TO 10 OCLOCK. REPLACED PRECOOLER ASSY. LEAK CHECK NORMAL IAW MM 36-12-01. 2L74 4F4 F A20WE E23EA 20041129001992004112900199NM 2004 11 29 USAA040696 120041001A5313 STRINGER BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19601AU63825 22193 C-3 - STRINGER, 1 INCH DIAMETER, CORROSION AT STA 1460, STRINGER 26R, AFT CARGO. REPAIRED IAW SRM 53-00-03, 51-10-02. 2L72 4F4 FRTA2NM E12EU 20041130001962004113000196NM 2004 11 30 2004UALA01107 120041113A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29574UA 26686 AFT PIT FRAME DENTED AT STA 1480 BETWEEN STRINGERS S25L & S26L. REMOVED DAMAGED PORTION OF THE FRAME CAP. INSTALLED NESTED J ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041215000862004121500086WP 2004 12 15 ASAA0480531 120041002A57305930503106 ACCESS PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT WING LEAKING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, EVIDENCE OF FUEL LEAK FROM RT WING LOWER DOORS, NR 5 AND NR 7, FROM IB ENSURED HOLE CLEAN AND ROUND, TOUCH COUNTER SUNK, NDT FOR CRACKS. INSTALLED AD RIVET AND SHAVED BOTH SIDES OF REPAIR IAW EA 5710-01109 AND EA 10575. 2L72 4F4 FRTA6WE E9NE 20041215000302004121500030EA 2004 12 15 A6WA200440178 120041107A3397 SPLICE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT WRONG PART A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 FLOOR TRACK LIGHTING HAS WRONG SPLICES AT ROW NR 12. REMOVED AND REPLACED SPLICES AT ROW NR 12 IAW CRJ 200 WIRING MANUAL 20-17-10. 2L72 4F4 FRTA21EA E15NE 20041202001562004120200156EA 2004 12 2 VNAA0411004 120041116A3244299K631 TIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT MLG DAMAGED A VNAAO OTHER O OTHER LDLANDING 1 GL05262PS205 7962 POST FLIGHT INSPECTION OF THE AIRCRAFT BY THE CREW OF FLIGHT 2293 REVEALED THE LEFT INBOARD MAIN LANDING GEAR RETREADED TIRE HAD SHED APPROXIMATELY HALF ITS TREAD DURING LANDING AT MSP. UPON FURTHER INVESTIGATION FOD WAS FOUND ON THE LEFT INBOARD FLAP AND ON THE NR 1 ENGINE FAN BLADES. PSA MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLY. THE AIRCRAFT AND ENGINES WERE INSPECTED AND DETERMINED TO BE AIRWORTHY. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD FLAP. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221001582004122100158EA 2004 12 21 A6WA20044151 120041017A53206013501252 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31437AW 7744 FS 621-FS 625.3 INTERCOSTAL, RT SIDE STR 14R, IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PN 601R35012-52, IAW SRM 51-42-06. 2L72 4F4 FRTA21EA E15NE 20041221000122004122100012NM 2004 12 21 ASA0440201 120041029A53116546529 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHAND BIN CHANNEL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20050110001412005011000141EU 2005 1 10 USAA041024 120041201A5320D53472189200200 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19712US17054 1038 BFM - S1 CK - BEAM, 1.5 INCH X 1.5 INCH X .060 INCH DEEP; CORROSION; LEVEL 2; TASK NR JA-260-53500-005, MAIN CABIN FLOOR FR C68, Y1292. REMOVED AND REPLACED BEAM IAW SRM 53-00-14. 2L72 4F4 FRTA28NM E37NE 20050107000942005010700094NM 2005 1 7 USAA040938 120041110A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1- SKIN, 2 INCH BY 2 INCH AREA, CARBON FIBER DAMAGE, 120.5 INCH UP FROM BOTTOM, 6.25 INCH FORWARD OF T/E. FILLED AND INSTALLED REPAIR PLIES IAW 51-70-17 AND EA 79467. 2L72 4F4 FRTA16WE E21EU 20050111001692005011100169NM 2005 1 11 ASAA0410513 120041108A53136545800197 STRINGER BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON STRINGER. REMOVED AND REPLACED STRINGER. 2L72 4F4 FRTA16WE E2EA 20050124000992005012400099NM 2005 1 24 WLDA2004120 120041014A5754ARB16475 SKIN DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE LT WING NR2 SLATCRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11271 48518 DURING 2C+12A CHECK, FOUND LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK AT XIS 360. REPAIRED LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK PER EGAT EI W2004A57B-592 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 33 AND FIG 10). PERFORMED SLAT OPERATION AND CONDITION CHECK FOUND ALL NORMAL. 2L73 4F4 FRTA22WE E24NE 20050202000932005020200093NE 2005 2 2 ARWA20040901 220040907A7200 ENGINE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 2 SHUTDOWN A ARWAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO19791AL45204496 46150 671323 AT TOP OF DESCENT 08:23 ZULU, SHUT DOWN NR 2 ENGINE DUE TO OIL PRESS LIGHT ON AND OIL PRESS 30 PSI WITH ENGINE AT IDLE. WINDMILLING OIL PRESS 11 PSI N1 26.5 PERCENT. SECURED NR 2 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH GMM 6-3-4 AND 6-3-5. COMPLETED RED BORDER NR 18470. REMOVED NR 2 ENGINE S/N 671323 DUE TO OIL PRESSURE LOSS AND INSTALLED ENGINE S/N P-671360 IN ACCORDANCE WITH ARROW AIR JOB CARD NR DC8UN-O03. OPERATIONAL AND LEAK CHECK AT ENGINE RUN-UP IN ACCORDANCE WITH ARROW AIR JOB CARD NR DC8UN-093 AND DC8 MM 74-00; FOUND NORMAL, NO LEAKS NOTED. 2L74 4F4 F 4A25 1E8 20050215000282005021500028EU 2005 2 15 KBM2005F00003 120041227A7931704A37642043 TRANSDUCER SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE OIL PRESSURE FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP1937SH 627 2300 OIL PRESSURE GAUGE SHOWING NO INDICATION OF PRESSURE. REMOVED AND REPLACED. 1G71 3U3 UNCH9EU E19EU 20050215001052005021500105NM 2005 2 15 S2YA04044 120041128A5270 PROXIMITY SWITCH DORNERDO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR DIRTY A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13355SK 3124 DURING TAKEOFF, THE CREW NOTICED A CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX CLEANED THE PROXIMITY SWITCHES, OPENED AND CLOSED THE CARGO DOOR. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050223000562005022300056NE 2005 2 23 GLBA20030720 220040915A7200 ENGINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67 52043NE NR 2 MALFUNCTIONED A GLBAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 NM03245GL UE245 114445 NR 2 STARTED, DID RETURN TO IDLE POWER WITH LEVERFUL FORWARD NI SPOOLED DOWN SLOWLY ENG WAS SHUTDOWN BECAUSE OF THE AFX SYSTEM CAUSING IT TO GO INTO AND OUT OF FX. INSPECTED NR 2 ENG, NO DEFECTS NOTED. 2L72 4T4 TRTA24CE E26NE 20050302000612005030200061NM 2005 3 2 ASA0440382 120041227A573065C273599 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU LT WING CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON LT UPPER WING PANEL 8117 CUTOUT UPPER FLANGE. BLENDED CORROSION AND REPAIRED. (K) 2L72 4F4 FRTA16WE E21EU 20050330001162005033000116SO 2005 3 30 GUU2005F00002 120041216A3397 WIRE EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE EMERGENCY LIGHT CHAFED A GUUAK NONE O OTHER ININSP/MAINT 1 SO17282AS 120226 DURING PRE-FLIGHT, FOUND REAR EMERGENCY OVERWING LIGHTS INOPERATIVE. REPAIRED CHAFED WIRE ON RT REAR OVERWING LIGHT HARNESS. OPERATIONAL CHECK GOOD. (K) 2L72 4T4 TRTA31SO E20NE 20050330001372005033000137CE 2005 3 30 LJJ2005F00001 120041231A5711 SPAR BEECH 100 A100 1152915CE PWA PT6 PT6A27 52043EA LT WING CORRODED E LJJAK NONE O OTHER ININSP/MAINT 1 EA23601LM B116 CORROSION FOUND AT HOLE B, LWS 90.35, DURING INSPECTION OF LT S AND K SPAR STRAP. DER WAS CONSULTED FOR REPAIR. RECOMMEND CLOSE INSPECTION OF HOLES DURING REPETITIVE INSPECTIONS. ALSO RECOMMEND THE USE OF ANTI-CORROSION LUBRICANT DURING BOLT INSTALLATION. (K) 1L72 3T4 T A14CE E4EA 20050621001972005062100197NM 2005 6 21 2005UALA00529 120041228A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE STR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29590UA 28708 NUMEROUS ARCING SPOTS ON LOWER FUSELAGE SKIN AT BS 640-740, STR 25L TO 17R. SKIN HAS BEEN REPAIRED PER TIMCO REO (EVA) G09617, REV A WITH .063 EA. DOUBLER-TRIPLER. 2L72 4F4 FRTA2NM E17NE 20040130001632004013000163NM 2004 1 30 04FDEA00127 120040112A5753 FITTING DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP VANE T-FITTING NR 3 (COUNTING FROM INBOARD); FOUND CORROSION ON FWD HOLE BORE AREA. LT OUTBD FLAP VANE NR 3 TEE FITTING REPAIRED AS PER EA 1-5750-74289, WINGS - LEFT OUTBOARD FLAP - NR 3 FITTING SUPPORT VANE TO TRACK CORROSION. 2L73 4F RTA22WE 20040302001422004030200142NM 2004 3 2 SWAA040279 120040128A53116558280 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND R1 DOOR CUTOUT SUBFRAME CRACKED AT BS 303, RBL 56, WL 208. REMOVED AND REPLACED SUBFRAME SECTION PER SRM. 2L72 4F RTA16WE 20040414000662004041400066EU 2004 4 14 04FDEA00924 120040412A5347 CARGO TRACK AIRBUS300 A300F4605R 3930327EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25651FE 728 MAIN DECK CARGO COMP 2ND SEAT TRACK FROM CENTER RT SIDE BETWEEN FRAMES 74 AND 75, 1 EA AREA OF CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT AND FABRICATED NEW SEAT TRACK SECTION IAW A300 SRM 53-10-16 FIG 208. LOCATED AND DRILLED NEW SPLICES, INSTALLED SEAT TRACK AND SPLICES IAW A300 SRM 53-10-16 FIG 208. 2L72 4F RTA35EU 20040826000182004082600018NM 2004 8 26 04FDEA02370 120040805A5710ARC1991 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25578FE 48458 LT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.001, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA# 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040419002052004041900205NM 2004 4 19 SWAA041008 120040407A53306545774 SKIN BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29682SW 23496 DURING THRU FLIGHT CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040504000332004050400033NM 2004 5 4 ASAA040150 120040323A5310654588533 SHEAR TIE BOEING737 737290C 138448VNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 OKC - DURING MAINTENANCE, FOUND E/E COMPARTMENT AT STATION 328 HAS SHEAR TIE FLANGE CORRODED. REPAIR IAW SRM. (M) 2L72 4F A16WE 20040513000802004051300080NM 2004 5 13 04FDEA01181 120040510A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25597FE 48596 LEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-75954, LT AND RT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20050223001702005022300170WP 2005 2 23 04FDEA02906 120041011A5720ARC01542 SUPPORT DOUG MD10 MD1010F 3022112WP ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE70219 46626 BORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIGINAL BORE 2.530 INCH FINAL 2.543 INCH MATERIAL LOSS .013 INCH. FABBED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81474. PERFORMED MPI IAW DPS 4.704. CAD PLATED BUSHING IAW DACCMM 57-44-07. ALODINED AND PRIMED BORE IAW DC10 SRM 51-201 VOLUME II. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-07. 2L73 4F RTA22WE 20040421001142004042100114NM 2004 4 21 04FDEA00979 120040416A5313 STRINGER BOEING727 727200 138407ENM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25283FE 22350 STR 17L IS CRACKED AT BS 385 LBL 65 WL 208. CUT AND REMOVED STR AND INSTALLED REPAIR AT BS 370 TO BS 407, STR 17L, WL 208 IAW SRM 51-40-4. 2L73 4F RTA3WE 20050107001842005010700184NM 2005 1 7 SWAA050005 120041231A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29350SW 24409 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 977, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040317000482004031700048WP 2004 3 17 04FDEA00540 120040301A7603 ROLLER DOUG DC10 DC1010 3022110WP THRUST LEVER BROKEN A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25397FE 46631 GEAR UNSAFE HORN SOUNDED WHEN LEVER WAS RAISED ON T/O. HORN WAS SILENCED NORMALLY WITH THE GEAR HORN OFF BUTTON. THREE RED LIGHTS ON BOTH PANELS STAYED ON WITH HANDLE IN UP POSITION. GEAR WAS LOWERED AND 3 GREEN ANNUNCIATED. HYD PRESSURE & QUANTITY NORMAL. GEAR WAS RECYCLED WITH SAME RESULTS BUT NO HORN. JACKED A/C PER 07-11-00-2 DC-10-10 M/M SWUNG GEAR PER DC-10-10 M/M 32-30-00-5, WAS ABLE TO DUPLICATE. FOUND BROKEN ROLLER ON ACTUATOR FOR NR 3 THRUST LEVER LANDING GEAR WARNING HORN SWITCH. REPLACED ACTUATOR ON SWITCH S1-342, PER DC-10MM 76-11-04-2. CYCLED LANDING GEAR SEVERAL CYCLES, PER DC-10MM 32-30-00-5, ALL INDICATIONS NORMAL. 2L73 4F A22WE 20050118001052005011800105NM 2005 1 18 04FDEA03465 120041222A5511 SPAR CAP DOUG MD11 MD11 3023602NM HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 EMPENNAGE: HORIZONTAL STABILIZER RIGHT HAND UPPER SPAR CAP NR 36R BARREL NUT BORE CORROSION REWORKED FOUND EXCEEDED LIMIT. REPAIRED AS PER FEDEX EA 1-5510-78096. 2L73 4F RTA22WE 20040507000682004050700068EA 2004 5 7 SWIA200413260 120040503A274070609 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA HOR STAB TRIM MALFUNCTIONED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07958SW 7833 MACH TRIM WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM CONTROL UNIT IAW RJ MM 22-40-00. OPS CHECK GOOD. 2L72 4F RTA21EA 20040324000782004032400078SO 2004 3 24 SWIA200413001 120040304A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07584SW9290 9290 120352 CAPTAIN REPORTS OUTBOARD FLAPS HAD CONTROL FAULT MESSAGE DISPLAYED 2 TIMES IN A ROW. REMOVED AND REPLACED FLAP CONTROL UNIT AS REQUIRED. SYSTEM OPS CHECKS GOOD. 2L72 4T RTA31SO 20040406000592004040600059NM 2004 4 6 04FDEA00803 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 RIGHT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, OUTBOARD ACTUATOR BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-75997, WING TRAILING EDGE AND TRAILING EDGE DEVICES. RT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040804000132004080400013NM 2004 8 4 04FDEA02190 120040726A5347 SEAT TRACK BOEING727 727100 1384036NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION AROUND SEAT TRACK LINK AFT ATTACH BOLT BS 870 LBL 25 WL 205. *S/D* CORROSION ON AROUND SEAT TRACK LINK ATTACH BOLT AT BS 870 LBL 25 WL 205 WAS FOUND TO BE IN LIMITS. CORROSION ON LINK AT BS 870 LBL 25 WL 208 WAS OUT OF LIMITS. REMOVED & REPLACED LINK AT BS 870 LBL 25 WL 208 PER SRM 53-10-1, 53-10-5 & 51-30-2. 2L73 4F RTA3WE 20050926000892005092600089EA 2005 9 26 MASA200400666 120041129A4900 ODOR CNDAIRCL600 CL6002D24 1390016EA APU DETECTED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW07924FJ 15024 ASH 6221 EUG - THE PILOT REPORTED AN UNUSUAL SMELL WITH THE BLEEDS ON. ON CALL MAINTENANCE WAS DISPATCHED AND TROUBLESHOT THE PROBLEM TO THE APU. MAINTENANCE PLACED THE APU ON DEFERRAL. THE AIRCRAFT CONTINUED REVENUE SERVICE. 11/30 MAINTENACE RERACKED THE ECU, OPS GOOD. 2L72 4F RTA21EA 20040401000842004040100084NM 2004 4 1 SWAA040914 120040327A33506556633 LIGHT BOEING737 7373A4 1384585NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED EMERGENCY LIGHT PER MM. 2L72 4F RTA16WE 20040223001992004022300199EA 2004 2 23 MASA200400006 120040104A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG LEAKING A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0775987529 5987 ASH NR 2705) DURING THE RETRACTION OF THE GEAR HANDLE, THE NOSE GEAR UNSAFE LIGHT CAME ON. A/C RETURNED TO FIELD. MECHANIC REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD. 2L72 4F RTA21EA 20040916001972004091600197WP 2004 9 16 AALA20040881 120040822A3230 SCISSOR LINK DOUG DC9 DC983 3022083WP LT MLG CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21593AA 53256 SJC - LEFT GEAR SCISSORS UPPER LINK CRACKED AT FORWARD PIVOT POINT. REPLACED LEFT SCISSORS SUPPORT LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040217001712004021700171NE 2004 2 17 JYD2004F00000 120040122A64206516100010041 ROTOR HEAD SKRSKYS64 S64E 8142604NE PWA JFTD12JFTD12A4A 52047NE TAIL CRACKED B JYDRO OTHER O OTHER NRNOT REPORTED 1 NM09229AC848 64018 DURING NORMAL AIRCRAFT INSPECTION, THE FOLLOWING WAS FOUND: TWO SPANWISE CRACKS EXIST AT THE T/E ON THE OB SIDE. THE FIRST CRACK IS 7.25 INCHES FROM OB END OF THE POCKET AND IS 1.25 INCHES IN LENGTH. THE SECOND CRACK IS 14.5 INCHES FROM THE OB END OF THE POCKET AND IS 1.125 INCHES IN LENGTH. BOTH CRACKS ARE .375 INCH FROM THE T/E. THESE CRACKS ARE AT THE LEADING EDGE OF THE INSERT THAT RUNS THE LENGTH OF THE T/E. (MDR04-040) 2G72 4U4 U H4EA E15EA 20040303000572004030300057EA 2004 3 3 VNAA0402001 120040204A5270 SWITCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT EMER DOOR OUT OF ADJUST A VNAAO OTHER N FALSE WARNING CRCRUISE 1 GL07229PS 7898 DURING FLIGHT, THE CREW RECEIVED AN EMERGENCY DOOR INDICATION AT 25,000 FEET, THE INDICATION WENT OFF AT 10,000 FEET. MAINTENANCE INSPECTED AND ADJUSTED THE RIGHT HAND EMERGENCY DOOR SWITCH IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040304000632004030400063EA 2004 3 4 COMA0460166 120040222A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01819CA 7415 CARGO FLOOR ANGLE AT FS 621 LT SIDE CRACKED. REMOVED DAMAGED AREA OF LT CARGO FLOOR ANGLE. INSTALLED LT REPAIR ANGLE. ALL REPAIR AND FABRICATION WAS IAW REO 601R-53-61-004, CRJ SRM 51-23-00, CRJ SRM 51-25-06 AND CRJ SRM 51-25-16. 2L72 4F4 FRTA21EA E15NE 20040304000692004030400069EA 2004 3 4 COMA0470026 120040223A5230 DOOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE CARGO BAY UNSECURE A COMAA UNSCHED LANDING WP INADEQUATE Q C NO WARNING INDICATION CLCLIMB 1 SO01354CA 10064 FLIGHT 5075 CABIN ALTITUDE CAUTION, AIRCRAFT WOULD NOT PRESSURIZE. FOUND CARGO DOOR NOT CLOSED PROPERLY. INSPECTED DOOR, NO DEFECTS NOTED. SECURED DOOR CLOSED. 2L72 4F4 FRTA21EA E15NE 20040304000232004030400023EU 2004 3 4 04049331 120040218A3350 BULB JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE331* 01514WP EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27331UE 41099 DURING INSPECTION THE LT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T3 TRTA41NM E2WE 20040319000942004031900094WP 2004 3 19 DXTA200400255 220040304A7200TFE7315BR ENGINE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 1 FAILED E DXTAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 GL07872QS2900 258472 P107495 ON TAKEOFF, NR 1 ENGINE FAILED WITH A LOUD BANG JUST AFTER LIFTOFF, THE ENGINE SLOWED DOWN VERY QUICKLY AND SHOWED NO N1 ROTATION. ACCOMPLISHED AIR TURNBACK TO MSY AND LANDED WITHOUT INCIDENTS. INSPECTED NR 1 ENGINE FAN BLADES, FOUND NO DAMAGE. INSPECTED CASTINGS, FOUND NO DAMAGE. INSPECTED EXHAUST AND FOUND LAST STAGE OF LOW PRESSURE TURBINE MISSING 1 INCH - 1.5 INCH OFF OF ALL BLADES. REMOVED AND REPLACED NUMBER 1 ENGINE IAW HAWKER 800XP M/M CHAPTER 71-00-01 AND 71-00-02. 2L72 4F4 FRTA3EU E6WE 20040330000492004033000049EU 2004 3 30 2004UALA00252 120040317A5320 FLOOR SUPPORT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29411UA 464 AFT CABIN FLOORBOARD SUPPORT STRUCTURE AT RBL 46 IS CORRODED AT 2 LOCATIONS BETWEEN FRAMES 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SUPPORT STRUCTURE. 2L72 4F4 FRTA28NM E40NE 20040409000552004040900055 2004 4 9 2004UALA00286 420040228A2565 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 DOOR FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29174UA 24381 DOOR 2 RIGHT SLIDE FAILED OVER PRESSURE TEST AT 3.80 PSI DURING OVERHAUL. SLIDE OEM ANALYSIS OF FAILURE WAS INCONCLUSIVE. INFLATABLE PORTION OF SLIDE SCRAPPED. 2L74 4F4 FRTA20WE E24NE 20040329001362004032900136EU 2004 3 29 2004UALA00197 120040307A3260 UPLOCK AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE LT MLG DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29414UA 472 RETURN TO FIELD DUE TO LEFT MAIN GEAR NOT LOCKED INDICATION. REPLACED MLG UPLOCK ASSEMBLY AND PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION OF THE LANDING GEAR. 2L72 4F4 FRTA28NM E40NE 20040412000962004041200096SO 2004 4 12 SWIA200413080 120040228A5411 FRAME EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE RT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07216SW 120285 RIGHT NACELLE FRAME ONE CRACKED ON INBOARD AND OUTBOARD SIDES. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME ONE IAW 120 SB 120-54-0036 PART II AND 120 SRM 51-10-02 PG 3 PAR 3, ACCOMPLISHED PART II OF SB 120-54-0036. 2L72 4T4 TRTA31SO E20NE 20040421000112004042100011GL 2004 4 21 ALGA094198 220040419A725023053299 TURBINE WHEEL CLARK 1000 1000CLARK 2230102SW ALLSN 250C 250C30S 03013GL ENGINE OUT OF TOLERANCEE ALGAO OTHER L NO TEST NRNOT REPORTED 1 SW03PARTO FOUND FLOW AREA BELOW MIN. EFA 5.770. RETURNING PART TO VENDOR FOR WARRANTY CREDIT. 1Q71 3R3 U 2A6 E1GL 20040422001272004042200127 2004 4 22 DFJ2004F00000 420040315A6122 FITTING BEECH 76 76 1153005CE LYC O360 LO360A1G6 41514EA HARTZLHCM2Y HCM2YR GL GOVERNOR LEAKING E DFJAO OTHER K FLUID LOSS NRNOT REPORTED 1 CE036023E 1760628N ME179 L38971A FB808 FOUND PROPELLER GOVERNOR OIL LINE FITTING LEAKING OIL. CAUSED WHITE SMOKE IN FLIGHT DUE TO OIL LEAKING ON EXHAUST. POSSIBLE CAUSE, FITTING NOT PROPERLY TORQUED AT PROPER GOVERNOR OVERHAUL. RECOMMEND CHECKING TORQUE OF FITTING ON INSTALLATION OF PART. 1L72 3O3 O A29CE 1E10 5 CP43GL 20040423000082004042300008SO 2004 4 23 SIMA200406804 120040306A27303621005009 CONTROL UNIT EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL HORIZONTAL STAB INOPERATIVE A SIMAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW21811AE 145529 RECEIVED PITCH TRIM, .5 INOPERATIVE MESSAGE. CW ETN EB-27-0022R1 AND REPLACED HSCU OPS CHECKED GOOD. AC RETURNED TO SERVICE. (SW21200404959) 2L72 4F4 FRTT00011ATTE6CH 20040426000862004042600086NE 2004 4 26 ABXA040111 220040317A732171128726 FUEL CONTROL DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 4 ENGINE DEFECTIVE A ABXAO OTHER J WARNING INDICATION CRCRUISE 1 GL23812AX 156 46126 671139 NR 4 ENGINE, AFTER SETTING POWER FOR CRUISE, NR 4 ENGINE ROLLED BACK .15 EPR. EGT, FUEL FLOW N1 AND N2 ALL DROPPED. THROTTLE DID NOT MOVE. REPLACED NR 4 ENGINE FUEL CONTROL UNIT IAW 73-20-01. REPLACED NR 4 LOW PRESSURE FUEL FILTER. PERFORMED LEAK CHECK OF NR 4 ENGINE LOW PRESSURE FUEL FILTER ON ENGINE RUN. LEAK CHECKED GOOD. 2L74 4F4 F 4A25 1E8 20040430000462004043000046NE 2004 4 30 ASMF200404013 220040419A732076960615 FCU DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED W ASMFD RETURN TO BLOCK M OVER TEMP TXTAXI/GRND HDL 1 SW23803ML8991 928 49726 728169 AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HIGH TEMPERATURE AND EGT OSCILLATIONS ON ENGINE NR 2. AIRCRAFT WAS SENT TO THE HANGAR. THE LEFT FUEL CONTROL UNIT (FCU) WAS REPLACED IAW MM 73-20-01, TEST CORRECT. 2L72 4F4 FRTA6WE E9NE 20040426001152004042600115NM 2004 4 26 2004UALA00334 120040413A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME STA 1520 INNER FLANGE HAS DENT BELOW STR 25L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040518000652004051800065SW 2004 5 18 N431MA 120040210A6330222331617103 MOUNT BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE M/R GEARBOX DEBONDED E A1UAA UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 CE03431MA 47504 4703747159 ENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAINTENANCE FOR REPAIRS. AFTER TROUBLESHOOTING FOUND LATERAL ISOLATION MOUNT DE-BONDED. REMOVED AND INSTALLED SERVICEABLE UNIT. 1G72 3U3 U H9SW E5NE 20040528000272004052800027EU 2004 5 28 MALA040407 120040505A3350330131 BATTERY SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422XJ 340B422 UNIT FAILED ON WING CAPACITY CHECK. BATTERY POWER SUPPLY PN 3301-51 SN/1389, BATTERY FAILED CAPACITY CHECK ON BENCH. REPLACED BATTERY PN 3301-31 AND UNIT PASSES CMM CHECK. A/C RETURNED TO SERVICE 5/12/04. REFER TO IN HOUSE WO NR 367863 FOR ADDITIONAL INFORMATION. 2L72 4T4 TRTA52EU E8NE 20040608000842004060800084NE 2004 6 8 UIEA200400089 220040504A7200 ENGINE BOEING747 747228F 1384895NM GE CF6 CF650E2 30018NE NR 3 MALFUNCTIONED A UIEACE ABORTED TAKEOFF ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 EA15536MC 21576 PRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SET, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KNOTS, NR 3 ENGINE HAD 'BACKFIRED WITH A LOUD NOISE', WITH REDUCTION IN N1 RPM OF ABOUT 10-15 PERCENT AND PEAK EGT OF APPROX 920 DEG C WHILE OTHER ENGINE EGT WERE APPROX 800 DEGREES CELSIUS DISCONNECT THE TAKEOFF, AND S/D THE ENGINE ON WAY BACK TO RAMP. CHECKED INLET AND EXHAUST AREAS FOR DAMAGE AND FOD, NONE FOUND. VISUALLY INSPECTED SVS/VBV RIG CHECK IAW MM 75-30-00/75-31-02. NIL DISCREPANCIES. LOCKED OUT HIGH STAGE VALVE FOR TROUBLE. SHOOTING PERFORMED TAKEOFF POWER ROLL TO 80 KTS. ENGINE PERFORMANCE TO 112 PERCENT N1 NORMAL ON TWO RUNS. 2L74 4F4 F A20WE E23EA 20040608001412004060800141EU 2004 6 8 USAA040194 120040507A5311D5347218820200 FRAME AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19703UW 0904 FRAME, 1.5 INCHES L X 2.0 INCHES W AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, Y1292, C68, Z240. REMOVED AND REPLACED FRAME IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040614001572004061400157EU 2004 6 14 ULX2004F00012 120040301A2435150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENGINE FAILED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01230LA2550 284 3318 NO OUTPUT; OVERLOADED, CAUSING ARMATURE SHORTING, BRUSHES DESTROYED. MONITOR ELECTRICAL LOAD. 1G71 3U3 U H9EU E19EU 20040618001122004061800112EA 2004 6 18 ASOA04337 120040507A3350BF50390901 LENS CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE EMERGENCY LIGHT CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27707EV 10057 DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR. 2L72 4F4 FRTA21EA E15NE 20040618001062004061800106EU 2004 6 18 ASOA04394 120040531A3350LP1670 LAMP AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27640AS 405 DURING A GROUND INSPECTION IN VPS, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 6 A/B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT LAMP AT ROW 6 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20040712001962004071200196NM 2004 7 12 ASMF200406020 120040619A3240 BRAKE ASSY DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE AUTOBRAKE INOPERATIVE W ASMFLA ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SW23158PL 49761 AIRCRAFT PERFORMED TWO MISSED APPROACHES AND IT WAS SENT TO ACA TO UNSCHEDULED LANDING FOR REFUELING AND FOR INSTRUCTIONS OF AIR TRAFFIC CONTROL. DURING TRANSIT CHECK, CAPTAIN REPORTED AUTO BRAKE SYSTEM OUT OF SERVICE AND "AUTO BRAKE FAIL" LIGHT TURNED ON. SYSTEM WAS DEFERRED IAW MEL 32-9. 2L72 4F4 FRTA6WE E2EA 20040628001582004062800158NM 2004 6 28 HNAA0400057 120040525A712087110047001 MOUNT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07931HA 132 NR 1 ENGINE INBOARD AFT ENGINE MOUNT STRUT IS CRACKED AT UPPER WELD AREA. REMOVED AND REPLACED STRUT. 2H72 4T4 TRTA13NM E20NE 20040812000082004081200008NM 2004 8 12 AWXA200400760 120040615A532065516989 SPLICE BOEING737 7373S3 1384711NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 4 LT MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 907, STR 4 LT; FABRICATED A NEW REPLACEMENT SPLICE IAW DWG 65-51698-9; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARA 4-B AND 7-A. 2L72 4F4 FRTA16WE E2GL 20040813001622004081300162NM 2004 8 13 2004UALA00647 120040708A5310 CREASE BEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 CREASE BEAM BETWEEN BS 960 AND 984 AND RBL 64R TO 70R CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR DOUBLER. 2L72 4F4 FRTA2NM E17NE 20040722000402004072200040CE 2004 7 22 JEM2004F00005 120040617A551145A210853 RIB BEECH MU300 400A 1155402CE PWA JT15 JT15D1 52060NE HORIZONTAL STAB CRACKED B JEMRO OTHER O OTHER NRNOT REPORTED 1 CE01250AJ RK23 DURING A SCHEDULED INSPECTION OF THE HORIZONTAL STABILIZER SIDE ROLLER BRACKET ASSY AND AREA, IT WAS DISCOVERED THAT THE SUPPORTING BRACKETS BEHIND THE RIB AS WELL AS THE RIB ON THE LT AND RT SIDE ROLLER BRACKET WERE CRACKED. THE INSPECTION WAS ACCOMPLISHED USING A BORESCOPE AND INSERTING THROUGH THE DRAIN HOLE NEAR THE SIDE ROLLER SUPPORT BRACKETS, THE FOLLOWING PARTS WERE CHANGED: 1) 45A21146-6, 2) 45A21146-5, RIBS: 3) 45A2186-3, 4) 45A21086-4, 5) 45A21085-3, 6) 45A21085-4. 2H72 4F4 FRTA16SW E1NE 20040816001542004081600154NE 2004 8 16 2004UALA00602 220040622A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 FAILED A UALAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF A FLAME/FIRE TOTAKEOFF 1 WP29411UA 464 ON TAKEOFF ROLL, APPROX 20 TO 30 KTS, HEARD LOUD POP & RT YAW. TAKEOFF ABORTED. ANOTHER AIRPLANE REPORTED NR 2 ENGINE WAS ON FIRE. SHUTDOWN NR 2 ENGINE AND FIRED THE BOTTLE. 3RD STAGE COMPRESSOR BLADE FAILED DUE TO PREVIOUS FOD. REPLACED NR 2 ENGINE. OPERATIONS CHECK NORMAL. OEM IS WORKING ON A REDESIGN OF THIS BLADE AND ITS MID-SPAN SHROUD. 2L72 4F4 FRTA28NM E40NE 20040812000552004081200055EU 2004 8 12 2004UALA00700 120040728A3350 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE SEAT 15ABC INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29427UA 512 EEL LIGHTS ON SEATS 15ABC AND 24ABC ARE INOPERATIVE. REPLACED LIGHT ASSY. OPERATIONS CHECK NORMAL. 2L72 4F4 FRTA28NM E40NE 20040813000362004081300036EU 2004 8 13 04FDEA02338 120040801A5250 TEE FITTING AIRBUS310 A310 EU GE CF6 CF6* 30020GL COCKPIT DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25412FE 360 REF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-15, 51-40-20, AND 51-75-10 2L72 4F4 FRTA35EU E23EA 20040818001202004081800120SW 2004 8 18 ALGA096403 120040720A6210206015001109 BLADE BELL 206 206L4 1182110SW ALLSN 250C 250C20 03013GL MAIN ROTOR SEPARATED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03206DB2097 52127 FOUND CORROSION AND SEPARATION AT SKIN/SPAR INTERFACE NEAR LOWER OB GRIP FINGER DOUBLER. REMOVED AND REPLACED DEFECTIVE BLADE WITH NEW BLADE. SCRAPPED DEFECTIVE BLADE. 1G71 3U3 UNCH2SW E4CE 20040907001342004090700134NM 2004 9 7 P5CA0401173 120040717A2432 CHARGER BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE MAIN BATTERY SMOKE A P5CAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP23508MC 21644 SMOKE IN COCKPIT. MAIN BATTERY CHARGER FAULTY. SWAPPED MAIN CHARGER WITH APU CHARGER, OPS CHECK OK PER AMM 24-31-00. DEFERRED APU BATTERY CHARGER PER MEL 24-24. 2L74 4F4 F A20WE E23EA 20040908000812004090800081SO 2004 9 8 C2XA04TY130 120040802A531014521699003 SUPPORT BEAM EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL GALLEY CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION SIGNS OF CORROSION WERE FOUND ON SEVERAL NUTPLATES ON SUPPORT BEAM IN THE GALLEY. MAINT. REMOVED AND REPLACED ALL TOP CAPS IN THE GALLEY AREA IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 4C INSPECTION. 2L72 4F4 FRTT00011ATTE6CH 20040830000272004083000027EU 2004 8 30 04FDEA02565 120040826A5310 DOOR FRAME AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25677FE 791 AFT CARGO DOOR CUTOUT ON LOWER FWD FRAME, NOTED GOUGES/DAMAGED SURFACE APPROX 13 INCHES LONG. GOUGES RANGE FROM .080 INCH TO .2 INCH. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW A300/600 SRM 53-17-12. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW A300/600 SRM 53-17-12. 2L72 4F4 FRTA35EU E13NE 20040901000342004090100034SO 2004 9 1 C2XA04SH473 120040731A33503025103 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007C GL LT OVERWING INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716976 145171 DURING C CHECK THE PANEL 195 LT LATERAL WING TO FUSELAGE FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE EMERGENCY LIGHT IAW 145 AWM 20-50-00. THE LIGHT OPERATIONAL CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040913001582004091300158WP 2004 9 13 DHL2004804531 120040725A5753 SKIN DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT WING FLAP WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 LT WING IB FLAP UPPER SKIN WORN XW 91.000 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW ED EDW 27-4, DWG W27-R04 REV. IR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED PLATING SEGMENT IAW ED EDW 27-4, DWG W27-R04. FABRICATED NEW PLATING SEGMENT (AL 2024-T3 0.040), INNER STRAP (AL 2024-T3 0.050) IAW ED EDW 27-4, DWG W27-R04. CLEANED, TREATED AND PRIMED AREA, PLATING AND INNER STRAP INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG.9. INSTALLED NEW PLATING SEGMENT AND INNER STRAP WITH NEW FASTENERS IAW ED EDW 27-4, DWG W27-R04, SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. 2L74 4F4 FRT4A25 E2GL 20040914001422004091400142NM 2004 9 14 UIEA200400113 120040616A2821AD92272450 FUEL FILTER BOEING747 747243B 1384830NM GE CF6 CF650E2 30018NE NR 1 ENGINE CONTAMINATED A UIEAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 EA15518MC 23476 NR 1 ENGINE FAILED DURING CRUISE, FLIGHT LEVEL 350, .84 MACH, NORMAL FLIGHT. FOLLOWED PROCEDURES AND ATTEMPTED TO RESTART ENGINE WITH NO SUCCESS. ACCOMPLISHED ENGINE INLET AND EXHAUST INSPECTION ALL NORMAL. REPLACED NR 1 ENGINE FUEL FILTER IAW MM, LEAK CHECK, OK. ON ENGINE RUN UP, CHECKED CDP TUBES, TUBE DRAIN, HOLES, AND MEC CDP PORT FOUND ALL OK. ACCOMPLISHED MPA ENGINE RUN IAW MM. , THES NR 5, ALL PARAMETERS NORMAL. 2L74 4F4 F A20WE E23EA 20040913001862004091300186NM 2004 9 13 WLDA200479 120040802A5510ALC8101504 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER LT BARREL NUT HOLE NR 13.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB LT BARREL NUT HOLE NR 13 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040907001512004090700151NM 2004 9 7 2004UALA00745 120040806A3350 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE GALLEY INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29343UA 24247 FWD GALLEY EEL FLOOR LIGHT INOPERATIVE. REPLACED EEL GALLEY FLOOR STRIP. 2L72 4F4 FRTA16WE E2GL 20040913001552004091300155NM 2004 9 13 DHL2004745507 120040702A5330 SKIN BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT FUSE HAS A DENT AFT BS 1030 STR 25L. DAMAGED FWD TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1; FABRICATED DOUBLE (10.2500 INCH X 7.7500 INCH) 2024 T3 0.71 PO NR 900790, FILLER (2.1250 INCH X 1.7500 INCH) 2024 T3 0.63 PO NR 900781 IAW SRM 53-30-3 FIG 3 AND CUT OUT DAMAGED AREA AT STR NR 25L BS 1038 DIMENSION (2.1250 INCH X 1.7500 INCH); TREATED AND PRIMED IAW SRM 51-10-2; INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 3. 2L73 4F4 F A3WE E2EA 20040914000662004091400066EU 2004 9 14 YENA200444 120040819A2120 ODOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN DETECTED A YENAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA15542JB 1802 CABIN CREW AND PASSENGERS SMELLED A BURNING ODOR LIKE PLASTIC OR CABLES BURNING IN THE MIDDLE PORTION OF THE CABIN DURING OUR DESCENT. INFO NOTICE 2004-TO23TR COMPLIED WITH NO DEFECTS NOTED. INSPECTED CABIN, COCKPIT, CARGO AND AVIONICS COMPARTMENTS IAW 24-00-00-810-823, NO DEFECTS NOTED, A/C OK FOR SVC. 2L72 4F4 FRTA28NM E40NE 20040914000962004091400096CE 2004 9 14 DJFA2004012 120040725A3411 PITOT TUBE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE RT AIRSPEED CONTAMINATED E DJFAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 EA23283CW 5500713 AIRCRAFT DEPARTED AND DURING TAKEOFF ROLE AT ABOUT 50 KTS THE PILOTS NOTICED THE RT AIRSPEED WAS STILL AT 0. THEY ABORTED TAKEOFF AND RETURNED. THE MAINTENANCE PEOPLE CLEANED A BUG FROM INSIDE THE PITOT TUBE AND PERFORMED A HIGH SPEED TAXI WITH BOTH AIRSPEEDS WORK OK. 1L72 4F4 F A22CE E1NE 20040917001302004091700130NM 2004 9 17 AALA20040900 120040823A21216067727 FAN BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE RECIRCULATION FAILED A AALAO OTHER AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW21663AM 25297 ON LANDING RT RECIRCULATION FAN FAILED AT TOUCHDOWN AND ON TAXI IN SMOKE IN CABIN AND UNABLE TO CLEAR. FOUND EVIDENCE OF A FIRE IN THE CENTER EQUIPMENT BAY THAT BURNED THE INSULATION BLANKETS IN THE BAY. REPLACED THE RT RECIRCULATION FAN, AND THE BURNED INSULATION BLANKETS. REPLACED THE RT RECIRCULATION FAN CIRCUIT BREAKER AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 FRTA2NM E12EU 20040923000792004092300079EU 2004 9 23 KBM2004F00184 120040724A2110 CLUTCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE A/C COMPRESSOR INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19966SH350 6893186330 3787 A/C CLUTCH INOPERATIVE. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040923000812004092300081CE 2004 9 23 HYTA2004007 120040802A5711 SPAR CESSNA208 208B 2073701CE PWA PT6 PT6* 52043EA WINGS CHAFED E HYTAO OTHER O OTHER NRNOT REPORTED 1 AL01976E 208B0976 LOWER SURFACE OF LT AND RT FORWARD WING SPARS AND LIFT STRUT ATTACH FITTINGS HAVE BEEN CHAFED BECAUSE OF CONTACT WITH THE LIFT STRUT UPPER FAIRING/COVER. WORST DAMAGE WAS LESS THEN .005 INCH IN DEPTH AND WAS EASILY BLENDED OUT. APPLIED VINYL CHAFE TAPE TO SPAR AND STRUT FITTINGS TO PREVENT REOCCURRENCE. CAB02-2 REV 1 ADDRESSES THIS CONDITION BUT DOES NOT INCLUDE THIS S/N AIRPLANE. IT APPEARS THAT MFG CHANGED THE RIVET PATTERN IN THIS FAIRING/COVER ASSEMBLY, P/N 2621012-54 AND 55 ON LATER S/N AIRPLANES TO AVOID DAMAGE CAUSED BY RIVET HEADS. BUT FURTHER REDESIGN MAY BE NECESSARY TO ELIMINATE THE PROBLEM. APPLICATION OF CHAFE TAPE EFFECTIVELY PREVENTS DAMAGE. (M) 1H71 3T3 T A37CE E2NE 20040923001482004092300148NM 2004 9 23 2004UALA00783 120040723A5754 SKIN BOEING BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLAT BIRD STRIKE A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA A20401 26693 OUTBOARD END L/E SKIN DAMAGED BY BIRD STRIKE. REPLACED SECTION OF L/E SKIN. 2L72 4F4 FRTA2NM E17NE 20040928000522004092800052EA 2004 9 28 COMA0460527 120040901A7714 SENSOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT ENGINE INTERMITTENT A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01819CA 7415 LT ENGINE N1 FLUCTUATING BETWEEN 80 AND 86 PERCENT. COULD NOT DUPLICATE. CLEANED T2 SENSOR WIRING CONNECTOR. OPERATIONAL CHECK NORMAL. 2L72 4F4 FRTA21EA E15NE 20040922000982004092200098NM 2004 9 22 04FDEA02700 120040916A5510 STRUCTURE DOUG MD11 MD11 3023602NM GE CF6 CF680C2D1F 30025NE ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 CORROSION REMOVED ON 31R BARREL NUT BORE FOUND EXCEEDED LIMIT IAW EO 1-5510-7-5000 C3 PT1 FIG 03. RT HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31R, REPAIRED AS PER EA 1-5510-81555. 2L73 4F4 FRTA22WE E31N3 20041001000222004100100022WP 2004 10 1 0WX0400034 120040922A3350 POWER SUPPLY DOUG DC9 DC983 3022083WP PWA JT8 JT8D NE EMERGENCY LIGHT INOPERATIVE A WX0AK NONE O OTHER ININSP/MAINT 1 WP19862GA 49556 MAINTENANCE REPORTED OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 31 AND 35 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM REF 33-53-01. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA6WE E2EA 20041005000072004100500007SO 2004 10 5 C2XA04TY114 120040723A532014529696001 PLATE EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION AT FR 59 STR 19R,THE WATER SERVICE BASE PLATE, CORROSION WAS FOUND ON THE RIVETS. MAINTENANCE CLEANED THE EFFECTED AREA, BLENDED, ALLODINED, PRIMED, PAINTED AND APPLIED CORROSION INHIBITOR COMPOUND. ALL WORK WAS ACCOMPLISHED IAW CPM 51-01-00; SRM 51-10-03;04;05 AND CPM 51-61-00. A/C WILL BE RELEASED UPON COMPLETION OF THE 4C INSPECTION. 2L72 4F4 FRTT00011ATTE6CH 20041014001402004101400140NE 2004 10 14 ASOA04669 220040901A7320 EEC AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE MALFUNCTIONED A ASOAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO11532AS 458 DURING INITIATION OF DESCENT INTO DHN FROM ATL, AT APPROXIMATELY 14,000 FT WHEN PILOT PULLED POWER LEVERS BACK, LT ENGINE LEVER STUCK AT FIFTY FIVE DEGREES. PILOT LEVELED A/C OFF AT 13,700 FT & COMPLIED WITH QRH. PILOT PULLED HARD ON POWER LEVER TO MOVE IT TO FLT IDLE AN IT PULLED FREE. AT APPROX 3,500 FT WITH BOTH POWER LEVERS IN FLT IDLE LT ENGINE AGGRESSIVELY SURGED MULTIPLE TIMES. PILOT SHUTDOWN LT ENG, DECLARED AN EMERGENCY & A/C LANDED SAFELY IN DHN. MX INSPECTED LT ENG TELEFLEX CABLE & TURTLE BACK FOR BINDING, INTERROGATED LT ENG PCU AND EEC, PERFORMED LT ENG TRIM IAW ATR JIC 76-00. GROUND RAN LT ENG IN MULTIPLE CONFIG & BLEED CONFIG. NO DEFECTS NOTED. OPS CHKS GOOD. A/C OK FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 20041007000022004100700002EU 2004 10 7 CALA0400670 220040609A73201853M56P07 HMU BOEING737 737924 13848A1NM CFMINTCFM56 CFM562AFR 13802EU NR 2 ENGINE FAILED A CALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW27754107863 30127 AFTER TAKEOFF ABOUT 800 FT MSL HAD LARGE BANGING NOISE. APPEARED TO BE COMPRESSOR STALL IN NUMBER TWO ENGINE. SMALL DECREASE IN N1 NOTED. LANDED WITHOUT INCIDENT. COMPLIED WITH FIM 71-05 TASK 804 PARA A-E, NO FAULTS NOTED. REPLACED NUMBER TWO HMU AND PERFORMED REPAIR CONFIRMATION. ALL CHECKS WERE GOOD. PERFORMED BOROSCOPE OF ENGINE FOR ANY DAMAGE. NONE NOTED. 2L74 4F4 FRTA16WE E21EU 20041021000682004102100068EA 2004 10 21 VNAA0410006 120041009A5240 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE O2 SERVICING OPEN A VNAAO OTHER O OTHER CLCLIMB 1 GL05249PS 7926 ON CLIMBOUT CREW REPORTED A LOUD SQUEAL FROM THE RIGHT FORWARD SECTION OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND THE OXYGEN SERVICING DOOR OPEN. MAINTENANCE CLOSED THE DOOR AND PERFORMED A DETAILED VISUAL INSPECTION PER THE SRM. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041020001622004102000162NM 2004 10 20 04FDEA02879 120041005A5753ARC05021 HINGE DOUG DC10 DC10 N/A-SDRNM GE CF6 CF66D 30020GL ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25392FE 46626 LT WING OB FLAP IB HINGE, LOCATION NR 6, OB BORE IS CORRODED. REMOVED CORROSION, BEGINNING BORE DIAMETER 1.240, FINAL 1.266, MATERIAL LOSS 0.026 IAW DAC CMM 57-44-08, ETCH INSPECTED IAW DAC CMM 57-44-08 AND 20-11-02. PEENED IAW DAC CMM 57-44-08 AND 20-11-01.PRIMED IAW SRM 57-21-01 VOL II, FABBED BUSHING IAW DAC CMM 57-44-08 EA 8-5750-81470. CAD PLATED BUSHING IAW CMM 57-44-08 AND 20-10-01. INSTALLED AND HONED BUSHING IAW CMM 57-44-08. REF NON-ROUTINE NR N00564 2L73 4F4 FRTA22WE E23EA 20041101000732004110100073NM 2004 11 1 2004UALA00906 120040911A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 AFT PIT MAIN FRAME STA 1400, STR 25L TO 26L DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041102001172004110200117NM 2004 11 2 DL764040994 120041027A3350767 BULB BOEING767 767432ER 1385134NM GE CF6 CF680C2B7 NE EMERGENCY LIGHT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27836MH 29709 R1 EXTERNAL EMERGENCY LIGHT INOPERATIVE RELAMPED ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F4 FRTA1NM E13NE 20041119000402004111900040GL 2004 11 19 KBM2004F00222 220040904A7321EA470B3588 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE INACCURATE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19188TV 2704 FUEL SENDER NOT TRANSMITTING CORRECT QUANTITY. INSTALLED NEW UNIT. 1G71 3U3 U H2SW E4CE 20041103000302004110300030NE 2004 11 3 04057 220041027A7230 COMPRESSOR BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE STALLED A KCSAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 GL23716CK 19753 662566 NR 2 ENGINE COMPRESSOR STALLED IN FLT AT FL26,600 FT. EPR DECREASED AND EGT INCREASED. RETARDED THRUST LEVER, EGT DECREASED, PEAK EGT 895 DEGREES. PERFORMED ENGINE STALL INFLT CHECK. PERFORMED RAPID RESTART CHECK. N1 RPM DID NOT INCREASE AFTER RESTART WITH THRUST LEVER. PERFORMED IN FLT ENG. FAILURE/SHUTDOWN QRH-67. 2L74 4F4 F A20WE E20EA 20041102000692004110200069NE 2004 11 2 2004F00420 220040907A732032448716 HMU AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE ERRATIC A SIMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SW21414WF 127084 127084 ABORTED TAKEOFF DUE TO LEFT ENGINE NR 1 ITT WENT TO 771 DEGREES. REMOVED AND REPLACED LEFT ENGINE HYDROMECHANICAL UNIT. (M) 2H72 4T4 TRTA53EU E20NE 20041103001302004110300130SO 2004 11 3 MYN2004F00002 120041017A554051094 TORQUE TUBE PIPER PA31T PA31T1 7103126SO PWA PT6 PT6* 52043EA RUDDER CORRODED B MYNRO OTHER O OTHER NRNOT REPORTED 1 GL11300SR2310 31T8104022 FOUND RUST/CORROSION AND WATER STAIN, INDICATING WATER HAD ACCUMULATED TO A LEVEL OF MORE THAN 1 INCH AT THE BOTTOM RIB, FORE AND AFT OF THE SPAR. SB 1105A. TREATED CORROSION AND INSTALLED NEW TORQUE TUBE ASSEMBLY. 1L72 3T3 T A8EA E2NE 20041116000542004111600054NE 2004 11 16 AWXA200401023 220040913A7200 LINE BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE NR 2 ENG SENSE CHAFED A AWXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP28913AW240942477 22207 ON CLIMB-OUT EN ROUTE, NR 2 ENGINE WOULD NOT PRODUCE FULL CLIMB POWER, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MX TROUBLESHOT NR 2 ENGINE AND FOUND P1 SENSE LINE ATTACHED TO RT UPPER INLET COWL CHAFED THROUGH CAUSING LOW EPR READING, ALSO FOUND WIRE HARNESS IN SAME AREA CHAFED AND BEYOND REPAIR. R & R NR 2 ENGINE INLET COWL IAW BMM (DAMAGED PARTS ATTACHED TO COWLING). ENGINE RUN AT TAKEOFF POWER GOOD, BOTH ENGINES EPR MATCH. REPLACED CHAFED P1 AIR TUBE ON RT UPPER INLET COWL. DURING EXAMINATION OF CHAFED P1 PROBE WIRE HARNESS ASSY A SMALL WIRE FOUND BROKEN IN TWO AS WELL AS A SMALL AREA WHERE INSULATION WAS WORN, REPAIRED BROKEN AND CHAFED WIRES IAW SWPM 20-10-13. 2L72 4F4 FRTA2NM E12EU 20041124001512004112400151CE 2004 11 24 E812004F00009 120040908A3233 LOCK LEAR 60 60LEAR 5170707CE PWA 305 PW305A 52128NE ROD END DAMAGED B E81RO OTHER O OTHER NRNOT REPORTED 1 GL03253FX KL00015 241 CREW REPORTED MAIN GEAR DOORS WOULD NOT CLOSE AFTER LANDING GEAR RETRACTION. FOUND LT MLG NOT FULLY RETRACTING DUE TO ACTUATOR ROD END AND OUTER PISTON BEING LOOSE WHICH CAUSED ACTUATOR OVERALL LENGTH TO INCREASE. FOUND ROD END LOCK KEY OUT OF SLOT IN OUTER PISTON, APPROX 0.25 INCH GAP BETWEEN END OF OUTER PISTON AND JAMNUT. JAMNUT TO LOCK KEY SAFETY WIRE INTACT. TIGHTENED OUTER PISTON, ROD END, AND JAMNUT, AND ADJUSTED ACTUATOR IAW LT 60 MM 32-31-01. LANDING GEAR OPERATIONS NORMAL THROUGH SEVERAL CYCLES. 2L72 4F4 FRTA10CE E35NE 20041124000902004112400090EA 2004 11 24 A6WA200440147 120041011A2410 IDG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 MALFUNCTIONED A A6WAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 GL31417AW 7610 GEN NR 2 FAIL CASS MESSAGE FOLLOWED BY GEN 1 CASS MESSAGE. GEN NR 1 AND 2 RESET OPS NORMALLY. APU WAS RUNNING AND GEN OPS NORMALLY. SERVICED BOTH IDG IAW AMM 12-13-24. OPS CHECK GOOD. OK FOR SERVICE. NO LEAKS NOTED. NR 1 ENG 11 PUMPS AND NR 2 ENGINE 25 PUMPS. 2L72 4F4 FRTA21EA E15NE 20041130001312004113000131NE 2004 11 30 DLM88041036 220041116A7314 SHAFT 739001288 DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE FUEL PUMP SHEARED A DALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO27909DL 9749 49540 725661 EN ROUTE TO SDF NR 1 ENGINE FLAMED OUT. FOUND FUEL PUMP SHAFT SHEARED. REPLACED FUEL PUMP AND CONTROL. 2L72 4F4 FRTA6WE E9NE 20041207001032004120700103NM 2004 12 7 USAA040836 120040915A53201123579 ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 ZEE ANGLE, 6 INCHES BY 4 INCHES AREA, CORROSION, LEVEL 1; TASK NR C53-107-01, RT AFT ZEE ANGLE FROM STA 940-990. DEFECTIVE PART REPLACED WITH IDENT PN. 2L72 4F4 FRTA16WE E21EU 20041208001672004120800167GL 2004 12 8 RAIA00411019 220041117A7200AE3007A ENGINE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A RAIAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 CE03846HK332 14500855 312688 ORD - SMOKE IN CABIN AREA. MAINTENANCE REMOVED AND REPLACED NUMBER 1 ENGINE. 2L72 4T4 FRTT00011ATTE6CH 20041215000692004121500069WP 2004 12 15 ASAA0480495 120040924A5347593054787 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC, C-CHECK- PAX CABIN GALLEY 2 OB FLOOR ATTACH TRACK HAS CORROSION AT STA 237. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION OF SEAT TRACK IAW SRM 51-30-5. 2L72 4F4 FRTA6WE E9NE 20041215001202004121500120NM 2004 12 15 ASAA0410477 120041104A71106585378335 CAP BOEING737 737210C 1384459NM PWA JT8 JT8D17 52049NE ENGINE COWLING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02744AS 21822 SEA - IB CAP CRACKED AT 6 O`CLOCK POSITION. REPAIRED IAW EA. 2L72 4F4 F A16WE E2EA 20041221002022004122100202NM 2004 12 21 USAA040925 120041101A5347 SEAT TRACK BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41420 24557 PIT - Q1 - SEAT TRACK, .75 INCH LONG CRACK, IB RT SEAT TRACK STA 727B, UPPER FLANGE LOWER SURFACE AT VERTICAL RADIUS. CUT OUT SECTION AND REPLACED NEW AND DOUBLERS IAW SRM 53-00-52. 2L72 4F4 FRTA16WE E21EU 20041222000332004122200033NM 2004 12 22 2004UALA01205 120041211A5330 STRAP BOEING757 757222 1384956NM PWA 2037 PW2037 NE SKIN CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29579UA 26697 AFT PIT STA 1400 TEAR STRAP BETWEEN STRINGERS 28R & 29R CORRODED. FABRICATED & INSTALLED TEAR STRAP. 2L72 4F4 FRTA2NM E17NE 20041227000212004122700021NM 2004 12 27 2004UALA01120 120041112A5330 BEAR STRAP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BS ABOVE STR DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29301UA 23642 REPAIR AT AFT CARGO DOOR BEAR STRAP BS 807 ABOVE STR 25 RT AT CARGO DOOR OPENING IS INSUFFICIENT. FABRICATED EXTERNAL DOUBLER,TRIPLER AND FILLER AND INSTALLED, 2L72 4F4 FRTA16WE E2GL 20041227000282004122700028NM 2004 12 27 2004UALA01165 120041129A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 FLOORBEAM AT STA 365 BL0 TO RBL15 CORRODED. REMOVED CORROSION AND INSTALLED FLOOR BEAM REPAIR. 2L72 4F4 FRTA2NM E17NE 20050106002092005010600209EU 2005 1 6 ASAA0440167 220041004A7200CFM563C1 ENGINE BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU NR 1 ENGINE FAILED A ASAAEA ENGINE SHUTDOWN UNSCHED LANDING EM VIBRATION/BUFFET OVER TEMP CRCRUISE 1 NM02709AS401426826 28896 ENROUTE, AT 35,000 FT, APPROX .75 PWR, NR 1 ENG INDICATIONS BECAME ERRATIC (NO EXCESSIVE VIBRATION INDICATED ON VIB METER). F/A HEARD LOUD BANG JUST BEFORE FLT CREW HEAR A THUD. IN A FEW SECONDS, ENG OVERTEMPED (APPROX 982 DEGREES C) PERFORMED EMERGENCY SHUTDOWN AND DID NOT FIRE BOTTLES. ACCOMPLISHED SINGLE ENG LANDING. REMOVED AND REPLACED ENGINE. 2L72 4F4 FRTA16WE E21EU 20050104000472005010400047EU 2005 1 4 ASOA04867 120041005A5343S5357810420100 TRUSS AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE RT MLG TRUSS AT FS 26 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT MLG TRUSS AT FS 26 IAW EO 72-53-0157. 2H72 4T4 TRTA53EU E20NE 20050110001392005011000139NM 2005 1 10 USAA040972 120041111A5711 SPAR BOEING737 737301 1384611NM CFMINTCFM56 CFM563B1US GL LT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - LT SPAR UPPER CHORD, .0625 INCH CRACK; NR 2 HOLE VERTICAL LEG OF LT SPAR UPPER CHORD AT MLG SUPPORT. INSTALLED FATIGUE ENHANCEMENT PLATE IAW EA 79286A. 2L72 4F4 FRTA16WE E2GL 20050111001452005011100145NM 2005 1 11 ASAA0410575 120041122A531565549062 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON FLOORBEAM UPPER FLANGE. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED. 2L72 4F4 FRTA16WE E2EA 20050113000042005011300004EA 2005 1 13 UIA9318 120041024A2421B1708001A GENERATOR DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 1 AC FAULTY Z A UNSCHED LANDING S AFFECT SYSTEMS CRCRUISE 1 TW0015223 404 123206 IN AIR NR 1 AC GENERATOR CAUTION LIGHT ON, A/C AIR TURNBACK. AFTER A/C LANDING CHECK FOUND NR 1 AC GENERATOR FAULTY, IAW AMM24-21-00 REPLACED AC GENERATOR, GROUND ENG RUNNING OPERATIONAL CHECK, CONDITION NORMAL. 2H72 4T4 TRTA13NM E20NE 20050228003022005022800302SO 2005 2 28 SIMA200434503 120041208A3350 CONNECTOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN LOOSE A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21651AE 145422 CREW REPORTED THE EMERGENCY LIGHTS AT SEAT 3BC AND GALLEY SERVICE DOOR ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR PLUG LOOSE ON BATTERY PACK RECONNECTED CONNECTOR PLUG. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501826) (K) 2L72 4T4 FRTT00011ATTE6CH 20050307003272005030700327WP 2005 3 7 ASAA0480568 120041118A5310991960387 SHEAR TIE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02934AS 49235 C-CHECK - SHEAR TIE IS CORRODED. REPLACED SHEAR TIE.(K) 2L72 4F4 F A6WE E9NE 20050308001892005030800189NM 2005 3 8 C7WA200400033 120040605A2730680005005 PCU BOEING727 7272J7 138400ENM PWA JT8 JT8D15A 52051NE LT ELEVATOR LEAKING A C7WAO OTHER K FLUID LOSS CRCRUISE 1 SO17128NA 20879 IN CRUISE NOTED DECREASING HYDRAULIC A-SYSTEM QUANTITY. FOLLOWED ABNORMAL PROCEDURES QUANTITY STABILIZED AT .6 GALLONS. FOUND LT ELEVATOR POWER CONTROL UNIT LEAKING. REMOVED AND REPLACED LT ELEVATOR PCU IAW MM. OPS AND LEAK CHECK GOOD. 2L73 4F4 F A3WE E2EA 20050310001342005031000134NM 2005 3 10 ASAA0470023 120041026A53212024T3 FLOOR PANEL BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE CABIN CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION ON NR4 FLOOR PANEL, AFT CARGO BAY. FABRICATED NEW IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050311000782005031100078NM 2005 3 11 S2YA04027 120040826A52709402 PROXIMITY SENSOR DORNERDO32 DO328300 NM PWA 306 PW306B NE CARGO DOOR INOPERATIVE A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13352SK10972 3111 DURING FLIGHT, THE CREW REPORTED CARGO DOOR OPEN INDICATION. THE CREW MADE AN AIR-TURN-BACK. THE AC WAS INSPECTED BY MECHANIC WHO CHECKED THE PSEU`S MEMORY AND FOUND THE CARGO DOOR OVER-CENTER PROXIMITY SENSOR HAD LOGGED SEVERAL FAULTS. MECHANIC REPLACED THE PROXIMITY SENSOR. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050308001352005030800135CE 2005 3 8 GUU2004F00043 120041119A55241016200131 HINGE BRACKET BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO178154619047 UE187 AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. 2L72 4T4 TRTA24CE E26NE 20050406000222005040600022NM 2005 4 6 72300063 120041102A5340 FITTING BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 CORROSION ON END FITTING APPROX 2.5 INCH BY 6 INCH BY 4 INCH. 2L73 4F4 FRTA3WE E2EA 20050408000222005040800022WP 2005 4 8 IXXA0500062O 120040406A7931 WARNING LIGHT DOUG DC8 DC873F 302199FWP PWA JT3D JT3D7 52039NE NR 1 ENGINE OIL ILLUMINATED A IXXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW11606AL663392633 46044 644664 DURING TAKEOFF FROM TAPA CREW REJECTED TAKEOFF DUE TO NR 1 ENGINE OIL LOW PRESSURE LIGHT ILLUMINATING AT 110KNTS. CREW RETURNED TO REMOTE PARKING WITHOUT INCIDENT. BRAKE ENERGY CHART CHECKED. MAINTENANCE DEFERRED IN ACCORDANCE WITH MEL 79-7 CAT "D". 2L74 4F4 FRT4A25 1E8 20050526000892005052600089SO 2005 5 26 CSA2005F00000 120041218A2140CD21402 MOTOR PIPER PA31T PA31T3 7103128SO PWA PT6 PT6* 52043EA HEATER BLOWER FAILED E CSAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 AL01217CS 31T8275014 PILOT RETURNED TO AIRPORT SHORTLY AFTER DEPARTURE (0.1 HOUR FLIGHT TIME). REPORTED BURNED ELECTRICAL ODOR IN COCKPIT. INVESTIGATION OF COMPLAINT REVEALED THAT THE FORWARD HEATER COMBUSTION BLOWER WAS NOISY AND VIBRATED DURING HEATER OPERATION, REMOVED BLOWER ASSY, FOUND MOTOR COMPONENTS, I.E. ENDPLATES AND FRAME LOOSE, FAN HUB LOOSE AND A 1.5 INCH X 0.5 INCH PIECE OF PAPER LODGED IN FAN. PAPER CAUSED FAN OUT OF BALANCE WHICH LED TO FAN AND MOTOR COMPONENTS VIBRATING LOOSE AND CAUSING MOTOR TO RUN HOT. (K) 1L72 3T3 T A8EA E2NE 20051109000502005110900050CE 2005 11 9 UAT2005F00002 120041129A2434DOFF10300B ALTERNATOR CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO DC SYSTEM FAILED E UATAO OTHER O OTHER NRNOT REPORTED 1 AL0373217 391 20700572 ALTERNATOR FAILED AT 391.8 TSO. REPLACED WITH SERVICEABLE UNIT. OPS CHECK GOOD. (K) 1H71 3O3 O A16CE E5CE 20060201000792006020100079WP 2006 2 1 IXXA060097S 120041002A5712 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS635. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS635. IAW SRM 57-2-0, 51-1-20, 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20040414000022004041400002NM 2004 4 14 04FDEA00826 120040401A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25598FE 48597 LEFT WING AFT (FLAP SIDE) OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76654 LT OUTBOARD FLAP OUTBOARD HINGE BRACKET PIVOT BEARINGS - CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040823001442004082300144NM 2004 8 23 USAA040357 120040720A5315113851 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19426US41553 24548 PIT - FOUND FLOOR SUPPORT CORRODED .5 INCH DIAMETER AT 4 SCREW HOLES UPPER EDGE FLOORBEAM FLANGE STATON 967-986.5 LBL 16. REMOVED AND REPLACED SUPPORT PER SRM 53-60-51. (M) 2L72 4F RTA16WE 20040830000562004083000056NM 2004 8 30 UPS04M42937 120040621A5510 STRUCTURE DOUG MD11 MD11F 3023600NM ZONE 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:C RT HORIZ STAB BARREL NUT HOLE NR 13 FOUND CORRODED. CORROSION REMOVED AND REAMED AT B/N HOLE NR 13 RT, IAW EO MD11-5510-19409-G ,0.988 INCH DIAMETER DEEP FOUND OUT OF LIMIT. REPAIR SLEEVE BUSHING FAB IAW EO MD11-5510-19409-G.PR1422B2 SEALANT APPLIED AT B/N HOLE NR 13 RT IAW EN:1231-04. REPAIR SLEEVE BUSHING INSTALLED AT RT NR 13 B/N HOLE IAW EO M D11-5510-19409-G AND EN:1231-04, FOUND WITHIN LIMIT AND SATISFACTORY. 2L73 4F RTA22WE 20040401000752004040100075NM 2004 4 1 SWAA040909 120040327A335007912 COVER BOEING737 7373H4 1384600NM EMERGENCY LIGHT LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29379SW 26586 EEPLS COVER AT FWD CABIN LOOSE. REINSTALLED EEPLS COVER PER MM. 2L72 4F RTA16WE 20050222001652005022200165NM 2005 2 22 04FDEA01955 120040706A5753ARC198414 HINGE BRACKET DOUG MD11 MD11F 3023600NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.126 INCH AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, TITLE: WINGS, LEFT AND RIGHT OUTBOARD FLAP, INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040428000572004042800057NM 2004 4 28 SWAA041077 120040415A552365C2638415M TAB BOEING737 7373H4 1384600NM LT ELEVATOR DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED C2 CHECK, FOUND LT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM. 2L72 4F RTA16WE 20040616000082004061600008NM 2004 6 16 ASAA0410208 120040426A526065566562 MOUNT FITTING BOEING737 737290C 138448VNM AIRSTAIR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 OKC - DURING C-CHECK, FOUND AFT AIRSTAIR FORWARD MOUNT FITTING IS CRACKED. REMOVED DAMAGED FITTING AND INSTALLED REPLACEMENT FITTING IAW SRM 51-10-1. (M) 2L72 4F A16WE 20040628000532004062800053SO 2004 6 28 SWIA200413414 120040604A2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203SO LAVATORY ACTIVATED A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 NM07215SW 120281 LAVATORY SMOKE ALARM WENT OFF. TURNED OFF PACKS. SMOKE ALARM STOPPED AFTER A FEW MINUTES. RAN APU AND ENGINES AND BOTH PACKS FOR 45 MINS. OPERATIONAL CHECKED GOOD. 2L72 4T RTA31SO 20040727000462004072700046NM 2004 7 27 04FDEA02134 120040719A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25613FE 48749 LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.394 AND REPAIRED AS PER FEDEX EA NR 1-5750-77942. TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040525000642004052500064EU 2004 5 25 DHL3642004509 120040313A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01364DH 141 DURING C-CHECK, MAIN CARGO COMPARTMENT SEAT TRACK FLANGES HAVE CORROSION BETWEEN FR. 33 AND FR 36 RBL 36 ( MKD ) REMOVED CORROSION FROM SEAT TRACK FLANGES BETWEEN FR. 33 TO 36, RBL 36 IAW A300 SRM 51-40-11. MAT. LOSS FROM FR. 35 TO FR. 36 = 0.020 TO 0.030, FOUND TO BE OUT OF LIMITS IAW A300 SRM 53-10-00 FIG. 12 ( NOMINAL THICKNESS 0.090). 3) CUT OUT DAMAGED SEAT TRACK SECTION FROM FR. 32 1/2 TO FR. 35 1/2 62 IAW A300 SRM 53-10-10 FIG. 724. TRIMMED NEW SECTION TO HI IAW A300 SRM 53-10-10 FIG. 724 51-27-00 MAT. USED. SEAT TRACK PO 6012336 P/N = 24072359, 4 FT. LENGHT. TREATED AND PRIMED, POLIWHITE NEW PART IAW A300 SRM 51-40-12. INSTALLED NEW SEAT TRACK SECTION FROM FR 32.5 TO 35.5 IAW A300 SRM 53-10-10 FIG.2L72 4F RTA35EU 20040218000262004021800026NM 2004 2 18 04FDEA00145 120040113A5744ARC0502 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RT OB FLAP IB HINGE (WING MOUNTED), LOWER OB ATTACH HOLE (SPAR MOUNTED) CORRODED AT SPOT FACES. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040115002032004011500203NM 2004 1 15 04FDEA00002 120040101A3260 CONNECTOR BOEING727 727100 1384036NM NLG CONTAMINATED A FDEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO25190FE 19083 UNSAFE NOSE GEAR INDICATION - NO GREEN LIGHT. RAN PROCEDURE PER QRH. RECYCLED GEAR. VIEWED NOSE GEAR PORT WITH A GEAR DOWN & LOCKED INDICATION NORMAL. NOSE GEAR GREEN LIGHT ILLUMINATED UPON FINAL APPROACH. AFTER JACKING A/C REMOVED CANNON PLUG FROM DOWNLOCK SWITCH S93 FOUND CANNON PLUG DETERIORATED WITH SKYDROL AND WATER, REMOVED AND REPLACED CANNON PLUG AS PER STD WIRING PRAC AND 32-64-01. ACTUATED NOSE GEAR NUMEROUS TIMES. NOSE GEAR DOWNLOCK INDICATING SYS OP CKS GOOD. OK FOR SERVICE. 2L73 4F RTA3WE 20050112000632005011200063WP 2005 1 12 05FDEA00012 120040426A5712ARB70602 RIB DOUG MD10 MD1010F 3022112WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568050 47804 WINGS - RT WING RIB UPPER CAP CRACKS AT XORS 372 AROUND CUTOUTS FOR STRINGER 12 AND 13. TRIMMED OUT AND ROUNDED CRACKS, INSTALLED REPAIR ANGLE AND DOUBLER TO RESTORE STRENGTH IAW FEDEX AE 8-5710-75716. 2L73 4F RTA22WE 20040506001032004050600103NM 2004 5 6 CALA0400450 120040502A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND RIGHT Z-CHANNEL CORRODED IN AFT CARGO AREA AT STA 727+4 TO 767. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040115000632004011500063NM 2004 1 15 04FDEA00100 120040112A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 RIGHT OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE FOUND CORRODED ON BORE AND SPOT FACES. RT OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT ATTACH PIN LOCK PLATE BOLT HOLE BORE AND SPOT FACES CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74280, WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040406000952004040600095NM 2004 4 6 04FDEA00665 120040316A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 LT WING - OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75970, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/ OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041213000082004121300008NM 2004 12 13 SWAA043569 120041207A57536546481122 SPINDLE BOEING737 7375H4 138449DNM RT WING TE FLAP WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29508SW 24185 DURING SCHEDULED SERVICE CHECK, RT WING OUTBOARD T/E AFT MID FLAP SPINDLE HAS EXCESSIVE PLAY. REMOVED RT SPINDLE PER MM. 2L72 4F RTA16WE 20040929001372004092900137NM 2004 9 29 DL73S040904 120040920A2710 MIXING VALVE BOEING737 737232 1384475NM AILERON DIRTY A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO27318DL 23090 CONTROL YOKE HAS DEAD ZONE FEEL PLUS/MINUS SIX DEGREES OF CENTER WITH NO AILERON MOVEMENT. REMOVED DIRT AND DEBRIS FROM AILERON MIXING UNIT. 2L72 4F RTA16WE 20040209000962004020900096NE 2004 2 9 SWIA200412799 220040123A732278639010 HMU EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 NM07188SW3538 3538 10133 ON CLIMBOUT FROM SLC, RECEIVED AN APPARENT AUTOFEATHER ON THE LEFT ENGINE. THE PROP FEATHERED AND TORQUE INDICATED 145 PERCENT. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. REMOVED AND REPLACED LEFT TSCU, HMU AND EEC. OPS CHECKS GOOD OF ALL SYSTEMS. TSCU P/N: 30005-0000-57, S/N OFF: 855.73-301. HMU P/N OFF: 786390-0, S/N OFF: M80009. EEC P/N OFF: 800414-2-003, S/N OFF: 90049994. 2L72 4T4 TRTA31SO E20NE 20040223000912004022300091NM 2004 2 23 CALA0400005 120040106A80113507138040 STARTER BOEING777 777224 1385225NM GE GE90 GE9090B NE NR 1 ENGINE LEAKING A CALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW277800417965 27580 900229 THE NR 1 ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DECREASE DURING CRUISE. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT WAS DIVERTED WHERE IT LANDED WITHOUT INCIDENT. THE STARTER SIGHT GLASS HOUSING WAS FOUND SHEARED. THE NR 1 ENGINE STARTER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00001SEE00049EN 20040223001612004022300161CE 2004 2 23 GNL2004F00000 120040102A56109031002P WINDSCREEN BEECH 90 E90 1152914CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED E GNLAB EMER. DESCENT O OTHER CRCRUISE 1 SW01304LG4465 LW231 THE AIRCRAFT WAS AT 22,000 FT ENROUTE, WHEN THE CO-PILOTS WINDSCREENS INNER PLY CRACKED LIKE A SPIDER WEB ACROSS THE ENTIRE WINDSCREEN. THE PRESSURIZATION STARTED TO FAIL, THE CABIN CLIMBED TO 10,000 FT. THE PILOT DECLARED AN EMERGENCY, ASKED CENTER FOR BELOW 14,000 FT. THE AC LANDED. THE EXTERIOR OF THE WINDSCREEN IS IN TACT. NO STRIKE, OR PITS, THE CRACKED STARTED IN THE LOWER IB CORNER. THE WIND SCREEN WAS INSTALLED IN 8-96 AND LASTED 4465.0 HOURS. 1L72 3T4 T 3A20 E4EA 20040303000882004030300088SW 2004 3 3 ALG2004F00003 120040204A634022A690 TACH GENERATOR BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW032201W 3477 DURING TAKE OFF FROM VENICE ROTOR TACH WENT TO ZERO, LOW ROTOR LIGHT ILLUMINATED WITH LOW ROTOR HORN. RETURNED TO VENICE, LANDED AND NOTIFIED MAINTENANCE AND CUSTOMER. MAINTENANCE REMOVED AND REPLACED ROTOR TACH GENERATOR. AC GROUND RUN LEAK CHECKED AND OPS CHECKED GOOD. (SW03200405508) 1G71 3U3 U H2SW E4CE 20040303001292004030300129 2004 3 3 2004UALA00131 420040214A2230 AUTOTHROTTLE SYS BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT MALFUNCTIONED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29657UA 27112 FLIGHT ABORTED TAKEOFF AT 100 KTS DUE TO AUTOTHROTTLE INDICATION. RETURNED TO BLOCKS. THRUST MANAGEMENT COMPUTER WAS REMOVED AS A PRECAUTION. UNIT CHECKED OK IN THE SHOP. MCDP FAULT DATA DID NOT RECORD ANY TMC-RELATED FAULTS DURING THE EVENT. REASON FOR THE ANOMALOUS AUTO-THROTTLE INDICATION IS UNKNOWN. 2L72 4F4 FRTA1NM E24NE 20040303001772004030300177EA 2004 3 3 MASA200400065 120040204A3350LS6006182 LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ROW 5 INTERMITTENT A MASAK NONE L NO TEST ININSP/MAINT 1 SW0737218 7218 EMERGENCY FLOOR PATH LIGHTING AT ROW 5 INTERMITTENT. MECHANIC REPLACED LIGHT STRIP. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20040308000472004030800047GL 2004 3 8 C2XA04IA015 220040220A7200AE3007A1P ENGINE EMB 145 EMB145XR 3260214SO ALLSN AE300 AE3007A GL NR 2 FLAMED OUT A C2XAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SW27211292366 2366 145703 CAE312378 DURING CLIMBOUT THROUGH 27,000 FT THE NR 2 ENGINE FAILED. ATTEMPTS WERE MADE TO RESTART THE ENGINE WITHOUT SUCCESS. THE AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT WHERE THE AFFECTED ENGINE WAS REPLACED. 2L72 4F4 FRT TE6CH 20040319000272004031900027NM 2004 3 19 P5CA0401051 120040306A36109788926 RELIEF VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650E2 30018NE NR 4 ENGINE ILLUMINATED A P5CAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP23505MC 21251 517529 AT APPROX 6,000 FT NR 4 ENG LOOP FAULT LT ILLUMINATED NACELLE TEMPS A&B OBSERVED RAPIDLY CLIMBING TO 9. REMOVED AND REPLACED HIGH PRESS VLV, HIGH PRESS BLEED VLV HARNESS. REMOVED AND REPLACED PRESSURE RELIEF VLV. ENG OPS CHECKED GOOD, NO DEFECTS NOTED PER MM 36-11-05 & MM 36-11-03. 2L74 4F4 FRTA20WE E23EA 20040325000232004032500023NE 2004 3 25 TRB2004F00011 220040307A73208201541001 EEC AEROSPATR72 ATR72212A 8680902EU PWA PW120 PW127 NE RT ENGINE FLUCTUATES A TRBAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO21538AT 538 RT ENGINE TORQUE FLUCTUATION DURING FLIGHT. CREW PROCEEDED TO SHUTDOWN THE ENGINE AND FOLLOW EMERGENCY PROCEDURES. REMOVED AND REPLACED RT ENGINE ELECTRONIC CONTROL. (SDR2004018) 2H72 4T4 TRTA53EU E20NE 20040325001462004032500146EU 2004 3 25 BAQA093649 120040217A6210117151321 BLADE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE MAIN ROTOR DAMAGED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03911TG 7506 LEAD/LAG IN EXCESS OF 20MM, INSTALLED A/C TT 5145.8, REMOVED AC TT 5146.2 FOR A TOTAL .4 HOURS. RECEIVED BLADE ON EXCHANGE FROM AEC UNDER OUR PO 8-080114-36. WOULD LIKE TO HAVE THIS BLADE BACK AFTER REPAIR, SEEMS TO HAVE A GOOD HISTORY OF BEING ABLE TO STAY IN THE AIR. S/N 1012 ; LEAD/LAG IN EXCESS OF 20MM PENDABS ALSO NEED REINSTALLED (DIFFERENT STYLE). INSTALLED A/C TT 5145.8, REMOVED A/C TT 5146.2 FOR A TOTAL OF .4 HOURS. LAST REPAIR OF BLADE WAS UNDER PO 8-080114-31. (ALSO A WARRANTY REPAIR) 1G72 3U3 UNCH13EU E19EU 20040325001512004032500151EU 2004 3 25 BAQA093670 120040222A6730D107614 SHAFT BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101* NE SERVO MOTOR FAILED B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KC 7168 ACTUATOR FAILED OUT OF BOX. LAST REPAIR 8-080019-83, SHAFT ON ACTUATOR IS ONLY MOVING ONE INCH IN EITHER DIRECTION AND THEN LOCKING UP. REPLACED WITH UNIT FROM ASSET. 1G72 3U3 UNCH13EU E5NE 20040420000262004042000026NM 2004 4 20 2004UALA00318 120040408A2550 ROLLER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CARGO BAY SPARKS A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29603UA 21864 FWD CARGO PIT POWER DRIVE ROLLER SPARKING AND SMOKING. POWER DRIVE UNIT CABLE CHAFED AGAINST CLAMP ATTACH SCREW ON BOTTOM OF PDU, DUE TO BROKEN CABLE CLAMP. SCREW APPEARS TO HAVE BURN MARKS FROM ARCING. PDU REPLACED. 2L72 4F4 FRTA1NM E3NE 20040421000092004042100009 2004 4 21 BAQA093734 420040309A342455508340N5L INDICATOR UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS1A NE TURN AND BANK RATCHETING W BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03135LC224 0296 INDICATOR IS RATCHETY AND STICKY. REPLACED WITH SERVICABLE UNIT. 03/11/2004 1G72 3U3 U H88EU E34NE 20040422001522004042200152SO 2004 4 22 LER2004F00000 120040309A28103734332 TUBE PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360* 17025SO FUEL SYS FRACTURED E LERAO OTHER O OTHER NRNOT REPORTED 1 NM114023U 347570229 FUEL LINE FRACTURED CAUSING FUEL STARVATION AND ENGINE FAILURE. 1L72 3O3 O A7SO E9CE 20040427000282004042700028EA 2004 4 27 A6WA200440030 120040311A2611 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CARGO SMOKE FALSE ACTIVATIONA A6WAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31425AW 7663 SMOKE CARGO WARNING WHILE TAXIING. RETURN TO GATE. CARGO PIT CHECK FOR SMOKE, NONE NOTED. NO ODOR NOTED. COMPLIED WITH OPS TEST OF CARGO SMOKE DETECTION SYSTEM. IAW MM 26-15-00. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040505000332004050500033EU 2004 5 5 USA2004F00032 120040408A2560170683353405 BELLCRANK EMB ERJ170ERJ170100 EU GE CF34 CF34* NE PAX DOOR DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19801MA 17000012 WHILE ATTEMPTING TO OPEN THE MAIN ENTRY DOOR, THE FLIGHT ATTENDANT NOTICED THE SLIDE DROPPING OUT OF ITS COVER. MAINTENANCE WAS CALLED TO DISCONNECT THE GIRT BAR AND REPLACE THE SLIDE. REMOVED SLIDE GIRT BAR BUT UNABLE TO INSTALL SAME GIRT BAR DUE TO DAMAGED BELLCRANK. MAINTENANCE REPLACED SLIDE ASSY AND BELLCRANK ASSY. 2L74 4F4 FRTA56NM E15NE 20040423000142004042300014EU 2004 4 23 COE2004F00000 120040304A2430153912B CONTROL PANEL FOKKERF27 F27MK600 4990706EU RROYCEDART DART5327R 54509NE ROTOL R4304 R1934304 EU LT GENERATOR FAILED A COEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM13741FE 10387 14154 DRG1466 AFTER TAKEOFF, LEFT ENGINE GENERATOR WOULD NOT CARRY A LOAD. CREW TURNED BACK WHERE MAINTNANCE WAS AVAILABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT GENERATOR CONTROL PANEL. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 T A817 E297 6 CP899 20040504000202004050400020EA 2004 5 4 SWIA200413123 120040117A3230 TRUNNION CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT MLG DAMAGED A SWIAO OTHER O OTHER LDLANDING 1 NM07595SW 7292 HARD LANDING AFTER ILS APPROACH. AIRCRAFT BOUNCED AND, PRIOR TO SUBSEQUENT LANDING, THE LT WING TIP MADE CONTACT WITH RUNWAY.HARD OVERWEIGHT LANDING INSPECTION COMPLIED WITH IAW ST 12-407 ST 12-407. (AIRCRAFT CURRENTLY UNDERGOING LANDING GEAR REPLACEMENT) UPDATE: 02/16/04 - REMOVE AND REPLACE LEFT MLG TRUNNION & PIN IAW BOMBARDIER MANUFACTURING DRAWING'S & APPLICABLE REO'S FOR LT MLG TRUNNION. 2L72 4F4 FRTA21EA E15NE 20040505001732004050500173SO 2004 5 5 CSL2004F00000 220040326A85206419311075 THRU BOLT CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO ENGINE BROKEN B CSLRK NONE O OTHER ININSP/MAINT 1 CE01678JS 414A0090 266546R DURING 100 HOUR INSPECTION, FOUND CRANKCASE THRU BOLT BROKEN AT LOWER FORWARD NR 2 CYLINDER. 1L72 3O3 O A7CE E8CE 20040507001082004050700108EA 2004 5 7 SWIA200413178 120040413A5320 STRUCTURE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07413SW 7102 MAIN FUSELAGE FITTING CRACKED AT FS 460.00 LB19 OUTBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11 AND CONTINUATION SHEETS REF RII 53-401. 2L72 4F4 FRTA21EA E15NE 20040512000462004051200046CE 2004 5 12 BAQA094408 120040505A324050030967 BRAKE ASSY LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP MLG WORN E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA0340DK 301 092 BRAKE ASSY WORN TO LIMITS. REPLACED WITH SERVICABLE UNIT. 05/06/2004 2L72 4F4 F A10CE E6WE 20040504000632004050400063SO 2004 5 4 SIMA200410703 120040415A27503632001003 PDU EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL T/E FLAP MALFUNCTIONED A SIMAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW21835AE 145634 DURING APPROACH WHEN FLAPS WERE SELECTED FROM 9 DEG TO 22 DEG, EICAS MESSAGE (SPS ADVANCED). FLAP POSITION INDICATOR BOX WENT AMBER WITH AMBER DASH WITH NO FLAP INDICATION, RMU PAGE SHOWING NO FLAP INDICATION BUT AMBER DASHES, EICAS DID NOT PRESENT A FLAP FAIL MESSAGE, BUT WE PROCEEDED WITH FLAPS FAIL PROCEDURE AOM VOL 1, REPLACED FLAP POWER DRIVE UNIT. AC RETURNED TO SERVICE 2L72 4F4 FRTT00011ATTE6CH 20040514000692004051400069CE 2004 5 14 PAI2004F00001 120040416A2910620701098 LINE CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP HYD SYSTEM CHAFED B PAIRO OTHER O OTHER NRNOT REPORTED 1 SO05460CP7173 6500021 FOUND RT GROUND SPOILER HYD LINE CHAFED THROUGH BY AILERON CABLE, AFTER SEEING EVIDENCE OF HYDRAULIC FLUID DRIPPING OFF OF WING SKID. IT IS IN THE WING T/E AREA AT STA WS85. INSIDE THE FLAP ACTUATOR/TRACK MOUNT. IMPOSSIBLE TO SEE WITHOUT AID OF MIRROR AND MOVING WIRE BUNDLE OUT OF WAY. COULD OF LEAD TO LOSS OF HYDRAULIC FLUID AND PRESSURE IF AC HAD FLOWN ANY LONGER, SUGGEST CLOSER AND A MORE DETAILED INSP OF THE AREA. DURING PHASE 5 INSPECTION OR ANY TIME ANY WORK IS ACCOMPLISHED IN THE AREA THAT MAY DISTURB ANY HYDRAULIC LINES OR WIRE BUNDLES. VERY CLOSE CLEARANCE IN THAT AREA. 2L72 4F4 F A9NM E6WE 20040601001512004060100151WP 2004 6 1 AALA2040593 120040526A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170504 49798 DFW CEILING EMERGENCY LIGHTS FROM ROWS 21 THROUGH 27 INOPERATIVE. REPLACED BATTERY PACK AT B5106 FOR AFT CABIN CEILING EMERGENCY LIGHTS AT ROWS 21 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E2EA 20040517000762004051700076NM 2004 5 17 2004UALA00424 120040502A5320 STIFFENER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29668UA16875 30024 BS 246 FLOORBEAM VERTICAL STIFFENER AT RBL 11 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED VERTICAL STIFFENER 2L72 4F4 FRTA1NM E24NE 20040604001042004060400104EU 2004 6 4 USAA040171 120040428A5321D5367175505200 FLOOR PANEL AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE FUSELAGE DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19101UW 0936 FLOOR PANEL 4 INCH X 4 INCH AREA, DELAMINATION, 31.25 CM FWD OF FR 68, Y 756.25. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. 2L72 4F4 FRTA28NM E2GL 20040614001982004061400198EU 2004 6 14 ASO2004F00008 120040307A5347 SEAT TRACK AEROSPATR72 ATR72 EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING C-CHECK, THE LEFT SIDE SEAT TRACK AT FRAMES 36-39 AS WELL AS THE RT SIDE SEAT TRACK FROM FRAME 39-40 WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED SEAT TRACKS IAW SRM. AIRCAFT WAS RELEASED FORM C-CHECK ON MARCH 21, 2004. (ASOA04369) 2H72 4T4 TRT E20NE 20040622001752004062200175EU 2004 6 22 ASOA04352 120040427A5320 COVER AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CARGO BAY CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27532AS 458 DURING C-CHECK INSPECTION, THE ALUMINUM COVERING ON FLOOR PANEL 256 HF, AS WELL AS THE COVER PLATE AT FLOOR PANEL 256 GF WERE FOUND CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED BOTH THE CORRODED ALUMINUM COVERING AND THE FLOOR COVER PLATE IAW SRM 536210. AIRCRAFT WAS RELEASED FROM C-CHECK ON MAY 14, 2004. 2H72 4T4 TRTA53EU E20NE 20040622001962004062200196WP 2004 6 22 GTIA040473 120040323A5315 FLOORBEAM DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 AFT PIT STA 1309 FLOORBEAM CORRODED AT LOWER SIDE LBL 30-RBL 30. CUT FLOORBEAM AT STA 1309 LBL 33. FABED 2 EA L ANGLES. FABRICATED NEW FLOORBEAM AND SPLICE DOUBLER. RT OB FITTING OUT OF LIMITS. FABRICATED FLOORBEAM SUPPORT ANGLE. INSTALLED FLOORBEAM. 2 EA (L) ANGLES SPLICE DOUBLER AND SUPPORT FITTING. 2L72 4F4 F A6WE E2EA 20040623000582004062300058WP 2004 6 23 GTIA040534 120040429A5347 SEAT TRACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 LT OB SEAT TRACK FS 927 THRU FS 1098 CORRODED AND GOUGED. REMOVED LT OB SEAT TRACK FS 915, FS 1098. LOCATED AND DRILLED NEW SEAT TRACK. LOCATED AND DRILLED 2 EA SPLICES. INSTALLED SEAT TRACK AND 2 EA SPLICES. 2L72 4F4 FRTA6WE E2EA 20040715000502004071500050EA 2004 7 15 SWIA200413512 120040622A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07906SW 7510 FS 484 RIGHT INTERCOSTAL RBL 27 ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-42-13, 51-25-16, 51-21-11. 2L72 4F4 FRTA21EA E15NE 20040630000422004063000042SO 2004 6 30 SIMA200413503 120040514A3350110049 CHARGER EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21810AE 145525 DISC-EMERGENCY LIGHTS AFT OF EMERGENCY EXIT ROW COME ON AFTER BATTERIES TURNED OFF WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD, NO FURTHER DEFECTS. (SW21200406974) 2L72 4F4 FRTT00011ATTE6CH 20040830001352004083000135SW 2004 8 30 PNSA040707 120040719A3213 STRUT FRCHLDSA227 SA227DC 3377521SW GARRTTTPE331TPE33112UHR WP LT MLG SEIZED A PNSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03892DC DC892B HAD A NORMAL TAKEOFF CREW RAISED LANDING GEAR AND LANDING GEAR DID NOT RESPOND, GEAR REMAINED DOWN AND LOCKED. CREW MADE AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. MAINT DISCOVERED THAT THE LT MAIN GEAR STRUT WAS SEIZED IN UPPER HOUSING, THE LT MAIN GEAR ASSY WAS CHANGED AND A/C RETURNED TO SERVICE. 2L72 4T4 TRTA18SW E4WE 20040831000322004083100032SO 2004 8 31 CHQA000521 120040725A2120 ODOR EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL COCKPIT DETECTED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL11278SK 145370 DURING CRUISE, AT 10,000 FT, NOTICED A STRONG ELECTRICAL ODOR COMING FROM UNDER THE CAPTAINS PFD. ONCE ON THE GROUND DETERMINED THAT THE CAPTAINS PFD WAS CONSIDERABLY HOTTER THAT THE OTHER TUBES. TURNED OFF THE AVIONICS AND THE HEAT SUBSIDED. INSPECTED AVIONICS BAY FOR ELECTRICAL ODOR. ALSO INSPECTED THE BATTERY COMPARTMENT AND NO ODOR WAS NOTED. INSPECTED THE PFD'S AND FOUND TEMPERATURES TO BE NORMAL. COULD NOT GET ANY ELECTRICAL ODOR FROM THE COCKPIT WITH THE APU AND AVIONICS TURNED ON FOR ABOUT 30 MINUTES. 2L72 4T4 FRTT00011ATTE6CH 20040901000182004090100018WP 2004 9 1 MWEA040132 120040810A534059524211 FITTING DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE GALLEY CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 CORROSION AT GALLEY 1 FORWARD ATTACH POINT JUST AFT OF WATER SUPPLY PAN FITTING AT STATION 160 AND RT OF THE BUTT LINE. FABRICATED AND INSTALLED FITTING. 2L72 4F4 F A6WE E2EA 20040901000212004090100021SO 2004 9 1 SWIA200413677 120040804A27503472001001 CONTROL UNIT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE OB FLAPS MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07215SW9307 6135 120281 OB FLAPS DID NOT EXTEND WHEN ANY OF THE FLAPS SETTINGS WAS SELECTED. REMOVED AND REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20040908000622004090800062EU 2004 9 8 KBM2004F00197 120040626A2150540028C2A ELECTRICAL BOX SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE AIR CONDITIONER INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19230SH 2337 A/C BLOWING WARM AIR. REMOVED AND REPLACED ELECT BOX ASSY. 1G71 3U3 UNCH9EU E19EU 20040818001732004081800173NM 2004 8 18 WLDA200446 120040802A5512ALC8104502 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 23.PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 23 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040819001022004081900102CE 2004 8 19 63594 120040802A26121293640371 FIRE DETECTOR BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT ENGINE MALFUNCTIONED A AMWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE07182YV UE182 ON TAKEOFF ROLL OUT, FLIGHT CREW OBSERVED LT ENGINE FIRE BOTTLE DISCHARGED ANNUN. ILLUMINATED. CREW ABORTED TAKE OFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDENT. THE BOTTLE WAS SAID THAT IT WAS NOT DISCHARGED. REMOVED AND REPLACED 173 PC BOARD FIRE DETECTION. OPS CK GOOD. NO FURTHER DEFECTS NOTED. P/N 129-364037-1 S/N 380-F-94. 2L72 4T3 TRTA24CE E2NE 20040908000122004090800012CE 2004 9 8 TRK2004F00000 120040701A24202105279 PULLEY CESSNA210 P210N 2073454CE CONT O520 TSIO520* 17040SO ALTERNATOR SEPARATED B TRKRO OTHER O OTHER NRNOT REPORTED 1 SO15210TS P21000128 THE ALTERNATOR WAS REPLACED AND THE NUT FOR THE PULLEY WHICH IS PART OF THE STC WAS TORQUED IAW THE STC. APPROXIMATELY 10 HOURS LATER THE PULLEY CAME OFF THE ALTERNATOR. THERE IS NO WOODRUFF KEY, TAPERED PULLEY SHAFT OR ANY TYPE OF SAFETY USED DURING THE INSTALLATION OF THE PULLEY IAW THE STC. MFG NOTIFIED OF THE LOSS OF THE PULLEY AND THE TECH ADVISED THAT THEY BE CALLED AGAIN IF THE PULLEY COMES OFF AND THE ENGINEERING MAY ADDRESS THE ISSUE, BELIEVE THE PULLEY CAME LOOSE DUE TO THE FACT THAT THERE IS NO TYPE OF SAFETY FOR THE NUT ON THE PULLEY. 1H71 3O3 O 3A21 E8CE 20040914001932004091400193NM 2004 9 14 UIEA200400104 120040602A5311 FRAME BOEING747 747212B 1384886NM GE CF6 CF650E2 30018NE DAMAGED G UIEAK NONE O OTHER ININSP/MAINT 1 EA15808MC 21048 D CHECK, DURING MAINT INSP FOUND COCKPIT EMERGENCY EXIT DOOR CUTOUT FRAME AND CHORDS DAMAGED BETWEEN STA 360 AND 380 WITH MISDRILLED HOLES BETWEEN STRINGER 2L AND 2AL. SEVERAL MISDRILLED HOLES AND DRILL STARTS WERE REPAIRED AS FOLLOWS. FOR BS 360, WEB DAMAGE WAS TRIMMED OUT AND REPLACEMENT WEB WAS SPLICED IN. THE CHORD DAMAGED WAS BLENDED OUT. FOR BS 380, THE WEB WAS CUT BETWEEN S2AL AND S3L AND REPLACED TO S0 WITH A WEB SPLICE AT THE CUT LOCATION. THE INNER CHORD DAMAGE WAS TRIMMED OUT AND REPAIR ANGLE INSTALLED. 2L74 4F4 F A20WE E23EA 20040830002152004083000215NM 2004 8 30 DHL200474005 120040716A5711 SPAR BOEING727 7272Q9 138448MNM PWA JT8 JT8D17 52049NE LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 DURING AN (A) CHECK, INTERIM REPAIR INSTALLED ON LT WING STA.137.8 LOWER FRONT SPAR CHORD PLATE. REMOVED INTERM REPAIR AND TRIMMED OFF 3.7500 INCH IB END SECTION OF LT WING FRONT SPAR LWR CHORD PLATE FROM WS 136.00 T0 139.75 DUE TO CORROSION DAMAGE BEYOND ALLOWABLE LIMITS, BLEND OUT .8750 X 1.3750 AREA OF CORROSION ON LT WING LWR INSPAR SKIN, FWD EDGE AT WS 138.25 MATERIAL LOSS 0.050 INCH WITHIN LIMITS, IAW SRM 57-30-1 FIG.1 TABLE 2,AND DETAIL 4, FABRICATED -2 REPAIR STRAP 10 X 2.75 INCH AND -1 FILLER 3.75 X 2.75 INCH FROM 2024-T3 0.125 MATERIAL PO 900732, TREAT/PRIME INSPAR SKIN BLEND OUT AND REPAIR PARTS AND INSTALLED ON LT WING, L/E LOWER CHORD PLATE AT WS 137.00. 2L73 4F4 FRTA3WE E2EA 20040914000622004091400062WP 2004 9 14 DHL2004804526 120040723A53203646688505 CLIP DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH80489 46124 ITEM REF. NR. 0910: AFT. ACCY. COMPT. CLIP CRACKED 1.500 AT STA. 660.000 L-22L. REMOVED CRACKED CLIP IAW SRM 53-1-0 PG.1, SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL AISI 4130 0.050) IAW SRM 53-4-1 PG. 140, EA5310-032, DWG 3646688. PERFORMED HEAT TREATMENT IAW DPS 5.00-1. PERFORMED NDT INSPECTION IAW NDT SPM PART 08.00.07/07. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACE IAW SRM 51-1-11 PG.9. INSTALLED NEW CLIP IAW SRM 51-1-20D PG.9. 2L74 4F4 FRT4A25 E2GL 20040914001562004091400156NM 2004 9 14 ASMF200407022 120040719A2820AV16B1736D VALVE DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE FUEL SYSTEM FAILED W ASMFK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 SW23160PL11575 49763 DURING FUELING IN TRANSIT CHECK, FILLED FUEL CENTRAL VALVE FAILED. VALVE, TOTALIZER AND FUEL QUANTITY INDICATOR WERE CHECKED IAW MM 28-40-02, ALL CORRECT. DURING TRANSIT CHECK AT MEX VALVE FAILED AGAIN AND IT WAS REPLACED IAW MM 28-20-02, TEST CORRECT. 2L72 4F4 FRTA6WE E2EA 20040915000342004091500034 2004 9 15 XNOA1197 420040827A2200 PITCH CONTROL AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE PITCH TRIM MALFUNCTIONED A XN0AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL23373PC 218 ON TAXI PITCH TRIM INOPERATIVE. TRANSFERED TO DMI NR 4527, IAW ENA A300 MEL REF 22-11-03, PLACARDS INSTALLED. (STATUS: ORIG/OPEN) 2L72 4F4 FRTA35EU E23EA 20040915000592004091500059EU 2004 9 15 UPS04143049 120040903A3510 OXYGEN MASK AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE COCKPIT INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01122UP 0807 F/O 02 MASK WILL NOT TEST PROPERLY. REINSTALLED F/O 02 MASK. TEST OKAY. 2L72 4F4 FRTA35EU E24NE 20040917001022004091700102NM 2004 9 17 UPS04443113 120040817A5714 SHEAR TIE BOEING747 747200 1384847NM PWA JT9 JT9D7Q 52054NE CTR TANK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01520UP 21943 INSPECTION TYPE: C, CTR TANK FRONT SPAR UPPER CHORD SHEAR TIE FOUND CRACKED AT LBL 35 INCH CTR TANK FRONT SPAR UPPER CHORD, SHEAR TIE REPLACED AT LBL 35 INCH IAW SRM 51-10-01 PG 8. 2L74 4F4 FRTA20WE E3NE 20040922000652004092200065EA 2004 9 22 COMA0460530 120040914A2750 CONTROL SYSTEM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS INOPERATIVE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01409CA 7441 FLIGHT 5502 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT. IAW AD 98-20-01. 2L72 4F4 FRTA21EA E15NE 20040920001332004092000133 2004 9 20 KBM2004F00116 420040712A34245070020910 INDICATOR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE TURN AND BANK INOPERATIVE E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH124 3141 TURN AND BANK, WILL NOT POWER ON. MEL AC (DMI NR 19 DUE 7-20-04). 1G71 3U3 U H9EU E19EU 20040929000592004092900059NM 2004 9 29 P5CA0401196 120040914A5730 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 RIGHT UPPER WING SKIN HAS CORROSION ALONG FWD OF MID SPAR. BLENDED OUT CORROSION, TREATED & PRIMED. 2L74 4F4 F A20WE E20EA 20041020001692004102000169WP 2004 10 20 DHL2004801527 120040902A5711 FRAME DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 NR. 1358: RT WING CENTER L/E UPPER FORMER CRACKED 0.500, STA. XFS 379.000. REMOVED FASTENERS IAW SRM51-1-20D PG. 21, SRM 51-1-21 PG.1. FABRICATED ANGLE DOUBLER (2024-T3 0.032)IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER WITH NEW FASTENERS IAW SRM 51-1-20D PG.9, SRM 51-1-21 PG.1, SRM 57-2-0 PG. 9-10. 2L74 4F4 FRT4A25 E2GL 20041101000602004110100060NM 2004 11 1 2004UALA00859 120040907A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29565UA 26669 STATION 1640 FLOORBEAM CORRODED, RBL 54, AFT OF GALLEY MOUNT. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM WAS REPAIRED WITH U-CHANNEL ANGLE SPLICE REPAIR AND MODIFIED INTERCOSTAL. 2L72 4F4 FRTA2NM E17NE 20041101001412004110100141NM 2004 11 1 2004UALA00923 120041010A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 FLOORBEAM T-CAP AT BS 324, RBL 55 TO RBL 60 IS CORRODED. SPLICED IN A NEW PORTION OF THE FLOORBEAM. 2L72 4F4 FRTA2NM E17NE 20041026001102004102600110WP 2004 10 26 AALA20041056 120041011A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21496AA 49734 FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 F A6WE E9NE 20041026001502004102600150SO 2004 10 26 CHQA000568 120041016A3350 LAMP EMB 135 EMB135KL 3260302SO ALLSN AE300 AE3007A GL EMERGENCY LIGHT BURNED OUT A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11378 145593 RT OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED INOPERATIVE LIGHT. OPS CHECK GOOD IAW MM 33-50-07. 2L72 4F4 FRTT00011ATTE6CH 20041103001322004110300132NE 2004 11 3 ALG2004F00056 120041009A76007690001880106 AMPLIFIER SKRSKYS76 S76 8143010NE ALLSN 250C 250C30S 03013GL DROOP COMP INOPERATIVE E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03705AL 760267 CAE890773S IN CRUISE FLIGHT, BOTH ENGINES STARTED SURGING, EMERGENCY CHECK LIST COMPLIED WITH AND RUN ON LANDING. MAINTENANCE COMPLIED WITH VISUAL INSP OF BOTH ENGINES AND N1 AND N2 CONTROL SYSTEMS, COMPLIED WITH GROUND RUN CHECK AND AFTER ABOUT FIVE MINUTES EXPERIENCED ENGINE SURGE. TROUBLESHOOTING REVEALED THE FORWARD MOUNTED DROOP AMPLIFIER TO BE AT FAULT, REPLACED AMPLIFIER AND DID A 20 MINUTE GROUND RUN AND GROUND CHECK OF BOTH AMPLIFIERS ALL SYSTEMS NORMAL. 1G72 3U3 U H1NE E1GL 20041119000322004111900032NM 2004 11 19 USAA040813 120040829A5310 CLIP BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, CLIP EST. .125 INCH CRACK, STA 500B S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40. 2L72 4F4 FRTA16WE E2GL 20041026001812004102600181EU 2004 10 26 DHL2004363518 120040930A53476022457 SEAT TRACK AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01363DH 85 DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3892, FR. 26.5 - FR. 35.5 RBL 36 INCH MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS IAW A-300 SRM 51-40-11. REMOVED SEAT TRACK FROM FR. 26.5 TO FR. 35.5 AT RBL 36 INCHES IAW A-300 51-30-30. REPLACED SEAT TRACK IAW A-300 SRM 51-10-40. INSTALLED NEW SEAT TRACK FROM FR. 26.5 TO FR. 35.5 AT RBL 38 IAW A-300 SRM 53-10-10 / 51-10-40. MATERIAL USED: 60-22457, PO NR 24302234. 2L72 4F4 FRTA35EU E23EA 20041103000682004110300068NM 2004 11 3 04FDEA02962 120041021A5531 SPAR DOUG MD11 MD11F 3023600NM GE CF6 CF680C2* GL ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25602FE 48402 EMPENNAGE, UPPER VERTICAL STAB AT FRONT SPAR BERWEEN ZFR 400.681 TO 424.219 LT EXTRUSION EXTERIOR SURFACE FOUND CORRODED. FOUND WITHIN LIMIT AS PER FEDEX EA #1-5530-81581. 2L73 4F4 FRTA22WE E23EA 20041118000332004111800033 2004 11 18 2004UALA00964 420041016A239717715601 WIRE HARNESS BOEING777 777222 1385219NM PWA PW4077PW4077 NE ENTERTAIN SYS CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29775UA 26947 EVIDENCE OF PREVIOUS FIRE IN CEILING ABOVE DOOR 1L FWD BULKHEAD. CEILING INSULATION BURNED AND PARTIALLY DESTROYED. WIRE BUNDLE FOUND CHAFED IS SECURED TO BRACKET INSTALLED ON THE VIDEO CONTROL CLOSET, FOUND BRACKET AND WIRE BUNDLE INSTALLED INCORRECTLY. RE-INSTALLED BRACKET CORRECTLY, SECURED WIRE BUNDLE AND REPAIRED DAMAGED WIRING. 2L72 4F4 FRTT0001SE E46NE 20041118000532004111800053NM 2004 11 18 2004UALA01016 120041102A3350 SIGN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY EXIT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29388UA 24663 EMERGENCY EXIT SIGNS INOP AT LT OVERWING EXIT HATCH, FWD OF LT OVERWING EXIT HATCH AND MID AISLE CEILING AT ROW 10. REPLACED BATTERY PACK FOR ITEM M1134. 2L72 4F4 FRTA16WE E2GL 20041124000112004112400011NM 2004 11 24 GAIA04128 120040910A5311 FRAME BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DENTED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 400 DENTED ABOVE STR 8, LT. REF FASI NR 86677, CUT OUT DAMAGED AREA DIM 1.0 X 3.50, INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1. 2L73 4F4 F A3WE E2EA 20041129000442004112900044NM 2004 11 29 USAA040800 120041002A5320 BRACKET BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, BRACKET, 1 INCH X .2500 INCH CRACK, (L) BRACKET, STA 350 RBL 20. FABRICATED NEW BRACKET IAW DWG 69-74588. 2L72 4F4 FRTA16WE E2GL 20041129000762004112900076NM 2004 11 29 USAA040798 120041029A5420 CHANNEL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 2 PYLON CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US55352 22956 PIT, Q5, CHANNEL, 6 INCH LONG CRACK, NR 2 PYLON LOWER CHANNEL NAC STA 363. REMOVED AND REPLACED CHANNEL IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E2GL 20041129001912004112900191EA 2004 11 29 A6WA200440152 120041017A53306013501251 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31437AW 7744 FS 621-FS 625.3 INTERCOSTAL, LT SIDE, AT STR 14R IS CRACKED NEAR RADIUS, APPROX .75 INCH LONG. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL, PN 601-35012-51, IAW SRM 51-42-06. 2L72 4F4 FRTA21EA E15NE 20041203000772004120300077NE 2004 12 3 NACA20040058 220041109A7421URHB32E SPARK PLUG DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 12 CYLINDER CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL036174C18 18 44075 P33324 NR 1 ENGINE SHUT DOWN DUE TO BACKFIRING AND RUNNING ROUGH. FOUND NR 12 CYLINDER FRONT AND REAR SPARK PLUGS WITH CRACKED CERAMICS. REPLACED PLUGS, OP CHECKED GOOD. 2L74 4R4 R 6A3 5E8 20041129002072004112900207WP 2004 11 29 JRAA0520042 120040520A5315 FLOORBEAM CVAC 440 440 2422902WP RROYCEDART DART54210 54522EU FUSELAGE CORRODED E JRAAK NONE O OTHER ININSP/MAINT 1 GL11587CA 463 DURING A SCID INSPECTION 53-20, CORROSION WAS FOUND ON FLOORBEAM AT STA 681.0 RT SIDE AT BELTFRAME. AN AREA OF APPROX 3 INCHES X 5 INCHES ON THIS FLOORBEAM WAS FOUND CORRODED AT BELTFRAME ATTACH POINT AROUND RIVETS. THE CORROSION HAD PROGRESSED THROUGH 50 PERCENT OF THE BEAM`S THICKNESS IN ONE AREA. REPAIR IN PROGRESS AT THIS TIME. 2L72 4R4 T 6A6 E5EU 20041215000322004121500032EU 2004 12 15 ASOA04838 120041005A5415 ATTACH BRACKET AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE RT NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27632AS 338 DURING A C-CHECK, THE RT ENGINE LOWER NACELLE FORWARD LT CHANNEL NEAR THE UPPER COWLING ATTACHMENT BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CRACKED LT UPPER EDGING OF THE RT ENGINE LOWER NACELLE IAW SRM 51-25-01. 2H72 4T4 TRTA53EU E20NE 20041215000532004121500053NM 2004 12 15 ASAA0410431 120041020A53117075T6 FRAME BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - FRAME IS CORRODED. REMOVED CORRODED CAP, FABRICATED NEW CAP TO BE INSTALLED ON CARD NR 4846121. 2L72 4F4 FRTA16WE E2EA 20041221000432004122100043EA 2004 12 21 ASOA04903 120041116A5320601R31171179 CLIP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27901EV 7616 DURING A C-CHECK, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL 36, RBL36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL36 AND RBL 36 IAW EO 600-53-0098. 2L72 4F4 FRTA21EA E15NE 20041215000572004121500057NM 2004 12 15 ASAA0410468 120041104A531565549012 FLOORBEAM BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02747AS 23124 OKC- FLOORBEAM HAS CORROSION ON FORWARD FLANGE. REMOVED DAMAGE, FLAP PEENED, FABRICATED AND INSTALLED REPAIR STRAP SECTION IAW EA. 2L72 4F4 FRTA16WE E2EA 20041222001542004122200154NE 2004 12 22 GLBA20030769 220041208A73141143890425 PUMP BEECH 1900 1900D 1154162CE PWA PT6 PT6A67B 52043NE FUEL SYSTEM MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03179GL1330 1330 UE179 LT FUEL LOW PRESSURE ANNUN CAME ON IN FLT. REMOVED AND REPLACED LP FUEL PUMP. 2L72 4T4 TRTA24CE E26NE 20050105000142005010500014NM 2005 1 5 DL76L041122 120041219A3610361002145 CONTROLLER BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE BLEED AIR SYS FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27190DN 28447 724656 LEFT BLEED PROBLEM ON CLIMBOUT. RETURNED TO JFK. REPLACED PRV CONTROLLER PER M/M. 2L72 4F4 FRTA1NM E24NE 20050106001092005010600109NM 2005 1 6 2004UALA01236 120041218A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29573UA 26685 FUSELAGE EXTERNAL SKIN HAS CORROSION AROUND FASTENER HOLES TO FWD LEFT UPPER WING TO BODY FAIRING ATTACH PTS. 2L72 4F4 FRTA2NM E17NE 20050110000852005011000085EU 2005 1 10 USAA041001 120041116A5320D5347218820400 BEAM AIRBUSA319 A319112 3930323EU CFMINTCFM56 CFM565B5 NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - BEAM, 3.5 INCH X 3 INCH X .03 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; MAIN CABIN BEAM BTW FR 68-69, BL Y1162. REMOVED AND REPLACED BEAM IAW SRM 51-77-00, 53-00-14, 51-42-11. 2L72 4F4 FRTA28NM E37NE 20041228001462004122800146NE 2004 12 28 AWXA200401412 220041219A7230 STATOR VANE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 2 ENGINE LACK OF LUBE A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28670AW 2029 ON TAKEOFF AT BOS EN ROUTE FOR LAS JUST PRIOR TO 80 KTS RECEIVED ECAM MESSAGE NR 2 ENGINE COMPRESSOR VANE FAULT, REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT NR 2 ENGINE COMPRESSOR VANE FAULT IAW TSM 75-30-08-810-846, TSM RECOMMENDED A VARIABLE STATOR VANE (VSV) LUBE, LUBED VSV IAW AMM 75-32-42-02, POWER ASSURANCE RUN WAS GOOD. 2L72 4F4 FRTA28NM E40NE 20050104000062005010400006EU 2005 1 4 ASOA04882 120041104A3350LP1670 LIGHT AEROSPATR72 ATR72 EU PWA PW120 PW127 NE CABIN NOT SEATED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27642AS 395 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT AT ROW 10D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE EMERGENCY FLOOR TRACK LIGHT LAMP AT ROW 10D WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESEATED THE EMERGENCY FLOOR TRACK LIGHT LAMP AT ROW 10D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20050110001762005011000176NM 2005 1 10 USAA041048 120041109A554265C2584151 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - RUDDER TOP LAYER, .2500 INCH X .2500 INCH AREA, DELAMINATION, 32 INCHES FWD OF T/E, 54.5 INCH UP FROM BOTTOM LT SIDE. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTILAYER REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E21EU 20050111001512005011100151NM 2005 1 11 ASA0440235 120041112A551265C274942 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU HORIZ STAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02780AS 25112 RT HORIZONTAL STABILIZER, LOWER SKIN CRACKED 2 INCHES FWD OF BREAK SPAR. REPAIRED CRACK IAW EA. 2L72 4F4 FRTA16WE E21EU 20050202000942005020200094WP 2005 2 2 DJFA2004029 220041021A7321307080022 FUEL CONTROL CESSNA650 650 2076802CE GARRTTTPE731TFE7313C WP NR 2 ENGINE UNSERVICEABLE E DJFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23381CW2672 2672 6500111 P87307C CREW REPORTED THAT WHILE AT V2 RIGHT FUEL COMPUTER ANNUNCIATOR ILLUMINATED AND THE NR 2 ENGINE ROLLED BACK TO 70 PERCENT AND STARTED SURGING. THE AIRCRAFT ROLLED RIGHT AT APPROXIMATELY 50 FEET IN THE AIR. CORRECTIVE ACTION WAS TAKEN TO MAINTAIN CENTERLINE AND CLIMB. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED BACK AT KJAC WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT FUEL CONTROL UNIT, AND TIGHTENED LOOSE T2 CANNON PLUG AND P2 LINE B-NUT AT THE PT2 SENSOR. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 F A9NM E6WE 20050201000772005020100077NE 2005 2 1 ASMF200411001 220041103A7200 ENGINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT DAMAGED W ASMFA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SW23204AM16900207 49404 728194 CAPTAIN REPORTED THAT AT 35,000 FT WITH ICE CONDITION, RT ENGINE COMPRESSOR WAS STALLED AND ABNORMAL PROCEDURE WAS PERFORMED. AIRCRAFT WAS SENT TO THE HANGAR AND BOROSCOPE INSPECTION ON 6TH, 7TH AND 13TH STAGES OF RT ENGINE WAS PERFORMED IAW MM 72-00-00. CHIP DETECTORS WERE CHECKED, BEING CORRECT. INLET AND OUTLET OF ENGINE WERE CHECKED IAW MM 71-00-00 AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-01, ALL CORRECT 2L72 4F4 FRTA6WE E9NE 20050215000102005021500010EU 2005 2 15 USAA041082 120041213A5321D53610060500000 FLOOR PANEL AIRBUS320 A320214 3930316EU CFMINTCFM56 CFM565B4 NE CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19104UW12113 0863 BFM - S1 - PANEL, 4 INCHES X 1 INCH X 0.060 INCH AREA, CORROSION; NO LEVEL OR TASK, MAIN CABIN FLOOR PANEL, 221FF. REMOVED AND REPLACED PANEL IAW SRM. (K) 2L72 4F4 FRTA28NM E38NE 20050228003372005022800337NM 2005 2 28 ASA0440370 120041227A531165465262 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - UPPER LOBE INTERIOR FRAME CRACKED AT PSU SUPPORT MOUNT BRACKET. REPAIRED CRACKED FRAME. (K) 2L72 4F4 FRTA16WE E21EU 20050310001492005031000149WP 2005 3 10 ASAA0480577 120041130A533059360071 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK - SKIN DENTED. RE-CONTOURED SKIN. INSTALLED DOUBLER. 2L72 4F4 FRTA6WE E9NE 20050330001132005033000113EA 2005 3 30 REXA05001 120041231A2750855D10011 BPSU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FLAPS FAILED A REXAO OTHER O OTHER APAPPROACH 1 SO258416B10416 7416 FLAPS FAILED AT 30 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. (K) 2L72 4F4 FRTA21EA E15NE 20040607000952004060700095NM 2004 6 7 04FDEA01078 120040423A5753ARC0512503 HINGE BRACKET DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25590FE 48505 LEFT WING, FOUND INBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-76022, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20041202002042004120200204CE 2004 12 2 DXTA200400348 120040725A3260 UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL07950QS 7500050 CLIMBING THROUGH FL390 NOSE LANDING GEAR CYCLED 5 TO 8 TIMES (VERY HARD) GEAR LIGHT CAME ON DURING EACH CYCLE. DESCENDED AND AT 8000 AND 250 KTS ONE MORE CYCLE. COMPLIED WITH LANDING GEAR CONTROL VALVE / MANIFOLD BLEED RATE CHECKLIST, DURING INSPECTION FOUND NOSE AND LEFT MLG UPLOCK SWITCH OUT OF LIMITS. READJUSTED NOSE AND LEFT UPLOCK SWITCH ALL WORK DONE IAW CHAP 32-20-00 OF THE CITATION 750 MM. 2L72 4J RTT00007WI 20040603000612004060300061EU 2004 6 3 04FDEA01415 120040523A2751 WARNING SYSTEM AIRBUS310 A310203 3930313EU COCKPIT ACTIVATED A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25410FE 356 ON DEPARTURE ECAM ALERT FLAPS SYS 2 FAULT. RECYCLED TO NO AVAIL. CATEGORY: C EXPIRATION: 01JUN04 "MEL 27-51-01-01: NR 2 SLATS / FLAPS CONTROL COMPUTER INOP. C/W PROCEDURES IN MEL 27-51-01-01, SYSTEM TESTS ARE OK. REMOVED & REPLACED NR 2 SFCC IAW A310 MM 27-51-18-4. OPS CHECKED GOOD. 2L72 4F RTA35EU 20040428000762004042800076NM 2004 4 28 SWAA041064 120040414A53116554892 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME WEB AT BS 304, STRINGER 16L, CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER ER. 2L72 4F RTA16WE 20040223000072004022300007NM 2004 2 23 G6OA04001 120040104A217018084934 COALESCER BAG DOUG MD11 MD11F 3023600NM AIR COND BAYS CONTAMINATED A G6OAAG UNSCHED LANDING O2 MASK DEPLOYED BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 EA27705GC 48412 FIFTEEN MINUTES INTO FLT, AT FLT LEVEL 310, THE LEVEL 2 (AIR SYS 1 PRESS LOW) AND (AIR SYS 2 PRESS LOW) ILLUMINATED. SMOKE WAS OBSERVED IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND DIVERSION INTIATED TO KSDF. DURING DESCENT , THE LEVEL 2 AIR SYS 3 LOW PRESS LIGHT ILLUMINATED. COALESCER BAGS CONTAMINATED WITH GLYCOL. 2L73 4F RTA22WE 20040401001092004040100109NM 2004 4 1 04FDEA00747 120040325A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25579FE 48470 FUSELAGE TRANSVERSE FRAME DENTED AT FS Y= 1761 BETWEEN LONGERONS 12R AND 13R. COMPLIED WITH FEDEX EA 1-5310-75999, REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESSMENT PER EO (NR 1-2520-7-3308) 2L73 4F RTA22WE 20040414002052004041400205NM 2004 4 14 04FDEA00236 120040128A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 FWD CARGO BAY, FRAME DENTED STA 680 STR 23 LT COMING CUT OUT DENTED MATERIAL 1 X 1 INCH FROM FRAME AT BS 680 STR 23L AND REPAIRED PER SRM 53-10-1, 51-40-3 USING 7075-T6 .050 LOT #466242. 2L73 4F RTA3WE 20040830001922004083000192EU 2004 8 30 AWXA200400705 120040613A5347D5337111200000 SEAT TRACK AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 MAJOR REPAIR - DURING C-04 CHECK CORROSION (LITE TO MODERATE PITTING) WAS FOUND ON THE LT OB Y1292 SEAT TRACK FR41-FR47. MAINTENANCE REMOVED AND REPLACED SEAT TRACK AT FR 41-47 IAW A320 SRM 51-42-11 FIGURES 9,10,12,18. 2L72 4F RTA28NM 20050118001122005011800112EU 2005 1 18 04FDEA03498 120041228A5310 SUPPORT BEAM AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25422FE 346 FR 87 LT TO RT SIDE UPPER SUPPORT BEAM HAS 70 SQ INCH OF CORROSION IN THS BAY. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED BEAM IAW SRM 51-40-21 AND 51-74-10. 2L72 4F RTA35EU 20041021000042004102100004NM 2004 10 21 ASAA0410387 120040902A5311 FRAME BOEING737 7372X6C 1384552NM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 PAE - FOUND FRAME CRACKED INBOARD FLANGE STATION 296. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2L72 4F RTA16WE 20040203001372004020300137NE 2004 2 3 MALA040124 220040121A7220200304015 ENGINE BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE NR 2 SHUTDOWN A MALAO OTHER YP ENGINE STOPPAGE NO WARNING INDICATION CLCLIMB 1 GL15532XJ E2366 DURING FLIGHT 3627, ON CLIMBOUT WHILE PASSING THRU FL250, NR 2 ENGINE AUTOMATICALLY SHUTDOWN WITH NO INDICATION OF OVERSPEED OR FIRE. QRH PROCEDURES COMPLIED. ALL OTHER ENGINE PARAMETERS LOOKED NORMAL AT THE TIME OF SHUTDOWN. MAINTENANCE REMOVED & REPLACED NR 2 ENGINE P/N 2-003-040-15, IAW JOB CARD 7100-502, S/N ON P07706, S/N OFF P07860. REF JOB CARD FOR DETAILS. OPS & LEAK CHECKS GOOD. 2H74 4F4 FRTA49EU E6NE 20040220000832004022000083EA 2004 2 20 SWIA200412855 120040202A2750865D1007 PDU CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 NM07941SW 7750 FLAPS 1/2 SPEED MESSAGE. REPLACED FLAP POWER DRIVER UNIT IAW MM 27-52-01-000-801. OPS CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 20040303000422004030300042 2004 3 3 BAQA092514 420040203A3455 POTENTIOMETER LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP VOLUME INTERMITTENT B BAQAK NONE O OTHER ININSP/MAINT 1 EA0340DK 11545 37327 092 VOLUME POT INTERMITTENT. REPLACED WITH SERVICEABLE UNIT. 02/04/2004 2L72 4F4 F A10CE E6WE 20040219002282004021900228EU 2004 2 19 027751 120040207A3210 LANDING GEAR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MAINS MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1719XS 340A019 DURING CLIMBOUT FROM PIT THE AIRCREW RAISED THE GEAR HANDLE, THE TRANSIENT LIGHT REMAINED ON AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE CREW ATTEMPTED ANOTHER GEAR CYCLE AND HAD THE SAME RESULTS. A/C RETURNED TO PIT. 2L72 4T4 TRTA52EU E8NE6 20040415000532004041500053NE 2004 4 15 QXEA200400178 220040226A73204120T00P15 FADEC CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE LT ENGINE MALFUNCTIONED A QXEAK NONE J WARNING INDICATION DEDESCENT 1 NM09615QX4901 10065 GEE965293 PDX - FLIGHT 2491 AT TOP OF DESCENT, FLIGHT LEVEL 390 FT WITH INITIAL THROTTLE REDUCTION BY A THIRD, MOVED SLOW, LEFT ENGINE FLAME-OUT CAUTION MESSAGE FOR 14-15 SECONDS. NO ABNORMAL ENGINE INDICATIONS. REPLACED LEFT FADEC AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA EOOO63EN 20040415001312004041500131NM 2004 4 15 2004UALA00305 120040402A5313 STRINGER AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29826UA 989 STRINGER 7L WAS DENTED JUST FORWARD OF FRAME 7. MAJOR REPAIRED ACCOMPLISHED. REPLACED STRINGER. 2L72 4F4 FRTA28NM E40NE 20040503002812004050300281CE 2004 5 3 YDB2004F00000 120040301A1430NAS100327H BOLT LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP CABIN DOOR BROKEN E O OTHER O OTHER NRNOT REPORTED 1 SO0935ED 215 RETURNING FROM LAST FLIGHT OF DAY PILOTS REPORTED A LOUD BANG IN UPPER MID CABIN AREA. MAINTENANCE INVESTIGATED AND FOUND UPPER CABIN DOOR FWD TORSION BAR ANCHOR BOLT BROKEN. BOLT APPEARS TO HAVE FATIGUE TYPE FAILURE. 2L72 4F4 F A10CE E6WE 20040505000322004050500032NE 2004 5 5 USA2004F00030 220040323A73211820M89P07 ECU AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A USAAO OTHER J WARNING INDICATION APAPPROACH 1 EA19117UW12013 1224 779730 ENROUTE, DURING APPROACH, RECEIVED ECAM MESSAGE, (ENG 1 FAIL), WHILE AIRCRAFT WAS AT 6,000 FEET WITH IDLE THRUST SELECTED. THE CREW TRIED, UNSUCCESSFULLY, TO RESTART THE ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 12 MINUTES. MAINTENANCE REPLACED THE LEFT ENGINE ELECTRONIC CONTROL UNIT AND INTERMEDIATE PRESSURE CHECK VALVE. OPERATIONALLY AND FUNCTIONALLY CHECKED, OK. 2L72 4F4 FRTA28NM E2GL 20040525000552004052500055NE 2004 5 25 VNAA0405005 220040504A73205071T98P03 AMPLIFIER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE FAILED A VNAAO OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL07215PS930 7880 AFTER TAKEOFF, THE LT ENGINE SURGED 10 PERCENT AND THE CREW RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE NR 1 CONTROL AMPLIFIER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20040521000502004052100050NM 2004 5 21 PCAA0405199 120040430A7931522848 INDICATOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 OIL PRESS ERRATIC A PCAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA13825EX258126283 388 120016 ABORTED TAKEOFF DUE TO THE NR 1 OIL PRESSURE FLUCTUATING DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE INDICATOR AND PRESSURE TRANSMITTER. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 20040601000152004060100015EA 2004 6 1 QXEA200400358 120040523A5240CC670381001 ROLLER CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF34* NE SERVICE DOOR LACK OF LUBE A QXEAO OTHER O OTHER UKUNKNOWN 1 NM09606QX6523 10023 SEA FLIGHT 2464, GALLEY SERVICE DOOR HARD TO OPEN. MAINTENANCE INSPECTED THE DOOR AND THEN CLEANED AND LUBED THE DOOR ROLLERS. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20040614003182004061400318WP 2004 6 14 GTIA040456 120040321A57535930495501 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D1 52044NE LT WING FLAP DELAMINATED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23817NK 49141 LT WING IB FLAP OB VANE DELAMINATED. REMOVED LT IB OB FLAP VANE. INSTALLED VANE. 2L72 4F4 F A6WE E2EA 20040614001542004061400154NM 2004 6 14 GAKA144E 120040512A6320900D1400006101 TRANSMISSION DOUG MD900 MD900 3027375NM PWA PW206 PW206A NE MAIN ROTOR CONTAMINATED E GAKAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CRCRUISE 1 NM11902SL 90000027 WHILE IN CRUISE FLIGHT, MAIN ROTOR TRANSMISSION OIL PRESSURE FLUCTUATION OCCURRED RESULTING IN A FLUCTUATION BETWEEN 65-80 PSI., WITH AN ILLUMINATION OF THE LOW OIL PRESSURE WARNING LIGHT. PILOT LANDED IMMEDIATELY AT HELIPAD. TWO QUARTS OF TRANSMISSION OIL WAS ADDED TO MOBIL SHC 626, CAUSING FOAMING AND THE ABOVE OIL PRESSURE FLUCTUATION. RE-PLACARD TRANSMISSION NEAR SIGHT GLASS IN PLAIN VIEW TO PREVENT MIXING OF OILS. DUE TO PLACARD BEING OBSTRUCTED BY NACA INLET AND FLT MANUAL WORDING. UNLESS PILOT AND/OR MECH WAS POSITIVE OF TRANS PN, IT IS EASY TO ADD WRONG TYPE OF OIL. FLUSHED TRANSMISSION TWICE AND RESERVICE WITH APPROXIMATELY 10 QUARTS OF CORRECT OIL, SYSTEM OPS NORMAL AND AIRCRAFT RETURNED TO SERVI1G72 3U3 UNCH19NM E42NE 20040614002632004061400263CE 2004 6 14 GUU2004F00019 120040520A360011891006229 HOSE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA LT NACELLE LOOSE A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO1748544 UE183 DURING FLT, LT RED T HANDLE LIGHT ILLUMINATED. RESECURED LT ENGINE BLAST TUBE. OPERATIONAL CHECK NORMAL. 2L72 4T3 TRTA24CE E2NE 20040616002012004061600201NM 2004 6 16 2004UALA00556 120040607A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 CABIN FLOORBEAM FS 1640 HAS CORROSION AROUND NUT PLATE HOLES FROM RBL 14 TO RBL 44 UPPER AFT FLANGE BOTH SIDES OF FLANGE. FABRICATED & INSTALLED FLOORBEAM AND SPLICE ANGLES. 2L72 4F4 FRTA2NM E17NE 20040616002162004061600216NM 2004 6 16 2004UALA00440 120040504A335060243 LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29331UA 24192 EMERGENCY EXIT LIGHT (EEL) INOP FROM SEAT 15 AFT. REPLACED LAST TWO SEGMENTS OF EEL LIGHTS. CLEANED WATER FROM EEL LIGHTS LAST THREE ROWS. 2L72 4F4 FRTA16WE E2GL 20040628002002004062800200EU 2004 6 28 XNOA1186 120040512A36109054M51G01 DUCT AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE NR 2 ENGINE LOOSE A XN0AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23372PC 196 517691 FIRE INDICATION ON NR 2 ENG. QRH COMPLETED, FIRE BOTTLE NOT DISCHARGED. OPS CHECK FIRE DETECTION SYSTEM IAW A300 MM REF 26-12-00, NO DEFECTS NOTED, OPS CHECKS GOOD. FOUND NR 2 ENGINE RECOUP DUCT RUPTURED. REMOVED AND REPLACED BOTH SECTIONS OF DUCT IAW A300 MM REF 20-21-12, NO LEAKS NOTED. 2L72 4F4 FRTA35EU E23EA 20040630000722004063000072CE 2004 6 30 UG8AGM0414 120040108A2810 FUEL TANK CESSNA750 750 2076810CE ALLSN AE300 AE3007A GL WING LEAKING A UG8AK NONE K FLUID LOSS ININSP/MAINT 1 GL235114 7500017 WING TANK (0) FILL ON AND VENTING FUEL FOR 3 MIN. 3400 LBS. FUEL. CREW REMINDED OF SL750-28-02 LETTER IN ALL AIRCRAFT LOG BOOKS REGARDING THIS CONDITION AND WHAT STEPS ARE NEEDED TO CORRECT THIS CONDITION. NO ACTION TAKEN. CONDITION IS NORMAL REGARDING THE LATE FILING OF THIS SDR, IT WAS DISCOVERED AS REPORTABLE, FOUND DURING AN AUDIT OF AIRCRAFT RECORDS. 2L72 4J4 FRTT00007WITE6CH 20040712000852004071200085NE 2004 7 12 MALA040473 220040624A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT & RT OUT OF RIG A MALAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 GL15364PX 340B262 A/C WOULD NOT GO INTO BOTTOM GOVERNING. HISTORY SHOWS LQC WAS THE LAST STATION WHERE ENGINE RIGGING WAS PERFORMED. A/C HAD NEITHER ENGINE CAPABLE OF GOING INTO REVERSE WHEN IT LANDED IN MEM ON A REPOSITION FLIGHT. MAINTENANCE PERFORMED RIGGING OF BOTH LT AND RT ENGINE CONDITION LEVERS FROM WING TO HMU CABLE IAW SF 340 AMM 76-10-00-05. PERFORMED ENGINE RUNS AS REQUIRED IAW 71-00-00-5. ADJUSTED CONDITION LEVERS AND REMOVED AND REINSTALLED DC GENERATORS ON BOTH SIDES. 2L72 4T4 TRTA52EU E8NE 20040708001892004070800189 2004 7 8 2004F00148 420040602A6122DCFS290D9T3 GOVERNOR CESSNA340 340A 2076405CE CONT O520 TSIO520NB 17040SO MCAULY3AF32C3AF32C505 GL RT ENGINE MAKING METAL E E ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 NM04115BH 173 340A1531 519779 022550 DURING CRUISE, AT AN ALTITUDE OF 10,000 FEET, THE PILOT NOTICED A REDUCTION IN MANIFOLD PRESSURE AND POWER FOR THE RIGHT ENGINE. THE RIGHT PROPELLER STARTED TO FEATHER. THE PILOT SHUT DOWN THE RIGHT ENGINE AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. POST FLIGHT INSPECTION FOUND THE RIGHT PROPELLER GOVERNOR HAD FAILED INTERNALLY. 1L72 3O3 O 3A25 E8CE 5 CP22EA 20040721000172004072100017NE 2004 7 21 AMTA200400623 220040601A7200 ENGINE LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122B NE NR 2 MALFUNCTIONED A AMTAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL11194AT 193B1230 10236 HIGH SHUDDER AND TGT ON CLIMB. NO FIRE INDICATION. LOW OIL QUANTITY, PRECAUTIONARY ENGINE FAILURE PERFORMED. REMOVED AND REPLACED NR 2 ENGINE IAW MM M11-71-02. COMPLIED WITH OPERATIONAL CHECKS, TESTS 1, 3, 4, 9, 12, 14 AND 15. NO LEAKS NOTED. (M) 2L73 4F4 F A23WE E12EU 20040813001022004081300102NM 2004 8 13 2004UALA00692 120040723A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29783UA 26950 FUSELAGE DAMAGE LOCATED 4 INCHES BELOW STRINGER 29L AT STA 655, GOUGE IS 7 INCHES LONG WITH MAX DEPTH .020 INCH. MAJOR REPAIR. DOUBLER IS INSTALLED AT STA 632-642, STR 28L ON LT FUSELAGE EXT SKIN. DOUBLER IS 22 INCHES BY 14 INCHES. 2L72 4F4 FRTT0001SE E46NE 20040823000442004082300044WP 2004 8 23 ABXA040290 120040804A5230591014167 PAN DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FWD CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 FORWARD LOWER CARGO DOORS OUTER PAN WAS CRACKED AT HI-LOCK ALONG AFT EDGE, CENTER STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM. 2L72 4F4 F A6WE E2EA 20040901000762004090100076WP 2004 9 1 0401199882 120040616A5312 BULKHEAD DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01670MC 47659 DURING H-CHECK FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT Z=6.0 NEAR L18R. REPAIRED IAW EA 98-199571. 2L72 4F4 FRTA6WE E2EA 20040813001702004081300170NM 2004 8 13 2004UALA00628 120040629A5330 SPLICE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE SKIN CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 SKIN SPLICE STRAP AT STA 1400 CORRODED BETWEEN STRINGERS 27L AND 30. MAJOR REPAIR ACCOMPLISHED. REPLACED SECTION BETWEEN STR 26L AND 28L AND INSTALLED EXTERNAL DOUBLER CENTERED ON STR 29L. 2L72 4F4 FRTA2NM E17NE 20040907000902004090700090NM 2004 9 7 P5CA0401162 120040802A5753 FAIRING BOEING747 747249F 1384849NM PWA JT9 JT9D7Q 52054NE FLAP TRACK DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23920FT 22237 DELAMINATION ON SEVERAL AREA OF NR 3 FLAP TRACK, AFT FAIRING RT WING. REMOVED DAMAGE AREA & REBONDED PER SRM 51-40-15. 2L74 4F4 F A20WE E3NE 20040908000892004090800089CE 2004 9 8 GLBA20030654 120040624A5210 STRUCTURE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA CABIN DOOR CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03253GL UE253 CABIN DOOR CORROSION, REPAIRED DOOR. 2L72 4T3 TRTA24CE E2NE 20040908001012004090800101NM 2004 9 8 AWXA200400771 120040710A5347D53472210000 SEAT TRACK AIRBUSA319 A319132 3930340NM IAE V2500 V2500A1 NE FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28806AW 1056 DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2. 2L72 4F4 FRTA28NM E311NE 20040818001862004081800186NM 2004 8 18 WLDA200455 120040802A5512ALC8101504 PANEL DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11278WA 48746 ITEM: DURING 4C-CHECK, PERFORMED INSPECTION IAW EO 02-5510-098 REV NR 1, FOUND CORROSION LOCATED AT HORIZONTAL STABILIZER RT BARREL NUT HOLE NR 6. PERFORMED CORROSION REPAIR IAW EO 02-5510-098 REV NR 1. CONDITION CHECK OF HORIZONTAL STAB RT BARREL NUT HOLE NR 6 FOUND SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20040823000352004082300035WP 2004 8 23 ABXA040292 120040805A53134912798501 LONGERON DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 LONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5. 2L72 4F4 F A6WE E2EA 20040830001182004083000118SW 2004 8 30 ALGA096938 120040627A63206893672 GEAR BELL 407 407 1182206SW ALLSN 250C 250C47B GL GEARBOX DEFECTIVE B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03617AL765 53265 CAE847222 REMOVED GEAR DUE TO UNEVEN WEAR PATTERN, REPLACED PART WITH NEW ITEM. 1G71 3U3 UO H2SW E1GL 20040913001072004091300107NM 2004 9 13 DHL2004745512 120040703A5310 WINDOW FRAME BOEING727 727224 1384076NM PWA JT8 JT8D* NE FUSELAGE DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01745DH 20665 DURING A C-CHECK, THE FOLLOWING DESCREPANCIES WERE NOTED; RT "F-N" WINDOW POST CROCK INDICATION AT POINT N MOST OB BOLT HOLE TOP FRAME WINDOW NR 5 MARKED NDT X-RAY FINDING. INSTALLED RT WINDOW POST REPAIR KIT PN65635282-8 PO NR 427441 IAW S/B 727-53-0086 REV 11 PART NR. 2L73 4F4 F A3WE E2EA 20040819000042004081900004EU 2004 8 19 KBM2004F00160 120040721A2110507 COMPRESSOR SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE AIR CONDITIONER SEIZED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19350SH 2957 A/C COMPRESSOR AND PULLEY BEARING SEIZED. REPLACED COMPRESSOR ASSY AND BELT. 1G71 3U3 UNCH9EU E19EU 20040914001862004091400186NE 2004 9 14 ANCF200400023 220040802A7200 ENGINE DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT BIRD INGESTION W ANCFC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 SO23190AN 53190 726846 A BIG BIRD WAS INGESTED THE TAKE OFF ROLL IN THE RT ENG TAKE OFF WAS CONTINUED IT OPERATED, AT ROTATION RT ENG WAS REDUCED AT 800 FT TO IDLE AIR RETURN WAS MADE AFTER THE SURGE CHECKLIST WAS ACCOMPLISHED REDUCED TAKEOFF FLEX WAS 1.84 AFTER IMPACT IT WENT DOWN TO 1.64. ACCOMPLISHED BOROSCOPE INSPECTION TO RT ENGINE S/N 726846 TO FAN BLADE 1.5 STAGE COMPRESSOR BLADE, 6 STAGE COMPRESSOR BLADE AND 7 STAGE COMPRESSOR BLADE NO DAMAGE WAS FOUND IAW AMM 72-00-00 PAGE 601 TO 642 ENGINE RUN UP WAS ACCOMPLISHED IAW AMM 71-00-00 SATISFACTORY. 2L72 4F4 FRT E9NE 20040913000802004091300080EU 2004 9 13 CX7A194J0446 120040805A3297 WIRE HARNESS SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT MLG INDICATOROPEN A CX7AO OTHER N FALSE WARNING LDLANDING 1 GL03314CE 340B335 LT GEAR INDICATION INOPERATIVE, PRESS TO TEST OK. FOUND DOWNLOCK AT SGA OPEN AT J1. RECONNECTED WIRE DG505 TO GROUND. 2L72 4T4 TRTA52EU E8NE 20040913000832004091300083SO 2004 9 13 C2XA04BT078 120040715A335066367 LIGHT EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2713990 145277 CREW REPORTED, (STRIP OF EMERGENCY AISLE PATH LIGHTS NOT WORKING.) MAINTENANCE RELEASED THE AIRCRAFT IAW MEL NR 33-50-00/02 CATEGORY C-PLACARD NR 044167 AND RETURNED THE AIRCRAFT TO SERVICE. ON IAD RON 07/16/2004 MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED FORWARD AISLE PATH EMERGENCY LIGHT STRIP IAW AMM NR 33-50-12, OPS. CHECKED GOOD AND MEL PLACARD CLEARED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040913001402004091300140CE 2004 9 13 62683 120040630A29101013880083 VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6* 52043EA HYD SYSTEM MALFUNCTIONED A AMWAO OTHER J WARNING INDICATION APAPPROACH 1 CE07173YV UE173 LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. GEAR FINALLY EXTENDED ON THE SECOND ATTEMPT. REMOVED AND REPLACED HYD SERVICE VALVE. OPS CK GOOD. 2L72 4T3 TRTA24CE E2NE 20040928000392004092800039NM 2004 9 28 04FDEA02801 120040922A5320 INTERCOSTAL BOEING727 727200 138407ENM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25240FE 20978 FWD CARGO, INTERCOSTAL IS CRACKED AT STRINGER 25L STA.624. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED,TREATED AND PRIMED NEW INTERCOSTAL IAW SRM 51-20-1 FIG.6, 51-30-5 AND 51-10-2. INSTALLED IAW SRM 51-30-2. FABRICATED INTERCOSTAL USING 2024-T3 .050, BATCH NR 8692, P.O. NR MST0012781. 2L73 4F4 FRTA3WE E2EA 20040922000762004092200076EA 2004 9 22 SWIA200413799 120040612A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW LT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTION.) SB 601R-53-055 REVISION A, STRUCTURAL REPAIR AT FUSELAGE STATION (FS) 718.00 BETWEEN STRINGERS 10 AND 12, PART B INCORPORATED. 2L72 4F4 FRTA21EA E15NE 20040923000342004092300034CE 2004 9 23 DXTA200400383 120040907A3230AIR4854313 VALVE RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP MLG MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07873QS1793 258573 UPON GEAR RETRACTION THE RT GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED, COULD ALSO HEAR WIND NOISE. REMOVED AND REPLACED THE RT REVERSING VALVE IAW MM CHAPTER 22-30-31, OPS CHECK SATISFACTORY. 2L72 4F4 FRTA3EU E6WE 20041001000542004100100054EA 2004 10 1 COMA0460548 120040928A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01967CA 7134 FUSELAGE IS CRACKED ON RT SIDE JUST AFT OF NOSE LANDING GEAR DOOR AT FS 230. REPARIED IAW REO 601R-53-11-048. 2L72 4F4 FRTA21EA E15NE 20040920000192004092000019NM 2004 9 20 AWXA200401030 120040909A534765403526 GALLEY TRACK BOEING737 7373G7 1384595NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28308AW 24710 DURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY IB TRACK AT BS 294 RBL 16, WL 208.5. MAINTENANCE REMOVED DAMAGED SECTION OF FORWARD GALLEY IB TRACK AT BS 294 RBL 16; FABRICATED A NEW REPLACEMENT SECTION OF TRACK IAW DWG 65-45834-6; INSTALLED REPAIR PART IAW SRM 51-40-02, FIG. 2 & 13. 2L72 4F4 FRTA16WE E21EU 20041027000492004102700049NM 2004 10 27 2004UALA00880 120040917A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 FWD PIT FRAME AT BS 520 AND STR 24L IS DENTED ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER ANGLE. 2L72 4F4 FRTA2NM E17NE 20041027000952004102700095WP 2004 10 27 R2J2004F00003 220040915A722031018303 DUCT MTSBSIMU2 MU2B40 5780440CE GARRTTTPE331TPE33110 01514WP LOOSE VANES LOOSE B R2JRO OTHER O OTHER NRNOT REPORTED 1 EA21361MA4055 429SA P36199 ENGINE WAS TORN DOWN FOR AN AUDIT OF ITS SB AND TBO CONFIGURATION, DUE TO CROSSOVER DUCT (DIFFUSER) FAILURE OF ITS (SISTER ENGINE) ON THE SAME AIRCRAFT. IT WAS FOUND, THE MAINTENANCE RECORDS CONCERNING SB STATUS AND TBO STATUS WERE IN ERROR ON THIS ENGINE ALSO AND INSPECTION OF THE CROSS0VER DUCT ASSEMBLY IN THIS ENGINE WAS FOUND VERY LOOSE, BUT NOT YET FAILED. FAILURE OF THIS PART WAS IMMINENT AND SEALS IN THIS DUCT WERE MOSTLY FAILED, AFFECTING COMPRESSOR AND ENGINE POWER. (EA21200502933) 1H72 3T4 TRTA10SW E4WE 20041102000432004110200043EU 2004 11 2 2004UALA00776 120040818A2910 HYDRAULIC SYSTEM AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GREEN SYSTEM LOW A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29417UA 483 FLT EXPERIENCED LOSS OF ALL QTY GREEN HYDRAULIC SYSTEM. DECLARED EMERGENCY & CONTINUED TO PLANNED DESTINATION. AIRCRAFT LOST GREEN HYDRAULIC QUANTITY INFLIGHT. LANDING GEAR EXTENDED VIA GRAVITY. OAKLAND SERVICED GREEN SYSTEM TO FULL. RAN ALL SYSTEMS, VERIFIED NO LEAKS AND CHECKED ECAM FOR QUANTITY AND PRESSURE. ALL INDICATIONS NORMAL. 2L72 4F4 FRTA28NM E40NE 20041122002692004112200269NM 2004 11 22 USAA040717 120040910A5754 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 3 SLAT TE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 LOWER SKIN, 1 INCH LENGTH, CHAFE WEAR, NR 3 SLAT LOWER SURFACE TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW DOUBLER, FILLER, NEW CORE, TOP DOUBLER, IAW SRM 51-70-10. 2L72 4F4 FRTA16WE E21EU 20041124001142004112400114NE 2004 11 24 A6WA200440154 220041017A7200 COVER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 1 ENGINE UNSECURE A A6WAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31450AW 7823 IN FLIGHT, LOW OIL PRESSURE ILLUMINATED NR 1 ENGINE OIL PRESSURE FLUCTUATED AT CLIMB AND IDLE SETTINGS. AC RETURNED TO FIELD AT 32,000 FT. PRESSURE DROPPED TO 25 PSI THROTTLE BACK PRESSURE TO 60 PERCENT AT 33,000 FT PRESSURE FLUCTUATED 40 PERCENT-50 PERCENT-45 PERCENT- 55 PERCENT. FOUND CRANKING PAD COVER OFF, REINSTALLED COVER. ADDED 1 QUART OIL, IAW AMM 72-00-00. PERFORMED ENGINE RUNS IAW AMM 71-00-00. NO DEFECTS NOTED. 2L72 4F4 FRTA21EA E15NE 20041124001632004112400163SO 2004 11 24 O2G2004F00005 120041011A2130 CONVERTER GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU CABIN PRESSURE FAILED E O2GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE03590DA8449 5669 445 RT CONVERTER FAILED AND LOST AUTO CONTROL OF PRESSUREIZATION. RAN CHECKLIST SEVERAL TIMES WITH NO EFFECT. REMOVE AND REPLACED CONVERTER. 2L72 4F4 F A12EA E2EU 20041129000502004112900050NM 2004 11 29 ASAA0410407 120040928A53306545767541 SKIN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 DAMAGE ON SKIN. REPAIRED DAMAGE ON SKIN. 2L72 4F4 FRTA16WE E2EA 20041201000862004120100086NE 2004 12 1 DLM88041047 220041121A7261 OIL FILTER DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE CLOGGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27998DL36667 53370 725627 ON CLIMBOUT GOT FLICKERING MASTER CAUTION THEN LT OIL STRAINER CLOGGED MSG. FOLLOWED IAW. REPLACED OIL FILTER, NO METAL OR CARBON. 2L72 4F4 FRTA6WE E9NE 20041201001202004120100120NE 2004 12 1 COMA0460616 220041111A72615018T49P01 CARBON SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT ENGINE UNRELIABLE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01814CA 7387 FLIGHT 5912 RT ENGINE OIL PRESSURE AND TEMP DROPPING DURING FLIGHT. IFSD REPLACED THE ACCESSORY DRIVE GEARBOX CARBON SEALS AT AXIS BB, D AND F. 2L72 4F4 FRTA21EA E15NE 20041207000852004120700085NM 2004 12 7 USAA040847 120041018A532065C10592154 INTERCOSTAL BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 INTERCOSTAL, .5 INCH CRACK, STA 947.5, LBL43. REPLACED INTERCOSTAL IAW SRM 51-70-11. 2L72 4F4 FRTA16WE E2GL 20041129001602004112900160NM 2004 11 29 GAIA04162 120040910A5314 KEELBEAM BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND LT WHEEL WELL KEELBEAM WEB CRACKED AT BS870, AT FORWARD SIDE OF APU CUT-OUT. REF FASI NR 86981, ACCOMPLISHED DOUBLER REPAIR IAW SRM51-40-2. 2L73 4F4 F A3WE E2EA 20041129002062004112900206CE 2004 11 29 CED2004F00004 120040528A2612 FIRE WARNING LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE NR 2 ENGINE FALSE ACTIVATIONE CEDAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW058005Y 121 241C287A WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR 2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT. ONCE CREW LANDED THEY COULD FIND NO EVIDENCE OF FIRE. MAINTENANCE CREW IS ENROUTE TO AIRCRAFT. SUSPECT FALSE FIRE WARNING INDICATION. 2L72 4J4 J A10CE 1E16 20041210000302004121000030 2004 12 10 GTIA040791 420040930A2565 SLIDE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE L2 DOOR LOOSE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23819NK 48016 SLIDE PACK ON L2 DOOR LOOSE FROM DOOR. RESECURED SLIDE PACK ON L2 DOOR IAW MM 25-62-00. 2L72 4F4 F A6WE E9NE 20041215000042004121500004NM 2004 12 15 USAA040902 120041029A5343 SUPPORT FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT MLG AFT SPAR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - L/G SUPPORT FITTING, .2500 INCH CRACK, LT MLG SUPPORT FITTING AT REAR SPAR. REMOVED AND REPLACED WITH NEW FITTING IAW EO 5702V054. 2L72 4F4 FRTA16WE E21EU 20041215000502004121500050NM 2004 12 15 ASAA0410422 120041003A5340654868957 ANGLE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION ON UPPER FLANGE OF L-ANGLE. REMOVED CORROSION IN AN AREA 1 INCH X 20 INCHES. REMOVING .075 INCHES FROM AN ORIGINAL .200 INCHES, FOUND TO BE OUT OF LIMITS. REPAIRED IAW EA. 2L72 4F4 FRTA16WE E2EA 20041215001022004121500102WP 2004 12 15 ASAA0480507 120040924A573059368449 SKIN DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT WING GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, RT WING LOWER IB T/E SKIN GOUGED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-10-4, 57-22-3. 2L72 4F4 FRTA6WE E9NE 20041221000172004122100017WP 2004 12 21 GTIA040832 120040930A5347 SPLICE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE LT CARGO TRACK CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23823NK 48020 SAS B00176-18-00074; AFT PIT CORROSION UNDERSIDE L/T CARGO TRACK SPLICE AT FS 1231-1250. REMOVED CORROSION IAW SRM 51-10-3, REMOVED DAMAGED CARGO TRACK, DRILLED AND LOCATED HOLES IN NEW CARGO TRACK SPLICE AT FS 1231-1250. REMOVED CORROSION IAW SRM 51-10-3, REMOVED DAMAGED CARGO TRACK, DRILLED AND LOCATED HOLES IN NEW CARGO TRACK, TREATED AND PRIMED AND TOPCOAT CARGO TRACK. 2L72 4F4 F A6WE E9NE 20041228001142004122800114NE 2004 12 28 XNOA1218 220041221A7200 ENGINE BOEING727 727200 138407ENM PWA JT8 JT8D9A 52048NE NR 1 MALFUNCTIONED A XN0AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL2379754 21363 NR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME. 2L73 4F4 FRTA3WE E2EA 20050104000192005010400019EA 2005 1 4 ASOA04880 120041103A5242H34455 HANDLE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE E/E BAY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27845AS 7324 DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 20050104000432005010400043EA 2005 1 4 ASOA04901 120041114A33504871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE CABIN DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27863AS 7487 DURING A GROUND INSPECTION, THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 OPERATIED INTERMITTENTLY. MAINTENANCE RESECURED THE CONNECTION TO THE EMERGENCY FLOOR TRACK LIGHT BETWEEN ROWS 6 AND 7 AND ALSO REMOVED AND REPLACED A SECTION OF THE FLOOR TRACK COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OF FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041221001592004122100159NE 2004 12 21 JX62004F00001 220041110A7200JT15D4 ENGINE MTSBSIMU300 MU300 5780602CE PWA JT15 JT15D4 52112NE NR 1 FAILED E JX6AO OTHER J WARNING INDICATION DEDESCENT 1 CE09824DW11443 A075SA PCE71099 DURING DESCENT, THE FLIGHT CREW REDUCED THE POWER LEVERS TO IDLE. NOTICED THAT THE ENGINE PITCH NOISE CHANGED CONSIDERABLY. THE MASTER CAUTION LIGHT CAME ON WITH AN (ENG LO OIL PRESS) LIGHT. THE CREW FOLLOWED THE CHECKLIST FOR AN ENGINE FAILURE OR ENGINE SHUTDOWN IN FLIGHT, AND SHUT THE ENGINE DOWN. DECLARED AN EMERGENCY AND CONTINUED WITHOUT FURTHER INCIDENT. 2H72 4F4 FRTA14SW E1NE 20050106001002005010600100NM 2005 1 6 2004UALA01252 120041227A2120 ODOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DETECTED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP29592UA 28143 OILY SMELL IN CABIN AFTER ENGINE START AND REMAINED DURING FIRST HOUR OF FLIGHT WITH LEFT ENG BLEED AND LEFT AIR COND ON. 2L72 4F4 FRTA2NM E17NE 20050110001592005011000159NM 2005 1 10 USAA040983 120041110A575465C26603100 STRUCTURE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 4 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19518AU49476 23704 PIT - Q5 - NR 4 SLAT, SEVERAL .1250 INCH TO .2500 INCH CRACKS, LWR SURFACE, AFT ROW RIVETS AREA OF ACTUATOR. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. 2L72 4F4 FRTA16WE E21EU 20050113000432005011300043NM 2005 1 13 2004UALA01197 120041208A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29576UA 26690 DENT ON INNER FRAME CHORD AT STA 660 NEAR STR-24L. CAUSED BY TYPICAL CARGO LOADING. "J" ANGLE REPAIR WAS ACCOMPLISHED. 2L72 4F4 FRTA2NM E17NE 20050222001852005022200185GL 2005 2 22 ERAA096619 220040410A7323252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE SPLIT B ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH11503 S675 CAUSING TORQUE SPLITS. INPUT LEVER STIFF. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20050307003452005030700345NM 2005 3 7 ASAA0410683 120041130A532069353521 ANGLE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE, D-CHECK: CORROSION ON WEB ANGLE. REPLACED WEB ANGLE. 2L72 4F4 FRTA16WE E2EA 20050308000622005030800062NE 2005 3 8 200411009 220041116A7200 COVER DOUG MD80 MD83 3023681NM PWA JT9 JT9D* NE RT ENGINE CRACKED W ASMFC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW23881LF 53051 728260 AIRCRAFT WITH CAPTAIN REPORT THAT EGT DIFFERENCES BETWEEN ENGINES CONTINUE AT TAKEOFF RUN, LEFT ENGINE HAD EPR 1.87, EGT 510 °C, RIGHT ENGINE HAD EPR 1.78, EGT 580 °C AND THE ACCELERATION WAS STOPPED AT THIS POINT. AIRCRAFT WAS SENT TO THE HANGAR AND CIRCUMFERENTIAL CRACK BETWEEN 6 TO 7 HRS POS OF SECONDARY PATH COVER WAS DETECTED AND RIGHT ENGINE WAS REPLACED IAW MM 71-00-01 AND 71-00-02, TESTS WERE CORRECT. 2L72 4F4 FRT E20EA 20050310001642005031000164WP 2005 3 10 ASAA0480584 120041130A5752591041449 TAB DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ELEVATOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02962AS 53076 HV-CHECK-LT ELEVATOR GEARED TAB LOWER SURFACE IS DENTED. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER.(K) 2L72 4F4 FRTA6WE E9NE 20050321002452005032100245EA 2005 3 21 ASOA04946S 120041129A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27860AS 7433 DURING AN A-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT BATT RIB ASSY AT WS 53.60 IAW EO. (K) 2L72 4F4 FRTA21EA E15NE 20050406000162005040600016NM 2005 4 6 72300061 120041017A5330 SKIN BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 2 INCH BY 2 INCH AREA OF CORROSION AROUND ANTENNA MOUNT ON FUSE SKIN. 2L73 4F4 FRTA3WE E2EA 20060216002092006021600209WP 2006 2 16 IXXA060162S 120040611A5712 RIB DOUG DC8 DC873F 302199FWP GE CFM56 CFM56* 13802NE LT WING GOUGED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK, FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SRM 57-2-0, 57-5-0, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20041228001252004122800125NM 2004 12 28 C1HA200493017 120041124A5230 WEB BOEING727 727212 138407GNM CARGO DOOR CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 GL15293AS 21348 AFT CARGO DOOR INNER AFT WEB IS CRACKED OUT. INSTALLED DOUBLER PER SRM, MINOR. 2L73 4F A3WE 20041022000262004102200026EA 2004 10 22 SWIA200413979 120041014A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07903SW 7425 REAR RIGHT EMERGENCY LIGHTS INOPERATIVE. RELAMPED AFT EMERGENCY INTERIOR OVERHEAD LIGHT IAW CRJ AMM REF CHAP 33-50-00, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20041022000552004102200055EA 2004 10 22 SWIA200413775 120040905A274183963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07937SW3851 3851 7735 DURING PRESTART CHECK, STAB TRIM CHANNEL 1 STATUS MESSAGE. REMOVED AND REPLACED HSTA AND HSTMCU IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1015. 2L72 4F RTA21EA 20040607000592004060700059NM 2004 6 7 04FDEA01619 120040604A2810 STRUCTURE BOEING727 727200 138407ENM CTR FUEL TANK CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25222FE 20933 CORROSION AT LOWER SURFACE OF CTR FUEL TANK, BS 830, RBL 26, WL 160, JUST ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION AT LOWER SURFACE OF CENTER FUEL TANK - BS 830, RBL 26, WL 160 ABOVE PRIMARY HEAT EXCHANGERS FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. REPAIRED AREA PER SRM 57-30-3. 2L73 4F RTA3WE 20050103001292005010300129NM 2005 1 3 04FDEA03419 120041215A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25577FE 48469 MAIN DECK - SEAT TRACK RBL 8 CORRODED AT STA 535 TO STA 575. REMOVED AS PER SRM 51-21-01 VOL II. MATERIAL THICKNESS=0.100, MATERIAL REMOVED=0.034, MATERIAL REMAINED=0.066 AND FOUND OUT OF LIMIT AS PER SRM 53-70-00 FIG 3 VOL I. DAMAGED TRACK CUT AS PER SRM 53-70-00 FIG 1 VOL I AND REMOVED AS PER SRM 51-31-01 VOL II. REPAIR SPLICE AND REPAIR SEAT TRACK FABRICATED AS PER SRM 53-70-00 FIG 1 VOL I. REPAIR PARTS INSTALLED AS PER SRM 53-70-00 FIG 1 VOL I AND SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20040520000832004052000083NM 2004 5 20 P5CA0401074 120040415A573065B11632155 PANEL BOEING747 7472D3B 1384805NM LT WING DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23505MC 21251 LT WING ACCESS PANEL OB AND FWD OF NR 4 FLAP TRACK FIX FAIRING 3 X 3 INCH HOLE. REMOVED DAMAGED ACCESS PANEL FOR REPAIRS, INSTALLED SERVICEABLE PANEL IAW SRM. 2L74 4F RTA20WE 20040218001022004021800102NM 2004 2 18 04FDEA00234 120040128A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 FWD CARGO BAY, FRAME DENTED STA 700 STR 23L. REMOVED DENTED MATERIAL FROM FWD CARGO BAY, FRAME AT BS 700, STR 23L, 24L AND REPAIRED PER SRM 51-40-3 USING 7075-T6 .050 LOT 466242, CUT OUT WAS 1X1 INCH. 2L73 4F RTA3WE 20040604000092004060400009WP 2004 6 4 04FDEA01439 120040525A3260 WARNING LIGHT DOUG DC10 DC1030 3023501WP COCKPIT INTERMITTENT A FDEAK NONE N FALSE WARNING CLCLIMB 1 SO25306FE 48287 LEFT MAIN GEAR LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP/IN, S/O PANEL LEFT GEAR (MAIN) LIGHT WAS INTERMITTENTLY ON. COMPLETED RED TABS, ALL LIGHTS CHECKED OUT. PERFORMED SELF CHECK OF PSEU CHECK CHANNELS 8, 12, 16 AND 20, NO FAULTS NOTED AND PER DC-10-30, QRH 2-6-2-6, OPS CHECK GOOD IAW DC-10-30 TAFI 32-30-00. 2L73 4F A22WE 20040927000482004092700048SO 2004 9 27 CHQA000530 120040725A3350 LIGHT EMB 145 EMB145MR 3260213SO CABIN MISINSTALLED A CHQAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL11975RP 145322 SEVERAL EMERGENCY FLOOR LIGHTING STRIPS ARE INSTALLED INCORRECTLY. INSTALLED EMERGENCY FLOOR PROXIMITY LIGHTING STRIP IN CORRECT POSITIONS IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD. 2L72 4T RTT00011AT 20040920001842004092000184 2004 9 20 SWAA042681 420040915A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040720000322004072000032NM 2004 7 20 SWAA042015 120040716A53306545768 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 315, STRINGER 19R, CRACKED. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040202001872004020200187NE 2004 2 2 CALA0400021 220040114A7200 ENGINE BOEING757 757224 1384958NM RROYCERB211 RB211535E43754555NE NR 1 MAKING METAL A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2719136 29285 31556 SMOKE WITH OILY ODOR REPORTED IN CABIN & NR 1 ENG AUTO SHUTDOWN. A/C DIVERTED & LANDED WITHOUT INCIDENT. INSP OF NR 1 ENG FOUND CHIP DETECTORS COVERED IN METAL, ENG OIL QTY ZERO, & DAMAGE TO NR 1 ENG FAN & COWL. A/C OUT OF SERVICE FOR REMOVAL OF NR 1 ENG. INVEST REVEALED THAT THE CAUSE OF ENGINE FAILURE WAS DUE TO FAN BLADE FAILURE CAUSED BY SOFT BODY FOD IMPACT. RESULTING DAMAGE FROM THE FAILURE OF THE FAN BLADES INCLUDED A HOLE IN THE NOSE COWL, DAMAGE TO THE FAN COWL, AND THE SEVERING OF OIL SUPPLY TUBES AND SPEED PROBE HARNESS. INVEST REVEALED THAT ENGINE DID NOT AUTO SHUTDOWN (AS PREVIOUSLY STATED), RATHER THE SPEED INDICATION DROPPED TO ZERO DUE TO SEVERING OF THE PROBE HARNESS. 2L72 4F4 FRTA2NM E12EU 20040209000722004020900072NE 2004 2 9 F3LA200400003 220040125A72303380021140 FAN BLADE AIRBUSA319 A319111 3930336NM GE CFM56 CFM56* 13802NE NR 1 ENGINE BENT A F3LAK NONE O OTHER ININSP/MAINT 1 NM03923FR 2019 575641 ON WALKAROUND, FLIGHT CREW REPORTED NR 1 ENGINE BLADES BENT. REPLACED DAMAGED FAN BLADES AT POSITIONS 2, 3, 4, 6, 7, 8, 9, 10, 11, 12, 15, 16, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 34, AND 35. POSITIONS 14, 18, 32 AND 36 WERE NOT MOVED. POSITIONS 1, 5, 13 AND 17 WERE REMOVED SERVICEABLE. POSITIONS 10, 12, 19, 22, 27, 30, 31, 33 AND 35 WERE REMOVED UNSERVICEABLE. COMPLIED WITH WORK CARD MP72400-1 AND NO DEFECTS WERE NOTED PER AMM 72-21-00-300-028. IT IS SUSPECTED DAMAGE WAS RESULT OF ICE INGESTION. 2L72 4F4 FRTA28NM E2GL 20040303002152004030300215EU 2004 3 3 2004UALA00122 120040213A2910 CHECK VALVE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE HYD SYSTEM OVERHEATED A UALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29448UA 842 RETURN TO FIELD DUE TO YELLOW HYDRAULIC SYSTEM OVERHEAT. REPLACED THE YELLOW ELECTRIC PUMP CHECK VALVE 3083GM. CHECK VALVE WAS BROKEN INTERNALLY. 2L72 4F4 FRTA28NM E40NE 20040304000202004030400020EU 2004 3 4 BAQA092352 120040216A6330L633M2010105 MOUNT UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE M/R GEARBOX LEAKING B BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03603ME156 0284 MAIN ROTOR GEARBOX MOUNT PLUNGER RETRACTED, LEAKING. UNIT WAS INTENDED FOR A/C S/N 0009, BUT WAS USED FOR A/C S/N 0284. REPLACED WITH SERVICEABLE UNIT. 02/23/2004 1G72 3U3 U H88EU E42NE 20040317000232004031700023NM 2004 3 17 2004UALA00167 120040219A5397 WIRE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29653UA 25391 WIRE DAMAGE AFT CARGO PIT STA 1230. THERE WAS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE DAMAGE. THERE WAS NO APPARENT CHAFING. THERE WERE METAL CHIPS NOTED IN THE AREA, BUT NONE FOUND DIRECTLY ON OR BELOW THE WIRE BUNDLE. IT IS UNKNOWN, AS TO WHETHER THESE MAY HAVE CONTRIBUTED TO THE DAMAGE. WIRES W710-551-20, W710-582-20, W710-307R/Y/B-20, W710-338R/Y/B-20, W710-335R/Y/B-20, W710-304R/Y/B-20, W710-167-20, W710-592-20, W710-581-20, W710-591-20, W710-323R/Y/B-20, W710-572-20, W710-502-20 HAVE BEEN REPAIRED OR REPLACED AS REQUIRED. ITEM IS BEING REVIEWED WITH BOEING. 2L72 4F4 FRTA1NM E24NE 20040325000752004032500075 2004 3 25 AC2A093324 420040130A3425430375001105 DISPLAY BELL 430 430 1182150SW ALLSN 250C 250C* GL INST PANEL INOPERATIVE B AC2AK NONE O OTHER ININSP/MAINT 1 SO07430CH6588 49037 LT DISPLAY STAYES DIM 5-10 MINUTES AFTER POWERING UP. REPLACED UNIT 1G72 3U3 URTH9SW E4CE 20040329001462004032900146NM 2004 3 29 2004UALA00207 120040307A4910 SHROUD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE APU INLET CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29202UA 24717 UPPER APU INLET SHROUD CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW BULKHEAD. 2L72 4F4 FRTA16WE E2GL 20040412001322004041200132NM 2004 4 12 2004UALA00278 120040324A5743 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29203UA 24718 THE RIGHT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. FITTING REPLACED. 2L72 4F4 FRTA16WE E2GL 20040422001702004042200170CE 2004 4 22 KW32004F00001 120040401A3260444EN2R SQUAT SWITCH LEAR 45 45LEAR 5170805CE GARRTTTFE731TFE731* 01518WP MLG INOPERATIVE B KW3RO OTHER O OTHER NRNOT REPORTED 1 WP07401Q 217 DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT ONE EACH SET SCREW WAS MISSING FROM LT IB, RT IB, AND RT OB LEVER ARMS. PROBABLE CAUSE UNKNOWN AT THIS TIME. MISSING SET SCREWS, PN 632UNC2A MUST BE INSTALLED IAW MM. 2L72 4F4 FRTT00008WIE6WE 20040429000742004042900074EU 2004 4 29 BAQA093758 120040324A6330L633M2010104A004MOUNT UROCOPEC135 EC135T1 5620026EU TMECA ARRIUSARRIUS2B1 NE M/R GEARBOX LEAKING E BAQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA03522ME920 0144 LEAKING AND RETRACTED TOO FAR. REPLACED WITH SERVICABLE UNIT. 03/26/2004 1G72 3U3 U H88EU E34NE 20040505000502004050500050EU 2004 5 5 SDR2004019 120040313A3222D56797 AXLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE NLG BROKEN A TRBAO OTHER O OTHER TXTAXI/GRND HDL 1 SO21438AT17825 438 WHILE PERFORMING AN ENGINE POWER CHECK, THE NOSE GEAR AXLE (LT) ASSEMBLY BROKE DOWN. REMOVED AND REPLACED THE NOSE GEAR SHOCK ABSORBER ASSY. 2H72 4T4 TRTA53EU E20NE 20040426001172004042600117NM 2004 4 26 2004UALA00336 120040413A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29557UA 26653 AFT PIT FUSELAGE FRAME STA 1440, INNER FLANGE HAS A DENT AT STR 26L. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR ANGLE. 2L72 4F4 FRTA2NM E17NE 20040505000312004050500031EU 2004 5 5 USA2004F00027 120040416A32301701941B MODULE EMB ERJ170ERJ170100 EU GE CF34 CF34* NE COCKPIT FAULTY A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19802MD233 17000013 CREW WAS UNABLE TO MOVE THE LANDING GEAR LEVER TO THE (UP) POSITION AFTER TAKEOFF. FLIGHT RETURNED WITHOUT INCIDENT. MAINTENANCE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND SPDA 1 POWER MODULE OPERATIONALLY CHECKS SATISFACTORY. 2L74 4F4 FRTA56NM E15NE 20040507000202004050700020GL 2004 5 7 BAQA094292 220040406A73141C2711FR PUMP AGUSTAA109 A109A2 0260120EU ALLSN 250C 250C20B 03013GL FUEL SYSTEM INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03109CJ4246 7280 FUEL PUMP INOPERATIVE. REPLACED WITH SERVICABLE UNIT. 04/29/2004 1G72 3U3 U H7EU E4CE 20040510002752004051000275NM 2004 5 10 2004UALA00408 120040423A32116549488 FITTING BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LT MLG CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29390UA39710 24665 THE LT MLG BEAM O/B FITTING WAS FOUND CRACKED BEYOND LIMITS. FITTING WAS REPLACED 2L72 4F4 FRTA16WE E2GL 20040504000672004050400067EU 2004 5 4 SIMA200410110 120040331A5330 SKIN SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21374AE 340B374 DURING AN MBV INSPECTION AND REPAIR OF HAIL DAMAGE. FROM PREVIOUS REPAIR STATEMENT TWO DENTS AT STA 464 AND 487. RECONTOURED THE TWO DENTS AND PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW REPAIR STATEMENT. 2L72 4T4 TRTA52EU E8NE 20040506000242004050600024EU 2004 5 6 PG9R117580A 120040119A1810350A21004828 FITTING UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE CRACKED B PG9RO OTHER O OTHER NRNOT REPORTED 1 WP19130PH663 3670 FORWARD FITTINGS CRACKED. (RMA NR R046607) 1G72 3U3 U H9EU E00054EN 20040510002542004051000254NM 2004 5 10 2004UALA00384 120040420A5320 INTERCOSTAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29387UA 24662 CABIN L1 DOOR SURROUND STRUCTURE INTERCOSTAL WEB CRACKED AT BS 294.5 STR 7L. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW INTERCOSTAL. 2L72 4F4 FRTA16WE E2GL 20040512001052004051200105GL 2004 5 12 ERAA094436 220040215A7320252466715 GOVERNOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE MALFUNCTIONED A ERAAO OTHER O OTHER NRNOT REPORTED 1 AL03294EH12236 S675 TORQUE SPLITS; GOVERNOR LAGS. WARRANTY REPAIR ACTION TAKEN: SENT FOR REPAIR. REPAIRED AND TESTED IAW MFG OHM FORM 15-1095A. 1G72 3U3 U H3EU E4CE 20040609000842004060900084EU 2004 6 9 MALA040405 120040519A5230HS523J019006 DOOR BAC 146 AVRO146RJ85A1500097EU LYC LF507 LF5071F NE CARGO BAY OPEN A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15529XJ E2363 LOWER DOOR NOT SHUT ILLUMINATED IN FLIGHT AT APPROX 9000 FT. STAYED ON FOR DURATION OF FLIGHT. AIR RETURN. MAINTENANCE REMOVED AND REPLACED REAR CARGO DOOR IAW AMM 52-31-21 201/202 ALL CHECKS GOOD. PN ON/OFF HS523J019-006 SN ON HAF/DH-0118 SN OFF HAF/DH-157. 2H74 4F4 FRTA49EU E6NE 20040609001162004060900116NM 2004 6 9 DL767040463 120040526A5720111T20053AND4 STIFFENER BOEING767 767232 1385132NM GE CF6 CF680 30025NE WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27112DL 22224 CRACKS WERE NOTED IN THE RADIUS OF THE RBL AND LBL 10 VERTICAL STIFFENERS OF THE CENTER SECTION FRONT SPAR. CRACKS WERE LOCATED APPROXIMATELY 5 INCHES FROM TOP OF STIFFENER. DAMAGE WAS REMOVED AND SPLICE INSTRUCTIONS PROVIDED VIA ERA 090218-14. 2L72 4F4 FRTA1NM E13NE 20040623000962004062300096 2004 6 23 GTIA040518 420040528A2565 CABLE DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE GIRT BAR MISROUTED A GTIAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 GL23830NK 49932 R1 DOOR EMERGENCY/SLIDE COVER CABLE TO GIRT BAR ROUTED IMPROPERLY. ROUTED GIRT BAR CABLE. 2L72 4F4 F A6WE E2EA 20040630000762004063000076EU 2004 6 30 USAA040321 120040608A5311D53111414202 FRAME AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE FUSELAGE CORRODED A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19709UW 0997 FRAME, 1.0 INCH X 5 INCHES X 0.71 INCH AREA, CORROSION; LEVEL 2; FR 21 AT Y254. INSTALLED NEW FRAME IAW SRM. INSTALLED NEW FRAME IAW SRM. 2L72 4F4 FRTA28NM E2GL 20040630001012004063000101NE 2004 6 30 ALG2004F00030 120040505A53127620123008122 BULKHEAD SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S1 60030NE FUSELAGE CRACKED E ALGAO OTHER O OTHER NRNOT REPORTED 1 SW0320509302 760545 20639TEC BULKHEAD CRACKED FROM RT HAND STIFFNER BL18 TO EDGE OF CUT OUT FOR BAGGAGE DOOR. CRACKS FORM RIVET HOLE TO EDGE. DOOR ASSEMBLY ALSO CRACKS AROUND UPPER ATTACHMENT RIVETS. 1G72 3U3 UNCH1NE E19EU 20040716000282004071600028SO 2004 7 16 SWIA200413497 120040530A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07284YV 120284 LEFT FRAME 13 FLOOR PROP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME 13 FLOOR PROP ON LEFT SIDE IAW SRM 53-10-10. 2L72 4T4 TRTA31SO E20NE 20040628001442004062800144NE 2004 6 28 010461 220040505A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 1 SURGES A UHLAA UNSCHED LANDING O OTHER CRCRUISE 1 GL17121CQ 121 FLT 4563 FROM PIT TO AVP, 10 MINUTES INTO THE FLIGHT, AIRCREW FELT NR 1 ENGINE SURGE. AIRCREW REDUCED POWER TO 25 PERCENT AND THE ENGINE STEADIED ITSELF. AIRCRAFT RETURNED TO THE GATE. 2L72 4T4 TRTA52EU E8NE6 20040712000462004071200046EU 2004 7 12 KBM2004F00114 120040321A6330704A33633075 SUSPENSION BAR SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE REAR MGB WORN E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19345SH4165 3345 SUSPENSION BAR, LT SIDE REAR MAIN GEARBOX SUPPORT BAR HAS EXCESSIVE BEARING PLAY. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20040816000282004081600028NM 2004 8 16 2004UALA00573 120040612A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 FUSELAGE FRAME AT STA 1420 STR 25L HAS THREE DENTS. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20040816001862004081600186NM 2004 8 16 2004UALA00613 120040624A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29560UA 26660 FLOORBEAM CAP AT BS 324, LBL 50 - LBL 72 CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH T-CAP SPLICE. 2L72 4F4 FRTA2NM E17NE 20040819000322004081900032SO 2004 8 19 RAIA00408001 120040801A801135059105 STARTER EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL NR 1 ENGINE INOPERATIVE A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03823HK16313 145475 LT ENGINE NO ROTATION AT START. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AIR TURBINE STARTER. 2L72 4T4 FRTT00011ATTE6CH 20040819000652004081900065WP 2004 8 19 2004F00237 120040814A7830 SLEEVE DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE THRUST REVERSER CRACKED A K NONE O OTHER ININSP/MAINT 1 SO25322FE 47908 NR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502. 2L73 4F4 FRTA22WE E23EA 20040722000472004072200047NM 2004 7 22 USAA040232 120040503A5311 FRAME BOEING737 737301 1384611NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19585US 23930 FRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004. 2L72 4F4 FRTA16WE E2GL 20040823001142004082300114SO 2004 8 23 LR7A04077 120040716A5230 SKIN LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 2665 4590 DURING SCHEDULED C-5 INSPECTION PER IAW CARD HC5321 FOUND CARGO DOOR EXTERIOR SKIN DENTED AT FS 900 - 930, WL 195 - 210, LBL 15 - RBL 15 AND FS 930 - 960, WL195 - 210, LBL 15 - RBL 15. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2132. 2H74 4T4 T A1SO E282 20040830000922004083000092EU 2004 8 30 AALA20040883 120040818A7120 MOUNT AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE RT ENGINE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW2170054 461 RT IB AFT ENGINE MOUNT BOLT COUNTER BORE CORRODED. CORROSION REMOVED AND COUNTER BORE TREATED, PRIMED, AND PAINTED IAW ESO 30595 DATED 8/18/04. (CLOSED) 2L72 4F4 FRTA35EU E13NE 20040831000332004083100033EU 2004 8 31 U30A200400008 120040711A2120 ODOR AIRBUS320 A320214 3930316EU GE CFM56 CFM56* 13802NE COCKPIT DETECTED A U30AD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA17261AV 1615 AFTER PUSH BACK, THE AFT F/A'S REPORTED AN (ELECTRICAL) BURNING ODOR. THE FLIGHT CREW WAS NOTIFIED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT IAW TSM 24-00-00-810-823 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA28NM E2GL 20040813001132004081300113NM 2004 8 13 2004UALA00654 120040711A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 CABIN FLOORBEAM CORRODED AT STA 324, RBL 62. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS CUT OUT ON THE UPPER T-CAP AND REPLACEMENT WAS FABBED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20040819000702004081900070WP 2004 8 19 ARWA20040602 120040619A7711JG29842 INDICATOR DOUG DC8 DC863F 302198FWP PWA JT3D JT3D3 52039NE EPR ERRATIC A ARWAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO19906R 46087 LOG PAGE NR 107344, AFTER ALL ENGINES SPOOLED AND TAKEOFF STARTED NR 1 EPR (ENGINE PRESSURE RATIO) ERRATIC; DISCONTINUED TAKEOFF AND TAXIED BACK TO RAMP. TRANSFERRED TO DMI NR 18568 IAW MM. AIRCRAFT RELEASED IAW MEL NR 77-1-2 CAT (A). REMOVED AND REPLACED NR 1 EPR INDICATOR; CHECKED SYSTEM ON GROUND, OK IAW MM 77-11-0 AND 71-00. CLEARED DMI NR 18568. 2L74 4F4 F 4A25 1E8 20040913002092004091300209SO 2004 9 13 C2XA04TY132 120040802A532014529495003 SUPPORT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FLOOR SILL CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FORWARD FLOOR SILL SUPPORT IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR SILL SUPPORT IAW SRM 51-40-02. 2L72 4F4 FRTT00011ATTE6CH 20040915000922004091500092NM 2004 9 15 MYW2004F00006 120040604A2410976J5981 GENERATOR BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 3 ENGINE FLUCTUATES A MYWAC ABORTED TAKEOFF HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SO19802MA 22433 DURING TAKE OFF ROLL, GENERATOR DROPPED OFF LINE FOLLOWED BY NR 3 GEN LIGHT. REJECTED TAKE OFF AT 75 KNOTS. ACCOMPLISHED AOM PROCEDURE GENERATOR CHECKLIST ZA9-1 AND REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. FOUND NR 3 GENERATOR FREQUENCY FLUCTUATING. TRANSFERRED TO DMI 6159 IAW MEL 24-1 PLACARDS INSTALLED AND DISCONNECTED NR 3 CSD. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED NR 3 GENERATOR AND CSD IAW MM. OPS CHECK AND LEAK CHECK GOOD ON ENGINE RUN. CLEARED DMI 6159. 2L73 4F4 F A3WE E2EA 20040923000402004092300040CE 2004 9 23 VDA2004F00000 120040625A2121 FAN BEECH 99 99A 1154003CE PWA PT6 PT6A28 EA VENT BLOWER FAILED E YDACO OTHER O OTHER NRNOT REPORTED 1 AL0399GH 701 300 U112 THE CENTRIFUGAL FAN ASSY CAME APART, SHED ALL THE BLADES. POSSIBLE THAT THE FAN WAS OUT OF BALANCE. POSSIBLE THAT THE FAN WAS THROWN OUT OF BALANCE BY INGESTION OF MATERIAL THROUGH THE AIR RETURN SYSTEM OF THE AIRCRAFT. INSPECTION OF THE VENT RETURN SYSTEM SCREEN ASSY. 1L72 3T4 T A14CE E4EA 20040922001912004092200191NE 2004 9 22 AWXA200400712 220040705A7200V2527A5 ENGINE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE NR 1 WORN A AWXAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP28642AW1706315372 584 V10576 ON TAKEOFF AT PHX EN ROUTE FOR OAK AT 1.05 EPR APPLICATION OF FLEX POWER NR 1 ENGINE EGT INDICATOR FLASHED AMBER AT APPROXIMATELY 610 DEGREES, REJECTED TAKEOFF AT 40 KNOTS. MAINTENANCE PERFORMED A HPC & HOT SECTION BORESCOPE INSPECTION IAW TSM 77-00-00-810-837 & T/C I5M72309. *S/D* DUE TO HIGH TIME AND OTHER MINOR ENGINE RELATED DISCREPANCIES REMOVED NR 1 ENGINE IAW T/C R5M71302. 2L72 4F4 FRTA28NM E40NE 20040923001232004092300123EU 2004 9 23 121271 120040826A7930 CHIP DETECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE MALFUNCTIONED A UHLAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1735SZ 35 187 DURING CLIMB THE LT ENGINE CHIP DETECTOR WARNING LIGHT ILLUMINATED FOR A FEW SECONDS THEN WENT OUT. THE CREW NOTIFIED MOC AND TURNED TO GO BACK TO IAD. ON 5 MILE FINAL THE LT CHIP DETECTOR LIGHT RE-ILLUMINATED AND WOULD NOT EXTINGUISH. THE CREW FOLLOWED THE QRH AND SHUT THE AFFECTED ENGINE DOWN. A/C TAKEN OUT OF SERVICE. IAD MAINTENANCE REMOVED AND REPLACED THE LT CHIP DETECTOR. GROUND RAN LT ENGINE, NO DEFECTS NOTED OPS CHECKS GOOD. A/C RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE6 20040922000592004092200059NE 2004 9 22 GTIA040676 220040718A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE NR 2 FAILED A GTIAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL23827NK 49793 725674 ENGINE FAILURE AT 29,000 FT WHEN POWER WAS REDUCED TO CRUISE. ALL PARAMETERS NORMAL ENGINE STARTED TO VIBRATE RT ENGINE OIL PRESS WENT TO 0 SHUT DOWN RT ENGINE RT OIL TEMP WENT TO 166 DEGREES AFTER SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. (M) 2L72 4F4 FRTA6WE E9NE 20041001000902004100100090NM 2004 10 1 04FDEA02812 120040923A5311 FRAME DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 TRANSVERSE FRAME AT LT STA Y= 1701 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-DTA. 2L73 4F4 FRTA22WE E31N3 20040920000292004092000029EU 2004 9 20 04FDEA02674 120040910A7603 THROTTLE AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE NR 2 OBSTRUCTED A FDEAC ABORTED TAKEOFF CRJF.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 SO25668FE 772 RTO DUE TO LOW POWER NR 2, ENG NR 2 THROTTLE WOULD NOT ADVANCE PAST REF. POINT 30 AND N1 ADVANCED TO 93 PERCENT VS 108 PERCENT REQUIRED. RTO OCCURRED AT 90 KTS. ENT BY: 273927 RPT BY: 096714 SHGN 11SEP04 02:40 GDL U IN WORK, ENT BY: 273927 RPT BY: 273927 FACT 11SEP04 03:37 GDL U FOUND DSUZ SCREW BLOCKING NR 2 THROTTLE MECHANISM. INSPECTED SAME AND NO DAMAGE FOUND ON IT. TESTED FADEC NO FAULTS IN MEMORY. REF. TSM 76-00-30 AND AMM 73-38-00-5-F. OK FOR SERVICE. ENT BY: 273927 RPT BY: 273927 2L72 4F4 FRTA35EU E13NE 20041001001062004100100106CE 2004 10 1 4122 120040926A2910605700311 LINE LEAR 60 60LEAR 5170707CE PWA 305 PW305 NE HYD RESERVOIR BLOWN E BSYAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL07560AN 138 PCE0111 AIRCRAFT IN ROUTE TO BTV FROM LNS SELECTED GEAR DOWN. DID NOT GET ALL THREE DOWN AND LOCK INDICATIONS, DIVERTED TO BDL BLEW GEAR DOWN AND LANDED NO PROBLEMS. MAINTENANCE FOUND HYD. LINE ON RT ENGINE PRESSURE LINE HAD BLOWN DEPLETING ALL FLUID FROM RESERVOIR. 2L72 4F4 FRTA10CE E35NE 20041001001122004100100112CE 2004 10 1 FTU2004F00006 120040722A213310357626 OUTFLOW VALVE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE CABIN PRESSURE BROKEN B FTURO OTHER O OTHER NRNOT REPORTED 1 NE05727C 5500485 AC WITH A PRESSURIZATION COMPLAINT. GROUND PRESSURIZATION DISCOVERED A LARGE FLOW OF AIR UNDER THE REAR CABIN FLOOR IN THE AREA OF THE OUTFLOW VALVES. FURTHER INVESTIGATION FOUND THE SUPPORT VANES FOR THE NOISE SUPPRESSORS WERE BROKEN CAUSING THE OUTFLOW VALVE TO COCK AND JAM DURING OPERATION NOT ALLOWING THE VALVE TO CLOSE COMPLETELY. CLOSE INSPECTION OF THE 3 SUPPORT VANES IS VERY IMPORTANT. THIS VALVE HAS BEEN IN THIS AC SINCE DAY ONE(20 YEARS). CLOSE INSPECTION OF THE OTHER VALVE WAS COMPLIED WITH, NO DEFECTS FOUND. NEW OUTFLOW VALVE INSTALLED, OPS CHECKED GOOD. (NE05200408329) 1L72 4F4 F A22CE E1NE 20041013000112004101300011NM 2004 10 13 2004UALA00877 120040917A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSLEAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29566UA 26670 CABIN FLOORBEAM CAP IS CORRODED AT BS 365 FROM RBL 28 TO RBL 42. TYPICAL CORROSION FOUND ON EXISTING STRAP REPAIR. STRAP REPAIR WAS REMOVED, CORROSION CLEANED, AND STRAP REPAIR REPLACED. 2L72 4F4 FRTA2NM E17NE 20041018000322004101800032WP 2004 10 18 ASMF200410001 120041004A5523 TAB DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ELEVATOR LIGHTNING STRIKEW ASMFO OTHER O OTHER NRNOT REPORTED 1 SW23216AM 49586 DURING TRANSIT CHECK, CAPTAIN REPORTED LIGHTNING STRIKE. THE FOLLOWING NON ROUTINE CARDS WERE GENERATED AND ATTENDED TO CORRECT DAMAGES. RT ELEVATOR GEAR TAB T/E IN 5 SMALL POINTS. RT ELEVATOR ANTI-FLOAT TAB T/E. TWO FASTENERS MELTED FUSELAGE SKIN IN JOINT WITH TAIL CONE LOCATED AT 5:30 HOURS POSITION AND MISSING MATERIAL IN FUSELAGE SKIN EDGE AT SAME PLACE. FASTENERS WERE REPLACED AND FUSELAGE SKIN WAS REPAIRED, ALL CORRECT. MISSING MATERIAL IN 4 INCHES OF DIAMETER IN TAIL CONE SURFACE LOCATED AT 5 HOURS POSITION IN RT SIDE. DAMAGED PAINT WAS REMOVED AND NO DAMAGES WERE DETECTED, AFFECTED AREA WAS REPAINTED. LT ELEVATOR CONTROL TAB T/E. NO STRUCTURAL DAMAGES WERE DETECTED. 2L72 4F4 FRTA6WE E9NE 20041020000072004102000007NM 2004 10 20 ASAA0410378 120040819A5310654655721 SHEAR TIE BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 FOUND CORROSION ON SHEAR TIE AROUND LOWER FASTENER. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM. (M) 2L72 4F4 FRTA16WE E2EA 20041021000642004102100064EA 2004 10 21 VNAA0410004 120041007A2720600902027 PIVOT ASSY CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE LT RUDDER PEDAL FAILED A VNAAO OTHER O OTHER NRNOT REPORTED 1 GL05213PS1566 7879 CREW REPORTED THAT RUDDER PEDALS ARE MAKING A CLICKING SOUND. AIRCRAFT WAS FERRIED TO DAYTON. MAINTENANCE INSPECTED AND FOUND LEFT HAND PIVOT ASSEMBLY CAUSING SOUND. MAINTENANCE REPLACED THE PIVOT ASSEMBLY IN ACCORDANCE WITH THE BOMBARDIER MANTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041101000812004110100081NM 2004 11 1 2004UALA00917 120041006A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29568UA 26674 AFT PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT AREA OF DAMAGE. FABRICATED AND INSTALLED NEW SPLICE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041103000992004110300099NM 2004 11 3 P5CA0401254 120041018A5313 STRINGER BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FUSELAGE STRINGER 9R HAS CRACKS AT BODY STATIONS 1372 AND 1394. REMOVED SHEAR TIE CLIPS, REMOVED STRINGER 11R FOR ACCESS, REMOVED STRINGER INSTALLATION AND INSTALLED NEW STRINGER IAW SRM 51-30-02 , REMOVE STRINGERS AND SHEAR TIE CLIPS. 2L74 4F4 F A20WE E20EA 20041115001012004111500101NM 2004 11 15 2004UALA00996 120041029A2597 WIRE HARNESS AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE ESCAPE SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29805UA 783 SLIDE LIGHTS ARE BLOWN. RESISTANCE TEST DOES NOT PASS. RESERVOIR VALVE ASSEMBLY FRAYED. SUPPLEMENTAL DATA UPDATE SHOP FINDINGS REVEALED THAT ELECTRICAL HARNESS AND LAMPS WERE FOUND DAMAGED HENCE THE TEST OF THE UNIT WHILE INSTALLED ON THE AIRCRAFT FAILED. BUSTED BULBS ARE PERHAPS ATTRIBUTED TO AGE, WHILE HARNESS AND VALVE FRAYING ARE ATTRIBUTED TO IN-SERVICE ENVIRONMENTAL CAUSES SUCH AS VIBRATION. REPLACED ELECTRICAL HARNESS, LAMPS, AND ALSO THE RESERVOIR VALVE ASSEMBLY. 2L72 4F4 FRTA28NM E40NE 20041119000392004111900039 2004 11 19 KBM2004F00220 420040905A3422103002201 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL FAILED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19115SH3236 3141 WILL NOT HOLDING HEADING. REMOVED AND REPLACED DIRECTIONAL GYRO. 1G71 3U3 U H9EU E19EU 20041027000352004102700035 2004 10 27 UPS04143325 420041007A2565 LIGHT AIRBUSA300 A300F4622R 3930360EU PWA 4158 PW4158 NE EVAC SLIDE INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01126UP 0810 DURING PREFLIGHT TEST OF EMERGENCY EVACUATION SLIDE, THE AURAL SOUND WORKS BUT THE LIGHT DOES NOT ILLUMINATE. RESET ASPSU IAW MM 52-73-18-4. DEFERRAL CLEARED. 2L72 4F4 FRTA35EU E24NE 20041028000272004102800027EA 2004 10 28 ASOA04478 120040701A2741601R517063 TRIM PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STAB STUCK A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27901EV 7616 DURING TAKEOFF, AT APPROXIMATELY 800 FEET THE STAB TRIM AND MACH TRIM DISENGAGED AND THE CREW RE-ENGAGED THEM. WHILE CLIMBING THROUGH 14,00 FEET WITH THE AUTOPILOT ON, STAB TRIM AND MACH TRIM MESSAGES APPEARED AND THEY DISENGAGED AGAIN. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY THE TOWER. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY WITH THE FLAPS SELECTED AT 45 DEGREES. MAINTENANCE FOUND THE STAB TRIM PANEL CHANNEL 1 BUTTON STUCK PARTIALLY IN AND REMOVED AND REPLACED THE STAB TRIM PANEL. SYSTEM BITE TEST AND OPS CHECK WERE PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041101000412004110100041NM 2004 11 1 2004UALA00801 120040807A5315 FLOOR SUPPORT BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29564UA 26666 CABIN STATION 365, CL TO RBL 15 FLOOR SUPPORT HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP AND L-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041103000242004110300024SO 2004 11 3 LR7A04122 120041001A5311 FRAME LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03401LC 2585 4606 DURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5315 FOUND FS 1023 FRAME CRACKED AT WL 140, LBL 63. REPAIRED IAW SRM SMP 583 51-140-22. NR 0483. 2H74 4T4 T A1SO E282 20041103000282004110300028NM 2004 11 3 XNOA1205 120041027A2780 SWITCH BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE LE FLAPS DAMAGED A XN0AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL2376753 21249 NR 6 LED FAILED TO RETRACT AFTER T/O. FOUND PUSHED PIN AT NR 6 LED FLAP POS SWITCH. RESEATED PIN IAW MM CH. 20-11-07. OPS CHECKS GOOD IAW MM CH. 27-82-11. 2L73 4F4 F A3WE E2EA 20041122000822004112200082 2004 11 22 2004UALA01033 420041108A2565 SLIDE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 WILL NOT TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29556UA 26650 EMERGENCY ESCAPE SLIDE 2 WILL NOT TEST. CYLINDER ASSEMBLY TEMPERATURE COMPENSATED PRESSURE SWITCH (TCPS) WAS DETERMINED TO HAVE BEEN DAMAGED DUE TO HANDLING. 2L72 4F4 FRTA2NM E17NE 20041129000182004112900018NM 2004 11 29 UIEA200400192 120041115A541465B8904938 SKIN BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15512MC 21220 DURING SCHEDULED MAINTENANCE INSPECTION, THE BULKHEAD UPPER ASSY FORWARD ANGLE FRAME OF THE NR 2 PYLON LT AND RT SIDE WERE FOUND CRACKED. FABRICATED AND INSTALLED REPAIR ANGLES ON THE FORWARD AND AFT FRAMES IN THE REPAIR AREA. INSTALLED THE REPAIR ANGLES BY PICKING-UP ALL EXISTING FASTENER LOCATIONS AFFECTED BY THE REPAIR PARTS WITH LOCK FASTENERS. CONDUCT REPEAT DETAILED VISUAL INSPECTION OF THE FORWARD FRAMES AT THE REPAIRS AND ADJACENT CHORD AREA EVERY C-CHECK OR 18 MONTHS WHICHEVER IS FIRST, FOR CRACK, LOOSE FASTENERS AND DAMAGE. EO TO BE ISSUED TO ACCOMPLISH INSPECTION AT 18 MONTH INTERVALS OR C-CHECK WHICH EVER IS FIRST. 2L74 4F4 F A20WE E23EA 20041129000842004112900084NM 2004 11 29 USAA040785 120041002A5347 SEAT TRACK BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19383US 22956 PIT - Q5, SEAT TRACK, 2 INCH BY 4 INCH CORRODED AREA, LEVEL 1 TASK NR C53-107-02, AFT END OF RT OB SEAT TRACK, STA 947. MANUFACTURED FILLERS AND SPLICED IN A NEW SECTION IAW SRM 53-00-52. 2L72 4F4 FRTA16WE E2GL 20041129001582004112900158EA 2004 11 29 ASOA04776 120041003A3350110049 CHARGER CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27902EV161462102 7620 DURING A GROUND INSPECTION, THE MID CABIN OVERHEAD EMERGENCY EXIT SIGN AND THE FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY CHARGER FOR THE MID CABIN. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20041129001952004112900195NM 2004 11 29 USAA040704 120040903A5320 ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19514AU 23700 ANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03. 2L72 4F4 FRTA16WE E21EU 20041203000012004120300001WP 2004 12 3 ASAA0480522 120040928A575359121688 VANE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE RT OB FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02973AS 53449 OKC - C-CHECK, RT OB FLAP VANE IB END LOWER SKIN HAS NUMEROUS SMALL DENTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-70-2. 2L72 4F4 FRTA6WE E9NE 20041207000282004120700028NM 2004 12 7 USAA040834 120041008A5330 SKIN BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19394US52571 23316 SKIN, 1 INCH CRACK, BS 727D, STR 22R. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01. 2L72 4F4 FRTA16WE E2GL 20041207000542004120700054NM 2004 12 7 USAA040881 120041018A534065B57839430 ANCHOR FITTING BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 INCHES BY 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, RT LAV FLOOR STA 1016. 2L72 4F4 FRTA16WE E2GL 20041210000452004121000045SO 2004 12 10 B7T2004F00000 220040823A731064999413 HOSE CESSNA207 207 2073602CE CONT O520 IO520F 17032SO HARTZLHCC3Y HCC3YF1 GL NR 5 CYLINDER LEAKING E B7TAA UNSCHED LANDING KRJFLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AL031673U475 20700273 814751R EC1582A AIRCRAFT ON CLIMB-OUT, AT 200 FT AGL ENGINE SURGED AS IF IT WAS NOT RECEIVING ENOUGH FUEL. PILOT SWITCHED FUEL TANKS (FROM RT TANK TO LT TANK) AND FUEL BOOST PUMP WAS TURNED ON AND ENGINE SMOOTH OUT FUEL BOOST WAS TURNED OFF AND IN APPROXIMATELY 10 SECONDS LATER ENGINE SURGED AGAIN AT THAT TIME BOOST PUMP WAS TURNED BACK ON AND ENGINE SMOOTHED OUT AND PILOT RETURNED, WHERE AIRCRAFT WAS LANDED WITHOUT INCIDENT. 1H71 3O3 O A16CE E5CE 5 CP25EA 20041215000432004121500043EU 2004 12 15 ASOA04849 120041029A33503012000 POWER SUPPLY AEROSPATR72 ATR72 EU PWA PW120 PW127 NE EMERGENCY LIGHT INOPERATIVE A ASOAK NONE O OTHER ININSP/MAINT 1 SO27640AS 405 DURING A GROUND INSPECTION, NUMEROUS EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT 73WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRT E20NE 20041201000392004120100039NM 2004 12 1 2004UALA01114 120041114A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29571UA 26681 FRAME AT BS 1400 STR 26L IS DAMAGED. CARGO PIT FRAME DAMAGE DUE TO CARGO HANDLING. FRAME SECTION REPLACED. 2L72 4F4 FRTA2NM E17NE 20041221000332004122100033NM 2004 12 21 ASA0440212 120041029A53116546550 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FRAME IS CRACKED AT LT OVERHEAD BIN RAIL SUPPORT BRACKET. REPAIRED CRACKED FRAME IAW EA. 2L72 4F4 FRTA16WE E21EU 20050110001702005011000170NM 2005 1 10 USAA041035 120041111A552265C25746154A SKIN BOEING737 737301 1384611NM GE CFM56 CFM563B1 13802NE RT ELEVATOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19352US45768 23555 PIT - Q4 - LOWER SKIN, COMPOSIT DAMAGE .3750 INCH GOUGING. COMPOSITE DAMAGE - SINGLE LAYER RT ELEVATOR AT STA 68 + 6 INCHES FROM FWD SPAR LOWER SKIN. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA. 2L72 4F4 FRTA16WE E2GL 20050105000052005010500005NE 2005 1 5 DL76L041133 220041223A7321 EEC BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE INOPERATIVE A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO27198DN48235 724692 28455 724692 RIGHT ENGINE EEC INOP LEFT EEC TURNED OFF PER PROCEDURE. REPLACED RIGHT ENGINE EEC PER MM, OPS CHECK OK. 2L72 4F4 FRTA1NM E24NE 20050113000452005011300045NM 2005 1 13 2004UALA01149 120041121A2613355574255 OVERHEAT LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE FAILED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29308UA 23669 DIVERTED TO PIT DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY . 2L72 4F4 FRTA16WE E2GL 20050215000942005021500094NM 2005 2 15 C7WA200400059 120041011A5511 STRUCTURE BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE HORIZONTAL STAB DAMAGED A C7WAO OTHER O OTHER NRNOT REPORTED 1 SO177635U 19908 RT HORIZONTAL STABILIZER BALANCE PANELS NR 2, NR 3, AND NR 4 CAVITIES T/E LOWER BEAM RUB BLOCKS ADJUSTMENT SCREW SAFETY WIRE HOLES CRACKED. INSTALLED SPLICE REPAIR ON RT HORIZONTAL STABILIZER T/E BEAM BALANCE PANELS CAVITIES NR 2, NR 3, AND NR 4. DAMAGED CHORD SECTION REMOVE. REPAIR ACCOMPLISHED IAW SRM. 2L73 4F4 F A3WE E2EA 20050302000452005030200045NM 2005 3 2 ASA0440393 120041230A53306545778103 SKIN BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - FUSELAGE EXTERNAL LONGITUDINAL LAP REPAIR AT STA 927, STR 20R NOT IAW SRM, ENGINEERING INSTRUCTIONS REQUIRED. REPAIRED IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050308002142005030800214NE 2005 3 8 ALG2005F00004 120041215A29137665009808102 PUMP SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL HYDRAULIC SYS INOPERATIVE E ALGAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW03522AL 760236 ON OPS CHECK FLIGHT FOR HYDRAULIC MODULE CHANGE AND GEAR RETRACTION CHECK, GEAR WILL NOT RETRACT RED UNSAFE LIGHT STAYS ON. MAINTENANCE REMOVED HYDRAULIC PUMP SN 195835 AND INSTALLED SERVICEABLE PUMP SN 19747. OPS/LEAK CHECK WAS GOOD ADJUSTED WEIGHT O WHEELS SWITCH, OPS CHECK WAS GOOD. (K) 1G72 3U3 U H1NE E1GL 20050321002392005032100239NE 2005 3 21 ASOA04778S 220041006A7230 COMPRESSOR CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 NE RT ENGINE DAMAGED A ASOAA UNSCHED LANDING CRAF.O.D. PARTIAL RPM/PWR LOSS FLAME/FIRE TOTAKEOFF 1 SO27722EV4965 1515 10127 DURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN A/C ACCOMPANIED BY A COMPRESSOR STALL ON RT ENGINE ALONG WITH TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL, NO FIRE INDICATIONS PRESENT. EMERGENCY WAS DECLARED AND A/C RETURNED, LANDING SAFELY WITH FLAPS SELECTED AT 20 DEGREES. MAINT FOUND FOD DAMAGE TO RT ENG COMPRESSOR STAGES 1-5. REMOVED AND REPLACED RT ENGINE. TEARDOWN REPORT CONCLUDED THAT FOREIGN OBJECT WAS INJECTED INTO RT ENG. OBJECT WAS IDENTIFIED AS LOW ALLOY STEEL NOT COMMON FOR ENGINE AIRFLOW MATERIAL , RESULTING IN DAMAGES TO FAN BLADES, COMPRESSOR ROTOR, STATOR, COMBUSTION CHAMBER, HIGH AND LOW PRESS TURBINE SECTIONS. 2L72 4F4 FRTA21EA EOOO63EN 20050330000232005033000023SO 2005 3 30 CYQ2005F00000 120040618A3210 LANDING GEAR PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2A GL RIGHT COLLAPSED E CYQAO OTHER O OTHER TXTAXI/GRND HDL 1 CE0135531 318052046 L118668A DJ9051A WHILE BACKTAXING ON RUNWAY, RT GEAR COLLAPSED. DON`T KNOW THE CAUSE. TO PREVENT RECURRENCE, NEVER TOUCH GEAR LEVER WHEN ON THE GROUND. (CE09200403958) (K) 1L72 3O3 O A20SO E14EA 5 CP33EA 20050406001752005040600175NM 2005 4 6 ASA044405 120041231A531565C3394423 FLOORBEAM BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 PAE - CORROSION ON FLOORBEAM, STA 360. REPAIRED FLOORBEAM IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050414000602005041400060EU 2005 4 14 BAQA2004628 120040628A5100DMN481 ANTENNA AGUSTAA109 A109E 0260119EU TMECA ARRIUSARRIUS2K1 NE TAILBOOM DAMAGED E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA037YL 11502 OVER THE PAST 24 MONTHS THIS AIRCRAFT HAS HAD 4 SETS OF NAV ANTENNAS INSTALLED. FAILURE MODE OF ANTENNA IS (RT ELEMENT BECOMES EXTREMELY WEAK) WHICH CAUSES NAV INDICATOR DISPLAY ERRORS OF UP TO 5 DEGREES, VISUAL INSPECTION INDICATES THAT RT NAVE ANTENNA ELEMENT IS EXPOSED TO A MUCH HIGHER TEMPERATURE THEN LT ELEMENT. RECENT FLIGHT PERFORMED WITH TEMPERATURE (IN FLIGHT) IN EXCESS OF 199 DEGREES F, THE DESIGN LIMIT FOR THIS ANTENNA IS 185 DEGREES F, IAW MFG. RECOMMENDATIONS INCLUDE USING AN ANTENNA SUITABLE FOR HIGH TEMPERATURE EXPOSURE OR RELOCATING ANTENNAS TO FUSELAGE, AWAY FROM EXHAUST. 1G72 3U3 URTH7EU E34NE 20050623001402005062300140NM 2005 6 23 72300199 120041118A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE FUSELAGE CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 2 X 1 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20040324000722004032400072 2004 3 24 SWAA040818 420040317A2565D31354 SLIDE BOEING737 7375H4 138449DNM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29519SW 25318 R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040601000562004060100056WP 2004 6 1 04FDEA01471 120040526A5753ARC1455 SUPPORT DOUG DC10 DC1010 3022110WP FLAP VANE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568056 47810 COMPLY WITH EA 8-5750-77428, WINGS - ARC1455 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77428. 2L73 4F A22WE 20040419001882004041900188NM 2004 4 19 SWAA041019 120040408A57536546435 SKIN BOEING737 737301 1384611NM RT WING TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED RON, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED RT WING OUTBOARD T/E AFT FLAP PER SRM. 2L72 4F RTA16WE 20040420000392004042000039NM 2004 4 20 04FDEA00912 120040412A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 RIGHT I/B FLAP, O/B HINGE PIVOT BORE AREA FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76659. TRAILING EDGE FLAPS RIGHT INBOARD FLAP FORWARD HINGE BRACKET (WING SIDE) CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040602000752004060200075NM 2004 6 2 04FDEA01358 120040520A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 RT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE FOUND CORRODED. RT WING I/B FLAP O/B HINGE (FLAP SIDE), I/B PIVOT PIN ATTACHMENT BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGE 446. ORIGINAL DIAMETER: 1.187, FINAL DIAMETER: 1.217, MAX ALLOWABLE DIAMETER: 1.220. WITHIN LIMIT AS PER CMM 57-52-03 PAGE 446. REPAIRED AS PER EA 1-5750-76679. TRAILING EDGE FLAPS RT INBOARD FLAP OUTBOARD SUPPORT BRACKET. CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20040721000832004072100083NM 2004 7 21 04FDEA02078 120040714A551065245712 BEAM BOEING727 727100 1384036NM HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25185FE 18871 CORROSION ON RT HORIZONTAL STAB UPPER T/E BEAM UPPER SURFACE, ABOVE NR 7 HINGE. REMOVED AND REPLACED RT HORIZONTAL STAB UPR T/E BEAM IAW SRM 51-10-2, 51-30-2, 51- 30-5, 51-30-8 AND SOPM 20-50-01 AND EA 7-5510-72372. 2L73 4F RTA3WE 20050103001422005010300142WP 2005 1 3 04FDEA03474 120041219A5320AEA00245 INTERCOSTAL DOUG DC10 DC1030 3023501WP LT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25309FE 48298 CORROSION FOUND ON INTERCOSTAL IN LEFT WHEEL WELL AT AFT BULKHEAD. REMOVED AND REPLACED INTERCOSTAL. 2L73 4F A22WE 20040811000202004081100020SO 2004 8 11 C2XA04IA085 120040701A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2712564 145618 CLE - FLIGHT 2846, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD AISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IN ACCORDANCE WITH EMB-145 AMM 33-50-12, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20041025000452004102500045EA 2004 10 25 SWIA200413651 120040725A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07936SW 7726 FS 621 FLOOR SUPPORT ANGLE RIGHT HAND SIDE CRACKED. ITEM FOUND AT C-CHECK. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV-B. 2L72 4F RTA21EA 20040506001052004050600105NM 2004 5 6 CALA0400452 120040502A5320BAC1496377 CHANNEL BOEING737 737824 13844BZNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2727239 28951 INSPECTION FOUND LEFT Z-CHANNEL IN AFT CARGO AREA CORRODED AT STA 727+4 TO 847. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040820000272004082000027NM 2004 8 20 AWXA200400786 120040716A3350BR964411 LIGHT BOEING757 7572S7 1384962NM SEAT ROW 21 LT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 DFW - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA2NM 20040827000242004082700024NM 2004 8 27 SWAA042456 120040825A52306547952 SEAL BOEING737 7373H4 1384600NM AFT CARGO DOOR TORN A SWAABA EMER. DESCENT UNSCHED LANDING O OTHER CRCRUISE 1 SW29357SW 26594 DECLARED EMERGENCY/DIVERSION. AT FL370 ALTITUDE WARNING HORN CAME ON. CABIN ALTITUDE WAS 9500 FT. WENT TO STANDBY ON PRESSURE CONTROLLER, NO HELP. WENT TO MANUAL AND STARTED AN EMERGENCY DESCENT, CABIN GOT TO 11500 FT. NO WARNING LIGHTS. REMOVED AND REPLACED AFT CARGO DOOR SEAL, PER MM. 2L72 4F RTA16WE 20041115002042004111500204NM 2004 11 15 04FDEA02633 120040903A5753ARC4125501 FITTING DOUG MD11 MD11F 3023600NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25615FE 48767 LT WING O/B FLAP STOP FITTING FOUND CRACKED. LEFT WING O/B FLAP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. 2L73 4F RTA22WE 20040202000862004020200086NM 2004 2 2 04FDEA00154 120040115A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25604FE 48460 LEFT OUTBOARD FLAP INBOARD HINGE (WING MOUNTED), OUTBOARD ACTUATOR LUG HOLE CORRODED AT BORE. COMPLIED WITH FEDEX EA 1-5740-74285, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20040519000452004051900045NM 2004 5 19 C8GA20040003 120040330A2910 B-NUT BOEING727 727227 1384078NM HYD LINE LOOSE A C8GAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO1589427 21365 FLT 1724 FROM KROC TO KPHL. ON APPROACH TO KPHL OBSERVED A COMPLETE LOSS OF B-SYSTEM HYDRAULIC FLUID. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL A-05-3, ADVISED ATC AND DECLARED EMERGENCY AS A PRECAUTIONARY. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND A B-NUT LOOSE ON RIGID RETURN LINE TO ELEVATOR FEEL CONTROL UNIT. TIGHTENED AND SECURED “B” NUT IAW B727 MM 20-10-5, SERVICED HYDRAULIC SYSTEM TO FULL AND NO LEAKS WERE NOTED DURING SYSTEM CHECKS. AIRCRAFT RETURNED TO SERVICE 2L73 4F A3WE 20040805001772004080500177NM 2004 8 5 ASAA0410332 120040709A532065458953 SPLICE BOEING737 737298C 1384490NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS 20794 PAE - FOUND STRINGER 26L SPLICE CAP AT BS 908 HAS OVERSIZED HOLES. REMOVED AND REPLACED STRINER 26L SPLICE CAP. (M) 2L72 4F RTA16WE 20040421001302004042100130NM 2004 4 21 04FDEA00957 120040414A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 LEFT WING O/B FLAP O/B HINGE ACTUATOR LUG O/B HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-76015. WING TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBD FLAP. OUTBOARD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040319001762004031900176NM 2004 3 19 SWAA040728 120040307A53116516301 FRAME BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29674AA 23252 DURING SCHEDULED D CHECK, FOUND BS 188 FRAME CRACKED AT WL 208, RT SIDE. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040820001292004082000129NM 2004 8 20 04FDEA01698 120040612A5744ARC0503 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.256 INCH. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5740-76741, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION. 2L73 4F RTA22WE 20041201001802004120100180NM 2004 12 1 AALA20041147 120041120A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21692AA 26972 SJU - DURING OVERNIGHT CHECK FOUND EMERGENCY FLOOR LIGHTING SYSTEM AT ROWS 15 TO 25 INOPERATIVE. FOUND BROKEN CONNECTOR AT ROW 16. REPAIRED BROKEN CONNECTOR AT ROW 16 FOR EMERGENCY FLOOR LIGHTING AT ROWS 15 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040928001082004092800108EA 2004 9 28 SWIA200413740 120040612A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07403SW AREAS OF CORROSION BELOW LEFTHAND EMERGENCY EXIT ON SIDE SEAT RAIL. ITEM FOUND AT C-CHECK INSPECTION. REMOVED SIDE SEAT RAIL AND INSTALLED NEW SEAT RAIL SECTION IAW REO 601R-53-00-055. 2L72 4F RTA21EA 20040308001082004030800108NM 2004 3 8 04FDEA00508 120040223A5744 HINGE DOUG MD11 MD11 3023602NM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25586FE 48487 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE FOUND CORRODED. RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AS PER CMM 57-44-09 AND FOUND WITHIN LIMITS AS PER DWG ARC 0503, SHT 2. COMPLIED AS PER EA 1-5740-74324, WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION 2L73 4F RTA22WE 20040206001832004020600183NM 2004 2 6 2004UALA00045 120040120A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29593UA 28144 THERE ARE TWO SMOOTH DENTS FWD OF DOOR 2L ON AN EXISTING PATCH. EACH DENT IS APPROX 2 INCHES WIDE BY .125 INCHES DEEP. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING DOUBLER WITH DOUBLER-TRIPLER. 2L72 4F4 FRTA2NM E17NE 20040224001292004022400129EU 2004 2 24 AALA20040221 120040211A2821 FILTER AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE ZONE 600 CLOGGED A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2114056 463 695400 JFK INFLIGHT T837/11 AT FLIGHT LEVEL 270 NUMBER 2 ENGINE FUEL CLOG LIGHT CAME ON WITH ECAM MESSAGE. REDUCED POWER TWO TO THREE KNOBS AND LIGHT WENT OUT. RETURNED TO STATION AND LANDED WITHOUT INCIDENT. FOUND FUEL FILTER CLOGGED. REPLACED FUEL FILTER AND AFTER RUN-UP ACCOMPLISHED SPECIAL ITEMS CARD 4925 WITH NO DEBRIS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA35EU E13NE 20040225001492004022500149NM 2004 2 25 2004UALA00116 120040210A5310 DOOR FRAME BOEING747 747451 1384940NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29105UA 26473 LEFT NR 5 MED, FWD FRAME INBOARD WEB IS CRACKED AT LOWER DOOR HINGE AREA. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED DOUBLER REPAIR. 2L74 4F4 FRTA20WE E24NE 20040303000762004030300076NM 2004 3 3 P5CA0401040 120040217A302013J55200 CLAMP BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE NR 2 ENG FAILED A P5CABJA EMER. DESCENT DUMP FUEL UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP23921FT 21575 689184 WHILE IN CLIMB FL 29-30 NR 2 ENG FIRE WARNING ON HANDLE AND BOTH FIRE LOOPS CAME ON. ENG SHUT DOWN AND A/C DIVERTED TO NRT. REMOVED AND REPLACED NOSE COWL ANTI-ICE CLAMP. LEAK CK OK IAW MM 30-21-00. 2L74 4F4 F A20WE E3NE 20040304000772004030400077CE 2004 3 4 XGN2004F00002 120040122A3260 SAFETY SWITCH CESSNA402 402B 207590PCE CONT O520 TSIO520* 17040SO NLG INOPERATIVE E XGNAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW054165G 402B1212 NOSE GEAR LIGHT WOULD NOT ILLUMINATE AND THE GEAR WARNING HORN WAS GOING OFF ON APPROACH. PILOT DID A FLY BY THE TOWER TO VERIFY NOSE GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENCES AND NOSE GEAR LIGHT ILLUMINATED AFTER TOUCH DOWN AND GEAR WARNING HORN ALSO SHUT OFF. NOT KNOWING HOW MANY HOURS ARE ON THE SAFETY SWITCH. I WOULD ASSUME THE SWITCH WAS WORN OUT.(SW05200404536/ SW05200404537) 1L72 3O3 O A7CE E8CE 20040301001132004030100113EA 2004 3 1 DFZ2004F00000 220040115A7320 SPLINE ADAPTER BEECH 200 200BEECH 1152920CE PWA PT6 PT6* 52043EA FCU BROKEN E DFZAO OTHER O OTHER NRNOT REPORTED 1 EA095LE A45429 BB195 PCE80563 RT ENGINE WENT TO FULL POWER IN THE AIR. INSPECTED, FOUND COUPLING SPLINE (PLASTIC) BETWEEN FCU AND FUEL PUMP, BROKEN. REMOVED AND INSTALLED OH FCU AND FUEL PUMP. 1L72 4T3 T A24CE E2NE 20040303000272004030300027WP 2004 3 3 MWEA040016 120040216A3260 WARNING LIGHT DOUG DC9 DC981 3022081WP PWA JT8 JT8D* NE NLG ILLUMINATED A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31803ME 48029 GEAR RETRACTION WITH GEAR HANDLE UP, THE NOSE GEAR RED UNSAFE LIGHT REMAINED ON. INSPECTED NOSE LANDING GEAR, GEAR EXTENSION/RETRACTION PERFORMED, INSPECTED PISTON AND ASSOCIATED PARTS, AND COMPLIED WITH TASK CARD 10819 FOR NOSE LANDING GEAR REPACK. NO DEFECTS WERE FOUND. 2L72 4F4 F A6WE E2EA 20040304000532004030400053CE 2004 3 4 AKG2004F00003 120040210A531210144009811 BULKHEAD BEECH 200 B200 1152922CE PWA PT6 PT6A60A 52043NE FUSELAGE DAMAGED B AKGRO OTHER O OTHER NRNOT REPORTED 1 CE05447AC7715 BB1042 IN COMPLETING AD, NOT ONLY WAS SCORING FOUND ACROSS THE MID SPAN, BUT ALSO ALL THE WAY AROUND WHERE THE (U) FRAME LAYS ON TOP OF THE BULKHEAD WEB. THERE IS NOT A PATCH REPAIR FOR THIS. THE BULKHEAD WEB WILL HAVE TO BE REPLACED. 1L72 4T4 T A24CE E4EA 20040319001942004031900194NM 2004 3 19 VNAA0402010 120040227A3260 SENSOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE HARTZLHDE6C HDE6C3B NE MLG CONTAMINATED A VNAAO OTHER P NO WARNING INDICATION CLCLIMB 1 GL07440JS 3058 AFTER TAKEOFF, THE CREW REPORTED NOT GETTING A GEAR UP AND LOCKED INDICATION AND DIVERTED TO DAY. MAINTENANCE INSPECTED AND FOUND 4 PIECES OF ICE IN THE WHEEL WELL AND REMOVED IT. MAINTENANCE THEN PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T4 TRTA45NM E20NE 6 CP34NE 20040325001122004032500112EU 2004 3 25 BAQA093305 120040223A7714430106202 PICKUP UROCOPEC135 EC135P2 5620027EU PWA PW206 PW206B 0 NE ENGINE INOPERATIVE B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03603ME178 0284 NRO WILL NOT READ ON GAGE, NO SIGNAL. REPLACED WITH SERVICABLE UNIT. 03/01/2004 1G72 3U3 U H88EU E42NE 20040329001662004032900166NM 2004 3 29 2004UALA00220 120040309A5314 KEELBEAM BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29603UA 21864 KEELBEAM AT BS 800.81 AND RBL 9.5, HAS AREA OF CORROSION AND EXFOLIATION ON LOWER SURFACE AT PANEL ATTACH HOLE. MAJOR REPAIR ACCOMPLISHED. REPAIRED KEELBEAM FLANGE WITH RETAINER. 2L72 4F4 FRTA1NM E3NE 20040330000592004033000059NM 2004 3 30 2004UALA00181 120040301A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29397UA 24672 CABIN OVERWING FRAME STA 616R HAS A CRACK ON I/B LOWER FASTENER BELOW FLOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE. 2L72 4F4 FRTA16WE E2GL 20040415000352004041500035EU 2004 4 15 2004UALA00265 120040321A5270 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE EMERGENCY EXIT OUT OF ADJUST A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29447UA 836 LEFT FWD OVERWING EXIT SHOWED OPEN ON ECAM. FLIGHT DIVERTED. THE SUBJECT DOOR'S PROXIMITY SWITCH WAS ADJUSTED. 2L72 4F4 FRTA28NM E40NE 20040422001462004042200146SW 2004 4 22 ULX2004F00007 120040310A3340017601 HOUSING BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL SPOTLIGHT CRACKED B ULXRO OTHER O OTHER NRNOT REPORTED 1 WP01212LA188 3957 CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONTROL OF WELDING PROCESS. 1G71 3U3 U H2SW E4CE 20040423000262004042300026WP 2004 4 23 GTIA040159 120040222A3397 TERMINAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE EMERGENCY LIGHT DEFECTIVE A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23834NK 49847 NUMEROUS EMERGENCY LIGHTS OUT IN CABIN. FOUND DEFECTIVE GROUND TERMINAL AT EMERGENCY LIGHT ASSY. REPAIRED TERMINAL LUG. 2L72 4F4 FRTA6WE E2EA 20040427000252004042700025NM 2004 4 27 USA2004F00003 120040217A524160B1002624 CABLE BOEING757 7572B7 1384964NM RROYCERB211 RB211* 54555NE R4 DOOR BROKEN A USAAO OTHER O OTHER NRNOT REPORTED 1 EA19621AU 27200 IT WAS REPORTED THAT CATERING HAD ATTEMPTED TO OPEN THE L4 DOOR FROM OUTSIDE. OPENING OF DOOR DID NOT FEEL CORRECT SO ATTEMPTED TO OPEN DOOR WAS ABORTED. WHEN DOOR WAS CHECKED FROM INSIDE, ARMING LEVER WAS FOUND TO BE IN ARMED POSITION. MAINTENANCE FOUND ASSIST BOTTLE DEPLETING INTO DISCHARGE LINE, EVEN THROUGH DOOR DID NOT OPEN FAR ENOUGH TO HAVE TRIGGERED ASSIST MECHANISM. DOOR WAS FOUND TO BE STIFF IN OPERATION. ASSIST BOTTLE WAS REPLACED AND DOOR LUBRICATED. OPERATION OF THE ARM/DISARM WAS CHECKED AND OPERATED NORMALLY. THE DOOR WAS FOLLOWED UP WITH A SUBSEQUENT LUBE. DUE TO ADDITIONAL CONCERNS, FURTHER CHECKS WERE PERFORMED. MAINTENANCE FOUND THE DISARM CABLE BROKEN AND REPLACED IT. 2L72 4F4 FRTA2NM A12EU 20040427000752004042700075EU 2004 4 27 BAQA093833 120040309A62304639205016 ROTOR SHAFT BOLKMS117 BK117A1 5626010EU LYC LTS101LTS101* NE MAST MOMENT INOPERATIVE E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03587MC5318 7086 MAST MOMENT SHAFT INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 03/18/2004 1G72 3U3 U H13EU E5NE 20040505001722004050500172SW 2004 5 5 DYC2004F00000 120040319A5510 EYEBOLT AIRTRCAT602 AT602 0390309SW PWA PT6 PT6A66 52043NE HORIZ STAB FAILED B DYCRO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL079075S 6020548 A TIP RECEIVED ON 4/20/04 THAT AN AIR TRACTOR BEING FERRIED TO CANADA FROM THE SOUTHERN US HAD A HORIZONTAL STAB FAILURE IN FLIGHT RESULTING IN A FORCED LANDING ON MARCH 19, 04. LEFT STABILIZER, STABILIZER PEDESTAL, LT V STRUT, LT TRIM TAB CONTROL RODS, LT ELEVATOR, RT ELEVATOR, AND BOTH STABILIZER TO STRUT BOLTS WERE REPLACED. INDICATIONS AT THIS TIME ARE THAT THE LT STABILIZER EYEBOLT FAILURE LEAD TO THIS DAMAGE AND FORCED LANDING. 1L71 3T4 TNCA19SW E26NE 20040512001402004051200140EU 2004 5 12 102851 120040322A7712 WARNING SYSTEM SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE ERRATIC A UHLAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 GL1735SZ 357 PILOT NOTICED THE TORQUE INDICATION BEING ERATIC ON THE RT ENGINE DURING TAKEOFF ROLLOUT AT ABOUT 70 KTS. PILOT RETARDED THE THROTTLES AND RETURNED TO THE GATE. 2L72 4T4 TRTA52EU E8NE6 20040505000492004050500049EU 2004 5 5 SDR2004020 120040314A3234F96GA0102 CONTROL HANDLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE COCKPIT INTERMITTENT A TRBAO OTHER O OTHER TOTAKEOFF 1 SO21438AT112737355 438 LANDING GEAR WILL NOT RETRACT. UNABLE TO MOVE GEAR SELECTOR HANDLE. REMOVED AND REPLACED GEAR SELECTOR HANDLE. 2H72 4T4 TRTA53EU E20NE 20040512001342004051200134EU 2004 5 12 150131 120040412A1420 CONNECTOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT TAILPIPE DISCONNECTED A UHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL17150CN 150CN 434 DURING CLIMB-OUT THE LH TAILPIPE HOT LIGHT ILLUMINATED ON THE CENTRAL WARNING PANEL. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. A/C TAKEN OUT OF SERVICE 4-12-04 AT 1415 (LT). PIT MX REMOVED MOISTURE CONTAMINATION FROM LT TAILPIPE SENSOR CONNECTION AND RESECURED CONNECTOR. A/C WAS GROUND RAN OPS CHECKS GOOD. A/C RETURNED TO SERVICE 4-12-04 AT 1620(LT). 2L72 4T4 TRTA52EU E8NE6 20040525001172004052500117EU 2004 5 25 BAQA094478 120040511A771454487099111 INDICATOR BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE N1 RPM BURNED OUT E BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03117KY858 7544 LED DISPLAY LIGHTING BURNED OUT. REPLACED WITH SERVICABLE UNIT. 1G72 3U3 UNCH13EU E19EU 20040614002432004061400243GL 2004 6 14 ALG2004F00025 220040520A753223073353 BLEED VALVE BELL 206 206L1 1182107SW ALLSN 250C 250C30P 03013GL ENGINE INOPERATIVE E ALGAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW032611 45417 WHILE TAKING OFF IN HMA HEARD POP AND AIRCRAFT YAWED, SYMPTOMS OF A COMPRESSOR STALL. LANDED STRAIGHT AHEAD AND HAD TOWER CALL OPS. MAINTENANCE REMOVED BLEED VALVE AND INSTALLED SERVICEABLE BLEED VALVE PN 23073353 SN FF44236. ALL WORK IAW 206L1MM. 1G71 3U3 U H2SW E1GL 20040623000312004062300031WP 2004 6 23 GTIA040540 120040501A5320 WEB DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FUSELAGE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 RT CUSP WEB FROM STA 579-617 CORRODED FROM BOTTOM SIDE. CUT OUT 2 EA SECTION CUSP WEB. AT STA 553-579 AND 579-602. FABRICATED 2 EA SECTION CUSP WEB. INSTALLED 2 EA REPAIR WEB SECTIONS. 2L72 4F4 FRTA6WE E2EA 20040623000942004062300094WP 2004 6 23 GTIA040505 120040501A5321 SEAL DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE FLOOR PANEL BROKEN A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23808NK 49504 FLOOR PANEL STA 1003-1079 CORNER BROKEN NO EDGE SEAL. FABRICATED NEW FLOOR PANEL. 2L72 4F4 FRTA6WE E2EA 20040707000332004070700033GL 2004 7 7 DXTA200400324 220040616A7200 ENGINE CESSNA750 750 2076810CE ALLSN AE3007AE3007C GL RIGHT OVERTEMP E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07955QS 7500055 CAE330055 DURING TAKEOFF ROLL, RIGHT ENGINE ITT EXCEEDED LIMITS, ENGINE EICAS EXCEEDED PAGE INDICATES 898 DEGREE CELSIUS FOR 5 SECONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4J4 FRTT00007WITE6CH 20040719000322004071900032WP 2004 7 19 ASMF200407013 120040709A323239567851 ACTUATOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D* NE NLG FAILED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW231003Y1306 48068 AIRCRAFT RETURNED AFTER TAKEOFF , IT WAS NOT POSSIBLE TO RETRACT THE NOSE LANDING GEAR WITH STRONG NOISE IN SUCH AREA. THREE FULL EXTENSION AND RETRACTION CYCLES WERE PERFORMED BUT NOSE LANDING GEAR DID NOT RETRACT. DURING CHECK, FORWARD DOOR WAS DETECTED DOWN, TESTS WERE PERFORMED AND THE ACTUATOR DID NOT SECURE THE DOOR. ACTUATOR WAS REPLACED AND NOSE LANDING GEAR TESTS WERE PERFORMED IAW MM 32-22-01, ALL CORRECT. ADDITIONALLY OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM 05-51-4, ALL CORRECT. 2L72 4F4 F A6WE E2EA 20040628000482004062800048 2004 6 28 SWIA200413438 420040613A3497 WIRE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE STICK SHAKER BROKEN A SWIAO OTHER J WARNING INDICATION NRNOT REPORTED 1 NM07915SW 7615 WIRES PULLED OUT OF CONNECTOR OF FIRST OFFICER'S STICK SHAKER. REPAIRED CONNECTOR PER AWM 20-17-10. OPERATIONAL CHECK GOOD PER AMM 27-35-01. 2L72 4F4 FRTA21EA E15NE 20040629001812004062900181EA 2004 6 29 SWIA200413462 120040615A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07452SW 7716 FS 280 RIGHT FLOORBEAM RBL 9.0 OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-41-21, 51-42-06, AND 51-23-00. 2L72 4F4 FRTA21EA E15NE 20040813002012004081300201NM 2004 8 13 2004UALA00671 120040718A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29561UA 26661 FWD CABIN FLOORBEAM AT BS 324 RBL 62 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW T-CAP. 2L72 4F4 FRTA2NM E17NE 20040816001552004081600155NM 2004 8 16 P5CA0401106 120040624A36109788926 VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE HIGH STAGE FAILED A P5CAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP23508MC 21644 530349 NR 3 ENGINE FIRE WARNING CAME ON DURING CLIMB, A & B LOOPS READ 7 TO 10 UNITS, THAN STABILIZED TO 4 UNITS SCALE WHEN THROTTLE MOVED TO IDLE. FOUND NR 3 ENGINE HIGH-STAGE BLEED VALVE LEAK. REMOVED AND REPLACED NR 3 ENGINE HIGH STAGE BLEED VALVE AS PER MM 36-11-03. NO LEAKS. 2L74 4F4 F A20WE E23EA 20040813000722004081300072NM 2004 8 13 2004UALA00711 120040731A2840 INDICATOR BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUEL SYSTEM MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29782UA 26948 DUAL FUEL INDICATION PROBLEM. THIS PROBLEM IS RELATED TO THE THE ISSUE DESCRIBED IN BOEING MAINTENANCE TIP 777-MT28-11, WHERE TWO OR MORE FAULTING TANK UNITS CAN CAUSE MULTIPLE NUISANCE FUEL SYSTEM FAULT MESSAGES. THE CENTER RH TANK UNIT #2 WAS IDENTIFIED AS ONE OF THE TRULY FAULTING PARTS, SO IT WAS REPLACED. THE SECOND TRUE FAULTING TANK UNIT HAS YET TO BE IDENTIFIED, SINCE IT APPARENTLY IS FAULTING INTERMITTENTLY. BUT WHEN IT IS IDENTIFIED, IT WILL BE REPLACED. THE AIRPLANE IS CURRENTLY NOT GENERATING ANY FAULT MESSAGES. THE FUEL QUANTITY PROCESSING UNIT (FQPU) WAS ALSO REPLACED PRECAUTIONARILY. 2L72 4F4 FRTT0001SE E46NE 20040818001532004081800153NE 2004 8 18 KBM2004F00138 220040608A72619560137250 MAGNETIC SEAL SNIAS 350 AS350B1 8680811EU TMECA ARRIELARRIEL1 60030NE NR 5 LEAKING E KBMAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP19215LA 2143 NR 5 MAG SEAL, LEAKING SEAL. REPLACED WITH RECONDITIONED UNIT. 1G71 3U3 U H9EU E19EU 20040816000992004081600099NM 2004 8 16 2004UALA00589 120040616A5512657378338 SKIN BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT HORIZ STAB LEDENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29391UA39017 24666 FOUND A 3.5 X 1.5 X 0.1875 DEEP DENT ON RIGHT HORIZONTAL STABILIZER LEADING EDGE APPROX 15 FEET FROM THE FUSELAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR. 2L72 4F4 FRTA16WE E2GL 20040908000402004090800040SO 2004 9 8 C2XA04IA111 120040821A3097 WIRE EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL WINDSHIELD FAILED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW2716918 145397 THE CREW REPORTED THAT THE NR 2 WINDSHIELD HEAT FAILED ACCOMPANIED WITH A BURNING SMELL. MAINTENANCE VERIFIED NORMAL OPERATION OF THE WINDSHIELD HEAT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 FRTT00011ATTE6CH 20040819000112004081900011WP 2004 8 19 MWEA040143 120040812A53209936534139 FLOOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE FUSELAGE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31809ME 48071 CENTER LINE FLOOR SUPPORT BETWEEN FRAME STATION 160 AND 200 CORRODED ON TOP AND SIDE. FABRICATED AND INSTALLED NEW SUPPORT. 2L72 4F4 F A6WE E9NE 20040823000712004082300071NM 2004 8 23 AALA20040848 120040811A2780 PSEU BOEING767 767323 1385205NM GE CF6 CF680C2B6 30025NE WING SLAT INOPERATIVE A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21381AN 25450 HNL INFLIGHT T296/11 LEADING EDGE SLAT ASYMMETRY WITH FLAP INDICATION BETWEEN ONE AND UP. RETURNED TO HNL AND LANDED OVERWEIGHT WITHOUT INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED IAW WORK CARD 05 96 11 WITH NO DISCREPANCIES FOUND. REPLACED FSEU AND PSEU. BITE CHECKED IAW AMM 32 09 04 4. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) NOTE: EXTENDED RANGE EVENT REPORT 1491. 2L72 4F4 FRTA1NM E13NE 20040830001602004083000160NM 2004 8 30 QXEA200400621 120040811A5330 SKIN BOMBDRDHC8 DHC8401 1390041NM PWC 150 PW150A EA ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09400QX 4030 SKIN DENTS IN FUSELAGE LT SIDE X 258.500 - X 281.000. REPAIRED IAW EA 6-53-304-D-. 2H72 4T4 TRTA13NM E00062EN 20040819000182004081900018EU 2004 8 19 KBM2004F00173 120040504A771456337078012 INDICATOR SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL NG FLUCTUATES E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19751H 922 3403 NG GAUGE FLUCTUATES BY I 0.5. REMOVED AND REPLACED. 1G71 3U3 U H9EU E4CE 20040917000852004091700085NM 2004 9 17 372PA0072 120040909A5315654583470 STRAP BOEING737 737306 13844BGNM GE CFM56 CFM563B1 13802NE FLOORBEAM CRACKED A PIDAK NONE O OTHER ININSP/MAINT 1 SO05372PA 23546 STRAP ON LOWER SURFACE OF FLOORBEAMS CRACKED AT BS 312 AND BS 344 AT BL 0. REPLACED STRAP IAW SRM 51-10-2. 2L72 4F4 FRTA16NE E2GL 20040930001872004093000187NM 2004 9 30 P5CA0401185 120040905A793141809104 TRANSMITTER BOEING747 74747UF 1384949NM GE CF6 CF680C2* GL NR 1 ENGINE OIL FAILED A P5CAO OTHER N FALSE WARNING CLCLIMB 1 WP23496MC 29257 704879 LOSS OF ENGINE NR 1 OIL PSI INDICATION ON LWR EICAS DURING CLIMB, NO EICAS MSG RECD OIL INDICATION HAD BEEN NORMAL THROUGHOUT TAXI. REPLACED NR 1 OIL PRESSURE TRANSMITTER PER MM 79-32-01. OPS CHECK ON RUN OK. 2L74 4F4 FRT1384945 E23EA 20040917001282004091700128WP 2004 9 17 AALA20040902 120040826A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21576AA 53153 EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F4 F A6WE E9NE 20041015000702004101500070WP 2004 10 15 DHL2004801552 120040926A5753 DOUBLER DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE TE FLAP DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH81349 46033 ITEM REF. NR. 1131: LT IB FLAP L/E UPPER PLATING HAS INTERIM REPAIR, XW 85.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R07, FAA FORM 8110-3 DATED 09-24-2004. REMOVED INTERIM REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED AREA IAW DWG W51-R07. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.040), INNER SPLICE DOUBLER (2024-T3AL 0.050) IAW DWG W51-R07. CLEANED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN SEGMENT INTERIOR, INNER SPLICE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT TO ALL FAYING SURFACES IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT, INNER SPLICE DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1, DWG W51-R07. 2L74 4F4 FRT4A25 E2GL 20041026001922004102600192EU 2004 10 26 ALGA097750 120040925A6510C651A20001101 DISC PACK UROCOPEC120 EC120B 8680987EU TMECA ARRIUSARRIU2F NE TAIL ROTOR CRACKED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03524AL 1263 CRACKED LAMINATE/REPLACED WITH NEW. 1G72 3U3 UNCR0001RD E34NE 20041101001202004110100120NM 2004 11 1 2004UALA00948 120041016A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29569UA 26677 AFT PIT FRAME UPPER FLANGE DENTED AT BS 1500 STR 26L. MAJOR REPAIR ACCOMPLISHED. TYPICAL AFT PIT FRAME DENTS FROM CARGO LOADING. INSTALLED J-ANGLE REPAIR. 2L72 4F4 FRTA2NM E17NE 20041102001262004110200126NM 2004 11 2 UPS04M43417 120041028A3510 OXYGEN MASK DOUG MD11 MD11F 3023600NM PWA 4460 PW4460 NE COCKPIT FAILED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01273UP 48574 CAPTAIN OXYGEN MASK WILL NOT RESET PROPERLY. REMOVED AND REPLACED CREW 02 MASK AND STOWAGE BOX IAW 35-13-01. LEAK TEST GOOD. 2L73 4F4 FRTA22WE E24NE 20041026001142004102600114WP 2004 10 26 AALA20041060 120041019A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217C 52053NE EMERGNECY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW217527A 49919 FORWARD ENTRY COCKPIT OVERHEAD EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY B5-23 FOR FORWARD ENTRY COCKPIT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED. 2L72 4F4 F A6WE E9NE 20041110000252004111000025EU 2004 11 10 DHL2004365005 120041103A3240355511011 CONTROL UNIT AIRBUS300 A300B4203 3930306EU GE CF6 CF650C2 30018NE AUTO-BRAKE INOPERATIVE A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01365DH 149 WHILE NORMAL BRAKES ARE BEING APPLIED, IF ANY AUTOBRAKE MODE IS SELECTED, EXPERIENCE A 3 SEC LOSS OF NORMAL BRAKES. IT IS AS IF THE ANTI SKID SYSTEM IS RELEASING THE BRAKES BUT THE ANTI SKID PANEL SHOWS NORMAL. REPLACED AUTOBRAKE CONTROL UNIT IAW MM 32-42-54. OPS CHECK GOOD AT THIS TIME. 2L72 4F4 FRTA35EU E23EA 20041123001282004112300128CE 2004 11 23 DXTA200400442 120041110A28218975131 FUEL FILTER RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP NR 1 ENGINE LEAKING E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07882QS 258482 P107571 NR 1 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF. INSPECTED BOTH ENGINES FOR EVIDENCE OF FUEL LEAK ETC. CHANGED BOTH FUEL FILTERS. LEAK CHECKED FILTERS, RAN BOTH ENGINES TO POWER SEVERAL TIMES, NO RED LOOK-UP LIGHT. ALL WORK IAW HONEYWELL MM CH 72-00-00. 2L72 4F4 FRTA3EU E6WE 20041026001602004102600160NM 2004 10 26 ANCF200400034 120041012A528059305832 DOOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE MLG INOPERATIVE W ANCFO OTHER J WARNING INDICATION CLCLIMB 1 SO23583AN 53183 AFTER TAKE OFF, THERE WAS INDICATION OF (GEAR DOOR OPEN LIGHT, LT MAIN GEAR UNSECURED) RED LIGHT ON WITH LANDING GEAR HANDLE UP WAS PERFORMED. AFTER ASKING CONTROL TOWER ABOUT ANY ABNORMALITIES, GEAR WAS RECYCLED, IN THIS CONDITION IT SHOWS GEAR DOOR OPEN LIGHT ON, ALL OF GEARS DOWN AND SECURE STOPPING CHECK LIST AT THIS POINT BECAUSE OF DIFFERENCE BETWEEN CONFIGURATION AND CHECK LIST. THE INFLIGHT GEAR DOOR OPEN LIGHT ON L,N,R GEAR LIGHT GREEN, CHECK LIST WAS PERFORMED, PROCEED TO LAND IN THIS CONFIGURATION. IAW AMM32-12-01 PAG 204-207 WAS REPLACED DOOR ASSY IB, IAW AMM 32-30-00 PAG 201-206 ADJUSTMENT/TEST EXTENSION AND RETRACTION AND ALTERNATE EXTENSION WAS PERFORMED, TEST ON GROUND SATISFACTORY. 2L72 4F4 FRT E9NE 20041027001452004102700145NE 2004 10 27 2004UALA00790 220040829A75326774E010000 BLEED VALVE AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE LEFT ENGINE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29810UA 843 V10428 RETURN TO FIELD DUE TO A DUAL ENGINE BLEED PROBLEM. *S/D* ADJUSTED RT BLEED LEAK DETECTION LOOP IN RT PACK BAY THAT WAS CONTACTING A DUCT CLAMP. THE BLEED LEAK WARNING RESULTED IN AUTOMATIC SHUTDOWN OF THE ASSOCIATED BLEED SYSTEM. CONCURRENTLY THE AIRCRAFT EXPERIENCED A MALFUNCTION OF THE NR 1 PRV - RESULTING IN LOSS OF PNEUMATIC SUPPLY FROM THE LT SYSTEM - THUS THE DUAL FAILURE. THE NR 1 PRV WAS REPLACED AND NO FURTHER BLEED DISCREPANCIES HAVE BEEN REPORTED. 2L72 4F4 FRTA28NM E40NE 20041028000242004102800024SO 2004 10 28 C2XA04TY121 120040726A532014525422003 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717928 145007 DURING A SCHEDULED 4C INSPECTION, CORROSION WAS FOUND ON THE FLOORBOARD SUPPORT FROM LAV TO CARGO. MAINT. REMOVED AND REPLACED THE SUPPORT FROM THE LAV TO THE CARGO IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F4 FRTT00011ATTE6CH 20041102001222004110200122NE 2004 11 2 04FDEA02993 220041025A7310 WARNING LIGHT AIRBUS310 A310 EU GE CF6 CF680A3 30025NE FUEL FILTER ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25410FE 356 FUEL FILTER CLOG LIGHT ON T/O AT 60KTS. REJECTED T/O. ALL INDICATIONS NORMAL ON 60 PERCENT RUNUP FOR ENG ANTI-ICE. ECAM WARNING STOPPED STOPPED AS SOON AS POWER WAS REDUCED. I THINK IT WAS NR 1 ENG, BUT AM NO T POSITIVE. ENT BY: 001941 RPT BY: 119121 FACT 24OCT04 15:12 RNO R GRD RUN TO 65 PERCENT WITH NO PROBLEM. REMOVED AND REPLACED 1 ENG. FUEL FILTER ASSY FOR T/S. LEAK AND OPS CKS, OK ON GRD RUN. MM 73-12-03. ENT BY: 001941 RPT BY: 001941 2L72 4F4 FRTA35EU E13NE 20041122001882004112200188NM 2004 11 22 USAA040728 120040917A5320BAC1509100505 FLOOR SUPPORT BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE SEPARATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19432US41131 24554 PIT - Q4, FLOOR SUPPORT, .1250 INCH GAP, SEPARATION. FLOOR SUPPORT SEPARATED FROM WEB, STA 986.5 BETWEEN STR 17L AND STR 21L. FABRICATED PART TO MATCH ORIGINAL IAW SRM 51-10-02. 2L72 4F4 FRTA16WE E21EU 20041124001112004112400111NM 2004 11 24 GAIA04146 120040910A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D7B 52053NE FUSELAGE DAMAGED A GAIAO OTHER O OTHER NRNOT REPORTED 1 SW07180AX 20041 DURING C-CHECK INSPECTION FOUND SKIN FASTENERS LOOSE AND PULLED THROUGH SKIN AT STA 1342. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 54-30-3, FIG 7. 2L73 4F4 F A3WE E2EA 20041124001362004112400136NM 2004 11 24 BJNA041003 120041010A33501619 BULB BOEING737 737282 13844ATNM PWA JT8 JT8D17A 52049NE EMERGENCY LIGHT BURNED OUT A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11344TM 23044 LT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB AND CLEANED SOCKET IAW AMM 33-51-101. 2L72 4F4 FRTA16WE E2EA 20041129001252004112900125EU 2004 11 29 KBM2004F00233 120041003A6410355A09103601 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR CRACKED E KBMAO OTHER O OTHER NRNOT REPORTED 1 WP19884SH509 2884 BEARING HALF SHELLS CRACKED BEYOND LIMITS. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 20041129000472004112900047EA 2004 11 29 ASOA04812 120041023A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27824AS 7203 DURING C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105. 2L72 4F4 FRTA21EA E15NE 20041129001962004112900196NE 2004 11 29 USA2004F00056 220040531A7261 ENGINE AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RIGHT LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19677UW 0380 THIS FLT WAS A VERIFICATION FLIGHT FOR RT ENGINE OIL LOSS. CREW NOTED THAT THE RT ENGINE WAS AGAIN LOSING OIL. FLIGHT DIVERTED. AFTER THE PREVIOUS FLIGHT (FL 98 ON 5/30/2004), EIGHT QUARTS OF OIL HAD BEEN ADDED TO THE ENGINE. MAINTENANCE PERFORMED TSM TASK 79-00-00-810-813 AND COMPLETED THE NR 3 BEARING COMPARTMENT BREATHER CHECK. NO DISCREPANCIES WERE FOUND. THE ENGINE WAS OPERATED FOR APPROXIMATELY FORTY-FIVE MINUTES WITH NO OIL LOSS. THE AIRCRAFT WAS RELEASED FOR THIS FLIGHT. FURTHER MAINTENANCE ACTION PENDING. 2L72 4F4 FRTA46NM 20041201000552004120100055NM 2004 12 1 2004UALA01131 120041116A3350 BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY LIGHT INOPERATIVE A UALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP29661UA 27158 BUSINESS CLASS EMERGENCY LIGHTS ON AFTER TAXI OUT. REPLACED EMERG LT POWER SUPPLY CHARGER ASSY, POWER SUPPLY BATTERY AND EEL BATTERY POWER PACK AT SEAT 1A. ALSO REPLACED EEL BATTERY POWER PACK AT SEAT 8A. 2L72 4F4 FRTA1NM E24NE 20041201001552004120100155NE 2004 12 1 127712 220040729A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT MALFUNCTIONED A UHLABA EMER. DESCENT UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 GL17360SZ 340A006 478 FLIGHT 7889 IAD-TYS. DURING CLIMBOUT OF IAD CREW REPORTED LOSS OF RT ENGINE POWER. CREW DECLARED AN EMERGENCY AND RETURNED TO IAD. 2L72 4T4 TRTA52EU E8NE6 20041207000762004120700076NM 2004 12 7 USAA040762 120041020A5315 FLOORBEAM BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19613AU39317 27144 CLT, C-4, FLOORBEAM, 2 INCHES BY 1 INCH, LEVEL 1 CORROSION, STA 324, RBL58, TO RBL60. ACCOMPLISHED TEE CAP REPAIR IAW EA 95913. 2L72 4F4 FRTA2NM E12EU 20041129002012004112900201EU 2004 11 29 DAT2004F00004 120040901A1430B3339 BOLT STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA HARTZLHCB5M HCB5MP3 GL PROPELLER CRACKED E DATAO OTHER O OTHER NRNOT REPORTED 1 GL13937MA457 SH3040 PS84296 EVA2141 IAW SDR REPLACEMENT OF POWER SECTION AND PROPELLER FOR VIABRATION, ON 09/01/04 (7) OF THE (8) PROP ATTACHMENT BOLTS, PN B3339 WERE FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WITH NEW ONES PURCHASED FROM VENDOR. AD86-06-02 WAS COMPLIED WITH IAW MFG SERVICE INSTRUCTIONS 140A AND IS NEXT DUE AT 20201.4 TAT AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T4 T A41EU E4EA 6 CP44GL 20041210000462004121000046NM 2004 12 10 ASAA0410484 120041105A532065565551 WEB BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE DOOR FRAME CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02746AS 23123 PAE - CORROSION AT AFT CARGO DOOR CUT-OUT FWD FRAME CLOSEOUT PANEL FASTENER HOLES. REPLACED AFT CARGO DOOR CLOSE-OUT WEB. 2L72 4F4 FRTA16WE E2EA 20041215000062004121500006NM 2004 12 15 COOSDR040031 120040823A5315 FLOORBEAM BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED B EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23994AJ 20942 MAIN CARGO CABIN, BODY STA 1110, UPPER CAP CORRODED IN SEVERAL PLACES, WL 208.1. 2L73 4F4 FRTA3WE E2EA 20041220001842004122000184SO 2004 12 20 O2G2004F00010 120041121A56101159SCB310214 WINDSHIELD GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU COCKPIT FAILED E O2GAB EMER. DESCENT O OTHER CRCRUISE 1 NE03590DA8511 5709 445 RT WINDSHIELD OUTER PANE FAILED, DURING FLIGHT. REMOVED AND REPLACED WINDSHIELD. (NE03200504208) 2L72 4F4 F A12EA E2EU 20041221001382004122100138WP 2004 12 21 GTIA040815 120041019A2150 A/C PACK DOUG DC9 DC983 3022083WP PWA JT8 JT8D1 52044NE RIGHT MALFUNCTIONED A GTIAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23836NK 53045 CABIN FILLED WITH SMOKE WHEN APU AIR WAS TURNED ON. FOUND RT PACK, DID AN AUTO SHUTDOWN. WHEN RT PACK COOLED DOWN, RAN LT AND RT PACK FOR 90 MINUTES. NO SMOKE AT THIS TIME. CHANGED LT AND RT COALESCER SOCKS FOR COMPANY CONV. WORK DOWN IAW MM 21-20-02. OPS AND LEAK CHECK GOOD AT THIS TIME. 2L72 4F4 FRTA6WE E2EA 20041223000122004122300012WP 2004 12 23 DJFA2004038 220041201A7321 CONNECTOR RAYTHNDH125 HAWKER800XP 7150012CE GARRTTTFE731TFE7315BR WP ENGINE COMPUTER DIRTY E DJFAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA23896CW 258516 P107575 CREW ABORTED TAKEOFF, DUE TO THE NR 1 ENGINE COMPUTER ANNUNCIATOR ILLUMINATING CONTINUOUSLY. MAINTENANCE DOWNLOADED THE NR 1 ENGINE COMPUTER AND FOUND A FAULT CODE FOR THE N2 MONOPOLE BEING SHORTED. THE CONNECTOR AND MONOPOLE WERE CLEANED AND FAULT CODES WERE CLEARED. OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA3EU E6WE 20050104000142005010400014EU 2005 1 4 ASOA04893 120041110A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE CABIN DISCHARGED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27533AS225114334 460 DURING A GROUND INSPECTION, THE FORWARD RT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT 43WL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20050106002082005010600208WP 2005 1 6 ASAA0480486 120040902A2560B19867103 LANYARD DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE TAIL SLIDE DISCONNECTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02956AS 53079 PRE-FLIGHT CHECK, AFT (TAIL) DOOR EMERGENCY SLIDE RELEASE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. 2L72 4F4 FRTA6WE E9NE 20050110001322005011000132NM 2005 1 10 USAA040970 120041118A574365C365452 FITTING BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU RT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19435US41422 24557 PIT - Q1 - FITTING, .25 INC CRACK, RT MLG SUPPORT FITTING, NR 2 HOLE; MODIFIED PART INSTALLED, REPLACED IAW EO 5702V054. 2L72 4F4 FRTA16WE E21EU 20050103001802005010300180NM 2005 1 3 USAA040949 120041019A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19516AU52364 23702 PIT - Q5 - SUPPORT ANGLE, 1.2500 INCH BY .5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, FLOOR SUPPORT, STA 859. BURNISHED, TREATED AND PRIMED IAW TYP REP 53-10-06B. 2L72 4F4 FRTA16WE E21EU 20050119000212005011900021NM 2005 1 19 2005UALA00010 120041230A5330 SKIN BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FUSELAGE PUNCTURED A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 AIRCRAFT DAMAGE AT DOOR 4 LEFT AT APPROX STA 1582 BELOW DOOR SILL. PUNCTURE THROUGH SKIN. UNDETERMINED CAUSE OF DAMAGE TO SKIN. REPAIRED PER SRM. 2L72 4F4 FRTA1NM E24NE 20050110000732005011000073EU 2005 1 10 USAA041012 120041110A5320D5347112420100 SHEAR WEB AIRBUSA319 A319112 3930323EU CFMINTCFM565CFM565B6 13802NE FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19711UW16698 1033 BFM - S1 - SHEAR WEB, 7 INCHES X 3 INCHES X .03 INCH AREA; CORROSION; LEVEL 2; TASK NR JA-260-53500; BTW BL- Y1162 AND Y1262. INSTALLED NEW SHEAR WEB IAW SRM. 2L72 4F4 FRTA28NM E37NE 20050126001442005012600144NE 2005 1 26 DJFA2004045 220041230A7261JT15D5 ENGINE BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE LEFT UNDERSERVICED E DJFAA UNSCHED LANDING W INADEQUATE Q C CLCLIMB 1 EA23775TA3921 3921 RK276 PCEJA0322 AFTER T/O, THE LT ENGINE OIL PRESS GAUGE HAD DROPPED TO ZERO IND. WHEN POWER WAS REDUCED THE LT ENGINE OIL TEMP HAD INCREASED. THE LT ENGINE WAS SHUT DOWN AND AN EMERG DECLARED. NO YELLOW OR RED ANNUNCIATORS HAD ILLUMINATED. A/C HAD DIVERTED TO KPFN AND LANDED SAFELY. MX INSPECTED THE WIRING FROM THE OIL PRESSURE TRANSDUCER AND FOUND NO DEFECTS. THE OIL PRESSURE GAUGES WERE SWAPPED FROM LT TO RT AND WERE FOUND TO BE OPS. GAUGES WERE SWAPPED BACK TO THEIR ORIGINAL POSITIONS. THE LT ENGINE OIL WAS FOUND TO BE OVER TWO QUARTS LOW. OIL WAS REPLENISHED TO MAX COLD LEVEL. ENGINE WAS RAN AND OIL PRESSURE HAD INCREASED AS REQUIRED. NO FURTHER DEFECTS WERE NOTED. THE A/C WAS RETURNED TO SERVICE. 2H72 4F4 FRTA16SW E25EA 20050127000592005012700059WP 2005 1 27 GTIA040850 120041104A2560 RECEPTACLE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217C 52053NE ESCAPE LINE CORRODED A GTIAO OTHER O OTHER NRNOT REPORTED 1 GL23810NK 48015 SAS NR B00182-05N-00118; OVERWING ESCAPE LINES REEL ASSY LT FWD AND AFT AND RT FWD AND AFT ATTACH HARDWARE SHEARED AND RECEPTACLES CORRODED. REMOVED AND REPLACED HARDWARE AND RIVNUTS ON LT AND RT OVERWING ESCAPE LINE REEL ASSY. 2L72 4F4 F A6WE E9NE 20050307003172005030700317NM 2005 3 7 ASAA0470040S 120041105A5311146A13003 FRAME BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02625AS 30792 PAE: DURING MAINTENANCE CHECK, FOUND CORROSION ON FRAME CAP AT BS 787. REPAIRED IAW SRM. (K) 2L72 4F4 FRTA16WE E00055EN 20050307003182005030700318NM 2005 3 7 ASAA0470030 120041026A5320 SUPPORT BOEING737 737790 13844CNNM GE CFM56 CFM567B24 NE FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 SW15626AS 30793 PAE: DURING C-CHECK, FOUND CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 500A TO 500D. REPAIRED IAW SRM.(K) 2L72 4F4 FRTA16WE E00055EN 20050308001572005030800157NM 2005 3 8 GAIA04175OP 120041204A3260H1010153 DOWNLOCK SWITCH BOEING727 7272J0 138407ENM PWA JT8 JT8D15 52051NE NLG FAILED A GAIAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW07281KH 21105 DURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. DECLARED EMERGENCY. LANDING AND TAXI IN UNEVENTFUL. TROUBLESHOOT NOSE GEAR INDICATION FOUND BAD DOWNLOCK SWITCH AND (DOWN-LOCK) SWITCH CONNECTOR. REMOVED AND REMOVED NLG DOWN SWITCH AND CONNECTOR IAW MM 32-61-71 AND WIRING MANUAL 20-61-19. ALL GROUND OPS CHECK GOOD, DOWN AND LOCK CHECK C/W RETRACT NLG UP AND DOWN SEVERAL TIMES, CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 FRTA3WE E2EA 20050330001022005033000102NM 2005 3 30 S2YA04038 120041014A3246AHA22262 WHEEL DORNERDO32 DO328300 NM PWA 306 PW306B NE NR 3 SEPARATED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13352SK6521 3111 AFTER FLIGHT, THE CREW DISCOVERED A DAMAGE TO THE NR 3 TIRE AND THE RT HYDRAULIC DOOR. MX INSPECTED THE ACAND FOUND NO OTHER DAMAGE. INSPECTION OF THE TIRE REVILED EVEN THOUGH IT WAS STILL INFLATED, PART OF THE RECAPPED TREAD HAD LET GO AND DAMAGED THE DOOR. MX REPLACED DOOR AND WHEEL ASSY. THE AC WAS RETURNED TO SERVICE WITH NO FURTHER DEFECTS. (K) 2H72 4T4 FRTA55NM E35NE 20050328000112005032800011NM 2005 3 28 72300084 120041028A5711 SPAR BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE WING CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 3 INCH AREA OF CORROSION ON SPAR CHORD VERT FLANGE. 2L73 4F4 FRTA3WE E2EA 20051017000012005101700001WP 2005 10 17 IXXA0500098S 120041211A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE BS 640 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11602AL943122991 45991 DURING A ROUTINE C-CHECK INSPECTION, FOUND FLOORBEAMS IN FUSELAGE CARGO COMPARTMENT WITH CORROSION DAMAGE AT STA FS 640.000 RBL 38. REPAIR ACCOMPLISHED BY REMOVING CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA, FABRICATED ANGLE REPAIR AND FILLER. CLEANED, TREATED AND PRIMED AREA, ANGLE REPAIR & FILLER. APPLIED PRC SEALANT AND FAYING SURFACES IAW SRM 51-1-8B, 51-2-1 FIG SHEET 7 AND 12 TR 51-13D, 53-2-0, 51-1-11, AND 51-1-20D. 2L74 4F4 FRT4A25 E2GL 20060201001102006020100110WP 2006 2 1 IXXA060116S 120040614A5330 SKIN PANEL DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C 13802NE ZONE 100 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11605AL935782554 46106 DURING ROUTINE C-CHECK FOUND AIR CONDITIONING ACCESSORY COMPARTMENT, INTERIOR STATION 38 BETWEEN LONGERON 32 RT AND LONGERON 33 RT CORRODED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN SECTION, LONGERON 32 RT AND 33 RT. FABRICATED NEW SKIN SECTION AND RECEIVED NEW LONGERONS. LOCATED ALL REPAIR PARTS, DRILLED, DEBURRED, TREATED, PRIMED, INSTALLED ALL REPAIR PARTS, AND NEW FASTENERS WET WITH SEALANT FROM STATION 32 TO 70 LONGERON 31 RT TO 35 RT. IAW DWG NR W20-R01 REV:IR DATED 7/1/04. 2L74 4F4 FRT4A25 E2GL 20060201000832006020100083WP 2006 2 1 IXXA060100S 120041002A5712 RIB DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C 13802NE ZONE 600 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11825BX858232773 45978 DURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS735. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS735. IAW SRM 57-2-0,57-1-20D 51-1-4, 51-1-5, AND 51-1-8. 2L74 4F4 FRT4A25 E2GL 20040115000772004011500077NM 2004 1 15 04FDEA00031 120040105A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25236FE 21330 DENT ON FUSELAGE SKINS AT 1090 BELOW STR 20L. DENT ON FUSELAGE SKIN BS 1090 BELOW STR 20 LT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REPAIRED DAMAGED AREA PER SRM 53-30-3. 2L73 4F RTA3WE 20040524000842004052400084NM 2004 5 24 P5CA0401087 120040430A528065B1166 DOOR BOEING747 747282B 1384860NM MLG CRACKED A P5CAO OTHER O OTHER LDLANDING 1 WP23921FT 21575 LEFT WING GEAR INBOARD SHOCK STRUT DOOR LEADING EDGE HAS CRACK. REPLACED DOOR. 2L74 4F A20WE 20040629000582004062900058NM 2004 6 29 04FDEA01665 120040610A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25610FE 48603 RIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.490, REMAINING THICKNESS=0.488, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040319001322004031900132 2004 3 19 SWAA040704 420040305A2565 INDICATOR BOEING737 7372H4 138448CNM R2 DOOR SLIDE OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29096SW 23055 R2 DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITION SLIDE ASSY PER MM. 2L72 4F A16WE 20040618000732004061800073WP 2004 6 18 DHL2004803519 120040401A5730 DOUBLER DOUG DC8 DC873 302199CWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH79338 46123 LEFT WING OUTBOARD STUB WING DOUBLER CRACKED 0.500 AT XFS 529.000 (LWR PART). REMOVED CRACKED DOUBLERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW DOUBLERS: INTERNAL (7075-T6AL 0.063), EXTERNAL (7075-T6AL 0.080) IAW SRM 57-2-1A PG 3. CLEANED, TREATED AND PRIMED AREA AND DOUBLERS IAW SRM 51-1-8B. INSTALLED DOUBLERS IAW SRM 57-2-1A PG 3, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. 2L74 4F RT4A25 20040407000952004040700095EU 2004 4 7 AALA20040406 120040327A3244 TIRE FOKKERF28 F28MK0100 4990807EU MLG SEPARATED A AALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW211463A 11483 ATL - INFLIGHT T1972 NUMBER 3 TIRE RECAP SEPARATED ON TAKEOFF CAUSING DAMAGE TO RIGHT HAND MAIN GEAR DOWNLOCK ACTUATOR, RIGHT HAND FLAPWELL, RIGHT HAND MID FLAP AND RIGHT HAND FLAP DRIVESHAFT, AND NUMBER 2 ENGINE INGESTED SOME FOREIGN OBJECT DAMAGE AND SUSTAINED DAMAGE TO FAN BLADES AND THE HONEYCOMB AREA AROUND THE BLADES. REPLACED RIGHT HAND ENGINE. INSPECTED RIGHT HAND LOWER WING, RIGHT HAND AFT FUSELAGE, RIGHT HAND ENGINE AND RIGHT HAND TAIL AREA FOR DAMAGE. REPAIRED DAMAGE PER MAINTENANCE MANUAL PROCEDURES ON TULSA BILL OF WORK DATED 03/30/04. 2L72 4F RT 20040209001802004020900180CE 2004 2 9 DXTA200400231 120040126A32304614 BYPASS VALVE CESSNA500 560CESSNA 2076750CE HYD SYSTEM FAULTY E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07305QS4693 5600261 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, HYDRAULIC PRESSURE LIGHT DID NOT ILLUMINATE. GEAR INDICATION WAS 3 GREEN AND NO RED. REMOVED AND REPLACED SUSPECTED FAULTY LANDING GEAR CENTER BYPASS VALVE AND PRESSURE RELIEF VALVE. PERFORMED LANDING GEAR RETRACTION AND EXTENSION, SYSTEM CHECKED GOOD. ALL WORK PERFORMED IAW CESSNA560 MM CHAPTER 29-11-06 AND 32-30-00. 2L72 4F RTA22CE 20040406000652004040600065WP 2004 4 6 04FDEA00676 120040316A1430 BOLT DOUG DC10 DC1010 3022110WP TE FLAP INCORRECT A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO2540061 46973 I/B FLAP O/B FITTING BOLT HAS THE INCORRECT BOLT IN THIS POSITION. *S/D* MX INSTALLED CORRECT BOLT IN A FOREMENTIONED POSITION. 2L73 4F A22WE 20040414001692004041400169NM 2004 4 14 SWAA040965 120040401A3211654610918 CLEVIS BOEING737 7373H4 1384600NM RT MLG CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND RT MLG BEAM ARM FWD CLEVIS LUG CRACKED. REMOVED AND REPLACED RT MLG CLEVIS PER MM. 2L72 4F RTA16WE 20040414000742004041400074NM 2004 4 14 04FDEA00901 120040412A5320 FLOOR SUPPORT DOUG MD11 MD11 3023602NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25601FE 48401 AFT CARGO COMPARTMENT, LEFT MOST O/B FLOOR SUPPORT UPPER & LOWER SURFACE FOUND WITH SEVERAL PLACES OF CORROSION. FLOOR SUPPORTS REMOVED AND REPLACED AS PER SRM 53-00-01 FIG 9 AND DWG AGA3857. 2L73 4F RTA22WE 20040601000402004060100040NM 2004 6 1 04FDEA01485 120040526A5753 HINGE DOUG MD11 MD11 3023602NM T/E FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25594FE 48552 LEFT WING - OUTBOARD FLAP AFT OUTBOARD HINGE, FOUND OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PG. 2-4. ORIG. DIAM.: 1.062, FINAL DIAM.: 1.093, REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP - OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR. 2L73 4F RTA22WE 20041122001432004112200143NM 2004 11 22 04FDEA02000 120040706A5347A6A7082505 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 MAIN DECK, SEAT TRACK CROWN AT STA 6-80, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 6-40 TO STA 7-0, LBL 47.5 CUT AND REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS INSTALLED AS PER SRM 51-31-01 VOLUME II AND 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20040610002072004061000207NM 2004 6 10 DL73S040451 120040520A25305374AD COFFEEMAKER BOEING737 737232 1384475NM AFT GALLEY MALFUNCTIONED A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO27308DL 23080 DURING FLIGHT AFT CABIN ATTENDANTS NOTICE ELECTRICAL SMELL IN THE AFT GALLEY. SHORTLY AFTER SMELL STARTED SMOKE DETECTOR IN AFT LAV STARTED TO SOUND. THE C/B FOR THE AFT GALLEY COFFEEMAKER POPPED AND THE SMELL WENT AWAY. THE AFT LAV SMOKE DETECTOR CONTINUED TO SOUND AND THE F/A DISCONNECTED THE BATTERY. THE FLIGHT THEN DIVERTED TO BNA IT WAS SCHEDULED LIT-ATL. MAINTENANCE FOUND THE AFT GALLEY COFFEEMAKER AT FAULT AND REPLACED SAME. 2L72 4F RTA16WE